c5 c10 c12 c14 c15 c16 c17 c18 c20 c25 c35 c40 c90 c100 c110 c120 c130 c140 c150 c152 c160 c170 c180 c190 c192 c200 c210 c220 c230 c240 c250 c260 c270 c280 c290 c300 c310a c310b c310c c310d c314a c314b c314c c314d c320a c320b c320c c324a c324b c324c c330 c332 c340 c350 c360 c370 c380 c390 c400 c410 c420 c430 c440 c450 c460 c490 c510a c510b c510c c510d c510e c510f c602 c604 c606 c608 c610 c612 c614 c616 c620 c640 c652 c654 c660 eof 1998010800191 19980108 00191 WP 1998 1 8 VJ9800001 1 19980101 A 3350 6030431 POWER PACK DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 937VV 45774 EMERGENCY CEILING LIGHTS AT SEAT ROWS 14, 15 AND 16 ARE OUT. REPLACED BATTERY POWER SUPPLY PACK; OPS CHECKS NORMAL IAW MM 33-53-0. 2 L 7 2 4F A6WE 1998010800205 19980108 00205 1998 1 8 9724561234 4 19980101 A 3414 2594466906 AIRSPEED IND DOUG DC10 DC1030 3023501 WP RT COCKPIT INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 234NW 36932 5626 46912 DURING CLIMB, THE FIRST OFFICER'S AIRPSEED INDICATOR WENT TO 0. AIRCRAFT RETURNED TO SEA AND LANDED WITHOUT INCIDENT. R EPLACED THE FIRST OFFICER'S AIRSPEED INDICATOR. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998010800220 19980108 00220 EU 1998 1 8 WWMA9800001 1 19980101 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A WWMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 15 254AE 1154 340B254 CARGO SMOKE LIGHT ILLUMINATED ON TAKEOFF, ABORTED TAKEOFF. MAINTENANCE FOUND BOTH CARGO SMOKE DETECTORS DIRTY AND THE A FT DETECTOR INTERMITTENTLY WOULD NOT TEST. REPLACED BOTH CARGO SMOKE DETECTORS. 2 L 7 2 4T RT A52EU 1998010800229 19980108 00229 NM 1998 1 8 98FDEA00001 1 19980101 A 2610 65249203 CONTROL UNIT BOEING 727 7272S2F 1384O81 NM E/E COMP MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 210FE 22932 98-0001 FIRE WARNING LIGHTS AND BELL ON FOR 1 SECOND AT CRUISE, (ON FORWARD INSTRUMENT PANEL) NO FURTHER INDICATIONS. E NGINE INSTRUMENTS ALL NORMAL. FOUND PIN PUSHED BACK IN FIRE DETECTOR CONTROL UNIT REMOVED AND REPLACED UNIT OPERATIONAL CHECKED GOOD. 2 L 7 3 4F A3WE 1998010800421 19980108 00421 NM 1998 1 8 MALA975847 1 19980103 A 3350 1013073 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 830MA 337 DURING INSPECTION THE EMERGENCY FLOOR TRACK LIGHT BULB INOP. MAINTENANCE RELAMPED, OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998010800422 19980108 00422 NM 1998 1 8 MALA975848 1 19980102 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 827MA 331 DURING INSPECTION EMERGENCY FLOOR TRACK LIGHT INOP BY MAIN EXIT. MAINTENANCE RELAMPED EMERGENCY FLOOR TRACK LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998010800423 19980108 00423 NM 1998 1 8 MALA975849 1 19980101 A 3320 1011801 SOCKET DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 827MA 331 DURING PREFLIGHT, NOTED SMOKE FROM PASSENGER DOOR STEP LIGHTING. MAINTENANCE FOUND TOP AIRSTAIR LIGHT SOCKET LOOSE. RE PLACED AIRSTAIR LIGHT ASSEMBLY, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998010800424 19980108 00424 NM 1998 1 8 MALA975850 1 19980101 A 3230 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM RT MLG MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 866MA 366 DURING LANDING GEAR RETRACTION OUT OF DTW, THE RIGHT MAIN LANDING GEAR FAILED TO RETRACT. THE RED UNSAFE LIGHT WAS ILLU MINATED ALONG WITH THE GEAR HANDLE IN TRANSIT LIGHT. ONCE LEVELED OFF THE RIGHT MAIN LANDING GEAR DID RETRACT. AIRCRAF T RETURNED TO DTW WITH GEAR EXTENDING NORMALLY. MAINTENANCE CYCLED GEAR SEVERAL TIMES EVERYTHING CHECKS NORMAL, SERVICE D AND BLEED HYDRAULIC SYSTEM. CYCLED GEAR WITH NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 1998010800425 19980108 00425 EU 1998 1 8 MALA975851 1 19980104 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 115XJ 340A115 DURING INSPECTION, TWO OVERHEAD EMERGENCY LIGHTS INOP AT ROW 8C AND 3A. MAINTENANCE RELAMPED OVERHEAD LIGHTS, ALL CHECK S GOOD. 2 L 7 2 4T RT A52EU 1998010800426 19980108 00426 NM 1998 1 8 MALA975852 1 19980105 A 3350 1013073 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 866MA 366 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE REPLACED EMERGENCY FLOOR TRACK LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998010800427 19980108 00427 EU 1998 1 8 MALA975853 1 19980102 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 109XJ 340A109 DURING INSPECTION EMERGENCY LIGHT AT 6A INOP. MAINTENANCE REPLACED LAMP, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998010800428 19980108 00428 EU 1998 1 8 MALA975854 1 19980104 A 3350 7239410802 LIGHT SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 112XJ 340A112 DURING INSPECTION, FLOOR TRACK LIGHT AT 4CD INOP. MAINTENANCE REPLACED FLOOR TRACK LIGHT AT 4CD, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998010800429 19980108 00429 EU 1998 1 8 MALA975855 1 19980104 A 3350 P4010021 BATTERY BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 504XJ E2311 DURING INSPECTION, FORWARD EMERGENCY FLASHLIGHT SEAL BROKEN. MAINTENANCE REPLACED BATTERY AND REINSTALLED SECURITY SEAL , OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998010800434 19980108 00434 NM 1998 1 8 RAAA98B2001 1 19980102 A 5314 KEEL BEAM WEB BOEING 727 72722C 138400F NM BS 940 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED 2B CHECK, FOUND KEEL BEAM WEB CRACKED APPROX 1.2 INCH AT BS 940 RBL 7 WL 148. REPAIRED PER SRM 51-40-2 FIG 1. M-54 NR 17. 2 L 7 3 4F A3WE 1998010800435 19980108 00435 NM 1998 1 8 RAAA98B2002 1 19980105 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 2 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998010800436 19980108 00436 SO 1998 1 8 RAAA98E9001 1 19980103 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EGRESS FLOOR PROXIMITY LIGHT AT PAX ROW 3 FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998010800437 19980108 00437 SO 1998 1 8 RAAA98E9002 1 19980105 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD EMERGENCY EXIT AND FWD CABIN PULL DOWN EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 4 4T 4A22 1998010800443 19980108 00443 1998 1 8 9800011234 4 19980101 A 3414 2594466906 AIRSPEED IND DOUG DC10 DC1030 3023501 WP RT FLIGHT DECK INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 234NW 36932 5626 46912 DURING CLIMB, THE FIRST OFFICER'S AIRSPEED INDICATOR WENT TO ZERO. AIRCRAFT RETURNED TO SEA AND LANDED WITHOUT INCIDENT . REPLACED THE FIRST OFFICER'S AIRSPEED INDICATOR, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A22WE 1998010800444 19980108 00444 NE 1998 1 8 9800026740 2 19980101 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7Q 52054 NE NR 1 FLAMEOUT A NWAA O OTHER X ENGINE FLAMEOUT LD LANDING 1 GL 01 640US 23888 702056 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE N1 INDICATION SPIKED AND THE ENGINE SHUT DOWN. MAINTENA NCE INSPECTED INLET AND EXHAUST WITH NO DEFECTS NOTED. THE NR 1 N1 INDICATOR WAS REPLACED AND AN ENGINE RUN WAS PERFORM ED INCLUDING REVERSE OPERATION. ALL INDICATIONS WERE NORMAL AND THE AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUSPECTS SNOW CONDITIONS MAY HAVE CAUSED THE SHUTDOWN IN REVERSE. 2 L 7 4 4F 4 F A20WE E3NE 1998010800445 19980108 00445 WP 1998 1 8 9800039948 1 19980101 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE CHECK, FOUND FLOOR PROXIMITY EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 5 THRU 7. MAINTENANCE REPLACED BATTERY PACK POWER SUPPLY AT RIGHT FORWARD OVERWING EXIT AREA, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998010800446 19980108 00446 WP 1998 1 8 9800049948 1 19980101 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE CHECK, FOUND EMERGENCY EXIT SIGN LIGHTS AT BOTH OVERWING EXITS INOPERATIVE. MAINTENANCE REPLACED BATTERY PA CK AT RIGHT FORWARD OVERWING EMERGENCY EXIT, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998010800447 19980108 00447 WP 1998 1 8 9800059150 1 19980102 A 3260 SWITCH DOUG DC9 DC914 3022034 WP LT MLG INOPERATIVE A NWAA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 01 8908E 45749 DURING DESCENT, THE LEFT MAIN LANDING GEAR DOWN AND LOCKED GREEN INDICATOR LIGHT DID NOT ILLUMINATE. FLIGHT CREW PERFOR MED COM PROCEDURES, VERIFIED LANDING GEAR DOWN AND LOCKED BY USE OF ON-BOARD PERISOPE, AND LANDED WITHOUT INCIDENT. MAI NTENANCE REPLACED THE LEFT LANDING GEAR EXTEND SWITCH, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998010800448 19980108 00448 WP 1998 1 8 9800069877 1 19980104 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST CR CRUISE 1 GL 01 786NC 48148 EMERGENCY EXIT LIGHTS AT SEAT ROWS 9 THRU 13 FLICKERED ON AND OFF IN FLIGHT. MAINTENANCE CHECKED ASSOCIATED WIRING AND REPLACED THE POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998010800449 19980108 00449 WP 1998 1 8 9800079877 1 19980103 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST CR CRUISE 1 GL 01 786NC 48148 DURING FLIGHT AND WHILE ON THE GROUND, EMERGENCY EXIT LIGHTS AT SEAT ROWS 9 THRU 13 FLICKERED ON AND OFF AND REMAINED IL LUMINATED CONTINUOUSLY WHEN FLIGHT IS SMOOTH. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998010800450 19980108 00450 NM 1998 1 8 9800086622 1 19980103 A 2910 B-NUT BOEING 747 747251B 1384892 NM NR 1 HYD SYST LOOSE A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 622US 21704 DURING APPROACH, THE NR 1 HYDRAULIC LOW QUANTITY LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS TOWED TO T HE GATE. REPLACED THE HYDRAULIC TRANSMITTER AND HYDRAULIC UNION ON NR 4 HYDRAULIC SYSTEM HEAT EXCHANGER PRESSURE LINE A ND SECURED B-NUT ON NR 1 ENGINE DRIVEN PUMP HYDRAULIC PRESSURE LINE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998010800452 19980108 00452 EA 1998 1 8 COMA9860001 1 19980102 A 3411 601R34110021 STATIC DRAIN CNDAIR CL600 CL6002B19 EA E/E COMPT LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 915CA 7013 EFIS COMP MON, ALT AND IAS CAUTION. REPLACED LEAKING STATIC SYSTEM DRAIN. 2 L 7 2 4F RT A21EA 1998010800453 19980108 00453 EA 1998 1 8 COMA9860002 1 19980103 A 3230 16400105 DRAG BRACE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 947CA 9597 5353 7077 NLG DISAGREE MESSAGE ON EICAS. REPLACED THE NLG DRAG BRACE ASSY. 2 L 7 2 4F RT A21EA 1998010800454 19980108 00454 EA 1998 1 8 COMA9860003 1 19980101 A 3230 601R751461 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 947CA 7077 NLG WARNING MESSAGE ON EICAS. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 1998010800477 19980108 00477 NM 1998 1 8 QXEA9800001 1 19980101 A 2611 MS25237387 BULB DHAV 302313 DHAV DHC8 DHC8102 2809003 NM CARGO COMP FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 823PH 110 BOI- SMOKE DETECTOR WARNING LIGHT DOES NOT TEST IN THE NR 1 POSITION. RELAMPED SMOKE DETECTOR, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998010800478 19980108 00478 NM 1998 1 8 QXEA9800002 1 19980101 A 2820 FILTER DHAV DHC8 DHC8202 2809007 NM NR 1 ENGINE DIRTY A QXEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 347PH 480 AFTER TAKEOFF DURING CLIMBOUT, THE NR 1 ENGINE LOW FUEL PRESSURE LIGHT ILLUMINATD AFTER THE BOOST PUMP WAS SWITCHED OFF. WHEN TURNING THE PUMP BACK ON THE LOW FUEL PRESSURE LIGHT GOES OUT. RETURNED TO THE FIELD AND ACCOMPLISHED AN UNEVENT FUL LANDING AT SEA. AIRCRAFT FERRIED FROM SEA TO PDX. REMOVED DEBRIS FROM THE NR 1 ENGINE JET PUMP FILTER SCREEN HOUSI NG. COMPLIED WITH POWER ASSURANCE RUNS, NO DEFECTS NOTED. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998010800479 19980108 00479 NM 1998 1 8 DL757980001 1 19980101 A 2530 OVEN BOEING 757 757232 1384965 NM GALLEY DIRTY A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 620DL 22910 PASSING 8K' ON DEPART. F/A REPORTED SMOKE IN AFT GALLEY CEILING AREA. OVENS TURNED OFF AND C/B'S PULLED, SMOKE DISSIPA TED. CHKD OVENS AND COFFEEMAKERS IN AFT GALLEY AND ALL GOOD. CHKD AFT GALLEY LIGHTS AND GOOD. DROPPED OVHD CEILING PA NEL AND AREA OK. AFT LAVS AND SMOKE DETECTORS GOOD. OK FOR SERVICE. SUSPECT SPILLED FOOD IN AFT OVENS. 2 L 7 2 4F RT A2NM 1998010800480 19980108 00480 NM 1998 1 8 DL757980002 1 19980101 A 5754 276002046 SKIN BOEING 757 757232 1384965 NM NR 6 LE SLAT DELAMINATED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 659DL 24421 AIR TURNBACK, A PORTION OF THE NR 6 L/E SLAT DELAMINATED AND RIPPED OFF. INSPECTION FOUND UPPER AFT PORTION OF THE NR 6 L/E SLAT DID DELAMINATE RIPPING OFF A QTY OF THE UPPER SLAT. ALSO, FOUND WAS A HOLE IN THE L/E OF THE WING APPROX 4.5 FT INBD OF THE RT ENG 3.5 IN BY 1.5 IN. 2 L 7 2 4F RT A2NM 1998010800481 19980108 00481 NM 1998 1 8 DLM88980004 1 19980102 A 3230 LOCKING CYL 39370335503 DOUG MD88 MD88 3023688 NM LT MLG SHEARED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 996DL MAL544 53363 AFTER GEAR RETRACTION, LEFT MAIN GEAR UNSAFE LIGHT ILLUM. GEAR HANDLE DOWN THREE GREEN AND NORMAL INDICATION. CONTROL TOWER CONFIRMED LEFT GEAR WAS EXTENDED. REPLACED LEFT GEAR OVERCENTER LOCKING CYLINDER WAS SHEARED AT ROD END. 2 L 7 2 4F RT A6WE 1998010800482 19980108 00482 NM 1998 1 8 DLM11980006 1 19980102 A 3350 5519881 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 803DE 48474 DURING EMERGENCY LIGHT TEST BATTERY -3 AND BATTERY -4 LOW MESSAGES ILLUMINATED. REPLACED BATTERY -3 AND BATTERY -4. EM ERGENCY LIGHTS CHECK NORMAL WITH NO ASSOCIATED MESSAGES. 2 L 7 3 4F RT A22WE 1998010800484 19980108 00484 NM 1998 1 8 DL76S980009 1 19980103 A 3350 LIGHT 1000677 BOEING 767 767332 1382001 NM COCKPIT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 117DL 2764 23276 COCKPIT DOOR EMERGENCY LIGHT INOP DURING TEST. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A1NM 1998010800487 19980108 00487 NM 1998 1 8 DHL98727001 1 19980101 A 5312 BULKHEAD FRAME BOEING 727 727228 NM AFT PRESS BLKHD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 727DH 20204 AT AFT BULKHEAD AFT ENTRY DOOR FRAME CRACKED AT NR 7 STOP LEFT AND RIGHT HAND. REPAIRED PER 727 S/B 53-0055. 2 L 7 3 4F A3WE 1998010800489 19980108 00489 NM 1998 1 8 P5CA9800001 1 19980102 A 5755 SKIN BOEING 747 747122 1384872 NM LT WING SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NR 5 SPOILER PANEL DELAMINATED. REPLACED SPOILER PANEL PER BOEING M/M 27-62-01. 2 L 7 4 4F A20WE 1998010800491 19980108 00491 1998 1 8 VNAA9801001 4 19980101 A 3140 7013348903 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 TRIPPED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 434JS 3051 WHILE SETTING POWER FOR TAKEOFF, LT ENGINE OIL PRESSURE INDICATION WAS ERRATIC ON EICAS PAGE. REDUCED POWER AND RETURNE D TO GATE. MAINTENANCE RERACKED THE NR 1 DATA ACQUISION UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-42-00. O PERATIONAL CHECK GOOD AND AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998010800492 19980108 00492 NM 1998 1 8 VNAA9801002 1 19980103 A 3060 B6444 DE-ICE LEAD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP DEFECTIVE A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 426JS 3038 DURING TAXI, LT PROPELLER HEAT FAILED. CREW RETURNED TO GATE AND CONTACTED MAINTENANCE CONTROL. DEFERRED LT PROPELLER HEAT SYSTEM IN ACCORDANCE WITH MEL 30-1-3. AIRCRAFT THEN COMPLETED FLIGHT TO PIT. PIT MAINTENANCE INSPECTED AIRCRAFT A ND REPAIRED BROKEN DE-ICE LEAD. OPERATIONAL CHECK OF SYSTEM GOOD AND AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998010800493 19980108 00493 EU 1998 1 8 MALA975856 1 19980101 A 3350 501171202 POWER PACK SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA A UNSCHED LANDING L NO TEST CL CLIMB 1 GL 15 408XJ 408 EMERGENCY POWER CAUTION LIGHT CAME ON AFTER LIFT OFF, PERFORMED QRH PROCEDURES. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED EMERGENCY POWER PACK, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998010800495 19980108 00495 EU 1998 1 8 MALA975858 1 19980103 A 2421 23080031 GENERATOR SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 417XJ 340B417 DURING FLIGHT, THE RIGHT AC GENERATOR FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RIGHT AC GENERATOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998010800496 19980108 00496 EU 1998 1 8 MALA975859 1 19980103 A 3350 7239410802 LIGHT SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 89XJ 089 DURING INSPECTION, ROW ONE EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998010800497 19980108 00497 NM 1998 1 8 MALA975860 1 19980105 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 826MA 330 DURING INSPECTION, ONE EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY FLOOR TRACK LIGHT, ALL CHECKS G OOD. 2 H 7 2 4T RT A13NM 1998010800498 19980108 00498 EU 1998 1 8 MALA975861 1 19980105 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO COMPT DIRTY A MALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 99XJ 099 ON TAKEOFF, THE CARGO SMOKE WARNING LIGHT ILLUMINATED. TAKEOFF WAS ABORTED. MAINTENANCE CLEANED SMOKE DETECTOR PHOTO O PTIC PER FAXED MAINTENANCE MANUAL REF 26-13-5, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998010800499 19980108 00499 EU 1998 1 8 MALA975862 1 19980104 A 2613 7239019506 TEST PANEL SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA K NONE N FALSE WARNING IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING PREFLIGHT INSPECTION, THE LEFT TAILPIPE HOT LIGHT NOT TESTING. MAINTENANCE REPLACED TEST PANEL 1, OPS CHECK OF F IRE TEST WAS GOOD. 2 L 7 2 4T RT A52EU 1998010800500 19980108 00500 EU 1998 1 8 MALA975863 1 19980105 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 595MA 340B216 DURING INSPECTION, EMERGENCY EXIT SIGN ABOVE 6A FELL OFF. MAINTENANCE REASSEMBLED AND INSTALLED EMERGENCY EXIT SIGN ASS EMBLY, OPS AND SECURITY CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998010800501 19980108 00501 NM 1998 1 8 W8PA980001 1 19980102 A 3397 WIRE BOEING 737 7373L9 1384470 NM CABIN DISCONNECTED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 960WP 23331 DEN- EMERGENCY FLOOR TRACK LIGHTING INOP FROM ROW 9 TO 11. RECONNECTED TRACK LIGHTING WIRE, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998010800502 19980108 00502 NM 1998 1 8 W8PA980002 1 19980101 A 3397 WIRE BOEING 737 73733R 1384407 NM CABIN BROKEN A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 963WP 28868 DEN- EMERGENCY TRACK LIGHTING INOP AT ROW 7 AND 15. REPAIRED WIRE AT ROW 7 AND 15, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998010800503 19980108 00503 NM 1998 1 8 W8PA980003 1 19980103 A 3350 S417N5092 LENS BOEING 737 7373L9 1384470 NM CABIN MISSING A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 960WP 23331 DEN- DURING INSPECTION, FOUND ROW 3 EMERGENCY LIGHT LENS MISSING. REPLACED ROW 3 EMERGENCY LIGHT LENS, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998010800504 19980108 00504 WP 1998 1 8 IXXA9800001 1 19980104 A 3310 SOCKET DOUG DC8 DC862F 3021972 WP GLARESHIELD SHORTED A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 41CX 46129 EN ROUTE, A BURNT ODOR WAS SENSED WHEN THE COCKPIT WHITE LIGHTING WAS TURNED ON. THE COCKPIT LIGHTING WAS TURNED OFF FO R THE REMAINDER OF THE FLIGHT. MAINTENANCE INVESTIGATED AND FOUND A GLARESHIELD FLUORESCENT LIGHT SOCKET SHORTED. MAIN TENANCE DEACTIVATED AND DEFERRED THE GLARESHIELD LIGHTING. 2 L 7 4 4F 4A25 1998010800505 19980108 00505 WP 1998 1 8 CALA9800001 1 19980104 A 2910 HYD LINE DOUG DC10 DC1030 3023501 WP LT ENGINE RUPTURED A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 87070 48292 THE AIRCRAFT LOST NR 1 HYDRAULIC SYSTEM QUANTITY WHILE EN ROUTE. FLIGHT MANUAL PROCEDURES WERE COMPLIED WITH AND THE AI RCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE LEFT PUMP SUCTION LINE RUPTURED. THE LINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998010800506 19980108 00506 NM 1998 1 8 CALA9800002 1 19980104 A 2910 HYD LINE BOEING 727 727232 1384082 NM LT MLG DOOR RUPTURED A CALA O OTHER J K WARNING INDICATION FLUID LOSS AP APPROACH 1 SW 09 45793 20647 THE AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY DURING GEAR EXTENSION WHILE ON APPROACH TO IAH. ABNORMAL AND EMERGENCY PR OCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT GEAR DOOR HYDRAULIC LINE RUPT URED. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL AND LEAK CHECKS WERE GOOD . 2 L 7 3 4F A3WE 1998010800507 19980108 00507 WP 1998 1 8 CALA9800003 1 19980106 A 5280 59305834001 SKIN DOUG DC9 DC982 3022082 WP LT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND A .5 INCH CRACK ABOVE BUMPER PAD IN LT MLG DOOR. THE CRACKED SKIN WAS REMOVED AND REPLACED IAW SRM 52- 05. 2 L 7 2 4F A6WE 1998010800508 19980108 00508 NE 1998 1 8 9800095641 2 19980102 A 7230 COMPRESSOR BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 541US 26488 716494 DURING TAKEOFF ROLL, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. TAKEOFF WAS ABORTED AT 10 KTS. BORESCOPE INSPECTI ON REVEALED COMPRESSOR DAMAGE. MAINTENANCE REPLACED THE NR 2 ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998010800509 19980108 00509 WP 1998 1 8 9800109762 1 19980105 A 3230 RETRACT MECH DOUG DC9 DC941 302207N WP NLG LACK OF LUBE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 762NW 47395 AFTER TAKEOFF, THE NOSE LANDING GEAR UNLOCK RED INDICATOR LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW FOLLOWED COM PROC EDURES AND RECYCLED THE LANDING GEAR HANDLE. ALL LANDING GEAR INDICATIONS CHECKED NORMAL AFTER 10 MINUTES AND AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE LUBRICATED THE NOSE LANDING GEAR ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998010800510 19980108 00510 WP 1998 1 8 9800129990 1 19980104 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG NOISE A NWAA O OTHER E VIBRATION/BUFFET CL CLIMB 1 GL 01 950E 47186 VIBRATION FOLLOWED BY A BANG OCCURRED FROM NOSE GEAR AREA ON GEAR RETRACTION AFTER TAKEOFF. FLIGHT WAS CONTINUED TO DES TINATION AND LANDED WITHOUT INCIDENT. NOTE: EMERGENCY EQUIPMENT WAS REQUESTED ON STANDBY AS A PRECAUTION. MAINTENANCE INSPECTED AREA AND NO PROBLEMS WERE FOUND. REPLACED BOTH NOSE TIRES AS A PRECAUTION. 2 L 7 2 4F A6WE 1998010800511 19980108 00511 WP 1998 1 8 9800139933 1 19980103 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG UNDERSERVICED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1334U 47280 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT I NCIDENT. MAINTENANCE SERVICED NOSE GEAR STRUT TO PROPER LEVELS. OPERATIONAL CHECK NORMAL ON GEAR CYCLE. 2 L 7 2 4F A6WE 1998010800512 19980108 00512 1998 1 8 9800149948 4 19980102 A 3417 2587400176 AIR DATA COMP DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8929E 57828 7444 45866 CAPTAIN'S ALTIMETER FLAGGED AND TCAS, AWAS AND AUTO-PILOT WERE INOPERATIVE AFTER TAKEOFF. FLIGHT WAS RETURNED TO MEM AN D LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED AIR DATA COMPUTER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998010800513 19980108 00513 WP 1998 1 8 9800159912 1 19980101 A 5280 GEAR DOORS DOUG DC9 DC931 3022065 WP NLG WORN A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 962N 47406 A LOUD VIBRATION WAS COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT WAS RETURNED TO PVD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOORS OUT OF ADJUSTMENT AND BEARINGS WORN. REPLACED BOTH FORWARD NOSE GEAR DOORS, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998010800514 19980108 00514 1998 1 8 9800169997 4 19980104 A 2312 TRANSCEIVER DOUG DC9 DC931 3022065 WP NR 1 MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8933E 47142 LOSS OF ALL RADIO COMMUNICATIONS OCCURRED WITH AIR TRAFFIC CONTROL AFTER TAKEOFF. FLIGHT WAS RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 VHF COMM TRANSCEIVER, NR 2 MICROPHONE, AND AUDIO CONTROL PANEL. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998010800516 19980108 00516 NM 1998 1 8 SWAA980001 1 19980103 A 2822 568125713005 BOOST PUMP BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE LT WING FAILED A A SWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SW 07 399SW 27693 CREW EXPERIENCED AN UNCOMMANDED NR 2 ENGINE SHUTDOWN WHILE ATTEMPING TO BALANCE FUEL USING CROSSFEED OPERATION. RESTAR TED ENGINE AND LANDED WITHOUT INCIDENT. REPLACED BOTH LEFT WING AFT AND FWD FUEL BOOST PUMPS AND PERFORMED FUEL FEED LI NE COUPLING VACUUM TEST PER BOEING M/M. 2 L 7 2 4F 4 F RT A16WE E2GL 1998010800517 19980108 00517 NM 1998 1 8 SWAA980002 1 19980105 A 2910 26010425 QUICK DISCONNECT BOEING 737 7372H4 138448C NM NR 2 BRAKE LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 60SW 21812 RETURNED TO PHX DUE TO EXPERIENCING A-SYSTEM HYDRAULIC PRESSURE LOSS RIGHT AFTER GEAR RETRACTION. AIRCRAFT LANDED WITHO UT INCIDENT. INSPECTED AND FOUND NR 2 BRAKE ASSEMBLY QUICK DISCONNECT BLANKING PLUG SHEARED AND LEAKING. REMOVED AND R EPLACED BRAKE ASSEMBLY, CHECKED FILTERS AND SERVICED HYDRAULIC SYSTEM PER BOEING M/M. 2 L 7 2 4F A16WE 1998010800518 19980108 00518 NM 1998 1 8 SWAA980003 1 19980105 A 5240 SEAL BOEING 737 7373H4 1384600 NM SERVICE DOOR PRESS LEAK A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 326SW 23690 RETURNED TO DAL DUE TO FWD SERVICE DOOR PRESSURE LEAK SQUEALING. AIRCRAFT LANDED WITHOUT INCIDENT. REWORKED DOOR SEAL MATING SURFACE AND PRESSURE CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998010800519 19980108 00519 NM 1998 1 8 UPS98625377 1 19980103 A 2610 47226601 OH DET CARD BOEING 767 76734AF 1385212 NM E/E COMPT FAILED A IPXA K NONE N FALSE WARNING AP APPROACH 1 SO 01 313UP 27764 INSPECTION TYPE-N/A, ON APP FIRE/ENG OVERHEAT EICAS MSG DISPLAYED AND SYS FAIL LT ILLUM. RESET, OPS NORMAL. REPLACED O H DETECTION CARD M687 (P/N 472266-01) OFF, (S/N 06), OPS CHK GOOD PER 26-10-01. 2 L 7 2 4F RT A1NM 1998010800527 19980108 00527 WP 1998 1 8 MWEA98888 1 19980104 A 3397 01864120 WIRE DOUG DC9 DC914 3022034 WP CABIN DEFECTIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 MTC FOUND TAIL COMPARTMENT EMERGENCY FLOOR TRACK LIGHTS INOP. MTC REPAIRED AFT SECTION WIRING AT LEFT LAV. 2 L 7 2 4F A6WE 1998010800528 19980108 00528 WP 1998 1 8 MWEA98887 1 19980103 A 3350 100865 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 DURING SERVICE CHECK, FOUND TAIL COMPARTMENT EMERGENCY FLOOR TRACK LIGHT INOP. MTC REMOVED AND REPLACED FLOOR TRACK LIG HT BATTERY PACK ASSEMBLY. 2 L 7 2 4F A6WE 1998010800529 19980108 00529 WP 1998 1 8 MWEA98889 1 19980104 A 5314 995774011 KEEL BEAM RIB DOUG DC9 DC914 3022034 WP BS 525 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DURING C-CHECK, FOUND LEFT KEEL BEAM RIB AT STATION 525 LOWER SIDE HAS A CRACK AT INBOARD END. MTC REMOVED AND REPLACED IAW SRM 53-01 FIG 2 SHEET 4 AND DAC DRAWING 9957740. 2 L 7 2 4F A6WE 1998010800530 19980108 00530 WP 1998 1 8 MWEA98890 1 19980103 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 64 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 DURING C-CHECK, FOUND FUSELAGE NOSE SKIN ON LEFT SIDE AT STATION 64 CRACKED. MTC REPAIRED IAW SRM 53-01 FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1998010800531 19980108 00531 WP 1998 1 8 MWEA98891 1 19980103 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 945-965 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 THE FUSELAGE INTERNAL SKIN DOUBLER SHOWED SIGNS OF CORROSION AT STATION 945 TO 965. MTC REPAIRED IAW SRM 53-04 FIG 12B SHEET 1 PAGE 33. 2 L 7 2 4F A6WE 1998010800532 19980108 00532 WP 1998 1 8 MWEA98892 1 19980104 A 5320 DOUBLER DOUG DC9 DC914 3022034 WP BS 76.55 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 DURING C-CHECK, FOUND 3 MODERATE GOUGES ON INTERNAL SIDE OF SKIN AT STATION 76.55 LONGERON 21R. MTC REPAIRED IAW SRM 53 -04 FIG 38 SHEET 18. 2 L 7 2 4F A6WE 1998010800533 19980108 00533 WP 1998 1 8 MWEA98893 1 19980105 A 3350 6011777 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 DURING C-CHECK, FOUND THE RIGHT HAND NACELLE EMERGENCY LIGHT REMAINS ILLUMINATED WITH SWITCH IN OFF POSITION. MTC REPLA CED EMERGENCY LIGHT BATTERY PACK ASSEMBLY. 2 L 7 2 4F A6WE 1998010800534 19980108 00534 WP 1998 1 8 MWEA98894 1 19980105 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 DURING C-CHECK, FOUND AFT ACCESSORY COMPARTMENT EMERGENCY LIGHTS ON STAIR HAND RAILS DIM. MTC REPLACED BATTERIES AND BA TTERY POWER SUPPLY IAW SRM 33-53-0. 2 L 7 2 4F A6WE 1998010800535 19980108 00535 WP 1998 1 8 MWEA98895 1 19980105 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 DURING C-CHECK, FOUND THE PAX ENTRY WAY AND GALLEY CEILING EMERGENCY LIGHTING DIM. MTC REPLACED THE BATTERY PACK AND BA TTERIES IAW SRM 33-53-0. 2 L 7 2 4F A6WE 1998010800637 19980108 00637 GL 1998 1 8 HEEA0012419 2 19980102 A 7261 6888547 INTERNAL SUMP 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE CAT33006 S787 CAE822541F ENGINE REMOVED DUE TO METAL IN OIL. UPON INSPECTION OF TURBINE PARTS NOTED: ERODED BEYOND SERVICEABLE LIMITS ON INTERN AL SUMP SEALS AND CRACKED. 1 G 7 2 3U 3 U H3EU E4CE 1998010800881 19980108 00881 SW 1998 1 8 PNSA980101 1 19980105 A 2742 ACTUATOR BARBERCOL 2719008001 SWRNGN SA227 SA227AC 8780603 SW HORIZ STAB MALFUNCTIONED A PNSA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 AL 03 640PA 176 AC759B WHILE F/O WAS TRIMMING AIRCRAFT, AIRCAFT PITCHED UP SHARPLY AND TRIM CONTROL COULD NOT BE REGAINED BY FO, CAPT OR OVERR IDE SYSTEM. FLIGHT CREW OVERPOWERED THE FLIGHT CONTROLS AND A SAFE LANDING WAS ACCOMPLISHED. STABILIZER WAS FOUND IN T HE FULL NOSE UP POSITION AND COULD NOT BE MOVED ELECTRICALLY. AFTER PHYSICALLY MOVING THE STABILIZER, TRIM WORKED NORMA LLY AND DID PASS TESTING PER AD97-23-01. ACTUATOR WAS REPLACED AND FLIGHT CHECK WAS NORMAL. NO FURTHER DISCREPANCIES H AVE BEEN FOUND SINCE WITH THE AIRFRAME. TEAR DOWN REPORT FROM BARBER COLMMAN SHOWED NORMAL OPERATION OF ACTUATOR. 2 L 7 2 4T RT A8SW 1998010800882 19980108 00882 NM 1998 1 8 W8PA980004 1 19980107 A 3350 3114981 REFLECTOR BOEING 737 7373B7 1384580 NM R2 DOOR INOPERATIVE A W8PA K NONE L NO TEST NR NOT REPORTED 1 NM 03 951WP 22951 DEN- R2 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED R2 DOOR EMERGENCY LIGHT REFLECTOR ASSY, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998010800883 19980108 00883 NM 1998 1 8 W8PA980005 1 19980106 A 3350 BULB BOEING 737 7373B7 1384580 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 951WP 22951 DEN- OVERHEAD EMERGENCY LIGHT AT ROW 23 IS INOP. REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998010800884 19980108 00884 NM 1998 1 8 W8PA980006 1 19980105 A 3350 OL3071BPEGPL LAMP BOEING 737 7373Q8 1384670 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 DEN- EMERGENCY FLOOR TRACK LIGHTING AT ROW 18 IS INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998010800885 19980108 00885 NM 1998 1 8 W8PA980007 1 19980104 A 3350 1155691 COVER BOEING 737 737301 1384611 NM CABIN MISSING A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 949WP 23230 DEN- FLOOR TRACK LIGHTING COVER IS MISSING AT ROW 4E. REPLACED COVER AT ROW 4E. 2 L 7 2 4F RT A16WE 1998010800886 19980108 00886 WP 1998 1 8 IXXA980002 1 19980107 A 2612 FIRE WARNING DOUG DC8 DC863F 302198F WP NR 4 ENGINE MALFUNCTIONED A IXXA K NONE O OTHER CR CRUISE 1 GL 23 867BX 46049 EN ROUTE, THE NUMBER FOUR ENGINE FIRE WARNING INTERMITTENTLY SOUNDED IN LIGHT TURBULENCE. THE FLIGHT CONTINUED TO TOL F OR AND UNEVENTFULL LANDING. MAINTENANCE INSPECTED THE ENGINE AND THE ASSOCIATED WIRING, WITH NO DISCREPANCIES NOTED. M AINTENANCE ACCOMPLISHED A SUCCESSFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL, AND THE AIRCRAFT WAS RE TURNED TO SERVICE. 2 L 7 4 4F 4A25 1998010800889 19980108 00889 EU 1998 1 8 AWXA9800002 1 19980104 A 2910 O-RING AIRBUS 320 A320231 3930325 EU GREEN HYD SYST LEAKING A AWXA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 28 635AW 092 ECAM MESSAGE IN CRUISE, GREEN SYSTEM LOW QUANTITY FOUND GREEN SYSTEM PTU MANIFOLD LEAKING FLUID AT PRIORITY VALVE MATING SURFACE. REMOVED PRIORITY VALVE FROM MANIFOLD AND REPLACED O-RINGS AND SQUARE SECTION SEALS ON BOBBINS AND REINSTALLED PER M/M 29-11-33. LEAK CHECK GOOD. 2 L 7 2 4F RT A28NM 1998010800890 19980108 00890 SO 1998 1 8 RAAA98E4001 1 19980106 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 RT AFT EMERGENCY EXIT PULLDOWN LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998010800918 19980108 00918 WP 1998 1 8 9800119867 1 19980103 A 2997 WIRE DOUG DC9 DC951 3022051 WP LT MLG WW BURNED A NWAA F ACTIVATE FIRE EXT. A FLAME/FIRE NR NOT REPORTED 1 GL 01 776NC 47786 FLIGHT CREW MEMEBER DISCOVERED A SMALL FLAME IN THE LEFT WHEEL WELL AT THE LOCATION OF THE ELECTRIC HYDRAULIC PUMP CANNO N PLUG. GROUND PERSONNEL EXTINGUISHED THE FIRE AND FLIGHT CREW EVACUATED AIRCRAFT AS A PRECAUTION. MAINTENANCE REPLACE D THE LEFT ELECTRIC HYDRAULIC PUMP AND REPAIRED CANNON PLUG WIRING, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998010800919 19980108 00919 NM 1998 1 8 9800172201 1 19980101 A 3230 65404676 DNLOCK ACTUATOR BOEING 727 727251 138408H NM NLG MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 201US 15610 7136 22154 DURING APPROACH WITH LANDING GEAR DOWN, NOSE LANDING GEAR FAILED TO EXTEND. LANDING GEAR WAS MANUALLY EXTENDED AND AIRC RAFT LANDED WITHOUT INCIDENT. REPLACED LOCK ACTUATOR AND PERFORMED GEAR SWING, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998010800920 19980108 00920 EU 1998 1 8 9800183250 1 19980104 A 3350 321454 POWER SUPPLY AIRBUS 320 A320212 EU CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 350NA 25119 11410 418 DURING EMERGENCY LIGHT TEST, RECEIVED FAULTS INT LOADS FWD L AND CO FWD L. MAINTENANCE REPLACED POWER SUPPLY AND BATTER Y PACK, OPERAITONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998010800921 19980108 00921 1998 1 8 9800193232 4 19980102 A 2565 C37103101103 SLIDE AIRBUS 320 A320211 3930320 EU PAX DOOR DEFECTIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 332NW 319 DURING INSPECTION OF PASSENGER DOOR EVACUATION SLIDE PACK RELEASE CABLE, FOUND DEFECTIVE CABLES ON SLIDES AT FORWARD RIG HT, AFT RIGHT, AND LEFT DOORS. REPLACED CABLES ON SLIDES AT AFT DOORS AND REPLACED SLIDE ASSEMBLY AT FORWARD DOOR. 2 L 7 2 4F RT A28NM 1998010800922 19980108 00922 NE 1998 1 8 9800201155 2 19980104 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 155US 46764 686175 DURING DESCENT, THE NR 3 ENGINE COMPRESSOR STALLED AND EXPERIENCED A FLAME-OUT. MAXIMUM EGT REACHED WAS 830C. THE CREW FOLLOWED COM PROCEDURES AND RESTART WAS SUCCESSFUL. THE ENGINE OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT. MAI NTENANCE INSPECTED THE ENGINE PER MM 71-00-00 WITH NO DEFECTS NOTED. MAXIMUM EGT WAS WITHIN LIMITS AND THE AIRCRAFT RET URNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1998010800923 19980108 00923 NM 1998 1 8 UPS98225379 1 19980104 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 1110-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-D, SEAT TRACK STA 1110 TO 1130 RBL 45 HAS CORROSION ON TOP AND BOTTOM OF FLANGES. REMOVED ALL CORROSION AND REMOVED AND REPLACED SEAT TRACK SPLICES IAW SRM 53-10-5 AND 51-10-6. 2 L 7 3 4F A3WE 1998010800924 19980108 00924 NM 1998 1 8 UPS98225381 1 19980106 A 3520 OXY MASK BOEING 727 72725C 138400H NM CABIN DEPLOYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, PAX O2 INADVERTENTLY DEPLOYED. STOWED PAX O2 MASKS. 2 L 7 3 4F A3WE 1998010800925 19980108 00925 NE 1998 1 8 UPS98525378 2 19980105 A 7321 ELECT ENG CNTRL BOEING 757 75724APF 1384969 NM PWA 2037 PW2040 NE RT ENGINE FAILED A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 418UP 23905 726508 INSPECTION TYPE-N/A ON SHORT FINAL, RT ENG FAILED. EPR REMAINED AT 1.0. N1 AND N2 WERE FROZEN, EGT 450C, AT ALL THRUST LEVER SETTINGS. ENG WAS NOT SHUT DOWN. ENG WENT TO FAIL-SAFE FLT IDLE POSITON. ENG RUN ON PRI AND SEC CHANNEL IN LGB WAS NORMAL. EEC WAS LATER CHANGED IN SDF. ENGINE RUN WAS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998010800926 19980108 00926 WP 1998 1 8 UPS98825380 1 19980106 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE-N/A JUST PRIOR TO TAXI OUT, EMERGENCY LTS ON WITH SW IN ARM POSITION. REMOVED AND REPLACED EMERGENCY BA TTERY PACK. ALSO, FOUND PIN PUSHED BACK ON CONNECTOR. REPAIRED PIN EMERGENCY LTS, OPS CHECKED GOOD PER MM 33-50-00. 2 L 7 4 4F RT 4A25 1998010800929 19980108 00929 WP 1998 1 8 UPS98825384 1 19980102 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 194 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN CABIN 3.0 INCH CRACK IN RT FWD SERVICE DOOR CUTOUT WEB, FS 194. REMOVED, FABRICATED AND INSTALL ED REPLACEMENT WEB IAW SRM 51-1-20D, 51-1-21, AND DWG 5615700. 2 L 7 4 4F RT 4A25 1998010800931 19980108 00931 NM 1998 1 8 QXEA9800003 1 19980102 A 3320 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 827PH 275 PDX - AFTER TAKEOFF FLIGHT ATTENDANT SMELLED BURNING SMELL AND OBSERVED OVERHEAD CABIN LIGHTS ON RIGHTHAND SIDE WENT OUT . INSPECTED ALL RIGHTHAND CEILING LIGHTS AND BALLAST ASSEMBLY. NO DEFECTS NOTED. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998010800932 19980108 00932 EU 1998 1 8 QXEA9800004 1 19980103 A 5210 R5294M4 ACTUATOR FOKKER F28 F28MK4000 4990810 EU PAX DOOR MALFUNCTION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 SEA - MAIN CABIN DOOR ACTUATOR BENT AND EMERGENCY RELEASE CABLE BROKEN. REPLACED ACTUATOR AND CABLE ASSEMBLY, OPERATION AL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998010800933 19980108 00933 EU 1998 1 8 QXEA9800005 1 19980103 A 3230 200498005 DNLOCK ACTUATOR FOKKER F28 F28MK4000 4990810 EU RT MLG MALFUNCTION A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 480AU 411 11229 FLIGHT DIVERTED TO BOI, RIGHT MAIN UNSAFE LIGHT ILLUMINATED. REPLACED MAIN LANDING GEAR DOWN LOCK ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998010800934 19980108 00934 WP 1998 1 8 QXEA9800006 2 19980103 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP NR 1 BIRD STRIKE A QXEA A UNSCHED LANDING C F.O.D. CR CRUISE 1 NM 09 26932 AC660 RETURN TO FIELD, BIRD STRIKE AFTER TAKEOFF. NR 1 ENGINE INLET SHOWS EVIDENCE OF INGESTION. INSPECTED AIRCRAFT AND NR 1 ENGINE IAW GARRETT MAINTENANCE MANUAL. NO PARTS REPLACED, OPERATIONAL CHECK GOOD. 2 L 7 2 4T 4 T RT A8SW E4WE 1998010800935 19980108 00935 NM 1998 1 8 QXEA9800007 1 19980104 A 3350 P4010021 BATTERY P20700012015 DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 822PH 106 PDX - FLIGHT ATTENDANT FLASHLIGHT DOES NOT TEST. REPLACED FLASHLIGHT BATTERY, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998010800936 19980108 00936 EU 1998 1 8 QXEA9800008 1 19980104 A 3350 MGG1055 POWER SUPPLY GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU GALLEY INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 GEG - SEVERAL 3 VOLT EMERGENCY LIGHT IN FORWARD GALLEY INOP. REPLACED NR 2 POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998010800937 19980108 00937 SW 1998 1 8 QXEA9800009 1 19980104 A 3310 SIDE PANEL SWRNGN SA227 SA227AC 8780603 SW RT COCKPIT SMOKING A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 26932 AC660 PDX - SMOKE COMING FROM COCKPIT RIGHTHAND SIDE PANEL. REMOVED, CLEANED AND REINSTALLED SIDE PANEL, OPERATIONAL CHECK GO OD. 2 L 7 2 4T RT A8SW 1998010800938 19980108 00938 NM 1998 1 8 98FDEA00003 1 19980105 A 2612 FIRE LOOP BOEING 727 727233 138408A NM NR 3 ENGINE WORN A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 221FE 20932 CREW VERBALLY REPORTED, ENGINE NR 3 FIRE LOOP-B, WITH FAULT LIGHT ON AND BELL/FIRE LIGHTS INTERMITTENTLY ACTUATING DURIN G FLIGHT. TROUBLESHOT B-LOOP AND FOUND ON ENG NR 3 FIREWALL FIRE DETECTION ELEMENT FORWARD CONNECTOR (D1498) CERAMIC IN SULATOR WORN, CAUSING FALSE INTERMITTENT FIRE DETECTION. DUE PARTS NOT IN STOCK AT GDL DEFERRED ENGINE NR 3 B-LOOP PER MINIMUM EQUIPMENT LIST 26-6B CONTROL NR 27935 EXPIRES 15 JAN 98. *S/D* REPLACED D-1498 ON FIREWALL FWD FIRE DETECTOR L OOP-B, CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998010800939 19980108 00939 NM 1998 1 8 98FDEA00004 1 19980106 A 3260 2314143 SWITCH BOEING 727 727225 1384077 NM RT MLG DOOR INOPERATIVE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 466FE 21292 RIGHT MAIN GEAR DOOR REMAINED LIT DURING RETRACTION. RECYCLED GEAR PER EMERGENCY PROCEDURES CHECK LIST. LIGHT REMAINED ILLUMINATED DURING RECYCLE, LIGHT WAS OUT DURING PREFLIGHT/GND OPERATION. REMAINED ON FOR EXTENSION/LDG. DUPLICATED R IGHT DOOR LIGHT ON/OFF AND FRONT PANEL DOOR WARNING LIGHT ON/OFF. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR WAR NING SWITCH, PER MAINTENANCE MANUAL 32-62-11. OPERATION CHECKED PER MAINTENANCE MANUAL 32-62-11 PAGE 501. 2 L 7 3 4F A3WE 1998010800940 19980108 00940 NM 1998 1 8 98FDEA00005 1 19980106 A 3020 DUCT BOEING 727 7272S2F 1384O81 NM NR 3 ENGINE COWL FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 216FE 22937 ENGINE NR 3 FIRE WARNING LIGHT ON CLIMBOUT 100 AGL. FOLLOWED RED TAB PROCEDURES. WARNING LIGHT WENT OUT WHEN THRUST LE VER RETARDED. FIRE WARNING SYSTEM CHECKED OK. RETURNED TO STL. *S/D* REMOVED TUBE PART NUMBER 777790, DUCT PART NUMB ER 1211318-002, FLANGE PART NUMBER 259-1068-501. INSTALLED TUBE, DUCT, AND DUCT FLANGE. LEAK CHECKS GOOD. DUE TO DUCT BREAK NR 3 UPPER COWL DAMAGED. REMOVED AND REPLACED SAME. 2 L 7 3 4F A3WE 1998010800941 19980108 00941 NM 1998 1 8 98FDEA00006 1 19980106 A 2610 FIRE LOOP BOEING 727 727227 1384078 NM NR 1 ENGINE LEAKS A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 490FE 21493 ENGINE 1 STRUT OVERHEAT LIGHT CAME ON DURING CLIMBOUT. FOLLOWED THE RED TAB PROCEDURES AND LIGHT EXTINGUISHED. FOUND F IRE LOOP NEAR TO AIRFRAME IN TWO PLACES UNDER 5401 PANEL. REARRANGED LOOP. RAN ENGINE TO CHECK FOR AIR LEAKS. FOUND N O AIR LEAKS. CLOSED AND SECURED ALL OPEN PANELS. 2 L 7 3 4F A3WE 1998010800942 19980108 00942 NM 1998 1 8 98FDEA00002 1 19980103 A 2910 SEAL BOEING 727 727227 1384078 NM RT ELEV HYD LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 487FE 21490 CLIMBOUT FL260 NOTICED THE HYD SYS-A QTY HAD DECREASE TOWARD THE 0 GAL IND WITH NORM SYS PRES OF 3000 PSI. THE FLUID QT Y IND BRKR WAS PULL THE RESET. SYS PRESS AND QTY REMAIN SAME, THE HYD SYS-A PUMP LO PRESS LIGHT BOTH FLICKERED AND SYS- A PRESS DECREASE THEN TOWARD 0 PSI. PERFORM STAB PROC AND THE CKLIST NAMED IN THE FOLLOW ORDER: HYD SYS LEAK OR LOSS, S YS-A RESTORATION LOSS, HYD SYS LEAK OR LOSS IN RANGE APPRO AND BEFORE LAND CKLIST. PERFORM A MAIN GEAR EXT PROC AND QTY LOSS. PER CKLIST CLOSED THE HYD SYS-A FLUID SHUTOFF SWITCH WITH THE ENG RUNNING. THE FLUID SOV SWITCH WERE CLOSED FOR APPROX 10 MIN. FND AFT FILT ER HOUSING LEAK ON RT ELEV PKG. REPLACED HSNG CAP AND SEALS, LEAK CK OK. 2 L 7 3 4F A3WE 1998010800943 19980108 00943 NM 1998 1 8 98FDEA00007 1 19980106 A 2613 OVERHEAT LIGHT BOEING 727 72722 1384002 NM AFT BODY ILLUMINATED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 181FE 18868 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT PASSING FL270. ENGINE ANTI-ICE WAS OPEN DURING CLIMBOUT. NR 1 BLEED WAS OPENED AND NR 2 BLEEDS CLOSED AND RED TAB PROCEDURE WERE INITIATED. THE LIGHT EXTINGUISHED SHORTLY AFTER NR 2 ENGINE ANTI-ICE WAS CLOSED. PROCEEDED TO DESTINATION WITH NR 1 AND 3 BLEEDS OPEN, NR 2 BLEEDS CLOSED BOTH PACKS ON. SYSTEM TESTS OK. RAN NR 1, 2, AND 3 ENGINES WITH BLEEDS ON. LEAK CHECKED PNEUMATIC DUCTING IN AFT AIRSTAIR FOR LEAKS. RAN NR 2 ENGINE AT 80 PERCENT N2 WITH BLEEDS ON AND TAI ON, LEAK CHECKED DUCTING AND NO LEAKS FOUND. INSPECTED LOOPS IN LEFT AND RIGHT SIDE OF AFT AIRSTAIRS, LOOPS BOTH CHECK NORMAL. COULD NOT DUPLICATE WRITE-UP. 2 L 7 3 4F A3WE 1998010800945 19980108 00945 NM 1998 1 8 DL72S980016 1 19980104 A 7120 CONE BOLT BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 58448 21273 695325 NR 1 ENG IDLES AT 1.2 EPR IN FLT. FOUND AFT ENG MOUNT CONE BOLT BROKEN. MTC IN PROGRESS REPLACING CONE BOLT AND ISOLATOR. 2 L 7 3 4F 4 F A3WE E2EA 1998010800946 19980108 00946 NM 1998 1 8 DL72S980017 1 19980104 A 3350 BATTERY PACK 900835 BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 418DA 9964 21271 695325 EMERG LIGHT AT F/C BULLNOSE INOP WHEN TESTED. REPLACED BATTERY PACK, OPN CKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998010800947 19980108 00947 NM 1998 1 8 DL72W980018 1 19980102 A 3530 4566M37B042NM PBE BOEING 727 727247 138408F NM CABIN DEFECTIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 PBE RED INDICATOR EXTENDED PASSED FLUSH. REPLACED PBE. 2 L 7 3 4F A3WE 1998010800948 19980108 00948 NM 1998 1 8 DL72W980019 1 19980102 A 3350 RPS1 POWER SUPPLY BOEING 727 7272Q8 138407W NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831L 21826 AFT SECTION OF EMERGENCY LIGHTS INOP FROM ROW 27. REPLACED 2 SOCKETS AND POWER SUPPLY. 2 L 7 3 4F A3WE 1998010800949 19980108 00949 NM 1998 1 8 DL72L980020 1 19980105 A 5754 SKIN BOEING 727 727232 1384082 NM RT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 CRACK IN LWR T/E SKIN AT ACTUATOR FITTING. REPAIRED SKIN PER SRM 57-50-3. 2 L 7 3 4F A3WE 1998010800950 19980108 00950 NM 1998 1 8 DL72L980021 1 19980105 A 5754 SPAR BOEING 727 727232 1384082 NM RT LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 FRONT SPAR CRACKED. REPAIRED SPAR PER SRM 51-40-3 (REF 57-50-2) ENG SIG. 2 L 7 3 4F A3WE 1998010800951 19980108 00951 NM 1998 1 8 DL76G980023 1 19980104 A 5330 141T385017 SKIN BOEING 767 7673P6 1385105 NM BS 22 DAMAGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 156DL 25354 THE FUSELAGE SKIN SUFFERED A LIGHTNING STRIKE AT A SKIN LAP SPLICE AT STA 220 AND WL 188. THE DAMAGE RESULTED IN A SMAL L (APPROX 1) CUTOUT IN THE UPPER SKIN PANEL OF THE SKIN LAP. THE DAMAGE WAS REPAIRED WITH A DOUBLER INSTALLED PER THE B 767 SRM 53-00-01, FIG 201 AND DOCUMENTED PER ER/A 363602-14. 2 L 7 2 4F RT A1NM 1998010800953 19980108 00953 NE 1998 1 8 DL72W980025 2 19980105 A 7200 ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 2813W 58238 695348 20869 695348 NR 3 ENG OIL STRAINER CLOG LIGHT ON / ENG SHUT DOWN. DIVERTED TO DFW. FOUND METAL ON CHIP DETECTOR AND FILTER. MTC IN PROGRESS, REPLACING ENG. 2 L 7 3 4F 4 F A3WE E2EA 1998010800959 19980108 00959 NM 1998 1 8 DL76L980031 1 19980105 A 2530 811150417 COFFEEMAKER BOEING 767 767332 1382001 NM GALLEY ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 197DN 28454 STRONG ODOR IN ALL GALLEYS, VERY UNCOMFORTABLE TO WORK IN FOR THE FLIGHT ATTENDANTS. FLIGHT ATTENDANTS ALSO REPORT THAT THERE IS NO DEFINABLE SOURSE AND IT SMELLS LIKE BURNED PAPER OR A HOT IRON. FOUND FIBERGLASS TAPE INSTALLED ON THE LOW ER COVER PLATE OF ALL 8 GALLEY COFFEEMAKER. MODIFIED COFFEEMAKERS PER ERA 310476-14. 2 L 7 2 4F RT A1NM 1998010800960 19980108 00960 NM 1998 1 8 DLM88980033 1 19980105 A 3350 BATTERY CHARGER RPS1 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 951DL 49882 FIRST CLASS EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A6WE 1998010800961 19980108 00961 WP 1998 1 8 ARWA970102 1 19980105 A 7110 5757519501 COWL DOUG DC8 DC862 3021970 WP NR 4 ENGINE MISSING A ARWA O OTHER D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 19 1808E 46105 ON POST FLIGHT, FOUND NR 4 ENGINE OUTBOARD AFT COWL MISSING. REMOVED AND REPLACED NR 4 OUTBOARD COWLING FOR A NEW ONE I AW 71-00-00. ALSO, INSPECTED NR 4 ENGINE AND OUTBOARD RIGHT WING, NO DAMAGE NOTED. 2 L 7 4 4F 4A25 1998010800962 19980108 00962 WP 1998 1 8 ARWA980101 1 19980107 A 2720 128E CONTROL CABLE DOUG DC8 DC862 3021970 WP RUDDER THROW BROKEN A ARWA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 19 802BN 45909 AIRCRAFT RETURNED TO BLOCKS RUDDER MOVEMENT LIMITED, HAS NOT FULL DEFLECTION WITH FLAPS DOWN. T/S FOUND RUDDER THROW LI MITER CABLE BROKEN. REMOVED AND REPLACED CABLE IAW 91-10-19 RIGGED IAW 27-50-0 OPS NORMAL. 2 L 7 4 4F 4A25 1998011500089 19980115 00089 EU 1998 1 15 MALA975864 1 19980105 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 115XJ 340A115 DURING INSPECTION, EMERGENCY LIGHT AT PASSENGER BOARDING DOOR INOP. MAINTENANCE REPLACED 3 FORWARD EMERGENCY BATTERY PA CKS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998011500091 19980115 00091 NE 1998 1 15 CALA9800004 2 19980104 A 7200 803605 SUPPORT COVER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE BROKEN A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 16804 49246 708525 THE FLIGHT ATTENDANT REPORTED, LIGHT SMOKE IN THE CABIN WHILE EN ROUTE. WHILE ACCOMPLISHING ABNORMAL PROCEDURES THE RT ENGINE OIL QUANTITY BEGAN TO DECREASE. THE AIRCRAFT WAS DIVERTED TO OMA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE SUPPORT CASE COVER BROKEN. THE SUPPORT COVER WAS REPLACED. IN ADDITION, THE COALESCER BAGS WERE REPLACED AND A BURNOUT OF THE HIGH PRESSURE PNEUMATIC SYSTEM WAS PERFORMED IAW MM 21-20-02, PAGE 209-216. 2 L 7 2 4F 4 F A6WE E9NE 1998011500092 19980115 00092 WP 1998 1 15 CALA9800005 1 19980107 A 2913 6506606 HYD PUMP DOUG DC10 DC1010 3022110 WP NR 1 ENGINE FAILED A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 68041 21311 46900 THE NR 1 ENGINE HYDRAULIC PUMP PRESSURE LOW LIGHT ILLUMINATED WHILE ON APPROACH. THERE WAS NO CHANGE IN HYDRAULIC PRESS URE OR QUANTITY. THE HYDRAULIC SYSTEM LOSS CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTE NANCE FOUND THE NR 1 ENGINE LEFT HYDRAULIC PUMP HAD A SHEARED SHAFT. THE PUMP WAS REMOVED AND REPLACED IAW MM 29-11-01. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998011500093 19980115 00093 1998 1 15 9800219909 4 19980105 A 3421 258733511 VERTICAL GYRO DOUG DC9 DC931 3022065 WP LT COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 958N 40118 3546 47254 CAPTAIN'S FLIGHT DIRECTOR FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO CLE AND LANDED WITHOUT INCIDENT. REPLACED CAPTA IN'S VERTICAL GYRO, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998011500094 19980115 00094 WP 1998 1 15 9800229946 1 19980105 A 2432 BATTERY CHARGER DOUG DC9 DC931 3022065 WP BATTERY COMPT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8926E 45863 BATTERY CHARGER ANNUNCIATOR LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED BATTERY CHARGER AND MAIN BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998011500095 19980115 00095 1998 1 15 6500239965 4 19980107 A 2565 113317 SLIDE BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 911RW 13646 1012 47149 DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE BATTERY PACK FAILED TEST. REPLACED SLIDE, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500096 19980115 00096 WP 1998 1 15 9800249920 1 19980107 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 942N 47459 DURING LINE MAINTENANCE INSPECTION, FOUND ROW 18DEF EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F A6WE 1998011500097 19980115 00097 WP 1998 1 15 9800259996 1 19980107 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8932E 47141 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 8, 9, AND 10 INOPERATIVE. REPAIRED B ROKEN WIRE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998011500098 19980115 00098 WP 1998 1 15 9800269948 1 19980106 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE CHECK, FOUND FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 5 THRU 7. MAINTENANCE REPLACED BATTERIES AT SEAT ROW 11DEF, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500099 19980115 00099 WP 1998 1 15 9800279948 1 19980102 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE CHECK, FOUND SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 5 THRU 7. MAINTENANCE REPLACED POW ER SUPPLY AND BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500100 19980115 00100 WP 1998 1 15 9800289948 1 19980104 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 5 THRU 7. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500101 19980115 00101 WP 1998 1 15 9800299988 1 19980105 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8944E 471671 DURING LINE CHECK, FOUND EMERGENCY PATHWAY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 14 THRU 17. MAINTENANCE REPLACED BLOWN FUSE AT SEAT ROW 12 RIGHT, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500102 19980115 00102 WP 1998 1 15 9800309908 1 19980103 A 3397 WIRE DOUG DC9 DC931 3022065 WP CATWALK BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 958N 47254 DURING LINE CHECK, FOUND CATWALK/EMERGENCY JETTISON HANDLE EXIT LIGHTS INOPERATIVE. MAINTENANCE SPLICED BROKEN WIRE, OP ERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500103 19980115 00103 WP 1998 1 15 9800319607 1 19980102 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 607NW 47232 DURING LINE CHECK, FOUND FORWARD GALLEY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATION AL CHECK OK. 2 L 7 2 4F A6WE 1998011500104 19980115 00104 WP 1998 1 15 9800329965 1 19980103 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 911RW 47149 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE AFTER 10 MINUTE CHECK. MAINTENANCE REPLACED LEFT NACE LLE BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500105 19980115 00105 WP 1998 1 15 9800339918 1 19980103 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 940N 47572 DURING LINE CHECK, FOUND RIGHT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHE CK OK. 2 L 7 2 4F A6WE 1998011500106 19980115 00106 WP 1998 1 15 9800349878 1 19980106 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 5 THRU 8. MAINTENANCE REPLACED FUSE IN POWER SU PPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998011500107 19980115 00107 WP 1998 1 15 9800359866 1 19980106 A 3350 CHARGER DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED CHARGER AND BATTERIES , OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998011500108 19980115 00108 NE 1998 1 15 9800366717 2 19980105 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 1 FAILED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 617US 21121 662545 ON FINAL APPROACH, THE CREW NOTICED THE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED FOR THE NR 1 ENGINE. AFTER LANDING, THE NR 1 ENGINE EGT EXCEEDED REDLINE AND THE CREW SHUT DOWN THE ENGINE. MAINTENANCE REPLACED THE NR 1 ENGINE. 2 L 7 4 4F 4 F A20WE E20EA 1998011500109 19980115 00109 EU 1998 1 15 WWMA9800004 1 19980106 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 345SB 340B345 DURING PREFLIGHT, CREW FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED ALL 5 EMERGENCY LIGHT BATTERY PACKS 20LN, 21LN, 22L N, 23LN AND 24LN. 2 L 7 2 4T RT A52EU 1998011500110 19980115 00110 EU 1998 1 15 WWMA9800003 1 19980105 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 247AE 340B247 EMERGENCY LIGHTS AT ROW 9A, 11A AND EXIT LIGHT AT 8A FAIL TO ILLUMINATE. REPLACED EMERGENCY POWER SUPPLY 23LN. 2 L 7 2 4T RT A52EU 1998011500111 19980115 00111 EU 1998 1 15 WWMA9800002 1 19980104 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO DIRTY A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 350CF 340B350 CARGO SMOKE LIGHT ILLUMINATED INTERMITTENTLY EVERY 15 TO 18 SECONDS DURING PREFLIGHT. MAINTENANCE CLEANED SMOKE DETECTO R AND RESECURED LOOSE CANNON PLUG. 2 L 7 2 4T RT A52EU 1998011500112 19980115 00112 SW 1998 1 15 QXEA9800010 1 19980104 A 3310 SIDE PANEL SWRNGN SA227 SA227AC 8780603 SW RT COCKKPIT SMOKING A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 26932 AC660 SMOKE COMING FROM RIGHT SIDE PANEL. FOUND TO BE REAR MOST RIGHTHAND CIRCUIT BREAKER EDGE LIGHTING DISCONNECTED. PANEL SECURED AND STOWED WIRES. PLACED ON MEL IAW MEL 33-1. MEL CLEARED BY REMOVING, CLEANING, AND REINSTALLING THE SIDE PAN EL, OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 L 7 2 4T RT A8SW 1998011500113 19980115 00113 NM 1998 1 15 QXEA9800011 1 19980106 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 826PH 214 SEA - EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR FLOOR INOP. REPAIRED DEFECTIVE WIRING, NO PARTS REPLACED. OPERATIONAL CH ECK GOOD. 2 H 7 2 4T RT A13NM 1998011500114 19980115 00114 NM 1998 1 15 QXEA9800012 1 19980106 A 3350 SWITCH DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 823PH 110 PDX - FLIGHT ATTENDANT EMERGENCY LIGHTING SWITCH NORM LIGHT INOP. REPLACED SWITCH, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998011500115 19980115 00115 NM 1998 1 15 QXEA9800013 1 19980106 A 6120 AUTOFEATHER DHAV DHC8 DHC8202 2809007 NM PROP SYST FAILED TEST A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 355PH 500 MFR - AIRCRAFT AUTO FEATHER TEST INOP. MAINTENANCE CYCLED POWER LEVERS SEVERAL TIMES, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998011500116 19980115 00116 1998 1 15 98FDEA00008 4 19980107 A 3417 HG480B13 AIR DATA COMP BOEING 727 727233 138408A NM E/E COMP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 257FE 20939 AIR DATA COMPUTER NR 1 CIRCUIT BREAKER POPPED ON TAKEOFF ROLL, CONTINUED TO TROUBLESHOOT PROBLEM IN AIR. CIRCUIT BREAKE R WOULD NOT RESET. RETURNED TO SDF FOR MAINTENANCE TO WORK. REMOVED AND REPLACED AIR DATA COMPUTER PER MAINTENANCE MAN UAL 34-12-0 PAGES 8 AND 9. OPERATIONAL CHECK OK, PERFORMED PITOT/STATIC LOW RANGE PER MAINTENANCE MANUAL 34-11-0 PAGES 503 AND 504. 2 L 7 3 4F RT A3WE 1998011500117 19980115 00117 1998 1 15 98FDEA00009 2 19980107 A 7510 ANTI-ICE VALVE BOEING 727 727227 1384078 NM NR 1 ENGINE LEAKING A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 490FE 21493 ENGINE 1 STRUT OVERHEAT LIGHT CAME ON DURING CLIMBOUT. FOLLOWED THE RED TAB PROCEDURES AND LIGHT EXTINGUISHED. REMOVED AND REPLACED NR 1 ENGINE ANTI-ICE VALVE GASKET ON TOP SIDE OF VALVE. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 ENGIN E STRUT OVERHEAT SENSE LINE PER MAINTENANCE MANUAL 26-14-1. GROUND RUN OPERATIONAL CHECK GOOD. RAN AIRCRAFT AT TAKEOFF POWER FOR 5 MINUTES NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1998011500118 19980115 00118 NM 1998 1 15 98FDEA00010 1 19980107 A 5313 651838727 STRINGER BOEING 727 72722 1384002 NM BS 1080 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 CORROSION ON STR 29 LT KEEL BEAM LT BS 1080, WL 140. *S/D* REMOVED CORROSION ON STR 29L AT BS 1080 TO 1095, WL 140. F OUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. REMOVED CORRODED PIECE IAW FEDEX SRM 53-10-3. FABRICATED REPAIR PARTS PER FEDEX SRM 53-10-3 AND INSTALLED. 2 L 7 3 4F A3WE 1998011500119 19980115 00119 NM 1998 1 15 98FDEA00011 1 19980107 A 5320 65198622 CHORD BOEING 727 72722 1384002 NM BS 294-350 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 CORROSION (C53-224-03 1, 2) ON RT MID CHORD BS 315 TO 335, RBL 15, WL 169 WILL REQUIRE REMOVAL OF NOSE LANDING GEAR TO G AIN ACCESS. *S/D* REMOVED DAMAGED CHORD AND INSTALLED NEW CHORD BS 259 TO 351, WL 169, RBL 15 IAW FEDEX DRG 65-18415. 2 L 7 3 4F A3WE 1998011500120 19980115 00120 NM 1998 1 15 98FDEA00012 1 19980107 A 2497 WIRE DOUG MD11 MD11F 3023600 NM CARGO COMPT FIRE A A FDEA K NONE A FLAME/FIRE IN INSP/MAINT 1 SO 25 614FE 48528 CENTER CARGO COMPARTMENT NR 4L ROLLER INOP., PAP5 C/B. REMOVED FLOOR BOARDS, FOUND THE WIRING, UNDER THE FLOOR HAD A FI RE. WIRING WAS BURNED UP, ALSO BELLFRAME HAD HOLE BURNED THRU FRAME AT STA 1641, BETWEEN LONG 47 AND 48. NOTED ON NO. 02 AND 24, DURING B-CHECK MAINT REMOVED DAMAGED AREA, VERIFIED ALL DAMAGE REMO VED EDDY CURRENT INSPECTED AREA. NO IND ICATIONS OF CRACKS NOTED. INSTALLED DOUBLER PER SRM 53-30-00, ITEM 2. WIRING PROBLEM: SPLICED WIRES PER WIRING DIAGRAM 25-52-06, OPS. CHK OF LOADING SYSTEM FOUND NORMAL, PER M/M 25-50. SIGNED OFF MACH ITEM 25-50/2769. RELEASE A/C 1-7-9 8. 2 L 7 3 4F RT A22WE 1998011500121 19980115 00121 WP 1998 1 15 ABXA9800001 1 19980106 A 3297 WIRE DOUG DC8 DC863F 302198F WP LANDING GEAR OUT OF POSITION A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 812AX 46126 DURING GEAR RETRACTION, THE LANDING GEAR LEVER WAS BINDING AND COULD NOT BE MOVED TO THE LATCH-CHECK OR UP POSITION. RE CYCLED GEAR HANDLE TO DOWN POSITION. MOVED HANDLE TO UP POSITION, BINDING REMAINED BUT GEAR INDICATED UP. FOUND WIRING JAMMED BETWEEN LANDING GEAR CONTROL PULLEY AND CONTROL CABLES. REMOVED AND REPAIRED WIRING. PERFORMED OPS CHECK OF LA NDING GEAR IAW WITH DC8 MM 32-31-1 AND OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998011500122 19980115 00122 NM 1998 1 15 P5CA9800002 1 19980106 A 5320 HINGE BOEING 747 747122 1384872 NM BS 1020 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LEVEL 1 CORROSION AND BARE METAL AND FRETTING FOUND ON MOUNTING FLANGES FOR AIR CONDITIONING HINGE PANELS IN SEVERAL PLA CES LT AND RT SIDES. REMOVED SURFACE CORROSION TREATED AND PRIMED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1998011500123 19980115 00123 NM 1998 1 15 P5CA9800003 1 19980106 A 5314 KEEL BEAM BOEING 747 747122 1384872 NM BS 1239-1484 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 INNER SURFACE AT KEEL BEAM STA 1239 TO 1484 SEEN THRU LIGHTENING HOLE BUBBLING AND FLAKING PAINT. CLEANED AREA AND PRIM ED BARE METAL PER BOEING SRM 51-10-02. 2 L 7 4 4F A20WE 1998011500124 19980115 00124 NM 1998 1 15 P5CA9800004 1 19980105 A 5280 SKIN BOEING 747 747122 1384872 NM RT MLG DOOR PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 RT WING GEAR UPPER STRUT DOOR INNER SKIN PUNCTURED ALONG AFT EDGE OF PLACARD. FABRICATED AND INSTALLED REPAIR PARTS IAW BOEING SRM 52-80-02. 2 L 7 4 4F A20WE 1998011500125 19980115 00125 1998 1 15 P5CA9800005 4 19980105 A 3444 ANTENNA BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LEVEL 1 CORROSION FOUND ON FWD CENTER RADIO ALT ANTENNA. CLEANED IAW STANDARD PRACTICES, OPS CHECK GOOD IAW MM 34-37-00 . 2 L 7 4 4F A20WE 1998011500126 19980115 00126 NM 1998 1 15 P5CA9800006 1 19980107 A 5245 ANGLE BOEING 747 747122 1384872 NM AC DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FWD AIR COND ACCESS PANEL 191A FWD HINGE ATTACH ANGLE CRACKED. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998011500175 19980115 00175 WP 1998 1 15 VJ9800003 1 19980108 A 2560 591769637 SLIDE COVER DOUG DC9 DC932 3022066 WP L1 DOOR LOOSE A VJ6A K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 924VV 47278 ON ARRIVAL AT GATE, EMERGENCY SLIDE COVER CAME AJAR WHEN MAIN PASSSENGER DOOR WAS OPENED. REINSTALLED SLIDE COVER IAW M M 25-00 AND PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998011500176 19980115 00176 NM 1998 1 15 K3HA980001 1 19980107 A 3350 81 LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 RIGHT WING CENTER OVERWING EMERGENCY LIGHT INOP. RELAMPED CENTER OVER WING EMERGENCY LIGHT RIGHT HAND WING. 2 L 7 3 4F A3WE 1998011500182 19980115 00182 NM 1998 1 15 RAAA98B2003 1 19980108 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998011500183 19980115 00183 NM 1998 1 15 RAAA98B2004 1 19980108 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998011500184 19980115 00184 NM 1998 1 15 RAAA98B2005 1 19980108 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998011500185 19980115 00185 SO 1998 1 15 RAAA98E9003 1 19980108 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998011500186 19980115 00186 1998 1 15 CALA9800006 4 19980108 A 2565 D31591478 SLIDE BOEING 737 7373T0 1384582 NM R 1 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 63305 29833 23356 INSPECTION FOUND THE R-1 DOOR SLIDE PRESSURE LOW. THE R-1 DOOR SLIDE WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1998011500187 19980115 00187 NM 1998 1 15 CALA9800007 1 19980108 A 3230 SENSOR BOEING 737 7373T0 1384582 NM RT MLG OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 71314 23365 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM IAH. THE GEAR HANDLE WOULD NOT GO PAST OFF POSITION. MAINTENANCE FOUND THE MAIN GEAR AIR SAFETY SENSOR OUT OF ADJUSTMENT. THE AIR SAFETY SENSOR WAS ADJUSTED/TESTED IAW MM 32-09-01 AND GEAR HANDLE OPERATION WAS GOOD. 2 L 7 2 4F RT A16WE 1998011500188 19980115 00188 WP 1998 1 15 CALA9800008 1 19980106 A 3350 AD4002P BATTERIES SAFT DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12514 48113 INSPECTION FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 18-22 INOPERATIVE. THE BATTERIES IN CHARGER WERE REPLACED AND O PERATION OF THE LIGHTS WAS RESTORED. 2 L 7 2 4F A6WE 1998011500189 19980115 00189 WP 1998 1 15 CALA9800009 1 19980107 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 936AS 49363 INSPECTION FOUND Z-ANGLE BEAM REPAIR STRAP CORRODED AT AFT CARGO BIN LOWER DOOR JAMB. THE REPAIR STRAP WAS REPLACED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998011500190 19980115 00190 WP 1998 1 15 CALA9800010 1 19980108 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 562-595 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND LOWER LT DOOR JAMB LONGERON (INSIDE NR 1 A/C PACK COMPARTMENT) AT STA 562-595 CORRODED. A NEW LONGERON SECTION, REPAIR ANGLES, AND STRAPS WERE FABRICATED AND INSTALLED IAW ECRA 5310-03653. 2 L 7 3 4F A22WE 1998011500191 19980115 00191 EU 1998 1 15 9800373202 1 19980105 A 2750 D5757030500200 RETRACT MECH AIRBUS 320 A320211 3930320 EU TE FLAPS OUT OF ADJUST A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 302US 32 DURING APPROACH WHEN FLAPS POSITION ONE SELECTED, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT MESSAGE. DIVERTED TO IAD FOR LONGER RUNWAY AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAP SYSTEM. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998011500192 19980115 00192 NM 1998 1 15 9800386608 1 19980107 A 3230 RETRACT MECH BOEING 747 747151 1384891 NM LANDING GEAR LACK OF LUBE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 608US 19785 DURING CLIMB, THE RED LANDING GEAR LIGHT ILLUMINATED AND BOTH THE PRIM AND ALT GEAR INDICATED R BODY DOWN. RECYCLED LAN DING GEAR. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. LUBRICATED RIGHT BODY LANDING GEAR MECHANISM . OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998011500193 19980115 00193 1998 1 15 9800399944 4 19980108 A 3417 2587400176 CADC DOUG DC9 DC931 3022065 WP E/E COMPT INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 1309T 33610 2048 47316 DURING CLIMB-OUT, CAPTAIN'S ALTIMETER AND VERTICAL AIRSPEED INDICATOR BECAME INOPERATIVE. AIRCRAFT RETURNED TO ORIGINAT ION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 CENTRAL AIR DATA COMPUTER. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500194 19980115 00194 WP 1998 1 15 9800409915 1 19980108 A 2150 2045054 ACM DOUG DC9 DC931 3022065 WP TAIL COMPT INOPERATIVE A NWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 965N 38641 6031 47417 IN CRUISE FLIGHT, SMOKE IN CABIN ACTIVATED FORWARD LAVATORY SMOKE ALARM. FLIGHT CREW DECLARED RED EMERGENCY AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CYCLE MACHINE AND THE LEFT AND RIGHT COALESCER BAG F ILTERS. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500195 19980115 00195 WP 1998 1 15 9800419305 1 19980107 A 3310 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 307RC 48086 DURING CLIMB-OUT, FLIGHT CREW DISCOVERED SMOKE COMING FROM UNDER COPILOT'S GLARESHIELD. SMOKE DISIPATED RAPIDLY. FLIGH T RETURNED TO ORIGINATION AS A PRECAUTION AND LANDED WITHOUT INCIDENT. MAINTENANCE DISCOVERED A BROKEN GLARESHIELD LIGH T BULB. DEFERRED COCKPIT GLARESHIELD LIGHTING PER MEL 33-1 AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 2 4F A6WE 1998011500196 19980115 00196 SO 1998 1 15 COMA9810002 1 19980106 A 5311 12008896001 FRAME T-SECTION EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT MIDDLE T-SECTION AT FRAME 16 TO BE HEAVILY CORRODED. REMOVED CORR ODED T-SECTION AND INSTALLED SERVICABLE T-SECTION USING EMB120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500197 19980115 00197 SO 1998 1 15 COMA9810003 1 19980106 A 5320 12046156001 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500198 19980115 00198 SO 1998 1 15 COMA9810004 1 19980107 A 5320 12005805003 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CENTER BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRA P AND INSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500199 19980115 00199 SO 1998 1 15 COMA9810005 1 19980107 A 5320 12046963001 BUTTSTRAP EMB 120 EMB120RT SO LAVATORY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 BUTTSTRAP TO BE HEAVILY CORRODED. REMOVED CORRODED BUTTSTRAP AND I NSTALLED SERVICABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500200 19980115 00200 SO 1998 1 15 COMA9810006 1 19980107 A 5320 12005803001 SILL EMB 120 EMB120RT SO LAVATORY CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 DURING 2C INSPECTION TASK 5310-131-01I REVEALED NR 1 CABIN SILL RIGHT TO BE HEAVILY CORRODED. REMOVED CORRODED SILL AND INSTALLED SERVICABLE SILL USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500201 19980115 00201 SO 1998 1 15 COMA9810007 1 19980107 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 DURING 2C INSPECTION TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM AND INS TALLED SERVICABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500202 19980115 00202 SO 1998 1 15 COMA9810008 1 19980107 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 20 TO BE HEAVILY CORRODED. REMOVED CROSSBEAM A ND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500203 19980115 00203 SO 1998 1 15 COMA9810009 1 19980107 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 23 TO BE CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERV ICEABLE CROSSBEAM USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500204 19980115 00204 SO 1998 1 15 COMA9810010 1 19980106 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 2C INSPECTION TASK 5310-131-01I REVEALED THAT THE RIGHT CROSSBEAM AT FRAME 16 WAS CORRODED TO LIMITS. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500205 19980115 00205 SO 1998 1 15 COMA9810011 1 19980106 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 2C TASK 5320-147-03I REVEALED CROSSBEAM (RIGHT) AT FRAME 23 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500206 19980115 00206 SO 1998 1 15 COMA9810012 1 19980106 A 5320 12006647001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 2C TASK 5320-147-03I REVEALED LEFT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERVI CABLE PART USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500207 19980115 00207 SO 1998 1 15 COMA9810013 1 19980106 A 5320 12004449003 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 2C TASK 532D-147-03I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALL ED SERVICEBLE PART USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500208 19980115 00208 SO 1998 1 15 COMA9810014 1 19980107 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 2C TASK 151-01Z REVEALED LEFT CROSSBEAM TO BE CORRODED AT FRAME 33. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBE AM USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500209 19980115 00209 SO 1998 1 15 COMA9810015 1 19980107 A 5320 12006647002 CROSSBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 205CA 18441 120205 2C TASK 532D-147-03I REVEALED RIGHT CROSSBEAM AT FRAME 28 TO BE CORRODED. REMOVED CORRODED CROSSBEAM AND INSTALLED SERV ICEABLE PART USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998011500210 19980115 00210 SO 1998 1 15 COMA9810016 1 19980106 A 3260 2050500101 HARNESS EMB 120 EMB120RT SO LT MLG DAMAGED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 462CA 120264 WEIGHT ON WHEELS SAFETY LATCH ON LANDING GEAR CONTROL DID NOT RELEASE AFTER TAKEOFF. REPLACED THE LEFT MLG WEIGHT ON WH EELS SWITCH HARNESS. 2 L 7 2 4T RT A31SO 1998011500211 19980115 00211 SO 1998 1 15 COMA9810017 1 19980106 A 3350 12021299001 LIGHT EMB 120 EMB120RT SO RT EXTERIOR INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 137H 120137 RIGHT AFT EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED LIGHT ASSY. 2 L 7 2 4T RT A31SO 1998011500212 19980115 00212 EA 1998 1 15 COMA9860006 1 19980101 A 2820 601R6240115 CONDUIT CNDAIR CL600 CL6002B19 EA CTR FUEL TANK CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 11050 7013 DURING COMPLIANCE OF SB601R-28-008, THE CONDUIT FOR WIRING TO RIGHT FUEL CROSSFLOW SOV WAS FOUND CHAFED THROUGH THE WALL THICKNESS. THE CHAFING TOOK PLACE BETWEEN THE CONDUIT AND THE FUEL LINE SUPPORT BRACKET AT STATION 485 RBL 24 WL 57. R EPLACED DAMAGED WIRING CONDUIT. 2 L 7 2 4F RT A21EA 1998011500213 19980115 00213 NM 1998 1 15 UPS98225392 1 19980107 A 2720 RUDDER BOEING 727 72731C 1384011 NM EMPENNAGE SPLIT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 922UP 19231 DURING EACH LEG, THE RUDDER TRIES TO SPLIT AT VARIOUS SPEEDS AND ALTITUDES. INSPECTED RUDDER SYSTEM FOR LOOSE TABS OR C OMPONENTS, NONE FOUND. COULD NOT DUPLICATE ON GROUND, ALL WORK DONE IAW MM 27-20 AND 27-30-143. NO FAULTS NOTED. ALL OPS CHECKS NORMAL, A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 1998011500220 19980115 00220 EU 1998 1 15 WWMA9800005 1 19980106 A 3397 WIRE SAAB SF340 340B 7860101 EU CABIN BROKEN A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 256AE 340B256 EMERGENCY LIGHT ABOVE SEAT 8A FAILED TO ILLUMINATE DURING PREFLIGHT TEST. REPAIRED BROKEN WIRES AT LIGHT ASSEMBLY. 2 L 7 2 4T RT A52EU 1998011500221 19980115 00221 1998 1 15 98FDEA00013 4 19980107 A 3417 HG480B13 AIR DATA COMP BOEING 727 727233 138408A NM E/E COMPT FAILED A FDEA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 25 257FE 20939 98-0010 - NR 1 AIR DATA COMPUTER CIRCUIT BREAKER TRIPPED ON CLIMB-OUT, EFFECTING CAPTAIN'S AIRSPEED, ALTIMETER, GPWS. R ESET CIRCUIT BREAKER TRIPPED AGAIN. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER. SYSTEM OPERATIONAL AND LEAK CHECKS GO OD. 2 L 7 3 4F RT A3WE 1998011500222 19980115 00222 1998 1 15 98FDEA00014 4 19980107 A 3417 HG480B13 AIR DATA COMP BOEING 727 727233 138408A NM E/E COMPT FAILED A FDEA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 SO 25 257FE 20939 98-0011 - ON CLIMB-OUT (APPROX 2000FT) CAPTAIN LOST AIRSPEED, ALTIMETER, GPWS. SUSPECTED NR 1 AIR DATA COMPUTER FAILURE . ALL CIRCUIT BREAKERS CHECK, NONE TRIPPED. RED TABS COMPLIED WITH. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER. PER FORMED LOW LEVEL LEAK OF CAPTAINS'S PITOT/STATIC SYSTEM. LEAK CHECKS GOOD. AIR DATA COMPUTER FUNCTION TEST IS GOOD. A LTIMETER ALERT AND GPWS CHECK GOOD. 2 L 7 3 4F RT A3WE 1998011500223 19980115 00223 NM 1998 1 15 98FDEA00015 1 19980108 A 3610 PNEUMATIC DUCT BOEING 727 72722 1384002 NM NR 3 ENGINE BLOWN A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 196FE 19145 REJECTED TAKEOFF AT 85 KNOTS DUE TO NR 3 ENGINE FIRE WARNING. COMPLETED ENGINE FIRE CHECK LIST AND REJECTED TAKEOFF CHE CK LIST. REJECTED TAKEOFF BRAKE COOLING CHART INDICATED 29 MINUTES COOL DOWN IN BLOCKS AT 0339 Z. INSPECTED TIRES AND BRAKES AT 0410Z, OK FOR SERVICE. INSPECTED NR 3 ENGINE, FOUND PNEUMATIC DUCT AT STARTER BLOWN. REPLACED PNEUMATIC DUCT ASSEMBLY NO LEAKS NOTED. 2 L 7 3 4F A3WE 1998011500224 19980115 00224 NM 1998 1 15 98FDEA00016 1 19980108 A 5297 WIRE BOEING 727 72725 1384006 NM CARGO DOOR LOOSE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 154FE 18287 WHEN PASSING THROUGH FLIGHT LEVEL 270, MAIN CARGO DOOR LIGHT ILLUMINATED WITH NO LOSS OF PRESSURIZATION. DESCENDED TO 1 0,000, DEPRESSURIZED AIRCRAFT. LIGHT STAYED ON UNTIL LANDED. REPRESSURIZED AFTER LANDING, NO LIGHT ON. FOUND LOOSE WI RE ON NORMALLY CLOSED AFT SWITCH, CYCLED DOOR, DOOR WOULD NOT LOCK EVERYTIME. FOUND FORWARD 2 LOCKS WOULD NOT LOCK, REQ UIRES RIGGING. M/M 52-34-9, PAGE 503. (THIS IS A CHRONIC REPEAT). MAIN CARGO DOOR ACCESS PANELS REMOVED. PERFORMED M AIN CARGO DOOR ADJUSTMENT AND TEST FOUND FWD TORQUE TUBE SWITCH LATCH COND: OPEN OUT OF ADJUSTMENT. ADJUST PER M/M 52- 34-9. OPERATIONAL CHECK GOOD AT THIS TIME. ALSO CLEANED AND LUBED SWITCHES. REQ ITEM INSP COMPLIED WITH. 2 L 7 3 4F A3WE 1998011500225 19980115 00225 NM 1998 1 15 98FDEA00017 1 19980108 A 5320 65198614 CHORD BOEING 727 72722 1384002 NM BS 336 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 NR 0328 003, CORROSION C53-111-03 1/2 ON RT LOWER NOSE CHORD BS 336 TO 350, RBL 17, WL 149. FOUND CORROSION ON RT LOWER NOSE CHORD BS 336 TO BS 350, RBL 17, WL 149 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REMOVED AND REPLACED CHORD BS 284 TO BS 350 RT, RBL 17, WL 149 IAW FED-EX DRAWING 65-18415 SHT 2. 2 L 7 3 4F A3WE 1998011500226 19980115 00226 NM 1998 1 15 98FDEA00018 1 19980108 A 5320 65198613 ANGLE BOEING 727 72722 1384002 NM BS 336 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 NR 0329 004, CORROSION C53-111-03-1/2 ON LT LOWER NOSE CHORD BS 336 TO 350, LBL 17, WL 149. FOUND CORROSION ON LT LOWER NOSE ANGLE BS 336 TO 350, LBL 17, WL 149 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-01. REMOVED AND REPLACED ANGLE BS 28 4 TO BS 350, LBL 17, WL 149 IAW FED-EX DRAWING 65-18415 SHT 2. STORED AIRCRAFT PER FED-EX EA 7-5100-37391. 2 L 7 3 4F A3WE 1998011500227 19980115 00227 NM 1998 1 15 98FDEA00019 1 19980109 A 3260 GEAR INDICATION BOEING 727 72725C 138400H NM LANDING GEAR MALFUNCTION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 127FE 19719 98-0014 - AFTER TAKEOFF WITH GEAR HANDLE UP ALL 3 LANDING GEAR UNSAFE AND DOOR LIGHTS ON FWD PANEL WERE ON WHILE ONLY TH E TAIL SKID LIGHT WAS ON AT THE SECOND OFFICER'S PANEL. FOLLOWED THE RED TABS, RECYCLED THE LANDING GEAR AND ALL LIGHTS WENT OUT. CHECK TAIL SKID SWITCH AND GEAR LIGHTS WORKS OK ON GROUND, COULD NOT DUPLICATE PROBLEM ON GROUND. AIRCRAFT OK FOR SERVICE. 2 L 7 3 4F A3WE 1998011500228 19980115 00228 WP 1998 1 15 MWEA98896 1 19980108 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 501ME 47132 GALLEY DOOR SLIDE FELL OFF. MAINTENANCE RESECURED SLIDE ASSEMBLY TO DOOR. 2 L 7 2 4F A6WE 1998011500229 19980115 00229 NM 1998 1 15 DL72S980034 1 19980106 A 7110 SKIN BOEING 727 727232 1384082 NM NR 2 ENG INLET CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 .5 INCH CRACK EXTENDING FROM NR 2 ENG DUCT HOUSING ACCESS PANEL 9524R. REPAIRED PER MM 54-30-0 P 803. 2 L 7 3 4F A3WE 1998011500230 19980115 00230 NM 1998 1 15 DL76L980035 1 19980106 A 2781 INDICATION BOEING 767 767332 1382001 NM LE SLAT MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 179DN 25144 AT FL350, LEADING EDGE SLAT ASSY LIGHT CAME ON. FLAP IND SHOWED HALFWAY BETWEEN UP AND 1. LIGHT CAME ON 4 OR 5 TIMES. AFTER SLOWING AND GOING TO FL260, NO FURTHER INDICATIONS CAME ON. DIVERTED TO JFK. INDICATION REOCCURRED ON DESCENT. 2 L 7 2 4F RT A1NM 1998011500231 19980115 00231 NM 1998 1 15 DLM90980036 1 19980106 A 2450 RELAY 5D03541 DOUG MD90 MD9030 3023690 NM E/E COMPT FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 906DA 53386 SHORTLY AFTER T/O, EMERGENCY PWR IN USE LIGHT CAME ON. CAPT PFD FAILED. LATER ACS FAULT MSG IN OAP. RETURNED TO ABQ. REMOVED AND REPLACED RELAY R2-47. 2 L 7 2 4F RT A6WE 1998011500232 19980115 00232 NM 1998 1 15 DL73E980037 1 19980106 A 5330 6545775581 SKIN BOEING 737 7372S3 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 FUSELAGE/SKIN, FS 727A-727B, S-16R-17R, REPAIRED FOR SKIN CRACKS. THE FUSELAGE SKIN BETWEEN FS 727A AND 727B AND BETWEE N STRINGER 16R AND 17R WAS FOUND WITH A 3.25 LONG CRACK AND A 2.25 LONG CRACK. THE CRACKS WERE CUT OUT AND A REPAIR DOU BLER WAS INSTALLED PER ER/A 363613-14, REV A. 2 L 7 2 4F RT A16WE 1998011500233 19980115 00233 NM 1998 1 15 DLM88980039 1 19980107 A 4990 OIL SYST DOUG MD88 MD88 3023688 NM APU LEAKING A DALA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SO 27 947DL 49878 WHEN WING ANTI-ICE WAS TURNED ON CABIN TEMP, IT GOT VERY HOT WITH AN ACCOMPANYING SMELL, ALSO SMOKE (LIGHT) THROUGHOUT C ABIN WHICH ACTIVATED SMOKE ALARM IN REAR LAV. FOUND APU LEAKING OIL INTO APU. CORRECTED LEAK, PERFORMED BURNOUT. 2 L 7 2 4F RT A6WE 1998011500234 19980115 00234 NM 1998 1 15 DL76L980040 1 19980107 A 3350 FUSE BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DN 24759 EMERGENCY TRACK LIGHTS INOP ROWS 23 -27. REPLACED FUSES, SYSTEM OPS CHECK GOOD. 2 L 7 2 4F RT A1NM 1998011500235 19980115 00235 NE 1998 1 15 DLL17980041 2 19980107 A 7260 BEARING LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 1 ENGINE OIL LEAK A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 769DL 56361 193H1218 14763 NR 1 ENGINE OIL QTY PROGRESSIVELY DROPPED UNTIL REACHING ZERO AFTER 4 HOURS OF FLIGHT, WITH QTY AT ZERO, TEMP AND PRESS AT 104 DEG AND 62 PSI AND STEADY. REPLACED REAR BEARING COVER AND GASKETS. NO LEAKS. 2 L 7 3 4F 4 F A23WE E12EU 1998011500236 19980115 00236 NM 1998 1 15 DL72L980043 1 19980107 A 3350 900542 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 513DA 21315 RT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED OVERWING EMERGENCY EXIT LIGHT BASE. 2 L 7 3 4F A3WE 1998011500237 19980115 00237 NM 1998 1 15 DL72S980044 1 19980107 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 545DA 22494 AFT EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998011500239 19980115 00239 NM 1998 1 15 DL72K980046 1 19980107 A 2910 307031S58D QUICK DISCONNECT BOEING 727 727232 1384082 NM B-HYD SYST LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 471DA 20748 IN FLIGHT SYSTEM 'B' HYDRAULIC FAILURE AT 10,000 FT. TOTAL LOSS OF SYSTEM 'B' FLUID. AIRBORNE DIVERT TO IAD. REPLACED QUICK DISCONNECT 'B' RES TO PRESSURE SIDE OF PUMP HYD FITTING. SVC SYS PER SRM 2-29-88, LEAK CHECK PER MM 11-25-83 LEA K CHECK GOOD. 2 L 7 3 4F A3WE 1998011500247 19980115 00247 NM 1998 1 15 P5CA9800008 1 19980105 A 5244 HINGE BOEING 747 747122 1384872 NM ACM DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 1 ACM DOOR PANEL 191A HINGES HAVE LIGHT CORROSION. REMOVED CORROSION IAW SRM 51-10-06. TREATED AND PRIMED IAW SRM 5 1-10-02. 2 L 7 4 4F A20WE 1998011500248 19980115 00248 NM 1998 1 15 P5CA9800009 1 19980105 A 5280 SKIN BOEING 747 747122 1384872 NM LT MLG DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 LBG O/B DOOR INNER SKIN BULGED AT AFT EDGE. REMOVED CORROSION AND REPAIRED PER SRM 51-10-03 FABRICATED DOUBLER PER SRM 52-80-02. 2 L 7 4 4F A20WE 1998011500249 19980115 00249 WP 1998 1 15 RRXA98002 1 19980108 A 5230 VENT DOUG DC8 DC862F 3021972 WP CARGO DOOR OPEN A RRXA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 WP 15 998CF 46139 LOUD EXPLOSION, DECOMPRESSION AT APROX 29,000FT, CARGO VENT DOOR WARNING LIGHT ON. VISUAL ON GROUND, THE CABIN VENT DOO R WAS FULL OPEN. FOUND VENT DOOR MANUAL HANDLE IMPROPERLY STOWED, ALLOWING LINKAGE TO RELEASE UNDER PRESSURIZATION. I NSPECTED AND OPERATED MECHANISM AND STOWED HANDLE PROPERLY. DOOR SECURE AND OPS CKS GOOD MANUALLY IAW NATIONAL AIRCRAF T SERVICE VENT DOOR MAINTENANCE MANUAL. CARGO DOOR VENT DOOR ELECTRICAL FUNCTION INOP IN OPENING POSITION. TRANSFERRED TO DMI LOG NR 801040 IAW EWA MEL 52-7 CAT B PLACARD INSTALLED. 2 L 7 4 4F 4A25 1998011500250 19980115 00250 WP 1998 1 15 RRXA98003 1 19980109 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 3-13 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8091U 45995 WHILE AIRCRAFT SAT ON GROUND AT KMCN, JET BLAST FROM OTHER AIRCRAFT BLOW PASSENGERS STAIR INTO LT WING LEADING EDGE. PA SSENGERS STAIR DAMAGED LT WING LEADING EDGE AT STA XFS=13 TO 3.0. REMOVED DAMAGED SECTION FROM LEADING EDGE, DAMAGE EXC EEDED LIMITATIONS IAW DC-8 SRM CHAPTER 57. REPAIRED LT WING LEADING EDGE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D76-R01 AND DC-8 SRM 51-1-12 AND 51-1-21. 2 L 7 4 4F RT 4A25 1998011500251 19980115 00251 1998 1 15 VNAA9801003 4 19980108 A 3442 7008470822 RADAR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT DEFECTIVE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 434JS 4656 3100 3051 AFTER TAKEOFF, CREW RECEIVED A WEATHER RADAR FAIL MESSAGE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND RADAR UNIT DEFECTIVE. REPLACED UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-4 1-00. OPERATIONAL CHECK GOOD AND AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998011500350 19980115 00350 NE 1998 1 15 VJ9800004 2 19980109 A 7314 371900 FUEL PUMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE RT ENGINE FAILED A VJ6A E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SO 11 916VV 47445 ON DESCENT AT FL80, AIRSPEED AT 250 KTS, THROTTLES AT IDLE AND N2 AT 20 PERCENT, RT ENGINE FLAMED OUT. REPLACED NR 2 E NGINE FUEL PUMP IAW MM 73-10-1; RAN ENGINE, OPS AND LEAK CHECKED GOOD. OBSERVATIONS ARE A SHEARED SHAFT IN FUEL PUMP. 2 L 7 2 4F 4 F A6WE E2EA 1998011500351 19980115 00351 1998 1 15 VJ9800005 4 19980111 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR LOW PRESSURE A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 907VJ 47444 GALLEY DOOR EMERGENCY SLIDE PRESSURE INDICATES LOW. REPLACED R1 DOOR SLIDE IAW MM 25-60 AND PERFORMED REQUIRED INSPECTI ONS. 2 L 7 2 4F A6WE 1998011500352 19980115 00352 NM 1998 1 15 AWXA9800003 1 19980106 A 3397 WIRE BOEING 737 737297 1384480 NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 147AW 22630 SEAT 1L EMERGENCY LIGHT INOP. RECONNECTED WIRE HARNESS, OPS GOOD. STC NR SA3432NM 2 L 7 2 4F A16WE 1998011500356 19980115 00356 NM 1998 1 15 AWXA9800009 1 19980107 A 3350 849029 BATTERY PACK BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 905AW 23567 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP. REPLACED SEVERAL EMERGENCY LIGHT BATTERY PACKS. 2 L 7 2 4F RT A2NM 1998011500358 19980115 00358 EU 1998 1 15 AWXA9800011 1 19980107 A 2913 4205400 HYD PUMP AIRBUS 320 A320231 3930325 EU LT ENGINE FAILED A AWXA O OTHER J WARNING INDICATION UK UNKNOWN 1 WP 28 631AW 609 077 A/C ARRIVED W/A TOTAL GREEN HYD SYSTEM FAILURE. REMOVED FROM SERVICE TO REPLACE LT ENG HYD PUMP AND MLG PRIORITY VALVE. EMERGENCY WAS DECLARED. 2 L 7 2 4F RT A28NM 1998011500359 19980115 00359 NM 1998 1 15 AWXA9800012 1 19980108 A 3397 WIRE BOEING 757 7572G7 1384963 NM CABIN DISCONNECTED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX LIGHTS INOP AT 15L, 20L, AND 21L. REPAIRED AND RECONNECTED LIGHT WIR ING. 2 L 7 2 4F RT A2NM 1998011500360 19980115 00360 NM 1998 1 15 CALA9800011 1 19980111 A 3297 WIRE BOEING 727 727232 1384082 NM NLG SENSOR BROKEN A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 511PE 20634 THE AIRCRAFT HAD A BRIEF HISTORY OF THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATING INTERMITTENTLY IN FLIGHT AND WHEN GEAR W AS EXTENDED FOR LANDING. MAINTENANCE FOUND A BROKEN WIRE AT NOSE GEAR POSITION SENSOR. THE SENSOR WIRE WAS REPAIRED. O PERATION AND INDICATIONS CHECKED GOOD. 2 L 7 3 4F A3WE 1998011500361 19980115 00361 NM 1998 1 15 CALA9800012 1 19980110 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16784 20639 INSPECTION FOUND CABIN AISLE OVERHEAD EMERGENCY LIGHT AT ROW 2 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1998011500362 19980115 00362 WP 1998 1 15 CALA9800013 1 19980110 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 936AS 49363 PULL FROM THE TAIL CONE INTERIOR RELEASE HANDLE WAS EXCESSIVE AT 40 POUNDS. THE LATCH CABLES WERE RIGGED IAW MM 53-53-0 0. 2 L 7 2 4F A6WE 1998011500363 19980115 00363 WP 1998 1 15 CALA9800014 1 19980110 A 5320 BRACKET DOUG DC9 DC982 3022082 WP CARGO COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 936AS 49363 INSPECTION FOUND BRACKET ANGLE CRACKED IN MID BAG BIN ABOVE LT OUTBOARD FORWARD CORNER OF FUEL TANK. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998011500364 19980115 00364 NM 1998 1 15 UPS98225394 1 19980108 A 3350 LIGHT BOEING 727 72751C 1384015 NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE-N/A, COCKPIT EMER EXIT LT WILL NOT EXT WHEN POWER IS TURNED OFF WITH LTS OFF. REMOVED AND REPLACED EMER EXIT LIGHT ASSY, OPS NORMAL (S/N 4249) ON, (S/N 5538) OFF. 2 L 7 3 4F A3WE 1998011500365 19980115 00365 NM 1998 1 15 UPS98225395 1 19980108 A 3350 LIGHT BOEING 727 72725C 138400H NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION TYPE-N/A, COCKPIT EXIT LIGHT CAME ON AFTER LANDING WITH SWITCH IN OFF. SECURED COCKPIT EMER EXIT LIGHT, OPER ATION OK. 2 L 7 3 4F A3WE 1998011500366 19980115 00366 EU 1998 1 15 QXEA9800014 1 19980107 A 3350 5515900004 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 PDX- EMERGENCY EXIT SIGN AT THE FRONT OF THE PASSENGER CABIN IS OUT. REPLACED EMERGENCY EXIT SIGN CIRCUIT BOARD, OPERAT IONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998011500367 19980115 00367 EU 1998 1 15 QXEA9800015 1 19980107 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 GEG- DURING INSPECTION, SEVERAL OVERHEAD EVACUATION LIGHTS WERE NOTICED TO BE INOP. RELAMPED EFFECTED LIGHTS, OPERATION AL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998011500368 19980115 00368 NM 1998 1 15 98FDEA00021 1 19980109 A 2612 B-LOOP BOEING 727 727233 138408A NM NR 2 ENGINE INOPERATIVE A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 220FE 20934 NR 2 ENGINE FIRE DETECTION LIGHT ILLUMINATED IN FLIGHT ACCOMPLISHED RED TAB PROCEDURES AND LIGHT REMAINED ON. GOOD FIRE PROTECTION VERIFIED THROUGH RED TABS AND MINIMUM EQUIPMENT LIST (WARNING, FIRE WARNING TEST GOOD). IDENTIFY B-LOOP INO PERATIVE NR 2 ENGINE. PULL B-LOOP CIRCUIT BREAKER. SELECTED A-LOOP ON PANEL OK TO CONTINUE PER MINIMUM EQUIPMENT LIST 26-6B, CONTROL. NR 28206 CAT C ITEM EXPIRES 19JAN98. 2 L 7 3 4F RT A3WE 1998011500369 19980115 00369 NM 1998 1 15 98FDEA00022 1 19980109 A 5315 FLOORBEAM BOEING 727 7272S2F 1384O81 NM BS 880 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 212FE 22934 FLOORBEAM UPPER CHORD FWD SIDE LWR SURFACE GOUGED BS 880 RBL 55 WL 208. BLENDED OUT GOUGE, FABRICATED REPAIR STRAP FROM .071 7075-T6. INSTALLED STRAP PER AMERICAN AIRLINES REPAIR 53-10-07-2 FIG 1 3/20/96. 2 L 7 3 4F A3WE 1998011500370 19980115 00370 WP 1998 1 15 9800002 1 19980109 A 5753 99575791 SKIN DOUG DOUG DC9 DC941 302207N WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND THE LT FLAP LOWER SURFACE SKIN AT STA XRS 137 CORRODED. REPLACED SKIN IAW DC9 SRM 51-30-1, 51-30- 3, 51-10-4. 2 L 7 2 4F A6WE 1998011500371 19980115 00371 WP 1998 1 15 9800003 1 19980109 A 5320 99101515 CUSP WEB DOUG DOUG DC9 DC941 302207N WP BS 640 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND THE LT CUSP WEB CRACKED AT A LIGHTENING HOLE AT STA 640. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998011500372 19980115 00372 WP 1998 1 15 9800004 1 19980109 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND LONGERON 17L CRACKED AT THE FRAME ATTACH BOLTS STA 1056. REPLACED LONGERON FROM STA 1036 TO 1072 DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998011500373 19980115 00373 WP 1998 1 15 9800005 1 19980109 A 5313 59114277 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STA 1041. REPAIRED LONGERON DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998011500374 19980115 00374 WP 1998 1 15 9800006 1 19980109 A 5320 99577397 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1024 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND 2 SHEAR TIES CRACKED AT STA 1024 BETWEEN LONGERONS 14R AND 15R AND BETWEEN 15R AND 16R. REPLACED SHEAR TIES IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998011500375 19980115 00375 WP 1998 1 15 9800007 1 19980109 A 5320 3957174503 FITTING DOUG DOUG DC9 DC941 302207N WP BS 1153 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE VENTRAL STAIR DOOR JAMB FITTING ON THE RT SIDE AT STA 1153 CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998011500376 19980115 00376 WP 1998 1 15 9800008 1 19980109 A 5320 99118605 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1185 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND AFT ACCESSORY COMPARTMENT FRAME STA 1185 SHEAR TIE JUST LT OF LONGERON 1 CRACKED, 8 INCHES LON G. REPLACED SHEAR TIE. 2 L 7 2 4F A6WE 1998011500377 19980115 00377 WP 1998 1 15 9800009 1 19980109 A 5311 99577411 FRAME DOUG DOUG DC9 DC941 302207N WP BS 577 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND FRAME AT STA 577 CORRODED JUST OUTBD OF LONGERON 27R. REPLACED FRAME IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998011500378 19980115 00378 WP 1998 1 15 9800010 1 19980109 A 5730 59127372 PANEL DOUG DOUG DC9 DC941 302207N WP WS 353-445 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE RT WING TRAILING EDGE HONEYCOMB PANEL BETWEEN STA XRS 353 TO 445 LOWER SURFACE CORRODED FI VE PLACES AT THE TRAILING EDGE OF THE PANEL AND BULGED AROUND SEVERAL FASTENER HOLES ON THE UPPER SURFACE. REPLACED TRA ILING EDGE PANEL IAW DC9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1998011500379 19980115 00379 WP 1998 1 15 9800011 1 19980109 A 5311 591359615 FORMER DOUG DOUG DC9 DC941 302207N WP BS 1132 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND A FORMER AT STA 1132 BULGED AND CRACKED BETWEEN LONGERONS 13R AND 14R. REPAIRED FORMER IAW DC 9 SRM 53-03. 2 L 7 2 4F A6WE 1998011500380 19980115 00380 WP 1998 1 15 9800012 1 19980109 A 5743 5924841501 FITTING DOUG DOUG DC9 DC941 302207N WP LT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47499 DURING MOD/D-CHECK, FOUND THE LT MLG TRUNNION FITTING CORRODED BEYOND LIMITS AT THE LOWER OUTBD FLANGE AND THE SIDE BRAC E ATTACH LUG. REPLACED TRUNNION FITTING IAW ABX EA 57430025003. 2 L 7 2 4F A6WE 1998011500382 19980115 00382 NM 1998 1 15 DLM88980047 1 19980108 A 2910 290051518 HYD LINE DOUG MD88 MD88 3023688 NM LT TR UNIT RUPTURED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 933DL 49720 APU AIR CONDITIONING PUTS SMOKE IN CABIN. FOUND RUPTURED LEFT THRUST REVERSER HYD PRESS LINE. 2 L 7 2 4F RT A6WE 1998011500383 19980115 00383 NM 1998 1 15 DL72K980049 1 19980108 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 491DA WA7734 21060 RT WING FWD EMERGENCY EXTERIOR LIGHT INOP. REPLACED PWR SUPPLY AND BATTERY PACK CKS GOOD. 2 L 7 3 4F A3WE 1998011500384 19980115 00384 NM 1998 1 15 DLM11980057 1 19980108 A 3350 BATTERY PACK 5519881 DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 804DE 48475 BATTERY PACKS NR 5 AND 6 FAILED EMER LTS TEST: FAIL MSGS WERE BATT NR 5 LO AND BATT NR 6 LO. REPLACED BOTH BATTERY PACK S IN NR 5 AND 6 CHARGERS, OPERATION NORMAL. 2 L 7 3 4F RT A22WE 1998011500386 19980115 00386 NM 1998 1 15 DL72W980059 1 19980106 A 5753 SKIN BOEING 727 727247 138408F NM NR 1 TE MID FLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 LEADING EDGE SKIN WORN 60 FROM O/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 803. 2 L 7 3 4F A3WE 1998011500387 19980115 00387 NM 1998 1 15 DLM88980060 1 19980109 A 3350 CONNECTOR RPS1B DOUG MD88 MD88 3023688 NM CABIN LOOSE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 934DL 49721 EMERGENCY TRACK LIGHTS INOP FROM SEAT 4C TO SEAT 15D. RESEATED CONNECTOR ON POWER SUPPLY, CKS GOOD. 2 L 7 2 4F RT A6WE 1998011500388 19980115 00388 NM 1998 1 15 DL72W980061 1 19980106 A 5313 STRINGER BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 AT HMV, FOUND STRINGER CRACKED INSIDE ACCESS 9504 ON RT SIDE 4TH BAY UP. FAB NEW REPAIR PER MM 55-30-00, INSTALLED PER MM 55-30-00 FIG 803. 2 L 7 3 4F A3WE 1998011500390 19980115 00390 NM 1998 1 15 DL72S980063 1 19980107 A 5754 SKIN BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 NUMBER 4 L/E SLAT HAD A CRACK FROM THE FENCE MOUNTING BOLT HOLE. INSTALLED A REPAIR DOUBLER PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998011500391 19980115 00391 NM 1998 1 15 DL72K980064 1 19980109 A 7120 BACN10JC12 NUT BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MISSING A A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 700190 FOUND DURING C-1 CHECK, UPPER ENGINE MOUNT CONE BOLT NUT MISSING AND BOLT BACKED OUT ABOUT .25 INCH. LOWER ENGINE MOUNT CONE BOLT NUT LOOSE, NO TORQUE STRIPS. DROPPED ENGINE AND REPLACED CONE BOLTS REF TRANS 4T216, OPN 5130, ERA 279520-14 , SI 4-72242-12. 2 L 7 3 4F 4 F A3WE E2EA 1998011500392 19980115 00392 NM 1998 1 15 DL72S980065 1 19980109 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA 20746 EMERGENCY LIGHTS INOP AT SEVERAL LOCATIONS IN CABIN. REPLACED 3 BATTERY PACKS, OPN NOW NORMAL. 2 L 7 3 4F A3WE 1998011500393 19980115 00393 NM 1998 1 15 DL72K980067 1 19980109 A 3350 3114981 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 472DA 20749 ON L/O, FOUND LT FWD ENTRY DOOR EXTERIOR EMERGENCY LIGHT OUT. REPLACED LIGHT ASSY, OPS CK GOOD. 2 L 7 3 4F A3WE 1998011500394 19980115 00394 NE 1998 1 15 DL72W980068 2 19980109 A 7200 ENGINE BOEING 727 727247 138408F NM PWA JT8 JT8D9A 52048 NE NR 1/2 BIRD STRIKE A DALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 2809W 20581 AIRCRAFT FLEW THROUGH FLOCK OF GEESE. NR 1 AND 2 ENGINES WILL BE REPLACED. NR 3 WILL BE BORESCOPED. NR 6 SLAT WILL BE REPLACED. RADOME AND RADAR ANTENNA WILL BE REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1998011500395 19980115 00395 NM 1998 1 15 DL76S980069 1 19980110 A 3350 LIGHT 1317 BOEING 767 767332 1382001 NM LT OVERWING INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 119DL 23278 FOUND ON LAYOVER, LT OVERWING EMERGENCY LIGHTS INOP. RELAMPED, CHECKS GOOD. 2 L 7 2 4F RT A1NM 1998011500396 19980115 00396 NM 1998 1 15 DL76S980070 1 19980110 A 3350 STRIP BOEING 767 767332 1382001 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 136DL 23146 WKG MCO-CLOSET 2L EMER TRACK LIGHTING STRIP DAMAGED. REPLACED STRIP, OPS CK NRML. REMOVED MCO. 2 L 7 2 4F RT A1NM 1998011500397 19980115 00397 WP 1998 1 15 ARWA980102 1 19980105 A 7110 5757519501 COWL DOUG DC8 DC862 3021970 WP NR 4 ENGINE MISSING A ARWA O OTHER D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 19 1808E 46105 ON POST FLIGHT, FOUND NR 4 ENGINE OUTBOARD AFT COWL MISSING. REMOVED AND REPLACED NR 4 OUTBOARD COWLING FOR A NEW ONE IAW 71-00-00. ALSO INSPECTED NR 4 ENGINE AND OUTBOARD RIGHT WING, NO DAMAGE NOTED. 2 L 7 4 4F 4A25 1998011500421 19980115 00421 NE 1998 1 15 98ZZZX196 2 19980107 A 8530 114652 CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE NR 7 EXH PORT CRACKED A VLLA O OTHER E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 GL 05 932H 34368 CP352830 ENGINE STARTED RUNNING ROUGH. FOUND NR 7 CYLINDER EXHAUST PORT CRACKED ON CYLINDER HEAD. 2 L 7 2 4R 4 R A669 5E4 1998011500436 19980115 00436 EU 1998 1 15 MALA975872 1 19980111 A 3610 321935 HP SHUTOFF VALVE SAAB SF340 SF340A 7850100 EU RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 115XJ 340A115 DURING FLIGHT THE LEFT BLEED CLOSED AND LEFT BLEED FAULT LIGHT MOMENTARILY ILLUMINATED WITH MASTER CAUTION, TRIED TO CON TROL LEFT BLEED WITH MANUAL CONTROL, UNABLE TO. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT HIGH PRESSURE BLEED SHUT OFF VALVE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998011500437 19980115 00437 NM 1998 1 15 MALA975873 1 19980107 A 3350 10126271 LENS DHAV DHC8 DHC8102 2809003 NM CABIN MISSING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 833MA 343 DURING INSPECTION, TWO EMERGENCY LIGHTS INOP AND AN EMERGENCY EXIT LIGHT COVER IS MISSING BY PASSENGER STAIRS. MAINTENA NCE RELAMPED EMERGENCY LIGHTS (PN MS25231-316) AND REPLACED EXIT SIGN WITH A NEW LENS, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998011500438 19980115 00438 NM 1998 1 15 MALA975874 1 19980110 A 3350 1013075 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 861MA 362 DURING INSPECTION, ONE RED FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998011500439 19980115 00439 NM 1998 1 15 MALA975875 1 19980110 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 830MA 337 DURING INSPECTION, ONE FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998011500441 19980115 00441 NM 1998 1 15 MALA975877 1 19980109 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 861MA 362 DURING INSPECTION, ALL EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED ALL SIX BATTERY PACKS, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998011500442 19980115 00442 NM 1998 1 15 MALA975878 1 19980108 A 3350 MS25231316 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 846MA 344 DURING INSPECTION, FORWARD OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED OVERHEAD LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998011500443 19980115 00443 EU 1998 1 15 MALA975879 1 19980107 A 2611 SMOKE DETECTOR BAC 146 AVRO146RJ85A 1500097 EU LAVATORY DIRTY A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 508XJ E2317 DURING INSPECTION, THE BACK LAVATORY SMOKE DETECTOR WILL NOT TEST. MAINTENANCE DEFERRED SMOKE DETECTOR, UPON CLEARING D EFERRAL MAINTENANCE TESTED SYSTEM AND COULD NOT DUPLICATE WRITE UP. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998011500444 19980115 00444 EU 1998 1 15 MALA975880 1 19980107 A 2611 72130003001 SMOKE DETECTOR BAC 146 AVRO146RJ85A 1500097 EU E/E COMPT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 501XJ E2208 DURING INSPECTION, THE ELECTRICAL SMOKE WARNING DOES NOT TEST. MAINTENANCE REPLACED THE ELECTRICAL SMOKE DETECTOR, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998011500445 19980115 00445 NM 1998 1 15 MALA975881 1 19980109 A 3260 864202 WOW SENSOR DHAV DHC8 DHC8102 2809003 NM NLG FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 826MA 330 AFTER TAKEOFF, THE WEIGHT ON WHEELS LIGHT STAYED ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NOSE LANDING GEAR RIGHT WOW SENSOR TARGET AND HT RIGHT MAIN LANDING GEAR LEFT WOW SENSOR. COMPLETED GEAR SWINGS AND OPS CHEC KS GOOD. 2 H 7 2 4T RT A13NM 1998011500446 19980115 00446 1998 1 15 MALA975883 4 19980109 A 2350 517019 REU SAAB SF340 340B 7860101 EU RT COCKPIT INTERNAL FAULT A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 422XJ 422 AFTER TAKEOFF, THE FO'S AUDIO PANEL IS INOP. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE REU, SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998011500447 19980115 00447 NM 1998 1 15 W8PA980008 1 19980110 A 2822 CIRCUIT BREAKER BOEING 737 737301 1384611 NM BOOST PUMP TRIPPED A W8PA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 950WP 23229 FUEL BOOST PUMP CIRCUIT BREAKER TRIPPED AFTER TAKEOFF. RETURNED TO DEN WITHOUT INCIDENT. 2 L 7 2 4F RT A16WE 1998011500449 19980115 00449 WP 1998 1 15 9800421154 1 19980107 A 7930 BYPASS SWITCH DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 ENGINE FAILED A NWAA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 01 154US 46763 686148 DURING CLIMBOUT, THE NR 1 ENGINE OIL FILTER BYPASS WARNING LIGHT ILLUMINATED FOR ONE MINUTE. ALL OTHER INDICATIONS WERE NORMAL AND THE LIGHT EXTINGUISHED WITH NO ACTION. DURING DESCENT INTO MSP, THE LIGHT ILLUMINATED AGAIN AND THE CREW SH UT DOWN THE NR 1 ENGINE. THE REMAINDER OF THE FLIGHT WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN ENG INE OIL FILTER AND THE FILTER BYPASS PRESSURE SWITCH. ENGINE RUN WAS NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1998011500450 19980115 00450 WP 1998 1 15 9800439871 1 19980108 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 780NC 48102 DURING LINE CHECK, FOUND CEILING EMERGENCY EXIT LIGHT INOPERATIVE AT SEAT ROW 21R. MAINTENANCE REPLACED POWER SUPPLY, O PERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998011500451 19980115 00451 WP 1998 1 15 9800449941 1 19980108 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3324L 47103 DURING LINE CHECK, FOUND LEFT AND RIGHT SIDE EMERGENCY EXIT LIGHTS DIM. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHE CK OK. 2 L 7 2 4F A6WE 1998011500452 19980115 00452 WP 1998 1 15 9800459921 1 19980108 A 3230 BYPASS ACTUATOR DOUG DC9 DC932 3022066 WP NLG BROKEN A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 943N 47459 DURING CLIMBOUT, A LOUD THUMP WAS EMITTED FROM NOSE WHEEL AREA FOLLOWED BY A CONTINUOUS VIBRATION. NOSE AND VIBRATION R EDUCED UPON LANDING GEAR EXTENSION. AIRCRAFT RETURNED TO ORIGINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BYPASS HANDLE ACTUATOR, LEFT NOSE LANDING GEAR DOOR, CABLE, AND SPRING, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500453 19980115 00453 WP 1998 1 15 9800469903 1 19980109 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE SPRUNG A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT INSUFFICIENT FORCE WAS REQUIRED TO REMOVE INTERIOR HANDLE. REPLACED HANDL E CLIPS, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998011500470 19980115 00470 WP 1998 1 15 9800479957 1 19980108 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 747-755 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CORROSION LONGERON 30L END FITTING FS 747 TO 755. REPLACED FITTING (P/N 3915135-515N) PER SRM 51- 01. 2 L 7 2 4F A6WE 1998011500471 19980115 00471 WP 1998 1 15 9800489957 1 19980108 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 749 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CORROSION ON LONGERON 29R END FITTING FS 749. REPLACED FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1998011500472 19980115 00472 WP 1998 1 15 9800499885 1 19980108 A 5311 FRAME DOUG DC9 DC951 3022051 WP BS 1275 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 401EA 47682 DURING H-CHECK, FOUND A CRACK IN THE FRAME CAP WHERE IT ATTACHES TO LONGERON 4R FS 1275. REPAIRED PER EA 98-153443. 2 L 7 2 4F RT A6WE 1998011500473 19980115 00473 WP 1998 1 15 9800509921 1 19980107 A 5320 PRESS PANEL DOUG DC9 DC932 3022066 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING L-CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL ON RIGHT SIDE AT FS 83. REP AIRED PER EA 99-153449. 2 L 7 2 4F A6WE 1998011500474 19980115 00474 WP 1998 1 15 9800519921 1 19980107 A 5320 PRESS PANEL DOUG DC9 DC932 3022066 WP BS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 47647 DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT LEFT OUTBOARD VERTICAL SUPPORT FS 105. REPAIRED EA 99-153448. 2 L 7 2 4F A6WE 1998011500475 19980115 00475 SO 1998 1 15 COMA9810018 1 19980108 A 3230 12041912001 SHUT OFF VALVE EMB 120 EMB120RT SO NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 257CA 120248 THE NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE NLG HYDRAULIC SOV. 2 L 7 2 4T RT A31SO 1998011500476 19980115 00476 SO 1998 1 15 COMA9810019 1 19980109 A 3230 2072500001 DOWNLOCK ACT ERAM 1973000015 EMB 120 EMB120RT SO NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 257CA 13255 287 120248 AFTER DEPARTURE, THE NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE AIRPORT. REPLACED THE DOWNLOCK ACTUATOR. 2 L 7 2 4T RT A31SO 1998011500477 19980115 00477 SO 1998 1 15 COMA9810020 1 19980110 A 3230 RETRACT MECH EMB 120 EMB120RT SO NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 257CA 120248 NOSE GEAR WOULD NOT RETRACT AFTER T/O. RECYCLED, NO LUCK. ALL RED AND GREEN LIGHTS ON N/G WERE ON WITH HANDLE IN UP PO SITION. ALL GEAR LOCKED DOWN NORMAL WITH HANDLE DOWN. FERRIED FROM MDW TO CVG WHERE LANDING GEAR SOLENOID VALVE, NOSE GEAR RESTRICTOR VALVE AND NOSE GEAR SEQUENCE VALVES WERE CHANGED RESULTING IN NORMAL OPERATIONAL CHECKS ON JACKS. SOLEN OID VALVE (S/N 738) TT 15662. RESTRICTOR VALVE (S/N 425) TT 15662. SEQUENCE VALVES (S/N 1738) TT 15662. SEQUENCE VALV ES (S/N 1540) TT 14239. 2 L 7 2 4T RT A31SO 1998011500478 19980115 00478 EA 1998 1 15 COMA9860007 1 19980111 A 3250 TRANSFORMER CNDAIR CL600 CL6002B19 EA E/E COMPT OUT OF ADJUST A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 943CA 7062 UPON GEAR EXTENSION, RECEIVED STEERING CAUTION MESSAGE. ADJUSTED THE ROTARY VARIABLE DIFFERENTIAL TRANSFORMER. 2 L 7 2 4F RT A21EA 1998011500479 19980115 00479 EA 1998 1 15 COMA9860008 1 19980112 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 951CA 5738 7091 FLAP FAIL CAUTION MESSAGE ACTIVATED DURING CRUISE FLIGHT. REPLACED THE LEFT FLAP BRAKE AND POSITION SENSOR UNIT. 2 L 7 2 4F RT A21EA 1998011500480 19980115 00480 EA 1998 1 15 COMA9860009 1 19980107 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT/RT TE FLAP MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 979CA 2201 7159 FLAP FAIL CAUTION MESSAGE DURING FLIGHT. REPLACED THE LEFT AND RIGHT BPSU. 2 L 7 2 4F RT A21EA 1998011500481 19980115 00481 EA 1998 1 15 COMA9860010 1 19980107 A 3020 12681 PRESS SW CNDAIR CL600 CL6002B19 EA LT ENGINE FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 940CA 10737 7048 LEFT ENGINE COWL ANTI-ICE CAUTION WARNING 5 MINUTES AFTER TAKEOFF. REPLACED THE LEFT ENGINE COWL ANTI-ICE PRESSURE SWIT CH. 2 L 7 2 4F RT A21EA 1998011500482 19980115 00482 1998 1 15 SWAA980004 4 19980105 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM ENTRY DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 627SW 27935 AT GATE, FWD ENTRY DOOR ESCAPE SLIDE ACCIDENTALLY DEPLOYED. REPLACED SLIDE ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998011500483 19980115 00483 NM 1998 1 15 SWAA980005 1 19980103 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FWD LT EMERGENCY FLASHLIGHT INOP. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1998011500484 19980115 00484 NM 1998 1 15 SWAA980006 1 19980103 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 911-913 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 911 TO 913 JUST BELOW S23L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998011500485 19980115 00485 1998 1 15 SWAA980007 4 19980107 A 2565 1061323649 SLIDE BOEING 737 7373A4 1384585 NM AFT ENTRY LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED A1, FOUND AFT ENTRY EMERGENCY SLIDE PRESSURE BELOW SERVICEABLE LIMIT. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998011500486 19980115 00486 NM 1998 1 15 SWAA980008 1 19980107 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED BELOW FASTENER AT WL 234, LBL 15.5 AND AT RBL 9.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500487 19980115 00487 NM 1998 1 15 SWAA980009 1 19980107 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 494 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER 22R CRACKED AT BS 494. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500488 19980115 00488 NM 1998 1 15 SWAA980010 1 19980107 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND MULTIPLE DENTS IN FUSELAGE FRAME AT BS 500. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500489 19980115 00489 NM 1998 1 15 SWAA980011 1 19980107 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 500 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME AT BS 500A GOUGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500490 19980115 00490 NM 1998 1 15 SWAA980012 1 19980107 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 520/500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIPS CRACKED AT BS 360, S9L, AT BS 520, S19L AT BS 294, LBL 52, AT BS 400, AT S28L, AT BS 277, WL 223, AND AT BS 500A, S26L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500491 19980115 00491 NM 1998 1 15 SWAA980013 1 19980107 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND BS 178 SIDE CHORD CRACKED AT BS 178 LT SIDE, WL 195 TO 194. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500492 19980115 00492 NM 1998 1 15 SWAA980014 1 19980107 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 308 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT 308, 3 BELOW S19R, AT BS 893, BETWEEN S22 AND 23L, AT BS 197, 1 0 BELOW S19R, AT BS 500B+5, AND AT BS 890, ABOVE S20L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500493 19980115 00493 NM 1998 1 15 SWAA980015 1 19980107 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 392-400 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AND CREASED AT 392 TO 400, AND AT BS 387, AT S23R. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1998011500494 19980115 00494 NM 1998 1 15 SWAA980016 1 19980107 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 205-270 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT 446, 4 BELOW S17R, AT BS 205, 10 BELOW S19R, AT BS 270, LBL 24 T O 34, AND AT B S227, 6 BELOW S24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500495 19980115 00495 NM 1998 1 15 SWAA980017 1 19980105 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 760/727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SCHEDULED T/C CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760 AT S17L, 3 AFT OF EXISTING DOUBLER AND AT BS 727C, AT S16R BETWEEN EXISTING DOUBLER. REPAIRED BOTH PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500496 19980115 00496 NM 1998 1 15 SWAA980018 1 19980101 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM SUPPORT STRAP CRACKED AT BS 312, AT BL 0 AND RBL 33 AND 46. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998011500497 19980115 00497 NM 1998 1 15 SWAA980019 1 19980101 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED BC1 CHECK, FOUND A 4 FUSELAGE SKIN CRACK 4 FWD OF OS BS 747, S26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998011500498 19980115 00498 NM 1998 1 15 SWAA980020 1 19980101 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED BC1 CHECK, FOUND A 1.5 FUSELAGE SKIN CRACK AT E&E COOLIN AND DUCT CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998011500499 19980115 00499 NM 1998 1 15 SWAA980021 1 19980101 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C1 CHECK, FOUND A FUSELAGE SKIN CRACK AT AFT SERVICE DOOR UPPER HINGE CUTOUT UPPER FWD CORNER. REPAIRE D PER SWA RA 1-353-1746. 2 L 7 2 4F RT A16WE 1998011500500 19980115 00500 NM 1998 1 15 SWAA980022 1 19980110 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 775 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED TERMINAL CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 775, AT S10. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500501 19980115 00501 NM 1998 1 15 SWAA980023 1 19980108 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 470 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 23SW 21338 DURING SCHEDULED SC CHECK, FOUND A FUSELAGE SKIN CRACK AT LAP JOINT BS 470, AT S14L, AT BS 480, AT S10L, AND AT BS 490, AT S14L. REPAIRED ALL PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500502 19980115 00502 NM 1998 1 15 SWAA980024 1 19980108 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK INDICATION AT BS 400, AT S5L TO 6L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500503 19980115 00503 NM 1998 1 15 SWAA980025 1 19980108 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACK INDICATION AT BS 520, AT S16L-17L, AND AT BS 967, AT S8L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500504 19980115 00504 NM 1998 1 15 SWAA980026 1 19980108 A 5320 CHANNEL BOEING 737 7372H4 138448C NM BS 361 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND U-CHANNELS CRACKED AT BS 361 S3L, AT BS 360, LBL 254, 69 AND 63. REPLACED PER BOEING SR M. 2 L 7 2 4F A16WE 1998011500505 19980115 00505 NM 1998 1 15 SWAA980027 1 19980108 A 5311 FRAME BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 663, AT S5L, AT BS 304, LBL 65, AND AT BS 291, S12R. REPA IRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500506 19980115 00506 NM 1998 1 15 SWAA980028 1 19980108 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 993-1006 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 993 TO 1006, ABOVE S14L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500507 19980115 00507 NM 1998 1 15 SWAA980029 1 19980108 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND I/B FRAME CHORD CRACKED AT FASTENER HOLE LT, S16, BS 639. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998011500508 19980115 00508 NM 1998 1 15 SWAA980030 1 19980111 A 2530 COFFEEMAKER BOEING 737 7372H4 138448C NM AFT GALLEY INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 IN FLIGHT NOTED AN ELECTRICAL TYPE SMELL AT AFT GALLEY AREA. DISCONNECTED POWER TO COFFEEMAKERS. REPLACED AFT LOWER CO FFEEMAKER PER BOEING M/M. 2 L 7 2 4F A16WE 1998011500509 19980115 00509 NM 1998 1 15 UPS98225396 1 19980108 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 1130 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, AFT CARGO BAY BS 1130 AT STR 26L FRAME IS DENTED. DENT FOUND OUT OF LIMITS PER SRM 51-30-1. FABRIC ATED REPAIR PARTS AND INSTALLED PER SRM 51-40-3 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998011500510 19980115 00510 NM 1998 1 15 UPS98225397 1 19980108 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE AT NUT PLATE BS 950F, LBL 12, WL 200. REMOVE D DAMAGED SECTION AND INSTALLED DOUBLER AND TRIPLER ANGLE AND FILLER IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998011500515 19980115 00515 NM 1998 1 15 UPS98225402 1 19980102 A 5754 BONDING JUMPER BOEING 727 7272A1 138407F NM NR 5 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, NR 5 K-FLAP O/B LOWER BONDING JUMPER HAS CORROSOION WHERE JUMPER ATTACHES. CORROSION FOUND OUT OF L IMITS PER SRM 57-50-01. CORROSION DAMAGE REMOVED AND STANDARD REPAIR COMPLETED PER SRM 57-50-3, SRM 51-20-2 AND SRM 51- 30-00. 2 L 7 3 4F A3WE 1998011500516 19980115 00516 NM 1998 1 15 UPS98225403 1 19980109 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION AFT CARGO BAY ON FLOORBEAM, FWD LOWER FLANGE UNDER NUT PLATES BS 1070, BL 0 TO LBL 10 WL 2 00. REMOVED DAMAGED SECTION AND REPAIRED LOWER FLANGE IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998011500517 19980115 00517 NM 1998 1 15 UPS98225404 1 19980109 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION ON FRAME BS 720D STR 10 TO 13 RT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW S RM 51-40-3. 2 L 7 3 4F A3WE 1998011500530 19980115 00530 WP 1998 1 15 UPS98825417 1 19980107 A 5313 975491333 LONGERON DOUG DC8 DC873F 302199F WP BS 220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, LONGERON 36 AT FS 220 CORRODED BEYOND LIMITS. REMOVED AND REPLACED LONG IAW SRM 51-1-21 AND 51-1-20D . 2 L 7 4 4F RT 4A25 1998011500533 19980115 00533 WP 1998 1 15 UPS98825420 1 19980105 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 776 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, SEAT TRACK EXFOLIATED FS 776 BL 0. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IA W SRM 53-1-7 AND 53-2-3. 2 L 7 4 4F RT 4A25 1998011500534 19980115 00534 WP 1998 1 15 UPS98825421 1 19980108 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1715 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN CABIN FLOOR BOARD SUPPORT CORROSION REMOVAL BEYOND LIMITS FS 1715 RBL 10 TO LBL 10. REMOVED, FA BRICATED, AND INSTALLED REPLACEMENT SUPPORT IAW DWG 5755032, SRM 53-7-3 AND 51-1-20. 2 L 7 4 4F RT 4A25 1998011500535 19980115 00535 EU 1998 1 15 WWMA9800009 1 19980110 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A WWMA K NONE L NO TEST CR CRUISE 1 WP 15 339SB 340B339 CREW REPORTED THE EMERGENCY FLOOR LIGHTS AT ROWS 3B, 4A AND 5B FAILED TO ILLUMINATE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF EMERGENCY LIGHTS AND COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T RT A52EU 1998011500536 19980115 00536 EU 1998 1 15 WWMA9800008 1 19980109 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 350CF 9150 340B350 CARGO SMOKE LIGHT ON THE CWP ILLUMINATED DURING PREFLIGHT. REPLACED FORWARD SMOKE DETECTOR, DETECTOR WAS OEM. 2 L 7 2 4T RT A52EU 1998011500537 19980115 00537 EU 1998 1 15 WWMA9800007 1 19980110 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 356SB 340B356 EMERGENCY ARM LIGHT ON THE FLIGHT ATTENDANTS PANEL FAILS TO ILLUMINATE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A52EU 1998011500538 19980115 00538 EU 1998 1 15 WWMA9800006 1 19980109 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 283AE 340B283 EMERGENCY ARM LIGHT ON THE FLIGHT ATTENDANTS PANEL FAILS TO ILLUMINATE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A52EU 1998011500539 19980115 00539 EU 1998 1 15 98FDEA00020 1 19980109 A 5270 WARNING SYST AIRBUS 310 A310222 3930315 EU CARGO DOOR MALFUNCTIONED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 420FE 339 BULK DOOR NOT CLOSED ECAM WARNING DURING TAKEOFF ROLL AT KNOTS. TAKEOFF ROLL DISCONTINUED AND RETURNED TO BLOCKS FOR DO OR INSPECTION. CLEANED AND RESECURED 36WS SWITCH AND INSPECTED ALL DOOR OPERATING MECHANISM FOUND NORMAL. CYCLED DOOR SEVERAL TIMES INDICATION ON ECAM NORMAL. 2 L 7 2 4F RT A35EU 1998011500540 19980115 00540 NM 1998 1 15 98FDEA00023 1 19980112 A 3350 P4010020 BATTERY BOEING 727 72727C 138400J NM PAX DOOR DISCHARGED A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 146FE 19110 FORWARD ENTRY DOOR ESCAPE SLIDE EMERGENCY LIGHT BATTERY IS DEAD. *S/D* REMOVED AND REPLACED FWD ENTRY DOOR ESCAPE SLID E EMERGENCY LIGHT BATTERY AND FUNCTIONAL TESTED IAW FED-EX M/M 33-50-121. 2 L 7 3 4F A3WE 1998011500541 19980115 00541 EU 1998 1 15 98FDEA00024 1 19980108 A 2750 RETRACT MECH AIRBUS 310 A310203 EU NR 1 TE FLAP MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 415FE 349 FLAPS STUCK AT APPROX 5 DEG ON RETRACTION. FLAPS SYS 1 AND 2 FAULT ILLUMINATED. FLAPS WOULD NOT EXTEND BEYOND 5 DEG ON LANDING. SLATS OPERATED NORMALLY. SFPI FLAP FAULT DID NOT ILLUMINATE. AIRCRAFT RETURNED TO LAS AND LANDED WITH NO IN CIDENCE. FOUND RIGHT WING NR 1 FLAP JACKSCREW AND RIGHT ANGLE GEARBOX CONTAMINATED. REMOVED AND REPLACED RIGHT NR 1 FL AP JACKSCREW, RIGHT ANGLE BOX, TORQUE LIMITER AND RIGHT PDU, RIGHT ANGLE GEARBOX. 2 L 7 2 4F RT A35EU 1998011500542 19980115 00542 NM 1998 1 15 98FDEA00025 1 19980112 A 5711 65185385 SPAR CHORD BOEING 727 72722 1384002 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 CORROSION (C53-132-02-1, 2) ALONG VERTICAL FLANGE OF BS 870 UPPER SPAR CHORD WL 180, RBL 65- LBL 65. *S/D* REMOVED AND REPLACED 870 UPPER SPAR CHORD WL 180, RBL 65 - LBL 65 IAW FED-EX EA 7-5100-37367 AND 7-5710-38653. 2 L 7 3 4F A3WE 1998011500543 19980115 00543 NM 1998 1 15 98FDEA00026 1 19980112 A 5712 65192921 BULKHEAD WEB BOEING 727 72722 1384002 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 CORROSION (C53-132-02-1, 2) IN NUMEROUS AREAS ON BS 870 BULKHEAD WEB OF CENTER WING SECTION. *S/D* REMOVED AND REPLACE D 870 BULKHEAD WEB OF CENTER WING SECTION PER EA 7-5710-38653. 2 L 7 3 4F A3WE 1998011500544 19980115 00544 NM 1998 1 15 98FDEA00027 1 19980112 A 5315 65163169 FLOORBEAM BOEING 727 72722 1384002 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 NR 0429 007, WHILE WORKING NR0408, FOUND CORROSION ON FLOORBEAM BS 344, RBL 17 OUT OF LIMITS AND DOUBLE HOLE DRILLED AT RBL 38, WL 208. REMOVED AND REPLACED BS 344 BEAM UPPER CHORD LBL 17 TO RBL 65 PER FED-EX DRAWING SR 27-53-007. 2 L 7 3 4F A3WE 1998011500545 19980115 00545 NM 1998 1 15 98FDEA00028 1 19980112 A 5320 651891555 CHORD BOEING 727 72722 1384002 NM BS 312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 WHILE WORKING NR 0329, FOUND FRAME FAIL-SAFE CHORD CORRODED AT BS 312, LBL 19, WL 153. *S/D* FOUND CORROSION DAMAGE ON FAIL-SAFE CHORD AT BS 312, LBL 19, WL 153 TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-1. REMOVED CHORD LBL 19 TO LBL 42. F ABRICATED NEW PART AND INSTALLED IAW FEDEX DRAWING 65-18915 SHT 3. 2 L 7 3 4F A3WE 1998011500546 19980115 00546 WP 1998 1 15 ABXA9800013 1 19980112 A 5250 5652502501 DOOR ASSY DOUG DC8 DC861 3021952 WP COCKPIT DEFECTIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 DURING POST FLIGHT INSPECTION, FOUND COCKPIT DOOR HARD TO OPEN. RESECURED HARDWARE ON DOOR, DOOR OPERATES NORMAL. 2 L 7 4 4F 4A25 1998011500547 19980115 00547 WP 1998 1 15 ABXA9800014 1 19980108 A 2612 CA3106KE10SL4S FIRE LOOP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE DISCONNECTED A A ABXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 804AX 45987 644128 DURING CRUISE, ENG FIRE WARNING MASTER LIGHT AND BELL ACTIVATED MOMENTARILY. UNABLE TO DETERMINE WHICH ENGINE CAUSED PR OBLEM. FUEL FLOW ON NR 3 ENGINE INCREASED APPROXIMATELY 700 PPH. SHUT DOWN NR 3 ENGINE, WITH ENGINE WINDMILLING, N1 WA S 26.5 PERCENT, N2 WAS 41.1 PERCENT AND OIL PRESSURE WAS 36 PSI. GROUND RAN NR 3 ENGINE. FUEL FLOW OPS CHECKED NORMAL. INSPECTED FIRE WARNING SYSTEMS ON ALL FOUR ENGINES. FOUND WIRE DISCONNECTED ON FIRE LOOP ON NR 1 ENGINE ABOVE DIFFUSE R CASE. RECONNECTED WIRE, NO DISCREPANCIES NOTED ON NR 2 , 3 AND 4 ENGINES. FIRE WARNING SYSTEM OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1998011500548 19980115 00548 NM 1998 1 15 VNAA9801006 1 19980109 A 3412 0102JG1AG01 TAT PROBE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E COMPT DEFECTIVE A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 425JS 2290 3037 DURING TAXI, THE CREW RECEIVED A TAT HEAT FAIL MESSAGE. CREW RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE TAT PROBE DEFECTIVE. TAT PROBE WAS REPLACED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-10-00. OPER ATIONAL CHECK GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998011500861 19980115 00861 NM 1998 1 15 K3HA980002 1 19980111 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 EMERGENCY PATH LIGHTING WAS OUT FOWARD OF PAX ROW 4DEF. REPAIRED BROKEN WIRE AS REQUIRED, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998011500862 19980115 00862 NM 1998 1 15 W8PA980009 1 19980111 A 3350 5872 COVER BOEING 737 7373Y0 1384671 NM CABIN DETACHED A W8PA K NONE O OTHER NR NOT REPORTED 1 NM 03 962WP 23748 EMERGENCY PATH LIGHTING COVER IS DETACHED AT THE OVERWING EXITS. REINSTALLED EMERGENCY TRACK COVER, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998011500863 19980115 00863 NM 1998 1 15 W8PA980010 1 19980112 A 3397 WIRE BOEING 737 7373K9 138447L NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 945WP 24212 DURING SERVICE CHECK, FOUND EMERGENCY TRACK LIGHTING INOP AT ROW 2 AND 4. SECURED LOOSE WIRES, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998011500864 19980115 00864 NM 1998 1 15 RAAA98B1001 1 19980113 A 5415 65187241 FITTING BOEING 727 72722C 138400F NM BS 1243 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 3784 19093 DURING SCHEDULED AD 89-23-17 INSPECTION, FOUND NR 1 ENGINE AFT MOUNT SUPPORT FITTING CRACKED AT BS 1243, LBL 60. TWO CR ACKS APPROX 1 IN EACH IN FITTING FWD SIDE UPPER FLANGE AND RADIUS. REPLACED AFT MOUNT SUPPORT FITTING PER S/B 727-54-00 17 AND DWG 65C34829, M-54 NR 14. 2 L 7 3 4F A3WE 1998011500865 19980115 00865 NM 1998 1 15 CALA9800016 1 19980112 A 3260 655825029 LOGIC CARD BOEING 737 7373T0 1384582 NM LANDING GEAR INOPERATIVE A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 69348 23586 THE RT MLG INDICATION WAS SHOWING RED AND GREEN AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISH ED. THE RED LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. MAINTENANCE FOUND THE M986 LOGIC CARD AT FAULT. THE M986 LOGIC CARD WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 32-09-20. 2 L 7 2 4F RT A16WE 1998011500866 19980115 00866 NM 1998 1 15 CALA9800017 1 19980112 A 3230 1030874 SOLENOID BOEING 737 737217 1384464 NM E/E COMPT INOPERATIVE A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 14233 19887 THE LANDING GEAR HANDLE WOULD NOT GO PAST THE OFF DETENT AFTER TAKEOFF. THE OVERRIDE DID NOT WORK EITHER. THE AIRCRAFT WAS RETURNED TO GSO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE M241 LEVER LATCH SOLENOID AT FAULT. THE S OLENOID WAS REPLACED IAW MM 32-31-31 AND WIRING DIAGRAM 32-31-01 AND OPERATION CHECKED GOOD. THE AIRCRAFT WAS JACKED AN D A RETRACTION CHECK WAS PERFORMED WITH NO DEFECTS NOTED. 2 L 7 2 4F A16WE 1998011500867 19980115 00867 NM 1998 1 15 CALA9800018 1 19980112 A 2710 6595600642 CONTROL MODULE BOEING 727 727224 1384076 NM AILERON LEAKING A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 32725 20655 THE A-SYSTEM HYDRAULIC OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF WHILE CLIMBING THROUGH 6000 FEET. A MINUTE LATER, THE A -HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. THE HYDRAULIC FAILURE CHECKLIST WAS PERFORMED, FUEL WAS DUMPED, AND THE AIRCRA FT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AILERON CONTROL MODULE LEAKING. THE AILERON CONTROL MODULE WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1998011500868 19980115 00868 WP 1998 1 15 CALA9800019 1 19980113 A 3350 25503025 BATTERIES MARATHON DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND EMERGENCY LIGHTS ON CEILING ABOVE ROW 1 TO 4 AND ROW 22 TO 30 INOPERATIVE. THE BATTERIES IN FORWARD CA BIN CEILING AND ABOVE ROW 24 WERE REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1998011500869 19980115 00869 NE 1998 1 15 9800521155 2 19980111 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 ENGINE STALLED A NWAA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 155US 46764 686156 AFTER STARTING DESCENT FROM FL330, THE NR 2 ENGINE COMPRESSOR STALLED. POWER WAS REDUCED TO IDLE AND AFTER EGT REACHING 820C THE ENGINE RECOVERED. WHILE DESCENDING FROM FL290, THE NR 2 ENGINE STALLED AGAIN WITH MAX EGT OF 760. THE CREW F OLLOWED COM PROCEDURES AND SHUT DOWN THE ENGINE. THE FIRST RESTART ATTEMPT WAS SUCCESSFUL AND THE ENGINE OPERATED NORMA LLY FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE AND REPLACED NUMEROUS BLEED COMPONENTS. ENGINE O PERATIONAL CHECK WAS NORMAL AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1998011500870 19980115 00870 NM 1998 1 15 9800532292 1 19980107 A 2781 INDICATOR BOEING 727 727251 138408H NM NR 3 LE FLAP INOPERATIVE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 292US 21503 DURING CLIMB ON FLAP RETRACTION, THE NR 3 LEADING FLAP DID NOT INDICATE UP AND LOCKED. AIRCRAFT RETURNED TO DTW AND LAN DED WITHOUT INCIDENT. REPLACED LEADING EDGE POSITION INDICATOR AND STRAIGHTENED NR 7 PIN ON CANNON PLUG OF NR 3 LEADING EDGE SWITCH, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998011500871 19980115 00871 NM 1998 1 15 9800546632 1 19980110 A 3320 CONNECTOR BOEING 747 747251B 1384892 NM CABIN SHORTED A NWAA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 632US 23112 DURING CRUISE, SMOKE OCCURRED ABOVE SEAT 4JK. FLIGHT CREW UTILIZED PORTABLE EXTINGUISHER TO ELIMINATE SMOKE. FLIGHT CR EW NOTICED CIRCUIT BREAKER HAD POPPED AND DID NOT RESET. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED AND RESTOWED WIRING AND CAPPED AT THE COLUMN TIMER DECODER, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998011500872 19980115 00872 EU 1998 1 15 9800553226 1 19980110 A 2420 RELAY AIRBUS 320 A320211 3930320 EU E/E COMP INTERMITTENT A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 326US 282 AFTER TAKEOFF, RECEIVED ECAM WARNING ELEC ESS BUSSES ON BAT. RETURNED TO YVR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAY 16XC, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998011500873 19980115 00873 SO 1998 1 15 COMA9810021 1 19980112 A 3260 MS3476L106P PROX SENSOR EMB 120 EMB120RT SO LT MLG DEFECTIVE A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 463CA 1267 DURING APPROACH, THE LANDING GEAR WOULD NOT EXTEND, LEFT MLG A-SYSTEM GREEN LIGHT ILLUMINATED. REPLACED THE LEFT MLG A- DOWNLOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1998011500874 19980115 00874 SO 1998 1 15 COMA9810022 1 19980112 A 3350 0L3071BPEGPL LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 241CA 1211 EMERGENCY LIGHTS AT ROW SIX ARE INOPERATIVE. REPLACED LAMP FOR ROW SIX FLOOR EMERGENCY LIGHT TRACK. 2 L 7 2 4T RT A31SO 1998011500875 19980115 00875 NE 1998 1 15 COMA9810023 3 19980113 A 6111 8173861 BEARING RFC11NA6A EMB 120 EMB120RT SO PWA 118 PW118A NE HAMSTD 14RF 14RF9 NE NR 2 PROP BLADE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 263CA 2867 2867 874878 120255 115502 890632 DURING PROPELLER DYNAMIC BALANCING PROCEDURES, IT WAS DETERMINED THAT THE PROPELLER COULD NOT BE BALANCED. FURTHER INSP ECTION OF PROPELLER FOUND NR 2 BLADE TO BE EXCESSIVELY LOOSE. FURTHER INSPECTION FOUND BLADE PIN BEARING TO BE WORN TO 0.080 WALL THICKNESS ON ONE SIDE AND WEARING IN AN OVAL FASHION AND BLADE PIN WORN. REPLACED PIN AND BEARING AND RETURN ED BLADE TO SERVICE. AIRCRAFT WAS IN FOR SCHEDULED MAINTENANCE. 2 L 7 2 4T 4 T RT A31SO E20NE 6 C P11NE 1998011500876 19980115 00876 NM 1998 1 15 UPS98225434 1 19980113 A 5713 STRINGER BOEING 727 72722C 138400F NM WS 656 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, RW CRACK FOUND ON VENT STRINGER 13 FLANGE AT WS 656. ACCOMPLISHED VENT STRINGER REPAIR IAW UPS EO B 727-5710-0314. 2 L 7 3 4F A3WE 1998011500877 19980115 00877 NM 1998 1 15 UPS98225435 1 19980113 A 5311 FRAME BOEING 727 72722C 138400F NM BS 910 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, WHILE WORKING CUSTOMER CARD 664487 INT 149 FOUND CORROSION AROUND FASTENER HOLES ON FRAME BS 910 LBL 29 WL 297. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 53-10-4, 53-30-2, 51-20-0. 2 L 7 3 4F A3WE 1998011500878 19980115 00878 NM 1998 1 15 UPS98225436 1 19980113 A 5320 STIFFENER BOEING 727 72722C 138400F NM BS 255 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-01) ON HORIZONTAL STIFFENER AT BS 255 RBL 26, WL 165. REMOVED CORROSIO N, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-10-1, 51-10-6. 2 L 7 3 4F A3WE 1998011500887 19980115 00887 NM 1998 1 15 UPS98225446 1 19980104 A 5753 65192702 TRACK BOEING 727 72722C 138400F NM NR 4 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, NR 4 FLAP TRACK 2 HOLES AT SPOILER BEAM ATTACH POINT HAVE PITTING CORROSION. REMOVED AND REPLACED T RACK IAW SRM 51-30-2, 51-30-5, 51-10-1. 2 L 7 3 4F A3WE 1998011500888 19980115 00888 NM 1998 1 15 UPS98225447 1 19980104 A 5751 FITTING BOEING 727 72722C 138400F NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, UPON REMOVAL OF THE R/W I/B AILERON FOUND THE CENTER HINGE FITTING AIM CORRODED. REMOVED AND REPLAC ED IAW OHM 57-50-01 AND MM 27-10-01. 2 L 7 3 4F A3WE 1998011500890 19980115 00890 NM 1998 1 15 UPS98225449 1 19980112 A 5320 STIFFENER BOEING 727 72722C 138400F NM BS 255 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION ON HORIZONTAL STIFFENER AT BS 255, LBL 26, WL 165. ACCOMPLISHED EXTRUDED SECTION REPAIR I AW SRM 51-40-4. 2 L 7 3 4F A3WE 1998011500891 19980115 00891 NM 1998 1 15 UPS98225450 1 19980112 A 5720 69201122 BRACKET BOEING 727 72722C 138400F NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION ON EXPANSION LINK BS 740, RBL 13, WL 165. REMOVED AND REPLACED EXPANSION LINK SRM 51-10-1 , 53-10-1, 51-30-2. 2 L 7 3 4F A3WE 1998011500892 19980115 00892 NM 1998 1 15 UPS98225451 1 19980112 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION FLOORBEAM BS 420, RBL 45 TO 60, WL 208 OF LOWER SIDE AT UPPER FLANGE. CUT OUT DAMAGED SEC TION OF FLANGE AND ACCOMPLISHED REPAIR IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998011500893 19980115 00893 WP 1998 1 15 UPS98825422 1 19980110 A 2120 AIR DISTRBUTION DOUG DC8 DC871F 302199D WP COCKPIT ODOR A IPXA K NONE O OTHER CR CRUISE 1 SO 01 748UP 45948 INSPECTION TYPE-N/A, STRONG ODOR OF JET FUEL IN FLIGHT STATION THE ENTIRE FLIGHT. COULD NOT LOCATE EXACT SOURCE OF ODOR . VENTILATED COCKPIT FOR 12 HRS, SMELLS GOOD. 2 L 7 4 4F RT 4A25 1998011500898 19980115 00898 WP 1998 1 15 UPS98825427 1 19980107 A 5320 5645332117 DOUBLER DOUG DC8 DC873F 302199F WP BS 960-980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN W/W PRESURE FLOOR UPPER SURFACE FINGER DOUBLER CORRODED BEYOND LIMITS F/S 960 TO 980 RBL 62 TO 6 9. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5645332 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998011500904 19980115 00904 WP 1998 1 15 UPS98825433 1 19980103 A 5320 5615372673 DOUBLER DOUG DC8 DC873F 302199F WP BS 1420-1440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FINGER DOUBLER CORRODED AND CRACKED BEYOND LIMITS AT FS 1420 TO 1440 L-31L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5615372 SRM 51-1-21, 51-1-20D, AND 53-4-0. 2 L 7 4 4F RT 4A25 1998011500905 19980115 00905 EU 1998 1 15 WWMA9800011 1 19980112 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 232AE 340B232 DURING PREFLIGHT CHECKS, THE EMERGENCY LIGHT ABOVE SEAT 12C FAILED TO ILLUMINATE. RETIGHTENED LOOSE CONNECTOR ON THE BA CK OF THE LIGHT ASSEMBLY. 2 L 7 2 4T RT A52EU 1998011500906 19980115 00906 EU 1998 1 15 WWMA9800010 1 19980112 A 2611 SMOKE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 350CF 340B350 DURING PREFLIGHT, THE CARGO SMOKE LIGHT ON THE CWP ILLUMINATED. MAINTENANCE PERFORMED OPERATIONAL CHECK OF THE CARGO SM OKE DETECTION SYSTEM AND COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A52EU 1998011500907 19980115 00907 NM 1998 1 15 QXEA9800016 1 19980108 A 2910 82910010117 HYD LINE DHAV 82910002003 DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYST LEAKING A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 814PH 43 AFTER TAKEOFF, NOTICED AN ODORLESS CHEMICAL IRRITANT IN THE COCKPIT. THE IRRITANT WAS NOTICED IN THE COCKPIT FOR A PERI OD OF ABOUT 20 SECONDS. MX PERFORMED AN ENGINE RUN WITH BLEEDS ON AND TEMP HOT FROM IDLE TO TAKEOFF POWER RPM. NO IRRI TANT NOTED. PRESSURIZED HYD SYS AND INSPECTED FROM UNDER THE COCKPIT FLOOR TO ROW 2. FOUND HYD LINES JUST AFT OF THE F ORWARD PRESSURE BULKHEAD TO BE WET, BUT NO LEAKS FOUND. INSPECTED AND DETERMINED TO BE SAFE FOR GEAR DOWN FERRY FLIGHT TO PDX. IN PDX REPLACED GEAR-UP HYD LINE JUST AFT OF THE FORWARD PRESSURE BULKHEAD BY PERMA SWEDGE. SERVICED AND BLED THE NR 2 HYD SYS AND ACCOMPLISHED A GEAR SWING, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998011500908 19980115 00908 NM 1998 1 15 QXEA9800017 1 19980110 A 3350 1013079 LIGHTS GRIMES 82520977001 DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 347PH 480 SEA- FORWARD TWO FLOOR EMERGENCY PATH LIGHTS ARE INOP. REPLACED FORWARD 2 EMERGENCY FLOOR PATCH LIGHTING STRIPS, OPERAT IONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998011500909 19980115 00909 NM 1998 1 15 QXEA9800018 1 19980108 A 6120 AUTOFEATHER SYST DHAV DHC8 DHC8102 2809003 NM E/E COMPT FAILED TEST A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 818PH 58 EUG- AUTOFEATHER WILL NOT TEST PROPERLY. CYCLED POWER LEVERS AND PERFORMED AUTOFEATHER TEST AGAIN. TESTED GOOD, AIRCRA FT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998011500910 19980115 00910 EU 1998 1 15 QXEA9800019 1 19980107 A 2740 X00026415 CONTROL PANEL FOKKER A41324 FOKKER F28 F28MK4000 4990810 EU COCKPIT MALFUNCTION A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 484US 2625 2625 11234 ON DEPARTURE, BOTH HORIZIONTAL STABILIZER FLIGHT CONTROL CHANNEL CAUTION LIGHTS ILLUMINATED. ACCOMPLISHED THE EMERGENCY CHECKLIST, REVERTING THE STABILIZER SYSTEM TO MANUAL. ENCOUNTERED NO FURTHER PROBLEMS EN ROUTE, AND ACCOMPLISHED AN UN EVENTFUL LANDING AT FCA. IN FCA MAINTENANCE DRAINED AND SERVICED THE STABILIZER GEAR BOX, INSPECTED THE STICKING SWITCH AND HARNESS, CLEANED AND RECONNECTED ALL ELECTRICAL CONNECTIONS. PERFORMED A TEST OF THE STABILIZER ACTUATOR. REPLACE D THE FLIGHT CONTROL PANEL, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998011500911 19980115 00911 EU 1998 1 15 QXEA9800020 1 19980108 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 483US 11233 SEVERAL OVERHEAD EVACUATION LIGHTS ARE INOP. RELAMPED OVERHEAD LIGHTS, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998011500912 19980115 00912 EU 1998 1 15 QXEA9800021 1 19980112 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 FORWARD EMERGENCY LIGHT INOP. REPLACED LAMP, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998011500913 19980115 00913 EU 1998 1 15 QXEA9800022 1 19980108 A 3350 5515900004 CIRCUIT CARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 493US 11161 LIGHT BULB BURNT IN THE OVERHEAD EMERGENCY EXIT LIGHT ON THE LEFT SIDE. REPLACED LAMP CIRCUIT CARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998011500914 19980115 00914 EU 1998 1 15 QXEA9800023 1 19980109 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 476US 11224 UPON ARRIVAL, COULD NOT OPEN MAIN CABIN DOOR USING NORMAL ELECTRIC METHODS. PERFORMED EMERGENCY OPENING OF THE DOOR. A FTER EMERGENCY OPERATION DOOR OPERATED NORMALLY IN BOTH NORMAL AND EMERGENCY MODES. MAINTENANCE INSPECTED THE DOOR AND PERFORMED SEVERAL OPEN / CLOSE CYCLES FROM THE CABIN SWITCHES AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT RETURNED TO SERVICE, NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998011500915 19980115 00915 WP 1998 1 15 MWEA98012 1 19980106 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP FWD GALLEY FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 GALLEY SLIDE COVER FELL OFF. MTC REPLACED. 2 L 7 2 4F A6WE 1998011500916 19980115 00916 WP 1998 1 15 MWEA98013 1 19980108 A 2530 OVEN DOUG DC9 DC932 3022066 WP GALLEY DIRTY A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 602ME 48133 FLIGHT ATTEND TURNED OFF LT OVEN, PLASTIC MELTING ON ONE ELEMENT CAUSING SMOKE. MTC CLEANED PLASTIC FROM OVEN. 2 L 7 2 4F A6WE 1998011500917 19980115 00917 WP 1998 1 15 MWEA98014 1 19980110 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 GALLEY SLIDE COVER FELL OFF. MTC REINSTALLED. 2 L 7 2 4F A6WE 1998011500918 19980115 00918 WP 1998 1 15 MWEA98015 1 19980110 A 3350 60030431 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 800ME 45842 FLIGHT ATTEND FWD POS EMERG FLASHLIGHT DOESN'T BLINK. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998011500919 19980115 00919 WP 1998 1 15 MWEA98016 1 19980112 A 3350 081691 SOCKET DOUG DC9 DC914 3022034 WP TAIL WALKWAY GROUNDED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 800ME 45842 AFT 2 RED FLOOR LIGHTS AND TAIL WALKWAY EMERG LIGHTS INOP. MTC REPAIRED. 2 L 7 2 4F A6WE 1998011500920 19980115 00920 WP 1998 1 15 MWEA98017 1 19980112 A 2120 97852011 BLOWER DOUG DC9 DC932 3022066 WP AFT FUSELAGE FAILED A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 205ME 47601 DURING APU CONDITION CHECK GOT SMOKE IN CABIN. MTC REMOVED AND REPLACED GROUND BLOWER AND WATER SEP TEMP VALVE. 2 L 7 2 4F A6WE 1998011500921 19980115 00921 WP 1998 1 15 MWEA98018 1 19980113 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 814 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LT SIDE FUSE SKIN STA 814 L20 HAS DEEP GOUGE. MTC REPAIRED IAW SRM 53-04 FIG 38 VIEW R. 2 L 7 2 4F A6WE 1998011500922 19980115 00922 WP 1998 1 15 MWEA98019 1 19980113 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 RT ELEV TRAILING EDGE HAS 3 DEEP GOUGES STA XHS158 AND 204.1. MTC REPAIRED IAW SRM 53-03 FIG 15. 2 L 7 2 4F A6WE 1998011500923 19980115 00923 WP 1998 1 15 MWEA98020 1 19980113 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 NR 3 CABIN FS 200 GALLEY MOUNT SEAT TRACK CORRODED FWD END. MTC REPAIRED IAW SRM 53-05 FIG 4B. 2 L 7 2 4F A6WE 1998011500924 19980115 00924 1998 1 15 P5CA9800010 4 19980110 A 3441 INERTIAL NAV SYS BOEING 747 747132 1384882 NM NR 1 FAILED A P5CA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 WP 23 857FT 20246 NR 1 INS FAILED. THIS A/C EQUIPED WITH ONLY 2 INS SYSTEMS. A/C RETURNED TO AMS. REPLACED NR 1 INU IAW MM 34-41-07. N IL MALFUNCTION CODES FINE ALIGNMENT C/W. 2 L 7 4 4F A20WE 1998011500925 19980115 00925 WP 1998 1 15 RRXA98004 1 19980110 A 3310 BA1700MODB BALLAST DOUG DC8 DC873 302199C WP COCKPIT FAILED A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 105WP 46095 THERE WAS A FLASH AND THEN ELECTRICAL SMOKE FROM F/O'S SIDE PANEL UNDER WINDOW, BY MAP LIGHT. SMOKE STOPPED QUICKLY AND CLEARED OUT. NO PROBLEM AFTER THAT. FOUND GLARESHIELD FLUORESCENT LIGHTS INOP. REPLACED BALLAST PER MM 33-12. GLARE SHIELD FLUORESCENT LIGHTS OPS CHECK NORMAL. THIS CLEARS MEL CONT NR 801075 PLACARD REMOVED. 2 L 7 4 4F RT 4A25 1998011500926 19980115 00926 WP 1998 1 15 TC8A98001 1 19980112 A 3610 E71C07 HEAT EXCHANGER DOUG DC8 DC8F55 3021928 WP NR 4 DEFECTIVE A TC8A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 182SK 1165 8 45817 HEAVY SMOKE (BURNED OIL) FROM NASI'S NUMBER 1 AND NUMBER 2. RETURN TO MIAMI. FOUND OIL RESIDUE AT INPUT PORT NR 4 HEAT EXCHANGER. REMOVED AND REPLACED NR 4 HEAT EXCHANGER IAW DMM 36-1-3, SYSTEM OPS AND LEAKS CHECKS GOOD. PERFORMED GROUN D CABIN PRESSURE CHECK IAW 21-6-0, NO DEFECTS NOTED, NO SMOKE IN COCKPIT. CHECKED PNEUMATIC BLEED SYSTEM FOR ENGINE 1 T HRU 4 INDEPENDENTLY, NO DEFECTS, SYSTEM CHECKS GOOD IAW DMM 36-1-2. VERIFIED PROPER ENGINE OIL SERVICING IAW DMM 12-1-0 . PERFORMED GROUND IDLE / TAKEOFF POWER RUN IAW 71-00, ALL SYSTEM CHECK OK. 2 L 7 4 4F 4A25 1998012100005 19980121 00005 EU 1998 1 21 MALA975882 1 19980109 A 7603 FLIGHT IDLE STOP SAAB SF340 SF340A 7850100 EU ENGINE TRIPPED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 103XJ 340A103 AFTER TAKEOFF, THE FLIGHT STOP OPEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE RESET FLIGHT IDLE STOP OV ERRIDE THAT WAS TRIPPED IN OVERRIDE POSITION, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012100007 19980121 00007 NM 1998 1 21 CALA9800015 1 19980112 A 2910 693731789 HYD PWR PANEL BOEING 737 737524 1384721 NM COCKPIT INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 18622 9902 27526 CREW REPORTED, LOOSING BOTH ENGINE DRIVEN HYDRAULIC PUMPS WHILE EN ROUTE. THE NR 1 AND NR 2 HYDRAULIC PUMP LOW PRESSURE LIGHTS ILLUMINATED. WHILE TRYING TO ISOLATE PROBLEM THE SYSTEM CAME BACK ON LINE. THE AIRCRAFT WAS DIVERTED TO CLE WH ERE IT LANDED WITHOUT INCIDENT. BOTH HYDRAULIC PUMPS WERE INSPECTED AND FOUND GOOD. THE HYDRAULIC POWER CONTROL PANEL WAS REMOVED AND REPLACED IAW MM 29-11. IN ADDITION, THE BUS PROTECTION PANEL WAS REPLACED AS A PRECAUTIONARY MEASURE, O PERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1998012200051 19980122 00051 SO 1998 1 22 LR7A9734 1 19980107 A 7922 8A1006X THERMOSTAT LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 3 ENGINE FAILED A LR7A E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 AL 03 401LC 732 4606 550035 PRECAUTIONARY SHUTDOWN NR 3 ENGINE AT 0400Z DUE TO HIGH OIL TEMP. FERRIED AIRCRAFT TO ANC, REPLACED NR 3 ENGINE OIL COO LER THERMOSTAT PER LOCKHEED MM CHAPTER 79-20, PAGE 203. GROUND RUNS ACCOMPLISHED, SYSTEM OPERATIONALLY TESTS OK. 2 H 7 4 4T 4 T A1SO E282 1998012200052 19980122 00052 NM 1998 1 22 W8PA980011 1 19980113 A 3350 OL3071BPEGPL LAMP BOEING 737 7373K9 138447L NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 945WP 24212 DURING DAILY CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 1, 2, AND 3. RELAMPED TRACK LIGHTING, OPS CHECK GO OD. 2 L 7 2 4F RT A16WE 1998012200053 19980122 00053 NM 1998 1 22 W8PA980012 1 19980114 A 2560 SLIDE BOEING 737 7373K9 138447L NM L1 DOOR DETACHED A W8PA K NONE O OTHER NR NOT REPORTED 1 NM 03 945WP 24212 FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE IS DETACHED FROM DOOR. REINSTALLED SLIDE. 2 L 7 2 4F RT A16WE 1998012200054 19980122 00054 NM 1998 1 22 W8PA980013 1 19980113 A 7830 TR LIGHT BOEING 737 737317 138447P NM NR 1 ENGINE ILLUMINATED A W8PA J DUMP FUEL A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 NM 03 946WP 23173 NR 1 ENGINE THRUST REVERSER LIGHT ON AFT OVERHEAD PANEL ILLUMINATED IN FLIGHT. RETURNED TO MDW. DEFERED PER MEL 78-1 C AT C. 2 L 7 2 4F RT A16WE 1998012200055 19980122 00055 NM 1998 1 22 W8PA980014 1 19980113 A 2910 LINE BOEING 737 737301 1384611 NM B-HYD SYSTEM LEAKING A W8PA K NONE K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 03 950WP 23229 LOST QUANTITY AND PRESSURE ON B-HYDRAULIC SYSTEM AFTER PUSHBACK. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE FROM B-SY STEM ELECTRIC HYDRAULIC PUMP. FUNCTIONAL AND LEAK CHECK CHECK GOOD. 2 L 7 2 4F RT A16WE 1998012200056 19980122 00056 NM 1998 1 22 CALA9800020 1 19980113 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 1016 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 34315 23366 INSPECTION FOUND A GOUGE IN FUSELAGE SKIN AT STA 1016, S27R. A DOUBLER PLATE WAS INSTALLED IAW SRM 53-60-01. 2 L 7 2 4F RT A16WE 1998012200057 19980122 00057 NM 1998 1 22 CALA9800021 1 19980114 A 5330 SKIN BOEING 727 727227 1384078 NM BS 178 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND LEADING EDGE OF FORWARD UPPER FUSELAGE SKIN PEELED UP AT RADOME, STA 178. THE DAMAGED SKIN PANEL WAS R EMOVED, A NEW SKIN PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1998012200058 19980122 00058 NM 1998 1 22 CALA9800022 1 19980114 A 5330 SKIN BOEING 727 727227 1384078 NM BS 380 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 380, S17L. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 A ND 51-10-6. 2 L 7 3 4F A3WE 1998012200059 19980122 00059 NM 1998 1 22 CALA9800023 1 19980114 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK AROUND NUT PLATE HOLES IN FLOOR SUPPORT BETWEEN STA 950A AND 950B, RBL 0. THE FLOOR SU PPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-20-14. 2 L 7 3 4F A3WE 1998012200060 19980122 00060 NM 1998 1 22 CALA9800024 1 19980114 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1352 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND CORROSION AND DISHED RIVETS IN LT FUSELAGE SKIN JUST FORWARD OF NR 2 ENGINE FORWARD COWL, STA 1352, S20 L. THE FASTENERS WERE REMOVED IAW SRM 53-30-3. THE CORRODED SKIN WAS CUT OUT, A FILLER AND DOUBLER REPAIR WAS FABRICAT ED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1998012200061 19980122 00061 NM 1998 1 22 CALA9800025 1 19980114 A 5311 FRAME BOEING 727 727227 1384078 NM BS 970 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK IN FRAME AT STA 970, S27L. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10 -4 AND 51-10-2. 2 L 7 3 4F A3WE 1998012200062 19980122 00062 NM 1998 1 22 CALA9800026 1 19980114 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 1050-1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND CORROSION ALONG BOTTOM SIDE OF UPPER FLANGE OF INTERCOSTAL BETWEEN STA 1050 AND 1070 ABOVE S27R. THE L -ANGLE WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998012200063 19980122 00063 NM 1998 1 22 CALA9800027 1 19980114 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1050 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A HOLE THROUGH TOP OF FRAME AT STA 1050 ABOVE STRINGER 27R. THE DAMAGED AREA WAS CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1998012200064 19980122 00064 NM 1998 1 22 CALA9800028 1 19980114 A 5320 PANEL BOEING 727 727227 1384078 NM BS 269 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .125 INCH CRACK IN TOP RIGHT PANEL OF NOSE WHEEL WELL AT FS 269, RBL 10. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. THE CRACKED AREA WAS CUT OUT IAW EA 5362-01016. DOUBLER, STRAP, AND FILLER WERE FABRICATED AND INSTAL LED IAW EA 5362-01016 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1998012200065 19980122 00065 NM 1998 1 22 CALA9800029 1 19980114 A 5320 PANEL BOEING 727 727227 1384078 NM BS 264 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND THREE .125 INCH CRACKS IN TOP RIGHT PANEL OF NOSE WHEEL WELL AT FS 264, RBL 10. THREE .125 INCH CRACKS WERE ALSO FOUND IN TOP LEFT PANEL OF NOSE WHEEL WELL AT FS 264, LBL 10. FASTENERS WERE REMOVED AND THE CRACKED AREAS W ERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW EA 5362-01016. 2 L 7 3 4F A3WE 1998012200066 19980122 00066 NM 1998 1 22 CALA9800030 1 19980114 A 5320 PANEL BOEING 727 727227 1384078 NM BS 289 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND TWO .125 INCH CRACKS IN TOP CENTER PANEL OF NOSE WHEEL WELL AT FS 289, RBL 51. THE FASTENERS WERE REMO VED AND CRACKED AREAS WERE CUT OUT, A REPAIR WAS FABRICATED AND INSTALLED IAW EA 5362-01016. 2 L 7 3 4F A3WE 1998012200067 19980122 00067 NM 1998 1 22 CALA9800031 1 19980114 A 5210 SKIN BOEING 727 727227 1384078 NM L1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK IN L-1 DOOR INNER SKIN. THE CRACK WAS LOCATED 4 FROM FORWARD EDGE AND 10 BELOW UPPER T ORQUE TUBE. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-2, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10 -2, AND 51-30-2. 2 L 7 3 4F A3WE 1998012200068 19980122 00068 NM 1998 1 22 CALA9800032 1 19980114 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1263 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK IN AFT AIRSTAIR WAY RIGHT LOWER TORQUE BOX ATTACH ANGLE AT FS 1263. THE ANGLE WAS REMO VED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200069 19980122 00069 NM 1998 1 22 CALA9800033 1 19980114 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1173 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN AFT AIRSTAIR WAY RIGHT LOWER TORQUE BOX ANGLE AT STA 1173. A NEW ANGLE WAS INSTALLED IAW SRM 53-10-10. 2 L 7 3 4F A3WE 1998012200070 19980122 00070 NM 1998 1 22 CALA9800034 1 19980114 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 740 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND INTERCOSTAL CORRODED AT STA 740. THE CORRODED ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IN THE U PPER INTERCOSTAL IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998012200071 19980122 00071 NM 1998 1 22 CALA9800035 1 19980114 A 5311 FRAME BOEING 727 727227 1384078 NM BS 804 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1.5 INCH CRACK IN LEFT CIRCUMFERENTIAL FRAME REINFORCEMENT PLATE AT STA 804, STRINGER 14L. A 1.5 INC H CRACK WAS ALSO FOUND IN RIGHT CIRCUMFERENTIAL FRAME REINFORCEMENT PLATE AT STA 804, STRINGER 14R. FRAME REINFORCEMENT ANGLE REPAIRS WERE ACCOMPLISHED IAW SRM 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 1998012200072 19980122 00072 NM 1998 1 22 CALA9800036 1 19980114 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1263 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE ATTACH ANGLE IN AFT STAIR COMPARTMENT ON LT SIDE AT STA 1263. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-30-2. 2 L 7 3 4F A3WE 1998012200073 19980122 00073 NM 1998 1 22 CALA9800037 1 19980114 A 5320 CLIP BOEING 727 727227 1384078 NM BS 1283 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1.5 INCH CRACK IN FRAME TO STRINGER CLIP IN AFT STAIR COMPARTMENT ON RT SIDE AT STA 1283. THE STRING ER CLIP WAS REMOVED AND A NEW CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200074 19980122 00074 NM 1998 1 22 CALA9800038 1 19980114 A 5320 CLIP BOEING 727 727227 1384078 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN CLIPS ATTACHED TO BULKHEAD ON LT SIDE IN AFT STAIR COMPARTMENT AT STA 1183, WL 270 AN D WL 273. THE CLIPS WERE REMOVED, NEW CLIPS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200075 19980122 00075 NM 1998 1 22 9800566608 1 19980113 A 3260 SENSOR BOEING 747 747151 1384891 NM RT MLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 608US 19785 DURING CLIMB, THE RED LANDING GEAR LIGHT ILLUMINATED AND BOTH THE PRIM AND ALT GEAR INDICATED R BODY DOWN. RECYCLED LAN DING GEAR. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. SECURED ALL PRIMARY AND ALTERNATE INDICATOR CARDS AND REPLACED RIGHT BODY LANDING GEAR PRIMARY DOWN AND LOCK SENSOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998012200076 19980122 00076 WP 1998 1 22 9800579615 1 19980111 A 7331 8TJ55GAN1 POWER SUPPLY DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RT ENGINE INOPERATIVE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 615NW 47129 NR 2 FUEL FLOW INDICATION BECAME ERRATIC DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GA TE. MAINTENANCE PLACED THE NR 2 FUEL FLOW INDICATOR ON MEL. THE AIRCRAFT WAS RELEASED AND CONTINUED AS SCHEDULED. THE FUEL FLOW INDICATOR POWER SUPPLY WAS SUBSEQUENTLY REPLACED, OPERATIONAL CHECK WAS SATISFACTORY. 2 L 7 2 4F 4 F A6WE E2EA 1998012200077 19980122 00077 WP 1998 1 22 9800581220 1 19980110 A 2840 LIGHT DOUG DC10 DC1030 3023501 WP FUEL TRANS SYST ILLUMINATED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 220NW 46577 AFTER TAKEOFF, FUEL SCHEDULE LIGHT ILLUMINATED IN FLIGHT. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED TEST OF OUTBOARD FUEL TRANSFER SYSTEM, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998012200078 19980122 00078 EU 1998 1 22 9800593223 1 19980111 A 3231 201122008 UPLOCK AIRBUS 320 A320211 3930320 EU LT MLG DOOR FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 323US 272 DURING APPROACH FOLLOWING LANDING GEAR EXTENSION, LEFT MAIN GEAR DOOR INDICATED OPEN. RECYCLED LANDING GEAR AND RECEIVE D SAME INDICATION, LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT GEAR DOOR UPLOCK ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998012200079 19980122 00079 WP 1998 1 22 9800609878 1 19980112 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 5 THRU 8 INOPERATIVE. REPLACED BATTERIES, OPERA TIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998012200080 19980122 00080 WP 1998 1 22 9800619883 1 19980110 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 671MC 47660 FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 9 THRU 13 ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. REPLAC ED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200081 19980122 00081 WP 1998 1 22 9800629883 1 19980110 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 671MC 47660 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTERI ES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200082 19980122 00082 WP 1998 1 22 9800639948 1 19980109 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200083 19980122 00083 WP 1998 1 22 9800649948 1 19980106 A 3350 WIRES DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8929E 45866 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY LIGHTS AT ROW 6 INOPERATIVE. REPAIRED BROKEN WIRES, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200084 19980122 00084 WP 1998 1 22 9800659970 1 19980111 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200085 19980122 00085 WP 1998 1 22 9800669988 1 19980111 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8944E 47167 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1998012200086 19980122 00086 WP 1998 1 22 9800679607 1 19980112 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 607NW 47232 EMERGENCY LIGHTS AT GALLEY DOOR AND ON SIDES OF FORWARD CABIN SEATS ILLUMINATED DURING FLIGHT. REPLACED POWER SUPPLY AT GALLEY DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200087 19980122 00087 WP 1998 1 22 9800689611 1 19980109 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 611NA 47435 FLOOR PROXIMITY EMERGENCY LIGHTS AT OVERWING EXITS ILLUMINATED DURING FLIGHT. REPLACED POWER SUPPLY AT FS 657 AND BATTE RIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200088 19980122 00088 WP 1998 1 22 9800699756 1 19980111 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 756NW 47180 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT FORWARD GALLEY DOOR, FORWARD CABIN OVERHEAD, FLOOR PROXIMI TY, AND AFT STAIRS INOPERATIVE. REPLACED BATTERIES AND REPAIRED WIRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200089 19980122 00089 WP 1998 1 22 9800709758 1 19980111 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT AND FIRST FOUR RIGHT MAIN CABIN EMERGENC Y LIGHTS INOPERATIVE. REPLACED BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200090 19980122 00090 WP 1998 1 22 9800719760 1 19980109 A 3350 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NW 47288 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY/BATTER IES OVER RIGHT LAVATORY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998012200091 19980122 00091 WP 1998 1 22 9800729878 1 19980112 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES I N POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200092 19980122 00092 WP 1998 1 22 9800739877 1 19980110 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT AFT OVERWING EXIT EMERGENCY LIGHT AND FLOOR PROXIMITY LIGHTS BETWEEN ROW S 19 THRU 22 INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200093 19980122 00093 WP 1998 1 22 9800749872 1 19980110 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 12, 13, AND 14 INOPERATIVE. REPLACED BATTER IES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200094 19980122 00094 1998 1 22 UPS98225454 4 19980113 A 3414 AIRSPEED IND BOEING 727 72727C 138400J NM LT COCKPIT MALFUNCTIONED A IPXA K NONE O OTHER CL CLIMB 1 SO 01 910UP 19117 INSPECTION TYPE-N/A, ON CLIMBOUT CAPTAINS AIRSPEED INDICATOR BEGAN DECREASING, FO'S AIRSPEED CONTINUED TO INCREASE. STB Y AIRSPEED INDICATED ZERO CAPTAINS ALTIMETER SHOWED 2800 FT/FOS SHOWED 4000. CONTINUED ERRONEOUS INDICATION FOUND STATI C LEAK AT STBY ALT/A/S INDICATOR, W/STATIC LINE CAPPED. REMOVED AND REPLACED STBY ALT/A/S IND W/REF TO M/M 34-12-06. P ERFORMED PITOT STATIC LEAK CK ON CAPTS/F/O PITOT STATIC SYS W/REFTO M/M 34-11-00. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1998012200095 19980122 00095 NM 1998 1 22 UPS98225455 1 19980112 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION ON TOP OF FLOORBEAM BS 328 RBL 12 TO 16 WL 208 TASK CARD NR C53-224-03-1B. REPLACED FLOOR BEAM DAMAGED SECTION PER SRM 53-10-1 AND 53-10-8. 2 L 7 3 4F A3WE 1998012200097 19980122 00097 NM 1998 1 22 UPS98225458 1 19980114 A 5312 BULKHEAD BOEING 727 72722C 138400F NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CRACK IN BS 178 BULKHEAD RBL 9, WL 232. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-9, 51-30-2. 2 L 7 3 4F A3WE 1998012200098 19980122 00098 NM 1998 1 22 UPS98225459 1 19980114 A 5230 FRAME BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, FWD CARGO DOOR INBD SIDE OF FRAME CRACKED BELOW UPLATCH HOOK. STOP DRILLED CRACK, FABRICATED REPAIR PARTS, INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200099 19980122 00099 NM 1998 1 22 UPS98225460 1 19980108 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 448-570 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 484 TO BS 570 BL 0 WL 208. CORROSION ON SEAT TRACK WAS FOUN D TO BE WITHIN LIMITS AFTER CLEAN UP. HOWEVER, DENTS WERE FOUND ON BS 490 AND BS 571 WHICH WERE OUT OF LIMITS. SEAT TR ACK WAS REPLACED FROM BS 470 TO BS 600 IN ACCORDANCE WITH SRM 53-10-5, SRM 51-30-5, SRM 51-30-8, SRM 51-10-2. 2 L 7 3 4F A3WE 1998012200100 19980122 00100 NM 1998 1 22 UPS98225461 1 19980108 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON TOP CHORD OF FLOORBEAM AT BS 620 RBL 10 WL 208. CORROSION ON CHORD FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998012200101 19980122 00101 NM 1998 1 22 UPS98225462 1 19980108 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT BS 480 LBL 45 RBL 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AS MARKED. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998012200102 19980122 00102 NM 1998 1 22 UPS98225463 1 19980112 A 5320 6516279149 LINK BOEING 727 7272A1 138407F NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.00-02) ON EXPANSION LINK AT BS 740 TO 755 LBL 45. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED LINK PER SRM 51-20-1, 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1998012200103 19980122 00103 NM 1998 1 22 UPS98225464 1 19980112 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272A1 138407F NM BS 520/610 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (2-224-01) GOUGES AND BARE METAL ON SEAT TRACK AT BS 520 BS 610, LBL 60, WL 208. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-05, 51-30-08, MM 51 -20-31, OHM 20-50-01. 2 L 7 3 4F A3WE 1998012200104 19980122 00104 WP 1998 1 22 UPS98825453 1 19980113 A 2150 PACK DOUG DC8 DC871F 302199D WP COCKPIT FUMES A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 748UP 45948 INSPECTION TYPE-N/A, REF LOG PAGE NR 985883 STRONG SMELL OF JET FUEL IN COCKPIT AS SOON AS EITHER PACK IS TURNED ON OR G ETS WORSE WITH RECIRC FAN ON. VISUALLY INSPECTED BELLY FOR EVIDENCE OF FUEL, NONE FOUND. REMOVED AND REPLACED L AND R COALESCER BAGS, L AND R PACKS GRD RUN OPS AND LK CK'S OK. 2 L 7 4 4F RT 4A25 1998012200105 19980122 00105 EU 1998 1 22 QXEA980024 1 19980111 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 EXIT LIGHT AT ROW 8 ON LEFT SIDE INOP. RELAMPED EXIT SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998012200106 19980122 00106 NM 1998 1 22 MWEA98021 1 19980113 A 7711 EPR SYST DOUG MD88 MD88 3023688 NM LT ENGINE ICED UP A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 31 601ME 49762 NR 1 ENG EPR FAILED TO FULL ACCELERATE. PERFORMED LOW SPEED ABORT AT TAKEOFF. MTC CLEARED ICE FROM EPR SYSYTEM LT ENG. 2 L 7 2 4F RT A6WE 1998012200107 19980122 00107 WP 1998 1 22 MWEA98022 1 19980114 A 3350 6011777 BATTERY PACK DOUG DC9 DC914 3022034 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 400ME 45727 DURING SERV CHK, FOUND LT NACELLE EMERG LIGHT INOP. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998012200108 19980122 00108 WP 1998 1 22 MWEA98023 1 19980115 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FWD CARGO DOOR SKIN FOUND DENTED. MTC REPAIRED IAW SRM 52-05 FIG 3. 2 L 7 2 4F A6WE 1998012200109 19980122 00109 WP 1998 1 22 MWEA98024 1 19980115 A 5522 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 LT ELEV OBRD TRAIL EDGE HAS APPROX 1 QUARTER INCH COUNTER SINK HOLE. MTC REPAIRED IAW SRM 55-03 FIG 15. 2 L 7 2 4F A6WE 1998012200110 19980122 00110 NM 1998 1 22 DL72W980073 1 19980106 A 5313 STRINGER BOEING 727 727247 138408F NM TAIL CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 DURING ROUTINE HMV, FOUND STRINGER CRACKED INSIDE ACCESS 9504ON RT SIDE 4TH BAY UP. REPAIRED PER M/M 55-30-0 ON NRC 6 68. 2 L 7 3 4F A3WE 1998012200111 19980122 00111 WP 1998 1 22 DLL14980074 1 19980112 A 5712 RIB LKHEED 1011 1011385115 5265015 WP WS 503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 LT WING IWS 503 RIB UPPER CAP WAS FOUND CRACKED FWD OF STGR 18. REPAIRED PER ERA 331153-14. 2 L 7 3 4F A23WE 1998012200112 19980122 00112 NM 1998 1 22 DL757980075 1 19980109 A 5330 143N3200 SKIN BOEING 757 757232 1384965 NM BS 502.5 LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 626DL 22916 THE WINDOW BELT SKIN AT FS 502.5 SUFFERED A LIGHTNING STRIKE REQUIRING A .75 DIAMETER HOLE TO CLEAN-UP THE DAMAGE. THE HOLE WAS REPAIRED WITH AN ALUMINUM DOUBLER INSTALLED PER ER/A 363663-14, REV A. 2 L 7 2 4F RT A2NM 1998012200113 19980122 00113 WP 1998 1 22 DLL19980076 1 19980109 A 5711 1617204101 SPAR LKHEED 1011 10113853 5265020 WP WS 319-346 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 763DL 193Y1197 DURING INSPECTION OF THE LT WING REAR SPAR, 3 FASTENER HOLES WERE FOUND WITH CRACK INDICATIONS. THE HOLES WERE OVERSIZE D, COLDWORKED, INSPECTED, BUSHED, AND NEW FASTENERS INSTALLED PER ER/A 363637-14AD, REV A. 2 L 7 3 4F A23WE 1998012200114 19980122 00114 WP 1998 1 22 DLL19980078 1 19980110 A 5330 1538960 SKIN LKHEED 1011 10113853 5265020 WP BS 1836 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 763DL 193Y1197 THE FUSELAGE SKIN WAS FOUND WITH A CRACK EMANATING FROM TWO DRAIN MAST HOLES AT FS 1836 BETWEEN STRINGERS 39 AND 40. TH E SKIN WAS CUT OUT TO REMOVE THE CRACKS AND AN ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 363649-14, REV A. 2 L 7 3 4F A23WE 1998012200115 19980122 00115 NM 1998 1 22 DL72K980079 1 19980109 A 5744 FLAP TRACK SHIM BOEING 727 727232 1384082 NM RT INBD TRACK MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 DURING INSPECTION PER DAL SI 4-58662-12AD (AD 90-07-05), THE LAMINATED SHIM OF THE RT INBD FLAP TRACK WAS FOUND MIGRATED BEYOND THE .25 ALLOWED LIMIT. THE MIGRATED SHIM WAS REINSTALLED PER AD REQUIREMENTS AND ACCOMPLISHED PER ER/A 363668- 14AD. 2 L 7 3 4F A3WE 1998012200116 19980122 00116 NM 1998 1 22 DL72L980082 1 19980112 A 5330 SKIN BOEING 727 727232 1384082 NM AIRSTAIR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 FOUND DURING F-1 LETTER CHECK, .25 INCH CRACK AT LT CORNER OF AFT AIRSTAIR CUTOUT. REPAIRED PER M/M 53-30-0. 2 L 7 3 4F A3WE 1998012200117 19980122 00117 NM 1998 1 22 DL72L980083 1 19980112 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT FRONT SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 A .75 INCH CRACK NR 3 SLAT O/B TRACK VERTICAL STIFFENER ON WING FRONT SPAR. REPLACED ANGLE PER M/M 57-20-21 NR 14. 2 L 7 3 4F A3WE 1998012200118 19980122 00118 NM 1998 1 22 DL72L980084 1 19980112 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 FOUND DURING F-1 LETTER CHECK, RIGHT ELEVATOR LWR SKIN DAMAGED O/B OF TAB CUTOUT. ALSO, RIGHT ELEVATOR REAR SPAR LWR LE G DAMAGED O/B OF TAB CUTOUT. SKIN REPAIRED PER 55-20-3 FIG 4. SPAR REPAIRED PER SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1998012200119 19980122 00119 NM 1998 1 22 DL72K980085 1 19980112 A 3350 SIGN 1000677 BOEING 727 727232 1384082 NM R1 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 413DA 2110 21233 R1 OVERHEAD EMERGENCY EXIT SIGN WILL NOT ILLUM WHEN SELECTED. REPLACED R1 OVERHEAD EMERGENCY EXIT LIGHT ASSY, CKS NML. 2 L 7 3 4F A3WE 1998012200120 19980122 00120 NM 1998 1 22 DL72W980087 1 19980106 A 2782 BRACKET BOEING 727 727247 138408F NM NR 5 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 ANGLE CRACKED ON O/B SIDE OF NR 5 SLAT ACTUATOR BRACKET. REPAIRED PER M/M 57-54-0 PG 805. 2 L 7 3 4F A3WE 1998012200121 19980122 00121 NM 1998 1 22 DL72S980088 1 19980112 A 5542 65233332 SKIN BOEING 727 727232 1384082 NM RUDDER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 THE UPPER RUDDER WAS FOUND WITH MULTIPLE CRACKS ON THE RT SKIN PANEL BETWEEN RS 220 AND 242. THE PANEL WAS ORIGINALLY A BONDED ALUMINUM ASSEMBLY WITH BEADED STIFFENERS, BUT HAD BEEN PREVIOUSLY REPLACED WITH A REPAIR PANEL OF DIFFERENT CONS TRUCTION. THE PANEL HAS BEEN REPLACED WITH A NEW SKIN PANEL WITH ANGLE STIFFENERS IN PLACE OF THE ORIGINAL BEADS. THE REPAIR HAS BEEN ACCOMPLISHED PER ER/A 363680-14, REV A. 2 L 7 3 4F A3WE 1998012200123 19980122 00123 NM 1998 1 22 DLM11980090 1 19980110 A 3350 L205301 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 807DE 48478 BAT 6 LOW LIGHTS DURING EMERGENCY LIGHTS TEST AFT SECTION EMERGENCY FLOOR LIGHTS AND SIGNS INOP. FOUND LT DOOR EMERGENC Y LIGHT ASSY SHORTED TO GROUND L2-531. REPLACED LIGHT ASSY, OPN NORMAL. 2 L 7 3 4F RT A22WE 1998012200124 19980122 00124 EA 1998 1 22 BIER9801049 2 19980114 A 8530 73857 RING PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA NR 4 CYLINDER BROKEN B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 3521S 1226 1226 317952107 L79768A AT 50 HOUR INSP DURING OIL SUCTION SCREEN INSP, FOUND .125 INCH METAL PIECE, CLOSER INSP REVEALED THAT IT WAS AN OIL RIN G PART. REMOVED CYL, FOUND OIL CONTROL RING BROKEN AND PISTON LAND BROKEN WITH HOLE WORN IN PISTON. SUBMITTER STATES T HIS SHOWS THE IMPORTANCE OF CLOSE EXAMINATION OF OIL SUCTION SCREEN AND FILTER AT OIL CHANGE. 1 L 7 2 3O 3 O A20SO E14EA 1998012200125 19980122 00125 WP 1998 1 22 RRXA98005 1 19980115 A 5730 57583869559978 SKIN DOUG DC8 DC873F 302199F WP WS 69.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT PREFORMED SB 75-88, FOUND HOLES 1 AND 5 IN SPAR AND SKIN CRACKED IN LEFT WING AT STA 69.5. F ABRICATED AND INSTALLED MODIFICATION REPAIR IAW SB 57-88 AND FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04114. 2 L 7 4 4F RT 4A25 1998012200227 19980122 00227 NM 1998 1 22 CALA9800039 1 19980114 A 3230 CONTROL CABLE BOEING 737 737217 1384464 NM RT MLG OUT OF ADJ A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14233 19887 THE LANDING GEAR HANDLE COULD NOT BE MOVED BEYOND THE OFF POSITION AFTER TAKEOFF. ABNORMAL PROCEDURES WERE COMPLIED WIT H AND THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG TELEFLEX CABLE OU T OF ADJUSTMENT. THE CABLE AND AIR SAFETY SENSOR WERE ADJUSTED IAW MM 32-09-200. A GEAR SWING WAS PERFORMED SEVERAL TI MES AND NO DEFECTS WERE NOTED. 2 L 7 2 4F A16WE 1998012200228 19980122 00228 NM 1998 1 22 CALA9800040 1 19980114 A 3230 651781914 ACTUATOR BOEING 737 7373T0 1384582 NM NLG LOCK INOPERATIVE A CALA O OTHER O OTHER AP APPROACH 1 SW 09 14324 23375 THE AIRCRAFT HAD A BRIEF HISTORY WHERE THE LANDING GEAR WAS SLOW TO EXTEND. REPLACING THE LANDING GEAR TRANSFER VALVE D ID NOT HELP. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK ACTUATOR AND NLG TRANSFER CYLINDER. AN OPERATIONAL TEST AND GEAR SWING WERE PERFORMED IAW MM 32-31 WITH NO FAULTS NOTED. 2 L 7 2 4F RT A16WE 1998012200229 19980122 00229 WP 1998 1 22 CALA9800041 1 19980114 A 3260 CONNECTOR DOUG DC9 DC932 3022066 WP LANDING GEAR FAILED A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 12514 48113 THE RT MLG GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH. A MANUAL GEAR EXTENSION WAS P ERFORMED, BUT THE LIGHT DID NOT COME ON. A TOWER FLY-BY WAS CONDUCTED AND THE GEAR WAS CONFIRMED DOWN AND LOCKED. THE A IRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PIN 5 AT PLUG ON RT MLG DOWNLOCK SWITCH BROKEN. THE PLUG AND SWITCH WERE REPLACED AND OPERATIONAL CHECK WAS GOOD. 2 L 7 2 4F A6WE 1998012200230 19980122 00230 NM 1998 1 22 CALA9800042 1 19980114 A 5311 FRAME BOEING 727 727227 1384078 NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .125 INCH CRACK AT HI-LOK IN FRAME AT STA 312 BETWEEN STRINGER 6R AND 7R. THE CRACKED AREA WAS CUT O UT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-40-5, AND 53-10-4. 2 L 7 3 4F A3WE 1998012200231 19980122 00231 NM 1998 1 22 CALA9800043 1 19980114 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 400-420 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT FS 400 TO 420, BBL 0. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS F ABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998012200232 19980122 00232 NM 1998 1 22 CALA9800044 1 19980114 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK AT SCREW HOLE IN INTERCOSTAL AT FS 720 TO 720A, BL 0. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200233 19980122 00233 NM 1998 1 22 CALA9800045 1 19980114 A 5320 DOUBLER BOEING 727 727227 1384078 NM BS 576 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND TWO 1 INCH CRACKS AT HI-LOK ON DOUBLER UPPER SIDE OF CARGO DOOR CUTOUT FRAME AT FS 576, STRINGER 18R. T HE FASTENERS AND DOUBLER WERE REMOVED, A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998012200234 19980122 00234 1998 1 22 9800753232 4 19980113 A 2210 SC47003 ACTUATOR AIRBUS 320 A320211 3930320 EU NR 1 YAW DAMPER LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 01 332NW 18846 18846 319 DURING CRUISE, CREW NOTICED GREEN HYDRAULIC FLUID QUANTITY DECREASING. DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED THE NR 1 YAW DAMPER ACTUATOR, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998012200235 19980122 00235 WP 1998 1 22 9800769959 1 19980113 A 3233 ACTUATOR DOUG DC9 DC931 3022065 WP NLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 919RW 47162 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION WITH LOUD AIRSTREAM NOISE. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR ACTUATOR, BUNGEE CYLINDER, AND CHECK VALVE. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1998012200236 19980122 00236 1998 1 22 9800779880 4 19980113 A 2397 WIRE DOUG DC9 DC951 3022051 WP AUDIO PANEL BROKEN A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 675MC 47651 FLIGHT CREW SMELLED SMOKE UPON ENTERING COCKPIT AT GATE. MAINTENANCE FOUND BROKEN WIRING CAUSING ARC AT OBSERVER'S AUDI O CONTROL PANEL. REPAIRED WIRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200237 19980122 00237 WP 1998 1 22 9800789151 1 19980113 A 3080 ANTI-ICE LIGHT DOUG DC9 DC914 3022034 WP COCKPIT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8909E 45770 WING ANTI-ICE BLUE LIGHT DID NOT ILLUMINATE WITH AIRFOIL ANTI-ICE SELECTED. FLIGHT WAS RETURNED TO MSP AND LANDED WITHO UT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND. 2 L 7 2 4F A6WE 1998012200238 19980122 00238 WP 1998 1 22 9800799105 1 19980111 A 2740 CIRCUIT BREAKER DOUG DC9 DC915 3022036 WP PRIMARY TRIM TRIPPED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 95S 47205 PRIMARY TRIM FAILED AFTER TAKEOFF. SECONDARY SYSTEM OPERATED NORMALLY. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT I NCIDENT. MAINTENANCE FOUND A PHASE CIRCUIT BREAKER POPPED BEHIND FORWARD FLIGHT ATTENDANT SEAT. RESET CIRCUIT BREAKER, OPERATIONAL CHECK OF PRIMARY TRIM FULL TRAVEL WAS NORMAL. REPLACED PRIMARY TRIM MOTOR AS A PRECAUTION. 2 L 7 2 4F A6WE 1998012200239 19980122 00239 WP 1998 1 22 9800809152 1 19980114 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHT AT ROW 16 INOPERATIVE. REPLACED BATTERY PACK, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200240 19980122 00240 WP 1998 1 22 9800819152 1 19980114 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200241 19980122 00241 WP 1998 1 22 9800829852 1 19980114 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING PERIODIC CHECK, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 7 THRU 9 INOPERATIVE. REPLACED BATTERIES, OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200242 19980122 00242 WP 1998 1 22 9800839611 1 19980113 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611NA 47435 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200243 19980122 00243 WP 1998 1 22 9800849872 1 19980110 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE MAINTENANCE INSPECTION, FOUND AFT STAIRWELL SIDEWALL EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012200244 19980122 00244 EA 1998 1 22 COMA9860011 1 19980114 A 3350 LIGHTS CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 LEFT AND RIGHT EXTERIOR FORWARD EMERGENCY LIGHTS INOPERATIVE. DEFERRED FORWARD EXTERIOR EMERGENCY LIGHTS IN ACCORDANCE WITH MEL 33-51-2. 2 L 7 2 4F RT A21EA 1998012200255 19980122 00255 NM 1998 1 22 98FDEA00031 1 19980115 A 5315 65187451 FLOORBEAM BOEING 727 72722 1384002 NM BS 880 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 UPON REMOVAL OF RADIUS FILLER, FOUND DEEP GOUGE AT BS 880, LBL 15, WL 201.5. *S/D* BLENDED OUT GOUGE, CRACK AND CORROS ION AT BS 880, LBL 15, WL 201.5 ORIGINAL THICKNESS WAS .1, MATERIAL REMOVED WAS .045. BLENDOUT AREA IS .3 X .2, FOUND T O BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPAIRED FLOORBEAM PER FED-EX EA 7-5310-37396. 2 L 7 3 4F A3WE 1998012200256 19980122 00256 NM 1998 1 22 98FDEA00032 1 19980114 A 3020 ANTI-ICE DUCT BOEING 727 727227 1384078 NM NR 2 ENGINE BLOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 496FE 21670 ON CLIMBOUT AT 3000, LWR AFT BODY OVERHEAT LIGHT ILLUM. RAN CHECK LIST AND AFTER RETARD NR 2 THROTTLE LIGHT WENT OUT. E NG ANTI-ICE WAS OPENED JUST PRIOR TO ILLUM OF LWR AFT BODY OVERHEAT LIGHT. DECLARED EMERGENCY AND RETURN TO MEM. FOUND NR 2 ENG COWL THERMAL ANTI-ICE DUCT BLOWN. REMOVED AND REPLACED FIREWALL COUPLING, DUE VALVE INSTALLATION. DUCT REPLA CEMENT AND SEALANT ON NR 2 ENGINE SIDE OF FIREWALL BRACE ROD IN AFT STAIRWELL REMOVED. REMOVED PANEL LEFT SIDE VERTICAL STABILIZER, PANEL ON TRUCK. REINSTALL THERMAL ANTI-ICE VALVE AND DUCT. SEALED FIREWALL SIDE OF COUPLING. RAN NR 2 EN G, NO LEAKS NOTED AND OPERATION NORMAL. REINSTALL PANEL ON STAB AND SUPPORT ROD, OK FOR SERVICE. 2 L 7 3 4F A3WE 1998012200257 19980122 00257 NM 1998 1 22 98FDEA00033 1 19980114 A 3260 CONNECTOR BOEING 727 72722C 138400F NM RT MLG DOOR DIRTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 102FE 19193 THE RIGHT GEAR DOOR REMAINED OPEN AFTER GEAR HANDLE WAS PLACED UP. AFTER 2 MIN THE GEAR WAS RECYCLED PER RED TABS. THE RIGHT GEAR DOOR CONSISTENTLY IS SLOW TO CLOSE 2 MIN IN ON PAST 3 LANDINGS. OPERATED RIGHT GEAR DOOR PER MAINTENANCE MA NUAL 32-62 DOOR TEST GOOD. REMOVED CANNON PLUG FROM DOOR SWITCH FOUND WATER AND DIRT ON CONTACTS. CHECKED DOOR OPERATI ON, DOOR CHECKS GOOD. 2 L 7 3 4F A3WE 1998012200258 19980122 00258 NM 1998 1 22 98FDEA00034 1 19980114 A 3260 GEAR LIGHTS BOEING 727 72725C 138400H NM LANDING GEAR MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 127FE 19719 AFTER GEAR RETRACTION, ALL FOUR RED GEAR LIGHTS AND THE GREEN RIGHT GEAR LIGHT REMAINED ON WITH THE GEAR HANDLE IN THE U P POSITION. ALL GEAR DOORS INDICATED CLOSED WITH HANDLE IN OFF POSITION THE GREEN RIGHT GEAR LIGHT REMAINED ON. AGAIN ALL GEAR DOORS INDICATED CLOSED, WITH GEAR HANDLE DOWN, NORMAL INDICATIONS (3 GREEN, NO RED) APPEARED. RETURNED TO ATL. *S/D* SEE PREV HISTORY. REMOVED AND REPLACED LAND GEAR ASSY UNIT AND RE-KEY RACK AS PER 32-09-111 PAGE 401 UNIT KEY INCORRECTLY. STEP 5 POS IND AND WARN FAILING. TAIL SKID LIGHT COMES ON PER M/M SUPPLEMENT TAIL SKID OPER IS OK. REPLA CED RELAY R145. 2 L 7 3 4F A3WE 1998012200259 19980122 00259 NM 1998 1 22 98FDEA00035 1 19980115 A 5320 65504531 TEE FITTING BOEING 727 72722 1384002 NM BS 336 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 WHILE WORKING NR0328, FOUND CORROSION ON TEE FITTING AT BS 336, LBL 17, WL 150. *S/D* REMOVED AND REPLACED TEE FITTING AT BS 336, LBL 17, WL 155 IAW FED-EX DRAWING 65-18415. 2 L 7 3 4F A3WE 1998012200260 19980122 00260 WP 1998 1 22 CKSA98001 1 19980114 A 7931 WIRE DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 2 ENG PYLON BROKEN A CKSA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 23 806CK 45932 642294 NR 2 OIL LIGHT LOW PRESS CAME ON, T/R AND T/R DOOR LIGHT CAME ON, GEN FAIL LIGHT CAME ON, OIL PRESS THEN DROPPED AS DID OIL QUANTITY. COMPLETED NR 2 ENGINE SHUTDOWN. LATER AT TOD NR 2 ENGINE FIRE WARNING LIGHT (1/2 SYSTEM) CAME ON, FIRED BOTTLE. REPAIRED WIRING ON NR 2 ENGINE PYLON. NR 2 OIL LOW PRESS LT, T/R AND TR DOOR LIGHT, OIL PRESS INDICATOR, OIL Q UANTITY AND ENGINE FIRE WARNING ALL OPS CHECK GOOD ON ENGINE RUN. REMOVED AND REPLACED NR 2 FIRE BOTTLE IAW DC8 MM 26-4 -1. 2 L 7 4 4F 4 F 4A25 1E8 1998012200261 19980122 00261 EU 1998 1 22 MALA975884 1 19980113 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 109XJ 340A109 DURING INSPECTION, EMERGENCY LIGHT AT 9D INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012200262 19980122 00262 EU 1998 1 22 MALA975885 1 19980113 A 3350 1317 LAMP SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 107XJ 340A107 DURING INSPECTION, EMERGENCY LIGHTS IN ROW 4 AND 6 INOP. MAINTENANCE RELAMP EMERGENCY LIGHTS IN ROWS 4 AND 6, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012200263 19980122 00263 NM 1998 1 22 MALA975886 1 19980114 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998012200264 19980122 00264 NM 1998 1 22 MALA975887 1 19980115 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 829MA 335 DURING INSPECTION, ONE AFT FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998012200265 19980122 00265 EU 1998 1 22 MALA975888 1 19980113 A 2611 7213000300 SMOKE DETECTOR BAC 146 AVRO146RJ85A 1500097 EU CARGO BAY INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 501XJ E2208 ON PREFLIGHT THE CREW WAS UNABLE TO TEST THE ELECTRICAL BAY SMOKE DETECTION SYSTEM. MAINTENANCE REPLACED THE SMOKE DETE CTOR IN THE FORWARD CARGO BAY, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998012200266 19980122 00266 EU 1998 1 22 MALA975889 1 19980110 A 2421 31342001 GENERATOR SAAB SF340 SF340A 7850100 EU LEFT FAILED A MALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 15 68XJ 068 AFTER TAKEOFF, THE LEFT AC GENERATOR AND LEFT INTAKE CAUTION LIGHTS ILLUMINATED, WOULDN'T RESET. AIRCRAFT RETURNED TO R HI. MAINTENANCE REPLACED THE LEFT AC GENERATOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012200267 19980122 00267 NE 1998 1 22 MALA975890 2 19980112 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A MALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 15 48XJ 048 AFER TAKEOFF, THE LEFT ENGINE TORQUE SURGED TO 120 PERCENT, ALL ENGINE GAUGES APPEARED TO BE NORMAL. AS A PRECAUTIONARY SHUTDOWN ENGINE. AIRCRAFT RETURNED TO ATY. MAINTENANCE REPLACED THE LEFT ENGINE, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1998012200268 19980122 00268 WP 1998 1 22 CALA9800046 1 19980114 A 4920 TURBINE GARRETT 3812761 DOUG DC9 DC981 3022081 WP APU FAILED A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 13881 P0552 48045 THE APU WAS STARTED AFTER LANDING IN EWR AND RAN NORMALLY FOR A WHILE AND THEN FLAMED OUT. THE APU WOULD NOT RESTART. M AINTENANCE FOUND AN UNCONTAINED TURBINE WHEEL SEPARATION. THE SHROUD DID NOT CONTAIN THE TURBINE WHEEL WHICH CAUSED DAM AGE TO THE APU FIREWALL. THE APU WAS REMOVED AND REPLACED IAW MM 49-10-00. A SMALL HOLE FOUND IN THE APU FIREWALL WAS REPAIRED. APU OPERATION CHECKED NORMAL WITH NO LEAKS NOTED. *S/D* INVESTIGATION REVEALED THAT THE CAUSE OF TURBINE WH EEL FAILURE WAS DUE TO AN INCLUSION CREATED IN THE TURBINE WHEEL DURING THE MANUFACTURING PROCESS. 2 L 7 2 4F A6WE 1998012200269 19980122 00269 NM 1998 1 22 CALA9800047 1 19980114 A 5320 DOUBLER BOEING 727 727227 1384078 NM BS 604-608 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND THREE CRACKS AT HI-LOKS ON DOUBLER UPPER SIDE OF CARGO DOOR FRAME CUTOUT BETWEEN FS 604 TO 608, STRINGE R 10R. THE CRACKS WERE .25 TO 1 INCH LONG. THE FASTENERS AND DOUBLER WERE REMOVED. A NEW DOUBLER WAS FABRICATED AND I NSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998012200270 19980122 00270 NM 1998 1 22 CALA9800048 1 19980114 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK IN END OF STRINGER 15L AT STA 720C. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS FABRICA TED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5. 2 L 7 3 4F A3WE 1998012200271 19980122 00271 NM 1998 1 22 CALA9800049 1 19980114 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. THE CRACKED AREAS WERE CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3, FIGURE 5. 2 L 7 3 4F A3WE 1998012200272 19980122 00272 NM 1998 1 22 CALA9800050 1 19980114 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 996, RBL 36. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS F ABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6. 2 L 7 3 4F A3WE 1998012200273 19980122 00273 NM 1998 1 22 CALA9800051 1 19980114 A 5530 GUSSET BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK AT TOP CORNER AND A .5 INCH CRACK AT LOWER CORNER OF GUSSET ON RT SIDE OF VERTICAL STAB ILIZER AT STRINGER 9 BETWEEN RIB NR 6 AND NR 7. THE GUSSET PLATE WAS REMOVED, A NEW GUSSET PLATE WAS FABRICATED AND INS TALLED IAW SRM 55-30-2. 2 L 7 3 4F A3WE 1998012200274 19980122 00274 NM 1998 1 22 CALA9800052 1 19980114 A 2782 BRACKETS BOEING 727 727227 1384078 NM LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998012200275 19980122 00275 NM 1998 1 22 CALA9800053 1 19980114 A 2782 BRACKETS BOEING 727 727227 1384078 NM LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK IN INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1998012200276 19980122 00276 NM 1998 1 22 CALA9800054 1 19980114 A 5753 SKIN BOEING 727 727227 1384078 NM LT TE MIDFLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND LT WING INBOARD MIDFLAP SKIN CORRODED OUTBOARD OF INBOARD CARRIAGE MOUNT AREA. A SKIN REPAIR WAS INSTA LLED IAW SRM 57-50-4. 2 L 7 3 4F A3WE 1998012200277 19980122 00277 NM 1998 1 22 CALA9800055 1 19980114 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 3 SLAT INBOARD HOOK ATTACHES. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4. 2 L 7 3 4F A3WE 1998012200278 19980122 00278 NM 1998 1 22 CALA9800056 1 19980114 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .25 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE SKIN AT AFT END OF CUTOUT WHERE NR 4 SLAT OUTBOARD HOOK ATTACHES. A DOUBLER WAS INSTALLED IAW SRM 57-30-4. 2 L 7 3 4F A3WE 1998012200279 19980122 00279 NM 1998 1 22 CALA9800057 1 19980114 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING FIRST UPPER STRINGER FROM REAR SPAR, ABOVE RIB AT WS 656.50 . THE FASTENERS AND CLAMPS WERE REMOVED. THE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050. 2 L 7 3 4F A3WE 1998012200280 19980122 00280 NM 1998 1 22 CALA9800058 1 19980114 A 5730 SKIN BOEING 727 727227 1384078 NM WS 224 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 2 INCH CRACK IN LEADING EDGE SKIN AT DOUBLER STRAP INSIDE LT WING DIRECTLY ABOVE NR 2 LEADING EDGE FL AP ACTUATOR AT WS 224. THE CRACKED DOUBLER WAS REMOVED, A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998012200281 19980122 00281 NM 1998 1 22 CALA9800059 1 19980114 A 5712 RIB BOEING 727 727227 1384078 NM WS 130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STA 130 ABOVE HOT AIR DUCT PLENUM. ALS O, A .5 INCH CRACK WAS FOUND INSIDE LT WING LEADING EDGE AT RIB LEADING EDGE STATION 130 BELOW LIGHTENING HOLE AREA. DO UBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1998012200282 19980122 00282 NM 1998 1 22 CALA9800060 1 19980114 A 5730 SKIN BOEING 727 727227 1384078 NM WS 106 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND FOUR .5 INCH CRACKS AROUND FASTENERS OUTBOARD OF LAMP LIGHT IN WING LEADING EDGE INTERNAL SKIN AT FSS 1 06. THE CRACKED AREAS WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-10-6. 2 L 7 3 4F A3WE 1998012200283 19980122 00283 NM 1998 1 22 CALA9800061 1 19980114 A 5712 RIB BOEING 727 727227 1384078 NM WS 130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB INBOARD OF NR 4 LEADING EDGE FLAP AT LEADING EGDE STA 130. THE CRACK WAS STOP DRILLED AND AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-1, AND 51-30-2. 2 L 7 3 4F A3WE 1998012200284 19980122 00284 NM 1998 1 22 CALA9800062 1 19980114 A 5712 RIB BOEING 727 727227 1384078 NM WS 106.8 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN LOWER EDGE AT FSS 106.8. AN ANGLE RE PAIR WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998012200285 19980122 00285 NM 1998 1 22 CALA9800063 1 19980114 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .75 INCH CRACK IN RT WING STRINGER AT WS 656.5, TOP OF RIB ATTACH POINT ACCESS THROUGH PANEL 7617. T HE CRACK WAS STOP DRILLED AND THE AREA WAS REPAIRED IAW EA 5762-01050. 2 L 7 3 4F A3WE 1998012200286 19980122 00286 NM 1998 1 22 CALA9800064 1 19980114 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 629 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5 INCH CRACK AT FASTENER HOLE IN LT WING SECOND UPPER STRINGER FROM REAR SPAR ABOVE RIB AT WS 629. T HE FASTENERS AND CLAMPS WERE REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED, REPAIR PARTS WERE FABRICATED AND INST ALLED IAW EA 5762-01050 AND SRM 51-10-6. 2 L 7 3 4F A3WE 1998012200287 19980122 00287 WP 1998 1 22 CALA9800065 1 19980115 A 2612 ASL0387503 FIRE DETECTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE PINCHED A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 533MD 18444 46553 455784 THE NR 3 ENGINE A-FIRELOOP WARNING LIGHT ILLUMINATED DURING CLIMBOUT. A FIRE TEST WAS PERFORMED PER CHECKLIST AND THE B -LOOP TESTED GOOD. THE A-SYSTEM HAD A HISTORY OF FIRE WARNINGS. THE FLIGHT WAS CONTINUED USING B-LOOP ONLY. THE AIRCR AFT LANDED AT EWR WITHOUT FURTHER WARNINGS. MAINTENANCE FOUND THE FORWARD FAN FIRE DETECTION LOOP PINCHED. THE FORWARD FAN FIRE DETECTION LOOPS A AND B WERE REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1998012200288 19980122 00288 NM 1998 1 22 CALA9800066 1 19980115 A 5530 STRINGER BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER STRINGER NR 8 BETWEEN RIB NR 8 AND NR 9. THE FASTENER S WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2. 2 L 7 3 4F A3WE 1998012200289 19980122 00289 NM 1998 1 22 CALA9800067 1 19980115 A 5530 STRINGER BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER STRINGER NR 9 BETWEEN RIB NR 7 AND NR 8. THE CRACK WA S LOCATED AT ATTACH BOLT. THE FASTENERS WERE REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-2. 2 L 7 3 4F A3WE 1998012200290 19980122 00290 EU 1998 1 22 9800853248 1 19980112 A 2150 SKIN VALVE WARN AIRBUS 320 A320212 EU COCKPIT ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 348NW 410 DURING TAKEOFF ROLL, RECEIVED VENT SKIN VALVE FAULT MESSAGE. ABORTED TAKEOFF AT 50 KTS. MAINTENANCE TROUBLESHOOTING RE VEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1998012200291 19980122 00291 NE 1998 1 22 9800869996 2 19980114 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LEFT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8932E 47141 666774 DURING TAKEOFF ROLL, THE LEFT ENGINE WOULD NOT REACH TARGET EPR. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANC E PERFORMED OPERATIONAL CHECK OF THE LEFT ENGINE, ALL PARAMETERS WERE NORMAL. PROBLEM COULD NOT BE DUPLICATED. 2 L 7 2 4F 4 F A6WE E2EA 1998012200292 19980122 00292 WP 1998 1 22 9800879982 1 19980113 A 5350 CLIPS DOUG DC9 DC932 3022066 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 982US 45790 DURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO PULL THE INTERIOR RELEASE HANDLE FROM CLIP AND TO DEPLOY TAIL CONE. ADJUSTED HANDLE CLIPS AND RIGGED TAIL CONE DEPLOYMENT SYSTEM, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998012200293 19980122 00293 WP 1998 1 22 9800889301 1 19980113 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 301RC 48054 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE INTERIOR HANDLE FROM CLIPS. ADJUS TED CLIPS, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998012200294 19980122 00294 NE 1998 1 22 9800899928 2 19980112 A 7220 NOSE BULLET DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LT ENGINE OBSTRUCTED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8921E 45836 657294 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE WOULD NOT REACH TARGET EPR. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE . MAINTENANCE REMOVED OBSTRUCTION FROM THE LEFT ENGINE NOSE BULLET, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998012200295 19980122 00295 WP 1998 1 22 9800909855 1 19980111 A 7711 PT7 LINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE MOISTURE CONTAM A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 764NC 47717 696705 DURING TAKEOFF ROLL AT 85 KNOTS, THE RIGHT ENGINE WOULD NOT REACH TARGET EPR. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REMOVED MOISTURE FROM PT7 LINES, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1998012200296 19980122 00296 EU 1998 1 22 9800913209 1 19980114 A 2611 SMOKE DETECTOR AIRBUS 320 A320211 3930320 EU CARGO COMPT MALFUNCTIONED A NWAA A F UNSCHED LANDING ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 309US 118 DURING CLIMB, RECEIVED MESSAGE SMOKE AFT CARGO SMOKE. CREW DISCHARGED AFT CARGO FIRE EXTINGUISHER. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. NO INDICATION OF FIRE OR SMOKE UPON INSPECTION OF CARGO COMPARTMENT. MAINTENANCE TROUBLESHOO TING REVEALED NO DISCREPANCIES. 2 L 7 2 4F RT A28NM 1998012200297 19980122 00297 1998 1 22 9800929954 4 19980113 A 2565 13621228 SLIDE DOUG DC9 DC931 3022065 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 921RW 13 13 47164 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998012200298 19980122 00298 WP 1998 1 22 9800939102 1 19980115 A 3010 TEMP SENSOR DOUG DC9 DC915 3022036 WP RIGHT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 92S 47064 RIGHT ICE PROTECTION TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED ANTICIPATOR, THERMOSTAT, AND RIGHT TEMPERATURE SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200299 19980122 00299 NM 1998 1 22 UPS98225465 1 19980112 A 5347 BAC1520792 SEAT TRACK BOEING 727 7272A1 138407F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK AT BS 720C TO BS 745 RBL 25, WL 208. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED CORRODED SEAT TRACK, FABRICATED, INSTALLED REPAIR SEAT TRACK IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998012200300 19980122 00300 NM 1998 1 22 UPS98225466 1 19980112 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION AT BS 380 RBL 45 TO 63 WL 208 ON UPPER SURFACE OF FLOORBEAM AND BOTTOM SURFACE AT FASTENER HOLES (C53-224-01.05-01). CORROSION REMOVED IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. REPAIRED FLOORBEAM IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998012200301 19980122 00301 NM 1998 1 22 UPS98225467 1 19980112 A 5754 65162256A LUG BOEING 727 7272A1 138407F NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, NR 4 K-FLAP HAS CORROSION ON O/B UPPER LUG WHERE BONDING JUMPER ATTACHES. REMOVED AND REPLACED NR 4 K-FLAP IAW OHM 57-51-21 AND MM 27-81-01. 2 L 7 3 4F A3WE 1998012200302 19980122 00302 NM 1998 1 22 UPS98225468 1 19980113 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON TOP OF FLOORBEAM 950 RBL 25 TO 65. CORROSION REWORK OUT OF LIMITS I AW SRM 53-10-1. REPAIRED 950 FLOORBEAM RBL 25 TO 65 IAW TRAMCO/BFG EWO 98-2012 (UPS FILE 727-53-1983). 2 L 7 3 4F A3WE 1998012200303 19980122 00303 NM 1998 1 22 UPS98225469 1 19980113 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (4-25-02) AND MECHANICAL DAMAGE ON SEAT TRACK WELL AND TOOTH BETWEEN BS 980 TO 1010 LBL 25 . CORROSION REWORK OUT OF LIMTS IAW SRM 53-10-1. MECHANICAL DAMAGE WITHIN LIMITS IAW SRM 53-10-1. SEAT TRACK WAS REMO VED AND REPLACED IAW SRM 51-30-2, 51-10-02, 53-10-05. 2 L 7 3 4F A3WE 1998012200304 19980122 00304 NM 1998 1 22 UPS98225470 1 19980113 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 783.95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CRACK INDICATION NOTED AT FASTENER HOLE IN FRAME AT BS 783.95 APPROX WL 207 APPROX LBL 65. REPAIRED CRACK IN FRAME STA 783.95 LBL 65 WL 207 IAW UPS EO B727-5310-5474. 2 L 7 3 4F A3WE 1998012200305 19980122 00305 NM 1998 1 22 UPS98225472 1 19980113 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (4-25-02) ON SEAT TRACK FLANGE BETWEEN BS 720D TO 720F LBL 25. CORROSION REWORK OUT OF L IMITS IAW SRM 53-10-1. REMOVED AND REPLACED SEAT TRACK BS 720D TO BS 720F LBL 25 IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998012200306 19980122 00306 NM 1998 1 22 UPS98225473 1 19980114 A 5320 655615337 ANGLE BOEING 727 7272A1 138407F NM BS 380-410 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AT MOP SILL AT BOTTOM OF RT ENTRY DOOR BS 380 TO 410 RBL 63 WL 208 TOP AND BOTTOM SURFACES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON LWR SUPPORT ANGLE IAW 51-10-06, 53-10-1. REMOVED A ND REPLACED ANGLE IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998012200307 19980122 00307 NM 1998 1 22 UPS98225474 1 19980115 A 5320 CHORD BOEING 727 72722C 138400F NM BS 380/328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-01) ON NLG WHEEL WELL MID CHORD BS 318 AND BS 328 RBL 15 WL 170. REMOV ED CORROSION PART OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, 51-10-2, 51-20-4, 51-20-151. 2 L 7 3 4F A3WE 1998012200308 19980122 00308 NM 1998 1 22 UPS98225475 1 19980115 A 5320 CHORD BOEING 727 72722C 138400F NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-01) ON NLG DOGHOUSE FLOOR SUPPORT CHORD AT BS 351 RBL 30 WL 170 (BELOW FLOOR). REMOVED CORROSION PART OUT OF LIMITS, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-21-151, 51-10-2, 51-30-2 , 51-20-4 AND 51-30-5. 2 L 7 3 4F A3WE 1998012200309 19980122 00309 NM 1998 1 22 UPS98225477 1 19980114 A 5320 BAC14902888 CHORD BOEING 727 7272A1 138407F NM BS 1166 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON NUT PLATE AND FLOORBEAM AT STA 1166, LBL 10, WL 208. REMOVED CORROS ION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REPAIRED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998012200310 19980122 00310 NM 1998 1 22 UPS98225478 1 19980114 A 5330 SKIN BOEING 727 7272A1 138407F NM BS 1090 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, WHILE CLOSING FLOOR ON CARD 656802 FOUND CORROSION ON SKIN AT BS 1090 AT STR 28R. REMOVED CORROSION IAW SRM 51-10-6 REWORK OUT OF LIMITS IAW SRM 53-30-1. REPAIRED SKIN AT STA 1090 STR 28R IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1998012200311 19980122 00311 WP 1998 1 22 UPS98825479 1 19980111 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 420 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN CABIN SEAT TRACK AT FS 420 RBL 60 HAS LUG WORN BEYOND LIMITS. REPAIRED IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998012200312 19980122 00312 WP 1998 1 22 UPS98825480 1 19980103 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 55-360 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN CABIN SEAT TRACK LBL 62 FS 55 TO 360 IS WORN BEYOND LIMITS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-7-3. 2 L 7 4 4F RT 4A25 1998012200316 19980122 00316 WP 1998 1 22 UPS98825484 1 19980112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 861 WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, SEAT TRACK AT FS 861 RBL 47 IS WORN BEYOND LIMITS. REPAIRED IAW SRM ADDN DC8-5340-7779. 2 L 7 4 4F RT 4A25 1998012200318 19980122 00318 WP 1998 1 22 UPS98825486 1 19980115 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYP-N/A, SKIN BULGED AND HAS TWO POPPED HI-LOKS STA 1220 LONGERON 36. POSSIBLE CORROSION JUST UNDER AFT SIDE OF NR 3 PIT. REPAIRED PER UPS EO DC8-5330-10018A APPX B AND C ONLY. 2 L 7 4 4F RT 4A25 1998012200319 19980122 00319 WP 1998 1 22 UPS98825487 1 19980115 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE-N/A, BULGED SKIN AT STA 1150 LONGERON 15L. ALSO, HAS TWO POPPED HI-LOK, POSSIBLE CORROSION. REPAIRED D AMAGED AREA AS PER EO DC8-5330-10018 APPX B AND C ONLY. 2 L 7 4 4F RT 4A25 1998012200320 19980122 00320 EU 1998 1 22 WWMA9800012 1 19980114 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 297AE 12620 340B297 CARGO SMOKE LIGHT CAME ON IN FLIGHT, CREW FIRED THE NR 1 CARGO FIRE EXTINGUISHER. MAINTENANCE REPLACED THE FWD AND AFT CARGO SMOKE DETECTORS AND THE NR 1 CARGO FIRE BOTTLE. BOTH DETECTORS WERE ORIGINAL EQUIPMENT. 2 L 7 2 4T RT A52EU 1998012200321 19980122 00321 WP 1998 1 22 ABXA9800015 1 19980116 A 5730 5912369509 PANEL DOUG DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING C-CHECK, FOUND FUEL ACCESS PANEL NR 5912369-509 CORRODED BEYOND LIMITS. REPLACED PANEL. 2 L 7 2 4F A6WE 1998012200322 19980122 00322 WP 1998 1 22 ABXA9800016 1 19980116 A 5414 995819114 SKIN DOUG DOUG DC9 DC941 302207N WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND THE RIGHT ENGINE PYLON UPPER SKIN CRACKED INBD OF AFT ENGINE MOUNT AND 6 PULLED FASTENERS IN SAME AREA. REPAIRED SKIN IAW DC9 SRM 51-20-0. 2 L 7 2 4F A6WE 1998012200323 19980122 00323 WP 1998 1 22 ABXA9800017 1 19980116 A 5315 99115451 FLOORBEAM DOUG DOUG DC9 DC941 302207N WP BS 408 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND FLOORBEAM CORRODED AT STA 408 ABOVE THE FWD LOWER CARGO DOOR. REPAIRED FLOORBEAM IAW ABX REA D953 -22195 MR. 2 L 7 2 4F A6WE 1998012200324 19980122 00324 WP 1998 1 22 ABXA9800018 1 19980116 A 5400 991550032 ANGLE DOUG DOUG DC9 DC933F 302207A WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND ANGLE IN NR 2 ENGINE PYLON CRACKED AT AFT LOWER SPAR STRAP ABOVE PANEL 8212. REPLACED ANGLE IAW D C9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998012200325 19980122 00325 WP 1998 1 22 ABXA9800019 1 19980116 A 5400 591326241 ANGLE DOUG DOUG DC9 DC933F 302207A WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND UPPER PYLON ATTACH ANGLE CRACKED AT STA 980. REPAIRED ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1998012200326 19980122 00326 WP 1998 1 22 ABXA9800020 1 19980116 A 5320 991015529 PRESS PANEL DOUG DOUG DC9 DC933F 302207A WP RTMLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND RT WHEEL WELL PRESSURE PANEL CRACKED OUTBOARD AND AFT OF MAIN FRAME 718, UPPER CORNER OF AFT FLANG E. REPLACED DOUBLER IAW DC9 SRM 51-30. 2 L 7 2 4F A6WE 1998012200327 19980122 00327 WP 1998 1 22 ABXA9800021 1 19980116 A 5313 591140513 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STA 160. REPAIRED LONGERON 4L IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998012200328 19980122 00328 WP 1998 1 22 ABXA9800022 1 19980116 A 5313 59114277 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND LONGERON 16L CRACKED AT STA 965. REPAIRED LONGERON 16L IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998012200329 19980122 00329 WP 1998 1 22 ABXA9800023 1 19980116 A 5320 4911383502A FITTING DOUG DOUG DC9 DC933F 302207A WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND FUSELAGE FRAME MOUNT FOOT FITTING STA 980 LONGERON 18L CORRODED, (LT SIDE). REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998012200330 19980122 00330 WP 1998 1 22 ABXA9800024 1 19980116 A 5313 54364369 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND LONGERON 13R CRACKED AT STA 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998012200331 19980122 00331 WP 1998 1 22 ABXA9800025 1 19980116 A 5330 591142775 DOUBLER DOUG DOUG DC9 DC933F 302207A WP BS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND EXFOLIATION CORROSION IN INTERNAL FUSELAGE SKIN DOUBLER AT STA 996 JUST BELOW LONGERON 17R. REPLA CED FILLER DOUBLER IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998012200332 19980122 00332 NM 1998 1 22 DL72E980086 1 19980113 A 3350 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 831WA 21483 FA AFT FLASHLIGHT INOP. REPLACED BATTERY, OPN NML. 2 L 7 3 4F A3WE 1998012200333 19980122 00333 NM 1998 1 22 DL72S980091 1 19980113 A 5320 WEB BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 FOUND DURING F-2 LETTER CHECK, .0625 INCH CRACK AT UPPER EDGE OF TORQUE BOX LIGHTENING HOLE LT SIDE STA 1273. ROUTED OU T PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998012200334 19980122 00334 NM 1998 1 22 DL72S980092 1 19980113 A 5755 SKIN BOEING 727 727232 1384082 NM NR 3 SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 FOUND ON F-2 LETTER CHECK, NR 3 SPOILER TOP SKIN DELAMINATED O/B END 23 X 9. MADE FIBERGLASS REPAIR PER SRM 57-50-6 FIG 1. 2 L 7 3 4F A3WE 1998012200335 19980122 00335 NM 1998 1 22 DL733980093 1 19980113 A 3350 BATTERY PACK 20131A BOEING 737 737347 1384647 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 313WA 23599 ON LAYOVER CK, FOUND SEVERAL SECTIONS OF CABIN FLOOR EMERG EXIT LIGHTING WEAK. REPLACED 2 BATTERY PACKS. 2 L 7 2 4F RT A16WE 1998012200336 19980122 00336 NM 1998 1 22 DL733980094 1 19980113 A 3350 BATTERY PACK BPS73 BOEING 737 737347 1384647 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 313WA 17889 23599 ON LAYOVER INSP, FOUND SEVERAL SECTIONS OF FLOOR EMER EXIT LIGHTING WEAK. REPLACED 1 PWR SUPPLY RACK WITH BATTERY, SYS NOW OPS NML. 2 L 7 2 4F RT A16WE 1998012200337 19980122 00337 NM 1998 1 22 DL72S980097 1 19980113 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 FOUND DURING F-2 LETTER CHECK, NR 7 SLAT COVE SKIN ANGLE CRACKED O/B OF I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998012200338 19980122 00338 NM 1998 1 22 DL73K980098 1 19980113 A 2910 000AE908T06 HYD LINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE RUPTURED A DALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 311DL 23083 709211 ON EXTENSION OF FLAPS HHD LIGHT LOW PRESSURE ILLUMINATED WITH A-SYS QTY NEAR ZERO. REPLACED HYDRAULIC LINE. 2 L 7 2 4F 4 F RT A16WE E2EA 1998012200339 19980122 00339 NM 1998 1 22 DL72S980099 1 19980113 A 5320 TORQUE BOX BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 THE FS 1263 BEAM AND CHANNEL ON THE RT TORQUE BOX OF THE AFT VENTRAL STAIRWAY WERE FOUND WITH TYPICAL CRACKS PER S/B 53- 0129. THE CRACKED PARTS WERE REPLACED PER THE S/B INSTRUCTIONS AND DOCUMENTED PER ER/A 363704-14AD. 2 L 7 3 4F A3WE 1998012200340 19980122 00340 NM 1998 1 22 DL72S980101 1 19980114 A 5330 SKIN BOEING 727 727232 1384082 NM BS 304 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSPECTION PER EO4-60829-3, A CRACK WAS FOUND IN THE SKIN AND DOUBLER IN THE TYP LOCATION AS WELL AS A CRACK IN T HE STRAP, BUT ONE FASTENER ROW HIGHER THAN TYP. REPAIRED PER ERA 331195-14. 2 L 7 3 4F A3WE 1998012200341 19980122 00341 NM 1998 1 22 DL72S980102 1 19980114 A 5320 65571987 WEB BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 DURING INSTALLATION OF PREVENTATIVE MOD ON THE LHS KEEL BEAM PER SB727-53-0208 (EO 4-64433-3), A CRACK WAS FOUND IN THE WEB JUST ABOVE THE VERT FLANGE OF THE KEEL BEAM. REPAIRED PER ERA 331201-14. 2 L 7 3 4F A3WE 1998012200342 19980122 00342 NE 1998 1 22 DLL10980103 2 19980113 A 7311 RB21122B02 FUEL/OIL COOLER LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENGINE FAILED A DALA J A DUMP FUEL UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 716DA 48889 193C1095 010553 PAX REPORTED VAPOR TRAIL FROM NR 3 ENG, S/O AND CAPT CONFIRMED. FLT SERV REPORTED FUEL ODOR. DUMPED 37,000 LBS FUEL. R ETURNED TO LAX AFTER DISCUSSION WITH ATL MTC. NO ABNORMAL INDICATIONS IN COCKPIT LANDING GROSS WT 358,000 LBS. REPLACE D FUEL/OIL COOLER AND FUEL PUMP AND FFR, RAN ENG PER PFHB CH 077, TEST 3-9-20. ALL CHKS NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1998012200349 19980122 00349 NM 1998 1 22 DL72W980110 1 19980105 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 STRINGER CRACKED INSIDE VERTICAL STAB RT SIDE 3RD BAY UP FROM LOWER WEB. REPAIRED PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1998012200350 19980122 00350 NM 1998 1 22 DLM88980111 1 19980114 A 5330 593666751 SKIN DOUG MD88 MD88 3023688 NM BS 1193 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 THE FUSELAGE SKIN, INTERNAL DOULBER, EXTERNAL DOUBLER, AND LOWER SILL BEAM OF THE C3 DOOR CUTOUT WERE FOUND TORN DUE TO A GROUND EQUIPMENT IMPACT. THE LOWER SILL BEAM AND EXTERNAL DOUBLER WERE REPLACED. THE SKIN AND INTERNAL DOUBLER WERE REPAIRED WITH A DOUBLER AND TRIPLER. THE REPAIRS WERE ACCOMPLISHED PER ER/A 363674-14, REV A. 2 L 7 2 4F RT A6WE 1998012200351 19980122 00351 NM 1998 1 22 DL72W980112 1 19980106 A 2782 BRACKET BOEING 727 727247 138408F NM NR 3 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 NR 3 L/E SLAT ACTUATOR BRACKET CRACKED. REPAIRED PER M/M 57-54-0 FIG 804. 2 L 7 3 4F A3WE 1998012200352 19980122 00352 NM 1998 1 22 DL72W980118 1 19980106 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 THE 3RD BAY DOWN INSIDE ACCESS 9504 STRINGER IS CRACKED ON LT SIDE. STOP DRILLED CRACK, DYE CKD TO VERIFY CRACK END, FA B REPAIR PARTS PER M/M 55-30-0 FIG 803. INSTALLED REPAIR. 2 L 7 3 4F A3WE 1998012200353 19980122 00353 NM 1998 1 22 DL72W980119 1 19980106 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 THE 3RD BAY DOWN INSIDE ACCESS 9504 ON LT SIDE STRINGER HAS .25 INCH CRACK EMANATING FROM BELOW BOLT HEAD. DYE CHECKED AREA PER PS 900-6-3. AREA VERIFIED AS CRACKED. STOP DRILLED ENDS OF CRACKS. DYE CKD TO VERIFY CRACK END. FAB REPAIR PARTS PER M/M 55-30-0 FIG 803. OK TO INSTALL REPAIR. 2 L 7 3 4F A3WE 1998012200375 19980122 00375 SW 1998 1 22 98ZZZX285 1 19980109 A 2910 27810322683 HYDRAULIC LINE FRCHLD SA227 SA227DC 3377521 SW LT MLG WW CRACKED A EQGA A O UNSCHED LANDING OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 19 847LS DC847B DFW/ELD - FLT 1251 - WHILE IN CRUISE 30 MINUTES INTO FLIGHT, BOTH HYD LIGHTS ILLUMINATED. CREW NOTICED GAUGES BLEEDING DOWN. BLEED DOWN STOPPED WHEN GAUGES WERE IN YELLOW ARC. CREW FOLLOWED ABNORMAL CHECKLIST AND CONTACTED MAINT AND FLIG HT DISPATCH. CREW ADVISED TO DIVERT TO HOT. ON APPROACH TO HOT, CREW MANUALLY EXTENDED LG AND LANDED ZERO FLAPS WITH N O INCIDENT. MAINT INSPECTED ACFT AND FOUND HYD LINE IN LT ENG NACELLE CHAFING WHERE LINE TRAVELED THRU FIREWALL. B-NUT ON LINE WHERE LINE TRAVELS THRU FIREWALL HAD BACKED OFF ALLOWING LINE TO VIBRATE AND CHAFE THRU. MAINT REPLACED LINE A ND OTHER LINES SHOWING DETERIORATION AND REPLACED AND REPOSITIONED ADEL CLAMPS TO ENSURE PROPER ROUTING OF ALL LINES. 2 L 7 2 4T RT A18SW 1998012200376 19980122 00376 WP 1998 1 22 98ZZZX286 2 19980109 A 7320 FCU SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE REQUIRED ADJUST A EQGA C D ABORTED TAKEOFF RETURN TO BLOCK O R OTHER PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 19 459AM AC700 BWD/DFW - FLT 1230 - ON TAKEOFF ROLL JUST BEFORE V1, EXPERIENCED A POWER DROP IN LT ENGINE AND ACFT YAWED TO THE LEFT. A BORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER ABNORMALITIES NOTED. MAINTENANCE CONTROL DISPATCHED FROM DFW AND AD JUSTED SCREW 'X' ON LT ENGINE ONE FULL TURN AND ADJUSTED THE FUEL FLOW 20 CLICKS. MAINTENANCE AND FLIGHT CREW PERFORMED GROUND RUNS AND FULL POWER ASSURANCE RUNS. ALL INDICATIONS WITHIN PARAMETERS. AIRCRAFT RELEASED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 1998012200405 19980122 00405 NE 1998 1 22 HEEA0012420 1 19980105 A 7931 7645001078101 INDICATOR SKRSKY S76 S76A 8143006 NE ENG OIL STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 NR2 ENGINE OIL PRESSURE NEEDLE FLUCTUATES ON TEMP/PRESS INDICATOR. 1 G 7 2 3U H1NE 1998012200406 19980122 00406 NE 1998 1 22 HEEA0012421 1 19980105 A 6410 7610105101041 BLADE SKRSKY S76 S76 8143010 NE T/R PADDLE B SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4836 760063 TRAILING EDGE SPLIT OPEN ON PADDLE "B" AND HOLE IN THE LEADING EDGE ABRASION STRIP. 1 G 7 2 3U H1NE 1998012200407 19980122 00407 NE 1998 1 22 HEEA0012422 1 19980105 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R HORN B DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 9943 760167 PITCH HORN "B" HAS REACHED RETIREMENT TIME. 1 G 7 2 3U H1NE 1998012200408 19980122 00408 NE 1998 1 22 HEEA0012423 1 19980105 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 443 760035 T/R BLADE PRIMARY RUBBER LIFTING. 1 G 7 2 3U H1NE 1998012200409 19980122 00409 NE 1998 1 22 HEEA0012424 1 19980105 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 707AE 408 760276 T/R BLADE LINER BETWEEN THE SPAR AND THE PLUG TORN AND UNBONDED. 1 G 7 2 3U H1NE 1998012200410 19980122 00410 EU 1998 1 22 HEEA0012425 1 19980105 A 2822 D10731814 ROTOR D107318D1 BOLKMS 105 BO105S 5626006 EU BOOST PUMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 682 112976 S737 BOOST PUMP WAS REMOVED FOR BEING INOPERATIVE. ARMATURE SHORTED. DISASSEMBLED AND FOUND THAT BEARING CAME APART AND CAU SED ARMATURE TO BURN UP. SENT TO MIR BEARING WAS RECEIVED IN BEARING KIT P/N D107318-21. 1 G 7 2 3U H3EU 1998012200411 19980122 00411 EU 1998 1 22 HEEA0012426 1 19980105 A 2435 230322111 ARMATURE 23032048 BOLKMS 117 BK117B1 5626012 EU GENERATOR SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 24569 7152 GENERATOR FAILED (SHORTED OUT) 1 G 7 2 3U H13EU 1998012200412 19980122 00412 EU 1998 1 22 HEEA0012427 1 19980105 A 6420 105317381 INNER SLEEVE BOLKMS 117 BK117B2 5626013 EU T/R HEAD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 132AE 1802 7238 T/R HEAD BEARING BUSHING SEATS AND SEAL RIDE WORN. 1 G 7 2 3U NC H13EU 1998012200413 19980122 00413 EU 1998 1 22 HEEA0012428 1 19980105 A 6420 105317381 INNER SLEEVE BOLKMS 117 BK117A3 5626015 EU T/R HEAD WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 T/R HEAD BEARING BUSHING SEATS AND SEAL RIDE WORN. 1 G 7 2 3U H13EU 1998012200414 19980122 00414 EU 1998 1 22 HEEA0012429 1 19980105 A 7714 DL40438 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH N2 FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4302G S853 N2 NR2 NEEDLE INDICATES 30% LOW AT 100% RPM. TIME SINCE REPAIR 23:50. 1 G 7 2 3U H3EU 1998012200415 19980122 00415 SW 1998 1 22 HEEA0012430 1 19980105 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2258F 9901 33073 BLADE RECEIVED FROM VENDOR WITH NO WEIGHTS IN FORWARD ROOT POCKET; BLADE IS HEAVY AND CANNOT BALANCE 1 G 7 2 4U H4SW 1998012200416 19980122 00416 SW 1998 1 22 HEEA0012431 1 19980105 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 6908 M/R BLADE HAS BOTH UPPER FRETTING PADS UNBONDED. 1 G 7 2 4U H4SW 1998012200417 19980122 00417 SW 1998 1 22 HEEA0012432 1 19980105 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 576 M/R BLADE HAS SEPARATION ON THE TRAILING EDGE DOUBLER WHICH IS BEYOND THE LIMITS. 1 G 7 2 4U H4SW 1998012200418 19980122 00418 1998 1 22 HEEA0012433 4 19980105 A 3457 0110010600 GPS165 GARMIN INTL BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 GPS 165 UNIT MESSAGE: INTERNAL BATTERY LOW. 1 G 7 2 4U H4SW 1998012200419 19980122 00419 1998 1 22 HEEA0012434 4 19980105 A 3453 4530093 RECEIVER ARNAV20 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3178K 45765 LORAN RECEIVER WILL NOT ACKNOWLEDGE WAYPOINT ALERT. 1 G 7 1 3U H2SW 1998012200420 19980122 00420 1998 1 22 HEEA0012435 4 19980105 A 3442 MI5852013 INDICATOR P4001 BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 RADAR SYSTEM WOULD COME ON, BUT SCREEN WAS BLANK. AFTER AWHILE, SYSTEM WOULD SHUTDOWN. 1 G 7 1 4U H4SW 1998012200421 19980122 00421 1998 1 22 HEEA0012436 4 19980105 A 3457 S67157539 GPS ANTENNA BELL 206 206L1 1182107 SW GPS SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2761N 45277 GPS ANTENNA WILL NOT PICK UP SATELLITES OR FIND ITSELF. 1 G 7 1 3U H2SW 1998012200422 19980122 00422 SW 1998 1 22 HEEA0012437 1 19980105 A 7930 174035201 INDICATOR 174000103 BELL 206 206L1 1182107 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22425 31 3989 45743 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998012200423 19980122 00423 SW 1998 1 22 HEEA0012438 1 19980105 A 7930 174035201 INDICATOR 174000103 BELL 206 206L1 1182107 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019G 445 45247 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998012200424 19980122 00424 SW 1998 1 22 HEEA0012439 1 19980105 A 7930 174035201 INDICATOR 174000103 BELL 206 206B3 1181506 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2145C 4073 3456 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998012200425 19980122 00425 SW 1998 1 22 HEEA0012440 1 19980105 A 7930 174035201 INDICATOR 174000103 BELL 206 206L1 1182107 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 4022 45291 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998012200426 19980122 00426 SW 1998 1 22 HEEA0012441 1 19980105 A 7930 174035201 INDICATOR 174000103 BELL 206 206L1 1182107 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10814 4246 45415 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK 1 G 7 1 3U H2SW 1998012200427 19980122 00427 SW 1998 1 22 HEEA0012442 1 19980105 A 7930 174035201 INDICATOR 174000103 BELL 206 206L3 1182108 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6160Y 4433 51609 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998012200428 19980122 00428 SW 1998 1 22 HEEA0012443 1 19980105 A 7930 174035201 INDICATOR 174000103 BELL 206 206L3 1182108 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 467 51495 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998012200429 19980122 00429 1998 1 22 HEEA0012444 4 19980105 A 2312 064105430 TRANSCEIVER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31077 51520 TRANSCEIVER FREQUENCY DISPLAY INOPERATIVE. 1 G 7 1 3U H2SW 1998012200430 19980122 00430 1998 1 22 HEEA0012445 4 19980105 A 3444 066304400 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 760275 RADAR ALTIMETER NEEDLE WILL START SPINNING FOR A FEW SECONDS THEN STOP. 1 G 7 2 3U H1NE 1998012200431 19980122 00431 GL 1998 1 22 HEEA0012446 2 19980105 A 7320 23068651 HMU BELL 407 407 SW ALLSN 250C 250C47B GL ENGINE FAILED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 417PH 578 53038 FADEC DEGRADE AND RESTART FAULT LIGHT ON IN FLIGHT. REPLACEMENT S/N ALM0437. 1 G 7 1 3U 3 U O H2SW E1GL 1998012200436 19980122 00436 SW 1998 1 22 HEEA0012451 1 19980105 A 2436 214175153105 REGULATOR BELL 214 214ST 1182106 SW DC SYS INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 745H 28200 VOLTAGE REGULATOR INOPERATIVE. 2 G 7 2 4U H10SW 1998012200437 19980122 00437 NE 1998 1 22 HEEA0012452 2 19980106 A 7320 6038T62P24 HMU BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE NR 1 ENGINE FAILED E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 5748M 28102 NR 1 ENGINE FAILED IN FLIGHT. 2 G 7 2 4U 4 U H10SW E8NE 1998012200438 19980122 00438 1998 1 22 HEEA0012453 4 19980106 A 2370 9806019001 CVR BEECH 200 200CBEECH 1152926 CE COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 39PH 4058 BL3 CVR WILL NOT TEST. 1 L 7 2 4T A24CE 1998012200439 19980122 00439 1998 1 22 HEEA0012454 4 19980106 A 2370 9806019001 CVR BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5736D 2816 31135 CVR FAILED TEST. 1 G 7 1 4U H4SW 1998012200440 19980122 00440 SW 1998 1 22 HEEA0012455 1 19980106 A 2913 214076033101 PUMP BELL 214 214ST 1182106 SW HYD SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3897N 28106 HYD PUMP LEAKING AT OUTLET FITTING. 2 G 7 2 4U H10SW 1998012200441 19980122 00441 NE 1998 1 22 HEEA0012456 2 19980106 A 7210 3024780 COMBINING GRBOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE MAKING METAL E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 6559Z 14154 36019 COMBINING GEARBOX HAS METAL ON PLUG AND FILTER. 1 G 7 2 4U 4 U H4SW E22EA 1998012200442 19980122 00442 NE 1998 1 22 HEEA0012457 2 19980106 A 7250 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE GAS GEN CASE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 11668 33113 ENGINE HAS CRACK IN GENERATOR CASE. 1 G 7 2 4U 4 U H4SW E22EA 1998012200443 19980122 00443 SW 1998 1 22 HEEA0012458 1 19980106 A 7714 206075682107 INDICATOR BELL 206 206L3 1182108 SW GAS PROD IND FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8592X 51508 GAS PRODUCER INDICATOR NEEDLES OSCILLATES DURING STARTING CYCLE. 1 G 7 1 3U H2SW 1998012200444 19980122 00444 SW 1998 1 22 HEEA0012459 1 19980106 A 6240 206075681105 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 DUAL TACH NEEDLE STICKS UP TO 30%. 1 G 7 1 3U H2SW 1998012200445 19980122 00445 SW 1998 1 22 HEEA0012460 1 19980106 A 3150 214175122111 PANEL BELL 412 412 1182202 SW MASTER CAUTION FAILED E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 33008 36004 DOESN'T TURN ON MASTER CAUTION LIGHT. 1 G 7 2 4U H4SW 1998012200446 19980122 00446 SW 1998 1 22 HEEA0012461 1 19980106 A 6240 206075681117 INDICATOR BELL 206 206L1 1182107 SW DUAL TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11027 45411 DUAL TACH ROTOR NEEDLE NOT WORKING. 1 G 7 1 3U H2SW 1998012200447 19980122 00447 EU 1998 1 22 HEEA0012462 1 19980106 A 6320 319A62000003 GEARBOX AEROSP SA316 SA315B 8680615 EU M/R GRBOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9151A 8427 238540 MAIN GRBOX CASE CORROSION. 1 G 7 1 4U H1IN 1998012200448 19980122 00448 SW 1998 1 22 HEEA0012463 1 19980106 A 6720 7001484 YAW CONTROL BELL 412 412 1182202 SW T/R CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 YAW CONTROL SHOWS FULL RIGHT DEFLECTION. 1 G 7 2 4U H4SW 1998012200449 19980122 00449 SW 1998 1 22 HEEA0012464 1 19980106 A 6330 206033506103 RESTRAINT BELL 206 206L1 1182107 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3178K 45765 TRANSMISSION RESTRAINT HAS WORN BEARINGS. 1 G 7 1 3U H2SW 1998012200450 19980122 00450 SW 1998 1 22 HEEA0012465 1 19980106 A 6330 206033506103 RESTRAINT BELL 206 206L3 1182108 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141BH 51303 TRANSMISSION RESTRAINT HAS WORN BEARINGS. 1 G 7 1 3U H2SW 1998012200451 19980122 00451 WP 1998 1 22 VJ9700006 1 19980115 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 947VV 47555 RT OVERHEAD EMERGENCY LIGHT OUT. REPLACED POWER SUPPLY, OPS CHECKED NORMAL IAW MM 3350. 2 L 7 2 4F A6WE 1998012200452 19980122 00452 WP 1998 1 22 VJ9800007 1 19980118 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR DAMAGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 930VV 47723 R1 DOOR EMERGENCY SLIDE DISLODGED WHEN RAMP AGENT OPENED DOOR. REPLACED SLIDE ASSEMBLY IAW MM 25-62-0 AND PERFORMED REQ UIRED INSPECTION. 2 L 7 2 4F A6WE 1998012200453 19980122 00453 NM 1998 1 22 MALA975891 1 19980117 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 864MA 363 DURING INSPECTION TWO OVERHEAD CABIN EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE FORWARD CABIN BATTERY PACK, OPS CH ECK GOOD. 2 H 7 2 4T RT A13NM 1998012200454 19980122 00454 NM 1998 1 22 MALA975892 1 19980116 A 3350 MS25231316 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 864MA 363 DURING INSPECTION A CENTER AISLE EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998012200455 19980122 00455 EU 1998 1 22 MALA975893 1 19980115 A 3234 D49412001 CONTROL PANEL SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA O OTHER O OTHER DE DESCENT 1 GL 15 420XJ 420 DURING DESCENT, THE LANDING GEAR CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET, UNABLE TO EXTEND LANDING GEAR. CRE W REFERRED TO QRH, EMERGENCY LANDING GEAR EXTENTION USED. AIRCRAFT LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL PANEL, SEPARATION BOLTS AND JACKS. CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 1998012200456 19980122 00456 EU 1998 1 22 MALA975894 1 19980115 A 3060 666000219 BRUSH BLOCK SAAB SF340 340B 7860101 EU LT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 416XJ 416 DURING CRUISE FLIGHT, THE LEFT PROP CAUTION LIGHT ILLUMINATED AFTER TURNING PROP HEAT ON. AIRCRAFT RETURNED TO MSP. MA INTENANCE REPLACED THE PROP BRUSH BLOCK AND FOUR DE-ICE LEADS (PN 660714246), OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012200457 19980122 00457 EU 1998 1 22 MALA975895 1 19980115 A 2120 AIR DISTRIBUTION SAAB SF340 SF340A 7850100 EU COCKPIT ODOR A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 107XJ 340A107 DURING CRUISE FLIGHT AT 17,000, THE CREW SMELLED BURNING WIRE, NO SMOKE VISIBLE. CREW RAN QRH AND FOUND CIRCUIT BREAKER S L2, RH TAIL PIPE HOT DETECTION AND L8, EMERGENCY LIGHT CONTROL WERE OPEN. AIRCRAFT RETURNED TO DTW. MAINTENANCE REMO VED ACCESS PANEL BENEATH BREAKERS AND FOUND NO EVIDENCE OF BURNT WIRES, RESET BREAKERS. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012200458 19980122 00458 EU 1998 1 22 MALA975896 1 19980118 A 3350 6104789 BATTERY PACKS SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 586MA 340B165 DURING INSPECTION, ALL CABIN EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED ALL BATTERY PACKS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012200459 19980122 00459 EU 1998 1 22 MALA975897 1 19980119 A 3020 447301 DE-ICE MODULE SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 68XJ 068 DURING CRUISE, THE RIGHT INTAKE HEAT CAUTION CYCLES ON AND OFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED DE-ICE MODULE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012200460 19980122 00460 EU 1998 1 22 MALA975898 1 19980119 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 109XJ 340A109 DURING INSPECTION TWO OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE RELAMPED OVERHEAD EMERGENCY LIGHTS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012200461 19980122 00461 EU 1998 1 22 MALA975899 1 19980117 A 3241 39647 CONTROL SAAB SF340 340B 7860101 EU RT ANTI-SKID FAILED A MALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 15 404XJ 340B404 ON APPROACH, AFTER EXTENDING GEAR THE ANTI SKID CAUTION LIGHT ILLUMINATED. AIRCRAFT WAS DIVERTED BACK TO DTW. MAINTENA NCE REPLACED THE ANTI-SKID CONTROL VALVE, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012200462 19980122 00462 EU 1998 1 22 MALA975900 3 19980117 A 6112 660714246 LEAD SAAB SF340 SF340A 7850100 EU NR 4 PROP INTERNAL FAULT A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 114XJ 340A114 DURING CRUISE, THE RIGHT PROP DE-ICE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 4 PROP DE-ICE LEAD, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012200466 19980122 00466 NM 1998 1 22 K3HA980006 1 19980117 A 3350 P207003001 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 EMERGENCY FLASH LIGHT FORWARD INBOARD, NO RED FLASHING LIGHT AND BATTERY DRAINED. REMOVED AND REPLACED EMERGENCY FLASH LIGHT AND BATTERY (P/N P4-01-0021), OPS CHECKS OK. 2 L 7 3 4F A3WE 1998012200467 19980122 00467 NM 1998 1 22 W8PA980018 1 19980114 A 2730 CONTROLS BOEING 737 73733R 1384407 NM ELEVATOR MALFUNCTIONED A A W8PA O OTHER F FLT CONT AFFECTED LD LANDING 1 NM 03 963WP 28868 ELEVATOR JAMMED ON LANDING FLARE. REQUIRED APPROX 50 TO 60 LBS FORCE TO FREE THE ELEVATOR. INSPECTED ELEVATORS, ELEVAT OR POWER CONTROL UNIT, ALL ACCESSIBLE ELEVATOR CONTROL ASSY AND NO DEFECTS NOTED. COULD NOT DUPLICATE BINDING OR JAMMIN G. 2 L 7 2 4F RT A16WE 1998012200468 19980122 00468 NM 1998 1 22 W8PA980019 1 19980116 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN DISCONNECTED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 EMERGENCY TRACK LIGHTING IS INOP AT ROWS 20 THROUGH 23. FOUND WIRE DISCONNECTED AT ROW 20. RECONNECTED WIRE, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1998012200469 19980122 00469 EU 1998 1 22 AWXA9800014 1 19980111 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 635AW 092 EMERGENCY LIGHTS OVER R2 AND L2 AFT CENTER AISILE INOP. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1998012200470 19980122 00470 EU 1998 1 22 AWXA9800017 1 19980111 A 3350 321430 BATTERY PACK AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 646AW 271 LT MID CABIN EMERGENCY LIGHT BATTERY PACK WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK, OPS GOOD. 2 L 7 2 4F RT A28NM 1998012200471 19980122 00471 NM 1998 1 22 AWXA9800018 1 19980104 A 5315 FLOORBEAM BOEING 757 7572G7 1384963 NM BS 345 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 909AW 24522 DURING SCHEDULED C-8 INSPECTION, FOUND CORROSION ON TOP OF FLOORBEAM BS 345, BL 0, LBL 13. REMOVED, FABRICATED TOP CHOR D OF FLOORBEAM FROM RBL 19 TO LBL 52, BS 345, WL 208 PER SRM 53-00-51. 2 L 7 2 4F RT A2NM 1998012200472 19980122 00472 EU 1998 1 22 AWXA9800019 1 19980113 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 624AW 55 EMERGENCY EXIT LIGHT OVER LEFT OVERWING EXIT REPORTED OUT OR INTERMITTEN. RESET SYSTEM, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1998012200473 19980122 00473 NM 1998 1 22 AWXA9800020 1 19980109 A 3350 831136 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 EMERGENCY TRACK LIGHT OUT AT ROW 14, RELEASED UNDER MEL33-19 CONTROL NUMBER 93666. REPLACED LIGHT ASSY, CK GOOD, MEL CL EARED. 2 L 7 2 4F RT A16WE 1998012200474 19980122 00474 NM 1998 1 22 AWXA9800021 1 19980106 A 3397 WIRE BOEING 737 7373Y0 1384671 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 323AW 23684 EMERGENCY LIGHT ROW C INOP. FOUND WIRE BROKEN SPLICED IN WIRE, OPS CK NORMAL. 2 L 7 2 4F RT A16WE 1998012200475 19980122 00475 NM 1998 1 22 AWXA9800022 1 19980114 A 3350 321430 BATTERY BOEING 737 737112 1384412 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 OUTSIDE L-WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY FOR L OUTSIDE EMERGENCY LIGHTS SYSTEM, OPS CK GOOD. S TC NR SA1889SO. 2 L 7 2 4F A16WE 1998012200476 19980122 00476 NM 1998 1 22 AWXA9800023 1 19980115 A 3397 WIRE BOEING 737 7372E3 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 D-ROW 6ABC EMERGENCY LIGHT INOP. FOUND BROKEN WIRE STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998012200477 19980122 00477 NM 1998 1 22 RAAA98B1002 1 19980117 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 FWD LT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998012200478 19980122 00478 NM 1998 1 22 RAAA98B1003 1 19980117 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 7 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998012200479 19980122 00479 NM 1998 1 22 RAAA98B2006 1 19980116 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998012200480 19980122 00480 NM 1998 1 22 RAAA98B2007 1 19980116 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998012200481 19980122 00481 NM 1998 1 22 CALA9800068 1 19980115 A 5330 DAMA11W1S SKIN BOEING 757 757224 1384958 NM FUSELAGE LOOSE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 21108 27298 THE FLIGHT ATTENDANT'S AND PASSENGERS REPORTED SMELLING SMOKE AT DOOR L2 WHILE ON FINAL APPROACH. THE AIRCRAFT LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND THE CONNECTOR PLUG FOR VDU TO LAV'S MONITOR BURNED. THE WIRES ABOVE L2 DOOR LAV WER E DISCONNECTED, CAPPED, AND STOWED. THE VIDEO MONITOR AT SEATS 7ABC WAS PLACARDED INOPERATIVE. MAINTENANCE ALSO FOUND UPPER FUSELAGE PANELS AT STA 700 FORWARD OF ANTENNA AND AFT OF UPPER BEACON LEAKING WATER INTO PASSENGER CABIN, WHICH CA USED THE CONNECTOR TO BE BURNED. THE UPPER BEACON WAS ALSO LEAKING. THE FUSELAGE PANELS AND UPPER BEACON WERE REMOVED, CLEANED, RESEALED, AND REINSTALLED. 2 L 7 2 4F RT A2NM 1998012200482 19980122 00482 WP 1998 1 22 CALA9800069 1 19980119 A 2822 6550934 BOOST PUMP DOUG DC9 DC932 3022066 WP LT MAIN TANK LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 12507 13929 47788 WHILE AT CRUISE, THE CREW ATTEMPTED TO BALANCE WING FUEL LOAD BY CROSSFEEDING FROM LEFT MAIN FUEL TANK TO RIGHT ENGINE. THE RIGHT ENGINE HESITATED (N1,N2,FF, AND EPR DECREASED) WITH FUEL CROSSFEED OPEN. THE RIGHT INLET FUEL PRESSURE LIGHT AND MASTER CAUTION LIGHT WERE FLICKERING. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MAIN TANK AFT BOOST PUMP LEAKING INTERNALLY. THE AFT BOOST PUMP WAS REMOVED AND REPLACED. THE PACKINGS ON LT MAIN TANK FORW ARD BOOST PUMP WERE REPLACED DUE TO LEAKAGE. THE FUEL CROSSFEED VALVE WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASU RE. THE RIGHT ENGINE WAS RUN AT TAKEOFF FOR FIVE MINUTES AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998012200483 19980122 00483 NM 1998 1 22 CALA9800070 1 19980115 A 5752 652172641K SKIN BOEING 727 727227 1384078 NM LT AILERON TAB BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND LT WING OUTBOARD AILERON TAB LOWER LEADING EDGE SKIN BENT AND DEBONDED. THE AILERON TAB WAS REMOVED AN D REPLACED IAW MM 27-10-41. 2 L 7 3 4F A3WE 1998012200484 19980122 00484 NM 1998 1 22 CALA9800071 1 19980115 A 5730 SKIN BOEING 727 727227 1384078 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .25 INCH CRACK IN RT WING LEADING EDGE SKIN AT NR 6 SLAT OUTBOARD HOOK. THE CRACK WAS STOP DRILLED P ER SRM 51-10-1, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4. 2 L 7 3 4F A3WE 1998012200485 19980122 00485 NM 1998 1 22 CALA9800072 1 19980115 A 5712 RIB BOEING 727 727227 1384078 NM WS 106.8 CRACKED A CALA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .75 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF BOTTLE PIN ABOVE PNEUMATIC DUCT FORWARD SUPPOR T BRACKET AT FSS 106.8. A REPAIR WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998012200486 19980122 00486 NM 1998 1 22 CALA9800073 1 19980115 A 5712 RIB BOEING 727 727227 1384078 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN RT WING LEADING EDGE RIB OUTBOARD OF NR 6 LEADING EDGE SLAT STA 234. AN ANGLE DOUBLE R WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998012200487 19980122 00487 NM 1998 1 22 CALA9800074 1 19980116 A 3350 20131A BATTERY PACK RADIANT BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34315 23366 THE FORWARD LEFT ENTRY DOOR EMERGENCY LIGHT FAILED FUNCTIONAL CHECK. THE BATTERY PACK WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A16WE 1998012200488 19980122 00488 NM 1998 1 22 CALA9800075 1 19980115 A 3350 1001011 LIGHT GRIMES BOEING 727 727227 1384078 NM AFT AIRSTAIR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND EMERGENCY FLOOD LIGHT AT LEFT SIDE OVER AFT AIRSTAIRS INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1998012200489 19980122 00489 NM 1998 1 22 9800946309 1 19980116 A 3350 CONNECTORS BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 699US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 23ABC TO 41ABC, 51KJH TO 66KH, 35HJ TO 42HJK, 20AC TO 41ABC, 72R TO 73R, AND AT ROW 31KJH. SECURED CONNECTORS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998012200490 19980122 00490 WP 1998 1 22 9800959754 1 19980118 A 5241 SEAL DOUG DC9 DC941 302207N WP GALLEY DOOR LOOSE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 754NW 47178 DURING CLIMB, HEARD A BANGING NOISE AT FORWARD GALLEY SERVICE DOOR. FLIGHT RETURNED TO DTW AND LANDED WITH NO FURTHER I NDICENTS. MAINTENANCE REATTACHED AESTHETIC SEAL. 2 L 7 2 4F A6WE 1998012200491 19980122 00491 EU 1998 1 22 9800963201 1 19980117 A 5610 WINDOW AIRBUS 320 A320211 3930320 EU LT COCKPIT CRACKED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 301US 31 DURING CLIMB, CAPTAIN'S WINDSHIELD HEAT SHORTED AND WINDSHIELD CRACKED. FLIGHT RETURNED TO MSP AND ACCOMPLISHED AN OVER WEIGHT LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WINDSHIELD AND PERFORMED OVERWEIGHT LANDING INSPECTION. 2 L 7 2 4F RT A28NM 1998012200492 19980122 00492 NE 1998 1 22 9800979868 2 19980115 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LEFT FAILED A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 777NC 47787 696709 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EXPERIENCED AN OVERSPEED CONDITION. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE DUE TO TURBINE DAMAGE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1998012200493 19980122 00493 WP 1998 1 22 9800989855 1 19980114 A 7711 611427611428 PT7 LINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE LEAKING A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 764NC 47717 696742 DURING TAKEOFF ROLL AT 80 KNOTS, THE LEFT ENGINE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETURN ED TO THE GATE. MAINTENANCE REPLACED PT7 LINES, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1998012200494 19980122 00494 WP 1998 1 22 9800999940 1 19980118 A 3350 113317 BATTERY DOUG DC9 DC932 3022066 WP PAX DOOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 50510 1218 47031 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LIGHTS BATTERY LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998012200495 19980122 00495 1998 1 22 9801009914 4 19980117 A 2565 13621228 SLIDE DOUG DC9 DC931 3022065 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 964N 8430 2349 47416 DURING LINE MAINTENANCE INSPECTION, FOUND AFT TAIL CONE EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200496 19980122 00496 WP 1998 1 22 9801019940 1 19980118 A 3350 113317 BATTERY DOUG DC9 DC932 3022066 WP PAX DOOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 50510 1218 47031 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE LIGHTS BATTERY LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998012200497 19980122 00497 WP 1998 1 22 9801029923 1 19980117 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 927RC 47469 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH FORWARD OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTER Y PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200498 19980122 00498 WP 1998 1 22 9801039997 1 19980118 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1998012200499 19980122 00499 WP 1998 1 22 9801049603 1 19980116 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603NW 47101 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD FLIGHT ATTENDANT LOWER FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200500 19980122 00500 WP 1998 1 22 9801059615 1 19980117 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 615NW 47129 DURING LINE MAINTENANCE INSPECTION, FOUND UPPER AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200501 19980122 00501 WP 1998 1 22 9801069623 1 19980117 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 623NW 47591 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT FORWARD LAVATORY INOPERATIVE. REPLACED BATTERY PACK AND PO WER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012200502 19980122 00502 SO 1998 1 22 COMA9810024 1 19980115 A 2731 ATG120TR SENSOR EMB 120 EMB120RT SO ELEVATOR TRIM DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 263CA 120255 TRIM WARNING DURING TAKEOFF. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1998012200503 19980122 00503 EA 1998 1 22 COMA9860012 1 19980116 A 3020 12681 SWITCH CNDAIR CL600 CL6002B19 EA LT ENG COWL MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 933CA 7040 LEFT COWL ANTI-ICE CAUTION MESSAGE. REPLACED THE COWL ANTI-ICE PRESSURE SWITCH. 2 L 7 2 4F RT A21EA 1998012200504 19980122 00504 EA 1998 1 22 COMA9860013 1 19980116 A 3030 7858062 HEAT CONTROLLERS CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 THE LEFT HAND PITOT AND STATIC HEAT FAILED. REPLACED THE NR 1 AND NR 3 ADS HEAT CONTROLLERS. 2 L 7 2 4F RT A21EA 1998012200505 19980122 00505 EA 1998 1 22 COMA9860014 1 19980115 A 3610 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 EA BLEED AIR DUCT MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 929CA 10821 183 7035 BLEED AIR DUCT LEAK WARNING DURING TAKEOFF. REPLACED THE BLEED LEAK CONTROL UNIT. 2 L 7 2 4F RT A21EA 1998012200507 19980122 00507 NM 1998 1 22 UPS98225490 1 19980116 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 870-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, SEAT TRACK STA 870 TO 1130 RBL 25 HAS AREAS OF CORROSION AND MECHANICAL DAMAGE. REMOVED CORRODED AN D MECHANICAL DAMAGED SEAT TRACK, FABRICATED AND INSTALLED REPAIR PARTS IAW 53-10-5, 51-30-5, 51-30-8, 51-20-2. 2 L 7 3 4F A3WE 1998012200508 19980122 00508 NM 1998 1 22 UPS98225491 1 19980116 A 5320 65198614 CHORD BOEING 727 72722C 138400F NM BS 334/351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION ON LOWER NOSE CHORD AROUND NUT PLATES BETWEEN BS 334 AND BS 351 RBL 17. REMOVED AND REPLA CED LOWER NOSE CHORD IAW SRM 51-30-2, 51-10-2, 51-20-04, MM 51-20-151. 2 L 7 3 4F A3WE 1998012200509 19980122 00509 NM 1998 1 22 UPS98225492 1 19980116 A 5320 STIFFENER BOEING 727 72722C 138400F NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CORROSION ON LOWER END OF VERTICAL STIFFENER ON NLG WHEEL WELL BS 328 LBL 15, WL 171. REMOVED AND R EPLACED VERTICAL STIFFENER IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200510 19980122 00510 NM 1998 1 22 UPS98225493 1 19980116 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 303 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, CRACK ON SIDE OF INTERCOSTAL AT STA 303 LBL 51, WL 261. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51 -10-1, 53-10-2, 51-10-2, 51-30-5. 2 L 7 3 4F A3WE 1998012200511 19980122 00511 NM 1998 1 22 UPS98225494 1 19980104 A 5320 SILL BOEING 727 7272A1 138407F NM BS 950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-03) ON MOPSILL BETWEEN BS 950 TO 950A, LBL 65 AROUND NUT PLATE HOLES. MOPS ILL BS 950 TO 950A FOUND TO BE OUT OF LIMITS SRM 51-40-4. REMOVED CORRODED AREA IAW SRM 53-10-1, FABRICATED AND INSTALL ED REPAIR PARTS SRM 51-40-2. 2 L 7 3 4F A3WE 1998012200512 19980122 00512 NM 1998 1 22 UPS98225495 1 19980114 A 5313 STRINGER BOEING 727 7272A1 138407F NM BS 720 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, DISCOVERED END OF STR 15L TO BE CRACKED AT BS 720+5. AREA OF DAMAGE REMOVED AND STRINGER END REPAIR ED PER SRM 53-10-3 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200513 19980122 00513 NM 1998 1 22 UPS98225496 1 19980116 A 5320 651757011 SILL BOEING 727 7272A1 138407F NM BS 294-304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, MOPSILL CRACKED LBL 54 STA 294 TO 304 WL 208. REPLACED MOPSILL AT LBL 54 STA 294 TO 304 WL 208 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012200514 19980122 00514 NM 1998 1 22 UPS98225497 1 19980115 A 5320 651627910 BEAM BOEING 727 7272A1 138407F NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON LONGITUDINAL BEAM ST 760 TO 848 LBL 45 WL 208. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED LONGITUDINAL BEAM IAW SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1998012200515 19980122 00515 NM 1998 1 22 UPS98225502 1 19980116 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, FWD CEILING EMER LIGHT HAS NO GREEN LAMP. REMOVED AND REPLACED BATTERY PACK, OPS CHK GOOD. 2 L 7 3 4F A3WE 1998012200516 19980122 00516 WP 1998 1 22 UPS98825488 1 19980101 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 705UP 45949 INSPECTION TYPE-C/CK, FRAME CORRODED AT STATION 1300, BETWEEN LONGERONS 36 AND 35L, MARKED. BLENDED OUT CORROSION IAW D C8 SRM 51-1-8, FABBED REPAIR DOUBLER IAW3 REO 04060 AND DC8 SRM 53-2-0 FIG 2, HEAT TREATED REPAIR DOUBLER IAW TPS 1003 , ALODINED AND PRIMED FRAME AND DOUBLER IAW DC8 SRM 51-1-8, INSTALLED REPAIR DOUBLER WITH HI-LOKS IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998012200519 19980122 00519 EU 1998 1 22 WWMA9800013 1 19980117 A 2612 72111211000 FIRE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 15 345SB 340B345 EN ROUTE, THE CARGO FIRE LIGHT ILLUMINATED, CREW FIRED THE NR 1 CARGO FIRE EXTINGUISHER AND DIVERTED TO GGG. REPLACED T HE NR 1 CARGO FIRE EXTINGUISHER AND THE FORWARD AND AFT CARGO FIRE DETECTORS. THE AFT DETECTOR WAS OEM WITH 9991 HRS TS N AND THE FWD DETECTOR HAD 5290 HRS TSR. 2 L 7 2 4T RT A52EU 1998012200520 19980122 00520 1998 1 22 QXEA9800025 4 19980113 A 2565 S130508 SLIDE FOKKER F28 F28MK4000 4990810 EU CABIN LOW PRESSURE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 126 11234 EMERGENCY ESCAPE SLIDE PRESSURE BELOW MINIMUM. REPLACED EMERGENCY ESCAPE SLIDE. 2 L 7 2 4F RT A20EU 1998012200521 19980122 00521 NM 1998 1 22 QXEA9800026 1 19980114 A 5280 BUSHING DHAV DHC8 DHC8102 2809003 NM MLG DOOR WORN A QXEA K NONE O OTHER CR CRUISE 1 NM 09 102AV 091 GEAR DOOR ON NR 1 SIDE WAS HANGING DOWN IN-FLIGHT, 10 TO 12 BOLT FOUND TO BE LOOSE ON GEAR DOOR. SECURED ROD END BOLT T O DOOR BRACKET PIVOT POINT WITH .032 STAINLESS SAFETY WIRE. FERRIED AIRCRAFT TO PDX. AT PDX, INSPECTED DOOR AREA FOR D AMAGE, NO DAMAGE FOUND. INSTALLED FORWARD GEAR DOOR ROD TO DOOR. REPLACED THREADED BUSHING. 2 H 7 2 4T RT A13NM 1998012200523 19980122 00523 EU 1998 1 22 QXEA9800028 1 19980115 A 2150 PACK FOKKER F28 F28MK4000 4990810 EU CABIN SMOKING A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 491US 11156 CABIN FILLS WITH SMOKE WHEN CABIN PACK IS ON. COCKPIT PACK OK. MAINTENANCE PLACED CABIN PACK ON MEL. MEL CLEARED BY O PERATING APU FOR 4 HOURS WITH APU ON, NO SMOKE NOTED. MEL CLEARED. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998012200524 19980122 00524 EU 1998 1 22 QXEA9800029 1 19980115 A 3350 LAMP FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 LEFT HAND EVACUATION EXIT LIGHT INOP. REPLACED LAMP, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998012200525 19980122 00525 NM 1998 1 22 QXEA9800030 1 19980115 A 2730 PULLEY GUARD DHAV DHC8 DHC8202 2809007 NM ELEVATOR CONTL LOOSE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 345PH 476 BEFORE TAKEOFF DURING NORMAL FLIGHT CONTROL CHECK, A CLICK WAS HEARD AND FELT AS THE CONTROL COLUMN WAS MOVED THROUGH IT S TRAVEL RANGE. THE SOUND APPEARS TO BE COMING FROM UNDER THE FLOOR. IT OCCURED WHEN IT WAS CLOSER TO THE FULL UP ELEV ATOR POSITION (COLUMN ABOUT 2/3 OF THE WAY TOWARD UP, ELEVATOR CONDITION IS INTERMITTANT). AIRCRAFT RETURNED TO THE GAT E. MAINTENANCE FOUND A LOOSE PULLEY GUARD ON PILOTS ELEVATOR CABLE. PULLEY TO BE SLIGHTLY BINDING. SECURED GUARD AS R EQUIRED. NO PARTS REPLACED, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998012200526 19980122 00526 NM 1998 1 22 98FDEA00036 1 19980115 A 3260 GEAR LIGHT BOEING 727 72725C 138400H NM RT MLG MALFUNCTION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 127FE 19719 REPEAT WRITE UP, REFERENCE 0132907. RIGHT GEAR GREEN LIGHT REMAINED ON WITH THE WARNING LIGHT CONTROL SWITCH IN THE DIM POSITION. CONTINUED TO MEM WITH AIRSPEED BELOW 320 KIAS/.83 MACH. WHEN PLACE LIGHT CONTROL SWITCH IN THE BRIGHT POSIT ION RIGHT GREEN GEAR LIGHT GOES OUT. JACKED AIRCRAFT AND CYCLED GEAR AT LEAST 20 TIMES, ALL GEAR AND TAIL SKID LIGHTS W ORKED NORMALLY. INSPECTED ALL GEAR SWITCHES AND PINS ON GEAR ACCESSORY UNIT PLUG ALL NORMAL. COULD NOT DUPLICATE ANY O F THE PREVIOUS LIGHT PROBLEMS. REPLACED RIGHT MAIN GEAR DOWN LOCK PRECAUTIONARY PER MAINTENANCE MANUAL 32-61-21. NEED BETTER DESCRIPTION FROM FLIGHT CREW OF PROBLEM. 2 L 7 3 4F A3WE 1998012200527 19980122 00527 WP 1998 1 22 98FDEA00037 1 19980116 A 2612 FIRE DETECTOR DOUG DC10 DC1010CF 3023502 WP NR 2 ENGINE FAILED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING UK UNKNOWN 1 SO 25 054FE 47808 ON PUSHBACK PRIOR TO STARTING NR 2 ENG, ENG NR 2 LOOP-A LIGHT ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE P2-8-11. FIRE D ETECTOR LOOP LIGHT ILLUMINATED WITHOUT FIRE WARNING. SHUT DOWN APU, FIRED BOTH ENGINE 2 FIRE BOTTLES (AFTER FIREBELL AN D LIGHT IN FUEL LEVER ILLUMINATED) NO EFFECT. ENGINE NR 2 LOOP-B FIRE DETECTOR SYSTEM OPS CHECKS NORMALLY. ENGINE NR 2 LOOP-A LIGHT DEFERRED PER MEL 26-1A, CTL NR 28626. CATEGORY C EXP DATE 26JAN98. REMOVED AND REPLACED BOTH FIREBOTTLES (ENG NR 2/APU) IAW 26-21-02, P11 AND SUBS. 2 L 7 3 4F RT A22WE 1998012200528 19980122 00528 WP 1998 1 22 98FDEA00038 1 19980117 A 8012 START VALVE DOUG DC10 DC1010CF 3023502 WP NR 1 ENGINE FAILED A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 054FE 47808 DURING CLIMBOUT, ENG NR 1 START VALVE OPEN LIGHT ILLUMINATED. REMOVED PNEUM SUPPLY FROM NR 1 MANIFOLD AND RETURNED TO O AK. ENGINE OPERATION APPEARED NORMAL. DUMPED FUEL TO LANDING WEIGHT OF 375.000 PRIOR TO LANDING. START VALVE LIGHT WE NT OUT AFTER 3 TO 5 MINUTES. REMOVED AND REPLACED NR 1 ENG START VALVE IAW M/M 80-11-03. ALL IND NORMAL COWLS CLOSED A ND LOCKED. 2 L 7 3 4F RT A22WE 1998012200529 19980122 00529 WP 1998 1 22 98FDEA00039 1 19980117 A 8012 START VALVE DOUG DC10 DC1010CF 3023502 WP NR 1 ENGINE FAILED A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 054FE 47808 DURING CLIMBOUT, ENGINE 1 START VALVE OPEN LIGHT ILLUMINATED. REMOVED PNEUMATIC SUPPLY FROM NR 1 MANIFOLD AND RETURNED TO OAK. ENGINE OPERATION APPEARED NORMAL. LIGHT REMAINED ON THROUGHOUT APPROACH AND LANDING. DUMPED FUEL TO LANDING W EIGHT OF 375,000. FOUND CHAFED WIRING 2ND CLAMP FROM VALVE. INSULATED WIRING AND REMOVED CANON PLUGS FROM VALVE. ALSO , FOUND MICRO SWITCH BAD ON VALVE. VALVE (P/N 397892-1). 2 L 7 3 4F RT A22WE 1998012200530 19980122 00530 WP 1998 1 22 98FDEA00040 1 19980115 A 2820 COUPLING DOUG DC10 DC1030F 3023504 WP NR 3 ENGINE LEAKING A FDEA K NONE K FLUID LOSS UK UNKNOWN 1 SO 25 305FE 47870 FUEL LEAKING OUT OF AFT PYLON J-BOX. RAN ENG AND INSPECT FUEL SYS AND FUEL NOZZLES, NO LEAKS NOTED. REMOVED PYLON CAPS AND SIDE PANEL TO INSPECT FUEL LINE. CAP LOOSE, NO LEAKS NOTED. FOUND DAMAGED FWD GAMMA COUPLING OF NR 3 ENGINE. REM OVED AND REPLACED BOTH SETS OF FWD ON FWD LINE AT TOP OF PYLON FWD OF PRECOOLER. LEAK AND OPS CKS OK ON ENG RUN CAPS AN D PANELS SECURED. 2 L 7 3 4F RT A22WE 1998012200531 19980122 00531 EU 1998 1 22 98FDEA00041 1 19980116 A 3230 RETRACT MECH AIRBUS 310 A310203 EU NLG LACK OF LUBE A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 405FE 237 FINAL APPROACH AT IND ECAM MSG, GEAR NOT DOWN L/G GRAVITY EXTENTION. COMPLETED L/G UNSAFE INDICATED. BOTH SYS 1 AND SY S 2 IND NOSE GEAR UNLOCKED. COMPLETED L/G GRAVITY EXTENTION GEAR DID NOT COME DOWN. FLEW BOX PATTERN IN SHARP HIGH G-T URN, HEARD NOSE GEAR LOCK IN PLACE. SYS 1 AND SYS 2 INDICATED DOWN. ECAM MSG, NO NOSE GEAR STEERING. CONFIRMED NO NOS E GEAR STEERING ON ROLLOUT/TAXI. PINNED AND TOWED IN, L/G EXTENTION AND RETRACTION TEST, LUBED NLG BEARINGS AND ALL REL ATED COMPONENTS. OPERATION NOW OK. 2 L 7 2 4F RT A35EU 1998012200533 19980122 00533 WP 1998 1 22 MWEA98025 1 19980116 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 DURING SERVICE CHECK, FOUND CEILING EMERGENCY LIGHTING INOP AT ROWS 15 THROUGH 19. MTC REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT STATION 826. 2 L 7 2 4F A6WE 1998012200534 19980122 00534 NM 1998 1 22 DL73K980113 1 19980115 A 2150 VALVE 32194211 BOEING 737 737232 1384475 NM NR 1 PACK STUCK OPEN A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 310DA P3695 23082 F/A REPORTED, DENSE ACRID SMOKE IN CAB AFTER T/O. SMOKE CONCENTRATED FROM ROWS 4 TO 10. DENSE FROM 4 FT ABOVE FLOOR TO CEILING CAB LIGHTS WERE LOW. SMOKE APPEARED TO BE GREY OR WHITE. CHANGED LT 35 DEGREE VLV AND SENSOR. RUN UP BOTH PA CKS WITH ENGINE. FOUND SYSTEM NORMAL. 2 L 7 2 4F RT A16WE 1998012200535 19980122 00535 NM 1998 1 22 DL76L980115 1 19980115 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DN 24759 ROW 23 THRU 27 LT/RT SIDE EMERG TRACK LTS INOP. REPLACED PWR SUPPLY CKS GOOD. 2 L 7 2 4F RT A1NM 1998012200536 19980122 00536 NM 1998 1 22 DL76L980116 1 19980115 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 180DN 25985 RT AFT EMERGENCY FLOOR TRACK LIGHTS INOP. FOUND BROKEN WIRE. REPAIRED WIRE, CKS NML. 2 L 7 2 4F RT A1NM 1998012200537 19980122 00537 WP 1998 1 22 DLL10980117 1 19980115 A 3350 BULB 2233 LKHEED 1011 10113851 5265010 WP EXTERIOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 723DA 193C1150 L2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED, CK'S NORMAL. 2 L 7 3 4F A23WE 1998012200539 19980122 00539 NM 1998 1 22 DL72K980124 1 19980116 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 A .375 INCH CRACK PAST ROUT OUT AT LIGHTENING HOLE LT TORQUE BOX VERT WEB STA 1303. REPAIRED PER MM 53-11-0 P 828. 2 L 7 3 4F A3WE 1998012200540 19980122 00540 NM 1998 1 22 DL72K980125 1 19980116 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 A .3125 INCH CRACK LT TORQUE BOX VERT WEB LIGHTENING HOLE ADJACENT TO PREVIOUS REPAIR. REPAIRED PER MM 53-11-0 P 828. 2 L 7 3 4F A3WE 1998012200541 19980122 00541 NM 1998 1 22 DL72K980126 1 19980116 A 5532 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 1 CRACK ACROSS RIVET HOLE AT VERT. STAB SKIN FWD OF R/H LWR CORNER OF SADDLE PANEL CUT OUT. FO UND ON B-2 LETTER CHECK INSTALLED DOUBLER PER M/M 54-30-0 #1 2 L 7 3 4F A3WE 1998012200542 19980122 00542 NM 1998 1 22 DLM88980127 1 19980116 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 962DL 49981 NOSE GEAR UNSAFE (RED) INDICATION WHEN GEAR HANDLE WAS RAISED AFTER TAKEOFF. CYCLED HANDLE SAME RESULTS. LEFT GEAR DOW N AND RETURNED TO ATL. FOUND NOSE STRUT FLAT. SERVICED STRUT. 2 L 7 2 4F RT A6WE 1998012200543 19980122 00543 NM 1998 1 22 DL757980128 1 19980116 A 3350 POWER SUPPLY BPS3 BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 631DL 2077 23612 F/C FLOOR EMERG LIGHTING INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A2NM 1998012200544 19980122 00544 NM 1998 1 22 DL72S980132 1 19980117 A 3350 334102487 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 21145 AFT EXIT AISLE OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, SYSTEM OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1998012200545 19980122 00545 NM 1998 1 22 DL72S980133 1 19980117 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA 20746 OVERHEAD AISLE EMERG LIGHT INOP AT ROW 26. FOUND BATTERY PACK LOOSE. SECURED, OPN CKS OK. 2 L 7 3 4F A3WE 1998012200546 19980122 00546 NM 1998 1 22 DL72S980134 1 19980117 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA 14653 20746 LIGHTED EXIT SIGN EMERG LIGHT INOP OVER RT OVERWING EXIT. REPLACED BATTERY PACK, OPN CKS OK. 2 L 7 3 4F A3WE 1998012200547 19980122 00547 NM 1998 1 22 DL72S980135 1 19980117 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 476DA 24533 20753 AFT LT EXT EMERG LIGHT INOP. REPLACED BATTERY PACK M955, CHKS GOOD. 2 L 7 3 4F A3WE 1998012200548 19980122 00548 WP 1998 1 22 DLL14980136 1 19980117 A 5610 WINDSHIELD 1634896102 LKHEED 1011 1011385115 5265015 WP RT COCKPIT DAMAGED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 737D 3506LR 193C1228 STRONG BURNING ODOR IN COCKPIT FROM F/O WINDSHIELD. REPLACED WINDSHIELD AND CONTROLLER (S/N 3506LR) CONTR (S/N 5080012 ). 2 L 7 3 4F A23WE 1998012200549 19980122 00549 NM 1998 1 22 DL76G980137 1 19980117 A 2130 214C40175 SWITCH BOEING 767 7673P6 1385105 NM CABIN MALFUNCTIONED A DALA O OTHER N FALSE WARNING CL CLIMB 1 SO 27 154DL 25241 PAX OXY MASKS DEPLOYED IN CLIMB AT FL 390. FOUND S119 CABIN ALTITUDE PRESSURE SWITCH AT FAULT MAKING CONTACT AT 6,300 F EET CABIN ALTITUDE INSTEAD OF 14,000 FEET CABIN ALTITUDE. REPLACED SWITCH SYSTEM CHECKS GOOD PER M/M. REPLACED USED OX Y GENERATORS AND STOWED MASKS. 2 L 7 2 4F RT A1NM 1998012200550 19980122 00550 NM 1998 1 22 DLM88980139 1 19980118 A 3222 SCHRADER VALVE DOUG MD88 MD88 3023688 NM NLG STRUT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 911DE 49967 AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT. A/C RETURNED TO CVG. FOUND FLUID LEVEL OK AND LOW ON AIR. REPLACED SCHRA DER VLV, RESERVICED FLUID AND AIR. A/C NOSE JACKED AND NOSE GEAR RETRACTED OK. TAXIED A/C. NOSE STRUT IS NOW HOLD ING FLUID AND AIR. NO OTHER PROBLEMS NOTED. 2 L 7 2 4F RT A6WE 1998012200551 19980122 00551 NM 1998 1 22 DLM88980141 1 19980118 A 3350 20131A BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 937DL 49810 ON LAYOVER, NR 2 CHK OF A/C 937 FOUND EMERGENCY FLOOR TRACK LIGHTING INOP FROM SEAT 24DE TO BACK OF A/C. REPLACED BATT PACK ABOVE SEAT 37DE FOR AFFECTED TRACK LIGHTING, OPS CHK NML. 2 L 7 2 4F RT A6WE 1998012200552 19980122 00552 NM 1998 1 22 DLM88980142 1 19980118 A 3350 20131A BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 938DL 49811 ON LAYOVER, NR 2 CHECK FOUND EMERGENCY TRACK LIGHTING ON FLOOR IN AFT OF A/C INOP. BORROWED EMERGENCY TRACK LIGHTING BA TTERY PACK FROM TWA (S/N 30). INSTLD PACK IN EMERGENCY BATTERY PACK POSITION IN OVERHEAD BIN ABOVE SEAT 37DE. ALL EME RGENCY TRACK LIGHTING OPS CHK NML AT THIS TIME. 2 L 7 2 4F RT A6WE 1998012200553 19980122 00553 NM 1998 1 22 DL72W980143 1 19980106 A 7110 ANGLE BOEING 727 727247 138408F NM NR 2 ENG COWL WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 THE NR 2 ENGINE FWD COWL MATING SURFACE ANGLE (STA 1352) IS WORN AT 6 O'CLOCK POSITION. ROUTED OUT DAMAGE PER MM 53-11- 0 PG 801. INSTALLED REPAIR ANGLE AND FILLES INSTALLED CLOSE OUT PANELS. 2 L 7 3 4F A3WE 1998012200554 19980122 00554 NM 1998 1 22 DL72S980144 1 19980118 A 5730 65877421AND2 SKIN BOEING 727 727225 1384077 NM CENTER WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 CORROSION WAS FOUND DURING 4-37113-3 IN THE CENTER WING LWR SKIN. DAMAGE LOCATED BETWEEN S3C AND S7C FROM RBL 15 TO RBL 32 ON THE LWR SURFACE. REPAIRED PER ERA 331186-14AD. 2 L 7 3 4F A3WE 1998012200555 19980122 00555 WP 1998 1 22 DLL14980145 1 19980118 A 5330 1503140167169 SKIN LKHEED 1011 1011385115 5265015 WP BS 739 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 CORROSION FOUND IN THE STR 41 LAP JOINT ON BOTH UPPER AND LWR SKIN PANELS BETWEEN STA 729 AND 749. REPAIR PER ERA 33116 7-14. 2 L 7 3 4F A23WE 1998012200556 19980122 00556 WP 1998 1 22 DLL14980146 1 19980118 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 729 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 DENTS FOUND IN FUSELAGE SKIN BETWEEN FS 703 AND FS 729, FROM S21 TO S24. REPAIRED PER ERA331174-14. 2 L 7 3 4F A23WE 1998012200557 19980122 00557 NM 1998 1 22 DL72S980147 1 19980119 A 5313 65583873 STRINGER BOEING 727 727232 1384082 NM BS 990 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 STRINGER 30 WAS CORRODED NEAR FS 990. THE STRINGER WILL BE CUT AT FS 990 AND A REPLACEMENT SECTION SPLICED IN. REPAIR PER ERA331185-14. 2 L 7 3 4F A3WE 1998012200558 19980122 00558 NM 1998 1 22 DLM88980149 1 19980117 A 4920 APU DOUG MD88 MD88 3023688 NM AFT FUSELAGE FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 910DE 4007 53419 P80149 DURING CLIMBOUT, CABIN FILLED WITH BLUE SMOKE. RETURNED TO ATL. BOTH PACKS ON AND SMOKE DET CAPTS SIDE AFT WENT OFF. F OUND APU LEAKING OIL. REPLACED APU. 2 L 7 2 4F RT A6WE 1998012200564 19980122 00564 NM 1998 1 22 P5CA9800012 1 19980116 A 5753 FASTENERS BOEING 747 747124 1384874 NM LT TE MIDFLAP MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 L/W O/B T/E MIDFLAP FOUND MISSING FASTENERS. REPLACED MISSING FASTENERS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998012200565 19980122 00565 NM 1998 1 22 P5CA9800013 1 19980116 A 2820 FUEL LINE BOEING 747 747124 1384874 NM NR 1 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 FUEL LINE LOOSE ON NR 1 PYLON BULKHEAD AFT UPPER BLOW OUT PANEL. RE-TORQUED B-NUTS IAW MM 20-11-05. 2 L 7 4 4F A20WE 1998012200566 19980122 00566 NM 1998 1 22 P5CA9800014 1 19980116 A 5753 SKIN BOEING 747 747124 1384874 NM LT TE FOREFLAP GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 GOUGE IN L/W I/B T/E FOREFLAP IN LOWER SURFACE. REPARIED FOREFLAP BY USING FIBERGLASS OVERLAYS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998012200567 19980122 00567 NM 1998 1 22 P5CA9800015 1 19980113 A 5730 FASTENERS BOEING 747 747124 1384874 NM RT WING WORKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 RT WING FLYING PANEL OUTBD ATTACH POINT HAS WORKING FASTENERS. REPAIRED DAMAGED FASTENER HOLES WITH POTTING COMPOUND AN D FIBERGLASS OVERLAYS IAW SRM 51-40-14. 2 L 7 4 4F A20WE 1998012200568 19980122 00568 NM 1998 1 22 P5CA9800016 1 19980110 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING MISSING A P5CA K NONE E D VIBRATION/BUFFET INFLIGHT SEPARATION CR CRUISE 1 WP 23 853FT 19753 DURING CRUISE, MARKED AIRFRAME VIBRATION. REPLACED RT INBD FOREFLAP AND REPAIRED RT INBD MIDFLAP AND RT STABILIZER L/E. ALSO, REPLACED RT FLYING PANEL. 2 L 7 4 4F A20WE 1998012200569 19980122 00569 WP 1998 1 22 RRXA98006 1 19980115 A 2930 PRESSURE IND DOUG DC8 DC863F 302198F WP NR 2/3 HYD SYST MALFUNCTIONED A RRXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 865F 46088 HYD OVER TEMP/AILERON AND RUDDER LIGHT CAME ON DURING FLT. BY-PASSED BOTH ENG PUMPS, THEN ONE AT A TIME (NOTED NO PRESS ). HYD QTY NORMAL, AUX PUMP WORKED NORMAL. RAN NR 2 AND NR 3 ENGS CHECKED BOTH ENG HYD SYSTEMS PUMPS, NO DEFECTS NOTED . PRESSURES WERE NORMAL, TEMP WAS NORMAL, ALL LIGHTS NORMAL. 2 L 7 4 4F 4A25 1998012200570 19980122 00570 SW 1998 1 22 HEEA0012466 1 19980106 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 NR1 TRIPLE TACH INDICATOR NEEDLE INOPERATIVE. 1 G 7 2 4U H4SW 1998012200571 19980122 00571 1998 1 22 HEEA0012467 4 19980106 A 3432 5222638006 INDICATOR BEECH 200 200BEECH 1152920 CE GLIDESLOPE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30PH BB635 COURSE INDICATOR GLIDESCOPE STAYS FLAGGED AND INOPERATIVE. 1 L 7 2 4T A24CE 1998012200572 19980122 00572 1998 1 22 HEEA0012468 4 19980106 A 3417 214175421101 AIR DTA COMPUTER BELL 214 214ST 1182106 SW NR 2 ENG PWR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 ADC DOESN'T SHOW NR2 ENGINE POWER CHECK. 2 G 7 2 4U H10SW 1998012200573 19980122 00573 1998 1 22 HEEA0012469 4 19980106 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW HSI COURSE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 HSI COURSE WINDOW NUMBERS JAMMED. 1 G 7 2 4U H4SW 1998012200574 19980122 00574 1998 1 22 HEEA0012470 4 19980106 A 3425 1113025 INDICATOR SKRSKY S76 S76A 8143006 NE HSI RMI STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5435V 760158 HSI RMI NEEDLE STICKING INTERMITTENTLY. 1 G 7 2 3U H1NE 1998012200575 19980122 00575 1998 1 22 HEEA0012471 4 19980106 A 2210 214074303115 AMPLIFIER ASSY BELL 214 214ST 1182106 SW AUTO FLIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 AMPLIFIER ASSY FAULTY. PITCH CHANNEL WOULD NOT STAY ON LINE. 2 G 7 2 4U H10SW 1998012200576 19980122 00576 SW 1998 1 22 HEEA0012472 1 19980106 A 6321 214175122111 PANEL BELL 412 412 1182202 SW BRAKE WARN MALFUNCTION E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 107X 33113 PILOT SIDE ROTOR BRAKE, LIGHT STAYS ON DIM. 1 G 7 2 4U H4SW 1998012200577 19980122 00577 1998 1 22 HEEA0012473 4 19980106 A 2210 214074305105 AMPLIFIER ASSY BELL 214 214ST 1182106 SW FBW ELEV FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 3897N 28106 AMPLIFIER ASSY TRIPS OFF IN FLIGHT. 2 G 7 2 4U H10SW 1998012200578 19980122 00578 SW 1998 1 22 HEEA0012474 1 19980106 A 7722 206375007103 INDICATOR BELL 206 206L1 1182107 SW ENG TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 20898 45721 TOT INDICAOR INCORRECT READING. 1 G 7 1 3U H2SW 1998012200579 19980122 00579 EU 1998 1 22 HEEA0012475 1 19980106 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER CR CRUISE 1 SW 03 205UC S668 MAST MOMENT INDICATOR PEGS OUT IN FLIGHT. 1 G 7 2 3U H3EU 1998012200580 19980122 00580 EU 1998 1 22 HEEA0012476 1 19980106 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER CR CRUISE 1 SW 03 205UC S668 MAST MOMENT TORQUE TRANSMITTER PEGS OUT IN FLIGHT. 1 G 7 2 3U H3EU 1998012200581 19980122 00581 EU 1998 1 22 HEEA0012477 1 19980106 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 S818 TORQUE TRANSMITTER INOPERATIVE IN TEST MODE. 1 G 7 2 3U H3EU 1998012200582 19980122 00582 EU 1998 1 22 HEEA0012478 1 19980106 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 S818 MAST MOMENT INDICATOR INOPERATIVE IN TEST MODE. 1 G 7 2 3U H3EU 1998012200583 19980122 00583 EU 1998 1 22 HEEA0012479 1 19980106 A 6240 KDW021A WARNING BOX BOLKMS 105 BO105S 5626006 EU ROTOR RPM FAILED E HEEA K NONE N FALSE WARNING CR CRUISE 1 SW 03 6607K S841 ROTOR RPM WARNING LIGHT COMES ON IN FLIGHT. 1 G 7 2 3U H3EU 1998012200584 19980122 00584 1998 1 22 HEEA0012480 4 19980106 A 2210 7690001804103 INDICATOR PANEL SKRSKY S76 S76A 8143006 NE YAW POSITION FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 YAW INDICATOR PANEL FAILED. CANNOT READ POSITIONS. 1 G 7 2 3U H1NE 1998012200585 19980122 00585 EU 1998 1 22 HEEA0012481 1 19980106 A 3610 97914211 VALVE BOLKMS 105 BO105S 5626006 EU BLEED SOV FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 BLEED SOV WOULD NOT OPEN. INOPERATIVE. 1 G 7 2 3U H3EU 1998012200586 19980122 00586 1998 1 22 HEEA0012482 4 19980106 A 2562 3000 ELT BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA ELT OUTPUT DISTORTED. 1 G 7 2 4U H4SW 1998012200587 19980122 00587 1998 1 22 HEEA0012483 4 19980106 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE NR 1 PITCH FAILED E HEEA K NONE F FLT CONT AFFECTED CR CRUISE 1 SW 03 1547D 760077 NR 1 PITCH STARTS TO KICK 45 MINUTES TO 1 HOUR IN FLIGHT. 1 G 7 2 3U H1NE 1998012200588 19980122 00588 1998 1 22 HEEA0012484 4 19980106 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 760275 VERT GYRO PRECESSES. 1 G 7 2 3U H1NE 1998012200589 19980122 00589 1998 1 22 HEEA0012485 4 19980106 A 2562 ACRRLB21 EPIRB BELL 212 212 1181420 SW ANTENNA DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 EPIRB ANTENNA BROKEN AND BODY CRACKS IN BOTTOM. 1 G 7 1 4U H4SW 1998012200590 19980122 00590 SW 1998 1 22 HEEA0012486 1 19980106 A 6220 412030437103 CAP ASSY BELL 412 412 1182202 SW M/R AFT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 AFT CAP ASSY HAS WORN RUBBER. 1 G 7 2 4U H4SW 1998012200591 19980122 00591 SW 1998 1 22 HEEA0012487 1 19980106 A 3340 A490A POWER SUPPLY WHELEN BELL 206 206L1 1182107 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019G 45247 POWER SUPPLY WILL NOT FLASH THE STROBE BULB. 1 G 7 1 3U H2SW 1998012200592 19980122 00592 EU 1998 1 22 HEEA0012488 1 19980106 A 3340 A413AHDACF1428 POWER SUPPLY WHELEN BOLKMS 105 BO105S 5626006 EU LIGHTS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 POWER SUPPLY INOPERATIVE LIGHTS ARE OUT. 1 G 7 2 3U H3EU 1998012200593 19980122 00593 EU 1998 1 22 HEEA0012489 1 19980106 A 3340 A413AHDACF1428 POWER SUPPLY WHELEN BOLKMS 105 BO105S 5626006 EU LIGHTS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 POWER SUPPLY INOPERATIVE. NO OUTLET WORKS, SMALL RATTLE INSIDE. 1 G 7 2 3U H3EU 1998012200594 19980122 00594 SW 1998 1 22 HEEA0012490 1 19980106 A 3340 A413AHDADF1428 POWER SUPPLY WHELEN BELL 206 206L3 1182108 SW LIGHTS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X 51486 POWER SUPPLY INOPERATIVE. 1 G 7 1 3U H2SW 1998012200595 19980122 00595 SW 1998 1 22 HEEA0012491 1 19980106 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 45634 TRANSMISSION RESTRAINT HAS WORN BEARINGS. 1 G 7 1 3U H2SW 1998012200596 19980122 00596 SW 1998 1 22 HEEA0012492 1 19980106 A 7714 206075682107 INDICATOR BELL 206 206L3 1182108 SW GAS PRODUCER ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31073 51519 GAS PRODUCER NEEDLE HAS ERRATIC OPERATION. 1 G 7 1 3U H2SW 1998012200597 19980122 00597 SW 1998 1 22 HEEA0012493 1 19980106 A 2932 205076044007 SWITCH BELL 214 214ST 1182106 SW HYD PRESS FAILED E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 3897N 28106 PRESSURE LIGHT STAYS ON. 2 G 7 2 4U H10SW 1998012200598 19980122 00598 SW 1998 1 22 HEEA0012495 1 19980106 A 2820 2C271 CARTRIDGE BELL 206 206B3 1181506 SW FUEL SYS INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2276B 3628 FUEL SYS CARTRIDGE INOPERATIVE. 1 G 7 1 3U H2SW 1998012200599 19980122 00599 SW 1998 1 22 HEEA0012496 1 19980106 A 5510 206023119151A STABILIZER ASSY BELL 206 206L3 1182108 SW GUIDE PINS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205FC 51130 STAB ASSY GUIDE PINS STUCK. SEPARATED ON FRONT EDGE. 1 G 7 1 3U H2SW 1998012200600 19980122 00600 SW 1998 1 22 HEEA0012497 1 19980106 A 6320 204040386001 CASE ASSY BELL 412 412 1182202 SW M/R XMSN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 CASE ASSY HAS CORROSION PITS ON LOWER FLANGE AND PILOT DATA SURFACES. 1 G 7 2 4U H4SW 1998012200601 19980122 00601 SW 1998 1 22 HEEA0012498 1 19980106 A 6330 206033506101 RESTRAINT BELL 206 206L1 1182107 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10814 45415 TRANSMISSION RESTRAINT BEARINGS WORN. 1 G 7 1 3U H2SW 1998012200602 19980122 00602 SW 1998 1 22 HEEA0012499 1 19980106 A 6320 212040190101 ADAPTER BELL 412 412 1182202 SW SEAL RIDE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 ADAPTER HAS CORROSION AT SEAL RIDE. 1 G 7 2 4U H4SW 1998012200603 19980122 00603 NE 1998 1 22 HEEA0012500 1 19980106 A 7334 7645001078119 TRANSMITTER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 FUEL PRESSURE TRANSMITTER READS HIGH OUT OF TOLERANCE. 1 G 7 2 3U 3 U H1NE E1GL 1998012200604 19980122 00604 SW 1998 1 22 HEEA0012501 1 19980106 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 11 33022 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998012200605 19980122 00605 SW 1998 1 22 HEEA0012502 1 19980106 A 6330 206033554101 LINK ASSY BELL 206 206L1 1182107 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 45381 TRANSMISSION LINK ASSY WORN. 1 G 7 1 3U H2SW 1998012200606 19980122 00606 SW 1998 1 22 HEEA0012503 1 19980106 A 6330 206033518007 STOP ASSY BELL 206 206L1 1182107 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5006F 45181 TRANSMISSION STOP ASSY HAS WORN RUBBER. 1 G 7 1 3U H2SW 1998012200607 19980122 00607 SW 1998 1 22 HEEA0012504 1 19980106 A 6320 212040149001 GEAR ASSY BELL 412 412 1182202 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 GEAR ASSY HAS WORN SEAL RIDE. 1 G 7 2 4U H4SW 1998012200608 19980122 00608 SW 1998 1 22 HEEA0012505 1 19980106 A 6330 206033506103 RESTRAINT BELL 206 206L3 1182108 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251V 51404 TRANSMISSION RESTRAINT HAS BEARINGS WORN. 1 G 7 1 3U H2SW 1998012200609 19980122 00609 SW 1998 1 22 HEEA0012506 1 19980106 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW NR 1 ENG TORQUE STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 NR1 ENGINE TORQUE NEEDLE STICKS AND IS ERRATIC. 1 G 7 2 4U H4SW 1998012200610 19980122 00610 EU 1998 1 22 HEEA0012507 1 19980106 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ROTOR MAST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 TORQUE TRANSMITTER INDICATES HIGH, DOES NOT INDICATE CORRECTLY. 1 G 7 2 3U H3EU 1998012200611 19980122 00611 EU 1998 1 22 HEEA0012508 1 19980106 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 MAST MOMENT INDICATOR INDICATES HIGH, DOES NOT INDICATE CORRECTLY. 1 G 7 2 3U H3EU 1998012200612 19980122 00612 EU 1998 1 22 HEEA0012509 1 19980106 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ROTOR TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 TORQUE TRANSMITTER INDICATES HIGH, DOES NOT INDICATE CORRECTLY. 1 G 7 2 3U H3EU 1998012200613 19980122 00613 EU 1998 1 22 HEEA0012510 1 19980106 A 2422 2A10001G INVERTER BOLKMS 105 BO105S 5626006 EU AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 INVERTER FAILED. NO POWER TO 110 VAC. 1 G 7 2 3U H3EU 1998012200614 19980122 00614 EU 1998 1 22 HEEA0012511 1 19980106 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU OIL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y S669 OIL SYS VALVE WILL NOT OPEN. 1 G 7 2 3U H3EU 1998012200615 19980122 00615 EU 1998 1 22 HEEA0012512 1 19980106 A 7334 BSE206150G3 TRANSDUCER BOLKMS 105 BO105S 5626006 EU FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911EB S812 TRANSDUCER READS HIGH OUT OF TOLERANCE AT 95 PSI. 1 G 7 2 3U H3EU 1998012200616 19980122 00616 1998 1 22 HEEA0012513 4 19980106 A 3425 066304605 HSI CONTROL HUGHES 269 269C 4470504 WP COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6123A S1523 HSI HEADING POINTER WILL NOT INDICATE. 1 G 7 1 3O 4H12 1998012200617 19980122 00617 1998 1 22 HEEA0012514 4 19980106 A 3423 C2300DL4B COMPASS BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251Z 45756 COMPASS [24 VOLT] IS OUT OF LIMITS. 1 G 7 1 3U H2SW 1998012200618 19980122 00618 1998 1 22 HEEA0012515 4 19980106 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE I FLT. ATTITUDE INST. NR NOT REPORTED 1 SW 03 3893N 33010 RATE GYRO INOPERATIVE. WILL NOT PULL RT FLAG ON HSI AND WILL NOT SHOW DEFLECTION IN TURN. 1 G 7 2 4U H4SW 1998012200619 19980122 00619 SW 1998 1 22 HEEA0012516 1 19980106 A 2820 214066226103 CHECK VALVE BELL 412 412 1182202 SW FUEL SYS LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1202T 33112 CHECK VALVE LEAKS THROUGH WIRES. 1 G 7 2 4U H4SW 1998012200692 19980122 00692 SW 1998 1 22 ASE98001 1 19980102 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW LANDING GEAR MALFUNCTIONED A EQGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 19 702M AC702 DFW-ELD - FLT 1253 - AFTER TAKEOFF, WHEN GEAR WAS SELECTED UP, GEAR FAILED TO RETRACT. CONTINUED CLIMB TO SAFE LEVEL AN D COMPLETED CHECKLIST, CONTACTED ATC FOR CLEARANCE TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND EMERGENCY EXTENSION SELECTOR IN EMERGENCY POSITION. MAINTENANCE ISSUED A SPECIAL FLIGHT PERMIT FROM DFW-HOT WITH GEAR LOCKED DOWN FOR PURPOSES OF FURTHER MAINTENANCE. AIRCRAFT WAS PLACED ON JACKS IN HOT AND EMERGENCY EXTENSION SLECTOR MOVED TO NORM POSITION. GEAR WAS SWUNG NUMEROUS TIMES WITH NORMAL RESULTS. A/C WAS DETERMINED SERVICEABLE AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998012200693 19980122 00693 NM 1998 1 22 ASE97013 1 19980102 A 7330 BYPASS LIGHT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE FUEL SYSTEM ILLUMINATED A EQGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 19 350AD 3050 ASE-DEN - FLT 368 - DURING TAKEOFF ROLL, PRIOR TO 70 KNOTS, AN AMBER FUEL FILTER BYPASS MESSAGE APPEARED ON THE CAS FIEL D. CREW ELECTED TO ABORT THE TAKEOFF AND TAXIED CLEAR OF THE RUNWAY. AT THIS POINT, THE MESSAGE HAD DISAPPEARED AND TH ERE WERE NO OTHER INDICATIONS OF AN ABNORMAL CONDITION. THE CREW RETURNED TO THE GATE AND CONSULTED MAINTENANCE. MAINT ENANCE AND THE FLIGHT CREW PERFORMED A FULL RUN UP WITH ALL INDICATIONS NORMAL. AIRCRAFT WAS RELEASED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A45NM E20NE 1998012200694 19980122 00694 SW 1998 1 22 ASE97012 1 19980102 A 2910 27810322682 HYDRAULIC LINE FRCHLD SA227 SA227DC 3377521 SW LT MLG WW CRACKED A EQGA O OTHER J S WARNING INDICATION AFFECT SYSTEMS AP APPROACH 1 SW 19 847LS DC847B FLT 1217 - DFW-HOT - ON APPROACH IN TO HOT, OBSERVED A HYDRAULIC PRESSURE FLUCTUATION. CREW MANUALLY EXTENDED LANDING G EAR AND LANDED IN HOT WITHOTU INCIDENT. UPON ARRIVAL, CREW NTOED OBVIOUS SIGNS OF LEAKAGE IN LEFT WHEEL WELL. MAINTENA NCE CONTROL WAS NOTIFIED. MAINTENANCE INSPECTED LEFT WHEEL WELL AND IDENTIFIED CRACKED HYDRAULIC LINE. LINE WAS REPLAC ED AND HYDRAULIC SYSTEM SERVICED ACCORDINGLY. OPERATIONAL AND LEAK CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A18SW 1998012200739 19980122 00739 NM 1998 1 22 TWAA9800201 1 19980102 A 3260 69482723 CARD BOEING 727 727231 1384079 NM RT MLG FAILED A TWAA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 54334 20461 LIT - FLT 207 - DURING APPROACH, RIGHT MAIN LANDING GEAR DOWN GREEN LIGHT NOT INDICATED. REPLACED MASTER DIM AND TEST C ARD MFG PART NR 69-48272-3. (M) 2 L 7 3 4F A3WE 1998012200740 19980122 00740 WP 1998 1 22 TWAA9800202 1 19980102 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A TWAA K NONE O OTHER TX TAXI/GRND HDL 1 CE 05 998R 47030 STL - FLT 693 - DURING SCHEDULED INSPECTION, FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998012200741 19980122 00741 WP 1998 1 22 98ZZZM83 1 19980102 A 3350 6011777 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A TWAA K NONE O OTHER TX TAXI/GRND HDL 1 CE 05 998R 47030 STL - FLT 693 - DURING SCHEDULED INSPECTION, FOUND LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998012200742 19980122 00742 NM 1998 1 22 TWAA9800203 1 19980103 A 3260 IN3311B DIODE BOEING 727 727231 1384079 NM RT MLG FAILED A TWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CE 05 54334 20461 DTW - FLT 267 - DURING APPROACH, NO GREEN DOWNLOCK LIGHT ON RIGHT MAIN LANDING GEAR. REPLACED LIGHT SOCKET DIODE MFG P/ N IN3311B. (M) 2 L 7 3 4F A3WE 1998012200743 19980122 00743 NM 1998 1 22 TWAA9800204 1 19980104 A 2150 6411002 SWITCH BOEING 727 727231 1384079 NM RT PACK FAILED A TWAA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 54342 21629 PHX - FLT 646 - DURING CLIMB, UNABLE TO MAINTAIN CABIN BELOW ONE THOUSAND FEET AT FL210 ONE PACK INOP. REMOVED DEBRIS F ROM UNDER C-3 DOOR SEAL AND REPLACED RT PACK TEMP SWITCHES. (M) 2 L 7 3 4F A3WE 1998012200744 19980122 00744 NM 1998 1 22 98ZZZM84 1 19980104 A 2150 5486206 SWITCH BOEING 727 727231 1384079 NM RT PACK FAILED A TWAA J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 54342 21629 PHX - FLT 646 - DURING CLIMB, UNABLE TO MAINTAIN CABIN BELOW ONE THOUSAND FEET AT FL210 ONE PACK INOP. REMOVED DEBRIS F ROM UNDER C-3 DOOR SEAL AND REPLACED RT PACK TEMP SWITCHES. (M) 2 L 7 3 4F A3WE 1998012200745 19980122 00745 NM 1998 1 22 TWAA9800205 1 19980104 A 2150 32167441 VALVE BOEING 727 727231 1384079 NM RT PACK SOV FAILED A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 54334 20461 MCI - FLT 653 - DURING CLIMB, UNABLE TO CONTROL CABIN PRESSURE 6.0 MAXIMUM PSI DIFFERENTIAL. REPLACED RIGHT FORWARD PAC K SHUTOFF VALVE. (M) 2 L 7 3 4F A3WE 1998012200746 19980122 00746 NM 1998 1 22 TWAA9800206 1 19980104 A 5210 MECHANISM BOEING 727 727231 1384079 NM PAX DOOR OUT OF ADJUST A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 54351 21983 STL - FLT 385 - DURING CLIMB, R-1 DOOR LEAKING AND UNABLE TO PRESSURIZE CABIN. ADJUSTED DOOR RIG. (M) 2 L 7 3 4F A3WE 1998012200747 19980122 00747 NM 1998 1 22 TWAA9800301 1 19980103 A 2730 401602728 COMPUTER BOEING 727 727231 1384079 NM ELEV FEEL SYSTEM FAILED A TWAA A J UNSCHED LANDING DUMP FUEL K FLUID LOSS CL CLIMB 1 CE 05 24343 4005D 21630 FLT 475 - STL - DURING CLIMB, SYSTEM 'A' HYDRAULIC LOW PRESSURE LIGHTS ILLUMINATED WITH AN ASSOCIATED HYD QTY LOSS. FUE L DUMPING WAS USED. FOUND THE ELEVATOR FEEL COMPUTER WITH A RUPTURED SEAL. REPLACED FEEL COMPUTER P/N 401-60272-8. OP ERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998012200748 19980122 00748 WP 1998 1 22 TWAA9800302 1 19980103 A 3244 9550267 TIRE DOUG DC9 DC932 3022066 WP NLG PUNCTURED A TWAA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 05 996Z 47028 RDU - FLT 639 - DURING PUSHBACK, THE TOW BAR PIN BROKEN AND PUNCTURED THE RIGHT NOSE GEAR TIRE. REPAIRED TOW BAR PIN. R EPLACED RIGHT NOSE TIRE AND WHEEL ASSY MFG P/N 9550267. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1998012200749 19980122 00749 WP 1998 1 22 TWAA9800101 1 19980101 A 2131 21171802 CONTROLLER DOUG DC9 DC982 3022082 WP CABIN FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 957U 49702 IAD - FLT 123 - DURING CRUISE AT 27,000 FT, LOST PRIMARY AND SECONDARY PRESSURIZATION CONTROL REMOVED AND REPLACED NR 1 PRESS CONTROL, MFG NR 2117180-2. (M) 2 L 7 2 4F A6WE 1998012200754 19980122 00754 EU 1998 1 22 SIMA980011 1 19980101 A 2121 EVTA1926DC FAN AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 251AE 418 250 ORD - FLT 4164 - CAPTAIN NOTED, AFTER POWERING UP A/C, SMOKE WAS COMING FROM QUADRANT AND STRONG SMOKE SMELL WAS IN CABI N AND COCKPIT. MX INSPECTED AND FOUND AVIONICS VENT FAN BURNED. RAI FAN IAW JIC 21-23-21. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998012200768 19980122 00768 EU 1998 1 22 RAIA980103 1 19980105 A 2612 516531152 FIRE CONTROLLER AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FAILED A RAIA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7408 - STL - RIGHT ENGINE FIRE INDICATION ILLUMINATED, CREW FIRED BOTH ENGINE FIRE BOTTLES AFTER ENGINE SHUTDOWN. M AINTENANCE INSPECTED FOUND FAULTY FIRE WIRE CONTROLLER GIVING ERRONEOUS WARNING, REPLACED CONTROLLER. (M) 2 H 7 2 4T RT A53EU 1998012200769 19980122 00769 1998 1 22 RAIA980104 4 19980105 A 3452 6226590001 CONTROL ADAPTER BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 340TE 939 FLT 7025 - STL - SMOKE ODOR N COCKPIT, BOTH TRANSPONDERS INOPERATIVE. MAINTENANCE REPLACED ATC CONTROL ADAPTER. (M) 2 L 7 2 4T RT A56EU 1998012200805 19980122 00805 EU 1998 1 22 ASOA98001 1 19980102 A 5315 S53572505200 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 DURING SCHEDULED MAINTENANCE, FOUND CRACKED FLOORBEAM AT FRAME 26. INSPECTED FLOORBEAM IAW AI (R) FAX QS/ET603.4275/97, DS/ET603.4237/97 AND EO72-53-0026, SPECIFICATIONS FOR INSPECTION AT C-CHECK AND REINSPECTION EVERY 750 FLIGHTS. (M) 2 H 7 2 4T RT A53EU 1998012200808 19980122 00808 NM 1998 1 22 TAOA019801 1 19980103 A 2421 976J4981 GENERATOR BOEING 727 727227 1384078 NM NR 1 ENGINE FAILED A TAOA O OTHER J H WARNING INDICATION ELECT. POWER LOSS-50 PC AP APPROACH 1 EA 15 927TS 20837 FLT 6041 - BOS-LGA - WHILE ON APPROACH FOR LANDING AT LAGUARDIA AIRCRAFT HAD AN UNDER VOLTAGE ON NR 1 GENERATOR. EXECUT ED A GO-AROUND AND RAN CHECKLIST FOR ELECTRICAL FAILURE. REPLACED NR 1 GENERATOR, OPERATIONAL CHECK NORMAL IAW MM CHAPT ER 24-20-1. (M) 2 L 7 3 4F A3WE 1998012200813 19980122 00813 NM 1998 1 22 P2EA98001 1 19980101 A 7110 657019426 PANELS BOEING 737 737244 138448U NM NR 2 ENGINE MISSING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 PIT - FLT 424 - DURING POST FLIGHT WALKAROUND INSPECTION, 2 AFT COWLING PANELS WERE NOTED MISSING ON NR 2 ENGINE. REPLA CED MISSING COWLING PANELS. SECURED LATCHES. NO OTHER DEFECTS NOTED. A/C OK FOR SERVICE. COWL PANELS DEPARTED A/C DU RING T/O ROLL AT MDW. MISSING COWL PANELS WERE LOCATED ON RUNWAY AT MDW. (M) 2 L 7 2 4F A16WE 1998012200814 19980122 00814 NM 1998 1 22 98ZZZM85 1 19980101 A 7110 6570193509 PANELS BOEING 737 737244 138448U NM NR 2 ENGINE MISSING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 PIT - FLT 424 - DURING POST FLIGHT WALKAROUND INSPECTION, 2 AFT COWLING PANELS WERE NOTED MISSING ON NR 2 ENGINE. REPLA CED MISSING COWLING PANELS. SECURED LATCHES. NO OTHER DEFECTS NOTED. A/C OK FOR SERVICE. COWL PANELS DEPARTED A/C DU RING T/O ROLL AT MDW. MISSING COWL PANELS WERE LOCATED ON RUNWAY AT MDW. (M) 2 L 7 2 4F A16WE 1998012200822 19980122 00822 NM 1998 1 22 MASA98003 1 19980105 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 436YV 436 DURING LINE CHECK INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHE CK GOOD. (M) 2 H 7 2 4T RT A13NM 1998012200823 19980122 00823 SO 1998 1 22 MASA98001 1 19980101 A 3350 1317 BULB EMB 120 EMB120RT SO LT EXTERIOR FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 269UE 120194 FLT 5558 - JAX-GNV - CREW FOUND EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998012200989 19980122 00989 NM 1998 1 22 CALA9800076 1 19980116 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1283 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 INCH CRACK IN FRAME TO FUSELAGE ATTACH ANGLE IN AFT STAIR COMPARTMENT, RT SIDE, STA 1283. THE ANGL E WAS REMOVED, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998012200990 19980122 00990 NM 1998 1 22 CALA9800077 1 19980116 A 5730 SKIN BOEING 727 727227 1384078 NM WS 224 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 2 INCH CRACK IN RT WING LEADING EDGE LOWER SKIN ABOVE NR 5 LEADING EDGE FLAP ACTUATOR, WS 224. THE C RACKED AREA WAS REMOVED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998012200991 19980122 00991 NM 1998 1 22 CALA9800078 1 19980116 A 5720 BRACKET BOEING 727 727227 1384078 NM WS 232 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .2812 INCH CRACK OUTBOARD OF NR 8 SPOILER ACTUATOR IN RT WING INBOARD TRAILING EDGE PANEL SUPPORT BRA CKET AT WS 232. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30- 2 AND ECRA 5750-02878. 2 L 7 3 4F A3WE 1998012200992 19980122 00992 WP 1998 1 22 CALA9800079 1 19980117 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58545 47094 INSPECTION FOUND THREE EACH .5 INCH CRACKS AT RIVETS OF AFT PRESSURE BULKHEAD T-CAP SKIN, STA 996, LONGERON 8-9R. A SKI N REPAIR WAS INSTALLED IAW DACO DRAWING J060138. 2 L 7 2 4F A6WE 1998012200993 19980122 00993 NM 1998 1 22 CALA9800080 1 19980117 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUT ON UPPER FORWARD FLANGE LOWER SURFACE AT STA 328, LBL 48. THE FLOORBEAM W AS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 53-10-8 AND 53-20-11. 2 L 7 3 4F RT A3WE 1998012200994 19980122 00994 NM 1998 1 22 CALA9800081 1 19980117 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND FLOORBEAM CORRODED AT CLIPNUTS, STA 380, RBL 24 TO RBL 62. TWO L-ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-30-8 FIGURE 8. 2 L 7 3 4F RT A3WE 1998012200995 19980122 00995 NM 1998 1 22 CALA9800082 1 19980117 A 5330 SKIN BOEING 727 727243 138408D NM BS 1060 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1060, STRINGER 27L. THE CORROSION WAS REMOVED AND THE SKIN WAS REPAIRED IAW SRM 53-30-3. 2 L 7 3 4F RT A3WE 1998012200996 19980122 00996 NM 1998 1 22 CALA9800083 1 19980119 A 4920 38067811 TORUS BOEING 727 727243 138408D NM APU COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 26244 21270 INSPECTION FOUND A 5 INCH CRACK IN INBOARD WELD SEAM OF APU TORUS ASSEMBLY. THE APU WAS REMOVED AND REPLACED IAW MM 49- 10-01. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F RT A3WE 1998012200997 19980122 00997 NM 1998 1 22 CALA9800084 1 19980117 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 10 TO RBL 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998012200998 19980122 00998 NM 1998 1 22 CALA9800085 1 19980117 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, BBL 0 TO RBL 30. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998012200999 19980122 00999 1998 1 22 HEEA0012584 4 19980115 A 3413 212070239001 INDICATOR BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 RATE OF CLIMB INDICATOR. INSPECT FOR POSSIBLE WATER DAMAGE. COMPLY WITH ASB 214ST-97-79, PART 2. 1 G 7 2 4U H4SW 1998012600001 19980126 00001 NM 1998 1 26 DL73K980066 1 19980109 A 4950 3804285 APU BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE AFT FUSELAGE ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 319DL 24947 23091 P50172 SMOKE ALARM WENT OFF IN FWD LAV CREW COULD SMELL ACRID SMELL. FOUND APU PUTTING OIL INTO PNEUMATIC DUCTS. FWD APU TO M CO REPLD DETECTOR BATTERY, REPLD LT AND RT COALESCER BAGS RAN BOTH ENGS AT 1.80 EPR FOR APPROX 15 MINS TO BURN OIL SMEL L OUT. 2 L 7 2 4F 4 F RT A16WE E2EA 1998012600002 19980126 00002 WP 1998 1 26 DLL19980077 1 19980112 A 2612 RB211524B4I FIRE WARNING LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 3 ENGINE FALSE WARNING A DALA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SO 27 763DL 193Y1197 014782 NR 3 ENG FIRE WARNING INFLIGHT. SHUT DOWN ENG IAW POM. FUEL AND IGN OFF, FIRE HDL PULLED, HYD PUMP OFF AND IDG DISC. R EPLACED UPPER AND LOWER GAS GENERATOR LOOP ASSYS. 2 L 7 3 4F 4 F A23WE E12EU 1998012600005 19980126 00005 NM 1998 1 26 P5CA9800011 1 19980116 A 5753 SKIN BOEING 747 747124 1384874 NM LT TE FOREFLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEVEL 1 CORROSION FOUND ON L/W O/B T/E FOREFLAP SURFACE. REMOVED CORROSION AND TREATED IAW SRM 51-10-06. 2 L 7 4 4F A20WE 1998012600010 19980126 00010 NM 1998 1 26 TSAA9833001 1 19980101 A 3350 8731002511 SIGN BOEING 737 737230C 1384472 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 ON SERVICE CHECK, FOUND FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED IDENTIFIER ASSY. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998012600021 19980126 00021 NM 1998 1 26 VNAA9801007 1 19980116 A 3260 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LANDING GEAR DIRTY A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 436JS 3052 DURING TAXI FOR TAKEOFF, A PROXY SYSTEM FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATIO N MAINTENANCE INSPECTED AND CLEANED THE LDGLK1 CANNON PLUG, THEN PERFORMED OPERATIONAL TEST IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-60-00. THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998012900001 19980129 00001 NM 1998 1 29 UPS98225511 1 19980120 A 3350 COVER BOEING 727 727247 138408F NM PAX DOOR FELL OFF A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE-N/A, EMERG EXIT LIGHT OVER MAIN DOOR COVER FELL OFF. RESECURED COVER F/EMER LIGHT, CKS NORMAL. 2 L 7 3 4F A3WE 1998012900002 19980129 00002 WP 1998 1 29 UPS98825503 1 19980119 A 5313 STRINGER DOUG DC8 DC871F 302199D WP CFM56 BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-B CK, CORROSION FOUND AT STR 30R BETWEEN STR 25 TO 35 DOME NUT ATTACH POINTS FOR EXTERNAL AIR COND DOOR GRND HOOK UP. EXPOSED STRINGER AREAS WITH CORROSION. BLENDED 5 AERAS OF CORROSION PERFORMED THICKNESS TEST PER QC THIC KNESS TESTER CL304. REPAIRED PER EO DC8-5310-9989. 2 L 7 4 4F RT 4A25 1998012900003 19980129 00003 WP 1998 1 29 UPS98825504 1 19980108 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN CABIN FLOOR BOARD SUPPORT CORROSION REMOVAL BEYOND ALLOWABLE LIMITS FS 1680 RBL 5 TO RBL 28. RE MOVED, FABRICATED, AND INSTALLED REPLACEMENT SUPPORT IAW SRM 57-7-3 FIG 5A. 2 L 7 4 4F RT 4A25 1998012900004 19980129 00004 WP 1998 1 29 UPS98825505 1 19980112 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 879-940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN GEAR WHEEL WELL PRESSURE FLOOR UPPER SURFACE DOUBLERS CORRODED BEYOND LIMITS FS 879 TO 940 LBL 6 TO RBL 6. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 51-1-21 AND DWG 5645332-123, 125, AND 127. 2 L 7 4 4F RT 4A25 1998012900005 19980129 00005 WP 1998 1 29 UPS98825506 1 19980102 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 20 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, SEVERAL POPPED FASTENERS AND BULGING CORROSION UNDER FINGER DOUBLER AT LBL 24 FS -20 COCKPIT SUBFLOOR . REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-3-1 AND DWG 5612298. 2 L 7 4 4F RT 4A25 1998012900011 19980129 00011 WP 1998 1 29 UPS98825513 1 19980104 A 5320 CLIP DOUG DC8 DC873F 302199F WP BS 220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, LONGERON 1 ATTACH CLIP CORRODED BEYOND LIMITS FS 220. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIP IAW SRM 51-1-21 AND DWG 2643619. 2 L 7 4 4F RT 4A25 1998012900013 19980129 00013 WP 1998 1 29 UPS98825515 1 19980113 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, SEAT TRACK CORROSION REMOVAL BEYOND LIMITS FS 902 LBL 60. REMOVED, FABRICATED, AND INSTALLED REPLACE MENT SECTION IAW SRM 53-7-3. 2 L 7 4 4F RT 4A25 1998012900014 19980129 00014 NM 1998 1 29 QXEA9800033 1 19980116 A 2400 ELECT SYST DHAV DHC8 DHC8102 2809003 NM E/E COMPT DAMAGED A QXEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NM 09 820PH 63 EN ROUTE, ACFT EXPERIENCED ST ELMOS FIRE ON THE WINDSHIELD WITH SOME PRECIPITATION STATIC. THE MASTER CAUTION LIGHT CAM E ON. STARTED THE EMERGENCY CHECKLIST. PULLED LT TRU CIRCUIT BREAKER. 1 MIN LATER, EXPERIENCED LOSS OF PANEL LIGHT ON THE OVERHEAD, GLARESHIELD AND THE CAPTAIN'S INSTRUMENTS. THE DC VOLTMETER SHOWED ONLY BATTERY POWER. RETURNED TO PDX. RESET AC/DC GENERATORS, ALL POWER CAME BACK AND STAYED ON UNTIL LOWERED THE GEAR ON FINAL. AFTER THE GEAR CAME DOWN, EXPERIENCED NR 1 AC GENERATOR CAUTION LIGHT (THE GEN WON'T RESET). ACFT LANDED WITHOUT INCIDENT. MX R/R NR 1 AC GEN, N R 1 GCU, AC PWR MONITOR, AC PWR MONITOR ELEC CONNECTOR AND REMOTE CONTROL C/B. PERFORMED TEST OF THE ELEC SYSTEM. 2 H 7 2 4T RT A13NM 1998012900015 19980129 00015 EU 1998 1 29 QXEA9800037 1 19980120 A 3350 MGG1055 BULB GRIMES 5515900004 FOKKER F28 F28MK4000 4990810 EU GALLEY FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 EMERGENCY LIGHT AT THE GALLEY SERVICE DOOR IS INOP. MAINTENANCE RELAMPED THE EMERGENCY LIGHT AT THE GALLEY SERVICE DOOR , OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998012900016 19980129 00016 NM 1998 1 29 98FDEA00043 1 19980120 A 3260 CONNECTOR BOEING 727 727233 138408A NM NLG CORRODED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 269FE 21675 NOSE GEAR UNSAFE LIGHT (RED) WITH LANDING GEAR HANDLE UP. ALL DOOR LIGHTS OUT. (CYCLED GEAR AND PROBLEM REMAINS, RED N OSE GEAR LIGHT ON) NOTE: NORMAL GEAR DOWN, NORMAL HYDRAULICS. AFTER 45 MINUTES, GREEN NOSE GEAR LIGHT ALSO ILLUMINATED AT THE SAME TIME, BUT RATHER DIM. *S/D* INSTALL 3 GEAR PINS. WHILE CHECKING POSITION AND LOCK SWITCHES PER M/M 32-61 -71 DUPLICATED PROBLEM. FOUND CORROSION IN CANNON PLUG FOR POSITION SWITCH. CLEANED CORROSION FROM SWITCH AND CANNON P LUG. SYSTEM FUNCTIONAL CHECK OK, PER M/M 32-61-71. GEAR PINS REMOVED. 2 L 7 3 4F RT A3WE 1998012900075 19980129 00075 NM 1998 1 29 DHL98708001 1 19980121 A 3270 BACC45FT12C12S CONNECTOR BOEING 727 72725 1384006 NM TAIL SKID WATER CONTAM A DHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 708DH 18275 ON APPROACH AFTER GEAR EXTENSION, NOTED NO TAIL SKID LIGHT. CYCLED AT 500 FEET AGL, GOT TOO LOW GEAR ON GPWS. EXECUTE D GO-AROUND. EXECUTED PROCEDURES AND CYCLED GEAR, DURING GEAR EXTENSION, TAIL SKID CAME DOWN AND LANDED NORMALLY. INS P AND TEST TAIL SKID PER M/M. FOUND WATER IN CANNON PLUG. CLEANED, OPS CHECK NORMAL. PERFORMED SELF TEST ON GPWS, NOR MAL INSP AND INSPECT CHECKED LDG SYSTEM FOUND NORMAL. 2 L 7 3 4F A3WE 1998012900076 19980129 00076 WP 1998 1 29 RRXA98007 1 19980120 A 3230 UPLATCH DOUG DC8 DC871 302199A WP LANDING GEAR LACK OF LUBE A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 811AL 46099 FAILED GEAR UPLATCH CHECK, ACCOMPLISHED QRH PROCEDURES, NO HELP. SOUNDS LIKE NOSE GEAR COMING OUT. FOUND NOSE GEAR UPL ATCH AND LEFT GEAR UPLATCH STIFF. LUBED BOTH UPLATCHES. OPS CHECKS GOOD ON NUMEROUS RETRACTION CYCLES IAW MM 7-11-0 AN D 32-30-0. 2 L 7 4 4F 4A25 1998012900077 19980129 00077 NM 1998 1 29 K3HA980003 1 19980113 A 3350 0816901 SOCKET BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY PATH LIGHT LENS AND SOCKET ASSEMBLY MISSING ADJACENT TO SEAT ROW 3ABC. REPLACED EMERGENCY PATH SOCKET ASSEMBL Y AND LENS (P/N 07912) AT ROW 3ABC, OPS CHECK OK ON TEST. 2 L 7 3 4F A3WE 1998012900078 19980129 00078 NM 1998 1 29 K3HA980004 1 19980113 A 3350 07912 LENS BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY PATH LIGHT LENS MISSING ADJACENT TO SEAT ROW 25DEF. REPLACED LIGHT LENS EMERGENCY PATH MISSING ADJACENT TO SE AT ROW 25DEF. 2 L 7 3 4F A3WE 1998012900079 19980129 00079 NM 1998 1 29 K3HA980005 1 19980113 A 3350 08199000111 TRACK BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY PATH LIGHT TRACK LAST TWO FEET OF TRACK TAPED OVER. REPLACED UPPER AND LOWER TRACK LAST TWO FEET, OPS CHECK G OOD. 2 L 7 3 4F A3WE 1998012900093 19980129 00093 SW 1998 1 29 98ZZZX324 1 19980114 A 5312 222031056103 BULKHEAD BELL 222 222U 1182140 SW BS 270 CRACKED A S A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 222HX 47533 FOUND 2 EACH CRACKS IN AFT MAIN ROOF BEAM AT LT NODAL BEAM SUPPORT. BS 270, WL 79.0, LBL 9.90. 1 G 7 2 3U H9SW 1998012900095 19980129 00095 NM 1998 1 29 98ZZZX326 1 19980112 A 2612 DETECTOR BOEING 727 727223 1384074 NM NR 1 ENG STRUT MALFUNCTIONED A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 6822 19700 MIA - ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT. (APPROXIMATELY 1,000 AFL). CONDUCTED AND COMPLETED STRUT OVERHEAT LIGHT EMERGENCY CHECKLIST. RETARDED NR 1 THROTTLE TO IDLE LIGHT (STRUT NR 1). EXTINGUISHED AFTER 1.50 MINUTE S. REPLACED NR 1 ENGINE STRUT OVERHEAT DETECTION ELEMENT. NR 1 STRUT OVERHEAT DETECTION TESTS OK. NO LEAKS FOUND IN S TRUT AREA ON RUN-UP. NO OVERHEAT WARNING ON ENGINE RUN. 2 L 7 3 4F A3WE 1998012900096 19980129 00096 NM 1998 1 29 98ZZZX327 1 19980112 A 2400 BREAKER BOEING 727 727223 1384074 NM FE PANEL SMOKE A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 709AA 22466 ORD - AFTER TAKEOFF, SMOKE AND FUMES FROM BEHIND F/E. PULLED RADIO PRIMARY CIRCUIT BREAKER AND SMOKE AND FUMES WENT AWA Y. REF: PREVIOUS WRITE-UP 07. REPLACED PANEL AND INSTALLED RADIO PRIMARY CIRCUIT BREAKER AND VARIABLE CONTROL TRANSFO RMER. CHECKED ALL CENTER PANEL LIGHTS FOR ONE HOUR AND CHECKED BEHIND B-18 CIRCUIT BREAKER PANEL. ALL CHECKED NORMAL. 2 L 7 3 4F A3WE 1998012900137 19980129 00137 EU 1998 1 29 MALA975901 1 19980122 A 2450 A2043C PDU SAAB SF340 SF340A 7850100 EU RIGHT FAILED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 68XJ 068 DURING INSPECTION, A STRONG ELECTRICAL BURNING SMELL WAS NOTED COMING FROM THE GPU RECEPTACLE AREA. MAINTENANCE FOUND P OSITIVE WIRES OVERHEATED, REPLACED THE RIGHT PDU AND RESECURED WITH NEW POSITIVE WIRES. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012900138 19980129 00138 NM 1998 1 29 MALA975902 1 19980121 A 3350 10126269 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 822MA 326 DURING INSPECTION, THE RIGHT EMERGENCY EXIT WINDOW STRIP LIGHT BROKEN. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CH ECK GOOD. 2 H 7 2 4T RT A13NM 1998012900139 19980129 00139 NM 1998 1 29 MALA975903 1 19980121 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 DURING INSPECTION 2 EXITS SIGNS WITH ONE BURNT OUT BULB EACH. MAINTENANCE REPLACED BULB IN BOTH EXIT SIGNS. ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998012900140 19980129 00140 EU 1998 1 29 MALA975904 1 19980119 A 2611 SMOKE LIGHT SAAB SF340 SF340A 7850100 EU AVIONICS COMPT ILLUMINATED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 76XJ 076 AFTER LANDING, THE CREW REPORTED AVIONICS SMOKE WARNING LIGHT ILLUMINATED FOR 2 MINUTES, THEN EXTINGUISHED. MAINTENANCE REMOVED AFT AVIONICS COMPARTMENT PANEL, INSPECTED EQUIPMENT, WIRING AND COMPARTMENT. NO DEFECTS NOTED. ALL CHECKS GOO D, ALL AVIONICS SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900141 19980129 00141 EU 1998 1 29 MALA975905 1 19980119 A 3040 7256100501 TERMINAL SAAB SF340 SF340A 7850100 EU LT COCKPIT MELTED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 107XJ 340A107 DURING FLIGHT, A BURNING SMELL COMING FROM THE LEFT AC SYSTEM, CREW SHUT OFF BLEED SYSTEM. AIRCRAFT LANDED WITHOUT INCI DENT. MAINTENACE FOUND LOWER TERMINAL BLOCK MELTED ON WINDSHIELD, REPLACED WINDSHIELD. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012900142 19980129 00142 EU 1998 1 29 MALA975906 1 19980120 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 89XJ 089 DURING INSPECTION, ROW 7/8 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED OVERHEAD EMERGENCY LIGHT. ALL CHECKS GO OD. 2 L 7 2 4T RT A52EU 1998012900143 19980129 00143 EU 1998 1 29 MALA975907 1 19980120 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 89XJ 089 DURING INSPECTION, EMERGENCY LIGHT AT ROW 1 INOP. MAINTENANCE RELAMPED OVERHEAD EMERGENCY LIGHT. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012900144 19980129 00144 1998 1 29 MALA975908 2 19980120 A 7530 5056T88PO1 SHUTOFF VALVE SAAB SF340 SF340A 7850100 EU LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 98XJ 098 DURING CLIMB-OUT, THE LT AIR VALVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT BLEED AI R SHUTOFF VALVE. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012900145 19980129 00145 EU 1998 1 29 MALA975909 1 19980120 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 103XJ 340A103 DURING INSPECTION, THE EMERGENCY LIGHT AT 9A INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT AT 9A. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012900146 19980129 00146 NM 1998 1 29 MALA975910 1 19980120 A 3350 1013075 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 828MA 333 DURING INSPECTION, ONE RED EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998012900147 19980129 00147 EU 1998 1 29 MALA975911 1 19980121 A 3020 ND0075220033 THERMAL CONTROL SAAB SF340 340B 7860101 EU LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 592MA 340B199 AFTER TAKEOFF, THE LEFT ENGINE INTAKE HEAT LIGHT ILLUMINATES, INTERMITTENTLY. AIRCRAFT RETURNED TO MSP. MAINTENANCE RE PLACED THE THERMAL CONTROLLER. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012900148 19980129 00148 NM 1998 1 29 W8PA980020 1 19980120 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN DISCONNECTED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 DEN - TWO EMERGENCY TRACK LIGHTS ARE INOP AT ROW 18. RECONNNECTED WIRES, AT ROW 18. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998012900149 19980129 00149 NM 1998 1 29 W8PA980021 1 19980121 A 3350 LAMP BOEING 737 7373B7 1384580 NM CABIN FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 951WP 22951 DEN - AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IS INOP. REPLACED LAMP, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998012900150 19980129 00150 NM 1998 1 29 W8PA980022 1 19980117 A 3350 1619 LAMP BOEING 737 737317 138447P NM R1 DOOR FAILED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 946WP 23173 DEN - R1 DOOR EMERGENCY LIGHT ON EXTERIOR OF AIRCRAFT IS INOP. REPLACED LAMP, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998012900152 19980129 00152 NM 1998 1 29 W8PA980026 1 19980119 A 3350 CONNECTOR BOEING 737 7373B7 1384580 NM CABIN DISCONNECTED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 951WP 22951 DEN - EMERGENCY TRACK LIGHT INOP AT ROW 15. RECONNECTED EMERGENCY LIGHT. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998012900153 19980129 00153 EU 1998 1 29 AWXA9800024 1 19980118 A 3350 2514353 LENS AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 637AW 099 EMERGENCY EXIT LIGHT COVER 9D BROKEN. INSTALLED NEW LIGHT COVER AT 9D. 2 L 7 2 4F RT A28NM 1998012900154 19980129 00154 NM 1998 1 29 AWXA9800025 1 19980119 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 187AW 22654 D-SEAT 4C EMERGENCY PATHWAY LIGHT INOP. REPAIRED BROKEN WIRES, OPS GOOD STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998012900155 19980129 00155 NM 1998 1 29 AWXA9800028 1 19980118 A 3350 900835A BATTERY PACK BOEING 737 7372U9 1384498 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 D-ROW 1-5 EMERG LIGHT INOP NR 3021349 USED ALL READY. REMOVED AND REPLACED EMERG LIGHT BATTERY AND REPAIRED BROKEN WIRE AT BATTERY PACK, OPS CK GOOD. STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998012900157 19980129 00157 NM 1998 1 29 AWXA9800030 1 19980106 A 5330 SKIN BOEING 737 73733A 1384673 NM GALLEY DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 169AW 23630 DURING SCHEDULED C-13 INSPECTION, FOUND CRACK ON EXTERNAL SKIN AT FWD GALLEY DOOR THRESHOLD AFT LOWER CORNER. SKIN CRAC K IN EXTERNAL SKIN AT LOWER AFT CORNER OF FWD GALLEY DOOR CUTOUT. STOP DRILLED, FABRICATED DOUBLER AND TRIPLER PARTS AN D INSTALLED DOUBLER AND TRIPLER IAW, SRM 53-10-01 AT BS 344 RT, WL 208. 2 L 7 2 4F RT A16WE 1998012900158 19980129 00158 WP 1998 1 29 CALA9800088 1 19980121 A 3260 CONNECTOR DOUG DC9 DC983 3022083 WP NLG SENSOR LOOSE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 938MC 49525 WHEN GEAR WAS EXTENDED ON FINAL APPROACH TO IAH, THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AND THE GEAR WARNIN G HORN SOUNDED ABOUT FIVE SECONDS LATER. THE GEAR WAS CYCLED AND THE GREEN NOSE GEAR LIGHT ILLUMINATED AND THE WARNING HORN STOPPED 15 SECONDS LATER. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG DOWNLOCK SENSOR CANNON PLUG LOOSE. THE CANNON PLUG WAS SECURED. A SIMULATED GEAR SWING WAS PERFORMED AND ALL INDICATIONS CHECKED NORMAL. 2 L 7 2 4F RT A6WE 1998012900159 19980129 00159 WP 1998 1 29 CALA9800089 1 19980119 A 2910 7912641554 HYD LINE DOUG DC9 DC931 3022065 WP NR 1 ENG TR RUPTURED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 18563 47487 AIRCRAFT LOST THE LEFT SYSTEM HYDRAULIC QUANTITY DURING CLIMB-OUT OF IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LAN DED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE THRUST REVERSER CONTROL VALVE HYDRAULIC LINE RUPTURED. THE HYD RAULIC LINE WAS REPAIRED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998012900160 19980129 00160 NM 1998 1 29 CALA9800090 1 19980119 A 5753 SKIN BOEING 727 727243 138408D NM RT TE MIDFLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND RT WING INBOARD MID-FLAP UPPER SKIN PILLOWED WITH DISHED FASTENERS IN AREA ABOVE REAR SPAR UPPER CHORD APPROXIMATELY 21 INCHES FROM INBOARD END AND EXTENDING OUTBOARD 6.5 INCHES. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-04, FIGURE 8 AND 51-30-2. 2 L 7 3 4F RT A3WE 1998012900161 19980129 00161 NM 1998 1 29 CALA9800091 1 19980119 A 5510 LUGS BOEING 727 727243 138408D NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND HORIZONTAL STABILIZER LEFT AND RIGHT BEARING SUPPORT VERTICAL LUGS CORRODED. THE LT VERTICAL LUGS WER E REWORKED IAW ECRA 5550-01033. THE RT VERTICAL LUGS WERE REWORKED IAW ECRA 5550-01141. 2 L 7 3 4F RT A3WE 1998012900162 19980129 00162 NM 1998 1 29 CALA9800092 1 19980120 A 5320 FRAME BOEING 727 727243 138408D NM R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 3.5 CRACK IN UPPER AFT CORNER OF R-1 DOOR FRAME. A REPAIR WAS FABRICATED AND INSTALLED IAW DRAWING 6 9-69978, SRM 57-10-02, AND ECRA 5240-01223. 2 L 7 3 4F RT A3WE 1998012900163 19980129 00163 WP 1998 1 29 CALA9800093 1 19980119 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 47638 INSPECTION FOUND FLOOR SUPPORT FORWARD OF LEFT OUTBOARD SEAT TRACK CORRODED AT STA 160-200. A NEW FLOOR SUPPORT WAS INS TALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998012900164 19980129 00164 NM 1998 1 29 CALA9800094 1 19980120 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 1006 TO 1016, LBL 6 TO 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1998012900165 19980129 00165 NM 1998 1 29 CALA9800095 1 19980121 A 5320 SUPPORT BOEING 737 7373T0 1384582 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOOR SUPPORT CORRODED FROM STA 947-967, RBL 18. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51 -10-2. 2 L 7 2 4F RT A16WE 1998012900166 19980129 00166 NM 1998 1 29 CALA9800096 1 19980122 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 0 TO RBL 29. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-5 1. 2 L 7 2 4F RT A16WE 1998012900167 19980129 00167 NM 1998 1 29 CALA9800097 1 19980122 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOORBEAM CORRODED AT STA 967, LBL 15. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998012900168 19980129 00168 WP 1998 1 29 CALA9800098 1 19980121 A 5350 3913359545 CABLE DOUG DC9 DC982 3022082 WP TAIL CONE DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 936AS 49363 INSPECTION FOUND TAILCONE RELEASE CABLE KINKED AT TOP LEFT PULLEY. THE CABLE WAS REMOVED AND REPLACED AND RIGGED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998012900169 19980129 00169 NM 1998 1 29 CALA9800099 1 19980122 A 5310 STRUCTURE BOEING 727 727224 1384076 NM BS 440-480 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 THE AIRCRAFT SUSTAINED GROUND DAMAGE TO THE FUSELAGE SKIN, STRINGER, AND FRAMES AT STA 440-480, STRINGERS 14-19L. THE FU SELAGE SKIN AND STRINGER WERE REPAIRED IAW ECRA 5330-02621. THE FRAMES WERE REPAIRED IAW ECRA 5310-03656, SRM 51-40-3, AND 53-10-3. 2 L 7 3 4F A3WE 1998012900170 19980129 00170 NM 1998 1 29 9801206305 1 19980121 A 3260 SWITCH BOEING 747 747451 1384940 NM LT MLG MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 665US 23820 DURING TAKEOFF, RECEIVED A GEAR CONFIGURATION TAKEOFF WARNING MESSAGE. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GAT E. RESEATED THE RIGHT ACTUATOR SWITCH ON THE LEFT BODY LANDING GEAR. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998012900171 19980129 00171 NE 1998 1 29 9801219938 2 19980108 A 7314 378200 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LT ENGINE DAMAGED A NWAA C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 GL 01 1798U 31210 8218 47369 656091 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE FLAMED OUT. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE R EPLACED THE LEFT ENGINE FUEL CONTROL UNIT. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1998012900172 19980129 00172 WP 1998 1 29 9801221234 1 19980118 A 3610 1555M77601 DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 1 ENGINE DAMAGED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 234NW 46912 455479 ON INITIAL CLIMB-OUT (BOM), THE NR 1 ENGINE FIRE WARNING LOOP A LIGHT ILLUMINATED. THREE MINUTES LATER THE NR 1 ENGINE FIRE WARNING LOOP B LIGHT ALSO ILLUMINATED. POWER WAS REDUCED TO 60 PERCENT ON THE NR 1 ENGINE AND BOTH INDICATIONS EXT INGUISHED. ALL OTHER ENGINE PARAMETERS WERE NORMAL. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO BOM. MAINTENANCE INS PECTED THE ENGINE AND FOUND TWO COMPRESSOR BLEED DUCTS HAD BECOME SEPARATED AT A THREADED CONNECTION. ONE DUCT WAS REPL ACED AND THE FOLLOW-UP ENGINE RUN AT FULL POWER WAS NORMAL. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE A23EA 1998012900173 19980129 00173 EU 1998 1 29 9801233248 1 19980119 A 3350 BULBS AIRBUS 320 A320212 EU CABIN FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 348NW 410 DURING EMERGENCY LIGHT TEST, FOUND BOTH RIGHT OVERWING EXIT HANDLE ILLUMINATION LIGHTS INOPERATIVE. MAINTENANCE REPLACE D THE LIGHT BULBS. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998012900174 19980129 00174 WP 1998 1 29 9801259762 1 19980120 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NW 47395 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900175 19980129 00175 NE 1998 1 29 9801262713 2 19980120 A 7321 17636011 FUEL CONTROL BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17R 52049 NE RT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 716RC 32841 9242 22021 689862 AS TAKEOFF POWER WAS APPLIED, THE RIGHT ENGINE WAS SLOW RESPONDING TO THROTTLE SETTING. CREW ABORTED TAKEOFF AND RETURN ED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL CONTROL ASSEMBLY. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998012900176 19980129 00176 WP 1998 1 29 9701271234 1 19980119 A 3610 1555M23G02 DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 1 ENGINE CRACKED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 234NW 46912 455479 DURING TAKEOFF ROLL, THE NR 1 ENGINE FIRE WARNING ILLUMINATED. THE TAKEOFF WAS ABORTED AT 120 KNOTS AND THE AIRCRAFT RE TURNED TO THE GATE. MAINTENANCE FOUND A 14TH STAGE BLEED AIR DUCT CRACKED. THE DUCT WAS REPLACED AND ENGINE RUN AT HIG H POWER WAS NORMAL. 2 L 7 3 4F 4 F A22WE A23EA 1998012900177 19980129 00177 WP 1998 1 29 9801289988 1 19980121 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8944E 47167 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 14 THROUGH 17 INOPERATIVE. REPLACED BLOWN FUSE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900178 19980129 00178 WP 1998 1 29 9801299930 1 19980121 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1998012900179 19980129 00179 WP 1998 1 29 9801309916 1 19980120 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 949N 47566 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS FOR CATWALK AND DOOR RELEASE HANDLE INOPERATIVE. MAINTENANCE ACCOMPLISHED INTERIM REPAIR TO WIRING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998012900180 19980129 00180 WP 1998 1 29 9801319914 1 19980121 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 964N 47416 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT DOOR SIGN LIGHT INOPERATIVE. REPLACED FUSE. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900181 19980129 00181 EU 1998 1 29 9801243237 1 19980119 A 3350 321430 BATTERY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 337NW 358 DURING EMERGENCY LIGHT TEST, RECEIVED MESSAGE COM R. MAINTENANCE REPLACED POWER SUPPLY MODULE. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998012900182 19980129 00182 WP 1998 1 29 9801329857 1 19980121 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 766NC 47739 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONA L CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012900183 19980129 00183 WP 1998 1 29 9801339885 1 19980121 A 3230 UPLATCH DOUG DC9 DC951 3022051 WP LT MLG NOT SECURED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 401EA 47682 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GAR RETRACTION. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INC IDENT. MAINTENANCE FOUND LEVER ON LEFT MAIN GEAR UPLATCH NOT SECURE. SECURED LEVER. OPERATIONAL CHECK NORMAL. AIRCR AFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1998012900184 19980129 00184 1998 1 29 9801349304 4 19980122 A 2565 100503119 SLIDE DOUG DC9 DC982 3022082 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 931MC 17272 3853 48057 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998012900185 19980129 00185 WP 1998 1 29 9801359878 1 19980122 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT AND SEAT MOUNTED LIGHTS BETWEEN ROWS 5 T HROUGH 12 INOPERATIVE. REPLACED FUSE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998012900186 19980129 00186 1998 1 29 9801369974 4 19980122 A 2565 13317 SLIDE DOUG DC9 DC931 3022065 WP PAX DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 37864 3033 47347 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EVACUATION SLIDE BOTTLE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998012900187 19980129 00187 SO 1998 1 29 COM9810026 1 19980120 A 2612 6468 CONTROL CONTROL EMB 120 EMB120RT SO COCKPIT FAILED A COMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 463CA 13401 120267 APU FIRE WARNING DURING GROUND OPERATIONS, FALSE WARNING. REPLACED FIRE DETECTION CONTROL MODULE. 2 L 7 2 4T RT A31SO 1998012900188 19980129 00188 SO 1998 1 29 COMA9810027 1 19980119 A 2910 12039829009 HYD LINE EMB 120 EMB120RT SO LT NACELLE CHAFED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 268CA 120262 GREEN HYDRAULIC SYSTEM LOW LEVEL WARNING. REPAIRED LEAKING HYDRAULIC LINE LEFT ENGINE NACELLE. 2 L 7 2 4T RT A31SO 1998012900196 19980129 00196 NM 1998 1 29 SWAA980045 1 19980120 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1004/1009 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D CHECK, FOUND STRINGER 27L CORRODED AT BS 1004, AND AT S27R AT BS 1009. REPLACED DAMAGED SECTIONS PE R BOEING SRM. 2 L 7 2 4F A16WE 1998012900197 19980129 00197 NM 1998 1 29 SWAA980046 1 19980120 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 867-878 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D CHECK, FOUND STRINGER 24R DAMAGED AT BS 867-878. REPLACED DAMAGED SECTIONS PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900198 19980129 00198 NM 1998 1 29 SWAA980047 1 19980120 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 941 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D CHECK, FOUND STRINGER 24R WITH A HOLE AT BS 941. REPLACED DAMAGED SECTIONS PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900199 19980129 00199 NM 1998 1 29 SWAA980048 1 19980120 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D CHECK, FOUND CORROSION ON SHEAR TIE AT BS 947, BETWEEN S24 AND 25. REPLACE SHEAR TIE PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900200 19980129 00200 NM 1998 1 29 SWAA980049 1 19980120 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 787 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME DENTED AT BS 787. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900201 19980129 00201 NM 1998 1 29 SWAA980050 1 19980120 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 947, S24L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900202 19980129 00202 NM 1998 1 29 SWAA980051 1 19980120 A 5511 RIB BOEING 737 7372H4 138448C NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D CHECK, LT HORZ STAB L/E PANEL CRACKED RIB AT STA 105.26. REPLACED DAMAGED SECTION AND INSTALLED REPA IR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900203 19980129 00203 NM 1998 1 29 SWAA980052 1 19980120 A 3260 655825029 CARD BOEING 737 7373H4 1384600 NM E/E BAY FAILED A SWAA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 335SW 23939 AFTER TAKEOFF, AND NORMAL GEAR RETRACTION, GEAR HANDLE CENTERED. GEAR EXTENDED WITH BOTH RED AND GREEN LIGHTS. RAISED HANDLE, GEAR RETRACTED, BUT RED UNSAFE LIGHTS REMAINED ON. GEAR WAS AGAIN EXTENDED AND RETRACTED BUT TOOK EXCESSIVE AM OUNT OF TIME TO RETRACT. REPLACED PC CARD 986 AND PERFORMED RETRACT TEST PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998012900204 19980129 00204 1998 1 29 SWAA980053 2 19980116 A 7510 567620 DUCT BOEING 737 7372H4 138448C NM NR 1 RUPTURED A SWAA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 73SW 22673 NR 1 ENGINE FIRE WARNING INDICATION IN FLIGHT. ACTIVATED FIRE BOTTLES AND PERFORMED ENGINE SHUTDOWN CHECKLIST. MADE AN UNEVENTFUL LANDING AT STL. INSPECTED AND FOUND ANTI-ICE VALVE LINE RUPTURED. REPLACE LINE, ENGINE OIL STRAINER, HYD P UMP CASE DRAIN FILTER AND FIRE BOTTLES PER BOEING M/M. 2 L 7 2 4F A16WE 1998012900205 19980129 00205 NM 1998 1 29 SWAA980054 1 19980116 A 5330 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED B/C4 CHECK, FOUND FUSELAGE SKIN DENTED AT BS 478, AT S26R, AT BS 1020, AT S13L, AT BS 1006, AT S14L, AN D AT BS 993, A14L. REPAIRED ALL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998012900206 19980129 00206 NM 1998 1 29 SWAA980055 1 19980118 A 3350 2013A BATTERY BOEING 737 7373A4 1384585 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 678AA 23290 DURING WALKAROUND, FOUND EMERGENCY EXIT LIGHTING PARTIALLY INOP IN FORWARD CABIN AREA. REMOVED AND REPLACED BATTERY PAC K PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998012900207 19980129 00207 NM 1998 1 29 SWAA980056 1 19980115 A 3233 69355006 ACTUATOR BOEING 737 7373A4 1384585 NM LT MLG FAILED A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 673AA 23251 ON CLIMB-OUT AFTER GEAR RETRACTION, LEFT MAIN GEAR EXTENDED WITH HANDLE IN UP POSITION. REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998012900208 19980129 00208 NM 1998 1 29 SWAA980057 1 19980115 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 28SW 21339 DURING WALKAROUND CHECK, FOUND FWD GALLEY OVERHEAD EMERGENCY EXIT LIGHT REMAINING ILLUMINATED WITH SWITCH IN OFF. REPLA CED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1998012900209 19980129 00209 NM 1998 1 29 SWAA980058 1 19980116 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 964 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED B/C4 CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 964, NEAR S24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998012900210 19980129 00210 NM 1998 1 29 SWAA980059 1 19980114 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 85SW 22826 DURING SCHEDULED A2 CHECK, FOUND MID CABIN OVERHEAD EMEGENCY EXIT LIGHT FLASHING DURING OP CHECK. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1998012900211 19980129 00211 NM 1998 1 29 UPS98225516 1 19980118 A 5320 BAC15O5100299 ANGLE BOEING 727 72722C 138400F NM BS 259 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE:SI CORROSION (SDN C53-111-01.00-01) ON VERTICAL L ANGLE AT BS 259, LBL 26, WL 155 TO WL 165. CORROSION REMOVAL OUT OF LIMITS, REMOVED DAMAGED L ANGLE, FABRICATED REPAIR PARTS, INSTALLED PER SRM 51-40-4. 2 L 7 3 4F A3WE 1998012900213 19980129 00213 NM 1998 1 29 UPS98225518 1 19980104 A 5753 6614734 BEAM BLOCK BOEING 727 7272A1 138407F NM NR 3 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:SI NR 3 FLAP TRACK REAR SPAR ATTACH POINT HAS CORROSION, ALSO BOTH FAIL/SAFE ATTACH HOLES. FLAP TRACK B EAM BLOCK REMOVED, FOUND OUT OF LIMITS AND REPLACED WITH NEW ITEM PER SRM 57-30-5, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998012900214 19980129 00214 NM 1998 1 29 98FDEA00046 1 19980122 A 3260 CONNECTOR BOEING 727 727233 138408A NM NLG CORRODED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 269FE 21675 98-0030 - AFTER TAKEOFF GEAR UP: RED NOSE GEAR LIGHT REILLUMINATED AFTER HANDLE PLACED TO OFF. RED TABS, NO HELP. RED LIGHT COMES ON AFTER DELAY, NOT IMMEDIATELY WHEN PLACING HANDLE TO OFF. REMOVED AND REPLACED NOSE GEAR LOCK SWITCH S96 AND NOSE LANDING GEAR POSITION SWITCH S93. WOULD NOT PASS ADJUSTMENT AND TEST PROCEDURES. FOUND PINS A AND C SHORTED IN CANNON PLUG D300. REMOVED CANNON PLUG AND PINS D300. PASSED ADJUSTMENT AND TEST PER MAINTENANCE MANUAL 32-61-71 OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998012900215 19980129 00215 NM 1998 1 29 98FDEA00047 1 19980123 A 3020 39270811 THERMO VALVE BOEING 727 7272S2F 1384O81 NM NR 2 ENGINE MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 212FE 22934 ON CLIMBOUT, GOT ANTI-ICE DUCT OVERHEAT LIGHT NR 1 AND NR 3 ENGINES WERE BOTH OFF THE TEMPERATURE SCALE. FOLLOWED RED T ABS, LIGHT WENT OUT AFTER 1 TO 2 MINUTES ON LANDING. LIGHT CAME ON AGAIN WITH WINGS OFF AND ENGINE ANTI-ICE OPEN. REMO VED AND REPLACED NR 2 ENGINE COWL ANTI-ICE THERMOSTATIC VALVE PER MAINTENANCE MANUAL 30-21-21. NR 2 ENGINE COWL ANTI-IC E THERMAL SWITCH, AND WING ANTI-ICE THERMAL SWITCH. OPERATIONAL CHECK GOOD ON GROUND. 2 L 7 3 4F A3WE 1998012900216 19980129 00216 NM 1998 1 29 98FDEA00045 1 19980121 A 3260 656021123 CONTROL MODULE BOEING 727 727233 138408A NM E/E COMP MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 269FE 21675 98-0029 NOSEGEAR UNSAFE, LANDING GEAR HANDLE UP DOOR LIGHTS OUT. REPLACED LANDING GEAR ACCESSORY CONTROL MODULE PER MA INTENANCE MANUAL 32-09-121 PAGE 401 TEST PER 32-09-122 PARAGRAPH 6A, PAGE 505. 2 L 7 3 4F RT A3WE 1998012900217 19980129 00217 WP 1998 1 29 ABXA00035 1 19980126 A 5610 KR3E6 ROD DOUG DOUG DC8 DC861 3021952 WP COCKPIT BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 845AX 46157 CAPTAIN'S WINDOW (EMERG EXIT) LATCH PIN WAS FOUND BROKEN DURING PREFLIGHT. REPLACED LOWER FORWARD LINKAGE ROD IAW DC8 M M 56-10-3, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998012900218 19980129 00218 NM 1998 1 29 DLM88980165 1 19980120 A 2913 HYD PUMP DOUG MD88 MD88 3023688 NM NR 1 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 968DL 53161 AFTER TAKEOFF, RT HYD PRESS WENT TO ZERO WITH - RIGHT HYD LOW, MSG ON OAP. FOLLOWED POM PROCEDURES AUX/TRANS PUMPS TURN ED ON. PRESS RETURNED TO NORMAL DECLARED EMERGENCY. REPLACED RT ENG HYD PUMP AND FILTERS. 2 L 7 2 4F RT A6WE 1998012900219 19980129 00219 WP 1998 1 29 DLL10980167 1 19980120 A 3230 1516207122 SEQUENCE VALVE LKHEED 1011 10113851 5265010 WP LT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 719DA 193C1135 AFTER T/O, THE DOOR RED AND INTRANSIT LIGHTS DID NOT GO OUT. LANDING GEAR LOWERED PER PROCEDURES, RIGHT GEAR GREEN LIGH T DID NOT COME ON. MANUALLY EXTENDED GEAR, LIGHT CAME ON. LEFT MLG SEQUENCE VLV REPLACED, RT MLG RETRACT ACTUATOR REP LACED, RIGGING THE RT MLG SEQUENCE VALVE. 2 L 7 3 4F A23WE 1998012900222 19980129 00222 NM 1998 1 29 DL72S980175 1 19980121 A 5542 SKIN BOEING 727 727232 1384082 NM RUDDER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 FOUND ON C2 LETTER CK, TWO .75 INCH CRACKS OUT OF TWO ADJACENT RIVETS LT SIDE OF LOWER RUDDER. REPAIRED PER SRM 55-20-3 REF SRM 55-40-2 FIG 1 FOR INFO. 2 L 7 3 4F A3WE 1998012900223 19980129 00223 NM 1998 1 29 DL72L980176 1 19980121 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 501DA 21303 RT SIDE OVERWING EMERGENCY LIGHTS BLINKING. REPLACED BATTERY PACK, OPERATION GOOD. 2 L 7 3 4F A3WE 1998012900224 19980129 00224 NM 1998 1 29 DL757980177 1 19980122 A 5240 SKIN 146N61302 BOEING 757 757232 1384965 NM R4 DOOR GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 657DL 238 24419 R4 DOOR SKIN WAS FOUND GOUGED AT THE LWR HINGE CUTOUT. REPAIRED PER ERA 331237-14. 2 L 7 2 4F RT A2NM 1998012900225 19980129 00225 NM 1998 1 29 DLM88980178 1 19980122 A 5330 5953050 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 983DL 53247 FUSELAGE SKIN WAS FOUND DENTED AT STA 237 BETWEEN L18L AND L19L. CUTOUT DIMENSIONS WERE 9 BY 13.5. REPAIRED PER ERA 33 1252-14. 2 L 7 2 4F RT A6WE 1998012900226 19980129 00226 NM 1998 1 29 DLM88980179 1 19980122 A 5330 5911406 SKIN DOUG MD88 MD88 3023688 NM BS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 983DL 53247 FUSELAGE SKIN FOUND DENTED AT STA 218 BETWEEN L17L AND L18L. REPAIRED PER ERA 331258-14. 2 L 7 2 4F RT A6WE 1998012900227 19980129 00227 NM 1998 1 29 DLM88980180 1 19980122 A 5510 3918017503 BRACKET DOUG MD88 MD88 3023688 NM LT HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 983DL 53247 XE103.816 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORIZ STAB WAS FOUND TO HAVE CORROSION. CORROSION IS IN THE BORE OF THE INBD AND OUTBD LUGS. CORROSION REMOVED BY OVERSIZING THE BORE FROM 0.6245/0.6255 TO A FINAL DIAMETER OF 0. 6365. REWORKED PER ERA 331242-14. 2 L 7 2 4F RT A6WE 1998012900228 19980129 00228 NM 1998 1 29 DLM88980181 1 19980122 A 5510 4918019501 BRACKET DOUG MD88 MD88 3023688 NM LT/RT HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 983DL 53247 XE225.834 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT AND RT HORIZONTAL STAB WAS FOUND TO CONTAIN CORROSION. THE CORROSION IS IN THE BORE OF THE INBD LUG. CORROSION WAS REMOVED BY OVERSIZING THE BORE FROM 0.562/0.563 TO A FINAL DIAM ETER OF 0.586. REWORKED PER ERA 331239-14. 2 L 7 2 4F RT A6WE 1998012900229 19980129 00229 NM 1998 1 29 DLM88980182 1 19980122 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 983DL 53247 FS 1418 WAS CRACKED AT L2R. THIS IS ONE OF THE TYPICAL LOCATIONS COVERED BY SB53-184. THE CRACK IS 1.125. THE SUBJECT AIRCRAFT IS NOT LISTED IN THE EFFECTIVITY OF THE SB. REPAIRED PER ERA 331243-14. 2 L 7 2 4F RT A6WE 1998012900230 19980129 00230 NM 1998 1 29 DLM88980183 1 19980122 A 5510 5918113501 BRACKET DOUG MD88 MD88 3023688 NM LT HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 983DL 53247 XE14.525 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORIZ STAB WAS FOUND CORRODED. THE CORROSION IS IN THE BORE OF THE INBD LUG. THE CORROSION WAS REMOVED BY OVERSIZING THE 0.4999/0.5009 BORE TO A FINAL DIAMETER OF 0.5080. REWORKE D PER ERA 331236-14. 2 L 7 2 4F RT A6WE 1998012900231 19980129 00231 NM 1998 1 29 DL73K980184 1 19980122 A 5330 SKIN BOEING 737 737232 1384475 NM BS 379 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 SKIN AT THE COOLING DUCT CUTOUT AT BS 379, APPROXIMATELY BL0 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. CRACK IS APPROXIMATELY 1.5 IN LENGTH AND IS TYPICAL OF CRACKS DESCRIBED BY SB 737-53-1117. REPAIRED PER ERA 331270-14 (SB 737-53 -1117). 2 L 7 2 4F RT A16WE 1998012900232 19980129 00232 NM 1998 1 29 DL72E980187 1 19980121 A 3350 BATTERY PACK S106 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 551 21481 RIGHT FORWARD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998012900233 19980129 00233 NM 1998 1 29 DL72E980188 1 19980121 A 3350 BATTERY PACK S106 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 11605 21481 LEFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998012900241 19980129 00241 NM 1998 1 29 DHL9871707C 1 19980108 A 5753 SKIN BOEING 727 72723 1384004 NM RT TE MIDFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, O/B MID FLAP T/E END DELAMINATED. INSTALLED REPAIR PER SRM 51-40-8. REPAIR 17 BY 4 N/R 2169. 2 L 7 3 4F A3WE 1998012900242 19980129 00242 NM 1998 1 29 DHL9871708C 1 19980104 A 5713 STRINGER BOEING 727 72723 1384004 NM BS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, RT WING UPPER AFT STR CRACKED AT WS 656.5. HFEC, INSTALLED REPAIRED ANGLES PER S/B 57A159, ANGLES 10.6 AND 4.3, N/R 2166. 2 L 7 3 4F A3WE 1998012900243 19980129 00243 NM 1998 1 29 DHL9871709C 1 19980104 A 5712 RIB BOEING 727 72723 1384004 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, RT WING RIB STA 601.5 CRACKED AT LOWER FLANGE AT STR 6. STOP DRILLED END OF CRACK, ACCOMPLISHED NDT, AND IN STALLED DOUBLER REPAIR PER SRM 57-10-5, 9.75 BY 3.75, N/R 2167. 2 L 7 3 4F A3WE 1998012900245 19980129 00245 NM 1998 1 29 DHL9871711C 1 19980102 A 5320 ANGLE BOEING 727 72723 1384004 NM BS 618 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, L ANGLE AT FLOOR LEVEL RBL 64 CRACKED AND MISSING PIECE FROM STA 618. REPLACED ANGLE FROM 605 TO 620 PER SR M 51-10-1, N/R 3189. 2 L 7 3 4F A3WE 1998012900246 19980129 00246 NM 1998 1 29 DHL9871712C 1 19980102 A 5320 ANGLE BOEING 727 72723 1384004 NM BS 605 BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, L ANGLE AT STA 605, AT RBL 64 BENT AT FWD END OF AIR DUCT. REPLACED ANGLE FROM 605 TO 620 PER SRM 51-10-1, N/R 3188. 2 L 7 3 4F A3WE 1998012900247 19980129 00247 NM 1998 1 29 DHL9871713C 1 19980102 A 5344 655343313 FITTING BOEING 727 72723 1384004 NM CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, LOWER AFT CARGO COMPT DOOR CUTOUT , 2ND STOP FITTING FROM AFT BOTTOM CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-10-1, N/R 3198. 2 L 7 3 4F A3WE 1998012900248 19980129 00248 NM 1998 1 29 DHL9871714C 1 19980102 A 5347 SEAT TRACK BOEING 727 72723 1384004 NM BS 620 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, SEAT TRACK NR 2 AND FLOORBEAM DAMAGED AT BS 620 LEFT SIDE. CUT OUT DAMAGED SECTION FROM BS 620 TO 640, CUTO UT DAMAGED UPPER CHORD BEAM 11 STA 620 LBL 39. INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8, 28. INSTALLED NEW SECTION O F SEAT TRACK PER SRM 53-10-5 FROM 620 TO 640, N/R 5140. 2 L 7 3 4F A3WE 1998012900249 19980129 00249 NM 1998 1 29 DHL9871715C 1 19980102 A 5312 RIB BOEING 727 72723 1384004 NM BS 500 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, STA 500 CIR RIB CRACKED BELOW STR 16R WEB AT INBD FACE. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR P ER SRM 51-10-2 16 BY 5.25, N/R 5144. 2 L 7 3 4F A3WE 1998012900250 19980129 00250 NM 1998 1 29 DHL9871716C 1 19980102 A 5312 RIB BOEING 727 72723 1384004 NM BS 520 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C-CHECK, STA 520 CIR RIB I/B FLANGE CRACKED BELOW S-16 R WEB TIE CLIP. CUT OUT DAMAGED AREA , INSTALLED DOUBLER REP AIR PER SRM 51-40-3 16 BY 5.25, FILLER 16 BY 4.25, N/R 5146. 2 L 7 3 4F A3WE 1998012900251 19980129 00251 NM 1998 1 29 DHL9871717C 1 19980102 A 5320 FLANGE BOEING 727 72723 1384004 NM BS 540 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, STA 540 I/B FLANGE DENTED BELOW S-16 R. REMOVED AND REPLACED DOUBLER REPAIR PER SRM 51-40-3, 12.75 BY 4.5, FILLER 12.75 BY 4, N/R 5147. 2 L 7 3 4F A3WE 1998012900252 19980129 00252 NM 1998 1 29 DHL9871718C 1 19980102 A 5320 FLANGE BOEING 727 72723 1384004 NM BS 580 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, STA 580 I/B FLANGE DENTED BELOW S-16R WEB. REMOVED PREVIOUS REPAIR, INSTALLED DOUBLER PER SRM 51-40-3, 15 BY 4.5, N/R 5151. 2 L 7 3 4F A3WE 1998012900253 19980129 00253 NM 1998 1 29 DHL9871719C 1 19980102 A 5320 ANGLE BOEING 727 72723 1384004 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, ANGLE CRACKED BENEATH SEAL RETAINER ABOVE AFT OF RT MLG DOOR AFT I/B HINGE. REMOVED AND REPLACED ANGLE SUP PORT PER SRM 51-10-1, 12 BY 4, N/R 7010. 2 L 7 3 4F A3WE 1998012900254 19980129 00254 NM 1998 1 29 DHL9871720C 1 19980102 A 7110 COWLING BOEING 727 72723 1384004 NM NR 1 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE TOP COWLING OVERHEAD AFT CATCH INNER DOUBLER CHAFFED THROUGH. REPLACED INNER DOUBLER PER SRM 54 -10-3, 8 BY 6, N/R 6124. 2 L 7 3 4F A3WE 1998012900269 19980129 00269 NM 1998 1 29 DHL9871735C 1 19980105 A 5712 RIB BOEING 727 72723 1384004 NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, UPPER FLANGE OF WING RIB CRACKED AT STR 13 ATTACH FASTENER, WS 686.5. INSTALLED RIB REPAIR PER SRM 57-10-5, 9.75 BY 3.75, N/R 1239. 2 L 7 3 4F A3WE 1998012900270 19980129 00270 NM 1998 1 29 DHL9871736C 1 19980105 A 5712 RIB BOEING 727 72723 1384004 NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, LEFT WING INTERIOR, LOWER FLANGE OF WING RIB CRACKED AT STR 8 WS 686.5. INSTALLED RIB REPAIR PER SRM 57-10 -5, 9.75 BY 3.75, N/R 1238. 2 L 7 3 4F A3WE 1998012900271 19980129 00271 NM 1998 1 29 DHL9871737C 1 19980105 A 5712 RIB BOEING 727 72723 1384004 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, LOWER FLANGE OF WING RIB CRACKED AT STR 6 ATTACH FASTENER WS 629. INSTALLED DOUBLER REPAIR AT LOWER RIB FL ANGE PER SRM 57-10-5, 9.75 BY 3.75, N/R 1237. 2 L 7 3 4F A3WE 1998012900272 19980129 00272 NM 1998 1 29 DHL9871738C 1 19980105 A 5321 FLOOR PANEL BOEING 727 72723 1384004 NM BS 720 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, RT SIDE STA 720 NR 6 FLOOR PANEL IS DELAMINATED. REPLACED PANEL PER SRM 51-30-2, 27 BY 16.5, N/R 5131. 2 L 7 3 4F A3WE 1998012900281 19980129 00281 NM 1998 1 29 DHL9871747C 1 19980105 A 5712 RIB BOEING 727 72723 1384004 NM WS 546 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, LEFT WING INTERIOR, LOWER FLANGE OF WING RIB CRACKED AT STRINGER 8 ATTACH FASTENER, WS 546.5. INSTALLED RI B REPAIR PER SRM 57-10-5, 9 BY 3.75, N/R 1236. 2 L 7 3 4F A3WE 1998012900290 19980129 00290 NM 1998 1 29 DHL9871756C 1 19980103 A 5350 TAIL CONE BOEING 727 72723 1384004 NM AFT FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, TAILCONE DELAMINATED. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, N/R 4023. 2 L 7 3 4F A3WE 1998012900300 19980129 00300 NM 1998 1 29 DHL9871766C 1 19980102 A 5320 BAC1515531 ANGLE BOEING 727 72723 1384004 NM BS 504 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, L ANGLE AT FLOOR LEVEL AT RBL 64 CRACKED AT STA 504. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 LONG, N /R 5143. 2 L 7 3 4F A3WE 1998012900301 19980129 00301 NM 1998 1 29 DHL9871767C 1 19980102 A 5320 ANGLE BOEING 727 72723 1384004 NM BS 524 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, L ANGLE CRACKED AT FLOOR LEVEL AT RBL 664, STA 524 CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 LONG, N/R 5143. 2 L 7 3 4F A3WE 1998012900302 19980129 00302 NM 1998 1 29 DHL9871768C 1 19980102 A 5320 BAC1515531 ANGLE BOEING 727 72723 1384004 NM BS 544 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, L ANGLE AT FLOOR LEVEL RBL 64, STA 544 CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 INCHES LONG, N/R 5148. 2 L 7 3 4F A3WE 1998012900303 19980129 00303 NM 1998 1 29 DHL9871769C 1 19980102 A 5320 BAC1515531 ANGLE BOEING 727 72723 1384004 NM BS 558 BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, L ANGLE AT FLOOR LEVEL RBL 64 BENT STA 558. REMOVED AND REPLACED ANGLE PER SRM 51-40-4, 80 LONG, N/R 5150. 2 L 7 3 4F A3WE 1998012900304 19980129 00304 NM 1998 1 29 DHL9871770C 1 19980102 A 5320 BAC1515531 ANGLE BOEING 727 72723 1384004 NM BS 585 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, L ANGLE AT FLOOR LEVEL AT RBL 64 CRACKED AT STA 585. REMOVED AND REPLACED ANGLE PER SRM 51-40-4 FROM STA 4 90 TO 590, N/R 5152. 2 L 7 3 4F A3WE 1998012900309 19980129 00309 NM 1998 1 29 DHL9871775C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE FIXED COWL 3RD HINGE FROM FRONT FLANGE WORN. STOP DRILL CRACK, INSTALLED REPAIR PER SRM 51-40-3 , 4 BY 4, N/R 6095. 2 L 7 3 4F A3WE 1998012900310 19980129 00310 NM 1998 1 29 DHL9871776C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE NOSE COWL HAS SEVERAL CRACKS IN EXTERIOR SKIN. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SR M 54-30-3. DOUBLER, 12 BY 2.5, FILLER 3.75 BY 2.75, N/R 6109. 2 L 7 3 4F A3WE 1998012900311 19980129 00311 NM 1998 1 29 DHL9871777C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE BOTTOM COWLING EXTERIOR SKIN DENTED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER PER SRM 54-10 -3 9 BY 7, FILLER 5 BY 2, N/R 6112. 2 L 7 3 4F A3WE 1998012900312 19980129 00312 NM 1998 1 29 DHL9871778C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE BOTTOM 5TH RIB FROM FRONT 7 O'CLOCK POSITION CHAFFED THROUGH. REMOVED AND REPLACED DOUBLER PER SRM 54-10-3, 8 BY 3, N/R 6116. 2 L 7 3 4F A3WE 1998012900313 19980129 00313 NM 1998 1 29 DHL9871779C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE BOTTOM COWLING NR 4 LATCH CUTOUT AREA DOUBLER CRACKED. REPLACED DOUBLER PER SRM 51-40-3, 8 BY 7 , N/R 6117. 2 L 7 3 4F A3WE 1998012900314 19980129 00314 NM 1998 1 29 DHL9871780C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE TOP COWLING OUTBD 3RD LATCH CUTOUT METAL TORN. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SR M 54-10-3 DOUBLER 3 BY 2.5', FILLER 1 BY 5, N/R 6121. 2 L 7 3 4F A3WE 1998012900315 19980129 00315 NM 1998 1 29 DHL9871782C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE TOP COWL INNER STRUCTURE NR 7 RIB FROM FRONT TO BACK CHAFFED THROUGH. INSTALLED DOUBLER PER SRM 54-10-3, 8 BY 1.25 BY .75, FILLER 1 BY .75, N/R 6126. 2 L 7 3 4F A3WE 1998012900316 19980129 00316 NM 1998 1 29 DHL9871783C 1 19980109 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE UPPER COWLING NR 1 I/B FRAME SECTION CRACKED. REPLACED FRAME SECTION PER SRM 51-40-3, 15 BY 6, N/R 6135. 2 L 7 3 4F A3WE 1998012900318 19980129 00318 NM 1998 1 29 DHL9877181C 1 19980102 A 7110 COWL BOEING 727 72723 1384004 NM NR 1 ENGINE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, NR 1 ENGINE TOP COWLING BLOWOUT PANEL INNER TOP DOUBLER CHAFFED THROUGH. REPLACED DOUBLER PER SRM 54-10-3, 1.5 BY 12, N/R 6125. 2 L 7 3 4F A3WE 1998012900320 19980129 00320 NM 1998 1 29 P5CA9800028 1 19980114 A 5730 FLYING PANEL BOEING 747 747124 1384874 NM RT WING LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 R/W FLYING PANEL O/B DOUBLER ATTACH POINT WORKING FASTENERS. REPAIRED IAW SRM 51-40-14. 2 L 7 4 4F A20WE 1998012900321 19980129 00321 NM 1998 1 29 P5CA9800029 1 19980116 A 5730 FLYING PANEL BOEING 747 747124 1384874 NM LT WING LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 L/W FLYING PANEL INCOMPLETE FASTENERS INSTALLATION. REMOVED AND REPLACED FASTENERS IAW ARM 51-30-02. 2 L 7 4 4F A20WE 1998012900322 19980129 00322 NE 1998 1 29 P5CA9800030 2 19980116 A 7250 R-RAIL BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 685904 NR 3 ENGINE R RAIL AT 60 DEGREE POSITION LIGHTENING HOLE OD RADIAL CRACK. WELDED IAW PWA 72-53-01 REPAIR NR 14. 2 L 7 4 4F 4 F A20WE E20EA 1998012900323 19980129 00323 NM 1998 1 29 P5CA9800031 1 19980116 A 5330 PANEL BOEING 747 747124 1384874 NM FUSELAGE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 HOLE FOUND IN PANEL 191B. REPAIRED PUNCTURE WITH FIBERGLASS OVERLAYS IAW 747 SRM 51-40-14. 2 L 7 4 4F A20WE 1998012900324 19980129 00324 NM 1998 1 29 P5CA9800032 1 19980116 A 5320 SUPPORT BOEING 747 747124 1384874 NM BS 1820 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 AFT CARGO BS 1820 LT SIDE WALL BROKEN SUPPORT. REPAIRED IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998012900325 19980129 00325 NM 1998 1 29 P5CA9800033 1 19980121 A 5320 RIVET BOEING 747 747132 1384882 NM BS 1300 FAILED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 KEEL BEAM AREA, BS 1300 RIVET HEAD POPPED OFF. REMOVED AND REPLACED FASTENER IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998012900326 19980129 00326 NE 1998 1 29 P5CA9800034 2 19980121 A 7230 FAN BLADE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACK A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 685970 NR 3 ENGINE, NR 5 FAN BLADE HAS A CRACK AT L/E. REMOVED CRACK BY BLENDING IAW MM 72-31-02. 2 L 7 4 4F 4 F A20WE E20EA 1998012900327 19980129 00327 NM 1998 1 29 P5CA9800035 1 19980121 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 1800 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 AFT PIT STA 1800 FLOORBEAM FLANGE CRACKED AT RT END APPROX RBL 50. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-10-01. FA BRICATED NEW FLOORBEAM IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998012900328 19980129 00328 NE 1998 1 29 TC8A98002 2 19980121 A 7230 COMPRESSOR DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 184SK 45981 642493 NR 2 ENGINE COMPRESSOR STALLED ON TAKEOFF, ABORTED TAKEOFF. INSPECTED ENGINE IAW 72-00, PERFORM GROUND RUN IAW TCA MIP VOL 2, OPS CHECK NORMAL, NO STALLS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1998012900329 19980129 00329 NM 1998 1 29 K3HA980007 1 19980122 A 3350 387 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 18. RELAMPED AND OPS CHECKS OK. 2 L 7 3 4F A3WE 1998012900330 19980129 00330 NM 1998 1 29 K3HA980008 1 19980123 A 3350 079123 LENS BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 354PA 20624 EMERGENCY PATH LIGHT RED LENS MISSING FORWARD OF SEAT ROW 31DEF. REPLACED MISSING RED LENS AT 31DEF. 2 L 7 3 4F A3WE 1998012900331 19980129 00331 NM 1998 1 29 W8PA980027 1 19980122 A 3350 BATTERY BOEING 737 73733R 1384407 NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 966WP 28871 DEN- FWD LEFT EMERGENCY FLASHLIGHT IS INOP. REPLACED BATTERY PER CHAPTER 25-60-00, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998012900332 19980129 00332 NM 1998 1 29 W8PA980028 1 19980121 A 3350 LIGHT BOEING 737 7373B7 1384580 NM CABIN LOOSE A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 953WP 23384 DEN- EMERGENCY LIGHT AT ROW 17 IS OUT OF THE TRACK. REINSTALLED LIGHT INTO TRACK, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998012900348 19980129 00348 NM 1998 1 29 QXEA9800038 1 19980120 A 5210 85210109009 HANDRAIL DHAV 85210152001 DHAV DHC8 DHC8102 2809003 NM PAX DOOR MALFUNCTION A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 816PH 54 PDX- MAIN CABIN IS DIFFICULT TO OPEN. REPLACED BOTH THE FORWARD AND AFT MAIN CABIN DOOR HANDRAILS, OPERATIONAL CHECKS G OOD. 2 H 7 2 4T RT A13NM 1998012900349 19980129 00349 NM 1998 1 29 QXEA9800039 1 19980122 A 3350 6038443 PWR SUPPLY DHAV 82410191011 DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTION A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 357PH 504 SEA- EMERGENCY EGRESS LIGHT AT THE RIGHT FORWARD SECTION OF THE CABIN, RIGHT FORWARD EMERGENCY EXIT SIGN, AND THE FORWAR D OVERHEAD CABIN LIGHTS ARE ALL INOP. REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY 3351 PS-2. OPERATIONAL CHE CKS GOOD. 2 H 7 2 4T RT A13NM 1998012900350 19980129 00350 EU 1998 1 29 QXEA9800040 1 19980121 A 3350 5515900004 CIRCUIT CARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 11156 SEA- THE LAMPS FOR THE LEFT AND RIGHT ARROWS ON THE FORWARD EMERGENCY EXIT SIGN DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY EXIT SIGN CIRCUIT CARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998012900351 19980129 00351 EU 1998 1 29 QXEA9800041 1 19980122 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 480AU 11229 BIL- MAIN CABIN DOOR IS DIFFICULT TO OPEN. CLEANED AND LUBRICATED DOOR MECHANISM, OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998012900352 19980129 00352 WP 1998 1 29 98FDEA00044 1 19980120 A 5312 BULKHEAD STRIP DOUG DC10 DC1010F 3022111 WP BS 1156 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 051FE 47805 RT SIDE OF Y 1156 PRESS BULKHEAD AT LONG 40 AREA HAS MANY BAD RIVETS AND THE ATTACHMENT STRIP IS PULLING AWAY FROM THE P ANEL, CAUSING A PRESSURIZATION LEAK. THIS WAS AN AREA OF A PREVIOUS REPAIR. *S/D* REMOVED RIVETS AS REQUIRED. DRILLE D HOLES TO FIRST OVERSIZE AND INSTALLED HI-LOKS PER SRM 51-00-01. REFER SNRM NR N00085. 2 L 7 3 4F A22WE 1998012900353 19980129 00353 NM 1998 1 29 DLM88980185 1 19980122 A 5522 SKIN 5930557505 DOUG MD88 MD88 3023688 NM LT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 983DL 53138 53247 LT ELEVATOR UPPER AND LOWER SKIN AND REAR CLOSING CHANNEL WERE DAMAGED WHILE PERFORMING MAINTENANCE. REPAIRED PER ERA 3 31260-14. 2 L 7 2 4F RT A6WE 1998012900354 19980129 00354 WP 1998 1 29 DLL14980193 1 19980122 A 3350 POWER PACK LKHEED 1011 1011385115 5265015 WP L1-DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1739D 59674 193C1237 EMERG EXTERIOR LIGHT AT L1 DOOR INOP. REPLACED POWER PACK, OPS OK. 2 L 7 3 4F A23WE 1998012900355 19980129 00355 NM 1998 1 29 DL72W980194 1 19980109 A 5753 652163233 SPAR BOEING 727 727247 138408F NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 AFT LOWER SPAR RAIL CRACKED TWO PLACES 33 AND 36 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998012900356 19980129 00356 NM 1998 1 29 DL72W980195 1 19980123 A 5753 652163234 ANGLE BOEING 727 727247 138408F NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 REPAIR DOULBER CRACKED ON LOWER CHORD ANGLE 33 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998012900357 19980129 00357 NM 1998 1 29 DL76L980197 1 19980123 A 3350 BATTERY PACK 20131A BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 180DN 5972 25985 RT AISLE EMERGENCY OVERHEAD SIGN INOP AT WING EXIT POSITION. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 1998012900358 19980129 00358 NM 1998 1 29 DL757980198 1 19980122 A 5754 114N4002 WEDGE BOEING 757 757232 1384965 NM NR 10 TE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 644DL 23998 THE NR 10 SLAT WAS FOUND WITH A 2 X 2 AREA OF DELAMINATION ON THE TRAILING EDGE WEDGE. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363806-14AD. 2 L 7 2 4F RT A2NM 1998012900359 19980129 00359 NM 1998 1 29 DL757980199 1 19980120 A 5414 SKIN BOEING 757 757232 1384965 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 640DL 23994 THREE CRACKS WERE FOUND IN THE INBD STRUT SKIN OF THE NR 2 ENGINE PYLON. THE CRACKS WERE IN THE TYPICAL CUTOUT AREA AT NAC STA 107. THE CRACKS WERE CUTOUT AND REPAIRED WITH A TITANIUM DOUBLER AND TRIPLER PER DAL B757 SRM 54-51-01, FIG 203 AND DOCUMENTED PER ER/A 363804-14. 2 L 7 2 4F RT A2NM 1998012900360 19980129 00360 NM 1998 1 29 DLM88980200 1 19980122 A 2120 AIR DISTRIBUTION DOUG MD88 MD88 3023688 NM CABIN ODOR A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 905DL 49536 ON FINAL APPROACH, AN ACRID BURNING SMELL WAS DETECTED IN CBN/ CKPT. BOTH AFT SMOKE DETS WENT OFF. NO VISIBLE CONTAMIN ATION NOTED. PERFORMED DUCT BURNOUT PROCEDURES PER MM. INSP AREA FOR LKS AND SMELL/ NO PROBS NOTED. COALESCER BAGS PR EV RPLD. 2 L 7 2 4F RT A6WE 1998012900361 19980129 00361 WP 1998 1 29 DLL14980201 1 19980123 A 5330 1503492 SKIN LKHEED 1011 1011385115 5265015 WP BS 345 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 DENTS FOUND IN THE FUSELAGE SKIN BETWEEN FS 330 AND FS 360 BETWEEN S49 AND 50. REPAIRED PER ERA 331248-14. 2 L 7 3 4F A23WE 1998012900362 19980129 00362 WP 1998 1 29 DLL14980202 1 19980123 A 5330 1503679165 SKIN LKHEED 1011 1011385115 5265015 WP BS 1315 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 FUSELAGE SKIN IN THE KEELSON AREA BETWEEN LBL 16 AND LBL 42.5 FROM FS 1273 TO 1363 WAS CORRODED. SPLICED PER ERA 331192 -14. 2 L 7 3 4F A23WE 1998012900363 19980129 00363 NM 1998 1 29 DL72S980203 1 19980120 A 5330 655456512 SKIN BOEING 727 727225 1384077 NM BS 500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 THE FUSELAGE SKIN BETWEEN STA 490 TO 520 WAS FOUND CORRODED AT STRINGER 27R. THE DAMAGED SKIN WAS CUTOUT AND A DOUBLER AND STRUCTURAL FILLER WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 363702-14, REV B. 2 L 7 3 4F A3WE 1998012900364 19980129 00364 NM 1998 1 29 DL72S980204 1 19980123 A 5330 655458297 SKIN BOEING 727 727232 1384082 NM BS 1030 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 FUSELAGE SKIN DAMAGE AT BS 1030 AND S3L OCCURRED. REPAIRED PER ERA 331249-14. 2 L 7 3 4F A3WE 1998012900365 19980129 00365 NM 1998 1 29 DL72S980205 1 19980119 A 5743 6582162 BEAM BOEING 727 727225 1384077 NM MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 TYPICAL CORROSION WAS FOUND IN MANY OF THE HOLE BORES OF THE LT AND RT MAIN LANDING GEAR SUPPORT BEAMS AT THE SKIN PANEL ATTACH LOCATIONS. SURFACE CORROSION WAS ALSO FOUND ON THE BEAMS. THE SURFACE WAS MACHINED TO REMOVE CORROSION AND TH E HOLE BORES WERE OVERSIZED. BUSHINGS AND OVERSIZE FASTENERS WERE INSTALLED PER ER/A 363569-14. 2 L 7 3 4F A3WE 1998012900366 19980129 00366 WP 1998 1 29 DLL10980206 1 19980123 A 3244 TIRE LKHEED 1011 10113851 5265010 WP NLG SEPARATED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 728DA 193C1173 AFTER V1 ON T/O ROLL, THERE WAS A LOT OF VIBRATION FROM THE NOSEWHEEL. AFTER LIFTOFF C-SYSTEM LOST MOST OF ITS QTY. RE TURNED TO ATL. FOUND LT NOSE TIRE CAME APART AND BROKE THE C-SYS LINE TO THE NOSE STEERING ACTUATOR. REPLACED SAME AND RELACED WHEEL ASSY. 2 L 7 3 4F A23WE 1998012900367 19980129 00367 NM 1998 1 29 DL767980207 1 19980121 A 5320 PRESSURE DECK BOEING 767 767232 1385132 NM BS 977 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 103DA 22215 THE WHEEL WELL PRESSURE DECK WAS FOUND WITH A CRACK AT 977 ON THE LEFT HAND SIDE AT LBL 35, THE CRACK IS 12 INCHES LONG. THE CRACK WAS REPAIRED PER 767-200 SRM 53-50-51 FIG 202 AND ERA 363828-14. AN EIGHT INCH CRACK WAS ALSO FOUND ON THE RIGHT HAND SIDE AT RBL 24.5. IT WAS REPAIRED PER SRM 53-50-51-2-204. REPAIRS WERE MADE ON NR CARDS 1, 2 AND 6. 2 L 7 2 4F RT A1NM 1998012900368 19980129 00368 NM 1998 1 29 DL72E980208 1 19980123 A 3350 20131A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 283WA 21485 TRACK LIGHTING INOP IN FIRST CLASS. REPLACED BATTERY PACK, CKS GOOD. 2 L 7 3 4F A3WE 1998012900369 19980129 00369 NM 1998 1 29 DLM11980210 1 19980123 A 3350 BATTERY PACK 6044113 DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805DE 0041 48476 L2 EMER EXIT BATTERY PACK FAILS TEST, READS LOW. REPLACED L-2 BATTERY PACK, CKS GOOD. 2 L 7 3 4F RT A22WE 1998012900370 19980129 00370 NM 1998 1 29 P5CA9800036 1 19980122 A 5314 ANGLE BOEING 747 747132 1384882 NM BS 1310 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 ANGLE CRACKED BOTTOM OF KEEL BEAM APPROX STA 1310. REMOVED AND REPLACED ANGLE BOTTOM OF KEEL BEAM STA 1310 IAW SRM 51-30 -02 AND 51-10-01. 2 L 7 4 4F A20WE 1998012900371 19980129 00371 NM 1998 1 29 P5CA9800037 1 19980122 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1780 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 SEAT TRACK CRACKED AT BS 1780 AT RBL 50. REPAIRED IAW SRM 53-10-05 FIG 5. 2 L 7 4 4F A20WE 1998012900372 19980129 00372 NM 1998 1 29 P5CA9800038 1 19980122 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1360 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON PANEL SUPPORT ANGLE BRACKET KEEL BEAM AREA STA 1360. REMOVED T- EXTRUSION AND ANGLE BRACKET AND REP LACED WITH NEW FABRICATED ANGEL IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998012900373 19980129 00373 NM 1998 1 29 P5CA9800039 1 19980122 A 5755 PANEL BOEING 747 747132 1384882 NM NR 12 SPOILER CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON #12 SPOILE PANEL UPPER SERVICE - LITE CORROSION. REMOVED CORROSION PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998012900374 19980129 00374 NM 1998 1 29 RAAA98B1004 1 19980125 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 FWD RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998012900375 19980129 00375 GL 1998 1 29 RAAA98E8001 2 19980123 A 7230 6828400 COMPRESSOR LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 3 ENGINE FAILED A A RAAA E ENGINE SHUTDOWN A E M FLAME/FIRE VIBRATION/BUFFET OVER TEMP TX TAXI/GRND HDL 1 AL 03 178RV 36412 8155 188C2010 501227 DURING GROUND START OPERATION WITH NR 3 ENG IN HIGH SPEED GROUND IDLE AND SUPPLYING BLEED AIR TO START NR 4 ENG FLT CREW REPORTED LOUD BANG WITH RAPID RPM AND TIT RISE NR 3 ENGINE. SHUTDOWN NR 3 ENG WITH EMERGENCY HANDLE. NO COWL PENETRAT ION OR 1ST STAGE FOD NOTED. METALIC PARTICLES (LESS THAN .0625 IN.) IN EXHAUST AREA BUT NO TURBINE DAMAGE NOTED. COMPR ESSOR CASE SPLITLINE BOLTS FAILED FROM 7TH STAGE FORWARD WITH CASE SPLITLINE MATING SURFACES SEPARATED APPROX .25 IN TO .375 IN. EXTENSIVE DAMAGE TO 5TH AND 10TH STAGE BLADES NOTED AND BLEED MANIFOLDS PARTIALY FILLED WITH COMPRESSOR BLADE PIECES. CHANGED ENGINE PER EF 71-1-0. 2 L 7 4 4T 4 T 4A22 E282 1998012900376 19980129 00376 WP 1998 1 29 CALA9800100 1 19980124 A 3297 WIRE DOUG DC9 DC982 3022082 WP NLG BROKEN A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 14814 49112 THE NLG INDICATED RED UNSAFE WHEN GEAR WAS EXTENDED, BUT THE COCKPIT INDICATOR PIN SHOWED DOWN AND LOCKED ON APPROACH TO EWR. A GO-AROUND WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BROKEN WIRE ON NLG DOWNL OCK SENSOR. THE WIRE WAS SPLICED. A GEAR SWING WAS PERFORMED IAW MM 32-31-00 WITH OPERATION AND INDICATIONS CHECKING G OOD. 2 L 7 2 4F A6WE 1998012900377 19980129 00377 WP 1998 1 29 CALA9800101 1 19980124 A 2913 3508806 HYD PUMP DOUG DC10 DC1030 3023501 WP NR 3 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 37077 4456 46981 THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT CAME ON JUST PRIOR TO LANDING AT LGW. THE ELEVATOR FEEL CHANNEL LIGHT CAME ON AFTER LANDING. THE AIRCRAFT HAD LOST FLUID FROM THE NR 3 HYDRAULIC SYSTEM. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN R IGHT HYDRAULIC PUMP HOUSING LEAKING. THE HYDRAULIC PUMP WAS REMOVED AND REPLACED. THE NR 3 HYDRAULIC SYSTEM WAS SERVIC ED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998012900378 19980129 00378 WP 1998 1 29 CALA9800102 1 19980123 A 5341 FITTING DOUG DC9 DC932 3022066 WP RT WING/FUS CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 47638 INSPECTION FOUND A 3 INCH CRACK IN RT WING TO FUSELAGE ATTACH FITTING AT FRONT SPAR. A STRAP WAS INSTALLED ON WING TO F USELAGE ATTACH ANGLE IAW ECRA 5340-0100. 2 L 7 2 4F A6WE 1998012900379 19980129 00379 WP 1998 1 29 CALA9800103 1 19980124 A 3320 03980 BALLAST DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 09 93875 49125 AN ELECTRICAL ODOR WAS REPORTED IN MAIN CABIN IN THE VICINITY OF ROW 15 WHILE AIRCRAFT WAS ON THE GROUND IN TPA. MAINTE NANCE FOUND BALLAST FOR OVERHEAD LIGHTS AT ROW 15 AT FAULT. THE BALLAST WAS REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998012900380 19980129 00380 NM 1998 1 29 9801386303 1 19980125 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 22HJK - LAV DR2R AND FROM ROWS 51HJK TO 62HJK . RECONNECTED WIRES, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998012900381 19980129 00381 EU 1998 1 29 9801393205 1 19980122 A 2910 HYD SYST AIRBUS 320 A320211 3930320 EU YELLOW HYD SYST REQD SERVICE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 305US 41 DURING TAKEOFF ROLL, RECEIVED HYD Y RSVR LO LVL MESSAGE. ABORTED TAKEOFF AT 80 KNOTS WITHOUT INCIDENT. MAINTENANCE SER VICED YELLOW HYDRAULIC SYSTEM, NO LEAKS FOUND. 2 L 7 2 4F RT A28NM 1998012900382 19980129 00382 EU 1998 1 29 9801403215 1 19980122 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 315US 171 DURING EMERGENCY LIGHT TEST, RECEIVED EPSU INT LOAD AFT L MESSAGE. MAINTENANCE REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998012900383 19980129 00383 SO 1998 1 29 COMA9810028 1 19980123 A 2910 HYD SYST EMB 120 EMB120RT SO GREEN HYD SYST REQD SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 159CA 120159 GREEN HYDRAULIC QUANTITY LOW. SERVICED HYDRAULIC SYSTEM, INSPECTED FOR LEAKS AND NONE FOUND. 2 L 7 2 4T RT A31SO 1998012900384 19980129 00384 SO 1998 1 29 COMA9810029 1 19980123 A 5610 NP1513111 WINDSHIELD EMB 120 EMB120RT SO LT COCKPIT CRACKED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 264CA 15078 120256 PILOTS WINDSHIELD CRACKED. REPLACED WINDSHIELD. 2 L 7 2 4T RT A31SO 1998012900385 19980129 00385 EA 1998 1 29 COMA9860020 1 19980122 A 5310 STRUCTURE CNDAIR CL600 CL6002B19 EA FUSELAGE DAMAGED A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 917CA 7017 AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF. MAJOR STRUCTURAL DAMAGE WAS FOUND AT RIGHT HAND FORWARD SECTION OF FUSELAG E. PROBABLE CAUSE IS GROUND EQUIPMENT. AIRCRAFT FERRIED TO WVAC FOR REPAIRS. 2 L 7 2 4F RT A21EA 1998012900386 19980129 00386 1998 1 29 COMA9860021 4 19980122 A 3445 TCAS CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 943CA 7062 AIRCRAFT SUSTAINED NEGATIVE 'GS' FOR 5 SECONDS DUE TO TCAS RA COMMAND, (FALSE WARNING). COMPLIED WITH TURBULANCE AND HA RD LANDING INSPECTIONS. NO DAGMAGE NOTES. 2 L 7 2 4F RT A21EA 1998012900387 19980129 00387 EA 1998 1 29 COMA9860022 1 19980124 A 3350 364911 LAMP CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912CA 7011 FLOOR EMERGENCY LIGHTING AT ROW 7 IS INOP. RESECURED LIGHTING STRIP INTO RECEPTACLE. 2 L 7 2 4F RT A21EA 1998012900388 19980129 00388 EA 1998 1 29 COMA9860023 1 19980122 A 2741 WARNING CNDAIR CL600 CL6002B19 EA STAB TRIM ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 966CA 7132 STAB TRIM AND MACH TRIM CAUTION MESSAGE. PERFORMED FUNCTIONAL CHECK OF SYSTEM. NO FAULTS FOUND. 2 L 7 2 4F RT A21EA 1998012900389 19980129 00389 NM 1998 1 29 UPS98225524 1 19980122 A 5320 CHORD BOEING 727 72722C 138400F NM BS 880.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 928UP 19091 INSPECTION TYPE-SI, WHILE WORKING CUSTOMER ID 664363 FUSELAGE 136 FOUND CORROSION ON LOWER SURFACE OF LOWER PRESSURE BOX CHORD AT BS 880.5, RBL 65, WL 199. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-6, REPAIRED PER SRM 53-10 -8. 2 L 7 3 4F A3WE 1998012900390 19980129 00390 NM 1998 1 29 UPS98425539 1 19980122 A 5220 ESCAPE HATCH BOEING 747 747123 1384873 NM COCKPIT WILL NOT STOW A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-N/A, COCKPIT CEILING ESCAPE HATCH OUTSIDE LATCH WILL NOT STAY STOWED, BY OPERATING INTERIOR LATCH OUTSID E HANDLE POPS UP. REF MM 52-21-00, CLEANED AND LUBED EXIT HATCH HANDLE AND INTERIOR MECHANISM, REMOVED BUFF FROM HANDLE GUIDE. OPERATED DOOR SEVERAL TIMES, NO DEFECTS NOTED. 2 L 7 4 4F A20WE 1998012900391 19980129 00391 NM 1998 1 29 UPS98425540 1 19980125 A 3350 S1356B37 LIGHT BOEING 747 747123 1384873 NM CABIN MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-N/A, EMERGENCY LIGHT IN CEILING ABOVE STAIRWELL WILL NOT SHUT OFF. REMOVED AND REPLACED LIGHT ASSY, CK OK. 2 L 7 4 4F A20WE 1998012900393 19980129 00393 WP 1998 1 29 UPS98825528 1 19980113 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 200-220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, DOUBLER AT FS 200 TO 220 LONG 28L EXFOLIATED OUT OF LIMITS (INTERNAL). REMOVED, FABRICATED, AND INST ALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5773863. 2 L 7 4 4F RT 4A25 1998012900394 19980129 00394 WP 1998 1 29 UPS98825529 1 19980109 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 8-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, INTERNAL DOUBLER AROUND A/C ACCESS CORRODED BEYOND LIMITS FS 8 TO 70 L-34R TO L-33R. REMOVED, FABRIC ATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5649028. 2 L 7 4 4F RT 4A25 1998012900395 19980129 00395 WP 1998 1 29 UPS98825530 1 19980103 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 190-450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FUSELAGE SKIN CORRODED BEYOND LIMITS AND INTERNAL DOUBLERS CORRODED BEYOND LIMITS. REMOVED, FABRICAT ED, AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 51-1-21 AND DWG 9755878-1 AND 9754011-505. REMOVED AND REPLACED SKIN IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998012900396 19980129 00396 WP 1998 1 29 UPS98825532 1 19980107 A 5320 3755822502N FITTING DOUG DC8 DC873F 302199F WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, TORQUE BOX FITTING CRACKED AT FS 280 BETWEEN L-35L AND L-36. REMOVED AND REPLACED FITTING IAW SRM 53 -2-0. 2 L 7 4 4F RT 4A25 1998012900397 19980129 00397 WP 1998 1 29 UPS98825533 1 19980105 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 702 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FLOORBEAM FS 702 RBL 40 UPPER AFT FLANGE EXFOLIATED. REPAIRED IAW DHC SK 852-198. 2 L 7 4 4F RT 4A25 1998012900398 19980129 00398 WP 1998 1 29 UPS98825534 1 19980106 A 5511 5654549501 SPAR CAP DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, LT HORIZ STAB ATTACH ANGLE INSIDE AUX SPAR AREA CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20 AND 51-1-21. 2 L 7 4 4F RT 4A25 1998012900399 19980129 00399 WP 1998 1 29 UPS98825535 1 19980105 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 808-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, SEAT TRACK EXFOLIATED FS 808 LBL 22.5 AND AT FS 870. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998012900400 19980129 00400 WP 1998 1 29 UPS98825537 1 19980115 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 808-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, SEAT TRACK EXFOLIATED FS 808 AND 870 LBL 45. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998012900401 19980129 00401 WP 1998 1 29 UPS98825544 1 19980111 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 40 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, COCKPIT SUBFLOOR FINGER DOUBLER CORRODED FS -40 RBL 55. REMOVED, FABRICATED, AND INSTALLED REPLACEME NT DOUBLER IAW SRM 51-1-21 AND DWG 5612298. 2 L 7 4 4F RT 4A25 1998012900402 19980129 00402 EU 1998 1 29 QXEA9800042 1 19980123 A 3350 1820 LAMP FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 GEG - OVERHEAD EVACUATION LIGHT AT ROW 4 IS INOP. MAINTENANCE RELAMPED. 2 L 7 2 4F RT A20EU 1998012900403 19980129 00403 EU 1998 1 29 QXEA9800043 1 19980123 A 2170 COALESCER FOKKER F28 F28MK4000 4990810 EU CABIN DIRTY A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 491US 11156 SEA - AFTER APU START WITH AIR ON AND EITHER PACK ON, SMOKE FILLED CABIN. REPLACED WATER SEPARATOR SOCKS. 2 L 7 2 4F RT A20EU 1998012900404 19980129 00404 NM 1998 1 29 QXEA9800044 1 19980124 A 6120 AUTOFEATHER DHAV DHC8 DHC8202 2809007 NM PROP SYST MALFUNCTIONED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PUW - AUTOFEATHER WOULD NOT TEST. MAINTENANCE CONTROL HAD CREW CYCLE ECU'S, POWER LEVERS AND CONDITION LEVERS STATICALL Y, THEN STARTED ENGINES AND TESTED SYSTEM. OPERATIONAL CHECK GOOD, NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998012900405 19980129 00405 NM 1998 1 29 QXEA9800045 1 19980124 A 2731 CONTROLS DHAV DHC8 DHC8102 2809003 NM ELEV TRIM LACK OF LUBE A QXEA K NONE O OTHER CR CRUISE 1 NM 09 820PH 63 SEA - ELEVATOR TRIM INOP -10 TO -29 DEGREES CELCIUS. LUBRICATED LEFT AND RIGHT ELEVATOR TRIM ACTUATORS AND ASSOCIATED C HAINS. OPERATED ELEVATOR TRIM FULL TRAVEL SEVERAL TIMES, CHECK GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998012900406 19980129 00406 EU 1998 1 29 QXEA9800046 1 19980125 A 3350 MFF1055 BULB GRIMES 5515900004 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 GEG - EMERGENCY EXIT LIGHT AT ROW 8E NOT ILLUMINATED. MAINTENANCE RELAMPED, OPERATION CHECK GOOD. 2 L 7 2 4F RT A20EU 1998012900407 19980129 00407 NM 1998 1 29 98FDEA00050 1 19980122 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 FWD CARGO BS 700 FRAME DENTED BETWEEN STRINGER 23 LT TO STR 25 LT. REMOVED DAMAGED AREA OF BELLFRAME 10 LONG USING .25 DRILL AT ENDS TO MAINTAIN .25 RADIUS. FABRICATED FROM PANEL (P/N EY74) 7075-T6 X .063 THICK AND INSTALLED DOUBLER PER S RM 53-10-07-5 (AARD) TREATED AND PRIMED ALL EFFECTED AREAS PRIOR TO INSTALLATION LENGTH OF PANEL USED 20 LONG. 2 L 7 3 4F RT A3WE 1998012900408 19980129 00408 NM 1998 1 29 98FDEA00051 1 19980122 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 FWD CARGO STATION 500 AT STRINGER 23 LT HAS DENTED FRAME. NR 0330 LOWER FWD CARGO LT SIDE BS 500 LT BELLFRAME DENTED AT STR 24 LT. REMOVED DAMAGED AREA OF BELT FRAME STRINGER 23 TO 25 LT USING .25 DRILL FOR CORNER RADIUS. FABRICATED REPA IR FROM SHOP MANUFACTURED APPROVED PART (P/N EY74) 7075-T6 X 063 THICK USING PROPER FASTENERS, SHIMS (AT LOWER END) AND TREATED AND PRIMED PARTS. INSTALLED ALL PARTS PER SRM 53-10-07-3 AARB. 2 L 7 3 4F RT A3WE 1998012900409 19980129 00409 NM 1998 1 29 98FDEA00052 1 19980121 A 5311 FRAME BOEING 727 727233 138408A NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 FORWARD CARGO AT BS 680 LT FRAME DENTED BETWEEN STRINGER 22 LT AND 25 LT. REMOVED 13 DAMAGED SECTION USING .25 RADII ON RELIEF AREAS. FABRICATED AND INSTALLED DOUBLER OF .063 THICK 7075-T6 MATERIAL (P/N 563886) 24 LONG AND INSTALLED REPAI R IAW SRM 53-10-04 PAGE 5, FIGURE 1. 2 L 7 3 4F RT A3WE 1998012900410 19980129 00410 NM 1998 1 29 98FDEA00053 1 19980122 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0682, WORK CARD NR 72C237-02, BS 1070, RBL 60 TO LBL 24, LOWER FWD FLANGE CORRODED OF FLOORBEAM. CUT OUT CORROSION D AMAGE. INSTALLED FLOORBEAM REPAIR DOUBLER PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 1998012900411 19980129 00411 EU 1998 1 29 98FDEA00048 1 19980126 A 2913 MX386399 HYD ELEC PUMP AIRBUS 310 A310222 3930315 EU GREEN HYD SYST SHORTED A FDEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 25 449FE 217 BURNT 101 VU WIRING CAUSED BY GREEN HYDRAULIC PUMP INTERNALLY SHORTED. C/B DID NOT POP. THIS CAUSED WIRING BEHIND 101 VU PANEL TO SMOKE AND BURN UP. REPLACED GREEN ELECTRIC HYDRAULIC PUMP. REPLACED 50 AMP CIRCUIT BREAKER, REPAIRED BURNT WIRING. 2 L 7 2 4F RT A35EU 1998012900412 19980129 00412 EU 1998 1 29 98FDEA00049 1 19980126 A 2910 AE70592612 HOSE AIRBUS 310 A310222 3930315 EU NR 2 ENGINE LEAKING A FDEA O OTHER K FLUID LOSS IN INSP/MAINT 1 SO 25 419FE 345 FOUND LEAKING HYDRAULIC LINES ON NR 2 ENGINE THAT BURNT HOLE IN PAN. REPLACED ALL HYDRAULIC LINES, PAN AND BLANKETS. 2 L 7 2 4F RT A35EU 1998012900413 19980129 00413 WP 1998 1 29 ABXA9800036 1 19980122 A 5250 AR25291GR41 LATCH DOUG DOUG DC9 DC941 302207N WP COCKPIT DOOR OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 COCKPIT DOOR WOULD NOT OPEN. LUBRICATED AND ADJUSTED DOOR LATCH ASSEMBLY. 2 L 7 2 4F A6WE 1998012900414 19980129 00414 WP 1998 1 29 ABXA9800037 1 19980123 A 5311 2537716 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 1040 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 ZEE-FRAME AT STATION 1040 CORRODED BEYOND LIMITS. REPAIRED IAW ABX REA D853-0229 AND DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1998012900415 19980129 00415 WP 1998 1 29 ABXA9800038 1 19980123 A 5311 2750825 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 1120 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 811AX 46113 FRAME CORRODED BEYOND LIMITS AT STATION 1120, LONGERON 36. REPAIRED IAW ABX REA D853-21894MR AND DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998012900416 19980129 00416 WP 1998 1 29 ABXA9800039 1 19980123 A 3230 459734005505 CYLINDER DOUG DOUG DC8 DC863F 302198F WP LT MLG DEFECTIVE A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 812AX 4552 46126 DURING CLIMBOUT, RED LANDING GEAR UNSAFE LIGHT ILLUMINATED. LEFT MAIN LANDING GEAR INDICATED UNLATCHED. RECYCLED LANDI NG GEAR, NO HELP. LANDING WAS UNEVENTFUL. REPLACED LEFT MAIN LANDING GEAR UPLATCH MECHANISM CYLINDER IAW DC8 MM 32-31- 3, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998012900417 19980129 00417 1998 1 29 ABXA9800040 4 19980122 A 3440 36143091006 MFD DOUG DC8 DC863F 302198F WP COCKPIT MALFUNCTION A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 826AX 235 46061 FAINT BURNING ODOR WAS REPORTED BY CREW DURING FLIGHT AND ON GROUND. PROBLEM WAS DETERMINED TO BE MULTI-FUNCTION DISPLA Y (MFD). REPLACED DISPLAY UNIT IAW DC8 MM 34-20, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998012900418 19980129 00418 SO 1998 1 29 SWIA971065 1 19980110 A 2913 PV302229 HYD PUMP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 214SW 120280 AFTER TAKEOFF DURING GEAR RETRACTION, LEFT MAIN HYDRAULIC PUMP FAILED. RETRY FAILED. RETURNED AND LANDED AT SLC. REMO VED AND REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP. CHANGED HYDRAULIC FILTER ON LEFT PACK, FOUND NO CONTAMINATION. OPS CHECKS AND LEAKS CHECKS GOOD IAW MM 29. 2 L 7 2 4T 4 T RT A31SO E20NE 1998012900419 19980129 00419 SO 1998 1 29 SWIA971066 1 19980106 A 3230 HARNESS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG FAILED A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 209SW 120269 AT CRUISE, THE LEFT MAIN A GREEN INDICATION CAME ON, TRIED TO PUT TO GEAR DOWN NOTHING HAPPENED. USED THE ELECTRICAL OV ERRIDE CHECK LIST AND GEAR CAME DOWN. REMOVED AND REPLACED THE LEFT MLG DOWNLOCK A HARNESS IAW MM 32-61-01, OPS CHECKS GOOD. PERFORMED GEAR SWING, OPS AND INDICATION CHECKS GOOD IAW MM 32-30-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998012900420 19980129 00420 SO 1998 1 29 SWIA971067 1 19980107 A 3020 DE-ICE MONITOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 194SW 120120 RIGHT ENGINE INTAKE DE-ICE INOP AFTER 10 MIN. RETURNED TO SLC. REPLACED DE-ICE MONITOR IAW MM 30-00-00. RAN ENGINES F OR 30 MINUTES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998012900421 19980129 00421 EA 1998 1 29 SWIA971068 1 19980107 A 4990 OIL SYST CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE APU REQD SERVICE A SWIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 NM 07 408SW 7055 AT 57 MIN TO GO TO EUG, WE RECEIVED AND APU OIL TEMPERATURE MESSAGE. QRH CALLED FOR A DIVERSION TO NEAREST SUITABLE AIR PORT. SINCE EUG WAS IFR, THE SHUT DOWN OF APU WAS NOT AN OPTION. DIVERTED TO BOI. SERVICED APU OIL QUANTITY TO FULL, OPS CHECKS APU NORMAL PER MM 12-13-00. 2 L 7 2 4F 4 F RT A21EA E15NE 1998012900422 19980129 00422 NE 1998 1 29 SWIA971069 2 19980108 A 7261 OIL SYST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE REQD SERVICE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 186SW 120034 AFTER DEPARTURE FROM EKO, HAD A INTERMITTENT LOW OIL PRESSURE INDICATION ON LEFT ENGINE. RETURNED TO EKO. ADDED TWO QU ARTS OF EXXON 2380 OIL TO LEFT ENGINE PER INSTRUCTIONS FROM MAINTENANCE CONTROL. AIRCRAFT WAS RUN UP TO 100 PERCENT ENG INE INSTRUMENTS SHOW BOTH ENGINES NORMAL AND STEADY. NOTE: ALSO ADDED ONE QUART OF OIL TO RIGHT ENGINE. LEFT ENGINE W AS AT ADD 3 BEFORE OIL WAS ADDED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998012900423 19980129 00423 SO 1998 1 29 SWIA971070 1 19980108 A 3610 97962641 BLEED SO VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 203SW 120240 DURING CLIMBOUT, CABIN WOULD NOT PRESSURIZE IN AUTO OR MANUAL MODE. AFTER ENGINE START NOTICED LEFT BLEED CLOSED LIGHT WAS DIFFICULT TO EXTINGUISH. FLIPPED THE BLEED SWITCH SEVERAL TIMES BEFORE LIGHT WOULD EXTINGUISH. RETURNED TO SGU. R EMOVED AND REPLACED LEFT BLEED SHUT OFF VALVE IAW MM 25-30-00, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998012900424 19980129 00424 SO 1998 1 29 SWIA971072 1 19980101 A 3232 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 RIGHT MAIN GEAR WOULDN'T RETRACT UNTIL GEAR WAS CYCLED TWICE THEN THE RIGHT MAIN GEAR CAME UP AFTER 1 MIN AT 180 KIAS. R ETURNED TO FIELD. FOUND RIGHT INBOARD FORWARD GEAR DOOR ACTUATOR TO BE TO LONG AND PUSHING GEAR DOOR PAST INBOARD SEQUE NCE VALVE. ADJUSTED INBOARD MLG DOOR ACTUATOR IN ONE AND A HALF TURNS. SWUNG GEAR SEVERAL TIMES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998012900425 19980129 00425 NM 1998 1 29 P5CA9800040 1 19980124 A 5755 SKIN BOEING 747 747132 1384882 NM NR 3 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LT WING NR 3 SPOILER UPPER SKIN DELAMINATION. REMOVED AND REPLACED NR 3 SPOILER PER MM 27-61-02. 2 L 7 4 4F A20WE 1998012900426 19980129 00426 NM 1998 1 29 P5CA9800041 1 19980125 A 5720 FAIRING BOEING 747 747132 1384882 NM NR 7 FIXED CANOE WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 7 FIXED FAIRING CANOE NEEDS COMPOSIT REPAIR. REPAIRED FIXED FAIRING BY USING FIBERGLASS OVERLAYS IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998012900427 19980129 00427 NM 1998 1 29 P5CA9800042 1 19980123 A 5755 SKIN BOEING 747 747132 1384882 NM NR 11 SPOILER DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 11 SPOILER UPPER SKIN IN NEED OF REPAIR. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998012900428 19980129 00428 NM 1998 1 29 P5CA9800043 1 19980124 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE MIDFLAP DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 R/W O/B T/E MIDFLAP LOWER SIDE DELAMINATION. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998012900429 19980129 00429 NM 1998 1 29 P5CA9800044 1 19980125 A 5755 SKIN BOEING 747 747132 1384882 NM NR 8 SPOILER DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT WING NR 8 SPOILER LWR SURFACE HAS AREA OF DELAMINATION. REMOVED DISBONDED SKIN AND DAMAGED CORE. BONDED NEW CORE FI LLER AND DOUBLERS IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998012900430 19980129 00430 NM 1998 1 29 P5CA9800045 1 19980122 A 7830 SLEEVE BOEING 747 747249F 1384849 NM PWA JT9 JT9D7Q 52054 NE NR 1 ENGINE TR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 702238 NR 1 ENGINE FAN REVERSER SLEEVE DAMAGED AT THE 5 O'CLOCK POSITION. REPAIRED AS PER SRM 54-30-03. 2 L 7 4 4F 4 F A20WE E3NE 1998012900431 19980129 00431 1998 1 29 P5CA9800046 4 19980125 A 3441 788658011 INU BOEING 747 747124 1384874 NM COCKPIT FAILED A P5CA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 WP 23 855FT 19733 AFTER TAKEOFF, NR 2 INS WARNING LIGHT ILLUMINATED WITH THE FOLLOWING CODES 34, 42, 102 AND 56. REPLACED NR 2 INU SYSTEM ALIGNED TO 05, OK NO FAULT PER M/M 34-41-03. 2 L 7 4 4F A20WE 1998012900432 19980129 00432 NM 1998 1 29 P5CA9800047 1 19980123 A 7620 BAC63AF243058 CONNECTOR BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE CONTAMINATED A P5CA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 WP 23 855FT 19733 685654 DURING CLIMB AT APPROX 37,000 FT, NR 1 ENG FLAMED OUT. AFTER SEVERAL ATTEMPTS AT A RESTART THE ENGINE LIT OFF AND FLAME D OUT AGAIN. ENGINE FIREWALL PLUG DOO14J FOUND CONTAMINATED. CLEANED PLUG AND RESEATED PIN NR 17. ELECTRICALLY CHECKED OUT PER WDM 76-11-11. 2 L 7 4 4F 4 F A20WE E20EA 1998012900433 19980129 00433 NM 1998 1 29 VNAA9801011 1 19980124 A 2750 1050A000003 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE TE FLAPS TRIPPED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 461PS 3858 3075 DURING TAXI FOR TAKEOFF, A FLAP CONTROL FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE AND MAINTEN ANCE WAS CALLED. MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27 -50-00. OPERATIONAL CHECKS WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998012900434 19980129 00434 NM 1998 1 29 TWRA9801 1 19980112 A 3510 OXY REGULATOR BOEING 747 747131 1384881 NM COCKPIT LEAKING A TWRA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 608FF 19672 AIRCRAFT AIR TURN BACK DUE TO DEPLETED CREW OXYGEN DOWN TO ZERO. FOUND LEAK AT CREW STATION REGULATOR, REPAIRED, REPLAC ED OXYGEN BOTTLE. LEAK CHECK GOOD. (X) 2 L 7 4 4F A20WE 1998012900435 19980129 00435 EU 1998 1 29 WTAA980006 1 19980110 A 3297 622800200 WIRE BAG JETSTM JETSTM3101 1500215 EU NLG BROKEN A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 402UE 734 SFO - NOSE GEAR INTRANSIT LIGHT ILLUMINATED DURING GEAR RETRACTION. AIRCRAFT RETURNED TO STATION. MAINTENANCE REPAIRED BROKEN WIRE AT UPLOCK MICROSWITCH, PN 622800200. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1998012900436 19980129 00436 SO 1998 1 29 WTAA980004 1 19980109 A 3350 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A WTAA K NONE L NO TEST UK UNKNOWN 1 WP 17 201YW 120201 BFL - FORWARD SECTION OF EMERGENCY FLOOR LIGHTING REPORTED INOPERATIONAL. MAINTENANCE DEFERRED EMERGENCY LIGHTS PER MEL 33-50-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL, COULD NOT DUPLICATE PROBLEM. OPERA TIONAL CHECK SATISFACTORY. (X) 2 L 7 2 4T RT A31SO 1998012900437 19980129 00437 EA 1998 1 29 98ZZZX369 1 19980102 A 2910 HYDRAULIC LINE DHAV DHC7 DHC7102 2802708 EA NR 4 NACELLE LEAKING A CICA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 17 4860J 4860J 19 PRIOR TO FLIGHT FROM MIA, MECHANIC FOUND HYDRAULIC LEAK IN NR 4 NACELLE AND NR 2 HYDRAULIC QUANTITY LOW. INSPECTION FOU ND HYDRAULIC LINES PRESSURE AND RETURN ARE CHAFED AND CRACKED. LINES WERE REPLACED WITH TEMP FLEX LINES. INSPECTED AND FOUND NO LEAKS. AIRCRAFT FERRIED TO FLL AND TEMFLEX LINES REPLACED WITH HARD LINES. FAIR LEAD HOLDING LINE WAS MELTED AND LINES VIBRATED. FAIR LEAD REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 4 4T A20EA 1998012900441 19980129 00441 NM 1998 1 29 TSAA9833002 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OSP CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 44,189:44 HOURS. TAC: 57,305. (X) 2 L 7 2 4F A16WE 1998012900442 19980129 00442 NM 1998 1 29 TSAA9833003 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 44,189:44 HOURS. TAC: 57,305. (X) 2 L 7 2 4F A16WE 1998012900443 19980129 00443 NM 1998 1 29 TSAA9833004 1 19980103 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 37,413:12 HOURS. TAC: 71.643. (X) 2 L 7 2 4F A16WE 1998012900444 19980129 00444 NM 1998 1 29 TSAA9833005 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X) 2 L 7 2 4F RT A16WE 1998012900445 19980129 00445 NM 1998 1 29 TSAA9833006 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X) 2 L 7 2 4F RT A16WE 1998012900446 19980129 00446 NM 1998 1 29 TSAA9833008 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X) 2 L 7 2 4F RT A16WE 1998012900447 19980129 00447 NM 1998 1 29 TSAA9833009 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 33,483:34 HOURS. TAC: 39,664. (X) 2 L 7 2 4F RT A16WE 1998012900448 19980129 00448 NM 1998 1 29 TSAA9833010 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X) 2 L 7 2 4F RT A16WE 1998012900449 19980129 00449 NM 1998 1 29 TSAA9833011 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X) 2 L 7 2 4F RT A16WE 1998012900450 19980129 00450 NM 1998 1 29 TSAA9833012 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X) 2 L 7 2 4F RT A16WE 1998012900451 19980129 00451 NM 1998 1 29 TSAA9833013 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. (X) 2 L 7 2 4F RT A16WE 1998012900452 19980129 00452 NM 1998 1 29 TSAA9833014 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 43,419:53 HOURS. TAC: 60,763. 2 L 7 2 4F RT A16WE 1998012900453 19980129 00453 NM 1998 1 29 TSAA9833015 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 30,406:02 HOURS. TAC: 35,874. (X) 2 L 7 2 4F RT A16WE 1998012900454 19980129 00454 NM 1998 1 29 TSAA9833016 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LGIHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 30,406:02 HOURS. TAC: 35,874. (X) 2 L 7 2 4F RT A16WE 1998012900455 19980129 00455 NM 1998 1 29 TSAA9833017 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. TAT: 30,406:02 HOURS. TAC: 35,874. (X) 2 L 7 2 4F RT A16WE 1998012900456 19980129 00456 NM 1998 1 29 TSAA9833018 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK FOUND POSITION NR 5 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. TAT: 30,406:01 HOURS. TAC: 35,874. (X) 2 L 7 2 4F RT A16WE 1998012900484 19980129 00484 WP 1998 1 29 GAIA9802 1 19980108 A 2612 FIRE WARNING CVAC 240 240D 2422660 WP CARGO COMPT ACTIVATED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 94258 119 CLE/YIP - FLT 258 - DURING CRUISE, FLIGHT CREW NOTED THE FIRE DETECTION WARNING SYSTEM CAME ON TWICE FOR A FEW SECONDS, FOR THE FWD CARGO/ELECT COMPARTMENT. THE AIRCRAFT HAS BEEN GROUNDED AT YIP AND WILL REMAIN THERE TILL THE FIRE WARNING SYSTEM CAN BE PROPERLY CORRECTED. (X) 2 L 7 2 4R RT A793 1998012900485 19980129 00485 WP 1998 1 29 GAIA9801 1 19980105 A 2612 FIRE WARNING DOUG DC9 DC915F 3022037 WP NR 2 ENGINE ILLUMINATED A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 112PS 47013 KHA - FLT 112 - YIP TO YIP. WHILE IN CRUISE, THE NR 2 ENGINE A-LOOP LIGHT ILLUMINATED. THE FLIGHT CREW PERFORMED FIRE CHECK, ALL NORMAL. DURING TAXI, BOTH LOOPS TESTED NORMAL. INSPECTION PERFORMED FIRE WARNING TEST PER DC-9 MM. ALL TES TS OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F A6WE 1998012900486 19980129 00486 NM 1998 1 29 TSAA9833019 1 19980102 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 30,406:01 HOURS. TAC: 35,874. (X) 2 L 7 2 4F RT A16WE 1998012900487 19980129 00487 NM 1998 1 29 TSAA9833020 1 19980102 A 3350 6013211 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 ON SERVICE CHECK, FOUND LT OVERWING EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. TAT: 28,188:25 HOURS. TAC: 32,705. (X) 2 L 7 2 4F A16WE 1998012900488 19980129 00488 NM 1998 1 29 TSAA9833021 1 19980105 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 46,104:23 HOURS. TAC: 59,386. (X) 2 L 7 2 4F A16WE 1998012900489 19980129 00489 NM 1998 1 29 TSAA9833022 1 19980105 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 46,104:23 HOURS. TAC: 59,386. (X) 2 L 7 2 4F A16WE 1998012900490 19980129 00490 NM 1998 1 29 TSAA9833023 1 19980105 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 46,104:23 HOURS. TAC: 59,386. (X) 2 L 7 2 4F A16WE 1998012900491 19980129 00491 NM 1998 1 29 TSAA9833024 1 19980105 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 27,863:43 HOURS. TAC: 31,837. (X) 2 L 7 2 4F A16WE 1998012900492 19980129 00492 WP 1998 1 29 AALA980014 1 19980104 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 443AA 49469 ORD - FLT 0204 - AFTER TAKEOFF MIA, GEAR WARNING LIGHTS ILLUMINATED. AFTER REACHING CRUISE ALTITUDE AND THROTTLES RETAR DED, LIGHTS EXTINGUISHED. PROCEEDED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH CONTROL. ACCOMPLIS HED GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998012900493 19980129 00493 WP 1998 1 29 AALA980051 1 19980109 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 451AA 49477 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE FOUND INOPERATIVE. REPLACED EM ERGENCY FLOOR PATH LIGHTING FORWARD MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F A6WE 1998012900494 19980129 00494 EU 1998 1 29 REXA98001 1 19980105 A 2613 OVERHEAT SENSOR SAAB SF340 SF340A 7850100 EU RT ENGINE CONTAMINATED A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 407BH 340A078 RIGHT HAND TAIL PIPE HOT LIGHT IN-FLIGHT. CLEANED MOISTURE FROM TAILPIPE OVER HEAT SENSOR. CREW RAN A/C SYSTEM. OPS C HECKED GOOD. (X) 2 L 7 2 4T RT A52EU 1998012900495 19980129 00495 1998 1 29 REXA98002 4 19980104 A 3445 TCAS SAAB SF340 SF340A 7850100 EU COCKPIT INOPERATIVE A REXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 107PX 340A010 TCAS INOPERABLE. GROUND TEST TCAS, SYSTEM TEST GOOD. GOOD FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1998012900496 19980129 00496 1998 1 29 REXA98003 4 19980106 A 3442 6224022001 RADAR R/T SAAB SF340 SF340A 7850100 EU FWD FUSELAGE FAILED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 935MA 147 340A073 RADAR INTERMITTENT, BUT ALSO CYCLED THROUGH ALL RINGS, MODES, EVEN TURN OFF/ON BY ITSELF. REMOVED AND REPLACED RADAR R/ T. (X) 2 L 7 2 4T RT A52EU 1998012900497 19980129 00497 EU 1998 1 29 REXA98004 1 19980107 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 346AM 340A032 RIGHT HAND TAIL PIPE HOT LIGHT ON. CLEANED CANNON PLUGS ON TAILPIPE OVERTEMP SPOT DETECTORS. OPS CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998012900498 19980129 00498 EU 1998 1 29 REXA98005 1 19980108 A 3020 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 344AM 340A030 RIGHT HAND INTAKE HEAT INOPERABLE. CYCLING ON CLIMB-OUT. CLEANED OIL OUT OF RIGHT HAND THERMAL CONTROLLER AND LOAD MON ITOR CANNON PLUGS. (X) 2 L 7 2 4T RT A52EU 1998012900499 19980129 00499 NE 1998 1 29 REXA98006 2 19980108 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT OVERTEMP A REXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 347AM 340A039 ABORTED TAKEOFF, LEFT ENGINE TEMP 932 DEGREES. RAN ENGINES UP TO 108 PERCENT TORQUE. WITH LOW PRESSURE BLEEDS ON, TEMP WAS 900 DEGREES. OPS CHECK OK. (X) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998012900500 19980129 00500 EU 1998 1 29 REXA98007 1 19980108 A 3240 63740 MAXARET BRAKE BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 311PX H2167 679 RIGHT HAND MAIN BRAKE DOES NOT WORK AT ALL WITH RUDDER PEDALS. REMOVED AND REPLACED RIGHT HAND MAXARET BRAKE ASSY. OPS CHECK GOOD. (X) 2 L 7 2 4T RT A21EU 1998012900501 19980129 00501 NE 1998 1 29 REXA98008 2 19980111 A 7200 31033101 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A REXA E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 SO 25 110PX 367221KU 340A023 367221KU RAPID RISE IN ITT ON RIGHT HAND ENGINE. SHUT DOWN AND RETURNED TO SDF. REMOVED AND REPLACED RIGHT HAND ENGINE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998012900502 19980129 00502 EU 1998 1 29 REXA98009 1 19980111 A 7722 523347 ITT GAUGE SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A REXA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 112PX 10861020 340A025 DURING CLIMB, ITT FLUCTUATED ON RIGHT GAUGE ERRATICALLY. REMOVED AND REPLACED RIGHT HAND ITT GAUGE. OPS CHECK GOOD. ( X) 2 L 7 2 4T RT A52EU 1998012900503 19980129 00503 EU 1998 1 29 REXA98010 1 19980110 A 3020 NH2466807103 DUCT SAAB SF340 SF340A 7850100 EU LT ENGINE INOPERATIVE A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 108PX L169219 340A012 LEFT HAND INTAKE HEAT INOPERABLE. REMOVED AND REPLACED 4H INTAKE LOWER DUCT. TEST GOOD. OK FOR SERVICE. (X) 2 L 7 2 4T RT A52EU 1998012900504 19980129 00504 NE 1998 1 29 REXA98011 2 19980109 A 7261 OIL SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE REQUIRED SERVICE A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 344AM 340A030 ON TAXI, RIGHT HAND ENGINE OIL PRESSURE LIGHT CAME ON. RIGHT HAND ENGINE OIL LEVEL LOW, ADDED ONE QUART OF OIL. RUN-UP CHECKS GOOD. (X) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998012900505 19980129 00505 1998 1 29 REXA98012 4 19980110 A 3422 FLUX GATE SAAB SF340 340B 7860101 EU LEFT OUT OF ADJUST A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 360PX 340B220 IN CLIMB, AIRCRAFT HAD A 10 TO 15 DEGREE HEADING SPLIT. ADJUSTED LEFT HAND FLUX GATE. GROUND OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A52EU 1998012900506 19980129 00506 EU 1998 1 29 REXA98013 1 19980113 A 7603 CONDITION LEVER SAAB SF340 SF340A 7850100 EU RT ENGINE OUT OF ADJUST A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 327PX 340A059 BOTTOMING GOVERNOR IS ENGAGED BELOW MINIMUM GATE ON RIGHT HAND ENGINE. RIGGED RIGHT HAND CONDITION LEVER IAW AMM 76-10- 00. GROUND RUNS CHECKED GOOD. (X) 2 L 7 2 4T RT A52EU 1998012900507 19980129 00507 NM 1998 1 29 P2EA98003 1 19980112 A 2820 VALVE BOEING 737 737222 1384473 NM LT WING FAILED A P2EA O OTHER O OTHER AP APPROACH 1 CE 05 209US 19548 PIT - FLT 435 - EMERGENCY DECLARED, LANDING AT DESTINATION AIRPORT UNEVENTFUL, WITH CROSSFEED OPEN AND LEFT BOOST PUMPS OFF, FUEL CONTINUED TO BURN OUT OF THE LEFT WING TANK. REPLACED FUEL CROSSFEED VALVE PER MM 28-22-21. LEAK AND OPS CHE CK OK. RAN ENGINES AND ABLE TO FEED FROM LEFT OR RIGHT SIDE. (M) 2 L 7 2 4F A16WE 1998012900511 19980129 00511 NM 1998 1 29 TWAA9800401 1 19980107 A 3310 3188571013 LIGHT BASE BOEING 727 727231 1384079 NM COCKPIT SHORTED A TWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 54334 20461 STL - FLT 519 - DURING TAXI, SMOKE AND SPARKS EMITTED FROM THE WINDSHEAR ANNUNCIATOR INDICATOR MFG PN 318-8571-013. REP LACED SHORTED LIGHT BASE OF THE WINDSHEAR ANNUNCIATOR. OPERATIONAL CHECK NORMAL. CHECK-C 04. 08-12-97. JFK. (X) 2 L 7 3 4F A3WE 1998012900512 19980129 00512 NM 1998 1 29 USAA980006 1 19980110 A 5313 STRINGER BOEING 737 7374B7 1384702 NM BS 1040 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 784AU 19266 25023 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH WORN AREA BS 1040 PLUG 4 S26L STRINGER. INSTALLED DO UBLER, REPAIRED PER SRM 53-00-03. (X) 2 L 7 2 4F RT A16WE 1998012900516 19980129 00516 WP 1998 1 29 USAAD98003 1 19980104 A 2421 976J2526 GENERATOR DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 824US 49143 CLT - FLT 1754 - CLIMBING THROUGH 12,000 FT, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT R ETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND CSD. THE APU GENERATOR AND CONTROL UNIT WERE ALSO REPLACED. BOTH SYSTEMS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998012900517 19980129 00517 WP 1998 1 29 98ZZZX378 1 19980104 A 2424 947F9453 GCU DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 824US 49143 CLT - FL 1754 - CLIMBING THROUGH 12,000 FEET, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND THE APU GENERATOR CONTROL UNIT. TH E SYSTEMS THEN OPERATED NORMALLY. REF: OPERATOR CONTROL NR USAAD98003. 2 L 7 2 4F A6WE 1998012900518 19980129 00518 EU 1998 1 29 USAAF98001 1 19980101 A 2720 703852 RUDDER MANIFOLD FOKKER F28 F28MK0100 4990807 EU NR 2 HYD SYST FAILED A USAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 EA 19 880US 11331 PIT - FL 356 - EN ROUTE PIT/CAK, CREW RECEIVED THE NR 2 HYDRAULIC SYSTEM LOW QUANTITY WARNING. CREW PERFORMED NECESSARY PROCEDURES. FLIGHT RETURNED TO PIT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 RUDDER SYSTEM M ANIFOLD. (X) 2 L 7 2 4F RT 1998012900520 19980129 00520 NM 1998 1 29 USAASB98002 1 19980106 A 3350 AD20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 411US 23880 CLE - MAINTENANCE FOUND THE SEAT ROW EMERGENCY LIGHTS INOPERABLE AT ROWS 1 AND 2. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. REF: OPERATOR CONTROL NR 98ZZZX379. (X) 2 L 7 2 4F RT A16WE 1998012900521 19980129 00521 NM 1998 1 29 98ZZZX379 1 19980106 A 3350 20121 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 411US 23880 CLE - MAINTENANCE FOUND THE SEAT ROW EMERGENCY LIGHTS INOPERABLE AT ROWS 1 AND 2. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK GOOD. REF: OPERATOR CONTROL NR USAASB98002. 2 L 7 2 4F RT A16WE 1998012900522 19980129 00522 NM 1998 1 29 USAASB98007 1 19980110 A 5210 10604765 DOOR SEAL BOEING 737 737301 1384611 NM PASSENGER DOOR NOT SEATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 SDF - FLT 425 - AUTO-FAIL LIGHT ON PRESSURIZATION PANEL ILLUMINATED SHORTLY AFTER TAKEOFF. OUTFLOW VALVE SHOWED CLOSED. CREW COULD NOT PRESSURIZE AIRCRAFT IN STANDBY OR AUTO. FLIGHT RETURNED TO FIELD AT SDF AND LANDED WITHOUT FURTHER INC IDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT LEFT ENTRY DOOR SEAL TWISTED AND NOT SEATED PROPERLY. ADJ USTED AND SEATED SEAL. PRESSURIZED AIRCRAFT ON GROUND. OPS CHECK GOOD MER MM. (X) 2 L 7 2 4F RT A16WE 1998012900523 19980129 00523 NM 1998 1 29 USAA980004 1 19980110 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 784AU 19266 25023 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND .75 INCH CRACK BS 294.5 RBL 55 INCHES WL 209 FRAME. INSTALLED DOUBLER REPAIRED PER SRM 51-70-11 737-400. (X) 2 L 7 2 4F RT A16WE 1998012900524 19980129 00524 NM 1998 1 29 USAA980005 1 19980110 A 5311 FRAME BOEING 737 7374B7 1384702 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 784AU 19266 25023 INT - DURING 'Q-3' CHECK, VISUAL INSPECTION FOUND 50 INCHES OF CORROSION BS 986.5 LBL 44 RBL 46 FRAME. REMOVED UPPER FL ANGE AND INSTALLED REPLACEMENT PER TR 53-60-1. CORROSION TASK NR: C53-107-02. CORROSION LEVEL: 2. (X) 2 L 7 2 4F RT A16WE 1998012900539 19980129 00539 EU 1998 1 29 SABA980003 1 19980109 A 2160 7252C000 TEMP VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LEFT STUCK A SABA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 33 962AE 4863902 962 LEX - FLT 5214 - FLT FROM LEX TO CLT ON CLIMB-OUT, THE AIRCREW OBSERVED A SMELL AND SAID IT SMELLED LIKE PLASTIC BURNING . A FEW SECONDS LATER THE LEFT BLEED AIR LIGHT CAME ON AND WOULD NOT EXITNGUISH. SMOKE BEGAN TO FILL THE COCKPIT FROM THE CENTER CONSOLE. AIRCREW TURNED OFF THE LT FLOW PACK. SMELL AND SMOKE CLEARED THE COCKPIT. IN FLT EMERGENCY WAS DE CLARED. EMERGENCY PROCEDURES WERE USED. A/C RETURNED TO LEX WITH NO OTHER PROBLEMS. MX CREW WAS DEPLOYED FROM CLT TO LEX. MX FOUND THE TEMP CONTROL VALVE STUCK IN THE OPEN POSITION. LT BLEED AIR DEACTIVATED AND DEFERRED TOMSL NR 01998- 03C. A/C RETURNED TO CLT FOR REPAIR. MX REMOVED AND REPLACED LT TEMP CONTROL VALVE. SYSTEM RUN AND OPS CHECKED GOOD. 2 L 7 2 4T 3 T RT A56EU E3WE 1998012900540 19980129 00540 NM 1998 1 29 TAOA019806 1 19980112 A 3350 90052 BATTERY BASE BOEING 727 727227 1384078 NM L-2 DOOR SHORTED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 926TS VA5226 20774 FLT 6521 - OVERNIGHT L/S CHECK - L-2 DOOR EMERGENCY EXIT DOOR SIGN INOPERABLE. REPLACED BATTERY PACK BASE, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. 2 L 7 3 4F A3WE 1998012900541 19980129 00541 NM 1998 1 29 TAOA019807 1 19980113 A 3350 1000677 LIGHT BOEING 727 727254 138408L NM CABIN FAILED A TAOA K NONE L NO TEST CR CRUISE 1 EA 15 914TS 2019 20251 BOS/LGA - FLT 6060 - FORWARD LEFT OVERWING EMERGENCY LIGHT INOPERABLE. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK NORMA L PER MM CHAPTER 33-50. 2 L 7 3 4F A3WE 1998012900542 19980129 00542 NM 1998 1 29 TAOA019808 1 19980113 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM L-2 DOOR DISCHARGED A TAOA K NONE L NO TEST CR CRUISE 1 EA 15 919TS 22817 20447 LGA/BOS - FLT 6150 - L-2 DOOR EMERGENCY EXIT SIGN INOPERABLE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM CH APTER 33-50. 2 L 7 3 4F A3WE 1998012900545 19980129 00545 NM 1998 1 29 MASA98004 1 19980108 A 3350 PE2 BULB GRIMES 10005511 DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 62991 456 DURING TESTING OF AIRCRAFT EMERGENCY LIGHTS, NOTED THE OVERHEAD PORTABLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENA NCE REMOVED AND REPLACED THE BULB. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998012900546 19980129 00546 WP 1998 1 29 GTIA9800005 1 19980112 A 2560 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR FELL OFF A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 DTW - FLT 636 - GALLEY SERVICE DOOR SLIDE KEEPS FALLING OFF. RE-INSTALLED GALLEY SERVICE DOOR SLIDE IAW DC-9 MM 25-62-0 . OPS CHECK GOOD. RII INSPECTION PERFORMED. (X) 2 L 7 2 4F A6WE 1998012900547 19980129 00547 WP 1998 1 29 GTIA9800007 1 19980112 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 DTW - FLT 620 - CABIN EMERGENCY FLOOR LIGHTS HAVE SEVERAL BULBS OUT. RE-SECURED CANNON PLUG AT FORWARD BATTERY PACK. E MERGENCY LIGHTING (CABIN). OPS CHECK NORMAL PER DC-9 MM 33-53-0. (X) 2 L 7 2 4F A6WE 1998012900580 19980129 00580 NM 1998 1 29 AALA980002 1 19980101 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 320AA 22321 SFO - DURING MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H THROUGH 30H WOULD NOT ILLUMINATE. REPAIRED EMERGENCY E XIT LIGHT CHAFED WIRE AT SEAT ROW 28H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900581 19980129 00581 NM 1998 1 29 AALA980006 1 19980103 A 3350 0201820001 SIGN BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 SFO - DURING OVERNIGHT CHECK, FIRST CLASS GALLEY EMERGENCY EXIT SIGN FOUND BROKEN. REPLACED FIRST CLASS GALLEY EMERGENC Y EXIT SIGN BASE ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900582 19980129 00582 NM 1998 1 29 AALA980007 1 19980104 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383AN 26995 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 22HJ FOUND INOPERATIVE. RECONNECTED LOOSE EMERGENC Y EXIT LIGHT CONNECTOR AT PASSENGER SEAT 22HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900583 19980129 00583 NM 1998 1 29 AALA980008 1 19980102 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 27AB FOUND INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT 27AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900584 19980129 00584 WP 1998 1 29 AALA980009 1 19980102 A 3222 5920629513 STRUT PISTON DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 587AA CPI1004 53250 DFW - FLT 0607 - DURING TAKEOFF, UNABLE TO RETRACT NOSE GEAR. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. AI RCRAFT WAS NOT OVERWEIGHT. REPLACED NOSE GEAR STRUT PISTON. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998012900585 19980129 00585 WP 1998 1 29 AALA980011 1 19980126 A 3211 TRUNNION DOUG DC10 DC1030 3023501 WP RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION IN FORWARD LUG OF AFT TURNNION. REMOVED CORROSION BY BORING LUG TO 4.125 DIAMETER. INSTALLED OVE RSIZE BUSHING AND SHIM PER SRM 57-20-00. (M) 2 L 7 3 4F A22WE 1998012900586 19980129 00586 NM 1998 1 29 AALA980017 1 19980105 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 332AA 22331 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 26A/B FOUND INOPERATIVE. RECONNECTED LOOSE EMERGEN CY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 26A/B. SYSTEM FOUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900587 19980129 00587 NM 1998 1 29 AALA980018 1 19980105 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361AA 24042 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 32A/B FOUND INOPERATIVE. RECONNECTED LOOSE EMERGEN CY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 32A/B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900588 19980129 00588 NM 1998 1 29 AALA980019 1 19980105 A 3350 5635643 LIGHT SYMBOLIC BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324AA 22325 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT AFT RIGHT LAVATORY FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AT AFT RIGHT LAVATORY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900589 19980129 00589 NM 1998 1 29 AALA980020 1 19980105 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645AA 24603 DFW - DURING OVERNIGHT CHECK, FORWARD EMERGENCY EXIT FLOOR LIGHT FOUND INOPERATIVE. REPLACED LIGHT STRIP AT FORWARD EME RGENCY EXIT FLOOR. SYSTEM FOUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998012900590 19980129 00590 NM 1998 1 29 AALA980022 1 19980101 A 2421 IDG BOEING 767 767223 1385123 NM NR 1 ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION DE DESCENT 1 SW 07 322AA 22323 JFK - FLT 1786 - LEFT GENERATOR FAILED AFTER DESCENT FOR APPROACH. LEFT GENERATOR DRIVE LIGHT ILLUMINATED. DISCONNECTE D LEFT GENERATOR IAW PROCEDURE. STATUS - L IDG OIL TEMP. REMOVED AND REPLACED NR 1 ENGINE IDG PER MM. ACCOMPLISHED RU N-UP AND LEAK CHECK. ACCOMPLISHED DISCONNECT. ALL CHECKS OK. NO MESSAGE FOUND. 32224FBB1/0350.02JAN.JFK. (X) 2 L 7 2 4F RT A1NM 1998012900591 19980129 00591 NM 1998 1 29 AALA980023 1 19980103 A 2612 FIRE PANEL BOEING 767 767323 1385205 NM COCKPIT FAILED A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 389AA 27449 MIA - FLT 0946 - STATUS MESSAGE ENG OVHT LP 1. REPLACED RT ENGINE OVERHEAT LP 1 PER MM. ACCOMPLISHED ALL REQUIRED CHEC KS PER MM. ALL CHECKS OK. REMOVED MEL 01-40D-A AND CLEARED MIC SHEET. 38926242E/0848.03JAN.DFW. (X) 2 L 7 2 4F RT A1NM 1998012900592 19980129 00592 NM 1998 1 29 AALA980025 1 19980105 A 2421 IDG BOEING 767 767223 1385123 NM LT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 332AA 22331 BRU - FLT 0088 - EICAS LEFT GENERATOR DRIVE MESSAGE AT LIFT-OFF ACCOMPANIED WITH AN OVERHEAD GENERATOR DRIVE LIGHT. STE ADY INDICATIONS. DISCONNECTED LEFT GENERATOR DRIVE PER CHECKLIST. REMOVED AND REPLACED LEFT ENG IDG PER MM 20703. PER FORMED IDG. OPS CHECK AND LEAK CHECK ALL CHECKED GOOD. REMOVED PLACARD, CLEARED MIC. 33224F7C2/1419.05JAN.BRU. (X) 2 L 7 2 4F RT A1NM 1998012900593 19980129 00593 NM 1998 1 29 AALA980027 1 19980106 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321AA 22322 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEATS 22HJ, 25AB, AND 33HJ WERE FOUND INOPERABLE. REPLA CED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEATS 22HJ, 25AB, AND 33HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 2 4F RT A1NM 1998012900594 19980129 00594 WP 1998 1 29 AALA980028 1 19980106 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 463AA 49593 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 21DEF FOUND INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT CONNECTOR AT PASSENGER SEAT 21DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998012900595 19980129 00595 NM 1998 1 29 AALA980029 1 19980106 A 3350 0201820001 LIGHT BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321AA 22322 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT MID-RIGHT HAND GALLEY FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AT MID-RIGHT HAND GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900596 19980129 00596 NM 1998 1 29 AALA980030 1 19980106 A 3350 0201922001 SOCKET BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT SEAT 9AB FOUND INOPERATIVE. REPLACED SOCKET AT SEAT 9AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900597 19980129 00597 WP 1998 1 29 AALA980031 1 19980105 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 236AA 49251 DFW - DURING OVERNIGHT CHECK, NOSE LANDING GEAR GREEN LIGHT WOULD NOT ILLUMINATE WITH HANDLE DOWN. REPLACED NLG UPLOCK SENSOR. ACCOMPLISHED NLG RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998012900598 19980129 00598 WP 1998 1 29 AALA980032 1 19980106 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 249AA 49269 DFW - FLT 0405 - AFTER TAKEOFF BDL, NOSE LANDING GEAR RED LIGHT ILLUMINATED FOR APPROXIMATELY FIVE MINUTES AND THEN EXTI NGUISHED WITH NO OTHER ABNORMAL INDICATIONS. AIRCRAFT PROCEEDED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED NLG UPLOC K SENSOR. ACCOMPLISHED NLG RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998012900599 19980129 00599 NM 1998 1 29 AALA980033 1 19980107 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 369AA 25196 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 31AB FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LI GHT CONNECTOR AT PASSENGER SEAT 31AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900600 19980129 00600 NM 1998 1 29 AALA980034 1 19980107 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 628AA 24586 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND COACH WERE FOUND INOPERABLE. REP LACED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE BETWEEN FIRST CLASS AND COACH. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 2 4F RT A2NM 1998012900601 19980129 00601 NM 1998 1 29 AALA980035 1 19980107 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 628AA 24586 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHT FOUND INOPERATIVE. REPLACED LIGHT STRIP AT EMERGENCY EXIT FLOO R. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998012900602 19980129 00602 NM 1998 1 29 AALA980042 1 19980108 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385AM 27059 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEATS 39A/B AND 40A/B FOUND INOPERATIVE. REPLACED EMERG ENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 39A/B AND 40A/B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900603 19980129 00603 NM 1998 1 29 AALA980049 1 19980111 A 3350 P4010051 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 638AA 24596 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT SIDEWALL SIGN AT R2 FOUND INOPERATIVE. REPLACED FORWARD EXIT SIGN MODULE A T R2 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998012900604 19980129 00604 1998 1 29 AALA980094 4 19980109 A 3460 FMC BOEING 767 767223 1385123 NM RIGHT FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 313AA 22316 LHR - FLT 0095 - IN-FLIGHT, RIGHT FMC FAILED. REPLACED RT FMC AND RT CDU. PERFORMED CROSS-LOAD PER SIC 2900. ALL OPS AND INDICATIONS NOW NORMAL. 31334F8FF/1520.09JAN.LHR. (X) 2 L 7 2 4F RT A1NM 1998012900605 19980129 00605 NM 1998 1 29 AALA980095 1 19980110 A 2421 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 39365 24046 DFW - FLT 0049 - RIGHT GENERATOR DRIVE LIGHT ON AND EICAS RIGHT GENERATOR DRIVE DISCONNECTED RIGHT GENERATOR DRIVE. TRO UBLESHOT, FOUND OIL PRESSURE FAULTED. REPLACED RIGHT ENGINE IDG. ACCOMPLISHED CARD 4944. RAN ENGINE, LEAK CHECK OK. A PPROVED FOR SERVICE. 3652406CE/1506.10JAN.DFW. (X) 2 L 7 2 4F RT A1NM 1998012900606 19980129 00606 NM 1998 1 29 AALA980096 1 19980110 A 2421 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 383AN 26995 GIG - FLT 0905 - RIGHT GENERATOR DRIVE AND RIGHT GENERATOR OFF LIGHT AND EICAS MESSAGE. RIGHT GENERATOR DISCONNECTED FO R REMAINDER OF FLIGHT. REMOVED AND REPLACED RIGHT IDG PER MM 24-11-01-4-1, PAGES 401 THROUGH 413. OPS CHECK OK. RAN E NGINE PER MM. OPS CHECK OF RT IDG OF REMOVED PLACARD AND CLEARED MIC SHEET. RT IDG OK FOR SERVICE. (X) 2 L 7 2 4F RT A1NM 1998012900607 19980129 00607 NM 1998 1 29 AALA980097 1 19980112 A 3350 LAMP HOLDER BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 332AA 22331 LHR - DURING MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 31B WOULD NOT ILLUMINATE. RECONNECTED LAMP HOLDER AND RESECU RED WIRES AT SEAT ROW 31B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998012900608 19980129 00608 EU 1998 1 29 MALA975912 1 19980122 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 991XJ 091 DURING INSPECTION, OVERHEAD EMERGENCY LIGHT INOP AT SEAT 2A. MAINTENANCE RELAMPED OVERHEAD EMERGENCY LIGHT, OPS CHECK G OOD. 2 L 7 2 4T RT A52EU 1998012900609 19980129 00609 NM 1998 1 29 MALA975913 1 19980123 A 4950 APU DHAV DHC8 DHC8102 2809003 NM APU COMPT CONTAMINATED A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 827MA 331 DURING TAXI, SMOKE IN THE CABIN AND COCKPIT WITH ENGINE BLEEDS ON. CREW RETURNED TO THE GATE. MAINTENANCE INSPECTED AN D FOUND APU INGESTED DE-ICE FLUID. CLEANED AND DRIED SYSTEM, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998012900610 19980129 00610 EU 1998 1 29 MALA975914 1 19980124 A 3020 NH24668081 DUCT SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 76XJ 076 AFTER TAKEOFF, THE LEFT INTAKE HEAT LIGHT ILLUMINATED. COMPLETED QRH AND RETURN TO MSP. MAINTENANCE REPLACED UPPER DUC T AND IPD EXHAUST NOZZLE HEATER, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900611 19980129 00611 EU 1998 1 29 MALA975915 1 19980122 A 5610 7256100501 WINDSHIELD SAAB SF340 SF340A 7850100 EU RT COCKPIT CRACKED A MALA K NONE C F.O.D. CL CLIMB 1 GL 15 99XJ 099 THE RIGHT WINDSHIELD OUTER PANE CRACKED DUE TO BIRD STRIKE ON CLIMB. MAINTENANCE REPLACED THE RIGHT WINDSHIELD, ALL CHE CKS GOOD. 2 L 7 2 4T RT A52EU 1998012900612 19980129 00612 EU 1998 1 29 MALA975916 1 19980124 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119XJ 119 DURING INSPECTION, EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900613 19980129 00613 EU 1998 1 29 MALA975917 1 19980124 A 3350 7239410802 LIGHT SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, ONE FLOOR TRACK LIGHT INOP. MAINTENANCE REPLACED LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900614 19980129 00614 EU 1998 1 29 MALA975918 1 19980122 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 586MA 340B165 DURING INSPECTION, THE EMERGENCY LIGHT AT SEAT 4C FLOOR INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900615 19980129 00615 EU 1998 1 29 MALA975919 1 19980122 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU RT COCKPIT CRACKED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 586MA 340B165 DURING CLIMB, THE RIGHT WINDSHIELD CRACKED OUTER PANE. AIRCRAFT RETURNED TO BJI. MAINTENANCE REPLACED THE RIGHT WINDSH IELD, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900616 19980129 00616 EU 1998 1 29 MALA975920 1 19980126 A 2610 WIRE SAAB SF340 SF340A 7850100 EU RT TAILPIPE BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING TEST OF RIGHT TAILPIPE HOT LIGHT INOP. MAINTENANCE REPAIRED BROKEN WIRE INBOARD DETECT SENSOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900617 19980129 00617 EU 1998 1 29 MALA975921 1 19980124 A 5270 WARNING LIGHT SAAB SF340 340B 7860101 EU PAX DOOR ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 407XJ 340B407 DURING CLIMB, THE MAIN DOOR HANDLE LIGHT ILLUMINATED. CREW RETURNED TO ESC. MAINTENANCE DEFERRED PAX DOOR HANDLE WARNI NG SYSTEM PER MEL 52-70-1-2C. 2 L 7 2 4T RT A52EU 1998012900618 19980129 00618 EU 1998 1 29 MALA975922 1 19980123 A 2610 CONNECTOR SAAB SF340 340B 7860101 EU LT ENGINE LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 408XJ 408 DURING INSPECTION PERFORMED FIRE TEST, TAILPIPE HOT LIGHT STAYED ON. RESET AND TRIED AGAIN, FAILED. MAINTENANCE CLEANE D AND RESECURED CANNOM PLUG IN THE LEFT ENGINE COMPARTMENT, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998012900619 19980129 00619 NE 1998 1 29 CALA9800104 2 19980123 A 7261 800195 GARLOCK SEAL 705117K BOEING 747 747243B 1384830 NM PWA JT9 JT9D7F 52054 NE CSD LEAKING A CALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 33021 0943 20520 685729 THE NR 3 ENGINE OIL QUANTITY DECREASED TO ZERO WHILE EN ROUTE. THE NR 3 ENGINE WAS SHUTDOWN AND THE AIRCRAFT LANDED AT HNL WITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAKING FROM CSD DRIVE PAD. THE GARLOCK SEAL AND ALL OIL SEALS WERE REMOVE D AND REPLACED IAW MM 72-61-07, PAGE 401. THE NR 3 ENGINE WAS SERVICED WITH OIL AND THE ENGINE WAS RUN WITH NO LEAKS DE TECTED. 2 L 7 4 4F 4 F A20WE E20EA 1998012900620 19980129 00620 NM 1998 1 29 CALA9800105 1 19980124 A 5712 RIB BOEING 727 727227 1384078 NM WS 130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 2 INCH CRACK AT FASTENER IN RT WING RIB INBOARD OF NR 4 LEADING EDGE FLAP AT L/E STA 130. THE CRACKE D AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998012900621 19980129 00621 NM 1998 1 29 CALA9800106 1 19980125 A 3350 6104789 BATTERY PACK BOEING 737 737219 1384469 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10248 20344 INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 4 FORWARD. THE BATTERY PACK WAS REMOVED AND REPLACED. 2 L 7 2 4F A16WE 1998012900622 19980129 00622 WP 1998 1 29 CALA9800107 1 19980126 A 5530 ANGLE DOUG DC10 DC1030 3023501 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND A 1.2 INCH CRACK IN RT LOWER VERTICAL STABILIZER DRAG ANGLE AT FORWARD CENTER SPAR POSITION. THE ANGLE WAS REPAIRED IAW SRM 53-20-00, FIGURE 3. 2 L 7 3 4F A22WE 1998012900623 19980129 00623 NM 1998 1 29 9801376305 1 19980124 A 2760 CONTROL MECH BOEING 747 747451 1384940 NM SPOILER SYST OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 665US 23820 DURING TAKEOFF, RECEIVED A SPOILER CONFIGURATION TAKEOFF WARNING. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE. ADJUS TED THE SPEED BRAKE CONTROL SYSTEM AND REPLACED THE AUTO SPEED BRAKE ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998012900625 19980129 00625 WP 1998 1 29 9801429859 1 19980124 A 3222 STRUT DOUG DC9 DC951 3022051 WP NLG REQUIRED SERVICE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 768NC 47729 AFTER TAKEOFF, GROUND SHIFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE. AIRCRAFT RETURNED TO MEM AND LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE SERVICED NOSE STRUT, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998012900626 19980129 00626 WP 1998 1 29 9801439301 1 19980124 A 5350 TAIL CONE DOUG DC9 DC982 3022082 WP AFT FUSELAGE DEPLOYED A NWAA K NONE O OTHER LD LANDING 1 GL 01 301RC 48054 DURING LANDING ROLLOUT, THE AIRCRAFT EXPERIENCED AN INADVERTANT TAIL CONE DEPLOYMENT. MAINTENANCE REPLACED TAIL CONE AS SEMBLY AND SLIDE. 2 L 7 2 4F A6WE 1998012900627 19980129 00627 WP 1998 1 29 9801449102 1 19980123 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 92S 47064 DURING MAINTENANCE INSPECTION, FOUND EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1998012900628 19980129 00628 WP 1998 1 29 9801459178 1 19980124 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING MAINTENANCE INSPECTION, FOUND LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1998012900629 19980129 00629 WP 1998 1 29 9801469302 1 19980123 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302RC 48055 DURING MAINTENANCE INSPECTION, FOUND OVERHEAD LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900630 19980129 00630 WP 1998 1 29 9801479884 1 19980125 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 677MC 47756 DURING MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F RT A6WE 1998012900631 19980129 00631 WP 1998 1 29 9801489102 1 19980125 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 92S 47064 DURING MAINTENANCE INSPECTION, FOUND EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL C HECK OK. 2 L 7 2 4F A6WE 1998012900632 19980129 00632 WP 1998 1 29 9801499917 1 19980124 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 5 THRU 9 INOPERATIVE. REPLACED BATTERI ES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900633 19980129 00633 WP 1998 1 29 9801509908 1 19980124 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 958N 47254 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900634 19980129 00634 WP 1998 1 29 9801519908 1 19980124 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 958N 47254 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900635 19980129 00635 WP 1998 1 29 9801529903 1 19980123 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 953N 47083 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900636 19980129 00636 WP 1998 1 29 9801539989 1 19980125 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998012900637 19980129 00637 WP 1998 1 29 9801549301 1 19980124 A 5350 TAIL CONE DOUG DC9 DC982 3022082 WP AFT FUSELAGE FELL OFF A NWAA K NONE O OTHER LD LANDING 1 GL 01 301RC 48054 DURING LANDING ROLLOUT, TAIL CONE FELL OFF THE AIRCRAFT AND DEPLOYED SLIDE. MAINTENANCE REPLACED AND RIGGED THE SLIDE A ND TAIL CONE, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998012900638 19980129 00638 NM 1998 1 29 9801552292 1 19980123 A 3610 PNEUMATIC SW BOEING 727 727251 138408H NM NR 2 ENGINE FAILED A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 292US 21503 DURING TAKEOFF ROLL, AUTO PACK INDICATION ILLUMINATED. ABORTED TAKEOFF WITHOUT INCIDENT AND RETURNED TO THE GATE. REPL ACED NR 2 ENGINE PNEUMATIC SWITCH. 2 L 7 3 4F A3WE 1998012900639 19980129 00639 WP 1998 1 29 9801569752 1 19980126 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERA TIONAL CHECK OK. 2 L 7 2 4F A6WE 1998012900640 19980129 00640 WP 1998 1 29 9801579864 1 19980126 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 773NC 47775 DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERA TIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998012900641 19980129 00641 WP 1998 1 29 9801589884 1 19980126 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 984US 47383 DURING INSPECTION, THE EMERGENCY FLASHLIGHT AT LOCATION 1L WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998012900642 19980129 00642 NM 1998 1 29 98FDEA00054 1 19980126 A 5320 651841713 STIFFENER BOEING 727 72722 1384002 NM BS 303 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 CORROSION (C53-224-03-1/2) ON NOSE WHEEL WELL HORIZONTAL STIFFENER BS 303, RBL 8, WL 180. *S/D* REMOVED AND REPLACED HORIZONTAL STIFFENER BS 303, RBL 8, WL 180 IAW FEDEX DRAWING NR 65-18417.00. 2 L 7 3 4F A3WE 1998012900706 19980129 00706 NM 1998 1 29 W8PA980029 1 19980122 A 5320 ANGLE BOEING 737 737301 1384611 NM E/E COMPT CRACKED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 PAE- E AND E BAY RACK SUPPORT CRACKED. REMOVED CRACKED ANGLE, FABRICATED NEW SUPPORT ANGLE AND INSTALLED. 2 L 7 2 4F RT A16WE 1998012900707 19980129 00707 NM 1998 1 29 W8PA980030 1 19980122 A 5210 FITTING BOEING 737 737301 1384611 NM PAX DOOR GOUGED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 PAE- FWD ENTRY DOOR UPPER AND LOWER FWD CATCH ROLLER FITTINGS GOUGED. BLENDED UPPER FWD LATCH, PLACED LOWER FITTING. O UT OF LIMITS. 2 L 7 2 4F RT A16WE 1998012900708 19980129 00708 NM 1998 1 29 W8PA980031 1 19980122 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 500 CORRODED A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 PAE- FWD CARGO BAY, CORROSION ON FLR TO SIDEWALL SUPPORT, BS 500C-500C+3, LBL 25. REMOVED CORROSION, REMOVED AND REPAIR ED. FLOOR SUPPORT, OUT OF LIMITS. 2 L 7 2 4F RT A16WE 1998012900709 19980129 00709 NM 1998 1 29 W8PA980032 1 19980122 A 5530 ANGLE BOEING 737 737301 1384611 NM LT VERT STAB WORN A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 948WP 23259 PAE- LT VERTICAL STABILIZER TO BODY CLOSURE ANGLE IS CHAFED AND WORN THROUGH ON AFT END. REMOVED ANGLE, INSTALLED NEW A NGLE. 2 L 7 2 4F RT A16WE 1998012900710 19980129 00710 SO 1998 1 29 RAAA98E4002 1 19980128 A 5320 PRESS WEB LKHEED 188 188C 5262604 SO BS 173.3 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED, NR 1 CHECK FOUND FLT STATION PRESSURE DECK WEB CRACKED LBL 43 TO LBL 55 AT FS 173.3. REPAIRED PER SRM 53-1-5, FIG 1 AND 53-2-1, FIG 2 (SHEET 5) AND (SHEET 3). M-54 NR 51. 2 L 7 4 4T 4A22 1998012900711 19980129 00711 WP 1998 1 29 CALA9800108 1 19980126 A 2820 VENT BOX DOUG DC9 DC932 3022066 WP LT WING TIP LEAKING A CALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 09 18544 47219 THE CREW OBSERVED FUEL LEAKING FROM LT WING OUTBOARD OF AILERON WHILE EN ROUTE. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LEAKING AT LT WING TIP ON FORWARD SPAR BY VENT BOX. THE VENT BOX AN D AREA WERE RESEALED IAW SRM 51-23-00. LEAK CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998012900712 19980129 00712 NM 1998 1 29 CALA9800109 1 19980127 A 5330 SKIN BOEING 727 727243 138408D NM BS 1030 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1030 BETWEEN STRINGERS 20-21L. A REPAIR WAS FABRICATED AND INSTALLED IAW S RM 53-30-3 AND 51-10-6. 2 L 7 3 4F RT A3WE 1998012900713 19980129 00713 NM 1998 1 29 CALA9800110 1 19980127 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 616-660 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND RT FLOOR SUPPORT IN FORWARD BAGGAGE BIN CORRODED FROM DTA 616 TO 660. THE FLOOR SUPPORT WAS REMOVED AN D A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F RT A3WE 1998012900714 19980129 00714 NM 1998 1 29 CALA9800111 1 19980127 A 5320 ANGLE BOEING 727 727243 138408D NM BS 616 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND Z-ANGLE CORRODED AT STA 616 ABOVE STRINGER 26R IN FORWARD BAGGAGE BIN. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F RT A3WE 1998012900715 19980129 00715 NM 1998 1 29 CALA9800112 1 19980127 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND FLOORBEAM CORRODED ON AND AROUND NUT PLATES IN E AND E COMPARTMENT UNDER GALLEY AT STA 380. THE CORROD ED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-4, AND 51-10-1. 2 L 7 3 4F RT A3WE 1998012900716 19980129 00716 NM 1998 1 29 CALA9800113 1 19980127 A 5730 SKIN BOEING 727 727243 138408D NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A .625 INCH CRACK IN LT WING UPPER FIXED LEADING EDGE SKIN WHERE NR 3 SLAT OUTBOARD HOOK ATTACHES. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLER, BACK STRAP, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2. 2 L 7 3 4F RT A3WE 1998012900717 19980129 00717 NM 1998 1 29 CALA9800114 1 19980127 A 5720 ANGLE BOEING 727 727243 138408D NM WS 130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A 6 INCH CRACK AT FASTENERS IN SUPPORT ANGLE INSIDE LT WING INBOARD LEADING EDGE AREA AFT OF NR 1 LEADI NG EDGE FLAP INBOARD END AT L/E STA 130. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51- 30-2 AND 51-10-1. 2 L 7 3 4F RT A3WE 1998012900718 19980129 00718 NM 1998 1 29 CALA9800115 1 19980127 A 5754 SKIN BOEING 727 727243 138408D NM NR 4 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A .375 INCH CRACK IN LT WING NR 4 SLAT LOWER SKIN JUST OUTBOARD OF INBOARD TRACK AREA. THE CRACKED ARE A WAS BLENDED OUT. A PATCH REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-50-1, 51-10-2, AND 57-50-3. 2 L 7 3 4F RT A3WE 1998012900719 19980129 00719 NM 1998 1 29 CALA9800116 1 19980127 A 5720 ANGLE BOEING 727 727243 138408D NM WING RIB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A 2 INCH CRACK THROUGH TWO FASTENER HOLES OF RIB SUPPORT ANGLE AT WING LEADING EDGE SLAT STA 0. THE RI B SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998012900720 19980129 00720 NM 1998 1 29 CALA9800117 1 19980127 A 5713 STRINGER BOEING 727 727243 138408D NM WS 656.50 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A .5 INCH CRACK IN VENT BOX STRINGER INSIDE LT WING TANK ACCESS 7217, WS 656.50. A REPAIR WAS INSTALLE D IAW EA 5712-01050. 2 L 7 3 4F RT A3WE 1998012900721 19980129 00721 NM 1998 1 29 CALA9800118 1 19980127 A 5730 SKIN BOEING 727 727243 138408D NM LT WING TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A .25 INCH CRACK IN LT WING TRAILING EDGE UPPER SKIN AT NR 3 SPOILER SECOND CUTOUT FROM INBOARD HINGE. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-30-2. 2 L 7 3 4F RT A3WE 1998012900722 19980129 00722 NM 1998 1 29 CALA9800119 1 19980127 A 5730 SKIN BOEING 727 727243 138408D NM LT WING TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A .1875 INCH CRACK IN LT WING TRAILING EDGE UPPER SKIN AT NR 3 SPOILER THIRD CUTOUT FROM INBOARD HINGE. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2. 2 L 7 3 4F RT A3WE 1998012900723 19980129 00723 NM 1998 1 29 CALA9800120 1 19980127 A 2782 BRACKET BOEING 727 727243 138408D NM NR 1 SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A 3 INCH CRACK IN INBOARD MOUNT BRACKET WHERE NR 1 SLAT ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F RT A3WE 1998012900724 19980129 00724 NM 1998 1 29 CALA9800121 1 19980127 A 5320 ANGLE BOEING 727 727243 138408D NM BS 1273 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A 1 INCH CRACK IN FORWARD SUPPORT ANGLE OF AFT AIRSTAIRS RT SIDE STA 1273 (TORQUE BOX). ALSO, A 1 INCH CRACK WAS FOUND IN UPPER ANGLE OF AFT SIDE OF BULKHEAD IN AFT AIRSTAIR AREA ON RT SIDE AT STA 1273. NEW ANGLES WERE FA BRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998012900725 19980129 00725 NM 1998 1 29 CALA9800122 1 19980127 A 5320 BRACKET BOEING 727 727243 138408D NM BS 1263 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A 1 INCH CRACK ON AFT SIDE OF AFT AIRSTAIRS ACTUATOR ATTACH BULKHEAD SUPPORT BRACKET AT STA 1263. A NE W BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998012900726 19980129 00726 NM 1998 1 29 CALA9800123 1 19980127 A 5320 ANGLE BOEING 727 727243 138408D NM BS 1263 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A 1.5 INCH CRACK IN AFT STAIRS ACTUATOR ATTACH ANGLES AT STA 1263 INSIDE RT TORQUE BULKHEAD. NEW ANGLE S WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F RT A3WE 1998012900727 19980129 00727 NM 1998 1 29 CALA9800124 1 19980127 A 3350 900835A BATTERY PACK GRIMES BOEING 727 727243 138408D NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 578PE 21661 THE EMERGENCY PATH LIGHTING AT FIRST CLASS SECTION AND ROWS 17 TO 22 FAILED CAPACITANCE TEST. TWO BATTERY PACKS WERE REM OVED AND REPLACED. 2 L 7 3 4F RT A3WE 1998012900728 19980129 00728 NM 1998 1 29 CALA9800125 1 19980127 A 3350 S106 BATTERY PACK MARATHON BOEING 727 727243 138408D NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 578PE 21661 THE EMERGENCY LIGHTING AT MID CABIN CEILING EXIT LIGHT, COCKPIT DOOR EXIT LIGHT, AND L-1 AND R-1 LOWER EXIT LIGHTS FAILE D CAPACITANCE TEST. THE BATTERY PACK WAS REMOVED AND REPLACED. 2 L 7 3 4F RT A3WE 1998012900729 19980129 00729 NM 1998 1 29 9801596613 1 19980125 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT END FITTINGS FOR STR 49R TO 51R AT FS 2360. REPLACED FITTINGS PER BOE ING DRAWING 65B02634. 2 L 7 4 4F A20WE 1998012900730 19980129 00730 NM 1998 1 29 9801606613 1 19980125 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING PERIODIC CHECK, FOUND CORROSION ON THE FORWARD END FITTINGS FOR STR 46R, 50R, AND 51R AT FS 2360. REPLACED FITTI NGS PER BOEING DRAWING 65B02634. 2 L 7 4 4F A20WE 1998012900731 19980129 00731 NM 1998 1 29 9801616613 1 19980125 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING PERIODIC CHECK, FOUND CORROSION ON THE FORWARD END FITTINGS FOR STR 48L TO 51L AT FS 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02634. 2 L 7 4 4F A20WE 1998012900732 19980129 00732 NM 1998 1 29 9801626613 1 19980125 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT END FITTINGS FOR STR 48L, 49L, 50L, AND 51L AT FS 2360. REPLACED FITT INGS PER BOEING DRAWING 65B02634. 2 L 7 4 4F A20WE 1998012900733 19980129 00733 NM 1998 1 29 9801636718 1 19980123 A 5320 FITTING BOEING 747 747251F 1384898 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 38L AND 40L AT FS 2360. REPLACED FITTINGS (P/N 65B04370- 45) PER BOEING DRAWING 65B04160. 2 L 7 4 4F A20WE 1998012900734 19980129 00734 NM 1998 1 29 9801646718 1 19980126 A 5320 FITTING BOEING 747 747251F 1384898 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 38R AND 40R AT FS 2360. REPLACED FITTINGS (P/N 65B04370- 46) PER BOEING DRAWING 65B04160. 2 L 7 4 4F A20WE 1998012900735 19980129 00735 NM 1998 1 29 9801656718 1 19980123 A 5320 FITTING BOEING 747 747251F 1384898 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 42R, 44R, 46R, 48R, 49R, 50R, AND 51R AT FS 2360. REPLAC ED FITTINGS (P/N 65B04370-8) PER BOEING DRAWING 65B04161. 2 L 7 4 4F A20WE 1998012900736 19980129 00736 NM 1998 1 29 9801666718 1 19980123 A 5320 FITTING BOEING 747 747251F 1384898 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR STR 42L, 44L, 46L, 48L, 49L, 50L, AND 51L AT FS 2360. REPL ACED FITTINGS (P/N 65B04370-7) PER BOEING DRAWING 65B04161. 2 L 7 4 4F A20WE 1998012900737 19980129 00737 SO 1998 1 29 COMA9810030 1 19980126 A 3150 80055711 AURAL WARN UNIT EMB 120 EMB120RT SO E/E COMPT LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 263CA 12813 8 120255 TAKEOFF TRIM AURAL WARNING DURING TAKEOFF. SECURED LOOSE AURAL WARNING UNIT IN RACK. 2 L 7 2 4T RT A31SO 1998012900738 19980129 00738 SO 1998 1 29 COMA9810031 1 19980124 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 259CA 2198 63 120252 EMERGENCY EXIT SIGNS AT ROW 5 ARE INOP. REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4T RT A31SO 1998012900739 19980129 00739 SO 1998 1 29 COMA9810032 1 19980124 A 3350 1013073 BULB EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 267CA 120259 FLOOR EMERGENCY LIGHT AT GALLEY AREA IS INOP. REPLACED BULB. 2 L 7 2 4T RT A31SO 1998012900740 19980129 00740 EA 1998 1 29 COMA9860024 1 19980125 A 3222 16050101 STRUT CNDAIR CL600 CL6002B19 EA NLG LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 933CA 7040 NOSE LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. RESEALED AND RESERVICED NLG SHOCK STRUT. 2 L 7 2 4F RT A21EA 1998012900741 19980129 00741 EA 1998 1 29 COMA9860025 1 19980126 A 2750 601R930043 CONTROL LEVER CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 977CA 970 7157 AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. REPLACED FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 1998012900742 19980129 00742 EA 1998 1 29 COMA9860026 1 19980126 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 949CA 7080 CABIN DOOR OUTER HANDLE CAUTION MESSAGE ON EICAS. INSPECTED DOOR MECHANISM AND FOUND NO DEFECTS. DEFERRED DOOR WARNING SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 1998012900743 19980129 00743 NM 1998 1 29 SWAA980060 1 19980122 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 28SW 21339 DURING WALKAROUND CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M . 2 L 7 2 4F A16WE 1998012900744 19980129 00744 NM 1998 1 29 SWAA980061 1 19980122 A 3350 613211 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEIN G M/M. 2 L 7 2 4F A16WE 1998012900745 19980129 00745 NM 1998 1 29 SWAA980062 1 19980122 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 67SW 22356 DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEI NG M/M. 2 L 7 2 4F A16WE 1998012900746 19980129 00746 NM 1998 1 29 SWAA980063 1 19980121 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 807 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 807, LBL 27. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900747 19980129 00747 NM 1998 1 29 SWAA980064 1 19980121 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 299 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 299, LBL 11. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900748 19980129 00748 NM 1998 1 29 SWAA980065 1 19980121 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1140 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND VERTICAL STRAP CRACKED AT BS 1140, ABOVE S12L. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900749 19980129 00749 NM 1998 1 29 SWAA980066 1 19980121 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1140 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND HORIZONTAL STRAP CRACKED AT BS 1140, ABOVE S12R. REPLACED DAMAGED SECTION PER BOEING SR M. 2 L 7 2 4F A16WE 1998012900750 19980129 00750 NM 1998 1 29 SWAA980067 1 19980121 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 522 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER 16R DAMAGED AT BS 522. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900751 19980129 00751 NM 1998 1 29 SWAA980068 1 19980121 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 198 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND COCKPIT WINDOW POST SKIN LIGHTNING STRIKE DAMAGED AT BS 198, WL 253. RESKINNED POST PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900752 19980129 00752 NM 1998 1 29 SWAA980069 1 19980121 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 287 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 287 2 ABOVE S18R, AND AT BS 307, AT RBL 1.75. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1998012900753 19980129 00753 NM 1998 1 29 SWAA980070 1 19980121 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 596 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER S16R CRACKED AT BS 596. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900755 19980129 00755 NM 1998 1 29 SWAA980072 1 19980121 A 5320 WEB BOEING 737 7372H4 138448C NM BS 710 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 710. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900756 19980129 00756 NM 1998 1 29 SWAA980073 1 19980121 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 289.5 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND SKIN GOUGED AT FWD SERVICE DOOR HINGE CUTOUT AT BS 289.5, AND AT BS 358, BETWEEN S4 AND 5L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900757 19980129 00757 NM 1998 1 29 SWAA980074 1 19980121 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 350 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER CORRODED AT BS 350, S25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900758 19980129 00758 NM 1998 1 29 SWAA980075 1 19980121 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, S20R. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900759 19980129 00759 NM 1998 1 29 SWAA980076 1 19980121 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT S27L AND R, BS 907. REPLACED DAMAGED SECTION PER BOEING SRM . 2 L 7 2 4F A16WE 1998012900760 19980129 00760 NM 1998 1 29 SWAA980077 1 19980121 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 5, LBL 8 - LBL 16, AND RBL 1- 2. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1998012900761 19980129 00761 NM 1998 1 29 SWAA980078 1 19980121 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 500 HOLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND AN OBLONG HOLE IN LOWER ROW OF LAP JOINT, BS 500+2, AT S14L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900762 19980129 00762 NM 1998 1 29 SWAA980079 1 19980121 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 1011, S4R AND 988, S4R, AT BS 491, S14R, AT BS 727+11, S4L, A T BS 727B+1, S4L, AT BS 767+4 AT S4L, AT BS 797+4, S4L, AT BS 870 TO 875, S24R, AND AT BS 932, AT S4R. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1998012900763 19980129 00763 NM 1998 1 29 SWAA980080 1 19980121 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 908-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN LAP CORROSION AT BS 908 TO 1016 AT S4L. REPAIRED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998012900764 19980129 00764 NM 1998 1 29 SWAA980081 1 19980121 A 5320 CHANNEL BOEING 737 7372H4 138448C NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 500B, S16R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998012900765 19980129 00765 NM 1998 1 29 SWAA980082 1 19980121 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGED WITH A HOLE AT BS 500B+13, S16L. REPLACED DAMAGED SECTION PER BOEING S RM. 2 L 7 2 4F A16WE 1998012900766 19980129 00766 NM 1998 1 29 SWAA980083 1 19980117 A 7830 141225 ISOLATION VALVE BOEING 737 7372H4 138448C NM TR SYST FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 23SW 21338 RETURNED TO DAL DUE TO THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATING. MADE AN UNEVENTFUL LANDING. REPLACED ISOLAT ION VALVE PER BOEING M/M. 2 L 7 2 4F A16WE 1998012900767 19980129 00767 NM 1998 1 29 SWAA980084 1 19980117 A 3231 MECHANISM BOEING 737 7373H4 1384600 NM NLG/LT MLG DOOR OUT OF ADJUST A A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 390SW 26593 AFTER TAKEOFF, CREW REPORTED A VERY PRONOUNCED SIDE TO SIDE VIBRATION, YAW DAMPER WAS THEN TURNED OFF, NO HELP. DIVERTE D TO PHX AND MADE AN UNEVENTFUL LANDING. REPLACED RUDDER PCU AND YAW DAMPER COUPLING AS A PRECAUTION PER BOEING M/M. A FTER FURTHER TROUBLESHOOTING AND TEST FLIGHTS, DURING GROUND GEAR RETRACTION TEST, FOUND NOSE GEAR AND LEFT MAIN GEAR DO ORS OUT OF ADJUSTMENT. 2 L 7 2 4F RT A16WE 1998012900768 19980129 00768 NM 1998 1 29 UPS98225549 1 19980121 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM DOORSTOP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, DOOR STOP INTERCOSTAL FOUND CRACKED. INTERCOSTAL FABRICATED FROM 7075-0, 0.050 INCH THICK AND INSTAL LED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012900769 19980129 00769 NM 1998 1 29 UPS98225550 1 19980110 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, 2 CRACKS FOUND AROUND TOP FASTENER HOLES IN FRAME ANGLE BS 880 LT AT STRINGER 15. REPAIRED IAW SRM 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 1998012900770 19980129 00770 NM 1998 1 29 UPS98225552 1 19980122 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 740 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, STRINGER END FOUND DAMAGED ON REMOVAL TO AID BS 740 FITTING REPLACEMENT, DUE TO INCORRECT FITMENT INT O STRINGER 16R AT BS 740. STRINGER END AND STRINGER SECTION BETWEEN BS 740 AND 760 REPLACED IAW DRG NR 65C13724. 2 L 7 3 4F A3WE 1998012900771 19980129 00771 NM 1998 1 29 UPS98225554 1 19980121 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, LOWER FWD CARGO COMPARTMENT SHEAR TIE AT FRAME 540 ABOVE STRINGER 18L IS CRACKED. SHEAR TIE REPAIRED IAW SRM 51-40-03 FIGURE 1. 2 L 7 3 4F A3WE 1998012900772 19980129 00772 NM 1998 1 29 UPS98225555 1 19980121 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, LOWER FWD CARGO COMPARTMENT STRINGER 19L BETWEEN BS 580 AND 600 IS CRACKED. STRINGER REPAIRED IAW SR M 53-10-3. 2 L 7 3 4F A3WE 1998012900773 19980129 00773 NM 1998 1 29 UPS98225556 1 19980121 A 5320 WEB BOEING 727 72722C 138400F NM BS 220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CORROSION ON WEB OF AFT LT CORNER OF LOWER FORWARD NOSE CUTOUT, BS 220 APPROX, WL 156 APPROX. WEB RE PLACED IAW SRM 57-30-2. 2 L 7 3 4F A3WE 1998012900774 19980129 00774 NM 1998 1 29 UPS98225561 1 19980121 A 5320 DOOR STOP BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, LOWER AFT CARGO DOOR, NR 1 FWD STRUCTURAL STOP CRACKED. STOP REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012900775 19980129 00775 NM 1998 1 29 UPS98225563 1 19980121 A 5753 FLAP CARRIAGE BOEING 727 72722C 138400F NM NR 7 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 7 FLAP CARRIAGE HAS CORROSION INSIDE SPINDLE BARE AND AROUND LARGE BEARING SEAT. NR 7 FLAP CARRIA GE REPLACED IAW OHM 57-52-11 AND 27-51-13. 2 L 7 3 4F A3WE 1998012900776 19980129 00776 NM 1998 1 29 UPS98225564 1 19980121 A 5753 FLAP CARRIAGE BOEING 727 72722C 138400F NM NR 8 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 8 FLAP CARRIAGE IS CORRODED INSIDE SPINDLE BARE AND AROUND LARGE BEARING SEAT AREA. NR 8 FLAP CAR RIAGE REPLACED IAW OHM 57-52-11 AND MM 27-51-13. 2 L 7 3 4F A3WE 1998012900777 19980129 00777 NM 1998 1 29 UPS98225566 1 19980116 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, TWO CRACKS DISCOVERED AT TOP FASTENER HOLES IN FRAME ANGLE BS 920 LT AT STRINGER 15. REPAIR CARRIED OUT IAW SRM 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 1998012900778 19980129 00778 NM 1998 1 29 UPS98225567 1 19980116 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 900 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, TWO CRACKS DISCOVERED AT TOP FASTENER HOLES IN FRAME ANGLE BS 900 LT AT STRINGER 15. REPAIR CARRIED OUT IAW SRM 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 1998012900779 19980129 00779 NM 1998 1 29 UPS98225570 1 19980116 A 5730 SKIN BOEING 727 72722C 138400F NM WS 105 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CRACK ON INNER SKIN L/E STN 105 (RIGHT HAND WING LEADING EDGE). DAMAGE REPAIRED IAW SRM 57-30-4. 2 L 7 3 4F A3WE 1998012900780 19980129 00780 NM 1998 1 29 UPS98225574 1 19980119 A 5347 654197736 SEAT TRACK BOEING 727 72722C 138400F NM BS 344-360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, SHORT SECTION OF SEAT TRACK BETWEEN BS 344 AND BS 360 AT RBL 62 IS CRACKED. SECTION OF SEAT RAIL REP LACED IAW IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012900781 19980129 00781 NM 1998 1 29 UPS98225576 1 19980118 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 735 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CORROSION ON STRINGER 21R BS 735. STRINGER REPAIR CARRIED IAW SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1998012900782 19980129 00782 NM 1998 1 29 UPS98225577 1 19980121 A 5320 CLEAT BOEING 727 72722C 138400F NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CRACKED CLEAT BS 1010, STRINGER 3L. REPLACED STRINEGR CLIP IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998012900783 19980129 00783 NM 1998 1 29 UPS98225578 1 19980119 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, SEVERAL AREAS OF CORROSION ON UPPER CHORD OF FLOORBEAM, BS 344 BL 0 TO LBL 50. ALSO, EXISTING SPLICE FROM LBL 54 TO RBL 16. NEW UPPER CHORD OF BS 344 FLOORBEAM REPLACED IAW SRM 51-30-02 AND DRAWING 65-16316. 2 L 7 3 4F A3WE 1998012900784 19980129 00784 NM 1998 1 29 UPS98225579 1 19980119 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CORROSION IN FLOORBEAM UPPER CHORD AT BS 312 LBL 46 AT EXISTING BLENDOUT. AREA REPAIRED IAW SRM 53-1 0-8. 2 L 7 3 4F A3WE 1998012900785 19980129 00785 NM 1998 1 29 UPS98225580 1 19980118 A 5741 69139017 BOTTLE PIN BOEING 727 72722C 138400F NM LT WING/FUS PITTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, LT REAR SPAR BOTTLE PIN HAS WEAR AND LIGHT PITTING. LT AFT BOTTLE PIN REPLACED IAW MM 57-41-01. 2 L 7 3 4F A3WE 1998012900786 19980129 00786 NM 1998 1 29 UPS98225581 1 19980118 A 5741 65139017 BOTTLE PIN BOEING 727 72722C 138400F NM BS 870 PITTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, RIGHT HAND REAR BOTTLE PIN HAS WEAR AND LIGHT PITTING. RIGHT HAND AFT BOTTLE PIN REPLACED IAW MM 57- 41-01. 2 L 7 3 4F A3WE 1998012900787 19980129 00787 WP 1998 1 29 UPS98825546 1 19980103 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FS 450 LONG 34L TO 34R FINGER DOUBLER CRACKED AND CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLA CEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5755271. 2 L 7 4 4F RT 4A25 1998012900788 19980129 00788 WP 1998 1 29 UPS98825547 1 19980109 A 5320 FLOOR PAN DOUG DC8 DC873F 302199F WP BS 1740-1750 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, MAIN CABIN FLOOR PAN AT FS 1740 TO 1750 LBL 12 TO LBL 20 CORRODED BEYOND LIMITS. REMOVED, FABRICATED , AND INSTALLED REPLACEMENT IAW SRM 51-1-21 AND DWG 5755032. 2 L 7 4 4F RT 4A25 1998012900790 19980129 00790 WP 1998 1 29 UPS98825558 1 19980104 A 5210 DOOR WEB DOUG DC8 DC873F 302199F WP BS 70 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FWD MAIN ENTRY DOOR WEB AT FS 70 STR-17L IS CRACKED 2 PLCS. REMOVED, FABRICATED, AND INSTALLED REPLA CEMENT WEB IAW SRM 51-1-21 AND DWG 5597646. 2 L 7 4 4F RT 4A25 1998012900791 19980129 00791 WP 1998 1 29 UPS98825559 1 19980102 A 5330 SKIN DOUG DC8 DC873F 302199F WP PAX DOORWAY CRACK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, CRACK IN SKIN FWD LOWER CORNER OF AFT ENTRY DOOR. REPAIRED IAW UPS EO DC8-5330-9985-A. 2 L 7 4 4F RT 4A25 1998012900792 19980129 00792 WP 1998 1 29 UPS98825560 1 19980105 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FLOORBEAM FS 960 LBL 60 FWD UPPER FLANGE EXFOLIATED. REPAIRED IAW DHC SK-852-159. 2 L 7 4 4F RT 4A25 1998012900793 19980129 00793 WP 1998 1 29 UPS98825582 1 19980114 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 781-798 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, SEAT TRACK CORRODED BEYOND LIMITS AT FS 781 AND 798. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-7-2, 53-2-3, AND 51-1-21. 2 L 7 4 4F RT 4A25 1998012900794 19980129 00794 EU 1998 1 29 WWMA9800015 1 19980126 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 348SB 340B348 CREW FOUND ALL EMERGENCY LIGHTS WOULD NOT TEST DURING PREFLIGHT. MAINTENANCE REPLACED ALL 5 EMERGENCY BATTERY PACKS AT POSITIONS 20LN, 21LN 22LN, 23LN AND 24LN. 2 L 7 2 4T RT A52EU 1998012900795 19980129 00795 EU 1998 1 29 WWMA9800014 1 19980123 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 334AE 340B334 DURING PREFLIGHT, CREW FOUND THE EMERGENCY EXIT SIGN ABOVE SEAT 8A BROKEN. REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4T RT A52EU 1998012900796 19980129 00796 EU 1998 1 29 QXEA9800047 1 19980126 A 3350 MGG1280 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 GEG - EXIT SIGN LIGHT AT ENTRY DOOR INOP. RELAMPED, OPERATIONAL CHECK IS GOOD. 2 L 7 2 4F RT A20EU 1998012900797 19980129 00797 EU 1998 1 29 QXEA9800048 1 19980127 A 3350 5515900004 PRINTED CIRCUIT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 SEA - CEILING EXIT SIGN RIGHT ARROW ON AFT SIDE DOES NOT ILLUMINATE. THE EMERGENCY EXIT SIGN CIRCUIT BOARD ASSY WAS REP LACED. AN OPERATIONAL CHECK OF THE LIGHTS INDICATES NORMAL OPERATION. 2 L 7 2 4F RT A20EU 1998012900798 19980129 00798 WP 1998 1 29 98FDEA00055 1 19980122 A 5531 SPAR DOUG DC10 DC1010F 3022111 WP VERT STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 051FE 47805 UPPER VERT STAB REAR SPAR HAS TWO CRACKS AT LT O/B HI-LOK HOLE, .75 INCH LONG GOING OUT OF THE HI-LOK HOLE AND A .625 IN CH LONG GOING TANGENT WITH ANGLE RADIUS. CRACKED BASE ANGLE ON CONDITION II PER EO 8-5530-7-4303. REMOVED CRACKED ANGL E, INSTALLED NEW ANGLE PER EO 8-5530-7-4303. 2 L 7 3 4F A22WE 1998012900799 19980129 00799 WP 1998 1 29 ABXA9800041 1 19980125 A 7931 M057281 INDICATOR DOUG DC8 DC863F 302198F WP NR 3 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 828AX 371 45999 NR 3 ENGINE OIL PRESSURE FLUCTUATED BETWEEN 36 AND 45 PSI. SHUT DOWN NR 3 IAW DC8 ENGINE SECURING CHECKLIST. REPLACED NR 3 ENGINE OIL PRESSURE INDICATOR IAW DC8 MM 79-32-0, OPS CHECKED NORMAL. 2 L 7 4 4F 4A25 1998012900800 19980129 00800 WP 1998 1 29 ABXA9800042 1 19980127 A 3350 5708458503 BATTERY DOUG DC8 DC862 3021970 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 804AX 45987 DURING PREFLIGHT, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHTS BATTERY PACK. 2 L 7 4 4F 4A25 1998012900801 19980129 00801 WP 1998 1 29 MWEA98077 1 19980121 A 5754 SLAT DOUG DC9 DC932 3022066 WP NR 5 LE SLAT DENTED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 501ME 47132 THE NR 5 RT SLAT LEADING EDGE HAS 3 DENTS OUT OF SERVICEABLE LIMITS. MTC INSTALLED REPAIR IAW TEL-X ISC-MIS-005/DC/RBH. 2 L 7 2 4F A6WE 1998012900802 19980129 00802 WP 1998 1 29 MWEA98078 1 19980105 A 3350 6011777 BATTERY PACK DOUG DC9 DC914 3022034 WP LT NACELLE DEFECTIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 600ME 45725 DURING TRANSIT CHECK, FOUND LT NACELLE EMERGENCY BATTERY PACK INOP. MTC REMOVED AND REPLACED LT EMERGENCY BATTERY POWER SUPPLY. 2 L 7 2 4F A6WE 1998012900803 19980129 00803 WP 1998 1 29 MWEA98079 1 19980125 A 3350 100865 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 600ME 45725 DURING TRANSIT CHECK, FOUND AFT EMERGENCY TRACK LIGHTING INOP. MTC REMOVED AND REPLACED BATTERY PACK AND SEVERAL LIGHT SOCKETS IN AFT ACCESSORY CAT WALK HARNESS. 2 L 7 2 4F A6WE 1998012900804 19980129 00804 WP 1998 1 29 MWEA98091 1 19980128 A 5311 991961750IN FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND MAIN FRAME AT FS 699 FOUND CRACKED IN WEB BETWEEN PTC AND PT. F-PT.E. REMOVED CRACKED FRAME AND INSTALLED SER VICEABLE FRAME IAW DC9 SERVICE BULLETIN 53-131. 2 L 7 2 4F A6WE 1998012900805 19980129 00805 WP 1998 1 29 MWEA98092 1 19980128 A 5311 9919617502N FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 MAIN FRAME AT FS 699 WAS FOUND CRACKED. REMOVED CRACKED FRAME AND INSTALLED SERVCABLE FRAME IAW DC9 SERV BULLETIN 53-13 1. 2 L 7 2 4F A6WE 1998012900806 19980129 00806 WP 1998 1 29 MWEA98093 1 19980128 A 5315 2777896 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 PREV REPORT NOTED ON FLOORBEAM AT FS 980 REPAIR FOUND NOT TO COMPLY WITH SRM. FABRICATED REPAIR SECT OF BEAM IAW SRM 53 -05 FIG 79, INSTALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998012900807 19980129 00807 WP 1998 1 29 MWEA98094 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 737 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 A CRACK WAS DISCOVERED IN LONGERON 3 LEFT AT FS 737. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SECTIONS IA W 53-02 FIG 18, INSTALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998012900808 19980129 00808 WP 1998 1 29 MWEA98095 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 737 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 2 RIGHT WAS FOUND CRACKED AT FS 737. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SECTIONS IAW 53-02 FIG 18, INSTALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998012900809 19980129 00809 WP 1998 1 29 MWEA98096 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 5 LEFT FS 699 WAS FOUND TO HAVE CRACKS IN BOTH FLANGES. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SECTION IAW SRM 53-02 FIG 18, INSTALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998012900810 19980129 00810 WP 1998 1 29 MWEA98097 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 2 RIGHT FS 699 WAS FOUND CRACKED IN BOTH FLANGES. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SECTI ONS OF LONGERON IAWS RM 53-02 FIG 18. 2 L 7 2 4F A6WE 1998012900811 19980129 00811 WP 1998 1 29 MWEA98098 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 3 RIGHT AT FS 699 WAS FOUND TO HAVE A CRACK IN THE RT FLANGE. REMOVED DAMAGED SECTIONS OF LONGERON, FABRICATED REPAIR SECTION IAW SRM 5302 FIG 18. INSTALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998012900812 19980129 00812 WP 1998 1 29 MWEA98099 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 658 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 5L AT FS 658 WAS FOUND TO HAVE CRACKS IN BOTH FLANGES. REMOVED DAMAGED SECTION OF LONGERON FABRICATED RPR SECT IONS IN ACCORD WITH SRM 53-02 FIG 18. INSTALLED REPAIR SECTION IAW SRM 51-30. 2 L 7 2 4F A6WE 1998012900813 19980129 00813 WP 1998 1 29 MWEA98101 1 19980126 A 3040 DE-ICE SYST DOUG DC9 DC915 3022036 WP LT WINDSHIELD MISWIRED A MWEA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 31 900ME 45841 CAPTAINS WINDSHIELD DEVELOPED ICE ON IT IMPAIRING VISIBILITY. MTC SWAPPED WIRES AT THE WINDSHIELD TEMP SENSOR AND RESET THE TRIPPED CIRCUIT BREAKER. 2 L 7 2 4F A6WE 1998012900814 19980129 00814 WP 1998 1 29 MWEA98100 1 19980127 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 THE GALLEY SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998012900815 19980129 00815 NM 1998 1 29 SCNA98002 1 19980113 A 5320 FLOOR SUPPORT BOEING 727 727225 1384077 NM BS 328/344 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 FLOOR SUPPORT CORRODED BETWEEN BS 328 AND BS 344, WL 207, RT BL 48 INCH (APPROX). REMOVED DAMAGED SECTION, FABRICATED A ND INSTALLED NEW FLOOR SUPPORT IAW BOEING 727 SRM 53-12-03, 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998012900817 19980129 00817 NM 1998 1 29 SCNA98003 1 19980113 A 5320 SUPPORT BOEING 727 727225 1384077 NM BS 328 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 FLOOR SUPPORT CORRODED BETWEEN BS 312 AND BS 328, WL 207, RT BL 48 INCH (APPROX). FABRICTAED AND INSTALLED NEW FLOOR SU PPORT IN ACCORDANCE WITH BOEING SRM 53-12-3, 51-10-2 AND 53-11-3. 2 L 7 3 4F A3WE 1998012900818 19980129 00818 NM 1998 1 29 SCNA98004 1 19980115 A 5320 SUPPORT BOEING 727 727225 1384077 NM BS 1180 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 AFT CARGO AT BS 1180 WL 208 FROM RBL 23 THROUGH 30 FLOOR SUPPORT STIFFENER CRACKED AND CORRODED. FABRICATED AND INSTALL ED FLOOR SUPPORT IAW BOEING 727 SRM 51-30-2, 51-10-2 AND 51-10-6. 2 L 7 3 4F A3WE 1998012900819 19980129 00819 NM 1998 1 29 SCNA98005 1 19980120 A 5210 SEAL BOEING 727 727225 1384077 NM PAX DOOR DAMAGED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 282SC 22558 ON TAKEOFF CLIMBING THROUGH 13000 CABIN DID NOT PRESSURIZE. CLEANED AND RESEALED DAMAGED SEAL AT STA 1183. 2 L 7 3 4F A3WE 1998012900820 19980129 00820 NM 1998 1 29 SCNA98006 1 19980114 A 5230 FRAME BOEING 727 727225 1384077 NM CARGO DOOR CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 AFT CARGO DOOR TOOLING HOLE FWD FRAME CRACKED LOWER CORNER. STOP DRILLED CRACKED, FABRICATED AND INSTALLED REPAIR DOUBL ER IAW SB 72753A0199. 2 L 7 3 4F A3WE 1998012900821 19980129 00821 NM 1998 1 29 SCNA98007 1 19980121 A 2150 32194211 35 DEGREE VALVE BOEING 727 727225 1384077 NM RT PACK FAULTY A SCNA A UNSCHED LANDING L NO TEST CL CLIMB 1 GL 15 282SC 22558 FAILED TO PRESSURIZE ON TAKEOFF. TIGHTEN LINES AT FLOW CONTROL VALVE AND REMOVED AND REPLACED 35 DEGREE CONTROL VALVE. FUNCTIONALLY TESTED NORMAL ON GROUND. 2 L 7 3 4F A3WE 1998012900822 19980129 00822 NM 1998 1 29 SCNA98008 1 19980121 A 2150 EXHAUST VALVE BOEING 727 727225 1384077 NM E/E COMPT INOPERATIVE A SCNA A UNSCHED LANDING L NO TEST TO TAKEOFF 1 GL 15 282SC 22558 UNABLE TO PRESSURIZE AIRCRAFT ON CLIMB-OUT. RETURNED TO LAS AND FOUND E/E EXHAUST VALVE NOT CLOSING AT 3PSI. REMOVED A ND REPLACED EXHAUST VALVE IN ACCORDANCE WITH BOEING 727 MM 21-58-00 AND FUNCTIONALLY TESTED GOOD. 2 L 7 3 4F A3WE 1998012900823 19980129 00823 NM 1998 1 29 P5CA9800048 1 19980125 A 3230 65B015397 ACTUATOR BOEING 747 747132 1384882 NM RT MLG TILT LEAKING A P5CA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 857FT 20246 NR 4 HYDRAULIC SYSTEM FLUID LOSS TO 1.6 GALLONS. DECLARED EMERGENCY TO PROVIDE TIME FOR ABNORMAL PROCEDURES. EMERGENCY TERMINATED AFTER LANDING ALL SYSTEMS FUNCTIONED NORMAL. FOUND RIGHT WING POSITIONING ACTUATOR LEAKING. REPLACED PER B OEING M/M 32-11-20. 2 L 7 4 4F A20WE 1998012900824 19980129 00824 NM 1998 1 29 P5CA9800049 1 19980126 A 2910 65B9017057 LINE BOEING 747 747132 1384882 NM NR 4 PYLON CRACKED A P5CA O OTHER K FLUID LOSS CR CRUISE 1 WP 23 857FT 20246 NR 4 HYDRAULIC SYSTEM FLUID LOSS TO 1.6 GALLONS. FOUND CRACKED PRESSURE LINE IN NR 4 PYLON. REPLACED LINE, ENGINE DRIV EN PUMP CASE DRAIN AND PRESSURE FILTERS PER BOEING MAINTENANCE MANUAL 29-11-23, 29-11-05, AND 29-11-18. 2 L 7 4 4F A20WE 1998012900825 19980129 00825 NM 1998 1 29 P5CA9800050 1 19980126 A 3260 WARNING LIGHT BOEING 747 747238B 1384828 NM LT/RT MLG ILLUMINATED A P5CA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 23 921FT 21575 LEFT WING AND RIGHT WING PRIMARY AND ALTERNATE TILT LIGHTS ON. ALSO, LEFT AND RIGHT WING LANDING GEAR DOOR PRIMARY AND ALTERNATE LIGHTS ON WHEN THE GEAR HANDLE PLACED TO THE OFF POSITION. LEFT AND RIGHT WING TILT AND DOOR SENSORS CHECKED OK, GEAR RETRACTION AND EXTENSION CHECKED NORMAL PER BOEING MAINTENANCE MANUAL 32-32-00, 32-33-00 AND 32-34-00 UNABLE TO DUPLICATE FAULT. 2 L 7 4 4F A20WE 1998012900826 19980129 00826 1998 1 29 RRXA98008 4 19980127 A 3421 258733511 VERTICAL GYRO DOUG DC8 DC862 3021970 WP NR 2 MALFUNCTIONED A RRXA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 WP 15 994CF 45956 ON APPROACH, F/O HORIZON WENT TO 6 DEG NOSE UP - HORIZON LIGHT ON - ON GO AROUND F/O SHOWED 15 DEG NOSE UP. CAPT 5 DEG NOSE UP. REMOVED AND REPLACED NR 2 VG AND NR 2 INSTRUMENT AMP FOR PRECAUTION. F/O HORIZON OPS CHECKS GOOD IAW DC-8 MM CHAP 34. 2 L 7 4 4F 4A25 1998012900830 19980129 00830 NM 1998 1 29 VNAA9801012 1 19980126 A 3610 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT LOOSE A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 442JS 3060 THE RIGHT HAND HIGH PRESSURE BLEED VALVE WOULD NOT CLOSE, DURING TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND FOUND THE HIGH PRESSURE BLEED VALVE CANNON PLUG TO BE LOOSE. MAINTENANCE SECURED AND FUNCTION CHECKED THE RIGHT HAND HIGH PRESSURE BLEED VALVE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-07. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998012900831 19980129 00831 WP 1998 1 29 CKSA98002 1 19980124 A 3350 516574 POWER PACK LKHEED 1011 1011385115 5265015 WP BS 855 INOPERATIVE A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 DURING EMERGENCY LIGHT SYSTEM TEST, FOUND NR 4R EXIT LIGHT ON INTERMITTENTLY. REMOVED AND REPLACED NR 4R EMERGENCY POWE R PACK IAW L1011 MM 33-51-03, OPS CHECK GOOD. 2 L 7 3 4F A23WE 1998012900837 19980129 00837 EU 1998 1 29 SIMA980051 1 19980105 A 3350 852516R12BOPNH CONNECTOR AEROSP ATR72 ATR72212 EU PAX DOOR DAMAGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AT 345 DFW - FLT 3603 - DOOR PAX UNLOCK LIGHT AND EXIT LIGHT INOP. REPLACED ENTRANCE DOOR CANNON PLUG. PERFORMED OPERATIONAL CHECK OF DOOR WARNING AND EMERGENCY LIGHT SYSTEM SATISFACTORILY IN ACC WITH JIC'S. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998012900838 19980129 00838 EU 1998 1 29 SIMA980031 1 19980103 A 2611 7211121100 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E COMPT FAILED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 380AE A4163 340B380 DFW - AFTER TAKEOFF, AVIONICS SMOKE WARNING CAME ON AND REMAINED ON. NO VISIBLE SMOKE OR NOTABLE ODOR WAS PRESENT. FLI GHT RETURNED TO DFW. REPLACED AVIONICS SMOKE DETECTOR. SYSTEM TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998012900949 19980129 00949 NM 1998 1 29 EISA97286 1 19980104 A 7997 WIRE BOEING 727 727221 1384071 NM OIL TEMP BULB BROKEN A EISA C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN N FALSE WARNING TO TAKEOFF 1 SW 07 367PA 22539 NR 2 OIL TEMP ABOVE RED LINE ON TAKEOFF ENGINE SHUTDOWN. REPAIRED BROKEN WIRE AT TEMP BULB ON NR 2 ENGINE, OPS CHECK NO RMAL. (M) 2 L 7 3 4F A3WE 1998012900953 19980129 00953 SO 1998 1 29 C2XA98CL001 1 19980105 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR TORN A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 16724 120171 CLE - FLT 3180 - CREW REPORTED THAT THE MANUAL AND AUTO PRESSURIZATION WAS INOPERATIVE. AIRCRAFT RETURNED TO FIELD WITH OUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE CARGO DOOR SEAL IAW EMB 120MM 52 -30-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY IAW EMB120MM 21-30-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998012900954 19980129 00954 SO 1998 1 29 C2XA98IA001 1 19980107 A 5320 12022670001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, FOUND LEFT VERTICAL FLOOR SUPPORT AT FRAME 13 CRACKED. MAINTENANCE STOP DRILLED THE CR ACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02/51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998012900955 19980129 00955 SO 1998 1 29 C2XA98IA002 1 19980107 A 5320 12022670002 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT VERTICAL FLOOR SUPPORT AT FRAME 13 CRACKED. MAINTENANCE STOP DRILLED THE C RACK AND INSTALLED REPAIR DOUBLER IAW EMB120 SRM 51-10-02/51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1998012900956 19980129 00956 SO 1998 1 29 C2XA98IA003 1 19980107 A 5720 12031657002 ANGLE EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING TO FUSELAGE FAIRING 194 LOWER ATTACHMENT ANGLE CRACKED AT AFT END. MA INTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998012900957 19980129 00957 SO 1998 1 29 C2XA98IA004 1 19980108 A 5530 14531597601 DRAG ANGLE EMB 120 EMB120RT SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 27707 120095 IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER RIGHT SIDE DRAG ANGLE CRACKED. MAINTENANCE REMOVED DAMAGED S ECTION AND INSTALLED NEW SECTION IAW EC5530-01013. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998012900958 19980129 00958 EU 1998 1 29 C2XA98IA005 1 19980107 A 5320 S53971402202 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE (BELLY) FAIRING SUPPORT WEB CRACKED AT CHORD. MAINTENANCE STOP DRILLE D THE CRACK AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998012900959 19980129 00959 EU 1998 1 29 C2XA98IA006 1 19980107 A 5315 S53672215202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14825 170 IAH - DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BEAM CORRODED AT FRAME 39. MAINTENANCE REMOVED THE DAMAGED AREAS O F THE BEAM AND INSTALLED TWO REPAIR SECTIONS ON LEFT SIDE IAW ATR 42 SRM 51-21-42/EC5310-01037. THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998012900960 19980129 00960 SO 1998 1 29 C2XA98CL002 1 19980105 A 2910 12035506035 HYD LINE EMB 120 EMB120RT SO LT MLG WW CRACKED A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 57734 120199 CLE - FLT 3182 - CREW REPORTED THAT THEY RECEIVED A LOW LEVEL AND LOW PRESSURE INDICATION ON TEH LEFT GREEN HYDRAULIC SY STEM. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACE D THE LEFT HYDRAULIC PUMP SUCTION LINE IAW EMB-120 MM 20-10-03 AND EMB-120 IPC 29-30-00. OPERATIONAL AND LEAK CHECKS WE RE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998012900998 19980129 00998 SO 1998 1 29 WTAA980003 1 19980104 A 3230 12032943000 SEQUENCE VALVE EMB 120 EMB120RT SO LT MLG WW OUT OF ADJUST A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 250YV 120250 FAT - LEFT MAIN GEAR FAILED TO RETRACT AFTER DEPARTURE. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE ADJ USTED LEFT MAIN GEAR INBOARD FORWARD DOOR SEQUENCE VALVE. PERFORMED GEAR SWINGS. OPERATIONAL CHECK SATISFACTORY. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998020500001 19980205 00001 WP 1998 2 5 9801679908 1 19980123 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE DEPLOYMENT HANDLE FROM CLIPS. REP LACED SPRING CLIPS, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998020500002 19980205 00002 WP 1998 2 5 9801689862 1 19980126 A 5210 DOOR DOUG DC9 DC951 3022051 WP PAX DOOR OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 771NC 47769 MAIN CABIN DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE REPLACED NYLON WASHERS ON BAYONET ROD, ADJUSTED DOOR ROTATION, AND BAYONET ROD, FUNCTIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998020500003 19980205 00003 NE 1998 2 5 9801691152 2 19980127 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA O OTHER O OTHER LD LANDING 1 GL 01 152US 46761 686166 DURING LANDING ROLLOUT, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT REACHED 670C AND THE ENGINE WAS SHUT DOWN. THE CRE W RESTARTED THE ENGINE WHILE TAXIING WITH ALL PARAMETERS NORMAL. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE ENGIN E AND AN OPERATIONAL CHECK OF THE RABS WITH NO DEFECTS FOUND. THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1998020500004 19980205 00004 WP 1998 2 5 9801709102 1 19980127 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 01 92S 47064 DURING TAXI, THE CABIN OVERHEAD EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN THE OFF POSITION. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998020500005 19980205 00005 WP 1998 2 5 9801719102 1 19980127 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 779NC 48101 DURING INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PAC K, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998020500006 19980205 00006 WP 1998 2 5 9801729612 1 19980123 A 3222 5910448531 STRUT DOUG DC9 DC932 3022066 WP NOSE GEAR FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 612NW 5406 5406 47436 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT I NCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR STRUT ASSEMBLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500007 19980205 00007 WP 1998 2 5 9801739920 1 19980126 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 942N 47459 DURING LINE MAINTENANCE INSPECTION, FOUND AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500008 19980205 00008 WP 1998 2 5 9801749995 1 19980126 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND ALL TAIL CONE EMERGENCY CATWALK PATHWAY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500009 19980205 00009 WP 1998 2 5 9801759612 1 19980124 A 3260 GROUND SENSE DOUG DC9 DC932 3022066 WP NLG OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 612NW 47436 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT I NCIDENT. MAINTENANCE RIGGED GROUND SENSE CONTROL MECHANISM, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500010 19980205 00010 NM 1998 2 5 UPS98225599 1 19980112 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, ON REMOVAL OF BUSHINGS FROM NR 4 AND NR 5 FLAP TRACK WING LUGS, CORROSION WAS FOUND IN THE BORE AREA REWORKED IAW SRS ENGINEERING ORDER 98-01-024. 2 L 7 3 4F A3WE 1998020500011 19980205 00011 NM 1998 2 5 UPS98225600 1 19980116 A 5320 INTERCOSTAL BOEING 727 72722C 138400F NM BS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, INTERCOSTAL TO BEAM TIE CRACKED AT BS 304, LBL 12. NEW BRACKET INSTALLED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998020500012 19980205 00012 NM 1998 2 5 UPS98225601 1 19980111 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM WS 224 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 6 FLAP TRACK PAD B HAS CORROSION. CORROSION REMOVED AND PAD REPAIRED IAW SRS ENGINEERING ORDER 98 -01-0 16. 2 L 7 3 4F A3WE 1998020500013 19980205 00013 NM 1998 2 5 UPS98225602 1 19980111 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM WS 203 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 6 FLAP TRACK WING LUG, WBL 203 APPROX, HAS CORROSION. CORROSION REMOVED AND REPAIR THEN CARRIED O UT PER SRS ENGINEERING OR DER 98-01-012. 2 L 7 3 4F A3WE 1998020500014 19980205 00014 NM 1998 2 5 UPS98225603 1 19980112 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM WS 203 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 3 FLAP TRACK WING LUG WBL 203 HAS CORROSION. CORROSION REMOVED AND REPAIR THEN CARRIED OUT PER SR S ENGINEERING OR DER 98-01-018. 2 L 7 3 4F A3WE 1998020500015 19980205 00015 NM 1998 2 5 UPS98225604 1 19980121 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM WS 442 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, WING LUG FOR NR 8 FLAP TRACK WBL 442 HAS CORROSION. CORROSION REMOVED AND THEN REPAIRED PER SRS ENGI NEERING ORDER 98-01- 023. 2 L 7 3 4F A3WE 1998020500016 19980205 00016 NM 1998 2 5 UPS98225605 1 19980123 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, TWO CRACKS AT TOP FASTENER HOLES IN FRAME ANGLE BS 880 RT AT STRINGER 15. REPAIR CARRIED OUT WITH NE WLY FABRICATED REPAIR ANGLE PER SRM 51-40- 3 FIGURE 1. 2 L 7 3 4F A3WE 1998020500017 19980205 00017 NM 1998 2 5 UPS98225606 1 19980121 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM WS 348 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, WING LUG FOR NR 7 FLAP TRACK WBL 348 APPROX HAS CORROSION. CORROSION REMOVED AND LUG REPAIRED IAW SR S ENGINEERING ORDER 98-01-0 22. 2 L 7 3 4F A3WE 1998020500018 19980205 00018 NM 1998 2 5 UPS98225607 1 19980121 A 5720 ANGLE BOEING 727 72722C 138400F NM FRONT SPAR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, TEE ANGLE AT FRONT SPAR UPPER CHORD BBL 24.5 RT CRACKED (WING CENTER SECTION INTERIOR). TEE ANGLE RE PLACED IAW EO B727-5710-4575. 2 L 7 3 4F A3WE 1998020500019 19980205 00019 NM 1998 2 5 UPS98225608 1 19980110 A 5343 FITTING BOEING 727 72722C 138400F NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, ON REMOVAL OF NLG DRAG BRACE SUPPORT FITTING, CORROSION WAS DISCOVERED ON THE DRAG BRACE SUPPORT BEAM . BEAM REPAIRED IAW SRS ENGINEERING ORDER 98-01-004. 2 L 7 3 4F A3WE 1998020500020 19980205 00020 NM 1998 2 5 UPS98425614 1 19980126 A 5313 STRINGER BOEING 747 747123F NM BS 1820-1840 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, EVIDENCE OF CORROSION FROM STA 1820 TO 1840 AT STRINGER 51R. *S/D* INSTALLED TEMPORARY REPAIR DOU BLER FOR FERRY FLIGHT TO HAVE PERMANENT REPAIR INSTALLED. TEMP REPAIR WAS INSTALLED PER SRM 53-30-03. FERRY PERMIT NR 9029, REF CONTROL NR UPS98425677 FOR CORRECTIVE ACTION. 2 L 7 4 4F A20WE 1998020500021 19980205 00021 NM 1998 2 5 UPS98425615 1 19980126 A 5320 FASTENERS BOEING 747 747123F NM BS 1830-1850 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, EVIDENCE OF CORROSION AND CRACKED FASTENER HEADS FROM STA 1830 TO 1850 AT STRINGER 48R. *S/D* DEF ERRED FOR ONE TIME FERRY FLIGHT. FERRY PERMIT NR 9029/DMI NR 145981, REF CONTROL NR UPS98425665 FOR CORRECTIVE ACTION. 2 L 7 4 4F A20WE 1998020500022 19980205 00022 NM 1998 2 5 UPS98425616 1 19980126 A 5330 SKIN BOEING 747 747123F NM BS 1740-1770 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 EXT LOWER BELLY SKIN CORROSION APPOX 20 INCHES IN DIAMETER AT BL 0 AND BS 1740-1770. DEFERRED FOR ONE TIME FERRY FLIGHT . FERRY PERMIT NR 9029/DMI NR 145983. TRANSFERRED TO NRC 735004. REMOVED CORROSION ON LWR BELLY SKIN IAW SRM 51-10-1. UT THICKNESS PER B747 NTM PT.1, 51-04-00, NOMINAL THICKNESS .065- .070. AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-30- 01 FIGS 1 AND 2. TREATED AREA IAW SRM 51-10-02. LOG PAGE 412 ITEM 3. 2 L 7 4 4F A20WE 1998020500023 19980205 00023 WP 1998 2 5 UPS98825583 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 505 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, MAIN CABIN FS 505 BL 0 SEAT TRACK HAS HEAVY CORROSION AND CRACKED. REMOVED, FABRICATED, AND INSTALLE D REPLACEMENT SECTION OF TRACK IAW DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 1998020500024 19980205 00024 WP 1998 2 5 UPS98825584 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, SEAT TRACK SPLIT AND CRACKED FS 1220 LBL 24. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 1998020500025 19980205 00025 WP 1998 2 5 UPS98825585 1 19980121 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, SEAT TRACK CORRODED OUT OF LIMITS FS 1660 RBL 38 AFT ACCESSORY COMP. REMOVED, FABRICATED, AND INSTAL LED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998020500026 19980205 00026 WP 1998 2 5 UPS98825586 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, MAIN CABIN SEAT TRACK HAS HEAVY CORROSION FS 1210 BL 0. REPAIRED IAW UPS DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 1998020500027 19980205 00027 WP 1998 2 5 UPS98825587 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 747.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 747.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500028 19980205 00028 WP 1998 2 5 UPS98825588 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 597.5. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500029 19980205 00029 WP 1998 2 5 UPS98825589 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 466.651 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA XS 466.651. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500030 19980205 00030 WP 1998 2 5 UPS98825590 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 484.395 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XS 484.395. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500031 19980205 00031 WP 1998 2 5 UPS98825591 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER STA XFS 778.750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500032 19980205 00032 WP 1998 2 5 UPS98825592 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 635.000. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500033 19980205 00033 WP 1998 2 5 UPS98825593 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 653.750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500034 19980205 00034 WP 1998 2 5 UPS98825594 1 19980120 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 728.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E AT STA XFS 728.750 UPPER ARM CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500035 19980205 00035 WP 1998 2 5 UPS98825595 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 647.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA XFS 647.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500036 19980205 00036 WP 1998 2 5 UPS98825596 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 622.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500037 19980205 00037 WP 1998 2 5 UPS98825597 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 297.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA 297.50. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500038 19980205 00038 WP 1998 2 5 UPS98825598 1 19980119 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, RT WING L/E AT STA XFS 778.750 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500040 19980205 00040 WP 1998 2 5 UPS98825611 1 19980125 A 5240 SKIN DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-S/N, CRACK FOUND IN FWD LOWER CORNER OF LEFT AFT UPPER DECK SERVICE DOOR. INSTALLED TEMP REPAIR IAW SRM 53-2-1 PERMANENT REPAIR TO BE ACCOMPLISHED WITH IN 1000 CYCLES. 2 L 7 4 4F RT 4A25 1998020500043 19980205 00043 EU 1998 2 5 WWMA9800017 1 19980127 A 2612 72111211000 FIRE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 348SB 5 340B348 CARGO FIRE LIGHT DOES NOT ILLUMINATE DURING PREFLIGHT TEST. REPLACED THE AFT CARGO FIRE DETECTOR. DETECTOR WAS MOD A W ITH 5 HRS TIME SINCE REPAIR AND MODIFICATION. 2 L 7 2 4T RT A52EU 1998020500044 19980205 00044 EU 1998 2 5 WWMA9800016 1 19980126 A 2910 GPP125012 PRESS SWITCH SAAB SF340 340B 7860101 EU HYDRAULIC SYST FAILED A WWMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 15 349SB 340B349 HYDRAULIC SYSTEM FAILED ON TAXI. MAINTENANCE FOUND THE HYDRAULIC PRESSURE SWITCH HAD FAILED AND THUS NOT TURNING ON THE PRESSURE PUMP. THE PRESSURE SWITCH WAS REPLACED AND THE HYDRAULIC MOTOR WAS ALSO REPLACED DUE TO UNUSUAL GRINDING NOIS ES. MOTOR (P/N 4018502) (S/N EQ32) HAD 2674 HRS TSO. 2 L 7 2 4T RT A52EU 1998020500045 19980205 00045 NM 1998 2 5 QXEA9800049 1 19980126 A 3350 6038443 POWER SUPPLY DHAV 82410191011 DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTION A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 353PH 496 SEA- FORWARD FLOOR EMERGENCY EGRESS LIGHTS ARE INOP. REPLACED BATTERY POWER SUPPLY AND BATTERY PACK 3352 PS1, OPERATION AL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998020500046 19980205 00046 EU 1998 2 5 QXEA9800050 1 19980127 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 493US 11161 BOI- EMERGENCY EXIT LIGHT ON GALLEY SERVICE DOOR IS INOP (LOWER RIGHT CORNER). RELAMPED EMERGENCY LIGHT, OPERATIONAL CH ECKS GOOD. 2 L 7 2 4F RT A20EU 1998020500047 19980205 00047 NM 1998 2 5 98FDEA00056 1 19980128 A 5320 65196043 SHEAR WEB BOEING 727 727227 1384078 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 482FE 21464 UPON REMOVAL OF 1176 REINFORCEMENT CHORD ON NR 0094, DISCOVERED CORROSION ON SHEAR WEB AT BS 1176, RBL 32, WL 208. *S/D * REMOVED AND REPLACED SHEAR WEB FROM BS 1171 TO 1177, RBL 16 TO RBL 44 PER FED-EX SRM 51-40-2. 2 L 7 3 4F A3WE 1998020500048 19980205 00048 NM 1998 2 5 98FDEA00057 1 19980128 A 5320 65317731 CHORD BOEING 727 727227 1384078 NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 482FE 21464 CORROSION (C53-224-08) ON 1176 REINFORCEMENT CHORD AT BS 1176, RBL 7, WL 208. *S/D* REMOVED AND REPLACED REINFORCEMENT CHORD AT BS 1176, RBL 65 TO LBL 65, WL 208 PER FED-EX SRM 51-30-2 AND BOEING DRAWING NR 65-19606. 2 L 7 3 4F A3WE 1998020500049 19980205 00049 NM 1998 2 5 98FDEA00058 1 19980128 A 5320 6519606160 SHEAR WEB BOEING 727 727227 1384078 NM BS 1175 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 482FE 21464 CORROSION (C53-224-04) ON TOP AND BOTTOM OF SHEAR WEB AT BS 1175, RBL 1 TO 15, WL 208. *S/D* REMOVED AND REPLACED DAMA GED SHEAR WEB, BS 1140 TO 1176, RBL 20 TO LBL 20, WL 208 IAW FED-EX SRM 51-30-2, 51-20-1. 2 L 7 3 4F A3WE 1998020500050 19980205 00050 NM 1998 2 5 98FDEA00059 1 19980128 A 5270 ANNUNCIATOR BOEING 727 727227 1384078 NM CARGO DOOR INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 485FE 21488 PASSING 1000 FT ON T/O, THE MAIN CARGO DOOR WARNING LIGHT CAME ON. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL: 52-4A CAT EGORY: A EXPIRATION: 29-JAN-98. MAIN CARGO DOOR ANNUNCIATOR LIGHT INOP. MAIN CARGO DOOR IS CLOSED AND LOCKED PRIOR TO EACH BLOCK OUT OK TO CONTINUE CAT A EXP 29 JAN 98 CONTROL NR 29169 CARGO DOOR VERIFIED CLOSED AND LOCKED. 2 L 7 3 4F A3WE 1998020500051 19980205 00051 WP 1998 2 5 MWEA98102 1 19980128 A 5730 PANEL DOUG DC9 DC932 3022066 WP WS 1132 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LWR LT WING PANEL 113A FOUND TO HAVE CORRODED SCREW HOLES SUBSEQ BLENDING SHOWED CORROSION BEYOND LIMITS. REMOVED DAMAG ED PART FABRIC REPLACEMENT PANEL IAW SRM 57-31-1, INSTALLED REPLACEMENT PANEL IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500052 19980205 00052 WP 1998 2 5 MWEA98103 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 17R WAS FOUND CRACKED AT FS 965. REMOVED DAMAGED SECTION OF LONGERON FABRICATED REPAIR PARTS IAW SRM 53-02 FIG 18, INSTALLED REPAIR PARTS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500053 19980205 00053 WP 1998 2 5 MWEA98104 1 19980128 A 5311 2777930 FRAME DOUG DC9 DC932 3022066 WP BS 237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FRAME AT STA 237 LONGERON 30 WAS FOUND CORRODED. REMOVED DAMAGED SECTION OF FRAME FABRICATED REPAIR PARTS IAW SRM 53-03 FIG 2A, INSTALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500054 19980205 00054 WP 1998 2 5 MWEA98105 1 19980128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 434/446 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL BETWEEN FS 434 AND FS 446 LONGERON 29R FOUND CORRODED. REMOVED DAMAGED INTERCOSTAL FABRICATED REPLACEMENT I NTERCOSTAL IAW/SRM 53-11-2, INSTALLED FABRICATED INTERCOSTAL IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500055 19980205 00055 WP 1998 2 5 MWEA98106 1 19980128 A 5311 2777930 FRAME DOUG DC9 DC932 3022066 WP BS 503 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FRAME AT FS 503 WAS FOUND CORRODED BETWEEN LONGERON 28L AND LONGERON 28R. REMOVED DAMAGED SECT OF FRAME FROM LONG 27L- 27R, FABRICATED REPR PARTS IAW SRM 53-03 FIG 2A, INSTALLED RPR PARTS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500056 19980205 00056 WP 1998 2 5 MWEA98107 1 19980128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 351-362 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL AT LONGERON 29R FS 351 TO FS 362 WAS FOUND CORRODED. REMOVED DAMAGED INTERCOSTAL, FABRICATION REPLACEMENT I NTERCOSTAL IAW SRM 53-11-2, INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500057 19980205 00057 WP 1998 2 5 MWEA98108 1 19980128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 229-237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL BETWEEN FS 229 TO 237 BETWEEN LONGERON 27L AND 28L WAS FOUND CORRODED. REMOVED DAMAGED INTERCOSTAL, FABRICA TED REPLACEMENT INTERCOSTAL IAW SRM 53-11-2, INSTALLED INTERCOSTAL IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500058 19980205 00058 WP 1998 2 5 MWEA98109 1 19980128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 229 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL WAS FOUND CORRODED BETWEEN FS 229 AND FS 237 LONGERON 27R AND 28R. REMOVED DAMAGED INTERCOSTAL, FABRICATED REPAIR INTERCOSTAL IAW 53-11-2, INSTALLED REPAIR INTERCOSTAL IN ACCORDANCE WITH SRM 51-30. 2 L 7 2 4F A6WE 1998020500059 19980205 00059 WP 1998 2 5 MWEA98110 1 19980128 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 586 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION FOUND INSIDE LONGERON FITTING SPLICE AT FS 586 LONGERON 28R, CORROSION REMOVAL WENT BEYOND LIMITS. REMOVED DA MAGED PART, FABRICATED REPLACE PART IAW SRM 53-11-2, INSTALLED FAB PART IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500060 19980205 00060 WP 1998 2 5 MWEA98123 1 19980128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 408 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AN INTERCOSTAL WAS FOUND CORRODED AND CRACKED AT FRAME STA 408 BELOW LONGERON 18R. REMOVED DAMAGED SEC OF INTERCOSTAL, FABRICATED REPAIR PART IAW SRM 53-11-2, INSTALLED REPAIR PART IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500061 19980205 00061 WP 1998 2 5 MWEA98124 1 19980128 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 351-370 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL BETWEEN FS 351 AND FS 370 BS 40 LT FOUND TO BE CORRODED. REMOVED DAMAGED INTERCOSTAL, FABRICATED REPAIR PAR T IAW SRM 53-11-2 SRM 51-10-2, INSTALLED REPAIR PART IAW SRM. 2 L 7 2 4F A6WE 1998020500062 19980205 00062 WP 1998 2 5 MWEA98125 1 19980128 A 5320 5910142 GUSSETT DOUG DC9 DC932 3022066 WP BS 370 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 A TAPERED STRAP (GUSSETT) WAS FOUND SEVERELY CORRODED AT FS 370 LONGERON 19R. REMOVED DAMAGED GUSSETT, FABRICATED REPAI R GUSSETT IAW 53-15-2, INSTALLED GUSSETT IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500063 19980205 00063 WP 1998 2 5 MWEA98126 1 19980128 A 5320 5911412 DOUBLER DOUG DC9 DC932 3022066 WP BS 518 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE AUX FUEL SHROUD DRAIN DOUBLER WAS FOUND CORRODED FS 518. REMOVED DAMAGED DOUBLER, FABRICATED REPLACEMENT DOUBLER IA W PRINT 5911412, INSTALLED REPAIR DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500064 19980205 00064 WP 1998 2 5 MWEA98127 1 19980128 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 560 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION WAS FOUND ON FWD AUX TANK SUMP DRAIN AT FS 560 LONGERON 28L. FABRICATED REPLACMENT DOUBLER, REMOVED DAMAGED D OUBLER, INSTALLED REPLACEMENT DOUBLER IAW DRAWING 5911412 AND SRM 51-30. 2 L 7 2 4F A6WE 1998020500065 19980205 00065 WP 1998 2 5 MWEA98128 1 19980128 A 5320 5911412 DOUBLER DOUG DC9 DC932 3022066 WP BS 389 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE RADAR ALTIMETER DOUBLER WAS FOUND CORRODED AT FS 389 LONGERON 30-29 LEFT. REMOVED DAMAGED DOUBLER, FABRICATED REPLA CEMENT DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500066 19980205 00066 WP 1998 2 5 MWEA98129 1 19980128 A 5320 5911412 DOUBLER DOUG DC9 DC932 3022066 WP BS 332 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 77013 RADAR ALTIMETER DOUBLERS WERE FOUND CORRODED AT FS 332 LONGERONS 30 AND 29L. REMOVED DAMAGED DOUBLERS, FABRICATED REPLA CEMENT DOUBLERS IAW PRINT 5911412, INSTALLED FABRICATED DOUBLERS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500067 19980205 00067 WP 1998 2 5 MWEA98130 1 19980128 A 5313 3924050501N LONGERON DOUG DC9 DC932 3022066 WP BS 544-586 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 28 LEFT WAS FOUND TO HAVE CORROSION FROM FS 544 TO FS 586. REMOVED DAMAGED SECT OF LONGERON 28L FROM FS 544 TO FS 586, FABRICATED REPLACEMENT SEC OF LONGERON FROM DRWNG 3924050, INSTALLED REPAIR PART IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500068 19980205 00068 WP 1998 2 5 MWEA98131 1 19980128 A 5311 2777930 FRAME DOUG DC9 DC932 3022066 WP BS 237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FRAME AT FS 237 WAS FOUND TO BE CORRODED AT LONGERON 30. REMOVED DAMAGED SECTION FRAME, FABRICATED REPAIR SECTIONS OF F RAME IAW SRM 53-03 FIG 2A, INSTALLED REPAIR SECTIONS ON FRAME AT FS 237 IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500069 19980205 00069 WP 1998 2 5 MWEA98132 1 19980128 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 229-355 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 29 RT WAS FOUND TO HAVE NUMEROUS AREA OF CORROSION FROM FS 229 TO FS 355. REMOVED DAMAGED SEC OF LONGERON 29 R T FROM FS 229 TO FS 355, OBTAINED NEW LONGERON 29 RT, INSTALLED NEW LONGERON 29 RT FROM FS 229 TO 355. 2 L 7 2 4F A6WE 1998020500070 19980205 00070 WP 1998 2 5 MWEA98133 1 19980128 A 5313 59203192 LONGERON DOUG DC9 DC932 3022066 WP BS 237-415 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 15 212ME 47701 LONGERON 30 FOUND TO HAVE NUMEROUS AREAS OF CORROSION FROM FS 237 TO FRAME STA 415. REMOVED DAMAGED SECTION OF LONGERON 30 FS 237 TO FS 415, OBTAINED NEW LONGERON 30, INSTALLED LONGERON IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500071 19980205 00071 WP 1998 2 5 MWEA98134 1 19980128 A 5313 5920319 LONGERON DOUG DC9 DC932 3022066 WP BS 229-420 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 29L WAS FOUND TO BE HEAVILY CORRODED FROM FS 229 TO FS 420. REMOVED DAMAGED SECTION OF LONGERON, OBTAINED AND INSTALLED NEW LONGERON FROM FS 420 IAW 53-11-02 AND 51-30. 2 L 7 2 4F A6WE 1998020500072 19980205 00072 WP 1998 2 5 MWEA98135 1 19980128 A 5313 2777923 LONGERON DOUG DC9 DC932 3022066 WP BS 585-639 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 2 RIGHT AT FUSELAGE STATION 617 WAS FOUND CRACKED. REMOVED LONGERON FROM FS 585 TO FS 639, OBTAINED NEW LONGER ON MATERIAL, INSTALLED LONGERON IAW SRM 51-30. 2 L 7 2 4F A6WE 1998020500073 19980205 00073 NM 1998 2 5 SCNA98009 1 19980105 A 5210 STRAP BOEING 727 7272A1 138407F NM 2R DOOR OUT OF POSITION A SCNA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 15 286SC 21601 AIR RETURN DUE TO DOOR STRAP NOISE FROM DOOR 2R. REMOVED DOOR STRAP FROM DOOR AND INSPECTED DOOR SKIN AND NR 3 ENGINE C 1 AND C2 DISCS FOR DAMAGE. NO DAMAGE FOUND AND OPS CHECK OK. 2 L 7 3 4F A3WE 1998020500076 19980205 00076 NE 1998 2 5 P5CA9800051 2 19980127 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 FLAMED OUT A P5CA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 WP 23 851FT 19756 686076 NR 4 ENGINE FLAMED OUT AT FL 390 DURING MODERATE TURBULENCE. ENGINE RELIT SHORTLY THEREAFTER. ALL PARAMETERS WERE NORM AL. NR 4 ENGINE INTAKE AND TAIL PIPE VISUAL CHECK NORMAL. NO METAL FOUND IAW MM 71-00-00. BORESCOPE IAW MM 72-00-00, NO DAMAGE FOUND. REMOVED AND REPLACED FUEL FILTER PER MM 72-00-00. 2 L 7 4 4F 4 F A20WE E20EA 1998020500077 19980205 00077 WP 1998 2 5 RRXA98009 1 19980123 A 2752 57726935019 FLAP ACTUATOR DOUG DC8 DC871F 302199D WP LT TE FLAP MALFUNCTIONED A RRXA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 WP 15 8076U 45941 UPON FLAP EXTENSION PAST FLAPS 15 DEG FLAPS SPLIT 6-8 DEG. TRIED TO EXTEND FLAPS SEVERAL TIMES AFTER RETRACTING FLAPS F IRST. FLAPS CONTINUE TO SPLIT PAST 15 DEG, AIRCRAFT ROLLED TO THE LEFT. REMOVED AND REPLACED LEFT WING OUTBOARD FLAP A CTUATOR/LINK ASSY AND LINK BOLT, IAW MM 27-51-9, OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1998020500078 19980205 00078 WP 1998 2 5 RRXA98010 1 19980127 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 902 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 DURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT AT STA 902 WITH CORROSION DAMAGE BEYOND LIMITATIONS IAW DC-8 SRM. R EMOVED LONGERON 24 RIGHT AND REPLACED WITH NEW LONGERON. USED SB 57-27 AND TIMCO JOB CARD FOR SHIMMING. 2 L 7 4 4F RT 4A25 1998020500080 19980205 00080 EU 1998 2 5 HEEA0012586 1 19980119 A 3340 A490ATSD1F POWER SUPPLY SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 POWER SUPPLY WIRE NOT SUPPLYING POWER TO STROBE LIGHT. 1 G 7 1 3U H9EU 1998020500081 19980205 00081 SW 1998 2 5 HEEA0012588 1 19980120 A 2435 23081018 STARTER BELL 407 407 SW ENG START GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 STARTER GENERATOR WON'T START AIRCRAFT. 1 G 7 1 3U O H2SW 1998020500082 19980205 00082 GL 1998 2 5 HEEA0012589 2 19980120 A 7250 23031426 NOZZLE 23035128 BELL 206 206L 1181522 SW ALLSN 250C 250C30P 03013 GL NR 4 DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 62127 CAT90180 52023 CAE895122 DURING MACHINING COATING FLAKING OUT OF NR4 NOZZLE NR4 TIP PATH. 1 G 7 1 3U 3 U H2SW E1GL 1998020500083 19980205 00083 NE 1998 2 5 HEEA0012590 2 19980120 A 7310 430137601 NOZZLE BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ENG FUEL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 136AE 926 7234 LE45581AEF FUEL LEAK DEVELOPED IN SOLID TUBING BETWEEN FUEL NOZZLES. TUBE APPEARS TO HAVE SMALL PIN HOLE OR CRACK IN ONE OF THE SO LID TUBES. 1 G 7 2 3U 3 U NC H13EU E5NE10 1998020500084 19980205 00084 EU 1998 2 5 HEEA0012591 1 19980121 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4031L 325 2907 PITCH CONTROL ROD BEARING WORN. 1 G 7 1 3U H9EU 1998020500085 19980205 00085 EU 1998 2 5 HEEA0012593 1 19980121 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORNY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4036H 59 2919 PITCH CONTROL ROD BEARING HAS PLAY. 1 G 7 1 3U H9EU 1998020500086 19980205 00086 EU 1998 2 5 HEEA0012594 1 19980121 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4036H 364 2919 PITCH CONTROL ROD BEARING HAS PLAY. 1 G 7 1 3U H9EU 1998020500087 19980205 00087 EU 1998 2 5 HEEA0012596 1 19980122 A 6220 704A3363310951 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 793 2771 SPHERICAL STOP ASSY SEPARATION. SERIAL NUMBERS REMOVED ARE 11731, 11725, AND 11733. REPLACEMENT SERIAL NUMBERS ARE 12 494, 12498, AND 12563. 1 G 7 1 3U H9EU 1998020500088 19980205 00088 SW 1998 2 5 HEEA0012600 1 19980122 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE NR 7 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 NR7 THOMAS COUPLING DISC CRACKED. 1 G 7 1 3U O H2SW 1998020500089 19980205 00089 SW 1998 2 5 HEEA0012601 1 19980122 A 6300 406010423101 DRIVE LINK BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 1170 53016 SUSPECT WORN DRIVE LINK PIVOT BUSHINGS. 1 G 7 1 3U O H2SW 1998020500090 19980205 00090 SW 1998 2 5 HEEA0012602 1 19980122 A 6300 406010426101 LINK ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 1170 53016 SUSPECT WORN LINK ASSY PIVOT BUSHINGS. 1 G 7 1 3U O H2SW 1998020500091 19980205 00091 EU 1998 2 5 HEEA0012603 1 19980122 A 7714 56337078012 INDICATOR SNIAS 350 AS350B2 8680813 EU ENGINE FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 2653 ENG TACH INDICATOR FLUCTUATES. 1 G 7 1 3U H9EU 1998020500092 19980205 00092 1998 2 5 HEEA0012605 4 19980122 A 3421 5040017901 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT ATTITUDE INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 2653 ATTITUDE INDICATOR INTERMITTENT, FLAG WILL NOT PULL. 1 G 7 1 3U H9EU 1998020500093 19980205 00093 EU 1998 2 5 HEEA0012606 1 19980122 A 7931 642790041 TRANSMITTER SNIAS 350 AS350B2 8680813 EU OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 3600 2862 OIL PRESS TRANSDUCER OIL PRESSURE FLUCTUATING. 1 G 7 1 3U H9EU 1998020500094 19980205 00094 EU 1998 2 5 HEEA0012607 1 19980122 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R PITCH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 151 2862 PITCH CONTROL ROD HAS WORN BEARINGS. 1 G 7 1 3U H9EU 1998020500095 19980205 00095 EU 1998 2 5 HEEA0012608 1 19980122 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R PITCH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 121 2820 PITCH CONTROL ROD HAS PLAY ON BEARINGS. 1 G 7 1 3U H9EU 1998020500096 19980205 00096 EU 1998 2 5 HEEA0012609 1 19980122 A 6320 350A37116200 STOP SNIAS 350 AS350B2 8680813 EU YOKE ASSY BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 155 2820 YOKE ASSY STOP BROKEN. 1 G 7 1 3U H9EU 1998020500097 19980205 00097 EU 1998 2 5 HEEA0012610 1 19980122 A 7700 0301017690 HARNESS SNIAS 350 AS350B2 8680813 EU ENG T4 FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 2873 T4 NEEDLE STICKS AND RELEASE ON MOST START UPS, AFTERWARDS APPEARS NORMAL. 1 G 7 1 3U H9EU 1998020500098 19980205 00098 EU 1998 2 5 HEEA0012611 1 19980122 A 2821 402A124 ELEMENT SNIAS 350 AS350B2 8680813 EU FUEL FILTER DIRTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 2653 FUEL FILTER ELEMENT DIRTY. 1 G 7 1 3U H9EU 1998020500099 19980205 00099 SW 1998 2 5 HEEA0012612 1 19980122 A 6300 406010425107 LEVER ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 1170 53016 LEVER ASSY WORN TEFLON BUSHINGS. SERIAL NUMBERS REMOVED ARE A1624 AND A1629. 1 G 7 1 3U O H2SW 1998020500100 19980205 00100 SW 1998 2 5 HEEA0012613 1 19980122 A 6321 206340301103 ROTOR BRAKE BELL 407 407 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 1144 53070 ROTOR BRAKE PADS MISSING. 1 G 7 1 3U O H2SW 1998020500101 19980205 00101 EU 1998 2 5 HEEA0012614 1 19980122 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 324 2820 ANTI COLLISION LIGHT INOPERABLE. 1 G 7 1 3U H9EU 1998020500102 19980205 00102 SW 1998 2 5 HEEA0012615 1 19980122 A 3340 099800003 SEARCH LIGHT BELL 230 230 1182149 SW EXT LIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 SEARCH LIGHT BULB WILL NOT ILLUMINATE. 1 G 7 2 3U NC H9SW 1998020500103 19980205 00103 SW 1998 2 5 HEEA0012616 1 19980122 A 2430 1820300150 SHUNT BELL 230 230 1182149 SW NR 1 GEN FAILED E HEEA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 03 230UN 23009 NR1 GENERATOR WOULD NOT COME ON LINE. 1 G 7 2 3U NC H9SW 1998020500104 19980205 00104 SW 1998 2 5 HEEA0012617 1 19980123 A 3212 407350301101 FLOAT BAG BELL 407 407 SW LT FLOAT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 FLOAT BAG LEAKING. 1 G 7 1 3U O H2SW 1998020500105 19980205 00105 EU 1998 2 5 HEEA0012620 1 19980123 A 2912 806966 ELEMENT SNIAS 350 AS350B2 8680813 EU HYD SYS DIRTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4036H 300 2919 HYD FILTER WAS IN BYPASS. 1 G 7 1 3U H9EU 1998020500106 19980205 00106 SW 1998 2 5 HEEA0012621 1 19980123 A 3242 D01381 PUCKS BELL 407 407 SW RT AFT BRAKE MISSING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 PUCK CAME OFF RIGHT REAR BRAKE CALIPER. 1 G 7 1 3U O H2SW 1998020500107 19980205 00107 SW 1998 2 5 HEEA0012623 1 19980123 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R NR 2 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 NR2 THOMAS COUPLING DISC CRACKED. 1 G 7 1 3U O H2SW 1998020500108 19980205 00108 SW 1998 2 5 HEEA0012625 1 19980123 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 NR3 T/R DRIVE SHAFT COUPLING HARDWARE BELOW TORQUE AS PER AD 97-22-15. 1 G 7 1 3U O H2SW 1998020500109 19980205 00109 SW 1998 2 5 HEEA0012626 1 19980123 A 6520 406040400115 GEARBOX BELL 407 407 SW T/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 2214 53003 T/R GR BOX INPUT AND OUTPUT SEALS LEAKING OIL. ALSO GEARBOX VENT LINE LEAKING EXCESSIVELY. 1 G 7 1 3U O H2SW 1998020500110 19980205 00110 SW 1998 2 5 HEEA0012627 1 19980123 A 6300 406012129101 LINK ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 LINK ASSY BEARING WORN. REPLACEMENT TAKEN FROM CONSIGNMENT KIT. 1 G 7 1 3U O H2SW 1998020500111 19980205 00111 SW 1998 2 5 HEEA0012628 1 19980123 A 6322 406040339105 BEARING 407040303101 BELL 407 407 SW T/R ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH A15773 53072 ROUGH BEARING. EVALUATE AS NECESSARY PER YOUR REQUEST. SERIAL NUMBERS REMOVED ARE F96-0132 AND F96-0119. 1 G 7 1 3U O H2SW 1998020500112 19980205 00112 SW 1998 2 5 HEEA0012629 1 19980123 A 7810 212061202009 DUCT ASSY BELL 212 212 1181420 SW LT ENG EXH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 DUCT ASSY DEFECTIVE REMOVED FOR EXCHANGE. 1 G 7 1 4U H4SW 1998020500113 19980205 00113 EU 1998 2 5 MALA975923 1 19980127 A 3350 66363 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 434XJ 434 DURING INSPECTION 8A, FLOOR TRACK EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998020500114 19980205 00114 EU 1998 2 5 MALA975924 1 19980128 A 3260 UPLOCK BAC 146 AVRO146RJ85A 1500097 EU LT MLG LACK OF LUBE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 503XJ E2310 AFTER DEPARTURE FROM MSP ON GEAR RETRACTION, THE LEFT MAIN RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND DID NOT EXTINGU ISH. CYCLED GEAR WITH NO CHANGE, AIRCRAFT RETURNED TO MSP. MAINTENANCE CLEANED AND LUBED UPLOCKS FOR GEAR AND DOOR. A LL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998020500115 19980205 00115 NM 1998 2 5 K3HA980009 1 19980129 A 2500 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT DOES NOT BLINK. REMOVED AND REPLACED. OPS CHECK OK. 2 L 7 3 4F A3WE 1998020500116 19980205 00116 NM 1998 2 5 W8PA980033 1 19980124 A 3350 P4010021 BATTERY BOEING 737 737301 1384611 NM CABIN DISCHARGED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 949WP 23230 DEN - FWD EMERGENCY FLASHLIGHT IS INOP. REPLACED BATTERY, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998020500117 19980205 00117 NM 1998 2 5 W8PA980034 1 19980128 A 3350 LIGHT BOEING 737 7373L9 1384470 NM CABIN MISSING A W8PA K NONE O OTHER IN INSP/MAINT 1 NM 03 961WP 23332 DEN - ORANGE STRIP ON EMERGENCY FLOOR TRACK LIGHTING IS MISSING. INSTALLED ORANGE STRIP ON FLOOR TRACK. 2 L 7 2 4F RT A16WE 1998020500118 19980205 00118 SO 1998 2 5 SRAA98A0114 1 19980125 A 2150 838321 HEAT EXCHANGER LKHEED 382 382G 526414U SO CARGO COMPT DEFECTIVE A SRAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 905SJ 4472 AFTER 40 MINUTES OUT OF HNL FLIGHT 2039, AIRCRAFT LOST PRESSURIZATION, COULD ONLY MAINTAIN 10,000 FT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON SHORTLY AFTER. ACCOMPLISHED AIR TURN BACK TO HNL. REMOVED AND REPLACED CARGO COMPARTMENT AIRCON DITIONING HEAT EXCHANGER AND ACCOMPLISHED ENGINE RUN UP, USING BLEED AIR SYSTEM, OPS CHECKED GOOD PER MM CH 21. 2 H 7 4 4T A1SO 1998020500119 19980205 00119 WP 1998 2 5 SRAA98A0115 1 19980127 A 3610 52057001401 COUPLING DOUG DC8 DC873F 302199F WP RT PNEU SYST LEAKING A SRAA H DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 23 873SJ 46091 DURING FLIGHT 133 TO BRU, THE RIGHT MANIFOLD FAIL LIGHT CAME ON WITH MANIFOLD AIR TEMP INDICATED AT APPROX 260 C. EMERG ENCY PROCEDURES EXECUTED IAW QRH/AOM, MANIFOLD FAIL LIGHT EXTINGUISHED. REPLACED PNEUMATIC COUPLING AND DUCT ASS'Y IN F ORWARD COMPARTMENT, PERFORMED PNEUMATIC DECAY TEST IAW CH 36 AND FOUND NO LEAKS NOTED. 2 L 7 4 4F RT 4A25 1998020500120 19980205 00120 SO 1998 2 5 SRAA98A0116 1 19980129 A 2820 FITTING LKHEED 382 382G 526414U SO CENTER FUEL SYS LEAKING A SRAA H DEACTIVATE SYST/CIRCUITS K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 912SJ 4388 AFTER LANDING DURING ROLL OUT AND TURN OFF TO PARKING AT DNA FLIGHT 407, NOTICED FUEL ODORS IN CARGO COMPARTMENT. AFTER PARKING AIRCRAFT FOUND FUEL DRIPPING FROM CENTER WING AREA CAVITY DRAIN LINE. TURNED OFF ALL AIRCRAFT POWER, EVACUATED AIRCRAFT AND FIRE DEPARTMENT WAS CALLED TO STANDBY. FOUND FUEL LEAKING FROM WIGGINS FITTINGS ON REFUEL MANIFOLD IN CEN TER WING DRY BAY AT LHS BULKHEAD. REPLACED PACKING IN WIGGINS FITTINGS PER LMM CH 28-21. PERFORMED PRESSURE CHECK WITH BOOST PUMPS AND REFUEL TRUCK. OPS CHECKED GOOD, NO LEAKS NOTED. 2 H 7 4 4T A1SO 1998020500121 19980205 00121 NM 1998 2 5 CALA9800126 1 19980127 A 5210 STOP BOEING 727 727227 1384078 NM L 1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 1 CRACK IN L-1 AFT UPPER DOOR STOP AT FITTING. THE L-1 AFT UPPER DOOR STOP WAS REMOVED AND REPLACED IAW SRM 52-40-1. 2 L 7 3 4F A3WE 1998020500122 19980205 00122 NM 1998 2 5 CALA9800127 1 19980127 A 5532 SKIN BOEING 727 727227 1384078 NM BS 1343 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A .5, 1, AND 2 CRACK IN RT SIDE OF VERTICAL STABILIZER SKIN LOWER SECTION AT STA 1343. THE AREA WAS RE PAIRED IAW ECRA 5530-01190. 2 L 7 3 4F A3WE 1998020500123 19980205 00123 NM 1998 2 5 CALA9800128 1 19980127 A 5712 RIB BOEING 727 727227 1384078 NM WS 130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND A 2 INCH CRACK AT FASTENER OF RT WING LEADING EDGE RIB, INBOARD OF NR 4 LEADING EDGE FLAP, AT L/E STA 1 30. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998020500124 19980205 00124 NM 1998 2 5 CALA9800129 1 19980127 A 3350 1000679 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND, THE AFT ENTRY EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACE D. 2 L 7 3 4F A3WE 1998020500125 19980205 00125 NM 1998 2 5 CALA9800130 1 19980127 A 3350 30043213 SOCKET BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND, RT FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INTERMITTENT. THE LIGHT SOCKET WAS REPLACED IAW MM 3 3-51-00. 2 L 7 2 4F RT A16WE 1998020500126 19980205 00126 WP 1998 2 5 CALA9800131 1 19980128 A 5312 BULKHEAD DOUG DC10 DC1030 3023501 WP BS 1521 FRETTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND, FRETTING ON CLG AFT PRESSURE BULKHEAD AT STA 1521. A REPAIR WAS ACCOMPLISHED IAW DOUGLAS DRAWING 90-5 3-1022. 2 L 7 3 4F A22WE 1998020500127 19980205 00127 WP 1998 2 5 CALA9800132 1 19980128 A 5210 BEAM DOUG DC9 DC932 3022066 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 47638 INSPECTION FOUND, A 1.25 INCH CRACK IN NR 1 BEAM, A .75 INCH CRACK IN NR 2 BEAM, AND A .5 INCH CRACK IN NR 3 BEAM OF MAI N CABIN DOOR. REPAIR DOUBLERS WERE INSTALLED IAW SRM 52-05, FIGURE 31. 2 L 7 2 4F A6WE 1998020500128 19980205 00128 WP 1998 2 5 CALA9800133 1 19980128 A 5210 PAN DOUG DC9 DC932 3022066 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19504 47638 INSPECTION FOUND, A 6 INCH CRACK AT AFT UPPER CORNER OF MAIN CABIN DOOR PAN. THE AREA WAS REPAIRED IAW ECRA 5211-01020. 2 L 7 2 4F A6WE 1998020500129 19980205 00129 WP 1998 2 5 CALA9800134 1 19980128 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 THE PULL FROM EXTERIOR TAILCONE RELEASE HANDLE WAS LOW. THE TAILCONE CABLES WERE ADJUSTED. 2 L 7 2 4F A6WE 1998020500130 19980205 00130 NM 1998 2 5 CALA9800135 1 19980129 A 5754 ANGLE BOEING 727 727243 138408D NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND, A 2.25 INCH AND 1.5 INCH CRACK AT INBOARD UPSTOP AREA BELOW TELESCOPING ANTI-ICE DUCT OF LT WING NR 2 SLAT CHORD ANGLE. THE ANGLE WAS REPAIRED IAW SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998020500131 19980205 00131 NM 1998 2 5 CALA9800136 1 19980129 A 2782 BRACKET BOEING 727 727243 138408D NM LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND A .75 IN H CRACK IN LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED AN D REPLACED IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998020500132 19980205 00132 NM 1998 2 5 CALA9800137 1 19980129 A 2782 BRACKET BOEING 727 727243 138408D NM LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND, A .75 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR INBOARD ATTACH BRACKET. THE BRACKET WAS R EMOVED AND REPLACED IAW SRM 51-40-3, 51-10-1, AND 51-30-2. 2 L 7 3 4F RT A3WE 1998020500133 19980205 00133 NM 1998 2 5 CALA9800138 1 19980129 A 5312 BULKHEAD BOEING 727 727227 1384078 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76752 21248 INSPECTION FOUND, A 1 CRACK IN FORWARD FACE OF STA 1183 BULKHEAD ON RT SIDE ABOVE OUTFLOW VALVE. A WEB REPAIR WAS INSTA LLED IAW BOEING DRAWING NR 65C31446, SRM 51-30-0, AND ECRA 553A0022. 2 L 7 3 4F A3WE 1998020500134 19980205 00134 WP 1998 2 5 CALA9800139 1 19980129 A 3350 BATTERY PACK GRIMES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14839 49635 INSPECTION FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS ON LEFT AND RIGHT SIDE INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-0. 2 L 7 2 4F A6WE 1998020500135 19980205 00135 WP 1998 2 5 CALA9800140 1 19980130 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 INSPECTION FOUND CORROSION ON WEB UNDER TIEDOWN RAIL IN AFT BAGGAGE BIN AT STA 1211, RBL 13, NEAR LOWER AFT CORNER OF EN TRY. THE CORROSION WAS REMOVED. DOUBLER AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 53-01 AND 53-14-3. 2 L 7 2 4F A6WE 1998020500136 19980205 00136 WP 1998 2 5 CALA9800141 1 19980130 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BAGGAGE COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 INSPECTION FOUND CORROSION ON FLOOR SUPPORT ANGLE ATTACHED TO MID CARGO BIN AFT WALL, LOWER RT SIDE. A NEW FLOOR SUPPOR T ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998020500137 19980205 00137 WP 1998 2 5 9801769914 1 19980128 A 5270 WARNING LIGHT DOUG DC9 DC931 3022065 WP VENTRAL STAIRS ILLUMINATED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 964N 47416 DURING CLIMB, THE AFT STAIRWAY DOOR LIGHT CAME ON. FLIGHT RETURNED TO CMH WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND VENTRAL STAIR DOOR UPLOCK SWITCH COVER BROKEN AND THE SWITCH AND CANNON PLUG RUBBING ON LOOSE TRIM AROUND OPENING OF DOO R. REPLACED SWITCH COVER FOR LEFT SWITCH, REMOVED LOOSE TRIM, AND RELAMPED DOOR OPEN LIGHT IN VENTRAL STAIR AREA. ALL SWITCHES CHECKED GOOD. CHECKED OPERATION OF DOOR, ROLLER, AND HOOK IN THE UPLOCK POSITION PER MM 52-63-00. 2 L 7 2 4F A6WE 1998020500138 19980205 00138 WP 1998 2 5 9801779975 1 19980128 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 DURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE EXTERIOR RELEASE HANDLE FROM CLIPS A ND INADEQUATE FORCE WAS REQUIRED TO REMOVE INTERIOR RELEASE HANDLE FROM CLIPS. ADJUSTED CLIPS. FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998020500139 19980205 00139 NM 1998 2 5 9801785524 1 19980124 A 3297 WIRE BOEING 757 757251 1384970 NM LT MLG FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 524US 23618 AS POWER WAS APPLIED FOR TAKEOFF, THE ANTI-SKID WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETUR NED TO THE GATE. MAINTENANCE REPAIRED WIRING FOR NR 4 ANTI-SKID TRANSDUCER. SYSTEM OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1998020500140 19980205 00140 WP 1998 2 5 9801791156 1 19980126 A 7830 ACTUATOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 TR UNIT OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 156US 46765 686164 ON TAKEOFF ROLL AT APPROXIMATELY 60 KNOTS, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS AB ORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE THRUST REVERSER AND ADJUSTED A LOCK ACTUATOR. T HE OPERATIONAL CHECK OF THE THRUST REVERSER WAS NORMAL AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1998020500141 19980205 00141 WP 1998 2 5 9801809102 1 19980128 A 3350 LIGHT DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 92S 47064 DURING AIRCRAFT SHUTDOWN AT THE GATE, ROWS 8-12 FLOOR PROXIMITY EMERGENCY LIGHTS ILLUMINATED WITH SWITCH IN THE OFF POSI TION. MAINTENANCE REPLACED 6 IMPROPER EMERGENCY LIGHT BULBS AND REPAIRED A CHAFED WIRE BETWEEN ROWS 8 AND 9. OPERATION AL CHECK OF SYSTEM WAS NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998020500142 19980205 00142 WP 1998 2 5 9801819933 1 19980128 A 3350 CONNECTORS DOUG DC9 DC931 3022065 WP CABIN DIRTY A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1334U 47280 DURING LINE MAINTENANCE INSPECTION, FOUND THE RIGHT OVERWING EMERGENCY EXIT AND AFT AIRSTAIR EMERGENCY LIGHTS INOPERATIV E. CLEANED CONNECTION IN AIRSTAIR LAMP AND TIGHTENED GROUND LUG ON LIGHT ASSEMBLY AT FORWARD RIGHT OVERWING EXIT SIGN. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500143 19980205 00143 WP 1998 2 5 9801829979 1 19980128 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 13 AND 14 INOPERATIVE. REPLACED BATTER IES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500144 19980205 00144 WP 1998 2 5 9801839996 1 19980128 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP LT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8932E 47141 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY P ACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500149 19980205 00149 WP 1998 2 5 9801849957 1 19980128 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 604 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M CHECK, FOUND CORROSION ON END FITTING FOR LONGERON 27R AT FS 604. REPLACED END FITTING PER SRM 51-01. 2 L 7 2 4F A6WE 1998020500150 19980205 00150 WP 1998 2 5 9801859940 1 19980115 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 108 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING L CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE RIGHT OUTBOARD AND INB OARD VERTICAL SUPPORTS FS 108. REPAIRED PER EA 99-153484. 2 L 7 2 4F A6WE 1998020500151 19980205 00151 WP 1998 2 5 9801869940 1 19980115 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 108 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3322L 47031 DURING L CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE LEFT OUTBOARD VERTICA L SUPPORT FS 108. REPAIRED PER EA 99-153484. 2 L 7 2 4F A6WE 1998020500152 19980205 00152 WP 1998 2 5 9801879903 1 19980117 A 5312 DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 953N 47083 DURING PERIODIC CHECK, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD UPPER LEFT WEB DOUBLER. REPAIRED PER EA 99-154224. 2 L 7 2 4F A6WE 1998020500153 19980205 00153 WP 1998 2 5 9801889867 1 19980119 A 5320 PRESSURE WEB DOUG DC9 DC951 3022051 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING L CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE RIGHT OUTBOARD VERTIC AL ATTACH ANGLE FS 110. REPAIRED PER EA 98-153495. 2 L 7 2 4F RT A6WE 1998020500154 19980205 00154 WP 1998 2 5 9801899867 1 19980119 A 5320 PRESSURE WEB DOUG DC9 DC951 3022051 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 776NC 47786 DURING L CHECK, FOUND A CRACK IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT THE LEFT OUTBOARD VERTICA L ATTACH ANGLE FS 110. REPAIRED PER EA 98-153495. 2 L 7 2 4F RT A6WE 1998020500155 19980205 00155 WP 1998 2 5 9801909102 1 19980129 A 3350 6014113 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 92S 47064 DURING LINE MAINTENANCE INSPECTION, FOUND MID CABIN EMERGENCY ESCAPE PATH LIGHTING REMAINING ON AFTER BATTERY SHUTDOWN. REPLACED BATTERY PACK AT OVERWING EXIT UNDER PSU PANEL. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500156 19980205 00156 WP 1998 2 5 9801919154 1 19980129 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998020500157 19980205 00157 WP 1998 2 5 9801929874 1 19980129 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 783NC 48108 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD MOUNTED CENTER AISLE EMERGENCY LIGHTS BETWEEN ROWS 21 THROUGH 23 WOUL D NOT TEST. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998020500158 19980205 00158 EA 1998 2 5 COMA9860027 1 19980127 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 920CA 7022 FLOOR EMERGENCY LIGHTS AFT OF ROW 8 ARE INOP. SECURED LOOSE WIRING CONNECTOR. 2 L 7 2 4F RT A21EA 1998020500159 19980205 00159 EA 1998 2 5 COMA9860028 1 19980127 A 3260 DISAGREE MESSAGE CNDAIR CL600 CL6002B19 EA NLG ACTIVATED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 931CA 7037 NOSE LANDING GEAR DISAGREE MESSAGE WHEN GEAR SELECTED DOWN. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERV ICE. 2 L 7 2 4F RT A21EA 1998020500160 19980205 00160 NM 1998 2 5 UPS98225619 1 19980116 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 880 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:D ON REMOVAL OF DAMAGE ON OUTER CHORD OF FRAME AT BS 880 RT STRINGER 15R, SUSPECT CRACK FOUND IN LOWER H OLE STRINGER. REPAIR CARRIED IAW SRM 53-10-3 2 L 7 3 4F A3WE 1998020500161 19980205 00161 NM 1998 2 5 UPS98225623 1 19980127 A 5320 WEB BOEING 727 72722C 138400F NM BS 1380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:D, FOUND CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL LT SIDE, BS1380 CRACKED WEB REMOVED. NE W WEB FABRICATED AND INSTALLED IAW DRAWING 65 -17555. 2 L 7 3 4F A3WE 1998020500162 19980205 00162 NM 1998 2 5 UPS98225625 1 19980127 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:D UPPER CHORD ANGLE OF BS 740 LOWER SECTION WL 170.5, BETWEEN LBL 40 AND RBL40, FOUND CORRODED AT VARIOU S LOCATIONS. CORRODED UPPER CHORD ANGLE REMOVED AND NEW CHORD ANGLE FITTED IAW DRAWING 65-15940. 2 L 7 3 4F A3WE 1998020500163 19980205 00163 NM 1998 2 5 UPS98225626 1 19980124 A 5311 FRAME BOEING 727 72722C 138400F NM BS 783.95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE:, ON INSPECTION FOUND CRACK ON FRAME BS 783.958 RT AT FOURTH FASTENER ABOVE FLOOR. REPAIR CARRIED OUT I AW APPENDIX C OF EO B727-5310-5474 AND SRS ENGINEERING ORDER 98-01-021. 2 L 7 3 4F A3WE 1998020500164 19980205 00164 NM 1998 2 5 UPS98425618 1 19980126 A 3350 LIGHT BOEING 747 747123F NM UPPER DECK INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 2 UPPER DECK EMERGENCY LIGHTS INOP, REMOVED LIGHTS. REMOVED AND REPLACED ONE EMERGENCY LIGHT PACK, RESEATED ONE. BOTH OPS CK GOOD ON TEST. 2 L 7 4 4F A20WE 1998020500165 19980205 00165 WP 1998 2 5 UPS98825617 1 19980102 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE:D, LT WING L/E OUTBOARD SIDE OF THE STA XS250.089 RIB, THE UPPER SKIN INTERNAL DOUBLER IS CRACKED. REMO VED, FABRICATED, AND INSTALLED REPLACEMENT SKIN IAW DWG 5769589 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998020500166 19980205 00166 WP 1998 2 5 UPS98825620 1 19980119 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C, RT WING L/E AT STA XFS 400.00, THE EXTERNAL SKIN HAS CRACK. REPAIRED IAW SRM ADDN DC8-5720-7767. 2 L 7 4 4F RT 4A25 1998020500167 19980205 00167 WP 1998 2 5 UPS98825621 1 19980119 A 5313 36471172N LONGERON DOUG DC8 DC871F 302199D WP BS 960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C LONGERON 24L FITTING CRACKED AT F/S 960. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 53-2-0. 2 L 7 4 4F RT 4A25 1998020500168 19980205 00168 WP 1998 2 5 UPS98825624 1 19980119 A 5313 36469561 LONGERON DOUG DC8 DC871F 302199D WP BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:C LONGERON 24L FITTING HAS HEAVY CORROSION F/S 940. REMOVED AND REPLACED FITTING IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998020500169 19980205 00169 NM 1998 2 5 98FDEA00060 1 19980123 A 5311 FRAME BOEING 727 727233 138408A NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0507 LOWER FWD CARGO COMPARTMENT BS 520 FUSE FRAME DENTED AT STRINGER 22L TO STR 24L. REMOVED DAMAGED SECTION OF FUS E FRAME. INSTALLED REPAIR DOUBLER PER AARD SRM 53-10-07-3 PG (ES0 11697). 2 L 7 3 4F RT A3WE 1998020500170 19980205 00170 NM 1998 2 5 98FDEA00061 1 19980129 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 1051 72 C237 02 UPPER LOBE BS 1050, RBL 20 CORROSION ON TOP LEG OF FLOORBEAM. REMOVED CORROSION CUTOUT DAMAGED AREA. FABRICATED REPAIR PARTS. INSTALLED REPAIR PER SRM 53-10-8 FIG 1. 2 L 7 3 4F RT A3WE 1998020500171 19980205 00171 NM 1998 2 5 98FDEA00062 1 19980129 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0683 AND NR 1044 72 C237-02 UPPER LOBE BS 1070, RBL 20 - RBL 35, CORROSION ON TOP SIDE OF FLOORBEAM. CUTOUT 2 AREAS OF CORROSION ON FLOORBEAM T CAP. INSTALLED REPAIR FROM RBL 16 - RBL 54, PER SRM 53-10-8, FIG 1. 2 L 7 3 4F RT A3WE 1998020500172 19980205 00172 NM 1998 2 5 98FDEA00063 1 19980129 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0727 72 C235-02 UPPER LOBE, BS 344, LBL 60 - RBL 20. CORROSION ON FLOORBEAM UPPER CAP. REMOVED OLD UPPER FLOORBEAM T-CAP. INSTALLED NEW T-CAP FROM LT TO RT SIDE OF FUSELAGE PER SRM 53-10-8 AND SRM 27-53-007, SHEET 1 OF 1. 2 L 7 3 4F RT A3WE 1998020500173 19980205 00173 NM 1998 2 5 98FDEA00064 1 19980124 A 5311 FRAME BOEING 727 727233 138408A NM BS 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0508 FWD CARGO, BELT FRAME AT BS 600L DENTED JUST ABOVE STR 23L. REMOVED DAMAGED AREA OF FRAME AND REPAIRED WITH TYP ICAL FORMED SECTION REPAIR PER SRM 51-40-3 PG 1, FIG 1. 2 L 7 3 4F RT A3WE 1998020500174 19980205 00174 NM 1998 2 5 98FDEA00065 1 19980120 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 496FE 21670 NR 0682 72 C 237-02 BS 1070, RBL 60 TO LBL 24 LOWER FORWARD FLANGE CORRODED. REMOVED CORRODED AREA OF FLOORBEAM FLANGE AND REPAIRED WITH FLOORBEAM REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998020500175 19980205 00175 NM 1998 2 5 98FDEA00066 1 19980127 A 5320 WEB BOEING 727 727233 138408A NM BS 913.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0141 BS 913.5 LEFT MAIN WHEEL WELL HAS CRACK ABOVE FILLER OF FLANGE. CONFIRMED WITH HFEC IN NOTED AREA. STOP DRILLE D CRACK PER SRM 51-10-1 AND INSTALLED MODIFICATION KIT P/N 5561732 (ON ORDER FORM NR 43326) IN ACCORDANCE WITH BOEING 72 7 SRM 53-10-2 PAGE 28P (K) FIG 3 FRAME MODIFICATION BS 913.5. 2 L 7 3 4F RT A3WE 1998020500176 19980205 00176 WP 1998 2 5 MWEA98136 1 19980128 A 3230 182205 SOLENOID VALVE DOUG DC9 DC932 3022066 WP LT MLG INOPERATIVE A MWEA O OTHER J WARNING INDICATION IN INSP/MAINT 1 GL 31 502ME 48132 ALT GEAR PUMP INOP DEFFERED PER MEL 29-7B, A/C REROUTED TO MKE FOR REPAIRS. MAINTENANCE REMOVED AND REPLACED LT ALT GEA R PUMP SOLENOID VALVE. 2 L 7 2 4F A6WE 1998020500177 19980205 00177 NM 1998 2 5 MWEA98137 1 19980129 A 3350 60030431 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 601ME 49762 FWD QUARTER OF PAX EMERGENCY ESCAPE LIGHTS VERY DIM. MAINTENANCE REPLACED BATTERYS. 2 L 7 2 4F RT A6WE 1998020500178 19980205 00178 WP 1998 2 5 MWEA98138 1 19980129 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP GALLEY DIRTY A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 FWD SERVICE DOOR GIRT BAR DIFFICULT TO INSTALL AND REMOVE. MAINTENANCE CLEANED LATCH. 2 L 7 2 4F A6WE 1998020500179 19980205 00179 NM 1998 2 5 DL72L980216 1 19980126 A 3350 1102833 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 508DA 21310 AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1998020500181 19980205 00181 NM 1998 2 5 DL72S980220 1 19980126 A 5311 65C2030313 FRAME BOEING 727 727232 1384082 NM BS 303.9 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 THE 65C20303-13 REPLACEMENT WEB PREVIOUSLY INSTALLED AS PART OF THE 65C20303-25 FRAME REPAIR KIT WAS FOUND CRACKED. THE -25 KIT WAS INSTALLED BY ERA 111762-14, CIRCA 6/86. THE CRACK IS LOCATED AT APPROX WL216. REPAIRED PER ERA 331194-14A D. 2 L 7 3 4F A3WE 1998020500182 19980205 00182 NM 1998 2 5 DL73K980221 1 19980126 A 5511 6550578525 SPAR CHORD BOEING 737 737232 1384475 NM HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 CORROSION FOUND ON THE UPPER SURFACE OF THE AFT FLANGE OF THE HORIZ STAB REAR SPAR UPPER CHORD. REPAIRED PER ERA 331272 -14. 2 L 7 2 4F RT A16WE 1998020500183 19980205 00183 NM 1998 2 5 DL73K980222 1 19980126 A 5743 654948818 FITTING BOEING 737 737232 1384475 NM RT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 DURING INSPECTION PER SB 737-57-1216 TWO CRACKS WERE FOUND IN THE MLG BEAM AFT SUPPORT FITTING ON THE RS OF THE RT WING. THE INBD CRACK LOCATION IS TYP PER SB. THE OUTBOARD FASTENER LOCATION WAS OS TO 0.438 DIAM AND THE CRACK WAS REMOVED. REPAIRED PER ERA 331269-14. 2 L 7 2 4F RT A16WE 1998020500184 19980205 00184 NM 1998 2 5 DL73K980223 1 19980126 A 5312 65163007 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 319DL 23091 SEVERAL CRACKS FOUND IN THE FS 178 BULKHEAD. REPAIRED PER ERA 331261-14. 2 L 7 2 4F RT A16WE 1998020500185 19980205 00185 NM 1998 2 5 DLM88980225 1 19980126 A 2740 RELAY DOUG MD88 MD88 3023688 NM E/E COMPT INOPERATIVE A A DALA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 27 998DL 53370 ON T/O STABILIZER TRIM WENT TO FULL NOSE DOWN. REPLACED NOSE DOWN TRIM RELAY R20-13. 2 L 7 2 4F RT A6WE 1998020500186 19980205 00186 NM 1998 2 5 DL73E980226 1 19980126 A 5230 SEAL 10608211 BOEING 737 737247 138448D NM CARGO DOOR TORN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 239WA 23187 CLIMBING THROUGH FL242 CABIN ALT WARN HORN. CABIN ALT OBSERV CLIMB THROUGH 10000 AND AIRCRAFT LEVELED. DESCENT BEGAN A ND CABIN ALT CLIMBED TO 13500, NO HELP IN STBY OR MAN, PRESS MODE OUTFLW VLV FULLY CLOSED AND FWD VALVE CLOSED LIGHT ON ENTIRE TIME. CHECKED ENTRY SERVICE CARGO DOOR SEALS. FOUND WORN FWD CARGO DOOR SEAL. REPLACED FWD CARGO DOOR SEAL. P RESSURIZED A/C, ALL IND GOOD, NO LEAKS. 2 L 7 2 4F A16WE 1998020500187 19980205 00187 NM 1998 2 5 DL72S980227 1 19980126 A 2782 ANGLE BOEING 727 727232 1384082 NM NR 3 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND 0N A2 LETTER CK, NR 3 L/E FLAP ACTUATOR BOX CRACKED AT OUTBOARD LOWER CORNER. REPAIRED PER MM 57-20-21 AND ERA. 2 L 7 3 4F A3WE 1998020500188 19980205 00188 NM 1998 2 5 DL72S980228 1 19980126 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223/1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND ON A2 LETTER CK, TORQUE BOX WEB CRACKED .5 INCH AT DOUBLER UPPER LIGHTNING HOLE STA 1223 AND .25 INCH CRACK AT LIG HTNING HOLE FWD STA 1243. REPAIR PER ERA 363858-14 AND M/M 53-11-0. 2 L 7 3 4F A3WE 1998020500189 19980205 00189 NM 1998 2 5 DL72S980229 1 19980126 A 5320 PRESSURE DECK BOEING 727 727232 1384082 NM BS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND ON A2 LETTER CK, 1 INCH CRACK AT LEFT MLG W/W PRESSURE DECK BEAD STA 950 AT LBL 63. STOP DRILLED CRACK PER MM 53 -14-0. 2 L 7 3 4F A3WE 1998020500190 19980205 00190 NM 1998 2 5 DL72K980231 1 19980117 A 5320 6517517 BEAM BOEING 727 727232 1384082 NM BS 1263/1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 FUSELAGE/VENTRAL STAIRWELL, RT TORQUE BOX. REPLACEMENT OF CRACKED FS 1263 AND 1273 BEAMS AND CHANNELS. THE FS 1263 BEA M AND CHANNEL AND THE FS 1273 BEAM WERE FOUND WITH THE TYPICAL CRACKS IN THE RT VENTRAL STAIRWAY TORQUE BOX. THE DAMAGE D PARTS WERE REPLACED WITH NEW PARTS PER S/B53-0129 AND DOCUMENTED PER ER/A 363753-14AD. 2 L 7 3 4F A3WE 1998020500191 19980205 00191 NM 1998 2 5 DL72L980232 1 19980121 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1205 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 FUSELAGE SKIN FS 1205-1215, STRINGER 23R AND REPAIR FOR SKIN DENTS. THE FUSELAGE SKIN WAS FOUND WITH TWO DENTS BETWEEN FS 1205 AND 1215 JUST ABOVE STRINGER 23R. THE DENTS WERE CUTOUT AND AN EXTERNAL SHEET METAL DOUBLER WAS INSTALLED PER E R/A 363791-14. 2 L 7 3 4F A3WE 1998020500192 19980205 00192 NM 1998 2 5 DLM88980233 1 19980127 A 5320 5912494 JAMB DOUG MD88 MD88 3023688 NM C1 DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 940DL 49813 FUSELAGE C1 DOOR CUTOUT LOWER JAMB PAN, SPLICE REPAIR OF CORRODED JAMB PAN. THE LOWER JAMB PAN AT THE C1 DOOR CUTOUT LO WER SILL WAS FOUND CORRODED. A NEW SECTION OF PAN WAS SPLICED IN AT THE LOWER SILL PER ER/A 363864-14. 2 L 7 2 4F RT A6WE 1998020500193 19980205 00193 NM 1998 2 5 DL72S980234 1 19980127 A 5330 65545902 SKIN BOEING 727 727232 1384082 NM BS 680 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FUSELAGE SKIN FS 680, STRINGER 26L-28L, REPAIR FOR CORROSION CUTOUTS. TWO AREAS OF CORROSION WERE CUTOUT OF THE FUSELAG E SKIN AT FS 680 BETWEEN STRINGERS 26L AND 28L. THE CUTOUTS WERE REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 3 63860-14, REV A. 2 L 7 3 4F A3WE 1998020500194 19980205 00194 NM 1998 2 5 DL72S980236 1 19980128 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 468DA 20745 EMERGENCY LIGHTS AT L-1, L-2, R-2 ABOVE DOOR INOP. REPLACED EMERGENCY BATTERIES PACK AT L-1, L-2, R-2. EMERGENCY LIGHT S CHECK GOOD. 2 L 7 3 4F A3WE 1998020500195 19980205 00195 WP 1998 2 5 DLL17980242 1 19980128 A 2780 HYD MOTOR 391357 LKHEED 1011 10113853 5265020 WP A-HYD SYST FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 766DA MX229095A 193H1207 DURING SLAT RETRACTION AFTER TAKEOFF A SYSTEM HYDRAULIC QTY DECREASED. TRIED POWER TRANSFER UNIT, QTY STILL DECREASED. FOUND A SYSTEM HYDRALIC MOTOR ON SLAT PWR DRIVE UNIT. MOTOR HOUSING SEVERLY CRACKED AND LEAKING. REPLACED MOTOR ASSY LRU. PERFORMED FUNCTIONAL CK AS PER MM 27-81-10. RTND FAILED MOTOR DAL P/N 277001240 TO SHOP. 2 L 7 3 4F A23WE 1998020500196 19980205 00196 NM 1998 2 5 DL72S980243 1 19980129 A 5720 651625523 FITTING BOEING 727 727232 1384082 NM WS 656 MISLOCATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 WHILE PERFORMING A REPAIR TO WING STR 9 PER MM 57-13-0, FIG 802 AT WS656.5 AN EXISTING HOLE ON THE TOP FLANGE OF THE RIB CHORD ASSY FALLS OUT IN THE RADIUS OF THE STRINGER TO RIB ATTACHMENT ANGLE. REWORKED PER ERA 331251-14AD. 2 L 7 3 4F A3WE 1998020500197 19980205 00197 WP 1998 2 5 DLL14980244 1 19980129 A 5720 DOUBLER LKHEED 1011 1011385115 5265015 WP WS 315-336 OVERSIZED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 AD95-20-04 MANDATES INSPECT OF WING UPPER SKIN SPLICE ON BOTH RT AND LT WING. APPROX 40 FASTENERS PER WING ARE TO BE IN SPECTED USING LFEC. DUE TO THE -250 MOD THERE IS AN EXTERNAL DOUBLER WHICH PREVENTS INSPECTION OF ALL FASTENERS, AS ALL FASTENERS WHERE NOT PICKED UP IN THE MOD DOUBLER (I.E., FLUSH UNDER DOUBLER). INSPECTED AND REWORKED PER ERA 331234-14 AD. 2 L 7 3 4F A23WE 1998020500198 19980205 00198 WP 1998 2 5 DLL14980245 1 19980129 A 5711 SPAR CAP LKHEED 1011 1011385115 5265015 WP WS 319 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1738D 193C1234 SEVERAL FASTENERS COMMON TO THE LT WING REAR SPAR UPPER CAP, WING SKIN, -250 MOD DOUBLER AND EXISTING EXTERNAL REPAIR DO UBLER WERE REMOVED PER EO 7-71199-12AD BEFORE REALIZING THE THE EO HAD BEEN SCHEDULED INCORRECTLY. HOWEVER, SOME HOLES WERE DAMAGED DURING FASTENER REMOVAL. REPAIRED PER ERA 331183-14AD. 2 L 7 3 4F A23WE 1998020500199 19980205 00199 NM 1998 2 5 DL72S980246 1 19980128 A 5521 FITTING BOEING 727 727232 1384082 NM RT ELEVATOR LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 HORIZONTAL STABILIZER, RT ELEVATOR, REPAIR FOR LOOSE HINGE FITTING. THE STA 81.44 HINGE FITTING ON THE RT ELEVATOR WAS FOUND. LOOSE DURING INSPECTIONS REQUIRED PER AD 96-06-05. THE LOOSE FITTING WAS TIGHTENED PER PROCEDURES IN BAC S/B 72 7-55-0089 AND DOCUMENTED PER ER/A 363884-14AD. 2 L 7 3 4F A3WE 1998020500200 19980205 00200 NM 1998 2 5 DL76G980249 1 19980128 A 3260 849704 PSEU BOEING 767 7673P6 1385105 NM E/E COMPT FAILED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 153DL 24985 EN ROUTE FLAP (TAKEOFF CONFIG) MESSAGE IN CRUISE FOR 10SEC. REOCCURRED WITH PROBE HEAT MESSAGE, THREE GEAR LIGHTS, FLAP WARNING AND NOSE A/G DISAGREE. NOSE GEAR A/G DISAGREE REMAINED ON THROUGHOUT REST OF FLIGHT. PSEU REPLACED AS SUSPECT COMPONENT AND AIRCRAFT TEST HOP ACCOMPLISHED, ALL SYSTEMS GOOD. 2 L 7 2 4F RT A1NM 1998020500202 19980205 00202 NM 1998 2 5 DHL9871787C 1 19980102 A 5344 65534333 FITTING BOEING 727 72723 1384004 NM CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 717DH 19389 AT C CHECK, LOWER AFT CARGO COMPT DOOR CUTOUT, LOWER FORWARD STOP FITTING CRACKED. REPLACED FITTING PER SRM 51-30-2, N/ R 3191. 2 L 7 3 4F A3WE 1998020500211 19980205 00211 SO 1998 2 5 98ZZZX446 2 19980116 A 8540 AN90028 GASKET CESSNA 421 421C 2076016 CE CONT O520 GTSIO520D 17032 SO OIL SCREEN FAILED A MOGA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 25 98437 421C0040 786025 ON TAKEOFF, PILOT NOTICED OIL ON RT COWLING. ACFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND AN900-28 GAS KET AT OIL SCREEN COVER ADAPTER LEAKING. GASKET WAS REPLACED AND ENGINE TEST RAN OK. 1 L 7 2 3O 3 O A7CE E7CE 1998020500216 19980205 00216 WP 1998 2 5 USAAD98001 1 19980104 A 2120 AIR DISTRIBUTION DOUG DC9 DC931 3022065 WP CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 973VJ 47099 PIT - FLT 942 - AFTER TAKEOFF, THE FLIGHT ATTENDANT REPORTED SMOKE SMELL IN THE LAVATORY. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE INLETS AND EXHAUSTS. THE ENGINES WERE RUN AT TAKEOFF POWER WI TH THE AIR BLEEDS OPERATED IN VARIOUS CONFIGURATIONS. NO ANOMALIES OR SMOKE WERE NOTED. THERE WERE NO OVERHEAT OR FIRE INDICATIONS. THE AIRCRAFT WAS THEN RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4F A6WE 1998020500241 19980205 00241 NM 1998 2 5 P2EA98002 1 19980102 A 7711 500790 PT7 LINE BOEING 737 737247 138448D NM NR 2 ENGINE BROKEN A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 05 912MP 19607 ATL - FLT 119 - NO EMERGENCY DECLARED. TAKEOFF ABORTED, ROLL OUT AND RETURN TO GATE NORMAL. ON TAKEOFF, THE RIGHT ENGI NE EPR FAILED TO GO ABOVE APPROX 1.6 EPR. BOTH ENGINE INDICATIONS WERE N1 - 98 PERCENT, N2 - 100 PERCENT EGT AT 500 DEG REES, TAKEOFF ABORTED. REPLACED BROKEN PT7 LINE AT 5 O'CLOCK POSITION. NR 2 ENGINE, LEAK AND OPS CHECK OK REF MM 71-09 -200. (M) 2 L 7 2 4F A16WE 1998020500242 19980205 00242 CE 1998 2 5 98ZZZX474 1 19980107 A 2160 12490411 TORQUE MOTOR LEAR 55 55LEAR 5170702 CE AFT COMPARTMENT SHORTED A A LBWA A UNSCHED LANDING B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP CR CRUISE 1 NE 03 126KD 6128 096 DURING CRUISE, COCKPIT FILLED WITH SMOKE AND HOT AIR AND A DUCT OVERHEAT CONDITION WAS OBSERVED. THE CREW WAS UNABLE TO CONTROL CABIN HEAT VIA COCKPIT TEMPERATURE CONTROL. THE CREW REDUCED POWER AND ALTITUDE IN ORDER TO REDUCE BLEED AIR F LOW THORUGH THE DUCT. THE AIRCRAFT DIVERTED TO THE NEAREST SUITABLE AIRPORT AND LANDED SAFELY. IT WAS LEARNED THAT TOR QUE MOTOR FAILED CAUSING UNCONTROLLABLE DUCT HEAT. 2 L 7 2 4F A10CE 1998020500298 19980205 00298 EU 1998 2 5 HAIHCMA0160 1 19980127 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU REAR ROTOR TORN E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 603 2889 REAR ROTOR LAMIFICATIONS ARE TORN BEYOND LIMITS . 1 G 7 1 3U H9EU 1998020500300 19980205 00300 SW 1998 2 5 HEEA0012494 1 19980106 A 7931 214060057103 SWITCH BELL 214 214ST 1182106 SW OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 OIL PRESS SWITCH FALSE PRESSURE INDICATION. 2 G 7 2 4U H10SW 1998020500301 19980205 00301 SW 1998 2 5 HEEA0012554 1 19980109 A 3340 407362005103 SWITCH BELL 407 407 SW LIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 404PH 60 53188 SWITCH INOPERATIVE. 1 G 7 1 3U O H2SW 1998020500302 19980205 00302 SW 1998 2 5 HEEA0012580 1 19980114 A 5302 1200591 SHIM BELL 212 212 1181420 SW TAILBOOM DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 PEELABLE SHIM BLOCKS MISSING FROM ONE END OF SHIM. SHIMS NOT SERVICEABLE AS IS 1 G 7 1 4U H4SW 1998020500303 19980205 00303 EU 1998 2 5 HEEA0012592 1 19980121 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4036H 305 2919 PITCH CONTROL ROD BEARING HAS PLAY. 1 G 7 1 3U H9EU 1998020500304 19980205 00304 SW 1998 2 5 HEEA0012598 1 19980122 A 6200 407010206103B SPRING BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 WORN BEARING. 1 G 7 1 3U O H2SW 1998020500305 19980205 00305 SW 1998 2 5 HEEA0012599 1 19980122 A 6200 407010206103A SPRING BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 WORN BEARING. 1 G 7 1 3U O H2SW 1998020500306 19980205 00306 EU 1998 2 5 HEEA0012604 1 19980122 A 6400 704A33633075 TUBE SNIAS 350 AS350B2 8680813 EU T/R REAR BAR SCORED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 4980 2771 LARGE SCORE ON TUBE BEYOND LIMITS. 1 G 7 1 3U H9EU 1998020500307 19980205 00307 SW 1998 2 5 HEEA0012630 1 19980126 A 6240 214074280105 DETECTOR BELL 214 214ST 1182106 SW ROTOR RPM FAILED E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 5748M 28102 LOW ROTOR LIGHT WILL NOT COME ON. 2 G 7 2 4U H10SW 1998020500308 19980205 00308 SW 1998 2 5 HEEA0012631 1 19980126 A 7722 212075067109 INDICATOR BELL 412 412 1182202 SW ENG ITT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141PH 33197 ITT INDICATOR WHEN HOT UNIT STICKS AT ZERO. 1 G 7 2 4U H4SW 1998020500309 19980205 00309 EU 1998 2 5 HEEA0012632 1 19980126 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B1 5626012 EU TORQUE IND DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 PRESS TRANSDUCER CAUSES 30% SPLIT INTERMITTENTLY. 1 G 7 2 3U H13EU 1998020500310 19980205 00310 1998 2 5 HEEA0012633 4 19980126 A 3424 GG2479AB03 GYRO BELL 412 412 1182202 SW TURN RATE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 RATE OF TURN NEEDLE INOPERATIVE. GYRO FAILED 1 G 7 2 4U H4SW 1998020500311 19980205 00311 CE 1998 2 5 HEEA0012634 1 19980126 A 2430 51530007B PANEL BEECH 200 200BEECH 1152920 CE GEN CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30PH BB635 GEN CONTROL PANEL FAILED. WOULD NOT LET BOTH GENERATORS ON LINE. 1 L 7 2 4T A24CE 1998020500312 19980205 00312 CE 1998 2 5 HEEA0012635 1 19980126 A 2434 230481030 ARMATURE BEECH 200 200BEECH 1152920 CE DC GEN ALT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 789DS BB478 BEARING FAILURE, ARMATURE SHORTED. 1 L 7 2 4T A24CE 1998020500313 19980205 00313 EU 1998 2 5 HEEA0012636 1 19980126 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117B2 5626013 EU TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 TRANSDUCER OUTPUT IS 1 VOLT CONTINUOUSLY. 1 G 7 2 3U NC H13EU 1998020500314 19980205 00314 SW 1998 2 5 HEEA0012637 1 19980126 A 2437 214175250103 INDICATOR BELL 214 214ST 1182106 SW DC IND FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 INDICATOR FLUCTUATES. 2 G 7 2 4U H10SW 1998020500315 19980205 00315 EU 1998 2 5 HEEA0012638 1 19980126 A 7714 1179405303 INDICATOR BOLKMS 117 BK117A4 5626017 EU TRIPLE TACH FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 NR2 NEEDLE WILL FLUCTUATE INTERMITTENTLY. 1 G 7 2 3U H13EU 1998020500316 19980205 00316 1998 2 5 HEEA0012639 4 19980126 A 2562 ELT1104 ELT NARCO BOLKMS 117 BK117A4 5626017 EU COCKPIT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 NARCO ELT CRACKED. SENT TO ARTEX AIRCRAFT SUPPLIES FOR INSPECTION AND REPAIR. 1 G 7 2 3U H13EU 1998020500317 19980205 00317 NE 1998 2 5 HEEA0012640 1 19980126 A 3500 50C002410 INDICATOR SKRSKY S76 S76A 8143006 NE OXY SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 INDICATOR INOPERATIVE. 1 G 7 2 3U H1NE 1998020500318 19980205 00318 SW 1998 2 5 HEEA0012641 1 19980126 A 2436 206075447007 REGULATOR BELL 206 206L3 1182108 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54641 51184 GENERATOR WILL NOT COME ON LINE. REG FAILED 1 G 7 1 3U H2SW 1998020500319 19980205 00319 SW 1998 2 5 HEEA0012642 1 19980126 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 TRIPLE TACH INDICATOR SPLIT AND EXCESSIVE FRICTION ERROR. 1 G 7 2 4U H4SW 1998020500320 19980205 00320 SW 1998 2 5 HEEA0012643 1 19980126 A 2822 205060606003 PUMP BELL 412 412 1182202 SW FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA PUMP CAUSING PRESSURE FLUCTUATION. EXTREMELY NOISY. 1 G 7 2 4U H4SW 1998020500321 19980205 00321 EU 1998 2 5 HEEA0012644 1 19980126 A 7714 65011035 INDICATOR BOLKMS 105 BO105S 5626006 EU TACH INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL S717 TACH INDICATOR INTERMITTENT OPERATION. 1 G 7 2 3U H3EU 1998020500322 19980205 00322 EU 1998 2 5 HEEA0012645 1 19980126 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ROTOR FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5421E S806 TORQ TRANSMITTER WILL NOT CALIBRATE OR TEST. 1 G 7 2 3U H3EU 1998020500323 19980205 00323 EU 1998 2 5 HEEA0012646 1 19980126 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5421E S806 MAST MOMENT INDICATOR WILL NOT CALIBRATE OR TEST. 1 G 7 2 3U H3EU 1998020500324 19980205 00324 EU 1998 2 5 HEEA0012647 1 19980126 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E S806 TORQUE TRANSMITTER READS HIGH OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1998020500325 19980205 00325 EU 1998 2 5 HEEA0012648 1 19980126 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E S806 MAST MOMENT INDICATOR READS HIGH OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1998020500326 19980205 00326 SW 1998 2 5 HEEA0012649 1 19980126 A 2842 EA4703587 PROBE BELL 206 206B3 1181506 SW TANK UNIT LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39122 3312 TANK UNIT HEAD IS LOOSE FROM TUBE. 1 G 7 1 3U H2SW 1998020500327 19980205 00327 SW 1998 2 5 HEEA0012650 1 19980126 A 2822 164A199 PUMP BELL 206 206L1 1182107 SW FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5017G 45228 BOOST PUMP HAS GRINDING NOISE AND INTERMITTENT LIGHT. 1 G 7 1 3U H2SW 1998020500328 19980205 00328 SW 1998 2 5 HEEA0012651 1 19980126 A 7714 206070266009 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406EH 45183 INDICATOR STICKING AND EXCESSIVE FRICTION ERROR. 1 G 7 1 3U H2SW 1998020500329 19980205 00329 1998 2 5 HEEA0012652 4 19980126 A 3421 206075606103 GYRO BELL 407 407 SW COCKPIT DG FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DIR GYRO PRECESSES. 1 G 7 1 3U O H2SW 1998020500330 19980205 00330 SW 1998 2 5 HEEA0012653 1 19980126 A 3340 A490ATSDF1428 POWER SUPPLY WHELEN BELL 206 206L1 1182107 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1076T 45373 POWER SUPPLY WILL NOT BUILD UP POWER. 1 G 7 1 3U H2SW 1998020500331 19980205 00331 NE 1998 2 5 HEEA0012654 1 19980126 A 3230 4608 VALVE SKRSKY S76 S76A 8143006 NE MLG LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1546K 760082 PRIORITY VALVE LEAKING. 1 G 7 2 3U H1NE 1998020500332 19980205 00332 NE 1998 2 5 HEEA0012655 1 19980126 A 3230 4608 VALVE SKRSKY S76 S76A 8143006 NE MLG LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4253S 760035 PRIORITY VALVE LEAKING. 1 G 7 2 3U H1NE 1998020500333 19980205 00333 NE 1998 2 5 HEEA0012656 1 19980126 A 6220 7610608000049 DAMPER SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 M/R DAMPER WEAR SPOT ON PISTON. 1 G 7 2 3U H1NE 1998020500334 19980205 00334 NE 1998 2 5 HEEA0012657 1 19980126 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 M/R DAMPER WEAK. 1 G 7 2 3U H1NE 1998020500335 19980205 00335 SW 1998 2 5 HEEA0012658 1 19980126 A 2430 200SGL1156 STATOR ASSY BELL 206 206L3 1182108 SW DC SYS SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 STATOR ASSY SHORTED TO GROUND. FAILED HY-POT TEST. 1 G 7 1 3U H2SW 1998020500336 19980205 00336 1998 2 5 HEEA0012659 4 19980126 A 3422 060001500 GYRO KG102A BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 92MT 51175 GYRO INOPERATIVE, CARD DOES NOT MOVE. 1 G 7 1 3U H2SW 1998020500337 19980205 00337 1998 2 5 HEEA0012660 4 19980126 A 3425 066304604 INDICATOR KI525A HUGHES 269 269C 4470504 WP COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102LU S1548 HEADING INDICATOR INOPERATIVE. 1 G 7 1 3O 4H12 1998020500338 19980205 00338 SW 1998 2 5 HEEA0012661 1 19980126 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 STEP ACTUATOR POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1998020500339 19980205 00339 SW 1998 2 5 HEEA0012662 1 19980126 A 7712 222375077111 TRANSMITTER BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 TRANSMITTER PEGGED ON MAX. 2 G 7 2 4U H10SW 1998020500340 19980205 00340 1998 2 5 HEEA0012663 4 19980126 A 3414 214175299107 INDICATOR BELL 214 214ST 1182106 SW COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 AIR SPEED NEEDLE STICKS. 2 G 7 2 4U H10SW 1998020500341 19980205 00341 NE 1998 2 5 HEEA0012664 1 19980126 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 M/R DAMPER WEAK. 1 G 7 2 3U H1NE 1998020500342 19980205 00342 EU 1998 2 5 HEEA0012665 1 19980126 A 7921 37010200004 OIL COOLER BOLKMS 105 BO105S 5626006 EU ENGINE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 967MB S737 OIL COOLER LEAKING. 1 G 7 2 3U H3EU 1998020500343 19980205 00343 SW 1998 2 5 HEEA0012666 1 19980126 A 2820 2C271 CARTRIDGE BELL 206 206L1 1182107 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5005B 45175 FUEL CARTRIDGE POPS CIRCUIT BREAKER. 1 G 7 1 3U H2SW 1998020500344 19980205 00344 SW 1998 2 5 HEEA0012667 1 19980126 A 6240 206076373001 TACH GENERATOR BELL 206 206L1 1182107 SW ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251Z 45756 TACH GEN HAS NO ROTOR NEEDLE INDICATION. 1 G 7 1 3U H2SW 1998020500345 19980205 00345 SW 1998 2 5 HEEA0012668 1 19980126 A 6710 206062721113 ACTUATOR BELL 206 206B3 1181506 SW DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Q 3625 ACTUATOR POPS CIRCUIT BREAKER. 1 G 7 1 3U H2SW 1998020500346 19980205 00346 SW 1998 2 5 HEEA0012671 1 19980126 A 6240 206076373001 TACH GENERATOR BELL 206 206L1 1182107 SW ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11027 45411 TACH GEN FAILED. LOW RPM AUDIO SOUNDS INTERMITTENTLY. 1 G 7 1 3U H2SW 1998020500347 19980205 00347 SW 1998 2 5 HEEA0012672 1 19980126 A 6710 206062721109 ACTUATOR BELL 206 206L4 1182110 SW DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 52037 ACTUATOR ARM EXTENDS AND THEN RETRACTS WHEN KEPT UP. 1 G 7 1 3U NC H2SW 1998020500348 19980205 00348 NM 1998 2 5 W8PA980035 1 19980130 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM CABIN DISCONNECTED A W8PA K NONE L NO TEST IN INSP/MAINT 1 NM 03 956WP 24299 DEN- EMERGENCY TRACK LIGHTING AT ROWS 16 TO 19 IS INOP. REINSTALLED TRACK LIGHTING, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1998020500349 19980205 00349 SO 1998 2 5 RAAA98E4003 1 19980131 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 167 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND LEFT WING UPPER NR 7 PANEL CORRODED AT WS 167. REPAIRED PER SRM 57-2-1 FIG 3, SHEET 11 AND 57-2-1, FIG 3, SHEET 26. M-54 NR 33. 2 L 7 4 4T 4A22 1998020500350 19980205 00350 SO 1998 2 5 RAAA98E4004 1 19980131 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 213 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND RIGHT WING LOWER NR 3 PANEL CORRODED AT WS 213. REPAIRED PER SRM 57-2-1 FIG 3, SHEET S 12 THRU 15. M-54 NR 35. 2 L 7 4 4T 4A22 1998020500351 19980205 00351 SO 1998 2 5 RAAA98E8002 1 19980129 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998020500352 19980205 00352 NM 1998 2 5 CALA9800142 1 19980131 A 3230 69141063 TRANS CYLINDER BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 12322 23373 WHEN GEAR HANDLE WAS SELECTED DOWN ON APPROACH, THE GEAR DID NOT EXTEND ON INITIAL ATTEMPT. THE GEAR WAS CYCLED AND EXT ENDED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE NLG TRANSFER CYLINDER AND NLG MODULAR PACKAGE WERE REMOVED AN D REPLACED IAW MM 32-33-31 AND 32-33-41. A LANDING GEAR EXTENSION AND RETRACTION TEST WAS PERFORMED IAW MM 32-33-00 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998020500353 19980205 00353 NM 1998 2 5 CALA9800143 1 19980131 A 3350 1000679 LIGHT GRIMES BOEING 727 727243 138408D NM COCKPIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17410 11809 21663 INSPECTION FOUND EMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. THE EXIT LIGHT WAS REMOVED AND REPLACED. 2 L 7 3 4F RT A3WE 1998020500354 19980205 00354 WP 1998 2 5 CALA9800144 1 19980131 A 2120 38003681 AIR DISTRIBUTION GARRETT DOUG DC9 DC982 3022082 WP CABIN SMOKE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 09 936AS 43776 49363 THE FLIGHT ATTENDANTS REPORTED HAZE IN CABIN WHILE ON DESCENT. BOTH PACKS WERE RUN ON AIR CART WITH CABIN AND PACKS CHE CKING GOOD. THE APU WAS RUN ALL NIGHT WITH PACKS ON. NO SMOKE IN CABIN OR LEAKS AT APU WERE NOTED. 2 L 7 2 4F A6WE 1998020500355 19980205 00355 NM 1998 2 5 CALA9800145 1 19980201 A 5730 PANEL BOEING 737 7373Q8 1384670 NM RT WING LEAKING A CALA O OTHER K FLUID LOSS CR CRUISE 1 SW 09 14384 26313 A FUEL LEAK FROM RT WING OVERWING FUEL TANK ACCESS PANEL LOCATED IN LINE WITH RIGHT ENGINE PYLON WAS OBSERVED WHILE EN R OUTE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND SEVERAL LOOSE FASTENERS AND ONE STRIPPED NUT PLAT E. THE PANEL WAS REMOVED AND THE NUT PLATE WAS REPLACED AND SEALED. A NEW PANEL AND SEAL WERE INSTALLED, LEAK CHECK WA S GOOD. 2 L 7 2 4F RT A16WE 1998020500356 19980205 00356 NM 1998 2 5 UPS98225628 1 19980111 A 5753 FLAP TRACK BOEING 727 72722C 138400F NM NR 3 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 3 FLAP TRACK CORROSION PAD B. CORROSION REMOVED AND REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 9 8-01-015. 2 L 7 3 4F A3WE 1998020500357 19980205 00357 NM 1998 2 5 UPS98225629 1 19980128 A 5400 TEE BOEING 727 72722C 138400F NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CRACK ON VERTICAL ANGLE ABOVE NR 2 ENGINE HORIZONTAL FIREWALL, LT SIDE AT STATION 1409 NR 2 ENGINE AF T MOUNT SUPPORT RIB CHORD. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-01-012R1. 2 L 7 3 4F A3WE 1998020500358 19980205 00358 NM 1998 2 5 UPS98225631 1 19980126 A 2710 FITTING BOEING 727 72722C 138400F NM WS 357 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, RT I/B AILERON TURNAROUND FITTING HAS CORROSION AROUND LOWER PULLEY MOUNT HOLE. RT I/B AILERON TURNA ROUND FITTING REPLACED IAW SRM 51-10-1 ADN MM20 -80-1. 2 L 7 3 4F A3WE 1998020500359 19980205 00359 NM 1998 2 5 UPS98225636 1 19980129 A 5230 BOLT BOEING 727 72722C 138400F NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, MAIN CARGO DOOR AFT HINGE BOLT ON PRESS RELIEF DOOR BADLY CORRODED. MAIN CARGO DOOR BOLT AND BUSHING REPLACED PER STANDARD PRACTICES 20- 50-01. 2 L 7 3 4F A3WE 1998020500360 19980205 00360 NM 1998 2 5 UPS98225637 1 19980127 A 5520 HINGE LUG BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, RT ELEVATOR NR 3 HINGE LUG ES 66.50 CRACKED. HINGE LUG FITTING REPAIRED IAW SRS ENGINEERING ORDER 98 -01-014. 2 L 7 3 4F A3WE 1998020500361 19980205 00361 NM 1998 2 5 UPS98225638 1 19980128 A 5520 65727841 REAR SPAR BOEING 727 72722C 138400F NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, LT ELEVATOR HAS CRACKED REAR SPAR, CRACKED HINGE LUG, AND CRACKED LOWER SKIN. REPLACEMENT ELEVATOR I NSTALLED IAW MM27-30-01. 2 L 7 3 4F A3WE 1998020500362 19980205 00362 NM 1998 2 5 UPS98225641 1 19980128 A 5753 CARRIAGE BOEING 727 72722C 138400F NM NR 3 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 3 FLAP CARRIAGE IS CORRODED IN SPINDLE BORE AND AROUND LARGE BEARING. SEAT CARRIAGE REPLACED IAW OHM 57-58-01. 2 L 7 3 4F A3WE 1998020500363 19980205 00363 NM 1998 2 5 UPS98225643 1 19980115 A 5520 STIFFENER BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, RIGHT HAND ELEVATOR ES 103.5 HAS CRACK IN LOWER SKIN STIFFENER IN REPAIRED AREA 19 FWD OF TRAILING ED GE. REPAIR CARRIED OUT IAW SRS EO 98-01-008. 2 L 7 3 4F A3WE 1998020500364 19980205 00364 NM 1998 2 5 UPS98225645 1 19980128 A 5320 65159682 FITTING BOEING 727 72722C 138400F NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, RT BS 740 FUSELAGE FITTING HAS NEW CRACK ON LOWER OUTBD WEB FLANGE (VERTICAL). FITTING REMOVED AND N EW FITTING INSTALLED PER UPS ENGINEERING ORDER B727-5310-7477C. 2 L 7 3 4F A3WE 1998020500365 19980205 00365 NM 1998 2 5 UPS98225647 1 19980123 A 5753 CARRIAGE BOEING 727 72722C 138400F NM NR 4 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 4 FLAP CARRIAGE DEAD WEIGHT ROLLER HOLES ON I/B AND O/B SIDES ARE CORRODED. HOLES OVERSIZED PER O HM 57-58-02. BUSHINGS MANUFACTURED AND INSTALLED PER OHM 57-58-02. 2 L 7 3 4F A3WE 1998020500366 19980205 00366 NM 1998 2 5 UPS98225649 1 19980122 A 5730 66171751 ACCESS PANEL BOEING 727 72722C 138400F NM NR 1 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, NR 1 FUEL ACCESS PANEL HAS CORROSION RT WING. FUEL ACCESS PANEL REPLACED IAW MM 28-11-21. 2 L 7 3 4F A3WE 1998020500367 19980205 00367 NM 1998 2 5 UPS98225650 1 19980129 A 2710 CASTING BOEING 727 72722C 138400F NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, LT I/B AILERON TURNAROUND FITTING HAS CORROSION AROUND LOWER PULLEY MOUNT HOLE. CASTING REPLACED IA W SRM 51-10-1 AND MM 20-80-1. 2 L 7 3 4F A3WE 1998020500368 19980205 00368 NM 1998 2 5 UPS98225652 1 19980129 A 5230 WEB BOEING 727 72722C 138400F NM CARGO COMPT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, ON FURTHER INSPECTION OF DAMAGED ANCHOR NUTS EXTRUSION WAS CORRODED AND WEB DAMAGED. REPLACED EXTRUS ION WITH 65-24258-1 IAW DRAWING 65C33855. 2 L 7 3 4F A3WE 1998020500369 19980205 00369 NM 1998 2 5 UPS98225653 1 19980130 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1090 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CORROSION BETWEEN INTERNAL STRUCTURE AND SKIN DOUBLER BS 1090 STR 18R. CORROSION REMOVED IAW SRM 51- 10-6. REPAIR CARRIED OUT IAW SRS EO 98 -01-025 R1. 2 L 7 3 4F A3WE 1998020500370 19980205 00370 NM 1998 2 5 UPS98225654 1 19980130 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1115 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND STRUCTURE AT BS 1115 BETWEEN S18R AND S19R. REPAIRED IAW SRS EO 9 8-01-025R1. 2 L 7 3 4F A3WE 1998020500371 19980205 00371 NM 1998 2 5 UPS98225656 1 19980130 A 5320 65229136 TEE BOEING 727 72722C 138400F NM BS 1409 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CRACK ON ANGLE ABOVE NR 2 ENGINE HORIZONTAL FIREWALL AT STATION 1409 RT SIDE (NR 2 ENG AFT MOUNT SUPP ORT RIB CHORD). SUPPORT RIB TEE CHORD REPLACED IAW DRAWING 65-22913 AND 65-17551. 2 L 7 3 4F A3WE 1998020500372 19980205 00372 WP 1998 2 5 UPS98825633 1 19980119 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 879 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LONGERON 24R FITTING AT FS 879 HAS CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-2-0. 2 L 7 4 4F RT 4A25 1998020500373 19980205 00373 WP 1998 2 5 UPS98825634 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 840-940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, SEAT TRACK AT LBL 44 FS 840 AND 940 CORRODED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTION OF TRACK IAW ADDN DC8-5320-8309-B. 2 L 7 4 4F RT 4A25 1998020500374 19980205 00374 WP 1998 2 5 UPS98825635 1 19980120 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, FS 1180 BTWN STR 35R TO 36 STR TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998020500375 19980205 00375 WP 1998 2 5 UPS98825639 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 648 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, MAIN CABIN AT FS 648 RBL 59.5 THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW DC8-5320- 5167-C. 2 L 7 4 4F RT 4A25 1998020500376 19980205 00376 WP 1998 2 5 UPS98825642 1 19980119 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, RT WING L/E AT STA XFS 772.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500377 19980205 00377 WP 1998 2 5 UPS98825644 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1138-1210 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, MAIN CABIN FS 1138 TO 1147 AND 1210 RBL 44, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 53-7-2. 2 L 7 4 4F RT 4A25 1998020500378 19980205 00378 WP 1998 2 5 UPS98825646 1 19980118 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB CRACKED ON LWR ARM BY AFT FASTENER STA 616.250. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998020500379 19980205 00379 WP 1998 2 5 UPS98825648 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, SEAT TRACK AT PLUG SLIT/CRACKED LBL 44 FS 600. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM ADDN DC8-5320-8309-B. 2 L 7 4 4F RT 4A25 1998020500381 19980205 00381 WP 1998 2 5 UPS98825658 1 19980105 A 5320 5641008501 FITTING DOUG DC8 DC873F 302199F WP BS 798.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FLOORBEAM TO CENTER WING BOX ATTACH FITTING CRACKED FS 798.5 LBL 47. REMOVED AND REPLACED FITTING IA W SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998020500382 19980205 00382 EU 1998 2 5 WWMA9800018 1 19980129 A 3350 26A00593600 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A WWMA K NONE O OTHER TX TAXI/GRND HDL 1 WP 15 356SB 340B356 LEFT EMEREGENCY EXIT LIGHT REPORTED BROKEN. REPLACED THE LEFT OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. 2 L 7 2 4T RT A52EU 1998020500383 19980205 00383 EU 1998 2 5 QXEA9800051 1 19980129 A 3350 5515900004 PRINTED CIRCUIT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 PDX - OVERHEAD EXIT LIGHT AT ROW 8 INOP. REPLACED EXIT LIGHT CIRCUIT BOARD, OPERATIONAL TEST SATISFACTORY. 2 L 7 2 4F RT A20EU 1998020500384 19980205 00384 EU 1998 2 5 QXEA9800052 1 19980129 A 3350 1312 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 PDX - EMERGENCY LIGHT 8 A/B INOP. RELAMPED, OP CHECK GOOD. 2 L 7 2 4F RT A20EU 1998020500386 19980205 00386 NM 1998 2 5 98FDEA00068 1 19980131 A 5341 651621928 FITTING BOEING 727 72721C 138400M NM BS 867 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 CORROSION (C57-174-01) ON RT BOTTLE PIN CASTING BS 867, WL 176 TO 170, RBL 65, WHILE WORKING NR 0734. *S/D* REMOVED AN D REPLACED FITTING AT BS 867, WL 176 TO 170, RBL 65 IAW FED-EX EA 7-5310-37362A. 2 L 7 3 4F A3WE 1998020500387 19980205 00387 NM 1998 2 5 98FDEA00069 1 19980131 A 5320 65C352491 FITTING BOEING 727 72721C 138400M NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 CRACKED AND CORRODED INDICATION NOTED BS 870 ROW NR 2 HOLES NR 5 LEFT HAND SIDE. *S/D* REPAIRED CRACK/CORROSION IN HOL E NR 5 ROW 2 BS 870 LEFT HAND PER EA NR 7-5330-38748. 2 L 7 3 4F A3WE 1998020500388 19980205 00388 NM 1998 2 5 98FDEA00070 1 19980131 A 5620 651985126 WINDOW FORGING BOEING 727 72721C 138400M NM BS 870-890 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 NR 0933 055, WHILE WORKING NR 0537, FOUND WINDOW FORGING BS 870-890, STR 10-14 RT TO BE CORRODED. REPAIRED WINDOW FORGI NG BS 870-890, STR 10-14 RT IAW FED-EX EA NR 7-5310-37418. 2 L 7 3 4F A3WE 1998020500389 19980205 00389 NM 1998 2 5 98FDEA00071 1 19980131 A 5313 BAC1498160 STRINGER BOEING 727 72721C 138400M NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 CORROSION (C53-224-01) ON STRINGER, BS 870 TO 950, STR 2 RT. *S/D* REPAIRED STRINGER 2 RT, BS 870 TO 950 PER FED-EX SR M 53-10-3. 2 L 7 3 4F A3WE 1998020500390 19980205 00390 NM 1998 2 5 98FDEA00072 1 19980131 A 5311 65C352492 FRAME BOEING 727 72721C 138400M NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 NR 0537 052, CRACK/CORRODED INDICATION NOTED BS 870, ROW 2 HOLE NR 1 RIGHT. ALSO, ROW 3, HOLES 1, 2, 3 AND 5. REPAIRED CRACK AND CORROSION INDICATIONS RT BS 870 ROW 2 HOLE NR 1 AND ROW 3 HOLES NR 1, 2, 3 AND NR 5 BY ACCOMPLISHING RT BS 87 0 TERMINAL FITTING PARTIAL REPLACEMENT IAW FED-EX EA 7-5310-37481 AND 7-5100-37427. 2 L 7 3 4F A3WE 1998020500391 19980205 00391 NM 1998 2 5 98FDEA00073 1 19980127 A 5313 STRINGER BOEING 727 727233 138408A NM BS 520 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 FWD CARGO STRINGER 26L CRACKED AT BS 520. REMOVED DAMAGED AREA OF STRINGER AND SPICED IN NEW SECTION PER SRM 53-10-3 PA GE 4B. 2 L 7 3 4F RT A3WE 1998020500392 19980205 00392 NM 1998 2 5 98FDEA00074 1 19980202 A 5320 DOUBLER BOEING 727 7272S2F 1384O81 NM PAX DOORWAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 FWD ENTRY DOOR CUTOUT LOWER HINGE CUTOUT HAS BEEN CUTOUT BEYOND FUSELAGE SKIN AND DEEP INTO BEAR STRAP AT FWD SECTION OF HINGE CUTOUT. INSTALLED LOWER HINGE CUTOUT DOUBLER PER S/B 727-53-0198 REV 1 AND EA 7-5330-29333. 2 L 7 3 4F A3WE 1998020500393 19980205 00393 NM 1998 2 5 98FDEA00075 1 19980202 A 5320 DOUBLER BOEING 727 7272S2F 1384O81 NM PAX DOORWAY DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 FWD ENTRY DOOR CUTOUT UPPER HINGE AREA HAS BEEN CUTOUT PAST FUSELAGE SKIN AND DEEP INTO BEAR STRAP AT FWD SECTION OF HIN GE CUTOUT. INSTALL UPPER HINGE CUTOUT DOUBLER PER S/B 727-53-0198 REV 1 AND EA 7-5330-29333. 2 L 7 3 4F A3WE 1998020500394 19980205 00394 NM 1998 2 5 98FDEA00076 1 19980202 A 5320 DOUBLER BOEING 727 7272S2F 1384O81 NM BS 600 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 UPPER LOBE, BS 600, RBL 66, FRAME DAMAGED APPROXIMATELY 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998020500395 19980205 00395 NM 1998 2 5 98FDEA00077 1 19980202 A 5320 DOUBLER BOEING 727 7272S2F 1384O81 NM BS 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 UPPER LOBE, BS 500, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998020500396 19980205 00396 NM 1998 2 5 98FDEA00078 1 19980202 A 5320 DOUBLER BOEING 727 7272S2F 1384O81 NM BS 520 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 UPPER LOBE, BS 520, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998020500397 19980205 00397 NM 1998 2 5 98FDEA00079 1 19980202 A 5320 DOUBLER BOEING 727 7272S2F 1384O81 NM BS 540 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 210FE 22932 UPPER LOBE BS 540, RBL 66 FRAME DAMAGED APPROX 5 ABOVE FLOOR. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998020500398 19980205 00398 WP 1998 2 5 DLL10980239 1 19980129 A 2560 MEGAPHONE MV10 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 727DA 193C1167 FOUND FWD MEGAPHONE CONTINUOUSLY SQUEALING IN CRADLE. REPLACED MEGAPHONE. 2 L 7 3 4F A23WE 1998020500399 19980205 00399 NM 1998 2 5 DL73K980240 1 19980129 A 3350 276005 FUSE BOEING 737 737232 1384475 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 308DL 23080 EMERGENCY LIGHT EXIT SIGN ABOVE L2 DOOR WOULD NOT TEST. REPLACED FUSE. 2 L 7 2 4F RT A16WE 1998020500400 19980205 00400 NM 1998 2 5 DL757980247 1 19980129 A 5754 114N4003186 WEDGE BOEING 757 757232 1384965 NM NR 9 LE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 682DA 26958 THE NR 9 SLAT ON THE RT WING WAS FOUND WITH 1.25 AREA OF DELAMINATION ON THE TRAILING EDGE WEDGE, 39 FROM THE OUTBD END. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363885-14AD. 2 L 7 2 4F RT A2NM 1998020500401 19980205 00401 NM 1998 2 5 DL76G980251 1 19980129 A 3350 POWER SUPPLY BPS73 BOEING 767 7673P6 1385105 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 155DL 42525 25269 F/C EMERGENCY TRACK LIGHTS INOP. REPLACED POWER SUPPLY SYS, CKS NML. 2 L 7 2 4F RT A1NM 1998020500402 19980205 00402 NM 1998 2 5 DL72S980254 1 19980129 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z VA6193 21858 RIGHT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK, CK'S GOOD. 2 L 7 3 4F A3WE 1998020500403 19980205 00403 NE 1998 2 5 DL73E980256 2 19980128 A 7260 GEARBOX BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A A DALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 381DL 33359 23608 709138 AT 2000 FT MSL AND 190 KTS NR 2 ENGINE HAD A COMPRESSOR STALL AND ENGINE POWER WAS REDUCED TO IDLE. ENGINE WAS SHUTDOWN WHEN F/A NOTICED METAL STICKING OUT OF INLET. MTC FOUND NOSE BULLET HAD BROKE OFF AND LODGED ITSELF IN THE INLET GUIDE . REPLACED GEARBOX AND DOME ASSY, BOROSCOPE SHOWED NO DAMAGE TO ENGINE. 2 L 7 2 4F 4 F A16WE E2EA 1998020500404 19980205 00404 NE 1998 2 5 DLL15980257 2 19980130 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 1 MALFUNCTIONED A DALA E ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 754DL 45302 193Y1181 14867 NR 1 ENG ROLLED BACK DURING ENG START AND HAD SUBSEQUENT TAILPIPE FIRE. INSPECTED ENG, NO DEFECTS NOTED. STARTED NR 1 ENG WAS SUCCESSFUL. 2 L 7 3 4F 4 F A23WE E12EU 1998020500405 19980205 00405 WP 1998 2 5 DLL17980259 1 19980129 A 2612 FIRE LOOP LKHEED 1011 10113853 5265020 WP NR 3 ENGINE LOOSE A DALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 27 769DL 30909 193H1218 14771 NR 3 ENG SHUT DOWN DUE TO FIRE INDICATION, FIRE WARNING. ENG SHUT DOWN PER PROCEDURE. CLEANED AND RETORQUED LOOP CONNE CTORS, CHECKS NORMAL. 2 L 7 3 4F A23WE 1998020500406 19980205 00406 NM 1998 2 5 DL73E980260 1 19980128 A 5312 65163007 BULKHEAD WEB BOEING 737 737247 138448D NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 243WA 23517 STA 178 BULKHEAD WEB WAS FOUND WITH CRACKS IN THE TYP LOCATIONS AT LBL 5.7 AND RBL 5.7. THE CRACKS WERE TRIMMED OUT WIT H 1 X 4 CUTOUTS. THE DAMAGED AREAS WERE REPAIRED WITH SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 363850-12, REV A. 2 L 7 2 4F A16WE 1998020500407 19980205 00407 NM 1998 2 5 DL72S980261 1 19980130 A 3230 SEQUENCE VALVE 1U10851 BOEING 727 727232 1384082 NM RT MLG CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 523DA 3092A 21583 14771 EXPERIENCED COMPLETE A-SYSTEM HYDRAULIC LOSS UPON GEAR RETRACTION AFTER TAKEOFF. REPLACED MAIN GEAR LOCK OPERATED SEQUE NCE VALVE. 2 L 7 3 4F A3WE 1998020500408 19980205 00408 NM 1998 2 5 DLM88980262 1 19980129 A 5330 99581561 SKIN DOUG MD88 MD88 3023688 NM FUSELAGE DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 942DL 49815 THE LT FUSELAGE WINDOW BELT SKIN AT WINDOWS 11, 13 AND 15 SUFFERED LIGHTNING DAMAGE TO THE UPPER CORNERS OF THE WINDOW C UTOUTS. THE DAMAGES WERE REPAIRED WITH A ONE-PIECE DOUBLER PER THE GUIDLINES OF DAC SRO9530053 AND ER/A 360060-14, REV F. 2 L 7 2 4F RT A6WE 1998020500409 19980205 00409 NM 1998 2 5 DLM88980263 1 19980130 A 3244 TIRE DOUG MD88 MD88 3023688 NM NR 1 FAILED A DALA O OTHER O OTHER LD LANDING 1 SO 27 911DE 49967 AFTER TOUCHDOWN AT APPROX 133 KTS CREW FELT A HARD SHUDDER AND A/C STARTED TO PULL TO LEFT. NO OTHER INDICATIONS IN THE COCKPIT OR ON THE ENGINES. NR 1 TIRE FAILED. 2 L 7 2 4F RT A6WE 1998020500410 19980205 00410 WP 1998 2 5 DLL10980264 1 19980130 A 3320 100477111 BALLAST LKHEED 1011 10113851 5265010 WP LAVATORY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 718DA 477 193C1097 BURNING ELECTRICAL SMELL 1ST CLASS LAV CAPT'S SIDE. REPLACED BALLAST, CHECK NORMAL. 2 L 7 3 4F A23WE 1998020500411 19980205 00411 WP 1998 2 5 DLL19980265 1 19980130 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 761DA 37814 193Y1208 EMERGENCY EXTERNAL LIGHTS AT L-2 DOOR INOP. REPLACED BATTERY PACK AT SEATS 12AB. 2 L 7 3 4F A23WE 1998020500412 19980205 00412 NM 1998 2 5 DL72L980266 1 19980130 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 505DA 21307 14771 L-2 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, CKS GOOD. 2 L 7 3 4F A3WE 1998020500413 19980205 00413 WP 1998 2 5 DLL17980267 1 19980130 A 3350 RPS1 PWR SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 769DL 193H1218 FLOOR E-PATH LIGHTS INOP ON TEST. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998020500414 19980205 00414 WP 1998 2 5 DLL13980268 1 19980130 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 FOUND DURING LAYOVER EMERGENCY EXIT SIGNS BY 2R DOOR INOP. POWER SUPPLY WAS REPLACED AND LIGHT OPERATION WAS NORMAL. 2 L 7 3 4F A23WE 1998020500415 19980205 00415 WP 1998 2 5 DLL10980269 1 19980131 A 3350 305 BULB LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 193C1226 LT SIDE EMERGENCY LIGHT AT WING RT INOP. RELAMPED, CKS GOOD. 2 L 7 3 4F A23WE 1998020500416 19980205 00416 WP 1998 2 5 DLL19980273 1 19980131 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 756DR 193Y1185 NR 5 BATT PACK (EMERGENCY LIGHT) WILL NOT HOLD CHARGE. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998020500417 19980205 00417 NM 1998 2 5 DHL98715001 1 19980129 A 7932 CONNECTOR BOEING 727 727155C 138404Z NM NR 2 ENGINE DIRTY A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 715DH 19618 ON CLIMBOUT, NR 2 ENGINE OIL QUANTITY DROPPED TO ZERO. CLEANED CONNECTOR AT TRANSMITTER, FOR FURTHER TROUBLESHOOTING, S WAPPED NR 2 AND NR 3 INDICATOR. CALIBRATED AND OPS CHECK GOOD PER MM 79-31-02. 2 L 7 3 4F A3WE 1998020500418 19980205 00418 NE 1998 2 5 ARWA980201 2 19980202 A 7200 ENGINE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 2 FAILED A ARWA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 19 1804 45896 CHECK NR 2 ENGINE FOR VIBRATIONS NR 2 THROTTLE AND START LEVEL HARD IN CRUISE. ACCOMPLISHED R/B 8269 REMOVED AND REPLAC ED NR 2 ENGINE IAW ARROW AIR J/C 6519 AND J/C 6528, OPERATIONS AND LEAK CHECKED NORMAL ON RUN UP, IAW J/C 6527. 2 L 7 4 4F 4 F 4A25 1E8 1998020500419 19980205 00419 1998 2 5 ARWA980202 4 19980202 A 3454 5222450015 RECEIVER DOUG DC8 DC862 3021970 WP NR 1 INOPERATIVE A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 810BN 45905 RETURN TO BLOCKS DUE TO NR 1 VOR OFF FLAG IN VIEW. REMOVED AND REPLACED NAV RECEIVER, NORMAL PER MM 34-00-00. 2 L 7 4 4F 4A25 1998020500420 19980205 00420 WP 1998 2 5 ARWA980203 1 19980202 A 3241 420531A CONTROL BOX DOUG DC8 DC862 3021970 WP ANTI-SKID SYST FAILED A ARWA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 802BN 45909 AFTER T/O, ANTI-SKID LIGHT CAME ON. REMOVED AND REPLACED ANTI-SKID CONTROL BOX, OPS CHECKED GOOD IAW MM 32-43-3. REMOV ED AND REPLACED DUAL ANTI-SKID VALVE, OPS CHECKED GOOD IAW MM 27-60 AND 32-43. RESET G/B. 2 L 7 4 4F 4A25 1998020500421 19980205 00421 WP 1998 2 5 CKSA98003 1 19980124 A 3350 516574 POWER PACK LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 3 EA EMERGENCY BATTERY PACKS AT DOORS R2, R3, R4 INOP. TROUBLESHOT EMERGENCY LIGHT SYSTEM, FOUND R4 OPERATIVE AND CHARG ING. REMOVED AND REPLACED R2 AND R3 BATTERY PACKS IAW L1011 MM 33-51-03, OPS CK GOOD. 2 L 7 3 4F A23WE 1998020500422 19980205 00422 WP 1998 2 5 CKSA98004 1 19980124 A 3350 516574 POWER PACK LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 ON EMERGENCY LIGHT SYSTEM TEST, FOUND L1 EXIT LIGHTS INOP. REMOVED AND REPLACED L1 BATTERY POWER PACK IAW L1011 MM 33-5 1-03, OPS CK GOOD. 2 L 7 3 4F A23WE 1998020500423 19980205 00423 WP 1998 2 5 TC8A98005 1 19980129 A 2781 H655 SWITCH DOUG DC8 DC861F 3021953 WP LE FLAPS FAILED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 184SK 45981 TRIP NR 1259, SLOT DISAGREEMENT LIGHT STAYED ON ON TAXI-OUT, RETURNED TO RAMP. ENTERED ON DMI 8052 CAT C, REMOVED AND R EPLACED INBOARD RT SWITCH, OPS CHECKED NORMAL IAW M/M 27-52-3, CLEARED DMI8052. 2 L 7 4 4F 4A25 1998020500424 19980205 00424 WP 1998 2 5 TC8A98006 1 19980130 A 5260 H201 SWITCH DOUG DC8 DC8F55 3021928 WP RT MLG DOOR FAILED A TC8A A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 GL 23 182SK 45817 STRONG VIBRATION AT NOSE LANDING GEAR DOOR. LANDING GEAR UNSAFE LIGHT ON. FOUND CRACKED HEAT EXCHANGER DUCT. WELDED A S PER DPM10-225 AND REPLACED BROKEN RT MAIN LANDING GEAR DOOR SWITCH, OPS CHECKED IAW MM 32-2-0 NORMAL. 2 L 7 4 4F 4A25 1998020500431 19980205 00431 CE 1998 2 5 98ZZZX483 1 19980116 A 3231 541045019 LINKAGE LEAR 60 60LEAR 5170707 CE NLG DOORS DISCONNECTED A J7SA K NONE W E INADEQUATE Q C VIBRATION/BUFFET IN INSP/MAINT 1 SW 21 212FX 099 NOSE GEAR VIBRATION AFTER TAKEOFF WITH GEAR UP AND INCREASED WITH SPEED. CONNECTED NOSE GEAR DOOR ACTUATING LINKAGE. M AINTENANCE REPORTED HAVING NOSE GEAR DOORS DISCONNECTED FOR PRIOR MAINTENANCE ON NOSE GEAR. 2 L 7 2 4F RT A10CE 1998020500483 19980205 00483 EU 1998 2 5 USAAF98002 1 19980108 A 2750 A83235419 SYNCHRONIZER FOKKER F28 F28MK0100 4990807 EU RT TE FLAP FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 884US 11338 PHL/IND - FLT 1799 - ON CLIMB-OUT FROM PHL AT 1,000 FEET WHEN FLAPS WERE RETRACTED, FLAP ASYMMETRY' ILLUMINATED AT 8 DEG REES OF FLAP. FLIGHT RETURNED TO PHL WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE RI GHT INBOARD FLAP SYNCHRO AND RIGGED THE SYSTEM. (X) 2 L 7 2 4F RT 1998020500484 19980205 00484 EU 1998 2 5 USAAF98004 1 19980113 A 3260 SK3852 INDICATOR MODULE FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 863US 11303 CLT - FLT 220 - THE GREEN LEFT MLG LIGHT STAYED ON AFTER RETRACTION, NO OTHER ABNORMAL INDICATIONS WERE PRESENT. THE AI RCRAFT RETURNED TO CLT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR INDICATION MODULE. GROUND CHECKS OK. REF: MM 32-61-02, PAGE 402. (X) 2 L 7 2 4F RT 1998020500485 19980205 00485 EU 1998 2 5 USAAF98005 1 19980113 A 3260 SWITCH FOKKER F28 F28MK0100 4990807 EU MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 850US 11276 PIT - FLT 670 - ON TAKEOFF, THE LANDING GEAR WOULD NOT COME UP. OVERRIDE WAS USED AND GEAR CAME UP. TAKEOFF CONFIGURAT ION RED WARNING MESSAGE. THEN FLT/GRD CONFIGURE AMBER MESSAGE, RED WARNING WENT OUT; ALSO, GOT ANTI-SKID AMBER MESSAGE AND STAB TRIM INDICATOR RAN TO FULL DOWN, SOME DOWN PRESSURE BUT NOT EXCESSIVE. DID OPERATE ELECTRICALLY. FLIGHT RETUR NED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. JACKED ACFT AND RETRACTED GEAR MANY TIMES. MAINTENANCE WAS UNABLE TO D UPLICATE ANY OF THE PROBLEMS. MAINTENANCE REPLACED BOTH MAIN GEAR GROUND FLIGHT SWITCHES PER FOKKER MM 32-63-01. AN AU TOPILOT CHECK WAS PERFORMED WITH NO DISCREPANCY FOUND. (X) 2 L 7 2 4F RT 1998020500486 19980205 00486 NM 1998 2 5 USAASB98006 1 19980108 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 252AU 22758 ROC - MAINTENANCE FOUND THE AFT LEFT AND RIGHT LOWER DOOR EMERGENCY EXIT LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998020500487 19980205 00487 NM 1998 2 5 USAASB98010 1 19980112 A 2750 6570945295 TQ SHAFT DOOR BOEING 737 7373B7 1384580 NM LT TE FLAP BROKEN A USAA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 EA 19 518AU 23704 PHL - FLT 931 - UPON ACCOMPLISHING CHECKLIST TO LAND AT PHL, CREW SET FLAPS AT 30 DEGREES AND NOTICED THE FLAPS WOULD NO T EXTEND PAST 8 DEGREES. A GO-AROUND WAS ACCOMPLISHED AT WHICH TIME THE ALTERNATE FLAP EXTENSION WAS PUT INTO PLACE WIT H NO HELP. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT WITH 8 DEGREE FLAPS. MAINTENANCE FOUND THE LEFT WING INBOARD FLAP, MID-FLAP TORQUE SHAFT CLEARANCE DOOR BROKEN AND JAMMING UP FLAP EXTENSION. REMOVED TORQUE SHAFT CLEARANC E DOOR AND RELEASED UNDER CDL 57-53-1. NEW DOOR HAS BEEN PROGRAMMED FOR INSTALLATION. (X) 2 L 7 2 4F RT A16WE 1998020500500 19980205 00500 NM 1998 2 5 TSAA9833025 1 19980108 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT ALL WELL LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,453:50 HOURS. TAC: 35,976. (X) 2 L 7 2 4F RT A16WE 1998020500501 19980205 00501 NM 1998 2 5 TSAA9833026 1 19980108 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT ALL WELL LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,453:50 HOURS. TAC: 35,976. (X) 2 L 7 2 4F RT A16WE 1998020500502 19980205 00502 NM 1998 2 5 TSAA9833027 1 19980108 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. TAT: 44,226:57 HOURS. TAC: 57,385. (X) 2 L 7 2 4F A16WE 1998020500503 19980205 00503 NM 1998 2 5 TSAA9833028 1 19980108 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRA FT RETURNED TO SERIVCE. TAT: 44,226:57 HOURS. TAC: 57,385. (X) 2 L 7 2 4F A16WE 1998020500504 19980205 00504 NM 1998 2 5 TSAA9833029 1 19980108 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 44,226:57 HOURS. TAC: 57,385. (X) 2 L 7 2 4F A16WE 1998020500505 19980205 00505 NM 1998 2 5 TSAA9833030 1 19980108 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 44,226:57 HOURS. TAC: 57,385. (X) 2 L 7 2 4F A16WE 1998020500506 19980205 00506 NM 1998 2 5 TSAA9833031 1 19980109 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHT WITH ON ALLS WELL. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 60,881. (X) 2 L 7 2 4F RT A16WE 1998020500507 19980205 00507 NM 1998 2 5 TSAA9833032 1 19980109 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT WITH ON ALLS WELL. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 60,881. (X) 2 L 7 2 4F RT A16WE 1998020500508 19980205 00508 NM 1998 2 5 TSAA9833033 1 19980109 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT WITH ON ALLS WELL. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 660,881. (X) 2 L 7 2 4F RT A16WE 1998020500509 19980205 00509 NM 1998 2 5 TSAA9833034 1 19980109 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X) 2 L 7 2 4F RT A16WE 1998020500510 19980205 00510 NM 1998 2 5 TSAA9833035 1 19980109 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X) 2 L 7 2 4F RT A16WE 1998020500511 19980205 00511 NM 1998 2 5 TSAA9833036 1 19980109 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X) 2 L 7 2 4F RT A16WE 1998020500512 19980205 00512 NM 1998 2 5 TSAA9833037 1 19980109 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 33,513:04 HOURS. TAC: 39,735. (X) 2 L 7 2 4F RT A16WE 1998020500513 19980205 00513 NM 1998 2 5 TSAA9833038 1 19980109 A 3350 963100211 SIGN BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED FLOOR LIGHT ASSY, OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 33,513:14 HOURS. TAC: 39,735. (X) 2 L 7 2 4F RT A16WE 1998020500514 19980205 00514 NM 1998 2 5 TSAA9853044 1 19980108 A 5330 SKIN BOEING 737 7372S5C 1384499 NM BS 446/442 DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 DURING QC OPERATIONS, AIRCRAFT SUSTAINED DAMAGE ON OUTER SKIN (AT TWO LOCATIONS). LOCATION OF DAMAGED AREAS WERE BS 446 (2 INCHES BY .50 INCH) AND BS 442 (.75 INCH BY .50 INCH) ON MAIN CARGO DOOR CUT OUT (ABOVE S18L). DAMAGED AREAS REPAIR ED PER EA 737-53-015 (ONE REPAIR FOR BOTH DAMAGED AREAS APPLIED). AIRCRAFT RETURNED TO SERVICE. TAT: 32,473:24 HOURS. TAC: 60,881. (X) 2 L 7 2 4F RT A16WE 1998020500517 19980205 00517 EU 1998 2 5 SIMA980041 1 19980104 A 5347 7294711701 CAP END SAAB SF340 340B 7860101 EU BS 296 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 ABI - LEFT SEAT TRACK END CAP HAD CORROSION BEYOND LIMITS AT FS 296, BL 18.3L. REMOVED AND REPLACED LT SEAT TRACK END C AP IAW SAAB SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998020500518 19980205 00518 EU 1998 2 5 SIMA980042 1 19980104 A 5347 7253721459 GALLEY TRACK SAAB SF340 340B 7860101 EU BS 225-261 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 ABI - RT LAVATORY AND GALLEY TRACK AT FS 225 - FS 261, BL 324, HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED RT LAVA TORY AND GALLEY TRACK IAW SAAB SRM 51-40-25. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998020500519 19980205 00519 EU 1998 2 5 SIMA980043 1 19980104 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 SEAT TRACK AT FS 297, BL 18.3L, FOUND TRACK CORRODED BEYOND LIMITS. A SPLICE REPAIR WAS DONE ON LT SEAT TRACK AT FS 297 , BS 18.3L IAW SAAB SRM 53-70-60. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998020500520 19980205 00520 EU 1998 2 5 SIMA980044 1 19980104 A 5320 7253710871 AIRSTAIR TRACK SAAB SF340 340B 7860101 EU BS 225-272 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 386AE 340B386 AIRSTAIR TRACK HAD CORROSION BEYOND LIMITS AT FS 225 - FS 272, BL 28L. REMOVED AND REPLACED AIRSTAIR TRACK IAW SAAB SRM 51-40-2. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998020500521 19980205 00521 1998 2 5 SIMA980132 4 19980113 A 3140 350A53000100 MFC BARFIELD AEROSP ATR72 ATR72212 EU NR 1 INTERMITTENT A SIMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 355AT 367 355 DFW - FLT 3829 - DURING ENGINE START-UP, NOSE LANDING GEAR INDICATED UNLOCKED. LIGHTS FLICKERED ALONG WITH OTHER WARNIN G LIGHTS FLICKERING AT SAME TIME. MAINTENANCE REPLACED NR 1 MFC UNIT PER JIC 31-48-81. PERFORMED OPERATION CHECKS INCL UDING EXTENDED ENGINE RUNS WITH NO FAULTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998020500522 19980205 00522 EU 1998 2 5 SIMA980191 1 19980119 A 3350 AQS1000 BATTERY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AC 0882 320 EMERGENCY LIGHTING INOPERATIVE, 66WL POWER SUPPLY CONTROLS THEM. REPLACED BATTERY PACK AT 66WL POWER SUPPLY IAW JIC 33- 51-21 SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998020500523 19980205 00523 EU 1998 2 5 SIMA980192 1 19980119 A 3350 AQS1000 BATTERY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 322AC 320 LBB - EMERGENCY BATTERY PACK AT 61WL HAS EVIDENCE OF POSSIBLE HEAT DAMAGE. REPLACED BATTERY PACK AT 61WL. OPS CHECK GO OD IAW JIC 33-51-21 SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998020500528 19980205 00528 GL 1998 2 5 RAIA980102 3 19980104 A 6110 750350333 O-RING BAG JETSTM JETSTM3201 1500217 EU ROTOL R333 R333482F12 GL LT PROP DOME FAILED A RAIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CE 03 436AM 728 891 UIN - FLT 7372 - LEFT ENGINE OIL PRESSURE DROPPED, CREW PERFORMED ENGINE SHUT DOWN. MAINTENANCE REPLACED LEFT PROPELLER DOME O-RING. (X) 2 L 7 2 4T RT A56EU 6 C P61GL 1998020500529 19980205 00529 SW 1998 2 5 HEEA0012673 1 19980126 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW DROOP COMP STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6748D 51106 ACTUATOR INTERMITTENTLY STICKS IN DIFFERENT POSITIONS. 1 G 7 1 3U H2SW 1998020500530 19980205 00530 NE 1998 2 5 HEEA0012674 1 19980126 A 2422 7655003007105 INVERTER SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 INVERTER CYCLES ON AND OFF. 1 G 7 2 3U H1NE 1998020500531 19980205 00531 SW 1998 2 5 HEEA0012675 1 19980126 A 6310 206040241001 HOUSING ASSY BELL 206 206L1 1182107 SW FREEWHEEL STRIPPED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5012V 45200 HOUSING ASSY THREADS STRIPPED. 1 G 7 1 3U H2SW 1998020500532 19980205 00532 NE 1998 2 5 HEEA0012676 1 19980126 A 6730 7630103902102 ACTUATOR SKRSKY S76 S76A 8143006 NE SERVO SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 ACTUATOR POPS COLLECTIVE BIAS CIRCUIT BREAKER. 1 G 7 2 3U H1NE 1998020500533 19980205 00533 SW 1998 2 5 HEEA0012677 1 19980126 A 6330 206033554101 LINK ASSY BELL 206 206L3 1182108 SW XMSN MOUNT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 49EA 51507 BEARING WORN AND RUBBER WORN. 1 G 7 1 3U H2SW 1998020500534 19980205 00534 SW 1998 2 5 HEEA0012678 1 19980126 A 6330 214031614128 PLATE ASSY BELL 214 214ST 1182106 SW MOUNT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 PLATE ASSY RUBBER STARTING TO TEAR. 2 G 7 2 4U H10SW 1998020500535 19980205 00535 SW 1998 2 5 HEEA0012679 1 19980126 A 6330 214031614127 PLATE ASSY BELL 214 214ST 1182106 SW MOUNT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 PLATE ASSY TORN RUBBER. 2 G 7 2 4U H10SW 1998020500536 19980205 00536 SW 1998 2 5 HEEA0012680 1 19980126 A 5343 212030437007 CAP ASSY BELL 212 212 1181420 SW SKID ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 CAP ASSY WORN RUBBER. 1 G 7 1 4U H4SW 1998020500537 19980205 00537 SW 1998 2 5 HEEA0012681 1 19980126 A 5343 212030437007 CAP ASSY BELL 212 212 1181420 SW SKID ATTACH WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 CAP ASSY WORN RUBBER. 1 G 7 1 4U H4SW 1998020500538 19980205 00538 EU 1998 2 5 HEEA0012682 1 19980126 A 7722 TM42745 INDICATOR BOLKMS 105 BO105S 5626006 EU ENG TOT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE S787 TOT INDICATOR READING IS ERRATIC. 1 G 7 2 3U H3EU 1998020500539 19980205 00539 NE 1998 2 5 HEEA0012683 1 19980126 A 7933 7645001078101 INDICATOR SKRSKY S76 S76A 8143006 NE ENG OIL DEFETIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 INDICATOR READS MINUS 25 DEGREES LOWER THAN OAT WHEN SYSTEM IS COLD. 1 G 7 2 3U H1NE 1998020500540 19980205 00540 EU 1998 2 5 HEEA0012684 1 19980126 A 7722 TM42745 INDICATOR BOLKMS 105 BO105S 5626006 EU ENG TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE S787 TOT INDICATOR LOW OR NO INDICATION. 1 G 7 2 3U H3EU 1998020500541 19980205 00541 SW 1998 2 5 HEEA0012685 1 19980126 A 6240 206070265101 INDICATOR BELL 206 206L1 1182107 SW ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W 45386 ROTOR NEEDLE DOES NOT MOVE. 1 G 7 1 3U H2SW 1998020500542 19980205 00542 SW 1998 2 5 HEEA0012686 1 19980126 A 7722 206375006101 INDICATOR BELL 206 206L1 1182107 SW ENG TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W 45386 TOT GAUGE WENT TO ZERO ON START UP AND CIRCUIT BREAKER POPPED. 1 G 7 1 3U H2SW 1998020500543 19980205 00543 1998 2 5 HEEA0012687 4 19980126 A 3424 206070274005 INDICATOR BELL 206 206L3 1182108 SW TURN & BANK FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 INDICATOR TURN NEEDLE IS INOPERATIVE. 1 G 7 1 3U H2SW 1998020500544 19980205 00544 1998 2 5 HEEA0012688 4 19980126 A 2562 ELT10 ELT NARCO BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 41791 51465 ELT FAILED 30 DAY OPERATIONAL TEST. 1 G 7 1 3U H2SW 1998020500545 19980205 00545 1998 2 5 HEEA0012689 4 19980126 A 3423 KCA0113W COMPASS SMITHIND BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X S808 STANDBY COMPASS WILL NOT SWING. 1 G 7 2 3U H3EU 1998020500546 19980205 00546 EU 1998 2 5 HEEA0012691 1 19980126 A 7714 DL4044 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205UC S668 NR1 AND NR2 NEEDLES HAVE EXCESSIVE SPLIT. 1 G 7 2 3U H3EU 1998020500547 19980205 00547 EU 1998 2 5 HEEA0012692 1 19980126 A 7714 DL4044 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3537T S349 NR2 NEEDLE INTERMITTENTLY STICKS ON LOW END. 1 G 7 2 3U H3EU 1998020500548 19980205 00548 EU 1998 2 5 HEEA0012693 1 19980126 A 6321 419210E CALIPER BOLKMS 105 BO105S 5626006 EU ROTOR BRAKE STRIPPED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB S737 ROTOR BRAKE CALIPER THREADS IN INLET PLATE STRIPPED. 1 G 7 2 3U H3EU 1998020500549 19980205 00549 SW 1998 2 5 HEEA0012694 1 19980126 A 5300 206033100261 SHELL ASSY BELL 206 206L1 1182107 SW FUSELAGE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 HOLE IN SHELL. 1 G 7 1 3U H2SW 1998020500550 19980205 00550 SW 1998 2 5 HEEA0012695 1 19980126 A 2422 214175104101 INVERTER BELL 214 214ST 1182106 SW AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 INVERTER POPS CIRCUIT BREAKER. 2 G 7 2 4U H10SW 1998020500551 19980205 00551 1998 2 5 HEEA0012696 4 19980126 A 3416 212070238003 ALTIMETER BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 WHEN DECREASING ALTIMETER KOLLSMAN WINDOW, NEEDLE MOVEMENT JUMPS 200 FEET AT 29-90. ADJUSTMENT KNOB IS STIFF AND RATCHE TY AT DIFFERENT SETTINGS. 1 G 7 2 4U H4SW 1998020500552 19980205 00552 1998 2 5 HEEA0012697 4 19980126 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 45381 KNOB BROKEN OFF. PERFORMED PRELIMINARY INSPECTION. REPLACED FACEPLATE ASSEMBLY P/N 200-2020-01, REPAIRED. ADJUSTED TO SPECS. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1998020500553 19980205 00553 1998 2 5 HEEA0012698 4 19980126 A 3452 071119208 CONTROL BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 DISPLAY DOES NOT LIGHT UP. PERFORMED PRELIMINARY INSPECTION. FOUND NO DISPLAY. SWAPPED DISPLAY DS103. NO HELP. SWAPP ED BOARDS. FOUND PROBLEM ON PROCESSOR BOARD. TROUBLESHOT AND FOUND BROKEN FOIL ON BOARD. REPAIRED BROKEN FOIL, REPAIR ED, INSTALLED MOD 2 KIT P/N050-2780-00 AND APPLIED HUMISEAL TO P305 HEADER. BENCH CHECK GOOD. 1 G 7 2 3U H13EU 1998020500554 19980205 00554 1998 2 5 HEEA0012699 4 19980126 A 3452 066106200 TRANSCEIVER KT76 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL S717 INTERMITTENT OPERATION WITH ATC. PERFORMED PRELIMINARY INSPECTION. FOUND POWER OUT LOW. ADJUSTED V101 CAVITY TUBE. NO HELP. REPLACED V101 CAVITY TUBE. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY. BENCH CHECK GOOD. 1 G 7 2 3U H3EU 1998020500555 19980205 00555 SW 1998 2 5 HEEA0012700 1 19980126 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 STARTER TERMINALS WORN, LOOSE AND BURNT. 2 G 7 2 4U H10SW 1998020500556 19980205 00556 EU 1998 2 5 HEEA0012701 1 19980126 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911BR 6555 S719 BLADE HAS SEPARATION AT THE TWO CENTER SCARF JOINTS BEYOND LIMITS AND A SMALL AMOUNT AT THE TIP OF THE BLADE. 1 G 7 2 3U H3EU 1998020500557 19980205 00557 1998 2 5 HEEA0012702 4 19980126 A 3451 066106600 TRANSCEIVER BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 33020 TRANSCEIVER WILL NOT WORK. FOUND Q103 TRANSISTOR, C106 CAPACITOR AND CR104 DIODE INOPERATIVE AND F1 FUSE BURNT. REPLACE D ALL THESE COMPONENTS. UNIT FIRED UP AND ADJUSTED POWER OUT AND PULSE WIDTH. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1998020500558 19980205 00558 1998 2 5 HEEA0012703 4 19980126 A 3452 6221270001 TRANSPONDER TDR90 BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 TRANSPONDER CONSTANTLY REPORTS CODE "7777" WITH IDENT MODE NO MATTER WHAT IS DIALED ON CONTROL HEAD. REPLACED WITH SERVI CEABLE UNIT. 1 G 7 2 4U H4SW 1998020500559 19980205 00559 NE 1998 2 5 HEEA0012706 1 19980126 A 2421 7655009005105 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 AC GENERATOR WILL NOT STAY ON LINE. 1 G 7 2 3U H1NE 1998020500560 19980205 00560 NE 1998 2 5 HEEA0012707 1 19980126 A 2422 7655009005105 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 31217 760229 AC GENERATOR BEARING LIGHT STAYS ON. 1 G 7 2 3U H1NE 1998020500561 19980205 00561 1998 2 5 HEEA0012708 4 19980126 A 3457 0845000000 GPS SKYNAV5000 SNIAS 350 AS350B2 8680813 EU COCKPIT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 2777 GPS "ENT" BUTTON INTERMITTENT. REPLACE FREQUENCY DUE TO CRACKS AROUND HOLE. 1 G 7 1 3U H9EU 1998020500562 19980205 00562 1998 2 5 HEEA0012709 4 19980126 A 3453 4530103 LORAN ARNAV21 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911HM S683 LORAN FALLS OFF LINE, DISPLAY AND HISTORY HAS SAME PROBLEMS. SENT TO ARNAV SYSTEMS, INC. FOR WARRANTY REPAIR. TIME SINC E REPAIR 24:50. 1 G 7 2 3U H3EU 1998020500563 19980205 00563 EU 1998 2 5 HEEA0012710 1 19980126 A 2822 D105300010 BEARING D107318D1 BOLKMS 105 BO105S 5626006 EU FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 682 112976 S737 BOOST PUMP WAS REMOVED FOR BEING INOPERATIVE. DISASSEMBLED AND FOUND THAT BEARING CAME APART AND CAUSED ARMATURE TO BUR N UP. BEARING WAS RECEIVED IN BEARING KIT D107318-21 ON 2-3-97. 1 G 7 2 3U H3EU 1998020500564 19980205 00564 EU 1998 2 5 HEEA0012711 1 19980126 A 2822 D105300010 BEARING D107318D1 BOLKMS 105 BO105S 5626006 EU FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 489 148147 S828 BOOST PUMP WAS REMOVED FOR BEING INOPERATIVE. DISASSEMBLED AND FOUND THAT BEARING CAME APART AND CAUSED ARMATURE TO BUR N UP. BEARING WAS RECEIVED IN BEARING KIT D107318-21 ON 1-4-97. SENT TO MIRAJ SPECIALTIES FOR WARRANTY CREDIT. 1 G 7 2 3U H3EU 1998020500565 19980205 00565 EU 1998 2 5 HEEA0012712 1 19980126 A 2822 D105300010 BEARING D107318D1 BOLKMS 105 BO105S 5626006 EU FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 595 156179 S818 BOOST PUMP WAS REMOVED FOR BEING INOPERATIVE. DISASSEMBLED AND FOUND THAT BEARING CAME APART. BEARING WAS RECEIVED IN B EARING KIT D107318-21. SENT TO MIRAJ SPECIALTIES FOR WARRANTY CREDIT. 1 G 7 2 3U H3EU 1998020500566 19980205 00566 EU 1998 2 5 HEEA0012713 1 19980126 A 2822 D105300010 BEARING D107318D1 BOLKMS 105 BO105S 5626006 EU FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205UC 843 156418 S668 BOOST PUMP WAS REMOVED FOR BEING INOPERATIVE. DISASSEMBLED AND FOUND THAT BEARING CAME APART. BEARING WAS RECEIVED IN B EARING KIT D107318-21. SENT TO MIRAJ SPECIALTIES FOR WARRANTY CREDIT. 1 G 7 2 3U H3EU 1998020500567 19980205 00567 SW 1998 2 5 HEEA0012714 1 19980127 A 5610 P21207601 WINDOW BELL 412 412 1182202 SW LT LOWER MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2261D 33076 UNABLE TO FIT L/H LOWER WINDOW ONTO FUSELAGE. 1 G 7 2 4U H4SW 1998020500568 19980205 00568 1998 2 5 HEEA0012715 4 19980127 A 3453 066402600 LORAN KLN88 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6610E 51424 LORAN DOES NOT DISPLAY DATA, DISPLAYS MOSTLY LINES. 1 G 7 1 3U H2SW 1998020500569 19980205 00569 1998 2 5 HEEA0012716 4 19980127 A 3453 066402600 LORAN KLN88 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 LORAN LOSES DATA BASE MEMORY. 1 G 7 2 3U H3EU 1998020500570 19980205 00570 1998 2 5 HEEA0012717 4 19980127 A 3416 066306401 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT ENCODER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 ENCODER READS LOW OUT OF TOLERANCE. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H1NE 1998020500571 19980205 00571 1998 2 5 HEEA0012718 4 19980127 A 3416 214175278101 ALTIMETER BELL 214 214ST 1182106 SW COCKPIT ENCODER ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 ENCODER HAS ERRATIC READINGS. TIME SINCE REPAIR 470:20. 2 G 7 2 4U H10SW 1998020500572 19980205 00572 GL 1998 2 5 HEEA0012719 2 19980127 A 7321 25490925 FUEL CONTROL BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 53119 51575 FUEL CONTROL DEFECTIVE. FOUR REMOVALS FOR STARTING PROBLEMS. 1 EACH LIGHT OFF TEMP. TOO HIGH, COULD NOT ADJUST. 3 EAC H REMOVALS FOR HANG STARTS AT 35% TO 40%, COULD NOT ADJUST. SENT TO ALLIED SIGNAL BENDIX WEST COAST FOR WARRANTY REPAIR. 1 G 7 1 3U 3 U H2SW E1GL 1998020500573 19980205 00573 1998 2 5 HEEA0012720 4 19980127 A 3457 0110005400 GPS 150 GARMININTL BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5000K 45167 GPS WILL NOT RECEIVE SIGNAL FROM SATELLITES, ALSO INTERNAL BATTERY DEAD. 1 G 7 1 3U H2SW 1998020500574 19980205 00574 SW 1998 2 5 HEEA0012721 1 19980127 A 5520 8000427 INSERT 206023119151 BELL 206 206L1 1182107 SW ELEV WRONG PART E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3892R 12364 45594 INSERTS AT CENTER TRAILING EDGE SIDE BOTH UPPER AND LOWER (6 EACH) USED TO INSTALL SUPPORT FOR HORN ASSEMBLY ON THE ELEV ATORS ARE 80-004-1-7 (8/32) AND SHOULD BE 80-004-2-7 (10/32) 1 G 7 1 3U H2SW 1998020500575 19980205 00575 NE 1998 2 5 HEEA0012723 1 19980127 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R BLADE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 M/R BLADE HAS MULTIPLE CRACKS ON LEADING EDGE ABRASION WITH SEPARATION. 1 G 7 2 3U H1NE 1998020500576 19980205 00576 1998 2 5 HEEA0012724 4 19980127 A 2312 064105430 TRANSCEIVER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 53119 198 51575 TRANSCEIVER SMOKED. WILL NOT TRANSMIT OR RECEIVE. 1 G 7 1 3U H2SW 1998020500577 19980205 00577 1998 2 5 HEEA0012725 4 19980127 A 2312 064105430 TRANSCEIVER BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 TRANSCEIVER LED DISPLAY GOES BLANK. 1 G 7 1 3U O H2SW 1998020500578 19980205 00578 1998 2 5 HEEA0012726 4 19980127 A 2312 064105430 TRANSCEIVER BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 THE "T" STAYS ON ALL THE TIME AND L/H SIDE OF DISPLAY GOES 188.88 SOMETIMES AND WILL NOT CHANGE. 1 G 7 1 3U O H2SW 1998020500579 19980205 00579 1998 2 5 HEEA0012727 4 19980127 A 2312 064105430 TRANSCEIVER BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2272J 3620 TRANSCEIVER HAS NO LED, NO TRANSMIT. NO RECEIVE, 9504 SHORTED. 1 G 7 1 3U H2SW 1998020500580 19980205 00580 1998 2 5 HEEA0012728 4 19980127 A 2312 6221879001 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 VHF TRANSMITS ON 130.32 GARBLED, WEAK AND UNREADABLE. 1 G 7 2 3U H1NE 1998020500581 19980205 00581 1998 2 5 HEEA0012729 4 19980127 A 3452 066107100 TRANSPONDER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 TRANSPONDER INOPERATIVE. 1 G 7 2 3U H1NE 1998020500582 19980205 00582 1998 2 5 HEEA0012730 4 19980127 A 3455 066104701 RECEIVER BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 ADF NOISY AND CUTS OUT INTERMITTENTLY. ALSO HAS WEAK SIGNAL STRENGTH. 1 G 7 2 4U H4SW 1998020500583 19980205 00583 1998 2 5 HEEA0012731 4 19980127 A 2312 064100900 TRANSCEIVER KTR905 BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3131S 30953 TRANSMITTER BROKEN, MODULATION VERY DISTORTED. 1 G 7 1 4U H4SW 1998020500584 19980205 00584 1998 2 5 HEEA0012732 4 19980127 A 3454 071121701 INDICATOR KDA692 BELL 214 214ST 1182106 SW COCKPIT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 INDICATOR GREEN NEEDLE VERY ERRATIC. 2 G 7 2 4U H10SW 1998020500585 19980205 00585 1998 2 5 HEEA0012733 4 19980127 A 2564 100103305 LIFE RAFT BELL 214 214ST 1182106 SW ACFT ROOF MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 8045T 28101 RUNNERS ON LIFE RAFT ASSEMBLY DO NOT LINE UP WITH RAISED CHANNELS ON AIRCRAFT ROOF. UNABLE TO INSTALL RAFT ASSEMBLY. 2 G 7 2 4U H10SW 1998020500586 19980205 00586 1998 2 5 HEEA0012734 4 19980127 A 3451 066106902 DME KDI573 BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 DME LIGHT DIM. REPLACED WEAK V901 PHOTODETECTOR. INSPECTED AND BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1998020500587 19980205 00587 SW 1998 2 5 HEEA0012737 1 19980127 A 5330 206031210311S SKIN BELL 206 206B3 1181506 SW NOSE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2270G 3610 NOSE SKIN HAS BEEN CUT TOO MUCH FROM TOP SECTION AND TABS ARE SHORT. 1 G 7 1 3U H2SW 1998020500588 19980205 00588 SW 1998 2 5 HEEA0012739 1 19980127 A 6420 214011801127 HUB 214011801117 BELL 214 214ST 1182106 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 955 A761 28106 T/R HUB INBOARD BEARINGS (2 EACH) P/N 214-011-819-101 WORN EXCESSIVELY. TRUNNION P/N 214-011-804-101 CORRODED. THRUST PLUG P/N 214-011-806-101 WORN. PARTS AND LABOR WILL BE INVOICED...WO#9800049-99. 2 G 7 2 4U H10SW 1998020500589 19980205 00589 SW 1998 2 5 HEEA0012744 1 19980129 A 5530 212030136019 RIB BELL 412 412 1182202 SW T/B FIN DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 TAIL BOOM FIN RIB HAS SANDING MARKS BEYOND 10 PERCENT OF METAL. 1 G 7 2 4U H4SW 1998020500590 19980205 00590 SW 1998 2 5 HEEA0012746 1 19980130 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 39 33022 STEP ACTUATOR WON'T EXTEND OR RETRACT. 1 G 7 2 4U H4SW 1998020500591 19980205 00591 SW 1998 2 5 HEEA0012747 1 19980130 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 55 36005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998020500592 19980205 00592 SW 1998 2 5 HEEA0012748 1 19980130 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 13 33022 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998020500617 19980205 00617 WP 1998 2 5 CALA9800146 1 19980130 A 5320 WEB DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 INSPECTION FOUND FLOOR SUPPORT WEB ATTACHED TO MID CARGO AFT WALL CORRODED. THE WEB WAS REMOVED, AN ANGLE WAS FABRICATE D AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998020500618 19980205 00618 WP 1998 2 5 CALA9800147 1 19980130 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 INSPECTION FOUND BELT FRAME CRACKED IN THREE PLACES AT STA 1418. THE CRACKS WERE LOCATED AT LONGERON 1, 2L, AND 2R AND MEASURED 1, .5 AND 2 INCH LONG RESPECTIVELY. THE FRAME WAS REPAIRED IAW ECRA 5310-03667. 2 L 7 2 4F A6WE 1998020500619 19980205 00619 WP 1998 2 5 CALA9800148 1 19980130 A 5320 ANGLE DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14839 49635 INSPECTION FOUND DORSAL FIN ATTACH ANGLE ON RT SIDE CRACKED AT RIVET. A NEW ATTACH ANGLE WAS INSTALLED IAW EA 5340-0101 2. 2 L 7 2 4F A6WE 1998020500620 19980205 00620 NM 1998 2 5 CALA9800149 1 19980130 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLES AT STA 500C TO 500D BETWEEN STRINGERS 26L AND 27L. THE CORRO DED AREA WAS REMOVED, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5320-01502. 2 L 7 2 4F RT A16WE 1998020500621 19980205 00621 WP 1998 2 5 CALA9800150 1 19980130 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP BS 148-160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN PANEL D AND E AT STA 148 TO 160, FORWARD ENTRY AREA. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-01, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998020500622 19980205 00622 WP 1998 2 5 CALA9800151 1 19980202 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 304-313 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 THE RT FORWARD FUSELAGE BETWEEN FS 304 TO 313 BELOW EXTERNAL STRAP AREA HAD A TEMPORARY REPAIR DOUBLER INSTALLED WITH BL IND FASTENERS. THE TEMPORARY REPAIR WAS REMOVED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6. 2 L 7 3 4F A22WE 1998020500623 19980205 00623 WP 1998 2 5 CALA9800152 1 19980202 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 753 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 753, LONGERON 50R. THE AREA WAS POLISHED AND REFORMED IAW SRM 53-20-00. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-20-00 AND 51-21-01. 2 L 7 3 4F A22WE 1998020500624 19980205 00624 WP 1998 2 5 CALA9800153 1 19980202 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 385 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 A TEMPORARY REPAIR EXTERNAL DOUBLER WAS INSTALLED WITH BLIND FASTENERS AT RT FORWARD FUSELAGE STA 385 BETWEEN LONGERON 2 7R TO 28R. THE TEMPORARY REPAIR WAS REMOVED IAW SRM 53-40-00. DOUBLERS WERE INSTALLED IAW SRM 51-31-0. 2 L 7 3 4F A22WE 1998020500625 19980205 00625 WP 1998 2 5 CALA9800154 1 19980202 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 999 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RIVET HEADS DISHED DUE TO CORROSION AT FS 999 BETWEEN LONGERON 51L AND 51R. THE CORRODED FLANGE CLIP W AS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-33-00. 2 L 7 3 4F A22WE 1998020500626 19980205 00626 WP 1998 2 5 CALA9800155 1 19980202 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1841 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1841, STRINGER 37. THE DENTED AREA WAS CUT OUT, A DOUBLER, FINGER DOUBL ER, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 6. 2 L 7 3 4F A22WE 1998020500627 19980205 00627 WP 1998 2 5 CALA9800156 1 19980202 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1900 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1900, STRINGER 36. THE DENTED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FA BRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 13. 2 L 7 3 4F A22WE 1998020500628 19980205 00628 WP 1998 2 5 CALA9800157 1 19980202 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1119-1113 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FRAME CORRODED IN CAC COMPARTMENT AT STA 1119 TO 1113, LONGERON 51L. THE FRAME WAS REMOVED, A NEW FRAM E WAS FABRICATED AND INSTALLED IAW SRM 51-90-00 AND 51-31-01. 2 L 7 3 4F A22WE 1998020500629 19980205 00629 WP 1998 2 5 CALA9800158 1 19980202 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 880 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON SKIN TO FRAME SHEAR TIE AT FS 880, LONGERON 44R IN FORWARD CARGO COMPARTMENT. THE SHEAR T IE WAS REPAIRED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1998020500630 19980205 00630 WP 1998 2 5 CALA9800159 1 19980202 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 880 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT FS 880, LBL 37 TO 39. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53- 00-01 AND 51-21-0. 2 L 7 3 4F A22WE 1998020500631 19980205 00631 WP 1998 2 5 CALA9800160 1 19980202 A 5320 STRAP DOUG DC10 DC1010 3022110 WP BS 1761 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CIRCUMFERENTIAL STRAP CORRODED AT STA 1761, LBL 51 TO 52. A REPAIR WAS INSTALLED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1998020500632 19980205 00632 WP 1998 2 5 CALA9800161 1 19980202 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1681 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON FRAME SHEAR TIE AT STA 1681 BETWEEN LONGERON 47 AND 48L. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1998020500633 19980205 00633 WP 1998 2 5 CALA9800162 1 19980202 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1721 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 5 INCH CRACK IN LT CIRCUMFERENTIAL FRAME AT STA 1721, LONGERON 13. THE CRACKED AREA WAS CUT OUT IAW SRM 53-30-00. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1998020500634 19980205 00634 WP 1998 2 5 CALA9800163 1 19980202 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1741 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 5 INCH CRACK IN LT CIRCUMFERENTIAL FRAME AT STA 1741, LONGERON 13. A REPAIR WAS ACCOMPLISHED IAW SRM 53-30-00, FIGURE 5. 2 L 7 3 4F A22WE 1998020500635 19980205 00635 WP 1998 2 5 CALA9800164 1 19980202 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1761 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 5 INCH CRACK IN LT CIRCUMFERENTIAL FRAME AT STA 1761, LONGERON 13. A REPAIR WAS ACCOMPLISHED IAW SRM 53-30-00, FIGURE 5. 2 L 7 3 4F A22WE 1998020500636 19980205 00636 WP 1998 2 5 CALA9800165 1 19980202 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1781 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 6 INCH CRACK IN LT CIRCUMFERENTIAL FRAME AT STA 1781, LONGERON 13. THE CRACKED AREA WAS REMOVED IAW SRM 51-31-01. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-0 AND 51-21-0. 2 L 7 3 4F A22WE 1998020500637 19980205 00637 WP 1998 2 5 9801931225 1 19980131 A 3610 8986263 REGULATOR VALVE DOUG DC10 DC1030 3023501 WP NR 1 PNEU SYST FAILED A NWAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 GL 01 225NW 17 46582 ON DEPARTURE, NR 1 PNEUMATIC TEMPERATURE LIGHT ILLUMINATED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE. UNABLE TO DEP RESSURIZE DUCT. REDUCED THROTTLE AND BROUGHT TEMPERATURE DOWN. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED PNEUMATIC PRESSURE REGULATOR VALVE, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998020500638 19980205 00638 NM 1998 2 5 9801946638 1 19980131 A 3397 WIRE BOEING 747 747251B 1384892 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 638US 23549 DURING LINE CHECK, FOUND E-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE ON LEFT SIDE OF AIRCRAFT. REPAIRED BROKEN WIRE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998020500639 19980205 00639 NE 1998 2 5 9801951143 2 19980130 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 MALFUNCTIONED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 133JC 46752 686128 DURING LANDING ROLLOUT AND WHILE IN REVERSE THRUST, THE NR 1 ENGINE EGT ROSE RAPIDLY TOWARD THE RED LINE LIMIT. THE ENG INE WAS SHUT DOWN BEFORE EXCEEDING ANY LIMITATIONS. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED. 2 L 7 3 4F 4 F A22WE E20EA 1998020500640 19980205 00640 EU 1998 2 5 9801963213 1 19980130 A 2130 VFT300A1AMDTA SKIN VALVE AIRBUS 320 A320211 3930320 EU E/E COMP FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 313US 18129 92 153 FOLLOWING TAKEOFF, CREW WAS UNABLE TO PRESSURE THE AIRCRAFT. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT COOLING SKIN AIR OUTLET VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998020500641 19980205 00641 WP 1998 2 5 9801979935 1 19980117 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1332U 47404 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE INTERIOR RELEASE HANDLE FROM TH E CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998020500642 19980205 00642 SO 1998 2 5 COMA9810033 1 19980129 A 5753 TRACKS EMB 120 EMB120RT SO TE FLAPS ICED UP A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 264CA 120256 FLAP DISAGREEMENT WARNING AFTER TAKEOFF. CLEANED ICE FROM FLAP TRACKS. 2 L 7 2 4T RT A31SO 1998020500643 19980205 00643 NM 1998 2 5 SWAA980085 1 19980131 A 2130 655281025 RELAY MODULE BOEING 737 7372H4 138448C NM E/E BAY FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 82SW 22731 RETURNED TO PHX AND MADE AN UNEVENTFUL LANDING DUE TO THE INABILITY TO PRESSURIZE AIRCRAFT, USING AUTO, STANDBY OR MANUA L MODES. REMOVED AND REPLACED RELAY UNIT MODULE AND CHECKED SYSTEM PER BOEING M/M. 2 L 7 2 4F A16WE 1998020500644 19980205 00644 EU 1998 2 5 SWAA980086 2 19980130 A 7200 3920028 ENGINE BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 695SW 23506 RETURNED TO PVD AND MADE AN UNEVENTFUL LANDING DUE TO BIRDSTRIKE TO NUMBER 1 ENGINE. PERFOMED BIRDSTRIKE INSPECTION, FO UND 3 ENGINE FAN BLADES BENT. REMOVED AND REPLACED COMPLETED SET OF FAN BLADES PER BOEING M/M, WITH A BORESCOPE SCHEDUL ED WITHIN 10 CYCLES . 2 L 7 2 4F 4 F RT A16WE E21EU 1998020500645 19980205 00645 NM 1998 2 5 SWAA980087 1 19980128 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 400 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTS AT BS 400, BETWEEN S24 AND 25R, AT BS 500, AT S24R, AT BS 1013, AT S 23R, AT BS 864, AT S18R, AND AT BS 500D PLUS 8, AT S22R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998020500646 19980205 00646 NM 1998 2 5 SWAA980088 1 19980128 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 533 PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D CHECK, FUSELAGE SKIN WAS ACCIDENTALLY PUNCTURED AT BS 533, BETWEEN S24 AND 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998020500647 19980205 00647 NM 1998 2 5 SWAA980089 1 19980128 A 5312 BULKHEAD BOEING 737 7373T0 1384582 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D CHECK, FOUND BULKHEAD AT BS 178 CRACKED AFT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998020500648 19980205 00648 NM 1998 2 5 SWAA980090 1 19980128 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 400 DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D CHECK, FOUND STRINGER DAMAGE AT BS 400, AT S20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998020500649 19980205 00649 NM 1998 2 5 SWAA980091 1 19980128 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 852 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 852, ABOVE S15R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998020500651 19980205 00651 NM 1998 2 5 UPS98225662 1 19980104 A 5753 652165128 FITTING BOEING 727 7272A1 138407F NM NR 5 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, RIGHT WING NR 5 FLAP TRACK FWD ATTACH FITTING I/B SIDE CORRODED (CORROSION C57-581-07.00-04). CORRO SION FOUND TO BE OUT OF LIMITS PER SRM 57-40-01. REPLACED WITH NEW FITTING IAW MM 32-11-51 AND OHM 20-50-03. 2 L 7 3 4F A3WE 1998020500652 19980205 00652 NM 1998 2 5 UPS98225663 1 19980127 A 5711 REAR SPAR BOEING 727 7272A1 138407F NM WS 686.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, L/W STRINGER 2ND FROM REAR SPAR ON UPPER SKIN AT WING STATION 686.5 IS CRACKED AT STRINGER 5 TO 10. REPAIRED L/W STRINGER 2ND FROM REAR SPAR (STR 10) AT STA 686.5 IAW UPS EO B727-5710-0314. 2 L 7 3 4F A3WE 1998020500653 19980205 00653 NM 1998 2 5 UPS98225664 1 19980127 A 5741 69139017 BOTTLE PIN BOEING 727 7272A1 138407F NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, R/W REAR BOTTLE PIN IS CORRODED. ALSO, FWD AND AFT BUSHINGS ARE MISSING SECTION OF MICARTA INNER SL EEVE CORROSION (C53-100-05.00-04). REMOVED AND REPLACED R/W AFT BOTTLE PIN ON NRC 657574 IAW MM 57-41-01, BUSHING REPLA CED ON AOG (BOEING) AGREEMENT 6-1171-TA-883. 2 L 7 3 4F A3WE 1998020500654 19980205 00654 NM 1998 2 5 UPS98425665 1 19980126 A 5330 SKIN BOEING 747 747123F NM BS 1830-1850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, FROM DEFERRED ITEM D145981 - EVIDENCE OF CORROSION AND CRACKED FASTENER HEAD FROM FS 1830 TO 1850 S TR 48R. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-03. 2 L 7 4 4F A20WE 1998020500655 19980205 00655 NM 1998 2 5 UPS98425666 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, FS 1780 BL 0 SHEAR TIE CRACKED. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1998020500656 19980205 00656 NM 1998 2 5 UPS98425667 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1780 BETWEEN STR 48R AND 49R. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1998020500657 19980205 00657 NM 1998 2 5 UPS98425668 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1800 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, CRACKED SHEAR TIE FS 1800 BL 0. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1998020500658 19980205 00658 NM 1998 2 5 UPS98425669 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1820 BL 0. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1998020500659 19980205 00659 NM 1998 2 5 UPS98425670 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1820 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, FS 1820 BETWEEN STR 51L AND 50L SHEAR TIE CRACKED. REPAIRED IAW SRM 53-10-4 FIG 3. 2 L 7 4 4F A20WE 1998020500660 19980205 00660 NM 1998 2 5 UPS98425671 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1840 BETWEEN STR 51R AND 50R. REPAIRED IAW SRM 53-10-4 FIG 3. 2 L 7 4 4F A20WE 1998020500661 19980205 00661 NM 1998 2 5 UPS98425672 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1840 BETWEEN STR 50R AND 49R. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1998020500662 19980205 00662 NM 1998 2 5 UPS98425673 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1780 BETWEEN STR 50L AND 51L. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1998020500663 19980205 00663 NM 1998 2 5 UPS98425674 1 19980128 A 5320 SHEAR TIE BOEING 747 747123F NM BS 1840 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, SHEAR TIE CRACKED FS 1840 BETWEEN STR 47R AND 48R. REPAIRED IAW SRM 53-10-04 FIG 3. 2 L 7 4 4F A20WE 1998020500664 19980205 00664 NM 1998 2 5 UPS98425675 1 19980128 A 5313 STRINGER BOEING 747 747123F NM BS 1800-1820 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, FS 1800 TO 1820 STRINGER 48R HAS EVIDENCE OF CORROSION. REMOVED DAMAGE, FABRICATED AND INSTALLED R EPAIR PARTS IAW SRM 53-10-3 FIG 8. 2 L 7 4 4F A20WE 1998020500665 19980205 00665 NM 1998 2 5 UPS98425676 1 19980129 A 5320 DOUBLER BOEING 747 747123F NM BS 1781-1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 51L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-2. 2 L 7 4 4F A20WE 1998020500666 19980205 00666 NM 1998 2 5 UPS98425677 1 19980129 A 5320 DOUBLER BOEING 747 747123F NM BS 1781-1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 51R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLAC EMENT DOUBLER IAW SRM 53-30-02. 2 L 7 4 4F A20WE 1998020500667 19980205 00667 NM 1998 2 5 UPS98425678 1 19980129 A 5320 DOUBLER BOEING 747 747123F NM BS 1781-1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 50R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLAC EMENT DOUBLER IAW SRM 53-30-02. 2 L 7 4 4F A20WE 1998020500668 19980205 00668 NM 1998 2 5 UPS98425679 1 19980129 A 5320 DOUBLER BOEING 747 747123F NM BS 1781-1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 49R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLAC EMENT DOUBLER IAW SRM 53-30-2. 2 L 7 4 4F A20WE 1998020500669 19980205 00669 NM 1998 2 5 UPS98425680 1 19980129 A 5320 DOUBLER BOEING 747 747123F NM BS 1781-1841 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, STRINGER DOUBLER CORRODED FS 1781 TO 1841 STR 48R. REMOVED DAMAGE, FABRICATED AND INSTALLED REPLAC EMENT DOUBLER IAW SRM 53-30-3 FIG 37. 2 L 7 4 4F A20WE 1998020500670 19980205 00670 WP 1998 2 5 UPS98825681 1 19980116 A 5320 DOOR FRAME DOUG DC8 DC873F 302199F WP BS 1620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-D, FS 1620 RT FRAME CORRODED BEYOND REPAIR AND SEVERAL MISDRILLED HOLES. REPAIRED IAW DHC SK-852-611. 2 L 7 4 4F RT 4A25 1998020500671 19980205 00671 EU 1998 2 5 WWMA9800019 1 19980201 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 245AE 340B245 EMERGENCY LIGHT AT SEAT 5B FAILED TO ILLUMINATE DURING TEST. REPLACED BULB. 2 L 7 2 4T RT A52EU 1998020500672 19980205 00672 NM 1998 2 5 QXEA9800053 1 19980131 A 2530 1095 BEV CONTAINER DHAV DHC8 DHC8202 2809007 NM GALLEY MALFUNCTION A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 NM 09 348PH 484 ON APPROACH AFTER GEAR EXTENSION, CREW EXPERIENCED A VERY STRONG RUBBER BURNING OR WIRE INSULATION TYPE SMELL. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION MAINTENANCE FOUND POTTING ON FORWARD BEVERAGE CONTAINER MELTED TO BOTTOM PIN. REMOVED AND REPLACED BEVERAGE CONTAINER. CHECK BLEED AIR SYSTEM FOR ALL TEMPERATURE MODES FOR BOTH CONTROL PANEL. CH ECKED AIRCRAFT ELECTRICAL POWER SOURCES (AC/DC/TRANSFORMER AND RECTIFIER UNITS/INVERTERS). PERFORMED OPERATIONAL CHECK OF ALL AIRCRAFT LIGHTING SYSTEM. NO DEFECTS AND NO UNUSUAL SMELL NOTED. 2 H 7 2 4T RT A13NM 1998020500673 19980205 00673 NM 1998 2 5 QXEA9800054 1 19980131 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 354PH 12247 279 498 RIGHT HAND FORWARD EGRESS LIGHT AND RIGHT HAND FORWARD EXIT SIGN NOT ILLUMINATING. MAINTENANCE REPLACED BATTERY PACK, O PERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998020500674 19980205 00674 NM 1998 2 5 QXEA9800055 1 19980130 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 822PH 14677 79 106 TWO FORWARD FLOOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY, OPERATIONAL CHECK GOOD . 2 H 7 2 4T RT A13NM 1998020500675 19980205 00675 EU 1998 2 5 QXEA9800056 1 19980130 A 3350 1720 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 EMERGENCY EXIT SIGN LIGHT OUT ON OVERWING EXIT. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998020500676 19980205 00676 EU 1998 2 5 QXEA9800057 1 19980130 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 THE 28V EVACUATION LIGHTS AT EXIT 9E AND OVERHEAD ROW 2 INOP. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998020500677 19980205 00677 NM 1998 2 5 98FDEA00080 1 19980202 A 2420 750860 IDG DOUG MD11 MD11F 3023600 NM NR 3 FAILED A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 612FE 48605 GEN 3 OFF LIGHT ON CLIMBOUT VOLTS O/FREQ 400,1 RESET ATTEMPTED. SEE PREVIOUS. PERFORMED T/SHOOTING PE. 3-13 WAS OPEN. REMOVED AND REPLACED NR 3 IDG PER MM 24-21-02. RUN ENGINE CHECKED OPERATION OF NR 3 IDG, FOUND NORMAL PER JRH MD-11. 2 L 7 3 4F RT A22WE 1998020500735 19980205 00735 WP 1998 2 5 ABXA9800043 1 19980130 A 2612 390D AMPLIFIER DOUG DC8 DC862 3021970 WP NR 1 ENGINE DEFECTIVE A ABXA E B ENGINE SHUTDOWN EMER. DESCENT N FALSE WARNING CR CRUISE 1 GL 23 804AX 45987 NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED IN CRUISE. DISCHARGED BOTH NR 1 AND NR 2 FIRE BOTTLES. SHUTDOWN NR 1 ENGINE , DIVERTED TO UNSCHEDULED LANDING. LANDING UNEVENTFUL. DETERMINED TO BE FALSE WARNING. INSPECTED ALL WIRING AND FIRE WARNING LOOPS. REPLACED FIRE WARNING SYSTEM AMPLIFIER. SYSTEM OPS CHECKED GOOD IAW DC8 MM 26-10-00. 2 L 7 4 4F 4A25 1998020500736 19980205 00736 WP 1998 2 5 MWEA98139 1 19980131 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 THE GALLEY SLIDE COVER CAME OFF AT THE GATE. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998020500737 19980205 00737 WP 1998 2 5 MWEA98140 1 19980130 A 2121 FAN DOUG DC9 DC932 3022066 WP E/E COMPT FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 31 205ME 47601 IN CRUISE FLIGHT, RADIO RACK FAN OFF, ANNUNCIATOR ILLUMINATED. RETURNED TO MCO TO REMOVE DOG IN FWD CARGO PIT. MTC DEF ERRED PER MEL 21-20. 2 L 7 2 4F A6WE 1998020500738 19980205 00738 WP 1998 2 5 MWEA98141 1 19980131 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 760 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FOUND CRACK ON EXTERIOR AT STATION 760 BETWEEN LONG 17R AND 18R. MTC REPAIRED IAW SRM 53-04 FIG 38 VIEW H. 2 L 7 2 4F A6WE 1998020500739 19980205 00739 WP 1998 2 5 MWEA98142 1 19980202 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-240 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING INSPECTION, FOUND GALLEY SEAT TRACK NR 3 IS CORRODED FROM STATION 200 TO STATION 240. MTC REPAIRED IAW SRM 53-05 FIG 40. 2 L 7 2 4F A6WE 1998020500740 19980205 00740 WP 1998 2 5 MWEA98143 1 19980202 A 5230 ANGLE DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING INSPECTION, FOUND THE AFT CARGO DOOR INNER DOOR PAN CRACKED IN FLANGE RADIUS. MTC REPAIRED IAW SRM 51-30-2 AND 5 1-30-5. 2 L 7 2 4F A6WE 1998020500741 19980205 00741 NM 1998 2 5 P5CA9800052 1 19980128 A 7110 COWL BOEING 747 747123 1384873 NM NR 1 ENGINE GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 ENGINE FAN COWL OUTBD SIDE AT 7 O'CLOCK GOUGED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998020500742 19980205 00742 NM 1998 2 5 P5CA9800053 1 19980131 A 5210 DOOR BOEING 747 747123 1384873 NM IL PAX DOOR DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 LEFT MAIN ENTRY DOOR DENTED UPPER HINGE AREA. REPAIRED PER SRM 51-30-02 AND SRM 52-11-14. 2 L 7 4 4F A20WE 1998020500743 19980205 00743 NM 1998 2 5 P5CA9800054 1 19980129 A 5400 ANGLE BOEING 747 747123 1384873 NM NR 2 PYLON BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 2 PYLON, LEFT SIDE ATTACH ANGLE BROKEN SLOT SEAL AREA. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500744 19980205 00744 NM 1998 2 5 P5CA9800055 1 19980128 A 2510 FASTENERS BOEING 747 747123 1384873 NM CREW LADDER LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 CREW LADDER 5 STEPS LOOSE FASTENERS. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500745 19980205 00745 NM 1998 2 5 P5CA9800056 1 19980128 A 5230 SKIN BOEING 747 747123 1384873 NM CARGO DOOR GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BS 580 FWD LOWER CARGO DOOR GOUGED. REPAIRED PER SRM 51-30-01 DETAIL 1. 2 L 7 4 4F A20WE 1998020500746 19980205 00746 NM 1998 2 5 P5CA9800057 1 19980131 A 5320 RACK BOEING 747 747123 1384873 NM E/E COMPT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 E AND E COMPARTMENT VERTICAL CANNON PLUGS RACK STATION 460 HAS 8 DAMAGED STANCHION. REMOVED AND REPLACED PER SRM 51-10- 01. 2 L 7 4 4F A20WE 1998020500747 19980205 00747 NM 1998 2 5 P5CA9800058 1 19980129 A 5230 SKIN BOEING 747 747123 1384873 NM CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FWD CARGO DOOR SKIN DAMAGED AT LWR AFT CORNER. REPAIRED PER SRM 52-30-00, 51-30-02, 51-10-02. 2 L 7 4 4F A20WE 1998020500748 19980205 00748 NM 1998 2 5 P5CA9800059 1 19980128 A 7110 RETAINER BOEING 747 747123 1384873 NM NR 3 COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 INBD POWER COWL SEAL RETAINER DAMAGED. REPAIRED PER SRM 51-01-01. 2 L 7 4 4F A20WE 1998020500749 19980205 00749 NM 1998 2 5 P5CA9800060 1 19980128 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 3 COWL LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 ENGINE OUTBD MAIN COWL U-BOLT FASTENERS LOOSE. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500750 19980205 00750 NM 1998 2 5 P5CA9800061 1 19980128 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 3 COWL MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 ENGINE OUTBD MAIN COWL PERVIOUS REPAIR FASTENERS MISSING. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500751 19980205 00751 NM 1998 2 5 P5CA9800062 1 19980128 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 3 COWL MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 ENGINE INBD POWER COWL FLANGE PIN BRACKET HAS 2 HI-LOK FASTENERS MISSING. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500752 19980205 00752 NM 1998 2 5 P5CA9800063 1 19980128 A 7110 COWL BOEING 747 747123 1384873 NM NR 4 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 ENGINE INBD MAIN POWER COWL DAMAGED. REPAIRED PER SRM 51-30-03, 51-10-01. 2 L 7 4 4F A20WE 1998020500753 19980205 00753 NM 1998 2 5 P5CA9800064 1 19980128 A 7110 RIVETS BOEING 747 747123 1384873 NM NR 4 COWL MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 ENGINE INBD POWER COWL NR 3 LATCH RETAINING PLATE RIVETS MISSING. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500754 19980205 00754 NM 1998 2 5 P5CA9800065 1 19980131 A 7110 RETAINER BOEING 747 747123 1384873 NM NR 4 COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 ENGINE INBD POWER COWL RETAINER DAMAGED. REMOVED AND REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998020500755 19980205 00755 NM 1998 2 5 P5CA9800066 1 19980128 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 4 COWL MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 ENGINE INBD MAIN COWL 2 FASTENERS MISSING. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500756 19980205 00756 NM 1998 2 5 P5CA9800067 1 19980127 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 3 COWL LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 ENGINE INBD MAIN COWL AFT BOTTOM PRECOOLER DOOR BRACKET LOOSE FASTENERS. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500757 19980205 00757 NM 1998 2 5 P5CA9800068 1 19980127 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 3 COWL LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 ENGINE INBD COWL PRECOOLER DOOR BRACKET LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500758 19980205 00758 NM 1998 2 5 P5CA9800069 1 19980131 A 7110 FRAME BOEING 747 747123 1384873 NM NR 3 COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 POWER COWL OUTBD SIDE NR 3 LATCH FRAME CRACKED. REPARIED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998020500759 19980205 00759 NM 1998 2 5 P5CA9800070 1 19980128 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 3 COWL LATCH MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 POWER COWL 5 LATCH ASSY MISSING FASTENERS. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500760 19980205 00760 NM 1998 2 5 P5CA9800071 1 19980131 A 7110 FRAME BOEING 747 747123 1384873 NM NR 1 COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 LT POWER COWL NR 5 LATCH FRAME CRACKED. REPAIRED PER SRM 51-10-01, 51-30-02. 2 L 7 4 4F A20WE 1998020500761 19980205 00761 NM 1998 2 5 P5CA9800072 1 19980129 A 7110 GUIDE PIN BOEING 747 747123 1384873 NM NR 1 COWL WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 ENGINE POWER COWL OUTBD SIDE WORN GUIDE PIN. REMOVED AND REPLACED OUTBD ASSY PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998020500762 19980205 00762 NM 1998 2 5 P5CA9800073 1 19980128 A 7110 FASTENERS BOEING 747 747123 1384873 NM NR 1 COWL LATCH MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 POWER COWL FWD LATCH FASTENER LOOSE MISSING FASTENERS. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500763 19980205 00763 NM 1998 2 5 P5CA9800074 1 19980130 A 7110 DOUBLER BOEING 747 747123 1384873 NM NR 1 COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 POWER COWL LEFT SIDE DOUBLER DAMAGED. REMOVED AND REPLACED DOUBLER PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500764 19980205 00764 NM 1998 2 5 P5CA9800075 1 19980131 A 7110 COWL BOEING 747 747123 1384873 NM NR 1 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 OUTBD POWER COWL HINGE AREA DAMAGED. REPAIRED PER SRM 54-30-01. 2 L 7 4 4F A20WE 1998020500765 19980205 00765 NM 1998 2 5 P5CA9800076 1 19980130 A 7110 FRAME BOEING 747 747123 1384873 NM NR 1 COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 POWER COWL LEFT SIDE LWR FRAME CHAFE/CRACK. REMOVED AND REPLACED FRAME PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998020500766 19980205 00766 NM 1998 2 5 P5CA9800077 1 19980131 A 7110 RIB BOEING 747 747123 1384873 NM NR 4 COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 4 RT POWER COWL NR 3 RIB ASSY DAMAGED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998020500767 19980205 00767 NM 1998 2 5 P5CA9800078 1 19980129 A 5753 RETAINER BOEING 747 747123 1384873 NM RT TE MIDFLAP BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT WING INBD MIDFLAP SEAL RETAINER BROKEN. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500768 19980205 00768 NM 1998 2 5 P5CA9800079 1 19980101 A 5753 PANEL BOEING 747 747123 1384873 NM LT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LT WING OUTBD MIDFLAP ASSY COVE LIP PANEL HAS 10 FT CRACK. REMOVED AND REPLACED LT MIDFLAP ASSY COVE LIP PANEL PER MM 2 7-51-31. 2 L 7 4 4F A20WE 1998020500769 19980205 00769 NM 1998 2 5 P5CA9800080 1 19980130 A 5312 BULKHEAD BOLT BOEING 747 747123 1384873 NM AFT PRESS BLKHD MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 AFT PRESSURE BULKHEAD LONGERON 8R BOLT MISSING. REMOVED AND REPLACED BOLT PER SRM 51-30-02, 51-30-04. 2 L 7 4 4F A20WE 1998020500770 19980205 00770 NM 1998 2 5 P5CA9800081 1 19980129 A 5753 CANOE ASSY BOEING 747 747123 1384873 NM RT WING HOLE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT WING NR 7 CANOE ASSY HOLE OUTBD SIDE. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998020500771 19980205 00771 NM 1998 2 5 P5CA9800082 1 19980131 A 7110 FRAME BOEING 747 747123 1384873 NM NR 3 COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 3 INBD CORE COWL AFT FRAME CRACKED AT BOTTON. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998020500772 19980205 00772 NM 1998 2 5 P5CA9800083 1 19980131 A 5414 PANEL BOEING 747 747123 1384873 NM NR 1 PYLON DAMAGE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 NR 1 PYLON UPPER AFT END HAS FIBERGLASS PANEL DAMAGE. REPAIRED PER SRM 51-40-09, 52-24-11. 2 L 7 4 4F A20WE 1998020500773 19980205 00773 NM 1998 2 5 P5CA9800084 1 19980130 A 5320 STIFFENER BOEING 747 747123 1384873 NM BS 1350 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 HORIZONTAL STIFFENER CORRODED AT STA 1350 AT KEEL BEAM AREA. REMOVED AND REPLACED STIFFENER ASSY AT STA 1350 KEEL BEAM AREA PER SRM 51-10-01, 51-30-02. 2 L 7 4 4F A20WE 1998020500774 19980205 00774 NM 1998 2 5 P5CA9800085 1 19980130 A 5320 STIFFENER BOEING 747 747123 1384873 NM BS 1030 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 HORIZONTAL STIFFENER IS CORRODED AT STA 1030 IN KEEL BEAM AREA. REMOVED AND REPLACED STIFFENER PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998020500775 19980205 00775 NM 1998 2 5 P5CA9800086 1 19980201 A 5720 65B00118211 TIP BOEING 747 747122 1384872 NM LT WING DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 ON WALKAROUND, FOUND DENT IN LEFT WING TIP PANEL FWD SECTION. REMOVED AND REPLACED WING TIP PER MM 57-23-01. 2 L 7 4 4F A20WE 1998020500776 19980205 00776 NM 1998 2 5 P5CA9800087 1 19980202 A 5730 01540902 PANEL BOEING 747 747123 1384873 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT WING TRAILING EDGE FIXED PANEL - FLYING PANEL- IS CRACKED. REMOVED AND REPLACED PER SRM 51-30-02, 51-10-01 AND MM 57-22-01. 2 L 7 4 4F A20WE 1998020500777 19980205 00777 NM 1998 2 5 VNAA9801014 1 19980129 A 3080 0871DWI ICE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 431JS 8784 3028 DURING TAXI, AN ICE DETECTOR FAIL WARNING MESSAGE WAS NOTED BY THE CREW. THE ICE DETECTOR WAS PREVIOUSLY DEFERRED, AND THE WARNING LIGHT SHOULD NOT ILLUMINATE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND DETERMINED THAT THE DETECTOR WAS FAULTED IN A WAY THAT CAUSED THE WARNING LIGHT TO ILLUMIMATE. MAINTENANCE REMOVED AND REPLACED THE ICE DETECTOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-51-00. OPERATION CHECKS WERE SATISFACTORY AND THE DEFERRAL W AS REMOVED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998020500798 19980205 00798 WP 1998 2 5 ORJA9801 1 19980101 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP CABIN FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS IN ROW 21-24 CAME ON IN FLIGHT. REPAIRED AND REPLACED BATTERY CHARGER AT AFT LEFT OVERWING EXIT IAW MM OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998020500799 19980205 00799 NM 1998 2 5 BJNA980101 1 19980103 A 2612 CONNECTOR BOEING 737 737214 138446R NM NR 2 FIRE DET LOOSE A BJNA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 11 457TM 20156 FIRE WARNING ENGINE NR 2 LIGHT AND BELL ALARM. DISCOVERED LOOSE AND WATER SOAKED CONNECTOR ON ENGINE NR 2, FIRE DETECTI ON LOOP. CLEANED CONNECTOR AND TIGHTENED PER BMM 26-11-0. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998020500808 19980205 00808 WP 1998 2 5 NOCA0193 1 19980105 A 2910 7036907615 LINE DOUG DC9 DC983 3022083 WP LT HYD SYSTEM RUPTURED A NOCA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 15 183NA 49808 DURING CLIMB, LEFT HYDRAULIC QUANTITY LOW FOLLOWED BY LOSS OF SYSTEM PRESSURE AND LEFT HYDRAULIC PRESSURE ANNUNCIATOR. A IRCRAFT RETURNED TO JFK. ON GROUND, FOUND HYDRAULIC PRESSURE LINE FROM LEFT PRESSURE FILTER MODULE RUPTURED. REPLACED HYDRAULIC LINE AND LEFT ENGINE HYDRAULIC PUMP. OPS AND LEAK CHECKED OK. (M) 2 L 7 2 4F RT A6WE 1998020500845 19980205 00845 NM 1998 2 5 TAOA019805 1 19980110 A 3350 900542 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 4459 20447 FLT 6141 - BOS-LGA - RIGHT FORWARD OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK N ORMAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998020500846 19980205 00846 NM 1998 2 5 TAOA019803 1 19980108 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS R3289 20415 FLT 6500 - OVERNIGHT L/S LGA, LEFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998020500848 19980205 00848 CE 1998 2 5 98ZZZM153 1 19980102 A 2720 1145240381 ARM BEECH 1900 1900D 1154162 CE EMPENNAGE LOOSE A A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 861CA 5224 UE164 PILOT REPORTED ABNORMAL RUDDER CONTROL MOVEMENTS. INVESTIGATION AND INSPECTION OF CONTROL SYSTEM DISCOVERED RUDDER ARM ATTACHMENTS TO TORQUE SHAFT. LOOSE DUE TO LOOSE AND WORN FASTENERS (RIVETS) UNIT WAS REPLACED WITH NEW TORQUE SHAFT ASS EMBLE. 2 L 7 2 4T RT A24CE 1998020500849 19980205 00849 CE 1998 2 5 MASA98005 1 19980109 A 3243 9038000133 MASTER CYLINDER BEECH 1900 1900D 1154162 CE PILOTS RT BRAKE WORN A MASA K NONE O OTHER LD LANDING 1 SW 07 6YV UE6 FLT 5392 - BOS-PQI - CAPTAIN REPORTED LOSS OF RT BRAKES ON CAPTAINS SIDE ON LANDING. MAINTENANCE REMOVED AND REPLACED T HE MASTER CYLINDER. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998020500851 19980205 00851 WP 1998 2 5 NOCA0298 1 19980107 A 3350 P401021 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 FORWARD AND MID CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT INOP. BREAKAWAY BAND. REPLACED MID CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AND INSTALLED BREAKAWAY BANK. OPS CHECKED OK FOR FORWARD AND MID CABIN FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS. (M) 2 L 7 2 4F RT A6WE 1998020500859 19980205 00859 NM 1998 2 5 USAASB98001 1 19980102 A 3350 S106 BATTERY BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 228US 21817 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE AFT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE B ATTERIES. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998020500867 19980205 00867 EU 1998 2 5 SIMA980081 1 19980108 A 5330 S5367120500060 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 971NA 017 SAW - DURING MBV-2 INSPECTION MAINTENANCE DISCOVERED A DENT IN THE FUSELAGE SKIN 24 INCH AFT OF PAX DOOR. MAINTENANCE R EPAIRED THE DENT IAW SRM 51-21-27 FIGURE 403. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998020500899 19980205 00899 NM 1998 2 5 BJNA980102 1 19980108 A 2612 FIRE LOOP BOEING 737 737214 138446R NM NR 2 ENGINE CHAFED A BJNA O OTHER N FALSE WARNING CR CRUISE 1 WP 11 457TM 20156 NR 2 ENGINE FIRE WARNING SYSTEM INTERMITTENT LIGHT AND BELL, 3 SECONDS IN LENGTH IN CRUISE AND APPROACH EKO. REPAIRED C HAFED WIRE FOR UPPER LOOP AT STATIONARY COWL FORWARD SUPPORT PER BSWP MANUAL, 20-00-11. GROUND CHECKS NORMAL. RAN ENGI NE, NO PNEUMATICS LEAKS. (M) 2 L 7 2 4F A16WE 1998020500900 19980205 00900 NM 1998 2 5 WRLA98037 1 19980113 A 5330 AGA74191 SKIN DOUG MD11 MD11 3023602 NM BS 1710-1862 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE SKIN PANEL AT STATION 1710-1862 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. SKIN PANEL REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG'S NGA6314, AGA7419, AND NFA6374. (M) 2 L 7 3 4F RT A22WE 1998020500901 19980205 00901 NM 1998 2 5 WRLA98036 1 19980113 A 5311 ACJ72635 FRAME DOUG MD11 MD11 3023602 NM BS 1996 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1996 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG ACJ7363. (M) 2 L 7 3 4F RT A22WE 1998020500902 19980205 00902 NM 1998 2 5 WRLA98035 1 19980113 A 5311 AGA715121 FRAME DOUG MD11 MD11 3023602 NM BS 1986 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1986 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA8007, AGA7151, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500903 19980205 00903 NM 1998 2 5 WRLA98034 1 19980113 A 5311 AGA71523 FRAME DOUG MD11 MD11 3023602 NM BS 1986 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1986 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA 8007, AGA7151, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500904 19980205 00904 NM 1998 2 5 WRLA98033 1 19980113 A 5311 AGA71359 FRAME DOUG MD11 MD11 3023602 NM BS 1975 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1975 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA 8002, AGA7135, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500905 19980205 00905 NM 1998 2 5 WRLA98032 1 19980113 A 5311 AG8002415 FRAME DOUG MD11 MD11 3023602 NM BS 1975 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1975 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA8002, AGA7135, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500906 19980205 00906 NM 1998 2 5 WRLA98031 1 19980113 A 5311 AG800213 FRAME DOUG MD11 MD11 3023602 NM BS 1975 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1975 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA8002, AGA7135, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500907 19980205 00907 NM 1998 2 5 WRLA98030 1 19980113 A 5311 AGA71825 FRAME DOUG MD11 MD11 3023602 NM BS 1964 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1964 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7138, AGA7134, AGA7182, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500908 19980205 00908 NM 1998 2 5 WRLA98029 1 19980113 A 5311 AGA71823 FRAME DOUG MD11 MD11 3023602 NM BS 1964 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1964 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7138, AGA7134, AGA7182, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500909 19980205 00909 NM 1998 2 5 WRLA98028 1 19980113 A 5311 AGA7134405 FRAME DOUG MD11 MD11 3023602 NM BS 1964 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1964 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7138, AGA7134, AGA7182, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500910 19980205 00910 NM 1998 2 5 WRLA98056 1 19980113 A 5320 AGA798125 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA 7198. (M) 2 L 7 3 4F RT A22WE 1998020500911 19980205 00911 NM 1998 2 5 WRLA98055 1 19980113 A 5320 AGA798121 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPALCED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500912 19980205 00912 NM 1998 2 5 WRLA98054 1 19980113 A 5320 AGA798111 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLAFED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500913 19980205 00913 NM 1998 2 5 WRLA98053 1 19980113 A 5320 AFA389657 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500914 19980205 00914 NM 1998 2 5 WRLA98052 1 19980113 A 5320 AFA389645 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500915 19980205 00915 NM 1998 2 5 WRLA98051 1 19980113 A 5320 AFA389641 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500916 19980205 00916 NM 1998 2 5 WRLA98050 1 19980113 A 5320 AFA389639 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500917 19980205 00917 NM 1998 2 5 WRLA98049 1 19980113 A 5320 AGA72219 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500918 19980205 00918 NM 1998 2 5 WRLA98048 1 19980113 A 5320 AGA72217 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500919 19980205 00919 NM 1998 2 5 WRLA98047 1 19980113 A 5320 AGA72215 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981,A ND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500920 19980205 00920 NM 1998 2 5 WRLA98046 1 19980113 A 5320 AGA72213 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500921 19980205 00921 NM 1998 2 5 WRLA98044 1 19980113 A 5320 ACA76735 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500922 19980205 00922 NM 1998 2 5 WRLA98045 1 19980113 A 5320 ACA76739 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500923 19980205 00923 NM 1998 2 5 WRLA98070 1 19980113 A 5400 2215122 RING DOUG MD11 MD11 3023602 NM NR 2 ENGINE BENT A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 NR 2 ENGINE BELLMOUTH RING DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BELLMOUTH RING REPAIRED BY DOUGLAS AIRCRAFT COMPANY P ER ROHR ROD SKETCH PWRS065, REV 2. (M) 2 L 7 3 4F RT A22WE 1998020500924 19980205 00924 NM 1998 2 5 WRLA98069 1 19980113 A 5320 AWJ73433 POST DOUG MD11 MD11 3023602 NM BS 1841 BENT A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 POST AT STATION 1841 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. POST REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG NWJ63 08. (M) 2 L 7 3 4F RT A22WE 1998020500925 19980205 00925 NM 1998 2 5 WRLA98068 1 19980113 A 5320 AWJ73441 BEAM DOUG MD11 MD11 3023602 NM BS 1841 BENT A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 BEAM AT STATION 1841 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BEAM REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG NWJ63 08. (M) 2 L 7 3 4F RT A22WE 1998020500926 19980205 00926 NM 1998 2 5 WRLA98067 1 19980113 A 5320 AGA7978406 STANCHION DOUG MD11 MD11 3023602 NM BS 1968 BENT A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 STANCHION AT STATION 1968 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. STANCHION REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG AGA7978. (M) 2 L 7 3 4F RT A22WE 1998020500927 19980205 00927 NM 1998 2 5 WRLA98066 1 19980113 A 5320 AGA7978403 STANCHION DOUG MD11 MD11 3023602 NM BS 1968 BENT A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 STANCHION AT STATION 1968 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. STANCHION REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG AGA7978. (M) 2 L 7 3 4F RT A22WE 1998020500928 19980205 00928 NM 1998 2 5 WRLA98065 1 19980113 A 5320 AGA7978401 STANCHION DOUG MD11 MD11 3023602 NM BS 1968 BENT A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 STANCHION AT STATION 1968 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. STANCHION REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG AGA7978. (M) 2 L 7 3 4F RT A22WE 1998020500929 19980205 00929 NM 1998 2 5 WRLA98063 1 19980113 A 5312 AJC7050508 BULKHEAD DOUG MD11 MD11 3023602 NM BS 2007 WRINKLED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 BULKHEAD AT STATION 2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BULKHEAD REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DAC D WG AJC7050, ROD SKETCH 97-12-09-023. (M) 2 L 7 3 4F RT A22WE 1998020500930 19980205 00930 NM 1998 2 5 WRLA98062 1 19980113 A 5312 AJC7050505 BULKHEAD DOUG MD11 MD11 3023602 NM BS 2007 WRINKLED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 BULKHEAD AT STATION 2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BULKHEAD REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DAC D WG AJC7050, ROD SKETCH 97-12-09-023. (M) 2 L 7 3 4F RT A22WE 1998020500931 19980205 00931 NM 1998 2 5 WRLA98064 1 19980113 A 5320 AGA79853 STRUT DOUG MD11 MD11 3023602 NM BS 1986 BENT A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 STRUT AT STATION 1986 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. STRUT REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG AGA 7985. (M) 2 L 7 3 4F RT A22WE 1998020500932 19980205 00932 NM 1998 2 5 WRLA98061 1 19980113 A 5330 AGA3102501 SKIN DOUG MD11 MD11 3023602 NM BS 1831-2007 WRINKLED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 SKIN PANEL AT STATION 1831-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. SKIN PANEL REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG'S NGA6313, NJC6374, AND RON SKETCH 97-11-30-002. (M) 2 L 7 3 4F RT A22WE 1998020500933 19980205 00933 NM 1998 2 5 WRLA98060 1 19980113 A 5330 AGA73811 SKIN DOUG MD11 MD11 3023602 NM BS 1887-1902 WRINKLED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 SKIN PANEL AT STATION 1887-1902, LEFT SIDE DAMAGED DURING 'TAIL STRIKE' ACCIDENT. SKIN PANEL REPAIRED BY DOUGLAS AIRCRA FT COMPANY PER DAC DPS 3.69.9, AND ROD SKETCH 97-12-05-009. (M) 2 L 7 3 4F RT A22WE 1998020500934 19980205 00934 NM 1998 2 5 WRLA98059 1 19980113 A 5330 NGA6313513 SKIN DOUG MD11 MD11 3023602 NM BS 1821-1887 WRINKLED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 SKIN PANEL AT STATION 1821-1887, LEFT SIDE DAMAGED DURING 'TAIL STRIKE' ACCIDENT. SKIN PANEL REPAIRED BY DOUGLAS AIRCRA FT COMPANY PER DAC DWG NGA6313, AND ROD SKETCH 97-11-30-001. (M) 2 L 7 3 4F RT A22WE 1998020500935 19980205 00935 NM 1998 2 5 WRLA98058 1 19980113 A 5320 AGA71984 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED DOUGLAS AIRCRAFT COMPANY P ER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500936 19980205 00936 NM 1998 2 5 WRLA98057 1 19980113 A 5320 AGA71983 INTERCOSTAL DOUG MD11 MD11 3023602 NM BS 1841-2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 INTERCOSTAL AT STATION 1841-2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. INTERCOSTAL REPLACED BY DOUGLAS AIRCRAFT COMPAN Y PER DAC DWG'S ACA7673, AGA7221, AFA3896, AGA7981, AND AGA7198. (M) 2 L 7 3 4F RT A22WE 1998020500937 19980205 00937 NM 1998 2 5 WRLA98013 1 19980113 A 5311 AGA71293 FRAME DOUG MD11 MD11 3023602 NM BS 1902 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1902 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7129, AGA7147, AND AGA3850. (M) 2 L 7 3 4F RT A22WE 1998020500938 19980205 00938 NM 1998 2 5 WRLA98012 1 19980113 A 5311 AGA3849P4000 FRAME DOUG MD11 MD11 3023602 NM BS 1887 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1887 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7350, AGA7356, AGA3849. (M) 2 L 7 3 4F RT A22WE 1998020500939 19980205 00939 NM 1998 2 5 WRLA98011 1 19980113 A 5311 AGA735621 FRAME DOUG MD11 MD11 3023602 NM BS 1887 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1887 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7350, AGA7356, AGA3849. (M) 2 L 7 3 4F RT A22WE 1998020500940 19980205 00940 NM 1998 2 5 WRLA98010 1 19980113 A 5311 AGA735031 FRAME DOUG MD11 MD11 3023602 NM BS 1887 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1887 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7350, AGA7356, AGA3849. (M) 2 L 7 3 4F RT A22WE 1998020500941 19980205 00941 NM 1998 2 5 WRLA98009 1 19980113 A 5311 AGA3848P4000 FRAME DOUG MD11 MD11 3023602 NM BS 1871 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1871 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7351, AGA7355, AGA3848. (M) 2 L 7 3 4F RT A22WE 1998020500942 19980205 00942 NM 1998 2 5 WRLA98008 1 19980113 A 5311 AGA7355405 FRAME DOUG MD11 MD11 3023602 NM BS 1871 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1871 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7351, AGA7355, AGA3848. (M) 2 L 7 3 4F RT A22WE 1998020500943 19980205 00943 NM 1998 2 5 WRLA98007 1 19980113 A 5311 AGA734131 FRAME DOUG MD11 MD11 3023602 NM BS 1871 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1871 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7351, AGA7355, AGA3848. (M) 2 L 7 3 4F RT A22WE 1998020500944 19980205 00944 NM 1998 2 5 WRLA98006 1 19980113 A 5311 AGA00163 FRAME DOUG MD11 MD11 3023602 NM BS 1853 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1853 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7136, AGA7150, AGA3847. (M) 2 L 7 3 4F RT A22WE 1998020500945 19980205 00945 NM 1998 2 5 WRLA98005 1 19980113 A 5311 AGA700611 FRAME DOUG MD11 MD11 3023602 NM BS 1853 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1853 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7136, AGA7150, AGA3847. (M) 2 L 7 3 4F RT A22WE 1998020500946 19980205 00946 NM 1998 2 5 WRLA98004 1 19980113 A 5311 AGA71253 FRAME DOUG MD11 MD11 3023602 NM BS 1841 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1841 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7098, AGA7125, AGA7170, AND NGA6314. (M) 2 L 7 3 4F RT A22WE 1998020500947 19980205 00947 NM 1998 2 5 WRLA98003 1 19980113 A 5311 AFA7099 FRAME DOUG MD11 MD11 3023602 NM BS 1821 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1821 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7097, AGA7099, AND DAC ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500948 19980205 00948 NM 1998 2 5 WRLA98002 1 19980113 A 5311 AFA71663 FRAME DOUG MD11 MD11 3023602 NM BS 1801 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATINO 1801 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AFA7166, AND DAC ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500949 19980205 00949 NM 1998 2 5 WRLA98027 1 19980113 A 5311 AGA71345 FRAME DOUG MD11 MD11 3023602 NM BS 1994 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1994 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7138, AGA7134, AGA7182, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500950 19980205 00950 NM 1998 2 5 WRLA98026 1 19980113 A 5311 AGA7202501 FRAME DOUG MD11 MD11 3023602 NM BS 1959 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1959 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG AGA7202. (M) 2 L 7 3 4F RT A22WE 1998020500951 19980205 00951 NM 1998 2 5 WRLA98025 1 19980113 A 5311 AGA71333 FRAME DOUG MD11 MD11 3023602 NM BS 1953 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1953 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7133, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500952 19980205 00952 NM 1998 2 5 WRLA98024 1 19980113 A 5311 AGA72237 FRAME DOUG MD11 MD11 3023602 NM BS 1946 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1946 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG AGA7223. (M) 2 L 7 3 4F RT A22WE 1998020500953 19980205 00953 NM 1998 2 5 WRLA98023 1 19980113 A 5311 AGA7183P417 FRAME DOUG MD11 MD11 3023602 NM BS 1942 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1942 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7132, AGA7183, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500954 19980205 00954 NM 1998 2 5 WRLA98022 1 19980113 A 5311 AGA71323 FRAME DOUG MD11 MD11 3023602 NM BS 1942 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1942 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7132, AGA7183, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500955 19980205 00955 NM 1998 2 5 WRLA98021 1 19980113 A 5311 AGA72225 FRAME DOUG MD11 MD11 3023602 NM BS 1937 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1937 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG AGA7222. (M) 2 L 7 3 4F RT A22WE 1998020500956 19980205 00956 NM 1998 2 5 WRLA98020 1 19980113 A 5311 AGA713111 FRAME DOUG MD11 MD11 3023602 NM BS 1931 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1931 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7131, AGA7534, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500957 19980205 00957 NM 1998 2 5 WRLA98019 1 19980113 A 5311 AGA75343 FRAME DOUG MD11 MD11 3023602 NM BS 1931 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1931 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7131, AGA7534, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500958 19980205 00958 NM 1998 2 5 WRLA98018 1 19980113 A 5311 AGA720113 FRAME DOUG MD11 MD11 3023602 NM BS 1926 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1926 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG AGA7201. (M) 2 L 7 3 4F RT A22WE 1998020500959 19980205 00959 NM 1998 2 5 WRLA98017 1 19980113 A 5311 AGA7184P4101 FRAME DOUG MD11 MD11 3023602 NM BS 1921 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1921 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG'S AGA7130, AGA7184, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500960 19980205 00960 NM 1998 2 5 WRLA98016 1 19980113 A 5311 AGA713011 FRAME DOUG MD11 MD11 3023602 NM BS 1921 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1921 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7130, AGA7184, AND ROD SKETCH 97-11-25-012. (M) 2 L 7 3 4F RT A22WE 1998020500961 19980205 00961 NM 1998 2 5 WRLA98015 1 19980113 A 5311 AGA3850P4001 FRAME DOUG MD11 MD11 3023602 NM BS 1902 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1902 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7129, AGA7147, AND AGA3850. (M) 2 L 7 3 4F RT A22WE 1998020500962 19980205 00962 NM 1998 2 5 WRLA98014 1 19980113 A 5311 AGA714715 FRAME DOUG MD11 MD11 3023602 NM BS 1902 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE FRAME AT STATION 1902 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. FRAME REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DA C DWG'S AGA7129, AGA7147 AND AGA3850. (M) 2 L 7 3 4F RT A22WE 1998020500963 19980205 00963 NM 1998 2 5 WRLA98043 1 19980113 A 5312 NJC6040337 BULKHEAD DOUG MD11 MD11 3023602 NM BS 2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 BULKHEAD AT STATION 2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BULKHEAD REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DAC D WG'S NCJ6040, AJC7207, AND ROD SKETCH 97-11-19-015. (M) 2 L 7 3 4F RT A22WE 1998020500964 19980205 00964 NM 1998 2 5 WRLA98042 1 19980114 A 5312 AJC72402 BULKHEAD DOUG MD11 MD11 3023602 NM BS 2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 BULKHEAD AT STATION 2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BULKHEAD REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DAC D WG'S NCJ6040, AJC7207, AND ROD SKETCH 97-11-19-015. (M) 2 L 7 3 4F RT A22WE 1998020500965 19980205 00965 NM 1998 2 5 WRLA98041 1 19980113 A 5312 AJC72401 BULKHEAD DOUG MD11 MD11 3023602 NM BS 2007 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 BULKHEAD AT STATION 2007 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BULKHEAD REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER DAC D WG'S NCJ6040, AJC7207, AND ROD SKETCH 97-11-19-015. (M) 2 L 7 3 4F RT A22WE 1998020500966 19980205 00966 NM 1998 2 5 WRLA98040 1 19980113 A 5330 AJC7207325 SKIN DOUG MD11 MD11 3023602 NM BS 2033-2047 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE SKIN PANEL AT STATION 2033-2047 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. SKIN PANEL REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG'S AJC7025, AND AJC7027. (M) 2 L 7 3 4F RT A22WE 1998020500967 19980205 00967 NM 1998 2 5 WRLA98039 1 19980113 A 5330 AJC72079 SKIN DOUG MD11 MD11 3023602 NM BS 1997-2033 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE SKIN PANEL AT STATION 1997-2033 DAMAGED DURING 'TAIL STRIKE' ACCIDENT. SKIN PANEL REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG'S AJC7264, AND AJC7207. (M) 2 L 7 3 4F RT A22WE 1998020500968 19980205 00968 NM 1998 2 5 WRLA98038 1 19980113 A 5330 AGA7418501 SKIN DOUG MD11 MD11 3023602 NM BS 1862-1997 CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 FUSELAGE SKIN PANEL AT STATION 1862-1997 DAMAGED DURNG 'TAIL STRIKE' ACCIDENT. SKIN PANEL REPLACED BY DOUGLAS AIRCRAFT COMPANY PER DAC DWG'S NGA6314, NCJ6374, AND AGA7416. (M) 2 L 7 3 4F RT A22WE 1998020500973 19980205 00973 NM 1998 2 5 98ZZZM159 1 19980106 A 3350 07912 LENS BOEING 737 737214 138446R NM CABIN MISSING A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 DURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMP ED AND REPLACED LENS, OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 1998020500974 19980205 00974 NM 1998 2 5 98ZZZM160 1 19980106 A 3350 3071BPE LAMP BOEING 737 737214 138446R NM CABIN MISSING A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 DURING LAYOVER CHECK OF AIRCRAFT 460, FOUND LENS AND LAMP MISSING FROM FLOOR EMERGENCY TRACK LIGHTING ROW 23DEF. RELAMP ED AND REPLACED LENS, OPS CHECKED GOOD. (M) 2 L 7 2 4F A16WE 1998020500975 19980205 00975 1998 2 5 98ZZZM161 4 19980109 A 3417 HG180U281 ADC BOEING 737 7372P6 NM NR 1 INOPERATIVE A ZZDA O OTHER O OTHER CR CRUISE 1 SO 15 EICJW 21355 DURING FLT 920 FROM MCO, THE AIRDATA COMPUTER FAILED. THE AIRCRAFT RETURNED TO MCO. REPLACED THE NR 1 AIR DATA COMPUTE R. TESTED THE ADC SYSTEM, ALL NORMAL. (M) 2 L 7 2 4F RT A16WE 1998020500999 19980205 00999 NM 1998 2 5 B4MR98012 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 660-860 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND FROM FS 660 TO FS 860 RBL 44 SEAT TRACK HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 53-10-5 FIG 1 AND 53-10-5 FIG 7. NON-ROUTINE TASK CARD NUMBER 11965. 2 L 7 3 4F RT A3WE 1998021100006 19980211 00006 WP 1998 2 11 DLL15980250 1 19980129 A 2910 RB211524B4I HYD LINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 2 ENGINE RUPTURED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 754DL 59648 193Y1181 014625 A/C REJECTED T/O DUE TO C-SYS LOST. FOUND NR 2 ENG RT HYD PUMP PRESS LINE BAD. REPLACED SAME, GROUND OPS NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1998021100019 19980211 00019 1998 2 11 HEEA0012690 4 19980126 A 3454 066308105 INDICATOR BOLKMS 117 BK117A3 5626015 EU COCKPIT NAV FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7040U 7180 COMPASS FLAG STAYS IN VIEW. 1 G 7 2 3U H13EU 1998021100075 19980211 00075 SW 1998 2 11 98ZZZX552 1 19980114 A 2910 790220 LINE GULSTM 500 500B 0141106 SW LT/RT WS 24 RUPTURED A HXUA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 09 78384 21000 500B1297112 HYDRAULIC LEAK IN PRESSURE LINE LEFT AND RIGHT WING AT WS 24. LINE FAILED BECAUSE OF CORROSION PITS UNDER IDENTIFICATIO N TAPE. AREA NORMALLY IS FREE OF MOISTURE. 1 H 7 2 3O 6A1 1998021100077 19980211 00077 EA 1998 2 11 98ZZZX554 2 19980114 A 8520 66734 STUD GULSTM 500 500B 0141106 SW LYC O540 IO540B1A5 41532 EA NR 5 CYLINDER FAILED A HXUA E A ENGINE SHUTDOWN UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 NM 09 23KM 250 143153 L760548 NR 5 CYLINDER THROUGH-STUD BROKE CAUSING STUDS 56-15 TO BREAK. CYLINDER BECAME LOOSE. ENGINE RAN ROUGH. ENGINE SHUT D OWN AND SAFE LANDING MADE. SUBMITTER SUGGESTED A POSSIBLE CAUSE AS OVERTORQUE OF CYLINDER HOLD-DOWN STUDS. 1 H 7 2 3O 3 O 6A1 1E4 1998021100091 19980211 00091 NE 1998 2 11 98ZZZX568 2 19980101 A 7310 43013761 MANIFOLD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FUEL LEAKS A A RMXA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 05 8765J 1G02324 S7054 LE45314 SUBMITTER STATES EXCESSIVE FUEL MANIFOLD LEAKS OVER THE LAST 18 MONTHS. ALLIED SIGNAL IS IN THE PROCESS OF RELEASING AN ASB LIMITING THE LIFE OF THE FUEL MANIFOLD TUBES. OTHER OPERATORS SUBMITTER CONTACTED ARE HAVING THE SAME PROBLEMS. O MNIFLIGHT HAS GONE TO A POST-FLIGHT CHECK AND A SHIFT-CHANGE CHECK OF THIS MANIFOLD. 1 G 7 2 3U 3 U H13EU E5NE 1998021100147 19980211 00147 NM 1998 2 11 TSAA9833042 1 19980112 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY SLIDE LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 33,534:51 HOURS. TAC: 39,782. 2 L 7 2 4F RT A16WE 1998021100148 19980211 00148 WP 1998 2 11 CALA9800173 1 19980204 A 2170 21D101 COALESCER BAGS DOUG DC9 DC932 3022066 WP CABIN DIRTY A CALA A D UNSCHED LANDING RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 17543 45789 SMOKE APPEARED IN THE CABIN AND COCKPIT AFTER TAKEOFF WITH THE ENGINE AND AIRFOIL ANTI-ICE ON. ALSO, THE RT AIR CONDITI ONING SUPPLY TEMP HIGH LIGHT ILLUMINATED. THE AIRFOIL ANTI-ICE WAS TURNED OFF AND THE SMOKE DISSIPATED. THE AIRCRAFT W AS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND COALESCER BAGS WITH OILY SUBSTANCE, WATER, AND D IRT PRESENT. THE COALESCER BAGS WERE REPLACED. THE ENGINES WERE RUN WITH PACKS AND ANTI-ICE SYSTEMS ON AND NO SMOKE WA S PRESENT. 2 L 7 2 4F A6WE 1998021100149 19980211 00149 WP 1998 2 11 CALA9800174 1 19980204 A 3010 42G304 SWITCH DOUG DC9 DC982 3022082 WP ANTI-ICE SYS INOPERATIVE A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 72830 35208 49490 WHEN THE AIRFOIL ANTI-ICE WAS CYCLED TO TAIL MODE ON FINAL APPROACH, THE ICE PROTECTION SUPPLY PRESSURE HIGH LIGHT BEGAN TO FLICKER ON AND OFF ACCOMPANIED BY OIL SMELL AND SMOKE IN COCKPIT. THE ANTI-ICE WAS TURNED OFF AND THE SMOKE CEASED. THE ANTI-ICE SUPPLY PRESSURE SWITCH WAS REPLACED AND THE LT WATER SEPARATOR BAG WAS CHANGED. LEAK AND OPERATIONAL CHE CKS WERE GOOD. 2 L 7 2 4F A6WE 1998021100150 19980211 00150 WP 1998 2 11 CALA9800175 1 19980202 A 5754 SKIN DOUG DC10 DC1030 3023501 WP LT LE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND A 2 X 3 DENT IN LT INBOARD LEADING EDGE SLAT WITH SIX POPPED RIVETS AT STA XIS 240.844. REPAIRED IAW E CRA 5750-02897 AND PLACED ON DIP TO REPLACE RIB WITHIN 365 DAYS OR NEXT C-CHECK. 2 L 7 3 4F A22WE 1998021100151 19980211 00151 WP 1998 2 11 CALA9800176 1 19980203 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1129 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36L. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53 -00-00. 2 L 7 3 4F A22WE 1998021100152 19980211 00152 NM 1998 2 11 CALA9800177 1 19980203 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 294.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 1.5 INCH CRACK ON UPPER FLANGE OF CABIN FLOOR SUPPORT THREE INCHES AFT OF FLOORBEAM AT STA 294.5, RBL 45. THE FLOOR SUPPORT WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1, 51-10-1, 5 1-40-3, FIGURE 3, AND 51-30-2. 2 L 7 3 4F RT A3WE 1998021100153 19980211 00153 NM 1998 2 11 CALA9800178 1 19980203 A 5330 SKIN BOEING 727 727243 138408D NM BS 510 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 5.25 INCH CRACK IN FUSELAGE SKIN AT STA 510 BETWEEN STRINGER 25 AND 26R. A DOUBLER WAS FABRICATED AN D INSTALLED IAW SRM 53-30-3. THE DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-8 AND 51-30-3. 2 L 7 3 4F RT A3WE 1998021100154 19980211 00154 NM 1998 2 11 CALA9800179 1 19980203 A 5313 STRINGER BOEING 727 727243 138408D NM BS 680-700 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED BETWEEN STA 680 AND 700. THE STRINGER SPLICE WAS RE MOVED AND A STRINGER SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-30-02, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F RT A3WE 1998021100155 19980211 00155 NM 1998 2 11 CALA9800180 1 19980203 A 5520 SUPPORT BOEING 727 727243 138408D NM LT/RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 1.25 INCH CRACK IN LT ELEVATOR SUPPORT AT TRAILING EDGE OF ELEVATOR OUTBOARD OF INBOARD TRIM TAB HING E BEARING. A 1.25 INCH CRACK WAS FOUND IN RT ELEVATOR OUTBOARD SUPPORT FOR ELEVATOR TRAILING EDGE AT TRIM TAB MOUNT ARE A. THE SUPPORTS WERE REMOVED, NEW SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2. 2 L 7 3 4F RT A3WE 1998021100156 19980211 00156 NM 1998 2 11 CALA9800181 1 19980204 A 5330 SKIN BOEING 727 727243 138408D NM BS 68 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND FUSELAGE SKIN TEAR STRAP CORRODED IN FORWARD CARGO COMPARTMENT AT BS 68, STRINGER 28R. A DOUBLER WAS F ABRICATED AND INSTALLED IAW SRM 53-30-4, 51-30-8, 51-30-3, FIGURE 12, AND 51-10-2. 2 L 7 3 4F RT A3WE 1998021100157 19980211 00157 NM 1998 2 11 CALA9800182 1 19980204 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND FLOORBEAM CORRODED AT CLIP NUTS, STA 380 BETWEEN RBL 24 AND 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53- 10-8. 2 L 7 3 4F RT A3WE 1998021100158 19980211 00158 NM 1998 2 11 CALA9800183 1 19980204 A 5330 SKIN BOEING 727 727243 138408D NM BS 279 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 279, STRINGER 22L. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SR M 51-30-1, FIGURE 1, 53-30-3, FIGURE 13, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F RT A3WE 1998021100159 19980211 00159 WP 1998 2 11 CALA9800184 1 19980204 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1129 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND A 2 INCH CRACK IN LONGERON AT STA 1129, STRINGER 36R. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53 -10-00. 2 L 7 3 4F A22WE 1998021100160 19980211 00160 WP 1998 2 11 CALA9800185 1 19980204 A 5210 ANGLE DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND A 1.4 INCH CRACK IN AFT CABIN DOOR ANGLE INSIDE DOOR AT CENTER RIGHT DOOR STOP. THE ANGLE WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998021100161 19980211 00161 WP 1998 2 11 CALA9800186 1 19980205 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND AFT FUSELAGE TAIL CONE EXTERIOR RELEASE HANDLE CLIPS BENT AND BROKEN. NEW CLIPS WERE INSTALLED AND TES TED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998021100162 19980211 00162 WP 1998 2 11 CALA9800187 1 19980205 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155-1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND CORROSION ON THRESHOLD SUPPORT TEE BETWEEN STA 1155 AND 1174 AT AFT CARGO DOOR CUTOUT. THE THRESHOLD S UPPORT WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1998021100163 19980211 00163 WP 1998 2 11 CALA9800188 1 19980205 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1155, LONGERON 30 IN AFT CARGO COMPARTMENT. THE FLOOR SUPPORT WAS REPLAC ED IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1998021100164 19980211 00164 NM 1998 2 11 9802176309 1 19980204 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND E-ZONE AND ROW 31HK FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED LIGHT ASSEMBLIES, OPE RATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998021100165 19980211 00165 NM 1998 2 11 9802182288 1 19980129 A 3350 POWER SUPPLY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 288US 21376 DURING PREFLIGHT, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERAT IONAL CHECK OK. 2 L 7 3 4F A3WE 1998021100166 19980211 00166 NM 1998 2 11 9802192288 1 19980129 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 288US 21376 AFT AIRSTAIR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998021100167 19980211 00167 NE 1998 2 11 9802206729 2 19980201 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 2 FAILED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 629US 22388 662633 APPROXIMATELY 30 MINUTES AFTER TAKEOFF, THE NR 2 ENGINE FILTER BYPASS WARNING LIGHT ILLUMINATED. THE ENGINE WAS SHUT DO WN AND THE AIRCRAFT RETURNED TO ANC. MAINTENANCE FOUND THE NR 2 ENGINE MAIN OIL FILTER CLOGGED. THE AIRCRAFT WAS FERRI ED ON THREE ENGINES TO MSP FOR AN ENGINE CHANGE. 2 L 7 4 4F 4 F A20WE E20EA 1998021100168 19980211 00168 WP 1998 2 11 9802219102 1 19980203 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 92S 47064 DURING INSPECTION, THE FLOOR PROXIMITY EMERGENMCY LIGHTS LOCATED IN THE CENTER CABIN WERE FOUND TO BE INOPERATIVE. MAIN TENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021100169 19980211 00169 WP 1998 2 11 9802229877 1 19980203 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING INSPECTION, THE OVERHEAD EMERGENCY LIGHTS LOCATED IN THE FIRST CLASS SECTION WERE FOUND TO BE INOPERATIVE. MAINT ENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021100170 19980211 00170 WP 1998 2 11 9802239854 1 19980202 A 3222 STRUT DOUG DC9 DC951 3022051 WP NLG DEFLATED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 763NC 47716 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. ALSO, NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATE D. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. INDICATIONS RETURNED TO NORMAL AFTER GEAR WAS EXTENDED FOR LANDING. MAINTENANCE FOUND NOSE LANDING GEAR STRUT DEFLATED. REPLACED NOSE STRUT SEALS AND SERVICED STRUT TO PROPER LE VELS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998021100171 19980211 00171 WP 1998 2 11 9802249856 1 19980204 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING INSPECTION, THE AFT ATTENDANT EMERGENCY FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021100172 19980211 00172 SO 1998 2 11 COMA9810036 1 19980202 A 2121 EVAC532C2 FAN EMB 120 EMB120RT SO COCKPIT FAILED A COMA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 159A 17806 120159 AT CRUISE FLIGHT THE COCKPIT AND CABIN STARTED FILLING UP WITH SMOKE. CREW DESCENDED FROM 17,000 FT AND MADE UNSCHEDULE D LANDING. FOUND RIGHT RECIRCULATION FAN TO BE FAULTY. REMOVED AND REPLACED FAN. 2 L 7 2 4T RT A31SO 1998021100173 19980211 00173 EA 1998 2 11 COMA9860036 1 19980202 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 01 931CA 7037 HAD TO CYCLE LANDING GEAR TWICE TO GET NLG DOWN AND LOCK. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 1998021100174 19980211 00174 NM 1998 2 11 UPS98225709 1 19980122 A 5753 65327348 SUPPORT BOEING 727 7272A1 138407F NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, NR 7 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT AFT BOLT HOLES FLAP TRACK FWD ATTACH POINT BUSHING HAS MIGRATED. ALSO, FWD HARDWARE REQUIRES REPLACEMENT I/B AND O/B AT RADIUS BLOCKS. REPLACED NR 7 FLAP TRACK FITTING IAW SRM 51-10-1 WILL BE INSTALLED ON TC C57-581-04-4D. 2 L 7 3 4F A3WE 1998021100175 19980211 00175 NM 1998 2 11 UPS98225710 1 19980118 A 5753 652165127 SUPPORT BOEING 727 7272A1 138407F NM TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, NR 4 FLAP TRACK FWD ATTACH FITTING IS CORRODED AT FLAP TRACK FWD ATTACH LUG I/B SIDE. REMOVED AND R EPLACED NR 4 FLAP TRACK FWD FITTING IAW MM 32-11-51. 2 L 7 3 4F A3WE 1998021100176 19980211 00176 NM 1998 2 11 UPS98225711 1 19980202 A 5531 651869052 RIB BOEING 727 7272A1 138407F NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE-SI, FRETTING CORROSION ON VERTICAL STAB L/E FAIRING RIB, FWD LIP AT FIN STA 55.9. RECEIVED NEW TEE-EXT RUDED RIB AND INSTALLED WEB TO NEW RIB PER 727 SRM 51-30-2. 2 L 7 3 4F A3WE 1998021100177 19980211 00177 NM 1998 2 11 UPS98425712 1 19980128 A 5330 SKIN BOEING 747 747123 1384873 NM AFT FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 674UP 20100 INSPECTION TYPE-N/A, UPON ARRIVAL FOUND SKIN DAMAGE AND PUNCTURED I/B OF TAIL STAND BAIL FITTING PUNCTURE IS APPROXIMATE LY 2 INCH LENGTH. TRANSFERRED TO L/P 319551 ITEM 1. REPAIRED DAMAGED SKIN AS PER EO B747-5330-10025A. CLOSED OUT NON- ROUTINE CARDS. 2 L 7 4 4F A20WE 1998021100178 19980211 00178 WP 1998 2 11 UPS98825707 1 19980202 A 3350 BATTERY DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-N/A, EMERGENCY LIGHTS BATTERY DEAD. CHARGED AND REINSTALLED EMERGENCY BATTERY, OP CHKS GOOD. 2 L 7 4 4F RT 4A25 1998021100179 19980211 00179 EU 1998 2 11 QXEA9800059 1 19980203 A 3350 551590004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTION A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 FORWARD OVERWING EXIT SIGN LIGHTS INOP. MAINTENANCE REPLACED CIRCUIT BOARD, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998021100180 19980211 00180 NM 1998 2 11 98FDEA00085 1 19980204 A 3030 9844886G1 HEATER BOEING 727 72722 1384002 NM RT STATIC PORT INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SO 25 167FE 18864 RIGHT STATIC LIGHT ON PITOT STATIC HEATER MONITOR PANEL ILLUMINATED WITH RIGHT SWITCH ON. FOUND FIRST OFFICER'S RIGHT ST ATIC PORT NOT HEATING. REPLACED HEATER, OPERATIONAL CHECKED PER MAINTENANCE MANUAL 30-31-0. LEAK CHECKED PER MAINTENAN CE MANUAL 34-11-0. 2 L 7 3 4F A3WE 1998021100181 19980211 00181 WP 1998 2 11 98FDEA00042 1 19980120 A 5312 BULKHEAD STRIP DOUG DC10 DC1010F 3022111 WP BS 1156 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 051FE 47805 LT SIDE OF Y-1156 PRESS BULKHEAD, AFT FACE, ATTACHMENT STRIP IS CRACKED FROM UPPER EDGE DOWNWARD THROUGH 1ST ROW OF RIVE TS TO SECOND ROW 1.4 LONG. ALSO, 1 SHEARED RIVET, FWD FACE ATTACHMENT STRIP IS CRACKED AT TOP ROW OF T-CAP TO STRIP ATT ACH RIVETS. CRACK IS Y SHAPED LONG LEG 1.6 SHORT LEG 1. LONG LEG DISAPPEARS UNDER FITTING AT OUTBOARD END. BOTH CRACK S IN AREA OF LONGERON NR 40 ATTACH. *S/D* REMOVED DAMAGED ATTACH STRIP AND SPLICED IN NEW SECTION AS PER EA NR 8-5340- 35200. 2 L 7 3 4F A22WE 1998021100182 19980211 00182 NM 1998 2 11 98FDEA00086 1 19980205 A 3297 WIRE DOUG MD11 MD11F 3023600 NM LANDING GEAR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 605FE 48514 AFTER TAKEOFF AND GEAR RETRACTION HAD 4 RED GEAR UNSAFE LIGHTS. FOLLOWED EMERGENCY PROCEDURES THAT HAD US CYCLE GEAR SE VERAL TIMES WITH NO SUCCESS. GEAR EXTENDS NORMALLY. VERIFIED PROBLEM WAS WITH INDICATION. WHILE ON GROUND INDICATION DID NOT SHIFT FROM GREEN TO RED WITH GEAR HANDLE PULLED. FOUND WIRE HARNESS INTERFERING WITH GEAR HANDLE SWITCH OPERATI ON. SECURED WIRING AWAY FROM HANDLE SWITCH AND HANDLE SWITCH OPERATED NORMAL. 2 L 7 3 4F RT A22WE 1998021100183 19980211 00183 NM 1998 2 11 98FDEA00087 1 19980205 A 5320 65198621 CHORD BOEING 727 72725 1384006 NM BS 351 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 156FE 18289 CORROSION (C53- 224-03) BS 351.2, WL 168, LBL 16 ON NOSE WHEEL WELL CHORD. *S/D* CORROSION BS 351.2, WL 168, LBL 16 ON NOSE WHEEL WELL CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED LT MED CHORD BS 294.5 -0 350 AND REPLA CED WITH NEW (P/N 65-19862-19) IAW BOEING DWG 65-18415 AND FED-EX SRM 51-30-2. 2 L 7 3 4F A3WE 1998021100184 19980211 00184 NM 1998 2 11 98FDEA00088 1 19980205 A 5320 65198622 CHORD BOEING 727 72725 1384006 NM BS 300 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 156FE 18289 NR 0401 004 WHILE WORKING NR 0259 FOUND CORROSION BS 300, WL 168, RBL 16 ON NOSE WHEEL WELL CHORD. REMOVED AND REPLACED NOSE WHEEL WELL CHORD BS 300, WL 168, RBL 16 IAW FED-EX DRAWING 65-18415 AND FED-EX SRM 51-30-2. 2 L 7 3 4F A3WE 1998021100185 19980211 00185 NM 1998 2 11 98FDEA00089 1 19980205 A 5320 654939820 CASTING BOEING 727 72721C 138400M NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 NR 0978 058, CORROSION (C53-224-02) ON CARGO NET CASTING BS 360 TO 380 IN WELL OF CASTING UNDER NET TIE DOWN RBL 45, WL 208. REPLACED CARGO NET CASTING BS 360 TO 380, RBL 45, WL 208 PER FED-EX 51-30-2. 2 L 7 3 4F A3WE 1998021100186 19980211 00186 WP 1998 2 11 MWEA98144 1 19980204 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP PAX DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING TRANSIT CHECK, FOUND FORWARD ENTRY DOOR SLIDE COVER FELL OFF. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1998021100187 19980211 00187 WP 1998 2 11 MWEA98145 1 19980204 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 37 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING C-CHECK, FOUND A CRACK THROUGH A FASTENER HOLE ON AFT FACE OF STATION 37 BULKHEAD. MTC REPAIRED IAW SRM 53-01 FI G 2. 2 L 7 2 4F A6WE 1998021100188 19980211 00188 WP 1998 2 11 MWEA98146 1 19980204 A 5400 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING C-CHECK, FOUND A CRACKED ANGLE ON LT PYLON STATION 1019. MTC REPAIRED IAW SRM 54-01 FIG 2 AND 51-30-05. 2 L 7 2 4F A6WE 1998021100189 19980211 00189 NM 1998 2 11 DL757980276 1 19980201 A 3350 BATTERY 61020 BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 664DN 25012 R-3 FLASHLIGHT WON'T BLINK. FOUND FLASHLIGHT OUT OF HOLDER ASSY. REPLACED BATTERY PLACARD AND STRAP, OPN NORM. 2 L 7 2 4F RT A2NM 1998021100190 19980211 00190 NM 1998 2 11 DL72S980278 1 19980202 A 5330 65545664 SKIN BOEING 727 727225 1384077 NM BS 490 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 FUSELAGE SKIN WAS FOUND CORRODED BETWEEN STA 480 AND 500 AND BETWEEN S28L AND BL 0. THE CORROSION WAS TRIMMED AWAY WITH A 9 BY 20 CUTOUT. REPAIRED PER ERA 363693-14. 2 L 7 3 4F A3WE 1998021100191 19980211 00191 NM 1998 2 11 DL72S980279 1 19980122 A 5754 STIFFENERS BOEING 727 727232 1384082 NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 2 EA WING L/E SPAR STIFFENERS CRACKED NR 3 L/E SLAT OUTBD TRACK ROLLER FITTING ATTACH. INSTALLED NEW ANGLES PER M/M 57- 20-21. 2 L 7 3 4F A3WE 1998021100192 19980211 00192 NM 1998 2 11 DL73S980280 1 19980202 A 5330 SKIN BOEING 737 737232 1384475 NM BS 379 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 FUSELAGE SKIN AT COOLING DUCT CUTOUT AT BS 379, BL 0 WAS FOUND CRACKED AT THE AFT EDGE OF THE CUTOUT. CRACK IS APPROX. 1.5 INCH LENGTH AND IS TYP PER SB 737-53-1117, R1. REPAIR PER ERA 331307-14. 2 L 7 2 4F RT A16WE 1998021100193 19980211 00193 NM 1998 2 11 DL72S980281 1 19980122 A 5720 STIFFENERS BOEING 727 727232 1384082 NM NR LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 2 EA WING L/E SPAR STIFFENERS CRACKED AT NR 4 L/E SLAT INBD TRACK ROLLER FITTING ATTACH. REPLACED STIFFENERS PER M/M 57 -20-21. 2 L 7 3 4F A3WE 1998021100194 19980211 00194 NM 1998 2 11 DL72K980284 1 19980128 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 ON MV2, FOUND AT STA 870 BLKHD WEB IS CRACKED AT LWR END JUST LEFT OF DELTA BEAM. REMOVED DAMAGED SECTION OF WEB, FABD NEW REPAIR PER SRM 53-10-9 FIG 4, INSTALLED DOUBLER PER SAME. 2 L 7 3 4F A3WE 1998021100195 19980211 00195 NM 1998 2 11 DL72K980285 1 19980121 A 7110 COWL RING BOEING 727 727232 1384082 NM NR 2 ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 AT MV2, FOUND COWL LANDING RING WORN SEVERAL PLACES AND TEMP REP AIR AT 6 CLOCK POS. INSTALLED NEW REPAIR PER MM 53-11- 0 PG 801. 2 L 7 3 4F A3WE 1998021100196 19980211 00196 WP 1998 2 11 DLL13980286 1 19980130 A 5711 1528363101 REAR SPAR LKHEED 1011 10113851 5265010 WP WS 293-346 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 784DA 193A1038 DURING INSPECTIONS, SEVERAL HOLES IN THE LT AND RT WING REAR SPAR UPPER CAP WERE FOUND CRACKED IN THE SKIN-TO-CAP AND CA P-TO-WEB HOLES. THE HOLES WERE OVERSIZED, COLD-WORKED, AND BUSHED. REPAIR DOUBLERS WERE INSTALLED ON THE CAP, SKIN AN D WEB PER ER/A 363783-14AD REV A. 2 L 7 3 4F A23WE 1998021100197 19980211 00197 NM 1998 2 11 DL72L980287 1 19980130 A 5330 SKIN BOEING 727 727232 1384082 NM BS 715 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 CORROSION WAS FOUND IN THE SKIN AT FS 705, BL 0. BECAUSE OF THE CORROSION AND THE PRESENSE OF EXISTING REPAIRS IN THE A REA THE SKIN WAS SPLICED AT APPROX FS 715 FROM STR 26L TO 26R. THE NEW SECTION OF SKIN WAS SPLICED PER B727 SRM 53-30-3 , EXCEPT THE SPLICE ENDS WERE MODIFIED TO ACCOMODATE THE S-26 LAP SPLICES. THE REPAIR WAS ACCOMPLISHED PER ER/A 363516- 14, REV C. 2 L 7 3 4F A3WE 1998021100198 19980211 00198 NM 1998 2 11 DL72S980290 1 19980202 A 5754 STIFFENER BOEING 727 727232 1384082 NM LT FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 FOUND AT LETTER CHECK E1, L/E SPAR STIFFENER CRACKED O/B SIDE NR 7 SLAT O/B TRACK. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998021100199 19980211 00199 NM 1998 2 11 DL72S980291 1 19980202 A 5754 STIFFENER BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 FOUND AT E1 LETTER CK, L/E SPAR STIFFENER CRACKED I/B SIDE OF 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998021100200 19980211 00200 NM 1998 2 11 DL72S980292 1 19980202 A 5754 STIFFENER BOEING 727 727232 1384082 NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 L/E SPAR STIFFENER CRACKED NR 2 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21 PG 813. 2 L 7 3 4F A3WE 1998021100201 19980211 00201 NM 1998 2 11 DL72K980295 1 19980203 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 471DA 20748 LOWER SKIN DAMAGED 58 INCHES FROM O/B END. REPAIRED PER SRM 55-20-3. NR 2895. 2 L 7 3 4F A3WE 1998021100202 19980211 00202 NM 1998 2 11 DL72E980297 1 19980203 A 5320 WEB BOEING 727 727247 138408F NM BS 1240 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 FOUND ON B1 LETTER CK, .25 INCH CRACK IN LIGHTENING HOLE LT VERT TORQUE BOX WEB. ROUTED OUT DAMAGED AREA PER MM 53-11-0 . 2 L 7 3 4F A3WE 1998021100203 19980211 00203 NM 1998 2 11 DL72E980299 1 19980203 A 5532 SKIN BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 FOUND DURING B-1 LETTER CHECK, 1.3125 INCH CRACK VERTICAL STAB SKIN AT BASE LT SIDE JUST ABOVE FUSELAGE STA 1340. REPAI RED PER M/M 55-30-0. 2 L 7 3 4F A3WE 1998021100204 19980211 00204 NM 1998 2 11 DL76L980300 1 19980203 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 182DN 25987 LT OVERWING EMERG EXIT SPOILER AND SLIDE SQUIBS WON'T TEST. REPLACED PWR SUPPLY AND BATT PACK. 2 L 7 2 4F RT A1NM 1998021100205 19980211 00205 NM 1998 2 11 DL757980302 1 19980202 A 5754 114N4005158 WEDGE BOEING 757 757232 1384965 NM NR 7 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 673DL 25978 THE NR 7 SLAT TRAILING EDGE WAS FOUND WITH A 4 X 5.5 AREA OF DELAMINATION ON THE LOWER SURFACE. THE DAMAGE WAS REPAIRED PER THE B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363912-14. 2 L 7 2 4F RT A2NM 1998021100207 19980211 00207 NM 1998 2 11 P5CA9800089 1 19980121 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2080 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FRAME AT BS 2080 STR 25 FOUND CRACKED. REPAIRED PER REPAIR SCHEME 53-60-33629. 2 L 7 4 4F A20WE 1998021100208 19980211 00208 NM 1998 2 11 P5CA9800090 1 19980121 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2060 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FRAME AT BS 2060 STRINGER 15 FOUND CRACKED. REPAIRED PER REPAIR SCHEME 53-60-33628. 2 L 7 4 4F A20WE 1998021100209 19980211 00209 NM 1998 2 11 P5CA9800091 1 19980121 A 5320 TIE CLIP BOEING 747 747132 1384882 NM BS 2180 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 STRINGER TIE CLIP AT BS 2180 STRINGER 12 FOUND CRACKED. REPLACED CLIP PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100210 19980211 00210 NM 1998 2 11 P5CA9800092 1 19980121 A 5311 FRAME BOEING 747 747132 1384882 NM BS 880 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FRAME CRACKED AT STRINGER CUTOUT DOUBLER. REPAIRED PER REPAIR SCHEME RS 53-22-33668 REF BOEING TELEX NR PAO HKG 98-0036 RE. 2 L 7 4 4F A20WE 1998021100211 19980211 00211 NM 1998 2 11 P5CA9800093 1 19980121 A 5320 SHEAR TIE BOEING 747 747132 1384882 NM BS 880 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FRAME SHEAR TIE CRACKED AT BS 880 LEFT STRINGERS 10 TO 11. REPAIRED PER REPAIR SCHEME 53-22-33669 AND BOEING TELEX. 2 L 7 4 4F A20WE 1998021100212 19980211 00212 NM 1998 2 11 P5CA9800094 1 19980121 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2040 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FRAME I/B FLANGE CRACKED AT FUSELAGE RIGHT BS 2040 STRINGER 15. REPAIRED PER REPAIR SCHEME 53-60-33627 AND BOEING TELEX . 2 L 7 4 4F A20WE 1998021100213 19980211 00213 NM 1998 2 11 P5CA9800095 1 19980121 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1760 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FRAME I/B FLANGE CRACKED AT FUSELAGE RIGHT BS 1760 STRINGER 15. REPAIRED PER REPAIR SCHEME 53-60-33626 AND BOEING TELEX . 2 L 7 4 4F A20WE 1998021100214 19980211 00214 NM 1998 2 11 P5CA9800096 1 19980121 A 5412 BULKHEAD BOEING 747 747132 1384882 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 2 PYLON BULKHEAD RT TOP CORNER FILLET PLATE FASTENER HOLES 2 EA CRACKED. DOUBLER REPAIRED PER REPAIR SCHEME 54-51-33 638 AND SB. 2 L 7 4 4F A20WE 1998021100215 19980211 00215 NM 1998 2 11 P5CA9800097 1 19980121 A 5210 REVEAL BOEING 747 747132 1384882 NM L4 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 L4 DOOR FWD CUTOUT UPPER CORNER REVEAL CRACKED 2 PLACES. REPAIRED PER HAECO REPAIR SCHEME R-53-61-33667. 2 L 7 4 4F A20WE 1998021100216 19980211 00216 NM 1998 2 11 P5CA9800098 1 19980121 A 5720 CHORD BOEING 747 747132 1384882 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LT WING LOWER CHORD FASTENER HOLE CRACK ON WEB AT 4 O'CLOCK POSITION. REPAIRED HOLE TO OVERSIZED TO .562 NDT NO CRACK F OUND PER HAECO RS 57-21-33654. 2 L 7 4 4F A20WE 1998021100217 19980211 00217 NM 1998 2 11 P5CA9800099 1 19980121 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1605 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION AT FUSELAGE LEFT STRINGER 20 AT BS 1605. BLENDED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100218 19980211 00218 NM 1998 2 11 P5CA9800100 1 19980121 A 5320 FORGING BOEING 747 747132 1384882 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FOUND ON FUSELAGE WINDOW FORGING. CORROSION BLENDED AND TREATED. REMAINING THICKNESS .081 INCHES DEE P PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100219 19980211 00219 NM 1998 2 11 P5CA9800101 1 19980121 A 5330 SKIN BOEING 747 747132 1384882 NM BS 2000-2120 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FOUND ON LAP SEAM FUSELAGE LEFT AT BS 2000 TO 2120. BLENDED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100220 19980211 00220 NM 1998 2 11 P5CA9800102 1 19980121 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1741 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FOUND ON SKIN LAP AT FUSELAGE RIGHT BS 1741 TO 2100 STRINGER 12. BLENDED AND TREATED PER SRM 51-10-01 . 2 L 7 4 4F A20WE 1998021100221 19980211 00221 NM 1998 2 11 P5CA9800103 1 19980121 A 5711 SPAR WEB BOEING 747 747132 1384882 NM CENTER TANK CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CENTER TANK REAR SPAR WEB FOUND CORROSION AT LT OVERRIDE JETTISON PUMP BONDING JUMPER ATTACH AREA. BLENDED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100222 19980211 00222 NM 1998 2 11 P5CA9800104 1 19980121 A 5280 CHANNEL BOEING 747 747132 1384882 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FWD HINGE SUPPORT CHANEL CRACKED LT BODY O/B STRUT DOOR. SUPPORT CHANEL REPAIRED PER SRM 51-40-03 FIG 4. 2 L 7 4 4F A20WE 1998021100223 19980211 00223 NM 1998 2 11 P5CA9800105 1 19980121 A 5753 CHANNEL BOEING 747 747132 1384882 NM NR 16 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RT WING NR 16 L/E FLAP PANEL UPPER O/B HINGE ATTACH CHANEL CRACKED. REPAIRED CHANEL PER SRM 51-10-01 PG 18. 2 L 7 4 4F A20WE 1998021100224 19980211 00224 NM 1998 2 11 P5CA9800106 1 19980121 A 5320 BRACKET BOEING 747 747132 1384882 NM BS 1840 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FUSELAGE BS 1840 TO 1860 BL 30 PDU SUPPORT ATTACH BRACKET CRACKED. REPAIRED BRACKET PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100225 19980211 00225 NM 1998 2 11 P5CA9800107 1 19980121 A 5755 65B023001 DOUBLER BOEING 747 747132 1384882 NM NR 8 SPOILER CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 8 SPOILER ROD END FITTING DOUBLER CRACKED AT FASTENER HOLES. REPLACED NR 8 SPOILER PER MM 27-61-01. 2 L 7 4 4F A20WE 1998021100226 19980211 00226 NM 1998 2 11 P5CA9800108 1 19980121 A 5754 RIB BOEING 747 747132 1384882 NM NR 14 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 14 L/E FLAP PANEL I/B WEB LOWER RADIUS CRACKED. REPLACED FLAP SUPPORT RIB PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100227 19980211 00227 NM 1998 2 11 P5CA9800109 1 19980121 A 5754 BRACKET BOEING 747 747132 1384882 NM NR 14 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 14 LE FLAP BULNOSE FAIRING MOST I/B AND MOST O/B ATTACH ARM TO FLAP PANEL BRACKETS ARE CRACKED. REPLACED BRACKETS PE R SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100228 19980211 00228 NM 1998 2 11 P5CA9800110 1 19980121 A 5754 BRACKET BOEING 747 747132 1384882 NM NR 13 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 13 L/E FLAP BULLNOSE MOST I/B ATTACH ARM BRACKET ON FLAP PANEL IS CRACKED. REPLACED BRACKET PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100229 19980211 00229 NM 1998 2 11 P5CA9800111 1 19980121 A 5754 WEB BOEING 747 747132 1384882 NM NR 13 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 13 L/E FLAP PANEL I/B WEB UPPER RADIUS CRACKED. REPAIRED PER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 1998021100230 19980211 00230 NM 1998 2 11 P5CA9800112 1 19980121 A 5755 65B022501 PANEL BOEING 747 747132 1384882 NM NR 10 SPOILER CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 10 SPOILER PANEL AT ROD END FITTING FILLET AREA CRACKED. REPLACED SPOILER PANEL PER SRM 27-61-02. 2 L 7 4 4F A20WE 1998021100231 19980211 00231 NM 1998 2 11 P5CA9800113 1 19980121 A 5755 65B022501 PANEL BOEING 747 747132 1384882 NM NR 3 SPOILER CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 3 SPOILER PANEL AT ROD END ATTACH FITTING FILLET AREA IS CRACKED. REPLACED SPOILER PANEL PER MM 27-61-02. 2 L 7 4 4F A20WE 1998021100232 19980211 00232 NM 1998 2 11 P5CA9800114 1 19980121 A 5320 TIE CLIP BOEING 747 747132 1384882 NM BS 2220 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 STRINGER TIE CLIP CRACKED AT FUSELAGE BS 2220 STRINGER 22L. REPLACED CLIP PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100233 19980211 00233 NM 1998 2 11 P5CA9800115 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK CROWN FLANGE AT BS 1500 TO 1520, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-1 0-01. 2 L 7 4 4F A20WE 1998021100234 19980211 00234 NM 1998 2 11 P5CA9800116 1 19980121 A 5753 PANEL BOEING 747 747132 1384882 NM LT TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LT I/B AFT FLAP LOWER CENTER STRESS PANEL DELAMINATED AT CENTER AREA. REPLACED STRESS PANEL PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100235 19980211 00235 NM 1998 2 11 P5CA9800117 1 19980121 A 2750 LINK BOEING 747 747132 1384882 NM NR 6 TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 6 CANOE FAIRING PIVOTING LINK I/B SURFACE LWR SECTION IS CRACKED. REPLACED LINK ASSY PER MM 27-51-26. 2 L 7 4 4F A20WE 1998021100236 19980211 00236 NM 1998 2 11 P5CA9800118 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1910 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1910, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100237 19980211 00237 NM 1998 2 11 P5CA9800119 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION IN SEAT TRACK FLANGE AT BS 1900 TO 1905, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100238 19980211 00238 NM 1998 2 11 P5CA9800120 1 19980121 A 5400 CHANNEL BOEING 747 747132 1384882 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 3 PYLON SKIRT BEAM AREA HYD PRESS FILTER MODULE UPPER SUPPORT CHANEL CRACKED. REPLACED CHANNEL PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100239 19980211 00239 NM 1998 2 11 P5CA9800121 1 19980121 A 5400 CHANNEL BOEING 747 747132 1384882 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 4 PYLON SKIRT BEAM AREA HYD PRESS FILTER SUPPORT CHANNELS CRACKED. REPLACED CHANNELS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100240 19980211 00240 NM 1998 2 11 P5CA9800122 1 19980121 A 5712 RIB BOEING 747 747132 1384882 NM NR 2 MAIN TANK CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 2 MAIN TANK LOWER REP STIFFENER CRACKED RIB. ALSO, WEB UNDER STIFFENER CRACKED. REPLACED STIFFENER AND REPAIRED WEB PER SRM 51-10-01 AND 57-10-05 FIG 2. 2 L 7 4 4F A20WE 1998021100241 19980211 00241 NM 1998 2 11 P5CA9800123 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2135 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK LOWER SURFACE AT BS 2135, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100242 19980211 00242 NM 1998 2 11 P5CA9800124 1 19980121 A 5210 GATE BOEING 747 747132 1384882 NM L1 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 L1 DOOR UPPER GATE CRACKED AT AREA 2 LOCATION. REPLACED GATE PER MM 51-11-01. 2 L 7 4 4F A20WE 1998021100243 19980211 00243 NM 1998 2 11 P5CA9800125 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1515 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1515, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100244 19980211 00244 NM 1998 2 11 P5CA9800126 1 19980121 A 5210 FRAME BOEING 747 747132 1384882 NM R 2 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 R2 DOOR AFT UPPER CORNER OF FRAME IS CRACKED. REPAIRED FRAME PER SRM 52-10-02 FIG 10. 2 L 7 4 4F A20WE 1998021100245 19980211 00245 NM 1998 2 11 P5CA9800127 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1657 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1657 TO 1660, RBL 95. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100246 19980211 00246 NM 1998 2 11 P5CA9800128 1 19980121 A 5280 CHANNEL BOEING 747 747132 1384882 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LT BLG O/B STRUT DOOR CRACKED UNDER FWD STOP FITTING. CRACKED CHANNEL REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100247 19980211 00247 NM 1998 2 11 P5CA9800129 1 19980121 A 5720 ANGLE BOEING 747 747132 1384882 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RT WING T/E ACCESS PANEL 672 EB INBOARD SUPPORT FRAME AFT MOUNTING ANGLE CRACKED. SUPPORT ANGLE REPAIRED PER SRM 51-10- 01. 2 L 7 4 4F A20WE 1998021100248 19980211 00248 NM 1998 2 11 P5CA9800130 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1780 TO 1800, LBL 75. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100249 19980211 00249 NM 1998 2 11 P5CA9800131 1 19980121 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1620 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FUSELAGE BS 1620 BL 50 TO 57 RIGHT BODY FAIRING SUPPORT FRAME CRACKED. FRAME REPAIRED PER SRM 53-50-04 FIG 2. 2 L 7 4 4F A20WE 1998021100250 19980211 00250 NM 1998 2 11 P5CA9800132 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1800 TO 1810, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100251 19980211 00251 NM 1998 2 11 P5CA9800133 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1820 TO 1840, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100252 19980211 00252 NM 1998 2 11 P5CA9800134 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1860 TO 1880, LBL 96. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100253 19980211 00253 NM 1998 2 11 P5CA9800135 1 19980121 A 5754 WEB BOEING 747 747132 1384882 NM NR 16 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 16 L/E FLAP O/B WEB UPPER RADIUS CRACKED. STOP DRILLED AND REPAIRED PER SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 1998021100254 19980211 00254 NM 1998 2 11 P5CA9800136 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1875 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1875 TO 1880, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100255 19980211 00255 NM 1998 2 11 P5CA9800137 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK CROWN FLANGE AT BS 1760 TO 1880, LBL 76. REMOVED CORROSION AND TREATED PER BAC SRM 51-1 0-01. 2 L 7 4 4F A20WE 1998021100256 19980211 00256 NM 1998 2 11 P5CA9800138 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1900 TO 1920, LBL 33. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100257 19980211 00257 NM 1998 2 11 P5CA9800139 1 19980121 A 5210 SKIN BOEING 747 747132 1384882 NM L1 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 L1 DOOR LOWER HINGE CUTOUT CRACKED ADJACENT TO SEAL RETAINER. REPAIRED PER SRM 53-10-02 FIG 12. 2 L 7 4 4F A20WE 1998021100258 19980211 00258 NM 1998 2 11 P5CA9800140 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1885 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1885, RBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100259 19980211 00259 NM 1998 2 11 P5CA9800141 1 19980121 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 FUSELAGE LEFT BS 960 LBL 10 RBL10 FUSE FDW BODY FAIRING SUPPORT FRAME FOUND CRACKED AND CORRODED. REPAIRED FRAME PER SR M 53-50-04 FIG 2. 2 L 7 4 4F A20WE 1998021100260 19980211 00260 NM 1998 2 11 P5CA9800142 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK AT BS 1920 TO 2040, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100261 19980211 00261 NM 1998 2 11 P5CA9800143 1 19980121 A 5510 SPLICE BOEING 747 747132 1384882 NM HORIZ STAB CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION FOUND ON LWR AFT SPLICE PLATES LT AND RT HOLE SPLICE PLATE. FOUND 2 EA LOOSE BOLTS. AFTER REMOVAL OF BOLTS FOUND CRACK IN SPLICE PLATE. REMOVED AND TREATED CORROSION DRILLED OVERSIZED BORE ON HOLE WITH CRACK, NDT, SHOT PEENED AND REINSTALLED FASTENERS SRM 51-10-01 BOEING TELEX PAO HKG 98-0058RE. 2 L 7 4 4F A20WE 1998021100262 19980211 00262 NM 1998 2 11 P5CA9800144 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2250 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 2250 TO 2260, LBL 11. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100263 19980211 00263 NM 1998 2 11 P5CA9800145 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 480, RBL 43. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100264 19980211 00264 NM 1998 2 11 P5CA9800146 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON SEAT TRACK AT BS 560 TO 580, RBL 8. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100265 19980211 00265 NM 1998 2 11 P5CA9800147 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2099 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SEAT TRACK BROKEN AT BS 2099, LBL 66. REPLACED SEAT TRACK PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100266 19980211 00266 NM 1998 2 11 P5CA9800148 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 5601 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SEAT TRACK CRACKED AT BS 560, LBL 11. REPLACED SEAT TRACK PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100267 19980211 00267 NM 1998 2 11 P5CA9800149 1 19980121 A 5754 BRACKET BOEING 747 747132 1384882 NM NR 15 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 15 L/E FLAP BULLNOSE ATTACH ARM BRACKET MOST I/B IS CRACKED. REPLACED ARM BRACKET PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100268 19980211 00268 NM 1998 2 11 P5CA9800150 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 700 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SEAT TRACK CRACKED AT BS 700, LBL 29. REPAIRED SEAT TRACK PER BAC SRM 53-10-05. 2 L 7 4 4F A20WE 1998021100269 19980211 00269 NM 1998 2 11 P5CA9800151 1 19980121 A 5320 STIFFENER BOEING 747 747132 1384882 NM RT MLG WW CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RT BLG WHEEL WELL AFT BULKHEAD BS 1480 BULKHEAD STIFFENER ADJACENT TO OLEO STRUT STOWAGE FAIRING IS CRACKED. ALSO, WEB UNDER STIFFENER IS CRACKED. REPLACED STIFFENER AND REPAIRED WEB PER SRM 51-10-01 AND 51-40-02. 2 L 7 4 4F A20WE 1998021100270 19980211 00270 NM 1998 2 11 P5CA9800152 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 5131 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SEAT TRACK CRACKED AT BS 513 TO 516, LBL 11. REPLACED SEAT TRACK PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100271 19980211 00271 NM 1998 2 11 P5CA9800153 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 517 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 SEAT TRACK FLANGE CRACKED AT BS 517 TO 523, LBL 33. REPLACED SEAT TRACK PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100272 19980211 00272 NM 1998 2 11 P5CA9800154 1 19980121 A 5210 RETAINER BOEING 747 747132 1384882 NM L1 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 R1 DOOR LOWER HINGE CUTOUT AREA ADJACENT TO PRES SEAL RETAINER IS CRACKED. REPAIRED PER SRM 51-10-02 FIG 12. 2 L 7 4 4F A20WE 1998021100273 19980211 00273 NM 1998 2 11 P5CA9800155 1 19980121 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1575 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 STRINGER 16R END CRACKED AT BS 1575. REPAIRED STRINGER PER BAC SRM 53-10-03. 2 L 7 4 4F A20WE 1998021100274 19980211 00274 NM 1998 2 11 P5CA9800156 1 19980121 A 2510 LADDER BOEING 747 747132 1384882 NM COCKPIT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 MAIN DECK TO UPPER DECK CREW LADDER BOTTOM STEP CRACKED BOTH SIDES, NR 3 STEP CRACKED RT SIDE, NR 4 STEP CRACKED LT SIDE . REPAIRED LADDER STEPS PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1998021100275 19980211 00275 NM 1998 2 11 P5CA9800157 1 19980121 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 2184 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 STRINGER 14L END CRACKED AT BS 2184. REPLACED STRINGER PER BAC SRM 51-40-01. 2 L 7 4 4F A20WE 1998021100276 19980211 00276 NM 1998 2 11 P5CA9800158 1 19980121 A 5400 CHANNEL BOEING 747 747132 1384882 NM NR 3 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 3 PYLON THROTTLE PUSH PULL CABLE ATTACH CHANNEL ADJACENT TO ANTI-ICE DUCT IS CRACKED. REPAIRED PER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 1998021100277 19980211 00277 NM 1998 2 11 P5CA9800159 1 19980121 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1617 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON STRINGER 22L AT BS 1617. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-02. 2 L 7 4 4F A20WE 1998021100278 19980211 00278 NM 1998 2 11 P5CA9800160 1 19980121 A 5313 LONGERON BOEING 747 747132 1384882 NM BS 1582 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON LONGERON AT LEFT BS 1583. REMOVED CORROSION AND TREATED PER BAC SRM 53-10-01. 2 L 7 4 4F A20WE 1998021100279 19980211 00279 NM 1998 2 11 P5CA9800161 1 19980121 A 5320 STIFFENER BOEING 747 747132 1384882 NM BS 42 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 UPPER DECK FLOORBEAM STIFFENER CRACKED AT RBS 440, RBL 42. REPAIRED STIFFENER PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100280 19980211 00280 NM 1998 2 11 P5CA9800162 1 19980121 A 5720 STIFFENER BOEING 747 747132 1384882 NM WS 669.5 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT WING STRINGER 22 WINT STA 669.5 VERTICAL STIFFENER CRACKED AT UPPER NR 1 FASTENER HOLE. REPLACED STIFFENER PER SR M 51-10-01. 2 L 7 4 4F A20WE 1998021100281 19980211 00281 NE 1998 2 11 P5CA9800163 2 19980121 A 7250 RAIL BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACK A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 663026 NR 3 ENG TEC S-RAIL AT 1:30 POSITION HAS A RACE TRACK SLOT O/D CRACK. WELDED AND RELIEVED PER PWA MM 72-53-01 NR 22. 2 L 7 4 4F 4 F A20WE E20EA 1998021100282 19980211 00282 NM 1998 2 11 P5CA9800164 1 19980121 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 1780 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON MAIN DECK FLOORBEAM UPPER CHORD SURFACE AT BS 1780, LBL 10 TO RBL 10. REMOVED CORROSION AND TREATE D PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100284 19980211 00284 NE 1998 2 11 P5CA9800166 2 19980121 A 7250 RAIL BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 663026 NR 3 ENG TEC S-RAIL AT 11:45 POSITION HAS A CLEVIS PIN HOLE CRACK. REMOVED ENG MOUNT, WELDED AND RELIEVED AND REINSTALL ED MOUNT PER PWA MM 72-53-01 NR 22. 2 L 7 4 4F 4 F A20WE E20EA 1998021100285 19980211 00285 NM 1998 2 11 P5CA9800167 1 19980121 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON MAIN DECK FLOORBEAM TOP CHORD AT BS 1580, RBL 8 TO RBL 11. REMOVED CORROSION AND TREATED PER BAC S RM 51-10-01. 2 L 7 4 4F A20WE 1998021100286 19980211 00286 NE 1998 2 11 P5CA9800168 2 19980121 A 7250 RAIL BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 663026 NR 3 ENG TEC R-RAIL AT 10 O'CLOCK POSITION HAS CRACKED RADIAL LIGHTING HOLE. WELDED AND STRESS RELIEVED PER PWA MM 72-5 3-01 NR 22. 2 L 7 4 4F 4 F A20WE E20EA 1998021100287 19980211 00287 NM 1998 2 11 P5CA9800169 1 19980121 A 5320 TIE CLIP BOEING 747 747132 1384882 NM BS 1335 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED STRINGER 15R TIE CLIP AT BS 1335. REPLACED STRINGER TIE CLIP PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100288 19980211 00288 NM 1998 2 11 P5CA9800170 1 19980121 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1920 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED SIDEWALL FRAME AT BS 1920, S 13R. REPAIRED FRAME PER BAC SRM 53-10-04. 2 L 7 4 4F A20WE 1998021100289 19980211 00289 NM 1998 2 11 P5CA9800171 1 19980121 A 5414 SKIN BOEING 747 747132 1384882 NM NR 4 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 4 PYLON HAS DEEP CHAFE MARKS AT UPPER EXTERNAL SKIN CROWN AREA. REPAIRED PER REPAIR SCOPE (HAECO) BLENDED O/B DEEP N DT NO CRACKS, INSTALLED REPAIR PER RS 54-51-33635. 2 L 7 4 4F A20WE 1998021100290 19980211 00290 NM 1998 2 11 P5CA9800172 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON LT WING LOWER SURFACE SKIN 70 INCHES AFT OF FRONT SPAR BEHIND NR 1 PYLON. REMOVED HI-LOKS BLENDED SHOT PEENED AND TREATED AND INSTALLED HI-LOKS PER SRM 51-10-02 AND 51-10-01 AND OHM 20-10-03. 2 L 7 4 4F A20WE 1998021100291 19980211 00291 NM 1998 2 11 P5CA9800173 1 19980121 A 5320 TIE BRACKET BOEING 747 747132 1384882 NM BS 2220 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED STRINGER 21R FRAME TIE BRACKET AT BS 2220. REPLACED BRACKET PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100292 19980211 00292 NM 1998 2 11 P5CA9800174 1 19980121 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 920 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED TENSION TIE AT BS 920, S 8 AND 9. REPAIRED TENSION PER SB 747 53-2371. 2 L 7 4 4F A20WE 1998021100293 19980211 00293 NM 1998 2 11 P5CA9800175 1 19980121 A 5753 WEB BOEING 747 747132 1384882 NM NR 16 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 16 L/E FLAP O/B WEB UPPER RADIUS IS CRACKED. STOP DRILLED AND REPAIRED O/B SUPPORT PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998021100294 19980211 00294 NM 1998 2 11 P5CA9800176 1 19980121 A 5320 WEB BOEING 747 747132 1384882 NM MAIN DECK CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 MAIN DECK RT O/B FLOOR SUPPROT HORIZONTAL WEB FOUND CRACKED. REPAIRED PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1998021100295 19980211 00295 NM 1998 2 11 P5CA9800177 1 19980121 A 5320 FRAME BOEING 747 747132 1384882 NM BS 2674 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 APU COMPT LEFT BS 2674 WL 310 FRAME CRACKED AND DAMAGED. STOP DRILLED AND REPAIRED AREA CRACKED PER SRM 51-10-01 AND 51 -40-03 FIG 2. 2 L 7 4 4F A20WE 1998021100296 19980211 00296 NM 1998 2 11 P5CA9800178 1 19980121 A 5320 TIE BOEING 747 747132 1384882 NM BS 1080 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED FRAME TIE AT BS 1080, S 3R TO 4R. REPLACED FRAME TIE PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100297 19980211 00297 NM 1998 2 11 P5CA9800179 1 19980121 A 5320 BRACKET BOEING 747 747132 1384882 NM BS 2674 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 APU COMPT BS 2674 LEFT WL 310 INTER FRAME SUPPORT BRACKET CRACKED. REPLACED BRACKET PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100298 19980211 00298 NM 1998 2 11 P5CA9800180 1 19980121 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1582 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CORROSION ON FLOOR SUPPORT ANGLE AT BS 1582, RBL 116. REPLACED SUPPORT ANGLE PER BAC SRM 51-40-04. 2 L 7 4 4F A20WE 1998021100299 19980211 00299 NM 1998 2 11 P5CA9800181 1 19980121 A 5330 SKIN BOEING 747 747132 1384882 NM BS 720-740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON FUSELAGE SKIN AT BS 720 TO 740, STR 0. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100300 19980211 00300 NM 1998 2 11 P5CA9800182 1 19980121 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2685 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 APU COMPARTMENT BS 2685 RIGHT WL 306 FRAME CRACKED. STOP DRILLED AND REPAIRED PER SRM 51-10-01 AND 51-40-03 FIG 2. 2 L 7 4 4F A20WE 1998021100301 19980211 00301 NM 1998 2 11 P5CA9800183 1 19980121 A 5720 BRACE BOEING 747 747132 1384882 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT WING L/E RIB TO FRONT SPAR LWR CHORD TUBE BRACE FWD END CRACKED. REPLACED BRACE PER MM 20-51-01. 2 L 7 4 4F A20WE 1998021100302 19980211 00302 NM 1998 2 11 P5CA9800184 1 19980121 A 5510 ATTACH PLATES BOEING 747 747132 1384882 NM RT HORIZ STAB CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED INTERNAL ATTACH PLATES AND FRAMES (12) AT PANEL 341BR ON RIGHT HORIZONTAL STABILIZER. REPAIRED PARTS PER BAC SR M 55-10-06. 2 L 7 4 4F A20WE 1998021100303 19980211 00303 NE 1998 2 11 P5CA9800185 2 19980121 A 7250 RAIL BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 662570 NR 4 ENG TEC R-RAIL AT 11 O'CLOCK POSITION PREVIOUS WELD AT LIGHTING HOLE SLOT INNER RADIUS CRACKED. WELDED AND NORMALI ZED PER PWA MM 72-53-01 NR 22. 2 L 7 4 4F 4 F A20WE E20EA 1998021100304 19980211 00304 NM 1998 2 11 P5CA9800186 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON RT WING UPPER SURFACE BETWEEN MID AND REAR SPARS WS 550, 915, 1215, 1470. BLENDED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100305 19980211 00305 NM 1998 2 11 P5CA9800187 1 19980121 A 5511 FRAME BOEING 747 747132 1384882 NM RT HORIZ STAB CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED INTERNAL FRAMES (2) AT PANEL 341BR ON RIGHT HORIZONTAL STABILIZER. REPAIRED FRAMES PER BAC SRM 55-10-06. 2 L 7 4 4F A20WE 1998021100306 19980211 00306 NM 1998 2 11 P5CA9800188 1 19980121 A 5511 FRAME BOEING 747 747132 1384882 NM LT HORIZ STAB CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED INTERNAL FRAMES AND ATTACH PLATES (6) AT PANEL 341CL ON LEFT HORIZONTAL STABILIZER. REPAIRED FRAMES AND PLATES PER BAC SRM 55-10-06. 2 L 7 4 4F A20WE 1998021100307 19980211 00307 NM 1998 2 11 P5CA9800189 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM WS 540-830 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION RIGHT WING UPPER SURFACE BETWEEN FRONT AND MID SPARS STR 14 TO 30 WING STA 540 TO 830. BLENDED AND TR EATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100308 19980211 00308 NM 1998 2 11 P5CA9800190 1 19980121 A 5522 SKIN BOEING 747 747132 1384882 NM LT INBD ELEV CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACK ON AFT INBOARD CORNER OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR ACCOMPLISHED PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1998021100309 19980211 00309 NM 1998 2 11 P5CA9800191 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON LT WING UPPER SURFACE ALONG FRONT SPAR SKIN AT FASTENER HEADS. BLENDED AND TREATED PER SRM 51-10-0 1. 2 L 7 4 4F A20WE 1998021100310 19980211 00310 NM 1998 2 11 P5CA9800192 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM WS 1525-1545 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION RT UPPER WING SURFACE BETWEEN FRONT AND REAR SPAR STRINGER 1 TO 25 WING STA 1525 1545. BLENDED AND TR EATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100311 19980211 00311 NM 1998 2 11 P5CA9800193 1 19980121 A 5320 FORGING BOEING 747 747132 1384882 NM BS 1560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON LEFT MAIN DECK WINDOW FRAME FORGING FORWARD EDGE AT BS 1560. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100312 19980211 00312 NM 1998 2 11 P5CA9800194 1 19980121 A 5320 FORGING BOEING 747 747132 1384882 NM BS 1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON LEFT MAIN DECK WINDOW FRAME FORGING FORWARD EDGE AT BS 1620. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100313 19980211 00313 NM 1998 2 11 P5CA9800195 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION ON RIGHT WING UPPER SURFACE FORWARD OF INBOARD AILERON. REMOVED CORROSION AND TREATED PER BAC SRM 51- 10-02 AND BAC OHM 20-10-03. 2 L 7 4 4F A20WE 1998021100314 19980211 00314 NM 1998 2 11 P5CA9800196 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED AND CHAFED RIGHT WING LOWER LEADING EDGE SKIN. REPAIRED PER BAC SRM 57-30-04. 2 L 7 4 4F A20WE 1998021100315 19980211 00315 NM 1998 2 11 P5CA9800197 1 19980121 A 5751 WEB BOEING 747 747132 1384882 NM INBD AILERON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 CRACKED INBOARD AILERON OUTBOARD WEB. REPAIRED PER BAC SRM 51-40-02. 2 L 7 4 4F A20WE 1998021100317 19980211 00317 NM 1998 2 11 B4MR98013 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 680-740 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND FS 680 TO FS 740 RBL 25 SEAT TRACK HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 53-10-5 FIG 1. CORROSION TASK CARD NUMBER C53-224-03. NON-ROUTINE TASK CARD NUMBER 11978. 2 L 7 3 4F RT A3WE 1998021100318 19980211 00318 NM 1998 2 11 B4MR98014 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 1112 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND FS 1112 RBL 24 SEAT TRACK HAS CORROSION. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBE R C53-224-03. NON-ROUTINE TASK CARD NUMBER 11974. 2 L 7 3 4F RT A3WE 1998021100319 19980211 00319 NM 1998 2 11 B4MR98015 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 1130-1170 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND FROM FS 1130 TO FS 1070 RBL 44 SEAT TRACK HAS CORROSION. REMOVED CORROSION FS 113 0 THRU 1170 RBL 44 IAW SRM 51-10-6 OUT OF LIMITS IAW SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 53-10-5 FIG 7. CORROSIO N TASK CARD NUMBER C53-224-03. NON-ROUTINE TASK CARD NUMBER 11976. 2 L 7 3 4F RT A3WE 1998021100320 19980211 00320 NM 1998 2 11 B4MR98016 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 950.5-1110 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND FS 950.5 TO 1110 LBL 24 SEAT TRACK HAS AREA OF CORROSION AND WORN. REMOVED COR ROSION IAW B727 SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 53-10-5. C- CHECK WORK CARD NUMBER 40090. NON-ROUTINE TASK CARD NUMBER 14942. 2 L 7 3 4F RT A3WE 1998021100321 19980211 00321 NM 1998 2 11 B4MR98017 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 950-1050 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND FS 950F TO 1050 LBL 44 SEAT TRACK HAS AREA OF CORROSION AND WORN. REMOVED WORN AREAS IAW B727 SRM 51-10-1. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 53-10-5. C -CHECK WORK CARD NUMBER 40090. NON-ROUTINE TASK CARD NUMBER 14943. 2 L 7 3 4F RT A3WE 1998021100322 19980211 00322 NM 1998 2 11 B4MR98018 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 1070-1110 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND FS 1070 TO FS 1110 SEAT TRACK HAS CORROSION AND WORN SPOTS. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS. INSTALLED REPAIR IAW B727 SRM 53-10-5. C-CHECK WORK CARD NUMBER 40090. NON-ROUTINE TAS K CARD NUMBER 14938. 2 L 7 3 4F RT A3WE 1998021100323 19980211 00323 NM 1998 2 11 B4MR98019 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 950-990 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND FS 950B TO 990 RBL 24 SEAT TRACK HAS AREA OF CORROSION AND WORN. REMOVED CORRO SION AND WORN AREAS IAW B727 SRM 51-10-1. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SR M 53-10-5. C-CHECK WORK CARD NUMBER 40090. NON-ROUTINE TASK CARD NUMBER 14941. 2 L 7 3 4F RT A3WE 1998021100324 19980211 00324 NM 1998 2 11 B4MR98020 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 328-360 DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND SEAT TRACK BETWEEN FS 328 AND 360 RBL 18 HAS DRILL HOLE. REMOVED DAMAGED SEAT TRACK IAW SRM 53-10-5. INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-5. C-CHECK WORK CARD NUMBER 40090. NON-ROUTINE TAS K CARD NUMBER 14936. 2 L 7 3 4F RT A3WE 1998021100325 19980211 00325 NM 1998 2 11 B4MR98021 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 950-1030 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND SEAT TRACK BETWEEN FS 950A AND 1030 RBL 44 HAS SEVERAL AREAS CORROSION AND WORN . REMOVED CORROSION AND WORN AREAS IAW B727 SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REP AIR IAW B727 SRM 53-10-5. C-CHECK WORK CARD NUMBER 40090. NON-ROUTINE TASK CARD NUMBER 14937. 2 L 7 3 4F RT A3WE 1998021100326 19980211 00326 NM 1998 2 11 B4MR98022 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 720 WORN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND SEAT TRACK WORN BETWEEN FS 720A AND 720B LBL 44. SEAT TRACK WORN BEYOND LIMITS IAW B727 SRM 53-10-1. INSTALLED NEW SEAT TRACK IAW SRM 53-10-5. C-CHECK WORK CARD NUMBER 40090. NON-ROUTINE TASK CAR D NUMBER 14933. 2 L 7 3 4F RT A3WE 1998021100327 19980211 00327 NM 1998 2 11 B4MR98023 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 880-900 WORN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND SEAT TRACK WORN BETWEEN FS 880 TO 900 LBL 24. REMOVED WORN AREAS IAW B727 SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 53-10-5. C-CHECK WORK CARD NUMB ER 40090. NON-ROUTINE TASK CARD NUMBER 14934. 2 L 7 3 4F RT A3WE 1998021100328 19980211 00328 NM 1998 2 11 B4MR98024 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 480-690 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND CORROSION STA 480 TO STA 690 RBL 24 SEAT TRACK. REMOVED CORROSION IAW B727 SRM 51-10-1. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED SEAT TRACK IAW B727 SRM 53-10-5. C-CHECK WORK CAR D NUMBER 40090. NON-ROUTINE TASK CARD NUMBER 14910. 2 L 7 3 4F RT A3WE 1998021100329 19980211 00329 NM 1998 2 11 B4MR98025 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 783-795 WORN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND SEAT TRACK WORN BETWEEN FS 783 TO 795 RBL 24. REMOVED CORROSION, CORROSION REM OVAL BEYOND LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 53-10-5 FIG 2. C-CHECK WORK CARD NUMBER 40090. NON-ROUTINE TASK CARD NUMBER 14932. 2 L 7 3 4F RT A3WE 1998021100330 19980211 00330 NM 1998 2 11 B4MR98026 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 1130 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND FS 1130 LBL 44 SEAT TRACK HAS CORROSION. REMOVED SEAT TRACK IAW B727 SRM 51-10-6, OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED SEAT TRACK IAW B727 SRM 51-30-2. CORROSION TASK CARD NUMBER C53-224-03. NON-ROUTINE TASK CARD NUMBER 14808. 2 L 7 3 4F RT A3WE 1998021100331 19980211 00331 NM 1998 2 11 B4MR98027 1 19980201 A 5347 SEAT TRACK BOEING 727 727243 138408D NM BS 480-660 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE C-CHECK INSPECTION, FOUND CORROSION BETWEEN STA 480 TO 660 RBL 44 SEAT TRACK. REMOVED CORROSION IAW B727 SRM 51-10-1, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED DAMAGED SEAT TRACK AT STA 480 TO 520 AND STA 580 TO 660 IAW B727 SRM 53-10-5. INSTALLED IAW B727 SRM 51-30-2. C-CHECK WORK CARD NUMBER 40090. NON-ROUTINE TASK CARD NU MBER 14909. 2 L 7 3 4F RT A3WE 1998021100332 19980211 00332 WP 1998 2 11 CKSA98005 1 19980131 A 2130 PNEU CONTL SYST DOUG DC8 DC8F54 3021926 WP FWD FUSELAGE MALFUNCTIONED A CKSA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 8052U 46009 AFTER TAKEOFF, TURNED ON NR 1 NASI SYSTEM HEAVY SMOKE IN THE COCKPIT. TURNED SYSTEM OFF SMOKE CLEARED RETURNED TO MIAMI . FOUND NASI SYSTEM TO BE AT FAULT. TRANSFERRED TO DMI CONTROL NR 867031 PER AIA DC8 MEL 21-65-1-C PLACARD INSTALLED. OPS CHECKED NR 1 AND NR 2 NASI SYSTEM IAW NASI MM AT PART POWER AND REDUCED POWER, IN HIGH AND LOW BLEEDS NO SMOKE EVID ENT IN COCKPIT, NO OTHER DEFECTS NOTED. THIS CLEARS DMI 867031 PLACARDS REMOVED. MONITORED FOR 3 DAYS/7 FLIGHTS WITH N O REOCCURRENCE. 2 L 7 4 4F 4A25 1998021100333 19980211 00333 WP 1998 2 11 CKSA98006 1 19980130 A 2130 PRESSURIZATION DOUG DC8 DC863F 302198F WP CABIN MALFUNCTIONED A CKSA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 23 811CK 46147 A/C CANNOT HOLD FL350 WITH THREE TC'S ON, CABIN WILL CLIMB PAST 10,000 FT HAD TO DESCENT TO FL310. OPS CK ON GRND NORMA L MM 21-31-0, ADVISE CREW COMMENTS. AIRCRAFT DUE GROUND PRESSURIZATION CHECK. PRESSURIZED AIRCRAFT ON GROUND. PRESSUR IZATION WAS WITHIN LIMITS ON GROUND. OPS CHECK GOOD IAW DC8 MM 21-31-0. 2 L 7 4 4F 4A25 1998021100334 19980211 00334 EU 1998 2 11 MALA975947 1 19980204 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, OVERHEAD 2A EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998021100335 19980211 00335 EU 1998 2 11 MALA975948 1 19980204 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING INSPECTION, 3 OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998021100336 19980211 00336 EU 1998 2 11 MALA975949 1 19980202 A 2710 7227151621 CENTERING MECH SAAB SF340 SF340A 7850100 EU LT AILERON MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 46XJ 046 WHILE IN FLIGHT, THE AILERONS WOULD BIND UP AND RELEASE WHEN TURNED TO THE LEFT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT AILERON CENTERING MECHANISM ASSEMBLY. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998021100337 19980211 00337 NM 1998 2 11 MALA975950 1 19980203 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 830MA 337 DURING INSPECTION, ONE RIGHT FLOOR TRACK EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998021100338 19980211 00338 NM 1998 2 11 MALA975951 1 19980203 A 3230 UPLOCK ACT DHAV DHC8 DHC8102 2809003 NM RT MLG LACK OF LUBE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 866MA 366 DEPARTING CRW, ON GEAR RETRACTION, RIGHT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED. AIRCRAFT PROCEEDED TO DTW AS AN ALTERN ATE. MAINTENANCE PERFORMED OPS CHECK, COULD NOT DUPLICATE. CLEANED AND LUBED UPLOCK ACTUATOR AND ROLLER. ALL CHECKS G OOD. 2 H 7 2 4T RT A13NM 1998021100339 19980211 00339 EU 1998 2 11 MALA975952 1 19980202 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 112XJ 340A112 DURING INSPECTION, SEAT 9A EMERGENCY OVERHEAD LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998021100340 19980211 00340 EU 1998 2 11 MALA975953 1 19980203 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 341-359 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 403XJ 340B403 DURING 4K CHECK, FOUND DENTS AND SEVERE OIL CANNING BETWEEN STATIONS 341 AND 359 FROM WL 100 TO WL 88. THESE DENTS ARE ON THE RIGHT SIDE OF THE AIRCRAFT. MAINTENANCE REPAIRED THIS AREA WITH A DOUBLER/TRIPLER OVERLAP REPAIR AND BONDED TO T HE FUSELAGE SKIN. COMPLETED WITH ACCORDANCE TO SAAB SRM 57-70-10. 2 L 7 2 4T RT A52EU 1998021100341 19980211 00341 1998 2 11 SRAA98A0202 3 19980203 A 6110 PROPELLER LKHEED 382 382E 526413U SO NR 1 ENGINE LEAKING A SRAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 901SJ 4299 DURING CLIMB-OUT FROM MHZ FLIGHT 507, NR 1 ENGINE RPM WENT TO 104 PERCENT NO CHANGE IN MECHANICAL GOVERNING, NR 1 PROP P ITCH LOCKED, FEATHERED NR 1 PROP AND FOUND PROP FAILED TO COMPLETELY FEATHERED, MAINTAINED 50 PERCENT RPM SHUT DOWN NR 1 ENGINE ACCOMPLISHED AIR TURN BACK TO MHZ. FOUND NR 1 PROP BLADE BOOT SEALS LEAKING. REPLACED NR 1 PROP ASSEMBLY IAW S AT J/C 6101, 6101-1, 6102, 6103. PERFORMED ENGINE RUN UP IAW J/C 7101 AND 7101-2. ALL OPS CHECKED GOOD. 2 H 7 4 4T A1SO 1998021100342 19980211 00342 SO 1998 2 11 RAAA98E9004 1 19980205 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD RT AND AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISC HARGED. 2 L 7 4 4T 4A22 1998021100343 19980211 00343 SO 1998 2 11 RAAA98E9005 1 19980205 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 13 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998021100344 19980211 00344 SO 1998 2 11 RAAA98E9006 1 19980205 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT LT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT DUE FAILED. 2 L 7 4 4T 4A22 1998021100345 19980211 00345 WP 1998 2 11 CALA9800189 1 19980205 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP LANDING GEAR ICED UP A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 16892 49391 THE LANDING GEAR HANDLE WOULD NOT GO DOWN UPON GEAR EXTENSION ON APPROACH TO DEN. THE GEAR WAS EXTENDED USING THE EMERG ENCY GEAR EXTENSION HANDLE. THE REGULAR GEAR HANDLE WAS THEN ABLE TO BE MOVED TO THE DOWN POSITION WITH THREE GREEN LIG HTS DISPLAYED. THE AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION OF THE GEAR FOUND ALL THREE GEAR HAD ICE BUILD UP. AL L THREE GEAR WERE DE-ICED AT THE GATE AREA. A NOSE GEAR SWING WAS PERFORMED SEVERAL TIMES. GEAR HANDLE OPERATION WAS S MOOTH UP AND DOWN AND ALL GEAR LIGHT INDICATIONS WERE NORMAL. 2 L 7 2 4F A6WE 1998021100346 19980211 00346 NM 1998 2 11 CALA9800190 1 19980204 A 5313 STRINGER BOEING 727 727243 138408D NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND STRINGER 27R CORRODED IN AFT CARGO COMPARTMENT BETWEEN STA 720 AND 720A. THE CORRODED SECTION OF STRIN GER AND SKIN WERE REMOVED. A STRINGER REPAIR, REPAIR SPLICES, AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3 , FIGURE 1, 53-30-3, FIGURE 3, 51-10-2, 53-10-3, FIGURE 1, AND MM 51-21-2. 2 L 7 3 4F RT A3WE 1998021100347 19980211 00347 NM 1998 2 11 CALA9800191 1 19980204 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 303.9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND CABIN FLOOR SUPPORT WEB CRACKED .125 BEYOND STOP DRILL HOLE AT STA 303.9, LBL 45. THE FLOOR SUPPORT WE B WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-1. 2 L 7 3 4F RT A3WE 1998021100348 19980211 00348 WP 1998 2 11 CALA9800192 1 19980205 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP BS 475 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND CORROSION AT LOWER LT CORNER OF DOOR IN AVIONICS COMPT AT REAR PRESSURE BULKHEAD STA 475, LT HORIZONTAL AND VERTICAL BEHIND GUSSET PLATE. THE AREA WAS REPAIRED IAW SRM 53-12-01. 2 L 7 3 4F A22WE 1998021100349 19980211 00349 WP 1998 2 11 CALA9800193 1 19980205 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 450 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14062 47863 INSPECTION FOUND CORROSION IN FRAME AND INTERCOSTALS IN AVIONICS BAY AT STA 450 BETWEEN STRINGER 44 AND 64L. THE AREA W AS REPAIRED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1998021100350 19980211 00350 WP 1998 2 11 CALA9800194 1 19980205 A 5320 BEAM DOUG DC9 DC981 3022081 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND MID BAGGAGE BIN DOOR JAMB BEAM CORRODED. THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998021100351 19980211 00351 WP 1998 2 11 CALA9800195 1 19980205 A 5341 FITTING DOUG DC9 DC932 3022066 WP BS 605 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 47798 INSPECTION FOUND A .75 INCH CRACK IN RT WING TO FUSELAGE DAGGER FITTING AT STA 605, LONGERON 22-23R. AN ATTACH ANGLE RE PAIR WAS INSTALLED IAW ECRA 5341-01002. 2 L 7 2 4F A6WE 1998021100352 19980211 00352 WP 1998 2 11 9802259936 1 19980205 A 5610 WINDSHIELD DOUG DC9 DC931 3022065 WP LT COCKPIT CRACKED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 1799U 47370 ON LEVEL OFF AT FL330, FOUND A CRACK IN THE FIRST OFFICER'S WINDSHIELD, ACCOMPLISHED COM PROCEDURE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WINDSHIELD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998021100353 19980211 00353 WP 1998 2 11 9802269925 1 19980204 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND AFT LEFT LAVATORY EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021100354 19980211 00354 WP 1998 2 11 9802279989 1 19980204 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1998021100355 19980211 00355 NE 1998 2 11 WWMA9800022 2 19980131 A 7230 6068T45P03 REAR SHAFT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COMPRESSOR SHEARED A A WWMA O OTHER Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 WP 15 335AE 8471 340B335 ENG WAS INSTALLED AND MX WAS PERFORMING ENG BREAK IN RUNS IAW SAAB AMM 71-00-00 PAGES 516-518. THE POWER LEVER WAS ADVA NCED FROM 46 PERCENT TO 68 PERCENT TQ WHEN TEMP STARTED TO INCREASE FASTER THAN NORMAL. WHEN THE POWER LEVER WAS RETARDE D, TWO AUDIABLE POPS WERE HEARD WITH CORRESPONDING OVER TEMP LIGHTS. A BOROSCOPE INSPECTION REVEALED EXCESSIVE RUB AT S TAGE 4-5 OF THE COMPRESSOR ROTOR. THE COMPRESSOR IMPELLOR HAD ALSO CUT INTO IT'S SHROUD. THE COMPRESSOR WAS RUBBING WHE N THE ENG WAS TURNED BY HAND BUT THE COMPRESSOR SECTION WAS NOT TURNING WITH THE HOT SECTION. FOUND THAT THE COMPRESSOR ROTOR REAR SHAFT HAD FAILED. THE ENG WAS SENT TO GE FOR EVALUATION. 2 L 7 2 4T 4 T RT A52EU E8NE 1998021100356 19980211 00356 EU 1998 2 11 WWMA9800021 1 19980204 A 2612 703072 SENSING ELEMENT SAAB SF340 340B 7860101 EU LT ENGINE INOPERATIVE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 232AE 340B232 FLIGHT 5004, AEX, THE LEFT ENGINE FIRE PROTECTION SYSTEM WOULD NOT TEST CORRECTLY. MAINTENANCE REPLACED THE LEFT ENGIN E SENSING ELEMENT. 2 L 7 2 4T RT A52EU 1998021100357 19980211 00357 EU 1998 2 11 WWMA9800020 1 19980201 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 306AE 340B306 EMERGENCY LIGHT AT SEAT 4A FOUND INOPERATIVE DURING TEST, REPLACED BULB. 2 L 7 2 4T RT A52EU 1998021100358 19980211 00358 WP 1998 2 11 ABXA9800054 1 19980204 A 5320 4915402 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 965 SPLIT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND FITTING ON FLOOR SUPPORT AT STA 965 AND RBL 22, BELOW AFT INBOARD EDGE OF PYLON BULKHEAD SPLIT. R EPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998021100359 19980211 00359 WP 1998 2 11 ABXA9800055 1 19980203 A 5755 3923255501 FITTING DOUG DOUG DC9 DC931 3022065 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND THE LEFT WING INBD SPOILER TORSION BAR CENTER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 S RM 51-30-22. 2 L 7 2 4F A6WE 1998021100360 19980211 00360 WP 1998 2 11 ABXA9800056 1 19980203 A 5321 99100787 FLOOR DOUG DOUG DC9 DC931 3022065 WP BS 200-207-218 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND SUB-FLOOR CRACKED, STA 207 AT RBL 22, STA 200 AT RBL 4, AND STA 218 AT LBL 3 AND 9. REPAIRED CRAC KED SUB-FLOOR IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998021100361 19980211 00361 WP 1998 2 11 ABXA9800057 1 19980204 A 5320 49113832N FITTING DOUG DOUG DC9 DC931 3022065 WP BS 237 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND THE RIGHT FRAME FOOT AT STA 237 CORRODED. REPLACED FRAME FOOT IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998021100362 19980211 00362 WP 1998 2 11 ABXA9800058 1 19980204 A 5320 49113832N FITTING DOUG DOUG DC9 DC931 3022065 WP BS 256 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND THE RIGHT FRAME FOOT AT STA 256 CORRODED. REPLACED FRAME FOOT IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998021100363 19980211 00363 WP 1998 2 11 ABXA9800059 1 19980204 A 5730 591216147 PANEL DOUG DOUG DC9 DC941 302207N WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE LEFT WING UPPER INBOARD TRAILING EDGE PANEL HONEYCOMB STRUCTURE CORRODED. REPLACED TRAILI NG EDGE PANEL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998021100364 19980211 00364 WP 1998 2 11 ABXA9800060 1 19980204 A 5330 591142229 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK COMPLIANCE WITH AD 96-10-11 AND S/B DC9-53A147, FOUND CRACKS IN EXTERIOR SKIN AT FS 996 BETWEEN LONGERONS 2L-3L, 3L-4L, 4L-5L AND 5L-6L. REPAIRED CRACKS IAW ABX EA 53-11005-104. 2 L 7 2 4F A6WE 1998021100365 19980211 00365 WP 1998 2 11 ABXA9800061 1 19980204 A 5330 591142231 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK COMPLIANCE WITH AD 96-10-11 AND S/B 53A147, FOUND CRACKS IN EXTERIOR SKIN AT FS 996 BETWEEN LONGERONS 3R- 4R. REPAIRED CRACKS IAW ABX EA 53-11005-104. 2 L 7 2 4F A6WE 1998021100366 19980211 00366 NM 1998 2 11 DLM88980301 1 19980204 A 2170 10NPB122502AD COALESCER BAG DOUG MD88 MD88 3023688 NM LT/RT DIRTY A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 912DL 49543 ON FINAL AT APPROX 4000 FT GOT A BURNING SMELL IN COCKPIT AND THE CABIN. BOTH AFT LAV SMOKE ALARMS SOUNDED. ORDER CLEA RED AND SMOKE ALARMS STOPPED JUST AFTER LANDING. INSPECTION A/C FOR FLUID LEAKS. FOUND RESIDUAL DE-ICE FLUID. REPLACE D BOTH A/C WATER SEPARATOR BAGS AND PERFORMED DUCT BURNOUT. ODOR DISSIPATED. RUNUP NORMAL. 2 L 7 2 4F RT A6WE 1998021100367 19980211 00367 NM 1998 2 11 DL72L980303 1 19980204 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 FOUND ON F1 LETTER CK 2.5 INCH CRACK ON, THE RT ELEVATOR LOWER SKIN AT THE FWD INBD END. REPAIRED PER MM 55-20-3. 2 L 7 3 4F A3WE 1998021100368 19980211 00368 NM 1998 2 11 DL72L980304 1 19980204 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 1 INCH VISIBLE CRACK SPAR STIFFENER AT NR 3 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21 P 813. 2 L 7 3 4F A3WE 1998021100369 19980211 00369 NM 1998 2 11 DL72L980305 1 19980204 A 5720 DOUBLER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 REPAIR DOUBLER CRACKED NR 1 L/E FLAP ACT MOUNT BOX I/B SIDE. REPAIRED PER MM 57-20-21 P 811. 2 L 7 3 4F A3WE 1998021100370 19980211 00370 NM 1998 2 11 DL72L980306 1 19980204 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 FOUND AT F1 LETTER CHECK, .5 INCH CRACK AT NR 7 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998021100371 19980211 00371 NM 1998 2 11 DL72L980307 1 19980204 A 5754 RIB BOEING 727 727232 1384082 NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 FOUND AT F1 LETTER CK, 1.25 INCH CRACK AT NR 6 SLAT I/B ACTUATOR ATTACH RIB. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998021100372 19980211 00372 NM 1998 2 11 DL72L980308 1 19980204 A 5720 ANGLE BOEING 727 727232 1384082 NM NR 6 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 FOUND AT F1 LETTER CK, .5 INCH CRACK AT NR 6 SLAT COVE SKIN ANGLE AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998021100373 19980211 00373 NM 1998 2 11 DL72K980314 1 19980121 A 2782 ACTUATOR MOUNT BOEING 727 727232 1384082 NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 AT MV2, FOUND CRACK NR 2 FLAP O/B MOUNT CORRODED. FABRICATED REP AIR DOUBLER PER MM 57-20-21 FIG 807. INSTALLED REPAIR ED ACTUATOR MOUNT ON A/C. 2 L 7 3 4F A3WE 1998021100374 19980211 00374 NM 1998 2 11 DL72K980315 1 19980122 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 AT MV2, FOUND STRINGER CRACKED FIN ATA 110.4 STR 10 LT STRINGER IS CRACKED INSIDE VERT STAB. FABRICATED REPAIR DOUBLER PER MM 55-30-00 FIG 803. 2 L 7 3 4F A3WE 1998021100375 19980211 00375 NM 1998 2 11 DL72K980316 1 19980127 A 5400 LIP BOEING 727 727232 1384082 NM NR 2 PYLON GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 AT MV2, FOUND DEEP GOUGE IN NR 2 PYLON LIP 5 O'CLOCK POSITION. FABRICATED REPAIR DOUBLER/FILLER PER MM 53-11-00 PG 801. 2 L 7 3 4F A3WE 1998021100376 19980211 00376 NM 1998 2 11 DL72S980317 1 19980205 A 2150 214001048 CONTROLLER B70402 BOEING 727 727232 1384082 NM LT/RT PACK MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 499DA 044C2288 21143 AT FL 2500 WITH ONE PACK RUNNING, CABIN STARTED TO CLIMB, DIVERTED INTO DFW. MAINTENANCE IN PROGRESS. RT PACK ON PREVI OUS MCO. RT PACK REPLACED ACM. CKS GOOD. LT PACK REPLACED 35 DEGREE SENSOR AND 35 DEGREE CONTROLLER. PRESSURIZE D A/C USING BOTH PACKS, CKS GOOD. 2 L 7 3 4F A3WE 1998021100377 19980211 00377 NM 1998 2 11 DL72S980319 1 19980203 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 .75 INCH CRACK ON FLOORBEAM STA 344 AT LBL 30 AT FLOOR PANEL FASTENER HOLE. DRILLED UP REPLACEMENT SECTION PER SRM 53-1 0-8. 2 L 7 3 4F A3WE 1998021100378 19980211 00378 NM 1998 2 11 DHL98717001 1 19980205 A 5230 MACHANISM BOEING 727 72723 1384004 NM CARGO DOOR LACK OF LUBE A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 717DH 19389 AFTER DEP, CARGO DOOR 'UNLOCKED' LIGHT ILLUMINATED, LOST PRESSURIZATION. LIGHT WENT OUT, REGAINED PRESSURIZATION. LIGH T ILLUMINATED AGAIN AND LOST PRESSURIZATION. LIGHT WENT OUT, PRESSURIZATION NEVER RETURNED TO NORMAL. INSPECTED CARGO DOOR, CYCLED DOOR SEVERAL TIMES, LUBED LOCKS AND ROLLERS. COULD NOT DUPLICATE PROBLEM. 2 L 7 3 4F A3WE 1998021100379 19980211 00379 NM 1998 2 11 DHL98707001 1 19980204 A 5312 BULKHEAD BOEING 727 72722 1384002 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 FOUND SUSPECTED CRACK AT AFT AIRSTAIR DOOR JAMB (1183 BULKHEAD) RIGHT SIDE AT 2ND STOP FROM THE TOP. CRACKED CONFIRME D, STOP DRILLED CRACK, EDDY CURRENT STOP DRILL, INSTALLED DOUBLER REPAIR PER 98PMSI189D-1B ENGINEERING DRAWING. 2 L 7 3 4F A3WE 1998021100380 19980211 00380 NM 1998 2 11 P5CA9800198 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, RT WING UPPER SURFACE ALONG MIDSPAR AREA ON SKIN. BLENDED AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100381 19980211 00381 NM 1998 2 11 P5CA9800199 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, RT WING UPPER SURFACE ALONG FRONT SPAR. BLENDED AND TREATED PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100382 19980211 00382 NM 1998 2 11 P5CA9800200 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, ON LT WING UPPER SURFACE BETWEEN FRONT AND MIDSPAR. BLENDED AND TREATED PER BAC 51-10-01. 2 L 7 4 4F A20WE 1998021100383 19980211 00383 NM 1998 2 11 P5CA9800201 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, ON LT WING UPPER SURFACE AFT OF FRONT SPAR. BLENDED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100384 19980211 00384 NM 1998 2 11 P5CA9800202 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, LT WING UPPER SURFACE ALONG FRONT SPAR SPOTS OF CORROSION AROUND FASTENER HEADS ALONG FRONT SPAR. BL ENDED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100385 19980211 00385 NM 1998 2 11 P5CA9800203 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, LT WING UPPER SURFACE AT REAR SPAR. BLENDED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100386 19980211 00386 NM 1998 2 11 P5CA9800204 1 19980121 A 5320 FORGING BOEING 747 747132 1384882 NM BS 1600-1620 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND ON WINDOW FORGING FWD EDGE BS 1600-1620. BLENDED AND TREATED PER BOEING TELEX PAO-HKG-98-0042R E 23/01/98. 2 L 7 4 4F A20WE 1998021100387 19980211 00387 NM 1998 2 11 P5CA9800205 1 19980121 A 5320 FORGING BOEING 747 747132 1384882 NM WINDOW BS 1580 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND ON WINDOW FORGING FWD EDGE BS 1580-1600. BLENDED AND TREATED PER BOEING TELEX PAO-HKG-98-0042R E 23/1/98. 2 L 7 4 4F A20WE 1998021100388 19980211 00388 NM 1998 2 11 P5CA9800206 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND ON RT WING UPPER SURFACE REAR SPAR AREA. BLENDED AND SHOT PEENED AND TREATED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100389 19980211 00389 NM 1998 2 11 P5CA9800207 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND LT WING LOWER SKIN 62 INCHES AFT OF FRONT SPAR. BLENDED AND TREATED PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1998021100390 19980211 00390 NM 1998 2 11 P5CA9800208 1 19980121 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND LOWER SKIN 38 INCHES AFT OF FRONT SPAR STRINGER 10. BLENDED AND TREATED PER BOEING SRM 57-30-0 1. 2 L 7 4 4F A20WE 1998021100391 19980211 00391 NM 1998 2 11 P5CA9800209 1 19980121 A 5343 TRUNNION BOEING 747 747132 1384882 NM RT MLG CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND ON RT I/B BODY GEAR TRUNNION AND TRUNNION CAP. TRUNNION BORE MACHINED NDT OK AND BUSHING CUT P ER BOEING SRM 53-10-08 ITEM 1-24. 2 L 7 4 4F A20WE 1998021100392 19980211 00392 NM 1998 2 11 P5CA9800210 1 19980121 A 5343 TRUNNION BOEING 747 747132 1384882 NM LT MLG CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND LT I/B BODY GEAR TRUNNION AND TRUNNION CAP. TRUNNION BORE MACHINED NDT OK BUSHING CUT TRUNNION CAP. REPLACED PER BOEING SRM 53-10-08 ITEM 1-24. 2 L 7 4 4F A20WE 1998021100393 19980211 00393 NM 1998 2 11 P5CA9800211 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1920-2040 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 2 CORROSION, ON MAIN DECK SEAT TRACK FLANGE BS 1920-2040. REPLACED TRACK PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998021100394 19980211 00394 NM 1998 2 11 P5CA9800212 1 19980121 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM MAIN DECK CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEVEL 1 CORROSION, FOUND ON MAIN DECK SEAT TRACK AT BS 1900 BL 11. BLENDED AND TREATED PER BOEING SRM 53-10-01. 2 L 7 4 4F A20WE 1998021100395 19980211 00395 WP 1998 2 11 RRXA98013 1 19980203 A 3610 56194331 CHECK VALVE DOUG DC8 DC863 302198A WP LEFT MALFUNCTIONED A RRXA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 15 950R 45903 A/C DEPRESSURIZED AT 33,000 DESCEND TO 17,000 TO HOLD 12,000 FT CABIN. NR 1 T/C INOP. INSTALLED SERVICEABLE WARM AIR C K VALVE ON LT PNEU MANIFOLD. SECURED LOOSE DUCTING, A/C PRESSURIZATION AND LEAK CK GOOD, NR 1 T/C GRD CKS GOOD. 2 L 7 4 4F 4A25 1998021100396 19980211 00396 NM 1998 2 11 K3HA980011 1 19980207 A 3350 3071BPEGPL BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 EMERGENCY PATH LIGHT AT SEAT 3ABC INOP. RELAMPED EMERGENCY PATH LIGHT AT SEAT 3ABC, OPS CHECK OK. 2 L 7 3 4F A3WE 1998021100397 19980211 00397 NM 1998 2 11 K3HA980012 1 19980209 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN OUT OF POSITION A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 EMERGENCY TRACK LIGHTING OFF TRACK ON FIRST ROW. TRIM OUT MOLDING AND INSTALLED LENS. REPOSITION WIRING AND INSTALL TR ACK. 2 L 7 3 4F A3WE 1998021100398 19980211 00398 GL 1998 2 11 SRAA98B0107 2 19980110 A 7200 ENGINE LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 4 DAMAGED A SRAA F ACTIVATE FIRE EXT. Y ENGINE STOPPAGE LD LANDING 1 GL 23 909SJ 4763 ON LANDING AT MYU FLIGHT 1902, AIRCRAFT LANDED ON ICY SURFACE AND DEPARTED FROM RUNWAY. AIRCRAFT SUSTAINED NR 4 ENGINE AND PROP DAMAGE. DUE TO CONTACT WITH SNOW BANK NR 4 ENGINE FIRE, EXTINGUISHED WITH NR 1 BOTTLE. AIRCRAFT HAS BEEN REMO VED FROM SNOW BANK AND EVALUATED FOR POST INCIDENT DAMAGE. INSPECTED NR 4 ENGINE STRUCTURES BY NDT PER J/C 5192 AND 519 2-3 NO DEFECTS FOUND. REPLACED NR 4 ENGINE ASS'Y AND PROP, ALSO INSPECTED THE NR 3 ENGINE AND FOUND NR 3 PROP NICKED. R EPLACED NR 3 PROP ASSEMBLY PER SAT J/C 6101, 6102, 6103. PERFORMED ENGINE RUN UP, OPS CHECKED GOOD. 2 H 7 4 4T 4 T A1SO E282 1998021100399 19980211 00399 SO 1998 2 11 RAAA98E8003 1 19980206 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998021100400 19980211 00400 SO 1998 2 11 RAAA98E8004 1 19980206 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FWD RT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT. 2 L 7 4 4T 4A22 1998021100401 19980211 00401 NM 1998 2 11 UPS98425714 1 19980206 A 3350 90084 LIGHT BOEING 747 747123F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 CREW UPPER DECK SLIDE DOOR EMERGENCY FWD LIGHT WILL NOT ILLUMINATE (DOOR SILL FRAME). REPLACED CARTRIDGE ASSY. 2 L 7 4 4F A20WE 1998021100402 19980211 00402 NM 1998 2 11 UPS98425715 1 19980202 A 5511 REAR SPAR BOEING 747 747121 1384871 NM RT STABILIZER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE:C, RT STABILIZER REAR SPAR LWR CHORD CORRODED AT STA 473-476. SECTION SPLICED AT LWR CHORD IAW 55-10-05 . 2 L 7 4 4F A20WE 1998021100403 19980211 00403 EU 1998 2 11 QXEA9800060 1 19980205 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 PDX - EXIT SIGN OVER COCKPIT DOOR INOP. REPLACED SIGN, OP'S CHECK GOOD. 2 L 7 2 4F RT A20EU 1998021100404 19980211 00404 WP 1998 2 11 ABXA9800062 1 19980207 A 3350 60030451 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 947AX 582 47004 EMERGENCY LIGHTS ILLUMINATED WITH POWER OFF AND LIGHT SWITCH IN THE OFF POSITION. REPLACED EMERGENCY LIGHT BATTERY PACK . 2 L 7 2 4F A6WE 1998021100405 19980211 00405 WP 1998 2 11 ABXA9800063 1 19980205 A 3230 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG LACK OF LUBE A ABXA K NONE J WARNING INDICATION LD LANDING 1 GL 23 909AX 47148 WHEN GEAR SELECTED DOWN, MAIN GEAR CAME DOWN AND LOCKED. GEAR DOORS CYCLED NORMALLY. NOSE GEAR WOULD NOT COME DOWN, NO NOSE GEAR INDICATION AT ALL. RECYCLED GEAR, SAME RESULT. COMPLIED WITH ABNORMAL PROCEDURES, FREE FELL NOSE LANDING GE AR. GEAR CAME DOWN AND LOCKED. MAIN LANDING GEAR CYCLED NORMALLY. LUBRICATED NOSE LANDING GEAR MECHANISM AND PERFORMED GEAR SWING WITH AND WITHOUT GEAR DOORS HOOKED UP. NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1998021100406 19980211 00406 WP 1998 2 11 ABXA9800064 1 19980205 A 3230 4641188 HOOK DOUG DC8 DC863 302198A WP NLG OUT OF ADJUST A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 813AX 46136 NOSE GEAR FAILED UPLATCH CHECK. RECYCLED GEAR SEVERAL TIMES AND PERFORMED ALTERNATE UPLATCH CHECK WITH SAME RESULTS. A DJUSTED NOSE UPLATCH MECHANISM IAW DC8 MM 32-31-0. PERFORMED GEAR SWING AND UPLATCH CHECK. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998021100407 19980211 00407 WP 1998 2 11 DHL98807001 1 19980204 A 5230 DOOR DOUG DC8 DC873F 302199F WP BS 310 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 A PIT DOOR, STA 310 LOWER MIDDLE SECTION FOUND EXTERNAL PATCH ON DOOR PULLED LOOSE WITH TWO CRACKS AND SECTION OF PATCH MISSING. REMOVED DAMAGED SKIN AREA 4.25 BY 3.25. INSTALLED FLUSH PATCH WITH BACKING DOUBLER PER DACO SRM 52-2-0. 2 L 7 4 4F RT 4A25 1998021100408 19980211 00408 1998 2 11 SWIA971073 4 19980108 A 3452 6226523001 TRANSPONDER EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NR 1 FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 190SW 120050 DEPARTING SAN, LOCAL APPROACH REPORTED THAT THE 3RD DIGIT ON NR 1 TRANSPONDER WAS SHOWING A DIFFERENT NUMBER THAN WAS AS SIGNED. TRIED NR 2 TRANSPONDER AND IT WAS TOTALLY INOPERABLE. WAS TOLD BY DISPATCH TO DIVERT TO LAX. INSTALLED NEW CO NTROL HEAD CTRL 92 AT NR 1 TRANSPONDER. PERFORMED TRANSPONDER TEST SEQUENCE WITH TEST BOX AND PITOT STATIC CHECK FOR AL TITUDE READ OUT. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100409 19980211 00409 SO 1998 2 11 SWIA971074 1 19980106 A 2910 HYD LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE BLUE HYD SYST FAILED A SWIA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 204SW 120243 TOTAL LOSS OF BLUE HYDRAULIC SYSTEM FLUID. QUANTITY WENT TO ZERO AND PRESSURE INDICATOR WENT TO ZERO WITH ASSORTED LIGH TS. UNABLE TO EXTEND FLAPS. REPAIRED HYDRAULIC LINE ON FLUID RESERVOIR 4TH LINE. REPLACED RIGHT ENGINE HYDRAULIC PUMP AND ALSO REPLACED RIGHT HYDRAULIC PACK HIGH PRESSURE SWITCH. RAN ENGINE HYDRAULIC SYSTEM AND OPS CHECKS GOOD WITH NO LEAKS. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100410 19980211 00410 NE 1998 2 11 SWIA971075 2 19980108 A 7261 OIL SYST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE REQD SERVICE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 186SW 120034 MOMENTARY LOW OIL PRESSURE INDICATION ON LEFT ENGINE ON CLIMB-OUT. RETURNED TO TWF. SERVICED OIL TO THE ADD 1 QUART MA RK ON SIGHT GLASS. CHECKED ENGINE FOR OIL LEAKS BUT NONE WERE NOTED. GROUND RUN CHECKS GOOD WITH NO LEAKS. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100411 19980211 00411 SO 1998 2 11 SWIA971076 1 19980129 A 3010 SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT STABILIZER FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 232SW 120306 RIGHT INBOARD STABILIZER BOOT FAILS. RETURNED TO FIELD. REPLACED PRESSURE SWITCH FOR RIGHT INBOARD STABILIZER. OPS CH ECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100412 19980211 00412 SO 1998 2 11 SWIA971077 1 19980111 A 2750 12042642507 SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 197SW 120186 AT 400 FT CALLED FOR FLAPS UP AND GOT FLAP ASYMMETRY INDICATION. RETURNED TO LAX. INSTALLED SERVICEABLE FLAP HANDLE AS SEMBLY. CYCLED FLAPS EXTENSIVELY WITH NO ASYMMETRY NOTED. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100413 19980211 00413 SO 1998 2 11 SWIA971078 1 19980129 A 2752 3082001007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RE FLAPS FAILED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 197SW 120186 SELECTING FLAPS DOWN, NACELLES WOULD NOT EXTEND CAUSING DISAGREEMENT. WHEN FLAPS ARE RETRACTED THE INBOARDS LAG. CYCLE D FLAPS SEVERAL TIMES ON GROUND AND UNABLE TO DUPLICATE. OHMED WIRE FROM CONTROL BOX TO ANNUNCIATOR, CHECKS GOOD. OHME D WIRING FROM CONTROL BOX TO ACTUATORS AND FOUND MEGA OHM READINGS ON ALL PINS FROM LEFT NACELLE ACTUATOR TO GROUND. DI SCONNECTED PLUG AT ACTUATOR, READINGS CHECKS GOOD. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100414 19980211 00414 SO 1998 2 11 SWIA971079 1 19980111 A 3230 UPLOCK HOOK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 217SW 120286 RIGHT MAIN GEAR ABNORMAL INDICATION UPON RETRACTION. THE RED A,B SYSTEM LIGHT WOULD NOT EXTINGUISH WITH GEAR HANDLE IN THE UP POSITION. RETURNED TO SLC. ADJUSTED LEFT AND RIGHT MAIN UPLOCK HOOK IAW MM 32-32-09. CHECKED ADJUSTMENT OF GEA R INDICATION IAW MM 32-61-01. CHECKED FREE FALL AND ELECTRIC OVERRIDE AND CYCLED GEAR 20 TIMES. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100415 19980211 00415 WP 1998 2 11 ARWA980204 2 19980205 A 7200 ENGINE DOUG DC8 DC862 3021970 WP GARRTT TPE331 TPE33111U 01514 WP NR 2 LEAKING A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 810BN 45905 NR 2 ENGINE NO OIL PRESSURE/OIL QUANTITY WENT DOWN TO 1.5 QUARTS. REMOVED AND REPLACED NR 2 ENGINE. PERFORMED ENGINE N R 2 CHANGE AS PER ARROW AIR PAPER WORK 8275 ENGINE S/N OFF 671003, ENGINE S/N ON 645654. 2 L 7 4 4F 4 T 4A25 E4WE 1998021100416 19980211 00416 NM 1998 2 11 VNAA9802004 1 19980205 A 4950 GTCP36150DD APU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AFT FUSELAGE SMOKING A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 458PS 45243 20486 3068 AFTER T/O, THE COCKPIT AND CABIN FILLED WITH SMOKE. CREW SHUT DOWN ENVIROMENTAL CONTROL SYSTEMS AND RECIRCULATION FANS. ALSO, APU WAS SHUT DOWN. THE SMOKE CLEARED FROM THE A/C. THE A/C RETURNED TO THE FIELD AND LANDED, W/O ANY FURTHER I NCIDENTS. MX INSPECTED AND DETERMINED DE-ICE FLUID WAS INGESTED INTO APU, AND CAUSED THE SMOKE. MX RAN THE ENVIROMENTA L SYSTEMS, IAW DORNIER MM 21-21-00 TO REMOVE ANY RESIDUAL SMELLS FROM THE SYSTEM, AND DEFERRED THE APU IAW THE DORNIER 3 28 MEL. A/C WAS RETURNED TO SERV. 06 FEB 98, THE APU WAS OP'S CHECKED IAW DORNIER MM 49-10-00 AND 21-21-00. THE DEFE RRAL WAS REMOVED, AND THE A/C WAS RETURNED TO SERV. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998021100417 19980211 00417 WP 1998 2 11 CKSA98009 1 19980205 A 3260 H206B SWITCH DOUG DC8 DC852 3021922 WP LT MLG DOOR MALFUNCTION A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 810CK 45814 LEFT GEAR UNSAFE LIGHT ON AT ALL TIMES UNTIL DOWN AND LOCKED. REPLACED LEFT GEAR DOOR SWITCH. SYSTEM OPS CHECKS NORMAL IAW MM CHAPTER 32-7. 2 L 7 4 4F 4A25 1998021100418 19980211 00418 EU 1998 2 11 MALA975954 1 19980205 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 429XJ 429 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT AT ROW 7 AND 8 INOP. MAINTENANCE DEFERRED PER MEL 33-53-2(C). ENTERED I NTO DMR AND MXC NOTIFIED. 2 L 7 2 4T RT A52EU 1998021100419 19980211 00419 EU 1998 2 11 MALA975955 1 19980206 A 2436 51539007A GCU SAAB SF340 SF340A 7850100 EU RT DC GEN FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 98XJ 098 RIGHT GENERATOR FAILED IN FLIGHT, AFTER RESETTING, IT FAILED AGAIN. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED RIG HT DC GCU, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998021100420 19980211 00420 EU 1998 2 11 MALA975956 1 19980206 A 2435 23080031 STARTER GEN SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 98XJ 098 RIGHT GENERATOR FAILED IN FLIGHT, AFTER RESETTING, FAILED AGAIN. AFTER 10 MINUTES THE RIGHT GENERATOR OVER TEMP CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE STARTER/GENERATOR, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998021100421 19980211 00421 NE 1998 2 11 MALA975957 2 19980204 A 7321 7086M60611 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE FAILED A MALA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 99XJ 099 AFTER LANDING ROLLOUT, RIGHT ENGINE FLAMED OUT. TOWER REPORTED SMOKE FROM RIGHT ENGINE, AT THE SAME TIME THE RIGHT ENGI NE OIL PRESSURE LIGHT ILLUMINATED. MAINTENANCE REPLACED THE RIGHT ECU, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998021100422 19980211 00422 EU 1998 2 11 MALA975958 1 19980206 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 99XJ 099 DURING INSPECTION, EMERGENCY LIGHT AT SEAT 6A INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998021100423 19980211 00423 NM 1998 2 11 MALA975959 1 19980208 A 3350 OL3071BPE BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 DURING INSPECTION, ONE RED FLOOR TRACK LIGHT AND ONE EXIT LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT A SEAT 1 D E (PN 10-1307-5) AND RELAMPED EXIT SIGN AT PASSENGER DOOR, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998021100424 19980211 00424 EU 1998 2 11 MALA975960 1 19980208 A 2613 HEAT SENSOR SAAB SF340 340B 7860101 EU RT ENGINE DIRTY A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 424XJ 424 PRIOR TO TAKEOFF, THE RIGHT TAILPIPE HOT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND C LEANED AFT HEAT SENSING UNIT OF RIGHT TAILPIPE, RUNS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998021100425 19980211 00425 EU 1998 2 11 MALA975961 1 19980119 A 5310 STRUCTURE SAAB SF340 340B 7860101 EU BS 670-694 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 416XJ 416 DURING INSPECTION, CREASE AT TAIL STAND ON BOTTOM AFT FUSELAGE. MAINTENANCE SPLICED STRINGER STA 678 TO 694 IAW SAAB 34 0 SRM 53-80-20. MAINTENANCE REPAIRED FRAME BY CUTTING OUT DAMAGE AND FABRICATED DOUBLER, INSTALLED IAW SAAB 340 SRM 53- 70-30. MAINTENANCE REMOVED DAMAGE SKIN, FABRICATED AND INSTALLED DOUBLER/TRIPLER IAW SAAB 340 SAAB 53-80-10. 2 L 7 2 4T RT A52EU 1998021100426 19980211 00426 EU 1998 2 11 MALA975962 1 19980114 A 5312 BULKHEAD SUPPORT SAAB SF340 SF340A 7850100 EU BS 272 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING HEAVY CHECK, FOUND BULKHEAD FLOOR SUPPORT FLANGES RIGHT STA 272.0 CORRODED. MAINTENANCE REPAIRED BY CUTTING THE FLANGE AWAY AND FABRICATING A 90 DEGREE REPAIR ANGLE IAW SRM 51-00-42/43 AND 51-20-50. 2 L 7 2 4T RT A52EU 1998021100427 19980211 00427 EU 1998 2 11 MALA975963 1 19980119 A 5330 SKIN SAAB SF340 SF340A 7850100 EU BS 602 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING HEAVY CHECK, STA 602 HAS 2 DENTS THAT ARE LOCATED APPROX 24 BELOW PASSENGER WINDOW. MAINTENANCE REMOVED DAMAGE A REA AND INSTALLED AN EXTERNAL REPAIR DOUBLER IAW SAAB SRM 53-70-10. 2 L 7 2 4T RT A52EU 1998021100428 19980211 00428 NM 1998 2 11 M8XA9800002 1 19980207 A 2760 INDICATION DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE SPOILER SYST MALFUNCTIONED A M8XA C D ABORTED TAKEOFF RETURN TO BLOCK P NO WARNING INDICATION TO TAKEOFF 1 NM 03 329MX 3049 CREW REPORTED THAT THEY RECEIVED NO VISUAL EICAS INDICATION THAT THE GROUND SPOILERS WERE ARMED AFTER THE CONDITION LEVE RS WERE ADVANCED TO THE TAKEOFF POSITION. CREW ELECTED TO ABORT TAKEOFF AND RETURN TO THE GATE. CONTRACT MAINTENANCE P ERFORMED GROUND SPOILER INHIBITION-FUNCTION TEST IAW DO328 MM 27-61-00, NO DEFECTS NOTED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998021100429 19980211 00429 WP 1998 2 11 9802281160 1 19980207 A 7830 TR UNIT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 160US 46769 686169 DURING LANDING ROLL AND WHILE COMING OUT OF REVERSE THRUST, THE NR 2 ENGINE THRUST REVERSER REMAINED DEPLOYED. THE CREW ATTEMPTED TO RECYCLE THE REVERSER AND A COMPRESSOR STALL OCCURRED. THE ENGINE WAS SHUT DOWN WITH A MAXIMUM EGT OF 800C . MAINTENANCE INSPECTED THE ENGINE INCLUDING A BORESCOPE WITH NO TROUBLE FOUND. THE RABS CHECK AND REVERSER OPERATION ALL CHECKED NORMAL. 2 L 7 3 4F 4 F A22WE E20EA 1998021100430 19980211 00430 NE 1998 2 11 9802296613 2 19980206 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 4 FLAMED OUT A NWAA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 01 613US 20358 689633 JUST BEFORE TOP OF DESCENT AT FL370, THE NR 4 ENGINE FLAMED OUT. THE ENGINE WAS RESTARTED NORMALLY AT FL310 AND PERFORM ED WITHOUT ANY PROBLEMS FOR THE REMAINEDER OF THE FLIGHT. MAINTENANCE VISUALLY INSPECTED THE ENGINE WITH NO DEFECTS NOT ED. THE ENGINE FUEL FILTER AND EVC FUEL FILTER WERE REPLACED AS A PRECAUTION. 2 L 7 4 4F 4 F A20WE E20EA 1998021100431 19980211 00431 WP 1998 2 11 9802309851 1 19980208 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY L IGHTS BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021100432 19980211 00432 WP 1998 2 11 9802319877 1 19980208 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN PINCHED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY LIGHTS LOCATED IN FIRST CLASS WERE FOUND TO BE INOPERATIVE. MAINTENANC E REPAIRED PINCHED WIRE IN ROW 3 FOOT REST, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021100433 19980211 00433 SO 1998 2 11 COMA9810037 1 19980208 A 3350 1317 LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 241CA 120211 OVERHEAD EMERGENCY LIGHT AT ROW 2B IS INOP. REPLACED THE LIGHT BULB. 2 L 7 2 4T RT A31SO 1998021100434 19980211 00434 SO 1998 2 11 COMA9810038 1 19980206 A 7712 SEDLOC2R TQ INDICATOR EMB 120 EMB120RT SO INST PANEL MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 162CA 120150 DURING TAKEOFF, THE RIGHT HAND TORQUE INDICATION WAS 195 PERCENT. REPLACED THE TORQUE INDICATOR. 2 L 7 2 4T RT A31SO 1998021100435 19980211 00435 SO 1998 2 11 COMA9810039 1 19980205 A 2731 ATG120TR SENSOR EMB 120 EMB120RT SO ELEV TRIM TAB MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 267CA 120259 TAKEOFF TRIM WARNING SOUNDED. REPLACED THE ELEVATOR TRIM TAB PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1998021100436 19980211 00436 SO 1998 2 11 COMA9810040 1 19980205 A 3397 W610001720 WIRE EMB 120 EMB120RT SO RT WING SHORTED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 156CA 120156 NAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED. REPAIRED SHORTED WIRE RIGHT HAND WING. 2 L 7 2 4T RT A31SO 1998021100437 19980211 00437 EA 1998 2 11 COMA9860037 1 19980205 A 2613 601R593201 OVERHEAT SENSORS CNDAIR CL600 CL6002B19 EA RT WING MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 981CA 7163 ANTI-ICE DUCT CAUTION MESSAGE ON EICAS. COULD NOT DUPLICATE DISCREPANCY. REPLACED ALL OF THE RIGHT HAND WING OVERHEAT SENSORS. 2 L 7 2 4F RT A21EA 1998021100438 19980211 00438 EA 1998 2 11 COMA9860038 1 19980207 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 981CA 7163 SMOKE TOILET CAUTION MESSAGE ON EICAS. REPLACED SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 1998021100439 19980211 00439 EA 1998 2 11 COMA9860039 1 19980207 A 5210 LATCH MECH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 916CA 7014 PASSENGER DOOR OUTER HANDLE WARNING DURING FLIGHT. ADJUSTED DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1998021100440 19980211 00440 NM 1998 2 11 UPS98225718 1 19980208 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, EMERGENCY LIGHT RECEIVER BATTERIES NEED REPLACEMENT. ACCOMPLISHED TASK CARD 2403, EMERGENCY LIGHT RECEIVER BATTERIES REMOVED AND REPLACED BATTERIES, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1998021100441 19980211 00441 NM 1998 2 11 UPS98425717 1 19980207 A 3350 S1356B37 BATTERY BOEING 747 747123F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-1A, EMERGENCY LIGHT INOP ENTRY DOOR AND THE CEILING MAIN DECK FWD OF STAIR AND AFT OF STAIR. REPLACED B OTH BATTERY/LIGHT ASSY. 2 L 7 4 4F A20WE 1998021100442 19980211 00442 NM 1998 2 11 UPS98425719 1 19980206 A 3350 LIGHT BOEING 747 747123F NM CREW DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A REF M 146611, FWD SLIDE LIGHT CREW DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATT PACK A T FWD SLIDE, OPS GOOD THIS CLEARS M 146611 PLACARD REMOVED. 2 L 7 4 4F A20WE 1998021100443 19980211 00443 NM 1998 2 11 UPS98425720 1 19980208 A 3350 S1356B37 BATTERY BOEING 747 747123F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP ENTRY DOOR AND THE CEILING MAIN DECK FWD OF STAIR AND AFT OF STAIR A370200 37 0204. REPLACED STA 600 BATTERY PACK (P/N S1356B37), (S/N 19553) ON, (S/N 1849 2359045) OFF, AFT OF STAIR REPLACED STA 6 00 BATTERY PACK (P/N 13J6B37) (S/N 25613) ON, (S/N 34035) OFF, BOTH CEILING AND ENTRY LIGHTS CHECKED OK. 2 L 7 4 4F A20WE 1998021100444 19980211 00444 WP 1998 2 11 UPS98825716 4 19980207 A 2565 5561004DC BOTTLE DOUG DC8 DC871F 302199D WP ESCAPE SLIDE LOW PRESSURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-A, FOUND ESCAPE SLIDE BOTTLE PRESSURE BELOW MINIMUMS, GUAGE READ 2300 PSI. REMOVED AND REPLACED ESCAPE SLIDE PER MM 25-60-01. 2 L 7 4 4F RT 4A25 1998021100445 19980211 00445 EU 1998 2 11 WWMA9800025 1 19980206 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 356SB 340B356 DURING PREFLIGHT, THE EMERGENCY FLOOR LIGHTS AT SEATS 6 AND 7 WERE FOUND TO BE INTERMITTANT. MAINTENANCE TIGHTNED LOOSE CONNECTOR AT THE POWER SUPPLY. 2 L 7 2 4T RT A52EU 1998021100446 19980211 00446 NE 1998 2 11 WWMA9800024 2 19980206 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT/RT MALFUNCTIONED A WWMA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 15 283AE 340B283 FLYING THROUGH SEVERE RAIN STORMS THE LEFT AND RIGHT ENGINES EXPERIENCED POWER INTERRUPTIONS, THEY OCCURED WITH AND WITH OUT THE ENGINE ANTI-ICE ON. A 10 PERCENT TO 20 PERCENT LOSS OF TORQUE WAS NOTED WITH YAW CHANGES AND AUDIBLE BANGS. AL SO, BOTH IGNITION LIGHTS CAME ON. THE AIRCRAFT LANDED IN LAX WITHOUT INCIDENT. MAINTENANCE PERFORMED ENGINE AND BORESC OPE INSPECTIONS ON BOTH THE LEFT AND RIGHT ENGINES IAW FAULT ISOLATION GUIDES IN THE GE MM 72-00-00 PAGES 139 TO 147. N O DISCREPANCIES WERE FOUND, THE FLIGHT DATA RECORDER AND THE FDAU WERE REMOVED FOR STATISTICAL DOWNLOADING. 2 L 7 2 4T 4 T RT A52EU E8NE 1998021100447 19980211 00447 EU 1998 2 11 WWMA9800023 1 19980208 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 280AE 340B280 OVERHEAD EMERGENCY LIGHTS AT 14A, 12C AND FLOOR EMERGENCY LIGHTS IN THE REAR OF THE AIRCRAFT FAIL TO ILLUMINATE DURING T EST. REPLACED EMERGENCY LIGHT POWER PACK 24LN. 2 L 7 2 4T RT A52EU 1998021100448 19980211 00448 NM 1998 2 11 QXEA9800061 1 19980206 A 7921 28E996 OIL COOLER P&WC DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE LEAKING A QXEA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 820PH 23432 63 FLIGHT WAS ORIGINALLY TO SUN VALLEY, BUT COULD NOT LAND DUE TO WEATHER. REROUTED TO TWIN FALLS. WHILE UNDERWAY, NR 1 O IL PRESSURE WENT TO 10 PSI, AS A PRECAUTIONARY THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN BOI. MAINTENANCE FOUND THE OIL COOLER LEAKING AND REMOVED AND REPLACED IT. AIRCRAFT WAS GROUND RUN, NO LEAKS NOTED. 2 H 7 2 4T RT A13NM 1998021100449 19980211 00449 NM 1998 2 11 98FDEA00090 1 19980210 A 2782 651781823 ACTUATOR BOEING 727 72725 1384006 NM NR 2 LE SLAT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 504FE 18274 NR 2 LED WOULD NOT RETRACT AFTER T/O. ACCOMPLISHED RED TABS. REMOVED AND REPLACED NR 2 SLAT ACT THRU STEP G AS PER M/M 27-81-32 PG 408.80531. COMPLETED INSTALLATION, CONNECTED ROD END AND INSTALLED PANELS, LEAK AND OPS CK OK. 2 L 7 3 4F A3WE 1998021100450 19980211 00450 WP 1998 2 11 MWEA98147 1 19980209 A 5522 SKIN DOUG DC9 DC932 3022066 WP RT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING INSPECTION, FOUND LIGHT CORROSION ON EXTERIOR SURFACE OF LOWER SKIN ON RIGHT ELEVATOR XE 157.9. MTC REPAIRED IAW SRM 55-03 FIG 14 SHEET 2 AND SRM 51-30. 2 L 7 2 4F A6WE 1998021100451 19980211 00451 WP 1998 2 11 MWEA98148 1 19980209 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP AFT PRES BLKHD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING INSPECTION, FOUND LIGHT CORROSION ON FWD SIDE OF APB LEFT SIDE FROM APPROXIMATELY LONG 26L TO 28L. MTC REPAIRED IAW SRM 53-03 FIG 9 SHEET 1 AND 51-30-5. 2 L 7 2 4F A6WE 1998021100452 19980211 00452 WP 1998 2 11 MWEA98149 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-240 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING INSPECTION, FOUND HEAVY CORROSION ON GALLEY SEAT TRACK NR 4 FROM STATION 200 TO 240. MTC REPAIRED IAW SRM 51-30- 2 AND SRM 53-05 FIG 4F. 2 L 7 2 4F A6WE 1998021100453 19980211 00453 WP 1998 2 11 MWEA98150 1 19980207 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 DURING INSPECTION, FOUND AFT NACELLE LT EMERGENCY LIGHT INOP. MTC REMOVED AND REPLACED AFT NACELLE LT EMERGENCY LIGHT B ATTERY PACK IAW DC9 MM 33-50. 2 L 7 2 4F A6WE 1998021100454 19980211 00454 WP 1998 2 11 MWEA98151 1 19980207 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP FWD GALLEY LACK OF LUBE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 209ME 47730 THE GALLEY SLIDE GIRT BAR IS DIFFICULT TO ARM AND DISARM. MTC CLEANED AND LUBED GIRT BAR LATCHES. 2 L 7 2 4F A6WE 1998021100455 19980211 00455 WP 1998 2 11 MWEA98152 1 19980208 A 5753 FAIRING DOUG DC9 DC932 3022066 WP RT TE FLAP VANE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 DURING INSPECTION, FOUND THE RT FLAP FIXED VANE FAIRING DAMAGED. MTC REPAIRED IAW SRM 51-30-2 AND 57-01 FIG 3 SHEET 2. 2 L 7 2 4F A6WE 1998021100456 19980211 00456 WP 1998 2 11 MWEA98153 1 19980207 A 5753 5910042506 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 DURING INSPECTION, FOUND PUNCTURE DAMAGE ON TOP SURFACE OF RT FLAP CENTER FIXED VANE AT STATION XRS 260. MTC REPAIRED I AW SRM 57-04 P25 AND SRM 51-70-2. 2 L 7 2 4F A6WE 1998021100457 19980211 00457 NM 1998 2 11 P5CA9800213 1 19980206 A 5512 SKIN BOEING 747 747238B 1384828 NM LT HORIZ STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 DURING AIRCRAFT SERVICING, DYNAIR HIGHLIFT FELL ONTO LEFT HAND STABILIZER. REPAIRED PER POLAR MA 5510-02:01. 2 L 7 4 4F A20WE 1998021100458 19980211 00458 NE 1998 2 11 P5CA9800214 2 19980208 A 7261 O-RING BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 OIL FILTER CUT A P5CA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 23 852FT 19757 662462 LOW OIL QUANTITY INFLIGHT DOWN TO 1.06 GALS. PRECAUTIONARY SHUT-DOWN. FOUND O-RING FOR MAIN OIL FILTER DAMAGED. REPLA CED O-RING RAN ENG AFTER OIL SERVICING, NO LEAKS FOUND. RESERVICED ENGINE AFTER RUN TO TOTAL OF 28 QTS PER MM REF 72-61 -05. 2 L 7 4 4F 4 F A20WE E20EA 1998021100459 19980211 00459 NM 1998 2 11 P5CA9800215 1 19980206 A 5753 PANEL BOEING 747 747122 1384872 NM LT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT INBD MIDFLAP COVE LIP PANEL AT OUTBOARD END CRACKED. STOP DRILLED CRACK/INSTALLED FIBERGLASS OVERLAYS PRIMED AND PAI NTED PER SRM 51-40-15 AND 51-24-11. 2 L 7 4 4F A20WE 1998021100460 19980211 00460 NM 1998 2 11 P5CA9800216 1 19980106 A 5753 PANEL BOEING 747 747122 1384872 NM LT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT INBD MIDFLAP COVE LIP PANEL AT OUTBD END CRACKED. STOP DRILLED CRACK/INSTALLED FIBERGLASS OVERLAYS PRIMED AND PAINTE D PER SRM 51-40-15 AND 51-24-11. 2 L 7 4 4F A20WE 1998021100461 19980211 00461 NM 1998 2 11 P5CA9800217 1 19980206 A 5532 PANEL BOEING 747 747122 1384872 NM VERT STAB DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 COMP PANEL NR 324L ON LT SIDE OF VERTICAL STAB HAS 3 AREAS OF DELAMINATION. FABRICATED NEW PANEL MATERIAL, CUT NEW CORE , HOT BONDED CORE TO MATERIAL, CURED, TRIMMED TO FIT, PRIMED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998021100462 19980211 00462 NM 1998 2 11 P5CA9800218 1 19980206 A 5751 SKIN BOEING 747 747122 1384872 NM RT AILERON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RT OUTBD AILERON UPPER SURFACE OUTBD HAS SPEED TAPE REPAIR. REMOVED DAMAGED FIBERGLASS SKIN, REPAIRED SAME USING OVERLA YS AND FILLERS. PRIMED AND PAINTED PER SRM 51-40-07 AND 51-24-11. 2 L 7 4 4F A20WE 1998021100463 19980211 00463 NM 1998 2 11 P5CA9800219 1 19980206 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DISBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RT WING UPPER SURFACE PANEL DISBONDED. REMOVED DAMAGED CHECKED FOR MOISTURE. DID FIBERGLASS OVERLAYS AND FILLERS PRIME D AND PAINTED PER SRM 51-40-07 AND 51-24-11. 2 L 7 4 4F A20WE 1998021100464 19980211 00464 NM 1998 2 11 P5CA9800220 1 19980206 A 5755 SKIN BOEING 747 747122 1384872 NM NR 10 SPOILER DISBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 SPOILER RT WING HAS LARGE DISBONDED REPAIR TO UPPER SURFACE. REMOVED AND REPLACED NR 10 SPOILER PANEL PER MM 27-61-02. 2 L 7 4 4F A20WE 1998021100465 19980211 00465 NM 1998 2 11 P5CA9800221 1 19980205 A 5755 PANEL BOEING 747 747122 1384872 NM NR 8 SPOILER CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 8 SPOILER RT HAS CORROSION A BOTH INBD AND OUTBD SEALS. REMOVED AND REPLACED NR 8 SPOILER PANEL PER MM 27-61-01. 2 L 7 4 4F A20WE 1998021100466 19980211 00466 NM 1998 2 11 P5CA9800222 1 19980206 A 5350 FAIRING BOEING 747 747122 1384872 NM LOWER BODY CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FUSELAGE LOWER BODY FAIRING PANEL HAS CORROSION. REMOVED CORROSION, APPLIED FILLER, APPLIED CONDUCTIVE COATING, PRIMED AND PAINTED PER SRM 51-10-01, 51-40-08, 51-24-17. 2 L 7 4 4F A20WE 1998021100467 19980211 00467 NM 1998 2 11 P5CA9800223 1 19980205 A 5755 PANEL BOEING 747 747122 1384872 NM NR 6 SPOILER DISBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 6 SPOILER LT WING LOWER SURFACE HAS DISBONDED AREA. CUTOUT DAMAGED AREA, REPLACED CORE, FABRICATED FILLER AND DOUBLE R BONDED, CURED, SEALED, PRIMED AND PAINTED PER SRM 51-40-06 AND 51-24-11. 2 L 7 4 4F A20WE 1998021100468 19980211 00468 NM 1998 2 11 P5CA9800224 1 19980205 A 5755 SPOILER BOEING 747 747122 1384872 NM NR 4 SPOILER DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 SPOILER LT WING LOWER SURFACE HAS DELAMINATION. REMOVED AND REPLACED NR 4 SPOILER PANEL PER MM 27-61-02. 2 L 7 4 4F A20WE 1998021100469 19980211 00469 NM 1998 2 11 P5CA9800225 1 19980205 A 5755 SPOILER BOEING 747 747122 1384872 NM NR 1 SPOILER DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 1 SPOILER LT WING LWR SURFACE HAS DELAMINATION. CUTOUT DAMAGED AREA AND REPAIRED PER SRM 57-50-00 AND 51-24-11 AND M M 27-61-02. 2 L 7 4 4F A20WE 1998021100470 19980211 00470 NM 1998 2 11 P5CA9800226 1 19980205 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DAMAGE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 RT WING GEAR FLYING PANEL AFT CORNER HAS DAMAGE. REMOVED DAMAGED AREA, APPLIED FIBERGLASS FILLERS AND OVERLAYS, APPLIED CONDUCTIVE COATING PER SRM 51-40-11 AND 51-24-11. 2 L 7 4 4F A20WE 1998021100471 19980211 00471 NM 1998 2 11 P5CA9800227 1 19980205 A 5753 SKIN BOEING 747 747122 1384872 NM LT LE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LT INBOARD FOREFLAP L/E OUTBD SIDE DELAMINATED. REPAIRED DELAMINATION PER SRM 51-40-11 AND 51-24-11. 2 L 7 4 4F A20WE 1998021100472 19980211 00472 NM 1998 2 11 P5CA9800228 1 19980205 A 7120 MOUNT BOLT BOEING 747 747122 1384872 NM NR 4 ENGINE LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 4 PYLON FWD MOUNT INBD BOLT WASHER ON HEAD SIDE LOOSE. REMOVED WEIGHT OF ENGINE FROM FWD MOUNT. RETORQUED LOOSE BOL D PER MM 71-21-01. 2 L 7 4 4F A20WE 1998021100473 19980211 00473 WP 1998 2 11 CKSA98010 1 19980204 A 3260 H146 SWITCH DOUG DC8 DC852 3021922 WP LT MLG DOOR MALFUNCTION A CKSA K NONE N FALSE WARNING CL CLIMB 1 GL 23 810CK 45814 LT GEAR UNSAFE LIGHT ON AT ALL TIMES WITH GEAR UP AND LOCKED. WHEN GEAR PLACED IN DOWN POSITION LIGHT WENT OUT WHEN IT SHOULD HAVE BEEN ON. OK WITH GEAR DOWN AND LOCKED WITH 3 GREENS. REMOVED AND REPLACED UP LIMIT SWITCH IAW DC8 MM 32-7- 2 PAGE 201 CODE 1. NO TEST REQUIRED PER PARA 3 (PAGE 201). 2 L 7 4 4F 4A25 1998021100474 19980211 00474 NE 1998 2 11 CKSA98011 2 19980204 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 3 FLAMED OUT A CKSA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 23 103CK 293C1212 14509 PER CREW REPORT, NR 3 ENGINE FLAMED OUT DURING FLIGHT THRU HAIL STORM. ALL MCD INSPECTION, INLET AND EXHAUST AREAS CHEC KED FOR DAMAGE. NO DAMAGE NOTED, ENGINE GROUND RUN PERFORMED, ALL PARAMETERS NORMAL IAW 71-00-00. 2 L 7 3 4F 4 F A23WE E12EU 1998021100475 19980211 00475 NE 1998 2 11 TC8A98008 2 19980206 A 7200 ENGINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 1 STALLED A TC8A D RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 GL 23 183SK 45904 669735 BEFORE T/O, PUSHING THE THROTTLES FOR STATIC T/O, NR 1 ENGINE STALLED. TAXIED BACK TO THE RAMP. FOUND TWO SMALL PIECES OF BUSHES IN THE INTAKE. REMOVED, CLEANED, VISUALLY INSPECTED AND RAN UP THE ENGINE AT T/O POWER, FOUND OK. 2 L 7 4 4F 4 F 4A25 1E8 1998021100476 19980211 00476 WP 1998 2 11 TC8A98009 1 19980207 A 4980 491349103 ACTUATOR DOUG DC8 DC862F 3021972 WP APU EXHAUST DR FAILED A TC8A A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION UK UNKNOWN 1 GL 23 183SK 16858 45904 UNABLE TO PRESSURIZE IN FLIGHT. DUMPED FUEL, RETURNED TO KMIA. INSPECTED A/C AND FOUND APU EXHAUST DOOR OPEN. REMOVED AND REPLACED DOOR ACTUATOR IAW 49-00-10. PERFORMED PRESSURIZATION CHECK, SYSTEM OPS CHECK OK 21-10-2. 2 L 7 4 4F 4A25 1998021100550 19980211 00550 1998 2 11 SIMA980101 4 19980110 A 3140 LA4E20606HM0100 MULTI FUNCT COMP AEROSP ATR72 ATR72212 EU NR 2 FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 536AT 2171 536 BMI - FLT 4374 - AIRCRAFT DIVERTED TO BMI AFTER SEVERAL INTERMITTENT MALFUNCTION INDICATIONS OCCURRED. THE EMERGENCY BA TTERY CHARGE FAULT GEAR PANEL LIGHTS CYCLING ALONG WITH NR 2 ENGINE MOMENTARY SURGE. REPLACED NR 2 MFC IAW ATR JIC 31-4 8-81. PERFORMED OPERATIONAL CHECK SATISFACTORILY. RETURNED AIRCRAFT TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998021100551 19980211 00551 EU 1998 2 11 SIMA980151 1 19980115 A 5347 7253711245 END CAP SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 340B384 ABI - DURING MBV, FOUND LT TRACK END CAP HAD CORROSION BEYOND LIMITS AT FS 297 FROM BLL 18.3 TO BLL 32.8. REMOVED AND R EPLACED LT TRACK END CAP IAW SAAB 340 SRM 53-00-00 AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998021100552 19980211 00552 EU 1998 2 11 SIMA980152 1 19980115 A 5347 7253711243 END CAP SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 384AE 340B384 ABI - DURING MBV, FOUND RT TRACK END CAP HAD CORROSION BEYOND LIMITS AT FS 297 FROM BL ZERO TO BLR 32.8. REMOVED AND RE PLACED RT TRACK END CA IAW SAAB 340 SRM 53-00-00 AND AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998021100556 19980211 00556 NM 1998 2 11 98ZZZX651 1 19980118 A 6300 8866 SENSOR DOUG MD900 MD900 3027375 NM M/R FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 106 106 90000012 VIBRATION SENSOR UNIT REPEATEDLY TRIGGERS BMS FAULT 4 ON CHANNEL 2. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021100557 19980211 00557 NM 1998 2 11 98ZZZX652 1 19980118 A 7160 900CF330001101 ACTUATOR DOUG MD900 MD900 3027375 NM INLET DOOR FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 106 42 90000012 INLET DOOR LINEAR ACTUATOR UNIT INOPERATIVE. WILL NOT ACTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021100558 19980211 00558 NM 1998 2 11 98ZZZX653 1 19980118 A 5320 900FF337012102 SUPPORT ASSY DOUG MD900 MD900 3027375 NM RT INLET CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 106 90000012 RT INLET SUPPORT ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021100559 19980211 00559 NM 1998 2 11 98ZZZX654 1 19980118 A 5320 900FF337012101 SUPPORT ASSY DOUG MD900 MD900 3027375 NM LT INLET CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 106 90000012 LT INLET SUPPORT ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021100560 19980211 00560 NM 1998 2 11 98ZZZX655 1 19980118 A 7920 900P3650000105 HOSE DOUG MD900 MD900 3027375 NM LT ENG OIL LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 1878 90000012 LT ENGINE OIL HOSE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021100561 19980211 00561 NM 1998 2 11 98ZZZX657 1 19980118 A 6310 900D1400528101 INPUT PINION DOUG MD900 MD900 3027375 NM M/R DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 593 0062190083 90000012 INPUT PINION ASSY LEAKING OIL BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021100572 19980211 00572 NM 1998 2 11 98ZZZX668 1 19980120 A 7920 900P3650000105 HOSE DOUG MD900 MD900 3027375 NM LT ENG OIL LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 1878 90000012 LT ENGINE OIL HOSE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021100575 19980211 00575 NE 1998 2 11 HEEA0012704 2 19980126 A 7311 1940683 PRE COOLER BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101650B1 41560 NE FUEL/OIL CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 PRE COOLER HAS CRACKS IN STEEL TUBE. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U NC H13EU E5NE 1998021100576 19980211 00576 1998 2 11 HEEA0012705 4 19980126 A 3457 069010290703 NAV COMM KLX135 BELL 407 407 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1167G 53067 GPS/NAV COMM MESSAGE BUTTON INOPERATIVE. 1 G 7 1 3U O H2SW 1998021100577 19980211 00577 SW 1998 2 11 HEEA0012738 1 19980127 A 7120 209062105001 BEARING ROD END BELL 412 412 1182202 SW ENG MOUNT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ROD END HAS TOO MUCH PLAY ON NEW BEARING. 1 G 7 2 4U H4SW 1998021100578 19980211 00578 SW 1998 2 11 HEEA0012750 1 19980202 A 7810 407063001101 EXHAUST STACK BELL 407 407 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 53038 ENGINE EXHAUST STACK IS CRACKED. 1 G 7 1 3U O H2SW 1998021100579 19980211 00579 SW 1998 2 11 HEEA0012751 1 19980202 A 7810 407063001101 EXHAUST STACK BELL 407 407 SW ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 ENGINE EXHAUST STACK IS CRACKED. 1 G 7 1 3U O H2SW 1998021100580 19980211 00580 SW 1998 2 11 HEEA0012752 1 19980202 A 7331 407375016101 SIGNAL COND BELL 407 407 SW ALLSN 250C 250C47B GL FUEL FLOW MALFUNCTION E HEEA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 03 141MA 1205 53016 FUEL LOW LIGHT ON WITH 600 POUNDS OF FUEL. 1 G 7 1 3U 3 U O H2SW E1GL 1998021100581 19980211 00581 SW 1998 2 11 HEEA0012753 1 19980202 A 6320 407375005101 INDICATOR BELL 407 407 SW XMSN OIL TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 612PH 62 53199 NO INDICATION ON PRESSURE SIDE. 1 G 7 1 3U O H2SW 1998021100582 19980211 00582 SW 1998 2 11 HEEA0012754 1 19980202 A 7712 407375003107 INDICATOR BELL 407 407 SW ENG TORQUE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 406PH 68 53198 TORQUE INDICATOR WILL NOT COMPLETE SELF TEST. BAR GRAPH STARTS HALFWAY UP. 1 G 7 1 3U O H2SW 1998021100583 19980211 00583 SW 1998 2 11 HEEA0012755 1 19980202 A 7931 407375004101 INDICATOR BELL 407 407 SW ENG OIL PRESS FLUCTUATES E HEEA K NONE O OTHER CR CRUISE 1 SW 03 57416 1198 53070 ENG OIL PRESSURE FLUCTUATES BETWEEN 0 AND 150 IN FLIGHT. 1 G 7 1 3U O H2SW 1998021100584 19980211 00584 GL 1998 2 11 HEEA0012756 2 19980202 A 7261 174250008 FILTER BELL 230 230 1182149 SW ALLSN 250C 250C30G2 03013 GL ENG OIL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 ENG OIL FILTER NO BYPASS INDICATION. 1 G 7 2 3U 3 U NC H9SW E1GL 1998021100585 19980211 00585 GL 1998 2 11 HEEA0012757 2 19980203 A 7313 6879867 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 3 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E CAT33222 S806 TURBINE REMOVED DUE TO CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR 3 NOZZLE FORWARD FLANGE AND AREAS MARKED. INSTALLED A STANDARD AERO OVERHAULED NOZZLE. 1 G 7 2 3U 3 U H3EU E4CE 1998021100586 19980211 00586 GL 1998 2 11 HEEA0012758 2 19980203 A 7250 6898730 PT SUPPORT 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E CAT33222 S806 TURBINE REMOVED DUE TO CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: MEASURED .003 OVER SPECS (1.764-1.761) ON PT SUP PORT NR 6 DAMPER GROOVE AND CHROME FLAKING FROM NR 7 DAMPER GROOVE. 1 G 7 2 3U 3 U H3EU E4CE 1998021100588 19980211 00588 EU 1998 2 11 HEEA0012761 1 19980205 A 6310 350A35106920 PIN SNIAS 350 AS350B2 8680813 EU GIMBLE JOINT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 4954 2771 GIMBLE JOINT PIN WORN. SCRAPPED AT PHI. 1 G 7 1 3U H9EU 1998021100589 19980211 00589 1998 2 11 HEEA0012762 4 19980205 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2124Z 45646 TRANSCEIVER NO POWER. ADJUSTED CAVITY FOR GOOD POWER OUT AND ON FREQUENCY. REPLACED WEAK V301 PHOTODETECTOR. BENCH CHE CK GOOD. 1 G 7 1 3U H2SW 1998021100590 19980211 00590 SW 1998 2 11 HEEA0012763 1 19980205 A 6320 205040245001 BEARING 412040002113 BELL 412 412 1182202 SW TRANSMISSION CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S A150 36002 BEARINGS CORRODED. BEARING CAGE RUBBING AND TIGHTING UP ON INNER RACE. REPLACED WITH SERVICEABLE BEARING SET. 1 G 7 2 4U H4SW 1998021100591 19980211 00591 EU 1998 2 11 HEEA0012764 1 19980205 A 6320 4638304001 SUN GEAR 4638001004 BOLKMS 105 BO105S 5626006 EU TRANSMISSION SPALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4573B 933 S673 FOUND SPALLING ON SUN GEAR TEETH. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998021100592 19980211 00592 EU 1998 2 11 HEEA0012765 1 19980205 A 6320 4638303001 BEVEL GEAR 4638001004 BOLKMS 105 BO105S 5626006 EU TRANSMISSION SPALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4573B 933 S673 FOUND SPALLING ON BEVEL GEAR TEETH. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998021100593 19980211 00593 NE 1998 2 11 HEEA0012766 1 19980205 A 2432 30126002S BATTERY SKRSKY S76 S76A 8143006 NE DC SYS FAILLED E HEEA O OTHER J WARNING INDICATION AP APPROACH 1 SW 03 911MJ 760231 BATTERY OFF LIGHT CAME ON IN FLIGHT ON SHORT FINAL. FOUND BATTERY CIRCUIT BREAKER ON MASTER ELECTRICAL BOX POPPED. UNA BLE TO RESET BREAKER. WHEN TEMP SENSOR CONNECTOR DISCONNECTED FROM BATTERY CIRCUIT BREAKER STAYS IN. WHEN TEMP SENSOR CONNECTOR CONNECTED TO BATTERY CIRCUIT BREAKER POPS. SECOND OCCURRENCE ON THIS S/N BATTERY. (SAME PROBLEM ON 11-20-97) REPLACED BATTERY WITH A SERVICEABLE BATTERY. 1 G 7 2 3U H1NE 1998021100594 19980211 00594 GL 1998 2 11 HEEA0012767 2 19980205 A 7314 3881005 FUEL PUMP BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5742N 14063 45477 FUEL PUMP EXCESSIVELY WORN INTERNAL SPLINES. 1 G 7 1 3U 3 U H2SW E1GL 1998021100595 19980211 00595 NE 1998 2 11 HEEA0012768 1 19980205 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 BLADE END CAP OF TIP CAP IS DAMAGED. 1 G 7 2 3U H1NE 1998021100596 19980211 00596 NE 1998 2 11 HEEA0012769 2 19980205 A 7310 430137601 FUEL NOZZLE BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE ENGINE LEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 134AE 7237 LE45758AEF FUEL LEAK FROM TUBE BETWEEN TWO NOZZLES. FUEL LEAKS OUT ALONG BRAZE AT NOZZLE. 1 G 7 2 3U 3 U NC H13EU E5NE10 1998021100597 19980211 00597 1998 2 11 HEEA0012770 4 19980205 A 2312 064100900 TRANSCEIVER KTR905 BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 TRANSCEIVER WILL NOT TRANSMIT. FOUND UNIT NOT RECEIVING. FOUND V20 NOT WORKING. REPLACED Q209, Q208, Q203, Q204, AND Q 221 TRANSISTORS, CR209 DIODE, I216 AND I217 J.C. STILL NO TRANSMIT OR RECEIVE. 1 G 7 2 4U H4SW 1998021100598 19980211 00598 1998 2 11 HEEA0012771 4 19980205 A 3455 066104701 RECEIVER BELL 212 212 1181420 SW ADF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3131S 30953 ADF RECEIVER SLOW TO POINT AND LOW AUDIO. 1 G 7 1 4U H4SW 1998021100599 19980211 00599 1998 2 11 HEEA0012772 4 19980205 A 2312 069102525 RECEIVER KX165 BOLKMS 117 BK117B2 5626013 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 LOC RECEIVER NOT PULLING FLAG. 1 G 7 2 3U NC H13EU 1998021100600 19980211 00600 1998 2 11 HEEA0012773 4 19980205 A 3452 066107100 TRANSPONDER BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911NC 7026 TRANSPONDER HAS NO OUTPUT. 1 G 7 2 3U H13EU 1998021100601 19980211 00601 EU 1998 2 11 HEEA0012774 1 19980205 A 7930 174035201 INDICATOR 174000103 BOLKMS 105 BO105S 5626006 EU ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4302G 4008 S853 INOPERATIVE-DOES NOT WORK. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND I NDICATOR STILL DIDN'T WORK. 1 G 7 2 3U H3EU 1998021100602 19980211 00602 1998 2 11 HEEA0012775 4 19980205 A 3457 0110010600 GPS GPS165 BOLKMS 117 BK117B1 5626012 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 GPS WILL NOT CHARGE GPS BATTERY. 1 G 7 2 3U H13EU 1998021100603 19980211 00603 1998 2 11 HEEA0012776 4 19980205 A 2370 9806020023 CVR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 327 33076 TEST LIGHT REMAINS ON ALL THE TIME. TIME SINCE REPAIR 0:00. 1 G 7 2 4U H4SW 1998021100604 19980211 00604 SW 1998 2 11 HEEA0012777 1 19980205 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 10670 33077 HOLES IN THE M/R BLADE OUTBOARD LEADING EDGE ABRASION STRIP. 1 G 7 2 4U H4SW 1998021100605 19980211 00605 SW 1998 2 11 HEEA0012778 1 19980205 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R ERRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 10983 33077 M/R BLADE OUTBOARD LEADING EDGE STRIP WITH EROSION HOLES THROUGH THE STRIP. 1 G 7 2 4U H4SW 1998021100606 19980211 00606 SW 1998 2 11 HEEA0012779 1 19980205 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 5120 33022 PIECE OF INBOARD ABRASION STRIP MISSING ON THE TOP OUTBOARD END OF M.R BLADE. 1 G 7 2 4U H4SW 1998021100607 19980211 00607 1998 2 11 HEEA0012780 4 19980205 A 3452 066106200 TRANSCEIVER KT76 BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 TRANSPONDER DOESN'T POWER UP. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT RECEIVING AND IDENT LIGHT BLINKS. SWAPP ED V101 CAVITY TUBE. NO HELP. 1 G 7 1 3U O H2SW 1998021100608 19980211 00608 NE 1998 2 11 HEEA0012781 1 19980205 A 6210 7615009100048A BLADE SKRSKY S76 S76A 8143006 NE M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 10457 760230 M/R BLADE TIP RIB UNBONDED. 1 G 7 2 3U H1NE 1998021100609 19980211 00609 NE 1998 2 11 HEEA0012782 1 19980205 A 6210 7615009100051A BLADE SKRSKY S76 S76A 8143006 NE M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 9890 760230 BLADE TRIM TAB SPLIT OPEN AND SEPARATED. 1 G 7 2 3U H1NE 1998021100610 19980211 00610 NE 1998 2 11 HEEA0012783 1 19980205 A 6210 7615009100042A BLADE SKRSKY S76 S76A 8143006 NE M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 12229 760050 M/R BLADE FIBERGLASS SEPARATED UNDERNEATH THE SPLICE TITANIUM AT STATION 112.5 ON BOTH SURFACES. THE TRIM TAB HAS SOME SEPARATION ALSO. 1 G 7 2 3U H1NE 1998021100611 19980211 00611 NE 1998 2 11 HEEA0012784 2 19980205 A 7310 2C273 CARTRIDGE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENG FUEL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3893P 33012 FOUND PLUG ON OUTSIDE END OF CARTRIDGE TO BE LEAKING FUEL. FOUND ADAPTER THAT HOLDS PLUG HAS EXCESSIVE PLAY. 1 G 7 2 4U 4 U H4SW E22EA 1998021100612 19980211 00612 1998 2 11 HEEA0012785 4 19980205 A 3444 066104800 ALTIMETER KRA405 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 RADAR ALTIMETER NEEDLE FLUCTUATING AND WILL NOT SELF TEST PROPERLY. 1 G 7 2 3U H1NE 1998021100613 19980211 00613 1998 2 11 HEEA0012786 4 19980205 A 3454 071121627 NAV CONTROL SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 NAV CONTROL UNIT CAUSES NO DISPLAY ON KTS143 TEST BOX. CDI NEEDLE WILL NOT MOVE ON HSI. 1 G 7 2 3U H1NE 1998021100614 19980211 00614 1998 2 11 HEEA0012787 4 19980205 A 3444 066106103 ALTIMETER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206LS 51070 RADAR ALTIMETER READS 200 FEET AT ALL TIMES. 1 G 7 1 3U H2SW 1998021100615 19980211 00615 1998 2 11 HEEA0012788 4 19980205 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 104PH 3622 TRANSPONDER INOPERATIVE. 1 G 7 1 3U H2SW 1998021100616 19980211 00616 1998 2 11 HEEA0012789 4 19980205 A 3457 0110005400 GPS GPS150 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6160Z 51610 GPS BATTERY LOW INDICATED. 1 G 7 1 3U H2SW 1998021100617 19980211 00617 SW 1998 2 11 HEEA0012790 1 19980205 A 7930 174035201 INDICATOR 174000103 BELL 206 206L1 1182107 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 476 45598 INDICATOR INOPERATIVE-DOES NOT WORK. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TE STED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998021100618 19980211 00618 NM 1998 2 11 AALA984001 1 19980103 A 5347 SEAT TRACK BOEING 767 767323 1385205 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 390AA 27450 AFW - SEAT TRACK HAD CORROSION BEYOND SRM LIMITS AFTER BLENDOUT. REMOVE SEAT TRACK LIPS ON BOTH SIDE OF DAMAGED AREA PE R ENGINEERING MRB 767-1555. (M) 2 L 7 2 4F RT A1NM 1998021100627 19980211 00627 NE 1998 2 11 ASOA98002 2 19980106 A 7261 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT REQ'D SERVICE A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 11 258AS 120131 115498 FLT 8258 - EN ROUTE ADF-ATL, LEFT ENGINE OIL PRESSURE DROPPED TO 45 PSI. CREW SHUT DOWN THE LEFT ENGINE, DECLARED AND E MERGENCY AND DIVERTED TO BNA WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. A DELTA MECHANIC INSPECTED THE ENGINE AND FOUND NO LEAKS BEFORE OR AFTER SERVICING THE ENGINE WITH 6 QUARTS OF OIL. UPON RETURN TO ATL, THE ENGINE WA S REINSPECTED AND FOUND TO BE AT THE ADD 1 QUART LEVEL. NO EXTERNAL LEAKS WERE NOTED. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998021100631 19980211 00631 EU 1998 2 11 SIMA980083 1 19980108 A 3320 S9251155500100 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 144DD 074 IND - FLT 4390 - EN ROUTE TO ORD FROM CVG CREW DIVERTED A/C INTO IND DUE TO SMOKE IN CABIN. CREW LANDED A/C SAFELY. FO UND READING LIGHT AT 7A BULBS AND TRANSFORMER BURNED. DEFERRED READING LIGHTS PER MEL AND A/C WAS RETURNED TO SERVICE. R/I'D READING LIGHT ASSY FOR SEAT 7A. PERFORMED OPERATIONAL CHECK SATISFACTORILY. REMOVED MEL AND RETURNED A/C TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1998021100632 19980211 00632 EU 1998 2 11 SIMA980161 1 19980116 A 2121 EVTA1926DA FAN AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 223AT 457 223 GRB - FLT 4240 - JUST BEFORE ENGINE START, FLIGHT ATTENDANT NOTED SMOKE COMING FROM FWD PART OF MAIN CABIN. MAINTENANCE FOUND THAT THE AIR EXTRACTION FAN HAD FAILED. R/I'S AIR EXTRACTION FAN. PERFORMED OPERATIONAL CHECK SATISFACTORILY AN D RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021100633 19980211 00633 EU 1998 2 11 SIMA980102 1 19980110 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 301AE 340B301 DFW - FLT 3775 - LEFT OVERWING EMERGENCY LIGHT IS INOP. MAINTENANCE FOUND CONNECTOR PIN HAD BACKED OUT IN CONNECTOR AT LIGHT ASSY. REINSTALLED PIN IN CONNECTOR, PERFORMED OPERATIONAL CHECK AND RETURNED TO A/C TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998021100634 19980211 00634 WP 1998 2 11 ORJA9802 1 19980107 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 FORWARD ENTRY EMERGENCY LIGHT NEON CHARGE INDICATING LAMP INOP. REMOVED AND REPLACED EMERGENCY LIGHT IAW MM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998021100635 19980211 00635 WP 1998 2 11 ORJA9803 1 19980108 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 880RA 53186 EMERGENCY LIGHT INOP AT ROW 25. REMOVED AND REPLACED LIGHT ASSY, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998021100636 19980211 00636 WP 1998 2 11 ORJA9805 1 19980113 A 3350 EM1267 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS INOP AT ROWS 5-10. FOUND BLOWN FUSE, BROKEN WIRE, SHORTED BATTERY. REMOVED AND REPLACED FUSE, BATTERY REPAIRED WIRING, OPS GOOD. (M) 2 L 7 2 4F RT A6WE 1998021100639 19980211 00639 NM 1998 2 11 F3LA97175 1 19980117 A 5712 6547934US RIB BOEING 737 737201 1384454 NM WS 217 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - FIXED L/E NR 3 SLAT TRACK INBOARD MAIN TRACK, INBOARD ROLLER SUPPORT RIB HAS CRACK, FSS 271, SS 31.42. REMOVED AN D REPLACED CRACKED RIB IAW SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1998021100640 19980211 00640 NM 1998 2 11 F3LA98001 1 19980122 A 3244 TIRE BOEING 737 7372L9 1384497 NM NLG FAILED A F3LA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 270FL 22733 DEN - AIR TURNBACK UPON TAKEOFF, FLIGHT CREW REPORTED NOSE GEAR VIBRATION, NOSE GEAR RED IN TRANSIT LIGHT REMAINED ILLUM INATED AND SMELL OF RUBBER IN COCKPIT. MAINTENANCE FOUND NR 2 NOSE TIRE BLOWN. REPLACED NOSE GEAR INNER CYLINDER AND B OTH NOSE LANDIGN GEAR TIRE AND WHEEL ASSEMBLIES. (M) 2 L 7 2 4F RT A16WE 1998021100641 19980211 00641 NM 1998 2 11 F3LA98002 1 19980126 A 3350 BULB BOEING 737 737301 1384611 NM CABIN FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 578US 23257 DEN - DURING SERVICE CEHCK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 2 A B C INOPERATIVE. MAINTENANCE REPLA CED BULBS AND RESECURED WIRING CONNECTOR AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1998021100642 19980211 00642 NM 1998 2 11 F3LA97172 1 19980117 A 5330 SKIN BOEING 737 737201 1384454 NM RT A/C COMPT WORN A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - TWO HOLES BURNED (ERRODED) THROUGH UPPER FWD INBOARD SKIN ABOVE AIR CLEANER IN RT AC BAY. REPAIRED IAW SRM 53-30- 3, PAGE 9 AND PAGE 10. DAMAGE OCCURRED DUE TO ABRASIVE AIR LEAK FROM HOLE IN BLEED AIR CLEANER. IN RT AC BAY. REPAIRED IAW SRM 53-30-3, PAGE 9 AND PAGE 10. DAMAGE OCCURRED DUE TO ABRASIVE AIR LEAK FROM HOLE IN BLEED AIR CLEANER. (M) 2 L 7 2 4F A16WE 1998021100643 19980211 00643 NM 1998 2 11 F3LA97173 1 19980117 A 5320 WEB BOEING 737 737201 1384454 NM BS 661 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 20212 PAE - HORIZ WEB AT BS 661, LBL 67, LL 208 IS CRACKED. FABRICATED WEB USING 7075-T6 .040 AND INSTALLED PER SRM 51-10-2. (M) 2 L 7 2 4F A16WE 1998021100644 19980211 00644 NM 1998 2 11 F3LA97174 1 19980117 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 212US 1289118665 20212 EMERGENCY EXIT LIGHTS FAIL BATTERY CAPACITY TEST. BOTH OVERWING EXIT DOORS, CENTER AISLE, AFT ENTRY AND SERVICE DOOR SI DE LIGHTS AND BOTH AFT SLIDE LIGHTS FAIL TEST. REMOVED AND REPLACED BATTERY PACK AT POSITION M1051 AND POSITION M1052 P ER MM 33-51-31. FUNCTIONAL TEST OF EMERGENCY LIGHTS PER MM 33-51-11 IS GOOD. (M) 2 L 7 2 4F A16WE 1998021100645 19980211 00645 WP 1998 2 11 98ZZZM175 1 19980115 A 3310 BA170 BALLAST DOUG DC8 DC861 3021952 WP COCKPIT OVERHEATED A FXLA K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 19 30UA 45888 ON LANDING AT MIA EXPERIENCED ELECTRICAL WIRE OVERHEAT ODOR IN COCKPIT. GROUND INSPECTION REVEALED OVERHEATED BALLASTS FOR FLOURESCENT LIGHTS IN COCKPIT. REPLACED BOTH BALLASTS, SYSTEM CHECKED NORMAL. (M) 2 L 7 4 4F 4A25 1998021100646 19980211 00646 WP 1998 2 11 98ZZZM176 1 19980114 A 3231 510361 LINK DOUG DC8 DC8F54 3021926 WP NLG DOOR BROKEN A FXLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 57FB 45669 AFTER TAKEOFF SJU, EXPERIENCED VIBRATION AND NOISE IN NOSE WHEEL WELL AREA. RETURNED TO SJU AND LANDED WITHOUT INCIDENT . FOUND LEFT NOSE GEAR DOOR OPEN AND DOOR LINK BROKEN. REPLACED DOOR LINK AND DOOR OP CHECKED NORMAL. 2 L 7 4 4F 4A25 1998021100647 19980211 00647 NM 1998 2 11 EIAA98002 1 19980109 A 2450 BPCU BOEING 747 747273C 1384896 NM NR 2 CONTAMINATED A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 470EV 20653 JFK - AFTER TAKEOFF NR 1 GENERATOR TRIPPED OFF, UPPER YAW DAMPER LIGHT CAME ON ABOUT SAME TIME WITH SPLIT RUDDER INDICAT ION, SSB OPENED AND NR 3 AND NR 4 BTB'S OPENED. RETURNED TO JFK LANDING NORMAL. REMOVED WATER FROM LOWER CARGO AREA. R EMOVED AND REPLACED NR 2 BPCU PER MM 24-22-02. NR 1 GCU PER MM 24-23-01, AND RESEATED UPPER YAW DAMPER COMPUTER PER MM 22-16-00 ALL AREAS OPS CHECKED GOOD. WATER APPEARED TO HAVE COME FROM PALLETS IN POSITIONS NR 1 AND 2. (M) 2 L 7 4 4F A20WE 1998021100648 19980211 00648 WP 1998 2 11 EIAA98001 1 19980107 A 7603 THROTTLE DOUG DC9 DC933F 302207A WP LEFT FROZE UP A EIAA O OTHER O OTHER DE DESCENT 1 NM 09 940F 47414 GEG - UNABLE TO RETARD LEFT THROTTLE AT TOP OF DESCENT. COULD NOT MOVE THROTTLE UNTIL DESCENT TO LOWER ALTITUDE AND RAT READS, 15 DEGREE CELSIUS. (M) 2 L 7 2 4F A6WE 1998021100649 19980211 00649 SO 1998 2 11 WTAA980011 1 19980115 A 2131 22201T011400 CONTROLLER EMB 120 EMB120RT SO COCKPIT FAILED A WTAA O G OTHER O2 MASK DEPLOYED J WARNING INDICATION NR NOT REPORTED 1 WP 17 251YV 120251 SMF - AIRCRAFT LOST CABIN PRESSURIZATION WITH SYSTEM IN AUTO MODE. OXYGEN MASKS DEPLOYED. MAINTENANCE DEFERRED AUTO MO DE FOR PRESSURIZATION PER MEL 21-31-1. REINSTALLED OXYGEN MASKS. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENT LY CLEARED DEFERRAL BY REPLACING AUTO PRESSURIZATION CONTROLLER. OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1998021100650 19980211 00650 SO 1998 2 11 WTAA980009 1 19980114 A 5350 4358XV3 RADOME EMB 120 EMB120RT SO NOSE DELAMINATED A WTAA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 17 271YV 120271 FAT - EN ROUTE FAT TO MRY, WEATHER RADAR REPORTED PAINTING FALSE RETURNS. WEATHER CONDITIONS EN ROUTE REQUIRED AIRCRAFT TO RETURN TO STATION. MAINTENANCE REPLACED RADOME ASSEMBLY. WEATHER RADAR OPERATIONAL CHECK NORMAL ON GROUND. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998021100651 19980211 00651 SO 1998 2 11 WTAA980007 1 19980113 A 2612 ASIESA3000 SMOKE DETECTOR EMB 120 EMB120RT SO LAVATORY MALFUNCTIONED A WTAA K NONE N FALSE WARNING UK UNKNOWN 1 WP 17 193YV 120193 FAT - LAV SMOKE DETECTOR ACTIVATED. MAINTENANCE INSPECTED A/C FOR EVIDENCE OF SMOKE ODOR, NONE DETECTED. DEFERRED LAV SMOKE DETECTOR PER MEL 26-26-3. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING L AV SMOKE DETECTOR. (M) 2 L 7 2 4T RT A31SO 1998021100654 19980211 00654 EU 1998 2 11 WTAA980005 1 19980109 A 3310 2621337040 BULB BAG JETSTM JETSTM3101 1500215 EU COCKPIT FAILED A WTAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 17 402UE 734 SFO - SMOKE REPORTED IN COCKPIT DURING CRUISE. CREW DECLARED EMERGENCY AIRCRAFT RETURNED TO STATION. MAINTENANCE FOUND AUXILIARY HEAT BACKLIGHTING INOPERATIVE AT FIRST OFFICERS SKIRT PANEL. DEFERRED BACKLIGHTING PER MEL 33-1. AIRCRAFT R ETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY RELAMPING AUXILIARY HEAT BACKLIGHTING. OPERATIONAL CH ECK SATISFACTORY. (M) 2 L 7 2 4T RT A21EU 1998021100655 19980211 00655 EU 1998 2 11 WTAA980012 1 19980118 A 3230 RETRACT MECH BAG JETSTM JETSTM3101 1500215 EU MLG MALFUNCTIONED A WTAA O OTHER J WARNING INDICATION DE DESCENT 1 WP 17 427UE 811 SFO - CREW REPORTED MAIN GEAR FAILED TO EXTEND ON INITIAL EXTENSION. ALL OPERATIONS NORMAL ON SECOND EXTENSION ATTEMPT. MAINTENANCE INSPECTED LANDING GEAR MICROSWITCHES AND WIRE CONNECTIONS ON GEAR CONTROL VALVE. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998021100678 19980211 00678 NM 1998 2 11 GAIA9804 1 19980113 A 2613 356802255 OVERHEAT LOOP BOEING 727 727251 138408H NM AFT FUSELAGE FAILED A GAIA B EMER. DESCENT N FALSE WARNING CL CLIMB 1 SW 07 279US 21158 FLT 739 - LEFT OAK AND EXPERIENCED A LOWER AFT BODY OVERHEAT LIGHT ON. RAN CHECKLIST. LIGHT DID NOT GO OUT. RETURNED TO OAK AFTER DECLARING AND EMERGENCY. AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED LEFT SECTION 48 OVERHEAT LO OP PER MM 26-14-00. OPS CHECK GOOD ON ENGINE RUN UP AT MAX POWER SETTING. (M) 2 L 7 3 4F A3WE 1998021100679 19980211 00679 NM 1998 2 11 TWRA9803 1 19980120 A 2560 65B096337 GIRT BAR BOEING 747 747212B 1384886 NM L2 DOOR BROKEN A TWRA K NONE O OTHER TX TAXI/GRND HDL 1 EA 15 619FF 21316 AFTER BLOCKING IN AT LAX, L2 DOOR DID NOT GO TO FULL MANUAL. FOUND AFT SIDE GIRT BAR SLIDING BRACKET MISSING FROM GIRT BAR. L2 DOOR DEFERRED INOP DUE L2 DOOR IN MANUAL, GIRT BAR LOOSE, HINGE BROKEN. L2 DOOR AND EMERGENCY SIGNS MARKED NO EXIT HALF B AND HALF C ZONES BLOCKED OFF AND DO NOT SIT PER MEL 25-10-1B. REPLACED BROKEN LIFTER PER MM 52-11-07, REINS TALLED BUSTLE, OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1998021100680 19980211 00680 NM 1998 2 11 TAOA019809 1 19980115 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 21244 FLT 6141 - BOS-LGA - FOUND ON L/S CHECK, OVERHEAD EMERGENCY EXI LIGHT AT ROW 3 ABC INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998021100681 19980211 00681 EU 1998 2 11 VTZA98004 1 19980105 A 6120 31028701 NTS VALVE BAG JETSTM JETSTM3201 1500217 EU NR 1 ENGINE FAILED A VTZA D E RETURN TO BLOCK ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 EA 27 370MT 800 FLT 6475 - IAD-SCE - DURING TAXI FLIGHT, AIRCRAFT RETURNED TO GATE DUE TO NR 1 ENGINE FLAMED OUT ON TAXI. AIRCRAFT RETU RNED TO GATE AND WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NTS VALVE, OPS CHECK OK. AIR CRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021100682 19980211 00682 1998 2 11 VTZA98005 4 19980106 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 301UE 41012 FLT 6510 - IAD-LGA - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE NR 1 AHRS FAILED IN FLIGHT. AIRCRAFT RETUR NED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 AHRS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998021100683 19980211 00683 EU 1998 2 11 VTZA98006 1 19980106 A 3260 ATG135022 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 311UE 41029 FLT 6506 - IAD-LGA - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE RIGHT GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH ON GEAR UP. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED UPLOCK SWI TCH. MAINTENANCE PERFORMED GEAR SWING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998021100684 19980211 00684 EU 1998 2 11 VTZA98007 1 19980107 A 7722 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE DIRTY A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 370MT 800 FLT 6332 - IAD-PIT - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT EGT FLUCTUATION 600 TO 0 DEGREES AND S RL WAS OFF. AIRCRAFT RETURNED TO GATE AND WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED THE ZONE 2 CANNO N PLUG AND PERFORMED ENGINE RUN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021100685 19980211 00685 1998 2 11 VTZA98008 4 19980107 A 3413 A3206910106 VSI INDICATOR BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILURE A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 487UE 906 FLT 6248 - IAD-BGM - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO CAPTAINS VSI SCREEN WENT BLANK. AIRCRAFT RETURNED TO GATE AND WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED VIS INDICATOR, OPS CHECK OK. AIRCRA FT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021100686 19980211 00686 1998 2 11 VTZA98009 4 19980107 A 3452 6226590001 ADAPTER BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 494UE 810 FLT 6551 - IAD-CLE - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BOTH TRANSPONDERS FAILED. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED CAD C-2 COUPLER ADAPTER, OPS CHEC K OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021100687 19980211 00687 EU 1998 2 11 VTZA98002 1 19980104 A 2910 1379305A85 HYD LINE BAG JETSTM JETSTM3201 1500217 EU MLG FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 494UE 810 FLT 6197 - PHL-IAD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BOTH HYDRAULIC SYSTEMS WENT TO ZERO INDIC ATION. AIRCRAFT RETURNED TO GATE AND WITH NO FURTHER PROBLEMS. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING PROBLE M. MAINTENANCE INSPECTED AND REMOVED AND REPLACED MLG ACTUATOR UP PRESSURE LINE, OPS CHECK OK. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021100688 19980211 00688 EU 1998 2 11 VTZA98011 1 19980112 A 7712 8974764 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 497UE 904 FLT 6319 - IAD-CLE - DURING CLIMB, EXPERIENCED A PROBLEM WITH THE LEFT TORQUE GAUGE GOING TO 120 PERCENT. AIRCRAFT RETU RNED TO IAD AND THE GATE WHERE MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCHED TO THE AIRCRFT AND FOUND TH AT THERE WAS OIL IN THE STRAIN GAUGE CANNON PLUG. MAINTENANCE CLEANED THE OIL FROM THE CANNON PLUG AND RECALIBRATED THE TORQUE SIGNAL CONDITIONER IAW ALL MAINTENANCE PROCEDURES. ALL REQUIRED CHECKS WERE ACCOMPLISHED AND THE AIRCRAFT WAS R ELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021100690 19980211 00690 EU 1998 2 11 VTZA98062 1 19980210 A 2750 S148YMK83NP FLAP SWITCH BAG JETSTM JETSTM3201 1500217 EU FLAPS FAILURE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 490UE 909 FLT 6348 - IAD-GSO - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FLAPS WOULD NOT RETRACT PAST 10 DEGREES. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLAP SELECTOR SWITC H, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021100691 19980211 00691 EU 1998 2 11 SABA980001 1 19980102 A 5230 SD3112179XA ROD ASSY STBROS SD3 SD360 8100606 EU BAGG DOOR OUT OF ADJUST A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 159CC SH3759 ON FLT FROM CLT TO OAJ, AIRCRAFT RETURNED TO CLT DUE TO FORWARD BAGGAGE COMPARTMENT DOOR LIGHT ILLUMINATED. NO EMERGENC Y DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. PASSENGERS DEPLANED. MAINTENANCE ADJUSTED THE PUSH-PULL ROD ON TH E FORWARD BAGGAGE COMPARTMENT DOOR. DOOR OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 1998021100692 19980211 00692 EU 1998 2 11 RAIA980109 1 19980107 A 2430 1030032 SENSOR AEROSP ATR42 ATR42300 8680920 EU RT WING FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 421TE 102 FLT 7398 - STL - RIGHT DC GENERATOR FELL OFF LINE, WOULD NOT RESET. MAINTENANCE REPLACED RIGHT DC GENERATOR HALL EFFECT SENSOR. (M) 2 H 7 2 4T RT A53EU 1998021100693 19980211 00693 EU 1998 2 11 RAIA980108 1 19980107 A 2160 7252C000 VALVE BAG JETSTM JETSTM3201 1500217 EU LT ACM FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 433AM 885 FLT 7476 - STL - CREW REPORTED SMOKE IN COCKPIT. MAINTENANCE INSPECTED AND FOUND FAULTY TEMPERATURE CONTROL VALVE ON LE FT SIDE. REPLACED LEFT TEMP CONTROL VALVE. (M) 2 L 7 2 4T RT A56EU 1998021100694 19980211 00694 EU 1998 2 11 RAIA980107 1 19980107 A 7722 56B17A SENSOR BAG JETSTM JETSTM3201 1500217 EU LT EGT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 426AM 11177 874 FLT 7486 - STL - LEFT ENGINE EGT FLUCTUATES 100 DEGREES CELSIUS. MAINTENANCE REPLACED LEFT ENGINE T-2 SENSOR. (M) 2 L 7 2 4T RT A56EU 1998021100695 19980211 00695 1998 2 11 RAIA980106 4 19980107 A 3425 7002493902 HSI BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 875JX 875 FLT 7396 - STL - FIRST OFFICERS HSI FAILED. MAINTENANCE REPLACED FIRST OFFICERS HSI. (M) 2 L 7 2 4T RT A56EU 1998021100696 19980211 00696 EU 1998 2 11 RAIA980105 1 19980107 A 2612 51653151 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 434AM 887 FLT 7100 - STL - LEFT ENGINE FIRE LIGHT ILLUMINATED, CREW DISCHARGED BOTH FIRE BOTTLES, SHUT ENGINE DOWN, UNLOADED PASSE NGERS. MAINTENANCE REPLACED LEFT ENGINE FIRE WIRE CONTROLLER. (M) 2 L 7 2 4T RT A56EU 1998021100697 19980211 00697 EU 1998 2 11 RAIA980110 1 19980109 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT FUEL DOOR FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 551HK 41040 FLT 7454 - STL - REFUEL DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE REPLACED REFUEL DOOR MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1998021100698 19980211 00698 EU 1998 2 11 RAIA980101 1 19980103 A 2611 CA3108R12S3SF80 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE INOP A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 875JX 875 FLT 7344 - STL - LEFT SRL CAPTION ILLUMINATED DURING APPLICATION OF TAKEOFF POWER. MAINTENANCE REPLACED WIRE CONNECTION AT LEFT ENGINE T2 SENSOR. (M) 2 L 7 2 4T RT A56EU 1998021100699 19980211 00699 EU 1998 2 11 RAIA980112 1 19980114 A 3310 13730390K8 PANEL BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT SHORTED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 423AM 858 FLT 7075 - STL - SMOKE COMING FROM FIRST OFFICERS SKIRT PANEL. MAINTENANCE REPLACED FIRST OFFICERS SKIRT PANEL. (M) 2 L 7 2 4T RT A56EU 1998021100700 19980211 00700 EU 1998 2 11 RAIA980115 1 19980115 A 3310 LT52A CONVERTER BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A RAIA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 03 423AM 858 FLT 7416 - EVV - SMOKE COMING FROM FIRST OFFICERS SKIRT PANEL. MAINTENANCE REPLACED SKIRT PANEL BACKLIGHTING CONVERTER. (M) 2 L 7 2 4T RT A56EU 1998021100701 19980211 00701 EU 1998 2 11 RAIA980114 1 19980114 A 3010 1D1468155 SWITCH BAG JETSTM JETSTM3201 1500217 EU WING DE-ICE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 426AM 14215 874 FLT 7394 - STL - WING DE-ICE LIGHT DOES NOT ILLUMINATE IN FLIGHT. MAINTENANCE REPLACED WING DE-ICE BOOT PRESSURE SWITCH . (M) 2 L 7 2 4T RT A56EU 1998021100702 19980211 00702 EU 1998 2 11 RAIA980111 1 19980113 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 428AM 3358 877 FLT 7418 - STL - NOSE GEAR DOWN AND LOCKED INDICATION FLICKERS WITH GEAR IN THE UP AND LOCKED POSITION. MAINTENANCE REP LACED NOSE GEAR DOWN LOCK SWITCH. (M) 2 L 7 2 4T RT A56EU 1998021100706 19980211 00706 NM 1998 2 11 MASA98006 1 19980109 A 5210 85210263101 GAS STRUT DHAV DHC8 DHC8202 2809007 NM CABIN DOOR WORN A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 449YV 449 FLT - 7580 - DEN-GJT - CREW FOUND THAT THE AIRSTAIR DOOR WAS DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE REMOVED AND REPLACED THE GAS STRUT AND LUBRICATED THE DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998021100721 19980211 00721 WP 1998 2 11 HALA9800007 1 19980112 A 3350 41B004A007G3 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 660HA 48122 HNL - FLT 106 - ONE FORWARD SECTION OF OVERHEAD EMERGENCY LIGHTS IN THE CABIN ARE VERY DIM. REPLACED EMERGENCY LIGHT BA TTERIES. THE OPERATIONAL CHECK WAS GOOD. (M) 2 L 7 2 4F RT A6WE 1998021100722 19980211 00722 WP 1998 2 11 HALA9800001 1 19980101 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 601AP 47658 HNL - FORWARD CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES, OPS OK. (M) 2 L 7 2 4F RT A6WE 1998021100724 19980211 00724 WP 1998 2 11 HALA9800005 1 19980108 A 2820 O-RING DOUG DC9 DC951 3022051 WP FUEL SHROUD FAILED A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 662HA 47742 STRONG FUEL SMELL IN CABIN DURING GROUND OPERATION. REPLACED O-RING ON FUEL SHROUD DRAIN. (M) 2 L 7 2 4F RT A6WE 1998021100725 19980211 00725 WP 1998 2 11 HALA9800006 1 19980108 A 3411 FITTING DOUG DC10 DC1010 3022110 WP LT NR 1 ADC LOOSE A HALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 13 119AA 46519 PDX - FLT 25 - ON TAKEOFF ROLL, CAPTAIN HAD NO AIRSPEED IND, F/O AIRSPEED READ 115 KTS, DID HIGH SPEED ABORT. LEAK TEST ED CAPT PITOT/STATIC SYSTEM. FOUND LEAK AT NR 1 ADC QUICK DISCONNECT FITTING. RE-SEATED FITTING. SYSTEM LEAK CHECKS O K. BITE CHECK NR 1 ADC TEST OK. (M) 2 L 7 3 4F A22WE 1998021100726 19980211 00726 WP 1998 2 11 G60A017 1 19980107 A 4940 36000965 PAWL DOUG DC10 DC1030F 3023504 WP APU STARTER WORN A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 602GC 47923 IN THE PROCESS OF TROUBLESHOOTING, APU STARTING FAULT. THE PAWLS OF THE STARTER ADAPTER WERE FOUND TO BE WORN. PARTS W ERE ORDERED IDENTIFIED BY P/N FORM DC-10 IPC 49-44-01 ITEM 80. WHEN THE PARTS WERE RECEIVED THERE WAS ONLY AND ADAPTER WITHOUT THE PAWL. WHEN THE MANUFACTURER ALLIED-SIGNAL IPC WAS CHECKED THERE WAS A DIFFERENT P/N AND WHEN ORDERED IT CON TAINED THE COMPLETE ASSY. (M) 2 L 7 3 4F RT A22WE 1998021100727 19980211 00727 NM 1998 2 11 EISA98005 1 19980116 A 2612 CONNECTOR BOEING 727 727251 138408H NM NR 2 ENGINE DIRTY A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 263US 19982 FIRE WARNING BELL, NO LIGHT. CLEANED FIREWALL ELECTRICAL CONNECTORS ON NR 2 ENGINE AND RESEALED CONNECTORS. (M) 2 L 7 3 4F A3WE 1998021100728 19980211 00728 NM 1998 2 11 EISA98004 1 19980115 A 2611 CONNECTOR BOEING 727 727251 138408H NM CARGO COMPT DIRTY A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 263US 19982 CARGO SMOKE DETECTOR ILLUMINATED. CLEANED CONNECTORS AND BLEW OUT ALL DETECTORS WITH DRY NITROGEN, OPS CHECK OK IAW MM 26-00. (M) 2 L 7 3 4F A3WE 1998021100729 19980211 00729 NM 1998 2 11 GAIA9803 1 19980101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 560 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 855AA 20996 LEVEL 2 CORROSION FINDINGS DURING C-CHECK AT AAR OKLAHOMA, SEAT TRACK STATION 560 LBL 36 REPAIRED AAR CARD 2000-0246. R EPAIR ACCOMPLISHED IAW B727 SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1998021100730 19980211 00730 NM 1998 2 11 98ZZZM181 1 19980101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 560 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 855AA 20996 LEVEL 2 CORROSION FINDINGS DURING C-CHECK AT AAR OKLAHOMA, SEAT TRACK STATION 560 LBL 45. REPAIRD AAR CARD 2000-0247. 2 L 7 3 4F A3WE 1998021100731 19980211 00731 NM 1998 2 11 98ZZZM182 1 19980101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1090 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 855AA 20996 LEVEL 2 CORROSION FINDINGS DURNIG C-CHECK AT AAR OKLAHOMA, SEAT TRACK STATION 1090 RBL 24, REPAIRED AAR CARD 2000-0244. 2 L 7 3 4F A3WE 1998021100732 19980211 00732 NM 1998 2 11 98ZZZM183 1 19980101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 760 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 855AA 20996 LEVEL 2 CORROSION FINDINGS DURING C-CHECK AT AAR OKLAHOMA, SEAT TRACK STATION 760 RBL 24, REPAIRED AAR CARD 2000-0298. 2 L 7 3 4F A3WE 1998021100733 19980211 00733 NM 1998 2 11 98ZZZM184 1 19980101 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 760 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 855AA 20996 LEVEL 2 CORROSION FINDINGS DURING C-CHECK AT AAR OKLAHOMA, SEAT TRACK STATION 760 LBL 24, REPAIRED AAR CARD 2000-0297. 2 L 7 3 4F A3WE 1998021100734 19980211 00734 WP 1998 2 11 GAIA9802A 1 19980114 A 2612 237EAU RELAY CVAC 240 240D 2422660 WP E/E COMPT LOOSE A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 94258 119 FLT 258 - CLE-YIP - DURING CRUISE, CREW NOTED THE FIRE DETECTION WARNING SYSTEM CAME ON TWICE FOR A FEW SECONDS, FOG TH FWD CARGO/ELECT COMPARTMENT. A DETAIL INSPECTION OF THE FIRE DETECTION SYSTEM REVEALED A SCREW HAD CAME LOOSE INSIDE TH E 237 LEACH RELAY, CAUSING AN INTERMITTENT ACTIVATION OF THE FIREW WARNING SYSTEM IN FLIGHT. NO OTHER DEFECTS WERE NOTE D IN THE SYSTEM. GROUND CHECK OF THE FIRE DETECTION SYSTEM CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4R RT A793 1998021100735 19980211 00735 NM 1998 2 11 GAIA9805 1 19980119 A 3230 RETRACT MECH BOEING 727 727224 1384076 NM NLG MALFUNCTIONED A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 69740 20668 FLT 740 - DFW-MSY - CREW REPORTED ON LOG PAGE 1086-11 AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. RETURNED TO DFW WITHOU T INCIDENT. INSPECTED GEAR. PERFORMED GEAR SWING IAW BOEING MM 32-32-0 PAGE 501. COULD NOT DUPLICATE PROBLEM AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998021100743 19980211 00743 NM 1998 2 11 EISA98006 1 19980125 A 2612 FIRE BELL BOEING 727 727221 1384071 NM COCKPIT SOUNDED A EISA K NONE N FALSE WARNING CL CLIMB 1 SW 07 366PA 22538 DURING CLIMB-OUT, FIRE BELL SOUNDED AND NO LIGHT. RERACKED FIRE DETECTOR UNIT. OPS CHECK GOOD IAW MM 26-00-00. (M) 2 L 7 3 4F A3WE 1998021100744 19980211 00744 NM 1998 2 11 98ZZZM192 1 19980116 A 2751 INDICATION BOEING 727 727230 1384080 NM TE FLAPS MALFUNCTIONED A C8GA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 15 357KP 20675 FLT 172 - BDL-PHL - AFTER T/O AND FLAP RETRACTION, NR 2 SLAT INDICATED INTRANSIT. FLAPS RETURNED TO 2 DEGREES, NO GREEN SAFE LIGHT. FLAPS RETURNED TO UP POSITION, NR 2 SLAT INDICATED INTRANSIT AND NR 6 INDICATED DOWN. FLAPS RETURNED TO U P WITH SAME SLATS INDICATED. OPERATED FLAPS UP AND DOWN SEVERAL TIMES. CHECKS SATISFACTORILY. SUSPECT WEATHER CONDITI ON, FREEZING RAIN. A/C OK FOR SERVICE. NO FURTHER SUBSEQUENT INDICATIONS. 2 L 7 3 4F A3WE 1998021100745 19980211 00745 SO 1998 2 11 ASOA98005 1 19980118 A 2750 3075001007 COMPUTER EMB 120 EMB120RT SO TE FLAP SYSTEM DEFECTIVE A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 237AS 120051 ON APPROACH ATL-FAY, SELECTED TO 15 DEG,THE I/B AND NACELLE FLAPS TRACKED TO 15 DEG WHILE THE O/B PAIR ON THE LT SIDE ST OPPED AT 5 DEG'S, THE RT SIDE INDICATED 45 DEG'S. A POSITIVE ROLL WAS FELT. THE CREW PROCEEDED WITH THE ASSEMETRY CHEC KLIST, DECLARED AN EMERGENCY AND LANDED FAY WITHOUT FURTHER INCIDENT. LOCAL MX INSPECTED THE A/C AND FOUND SAFE FOR A Z ERO-FLAP FERRY FLT TO ATL. ATL MX CYCLED THE FLAPS 30 TIMES AND COULD NOT DUPLICATE THE PROBLEM. AS A PREVENTIVE MEASU RE, REMOVED AND REPLACED THE COMPUTER. THE FLAPS WERE THEN CYCLED ANOTHER 15 TIMES WITH NO DEFECTS NOTED. THE A/C WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998021100746 19980211 00746 SO 1998 2 11 ASOA98006 1 19980121 A 2435 23080013 STARTER/GEN EMB 120 EMB120RT SO RT ENGINE FAILED A ASOA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 11 235AS 120047 EN ROUTE TUL-DFW, THE RT MAIN STARTER/GENERATOR FAILED, THE DC BUSS 3 C/B TRIPPED, AND THE CENTRAL BUSS WAS LOST. THE C REW FOLLOWED TH POH PROCEDURES, DECLARED AN EMERGENCY AND DIVERTED TO OKC WHERE LANDING WAS MADE SAFELY AND WITHOUT FURT HER INCIDENT. LOCAL MX MET THE AIRCRAFT AND RESET THE DC BUSS C/B AND THE O/C RELAYS. NO HELP. DFW MX WAS DISPATCHED AND REMOVED AND REPLACED THE RIGHT ENGINE STARTER/GENERATOR. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998021100747 19980211 00747 WP 1998 2 11 USAAD98013 1 19980112 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 997VJ 47336 DTW - CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 13 THROUGH 19. MAINTENANCE REPLACED THE POWER SUPPLY (M) 2 L 7 2 4F A6WE 1998021100748 19980211 00748 WP 1998 2 11 USAAD98012 1 19980120 A 3260 UPLOCK DOUG DC9 DC981 3022081 WP RT MLG OUT OF ADJUST A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 828US 48028 PHL - FLT 1199 - RIGHT MAIN GEAR UNSAFE LIGHT STAYED ON AFTER TAKEOFF. RECYCLED GEAR AND THE PROBLEM REMAINED. MAINTEN ANCE ADJUSTED THE RIGHT MAIN LANDING GEAR UPLOCK. INDICATION SYSTEM INDICATION WAS NORMAL DURING TEST FLIGHT. (M) 2 L 7 2 4F A6WE 1998021100749 19980211 00749 NM 1998 2 11 USAABB98004 1 19980118 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND R1 DOOR EMERGENCY EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE EXIT IDENTIFIER. (M) 2 L 7 2 4F RT A2NM 1998021100750 19980211 00750 NM 1998 2 11 USAABB98005 1 19980110 A 3350 9221009 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 LAX - FOUND L4 EMERGENCY EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998021100751 19980211 00751 NM 1998 2 11 USAABB98007 1 19980112 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 624AU 27245 LAX - FLOOR EMERGENCY LIGHTING INOPERATIVE AT ROWS 4 AND 6. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998021100752 19980211 00752 NM 1998 2 11 USAABB98006 1 19980114 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 LAX - FLOOR EMERGENCY LIGHTING INOPERATIVE AT ROWS 9 AND 18. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. (M0 2 L 7 2 4F RT A2NM 1998021100753 19980211 00753 WP 1998 2 11 TWAA9800903 1 19980119 A 2530 OVEN DOUG DC9 DC982 3022082 WP GALLEY CONTAMINATED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 920TW 49369 STL - FLT 253 - DURING CRUISE, SMOKE FUMES WERE NOTICED. ICE BUCKET WAS MELTED IN THE OVEN. REMOVED THE BUCKET. (M) 2 L 7 2 4F A6WE 1998021100754 19980211 00754 WP 1998 2 11 TWAA9800902 1 19980118 A 3220 SPLASHGUARD DOUG DC9 DC951 3022051 WP NLG BENT A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 415EA 47749 DFW - FLT 558 - DURING CLIMB, THE NOSE GEAR WOULD NOT RETRACT. FOUND WEAR PLATE ON THE SPLASHGUARD BENT, TRIMMED THE SP LASHGUARD PROTECTOR. (M) 2 L 7 2 4F RT A6WE 1998021100755 19980211 00755 NE 1998 2 11 TWAA9800901 2 19980117 A 7260 745450001 GEAR BOX BOEING 747 747131 1384881 NM PWA JT9 JT9D7AH 52054 NE NR 2 ENGINE FAILED A TWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 53110 19676 4267 FCO - FLT 883 - DURING CRUISE, NR 2 ENGINE OIL PRESS SLOWLY WENT TO ZERO. SHUT DOWN THE ENGINE. REPLACED OIL PUMP MGR P/N 804659-1 AND GEAR BOX MFG P/N 746450-001. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998021100756 19980211 00756 WP 1998 2 11 TWAA9800802 1 19980116 A 3244 TIRES DOUG DC9 DC982 3022082 WP NLG CONTAMINATED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 CE 05 904TW 49156 STL - ON TAKEOFF ROLL, NOSE WHEEL VIBRATED. FOUND A PIECE OF ICE LODGED BETWEEN NOSE TIRES. REMOVED THE ICE. (M) 2 L 7 2 4F A6WE 1998021100757 19980211 00757 WP 1998 2 11 TWAA9800801 1 19980116 A 2150 39245431 REGULATOR DOUG DC9 DC931 3022065 WP RT PACK FAILED A TWAA B EMER. DESCENT O OTHER CL CLIMB 1 CE 05 991Z 47096 STL - FLT 283 - DURING CLIMB, CABIN ALTITUDE CONTINUED TO CLIMB. REPLACED RT PACK REGULATOR MFG P/N 392454-3-1. (M) 2 L 7 2 4F A6WE 1998021100758 19980211 00758 WP 1998 2 11 TWAA9800701 1 19980113 A 3260 DS077S295 CONNECTOR DOUG DC9 DC932 3022066 WP LT MLG CORRODED A TWAA K NONE P NO WARNING INDICATION LD LANDING 1 CE 05 923L 47109 OKC - FLT 95 - ON FINAL APPROACH, LEFT MAIN LANDING GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. FOUND 3 WIRES BROKEN ON CANNON PLUG. REPLACED CANNON PLUG. (M) 2 L 7 2 4F A6WE 1998021100759 19980211 00759 NM 1998 2 11 TWAA9800601 1 19980115 A 7930 BYPASS LIGHT BOEING 727 727231 1384079 NM NR 2 ENGINE ILLUMINATED A TWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 05 54340 20845 DCA - FLT 439 - DURING CRUISE, NR 2 ENGINE FILTER BYPASS ANNUNCIATOR ILLUMINATED. SHUTDOWN THE ENGINE. PLACARDED AS PE R MEDP 79-2. (M) 2 L 7 3 4F A3WE 1998021100760 19980211 00760 WP 1998 2 11 TWAA9800602 1 19980115 A 2810 FUEL TANKS DOUG DC9 DC932 3022066 WP LT WING OVERFILLED A TWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CE 05 921L 47107 MCI - FLT 425 - DURING CRUISE, FUEL STARTED LEAKING OUT OF THE AFT LEFT WING. FOUND BOTH MAIN TANKS OVER FUELED, 9800 LBS IN BOTH TANKS. TRANSFERRED FUEL TO CENTER TANK. (M) 2 L 7 2 4F A6WE 1998021100761 19980211 00761 WP 1998 2 11 TWAA9800603 1 19980115 A 2120 AIR DISTRIBUTION DOUG DC9 DC932 3022066 WP CABIN ODOR A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 925L 47357 MKE - FLT 656 - WHILE TAXIING, AFT CABIN SMELLED HOT OIL FUMES. RAN APU WITH BOTH PACKS FOUND NO OIL SMELL OR OIL LEAKS . (M) 2 L 7 2 4F A6WE 1998021100762 19980211 00762 WP 1998 2 11 TWAA9800501 1 19980109 A 5210 DOOR DOUG DC9 DC982 3022082 WP CABIN NOT CLOSED A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 952U 49266 STL - FLT 350 - DURING FLIGHT CLIMB, CABIN WOULD NOT PRESSURIZE IN AUTO OR MANUAL. CLOSED L-2 DOOR PROPERLY. (M) 2 L 7 2 4F A6WE 1998021100763 19980211 00763 WP 1998 2 11 98ZZZM193 1 19980116 A 2782 720002C ACTUATOR LKHEED 1011 10113851 5265010 WP NR 7 LE FLAP FAILED A WRNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 311EA 193A1012 AFTER TAKEOFF DURING FLAP RETRACTION FLAP/SLAT LOCK LIGHT ON, L/E TRANS LIGHT REMAINED ON. GREEN SLAT LIGHTS ON LEFT WI NG. NO LIGHTS ON RT WING. AIRCRAFT RETURNED TO BASE. LANDING NORMAL. REMOVED AND REPLACED NR 7 SLAT ACT IAW 27-81-21 . REMOVED AND REPLACED RIGHT TORQUE LIMITING BRAKE ASSEMBLY IAW 27-08-17. ALL SYSTEMS OPS CHECKED NORMAL. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 1998021100764 19980211 00764 WP 1998 2 11 WRLA98071 1 19980121 A 2830 AV16B1926C S/O VALVE DOUG DC10 DC1030 3023501 WP LT FUEL SYSTEM INOPERATIVE A WRLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 27 117WA 48318 DURING AIR TURN BACK FOR PASSENGER MEDICAL EMERGENCY, FLIGHT CREW ACTIVATED FUEL DUMP PROCEDURES TO REDUCE A/C WEIGHT TO BELOW MAXIMUM LANDING WEIGHT. DURING FUEL DUMP PROCEDURES, 'DUMP VALVE OPEN' LIGHT FAILED TO GO OFF WHEN DUMP SWITCH W AS POSITIONED TO CLOSE. FLIGHT CREW RESET C/B, BUT SAME INDICATION WAS NOTED. ADDITIONALLY FLIGHT CREW WAS UNABLE TO T RANSFER FUEL, CONFIRMING THE LEFT DUMP VALVE WAS IN THE OPEN POSITION. AIRCRAFT CONTINUED TO DEPARTURE AIRPORT AND MADE AN UNEVENTFUL LANDING. GROUND MX FOUND LEFT FUEL DUMP SYSTEM SHUT OFF VALVE WOULD NOT CLOSE ELECTRICALLY. PART WAS NO T AVAILABLE ON SITE. VALVE WAS MANUALLY CLOSED PER MM PROCEDURES AND DEFERRED PER MEL PROCEDURES. A/C RETURNED TO SERV 2 L 7 3 4F A22WE 1998021100765 19980211 00765 EU 1998 2 11 SIMA980231 1 19980123 A 3350 3012000 BATTERY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AT 497 399 DFW - FLT 3814 - SEVERAL OF THE EMERGENCY FLOOR LIGHTING ARE INOP, ALONG WITH THE AFT EMERGENCY EXIT LIGHTS. R/I'D BATT ERY PACK AND POWER SUPPLY, 72WL AND FUSE IN POWER SUPPLY 62WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021100766 19980211 00766 EU 1998 2 11 98ZZZM194 1 19980123 A 3350 3012001 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AT 497 399 DFW - FLT 3814 - SEVERAL OF THE EMERGENCY FLOOR LIGHTING ARE INOP, ALONG WITH THE AFT EMERGENCY EXIT LIGHTS. R/I'D BATT ERY PACK AND POWER SUPPLY, 72WL AND FUSE IN POWER SUPPLY 62WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021100767 19980211 00767 EU 1998 2 11 98ZZZM195 1 19980123 A 3350 F18L250V FUSE AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AT 497 399 DFW - FLT 3814 - SEVERAL OF THE EMERGENCY FLOOR LIGHTING ARE INOP, ALONG WITH THE AFT EMERGENCY EXIT LIGHTS. R/I'D BATT ERY PACK AND POWER SUPPLY, 72WL AND FUSE IN POWER SUPPLY 62WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021100768 19980211 00768 EU 1998 2 11 SIMA980242 1 19980124 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 12698 223 SAW - DURING PS2 CHECK, MAINTENANCE DISCOVERED SEVERAL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED EMERGENC Y LIGHT BATTERY PACKS AT LOCATION 29WL AND 3WL IAW JIC 335121-RAI-10010-003. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021100769 19980211 00769 EU 1998 2 11 SIMA980181 1 19980118 A 6120 S4003VB31 HARNESS AEROSP ATR42 ATR42300 8680920 EU RT ENGINE SHORTED A A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 21 427MQ 091 AZO - FLT 4171 - EN ROUTE TO GRR FROM ORD, THE RT PROP MOVED TO FEATHER UNCOMMANDED. THE ENG WAS SHUT DOWN AND A/C DIVE RTED TO AZO AND LANDED WITHOUT INCIDENT. CREW DID NOTE TORQUE IND WAS AT MAX AT THE TIME THE UNCOMMANDED FEATHER OCCURR ED. MX FOUND A CHAFED WIRE IN ENG WIRING HARNESS THAT ALLOWED THE FEATHERING CIRCUIT TO ACTIVATE. ENG HARNESS WAS REPL ACED. ADDITIONALLY, THE FDAU AND WAS DETERMINED THE TORQUE VALUES WERE WITHIN LIMITS FOR BOTH THE ENG AND PROP TO REMAI N IN SERV. PROP WAS REPLACED AS A PRECAUTIONARY MEASURE AT ENGINEERS REQUEST. FOLLOWING THE ABOVE MENTIONED MX, A SATI SFACTORY FUNCTIONAL TEST FLT WAS ACCOMPLISHED. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021100770 19980211 00770 NM 1998 2 11 98ZZZM196 1 19980117 A 3350 1000677 LIGHT BOEING 727 727222 1384073 NM CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 7645U 20039 DURING PREFLIGHT IN DAY, EMERGENCY EXIT LIGHT L-1 DOOR INOPERATIVE. REMOVED AND REPLACED ENTRY DOOR L-1 EMERGENCY EXIT LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1998021100772 19980211 00772 NM 1998 2 11 98ZZZM198 1 19980118 A 3310 1041021 LIGHT BOEING 727 72751C 1384015 NM COCKPIT BURNED A RYNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 07 436EX 19289 FLT 6704 - IND-SEA - HAD AN AIR RETURN TO IND CLIMBING OUT OF IND CREW EXPERIENCED A STRONG ELECTRICAL ODOR AND SMOKE WA S CLEARLY VISIBLE UNDER CAPTAINS GLARESHIELD. REMOVED AND REPLACED BOTH INBOARD FLOURESCENT LIGHT SOCKETS. (M) 2 L 7 3 4F A3WE 1998021100773 19980211 00773 1998 2 11 REXA98019 4 19980119 A 3425 CIRCUIT BREAKER BAG JETSTM JETSTM3101 1500215 EU LT HSI TRIPPED A REXA D RETURN TO BLOCK I FLT. ATTITUDE INST. TX TAXI/GRND HDL 1 SO 25 330PX 698 COMPASS SPLIT, LEFT APPEARS TO BE OFF. RESET LEFT HSI CIRCUIT BREAKER. (M) 2 L 7 2 4T RT A21EU 1998021100774 19980211 00774 1998 2 11 REXA98018 4 19980115 A 6122 8210263 PROP GOVERNOR BAG JETSTM JETSTM3101 1500215 EU RT ENGINE FAILED A REXA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 303PX 662 RIGHT RPM GAUGE STUCK AT 100 PERCENT. REMOVED AND REPLACED RIGHT PROP GOVERNOR. (M) 2 L 7 2 4T RT A21EU 1998021100775 19980211 00775 EU 1998 2 11 REXA98017 1 19980118 A 5101 STRUCTURE SAAB SF340 SF340A 7850100 EU AIRFRAME LIGHTNING STRIKE A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 346AM 340A032 LIGHTNING STRIKE INFLIGHT. PERFORMED LIGHTNING STRIKE INSPECTION IAW SAAB AMM. A/C OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1998021100776 19980211 00776 1998 2 11 REXA98016 4 19980115 A 2350 B692254 STATION BOX BAG JETSTM JETSTM3101 1500215 EU RT COCKPIT FAILED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 302PX 661 F/O INTERCOM INOP W/2 DIFFERENT HEAD SETS. F/O HEARD BUZZING SOUND PRIOR TO INTERCOM BECOMING INOP. REMOVED AND REPLAC ED F/O'S STATION BOX. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998021100777 19980211 00777 1998 2 11 REXA98015 4 19980115 A 2350 B692254 CONTROL PANEL BAG JETSTM JETSTM3101 1500215 EU RT COCKPIT FAILED A REXA O OTHER O OTHER DE DESCENT 1 SO 25 302PX 00192C 661 FO AUDIO PANEL WENT OUT AND NO RADION CONTACT WAS HEARD. REMOVED AND REPLACED AUDIO CONTROL PANEL. OPS CHECK GOOD. (M ) 2 L 7 2 4T RT A21EU 1998021100778 19980211 00778 1998 2 11 REXA98014 4 19980114 A 3414 6226728011 AIRSPEED IND SAAB SF340 SF340A 7850100 EU LT COCKPIT FAILED A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 407BH 006 340A078 CAPTAINS AIRSPEED INDICATOR INOP. REMOVED AND REPLACED CAPTAINS AIRSPEED INDICATOR. (M) 2 L 7 2 4T RT A52EU 1998021100779 19980211 00779 EU 1998 2 11 JBXA980031 1 19980117 A 2760 SPOILER FOKKER F28 F28MK0100 4990807 EU WING MALFUNCTIONED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 133ML 11330 RDU - FLT 448 - WHILE DEPARTING RDU FOR ALT CAPTAIN ABORTED TAKEOFF, AT 100 KTS DURING TAKEOFF ROLL A LIFT DUMPER FAULT WAS ANNUNCIATED ON THE LEFT MFDU. ASSIGNED TO DMI D04842 PER MEL 27-63-1-5. (M) 2 L 7 2 4F RT 1998021100780 19980211 00780 NM 1998 2 11 ASAA9810007 1 19980114 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE ON PALLET 5-9. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998021100781 19980211 00781 NM 1998 2 11 ASAA9810008 1 19980115 A 3350 873203041 TRANSMITTER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST DE DESCENT 1 NM 01 746AS 23123 ANC - DURNIG DESCENT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED AND THEN EXTINGUISHED AFTER 20 SECONDS. REPLACE D MID CABIN TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100782 19980211 00782 NM 1998 2 11 ASAA9840007 1 19980113 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 786AS 24795 SFO - FLT 377 - PRIOR TO FLGHT SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE TOWARDS THE AFT CABIN. R ECONNECTED WIRING AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100783 19980211 00783 WP 1998 2 11 ASAA9880008 1 19980112 A 5320 MEMBRANE DOUG DC9 DC982 3022082 WP BS 229 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 OAK - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR MEMBRANE UNDER GALLEY 2 INBOARD MOUNT AT FS 229. REPAIRED WITH DOU BLER IAW ASA EA 5320-01203. (M) 2 L 7 2 4F A6WE 1998021100789 19980211 00789 NM 1998 2 11 ASAA9810001 1 19980103 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 10-12. REPLA CED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100790 19980211 00790 NM 1998 2 11 ASAA9810002 1 19980106 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST CR CRUISE 1 NM 01 746AS 23123 ANC - FLT 46 - DURING FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 10-12 AND THE WALL MOUNTED EXIT IDENTIFIER B Y THE AFT AIRSTAIR DOOR ILLUMINATED. REPLACED BATTERY PACK AT ROWS 11 AND 12, AND THE AFT EXIT IDENTIFIER AND ALL LIGHT S OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100791 19980211 00791 NM 1998 2 11 98ZZZM199 1 19980106 A 3350 1060091101 SIGN BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST CR CRUISE 1 NM 01 746AS 23123 ANC - FLT 46 - DURING FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 10-12 AND THE WALL MOUNTED EXIT IDENTIFIER B Y THE AFT AIRSTAIR DOOR ILLUMINATED. REPLACED BATTERY PACK AT ROWS 11 AND 12, AND THE AFT EXIT IDENTIFIER AND ALL LIGHT S OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100792 19980211 00792 NM 1998 2 11 ASAA9810003 1 19980108 A 3350 8821004 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - FLT 30 - DURING RECON, ONE SECTION OF THE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PA CK AND TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100793 19980211 00793 NM 1998 2 11 98ZZZM200 1 19980108 A 3350 883200312 TRANSMITTER BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - FLT 30 - DURING RECON, ONE SECTION OF THE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PA CK AND TRANSMITTER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100794 19980211 00794 NM 1998 2 11 ASAA9810004 1 19980109 A 3350 LIGHT BOEING 737 7372Q8C 138448S NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, AN EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 20. RELEASED PER MEL 33-19. SUBSEQUENTLY REPAIRED LIGHT ASSEMBLY AT ROW 20 AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998021100795 19980211 00795 NM 1998 2 11 ASAA9810005 1 19980111 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTS REMAINED ILLUMINATED ON SEAT PALLET 2. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100796 19980211 00796 NM 1998 2 11 ASAA9840006 1 19980110 A 3350 S283T0143 BATTERY BOEING 737 7374S3 1384711 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE AFT GALLEY RT INBOARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100797 19980211 00797 WP 1998 2 11 ASAA9880009 1 19980113 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 49126 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998021100799 19980211 00799 NM 1998 2 11 ASAA9840002 1 19980108 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 PDX - DURING MAINTENANCE CHECK, TEH AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECT ED LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998021100800 19980211 00800 NM 1998 2 11 ASAA9840003 1 19980109 A 2750 65C308461 BELLCRANK BOEING 737 7374Q8 NM TE FLAP MISMANUFACTURED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING C-CHECK, THE BELLCRANK ASSEMBLY ON THE OUTBOARD AFT FLAP IS MISSING DRAIN HOLE. REPAIRED PER EA 2750-01036 . (M) 2 L 7 2 4F RT A16WE 1998021100801 19980211 00801 NM 1998 2 11 ASAA9840004 1 19980109 A 5720 655077368 FITTING BOEING 737 7374Q8 NM RT WING WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING C-CHECK, WEAR WAS FOUND ON THE LOWER SURFACE OF THE UPPER FLANGE ON THE RT WING T/E RIB FITTING. REPAIRED PER EA 5750-01269 AND BOEING TELEX M-7200-98-00052. (M) 2 L 7 2 4F RT A16WE 1998021100802 19980211 00802 NM 1998 2 11 ASAA980005 1 19980109 A 5414 65C2757411 SKIN BOEING 737 7374Q8 NM LT PYLON WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING C-CHECK, WEAR WAS FOUND ON THE LEFT ENGINE PYLON SKIN. REPAIRED PER EA 5450-01012 AND BOEING TELEX ASA-SEA -97-0507RR. (M) 2 L 7 2 4F RT A16WE 1998021100803 19980211 00803 WP 1998 2 11 ASAA9880001 1 19980102 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS REMAIN ON WITH THE MAIN BATTERY SWITCH O FF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998021100804 19980211 00804 WP 1998 2 11 ASAA9880002 1 19980102 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998021100805 19980211 00805 WP 1998 2 11 ASAA9880004 1 19980105 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 8 TO 12 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998021100806 19980211 00806 WP 1998 2 11 ASAA9880005 1 19980106 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT COVER AT ROW 3 WAS FOUND PULLED UP AND THE 2ND FORWARD L IGHT WAS INOPERATIVE. RECONNECTED THE CONNECTOR TO THE LIGHT ASSEMBLY AND REINSTALLED THE TRACK COVER AND OPERATED NORM ALLY. (M) 2 L 7 2 4F RT A6WE 1998021100807 19980211 00807 WP 1998 2 11 ASAA9880006 1 19980108 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L-1 DOOR DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 49925 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998021100808 19980211 00808 WP 1998 2 11 ASAA9880007 1 19980109 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP L-1 DOOR DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998021100809 19980211 00809 WP 1998 2 11 USAAD978010 1 19980117 A 3350 41B030CF00101 POWER SUPPLY DOUG DC9 DC931 3022065 WP CARGO COMPT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918VJ 48138 CMH - LEFT EXIT WINDOW EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998021100810 19980211 00810 WP 1998 2 11 USAAD98009 1 19980118 A 3230 39140165503 BUNGEE CYLINDER DOUG DC9 DC931 3022065 WP RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 982VJ 48158 PIT - FLT 1777 - DURING CLIMB-OUT THROUGH 11,000 FT, THE RIGHT GEAR AND GEAR DOOR UNSAFE LIGHT ILLUMINATED. ABNORMAL PR OCEDURES WERE FOLLOWED AND THE AIRCRAFT RETURNED TO THE FIELD. UPON GEAR EXTENSION ALL THREE GEAR INDICATED DOWN AND LO CKED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT GEAR BUNGEE CYLINDER ROD END BROKEN. THE BU NGEE CYLINDER WAS REPLACED AND THE GEAR WAS CYCLED. ALL INDICATION AND OPERATION WAS NORMAL. (M) 2 L 7 2 4F A6WE 1998021100811 19980211 00811 WP 1998 2 11 USAAD98008 1 19980106 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 PHL - LOW LEVEL LIGHTING ROWS 3, 6, AND 11 WEAK. MAINTENANCE REPLACED THE BATTERIES AT ROWS 3, 6, AND 11. SYSTEM THEN CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998021100812 19980211 00812 WP 1998 2 11 USAAD98005 1 19980111 A 2170 COALESCER BAG DOUG DC9 DC931 3022065 WP A/C COMPT DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 925VJ 48145 IND - FLT 1528 - AFTER TAKEOFF, THE PASSENGER CABIN HAD A STRONG ODOR COMING FROM THE AIR CONDITIONING PACKS. THE SMOKE DETECTORS IN THE LAVATORIES CAME ON BUT THERE WAS NO VISIBLE SMOKE. THE CREW DECIDED TO RETURN TO THE FIELD. THE AIRC RAFT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE PAU AND MEL, REPLACED THE WATER SEPARATOR COALESCER BAGS. RAN BOT H ENGINES WITH PACKS OPERATING, ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998021100813 19980211 00813 WP 1998 2 11 USAAD98011 1 19980119 A 5610 5912290505 WINDOW DOUG DC9 DC981 3022081 WP LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 826US 48026 PIT - FLT 1085 - DURING CLIMB-OUT AT 28,000, THE OUTER PANE OF THE CAPTAINS WINDOW CRACKED. THE AIRCRAFT RETURNED TO TH E FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAINS WINDOW. (M) 2 L 7 2 4F A6WE 1998021100814 19980211 00814 NM 1998 2 11 USAABB98003 1 19980108 A 2751 S251N40318 POSITION TRANS BOEING 757 7572B7 1384964 NM RT TE FLAP FAILED A USAA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 EA 19 611AU 27123 BWI - FLT 6 - ON APPROACH TO DCA, THE FLAPS FAILED TO MOVE AND CREW RECEIVED THE EICAS MESSAGE, 'TE FLAP ASYM'. FLT DIV ERTED TO BWI AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT FLAP POSITION TRANSMITTER. (M) 2 L 7 2 4F RT A2NM 1998021100815 19980211 00815 NM 1998 2 11 USAABB98002 1 19980104 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 608AU 22204 LAX - EMERGENCY AISLE LIGHTING AT ROW 1 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY. (M) 2 L 7 2 4F RT A2NM 1998021100817 19980211 00817 WP 1998 2 11 98ZZZM201 1 19980104 A 2410 696233B CSD DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 824US 49143 CLT - FLT 1754 - CLIMBING THROUGH 12,000 FT, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT R ETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND CSD. THE APU GENERATOR AND CONTROL UNIT WERE ALSO REPLACED. BOTH SYSTEMS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998021100818 19980211 00818 WP 1998 2 11 98ZZZM202 1 19980104 A 2420 947F9453 CONTROL UNIT DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 824US 49143 CLT - FLT 1754 - CLIMBING THROUGH 12,000 FT, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT R ETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND CSD. THE APU GENERATOR AND CONTROL UNIT WERE ALSO REPLACED. BOTH SYSTEMS THEN OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998021100823 19980211 00823 WP 1998 2 11 USAAD98007 1 19980111 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CARGO BIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 956VJ 47588 IND - RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP, BATTERY PACK AND THE POWER SUPPLY. LAM P P/N 4593, POSER SUPPLY P/N 6011777LB. (M) 2 L 7 2 4F A6WE 1998021100824 19980211 00824 WP 1998 2 11 USAAD98006 1 19980111 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 825US 49237 CLT - EMERGENCY LIGHTS IN TAIL COMPARTMENT CEILING INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M ) 2 L 7 2 4F A6WE 1998021100825 19980211 00825 NM 1998 2 11 USAASB98008 1 19980111 A 3350 AD20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY/EXIT/EVACUATION LIGHTS INOP, ROW 7 BULLNOSE, SEAT ROWS 6 THROUGH 9, BOTH CEILING EXIT LIGHTS, EXIT LIGHT FOR LEFT OVERWING AND ROW 11F SIDEWALL EXIT SIGN WITH ARROW. MAINTENANCE REMOVED AND R EPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998021100883 19980211 00883 SO 1998 2 11 C2XA98CL003 1 19980106 A 2910 NAS1602906 O-RING EMB 145 EMB145 SO NR 1 HYD SYSTEM FAILED A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 15932 145015 CLE - FLT 4227 - CREW REPORTED WHILE EN ROUTE FROM EWR, THEY RECEIVED A HYDRAULIC LOW QUANTITY SYSTEM 1 INDICATION FOLLO WED BY PRESSURE LOSS AND THE FAILURE OF THE SYSTEM. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAIN TENANCE REMOVED AND REPLACED A FAILED O-RING AT THE NR 1 HYDRAULIC SYSTEM PRIORITY VALVE IAW EMB-1465 MM 29-10-13. THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WAS ALSO REMOVED AND REPLACED IAW EMB-145 MM 29-10-03 AS A PRECAUTION. OPERATIONAL AN D LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT T00011AT 1998021100886 19980211 00886 CE 1998 2 11 MASA98002 1 19980101 A 6120 5038912121 PRESSURE SWITCH 1299100001 BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 218YV UE218 PIT/MBS - FLT 5999 - LEFT AUTOFEATHER FAILED ON CLIMB-OUT. MAINTENANCE REMOVED AND REPLACED PRESSURE SWITCH. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998021100896 19980211 00896 WP 1998 2 11 CALA9800196 1 19980209 A 4990 38003681 APU DOUG DC9 DC982 3022082 WP AFT FUSELAGE LOW OIL A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 937MC 29641 49450 WHILE OPERATING THE APU IN FLIGHT WITH THE AC CROSSTIE RELAY PLACARDED INOPERATIVE. THE APU AUTO SHUTDOWN. MAINTENANCE SERVICED THE APU WITH OIL, NO LEAKS WERE DETECTED. 2 L 7 2 4F A6WE 1998021100897 19980211 00897 WP 1998 2 11 CALA9800197 1 19980206 A 2760 CRANK ASSY DOUG DC10 DC1030 3023501 WP CTR PEDESTAL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13086 46917 THE AUTO SPOILERS WOULD NOT DEPLOY WHEN REVERSE THRUST WAS SELECTED. MAINTENANCE FOUND A 1 INCH CRACK IN THE AUTO SPOIL ER CRANK ASSEMBLY. THE CRANK ASSEMBLY WAS REPLACED IAW MM 27-62-01. 2 L 7 3 4F A22WE 1998021100898 19980211 00898 NM 1998 2 11 CALA9800198 1 19980207 A 5320 WEB BOEING 727 727243 138408D NM BS 872.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A .125 CRACK IN RT MLG WHEEL WELL PRESSURE WEB AT BS 872.5, RBL 52.25. A PRESSURE WEB REPAIR WAS FABRI CATED AND INSTALLED IAW ECRA 5310-03671. 2 L 7 3 4F RT A3WE 1998021100899 19980211 00899 WP 1998 2 11 CALA9800199 1 19980209 A 5210 BACB30US9K22 BOLT DOUG DC10 DC1030 3023501 WP DOOR 4R SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A SHEARED BOLT IN AFT FRAME OF DOOR 4R AT LONGERON 15R. THE BOLT WAS REPLACED IAW MM 20-50-02. 2 L 7 3 4F A22WE 1998021100900 19980211 00900 NM 1998 2 11 CALA9800200 1 19980209 A 5510 FITTING BOEING 737 7373T0 1384582 NM RT HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14347 23585 INSPECTION FOUND RT HORIZONTAL STABILIZER AFT LOWER FITTING OF AFT SPAR GOUGED. THE GOUGE WAS BURNISHED, AND THE AREA W AS SHOT PEENED, TREATED, AND PRIMED IAW ECRA 5550-01035. 2 L 7 2 4F RT A16WE 1998021100901 19980211 00901 NM 1998 2 11 CALA9800201 1 19980209 A 5510 FITTING BOEING 737 7373T0 1384582 NM LT HORIZ STAB GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14347 23585 INSPECTION FOUND THE LT HORIZONTAL STABILIZER AFT LOWER ATTACH FITTING GOUGED IN THREE AREAS ON LOWER SIDE. THE GOUGES W ERE BURNISHED, SHOT PEENED, TREATED, AND PRIMED IAW ECRA 5550-01035. 2 L 7 2 4F RT A16WE 1998021100902 19980211 00902 NM 1998 2 11 CALA9800202 1 19980209 A 5320 DOOR FRAME BOEING 727 727243 138408D NM BS 410 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND A 5 INCH CRACK IN UPPER AFT SECTION OF R-1 DOOR FRAME AT BS 410. THE CRACKED SECTION OF DOOR FRAME WAS CUTOUT IAW BOEING DRAWING 69-69978. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F RT A3WE 1998021100903 19980211 00903 WP 1998 2 11 CALA9800203 1 19980210 A 5210 FITTING DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND A 1.5 INCH CRACK IN AFT CABIN DOOR BEAM END FITTING AT LEFT CENTER STOP. A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998021100904 19980211 00904 WP 1998 2 11 CALA9800204 1 19980210 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND CORROSION IN LOWER FORWARD CORNER OF AFT CARGO DOOR CUTOUT AT STA 1155. A REPLACEMENT ANGLE WAS FABRIC ATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998021100905 19980211 00905 WP 1998 2 11 CALA9800205 1 19980210 A 5320 SPLICE DOUG DC9 DC982 3022082 WP BS 1220 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND CORROSION ON TIEDOWN RAIL SPLICE AT STA 1220, LONGERON 28L, IN AFT CARGO COMPARTMENT. THE SPLICE WAS R EMOVED AND A NEW SPLICE WAS FABRICATED AND INSTALLED IAW SRM 53-05-4. 2 L 7 2 4F A6WE 1998021100906 19980211 00906 NM 1998 2 11 98UAL900012 1 19980109 A 3211 H1977724 NUT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT MLG SPLIT A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7264U 21411 LEFT HAND MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING STUD INBOARD NUT SPLIT IN HALF. *S/D* REPLACED LEFT HAND MLG TRUNNION SUPPORT FITTING STUD INBOARD NUT AND WASHER, INSTALLED ROLLPIN AND SAFETIED. CHECK OF NUTS ACCOMPLISH AT A AND HIGHER CHECKS. 2 L 7 3 4F 4 F A3WE E2EA 1998021100907 19980211 00907 NM 1998 2 11 98UAL900023 1 19980119 A 3260 M986 CIRCUIT CARD BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LANDING GEAR FAILED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 357UA 24378 LANDED WITH AN UNSAFE GEAR INDICATION. *S/D* REPLACED CIRCUIT CARD. OPERATIONALLY CHECKED GEAR, GEAR CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998021100908 19980211 00908 NM 1998 2 11 98UAL900034 1 19980125 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 CEILING EMERGENCY EXIT SIGN BETWEEN FORWARD DOORS IS INOPERATIVE. *S/D* REPLACED FAILED BATTERY. 2 L 7 3 4F 4 F A3WE E2EA 1998021100909 19980211 00909 1998 2 11 98UAL900037 4 19980128 A 2312 6221181003 VHF TRANS BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE E/E COMPT FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 9065U 19946 LOST COMM ON FREQUENCY 127.8 MHZ ON NUMBER ONE VHF. COMM APPEARED WEEK ON OTHER FREQUENCIES AS WELL. *S/D* REPLACED N R 1 VHF COMM TRANSCEIVER, OP CHECKED GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1998021100910 19980211 00910 NM 1998 2 11 98UAL900042 1 19980129 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 176UA 24383 LEFT HALF OF CROSS ASILE 4 AND SEVERAL ROWS AFT ON RIGHT SIDE EEL LIGHTS INOP. REPLACED LEFT HALF OF CROSS ASILE EEL LI GHT STRIP, OPS CK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 1998021100911 19980211 00911 NM 1998 2 11 98UAL900043 1 19980131 A 2721 ACTUATOR MPC PRODUCTS U26B BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RUDDER TRIM FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 335UA 24230 RUDDER TRIM CIRCUIT BREAKER POPPED AND WOULD NOT RESET. RUDDER TRIM WAS INOPERABLE. *S/D* REPLACED RUDDER TRIM ACTUAT OR, SYSTEM OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998021100912 19980211 00912 GL 1998 2 11 98UAL900044 2 19980130 A 7313 9022M16G25 NOZZLE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE CRACKED A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 1837U 2954 47969 451453 NR 2 ENGINE HAS VIBRATION AND HUM THAT FOLLOWED THE THROTTLE. ENGINE REDUCED TO IDLE POWER AND DIVERTED TO LAS. *S/D* PRIMARY CAUSE OF ENGINE FAILURE WAS THE CRACKING OF THE HIGH PRESSURE TURBINE STAGE 1 NOZZLE. ON SEVERAL ADJACENT NOZZ LES, THE CRACKS WRAPPED AROUND THE AIRFOIL LEADING EDGE NEAR THE OUTER PLATFORMS. THIS ALLOWED THE INNER PLATFORMS TO M OVE AFT AND CONTACT THE LEADING EDGE INNER RADIUS OF THE STAGE 2 BLADE LEADING EDGES. SEPARATION OF A BLADE EVENTUALLY OCCURRED. OUR VENDOR, GE-ONTARIO, WILL NO LONGER ALLOW INSTALLATION OF T-2 NOZZLES WHICH HAVE RECEIVED MORE THAN 3 REPA IRS. 2 L 7 3 4F 4 F A22WE E23EA 1998021100913 19980211 00913 EU 1998 2 11 98UAL900045 1 19980202 A 3222 433343008964 SEAL AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG STRUT DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 409UA 462 NOSE LANDING GEAR FAILED TO RETRACT. *S/D* NLG SHOCK ABSORBER WAS UNDER SERVICED RESULTING IN A PARTIAL COMPRESSION NE AR END OF RETRACTION CYCLE. THIS ACTION CAUSED THE S/A EXTENDED PROXIMITY SENSORS TO MOVE OUT OF POSITION RESULTING IN THE LGCIU COMMANDING THE NOSE GEAR TO EXTEND. REPLACED SHOCK ABSORBER AND FOUND DYNAMIC SEAL DAMAGED FOLLOWING DISASSEM BLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1998021100914 19980211 00914 NE 1998 2 11 98UAL900046 2 19980205 A 7261 1B3725 OIL LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE BLOCKED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS CR CRUISE 1 WP 29 534UA 25129 NUMBER 2 ENGINE OIL QUANTITY DROPPED, OIL PRESSURE FLUCTUATED AND DROPPED TO 100 PSI. CREW SHUT DOWN ENGINE. *S/D* OI L LOSS WAS DUE TO EXCESSIVE CARBON IN THE NR 5 BEARING OIL SCAVENGE LINE. THE NR 5 BEARING OIL NOZZLE WAS BLOCKED BECAU SE THE LAST CHANCE FILTER IN THE OIL SUPPLY LINE WAS MISSED. IN THE FUTURE, INSPECTION OF THE LAST CHANCE FILTER WILL B E PERFORMED. ALSO, ADDITIONAL EXHAUST DUCT MAINTENANCE TO CLEAN OUT CARBON DEPOSITS HAS BEEN IMPLEMENTED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998021100915 19980211 00915 NM 1998 2 11 98UAL900047 1 19980204 A 3350 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7450U 21904 EMERGENCY EXIT SIGN AT FWD GALLEY DOOR INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1998021100999 19980211 00999 NM 1998 2 11 DL72S980350 1 19980109 A 3350 BR9279108 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 420DA 21273 FWD OVERWING EMERG EXIT SIGN, LOWER INOP. FOUND ON NR 2 L/O. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1998021800002 19980218 00002 WP 1998 2 18 CKSA98007 1 19980118 A 3350 5708458505 BATTERY PACK DOUG DC8 DC8F54 3021926 WP CABIN DISCHARGED A CKSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 8052U 46009 SMELLED SMOKE AND FOUND EMERGENCY LIGHT CHARGER C/B OPENED. TRACED SMOKE AND OPENED PANEL FOR BATTERY CHARGER FOR EMERG ENCY LIGHTS. PANEL SCREWS IN F/E DRAWER. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECKED NORMAL IAW DC8 MM 33 -31-1. 2 L 7 4 4F 4A25 1998021800007 19980218 00007 NM 1998 2 18 98ZZZX656 1 19980118 A 6310 900D1400528101 INPUT PINION DOUG MD900 MD900 3027375 NM M/R DRIVE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 261 0062190072 90000012 INPUT PINION ASSY LEAKING OIL BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998021800012 19980218 00012 WP 1998 2 18 DLL17980309 1 19980204 A 2612 FIRE LOOP LKHEED 1011 10113853 5265020 WP PWA PW4077 PW4077 NE NR 2 ENGINE CONTAMINATED A DALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 27 769DL 61086 193H1218 NR 2 ENG SHUT DOWN DUE TO ENG FIRE INDICATION. BOTH FIRE BOTTLES FIRED. FOUND BAD CONNECTORS ON THE GEAR CASE B-FIRE L OOP AND CONTAMINATED CONNECTOR ON A LOOP. 2 L 7 3 4F 4 F A23WE E46NE 1998021900020 19980219 00020 EU 1998 2 19 HEEA0012760 1 19980205 A 2500 AS2224 CONTROL SNIAS 350 AS350B2 8680813 EU CARGO MECH CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 4980 2771 CARGO CONTROL MECHANISM CORRODED HOUSING AND RUSTED CABLE. 1 G 7 1 3U H9EU 1998021900021 19980219 00021 SW 1998 2 19 HEEA0012791 1 19980205 A 7930 174035201 INDICATOR 174000103 BELL 206 206L3 1182108 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 363BH 3981 51345 ENG OIL INDICATOR INOPERATIVE-DOES NOT WORK. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998021900022 19980219 00022 SW 1998 2 19 HEEA0012792 1 19980205 A 7930 174035201 INDICATOR 174000103 BELL 206 206L3 1182108 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6610E 4168 51424 ENG OIL INDICATOR INOPERATIVE-DOES NOT WORK. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998021900023 19980219 00023 1998 2 19 HEEA0012793 4 19980205 A 2312 064101900 TRANSCEIVER KY196 BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21431 3452 TRANSCEIVER RECEIVES BUT DOES NOT TRANSMIT. 1 G 7 1 3U H2SW 1998021900024 19980219 00024 GL 1998 2 19 HEEA0012794 2 19980205 A 7314 3881005 FUEL PUMP BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG FUEL PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3892R 12284 45594 CAE860059 FOUND FUEL PUMP WITH PITTED DRIVE SPLINES AND GEARS. 1 G 7 1 3U 3 U H2SW E1GL 1998021900025 19980219 00025 SW 1998 2 19 HEEA0012795 1 19980205 A 6220 412010156113 SPINDLE BELL 412 412 1182202 SW M/R SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 4006 33005 BEARING SEPARATED FROM SPINDLE. 1 G 7 2 4U H4SW 1998021900026 19980219 00026 SW 1998 2 19 HEEA0012796 1 19980205 A 5610 P21207602 WINDOW BELL 412 412 1182202 SW RT CHIN BUBBLE MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 WINDOW DOES NOT FIT CONTOUR OF AIRCRAFT. WONT LOCATE WINDOW PROPERLY (DIFFERENCE IS TOO MUCH TO ALLOW) NOTE: TOP FORW ARD CORNER IS THE PROBLEM AREA. 1 G 7 2 4U H4SW 1998021900027 19980219 00027 1998 2 19 HEEA0012797 4 19980205 A 3453 4530103 LORAN ARNAV21 BELL 206 206L1 1182107 SW COCKPIT INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 45291 LORAN KEYPAD ASSY. INOPERATIVE AND ENVELOPE NUMBER SHOWING BLANK. 1 G 7 1 3U H2SW 1998021900028 19980219 00028 SW 1998 2 19 HEEA0012798 1 19980205 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS FAILED E HEEA K NONE H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 SW 03 1202T 33112 INVERTER WILL NOT COME ON LINE. 1 G 7 2 4U H4SW 1998021900029 19980219 00029 1998 2 19 HEEA0012799 4 19980205 A 3453 066402600 LORAN KLN88 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 KLN88 NO DISPLAY. 1 G 7 2 3U H3EU 1998021900030 19980219 00030 1998 2 19 HEEA0012800 4 19980205 A 3454 066107800 RECEIVER BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 VOR INOPERATIVE. 1 G 7 2 4U H4SW 1998021900031 19980219 00031 SW 1998 2 19 HEEA0012801 1 19980205 A 5321 206031313159A PANEL BELL 206 206L1 1182107 SW FLOOR MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 PANEL HOLES FOR DRAIN LINES MISPLACED. 1 G 7 1 3U H2SW 1998021900033 19980219 00033 1998 2 19 HEEA0012803 4 19980205 A 3453 071143100 ANTENNA KT83 BELL 206 206L1 1182107 SW LORAN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2759U 45267 LORAN LOSES SIGNAL. UNIT HAS PREVIOUS WRITE UPS FOR THIS COMPLAINT. 1 G 7 1 3U H2SW 1998021900034 19980219 00034 1998 2 19 HEEA0012804 4 19980205 A 3455 066107200 RECEIVER KR87 BOLKMS 105 BO105S 5626006 EU ADF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 818SH S753 NO LCD DISPLAY, AUDIO WEAK. 1 G 7 2 3U H3EU 1998021900035 19980219 00035 1998 2 19 HEEA0012805 4 19980205 A 3454 066107810 RECEIVER KNR634A SKRSKY S76 S76A 8143006 NE VOR INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 VOR INOPERATIVE. BENCH CHECK REQUIRED. 1 G 7 2 3U H1NE 1998021900036 19980219 00036 1998 2 19 HEEA0012806 4 19980205 A 2210 7683431 POTENTIOMETER 769000180210 SKRSKY S76 S76A 8143006 NE AFCS INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 292 81077521 INOPERATIVE. INSPECTED WHEN RECEIVED AND FOUND ONE EACH POTENTIOMETER TO HAVE OPEN SPOT IN NULL POSITION, ALSO FOUND ON E EACH POTENTIOMETER TO READ 0 VOLTS ON TEST. SENT TO H 1 G 7 2 3U H1NE 1998021900037 19980219 00037 1998 2 19 HEEA0012808 4 19980205 A 2312 40008310103 TRANSCEIVER RT14 BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 POPS CIRCUIT BREAKER AND SHOWS RT FAULT ON INDICATOR. 2 G 7 2 4U H10SW 1998021900038 19980219 00038 1998 2 19 HEEA0012809 4 19980205 A 2312 40008310105 TRANSCEIVER RT14 BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 GAIN TOO HIGH ON LOW RANGES. 2 G 7 2 4U H10SW 1998021900039 19980219 00039 1998 2 19 HEEA0012812 4 19980205 A 2211 4025008918 COMPUTER BELL 412 412 1182202 SW AFCS MALFUNCTION E HEEA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 3893P 33012 COMPUTER KICKING IN FLIGHT. 1 G 7 2 4U H4SW 1998021900040 19980219 00040 SW 1998 2 19 HEEA0012813 1 19980205 A 6320 222342420101 BEARING 209040173103 BELL 214 214ST 1182106 SW M/R GRBOX PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N A653 28106 BEARING PITTED. REPLACED WITH SERVICEABLE BEARING. 2 G 7 2 4U H10SW 1998021900041 19980219 00041 SW 1998 2 19 HEEA0012814 1 19980205 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 55 36005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998021900042 19980219 00042 SW 1998 2 19 HEEA0012815 1 19980205 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 16 36005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998021900043 19980219 00043 SW 1998 2 19 HEEA0012816 1 19980205 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W 45386 GENERATOR DOES NOT COME ON. REG FAILED 1 G 7 1 3U H2SW 1998021900044 19980219 00044 SW 1998 2 19 HEEA0012817 1 19980205 A 2436 163404731 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W 45386 VOLT REG NOT WORKING. GENERATOR WILL NOT COME ON LINE. 1 G 7 1 3U H2SW 1998021900045 19980219 00045 1998 2 19 HEEA0012818 4 19980205 A 3413 RC30VIL INDICATOR SKRSKY S76 S76A 8143006 NE VERT SPEED LEAKAGE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 RATE OF CLIMB INDICATOR CASE LEAKAGE. 1 G 7 2 3U H1NE 1998021900046 19980219 00046 1998 2 19 HEEA0012819 4 19980205 A 3416 59341 ALTIMETER BELL 206 206B3 1181506 SW COCKPIT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39122 3312 ALTIMETER CASE LEAKAGE AND CORROSION ON BARO KNOB. 1 G 7 1 3U H2SW 1998021900047 19980219 00047 1998 2 19 HEEA0012820 4 19980205 A 2210 2593996444 TARSYN BELL 412 412 1182202 SW AUTOFLIGHT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 TARSYS KICKS IN PITCH. 1 G 7 2 4U H4SW 1998021900048 19980219 00048 SW 1998 2 19 HEEA0012821 1 19980205 A 7931 206075187003 INDICATOR BELL 206 206L1 1182107 SW ENG OIL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251A 45755 INDICATES 5 PSI HIGH AT 100 PSI. 1 G 7 1 3U H2SW 1998021900049 19980219 00049 NE 1998 2 19 HEEA0012822 1 19980205 A 7714 7645001076101 TACH SKRSKY S76 S76A 8143006 NE GAS GEN INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 GAS GEN TACH NEEDLE AND DIGITS INOPERATIVE. 1 G 7 2 3U H1NE 1998021900050 19980219 00050 EU 1998 2 19 HEEA0012823 1 19980205 A 7921 3701020000 COOLER BOLKMS 105 BO105S 5626006 EU OIL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 721MB S752 LUBE COOLER LEAKING. 1 G 7 2 3U H3EU 1998021900051 19980219 00051 SW 1998 2 19 HEEA0012824 1 19980205 A 7931 206075188005 INDICATOR BELL 206 206L1 1182107 SW ENG OIL FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 45291 FLUCTUATES 5 PSI WHEN UNIT IS VIBRATED. 1 G 7 1 3U H2SW 1998021900052 19980219 00052 EU 1998 2 19 HEEA0012825 1 19980205 A 3340 A413AHDADF28V POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4302G S853 POWER SUPPLY INOPERATIVE. 1 G 7 2 3U H3EU 1998021900053 19980219 00053 SW 1998 2 19 HEEA0012826 1 19980205 A 3340 A490A POWER SUPPLY BELL 206 206L1 1182107 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1077A 45382 POWER SUPPLY VERY LOW OUTPUT. 1 G 7 1 3U H2SW 1998021900054 19980219 00054 SW 1998 2 19 HEEA0012827 1 19980205 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 155 33005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998021900055 19980219 00055 SW 1998 2 19 HEEA0012828 1 19980205 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW FLT CONT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 ROTARY ACTUATOR FORCE TRIM STICKS. 1 G 7 2 4U H4SW 1998021900056 19980219 00056 SW 1998 2 19 HEEA0012829 1 19980205 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 101 36005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998021900057 19980219 00057 SW 1998 2 19 HEEA0012830 1 19980205 A 6330 206033518007 STOP ASSY BELL 206 206L1 1182107 SW XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5745S 45491 STOP ASSY RUBBER GASKET WORN. 1 G 7 1 3U H2SW 1998021900058 19980219 00058 SW 1998 2 19 HEEA0012831 1 19980205 A 2820 206063640101 VALVE BELL 206 206L1 1182107 SW FUEL SYS STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W 45386 VALVE STICKS IN OPEN AND CLOSE POSITIONS. 1 G 7 1 3U H2SW 1998021900059 19980219 00059 SW 1998 2 19 HEEA0012832 1 19980205 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW M/R CONTROL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2775A 45297 ACTUATOR WILL NOT ADJUST TO LESS THAN 10% RANGE. 1 G 7 1 3U H2SW 1998021900060 19980219 00060 NE 1998 2 19 HEEA0012833 1 19980205 A 2840 23356 SWITCH SKRSKY S76 S76A 8143006 NE FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 LOW FUEL PRESSURE WILL NOT TURN ON MASTER CAUTION LIGHT. 1 G 7 2 3U H1NE 1998021900061 19980219 00061 SW 1998 2 19 HEEA0012834 1 19980205 A 7810 206064300005 EXHAUST ASSY BELL 206 206L1 1182107 SW ENG EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50182 45242 EXH ASSY CRACKED. EXCESSIVE LEAKAGE. 1 G 7 1 3U H2SW 1998021900062 19980219 00062 SW 1998 2 19 HEEA0012835 1 19980205 A 2436 206075447007 VOLT REGULATOR BELL 206 206L3 1182108 SW DC SYS FAILED E HEEA K NONE H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SW 03 979BH 51403 REG DROPPED OFF LINE AND WOULD NOT RESET. 1 G 7 1 3U H2SW 1998021900063 19980219 00063 1998 2 19 HEEA0012836 4 19980205 A 3416 D120P2T ANEROID BELL 206 206L3 1182108 SW ENCODER LEAKAGE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 210PH 51541 BARO ANEROID EXCESSIVE LEAKAGE AND ENCODER HAS ERRATIC READINGS. 1 G 7 1 3U H2SW 1998021900064 19980219 00064 NE 1998 2 19 HEEA0012837 1 19980205 A 6210 SB7004103 BEARING SKRSKY S76 S76A 8143006 NE M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 RUBBER EXTRUSION BEYOND LIMITS. 1 G 7 2 3U H1NE 1998021900065 19980219 00065 1998 2 19 HEEA0012838 4 19980205 A 3423 KCA0105W COMPASS BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 135AE S838 MAG COMPASS DOES NOT COMPENSATE. 1 G 7 2 3U H3EU 1998021900066 19980219 00066 1998 2 19 HEEA0012839 4 19980205 A 3423 KCA0105W COMPASS BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 S677 MAG COMPASS LEAKING. 1 G 7 2 3U H3EU 1998021900067 19980219 00067 1998 2 19 HEEA0012840 4 19980205 A 3423 KCA0105W COMPASS BOLKMS 117 BK117B2 5626013 EU COCKPIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 134AE 7237 MAG COMPASS FLUID LEAKING. 1 G 7 2 3U NC H13EU 1998021900068 19980219 00068 1998 2 19 HEEA0012841 4 19980205 A 3453 071143100 ANTENNA KA83 BELL 206 206L3 1182108 SW LORAN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41791 51465 ANTENNA WILL NOT PICK UP SIGNAL. INTERMITTENT. 1 G 7 1 3U H2SW 1998021900069 19980219 00069 1998 2 19 HEEA0012842 4 19980205 A 2210 7000299901 CONTROL BELL 412 412 1182202 SW AUTOPILOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 AUTOPILOT CONTROL INOPERATIVE. SMELLS BURNT. BROKEN LENS IN FRONT. 1 G 7 2 4U H4SW 1998021900071 19980219 00071 1998 2 19 HEEA0012846 4 19980205 A 3416 066030640001 ENCODER BELL 412 412 1182202 SW ALTIMETER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 ENCODER INDICATES HIGH OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998021900072 19980219 00072 SW 1998 2 19 HEEA0012847 1 19980205 A 2120 212073927003 CONTROLLER BELL 212 212 1181420 SW SERVO FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736D 31135 SERVO CONTROLLER INOPERATIVE. 1 G 7 1 4U H4SW 1998021900073 19980219 00073 SW 1998 2 19 HEEA0012848 1 19980205 A 7931 214060057103 SWITCH BELL 214 214ST 1182106 SW OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 SWITCH INOPERATIVE. 2 G 7 2 4U H10SW 1998021900074 19980219 00074 EU 1998 2 19 HEEA0012849 1 19980205 A 2844 BSE20660G1 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 91070 S145 PRESSURE DROPS TO ZERO. 1 G 7 2 3U H3EU 1998021900075 19980219 00075 SW 1998 2 19 HEEA0012850 1 19980205 A 6710 206062721113 ACTUATOR BELL 206 206B3 1181506 SW M/R CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2269A 3608 ACTUATOR MOTOR WILL NOT RUN. 1 G 7 1 3U H2SW 1998021900076 19980219 00076 SW 1998 2 19 HEEA0012851 1 19980205 A 6240 214074280105 DETECTOR BELL 214 214ST 1182106 SW ROTOR RPM FAILED E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 5748M 28102 ROTOR RPM LIGHT WILL NOT COME ON. 2 G 7 2 4U H10SW 1998021900077 19980219 00077 SW 1998 2 19 HEEA0012852 1 19980206 A 7714 214074280105 DETECTOR BELL 214 214ST 1182106 SW ENG RPM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 NR1 GAUGE INOPERATIVE. NR1 ENGINE OUT LIGHT FLICKERS. 2 G 7 2 4U H10SW 1998021900078 19980219 00078 SW 1998 2 19 HEEA0012853 1 19980206 A 2120 212073927003 CONTROLLER BELL 412 412 1182202 SW SERVO DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 SERVO CONTROLLER ROTATES PAST STOPS IN BOTH DIRECTIONS. 1 G 7 2 4U H4SW 1998021900079 19980219 00079 NE 1998 2 19 HEEA0012854 1 19980206 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 M/R DAMPER WEAK. 1 G 7 2 3U H1NE 1998021900080 19980219 00080 EU 1998 2 19 HEEA0012855 1 19980206 A 7722 50061051 INDICATOR BOLKMS 105 BO105S 5626006 EU ENG EGT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911FL S717 SEVERE FRICTION - CANNOT CALIBRATE. 1 G 7 2 3U H3EU 1998021900081 19980219 00081 SW 1998 2 19 HEEA0012856 1 19980206 A 2913 206076030101 PUMP BELL 206 206L3 1182108 SW HYD SYS DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 49EA 51507 SHAFT BENT AND UNABLE TO REMOVE SHAFT. 1 G 7 1 3U H2SW 1998021900082 19980219 00082 SW 1998 2 19 HEEA0012857 1 19980206 A 7722 3030083 TRIM COMPENSATOR BELL 412 412 1182202 SW ENG ITT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 ITT ERRATIC AND FLICKERS. 1 G 7 2 4U H4SW 1998021900083 19980219 00083 SW 1998 2 19 HEEA0012858 1 19980206 A 2810 206061661101 FUEL CELL BELL 206 206B3 1181506 SW FUEL SYS UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2270G 3610 FUEL CELL PEELING, UNBONDED FLANGES, MISSING HANGERS, CORROSION, BLISTERS ON INSIDE OF CELL. 1 G 7 1 3U H2SW 1998021900084 19980219 00084 1998 2 19 HEEA0012860 4 19980206 A 2211 7004206901 COMPUTER BOLKMS 117 BK117B2 5626013 EU CSAS DEFECTIVE E HEEA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 134AE 7237 CSAS COMPUTER DEFECTIVE. CONTROL KICKS IN FLIGHT. 1 G 7 2 3U NC H13EU 1998021900085 19980219 00085 EU 1998 2 19 HEEA0012861 1 19980206 A 6240 KDW021 WARNING BOX BOLKMS 105 BO105S 5626006 EU ROTOR RPM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911DD S830 RPM WARN BOX CAUSES INTERMITTENT RPM LIGHT TO ILLUMINATE WHEN AT 100 PERCENT. 1 G 7 2 3U H3EU 1998021900086 19980219 00086 NE 1998 2 19 HEEA0012862 1 19980206 A 2421 7655009005105 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 A/C WILL NOT COME ON LINE DUE TO GENERATOR FAILED. 1 G 7 2 3U H1NE 1998021900087 19980219 00087 1998 2 19 HEEA0012863 4 19980206 A 3422 2891ESR DIRECTION GYRO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5019G 45247 DIR GYRO WILL NOT SLAVE. 1 G 7 1 3U H2SW 1998021900088 19980219 00088 1998 2 19 HEEA0012864 4 19980206 A 3421 501145301 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE AUTOPILOT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 ATTITUDE INDICATOR ERRATIC AND UNRELIABLE. AUTOPILOT VERT GYRO MALFUNCTION 1 G 7 2 3U H1NE 1998021900089 19980219 00089 1998 2 19 HEEA0012865 4 19980206 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE AUTOPILOT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 186 760077 VERT GYRO KICK IN PITCH SYSTEM. 1 G 7 2 3U H1NE 1998021900090 19980219 00090 1998 2 19 HEEA0012866 4 19980206 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE PILOT ATTITUDE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 PILOT'S ATTITUDE INDICATOR PRECESSES. 1 G 7 2 3U H1NE 1998021900091 19980219 00091 EU 1998 2 19 HEEA0012867 1 19980206 A 7714 4011001 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724MB S756 TRIPLE INDICATOR ROTOR NEEDLE READS HIGH. UNIT OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1998021900092 19980219 00092 NE 1998 2 19 HEEA0012868 1 19980206 A 7334 7645001078119 TRANSMITTER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL FUEL PRESS LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 PRESSURE TRANSMITTER LEAKING OIL INTO ELECTRICAL CONNECTOR. 1 G 7 2 3U 3 U H1NE E1GL 1998021900093 19980219 00093 EU 1998 2 19 HEEA0012869 1 19980206 A 5321 350A21135921 FLOOR SNIAS 350 AS350B2 8680813 EU RT CABIN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 2427 2777 CORRODED. SCRAPPED AT PHI. 1 G 7 1 3U H9EU 1998021900094 19980219 00094 EU 1998 2 19 HEEA0012870 1 19980206 A 6330 579063 BEARING SNIAS 350 AS350B2 8680813 EU M/R MOUNT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 2777 LAMINATED BEARING DEFECTIVE. SCRAPPED AT PHI. 1 G 7 1 3U H9EU 1998021900151 19980219 00151 EA 1998 2 19 98ZZZX732 1 19980128 A 5610 6003303019 WINDSHIELD CNDAIR CL600 CL6002A12 1900304 EA LT OUTER PANE CRACKED A L N9WA B EMER. DESCENT O OTHER CR CRUISE 1 EA 11 1824T 3071 3029 DURING CRUISE AT FL 390 THREE HOURS INTO THE FLIGHT, THE LEFT OUTER WINDSCREEN CRACKED. THE CREW DECIDED TO DESCEND TO FL 310. APPROXIMATELY 30 MINUTES LATER, THE LT PANE CRACKED A SECOND TIME. THE CREW ELECTED TO DESCEND TO 10,000 FEET. AS A PRECAUTIONARY MEASURE, AN EMERGENCY WAS DECLARED WITH THE TOWER. THE ACFT CONTINUED TO DALLAS AT REDUCED SPEED. LANDED AT KDAL AT 0018Z (0122-98) WITHOUT INCIDENT. UPON EXAMINATION AT DALLAS, THE OUTER PANE OF THE WINDSCREEN WAS M ISSING APPROXIMATELY 25 PERCENT OF THE OUTER PLY SURFACE AREA. TC: 1,718. 2 L 7 2 4F RT A21EA 1998021900260 19980219 00260 NE 1998 2 19 HEEA0012807 1 19980205 A 7600 7630103902102 ACTUATOR SKRSKY S76 S76A 8143006 NE TURB CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 ACTUATOR WAS STIFF AND MOVED VERY SLOW. THEN SHAFT MOVED FREELY FOR A SHORT TIME. NOW SHAFT DOES NOT MOVE AT ALL. 1 G 7 2 3U H1NE 1998021900261 19980219 00261 1998 2 19 HEEA0012810 4 19980205 A 3442 40005040301 DRIVE ASSY BELL 214 214ST 1182106 SW RADAR ANT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 ANT DRIVE ASSY FAILED. CAUSES LARGE RED BAND ON SCREEN DURING TURNS AND ROLL INOPERATIVE. 2 G 7 2 4U H10SW 1998021900262 19980219 00262 NE 1998 2 19 HEEA0012843 1 19980205 A 6710 7640002000041 DAMPENER SKRSKY S76 S76A 8143006 NE COLLECTIVE DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 911MJ 760231 THROW OF COLLECTIVE DAMPER NOT SAME AS ONE REMOVED. 1 G 7 2 3U H1NE 1998021900263 19980219 00263 NE 1998 2 19 HEEA0012844 1 19980205 A 6710 7640002000041 DAMPENER SKRSKY S76 S76A 8143006 NE COLLECTIVE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 BEARING FILL OUT. COLLECTIVE DAMPER ASSY. WEAK AND RATCHETY. 1 G 7 2 3U H1NE 1998021900264 19980219 00264 NE 1998 2 19 HEEA0012859 1 19980206 A 7930 7645001078120 TRANSMITTER SKRSKY S76 S76A 8143006 NE ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ENG OIL TRANSMITTER TRANSMITS HIGH OUT OF TOLERANCE. 1 G 7 2 3U H1NE 1998021900265 19980219 00265 WP 1998 2 19 VJ9800008 1 19980206 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP NLG DIRTY A VJ6A O OTHER N FALSE WARNING AP APPROACH 1 SO 11 924VV 47278 ON FINAL APPROACH, NO GREEN LIGHT OBTAINED FOR NOSE GEAR BEING DOWN AND LOCKED IN POSITION. RECYCLED GEAR AND RECEIVED CONFIRMATION WITH 3 GREEN LIGHTS THAT GEAR WAS DOWN AND LOCKED. CLEANED AND CYCLED NOSE GEAR POSITION SWITCH. OPS CHEC KED NORMAL IAW MM 32-60. 2 L 7 2 4F A6WE 1998021900266 19980219 00266 NM 1998 2 19 AWXA9800027 1 19980117 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 186AW 22653 'D' EMERG LIGHT INOP AT SEAT 18C. RELAMPED, NO HELP ON 'C'. REPAIRED WIRING, OPS OKSTC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998021900267 19980219 00267 EU 1998 2 19 AWXA9800031 1 19980119 A 3350 FUSE AIRBUS 320 A320231 3930325 EU CABIN BLOWN A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 622AW 054 OVERWING EXIT HANDLE COVER LIGHTS DO NOT WORK. A/C RT FWD AND AFT RELAMP, NO HELP. REPLACED FUSE ON EMERGENCY LIGHT PW R PACK. 2 L 7 2 4F RT A28NM 1998021900268 19980219 00268 EU 1998 2 19 AWXA9800032 1 19980119 A 3350 CONNECTOR AIRBUS 320 A320231 3930325 EU CABIN BROKEN A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 622AW 054 INTERIOR EMERGENCY AISLE LIGHT INOP AT SEAT ROW 15. REPAIRED CONNECTOR AT ROW 15 WALL DISCONNECT, OPS OK. 2 L 7 2 4F RT A28NM 1998021900269 19980219 00269 NM 1998 2 19 AWXA9800034 1 19980122 A 3350 1060091101 LIGHT BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 179AW 22646 'D' L2 FWD EMERGENCY LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY F/C GOODSTC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998021900270 19980219 00270 NM 1998 2 19 AWXA9800035 1 19980122 A 3397 WIRE BOEING 737 7373B7 1384580 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 328AW 23377 'D FLOOR TRACK EMERG LIGHT AT ROW 4 INOP. REPAIRED WIRE AT ROW 4 SYSTEM, OPS CHECK GOOD STC NR SA1889SO. 2 L 7 2 4F RT A16WE 1998021900271 19980219 00271 EU 1998 2 19 AWXA9800036 1 19980122 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A AWXA K NONE L NO TEST UK UNKNOWN 1 WP 28 640AW 448 FWD LT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSY, OPS CHECK NORMAL. 2 L 7 2 4F RT A28NM 1998021900272 19980219 00272 NM 1998 2 19 AWXA9800037 1 19980127 A 3350 864705 POWER SUPPLY BOEING 737 7372U9 1384498 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 'D' EMERGENCY EXIT LIGHT BESIDE R1 AND L1 DOORS AND FIRST CLASS OVHD EXIT LIGHTS ARE ALL INOP. REMOVED AND REPLACED EME RGENCY LT PWR SUPPLY IN FIRST CLASS OVERHEAD, OPS CHECKS GOOD. STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998021900273 19980219 00273 NM 1998 2 19 AWXA9800038 1 19980128 A 3397 WIRE BOEING 757 757225 1384959 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 914AW 22208 DURING ROUTINE MAINTENANCE CHECK, FOUND FLOOR PROX EMERGENCY LIGHT ROW 19 INOP. RESPLICED WIRE. OPS CHECK GOOD. STC S A3143NM. 2 L 7 2 4F RT A2NM 1998021900274 19980219 00274 NM 1998 2 19 AWXA9800039 1 19980129 A 3397 WIRE BOEING 737 7373Y0 1384671 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 323AW 23684 EMERGENCY LIGHT AT ROW 12L IS INOP. REPAIRED WIRE, OPS CK GOOD. STC SA3140NM. 2 L 7 2 4F RT A16WE 1998021900275 19980219 00275 NM 1998 2 19 AWXA9800040 1 19980102 A 3350 831136 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 157AW 23779 'D' ROW 6 EMERGENCY EXIT LIGHT INOP. INSTALLED NEW ASSEMBLY, OPS CHECK NORMAL. STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998021900276 19980219 00276 NM 1998 2 19 AWXA9800041 1 19980203 A 3397 WIRE BOEING 737 7373G7 1384595 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 160AW 23782 'D' EMERGENCY LIGHT AT ROW 1 INOP. REPAIRED WIRE AT ROW NR 1 EMERGENCY LIGHT. OPS CHECK GOOD. STC SA3432NM. 2 L 7 2 4F RT A16WE 1998021900277 19980219 00277 EU 1998 2 19 AWXA9800043 1 19980208 A 2910 HYD SYST AIRBUS 320 A320231 3930325 EU GREEN HYD SYST REQD SERVICE A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 WP 28 631AW 077 LOST HYD PRESSURE AND FLUID FROM GREEN SYSTEM, FLUID LEVEL CAME BACK AFTER LANDING, TO ABOUT HALF FULL. INSPECTED A/C F OR LEAKS, NONE FOUND. SERVICED GREEN SYSTEM, 5 QUARTS, RAN ENGINES, ALL HYD SYSTEMS, PRESSURE AND FLUID LEVEL INDICATES NORMAL. A/C OK FOR SERVICE. 2 L 7 2 4F RT A28NM 1998021900278 19980219 00278 SW 1998 2 19 PNSA980102 1 19980120 A 3244 TIRE SWRNGN SA227 SA227AC 8780603 SW NR 3 MAIN FLAT A PNSA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 650PA 695 AC775B AFTER SHUTDOWN IN KSM, IT WAS NOTED THAT NR 3 MAIN TIRE WAS FLAT. REPLACED WHEEL/TIRE ASSY. 2 L 7 2 4T RT A8SW 1998021900279 19980219 00279 1998 2 19 PNSA980103 4 19980107 A 3421 G519A1 GYRO CESSNA 208 208 2073702 CE COCKPIT FAILED A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 9530F 20800088 ATTITUDE GYRO VERY SLOW TO ERECT. REPLACED GYRO, OPS CHECK OK. 1 H 7 1 3T NT A37CE 1998021900280 19980219 00280 WP 1998 2 19 PNSA980104 2 19980102 A 7412 30703782 EXCITER BOX SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE INOPERATIVE A PNSA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 650PA 7191 AC775B LT ENGINE WOULD NOT START, REPLACED IGNITION EXCITER BOX. OPS CHECK OK. 2 L 7 2 4T 4 T RT A8SW E4WE 1998021900281 19980219 00281 EU 1998 2 19 PNSA980105 1 19980123 A 3244 TIRE SAAB SF340 340B 7860101 EU NR 1 MAIN FLAT A PNSA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 675PA 839 206 NR 1 MAIN TIRE FLAT REPLACED WHEEL ASSY. 2 L 7 2 4T RT A52EU 1998021900282 19980219 00282 WP 1998 2 19 CALA9800206 1 19980210 A 2612 ASL0388501 FIRE DETECTOR DOUG DC10 DC1030 3023501 WP NR 2 ENGINE CHAFED A CALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 09 59083 47926 THE NR 2 ENGINE A FIRE LOOP DETECTOR LIGHT BEGAN TO FLICKER WHILE IN CRUISE FLIGHT FROM LGW TO EWR. WHEN THE NR 2 ENGIN E THRUST WAS REDUCED THE FLICKERING STOPPED. WHEN THRUST WAS ADDED THE FLICKERING RESUMED. THE NR 2 ENGINE WAS OPERATE D WITH PARTIAL THRUST, FUEL WAS DUMPED, AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENA NCE FOUND BROKEN CLAMPS AND LOOPS A AND B WERE CHAFING. THE NR 2 ENGINE LOWER CORE DETECTOR ASSEMBLY WAS REMOVED AND RE PLACED. THE NR 2 ENGINE FIRE DETECTION SYSTEM CHECKED GOOD. 2 L 7 3 4F A22WE 1998021900283 19980219 00283 NE 1998 2 19 CALA9800207 2 19980209 A 7530 728624 SENSE LINE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7F 52054 NE NR 2 ENGINE CRACKED A CALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 09 14024 20534 689566 THE NR 2 ENGINE LOST PARTIAL POWER WHILE IN CRUISE FLIGHT FROM HNL TO NRT. THE EPR DROPPED FROM 1.40 TO 1.13 AND N1 DRO PPED FROM 95 PERCENT TO 85 PERCENT. THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOU ND THE NR 2 ENGINE PS4 LINE TO THE 3.5 BLEED CONTROLLER CRACKED. THE LINE WAS REMOVED AND REPLACED IAW MM 75-31-14. A POWER ASSURANCE RUN CHECKED GOOD. 2 L 7 4 4F 4 F A20WE E20EA 1998021900284 19980219 00284 WP 1998 2 19 CALA9800208 1 19980206 A 3610 9057M84G02 DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE SEPARATED A A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14075 46922 517327 THE NR 1 ENGINE HAD A FIRE WARNING AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INC IDENT. INITIAL FINDINGS REVEALED NR 1 ENGINE 14TH STAGE DUCT SEPARATION. THE AIRCRAFT WAS TAKEN OUT OF SERVICE FOR REP AIR. THE 14TH STAGE DUCT WAS REMOVED AND REPLACED. IN ADDITION, THE ENGINE WAS BOROSCOPED DUE TO HIGH EGT EXPERIENCED AND NO DAMAGE WAS FOUND. AN ENGINE RUN WAS PERFORMED AND OPERATION CHECKED GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1998021900285 19980219 00285 WP 1998 2 19 9802329152 1 19980207 A 3350 6014113 POWER SUPPLY DOUG DC9 DC914 3022034 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING INSPECTION, THE EMERGENCY FLOOR PROXIMITY LIGHTS LOCATED IN FIRST CLASS SECTION WERE FOUND TO BE INOPERATIVE. MA INTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900286 19980219 00286 WP 1998 2 19 9802331154 1 19980208 A 3412 TAT WIRING DOUG DC10 DC1040 3023508 WP COCKPIT OUT OF POSITION A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 154US 46763 ON APPROACH INTO MSP UPON GEAR EXTENSION, ALL FOUR GEAR LIGHTS REMAINED RED. EXECUTED GO-AROUND AND RECYCLED GEAR HAND LE. RECEIVED ALL FOUR GREEN LIGHTS, FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WIRING FROM TAT INDICATOR INTERF ERING WITH GEAR HANDLE SWITCH. REPOSITIONED WIRE. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998021900287 19980219 00287 WP 1998 2 19 9802349983 1 19980209 A 5350 CABLE DOUG DC9 DC932 3022066 WP TAIL CONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 983US 47282 DURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXTERNAL RELEASE HANDLE HANGS UP ON HINGED SPRING DOOR DURING PULL TEST OF THE EMERGENCY RELEASE. ALSO, FOUND THE INTERIOR TAILCONE RELEASE CABLE WORN AT THE HANDLE. RESHAPED HINGED SPRING DOOR AND REPLACED CABLE. FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900288 19980219 00288 NE 1998 2 19 9802353233 2 19980204 A 7200 ENGINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 333NW 329 731476 DURING TAKEOFF AT APPROXIMATELY 200 FT AGL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND EGT ROSE. THE NR 1 ENGIN E WAS SHUT DOWN AND THE FLIGHT CREW RETURNED TO DEPARTURE AIRPORT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUN D METAL IN THE TAILPIPE. REPLACED THE NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM E29NE 1998021900289 19980219 00289 WP 1998 2 19 9802369968 1 19980206 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9332 47264 DURING INSPECTION, THE FLIGHT ATTENDANT FLASHLIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900290 19980219 00290 WP 1998 2 19 9802379925 1 19980207 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING INSPECTION, THE AFT OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY L IGHTS BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900291 19980219 00291 WP 1998 2 19 9802389982 1 19980208 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 982US 45790 DURING INSPECTION, THE FORWARD OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGEN CY LIGHTS BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900292 19980219 00292 WP 1998 2 19 9802399607 1 19980206 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 607NW 47232 DURING INSPECTION, THE EMERGENCY LIGHTS LOCATED AT DOOR 1R AND THE FIRST CLASS SEATS WERE FOUND TO BE INOPERATIVE. MAIN TENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900293 19980219 00293 WP 1998 2 19 9802409863 1 19980209 A 5350 RELEASE MECH DOUG DC9 DC951 3022051 WP TAIL CONE OUT OF ADJUST A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING TAILCONE FUNCTIONAL CHECK, FOUND THAT THE INTERIOR TAILCONE RELEASE HANDLE FAILED PULL TEST. ADJUSTED INTERNAL T AILCONE RELEASE SYSTEM. FUNCTIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021900297 19980219 00297 WP 1998 2 19 9802411236 1 19980206 A 5320 FITTING DOUG DC10 DC1030 3023501 WP BS 1811 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 236NW 46934 DURING M CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON END FITTING FOR LONGERON 45L, FS 1811. REPLACED END FITTING PER SRM 51-33-01, VOL 1. 2 L 7 3 4F A22WE 1998021900298 19980219 00298 WP 1998 2 19 9802429975 1 19980131 A 5320 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 DURING L CHECK, FOUND CRACKS IN THE NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL LEFT SIDE AT THE INBOARD AND OUTBOARD VERTICAL BEAM AT FS 110. REPAIRED PER EA 99-154615. 2 L 7 2 4F A6WE 1998021900299 19980219 00299 WP 1998 2 19 9802439975 1 19980202 A 5320 PRESSURE PANEL DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9339 47382 DURING L CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL RIGHT SIDE OUTBOARD VERTICAL BEAM AT FS 110. REPAIRED PER EA 99-154624. 2 L 7 2 4F A6WE 1998021900300 19980219 00300 NM 1998 2 19 9802446614 1 19980103 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 460 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 614US 20539 DURING M CHECK, FOUND CRACK IN FLOORBEAM WEB AT FS 460, RBL 80. REPAIRED PER EA 66-153168. 2 L 7 4 4F A20WE 1998021900301 19980219 00301 WP 1998 2 19 9802459878 1 19980201 A 5753 FITTING DOUG DC9 DC951 3022051 WP RT TE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 787NC 48149 DURING POST FLIGHT INSPECTION, FOUND CRACK IN THE RIGHT OUTBAORD FLAP HINGE RESULTING IN DAMAGE TO THE FLAP, FLAP COVE, FLAP HINGE FITTING FAIRING, AND THE BUTTE DOOR. REPLACED THE FLAP HINGE FITTING PER AMM. 2 L 7 2 4F RT A6WE 1998021900302 19980219 00302 EU 1998 2 19 9802463206 1 19980210 A 3350 CONNECTOR AIRBUS 320 A320211 3930320 EU CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 306US 60 DURING MAINTENANCE TEST OF THE EMERGENCY LIGHTS, FOUND ESCAPE PATH LIGHTS INOPERATIVE AT SEAT ROWS 25C, 26C, AND 27C. M AINTENANCE SECURED LOOSE CANNON PLUG. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998021900303 19980219 00303 EU 1998 2 19 9802473235 1 19980209 A 3397 WIRE AIRBUS 320 A320212 EU CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 335NW 340 DURING TEST OF EMERGENCY LIGHTS, FOUND ESCAPE PATH LIGHTS INOPERATIVE ON LAST THREE SEAT ROWS. MAINTENANCE REPAIRED BRO KEN WIRE AT SIDEWALL CONNECTOR. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998021900304 19980219 00304 WP 1998 2 19 9802489925 1 19980210 A 2751 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP FLIGHT DECK INOPERATIVE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 925US 47472 DURING CLIMB-OUT, THE RIGHT WING FLAP WOULD NOT RETRACT FROM THE 15 DEGREE POSITION, THE WINDSHEAR ANNUNCIATOR LIGHT ILL UMINATED, THE FIRST OFFICER'S SPEED COMMAND FLAG WAS IN VIEW, AND THE NR 1 AND NR 2 VHF RADIOS BECAME INOPERATIVE (BOTH WORKED NORMALLY IN EMERGENCY MODE). THE FLIGHT CREW RESTORED THE FLAP SETTING TO THE 15 DEGREE POSITION, RETURNED TO OR IGINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE RIGHT INSTRUMENT TRANSFORMER CIRCUIT BREAKER AND PULLED A ND COLLARED THE RIGHT FLAP INDICATOR CIRCUIT BREAKER PER MEL PROCEDURES. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED T O SERVICE. 2 L 7 2 4F A6WE 1998021900305 19980219 00305 WP 1998 2 19 9802509760 1 19980208 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 01 760NW 47288 DURING DESCENT, THE FLIGHT CREW DISCOVERED SMOKE IN THE AIRCRAFT CABIN. FLIGHT CREW DECLARED AN EMERGENCY, SHUT DOWN TH E CABIN LIGHTING SYSTEM, AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPAIRED WIRE ENDS AT S3-94 L741AH16 A ND L741Y20. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900306 19980219 00306 1998 2 19 9802519162 4 19980207 A 3418 COMPUTER DOUG DC9 DC914 3022034 WP STALL WARNING FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8907E 45748 DURING CLIMB-OUT, THE STALL WARNING STICK SHAKER ACTIVATED. FLIGHT CREW PULLED APPLICABLE STALL WARNING STICK SHAKER CI RCUIT BREAKERS, RETURNED TO ORIGINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT FLAP TRANSMITTER, T HE RIGHT FLAP TRANSMITTER, AND THE STALL WARNING COMPUTER. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900307 19980219 00307 WP 1998 2 19 9802529153 1 19980209 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8912E 45829 DURING LINE CHECK, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. OPERATIO NAL CHECK OK. 2 L 7 2 4F A6WE 1998021900308 19980219 00308 WP 1998 2 19 9802539909 1 19980209 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE CHECK, FOUND TAILCONE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONA L CHECK OK. 2 L 7 2 4F A6WE 1998021900309 19980219 00309 SO 1998 2 19 COMA9810041 1 19980206 A 2752 3082001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP MALFUNCTION A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 152CA 6210 120152 FLAP CONTROL FAULT WARNING. REPLACED THE RIGHT HAND NACELLE FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1998021900310 19980219 00310 NM 1998 2 19 UPS98225721 1 19980208 A 3350 BATTERIES BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 EMERGENCY LIGHT RECEIVER BATTERIES NEED REPLACEMENT. ACCOMPLISHED TASK CARD 2403, EMERGENCY LIGHT RECEIVER BATTERIES RE MOVED AND REPLACED BATTERIES. OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1998021900311 19980219 00311 NM 1998 2 19 UPS98225722 1 19980209 A 3350 9621033 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 LEFT FORWARD OVERWING EXIT MARKER, EMERGENCY LIGHTING BATTERY NEEDS REPLACEMENT PER TASK CARD 2403. PART ON REQ NR 4825 64. REMOVED AND REPLACED ROW LEFT EXIT MARKER BATTERY PACK. P/N ON AND OFF 96-21033. OPS NORMAL S/N ON TAG 00310263. 2 L 7 3 4F A3WE 1998021900312 19980219 00312 EU 1998 2 19 WWMA9800026 1 19980209 A 3320 F8T5CW LAMP SAAB SF340 340B 7860101 EU LAVATORY INTERMITTENT A WWMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 306AE 340B306 FLIGHT 3331 - DURING PREFLIGHT, THE LAVATORY SMOKE LIGHT WOULD ILLUMINATE WHEN THE LAV DOOR WAS CLOSED AND LOCKED. MAI NTENANCE FOUND THE FLUORESCENT LIGHTS INTERMITTENT CAUSING THE LAV SMOKE LIGHT TO ILLUMINATE. REPLACED THE LAVATORY FLU ORESCENT BULBS. 2 L 7 2 4T RT A52EU 1998021900313 19980219 00313 NM 1998 2 19 QXEA9800063 1 19980209 A 6120 SWITCH DHAV DHC8 DHC8202 2809007 NM POWER LEVER FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 355PH 500 PDX - AUTOFEATHER SYSTEM WILL NOT TEST. MAINTENANCE REPLACED POWER LEVER SWITCH. OPERATIONAL CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998021900314 19980219 00314 EU 1998 2 19 QXEA9800064 1 19980209 A 3350 1820 LAMP FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 SEA - UPPER EMERGENCY LIGHT LEFT OF FORWARD SERVICE DOOR INOP. MAINTENANCE RELAMPED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998021900315 19980219 00315 NM 1998 2 19 98FDEA00091 1 19980210 A 5315 6520832 FLOORBEAM BOEING 727 727233 138408A NM BS 1010 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR 0023 001, CORROSION LOWER CHORD BS 1010, WL 201, LBL 24 TO 36. REMOVED CORROSION ON LOWER CHORD, BS 1010, WL 201, LB L 1 TO 45.5. REMOVED LOWER FLANGE OF LOWER CHORD. FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-8 FIG 2. 2 L 7 3 4F RT A3WE 1998021900316 19980219 00316 NM 1998 2 19 98FDEA00092 1 19980210 A 5311 651593732 FRAME BOEING 727 72722 1384002 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 NR 0433 012, WHILE WORKING NR0301, FOUND FRAME TO BE CORRODED AT BS 680, RBL 24, WL 155 (STR 26). REMOVED DAMAGE AT BS 680, RBL 24 FROM STR 22-26 RT. FOUND TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REPAIRED DAMAGED FRAME AT BS 680, RBL 24, STR 22-26 RT IAW FED-EX SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1998021900317 19980219 00317 NM 1998 2 19 98FDEA00093 1 19980210 A 5320 65184174 WEB BOEING 727 72725 1384006 NM BS 306 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 156FE 18289 WHILE WORKING NR0159 FOUND CORROSION BETWEEN THE NOSE WHEEL WELL HORIZONTAL WEB AND BONDED DOUBLER AT BS 306, WL 182, LB L 14 TO RBL 14. *S/D* FOUND CORROSION ON WEB BS 306, WL 182, LBL 14 TO RBL 14 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10 -1. REPAIRED WEB BY REPLACING WEB SECTION FROM BS 294.5 TO BS 322.5, LBL 14 TO RBL 14, WL 182 IAW FED-EX DRAWING 65-184 17 AND FED-EX SRM 53-10-9. 2 L 7 3 4F A3WE 1998021900318 19980219 00318 NM 1998 2 19 98FDEA00094 1 19980210 A 5320 65189154 WEB BOEING 727 72725 1384006 NM BS 294-328 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 156FE 18289 NR 0400 006 WHILE WORKING NR0259, FOUND CORROSION ON FLOOR WEB BS 294-328, RBL 15-30, WL 168. FOUND CORROSION ON FLOOR WEB BS 294-328, RBL 15-30, WL 168 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. FABRICATED NEW WEB BS 294 TO 350, RBL 15- 30, WL 168 IAW FED-EX DRAWING 65-18915. WEB WILL BE INSTALLED ON CUSTOMER CARD NR0401. 2 L 7 3 4F A3WE 1998021900319 19980219 00319 NM 1998 2 19 98FDEA00095 1 19980210 A 5313 6534144109 LONG BEAM BOEING 727 72721C 138400M NM BS 838-843 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 NR 0557 041 STA-PAE - CORROSION (C53-224-01(2)) AROUND NUTCLIP HOLES LBL 45 LONGITUDINAL BEAM BS 838-843, WL 208. REMO VED AND REPLACED LBL 45 LONGITUDINAL BEAM WL 208 FROM BS 740 TO BS 848.5 PER BOEING 727 DRAWING 65-34144. 2 L 7 3 4F A3WE 1998021900320 19980219 00320 WP 1998 2 19 ABXA9800073 1 19980210 A 3260 CONNECTOR DOUG DC9 DC941 302207N WP RT MLG CORRODED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 956AX 47620 DURING INITIAL CLIMB, AFTER RAISING THE LANDING GEAR, THE RIGHT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED THE GEAR, LIGHT STILL REMAINED ON. LIGHT WENT OUT AFTER THREE MINUTES, WITH THE ENGINE DRIVEN HYDRAULIC PUMPS IN HIGH. CLEANED CORROS ION FROM PROXIMITY SWITCH CANNON PLUG. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998021900321 19980219 00321 WP 1998 2 19 DLL13980344 1 19980209 A 3397 WIRE LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 EMERGENCY LIGHT SOCKET WIRING BROKEN AT SEAR/ROW 11H. REPAIRED BROKEN WIRING. LIGHT OPERATIONAL CK NORMAL. 2 L 7 3 4F A23WE 1998021900322 19980219 00322 NM 1998 2 19 DL72S980348 1 19980209 A 5743 BEAM BOEING 727 727232 1384082 NM RT MLG SUPPORT CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 FOUND ON E2 LETTER CK, AFT SIDE OF MLG STRUT CHAFING FWD SIDE OF WALKING BEAM. REPAIRED PER MM 57-43-0. 2 L 7 3 4F A3WE 1998021900323 19980219 00323 NM 1998 2 19 DL72S980349 1 19980209 A 5531 RIB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 VERTICAL STAB RIB CHORD CRACKED AT FASTENER HOLE, FIN STA 157.2 AND STR 9 RT, FOUND ON E-2 LETTER CHECK. INSTALLED DOUB LER PER M/M 55-30-3 NR 2. 2 L 7 3 4F A3WE 1998021900324 19980219 00324 NM 1998 2 19 DL73K980351 1 19980109 A 3397 WIRE BOEING 737 737232 1384475 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 321DL 23093 FOUND LAST 3 SEAT ROWS EMERG EXIT LIGHTS INOP. FOUND ON NR 2 L/O. REPAIRED WIRING. 2 L 7 2 4F RT A16WE 1998021900325 19980219 00325 NM 1998 2 19 DL757980352 1 19980206 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681.8 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE PASSENGER FLOORBEAM, FS 1681.8, UPPER CAP, SPLICE REPAIR. THE UPPER CAP OF THE FS 1681.8 PASSENGER FLOORBEAM W AS FOUND CORRODED IN NUMEROUS AREAS. TO REPAIR THE DAMAGE, THE UPPER CAP WAS TRIMMED OFF AND A NEW CAP WAS FABRICATED F ROM ALUMINUM EXTRUSION AND INSTALLED IN ITS PLACE. THE REPAIR WAS ACCOMPLISHED PER ER/A 363852-14, REV A. 2 L 7 2 4F RT A2NM 1998021900326 19980219 00326 NM 1998 2 19 DL757980353 1 19980206 A 5320 146N53181 SHEAR PANEL BOEING 757 757232 1384965 NM BS 1680-1720 CUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 FUSELAGE FLOOR STRUCTURE SHEAR PANEL, FS 1681-1720, SPLICE REPAIR. TO GAIN ACCESS TO THE FS 1681.8 FLOORBEAM UPPER CAP, THE HORIZONTAL SUBFLOOR SHEAR PANEL HAD TO BE TRIMMED OFF FROM FS 1720 TO FS 1680. A NEW SECTION OF SHEAR PANEL WAS SP LICED IN PER ER/A 363925-14, REV A. 2 L 7 2 4F RT A2NM 1998021900327 19980219 00327 NM 1998 2 19 DL72W980354 1 19980210 A 5312 6516350 BLKHD STIFFENER BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 CRACKS WERE FOUND IN THE L/RBL 36083 VERT STIFFENER ON THE FWD SIDE OF THE BS 1183 BLKHD. CRACKS WERE LOCATED AT APPROX WL 238 AND WERE NO MORE THAN 2 IN LENGTH. REPAIR PER ERA 331332-14. 2 L 7 3 4F A3WE 1998021900328 19980219 00328 NM 1998 2 19 DL757980355 1 19980210 A 5511 185N700161 SPAR WEB BOEING 757 757232 1384965 NM RT HORIZ STAB WRINKLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 658DL 24420 THE AUX SPAR WEB OF THE RT HORIZ STAB WAS FOUND WRINKLED FROM AUX SPAR STA 220 TO 285. REPAIRED AND REWORKED PER ERA 33 1336-14. 2 L 7 2 4F RT A2NM 1998021900329 19980219 00329 NM 1998 2 19 DL72W980356 1 19980130 A 5753 ANGLE BOEING 727 727247 138408F NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 DURING SHOP INSPECTION, THE AFT SPAR ANGLE WAS FOUND CRACKED 37 FROM THE I/B END OF FLAP. THE CRACK WAS REPAIRED BY INS TALLING A DOUBLER PER 727 MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1998021900330 19980219 00330 NM 1998 2 19 DL72W980357 1 19980205 A 5753 ANGLE BOEING 727 727247 138408F NM RT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 DURING SHOP INSPECTION, THE AFT SPAR ANGLE WAS FOUND CRACKED 18 FROM IB END OF FLAP. THE ANGLE WAS REPAIRED BY INSTALLI NG A DOUBLER PER 727 MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1998021900331 19980219 00331 NM 1998 2 19 DL72W980358 1 19980205 A 5753 ANGLE BOEING 727 727247 138408F NM NR 3 TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 DURING SHOP, THE AFT SPAR ANGLE WAS FOUND CRACKED 34 FROM THE IB END OF THE FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1998021900431 19980219 00431 EU 1998 2 19 98ZZZX741 1 19980108 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - CORROSION INSIDE SEAT TRACK NR 8 BELT FRAMES 31 AND 33. REMOVED AND REPLACED NR 8 SEAT TRACK BELT FRAMES 26 TO 33 PER SRM 51-72-10-0. TST: 26,550 HOURS. CYCLES: 10,536. 2 L 7 2 4F RT A35EU 1998021900432 19980219 00432 NM 1998 2 19 AALA980021 1 19980105 A 3350 1001141 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 730AA 20737 TUL - AFT AIRSTAIR EMERGENCY LIGHT ASSY INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. TST: 67,414.53 H OURS. CYCLES: 44,081. (X) 2 L 7 3 4F A3WE 1998021900434 19980219 00434 NM 1998 2 19 AALA980055 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - STR 15R CHANNEL CRACKED STA 720B AT RIGHT ZEE LIGHT. INSTALLED REPAIR PER SRM 53-10-3, FIG 5. TST: 67,236. CYC LES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900435 19980219 00435 NM 1998 2 19 AALA980056 1 19980107 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION AT STR 23L, STA 720E TO 720F. REPAIRED STRINGER PER SRM 53-10-3, FIG 1, SHEET 4, DETAIL NR 1. TST: 67, 236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900436 19980219 00436 NM 1998 2 19 AALA980057 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - STR 15L CRACKED IN U-CHANNEL FROM END TO FIRST FASTENER STA 720B. REPAIRED STR PER SRM 53-10-3 FIG 5, SHEET 2. T ST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900437 19980219 00437 NM 1998 2 19 AALA980058 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - STR 15L CRACKED IN U-CHANNEL FROM END TO FIRST FASTENER AT 720C. REPAIRED STA PER 53-10-3, FIG 5, SHEET 2. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900438 19980219 00438 NM 1998 2 19 AALA980059 1 19980109 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1030-1040 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION ON STR 27R STA 1030 - STA 1040 AND SKIN UNDER STRINGER. REMOVED CORROSION, REPAIRED PER SRM 53-30-3, FI G 3. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900439 19980219 00439 NM 1998 2 19 AALA980060 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 580 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - STR 28L CRACKED, DAMAGED OUTBOARD LEG STA 580. REPAIRED STR PER SRM 53-10-3, FIG 1. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900440 19980219 00440 NM 1998 2 19 AALA980061 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 680-700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION UNDER STRINGER BETWEEN STA 680 - STA 700. REPAIRED DAMAGED AREA PER SRM 53-10-3. TST: 67,236 HOURS. C YCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900441 19980219 00441 NM 1998 2 19 AALA980062 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 680-700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION AT STR 26L BETWEEN STA 680 AND STA 700 (MKD). REPAIRED STRINGER PER SRM 53-10-3. TST: 67,236 HOURS. C YCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900442 19980219 00442 NM 1998 2 19 AALA980063 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 552/555 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - STR 27L HAS CORROSION ON BOTTOM AT STA 552 TO STA 555. REPAIRED STR PER SRM 53-10-3 FIG 1. TST: 67,236 HOURS. C YCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900443 19980219 00443 NM 1998 2 19 AALA980064 1 19980106 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION AT STR 23L STA 720E TO STA 720F. REPAIRED STRINGER PER SRM 53-10-3, FIG 1, SHEET 4, DETAIL NR 1. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900444 19980219 00444 NM 1998 2 19 AALA980065 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - SKIN BULGED OUT AND FRONT BROKEN IN SKIN LAP AND DOUBLER, STR 26R, STA 700. DAMAGED AREA REPAIRED PER SRM 53-30-3 , FIG 4. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900445 19980219 00445 NM 1998 2 19 AALA980066 1 19980107 A 5730 SKIN BOEING 727 727227 1384078 NM WS 431 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - AREA OF BULGED AND DISTORTED SKIN UPPER FIXED LEADING EDGE JUST ABOVE INBOARD END OF FUELING PANEL, POSSIBLE CORRO SION. REMOVED DAMAGED AREA, INSTALLED FLUSH REPAIR PER SRM 57-30-4. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900446 19980219 00446 NM 1998 2 19 AALA980067 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - SKIN BULGED OUT AT THE FLUSH REPAIR STA 580, STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3. TST: 67,236 HOUR S. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900447 19980219 00447 NM 1998 2 19 AALA980068 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - LOWER SKIN BULGED AT STR 27R STA 500. INSTALLED EXTERNAL DOUBLER AT STR 27R STA 500 PER SRM 53-30-3. TST: 67,23 6 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900448 19980219 00448 NM 1998 2 19 AALA980069 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 708 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - SKIN BULGING AROUND FASTENER HOLE STA 708 OUTBOARD STR 26R. REPLACED DAMAGED SKIN PER SRM 53-30-3 FIG 3. TST: 6 7,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900449 19980219 00449 NM 1998 2 19 AALA980070 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 681 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - FUSELAGE SKIN BULGED STA 681 BETWEEN STR 28L AND STR 28R. REPLACED DAMAGED SKIN PER SRM 53-30-3 FIG 3. TST: 67, 236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900450 19980219 00450 NM 1998 2 19 AALA980071 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 332 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - 3 INCH DENT AND GOUGE BELOW STR 24R, STA 332. REPAIRED MINOR DENT IN SKIN PER SRM 53-30-3 PAGE 154 FIG 24 SHEET 4 . TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900451 19980219 00451 NM 1998 2 19 AALA980072 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 552 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - SKIN BULGED OUT AT THE REPAIR STA 552, STR 28L. INSTALLED DOUBLER PER SRM 53-30-3, FIG 3. TST: 67,236 HOURS. C YCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900452 19980219 00452 NM 1998 2 19 AALA980073 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 715 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION UNDER STR 26R FROM STA 696 TO STA 715. REPAIRED PER SRM 53-30-3 FIG 14. TST: 67,236 HOURS. CYCLES: 4 4,034. (X) 2 L 7 3 4F A3WE 1998021900453 19980219 00453 NM 1998 2 19 AALA980074 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 990-1010 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION IN SEALANT AT STR 10R STA 990 - STA 1010 AT SKIN LAP. REPAIRED PER SRM 53-30-3 FIG 5 PER ESO 11697 DATE D 12-8-97. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900454 19980219 00454 NM 1998 2 19 AALA980075 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION UNDER STR 26R BETWEEN STA 720C TO STA 720D. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. TST: 67,236 H OURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900455 19980219 00455 NM 1998 2 19 AALA980076 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION UNDER STR 26R BETWEEN STA 720C TO STA 720D. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3. TST: 67,236 H OURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900456 19980219 00456 NM 1998 2 19 AALA980077 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 840-826 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION EMANATING FROM LONGITUDINAL SKIN LAP. INSTALLED EXTERNAL DOUBLER 11 INCHES BY 14 INCHES PER SRM 53-30-3 FIG 14 SHEETS 1 THROUGH 6. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900457 19980219 00457 NM 1998 2 19 AALA980078 1 19980106 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1030-1040 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - CORROSION COMING OUT AROUND FASTENERS AND SKIN AND BETWEEN SKIN AND STRINGER. CUT OUT DAMAGE, INSTALLED DOUBLER P ER SRM 53-30-3. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900458 19980219 00458 NM 1998 2 19 AALA980079 1 19980106 A 5510 BEAM BOEING 727 727227 1384078 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - SEVERAL AREAS OF CORROSION ON AFT EDGE OF RT HORIZONTAL REAR UPPER CHORD. REPLACED RT AFT HORIZONTAL BEAM. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900459 19980219 00459 NM 1998 2 19 AALA980080 1 19980106 A 5311 FRAME BOEING 727 727227 1384078 NM BS 277 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - BELL FRAME CRACKED STA 277 AT STR 16 LEFT. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 51-40-2. TST: 67,23 6 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900460 19980219 00460 NM 1998 2 19 AALA980081 1 19980106 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - STA 720, ABOVE STR 18L, BELT FRAME SHEAR TIE IS CRACKED. REPAIRED PER SRM 51-40-3. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900461 19980219 00461 NM 1998 2 19 AALA980082 1 19980107 A 5315 FLOOR BEAM BOEING 727 727227 1384078 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - APPROXIMATELY ONE-HALF DIAMETER OF DEEP CORROSION ON TOP OF FLOOR BEAM STA 1130 RBL 2411. REPAIRED AFFECTED AREA WITH STRAP DOUBLER PER ESO 11697 DATED 12-12-97. TST: 67,236 HOURS. CYCLES: 44,034. (X) 2 L 7 3 4F A3WE 1998021900462 19980219 00462 EU 1998 2 19 AALA980038 1 19980107 A 5210 RETAINER AIRBUS 300 A300B4605R 3930308 EU PASSENGER DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - CORROSION ON FORWARD LOWER JAMB OF DOOR SEAL RETAINER. SPLICED IN NEW SECTION OF DOOR SEAL RETAINER PER ESO 30595 DATED 1-6-98. TST: 26,550 HOURS. CYCLES: 10,536. (X) 2 L 7 2 4F RT A35EU 1998021900463 19980219 00463 EU 1998 2 19 AALA980039 1 19980107 A 5347 6022457 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - CORROSION ON TOP OF SEAT TRACK NR 10 BETWEEN FR 23 AND FR 24. REPLACED SEAT TRACK WITH NEW SECTION BETWEEN FR 21 AND FR 25 PER SRM 51-72-10-0. TST: 26,550 HOURS. CYCLES: 10,536. (X( 2 L 7 2 4F RT A35EU 1998021900464 19980219 00464 EU 1998 2 19 AALA980040 1 19980107 A 5320 A5327921220400 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - FLOOR BOARD SUPPORT HAS CORROSION IN TOP FLANGE AROUND FLOOR BOARD FASTENER HOLES. REPLACED FLOOR BOARD SUPPORT P ER SRM 51-72-10. TST: 26,550 HOURS. CYCLES: 10,536. (X( 2 L 7 2 4F RT A35EU 1998021900465 19980219 00465 NM 1998 2 19 AALA980089 1 19980112 A 5313 BAC1498133 STRINGER BOEING 727 727223 1384074 NM BS 477 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 703AA 22461 TUL - LEFT FUSELAGE STR 24L CRACKED AND FUSELAGE SKIN DENTED FROM STA 475 TO STA 478. INSTALLED STRINGER REPAIR PER SRM 53-10-3. INSTALLED FUSELAGE SKIN DOUBLER PER SRM 53-30-3. TST: 46,539 HOURS. CYCLES: 24,289. (X) 2 L 7 3 4F A3WE 1998021900466 19980219 00466 EU 1998 2 19 AALA980090 1 19980110 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - CORROSION FIRST STRINGER TO RIGHT OF BOTTOM CENTERLINE 58R BETWEEN FRAMES 61 AND 62. REMOVED AND REPLACED STR 58R FROM FRAMES 58 TO 62.5 PER SRM 51-72-10 AND SRM 53-10-14. TST: 26,550.31 HOURS. CYCLES: 10,536. (X) 2 L 7 2 4F RT A35EU 1998021900467 19980219 00467 EU 1998 2 19 AALA980091 1 19980109 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU LAVATORY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - INBOARD SUPPORT FOR LAVATORY 'L' CORRODED BETWEEN FRAMES 31 AND 33. INSTALLED NEW LAVATORY SUPPORT 2A TRACK PER S RM 51-72-10-0. TST: 26,550 HOURS. CYCLES: 10,536. (X) 2 L 7 2 4F RT A35EU 1998021900468 19980219 00468 EU 1998 2 19 AALA980092 1 19980109 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU LAVATORY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - CORROSION UNDER LAVATORY 'L' ON TRACK NR 3 BETWEEN FRAMES 31 AND 33. INSTALLED NEW TRACK NR 3 PER SRM 51-72-10-0 AND INSTALLED SPLICE ON TRACK PER SRM 53-10-16-2. TST: 26,550 HOURS. CYCLES: 10,536. (X) 2 L 7 2 4F RT A35EU 1998021900469 19980219 00469 EU 1998 2 19 AALA980093 1 19980110 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - NR 1 SEAT TRACK HAS CORROSION TOP OF SEAT TRACK BETWEEN FRAMES 32 AND 33. REMOVED CORROSION PER SRM 51-74-10-2 AN D INSTALLED REPAIR STRAP PER AAR 53-20-00-2. TST: 26,550.31 HOURS. CYCLES: 10,536. (X) 2 L 7 2 4F RT A35EU 1998021900470 19980219 00470 NM 1998 2 19 AALA980104 1 19980113 A 5730 SKIN BOEING 727 727223 1384074 NM WS 840 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON LOWER WING SKIN IN AREA AT RIGHT PRIMARY HEAT EXCHANGE, RBL 8-40, STA 840. REMOVED CORROSION AND INS TALLED REPAIR DOUBLER PER ESO 11697 DATED 1-6-98. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900471 19980219 00471 NM 1998 2 19 AALA980105 1 19980113 A 5330 SKIN BOEING 727 727223 1384074 NM BS 570-590 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON STR 26L, STA 577. SKIN GOUGED AT LAP UNDER STR 26L, STA 520 - STA 590. REMOVED DAMAGED SKIN AND INS TALLED FLUSH REPAIR SRM 53-30-3 FIG 6. REMOVED STRINGER AND INSTALLED NEW STRINGER AND SPLICE PER SRM 5-10-3 FIG 1. TS T: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900472 19980219 00472 NM 1998 2 19 AALA980106 1 19980113 A 5330 SKIN BOEING 727 727223 1384074 NM BS 392 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - DENT APPROXIMATELY 4 FEET AFT OF FORWARD ENTRY DOOR, LT SIDE, 6 INCHES BELOW CABIN FLOOR AND 2 INCHES LONG. REMOV ED DAMAGED PORTION OF SKIN AT INSTALLED REPAIR PER SRM 53-30-3. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900473 19980219 00473 NM 1998 2 19 AALA980107 1 19980113 A 5330 SKIN BOEING 727 727223 1384074 NM BS 380 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - DENT APPROXIMATELY 3 FEET AFT OF FORWARD ENTRY DOOR, LT SIDE APPROXIMATELY 3 INCHES BELOW CABIN FLOOR AND APPROXIM ATELY 2 INCHES LONG. REMOVED DAMAGED PORTION OF SKIN AND INSTALLED REPAIR PER SRM 53-30-3. TST: 53,792 HOURS. CYCLES : 33,779. (X) 2 L 7 3 4F A3WE 1998021900474 19980219 00474 NM 1998 2 19 AALA980108 1 19980113 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON TOP SIDE OF FLOOR BEAM STA 380 RBL 27 - RBL 65. REMOVED CORROSION PER SRM 51-10-6. REPAIRED DAMAGED AREA ON FLOOR BEAM PER SRM 53-10-8, PAGES 9-A AND 9-B. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900477 19980219 00477 NM 1998 2 19 AALA980111 1 19980113 A 5720 STIFFENER BOEING 727 727223 1384074 NM WS 160 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON VERTICAL STIFFENER ON FRONT SPAR ABOVE MANUAL DEFUELING VALVE. REMOVED CORRODED STIFFENER AND REPLAC ED WITH NEW STIFFENER AT LES 160. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900478 19980219 00478 NM 1998 2 19 AALA980112 1 19980113 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 580 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - SHEAR TIES INBOARD AND OUTBOARD OF STR 26L, STA 580, CRACKED. REMOVED AND REPLACED SHEAR TIES PER SRM 53-10-4, FI G 13. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900479 19980219 00479 NM 1998 2 19 AALA980113 1 19980113 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - STA 720E SHEAR TIE CORROSION BETWEEN STR 25 AND STR 26R. REPLACED SHEAR TIE, REF: SRM 51-30-2 AND SRM 51-10-6. T ST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900480 19980219 00480 NM 1998 2 19 AALA980114 1 19980113 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON SHEAR TIE STA 720E, STR 25 TO STR 26R. REMOVED AND INSTALLED NEW SHEAR TIE PER SRM 51-30-2, PAGE 31. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900481 19980219 00481 NM 1998 2 19 AALA980115 1 19980113 A 5311 FRAME BOEING 727 727223 1384074 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - 2 INCH AREA OF CORROSION ON STA 740 FRAME AT ATTACH POINT TO FUSELAGE BELLY SKIN BL ZERO TO LBL 2. REPLACED T-ANG LE AT 740 28L-28R PER SRM 51-10-01, PAGE 04. (X) 2 L 7 3 4F A3WE 1998021900482 19980219 00482 NM 1998 2 19 AALA980116 1 19980113 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - STA 680 STR 27R HAS CORROSION ON INBOARD AND OUTBOARD SIDES OF STRINGER. REPLACED STRINGER CAP, ALODINED, AND TRE ATED AFFECTED AREA PER SRM 51-10-2. (X) 2 L 7 3 4F A3WE 1998021900483 19980219 00483 NM 1998 2 19 AALA980117 1 19980113 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-1000 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON UPPER OUTBOARD FLANGE STR 29L STA 950F TO STA 1000. REMOVED CORROSION AND INSTALLED REPAIR PER ESO 1 1697 DATED 1-2-90. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998021900484 19980219 00484 EU 1998 2 19 AALA980126 1 19980114 A 5754 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU RT LE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - KRUEGER FLAP RT WING, UPPER SECTION HAS MODERATE CORROSION ON RIBS AND SKIN INTERNALLY. REMOVED AND REPLACED KRUE GER FLAP WITH SERVICEABLE PART PER SRM 51-72-10-0. FIT CHECK AND OPS CHECK PERFORMED ON E-58 NR 2376654. (X) 2 L 7 2 4F RT A35EU 1998021900485 19980219 00485 EU 1998 2 19 AALA980128 1 19980114 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - CORROSION ON FRAME 58 FROM BOTTOM CENTERLINE TO LEFT 4 STRINGERS. INSTALLED SPLICE DOUBLER PER SRM 53-10-13. TST : 26,550.31 HOURS. CYCLES: 10,536. (X) 2 L 7 2 4F RT A35EU 1998021900486 19980219 00486 EU 1998 2 19 AALA980129 1 19980114 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 19059 469 TUL - CORROSION ON FRAME 58 FROM BOTTOM CENTERLINE TO RIGHT 4 STRINGERS. INSTALLED FILLER AND DOUBLER PER SRM 53-10-13. TST: 26,550.31 HOURS. CYCLES: 10,536. (X) 2 L 7 2 4F RT A35EU 1998021900487 19980219 00487 WP 1998 2 19 AALA980131 1 19980105 A 5320 5912494501 JAMB DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 33414 49325 TUL - FORWARD CARGO DOOR JAMB BEAM HAS CORROSION ON UPPER AND LOWER LEG. REMOVED AND REPLACED WITH NEW LOWER DOOR JAMB PAN. TST: 34,516.38 HOURS. CYCLES: 19,391. (X) 2 L 7 2 4F A6WE 1998021900488 19980219 00488 WP 1998 2 19 AALA980176 1 19980119 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 420AA 49332 TUL - CORROSION AT ATTACH ANGLE, FORWARD FRAME FS 1287, LONGERON 24L. CUT OUT ATTACHED ANGLE, INSTALLED REPAIR PER SRM 53-03 FIG 7. TST: 34,569 HOURS. CYCLES: 19,529. (X) 2 L 7 2 4F A6WE 1998021900489 19980219 00489 WP 1998 2 19 AALA980177 1 19980119 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 420AA 49332 TUL - CORROSION ON AFT SIDE OF FRAME STA 1287, LONGERON 24L. CUT OUT DAMAGED AREA, INSTALLED ATTACH ANGLE REPAIR PER SR M 53-03 FIG 7. TST: 34,569 HOURS. CYCLES: 19,529. (X) 2 L 7 2 4F A6WE 1998021900491 19980219 00491 EU 1998 2 19 MALA975967 1 19980210 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING INSPECTION, EMERGENCY OVERHEAD LIGHTS INOP AT ROW 8 C/D AND 9A. MAINTENANCE RELAMPED BOTH OVERHEAD EMERGENCY LIG HTS. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998021900492 19980219 00492 EU 1998 2 19 MALA975968 1 19980210 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 115XJ 340A115 DURING INSPECTION 2A, OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED 2A'S OVERHEAD EMERGENCY LIGHT. OPS CHECK GOO D. 2 L 7 2 4T RT A52EU 1998021900493 19980219 00493 EU 1998 2 19 MALA975969 1 19980209 A 2613 1734362450 TEMP SWITCH SAAB SF340 340B 7860101 EU RT RT NACELLE FAILED A MALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 15 424XJ 424 DURING TAXI OUT, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BLOCK. MAINTENANCE MEGGED TEMP PROBES AND REPLACED THE LOWER INBOARD TEMP SWITCH IN THE RIGHT NACELLE. SYSTEM CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998021900494 19980219 00494 EU 1998 2 19 MALA975970 1 19980210 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING INSPECTION, AN OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED THE OVERHEAD EMERGENCY LIGHT. ALL CHECKS GOO D. 2 L 7 2 4T RT A52EU 1998021900495 19980219 00495 NM 1998 2 19 K3HA980013 1 19980213 A 3350 3071BPEGPL LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY PATH LIGHTING INOP AT R2 FLOOR. RELAMPED, OPS CHECK OK. 2 L 7 3 4F A3WE 1998021900496 19980219 00496 NM 1998 2 19 K3HA980014 1 19980213 A 3350 3071BPEGPL LAMP BOEING 727 727225 1384077 NM L2 FLOOR FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY PATH LIGHTING INOP AT L2 FLOOR. RELAMPED, OPS CHECK OK. 2 L 7 3 4F A3WE 1998021900497 19980219 00497 NM 1998 2 19 K3HA980015 1 19980213 A 3350 079123 LENS BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY TRACK LIGHT RED LENS MISSING AT L-1 DOOR. INSTALLED NEW LENS, OPS CHECK OK. 2 L 7 3 4F A3WE 1998021900498 19980219 00498 NE 1998 2 19 IXXA980004 2 19980212 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE LT WING DAMAGED A IXXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 824BX 28175 1474 45946 692207 EN ROUTE FROM TOL TO ATL, DURING CRUISE THE FLIGHT ENGINEER NOTICED A MARKED DECLINE IN THE NUMBER ONE ENGINE OIL QUANTI TY. THE CREW PERFORMED A PRECAUTIONARY INFLIGHT SHUTDOWN IAW COMPANY PROCEDURES, AND CONTINUED TO ATL MAKING AN UNEVEN TFUL LANDING. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE ENGINE HAD SUSTAINED A GROUND STRIKE WITH DAMAGE TO THE CO WLINGS, AND THE TRANSFER GEARBOX WAS ALSO IMPACTED. THE AIRCRAFT IS CURRENTLY REMOVED FROM SERVICE FOR INSPECTION AND ENGINE REPLACEMENT AT THIS TIME. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998021900499 19980219 00499 WP 1998 2 19 IXXA980005 1 19980212 A 3830 38YG23 PUMP DOUG DC8 DC862F 3021972 WP LT AFT LAV MALFUNCTIONED A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 41CX 46129 EN ROUTE FROM HIK TO SUU, THE LEFT AFT LAVATORY EMITTED AN ELECTRICAL BURNING ODOR WHEN THE LAV WAS FLUSHED. THE LAVATO RY COMPARTMENT WAS CLOSED OFF FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE OPERATED THE PUMP NUMEROUS TIMES, WITH NO DE FECTS NOTED. MAINTENANCE REMOVED THE PUMP AND VISUALLY INSPECTED, WITH NO DISCREPANCIES NOTED. MAINTENANCE REPLACEDTHE PUMP AS A PRECAUTIONARY MEASURE. 2 L 7 4 4F 4A25 1998021900500 19980219 00500 NM 1998 2 19 AWXA9800044 1 19980120 A 5315 FLOORBEAM BOEING 737 73733A 1384673 NM BS 294.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND CORROSION ON FLOORBEAM 294.5 TOP CHORD LBL 25 TO RBL 53, WL 208. REPAIRED UPPER CHORD OF FLOOR BEAM FROM LBL 60 TO RBL 60, BS 294.5, WL 208 PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998021900501 19980219 00501 NM 1998 2 19 AWXA9800045 1 19980120 A 5320 6517688125 SILL BOEING 737 73733A 1384673 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND CORROSION ON CHORD (MOPSILL) LT BS 344 - 312, WL 208, LBL 63. REMOVED AND REPLA CED CREASE BEAM (MOPSILL) PER SRM 51-10-15, 51-10-02, 51-40-02. 2 L 7 2 4F RT A16WE 1998021900502 19980219 00502 NM 1998 2 19 AWXA9800050 1 19980120 A 5330 SKIN BOEING 737 73733A 1384673 NM BS 328 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND CRACK IN SKIN AT FWD GALLEY DOOR CUTOUT LOWER CORNER BS 328, RBL 58, WL 206. RE PAIRED PER SRM 53-10-01. 2 L 7 2 4F RT A16WE 1998021900503 19980219 00503 NM 1998 2 19 AWXA9800051 1 19980121 A 5730 SKIN BOEING 737 73733A 1384673 NM NR 2 FLAP TRACK CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND CORROSION ON SKIN I/B HOLE NR 2 SLAP TRACK REAR SPAR ATTACHMENT. REPAIRED CORRO SION ON SKIN I/B HOLE NR 2 FLAP TRACK REAR SPAR PER ER 3-57-32-14. 2 L 7 2 4F RT A16WE 1998021900504 19980219 00504 NM 1998 2 19 AWXA9800052 1 19980211 A 3397 WIRE BOEING 737 737277 1384570 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 'D EMERGENCY LIGHTS INOP ROW 3, 6, 7, AND 9C. REPAIRED WIRES, STCSA3432NM. 2 L 7 2 4F RT A16WE 1998021900505 19980219 00505 NM 1998 2 19 AWXA9800047 1 19980119 A 5311 FRAME BOEING 737 73733A 1384673 NM BS 787 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND DENT IN AFT CARGO BAY FRAME AT BS 787, RBL 28. REPAIRED FRAME PER SRM 51-70-1. 2 L 7 2 4F RT A16WE 1998021900506 19980219 00506 NM 1998 2 19 AWXA9800048 1 19980119 A 5320 69353521 CLIP BOEING 737 73733A 1384673 NM BS 400 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND CRACKED STRINGER CLIP BS 400, STR 27 LT. REMOVED AND REPLACED STRINGER CLIP AT BS 400, STR 27 LT, IAW, SRM 51-40-2. 2 L 7 2 4F RT A16WE 1998021900507 19980219 00507 NM 1998 2 19 AWXA9800049 1 19980120 A 5311 FRAME BOEING 737 73733A 1384673 NM BS 727 DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND DENT IN AFT CARGO BAY FRAME BS 727A, RBL 32. REMOVED DAMAGED AREA, REPAIRED PER SRM 51-70-11. 2 L 7 2 4F RT A16WE 1998021900508 19980219 00508 NM 1998 2 19 RAAA98B2008 1 19980213 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998021900509 19980219 00509 WP 1998 2 19 CALA9800209 1 19980211 A 2910 1489951 SHUTOFF VLV DOUG DC10 DC1030 3023501 WP TAIL LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 12080 47981 THE NR 2 HYDRAULIC SYSTEM LOST QUANTITY AND PRESSURE SHORTLY AFTER TAKEOFF FROM IAH. FUEL WAS DUMPED AND THE AIRCRAFT W AS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 HYDRAULIC SYSTEM HYDRAULIC SHUTOFF VALV E IN TAIL FAILED. THE SHUTOFF VALVE WAS REMOVED AND REPLACED AND LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998021900510 19980219 00510 NE 1998 2 19 CALA9800210 2 19980211 A 7200 ENGINE BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 1 FLAMED OUT A CALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SW 09 34315 23366 720893 WHILE PULLING POWER BACK FROM CLIMB POWER IN RESPONSE TO A TCAS WARNING AFTER DEPARTING PHL, THE NR 1 ENGINE FLAMED OUT. THE ENGINE WAS RESTARTED AND THE AIRCRAFT WAS DIVERTED TO EWR WHERE IT LANDED WITHOUT INCIDENT. AN ENGINE FLAME OUT I NSPECTION OF THE NR 1 ENGINE WAS PERFORMED IAW MM 71-00-42 AND NO FAULTS WERE NOTED. THE MAIN FUEL FILTER WAS REMOVED A ND REPLACED AS A PRECAUTIONARY MEASURE. THE NR 1 ENGINE WAS OPERATED AT TAKEOFF POWER FOR SEVERAL MINUTES AND OPERATION CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998021900511 19980219 00511 WP 1998 2 19 CALA9800212 1 19980210 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND LONGERON 2L CRACKED AT STA 1418. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1998021900512 19980219 00512 WP 1998 2 19 CALA9800213 1 19980210 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERT FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND VERTICAL FIN INNER ATTACH ANGLE ON RT AND LT SIDES CRACKED. THE ANGLES WERE REMOVED AND REPLACED IAW SR M 51-30-5. 2 L 7 2 4F A6WE 1998021900513 19980219 00513 WP 1998 2 19 CALA9800214 1 19980210 A 5510 PIVOT PLATES DOUG DC9 DC981 3022081 WP HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND INBOARD AND OUTBOARD SET OF HINGE PIVOT PLATES CORRODED ON RT HORIZONTAL STABILIZER. THE OUTBOARD SET OF HINGE PIVOT PLATES WERE FOUND CORRODED ON LT HORIZONTAL STABILIZER. THE PIVOT PLATES WERE REMOVED AND REPLACED IAW S RM 51-30-5. 2 L 7 2 4F A6WE 1998021900514 19980219 00514 WP 1998 2 19 CALA9800215 1 19980211 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 THE TAILCONE EXTERIOR RELEASE HANDLE PULLED AT 15 POUNDS. THE TAILCONE WAS RIGGED IAW WORK CARD 08-5350-1-0008. 2 L 7 2 4F A6WE 1998021900515 19980219 00515 WP 1998 2 19 CALA9800216 1 19980211 A 5730 PANEL DOUG DC10 DC1030 3023501 WP LT WING CANNED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND LT WING TOP SURFACE PANEL OUTBOARD OF INBOARD AILERON OIL CANNING. THE OIL CANNED AREA WAS TRIMMED AND BLENDED OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998021900516 19980219 00516 WP 1998 2 19 CALA9800217 1 19980212 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND LONGERON 29R CORRODED UNDER FLANGE AT STA 1322. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2. 2 L 7 2 4F A6WE 1998021900517 19980219 00517 WP 1998 2 19 CALA9800218 1 19980212 A 3230 ACG73305501 ACTUATOR DOUG DC10 DC1030 3023501 WP NLG DOWNLOCK LEAKING A CALA K NONE K FLUID LOSS AP APPROACH 1 SW 09 14062 47863 THE NLG WAS VERY SLOW TO EXTEND AND INDICATE DOWN WHEN GEAR WAS LOWERED DURING TEST FLIGHT WHILE AIRCRAFT WAS IN D-CHECK AT MAN. MAINTENANCE FOUND THE NLG DOWNLOCK ACTUATOR LEAKING INTERNALLY. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-35-00. 2 L 7 3 4F A22WE 1998021900518 19980219 00518 NM 1998 2 19 CALA9800219 1 19980212 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A .375 CRACK AT LEFT WING FIXED LEADING EDGE SKIN ABOVE NR 4 SLAT INBOARD TRACK. THE CRACK WAS STOP DR ILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-05. 2 L 7 3 4F A3WE 1998021900519 19980219 00519 NM 1998 2 19 CALA9800220 1 19980212 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND LEFT WING INBOARD LEADING EDGE SKIN DENTED BETWEEN INBOARD LANDING LIGHT AND NR 3 LEADING EDGE FLAP ARE A. THE DENT WAS REWORKED IAW ECRA 5750-01352. 2 L 7 3 4F A3WE 1998021900520 19980219 00520 NM 1998 2 19 CALA9800221 1 19980212 A 5720 ANGLE BOEING 727 727224 1384076 NM LT LE RIB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A .5 AND 1 INCH CRACK AT FASTENERS IN CURVED ANGLE INSIDE LEFT WING LEADING EDGE RIB OUTBOARD SIDE AT S LAT STA 0 (AFT OF NR 4 SLAT INBOARD MOST END). THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998021900521 19980219 00521 NM 1998 2 19 CALA9800222 1 19980212 A 5720 SPLICE PLATE BOEING 727 727224 1384076 NM WS 224.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 2 INCH CRACK AT SPLICE PLATE INSIDE LEFT WING UPPER LEADING EDGE ABOVE NR 2 LEADING EDGE FLAP ACTUATO R/ANTI-ICE DUCT AREA, WS 224.5. THE SPLICE PLATE WAS REMOVED AND A STRAP WAS FABRICATED AND INSTALLED IAW SRM 57-50-2 A ND 51-30-2. 2 L 7 3 4F A3WE 1998021900522 19980219 00522 NM 1998 2 19 CALA9800223 1 19980213 A 5754 SLAT BOEING 737 7373T0 1384582 NM NR 6 LE FLAP DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14347 23585 A CATERING TRUCK STRUCK THE RT OUTBOARD NR 6 SLAT. A REPAIR WAS COMPLETED IAW SRM 57-43-01. 2 L 7 2 4F RT A16WE 1998021900523 19980219 00523 WP 1998 2 19 CALA9800224 1 19980212 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND A 2 CRACK IN BELTFRAME AT LONGERON 2R AND A 2 CRACK IN BELTFRAME AT LONGERON 2L, STA 1418. A DOUBLER W AS INSTALLED TO ENCOMPASS BOTH CRACKS IAW SRM 53-05, FIGURE 32 AND ECRA 5311-01039. 2 L 7 2 4F A6WE 1998021900524 19980219 00524 NM 1998 2 19 CALA9800225 1 19980212 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1333 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND LEFT FUSELAGE SKIN DENTED AT STA 1333 JUST ABOVE AIRSTAIR. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 53-30-03. 2 L 7 3 4F A3WE 1998021900525 19980219 00525 WP 1998 2 19 CALA9801208 1 19980216 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LONGERON 17L CRACKED OUT OF UPPER AND LOWER FRAME ATTACH HOLES AT FS 945. THE LONGERON WAS REMOVED IAW SRM 51-10-2. A NEW LONGERON WAS FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1998021900526 19980219 00526 NM 1998 2 19 CALA9800226 1 19980212 A 5754 RIB BOEING 727 727224 1384076 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 2 CRACK IN NR 2 LEADING EDGE SLAT RIB OUTBOARD OF ANTI-ICE DUCT. A REPAIR ANGLE WAS FABRICATED AND I NSTALLED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1998021900527 19980219 00527 NM 1998 2 19 CALA9800227 1 19980212 A 5320 FRAME BOEING 727 727224 1384076 NM CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND C-3 DOOR FRAME CORRODED AT CUTOUT AT FORWARD LOWER END WHERE IT MEETS THRESHOLD AT BS 1090. THE CORROD ED AREA WAS CUT OUT. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998021900528 19980219 00528 NM 1998 2 19 CALA9800228 1 19980212 A 3350 1000677 LIGHT GRIMES BOEING 727 727224 1384076 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND THE RT AFT GALLEY DOOR EMERGENCY EXIT LIGHT TOO DIM. THE LIGHT ASSEMBLY WAS REPLACED IAW MM 33-50-101. 2 L 7 3 4F A3WE 1998021900529 19980219 00529 NM 1998 2 19 CALA9800229 1 19980212 A 3397 WIRE BOEING 727 727224 1384076 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT CANNON PLUG. THE WIRE WAS REPAIRED AND THE BATTERIES WERE CHARGED. 2 L 7 3 4F A3WE 1998021900530 19980219 00530 NM 1998 2 19 CALA9800230 1 19980212 A 5754 SKIN BOEING 727 727224 1384076 NM NR 4 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND SEVERAL .375 INCH CRACKS FROM FASTENER HOLE AT NR 4 SLAT UPPER SKIN WHERE INBOARD HOOK MOUNTS. TWO .37 5 INCH CRACKS WERE FOUND AT NR 4 SLAT UPPER SKIN WHERE OUTBOARD HOOK MOUNTS. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1998021900531 19980219 00531 NM 1998 2 19 CALA9800231 1 19980212 A 5754 ANGLE BOEING 727 727224 1384076 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 3 INCH CRACK IN LT WING NR 2 SLAT CHORD ANGLE BELOW WHERE INBOARD STOP PAD MOUNTS. A NEW ANGLE WAS F ABRICATED AND INSTALLED IAW SRM 51-10-01. 2 L 7 3 4F A3WE 1998021900532 19980219 00532 NM 1998 2 19 CALA9800232 1 19980212 A 5753 CASTING BOEING 727 727224 1384076 NM LT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1 INCH CRACK IN LT OUTBOARD FOREFLAP OUTBOARD END CASTING LOWER ATTACH LUG. THE LT OUTBOARD FOREFLAP VANE WAS REMOVED AND REPLACED IAW MM 27-50-00. 2 L 7 3 4F A3WE 1998021900533 19980219 00533 NM 1998 2 19 CALA9800233 1 19980213 A 5730 FUEL PANEL BOEING 727 727232 1384082 NM LT WING LOOSE A CALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 09 14788 20642 A FUEL LEAK WAS REPORTED COMING FROM LT WING AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND LOOSE SCREWS AT THE NR 4 UNDERWING FUEL ACCESS PANEL OF THE LT WING. ALL SCREWS WER E RETORQUED AND LEAK CHECK WAS GOOD. 2 L 7 3 4F A3WE 1998021900534 19980219 00534 WP 1998 2 19 CALA9800234 1 19980214 A 2740 418575 TRIM MOTOR DOUG DC10 DC1030 3023501 WP HORZ STAB CRACKED A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 83071 72972 48293 THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED WHILE EN ROUTE TO EWR. APPROPRIATE CHECKLISTS WERE FOLLOWED AND B OTH PUMPS WERE SHUTOFF. THE HYDRAULIC FLUID DEPLETED TO ZERO VERY SLOWLY AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDEN T. MAINTENANCE FOUND THE HORIZONTAL STABILIZER TRIM MOTOR HOUSING CRACKED. THE STAB TRIM MOTOR WAS REMOVED AND REPLACE D IAW MM 29-00. SYSTEM OPERATIONAL AND LEAK CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998021900535 19980219 00535 WP 1998 2 19 CALA9800235 1 19980213 A 5280 SKIN DOUG DC10 DC1010 3022110 WP NLG DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND THE INNER SKIN OF BOTH THE RT AND LT FORWARD NOSE WHEEL WELL DOORS CORRODED ALONG FORWARD EDGE. THE CO RRODED AREAS WERE CUT OUT. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW ECRA 5280-01170 AND SRM 51-21-01. 2 L 7 3 4F A22WE 1998021900536 19980219 00536 WP 1998 2 19 CALA9800236 1 19980213 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1701, LONGERON 49L-50L. REMOVED AND REPLACED DOUBLER STRAP, FINGER DOUBL ER, AND LONGERON SPLICE IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998021900537 19980219 00537 WP 1998 2 19 CALA9800237 1 19980213 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 999-1010 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND STRINGER 52L CORRODED AT STA 999-1010 IN FORWARD CARGO COMPARTMENT. THE CORRODED AREA WAS CUT OUT IAW SRM 53-13-01. A REPAIR FITTING WAS FABRICATED AND INSTALLED IAW SRM 53-10-0 AND 51-21-0. 2 L 7 3 4F A22WE 1998021900538 19980219 00538 WP 1998 2 19 CALA9800238 1 19980213 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1641-1701 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 52R CORRODED FROM STA 1641-1701. THE CORROSION WAS REMOVED, TREATED, AND PRIMED IAW SRM 51-21 -01. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998021900539 19980219 00539 WP 1998 2 19 CALA9800239 1 19980213 A 5320 STRAP DOUG DC10 DC1010 3022110 WP BS 1661 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND STRAP CORRODED AT STA 1661 BETWEEN LONGERON 47-48L. THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE S TRAP WAS REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998021900540 19980219 00540 WP 1998 2 19 CALA9800240 1 19980213 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 475 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LT CIRCUMFERENTIAL FRAME CORRODED AT STA 475, LONGERON 48L. A SPLICE AND FRAME WERE INSTALLED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1998021900541 19980219 00541 WP 1998 2 19 CALA9800241 1 19980213 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 555 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CIRCUMFERENTIAL FRAME CORRODED AT STA 555, LONGERON 48L. CHORD ANGLES WERE FABRICATED AND INSTALLED IA W SRM 53-30-00. FRAME SPLICE A BRACKETS WERE REINSTALLED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1998021900542 19980219 00542 WP 1998 2 19 CALA9800242 1 19980213 A 5530 SUPPORT DOUG DC10 DC1010 3022110 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 CRACK IN CIRCUMFERENTIAL SUPPORT SIDE BRACE OF LT LOWER VERTICAL STABILIZER ABOVE NR 2 ENGINE DUCT. THE SUPPORT SIDE BRACE WAS REMOVED. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-00, 51-21-01, AND 51-31- 01. 2 L 7 3 4F A22WE 1998021900543 19980219 00543 WP 1998 2 19 CALA9800243 1 19980213 A 5400 STIFFENER DOUG DC10 DC1010 3022110 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 2 CRACK ON INBOARD SIDE OF LT UPPER SPAR WHERE CENTER HINGE OF LT REV COWL ATTACHES, NR 1 PYLON. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-33-01. 2 L 7 3 4F A22WE 1998021900544 19980219 00544 WP 1998 2 19 CALA9800244 1 19980213 A 5400 WEB DOUG DC10 DC1010 3022110 WP NR 1 PYLON CANNED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND UPPER SPAR WEB OF NR 1 PYLON OIL CANNED FORWARD OF HEAT EXCHANGER. A NEW WEB WAS FABRICATED AND INSTAL LED IAW SRM 54-11-2 AND 51-31-01. 2 L 7 3 4F A22WE 1998021900545 19980219 00545 WP 1998 2 19 CALA9800245 1 19980213 A 5753 STOP DOUG DC10 DC1010 3022110 WP LT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION AT TOP OF LEFT INBOARD FLAP OUTBOARD UPSTOP PLATE STRUCTURE ON TRAILING EDGE OUTBOARD NR 1 SP OILER PANEL. THE CORRODED U CHANNEL WAS REMOVED IAW SRM 51-21-01. A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 5 1-10-00, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998021900546 19980219 00546 WP 1998 2 19 CALA9800246 1 19980213 A 5720 BEAM DOUG DC10 DC1010 3022110 WP LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON BEAM ALONG AFT END OF ACCESS OPENING 541AB ON LT WING INBOARD LOWER TRAILING EDGE. THE BE AM WAS REMOVED AND REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1998021900547 19980219 00547 WP 1998 2 19 CALA9800247 1 19980213 A 5753 SKIN DOUG DC10 DC1010 3022110 WP NR 3 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 3.5 CRACK IN LT WING UPPER LEADING EDGE SKIN AT NR 3 SLAT ANTI-ICE TELESCOPING DUCT SPRING DOOR CUTOU T CORNER. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5730-01543. 2 L 7 3 4F A22WE 1998021900548 19980219 00548 WP 1998 2 19 CALA9800248 1 19980213 A 5730 SKIN DOUG DC10 DC1010 3022110 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION INSIDE SKIN FORWARD OF FRAME SPAR, AFT OF NR 8 SLAT CENTER AREA OF RT WING OUTBOARD LEADING E DGE. THE CORROSION WAS REMOVED IAW SRM 51-22-01. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AN D INSTALLED IAW SRM 57-10-00 AND 51-21-01. 2 L 7 3 4F A22WE 1998021900549 19980219 00549 WP 1998 2 19 CALA9800249 1 19980213 A 5730 SKIN DOUG DC10 DC1010 3022110 WP WS 885 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT WING OUTBOARD LEADING EDGE SKIN CORRODED UNDER NUT CHANNEL INSIDE SURFACE, FORWARD OF FRONT SPAR AFT OF NR 7 SLAT OUTBOARD AREA, XORS 885. THE CORROSION WAS REMOVED. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLER W AS FABRICATED AND INSTALLED IAW SRM 57-10-00 AND 51-21-01. 2 L 7 3 4F A22WE 1998021900550 19980219 00550 NM 1998 2 19 CALA9800250 1 19980212 A 5755 SKIN BOEING 727 727224 1384076 NM NR 4 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1.375 CRACK IN LT WING NR 4 SPOILER AT LOWER SKIN JUST INBOARD OF SECOND FROM INBOARD HINGE. THE NR 4 SPOILER WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1998021900551 19980219 00551 NM 1998 2 19 CALA9800251 1 19980212 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FOREFLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND LT INBOARD FOREFLAP INBOARD TRAILING EDGE SKIN DEBONDED WITH CHAFE MARKS ALONG UPPER SURFACE. THE FORE FLAP WAS REMOVED, REPAIRED AND REPLACED. 2 L 7 3 4F A3WE 1998021900552 19980219 00552 NM 1998 2 19 CALA9800252 1 19980212 A 5720 DOUBLER BOEING 727 727224 1384076 NM RT WINGTIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 2 INCH CRACK IN DOUBLER OF RT WINGTIP TRAILING EDGE AT WBL 626. THE WINGTIP WAS REMOVED AND A NEW DO UBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. THE WINGTIP WAS REINSTALLED IAW SRM 51-30-2 AND MM 33-40-0. 2 L 7 3 4F A3WE 1998021900553 19980219 00553 NM 1998 2 19 CALA9800253 1 19980212 A 5712 RIB BOEING 727 727224 1384076 NM RT WINGTIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1.5 CRACK IN WINGTIP MOUNT RIB AT WINGTIP AREA AFT OF NAV STROBE LIGHT. AN ANGLE DOUBLER WAS FABRICA TED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998021900554 19980219 00554 NM 1998 2 19 CALA9800254 1 19980212 A 5730 SKIN BOEING 727 727224 1384076 NM LT WINGTIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .625 INCH CRACK AND TWO SHEARED FASTENERS IN LEFT WINGTIP LOWER TRAILING EDGE SKIN. THE FASTENERS WE RE REMOVED AND THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-40-02. 2 L 7 3 4F A3WE 1998021900555 19980219 00555 NE 1998 2 19 9802496608 2 19980210 A 7200 ENGINE BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 1 FAILED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 01 608US 19785 662645 WHILE AT CRUISE, THE NR 1 ENGINE OIL QUANTITY DECREASED TO ZERO WITH THE PRESSURE AT 25 PSI. THE ENGINE WAS SHUT DOWN A ND THE AIRCRAFT RETURNED TO NRT. MAINTENANCE REPLACED THE NR 1 ENGINE THE EXACT PART CAUSING DIFFICULTY TO BE DETERMINE D. 2 L 7 4 4F 4 F A20WE E20EA 1998021900556 19980219 00556 WP 1998 2 19 9802549763 1 19980211 A 3350 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 763NW 47396 DURING LINE CHECK, FOUND FORWARD OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900557 19980219 00557 WP 1998 2 19 9802559857 1 19980211 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 766NC 47739 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F RT A6WE 1998021900558 19980219 00558 WP 1998 2 19 9802569993 1 19980211 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 14 AND 17 AND AFT OVERWING EMERG ENCY EXIT DOOR LIGHTS INOPERATIVE. REPLACED FUSE IN BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900559 19980219 00559 WP 1998 2 19 9802579979 1 19980210 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 9343 47439 FAA INSPECTOR OBSERVED FORWARD OVERHEAD EMERGENCY LIGHTS AS BEING WEAK. MAINENANCE REPLACED THE BATTERY PACK. OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900560 19980219 00560 NM 1998 2 19 9802586642 1 19980209 A 7603 250673 CONTROL CABLE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE DISCONNECTED A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 642NW 1802 1802 21942 702134 ON TAKEOFF ROLL (PEK), THE NR 4 ENGINE DID NOT RESPOND TO POWER LEVER MOVEMENT AND THE TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE POWER LEVER PUSH/PULL CABLE DISCONNECTED AT THE CABLE DRUM IN THE STRUT AREA. REPLACED THE CABLE DRUM. OPER ATIONAL CHECK NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1998021900561 19980219 00561 WP 1998 2 19 9802599911 1 19980212 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 961N 47405 DURING PERIODIC CHECK, FOUND TAILCONE CATWALK AND RELEASE HANDLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900562 19980219 00562 WP 1998 2 19 9802609758 1 19980210 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT FORWARD OVERWING EMERGENCY EXIT SIGN LIGHT INOPERATIVE. REPLACED BATTER Y PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900563 19980219 00563 WP 1998 2 19 9802619758 1 19980211 A 3350 CONNECTOR DOUG DC9 DC941 302207N WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT RIGHT FORWARD EMERGENCY EXIT AND BETWEEN ROWS 5 THROUGH 8 INOPERATIVE. MAINTNANCE FOUND LOOSE CONNECTION AT FORWARD EMERGENCY EXIT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900564 19980219 00564 WP 1998 2 19 9802629855 1 19980211 A 2150 CLAMP DOUG DC9 DC951 3022051 WP AC COMPARTMENT LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 764NC 47717 DURING CLIMB-OUT, THE TAIL COMPARTMENT TEMPERATURE HIGH INDICATION LIGHT ILLUMINATED. FLIGHT CREW FOLLOWED COM PROCEDUR E AND LANDED AT ALTERNATE AIRPORT WITHOUT INCIDENT. MAINTENANCE RESECURED THE PNEUMATIC CROSSFEED VALVE PUSHROD AND TIG HTENED THE AIR CONDITIONING SHUTOFF VALVE CLAMP. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021900565 19980219 00565 NM 1998 2 19 9802632290 1 19980212 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 290US 21378 DURING PREFLIGHT, FOUND AFT ENTRY EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998021900566 19980219 00566 NM 1998 2 19 9802646614 1 19980215 A 2910 HYDRAULIC LINE BOEING 747 747251B 1384892 NM NR 1 PYLON LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 01 614US 20359 DURING APPROACH, THE NR 1 HYDRAULIC SYSTEM DEPLETED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. RE PLACED THE NR 1 ENGINE DRIVEN PUMP AND PRESSURE LIN IN PYLON AREA. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998021900567 19980219 00567 WP 1998 2 19 9802659863 1 19980214 A 2131 CONTROLLER DOUG DC9 DC951 3022051 WP CABIN FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 722NC 47774 DURING CLIMB-OUT, THE CABIN AUTOMATIC PRESSURIZATION SYSTEM BECAME INOPERATIVE AND THE CABIN MANUAL PRESSURIZATION CONTR OL SYSTEM OPERATED POORLY. THE FLIGHT RETURNED TO SAT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CABIN PRES SURE CONTROLLER, CABIN CONTROL RESET REGULATOR, AND CLEANED THE CABIN CONTROL EJECTOR. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021900568 19980219 00568 WP 1998 2 19 9802669102 1 19980213 A 3350 BATTERY DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 92S 47064 DURING LINE CHECK, FOUND FLOOR EMERGENCY EXIT LIGHTS INOPERATIVE AT MID CABIN. MAINTENANCE REPLACED THE BATTERY. OPERA TIONAL CHECK OK. 2 L 7 2 4F A6WE 1998021900569 19980219 00569 WP 1998 2 19 9802679866 1 19980213 A 3260 0080004003 PROX CONTROL DOUG DC9 DC951 3022051 WP E/E COMPARTMENT INOPERATIVE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 775NC 35555 35555 47785 DURING CLIMB-OUT, THE LEFT MAIN LANDING GEAR UNLOCK INDICATION LIGHT REMAINED ILLUMINATED WITH ALL OTHER INDICATIONS NOR MAL. THE FLIGHT CREW RECYCLED THE LANDING GEAR HANDLE AND FOUND NORMAL OPERATION AND INDICATION OF THE LANDING GEAR SYS TEM. AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR PROXIMITY CONTROL UNIT. O PERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998021900570 19980219 00570 WP 1998 2 19 9802689978 1 19980213 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 9342 47391 AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY AND FLASHLIGHT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900571 19980219 00571 WP 1998 2 19 9802699919 1 19980215 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 941N 47450 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 11 AND 13 INOPERATIVE. REPLACED BLOWN FUSE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900572 19980219 00572 WP 1998 2 19 9802709915 1 19980214 A 2611 SMOKE DETECTOR DOUG DC9 DC931 3022065 WP LAVATORY MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 GL 01 965N 47417 FORWARD LAVATORY SMOKE DETECTOR ACTIVATED ALONG WITH BURNING SMELL IN FLIGHT. FLIGHT CREW PULLED ASSOCIATED CIRCUIT BRE AKERS AND RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE RESET CIRCUIT BREAKERS. ALSO, REPLACED SMOKE DETECTOR AND BOTH BALLASTS IN LAVATORY AS A PRECAUTION. NO EVIDENCE OF SMOKE OR OVERHEAT CONDITION WAS APPARENT. AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4F A6WE 1998021900573 19980219 00573 WP 1998 2 19 9802719997 1 19980214 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT ROW 8 INOPERATIVE. REPAIRED WIRING AT FLOOR NEAR ROW 8. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021900574 19980219 00574 SO 1998 2 19 COMA9810042 1 19980211 A 5270 MS230851 SWITCH EMB 120 EMB120RT SO CARGO DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 463CA 120267 CARGO DOOR WARNING AFTER TAKE OFF. ADJUSTED CARGO DOOR AFT MICROSWITCH. 2 L 7 2 4T RT A31SO 1998021900575 19980219 00575 SO 1998 2 19 COMA9810043 1 19980210 A 3230 MS34762106P CONNECTOR EMB 120 EMB120RT SO RT MLG LOOSE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 241CA 120211 LANDING GEAR CONTROL COULD NOT BE SELECTED UP. GROUND SAFETY LOCK ENGAGED. SECURED LOOSE QUICK DISCONNECT COUPLING AT RIGHT HAND MLG WEIGHT ON WHEELS PROXIMITY SENSOR WIRING HARNESS. 2 L 7 2 4T RT A31SO 1998021900576 19980219 00576 SO 1998 2 19 COMA9810044 1 19980210 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 259CA 20216 85 120252 EMERGENCY EXIT LIGHTS AT ROW 5 ARE INOP. REPLACED THE NR 2 EMERGENCY BATTERY PACK. 2 L 7 2 4T RT A31SO 1998021900577 19980219 00577 NE 1998 2 19 COMA9810045 2 19980210 A 7321 ECU EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 137H 120137 THE RIGHT PROPELLER RPM FLUCTUATED BETWEEN 100 AND 102.5 PERCENT AFTER TAKEOFF. DEFERRED THE RIGHT ENGINE ELECTRONIC CO NTROL SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021900578 19980219 00578 EA 1998 2 19 COMA9860040 1 19980211 A 3150 WARNING SYST CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 969CA 7141 LEFT STATIC HEAT AND LEFT AOA HEAT CAUTION MESSAGE. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4F RT A21EA 1998021900579 19980219 00579 EA 1998 2 19 COMA9860041 1 19980211 A 3350 20131A BATTERIES CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951CA 7091 EMERGENCY LIGHTING IS INOP. REPLACED THE EMERGENCY LIGHTING BATTERIES. 2 L 7 2 4F RT A21EA 1998021900580 19980219 00580 NE 1998 2 19 COMA9860042 2 19980210 A 7261 5077T94P02 TUBE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE LOOSE A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 976CA 7151 RIGHT ENGINE OIL PRESSURE DROPPED TO 25 PSI. ENGINE WAS SHUT-DOWN DURING FLIGHT. TIGHTENED LOOSE OIL LINE AT ENGINE LU BE PUMP. REPLENISHED 6 QUARTS OF OIL AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998021900581 19980219 00581 EA 1998 2 19 COMA9860043 1 19980214 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 EA RT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 934CA 9094 7042 CO-PILOTS SIDE WINDOW SHATTERED. REPLACED CO-PILOTS SIDE WINDSHIELD. 2 L 7 2 4F RT A21EA 1998021900582 19980219 00582 EA 1998 2 19 COMA9860044 1 19980212 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 979CA 7159 ONE SECTION OF EMERGENCY FLOOR LIGHTING IS INOP AND ONE EMERGENCY EXIT SIGN INOP. DRIED WET FLOOR LIGHTING AND REPLACED EXIT SIGN LIGHT BULB. 2 L 7 2 4F RT A21EA 1998021900583 19980219 00583 NM 1998 2 19 SWAA980092 1 19980128 A 5730 SKIN BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 28SW 21338 DURING SCHEDULED D CHECK, FOUND WING FIXED L/E SKIN CRACKED .75 PROTRUDING THROUGH FASTENER ON T/E OF SKIN JUST I/B OF E NG PYLON ON TOP OF WING. REPAIRED PER SWA RA 1-257-0524. 2 L 7 2 4F A16WE 1998021900584 19980219 00584 NM 1998 2 19 SWAA980093 1 19980203 A 5320 STIFFENER BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED C-CHECK, FOUND VERTICAL STIFFENER CRACKED AT TOP LIGHTING HOLE (APPROX 12 BELOW FLOOR LEVEL) AT FUSELAG E STA 540, 25 RT OF CENTERLINE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998021900585 19980219 00585 NM 1998 2 19 SWAA980094 1 19980203 A 5312 BULKHEAD SUPPORT BOEING 737 7372H4 138448C NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 29SW 21340 DURING SCHEDULED C1 CHECK, FOUND FWD BULKHEAD RT WING SUPPORT FRAME I/B FLANGE HAS 2 CRACK STA 663 AND STRINGER 18. REP AIRED PER BOEING S/B. 2 L 7 2 4F A16WE 1998021900586 19980219 00586 NM 1998 2 19 SWAA980095 1 19980203 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 790 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, DOUBLER CRACKED ABOVE STR 10R, B/S790. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998021900587 19980219 00587 NM 1998 2 19 SWAA980096 1 19980203 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND STR TO FRAME CLIP CRACKED B/S 360, STR 4 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998021900588 19980219 00588 NM 1998 2 19 SWAA980097 1 19980202 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND STR 10 RT AT BS 540 HAS CRACKED STR SPLICE FITTING PER HFEC. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998021900589 19980219 00589 NM 1998 2 19 SWAA980098 1 19980202 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED STR 14R B/S 908-937, WITH HFEC ROTATING PROBE INS PECTION. REPAIRED PER ACO 6717-53 PART II AND XEA X2-53-194. 2 L 7 2 4F A16WE 1998021900590 19980219 00590 NM 1998 2 19 SWAA980099 1 19980202 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 990 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED STR 14L B/S 990-1016, WITH HFEC ROTATING PROBE INS PECTION. REPAIRED PER ACO 6717-53 PART II AND XEA X2-53-194. 2 L 7 2 4F A16WE 1998021900591 19980219 00591 1998 2 19 SWAA980100 4 19980129 A 2565 1061323425 SLIDE BOEING 737 7372H4 138448C NM CABIN LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23019 DURING SCHEDULED A2, FOUND AFT ENTRY DOOR EMERGENCY EXIT SLIDE LOW PRESSURE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998021900592 19980219 00592 NM 1998 2 19 SWAA980101 1 19980120 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 67SW 22356 DURING SCHEDULED RON, FOUND GALLEY EMERGENCY EXIT LIGHT FELL OUT OF ITS BRACKET DURING CLIMB-OUT. THE BATTERY IN IT APP EARS DAMAGED. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998021900593 19980219 00593 NM 1998 2 19 SWAA980103 1 19980128 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED A2, FOUND 4 IN SKIN CRACK RT SIDE JUST AFT AND ABOVE NR 12 CABIN WINDOW. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900594 19980219 00594 NM 1998 2 19 SWAA980102 1 19980203 A 5730 SKIN BOEING 737 7373H4 1384600 NM BS 790 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22994 DURING SCHEDULED T-CHECK, FOUND SKIN CRACKS AT BS 790 STR 19 AND 20. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900595 19980219 00595 1998 2 19 SWAA980104 4 19980205 A 2565 D31354433 SLIDE BOEING 737 7375H4 138449D NM AFT ENTRY TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR SLIDE GIRT BAR MATERIAL TORN/FRAYED. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998021900596 19980219 00596 NM 1998 2 19 SWAA980105 1 19980129 A 5730 SKIN BOEING 737 7373H4 1384600 NM BS 943 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED TERM CHECK, FOUND 1.5 CRACK IN FUSELAGE EXTERIOR SKIN BS 943 STR 24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900597 19980219 00597 NM 1998 2 19 SWAA980106 1 19980131 A 5730 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED TERM CHECK, FOUND 6 IN FUSE SKIN CRACK RT SIDE ABOVE AND AFT OF NR 12 CABIN WINDOW. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998021900598 19980219 00598 NM 1998 2 19 SWAA980107 1 19980205 A 5730 SKIN BOEING 737 7373H4 1384600 NM R2 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C3 CHECK, FOUND R2 DOOR LOWER FUSELAGE HINGE CUTOUT FUSELAGE SIDE CRACKED 1.52. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998021900599 19980219 00599 NM 1998 2 19 SWAA980108 1 19980205 A 5711 RIB BOEING 737 7373H4 1384600 NM WS 208 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED C3 CHECK, FOUND L/E RIB AT WS 208 DAMAGED BY KRUEGER FLAP SCREW. GOUGE STARTS AT VERTICAL WEB AND CONT INUES .375 INCH ACROSS ANGLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900600 19980219 00600 NM 1998 2 19 SWAA980109 1 19980208 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 372 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED TERM CHECK, FOUND 4 INCH CRACK AT BS 372, 14 ABOVE FLOOR LINE ON LT SIDE OF A/C. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998021900601 19980219 00601 NM 1998 2 19 SWAA980110 1 19980131 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED 1/4 D CHECK, FOUND FLOORBEAM CRACKED UPPER SIDE AT BS 480 RBL 13. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900602 19980219 00602 NM 1998 2 19 SWAA980111 1 19980131 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 420-440 DOUBLE DRILLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED 1/4 D CHECK, FOUND FLOORBEAM HAS 12 DOUBLE DRILLED HOLES FROM BS 420-440 RBL 13. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900603 19980219 00603 NM 1998 2 19 SWAA980112 1 19980204 A 5312 BULKHEAD SKIN BOEING 737 7373H4 1384600 NM BS 178 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED A1 CHECK, FOUND BS 178 BLKHD AND SKIN DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900604 19980219 00604 NM 1998 2 19 SWAA980113 1 19980205 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 178 BLKHD 2 FT BELOW CAPT WINDOW AND RT FIXED L/E 4 FT FRO M FUSELAGE. REPAIRED PER SWA MPM. 2 L 7 2 4F RT A16WE 1998021900605 19980219 00605 NM 1998 2 19 SWAA980114 1 19980201 A 5330 SKIN BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUT-OUT CRACKED. REPAIRED PER SWA RA 1-353-1763. 2 L 7 2 4F RT A16WE 1998021900606 19980219 00606 NM 1998 2 19 SWAA980115 1 19980203 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 353SW 24889 DURING SCHEDULED 1/4 D CHECK, FOUND CRACK IN BS 178 SKIN AT RBL 1 WL 186. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998021900607 19980219 00607 1998 2 19 SWAA980116 4 19980204 A 2565 D31591474 SLIDE BOEING 737 7375H4 138449D NM PAX DOOR OUT OF DATE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED A-2 CHECK, FOUND FWD ENTRY DOOR SLIDE ASSY INSPECTION DUE. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998021900608 19980219 00608 NM 1998 2 19 SWAA980117 1 19980205 A 3350 20121 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING PRE-FLIGHT INSPECTION, FIRST 3 FLOOR PROX LIGHTS AT FRONT OF AIRCRAFT ARE INOP. REPAIRED FLOOR TRACK AT ROW 3ABC . 2 L 7 2 4F RT A16WE 1998021900609 19980219 00609 NM 1998 2 19 UPS98225723 1 19980101 A 5753 653273416 FITTING BOEING 727 7272A1 138407F NM NR 8 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:SI NR 8 FLAP TRACK FWD ATTACH FITTING IS CORRODED AROUND FLAP TRACK FWD ATTACH POINT BUSHING, AND BUSHIN G MIGRATED AND CORROSION IN FAIL/SAFE STRAP ATTACH POINT BOLT HOLES FWD ATTACH HARDWARE REQUIRES REPLACEMENT OUTBOARD AN D INBOARD. REWORKED AND INSTALLED FLAP TRACK SUPPORT FITTING PER ENGINEERING REPAIR NO 98-2085 AND MM 25-51-31. 2 L 7 3 4F A3WE 1998021900610 19980219 00610 NM 1998 2 19 UPS98225724 1 19980205 A 5330 SKIN BOEING 727 7272A1 138407F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 214UP 21342 INSPECTION TYPE:SI CORROSION (C53-224-01.00-02) ON INTERIOR OF SKIN AROUND PERIMETER OF SIDELIGHT BETWEEN BS 720B PLUS 5 AND 720C LBL 73 WL 218-228 BETWEEN STR 14L AND 16L. CORROSION OUT OF LIMITS IAW SRM 53-30-3. REPAIRED SKIN AROUND PER IF OF LT SIDELIGHT IAW BFG/TRAMCO EO 98-2051 UPS FILE NR 727-53-1995. 2 L 7 3 4F A3WE 1998021900611 19980219 00611 NM 1998 2 19 UPS98225728 1 19980211 A 5400 WEB BOEING 727 72722C 138400F NM BS 1381.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL, RT SIDE AT STATION 1381.5. WEB FABRICATED AND F ITTED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1998021900612 19980219 00612 WP 1998 2 19 UPS98825731 1 19980122 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, FWD LOWER CARGO COMPARTMENT LONGERON 36 CRACKED FROM FWD TORQUE BOX TO STA 220. REMOVED LONGERONS , REMOVED CORROSION FROM HANGER IAW DC8 SRM 51 1 8. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. DRILLED NEW LONGERONS FOR F IT IAW DC8 SRM 51 1 24. INSTALLED LONGERONS WITH HI-LOKS IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998021900613 19980219 00613 WP 1998 2 19 UPS98825732 1 19980124 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, LOWER FWD CARGO COMPARTMENT STA 300 BATH TUB FITTING CORRODED LONGERON 36 TO LONGERON 35 RIGHT. REMOVED FITTING REPLACED WITH NEW FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998021900614 19980219 00614 WP 1998 2 19 UPS98825733 1 19980130 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 190-390 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, L33 LEFT STA 190 TO 390 REQUIRED REPLACEMENT. REMOVED LONGERON STA 190-390, DRILLED NEW LONGERON HALVES IAW DC8 SR M 51 1 24. INSTALLED LONGERON WITH HI-LOKS AND RIVET6S IAW DC8 SRM 5 1 1 20D AND 51 1 21. 2 L 7 4 4F RT 4A25 1998021900615 19980219 00615 WP 1998 2 19 UPS98825734 1 19980127 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, AFT PIT BOTTOM OF CABIN FLOOR CORRODED 4 PLACES, BTL 12 L, 34R, 12R, AND 34R, STA 1240. CUT OUT DAMAGED IAW DC8 SRM 53 2 3 FIG 10, FABBED DOUBLERS FILLER, REPAIRED ANGLE AND INSTALLED IAW DC8 SRM 53 2 3 FIG 10, DC8 SRM 51 1 21, 51 1 20D. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. 2 L 7 4 4F RT 4A25 1998021900616 19980219 00616 NM 1998 2 19 UPS98225735 1 19980213 A 5751 FITTING BOEING 727 72751C 1384015 NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, I/B CENTER HINGE FITTING ON AILERON SIDE IS CORRODED ON O/B AILERON L/W. REMOVED AND REPLACED L/W O /B AILERON CENTER HINGE FITTING AILERON SIDE IAW SRM 51-30-2 AND 51-30-5. 2 L 7 3 4F A3WE 1998021900617 19980219 00617 NM 1998 2 19 UPS98225736 1 19980204 A 5315 FLOORBEAM BOEING 727 72751C 1384015 NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION (C53-224-01.05-01) ON TOP OF BS 312 FLOORBEAM, LBL 3, WL 208. CORROSION FOUND TO BE OUT O F LIMITS PER SRM 53-10-1 DAMAGED AREA REMOVED AND STANDARD REPAIR PERFORMED IAW WITH SRM 53-10-08 AND SRM 51-30-7. 2 L 7 3 4F A3WE 1998021900618 19980219 00618 NM 1998 2 19 UPS98225737 1 19980212 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 730-735 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION ON STRINGER 23L BS 730 TO 735 WL 155. REMOVED FASTENERS AND CUT STRINGER AT BS 712. INS TALLED STRINGER REPAIR PER SRM 53-10-3 FROM BS 712 TO 726, 726 TO 740 CORROSION FOUND WITHIN LIMITS. 2 L 7 3 4F A3WE 1998021900619 19980219 00619 NM 1998 2 19 UPS98225738 1 19980212 A 5320 652647356 ANGLE BOEING 727 72751C 1384015 NM BS 868 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION ON OUTBD SIDE OF INBD EXPANSION LINK STA 868, LBL 35, WL 161. REMOVED AND REPLACED EXPANS ION LINK ATTACH ANGLES IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998021900620 19980219 00620 NM 1998 2 19 UPS98225739 1 19980210 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 243 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) AROUND FASTENERS ON FRAME BS 243, RBL 25, WL 166. CORROSION OUT OF LIM ITS. REMOVED CORROSION, FABRICATED FILLER AND DOUBLER, INSTALLED IAW SRM 51-40-2, 51-10-2, 51-20-151. 2 L 7 3 4F A3WE 1998021900621 19980219 00621 NM 1998 2 19 UPS98225740 1 19980210 A 5320 6526312118 STIFFENER BOEING 727 72751C 1384015 NM BS 294 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION ON VERTICAL STIFFENER AT STA 294, RBL 5, WL 193 ON STIFFENER STRAP. REMOVED AND REPLACED STRAP ON STIFFENER IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998021900622 19980219 00622 NM 1998 2 19 UPS98225741 1 19980210 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 575 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION ON STR 21 RT, BS 575, WL 178. REMOVED DAMAGED SECTION OF STRINGER AND SPLICED IN REPAIR S ECTION IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1998021900623 19980219 00623 NM 1998 2 19 UPS98225742 1 19980210 A 5320 WEB BOEING 727 72751C 1384015 NM BS 243-251 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:S, CORROSION (C53-111-01.00-01) ON NOSE WHEELWELL PRESSURE WEB BS 243-251, LBL 235, WL 168-172 (AREA MAR KED). REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-02. REPAIRED PER SRM 53-10-9, 51-10-02. 2 L 7 3 4F A3WE 1998021900624 19980219 00624 NM 1998 2 19 UPS98225743 1 19980202 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 492-497 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION (SDN 53-111-01.00-02) ON STR 25 LT BS 492-497 WL 160. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED SECTION AND COMPLETED STANDARD REPAIR IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1998021900625 19980219 00625 NM 1998 2 19 UPS98225744 1 19980203 A 5320 INTERCOSTAL BOEING 727 72751C 1384015 NM BS 211.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE:SI, CORROSION (C53-111-01.00-01) ON INTERCOSTAL BS 211.8, RBL 25, WL 176. CORROSION OUT OF LIMITS. REM OVED INTERCOSTAL, FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 51-20-1, 51-10-3. 2 L 7 3 4F A3WE 1998021900626 19980219 00626 NM 1998 2 19 UPS98225745 1 19980213 A 5751 FITTING BOEING 727 72722C 138400F NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, RIGHT OUTBOARD AILERON PUSHROD ATTACH FITTING ON AILERON HAS SURFACE CORROSION AROUND LUG HOLES, FITT ING REPLACED IAW DRAWING 65-21766. 2 L 7 3 4F A3WE 1998021900627 19980219 00627 NM 1998 2 19 UPS98225746 1 19980206 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1245 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE:C, CRACK ON SKIN, AFT ENTRY STAIRS CENTER LINE APPROX BS 1245. REPAIR CARRIED OUT IAW SRM 53-10-2 FIGUR E 3. 2 L 7 3 4F A3WE 1998021900628 19980219 00628 NM 1998 2 19 UPS98425764 1 19980213 A 5240 FRAME BOEING 747 747123F NM LT SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 673UP 20325 REF LP 254182 ITEM 1 AND THIS LP ITEM 1, FOUND AFT LOWER CORNER OF NR 4 LEFT SERVICE DOOR, VERTICAL FRAME AND HORIZONTAL LOWER EDGE BEAM CRACKED IN RADIOUS. INSTALLED REPAIR DOUBLERS AS PER SRM 52-10-02. PRESSURE CHECK TO BE DONE ON LP 25 4184 ITEM 3, NO LEAKS NOTED. 2 L 7 4 4F A20WE 1998021900629 19980219 00629 NM 1998 2 19 UPS98425765 1 19980214 A 3350 LIGHT BOEING 747 747123F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 674UP 20100 EMERGENCY LIGHT OUT MAIN DECK STA 600 RT. NO EMERGENCY LIGHTING SYSTEM INSTALLED THIS POSITION. 2 L 7 4 4F A20WE 1998021900630 19980219 00630 WP 1998 2 19 UPS98825747 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, RT WING L/E AT STA XOLDI 6.225, THE UPPER L/E RIB HAS A 9 INCH CRACK. REPAIRED CRACKED L/E RIB AT ST A XOLDI 6.225 IAW DC-8 SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998021900631 19980219 00631 WP 1998 2 19 UPS98825748 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 747.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XF S747.500. REPAIRED IAW DC-8 SRM 5 7-2-0. 2 L 7 4 4F RT 4A25 1998021900632 19980219 00632 WP 1998 2 19 UPS98825749 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA, XFS 760.000, REPAIRED IAW DC8 SRM 57 -2-0. 2 L 7 4 4F RT 4A25 1998021900633 19980219 00633 WP 1998 2 19 UPS98825750 1 19980207 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 201.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM IS CRACKED BY AFT FASTENER AT STA XFS 201.250. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900634 19980219 00634 WP 1998 2 19 UPS98825751 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 797.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING LE RIB UPPER AND LWR ARM CRACKED BY AFT FASTENER AT STA XFS 797.500, REPAIRED IAW SRM ADDN DC 8-5720-4087. 2 L 7 4 4F RT 4A25 1998021900635 19980219 00635 WP 1998 2 19 UPS98825752 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 822.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER AT STA XFS 822.500. REPAIRED IAW SRM 57-2 -0. 2 L 7 4 4F RT 4A25 1998021900636 19980219 00636 WP 1998 2 19 UPS98825753 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 728.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA 728.750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900637 19980219 00637 WP 1998 2 19 UPS98825754 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 766.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER STA XFS 766.250. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900638 19980219 00638 WP 1998 2 19 UPS98825755 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 810.000. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900639 19980219 00639 WP 1998 2 19 UPS98825756 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER STA XFS- 772.500. REPAIRED IAW SRM 57-2-0 . 2 L 7 4 4F RT 4A25 1998021900640 19980219 00640 WP 1998 2 19 UPS98825757 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 785.000. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900641 19980219 00641 WP 1998 2 19 UPS98825758 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 791.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FASTENER AT STA XFS 791.250. REPAIRED IAW SRM 57-2 -0. 2 L 7 4 4F RT 4A25 1998021900642 19980219 00642 WP 1998 2 19 UPS98825759 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FSTR XFS 778.750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900643 19980219 00643 WP 1998 2 19 UPS98825760 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 803.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER AND LWR ARMS CRACKED BY AFT FSTR AT STA XFS803. 750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900644 19980219 00644 WP 1998 2 19 UPS98825761 1 19980209 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER STA 772.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900645 19980219 00645 WP 1998 2 19 UPS98825762 1 19980210 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C, RT WING L/E AT STR XFS 653.750, THE L/E RIB IS CRACKED. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900646 19980219 00646 WP 1998 2 19 UPS98825763 1 19980209 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR AT STA XFS 810.000. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998021900647 19980219 00647 EU 1998 2 19 WWMA9800030 1 19980212 A 3260 387 BULB SAAB SF340 340B 7860101 EU RT MLG DEFECTIVE A WWMA O OTHER P NO WARNING INDICATION LD LANDING 1 WP 15 297AE 340B297 RIGHT MAIN LANDING GEAR INDICATOR DID NOT ILLUMINATE ON THE FIRST GEAR EXTENSION ATTEMPT. IT FUNCTIONED NORMALLY ON THE SECOND TRY. AT THE GATE, THE LIGHT WENT OUT. MAINTENANCE REPLACED THE RIGHT INDICATOR BULB, CLEANED THE DOWNLOCK SWIT CH AND PERFORMED GEAR EXTENSION CHECKS. 2 L 7 2 4T RT A52EU 1998021900648 19980219 00648 EU 1998 2 19 WWMA9800029 1 19980216 A 3350 LIGHT SAAB SF340 340B 7860101 EU COCKPIT ILLUMINATED A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 280AE 340B280 DURING TAXI, THE EMERGENCY CALL LIGHT CAME ON AND WOULD NOT GO OUT. AIRCRAFT REURNED TO THE GATE, MAINTENANCE RESET THE PANEL AND PERFORMED OPERATIONAL CHECKS. 2 L 7 2 4T RT A52EU 1998021900649 19980219 00649 EU 1998 2 19 WWMA9800028 1 19980215 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 335AE 340B335 DURING PREFLIGHT, THE EMERGENCY EXIT LIGHT AT ROW 11A WOULD NOT ILLUMINATE. REPLACED BULB. 2 L 7 2 4T RT A52EU 1998021900650 19980219 00650 EU 1998 2 19 WWMA9800027 1 19980215 A 2120 AIR DISTRIBUTION SAAB SF340 340B 7860101 EU COCKPIT ODOR A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 338SB 340B338 CREW REPORTED A HOT SMELL OR BURNING INSULATION IN THE COCKPIT BUT NO SMOKE NOTED. MAINTENANCE REMOVED THE AVIONICS RAC K DOOR AND PANELS, CIRCUIT BREAKER PANELS, ACP, BOTH EFIS SCREENS, HOT JUGS, GALLEY LIGHTS AND THE TAPE PLAYER. INSPECT ED ALL AREAS, FOUND NO DAMAGE AND COULD DUPLICATE ANY ABNORMAL SMELL. 2 L 7 2 4T RT A52EU 1998021900651 19980219 00651 EU 1998 2 19 QXEA9800062 1 19980206 A 3310 16444 TRANSFORMER FOKKER FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 491US 11156 SEA - ELECTRICAL SMOKE FROM LOWER LEFT CAPTAIN’S INSTRUMENT PANEL. MAINTENANCE INSPECTED AND FOUND VARIABLE POWER TRANS FORMER IN CAPTAINS LEFT SIDE PANEL MELTED. REMOVED TRANSFORMER AND CAPPED WIRES. MAIN INSTRUMENT LIGHTING LT CIRCUIT B REAKER PULLED AND COLLARED. DEFERRED INSTRUMENT FLOOD LIGHTS PER MEL 33-1. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998021900652 19980219 00652 EU 1998 2 19 QXEA9800065 1 19980211 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 BOI - EMERGENCY LIGHT ON RIGHT SIDE ROW 8 IS INOP. MAINTENANCE REPLACED BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1998021900653 19980219 00653 NM 1998 2 19 98FDEA00096 1 19980211 A 5320 652083321 CHORD BOEING 727 727233 138408A NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION UPPER CHORD BS 1030, WL 208, LBL 11 TO 21. *S/D* REMOVED CORROSION BS 1030, WL 208, LBL 11 TO 21. FOUND TO BE IN LIMITS PER FED-EX SRM 53-10-01. ALODINED AND PRIMED ALL EFFECTED AREA. 2 L 7 3 4F RT A3WE 1998021900655 19980219 00655 NM 1998 2 19 98FDEA00098 1 19980211 A 5320 652083413 CHORD BOEING 727 727233 138408A NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR 0021 002, CORROSION LOWER CHORD BS 1050, WL 201, RBL 15. REMOVED DAMAGED AREA BS 1050, WL 201, RBL 13. FABRICATED R EPAIR PARTS, ALODINED AND PRIMED. INSTALLED REPAIR PARTS PER FED-EX SRM 53-10-08 FIG 8. 2 L 7 3 4F RT A3WE 1998021900656 19980219 00656 NM 1998 2 19 98FDEA00099 1 19980211 A 5311 BELLFRAME BOEING 727 727227 1384078 NM BS 560 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 NR 0172 71C209-02, BELLFRAME DENTED BS 560L BETWEEN STRINGERS 22-25L. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SR M 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1998021900657 19980219 00657 NM 1998 2 19 98FDEA00100 1 19980211 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 NR 0502 72C235-02, UPPER LOBE BS 720B - 720C, STR 15L CRACKED AT AFT FASTENER FWD OF ICE LIGHT HOUSING. REPAIRED CRACKE D STRINGER PER SRM 53-10-3 FIG 5. 2 L 7 3 4F A3WE 1998021900658 19980219 00658 NM 1998 2 19 98FDEA00101 1 19980211 A 5720 BEAM BOEING 727 727227 1384078 NM LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 NR 0794 7-5750-7-231, LEFT MLG BEAM CORRODED ON UNDERSIDE WHERE NR 4 FLAP TRACK CONTACTS IT. REMOVED CORROSION BLENDED AREA PER EA 7-5730-29358 EA - DATE 2/10/98. 2 L 7 3 4F A3WE 1998021900659 19980219 00659 NM 1998 2 19 98FDEA00102 1 19980206 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0221 BS 720B PLUS 5, STRINGER 15R END CRACKED AT HI-LOK FWD OF WING SCANNING LIGHT. CUT END OF STR HFEC CHECKED CUT EDGE OF STRINGER. FABRICATED U-CHANNEL OF .040 7075-T6 AND FILLERS. INSTALLED REPAIR IAW SRM 53-10-3 FIG 5. 2 L 7 3 4F RT A3WE 1998021900660 19980219 00660 NM 1998 2 19 98FDEA00103 1 19980206 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 420 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 264FE 21626 NR 0752, NR 0754, UPPER LOBE, BS 420, FLOORBEAM HAS DRILL MARK ALMOST THROUGH UPPER LIP AT RBL 6. ADDITIONAL DAMAGE FOU ND IN FLOORBEAM AT RBL 3 UPON REMOVAL OF SEAT TRACK. REMOVED DAMAGED AREAS OF FLOORBEAM AT RBL 3 AND RBL 6, BS 420, AND REPAIRED PER SRM 53-10-8 AND AARD 53-10-07. 2 L 7 3 4F RT A3WE 1998021900661 19980219 00661 NM 1998 2 19 98FDEA00105 1 19980212 A 5320 692083828 CHORD BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR 0025 006 CORROSION ON LOWER CHORD BS 1130, WL 201, LBL 25 TO RBL 25. REPAIRED LOWER CHORD AT BS 1130, WL 201, LBL 62 TO RBL 62. ALL WORK DONE IAW FED-EX EA NR 7-5310-37462. 2 L 7 3 4F RT A3WE 1998021900662 19980219 00662 NM 1998 2 19 98FDEA00104 1 19980212 A 5320 692083920 CHORD BOEING 727 727233 138408A NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION FOUND ON LOWER CHORD AT BS 1148, LBL 30 TO RBL 43, WL 201 FLOORBEAM. *S/D* REMOVED CORROSION BS 1148, LBL 30 TO RBL 43, WL 201. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-01. FABRICATED REPAIR PARTS, ALODINED AND PRIMED PA RTS. INSTALLED ALL REPAIR PARTS PER FED-EX EA NR 7-5310-37464. 2 L 7 3 4F RT A3WE 1998021900663 19980219 00663 NM 1998 2 19 98FDEA00106 1 19980212 A 3610 652244420 DUCT BOEING 727 727225 1384077 NM NR 3 ENGINE CRACKED A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 462FE 22550 IMMEDIATELY AFTER TAKEOFF, FIRE WARNING AND STRUT OVERHEAT NR 3 AND A NR 3 FIRE DETECTOR LIGHT ILLUMINATED. RED TABS PR OCEDURES FOLLOWED. STRUT OVERHEAT LIGHT WENT OUT AFTER ONE MINUTE AT IDLE POWER. ENGINE NR 3 EPR DROPPED .2 EPR BELOW OTHER ENGINES. *S/D* INSTALLED 8TH STAGE AIR DUCT OPERATIONAL. CHECKED GOOD ON THE GROUND NORMAL. 2 L 7 3 4F A3WE 1998021900664 19980219 00664 WP 1998 2 19 98FDEA00107 1 19980213 A 5511 SPAR DOUG DC10 DC1010F 3022111 WP LT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 054FE 47808 LT HORIZONTAL STABILIZER UPPER REAR SPAR CAP FWD BARREL NUT HOLE HAS A 1 INCH LONG CRACK INDICATION ON THE FWD EXPOSED F ACE. THE CRACK IS ONE INCH DOWN AND MARKED. REF WORK CARD 8551073310BPC SEQ 269. *S/D* REPLACED SECTION OF REAR UPPE R SPAR CAP PER EA 8-5510-35976. 2 L 7 3 4F A22WE 1998021900665 19980219 00665 EU 1998 2 19 98FDEA00108 1 19980215 A 2820 EXPANSION VLV AIRBUS 300 A300F4605R 3930327 EU RT FUEL TANK LEAKING A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 657FE 748 98-0041, SHORTLY AFTER T/O NOTICED THAT RT OUTER TANK WAS 1000 LBS LESS THAN LEFT OUTER TANK, CONT TO BURN OUT OF RT OUT ER TANK INSTEAD OF RT INNER. SECURED RT OUTER PUMPS, RT OUTER TANK CONTINUED TO DROP TO 5000 LBS WITH PUMPS OFF, RETURN ED TO MEM. C/W TSM 28-21-00 PG 142, OPS CHECK GOOD. REMOVED AND REPLACED RELAY 139QA, MOCC REQUEST OPS CHECK 28-21-00- 5 PG 504 (AUTO FUEL PUMP ADJ AND TEST) 285851. REPLACED RT INNER TANK THERMAL EXPANSION VALVE AND FUEL DRAIN VALVE. LE AK CHECKS GOOD. 2 L 7 2 4F RT A35EU 1998021900666 19980219 00666 NM 1998 2 19 98FDEA00109 1 19980216 A 5330 6518420111 SKIN BOEING 727 72721C 138400M NM BS 259.5 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 NR 0920 042, WHILE PERFORMING HFEC INSPECTION OF FASTENER HOLES. FOUND CRACK EMANATING FROM HOLE AT BS 259.5, STR 8 R. REPAIRED CRACK AT BS 259.5, STR 8R PER EO 7-5330-7-2319G PT5 AND DRAWING 69-62161. 2 L 7 3 4F A3WE 1998021900667 19980219 00667 NM 1998 2 19 98FDEA00082 1 19980203 A 5311 65163517 FRAME BOEING 727 72725 1384006 NM BS 425 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 156FE 18289 NR 0265 002, CORROSION (C53-224-03(1 AND 2) ON FRAME AT BS 425, LBL 11 - RBL 11, WL 150 (FWD OF E-BAY DOOR). FOUND FRAM E TO BE CORRODED BEYOND LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED BS 425 FRAME LBL 11 - RBL 13, WL 150 PER BO EING DRAWING 65-16351. 2 L 7 3 4F A3WE 1998021900668 19980219 00668 NM 1998 2 19 98FDEA00083 1 19980203 A 5313 652353533 STRINGER BOEING 727 72727C 138400J NM BS 460 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 145FE 19109 NR 0832 035, AFTER ACCESSING SKIN ON NR 0648, FOUND STRINGER 6 LT TO BE CRACKED AROUND A FASTENER HOLE AT BS 460. REMOV ED AND REPLACED LT STRINGER NR 6 SECTION, BS 450-490 IAW FED-EX SRM 53-10-3. 2 L 7 3 4F A3WE 1998021900669 19980219 00669 NM 1998 2 19 98FDEA00084 1 19980203 A 5320 652427626 FITTING BOEING 727 72725 1384006 NM BS 1180 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 156FE 18289 NR 0145 001, CORROSION (C53-224-04) ON BRACKET AT BS 1180, RBL 66, WL 208. CORROSION ON BRACKET AT BS 1180, RBL 66, WL 208 FOUND TO BE OUT OF LIMITS. REMOVED .060 FROM .080 ORIGINAL THICKNESS MATERIAL AS PER FED-EX SRM 53-10-1. REMOVED A ND REPLACED BRACKET PER FED-EX SRM 51-30-2 AND 51-30-5. REMOVED CORROSION ON STR FITTING BS 1180, RBL 66, WL 208 FOUND TO BE 100 PERCENT CORRODED AND OUT OF LIMITS PER FED-EX SRM 53-10-1. FABRICATED STR FITTING FROM .080 7075-TD. HEAT TR EATED TO 7075-T6 AS PER FED-EX SRM 51-20-1 AND INSTALLED PER FED-EX 57-30-2. 2 L 7 3 4F A3WE 1998021900670 19980219 00670 WP 1998 2 19 ABXA9800065 1 19980209 A 5753 995760016 FITTING DOUG DOUG DC9 DC931 3022065 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998021900671 19980219 00671 WP 1998 2 19 ABXA9800066 1 19980209 A 5400 591326237 ANGLE DOUG DOUG DC9 DC931 3022065 WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND LOWER PYLON TO FUSELAGE ATTACK ANGLE AT LEFT PYLON LEADING EDGE CRACKED. REPAIRED ANGLE IAW DC9 S RM 54-04. 2 L 7 2 4F A6WE 1998021900672 19980219 00672 WP 1998 2 19 ABXA9800067 1 19980209 A 5320 CUSP WEB DOUG DOUG DC9 DC931 3022065 WP BS 200-218 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND CUSP WEB AT STA 200-218 RIGHT SIDE CRACKED. REPAIRED CUSP WEB IAW ABX REA D953-22396-MR. 2 L 7 2 4F A6WE 1998021900673 19980219 00673 WP 1998 2 19 ABXA9800068 1 19980209 A 5320 991050131 CUSP WEB DOUG DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND CUSP WEB AT STA 218-237 RIGHT SIDE CORRODED. REPAIRED CUSP WEB IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998021900674 19980219 00674 WP 1998 2 19 ABXA9800069 1 19980209 A 5320 99577375 INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP BS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND INTERCOSTAL AT STA 996 AND LONGERON 13L EXFOLIATED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998021900675 19980219 00675 WP 1998 2 19 ABXA9800070 1 19980209 A 5320 99582337 INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP BS 945-965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 97009 DURING C-CHECK, FOUND INTERCOSTAL AT STA 945-965 AND LONGERON 29 RT CORRODED. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998021900676 19980219 00676 WP 1998 2 19 ABXA9800071 1 19980210 A 5320 99115434 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 560 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND VERTICAL SUPPORT CRACKED AT LOWER END AT LONGERON 23R AND STA 560. REPAIRED SUPPORT FITTING IAW D C9 DWG NR K05159. 2 L 7 2 4F A6WE 1998021900677 19980219 00677 WP 1998 2 19 ABXA9800072 1 19980210 A 5311 5911448503 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 851 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND EXFOLIATION CORROSION ON THE AFT FLANGE OF FRAME AT STA 851 BETWEEN LONGERON 29L AND 29R. 2 L 7 2 4F A6WE 1998021900678 19980219 00678 WP 1998 2 19 ABXA9800074 1 19980211 A 5610 BRES4435 ROD END DOUG DOUG DC8 DC862 3021970 WP LT COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 CAPTAINS CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED CAPTAIN'S SLIDING WINDOW ROD END ON UPPER LINK. OPS CH ECKED GOOD. 2 L 7 4 4F 4A25 1998021900679 19980219 00679 WP 1998 2 19 ABXA9800075 1 19980211 A 5330 591970731 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 897 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND FUSELAGE SKIN BULGED AND CRACKED .125 AT FASTENER HOLE UNDER LONGERON 30 AT STA 897. REPAIRED IAW ABX REA D953-22433-MR. 2 L 7 2 4F A6WE 1998021900680 19980219 00680 WP 1998 2 19 ABXA9800076 1 19980210 A 5313 591140959 LONGERON DOUG DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATIONS 275, 313, 389, AND 408. REPAIRED CRACKED SECTIONS OF LONGERON IA W DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998021900681 19980219 00681 WP 1998 2 19 ABXA9800077 1 19980210 A 5320 99234843 SUBFLOOR DOUG DOUG DC9 DC941 302207N WP BS 148-160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE COCKPIT SUBFLOOR AT STA 148-160 AND RBL 40-RBL 54 CRACKED. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998021900682 19980219 00682 WP 1998 2 19 ABXA9800078 1 19980210 A 5320 9910078367 SUBFLOOR DOUG DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE COCKPIT SUBLOOR AT STA 160 CRACKED THREE PLACES BETWEEN RBL 20 AND RBL 26. REPAIRED IAW D C9 SRM 53-01. 2 L 7 2 4F A6WE 1998021900683 19980219 00683 WP 1998 2 19 ABXA9800079 1 19980210 A 5711 5911301502 SPAR DOUG DOUG DC9 DC941 302207N WP WS 164 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE RIGHT WING LOWER REAR SPAR CRACKED 1.375 INCH LONG JUST INBOARD OF STA 164 FLAP HINGE FITT ING ATTACH STUD. REPAIRED REAR SPAR IAW ABX EA 51110027002. 2 L 7 2 4F A6WE 1998021900684 19980219 00684 WP 1998 2 19 MWEA98154 1 19980210 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING DELAMINATED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 23ME 47673 DURING INSPECTION, FOUND LT WING TRAILING EDGE PANEL NR 1504A IS DELAMINATED ON OUTBOARD EDGES. MAINTENANCE REPAIRED IA W DAC DRAWING NR 9957499 AND SRM 51-30 RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998021900685 19980219 00685 WP 1998 2 19 MWEA98158 1 19980210 A 3397 0105602001 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND LT NACELLE EMERGENCY LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK RE TURNED AC TO SERVICE. 2 L 7 2 4F A6WE 1998021900686 19980219 00686 WP 1998 2 19 MWEA98155 1 19980210 A 3350 6011777 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 502ME 48132 DURING INSPECTION, FOUND LT NACELLE EMERGENCY LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY BATTERY PACK RE TURNED AC TO SERVICE. 2 L 7 2 4F A6WE 1998021900687 19980219 00687 NM 1998 2 19 MWEA98156 1 19980212 A 2560 591769037 SLIDE COVER DOUG MD88 MD88 3023688 NM AFT GALLEY LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 701ME 49760 THE AFT GALLEY DOOR SLIDE COVER NOT ON PROPERLY. REPOSITIONED AFT GALLEY DOOR SLIDE COVER. 2 L 7 2 4F RT A6WE 1998021900688 19980219 00688 WP 1998 2 19 DLL10980359 1 19980210 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 720DA 193C1136 EMERGENCY LIGHT STRIP AT MID GALLEY CROSS-AISLE INOP. REPAIRED BROKEN WIRE AT SPLICE. 2 L 7 3 4F A23WE 1998021900689 19980219 00689 NM 1998 2 19 DL76S980361 1 19980207 A 2120 AIR DISTRIBUTION BOEING 767 767332 1382001 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 139DL 25984 FUMES FILLED CABIN DURING T/O ROLL, SMELLED LIKE O/HEATED OVEN OR BURNING PAPER DID NOT SMELL LIKE ELECT. SMOKE ALARMS IN AFT LAVS WENT ON. SMELL DISAPATED TEMPORARILY RTND ON LDG. RAN ENGS AT T/O PWR W/ACFT PACKS ON; NO SMOKE OR ODOR NO TICED IN CABIN. REPLACED RECIRC FILTERS, CHKD ALL LAV TRASH CONTAINERS AND FIRE EXTINGUISHER CKD, ALL COFFEEMAKERS AND OVENS. NO PROBLEMS NOTED, ACFT OK FOR SERVICE. 2 L 7 2 4F RT A1NM 1998021900690 19980219 00690 NM 1998 2 19 DL757980362 1 19980113 A 5414 311N3000 SKIN BOEING 757 757232 1384965 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 606DL 22813 NR 2 ENG NACELLE PYLON STRUT SKIN AT NAC STA 107.7 CRACKED SKIN AT INBD AND OUTBD SIDE. PERMANENT REPAIRS ACCOMPLISHED PER SRM 54-51-01-2-203 ON N/R CARD 19 AND 515 MIDVISIT. 2 L 7 2 4F RT A2NM 1998021900691 19980219 00691 NM 1998 2 19 DL72S980363 1 19980210 A 5313 65564416 STRINGER BOEING 727 727225 1384077 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 FUSELAGE/STRINGER 29R/FS 950D PLUS 10, FS 1007. SPLICE REPAIR A SECTION OF STRINGER 29R NEAR FS 950D PLUS 10 WAS FOUND BADLY CORRODED. THE STRINGER WAS CUT AT STATION 950D PLUS 10 AND THE AFT END REMOVED. A NEW SECTION WAS SPLICED IN PER ER/A 363641-14, REV C. 2 L 7 3 4F A3WE 1998021900692 19980219 00692 NM 1998 2 19 DLM88980364 1 19980211 A 5320 JAMB DOUG MD88 MD88 3023688 NM C1 DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 928DL 49715 FUSELAGE DOOR SURROUND C1 DOOR, LOWER JAMB PAN, SPLICE REPAIR. THE LOWER JAMB PAN OF THE FWD CARGO DOOR OPENING WAS FOU ND WITH EXTENSIVE CORROSION. THE CORRODED SECTION OF PAN WAS CUTOUT AND A NEW PIECE SPLICED IN PER THE GUIDLINES OF THE MD-88 SRM 53-05, FIG 44 AND AS DOCUMENTED IN ER/A 364000-14. 2 L 7 2 4F RT A6WE 1998021900693 19980219 00693 NE 1998 2 19 DLL10980366 2 19980211 A 7321 FUEL CONTROL LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB211524B4 54555 NE NR 1 ENGINE FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 722DA 68992 10658 193C1147 10658 T/O PWR SET ENG 1 FAILED TO ACCELERATE PROPERLY N3 LESS THAN 80 PERCENT EPR WOULD NOT GO ABOVE 1.18 {OTHERS SET AT 1.428 } AND N2WAS LOWER {APPROX 80} THAN OTHER ENGINES. REJECTED TAKEOFF AT 60 KTS. ENGINE ANTI-ICE WAS ON. REPLACED NR 1 E NG FUEL CONTROL AND FUEL PUMP PER MM AND TRIMMED ENG PER PFHB. OPS AND LK CK GOOD. 2 L 7 3 4F 4 F A23WE E12EU 1998021900694 19980219 00694 NM 1998 2 19 DL72S980368 1 19980211 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 499DA 10194 21143 ON LAYOVER CK, FOUND LT OVERWING EMERGENCY EXIT SIGN NOT ILLUMINATING. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998021900695 19980219 00695 WP 1998 2 19 DLL10980369 1 19980211 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 728DA 61439 193C1173 EMERGENCY LIGHTS FAILED AT L2, R2, LWR GAL AND RT GAL LIFT.REPLACED EMERGENCY LIGHT PWR SUPPLY UNIT. 2 L 7 3 4F A23WE 1998021900696 19980219 00696 NM 1998 2 19 DL76L980371 1 19980212 A 2913 887673 PUMP BOEING 767 767332 1382001 NM NR 1 ENGINE LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 173DN 24800 LT HYD SYS QTY DECREASED TO .81, SECURED LT ENG HYD PUMPS. DIVERTED TO LGW. FOUND LEFT ENGINE DRIVEN PUMP LEAKING, REP LACED SAME. OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1998021900698 19980219 00698 SO 1998 2 19 SWIA971081 1 19980209 A 3010 DE-ICE BOOTS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT/RT STAB FAILED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 213SW 120277 LEFT AND RIGHT INBOARD STABILIZER DE-ICE BOOTS AND INBOARD LEFT AND RIGHT WING DE-ICE BOOTS FAIL AFTER ABOUT 10 SECONDS OR LESS IN BOTH TIMERS AND LIGHT AND HEAVY CYCLE. RETURNED TO LAX. INSTALLED SERVICEABLE EJECTOR VALVE IAW MM 30-10-00 . RAN SYSTEM AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021900699 19980219 00699 SO 1998 2 19 SWIA971082 1 19980209 A 3060 PROP DE-ICE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 226SW 120296 AFTER TAKEOFF, THE LEFT INLET FAILED. RETURNED TO LAX. ON APPROACH LEFT PROPELLER DE-ICE FAILED ON TIMER 1 AND NORMAL. OPERATED LEFT PROPELLER AND DE-ICE FOR 20 MIN AND ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998021900700 19980219 00700 NM 1998 2 19 P5CA9800229 1 19980205 A 2751 65B156514 DRIVE ROD BOEING 747 747132 1384882 NM RT TE FLAP BROKEN A P5CA K NONE O OTHER LD LANDING 1 WP 23 857FT 20246 AFTER HARD LANDING, EXTERIOR INSPECTION FOUND RIGHT INBOARD FLAP NOT FULL UP. FOUND DRIVE RODS FOR THE AFT CANOE ASSEMB LY BROKEN AT THE NR 5 AND NR 6 POSITIONS. DRIVE RODS REPLACED PER BOEING M/M 27-51-01. NR 6 CANOE WAS FOUND WITH A HOL E. REPLACED PER BOEING M/M 27-51-26. NR 5 CANOE WAS FOUND DAMAGED. REPAIRED PER BOEING SRM 51-40-09. ON RETRACTION O F FLAPS THE INBOARD AILERON WAS CONTACTED AT THE AFT END. REPLACED AILERON PER BOEING M/M 27-11-01. RETRACTION ALSO DA MAGED THE NR 3 AFT FLAP REPAIRED PER BOEING SRM 51-40-06, 51-40-07 AND 51-40-09. COMPLIED WITH HARD LANDING INSPECTION PHASE 1 PER BOEING M/M 05-51-05. NO ADDITIONAL DISCREPANCIES FOUND. 2 L 7 4 4F A20WE 1998021900701 19980219 00701 NE 1998 2 19 RRXA98014 2 19980206 A 7230 COMPRESSOR DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE STALLED A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 998CF 46139 NR 1 ENGINE COMPRESSOR STALLS, SHUTDOWN IN-FLIGHT PER EWA PROCEEDURES. COMPLIED WITH FORM SP003, FOUND 2 BENT BLADES, B LENDED BLADES. FOUND TO BE WITH IN LIMITS PER PRATT AND WHITNEY MAINTENANCE MANUAL 72-0. NR 1 ENGINE OPS CKS GOOD AT A LL POWER SETTINGS. 2 L 7 4 4F 4 F 4A25 1E8 1998021900702 19980219 00702 WP 1998 2 19 RRXA98015 1 19980207 A 3244 1542511 TIRE DOUG DC8 DC862 3021970 WP MLG BLOW OUT A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 15 993CF 46028 AFTER LANDING, TOWER REPORTED SMOKE COMING FROM RT MAIN GEAR, AIRPORT OPS CHECKED ACFT AND FOUND NR 3 TIRE FLAT. REMOVE D AND REPLACED MAIN WHEEL ASSY IAW DC-8 MM CH 32-40-11. POST FAILURE (BLOW-OUT) INSPECTION C/W IAW EWA A/C MM CH 10. 2 L 7 4 4F 4A25 1998021900703 19980219 00703 NM 1998 2 19 RRXA98016 1 19980206 A 3230 656021132 ACCESSORY BOX BOEING 727 727222 1384073 NM LANDING GEAR FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 7642U 19915 LANDING GEAR HANDLE FAILED TO RAISE AFTER T/O. (LANDING GEAR LEVER LATCH FAILED TO RELEASE AFTER T/O). REMOVED AND RE PLACED LANDING GEAR ACCESSORY BOX IAW M/M 32. OPS CHECKS GOOD. 2 L 7 3 4F A3WE 1998021900704 19980219 00704 WP 1998 2 19 RRXA98017 1 19980208 A 5711 SPAR WEB DOUG DC8 DC863 302198A WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE INSPECTION, FOUND LEFT WING REAR SPAR WEB CRACKED IN TWO (2) LOCATIONS. RECEIVED (ONE TIME FERRY F LIGHT) AUTHORIZATION FROM FAA DER HOWARD PATTERSON REF NR 98-022/014-31, TO KMCN FOR REPAIR. 2 L 7 4 4F 4A25 1998021900705 19980219 00705 NM 1998 2 19 VNAA9802007 1 19980208 A 3260 2276500000 HARNESS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FAILED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 425JS 64553 647 3037 AFTER TAKEOFF, A PROXY FAIL WARNING MESSAGE ILLUMINATED DURING GEAR RETRACTION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED, WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPLACED THE LEFT DOWN LOCK SWITCH HARNESS IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 32-61-05. FUNCTION CHECKS WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED TO SERVICE . 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998021900706 19980219 00706 NM 1998 2 19 VNAA9802010 1 19980210 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 436JS 1003 1001 3052 DURING THE PREFLIGHT INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS FOUR AND SIX WERE FOUND TO BE INOPERATIVE. MAINTENA NCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERA TION CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998021900707 19980219 00707 1998 2 19 HEEA0012871 4 19980209 A 3414 206075725103 AIRSPD INDICATOR BELL 407 407 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 467PH 286 53142 PILOT REPORTED AIRSPEED INDICATOR READS 10 KNOTS LOW, BASED ON GPS READINGS. 1 G 7 1 3U O H2SW 1998021900708 19980219 00708 1998 2 19 HEEA0012872 4 19980209 A 3424 206070274101 INDICATOR BELL 407 407 SW COCKPIT T&B FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 TURN NEEDLE WILL NOT MOVE; EVEN THOUGH FLAG IS PULLED. 1 G 7 1 3U O H2SW 1998021900709 19980219 00709 SW 1998 2 19 HEEA0012876 1 19980209 A 2841 407375006101 INDICATOR BELL 407 407 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1167G 53067 FUEL QTY INDICATOR READS 450 POUNDS FIRST HOUR OF FLIGHT. 1 G 7 1 3U O H2SW 1998021900710 19980219 00710 SW 1998 2 19 HEEA0012877 1 19980209 A 6321 206340301103 ROTOR BRAKE BELL 407 407 SW PUCK DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1167G 502 53067 ROTOR BRAKE HAS ONE PUCK MISSING. 1 G 7 1 3U O H2SW 1998021900711 19980219 00711 SW 1998 2 19 HEEA0012880 1 19980209 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE SCRATCHED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 T/R DRIVE DISC SCRATCHED. 1 G 7 1 3U O H2SW 1998021900712 19980219 00712 SW 1998 2 19 HEEA0012881 1 19980209 A 6220 407010208101 STOP BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 STOP WORN BEYOND LIMITS. 1 G 7 1 3U O H2SW 1998021900713 19980219 00713 SW 1998 2 19 HEEA0012882 1 19980209 A 7712 407375003107 INDICATOR BELL 407 407 SW TORQUE FAILED E HEEA K NONE O OTHER HO HOVERING 1 SW 03 406PH 48 53198 WHILE HOVERING AT 68-71% TORQUE, TORQUE GAUGE STARTED INCREASING UNTIL REACHING FULL SCALE READING AND THEN WENT TO 0%. 1 G 7 1 3U O H2SW 1998021900714 19980219 00714 EU 1998 2 19 HEEA0012884 1 19980209 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU ANTI COLL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 2446 2777 ANTI COLL LIGHT SLOW FLASH. 1 G 7 1 3U H9EU 1998021900715 19980219 00715 1998 2 19 HEEA0012885 4 19980209 A 3120 B1894522222A CLOCK SNIAS 350 AS350B2 8680813 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 262 2777 CLOCK SECOND HAND RESET KNOB MISSING. 1 G 7 1 3U H9EU 1998021900716 19980219 00716 1998 2 19 HEEA0012886 4 19980209 A 3414 214175299105 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 AIRSPEED INDICATOR UNITS SENT TO MASCO FOR COMPLIANCE OF ASB 214ST-97-79. SERIAL NUMBERS ARE 216214 AND SECOND SERIAL N UMBER UNKNOWN. 2 G 7 2 4U H10SW 1998021900717 19980219 00717 EU 1998 2 19 HEEA0012887 1 19980209 A 6420 350A33200405 SPIDER SNIAS 350 AS350B2 8680813 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 755 2862 T/R SPIDER HAS WORN BEARING. 1 G 7 1 3U H9EU 1998021900718 19980219 00718 EU 1998 2 19 HEEA0012888 1 19980209 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU ANTI COLL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 141 2820 ANTI COLL LIGHT WILL NOT FLASH. 1 G 7 1 3U H9EU 1998021900719 19980219 00719 SW 1998 2 19 HEEA0012889 1 19980209 A 2821 222366621103 FUEL FILTER BELL 407 407 SW FUEL SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 141MA 53016 FUEL FILTER LEAKING. 1 G 7 1 3U O H2SW 1998021900720 19980219 00720 SW 1998 2 19 HEEA0012890 1 19980209 A 6321 206076047101 CYLINDER BELL 407 407 SW ROTOR BRAKE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 CYL ASSY WILL NOT HOLD PRESSURE, BLEEDS DOWN. 1 G 7 1 3U O H2SW 1998021900721 19980219 00721 SW 1998 2 19 HEEA0012893 1 19980209 A 3212 206050247131 COVER BELL 407 407 SW FLOAT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 FLOAT COVER MISSING END PIECE. 1 G 7 1 3U O H2SW 1998021900722 19980219 00722 SW 1998 2 19 HEEA0012898 1 19980210 A 2434 214175150105 GENERATOR BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 GENERATOR CAUSING HIGH FREQUENCY VIBRATIONS; APPEARS TO BE BENT. 2 G 7 2 4U H10SW 1998021900723 19980219 00723 SW 1998 2 19 HEEA0012899 1 19980210 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 18 33073 STEP ACTUATOR MOTOR WON'T EXTEND OR RETRACT. 1 G 7 2 4U H4SW 1998021900724 19980219 00724 SW 1998 2 19 HEEA0012900 1 19980210 A 2910 212076015001 VALVE BELL 412 412 1182202 SW HYD CHECK LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 293CA HYD CHECK VALVE LEAKS. 1 G 7 2 4U H4SW 1998021900725 19980219 00725 SW 1998 2 19 HEEA0012901 1 19980210 A 2910 212076015001 VALVE BELL 412 412 1182202 SW HYD CHECK LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 293CA HYD CHECK VALVE LEAKS. 1 G 7 2 4U H4SW 1998021900726 19980219 00726 SW 1998 2 19 HEEA0012902 1 19980210 A 2910 212076015001 VALVE BELL 412 412 1182202 SW HYD CHECK LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 293CA HYD CHECK VALVE LEAKS. 1 G 7 2 4U H4SW 1998021900727 19980219 00727 SW 1998 2 19 HEEA0012903 1 19980210 A 5260 SYLC502281 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 STEP ACTUATOR MOTOR INOPERATIVE; WON'T EXTEND OR RETRACT. 1 G 7 2 4U H4SW 1998021900728 19980219 00728 SW 1998 2 19 HEEA0012904 1 19980210 A 2910 212076015001 VALVE BELL 412 412 1182202 SW HYD CHECK DAMAGED E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2261D 33076 THREADS MASHED ON OUTPUT SIDE AND LEAKS FROM THREADS. 1 G 7 2 4U H4SW 1998021900730 19980219 00730 1998 2 19 HEEA0012909 4 19980210 A 3416 8140BS20LW5V ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 ALTIMETER UNIT HAS EXCESSIVE LEAKAGE AROUND BARO KNOB. 1 G 7 2 3U H1NE 1998021900731 19980219 00731 1998 2 19 HEEA0012910 4 19980210 A 3416 8140B35 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT ENCODER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 760275 ENCODER READS HIGH OUT OF TOLERANCE. 1 G 7 2 3U H1NE 1998021900732 19980219 00732 NE 1998 2 19 HEEA0012911 1 19980210 A 3230 4608 PRIORITY VALVE SKRSKY S76 S76A 8143006 NE GEAR FAILED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 5426U 760167 NR2 SERVO LIGHT WOULD COME ON WHEN GEAR IS LOWERED OR RAISED. 1 G 7 2 3U H1NE 1998021900733 19980219 00733 1998 2 19 HEEA0012912 4 19980210 A 2230 7611113 AMPLIFIER SKRSKY S76 S76A 8143006 NE YAW SLICE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 4253S 63 760035 YAW CHANNEL WON'T TEST. 1 G 7 2 3U H1NE 1998021900734 19980219 00734 SW 1998 2 19 HEEA0012913 1 19980210 A 2822 164A199 BOOST PUMP BELL 206 206L1 1182107 SW ENG FUEL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5017G 562 45228 BOOST PUMP NOPERATIVE. 1 G 7 1 3U H2SW 1998021900735 19980219 00735 NE 1998 2 19 HEEA0012914 1 19980210 A 2930 07113111321 SWITCH SKRSKY S76 S76A 8143006 NE HYD SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 707AE 760276 SWITCH LEAKS FROM WEEP HOLE. 1 G 7 2 3U H1NE 1998021900736 19980219 00736 SW 1998 2 19 HEEA0012915 1 19980210 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW STANDBY DC FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 BATTERY PACK INTERNAL FAILURE. 1 G 7 2 4U H4SW 1998021900737 19980219 00737 SW 1998 2 19 HEEA0012916 1 19980210 A 2432 39563001 BATTERY PACK BELL 412 412 1182202 SW STANDBY DC FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 1713 36002 BATTERY PACK INTERNAL FAILURE. 1 G 7 2 4U H4SW 1998021900738 19980219 00738 SW 1998 2 19 HEEA0012918 1 19980210 A 2841 412375001101 INDICATOR BELL 412 412 1182202 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 FUEL QTY INDICATOR DIGITS NOT TESTING. 1 G 7 2 4U H4SW 1998021900739 19980219 00739 NE 1998 2 19 HEEA0012919 1 19980210 A 2841 7645001078103 INDICATOR SKRSKY S76 S76A 8143006 NE FUEL QTY STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 NR 1 NEEDLE STICKS AT ZERO. 1 G 7 2 3U H1NE 1998021900740 19980219 00740 SW 1998 2 19 HEEA0012921 1 19980210 A 2422 ASH5845 INVERTER BELL 212 212 1181420 SW AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 INVERTER IS MAKING A LOUD NOISE. 1 G 7 1 4U H4SW 1998021900741 19980219 00741 SW 1998 2 19 HEEA0012922 1 19980210 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 TRIPLE TACH INDICATOR NEEDLE STICKS. 1 G 7 2 4U H4SW 1998021900742 19980219 00742 SW 1998 2 19 HEEA0012923 1 19980210 A 2460 A700AAP REVERSE CURRENT BELL 412 412 1182202 SW DC DIST MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 WON'T PULL OFF FLAG ON HSI. 1 G 7 2 4U H4SW 1998021900743 19980219 00743 SW 1998 2 19 HEEA0012926 1 19980210 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS FAILED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 3911L 33023 450VA INVERTER LIGHT COMES ON. 1 G 7 2 4U H4SW 1998021900744 19980219 00744 SW 1998 2 19 HEEA0012927 1 19980210 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11027 45411 GENERATOR WILL NOT COME ON LINE. 1 G 7 1 3U H2SW 1998021900745 19980219 00745 NE 1998 2 19 HEEA0012928 1 19980210 A 7712 7645001078106 INDICATOR SKRSKY S76 S76A 8143006 NE DUAL TORQUE INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 DUAL TORQUE NR1 NEEDLE INOPERATIVE. 1 G 7 2 3U H1NE 1998021900746 19980219 00746 SW 1998 2 19 HEEA0012929 1 19980210 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11027 45411 CAUSES STARTER TO RUN AFTER SHUTDOWN. 1 G 7 1 3U H2SW 1998021900747 19980219 00747 1998 2 19 HEEA0012930 4 19980210 A 3414 8000 AIRSPEED IND BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251Z 45756 AIRSPEED INDICATOR RANGE MARKINGS ARE FADED. 1 G 7 1 3U H2SW 1998021900748 19980219 00748 SW 1998 2 19 HEEA0012931 1 19980210 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 TRIPLE TACH INDICATOR ALL NEEDLES ARE ERRATIC. 1 G 7 2 4U H4SW 1998021900749 19980219 00749 SW 1998 2 19 HEEA0012932 1 19980210 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 450VA INVERTER WILL NOT TURN OFF. 1 G 7 2 4U H4SW 1998021900750 19980219 00750 SW 1998 2 19 HEEA0012933 1 19980210 A 2841 393008047 INDICATOR BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 FUEL QTY INDICATOR NEEDLE BROKEN INTERMITTENTLY NO MOVEMENT. 1 G 7 2 4U H4SW 1998021900751 19980219 00751 SW 1998 2 19 HEEA0012934 1 19980210 A 2841 393008047 INDICATOR BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 FUEL QTY INDICATOR NEEDLE STUCK AT 400 LBS. 1 G 7 2 4U H4SW 1998021900752 19980219 00752 1998 2 19 HEEA0012935 4 19980210 A 3416 066030640001 ALTIMETER BELL 412 412 1182202 SW COCKPIT ENCODER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 ENCODER INDICATES HIGH OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998021900753 19980219 00753 SW 1998 2 19 HEEA0012936 1 19980210 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R SERVO LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 5981 51540 M/R SERVO LEAKING, CYLINDER SCORED. 1 G 7 1 3U H2SW 1998021900754 19980219 00754 NE 1998 2 19 HEEA0012937 1 19980210 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 M/R DAMPER IS WEAK. 1 G 7 2 3U H1NE 1998021900755 19980219 00755 SW 1998 2 19 HEEA0012939 1 19980210 A 2436 206075447007 VOLT REGULATOR BELL 206 206L3 1182108 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21497 51518 GENERATOR WOULD FALL OFF LINE BUT WOULD RESET EACH TIME. 1 G 7 1 3U H2SW 1998021900756 19980219 00756 EU 1998 2 19 HEEA0012941 1 19980210 A 2841 206075189001 INDICATOR BOLKMS 117 BK117B2 5626013 EU FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 FUEL QTY INDICATOR HAS EXCESSIVE FRICTION PAST 50 GALLONS. 1 G 7 2 3U NC H13EU 1998021900757 19980219 00757 1998 2 19 HEEA0012942 4 19980210 A 3421 4021541671 GYRO BOLKMS 117 BK117B2 5626013 EU ARTIFICIAL HORIZ FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 HORIZON GYRO TUMBLES. 1 G 7 2 3U NC H13EU 1998021900758 19980219 00758 1998 2 19 HEEA0012943 4 19980210 A 3421 4021541671 INDICATOR BOLKMS 117 BK117B2 5626013 EU HORIZON FAULTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 ARTIFICIAL HORIZ FLAG SLOW TO PULL AND GLASS DIRTY. 1 G 7 2 3U NC H13EU 1998021900759 19980219 00759 SW 1998 2 19 HEEA0012944 1 19980210 A 2913 214076334105 PUMP BELL 214 214ST 1182106 SW HYD MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 HYD PUMP MAKING METAL. 2 G 7 2 4U H10SW 1998021900760 19980219 00760 1998 2 19 HEEA0012945 4 19980210 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW AUTO FLIGHT SEIZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 33020 TARSYN HSI FROZEN IN PLACE. 1 G 7 2 4U H4SW 1998021900761 19980219 00761 1998 2 19 HEEA0012946 4 19980210 A 3416 59341 ALTIMETER BELL 206 206L3 1182108 SW COCKPIT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205FC 51130 ALTIMETER LEAKING AT KNOB. 1 G 7 1 3U H2SW 1998021900762 19980219 00762 SW 1998 2 19 HEEA0012947 1 19980210 A 7712 206075185001 GAUGE BELL 206 206B3 1181506 SW TORQUE STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2270G 3610 TORQUE INDICATOR NEEDLE STICKING. 1 G 7 1 3U H2SW 1998021900763 19980219 00763 EU 1998 2 19 HEEA0012948 1 19980210 A 7714 DL43638 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER CR CRUISE 1 SW 03 4302G S853 TRIPLE TACH WENT TO ZERO THEN TO 104 AND STAYED DURING CRUISE FLIGHT. 1 G 7 2 3U H3EU 1998021900764 19980219 00764 SW 1998 2 19 HEEA0012950 1 19980210 A 8012 51539002N CONTROL UNIT BELL 412 412 1182202 SW NR 1 ENG START FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 NR 1 ENGINE STARTER ENGAGES ON SHUTDOWN. 1 G 7 2 4U H4SW 1998021900765 19980219 00765 EU 1998 2 19 HEEA0012952 1 19980210 A 2436 51565000R REGULATOR BOLKMS 105 BO105S 5626006 EU NR 2 GEN SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K S859 NR 2 GENERATOR INOPERATIVE. PUTS OUT VOLTAGE BUT NO AMPERAGE. 1 G 7 2 3U H3EU 1998021900766 19980219 00766 1998 2 19 HEEA0012954 4 19980210 A 3454 066303800 INDICATOR KING KI229 BOLKMS 105 BO105S 5626006 EU COCKPIT RMI INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 818SH S753 COCKPIT RMI INOPERATIVE. 1 G 7 2 3U H3EU 1998021900767 19980219 00767 1998 2 19 HEEA0012955 4 19980210 A 2230 7611113 AMPLIFIER SKRSKY S76 S76A 8143006 NE YAW SLICE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 YAW CHANNEL INOPERATIVE. 1 G 7 2 3U H1NE 1998021900768 19980219 00768 1998 2 19 HEEA0012956 4 19980210 A 3444 4014267901 ALTIMETER BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 RADAR ALTIMETER WILL NOT INDICATE ALTITUDE. 1 G 7 2 4U H4SW 1998021900769 19980219 00769 1998 2 19 HEEA0012957 4 19980210 A 3425 71252 GYRO BELL 412 412 1182202 SW HSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 263 36019 RATE OF TURN NEEDLE STUCK ON HSI. 1 G 7 2 4U H4SW 1998021900770 19980219 00770 SW 1998 2 19 HEEA0012958 1 19980210 A 2422 412075101103 INVERTER BELL 412 412 1182202 SW AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 VOLTMETER PEGS OUT WHEN 450VA INVERTER IS TURNED ON. 1 G 7 2 4U H4SW 1998021900771 19980219 00771 1998 2 19 HEEA0012959 4 19980210 A 3416 212070238003 INDICATOR BELL 412 412 1182202 SW ALTIMETER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 ALTIMETER INDICATOR HAS RATTLING NOISE IN INSTRUMENT. 1 G 7 2 4U H4SW 1998021900772 19980219 00772 SW 1998 2 19 HEEA0012960 1 19980210 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 ENGINE WILL NOT BATTERY START DUE TO HIGH VOLTAGE DRAW. 2 G 7 2 4U H10SW 1998021900773 19980219 00773 SW 1998 2 19 HEEA0012961 1 19980210 A 2436 104217A REGULATOR BELL 206 206B3 1181506 SW DC SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2269A 3608 VOLTS REG DEFECTIVE. NOT ADJUSTABLE ABOVE 270 FEET. 1 G 7 1 3U H2SW 1998021900774 19980219 00774 SW 1998 2 19 HEEA0012962 1 19980210 A 2436 15891F REGULATOR BELL 206 206B3 1181506 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 103PH 3000 DC REG FAILED. PEGS VOLTMETER. 1 G 7 1 3U H2SW 1998021900775 19980219 00775 SW 1998 2 19 HEEA0012967 1 19980210 A 2436 206075447007 VOLT REGULATOR BELL 206 206L3 1182108 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 210PH 51541 GENERATOR SLOW TO COME ON LINE. VOLTS REG FAILED 1 G 7 1 3U H2SW 1998021900776 19980219 00776 SW 1998 2 19 HEEA0012968 1 19980210 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R SERVO LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 205FC 3587 51130 SERVO LEAKING AT BOTH ENDS OF CYLINDER. TIME SINCE REPAIR 0:00. 1 G 7 1 3U H2SW 1998021900777 19980219 00777 1998 2 19 HEEA0012969 4 19980210 A 3416 212070238003 INDICATOR BELL 412 412 1182202 SW ALTIMETER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 LOOSE OBJECTS INSIDE UNIT. 1 G 7 2 4U H4SW 1998021900778 19980219 00778 SW 1998 2 19 HEEA0012972 1 19980210 A 2841 206063633103 INDICATOR BELL 206 206L3 1182108 SW FUEL QTY DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 210PH 51541 OIL INSIDE FACE. LIGHT TRAY BROKEN. 1 G 7 1 3U H2SW 1998021900779 19980219 00779 SW 1998 2 19 HEEA0012973 1 19980210 A 7722 212075420003 INDICATOR BELL 212 212 1181420 SW ITT TEMP STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736D 31135 ITT TEMP INDICATOR NEEDLE IS STICKING. 1 G 7 1 4U H4SW 1998021900780 19980219 00780 SW 1998 2 19 HEEA0012974 1 19980210 A 2915 212076006007 VALVE BELL 412 412 1182202 SW HYD SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 FILTER PRESSURE SWITCH STUCK CLOSED, CAUSING EXT. CLOG BUTTON TO POP RED. 1 G 7 2 4U H4SW 1998021900781 19980219 00781 EU 1998 2 19 HEEA0012977 1 19980210 A 2913 4002001 HYD PUMP BOLKMS 105 BO105S 5626006 EU HYD SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE S787 HYD PUMP NOT MAKING MINIMUM PRESSURE. 1 G 7 2 3U H3EU 1998021900782 19980219 00782 EU 1998 2 19 HEEA0012978 1 19980210 A 2913 4002001 HYD PUMP BOLKMS 105 BO105S 5626006 EU SEAL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5029H S670 HYD PUMP LEAKING SEAL. 1 G 7 2 3U H3EU 1998021900783 19980219 00783 SW 1998 2 19 HEEA0012980 1 19980210 A 6710 214001423105 ACTUATOR BELL 214 214ST 1182106 SW M/R INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ACTUATOR INOPERATIVE. 2 G 7 2 4U H10SW 1998021900784 19980219 00784 SW 1998 2 19 HEEA0012981 1 19980210 A 6710 214001423105 ACTUATOR BELL 214 214ST 1182106 SW M/R INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ACTUATOR INOPERATIVE. 2 G 7 2 4U H10SW 1998021900785 19980219 00785 SW 1998 2 19 HEEA0012985 1 19980210 A 2841 407375006101 INDICATOR BELL 407 407 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FUEL QTY INDICATOR GOES INOPERATIVE AT TIMES. 1 G 7 1 3U O H2SW 1998021900786 19980219 00786 SW 1998 2 19 HEEA0012993 1 19980210 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 435 33002 STEP ACTUATOR WON'T MOVE. 1 G 7 2 4U H4SW 1998021900787 19980219 00787 SW 1998 2 19 HEEA0012994 1 19980210 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 18 36005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998021900788 19980219 00788 SW 1998 2 19 HEEA0012996 1 19980210 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 STARTER WON'T ENGAGE. 2 G 7 2 4U H10SW 1998021900789 19980219 00789 SW 1998 2 19 HEEA0012997 1 19980210 A 7714 407375008101 DUAL TACH BELL 407 407 SW ENG RPM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CGOFL 53130 DUAL TACH STAYS ON ZERO ON START UP. 1 G 7 1 3U O H2SW 1998021900790 19980219 00790 SW 1998 2 19 HEEA0012998 1 19980210 A 6710 214001423109 ACTUATOR BELL 214 214ST 1182106 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ACTUATOR POPPING CIRCUIT BREAKERS. 2 G 7 2 4U H10SW 1998021900791 19980219 00791 NE 1998 2 19 HEEA0013001 1 19980210 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 DAMPERS WEAK AND LEAKING. SERIAL NUMBERS REMOVED ARE A061-01476 AND A061-01165. 1 G 7 2 3U H1NE 1998021900792 19980219 00792 NE 1998 2 19 HEEA0013002 1 19980210 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 M/R DAMPER HAS A DEAD SPOT. 1 G 7 2 3U H1NE 1998021900793 19980219 00793 1998 2 19 HEEA0013004 4 19980210 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW HSI MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA HSI INDICATOR YELLOW NEEDLE FLUCTUATES FROM L/H TO R/H LORAN MODE. 1 G 7 2 4U H4SW 1998021900794 19980219 00794 1998 2 19 HEEA0013005 4 19980210 A 3425 1113025 INDICATOR BELL 212 212 1181420 SW HSI SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27805 31106 HSI INDICATOR INTERNALLY SHORTED--BLOWS FUSE. 1 G 7 1 4U H4SW 1998021900795 19980219 00795 1998 2 19 HEEA0013006 4 19980210 A 3425 1113025 INDICATOR SKRSKY S76 S76A 8143006 NE HSI DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 HSI INDICATOR COURSE SET KNOB BINDING. 1 G 7 2 3U H1NE 1998021900796 19980219 00796 1998 2 19 HEEA0013007 4 19980210 A 3421 1113034 INDICATOR BELL 212 212 1181420 SW ATT INDICATOR BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 ATTITUDE INDICATOR PITCH KNOB BROKEN. 1 G 7 1 4U H4SW 1998021900797 19980219 00797 1998 2 19 HEEA0013008 4 19980210 A 2312 071104302 TRANSCEIVER KFS570B SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 TRANSCEIVER INOPERATIVE. 1 G 7 2 3U H1NE 1998021900799 19980219 00799 SW 1998 2 19 HEEA0013010 1 19980210 A 2430 51539002N CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 CONTROL UNIT INOPERATIVE. GENERATOR VOLTAGE 31.75 VOLT AND WILL NOT ADJUST. 1 G 7 2 4U H4SW 1998021900800 19980219 00800 EU 1998 2 19 HEEA0013012 1 19980210 A 7712 117940691 INDICATOR BOLKMS 117 BK117B1 5626012 EU DUAL TORQUE STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 TORQUE INDICATOR STICKS INTERMITTENTLY AND SPLITS. 1 G 7 2 3U H13EU 1998021900801 19980219 00801 1998 2 19 HEEA0013014 4 19980210 A 3425 1113025 INDICATOR SKRSKY S76 S76A 8143006 NE HSI STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 HSI INDICATOR COMPASS CARD STICKS. 1 G 7 2 3U H1NE 1998021900802 19980219 00802 1998 2 19 HEEA0013015 4 19980210 A 2210 7000299901 CONTROL BELL 412 412 1182202 SW AUTOPILOT BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 AUTO PILOT SAS/ATT. INDICATOR LIGHT BROKEN. 1 G 7 2 4U H4SW 1998021900803 19980219 00803 SW 1998 2 19 HEEA0013016 1 19980210 A 2913 214076033001 PUMP BELL 214 214ST 1182106 SW HYD FAILED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 6957Y 28139 HYD PUMP FAILED. NO PRESSURE. 2 G 7 2 4U H10SW 1998021900804 19980219 00804 1998 2 19 HEEA0013021 4 19980211 A 2330 002000002 AMPLIFIER BELL 412 412 1182202 SW PA SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 PA INOPERATIVE. RESOLDERED BROKEN RED POWER WIRE. REPLACED OPEN FUSE. REPAIRED. FUNCTION CHECK GOOD. 1 G 7 2 4U H4SW 1998021900805 19980219 00805 EU 1998 2 19 HEEA0013026 1 19980211 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU ANTI COLL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 71 2820 ANTI COLL LIGHT BULB BURNT OUT. 1 G 7 1 3U H9EU 1998021900806 19980219 00806 WP 1998 2 19 AALA980045 1 19980108 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1320 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 419AA 49331 TUL - STA 1320 FRAME CORRODED FORWARD SIDE, LONGERONS 29R-29L, LAVATORY - GALLEY SPILL. FABRICATED DOUBLER, J-CHANNEL, AFT ANGLE SHIM AND SPLICE PLATE, TREATED AND PRIMED PARTS. INSTALLED DOUBLER WITH HI-LOKS PER SRM 53-03 FIG 2A SHEET 4 PAGE 46. (X) 2 L 7 2 4F A6WE 1998021900807 19980219 00807 NM 1998 2 19 AALA984011 1 19980114 A 5347 SEAT TRACK BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 391AA 27451 AFW - SEAT TRACK CORROSION BEYOND SRM LIMITS. BLENDED AREA AND REMOVED TRACK LIPS PER ENGINEERING MRB 767-1566. TST: 13 ,600 HOURS. CYCLES: 2,171. (X) 2 L 7 2 4F RT A1NM 1998021900811 19980219 00811 NM 1998 2 19 AALA980013 1 19980104 A 3397 WIRE BOEING 727 727233 138408A NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 866AA 21371 IAH - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT FLOOR LIGHTS IN CABIN NOT OPERATING PROPERLY. REPAIRED BROKEN E MERGENCY EXIT FLOOR LIGHT WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A3WE 1998021900812 19980219 00812 NM 1998 2 19 AALA980133 1 19980117 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 861AA 21088 DTW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT FORWARD CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT LI GHT CONNECTOR AT FORWARD CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900813 19980219 00813 NM 1998 2 19 AALA980043 1 19980108 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 719AA 20612 DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT FLOOR LIGHTS IN FORWARD PASSENGER CABIN NOT OPERATING PROPERLY. REPLACED JUMPER WIRE AT FORWARD PASSENGER CABIN FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900814 19980219 00814 NM 1998 2 19 AALA980044 1 19980108 A 3350 10600919 LIGHT GRIMES BOEING 727 727227 1384078 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 719AA 20612 DFW - DURING OVERNIGHT CHECK, DISCOVERED COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED COCKPIT EMERGENCY EXIT LIGH T ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900815 19980219 00815 NM 1998 2 19 AALA980036 1 19980107 A 3350 1001141 LIGHT GRIMES BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900816 19980219 00816 NM 1998 2 19 AALA980098 1 19980112 A 3350 1TL13 SWITCH BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 729AA 20736 TUL - DURING MAINTENANCE, CABIN EMERGENCY EXIT LIGHTS WOULD NOT OPERATE AT AFT FLIGHT ATTENDANT STATION. REPLACED EMERG ENCY EXIT LIGHT SWITCH AT AFT FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900817 19980219 00817 NM 1998 2 19 AALA980119 1 19980114 A 3350 P4010051126 MODULE BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 861AA 21088 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR WAS FOUND INOPERATIVE. RE-SEATED EMERGENCY E XIT LIGHT MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900821 19980219 00821 EU 1998 2 19 AALA980100 1 19980113 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU FWD LAVATORY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1416A 11395 DFW - DURING OVERNIGHT CHECK, FIRST CLASS LAVATORY EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. RE-SECURED LOOSE WIRE AT FIRST CLASS LAVATORY EMERGENCY EXIT LIGHT BASE ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998021900824 19980219 00824 NE 1998 2 19 AALA980130 2 19980115 A 7261 OIL CAP AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 1 ENGINE LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 14068 511 JFK - FLT 0106 - AT 33,000 FEET, NR 1 ENGINE OIL PRESSURE WAS 32-34 PSI (NR 2 WAS 56 PSI) NR 1 OIL QUANTITY WAS 17 QUART S AT LEVEL OFF, BUT SLOWLY DROPPED TO 11 QUARTS BEFORE STABILIZING. FOUND OIL CAP LEAKING REPLACED CAP AND CHECK VALVE ASSY. LEAK CHECKS OK. (X) 2 L 7 2 4F 4 F RT A35EU E13NE 1998021900825 19980219 00825 NM 1998 2 19 AALA980052 1 19980108 A 2120 5774441 DUCT BOEING 727 727223 1384074 NM AFT FUSELAGE RUPTURED A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 702AA 22460 ORD - FLT 1966 - AFTER TAKEOFF ORD, FLIGHT CREW TURNED ON WING ANTI-ICE AND HEARD A LOUD BANG FOLLOWED BY VIBRATION. AI RCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. CHECK OF AIRCRAFT REVEALED TWO SUPPLY DUCTS RUPTURED. AIRCRAFT MAI NTENANCE REPLACED RUPTURED SUPPLY DUCTS AND AS A PRECAUTION, REPLACED ENGINE BLEED AIR SHUT-OFF VALVE. SYSTEM GROUND AN D LEAKED CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900826 19980219 00826 NM 1998 2 19 AALA980099 1 19980112 A 2510 6430A TRANSFORMER OECO BOEING 727 727223 1384074 NM COCKPIT DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 709AA 22466 ORD - FLT 1391 - AFTER TAKEOFF, COCKPIT CREW NOTED A LIGHT, BUT DEFINITE ELECTRICAL BURNING SMELL BEHIND FLIGHT ENGINEER 'S PANEL. CREW PULLED RADIO PRIMARY CURCUIT BREAKER TO SHUT OFF POWER AND ELIMINATE POSSIBLE FIRE HAZARD. SMELL DISSIP ATED, FLIGHT RETURNED ORD AND LANDED WITHOUT INCIDENT. REPLACED VARIABLE CONTROL TRANSFORMER, PANEL, AND INSTRUMENT RAD IO PRIMARY CIRCUIT BREAKER. CHECKED ALL CENTER PANEL LIGHTS FOR ONE HOUR AND P-18 CIRCUIT BREAKER PANEL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900827 19980219 00827 NM 1998 2 19 AALA980010 1 19980103 A 2820 FUEL TANSFER SYS BOEING 727 727223 1384074 NM NR 3 TANK MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 860AA 21087 DTW - FLT 0583 - DURING CRUISE FROM BDL/ORD, LATERAL FUEL IMBALANCE NOTED. NR 3 FUEL TANK WOULD NOT DECREASE. AIRCRAFT AIR INTERRRUPTED AND LANDED DTW WITHOUT INCIDENT. INSPECTED FUEL PANEL AND TRANSFERRED FUEL FROM TANK NR 3 TO TANKS 1 AND 2. UNABLE TO DUPLICATE ON GROUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. ACCOMPLISHED FUNCTIONAL CHECK, FLIGHT WITH NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900828 19980219 00828 NM 1998 2 19 AALA980012 1 19980104 A 2613 ELEMENT BOEING 727 727223 1384074 NM NR 1 ENGINE OUT OF POSITION A AALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SW 07 6822 19700 MCO - FLT 1941 - AFTER TAKEOFF MCO, NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. DUMPED FUEL AND LANDED WITHOUT INCIDENT. N R 1 ENGINE OVERHEAT DETECTOR ELEMENT WAS FOUND TOUCHING NR 1 ENGINE PRE-COOLER DUCTING. REPOSITIONED ELEMENT. SYSTEM G ROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998021900830 19980219 00830 WP 1998 2 19 AALA980197 1 19980122 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 431AA 49343 DFW - DURING OVERNIGHT CHECK, DISCOVERED BOTH STAIRWAY EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED STAIRWAY EMERGE NCY EXIT LIGHTING WIRES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900831 19980219 00831 WP 1998 2 19 AALA980213 1 19980124 A 2781 SENSOR DOUG DC9 DC982 3022082 WP NR 1 SLAT OUT OF ADJUST A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 407AA 49318 DFW - FLT 0308 - AFTER TAKEOFF DFW DURING CLIMB-OUT, FLIGHT CREW GOT A FLAP DISAGREE LIGHT, ILLUMINATED AND LATER EXTING UISHED. AFTER ACCELERATING TO 300 KNOTS, LIGHT ILLUMINATED WITH AURAL WARNING. NO ASYMMETRY NOTED DURING ANY PHASE OF THE FLIGHT. AIRCRAFT RETURNED AND LANDED DFW WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED AN INSPECTION OF WING FLAPS AN D SLATS, FOUND NR 1 SLAT SENSOR TOO CLOSE TO THE SENSOR. NR 1 SLAT SENSOR WAS ADJUSTED, AND A BITE TEST ACCOMPLISHED WI TH NO FURTHER FAULTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900832 19980219 00832 WP 1998 2 19 AALA980196 1 19980120 A 2170 21D101 COALESCER DOUG DC9 DC983 3022083 WP ACM BAY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 572AA 49458 DFW - FLT 1887 - DURING TAKEOFF, STRONG SMELL AND HAZE IN CABIN AND COCKPIT. DISSIPATED IN CLIMB. REMOVED AND REPLACED WATER SEPARATOR BAGS. ACCOMPLISHED PACK BURN. NO ODORS NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998021900833 19980219 00833 NM 1998 2 19 AALA980203 1 19980126 A 2560 H205213 LATCH BOEING 767 767323 1385205 NM SLIDE COMPT BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7375A 25202 ORD - FLT 0361 - DURING OVERNIGHT MAINTENANCE, LEFT HAND OVER WING SLIDE COMPARTMENT DOOR WOULD NOT OPEN NORMALLY. LATC H LINKAGE AT CENTER LATCH WAS FOUND BROKEN. REPLACED CENTER LATCH ON LEFT HAND OVER WING SLIDE COMPARTMENT AND AS A PRE CAUTION, REPLACED AFT ACTUATOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900835 19980219 00835 EU 1998 2 19 AALA980004 1 19980101 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU COCKPIT LOOSE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 1419D 11402 ORD - FLT 0653 - AFTER TAKEOFF SWF WHEN LANDING GEAR RETRACTED, LT MAIN LANDING GEAR GREEN LIGHT ILLUMINATED. RE-CYCLED GEAR AND GREEN LIGHT EXTINGUISHED AND NO OTHER INDICATIONS ON MFDU OF UNSAFE GEAR CONDITION. CREW CONTACTED TULSA TECH AND THEIR RECOMMENDATION WAS TO USE ALTERNATE GEAR EXTENSION PROCEDURES BEFORE LANDING ORD. ACCOMPLISHED ALTERNATE GEA R EXTENSION PROCEDURE AND AIRCRAFT LANDED ORD WITHOUT INCIDENT. MAINTENANCE FOUND TWO LOOSE BULBS LAYING BEHIND LEFT GE AR LIGHT CAPSULE SHORTING CENTER CONTACT TO GROUND CAUSING GREEN LIGHT TO ILLUMINATE. REMOVED BULBS AND REPLACED WITH S ERVICEABLE BULBS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998021900836 19980219 00836 EU 1998 2 19 AALA980048 1 19980110 A 3230 858202 PSEU ELDEC FOKKER F28 F28MK0100 4990807 EU E/E BAY MALFUNCTIONED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 1448A 269 11457 ORD - FLT 1066 - AFTER TAKEOFF MSP WHEN GEAR UP SELECTED, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. AI RCRAFT CONTINUED TO ORD WITH THE LANDING GEAR DOWN AND LOCKED AND LANDED ORD WITHOUT INCIDENT. AIRCRAFT WAS JACKED, LAN DING GEAR CYCLED SEVERAL TIMES, AND THE LANDING GEAR HANDLE OPERATED NORMALLY. MAINTENANCE UNABLE TO DUPLICATE. AS A P RECAUTION, MAINTENANCE REPLACED PSEU AND THE SYSTEM TESTED NO FAULTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998021900837 19980219 00837 NE 1998 2 19 AALA980041 2 19980108 A 7314 384300 FUEL PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 441AA 7720 49460 DFW - FLT 1389 - DURING TAKEOFF DFW, LT ENGINE SLOW TO SPOOL. AT LEVEL FLIGHT 22,000 FEET, LT EPR, N1 AND N2 STARTED FL UCTUATING. ENGINE WENT TO IDLE FOR A FEW SECONDS AND THEN STARTED OPERATING NORMALLY. AIRCRAFT RETURNED TO DFW AND LAN DED WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL PUMP AND FUEL CONTROL. LEAK CHECKED WITH NO DEFECTS FOUND. SYSTEM GRO UND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F 4 F A6WE E9NE 1998021900838 19980219 00838 WP 1998 2 19 AALA980015 1 19980102 A 3233 39281375001 ACTUATOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 516AM 49893 PHL - FLT 1511 - AFTER TAKEOFF PHL, NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO PHL AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED NLG RETRACT CYLINDER. ACCOMPLISHED GEAR RETRACTION AND OVERWEIGHT LANDING INSPECTION WITH NO DEFE CTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900839 19980219 00839 WP 1998 2 19 AALA980054 1 19980111 A 3222 5910448557 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 459AA 49564 PDX - FLT 1092 - AFTER TAKEOFF PDX, THE NOSE LANDING GEAR DID NOT RETRACT AND THE AIRCRAFT RETURNED PDX OVERWEIGHT WITHO UT INCIDENT. MAINTENANCE SERVICED NLG STRUT AND CYCLED GEAR SEVERAL TIMES WITH GEAR RETRACTING NORMALLY. AN OVERWEIGHT INSPECTION ACCOMPLISHED WITH NO DAMAGE NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900840 19980219 00840 WP 1998 2 19 AALA980050 1 19980109 A 3222 5920629513 PISTON DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 574AA 53151 DFW - FLT 1868 - AFTER TAKEOFF DFW, LANDING GEAR WAS RETRACTED AND THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. CREW A CCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT LANDED DFW OVERWEIGHT AND WITHOUT INCIDENT. MAINTENANCE REPLACED LOWER NLG PISTON, REPACKED AND SERVICED STRUT PER MM. AN OVERWEIGHT INSPECTION ACCOMPLISHED AND NO DISCREPANCIES NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900841 19980219 00841 WP 1998 2 19 AALA980053 1 19980110 A 2530 46700017 COFFEE MAKER DOUG DC9 DC982 3022082 WP GALLEY ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 474 49649 LIT - FLT 0826 - EN ROUTE IAH/ORD DURING CRUISE, FLIGHT ATTENDANT NOTED AN ELECTRICAL SMELL IN THE FIRST CLASS GALLEY AR EA. AIRCRAFT LANDED LIT WITHOUT INCIDENT. GALLEY COFFEE MAKERS AND OVENS WERE PLACARDED AND THE AIRCRAFT FERRIED TO OR D FOR FURTHER EVALUATION. MAINTENANCE OPERATED FIRST CLASS OVENS AND COFFEE MAKERS FOR ONE HOUR UNABLE TO DUPLICATE ELE CTRICAL SMELL. AS A PRECAUTION, BOTH COFFEE MAKERS WERE CHANGED. SYSTEM GROUND CHECKED, NORMAL OPERATION WITH NO SMOKE NOTED. (X) 2 L 7 2 4F A6WE 1998021900842 19980219 00842 NM 1998 2 19 AALA980118 1 19980114 A 2612 2156204A2602 FIRE DETECTOR AUTRONICS BOEING 757 757223 1384957 NM CARGO COMPT DEFECTIVE A AALA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 606AA 8660A7470 27057 DW - FLT 1203 - EN ROUTE SJU/DFW DURING CRUISE, AFT CARGO DETECTION STATUS CAME ON IN-FLIGHT. DISCHARGED BOTH AFT CARGO FIRE BOTTLES. AIRCRAFT LANDED DFW WITHOUT INCIDENT. CHECKED AFT CARGO COMPARTMENT AND CARGO FOR EVIDENCE OF FIRE OR O THER DAMAGE WITH NO DEFECTS NOTED. REPLACED BOTH FIRE WARNING DETECTORS AND THE TWO FIRE BOTTLES/SQUIBS THAT WERE EXTIN GUISHED IN-FLIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998021900843 19980219 00843 NM 1998 2 19 AALA980123 1 19980113 A 2751 215016001 INDICATOR GULL BOEING 757 757223 1384957 NM TE FLAPS TRIPPED A AALA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 SW 07 618AA 24526 SLC - FLT 2353 - DURING DESCENT INTO JAC, TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED AND AIRCRAFT DIVERTED TO SLC AND LANDED WITHOUT INCIDENT. FOUND LEFT HAND OUTBOARD FLAP TRANSMISSION FRICTION PIN TRIPPED. FRICTION PIN RESET AND FLAP S CYCLED WITH NO SYMMETRY FAULTS. SYSTEM GROUND CHECKED, NORMAL OPERATION AND AIRCRAFT RE-DEPARTED TO JAC. (X) 2 L 7 2 4F RT A2NM 1998021900846 19980219 00846 NM 1998 2 19 AALA980101 1 19980113 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39356 24037 SFO - DURING MAINTENANCE, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 30B INOPERATIVE. REPAIRED BROKEN WIRE AT EM ERGENCY EXIT LIGHT CONNECTOR, PASSENGER SEAT 30B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900847 19980219 00847 NM 1998 2 19 AALA980120 1 19980114 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388AA 27448 SFO - DURING MAINTENANCE, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 28HJ INOPERATIVE. REPAIRED BROKEN WIRE AT E MERGENCY EXIT LIGHT CONNECTOR PASSENGER SEAT 28HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900848 19980219 00848 NM 1998 2 19 AALA980137 1 19980117 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697AN 26977 DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENC Y FLOOR PATH LIGHTING WIRES IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998021900849 19980219 00849 NM 1998 2 19 AALA980170 1 19980119 A 3350 LIGHT BOEING 767 767223 1385123 NM AFT LAVATORY LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 327AA 22327 SFO - DURING OVERNIGHT MAINTENANCE, DISCOVERED EMERGENCY EXIT FLOOD LIGHT AT AFT RIGHT HAND LAVATORY POSITION INOPERATIV E. RE-SECURED EMERGENCY EXIT FLOOD LIGHT AT AFT RIGHT HAND LAVATORY POSITION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900850 19980219 00850 NM 1998 2 19 AALA980169 1 19980119 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 361AA 24042 SFO - DURING MAINTENANCE, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 34H INOPERATIVE. REPAIRED BROKEN WIRE AND R EPLACED PIN AND CONNECTOR FOR EMERGENCY EXIT LIGHT AT PASSENGER SEAT 34H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900851 19980219 00851 NM 1998 2 19 AALA980191 1 19980121 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 693AA 26973 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHT IN FORWARD CABIN INOPERATIVE. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE AT FORWARD CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998021900852 19980219 00852 NM 1998 2 19 AALA980192 1 19980120 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384AA 26996 SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 31HJ INOPERATIVE. RE-SEATED EMERGENCY E XIT LIGHT CONNECTOR AT PASSENGER SEAT 31HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900853 19980219 00853 NM 1998 2 19 AALA980193 1 19980120 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 381AN 25450 LHR - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 36HJ INOPERATIVE. REPLACED EMERGENCY EX IT LIGHT WIRE AT PASSENGER SEAT 36HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900854 19980219 00854 NM 1998 2 19 AALA980194 1 19980120 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339AA 22336 SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT SIGN AT LEFT AFT FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EM ERGENCY EXIT SIGN WIRE AT LEFT AFT FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900855 19980219 00855 NM 1998 2 19 AALA980190 1 19980121 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383AN 26995 SFO - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 38HJ INOPERATIVE. REPLACED EMERGENCY EX IT LIGHT CONNECTOR AT PASSENGER SEAT 38HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998021900856 19980219 00856 WP 1998 2 19 AALA980189 1 19980121 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 451AA 49477 DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT OVER WING EXIT ON RIGHT SIDE INOPERATIVE. REPAIRED BRO KEN EMERGENCY EXIT LIGHT WIRE AT RIGHT SIDE OVER WING EXIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900857 19980219 00857 WP 1998 2 19 AALA980136 1 19980117 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 246AA 49238 DFW - DURING OVERNIGHT CHECK, DISCOVERED FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FIRST CL ASS EMERGENCY EXIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900858 19980219 00858 WP 1998 2 19 AALA980135 1 19980116 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 590AA 53253 DFW - DURING OVERNIGHT CHECK, DISCOVERED FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FIRST CL ASS EMERGENCY EXIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998021900859 19980219 00859 WP 1998 2 19 AALA980132 1 19980118 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 587AA 53250 DFW - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED JUMPER WIRE FOR E MERGENCY EXIT LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900860 19980219 00860 WP 1998 2 19 AALA980186 1 19980121 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77421 49333 PHX - DURING OVERNIGHT CHECK, DISCOVERED EMERGENCY FLOOR LIGHTING NEAR PASSENGER SEAT 20DEF INOPERATIVE. REPLACED EMERG ENCY FLOOR LIGHT STRIP AT PASSENGER SEAT 20DEF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900861 19980219 00861 WP 1998 2 19 AALA980182 1 19980120 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 513AA 49890 DFW - DURING OVERNIGHT CHECK, DISCOVERED FORWARD GALLEY EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FORW ARD GALLEY EMERGENCY FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900869 19980219 00869 NM 1998 2 19 EISA98002 1 19980110 A 2780 MECHANISM BOEING 727 727223 1384074 NM NR 2 L/E FLAP OUT OF ADJUST A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 AFTER TAKEOFF, AMBER L/E FLAP LIGHT ILLUMINATED ON F/E PANEL, NR 2 STAYS ILLUMINATED. AIRCRAFT FEELS LIKE SLATS ARE DEP LOYED WHICH FLAPS ARE MOVED TO 20 POSITION. ADJUSTED AND RIGGED NR 2 L/E SLAT IAW MM CHAPTER 27. OPS CHECK GOOD. TT: 71,949:41 HOURS. TC: 49,405. (X) 2 L 7 3 4F A3WE 1998021900870 19980219 00870 NM 1998 2 19 EISA98003 1 19980109 A 2612 CONNECTOR BOEING 727 727251 138408H NM FIRE LOOP DIRTY A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 263US 19982 FIRE WARNING BELL SOUNDED AND AUTOPACK TRIP ACTIVATED. CLEANED FIRE LOOP CONNECTORS AND RAN FOR OVER 70 MINUTES. COULD NOT DUPLICATE, OPS CHECK GOOD. TT: 57,821:1 HOURS. TC: 47,618. (X) 2 L 7 3 4F A3WE 1998021900871 19980219 00871 SW 1998 2 19 98ZZZX743 1 19980118 A 2420 A703EB RELAY FRCHLD SA227 SA227DC 3377521 SW RT ENGINE INOPERATIVE A EQGA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 19 847LS 15 SM400D61 DC847B DFW/ELD - FLT 1253 - WHILE IN CRUISE AT FL 170, CREW RECEIVED RT GEN FAIL LIGHT. QRH CONSULTED AND GENERATOR SWITCH - OFF - RESET - ON INSTRUCTIONS FOLLOWED. GEN CAME BACK ON-INE. APPROX 3 MINUTES LATER, RT GEN FAIL LIGHT AGAIN ILLUMINA TED. QRH WAS FOLLOWED AND GENERATOR CAME ON-LINE. THREE MINUTES LATER, FAIL LIGHT ILLUMINATED AGAIN. CREW TURNED THE RT GENERATOR OFF AND CALLED FLIGHT CONTROL. AIRCRAFT DIVERTED INTO HOT AND LANDED WITH NO FURTHER ABNORMALITIES. MAINT ENANCE INSPECTED ACFT AND DETERMINED FAULT TO BE CAUSED BY FAULTY GENERATOR CONTROL RELAY. MAINTENANCE REPLACED RELAY A ND STARTER GENERATOR AS A PRECAUTION. ENGINE RUNS AND OPERATIONAL CHECKS SATISFACTORY. ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A18SW 1998021900887 19980219 00887 WP 1998 2 19 AALA980016 1 19980104 A 3222 2C9294 VALVE CRISSAIR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 516AM 49893 LAS - FLT 1342 - AFTER TAKEOFF LAS, NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO LAS AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPACKED NOSE LANDING GEAR AND REPLACED SERVICE VALVE. ACCOMPLISHED LEAK CHECK AND GEAR RETRACTION WITH NO DEFECTS FOUND. ACCOMPLISHED OVERWEIGHT CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998021900888 19980219 00888 NM 1998 2 19 USAASB98009 1 19980112 A 3350 AD20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 424US 23991 ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY/EXIT/EVACUATION LIGHTS INOP, ROW 12 RIGHT AND 20 LEFT BULLNOSE, SEAT MOU NTED LIGHTS AT ROWS 12 THROUGH 19 AND SIDEWALL EXIT LIGHT AT ROW 12F. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT ROW 20 CEILING, 5 INCHES LEFT OF AIRCRAFT CENTERLINE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998021900889 19980219 00889 NM 1998 2 19 USAA980008 1 19980110 A 5330 SKIN BOEING 737 737201 1384454 NM BS 935 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 225US 50879 21667 ROA - DURING BX-1 CHECK VISUAL INSPECTION, FOUND 1.75 INCH CRACK STATION 935 STRINGER 24L SKIN. INSTALLED DOUBLER, REPA IRED PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998021900890 19980219 00890 NM 1998 2 19 USAASB98005 1 19980106 A 2761 049415 SEAL BOEING 737 737201 1384454 NM RT SPOILER ACT FAILED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 233US 22273 BWI - FLT 2299 - FLT DEPARTED MHT THEN DIVERTED TO BWI DUE TO HYDRAULIC SYSTEM QTY DROPPING BELOW REFILL LINE. HYDRAULI C SYSTEM WAS SERVICED AND CHECKED FOR LEAKS. NO LEAKS WERE NOTED. FLIGHT THEN DEPARTED BWI AND RETURNED TO FIELD SHORT LY THEREAFTER DUE TO HYDRAULIC SYSTEM QTY AGAIN GRADUALLY DROPPING TO BELOW THE REFILL LINE. FLIGHT LANDED WITHOUT FURT HER INCIDENT. MAINTENANCE FOUND A BLOWN O-RING SEAL FOR THE RIGHT WING INBOARD SPOILER ACTUATOR. REPLACED SAME, SERVIC ED HYDRAULIC SYSTEM. GROUND TEST AND LEAK CHECK GOOD. ALSO, CHECKED ALL HYDRAULIC PUMPS. PUMPS WERE FOUND NORMAL. (M ) 2 L 7 2 4F A16WE 1998021900891 19980219 00891 NM 1998 2 19 USAASB98011 1 19980113 A 3234 MS253831 SWITCH BOEING 737 737201 1384454 NM GEAR HANDLE OUT OF ADJUST A USAA O OTHER O OTHER DE DESCENT 1 EA 19 241US 22443 BWI - FLT 254 - WHEN LANDING GEAR WAS EXTENDED, CREW RECEIVED 3 GREEN LIGHTS AND 3 RED LIGHTS. GEAR WAS CYCLED AND NORM AL GEAR INDICATION WAS RECEIVED, 3 GREEN LIGHTS AND NO RED LIGHTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED GEAR HANDLE DOWNLOCK SWITCH AND LUBED GEAR HANDLE SLIDE LOCK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998021900892 19980219 00892 NM 1998 2 19 USAASB98004 1 19980106 A 2170 V1211 SEPARATOR BAGS BOEING 737 737201 1384454 NM A/C BAY DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 226US 21815 CLT - FLT 776 - CLIMBING THROUGH 4,000 FEET, CREW SMELLED A SMOKY ODOR THAT RESEMBLED A BURNING CANDLE SMELL IN THE COCK PIT. ODOR WAS ALSO PRESENT IN THE CABIN. NO INDICATION OF SMOKE WAS PRESENT THROUGHOUT THE AIRCRAFT INCLUDING THE GALL EYS AND COCKPIT. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCI DENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE RAN THE PACKS USING APU AND ENGINE AIR. COULD NOT DUPLICA TE ODOR ON THE GROUND. FOUND WATER SEPARATOR BAGS DIRTY. REPLACED SAME. OPS AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998021900893 19980219 00893 NM 1998 2 19 USAASB98014 1 19980117 A 2910 B-NUT BOEING 737 737201 1384454 NM NR 3 SPOILER ACT LOOSE A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 226US 21815 SAV - FLT 1481 - AT FL 310, THE 'A' SYSTEM HYDRAULIC QTY SLOWLY DROPPED TO 1.2 GALLONS. CAPTAIN NOTICED THE QTY HAD BEE N SLOWLY DROPPING OVER THE LAST HOUR. THE, 'B' SYSTEM HYDRAULIC SYSTEM LOW QTY LIGHT ILLUMINATED. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT DIVERTED TO SAV. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE ON ITS OWN. MAINTENANC E FOUND A LOOSE CONNECTION ON THE NR 3 SPOILER ACTUATOR. TIGHTENED B-NUT. ALSO, TIGHTENED B-NUT ON FLIGHT CONTROL MODU LE. SERVICED HYDRAULIC SYSTEM AND CHECKED FOR LEAKS. NO LEAKS NOTED. (M) 2 L 7 2 4F A16WE 1998021900894 19980219 00894 NM 1998 2 19 USAASB98012 1 19980114 A 7930 42D107A1M BYPASS SW BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 233US 22273 BOS - FLT 786 - CLIMBING OUT FROM BOS ABOUT 8,000 FEET, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE, DECLARED AND EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOT AL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE CHECKED THE NR 1 ENGINE OIL AND FILTER FOR CONTAMINATION. CHECKED GO OD. REMOVED AND REPLACED THE OIL FILTER BYPASS SWITCH AND CANNON PLUG. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998021900895 19980219 00895 NM 1998 2 19 98ZZZM203 1 19980114 A 7930 BACC63BN12C3S CONNECTOR BOEING 737 737201 1384454 NM NR 1 ENGINE DIRTY A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 233US 22273 BOS - FLT 786 - CLIMBING OUT FROM BOS ABOUT 8,000 FEET, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE, DECLARED AND EMERGENCY AND RETURNED TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOT AL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE CHECKED THE NR 1 ENGINE OIL AND FILTER FOR CONTAMINATION. CHECKED GO OD. REMOVED AND REPLACED THE OIL FILTER BYPASS SWITCH AND CANNON PLUG. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998021900896 19980219 00896 NM 1998 2 19 USAA980009 1 19980109 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 42739 22444 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 767 STRINGER 19R FUSELAGE SKIN. REMOVED CRACKED SKIN AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900897 19980219 00897 NM 1998 2 19 USAA980010 1 19980109 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 42739 22444 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 4 INCH CORROSION STRINGER 27L, BSL 967. REMOVED CORRODED STR INGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900898 19980219 00898 NM 1998 2 19 USAA980000 1 19980103 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 39799 22797 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 520 PLUS 10 INCH STRINGER 15L. CUT OUT STRINGER INSTALLED STRINGER REPAIR. REPAIRED PER EA 43431, SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900899 19980219 00899 NM 1998 2 19 USAA980001 1 19980103 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 39799 22797 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STATION 520 PLUS 13 INCHES STRINGER 15R. CUT OUT DAMAGED AREA OF STRINGER, INSTALLED STRINGER REPAIR. REPAIRED PER EA 43431 SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900900 19980219 00900 NM 1998 2 19 USAA980003 1 19980103 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 39799 22797 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK STATION 727 BULKHEAD UPPER CHORD ANGLE RBL 25 INCH. I NSTALLED REPAIR ANGLE, REPAIRED PER TR 53-10-03A. (M) 2 L 7 2 4F A16WE 1998021900903 19980219 00903 EU 1998 2 19 USAAF98003 1 19980107 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK1000 4990808 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 868US 11313 IND - THE AFT RIGHT WING FAIRING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CORRESPONDING POWER SUPPLY AND BATTERY PACK. (M) 2 L 7 2 4F RT A20EU 1998021900904 19980219 00904 EU 1998 2 19 98ZZZM204 1 19980107 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK1000 4990808 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 868US 11313 IND - THE AFT RIGHT WING FAIRING EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE CORRESPONDING POWER SUPPLY AND BATTERY PACK. (M) 2 L 7 2 4F RT A20EU 1998021900905 19980219 00905 NE 1998 2 19 EISA98001 2 19980114 A 7200 ENGINE BOEING 727 727221 1384071 NM PWA JT8 JT8D15 52051 NE NR 2 FAILED A EISA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SW 07 367PA 22539 NR 2 ENGINE FAILED ON GO AROUND. REMOVED AND REPLACED NR 2 ENGINE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998021900906 19980219 00906 WP 1998 2 19 VTZA98013 2 19980108 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 494UE 810 FLT 6151 - IAD-PHF - ABORTED TAKEOFF DUE TO LEFT ENGINE WOULD ONLY MAKE 98 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED MAX FUEL, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998021900909 19980219 00909 WP 1998 2 19 WTAA980001 2 19980102 A 7321 NAS1351C3LL6 BOLT BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP FUEL CONTROL MISSING A WTAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 17 430UE 784 SBP - LEFT ENGINE LOST RPM DURING CLIMB-OUT, AIRCRAFT RETURNED TO STATION. MAINTENANCE RESECURED RPM LEVER ROD END ASSE MBLY. PERFORMED ENGINE RUN. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998021900911 19980219 00911 NE 1998 2 19 HNAA9898602 2 19980104 A 7314 311709402 FUEL PUMP DHAV DHC8 DHC8201 2809001 NM PWA 120 PW120A NE NR 2 ENGINE FAILED A HNAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 EA 07 986HA 2398 421 FLT 3464 - MCO-MIA - AFTER TAKEOFF, WHILE CLIMBING AT 13,000 FT, THE NR 2 ENGINE FAILED. THE CREW DECLARED AND EMERGENC Y AND RETURNED TO MCO WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 FUEL PUMP AND MECHANICAL FUEL CONTROL (MFC). (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1998021900912 19980219 00912 NE 1998 2 19 98ZZZM205 2 19980104 A 7314 311717502 FUEL PUMP DHAV DHC8 DHC8201 2809001 NM PWA 120 PW120A NE NR 2 ENGINE FAILED A HNAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 EA 07 986HA C31014V 421 FLT 3464 - MCO-MIA - AFTER TAKEOFF, WHILE CLIMBING AT 13,000 FT, THE NR 2 ENGINE FAILED. THE CREW DECLARED AND EMERGENC Y AND RETURNED TO MCO WITHOUT INCIDENT. REMOVED AND REPLACED THE NR 2 FUEL PUMP AND MECHANICAL FUEL CONTROL (MFC). (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1998021900914 19980219 00914 NE 1998 2 19 USAAD98004 2 19980108 A 7261 ACB735F1630Y1 FILTER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE CLOGGED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 937VJ 48117 PIT - FLT 1964 - DURING CRUISE, THE LEFT ENGIEN OIL STRAINER CLOG LIGHT CAME ON INTERMITTENTLY. THE OIL PRESSURE TEMPER ATURE REMAINED NORMAL. DURING REDUCED THRUST THERE WAS NOT CHANGE. THE CREW ELECTED TO DIVERT TO PIT WITH THE ENGINE O PERATED AT REDUCED POWER AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE OIL FILTER AND FILTER CLOG L IGHT SWITCH. THE ENGINE THEN OPERATED NORMALLY. (M) 2 L 7 2 4F 4 F A6WE E2EA 1998021900915 19980219 00915 WP 1998 2 19 98ZZZM206 1 19980108 A 7930 42D1091 SWITCH DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE CLOGGED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 937VJ 48117 PIT - FLT 1964 - DURING CRUISE, THE LEFT ENGIEN OIL STRAINER CLOG LIGHT CAME ON INTERMITTENTLY. THE OIL PRESSURE TEMPER ATURE REMAINED NORMAL. DURING REDUCED THRUST THERE WAS NOT CHANGE. THE CREW ELECTED TO DIVERT TO PIT WITH THE ENGINE O PERATED AT REDUCED POWER AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE OIL FILTER AND FILTER CLOG L IGHT SWITCH. THE ENGINE THEN OPERATED NORMALLY. (M) 2 L 7 2 4F 4 F A6WE E2EA 1998021900916 19980219 00916 EU 1998 2 19 JBXA980030 2 19980111 A 7532 32899023 BLEED VALVE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 2 ENGINE CLOSED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 105ML 11475 RDU - FLT 17 - IN CLIMB, PACKS PRESSURE CONTROLLER PACK FAULTED, COULD NOT RESET, RETURN TO RDU. PERFORMED BITE CHECK O N PRESSURE CONTROLLER FAULTED DUE TO NR 2 ENGINE BLEED VALVE CLOSED. (M) 2 L 7 2 4F 4 F RT 1998021900918 19980219 00918 NM 1998 2 19 ASAA981009 1 19980116 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHTS WERE FOUND TO BE DIM. REPLACED BATTERY TO SMOKE BARRIER LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998021900919 19980219 00919 1998 2 19 VTZA98015 4 19980114 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 320UE 41043 FLT 6236 - BWI-BOS - DURING CRUISE, EXPERIENCED A DISCREPANCY WITH THE NR 1 AHRS COMPUTER FAILING. AIRCRAFT DIVERTED TO IAD WHERE MAINTENANCE CONTROL AND MAINTENANCE WAS NOTIFIED. MAINTENANCE REMOVED AND REPLACED THE AHRS COMPUTER IAW MX PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998021900920 19980219 00920 WP 1998 2 19 TWAA9801201 1 19980121 A 4990 3812761 APU DOUG DC9 DC983 3022083 WP APU COMPT OIL LEAK A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 9302B 30804 49528 STL - FLT 345 - AFTER PARKING IN GATE, AIRCRAFT STARTED FILLING WITH SMOKE. REPLACED APU MFG P/N 381276-1 DUE TO OIL CO MING FROM INLET. (M) 2 L 7 2 4F RT A6WE 1998021900921 19980219 00921 NE 1998 2 19 TWAA9801102 2 19980119 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE LEFT FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN Z SIGNIFICANT FAILURE REPORT CR CRUISE 1 CE 05 9409F 53121 1225 AM - FLT 1508 - DURING CRUISE, VIBRATION OCCURED ON THE LEFT ENGINE. ENGINE SHUT DOWN. REPLACED LEFT ENGINE DUE TO FAI LURE CAUSED BY BLUE ICE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1998021900922 19980219 00922 NE 1998 2 19 TWAA9801101 2 19980120 A 7510 652673831 DUCT BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE DAMAGED A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 54330 20308 4018 SLC - FLT 844 - DURING CLIMB, NR 3 ENGINE FIRE WARNING OCCURED. ENGINE SPEED REDUCED TO IDLE. RETURNED TO SLC. REPLAC ED NR 3 ENGINE ANTI-ICE DUCT, MFG PART NUMBER 65-26738-31 DUE TO HOLE IN DUCT. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998021900923 19980219 00923 WP 1998 2 19 TWAA9801001 1 19980119 A 3260 49319271 SPRING DOUG DC9 DC951 3022051 WP LT MLG BROKEN A TWAA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 414EA 47746 STL - FLT 247 - DURING CRUISE, LEFT RED GEAR UNSAFE LIGHT ILLUMINATED. REPLACED BROKEN SPRING, MFG PART NR 4931927-1, O N LEFT GEAR UPLOCK TARGET. (M) 2 L 7 2 4F RT A6WE 1998021900924 19980219 00924 EU 1998 2 19 SABA980004 1 19980120 A 2120 AIR DISTRIBUTION BAG JETSTM JETSTM3101 1500215 EU COCKPIT ODOR A SABA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 33 161PC 675 CLT-HKY- FLT 5048 - CAPTAIN REPORTED A STRONG RUBBER OR BURNING SMELL IN THE COCKPIT. CAPTAIN TURNED OFF ALL FLOWS AND SMELL WENT AWAY. AIRCRAFT RETURNED TO CLT AND NO EMERGENCY WAS DECLARED ALSO. NO PASSENGERS WERE ABOARD THIS FLT. AIR CRAFT WAS INSPECTED AND GROUND RUN, THIS PROBLEM COULD NOT BE DUPLICATED. (M) 2 L 7 2 4T RT A21EU 1998021900925 19980219 00925 EU 1998 2 19 SABA980005 1 19980122 A 3297 WIRE BAG JETSTM JETSTM3201 1500217 EU RT MLG BROKEN A SABA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 33 962AE 962 CLT-AHN - FLT 5120 - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT STAYED ON AFTER TAKEOFF. CREW CYCLED GEAR SEVERAL TIMES AN D LIGHT REMAINED ON. AIRCRAFT RETURNED TO CLT AND NO EMERGENCY WAS DECLARED. MAINTENANCE WAS DISPATCHED AND INSPECTED THE AIRCRAFT AND FOUND A BROKEN WIRE ON THE UPLOCK SWITCH. WIRE WAS REPAIRED AND GEAR WAS OPS CHECKED AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998021900930 19980219 00930 NM 1998 2 19 USAA980015 1 19980117 A 5315 654681143 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 986.5 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 22959 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AT TOP OF THE FLOORBEAM AND SCREW HOLES .5 INCH BY .5 INCH STA TION 986.5. CORROSION TASK NR C 53-107-02. REPLACED T-CAP AT FLOORBEAM 986.5 PER REPAIR DOCUMENT SRM 53-10-05. (M) 2 L 7 2 4F RT A16WE 1998021900931 19980219 00931 NM 1998 2 19 USAA980014 1 19980117 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 37007 22959 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AT THE FASTENER STATION 328 FLOORBEAM RBBL 12 ON FRAME. CORRO SION TASK NR C 53-107-02. INSTALLED REPLACEMENT T-CAP SPLICE PER TYPICAL REPAIR DOCUMENT 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998021900932 19980219 00932 NM 1998 2 19 USAA980013 1 19980117 A 5313 STRINGER BOEING 737 7373B7 1384580 NM BS 887 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 37007 22959 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT STRINGER 21L, STATION 887 STRINGER. CORRO SION TASK NR C 53-202-01. INSTALLED STRINGER SPLICE PER REPAIR DOCUMENT SRM 53-00-03. (M) 2 L 7 2 4F RT A16WE 1998021900933 19980219 00933 NM 1998 2 19 USAA980012 1 19980117 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 947.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 37007 22959 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AT UPPER SURFACE AND SCREW HOLES AT FLOORBEAM STATION 947.5. C ORROSION TASK NR C 53-107-02. INSTALLED REPAIR STRAP PER REPAIR DOCUMENT NR SRM 53-00-51 FIGURE 203. (M) 2 L 7 2 4F RT A16WE 1998021900934 19980219 00934 NM 1998 2 19 USAA980011 1 19980117 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 22959 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON TOP OF FLOORBEAM AT THE SCREW HOLES AT STATION 967 FLOORBEA M. CORROSION TASK NR C-53-107-02. BURNISHED AND TREATED AREA OF MINOR CORROSION. REPLACED T-CAP WHERE NECESSARY PER R EPAIR DOCUMENT AND SRM 53-00-51 AND TYPICAL REPAIR NR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1998021900935 19980219 00935 NM 1998 2 19 USAASB98023 1 19980123 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 280AU 22892 CLT - MAINTENANCE FOUND THE FORWARD, CENTER AND AFT CABIN OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLA CED THE THREE BATTERY PACKS AT EACH INDIVIDUAL OVERHEAD LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998021900936 19980219 00936 WP 1998 2 19 USAAD98019 1 19980108 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 931VJ 47188 PHL - THE GALLEY DOOR ESCAPE SLIDE LIGHT AND THE CEILING EMERGENCY LIGHTS IN ROWS 13 THROUGH 18 ARE INOPERATIVE. MAINTE NANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998021900937 19980219 00937 WP 1998 2 19 98ZZZM207 1 19980108 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 931VJ 47188 PHL - THE GALLEY DOOR ESCAPE SLIDE LIGHT AND THE CEILING EMERGENCY LIGHTS IN ROWS 13 THROUGH 18 ARE INOPERATIVE. MAINTE NANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998021900938 19980219 00938 WP 1998 2 19 USAAD98020 1 19980129 A 3222 1D3224044 STRUT DOUG DC9 DC931 3022065 WP NLG LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 926VJ 48146 PIT - FLT 1712 - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. CREW RECYCLED GEAR TO NO AVAIL. FLIGHT RETURNED TO PIT AN D LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR PISTON ASSEMBLY AND PERFORMED A GEAR SWIN G. ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998021900940 19980219 00940 NM 1998 2 19 USAABB98010 1 19980123 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 617AU 27148 LGA - FOUND RIGHT FORWARD DOOR EXIT IDENTIFIER INOPERABLE. MAINTENANCE REPLACED THE EXIT IDENTIFIER. (M) 2 L 7 2 4F RT A2NM 1998021900941 19980219 00941 NM 1998 2 19 USAABB98009 1 19980120 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM R4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 LGA - FOUND RIGHT AFT SERVICE DOOR EXIT IDENTIFIER INOPERABLE. MAINTENANCE REPLACED THE EXIT IDENTIFIER ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998021900942 19980219 00942 WP 1998 2 19 TWAA9801501 1 19980126 A 5312 BULKHEAD JAMB DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 973Z 47033 STL - DURING MAINTENANCE CHECK, THE AFT PERSSURE BULKHEAD LOWER DOOR JAMB LOWER LEFT CORNER WAS FOUND CRACKED 1.375 INCH ABOVE -37 DOUBLER. REPAIRED PER EMLR 65796-J060088-515 AND SRM 51-30-0 STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998021900943 19980219 00943 WP 1998 2 19 TWAA9801405 1 19980125 A 3397 58531 WIRE DOUG DC9 DC931 3022065 WP CABIN WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 993Z 47082 STL - 698 - DURING OVERNIGHT MAINTENANCE, THE FLOOR EMERGENCY EGRESS LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 22 TO 24. REPLACED THE FEED CABLE FROM THE BATTERY PACK TERMINAL STRIP TO FLEX CABLE. (M) 2 L 7 2 4F A6WE 1998021900944 19980219 00944 WP 1998 2 19 TWAA9801404 1 19980125 A 3220 5929719501 DEFLECTOR DOUG DC9 DC951 3022051 WP NLG BENT A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 406EA 47686 STL - FLT 482 - AFTER TAKEOFF, NOSE LANDING GEAR WOULD NOT RETRACT. GREEN LIGHT WENT OUT. RED NOSE LIGHT CAME ON. NOI SE LEVEL INDICATED NOSE GEAR WAS DOWN. RETURNED TO STL. FOUND LT NOSE GEAR SPRAY DEFLECTOR JAMMING AGAINST FRAME. REP LACED LT SPRAY DEFLECTOR. (M) 2 L 7 2 4F RT A6WE 1998021900945 19980219 00945 WP 1998 2 19 TWAA9801403 1 19980126 A 2131 21171802 CONTROLLER DOUG DC9 DC982 3022082 WP LT/RT WORN A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 904TW 49156 MCI - FLT 337 - UPON LEVEL OFF AT FL350, CABIN CONTINUED TO CLIMB. DESCENDED TO FL240. CABIN ALTITUDE REACHED 13000 FT . REGAINED CONTROL OF CABIN WITH MANUAL CONTROL OF OUTFLOW VALVE. REPLACED BOTH CABIN PRESSUE CONTROLLERS AND BROKEN C LAMP ON A DUCT. (M) 2 L 7 2 4F A6WE 1998021900946 19980219 00946 NM 1998 2 19 TWAA9801402 1 19980125 A 3350 6013211 BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54352 21984 STL - FLT 463 - DURING OVERNIGHT MAINTENANCE CHECK, FOUND RT AFT ESCAPE SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1998021900947 19980219 00947 WP 1998 2 19 TWAA9801401 1 19980124 A 2133 39605011 VALVE DOUG DC9 DC931 3022065 WP RIGHT WORN A TWAA O OTHER O OTHER CL CLIMB 1 CE 05 991Z 47096 STL - FLT 107 - AFTER NORMAL TAKEOFF AND PRESSURIZATION NORMAL, AT APPROX 5000 MSL NOTICED OUTFLOW VALVE CLOSED AND PACK PRESSURE NORMAL BUT AIRCRAFT NOT PRESSURIZING. FLIGHT OPERATED AT 10,000 FT WITH PACKS OFF. REPLACED THE RIGHT AC FLO W CONTROL VALVE. ALSO, INSTALLED BLOWN DUCTS TO ACM. (M) 2 L 7 2 4F A6WE 1998021900948 19980219 00948 WP 1998 2 19 TWAA9801701 1 19980202 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 737 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 978Z 47250 STL - DURING OP16 MAINTENANCE CHECK, LONGERON 5L WAS FOUND WITH A .5 INCH CRACK AT STATION 737. REPAIRED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1998021900950 19980219 00950 NM 1998 2 19 TAOA019817 1 19980131 A 3350 1000679 LIGHT BOEING 727 727254 138408L NM CABIN FAILED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 914TS 20251 BOS - R-1 DOOR EMERGENCY LIGHT DOES NOT OPERATE WITH OTHER EMERGENCY LIGHTS. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY, OP ERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998021900951 19980219 00951 NM 1998 2 19 TAOA029801 1 19980201 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 20415 FLT 6530 - LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED CHARGING UNIT AND BATTERY PACK. OPERATIONAL CHEC K NORMAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998021900952 19980219 00952 NM 1998 2 19 TAOA019815 1 19980131 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 21244 FLT 6151 - DURING OVERNIGHT L/S LGA, FORWARD ENTRY AISLE EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY PACK, OPERAT IONAL CHECK NORMAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998021900953 19980219 00953 NM 1998 2 19 TAOA019816 1 19980131 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 21244 FLT 6151 - OVERNIGHT L/S LGA, EMERGENCY EXIT SIGN AT ROW 3 IS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NOR MAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998021900954 19980219 00954 NM 1998 2 19 TAOA019812 1 19980126 A 2782 1U1110 ACTUATOR BOEING 727 727225 1384077 NM NR 2 LE FLAP JAMMED A TAOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 922TS 20415 ON CLIMB-OUT, WHILE RETRACTING FLAPS FROM 5 DEGREES TO 10 DEGREES NR 2 LEADING EDGE FLAP REMAINED FULLY EXTENDED, CYCLED FLAPS NO HELP. REPLACED NR 2 LEADING EDGE FLAP ACTUATOR. OPERATIONAL CHECKS NORMAL PER MM CHAPTER 27-81-22. (M) 2 L 7 3 4F A3WE 1998021900955 19980219 00955 NM 1998 2 19 TAOA019813 1 19980125 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 926TS VA5628 20774 FLT 6131 - BOS-LGA - L-2 EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998021900956 19980219 00956 NM 1998 2 19 TAOA019814 1 19980128 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 4855 20415 FLT 6512 - DCA-LGA - LEFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECKS NORMAL P ER MM 33-50. (M) 2 L 7 3 4F A3WE 1998021900957 19980219 00957 EU 1998 2 19 SIMA980332 1 19980202 A 3233 D232130001 ACTUATOR AEROSP ATR72 ATR72212 EU LT MLG FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 355AT MW129 355 DFW - FLT 3521 - AFTER TAKEOFF BOTH MAIN GEARS INDICATED UNLOCKED WITH GEAR SELECTED UP, SELECTED GEAR DOWN, GOT 3 GREEN LIGHTS. RETURNED TO DFW LANDING WITHOUT INCIDENT. MAINTENANCE CHECKED ELECTRICAL SYSTEM WITH NO DISCREPANCIES NOTED, CHECK MAIN GEAR ACTUATORS. FOUND LEFT ACTUATOR INTERNAL LEAKING. R/I'D LEFT ACTUATOR AND PERFORMED RETRACTION TEST SAT ISFACTORILY, ALSO PERFORMED FLT FLEET SATISFACTORILY PRIOR TO RETURNING A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021900958 19980219 00958 EU 1998 2 19 SIMA980241 1 19980124 A 3320 83S0558800 POWER MODULE AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 288AM 288 CRP - FLT 3829 - PASSENGERS REPORTED A BURNT SMELL AND SMOKE NEAR ROW 9. FLT CREW PULLED C/B MAINTENANCE FOUND TRANSFOR MER ON 11 AB BURNED. DISCONNECTED TX FROM POWER SOURCE. ISSUED MEL 25-19 AND RETURNED A/C TO SERVICE. R/I'D READING L IGHT POWER MODULE AT ROW 11 AB. PERFORMED OPERATIONAL CHECK SATISFACTORILY. REMOVED MEL AND RETURNED A/C TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998021900959 19980219 00959 EU 1998 2 19 SIMA980271 1 19980127 A 3246 50092371 WHEEL SAAB SF340 340B 7860101 EU NR 1 WHEEL BROKEN A SIMA K NONE P NO WARNING INDICATION TX TAXI/GRND HDL 1 SW 21 373AE 340B373 DFW - FLT 3816 - CREW REPORTED AFTER LANDING AND WHILE TAXIING, THE NR 1 AND NR 2 MAIN TIRES BLEW OUT. MAINTENANCE FOUN D NR 1 WHEEL ASSY HAD APPROX ONE-THIRD OF INBOARD RIM FLANGE BROKEN OFF AND NR 2 TIRES INBOARD SIDE WALL DAMAGED. R/I'D NR 1 AND NR 2 WHEEL ASSYS. PERFORMED VISUAL INSPECTION OF LEFT GEAR AND ASSENT AIRFRAME FOR DAMAGE, NO DISCREPANCIES N OTED. REPLACED NR 1 AND NR 2 BRAKE ASSY AS PRECAUTIONARY. PERFORMED GEAR RETRACTION CHECK AND RETURNED A/C TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998021900960 19980219 00960 EU 1998 2 19 SIMA980291 1 19980129 A 5330 S5337131101260 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE PUNCTURE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 424MQ 045 SAW - MAINTENANCE DISCOVERED A SMALL HOLE IN THE FUSELAGE JUST AFT OF THE RIGHT ICE SHIELD. MAINTENANCE REPAIRED THE ON E INCH PUNCTURE BETWEEN FRAME 22 AND 23 AND BETWEEN STRINGER 13 RIGHT AND 14 RIGHT IAW SRM 53-00-00 PAGE 410 FIGURE 403. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998021900961 19980219 00961 EU 1998 2 19 REXA98042 1 19980202 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG FAILED A REXA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 110PX 340A023 LOST HYDRAULIC PRESSURE IN MAIN RESERVOIR WITH A CWP WARNING. REMOVED AND REPLACED RIGHT MAIN GEAR HYD SWIVEL. PERFORM ED GEAR SWING, CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900962 19980219 00962 EU 1998 2 19 REXA98041 1 19980131 A 7600 5308214 CONTROL QUADRANT SAAB SF340 SF340A 7850100 EU COCKPIT INOP A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 403BH 340A060 FI STOP LIGHT COMES ON IN FLIGHT, RESET ONCE, LIGHT CAME ON IN NEXT FLIGHT. GATE AIR RETURN. REMOVED AND REPLACED CONT ROL QUADRANT. (M) 2 L 7 2 4T RT A52EU 1998021900963 19980219 00963 NE 1998 2 19 REXA98040 2 19980131 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RIGHT FAILED A REXA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 346AM 340A032 GEE367210DKU RIGHT ENGINE OIL PRESSURE 0 PSI, AND RIGHT ENGINE OIL PRESSURE LIGHT ON. REMOVED AND REPLACED RIGHT ENGINE. PERFORMED GROUND RUN, CHECKS GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998021900964 19980219 00964 EU 1998 2 19 REXA98039 1 19980129 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3101 1500215 EU RIGHT INOP A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 305PX D35947 666 ON CLIMB-OUT, RIGHT RPM WENT TO ZERO AND BACK TO 100 PERCENT NUMEROUS TIMES. REMOVED AND REPLACED RIGHT TACH GENERATOR. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998021900965 19980219 00965 EU 1998 2 19 REXA98038 1 19980130 A 2720 RUDDER PEDAL BAG JETSTM JETSTM3101 1500215 EU RIGHT STUCK A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 302PX 661 RIGHT RUDDER PEDAL STUCK AFTER TAKEOFF ROLL. COULD NOT DUPLICATE ON GROUND. HAD A CREW TEST FLY AIRCRAFT, FOUND NOTHIN G WRONG WITH RUDDER. (M) 2 L 7 2 4T RT A21EU 1998021900966 19980219 00966 1998 2 19 REXA98037 4 19980129 A 3425 6226190113 AHRS COMPUTER SAAB SF340 SF340A 7850100 EU LEFT FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 326PX 285 340A054 RED FLAG ON R RMI OFF. FD FLAG ON. REMOVED AND REPLACED LEFT AHRS COMPUTER. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900967 19980219 00967 EU 1998 2 19 REXA98036 1 19980124 A 7712 CTOT SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A REXA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 25 370PX 340B300 LEFT CTOT WOULD NOT HOLD. CREW DID ANOTHER P-3 TST. OPS CHECK GOOD. TRIED ANOTHER T/O OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900968 19980219 00968 NE 1998 2 19 REXA98035 2 19980125 A 7210 77580010 PROP GEAR BOX SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A REXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 406BH UDAG0262 340A074 367165DKULH CREW SHUT DOWN LEFT ENGINE, NO OIL PRESSURE. COULD NOT FEATHER LEFT PROP. REMOVED AND REPLACED LEFT PROP GEARBOX. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998021900969 19980219 00969 NE 1998 2 19 REXA98034 2 19980127 A 7321 7086M60G11 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE SURGE A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 401BH ECDE5143 340A057 RIGH ENGINE HAS A POWR SURGE OF 5 TO 8 PERCENT IN THE 40 PERCENT TORQUE RANGE WHILE PUSHING UP POWER. REMOVED AND REPLA CED RIGHT ELECTRICAL CONTROL UNIT. GROUND RUN CHECKS GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998021900970 19980219 00970 EU 1998 2 19 REXA98033 1 19980126 A 3610 NH24668071 DUCT ASSY SAAB SF340 SF340A 7850100 EU LT ENGINE LOOSE A REXA F ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION CL CLIMB 1 SO 25 347AM 340A039 LEFT ENGINE INTAKE MATT HAD FIRE. SHUT DOWN ENGINE AND FIRED THE BOTTLE. REMOVED AND REPLACED LEFT LOWER DUCT ASSY. O PS CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900971 19980219 00971 EU 1998 2 19 REXA98032 1 19980125 A 3060 MS33205 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU RT PROP FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 108PX 340A012 RIGHT PROP DE-ICE WILL NOT COME ON WHEN SELECTED. REMOVED AND REPLACED PROP HEAT CONTROL CIRCUIT BREAKER. (M) 2 L 7 2 4T RT A52EU 1998021900972 19980219 00972 EU 1998 2 19 REXA98031 1 19980126 A 6120 PITCH TRIM SAAB SF340 SF340A 7850100 EU COCKPIT OUT OF POSITION A REXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 110PX 340A023 CONFIG LIGHT COMES ON WHEN POWER LEVERS ARE PUSHED UP. FOUND STANDBY PITCH TRIM OUT OF NORMAL RANGE CAUSING CONFIG LIGH T. MOVED TRIM TO NORMAL RANGE AND RESET TRIM. OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1998021900973 19980219 00973 EU 1998 2 19 REXA98030 1 19980126 A 2612 FIRE LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 326PX 340A054 RIGHT FIRE DETECTION FAIL CWP ILLUMINATED IN FLIGHT. CLEANED CONNECTOR ENDS ON RIGHT ENGINE FIRE DETECTION SENSOR LOOP. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900974 19980219 00974 EU 1998 2 19 REXA98029 1 19980126 A 2910 L38705A SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG FAILED A REXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 922MA 340A077 AFTER TAKEOFF AIRCRAFT LOST HYDRAULIC PRESSURE, DECLARED EMERGENCY. REMOVED AND REPLACED MAIN GEAR DOWN LOCK SWIVEL, GE AR SWING CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900975 19980219 00975 1998 2 19 REXA98028 4 19980123 A 3418 SIG SUMM UNIT BAG JETSTM JETSTM3101 1500215 EU RIGHT TRIPPED A REXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 318PX 689 ON APPROACH, RECEIVED A STALL WARNING HORN AND STICK SHAKER AT 135 KNS, FLAPS AT 35 DEGREES. RE-SET RIGHT SIGNAL SUMMIN G UNIT. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998021900976 19980219 00976 1998 2 19 REXA98027 4 19980124 A 3418 COMP RESISTOR BAG JETSTM JETSTM3101 1500215 EU LEFT OUT OF ADJUST A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 316PX 687 RIGHT STALL LGT FOLLOWED BY SHAKER, LEFT ENGINE WOULD NOT MAKE TORQ. NO FAULTS WERE FOUND ON STALL LGT AND ADJUSTED THE LEFT COMP RESISTOR. GROUND RUN CHECKS GOOD. (M) 2 L 7 2 4T RT A21EU 1998021900977 19980219 00977 1998 2 19 REXA98026 4 19980111 A 3414 A3615710160 AIRSPEED IND BAG JETSTM JETSTM3101 1500215 EU LT COCKPIT FAILED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 330PX 2238 698 DURING CLIMB-OUT, THE CAPTAIN AIRSPEED INDICATOR CLIMBED TO 245 KNS AND THEN SHOWED 80 KNS ONCE ON THE GROUND. REMOVED AND REPLACED CAPTAIN AIRSPEED INDICATOR. (M) 2 L 7 2 4T RT A21EU 1998021900978 19980219 00978 1998 2 19 REXA98024 4 19980122 A 3413 066500012804 VSI SAAB SF340 SF340A 7850100 EU RT COCKPIT FAILED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 401BH 4525 340A057 RIGHT VSI INOP ON TAXI. REMOVED AND REPLACED FO'S VSI, STATIC LEAK TEST, CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900979 19980219 00979 EU 1998 2 19 REXA98023 1 19980121 A 3610 SWITCH SAAB SF340 SF340A 7850100 EU LT BLEED AIR DIRTY A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 935MA 340A073 LEFT BLEED FAULT LIGHT CAME ON AND STAYED ON. CLEANED LOW AND HI BLEED VALVE, TEMP SWITCH, AND PRESS SWITCH CONNECTORS ON LEFT ENGINE. (M) 2 L 7 2 4T RT A52EU 1998021900980 19980219 00980 EU 1998 2 19 REXA98022 1 19980120 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E COMPT FAILED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 370PX A3071 340B300 AVIONICS SMOKE ILLUMINATED ON CWP DURING CLIMB-OUT, RETURNED TO PFN. REMOVED AND REPLAED AVIONICS SMOKE DETECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900981 19980219 00981 1998 2 19 REXA98021 4 19980120 A 3425 6226342022 EFIS TUBE SAAB SF340 SF340A 7850100 EU RIGHT INOPERATIVE A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 407BH 1212 340A078 RIGHT EFIS INOP. REMOVED AND REPLACED UPPER EFIS TUBE F/O'S SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998021900982 19980219 00982 1998 2 19 REXA98020 4 19980119 A 2312 PBD50825 CONNECTOR SAAB SF340 SF340A 7850100 EU NR 2 COMM ANT FAILED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 935MA 340A073 NR 2 COMM INOP. REMOVED AND REPLACED CO-AX CABLE CONNECTOR AT NR 2 COM ANTENNA. (M) 2 L 7 2 4T RT A52EU 1998021900983 19980219 00983 NM 1998 2 19 P2EA98021 1 19980130 A 5320 FRAME BOEING 737 737222 1384473 NM CARGO DOORWAY DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, AFT CARGO DOOR TEMPORARY REPAIR. INSTALLED PERMANENT REPAIR IAW SRM 51-40-3 AND EO 973752A043. ( M) 2 L 7 2 4F A16WE 1998021900984 19980219 00984 NM 1998 2 19 P2EA98020 1 19980130 A 5754 RIB BOEING 737 737222 1384473 NM NR 1 LE FLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, LEFT WING NR 1 SLAT AREA, INBOARD RAIL, OUTBOARD RIB CRACKED. REPAIRED IAW BOEING DRAWING 65C2565 8. (M) 2 L 7 2 4F A16WE 1998021900985 19980219 00985 NM 1998 2 19 P2EA98019 1 19980130 A 2782 FITTING BOEING 737 737222 1384473 NM NR 3 LE FLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, LEFT WING NR 3 SLAT ACTUATOR ATTACH FITTING CRACKED. REPLACED LEFT WING NR 3 SLAT ACTUATOR SUPPOR T FITTING IAW SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1998021900986 19980219 00986 NM 1998 2 19 P2EA98018 1 19980128 A 5330 SKIN BOEING 737 737222 1384473 NM BS 616/639 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, UPPER EXTERIOR FUSELAGE SKIN HAS 4 CRACKS AT VHF ANTENNA CUT OUT, BETWEEN BS 616 AND BS 639 AT STR INGER NR 1 AND NR 2 RIGHT. REPAIRED FUSELAGE SKIN SECTION IAW EO C00-3-53-039-98. (M) 2 L 7 2 4F A16WE 1998021900987 19980219 00987 NM 1998 2 19 P2EA98017 1 19980128 A 5330 SKIN BOEING 737 737222 1384473 NM BS 223/255 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, TEMPORARY SKIN REPAIR INSTALLED BETWEEN BS 223 AND BS 255 BETWEEN WL 204 AND WL 234R. INSTALLED P ERMANENT REPAIR PER BOEING S/B 737-53-1111 REV 1. (M) 2 L 7 2 4F A16WE 1998021900988 19980219 00988 NM 1998 2 19 P2EA98016 1 19980128 A 5330 SKIN BOEING 737 737222 1384473 NM BS 727/780 CORROSION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, LOWER EXTERIOR FUSELAGE SKIN BULGED (CORRODED) FROM BS 727 TO 780, STRINGER 20L. REPAIRED FUSELAG E FRAME SECTION IAW SRM 53-30-3 FIG 15. (M) 2 L 7 2 4F A16WE 1998021900989 19980219 00989 NM 1998 2 19 P2EA98015 1 19980127 A 5311 FRAME BOEING 737 737222 1384473 NM BS 312 CORROSION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, FUSELAGE FRAME CORRODED AT BS 312 BETWEEN STRINGERS 26R AND 27R (ELECTRONIC EQUIPMENT COMPARTMENT) . REPAIRED FUSELAGE FRAME SECTION IAW SRM 53-10-4 FIG 10. (M) 2 L 7 2 4F A16WE 1998021900990 19980219 00990 NM 1998 2 19 P2EA98014 1 19980127 A 5330 SKIN BOEING 737 737222 1384473 NM BS 787/800 CORROSION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, LOWER EXTERIOR FUSELAGE SKIN BULGED (CORROSION) FROM BS 787 TO BS 800, STRINGER 23R AND 25R. REPA IRED FUSELAGE SKIN SECTION IAW SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900991 19980219 00991 NM 1998 2 19 P2EA98013 1 19980127 A 5330 SKIN BOEING 737 737222 1384473 NM BS 907 CORROSION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, UPPER EXTERIOR FUSELAGE SKIN BULGED (CORROSION) AT BS 907, BETWEEN STRINGER 3L AND 3R. REPAIRED F USELAGE SKIN SECTION IAW SRM 53-30-3 FIG 28. (M) 2 L 7 2 4F A16WE 1998021900992 19980219 00992 NM 1998 2 19 P2EA98012 1 19980127 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 767 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, STRINGER 20R CORRODED AT BS 767. REPAIRED STRINGER IAW 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900993 19980219 00993 NM 1998 2 19 P2EA98011 1 19980126 A 5330 SKIN BOEING 737 737222 1384473 NM BS 907 CORROSION A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, LOWER EXTERIOR FUSELAGE SKIN BULGED (CORROSION) AT BS 907, BETWEEN STRINGER 18R AND 23R. REPAIRED FUSELAGE SKIN BUTT JOINT IAW 53-30-3 FIG 28. (M) 2 L 7 2 4F A16WE 1998021900994 19980219 00994 NM 1998 2 19 P2EA98010 1 19980126 A 5311 FRAME BOEING 737 737222 1384473 NM BS 500 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURNG C-CHECK, FUSELAGE FRAME UPPER FLANGE CRACKED IN FORWARD CARGO COMPRTMENT AT BS 500A, AT STRINGER 20R AND 21R , CRACK SIZE 14 INCH BY 4 INCH. REPAIRED CRACK IAW SRM 53-10-4 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900995 19980219 00995 NM 1998 2 19 P2EA98009 1 19980126 A 5311 FRAME BOEING 737 737222 1384473 NM BS 420 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, FUSELAGE FRAME UPPER FLANGE CRACKED IN FORWARD CARGO COMPARTMENT AT BS 420, BETWEEN STRINGER 22L A ND 23L, CRACK SIZE 13.5 INCH BY 2.5 INCH. REPAIRED CRACK IAW SRM 53-10-4 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900996 19980219 00996 NM 1998 2 19 P2EA98008 1 19980126 A 5311 FRAME BOEING 737 737222 1384473 NM BS 460 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, FUSELAGE FRAME UPPER FLANGE CRACKED IN FORWARD CARGO COMPARTMENT AT BS 460, STRINGER 20L AND 21L, CRACK SIZE 10.25 INCH BY 4 INCH. REPAIRED CRACK IAW SRM 53-10-4 FIG 1. (M) 2 L 7 2 4F A16WE 1998021900997 19980219 00997 NM 1998 2 19 P2EA98007 1 19980126 A 5330 SKIN BOEING 737 737222 1384473 NM BS 318 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, DENT IN LOWER EXTERIOR FUSELAGE SKIN AT BS 318, STRINGER 22 RT, DENT SIZE LENGTH 8.5 INCH BY WIDTH 7.5 INCH. REPAIRED DENT IAW SRM 53-30-3 FIG 7. (M) 2 L 7 2 4F A16WE 1998021900998 19980219 00998 NM 1998 2 19 P2EA98006 1 19980126 A 5311 FRAME BOEING 737 737222 1384473 NM BS 460 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - FUSELAGE FRAME CRACKED, IN FORWARD CARGO COMPARTMENT AT BS 460, BETWEEN STRINGER 28L AND 27R, CRACK SIZE 11 INCH B Y 4 INCH. REPAIRED FUSELAGE FRAME CRACK, PER SRM 53-10-4 FIG 10. (M) 2 L 7 2 4F A16WE 1998021900999 19980219 00999 NM 1998 2 19 VNAA9802014 1 19980212 A 3250 POTENIOMETER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING OUT OF ADJUST A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 460PS 3061 WHEN THE CONDITION LEVERS WERE BROUGHT FORWARD FOR TAKEOFF, A NOSE STEERING FAIL WARNING OCCURRED. THE TAKEOFF WAS ABOR TED AND THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE IN AZO INSPECTED AND APPROVED THE AIRCRAFT FOR A FERR Y FLIGHT INTO CAK. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY INCIDENT. MAINTENANCE IN CAK INSPECTED AND ADJUSTED THE NO SE STEERING POTENTIOMETERS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-51-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998022500008 19980225 00008 NM 1998 2 25 VJ9800009 1 19980209 A 3350 SWITCH BOEING 737 737214 138446R NM L1 DOOR FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 11 460AT 20158 EMERGENCY EXIT LIGHT WILL NOT ARM, ON FLIGHT CREW PRE FLIGHT. REMOVED AND REPLACED MICRO SWITCH IAW MM 33-51-121; OPS CHECKED GOOD. 2 L 7 2 4F A16WE 1998022500009 19980225 00009 NM 1998 2 25 AWXA9800046 1 19980115 A 5315 FLOORBEAM BOEING 737 73733A 1384673 NM BS 344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 168AW 23629 DURING SCHEDULED C-12 INSPECTION, FOUND CORROSION AROUND NUT-PLATE HOLE STA 344, WL 208, LBL 10 ON FLOORBEAM. REMOVED D AMAGED PORTION OF TOP CHORD FROM LBL 8.5 TO LBL 11, WL 208, STA 344 AND REPAIRED BEAM PER SRM 53-10-51, PAGES 224 - 228. 2 L 7 2 4F RT A16WE 1998022500010 19980225 00010 SO 1998 2 25 SWIA971083 1 19980209 A 3097 WIRE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT INTAKE BROKEN A SWIA O OTHER O OTHER CL CLIMB 1 NM 07 237SW 120314 INFLIGHT LEFT INTAKE DE-ICE INOP AND MULTIPLE WING AND STAB DE-ICE LIGHTS INOP CAME ON. RECYCLED AND CHANGED TIMERS BUT ALL STILL INOP. RETURNED TO LAX. CLEANED ALL EJECTORS AND CHECKED FOR LEAKS. ALL FOUND NORMAL. REPLACED RIGHT ENGIN E EJECTOR DUE TO BROKEN WIRE. PERFORMED GROUND RUN FOR 20 MINUTES AND ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998022500011 19980225 00011 1998 2 25 HEEA0013011 4 19980210 A 3160 913200 TREND MONITORING BOLKMS 117 BK117B1 5626012 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7059J 7151 DISPLAY "MEMORY STATUS BAD 12345ABC" WHEN TURNED ON. 1 G 7 2 3U H13EU 1998022500012 19980225 00012 WP 1998 2 25 CKSA98012 1 19980212 A 2612 FIRE LOOP DOUG DC8 DC855 3021927 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE CHAFFING A CKSA K NONE N FALSE WARNING CR CRUISE 1 GL 23 807CK 45767 644454 NR 2 ENG FIRE LIGHT ILLUMINATES INTERMITTENTLY INFLIGHT ACCOMPANIED BY BELL, SYSTEM CHECKS OK. FOUND FIRE LOOP CHAFING. REPOSITIONED RUBBER GROMMET, CLEANED CANNON PLUG AND LEAK CHECKED BLEED SYSTEM. OPS CHECKS GOOD IAW DC8 MM 26-2-0. 2 L 7 4 4F 4 F 4A25 1E8 1998022600001 19980226 00001 GL 1998 2 26 HEEA0013035 2 19980212 A 7250 23031494 SEAL 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 8 LAB SEAL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 533 CAT90616 760230 CAE890508S ENGINE REMOVED DUE TO FOD AND TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED: MEASURED .001 BELOW SPECS (1.2 520 - 1.2515) ON SEAL O.D. INSTALLED A NEW SEAL. 1 G 7 2 3U 3 U H1NE E1GL 1998022600002 19980226 00002 SW 1998 2 26 HEEA0012964 1 19980210 A 6330 206033506101 RESTRAINT BELL 206 206L3 1182108 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 129MR 51129 BEARINGS WORN BEYOND LIMITS. 1 G 7 1 3U H2SW 1998022600003 19980226 00003 EU 1998 2 26 HEEA0013031 1 19980211 A 5610 04011340990 WINDOW SNIAS 350 AS350B2 8680813 EU RT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 2820 RT WINDOW DEFECTIVESCRAPPED AT PHI. 1 G 7 1 3U H9EU 1998022600004 19980226 00004 SW 1998 2 26 HEEA0012953 1 19980210 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Q 45187 ACTUATOR SHAFT LOOSE IN MOTOR HOUSING. 1 G 7 1 3U H2SW 1998022600005 19980226 00005 NE 1998 2 26 HEEA0012938 1 19980210 A 7930 7645001078101 INDICATOR SKRSKY S76 S76A 8143006 NE ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 ENG OIL INDICATOR INDICATES LOW MID SCALE AND MOISTURE IN LENS. 1 G 7 2 3U H1NE 1998022600006 19980226 00006 SW 1998 2 26 HEEA0012940 1 19980210 A 7722 12444412 INDICATOR BELL 206 206B3 1181506 SW ENG TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2756P 2655 ENG TOT READS 10 LOW AT 800 DEGREES. 1 G 7 1 3U H2SW 1998022600007 19980226 00007 1998 2 26 HEEA0012924 4 19980210 A 3425 214075244001 RATE GYRO BELL 412 412 1182202 SW HSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 RATE GYRO FAILED. WON'T PULL OFF FLAG ON HSI. 1 G 7 2 4U H4SW 1998022600008 19980226 00008 SW 1998 2 26 HEEA0012920 1 19980210 A 6240 206070265101 INDICATOR BELL 206 206L1 1182107 SW M/R TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5012V 45200 DUAL TACH HAS A 4% SPLIT NEEDLE INDICATION ROTOR HIGH. 1 G 7 1 3U H2SW 1998022600009 19980226 00009 EU 1998 2 26 HEEA0012917 1 19980210 A 7722 10590947 INDICATOR BOLKMS 105 BO105S 5626006 EU ENG TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X S808 TOT INDICATOR STICKING AND UNABLE TO ADJUST. 1 G 7 2 3U H3EU 1998022600010 19980226 00010 SW 1998 2 26 HEEA0012908 1 19980210 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2250U 45754 ACTUATOR INOPERATIVE. 1 G 7 1 3U H2SW 1998022600011 19980226 00011 SW 1998 2 26 HEEA0012907 1 19980210 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251A 45755 ACTUATOR DOES NOT MOVE. 1 G 7 1 3U H2SW 1998022600012 19980226 00012 SW 1998 2 26 HEEA0012906 1 19980210 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 WILL NOT EXTEND OR RETRACT. SENT TO GLOBE MOTORS, INC. FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 1998022600013 19980226 00013 SW 1998 2 26 HEEA0012975 1 19980210 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW HORIZ STAB CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2759U 45272 STAB ASSY HAS PAINT PEELING OFF AND CORROSION DAMAGE. 1 G 7 1 3U H2SW 1998022600014 19980226 00014 SW 1998 2 26 HEEA0012879 1 19980209 A 6240 222375077119 TRANSMITTER BELL 407 407 SW ROTOR TORQUE FAILED E HEEA A UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 SW 03 406PH 48 53198 WHILE HOVERING AT 68-71 PERCENT TORQUE, TORQUE GAUGE STARTED INCREASING UNTIL REACHING FULL SCALE AND THEN WENT TO ZERO PERCENT INDICATION. 1 G 7 1 3U O H2SW 1998022600015 19980226 00015 SW 1998 2 26 HEEA0012963 1 19980210 A 6330 206033518005 STOP ASSY BELL 206 206L3 1182108 SW M/R XMSN DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4180F 51469 STOP ASSY RUBBER IS DETERIORATED. 1 G 7 1 3U H2SW 1998022600016 19980226 00016 GL 1998 2 26 HEEA0013034 2 19980212 A 7230 6895803 SCROLL 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG COMP WARPED E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 10761 CAC70578 45381 CAE860697 ENGINE REMOVED DUE TO LOW POWER. SCROLL REMOVED DUE TO EXCESSIVE AIR LEAKS ON TEST CELL BETWEEN SCROLL AND VANE AS MARK ED; WARPED FLANGE. 1 G 7 1 3U 3 U H2SW E1GL 1998022600017 19980226 00017 NE 1998 2 26 HEEA0013033 2 19980212 A 7310 430137601 FUEL NOZZLE BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101750B1 41560 NE FLOW DIVIDER LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 132AE 1541 7238 LE45556AEF FUEL LEAK DEVELOPED AT BRAZE FOR SOLID TUBING AT FLOW DIVIDER. 1 G 7 2 3U 3 U NC H13EU E5NE10 1998022600018 19980226 00018 GL 1998 2 26 HEEA0013024 2 19980211 A 7412 103815504 EXCITER SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL ENG IGN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 EXCITER WILL NOT FIRE IGNITION PLUGS. 1 G 7 2 3U 3 U H1NE E1GL 1998022600019 19980226 00019 GL 1998 2 26 HEEA0012991 2 19980210 A 7250 23055438 NOZZLE 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 889 CAT90184 760275 CAE890181S ENGINE REMOVED DUE TO TURBINE NR1 AND NR2 WHEEL CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: EXCESSIVE RUNOUT ON NR 2 NOZZLE 1ST STAGE TIP PATH .007 AND NR2 TIP PATH .005. INSTALLED A NEW NR2 NOZZLE. 1 G 7 2 3U 3 U H1NE E1GL 1998022600020 19980226 00020 GL 1998 2 26 HEEA0012990 2 19980210 A 7250 23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724MB 914 CAT37763 S756 CAE835286 ENGINE REMOVED DUE TO OIL STARVATION AND METAL IN OIL. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEA BLE LIMITS ON NR1 NOZZLE TRAILING EDGE VANES. INSTALLED A DALLAS AIRMOTIVE OVERHAULED NR1 NOZZLE. 1 G 7 2 3U 3 U H3EU E4CE 1998022600021 19980226 00021 GL 1998 2 26 HEEA0012989 2 19980210 A 7250 23008064 NOZZLE 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL 1ST STAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 889 CAT90184 760275 CAE890181S ENGINE REMOVED DUE TO TURBINE NR1 AND NR2 WHEEL CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICE ABLE LIMITS ON NR1 NOZZLE TRAILING EDGE VANES. INSTALLED A DALLAS AIRMOTIVE OVERHAULED NR1 NOZZLE. 1 G 7 2 3U 3 U H1NE E1GL 1998022600024 19980226 00024 GL 1998 2 26 HEEA0012986 2 19980210 A 7250 23060450 NOZZLE 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2145C 779 CAT34806 3456 TURBINE REMOVED DUE TO CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR 1 NOZZLE VANES TRAILING EDGE. INSTALLED A SERVICEABLE NR 1 NOZZLE. 1 G 7 1 3U 3 U H2SW E4CE 1998022600026 19980226 00026 NE 1998 2 26 HEEA0012970 2 19980210 A 7200 0292005220 ENGINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE POWER SECT MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 3384 2873 RECURRING METAL ON UPPER ELECTRICAL PLUG AND ON ELECTRICAL PLUG AT ENGINE OIL TANK. CHROME FLAKES IN OIL FILTER. 1 G 7 1 3U 3 U H9EU E19EU 1998022600027 19980226 00027 NE 1998 2 26 HEEA0012966 2 19980210 A 7210 3020184 ADAPTER BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA ADAPTER REMOVED WITH COMBINING GEARBOX. 1 G 7 2 4U 4 U H4SW E22EA 1998022600028 19980226 00028 NE 1998 2 26 HEEA0012965 2 19980210 A 7210 3024780 COMBINING GRBOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 11282 COMBINING GEAR BOX TRANSFERRING OIL. 1 G 7 2 4U 4 U H4SW E22EA 1998022600029 19980226 00029 SW 1998 2 26 HEEA0012883 1 19980209 A 6240 222375077119 TORQUE TRANSMITT BELL 407 407 SW ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 49 53198 TORQUE SLOWLY WENT UP, THEN FELL TO ZERO. 1 G 7 1 3U O H2SW 1998022600030 19980226 00030 SW 1998 2 26 HEEA0013027 1 19980211 A 6320 222375077113 TRANSMITTER BELL 407 407 SW TRANSMISSION INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 OIL TRANSMITTER INOPERATIVE. 1 G 7 1 3U O H2SW 1998022600031 19980226 00031 EU 1998 2 26 HEEA0013030 1 19980211 A 6520 350A33105803 LEVER SNIAS 350 AS350B2 8680813 EU T/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 284 2820 T/R GR BOX LEVER CONTROL BUSHINGS WORN. 1 G 7 1 3U H9EU 1998022600032 19980226 00032 EU 1998 2 26 HEEA0013018 1 19980210 A 5321 10522361 FLOOR COVER BOLKMS 105 BO105S 5626006 EU FUSELAGE FLOOR MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 3520T S539 FORWARD EDGE OF PANEL DOES NOT HAVE REINFORCEMENT STRIP BONDED ON FOR INSTALLATION OF PANEL TO MAIN FLOOR PANEL. 1 G 7 2 3U H3EU 1998022600033 19980226 00033 EU 1998 2 26 HEEA0012951 1 19980210 A 7714 DL41239 INDICATOR BOLKMS 105 BO105S 5626006 EU SINGLE RPM STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911EB S812 SINGLE RPM INDICATOR STICKING. 1 G 7 2 3U H3EU 1998022600034 19980226 00034 EU 1998 2 26 HEEA0012925 1 19980210 A 2435 GENERATOR BOLKMS 105 BO105S 5626006 EU NR 2 FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K S859 NR 2 GENERATOR INOPERATIVE. PUTS OUT VOLTAGE BUT NO AMPERAGE. 1 G 7 2 3U H3EU 1998022600035 19980226 00035 EU 1998 2 26 HEEA0012895 1 19980209 A 6220 117775P BALLJOINT SNIAS 350 AS350B2 8680813 EU STARFLEX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4034Q 446 2918 STARFLEX BALL JOINT WORN. 1 G 7 1 3U H9EU 1998022600036 19980226 00036 EU 1998 2 26 HEEA0012894 1 19980209 A 6220 350A31190703 STARFLEX SNIAS 350 AS350B2 8680813 EU M/R SPLINTERED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1522 2820 STARFLEX IS SPLINTERED. 1 G 7 1 3U H9EU 1998022600037 19980226 00037 EU 1998 2 26 HEEA0012891 1 19980209 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R P/C LINK WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 222 3004 BEARING WORN ON T/R P/C LINK. 1 G 7 1 3U H9EU 1998022600038 19980226 00038 SW 1998 2 26 HEEA0013032 1 19980212 A 6410 212010750105 BLADE BELL 212 212 1181420 SW T/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INSUFFICIENT SUPPORTING DOCUMENT. BLADE DEFECTIVE 1 G 7 1 4U H4SW 1998022600039 19980226 00039 SW 1998 2 26 HEEA0013029 1 19980211 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DISC CRACKED. 1 G 7 1 3U O H2SW 1998022600040 19980226 00040 SW 1998 2 26 HEEA0012949 1 19980210 A 7722 206375007103 INDICATOR BELL 206 206L3 1182108 SW ENG TOT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3108E 51498 TOT INDICATOR STICKS AT 540 DEGREES. 1 G 7 1 3U H2SW 1998022600041 19980226 00041 SW 1998 2 26 HEEA0013028 1 19980211 A 6322 406040339105 BEARING 406040320101 BELL 407 407 SW T/R DRIVE ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1167G 472 AFS747 53067 ROUGH BEARING. SERIAL NUMBERS REMOVED E96-0002 AND K96-2152. 1 G 7 1 3U O H2SW 1998022600042 19980226 00042 SW 1998 2 26 HEEA0012976 1 19980210 A 5510 206023119151 STABILIZER ASSY BELL 206 206L3 1182108 SW HORIZ STAB CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206LS 51070 STAB ASSY CORROSION. SEPARATED IN CORNER. 1 G 7 1 3U H2SW 1998022600043 19980226 00043 SW 1998 2 26 HEEA0013025 1 19980211 A 6300 406010417101 BEARING BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 WORN SPHERICAL BEARING. 1 G 7 1 3U O H2SW 1998022600044 19980226 00044 NE 1998 2 26 HEEA0013023 2 19980211 A 7412 106149501 IGNITER BOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENG IGN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 AIRCRAFT DIFFICULT TO START. IGNITER BOX FAILED 1 G 7 2 4U 4 U H4SW E22EA 1998022600045 19980226 00045 SW 1998 2 26 HEEA0012999 1 19980210 A 2140 212070444001 SENSOR BELL 412 412 1182202 SW CABIN HEAT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 DRIVE SHAFT PUSHED INTO HOUSING. 1 G 7 2 4U H4SW 1998022600046 19980226 00046 SW 1998 2 26 HEEA0012979 1 19980210 A 2140 205072277009 VALVE BELL 412 412 1182202 SW HEATER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 HEATER INOPERATIVE. WILL NOT BLOW HOT AIR. MIXING VALVE FAILED 1 G 7 2 4U H4SW 1998022600047 19980226 00047 SW 1998 2 26 HEEA0012982 1 19980210 A 6220 407010150103 FRAHM ASSY BELL 407 407 SW M/R DEFECTIVE E HEEA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 03 417PH 53038 M/R VIBRATION. 1 G 7 1 3U O H2SW 1998022600048 19980226 00048 GL 1998 2 26 HEEA0013022 2 19980211 A 7412 106149501 IGNITER BOX BELL 206 206B3 1181506 SW ALLSN 250C 250C20 03013 GL ENG IGN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2285B 3642 IGNITER BOX INTERMITTENT. 1 G 7 1 3U 3 U H2SW E4CE 1998022600049 19980226 00049 SW 1998 2 26 HEEA0013019 1 19980210 A 6720 PHI206L3957 SHAFT BELL 206 206L3 1182108 SW PITCH CHANGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31801 51074 CRACKS ON PITCH CHANGE SHAFT. REPLACED WITH SERVICEABLE PITCH CHANGE MECHANISM. 1 G 7 1 3U H2SW 1998022600050 19980226 00050 SW 1998 2 26 HEEA0013017 1 19980210 A 6240 206075681105 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31801 51074 DUAL TACH INDICATOR N2 NEEDLE STICKS. 1 G 7 1 3U H2SW 1998022600051 19980226 00051 SW 1998 2 26 HEEA0013013 1 19980210 A 6720 7001484 YAW CONTROL BELL 412 412 1182202 SW T/R CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 YAW CONTROL INOPERATIVE. 1 G 7 2 4U H4SW 1998022600052 19980226 00052 SW 1998 2 26 HEEA0013000 1 19980210 A 6320 205040231009 RING GEAR BELL 412 412 1182202 SW M/R XMSN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 RING GEAR CORROSION ON UPPER AND LOWER FLANGES. 1 G 7 2 4U H4SW 1998022600053 19980226 00053 SW 1998 2 26 HEEA0012995 1 19980210 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 18 33022 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998022600075 19980226 00075 NM 1998 2 26 VJ9800011 1 19980130 A 5280 ANGLE BOEING 737 7372L9 1384497 NM RT MLG DOOR BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 464AT 21278 RT MAIN LANDING GEAR ANGLE BROKEN AT AFT EYE BOLT HINGE POINT FOR OUTER DOOR. REPLACED ANGLE IAW SRM 57-15-2 AND 32-13- 21. 2 L 7 2 4F RT A16WE 1998022600076 19980226 00076 NM 1998 2 26 VJ9800012 1 19980131 A 5320 ANGLE BOEING 737 7372L9 1384497 NM BS 777-857 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 464AT 21278 AFT BAGGAGE COMPARTMENT FS 857 TO 777 FLOOR SUPPORT ALONG STR 26L CORROSION OUT OF LIMITS. REMOVED DAMAGED SUPPORT SECT ION AND REPLACED WITH A NEW SECTION IAW SRM 53-10-2. 2 L 7 2 4F RT A16WE 1998022600077 19980226 00077 WP 1998 2 26 VJ9800013 1 19980128 A 3350 41B004A0073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 919VV 47260 OVERHEAD EMERGENCY CEILING LIGHTS AT ROW 12 INOPERATIVE. REPLACED NICAD BATTERIES, OPS CHECKED GOOD IAW MM 33-50. 2 L 7 2 4F A6WE 1998022600078 19980226 00078 NM 1998 2 26 MALA975982 1 19980215 A 3350 3352P42 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 861MA 362 DURING INSPECTION, TWO RED EMERGENCY FLOOR TRACK LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACK, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998022600079 19980226 00079 EU 1998 2 26 MALA975983 1 19980213 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING INSPECTION, OVERHEAD EMERGENCY LIGHT 2A INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600080 19980226 00080 EU 1998 2 26 MALA975984 1 19980215 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 99XJ 099 DURING INSPECTION, OVERHEAD EMERGENCY LIGHTS INOP AT ROWS 1A, 2A, AND 3A. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600081 19980226 00081 NM 1998 2 26 MALA975985 1 19980215 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 828MA 333 DURING INSPECTION, ONE FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998022600082 19980226 00082 NM 1998 2 26 MALA975986 1 19980214 A 3350 OL307115 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 833MA 343 DURING INSPECTION, EMERGENCY EXIT SIGN HAS BULBS INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998022600083 19980226 00083 EU 1998 2 26 MALA975987 1 19980217 A 2613 CONNECTOR SAAB SF340 340B 7860101 EU RT TAILPIPE CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 418XJ 418 AFTER TAKEOFF, THE RIGHT TAILPIPE HOT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE CLEANED MOISTURE FROM R IGHT TAILPIPE EXHAUST SENSORS CANNON PLUG. GROUND RAN AIRCRAFT FOR 15 MINUTES, OPS CHECK OF FIRE DETECTION SYSTEM GOOD. 2 L 7 2 4T RT A52EU 1998022600084 19980226 00084 EU 1998 2 26 MALA975988 1 19980216 A 3020 CONNECTOR SAAB SF340 340B 7860101 EU LT INTAKE HEAT CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 592MA 340B199 DURING CLIMBOUT, THE LEFT ENGINE INTAKE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE CLEANED ALL CANNON PL UGS (31HE, 13HE, 15HE, 8AZ) FOR LEFT INTAKE HEAT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600085 19980226 00085 EU 1998 2 26 MALA975989 1 19980217 A 2613 245284 THERMAL SWITCH SAAB SF340 340B 7860101 EU RT NACELLE FAILED A MALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 586MA 340B165 DURING TAKEOFF, THE RIGHT TAILPIPE HOT LIGHT ILLUMINATED. TAKEOFF ABORTED. MAINTENANCE REPLACED THREE THERMAL SWITCHES IN RIGHT NACELLE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600086 19980226 00086 EU 1998 2 26 MALA975990 1 19980217 A 2613 WARNING LIGHT SAAB SF340 340B 7860101 EU RT TAILPIPE ILLUMINATED A MALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 429XJ 429 ON TAKEOFF, THE RIGHT TAILPIPE HOT LIGHT ILLUMINATED. ABORTED TAKE OFF. MAINTENANCE FOUND MOISTURE IN TAILPIPE. RAN A IRCRAFT FOR 20 MINUTES AND DRIED AREA, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600087 19980226 00087 EU 1998 2 26 MALA975991 1 19980217 A 3350 SIGN SAAB SF340 SF340A 7850100 EU CABIN LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 41XJ 041 DURING INSPECTION, FOUND RIGHT FORWARD EMERGENCY EXIT SIGN UNSECURED. MAINTENANCE RESECURED PANEL, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998022600088 19980226 00088 EU 1998 2 26 MALA975992 1 19980216 A 3350 7239410802 LAMP SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 991XJ 091 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT ROW 6A INOP. MAINTENANCE RELAMPED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998022600089 19980226 00089 NM 1998 2 26 CALA9800268 1 19980216 A 3897 HARNESS BOEING 727 727224 1384076 NM FLUSH TIMER CHAFED A CALA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 SW 09 79746 22449 FIRE AND SMOKE OCCURRED IN THE LT AFT LAV WHILE EN ROUTE. A FIRE EXTINGUISHER WAS USED TO PUT OUT THE FIRE. THE ACFT L ANDED AT IAH WITHOUT FURTHER INCIDENT. THE FIRE WAS CONTAINED WITHIN THE LAV. PRELIMINARY FINDINGS REVEALED THE WIRING TO THE LAV FLUSH TIMER IN THE LT AFT LAV BURNED. THE DAMAGED WIRING WILL BE REPLACED. *S/D* THE WIRE HARNESS SUPPLYI NG POWER TO THE TOILET FLUSH TIMER WAS CHAFED AT BOTH CLAMP POSITIONS ON THE AFT WALL OF THE LAV. ONE WIRE SHORTED TO G ROUND AT THE LOWER CLAMP POSITION. 2 L 7 3 4F A3WE 1998022600090 19980226 00090 WP 1998 2 26 CALA9800269 1 19980217 A 3010 10200074 SENSOR DOUG DC9 DC932 3022066 WP RT DE-ICE SYST INOPERATIVE A CALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SW 09 19504 47638 THE RT AIR CONDITIONING SUPPLY TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF WITH SMOKE IN THE CABIN. THE AIRFOIL ICE PROTE CTION WAS ON. THE PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE RT ICE PROTECTION HIGH TEMP SENSOR WAS REMOVED AND REPLACED IAW MM 30-10-6. THE ENGINES WERE RUN WITH PACKS OPERATING AND NO DEFECTS WERE NOTED. 2 L 7 2 4F A6WE 1998022600091 19980226 00091 NM 1998 2 26 CALA9800270 1 19980217 A 5210 80330034 BOTTLE BOEING 757 757224 1384958 NM L 2 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18119 27561 INSPECTION FOUND THE L-2 DOOR ASSIST BOTTLE PRESSURE LOW. THE L-2 DOOR ASSIST BOTTLE WAS REMOVED AND REPLACED IAW MM 52 -11-30. 2 L 7 2 4F RT A2NM 1998022600092 19980226 00092 WP 1998 2 26 CALA9800271 1 19980217 A 5320 CUSP BEAM DOUG DC9 DC981 3022081 WP BS 229 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND CUSP BEAM CORRODED AT STA 229, LONGERON 18L. REPAIRED IAW ECRA 5310-03678. 2 L 7 2 4F A6WE 1998022600093 19980226 00093 WP 1998 2 26 CALA9800272 1 19980217 A 5320 CUSP BEAM DOUG DC9 DC981 3022081 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND CUSP BEAM CORRODED AT STA 200, LONGERON 18L. REPAIRED IAW ECRA 5310-03678. 2 L 7 2 4F A6WE 1998022600094 19980226 00094 WP 1998 2 26 CALA9800273 1 19980218 A 5530 SKIN DOUG DC9 DC981 3022081 WP DORSAL FIN OVERSIZE HOLES A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND OVERSIZED HOLES IN FUSELAGE SKIN AT OUTER DORSAL FIN ATTACH ANGLE ON LEFT AND RIGHT SIDES. REPAIRED IA W ECRA 5340-01312. 2 L 7 2 4F A6WE 1998022600095 19980226 00095 WP 1998 2 26 CALA9800274 1 19980219 A 5230 SKIN DOUG DC9 DC981 3022081 WP BAGGAGE DOOR CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR SKIN CHAFED IN SEVERAL PLACES BELOW LOCK HANDLE. A REPAIR WAS FABRICATE D AND INSTALLED IAW ECRA 5230-01397. 2 L 7 2 4F A6WE 1998022600096 19980226 00096 WP 1998 2 26 CALA9800275 1 19980219 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1380 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND THAT THE LEFT HEAT VALVE HAD GOUGED THE FRAME INNER CAP AT STA 1380. A REPAIR STRAP WAS INSTALLED IAW ECRA 5311-01042. 2 L 7 2 4F A6WE 1998022600097 19980226 00097 1998 2 26 9802799874 4 19980217 A 3417 ADC DOUG DC9 DC951 3022051 WP RT COCKPIT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 783NC 48108 DURING CLIMBOUT, THE FIRST OFFICER'S ALTIMETER OFF FLAG AND THE ALTITUDE ALERTER OFF FLAG CAME INTO VIEW. FLIGHT RETURN ED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AIR DATA COMPUTER AND ALTITUDE ALERTER INDICATOR, OPERA TIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998022600098 19980226 00098 NM 1998 2 26 9802806305 1 19980217 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 25R TO 30R, 51L TO 55L, AND AT DOOR 3L. RECO NNECTED WIRES, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998022600099 19980226 00099 NM 1998 2 26 9802816301 1 19980215 A 3350 LIGHTS BOEING 747 747451 1384940 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ZONES D THRU E. RECONNECTED LIGHT, OPERATIONAL CH ECK GOOD. 2 L 7 4 4F RT A20WE 1998022600100 19980226 00100 WP 1998 2 26 9802829997 1 19980218 A 2751 ST12BD TRANSMITTER DOUG DC9 DC931 3022065 WP RT TE FLAP FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8933E 32678 13490 47142 STALL WARNING INDICATION FAILURE LIGHT ILLUMINATED ACCOMPANIED BY STICK SHAKER ACTIVATION DURING CLIMBOUT. FLIGHT WAS R ETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT FLAP POSITION TRANSMITTER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600101 19980226 00101 1998 2 26 9802839957 4 19980218 A 3454 6223257006 NAV RECEIVER DOUG DC9 DC931 3022065 WP E/E COMPARTMENT FAILED A NWAA K NONE O OTHER DE DESCENT 1 GL 01 915RW 36811 1804 47139 NR 1 NAV SYSTEM FAILED ON DESCENT INTO MDW. FLIGHT WAS DIVERTED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC ED THE NR 1 NAV RECEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600102 19980226 00102 WP 1998 2 26 9802849965 1 19980217 A 3610 SLEEVE DOUG DC9 DC931 3022065 WP LT HEAT EXCHANGE BLOWN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 911RW 47149 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO JAX AND LANDED WITHOUT INCIDE NT. MAINTENANCE FOUND LEFT HEAT EXCHANGER SLEEVE BLOWN AND PERI SEALS MISSING. REPLACED SLEEVE AND SEALS, LEAK AND OPE RATIONAL CHECK WAS NORMAL. 2 L 7 2 4F A6WE 1998022600103 19980226 00103 WP 1998 2 26 9802859614 1 19980217 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 614NW 47128 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ALONG CATWALK INOPERATIVE. REPLACED POWER SUPPLY AT FS 1133, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600104 19980226 00104 WP 1998 2 26 9802869993 1 19980216 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600105 19980226 00105 WP 1998 2 26 UPS98825800 1 19980206 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 322.75 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-C, RT WING L/E SECTION BETWEEN PYLONS AT XFS 322.750, L/E SKIN ON TOP AT FRONT SPAR HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED IAW SRM ADDN DC8-05720-7767-A. 2 L 7 4 4F RT 4A25 1998022600106 19980226 00106 WP 1998 2 26 UPS98825801 1 19980207 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-C, FS 1130 LBL 44 TRACK IS CORRODED BEYOND ALLOWABLE LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACE MENT SECTION OF TRACK IAW SRM ADDN DC8-5320-8309-B. 2 L 7 4 4F RT 4A25 1998022600107 19980226 00107 WP 1998 2 26 UPS98825802 1 19980207 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 7095 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XILD 7095. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600108 19980226 00108 WP 1998 2 26 UPS98825803 1 19980210 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, RT WING L/E AT STA XFS 635.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600109 19980226 00109 WP 1998 2 26 UPS98825804 1 19980210 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, RT WING L/E AT STA XFS 628.750 THE L/E UPPER RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600110 19980226 00110 WP 1998 2 26 UPS98825805 1 19980210 A 5712 RIB DOUG DC8 DC871F 302199D WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 THE UPPER L/E RIB HAS A 2 INCH CRACK AT MID SPAN. REPAIRED IAW SRM 57 -2-0. 2 L 7 4 4F RT 4A25 1998022600111 19980226 00111 WP 1998 2 26 UPS98825806 1 19980209 A 5313 LONGERON DOUG DC8 DC871F 302199D WP WS 35-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LONGERON 30R FS 35 TO 55 HAS HEAVY CORROSION AND OUT OF LIMITS. REMOVED AND REPLACED LONGERON IAW SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1998022600112 19980226 00112 EU 1998 2 26 WWMA9800033 1 19980216 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 356SB 340B356 DURING PREFLIGHT, THE EMERGENCY LIGHT AT ROW 6/7 FAILED TO ILLUMINATE. MAINTENANCE RESEATED BATTERY PACK CANNON PLUG. 2 L 7 2 4T RT A52EU 1998022600113 19980226 00113 EU 1998 2 26 WWMA9800032 1 19980216 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU LT COCKPIT FAILED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 338SB 340B338 CREW REPORTED SMELL OF HOT METAL OR INSULATION BURNING IN THE COCKPIT. MAINTENANCE FOUND THE LEFT FRONT COCKPIT WINDSHI ELD HEATING ELEMENTS BURNED OUT. REPLACED WINDSHIELD. 2 L 7 2 4T RT A52EU 1998022600114 19980226 00114 EU 1998 2 26 WWMA9800031 1 19980215 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU E/E COMPT DEFECTIVE A WWMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 15 243AE 340B243 AVIONICS SMOKE LIGHT ILLUMINATED DURING THE TAKEOFF ROLL, ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACE D THE AVIONICS SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998022600115 19980226 00115 NM 1998 2 26 QXEA9800069 1 19980214 A 2910 AEB215101 HYD LINE DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYST CRACKED A QXEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 09 813PH 21992 8458 32 EN ROUTE, NR 2 HYDRAULIC QUANTITY AND PRESSURE DROPPED TO ZERO WITH ASSOCIATED CAUTION LIGHTS. NR 1 HYDRAULIC QUANTITY DROPPED TO .5 QUARTS (PRESSURE ON NR 1 SYSTEM WAS NORMAL). PERFORMED EMERGENCY GEAR EXTENSION. LANDED WITHOUT INDICENT . MAINTENANCE REPLACED THE EXTRUDED AND LEAKING PRESSURE MANIFOLD O-RING. REPLACED CRACKED/LEAKING HARD LINE FROM PRES SURE MANIFOLD TO ENGINE SOFT LINE. ALSO, REPLACED HYDRAULIC PUMP AND PRESSURE MANIFOLD. PERFORMED LEAK CHECK, NO LEAKS NOTED. 2 H 7 2 4T RT A13NM 1998022600116 19980226 00116 WP 1998 2 26 98FDEA00117 1 19980218 A 2424 976J86310 GCU DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 316FE 48314 AFTER T/O, NR 2 GEN OFF LIGHT ILLUMINATED FOLLOWED WITH FLAP DISAGREE FLG IN VIEW AND C/B POPS. ALSO, CAN'T PRESS A/C O N LANDING APPROX 1000 FT, NR 2 ISOL, LIGHT ILLUMINATED RED TAB. REMOVED AND REPLACED NR 2 GCU AND BCU PER M/M 24-21-01. GND OPS PER JRH 8-2. RAN ALL THREE ENGS PER JRH 5A. 2 L 7 3 4F RT A22WE 1998022600117 19980226 00117 WP 1998 2 26 98FDEA00118 1 19980218 A 2130 PRESSURIZATION DOUG DC10 DC1030F 3023504 WP CABIN MALFUNCTIONED A FDEA A UNSCHED LANDING L NO TEST CL CLIMB 1 SO 25 301FE 46800 DURING CLIMBOUT, CABIN ALT BEGAN CLIMB AT SAME RATE AS A/C. PROBLEM START AT 5000 MSL: AUTO PRESS MODE WAS BEING USED. CABIN ALT RAPID REACH 5000 AND CONT TO CLIMB WITH A/C. USE OF SEMIAUTO STBY AND MANUAL MODES HAD NO EFFECT. CREW LEV EL OFF AT 10000 MSL CAB LVLD OFF 10000. RETURN TO IAD. INSP OUTFLOW VALVE. INSP ALL DOOR SEALS FOR DAMAGE, NO DEF FOU ND. RAN ENG PER JRH AND A/C ABLE TO PRESS MANUAL. DEF AUTO AND SEMIAUTO CABIN ALT CNTRL SYS PER MEL. MX BITE CHECK SY S ON GND CHECK NORMAL. NEXT FLT CREW COMMENTED THAT FLT CHECK WAS GOOD. MX CLEARED PER CREW COMMENT AND GND CHECK NORM AL. 2 L 7 3 4F RT A22WE 1998022600118 19980226 00118 NM 1998 2 26 98FDEA00119 1 19980219 A 2612 FIRE LOOP BOEING 727 727233 138408A NM NR 3 ENGINE MALFUNCTION A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 220FE 20934 NR 3 FIRE LIGHT ILLUMINATED WITH BELL AT FL 290. AFTER SWITCHING ESSENTIAL POWER, LIGHT AND BELL WENT OUT NEVER TO COME ON AGAIN. NEVER ANY INDICATION OF FIRE VISUALLY INSPECTED NR 3 ENGINE AND FIRE LOOP. LOOKED GOOD, OPS CHECKED GOOD. 2 L 7 3 4F RT A3WE 1998022600119 19980226 00119 EU 1998 2 26 98FDEA00120 1 19980218 A 2612 CG7P0 SMOKE DETECTOR AIRBUS 310 A310222 3930315 EU CARGO COMPT DEFECTIVE A FDEA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 25 418FE 343 APPROACHING LEVEL OFF AT FL 370, FWD CARGO COMPT SMOKE LIGHT AND ASSOC ECAM CAUTIONS ACTIVATED. NR 1 BOTTLE WAS DISCHAR GED AND NR 2 BOTTLE WAS ACTIVATED ON APPROACH. LIGHT WENT OUT AFTER DISCHARGE. REMOVED AND REPLACED SMOKE DET A AND B, OPS CHK NORMAL. INSPECTION OF FWD CARGO COMPT SHOWED NO EVIDENCE OF FIRE. 2 L 7 2 4F RT A35EU 1998022600120 19980226 00120 NM 1998 2 26 DL72K980394 1 19980216 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 471DA 20748 EMERGENCY EXIT SIGN AT R2 FLASHES THEN GOES OUT WHEN TESTED. REPLACED BATTERY PACK, CKS NML. 2 L 7 3 4F A3WE 1998022600121 19980226 00121 WP 1998 2 26 DLL10980396 1 19980213 A 5720 1506811103 STIFFENER LKHEED 1011 10113851 5265010 WP FRONT SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 725DA 193C1162 THE LBL 30 STIFFENER ON THE FRONT SPAR OF THE CENTER WING WAS FOUND WITH A .5 INCH CRACK EMANATING FROM THE SECOND LIGHT ENING HOLE FROM THE TOP. THE TOP SECTION OF STIFFENER WAS TRIMMED OFF AND A NEW SECTION SPLICED IN PER ER/A 363992-14, REV A. 2 L 7 3 4F A23WE 1998022600122 19980226 00122 NM 1998 2 26 DL72S980397 1 19980213 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 480 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 A 24 X 17.5 AREA OF SKIN WAS TRIMMED AWAY BETWEEN FS 480 AND FS 500, AND BETWEEN STRINGERS 27L AND 27R. THE SKIN CUTOUT WAS REPAIRED WITH A DOUBLER AND TRIPLER INSTALLED PERER/A 364006-14, REV A. 2 L 7 3 4F A3WE 1998022600124 19980226 00124 NM 1998 2 26 DL72S980401 1 19980217 A 3350 BATTERY PACK S111 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 416DA 21258 L1, R1, L2 AND R2 DOORS EMERGENCY LIGHTS INOP. REPLACED BATT PACKS. 2 L 7 3 4F A3WE 1998022600126 19980226 00126 NM 1998 2 26 RRXA98018 1 19980218 A 2611 CONNECTOR BOEING 727 727222 1384073 NM CARGO SMOKE DET LOOSE A RRXA O OTHER N FALSE WARNING AP APPROACH 1 WP 15 7642U 19915 ON FINAL APPROACH, THE MAIN CARGO SMOKE DETECTION LIGHT CAME ON. FOUND CONNECTOR AT SMOKE DETECTOR AMPLIFIER LOOSE, SEC URED, SYS OPS CK GOOD PER 727 MM. 2 L 7 3 4F A3WE 1998022600127 19980226 00127 NM 1998 2 26 VNAA9802015 1 19980217 A 3241 ACM30662 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 436JS 60395 4381 3052 DURING THE TAXI OUT FOR TAKEOFF, A ANTI-SKID FAIL WARNING MESSAGE OCCURED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENA NCE INSPECTED AND REPLACED THE RIGHT HAND OUTBOARD WHEEL SPEED SENSOR IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-4 2-13. OPERATION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998022600225 19980226 00225 EU 1998 2 26 MALA975993 1 19980218 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119XJ 119 DURING INSPECTION 8A, OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998022600226 19980226 00226 EU 1998 2 26 MALA975994 1 19980218 A 3020 NH24668151 INLET DUCT SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 412XJ 340B412 DURING CRUISE, THE LEFT ENGINE INTAKE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT L OWER INLET DUCT. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600227 19980226 00227 EU 1998 2 26 MALA975995 1 19980213 A 2410 728471B CSD BAC 146 AVRO146RJ85A 1500097 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 502XJ E2307 DURING CRUISE, THE NR 1 GENERATOR DRIVE HIGH TEMP ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED NR 1 ENG INE IDG/CSD ASSEMBLY. OPS AND LEAKS CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998022600228 19980226 00228 NM 1998 2 26 MALA975996 1 19980217 A 2424 51608003 GCU DHAV DHC8 DHC8102 2809003 NM LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 865MA 364 DURING CRUISE, NR 1 AC GENERATOR CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 AC GENERATOR CONTROL UNIT. ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998022600229 19980226 00229 1998 2 26 MALA975997 4 19980211 A 3414 640668901 ASI SAAB SF340 340B 7860101 EU RT COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 420XJ 420 DURING CRUISE FLIGHT AND CLIMB THROUGH 20,000 FEET, THE RIGHT ALTIMETER WAS INACCURATE, IT BEGAN INCREASING AS THE AIRCR AFT WAS CLIMBING. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE FO'S ASI. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600230 19980226 00230 EU 1998 2 26 MALA975998 1 19980216 A 3240 50125892 BRAKE SAAB SF340 SF340A 7850100 EU RH OB MLG WORN A MALA O OTHER O OTHER LD LANDING 1 GL 15 109XJ 340A109 ON LANDING IN MSP WHEN BRAKES ARE APPLIED, FULL RIGHT NOSEWHEEL AUTHORITY IS REQUIRED TO MAINTAIN DIRECTIONAL CONTROL. W HEN TAXIING TO GATE, NOTICED RIGHT BRAKE VERY WEAK. MAINTENANCE REPLACED THE POWER BRAKE VALVE AND THE RIGHT OUTBOARD B RAKE. TAXI CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600231 19980226 00231 NM 1998 2 26 MALA975999 1 19980218 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 826MA 330 DURING INSPECTION, ONE EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998022600232 19980226 00232 SO 1998 2 26 RAAA98E9007 1 19980219 A 5400 SHEAR TIE LKHEED 188 188C 5262604 SO NR 2 NACELLE CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 42551 188C2007 DURING SCHEDULED NR 1 CHECK, FOUND NR 2 NACELLE SHEAR TIE CRACKED (APPROX .25 IN) AT NAC STA -31, 13 INCHES ABOVE LOWER LONGERON. REPLACED SHEAR TIE PER SRM 51-2-9, M-54 NR 101. 2 L 7 4 4T 4A22 1998022600233 19980226 00233 WP 1998 2 26 CALA9800276 1 19980219 A 3231 LATCH MECHANISM DOUG DC9 DC932 3022066 WP LT MLG DOOR INOPERATIVE A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 19504 26010 47638 UPLATCH CHECK WAS UNSATISFACTORY. THE LEFT GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS WERE ILLUMINATED. THE GEAR WAS RECYCL ED AND RECHECKED, BUT WAS STILL UNSATISFACTORY. OPERATION WAS CONTINUED AT BELOW .70 MACH WITH RIGHT ENGINE HYDRAULICS ON HIGH. MAINTENANCE FOUND THE LT MLG DOOR LATCH MECHANISM AT FAULT, ALLOWING THE DOOR TO DROOP WITH HYDRAULIC POWER OF F. THE LATCH MECHANISM WAS REMOVED AND REPLACED IAW MM 32-31-4, PAGES 201-210. 2 L 7 2 4F A6WE 1998022600234 19980226 00234 WP 1998 2 26 CALA9800277 1 19980219 A 5210 PAN DOUG DC9 DC981 3022081 WP AFT ENTRY DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND A 1.5 CRACK IN AFT ENTRY DOOR PAN AND A 1.5 CRACK IN INNER PAN ANGLE AT CENTER RT DOOR STOP PAD. REPAI RS WERE INSTALLED IAW ECRA 5220-01034. 2 L 7 2 4F A6WE 1998022600235 19980226 00235 WP 1998 2 26 CALA9800278 1 19980220 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 1338 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND A .4375 INCH CRACK T CAP AT STA 1338, LONGERON 14R. REPAIRED IAW EA 5310-01272. 2 L 7 2 4F A6WE 1998022600236 19980226 00236 WP 1998 2 26 CALA9800279 1 19980220 A 5330 SKIN DOUG DC9 DC983 3022083 WP L1 DOORWAY DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938MC 49525 INSPECTION FOUND SEVEN SMALL DENTS 18 INCHES AFT OF LOWER AFT CORNER OF L-1 DOOR NEAR CUSP LINE. AN EDDY CURRENT INSPEC TION FOUND NO CRACKS. THE DENTS WERE PLACED ON DIP PER SRM 53-04, PAGE 212, CONDITION 2. THE DIP SPECIFIED INSPECTION EVERY 3500 LANDINGS AND REPAIR BY 15,000 LANDINGS. 2 L 7 2 4F RT A6WE 1998022600237 19980226 00237 WP 1998 2 26 CALA9800280 1 19980219 A 3610 8986264 PRSOV DOUG DC10 DC1030 3023501 WP NR 2 ENGINE INOPERATIVE A CALA A UNSCHED LANDING B M SMOKE/FUMES/ODORS/SPARKS OVER TEMP CL CLIMB 1 SW 09 525MD 46550 THE NR 2 PACK OVERHEATED WITH SMOKE ENTERING THE CABIN WHILE LEVELING OFF AT FL 280. THE AIRCRAFT WAS RETURNED TO DUS, WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE NR 2 ENGINE PRSOV WOULD NOT SHUT OFF ELECTRICALLY, CAUSING THE NR 2 PACK TO OVERTEMP AND TRIP. THE NR 2 PRSOV WAS LOCKED OUT MANUALLY AND THE NR 2 PNEUMATIC SYSTEM AND NR 2 PACK WERE PLACARDED INOPERATIVE. THE ENGINES WERE RUN AND ALL OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1998022600238 19980226 00238 WP 1998 2 26 9802879614 1 19980218 A 2720 37723745503 SO VALVE DOUG DC9 DC932 3022066 WP RUDDER LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 614NW 2579 2579 47128 DURING CRUISE ALTITUDE AT 29,000 FEET, RUDDER CONTROL MANUAL LIGHT BEGAN FLICKERING AND RIGHT HYDRAULIC SYSTEM WENT TO Z ERO. FLIGHT WAS CONTINUED TO DESTINATION. CREW DECLARED AN YELLOW EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RUDDER HYDRAULIC POWER SHUTOFF VALVE LEAKING. REPLACED VALVE. OPERATIONAL CHECK NORMAL. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998022600239 19980226 00239 WP 1998 2 26 9802889614 1 19980219 A 3397 WIRE DOUG DC9 DC932 3022066 WP TAIL COMPT SHORTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 614NW 47128 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS FOR TAILCONE PULL HANDLE INOPERATIVE. REPAIRED SHORTED WIRES UNDER WALKWAY AND REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600240 19980226 00240 WP 1998 2 26 9802899965 1 19980219 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 911RW 47149 RED EMERGENCY LIGHTS BETWEEN ROWS 10 THROUGH 12 AND WHITE EMERGENCY LIGHTS BETWEEN ROWS 13 THROUGH 15 ILLUMINATED FOR 15 MINUTES IN FLIGHT AND THEN WENT OUT. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE ON GROUND. REPLACED POWER SUP PLY AT AFT LEFT OVERWING EMERGENCY EXIT AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998022600241 19980226 00241 WP 1998 2 26 9802919752 1 19980218 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT SIGNS OVER AFT OVERWING EXIT DOORS INOPERATIVE. MAINTENANCE REPLACED BATT ERIES IN CHARGING UNIT. 2 L 7 2 4F A6WE 1998022600242 19980226 00242 WP 1998 2 26 9802929852 1 19980218 A 3350 BATTERY DOUG DC9 DC951 3022051 WP BATTERY PACK INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 5-9. MAINTENANCE REPLACED BATTERIES IN EMERGENCY EXIT LIGHT PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998022600243 19980226 00243 WP 1998 2 26 9802939307 1 19980217 A 2780 PULLEY DOUG DC9 DC982 3022082 WP LE SLAT BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 309RC 48088 DURING CLIMB-OUT, SLAT DISAGREE INDICATION LIGHT ILLUMINATED. FLIGHT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAIN TENANCE REPLACED CABLE RUN 2088 IN WHEEL WELL AREA AND A BROKEN PULLEY. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998022600244 19980226 00244 NM 1998 2 26 UPS98425814 1 19980218 A 2612 FIRE CARD BOEING 747 747123F NM E/E COMPT LOOSE A IPXA K NONE N FALSE WARNING UK UNKNOWN 1 SO 01 676UP 20101 IN FLIGHT TRANSIT MASTER FIRE WARNING LIGHT (FLASHED THREE). NO OTHER INDICATIONS. LIGHT TEST GOOD. RERACKED FIRE WAR NING CARDS, OPS CK GOOD PER M/M 26-11-00 AND 26-15 -00, 26-14-00, 26-16-00. OK FOR SERVICE. 2 L 7 4 4F A20WE 1998022600245 19980226 00245 WP 1998 2 26 UPS98825807 1 19980207 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 960-980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C LONGERON 24R, CRACK HAS EXTENDED BEYOND PREVIOUS STOP DRILL AFT PAST 980 BULKHEAD AND HAS EXTENDED PAS T STOP DRILL AT F/S 968 FWD TO F/S 962. REMOVED EXISTING REPAIR F/S 960-980, REMOVED LOWER FITTING F/S 960 IAW SRM 51-1 -20. STOP DRILLED CRACKS IAW SRM 53-2-2 FIG 5. NDT CHECK CONFIRMED CRACK TERMINATED BY STOP DRILL. REINSTALLED EXISTI NG REPAIR, AND FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998022600246 19980226 00246 WP 1998 2 26 UPS98825808 1 19980217 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 732.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C LT WING L/E AT STA XFS 732.750, THE L/E RIB IS CRACKED AT THE AFT LOWER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600247 19980226 00247 WP 1998 2 26 UPS98825809 1 19980217 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 791 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C LT WING L/E AT STA XFS 791.0. THE L/E RIB IS CRACKED AT THE LOWER AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600248 19980226 00248 WP 1998 2 26 UPS98825810 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, RT WING L/E AT STA XFS 628.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0 . 2 L 7 4 4F RT 4A25 1998022600249 19980226 00249 WP 1998 2 26 UPS98825811 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 366.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E LWR ARM OF RIB CRACKED BY GUSSET AT STA XFS 366.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600250 19980226 00250 WP 1998 2 26 UPS98825812 1 19980216 A 2560 SMOKE CURTAIN DOUG DC8 DC871F 302199D WP CABIN TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 718UP 46018 INSPECTION TYPE:SV, MAIN CABIN SMOKE CURTAIN TORN. REMOVED AND REPLACED SMOKE CURTAIN IAW DC8-25-50-02. 2 L 7 4 4F RT 4A25 1998022600251 19980226 00251 WP 1998 2 26 UPS98825815 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 741.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, RT WING L/E RIB AT STA XFS 741.250 IS CRACKED AT THE UPPER AFT END. REPAIRED CRACKED RIB IAW SRM 57- 2-0. 2 L 7 4 4F RT 4A25 1998022600252 19980226 00252 WP 1998 2 26 UPS98825816 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, RT WING L/E AT STA XFS 785.00, THE L/E RIB IS CRACKED AT THE UPPER AFT END. REPAIRED CRACKED RIB IA W SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600253 19980226 00253 WP 1998 2 26 UPS98825817 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 828.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER HOLE STA 828.750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600254 19980226 00254 WP 1998 2 26 UPS98825818 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 735 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LT WING L/E RIB LOWER ARM CRACKED BY AFT FASTENER STA XFS 735.000. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600255 19980226 00255 WP 1998 2 26 UPS98825819 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 647.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C RT WING L/E AT STA XFS 647.500, THE UPPER L/E RIB IS CRACKED AT AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600256 19980226 00256 WP 1998 2 26 UPS98825820 1 19980216 A 5330 SKIN DOUG DC8 DC873F 302199F WP CARGO DOORWAY DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 HOLE AND BULGE IN BELLY SKIN AT STRINGER 36 UNDER AND ABOUT 2 FT FWD OF NR 2 PIT DOOR. REPAIRED DAMAGED SKIN IAW EO DC8 -5330-10030-A SEE EO FOR SIGN-OFFS. 2 L 7 4 4F RT 4A25 1998022600257 19980226 00257 WP 1998 2 26 UPS98825821 1 19980205 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, FWD ACC COMP AT STA 680 RBL 24, SEAT TRACK SUPPORT FITTING IS CRACKED. REMOVED, FABRICATED, AND INST ALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 5773275. 2 L 7 4 4F RT 4A25 1998022600258 19980226 00258 WP 1998 2 26 UPS98825823 1 19980124 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, LOWER FWD CARGO COMPT STATION 320.000 LONG 33 LEFT TO LONG 32 LEFT, CORRODED BATHTUB FITTING. R EMOVED AND FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW PART NR 3755822 05N LOCATED AND DRILLED NEW PART IAW DC8 SRM 51-3 -2. REMOVED CORROSION AT STRUT AND HOLES IAW DC8 SRM 51-1-8. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW PA RT IAW DC8 SRM 51-1-50D. 2 L 7 4 4F RT 4A25 1998022600259 19980226 00259 WP 1998 2 26 UPS98825824 1 19980123 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1695 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CORRODED AT LONGERON 26 RIGHT. REMOVED BATH TUB FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8 INSTALLED NEW FITTING IAW DC8 SRM 51-1-2 1 AND 51-1-20D. TORQUED BOLTS IAW DC8 SRM 51-3-1 . 2 L 7 4 4F RT 4A25 1998022600260 19980226 00260 WP 1998 2 26 UPS98825825 1 19980123 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1695 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 28 RIGHT. REMOVED BATH TUB FITTING LOCATED AND D RILLED NEW FITTING IAW DC8 SRM 51-1-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-2 1 AND 51-1-20D. TORQUES IAW DC8 SRM 51-3-1 . 2 L 7 4 4F RT 4A25 1998022600261 19980226 00261 WP 1998 2 26 UPS98825826 1 19980123 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1695 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 30 RIGHT. REMVOED BATH TUB FITTING LOCATED AND D RILLED NEW FITTING IAW DC8 SRM 51-1-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-2 1 AND 51-1-20D. TORQUED IAW DC8 SRM 51-3-1 . 2 L 7 4 4F RT 4A25 1998022600262 19980226 00262 WP 1998 2 26 UPS98825827 1 19980123 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1685 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, STA 1685 BATH TUB FITTING CRACKED AT LONGERON 34 LEFT. REMOVED BATH TUB FITTING LOCATED AND DR ILLED NEW FITTING IAW DC8 SRM 51-1-21 A ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-21 A ND 51-1-20D. TORQUED BOLT IAW DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 1998022600263 19980226 00263 WP 1998 2 26 UPS98825828 1 19980123 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1695 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 30 LEFT. REMOVED BATH TUB FITTING LOCATED AND DR ILLED NEW FITTING IAW DC8 SRM 51-1-21. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-21 A ND 51-1-20D. TORQUED BOLT IAW DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 1998022600264 19980226 00264 WP 1998 2 26 UPS98825829 1 19980123 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1695 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, STA 1695 BATH TUB FITTING CRACKED AT LONGERON 26 LEFT. REMOVED BATH TUB FITTING LOCATED AND DR ILLED NEW FITTING IAW DC8 SRM 51-10-21 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-21 A ND 51-1-20D. TORQUED BOLT IAW DC8 SRM 51-3-1. 2 L 7 4 4F RT 4A25 1998022600265 19980226 00265 WP 1998 2 26 UPS98825830 1 19980123 A 5531 SPAR DOUG DC8 DC871F 302199D WP VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, VERTICAL STABILIZER FRONT SPAR LOWER CAP CORRODED STA 1750 FROM X 10 TO X 30. REMOVED CORROSIO N FROM VERTICAL STAB FRONT SPAR LOWER CAP AT FS 1750 FROM X30 TO X10 IAW DC8 SRM 51-1-8. ALODINED AND PRIMED AREA IAW D C 8 SRM 51-1-8 2 L 7 4 4F RT 4A25 1998022600266 19980226 00266 WP 1998 2 26 UPS98825831 1 19980123 A 5530 BRACKET DOUG DC8 DC871F 302199D WP BS 1720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, VERTICAL STAB FRONT SPAR ATTACH ANGLE IS CORRODED STA 1720 AT LONGERON 13 RIGHT. REMOVED CORRO SION FROM VERTICAL STAB FRONT SPAR ATTACH ANGLE AT FS 1720 LONGERON 13 RIGHT IAW DC8 SRM 51-1-8 ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8 2 L 7 4 4F RT 4A25 1998022600267 19980226 00267 WP 1998 2 26 UPS98825832 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 816.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C LT WING L/E RIB UPPER AND LOWER ARMS ARE CRACKED BY THE AFT FASTENER AT STA XFS816.250. REPAIRED CRAC KED RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600268 19980226 00268 WP 1998 2 26 UPS98825833 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 578.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.578.750. REPAIRED CRACKED L/E RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600269 19980226 00269 WP 1998 2 26 UPS98825834 1 19980206 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 735.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.735.750. REPAIRED CRACKED RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600270 19980226 00270 WP 1998 2 26 UPS98825835 1 19980207 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 84 LIGHTNING STRIKE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C, LIGHTNING STRIKE AT FS 84 LONG 21R, FOUND TO BE OUT OF LIMITS. REPAIRED EXTERNAL SKIN AT STA 84 LONG 21R IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 1998022600271 19980226 00271 WP 1998 2 26 UPS98825836 1 19980205 A 5311 3646688505 FRAME DOUG DC8 DC873F 302199F WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE:C FWD ACC COMP AT STA 660 BELOW STR 21R, FRAME HAS A 3 INCH CRACK NEAR RADIUS. REMOVED AND REPLACED FRA ME SECTION IAW DWG 364688 AND SRM 51-1 20-D. 2 L 7 4 4F RT 4A25 1998022600272 19980226 00272 WP 1998 2 26 UPS98825837 1 19980123 A 5531 SPAR DOUG DC8 DC871F 302199D WP VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D, CK VERTICAL STABILIZER FRONT SPAR CORRODED STA 1730 AT LONGERON 11 RIGHT. REMOVED CORROSION FROM FRO NT SPAR OF VERTICAL STABILIZER IAW DC8 SRM 51-1-8 ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998022600273 19980226 00273 WP 1998 2 26 UPS98825838 1 19980123 A 5531 SPAR DOUG DC8 DC871F 302199D WP VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK VERTICAL STABILIZER 5 LEFT FRONT SPAR CORRODED STA 1700-1740 FROM LONGERON 9 LEFT TO 18 LEFT ( A FT CABIN). REMOVED CORROSION IAW 51-1-8 TIMCO RFTS ENGINEERING DISPOSITION ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998022600274 19980226 00274 WP 1998 2 26 UPS98825839 1 19980123 A 5312 BULKHEAD BEAM DOUG DC8 DC871F 302199D WP BS 1756 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D CHECK, FORWARD SIDE OF AFT PRESSURE BULKHEAD VERTICAL BEAM FWD CAP IS CORRODED ON RIGHT SIDE 8 FROM TO P. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998022600275 19980226 00275 NM 1998 2 26 QXEA9800076 1 19980218 A 2120 AIR DISTRIBUTION DHAV DHC8 DHC8202 2809007 NM CABIN ODOR A QXEA K NONE L NO TEST AP APPROACH 1 NM 09 346PH 477 ACV - VERY STRONG SMELL OF SMOKE ON APPROACH. DID NOT HAVE HIGH DUCT TEMPS. SMELLED LIKE ELECTRICAL BUT NO VISIBLE SMO KE. MAINTENANCE GROUND RAN NR 1 AND NR 2 ENGINES. APPLIED ALL ELECTRICAL LOADS. NO DEFECTS NOTED. OPERATED NR 1 AND NR 2 BLEED SYSTEMS AND CABIN LIGHT SYSTEMS. NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998022600276 19980226 00276 NM 1998 2 26 98FDEA00121 1 19980220 A 5311 586040502 FRAME BOEING 727 72721C 138400M NM BS 254 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 NR 0926 043, STA-PAE - WHILE WORKING NR 0920 FOUND FRAME BEHIND NR 3 WINDOW ON THE RT SIDE AT BS 254, STR 9-11 RT TO BE CRACKED. REMOVED FRAME RT SIDE AT BS 254, STR 9-11. FABRICATED FRAME FROM 7075-T6.040. ALODINED AND PRIMED. INSTALLE D FRAME IAW SRM 51-10-3, 51-20-1, M/M 51-20-151 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998022600277 19980226 00277 NM 1998 2 26 98FDEA00122 1 19980220 A 3297 WIRE BOEING 727 727227 1384078 NM RETRACT MECH FAILED A FDEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 25 482FE 21464 LANDING GEAR HANDLE WOULD NOT COME UP. APPROPRIATE CHECK LISTS FOLLOWED WITH NEGATIVE RESULTS. LOG BOOK ENTRY REQUIRED . *S/D* REPAIRED SPLICE ON WIRE W526-206-22B PER FED-EX WPM 20-30-12. FUNCTIONAL CHECKED GOOD PER FED-EX M/M 32-31-11 . 2 L 7 3 4F A3WE 1998022600279 19980226 00279 WP 1998 2 26 ABXA9800110 1 19980217 A 2612 D5020 FIRE LOOP DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 812AX 46126 670969 NR 4 ENGINE FIRE WARNING BELL SOUNDED INTERMITTENTLY. ALL FOUR ENGINES WERE TESTED. NR 4 WOULD NOT TEST. NR 4 ENGINE WAS SECURED. CSD WAS DISCONNECTED AND NR 4 FIRE BOTTLE WAS DISCHARGED. NR 4 ENGINE FIRE LOOP ELEMENT WAS FOUND TO BE D EFECTIVE. REPLACED FIRE LOOP ELEMENT IAW DC8 MM 26-10-1. 2 L 7 4 4F 4 F 4A25 1E8 1998022600280 19980226 00280 WP 1998 2 26 ABXA00089 1 19980218 A 5320 99100783 SUBFLOOR DOUG DOUG DC9 DC931 3022065 WP BS 149 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND THE SUBFLOOR DIAPHRAM CRACKED AT STA 149, BL 0.0 AND STA 160 BL 0.0. REPAIRED SUBFLOOR IAW DC9 SR M 53-01. 2 L 7 2 4F A6WE 1998022600281 19980226 00281 WP 1998 2 26 ABXA9800090 1 19980218 A 5400 991550031 ANGLE DOUG DOUG DC9 DC931 3022065 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND ANGLE JUST INBD OF AFT ENGINE MOUNT IN NR 1 PYLON CRACKED AT LOWER FASTENER. REPLACED ANGLE IAW D C9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998022600282 19980226 00282 WP 1998 2 26 ABXA9800091 1 19980218 A 5400 591326244 ANGLE DOUG DOUG DC9 DC931 3022065 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND RIGHT PYLON TO FUSELAGE UPPER ATTACH ANGLE CRACKED AT STA 980. REPLACED ANGLE IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1998022600283 19980226 00283 WP 1998 2 26 ABXA9800092 1 19980218 A 5400 99582214 WEB DOUG DOUG DC9 DC931 3022065 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND RIGHT PYLON VERTICAL WEB CRACKED FORWARD AND INBOARD OF THE AFT ENGINE MOUNT. REPLACED WEB IAW DC 9 SRM 54-10-00 AND 51-10-5. 2 L 7 2 4F A6WE 1998022600284 19980226 00284 WP 1998 2 26 ABXA9800093 1 19980218 A 5313 59114277 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON 16L CRACKED FORWARD OF STA 945. REPLACED LONGERON FROM STA 935-965 IAW DC9 SRM 51-30-2 A ND 51-30-5. 2 L 7 2 4F A6WE 1998022600285 19980226 00285 WP 1998 2 26 ABXA9800094 1 19980218 A 5313 59114227 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON NR 1 CRACKED AT STA 718. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998022600286 19980226 00286 WP 1998 2 26 ABXA9800095 1 19980218 A 5313 591142221 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON 6L CRACKED AT STA 699. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998022600287 19980226 00287 WP 1998 2 26 ABXA9800096 1 19980218 A 5313 591142221 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 639 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND LONGERON 3R CRACKED AT STA 639. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998022600288 19980226 00288 WP 1998 2 26 ABXA9800097 1 19980218 A 5320 49125402 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND VERTICAL SUPPORT FITTING AT STA 965 FLOORBEAM CRACKED ON RIGHT SIDE IN AFT LOWER CARGO COMPT. RE PLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998022600289 19980226 00289 WP 1998 2 26 ABXA9800098 1 19980218 A 5320 991555117 INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND INTERCOSTAL CRACKED AFT OF STATION 996 AT LONGERON 5R. REPAIRED INTERCOSTAL IAW DC9 SRM K05159. 2 L 7 2 4F A6WE 1998022600290 19980226 00290 WP 1998 2 26 ABXA9800099 1 19980218 A 5741 99193644 FITTING DOUG DOUG DC9 DC931 3022065 WP WS 477 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND THE RIGHT WING, LOWER OUTBOARD HORIZONTAL FLANGE OF THE BULKHEAD/AILERON HINGE FITTING AT STA XRS4 77 INSIDE THE FUEL VENT TANK CORRODED BEYOND LIMITS. INSTALLED REPAIR IAW ABX REA D957-22556MR. 2 L 7 2 4F A6WE 1998022600291 19980226 00291 WP 1998 2 26 ABXA9800100 1 19980215 A 5720 36518091 FITTING DOUG DOUG DC8 DC861 3021952 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LEFT WING TRAILING EDGE PANEL VERTICAL SUPPORT FITTING BETWEEN SPOILER HINGE RIBS IS CRACKED AT UPPER EDGE JUST AFT OF M AIN LANDING GEAR TRUNNION. REPAIRED IAW DC8 SRM 57-1-0. 2 L 7 4 4F 4A25 1998022600292 19980226 00292 WP 1998 2 26 ABXA9800101 1 19980208 A 5510 3653396 ANGLE DOUG DOUG DC8 DC861F 3021953 WP HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 UPPER L-ANGLE CRACKED ON LEFT HORIZONAL STABILIZER OUTBOARD TIP. FABRICATED AND INSTALLED REPAIR PER REA D855-2265-MR. 2 L 7 4 4F 4A25 1998022600293 19980226 00293 WP 1998 2 26 ABXA9800102 1 19980208 A 5320 4758514517 TIE FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 1138 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 INTERCOSTAL TIE FITTING CRACKED AT STA 1138 ABOVE LONGERON 33R. REPAIRED IAW DACO DWG 4758514 AND SRM 51-18. 2 L 7 4 4F 4A25 1998022600294 19980226 00294 WP 1998 2 26 ABXA9800103 1 19980208 A 5753 576993315 SLOT VANE DOUG DOUG DC8 DC861F 3021953 WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LEFT OUTBOARD SLOT VANE AT INBOARD END ON LEADING EDGE CORRODED BEYOND LIMITS. REPAIRED IAW SRM 57-3-10 FIG 20. 2 L 7 4 4F 4A25 1998022600295 19980226 00295 WP 1998 2 26 ABXA9800104 1 19980208 A 5730 5769545 SKIN DOUG DOUG DC8 DC861F 3021953 WP WS 710.5 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LEFT WING LEADING EDGE SKIN CORRODED AT STA XFS 710.5. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F 4A25 1998022600296 19980226 00296 WP 1998 2 26 ABXA9800105 1 19980106 A 5320 3779659501 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 902 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LONGERON END FITTING CRACKED AFT OF STATION 902 LONGERON 3L. REPLACED LONGERON END FITTING IAW SRM 51-1-21. 2 L 7 4 4F 4A25 1998022600297 19980226 00297 WP 1998 2 26 ABXA9800106 1 19980127 A 5320 5750726 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 246-260 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 INTERCOSTAL CRACKED FS 246-260 LONGERON 33L. REPAIRED IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1998022600298 19980226 00298 WP 1998 2 26 ABXA9800107 1 19980129 A 5511 56545137 RIB DOUG DOUG DC8 DC861 3021952 WP RT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB LWR ARM CRACKED AT STA XFS 141.250. REPAIRED IAW DC8 SRM 55-31. 2 L 7 4 4F 4A25 1998022600299 19980226 00299 WP 1998 2 26 ABXA98108 1 19980129 A 5320 5616673 SUPPORT DOUG DOUG DC8 DC861 3021952 WP BS 1440 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 SUPPORT WEB CRACKED AT AFT LOWER CORNER AT STA 1440 BL 0 IN NR 4 CARGO COMPARTMENT. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998022600300 19980226 00300 WP 1998 2 26 ABXA9800109 1 19980106 A 5753 46495972 FITTING DOUG DOUG DC8 DC861 3021952 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 RIGHT WING TRAILING EDGE AT FLAP STA 410.00, THE OUTBOARD CANOE FITTING STIFFENER FITTING IS CRACKED AND CORRODED. REPL ACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F 4A25 1998022600304 19980226 00304 NM 1998 2 26 SCNA98013 1 19980118 A 5314 6518636378 KEEL BEAM BOEING 727 7272A1 138407F NM BS 870 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A SCHEDULED MAINTENANCE CHECK, A CRACK WAS LOCATED ON THE VERTICAL KEEL BEAM CHORD AT BS 870, APPROXIMATE RBL 3.5 . DURING REMOVAL AND REPLACEMENT OF THE CRACKED CHORD NO ADJACENT STRUCTURE WAS FOUND DAMAGED. 2 L 7 3 4F A3WE 1998022600305 19980226 00305 NM 1998 2 26 SCNA98014 1 19980118 A 5314 6518636378 KEEL BEAM BOEING 727 7272A1 138407F NM BS 870 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A SCHEDULED MAINTENANCE CHECK, A CRACK WAS LOCATED ON THE VERTICAL KEEL BEAM CHORD AT BS 870, APPROXIMATE RBL 3.5 . DURING REMOVAL AND REPLACEMENT OF THE CRACKED CHORD A KEEL BEAM SUPPORT ANGLE WAS FOUND CRACKED COMPLETELY THROUGH BO TH FLANGES AND A CRACK WAS DISCOVERED ON THE WEB. THE SUPPORT ANGLE WAS REMOVED AND REPLACED AND AN SRM REPAIR WAS ACCO MPLISHED ON THE WEB. 2 L 7 3 4F A3WE 1998022600312 19980226 00312 NM 1998 2 26 CKSA98016 1 19980218 A 5230 HINGE BOEING 727 727223 1384074 NM BS 590-600 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 19487 DURING ROUTINE CPCP INSPECTION FOUND: MAIN CARGO DOOR HINGE CRACKED AIRCRAFT SIDE AFT LOBE. REMOVED AND REPLACED DAMAGE D DOOR HINGE AFT UPPER FROM STA 590 - STA 600 IAW B727 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-100-01 PART 5 OF 6. NON-ROUTINE TASK CARD NUMBER 17118. 2 L 7 3 4F A3WE 1998022600313 19980226 00313 NM 1998 2 26 CKSA98017 1 19980218 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 629 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 19487 DURING ACCOMPLISHMENT OF AD 94-07-08 S/B 727-157-127 FOUND CRACK LT WING UPPER FWD STRINGER AFT EAR STA629 (INTERNAL). I NSTALLED REPAIR PARTS IAW BOEING B727 SERVICE BULLETIN 727-57-A159. NON-ROUTINE TASK CARD NUMBER 17131. 2 L 7 3 4F A3WE 1998022600314 19980226 00314 NM 1998 2 26 CKSA98018 1 19980218 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 686 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 720CK 19487 DURING ACCOMPLISHMENT OF AD 94-07-08 S/B 727-57-127 FOUND CRACK LT WING UPPER AFT STRINGER STA686 (INTERNAL). INSTALLED REPAIR IAW B727 SB 727-57-A159. NON-ROUTINE TASK CARD NUMBER 17132. 2 L 7 3 4F A3WE 1998022600315 19980226 00315 NM 1998 2 26 CKSA98019 1 19980209 A 3260 CLAMP BOEING 747 747269B NM LT MLG MISINSTALLED A CKSA O OTHER J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 GL 23 707CK 21541 AFTER T/O, MLG LEVER LOCK WOULD NOT RETRACT. ACCOMP ABNORMAL CHECKLIST, FOUND BOTH PRIMARY AND ALT WING GEAR TILT LIGHTS ILLUM. CYCLED PRIM DIS AND CONT L/G CB, MLG LEVER LOCK RETRACTED. WING GEAR PRI TILT LIGHT EXTINGUISHED AND GEAR RETRAC TED. APPROX 10 MIN AFTER GEAR RETRACTION MLG LOCK MOVED OUT OF STOWED POSITION AND BOTH PRI AND ALT WING GEAR TILT LIGHT S WERE ILLUMINATED WHEN TESTED. APPROX 1.5 HRS INTO FLIGHT W/O ANY INPUT THE MLG LOCK RETRACTED AND PRI WING GEAR TILT L IGHT EXTINGUISHED. FOUND INCORRECTLY INSTALLED ADEL CLAMP IN J BOX, CORRECTED CLAMP INSTALLATION. TESTED SYSTEM, FUNCTI ONING NORMAL. 2 L 7 4 4F RT A20WE 1998022600316 19980226 00316 WP 1998 2 26 CKSA98020 1 19980210 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 841 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT WING L/E DAMAGE TO XFS 841 APPROXIMA TE 1.5 FT. CUT OUT DAMAGED SECTION OF L/E AND FABRICATED FILLER PLATE AND REPAIR DOUBLER IAW SRM 57-2-1. OK TO TREAT A ND PRIME REWORK AREA AND REPAIR PARTS: TREATED AND PRIMED IAW SRM 51-1-8. OK TO INSTALL: INSTALLED REPAIR PARTS IAW SRM 57-2-1 SIZE OF REPAIRS: FILLER PLATE .063 BY 12.5 BY 3 2024-T3. REPAIR DOUBLER .063 BY 20 BY 20 2024-T3. NON-ROUTINE I TEM WORK CARD NUMBER 0004. 2 L 7 4 4F 4A25 1998022600317 19980226 00317 WP 1998 2 26 CKSA98021 1 19980210 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 120 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, DAMAGE LOWER FUSELAGE FS 120.0 STRINGER 35R AND 34R. CUT OUT DAMAGED SECTION OF SKIN AND FABRICATED REPAIR DOUBLER, FILLER PLATE AND FINGER DOUBLERS IAW SRM 5 3-2-1. CUT OUT DAMAGED SECTION OF LONGERON AND PREPARE A NEW SECTION OF LONGERON AND SPLICES IAW SRM 53-2-2 OK TO TREAT AND PRIME REWORK AREA, REPAIR DOUBLER, FILLER PLATE, FINGER DOUBLERS, LONGERON AND SPLICES: TREATED AND PRIMED IAW SRM 51-1-8. NON-ROUTINE ITEM WORK CARD NUMBER 0011. 2 L 7 4 4F 4A25 1998022600318 19980226 00318 WP 1998 2 26 CKSA98022 1 19980210 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 204 WRINKLED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, RT WING OUTBD FLAP INBD AREA AT STA 204 XRS HAS WRINKLED T/E. REMOVED DAMAGED SECTION OF T/E IAW SRM 51-1-21 AND FABRICATED NEW ONE USING SAME THICKNESS SAME MATERIAL IAW SRM 57-7-1 OK TO INSTALL NEW SECTION OF T/E: INSTALLED NEW SECTION OF T/E O/B FLAP INBD AREA STA 204 XRS I AW SRM 51-1-21A. SIZE OF NEW T/E: .032 BY 43 BY 4 BY 4 2024-T3. NON-ROUTINE ITEM WORK CARD NUMBER 0012. 2 L 7 4 4F 4A25 1998022600319 19980226 00319 WP 1998 2 26 CKSA98023 1 19980210 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 795 TORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LEFT WING, LOWER SKIN O/B OF O/B AILERO N WS XFS 795 RIP ON SKIN. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE IAW AIA INC SKETCH 2743 OK TO TREAT AN D PRIME. TREATED AND PRIMED IAW SRM 51-1-8. OK TO INSTALL NEW SKIN. INSTALLED NEW SKIN IAW AIA INC SKETCH 2743 EA D8- 57-022 SIZE OF NEW SKIN: 22 BY 32 .040 7075-T6 SPLICE .050 BY 3.25 BY 29 7075-T6. NON-ROUTINE ITEM WORK CARD 0013. 2 L 7 4 4F 4A25 1998022600320 19980226 00320 WP 1998 2 26 CKSA98024 1 19980210 A 5210 SKIN DOUG DC8 DC863F 302198F WP PAX DOOR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, FWD PASSENGER DOOR EXT SKIN AFT UPPER C ORNER OLD REPAIR CRACKED SECTION MISSING. REMOVED DAMAGED REPAIR IAW DC8 SRM 51-1-21. FABRICATED NEW REPAIR PER DC8 SR M 52-2-3 FIG 10. OK TO TREAT AND PRIME. REPAIRED AND AREA TREATED AND PRIMED PER DC8 SRM 51-1-8. DRILLING NEW REPAIR PER DC8 SRM 51-3-2 OK TO INSTALL REPAIR 34.5 BY 5.5 7075-T6 - 0.50. INSTALLED REPAIR IAW DC8 SRM 52-2-3 FIG 10. NON-RO UTINE ITEM WORK CARD 0017. 2 L 7 4 4F 4A25 1998022600321 19980226 00321 WP 1998 2 26 CKSA98025 1 19980210 A 5522 SKIN DOUG DC8 DC863F 302198F WP LT ELEVATOR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEV HINGE CUT-OUT AT XE 77.000 SKIN EDGES CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATERIA L IAW SRM 55-4-1. OK TO TREAT AND PRIME. TREATED AND PRIMED IAW SRM 51-1-8 OK TO INSTALL. INSTALLED NEW SKIN IAW SRM 5 1-1-21 SIDE OF SKIN, .040 BY 5 BY 2 - 2024-T3. NON-ROUTINE ITEM WORK CARD 0023. 2 L 7 4 4F 4A25 1998022600322 19980226 00322 WP 1998 2 26 CKSA98026 1 19980210 A 5522 SKIN DOUG DC8 DC863F 302198F WP LT ELEVATOR DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEVATOR AT STA XE 272.0 WEB SKIN FO R HINGE CUTOUT IS DAMAGED AND CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATERIAL IAW SRM 55-4-1. OK TO TREAT AND PRIME. TREATED AND PRIMED IAW SRM 51-1-8 OK TO INSTALL. INSTA LLED NEW SKIN IAW SRM 51-1-21 SIZE OF NEW SKIN, .040 BY 3.5 BY 2 2024-T3. NON-ROUTINE ITEM WORK CARD 0029. 2 L 7 4 4F 4A25 1998022600323 19980226 00323 WP 1998 2 26 CKSA98027 1 19980210 A 5522 SKIN DOUG DC8 DC863F 302198F WP LT ELEVATOR DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEVATOR AT STA XE 221.0 WEB SKIN FO R HINGE CUTOUT IS DAMAGED AND CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATERIAL IAW SRM 55-4-1. OK TO TREAT AND PRIME. TREATED AND PRIMED IAW SRM 51-1-8 OK TO INSTALL. INSTA LLED NEW SKIN IAW SRM 51-1-21 SIZE OF SKIN, .040 BY 3.5 BY 2 2024-T3. NON-ROUTINE ITEM WORK CARD 0030. 2 L 7 4 4F 4A25 1998022600324 19980226 00324 WP 1998 2 26 CKSA98028 1 19980210 A 5522 SKIN DOUG DC8 DC863F 302198F WP LT ELEVATOR DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DUE TO WEATHER IN MIAMI AIRPORT SUCH AS HIGH WINDS, TORNADO'S AND FLYING DEBRIS, LT ELEVATOR AT STA XE 149.0 WEB SKIN FO R HINGE CUT OUT IS DAMAGED AND CRACKED. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW ONE AS PER SAMPLE USING SAME THICKNESS SAME MATERIAL IAW SRM 55-4-1. OK TO TREAT AND PRIME, TREATED AND PRIMED IAW SRM 57-1-8 OK TO INSTALL. INSTA LLED NEW SKIN IAW SRM 51-1-21 SIZE OF SKIN, .040 BY 3.5 BY 2 2024-T3. NON-ROUTINE ITEM WORK CARD 0031. 2 L 7 4 4F 4A25 1998022600325 19980226 00325 EU 1998 2 26 AWXA9800053 1 19980212 A 2121 EVT3454G FAN AIRBUS 320 A320231 3930325 EU E/E COMPT FAILED A AWXA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 WP 28 626AW 53716 53716 65 INFLIGHT TURNBACK DUE TO ELECTRICAL SMOKE SMELL AS A RESULT OF AVIONICS VENTILATION BLOWER FAULT FOLLOWED BY SOUND OF BL OWER FAN SELF-DESTRUCTION. NO ECAM WARNINGS PRESENT. FOUND AVIONICS COOLING FAN FROZEN. REMOVED AND REPLACED. 2 L 7 2 4F RT A28NM 1998022600326 19980226 00326 NM 1998 2 26 AWXA9800054 1 19980217 A 2120 AIR DISTR BOEING 737 737277 1384570 NM CABIN SMOKE A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 183AW 22650 CREW REPORTED, SMOKE IN THE CABIN. A/C RETURNED TO DEN ATBC. CONTRACT MX CHECKED BOTH PACKS, RECIR FAN, LIGHT BALLAST, EYEBALL VENTS, RAN PACKS WITH ENGINES AND APU, PRESSURIZED THE A/C. MX COULDN'T DUPLICATE THE PROBLEM, CREW REFUSED, A /C FLIGHT WAS CANCELLED. STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998022600327 19980226 00327 NM 1998 2 26 AWXA9800055 1 19980217 A 3397 WIRE BOEING 737 73733A 1384673 NM CABIN BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 172AW 23631 EMERGENCY AISLE LIGHT ROW 1 SEAT LIGHT INOP. REPAIRED BROKEN WIRE, OPS CK GOOD. STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998022600328 19980226 00328 NM 1998 2 26 AWXA9800056 1 19980218 A 3350 033006 POWER SUPPLY BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 322AW 25400 EMERGENCY LIGHTS INOP AISLE 6, 7, 8, 9, AND 10. REPLACED FUSES IN POWER SUPPLY. STC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998022600329 19980226 00329 NM 1998 2 26 AWXA9800057 1 19980218 A 3350 6104789 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 188AW 22655 L1 AND R1 ENTERIOR EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED FWD CARGO PIT LT SIDEWALL EMERGENCY LIGHT BATTE RY PACK, OP CHECK GOOD. 2 L 7 2 4F RT A16WE 1998022600330 19980226 00330 EU 1998 2 26 AWXA9800058 1 19980218 A 2910 O-RING AIRBUS 320 A320231 3930325 EU GREEN HYD SYST FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 627AW 66 EMERGENCY DECLARED, GREEN SYSTEM RSVR LO LEVEL EN ROUTE. DIVERT TO LAS. REPLACED O-RING ON PRESSURE SWITCH ON GREEN MA IN HYDRAULIC POWER MANIFIOLD, SERVICED ALL THREE MANIFOLDS, RESET EMERGENCY GEAR HANDLE. 2 L 7 2 4F RT A28NM 1998022600331 19980226 00331 NM 1998 2 26 AWXA9800059 1 19980219 A 3397 WIRE BOEING 737 7372A6 138448B NM CABIN LOOSE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 20194 EMER LIGHT INOP AT 9BC. RECONNECTED WIRING. STC NR SA3432NM. 2 L 7 2 4F A16WE 1998022600332 19980226 00332 NM 1998 2 26 AWXA9800060 1 19980219 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 AFT EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED BATTERY PACK FOR AFT EMERGENCY EXIT SIGN SYSTEM, OPS CHECKS GOOD. S TC NR SA3432NM. 2 L 7 2 4F RT A16WE 1998022600333 19980226 00333 NM 1998 2 26 AWXA9800061 1 19980205 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 329 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING SCHEDULED C-12 INSPECTION, FOUND CRACK INDICATION AT FWD GALLEY DOORWAY LOWER AFT CORNER, BS 329, WL 209, BETWEEN STR 17 AND 18. REPAIRED FWD GALLEY DOORWAY LOWER AFT CORNER CRACKED CONDITION PER SRM 53-10-01. 2 L 7 2 4F RT A16WE 1998022600334 19980226 00334 NM 1998 2 26 AWXA9800062 1 19980204 A 5320 6517688U180 SILL BOEING 737 7373G7 1384595 NM BS 307-353 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING SCHEDULED C-12 INSPECTION, FOUND NUMEROUS SPOTS OF CORROSION ON FWD ENTRY DOOR MOPSILL (CREASE BEAM) BS 307 TO 35 3. REMOVED AND REPLACED MOPSILL (CREASE BEAM) FROM BS 307 TO BS 353, WL 208, LBL 55 PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1998022600335 19980226 00335 NM 1998 2 26 AWXA9800063 1 19980204 A 5313 BAC1498137 STRINGER BOEING 737 7373G7 1384595 NM BS 350/360 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING SCHEDULED C-12 INSPECTION, FOUND CRACK IN STRINGER 14L AT BS 360 AND 350. REPAIRED PER SRM 51-70-13, 51-10-02 AN D 51-40-02. 2 L 7 2 4F RT A16WE 1998022600336 19980226 00336 NM 1998 2 26 AWXA9800064 1 19980129 A 5347 BAC1520841 SEAT TRACK BOEING 737 7373G7 1384595 NM BS 701-727 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING SCHEDULED C-12 INSPECTION, FOUND CORROSION ON SEAT TRACK BS 727, RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM 701 TO 727 + 9 PER SRM 53-00-52. 2 L 7 2 4F RT A16WE 1998022600337 19980226 00337 NM 1998 2 26 AWXA9800065 1 19980205 A 5320 65458076 FRAME BOEING 737 7373G7 1384595 NM GALLEY DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING SCHEDULED C-12 INSPECTION, FOUND INDICATION OF A CRACK AT FWD GALLEY DOOR FWD FUSELAGE FRAME AT NR 1 STOP PAD FIT TING. REMOVED AND REPLACED FRAME STUB PER SRM 51-40-02, 51-20-05 AND 51-03-01. 2 L 7 2 4F RT A16WE 1998022600338 19980226 00338 NM 1998 2 26 AWXA9800066 1 19980205 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 520 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 158AW 23780 DURING SCHEDULED C-12 INSPECTION, FOUND DAMAGED EXTERNAL SKIN AROUND GROUND AIR SERVICE DOOR (2 AREAS MARKED) BL 0, BS 5 20, WL 148.5. REPAIRED PER ER 3-53-33-21. 2 L 7 2 4F RT A16WE 1998022600339 19980226 00339 WP 1998 2 26 CALA9800281 1 19980221 A 2910 7936907665 HYD LINE DOUG DC9 DC982 3022082 WP RT HYD SYST BROKEN A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 77827 49487 THE RT HYDRAULIC SYSTEM PRESSURE AND QUANTITY WERE LOST ON APPROACH. APPROPRIATE CHECKLISTS WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE TO RUDDER CONTROL VALVE BROKEN. THE HY DRAULIC LINE WAS REMOVED AND REPLACED PER MM 29-10-5. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998022600340 19980226 00340 WP 1998 2 26 9802949941 1 19980220 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 566 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CRACK IN LONGERON 27L END FITTING AT FS 455. REPLACED END FITTING PER DWG 5911412 AND SRM 53-02. 2 L 7 2 4F A6WE 1998022600341 19980226 00341 WP 1998 2 26 9802959941 1 19980220 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 567 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CRACK IN LONGERON 28R END FITTING AT FS 567. REPLACED END FITTING PER DWG 5911412 AND SRM 53-02. 2 L 7 2 4F A6WE 1998022600342 19980226 00342 NM 1998 2 26 9802962202 1 19980115 A 5314 KEEL BEAM BOEING 727 727251 138408H NM BS 970-1000 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 202US 22155 DURING M-CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF LEFT KEEL BEAM, FS 970 TO 1000. REPAIRED PER EA 22-153291. 2 L 7 3 4F A3WE 1998022600343 19980226 00343 NM 1998 2 26 9802972202 1 19980109 A 5314 KEEL BEAM BOEING 727 727251 138408H NM BS 950-970 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 202US 22155 DURING M-CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF RIGHT KEEL BEAM FS 950 TO 970, RBL 7, WL 143. REPAIRED PER EA 22- 154475. 2 L 7 3 4F A3WE 1998022600344 19980226 00344 EU 1998 2 26 9802983241 1 19980120 A 5320 SILL AIRBUS 320 A320212 EU PAX DOORWAY CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 341NW 380 DURING PERIODIC CHECK, FOUND CORROSION AT THE LEFT AFT PASSENGER DOOR SILL PLATE. REPAIRED PER EA 32-154912. 2 L 7 2 4F RT A28NM 1998022600345 19980226 00345 NM 1998 2 26 9802996613 1 19980129 A 5313 LONGERON BOEING 747 747251B 1384892 NM BS 1740 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING PERIODIC CHECK, FOUND CRACK IN STR 42L AT FS 1740. REPAIRED PER EA 66-155129. 2 L 7 4 4F A20WE 1998022600346 19980226 00346 WP 1998 2 26 9803009941 1 19980206 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CRACK IN FRAME AT FS 83 RIGHT SIDE OF CENTER WINDSHIELD LOWER CORNER. REPAIRED PER EA 99-151733. 2 L 7 2 4F A6WE 1998022600347 19980226 00347 WP 1998 2 26 9803019957 1 19980203 A 5320 PAN DOUG DC9 DC931 3022065 WP BS 680 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CRACK IN WINDOW RING PAN, LEFT SIDE FS 680. REPAIRED PER EA 99-154172. 2 L 7 2 4F A6WE 1998022600348 19980226 00348 WP 1998 2 26 9803029957 1 19980204 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 69 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND A CRACK IN THE UPPER COCKPIT FORWARD BEAM SUPPORT FITTING FS 69, RBL 10. REPAIRED PER EA 99-15417 4. 2 L 7 2 4F A6WE 1998022600349 19980226 00349 WP 1998 2 26 9803039957 1 19980206 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 256 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND A CRACK IN J-ANGLE OF FRAME 256 AT LONGERON 22R. REPAIRED PER EA 99-154937. 2 L 7 2 4F A6WE 1998022600350 19980226 00350 WP 1998 2 26 9803049957 1 19980202 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP BS 604 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CORROSION ON DOUBLER AT UNDERWING PRESSURE BULKHEAD FS 604. REPAIRED PER EA 99-110241. 2 L 7 2 4F A6WE 1998022600351 19980226 00351 WP 1998 2 26 9803051148 1 19980207 A 5320 PRESSURE PANEL DOUG DC10 DC1040 3023508 WP FUS 1368 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 148US 46757 DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD IN THE CENTER WHEEL WELL AT FS 1368. REPAIRED PER E A 11-154567. 2 L 7 3 4F A22WE 1998022600352 19980226 00352 WP 1998 2 26 9803061148 1 19980129 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1099 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 148US 46757 DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 48R AT FS 1099. REPAIRED PER EA 11-155274. 2 L 7 3 4F A22WE 1998022600353 19980226 00353 WP 1998 2 26 9803079941 1 19980213 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 680 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CRACK IN END FITTING FOR LONGERON 29R AT FS 680. REPLACED FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998022600354 19980226 00354 WP 1998 2 26 9803089941 1 19980206 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CORROSION ON END FITTING FOR LONGERON 21L AT FS 996. REPLACED FITTING (P/N 4914957-1) PER SRM 51- 30-1. 2 L 7 2 4F A6WE 1998022600355 19980226 00355 WP 1998 2 26 9803099952 1 19980212 A 5280 FITTING DOUG DC9 DC931 3022065 WP LT MLG DOOR CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING L-CHECK, FOUND A CRACK IN THE ATTACH FITTING FOR THE LEFT MAIN LANDING GEAR DOOR RETRACT CYLINDER AT THE KEEL. R EPLACED FITTING PER SRM 51-30. 2 L 7 2 4F A6WE 1998022600356 19980226 00356 NE 1998 2 26 9802903241 2 19980216 A 7200 3017855020 ENGINE AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A3 NE NR 1 FAILED A A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 341NW 17208 17208 380 731709 DURING CRUISE FLIGHT, NR 1 ENGINE FUEL FILTER CLOG ECAM ANNUNCIATED. FLIGHT CREW DIVERTED AIRCRAFT TO MEM. NR 1 ENGINE SHUT DOWN 20 MILES FROM MEM. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND THE FUEL FILTER CONTAMINATED WITH BRONZE PARTICLES AND THE LPT CASE HAD AN AREA OF BURN THRU AT THE 11:00 POSITION. REPLACED THE NR 1 ENGINE. AIRCRAFT TO BE FERRIED TO DLH FOR FURTHER INSPECITON. 2 L 7 2 4F 4 F RT A28NM E29NE 1998022600357 19980226 00357 WP 1998 2 26 9803109860 1 19980220 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 769NC 47757 DURING LINE CHECK, FOUND FORWARD EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHEC K OK. 2 L 7 2 4F RT A6WE 1998022600358 19980226 00358 WP 1998 2 26 9803119952 1 19980222 A 5210 MECHANISM DOUG DC9 DC931 3022065 WP CABIN DOOR OUT OF ADJUST A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 916RW 47144 MAIN CABIN DOOR COULD NOT BE OPENED USING THE EXTERIOR HANDLE. MAINTENANCE INSTALLED NEW SNUBBER AND RIGGED DOOR PER AM M 52-11-00, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998022600359 19980226 00359 NM 1998 2 26 9803126635 1 19980219 A 2410 705117A CSD BOEING 747 747227B 1384888 NM NR 1 ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 GL 01 635US 50364 11329 21682 DURING CRUISE, THE NR 1 ENGINE CONSTANT SPEED DRIVE OIL PRESSURE LIGHT ILLUMINATED. SHUT DOWN NR 1 ENGINE DUE TO AN UNS UCCESSFUL ATTEMPT TO DISCONNECT THE CONSTANT SPEED DRIVE. AIRCRAFT DIVERTED TO MNL AND LANDED WITHOUT INCIDENT. REPLAC ED THE NR 1 ENGINE CONSTANT SPEED DRIVE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998022600360 19980226 00360 NE 1998 2 26 9803131144 2 19980222 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE STALLED A NWAA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 GL 01 144JC 46753 686120 DURING CRUISE AT FL370, THE NR 2 ENGINE COMPRESSOR STALLED, EGT ROSE TO 940C AND THE ENGINE WAS SHUT DOWN. A RESTART AT TEMPT AT FL330 WAS SUCCESSFUL AND THE ENGINE OPERATION WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTE D THE ENGINE PER TAFT 71-00-00, PGS 126-127 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. THE EXACT PAR T CAUSING DIFFICULTY TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998022600361 19980226 00361 NM 1998 2 26 9803146716 1 19980218 A 8012 START VALVE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 616US 21120 62664 DURING CLIMB, THE NR 3 START VALVE LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO NRT. MAINT ENANCE CHANGED THE START VALVE AND THE START PRESSURE SWITCH. ALL INDICATIONS WERE NORMAL AND THE AIRCRAFT RETURNED TO SERVICE. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998022600362 19980226 00362 NE 1998 2 26 9803156614 2 19980214 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 614US 20359 662629 AFTER LANDING AND JUST AFTER STOWING THE THRUST REVERSERS, THE CREW NOTED THE LOW OIL PRESSURE WARNING LIGHT ON AND EGT INDICATION ABOVE REDLINE FOR THE NR 4 ENGINE. THE ENGINE WAS SHUT DOWN AFTER REACHING A MAX EGT OF 1132C FOR 73 SECONDS . MAINTENANCE REPLACED THE ENGINE FOR OVERTEMP. EXACT PART CAUSING THE COMPRESSOR STALL TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998022600363 19980226 00363 NE 1998 2 26 9803166611 2 19980218 A 7321 7590001 FUEL CONTROL BOEING 747 747251B 1384892 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 611US 70850 4983 20356 662730 ON TAKEOFF ROLL, THE NR 4 ENGINE WOULD NOT PRODUCE TAKEOFF EPR WITH THE THRUST LEVER AT THE MECHANICAL STOP. THE TAKEOF F WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL CONTROL AND THE FOLLOW-UP ENGINE RUN WAS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1998022600364 19980226 00364 NE 1998 2 26 COMA9810046 2 19980219 A 7261 310770101 BREATHER EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE DAMAGED A COMA O OTHER K FLUID LOSS CR CRUISE 1 SO 01 249CA 1 120230 LEFT ENGINE OIL PRESSURE FELL TO 50 PSI DURING FLIGHT. FOUND EXCESSIVE OIL LEAKAGE FROM ENGINE BREATHER SEAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1998022600365 19980226 00365 EA 1998 2 26 COMA9860045 1 19980221 A 2752 853D1009 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 965CA 3798 7131 AFTER LIFT OFF, 7 UNITS OF ROLL TRIM NEEDED TO REMAIN LEVEL. FLAPS FAILED DURING RETRACTION. THE LEFT OUTBOARD FLAP, I NBOARD ACTUATOR FAILED CAUSING STRUCTURAL DAMAGE AND DEFORMATION OF THE FLAP ASSY. REPLACED ACTUATOR AND FLAP ASSY. 2 L 7 2 4F RT A21EA 1998022600366 19980226 00366 EA 1998 2 26 COMA9860046 1 19980219 A 2750 7804011 CONTROL LEVER CNDAIR CL600 CL6002B19 EA INST PANEL MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 915CA 6196 249 7013 FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE FLAP CONTROL HANDLE. 2 L 7 2 4F RT A21EA 1998022600367 19980226 00367 NM 1998 2 26 SWAA980118 1 19980202 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 915-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 24SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED STR 4L BS 915 TO 947. REPAIRED PER SWA ACO 6717- 53. 2 L 7 2 4F A16WE 1998022600368 19980226 00368 1998 2 26 SWAA980119 4 19980202 A 3423 1784460655 COMPASS BOEING 737 7372H4 138448C NM NR 2 INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 SW 07 24SW 21535 AFTER TAKEOFF, NR 2 COMPASS BECAME INOP. RETURNED TO DALLAS AND MADE AN UNEVENTFUL LANDING. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998022600369 19980226 00369 NM 1998 2 26 SWAA980120 1 19980202 A 3350 LAMPS BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 54SW 21535 DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS EMERG EXIT SIDE LIGHT LAMPS INOP. REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998022600370 19980226 00370 NM 1998 2 26 SWAA980121 1 19980131 A 2130 655281025 RELAY BOEING 737 7372H4 138448C NM E/E COMPT INOP A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 AFTER TAKEOFF, UNABLE TO PRESSURIZE THE AIRCRAFT IN AUTO, STANDBY OR MANUAL MODES. REPLACED A/C RELAY UNIT PER BOEING M M. 2 L 7 2 4F A16WE 1998022600371 19980226 00371 NM 1998 2 26 SWAA980122 1 19980211 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 996 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 996, UNDER STR 20L APPROX 2.5 IN LENGTH. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1998022600372 19980226 00372 NM 1998 2 26 SWAA980123 1 19980216 A 2121 65771 COOLING FAN BOEING 737 7372H4 138448C NM CABIN SMOKING A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 68SW 22357 AFTER TAKEOFF, CREW REPORTED A ELECTRICAL SMELL OF HOT PLASTIC AT FL280 TURNED LEFT PACK COLDER AND GASPER FAN ON. SMOK E APPARENT IN FRONT HALF OF CABIN. REMOVED AND REPLACED NR 1 EQUIPMENT COOLING FAN PER BOEING MM. 2 L 7 2 4F A16WE 1998022600373 19980226 00373 NM 1998 2 26 SWAA980124 1 19980120 A 2150 26110114 PRECOOLER BOEING 737 7372H4 138448C NM NR 1 ENGINE FLICKERED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 AFTER TAKEOFF, NR 1 ENGINE OVHT LIGHT FLICKERED ON AND OFF DURING CLIMBOUT. IT PROGRESSED TO STEADY ON. EXTINGUISHED W HEN NR 1 ENG THROTTLE RETARDED TO IDLE THRUST. ALL OTHER ENGINE INDICATIONS WERE NORMAL. REMOVED AND REPLACED PRECOOL ER ON NR 1 ENG PER BOEING MM. 2 L 7 2 4F A16WE 1998022600374 19980226 00374 NM 1998 2 26 SWAA980125 1 19980123 A 2913 887477 PUMP BOEING 737 7373H4 1384600 NM B-HYD SYS LEAKING A SWAA O OTHER J WARNING INDICATION IN INSP/MAINT 1 SW 07 637SW 27710 AFTER TAKEOFF, HYDRAULIC SYSTEM B-PUMP PRESSURE LIGHT ILLUM DURING FLT. REMOVED AND REPLACED B-SYS HYD PUMP AND FILTERS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998022600375 19980226 00375 NM 1998 2 26 SWAA980126 1 19980210 A 5320 ANGLE BOEING 737 7372H4 138448C NM FWD DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C3 CHECK, FOUND 1 CRACK IN ANGLE AT FWD LOWER CORNER OF DOOR FRAME. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998022600376 19980226 00376 NM 1998 2 26 SWAA980127 1 19980130 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE OUTER SKIN CRACKED AT LOWER HINGE RADIUS OF AFT SERVICE DOOR UNDER PRODUCTION LAP JOINT DOUBLER. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600377 19980226 00377 NM 1998 2 26 SWAA980128 1 19980129 A 5320 STRAP BOEING 737 7373T0 1384582 NM BS 328 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM STABILIZER STRAP DAMAGE AT BS 328, RBL 32, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600378 19980226 00378 NM 1998 2 26 SWAA980130 1 19980130 A 5330 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED C3 CHECK, FOUND A .156 INCH LONG CRACK IN FUSELAGE SKIN AT L2 DOOR AT UPPER HINGE CUTOUT. REPAIRED PER SWA RA 1-353-1764. 2 L 7 2 4F RT A16WE 1998022600379 19980226 00379 EU 1998 2 26 SWAA980131 2 19980130 A 7230 1590M2P01 FAN BLADES BOEING 737 7373Q8 1384670 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE BENT A SWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 695SW 23506 DURING TAKEOFF AT GEAR RETRACTION NOTICED LOUD AIR NOISE AND VIBRATION ON NR 1 ENGINE. RETURNED TO PVD AND MADE AN UNEV ENTFUL LANDING. INSPECTED ENG, FOUND THREE FAN BLADES BENT DUE TO BIRD STRIKE. REPLACED FAN SET OF BLADES PER BOEING M M. 2 L 7 2 4F 4 F RT A16WE E21EU 1998022600380 19980226 00380 NM 1998 2 26 SWAA980129 1 19980130 A 5320 BEAM BOEING 737 7373T0 1384582 NM BS 390 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 390 RBL 65 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600381 19980226 00381 NM 1998 2 26 UPS98225846 1 19980203 A 5347 BAC15201432 SEAT TRACK BOEING 727 72751C 1384015 NM BS 970-1110 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (44-53-12) IN SEAT TRACK WELL BS 970 TO 1110 RBL 25, WL 208 CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED NEW TRACK AND SPLICE PER 53-10-5, INSTALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998022600382 19980226 00382 NM 1998 2 26 UPS98225847 1 19980217 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 887 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CRACK AT STR 14 LT BS 887 LBL 70 WL 229. REPAIRED CRACKED STR 14 LT AT STA 887, LBL 70, WL 229 IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1998022600383 19980226 00383 NM 1998 2 26 UPS98225848 1 19980217 A 5755 CORE BOEING 727 72751C 1384015 NM NR 7 SPOILER CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, WATER ENTRAPMENT NOTED IN LT WING NR 7 SPOILER I/B END FROM LEADING EDGE AFT 12 INCHES (X-RAY FILM V IEW NR 8). FURTHER INVESTIGATION REQUIRED. REMOVED 24 X 9 OF LOWER SURFACE SKIN AND 5 X 11.8 DAMAGED CORE CLEANED, DRI ED AND REPAIRED IAW SRM 51-40-6. 2 L 7 3 4F A3WE 1998022600384 19980226 00384 NM 1998 2 26 UPS98225849 1 19980203 A 5313 6518420270 STRINGER BOEING 727 72751C 1384015 NM BS 352-358 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 23L BS 352 TO 358. CORROSION FOUND OUT OF LIMITS PER SRM 53-10- 1. REPLACED STRINGER WITH NEW ITEM PER SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998022600385 19980226 00385 NM 1998 2 26 UPS98225850 1 19980203 A 5320 651841713 STIFFENER BOEING 727 72751C 1384015 NM BS 301 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-111-01.05-01) ON STIFFENER OF NOSE WHEEL WELL TOP PANEL BS 301 LBL 7, RLB 12, WL 184. CORROSION OUT OF LIMITS PER SRM 51-10-6. REPLACED PART WITH NEW ITEM PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998022600386 19980226 00386 NM 1998 2 26 UPS98225851 1 19980218 A 5230 BEAM BOEING 727 72751C 1384015 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, FORWARD CARGO DOOR NR 3 BEAM IS CRACKED IN OUTBD RADIUS 12 INCHES AFT FROM FORWARD EDGE OF DOOR, 16 INCHES DOWN FROM TOP EDGE OF DOOR. REMOVED AND REPLACED DOOR IAW MM ON SEPARATE NRC NR 465118. 2 L 7 3 4F A3WE 1998022600387 19980226 00387 NM 1998 2 26 UPS98225852 1 19980218 A 5320 SUPPORT BOEING 727 72751C 1384015 NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION ON FLOOR SUPPORT BS 328 TO 344, LBL 29, WL 208. REMOVED AND REPLACED FLOOR SUPPORT IAW SR M 51-30-2. 2 L 7 3 4F A3WE 1998022600388 19980226 00388 NM 1998 2 26 UPS98225853 1 19980218 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 485 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CRACKED STRINGER 24 RT BS 485, WL 165, RBL 35. STOP DRILLED ENDS AT CRACK AND INSTALLED REPAIR DOUB LERS OVER DAMAGED SECTION IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1998022600389 19980226 00389 NM 1998 2 26 UPS98225854 1 19980218 A 5347 SEAT TRACK BOEING 727 72751C 1384015 NM BS 730 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, WHILE WORKING CUST ID 2-224-22B FOUND CORROSION ON SEAT TRACK INBD FLANGE STA 730, LBL 65, WL 208. R EMOVED DAMAGED SECTION OF SEAT TACK AND SPLICED IN NEW SECTION IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998022600390 19980226 00390 NM 1998 2 26 UPS98225855 1 19980218 A 5347 SEAT TRACK BOEING 727 72751C 1384015 NM BS 861 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION AROUND NUT PLATES BS 861, RBL 24, WL 208. REMOVED AND REPLACED SECTION OF SEAT TRACK AND EXPANSION LINK IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998022600391 19980226 00391 NM 1998 2 26 UPS98225856 1 19980220 A 5754 RIB BOEING 727 72751C 1384015 NM NR 3 SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, WHILE WORKING CARD NR 465869 FOUND L/W NR 3 SLAT O/B TRACK O/B TRACK RIB CRACKED. INSTALLED NEW RIB AT O/B TRACK STATION PER 727 SRM 51-30-2. 2 L 7 3 4F A3WE 1998022600392 19980226 00392 NM 1998 2 26 UPS98225857 1 19980219 A 5744 653273415 FITTING BOEING 727 72751C 1384015 NM NR 1 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, NR 1 FLAP TRACK FWD FITTING IS CORRODED AROUND MOUNT HOLE. REPLACED FITTING PER SRM 51-10-1, NEW FI TTING SETUP AND MACHINED PER BOEING DRAWING 65-17357. 2 L 7 3 4F A3WE 1998022600393 19980226 00393 NM 1998 2 26 UPS98225858 1 19980219 A 5312 BULKHEAD SKIN BOEING 727 72751C 1384015 NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, BS 178 BULKHEAD IS CRACKED AROUND FASTENERS AT BS 10, WL 235. REMOVED DAMAGED AREA .5 X 3 ENCOMPASS ING 3 CRACKS. REPAIRED BS 178 AT LBL 10, WL 235, PER 727 SRM 53-10-9 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998022600394 19980226 00394 NM 1998 2 26 UPS98225859 1 19980219 A 5347 SEAT TRACK BOEING 727 72751C 1384015 NM BS 675-680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION ON CARGO TRACK IN WELL OF TRACK AT BS 675 TO 680, WL 155, RBL 15. REMOVED DAMAGED SECTION OF CARGO TRACK, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998022600395 19980226 00395 NM 1998 2 26 UPS98225860 1 19980219 A 5313 6534144109 BEAM BOEING 727 72751C 1384015 NM BS 765-825 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION ON LONGITUDINAL BEAM LBL 25, WL 208, BS 765 TO 825. REMOVED AND REPLACED UPPER CHORD OF L ONGITUDINAL BEAM IAW SRM 51-30-2, 51-20-1, 51-30-5. 2 L 7 3 4F A3WE 1998022600396 19980226 00396 NM 1998 2 26 UPS98225861 1 19980216 A 5754 65217505A BULLNOSE BOEING 727 72751C 1384015 NM NR 2 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, L/W NR 2 K-FLAP BULLNOSE I/B MOUNT LUG CORRODED AROUND I/B FASTENER. REMOVED CORRODED BULLNOSE, COR ROSION OUT OF LIMITS, INSTALLED SERVICABLE BULLNOSE IAW MM 27-81-01. 2 L 7 3 4F A3WE 1998022600397 19980226 00397 NM 1998 2 26 UPS98225870 1 19980222 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, EMERGENCY ESCAPE EXIT LIGHT HAS GREEN LIGHTS FLASHING. PERFORMED EMERGENCY LIGHT TEST PER 33-50-00 P101 LIGHTS WENT OUT, OPS CK NML. 2 L 7 3 4F A3WE 1998022600398 19980226 00398 WP 1998 2 26 UPS98825840 1 19980206 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP RT AUX TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-C, RT WING L/E AUX TANK O/B END INTERNAL DOUBLER HAS A 6 INCH CRACK. REPAIRED CRACKED INTERNAL DOUBLER IAW EO DC-8 5720-7767. 2 L 7 4 4F RT 4A25 1998022600399 19980226 00399 WP 1998 2 26 UPS98825841 1 19980209 A 5720 56422051 FITTING DOUG DC8 DC873F 302199F WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-C, LT WING LWR AUX SPAR TO REAR SPAR TIE FITTING HAS HEAVY CORROSION. REMOVED FABRICATED AND INSTALLED REPLACEMENT FITTING IAW 8110-3 APPROVED DHC SK 866-507. 2 L 7 4 4F RT 4A25 1998022600400 19980226 00400 WP 1998 2 26 UPS98825842 1 19980211 A 5320 37540231N FITTING DOUG DC8 DC871F 302199D WP NR 1 CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, NR 1 PIT AFT LWR T-BOLT STOP FITTING IS CRACKED ON THE LWR LEG. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1998022600401 19980226 00401 WP 1998 2 26 UPS98825843 1 19980209 A 5210 5615403197 WEB DOUG DC8 DC871F 302199D WP L-1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, MAIN ENTRY DOOR LWR AFT WEB IS BENT AND CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT WEB IA W SRM 53-3-2. 2 L 7 4 4F RT 4A25 1998022600402 19980226 00402 WP 1998 2 26 UPS98825844 1 19980209 A 5210 FRAME DOUG DC8 DC871F 302199D WP L-1 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, MAIN ENTRY DOOR LWR FRAME HAS A CRACK AND DEEP GOUGE. REPAIRED CRACKED FRAME IAW SRM 52-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998022600403 19980226 00403 WP 1998 2 26 UPS98825845 1 19980208 A 5320 575083766 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 641 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, STA 641 BETWEEN STR 26R TO 27R, SHEAR TIE HAS A 2 INCH CRACK. REMOVED FABRICATED AND INSTALLED REPLA CEMENT SHEAR TIE IAW SRM 53-4-1 FIG 40 AND DWG 5750837. 2 L 7 4 4F RT 4A25 1998022600404 19980226 00404 WP 1998 2 26 UPS98825862 1 19980209 A 5320 5649028 DOUBLER DOUG DC8 DC871F 302199D WP BS 35-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, INTERNAL DOUBLER HAS HEAVY CORROSION O/B OF LONGERON 30R BETWEEN FS 35 TO 55. REMOVED, FABRICATED, A ND INSTALLED REPLACEMENT DOUBLER IAW DWG 5649028 AND SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998022600405 19980226 00405 WP 1998 2 26 MWEA98178 1 19980220 A 5210 9955752 BEAM DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 NR 1 HORIZONTAL BEAM OF THE MAIN CABIN ENTRANCE DOOR WAS FOUND CRACKED AT THE FORWARD AND AFT ENDS. INSTALLED NEW BEAM IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600406 19980226 00406 WP 1998 2 26 MWEA98179 1 19980220 A 5210 5934796 FITTING DOUG DC9 DC932 3022066 WP PAX DOOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 MAIN CABIN DOOR THE END FITTING ON THE FORWARD END OF BEAM NR 3 WAS FOUND EXFOLIATED. INSTALLED NEW FITTING IAW SRM 51- 30. 2 L 7 2 4F A6WE 1998022600407 19980226 00407 WP 1998 2 26 MWEA98180 1 19980220 A 5210 5934796 FITTING DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 MAIN CABIN DOOR THE NR 1 BEAM AFT SUPPORT FITTING WAS FOUND CRACKED. INSTALLED NEW FITTING IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600408 19980226 00408 WP 1998 2 26 MWEA98181 1 19980220 A 5210 WEB DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 A CRACK WAS FOUND ON THE INTERIOR WEB IN THE AFT UPPER CORNER OF MAIN CABIN DOOR. FABRICATED REPAIR DOUBLER IAW SRM 52- 00 AND 52-11. 2 L 7 2 4F A6WE 1998022600409 19980226 00409 WP 1998 2 26 MWEA98182 1 19980220 A 5210 5914171 PAN DOUG DC9 DC932 3022066 WP PAX DOOR CRACK A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 MAIN CABIN DOOR A CRACK WAS FOUND ON THE UPPER FORWARD SECTION OF PAN ABOVE STOP F1. INSTALLED NEW PAN SECTION IAW SRM 51-30 AND 52-05. 2 L 7 2 4F A6WE 1998022600410 19980226 00410 WP 1998 2 26 MWEA98183 1 19980220 A 5522 5910412 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 212ME 47701 PREVIOUS REPAIR WAS NOTED ON THE LT ELEVATOR BETWEEN NOSE RIBS 8 AND 9 FROM OUTBOARD TIP REPAIR NOT IAW SRM. FABRICATED REPAIR DOUBLER IAW SRM 55-02. 2 L 7 2 4F A6WE 1998022600411 19980226 00411 WP 1998 2 26 MWEA98184 1 19980220 A 5312 991558 BULKHEAD CLIPS DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 WEB ATTACHED TO THE RADIAL STIFFENER ON THE APB WAS FOUND CRACKED ON THE OUTBOARD END. INSTALLED REPAIR CLIPS IAW SRM 5 1-30 AND DRAWING J060110. 2 L 7 2 4F A6WE 1998022600412 19980226 00412 WP 1998 2 26 MWEA98185 1 19980220 A 5311 99122439 FRAME DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE FRAME AT FS 965 WAS FOUND CRACKED AT THE INTERSECTION OF THE FORWARD LOWER PYLON SPAR. FABRICATED REPAIR PARTS IAW SRM 53-03 FIG 13. 2 L 7 2 4F A6WE 1998022600413 19980226 00413 NM 1998 2 26 MWEA98186 1 19980218 A 2560 11320 GIRT BAR DOUG MD88 MD88 3023688 NM SERVICE DOOR OUT OF POSITION A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 601ME 49762 AFT GALLEY SERVICE DOOR GIRT BAR IS VERY DIFFICULT TO DISARM. REPOSITIONED FABRIC ON GIRT BAR. 2 L 7 2 4F RT A6WE 1998022600414 19980226 00414 1998 2 26 MWEA98187 4 19980218 A 2565 D29985107 SLIDE DOUG MD88 MD88 3023688 NM AFT GALLEY INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 DUE TO SEVERAL WRITEUPS ON THE AFT GALLEY SLIDE GIRT BAR DIFFICULT TO ARM/DISARM. REPLACED AFT GALLEY SLIDE. 2 L 7 2 4F RT A6WE 1998022600415 19980226 00415 WP 1998 2 26 MWEA98188 1 19980219 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 69-101 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 TRUCK RAN INTO AIRCRAFT CAUSING DAMAGE TO RIGHT FWD AREA OF AIRCRAFT. MTC REPAIRED IAW SRM 53-01 FIG 2 SHEET 4 AND REMO VED AND REPLACED SKIN FROM STATION 69-101 IAW SRM 53-01 FIG 2 SHEET 3. 2 L 7 2 4F A6WE 1998022600416 19980226 00416 WP 1998 2 26 MWEA98189 1 19980219 A 5755 SHIM DOUG DC9 DC914 3022034 WP LT SPOILER CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND POPPED RIVET HEAD ON TOP OF LT FWD OF I/B SPOILER CTR HINGE. REMOVED AND REPLACED CORRODED SHIM. 2 L 7 2 4F A6WE 1998022600417 19980226 00417 WP 1998 2 26 MWEA98190 1 19980218 A 5730 SKIN DOUG DC9 DC932 3022066 WP LEFT WING PEELING A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 DURING INSPECTION, FOUND THE LT WING OUTBOARD TRAILING EDGE PANEL TOP SKIN PEELING BACK. MTC REPLACED SKIN IAW EA NR 57 -006. 2 L 7 2 4F A6WE 1998022600418 19980226 00418 WP 1998 2 26 MWEA98191 1 19980220 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 INSPECTION FOUND CORROSION UNDER THE LEFT WING FINGER DOUBLERS ON LOWER SKIN INSIDE TRAILING EDGE PANEL. REPLACED SKIN IAW EA NR 57-006. 2 L 7 2 4F A6WE 1998022600419 19980226 00419 NM 1998 2 26 DL72S980406 1 19980219 A 5754 65162222 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 NR 6 SLAT RIB CRACKED. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998022600420 19980226 00420 1998 2 26 DLM88980412 4 19980219 A 3417 ADC 347003175 DOUG MD88 MD88 3023688 NM E/E COMPT MALFUNCTIONED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 906DL 7004 49537 ON APP GPWS WARNING OF MODE 4A TOO LOW GEAR TOO LOW TERRAIN GEAR WAS DOWN FLAPS AT 40 DEG. GO-AROUND WAS ACCOMPLISHED AND GPWS CMPTR C/B PULLED. REPLACED R2-1 RELAY, REPLACED GPWS CMPTR, TESTS OK. REPLACED ADC CMPTR DUE TO HISTORY. PER FORMED CK OUT PER M/M 34-45-00 PARA F MODE 4, TESTS OK. 2 L 7 2 4F RT A6WE 1998022600421 19980226 00421 NM 1998 2 26 DL767980413 1 19980219 A 3350 LIGHT BOEING 767 767232 1385132 NM CARGO COMPT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 112DL 22224 ON L/O, FOUND ONE LT AND ONE RT EMERGENCY LIGHTS INOP AFT OF CARGO DOORS ON FUSELAGE. 2 L 7 2 4F RT A1NM 1998022600422 19980226 00422 WP 1998 2 26 DLL17980414 1 19980219 A 3350 LIGHT 3506892 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 769DL 193H1218 THE 25B EMERGENCY TRACK LIGHT INOP. FOUND SOCKET BAD, REPLACED SAME. 2 L 7 3 4F A23WE 1998022600423 19980226 00423 NM 1998 2 26 DL72K980415 1 19980209 A 2782 BRACKET BOEING 727 727232 1384082 NM RT LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 BRACKETS CRACKED RT WING L/E ATTACH BRACKETS FOR THE NR 5 KRUEGER FLAP ACTUATOR ARE CRACKED, O/B BRACKET LOWER CORNER AN D I/B BRACKET UPPER CORNER. STOP DRILLED CRACKS. STOP DRILLS OK. OK TO INSTALL REPAIRS PREVIOUS REPAIR PER MM 57-20-21 FIG 807 ALREADY EXISTS. FABRICATED REPAIR DOUBLER PER MM 57-20-21 FIG 807. REPLACED O/B BRACKET PER SRM 51-00. REMOV ED AND REINSTALLED NR 5 KRUEGER FLAP ACTUATOR, REPLACED PER M/M 57-20-21 CONT NR 944. 2 L 7 3 4F A3WE 1998022600424 19980226 00424 WP 1998 2 26 DLL13980416 1 19980215 A 3350 61020 BATTERY LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 EMERGENCY FLASHLIGHT INOP AT 2L. REPLACED BATTERY. 2 L 7 3 4F A23WE 1998022600425 19980226 00425 NM 1998 2 26 DL767980419 1 19980220 A 5754 WEDGE BOEING 767 767232 1385132 NM NR 4 LE SLAT DELAMINATION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 102DA 22214 THE UPPER SKIN OF THE LT WING NR 4 SLAT TRAILING EDGE WEDGE WAS FOUND WITH 2 AREAS 2 INCH DIAMETER DELAMINATIONS. THE T HE DAMAGE WAS REPAIRED PER THE B767 SRM AND DOCUMENTED PER ER/A 364074-14AD. 2 L 7 2 4F RT A1NM 1998022600426 19980226 00426 NM 1998 2 26 DL767980420 1 19980218 A 5754 WEDGE BOEING 767 767232 1385132 NM NR 5 LE SLAT DELAMINATION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 113DA 22225 THE UPPER SKIN OF THE LT WING NR 5 SLAT WAS FOUND WITH A 1 INCH DIAMETER AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364049-14AD. 2 L 7 2 4F RT A1NM 1998022600427 19980226 00427 NM 1998 2 26 DL767980421 1 19980218 A 5754 WEDGE BOEING 767 767232 1385132 NM NR 8 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 113DA 22225 THE UPPER SKIN OF THE RT WING NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 4 X 2.5 AREA OF DELAMINATION. THE DAMAGE W AS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364048-14AD. 2 L 7 2 4F RT A1NM 1998022600428 19980226 00428 NM 1998 2 26 DL72K980423 1 19980211 A 5412 SEAL RING BOEING 727 727232 1384082 NM NR 2 ENGINE COWL WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 MV-2, FOUND NR 2 ENG FIREWALL COWLING SEAL RING 9 O'CLOCK POSITION WORN THRU. REMOVED DAMAGE PER MM 53-11-00 PG 801, FA BD REPAIR INSTALLED PER AND PAINTED. 2 L 7 3 4F A3WE 1998022600429 19980226 00429 NM 1998 2 26 DL72K980424 1 19980220 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 913 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 STA 913 RT ANGLE IS CRACKED MLG W/W O/B SIDE ABOVE SHELF ANGLE. REPAIRED PER MM 53-11-0 P 834. 2 L 7 3 4F A3WE 1998022600430 19980226 00430 NM 1998 2 26 DL72K980425 1 19980220 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 NR 8 SLAT I/B AND O/B ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-20-21 P 812. 2 L 7 3 4F A3WE 1998022600431 19980226 00431 NM 1998 2 26 DL72K980426 1 19980220 A 5532 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 FOUND DURING B-2 LETTER CHECK, 2 EA .75 INCH CRACKS IN VERTICAL STAB RT SKIN AT BASE FS 1342 STAB STR 10. REPAIRED PER M/M 55-30-0. 2 L 7 3 4F A3WE 1998022600432 19980226 00432 NM 1998 2 26 DL72K980427 1 19980220 A 5320 WEB BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 481DA 20861 FOUND DURING B-2 LETTER CHECK, .5 INCH CRACK RT LWR TORQUE BOX TRANSVERSE WEB FS 1263 O/B OF NR 2 ENG FUEL SHROUD. REPA IRED PER SRM 53-10-10 FIG 4. 2 L 7 3 4F A3WE 1998022600433 19980226 00433 NM 1998 2 26 DL72K980431 1 19980220 A 3350 CHARGER 900542 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 410DA A1019 21222 ON L/O, FOUND FWD O/H EMERGENCY AISLE AND EXIT LIGHT INOP. FOUND CHARGER BAD. REPLACED CHARGER, CKS OK. 2 L 7 3 4F A3WE 1998022600434 19980226 00434 WP 1998 2 26 DLL10980434 1 19980221 A 3350 BATTERY PACK 5155741 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 722DA 54010 193C1147 R-4 EMERGENCY LIGHT BATTERY PACK FAILED TO HOLD CHARGE. REPLACED EMERGENCY BATTERY PACK. 2 L 7 3 4F A23WE 1998022600435 19980226 00435 1998 2 26 VNAA9802017 4 19980218 A 3440 701730011004 IAC DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 FAILED A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 460PS 4759 3061 DURING THE TAXI FOR TAKEOFF, THE FLIGHT MANAGEMENT SYSTEM WOULD NOT ALIGN WITH THE RUNWAY THAT WAS SELECTED. THE AIRCRA FT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 INTEGRATED AVIONICS COMPUTER IN ACCORDANCE WITH DO RNIER MAINTENANCE MANUAL 31-41-00. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998022600471 19980226 00471 NM 1998 2 26 VJ9800023 1 19980220 A 3350 CONNECTOR BOEING 737 737268 138448Q NM CABIN DIRTY A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 461AT 20976 AFT SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. CLEANED AND DRIED CONNECTIONS, OPS CHECKED NORMAL. 2 L 7 2 4F A16WE 1998022600472 19980226 00472 EU 1998 2 26 MALA976000 1 19980220 A 3350 LIGHT SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 107XJ 340A107 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT INOP AT 9C. MAINTENANCE RECYCLED POWER, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998022600473 19980226 00473 EU 1998 2 26 MALA976001 1 19980220 A 3020 ICE LIGHT SAAB SF340 340B 7860101 EU LT INTAKE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 595MA 340B216 DURING CLIMB, AFTER SELECTING FULL ICE, THE LEFT INTAKE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE RESET LOWER INLET DUCT CIRCUIT BREAKER IN LEFT NACELLE WHEEL WELL. INSPECTED INLETS, NO DEFECTS NOTED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998022600474 19980226 00474 EU 1998 2 26 MALA976002 1 19980221 A 3350 6104789 POWER PACK SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 115XJ 340A115 DURING INSPECTION, EMERGENCY LIGHTS INOP, MAIN BOARDING DOOR AND 2 EXIT COMPARTMENT LIGHTS. MAINTENANCE REPLACED CABIN EMERGENCY LIGHT POWER PACK, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600475 19980226 00475 EU 1998 2 26 MALA976003 1 19980221 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 423XJ 423 DURING INSPECTION, THE LOWER EMERGENCY EXIT LIGHT INOP AT 6A. MAINTENANCE RESECURED LOWER EXIT LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600476 19980226 00476 NE 1998 2 26 MALA976004 2 19980219 A 7510 6058T80P03 AISB VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT NACELLE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 76XJ 076 DURING CRUISE FLIGHT, THE RIGHT AIR VALVE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT ANTI-ICE START BLEED VALVE, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE6 1998022600477 19980226 00477 EU 1998 2 26 MALA976005 1 19980222 A 5720 ANGLE SAAB SF340 SF340A 7850100 EU WS 42 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 103XJ 340A103 DURING HEAVY CHECK, DISCOVERED CRACK IN SECONDARY SUPPORT ANGLE AT STA WS 42 ON BOTH LEFT AND RIGHT WING TRAILING EDGE. MAINTENANCE REMOVED 4 EACH FASTENERS AND PERFORMED EDDY CURRENT INSPECTIONS FOUND TO BE NO FURTHER DAMAGE TO SPAR CAP, WEB, RIB AND INTERNAL ANGLE. MAINTENANCE REAMED HOLES TO NEXT SIZE, INSPECTED AGAIN USING EDDY CURRENT AND REINSTALLED NEW FASTENERS AND SEALED. SAAB 340 STRUCTURAL REPAIR STATEMENT 72SDS0871. 2 L 7 2 4T RT A52EU 1998022600478 19980226 00478 EU 1998 2 26 MALA976006 1 19980221 A 3320 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING INSPECTION, SMOKE NOTED COMING FROM WINDOW SIDE LIGHT. REMOVED BULB AND SMOKE CEASED. WINDOW LIGHTING DEFERRED AS PER MEL 33-20-1C. 2 L 7 2 4T RT A52EU 1998022600479 19980226 00479 EU 1998 2 26 MALA976007 1 19980221 A 3350 60207 LAMP SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, LEFT FORWARD EMERGENCY EXIT LIGHT NEAR LEFT PASSENGER ENTRY DOOR FLOOR INOP. MAINTENANCE RELAMPED EM ERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998022600480 19980226 00480 NM 1998 2 26 MALA976008 1 19980219 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 865MA 364 DURING INSPECTION, EMERGENCY EXIT LIGHT INOP AT ROW 4A. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998022600481 19980226 00481 EU 1998 2 26 MALA976009 1 19980221 A 3350 LIGHT SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 68XJ 068 DURING INSPECTION, OVERHEAD EMERGENCY LIGHT 8CD INOP. MAINTENANCE DEFERRED LIGHT, IAW MEL 33-52-2C. 2 L 7 2 4T RT A52EU 1998022600482 19980226 00482 WP 1998 2 26 CALA9800282 1 19980221 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1811 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1811, STRINGER 47L. THE AREA WAS REPAIRED IAW SRM 51-10-00. 2 L 7 3 4F A22WE 1998022600483 19980226 00483 WP 1998 2 26 CALA9800283 1 19980221 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1561-1891 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON CORRODED AT STA 1561 TO 1891, LONGERON 52L. THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE LONGERON AND SPLICES WERE REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998022600484 19980226 00484 WP 1998 2 26 CALA9800284 1 19980221 A 5320 SHEAR TIE DOUG DC10 DC1010 3022110 WP BS 1810 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND SHEAR TIE CORRODED AT STA 1810, LONGERON 47 TO 48L. THE SHEAR TIE WAS REMOVED, AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-00 AND 51-30-0. 2 L 7 3 4F A22WE 1998022600485 19980226 00485 WP 1998 2 26 CALA9800285 1 19980221 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1815 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FRAME TO SKIN ATTACH ANGLE IN AFT BIN AT STA 1815 CORRODED BETWEEN LONGERON 44 AND 45L. THE ATTACH ANG LE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-00. 2 L 7 3 4F A22WE 1998022600486 19980226 00486 WP 1998 2 26 CALA9800286 1 19980221 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FRAME TO SKIN ATTACH ANGLES IN AFT BIN AT STA 1841 CORRODED FROM LONGERON 49L TO 45R. THE ATTACH ANGLE S WERE REMOVED AND REPLACED IAW SRM 51-21-01 AND 53-30-00. 2 L 7 3 4F A22WE 1998022600487 19980226 00487 WP 1998 2 26 CALA9800287 1 19980221 A 5347 TRACK DOUG DC10 DC1010 3022110 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND AFT CARGO COMPARTMENT LT SIDE TIE DOWN TRACK CORRODED FROM FRONT TO BACK AND DRAIN HOLE WAS FOUND CLOGG ED. A NEW TIE DOWN TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-00-01. 2 L 7 3 4F A22WE 1998022600488 19980226 00488 WP 1998 2 26 CALA9800288 1 19980221 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FRAME CIRCUMFERENTIAL BEAM CORRODED IN AFT BIN AT STA 1841, LONGERON 49L. THE OLD REPAIR WAS REMOVED A ND THE AREA WAS CLEANED. A NEW REPAIR WAS INSTALLED IAW SRM 53-30-0. 2 L 7 3 4F A22WE 1998022600489 19980226 00489 WP 1998 2 26 CALA9800289 1 19980221 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1721, LONGERON 52. THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE SPLI CE WAS REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998022600490 19980226 00490 WP 1998 2 26 CALA9800290 1 19980221 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1841-1871 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND STRINGER 48L CORRODED IN BULK CARGO COMPARTMENT AT STA 1841 TO 1871. THE STRINGER WAS REMOVED AND REPL ACED IAW SRM 53-10-0. 2 L 7 3 4F A22WE 1998022600491 19980226 00491 WP 1998 2 26 CALA9800291 1 19980221 A 5320 WEB DOUG DC10 DC1010 3022110 WP BS 595 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN LT WEB AT STA 595 BETWEEN LONGERONS 47 TO 48. FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-31-0. 2 L 7 3 4F A22WE 1998022600492 19980226 00492 WP 1998 2 26 CALA9800292 1 19980221 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1821 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND ANGLE BETWEEN FRAME AND SKIN IN AFT BAGGAGE COMPARTMENT CORRODED AT STA 1821, LONGERON 47L TO 48L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-0. 2 L 7 3 4F A22WE 1998022600493 19980226 00493 WP 1998 2 26 CALA9800293 1 19980221 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1805 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND ANGLE BETWEEN FRAME AND SKIN IN AFT BAGGAGE COMPARTMENT CORRODED AT STA 1805, LONGERON 47L TO 48L. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1998022600494 19980226 00494 WP 1998 2 26 CALA9800294 1 19980221 A 5400 SPAR WEB DOUG DC10 DC1010 3022110 WP NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 6 INCH CRACK IN NR 3 PYLON UPPER SPAR WEB AT STA YN 200. THE CRACK WAS STOP DRILLED, A DOUBLER WAS F ABRICATED AND INSTALLED IAW SRM 54-20-0. 2 L 7 3 4F A22WE 1998022600495 19980226 00495 WP 1998 2 26 CALA9800295 1 19980221 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND THREE CRACKS MEASURING .25 INCH TO .375 INCH LONG AT OUTBOARD SCREW AT UPPER TRAILING EDGE OF DROOP LEA DING EDGE SKIN OF LT WING. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-0. 2 L 7 3 4F A22WE 1998022600496 19980226 00496 WP 1998 2 26 CALA9800297 1 19980221 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1721-1741 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 47L SPLICE CORRODED IN MID CARGO AT STA 1721 TO 1741. FASTENERS WERE REMOVED IAW SRM 51-20-01 . THE CORRODED SECTION OF LONGERON WAS CUT OUT AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-00. 2 L 7 3 4F A22WE 1998022600497 19980226 00497 WP 1998 2 26 CALA9800298 1 19980222 A 5210 FITTING DOUG DC10 DC1010 3022110 WP L-1 DOOR BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND L-1 DOOR SIXTH STOP FITTING FROM BOTTOM BROKEN OFF AT AFT SIDE OF DOOR. THE STOP FITTING WAS REPLACED IAW MM 51-33-01. 2 L 7 3 4F A22WE 1998022600498 19980226 00498 WP 1998 2 26 CALA9800299 1 19980222 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1701-1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 1701 TO 1721, LONGERON 48L. THE FASTENERS WERE REMOVED IAW SRM 51-21-01 . THE CORRODED AREA WAS CUT OUT. A DOUBLER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND ECRA 5310-036 80. 2 L 7 3 4F A22WE 1998022600499 19980226 00499 WP 1998 2 26 CALA9800300 1 19980222 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1621-1670 ELONGATED HOLES A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND SEVERAL ELONGATED HOLES IN FUSELAGE SKIN FROM STA 1621 TO 1670, LONGERON 47 TO 48L. A REPAIR WAS INSTA LLED IAW SRM 53-21-0 AND 53-20-00. 2 L 7 3 4F A22WE 1998022600500 19980226 00500 WP 1998 2 26 CALA9800301 1 19980222 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1801 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FRAME TO FUSELAGE SKIN ATTACH ANGLE IN AFT CARGO COMPARTMENT CORRODED AT STA 1801, LONGERON 47-48L TO T HE ATTACH ANGLE. REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-0. 2 L 7 3 4F A22WE 1998022600501 19980226 00501 WP 1998 2 26 CALA9800302 1 19980223 A 5720 SUPPORT DOUG DC10 DC1010 3022110 WP LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND UPPER PANEL SUPPORT BEAM OF MLG FIXED SIDE BRACE CORRODED AT LT WING UPPER INBOARD TRAILING EDGE. THE AREA WAS REPAIRED IAW SRM 51-33-01. 2 L 7 3 4F A22WE 1998022600502 19980226 00502 WP 1998 2 26 CALA9800303 1 19980223 A 5320 WEB DOUG DC10 DC1030 3023501 WP BS 1841 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 INSPECTION FOUND PUNCTURES IN WEB PANEL AT STA 1841, LBL 38.5 TO 64. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-2 1-01 AND 53-00-01. 2 L 7 3 4F A22WE 1998022600503 19980226 00503 WP 1998 2 26 CALA9800304 1 19980223 A 5330 SKIN DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 INSPECTION FOUND FUSELAGE SKIN CRACKED AT LT AIR CONDITIONING BAY NR 1 DOOR AFT UPPER CORNER. THE CRACK WAS STOP DRILLE D IAW SRM 53-30-00. REPAIR DOUBLERS WERE FABRICATED AND INSTALLED 53-30-00, FIGURE 3, PAGE 19. 2 L 7 3 4F A22WE 1998022600504 19980226 00504 WP 1998 2 26 CALA9800305 1 19980223 A 5350 FITTING DOUG DC10 DC1030 3023501 WP TAIL CONE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 INSPECTION FOUND TAIL CONE RT LATCH HOOK FITTING WITH SUNK RIVETS AND A GOUGE JUST FORWARD OF INNER ACCESS DOOR ASSEMBLY AREA. THE DAMAGED AREA WAS REMOVED IAW SRM 51-31-01. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-52-01 AND 51-3 1-01. 2 L 7 3 4F A22WE 1998022600505 19980226 00505 WP 1998 2 26 CALA9800306 1 19980223 A 5753 SKIN DOUG DC10 DC1030 3023501 WP RT TE FLAP PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 INSPECTION FOUND A HOLE IN RT INBOARD FLAP LOWER SURFACE, FOUR INCHES FORWARD OF REAR SPAR. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-52-01, 51-30-00, AND 51-21-01. 2 L 7 3 4F A22WE 1998022600506 19980226 00506 WP 1998 2 26 CALA9800307 1 19980223 A 5753 ANGLE DOUG DC10 DC1030 3023501 WP LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 INSPECTION FOUND A 7 INCH CRACK IN ANGLE DOUBLER ON LT TRAILING EDGE FLAP HINGE PANEL 535JL. THE ANGLE DOUBLER WAS REMO VED. TWO DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 57-52-01 AND 51-30-01. 2 L 7 3 4F A22WE 1998022600507 19980226 00507 WP 1998 2 26 CALA9800308 1 19980223 A 5400 ANGLE DOUG DC10 DC1030 3023501 WP NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 INSPECTION FOUND A .25 INCH CRACK IN L-ANGLE ON TOP OF NR 3 PYLON AT AFT END OF HEAT EXCHANGER. THE ANGLE WAS REMOVED A ND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-01 AND 54-11-02. 2 L 7 3 4F A22WE 1998022600508 19980226 00508 WP 1998 2 26 CALA9800309 1 19980223 A 5230 ANGLE DOUG DC10 DC1030 3023501 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17087 47928 INSPECTION FOUND A 6 AND 4 INCH CRACK WITH CORROSION IN AFT CARGO DOOR FORWARD LOWER MOUNT ANGLE FOR GILL LINER. THE AN GLE WAS REMOVED AND REPLACEMENT PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-15-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998022600509 19980226 00509 NM 1998 2 26 SWAA980132 1 19980202 A 5330 SKIN BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER SWA RA 1-363 -11763. 2 L 7 2 4F RT A16WE 1998022600510 19980226 00510 NM 1998 2 26 SWAA980133 1 19980202 A 2121 6454051 FAN BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 617SW 27700 PRIOR TO ARRIVAL, CREW NOTICED ELECTRICAL TYPE FUMES IN GALLEY AREA. TURNED OFF GALLEY POWER, FUMES DISSIPATED. MADE A N UNEVENTFUL LANDING AT DTW. REMOVED AND REPLACED RECIRCULATION FAN, PER BOEING MM. 2 L 7 2 4F RT A16WE 1998022600511 19980226 00511 NM 1998 2 26 SWAA980134 1 19980202 A 3350 61228251 BATTERY PACK BOEING 737 7373T5 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED RON CHECK, FOUND FWD EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998022600512 19980226 00512 NM 1998 2 26 SWAA980135 1 19980202 A 5511 SUPPORT BOEING 737 7373T0 1384582 NM HORIZ STAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D-CHECK, FOUND RT STAB RIB AT STAB STA 129.5 HAD GOUGED L-ANGLE SUPPORT. REMOVED AND REPLACED RIB PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600513 19980226 00513 NM 1998 2 26 SWAA980136 1 19980203 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D-CHECK, FOUND CORROSION AT FLOORBEAM BS 986.5 RBL 22 TO 40 WL 208.1. REMOVED AND REPLACED UPPER CHORD AND SPLICE ANGLES PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600514 19980226 00514 NM 1998 2 26 SWAA980137 1 19980203 A 3350 BULB BOEING 737 7373T0 1384582 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D-CHECK, FOUND PSU EMERGENCY LIGHTS HAVE NUMEROUS INOP BULBS. RELAMPED LIGHTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998022600515 19980226 00515 NM 1998 2 26 SWAA980138 1 19980203 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 444 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED D-CHECK, FOUND DENT IN SKIN AT BS 444, STR 26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600516 19980226 00516 NM 1998 2 26 SWAA980139 1 19980204 A 5312 BULKHEAD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CRACKS ON BS 178 BULKHEAD AT WL 188, LBL 0.5 AND RBL 0.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600517 19980226 00517 NM 1998 2 26 SWAA980140 1 19980204 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 787 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND DENT IN FRAME BS 787, RBL 27, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600518 19980226 00518 NM 1998 2 26 SWAA980141 1 19980204 A 5320 TIE STRAP BOEING 737 7373A4 1384585 NM BS 774-858 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON PRIMARY SILL WEB TIE STRAP BS 774 TO 858, RBL 19, WL 164. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998022600519 19980226 00519 NM 1998 2 26 SWAA980142 1 19980204 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM HAS CORROSION AROUND NUT PLATE LOCATIONS, BS 727 TO 947, LBL 2.5, WL 158 . REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600520 19980226 00520 NM 1998 2 26 SWAA980143 1 19980204 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORROSION AROUND NUT PLATE LOCATIONS, BS 727 TO 947, RBL 7.5, WL 158. R EMOVED FLOORBEAM AND INSTALLED NEW FLOORBEAM PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600521 19980226 00521 NM 1998 2 26 SWAA980144 1 19980204 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 847-867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND VERTICAL SUPPORT WEB HAS CORROSION AT BS 847 TO 867, RBL 18.5, WL 163 IS OUT OF LIMITS. REMOVED AND REPLACED WEB PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600522 19980226 00522 NM 1998 2 26 SWAA980145 1 19980204 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 867 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND DENT IN FRAME AT BS 867, RBL 31, WL 168. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600523 19980226 00523 NM 1998 2 26 SWAA980146 1 19980205 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 209.75. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600524 19980226 00524 NM 1998 2 26 SWAA980147 1 19980205 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 767-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON VERTICAL SUPPORT WEB BS 767 TO 787, RBL 20, WL 156. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600525 19980226 00525 NM 1998 2 26 SWAA980148 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 827 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND DENT IN FRAME BS 827, LBL 28, WL 163. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600526 19980226 00526 NM 1998 2 26 SWAA980149 1 19980205 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 201.75 TO 202.75. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600527 19980226 00527 NM 1998 2 26 SWAA980150 1 19980205 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 4.7, WL 199 TO 199.75 AND WL 201.5 TO 202.25. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600528 19980226 00528 NM 1998 2 26 SWAA980151 1 19980205 A 5312 BULKHEAD WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, RBL 6.7, WL 202 TO 203. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600529 19980226 00529 NM 1998 2 26 SWAA980152 1 19980205 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 569 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND RT SKATE ANGLE CRACKED AT BS 569, RBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600530 19980226 00530 NM 1998 2 26 SWAA980153 1 19980205 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 294 AT STR 23 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600531 19980226 00531 NM 1998 2 26 SWAA980154 1 19980205 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 1106-1138 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND WEB WITH NUMEROUS DENTS AT BS 1106 TO 1138, RBL 15 TO RBL 30, WL 248. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600532 19980226 00532 NM 1998 2 26 SWAA980155 1 19980205 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 1106-1150 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND WEB WITH NUMEROUS DENTS AT BS 1106 TO 1150, LBL 15 TO 32, WL 248. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600533 19980226 00533 NM 1998 2 26 SWAA980156 1 19980205 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 802 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND SUB THRESHOLD SUPPORT WEB DENTED AT BS 802, RBL 20, WL 158. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998022600534 19980226 00534 NM 1998 2 26 SWAA980157 1 19980205 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION ON FUSELAGE SKIN AT BS 328, RBL 65, WL 211. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998022600535 19980226 00535 NM 1998 2 26 SWAA980158 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 480, BETWEEN STR 8 AND 9 RT. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600536 19980226 00536 NM 1998 2 26 SWAA980159 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 827, BETWEEN STR 8 AND 9 LT. REMO VED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600537 19980226 00537 NM 1998 2 26 SWAA980160 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME IS CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 827, BETWEEN STR 8 AND 9 RT. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600538 19980226 00538 NM 1998 2 26 SWAA980161 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 867, BETWEEN STR 8 AND 9L. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600539 19980226 00539 NM 1998 2 26 SWAA980162 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 887, BETWEEN STR 8 AND 9 LT. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600540 19980226 00540 NM 1998 2 26 SWAA980163 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 887, BETWEEN STR 8 AND 9R. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600541 19980226 00541 NM 1998 2 26 SWAA980164 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 908, BETWEEN STR 8 AND 9L. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600542 19980226 00542 NM 1998 2 26 SWAA980165 1 19980205 A 5320 STRAP BOEING 737 7373A4 1384585 NM BS 1016, 1014 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT STRAP AT BS 1016, 1014 AND 1006 LBL 2.5 AND 7.5, WL 208. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600543 19980226 00543 NM 1998 2 26 SWAA980166 1 19980205 A 5320 BEAM BOEING 737 7373A4 1384585 NM BS 701/703 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 701 AND 703, RBL 70, WL 208. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600544 19980226 00544 NM 1998 2 26 SWAA980167 1 19980205 A 5320 BEAM BOEING 737 7373A4 1384585 NM BS 668 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON O/B CREASE BEAM CHORD AT BS 668, LBL 70, WL 209. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600545 19980226 00545 NM 1998 2 26 SWAA980168 1 19980205 A 5320 BEAM BOEING 737 7373A4 1384585 NM BS 699 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 699, LBL 70, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998022600546 19980226 00546 NM 1998 2 26 SWAA980169 1 19980205 A 5320 BEAM BOEING 737 7373A4 1384585 NM BS 794.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 794.5, RBL 67, WL 208. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998022600547 19980226 00547 NM 1998 2 26 QXEA9800077 1 19980219 A 2150 78279012 ACM DHAV DHC8 DHC8202 2809007 NM AFT FUSELAGE FOD A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 346PH 477 AIRCRAFT MAINTENANCE PERSONNEL REPORT A STRONG SMELL COMING FROM BLEED AIR UNIT WITH NOISE COMING FROM CARGO BAY AREA. R EPLACED AIR CYCLE MACHINE AND CONDENSOR/MIXER, OPERATIONAL TESTS GOOD. 2 H 7 2 4T RT A13NM 1998022600548 19980226 00548 NM 1998 2 26 QXEA9800078 1 19980219 A 3350 6038443 BATTERY PACK GRIMES DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 350PH 488 LEFT REAR EXTERIOR AND FORWARD CEILING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AT PS-3, OPERATIONAL TEST GOOD. 2 H 7 2 4T RT A13NM 1998022600549 19980226 00549 EU 1998 2 26 QXEA9800079 1 19980219 A 3350 A48351401 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 OVERHEAD EMERGENCY EXIT SIGN ABOVE AISLE ROW 8 IS ONLY PARTIALLY ILLUMINATED. REPLACED EXIT SIGN, OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A20EU 1998022600550 19980226 00550 1998 2 26 QXEA9800080 4 19980222 A 2565 D31697101 SLIDE SWITLIK W85002 FOKKER F28 F28MK4000 4990810 EU CABIN LOW PRESSURE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 477AU 469 11226 ESCAPE SLIDE PRESSURE LOW. REPLACED ESCAPE SLIDE ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998022600551 19980226 00551 EU 1998 2 26 QXEA9800081 1 19980222 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 490US 11152 OVERWING EMERGENCY EXIT SIGN LIGHT FOR THE HATCH AT 9E IS OUT. RELAMPED EXIT SIGN, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998022600552 19980226 00552 EU 1998 2 26 QXEA9800082 1 19980222 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 491US 11156 MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM THE INSIDE OF THE CABIN. CLEANED AND LUBRICATED THE DOOR MECHANISM, OPERATION AL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998022600553 19980226 00553 NM 1998 2 26 98FDEA00124 1 19980223 A 5320 652083321 CHORD BOEING 727 727233 138408A NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 CORROSION BS 1070, WL 201, LBL 45 - RBL 45 ON LOWER CHORD. *S/D* REPAIRED LOWER CHORD BS 1070, WL 201, LBL 45 - RBL 45 IAW FED-EX EA NR 7-5310-37461. 2 L 7 3 4F RT A3WE 1998022600554 19980226 00554 NE 1998 2 26 98FDEA00125 2 19980224 A 7200 ENGINE BOEING 727 727233 138408A NM PWA JT8 JT8D9A 52048 NE NR 1 BIRD STRIKE A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN C F.O.D. CL CLIMB 1 SO 25 270FE 22035 MULTIPLE BIRD STRIKE AT 1300 FT, FLAPS 5 DEGREES. NR 1 ENGINE WAS SHUT DOWN FOR VIBRATION AND SUBSEQUENT FAILURE. REMO VED AND REPLACED NR 1 ENGINE ASSEMBLY PER WORK CARD 70T0001 AND OPERATIONAL CHECKS GOOD. NO LEAKS NOTED ON RUN CHECK. R EFERENCE WORK CARD 70T0001, 70T0002, 70T0303-1. 2 L 7 3 4F 4 F RT A3WE E2EA 1998022600555 19980226 00555 NM 1998 2 26 98FDEA00126 1 19980223 A 5311 FRAME BOEING 727 727233 138408A NM BS 1110 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 271FE 22036 LOWER LOBE AFT CARGO BS 1110 FRAME DAMAGED BELOW LT EDGE SUPPORT PNL, ON TOP ANGLE, BETWEEN STR 27L TO 28L. REMOVED DAM AGED AND INSTALLED DOUBLER PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1998022600556 19980226 00556 NM 1998 2 26 98FDEA00127 1 19980223 A 5320 STIFFENER BOEING 727 727233 138408A NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 271FE 22036 LOWER LOBE AFT CARGO, BS 1183 BULKHEAD LOWER END OF VERTICAL STIFFENER AT RBL 8.0 CRACKED IN I/B RADIUS (INITIAL CRACK L ENGTH 1.875.). INSTALLED RBL 8 VERTICAL BEAM MODIFICATION AND REPAIR PER S/B 53-175R2, AD 90-06-09 AND DRAWING 65C29080 GN7. 2 L 7 3 4F RT A3WE 1998022600557 19980226 00557 NM 1998 2 26 98FDEA00128 1 19980223 A 5311 FRAME BOEING 727 727233 138408A NM BS 1130 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 271FE 22036 LOWER LOBE AFT CARGO BS 1130 FRAME DAMAGED BELOW LT EDGE SUPPORT PANEL ON TOP ANGLE BETWEEN STR 27L TO 28L. INSTALLED D OUBLER PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1998022600558 19980226 00558 NM 1998 2 26 98FDEA00129 1 19980213 A 5330 SKIN BOEING 727 727233 138408A NM BS 1050 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 271FE 22036 UPPER LOBE, FUSE CROWN SKIN GOUGED AT BS 1050 BETWEEN STRINGER 3L TO 4L. TRIMMED OUT DAMAGED AREA. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1998022600559 19980226 00559 NM 1998 2 26 98FDEA00130 1 19980220 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1165 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 FUSELAGE SKIN BULGED AT BS 1165 JUST OUTBOARD AND FORWARD OF RT STATIC PORT. INSTALLED REPAIR PER SRM 53-30-3. 2 L 7 3 4F A3WE 1998022600560 19980226 00560 NM 1998 2 26 98FDEA00131 1 19980219 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 STRINGER CRACKED AT FWD END FASTENER BS 720C + 12 (JUST AFT OF ICE LIGHT HOUSING). REPAIRED CRACKED STR PER SRM 53-10-3 , FIG 5. 2 L 7 3 4F A3WE 1998022600561 19980226 00561 NM 1998 2 26 98FDEA00132 1 19980223 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1148R CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 LOWER FUSE SKIN BULGE BETWEEN STR 26R AND STR 25R, BS 1148R. REMOVED ALL CORROSION AND INSTALLED FRAME SHEAR TIE REPAIR AT SKIN ATTACHMENT PER SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 1998022600562 19980226 00562 NM 1998 2 26 98FDEA00133 1 19980223 A 5311 BELTFRAME BOEING 727 727227 1384078 NM BS 1090 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 UPPER LOBE BELT FRAME DENTED AT RIVET INSTALLATION BS 1090, O/B OF STR 2R. REMOVED DAMAGED AREA AND INSTALLED DOUBLER P ER SRM 51-40-3. 2 L 7 3 4F A3WE 1998022600563 19980226 00563 NM 1998 2 26 98FDEA00134 1 19980223 A 5246 LAV SERV PANEL BOEING 727 727227 1384078 NM BS 1173 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 LOWER FUSE LT SIDE BS 1173L AFT LAV SERV PANEL HAS CORROSION BETWEEN PANEL INSERT AND FUSE STRUCTURE. ACCOMPLISHED LAV PANEL MOD PER E/A 7-5310-29355. 2 L 7 3 4F A3WE 1998022600564 19980226 00564 NM 1998 2 26 98FDEA00135 1 19980220 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 BS 344, LBL 44 TO RBL 25 FLOORBEAM HAS CORROSION AROUND NUTCLIP HOLES (TOP AND BOTTOM) AND ON TOP OF FLOORBEAM. REMOVED CORROSION ON TOP AND BOTTOM OF 344 FLOORBEAM AS PER SRM 51-10-6. INSTALLED NEW TOP CHORD FROM LBL 50 TO RBL 67 PER SR 27-53-007. 2 L 7 3 4F A3WE 1998022600565 19980226 00565 NM 1998 2 26 98FDEA00116 1 19980218 A 2612 FIRE LIGHT BOEING 727 727277 138408S NM APU MALFUNCTIONED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 25 240FE 20978 RED LIGHT ON IN AUXILIARY POWER UNIT FIRE HANDLE IN FLIGHT. TOOK OFF AT 0334Z AND NOTICED THE AUXILIARY POWER UNIT RED LIGHT ON AT 0400Z, FLIGHT LEVEL 310. PULLED THE HANDLE AND DISCHARGED THE AGENT. RED LIGHT REMAINED ON BUT WITH VARIAT ION OF INTENSITY. LATER RED FIRE WARNING LIGHTS UNDER GLARESHIELD CAME ON WITH VARYING INTENSITY. THIS HAPPENED AFTER RESETTING THE AUXILIARY POWER UNIT CIRCUIT BREAKER. ENGINE AND WHEEL WELL FIRE TEST OK. REMOVED AND REPLACED APU FIRE EXTINGUISH BOTTLE IAW MM 26-11-1. BOTTLE CIRCUIT CONTINUITY CKS NORM. ITEM REMAIN DEFER DUE TO APU WARN CIRCUIT INTEGR ITY. REMOVED AND REPLACED R421 BLOCKING RECTIFIER. REPLACED ALL PINS IN CONNECTOR D4858P. APU FIRE TEST OK. 2 L 7 3 4F RT A3WE 1998022600566 19980226 00566 WP 1998 2 26 98FDEA00123 1 19980223 A 7120 FITTING DOUG DC10 DC1010F 3022111 WP NR 1 PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 060FE 46970 NR 1 ENG FWD ENG MOUNT TRUSS FITTING HAS 25 TO 30 BOLTS LOOSE AND 1 SHEARED LT AND RT. *S/D* COMPLIED WITH EA 8-5410-3 5982 PYLON FORWARD ENG MOUNT TRUSS FITTING. FITTING BOLTS FOUND UNDER TORQUE (2) DURING PYLON INSP. 2 L 7 3 4F A22WE 1998022600603 19980226 00603 WP 1998 2 26 ABXA9800111 1 19980130 A 5753 5910042510 VANE DOUG DOUG DC9 DC941 302207N WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 954AX 80626 47612 RIGHT FLAP VANE DELAMINATED APPROXIMATELY 3 INCHES ON UPPER MID SURFACE AND 7 INCH CRACK THROUGH SKIN AT MID INBOARD LEA DING EDGE. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN. 2 L 7 2 4F A6WE 1998022600604 19980226 00604 WP 1998 2 26 ABXA9800112 1 19980219 A 2510 39010481 CABLE DOUG DOUG DC8 DC861 3021952 WP LT COCKPIT OUT OF ADJ A ABXA O OTHER O OTHER CR CRUISE 1 GL 23 841AX 45908 CAPTAIN'S SEAT DID NOT LOCK IN PLACE AND SLID BACK INADVERTENTLY, DURING CRUISE. ADJUSTED AND LUBRICATED LOCK PIN CABLE . 2 L 7 4 4F 4A25 1998022600605 19980226 00605 WP 1998 2 26 ABXA9800113 1 19980223 A 5250 AR25291 LATCH DOUG DOUG DC8 DC861 3021952 WP COCKPIT DOOR OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 COCKPIT DOOR WOULD NOT OPEN. ADJUSTED DOOR LATCH IAW DC8 MM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998022600606 19980226 00606 NM 1998 2 26 SCNA98021 1 19980121 A 2910 HOSES BOEING 727 7272J4 1384006 NM B-HYD SYSTEM FAILED A SCNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 285SC 21676 B-SYSTEM FLIGHT CONTROL AND BOTH B-PUMP LOW PRESSURE LIGHTS CAME ON THEN SLOWLY LOST QUANTITY. DIVERTED TO DENVER. REM OVED AND REPLACED TWO HYDRAULIC HOSES IN B-SYSTEM BAY AND CHANGED FILTERS. SERVICED HYDRAULIC SYSTEM AND FUNCTIONAL CHE CK GOOD. 2 L 7 3 4F RT A3WE 1998022600607 19980226 00607 NM 1998 2 26 P5CA9800239 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 2355 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 2355 TO 2365 STR 46L TO 46R. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02 BLEND OUT WITHIN SRM LIMIT 53-30-01. 2 L 7 4 4F A20WE 1998022600608 19980226 00608 NM 1998 2 26 P5CA9800240 1 19980218 A 5320 WEB BOEING 747 747128 1384894 NM BS 1241 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND LT W/G W/W INBD WEB AT STA 1241 WL 155. REMOVED AND TREATED AS PER SRM 5110-01, 51-10-02. BLEN D OUT AND REPAIRED PER SRM 51-40-04. 2 L 7 4 4F A20WE 1998022600609 19980226 00609 NM 1998 2 26 P5CA9800241 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 785 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 ONE EACH CRACK FOUND ON THE FASTENER HOLE OF SKIN LONGITUDINAL LAP SPLICE AT BS 785 STR 392 OUTER SKIN AREA RUNNING FORW ARD APPROX 0.51 LONG. RT STR 382 LAP REPAIRED AS PER SRM 53-30-03 FIG 17. 2 L 7 4 4F A20WE 1998022600610 19980226 00610 NM 1998 2 26 P5CA9800242 1 19980218 A 5320 STIFFENER BOEING 747 747128 1384894 NM BS 1000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE KEEL BOX ATTACH VERTICAL STIFFENER FOUND CRACKED AT BS 1000. STIFFENER REPAIRED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998022600611 19980226 00611 NM 1998 2 26 P5CA9800243 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1620-1680 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FUSELAGE SKIN AT BS 1620 TO 1680 STR 40L STR 43R. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51- 10-02 BLEND OUT WITHIN SRM LIMIT PER SRM 53-30-01. 2 L 7 4 4F A20WE 1998022600612 19980226 00612 NM 1998 2 26 P5CA9800244 1 19980218 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE BODY FAIRING SUPPORT FOUND SLIGHT CORROSION AT BS 1620 LBL 0 TO 60. CORROSION REMOVED AND TREATED PER SRM 51-1 0-01 AND 51-10-02. REPAIRED PER SRM 53-50-04. 2 L 7 4 4F A20WE 1998022600613 19980226 00613 WP 1998 2 26 ARWA980207 1 19980224 A 2710 46494011 BOLT DOUG DC8 DC862 3021970 WP AILERON CONTROLS SHEARED A ARWA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 19 1804 45896 UNABLE TO MOVE AILERONS IN MANUAL TO RIGHT. UNABLE TO MOVE RIGHT RUDDER PEDAL UPON FURTHER INSPECTION FOUND SHEARED BOL T AT LT MANUAL REVERSION MECHANISM LINKAGE JAMMING LINKAGE. REMOVED AND REPLACED BOLT, AILERON REVERSION SYSTEM OPS. C HECKED NORMAL IN MANUAL MODE IAW M/M 27-11-8. FOUND RUDDER SYSTEM OPS CHECKED NORMAL IN MANUAL REVERSION AND NORMAL MOD E IAW M/M 27-21-0. NO DEFECTS NOTED. 2 L 7 4 4F 4A25 1998022600614 19980226 00614 NM 1998 2 26 VNAA9802018 1 19980220 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 436JS 28935 1613 3052 DURING THE PREFLIGHT INSPECTION, AN EMERGENCY LIGHT WAS NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 5LK BATTERY PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATION CHECKS WERE COMPLETED, AND THE AIRC RAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998022600615 19980226 00615 WP 1998 2 26 CKSA98029 1 19980210 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 593-603 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FUSELAGE SKIN DAMAGE FS 593 TO FS 603 LT STR 49. REPAIRED SKIN DAMAGE IAW AIA EA NR L1-53-013 MARSHALLS DWG NR MT2-05-0 282. FAA APPROVED ON FORM 8110-3 DATED 2/10/98. 2 L 7 3 4F A23WE 1998022600616 19980226 00616 EU 1998 2 26 PLGA980119A 1 19980119 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT FAILED A PLGA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 NE 05 365BE A3713 340B299 BGR - FLT 4277 - AFTER TAKEOFF, THE CREW RECEIVED A CARGO COMPARTMENT SMOKE WARNING. THE WARNING LIGHT EXTINGUISHED AND THEN ILLUMINATED AGAIN. CREW FOLLOWED PROCEDURES AND DISCHARGED THE EXTINGUISHER BOTTLE. AIRCRAFT RETURNED TO BGR AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF SMOKE OR FIRE. BOTH SMOKE DETECTORS WERE REPLACED ALONG WIT H THE EXTINGUISHER BOTTLE. SYSTEM TESTED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998022600617 19980226 00617 EU 1998 2 26 PLGA980114B 1 19980114 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG LEAKING A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 05 743BA 340A093 FLT 4562 - LGA - AFTER TAKEOFF, THE CREW REPORTED THE MAIN HYDRAULIC SYSTEM WARNING LIGHT ILLUMINATED ALONG WITH LOW PRE SSURE AND QTY. CREW FOLLOWED PROCEDURES AND RETURNED TO LGA. MAINTENANCE FOUND HYDRAULIC LINE SWIVEL GOING TO RIGHT MA IN GEAR DOWN LOCK LEAKING. SWIVEL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998022600618 19980226 00618 EU 1998 2 26 PLGA980115A 1 19980115 A 3010 7257211525 BOOT SAAB SF340 340B 7860101 EU LT WING FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 363BE 340B293 BOS - FLT 4394 - AFTER TAKEOFF, THE CREW RECEIVED A DE-ICE BOOT TIMER LIGHT FAILURE. AIRCRAFT RETURNED TO BOS DUE TO WE ATHER CONDITIONS. MAINTENANCE REPLACED THE NR 6 DE-ICE BOOT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998022600619 19980226 00619 EU 1998 2 26 PLGA980114C 1 19980114 A 7712 CONNECTOR SAAB SF340 SF340A 7850100 EU LT ENGINE DIRTY A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 741BA 340A090 BTV - AFTER TAKEOFF, THE CREW REPORTED THE LEFT ENGINE TORQUE STARTED FLUCTUATIONS BETWEEN 80-90 PERCENT. THE LEFT OIL PRESSURE ALSO STARTED FLUCTUATIONS OF 20 PSI. AIRCRAFT RETURNED TO BTV AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANE D ELECTRICAL CONNECTORS TO ECU. ENGINE GROUND RAN WITH ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998022600620 19980226 00620 EU 1998 2 26 PLGA980114A 1 19980114 A 3213 STRUT SAAB SF340 SF340A 7850100 EU LT MLG REQ'D SERVICE A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 341BE 340A063 BOS - FLT 4297 - AFTER TAKEOFF, THE CREW RECEIVED A CONFIGURATION WARNING. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED LEFT MAIN GEAR STRUT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998022600621 19980226 00621 EU 1998 2 26 PLGA980113A 1 19980113 A 3060 VP3365A DE-ICE LEAD SAAB SF340 SF340A 7850100 EU LT PROP FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 342BE 340A096 BGR - FLT 4586 - AFTER DEPARTURE, THE LEFT PROP DE-ICE FAILURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BGR DUE TO WEATH ER CONDITIONS. MAINTENANCE REPLACED ONE PROP DE-ICE LEAD. SYSTEM TESTED GOOD AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998022600622 19980226 00622 NM 1998 2 26 P2EA98004 1 19980119 A 2130 RELIEF VALVE BOEING 737 737205 NM AFT FUSELAGE INOPERATIVE A P2EA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 412CE 20412 MCI-ATL - EXPERIENCED PRESSURIZATION PROBLEMS AND RETURNED BACK TO MCI. DURING TROUBLESHOOTING A CABIN PRESSURE SAFETY RELIEF VALVE WAS FOUND OPENING AT A LOWER PRESSURE THAN ALLOWED PER BOEING MM. A BLANKING PLATE WAS INSTALLED PER MEL. ALSO, DURING TROUBLESHOOTING A CRACK WAS FOUND IN THE LOWER AFT FRAME OF THE AFT CARGO COMPARTMENT DOOR BETWEEN THE SKI N AND SEAL RETAINER. A MAINTENANCE FERRY PERMIT WAS ISSUED FOR ACFT 412 TO FERYY TO PHX SO SABRETECH COULD REPAIR THE A FT CARGO DOOR. THE AFT CARGO COMPARTMENT DOOR WAS REPLACED BY SABERTECH AND THE AIRCRAFT RETURNED TO SERVICE WITH THE S AFETY RELIEF VALVE STILL ON MEL. (M) 2 L 7 2 4F A16WE 1998022600623 19980226 00623 WP 1998 2 26 ORJA9804 1 19980121 A 3350 FUSES DOUG DC9 DC983 3022083 WP CABIN BLOWN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 880RA 53186 EMERGENCY LIGHTS WILL NOT TEST. INSTALLED FUSES AT BATTERY PACK LOCATIONS L1 ENTRANCE DOOR RT FWD O/W EXIT LT AFT O/W E XIT, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998022600624 19980226 00624 WP 1998 2 26 ORJA9808 1 19980117 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS ROWS 21-24 WILL NOT TURN OFF. REMOVED AND REPLACED EMERGENCY LIGHTS ASSY, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998022600625 19980226 00625 WP 1998 2 26 ORJA9809 1 19980120 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN SEAT EMERGENCY LIGHTS INOP AT SEATS 21D THROUGH 25D. REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY PER MM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998022600627 19980226 00627 NM 1998 2 26 MASA98013 1 19980121 A 3350 GE316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 FLT 7463 - DEN-CPR - CREW REPORTED INTERIOR EMERGENCY LIGHTING, NR 1 OVERHEAD, TO BE INOP. MAINTENANCE REPLACED A BURNE D OUT BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998022600628 19980226 00628 1998 2 26 HALA9800018 4 19980119 A 3454 NPU DOUG DC10 DC1010 3022110 WP NR 2 FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 119AA 46519 FLT 26 - HNL - NAV UNREADABLE, BOTH HSI AND RMI HEADINGS WERE DIFFERENT IN NAV POSITION UP TO 50 DEGREES AT ONE POINT. H SI COURSE INDICATORS DID NOT AGREE WITH LEGS PAGE COURSE. NR 1 WENT TO VERIFY POSITION, NR 2 WENT TO DR. POSITION CHEC KED OK FOR BOTH. A/C RETURNED TO HNL, WHERE AN UNEVENTFUL LANDING WAS MADE. (M) 2 L 7 3 4F A22WE 1998022600638 19980226 00638 NM 1998 2 26 P2EA98022 1 19980203 A 3610 BACC10DU350ABF CLAMP BOEING 737 737222 1384473 NM NR 2 ENGINE LOOSE A P2EA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CE 05 603DJ 19955 DEN - FLT 604 - DEN-MCI - THE NR 2 ENGINE OVERHEAT LIGHT CAME ON INTERMITTENTLY WITH NO OTHER ABNORMAL INDICATIONS. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEN WHERE THE LANDING WAS UNEVENTFUL AT 2217Z. FRONTIER AIRLINES AN APPROVE D CONTRACT MAINTENANCE PROVIDER FOR VANGUARD AIRLINES WAS DISPATCHED AND FOUND THE NR 2 ENGINE EIGHT STAGE CHECK VALVE C LAMP WORN AND LOOSE. THE CLAMP WAS CHANGED AND AN AIRCRAFT 'RUN AND LEAK CHECK' WAS PERFORMED WITH NO FURTHER PROBLEMS. AIRCRAFT RETURNED TO MCI WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F A16WE 1998022600641 19980226 00641 WP 1998 2 26 98ZZZM224 1 19980127 A 2120 AIR DISTRIBUTION CVAC 340 34031 2422704 WP CABIN SMOKE A RENA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 01 3HH 173 LIGHT SMOKE IN CABIN AFTER TAKEOFF. 2 L 7 2 4R 6A6 1998022600648 19980226 00648 1998 2 26 HALA9800023 4 19980122 A 3421 VERTICAL GYRO DOUG DC10 DC1010 3022110 WP E/E COMPT FAILED A HALA O OTHER O OTHER CL CLIMB 1 WP 13 162AA 46943 LOS - FLT 931 - DURING CLIMB PASSING FL 210, WHEN A/P NR 1 INITIATED HDG CHANGE, AIRCRAFT WENT INTO A RAPID RATE OF ROLL . A/P NR 1 DISCONNECTED AUTOMATICALLY. CAPTAINS ADI DISPLAYED ATT FLAG AND SPEED FLAG. WHILE INTERCEPTING LOA HNL, AD I FAILED. REPLACED NR 1 VERTICAL GRYO. PERFORMED ADJ/TEST PER MM 34-23-00-OK. ALSO, PERFORMED BITE CHECKED NR 1 A/P M M 22-00-02. CHECKED GOOD. (M) 2 L 7 3 4F A22WE 1998022600649 19980226 00649 WP 1998 2 26 HALA9800025 1 19980127 A 3350 60030051 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 699HA 47763 LIH - FORWARD MOST CABIN AND COCKPIT OVERHEAD EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED THE POWER PACK BATTERIES. CONDITION SAME. REMOVED AND REPLACED THE BATTERY POWER SUPPLY. THE OPERATIONAL CHECK WAS OK. (M) 2 L 7 2 4F RT A6WE 1998022600650 19980226 00650 WP 1998 2 26 HALA9800024 1 19980124 A 3222 SEAL DOUG DC9 DC951 3022051 WP NLG STRUT FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 662HA 47742 FLT 267 - KOA - NOSEWHEEL WOULD NOT RETRACT AFTER TAKEOFF FROM KONA. ALL SYSTEMS INDICATED NORMAL. REMOVED AND REPLACE D LOWER NOSE STRUT SEALS PER MM 32-21-2 METHOD 'B' ITEMS 1 THROUGH 20. COMPLETED NOSE STRUT SEALS REPLACEMENT PER MM 32 -21-02 STEPS 21 THROUGH 35. OPERATIONAL CHECK AND LEAK CHECK OK. GEAR SWING OK. (M) 2 L 7 2 4F RT A6WE 1998022600651 19980226 00651 WP 1998 2 26 HALA9800026 1 19980127 A 3350 41B004A007G3 BATTERIES DOUG DC9 DC951 3022051 WP TAIL CONE DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 603DC 47784 HNL - TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERIES AND THE OPERATIONAL CHECK WAS GOOD. (M) 2 L 7 2 4F RT A6WE 1998022600652 19980226 00652 EU 1998 2 26 VTZA98014 1 19980114 A 3260 ATG132256 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 323UE 41059 IAD-ROC - FLT 6365 - DURING TAKEOFF, EXPERIENCED A DISCREPANCY WITH THE RED GEAR INTRANSIT LIGHT ILLUMINATION ON GEAR UP ACTIVATION. AIRCRAFT RETURNED TO IAD WHERE MAINTENANCE WAS DISPATCHED AND FOUND THAT THE LEFT MLG UPLOCK MICROSWITCH H AD FAILED. MAINTENANCE REMOVED AND REPLACED THE LEFT MGL UPLOCK MICROSWITCH AND PERFORMED THE REQUIRE CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998022600653 19980226 00653 EU 1998 2 26 VTZA98017 1 19980115 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE CONTAMINATED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 478UE 892 IAD-BWI - FLT 6468 - DURING TAXI, EXPERIENCED A LEFT FIRE DETECT LIGHT ILLUMINATION. AIRCRAFT RETURNED TO THE GATE WHER E MAINTENANCE FOUND WATER INGESTION IN THE ELEMENT CONNECTOR. MAINTENANCE CLEANED ELEMENT CONNECTOR AND PERFORMED APPRO PRIATE CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998022600654 19980226 00654 1998 2 26 VTZA98018 4 19980114 A 3413 066011450101 VSI INDICATOR BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 472UE 823 FLT 6420 - IAD-BUF - DURING CLIMB, THE FLIGHT EXPERIENCED A FLICKERING OF THE CAPTAINS VSI THEN GOING BLANK. AIRCRAFT R ETURNED TO IAD WHERE MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE RT TCAS VSI INDICATOR. ALL CHECKS WERE ACCOMP LISHED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998022600655 19980226 00655 EU 1998 2 26 VTZA98020 1 19980116 A 3260 S2700003 RELAY JETAIR JETSTM JETSTM4101 1500501 EU PEDESTAL FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 324UE 41017 FLT 6563 - IAD-RDU - DURING TAKEOFF, EXPERIENCED A DISCREPANCY WITH THE RED GEAR INTRANSIT LIGHT ILLUMINATION ON GEAR UP ACTIVATION. GEAR WAS CYCLED DOWN AND HAD THREE GREEN LIGHTS. AIRCRAFT RETURNED TO IAD WHERE MAINTENANCE WAS DISPATCHE D AND FOUND THAT THE FILAMENT TEST RELAY HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE TEST RELAY AND PERFORMED THE REQUIRE CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998022600656 19980226 00656 EU 1998 2 26 VTZA98021 1 19980115 A 7921 L86023281 OIL COOLER JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 321UE 41045 FLT 6402 - BOS-IAD - DURING CRUISE, EXPERIENCED A DISCREPANCY WITH THE RT OIL PRESSURE INDICATION FLUCTUATION. AIRCRAFT DIVERTED TO BDL, DECLARED AN EMERGENCY AND LANDED WITH NO FURTHER PROBLEM. MAINTENANCE WAS DISPATCHED AND FOUND THAT T HE RT ENGINE OIL COOLER IN-LINE BOSS WAS STRIPPED OUT. MAINTENANCE REMOVED AND REPLACED THE ENGINE OIL COOLER AND PERFO RMED THE REQUIRED CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998022600657 19980226 00657 1998 2 26 VTZA98022 4 19980122 A 3421 258719343 GYRO BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 490UE 909 FLT 6455 - IAD-PHL - DURING TAXI, THE FLT EXPERIENCED A FLAG ON THE FIRST OFFICERS HSI. AIRCRAFT RETURNED TO THE GATE W HERE MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE FIRST OFFICERS GYRO. ALL CHECKS WERE ACCOMPLISHED AND THE AIR CRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998022600658 19980226 00658 1998 2 26 VTZA98024 4 19980125 A 3413 066500012704 VSI INDICATOR BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 497UE 904 FLT 6351 - IAD-SWF - DURING TAXI, EXPERIENCED A PROBLEM WHEN THE CAPTAINS VSI WENT BLANK. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REMOVED AND REPLACED THE CAPTAI NS VSI INDICATOR. ALL REQUIRED CHECKS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998022600659 19980226 00659 EU 1998 2 26 VTZA98025 1 19980123 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU BAGG COMPT FAILED A VTZA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 491UE 911 FLT 6287 - CMH-IAD - DURING CRUISE, EXPERIENCED AN INTERMITTENT ILLUMINATION OF THE BAG SMOKE WARNING LIGHT. AIRCRAFT L ANDED AT IAD WITH NO PROBLEM. AIRCRAFT TAXIED TO THE GATE WHERE MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISP ATCHED TO THE AIRCRAFT AND REMOVED AND REPLACED THE BAGGAGE BAY SMOKE DETECTOR. ALL REQUIRED CHECKS WERE ACCOMPLISHED A ND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998022600660 19980226 00660 EA 1998 2 26 VTZA98028 1 19980127 A 3010 11513361 CONTROLLER CNDAIR CL600 CL6002B19 EA ANTI-ICE SYSTEM FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 623BR 7192 FLT 6697 - IAD-JAX - DURING TAKEOFF, EXPERIENCED A WING OVERHEAT WARNING. AIRCRAFT RETURNED TO THE GATE AND NOTIFIED MA INTENANCE CONTROL. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REMOVED AND REPLACED THE ANTI-ICE CONTROLLER. ALL RE QUIRED CHECKES WERE ACCOMPLISHED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 1998022600661 19980226 00661 1998 2 26 VTZA98030 4 19980127 A 3140 7003110901 EHSI SCREEN JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 303UE 41015 FLT 6516 - IAD-LGA - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE CAPTAINS EHSI SCREEN GOING BLANK. AIRCRAFT RETURNE D TO THE GATE, WHERE MAINTENANCE CONTROL AND MAINTENANCE WAS NOTIFIED. MAINTENANCE REMOVED AND REPLACED THE EHSI INDICA TOR IAW MAINTENANCE PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SER VICE. (M) 2 L 7 2 4T RT A41NM 1998022600662 19980226 00662 EU 1998 2 26 VTZA98031 1 19980127 A 3411 PITOT LINE BAG JETSTM JETSTM3201 1500217 EU LEFT CONTAMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 484UE 899 FLT 6528 - BUF-IAD - DURING TAKEOFF, EXPERIENCED A DISCREPANCY WITH THE CAPTAINS AIRSPEED INDICATOR READING 15 KNOTS LES S THAN THE FIRST OFFICERS. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CONTROL WAS NOTIFIED AND MAINTENANCE WAS DISPATC HED FROM IAD TO TROUBLESHOOT THE DISCREPANCY. MAINTENANCE FOUND WATER IN THE PITOT LINE, DRAINED WATER AND PERFORMED RE QUIRED CHECKS. ALL SYSTEMS WORKED NORMALLY. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998022600663 19980226 00663 EU 1998 2 26 VTZA98032 1 19980127 A 3260 327 BULB BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A VTZA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 27 486UE 905 FLT 6381 - IAD-CMH - DURING APPROACH, EXPERIENCED A DISCREPANCY WITH THE NOSE GEAR DOWN AND LOCK INDICATOR NOT ILLUMINAT ING. AIRCRAFT ABORTED APPROACH AND DECLARED EMERGENCY. SECONDARY INDICATION SHOWED THE AIRCRAFT NOSE LANDING GEAR BEIN G DOWN AND AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND MAINTENANCE WAS DISPATCHED FR OM IAD. UPON ARRIVAL MAINTENANCE FOUND THAT THE ONLY PROBLEM WAS LIGHT BULB WAS BURNED OUT. MAINTENANCE REMOVED AND RE PLACED THE LIGHT BULB. ALL SYSTEMS WORKED MANUALLY. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998022600664 19980226 00664 EU 1998 2 26 WTAA980014 1 19980120 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT MLG FAILED A WTAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 419UE 779 LAX - LEFT MAIN LANDING GEAR INTRANSIT LIGHT FAILS TO ILLUMINATE. MAINTENANCE REPAIRED BROKEN WIRES AT LEFT MAIN GEAR U PLOCK MICROSWITCH. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998022600666 19980226 00666 NM 1998 2 26 USAASB98022 1 19980123 A 3350 AD20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 411US 23880 CLT - MAINTENANCE FOUND THE MID-CABIN EMERGENCY EXIT LIGHTS WEAK DURING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM. MA INTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998022600667 19980226 00667 NM 1998 2 26 USAASB98021 1 19980122 A 3350 AD20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 LGA - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT AND THE LEFT AFT OVERWING EMERGNCY EXIT LIG HT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AND CHARGER ASSEMBLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998022600668 19980226 00668 NM 1998 2 26 98ZZZM225 1 19980122 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 405US 23885 LGA - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT AND THE LEFT AFT OVERWING EMERGNCY EXIT LIG HT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AND CHARGER ASSEMBLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998022600669 19980226 00669 NM 1998 2 26 USAASB98020 1 19980127 A 3350 3114981 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 435US 24557 EWR - MAINTENANCE FOUND THE FORWARD GALLEY SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE SEAL (P/N 31-1493-1). OPS CHECK GOOD PER MM 33-51-02. (M) 2 L 7 2 4F RT A16WE 1998022600671 19980226 00671 NM 1998 2 26 USAASB98024 1 19980127 A 7933 162BL804A OIL TEMP IND BOEING 737 737301 1384611 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 573US 23560 TPA - FLT 61 - DURNG CRUISE FLT, CAPT NOTICED THE NR 1 ENG OIL TEMP GAUGE WAS AT THE RED LINE. CAPT REDUCED POWER AND T HE OIL TEMP DROPPED IN THE YELLOW. AT IDLE, TEMP REMAINED IN YELLOW FOR 10 MIN AND THEN DROPPED TO TOP OF GREEN BAND. A N EMERGENCY WAS DECLARED AND THE FLT DIVERTED TO TPA AND LANDED W/O FURTHER INCIDENT. UPON LANDING AND TAXIING TO THE G ATE, OIL TEMP REMAINED IN THE UPPER GREEN RANGE. THE NR 1 ENG WAS NOT SHUT DOWN IN FLT. MX REMOVED AND REPLACED THE NR 1 ENG OIL TEMP INDICATOR AND OIL TEMP BULB. OIL QTY AND CHIP DETECTORS WERE CHECKED AND FOUND GOOD. RAN ENGINE. OIL TEMP NORMAL. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998022600672 19980226 00672 NM 1998 2 26 98ZZZM226 1 19980127 A 7933 1122514 OIL TEMP BULB BOEING 737 737301 1384611 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 573US 23560 TPA - FLT 61 - DURNG CRUISE FLT, CAPT NOTICED THE NR 1 ENG OIL TEMP GAUGE WAS AT THE RED LINE. CAPT REDUCED POWER AND T HE OIL TEMP DROPPED IN THE YELLOW. AT IDLE, TEMP REMAINED IN YELLOW FOR 10 MIN AND THEN DROPPED TO TOP OF GREEN BAND. A N EMERGENCY WAS DECLARED AND THE FLT DIVERTED TO TPA AND LANDED W/O FURTHER INCIDENT. UPON LANDING AND TAXIING TO THE G ATE, OIL TEMP REMAINED IN THE UPPER GREEN RANGE. THE NR 1 ENG WAS NOT SHUT DOWN IN FLT. MX REMOVED AND REPLACED THE NR 1 ENG OIL TEMP INDICATOR AND OIL TEMP BULB. OIL QTY AND CHIP DETECTORS WERE CHECKED AND FOUND GOOD. RAN ENGINE. OIL TEMP NORMAL. OPS CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998022600673 19980226 00673 NM 1998 2 26 USAASB98019 1 19980125 A 2612 6678 FIRE DETECTOR BOEING 737 7373B7 1384580 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 507AU 23382 PIT - FLT 167 - CAPT REPORTED THAT AT HIGH ALT AND HIGH POWER, THE NR 1 ENGINE 'B' LOOP FAULT LIGHT FLICKERED. AFTER SW ITCHING TO 'A' LOOP, HE RECEIVED FAULT LIGHT. CAPT NOTIFIED VIA ACARS WAS DIVERTING TO PIT DUE TO SAME PROBLEM IN PHL H AD REOCCURRED. IN PHL, MX INSPECTED FIRE LOOPS WITH NO DEFECTS NOTED AND REPLACED THE FIRE CONTROL PANEL AS PRECAUTIONA RY. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RE PLACED THE NR 1 ENG CORE FIRE DETECTOR SENSOR ASSY WHICH WAS FOUND BAD ALONG WITH THE CORE WIRING HARNESS DUE TO A HIGH RESISTANCE. ALSO, REPLACED THE NR 1 ENGINE PYLON FIRE LOOP DETECTOR AS PRECAUTIONARY. RAN ENGINE AT POWER WITH BLEED 2 L 7 2 4F RT A16WE 1998022600674 19980226 00674 NM 1998 2 26 98ZZZM227 1 19980125 A 2612 667201 FIRE DETECTOR BOEING 737 7373B7 1384580 NM NR 1 PYLON FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 507AU 23382 PIT - FLT 167 - CAPT REPORTED THAT AT HIGH ALT AND HIGH POWER, THE NR 1 ENGINE 'B' LOOP FAULT LIGHT FLICKERED. AFTER SW ITCHING TO 'A' LOOP, HE RECEIVED FAULT LIGHT. CAPT NOTIFIED VIA ACARS WAS DIVERTING TO PIT DUE TO SAME PROBLEM IN PHL H AD REOCCURRED. IN PHL, MX INSPECTED FIRE LOOPS WITH NO DEFECTS NOTED AND REPLACED THE FIRE CONTROL PANEL AS PRECAUTIONA RY. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RE PLACED THE NR 1 ENG CORE FIRE DETECTOR SENSOR ASSY WHICH WAS FOUND BAD ALONG WITH THE CORE WIRING HARNESS DUE TO A HIGH RESISTANCE. ALSO, REPLACED THE NR 1 ENGINE PYLON FIRE LOOP DETECTOR AS PRECAUTIONARY. RAN ENGINE AT POWER WITH BLEED 2 L 7 2 4F RT A16WE 1998022600675 19980226 00675 NM 1998 2 26 98ZZZM228 1 19980125 A 2612 6131508551 WIRE HARNESS BOEING 737 7373B7 1384580 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 507AU 23382 PIT - FLT 167 - CAPT REPORTED THAT AT HIGH ALT AND HIGH POWER, THE NR 1 ENGINE 'B' LOOP FAULT LIGHT FLICKERED. AFTER SW ITCHING TO 'A' LOOP, HE RECEIVED FAULT LIGHT. CAPT NOTIFIED VIA ACARS WAS DIVERTING TO PIT DUE TO SAME PROBLEM IN PHL H AD REOCCURRED. IN PHL, MX INSPECTED FIRE LOOPS WITH NO DEFECTS NOTED AND REPLACED THE FIRE CONTROL PANEL AS PRECAUTIONA RY. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND RE PLACED THE NR 1 ENG CORE FIRE DETECTOR SENSOR ASSY WHICH WAS FOUND BAD ALONG WITH THE CORE WIRING HARNESS DUE TO A HIGH RESISTANCE. ALSO, REPLACED THE NR 1 ENGINE PYLON FIRE LOOP DETECTOR AS PRECAUTIONARY. RAN ENGINE AT POWER WITH BLEED 2 L 7 2 4F RT A16WE 1998022600676 19980226 00676 NM 1998 2 26 USAASB98015 1 19980117 A 3260 106180350 LIGHT BOEING 737 737201 1384454 NM RT MLG FAILED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 242US 22444 CLT - FLT 209 - ON APPROACH INTO CLT, CREW DID NOT RECEIVE A DOWN AND LOCKED INDICATION FOR THE RT MLG. CREW TESTED LIG HT AND CONFIRMED THE LIGHT WAS OPERATIONAL. CREW RECYCLED THE GEAR AND AGAIN RECEIVED NO DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR. CREW ACCOMP A GO-AROUND AND PERFORMED MANUAL GEAR EXTENSION CHECKLIST. FIRST OFFICER VERIFIED GE AR WAS DOWN AND LOCKED THROUGH VIEWPORTS. A FLYBY WAS ALSO ACCOMP FOR TOWER TO CONFIRM GEAR WAS DOWN. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED SAFELY WITHOUT INCIDENT. GEAR WAS PINNED AND TOWED TO THE GATE. MAINTENANCE FOUND A BA D LIGHT SOCKET FOR THE RT MLG DOWN INDICATION. REPLACED SAME. OPS CHECK GOOD. STOWED GEAR PINS. (M) 2 L 7 2 4F A16WE 1998022600677 19980226 00677 EU 1998 2 26 USAAF98006 1 19980116 A 3241 CONNECTOR FOKKER F28 F28MK0100 4990807 EU ANTI-SKID CONTL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 852US 11280 FLT 1707 - CLT-IAD - EN ROUTE TO IAD, LIFT DUMPER FAULT ANNUNCIATED. FLT RETURNED TO CLT AND LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE FOUND TWO PINS (2 AND 53) AT ANTI-SKID CONTROL BOX WERE PUSHED BACK IN THE CONNECTOR. REPAIRED THE CONNECTOR AND REPLACED K1197, K1198, K1261A AND K1730 AS PRECAUTIONARY. SYSTEM TESTED OK. (M) 2 L 7 2 4F RT 1998022600678 19980226 00678 EU 1998 2 26 USAAF98007 1 19980114 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 865US 11308 IND - MAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE AT FORWARD CABIN FLOOR, GALLEY AND COCKPIT. REPLACED THE BATTERY P ACK. (M) 2 L 7 2 4F RT 1998022600679 19980226 00679 NM 1998 2 26 USAASB98013 1 19980112 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 PHL - DURING OPERATIONAL CHECK OF THE EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE AFT OVERHEAD EMERGENCY EXIT LIGHT IN OP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998022600680 19980226 00680 WP 1998 2 26 USAAD98018 1 19980124 A 3350 8732030153 CONTROL MODULE DOUG DC9 DC982 3022082 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 824US 49143 CLT - CABIN EMERGENCY LOW LEVEL LIGHTING FAILED TO EXTINGUISH AFTER TEST. MAINTENANCE REPLACED THE EMERGENCY LOW LEVEL LIGHTING CONTROL MODULE. (M) 2 L 7 2 4F A6WE 1998022600681 19980226 00681 WP 1998 2 26 USAAD98017 1 19980123 A 3222 MS288892 VALVE DOUG DC9 DC931 3022065 WP NLG STRUT LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 926VJ 48146 CLT - FLT 7002 - AFTER TAKEOFF, THE NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT RETURNED TO THE F IELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE LANDING GEAR STRUT FLAT. THE SERVICING (SCHRADER) VALVE W AS REPLACED AND THE STRUT SERVICED. ALL CHECKED NORMAL DURING RETRACTION AND TAXI CHECKS. (M) 2 L 7 2 4F A6WE 1998022600682 19980226 00682 WP 1998 2 26 USAAD98016 1 19980123 A 3230 59516395001 CYLINDER DOUG DC9 DC931 3022065 WP NLG FAILED A USAA K NONE J WARNING INDICATION AP APPROACH 1 EA 19 913VJ 45846 CTL - FLT 369 - ON APPROACH, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHEN THE LANDIG GEAR WAS LOWERED. THE FLT CREW RECY CLED THE GEAR BUT THE LIGHT REMAINED. THE FLT CREW THEN PULLED THE MANUAL GEAR RELEASE LEVER IN THE COCKPIT. THE FLIGH T LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NLG BUNGEE CYLINDER AND ACCOMPLISHED A GEAR SWING. ALL INDICATION AND OPERATION WAS NORMAL. (M) 2 L 7 2 4F A6WE 1998022600683 19980226 00683 NM 1998 2 26 USAASB98003 1 19980105 A 3610 32144464 HIGH STAGE VALVE BOEING 737 7374B7 1384702 NM NR 1 ENGINE STICKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 443US 24842 PIT - FLT 292 - PRIOR TO DEPART, CREW REPORTED A LOUD NOISE COMING FROM AIR CONDITIONING PACK. A/C WAS RELEASED WITH TH E RT PACK ON MEL. THEN UPON CLIMB-OUT FROM PIT, A/C WAS UNABLE TO MAINTAIN PRESSURIZATION OFF THE LT PACK. A/C WOULD N OT PRESSURIZE IN AUTO, STANDBY OR MANUAL. OUTFLOW VALVE SHOWED FULL CLOSED BUT CABIN CLIMBED 1,500 FPM. CAPT ELECTED T O RETURN TO FIELD AT PIT. THE FLT LANDED W/O INCIDENT WITH NO EMERGENCY BEING DECLARED. MX REMOVED AND REPLACED LT ACM WITH NO HELP. FOUND THE LT ENG HIGH STAGE VALVE STICKING. REPLACED SAME ALONG WITH THE HIGH PRESSURE REGULATOR. OPS CHECK GOOD ALONG WITH ENGINE GROUND RUN. CLEARED RT PACK MEL BY REPLACING FROZEN RT ACM AND BROKEN SENSE LINE AT RT PAC 2 L 7 2 4F RT A16WE 1998022600684 19980226 00684 NM 1998 2 26 TAOA019811 1 19980122 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 5458 20445 FLT 6181 - BOS-LGA - R-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK NO RMAL PER MM 33-50. (M) 2 L 7 3 4F A3WE 1998022600685 19980226 00685 NM 1998 2 26 TAOA019810 1 19980121 A 3350 10617843 LIGHT BOEING 727 727225 1384077 NM FWD RT OVERWING FAILED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 198 20447 FLT 6060 - LGA-BOS - FORWARD RIGHT OVERWING INTERNAL EMERGENCY LIGHTS WON'T TEST. REPLACED BASE ASSEMBLY, OPERATIONAL C HECKS NORMAL. (M) 2 L 7 3 4F A3WE 1998022600686 19980226 00686 WP 1998 2 26 TWAA9801303 1 19980123 A 2410 696233B CSD DOUG DC9 DC931 3022065 WP LT ENGINE MALFUNCTIONED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 987Z 47137 STL - FLT 542 - LOW SPEED ABORT ELECTRICAL FLUCTUATIONS BETWEEN RT AND LT SYSTEMS. REPLACED LT ENGINE CSD. (M) 2 L 7 2 4F A6WE 1998022600687 19980226 00687 NM 1998 2 26 TWAA9801302 1 19980124 A 3350 6013211 BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64339 20844 STL - FLT 325 - L2 DOOR EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE BY MECHANIC. REPLACED ESCAPE LIGHT BATTERY PACK ASSY . (M) 2 L 7 3 4F A3WE 1998022600688 19980226 00688 WP 1998 2 26 TWAA9801301 1 19980122 A 3010 39244412 VALVE DOUG DC9 DC982 3022082 WP AIRFOIL DE-ICE FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 918TW P422 49367 STL - FLT 229 - DURING CLIMB-OUT OF STL, WITH AIRFOIL ANTI-ICE ON AIRFOIL ICE PROTECT PRESS ABNORMAL LIGHT ON ANN PANEL CAME ON. REPLACED ANTI-ICE PRESS REG VALVE. (M) 2 L 7 2 4F A6WE 1998022600689 19980226 00689 WP 1998 2 26 TWAA9801202 1 19980122 A 3233 39208025507 ACTUATOR DOUG DC9 DC932 3022066 WP RT ENGINE LEAKING A TWAA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 CE 05 921L 47107 YYZ - FLT 605 - AFTER TAKEOFF, RT HYDRAULIC SYSTEM INDICATED A FLUID LOSS. REPLACED LEFT MLG RETRACT CYLINDER AND RT EN GINE HYDRAULIC PUMP. (M) 2 L 7 2 4F A6WE 1998022600690 19980226 00690 WP 1998 2 26 98ZZZM229 1 19980122 A 2913 314196 PUMP DOUG DC9 DC932 3022066 WP RT ENGINE LEAKING A TWAA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 CE 05 921L 47107 YYZ - FLT 605 - AFTER TAKEOFF, RT HYDRAULIC SYSTEM INDICATED A FLUID LOSS. REPLACED LEFT MLG RETRACT CYLINDER AND RT EN GINE HYDRAULIC PUMP. (M) 2 L 7 2 4F A6WE 1998022600693 19980226 00693 CE 1998 2 26 98ZZZM232 1 19980118 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900 1154160 CE LANDING GEAR MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 192GA 55 UB17 FLT 7489 - FPO-MIA - GEAR REMAINS DOWN WITH HANDLE IN UP POSITION. REPLACED LANDING GEAR CONTROL HANDLE ASSY. OPERATIO N CHECKS SATISFACTORY ON JACKS. (M) 2 L 7 2 4T RT A24CE 1998022600694 19980226 00694 CE 1998 2 26 98ZZZM233 1 19980115 A 2910 HYD FLUID BEECH 1900 1900 1154160 CE HYD SYSTEM REQ'D SERVICE A GUUA O OTHER J WARNING INDICATION CL CLIMB 1 SO 19 192GA UB17 FLT 7396 - MCO-MIA - LANDING GEAR WOULD NOT RETRACT. DETERMINED HYDRAULIC FLUID TO BE LOW. SERVICED SYSTEM, SATISFACT ORY OPERATIONAL CHECKS ON JACKS. (M) 2 L 7 2 4T RT A24CE 1998022600695 19980226 00695 CE 1998 2 26 98ZZZM234 1 19980107 A 3260 INDICATION BEECH 1900 1900 1154160 CE LANDING GEAR MALFUNCTIONED A GUUA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 19 188GA UB14 FLT 7486 - MCO-MIA - LANDING GEAR RED LIGHT FLICKERED DURING TURBULENCE. INSPECTED LANDING GEAR SYSTEM, CHECKED RIGGING , WITH AIRCRAFT ON JACKS, COULD NOT DUPLICATE. (M) 2 L 7 2 4T RT A24CE 1998022600696 19980226 00696 CE 1998 2 26 98ZZZM235 1 19980107 A 7120 TRUSS BEECH 1900 1900 1154160 CE NR 1 ENGINE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 189GA UB9 ON INSPECTION, NR 1 ENGINE TRUSS INBOARD SIDE UPPER HAS CRACK. WELDED CRACK IAW MANUFACTURERS REPAIR INSTRUCTIONS CONTA INED IN KIT NR 114-9033-1, PARAGRAPH 16. (M) 2 L 7 2 4T RT A24CE 1998022600697 19980226 00697 CE 1998 2 26 98ZZZM236 1 19980123 A 5521 10162001445 SPAR CAP BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 198GA UB5 AT SCHEDULED, EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION TH E LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS PART NR 'S 101-920014-45, AND 101-620014- 47. (M) 2 L 7 2 4T RT A24CE 1998022600698 19980226 00698 CE 1998 2 26 98ZZZM237 1 19980123 A 5520 BRACKET BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 198GA UB5 AT SCHEDULED EMPENNAGE INSPECTION, DETERMINED LEFT ELEVATOR OUTBOARD AND CENTER HINGE ATTACH BRACKETS TO HAVE INTERGRANU LAR CORROSION. REMOVE AND REPLACED OUTBOARD AND CENTER HINGE, ATTACH BRACKETS. (M) 2 L 7 2 4T RT A24CE 1998022600699 19980226 00699 CE 1998 2 26 98ZZZM238 1 19980129 A 3234 CONTROL HANDLE BEECH 1900 1900 1154160 CE LANDING GEAR MALFUNCTIONED A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 192GA 409 UB17 FLT 7448 - TPA-EYW - LANDING GEAR WILL NOT RETRACT. AIRCRAFT RETURNED TO TPA AND WITHOUT INCIDENT. AIRCRAFT WAS FERRIE D TO MIA WHERE MAINTENANCE REPLACED THE LANDING GEAR CONTROL HANDLE ASSY. (M) 2 L 7 2 4T RT A24CE 1998022600700 19980226 00700 NM 1998 2 26 GAIA9807 1 19980205 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION SKIN SPLICE BS 720C-720D. REPAIR ED PER SRM ON PMS NR 3363. (M) 2 L 7 3 4F A3WE 1998022600701 19980226 00701 NM 1998 2 26 98ZZZM239 1 19980205 A 5320 CHORD BOEING 727 727223 1384074 NM BS 1177 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVE 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION CHORD BS 1177. REPAIRED PER SRM O N PMS NR 5861. REFERENCE GAIA9807. 2 L 7 3 4F A3WE 1998022600702 19980226 00702 NM 1998 2 26 98ZZZM240 1 19980205 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 560-640 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVE 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION SEAT TRACK BS 560-640, LBL 25. RE PAIRED PER SRM ON PMS NR 5846. REFERENCE GAIA9807. 2 L 7 3 4F A3WE 1998022600703 19980226 00703 NM 1998 2 26 98ZZZM241 1 19980205 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 560-640 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION CORROSION SEAT TRACK BS 560-640, LBL 46. RE PAIRED PER SRM ON PMS NR 5845.. REFERENCE GAIA9807. 2 L 7 3 4F A3WE 1998022600704 19980226 00704 NM 1998 2 26 98ZZZM242 1 19980205 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 480-560 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION SEAT TRACK BS 480-560, LBL 24. R EPAIRED PER SRM ON PMS NR 5829. REFERENCE GAIA9807. 2 L 7 3 4F A3WE 1998022600705 19980226 00705 NM 1998 2 26 98ZZZM243 1 19980205 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 680-700 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION SEAT TRACK BS 680-700, LBL 25. R EPAIRED PER SRM ON PMS NR 5819. REFERENCE GAIA9807. 2 L 7 3 4F A3WE 1998022600706 19980226 00706 NM 1998 2 26 98ZZZM244 1 19980205 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1090 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION FLOORBEAM BS 1090, RBL 54-61. RE PAIRED PER SRM ON PMS NR 5803. GAIA9807. 2 L 7 3 4F A3WE 1998022600707 19980226 00707 NM 1998 2 26 98ZZZM245 1 19980205 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 732 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION FLOOR SUPPORT BS 732, LBL 9. REP AIRED PER SRM ON PMS NR 3346. REFERENCE GAIA9807. 2 L 7 3 4F A3WE 1998022600708 19980226 00708 NM 1998 2 26 GAIA9808 1 19980205 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 723 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION FLOOR SUPPORT BS 723, LBL 5. REP AIRED PER SRM ON PMS NR 3361. (M) 2 L 7 3 4F A3WE 1998022600709 19980226 00709 NM 1998 2 26 98ZZZM246 1 19980205 A 5320 CHORD BOEING 727 727223 1384074 NM BS 996 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION CHORD BS 996, LBL 54. REPAIRED P ER SRM ON PMS NR 5793. REF GAIA9808. 2 L 7 3 4F A3WE 1998022600710 19980226 00710 NM 1998 2 26 98ZZZM247 1 19980205 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1110 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION SEAT TRACK BS 1110-1120, RBL 24. REPAIRED PER SRM ON PMS NR 5778. REF GAIA9808. 2 L 7 3 4F A3WE 1998022600711 19980226 00711 NM 1998 2 26 98ZZZM248 1 19980205 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1110 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION SEAT TRACK BS 1110-1130, RBL 24. REPAIRED PER SRM ON PMS NR 5799. REF GAIA9808. 2 L 7 3 4F A3WE 1998022600712 19980226 00712 NM 1998 2 26 98ZZZM249 1 19980205 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 1166 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION ANGLE SUPPORT BS 1166, LBL 2025. REPAIRED PER SRM ON PMS NR 3367. REF GAIA9808. 2 L 7 3 4F A3WE 1998022600713 19980226 00713 NM 1998 2 26 98ZZZM250 1 19980205 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1148 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION FLOORBEAM BS 1148, LBL 10-20. RE PAIRED PER SRM ON PMS NR 3366. REF GAIA9808. 2 L 7 3 4F A3WE 1998022600714 19980226 00714 NM 1998 2 26 98ZZZM251 1 19980205 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 711 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION FLOOR SUPPORT BS 711, RBL 5. REP AIRED PER SRM ON PMS NR 3371. REF GAIA9808. 2 L 7 3 4F A3WE 1998022600715 19980226 00715 NM 1998 2 26 98ZZZM252 1 19980205 A 5320 SUPPORT BOEING 727 727223 1384074 NM BS 723 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6831 20184 THE FOLLOWING ITEMS WERE LEVEL 2 CORROSION FINDINGS DURING INDOC INSPECTION, CORROSION FLOOR SUPPORT BS 723, RBL 5. REP AIRED PER SRM ON PMS NR 3370. REF GAIA9808. 2 L 7 3 4F A3WE 1998022600716 19980226 00716 NM 1998 2 26 GAIA9806A 1 19980202 A 3297 WIRE BOEING 727 727251 138408H NM NLG BROKEN A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 279US 21158 FLT 738, ON APPROACH INTO MHR GOT AN UNSAFE NOSE GEAR INDICATION WHEN THE GEAR WAS EXTENDED. CYCLED SEVERAL TIMES AND N O CHANGE. AN UNEVENTFUL LANDING WAS MADE EXTENDED. CYCLED SEVERAL TIMES AND NO CHANGE. AN UNEVENTFUL LANDING WAS MADE . REPAIRED BROKEN WIRE IN THE LOCK POSITION SWITCH CONDUIT. GROUND CHECKS GOOD IAW 727 MM 32-09-121. (M) 2 L 7 3 4F A3WE 1998022600717 19980226 00717 WP 1998 2 26 98ZZZM253 1 19980201 A 2612 57775631 FIRE LOOP DOUG DC8 DC861 3021952 WP NR 4 ENGINE DEFECTIVE A FXLA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 19 30UA 45888 DURING CRUISE NR 4 ENGINE FIRE WARNING CAME ON. SHUT DOWN ENGINE AND FIRE WARNING CONTINUED. DISCHARGED FIRE EXTINGUIS HER AND FIRE WARNING CEASED. GROUND INSPECTION REVEALED NO EVIDENCE OF FIRE. FOUND DETECTION ELEMENT DEFECTIVE ON LOWE R ELEMENT ASSY. REPLACED ELEMENT ASSY AND CHECKED PNEUMATIC LINES FOR SECURITY. RAN ENGINE AND CHECKED OK. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1998022600718 19980226 00718 NM 1998 2 26 EIAA98006 1 19980203 A 7110 COWLING BOEING 747 747132 1384882 NM NR 4 ENGINE MISSING A EIAA O OTHER D INFLIGHT SEPARATION IN INSP/MAINT 1 NM 09 481EV 19896 HNL - ON POST FLIGHT AT HNL, FOUND FAN COWLING MISSING, AND OTHER SHEET METAL DAMAGE TO NR 4 ENGINE. (M) 2 L 7 4 4F A20WE 1998022600719 19980226 00719 NM 1998 2 26 EIAA98004 1 19980128 A 2730 936005009 PCU BOEING 747 747132 1384882 NM RT ELEV FAILED A EIAA K NONE O OTHER CL CLIMB 1 NM 09 481EV 19896 JFK - DURING CLIMB THROUGH FL300 WITH AUTOPILOT OFF, EXPERIENCED A SHARP NOSE UP JERKING MOTION. LEFT ELEVATOR POSITION INDICATOR INDICATING UP AND DOWN DEFLECTIONS. POSITIONED HYDRAULIC SYSTEM IN FLIGHT CONDITION. HYDRAULIC POWER SWITCH TO CLOSED, THE UNUSUAL MOTION STOPPED. REMOVED AND REPLACED RIGHT INBOARD ELEVATOR POWER CONTROL PACK PER MM 27-31-07, OPS CHECK GOOD. (M) 2 L 7 4 4F A20WE 1998022600720 19980226 00720 NM 1998 2 26 EIAA98003 1 19980126 A 2120 AIR DISTRIBUTION BOEING 747 747132 1384882 NM COCKPIT FUMES A EIAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NM 09 479EV 19898 HKG - FUEL FUMES IN COCKPIT IMMEDIATELY AFTER ROTATION, LASTED 10 MINUTES, PACKS OFF. INSPECTED ACM'S COMPARTMENT, WING S AND APU AREA. NO FUEL LEAK EVIDENCE FOUND. (M) 2 L 7 4 4F A20WE 1998022600721 19980226 00721 NM 1998 2 26 98ZZZM254 1 19980126 A 2820 344N2015 MANIFOLD DUCT BOEING 757 75723APF 1384966 NM RT FUEL TANK CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK INSPECTION, FOUND RIGHT CENTER FUEL TANK FUELING MANIFOLD DUCT CRACKED. PART REPLACD IAW 28-21-01. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1998022600722 19980226 00722 NM 1998 2 26 98ZZZM255 1 19980126 A 2750 113N23631 SUPPORT BEAM BOEING 757 75723APF 1384966 NM LT TE FLAP CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK INSPECTION, FOUND LEFT INBOARD T/E FLAP BELLCRANK SUPPORT BEAM CRACKED. REPAIRED BELLCRANK SUPPORT BEAM ASSY. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998022600723 19980226 00723 SO 1998 2 26 C2XA98CL007 1 19980125 A 3233 1959510006 ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SW 09 31711 120107 CLE - FLT 3114 - CREW REPORTED THAT WHEN GEAR WAS CYCLED UP THEY FELT A STRONG VIBRATION FROM THE LEFT MAIN GEAR WITH TH E 'A' INDICATION REMAINING ILLUMINATED. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE THE LEFT MAIN GEAR ACTUATOR IAW EMB-120 MM 32-32-10. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998022600724 19980226 00724 EU 1998 2 26 C2XA98BT005 1 19980126 A 3350 3011180 POWER PACK AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 BTV - FLT 3685 - ARRIVED BTV ON SCHEDULED TURN, CREW REPORTED FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FO UND A BAD POWER PACK. REMOVED AND REPLACED UNIT WITH SERVICEABLE PART AND OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998022600725 19980226 00725 EU 1998 2 26 C2XA98BT004 1 19980114 A 7797 WIRE AEROSP ATR42 ATR42320 8680930 EU NR 1 ENGINE SHORTED A C2XA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SW 09 14822 163 EWR - FLT 3572 - EN ROUTE PHL-EWR - CREW REPORTED, LOST NR 1 ENGINE EN ROUTE TO EWR. TORQUE AND NP ON NR 1 WENT TO ZERO . TROUBLESHOT ENGINE, SUSPECTED INTERMITTENT TSU SIGNAL. REMOVED AND REPLACED TSU ON NR 1 SIDE. GROUND CHECK GOOD. R EQUESTED TEST FLIGHT. AFTER TEST FLIGHT, ON SHUTDOWN NR 1 TORQUE INCREASED TO OVER 50 PERCENT WHEN CL TO FEATHER DETENT /SCU CIRCUIT BREAKER POPPED. REPAIRED SHORTED WIRING OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998022600726 19980226 00726 EU 1998 2 26 C2XA98BT006 1 19980211 A 6130 FE1595007 PROP BRAKE AEROSP ATR42 ATR42320 8680930 EU RT ENGINE DAMAGED A C2XA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J A Z WARNING INDICATION FLAME/FIRE SIGNIFICANT FAILURE REPORT TX TAXI/GRND HDL 1 SW 09 15818 153 EWR - AFTER INVESTIGATION NEWARK LINE MX FOUND PROP BRAKE SLIPPED AND OVERHEATED CAUSING FIRE IN RIGH ENGINE NACELLE. B OTH FIRE BOTTLES WERE REPLACED. REMOVED AND REPLACED PROP BRAKE ASSY REFERENCED M-602 947757 FOR WORK ACCOMPLISHED. AI RCRAFT RETURNED FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1998022600727 19980226 00727 EU 1998 2 26 C2XA981A007 1 19980202 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FOUND FRAME NR 36 FLOORBEAM CORRODED. MAINTENANCE REPAIRED THE FLOORBEAM USING DOUBLER REPAIRS IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01037. THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998022600728 19980226 00728 EU 1998 2 26 C2XA98IA008 1 19980202 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 97841 280 IAH - DURING C-CHECK INSPECTION, FOUND FLIGHT ATTENDANTS RIGHT SEAT TRACK CORRODED IN SEVERAL AREAS. MAINTENANCE REMOVE D AND REPLACED THE SEAT TRACK IAW ATR-42 STRUCTURAL REPAIR MANUAL 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1998022600730 19980226 00730 CE 1998 2 26 98ZZZM257 1 19980122 A 5753 BULKHEAD BEECH 1900 1900D 1154162 CE RT TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 244YV UE244 ICT MAINTENANCE FOUND SMALL CRACK IN DOVETAIL BULKHEAD. REPAIRED IAW AMWA TO 1900-27-00-0001. ICT MAINTENANCE FOUND 2 CRACKS IN TOP SKIN. REPAIRED IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998022600731 19980226 00731 CE 1998 2 26 98ZZZM258 1 19980115 A 5753 SKIN BEECH 1900 1900D 1154162 CE LT TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 244YV UE244 ICT MAINTENANCE FOUND SMALL CRACK IN TOP SKIN OF LEFT OUTBOARD FLAP AT INBOARD ATTACH BRACKET. REPAIRED IAW AMWA TO 190 0-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998022600732 19980226 00732 NM 1998 2 26 ASAA9810006 1 19980112 A 5210 MECHANISM BOEING 737 737298C 1384490 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 745AS 20794 ANC - PRIOR TO DEPARTURE, THE L1 DOOR WAS HARD TO CLOSE. LUBED ROLLERS AND DOOR HANDLE AND L1 DOOR OPERATED NORMALLY. ( M) 2 L 7 2 4F RT A16WE 1998022600733 19980226 00733 NM 1998 2 26 ASAA9840010 1 19980119 A 5240 69703751 RELEASE ASSY BOEING 737 7374Q8 NM R1 DOOR INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 765AS 25102 PDX - DURING MAINTENANCE CHECK, THE THE R1 DOOR HOLD OPEN RELEASE ASSEMBLY WOULD NOT HOLD DOOR OPEN. REPLACED DOOR HOLD OPEN RELEASE ASSY, OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998022600736 19980226 00736 WP 1998 2 26 ASAA9880003 1 19980102 A 5210 HOOK DOUG DC9 DC982 3022082 WP L1 DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 SEA - AFTER ARRIVAL OF FLT 721 - CREW REPORTED THE L1 DOOR WOULD NOT LATCH OPEN. STAIGHTENED THE GUS LOCK HOOK AND OPER ATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998022600737 19980226 00737 WP 1998 2 26 ASAA9880017 1 19980124 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT GALLEY ILLUMINATE WITH ELECTRICAL POWER OFF. R EPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998022600738 19980226 00738 WP 1998 2 26 ASAA9880016 1 19980123 A 3350 900835A BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY AND FORWARD GALLEY WERE FOUND INOPERA TIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998022600739 19980226 00739 WP 1998 2 26 ASAA9880015 1 19980122 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 014597101 49126 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE VERY DIM AT THE AFT GALLEY. REPLACE D BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998022600740 19980226 00740 WP 1998 2 26 ASAA9880014 1 19980122 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 947AS 53020 LAX - PRIOR TO FLT 513 - CREW REPORTED, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN FIRST CLASS. RE INSTALLED LOOSE ELECTRICAL LIGHT CONNECTOR AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998022600741 19980226 00741 WP 1998 2 26 ASAA9880013 1 19980121 A 3350 014597101 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 940AS 49825 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY EXIT LIGHTS WERE FOUND TO BE VERY DIM AT ROWS 24 THROUGH 27. REP LACED BATTERIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998022600742 19980226 00742 NM 1998 2 26 ASAA9840017 1 19980125 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE FORWARD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REC ONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998022600743 19980226 00743 NM 1998 2 26 ASAA9840016 1 19980123 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO AND AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERA TIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998022600744 19980226 00744 NM 1998 2 26 ASAA9840011 1 19980121 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PDX - DURING MAINTENANCE CHECK, THE FORWARD THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998022600745 19980226 00745 NM 1998 2 26 ASAA9840009 1 19980117 A 3350 S283T0143 BATTERY BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 780AS 25112 SEA - DURING MAINTENANCE CHECK, THE L2 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED POWER SUPPLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998022600746 19980226 00746 NM 1998 2 26 ASAA9810010 1 19980120 A 3350 873203041 TRANSMITTER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST CR CRUISE 1 NM 01 746AS 23123 ANC - FLT 54 - DURING FLIGHT IT WAS REPORTED THAT THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED UNCOMMANDED AND THEN EXTINGUISHED AFTER A FEW MINUTES. REPLACED FORWARD AND AFT TRANSMITTERS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998022600747 19980226 00747 NM 1998 2 26 PCAA9800709 1 19980130 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 RIGHT FLOOR EMERGENCY PROXIMITY LIGHTS INOPERATIVE. SECURED CONNECTORS ON RIGHT LIGHT STRIPS. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998022600748 19980226 00748 NM 1998 2 26 PCAA9800707 1 19980126 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 816EX 329 FIRST THREE FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM BULBS ARE INOPERATIVE. REPAIRED FLOOR EMERGENCY PROXIMITY LIGHTIN G SYSTEM WIRING CIRCUIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998022600749 19980226 00749 EU 1998 2 26 WTAA980024 1 19980225 A 3610 CA061R10S235F80 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A WTAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 17 427UE 811 BFL - SMOKE IN CABIN REPORTED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE DEFERRED LEFT PACK PER MEL 2 1-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING LEFT ENGIEN 4PSI CANNON PLUG . OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A21EU 1998022600750 19980226 00750 EU 1998 2 26 WTAA980018 1 19980203 A 3230 7445B VALVE BAG JETSTM JETSTM3101 1500215 EU GEAR RELEASE TRIPPED A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 418UE 780 BUR - GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO LAX FOR REPAIRS. MAINTENANCE RESET LANDING GEAR BYPASS PIN ON RELEASE VALVE ASSY. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT R ELEASED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998022600751 19980226 00751 EU 1998 2 26 WTAA980021 1 19980204 A 3233 6158E RETRACTION JACK BAG JETSTM JETSTM3101 1500215 EU NLG FAILED A WTAA O OTHER J WARNING INDICATION CL CLIMB 1 WP 17 402UE 734 LAX - NOSE GEAR FAILED TO RETRACT ON INITIAL ATTEMPT. RETRACTION NORMAL ON SECOND ATTEMPT. MAINTENANCE REPLACED NOSE G AER RETRACTION JACK. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998022600752 19980226 00752 EU 1998 2 26 WTAA980020 1 19980203 A 5270 WARNING BAG JETSTM JETSTM3101 1500215 EU DOOR ACTIVATED A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 421UE 804 FAT - DOOR WARNING INDICATION ILLUMINATED ON TAKEOFF. AIRCRAFT RETURNED TO STATION. MAINTENANCE INSPECTED DOOR AND MIC ROSWITCHES. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998022600753 19980226 00753 EU 1998 2 26 WTAA980025 1 19980205 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG DIRTY A WTAA O OTHER N FALSE WARNING DE DESCENT 1 WP 17 429UE 807 LAX - RIGHT MAIN LANDING GEAR DOWN AND LOCK INDICATION FAILED TO ILLUMINATE ON GEAR EXTENSION. MAINTENANCE CLEANED AND LUBED RIGHT MAIN LANDING GEAR DOWNLOCK MICROSWITCH. PERFORMED TEST FLIGHT. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998022600754 19980226 00754 EU 1998 2 26 WTAA980019 1 19980203 A 3040 111267 CONTROLLER BAG JETSTM JETSTM3101 1500215 EU LT WINDSHIELD FAILED A WTAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 17 420UE 788 SFO - LEFT WINDOW HEAT CAPTION ILLUMINATED ON CAP PANEL DURING TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED LEFT WIN DSHIELD HEAT CONTROLLER. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1998022600755 19980226 00755 SO 1998 2 26 WTAA980026 1 19980206 A 5350 RADOME EMB 120 EMB120RT SO FWD FUSELAGE BIRDSTRIKE A WTAA K NONE C F.O.D. AP APPROACH 1 WP 17 271YV 120271 SBA - BIRDSTRIKE ON NOSE DURING APPROACH REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998022600756 19980226 00756 EU 1998 2 26 WTAA980028 1 19980208 A 5230 DOOR BAG JETSTM JETSTM3101 1500215 EU BAGG COMPT NOT LATCHED A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 331CA 793 LAX - POD DOOR CAME OPEN TAKEOFF. AIRCRAFT RETURNED TO STATION. MAINTENANCE INSPECTED POD DOOR AND LATCH MECHANISM FOR DAMAGE. NO DAMAGE NOTED. RESECURED DOOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998022600757 19980226 00757 NM 1998 2 26 USAASB98017 1 19980122 A 5210 DOOR BOEING 737 7372B7 1384560 NM PAX DOOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 269AU 22881 LGA - FLT 324 - DURING CLIMB-OUT OF LGA, AT APPROXIMATELY 17,200 FEET, A LOUD BANG WAS HEARD AROUND THE LEFT FORWARD ENT RY DOOR. PRESSURIZATION COULD NOT KEEP UP WITH THE AIRCRAFT. FLIGHT RETURNED TO FIELD AT LGA AND LANDED WITHOUT FURTHE R INCIDENT. NO EMERGENCY WAS DECLARED. UPON GATE ARRIVAL, CREW COULD NOT GET THE FORWRD ENTRY DOOR OPENED. PASSENGERS WERE DEPLANED VIA STAIRS THROUGH FORWARD RIGHT SERVICE DOOR. (M) 2 L 7 2 4F A16WE 1998022600758 19980226 00758 NM 1998 2 26 USAASB98030 1 19980204 A 7711 EPR INDICATION BOEING 737 7372B7 1384560 NM NR 2 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 280AU 22892 MCI - FLT 878 - FLT RETURNED FIELD AT MCI DUE TO NR 2 ENGINE APPEARED TO LOSE POWER. INDICATION SHOWED INCREASING EGT AND DECREASING EPR. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. NO EMERGENCY WAS DECLARED. MAINTEN ANCE VISUALLY INSPECTED THE NR 2 ENGINE INLET AND EXHAUST. NO DISCREPANCIES NOTED. ACCOMPLISHED POWER RUNUP WITH CREW. ALL ENGINE PARAMETERS AND INDICATIONS WITHIN LIMITS. (M) 2 L 7 2 4F A16WE 1998022600759 19980226 00759 NM 1998 2 26 USAABB98014 1 19980203 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM L-3 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 LAX - FOUND L-3 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE L-3 EXIT IDENTIFIER. (M) 2 L 7 2 4F RT A2NM 1998022600760 19980226 00760 1998 2 26 USAABB98011 4 19980129 A 3414 4039891903 AIRSPEED IND BOEING 767 7672B7 1385107 NM RT COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 654US 25225 CDG - FLT 23 - AFTER TAKEOFF, CREW RECEIVED AIRSPEED FLAG ON FIRST OFFICERS INDICATOR. USING THE ALTERNATE AIR DATA SEL ECTION DID NOT CORRECT THE FAULT. INDICATION DID WORK PROPERLY BELOW 100 KNOTS. FLIGHT RETURNED TO CDG AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICERS AIRSPEED INDICATOR. (M) 2 L 7 2 4F RT A1NM 1998022600761 19980226 00761 NM 1998 2 26 USAA980030 1 19980123 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 7 INCH CRACK, TWO 3.5 INCH CRACKS IN FUSELAGE SKIN AT BS 727 A PLUS 3, T O BS 727B BETWEEN STRINGER 18 AND STRINGER 19 ON LEFT SIDE. INSTALLED DOUBLER, REPAIRED PR SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998022600762 19980226 00762 NM 1998 2 26 USAA980045 1 19980131 A 5330 SKIN BOEING 737 737201 1384454 NM BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 48864 21818 ROA - DURING CX-6 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .625 INCH CRACK BS 945 STRINGER 24L FUSELAGE SKIN. REMOVE D CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 3. (M) 2 L 7 2 4F A16WE 1998022600763 19980226 00763 NM 1998 2 26 USAA980052 1 19980131 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 48864 21818 INT - DURING 1/2C-CHECK, FOUND 4 INCH BY 20 INCH SKIN BULGES AT RIGHT KEEL BEAM SPLICE AT BS 727 THROUGH BS 727A. CUT O UT FUSELAGE SKIN TO GAIN ACCESS TO KEEL BEAM, BLENDED OUT CORROSION, VERIFIED NO CRACKS AND INSTALLED REPAIR PER EA 4359 6. (M) 2 L 7 2 4F A16WE 1998022600764 19980226 00764 NM 1998 2 26 USAA980053 1 19980131 A 5330 SKIN BOEING 737 737201 1384454 NM BS 800/810 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 48864 21818 INT - DURING 1/2C-CHECK, FOUND 2 INCH BY 4 INCH BULGE AT BS 800 AND 2 INCH BY 3 INCH BULGE AT BS 810 SKIN BETWEEN STRING ER 26R AND STRINGER 27R. REMOVED CORROSION AND INSTALLED REPAIRS PER SRM 51-40-3 AND BAC DWG 65-46551. (M) 2 L 7 2 4F A16WE 1998022600765 19980226 00765 1998 2 26 TWRA9806 4 19980204 A 2565 D30441103 SLIDE BOEING 747 747121 1384871 NM 5L DOOR BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 609FF 0158 20354 DURING SCHEDULED SLIDE DEPLOYMENT AT 5L DOOR, SLIDE FAILED TO DEPLOY. ON INVESTIGATION FOUND LEFT SIDE RELEASE CABLE WO ULD NOT PULL PIN OUT OF THE PACKBOARD DUE TO THREADER STRAP BROKEN OFF FROM CABLE. SLIDE WAS REPLACED. (M) 2 L 7 4 4F A20WE 1998022600766 19980226 00766 WP 1998 2 26 TWAA9801801 1 19980203 A 3350 58531 FEEDER STRIP DOUG DC9 DC951 3022051 WP CABIN WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING OVERNIGHT MAINTENANCE CHECK, THE EGRESS LIGHTS IN FORWARD COACH WERE FOUND INOPERATIVE. REPLACED FEEDER ST RIP AT CABIN ROW 8DEF. (M) 2 L 7 2 4F RT A6WE 1998022600767 19980226 00767 WP 1998 2 26 TWAA9801901 1 19980205 A 3230 H50002125218 LATCH ASSY DOUG DC9 DC934 302207E WP NLG WORN A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 927L 48123 STL - FLT 372 - ON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR AND NOSE GEAR UNSAFE LIGHT REMAIN ED ON BUT MAIN GEAR INDICATION NORMAL. PLACED GEAR HANDLE DOWN AND NORMAL INDICATION. RETURNED TO STL. REPLACED MAINT ENANCE BYPASS HANDLE LOCKING LATCH. (M) 2 L 7 2 4F RT A6WE 1998022600768 19980226 00768 EU 1998 2 26 SIMA980333 1 19980202 A 3350 3012017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AE 0574 494 GRR - FORWARD CABIN FLOOR EMERGENCY LIGHTING INOP. RAI POWER SUPPLY FOR FLOOR LIGHTING. PERFORMED OPERATIONAL CHECK SA TISFACTORILY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998022600769 19980226 00769 EU 1998 2 26 REXA98043 1 19980203 A 2730 TRIM SAAB SF340 340B 7860101 EU ELEVATOR OUT OF POSITION A REXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 369PX 340B295 ABORTED TAKEOFF DUE TO CONFIG LIGHT. CREW DISCOVERED TRIM TO BE OUT OF THE GREEN ARC. (M) 2 L 7 2 4T RT A52EU 1998022600770 19980226 00770 1998 2 26 REXA98044 4 19980204 A 3418 STICK PUSHER BAG JETSTM JETSTM3101 1500215 EU E/E COMPT TRIPPED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 302PX 661 BOTH STALL CAP LIGHTS CAME ON IN FLIGHT. NO SHAKER. RESET STICK PUSHER. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998022600771 19980226 00771 NM 1998 2 26 MYWA980002 1 19980201 A 3350 1102833 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 887MA 21857 DURING PREFLIGHT INSPECTION, FOUND FORWARD ENTRANCE EMERGENCY EXIT LIGHT AT BOTTOM RT SIDE INOP. FOUND CONNECTION UNDER LIGHT DIRTY, CLEANED AND REINSTALLED. OPS CHECK GOOD 33-30-10. (M) 2 L 7 3 4F A3WE 1998022600772 19980226 00772 1998 2 26 98ZZZM259 4 19980116 A 3425 6229681001 EFIS DISPLAY BEECH 1900 1900D 1154162 CE INSTRUMENT PANEL SHORTED A JJBA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 01 848CA UE53 ON TAXI OUT FROM GATE, SMOKE WAS OBSERVED COMING FROM RIGHT SIDE OF INSTRUMENT PANEL. PASSENGERS WERE EVACUATED FROM AI RCRAFT. FOUND EFIS DISPLAY SHORTED. (M) 2 L 7 2 4T RT A24CE 1998022600773 19980226 00773 CE 1998 2 26 98ZZZM260 1 19980130 A 3040 MF24166D1 RELAY BEECH 1900 1900D 1154162 CE COCKPIT SHORTED A JJBA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 01 842CA UE41 ELECTRICAL ODOR FROM BEHIND INSTRUMENT PANEL DURING DESCENT FROM 4000 FEET. FOUND RELAY K119 WINDSHIELD HEAT SHORTED. 2 L 7 2 4T RT A24CE 1998022600774 19980226 00774 NM 1998 2 26 GAIA9810 1 19980209 A 3350 BULB BOEING 727 727214 138407R NM CABIN FAILED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 750US 21512 UPON ARRIVAL AT CLT, THE L-1 DOOR EMERGENCY EXIT LIGHT WAS REPORTED INOP. REMOVED AND REPLACED BULBS. SYSTEM TESTED AN D CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998022600775 19980226 00775 NM 1998 2 26 GAIA9809 1 19980206 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6827 20180 UPON ARRIVAL TOL, CREW REPORTS EMERGENCY EXIT LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EXIT LIGHT IAW MM ATA 33-5 0. SYSTEM CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998022600776 19980226 00776 NM 1998 2 26 98ZZZM261 1 19980126 A 5280 DOOR BOEING 757 75723APF 1384966 NM LT MLG CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND L/E AT LEFT INBOARD GEAR DOOR CRACKED AND DELAMINATED. REPAIRED PER SRM 52-80-02. A/C RETURNED T O SERVICE. (M) 2 L 7 2 4F RT A2NM 1998022600777 19980226 00777 NM 1998 2 26 BJNA980201 1 19980202 A 5210 90100722 SNUBBER BOEING 737 737214 138446R NM PAX DOOR MISINSTALLED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 20156 AIR LEAK IN L1 DOOR, GROUND PRESSURIZED AIRCRAFT. FOUND LOWER DOOR HINGE SNUBBER INSTALLED BACKWARDS. REPOSITIONED SNU BBER IAW BOEING MM CHAPTER 52-11-0 PAGE 406. REPLACED FLAPPER SEAL IAW STANDARD PRACTICES. OPS NORMAL. (M) 2 L 7 2 4F A16WE 1998022600778 19980226 00778 1998 2 26 USAAD98015 4 19980121 A 2565 13621224 SLIDE DOUG DC9 DC931 3022065 WP AFT FUSELAGE SLOW TO OPERATE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918VJ 48138 BOS - AFT ESCAPE SLIDE REQUIRED 15 SECONDS TO DEPLOY DURING TEST. MAINTENANCE REPLACED THE SLIDE ASSY. (M) 2 L 7 2 4F A6WE 1998022600779 19980226 00779 NM 1998 2 26 USAASB98025 1 19980130 A 5610 5893543110 WINDSHIELD BOEING 737 737201 1384454 NM RT COCKPIT DEFECTIVE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 236US 14794 22352 ORF - FLT 1279 - CAPT REPORTED VIA ACARS THAT FLIGHT WAS RETURNING TO FIELD AT ORF DUE TO A LOUD AIRLEAK COMING FROM THE F/O'S WINDSHIELD. NOISE WAS TOO LOUD TO COMMUNICATE IN COCKPIT. CLIMBED TO 5,000 FEET TO SEE IF THERE WOULD BE ANY CH ANGE, BUT NOISE GOT WORSE. FLIGHT RETURNED TO FIELD AT ORF AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLA RED. MAINTENANCE REMOVED AND REPLACED THE F/O'S FORWARD WINDSHIELD IN ASSOCIATION WITH MM. PRESSURIZED AIRCRAFT. NO L EAKS NOTED. (M) 2 L 7 2 4F A16WE 1998022600780 19980226 00780 WP 1998 2 26 USAA980050 1 19980125 A 5311 BELLFRAME DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804US 44832 48052 PIT - DURING Q-6 CHECK, FOUND .5 INCH CRACK AT TAIL INERIOR BELLFRAME, TAIL INTERIOR STATION 1437. CUT OUT DAMAGED SECT ION AND SPLICED IN A NEW SECTION PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1998022600781 19980226 00781 WP 1998 2 26 USAA980048 1 19980125 A 5311 BELLFRAME DOUG DC9 DC981 3022081 WP BS 1297 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804US 44832 48052 PIT - DURING Q-6 CHECK, FOUND ONE .5 INCH CRACK AT BELLFRAME AT STATION 1297, LONGERON 8L. CUT OUT DAMAGED SECTION AND SPLICED IN A NEW SECTION PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1998022600782 19980226 00782 WP 1998 2 26 USAA980049 1 19980125 A 5330 SKIN DOUG DC9 DC981 3022081 WP S 769 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 804US 44832 48052 PIT - DURING Q-6 CHECK, FOUND 1 INCH BY 1 INCH AND 1.5 INCH BY 2 INCH AREAS OF CORROSION UNDE RT WING TO FUSELAGE FILLET PANEL ON SKIN, STATION 769. BLENDED AREAS AND INSTALLED DOUBLERS PER SRM 53-04 FIG 53. CORROSION LEVEL 1, CORROSIN TA SK NR C22-57301. (M) 2 L 7 2 4F A6WE 1998022600783 19980226 00783 NM 1998 2 26 USAA980040 1 19980123 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK FLOORBEAM BS 520, RBL 24. INSTALLED DOUBLER AND MOD REPAI RED PER EA 43461. (M) 2 L 7 2 4F A16WE 1998022600784 19980226 00784 NM 1998 2 26 USAA980038 1 19980123 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 5 INCH SKIN BULGED FUSELAGE SKIN BS 727, STRINGER 27L, STRING ER 27R BELLY. INSTALLED DOUBLER AND FILLERS, REPAIRED PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998022600785 19980226 00785 NM 1998 2 26 USAA980037 1 19980123 A 5320 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK BS 727 RT STRINGER 18A FORWARD FASTENER HOLE CRACKE D FORWARD FLANGE OF OUTBOARD CHORD. INSTALLED CHORD KIT, REPAIRED PER EA 5394GO68 CARD NR 2-21-93834. (M) 2 L 7 2 4F A16WE 1998022600786 19980226 00786 NM 1998 2 26 USAA980036 1 19980123 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 CRACKS, .5 INCH AND 1.5 INCHES LONG AT BS 520 RBL 45 FLOORBEAM. INSTA LLED KIT, REPAIRED PER EA 43461. (M) 2 L 7 2 4F A16WE 1998022600787 19980226 00787 NM 1998 2 26 USAA980035 1 19980123 A 5312 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 LBL 4.5 AT LOWER LEFT ANT MOUNT BULKHEAD WEB. STOP DRILLED, NDT INSPECTION AND INSTALLED FILLERS AND DOUBLER PER TR 53-10-11. (M) 2 L 7 2 4F A16WE 1998022600788 19980226 00788 NM 1998 2 26 USAA980034 1 19980123 A 5320 FRAME BOEING 737 737201 1384454 NM FWD DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK FORWARD DOOR FRAME AT UPPER HINGE CUTOUT. STOP DRILLED CRACK, NDT INSPECTION, INSTALLED REPAIR DOUBLER, REPIRED PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998022600789 19980226 00789 NM 1998 2 26 USAA980033 1 19980123 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 520, LBL 24 FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER EA 43461. (M) 2 L 7 2 4F A16WE 1998022600790 19980226 00790 NM 1998 2 26 USAA980032 1 19980123 A 5311 FRAME BOEING 737 737201 1384454 NM BS 990 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORRODED AREA BS 990 WL 208 STRINGER 17R FRAME. INSTAL LED FILLER AND DOUBLER, REPAIRED PER SRM 51-40-3. CORROSION TASK NR C53-107-07, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998022600791 19980226 00791 NM 1998 2 26 USAA980031 1 19980123 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 344-348 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA BS 344 TO BS 348 STRINGER 25L. SPLICED I N NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998022600792 19980226 00792 NM 1998 2 26 USAA980028 1 19980123 A 5511 SPAR LUG BOEING 737 737201 1384454 NM RT HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DUIRNG Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVIS LUG B ORE RT LOWER HORIZONTAL STABILIZER. INSTALLED OVERSIZED BUSHINGS, REPAIRED PER EA 43494. (M) 2 L 7 2 4F A16WE 1998022600793 19980226 00793 NM 1998 2 26 USAA980029 1 19980123 A 5511 SPAR LUG BOEING 737 737201 1384454 NM LT HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVEIS LUG BORE LEFT HORIZONTAL LOWER STABILIZER. INSTALLED OVERSIZED BUSHINGS, REPAIRED PER EA 43494. (M) 2 L 7 2 4F A16WE 1998022600794 19980226 00794 NM 1998 2 26 USAA980027 1 19980123 A 5320 CLIP BOEING 737 737201 1384454 NM BS 345-363 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED AREA E/E BS 345 TO BS 363 STRINGER AND TIE CLIP. INSTALLED STR INGER SPLICE REPAIR AND REPLACED TIE CLIP PER DRAWING 69-46831-1 AND SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSI ON LEVEL 2. (M) 2 L 7 2 4F A16WE 1998022600795 19980226 00795 NM 1998 2 26 USAA980026 1 19980123 A 5330 SKIN BOEING 737 737201 1384454 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH AFT SERVICE DOOR CUTOUT UPPER HINGE, UPPER FORWARD END SKI N. INSTALLED DOUBLERS, REPAIRED PER EA 43495. (M) 2 L 7 2 4F A16WE 1998022600796 19980226 00796 NM 1998 2 26 USAA980025 1 19980123 A 5330 SKIN BOEING 737 737201 1384454 NM BS 947 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND PREVIOUS DOUBLER STATION 947 STRINGER 20L TO STRINGER 21L SKIN. INSTALL ED EXT SKIN REPAIR, REPAIRED PER EA 43493. (M) 2 L 7 2 4F A16WE 1998022600797 19980226 00797 NM 1998 2 26 USAA980024 1 19980123 A 5511 SPAR BOEING 737 737201 1384454 NM RT HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY .125 INCH CORRODED AREA RT HORIZONTAL STABILIZER UPPER OUTBOAR D REAR SPAR TERMINAL LUG. INSTALLED OVERSIZED BUSHING, REPAIRED PER EA 43472. (M) 2 L 7 2 4F A16WE 1998022600798 19980226 00798 NM 1998 2 26 USAA980022 1 19980123 A 5311 FRAME BOEING 737 737201 1384454 NM BS 787 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND APPROX 2 INCH BY 2 INCH AREA OF CORROSION LOWER CHORD OF FRAME AT STATIO N 787 LEFT KEEL BEAM. INSTALLED REPAIR DOUBLER AND ATTACH ANGLES, REPAIRED PER SRM 53-10-4, FIG 9. CORROSION TASK NR C 53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998022600799 19980226 00799 NM 1998 2 26 USAA980021 1 19980123 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 968 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION FOUND APPROX 2 INCH BY 2 INCH AREA CORRODED STRINGER 25L AT STATION 968. INSTA LLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998022600800 19980226 00800 NM 1998 2 26 USAA980019 1 19980123 A 5511 SPAR BOEING 737 737201 1384454 NM LT HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION SPAR CLEVIS LUG LEFT UP PER HORIZONTAL STABILIZER. INSTALLED OVERSIZED BUSHING, REPAIRED PER EA 43494. (M) 2 L 7 2 4F A16WE 1998022600801 19980226 00801 NM 1998 2 26 USAA980020 1 19980123 A 5511 SPAR BOEING 737 737201 1384454 NM RT HORIZ STAB CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .125 INCH BY 1 INCH CORRODED AREA CENTER SECTION FRONT SPAR CLEVIS LUG B ORE RT HORIZONTAL UPPER STABILIZER. INSTALLED OVERSIZED BUSHING, REPAIRED PER 43494. (M) 2 L 7 2 4F A16WE 1998022600802 19980226 00802 NM 1998 2 26 USAA980039 1 19980123 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 907-927 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORRODED AREA 20 INCHES BS 907-927 STRINGER 25L. INSTALLED STRINGER REP AIR SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998022600803 19980226 00803 NM 1998 2 26 USAA980023 1 19980123 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 907-927 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 234US 46263 22274 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 4 INCH BY 1 INCH CORRODED AREA BS 907 - BS 927, S27R STRINGER. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998022600804 19980226 00804 NM 1998 2 26 USAA980046 1 19980128 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 284AU 37413 23131 ROA - DURING CX-4 CHECK, FOUND 2 INCH BY 6 INCH CORROSION AT BS 967 STRINGER 26 LEFT. REMOVED CORROSION AND INSTALLED S TRINGER SPLICE PER SRM 53-10-3 PAGE 3. (M) 2 L 7 2 4F A16WE 1998022600805 19980226 00805 NM 1998 2 26 USAA980018 1 19980126 A 5330 SKIN BOEING 737 737201 1384454 NM BS 750 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 40953 22756 ROA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND .3125 INCH CRACK BS 750 STRINGER 19R FUSELAGE SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998022600806 19980226 00806 NM 1998 2 26 USAA980041 1 19980126 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 40953 22756 ROA - DURING CX-3 CHECK, FOUND .375 INCH CRACK ON FUSELAGE SKIN AT BS 727 A PLUS 12 STRINGER 18 RT. INSTALLED DOUBLER P ER SRM 53-30-3 FIGURE 1. (M) 2 L 7 2 4F A16WE 1998022600807 19980226 00807 NM 1998 2 26 USAA980042 1 19980126 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 40953 22756 ROA - DURING CX-3 CHECK, FOUND 1 INCH CRACK ON FUSELAGE SKIN AT BS 727 PLUS B PLUS 10 STRINGER 17 RIGHT. DETECTED BY VI SUAL/EDDY CURRENT. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (M) 2 L 7 2 4F A16WE 1998022600808 19980226 00808 NM 1998 2 26 USAA980043 1 19980126 A 5330 SKIN BOEING 737 737201 1384454 NM BS 750 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 249US 40953 22756 ROA - DURING CX-3 CHECK, FOUND .75 INCH CRACK ON FUSELAGE SKIN AT BS 750 STRINGER 18 LEFT. DETECTED BY VISUAL/EDDY CURR ENT. INSTALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (M) 2 L 7 2 4F A16WE 1998022600809 19980226 00809 NM 1998 2 26 USAA980047 1 19980128 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 41734 22755 CLT - DURING VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.1 INCH CRACK AT A PREVIOUS REPAIRED AREA FWD ADN AFT BS 767 S TRINGER 18L ON THE SKIN. FWD AREA CUTOUT 6 INCH BY 6 INCH AFT AREA 4 INCH BY 2 INCH CUTOUT. INSTALLED DOUBLER PER REPA IR DOCUMENT SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1998022600810 19980226 00810 NM 1998 2 26 USAA980017 1 19980116 A 5330 SKIN BOEING 737 737201 1384454 NM ENTRY DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 45591 22275 ROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER SKIN. DOUBLE R REPAIR INSTALLED, REPAIRED PER EA 61143. (M) 2 L 7 2 4F A16WE 1998022600811 19980226 00811 NM 1998 2 26 USAA980016 1 19980116 A 5330 SKIN BOEING 737 737201 1384454 NM BS 945 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 45591 22275 ROA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK STRINGER 24L, STATION 945 SKIN. INSTALLED DOUBLER, REP AIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998022600812 19980226 00812 NM 1998 2 26 USAASB98028 1 19980201 A 3350 110049 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 505AU 23380 CLT - PILOT REPORTED, THE EMERGENCY EXIT LIGHTING AT THE FORWARD CABIN FLOOR SECTION WAS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998022600813 19980226 00813 SO 1998 2 26 RAAA98E9008 1 19980223 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO PAX CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 17 AND 21 FLOOR PROXIMITY EGRESS LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 4 4T 4A22 1998022600814 19980226 00814 WP 1998 2 26 CALA9800310 1 19980224 A 5320 SHEAR TIES DOUG DC10 DC1010 3022110 WP BS 1701-1741 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND SHEAR TIES CORRODED IN MID CARGO COMPARTMENT AT STA 1701, 1721, AND 1741, LONGERON 48L. THE SHEAR TIES WERE REMOVED, NEW SHEAR TIES WERE FABRICATED AND INSTALLED IAW SRM 51-10-00 AND 53-10-00. 2 L 7 3 4F A22WE 1998022600815 19980226 00815 WP 1998 2 26 CALA9800311 1 19980224 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1139-1159 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 43L CORRODED IN CENTER ACCESSORY COMPARTMENT FROM STA 1139 TO 1159. A NEW LONGERON WAS INSTAL LED IAW SRM 51-31-01 AND 53-10-00. 2 L 7 3 4F A22WE 1998022600816 19980226 00816 WP 1998 2 26 CALA9800312 1 19980224 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1701-1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND STRINGER IN MID CARGO LOWER BILGE AREA CORRODED AT LONGERON 50R, STA 1701 TO 1721. THE CORRODED AREA W AS REMOVED, A STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00. 2 L 7 3 4F A22WE 1998022600817 19980226 00817 WP 1998 2 26 CALA9800313 1 19980224 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1661-1681 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1661 TO 1681 BETWEEN LONGERON 43 AND 44L. THE CORRODED AREA WAS CUT OUT, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, 51-21-01, AND 51-41-01. 2 L 7 3 4F A22WE 1998022600818 19980226 00818 WP 1998 2 26 CALA9800314 1 19980224 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1018 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 45R ATTACH ANGLE IN FORWARD BELLY COMPARTMENT BILGE AREA CORRODED AT STA 1018. THE ATTACH ANG LE WAS REMOVED AND REPLACED IAW SRM 51-30-00. 2 L 7 3 4F A22WE 1998022600819 19980226 00819 WP 1998 2 26 CALA9800315 1 19980224 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 49R CORRODED AT STA 1841. THE CORRODED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 5 3-10-00. 2 L 7 3 4F A22WE 1998022600820 19980226 00820 WP 1998 2 26 CALA9800316 1 19980224 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON UPPER CAP OF FLOORBEAM IN C-2 CARGO COMPARTMENT AT STA 1701, RBL 37. THE CORROSION WAS RE MOVED IAW SRM 51-21-01. DOUBLERS AND FILLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 53-60-01. 2 L 7 3 4F A22WE 1998022600821 19980226 00821 WP 1998 2 26 CALA9800317 1 19980224 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1741 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 1741, STRINGER 47L. THE FASTENERS WERE REMOVED IAW SRM 51-30-01. A SECT ION OF STRINGER WAS CUT OUT IAW SRM 53-10-00. HOLES WERE DRILLED IAW SRM 53-10-00. THE NEW PARTS WERE INSTALLED IAW SR M 51-21-01 AND 53-10-00. 2 L 7 3 4F A22WE 1998022600822 19980226 00822 WP 1998 2 26 CALA9800318 1 19980224 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 48L CORRODED AT STA 1721. THE CORRODED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-10-0. NEW HOLES WERE DRILLED ON LONGERON, A SPLICE ANGLE WAS FABRICATED, AND PARTS WERE INSTALLED IAW SRM 53-10-0 AND ECRA 5310-03 680. 2 L 7 3 4F A22WE 1998022600823 19980226 00823 WP 1998 2 26 CALA9800319 1 19980224 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FINGER DOUBLER CORRODED AT STA 1721, LONGERON 48L. THE FASTENERS WERE REMOVED IAW SRM 51-31-0. A FING ER DOUBLER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND ECRA 5310-03680. 2 L 7 3 4F A22WE 1998022600824 19980226 00824 WP 1998 2 26 9803171157 1 19980222 A 7830 TR UNIT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE MALFUNCTIONED A NWAA E ENGINE SHUTDOWN O OTHER LD LANDING 1 GL 01 157US 46766 686171 DURING LANDING ROLLOUT, THE NR 3 ENGINE THRUST REVERSER DID NOT STOW AND THE ENGINE COMPRESSOR STALLED. THE EGT REACHED 1000C AND THE ENGNE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE AND DEFERRED THE REVERSER PER MEL 78-1A. THE REVE RSER WAS STOWED AND DEACTIVATED PER MEL DDG. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998022600825 19980226 00825 NE 1998 2 26 9803189139 2 19980221 A 7230 COMPRESSOR DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7 52053 NE LT ENGINE STALLED A NWAA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 01 948L 47049 657567 AS AIRCRAFT LEVELED OFF AT 35,000 FEET DURING POWER REDUCTION, THE LEFT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW FURT HER REDUCED LEFT ENGINE POWER. STALLS CEASED AND AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1998022600826 19980226 00826 NM 1998 2 26 9803192712 2 19980219 A 7261 626447 RELIEF VALVE BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17R 52049 NE CENTER ENGINE FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 712RC 22020 689858 DURING CLIMB AT 29,000 FEET, THE CENTER ENGINE OIL PRESSURE INDICATION DECREASED TO 30 PSI. AIRCRAFT DIVERTED TO SLC AN D LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER ENGINE OIL PRESSURE RELIEF VALVE. ENGINE OPERATIONA L CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998022600827 19980226 00827 WP 1998 2 26 9803209906 1 19980220 A 3610 5958765503 MANIFOLD DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE LT ENGINE CRACKED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 956N 47252 648761 DURING CLIMB AT 800 FEET, THE LEFT ENGINE EXPERIENCED A FIRE WARNING INDICATION. CREW RETARDED THE LEFT ENGINE THROTTLE SETTING AND INDICATION CEASED. AIRCRAFT RETURNED TO GCM AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE 13TH STAGE MANIFOLD ON THE LEFT ENGINE. ENGINE OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998022600828 19980226 00828 WP 1998 2 26 9803219997 1 19980223 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT FORWARD CABIN AFT AISLE AND AT ROWS 2 AND 3 INOPE RATIVE. REPLACED BATTERIES IN PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600829 19980226 00829 WP 1998 2 26 9803229965 1 19980223 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 911RW 47149 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600830 19980226 00830 WP 1998 2 26 9803239965 1 19980223 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 911RW 47149 FLIGHT ATTENDANT REPORTED, EMERGENCY LIGHTS AT ROWS 11, 12, AND 13 INTERMITTENTLY ILLUMINATE WITH SWITCH IN THE OFF POSI TION. REPLACED BATTERIES AND CHARGER AT ROW 12 ON EFT LEFT SIDE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600831 19980226 00831 WP 1998 2 26 9803249970 1 19980220 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9334 47247 FLIGHT ATTENDANT REPORTED, AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600832 19980226 00832 WP 1998 2 26 9803259933 1 19980222 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1334U 47280 DURING LINE MAINTENANCE INSPECTION, FOUND AFT FLIGHT ATTENDANT, TAIL COMPARTMENT AND NACELLE EMERGENCY LIGHTS INOPERATIV E. REPLACED POWER SUPPLY AND CHARGER TO B5-27 UNIT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600833 19980226 00833 WP 1998 2 26 9803269609 1 19980223 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998022600834 19980226 00834 SO 1998 2 26 COMA9810047 1 19980223 A 3230 12038594001 CONTROL BOX EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 267CA 12833 2891 120259 LANDING GEAR WILL NOT RETRACT. REPLACED THE LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1998022600835 19980226 00835 SO 1998 2 26 COMA9810048 1 19980222 A 3230 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 269CA 19373 1139 120263 UNABLE TO RAISE LANDING GEAR AFTER TAKEOFF. BOTH INTRANSIT RED AND GREEN SAFE INDICATORS WERE ON. REPLACED THE LANDING GEAR RELAY BOX. 2 L 7 2 4T RT A31SO 1998022600836 19980226 00836 EA 1998 2 26 COMA9860047 1 19980221 A 3411 481500502 LINE CNDAIR CL600 CL6002B19 EA NR 1 PITOT LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 915CA 336 7013 THE CAPTINS AIRSPEED INDICATOR DID NOT RESPOND DURING TAKEOFF, INDICATION STUCK AT 40 KNOTS. INSPECTED AND FOUND NR 1 P ITOT LINE LOOSE AT NR 1 ADC. RECONNECTED NR 1 PITOT LINE AND PERFORMED PITOT/STATIC CHECK. 2 L 7 2 4F RT A21EA 1998022600837 19980226 00837 WP 1998 2 26 UPS98825863 1 19980217 A 5320 575071571 SUPPORT DOUG DC8 DC871F 302199D WP BS 1040-1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, FS 1040 TO 1060 ABOVE STR 33R FLOOR SUPPORT ANGLE HAS CORROSION REMOVAL WENT OUT OF LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 53-11-0 AND 51-1-21. 2 L 7 4 4F RT 4A25 1998022600838 19980226 00838 NM 1998 2 26 UPS98225871 1 19980219 A 5753 65192491 TRACK BOEING 727 727247 138408F NM NR 6 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-SI, CORROSION (C57-581-06.00-04) NR 6 T/E FLAP TRACK SPOILER BEAM MOUNT PAD CORRODED. REMOVED CORRODED FLAP TRACK AND INSTALLED SERVICABLE FLAP TRACK IAW MM 27-51-31, REF TC NR C57-581-04-4D. 2 L 7 3 4F A3WE 1998022600839 19980226 00839 NM 1998 2 26 UPS98225872 1 19980211 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM FASTENER HOLE BS 380, LBL 50, WL 208. MECHANICALLY REM OVED CORROSION, FOUND OUT OF LIMITS PER SRM 53-10-2, 53-10-6. REPAIRED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998022600840 19980226 00840 NM 1998 2 26 UPS98225873 1 19980210 A 5320 INTERCOSTAL BOEING 727 727247 138408F NM BS 546 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE-SI, CORROSION (SDN C53-111-01.00-02) ON INTERCOSTAL RBL 27, BS 546, WL 147 FWD CARGO BAY. CORROSION FOU ND TO BE OUT LIMITS PER SRM 53-10-1. FABRICATED PART PER SRM 51-10-3 AND INSTALLED PER SRM 51-30-2, SRM 51-40-2 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1998022600841 19980226 00841 NM 1998 2 26 UPS98225874 1 19980210 A 5754 65172887 RIB BOEING 727 72751C 1384015 NM NR 3 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, WHILE WORKING CARD NR 465720 FOUND CRACKED RIB ON L/W NR 3 SLAT AT SLAT STA 128 TO 950. REMOVED CRA CKED RIB, REPLACED WITH NEW RIB IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998022600842 19980226 00842 NM 1998 2 26 UPS98225875 1 19980204 A 5315 FLOORBEAM BOEING 727 72751C 1384015 NM BS 420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AND GOUGE ON BS 420 FLOORBEAM LBL 19, RBL 56, WL 208. CORROSION FOUND OUT OF LIMITS PER SRM 53-10-1. COMPLETED STANDARD UPPER CHORD REPAIR PER SRM 53-10-8, SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1998022600843 19980226 00843 NM 1998 2 26 UPS98225876 1 19980221 A 2720 65207883 QUADRANT BOEING 727 72751C 1384015 NM RUDDER CONTROL CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, AFT RUDDER CONTROL QUADRANT AREAS OF CORROSION AROUND FASTENERS. CORROSION REWORK OUT OF LIMITS. REMOVED OVER .75 OF THICKNESS. REMOVED AND REPLACED AFT RUDDER QUADRANT IAW MM 27-20-71. 2 L 7 3 4F A3WE 1998022600844 19980226 00844 NM 1998 2 26 UPS98225877 1 19980208 A 5320 7075T6 INTERCOSTAL BOEING 727 72751C 1384015 NM BS 211-220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON INTERCOSTAL BS 211.8 TO 219.8, LBL 25, WL 176. CORROSION REWORK OUT OF LIMITS IAW SRM 53-10-1. REPLACED INTERCOSTAL STA 211.8 TO 219.8, LBL 25, WL 176 IAW SRM 51-20-1, 51-30-2, 51-10-3. 2 L 7 3 4F A3WE 1998022600845 19980226 00845 NM 1998 2 26 UPS98225878 1 19980204 A 5315 BAC14902831 FLOORBEAM BOEING 727 72751C 1384015 NM BS 400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM BS 400, LBL 25, WL 208, UPPER FLANGE. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. COMPLETED STANDARD T-CHORD REPAIR PER SRM 53-10-8, SRM 51-30-2 AND MM 51-20-31. 2 L 7 3 4F A3WE 1998022600846 19980226 00846 NM 1998 2 26 UPS98225879 1 19980204 A 5315 BAC15123397 FLOORBEAM BOEING 727 72751C 1384015 NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) AND BARE METAL ON FLOORBEAM BS 480, LBL 45 TO 59, WL 208. CORROSION FO UND TO BE OUT OF LIMITS PER SRM 53-10-1. COMPLETED STANDARD UPPER CHORD SPLICE PER SRM 53-10-8, FIG 5, SRM 51-30-2 AND MM 51-20-21. 2 L 7 3 4F A3WE 1998022600847 19980226 00847 NM 1998 2 26 UPS98425886 1 19980224 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-N/A, CREW UPPER DECK EMERGENCY DOOR UPPER DOOR FRAME LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, OP S CHECK GOOD. 2 L 7 4 4F A20WE 1998022600848 19980226 00848 WP 1998 2 26 UPS98825880 1 19980211 A 5320 3755822505 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, SHEAR TIE FITTING AT FS 300 LONG 30L HAS MODERATE CORROSION AROUND FASTENERS. REMOVED AND REPLACED S HEAR TIE FITTING IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998022600849 19980226 00849 WP 1998 2 26 UPS98825881 1 19980211 A 5320 4758514519N TIE FITTING DOUG DC8 DC871F 302199D WP BS 1232 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, FS 1232 AT STR 33R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D . 2 L 7 4 4F RT 4A25 1998022600850 19980226 00850 WP 1998 2 26 UPS98825882 1 19980209 A 5320 4612650N FITTING DOUG DC8 DC871F 302199D WP BS 8 LT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LONGERON 33L FITTING AT FS 8 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998022600851 19980226 00851 WP 1998 2 26 UPS98825883 1 19980209 A 5320 47117221 FITTING DOUG DC8 DC871F 302199D WP BS 8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LONGERON 34R FITTING AT FS 8 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998022600853 19980226 00853 WP 1998 2 26 UPS98825885 1 19980211 A 5320 36431112 FITTING DOUG DC8 DC871F 302199D WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, MAIN CARGO DECK UPPER SURFACE WING CTR SECTION FS 781 RBL 62 CORROSION BETWEEN 2 FASTENERS AND CRACKE D. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998022600854 19980226 00854 EU 1998 2 26 WWMA9800037 1 19980221 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 309AE 340B309 DURING PREFLIGHT, THE FLIGHT ATTENDANTS EMERGENCY ARM LIGHT FAILED TO ILLUMINATE. REPLACED BULB. 2 L 7 2 4T RT A52EU 1998022600855 19980226 00855 EU 1998 2 26 WWMA9800035 1 19980223 A 2530 38512 RECEPTICLE SAAB SF340 340B 7860101 EU GALLEY BURNED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 332AE 340B332 CREW REPORTED ELECTRICAL SMELL IN THE GALLEY AREA. SUSPECTED THE COFFEE JUG. MAINTENANCE FOUND THE NR 1 HOT JUG RECEPT ICLE BURNED. REPLACED THE RECEPTICLE AND THE NR 1 HOT JUG. 2 L 7 2 4T RT A52EU 1998022600856 19980226 00856 EU 1998 2 26 WWMA9800034 1 19980222 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 324AE 340B324 DURING PREFLIGHT, OVERHEAD EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE PERFORMED GROUND TEST OF EMERGENCY L IGHT SYSTEM AND FOUND ALL LIGHTS TO ILLUMINATE PROPERLY IAW SAAB AMM 33-55-00. 2 L 7 2 4T RT A52EU 1998022600857 19980226 00857 NM 1998 2 26 QXEA9800083 1 19980223 A 3350 10005511 LIGHT GRIMES 82510202001 DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 841PH 82 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED OVERHEAD EMERGENCY LIGHT ASSEMBLY, OP'S CHECK NORMAL AS PER DE HAVI LLAND MM. 2 H 7 2 4T RT A13NM 1998022600858 19980226 00858 NM 1998 2 26 98FDEA00136 1 19980224 A 2612 FIRE DETECTOR BOEING 727 727233 138408A NM APU FAILED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SO 25 278FE 22345 AUXILIARY POWER UNIT FIRE WARNING LIGHT (NO AURAL) AND GLARESHIELD LIGHT ILLUMINATED AT FLIGHT LEVEL 310 0+30 MINUTES. A UXILIARY POWER UNIT FIRE HANDLE PULLED AND DISCHARGED AUXILIARY POWER UNIT FIRE BOTTLE. *S/D* FOUND RECTIFIER/DIODE AS SY RACK RECEPTACLE E1-5 AND PLUG E2 EATEN UP WITH CORROSION. REPLACED BLOCKING RECTIFIER R421. REMOVED AND REPLACED RE LAY R175 AND TRANSFORMER T147. FIRE TEST WORKS FOR 3 SECONDS,THEN WARNING STOPS WITH SWITCH STILL IN THE TEST POSITION. NEEDS NEW APU FIRE DETECTOR OPERATING POWER UNIT M438. REMOVED AND REPLACED POWER UNIT FIRE AND OVERHEAT DETECTOR. FI RE TEST ON APU OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998022600859 19980226 00859 NM 1998 2 26 98FDEA00137 1 19980224 A 4950 BLEED AIR DUCT DOUG MD11 MD11F 3023600 NM APU CONTAMINATED A FDEA A J UNSCHED LANDING DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 609FE 48549 SHORTLY AFTER TAKEOFF, EXPERIENCED AN UNKNOWN ODOR THE F/O AND RFO EXPERIENCED A BURNING SENSATION IN THE EYES. CREW WE NT ON 100 PERCENT O2 AND ACCOMPLISHED ALL CHECKLIST ITEMS. RETURNED TO EWR. COMPLIED WITH CHECKLIST AND DUMPED APPROX 65.0 LBS FUEL. REMOVED (3) COALESCER SOCKS FROM PACKS, FOUND THEM TO BE DIRTY WITH OIL RESIDUE. RAN NR (3) ENGINE AND ALL PACKS PER M/M 21-53-00-7. INSTALLED (3) NEW COALESCER SOCKS AND RAN ALL ENGINES FOR 20 MIN TO EACH RESPECTIVE PACK, NO ODOR OR FUMES WERE FOUND TO BE PRESENT IN CABIN. FOUND LARGE AMOUNTS OF OIL ON THE BLEED DUCT AND BLEED VALVE OF TH E APU. CLEANED OIL FROM DUCT MANIFOLD AND DEFERRED APU PER MEL. 2 L 7 3 4F RT A22WE 1998022600860 19980226 00860 SO 1998 2 26 BIER9802050 2 19980223 A 7414 10357281 CONDENSOR PIPER PA34 PA34200T 7103406 SO CONT O360 TSIO360EB 17025 SO RT MAG SHORTED B BIEA K NONE R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 EA 21 9211K 293 347670191 265924R PILOT REPORTED, EXCESS RPM DROP ON RUN-UP, INSP OF MAG INTERNALS REVEALED TOP OF CONDENSOR, WHERE WIRE IS SOLDERED TO CO NDENSOR WAS CONTACTING MAG CAP. IT HAD FINALLY WORN THROUGH THE INSULATING PAINT AT THE TOP. SUBMITTER STATES, THE SOL DER JOINT AND WIRE WAS TOO TALL AT MANUFACTER AND INSTALLATION BY MANUF. 1 L 7 2 3O 3 O A7SO E9CE 1998022600872 19980226 00872 CE 1998 2 26 98ZZZX852 1 19980211 A 2121 EM630 MOTOR ELECTROMECH BEECH 1900 1900C 1154161 CE CABIN VENT OVERHEATED A YADA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 AL 01 41UE 1734 469 UC41 CREW REPORTED VERY STRONG SMELL OF SOMETHING ELECTRICAL BURNING. AIRCRAFT RETURNED TO ANC AND LANDED WITH NO PROBLEMS. MAINTENANCE FOUND SHORTED VENT BLOWER MOTOR. REPLACED VENT BLOWER, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 1998022600875 19980226 00875 NM 1998 2 26 VJ9800025 1 19980224 A 3350 LIGHT BOEING 737 7372P6 NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 11 1PC 21613 CENTER AISLE, AFT AND OUTSIDE EMERGENCY LIGHTS INOPERATIVE. PERFORMED FUNCTIONAL CHECK OF INTERIOR AND EXTERIOR EMERGEN CY LIGHT SYSTEM ON AIRCRAFT AND OPS CHECKED NORMAL IAW MM 33-51-00. 2 L 7 2 4F RT A16WE 1998022600876 19980226 00876 WP 1998 2 26 VJ9800026 1 19980225 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP R1 DOOR LOOSE A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 907VJ 47444 R1 DOOR EMERGENCY SLIDE COVER BECAME DISLODGED. REPLACED COVER AND PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998022600877 19980226 00877 WP 1998 2 26 CALA9800320 1 19980223 A 2910 7912641969 HYD LINE DOUG DC9 DC982 3022082 WP TR CONTL VALVE BROKEN A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 77827 49487 THE RT HYDRAULIC SYSTEM PRESSURE LOW LIGHT ILLUMINATED AND PRESSURE DROPPED TO ZERO WHILE EN ROUTE. ALTERNATE GEAR EXTE NSION WAS USED. WHEN THE AIRCRAFT LANDED AT RSW THE RT MAIN GEAR DOOR SKID PLATE WAS DAMAGED. MAINTENANCE FOUND HYDRAU LIC LINE BROKEN AT RIGHT THRUST REVERSER CONTROL VALVE. A FLEX LINE WAS INSTALLED AND A DIP WAS ISSUED TO REPLACE THE L INE WITHIN 500 FLIGHTS OR 1200 FLIGHT HOURS. THE RT MLG DOOR SKID AND SPACER WERE REMOVED IAW ECRA 5280-91175 AND A DIP WAS ISSUED TO REPAIR WITHIN TWO CYCLES. THE SKID AND SPACER WERE INSTALLED WHILE AIRCRAFT WAS OUT OF SERVICE IN EWR AN D THE DIP WAS CLOSED. 2 L 7 2 4F A6WE 1998022600878 19980226 00878 WP 1998 2 26 CALA9800321 1 19980223 A 3231 59151695511 LATCH MECH DOUG DC9 DC932 3022066 WP LT MLG DOOR WORN A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 12507 47788 THE LT GEAR UNSAFE LIGHT REMAINED ILLUMINATED ATER GEAR RETRACTION (REPEAT PROBLEM - LANDING GEAR SWITCH PREVIOUSLY CHAN GED). THE CHECKLIST WAS COMPLETED WITH NO CHANGE. THE FLIGHT WAS CONTINUED TO CLE WHERE THE AIRCRAFT LANDED WITHOUT IN CIDENT. MAINTENANCE FOUND THE LT MLG DOOR LATCH MECHANISM LINKAGE WORN. THE LATCH MECHANISM WAS REMOVED, REPLACED AND RIGGED IAW MM 32-31-4, PAGES 201-210. LANDING GEAR OPERATION AND INDICATIONS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998022600879 19980226 00879 WP 1998 2 26 CALA9800322 1 19980224 A 3350 EMBS1392 BATTERY CHARGER ENGMAGNETICS DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13088 4066 46850 MAINTENANCE REPORTED THAT THE EMERGENCY LIGHT TEST WAS INOPERATIVE. THE BATTERY CHARGER AND PACK AT DOOR 3L WERE REMOVE D AND REPLACED. 2 L 7 3 4F A22WE 1998022600880 19980226 00880 WP 1998 2 26 CALA9800323 1 19980224 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FUSELAGE SKIN CORRODED INSIDE AND OUTSIDE AT STA 1721 BETWEEN LONGERON 47 AND 48L. THE SKIN WAS REMOVE D AND PURSER WAS INSTALLED IAW SRM 51-31-01. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-20-0. 2 L 7 3 4F A22WE 1998022600881 19980226 00881 WP 1998 2 26 CALA9800324 1 19980224 A 5720 BEAM DOUG DC10 DC1010 3022110 WP LT WING TE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LT WING INBOARD TRAILING EDGE CORRODED ON UPPER PANEL SUPPORT BEAM FORWARD OF MLG FIXED SIDE BRACE. TH E CORRODED AREA WAS CUT OUT, A NEW BEAM SECTION AND SPLICES WERE INSTALLED IAW ECRA 5721-01005. 2 L 7 3 4F A22WE 1998022600882 19980226 00882 WP 1998 2 26 CALA9800325 1 19980224 A 3830 SERVICE PANEL DOUG DC10 DC1010 3022110 WP MID LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND MID LAVATORY SERVICE PANEL CORRODED INSIDE HOUSING WITH CORROSION ON INSIDE OF CUTOUT AT RT AFT CORNER. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5330-02628. 2 L 7 3 4F A22WE 1998022600883 19980226 00883 WP 1998 2 26 CALA9800326 1 19980224 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1661-1681 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 43L CORRODED BETWEEN STA 1661 AND 1681. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-00, A REP AIR WAS INSTALLED IAW SRM 51-21-01 AND 51-33-01. 2 L 7 3 4F A22WE 1998022600884 19980226 00884 WP 1998 2 26 CALA9800327 1 19980224 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1721 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND UPPER CAP OF FLOOR SUPPORT IN CENTER CARGO COMPARTMENT CORRODED AT STA 1721, RBL 33. THE CORRODED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-00-01 AND 51-21-01. 2 L 7 3 4F A22WE 1998022600885 19980226 00885 WP 1998 2 26 CALA9800328 1 19980224 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP BS 1853 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND SPLICE IN AFT CARGO BIN CORRODED AT STA 1853, LONGERON 42L. NEW PARTS WERE FABRICATED AND INSTALLED IA W SRM 51-21-00. 2 L 7 3 4F A22WE 1998022600886 19980226 00886 WP 1998 2 26 CALA9800329 1 19980224 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1821 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND UPPER CAP OF FLOORBEAM IN AFT BIN CORRODED IN SPOTS FROM LEFT TO RIGHT END AROUND SCREW HOLES AND TIE D OWN TRACK MOUNT SCREWS AT BOTTOM, STA 1821. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998022600887 19980226 00887 WP 1998 2 26 UPS98825887 1 19980209 A 5210 INTERCOSTAL DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, MAIN ENTRY DOOR INTERCOSTAL HAS CRACK IN THE RADIUS AS VIEWED THRU UPPER FWD LIGHTENING HOLE. REPAIR ED IAW SRM 52-3-2. 2 L 7 4 4F RT 4A25 1998022600888 19980226 00888 WP 1998 2 26 UPS98825888 1 19980210 A 5320 4611067D FITTING DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LONGERON 33R END FITTING AFT SIDE OF FS 70 IS EXFOLIATED (HEAVY CORROSION). REMOVED AND REPLACED FIT TING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998022600889 19980226 00889 NM 1998 2 26 98FDEA00138 1 19980224 A 5300 65175302 SKIN BOEING 727 72725 1384006 NM BS 1342 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 156FE 18289 WORKING FASTENERS IN RT SIDE OF FUSELAGE OF NR 2 ENGINE AT BS 1342 BETWEEN RAIN GUTTER AND ACCESS PANEL. *S/D* REMOVED DAMAGED SECTION OF SKIN BS 1328 TO 1342, STR 20 RT TO STR 27 RT PER FED-EX SRM 53-30-3 FIG 15A. FABRICATED REPAIR PART S AND INSTALLED REPAIR PARTS PER FED-EX SRM 53-30-3 FIG 15A. 2 L 7 3 4F A3WE 1998022600890 19980226 00890 NM 1998 2 26 98FDEA00139 1 19980225 A 3260 SWITCH BOEING 727 727233 138408A NM TAIL SKID OUT OF ADJUST A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 218FE 21101 TAIL SKID LIGHT ILLUMINATES WHEN GEAR IS PLACED TO DOWN AND LOCKED POSITION IN THE AIR. GEAR WAS RECYCLED AND LIGHT REM AINS ON. ADJUSTED AND CLEANED THE TAIL SKID WARNING LIGHT SWITCH, (DOWN LOCK), PER MAINTENANCE MANUAL 32-71-01. GROUND CHECK OK. 2 L 7 3 4F RT A3WE 1998022600891 19980226 00891 WP 1998 2 26 ABXA9800124 1 19980224 A 3260 SWITCH DOUG DC9 DC932 3022066 WP LT MLG SHORTED A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 939AX 47201 LEFT GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH THE GEAR HANDLE UP. RECYCLED GEAR, NO CHANGE. REPAIRED SHORTED PIN NR 6 ON THE LEFT MAIN LANDING GEAR DOWN LOCK LIMIT SWITCH. OPS CHECKED GOOD ON GEAR SWING. 2 L 7 2 4F A6WE 1998022600892 19980226 00892 WP 1998 2 26 ABXA9800125 1 19980223 A 7933 15098521 REGULATOR DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE MALFUNCTION A ABXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 843AX 46017 644954 NR 2 ENGINE OIL TEMPERATURE WENT TO 153 DEG DURING CLIMB. REDUCED POWER TO IDLE, BUT TEMPERATURE REMAINED THE SAME. SH UT DOWN NR 2 ENGINE. REPLACED NR 2 ENGINE OIL TEMPERATURE REGULATOR AND NR 2 OIL STRAINER. OPS CHECKED GOOD IAW DC8 MM . 2 L 7 4 4F 4 F 4A25 1E8 1998022600893 19980226 00893 WP 1998 2 26 MWEA98192 1 19980223 A 5720 9919369 TEE DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RT HAND WING T-CAP WAS FOUND TO BE EXCESSIVELY CORRODED WING STA XCW 58. T-CAP AT STA XCW 58 WAS REMOVED AND REPLACED I AW DOUGLAS SERVICE BULLETIN 57-98 REV 8. 2 L 7 2 4F A6WE 1998022600894 19980226 00894 WP 1998 2 26 MWEA98193 1 19980223 A 5312 BULKHEAD WEB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 WEB ATTACHED TO RADIAL STIFFENER APB FOUND CRACKED AT THE O/B END LONG14R. STOP DRILLED CRACK, FABED REPAIR ANGLES IAW DRAW J060110, INSTALLED REPAIR ANGLES IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600895 19980226 00895 WP 1998 2 26 MWEA98194 1 19980223 A 5542 5910256 SKIN DOUG DC9 DC932 3022066 WP RUDDER MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 212ME 47701 PREVIOUS FLUSH REPAIR WAS FOUND RUDDER RIB 22 REPAIR DOES NOT CONFORM TO SRM. REMOVED PREVIOUS REPAIR AND FAB DOUBLER I AW SRM 55-03 FIG 11, INSTALLED REPAIR DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600896 19980226 00896 WP 1998 2 26 MWEA98195 1 19980223 A 5312 BULKHEAD WEB DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT HAND LOWER WEB OF THE BULKHEAD AT FS 965 WAS FOUND CRACKED IN SEVERAL PLACES. REMOVED DAMAGED SEC OF WEB, FAB REP AIR PARTS IAW SRM 53-03 FIG 19, INSTALLED REPAIR PARTS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600897 19980226 00897 WP 1998 2 26 MWEA98196 1 19980223 A 5315 5910347 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 916 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FLOORBEAM AT FS 916 WAS FOUND CHAFED FROM THE FLOORBOARDS FROM RBL 20 - LBL 20. BLENDED AREA OF BEAM, FABRICATED REPAIR STRAP IAW SRM 53-05 FIG 20, INSTALLED STRAP IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600898 19980226 00898 WP 1998 2 26 MWEA98197 1 19980223 A 5315 5910347 FLOORBEAM DOUG DC9 DC932 3022066 WP CABIN CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FLOORBEAM AT FS FOUND WITH CHAFE MARKS FROM FLOORBOARDS RBL 20 - LBL 20. BLENDED AREA OF BEAM, FAB REPAIR STRAP IAW SRM 5305 FIG 20, INSTALLED REPAIR STRAP IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600899 19980226 00899 WP 1998 2 26 MWEA98198 1 19980223 A 5330 5916493 SKIN DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 EXTER FUSE SKIN WAS FOUND CRACKED AROUND A FASTENER FS 965, 3 INCHES ABOVE LONG 14R. REMOVED DAMAGED SEC OF SKIN, FABED FILLER AND REPAIR DOUBLER IAW SRM 53-04, INSTALLED FILLER AND DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600900 19980226 00900 WP 1998 2 26 MWEA98199 1 19980223 A 5241 5910081 BEAM DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 GALLEY SERVICE DOOR WAS FOUND TO HAVE A CRACK IN THE NR 2 BEAM AT THE FORWARD END. STOP DRILLED CRACK, FABRICATED REPAI R DOUBLER IAW SRM 52-05 FIG 25, INSTALLED DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600901 19980226 00901 WP 1998 2 26 MWEA98200 1 19980223 A 5241 39536861 FITTING DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FORWARD END FITTING ON THE GALLEY SERVICE DOOR 4 HORIZONTAL BEAM WAS FOUND CRACKED. REMOVED DAMAGED PART ORDERED NEW PA RT, INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1998022600902 19980226 00902 1998 2 26 DL72S980436 4 19980222 A 3444 RADIO ALT 5224825008 BOEING 727 727232 1384082 NM CAPTS SIDE MALFUNCTIONED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 534DA 4376 22047 RADIO ALT (CAPTS) SHOWED 2000 AGL WHILE 10000 MSL. THIS WAS FOLLOWED BY A GPWAS PULL UP WARNING AND THEN ELECTRICAL SMO KE IN THE COCKPIT. PULLED CAPTS R/A CB SMOKE DISSIPATED AFTER RUNNING CK LIST LANDED NORMALLY. REPLACED CAPTS R/A IND AND NR 1 R/A TRANSCVR RAN BOTH PACKS AND GND OPS CKS OK. 2 L 7 3 4F A3WE 1998022600903 19980226 00903 NM 1998 2 26 DL76S980438 1 19980222 A 7932 TRANSMITTER BOEING 767 767332 1382001 NM OIL QTY INOPERATIVE A DALA K NONE N FALSE WARNING CR CRUISE 1 SO 27 133DN 24982 CENTER SYSTEM RESVR LIGHT ON OVERHEAD PANEL ILLUMINATED. STATUS PAGE SHOWED CENTER SYSTEM QUANTITY AT ZERO. VERIFIED T HAT SYSTEM QUANTITY WAS OK. REPLACED OIL QUANTITY TRANSMITTER, SYSTEM OPS CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1998022600904 19980226 00904 NM 1998 2 26 DLM88980439 1 19980222 A 2130 PRESSURIZATION DOUG MD88 MD88 3023688 NM COCKPIT MALFUNCTIONED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 967DL 53116 AUTO 1 AND 2 INOP LOST PRESURIZATION. UNABLE TO CONTROL CABIN IN MANUAL MODE AT 27000. AUTO 1 AND 2 INOP ILLUMINATED. CABIN WAS IN DESCENT AT 1500 FPM AND REMAINED IN DESCENT. FOLLOWED PROCEDURES PER POM. WEMT TO MANUAL MODE, THEN CABI N WOULD NOT CONTROL. UNABLE TO CONTROL OUTFLOW VALVE. CABIN BEGAN TO CLIMB. TESTED CONTROLLERS AND OUTFLOW VALVE, UNA BLE TO DUPLICATE. 2 L 7 2 4F RT A6WE 1998022600905 19980226 00905 NM 1998 2 26 DL757980440 1 19980222 A 3350 FUSE BOEING 757 757232 1384965 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 631DL 23612 ALL EMERG F/C FLOOR TRACK LIGHTING AN BOTH R-2 L-2 DIRECTIONAL EMERGENCY LIGHTS INOP. REPLACED FUSE IN M9101 PWR SUPPLY , CKS OK. 2 L 7 2 4F RT A2NM 1998022600906 19980226 00906 NM 1998 2 26 DLM88980441 1 19980222 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM TAIL COMPT LEAKING A DALA K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS AP APPROACH 1 SO 27 978DL 53259 SMELLED SMOKE IN CABIN WHEN APU STARTED ON APPROACH. FOUND LEAKING HYDRAULIC LINE IN TAIL COMPARTMENT. REPAIRED, PERFO RMED DUCT BURN-OUT. 2 L 7 2 4F RT A6WE 1998022600907 19980226 00907 NM 1998 2 26 DLM88980442 1 19980223 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN CHAFED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920DE 53423 AFT SECTION OF FLOOR TRACK EMERGENCY LIGHTS FROM SEAT 30 TO 38 INOP. FOUND WHEN REPLACING MISSING TRACK LIGHT SOCKET AT ROW 28. FOUND WIRE CHAFED AT LIGHT ASSEMBLY L2-848. REPAIRED WIRE, CK OK. 2 L 7 2 4F RT A6WE 1998022600908 19980226 00908 NM 1998 2 26 DL72S980443 1 19980223 A 3350 BATTERY PACK S111 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 483DA 20863 FWD OVERWING EMERGENCY LIGHT IN CABIN FAILS TO TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998022600909 19980226 00909 NM 1998 2 26 DL757980444 1 19980220 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1580-1600 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 609DL 22816 THE FUSELAGE SKIN BETWEEN FS 1580 AND 1600 BETWEEN STR 18L AND 22L WAS BADLY TORN AND DENTED FROM GROUND EQUIPMENT. THE DAMAGE WAS CUT OUT AND A SKIN DOUBLER WAS INSTALLED PER ER/A 364067-14, REV A. THE UNDERLYING STRINGERS WERE REPAIRED PER THE B757 SRM. 2 L 7 2 4F RT A2NM 1998022600910 19980226 00910 NM 1998 2 26 DL757980445 1 19980220 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1665 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 THE FUSELAGE SKIN AT FS 1665 AND STRINGER 25R WAS BADLY DENTED AT THE FWD END OF A DRAIN MAST. INSTALLATION DUE TO GROU ND SERVICE DAMAGE. THE DAMAGED AREA WAS CUT OUT AND A SKIN DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 364032-14, REV A . 2 L 7 2 4F RT A2NM 1998022600911 19980226 00911 NM 1998 2 26 DL757980446 1 19980220 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1755 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 THE FUSELAGE SKIN WAS DENTED, SCRATCHED AND GOUGED NEAR STRINGER 29R BETWEEN FS 1743 AND 1768. THE DAMAGED AREA WAS CUT OUT AND SKIN DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 364040-14, REV A. 2 L 7 2 4F RT A2NM 1998022600912 19980226 00912 NM 1998 2 26 DL757980447 1 19980220 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1560 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 THE FUSELAGE SKIN HAD NUMEROUS GOUGES, DENTS AND SCRATCHED BETWEEN FS 1550 AND 1621 AND BETWEEN STRINGERS 26L AND 26R. T HE DAMAGED SECTION OF SKIN WAS REMOVED AND A NEW SECTION WAS SPLICED IN PER ER/A 364044-14, REV B. 2 L 7 2 4F RT A2NM 1998022600913 19980226 00913 NM 1998 2 26 DL757980448 1 19980220 A 5330 SKIN BOEING 757 757232 1384965 NM BS 1630 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 603DL 22810 THE FUSELAGE SKIN BETWEEN FS 1627 AND 1639 AND BETWEEN STR 28L AND 29L WAS DENTED AND GOUGED DUE TO GROUND DAMAGE. THE DAMAGED AREA WAS CUT OUT AND A SKIN DOUBLER WAS INSTALLED PERER/A 364038-14, REV B. 2 L 7 2 4F RT A2NM 1998022600914 19980226 00914 WP 1998 2 26 DLL10980449 1 19980220 A 5312 BULKHEAD WEB LKHEED 1011 10113851 5265010 WP BS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 714DA 193C1090 THE FS 1212 BULKHEAD WEB WAS FOUND WITH A .25 LONG CRACK AT RBL 42.5. THE CRACK WAS ROUTED OUT AND A LOCAL DOUBLER REPA IR INSTALLED PER ER/A 364062-14AD, REV A. THE REPAIR WAS GRANTED AMOC APPROVAL FOR AD 96-20-10. 2 L 7 3 4F A23WE 1998022600915 19980226 00915 NM 1998 2 26 DL73K980450 1 19980223 A 5320 INTERCOSTAL BOEING 737 737232 1384475 NM BS 338 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 326DL 23098 DURING INSPECTION PER SI3-55852-12AD, THE R1 DOOR AFT FRAME INTERCOSTALS BETWEEN FS 332 AND 344 WERE FOUND CRACKED AT TW O LOCATIONS, AT STG 8A AND 11. REPAIRED PER ERA 331396-14AD. 2 L 7 2 4F RT A16WE 1998022600916 19980226 00916 NM 1998 2 26 DL72S980451 1 19980221 A 3350 BATTERY PACK S106 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 535DA 10163 22048 DURING S/C, FOUND AFT EMERG EXIT SIGN INOP WHEN TESTING EMERG LIGHTS. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998022600917 19980226 00917 NM 1998 2 26 DL72W980452 1 19980223 A 5521 65169351 SPAR BOEING 727 727247 138408F NM LT ELEVATOR MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 296WA 22533 DURING ACCOMPLISHMENT OF THE REAR SPAR MOD ON THE LT ELEVATOR IT WAS NOTED THAT SEVERAL HOLES WERE OVERSIZED. REPAIRED PER ERA 331369-14AD. 2 L 7 3 4F A3WE 1998022600918 19980226 00918 NM 1998 2 26 DL72W980453 1 19980223 A 5320 655612910 SILL BOEING 727 727247 138408F NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 THE C2 DOOR CUTOUT LOWER SILL WAS FOUND WITH CORROSION ON THE OUBTBD FLANGE OF THE OUTBD CHORD. REPAIRED PER ERA 331330 -14. 2 L 7 3 4F A3WE 1998022600919 19980226 00919 NM 1998 2 26 DL72W980454 1 19980223 A 5730 SKIN BOEING 727 727247 138408F NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 THE RMLG BEAM WAS DISCOVERED TO HAVE SEVERAL DAMAGE LOCATIONS. THE NR 2 SKIN PANEL ATTACH HOLE ON THE LWR FLANGE OF THE BEAM WAS FOUND WITH A CRACK IN THE BORE. THE OUTBD MLG SUPPORT LUG HOLE WAS FOUND CORRODED AND THE UNDERSIDE OF THE LW R FLANGE OF THE BEAM WAS CORRODED. REPAIRED PER ERA 331380-14 . 2 L 7 3 4F A3WE 1998022600920 19980226 00920 NM 1998 2 26 DLM88980455 1 19980223 A 5311 591395101 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 985DL 53312 AT FS 1418, MTC FOUND A CRACK AT L2L AND L2R ON THE FS 1418 FRAME. REPAIRED PER ERA 331389-14. 2 L 7 2 4F RT A6WE 1998022600921 19980226 00921 NM 1998 2 26 DLM88980456 1 19980223 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM BS 219 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 985DL 53312 FUSELAGE SKIN WAS FOUND DENTED AT STA 219 BETWEEN S18L AND 19L. REPAIRED PER ERA 331377-14. 2 L 7 2 4F RT A6WE 1998022600922 19980226 00922 NM 1998 2 26 DL72K980457 1 19980223 A 5330 SKIN BOEING 727 727232 1384082 NM L1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 A TIME LIMITED REPAIR AT THE L1 DOOR UPPER HINGE CUTOUT WAS REMOVED AND THE SKIN AND INTERNAL STRUCTURE WAS INSPECTED. T HE STRAP WAS FOUND CRACKED AS WELL AS 4 OTHER HOLE LOCATIONS IN THE SKIN ASSY. REPAIRED PER ERA 331410-14. 2 L 7 3 4F A3WE 1998022600923 19980226 00923 NM 1998 2 26 DL72K980458 1 19980223 A 5313 65583872 STRINGER BOEING 727 727232 1384082 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 STG 28R WAS FOUND WITH CORROSION FROM FS 950F+10 AFT. THE STG WAS CUT AT FS 950E+10 AND WILL BE REPLACED AFT TO THE FAC TORY SPLICE AT FS 1010. REPAIRED PER ERA 331405-14. 2 L 7 3 4F A3WE 1998022600924 19980226 00924 NM 1998 2 26 DL72W980459 1 19980223 A 5754 BRACKET BOEING 727 727247 138408F NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 FOUND AT B2 LETTER CHECK, NR 2 LE FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER EDGE. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998022600925 19980226 00925 NM 1998 2 26 DL72W980460 1 19980223 A 5320 WEB BOEING 727 727247 138408F NM LWR TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 FOUND DURING B-2 LETTER CHECK, LWR RT TORQUE BOX VERTICAL WEB CRACKED FS 1214. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998022600926 19980226 00926 NM 1998 2 26 DL72W980461 1 19980223 A 5320 WEB BOEING 727 727247 138408F NM LWR TORQUE BOX CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 FOUND DURING B-2 LETTER CHECK, LWR LT VERTICAL WEB CRACKED FS 1233 AND FS 1229. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998022600927 19980226 00927 NM 1998 2 26 DL72W980462 1 19980223 A 5320 WEB BOEING 727 727247 138408F NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 I/B VERT WEB CRACKED AT UPPER FASTENER HOLE STA 1233 LT SIDE. INSTALLED PERM REPAIR DOUBLER PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998022600928 19980226 00928 NM 1998 2 26 DL72W980463 1 19980223 A 5320 WEB BOEING 727 727247 138408F NM BS 1229 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 A .25 INCH CRACK AT UPPER LIGHTENING HOLE STA 1229 LT SIDE OF I/B VERT WEB. ROUTED OUT DAMAGE PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998022600929 19980226 00929 NM 1998 2 26 DL72W980465 1 19980223 A 5320 WEB BOEING 727 727247 138408F NM BS 1214 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2814W 20870 I/B VERT TORQUE BOX WEB CRACKED AT UPPER FASTENER STA 1214 RT SIDE. INSTALLED PERM REPAIR DOUBLER PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998022600930 19980226 00930 NM 1998 2 26 DL76S980466 1 19980223 A 5754 SKIN BOEING 767 767332 1382001 NM NR 2/4 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 116DL 23275 THE NR 2 LEADING EDGE SLAT WAS FOUND WITH A 5 DIA DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. THE NR 4 S LAT WAS FOUND WITH A 7 DIA DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. BOTH DELAMINATIONS WERE REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364089-14AD. 2 L 7 2 4F RT A1NM 1998022600931 19980226 00931 WP 1998 2 26 DHL9780601C 1 19980106 A 5320 SILL DOUG DC8 DC873F 302199F WP B 2 DOORWAY DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, B-2 DOOR SILL DENTED. REMOVED AND REPLACED SILL PER SRM 51-21-21. 2 L 7 4 4F RT 4A25 1998022600932 19980226 00932 WP 1998 2 26 DHL9780673C 1 19980114 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 510 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN CARGO COMPT FS 510 LINE NR 3 FLOOR TRACK HOLES ELONGATED. CUT OUT DAMAGED SECTION AND FABRICATED REPAI R PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998022600933 19980226 00933 WP 1998 2 26 DHL9880602C 1 19980210 A 5753 FAIRING DOUG DC8 DC873F 302199F WP LT TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING I/B FLAP AT XW 97 FORWARD FAIRING DAMAGED. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER PER S RM 51-1-8. 2 L 7 4 4F RT 4A25 1998022600934 19980226 00934 WP 1998 2 26 DHL9880603C 1 19980202 A 5753 FITTING DOUG DC8 DC873F 302199F WP LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING FLAP LINK HANGER ASSY STA 97 FWD RUBBING AGAINST FLAP HINGE. REMOVED LINKS AND DAMAGED FITTING, REW ORKED AREA AND INSTALLED NEW FITTING PER SRM 51-1-21 AND S/B 27-249. 2 L 7 4 4F RT 4A25 1998022600935 19980226 00935 WP 1998 2 26 DHL9880604C 1 19980205 A 5753 TRACK DOUG DC8 DC873F 302199F WP RT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING I/B FLAP TRACK ASSY WORN. REMOVED AND REPLACED TRACK PER MM 27-51-3. 2 L 7 4 4F RT 4A25 1998022600936 19980226 00936 WP 1998 2 26 DHL9880605C 1 19980116 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT BAGGAGE COMPT JUST UNDER SLIDING DOOR AT STA 1180 BETWEEN L29L AND L28L, FITTING CRACKED. REMOVED AND R EPLACED FITTING PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998022600937 19980226 00937 WP 1998 2 26 DHL9880606C 1 19980210 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1038 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, UPPER FUSELAGE STA 1038 RT BETWEEN LONGS 2 AND 3 SPLICE FITTING ATTACH FUSELAGE SKIN HAS .75 INCH CRACK. RE MOVED AND REPLACED FITTING PER SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998022600938 19980226 00938 WP 1998 2 26 DHL9880607C 1 19980113 A 5744 FITTING DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING I/B AILERON L/E DAMPER BRACKET CRACKED. REMOVED AND INSTALLED NEW FITTING PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600939 19980226 00939 WP 1998 2 26 DHL9880608C 1 19980120 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, REAR PRESSURE BULKHEAD FWD SIDE AT FS 1766 RT SIDE OF BULKHEAD BETWEEN LONGERON 10 AND 11 HAS 3.5 INCH CRACK . CUT OUT CRACK AND FABRICATED REPAIR DOUBLER AND INSTALLED DOUBLER REPAIR PER SRM 53-2-5. 2 L 7 4 4F RT 4A25 1998022600940 19980226 00940 WP 1998 2 26 DHL9880609C 1 19980204 A 5744 FITTING DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT FLAP HINGE SUPPORT FITTING AT STA 97 NR 2 HOLE HAS CRACK. REAMED HOLE AND HFEC NO FURTHER CRACK FOUND PE R DC-8 MM 51-3-4. 2 L 7 4 4F RT 4A25 1998022600941 19980226 00941 WP 1998 2 26 DHL98806100 1 19980128 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 60 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 60 LINE NR 2 FLOOR TRACK DAMAGED. REMOVED DAMAGED TRACK AND FABRICATED REPAIR PER SRM 53-2-3, 95 OF TRAC K REPLACED. 2 L 7 4 4F RT 4A25 1998022600942 19980226 00942 WP 1998 2 26 DHL98806101 1 19980211 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 3 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, R-WING NR 3 FLIGHT SPOILER DELAMINATED UPPER AND LOWER. REMOVED AND REPAIRED SPOILER AND INSTALLED PER MM 2 7-60-0. 2 L 7 4 4F RT 4A25 1998022600943 19980226 00943 WP 1998 2 26 DHL98806102 1 19980211 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING NR 5 FLIGHT SPOILER UPPER DELAMINATED. REMOVED, REPAIRED AND REPLACED THE SPOILER PER MM 27-60-0. 2 L 7 4 4F RT 4A25 1998022600944 19980226 00944 WP 1998 2 26 DHL98806103 1 19980202 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 289 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING UPPER WING PANEL XRS 589 DELAMINATED. REMOVED, REPAIRED AND REPLACED DAMAGED PANEL PER SRM 51-1-15. 2 L 7 4 4F RT 4A25 1998022600945 19980226 00945 WP 1998 2 26 DHL98806104 1 19980122 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 659 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, R/W UPPER WING PANEL XRS 659 DELAMINATED. REMOVED AND REPLACED DAMAGED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600946 19980226 00946 WP 1998 2 26 DHL98806105 1 19980125 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 106 PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING LOWER STA XW 106 HAS PUNCTURE UPPER SIDE. REMOVED, REPAIRED AND REPLACED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600947 19980226 00947 WP 1998 2 26 DHL98806106 1 19980124 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, R/W LOWER WING PANEL HAS INTERM REPAIR. REMOVED, REPAIRED AND REINSTALLED DAMAGED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600948 19980226 00948 WP 1998 2 26 DHL98806107 1 19980130 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 693 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, R/W PANEL STA XRS 693 LOWER WING BOTH SIDES DELAMINATED. REMOVED DAMAGED PANEL, REPAIRED AND INSTALLED PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600949 19980226 00949 WP 1998 2 26 DHL98806108 1 19980122 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 421-436 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, O/B TRAILING EDGE OF WING STA XW 421 TO 436 LOWER SURFACED HAS DELAMINATION. INSTALLED REPAIRED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600950 19980226 00950 WP 1998 2 26 DHL9880610C 1 19980112 A 5755 FITTING DOUG DC8 DC873F 302199F WP NR 1 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING NR 1 SPOILER O/B CENTER HINGE FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM 27-61-1. 2 L 7 4 4F RT 4A25 1998022600951 19980226 00951 WP 1998 2 26 DHL98806110 1 19980211 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 5 SPOILER HAS PLAY AND SURFACE DELAMINATION. REMOVED AND REPLACED SPOILER PER MM 27-60-0. 2 L 7 4 4F RT 4A25 1998022600952 19980226 00952 WP 1998 2 26 DHL98806111 1 19980211 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 5 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 5 FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE PER MM 27-50-0. 2 L 7 4 4F RT 4A25 1998022600953 19980226 00953 WP 1998 2 26 DHL98806112 1 19980130 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 4 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FLAP VANE NR 4 HAD DELAMINATION. REMOVED, REPAIRED AND REINSTALLED VANE PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1998022600954 19980226 00954 WP 1998 2 26 DHL98806113 1 19980211 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 2 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, SPOILER NR 2 HAS PLAY AND DELAMINATION. REMOVED, REPAIRED AND REINSTALLED SPOILER PER MM 27-60-0. 2 L 7 4 4F RT 4A25 1998022600955 19980226 00955 WP 1998 2 26 DHL98806114 1 19980130 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 3 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, I/B FLAP VANE NR 3 DELAMINATED. REMOVED AND REPLACED PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1998022600956 19980226 00956 WP 1998 2 26 DHL98806115 1 19980211 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 2 TE FLAP DELAMINATION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 2 VANE FLAP HAS DELAMINATION. REMOVED, REPAIRED AND REINSTALLED PER MM 27-51-174. 2 L 7 4 4F RT 4A25 1998022600957 19980226 00957 WP 1998 2 26 DHL98806116 1 19980211 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 1 TE FLAP DELAMINATION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 1 I/B VANE DELAMINATED. REMOVED AND REPLACED PANEL PER MM 27-50-00. 2 L 7 4 4F RT 4A25 1998022600958 19980226 00958 WP 1998 2 26 DHL98806117 1 19980211 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 1 SPOILER DELAMINATION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, SPOILER NR 1 HAS DELAMINATION. REMOVED PANEL, REPAIRED AND REINSTALLED PER MM 27-61-1. 2 L 7 4 4F RT 4A25 1998022600959 19980226 00959 WP 1998 2 26 DHL98806118 1 19980211 A 5330 SKIN DOUG DC8 DC873F 302199F WP CARGO DOORWAY TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, C2 CARGO DOOR LOWER FWD CORNER CUTOUT SKIN TORN. TRIMMED DAMAGED AREAS AND FABRICATED REPAIR DOUBLER PER SR M 51-1-8. INSTALLED DOUBLER AND TRIPLER PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998022600960 19980226 00960 WP 1998 2 26 DHL9880611C 1 19980120 A 5312 WEB BULKHEAD DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, REAR PRESSURE BULKHEAD FWD SIDE AT FS 1766 LEFT SIDE BULKHEAD WEB BETWEEN LONGERON 10 AND 11 HAS .25 INCH CR ACK. CUT OUT SECTION AND INSTALLED REPAIR PER SRM 53-2-5. 2 L 7 4 4F RT 4A25 1998022600961 19980226 00961 WP 1998 2 26 DHL9880612C 1 19980116 A 5540 WEB DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RUDDER STA ZR 283 IN MOUNT HINGE CUTOUT LOWER SIDE SKIN WEB HAS CRACK AND DENT. REMOVED DAMAGED WEB AND FAB RICATED NEW PER SRM 55-6-0, INSTALLED WEB SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600962 19980226 00962 WP 1998 2 26 DHL9880613C 1 19980112 A 5230 ANGLE DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN CARGO DOOR FWD LOWER CORNER SEAL RETAINER ANGLE CRACKED AT RADIUS. STOP DRILL AND FABRICATED REPAIR PE R SRM 51-18, 2 FT X 2 FT. 2 L 7 4 4F RT 4A25 1998022600963 19980226 00963 WP 1998 2 26 DHL9880614C 1 19980208 A 5280 BRACKET DOUG DC8 DC873F 302199F WP RT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT MAIN LANDING GEAR STRUT CENTER DOOR AFT LOWER SUPPORT BRACKET CRACKED AT I/B AND O/B ATTACH POINTS. REMO VED AND REPLACED BRACKET PER MM 32-12-1. 2 L 7 4 4F RT 4A25 1998022600964 19980226 00964 WP 1998 2 26 DHL9880615C 1 19980108 A 5280 BRACKETT DOUG DC8 DC873F 302199F WP LT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT MAIN LANDING GEAR STRUT CENTER DOOR AFT LOWER BRACKET CRACKED AT I/B ATTACH POINT. REMOVED AND REPLACED BRACKET PER MM 32-1-21. 2 L 7 4 4F RT 4A25 1998022600965 19980226 00965 WP 1998 2 26 DHL9880616C 1 19980118 A 5720 TIP DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LEFT WING TIP HAS TEMP REPAIR AND CRACK. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLERS PER SRM 51-1-8. 9 X 6.25, FILLERS 2.5 X 5.25. 2 L 7 4 4F RT 4A25 1998022600966 19980226 00966 WP 1998 2 26 DHL9880617C 1 19980126 A 5312 BULKHEAD ANGLE DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, PRESSURE BULKHEAD AFT AT STA 1766 RT SIDE AT S-12 AT DOUBLER ANGLE HAS 5 CRACK. STOP DRILLED .250 AND FABRI CATED REPAIR ANGLE PER SRM 53-2-3. INSTALLED REPAIR DOUBLER PER SRM 53-2-85. 2 L 7 4 4F RT 4A25 1998022600967 19980226 00967 WP 1998 2 26 DHL9880618C 1 19980116 A 5414 PLATE DOUG DC8 DC873F 302199F WP NR 2 PYLON WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, 32 PYLON STRINGER FWD END WORN BY CHAFING. REMOVED WORN PLATE, FABRICATED NEW PLATE PER SRM 54-3-1 AND INST ALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600968 19980226 00968 WP 1998 2 26 DHL9880619C 1 19980213 A 5330 SKIN DOUG DC8 DC873F 302199F WP LT FUESLAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, TEMP SKIN REPAIR LOCATED BELOW NR 5 MCD FLOOR LATCH PIN COMING APART. REMOVED, REPAIRED AND FABRICATED DOUB LER PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998022600969 19980226 00969 WP 1998 2 26 DHL9880620C 1 19980112 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RUDDER AT STA ZR Z83 IN MOUNT HINGE CUTOUT TOP SKIN WEB AREA CORRODED. FOUND LEVEL 2 CORR. REMOVED WEB AND FABRICATED NEW PER SRM 55-1-0, 11.75 X 7.80. INSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600970 19980226 00970 WP 1998 2 26 DHL9880621C 1 19980211 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING TRAILING EDGE LOWER SURFACE PANEL AT TAIL END OF NR 2 PYLON CRACKED. REMOVED AND REPAIRED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600971 19980226 00971 WP 1998 2 26 DHL9880622C 1 19980211 A 5753 ICE SHIELD DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT FLAP I/B ICE SHIELD I/B TRACK GAUGE O/B TRACK HAS CRACK. REMOVED AND REPLACED DAMAGED TRACK PER SRM 51- 1-3. 2 L 7 4 4F RT 4A25 1998022600972 19980226 00972 WP 1998 2 26 DHL9880623C 1 19980106 A 5522 FAIRING DOUG DC8 DC873F 302199F WP LT ELEVATOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LEFT ELEVATOR AT ELEVATOR MOUNT FITTING CUTOUTS UPPER AND LOWER FAIRINGS DENTED, CRACKED AND BENT. STRAIGH TENED DEFORMITY, RESTORED TO ORIGINAL CONTOUR. TRIMMED CRACKED AREA, PERFORMED DYE PEN AND NO CRACK NOTED. 2 L 7 4 4F RT 4A25 1998022600973 19980226 00973 WP 1998 2 26 DHL9880624C 1 19980211 A 5320 JAMB DOUG DC8 DC873F 302199F WP SERVICE DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FWD RT SERVICE DOOR INTERIOR LOWER AFT JAMB TORN. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR DOUBLER PE R EO MMC382N1039. FABRICATED INNER WEB PER SRM 53-10-0. 2 L 7 4 4F RT 4A25 1998022600974 19980226 00974 WP 1998 2 26 DHL9880625C 1 19980106 A 5753 TRACK DOUG DC8 DC873F 302199F WP RT TE FLAP WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING FLAP CENTER HINGE UPPER VANE TO FLAP ATTACH FRAME BADLY WORN ON RIGHT SIDE. REMOVED DAMAGED TRACK ASSY PER SRM 51-3-0 AND INSTALLED NEW TRACK PER SRM. 2 L 7 4 4F RT 4A25 1998022600975 19980226 00975 WP 1998 2 26 DHL9880626C 1 19980123 A 5753 RIB DOUG DC8 DC873F 302199F WP RT TE FLAP TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING INBD FLAP FLAP LT OUTBD RIB T/E TORN. STOP DRILLED AND FABRICATED DOUBLER. INSTALLED PER SRM 51-1- 8, 10 X 1. 2 L 7 4 4F RT 4A25 1998022600976 19980226 00976 WP 1998 2 26 DHL9880627C 1 19980129 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 122 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LOWER AFT FUS C-3 DOOR COMPT UNDER SLIDING DOOR INNER SUPPORT FITTING AT FS 122 AND L35R CORRODED. REMOVED CORROSION, REMOVED FITTING, FABRICATED ANGLE AND INSTALLED PER SRM 53-2-0. FITTING 125 X 3.5 X .93 X 1.81. 2 L 7 4 4F RT 4A25 1998022600977 19980226 00977 WP 1998 2 26 DHL9880628C 1 19980211 A 5313 STRINGER DOUG DC8 DC873F 302199F WP BS 1250-1270 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, CUSP EXTRUSION LT AT STA 1260 CORRODED. FOUND LEVEL 2 EXFOLIATED CORROSION. REMOVED DAMAGED AREA FROM FS 1 250 TO 1270, FABRICATED EXTRUSION AND INSTALLED PER EO MMC 382N0820 AND SRM 53-2-5. 2 L 7 4 4F RT 4A25 1998022600978 19980226 00978 WP 1998 2 26 DHL9880629C 1 19980211 A 5230 ANGLE DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FWD LOWER CARGO COMPT C-1 INNER L-35 I/B AND O/B T/E ANGLES CRACKED AT FS 280. REMOVED DAMAGED SECTION OF T IE ANGLE AT 35L, I/B SIDE FROM FS 310 AND FABRICATED FILLER FROM EXTRUSIO. REMOVED DAMAGED SECTION OF TIE ANGLE FROM O/ B FS 307 TO 315 AND FABRICATED FILLER 8 LONG. INSTALLED PER EO MMC382N0804 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998022600979 19980226 00979 WP 1998 2 26 DHL9880630C 1 19980113 A 5230 97540552 FITTING DOUG DC8 DC873F 302199F WP CARGR DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, SLIDE DOOR AFT CARGO AFT COMPT SLIDE DOOR LOWER AFT DOOR COVER SUPPORT FITTING IS CRACKED. REMOVED AND REPL ACED SUPPORT FITTING PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600980 19980226 00980 WP 1998 2 26 DHL9880631C 1 19980211 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 190 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FWD SERVICE DOOR CUTOUT AFT CIRCUMFERENTIAL FRAME AT STA 190 L-20R HAS INTERM REPAIR FRAME CRACKED IN HALF. REMOVED PREVIOUS REPAIR DOUBLER AND FABRICATED NEW REPAIR DOUBLERS PER EO MMC382N0807, 7.5 X 4.0 X 1.6. 2 L 7 4 4F RT 4A25 1998022600981 19980226 00981 WP 1998 2 26 DHL9880632C 1 19980113 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 980 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT BAGGAGE COMPARTMENT FWD BULKHEAD AT STA 980, GILL LINER FRAME SUPPORT IS DAMAGED AT UPPER AND LOWER AREA S. CUT OUT DAMAGED SECTION, FABRICATED REPAIR AND INSTALLED PER SRM 51-1-21, 3 X 10. 2 L 7 4 4F RT 4A25 1998022600982 19980226 00982 WP 1998 2 26 DHL9880633C 1 19980211 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1080-1120 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT CARGO COMPT RT SIDE TUNNEL AREA BETWEEN STA 1080 AND 1120 CORROSION ON VERTICAL SUPPORT. REMOVED FITTI NG, FABRICATED AND INSTALLED NEW FITTING PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600983 19980226 00983 WP 1998 2 26 DHL9880634C 1 19980109 A 5320 HOUSING DOUG DC8 DC873F 302199F WP CARGO COMPT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, REAR CARGO COMPT AFT CARGO DOOR UPPER CEILING AREA METAL HOUSING NEXT TO DOOR HINGE IS CRACKED. STOP DRILLE D AND INSTALLED REPAIR DOUBLER 4 X 3 PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998022600984 19980226 00984 WP 1998 2 26 DHL9880635C 1 19980202 A 5330 SKIN DOUG DC8 DC873F 302199F WP PAX DOORWAY TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN ENTRY DOOR LOWER FWD I/B FRAME SKIN TORN .5. REMOVED DAMAGED SECTION OF SKIN AND FABRICATED NEW .5 X 1 0.5 PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600986 19980226 00986 WP 1998 2 26 DHL9880637C 1 19980211 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1280 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT BAGGAGE COMPT LT SIDE TUNNEL AT STA 1280 L-1 CORROSION ON VERTICAL SUPPORT UNDER ANCHOR NUTS. REMOVED F ITTING AND REPLACED PER DWG 3773077 AND SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998022600987 19980226 00987 WP 1998 2 26 DHL9880638C 1 19980121 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LEFT WING LOWER SURFACE SAT 351, FWD OF FAIRING SHOWS LIGHT CORROSION. REMOVED DAMAGED SECTION AND FABRICAT ED NEW DOUBLER 4 X 5 PER SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998022600988 19980226 00988 WP 1998 2 26 DHL9880639C 1 19980104 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 60 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, SEAT TRACK NR 4 AT STA 60 SLOTS WORN OUT. CUT OUT DAMAGED SECTION AND REPLACED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998022600989 19980226 00989 WP 1998 2 26 DHL9880640C 1 19980119 A 5540 ANGLE DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RUDDER ANGLE AT BASE LEFT SIDE CRACKED AND CORRODED. STOP DRILLED AND FABRICATED DOUBLER PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998022600990 19980226 00990 WP 1998 2 26 DHL9880641C 1 19980104 A 5540 ANGLE DOUG DC8 DC873F 302199F WP RUDDER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RUDDER ANGLE AT BASE LEFT SIDE CRACKED AND DISTORTED. REMOVED DAMAGED ANGLE AND INSTALLED NEW PER SRM 51-3 -0, 25 X 2.5 2 L 7 4 4F RT 4A25 1998022600991 19980226 00991 WP 1998 2 26 DHL9880642C 1 19980104 A 5542 SKIN DOUG DC8 DC873F 302199F WP RUDDER WRINKLED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RUDDER AT STA ZR 284.75 RT SIDE SKIN WRINKLED. CUT OUT DAMAGED SECTION OF SKIN FROM ZR 295 TO ZR 272. 2 AN D FABRICATED REPAIR SPLICE FROM ZR 295 37 X 2.5 AND REPLACEMENT SKIN 25 X 37 PER SRM 51-1-8 AND EO MMC283N0597. RUDDER REBALANCED PER MM 51-4-6. 2 L 7 4 4F RT 4A25 1998022600992 19980226 00992 WP 1998 2 26 DHL9880643C 1 19980124 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 191 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT WING AT T/E BETWEEN XW 191, LOWER PANEL INTERIOR SURFACE AFT OF DUMP CHUTE DELAMINATED. REMOVED AND REP LACED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600993 19980226 00993 WP 1998 2 26 DHL9880644C 1 19980111 A 5414 FAIRING DOUG DC8 DC873F 302199F WP NR 4 PYLON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, PYLON NR 4 ON RT SIDE OF PYLON ABOVE EXHAUST CASE AFT COWL FAIRING TO PYLON DELAMINATING. REMOVED, REPAIRED AND INSTALLED FAIRING PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600994 19980226 00994 WP 1998 2 26 DHL9880645C 1 19980102 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP RT COCKPIT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, ELONGATED HOLED ON COPILOT SEAT TRACK. REMOVED REPAIR TEE FWD TRACKS PER SRM 51-1-20D, MILLING DOWN ENTIRE SURFACE DEPTH OF .5 IN. FABRICATED STRAPS AND INSTALLED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998022600995 19980226 00995 WP 1998 2 26 DHL9880646C 1 19980129 A 5347 3657504 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FLIGHT ENGINEERS SEAT TRACK ELONGATED HOLES. REMOVED AND REPLACED TRACK PER SRM 53-3-0. 2 L 7 4 4F RT 4A25 1998022600996 19980226 00996 WP 1998 2 26 DHL9880647C 1 19980125 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LOWER SURFACE T/E AFT REAR SPAR HINGED PANELS, INTERIOR SURFACE DELAMINATED. REMOVED AND REPLACED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998022600997 19980226 00997 WP 1998 2 26 DHL9880648C 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 600 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FUS STA LINE NR 6 FLOOR TRACK WORN. CUT OUT DAMAGED AREA, FABRICATED PLUG AND INSTALLED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998022600998 19980226 00998 WP 1998 2 26 DHL9880649C 1 19980112 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1600 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FUS STA 1600, LINE NR 6 FLOOR TRACK WORN AND DAMAGED. REMOVED SECTION, INSTALLED SPLICED AND NEW TRACK PER SRM 53-21-2, 40 LONG. 2 L 7 4 4F RT 4A25 1998022600999 19980226 00999 WP 1998 2 26 RRXA98020 1 19980106 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 408-457 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND LEFT WING SKIN PANEL WITH CRACK BEYOND LIMITATIONS IAW DC-8 SRM AT, XW 408 TO XS457. F ABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH D85-R02 AND DC-8 SRM 51 -1-21. 2 L 7 4 4F RT 4A25 1998030300002 19980303 00002 WP 1998 3 3 ARWA980206 1 19980218 A 2780 472085119 COMPARATOR LKHEED 1011 1011385115 5265015 WP LE FLAPS INOPERATIVE A ARWA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SO 19 306GB 1138 IN APPROACH, LEADING EDGE FLAPS LOCK AT ZERO DEGREE POSITION. REMOVED AND REPLACED FLAPS ASYMMETRY COMPARATOR, OPS CHEC KED NORMAL. FLAPS AND SLATS IAW MM 27-51-0. 2 L 7 3 4F A23WE 1998030300011 19980303 00011 WP 1998 3 3 VJ9800021 1 19980107 A 5754 PLATE DOUG DC9 DC932 3022066 WP NR 2 LE SLAT DAMAGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 906VJ 47379 DURING C CHECK, FOUND NR 2 SLAT REQUIRED REPLACEMENT. FABRICATED AND INSTALLED IAW DC9 SRM 57-09 FIG 10A AND AEROCORP E O 98-795. 2 L 7 2 4F A6WE 1998030300012 19980303 00012 NM 1998 3 3 DLM88980432 1 19980221 A 4920 38005041 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU COMPT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 991DL 4653 53343 APU SHUTDOWN AUTOMATICLLY, ATTEMPT AT RESTART UNSUCCESSFUL. LEFT GENERATOR ON MCO. DIVERTED TO CVG. REPLACED APU. 2 L 7 2 4F 4 F RT A6WE E9NE 1998030300015 19980303 00015 NM 1998 3 3 VJ9800024 1 19980223 A 3350 110049 BATTERY CHARGER BOEING 737 7372P6 NM CABIN FAILED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 1PC 21613 APPROXIMATELY 10 LIGHTS WERE NOT ILLUMINATED IN FORWARD SECTION OF EMERGENCY PATH LIGHTING. REMOVED AND REPLACED FWD BA TTERY CHARGER, OPS CHECKED OK IAW MM 33-51-51. 2 L 7 2 4F RT A16WE 1998030300016 19980303 00016 WP 1998 3 3 DHL98806109 1 19980211 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 6 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 6 FLAP VANE HAS DELAMINATION. REMOVED AND SENT FOR REPAIR AND REINSTALLED PER MM 27-60-0. 2 L 7 4 4F RT 4A25 1998030300017 19980303 00017 EU 1998 3 3 VTZA98023 1 19980125 A 3020 3D354701 PRESSURE SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NR 2 CCT CIRCUIT FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 316UE 41055 FLT 6499 - IAD-ROA - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE CCT NR 2 A/F DE-ICE FAULT ILLUMINATING WITH THE SYS TEM TURNED OFF. AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE CONTROL AND MAINTENANCE WAS NOTIFIED. MAINTENANCE REMOVED AND REPLACED THE PRESSURE SWITCH FOR THE NR 2 CCT SYSTEM IAW MAINTENANCE PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OU TLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998030500002 19980305 00002 CE 1998 3 5 98ZZZX856 1 19980119 A 7603 66003291 CONTROL CABLE LEAR 35 35A 5170602 CE FUEL CONTROL FAILED A VLLA K NONE O OTHER IN INSP/MAINT 1 GL 05 108RB 00144 35097 PILOT ATTEMPTED TO ADVANCE LT THROTTLE FROM FLIGHT IDLE. ENGINE DID NOT RESPOND. FOUND THE CABLE ELEMENT BROKEN 6 INCHE S AFT OF FUEL CONTROL POWER CONTROL ASSEMBLY. 2 L 7 2 4F A10CE 1998030500014 19980305 00014 NE 1998 3 5 98ZZZX868 2 19980122 A 7261 AS3209116 PACKING STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE OIL XFER TUBE BROKEN A PIVA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 WP 13 711PK 1231 SH3696 97346 PRECAUTIONARY SHUT DOWN OF NR 2 ENGINE IN-FLIGHT. LOW TORQUE AND LOW OIL PRESSURE. FOUND OIL LEAK ON FRONT SCAVENGE OI L TRANSFER TUBE AREA. REPLACED AS 3209-117 PACKING. 2 H 7 2 4T 4 T A41EU E4EA 1998030500035 19980305 00035 CE 1998 3 5 98ZZZX889 1 19980212 A 8120 4066109005 TURBOCHARGER CESSNA 210 T210M 2073451 CE ENG EXH SYS FAILED A GNXA O OTHER O OTHER AP APPROACH 1 SW 01 6687B 114 NCR0272 21062819 ONE BENT BLADE AND ONE BLADE SEPARATED AT HALF ITS LENGTH. PART FAILED ON FINAL APPROACH TO LANDING. COMPRESSOR SHAFT AND TURBINE SHAFT BENT. NO KNOWN REASON FOR COMPRESSOR BLADE TO HAVE SEPARATED, OR FOR SHAFT TO HAVE BENT, NO EVIDENCE OF FOREIGN OBJECTS BEING INJESTED INTO TURBOCHARGER. 1 H 7 1 3O 3A21 1998030500045 19980305 00045 NM 1998 3 5 NOCA0498 1 19980112 A 3232 2745710 ACTUATOR BOEING 757 75723A 1384967 NM RT MLG DOOR FAILED A NOCA O OTHER O OTHER AP APPROACH 1 EA 15 757NA 24567 GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENDED. FOUND RIGHT MLG DOOR OPEN APPROXIMATELY 18 INCHES. VISUALLY INSPECTED RT MLG DOOR, DOOR SEALS, AND SURROUNDING WW AREA FOR DAMAGE. NONE FOUND. REPLACED RIGHT HAND GEAR DOOR ACTUA TOR. (X) 2 L 7 2 4F RT A2NM 1998030500046 19980305 00046 1998 3 5 TWAA9801406 4 19980126 A 3421 2587335113 GYRO DOUG DC9 DC982 3022082 WP NR 1 WORN A TWAA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CE 05 925TW 49357 STL - FLT 455 - STARTING DESCENT INTO OMA, BOTH FLIGHT DIRECTORS FAILED. RETURNED TO FLIGHT ORIGINATION STATION, STL. R EPLACED NR 1 VERTICAL GYRO. CHECK-C, 8-17-97 BFM. (X) 2 L 7 2 4F A6WE 1998030500047 19980305 00047 NE 1998 3 5 TWAA9801702 2 19980129 A 7230 COMP BLADES DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE LT ENGINE FRACTURED A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 9630A 53561 3245 SEA - FLT 30 - CLIMBING OUT, LEFT ENGINE HAD COMPRESSOR STALL AT 5000 FT AND ANOTHER AT 7000 FT. EGT JUMPED 40 TO 50 DE GREES HIGHER THAN RT ENGINE. RETURNED TO SEA. FOUND METAL IN TAIL PIPE. CHANGED THE ENGINE. DURING ENGINE TEAR DOWN FOUND SEVEN EACH NINTH STAGE COMPRESSOR BLADES FRACTURED. MISSING BLADES AND DAMAGE TO THE OTHER STAGES CAUSED HIGH PRE SSURE COMPRESSOR STALLS. BLADES MFG PART NR 798209 AND 809809. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1998030500048 19980305 00048 1998 3 5 TWAA9801602 4 19980131 A 3422 2587335113 GYRO DOUG DC9 DC982 3022082 WP NR 1 FAILED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 928TW 48012 MCI - FLT 347 - ABORTED TAKEOFF, CAPTAIN'S ATTITUDE INDICATOR FAILED. REPLACED INDICATOR AND DIMMER CONTROL. ABORTED T AKEOFF SECOND TIME WITH CAPTAIN'S ATTITUDE INDICATOR FAILED. CHECKED ATTITUDE INDICATOR WIRING CONTINUITY, AND REPLACED NR 1 VG AND NR 1 SYMBOL GEN. CHECK-C ON 1-23-98 MCI. 2 L 7 2 4F A6WE 1998030500050 19980305 00050 NE 1998 3 5 98ZZZX900 2 19980204 A 7530 579282 STATOR BOEING 737 7372H5 138448E NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE DAMAGED A E9WA K NONE O OTHER IN INSP/MAINT 1 SO 05 220US LZNDWA 20453 665864 DURING B-CHECK, NR 2 ENGINE INSPECTION FOUND FIRST STAGE COMPRESSOR STATOR VANE DAMAGE. ONE VANE HAD RIVETS SHEARED, VA NE SHIFTED AND CAUSED DAMAGE TO ADJACENT VANE. REPLACED 1ST STAGE COMPRESSOR STATOR ASSY ON WING PER MM 72-00-21, 72-00 -23, AND 72-00-33. PERFORMED ALL CHECKS INCLUDING AVM TEST. NO DISCREPANCIES NOTED. FAILED ASSY TO BE EVALUATED. EN GINE BORESCOPE INSPECTION REVEALED NO DAMAGE TO ENGINE. 2 L 7 2 4F 4 F A16WE E2EA 1998030500051 19980305 00051 NM 1998 3 5 98ZZZX901 1 19980125 A 3350 6104789 BATTERY BOEING 737 7372H5 138448E NM CABIN DISCHARGED A E9WA K NONE L NO TEST IN INSP/MAINT 1 SO 05 220US 20453 INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FORWARD SERVICE DOORS DO NOT ILLUMINATE. FOUND ON RON SVC C HECK. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW B737 MM 33-50. OPERATIONAL CHECKS OK. REF: OPERATOR CONT ROL NR 98ZZZX902. 2 L 7 2 4F A16WE 1998030500052 19980305 00052 NM 1998 3 5 98ZZZX902 1 19980125 A 3350 6013211LB POWER SUPPLY BOEING 737 7372H5 138448E NM CABIN INOPERATIVE A E9WA K NONE L NO TEST IN INSP/MAINT 1 SO 05 220US 20453 INTERIOR AND EXTERIOR EMERGENCY LIGHTS AT FORWARD ENTRY AND FORWARD SERVICE DOORS DO NOT ILLUMINATE. FOUND ON RON SVC C HECK. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY IAW B737 MM 33-50. OPERATIONAL CHECKS OK. REF: OPERATOR CONT ROL NR 98ZZZX901. 2 L 7 2 4F A16WE 1998030500053 19980305 00053 NM 1998 3 5 EISA98013 1 19980216 A 2612 5116842 AURAL WARNING BOEING 727 727221 1384071 NM COCKPIT MALFUNCTIONED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 366PA 22538 FIRE BELL SOUNDED EN ROUTE FROM HDN TO DFW. REMOVED AND REPLACED AURAL WARNING UNIT. TT: 31,095:9 HOURS. TC: 16,292 . (X) 2 L 7 3 4F A3WE 1998030500054 19980305 00054 NM 1998 3 5 EISA98012 1 19980208 A 2612 FIRE BELL BOEING 727 727221 1384071 NM COCKPIT SOUNDED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 366PA 22538 FIRE BELL SOUNDED IN-FLIGHT WITH BOTH PILOT AND COPILOT MASTER FIRE WARNING LIGHTS ILLUMINATED. NO AREA OR POSITION LIG HT ILLUMINATED. INSPECTED ENGINE FOR LEAKS. ALSO, INSPECTED FIRE LOOPS FOR WEAR AND DAMAGE AND DEFECTS. NONE NOTED. O PS CHECK GOOD. (X) 2 L 7 3 4F A3WE 1998030500056 19980305 00056 NM 1998 3 5 EIAA98007 1 19980112 A 5510 WEB BOEING 747 747273C 1384896 NM RT HORIZ STAB DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, RT HORIZONTAL STAB INTERNAL WEB DENTED AT STATION 281.8 20 INCHES FORWARD OF AFT SPA R. INTERNAL RIB WEB REPAIR IAW SRM 55-10-06 FIG 4. (M) 2 L 7 4 4F A20WE 1998030500057 19980305 00057 NM 1998 3 5 EIAA98008 1 19980114 A 5312 BULKHEAD ANGLE BOEING 747 747273C 1384896 NM BS 400 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 400 BULKHEAD AFT FACE AT RBL 1 FLOOR SUPPORT ATTACH ANGLE CRACKED. ANGL E REPLACED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998030500058 19980305 00058 NM 1998 3 5 EIAA98009 1 19980114 A 5312 BULKHEAD ANGLE BOEING 747 747273C 1384896 NM BS 400 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 400 BULKHEAD AFT FACE AT RBL 6 FLOOR SUPPORT ATTACH ANGLE CRACKED. ANGL E REPLACED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998030500059 19980305 00059 NM 1998 3 5 EIAA98010 1 19980114 A 5312 BULKHEAD ANGLE BOEING 747 747273C 1384896 NM BS 400 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 400 BULKHEAD AFT FACE AT RBL 19 FLOOR SUPPORT ATTACH ANGLE CRACKED. ANG LE REPLACED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998030500060 19980305 00060 NM 1998 3 5 EIAA98011 1 19980115 A 5320 ANGLE BOEING 747 747273C 1384896 NM BS 1960 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, BULK CARGO BS 1960 LBL 38 LONGITUDINAL FLOOR SUPPORT CRACKED. REPLACED FLOOR SUPPOR T 'Z' ANGLE IAW SRM 51-40-03 FIG 2. (M) 2 L 7 4 4F A20WE 1998030500061 19980305 00061 NM 1998 3 5 EIAA98012 1 19980120 A 5320 ANGLE BOEING 747 747273C 1384896 NM BS 380 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, UPPER DECK BS 380 STRINGER ANGLE CRACKED AT STRINGER 2L. ANGLE REPAIRED IAW SRM 51- 10-01. (M) 2 L 7 4 4F A20WE 1998030500062 19980305 00062 NM 1998 3 5 EIAA98013 1 19980120 A 5311 FRAME BOEING 747 747273C 1384896 NM BS 380 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, UPPER DECK BS 380 FRAME CRACKED AT STRINGER 7L. FRAME REPAIRED IAW SRM 51-10-04 FIG 85. (M) 2 L 7 4 4F A20WE 1998030500063 19980305 00063 NM 1998 3 5 EIAA98014 1 19980120 A 5320 SHEAR TIE BOEING 747 747273C 1384896 NM BS 1840 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1840 AT STRINGER 46L - 47L SHEAR TIE IS CRACKED. SHEAR TIE REPAIRED BY SRM 53-10-04 FIG 3. (M) 2 L 7 4 4F A20WE 1998030500064 19980305 00064 NM 1998 3 5 EIAA98015 1 19980121 A 5320 ANGLE BOEING 747 747273C 1384896 NM BS 1335 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, BS 1335 FRAME TO WHEEL WELL PRESSURE DECK SUPPORT ANGLE CRACKED. SUPPORT ANGLE REPL ACED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998030500065 19980305 00065 NM 1998 3 5 EIAA98016 1 19980121 A 5347 TIE DOWN TRACK BOEING 747 747273C 1384896 NM BS 1700-1720 BROKEN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, BS 1700-1720 LBL 33 TIE DOWN TRACK 01B FLANGE BROKEN. TIE DOWN TRACK REPAIRED IW SR M 53-10-05 FIG 16. (M) 2 L 7 4 4F A20WE 1998030500066 19980305 00066 NM 1998 3 5 EIAA98017 1 19980123 A 5400 FITTING BOEING 747 747273C 1384896 NM NR 1 PYLON CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, NR 1 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M) 2 L 7 4 4F A20WE 1998030500067 19980305 00067 NM 1998 3 5 EIAA98018 1 19980123 A 5400 FITTING BOEING 747 747273C 1384896 NM NR 2 PYLON CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, NR 2 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M) 2 L 7 4 4F A20WE 1998030500068 19980305 00068 NM 1998 3 5 EIAA98019 1 19980123 A 5400 FITTING BOEING 747 747273C 1384896 NM NR 3 PYLON CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, NR 3 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M) 2 L 7 4 4F A20WE 1998030500069 19980305 00069 NM 1998 3 5 EIAA98020 1 19980123 A 5400 FITTING BOEING 747 747273C 1384896 NM NR 4 PYLON CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON UPPER SPAR FITTING CORROSION FOUND IN LUG BORE. REMOVED CORROSION IAW SB 54.2164 FIG 2. (M) 2 L 7 4 4F A20WE 1998030500070 19980305 00070 NM 1998 3 5 EIAA98021 1 19980126 A 7120 BUSHING BOEING 747 747273C 1384896 NM NR 1 ENGINE WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FORWARD UPPER ENGINE MOUNT HANGERS MOUNT BUSHING WORN. BUSHINGS REPLAC ED IAW OHW 20-50-03. (M) 2 L 7 4 4F A20WE 1998030500071 19980305 00071 NM 1998 3 5 EIAA98022 1 19980127 A 5320 ANGLE BOEING 747 747273C 1384896 NM BS 180 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, NOSE CARGO DOOR BS 180 AT STRINGER 28A-R THE STRINGER TO FRAME ATTACH IS DAMAGED. A NGLE REPLACED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998030500072 19980305 00072 NM 1998 3 5 EIAA98023 1 19980127 A 5320 SUPPORT BOEING 747 747273C 1384896 NM BS 287 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, COCKPIT BS 287 FRAME TO STRINGER 2L ATTACH CHORD SUPPORT FOUND CRACKED. SUPPORT R EPLACED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998030500073 19980305 00073 NM 1998 3 5 EIAA98024 1 19980127 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 1720 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, BS 1720 LBL 80 FLOORBEAM FOUND CORROSION AND CRACK. REPAIRED FLOORBEAM IAW SRM 53 -10-07 FIG 12. (M) 2 L 7 4 4F A20WE 1998030500074 19980305 00074 NM 1998 3 5 EIAA98025 1 19980127 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM BS 2060-2080 CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, BS 2060-1080 ABL 89 SEAT TRACK FLANGE UPPER AND LOWER SURFACES HAS CORROSION. SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A. (M) 2 L 7 4 4F A20WE 1998030500075 19980305 00075 NM 1998 3 5 EIAA98026 1 19980127 A 5311 FRAME BOEING 747 747273C 1384896 NM BS 2300 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, L5 DOOR CUTOUT AT BS 2300 FRAME 01B AREA IS CRACKED AT STRINGER 22L-23L. FRAME WE B REPAIRED IAW SRM 53-10-04 FIG 3. (M) 2 L 7 4 4F A20WE 1998030500076 19980305 00076 NM 1998 3 5 EIAA98027 1 19980127 A 5311 FRAME BOEING 747 747273C 1384896 NM BS 320 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, COCKPIT BS 320 LEFT STRINGER 1 TO STRINGER 2, FRAME FOUND CRACKED. FRAME WEB REPL ACED IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998030500077 19980305 00077 NM 1998 3 5 EIAA98028 1 19980127 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM CABIN CORROSION A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, SEAT TRACK FLANGE FOUND CORROSION AND CRACK. SEAT TRACK REPAIRED IAW SRM 53-10-05 FIG 1A. (M) 2 L 7 4 4F A20WE 1998030500078 19980305 00078 NM 1998 3 5 EIAA98029 1 19980127 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 2340 CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, FLOOR SUPPORT CORROSION BS 2340 AT ABL 32. FLOORBEAM AND FLOOR SUPPORT REPAIRED I AW SRM 51-40-4 FIG 1. (M) 2 L 7 4 4F A20WE 1998030500079 19980305 00079 NM 1998 3 5 EIAA98030 1 19980128 A 5412 BULKHEAD FTG BOEING 747 747273C 1384896 NM WS 669.5 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING WS 669.5 PYLON BULKHEAD SUPPORT FWD BACK UP FITTING CRACKED AT UPPER ARE A ALONG FASTENERS AT STRING 24. BACK UP FITTING REPLACED IAW SB 54A 2159 FIG 25. (M) 2 L 7 4 4F A20WE 1998030500080 19980305 00080 NM 1998 3 5 EIAA98031 1 19980128 A 5720 TIE CAP BOEING 747 747273C 1384896 NM WS 669.5 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING WS 669.5 UPPER MOST FWD SHEAR TIE CAP CRACKED. SHEAR TIE CAP REPAIRED I AW SB 57-2273 FIG 8 AND 9. (M) 2 L 7 4 4F A20WE 1998030500081 19980305 00081 NM 1998 3 5 EIAA98032 1 19980128 A 5753 PANEL BOEING 747 747273C 1384896 NM TE FLAP DELAMINATED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LEFT OUTBOARD AFT FLAP PANEL 588 JT DELAMINATED. REPAIRED IAW SRM 51-40-06 PARA 3 RS 57-51-33622. (M) 2 L 7 4 4F A20WE 1998030500082 19980305 00082 NM 1998 3 5 EIAA98033 1 19980128 A 5311 FRAME BOEING 747 747273C 1384896 NM BS 2669 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, APU COMPARTMENT, VERTICAL FRAME CRACKED AT BS 2669 W/L 310 RT SIDE. REPAIRED IAW SRM 51-40-03 FIG 3. (M) 2 L 7 4 4F A20WE 1998030500083 19980305 00083 NM 1998 3 5 EIAA98034 1 19980115 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 340-400 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, FUSELAGE BS 340-400 STRINGER GL LAP SPLICE TOP ROW FASTENER HOLES, FOUND 27 HOLES CRACKED. REPAIRED SKIN LAP IAW SRM 53-30-03 FIG 26. (M) 2 L 7 4 4F A20WE 1998030500084 19980305 00084 NM 1998 3 5 EIAA98036 1 19980114 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 340-380 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, RT BS 340-380 S6 LAP SPLICE TOP ROW FASTENER, FOUND THREE HOLES CRACKED ON UPPER S KIN. REPAIRED IAW EV - EO 53-747-1032-90 REV B AND BOEING DWG 65B28215 SHEET 1. (M) 2 L 7 4 4F A20WE 1998030500085 19980305 00085 NM 1998 3 5 EIAA98035 1 19980204 A 5400 BRACE BOEING 747 747273C 1384896 NM NR 1 PYLON CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON DIAGONAL BRACE UNDER WING FITTING HAS CORROSION UNDER BUSHING. REPAIRE D IAW SB 57-2246. LUG BORE AFTER INSURANCE CUT 2.457 INCH. (M) 2 L 7 4 4F A20WE 1998030500086 19980305 00086 NM 1998 3 5 EIAA98037 1 19980204 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM BS 701 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURNG 'C5/D' CHECK INSPECTION, SEAT TRACK FOUND CRACKED BS 701, RBL 11. REPAIRED IAW SRM 53-10-05 FIG 14. (M) 2 L 7 4 4F A20WE 1998030500087 19980305 00087 NM 1998 3 5 EIAA98038 1 19980204 A 5412 BULKHEAD ANGLE BOEING 747 747273C 1384896 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON AFT ENGINE MOUNT BULKHEAD RADIUS ANGLES CRACKING, ADJACENT TO FRONT SPA R NAC STATION 221. REPAIRED IAW SRM 54-10-03 FIG 19. (M) 2 L 7 4 4F A20WE 1998030500088 19980305 00088 NM 1998 3 5 EIAA98039 1 19980204 A 5414 SKIN BOEING 747 747273C 1384896 NM NR 3 PYLON ELONGATED HOLES A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON LEFT SKIN HAS ELONGATED HOLES AT NAS STATION 180. REPAIRED IAW SB 54-2 034 FIG 5. (M) 2 L 7 4 4F A20WE 1998030500089 19980305 00089 NM 1998 3 5 EIAA98040 1 19980206 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 2140 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, BS 2140 LBL 98 FLOORBEAM UPPER CHORD HAS CORROSION AND CRACK. REPAIRED IAW SRM 53 -10-07 FIG 12. (M) 2 L 7 4 4F A20WE 1998030500090 19980305 00090 NM 1998 3 5 EIAA98041 1 19980206 A 5411 FRAME BOEING 747 747273C 1384896 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON INTERIOR O/B VERTICAL FRAME AT STATION 180 IS CRACKED AT THE UPPER CORN ER. REPAIRED IAW SRM 54-10-03 FIG 1. (M) 2 L 7 4 4F A20WE 1998030500091 19980305 00091 NM 1998 3 5 EIAA98042 1 19980206 A 5320 FITTING BOEING 747 747273C 1384896 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, BS 1480 RBL 33 LONGITUDINAL FLOORBEAM 01B LOWER SUPPORT FITTING CRACKED. FITTING REPLACED IAW SRM 51-10-1. (M) 2 L 7 4 4F A20WE 1998030500092 19980305 00092 NM 1998 3 5 EIAA98043 1 19980206 A 5210 FITTING BOEING 747 747273C 1384896 NM R1 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 DURING 'C5/D' CHECK INSPECTION, R1 DOOR DOOR BODY TORQUE TUBE SUPPORT FITTING CRACKED. FITTING REPLACED IAW SRM 51-10-0 1. (M) 2 L 7 4 4F A20WE 1998030500093 19980305 00093 NM 1998 3 5 EIAA98044 1 19980206 A 5510 PIN BOEING 747 747273C 1384896 NM LT HORIZ STAB SEIZED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LEFT HORIZONTAL STAB HINGE BOLT ADJUSTMENT NUT SEIZED. HINGE PIN ASSEMBLE MODIFIE D IAW SB 747-55-2020 REV 7. (M) 2 L 7 4 4F A20WE 1998030500094 19980305 00094 NM 1998 3 5 EIAA98045 1 19980207 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 760 CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, FLOORBEAM BS 760 LBL 34 LOWER CHORD HAS CORROSION. REPAIRED IAW SRM 53-10-07 FIG 12. (M) 2 L 7 4 4F A20WE 1998030500095 19980305 00095 NM 1998 3 5 EIAA98046 1 19980207 A 5313 STRINGER BOEING 747 747273C 1384896 NM BS 1680 CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO BS 1680 STRINGER 40L HAS CORROSION. REPAIRED IAW SRM 53-10-03 FIG 1. ( M) 2 L 7 4 4F A20WE 1998030500096 19980305 00096 NM 1998 3 5 EIAA98047 1 19980207 A 5347 SEAT TRACK BOEING 747 747273C 1384896 NM BS 560-580 CORROSION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, BS 560 -580 AT RBL 55 SEAT TRACK HAS CORROSION. REPAIRED IAW SRM 53-10-05. (M) 2 L 7 4 4F A20WE 1998030500097 19980305 00097 NM 1998 3 5 EIAA98048 1 19980207 A 7120 BEARING BOEING 747 747273C 1384896 NM NR 4 PYLON ROTATING A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON THRUST LINK BEARING IS ROTATING IN THE HOUSING. BEARING REPLACED IAW O HM 20-50-03. (M) 2 L 7 4 4F A20WE 1998030500098 19980305 00098 NM 1998 3 5 EIAA98049 1 19980207 A 5751 SKIN BOEING 747 747273C 1384896 NM RT AILERON DELAMINATION A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, RT OUTBOARD AILERON HAS SMALL AREA OF DELAMINATINO ON LOWER SURFACE OUTBOARD END. FIBERGLASS REPAIRED IAW SRM 51-40-15 FIG 7. (M) 2 L 7 4 4F A20WE 1998030500099 19980305 00099 NM 1998 3 5 EIAA98050 1 19980207 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 1800 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO BS 1800 AT RBL 6, FLOORBEAM VERTICAL WEB IS DAMAGED. REPAIRED WEB IAW S RM 51-40-02 FIG 1. (M) 2 L 7 4 4F A20WE 1998030500100 19980305 00100 NM 1998 3 5 EIAA98051 1 19980207 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 1820 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO BS 1820 LBL 22, FLOORBEAM VERTICAL WEB DAMAGED. REPAIRED WEB IAW SRM 51 -40-02 FIG 1. (M) 2 L 7 4 4F A20WE 1998030500101 19980305 00101 NM 1998 3 5 EIAA98052 1 19980208 A 7120 BUSHING BOEING 747 747273C 1384896 NM NR 4 PYLON WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. (M ) 2 L 7 4 4F A20WE 1998030500102 19980305 00102 NM 1998 3 5 98ZZZX904 1 19980208 A 7120 BEARING BOEING 747 747273C 1384896 NM NR 4 ENGINE WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING C5/D-CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END F ITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. REFE RENCE: OPERATOR CONTROL NR EIAA98052. 2 L 7 4 4F A20WE 1998030500103 19980305 00103 NM 1998 3 5 EIAA98053 1 19980208 A 7120 BUSHING BOEING 747 747273C 1384896 NM NR 3 PYLON WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. ENGINE UPPER MO UNT BUSHING REPLACED IAW OHM 20-50-03. (M) 2 L 7 4 4F A20WE 1998030500104 19980305 00104 NM 1998 3 5 EIAA98054 1 19980209 A 5720 SHIM BOEING 747 747273C 1384896 NM LT WING DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING LANDING GEAR SUPPORT BEAM OUTBOARD END FITTING SHIM DAMAGED. SHIMS REPL ACED IAW MM 57-15-01. (M) 2 L 7 4 4F A20WE 1998030500105 19980305 00105 NE 1998 3 5 EIAA98055 2 19980215 A 7230 COMPRESSOR BOEING 747 747132 1384882 NM PWA JT9 JT9D7AH 52054 NE NR 2 ENGINE STALLED A EIAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 NM 09 479EV 19898 662553 NR 2 ENGINE HAD COMPRESSOR STALLED AT FL 390. CHECKED ENGINE PARAMETERS, SHUTDOWN ENGINE. DECLARED AN EMERGENCY TO GET DESCENT CLEARANCE TO FL 310. LANDED YSSY NO PROBLEMS. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998030500106 19980305 00106 NM 1998 3 5 EIAA98056 1 19980205 A 5320 SUPPORT BOEING 747 747273C 1384896 NM BS 1266 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURNIG 'C5/D' CHECK INSPECTION, FUSELAGE KEEL BEAM LOWER PANEL SUPPORT CORRODED T BS 1266 LBL 16 RBL 16. PANEL SU PPORT REPLACED IAW SRM 51-10-1. (M) 2 L 7 4 4F A20WE 1998030500107 19980305 00107 NM 1998 3 5 EIAA98057 1 19980212 A 3211 TRUNNION BOEING 747 747273C 1384896 NM LT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LEFT WING GEAR FWD TRUNNION H FITTING AND RETAINER NUT SEIZED. TRUNNION BEARING H FITTING REPLACED IAW MM 57-43-01. (M) 2 L 7 4 4F A20WE 1998030500108 19980305 00108 NM 1998 3 5 EIAA98058 1 19980202 A 5711 SPAR WEB BOEING 747 747273C 1384896 NM WS 1454 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, RT WING FRONT SPAR WEB AT WS 1454 HAS CORROSION. CORRODED WEB WAS TRIMMED OFF. R EPAIRED BY INSTALLING REPAIR DOUBLER, ANGLE AND FILLED AS PER HAECO RS R57-21-38620. (M) 2 L 7 4 4F A20WE 1998030500109 19980305 00109 WP 1998 3 5 9803279751 1 19980223 A 3260 CONTROL CABLE DOUG DC9 DC941 302207N WP NLG OUT OF ADJ A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 751NW 47115 DURING CLIMB-OUT, THE AUTO SPOILER DO NOT USE INDICATION ILLUMINATED AND THE AUTOMATIC PRESSURIZATION CONTROL BECAME INO PERATIVE AFTER LANDING GEAR RETRACTION. THE FLIGHT CREW FOLLOWED GROUND SHIFT FAILRUE PROCEDURES IN COM. DIVERTED TO O RD AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED THE GROUND SHIFT CABLES. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998030500110 19980305 00110 WP 1998 3 5 9803289878 1 19980224 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST CR CRUISE 1 GL 01 787NC 48149 DURING FLIGHT, FOUND SEAT 6D PROXIMITY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK O K. 2 L 7 2 4F RT A6WE 1998030500111 19980305 00111 WP 1998 3 5 9803299138 1 19980224 A 3397 WIRE DOUG DC9 DC915 3022036 WP CABIN MISINSTALLED A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 9348 45787 DURING PREFLIGHT, THE EMERGENCY EXIT LIGHTS CHARGING CIRCUIT BREAKER WAS FOUND TO BE POPPED. MAINTENANCE CORRECTED MIS- WIRING AT ATTENDANT'S EMERGENCY EXIT LIGHT SWITCH AND REPLACED THE RIGHT NACELLE EMERGENCY BATTERY PACK. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1998030500112 19980305 00112 WP 1998 3 5 9803309760 1 19980223 A 2780 59268805501 VALVE DOUG DC9 DC941 302207N WP TE SLATS MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 750NW 41262 2414 47114 SLAT DISAGREEMENT AND BLUE EXTEND LIGHTS REMAINED ON AFTER SLATS WERE RETRACTED. FLAP/SLAT HANDLE WAS DIFFICULT TO MOVE FROM ZERO TO RETRACT POSITION. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED SLAT CONT ROL VALVE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998030500113 19980305 00113 WP 1998 3 5 9803319863 1 19980225 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, FOUND EMERGENCY LIGHTS DIM. MAINTENANCE ACCOMPLISHED EA 98-0911488. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998030500114 19980305 00114 NM 1998 3 5 9803326716 1 19980223 A 2780 FLAPS BOEING 747 747251F 1384898 NM NR 1 LE FLAPS VIBRATING A NWAA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CL CLIMB 1 GL 01 616US 21120 DURING CLIMB, THE AIRCRAFT EXPERIENCED VIBRATIONS AND THE NR 1 LEADING EDGE FLAP NEEDED TO BE RAISED ELECTRICALLY. AIRC RAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 LEADING EDGE FLAP POWER DRIVE UNIT. OPERATIONAL CH ECK GOOD. SPECIFIC PART CAUSING FAULT TO BE DETERMINED. 2 L 7 4 4F A20WE 1998030500115 19980305 00115 WP 1998 3 5 9803339153 1 19980225 A 3260 RETRACT MECH DOUG DC9 DC914 3022034 WP NLG LACK OF LUBE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8912E 45829 DURING CLIMB-OUT, THE FLIGHT CREW HEARD A POPPING SOUND FROM THE NOSE LANDING GEAR AREA. THE CAPTAIN RECYCLED THE LANDI NG GEAR AND FOLLOWED COM PROCEDURES. AFTER RECYCLING, THE RIGHT MAIN LANDING GEAR RED ANNUNCIATOR LIGHT REMAINED ILLUMI NATED. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND LUBRICATED THE NOSE LANDING G EAR AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK ASSEMBLY AND ROLLOW-UP TORQUE TUBE. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998030500116 19980305 00116 WP 1998 3 5 9803349931 1 19980225 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING PERIODIC CHECK, FOUND RIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY. OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500117 19980305 00117 WP 1998 3 5 9803359957 1 19980224 A 3231 TORQUE TUBE DOUG DC9 DC931 3022065 WP LT MLG DOOR FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 915RW 47139 ON APPROACH INTO CLE, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW PERFORMED EMERGENCY GEAR EXTE NSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. DAMAGE TO THE LEFT INBOARD DOOR WAS INCURRED ON LANDING. MAINTE NANCE FOUND LEFT MAIN GEAR DOOR TORQUE TUBE SEQUENCE ROD ATTACH FITTING RIVET FAILED. REPLACED TORQUE TUBE, LEFT DOOR A SSEMBLY, AND RIGHT DOOR BUMPER SKID PLATE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998030500118 19980305 00118 WP 1998 3 5 UPS98825889 1 19980123 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK AFT 6 PIT STA 1260-1280 LONGERON 34 LEFT CRACKED. REMOVED CRACKED LONGERON 34 LEFT STA 1260-1350 I AW DC8 SRM 51 1 20D. DRILLED NEW LONGERON IAW DC8 SRM 51 1 20D. INSTALLED NEW LONGERON I 9AW DC8 SRM 51 1 20D NAD 51 3 0. 2 L 7 4 4F RT 4A25 1998030500119 19980305 00119 WP 1998 3 5 UPS98825890 1 19980124 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK BATH TUB CORRODED FS 280 L 28 TO 29R. REMVOED FITTING FABBED SPLICES FOR NEW FITTING IAW DC8 SRM 5 3 2 0 FIG 2D. INSTALLED NEW FITTING WITH SPLICES IAW DC8 SRM 53 2 0 FIG 2 D AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998030500120 19980305 00120 WP 1998 3 5 UPS98825892 1 19980210 A 5312 561306481 BULKHEAD ANGLE DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C AFT SIDE OF F/S 70 O/B OF 33R LOWER BULKHEAD L ANGLE HAS HEAVY CORROSION AROUND BOLT AND BETWEEN IT AN D LONGERON FITTING. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR CHORD IAW SRM 53-2-5 51-1-20D, AND DWG 5613064. 2 L 7 4 4F RT 4A25 1998030500121 19980305 00121 WP 1998 3 5 UPS98825893 1 19980210 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C F/S 260 RBL 48 - SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTI ON OF TRACK IAW SRM ADDM DC8-5320-8309. 2 L 7 4 4F RT 4A25 1998030500122 19980305 00122 WP 1998 3 5 UPS98825894 1 19980210 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1207 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C F/S 1207 LBL 59, SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECTI ON OF TRACK IAW SRM 53-7-2. 2 L 7 4 4F RT 4A25 1998030500139 19980305 00139 WP 1998 3 5 MWEA98201 1 19980224 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 313 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CRACK FOUND ON EXTERNAL FUSELAGE SKIN AT FS 313 APPROX 2.5IN BELOW LONGERON 16R. REMOVED DAMAGED SEC SKIN FAB REPAIR FI LLER, DOUBLERS IAWSRM 5304 FIG 38. INSTALLED RREPAIR FILLERS, DOUBLERS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998030500140 19980305 00140 WP 1998 3 5 MWEA98202 1 19980224 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 945-996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION FOUND ON LONGERON 28R FROM FS 945 TO 996. DAMAGE SEC OF LONGERON REMOVED, A REPLACEMENT SECTION OF LONGERON W AS FABRICATED IAW SRM 5311. INSTALLED SECTION OF LONGERON IAW SRM 5130. 2 L 7 2 4F A6WE 1998030500141 19980305 00141 WP 1998 3 5 MWEA98203 1 19980224 A 5320 39145901 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON ATTACH FITTING AT FS 996 LONGERON 24R FOUND CORRODED OUT OF LIMITS. FITTING REMOVED NEW ONE PROCURED REPLACEME NT INSTALLED IAW SRM 51-30. 2 L 7 2 4F A6WE 1998030500142 19980305 00142 WP 1998 3 5 MWEA98204 1 19980224 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1121 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 STATIC DISCHARGE DAMAGE FOUND ON EXTERNAL FUSELAGE SKIN AT STATION 1121.225 BETWEEN LONG 4R AND 6R IAW SRM 53-04 FIG 4. MAINTENANCE REPAIRED SRM 53-10. 2 L 7 2 4F A6WE 1998030500143 19980305 00143 WP 1998 3 5 MWEA98205 1 19980224 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 20L FOUND CORRODED BY THE AFT PRESSURE BULKHEAD FS 996. REMOVED DAMAGED SECTION LONGERON FABRICATED REPLACEMEN T SECTION OF LONGERON IAW SRM 5311. INSTALLED REPLACEMENT LONGERON IAWSRM 5130. 2 L 7 2 4F A6WE 1998030500144 19980305 00144 WP 1998 3 5 MWEA98207 1 19980224 A 5241 5910081 BEAM DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 GALLEY SERVICE DOOR NR 4 HORIZONTAL BEAM FOUND CRACKED AT FWD END ADJACENT TO OUTER SKIN. STOP DRILLED CRACK FAB REPAIR ANGLE IAW SRM 5205 FIG 25. INSTALLED REPAIR ANGLE IAW SRM 5130. 2 L 7 2 4F A6WE 1998030500145 19980305 00145 WP 1998 3 5 MWEA98208 1 19980224 A 5241 WEB DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 GALLEY DOOR INNER WEB WAS FOUND CRACKED BELOW THE BAYONET. REMOVED DAMAGED SECTION FABRICATED DOUBLER IAW SRM 520. INS TALLED DOUBLER IAW SRM 5130. 2 L 7 2 4F A6WE 1998030500147 19980305 00147 WP 1998 3 5 MWEA98210 1 19980224 A 5241 ANGLE DOUG DC9 DC932 3022066 WP GALLEY DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 GALLEY SERVICE DOOR A DOUBLER ANGLE ON THE AFT END OF NR 1 HORIZONTAL BEAM WAS FOUND CRACKED. REMOVED CRACKED ANGLE AND FAB. REPLACEMENT ANGLE IAW SRM 5301. INSTALLED FAB ANGLE IAW SRM 5130. 2 L 7 2 4F A6WE 1998030500148 19980305 00148 NM 1998 3 5 VNAA9802020 1 19980224 A 3060 3E2515 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP DIRTY A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 427JS 262 3039 THE LEFT PROPELLER HEAT FAILED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTEN ANCE INSPECTED AND CLEANED THE LEFT PROPELLER BRUSH BLOCK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-61-05. OPER ATION CHECKS WERE COMPLETED AND, THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998030500248 19980305 00248 WP 1998 3 5 AALA980313 1 19980216 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7506 49800 ORD - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 9. RE-SECURED EMERGENCY EXIT LIGHT STRIP AT ROW 9. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998030500249 19980305 00249 WP 1998 3 5 AALA980314 1 19980216 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 582AA 53159 DFW - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 10. RE-SECURED EMERGENCY EXIT LIGHT STRIP A T ROW 10. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998030500250 19980305 00250 NM 1998 3 5 AALA980277 1 19980208 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 873AA 21385 IAH - DURING OVERNIGHT MAINTENANCE, AFT VAULT DOOR LEFT AND RIGHT SIDE EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPAIRED CHAFED WIRES AND AS A PRECAUTIONARY, REPLACED BATTERY AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 3 4F A3WE 1998030500251 19980305 00251 NM 1998 3 5 AALA980253 1 19980206 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 707AA 22464 MIA - DURING OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING AT PASSENGER SEAT ROWS 9 TO 15 INOPERATIVE. REPLACED BROKE N WIRE AT EMERGENCY FLOOR LIGHT PASSENGER SEAT ROWS 9 TO 15. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998030500252 19980305 00252 NM 1998 3 5 AALA980303 1 19980210 A 3350 1000679 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 877AA 210069 21389 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT HAND FORWARD SERVICE DOOR EMERGENCY LIGHT FAILED TO ILLUMINATE. REPLACED RIGH T HAND FORWARD SERVICE DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998030500253 19980305 00253 EU 1998 3 5 AALA980207 1 19980125 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 41063 506 MIA - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT FLOOR TRACT LIGHTING AT PASSENGER SEATS 8B AND 10B INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PASSENGER SEAT 8B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998030500254 19980305 00254 NM 1998 3 5 AALA980172 1 19980118 A 3350 LIGHTS DOUG MD11 MD11 3023602 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST CR CRUISE 1 SW 07 1765B 48596 LHR - FLT 0086 - DURING FLIGHT, EMERGENCY FLOOR LIGHTS ALONG RIGHT SIDE CAME ON. RE-CYCLED EMERGENCY LIGHT SWITCH AND P ERFORMED EMERGENCY LIGHT TEST. SYSTEM OPERATIONAL CHECKED NORMAL. (X) 2 L 7 3 4F RT A22WE 1998030500255 19980305 00255 WP 1998 3 5 AALA980220 1 19980127 A 3350 1703663 SOCKET DOUG DC10 DC1010 3022110 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 135AA 47830 SFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT LIGHT AT PASSENGER SEAT 23H INOPERATIVE. REPLACED BROKEN EMERG ENCY EXIT LIGHT CONTACT SOCKET AT PASSENGER SEAT 23H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1998030500256 19980305 00256 EU 1998 3 5 AALA980224 1 19980127 A 3230 STRUT AIRBUS 300 A300B4605R 3930308 EU NLG DRAG STRUT ICED UP A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 25071 514 ORY - FLT 0146 - DURING APPROACH ORY, LANDING GEAR HANDLE SELECTED DOWN, NOSE LANDING GEAR FAILED TO INDICATE SAFE. CRE W CYCLED GEAR AND THE UNSAFE MESSAGE EXTINGUISHED. AIRCRAFT LANDED ORY WITHOUT INCIDENT. INSPECTION FOUND DRAG STRUT C OVERED IN ICE. STRUT WAS CLEANED AND LUBRICATED, SENSORS WERE CHECKED AND OPERATED NORMALLY. SYSTEM GROUND CHECKED NOR MAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998030500258 19980305 00258 NM 1998 3 5 AALA980232 1 19980129 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 872AA 21384 DFW - DURING OVERNIGHT CHECK, FIRST CLASS EMERGENCY FLOOR LIGHT FOUND INOPERATIVE. REPLACED LIGHT STRIP AT FIRST CLASS EMERGENCY FLOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998030500259 19980305 00259 WP 1998 3 5 AALA980235 1 19980130 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 498AA 49736 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN MID-CABIN WERE FOUND INOPERATIVE. RECONNECTED L OOSE EMERGENCY FLOOR PATH LIGHTING CONNECTOR AT MID-CABIN. SYSTEM GOUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998030500260 19980305 00260 WP 1998 3 5 AALA980236 1 19980131 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 463AA 49593 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED FORWARD EMERGENCY EX IT LIGHT IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998030500261 19980305 00261 EU 1998 3 5 AALA980206 1 19980124 A 2170 20D102 COALESER AIRBUS 300 A300B4605R 3930308 EU CABIN DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7083A 645 JFK - FLT 0105 - AFTER TAKEOFF JFK, FLIGHT ATTENDANT NOTED A STRONG ELECTRICAL/OIL SMELL IN CABIN. AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED ALL COALESCER BAGS AND BURNED PACKS OFF AFTER CHANGE. SYSTEMS CHECKED NORMA L OPERATION AND AIRCRAFT RELEASED INTO SERVICE. (X) 2 L 7 2 4F RT A35EU 1998030500262 19980305 00262 EU 1998 3 5 AALA980121 1 19980114 A 2611 CG7GT10 SMOKE DETECTOR FOKKER F28 F28MK0100 4990807 EU AFT LAVATORY DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1412A 11370 ORD - FLT 1828 - AFTER TAKEOFF, LEFT AFT LAVATORY SMOKE DETECTOR SOUNDED. A SLIGHT ODOR WAS DETECTED IN THE CABIN, AIRC RAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REMOVED ALL LAVATORY WALLS AND CEILING PANELS, CHECKED ALL LIGHTS, SI GNS, FLUSH MOTOR, ELECT WIRING AND CONNECTORS. FOUND NO SIGN OF ELECTRICAL DAMAGE OR SMOKE SMELL. REPLACED LEFT LAVATO RY SMOKE DETECTOR, ALL TESTS CHECKED NORMAL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998030500263 19980305 00263 EU 1998 3 5 AALA980204 1 19980123 A 3260 SWITCH FOKKER F28 F28MK0100 4990807 EU NLG FROZEN A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 1454D 11466 ORD - FLT 0853 - DURING APPROACH ORD, FLIGHT CREW RECEIVED A NOSE GEAR UNSAFE CONDITION UPON TOUCHDOWN. AIRCRAFT LANDED ORD WITHOUT INCIDENT. INSPECTION OF NOSE WHEELWELL FOUND PACKED SNOW AND ICE. NOSE LANDING GEAR CLEARED OF SNOW AND I CE, LUBRICATED, GEAR RETRACTED AND EXTENDED SEVERAL TIMES WITH NORMAL INIDCATION. SYSTEM GROUND CHECKED, NORMAL OPERATI ON. (X) 2 L 7 2 4F RT 1998030500264 19980305 00264 NM 1998 3 5 WRLA98072 1 19980207 A 2820 4059025907 CONTROLLER DOUG MD11 MD11 3023602 NM E/E COMPARTMENT FAILED A WRLA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 27 275WA 48631 DURING INITIAL CLIMB-OUT, FLIGHT CREW WAS UNABLE TO CONTROL FUEL TANK FILL VALVES IN AUTO/MANUAL. FLIGHT CREW ELECTED T O RETURN TO POINT OF DEPARTURE FOR MAINTENANCE ACTION. AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT INCID ENT. GROUND MAINTENANCE FOUND FUEL SYSTEM CONTROLLER FAULTING ON CENTRALIZED FAULT DISPLAY. REPLACED FUEL SYSTEM CONTR OLLER. PERFORMED 'RETURNED-TO-SERVICE" TEST OF FUEL SYSTEM WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1998030500265 19980305 00265 NM 1998 3 5 WRLA98073 1 19980207 A 2820 2720121MS CONTROLLER DOUG MD11 MD11 3023602 NM NR 1 FILL VALVE FAILED A WRLA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 27 275WA 48631 DURING INITIAL CLIMB-OUT, FLIGHT CREW WAS UNABLE TO CONTROL THE NR 1 FUEL TANK FILL VALVE. FLIGHT CREW ELECTED TO RETUR N TO POINT OF DEPARTURE FOR MAINTENANCE ACTION. AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT INCIDENT. G ROUND MAINTENANCE FOUND THE NR 1 FUEL TANK FILL VALVE FAULTING ON CENTRALIZED FAULT DISPLAY. REPLACED NR 1 FUEL TANK FI LL VALVE CONTROLLER. AS A PRECAUTION, ALSO REPLACED THE ANCILLARY FUEL SYSTEMS CONTROLLER. PERFORMED 'RETURNED-TO-SERV ICE' TEST OF FUEL SYSTEM WITH NO FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F RT A22WE 1998030500266 19980305 00266 EU 1998 3 5 USAAF98014 1 19980209 A 3230 UPSTOP FOKKER F28 F28MK0100 4990807 EU RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 894US 11379 PIT - FLT 0864 - AFTER TAKEOFF FROM PIT, THE RT MLG WOULD NOT RETRACT. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MLG UPSTOP DAMPER (RS) MALFUNCTIONING. SERVICED UPSTOP DAMPER PER F100 MM 32-11-0 5. PERFORMED OPERATIONAL TEST PER F100 MM 32-11-05. CHECKS NORMAL. (X) 2 L 7 2 4F RT 1998030500267 19980305 00267 NM 1998 3 5 USAABB98018 1 19980206 A 3350 210121 POWER SUPPLY BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 652US 24765 LAX - FOUND EMERGENCY EXIT SIGNS ABOVE ROW 29 INOPERABLE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK. (X) 2 L 7 2 4F RT A1NM 1998030500268 19980305 00268 NM 1998 3 5 USAABB98015 1 19980205 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 LAX - FOUND L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A2NM 1998030500269 19980305 00269 NM 1998 3 5 USAABB98016 1 19980201 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 PHL - FOUND EXIT IDENTIFIER AT L4 DOOR INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. 2 L 7 2 4F RT A2NM 1998030500270 19980305 00270 NM 1998 3 5 USAABB98019 1 19980213 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 632AU 27810 ALX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 33. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F RT A2NM 1998030500271 19980305 00271 WP 1998 3 5 USAA980056 1 19980210 A 5230 PAN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923VJ 39910 48143 PIT - DURING C-2 CHECK, FOUND .20 INCH CRACK AT RADIUS OF INNER PAN LOWER AFT CORNER BELOW BAYONET. STOP DRILLED AND IN STALLED DOUBLER PER SRM 52-05 FIG 26A. (X) 2 L 7 2 4F A6WE 1998030500272 19980305 00272 WP 1998 3 5 USAA980057 1 19980210 A 5230 SKIN DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923VJ 39910 48143 PIT - DURING C-2 CHECK, FOUND .1250 INCH CRACK AT DOOR SKIN AT RIVET IN SECOND BEAM FROM BOTTOM. REMOVED CRACKED AREA AN D INSTALLED DOUBLER PER SRM 52-05 FIG 3. (X) 2 L 7 2 4F A6WE 1998030500273 19980305 00273 WP 1998 3 5 USAA980058 1 19980207 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1095 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 977VJ 39098 48155 PIT - DURING C5 CHECK, FOUND 1.25 INCH LONG CRACK IN SKIN AT STA 1095 BETWEEN LONGERONS 3R AND 4R. INSTALLED DOUBLER PE R SRM 53-04 FIG 27. (X) 2 L 7 2 4F A6WE 1998030500274 19980305 00274 WP 1998 3 5 USAAD98024 1 19980211 A 3610 59586971 DUCT DOUG DC9 DC931 3022065 WP RT ENGINE RUPTURED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 929VJ 48118 LGA - FLT 1470 - AT APPROXIMATELY V1, THE RIGHT ENGINE EPR DROPPED FROM 2.00 TO 1.70. AT ROTATION, GOT FIRE INDICATION BELL AND LIGHTS. AFTER REDUCING THROTTLE, THE FIRE INDICATION WENT OUT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE HIGH PRESSURE PNEUMATIC SUPPLY DUCT. (X) 2 L 7 2 4F A6WE 1998030500275 19980305 00275 NM 1998 3 5 USAA980055 1 19980107 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 885 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 230AU 48323 21975 ROA - DURING 'CX-6' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND 2.75 INCH CRACK STR 24R STA 885 SKIN (FUSELAGE). STOP D RILLED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (X) 2 L 7 2 4F A16WE 1998030500276 19980305 00276 NM 1998 3 5 USAASB98040 1 19980214 A 2150 32194211 VALVE BOEING 737 7373B7 1384580 NM LT ACM STUCK A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 391US 55570 18511 23313 BOS - FLT 1837 - AFTER TAKEOFF FROM BOS, THE AIRCRAFT WOULD NOT PRESSURIZE. CABIN CLIMBS WITH THE AIRCRAFT. AT 4,000 F EET, THE CABIN PRESSURE WAS STILL READING 4,000 FEET. THE RIGHT PACK WAS ON MEL. FLIGHT RETURNED TO FIELD AT BOS AND L ANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK WATER SEPARA TOR COALESCER BAG (PN V121-1) AND FREED UP A STUCK 35 DEGREE CONTROL VALVE. OPERATIONAL CHECK GOOD. CLEARED RIGHT PACK MEL BY REPLACING THE 35 DEGREE TEMPERATURE CONTROL BOX (PN 607510-3). 2 L 7 2 4F RT A16WE 1998030500277 19980305 00277 NM 1998 3 5 USAASB98038 1 19980213 A 4920 3804284262 APU BOEING 737 737301 1384611 NM AFT FUSELAGE OIL CONTAMINATED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 574US 58211 23739 CLT - FLT 2333 - AIRCRAFT WAS DISPATCHED FROM DCA WITH THE NR 1 ENGINE CSD/GENERATOR ON MEL. AT FL 350, THE APU HAD AN AUTO SHUTDOWN WITH HIGH OIL TEMP. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARE D. MAINTENANCE FOUND THE APU HAD FAILED INTERNALLY DUE TO METAL IN THE OIL. APU HAS BEEN PROGRAMMED FOR REPLACEMENT AN D WAS RELEASED INOP PER MEL. THE MEL ON THE NR 1 ENGINE CSD/GENERATOR WAS CLEARED BY REMOVING AND REPLACING THE CSD AND THE OIL COOLER. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998030500278 19980305 00278 CE 1998 3 5 S2YA98006 1 19980214 A 3297 WIRE BEECH 1900 1900D 1154162 CE LANDING GEAR CHAFED A S2YA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 881SK UE88 MKE - FLT 6350 - DURING APPROACH, MKE TO MKE TRAINING FLIGHT, CREW SELECTED LG DOWN, DID NOT EXTEND. WHEN CREW SELECTED LANDING GEAR DOWN, LG RELAY CB OPENED. CREW DECLARED EMERG, MANUALLY EXTENDED MLG, AND AFTER RECEIVING A 3-DOWN LOCKED IND, MADE SAFE LANDING. MAINT INSP ACFT AND REPLACED LG GROUND SERVICE VALVE. AFTER GROUND CYCLES, ACFT TEST FLOWN, L G FAILED TO EXTEND WITH LG RELAY CB OPENING. MAINT INSP ACFT AND REPLACED TB-150, SPLICED A WIRE AT RT GEAR UPLOCK SWIT CH. AFTER GROUND CYCLES, ACFT TEST FLOWN, LG FAILED, CB OPENING. MAINT INSP, FND WIRE G11A22 CHAFING TO GROUND, LT WIN G CENTER SECT. WIRE REPAIRED, GEAR GROUND OPERATED, ACFT TEST FLOWN. TEST FLT SUCCESSFUL, ACFT RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 1998030500279 19980305 00279 CE 1998 3 5 S2YA98005 1 19980210 A 3230 RETRACT MECH BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A S2YA O OTHER J WARNING INDICATION AP APPROACH 1 GL 13 881SK UE88 MSN/MKE - FLT 1158 - DURING APPROACH, CREW SELECTED LANDING GEAR DOWN WHICH FAILED TO EXTEND. CREW DECLARED AN EMERGENC Y AND MANUALLY EXTENDED LANDING GEAR. AFTER RECEIVING ALL 3 GEAR DOWN AND LOCKED INDICATIONS, MADE UNEVENTFUL LANDING. MAINTENANCE INSPECTED AND GROUND OPERATED THE LANDING GEAR AND NO PROBLEMS NOTED WITH THE SYSTEM. AFTER A SATISFACTORY TEST FLIGHT, AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998030500280 19980305 00280 CE 1998 3 5 S2YA98004 1 19980115 A 3150 727725 CIRCUIT BREAKER BEECH 1900 1900D 1154162 CE RT COCKPIT FAILED A S2YA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 13 87SK UE87 GRR/MKE - FLT 1125 - DURING FLIGHT, SMOKE STARTED TO COME OUT FROM BEHIND THE RT COCKPIT CB PANEL. THE CREW STARTED PUL LING CIRCUIT BREAKERS UNTIL THEY FOUND THE ONE THAT MADE THE SMOKE STOP. ONCE THE SMOKE WAS STOPPED, THE CREW REQUESTED PRIORITY LANDING CLEARANCE. AFTER A SAFE LANDING IN MKE, MAINTENANCE REPLACED THE AURAL WARNING CIRCUIT BREAKER AND CL EANED THE GLYCOL OUT FROM BEHIND THE CIRCUIT BREAKER PANEL. (X) 2 L 7 2 4T RT A24CE 1998030500281 19980305 00281 CE 1998 3 5 S2YA98003 1 19980113 A 5270 SWITCH BEECH 1900 1900D 1154162 CE PASSENGER DOOR DIRTY A S2YA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 13 85SK UE85 MKE/CLE - FLT 1158 - DURING FLIGHT, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE CREW DIVERTED TO THE NEAREST SUITABLE A IRPORT, LAN. AFTER A SAFE LANDING, THE ANNNUNCIATOR WAS PLACED ON MEL. THE FLIGHT THEN CONTINUED ON TO CLE. ON 1-14-9 8, MAINTENANCE CLEARED THE CABIN DOOR ANNUNCIATOR SWITCH, OPERATION CHECKED GOOD, AND THE MEL WAS CLEARED. (X) 2 L 7 2 4T RT A24CE 1998030500282 19980305 00282 CE 1998 3 5 S2YA98002 1 19980112 A 5610 10138402521 WINDSHIELD BEECH 1900 1900D 1154162 CE LT COCKPIT CRACKED A S2YA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 891SK 5013 UE89 MKE/CMH - WHILE CLIMBING THROUGH FL 120, THE CAPTAIN'S WINDSHIELD CRACKED. THE CREW NOTIFIED ATC, DECLARED AN EMERGENC Y AND RETURNED TO MKE. AFTER MAKING A SAFE LANDING, MAINTENANCE REPLACED THE WINDSHIELD AND RETURNED AIRCRAFT TO SERVIC E. THE CRACK WAS FOUND IN THE OUTER PLY OF THE WINDSHIELD; WITH CRACKING IN THE OUTER PLY, CONTINUED FLIGHT IS ALLOWED. (X) 2 L 7 2 4T RT A24CE 1998030500283 19980305 00283 1998 3 5 S2YA98001 4 19980110 A 3416 ALTIMETER BEECH 1900 1900D 1154162 CE LT COCKPIT MALFUNCTIONED A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 81SK UE81 AT 2,000 FEET, THE CAPTAIN'S ALTIMETER FLAGGED AND THE AIRSPEED INDICATOR FROZE. THE CREW SWITCHED TO ALT STATIC, AND T HE AIRSPEED WENT TO NORMAL, ALTIMETER REMAINED FLAGGED. THE CREW RETURNED TO ESC. AFTER SAFE LANDING IN ESC, AIRCRAFT FERRIED TO MKE WHERE MAINTENANCE INSPECTED THE PITOT AND STATIC DRAINS, PERFORMED PITOT FUNCTION AND LEAK CHECK TO 280 K NOTS. PERFORMED A STATIC LEAK CHECK TO 24,000 FEET. NO DEFECTS NOTED IN EITHER THE PITOT OR STATIC SYSTEMS. (X) 2 L 7 2 4T RT A24CE 1998030500284 19980305 00284 NM 1998 3 5 TWAA9802203 1 19980211 A 4990 1601262 OIL REGULATOR BOEING 767 767205 1385121 NM APU LEAKING A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 650TW 23057 STL - FLT 842 - AIRCRAFT WAS OPERATING WITH THE LT GENERATOR PLACARDED INOPERABLE PER MEL. IN-FLIGHT, THE APU AUTO SHUT DOWN WITH EICAS MSG - APU LOW OIL PRESS. DIVERTED TO STL. REPLACED THE LEFT IDG AND PLACARDED THE APU INOP PER MEL. A IRCRAFT OPERATED TO LAYOVER STATION WHERE THE APU OIL COOLER/REGULATOR WAS REPLACED. CHECK-C 1-19-98 AT LAX. (X) 2 L 7 2 4F RT A1NM 1998030500285 19980305 00285 WP 1998 3 5 TWAA9802202 1 19980211 A 3350 57761 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 902TW 49153 STL - FLT 30 - THE EGRESS LIGHTING CAME ON IN-FLIGHT BETWEEN ROWS 15 AND 21. REPLACED BATTERY PACK. CHECK-C ON 1-25-98 STL. (X) 2 L 7 2 4F A6WE 1998030500286 19980305 00286 NM 1998 3 5 TWAA9802201 1 19980211 A 3350 6104783 POWER PACK BOEING 727 727231 1384079 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64339 20844 STL - DURING MAINTENANCE CHECK, THE AFT CABIN EGRESS LIGHTS WERE FOUND INOPERABLE FROM ROW 27 AFT. REMOVED WATER FROM E GRESS LIGHT STRIP AND REPLACED POWER PACK. CHECK-C 5-12-97 MCI. (X) 2 L 7 3 4F A3WE 1998030500287 19980305 00287 WP 1998 3 5 TWAA9802403 1 19980214 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9403W 53139 STL - DURING MAINTENANCE CHECK, FOUND EGRESS LIGHTS BURNED OUT AT ROWS 1, 4, 5, 22, 25, 28, AND 30. REPLACED LAMPS. CH ECK-C 11-6-97 LAX. (X) 2 L 7 2 4F RT A6WE 1998030500288 19980305 00288 NE 1998 3 5 TWAA9802402 2 19980216 A 7230 739483 BEARING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE LT ENGINE FAILED A TWAA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 CE 05 919TW 49368 3258 MEM - FLT 1226 - DURING FLIGHT, THE LEFT ENGINE, SPOOLED DOWN. MADE UNSCHEDULED LANDING AT MEM. REPLACED ENGINE. ENGI NE WAS DISASSEMBLED AND FOUND NR 3 BEARING WAS THE INITIAL FAILURE. IT THEN CAUSED OTHER FAILURES. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998030500289 19980305 00289 WP 1998 3 5 TWAA9802401 1 19980215 A 3350 14597101 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 986Z 47589 STL - DURING MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS OUT AT ROW 16 RT AND LT SIDES. REPLACED BATTERIES IN POWER PACK. CHECK-C 5-9-97 STL. (X) 2 L 7 2 4F A6WE 1998030500290 19980305 00290 1998 3 5 TWAA9802301 4 19980212 A 2320 TP4080X32128 PRINTER DOUG DC9 DC983 3022083 WP COCKPIT FAILED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 EIBWD 49575 STL - FLT 612 - DURING CRUISE, RECEIVED ELECTRICAL SHOCK FROM ACARS PRINTER WHEN TOUCHED. RECONNECTED CANNON PLUG ON AC ARS PRINTER, MFG PN TP4080X32128. OP-16 11-24-97 MCI. (X) 2 L 7 2 4F RT A6WE 1998030500291 19980305 00291 NM 1998 3 5 TWRA9804 1 19980126 A 2810 FUEL TANKS BOEING 747 747130 1384880 NM CTR WING LEAKING A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 603FF 19746 AFTER TAKEOFF ROLL, SMELLED A STRONG FUEL ODOR IN THE COCKPIT, UPPER DECK AND CENTER OF THE AIRCRAFT. ON TAXI THERE IS NO SMELL. BUT, WHEN AIRCRAFT PITCHES 13 DEGREES - 15 DEGREES IT SMELLS. A/C REMOVED FROM SERVICE. FOUND FUEL LEAKING FROM NR 2M, NR 3 AND CENTER WING TANKS, REPAIRED LEAKS IAW 28-22-00. APPLIED SECONDARY FUEL VAPOR BARRIER IAW 747-57-2 253. FUELED AIRCRAFT, NO LEAKS FOUND. (M) 2 L 7 4 4F A20WE 1998030500292 19980305 00292 NM 1998 3 5 TWRA9808 1 19980217 A 3350 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 611FF 20502 L1 BUSSLE LIGHT WILL NOT TURN OFF. PIN NR 3 MISSING GROUND PER WDM 33-59-11. REPAIRED GROUND AND OPS CHECK PER MM 33-5 1-00. L1 BUSSLE LIGHT OPS OK. (X) 2 L 7 4 4F A20WE 1998030500293 19980305 00293 NM 1998 3 5 TAOA029806 1 19980214 A 3397 WIRE BOEING 727 727254 138408L NM CABIN BROKEN A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 916TS 20437 EPL LIGHTS AT ROW 16 THROUGH ROW 19 INOPERATIVE AT FLOOR TRACK. REPAIRED BROKEN WIRE AND REINSTALLED EPL TRACK SECTION. OPERATIONAL CHECK NORMAL PER MM 33-50-0. (FLIGHT 6530 FOUND ON L/S LGA). (X) 2 L 7 3 4F A3WE 1998030500294 19980305 00294 NM 1998 3 5 TAOA029807 1 19980214 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 7319 20415 EMERGENCY EXIT LIGHT AT AFT EXIT DOOR IS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM 33-50-0 (F LIGHT 6541 FOUND ON L/S CHECK DCA). (X) 2 L 7 3 4F A3WE 1998030500295 19980305 00295 NM 1998 3 5 TAOA029805 1 19980212 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 21244 FLT 6141, L/S OVERNIGHT, EMERGENCY EXIT LAMP AT 3 ABC OVERHEAD INOPERATIVE. REPLACED BASE ASSEMBLY AND BATTERY PACK, OP ERATIONAL CHECK NORMAL PER MM 33-50-00. (M) 2 L 7 3 4F A3WE 1998030500296 19980305 00296 EU 1998 3 5 SIMA980422 1 19980211 A 5320 S5367131828001 SILL AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE BETWEEN FRAME 36 AND FRAME 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL PLATE IAW SER 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998030500297 19980305 00297 EU 1998 3 5 SIMA980421 1 19980211 A 5321 11S53173206003 FLOOR AEROSP ATR42 ATR42300 8680920 EU COCKPIT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 433MQ 151 SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THE COCKPIT COPILOT FLOOR PANEL BETWEEN FRAMES 7 AND 9 CORRODED. M AINTENANCE REPAIRED THE FLOOR PANEL IAW ATR DRAWING S531R0161 ISSUE A. AIR ISSUED A SRAS. AIRCRAFT RETURNED TO SERVICE . (X) 2 H 7 2 4T RT A53EU 1998030500298 19980305 00298 NM 1998 3 5 NOCA05/98 1 19980213 A 3350 767 LAMP BOEING 757 75728A 1384976 NM R4 DOOR FAILED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE AT DOOR R4. RELAMPED EXTERIOR EMERGENCY LIGHT AT DOOR R4. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A2NM 1998030500299 19980305 00299 NM 1998 3 5 P2EA98026 1 19980212 A 2910 HYDRAULIC LINE BOEING 737 737222 1384473 NM A HYD SYSTEM LEAKED A P2EA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 05 208AU 19547 THE AIRCRAFT EXPERIENCED LOSS OF A-SYSTEM HYDRAULIC QUANTITY IN-FLIGHT FROM MCI TO DFW. AN UNEVENTFUL LANDING ACCOMPLIS HED AT DFW. DELTA AIRLINES MAINTENANCE, A CONTRACT MAINTENANCE PROVIDER FOR VANGUARD AIRLINES, WAS DISPATCHED AND DISCO VERED A HYDRAULIC LINE WITH A PINHOLE WHICH CREATED THE LOSS OF QUANTITY AND PRESSURE. THE LINE, WHICH WAS LOCATED OUTB OARD OF THE RIGHT WHEELWELL, WAS REPLACED WITH A TEMPORARY FLEXIBLE LINE PER VANGUARD AIRLINES GMM CHAPTER 14. (X) 2 L 7 2 4F A16WE 1998030500300 19980305 00300 WP 1998 3 5 ORJA9824 1 19980211 A 3520 OXYGEN MASKS DOUG DC9 DC983 3022083 WP CABIN MALFUNCTIONED A ORJA O OTHER O OTHER CL CLIMB 1 WP 11 871RA 49788 AT LEVEL FLIGHT FL 310, CABIN PRESSURE ALT AT 6,500. F/A NOTIFIED ALL OXYGEN MASKS HAD DROPPED. PASSENGERS ADVISED NOT TO PULL MASKS. CHECKEDF OR GENERATOR ACTIVATION. RESET DOORS, PERFORMED OXYGEN MASK EJECT SWITCH CHECK PER MM 35-20-0 0. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A6WE 1998030500301 19980305 00301 NM 1998 3 5 MZZA98081 1 19980210 A 2131 7612608 CONTROLLER BOEING 727 7272F9 138407D NM CABIN FAILED A MZZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 13 75429 0536 21427 GUM - FLT 0975 - L/P 7963825 - AT APPROXIMATELY 25 MINUTES OUT AFTER TAKEOFF, CREW ADVISED CABIN CLIMBING AT 400 FEET P ER MINUTE WITH AIRCRAFT AT FL 29.0. UNABLE TO CONTROL PRESSURIZATION AT ALL MODES AUTO/STANDBY/MANUAL. MAINTENANCE TRO UBLESHOT SYSTEM AND REPLACED CABIN PRESSURE CONTROLLER PER MM 21-31-00. GROUND CHECKS OK. MAINTENANCE REQUEST CREW FOR EVALUATION AND SUBSEQUENT FLIGHTS. ALL SYSTEM WORKS NORMAL. (X) 2 L 7 3 4F RT A3WE 1998030500302 19980305 00302 NE 1998 3 5 HALA9800040 2 19980209 A 7250 TURBINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE FAILED A HALA C D ABORTED TAKEOFF RETURN TO BLOCK Y ENGINE STOPPAGE TO TAKEOFF 1 WP 13 601AP 47658 69669 HNL - FLT 158 - ON TAKEOFF ROLL FROM HNL, THE NR 2 ENGINE TURBINE CAME APART. IN PROCESS OF INSPECTING A/C FOR DAMAGE A ND CHANGING OUT THE NR 2 ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 1998030500303 19980305 00303 NM 1998 3 5 USAABB98017 1 19980107 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 LAX - FOUND EXIT IDENTIFIER INOPERATIVE AT R1 DOOR. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A2NM 1998030500304 19980305 00304 NM 1998 3 5 MZZA98079 1 19980208 A 3260 2314143 SWITCH BOEING 727 727224 1384076 NM LT MLG DOOR INOPERATIVE A MZZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 69741 22250 GUM - FLT 0949 - L/P 7950069 - AIR RETURN DUE TO LEFT LANDING GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION. MAINTE NANCE REQUESTED FOR FLY-BY TO CONFIRM GEAR DOOR CLOSED. MAINTENANCE TROUBLESHOT SYSTEM, FOUND LEFT LANDING GEAR DOOR SW ITCH BAD. PLACARDED DOOR LIGHT INOP AND FLT DISPATCHED WITHOUT FURTHER INCIDENT. SAIPAN STATION REMOVED AND REPLACED L EFT GEAR DOOR WARNING SWITCH PER MM 32-62-11. OPS CHECKS GOOD AND RELEASED AIRCRAFT FOR SERVICE. (X) 2 L 7 3 4F A3WE 1998030500305 19980305 00305 NM 1998 3 5 K3HA980016 1 19980223 A 3350 110049 BATTERY CHARGER BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 FORWARD PORTION OF EMERGENCY PATH LIGHTING WAS OUT. INSTALLED NEW BATTERY CHARGER. 2 L 7 3 4F A3WE 1998030500306 19980305 00306 NM 1998 3 5 K3HA980017 1 19980219 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN EXPOSED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 EMERGENCY PATH LIGHT TRACK OUT AND WIRING EXPOSED FORWARD ACROSS FROM FORWARD GALLEY. REPOSITIONED EMERGENCY PATH LIGHT ING TRACK. 2 L 7 3 4F A3WE 1998030500307 19980305 00307 NM 1998 3 5 K3HA980018 1 19980222 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN CORRODED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT DOES NOT COME ON. CLEANED BATTERY TERMINALS. OPERATIONAL CHECKS OK. 2 L 7 3 4F A3WE 1998030500308 19980305 00308 NM 1998 3 5 RAAA98B2009 1 19980225 A 3350 1000679 EMERGENCY LIGHT BOEING 727 72722C 138400F NM CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 MID CABIN DOOR EMERGENCY EXIT LIGHT FLASHES ON AND OFF. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 3 4F A3WE 1998030500310 19980305 00310 WP 1998 3 5 CALA9800330 1 19980224 A 2797 WIRE DOUG DC9 DC981 3022081 WP HORIZ STAB BURNED A CALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 SW 09 16884 48074 THE AIRCRAFT WAS RETURNED TO IAH WHEN THE PRIMARY TRIM BECAME INOPERATIVE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE OPENED DOGHOUSE ON VERTICAL STABILIZER AND FOUND WIRE BUNDLES BURNED. NEW WIRES WERE SPLICED IN TO PLUG P 10-399 FOR PRIMARY TRIM MOTOR IAW MM 27-41-01 AND STANDARD PRACTICES 20-50-01. THE WIRING IN THE AREA WAS INSPECTED AND WRAPPED IAW STANDARD PRACTICES. THE PRIMARY TRIM MOTOR WAS REMOVED AND REPLACED IAW MM 27-40-01. WIRING CLEARANCE AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998030500311 19980305 00311 NE 1998 3 5 CALA9800331 2 19980226 A 7230 BEARING BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A CALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 09 14334 23572 721737 THE AIRCRAFT WAS DIVERTED TO SHV AFTER THE NR 2 ENGINE GAVE OFF TWO LOUD BANGS FOLLOWED BY AIRCRAFT VIBRATION AND WITH T HE NR 2 ENGINE GOING TO IDLE. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE GEARBOX A FT CHIP DETECTOR FULL OF METAL CHIPS AND THE COMPRESSOR COULD NOT BE TURNED. THE NR 2 ENGINE WILL BE REPLACED. TEARDOW N REVEALED NR 4 BEARING FAILURE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998030500312 19980305 00312 NM 1998 3 5 CALA9800332 1 19980224 A 3350 20131A BATTERY RADIANT BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12313 23364 THE R-1 INSIDE OVERDOOR LIGHT, L-1 OUTSIDE SLIDE LIGHT, AND INSIDE FRONT STANDBY LIGHTS FAILED BATTERY CHECK. REPLACED BATTERY PACK AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998030500313 19980305 00313 NM 1998 3 5 CALA9800333 1 19980224 A 3350 20131A BATTERY RADIANT BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12313 23364 THE R-2 INSIDE OVER DOOR LIGHT, L-2 OUTSIDE SLIDE LIGHT, AND CENTER BACK OVERHEAD LIGHTS FAILED BATTERY CHECK. REPLACED BATTERY PACK AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998030500314 19980305 00314 WP 1998 3 5 CALA9800334 1 19980225 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 INSPECTION FOUND AFT BAGGAGE BIN VERTICAL THRESHOLD SUPPORT BETWEEN STA 1155 AND 1212 CORRODED. A NEW STANDOFF WAS INST ALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998030500315 19980305 00315 WP 1998 3 5 CALA9800335 1 19980226 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 INSPECTION FOUND A 1.5 CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. THE BEAM WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998030500316 19980305 00316 WP 1998 3 5 CALA9800336 1 19980226 A 5312 BULKHEAD T DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 2.5 CRACK THROUGH FASTENER HOLE ON VERTICAL LEG OF BULKHEAD T AT STA 1156 BETWEEN LONGERON 40L AND 39 L. A NEW TEE CAP WAS INSTALLED IAW EA SA003-5310-03391. 2 L 7 3 4F A22WE 1998030500317 19980305 00317 WP 1998 3 5 CALA9800337 1 19980226 A 5400 STIFFENER DOUG DC10 DC1010 3022110 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN VERTICAL STIFFENER AT TOP OF NR 1 PYLON ON AFT SIDE OF YN 342.0 FORGING AT INBOARD SI DE. REPAIR WAS ACCOMPLISHED IAW SRM 54-00-01. 2 L 7 3 4F A22WE 1998030500318 19980305 00318 WP 1998 3 5 CALA9800338 1 19980226 A 5754 RIB DOUG DC10 DC1010 3022110 WP NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 4 CRACK IN FLANGE OF LT NR 1 SLAT OUTBOARD END RIB. THE WEB AND RIB WERE REMOVED IAW SRM 51-31-10. A NEW RIB WAS INSTALLED IAW 51-31-10 AND 51-21-01. SKIN WAS INSTALLED IAW SRM 51-01-10. 2 L 7 3 4F A22WE 1998030500319 19980305 00319 WP 1998 3 5 CALA9800339 1 19980226 A 5751 RIB DOUG DC10 DC1010 3022110 WP LT AILERON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN OUTBOARD RIB OF LT OUTBOARD AILERON. THE RIB WAS REMOVED AND A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 57-51-01. 2 L 7 3 4F A22WE 1998030500320 19980305 00320 WP 1998 3 5 CALA9800340 1 19980226 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 580-595 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LONGERON 48L CORRODED AROUND FASTENERS FROM STA 595 FORWARD TO STA 580 INSIDE OF LT A/C BAY. THE LONGE RON WAS REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998030500321 19980305 00321 WP 1998 3 5 CALA9800341 1 19980226 A 5720 BRACKET DOUG DC10 DC1010 3022110 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION AT BRACKET ATTACHED TO RT WING TRAILING EDGE BEAM WHERE PANEL REMOVED, FORWARD OF NR 1 SPOILE R OUTBOARD HINGE AREA. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-33-01, 53-00-01, AND 51-21-01. 2 L 7 3 4F A22WE 1998030500322 19980305 00322 EA 1998 3 5 COMA9860048 1 19980224 A 3241 140153 TRANSDUCER CNDAIR CL600 CL6002B19 EA LT MLG DESTROYED A COMA L A ABORTED APPROACH UNSCHED LANDING O OTHER AP APPROACH 1 SO 01 978CA 3069 7158 ANTI-SKID CAUTION MESSAGE WHEN LANDING GEAR EXTENDED. REPLACED THE LEFT OUTBOARD WHEEL SPEED TRANDUCER. 2 L 7 2 4F RT A21EA 1998030500323 19980305 00323 EU 1998 3 5 WWMA9800041 1 19980225 A 2613 7239019506 TEST PANEL SAAB SF340 340B 7860101 EU NR 1 ENGINE DEFECTIVE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 269AE 340B269 DURING PREFLIGHT, LEFT TAILPIPE HOT LIGHT WOULD NOT TEST. REPLACED SERVICABLE OVERHEAD TEST PANEL NR 1. 2 L 7 2 4T RT A52EU 1998030500324 19980305 00324 EU 1998 3 5 WWMA980040 1 19980226 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 343SB 340B343 EMERGENCY LIGHTS CAME ON IN FLIGHT. REPLACED ALL 5 EMERGENCY LIGHT BATTERIES. 2 L 7 2 4T RT A52EU 1998030500325 19980305 00325 EU 1998 3 5 WWMA9800039 1 19980226 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE L NO TEST CR CRUISE 1 WP 15 243AE 340B243 EMERGENCY EXIT SIGN AT 8A WAS FOUND TO BE HANGING BY THE WIRES. MAINTENANCE REINSTALLED INTERNAL SCREWS IN THE EXIT SIG N AND PERFORMED OPERATIONAL CHECKS. 2 L 7 2 4T RT A52EU 1998030500326 19980305 00326 EU 1998 3 5 WWMA9800038 1 19980224 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 324AE 340B324 EMERGENCY LIGHTS AT SEATS 7BC AND 8A FAILED TO ILLUMINATE DURING PREFLIGHT TEST. REPAIRED BROKEN WIRE AT FUSE AND REPLA CED EMERGENCY POWER SUPPLY. 2 L 7 2 4T RT A52EU 1998030500339 19980305 00339 EU 1998 3 5 QXEA9800119 1 19980225 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU LT EMER EXIT FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 GEG - LEFT AFT OVERWING EMERGENCY EXIT LIGHT IS INOP. RELAMPED EXIT LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998030500340 19980305 00340 WP 1998 3 5 98FDEA00140 1 19980217 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP BS 459 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 391FE 46625 VCE: N2103 - AT STA NR 459 Z= -78, X = - 63 A CRACK WAS FOUND ON THE FRAME (RT SIDE). REF NRC NR N2064. REPAIRED FRAM E IAW SRM 53-30-00, FIG 5. 2 L 7 3 4F A22WE 1998030500341 19980305 00341 WP 1998 3 5 ABXA9800114 1 19980126 A 5712 57694684 RIB DOUG DOUG DC8 DC861 3021952 WP WS 585 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 RIGHT WING LEADING EDGE, OUTBOARD OF NR 4 PYLON INBOARD LWR RIB CRACKED AT XFS 585. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998030500342 19980305 00342 WP 1998 3 5 ABXA9800115 1 19980126 A 5712 576947140 RIB DOUG DOUG DC8 DC861 3021952 WP WS 497.491 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 RIGHT WING LEADING EDGE RIB AT STA XS 497.491 IS CRACKED AT AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998030500343 19980305 00343 WP 1998 3 5 ABXA9800116 1 19980126 A 5320 4750521IN SPLICE DOUG DOUG DC8 DC861 3021952 WP BS 690 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LONGERON NR 1 SPLICE FITTING CRACKED AT STA 690. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998030500344 19980305 00344 WP 1998 3 5 ABXA9800117 1 19980126 A 5311 56100883 FRAME DOUG DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 FRAME 80 INBOARD FLANGE CRACKED AT LONGERON 8L. REPAIRED IAW DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998030500345 19980305 00345 WP 1998 3 5 ABXA9800118 1 19980126 A 5720 36436363 BRACKET DOUG DOUG DC8 DC861 3021952 WP WS 63 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LEFT WING SPAR AREA AT STA XFS 63 HAS CRACKED BRACKET. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3643636. 2 L 7 4 4F 4A25 1998030500346 19980305 00346 WP 1998 3 5 ABXA9800119 1 19980126 A 5720 576951521 ANGLE DOUG DOUG DC8 DC861 3021952 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LEFT WING OUTBOARD OF NR 2 PYLON UPPER STIFFENER ANGLE IS CRACKED. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998030500347 19980305 00347 WP 1998 3 5 ABXA9800120 1 19980126 A 5712 576947135 RIB DOUG DOUG DC8 DC861 3021952 WP WS 741.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LEFT WING LEADING EDGE RIB, STA XFS 741.25 CRACKED AT UPPER END. REPAIRED IAW DWG K05056-7008 AND DC8 SRM 51-18 AND 51- 1-20D. 2 L 7 4 4F 4A25 1998030500348 19980305 00348 WP 1998 3 5 ABXA9800121 1 19980126 A 5712 5769469 RIB DOUG DOUG DC8 DC861 3021952 WP WS 192 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 RIGHT WING LEADING EDGE, INBOARD OF NR 3 PYLON, LEADING EDGE PANEL, UPPER RIB CRACKED AT STA XFS 192. REPAIRED IAW DC8 SRM 51-1-20D AND ABX DWG K0-5056-7007. 2 L 7 4 4F 4A25 1998030500349 19980305 00349 WP 1998 3 5 ABXA9800122 1 19980126 A 5720 576985937 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LEADING EDGE STUB WING INBOARD, UPPER INTERCOSTAL CRACKED. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 5769859-37. 2 L 7 4 4F 4A25 1998030500350 19980305 00350 WP 1998 3 5 ABXA9800123 1 19980126 A 5712 576958981 RIB DOUG DOUG DC8 DC861 3021952 WP WS 6225 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 LT WING L/E RIB AT STA XOLDI 6225, ABOVE THE PNEUMATIC DUCT IS CRACKED, APPROXIMATELY 2.75. REPAIRED IAW DC8 SRM 57-2-0 . 2 L 7 4 4F 4A25 1998030500351 19980305 00351 WP 1998 3 5 MWEA98211 1 19980225 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FLOORBEAM SUPPORT STRUT AT FS 965 FOUND CORRODED OVER A LARGE AREA. REMOVED AND REPLACED STRUT. 2 L 7 2 4F A6WE 1998030500352 19980305 00352 WP 1998 3 5 MWEA98212 1 19980225 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE FS 965 FLOORBEAM LEFT SUPPORT STRUT FOUND WITH NUMEROUS AREAS OF CORROSION. REPAIRED DAMAGED SECTION OF SUPPORT STR UT. 2 L 7 2 4F A6WE 1998030500353 19980305 00353 WP 1998 3 5 MWEA98213 1 19980225 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 718 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 STATIC DISCHARGE DAMAGE WAS FOUND ON EXTERNAL FUSELAGE SKIN FS 718 LONGERON 2R. FABRICATED AND INSTALLED REPAIR DOUBLER . 2 L 7 2 4F A6WE 1998030500354 19980305 00354 WP 1998 3 5 MWEA98214 1 19980225 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 A DENT WITH AERODYNAMIC FILLER WAS FOUND AT FS 218 LONGERON 16R TO 17R INVESTIGATION REVEALED THE DENT TO BE OUT OF LIMI TS. REMOVED AND REPLACED SECTION OF SKIN. 2 L 7 2 4F A6WE 1998030500355 19980305 00355 NM 1998 3 5 DLM90980472 1 19980224 A 5610 WINDSHIELD 5912290507 DOUG MD90 MD9030 3023690 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 908DA 53388 BURNING SMELL FROM BEHIND TRIM AT CAPT/CENTER WINDSHIELD. FOUND WINDOW HEAT CONNECTION TERMINAL DAMAGED. REPLACED CONN ECTOR AND HARNESS. ALSO, REPLACED WINDSHIELD. 2 L 7 2 4F RT A6WE 1998030500356 19980305 00356 NM 1998 3 5 DLM88980473 1 19980224 A 3510 OXY MASK MC1004101 DOUG MD88 MD88 3023688 NM RT COCKPIT FAILED A DALA K NONE O OTHER CR CRUISE 1 SO 27 999DN 53371 FIRST OFFICER'S O2 MASK HARNESS FAILED WHILE ATTEMPED TO USE IN FLT. REPLACED FIRST OFFICERS MASK ASSEMBLY. 2 L 7 2 4F RT A6WE 1998030500357 19980305 00357 NM 1998 3 5 DL75A980474 1 19980224 A 3320 920056 SWITCH BOEING 757 757212 NM CABIN INTERMITTENT A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 750AT 23126 INFLIGHT, FLIGHT ATTENDANT AND PASSENGER REPORTED FUMES WHICH SMELLED LIKE SMOLDERING RUBBER IN THE AREA OF THE LAST THR EE ROWS IN PASSENGER CABIN. STRONGER ON CO-PILOTS SIDE. FUMES WERE INTERMITTENT. MAINTENANCE CHECKED AREA, NO VISIBLE SIGNS OF FUMES. NO HOT AREAS LOCATED BEHIND PSU'S OR SIDEWALLS. FOUND 45F READING LIGHT FLICKERING. REPLACED READING LIGHT SWITCH. OPERATION CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1998030500358 19980305 00358 NM 1998 3 5 DL72W980476 1 19980223 A 5330 65562312 SKIN BOEING 727 727247 138408F NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FUSELAGE SKIN R1 DOOR CUTOUT UPPER HINGE CUTOUT, REPAIR FOR CRACK IN REINFORCING DOUBLER (BEAR STRAP). THE UPPER HINGE CUTOUT OF THE R1 DOOR CUTOUT WAS FOUND TO HAVE A TYPICAL CRACK IN THE REINFORCING DOUBLER (BEAR STRAP) THE CRACK WAS IN LOCATION D PER BOEING S/B 727-53-0136. THE CRACK WAS REPAIRED WITH A SKIN DOULBER PER THE S/B AND AS DOCUMENTED IN ER/ A 364078-14. 2 L 7 3 4F A3WE 1998030500359 19980305 00359 NM 1998 3 5 DL76L980477 1 19980224 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 191DN 28448 ON LAYOVER CHECK, FOUND EMERGENCY LIGHT INOP AT 22B. FOUND BROKEN WIRE AT PLUG NEAR SIDEWALL. REPAIRED BROKEN WIRE. E MERGENCY LIGHT CK OK. 2 L 7 2 4F RT A1NM 1998030500360 19980305 00360 WP 1998 3 5 DHL98807002 1 19980226 A 3244 26014112 TIRE DOUG DC8 DC873F 302199F WP MLG FAILED A DHLA K NONE O OTHER LD LANDING 1 SO 01 807DH 45990 NR 4 MAIN BLOWN ON TAXI IN. REMOVED AND REPLACED MAIN WHEEL ASSY. 2 L 7 4 4F RT 4A25 1998030500361 19980305 00361 SO 1998 3 5 SWIA971084 1 19980221 A 5230 RETRACT MECH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 196SW 120151 AFTER TAKEOFF, LEFT MAIN GEAR WOULD NOT RETRACT. CYCLED TWICE AND FIRST TRY SHOWED ONLY RED LIGHTS FOR LEFT. SECOND SH OWED RED AND GREEN LIGHTS FOR LEFT GEAR. FOUND LEFT FORWARD INBOARD GEAR DOOR OPEN. CLOSED DOOR AND ADJUSTED SPRING FO R DOOR LATCHES. PERFORMED LANDING GEAR RETRACTION CHECKS AND CYCLED GEAR SEVERAL TIMES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998030500362 19980305 00362 SO 1998 3 5 SWIA971085 1 19980223 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG FAILED A SWIA O OTHER N FALSE WARNING DE DESCENT 1 NM 07 186SW 120034 RIGHT MAIN GEAR IGNITION A GREEN LIGHT ON IN FLIGHT. GEAR WOULD NOT EXTEND NORMALLY SO USED EMERGENCY OVERRIDE TO EXTEN D. REPLACED RIGHT MAIN A SYSTEM DOWN LOCK SENSOR PER MM 32-60-00. LANDING GEAR FUNCTIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998030500363 19980305 00363 1998 3 5 SWIA971086 4 19980222 A 3417 ADC CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 1 FAILED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 410SW 7066 ON APPROACH TO EUG PFD NR 1 LOST ALL AIR DATA (AIRSPEED, ALTITUDE, ATTITUDE, VSI) ALSO MACH TRIM. REMOVED AND REPLACED IDC 4000 CONVERTER. ALL SYSTEMS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 1998030500364 19980305 00364 SO 1998 3 5 SWIA971087 1 19980224 A 3230 12038594001 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 196SW 120151 ON APPROACH INTO SAN, SELECTED GEAR DOWN AND GEAR HUNG FOR 45 SECONDS TO 1 MINUTE THEN ALL THREE GEAR CAME DOWN. INSTAL LED SERVICEABLE LANDING GEAR CONTROL BOX AND SWUNG LANDING EXTENSIVELY. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998030500365 19980305 00365 SO 1998 3 5 SWIA971088 1 19980227 A 3020 INLET BOOT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 224SW 120294 RIGHT ENGINE INLET DE-ICE BOOT FAILED IN FLIGHT. RETURNED TO FIELD. REPLACED INLET DUCT ASSEMBLY WITH SERVICEABLE DUCT AND DE-ICE BOOT. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998030500366 19980305 00366 SO 1998 3 5 SWIA971089 1 19980223 A 2731 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE ELEVATOR TRIM DIRTY A SWIA O OTHER J WARNING INDICATION CR CRUISE 1 NM 07 220SW 120288 TRIM WHEEL FROZEN IN FLIGHT, WHICH KICKED AUTO PILOT OFF DUE TO TRIM FAILURE. DESCENDED TO LOWER ALTITUDE WHERE TRIM RE TURNED TO NORMAL OPERATION. CLEANED AUTO HUB BOTH LEFT AND RIGHT ELEVATOR TRIM ACTUATOR. OPS CHECKS GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1998030500367 19980305 00367 EA 1998 3 5 SWIA971091 1 19980224 A 2750 FECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 410SW 7066 FLAP FAIL MSESSAGE DURING FLAP RETRACTION ON CLIMB-OUT. RETURNED FOR LANDING. REMOVED FLAP PDU AND FECU AND REPLACED W ITH SERVICEABLE UNITS IAW MM 27-52-01. ALL CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1998030500368 19980305 00368 NM 1998 3 5 P5CA9800250 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 614-642 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION LT/W MIDSPAR W/S 614-642 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10 -02. BLENDED OUT WITHIN SRM LIMIT 57-30-01. 2 L 7 4 4F A20WE 1998030500369 19980305 00369 NM 1998 3 5 P5CA9800251 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 660-680 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FRONT SPAR AREA WS 660-680 UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-0 2. BLENDED OUT WITHIN SRM LIMIT 57-30-01. 2 L 7 4 4F A20WE 1998030500370 19980305 00370 NM 1998 3 5 P5CA9800252 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1112-1155 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION LT WING FRONT SPAR WS 1112-1155 UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10- 02. BLENDED OUT WITHIN SRM LIMIT 57-30-01. 2 L 7 4 4F A20WE 1998030500371 19980305 00371 NM 1998 3 5 P5CA9800253 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND AT LT WING O/B LOWER SKIN T/E AREA PREVIOUS REWORK AREA O/B AILERON MID AREA. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 BLEND OUT WITHIN SRM LIMIT 57-30-01. 2 L 7 4 4F A20WE 1998030500372 19980305 00372 NM 1998 3 5 P5CA9800254 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND LT WING LOWER SKIN O/B SURFACE AT MID SPAR BETWEEN PANEL 554GB AND 555 AB. REMOVED CORROSION AN D TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS PER 57-30-01. 2 L 7 4 4F A20WE 1998030500373 19980305 00373 NM 1998 3 5 P5CA9800255 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 382-411 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND LT WING MID SPAR AREA WS 382-411 AND WBL 150-235 UPPER SURFACE SKIN. CORROSION REMOVED AND TRE ATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01. 2 L 7 4 4F A20WE 1998030500374 19980305 00374 NM 1998 3 5 P5CA9800256 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 350-380 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND LEFT WING SPANWISE BEAM NR 3 AREA WS 350 - 380 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATE D PER SRM 51-10-01 AND 51-70-02. BLENDED OUT WITHIN SRM LIMIT 57-30-01. 2 L 7 4 4F A20WE 1998030500375 19980305 00375 NM 1998 3 5 P5CA9800257 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 440-455 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 440-455 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51 -10-01 AND 51-10-02. BLEND OUT WITHIN SRM LIMIT 57-30-01. 2 L 7 4 4F A20WE 1998030500376 19980305 00376 NM 1998 3 5 P5CA9800258 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 469-499 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREAS WS 469-499 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 5 1-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT PER 57-30-01. 2 L 7 4 4F A20WE 1998030500377 19980305 00377 NM 1998 3 5 P5CA9800259 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 520-530 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 520-530 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51 -10-01, 51-10-02. BLENDED OUT PER SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500378 19980305 00378 NM 1998 3 5 P5CA9800260 1 19980218 A 5730 SKIN BOEING 747 747128 1384894 NM WS 557-586 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND LEFT WING MIDSPAR AREA WS 557-586 UPPER SURFACE SKIN. CORROSION REMOVED AND TREATED PER SRM 51 -10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT PER 57-30-01. 2 L 7 4 4F A20WE 1998030500379 19980305 00379 NM 1998 3 5 P5CA9800261 1 19980218 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1130 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND ON NUTPLATE SUPPORT RT STA 1130 AT UPPER WING TO BODY FILLET FAIRING AREA. CORROSION REMOVED A S PER SRM 51-10-01 AND TREATED AS PER 51-10-02. 2 L 7 4 4F A20WE 1998030500380 19980305 00380 NM 1998 3 5 P5CA9800262 1 19980218 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1580 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORRSOION, FOUND FUSELAGE BODY FAIRING SUPPORT AT BS 1580 LBL LEFT 0 THROUGH 245. REMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMITS 53-30-01. 2 L 7 4 4F A20WE 1998030500381 19980305 00381 NM 1998 3 5 P5CA9800263 1 19980218 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1620 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND AT FUSELAGE BODY FAIRING SUPPORT AT BS 1620 LBL O THROUGH 60. CORROSION REMOVED AND TREATED PE R SRM 51-10-01 AND 51-10-02. BLENDED OUT AND REPAIRED PER 53-50-04. 2 L 7 4 4F A20WE 1998030500382 19980305 00382 NM 1998 3 5 P5CA9800264 1 19980218 A 5350 FAIRING BOEING 747 747128 1384894 NM FUSELAGE DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE BODY FAIRING EXTERIOR MID AREA FOUND DELAMINATION FAIRING 192KR. BODY FAIRING FIBERGLASS REPAIRED PER SRM 51-4 0-14. 2 L 7 4 4F A20WE 1998030500383 19980305 00383 NM 1998 3 5 P5CA9800265 1 19980218 A 5280 DOOR BOEING 747 747128 1384894 NM LT MLG STRUT DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT W/G I/B STRUT DOOR AFT EXTERIOR SKIN FOUNDED DEBONDED AT I/B EDGE. FIBERGLASS REPAIRED PER SRM 51-40-06 PARA 2E. 2 L 7 4 4F A20WE 1998030500384 19980305 00384 NM 1998 3 5 P5CA9800266 1 19980218 A 5280 DOOR BOEING 747 747128 1384894 NM LT MLG STRUT CRACK A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT W/G I/B STRUT DOOR, FWD END FAIRING FWD EDGE FOUND FABRIC CRACK. FIBERGLASS REPAIRED AS PER SRM 51-40-06 APRA 2E. 2 L 7 4 4F A20WE 1998030500385 19980305 00385 NM 1998 3 5 P5CA9800268 1 19980218 A 5753 FOREFLAP BOEING 747 747128 1384894 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING O/B FLAP NOSE AREA NR 8 FLAP TRACK I/B FOUND SPONGED AS MARKED APPROX 4 BY 6 INCHES. FIBERGLASS REPAIRED AS PER SRM 51-40-14. 2 L 7 4 4F A20WE 1998030500386 19980305 00386 NM 1998 3 5 P5CA9800270 1 19980218 A 7110 COWL BOEING 747 747128 1384894 NM NR 2 ENGINE DISBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 2 LEFT FAN COWL INTERNAL MIDDLE AREA HONEY COMB DISBONDED. HOT BOND REPAIRED AS PER SRM 51-40-06 FIG 17A. HOT BOND REPAIRED AS PER SRM 51-40-06 FIG 17A. 2 L 7 4 4F A20WE 1998030500387 19980305 00387 NM 1998 3 5 P5CA9800271 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 2598 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DENT FOUND IN RT BODY SKIN AT 6 O'CLOCK POSITION ON SKIN AFT OF STA 2598 WL 212. DENT AREA PATCH REPAIRED AS PER SRM 53 -50-03 FIG 4 AND SRWS 912822. 2 L 7 4 4F A20WE 1998030500388 19980305 00388 NM 1998 3 5 P5CA9800272 1 19980214 A 5512 SKIN BOEING 747 747128 1384894 NM HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, DELAMINATION AND CRACK ON LEFT HORIZONTAL STABLIZER INBOARD TRAILING EDGE FIXED PANEL. DAMAGED AREA TRIMMED PER BAC SRM 51-10-01 AND FIBERGLASS REPAIR MADE PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998030500389 19980305 00389 NM 1998 3 5 P5CA9800273 1 19980214 A 5512 SKIN BOEING 747 747128 1384894 NM HORIZ STAB DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DELAMINATION IN SEVERAL OUTBOARD AREAS ON RIGHT HORIZONTAL STABILIZER TRAILING EDGE FIXED PANEL. TRIMMED DAMAGE PER BAC SRM 51-10-01 AND MADE FIBERGLASS REPAIR PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998030500390 19980305 00390 NM 1998 3 5 P5CA9800274 1 19980214 A 5512 SKIN BOEING 747 747128 1384894 NM HORIZ STAB CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 CRACK ON RIGHT HORIZONTAL STABILIZER TRAILING EDGE FIXED PANEL INBOARD AREA. TRIMMED DAMAGE PER BAC SRM 51-10-01 AND MA DE FIBERGLASS REPAIR PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998030500391 19980305 00391 NM 1998 3 5 P5CA9800275 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 2618 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DENT FOUND IN SKIN AND SUSPECT SKIN CRACK AT 6 O'CLOCK POSITION AT STA 2618. DENT AREA DRESSED PER SRM 51-10-01 AND TRE ATED PER SRM 51-01-02 AND CONDITION CHECK FOUND WITHIN SRM 53-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500392 19980305 00392 NM 1998 3 5 P5CA9800276 1 19980214 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1760/1780 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DENT ON FUSELAGE SKIN AT BS 1760 TO 1780, STR 41R AND 42R. BLENDED DAMAGED AREA PER BAC SRM 51-40-01 AND PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION, NO CRACKS FOUND. 2 L 7 4 4F A20WE 1998030500393 19980305 00393 NM 1998 3 5 P5CA9800277 1 19980218 A 5313 STRINGER BOEING 747 747128 1384894 NM BS 910-920 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FWD CARGO COMPARTMENT BS 910-920 STRINGER FOUND CORROSION. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1 REFSRWS 912817. 2 L 7 4 4F A20WE 1998030500394 19980305 00394 NM 1998 3 5 P5CA9800278 1 19980214 A 5522 SKIN BOEING 747 747128 1384894 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DELAMINATION ON SEVERAL AREAS OF LEFT OUTBOARD ELEVATOR UPPER SURFACE. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500395 19980305 00395 NM 1998 3 5 P5CA9800279 1 19980218 A 5730 PANEL BOEING 747 747128 1384894 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING TOP T/E FIXED PANEL DEBONDED AND A PUNCH HOLD FOUND AT I/B AILERON I/B. FIBERGLASS REPAIRED AS PER SRM 51-40-15 . 2 L 7 4 4F A20WE 1998030500396 19980305 00396 NM 1998 3 5 P5CA9800280 1 19980214 A 5512 PANEL BOEING 747 747128 1384894 NM HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON UPPER SURFACES OF ALL TRAILING EDGE FIXED PANELS ON LEFT HORIZONTAL STABIBLIZER. REMOVED CORROSIO N AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500397 19980305 00397 NM 1998 3 5 P5CA9800281 1 19980218 A 7110 COWL BOEING 747 747128 1384894 NM NR 2 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 2 T/R FAN TRANSLATING COWL AT 9 O'CLOCK POSITION RT SIDE DENTED. REPAIRED AS PER SRM 51-40-00 PARA 2E. 2 L 7 4 4F A20WE 1998030500398 19980305 00398 NM 1998 3 5 P5CA9800282 1 19980226 A 5620 WINDOW BOEING 747 747122 1384872 NM RT UPPER DECK CRAZED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 FOUND MOST AFT WINDOW ON RT SIDE UPPER DECK CRAZED. REMOVED AND REPLACED PER MM 56-21-00. 2 L 7 4 4F A20WE 1998030500399 19980305 00399 NM 1998 3 5 P5CA9800283 1 19980214 A 5522 SKIN BOEING 747 747128 1384894 NM LT ELEVATOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 CRACK ON UPPER SURFACE OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500400 19980305 00400 NM 1998 3 5 P5CA9800284 1 19980214 A 5522 SKIN BOEING 747 747128 1384894 NM RT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DELAMINATION ON SEVERAL AREAS OF THE RIGHT OUTBOARD ELEVATOR UPPER SURFACE. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15 . 2 L 7 4 4F A20WE 1998030500401 19980305 00401 NM 1998 3 5 P5CA9800285 1 19980214 A 5512 PANEL BOEING 747 747128 1384894 NM HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON THE UPPER SURFACE OF ALL TRAILING EDGE FIXED PANELS ON THE RIGHT HORIZONTAL STABILIZER. REMOVED C ORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500402 19980305 00402 NM 1998 3 5 P5CA9800286 1 19980214 A 5312 BULKHEAD BOEING 747 747128 1384894 NM BS 2658 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON THE FORWARD SIDE OF THE APU BULKHEAD AT STATION 2658, RIGHT BODY LINE 512. CORROSION REMOVED AND AREA TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500403 19980305 00403 NM 1998 3 5 P5CA9800287 1 19980214 A 5522 SKIN BOEING 747 747128 1384894 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DELAMINATION ON UPPER SURFACE OF LEFT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500404 19980305 00404 NM 1998 3 5 P5CA9800288 1 19980217 A 5240 SKIN BOEING 747 747128 1384894 NM SERVICE DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UD R/H/S CREW SERVICE DOOR FWD AND AFT CORNER CRACKED. SKIN REPAIR PER SRM 52-00-03 FIG 3. 2 L 7 4 4F A20WE 1998030500405 19980305 00405 NM 1998 3 5 P5CA9800289 1 19980217 A 5320 SILL BOEING 747 747128 1384894 NM SERVICE DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 U/D R/H/S CREW SERVICE DOOR LOWER DOOR SILL AREA FWD CORNER REVEAL FOUND CRACKED. FWD CORNER REVEAL REPLACED PER SRM 51 -10-10 P 18. 2 L 7 4 4F A20WE 1998030500406 19980305 00406 NM 1998 3 5 P5CA9800290 1 19980217 A 5753 SKIN BOEING 747 747128 1384894 NM RT TE FLAP DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT /W INBD T/E FLAP AFT FLAP FOUND DENT MARK AT MID SECTION BOTTOM NR 5 AND NR 6 FLAP TRACK. FIBERGLASS REPAIRED PER SR M 51-40-15. 2 L 7 4 4F A20WE 1998030500407 19980305 00407 NM 1998 3 5 P5CA9800291 1 19980218 A 5730 PANEL BOEING 747 747128 1384894 NM WS 890-917 CHIPPED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING L/E UPPER FIXED PNL WS 890-917 T/E FABRIC PATCH FOUND CHIPPED AND GLASS REPAIRED AS PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500408 19980305 00408 NM 1998 3 5 P5CA9800292 1 19980214 A 5522 SKIN BOEING 747 747128 1384894 NM RT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DELAMINATION OF FIVE AREAS ON UPPER SURFACE OF THE RIGHT INBOARD ELEVATOR. FIBERGLASS REPAIR MADE PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500409 19980305 00409 NM 1998 3 5 P5CA9800293 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON UPPER SURFACE OF LOWER WING SKIN IN LEADING EDGE CAVITY FORWARD OF FRONT SPAR. CORROSION REMOVED AND AREA TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500410 19980305 00410 NM 1998 3 5 P5CA9800294 1 19980214 A 5512 SKIN BOEING 747 747128 1384894 NM HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 CORROSION INSIDE CENTER SECTION OF THE HORIZONTAL STABILIZER BETWEEN STRINGERS 54 AND 55, STAB RIGHT BODY LINE 15 TO 43. 5. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500411 19980305 00411 NM 1998 3 5 P5CA9800295 1 19980214 A 5312 BULKHEAD BOEING 747 747128 1384894 NM BS 2658 DEFORMED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DEFORMATION AT 6 O'CLOCK POSITION ON APU FIRE BULKHEAD AT STATION 2658. DRESSED OUT DEFORMED AREA PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998030500412 19980305 00412 NM 1998 3 5 P5CA9800296 1 19980214 A 5312 BULKHEAD BOEING 747 747128 1384894 NM BS 140 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 CRACKED ON BODY STATION 140 BULKHEAD AT LBL 38. REPAIRED AREA WEB PER BAC SRM 53-10-06. 2 L 7 4 4F A20WE 1998030500413 19980305 00413 NM 1998 3 5 P5CA9800297 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10- 01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500414 19980305 00414 NM 1998 3 5 P5CA9800298 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM BS 440-586 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON UPPER SKIN OF RIGHT WING REAR SPAR AREA AT WS 440 TO 586. REMOVED CORROSION AND TREATED PER BAC S RM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500415 19980305 00415 NM 1998 3 5 P5CA9800299 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1336 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1336 TO 1485. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500416 19980305 00416 NM 1998 3 5 P5CA9800300 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1240-1270 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1240 TO 1270. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500417 19980305 00417 NM 1998 3 5 P5CA9800301 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1210-1240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1210 TO 1240. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500418 19980305 00418 NM 1998 3 5 P5CA9800302 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1010-1050 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1010 TO 1050. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500419 19980305 00419 NM 1998 3 5 P5CA9800303 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 724-752 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 724 TO 752. REMOVED CORROSION AND TREATED AREA P ER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500420 19980305 00420 NM 1998 3 5 P5CA9800304 1 19980217 A 5720 FAIRING BOEING 747 747128 1384894 NM LT WING SPONGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING NR 2 FIXED FAIRING MARKED AREA FOUND SPONGED. NR 2 FIXED FAIRING FIBERGLASS REPAIRED AS PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500421 19980305 00421 NM 1998 3 5 P5CA9800305 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1105-1115 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON RIGHT WING UPPER SKIN IN THE MID SPAR AREA AT WS 1105 TO 1115. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500422 19980305 00422 NM 1998 3 5 P5CA9800306 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 900-920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN IN THE REFUEL AREA AT WS 900 TO 920. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500423 19980305 00423 NM 1998 3 5 P5CA9800307 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1516-1548 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON RIGHT WING UPPER SKIN FROM WS 1516 TO 1548 FROM MID SPAR TO REAR SPAR. REMOVED CORROSION AND TREA TED AREA PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN SRM 57-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500424 19980305 00424 NM 1998 3 5 P5CA9800308 1 19980217 A 5753 FLAP BOEING 747 747128 1384894 NM RT TE AFT FLAP SPONGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WIN O/B AFT FLAP FOUND ONE LOCATION SPONGED JUST O/B T/E LWR SURFACE. FIBERGLASS REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500425 19980305 00425 NM 1998 3 5 P5CA9800309 1 19980217 A 5280 DOOR BOEING 747 747128 1384894 NM RT MLG STRUT DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING GEAR I/B STRUT DOOR AFT EDGE FOUND DISBONDED. FIBERGLASS REPAIRED PER SRM 51-40-06 PARAGRAPH 2. 2 L 7 4 4F A20WE 1998030500426 19980305 00426 NM 1998 3 5 P5CA9800310 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION OF THE UPPER WING SKIN AT WBL 834 FROM MID SPAR TO REAR SPAR. REMOVED CORROSION AND TREATED PER BAC S RM 51-10-01 AND 51-10-02, REPAIR WITHIN THE LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500427 19980305 00427 NM 1998 3 5 P5CA9800311 1 19980217 A 5320 SIDEWALL BOEING 747 747128 1384894 NM RT MLG WW CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT BODY GEAR W/W O/B SIDEWALL AT BS 1475 APPROX SPLICE PLATE LOWER ATTACH CHORD CORROSION. CORROSION REMOVED AND TREATE D PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500428 19980305 00428 NM 1998 3 5 P5CA9800312 1 19980217 A 5753 SKIN BOEING 747 747128 1384894 NM RT TE FOREFLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING I/B T/E FOREFLAP L/E LOWER SURFACE BETWEEN NR 5 AND NR 6 FLAP TRACKS HAS LIGHT SURFACE CORROSION ON SKIN PANEL. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 AND FILLER REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998030500429 19980305 00429 NM 1998 3 5 P5CA9800313 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 382-420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 382 TO 420. REMOVED CORROSION AND TREATED PER BA C SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS PER SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500430 19980305 00430 NM 1998 3 5 P5CA9800314 1 19980217 A 5753 SKIN BOEING 747 747128 1384894 NM LT TE FOREFLAP DISBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING I/B FOREFLAP I/B PANEL FOUND SKIN DISBONDED AT CORROSION REWORK LOCATION 2 BY 10 INCHES. HOT BOND REPAIRED PER SRM 51-40-06 FIG 17 AND FIG 17A. 2 L 7 4 4F A20WE 1998030500431 19980305 00431 NM 1998 3 5 P5CA9800315 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 807-834 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 807 TO 834. REMOVED CORROSION AND TREATED PER BA C SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS PER SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500432 19980305 00432 NM 1998 3 5 P5CA9800316 1 19980217 A 5412 BULKHEAD BOEING 747 747128 1384894 NM NR 3 ENGINE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND ON NR 3 ENG BULKHEAD TO FIREWALL FWD LT CORNER AREA IN STRUCTURE (FWD ING MOUNT BULKHEAD STRUCT URE). SURFACE CORROSION REMOVED ON FWD BULKHEAD AT FIREWALL FWD LWR LT CORNER PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500433 19980305 00433 NM 1998 3 5 P5CA9800317 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 917-944 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 917 TO 944. REMOVED CORROSION AND TREATED PER B AC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500434 19980305 00434 NM 1998 3 5 P5CA9800318 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1175-1190 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 1175 TO 1190. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500435 19980305 00435 NM 1998 3 5 P5CA9800319 1 19980218 A 7110 TR SLEEVE BOEING 747 747128 1384894 NM NR 1 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 1 ENG FAN T/R TRANSLATING SLEEVE AT 9 O'CLOCK POSITION NEEDS REPAIR INSIDE AND OUTSIDE. FILLER REPAIRS CARRIED OUT P ER SRM 51-40-06 PARA 2B. 2 L 7 4 4F A20WE 1998030500436 19980305 00436 NM 1998 3 5 P5CA9800320 1 19980218 A 5754 FLAP BOEING 747 747128 1384894 NM NR 3 LE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING NR 3 L/E FLAP INBD ACTUATING ARM NOSE AREA L/E NOSE BEAM RIB CHORD FLANGE AT LOWER END FOUND CRACK. NOSE BEAM R IB CHORD REPAIRED PER SRM 57-20-03. 2 L 7 4 4F A20WE 1998030500437 19980305 00437 NM 1998 3 5 P5CA9800321 1 19980217 A 5280 SKIN BOEING 747 747128 1384894 NM LT MLG STRUT DR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING GEAR O/B STRUT DOOR INNER SKIN LOWER EDGE FOUND CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 5 1-10-02. 2 L 7 4 4F A20WE 1998030500438 19980305 00438 NM 1998 3 5 P5CA9800322 1 19980218 A 5400 BRACE BOEING 747 747128 1384894 NM NR 2 PYLON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 2 ENG DIAGONAL BRACE WORN ON AFT END ON LT SIDE. AREA SMOOTHED OUT AND SHOT PEENED. NO CRACKS NOTED PER SRM 51-10-0 2, OHM 20-10-03, NDT PT 6 51-00-00 FIG 4. 2 L 7 4 4F A20WE 1998030500439 19980305 00439 NM 1998 3 5 P5CA9800323 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1224-1252 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 1224 TO 1252. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500440 19980305 00440 NM 1998 3 5 P5CA9800324 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1265-1285 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN REAR SPAR AREA AT WS 1265 TO 1285. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500441 19980305 00441 NM 1998 3 5 P5CA9800325 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1270 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 1270 TO 1290. REMOVED CORROSION AND TREATED PER B AC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500442 19980305 00442 NM 1998 3 5 P5CA9800326 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1392-1482 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1392 TO 1482. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500443 19980305 00443 NM 1998 3 5 P5CA9800327 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1336-1392 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1336 TO 1392. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500444 19980305 00444 NM 1998 3 5 P5CA9800328 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1280-1336 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1280 TO 1336. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500445 19980305 00445 NM 1998 3 5 P5CA9800329 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1485-1548 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1485 TO 1548. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500446 19980305 00446 NM 1998 3 5 P5CA9800330 1 19980217 A 7110 SKIN BOEING 747 747128 1384894 NM NR 3 ENG COWL DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 3 ENG NOSE COWL RT AFT LOWER ACOUSTIC PANEL OUTER SKIN DAMAGED, ACOUSTIC PANEL REPAIRED FIBERGLASS REPAIR PER SRM 51- 30-02. 2 L 7 4 4F A20WE 1998030500447 19980305 00447 NM 1998 3 5 P5CA9800331 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1130-1252 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1130- TO 1252. REMOVED CORROSION AND TREATED PE R BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500448 19980305 00448 NM 1998 3 5 P5CA9800332 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1056-1110 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1056 TO 1110. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500449 19980305 00449 NM 1998 3 5 P5CA9800333 1 19980217 A 5350 FAIRING BOEING 747 747128 1384894 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE BODY FAIRING 193G AND 194G EXTERIOR LAYER FOUND CRACKED AND DELAMINATED. AREA REPAIRED PER SRM 51-24-11. 2 L 7 4 4F A20WE 1998030500450 19980305 00450 NM 1998 3 5 P5CA9800334 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 353-411 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 353 TO 411. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500451 19980305 00451 NM 1998 3 5 P5CA9800335 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 411-469 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 411 TO 469. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500452 19980305 00452 NM 1998 3 5 P5CA9800336 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 469-499 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 469 TO 499. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500453 19980305 00453 NM 1998 3 5 P5CA9800337 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 499-557 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 499 TO 557. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500454 19980305 00454 NM 1998 3 5 P5CA9800338 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1168-1224 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN WBL 834 FROM MID TO REAR SPAR AT WS 1168 TO 1224. REMOVED CORROSION AND T REATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500455 19980305 00455 NM 1998 3 5 P5CA9800339 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1252-1282 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 1252 TO 1282. REMOVED CORROSION AND TREATED PER BA C SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500456 19980305 00456 NM 1998 3 5 P5CA9800340 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1308-1336 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 1308 TO 1336. REMOVED CORROSION AND TREATED PER BA C SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500457 19980305 00457 NM 1998 3 5 P5CA9800341 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1364-1392 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE RIGHT WING UPPER SKIN IN MID SPAR AREA AT WS 1364 TO 1392. REMOVED CORROSION AND TREATED PER B AC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500458 19980305 00458 NM 1998 3 5 P5CA9800342 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1423-1485 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 1423 TO 1485. REMOVED CORROSION AND TREATED PER BA C SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500459 19980305 00459 NM 1998 3 5 P5CA9800343 1 19980218 A 5311 FRAME BOEING 747 747128 1384894 NM BS 720 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 720 FOUND CRACKED AT STR 9R CUTOUT. FRAME REPAIRED AT UD BS 720 STR 9 R PER SRM 53-10-04. 2 L 7 4 4F A20WE 1998030500460 19980305 00460 NM 1998 3 5 P5CA9800344 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1320-1485 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1320 TO 1485. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500461 19980305 00461 NM 1998 3 5 P5CA9800345 1 19980216 A 5330 SKIN BOEING 747 747128 1384894 NM BS 2000-2020 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 BS 2000-2020 STR 33L -34L FUSELAGE SKIN FOUND DENT. AREA SMOOTHED OUT PER SRM 51-01-01, TREATED PER SRM 51-10-02, NO CR ACK EVIDENT. 2 L 7 4 4F A20WE 1998030500462 19980305 00462 NM 1998 3 5 P5CA9800346 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1252-1280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1252 TO 1280. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500463 19980305 00463 NM 1998 3 5 P5CA9800347 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 1224-1252 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN FRONT SPAR AREA AT WS 1224 TO 1252. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500464 19980305 00464 NM 1998 3 5 P5CA9800348 1 19980214 A 5730 SKIN BOEING 747 747128 1384894 NM WS 889-917 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT WING UPPER SKIN IN MID SPAR AREA AT WS 889 TO 917. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02, REPAIR WITHIN LIMITS OF SRM 57-30-01. 2 L 7 4 4F A20WE 1998030500465 19980305 00465 NM 1998 3 5 P5CA9800349 1 19980218 A 5720 FAIRING BOEING 747 747128 1384894 NM RT WING SPONGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING #7 FIXED FAIRING MARKED AREA FOUND SPONGED. FIBERGLASS REPAIR AS PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500466 19980305 00466 NM 1998 3 5 P5CA9800350 1 19980214 A 5350 FAIRING SUPPORT BOEING 747 747128 1384894 NM BS 1175 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON AIR CONDITIONING ACCESS PANEL SUPPORT AT BS 1175 TO 1235, LBL 60. REMOVED CORROSION AND TREATED PE R BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500467 19980305 00467 NM 1998 3 5 P5CA9800351 1 19980218 A 5311 FRAME BOEING 747 747128 1384894 NM BS 620 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 620 STR 7R CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D BS 620 STR 7R PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500468 19980305 00468 NM 1998 3 5 P5CA9800353 1 19980216 A 5311 FRAME BOEING 747 747128 1384894 NM BS 600 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 600 STR 7R AND 8R CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 600 STR 7R AND STR 8R PER SRM 53-1 0-04 FIG 54. 2 L 7 4 4F A20WE 1998030500469 19980305 00469 NM 1998 3 5 P5CA9800354 1 19980217 A 5311 FRAME BOEING 747 747128 1384894 NM BS 640 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 640 8R CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D STA 640 STR 84 SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500470 19980305 00470 NM 1998 3 5 P5CA9800355 1 19980216 A 5311 FRAME BOEING 747 747128 1384894 NM BS 680 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 680 STR 7AR AND 8R CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 680 STR 8R PER SRM 53-10-04 FIG 5 4. 2 L 7 4 4F A20WE 1998030500471 19980305 00471 NM 1998 3 5 P5CA9800356 1 19980218 A 5311 FRAME BOEING 747 747128 1384894 NM BS 640 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 660 STR 7AL CUTOUT AREA FOUND CRACKED. FRAME REPAIRED AT U/D BS 640 STR 7AL PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500472 19980305 00472 NM 1998 3 5 P5CA9800357 1 19980218 A 5311 FRAME BOEING 747 747128 1384894 NM BS 600 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 600 STR 8L CUTOUT AREA FOUND CRACKED. U/D BS 600 FRAME REPAIR AT STR 8L PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500473 19980305 00473 NM 1998 3 5 P5CA9800358 1 19980216 A 5311 FRAME BOEING 747 747128 1384894 NM BS 580 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 580 STR 6AL-7AL CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 580 STR 6AL AND 7AL PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500474 19980305 00474 NM 1998 3 5 P5CA9800359 1 19980216 A 5311 FRAME BOEING 747 747128 1384894 NM BS 540 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 540 STR 7AL CUTOUT AREA FOUND CRACKED. FRAME REPAIR AT U/D BS 540 STR 7AL PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500475 19980305 00475 NM 1998 3 5 P5CA9800360 1 19980218 A 5311 FRAME BOEING 747 747128 1384894 NM BS 540 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 540 FOUND CRACKED AT STR 7R AND 7AR AND 8R CUTOUT AREA. FRAME REPAIR AT U/D BS 540 STR 7R, 7AR AND 8R PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500476 19980305 00476 NM 1998 3 5 P5CA9800361 1 19980218 A 5753 FOREFLAP BOEING 747 747128 1384894 NM LT TE FOREFLAP CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING INBD FORE FLAP I/B TOP SURFACE PANEL FOUND SURFACE CORROSION AT 3 LOCATIONS. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500477 19980305 00477 NM 1998 3 5 P5CA9800362 1 19980218 A 5311 FRAME BOEING 747 747128 1384894 NM BS 720 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 STA 720 FRAME FOUND CRACKED AT STR 9L CUTOUT. FRAME REPAIRED AT U/D BS 720 STR 9L PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500478 19980305 00478 NM 1998 3 5 P5CA9800363 1 19980216 A 5311 FRAME BOEING 747 747128 1384894 NM BS 700 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK STA 700 FRAME FOUND CRACKED AT STR 7AR AND 9R CUTOUT. FRAME REPAIRED AT U/D BS700 STR 7AR AND 9R PER SRM 53- 10-01 FIG 54. 2 L 7 4 4F A20WE 1998030500479 19980305 00479 NM 1998 3 5 P5CA9800364 1 19980216 A 5311 FRAME BOEING 747 747128 1384894 NM BS 720 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK STA 720 FRAME FOUND CRACKED AT STR 8R CUTOUT. FRAME REPAIRED AT U/D BS 720 STR 8R PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998030500480 19980305 00480 NM 1998 3 5 P5CA9800365 1 19980213 A 5320 65B105469 ANGLE BOEING 747 747128 1384894 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON FUSELAGE ACCESS DOOR 191AL FORWARD HINGE ATTACH ANGLE. REPLACED ATTACH ANGLE PER BAC MM 20-51-01. 2 L 7 4 4F A20WE 1998030500481 19980305 00481 NM 1998 3 5 P5CA9800366 1 19980216 A 5280 DOOR BOEING 747 747128 1384894 NM RT MLG STRUT DISBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING GEAR STRUT DOOR AFT EDGE FOUND DEBONDED. HOT BOND REPAIR PER SRM 51-40-06 FIG 17A. 2 L 7 4 4F A20WE 1998030500482 19980305 00482 NM 1998 3 5 P5CA9800367 1 19980213 A 5320 ANGLE BOEING 747 747128 1384894 NM BS 920 - 950 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON BODY FAIRING LONGITUDINAL SUPPORT ANGLES AT BS 920 TO 950, LBL 5 TO RBL 5. REPLACED SUPPORT ANGLES PER BAC SRM 51-10-01. 2 L 7 4 4F A20WE 1998030500483 19980305 00483 NM 1998 3 5 P5CA9800368 1 19980218 A 5240 DOOR BOEING 747 747128 1384894 NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DOOR 315AL AFT AREA AT RIB FOUND DENTED 12 INCHES LONG. DOOR 315 AL DRESSED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998030500484 19980305 00484 NM 1998 3 5 P5CA9800369 1 19980215 A 5330 SKIN BOEING 747 747128 1384894 NM RT MLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON UPPER SURFACE SKIN IN THE RIGHT BODY GEAR WHEEL WELL OUT BOARD OF GEAR RETRACT ACTUATOR FITTING. R EMOVED CORROSION AND TREATED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500485 19980305 00485 NM 1998 3 5 P5CA9800370 1 19980215 A 5320 SPLICE BOEING 747 747128 1384894 NM RT MLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON SPLICE PLATE OF OUTBOARD SIDEWALL IN RIGHT BODY GEAR WHEEL WELL AT S1475, WL 150. REMOVED CORROSIO N AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500486 19980305 00486 NM 1998 3 5 P5CA9800371 1 19980213 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 880 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON BODY FAIRING SUPPORT AT S 880, BL 0 TO RBL 12. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500487 19980305 00487 NM 1998 3 5 P5CA9800372 1 19980213 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1215 - 1235 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON FUSELAGE ACCESS PANEL 191KL UPPER SUPPORT CHANNEL AT S 1215 TO BS 1235. REMOVED CORROSION AND TREA TED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500488 19980305 00488 NM 1998 3 5 P5CA9800373 1 19980213 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1175 - 1235 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON FUSELAGE AIR CONDITIONING BAY ACCESS PANEL SUPPORT AT BS 1175 TO BS 1235. REMOVED CORROSION AND T REATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500489 19980305 00489 NM 1998 3 5 P5CA9800374 1 19980218 A 5312 BULKHEAD BOEING 747 747128 1384894 NM BS 140 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE BS140 B/H FWD FACE FOUND CRACKED AT RBL 38 2 PLACES. WEB REPAIRED AS PER SRM 53-10-04 FIG 89. 2 L 7 4 4F A20WE 1998030500490 19980305 00490 NM 1998 3 5 P5CA9800375 1 19980213 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1235 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON FUSELAGE AIR CONDITIONING BAY ACCESS PANEL SUPPORT AT BS 1235, LBL 100 TO RBL 60. REMOVED CORROSIO N AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500491 19980305 00491 NM 1998 3 5 P5CA9800376 1 19980213 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1350 - 1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL SUPPORT AT BS 1350 TO BS 1480. REMOVED CORROSION AND TREATED PER BAC SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500492 19980305 00492 NM 1998 3 5 P5CA9800377 1 19980215 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1350 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON UPPER SURFACE PANEL IN RIGHT WING GEAR WHEEL WELL AT BS 1350, RBL 15 TO 90. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500493 19980305 00493 NM 1998 3 5 P5CA9800378 1 19980218 A 5311 FRAME BOEING 747 747128 1384894 NM BS 680 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER DECK FRAME 680 STR 7AL CUTOUT AREA FOUND CRACKED. DENT SMOOTHED OUT AND TREATED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500494 19980305 00494 NM 1998 3 5 P5CA9800379 1 19980218 A 5753 SKIN BOEING 747 747128 1384894 NM RT TE MIDFLAP DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING O/B MID FLAP I/B TOP ACCESS PANEL NR 687LT FOUND LOWER MID AREA SKIN CORROSION AND DELAMINATED. HOT BOND REPAIR S PER SRM 51-40-06 FIG 17. 2 L 7 4 4F A20WE 1998030500495 19980305 00495 NM 1998 3 5 P5CA9800380 1 19980218 A 5320 BEAM BOEING 747 747128 1384894 NM BS 1260 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND AT RT WING W/W O/B UPPER LONGITUDINAL BEAM WEB UPPER SURFACE AT STA 1260 WL 180. CORROSION REMO VED AND TREATED PER SRM 51-10-01, 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-30-01. 2 L 7 4 4F A20WE 1998030500496 19980305 00496 NM 1998 3 5 P5CA9800381 1 19980219 A 5330 SKIN BOEING 747 747128 1384894 NM RT MLG WW CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING GEAR W/W CEILING SKIN AT STA 1320 O/B FOUND CORROSION. REMOVED AND TREATED AS PER SRM 51-10-01, 51-10-02. BLEN DED OUT WITHIN SRM LIMIT 53-30-01. 2 L 7 4 4F A20WE 1998030500497 19980305 00497 NM 1998 3 5 P5CA9800382 1 19980215 A 5330 SKIN BOEING 747 747128 1384894 NM RT MLG WW CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION IN RIGHT BODY GEAR OUTBOARD WHEEL WELL INTERIOR SKIN. REMOVED CORROSION AND TREATED AS PER BAC SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500498 19980305 00498 NM 1998 3 5 P5CA9800383 1 19980219 A 5320 WEB BOEING 747 747128 1384894 NM BS 1341-1349 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION LT WING GEAR W/W STA 1341-1349 UPPER BEAM WEB UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51 -10-01, 51-10-02 BLENDED OUT WITHIN SRM LIMITS 53-30-01. 2 L 7 4 4F A20WE 1998030500499 19980305 00499 NM 1998 3 5 P5CA9800384 1 19980215 A 5320 SPLICE BOEING 747 747128 1384894 NM BS 1372 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON SPLICE PLATE IN RIGHT BODY GEAR WHEEL WELL AT BS 1372, WL 150. REMOVED CORROSION AND TREATED PER B AC SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998030500500 19980305 00500 NM 1998 3 5 P5CA9800385 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM RT MLG WW CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING W/W FWD RT CENTER TANK JETTISON PUMP BONDING JUMPER ATTACH POINT FOUND SKIN CORROSION. CORROSION REMOVED AND TR EATED PER SRM 51-10-01, 51-10-02 BLENDED OUT PER SRM 57-10-01. 2 L 7 4 4F A20WE 1998030500501 19980305 00501 NM 1998 3 5 P5CA9800386 1 19980219 A 5320 SPLICE BOEING 747 747128 1384894 NM BS 1438 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND AT LT BODY GEAR O/B SPLICE CHORD AT STA 1438. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 5 1-10-02. BLENDED OUT WITHIN SRM LIMIT 53-10-01. 2 L 7 4 4F A20WE 1998030500502 19980305 00502 NM 1998 3 5 P5CA9800387 1 19980219 A 5314 KEEL BEAM BOEING 747 747128 1384894 NM LT MLG WW CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION AT LT BODY GEAR WHEEL WELL KEEL BEAM UPPER SURFACE. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AN D 51-10-02. BLENDED OUT WITHIN SRM LIMITS 53-30-01. 2 L 7 4 4F A20WE 1998030500503 19980305 00503 NM 1998 3 5 P5CA9800388 1 19980219 A 5280 DOOR BOEING 747 747128 1384894 NM LT MLG STRUT CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT BODY GEAR STRUT DOOR INNER SKIN FOUND SURFACE CORROSION. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02 . BLENDED OUT WITHIN SRM LIMIT 52-00-02. 2 L 7 4 4F A20WE 1998030500504 19980305 00504 NM 1998 3 5 P5CA9800389 1 19980219 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1346 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING GEAR BEAM FWD SIDE WING FAIRING SUPPORT AFT FACE FOUND CORROSION AT STA 1346 WBL 148. CORROSION REMOVED AND TRE ATED PER SRM 51-10-01 AND 51-10-02 BLENDED OUT WITHIN SRM LIMITS PER 53-10-01. 2 L 7 4 4F A20WE 1998030500505 19980305 00505 NM 1998 3 5 P5CA9800390 1 19980219 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1350-1380 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT BODY GEAR W/W STAT 1350-1380 LOWER FIXED PANEL FOUND CORROSION AT SKIN AND ANGLES. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLENDED OUT WITHIN SRM LIMIT 53-10-01. 2 L 7 4 4F A20WE 1998030500506 19980305 00506 NM 1998 3 5 P5CA9800391 1 19980219 A 5522 PANEL BOEING 747 747128 1384894 NM HORIZ STAB DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT HORIZ STAB LOWER T/E FIXED PANEL 334GBL FOUND DELAMINATION. HOT BOND REPAIRED PER SRM 51-40-06 PARA 3. 2 L 7 4 4F A20WE 1998030500507 19980305 00507 NM 1998 3 5 P5CA9800393 1 19980219 A 5730 SKIN BOEING 747 747128 1384894 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING LOWER SKIN NR 4 MAIN TANK AFT BOOST PUMP HOUSING CUTOUT FOUND HEAVY CORROSION. CORROSION REMOVED BLEND OUT NOT WITHIN SRM LIMIT 57-30-03. REPAIRED PER PAO HKG 98-0068TE AND 0070RE AND SRM 57-30-03 FIG 3. 2 L 7 4 4F A20WE 1998030500508 19980305 00508 NM 1998 3 5 P5CA9800394 1 19980219 A 5320 BONDING JUMPER BOEING 747 747128 1384894 NM NR 2 TANK CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING REAR SPAR WEB HEAVY CORROSION AT ATTACHMENT OF BONDING JUMPER OF NR 2 TANK I/B JETTISON PUMP AREA. REMOVED CORR OSION PER SRM 51-10-01 BLEND OUT NOT WITHIN LIMIT 57-10-01. REPAIRED PER BOEING PAO-HKG-98-0073RE-INSTALL FILLERS DOUBL ERS AND TREAT AREA. 2 L 7 4 4F A20WE 1998030500509 19980305 00509 NM 1998 3 5 P5CA9800395 1 19980129 A 5350 FAIRING BOEING 747 747128 1384894 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE BODY FAIRING 1920 FOUND PUNCTURE HOLE AND DELAMINATION. BODY FAIRING FIBERGLASS REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500510 19980305 00510 NM 1998 3 5 P5CA9800396 1 19980218 A 5320 SPLICE BOEING 747 747128 1384894 NM BS 1350 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 BS 1350 R/H/S OVERWING LONGERON SPLICE FITTING FOUND CRACKED. LONGERON SPLICE FITTING REPLACED IAW SRM 51-01-01. 2 L 7 4 4F A20WE 1998030500511 19980305 00511 NM 1998 3 5 P5CA9800397 1 19980218 A 5313 STRINGER BOEING 747 747128 1384894 NM BS 884 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND AT RT STA 884 STR 44R. CORRSOION REMOVED PER SRM 51-10-01 BLEND OUT NOT WITHIN SRM LIMIT 53-10- 03. STRINGER REPAIRED PER SRM 53-10-03 FIG 1 AND TREATED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1998030500512 19980305 00512 NM 1998 3 5 P5CA9800398 1 19980219 A 5320 ANGLE BOEING 747 747128 1384894 NM BS 1370-1400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE UPPER BODY FAIRING NR 294FR LOWER SUPPORT ANGLE BETWEEN BS 1370-1400 FOUND CORROSION AROUND FLOAT NUTS. CORROS ION REMOVED PER SRM 51-01-01, BLEND OUT NOT WITHIN SRM LIMITS 53-10-01. REPAIRED PER SRM 51-40-04 FIG 3 AND TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1998030500513 19980305 00513 NM 1998 3 5 P5CA9800399 1 19980218 A 5320 SUPPORT BOEING 747 747128 1384894 NM BS 1540 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE BODY FAIRING SUPPORT FOUND SLIGHT CORROSION AT BS 1540 LBL 60 - RBL 40. CORROSION REMOVED PER SRM 51-01-01. B LEND OUT NOT WITHING SRM LIMITS 53-10-01 FIG 1, BODY FAIRING SUPPORT REPAIRED PER SRM 53-50-01 AND TREATED PER SRM 51-10 -02. 2 L 7 4 4F A20WE 1998030500514 19980305 00514 NM 1998 3 5 P5CA9800400 1 19980218 A 5313 STRINGER BOEING 747 747128 1384894 NM BS 1670-1682 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND AFT CARGO COMPARTMENT BS 1670-1682 ST 44R. STRINGER REPAIRED IAW RS R-53-11-33645. 2 L 7 4 4F A20WE 1998030500515 19980305 00515 NM 1998 3 5 P5CA9800401 1 19980215 A 5320 SPLICE BOEING 747 747128 1384894 NM BS 1438 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE SPLICE PLATE IN THE RIGHT BODY GEAR WHEEL WELL AT BS 1438, WL 150. CORROSION REMOVED AND TREAT ED PER SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998030500516 19980305 00516 NM 1998 3 5 P5CA9800402 1 19980218 A 5320 STIFFENER BOEING 747 747128 1384894 NM BS 1050 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND FUSELAGE BS 1050 RBL 10 KEEL BEAM O/B FACE ATTACH VERTICAL STIFFENER. CORROSION REMOVED AND TR EATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT WITHIN SRM LIMITS 53-10-01. 2 L 7 4 4F A20WE 1998030500517 19980305 00517 NM 1998 3 5 P5CA9800403 1 19980212 A 5330 SKIN BOEING 747 747128 1384894 NM BS 840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON FUSELAGE SKIN AT BS 840, LBL 4 TO RBL 4. CORROSION REMOVED AND TREATED PER SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998030500518 19980305 00518 NM 1998 3 5 P5CA9800404 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1736 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND BS 1736 STR 46R-49R FUSELAGE SKIN. CORROSION REMOVED PER SRM 51-10-01 AND TREATED PER SRM 51-1 0-02. BLEND OUT WITHIN SRM LIMIT 53-30-01. 2 L 7 4 4F A20WE 1998030500519 19980305 00519 NM 1998 3 5 P5CA9800405 1 19980210 A 5330 ACCESS PANEL BOEING 747 747128 1384894 NM KEEL BEAM CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON KEEL BEAM ACCESS PANEL191GG. CORROSION REMOVED AND TREATED PER BAC SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998030500520 19980305 00520 NM 1998 3 5 P5CA9800406 1 19980218 A 5320 CHORD BOEING 747 747128 1384894 NM BS 2598 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE BS 2598 B/H ATTACH CHORD FOUND CRACKED AT RT STR 11R - STR 12R RIVET HOLES. BULKHEAD CHORD REPAIRED PER SRM 51 -40-04. 2 L 7 4 4F A20WE 1998030500521 19980305 00521 NM 1998 3 5 P5CA9800407 1 19980218 A 5320 ANGLE BOEING 747 747128 1384894 NM BS 2598 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 APU BATTERY COMPARTMENT BS 2598 STR 22-STR 23, LT SIDE FITTING FRAME CHORD ATTACH ANGLE FOUND CRACKED. ANGLE REPLACED P ER SRM 51-10-01. 2 L 7 4 4F A20WE 1998030500522 19980305 00522 NM 1998 3 5 P5CA9800408 1 19980213 A 5246 SKIN BOEING 747 747128 1384894 NM LAV SERVICE DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON MID LAVATORY SERVICE DOOR CUTOUT SKIN. CORROSION REMOVED AND TREATED PER BAC SRM 51-10-01, 51-10-0 2. 2 L 7 4 4F A20WE 1998030500523 19980305 00523 NM 1998 3 5 P5CA9800409 1 19980213 A 5245 ACCESS PANEL BOEING 747 747128 1384894 NM BS 1160 - 1175 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON AIR CONDITIONING BAY ACCESS PANEL AT BS 1160 TO 1175, LBL 60. CORROSION REMOVED AND TREATED PER BA C SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998030500524 19980305 00524 NM 1998 3 5 P5CA9800410 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 500 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE SKIN DEEP LIGHTNING STRIKE MARK REVEALED AT STA 500 STR 36L. SKIN REPAIRED PER SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 1998030500525 19980305 00525 NM 1998 3 5 P5CA9800411 1 19980213 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1235 - 1255 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DENT ON ON FUSELAGE SKIN FORWARD OF ACCESS PANEL 192NR FROM BS 1235 TO 1255. CORROSION REMOVED AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500526 19980305 00526 NM 1998 3 5 P5CA9800412 1 19980218 A 2760 CABLE COVER BOEING 747 747128 1384894 NM BS 1250 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 MAIN DECK LT STA 1250 SIDEWALL UPPER CONTROL CABLE PULLEY METAL COVER FOUND MOUNTING BRACKET CRACK AND DEFORMED. MOUNTI NG BRACKET REPLACED AS PER SRM 51-10-01 AND SPEED BRAKE CABLE RIGGING CHECKED PER MM 27-62-02. 2 L 7 4 4F A20WE 1998030500527 19980305 00527 NM 1998 3 5 P5CA9800413 1 19980213 A 5320 ANGLES BOEING 747 747128 1384894 NM BS 880 - 910 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON FUSELAGE BODY FAIRING LONGITUDINAL SUPPORT ANGLES AT BS 880 TO 910, LBL 5 TO RBL 5. REMOVED CORROS ION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500528 19980305 00528 NM 1998 3 5 P5CA9800414 1 19980218 A 5250 ANGLE BOEING 747 747128 1384894 NM ACCESS DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE ACCESS DOOR 192M MID AND AFT HINGE LOWER HALF ATTACH ANGLE FOUND CORROSION. ANGLE REPLACED PER MM 20-50-01. 2 L 7 4 4F A20WE 1998030500529 19980305 00529 NM 1998 3 5 P5CA9800415 1 19980218 A 5250 ANGLE BOEING 747 747128 1384894 NM FUSELAGE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 FUSELAGE ACCESS DOOR PANEL NR 192ER MID HINGE LOWER HALF ATTACH ANGLE FOUND CORROSION. ATTACH ANGLE REPLACED AS PER MM 20-50-01. 2 L 7 4 4F A20WE 1998030500530 19980305 00530 NM 1998 3 5 P5CA9800416 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM NR 3 FUEL TANK CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT WING NR 3 MAIN FUEL TANK JETTISON PUMP CUTOUT AREA OF REAR SPAR BONDING ATTACH POINT CORROSION. CORROSION REMOVED AN D TREATED PER SRM 51-01-01, 51-10-02. BLEND OUT WITHIN SRM LIMIT 57-10-01. 2 L 7 4 4F A20WE 1998030500531 19980305 00531 NM 1998 3 5 P5CA9800417 1 19980218 A 5511 SPAR BOEING 747 747128 1384894 NM HORIZ STAB CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION, FOUND INSIDE HORIZONTAL STAB REAR SPAR UPPER CHORD AND SKIN AREA AT RBL 43.5. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. BLEND OUT PER SRM LIMIT 55-10-01. 2 L 7 4 4F A20WE 1998030500532 19980305 00532 1998 3 5 P5CA9800418 4 19980218 A 2360 STATIC WICK BOEING 747 747128 1384894 NM RUDDER CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 UPPER RUDDER STATIC DISCHARGER 2ND AND 3RD FROM TOP FOUND WITH CORROSION ON ATTACH STRIP. STATIC CHARGE BASE 2ND AND 3R D REPLACED PER SRM 51-01-01. 2 L 7 4 4F A20WE 1998030500533 19980305 00533 NM 1998 3 5 P5CA9800419 1 19980218 A 5510 STABILIZER BOEING 747 747128 1384894 NM RT HORIZ STAB CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 RT HORIZONTAL STABILIZER SLOT SEAL CRACKED AT FWD LOWER AREA. FIBERGLASS REPAIR CARRIED OUT PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500534 19980305 00534 NM 1998 3 5 P5CA9800420 1 19980218 A 7110 COWL BOEING 747 747128 1384894 NM NR 3 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 3 ENGINE INLET COWL LT SIDE PANEL AFT DELAMINATED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998030500535 19980305 00535 NM 1998 3 5 P5CA9800421 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 942 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND AT RT STA 942 STR 44R. CORROSION REMOVED AND TREATES PER SRM 51-10-01, 51-10-02. BLEND OUT NOT WITHIN SRM LIMIT 53-10-01. REPAIRED PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 1998030500536 19980305 00536 NM 1998 3 5 P5CA9800422 1 19980218 A 7110 SUPPORT BOEING 747 747128 1384894 NM NR 4 NOSE COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 4 ENG NOSE COWL ANTI-ICE DUCT SUPPORT CRACKED AT STA 180. WELDING CARRIED OUT PER BAC 5975. 2 L 7 4 4F A20WE 1998030500537 19980305 00537 NM 1998 3 5 P5CA9800423 1 19980218 A 5330 SKIN BOEING 747 747128 1384894 NM BS 880 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION AT BS 880-900 ST 38L. CORROSION REMOVED AND TREATED PER SRM 51-01-01, 51-10-02. BLEND OUT NOT WITHIN LIMITS PER SRM 53-110-01. STRINGER REPAIRED PER SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 1998030500538 19980305 00538 NM 1998 3 5 P5CA9800424 1 19980218 A 5753 FAIRING BOEING 747 747128 1384894 NM LT WING SPONGY A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LT WING I/B T/E FLAP INBD NR 4 CANOE FAIRING SEVEAL AREAS SPONGY DISBONDING AND PUNCHED HOLE FOUND. FIBERGLASS REPAIR P ER SRM 51-40-14. 2 L 7 4 4F A20WE 1998030500539 19980305 00539 NM 1998 3 5 P5CA9800425 1 19980218 A 5320 FITTING BOEING 747 747128 1384894 NM BS 1350 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION FOUND FUSELAGE RT OVERWING LONGERON SPLICE FITTING AT BS 1350, TAPER FILLER. TAPER FILLER REPLACED PE R SRM 51-10-01. 2 L 7 4 4F A20WE 1998030500540 19980305 00540 NM 1998 3 5 P5CA9800426 1 19980218 A 7110 COWL BOEING 747 747128 1384894 NM NR 1 ENGINE DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 NR 1 ENG NOSE COWL AT THE 5 O'CLOCK POSITION DELAMINATION. NR 1 ENG NOSE COWL ACCOUSTIC PANEL REPAIRED AS PER SRM 54-30 -03 FIG 7 AND SRM 54-30-03 FIG 29A. 2 L 7 4 4F A20WE 1998030500541 19980305 00541 NM 1998 3 5 P5CA9800427 1 19980213 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1460 - 1480 DEFORMED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DEFORMATION IN FUSELAGE SKIN AT BS 1460 TO 1480, S32L TO S34L. DAMAGED AREA SMOOTHED AND TREATED PER BAC SRM 51-10-01 A ND 51-10-02. REPAIR WITHIN SRM 53-30-01 LIMITS. 2 L 7 4 4F A20WE 1998030500542 19980305 00542 NM 1998 3 5 P5CA9800428 1 19980213 A 5330 SKIN BOEING 747 747128 1384894 NM BS 1730 - 1740 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DENT ON FUSELAGE SKIN AT FROM BS 1730 TO 1740, S38R TO 39R. SMOOTHED OUT DAMAGED AREA AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. REPAIR WITHIN LIMITS OF SRM 53-30-01. 2 L 7 4 4F A20WE 1998030500543 19980305 00543 NM 1998 3 5 P5CA9800429 1 19980215 A 5754 PANEL BOEING 747 747128 1384894 NM NR 13 LE FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON NUMBER 13 LEADING EDGE FLAP INBOARD CORNER INTERNAL PANEL. REMOVED CORROSION AND TREATED PER BAC S RM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500544 19980305 00544 NM 1998 3 5 P5CA9800430 1 19980212 A 5754 SKIN BOEING 747 747128 1384894 NM NR 11 FLAP DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DENT ON NUMBER 11 LEADING EDGE FLAP BULL NOSE SKIN. REPAIRED PER BAC SRM 51-40-01 AND TREATED PER SRM 51-10-02. 2 L 7 4 4F A20WE 1998030500545 19980305 00545 NM 1998 3 5 P5CA9800431 1 19980213 A 5753 SKIN BOEING 747 747128 1384894 NM LT TE FLAP DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DEBONDED AREA ON LEFT INBOARD TRAILING EDGE FORE FLAP SKIN. REPAIRED PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1998030500546 19980305 00546 NM 1998 3 5 P5CA9800432 1 19980212 A 5520 WEB BOEING 747 747128 1384894 NM LT ELEVATOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON LEFT OUTBOARD ELEVATOR OUTBOARD WEB. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10- 02. 2 L 7 4 4F A20WE 1998030500547 19980305 00547 NM 1998 3 5 P5CA9800433 1 19980212 A 5522 SKIN BOEING 747 747128 1384894 NM LT ELEVATOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON THE LEFT OUTBOARD ELEVATOR UPPER SURFACE. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 5 1-10-02. 2 L 7 4 4F A20WE 1998030500548 19980305 00548 NM 1998 3 5 P5CA9800434 1 19980215 A 5533 BRACKET BOEING 747 747128 1384894 NM VENTRAL FIN CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON TWO L SHAPED BRACKETS ON THE HORIZONAL STABILIZER VENTRAL FIN TRAILING EDGE. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500549 19980305 00549 NM 1998 3 5 P5CA9800435 1 19980215 A 5753 SKIN BOEING 747 747128 1384894 NM LT TE FOREFLAP DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 DEBONDED AREA ON UPPER SKIN OF INBOARD FOREFLAP INBOARD TRAILING EDGE. MADE FIBERGLASS REPAIR PER BAC SRM 51-40-14. 2 L 7 4 4F A20WE 1998030500550 19980305 00550 NM 1998 3 5 P5CA9800436 1 19980215 A 3213 STRUT BOEING 747 747128 1384894 NM LT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEVEL 1 CORROSION ON LEFT WING GEAR SHOCK STRUT INNER CYLINDER LOWER PORTION. REMOVED CORROSION AND TREATED PER BAC SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998030500551 19980305 00551 WP 1998 3 5 RRXA98022 1 19980225 A 5230 VENT DOOR DOUG DC8 DC873F 302199F WP CARGO DOOR OUT OF ADJUST A RRXA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 WP 15 795FT 46103 AT FL29000 MAIN CARGO VENT DOOR LIGHT ILLUMINATED. CABIN LOST PRESSURE AND EMERGENCY DESCENT WAS INITIATED. ADJ DOOR L IMIT SWITCH, CAM LATCH ROD ASSY AND OPS CHECK VENT DOOR IAW MM 52-30-00, DC 8 VENT DOOR MANUAL. INSPECTED ALL FITTINGS AND ATTACHMENTS, NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1998030500552 19980305 00552 NM 1998 3 5 VNAA9802022 1 19980225 A 4950 GTCP36150DD APU BLEED SYST DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN SMOKING A VNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 07 429JS 67299 11109 3043 DURING THE CLIMB-OUT AFTER TAKEOFF, THE CREW NOTICED SMOKE IN THE CABIN. THE CREW LEVELED OFF AND DECLARED AN EMERGENCY . THE SMOKE DISSIPATED AFTER THE AIRCONDITIONING WAS SELECTED OFF. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHO UT FURTHER INCIDENT. MAINTENANCE INSPECTED AND OPERATION CHECKED THE AIR CONDITIONING SYSTEMS, IN ACCORDANCE WITH DORNI ER MAINTENANCE MANUAL 36-10-00. MAINTENANCE DETERMINED THAT THE SMOKE WAS CAUSED BY THE AUXILIARY POWER PLANT BLEED. MAI NTENANCE DEFERRED THE AUXILIARY POWER PLANT IAW THE MEL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998030500553 19980305 00553 WP 1998 3 5 VJ9800027 1 19980210 A 5730 1A270601 SKIN DOUG DC9 DC932 3022066 WP WS 540 CRACKED A VJ6A K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 918VV 47320 AS A RESULT OF GROUND DAMAGE SUSTAINED TO THE LT O/B SECTION OF THE WING, A 1.25 INCH HOLE WAS PUNCTURED IN L/E SKIN ASS Y PANEL AT WING STA XRS540. HOLE CUT OUT, FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIRS IAW AEROCORP EO 98-792, R EV 1R, DATED 02/10/98. APPROVED BY FAA FORM 8110-3 BY DER NR SO-822 DATED 02/11/98. PART NUMBERS AFFECTED WERE 1A-2706 0-1, 1A-27061-1, 1A-27062-1, AND 1A-31402-1. LT WING STA XRS 540 AND XRS 480. 2 L 7 2 4F A6WE 1998030500554 19980305 00554 WP 1998 3 5 VJ9800028 1 19980228 A 3350 41B004AD073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 919VV 47260 FORWARD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY IAW MM 33-60. 2 L 7 2 4F A6WE 1998030500555 19980305 00555 NM 1998 3 5 CALA9800342 1 19980228 A 3234 GEAR HANDLE BOEING 737 7373T0 1384582 NM COCKPIT LACK OF LUBE A CALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 09 14324 23375 WHEN GEAR WAS EXTENDED ON APPROACH, THE CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS. RECEIVED TOO LO W GEAR WARNING BELOW 1000 FEET. THE GEAR WAS CYCLED DURING A GO-AROUND AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT L ANDED WITHOUT INCIDENT. MAINTENANCE ALL THREE GEAR AND FOUND NO DEFECTS. THE GEAR HANDLE WAS INSPECTED AND MAINTENANCE FOUND SLIDE TO BE STICKING. THE GEAR HANDLE SLIDE WAS CLEANED AND LUBRICATED. A SIMULATED GEAR RETRACTION WAS PERFORM ED AND NO DEFECTS WERE NOTED. 2 L 7 2 4F RT A16WE 1998030500556 19980305 00556 1998 3 5 CALA9800343 4 19980228 A 2565 5WD230500203 SLIDE DOUG DC10 DC1030 3023501 WP L-3 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND THE L-3 DOOR EMERGENCY SLIDE PACK PRESSURE LOW. THE L-3 DOOR EMERGENCY SLIDE WAS REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1998030500557 19980305 00557 1998 3 5 CALA9800344 4 19980228 A 2565 5WD230100201 SLIDE DOUG DC10 DC1030 3023501 WP L-1 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68065 46590 INSPECTION FOUND THE L-1 DOOR EMERGENCY SLIDE PACK PRESSURE LOW. THE L-1 DOOR EMERGENCY SLIDE WAS REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1998030500558 19980305 00558 NM 1998 3 5 CALA9800345 1 19980301 A 3230 161N50015 UPLOCK ACTUATOR BOEING 757 757224 1384958 NM LT MLG INOPERATIVE A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 14120 2980 27562 THE GEAR WARNING LIGHT AND GEAR DISAGREE EICAS MESSAGE WERE RECEIVED AFTER GEAR RETRACTION. THE GEAR HANDLE WAS MOVED T O THE OFF POSITION AND ALL WARNINGS WERE CLEARED. THE AIRCRAFT LANDED AT SEA WITHOUT INCIDENT. THE GEAR UPLOCK SYSTEM WAS INSPECTED WITH NO DEFECTS FOUND. NO MECHANICAL DEFECTS WERE NOTED. THE AIRCRAFT WAS FERRIED TO LAX. THE LT MLG UP LOCK RELEASE ACTUATOR WAS REMOVED AND REPLACED WHILE AT LAX. IN ADDITION, THE NR 1 ENGINE DRIVEN PUMP WAS REMOVED AND R EPLACED AS A PRECAUTIONARY MEASURE. SEVERAL GEAR SWINGS WERE PERFORMED WITH NO FAULTS NOTED. 2 L 7 2 4F RT A2NM 1998030500559 19980305 00559 NM 1998 3 5 CALA9800346 1 19980226 A 5753 SKIN BOEING 757 757224 1384958 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12116 27558 INSPECTION FOUND A 5.75 INCH CRACK IN RT WING OUTBOARD MIDFLAP OUTBOARD END AT BOTTOM SKIN. A .75 INCH CRACK WAS FOUND IN LT WING OUTBOARD MIDFLAP OUTBOARD END AT BOTTOM SKIN. REPAIRS WERE INSTALLED IAW ECRA 5750-02810. 2 L 7 2 4F RT A2NM 1998030500560 19980305 00560 WP 1998 3 5 CALA9800347 1 19980226 A 5730 SKIN DOUG DC9 DC981 3022081 WP WS 286 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 INSPECTION FOUND A 2.5 INCH CRACK ON RT WING LEADING EDGE SKIN AT FORWARD WS XOS 286 AND FORWARD OF ACCESS PANEL CUTOUT. AN INTERNAL AND EXTERNAL DOUBLER REPAIR WAS INSTALLED IAW ECRA 5720-01638. A DIP WAS ISSUED TO REPLACE SCREWS AND BLI ND RIVETS AT NEXT 1/4D CHECK OR 2500 FLIGHT HOURS. 2 L 7 2 4F A6WE 1998030500561 19980305 00561 WP 1998 3 5 CALA9800348 1 19980227 A 5720 DOUBLER DOUG DC10 DC1030 3023501 WP WS 827 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND A 1 INCH CRACK IN LT LOWER LEADING EDGE STRINGER DOUBLER AT STA XORS 827. REPAIRED IAW SRM 57-10-00, F IGURE 49. 2 L 7 3 4F A22WE 1998030500562 19980305 00562 WP 1998 3 5 CALA9800349 1 19980227 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 826 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 INSPECTION FOUND A 2.5 INCH CRACK IN FITTING AT STA 826, LONGERON 19L. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51- 30-2. 2 L 7 2 4F A6WE 1998030500563 19980305 00563 WP 1998 3 5 CALA9800350 1 19980228 A 5712 RIB DOUG DC10 DC1010 3022110 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 10 INCH CRACK IN RIB OF RT WING LOWER LEADING EDGE JUST OUTBOARD OF SLAT DRIVE MECHANISM. THE RIB WA S REMOVED AND A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-90-00. 2 L 7 3 4F A22WE 1998030500564 19980305 00564 WP 1998 3 5 CALA9800351 1 19980228 A 5720 BOLT DOUG DC10 DC1010 3022110 WP RT WING BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND BOLT BROKEN AT REAR SPAR LOWER SIDE ON REAR SPAR TO FUEL TANK ON RT WING OUTBOARD SUPPORT INBOARD AILER ON. THE RT ASSEMBLY STUDS WERE REMOVED AND REPLACED AND LEAK AND OPERATIONAL CHECKS WERE GOOD IAW MM 57-41-01. 2 L 7 3 4F A22WE 1998030500565 19980305 00565 WP 1998 3 5 CALA9800352 1 19980228 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 601 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND FLOORBEAM CORRODED INSIDE OF FORWARD BAGGAGE BIN BELOW RIGHT PALLET GUIDE RAIL AND BEAM WEB HAD A 3 INC H CRACK AT STA 601, LONGERON 43R. THE CORRODED SECTIONS OF BEAM WERE REMOVED, REPAIR SECTIONS WERE FABRICATED AND INSTA LLED IAW ECRA 5310-03668. 2 L 7 3 4F A22WE 1998030500566 19980305 00566 WP 1998 3 5 CALA9800353 1 19980228 A 5320 FITTING DOUG DC10 DC1010 3022110 WP BS 595 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND TENSION TIE FITTING CORRODED AT STA 595, LONGERON 48L. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51 -31-01. 2 L 7 3 4F A22WE 1998030500567 19980305 00567 WP 1998 3 5 CALA9800354 1 19980228 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1810 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON FUSELAGE SKIN AT STA 1810, LONGERON 45-47L. THE CORRODED AREA WAS REMOVED, STRAP AND FING ER DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-00, 51-21-01, 51-10-00, AND ECRA 5310-03680. 2 L 7 3 4F A22WE 1998030500568 19980305 00568 WP 1998 3 5 CALA9800355 1 19980228 A 5400 STIFFENER DOUG DC10 DC1010 3022110 WP NR 3 PYLON GALLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND VERTICAL STIFFENERS AT LEFT AND RIGHT SIDE OF NR 3 PYLON HAD ELONGATED HOLES AND WERE GALLED AT PAN SUP PORT RIB. THE STIFFENERS WERE REMOVED IAW SRM 51-10-1. NEW STIFFENERS WERE FABRICATED AND INSTALLED IAW SRM 51-10-00, 51-21-01, AND 51-10-1. 2 L 7 3 4F A22WE 1998030500569 19980305 00569 WP 1998 3 5 CALA9800356 1 19980228 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1361 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND UPPER SURFACE OF WING CENTER SECTION SKIN CORRODED FORWARD OF PRESSURE PANEL AT STA 1361, RBL 43 TO 85. REPAIRED IAW SRM 51-21-01. 2 L 7 3 4F A22WE 1998030500570 19980305 00570 WP 1998 3 5 CALA9800357 1 19980301 A 5751 SKIN DOUG DC10 DC1010 3022110 WP RT AILERON CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT WING INBOARD AILERON UPPER SKIN DELAMINATED AND CORRODED. THE AILERON WAS REMOVED, REPAIRED AND REI NSTALLED IAW MM 27-10-01. 2 L 7 3 4F A22WE 1998030500571 19980305 00571 WP 1998 3 5 CALA9800358 1 19980228 A 5754 VANE DOUG DC10 DC1010 3022110 WP LT LE FLAP DISBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LT WING INBOARD FLAP VANE DISBONDED ON UPPER SURFACE. THE FLAP VANE WAS REMOVED, REPAIRED, AND REINSTA LLED IAW MM 57-54-00. 2 L 7 3 4F A22WE 1998030500572 19980305 00572 WP 1998 3 5 CALA9800359 1 19980301 A 5754 VANE DOUG DC10 DC1010 3022110 WP RT LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD FLAP VANE AT STA XW 280. THE FLAP VANE WAS REMOVED, REPAIRED AND REI NSTALLED IAW MM 27-50-01. 2 L 7 3 4F A22WE 1998030500573 19980305 00573 WP 1998 3 5 9803369941 1 19980223 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 575 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CRACK IN LONGERON 30 END FITTING AT FS 575. REPLACED FITTING PER DWG 5911412 AND SRM 51-30-5. 2 L 7 2 4F A6WE 1998030500574 19980305 00574 WP 1998 3 5 9803379944 1 19980228 A 5610 WINDSHIELD DOUG DC9 DC931 3022065 WP LT COCKPIT CRACKED A NWAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 01 1309T 47316 DURING TAKEOFF, CAPTAIN'S WINDSHIELD CRACKED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD AND TEMPERATURE CONTROL. OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998030500575 19980305 00575 WP 1998 3 5 9803389916 1 19980226 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 949N 47566 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRING IN WIRE BUNDLE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500576 19980305 00576 NM 1998 3 5 9803396740 1 19980225 A 7711 EPR INDICATION BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 640US 23888 662539 DURING TAKEOFF ROLL, THE NR 1 ENGINE WOULD NOT REACH TAKEOFF EPR WITHOUT EXCEEDING THE EGT REDLINE. THE MAXIMUM EPR REA CHED WAS 1.30. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEANED THE EPR TRANSMITTER AND INDICATOR CONNECTIONS AND PERFORMED AN ENGINE BLEED CHECK PER MM 75-32-00 WITH NO DEFECTS NOTED. THE AIRCRAFT RETUR NED TO SERVICE. EXACT PART CAUSING DIFFICULTY TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998030500577 19980305 00577 NE 1998 3 5 9803401154 2 19980224 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 GL 01 154US 46763 686165 AT TOP OF DESCENT FL330, THE NR 3 ENGINE COMPRESSOR STALLED. ENGINE ANTI-ICE AND FUEL HEAT WERE ON. THE EGT REACHED 87 0C BEFORE THE ENGINE WAS SHUT DOWN. THE ENGINE RESTARTED NORMALLY AND OPERATED WITHOUT FURTHER DIFFICULTY FOR THE REMAI NDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER MM 71-00-00, PG 105 WITH NO DEFECTS NOTED. EXACT PART CAUSING DIFFICULTY TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998030500579 19980305 00579 WP 1998 3 5 9803429604 1 19980227 A 2810 VENT VALVE DOUG DC9 DC932 3022066 WP RIGHT STUCK A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 604NW 47222 RIGHT FUEL QUANTITY INDICATOR DROPPED IN EXCESS OF NORMAL FUEL BURN AFTER TAKEOFF. FLIGHT WAS RETURNED TO OKC AND LANDE D WITHOUT INCIDENT. MAINTENANCE VERIFIED STICK READINGS WITH FUEL QUANTITY INDICATORS. NO DISCREPANCIES WERE NOTED. I T IS SUSPECTED THAT THE RIGHT FUEL CLIMB VENT VALVE WAS STUCK OPEN DURING CLIMB. AIRCRAFT WAS REFUELED TO PROPER LEVELS AND RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998030500580 19980305 00580 1998 3 5 COMA9810049 4 19980302 A 6113 7847841 SPINNER BULKHEAD 7801008 EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE RT PROP CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 1145 1145 890806 1238 890806 DURING PREFLIGHT INSPECTION, THE RIGHT PROPELLER SPINNER BULKHEAD WAS FOUND TO BE CRACKED APPROXIMATELY 1.5 INCH ALONG T HE BULKHEAD OUTER WALL BEHIND BLADE NR 2. AIRCRAFT WAS FERRIED BACK TO CVG HANGAR AND BULKHEAD REMOVED FOR REPAIR. DAM AGE APPEARS TO BE DUE TO MATERIAL DEFECT, NO EXTERNAL DAMAGE WAS FOUND. 2 L 7 2 4T RT A31SO 6 C P11NE 1998030500581 19980305 00581 SO 1998 3 5 COMA9810050 1 19980226 A 3246 3006041 WHEEL 314461 EMB 120 EMB120RT SO MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 130G 16403 5 1625 120130 MECHANIC REMOVED WHEEL ASSEMBLY FROM A/C DUE TO TIRE WAS FOUND FLAT. WHEEL SHOP INFLATED TIRE AND FOUND INBOARD HALF CR ACKED AT BOTTOM OF KEY INSERT BOSS. WHEEL HALF (P/N 300-604-1) HAS BEEN REMOVED FROM SERVICE. 2 L 7 2 4T RT A31SO 1998030500582 19980305 00582 SO 1998 3 5 COMA9810051 1 19980227 A 3350 3071BPE LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 137H 120137 ONE LAMP INOP AT FORWARD EMERGENCY FLOOR PATH LIGHTING. REPLACED LAMP. 2 L 7 2 4T RT A31SO 1998030500583 19980305 00583 SO 1998 3 5 COMA9810052 1 19980223 A 2841 944101 FUEL TOTALIZER EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT MALFUNCTION A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 264CA 19972 3000 120256 FUEL TOTALIZER AND FUEL QUANTITY DISAGREE. REPLACED TOTALIZER. 2 L 7 2 4T 4 T RT A31SO E20NE 1998030500584 19980305 00584 EA 1998 3 5 COMA9860049 1 19980301 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 946CA 3797 2477 7072 FLAPS FAILED AT 8 DEGREES. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1998030500585 19980305 00585 NM 1998 3 5 98FDEA00141 1 19980227 A 2742 AJH7337507 ACTUATOR DOUG MD11 MD11F 3023600 NM LT HORIZ STAB JAMMED A FDEA A J UNSCHED LANDING DUMP FUEL F FLT CONT AFFECTED TO TAKEOFF 1 SO 25 612FE 48605 ON T/O AT FLAPS UP TRIM JAM AT 7.2 DEG NOSE UP. BOTH PICKLE SWITCH AND MANUAL TRIM SUITE CASE HANDLES, BUT NO MOVEMENT. CKD CIRCUIT BREAK AND RAN STAB INOP (2.5-12) NO HELP. TRIED BOTH AUTOPILOT, NO HELP. DUMP 110,000 LBS OF FUEL AND RE TURN TO KANSAI. ON FINAL TRIED ELEV FEEL SWITCH BUT DIDN'T HELP LAND WITH 28 DEG FLAPS MED BRAKE LAND WAS NORMAL (458,0 00 LBS). ON BLOCK IN POST FLT CREW COULD SEE NOTHING VISUALLY WRONG WITH STAB FND LT HORIZ STAB ACTUATOR ASSY AS FAULTY AND FUSE PIN WAS SHEARED ON STAB CHAIN DRIVE ASSY. REMOVED AND REPLACED LEFT HAND ACTUATOR ASSY PER EA 1-2740-29542 AN D REMOVED AND REPLACED DRIVE UNIT PER M/M 27-44-06-4. HORIZ STAB OPS NORM PER M/M 27-340-00-5. FCC 1 AND 2 AFS STAB R- 2 L 7 3 4F RT A22WE 1998030500586 19980305 00586 WP 1998 3 5 98FDEA00142 1 19980301 A 3260 PROX SENSOR DOUG DC10 DC1030F 3023504 WP LT MLG DAMAGED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 302FE 46801 BOTH FRONT AND BACK LEFT MAIN GEAR INDICATOR UNSAFE LIGHTS ILLUMINATED AFTER TAKEOFF. FOLLOWED RED TAB. FRONT LIGHT EX TINGUISED, BACK LIGHT REMAINED ILLUM UNTIL LEVEL OFF. PRIOR TO LANDING BOTH FRONT AND BACK LIGHT MAIN GEAR UNSAFE LIGHT S ILLUM, UNTIL LANDING GEAR WAS LOWERED. ALL GEAR LTS IN GREEN UPON LANDING. FOUND LEFT MAIN GEAR DOOR PROX SWITCH (SE NSOR) BADLY SCRATCHED. REMOVED AND REPLACED AND ADJUSTED SWITCH PER M/M 32-61-03. PERFORMED PROX BOX TEST, FOUND OK. 2 L 7 3 4F RT A22WE 1998030500587 19980305 00587 NM 1998 3 5 98FDEA00143 1 19980228 A 5313 652353522 STRINGER BOEING 727 72727C 138400J NM BS 540-740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 145FE 19109 NR 0776 036 CORROSION (C53-224-02) ON STRINGER 3 RT AT BS 540-740. REMOVED AND REPLACED STRINGER 3 RT FROM BS 520-620 A ND FROM BS 650-740 IAW FED-EX SRM 53-10-03. 2 L 7 3 4F A3WE 1998030500588 19980305 00588 WP 1998 3 5 ABXA9800126 1 19980225 A 5320 99105019 CUSP WEB DOUG DOUG DC9 DC931 3022065 WP BS 408 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND RIGHT CUSP WEB AT STATION 408 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998030500589 19980305 00589 WP 1998 3 5 ABXA9800127 1 19980225 A 5312 39164181 BULKHEAD ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND THE SLANT PANEL ANGLE STATION 690 AND LBL 8 CORRODED. REPAIRED ANGLE IAW ABX REA D953-22465-MR. 2 L 7 2 4F A6WE 1998030500590 19980305 00590 WP 1998 3 5 ABXA9800128 1 19980225 A 5313 591140911 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 237. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998030500591 19980305 00591 WP 1998 3 5 ABXA9800129 1 19980225 A 5320 991224316 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT LONGERON 17R AND STATION 965. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998030500592 19980305 00592 WP 1998 3 5 ABXA9800130 1 19980225 A 5313 59114279 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998030500593 19980305 00593 WP 1998 3 5 ABXA9800131 1 19980225 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED CRACKED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998030500594 19980305 00594 WP 1998 3 5 ABXA9800132 1 19980225 A 5313 59364369 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND LONGERON 13R CRACKED AT STATION 965. REPAIRED FRAME IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998030500595 19980305 00595 WP 1998 3 5 ABXA9800133 1 19980225 A 5311 995823859 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING C-CHECK, FOUND FRAME CRACKED AT LONGERON 17R AND STATION 980. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998030500596 19980305 00596 WP 1998 3 5 ABXA9800134 1 19980225 A 7830 5958782503 LINK DOUG DOUG DC9 DC932 3022066 WP NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE LOWER RIGHT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-5. 2 L 7 2 4F A6WE 1998030500597 19980305 00597 WP 1998 3 5 ABXA9800135 1 19980225 A 7830 5958782503 LINK DOUG DOUG DC9 DC932 3022066 WP NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING COMPLIANCE WITH AD 96-10-11, FOUND NR 2 ENGINE UPPER LEFT THRUST REVERSER DRIVER LINK CRACKED. REPLACED THRUST R EVERSER DRIVER LINK IAW DC9 MM 78-31-5. 2 L 7 2 4F A6WE 1998030500598 19980305 00598 WP 1998 3 5 MWEA98233 1 19980227 A 5320 9915510507 FITTING DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 KEEL BEAM FITTING AT FS 699 WAS FOUND CRACKED. REMOVED AND REPLACED CRACKED FITTING. 2 L 7 2 4F A6WE 1998030500599 19980305 00599 WP 1998 3 5 MWEA98234 1 19980227 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE NUMBER 6 SLAT TRACK RIB ON THE RIGHT WING WAS FOUND TO BE GOUGED. THE DAMAGED RIB WAS REMOVED AND A NEW ONE FABRICA TED AND INSTALLED. 2 L 7 2 4F A6WE 1998030500600 19980305 00600 WP 1998 3 5 MWEA98235 1 19980227 A 5720 99193701 DOUBLER DOUG DC9 DC932 3022066 WP WS 360.5 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 A PREVIOUSLY BLENDED AREA WAS FOUND ON THE FUEL TANK LOWER ACCESS PLATE MATING SURFACE DOUBLER AT XRS 360.5. REPAIR DOU BLER WAS FABRICATED AND INSTALLED. 2 L 7 2 4F A6WE 1998030500601 19980305 00601 WP 1998 3 5 MWEA98236 1 19980227 A 5320 9910078 WEB DOUG DC9 DC932 3022066 WP BS 190 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 SUBFLOOR WEB AT STA 190 LBL 50 WAS FOUND CORRODED MATERIAL LOSS 10090. REMOVED AND REPLACED SUBFLOOR FROM FS 160 TO 200 . 2 L 7 2 4F A6WE 1998030500602 19980305 00602 WP 1998 3 5 MWEA98237 1 19980227 A 5320 9910078 WEB DOUG DC9 DC932 3022066 WP BS 120-160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE SUBFLOOR WEB WAS FOUND CORRODED BETWEEN STATION 120 TO 160 LBL 8 TO RBL 148. REMOVED AND REPLACED DAMAGED WEB. 2 L 7 2 4F A6WE 1998030500603 19980305 00603 WP 1998 3 5 MWEA98238 1 19980227 A 5320 9910078 WEB DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE SUBFLOOR WEB IN THE FWD GALLEY AREA FROM FS 160 TO 200. REMOVED AND REPLACED DAMAGED FLOOR WEB. 2 L 7 2 4F A6WE 1998030500604 19980305 00604 WP 1998 3 5 MWEA98239 1 19980227 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 237 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE FLOORBEAM AT FS 237 LBL 45 TO 55 HAS AN IMPROPER REPAIR. REMOVED AND REPLACED REPAIR IAW SRM. 2 L 7 2 4F A6WE 1998030500605 19980305 00605 WP 1998 3 5 MWEA98240 1 19980227 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 218-237 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE SUBFLOOR WEB AT FS 218 TO FS 237 WAS FOUND CORRODED. REMOVED AND REPLACED DAMAGED SUBFLOOR WEB. 2 L 7 2 4F A6WE 1998030500606 19980305 00606 WP 1998 3 5 MWEA98242 1 19980227 A 5311 9511841 FRAME DOUG DC9 DC932 3022066 WP BS 1089 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE STATION 1089 CANTED FRAME FOUND WITH A CORRODED WEB AT LONGERON 12L. BLENDED CORROSION OUT OF LIMITS, FABRICATED RE PAIR FILLER AND DOUBLER, INSTALLED REPAIR. 2 L 7 2 4F A6WE 1998030500607 19980305 00607 WP 1998 3 5 MWEA98243 1 19980227 A 5312 9911841 BULKHEAD DOUBLER DOUG DC9 DC932 3022066 WP BS 1089 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 DOUBLER ON CANTED BULKHEAD 1089 LONGERON 11R WAS FOUND CORRODED. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 1998030500608 19980305 00608 WP 1998 3 5 MWEA98244 1 19980227 A 5312 2777922 BLKHD STIFFENER DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE 1121 CANTED BULKHEAD STIFFENER AT LONGERON 12L WAS FOUND EXFOLIATED. REMOVED AND REPLACED STIFFENER. 2 L 7 2 4F A6WE 1998030500609 19980305 00609 WP 1998 3 5 MWEA98245 1 19980227 A 5312 9911839 BLKHD STIFFENER DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE 1121 CANTED BULKHEAD LONGERON 14L STIFFENER WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER. 2 L 7 2 4F A6WE 1998030500610 19980305 00610 WP 1998 3 5 MWEA98246 1 19980227 A 5312 2777922 BLKHD STIFFENER DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE 1121 CANTED BULKHEAD LONGERON 13L STIFFENER WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER. 2 L 7 2 4F A6WE 1998030500611 19980305 00611 WP 1998 3 5 MWEA98247 1 19980227 A 5312 2777922 BLKHD STIFFENER DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE LONGERON 10R STIFFENER ON THE AFT SIDE OF THE STA 1121 CANTED FRAME WAS FOUND CORRODED. REMOVED AND REPLACED STIFFE NER. 2 L 7 2 4F A6WE 1998030500612 19980305 00612 WP 1998 3 5 MWEA98248 1 19980227 A 5312 2777922 BLKHD STIFFENER DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE STIFFENER ON LONGERON 14R CANTED BULKHEAD 1121 WAS FOUND CORRODED. REMOVED AND REPLACED STIFFENER. 2 L 7 2 4F A6WE 1998030500617 19980305 00617 EA 1998 3 5 98ZZZX909 2 19980124 A 8520 LW10842 CRANKSHAFT PIPER PA60 PA60601P 7106012 NM LYC O540 IO540S1A5 41532 EA NR 2 JOURNAL FAILED A A MSTA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NE 05 TGWOW 882 8 92152 61P068379633 L195974819 PILOT (OWNER) DEPARTING FROM AIRPORT AND CLIMBING THROUGH 4,000 FEET NOTED LOUD BANG AND SEVERE VIBRATION FROM LT ENGINE . ENGINE SHUT DOWN AND SECURED AND SAFE LANDING MADE. DISASSEMBLY OF ENGINE REVEALED CRANKSHAFT BROKEN. BREAK OCCURRE D AT THE REAR CHEEK OF THE NR 2 ROD JOURNAL IN THE RADII. CRANKCASE, RODS, CAMSHAFT, AND CYLINDERS ALL NOW N.G. 1 M 7 2 3O 3 O RT A17WE 1E4 1998030500643 19980305 00643 EU 1998 3 5 SIMA980341 1 19980203 A 5610 NP1588014 WINDSHIELD PPG AEROSP ATR72 ATR72212 EU RT COCKPIT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 538AT 95254H4809 538 ORD - FLT 4041 - VERY STRONG ELEC SMOKE ODOR IN-FLIGHT. REMOVED AND REPLACED RT WINDSHIELD, FOUND BURN SPOTS ON WINDSHI ELD. NO OTHER DEFECTS NOTED. PERFORMED OPERATIONAL CHECK SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998030500644 19980305 00644 NM 1998 3 5 ASAA9840008 1 19980115 A 5610 WINDOW BOEING 737 737490 1384715 NM LT COCKPIT LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 791AS 28886 LAX - FLT 418 - PRIOR TO FLIGHT, THE CAPTAIN'S SLIDING WINDOW WAS FOUND DIFFICULT TO OPEN AND LATCH. REMOVED DEBRIS FRO M TRACK AND LUBRICATED. WINDOW OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1998030500645 19980305 00645 SW 1998 3 5 98ZZZX935 1 19980116 A 2910 27810321057 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP NLG CRACKED A A MEJA O OTHER J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 17 788C AC340B BTV/ALB - AFTER TAKEOFF, NOSE WHEEL LANDING GEAR WOULD NOT STAY UP AND LOCKED. BOTH THE LEFT AND RIGHT HYDRAULIC PRESSU RE FAIL LIGHTS ILLUMINATED AND THE AIRCRAFT LOST ALMOST ALL HYDRAULIC PRESSURE. THE AIRCRAFT RETURNED TO BTV AND LANDED WITH AN EMERGENCY GEAR EXTENSION, NO FLAPS, AND NO NOSE WHEEL STEERING. MAINTENANCE FOUND A CRACK IN THE NLG LINE AT F USELAGE FEED-THROUGH AND REPLACED THE LINE. MAINTENANCE THEN REMOVED AND REPLACED THE UPLOCK SPRINGS WITH NEW SPRINGS. A GEAR SWING AND LEAK CHECK C/W AND NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 1998030500646 19980305 00646 SW 1998 3 5 98ZZZX936 1 19980115 A 2910 2781032075 HYDRAULIC LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP BS 69.35 FAILED A A MEJA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 17 788C AC430B ALB/ROC - EN ROUTE, LEFT AND RIGHT HYDRAULIC PRESSURE LIGHTS ILLUMINATED AND HYDRAULIC PRESSURE DROPPED ALMOST TO ZERO. CREW LANDED AT ROC WITH AN EMERGENCY GEAR EXTENSION, NO FLAP, AND NO NOSE WHEEL STEERING. LANDING UNEVENTFUL, NO EM ERGENCY DECLARED, AND AIR TRAFFIC CONTROL WAS NOT NOTIFIED. ACFT ISSUED A SPECIAL FLIGHT PERMIT AND A ONE-TIME FERRY FLT FROM ROC/BTV. MAINT AT BTV DISCOVERED THE NLG UP-LINE HAD A HOLE AT 90 DEGREE BEND AT STA 69.35 AND LINE WAS REPLAC ED. PRESS WAS INSUFFICIENT ON BOTH HYD PUMPS AND BOTH UNITS REPLACED WITH O/H UNITS. MAINT C/W A PUMP CAVITATION INSP, SERVICED HYD SYS, AND PERFORMED A GEAR SWING. NO DEFECTS NOTED ON LEAK CHECK OR OPS CHECK ACFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 1998030500647 19980305 00647 CE 1998 3 5 C2XA98CL004 1 19980107 A 3610 313823E4M0020 TUBE BEECH 1900 1900D 1154162 CE LT WING BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 87557 UE246 CLE - FLT 3006 - CREW REPORTED THE RIGHT HAND BLEED AIR FAIL LIGHT ILLUMINATED IN-FLIGHT. AIRCRAFT RETURNED TO FIELD WI THOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REPAIRED A BROKEN EVA TUBE IAW B1900D MM 26-11-00. OPE RATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1998030500648 19980305 00648 CE 1998 3 5 98ZZZX937 1 19980121 A 5753 SKIN BEECH 1900 1900D 1154162 CE RT TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 228YV 5544 UE179 UE228 ICT - OVERNIGHT MAINTENANCE FOUND 3 SMALL CRACKS ON THE BOTTOM SIDE OF THE RT OUTBOARD FLAP 3 INCHES FROM INBOARD END. R EPAIRED CRACK IAW AMWA TO 1900-00-0001. 2 L 7 2 4T RT A24CE 1998030500649 19980305 00649 CE 1998 3 5 MASA98010 1 19980115 A 5210 10151407611 HANDLE 1294000321 BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR LACK OF LUBE A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 219YV UE219 MTJ/DEN - IN DEN PILOT REPORTED THE PASSENGER DOOR WAS STIFF AND HARD TO OPEN. DEN MAINTENANCE LUBRICATED THE DOOR HAND LE. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998030500650 19980305 00650 EA 1998 3 5 VTZA98027 1 19980123 A 5610 601R330339 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A VTZA B EMER. DESCENT O OTHER CR CRUISE 1 EA 27 624BR 7211 IAD/BNA - FLT 6702 - DURING CRUISE ON 1-23-98 AT 1402 HOURS, EXPERIENCED A SHATTERING OF THE CAPTAIN'S WINDSCREEN. AIRC RAFT DECLARED AN EMERGENCY AND LANDED AT BNA WITH NO FURTHER PROBLEMS. MAINTENANCE CONTROL NOTIFIED AND DISPATCHED, REM OVED AND REPLACED CAPTAIN'S WINDSCREEN. ALL REQUIRED CHECKS ACCOMPLISHED AND AIRCRAFT WAS RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1998030500651 19980305 00651 NE 1998 3 5 UIEA9802 2 19980210 A 7200 ENGINE BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NR 3 FAILED A A UIEA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 EA 15 518MC 50143 23476 528411 ATB - FLT C1315 - ANC/TPE - NR 3 ENGINE FAILURE (FLAMEOUT) DURING CRUISE, FL 290, .84M..ENGINE VIBRATION NORMAL. ACCOMP LISHED ENGINE FAILURE SHUTDOWN CHECKLIST. AFTER CHECKLIST, N1 = 26.8, N2 = 0, F/F = 100, OIL PRESSURE = 0. FUEL DUMPED AND RETURNED TO ANC. DURING T/S, FOUND NR 3 ENGINE N2 INDICATION JUMP FROM ZERO TO 50 PERCENT AND LOUD CLUNKING SOUND HEARD COMING FROM THE CORE OF THE ENGINE. B-SUMP SCAVENGER INLET SCREEN HAS SEVERAL LARGE PIECES OF METAL. OTHER INLET SCREENS AND MAIN OIL SCREEN HAVE METALLIC PARTICLES. ENG REPLACED, S/N ON 517506. ENGINE OPERATION SATISFACTORY. (X) 2 L 7 4 4F 4 F A20WE E23EA 1998030500652 19980305 00652 NM 1998 3 5 TWAA9802204 1 19980212 A 2530 8201110000 OVEN BOEING 757 7572Q8 1384972 NM GALLEY DIRTY A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 701TW 28160 JFK - FLT 31 - THREE GALLEY OVENS EMITTED SMOKE WHEN DOOR OPENED AFTER USE. POSITIONS WERE A GALLEY NR 1 AND NR 2 OVENS , AND B-GALLEY NR 2 OVEN. BELIEVED CAUSED BY CLEANING SOLVENTS. REPLACED THE A-GALLEY NR 1 AND NR 2 OVENS, DEACTIVATED AND DEFERRED THE B-GALLEY NR 2 OVEN. CHECK-C 2-3-98 LAX. (X) 2 L 7 2 4F RT A2NM 1998030500671 19980305 00671 SW 1998 3 5 HEEA0013068 1 19980225 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 383 33006 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998030500672 19980305 00672 SW 1998 3 5 HEEA0013069 1 19980225 A 6220 412010182101 BEARING BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 570 33010 BEARING INNER RACE SHOULDER WORN ON ONE SIDE DUE TO LOST TORQUE OF NUT P/N MS14145L5 WHICH WAS CAUSED BY THE LACK OF THR EADS ON THIS NUT OR WASHER P/N AN960-516 NOT CONTACTING THE PITCH HORN FULLY AS NOTED IN ASB 412-98-92. PART ALREADY SE NT. 1 G 7 2 4U H4SW 1998030500673 19980305 00673 SW 1998 3 5 HEEA0013070 1 19980225 A 6220 412010182101 BEARING BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 864 33010 BEARING INNER RACE SHOULDER WORN ON ONE SIDE DUE TO LOST TORQUE OF NUT P/N MS14145L5 WHICH WAS CAUSED BY THE LACK OF THR EADS ON THIS NUT OR WASHER P/N AN960-516 NOT CONTACTING THE PITCH HORN FULLY AS NOTED IN ASB 412-98-92. PART ALREADY SE NT. 1 G 7 2 4U H4SW 1998030500674 19980305 00674 1998 3 5 HEEA0013071 4 19980225 A 3457 0845000000 GPS SKYNAV5000 BELL 206 206L3 1182108 SW COCKPIT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4180F 51469 MESSAGE SWITCH DAMAGED. SENT TO MAGELLAN SYSTEMS FOR INSPECTION AND REPAIR. 1 G 7 1 3U H2SW 1998030500675 19980305 00675 SW 1998 3 5 HEEA0013106 1 19980226 A 6710 206001057003 BEARING BELL 206 206L1 1182107 SW MIXING LEVER MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 BEARING TURN DOWN AREA WHERE THREADS END IS NOT TURNED DOWN TO FIT BELLCRANK ASSY. BUSHING HOLE ALSO DOESN'T HAVE PROPE R CHAFFED AREA. 1 G 7 1 3U H2SW 1998030500676 19980305 00676 WP 1998 3 5 VJ9800029 1 19980225 A 3210 FITTING DOUG DC9 DC932 3022066 WP LT MLG ELONGATED A VJ6A O OTHER O OTHER IN INSP/MAINT 1 SO 11 937VV 45774 OUTBOARD LOWER MAIN BOLT HOLE ELONGATED ON LEFT HAND MAIN LANDING GEAR, FOUND DURING COMPLIANCE INSPECTION OF AD 96-01-0 5 PER EO 12-5740-29-B1049 INSPECTION REQUIREMENT. REWORKED OUTBOARD LOWER MAIN LANDING GEAR FITTING IAW EO 12-5740-29-C 1397 AND AERCORP EO 98-799. 2 L 7 2 4F A6WE 1998030500677 19980305 00677 NM 1998 3 5 VJ9800030 1 19980202 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 987.5 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 464AT 21278 FLOORBEAM CAP HAS IG CORROSION AT FS 987.5, LBL18 TO RBL 45, WL 208 IN MAIN CABIN FLOOR AREA. REMOVED FLOORBEAM UPPER C AP AND REPLACED WITH NEW CAP ANGLE AT LBL 45 TO RBL 45 IAW 737 SRM 53-10-9 AND BOEING REPAIR SKPEMR 980219. 2 L 7 2 4F RT A16WE 1998030500678 19980305 00678 NM 1998 3 5 VJ980031 1 19980202 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 1016 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 464AT 21278 IG CORROSION ON FLOORBEAM CAP AND WEB FS 1016, LB 48, MAIN CABIN FLOOR AREA. REMOVED DAMAGED AREA AND INSTALLED REPAIR IAW 737 SRM 51-30-2 AND BOEING FAX PEM-DHN 98-0007TR. 2 L 7 2 4F RT A16WE 1998030500679 19980305 00679 1998 3 5 MALA976014 4 19980301 A 3425 6226190113 AHRS SAAB SF340 340B 7860101 EU LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 592MA 340B199 DURING FLIGHT, THE LEFT HEADING COMPAROTOR CAME ON DURING FLIGHT, COULDN'T RESET. AIRCRAFT RETURNED TO DTW. MAINTENANC E REPLACED THE NR 1 AHRS. SYSTEM TESTS IAW SF340 MM34. 2 L 7 2 4T RT A52EU 1998030500680 19980305 00680 EU 1998 3 5 MALA976015 1 19980226 A 7712 5066T52G05 SENSOR SAAB SF340 340B 7860101 EU LT ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 421XJ 421 AFTER TAKEOFF, THE LEFT ENGINE TEMP STARTED TO FLUCTUATE, FOLLOWED BY THE ENGINE RPM AND TORQUE; LEFT IGNITION LIGHT ALS O ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT NP SPEED SENSOR AND NO1 TORQUE SENSOR, ALL CHEC KS GOOD. 2 L 7 2 4T RT A52EU 1998030500681 19980305 00681 EU 1998 3 5 MALA976016 1 19980228 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 89XJ 089 DURING INSPECTION, AFT CABIN EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998030500682 19980305 00682 NM 1998 3 5 MALA976017 1 19980226 A 3350 0L3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 828MA 333 DURING INSPECTION, EMERGENCY EXIT IDENTIFIERS INOP AT ROW 4. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998030500683 19980305 00683 NM 1998 3 5 MALA976018 1 19980226 A 3350 ELE101262 SIGN DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 829MA 335 DURING INSPECTION, EXIT SIGN AT SEAT 4A IS BROKEN. MAINTENANCE REPLACED EXIT SIGN, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998030500684 19980305 00684 EU 1998 3 5 MALA976019 1 19980226 A 3350 CONNECTOR SAAB SF340 SF340A 7850100 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 107XJ 340A107 DURING INSPECTION, EMERGENCY FLOOR TRACK 9C/D INOP. MAINTENANCE RESECURED LOOSE CONNECTOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998030500685 19980305 00685 EU 1998 3 5 MALA976020 1 19980226 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING INSPECTION, 3 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998030500686 19980305 00686 EU 1998 3 5 MALA976021 1 19980228 A 3260 UPLOCK SENSOR SAAB SF340 340B 7860101 EU NLG ICED UP A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 420XJ 420 AFTER CLIMB GEAR DISAGREEMENT LIGHT IN GEAR HANDLE ILLUMINATED. FOLLOWED QRH AND DIVERTED TO MSP. MAINTENANCE FOUND EX CESSIVE ICE ACCUMULATED ON NOSE GEAR UPLOCK SENSOR. REMOVED ICE, COMPLETED SEVERAL GEAR SWINGS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998030500687 19980305 00687 NE 1998 3 5 MALA976022 2 19980228 A 7510 6068T56P01 BLEED VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 418XJ 418 DURING FLIGHT, THE LEFT ENGINE AIR VALVE CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE ANTI-ICE START BLEED VALVE, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998030500688 19980305 00688 EU 1998 3 5 MALA976023 1 19980227 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, 2A OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998030500689 19980305 00689 EU 1998 3 5 MALA976024 1 19980227 A 3350 LIGHT SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING INSPECTION, EMERGENCY LIGHT ON THE F/A PANEL INOP. MAINTENANCE RELAMPED SWITCH LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998030500690 19980305 00690 EU 1998 3 5 MALA976025 1 19980228 A 3350 7239410802 LIGHT SAAB SF340 SF340A 7850100 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 991XJ 091 DURING INSPECTION, TWO OVERHEAD EMERGENCY LIGHTS AND ONE FLOOR TRACK EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED OVERHEA D LIGHTS (PN 1317) AND FLOOR TRACK LIGHT. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998030500691 19980305 00691 NE 1998 3 5 MALA976026 2 19980302 A 7510 6068T56P01 ANTI-ICE VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE INTERNAL FAULT A MALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 15 430XJ 430 DURING DESCENT, THE RIGHT AIR VALVE LIGHT ILLUMINATED, UNABLE TO RESET. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT ANTI-ICE START BLEED VALVE, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998030500692 19980305 00692 EU 1998 3 5 MALA976027 1 19980302 A 3350 3071BPEGPL BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 107XJ 340A107 DURING INSPECTION, 6A EMERGENCY EXIT SIGN INOP. MAINTENANCE RELAMPED EXIT SIGN, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998030500693 19980305 00693 NM 1998 3 5 K3HA980019 1 19980226 A 3350 37067 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 VENTRAL STAIR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERYS (P/N 37067-001) (S/N MC-13) AND TIGHTENED LOOSE WIRE, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998030500694 19980305 00694 NM 1998 3 5 K3HA980020 1 19980227 A 3350 37067001 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 AFT VENTRAL AIRSTAIR EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED VENTRAL AIRSTAIR EMERGENCY EXIT SIGN BATTERYS (P/N 37067-001) (S/N KP1048) OPS CHECK OK. 2 L 7 3 4F A3WE 1998030500695 19980305 00695 NM 1998 3 5 RAAA98B2010 1 19980301 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AFT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998030500696 19980305 00696 SO 1998 3 5 RAAA98E8005 1 19980226 A 3350 CONTACTOR GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN OUT OF ADJUST A RAAA K NONE L NO TEST CR CRUISE 1 AL 03 178RV 188C2010 FWD RT OVERWING EXIT PULL DOWN EMERGENCY LIGHT FLASHES ON OCCASIONALLY IN FLIGHT. CLEANED AND ADJUSTED CONTACTS. 2 L 7 4 4T 4A22 1998030500697 19980305 00697 WP 1998 3 5 CALA9800360 1 19980302 A 3222 O-RING DOUG DC9 DC982 3022082 WP NLG STRUT LEAKING A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 92874 49122 THE NLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE FOUND THE NLG STRUT SCHRADER VALVE LEA KING. THE O-RING WAS REPLACED. THE NLG STRUT WAS SERVICED WITH NITROGEN AND A DIP WAS ISSUED FOR FULL SERVICE AT NEXT RON MAINTENANCE. 2 L 7 2 4F A6WE 1998030500698 19980305 00698 NM 1998 3 5 CALA9800361 1 19980302 A 3350 10617837 LIGHT IDD AEROSPAC BOEING 727 727243 138408D NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT ROW 28 AND 29 INOPERATIVE. THE EXIT SIGN WAS REMOVED AND REPLACED. ALSO, MAINTENANCE FOUND PIN AT SIGN CANNON PLUG BENT AND BROKEN WIRING. THE PIN AND WIRING WERE REPAIRED AND OPERATION OF THE LIGHT WAS NORMAL. 2 L 7 3 4F RT A3WE 1998030500699 19980305 00699 WP 1998 3 5 CALA9800362 1 19980228 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 636-693 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 INSPECTION FOUND MID BAGGAGE BIN Z-ANGLE CORRODED FROM STA 636 TO 693. A DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 63 . 2 L 7 2 4F A6WE 1998030500700 19980305 00700 WP 1998 3 5 CALA9800363 1 19980228 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1155-1211 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 INSPECTION FOUND AFT BAGGAGE BIN LOWER DOOR JAMB BEAM CORRODED FROM STA 1155 TO 1211. REPAIRED IAW SRM 53-05. 2 L 7 2 4F A6WE 1998030500701 19980305 00701 WP 1998 3 5 CALA9800364 1 19980228 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 INSPECTION FOUND A 4 INCH CRACK IN LONGERON 2R AT STA 1418. A SPLICE REPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18, SHE ET 2. 2 L 7 2 4F A6WE 1998030500702 19980305 00702 WP 1998 3 5 CALA9800365 1 19980228 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 INSPECTION FOUND CORROSION ON FUSELAGE SKIN UNDER VHF-3 ANTENNA AT STA 1174. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 53 30-02631. 2 L 7 2 4F A6WE 1998030500703 19980305 00703 WP 1998 3 5 CALA9800366 1 19980302 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 THE EXTERIOR TAILCONE RELEASE HANDLE PULLED FROM CLIPS AT FIVE POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND FUNCTIONAL CH ECK WAS GOOD IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998030500704 19980305 00704 WP 1998 3 5 CALA9800367 1 19980302 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17812 49250 THE TAILCONE INTERIOR RELEASE HANDLE PULLED FROM CLIPS AT FORTY POUNDS. THE HANDLE CLIPS WERE ADJUSTED AND FUNCTIONAL C HECK WAS GOOD IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998030500705 19980305 00705 WP 1998 3 5 CALA9800368 1 19980228 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 450 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND FLOORBEAM CORRODED AT STA 450 FROM CENTERLINE TO 24 RIGHT OF CENTERLINE. THE CORRODED SECTION OF FLOOR BEAM WAS REPLACED IAW GMM 10-900-01, PAGE 1. 2 L 7 3 4F A22WE 1998030500706 19980305 00706 WP 1998 3 5 CALA9800369 1 19980228 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 442 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT L-1 DOOR, STA 442. THE CORRODED SECTION OF BEAM WAS REPLACED IAW GMM 10 -900-01, PAGE 1. 2 L 7 3 4F A22WE 1998030500707 19980305 00707 NM 1998 3 5 9803432289 1 19980301 A 2751 1812993 INDICATOR BOEING 727 727251 138408H NM TE FLAPS FAILED A NWAA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 GL 01 289US 23338 3457 21377 DURING CLIMB, INBOARD FLAPS REMAINED IN TAKEOFF CONFIGURATION. FLIGHT WAS DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED INBOARD FLAP INDICATOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998030500708 19980305 00708 WP 1998 3 5 9803449992 1 19980301 A 2410 CSD DOUG DC9 DC931 3022065 WP LT ENGINE LOW OIL A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 8960E 45869 LEFT CSD OIL PRESSURE LOW LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED AT 70 KNOTS. MAINTENANCE FOUND CS D LOW ON OIL. RESERVICED AND REPLACED OIL FILTER. 2 L 7 2 4F A6WE 1998030500709 19980305 00709 WP 1998 3 5 9803459991 1 19980228 A 2130 AMPLIFIER DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8957E 47215 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE R EPLACED CABIN PRESSURE AMPLIFIER AND DIFFERENTIAL PRESSURE SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500710 19980305 00710 1998 3 5 9803469925 4 19980227 A 2565 13621228 SLIDE DOUG DC9 DC932 3022066 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 925US 50471 2089 47472 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE, CHECKED OK. 2 L 7 2 4F A6WE 1998030500711 19980305 00711 WP 1998 3 5 9803479103 1 19980228 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 93S 47078 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500712 19980305 00712 WP 1998 3 5 9803489301 1 19980301 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN CONTAMINATED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 301RC 48054 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS INOPERATIVE. CLEANED CANNON PL UG TO 8-24 BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500713 19980305 00713 WP 1998 3 5 9803499875 1 19980227 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 784NC 48109 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 1, 2, 3, AND 5 INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998030500714 19980305 00714 WP 1998 3 5 9803509925 1 19980227 A 3350 9661126 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 952N 47073 FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS WOULD NOT SHUT OFF IN FLIGHT. REPLACED POWER SUPPLY AND BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500715 19980305 00715 WP 1998 3 5 9803519979 1 19980228 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9343 47439 DURING PERIODIC CHECK, FOUND LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED BATTERY PACK, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500716 19980305 00716 WP 1998 3 5 9803529751 1 19980227 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 751NW 47115 DURING LINE MAINTENANCE INSPECTION, FOUND MID CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. TIGHTENED LOOSE WIRE AT BATTE RY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998030500717 19980305 00717 NM 1998 3 5 9803535501 1 19980221 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 501US 23190 DURING PREFLIGHT, FOUND DOOR 1R AND SEVERAL EMERGENCY LIGHTS IN FIRST CLASS ONLY STAY ON FOR ABOUT 5 SECONDS. REPLACED BATTERY PACK IN POWER SUPPLY M730, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998030500718 19980305 00718 NM 1998 3 5 9803545518 1 19980220 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 518US 23206 DURING PREFLIGHT, FOUND DOOR 3L EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY M735, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1998030500719 19980305 00719 NM 1998 3 5 9803552709 1 19980220 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 818EA 22555 DURING PREFLIGHT, FOUND FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998030500720 19980305 00720 NM 1998 3 5 9803562291 1 19980225 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 291US 21379 DURING PREFLIGHT, FOUND BOTH LEFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND CHARGER, OPERAT IONAL CHECK OK. 2 L 7 3 4F A3WE 1998030500721 19980305 00721 NM 1998 3 5 9803572290 1 19980226 A 3350 LIGHT BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 290US 21378 DURING PREFLIGHT, FOUND COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998030500722 19980305 00722 WP 1998 3 5 9803581226 1 19980228 A 3350 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 223NW 46583 DURING LINE CHECK, FOUND ESCAPE PATH LIGHTING FAILS EMERGENCY LIGHT TEST. REPLACED C-SECTION POWER SUPPLY AND BATTERY, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998030500723 19980305 00723 NM 1998 3 5 9803596740 1 19980213 A 7722 CONNECTOR BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE LOOSE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 640US 23888 662539 AFTER TAKEOFF DURING CLIMB, THE NR 1 ENGINE EGT BEGAN RISING RAPIDLY. THE NR 1 POWER LEVER WAS RETARDED TO MAINTAIN THE EGT WITHIN LIMITS. WITH ALL ENGINE EPRS MATCHED, THE NR 1 EGT WAS 250C ABOVE THE OTHERS. THE AIRCRAFT RETURNED TO ANC WITHOUT DIFFICULTY. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED. A PS4 LINE WAS RETORQUED AND THE FIREWALL CANNON PLUG FOR EGT WAS RESEATED. THE AIRCRAFT WAS RETURNED TO SERVICE. EXACT PART CAUSING DIFFICULTY TO BE DETERMINE D. 2 L 7 4 4F 4 F A20WE E20EA 1998030500724 19980305 00724 NM 1998 3 5 SWAA980170 1 19980205 A 5320 SKATE ANGLE BOEING 737 7373A4 1384585 NM BS 569 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND LT SKATE ANGLE CRACKED AT BS 569, LBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500725 19980305 00725 NM 1998 3 5 SWAA980171 1 19980205 A 5320 SHEAR WEB BOEING 737 7373A4 1384585 NM BS 931 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE ON SHEAR WEB AT BS 931, BL 0, WL 203.5. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998030500726 19980305 00726 NM 1998 3 5 SWAA980172 1 19980205 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 986.5, RBL 44, 32, 31, 27, 22, 15, LBL 44, 41, 35, 30, 24, 15, 5, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500727 19980305 00727 NM 1998 3 5 SWAA980173 1 19980205 A 5311 FRAME BOEING 737 7373A4 1384585 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FRAME I/B CHORD IS CRACKED AT BS 616, LBL 65, WL 200. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998030500728 19980305 00728 NM 1998 3 5 SWAA980174 1 19980206 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 792/872 EXFOLIATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM IS EXFOLIATED BETWEEN BS 792 AND 872. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500729 19980305 00729 NM 1998 3 5 SWAA980175 1 19980206 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 857 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED D-CHECK, FOUND CORROSION IN AND AROUND FLOORBEAM HOLE AT BS 857, RBL 14. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998030500730 19980305 00730 NM 1998 3 5 SWAA980176 1 19980205 A 5240 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674SW 23253 DURING SCHEDULED B/C2 CHECK, FOUND AFT SERVICE DOOR LWR HINGE CUTOUT CRACKED FROM LWR TO FWD CORNER EXTENDING BENEATH S KIN LAP TO NEAREST RIVET HOLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500731 19980305 00731 NM 1998 3 5 SWAA980177 1 19980204 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED BS 727 TO 947, LBL 7.5, WL 158. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998030500732 19980305 00732 NM 1998 3 5 SWAA980178 1 19980204 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED BS 727 TO 947, LBL 12, WL 158. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500733 19980305 00733 NM 1998 3 5 SWAA980179 1 19980204 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED BS 727 TO 947, RBL 2.5, WL 158. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998030500734 19980305 00734 NM 1998 3 5 SWAA980180 1 19980206 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORRODED AT BS 772, RBL 14. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500735 19980305 00735 NM 1998 3 5 SWAA980181 1 19980206 A 5330 SKIN BOEING 737 7373A4 1384585 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674SW 23252 DURING SCHEDULED C2 CHECK, FOUND OUTER FUSELAGE SKIN CRACKED BETWEEN UPPER FWD ENTRY DOORWAY RADIUS CUTOUT AND RAIN GUTT ER. REMOVED AND REPLACED PER SWA ACO 6317-53. 2 L 7 2 4F RT A16WE 1998030500736 19980305 00736 NM 1998 3 5 SWAA980182 1 19980206 A 5230 SKIN BOEING 737 7373A4 1384585 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 674SW 23252 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR OUTER SKIN CRACKED .125 INCH AT UPPER AFT CORNER OF HANDLE CUT OUT. REP AIRED PER SWA RA 1-A52-023. 2 L 7 2 4F RT A16WE 1998030500737 19980305 00737 NM 1998 3 5 SWAA980183 1 19980206 A 5320 SUPPORT BOEING 737 7373A4 1384585 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT IS CRACKED AT BS 540, LBL 1, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500738 19980305 00738 NM 1998 3 5 SWAA980184 1 19980206 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 294, RBL 54, WL 209. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500739 19980305 00739 NM 1998 3 5 SWAA980185 1 19980206 A 5320 SUPPORT BOEING 737 7373A4 1384585 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 669SW 23752 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, RBL 1, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500740 19980305 00740 NM 1998 3 5 SWAA980186 1 19980206 A 3350 300432 LIGHTS BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702SW 22054 DURING WALKAROUND CHECK, FOUND TWO EMERGENCY TRACK LIGHTS INOP. REPLACED LAMPS FOR TRACK LIGHT PER BOEING M/M. 2 L 7 2 4F A16WE 1998030500741 19980305 00741 NM 1998 3 5 SWAA980187 1 19980206 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 862 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORRODED AT BS 862, RBL 14. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500742 19980305 00742 NM 1998 3 5 SWAA980188 1 19980206 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 943 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 943, STR 24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998030500743 19980305 00743 NM 1998 3 5 SWAA980189 1 19980209 A 5240 SKIN BOEING 737 7373A4 1384585 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673SW 23251 DURING SCHEDULED BC4 CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500744 19980305 00744 NM 1998 3 5 SWAA980190 1 19980210 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING WALKAROUND CHECK, FOUND APPROX 5 INCH SKIN CRACK LEFT SIDE BETWEEN CABIN WINDOWS 11 AND 12. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998030500745 19980305 00745 NM 1998 3 5 SWAA980191 1 19980210 A 3350 65C27095 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 315SW 23337 DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998030500746 19980305 00746 NM 1998 3 5 UPS98225955 1 19980302 A 3350 BATTERY PACK BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 939UP 19532 INSPECTION TYPE-N/A, WITH EMERGENCY LIGHT SWITCH OFF, MAIN ENTRY DOOR EMERGENCY LIGHT ILLUMINATES. WHEN POWER IS REMOVE D FROM A/C RESEATING UNIT, HAD NO EFFECT LIGHT ASSY (S/N 27741). REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998030500747 19980305 00747 NM 1998 3 5 UPS98525954 1 19980302 A 5320 SUPPORT BOEING 757 75724APF 1384969 NM CARCO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 450UP 25472 INSPECTION TYPE-N/A, AFTER REMOVING NR 1 PIT BULKHEAD WALL AND FLOOR ANGLE, FOUND FLOOR SUPPORT BEAM CRACKED. REPAIRED FLOOR SUPPORT BEAM IAW SRM 51-70-11. 2 L 7 2 4F RT A2NM 1998030500748 19980305 00748 EU 1998 3 5 WWMA9800043 1 19980228 A 3350 2LA0059851 LIGHT SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 319AE 340B319 DURING PREFLIGHT, FOUND THE OVERHEAD LIGHT PANEL ABOVE SEAT 9A LOOSE. REPLACED THE EMERGENCY LIGHT PASSENGER SERVICE PA NEL. 2 L 7 2 4T RT A52EU 1998030500749 19980305 00749 EU 1998 3 5 WWMA9800042 1 19980226 A 2612 FIRE TEST SAAB SF340 340B 7860101 EU LT ENGINE MALFUNCTIONED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 306AE 340B306 DURING PREFLIGHT CHECKS, THE LEFT FIRE TEST FAILED TO FUNCTION. MAINTENANCE RERACKED THE WEU AND CYCLED THE AIRCRAFT PO WER SEVERAL TIMES, COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A52EU 1998030500750 19980305 00750 EU 1998 3 5 QXEA9800120 1 19980227 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU ROW 9A FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 BOI - EMERGENCY EXIT LIGHT ON ROW 9A INOP. MAINTENANCE RELAMPED LIGHT BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998030500751 19980305 00751 EU 1998 3 5 QXEA9800121 1 19980301 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 SEA - NR 1 AFT EVACUATION LIGHT FULL OF WATER. MAINTENANCE DRAINED AND CLEANED LIGHT. FOUND TWO OF THE FOUR LENS COVER NUT PLATES BROKEN. PERFORMED INTERIM REPAIR. NO PARTS REPLACED. OPERATIONAL TEST GOOD. AIRCRAFT RETURNED TO SERVICE . 2 L 7 2 4F RT A20EU 1998030500773 19980305 00773 EU 1998 3 5 QXEA9800117 1 19980302 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE BUCKLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FUSELAGE SKIN IS BUCKLED AT 3 LOCATIONS ALONG FUSELAGE SKIN SPLICE AT APPROXIMATELY 12 UP FROM RIGHT-HAND ACM COMP ARTMENT OPENING. REPAIRED IAW HORIZON AIR EA 4-53-610. 2 L 7 2 4F RT A20EU 1998030500775 19980305 00775 WP 1998 3 5 98FDEA00144 1 19980302 A 3260 806124 ELECTRONIC UNIT DOUG DC10 DC1030F 3023504 WP LANDING GEAR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 302FE 46801 AFTER TAKEOFF, GEAR HANDLE UP GAVE RED LEFT MAIN INDICATION ON F/O PANEL AND UP FRONT. RAN RED TAB, NO HELP. CHECKED W IRING INTEGRITY FROM S3-682 TERMINAL 4 AND 5 (PROX ELETR UNIT) AS PER WDM 32-61-04 PG 2, FOUND OK. REMOVED AND REPLACED PROXIMITY ELECTRONIC UNIT PER M/M 32-61-01-2. 2 L 7 3 4F RT A22WE 1998030500776 19980305 00776 NM 1998 3 5 98FDEA00145 1 19980302 A 5320 651841515 STIFFENER BOEING 727 72722C 138400F NM BS 346 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 NR 0272 001 CORROSION (C53-100-01(1)) ON NOSE WHEEL WELL BOX STIFFENER BS 346, WL 182, LBL 14. REMOVED AND REPLACED STI FFENER BS 346, WL 182, LBL 14 PER FED-EX DRAWING 65-18415 AND FED-EX SRM 51-30-2. 2 L 7 3 4F A3WE 1998030500777 19980305 00777 NM 1998 3 5 98FDEA00146 1 19980302 A 5230 6541990129 HINGE BOEING 727 72721C 138400M NM CARGO DOOR ELONGATED HOLES A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 UPON REMOVAL OF MAIN CARGO DOOR FWD END HINGE FOUND FASTENER HOLES TO BE ELONGATED REQUIRING REPLACEMENT OF FORWARD END HINGE. *S/D* REPAIRED MAIN CARGO DOOR FWD END HINGE PER FEDEX SRM 51-20-04 AND OHM 20-50-01. 2 L 7 3 4F A3WE 1998030500778 19980305 00778 NM 1998 3 5 98FDEA00147 1 19980223 A 2133 OUTFLOW VALVE BOEING 727 72725 1384006 NM CABIN FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 504FE 18274 AIRCRAFT WOULD NOT PRESSURE AFTER TAKEOFF WITH TWO PACKS ON AND OUTFLOW VALVE CLOSED. COMPLETED UNSCHEDULED CABIN PRESS URE CHANGE CHECK LIST WITH NEGATIVE RESULTS. PERFORMED PRESSURIZATION TEST PER MAINTENANCE MANUAL 21-30-0 PAGE 501 TO 5 03. FOUND LEFT OUTFLOW VALVE STAYING OPEN. REMOVED AND REPLACED LEFT OUTFLOW VALVE, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1998030500779 19980305 00779 WP 1998 3 5 ABXA9800136 1 19980302 A 3230 RETRACT MECH DOUG DC8 DC861 3021952 WP LANDING GEAR OUT OF ADJUST A ABXA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 23 853AX 46037 AFTER TAKEOFF AND GEAR RETRACTION, VIBRATION COULD BE FELT AND HEARD FROM NOSE GEAR AREA. ALL INDICATIONS WERE GOOD. R ECYCLED GEAR THREE TIMES, ON THIRD TIME, VIBRATION CEASED. REPLACED DOOR BUMPERS, AND PERFORMED ADJUST/TEST IAW DC8 MM 32-20-00, NO DEFECTS NOTED. 2 L 7 4 4F 4A25 1998030500780 19980305 00780 WP 1998 3 5 MWEA98265 1 19980302 A 5313 3924809 LONGERON DOUG DC9 DC932 3022066 WP BS 575-605 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 29R WAS FOUND CORRODED FROM FS 575 TO FS 605. REMOVED AND REPLACED LONGERON. 2 L 7 2 4F A6WE 1998030500781 19980305 00781 WP 1998 3 5 MWEA98266 1 19980302 A 5311 3913291 SPLICE DOUG DC9 DC932 3022066 WP BS 408-472 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON SPLICES AT FRAME STATION 408 AND 427 FOR LONGERON 30 WERE FOUND CORRODED. REMOVED AND REPLACED SPLICES. 2 L 7 2 4F A6WE 1998030500782 19980305 00782 WP 1998 3 5 MWEA98267 1 19980302 A 5313 5920319 LONGERON DOUG DC9 DC932 3022066 WP BS 415-596 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 30 WAS FOUND CORRODED FROM FS 415 TO FS 596 WITH EXCESSIVE MATERIAL LOSS AT ALL FRAMES. REMOVED AND REPLACED L ONGERON FROM FS 408 TO 596. 2 L 7 2 4F A6WE 1998030500783 19980305 00783 WP 1998 3 5 MWEA98268 1 19980302 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 484-503 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL BETWEEN FS 484 AND 503 LONGERON 27L AND 28L WAS FOUND CORRODED. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 1998030500784 19980305 00784 WP 1998 3 5 MWEA98269 1 19980302 A 5320 5910142 JAMB DOUG DC9 DC932 3022066 WP BS 370-427 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FORWARD CARGO DOOR JAMB PAN WAS FOUND CORRODED ALONG THE ENTIRE LOWER LENGTH FROM FS 370 TO FS 427. CORROSION BLENDED B EYOND LIMITS. REMOVED AND REPLACED SECTION OF PAN. 2 L 7 2 4F A6WE 1998030500785 19980305 00785 WP 1998 3 5 MWEA98270 1 19980302 A 5311 2777930 FRAME DOUG DC9 DC932 3022066 WP BS 351 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE FRAME AT FS 351 WAS FOUND TO HAVE CORROSION BETWEEN LONGERON 28L TO 28R. CORROSION WAS BLENDED BEYOND LIMITS. REMO VED AND REPLACED SECTION OF FRAME. 2 L 7 2 4F A6WE 1998030500786 19980305 00786 WP 1998 3 5 MWEA98271 1 19980302 A 5320 9919650 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 370-408 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE INTERCOSTAL AT LONGERON 29R FROM FS 370 TO 408 WAS FOUND CORRODED. REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 1998030500787 19980305 00787 WP 1998 3 5 MWEA98272 1 19980302 A 5311 2777930 FRAME DOUG DC9 DC932 3022066 WP BS 598 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 DURING D-CHECK, THE FRAME AT FS 598 HAS CORROSION BETWEEN LONGERON 28L AND 29R. CORROSION BLEND OUTS BEYOND LIMITS. FA BRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998030500788 19980305 00788 WP 1998 3 5 MWEA98273 1 19980227 A 2560 113313 SLIDE DOUG DC9 DC915 3022036 WP PAX DOOR DEPLOYED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 900ME 45841 THE FORWARD ENTRANCE DOOR SLIDE FELL OUT OF DOOR WHEN OPENED. MTC INSTALLED FORWARD ENTRANCE DOOR SLIDE. 2 L 7 2 4F A6WE 1998030500789 19980305 00789 WP 1998 3 5 MWEA98274 1 19980302 A 5312 BULKHEAD CLIP DOUG DC9 DC932 3022066 WP AFT BULKHEAD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 THE AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB LOWER RT TEE ANGLE ABOVE GUSSETT AND RT TEE CLIP INBOARD OF GUSSET AROUND FA STENERS HAS CORROSION. MTC REMOVED CORROSION. 2 L 7 2 4F A6WE 1998030500790 19980305 00790 WP 1998 3 5 MWEA98275 1 19980302 A 5312 BULKHEAD TEE DOUG DC9 DC932 3022066 WP AFT BULKHEAD CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 THE AFT PRESSURE BULKHEAD VENTRAL DOOR JAMB LOWER RT HORIZONTAL TEE HAS CORROSION. MTC FABRICATED REPLACEMENT TEE. 2 L 7 2 4F A6WE 1998030500792 19980305 00792 NM 1998 3 5 DL72S980479 1 19980226 A 2782 BRACKET BOEING 727 727232 1384082 NM RT LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FOUND DURING B-2 LETTER CHECK, NR 5 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998030500793 19980305 00793 NM 1998 3 5 DL72S980480 1 19980226 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FOUND DURING B-2 LETTER CHECK, NR 2 SLAT COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998030500794 19980305 00794 WP 1998 3 5 DLL10980481 1 19980226 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 720DA 69419 193C1136 COCKPIT AND L1 DOOR EMERG EXIT SIGNS INOP. REPLACED POWER SUPPLY UNIT, CKD NML. 2 L 7 3 4F A23WE 1998030500795 19980305 00795 NM 1998 3 5 DL72W980483 1 19980227 A 5320 WEB BOEING 727 727247 138408F NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FOUND ON MV1 CHECK, TWO .375 INCH CRACKS UPPER END OF TORQUE BOX VERTICAL WEB STA 1243. FABRICATED/INSTALLED DOUBLER P ER M/M 53-11-0. 2 L 7 3 4F A3WE 1998030500796 19980305 00796 NM 1998 3 5 DLM11980485 1 19980226 A 3350 LIGHT P20070030 DOUG MD11 MD11 3023602 NM PWA JT8 JT8D219 52053 NE CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 807DE 48478 726003 EMERGENCY FLASHLIGHT WOULD NOT TEST. REPLACED FLASHLIGHT. 2 L 7 3 4F 4 F RT A22WE E9NE 1998030500797 19980305 00797 NM 1998 3 5 DL72S980486 1 19980226 A 5320 WEB BOEING 727 727232 1384082 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 WHILE BUYING BACK N/R 52 FOUND LT TORQUE BOX VERTICAL WEB UPPER LIGHTENING HOLE STA 1243 CRACKED AT PREVIOUS ROUT OUT. REPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1998030500798 19980305 00798 NM 1998 3 5 DL757980487 1 19980227 A 3350 BULB 767 BOEING 757 757232 1384965 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 685DA 27588 R-1 DOOR EMERGENCY LIGHT INOP. RELAMPED, OPS CK OK. 2 L 7 2 4F RT A2NM 1998030500799 19980305 00799 NM 1998 3 5 DL72S980489 1 19980227 A 5754 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 537DA 22073 FOUND DURING D-1 LETTER CHECK, NR 6 L/E SLAT ACTUATOR ATTACH RIB CRACKED AT PREVIOUS REPAIR. REPAIRED PER M/M 57-54-0 A ND ERA 364139-14. 2 L 7 3 4F A3WE 1998030500800 19980305 00800 NM 1998 3 5 DL72S980492 1 19980228 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 409DA 21153 EMERGENCY LIGHTS ON AFT CARGO DOOR AND ABOVE EMERGENCY EXITS LFT SIDE FLASHING. REPLACED BOTH BATTERY PACKS. 2 L 7 3 4F A3WE 1998030500801 19980305 00801 WP 1998 3 5 DLL10980493 1 19980301 A 3397 WIRE 081691 LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 193C1180 EMERGENCY TRACK LIGHTING FIRST CLASS LEFT SIDE 2ND RED BULB INOP. REPLACED SOCKET AND LAMP, OPS NORMAL. 2 L 7 3 4F A23WE 1998030500802 19980305 00802 WP 1998 3 5 DLL10980494 1 19980301 A 3350 POWER SUPPLY 516574 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 60852 193C1180 EMERGENCY LIGHTS IN D-ZONE WILL ONLY STAY ILLUMINATED FOR 20 SECS WITH MASTER SW IN ON POSITION. REPLACED POWER SUPPLY, OPS NORMAL. 2 L 7 3 4F A23WE 1998030500803 19980305 00803 NM 1998 3 5 DL72S980495 1 19980228 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 534DA 22047 PORTABLE EMERGENCY LIGHT ABOVE R1 GALLEY DOOR IS INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1998030500804 19980305 00804 NM 1998 3 5 DL72S980496 1 19980227 A 2782 ACTUATOR 269002917 BOEING 727 727232 1384082 NM NR 2 LE SLAT LEAKING A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 489DA 153 21019 HYD SYS-A FAILURE IN FLT. REPLACED NR 2 LEADING EDGE SLAT ACTUATOR. 2 L 7 3 4F A3WE 1998030500805 19980305 00805 NM 1998 3 5 DL72W980500 1 19980227 A 5330 65545901 SKIN BOEING 727 727247 138408F NM BS 700 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 AN AREA OF CORROSION WAS DISCOVERED ON THE SKIN PANEL AT FS 700, BL 0. THE CORROSION WAS CUTOUT OVER A 7.75 X 6.75 AREA . THE REQUIRED SKIN REPAIR WAS GOING TO INFRINGE ON TWO PREVIOUSLY ACCOMPLISHED SKIN REPAIRS, SO THE PREVIOUS REPAIRS W ERE REMOVED AND A NEW SKIN DOUBLER REPAIR INSTALLED TO ENCOMPASS ALL OF THE DAMAGED AREAS. THE REPAIR WAS INSTALLED PER THE SRM GUIDELINES AND DOCUMENTED PER 364097. 2 L 7 3 4F A3WE 1998030500807 19980305 00807 WP 1998 3 5 RRXA98023 1 19980113 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 69.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, PERFORMED INSPECTION PROCEDURES IAW DC-8 (SB 57-88). RIGHT WING LOWER SURFACE AT STA 69.5 F OUND RIVET HOLES 1, 2, 3, 4, 5, B, D AND E HAD CRACKS BEYOND LIMITATIONS IAW (BAC). REWORK HOLES AND REPAIRED BY DOUBLE R REPAIR IAW SB 57-88 AND FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04123. 2 L 7 4 4F RT 4A25 1998030500808 19980305 00808 WP 1998 3 5 RRXA98024 1 19980124 A 5320 5711283505 FITTING DOUG DC8 DC871F 302199D WP CARGO COMPT DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND CARGO COMPARTMENT NET FITTING DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. FABRICATED NEW FITTING BY MATERIAL SUBSTITUTION AND INSTALLED IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04168. 2 L 7 4 4F RT 4A25 1998030500809 19980305 00809 WP 1998 3 5 RRXA98026 1 19980122 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 69.5 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, PERFORMED INSPECTION PROCEDURES IAW SB 57-38 ON RIGHT WING AT STA 69.5. FOUND (3) MISDRILLE D RIVET HOLES IN DOUBLER AND TRIPLER. REPAIRED RIVET HOLES BY OVERSIZED AND BUSHINGS INSTALLED IAW FAA APPROVED DER TIM CO ENGINEERING SKETCH REO-04184. 2 L 7 4 4F RT 4A25 1998030500810 19980305 00810 WP 1998 3 5 RRXA98027 1 19980124 A 5742 NAS4205 BOLT DOUG DC8 DC871F 302199D WP NR 2 PLYON MISSING A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND NR 2 PLYON SKATE ANGLE MISSING BOLT AT XW=253, 20 INCHES AFT OF FRONT SPAR. REPLACED BOLT BY INSTALLING FASTENER (NAS4205) BY MATERAIL SUBSTITUTION IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04195. 2 L 7 4 4F RT 4A25 1998030500811 19980305 00811 WP 1998 3 5 RRXA98028 1 19980124 A 5512 656174759 PANEL DOUG DC8 DC871F 302199D WP LT HOR STAB TE CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND LEFT SIDE HORIZONTAL STAB UPPER TE PANEL CORRODED BEYOND LIMITATIONS IAW DC-8 SRM. FA BRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04197. 2 L 7 4 4F RT 4A25 1998030500812 19980305 00812 WP 1998 3 5 RRXA98029 1 19980126 A 5753 2647279501 FITTING DOUG DC8 DC871F 302199D WP FLAP LINK SUPT MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, REMOVED FLAP LINK SUPPORT ASSY (P/N 2647279-501) FOR REPLACEMENT. NEW FLAP LINK SUPPORT ASS Y (P/N 2647279-501) WAS RECEIVED WITH ONE HOLE LOCATION OVERSIZE BY APPROX 0.006. ALTHOUGH THE AMOUNT OF THE OVERSIZE IS NEGLIGIBLE, STRUCTURALLY IT CAUSED THE BUSHING TO HAVE A CLEARANCE FIT INSTEAD OF INTERFERENCE FIT, IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04201. 2 L 7 4 4F RT 4A25 1998030500813 19980305 00813 WP 1998 3 5 RRXA98030 1 19980127 A 5720 5769933402 DOUBLER DOUG DC8 DC871F 302199D WP RT WING LE CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND RIGHT WING OUTBD LEADING EDGE SLOT BULLNOSE SKIN CHAFED ON OUTBD EDGE. SKIN WORN THRU AND INTO THE DOUBLER AT THE OUTBD ATTACHING POINTS. REMOVED CHAFED DAMAGED DOUBLER, FABRICATED AND INSTALLED NEW DOUBL ER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04207. 2 L 7 4 4F RT 4A25 1998030500814 19980305 00814 WP 1998 3 5 RRXA98031 1 19980126 A 5320 5975549451 DOUBLER DOUG DC8 DC871F 302199D WP BS 1160 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE AFTER BLEND-OUT PROCEDURES WAS PERFORMED TO DOUBLER (P/N 9754945-1) A T STA 1160 AND LONGERON 33 RIGHT BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED ALL CORROSION AND TREATED AREA IAW DC-8 SRM 5 1-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04211. 2 L 7 4 4F RT 4A25 1998030500815 19980305 00815 WP 1998 3 5 RRXA98032 1 19980127 A 5711 56536622 SPAR CAP DOUG DC8 DC871F 302199D WP RT TE FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND RIGHT WING INBD TE FLAP, UPPER SPAR CAP CRACKED AT THE INBD GSE ATTACHMENT POINTS. FA BRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04214. 2 L 7 4 4F RT 4A25 1998030500816 19980305 00816 WP 1998 3 5 RRXA98033 1 19980127 A 5330 9794011 SKIN DOUG DC8 DC871F 302199D WP BS 220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND EXTERIOR FUSELAGE SKIN AND DOUBLER AND REPAIR CORRODED BEYOND LIMITATIONS IAW AT STA 220 AND LONGERON 36. REMOVED ALL CORROSION FROM AREA AND TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED DAMAGED SECTIONS, F ABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS TO DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04218. 2 L 7 4 4F RT 4A25 1998030500817 19980305 00817 NM 1998 3 5 VNAA9802023 1 19980226 A 3242 BRAKES DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG WEAK A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 430JS 3044 DURING THE TAXI FOR TAKEOFF, THE CREW NOTED THAT THE AIRCRAFT'S BRAKES WERE WEAK. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND BLED, THE NORMAL BRAKE SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-07. OPERATIO NAL CHECKS WERE COMPLIED WITH AND, THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998030500915 19980305 00915 SO 1998 3 5 WTAA980016 1 19980122 A 3620 M1160140242 SENSOR EMB 120 EMB120RT SO RT ENGINE MISWIRED A WTAA E ENGINE SHUTDOWN N FALSE WARNING LD LANDING 1 WP 17 221YV 120221 BFL - DURING APPROACH RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED. CREW CLOSED RIGHT ENGINE BLEED VALVE AND DECLARED EMERG ENCY. AIRCRAFT LANDED WITHOUT INCIDENT. CREW SECURED RIGHT ENGINE IMMEDIATELY AFTER TOUCH DOWN. MAINTENANCE INSPECTED AIRCRAFT. NO EVIDENCE OF DUCT LEAK REPORTED. DEFERRED SUBSEQUENTLY CLEARED DEFERRAL BY REPAIRING WIRING AT DUCT LEAK SENSOR S0344. SYSTEM OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4T RT A31SO 1998030500916 19980305 00916 EU 1998 3 5 WTAA980015 1 19980126 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 418UE 780 OXR - LEFT ENGINE RPM INDICATION DROPPED TO ZERO ON TAKEOFF ROLL. TAKEOFF ABORTED. AIRCRAFT FERRIED TO LAX FOR REPAIRS . MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR. OPERATIONAL CHECK OF LEFT RPM GAUGE SATISFACTORY. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998030500917 19980305 00917 EU 1998 3 5 RAIA980201 1 19980201 A 3242 AHA1653 BRAKE ASSY AEROSP ATR72 ATR72202 8680940 EU LT MLG SMOKING A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 721TE 7890 217 FLT 7159 - STL - LEFT OUTBOARD BRAKE WAS SMOKING ON TAXI INTO GATE. MAINTENANCE INSPECTED LEFT OUTBOARD BRAKE. MAINTEN ANCE REMOVED AND REPLACED LEFT OUTBOARD BRAKE ASSEMBLY. TAXIED AIRCRAFT NO SMOKING NOTED. (M) 2 H 7 2 4T RT A53EU 1998030500918 19980305 00918 EU 1998 3 5 RAIA980135 1 19980130 A 2910 MS27371G0143 LINE AEROSP ATR42 ATR42300 8680920 EU GREEN HYD SYSTEM FAILED A RAIA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 03 424TE 20704 124 FLT 7417 - FYV - GREEN SYSTEM HYDRAULIC PRESSURE DROPPED TO ZERO. LOW LEVEL CAPTION ILLUMINATED. MAINTENANCE INSPECTED AND REPLACED GREEN HYDRAULIC PUMP PRESSURE LINE. (M) 2 H 7 2 4T RT A53EU 1998030500919 19980305 00919 EU 1998 3 5 RAIA980134 1 19980129 A 3610 ASNA214505 CLAMP AEROSP ATR42 ATR42300 8680920 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 03 422TE 106 FLT 7114 - STL - RIGHT ENGINE ONLY MADE 40 PERCENT TORQUE ON CLIMB-OUT, OIL PRESSURE CAPTION ILLUMINATED, CREW SHUT ENGI NE DOWN. MAINTENANCE INSPECTED AND FOUND HP BLEED VALVE CLAMP HAD FAILED. MAINTENANCE REPLACED HP BLEED VALVE CLAMP. 2 H 7 2 4T RT A53EU 1998030500920 19980305 00920 EU 1998 3 5 RAIA980133 1 19980128 A 3060 C40631 BRUSH BLOCK JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 560HK 5154 41076 FLT 7741 - JFK - RIGHT PROPELLER DE-ICE FAILED IN FLIGHT. MAINTENANCE REPLACED RIGHT PROPELLER DE-ICE BRUSH BLOCK. (M) 2 L 7 2 4T RT A41NM 1998030500921 19980305 00921 EU 1998 3 5 RAIA980132 1 19980129 A 3610 13711543L48 BLEED LINE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 427AM 12882 876 FLT 7023 - STL - LEFT FUEL LOW PRESSURE CAPTION ILLUMINATED AND FUEL PRESSURE INDICATING LOW. MAINTENANCE INSPECTED AND FOUND LEFT ENGINE BLEED LINE BROKEN. MAINTENANCE REPLACED LEFT ENGINE BLEED LINE. (M) 2 L 7 2 4T RT A56EU 1998030500922 19980305 00922 EU 1998 3 5 RAIA980131 1 19980129 A 2422 1B3501B13 INVERTER BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILED A RAIA B EMER. DESCENT H ELECT. POWER LOSS-50 PC LD LANDING 1 CE 03 871JX 384 871 FLT 4794 - LAX - NR 1 INVERTER FAILED, CREW SMELLED SMOKE. MAINTENANCE INSPECTED AND REPLACED NR 1 INVERTER. (M) 2 L 7 2 4T RT A56EU 1998030500923 19980305 00923 1998 3 5 RAIA980130 4 19980128 A 3421 7000622901 VERTICAL GYRO BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423AM 11251 858 FLT 7069 - STL - CAPTAINS ADI TUMBLED AFTER TAKEOFF. MAINTENANCE REPLACED CAPTAINS VERTICAL GYRO. (M) 2 L 7 2 4T RT A56EU 1998030500925 19980305 00925 EU 1998 3 5 RAIA980126 1 19980123 A 2932 137311D1447 TUBE BAG JETSTM JETSTM3201 1500217 EU HYD XMITTER LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 03 341TE 11072 950 STL - FLT 7469 - LOST HYDRAULIC PRESSURE ON DESCENT. REPLACED LINE TO HYDRAULIC PRESSURE TRANSMITTER. (M) 2 L 7 2 4T RT A56EU 1998030500926 19980305 00926 EU 1998 3 5 RAIA980125 1 19980123 A 3060 B40610 LEAD JETAIR JETSTM JETSTM4101 1500501 EU NR 2 PROP FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 560HK 3845 41076 JFK - FLT 7708 - NR 2 PROP HEAT FAULTED. REMOVED AND REPLACED HEATER LEAD. (M) 2 L 7 2 4T RT A41NM 1998030500927 19980305 00927 1998 3 5 TWRA9805 4 19980201 A 3416 9650184002 COMPUTER BOEING 747 747131 1384881 NM COCKPIT FAILED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 608FF 19672 TWO HOURS AFTER TAKEOFF AT 35.0 FT, ALT ALERT AND ALT ALERT PUSH TO RESET LIGHTS CAME ON, WARNING TONE SOUNDED. APPROX 1 MINUTE LATER ACRID SMELL OF HOT ELEC INSULATION WAS NOTICED BY F/E. CAPT FOUND ALT ALERT COMP C/B POPPED ON PT7. RES ET AND 20 SECONDS LATER LIGHTS REILLUMINATED, TONE SOUNDED AND C/B POPPED AGAIN APPROX 30 SECONDS LATER SAME SMELL. SME LL DISSIPATED AFTER 1 MINUTE. CHECKED AC/DC POWER AND GRD TO ALT ALER COMP. WIRES CHECKED OK PER W/D 34-12-41 PAGE 2. REMOVED AND REPLACED ALT ALERT COMPT PER MM 34-16-00 PAGE 501. OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1998030500928 19980305 00928 WP 1998 3 5 ORJA9807 1 19980114 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS ON CEILING ROWS 18-22 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AS REQUIRED. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998030500929 19980305 00929 WP 1998 3 5 ORJA9812 1 19980122 A 3350 EM1267 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHT 24, 23, 22 AND 21 WILL NOT TEST WHEN ON. USED SPARE BATTERIES, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998030500930 19980305 00930 WP 1998 3 5 ORJA9811 1 19980122 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY SEAT TRACK LIGHTING AND LEFT FWD WING EXIT SIGN CAME ON IN FLT WOULD NOT EXTINGUISHED. INSTALLED NEW CONNECTO R AT ROW 21 A/C AND REMOVED AND REPLACED EMERGENCY BATTERY CHARGER SYSTEMS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998030500931 19980305 00931 WP 1998 3 5 ORJA9813 1 19980124 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 FORWARD LEFT EMERGENCY EXIT WINDOW EMERGENCY LIGHTS OUT AND SEATS 14D, 15D, AND 16D. REMOVED AND REPLACED EMERGENCY EXI T LIGHT POWER SUPPLY AT FORWARD LEFT EMERGENCY EXIT WINDOW. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998030500932 19980305 00932 WP 1998 3 5 ORJA9806 1 19980115 A 3350 59306431 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 OVERWING EXIT EMERGENCY LIGHT AT ROW 21 A, C INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998030500933 19980305 00933 SO 1998 3 5 MASA98015 1 19980123 A 3350 3071BPE BULB EMB 120 EMB120RT SO CABIN FAILED A MASA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 289UE 120191 FLT 5559 - GNV-CLT - CREW REPORTED ONE LIGH TINOP AT ROW 9 FLOOR PROXIMITY ESCAPE PATH LIGHTING. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLA CED. (M) 2 L 7 2 4T RT A31SO 1998030500934 19980305 00934 SO 1998 3 5 MASA98008 1 19980114 A 3350 F02A250VIA FUSE EMB 120 EMB120RT SO CABIN BLOWN A MASA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 287UE 120183 FLT 5273 - TLH-MIA - PILOT REPORTED, A PORTION OF THE EMERGENCY LIGHTS ON EXITS AND FLOOR INOP. MAINTENANCE FOUND A BLO WN FUSE. REMOVED AND REPLACED FUSE, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998030500935 19980305 00935 SO 1998 3 5 MASA98012 1 19980121 A 3110 992161H111791 SWITCH EMB 120 EMB120RT SO INST PANEL SHORTED A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 07 269UE 120194 FLT 5271 - TPA-PNS - AIRCRAFT WAS ON APPROACH TO PNS WHEN THE CREW SMELLED AND SAW A SMALL AMOUNT OF SMOKE COMING FROM B EHIND THE CAPT'S INSTRUMENT PANEL. MAINTENANCE DISCOVERED THAT THE CAPT'S PUSH TO CANCEL BUTTON HAD SHORTED OUT. ITEM WAS DEFERRED PER MEL 31-50-3 AND AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE CAPT'S PUSH TO CANCEL SWITCH WAS REMOVED AND REPLACED. (M) 2 L 7 2 4T RT A31SO 1998030500936 19980305 00936 WP 1998 3 5 GTIA9800019 1 19980123 A 3820 5707638511 WATER HEATER DOUG DC9 DC931 3022065 WP LAVATORY FAILED A GTIA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 23 969ML 233350 47268 SMOKE NOTED IN LAVATORY, AIRCRAFT RIGHT. DISCOVERED SMOLDERING INSULATING MATERIAL IN TAIL COMPARTMENT. FOUND LAV WATE R HEATER INTERNAL LEAK AND SHORTED, DEFERRED PER MEL 25-12 DMI NR 492. PLACARDS INSTALLED. REMOVED AND REPLACED RIGHT LAV. WATER HEATER IAW DC-9 MM CHAPTER 38-11-4. OPERATIONAL CHECK GOOD NO LEAKS NOTED. (M) 2 L 7 2 4F A6WE 1998030500937 19980305 00937 WP 1998 3 5 GTIA9800018 1 19980123 A 3350 0611777 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941ML 1454 47131 FOUND ON 'A' CHECK, LEFT EMERGENCY OVERWING EVACUATION LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AS REQUIRED IAW DC -9 MM CHAPTER 33-53-0, OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998030500938 19980305 00938 EU 1998 3 5 DKAA98001 1 19980116 A 3230 RETRACT MECH AMD FALC20 FALCON20C5 2730107 EU LANDING GEAR ICED UP A DKAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 301R 3 AFTER TAKEOFF LANDING GEAR DOORS WOULD NOT CLOSE. CLEANED ICE AND SLUSH FROM LANDING GEAR AND CLEANED UPLOCKS. OPERATI ONAL CHECKS GOOD ON GEAR RETRACTION/EXTENSION TESTS IAW AMD MM 32-30. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A7EU 1998030500939 19980305 00939 EA 1998 3 5 98ZZZM262 1 19980109 A 2613 CONNECTOR DHAV DHC7 DHC7102 2802708 EA NR 2 ENGINE LOOSE A CICA A E UNSCHED LANDING ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 17 25AG 25 FLT 203 - MIA-PID - PILOT PERFORMED A PRECAUTIONARY SHUT DOWN OF NR 2 ENGINE BECAUSE OF HIGH ERRATIC T5. AIRCRAFT RETUR NED TO MIA AND LANDED WITH NO PROBLEM. AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR THREE ENGINE FERRY TO FLL. AN I NSPECTION OF THE AIRCRAFT FOUND T5 SYSTEM OPERATING NORMAL. TIGHTENED T5 CANNON PLUG. AIRCRAFT RELEASED FOR FLIGHT. ( M) 2 H 7 4 4T A20EA 1998030500941 19980305 00941 SO 1998 3 5 ASOA98008 1 19980126 A 2910 HYDRAULIC LINE EMB 120 EMB120RT SO LT MLG WW CHAFED A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 247AS 16746 120113 EN ROUTE DFW-ICT, RECEIVED A LOW LEVEL LIGHT ON THE GREEN HYDRAULIC SYSTEM WITH APPROPRIATE MAP AND C/W LIGHTS. CONSULT ED THE POH AND FOLLOWED THE PROCEDURE, CONTACTED MTC CNTL AND DECLARED AN EMERGENCY. RETURNED TO DFW WHERE A ZERO-FLAP LANDING WAS MADE WITHOUT FURTHER INCIDENT. DFW MAINTENANCE FOUND THE LEFT ENGINE HYDRAULIC PUMP PRESSURE LINE CHAFFED. FABRICATED NEW SECTION OF PRESSURE LINE AND PERMASWEGED IN. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998030500942 19980305 00942 SO 1998 3 5 ASOA98007 1 19980126 A 2550 INSULATION EMB 120 EMB120RT SO CARGO COMPT LOOSE A ASOA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 11 501AS 120273 IN CRUISE FLT AT 20,000 FT DFW-OKC, THE AURAL ALERT 'CABIN ALTITUDE' SOUNDED. THE CABIN WAS AT 10,000 FT AND CLIMBING A T 700 FPM. CREW PERFORMED CHECKLIST IAW/POH, DECLARED AN EMERGENCY AND DESCENDED TO 10,000 FEET AT WHICH POINT THE CABI N BEGAN TO REPRESSURIZE. LOCAL MAINTENANCE C/W THE MEL AND DEFERRED THE PRESSURIZATION, SECURING BOTH OUTFLOW VALVES. U PON ARRIVAL IN DFW, MAINTENANCE REMOVED THE SAFETY FROM THE OUTFLOW VALVES, FOUND WALL INSULATION BLOCKING OUTFLOW VALVE S FROM CLOSING AND SECURED INSULATION TO THE WALL. NO FURTHER DEFECTS WERE FOUND AND THE AIRCRAFT WAS RELEASED FOR FURT HER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998030500943 19980305 00943 NM 1998 3 5 AALA980088 1 19980116 A 5530 WEB BOEING 727 727227 1384078 NM BS 1363 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - APPROX .75 INCH CRACK IN WEB RADIUS AT UPPER CORNER ATTACH TO VERTICLE FIN RT SIDE STATION 1363. STOP DRILLED CRA CK, INSTALLED WEB ANGLE DOUBLER REPAIR PER SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 1998030500944 19980305 00944 NM 1998 3 5 AALA980087 1 19980106 A 5320 BEAM BOEING 727 727227 1384078 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - FOUND CRACK RIGHT SIDE 1183 BEAM FORWARD SIDE 24 INCHES OUTBOARD FROM VAULT DOOR FRAME STRINGER 13 AREA. INSTALLE D SERVICEABLE BEAM PREVENT MOD AND REPAIR PER BOEING BWG 65C34406 (S/B 727-53-0192). (M) 2 L 7 3 4F A3WE 1998030500945 19980305 00945 NM 1998 3 5 AALA980086 1 19980106 A 5320 WEB BOEING 727 727227 1384078 NM BS 1130-1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - RIGHT AFT LAV FLOOR WEB HAS SEVERAL AREAS OF CORROSION ON TOP SIDE. INSTALLED NEW FLOOR WEB PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1998030500946 19980305 00946 NM 1998 3 5 AALA980085 1 19980106 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - FOUND CORROSION AT SHEAR TIE STATION 680 BETWEEN STRINGER 26L AND STRINGER 27L. REPLACED SHEAR TIE PER SRM 51-10- 1. (M) 2 L 7 3 4F A3WE 1998030500947 19980305 00947 NM 1998 3 5 AALA980084 1 19980109 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - FOUND CORROSION ON SHEAR TIE STRINGER 26R AT STATION 720. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998030500948 19980305 00948 NM 1998 3 5 AALA980083 1 19980106 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 328 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 727AA 20734 TUL - FOUND STATION 328, 52LBL FLOORBEAM CORROSION. INSTALLED DOUBLER ON FLOORBEAM PER SRM 53-10-08 PAGE 49-53. (M) 2 L 7 3 4F A3WE 1998030500949 19980305 00949 NM 1998 3 5 USAASB98016 1 19980121 A 7930 1163P181 BYPASS SWITCH BOEING 737 737201 1384454 NM NR 2 ENGINE FAILED A USAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 19 245US 22751 CLT - FLT 765 - THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT ENROUTE TO CLT. CREW SHUT DOWN THE NR 2 E NGINE, ACCOMPLISHED PROCEDURES IN HANDBOOK AND DECLARED AN EMERGENCY. FLIGHT LANDED AT CLT WITHOUT FURTHER INCIDENT. T OTAL SINGLE ENGINE TIME WAS 18 MINUTES. MAINTENANCE INSPECTED THE NR 2 ENGINE MAIN OIL FILTER FOR CONTAMINATION. NONE FOUND. INSTALLED NEW OIL FILTER. ALSO, REMOVED AND REPLACED THE NR 2 ENGINE OIL FILTER BYPASS SWITCH. LEAK CHECK AND OPERATIONAL CHECK GOOD. ALL ENGINE PARAMETERS NORMAL. (M) 2 L 7 2 4F A16WE 1998030500950 19980305 00950 NE 1998 3 5 RAIA980127 2 19980123 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE NR 1 MALFUNCTIONED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 565HK 41082 75099 JFK - FLT 7749 - OIL CONTAMINATION LIGHT ILLUMINATED. INSPECTED CHIP DETECTOR FOUND NO DEBRIS, OBTAINED SOAP SAMPLE. R EMOVED ENGINE FOR INSPECTION PER SOAP, SOAP RECOMMENDATIONS 01/27. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1998030500951 19980305 00951 NE 1998 3 5 TWRA9802 2 19980113 A 7321 7590002 FUEL CONTROL BOEING 747 747131 1384881 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE MALFUNCTIONED A TWRA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 EA 15 608FF 19672 662217 WHILE CRUISING AT F/L 330, SMOOTH AIR, NR 3 ENGINE FLAMED OUT, FUEL PANEL SETTING WAS TANK TO ENGINE. USED TOWER AIR PR OCEDURES FOR INFLIGHT START ENGINE RESTARTED. ALL PARAMETERS NORMAL. PERFORMED NR 3 ENGINE FLAMEOUT TROUBLESHOOTING PR OCEDURES IAW MM 71-00-42 PAGE 118 AND 119 WINDMILL INSPECTION IAW MM 72-00-00 PAGE 682 P/Q. OPS AND LEAK CHECK OK. REM OVED AND REPLACED FUEL CONTROL MM 73-11-01. OPS AND LEAK CHECK OK. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998030500952 19980305 00952 NE 1998 3 5 TWAA9801304 2 19980122 A 7261 80465901 OIL PUMP BOEING 747 747131 1384881 NM PWA JT9 JT9D7AH 52054 NE NR 1 ENGINE FAILED A TWAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CE 05 93108 19674 4103 SNN - FLT 883 - ON DESCENT 33,000 FT, OIL PRESS IND FLUX DOWN TO ZERO PSI WITH THROTTLE AT IDLE. WITH ENG AT IDLE ON FI NAL OIL PRESS LIGHT ON. ENGINE SHUT DOWN AFTER LANDING. NR 1 ENGINE, REPLACED OIL PUMP. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998030500953 19980305 00953 NE 1998 3 5 EIAA98005 2 19980129 A 7230 771841 FAN BLADES BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE NR 1 ENGINE BENT A EIAA O OTHER C F.O.D. AP APPROACH 1 NM 09 470EV 20653 JFK - APPROACH INTO JFK RUNWAY 22L, APPROXIMATELY 50-100 FEET, HAD BIRD STRIKE IN NR 1 ENGINE. LANDED WITHOUT INCIDENT, WITH AN OUTSIDE AIR TEMP OF 42 DEGREES F. REMOVED AND REPLACED FIVE PAIRS OF FAN BLADES PER MM 72-31-02. INSPECTED NR 1 ENGINE FOR BIRD INGESTION, AND FOUND NO CORE ENGINE DAMAGE. PERFORMED ENGINE RUN NO DEFECTS NOTED. SUBSEQUENTLY ENG INE WAS CHANGED FOR A OIL LEAK THAT WAS NOT RELATED TO THE BIRD STRIKE. 2 L 7 4 4F 4 F A20WE E20EA 1998030500954 19980305 00954 NM 1998 3 5 TSAA9851080 1 19980202 A 5347 TRACK BOEING 737 7372M6C 1384708 NM CARGO COMPT CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPC CHECK, FOUND CORROSION ON RIGHT OUTBOARD TRACK AT DOOR SILL (AFT CARGO PIT). REPAIRED DAMAGE BY REPLACING TR ACK PER SRM 51-10-1. (M) 2 L 7 2 4F RT A16WE 1998030500955 19980305 00955 NM 1998 3 5 TSAA9851081 1 19980202 A 5320 SILL BOEING 737 7372M6C 1384708 NM CARGO DOOR CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPC CHECK, FOUND CORRODED CHORD ON AFT CARGO PIT DOOR SILL, TOP OF FRAME. REPAIRED DAMAGE BY REPLACING CHORD PER SRM 51-10-1. (M) 2 L 7 2 4F RT A16WE 1998030500956 19980305 00956 NM 1998 3 5 TSAA9853082 1 19980202 A 5312 BULKHEAD BOEING 737 7372M6C 1384708 NM BS 294 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPCP CHECK, FOUND EXFOLIATION CORROSION ON INTERIOR FUSELAGE LOWER LOBE BULKHEAD STATION 294, STRINGER 26L. CORR OSION IS LEVEL 2, CUTOUT DAMAGED AREA AND REPAIRED PER SRM 53-10-31 AND FASTENERS PER SRM 51-30-02. (M) 2 L 7 2 4F RT A16WE 1998030500957 19980305 00957 NM 1998 3 5 TSAA9857083 1 19980202 A 5730 SKIN BOEING 737 7372M6C 1384708 NM LT MAIN WING BOX CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPCP CHECK, FOUND CORROSION AT NR 6 RT AND NR 7 LEFT MAIN WING BOX LOWER SKIN ACCESS PANEL CUTOUT LIP. REPAIRED PER ECO 2869. (M) 2 L 7 2 4F RT A16WE 1998030500958 19980305 00958 NM 1998 3 5 TSAA9855085 1 19980202 A 5512 SKIN BOEING 737 7372M6C 1384708 NM HORIZ STAB CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPC CHECK, FOUND CRACKS AT HORIZONTAL STABILIZER LOWER SKIN ACCESS PANEL AT STATION 99.1 RT SIDE. REPAIRED PER E CO 2870 R2. (M) 2 L 7 2 4F RT A16WE 1998030500959 19980305 00959 NM 1998 3 5 TSAA9853086 1 19980202 A 5315 FLOORBEAM BOEING 737 7372M6C 1384708 NM BS 867 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPC CHECK, FOUND CORROSION AT SECTION 43 AND 46 FLOORBEAM LOWER CHORD AT BS 867, LBL 18.6 AND BS 480, RBL 50-55. REPAIRED PER EO 2874. (M) 2 L 7 2 4F RT A16WE 1998030500960 19980305 00960 NM 1998 3 5 TSAA9857087 1 19980202 A 5730 PANEL BOEING 737 7372M6C 1384708 NM WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPC CHECK, FOUND CORROSION AT WING LOWER SKIN PANEL, FUEL ACCESS DOOR CUTOUT LIP NR 9 RT. CORROSION IS LEVEL 2. REPAIRED PER ECO 2871. (M) 2 L 7 2 4F RT A16WE 1998030500961 19980305 00961 NM 1998 3 5 TSAA9853088 1 19980202 A 5320 FRAME BOEING 737 7372M6C 1384708 NM CARGO DOORWAY CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPC CHECK, FOUND AFT CARGO DOOR INBOARD DOOR SILL FRAME CRACKED. REPAIRED PER ECO 1700 R-4. (M) 2 L 7 2 4F RT A16WE 1998030500962 19980305 00962 NM 1998 3 5 TSAA9852089 1 19980202 A 5230 CROSSBEAM BOEING 737 7372M6C 1384708 NM CARGO DOOR CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 FORWARD CARGO DORO CROSSBEAM CRACKED. REPAIRED AREA PER ECO 2875 R1 (WEB). REPAIRED LOWER FRAME CORNER PER SRM 51-10-1 . (M) 2 L 7 2 4F RT A16WE 1998030500963 19980305 00963 EU 1998 3 5 SIMA980409 1 19980209 A 5313 S5367140030002 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THAT STRINGER 21 LEFT BETWEEN FRAMES 39 AND 40 CORRODED. MAINTENAN CE REPAIRED STRINGER 21 LEFT IAW SRM 53-00-00 FIG 428. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500964 19980305 00964 EU 1998 3 5 SIMA980408 1 19980209 A 3830 S5368201500200 VENTURI TUBE AEROSP ATR42 ATR42300 8680920 EU LAVATORY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE DISCOVERED, THE TOILET VENTURI TUBE ASSY CORRODED BETWEEN FRAME 40 AND 41. M AINTENANCE REMOVED AND REPLACED VENTURI IAW SRM 51-25-02. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500965 19980305 00965 EU 1998 3 5 SIMA980407 1 19980209 A 5320 S5367131829201 WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED, THE WEB AT STRINGER 14 RT BETWEEN FRAMES 39 AND CORRODED AND THE CR EASE BEAM WEB BETWEEN FRAMES 35 AND 36 CORRODED ON RIGHT SIDE. MAINTENANCE REMOVED AND INSTALLED BOTH WEBS IAW SRM 51-2 5-03. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500966 19980305 00966 EU 1998 3 5 98ZZZM263 1 19980209 A 5320 S5367121721101 WEB AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED, THE WEB AT STRINGER 14 RT BETWEEN FRAMES 39 AND CORRODED AND THE CR EASE BEAM WEB BETWEEN FRAMES 35 AND 36 CORRODED ON RIGHT SIDE. MAINTENANCE REMOVED AND INSTALLED BOTH WEBS IAW SRM 51-2 5-03. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500967 19980305 00967 EU 1998 3 5 WIMA980406 1 19980209 A 5315 S5367240601261 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THAT FLOORBEAM 36 AND 40 WERE CORRODED. MAINTENANCE REMOVED AND REP LACED FLOORBEAM 36 IAW SRM 51-25-01. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-61-40 FIGURE 412. A/C WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500968 19980305 00968 EU 1998 3 5 98ZZZM264 1 19980209 A 5315 S5367240901061 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THAT FLOORBEAM 36 AND 40 WERE CORRODED. MAINTENANCE REMOVED AND REP LACED FLOORBEAM 36 IAW SRM 51-25-01. MAINTENANCE REPAIRED FLOORBEAM 40 IAW SRM 53-61-40 FIGURE 412. A/C WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500969 19980305 00969 EU 1998 3 5 SIMA980405 1 19980209 A 5320 S5367800820002 SUPPORT AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT FLOOR SUPPORT BETWEEN FRAMES 39 AND 41 CORRODED AND THE LEFT FL OOR SUPPORT BETWEEN 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOOR SUPPORTS IAW SRM 51-25-03. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500970 19980305 00970 EU 1998 3 5 98ZZZM265 1 19980209 A 5320 S5367800821602 SUPPORT AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT FLOOR SUPPORT BETWEEN FRAMES 39 AND 41 CORRODED AND THE LEFT FL OOR SUPPORT BETWEEN 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOOR SUPPORTS IAW SRM 51-25-03. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500971 19980305 00971 EU 1998 3 5 SIMA980404 1 19980209 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS WERE CORRODED. THE LEFT OUTBOARD, LEFT AF T INBOARD, RIGHT AFT OUTBOARD, RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-25-04. A/C W AS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500972 19980305 00972 EU 1998 3 5 98ZZZM266 1 19980209 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS WERE CORRODED. THE LEFT OUTBOARD, LEFT AF T INBOARD, RIGHT AFT OUTBOARD, RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-25-04. A/C W AS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500973 19980305 00973 EU 1998 3 5 98ZZZM267 1 19980209 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING CPCP-4 INSPECTION MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS WERE CORRODED. THE LEFT OUTBOARD, LEFT AF T INBOARD, RIGHT AFT OUTBOARD, RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-25-04. A/C W AS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500974 19980305 00974 EU 1998 3 5 SIMA980403 1 19980209 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CARGO COMPT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURNG CPCP-4 INSPECTION MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS WERE CORRODED. THE LEFT AFT OUTBOARD, LEFT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT AFT CARGO, RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500975 19980305 00975 EU 1998 3 5 98ZZZM268 1 19980209 A 5347 S53678001212 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CARGO COMPT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURNG CPCP-4 INSPECTION MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS WERE CORRODED. THE LEFT AFT OUTBOARD, LEFT AFT INBOARD, RIGHT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT AFT CARGO, RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500976 19980305 00976 EU 1998 3 5 SIMA980402 1 19980209 A 2731 S2738197100400 ROD AEROSP ATR42 ATR42300 8680920 EU LT ELEVATOR TAB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING MBV-1 INSPECTION MAINTENANCE REPORTED THE LEFT ELEVATOR TRIM TAB CONTROL ROD WAS CORRODED. MAINTENANCE REM OVED AND REPLACED THE LEFT ELEVATOR TRIM CONTROL ROD IAW JIC 273141, RAI 10000-002. AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998030500977 19980305 00977 EU 1998 3 5 SIMA980401 1 19980209 A 5311 S536713112005 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 423MQ 030 SAW - DURING HMBV-1 INSPECTION REPORTED THAT FRAME 37 RIGHT AT FLOOR LEVEL WAS CORRODED. MAINTENANCE REPAIRED FRAME 37 RIGHT IAW SRM 53-67-70 FIGURE 402. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500978 19980305 00978 EU 1998 3 5 SIMA980382 1 19980207 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 422MQ 11747 0028 SAW - DURING PS-2 CHECK, MAINTENANCE DISCOVERED EMERGENCY LIGHT BATTERY PACK AT LOCATION 29 WL WAS INOP. MAINTENANCE RE MOVED AND REPLACED BATTERY PACK AT LOCATION 29WL. OPS CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998030500979 19980305 00979 EU 1998 3 5 SIMA980381 1 19980207 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AE 340B380 DFW - FLT 3699 - LEFT OVERHEAD EMERGENCY EXIT SIGN INOP. RESECURED OVERHEAD EMERGENCY EXIT SIGN AT 8A. OPERATIONAL CHE CKED GOOD IAW SAAB MM 336000 WITH NO OTHER DEFECTS NOTED. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998030500980 19980305 00980 EU 1998 3 5 SIMA980391 1 19980208 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 380AE 340B380 DFW - FLT 3880 - EMERGENCY LIGHT FLICKERS ON AND OFF AT ROW 8. MAINTENANCE FOUND BAD TERMINAL END ON EMERGENCY LIGHT AS SY. REPLACED LIGHT ASSEMBLY AND ALSO REPLACED POWER SUPPLY 23 LN AS PRECAUTIONARY. PERFORMED OPERATIONAL CHECK SATISFA CTORILY. RETURNED A/C TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998030500981 19980305 00981 NM 1998 3 5 MASA98016 1 19980125 A 3350 MS25231316 LAMP DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 ON INTERIOR LIGHT OPS CHECK, FOUND THE FARTHEST AFT CEILING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATED. MAINTENANCE FOU ND A BLOWN LIGHT BULB. REMOVED AND REPLACED BULB AND OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998030500982 19980305 00982 NM 1998 3 5 MASA98018 1 19980127 A 3350 MS25231316 LAMP DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 446YV 446 FLT 7710 - RAP-DEN - UPON ARRIVAL IN DEN, CREW REPORTED THE FORWARD UPPER EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998030500983 19980305 00983 SO 1998 3 5 MASA98017 1 19980126 A 3350 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A MASA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 340JS 120172 FLT 5548 - EYW-TPA - ON PREFLIGHT INSPECTION, PILOT REPORTED ONE SECTION OF FLOOR PATH EMERGENCY LIGHTING FAILED TO TEST . MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY. OPS CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M ) 2 L 7 2 4T RT A31SO 1998030500985 19980305 00985 WP 1998 3 5 HALA9800039 1 19980208 A 3610 PRESS CONTROL DOUG DC10 DC1010 3022110 WP NR 1 ENGINE FAILED A HALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 13 171AA 46906 HNL - FLT 03 - NR 1 ENGINE MANIFOLD FAIL (RED) LAMP ILLUMINATED AT TOP OF DESCENT WHEN THROTTLES WERE CLOSED TO IDLE. T EMP 210 DEGREES CELSIUS LIGHT EXTINGUISHED IN ABOUT 5 SECONDS AFTER NR 1 BLEED SWITCH TURNED OFF. (M) 2 L 7 3 4F A22WE 1998030500986 19980305 00986 NM 1998 3 5 EISA98011 1 19980201 A 2612 CONNECTOR BOEING 727 727251 138408H NM NR 2 FIREWALL WATER CONTAM A EISA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 263US 19982 CLIMBING THROUGH FL 240 FIREBELL CAME ON, SILENCED BELL NO OTHER INDICATIONS NOTED, BELL SOUNDED NUMEROUS TIMES DURING F LIGHT. REMOVED MOISTURE, CLEANED DRIED NR 2 ENGINE FIREWALL, DISCONNECT 3D1482J FIRE DETECTION SYSTEM, TEST NORMAL IAW B727 MM 27-00-00. (M) 2 L 7 3 4F A3WE 1998030500987 19980305 00987 NM 1998 3 5 EISA98007 1 19980130 A 2612 CONNECTOR BOEING 727 727251 138408H NM NR 1 FIREWALL DIRTY A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 263US 19982 IN FLIGHT FIRE BELL SOUNDED AND NO LIGHT ILLUMINATED. DISCONNECTED NR 1 AND NR 3 FIREWALL CONNECTORS, CLEANED CONTACTS, APPLIED DIELECTRIC SILICONE AND RECONNECTED. ALSO, SEALED CONNECTOR ON NR 2 ENGINE. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1998030500988 19980305 00988 NM 1998 3 5 98ZZZM269 1 19980130 A 2612 CONNECTOR BOEING 727 727251 138408H NM NR 3 FIREWALL DIRTY A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 263US 19982 IN FLIGHT FIRE BELL SOUNDED AND NO LIGHT ILLUMINATED. DISCONNECTED NR 1 AND NR 3 FIREWALL CONNECTORS, CLEANED CONTACTS, APPLIED DIELECTRIC SILICONE AND RECONNECTED. ALSO, SEALED CONNECTOR ON NR 2 ENGINE. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1998030500990 19980305 00990 WP 1998 3 5 GAIA9816 1 19980209 A 5320 5922241 CHANNEL DOUG DC9 DC915F 3022037 WP BS 776 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 47055 DURING INSPECTION OF CORROSION TASK 58-53301 WHILE AIRCRAFT WAS IN C-CHECK, LEVEL 2 CORROSION WAS FOUND ON A FLOOR CHANN EL AT FUSELAGE STATION 776 LBL 33. THE CHANNEL WAS REPAIRED IAW KITTY HAWK EA D9-53-051. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998030500991 19980305 00991 WP 1998 3 5 GAIA9815 1 19980209 A 5347 4924374 TRACK DOUG DC9 DC915F 3022037 WP BS 383 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 383 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998030500992 19980305 00992 WP 1998 3 5 98ZZZM271 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 428 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998030500993 19980305 00993 WP 1998 3 5 98ZZZM272 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 516 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998030500994 19980305 00994 WP 1998 3 5 98ZZZM273 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 602 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998030500995 19980305 00995 WP 1998 3 5 98ZZZM274 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 634 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998030500996 19980305 00996 WP 1998 3 5 98ZZZM275 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 695 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998030500997 19980305 00997 WP 1998 3 5 98ZZZM276 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 571 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998030500998 19980305 00998 WP 1998 3 5 98ZZZM277 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 568 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998030500999 19980305 00999 NM 1998 3 5 CKSA98083 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, INTERGRAN CORROSION ON FLOOR SUPPORT (ATTACHED TO T-ANGLE) AT BS 1920 RB L 39. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUT OUT CORRODED FLOOR SUPPORT SECTION IAW B747 SRM 51 -40-3. INSTALLED FLOOR SUPPORT AS PER B747 SRM 53-10-23. CORROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5. NON-ROUTI NE TASK CARD NUMBER 14781. 2 L 7 4 4F A20WE 1998031200111 19980312 00111 NM 1998 3 12 98ZZZX1010 1 19980129 A 6710 900C3010042105 BEARING DOUG MD900 MD900 3027375 NM M/R SHAFT BINDING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 821 0022 90000012 BALL SLIDER BEARING BINDING ON MAIN ROTOR SHAFT ASSY DURING COLLECTIVE MOVEMENT. REPLACED WITH NEW UNIT, CORRECTED PROB LEM. 1 G 7 2 3U NC H19NM 1998031200112 19980312 00112 NM 1998 3 12 98ZZZX1011 1 19980126 A 6710 900C3820021105 SERVO ACTUATOR DOUG MD900 MD900 3027375 NM M/R CONTROL BINDING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1904 0035 90000012 M/R CONTROL SERVO BINDING ON DOWN STROKE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998031200113 19980312 00113 EU 1998 3 12 DKAA98003 1 19980209 A 3231 A2238012 SWITCH AMD FALCON FALCON20 2730103 EU LT MLG DOOR FAILED A DKAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 192R 026 192 GEAR DOORS WOULD NOT CLOSE AFTER TAKEOFF. CLEANED AND ADJUSTED LT MLG DOOR ACTUATOR SWITCH. OPERATIONAL CHECKS GOOD. A IRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A7EU 1998031200114 19980312 00114 SO 1998 3 12 98ZZZX1012 2 19980212 A 8520 SA630R26 ROD BEARING CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO LT ENG NR 6 CYL FAILED A T4CA O OTHER O OTHER CR CRUISE 1 SO 17 269JH 1314 402B1213 275115R LEFT ENGINE SPUN NR 6 CYLINDER ROD BEARING ON TRIP BACK FROM NASSAU. ENGINE WAS OVERHAULED BY T.W. SMITH ENGINE. THE E NGINE HAD 1,313.9 HOURS SINCE OVERHAUL. 1 L 7 2 3O 3 O A7CE E8CE 1998031200117 19980312 00117 NM 1998 3 12 98ZZZX1015 1 19980126 A 7160 900CF330001101 ACTUATOR DOUG MD900 MD900 3027375 NM INLET DOOR FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 26 54 90000012 INLET DOOR LINEAR ACTUATOR FAILED IN OPEN POSITION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998031200118 19980312 00118 WP 1998 3 12 VJ9800032 1 19980304 A 3231 39567851 LINK ASSY DOUG DC9 DC932 3022066 WP LT NLG DOOR MALFUNCTIONED A VJ6A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 11 914VV 47486 DURING CLIMB, EXTENDED AND RETRACTED NLG BECAUSE OF NOISE AND VIBRATION. REPLACED LT NLG DOOR LINK ASSEMBLY, PERFORMED GEAR RETRACTION AND OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998031200119 19980312 00119 NM 1998 3 12 VJ9800033 1 19980228 A 3350 087691 LAMPHOLDER BOEING 737 7372L9 1384497 NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 11 737Q 21279 EMERGENCY FLOOR PATH LIGHT R-14 INOP. REPLACED LAMP HOLDER, BULB AND COVER IAW MM 33-50-01. 2 L 7 2 4F RT A16WE 1998031200120 19980312 00120 NM 1998 3 12 VJ9800034 1 19980301 A 3350 BR9279106 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 11 467AT 22055 RIGHT OVERWING EMERGENCY EXIT LIGHT BROKEN. REPLACED LIGHT ASSEMBLY IAW MM 33-50-01, OPS CHECKED OK. 2 L 7 2 4F A16WE 1998031200121 19980312 00121 WP 1998 3 12 CALA9800373 1 19980304 A 5755 NRC6052508 SKIN DOUG DC10 DC1010 3022110 WP NR 5 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LOWER SURFACE OF RT WING NR 5 SPOILER DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1998031200122 19980312 00122 WP 1998 3 12 CALA9800374 1 19980304 A 5755 NRC6047507 SKIN DOUG DC10 DC1010 3022110 WP NR 1 SPOILER DISBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LT WING NR 1 SPOILER CORRODED AND DISBONDED AT UPPER SURFACE OUTBOARD HINGE. THE SPOILER WAS REMOVED A ND REPLACED. 2 L 7 3 4F A22WE 1998031200123 19980312 00123 WP 1998 3 12 CALA9800375 1 19980304 A 5753 SKIN DOUG DC10 DC1010 3022110 WP LT TE FLAP BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LT INBOARD FLAP UPPER SURFACE BULGED WITH POPPED AND PULLING FASTENERS. THE LT INBOARD FLAP WAS REMOVE D AND REPLACED. 2 L 7 3 4F A22WE 1998031200124 19980312 00124 WP 1998 3 12 CALA9800376 1 19980304 A 5730 SKIN DOUG DC10 DC1010 3022110 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN LT WING LEADING EDGE SKIN AT NR 5 LEADING EDGE SLAT INBOARD TRACK CUTOUT. REMOVED FA STENER IAW SRM 51-31-01. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1998031200125 19980312 00125 WP 1998 3 12 CALA9800377 1 19980304 A 5753 SKIN DOUG DC10 DC1010 3022110 WP RT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A GOUGE IN RT WING OUTBOARD FLAP LOWER SKIN APPROXIMATELY 12 OUTBOARD OF OUTBOARD HINGE. THE GOUGED AR EA WAS CUT OUT IAW SRM 57-00-01. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-00-01, 51-21-01, 51-31-01, AND 51-41-01. 2 L 7 3 4F A22WE 1998031200126 19980312 00126 WP 1998 3 12 CALA9800378 1 19980304 A 5720 ANGLE DOUG DC10 DC1010 3022110 WP WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND ANGLE LOCATED BELOW AND INBOARD OF UPPER WING TRAILING EDGE MOST INBOARD AFT PANEL CORRODED. THE ANGLE WAS REMOVED IAW SRM 51-31-01. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998031200127 19980312 00127 WP 1998 3 12 CALA9800379 1 19980304 A 5755 SKIN DOUG DC10 DC1010 3022110 WP NR 4 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 2 INCH CRACK WITH DENT IN UPPER SURFACE OF RT WING NR 4 SPOILER. THE CRACKED AND DENTED AREA WAS CUT OUT, A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-71-00. 2 L 7 3 4F A22WE 1998031200128 19980312 00128 WP 1998 3 12 CALA9800380 1 19980305 A 5753 SKIN DOUG DC10 DC1010 3022110 WP RT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A DENT NEAR INBOARD LOWER CORNER OF RT INBOARD FLAP UPPER SKIN. THE DENTED AREA WAS CUT OUT IAW SRM 57 -00-01, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01. 2 L 7 3 4F A22WE 1998031200129 19980312 00129 WP 1998 3 12 CALA9800381 1 19980305 A 5753 FLAP DOUG DC10 DC1010 3022110 WP RT TE FLAP SPLIT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND INBOARD EDGE OF RT INBOARD FLAP TRAILING EDGE SPLIT. THE AREA WAS SANDED AND A FIBERGLASS OVERLAY WAS APPLIED IAW SRM 51-43-00. 2 L 7 3 4F A22WE 1998031200130 19980312 00130 WP 1998 3 12 CALA9800382 1 19980305 A 5311 FRAME DOUG DC10 DC1010 3022110 WP CARGO COMPT PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A HOLE ON CENTER CARGO AFT FRAME CUTOUT. THE HOLE WAS ROUNDED OUT IAW SRM 53-00-01. A DOUBLER WAS FAB RICATED AND INSTALLED IAW SRM 53-00-01 AND 51-21-01. 2 L 7 3 4F A22WE 1998031200131 19980312 00131 WP 1998 3 12 CALA9800383 1 19980305 A 5320 BRACKET DOUG DC10 DC1010 3022110 WP R1 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN WALL BRACKET AT R-1 DOOR FORWARD FRAME. A NEW BRACKET WAS FABRICATED AND INSTALLED I AW SRM 53-00-01. 2 L 7 3 4F A22WE 1998031200132 19980312 00132 WP 1998 3 12 CALA9800384 1 19980305 A 5711 SPAR CAP DOUG DC10 DC1010 3022110 WP WS 433-500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT WING REAR SPAR LOWER CAP CORRODED AROUND PLATE NUTS ON UPPER SURFACE FROM STA XORS 433 TO 500. A RE PAIR WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998031200133 19980312 00133 WP 1998 3 12 CALA9800385 1 19980305 A 5411 FRAME DOUG DC10 DC1010 3022110 WP NR 2 NACELLE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 4 AND 2 INCH CRACK ON CENTER FRAME ON LT SIDE OF NR 2 ENGINE INLET INSIDE PANEL NR 363EL. THE CRACKS WERE STOP DRILLED IAW SRM 51-90-00. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 54-00-01 AND 51-21-01. 2 L 7 3 4F A22WE 1998031200134 19980312 00134 NE 1998 3 12 9803605644 2 19980301 A 7530 45100 STATOR ALT BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 544US 26491 716476 DURING TAKEOFF ROLL, THE NR 2 ENGINE PRIMARY CONTROL MESSAGE ANUNCIATED AND THERE WAS NO EPR INDICATION. TAKEOFF WAS AB ORTED AT 10 KNOTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 EEC STATOR ALTERNATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1998031200135 19980312 00135 NE 1998 3 12 9803612296 2 19980302 A 7200 ENGINE BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE CENTER FAILED A NWAA E C D ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 296US 21788 700779 DURING TAKEOFF ROLL AT 90 KNOTS, THE CENTER ENGINE STALLED WITH ASSOCIATED DROP IN N1 AND EPR INDICATIONS. CREW ABORTED TAKEOFF, SHUT DOWN THE CENTER ENGINE, AND RETURNED TO THE GATE. A CONTAINED FAILURE OF THE CENTER ENGINE HAD OCCURRED. MAINTENANCE REPLACED THE CENTER ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1998031200136 19980312 00136 WP 1998 3 12 9803629906 1 19980302 A 2613 TEMP SENSORS DOUG DC9 DC931 3022065 WP TAIL COMPT FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 956N 47252 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO GCM AND LANDED WITHOUT INCIDE NT. MAINTENANCE REPLACED BOTH THE LEFT AND RIGHT TAIL COMPARTMENT TEMPERATURE SENSORS. OPERATIONAL CHECK NORMAL ON GRO UND. 2 L 7 2 4F A6WE 1998031200137 19980312 00137 WP 1998 3 12 9803639906 1 19980302 A 2613 TEMP SENSOR DOUG DC9 DC931 3022065 WP TAIL COMPT DIRTY A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 956N 47252 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO GCM AND LANDED WITHOUT INCIDE NT. MAINTENANCE OPERATED ENGINES AND INSPECTED PNEUMATIC DUCTING IN AFT TAIL CONE AREA FOR LEAKS. NO LEAKS WERE FOUND. CLEANED LEFT AND RIGHT TEMPERATURE SENSORS AS A PRECAUTION. 2 L 7 2 4F A6WE 1998031200138 19980312 00138 WP 1998 3 12 9803649909 1 19980303 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ON CATWALK AND AT INTERIOR TAIL CONE HANDLE INOPERATIVE. REP LACED BATTERIES IN BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031200139 19980312 00139 NE 1998 3 12 9803652717 2 19980303 A 7261 B7670 MAG PLUG BOEING 727 7272S7 138407Z NM PWA JT8 JT8D17 52049 NE RT ENGINE DAMAGED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 721RC 22492 707908 DURING CLIMB AT 10,000 FEET, THE NR 3 ENGINE OIL PRESSURE AND OIL QUANTITY INDICAITONS DROPPED TO ZERO WITH ASSOCIATED L OW OIL PRESSURE LIGHT ILLUMINATION. CREW SHUT DOWN THE NR 3 ENGINE. AIRCRAFT RETURNED TO GEG AND LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE INSPECTED THE MAIN OIL FILTER, MAG PLUGS, AND REPLACED THE AFT BEARING MAG PLUG. 2 L 7 3 4F 4 F A3WE E2EA 1998031200140 19980312 00140 EU 1998 3 12 9803663218 1 19980213 A 3231 201122008 UPLOCK AIRBUS 320 A320211 3930320 EU RT MLG DOOR MALFUNCTIONED A NWAA K NONE N FALSE WARNING AP APPROACH 1 GL 01 318US 206 DURING APPROACH FOLLOWING LANDING GEAR EXTENSION, RIGHT MAIN GEAR DOOR INDICATED OPEN. RECYCLED LANDING GEAR RECEIVED T HE SAME INDICAITON AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GEAR DOOR UPLOCK ASSEMBLY, OPERATIONAL C HECK OK. 2 L 7 2 4F RT A28NM 1998031200141 19980312 00141 NM 1998 3 12 9803672299 1 19980303 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 299US 22153 DURING PREFLIGHT, FOUND RIGHT AFT EXIT DOOR EMERGENCY LIGHT AND LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACE D BOTH BATTERY PACKS, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998031200142 19980312 00142 NM 1998 3 12 9803685636 1 19980218 A 2421 729825J IDG BOEING 757 757251 1384970 NM LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 536US 26670 7545 26483 LEFT GENERATOR WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT INTEGRATED DRIVEN GENERATOR UNIT WITH A SERVICEABLE PART. RUN-UP AND SYSTEM TEST WERE SA TISFACTORY. 2 L 7 2 4F RT A2NM 1998031200143 19980312 00143 NM 1998 3 12 9803695502 1 19980219 A 2424 734284A GCU BOEING 757 757251 1384970 NM LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 502US 39204 28268 32191 LEFT ENGINE GENERATOR DROPPED OFF LINE ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAI NTENANCE REPLACED THE GENERATOR CONTROL UNIT WITH A SERVICEABLE PART. RUN-UP AND SYSTEM CHECK WAS SATISFACTORY. 2 L 7 2 4F RT A2NM 1998031200144 19980312 00144 SO 1998 3 12 COMA9810053 1 19980303 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 168CA 17394 1133 120168 CABIN DOOR EMERGENCY EXIT SIGN IS INOPERABLE, EMERGENCY FLOOR PATH LIGHTING TO ROW 3 IS INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4T RT A31SO 1998031200145 19980312 00145 SO 1998 3 12 COMA9810054 1 19980304 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 162CA 120150 EMERGENCY EXIT SIGN AT SEAT 5A IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998031200146 19980312 00146 EA 1998 3 12 COMA9860050 1 19980303 A 5610 NP1393211 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 927CA 5122 7031 PILOTS WINDSHIELD SHATTERED DURING CRUISE FLIGHT AT 35,000 FT. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1998031200147 19980312 00147 WP 1998 3 12 UPS98825982 1 19980303 A 5720 36403052 ANGLE DOUG DC8 DC871F 302199D WP WS 408 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, RT WING T/E SPAR AT XW 408 LOWER SPLICE ANGLE IS EXFOLIATED. REMOVED AND REPLACED SPLICE ANGLE IAW S RM 51-3-0. 2 L 7 4 4F RT 4A25 1998031200148 19980312 00148 EU 1998 3 12 QXEA9800145 1 19980301 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 LIGHT BULB BURNT OUT IN EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR. MAINTENANCE REPLACED BULB AND FUNCTION TESTED. 2 L 7 2 4F RT A20EU 1998031200149 19980312 00149 EU 1998 3 12 QXEA9800146 1 19980129 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 FRAME 18075 AT STRINGER 58 IS CHAFED MORE THAN 50 PERCENT. BLENDED CHAFED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EA 4-53-339. 2 L 7 2 4F RT A20EU 1998031200165 19980312 00165 EU 1998 3 12 QXEA9800162 1 19980103 A 5320 FASTENER FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 482US 11231 CASTELLATION AT STRINGER 47 FRAME 15205 HAS TWO HI-LOKS INSTALLED WHERE ACCESS IS ACCESSABLE. HI- LOKS CORRECTLY INSTAL LED IAW FOKKER SRM 51-30-02 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998031200218 19980312 00218 EU 1998 3 12 QXEA9800217 1 19980113 A 5350 FAIRING FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 DENT 2.5 BY 2.0 AND .092 DEEP ADJACENT TO FRAME 10775 AND RIB BL13456 ON LOWER FAIRING DENT HAS CREASE IN THE BOTTOM. F ABRICATED AND INSTALLED REPAIR IAW FOKKER SRM 53-02-17 FIGURE 1, PAGE 3. 2 L 7 2 4F RT A20EU 1998031200220 19980312 00220 EU 1998 3 12 QXEA9800219 1 19980113 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 11000 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 482US 11231 DENT 3.2 X .75 WITH A SHARP CREASE IN THE BOTTOM AT STATION 11000 AND BETWEEN BL 1147L AND BK1002L DENT IS .103 DEEP. R EPAIRED DENT IAW FOKKER SRM 53-02-12 FIGURE 1, PAGE 3 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998031200231 19980312 00231 NM 1998 3 12 QXEA9800230 1 19980209 A 5320 BRACKET DHAV DHC8 DHC8102 2809003 NM LT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 FIVE BRACKETS THAT RETAIN LEFT HAND MAIN LANDING GEAR GRAVEL GUARD ARE SEVERLY CHAFED. INSTALLED BRACKETS IAW DHC-8 SRM 51-40-00. INSTALLED CAM LOC RECEPTICALS IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1998031200232 19980312 00232 NM 1998 3 12 QXEA9800231 1 19980212 A 5400 BRACKET DHAV DHC8 DHC8102 2809003 NM NACELLE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 821PH 104 NACELLE AFT WALL GRAVEL GUARD MOUNT BRACKETS CHAFED. REPAIRED IAW HORIZON EA 9-54-154. 2 H 7 2 4T RT A13NM 1998031200233 19980312 00233 WP 1998 3 12 98FDEA00148 1 19980303 A 2620 FIRE BOTTLE DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE DISCHARGED A FDEA F ACTIVATE FIRE EXT. O OTHER IN INSP/MAINT 1 SO 25 315FE 48313 ON PRE FLT CK, FOUND NR 2 ENG FIRE AGT 2 LOW LIGHT CAME ON. ON CK FOUND NR 2 ENG NR 2 BOTTLE DISCHARGE CARTRIDGE DISCHA RGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE AND CARTRIDGE AS PER M/M 26-21-02 AND M/M 26-21-01. ALSO, WIRING AND AGENT DISCHARGE S/W (S1-164) FUNCTION OK. CARTRIDGE (P/N 876296). 2 L 7 3 4F RT A22WE 1998031200234 19980312 00234 NM 1998 3 12 98FDEA00149 1 19980225 A 5754 SKIN BOEING 727 727233 138408A NM NR 8 LE SLAT CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 271FE 22036 RT WING NR 8 L/E SLAT, LOWER SKIN TANG BELOW INBD TRACK ATTACH CRACKED AND RIVETS PULLED. ACCOMPLISHED REPAIR ON RT WIN G NR 8 L/E SLAT FOR CRACKED LWR SKIN TANG BELOW INBOARD TRACK PER AA 7-5750-29381 AND AA SRM 57-50-1 PGS 7A AND 7B. 2 L 7 3 4F RT A3WE 1998031200235 19980312 00235 NM 1998 3 12 98FDEA00150 1 19980302 A 5542 SKIN BOEING 727 727227 1384078 NM RUDDER DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 TAIL, UPPER RUDDER NR 2 RUDDER TAB HINGE CUTOUT BRACKETS AND COVER FAIRING DAMAGED LT SIDE, AS IS RUDDER LT T/E FRAME IN SAME AREA. INSTALLED DOUBLER PER AA SRM 55-20-0 AND AA SRM 55-40-3. 2 L 7 3 4F A3WE 1998031200236 19980312 00236 NM 1998 3 12 98FDEA00151 1 19980302 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1026-1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 CORROSION ON RT SIDE OF STRINGER 30, BS 1026 TO 1030 IN AFT CARGO. REMOVED DAMAGED SECTION OF STRINGER 30. INSTALLED S TRINGER SPLICE AND DOUBLERS PER SRM 53-30-3. 2 L 7 3 4F A3WE 1998031200237 19980312 00237 NM 1998 3 12 98FDEA00153 1 19980305 A 2782 651781823 ACTUATOR BOEING 727 727233 138408A NM NR 8 LE SLAT FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 219FE 21102 98-0058 AFTER TAKEOFF WITH GEAR AND FLAPS UP, LEADING EDGE DEVICE INDICATIONS WERE NORMAL. SYSTEM 'A' LOST ALL QUANTITY . DURING HYDRAULIC LOSS CHECK LIST, LEADING EDGE DEVICE MALFUNCTION, LIGHT ON SLAT NR 8 WAS AMBER. AFTER AIRCRAFT TOW IN, FOUND NR 8 SLAT ACTUATOR BLOWN. REMOVED AND REPLACED PER MAINTENANCE MANUAL 27-81-32. REMOVED AND REPLACED SYSTEM FILTERS. TEST, BLED AND LEAK CHECK SYSTEM. NO LEAK, ALL FUNCTION NORMAL. RAN ENGINES 1 AND 2 PER JET RUN HANDBOOK AND TESTED PER CHAPTER 5A AND 9. GROUND CHECK NORMAL. SERVICED SYSTEM AS REQUIRED. 2 L 7 3 4F RT A3WE 1998031200238 19980312 00238 WP 1998 3 12 98FDEA00154 1 19980304 A 5512 SKIN DOUG DC10 DC1010F 3022111 WP LT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 LT HORIZONTAL STABILIZER UPPER FWD PLANK CRACKED FROM FWD EDGE 1.3 AFT THROUGH FASTENER HOLE AND BEYOND, 13 INCHES OUTBO ARD OF WORKING BULKHEAD. *S/D* INSTALLED DOUBLER PER SRM 55-20-00. 2 L 7 3 4F A22WE 1998031200239 19980312 00239 WP 1998 3 12 ABXA9800137 1 19980225 A 5730 5769859 SKIN DOUG DOUG DC8 DC863F 302198F WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 CORROSION ON LOWER SKIN AT LEFT WING LEADING EDGE, JUST INBOARD OF NR 2 STUB WING, AFT OF SLOT DOOR. REPAIRED IAW ABX REA D857-21927MR. 2 L 7 4 4F 4A25 1998031200240 19980312 00240 WP 1998 3 12 ABXA9800138 1 19980225 A 5720 5769589 DOUBLER DOUG DOUG DC8 DC863F 302198F WP WS 520.168 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 RIGHT WING LEADING EDGE INTERNAL DOUBLER CRACKED. REPAIRED IAW ABX REA D857-21919MR. 2 L 7 4 4F 4A25 1998031200241 19980312 00241 WP 1998 3 12 ABXA9800139 1 19980225 A 5712 9753293 RIB DOUG DOUG DC8 DC863F 302198F WP WS 253 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 CRACK AT LEADING EDGE RIB, NR 3 PYLON. REPAIRED IAW ABX REA D857-21918MR. 2 L 7 4 4F 4A25 1998031200242 19980312 00242 WP 1998 3 12 ABXA9800140 1 19980225 A 5711 56113402 SPAR CAP DOUG DOUG DC8 DC863F 302198F WP WS 81 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 LEFT WING UPPER SKIN FRONT SPAR CAP CORRODED. REPAIRED IAW ABX REA D857-21941MR. 2 L 7 4 4F 4A25 1998031200243 19980312 00243 WP 1998 3 12 ABXA9800141 1 19980225 A 5320 9754001509 WEB DOUG DOUG DC8 DC863F 302198F WP BS 270 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 STA 270, LONGERON 33L TO LONGERON 34L WEBBING IS CRACKED UNDER Z-FITTING IN TORQUE BOX. REPAIRED IAW ABX REA D853-21920 MR. 2 L 7 4 4F 4A25 1998031200244 19980312 00244 WP 1998 3 12 ABXA9800142 1 19980225 A 5311 2750825 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 1000 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 STA 1000 AT LONGERON 36 ATTACH AREA, FRAME FLANGE AND HARDWARE IS CORRODED. REPAIRED IAW ABX REA D853-21904MR. 2 L 7 4 4F 4A25 1998031200245 19980312 00245 WP 1998 3 12 ABXA9800143 1 19980225 A 5720 5616880 FITTING DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 818AX 46075 ATTACH FITTING CRACKED OUTBOARD, AFT SIDE OF STRINGERS 10 AT XRS 74, LEFT WING. REPAIRED IAW ABX REA D828-21938MR. 2 L 7 4 4F 4A25 1998031200246 19980312 00246 WP 1998 3 12 ABXA9800145 1 19980105 A 5320 57552717 DOUBLER DOUG DOUG DC8 DC861F 3021953 WP BS 450 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 INTERNAL FINGER DOUBLER CORRODED AT STATION 450 BETWEEN LONGERONS 31L TO 31R. REPAIRED IAW DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998031200247 19980312 00247 WP 1998 3 12 ABXA9800146 1 19980105 A 5712 5769471 RIB DOUG DOUG DC8 DC861 3021952 WP WS 651 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 RIGHT WING LEADING EDGE AT STATION XFS 651.00, THE UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K 05056 AND DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1998031200248 19980312 00248 WP 1998 3 12 ABXA9800147 1 19980113 A 5320 35792221 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1260 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 STATION 1260 TO 1280 LONGERON 34R SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998031200249 19980312 00249 WP 1998 3 12 ABXA9800148 1 19980120 A 5411 5779981 FRAME DOUG DOUG DC8 DC861 3021952 WP NR 3 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 NR 3 PYLON 2ND FROM AFT LOWER APRON FRAME CRACKED AT LEFT END. REPAIRED ANGLE IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998031200250 19980312 00250 WP 1998 3 12 ABXA9800149 1 19980114 A 5320 575072670 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 240 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 INTERCOSTAL CRACKED AT STATION 240 TO 260 LONGERON 33R. REPAIRED IAW DACO DWG 5750720 AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998031200251 19980312 00251 WP 1998 3 12 ABXA9800150 1 19980104 A 5311 47507431 FRAME DOUG DOUG DC8 DC861 3021952 WP BS 702 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 FRAME AT STA 702, LEFT SIDE CRACKED ABOVE CUSP. REPAIRED IAW DC8 SRM 53-7-0. 2 L 7 4 4F 4A25 1998031200252 19980312 00252 WP 1998 3 12 ABXA9800151 1 19980108 A 5320 37584951N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1239 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 STA 1239 ABOVE STRINGER 35A INTERCOSTAL TIE FITTING IS CORRODED. REPLACED INTERCOSTAL TIE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F 4A25 1998031200253 19980312 00253 WP 1998 3 12 ABXA9800152 1 19980227 A 5610 5613217509 WINDOW DOUG DOUG DC8 DC861 3021952 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 DURING POST FLIGHT INSPECTION, FOUND THAT CAPTAIN'S SLIDING WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. LUBRICATED AND INSP ECTED WINDOW, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998031200254 19980312 00254 1998 3 12 MWEA98276 4 19980302 A 3425 5223877001 ADI DOUG DC9 DC915 3022036 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 300ME 45718 THE FO ADI HAS A GYRO FLAG AND SHOWS 0 DEGREES WHEN TURNED INTO A LEFT OR RIGHT BANK. MTC REMOVED AND REPLACED NR 2 ADI . 2 L 7 2 4F A6WE 1998031200255 19980312 00255 WP 1998 3 12 MWEA98277 1 19980302 A 5312 BULKHEAD WEB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD ELONGATED HOLES A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 203ME 47673 THE AFT PRESSURE BULKHEAD WEB HAS 3 ELONG HOLES ON LT SIDE DOOR JAMB STA Z34 TO 48. MTC FABRICATED REPAIR DOUBLER AND B USHINGS IAW SVC MSP-0172/PDG ATA 09-053-30-01 DATED 09FEB98. 2 L 7 2 4F A6WE 1998031200256 19980312 00256 1998 3 12 MWEA98278 4 19980303 A 2565 113311DG SLIDE DOUG DC9 DC932 3022066 WP CABIN DOOR DEFECTIVE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 301ME 47190 THE MAIN DOOR SLIDE PRESSURE GAUGE INDICATES IN THE RED. MTC REPLACED SLIDE. 2 L 7 2 4F A6WE 1998031200257 19980312 00257 GL 1998 3 12 RRXA98064 2 19980228 A 7260 305115704060 SEAL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C5 GL NR 3 ENGINE CUT A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 8091U 45995 DURING CLIMBOUT LOST OIL QUANTITY ON NR 3 WITH OIL PRESSURE FLUCTUATING. PUT NR 3 THROTTLE TO IDLE, AFTER 2 MINUTES LOW OIL PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED INFLIGHT SHUTDOWN CHECKLIST. ON GROUND CHK FOUND STARTER CASE SEAL LEAKS . REMOVED STARTER AND REPLACED CUT CASE SEAL. REPLACED AND SERVICED STARTER, GRD RUN, NO LEAKS. NOTE CHECKED ENG FING ER SCREENS (4) OK. REPLACED SCREEN, NO LEAKS. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998031200258 19980312 00258 WP 1998 3 12 RRXA98065 1 19980227 A 3297 WIRE DOUG DC8 DC873F 302199F WP RT MLG BROKEN A RRXA O OTHER N FALSE WARNING AP APPROACH 1 WP 15 870TV 46086 UPON LOWERING GEAR, THE RT GREEN LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, NO HELP. RAISED AND LOWERED M/ G THREE TIMES, NO HELP WITH INDICATION. TOWER INDICATED GEAR ALL DOWN, LIGHT STILL REMAINS OFF. INSPECTED RIGHT MAIN G EAR, FOUND PIN 'K' AT GEAR DOWN SWITCH WIRE BROKEN. RE-PINNED WIRE, MANUALLY OPERATED SWITCH, SYSTEM TEST GOOD AS PER M M 32-2-0 AND M/M 32-60-1. 2 L 7 4 4F RT 4A25 1998031200259 19980312 00259 1998 3 12 VNAA9802024 4 19980228 A 2360 161251 STATIC WICK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WINGTIP FAILED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 422JS 3018 WHILE EN ROUTE, THE ACFT WAS STRUCK BY LIGHTNING. CONTINUED ON TO RDG. MX INSPECTED AND APPROVED THE ACFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT WAS COMPLETED WITHOUT INCIDENT. PIT MX COMPLIED WITH A LIGHTNING STRIKE INSPECTION IAW DORNIER MM 05-51-02. MX INSPECTED AND REPAIRED BURNT PAINT ON THE RIGHT HAND WING TIP AND REPLACED THE RIGHT HAND OUTB OARD WING TIP STATIC WICK. ALSO, DAMAGE WAS NOTED ON THE LEFT HAND MAIN LANDING GEAR FAIRING SPONSON. A REPAIR WAS CAR RIED OUT ON THE AREA IAW DORNIER SRM 51-77-31. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031200260 19980312 00260 NM 1998 3 12 VNAA9802025 1 19980228 A 2750 1050A000003 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE TE FLAPS FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 438JS 31261 3056 WHILE PREPARING FOR DEPARTURE, WHEN THE FLAPS WERE SELECTED TO 12 DEGREES, THE FLAP INDICATOR REMAINED AMBER. THE AIRCR AFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE FLAP CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENA NCE MANUAL 27-50-00. OPERATION CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031200261 19980312 00261 WP 1998 3 12 TC8A98012 1 19980303 A 2420 501280115 CONTROL PANEL DOUG DC8 DC8F55 3021928 WP NR 1 GENERATOR FAILED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 182SK 1746 45817 ON T/O, NR 2 AND NR 3 GENERATOR UNPARALLELED LIGHTS ILLUMINATED. VOLTS AND FREQS NORMAL, UNABLE TO PARALLEL, ABORTED TA KEOFF AT 80 KNTS. REMOVED AND REPLACED NR 1 GENERATOR CONTROL PANEL. ALSO, ADJUSTED VOLTAGE NR 2, 3, 4 ENGINES, OPS CH ECKS OK AT VARIOUS POWER SETTINGS AND LOADS IAW MM 24-5-7. 2 L 7 4 4F 4A25 1998031200262 19980312 00262 WP 1998 3 12 TC8A98013 1 19980303 A 2420 GENERATOR DOUG DC8 DC8F55 3021928 WP E/E COMPT MALFUNCTIONED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 182SK 45817 DURING TAXI OUT, MULTIPLE GENERATOR UNPARALLELED LIGHT ILLUMINATED 3, 4 AND 5 IN SEQUENCE. GENERATORS WOULD NOT PARALLE L. ENTERED IN DMI 8145 PER TCA MEL 24-8 CATEGORY C PLACARD INSTALLED. 2 L 7 4 4F 4A25 1998031200363 19980312 00363 EU 1998 3 12 HAIHCMA0178 1 19980303 A 6520 350A33215300 LAMIFICATION SNIAS 350 AS350B2 8680813 EU REAR ROTOR TORN E HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 602 2889 REAR ROTOR LAMIFICATION IS TORN BEYOND LIMITS AND THERE IS NO "J" GAP. 1 G 7 1 3U H9EU 1998031200364 19980312 00364 SW 1998 3 12 HEEA0013107 1 19980302 A 8010 SM20ACD200A21 RELAY BELL 206 206L3 1182108 SW STARTER BURNT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31801 51074 STARTER STAYS ENGAGED. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND CONTACTS WERE BURNT. 1 G 7 1 3U H2SW 1998031200365 19980312 00365 1998 3 12 HEEA0013108 4 19980302 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB S751 GPS DISPLAY FADES OUT AFTER 3 TO 4 MINUTES. NOTE: FADES MORE AT NIGHT. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H3EU 1998031200366 19980312 00366 1998 3 12 HEEA0013109 4 19980303 A 3452 066106200 TRANSPONDER KT76 BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 TRANSPONDER WILL NOT IDENT AND WILL NOT TEST. PERFORMED PRELIMINARY INSPECTION AND FOUND SWITCH BOARD INTERMITTENT. REP LACED SWITCH BOARD. ALSO FOUND PHOTOCELL NOT DIMMING PROPERLY. REPLACED PHOTOCELL. UNIT BENCH CHECK GOOD. 1 G 7 1 3U O H2SW 1998031200367 19980312 00367 SW 1998 3 12 HEEA0013110 1 19980303 A 6710 206001330001 SUPPORT ASSY BELL 206 206L1 1182107 SW CYCLIC CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 CYCLIC SUPPORT ASSY CORROSION BEYOND LIMITS AROUND BASE AREA. SCRAPPED PART AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1998031200368 19980312 00368 GL 1998 3 12 HEEA0013111 2 19980303 A 7310 206063637001 FITTING BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL FUEL MANIFOLD CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 FUEL MANIFOLD FITTING ASSY. HAS EXCESSIVE CORROSION ON EARS OF MANIFOLD AROUND BOLT HOLES. REPLACED WITH SERVICEABLE PAR T. 1 G 7 1 3U 3 U H2SW E1GL 1998031200369 19980312 00369 SW 1998 3 12 HEEA0013112 1 19980303 A 6510 327211 DISC SET BELL 206 206L1 1182107 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 DISC CORRODED AROUND BOLT HOLES. SCRAPPED DISC ASSY AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1998031200370 19980312 00370 SW 1998 3 12 HEEA0013113 1 19980303 A 6310 406040532101 BEARING 406040500113 BELL 206 206L4 1182110 SW COUPLING GROOVED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 5955 A1716 52037 BEARING HAS GROOVES ON ROLLERS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U NC H2SW 1998031200371 19980312 00371 SW 1998 3 12 HEEA0013114 1 19980303 A 6310 406040530101 BEARING 406040500113 BELL 206 206L4 1182110 SW COUPLING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 5955 A1716 52037 BEARING BREAKING DOWN ON ROLLER. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U NC H2SW 1998031200372 19980312 00372 SW 1998 3 12 HEEA0013115 1 19980303 A 6310 406040516101 INPUT SHAFT 406040500113 BELL 206 206L4 1182110 SW XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077B 5955 A1716 52037 INPUT SHAFT SPLINES WORN BEYOND LIMITS. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U NC H2SW 1998031200373 19980312 00373 1998 3 12 HEEA0013116 4 19980303 A 3452 066106200 TRANSPONDER KT76 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3108E 51498 ATC REPORTED TRANSPONDER AS INOPERATIVE. FOUND WEAK POWER OUT. REPLACED CAVITY OSCILLATOR V101. REPAIRED. REPLACED DE TERIORATED RESISTOR R477 AND PHOTOCELL V301 DUE TO WEAK REPLY LIGHT. REPAIRED. ADJUSTED FREQUENCY. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1998031200374 19980312 00374 1998 3 12 HEEA0013117 4 19980303 A 2312 071121524 CONTROL KFS598 BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 DISPLAY STAYS BRIGHT. PERFORMED PRELIMINARY INSPECTION. REPLACED V301 PHOTOCELL. REPAIRED. ALSO INSTALLED P201 HEADER , AND APPLIED HUMISEAL. CHECKED 5V LIGHTING. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1998031200375 19980312 00375 1998 3 12 HEEA0013118 4 19980303 A 3454 071121627 CONTROL BELL 214 214ST 1182106 SW NAV UNIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 DISPLAY IS NOT CHANNELING CORRECTLY. PERFORMED PRELIMINARY INSPECTION. FOUND PHOTOCELL LENS MISSING. INSTALLED PHOTOCE LL LENS P/N 088-0548-00. REPAIRED. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1998031200376 19980312 00376 1998 3 12 HEEA0013119 4 19980303 A 3452 066106200 TRANSPONDER KT76 BELL 407 407 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 BENCH CHECK NEEDED. REPLACED WEAK V301 PHOTODETECTOR, DETERIORATED R477 RESISTOR, INSTALLED MISSING IDENT PUSH BUTTON AN D INSTALLED HEAT SINK FOR Q415. ADJUSTED AS NEEDED AND BENCH CHECK GOOD. 1 G 7 1 3U O H2SW 1998031200377 19980312 00377 EU 1998 3 12 HEEA0013120 1 19980303 A 6320 4638201005 UPPER HOUSING 4638001001 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K 1327 S859 CRACK FOUND ON INBOARD RADIUS AND ACROSS RIB IN UPPER AREA OF HOUSING. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200378 19980312 00378 1998 3 12 HEEA0013121 4 19980303 A 2370 9806020023 CVR SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 706AE 655 760275 CVR WILL NOT TEST. 1 G 7 2 3U H1NE 1998031200379 19980312 00379 SW 1998 3 12 HEEA0013122 1 19980303 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 7470 36001 BLADE HAS BEEN REPAIRED PREVIOUSLY ON UPPER SURFACE AT STATION 121.25". THERE WAS EVIDENCE OF SKIN CRACK AT THE EDGE OF THE REPAIR. 1 G 7 2 4U H4SW 1998031200380 19980312 00380 1998 3 12 HEEA0013123 4 19980303 A 3457 13824120234 RECEIVER BELL 206 206L3 1182108 SW COCKPIT GPS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4180F 51469 GPS RECEIVER LOST ALL STATIONS. "WPT" BUTTON BACKLIGHTING INTERMITTENTLY. 1 G 7 1 3U H2SW 1998031200381 19980312 00381 1998 3 12 HEEA0013124 4 19980303 A 3457 0110005400 GPS GPS150 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22425 45743 COCKPIT GPS HAS NO DISPLAY. 1 G 7 1 3U H2SW 1998031200382 19980312 00382 1998 3 12 HEEA0013125 4 19980303 A 3452 066106200 TRANSPONDER KT76 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406EH 45183 TRANSPONDER REPORTED INOPERATIVE. NO CODE OR ALTIMETER READOUT. 1 G 7 1 3U H2SW 1998031200383 19980312 00383 NE 1998 3 12 HEEA0013126 1 19980303 A 2421 7655009005105 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 AC GENERATOR INOPERATIVE. THIS IS THE THIRD TIME THIS GENERATOR WAS REMOVED FOR BEING INOPERATIVE SINCE WE RECEIVED IT OVERHAULED 2-28-97. 1 G 7 2 3U H1NE 1998031200384 19980312 00384 1998 3 12 HEEA0013127 4 19980303 A 3453 453105004 LORAN SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 707AE 760276 LORAN WILL NOT SELF TEST OR ANY FUNCTION LIGHTS WHEN TURNED ON. 1 G 7 2 3U H1NE 1998031200385 19980312 00385 EU 1998 3 12 HEEA0013128 1 19980303 A 2822 D10731818 BEARING D107318D1 BOLKMS 105 BO105S 5626006 EU BOOST PUMP SEIZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911DD 490 125748M S830 PUMP INOPERATIVE. BEARINGS FROZE UP CAUSING PUMP TO FAIL. 1 G 7 2 3U H3EU 1998031200386 19980312 00386 EU 1998 3 12 HEEA0013129 1 19980303 A 2822 D105300010 BEARING D107318D1 BOLKMS 105 BO105S 5626006 EU BOOST PUMP SEIZED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911DD 490 125748M S830 PUMP INOPERATIVE. BEARINGS FROZE UP CAUSING PUMP TO FAIL. 1 G 7 2 3U H3EU 1998031200387 19980312 00387 1998 3 12 HEEA0013130 4 19980303 A 3453 066402600 LORAN KLN88 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5017G 45228 KLN88 NO DISPLAY. 1 G 7 1 3U H2SW 1998031200388 19980312 00388 SW 1998 3 12 HEEA0013131 1 19980303 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 10727 33010 M/R BLADE HAS FRETTING PAD UNBONDED ON LOWER LEADING EDGE SURFACE. 1 G 7 2 4U H4SW 1998031200389 19980312 00389 1998 3 12 HEEA0013132 4 19980303 A 2330 AA20030 PA AMPLIFIER BELL 206 206L1 1182107 SW CABIN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1072T 45385 PA AMPLIFIER LOW VOLUME. 1 G 7 1 3U H2SW 1998031200390 19980312 00390 1998 3 12 HEEA0013133 4 19980303 A 3454 066303800 RMI KING KI229 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205UC S668 WILL NOT SLAVE WITH HSI. 1 G 7 2 3U H3EU 1998031200391 19980312 00391 NE 1998 3 12 HEEA0013134 1 19980303 A 6200 7610208011042 PITCH HORN 761020800005 SKRSKY S76 S76A 8143006 NE M/R SYS GROOVED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 4298 A13402846 760181 DEEP GROOVE ON INBOARD LUG (WASHER AREA) APPROXIMATELY .025" IN DEPTH. SCRAPPED PART. REPLACED WITH SERVICEABLE PITCH H ORN. 1 G 7 2 3U H1NE 1998031200392 19980312 00392 1998 3 12 HEEA0013135 4 19980303 A 3452 066106200 TRANSPONDER KT76 BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Y 3626 TRANSPONDER ON/OFF SWITCH LOOSE. PERFORMED PRELIMINARY INSPECTION. FOUND ON/OFF SWITCH BROKEN. REPLACED FACEPLATE ASSY , REPAIRED. ADJUSTED TO SPECS. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1998031200393 19980312 00393 1998 3 12 HEEA0013136 4 19980303 A 3425 5040017901 ATT INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 POWER FLAG WON'T PULL - DOESN'T APPEAR TO COME ON. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 1998031200394 19980312 00394 SW 1998 3 12 HEEA0013137 1 19980303 A 5520 206030856111 ELEVATOR BELL 412 412 1182202 SW MOUNT HOLE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2298Z 33077 UNABLE TO INSTALL ELEVATOR DUE TO MOUNTING BOLT HOLE MISALIGNED WITH HORN. INSTALLED SERVICEABLE ELEVATOR. 1 G 7 2 4U H4SW 1998031200395 19980312 00395 SW 1998 3 12 HEEA0013138 1 19980303 A 6320 412040101101 SEAL 412040123101 BELL 412 412 1182202 SW M/R GR BOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 33008 365 A1159 36004 SEAL LEAKING. REPLACED WITH SERVICEABLE SEAL. 1 G 7 2 4U H4SW 1998031200396 19980312 00396 EU 1998 3 12 HEEA0013139 1 19980303 A 6230 4638205005 ROTOR MAST 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. MAST HAD CORROSION IN BUSHING BORES BEYOND LIMITS. SCRAPPED PART. REPLACED WITH SERVICEABLE PA RT. 1 G 7 2 3U H3EU 1998031200397 19980312 00397 EU 1998 3 12 HEEA0013140 1 19980303 A 6230 4638205009 SUPPORT TUBE 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. SUPPORT TUBE WORN ANODIZED SURFACE. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200398 19980312 00398 EU 1998 3 12 HEEA0013141 1 19980303 A 6230 4619205004 BUSHING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BUSHING LOCK AREA WORN. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200399 19980312 00399 EU 1998 3 12 HEEA0013142 1 19980303 A 6320 1054190206 OUTER DEFLECTION 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. OUTER DEFLECTION CRACKED. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200400 19980312 00400 EU 1998 3 12 HEEA0013143 1 19980303 A 6320 4619303053 WASHER 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. WASHER WORN. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200401 19980312 00401 EU 1998 3 12 HEEA0013144 1 19980303 A 6321 133273 DISC 4638001004 BOLKMS 105 BO105S 5626006 EU ROTOR BRAKE WARPED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BRAKE DISC WARPED. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200402 19980312 00402 EU 1998 3 12 HEEA0013145 1 19980303 A 6320 4638302013 SHAFT 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. WORN CLUTCH AREA. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200403 19980312 00403 EU 1998 3 12 HEEA0013146 1 19980303 A 6320 4638304002 GEAR 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX SPALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. GEAR SPALLING. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200404 19980312 00404 EU 1998 3 12 HEEA0013147 1 19980303 A 6320 4619204001 PLANETARY AXLE 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX PITTING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. PLANITARY AXLE PITTING. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200405 19980312 00405 EU 1998 3 12 HEEA0013148 1 19980303 A 6320 4619312040 CONNECTING SHAFT 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. CONNECTING SHAFT DRIVE SPLINES WORN. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200406 19980312 00406 EU 1998 3 12 HEEA0013149 1 19980303 A 6320 4619313006 SUN GEAR 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. SUN GEAR FRETTING CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200407 19980312 00407 EU 1998 3 12 HEEA0013150 1 19980303 A 6320 10541961 SLIDING SLEEVE 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. SLIDING SLEEVE HAS CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200408 19980312 00408 EU 1998 3 12 HEEA0013151 1 19980303 A 6320 4619312027 ACCY HOUSING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. ACCY HOUSING CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200409 19980312 00409 EU 1998 3 12 HEEA0013152 1 19980303 A 6320 4619213010 PLANETARY GEAR 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. PLANETARY GEAR HAS CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200410 19980312 00410 EU 1998 3 12 HEEA0013153 1 19980303 A 6320 4619308044 ELBOW 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. ELBOW HAS CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200411 19980312 00411 EU 1998 3 12 HEEA0013154 1 19980303 A 6320 4638304001 SUN GEAR 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX SPALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. SUN GEAR SPALLING. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200412 19980312 00412 EU 1998 3 12 HEEA0013155 1 19980303 A 6320 4619303060 DRIVE SHAFT 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. WORN GEAR SET. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200413 19980312 00413 WP 1998 3 12 VJ9800035 1 19980224 A 5330 1A29937 SKIN DOUG DC9 DC932 3022066 WP BS 242-304 DENTED A VJ6A O OTHER O OTHER IN INSP/MAINT 1 SO 11 901VJ 47275 DENT, 2.035 IN DEPTH, CROSSING 3 BAYS ON FUSELAGE SKIN STRETCHING FROM FS 242 TO FS 304 OUT OF LIMITS IAW DC9 SRM 53-04, FIG 38. FABRICATED DOUBLERS 14.75 TIMES 7.125 INCHES, 17 BY 7 INCHES AND 135 BY 8.7 INCHES USING TITANIUM .025 IAW EO 98-800; PRIMED IAW DC9 SRM 51-10-3 AND INSTALLED DOUBLERS IAW EO 98-800. 2 L 7 2 4F A6WE 1998031200414 19980312 00414 WP 1998 3 12 VJ9800036 1 19980225 A 5330 1A31376 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 901VJ 47275 EXTERNAL FUSELAGE SKIN BELOW FORWARD CARGO DOOR LOWER SILL PLATE HAS CORROSION. GROUND OUT LIMITS, FABRICATED AND INSTA LLED DOUBLER REPAIR IAW EO 98-794. REPAIR DOUBLER FABRICATED 2024 T3 .071 THICKNESS TIMES 69 BY 21 BY 7.50 TIMES 52.75 BY 21 INCHES. 2 L 7 2 4F A6WE 1998031200415 19980312 00415 WP 1998 3 12 VJ9800037 1 19980306 A 2560 113317 SLIDE COVER DOUG DC9 DC932 3022066 WP R1 DOOR LOOSE A VJ6A K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 924VV 47278 EMERGENCY ESCAPE SLIDE CAME LOOSE FROM MOUNTING BRACKET ON R1 DOOR. REINSTALLED SLIDE IN CASE AND NO DEFECTS NOTED. AC COMPLISHED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998031200416 19980312 00416 NM 1998 3 12 MALA976028 1 19980302 A 3350 1013075 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 832MA 341 DURING INSPECTION ROW 4 RED FLOOR TRACK EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998031200417 19980312 00417 EU 1998 3 12 MALA976029 1 19980303 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 89XJ 089 DURING INSPECTION, EMERGENCY LIGHTS WOULD INITIALLY ILLUMINATE DURING FLIGHT ATTENDANT TEST, BUT THEN SHUT OFF. MAINTEN ANCE REPLACED ALL BATTERY PACKS. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998031200418 19980312 00418 EU 1998 3 12 MALA976030 1 19980305 A 3350 5LN SWITCH SAAB SF340 SF340A 7850100 EU COCKPIT INOPERATIVE A MALA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 15 99XJ 099 AFTER DOOR WAS SHUT THE EMERGENCY LIGHT SWITCH DOES NOT SHOW ARMED. MAINTENACE RELAMPED SWITCH LIGHT. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998031200419 19980312 00419 NM 1998 3 12 K3HA980022 1 19980304 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 EMERGENCY EXIT SIGN AFT OF THE FORWARD LOWERED CEILING INOP. REPLACED BATTERY PACK ON EMERGENCY EXIT SIGN AFT OF THE L OWER CEILING. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998031200430 19980312 00430 WP 1998 3 12 IXXA980016 1 19980303 A 2550 SEALING TAPE DOUG DC8 DC862 3021970 WP CARGO COMPT MISINSTALLED A IXXA K NONE J WARNING INDICATION DE DESCENT 1 GL 23 728PL 45918 DURING DESCENT INTO HIK, THE NUMBER TWO AND FIVE MAIN CARGO COMPARTMENT SMOKE DETECTOR WARING LIGHTS ILLUMINATED. THE FL IGHT CREW TURNED OFF THE CARGO COMPARTMENT LIGHTING AND THE WARNING LIGHTS EXTINGUISHED. MAINTENANCE INSPECTED THE CARG O COMPARTMENT WITH THE LIGHTING SYSTEM ILLUMINATED. MAINTENANCE FOUND CONOLITE LINER SEALING TAPE PARTIALLY COVERING TW O COMPARTMENT LIGHT FIXTURES SMOLDERING. THE TAPE WAS REMOVED AND A SUCCESSFUL OPERATIONAL CHECK OF THE SMOKE DETECTION SYSTEM WAS PERFORMED IN ACCORDANCE WITH THE MAINTENANCE MANUAL, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1998031200431 19980312 00431 NM 1998 3 12 RAAA98B2011 1 19980305 A 3220 65176731 FITTING BOEING 727 72722C 138400F NM BS 351.2 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 57463 19098 DURING SCHEDULED NLG CHANGE AND ACCOMPLISHMENT OF CPCP TASK CARD C32-131-01 FOUND 2.1 INCH CRACK THROUGH DRAG BRACE SUPP ORT FITTING INTERCOSTAL RADIUS. CHANGED DRAG BRACE SUPPORT FITTING PER S/B 727 53-69, REV 2 M-54 NR 1. 2 L 7 3 4F A3WE 1998031200432 19980312 00432 NE 1998 3 12 CALA9800386 2 19980304 A 7250 TURBINE BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE FAILED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 32725 20655 666411 THE NR 3 ENGINE OIL PRESSURE WENT TO ZERO ACCOMPANIED BY ILLUMINATION OF THE LOW OIL PRESSURE LIGHT WHILE EN ROUTE FROM RSW TO EWR. THE NR 3 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINT ENANCE REMOVED AND REPLACED THE NR 3 ENGINE. EXAMINATION REVEALED TURBINE FAILURE ATTRIBUTED TO FUEL NOZZLE STREAKING. THE ENGINE EXITED THE FLEET WITHOUT A TEARDOWN. 2 L 7 3 4F 4 F A3WE E2EA 1998031200433 19980312 00433 WP 1998 3 12 CALA9800387 1 19980305 A 2910 7578724 FILTER CASE DOUG DC10 DC1030 3023501 WP NR 3 HYD SYST BROKEN A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 39081 47861 THE NR 3 HYDRAULIC SYSTEM LOST FLUID ACCOMPANIED BY ILLUMINATION OF THE HYDRAULIC SYSTEM ELEVATOR OFF LIGHT WHILE EN ROU TE FROM FCO TO EWR. FUEL WAS DUMPED AND THE AIRCRAFT WAS DIVERTED TO CDG WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE DRIVEN HYDRAULIC PUMP PRESSURE FILTER CASE ASSEMBLY BROKEN. THE FILTER CASE ASSEMBLY WAS REMOVED AND REPLACED. THE NR 3 HYDRAULIC SYSTEM WAS SERVICED AND LEAK CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998031200434 19980312 00434 WP 1998 3 12 CALA9800388 1 19980304 A 3260 DNLOCK SWITCH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A CALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 09 12508 47797 WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO IAH, NO GREEN LIGHTS ILLUMINATED FOR NOSE GEAR. THE UNSAFE GEAR INDICATIO N CHECKLIST WAS COMPLETED DURING A GO AROUND AND WHEN GEAR WAS LOWERED AGAIN CREW RECEIVED THREE GREEN AND LANDED UNEVEN TFULLY. MAINTENANCE CHECKED NLG SWITCHES AND CONDUIT AND PERFORMED SHAKEDOWN TEST OF THE CONDUIT WITH NO DEFECTS NOTED. THE NLG DOWNLOCK SWITCH WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F A6WE 1998031200435 19980312 00435 NM 1998 3 12 CALA9800389 1 19980305 A 3230 BACC18Z3R CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM LEVER LATCH TRIPPED A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 17316 23367 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE LEVER LATCH LOCK OVERRIDE WAS USED PER CHECKLIST AND THE GEAR RETRACTED. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEVER LATCH C IRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET AND TESTED IAW MM 32-31-21, PAGE 101 AND THE TEST WAS GOOD. 2 L 7 2 4F RT A16WE 1998031200436 19980312 00436 NM 1998 3 12 CALA9800391 1 19980305 A 2612 FIRE LOOP BOEING 737 7372C0 1384488 NM NR 2 ENGINE CHAFED A CALA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 14245 20074 THE NR 2 ENG FIRE WARNING LIGHT AND BELL ACTIVATED BRIEFLY SEVERAL TIMES IN FLIGHT. THE DURATION OF EACH WARNING WAS LE SS THAN ONE SECOND. THE NR 2 ENG FIRE LIGHT AND WARNING BELL CAME ON STEADY AFTER LANDING AT CLE. BOTH FIRE BOTTLES WE RE DISCHARGED, AND SHORTLY AFTERWARDS THE FIRE WARNING CEASED. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE NR 2 ENGINE OVERHEAT/NORMAL POSITION FIRE DETECTION SYSTEM WAS PLACARDED INOPERATIVE. *S/D* MAINTENANCE FOUND FIRE LOOP WIRE CHAFE D IN HALF AT DISCONNECT SOCKET PLUG FOR LOWER FORWARD LOOP ASSEMBLY. THE SOCKET PLUG AND INSULATION WERE REMOVED AND RE PLACED, OPERATION CHECKED GOOD. 2 L 7 2 4F A16WE 1998031200437 19980312 00437 NM 1998 3 12 CALA9800392 1 19980304 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOORBEAM CORRODED AT BOTH SIDES OF SCREW HOLES TO EDGE OF T-CAP AT STA 986.5. REPAIRED IAW SRM 53-00- 51. 2 L 7 2 4F RT A16WE 1998031200438 19980312 00438 NM 1998 3 12 CALA9800393 1 19980304 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOORBEAM CORRODED AT BS 967 UPPER T-CAP, LBL24. REPAIRED IAW SRM 53-00-51, FIGURE 202. 2 L 7 2 4F RT A16WE 1998031200439 19980312 00439 NM 1998 3 12 CALA9800394 1 19980305 A 5311 FRAME BOEING 747 747230B 1384889 NM BS 400 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 78019 20527 INSPECTION FOUND A 0.625 CRACK IN FRAME WEB AT BS 400, STRINGER 15L. REPAIRED IAW HAECO REPAIR SCHEME R53-12-33682. 2 L 7 4 4F A20WE 1998031200440 19980312 00440 NM 1998 3 12 CALA9800395 1 19980305 A 5320 INTERCOSTAL BOEING 737 7373T0 1384582 NM BS 967-986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND INTERCOSTAL CORRODED BETWEEN FS 967 AND 986.5 LEFT SIDE, 22 INCHES FROM CENTERLINE. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1998031200441 19980312 00441 WP 1998 3 12 CALA9800396 1 19980305 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP NR 2 RADIO ALT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938AS 49365 INSPECTION FOUND NR 2 RADIO ALT RECEIVER ANTENNA RETAINING DOUBLER CORRODED. THE RETAINING DOUBLER WAS REMOVED AND REPL ACED IAW SRM 51-00 AND 51-30-2. 2 L 7 2 4F A6WE 1998031200442 19980312 00442 NE 1998 3 12 9803706635 2 19980304 A 7200 ENGINE BOEING 747 747227B 1384888 NM PWA JT9 JT9D7Q 52054 NE NR 2 MALFUNCTIONED A NWAA E ENGINE SHUTDOWN O OTHER TX TAXI/GRND HDL 1 GL 01 635US 21682 702055 AFTER A NORMAL START OF THE NR 2 ENGINE AND WHEN STARTING THE NR 3 ENGINE, APPROXIMATELY 2 MINUTES LATER, THE NR 2 ENGIN E EGT ROSE TO 550C WITH BOTH N1 AND N2 DECREASING. THE ENGINE WAS SHUT DOWN. GROUND PERSONNEL REPORTED SOME TORCHING V ISIBLE FROM THE NR 2 ENGINE. THE ENGINE WAS RESTARTED AND OPERATED NORMALLY. 2 L 7 4 4F 4 F A20WE E3NE 1998031200443 19980312 00443 WP 1998 3 12 9803719905 1 19980305 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAILCONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE. RIGGED RELEASE SYSTEM. F UNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998031200444 19980312 00444 NM 1998 3 12 UPS98226017 1 19980304 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 1130-1175 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:SI CORROSION (C53-224-01.05-03) ON SEAT TRACK FLANGE STA 1130-1175, LBL 45, WL 208. REMOVED OUT OF LIMI TS SEAT TRACK FABRICATED AND INSTALLED NEW SEAT TRACK AND REPAIR PARTS IAW SRM 53-10-5, 51-30-2. 2 L 7 3 4F A3WE 1998031200445 19980312 00445 NM 1998 3 12 UPS98226018 1 19980302 A 5753 TRACK BOEING 727 727247 138408F NM TE FLAPS CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) ON NR 1 T/E FLAP TRACK FORWARD ATTACH FITTING ON O/B SIDE OF TRACK ATTAC H FLANGE AROUND BUSHING FITTING REWORKED PER ER 98-2225. 2 L 7 3 4F A3WE 1998031200446 19980312 00446 NM 1998 3 12 UPS98226019 1 19980302 A 5744 FITTING BOEING 727 727247 138408F NM TE FLAP TRACK FRETTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 4 T/E FLAP TRACK FWD ATTACH FITTING FRETTED ON INBOARD SIDE OF TRACK ATTACH POINT. REMOVED FITTING AND ROUTED TO MACHINE SHOP. FITTING REWORKED PER ER NO 98-2216. 2 L 7 3 4F A3WE 1998031200447 19980312 00447 NM 1998 3 12 UPS98226020 1 19980302 A 5753 FLAP TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 2 T/E FLAP TRACK CENTER AFT ATTACH MOUNT BOLT HOLE CORRODED. REMOVED CORRODED MOUNT ROUTED TO MACHINE SHOP FOR REWORK PER ER NR 98-2214, REINSTALL AFTER REWORK. 2 L 7 3 4F A3WE 1998031200448 19980312 00448 NM 1998 3 12 UPS98226021 1 19980218 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 595-684 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:SI CORROSION (4-25-02) ON MAIN DECK SEAT TRACK FLANGE FASTENER HOLES, AS MARKED AT BS 595-BS 684 RBL 23, WL 208. REMOVED OUT OF LIMITS SECTION OF SEAT TRACK, FABRICATED AND INSTALLED NEW SECTION OF SEAT TRACK AND REPAIR PAR TS IAW SRM 51-10-2, 53-10-5, 51-20-151. 2 L 7 3 4F A3WE 1998031200449 19980312 00449 NM 1998 3 12 UPS98226022 1 19980210 A 5347 BAC1570797 SEAT TRACK BOEING 727 727247 138408F NM BS 1125-1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:SI CORROSION (C53-224-01.00-03) ON SEAT TRACK UPPER FLANGE BS 1125-BS 1130,, LBL 55, WL 208. REMOVE COR ROSION AND OUT OF LIMITS IAW SRM 53-10-1. REPLACED TRACK IAW SRM 51-30-2, SRM 51-10-1, 51-10-1, 51-10-6 AND MM 51-20-15 1. 2 L 7 3 4F A3WE 1998031200450 19980312 00450 NM 1998 3 12 UPS98226023 1 19980303 A 5753 651920417 CARRIAGE BOEING 727 727247 138408F NM NR 1 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 212UP 21392 INSPECTION TYPE:SI CORROSION (C57-581-04.00-03) NR 1 FLAP CARRIAGE HAS CORROSION INSIDE OF SPINDLE CORRODED CARRIAGE WAS REMOVED SENT TO OUTSIDE VENDOR FOR REPAIR DETERMINED TO BE SERVICABLE AND REINSTALLED ON A/C IAW SRM 27-51-13. 2 L 7 3 4F A3WE 1998031200451 19980312 00451 WP 1998 3 12 UPS98825983 1 19980124 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1630-1640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK AFT ACCESSORY SECTION HAS CRACKED LONGERON STA 1630-1640 AND LONGERON 24 LEFT. REMOVED SECTION OF LONGERON AND REPLACED WITH NEW IAW DC8 SRM 53 2 2 AND 51 1 20D. INSTALLED SKIN DOUBLER AND FUSELAGE IAW DC8 SRM 53 2 1 FIG 7. 2 L 7 4 4F RT 4A25 1998031200452 19980312 00452 WP 1998 3 12 UPS98825985 1 19980124 A 5320 WEB DOUG DC8 DC871F 302199D WP CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK FWD LWR CARGO COMPT RIGHT HAND TUNNEL AT CUSP WEB ABOVE FWD TORQUE BOX IS CRACKED. FABBED DOUBLER IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 5 1 1 8. INSTALLED PART IAW DC8 SRM 51 3 0 AND 51 1 21 AND 51 1 2 1A. 2 L 7 4 4F RT 4A25 1998031200453 19980312 00453 WP 1998 3 12 UPS98825986 1 19980127 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK MAIN CABIN STA 680 AT L6L END FITTING. REMOVED CRACKED FITTING DRILLED AND INSTALLED NEW ONE IAW D C8 SRM 5 1 1 24 AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998031200454 19980312 00454 WP 1998 3 12 UPS98825988 1 19980227 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1758 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK FUSELAGE MAIN CABIN INTERIOR FLOOR BOARD SUPPORT CHANNEL HAVE CORROSION AND SEAT TRACK E AT STA 175 8 BLO IS CRACKED. REMOVED CRACKED HAT CHANNEL. REMOVED CORROSION FROM LEFT HAND FLOOR BOARD OUT OF LIMITS IAW DC8 SRM 53 2 0, LOCATED AND DRILLED NEW SECTION OF HAT IAW DC8 SRM 51 1 247. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED SEAT TRACK 1752 TO 1760 IAW SRM 51 1 20D. PRIMED HAT SECTION IAW DC8 SRM 51 1 8. INSTALLED ON AC IAW DC8 SRM 51 13 0. 2 L 7 4 4F RT 4A25 1998031200455 19980312 00455 WP 1998 3 12 UPS98825989 1 19980224 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK STA 320 AT LONG 35 L FITTING IS CRACKED. REMVOED EXISTING FITTING FABRICATED SPLICES IAW DC8 SRM 5 3 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED FITTING IAW DC8 SRM 5 1 1 20D. 2 L 7 4 4F RT 4A25 1998031200456 19980312 00456 WP 1998 3 12 UPS98825990 1 19980128 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK LEFT WING MIDDLE LEADING EDGE RIB CRACKED AT FUEL DOOR. RECEIVED REO FABRICATED PARTS HEAT TREATE D IAW REO 04277. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW REO 04277 AND DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998031200457 19980312 00457 WP 1998 3 12 UPS98825991 1 19980130 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 340 DAMGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK STA 340 L28L LONGERON IS DAMAGED AT Z FITTING. BLENDED OUT DAMAGED IAW UPS DC8 SRM 53 2 0. FABBED REPAIR STRAP IAW REO 04279 AND DC8 SRM 51 1 24. ALODINED AND PRIMED REPAIR AREA AND STRAP IAW DC8 SRM 51 1 8. INSTALL ED REPAIR IAW REO 04279 AND DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998031200458 19980312 00458 WP 1998 3 12 UPS98825992 1 19980127 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 1324 BULGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK AFT LOWER CARGO LEFT HAND TUNNEL HORIZONTAL WEB HAS REPAIR DOUBLER BULGED AT STA 1324 LBL 54. REMO VED REPAIR DOUBLER IAW SRM 51 1 21. FABBED NEW REPAIR DOUBLER IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW REPAIR DOUBLER IAW DC8 SRM 51 1 21. 2 L 7 4 4F RT 4A25 1998031200459 19980312 00459 WP 1998 3 12 UPS98825993 1 19980123 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, FWD LOWER CARGO COMPT L37 R CRACKED AT END AT STA 80R. REMOVED CRACKED LONGEORN FABBED FITTING IA W DWG 3757600. ALODINED AND PRIMED NEW FITTING INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998031200460 19980312 00460 WP 1998 3 12 UPS98825994 1 19980227 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, STA 300 L27 TO 28 L 'Z' FITTING CRACKED. REMVOED FITTING FABBED ANGLES IAW DC8 SRM 53 2 0. ALOD INED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED FITTING AND SPLICE ANGLES IAW DC8 SRM 51 1 20D AND 53 2 0. 2 L 7 4 4F RT 4A25 1998031200461 19980312 00461 WP 1998 3 12 UPS98825995 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 844-850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK CABIN SEAT TRACK H CORRODED AT STA 844 TO 850. REMOVED CORROSION IAW DC8 SRM 51 1 8 NOT WITHIN LIM ITS. REMOVED DAMAGED SECTION STA 844 TO 850. FABRICATED NEW SECTION OF TRACK AND SPLICES IAW DC8 SRM 53 2 3. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 20D AND 51 3 0 AND 53 2 3. 2 L 7 4 4F RT 4A25 1998031200462 19980312 00462 WP 1998 3 12 UPS98825996 1 19980127 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, ALC COMPARTMENT STA 1460 ABOVE LONGERON 34 R FITTING CORRODED INSIDE TORQUE BOX. REMOVED FITTING IAW DC8 SRM 51 1 21. DRILLED UP NEW FITTING IAW DC8 SRM 51 1 2. INSTALLED NEW FITTING IAW DC8 SRM 51 3 0. 2 L 7 4 4F RT 4A25 1998031200463 19980312 00463 WP 1998 3 12 UPS98825997 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1000-1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK UPPER CARGO SEAT TRACK RBL 60 CORRODED IN SWIVEL PLACES STA 1000 TO STA 1140. REMOVED CORRODED SEA T TRACK IAW DC8 SRM 53 2 3. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW TRACK AND SPLICES IAW DC8 SRM 5 3 2 3 AND 51 3 0. 2 L 7 4 4F RT 4A25 1998031200464 19980312 00464 WP 1998 3 12 UPS98825998 1 19980128 A 5320 EXTRUSION DOUG DC8 DC871F 302199D WP BS 1740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK SURFACE CORROSION ON FLOOR STRUCTURE AT STA 1740. REMOVED CORROSION AND DAMAGED EXTRUSION FABBED N EW EXTRUSION IAW DC8 SRM 53 7 1 AND DWGT 5755032. INSTALLED EXTRUSION IAW DC8 SRM 51 1 20D. ALODINED AND PRIMED IAW DC 8 SRM 51 1 8. 2 L 7 4 4F RT 4A25 1998031200465 19980312 00465 WP 1998 3 12 UPS98825999 1 19980301 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 435 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LT WING L/E RIB AT STA XS 435.0 CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998031200466 19980312 00466 WP 1998 3 12 UPS98826000 1 19980223 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 372.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LT WING L/E RIB AT STA XFS 372.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998031200467 19980312 00467 WP 1998 3 12 UPS98826001 1 19980223 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 379 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C LT WING L/E RIB AT STA XFS 379.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998031200468 19980312 00468 WP 1998 3 12 UPS98826002 1 19980227 A 5320 CUSP DOUG DC8 DC871F 302199D WP BS 453 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C F/S 453 CORROSION REMOVAL RT CUSP BEYOND LIMITS. REPAIRED IAW SRM ADDN DC8-5330-2159-B. 2 L 7 4 4F RT 4A25 1998031200469 19980312 00469 WP 1998 3 12 UPS98826003 1 19980225 A 5347 5887361511 CARGO TRACK DOUG DC8 DC871F 302199D WP CARGO COMPT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C NR 2 PIT, CARGO TRACK AFT DOOR RT SIDE HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLAC EMENT TRACK IAW SRM 51-3-0. AND DWG 5750726. 2 L 7 4 4F RT 4A25 1998031200470 19980312 00470 WP 1998 3 12 UPS98826004 1 19980303 A 5330 SKIN DOUG DC8 DC871F 302199D WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 797UP 45897 NR 4 PIT DOOR FRAME SKIN CRACKED IN UPPER AFT CORNER EO DC8-5330-4067A ISSUED. INSTALLED TEMP REPAIR TO DOOR JAM CORNER PER EO DC-8 5330-4067. 2 L 7 4 4F RT 4A25 1998031200471 19980312 00471 WP 1998 3 12 UPS98826006 1 19980127 A 2750 PULLEY BRACKET DOUG DC8 DC871F 302199D WP RT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK RIGHT MAIN WHEEL WELL FLAP CONTROL PULLEYS WORN AND HARDWARE EVIDENCE OF CORROSION JUST ABOVE GEAR DOOR UPLOCK OTBD. REMOVED AND REPLACED PULLEY BRACKET ON RIGHT SIDE IAW DC8 SRM 51 3 0. REMOVED AND REPLACED PULLEY HA RDWARE IAW DC8 MM 20 17 00. 2 L 7 4 4F RT 4A25 1998031200472 19980312 00472 WP 1998 3 12 UPS98826007 1 19980127 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK CORRODED HARDWARE AT STA 70 IN FLOORBEAM AFT OF LAV AREA. REMOVED CORRODED ANGLE AND REPLACED IAW DC8 SRM 51 1 20D AND 51 1 11. 2 L 7 4 4F RT 4A25 1998031200473 19980312 00473 WP 1998 3 12 UPS98826008 1 19980127 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 60-70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK CORROSION BETWEEN LAV SUB FLOOR, FLOORBEAMS AND SEAT TRACK, LAV AREA STA 60-70. REMOVED CORROSION FOUND CRACK FLOORBEAM STA 55 RBL 33. REMOVED DAMAGED AREA FABBED REPAIR FILLER AND ANGLE AND INSTALLED PER REO 4350. A LODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. 2 L 7 4 4F RT 4A25 1998031200474 19980312 00474 WP 1998 3 12 UPS98826009 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK SEAT TRACK B-C CORRODED AT STA 1240. REMOVED DAMAGED TRACK STA 1190 TO 1270. FABRICATED AND INSTA LLED NEW TRACK IAW DC8 SRM 51 3 0 AND 51 1 8 AND 53 2 3. 2 L 7 4 4F RT 4A25 1998031200475 19980312 00475 WP 1998 3 12 UPS98826010 1 19980127 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 640-660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, CORROISON ON LONGERON 31 RIGHT BETWEEN STA 640 AND 660. REMOVED CORROSION FABBED REPAIR STRAP PER REO 04338. ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED STRAP IAW DC8 SRM 5 1 1 20D AND 51 1 16. 2 L 7 4 4F RT 4A25 1998031200476 19980312 00476 WP 1998 3 12 UPS98826011 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 516-530 CORORDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, CABIN SEAT TRACK CORRODED STA 516-530. REMOVED SEAT TRACK STA 410 590. FABBED NEW SPLICES, DRILL ED NEW TRACK IAW DC8 SRM 53 3 2 AND 53 21 0. INSTALLED IAW DC8 SRM 53 2 3 AND 51 1 8 AND 51 3 0. 2 L 7 4 4F RT 4A25 1998031200477 19980312 00477 WP 1998 3 12 UPS98826012 1 19980123 A 5311 FRAME DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, FLC STA TO FRAME CORRODED BETWEEN LONGERON 27 RIGHT AND LONGERON 26 RIGHT. FABBED DOUBLER IAW DC8 SRM 53 2 58 FIG 8C-2 AND REO 04362, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51 1 8. INSTALLED DOUBLER IAW DC8 SRM 51 1 11 AND 51 1 20D AND 51 1 21. 2 L 7 4 4F RT 4A25 1998031200478 19980312 00478 WP 1998 3 12 UPS98826013 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 270 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, CABIN SEAT TRACK I IS GOUGED WORN AND CORRODED STA 270. REMOVED SEAT TRACK PLUG PRIMED SEAT TRACK PLUG IAW DC8 SRM 51 1 8. INSTALLED NEW SEAT TRACK PLUG IAW DC8 SRM 53 2 3. 2 L 7 4 4F RT 4A25 1998031200479 19980312 00479 WP 1998 3 12 UPS98826014 1 19980124 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, FWD LWR CARGO COMPT X SLIDE DOOR AREA BATH TUB FITTING CORRODED STA 300 L AT L32 L. FABRICATED RE PAIR ANGLES IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998031200480 19980312 00480 WP 1998 3 12 UPS98826015 1 19980124 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, FWD LWR CARGO COMPT ZX SLIDE AREA BATH TUB FITTING CORRODED AT STA 340L AT L29L. REMOVED CORROSIO N FROM FITTING IAW DC8 SRM 53 2 0. REMOVED CORRODED FITTING MATERIAL ID REPAIR ANGLE 7075 T6 .125 PO 249743 IAW DC8 SRM 53 2 0. RECEIVED FITTING FROM CUSTOMER TAG 00233648. FABRICATED REPAIR ANGLE IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998031200481 19980312 00481 WP 1998 3 12 UPS98826016 1 19980124 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE:D/CK, LWR FWD CARGO COMPT STA 300.000 LONGERON 29 LEFT TO 28L. CORRODED BATH TUB FITTING. REMOVED CORR ODED FITTING, FABRICATED REPAIR ANGLES AND CUT NEW FITTING IAW DC8 SRM 53 2 0. DRILLED NEW FITTING AND REPAIR ANGLES IA W DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED REPAIR ANGLES AND NEW FITTING IAW DC8 SRM 53 2 0 A ND 51 1 20D. 2 L 7 4 4F RT 4A25 1998031200482 19980312 00482 NM 1998 3 12 QXEA9800233 1 19980302 A 3234 570425 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTION A QXEA K NONE N FALSE WARNING AP APPROACH 1 NM 09 818PH 58 LEFT LANDING GEAR AMBER LIGHT ILLUMINATED, EXTENDED GEAR AND THE LEFT RED MAIN GEAR LIGHT ILLUMINATED. VISUAL INSPECTIO N NOTED THE LEFT MAIN GEAR FORWARD DOOR FULLY OPEN, AND THE REMAINING LEFT GEAR DOORS OPEN PARTLY. REPLACED THE MAIN LA NDING GEAR SELECTOR VALVE, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998031200483 19980312 00483 EU 1998 3 12 QXEA9800236 1 19980302 A 5210 HOOK LATCHES FOKKER F28 F28MK4000 4990810 EU PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 482US 11231 PDX - MAIN CABIN DOOR IS HARD TO OPEN AND LOCK. CLEANED THE CABIN DOOR HOOK LATCHES. OPERATIONAL CHECKS GOOD. AIRCRAF T RETURNED TO SERVICE. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998031200484 19980312 00484 NM 1998 3 12 98FDEA00155 1 19980305 A 5320 65163169 CHORD BOEING 727 72722C 138400F NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 CORROSION (C53-224-03, 1, 2) ON UNDERSIDE OF TOP CHORD BS 344, RBL 16, WL 207 AROUND HI-LOCK, AND AT RBL 31, WL 208. *S /D* REMOVED CORROSION ON UNDERSIDE OF TOP CHORD BS 344, RBL 16, WL 207. CORROSION FOUND TO BE WITHIN LIMITS PER FED-EX SRM 53-10-1. REMOVED CORROSION AT BS 344, RBL 31, WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPAIRED CORROSION DAMAGE AT BS 344, RBL 31, WL 208 PER FED-EX SRM 53-10-8. 2 L 7 3 4F A3WE 1998031200485 19980312 00485 NM 1998 3 12 98FDEA00156 1 19980305 A 5320 65192921 WEB BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 CORROSION (C53-132-02-1/2) ON WEB BS 870, RBL 65 LBL 65, WL 178 TO 148. *S/D* REMOVED AND REPLACED 870 CENTER TANK WEB PER FED-EX EA 7-5710-38738. 2 L 7 3 4F A3WE 1998031200486 19980312 00486 NM 1998 3 12 98FDEA00157 1 19980305 A 5711 65185371 SPAR CHORD BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 CORROSION (C53-132-02-1/2) ON LOWER REAR SPAR CHORD BS 870, LBL 65 TO RBL 65, WL 148. *S/D* REMOVED AND REPLACED LWR S PAR CHORD BS 870 LBL 65 - RBL 65 WL 148 PER FEDEX EA 7-5710-38738. 2 L 7 3 4F A3WE 1998031200487 19980312 00487 NM 1998 3 12 98FDEA00158 1 19980305 A 5711 65185381 SPAR CHORD BOEING 727 72722C 138400F NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 CORROSION (C53-132-02-1/2) ON UPPER REAR SPAR CHORD BS 870, LBL 65 - RBL 65, WL 178. *S/D* REMOVED AND REPLACED UPPER REAR SPAR CHORD BS 870 LBL 65 - RBL 65 WL 178 PER FEDEX EA 7-5710-38738. 2 L 7 3 4F A3WE 1998031200488 19980312 00488 WP 1998 3 12 98FDEA00159 1 19980305 A 5312 BULKHEAD TEE DOUG DC10 DC1010F 3022111 WP BS 1156 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 N00474, Y-1156 PRESS BULKHEAD TEE-CAP RT END HAS TWO CRACKS IN LONG 39 AREA. FIRST CRACK MOVES DOWN CANTED VERT LEG TO RADIUS (2.4). SECOND MOVES DOWN CANTED VERT LEG THROUGH RADIUS AND AFT IN AFT HORIZ. LEG AND DISAPPEARS UNDER FITTING ( 2 VISIBLE). MODIFY RIGHT BULKHEAD TEE CAP AT STA Y-1156 PER EO 8-5310-7-3327 PART 4 AND EA 8-5310-35937. 2 L 7 3 4F A22WE 1998031200489 19980312 00489 NM 1998 3 12 98FDEA00160 1 19980306 A 3260 SWITCH BOEING 727 72722 1384002 NM RT MLG DOOR DIRTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 198FE 19154 98-0059 ON TAKEOFF, RIGHT MAIN GEAR DOOR LIGHT CAME ON AND WOULD NOT GO OFF. CYCLED GEAR, LIGHT WENT OUT. INSPECTED AN D CLEANED RIGHT MAIN GEAR DOOR SWITCH. CYCLED DOOR SEVERAL TIMES. OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1998031200490 19980312 00490 WP 1998 3 12 MWEA98279 1 19980306 A 5720 DOUBLER DOUG DC9 DC932 3022066 WP WS 408 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND DENT ON LEFT WING INTERNAL LEADING EDGE DOUBLER STA XRS408. MAINTENANCE REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 1998031200491 19980312 00491 NM 1998 3 12 DL73K980508 1 19980303 A 5330 SKIN BOEING 737 737232 1384475 NM L2 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 FOUND DURING P-2 LETTER CHECK, 1.375 INCH CRACK IN FUSELAGE SKIN AT L-2 DOOR CUTOUT LWR FWD CORNER. INSTALLED TIME LIMI TED REPAIR PER SRM 53-30-3 FIG 24 AND ERA. 2 L 7 2 4F RT A16WE 1998031200492 19980312 00492 NM 1998 3 12 DL72S980511 1 19980303 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 470DA 13018 20747 EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACKS. 2 L 7 3 4F A3WE 1998031200493 19980312 00493 NE 1998 3 12 DL757980512 2 19980303 A 7530 3800035117 ACTUATOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENG CRACKED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 647DL 24218 DURING CLIMB-OUT, LEFT ENG WOULD NOT REACH COMMANDED CLIMB EPR N2 IND 100 FF MATCHED RT ENG EVENT RECORD PUSHED AT HIGHE R ALT. LEFT ENG EPR IND CONT TO FALL OFF OIL TEMP REACHED 129. REPLACED STATOR VANE ACTUATOR AND BRACKET. 2 L 7 2 4F 4 F RT A2NM E17NE 1998031200494 19980312 00494 NM 1998 3 12 DL72W980513 1 19980303 A 5330 65562312 SKIN BOEING 727 727247 138408F NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FUSELAGE SKIN R1 DOOR CUTOUT SURROUND UPPER HINGE CUTOUT, CRACK REPAIR. THE UPPER HINGE CUTOUT OF THE R1 DOOR CUTOUT WA S FOUND WITH A TYPICAL CRACK IN THE UNDERLYING REINFORCING DOUBLER (BEAR STRAP). THE SKIN WAS LOCALLY CUTOUT TO ACCESS THE CRACK ANDTHE CRACK WAS TRIMMED OUT OF THE BEAR STRAP. AN EXTERNAL DOUBLER/TRIPLER REPAIR WAS INSTALLED PER THE GU IDELINES OF BOEING S/B 727-53-0136 AND DOCUMENTED PER ER/A 364162-14. 2 L 7 3 4F A3WE 1998031200495 19980312 00495 NM 1998 3 12 DL76L980514 1 19980303 A 3350 LIGHTS BPS73 BOEING 767 767332 1382001 NM CABIN MALFUNCTIONED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 180DN 24732AND26 25985 LOG SHEET ITEM WHEN EMERGENCY LIGHTS SELECTED TO ARMED POSITION EMERGENCY FLOOR TRACK LIGHTS FROM ROW 14 TO RUN 36 REMAI NED ON. UPON A/C ARRIVAL ALL EMERG LIGHTS WERE OPERATING NORM. VERIFIED PROPER TEST AND CONTROL LOGIC SIGNAL AT D9047 AND D1088, ALL CKD GOOD. VISUALLY INSPECTED COCKPIT EMERG LIGHT SW AND ASSOC WIRING, NO TROUBLE FOUND. UNABLE TO DUPLI CATE FAULT. REPLACED PWR SUPPLIES M9009 AND M737 PRECAUTIONARY. EMERG LIGHTS CK NORM. CATEGORY 'E': PROBLEMS WITH SY STEMS CRITICAL TO ETOPS. 2 L 7 2 4F RT A1NM 1998031200496 19980312 00496 NM 1998 3 12 DL72S980515 1 19980304 A 5520 FITTING BOEING 727 727232 1384082 NM RT ELEV CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 FOUND AT F2 LETTER CHECK, RT ELEVATOR HINGE SUPPORT FITTING CRACKED BETWEEN NR 2 AND NR 3 BALANCE PANELS STA 99.79. REP AIRED PER M/M 55-10-31 AND ERA 364184-14. 2 L 7 3 4F A3WE 1998031200497 19980312 00497 WP 1998 3 12 DLL14980516 1 19980304 A 3350 POWER SUPPLY 672320101 LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 741DA 38046 193C1245 EMERGENCY TRACK LIGHTING OUT AFTER 20 SEC IN F/C CABIN. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998031200498 19980312 00498 NM 1998 3 12 DL72S980517 1 19980225 A 5320 WEB BOEING 727 727232 1384082 NM RIGHT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 DUPLICATE ORIGINAL SOILED. INSIDE ACCESS 9504 3RD BAY DOWN VERTICAL WEB IS CRACKED AT 2 LOC ON RT SIDE. REMOVED SECTIO N OF ANTI-ICE DUCT AND X BRACE FOR ACCESS. FAB REPAIR DOUBLER PER SRM 53-10-4 FIG 17. STOP DRILLED CRACK AND DYE CHECK ED PER SRM 53-10-4. OK TO INSTALL. INSTALLED DOUBLER PER SRM 53-10-4 FIG 17. INSTALLED ANTI-ICE DUCT AND X BRACE. 2 L 7 3 4F A3WE 1998031200499 19980312 00499 NM 1998 3 12 DL72S980518 1 19980225 A 5320 WEB BOEING 727 727232 1384082 NM LEFT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 INSIDE ACCESS 9504 3RD BAY DOWN VERTICAL WEB IS CRACKED ON LT SIDE. FAB REPAIR DOUBLER PER SRM 53-10-4 FIG 17. STOP DR ILLED CRACK AND DYE CHECK PER SRM 53-10-4. OK TO INSTALL DOUBLER. INSTALLED DOUBLER. 2 L 7 3 4F A3WE 1998031200500 19980312 00500 WP 1998 3 12 DLL14980519 1 19980304 A 3350 GROUND LKHEED 1011 1011385115 5265015 WP CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 736DY 193C1227 ON L/O, FOUND RT SECTION D FLOOR TRACK LIGHTING INOP. SWAPPED BATTERIES AND CONTROLLER, NO HELP. SWAPPED CHARGERS, NO HELP. RANG OUT WIRES AND FOUND LOOSE GROUND STUDS, TIGHTENED. OPS CK GOOD. 2 L 7 3 4F A23WE 1998031200501 19980312 00501 NM 1998 3 12 DL76S980522 1 19980213 A 3340 BULB 311 BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 120DL 23279 EXTERIOR EMERG LIGHT AFT OF WING INOP, LEFT SIDE. RELAMPED, CK GOOD. 2 L 7 2 4F RT A1NM 1998031200503 19980312 00503 NM 1998 3 12 VNAA9803004 1 19980302 A 3040 4298809AMDTA WIPER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT LACK OF LUBE A VNAA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 442JS 3060 THE RIGHT HAND WINDSCREEN WIPER FAILED TO STOW, ON THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTE NANCE INSPECTED AND LUBRICATED THE WINDSCREEN WITH WATER. OPERATION CHECKS WERE COMPLETED IN ACCORDANCE WITH DORNIER MA INTENANCE MANUAL 30-41-00. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031200504 19980312 00504 WP 1998 3 12 VJ9800038 1 19980306 A 2560 702957A SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR INOPERATIVE A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 949VV 47484 GALLEY DOOR SLIDE FELL OFF. REINSTALLED SLIDE IAW MM 2560 AND PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998031200505 19980312 00505 NM 1998 3 12 9803726613 1 19980204 A 5330 SKIN BOEING 747 747251B 1384892 NM BS 2020 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 613US 20358 DURING PERIODIC CHECK, FOUND CORROSION ON SKIN AT FS 2020 BETWEEN STR 43R TO 44R. REPAIRED PER EA 66-154323. 2 L 7 4 4F A20WE 1998031200506 19980312 00506 WP 1998 3 12 9803739905 1 19980116 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 160 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CRACK IN FRAME AT FS 160, LONGERON 29L. REPAIRED PER EA 99-154682. 2 L 7 2 4F A6WE 1998031200507 19980312 00507 WP 1998 3 12 9803749905 1 19980227 A 5720 FITTING DOUG DC9 DC931 3022065 WP BS 606 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 955N 47160 DURING H-CHECK, FOUND CRACK IN FRONT SPAR TO FRAME ATTACH FITTING AT FS 606 JUST ABOVE LONGERON 24L. REPAIRED PER EA 99 -154728. 2 L 7 2 4F A6WE 1998031200508 19980312 00508 WP 1998 3 12 9803759941 1 19980302 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 937 996 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CORROSION ON SKIN PANEL AT FS 937 TO 996, LONGERON 21R TO 26R. REPAIRED PER EA 99-154595. 2 L 7 2 4F A6WE 1998031200509 19980312 00509 WP 1998 3 12 9803769952 1 19980211 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 47144 DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 83. REPAIRED PER EA 99-154674. 2 L 7 2 4F A6WE 1998031200510 19980312 00510 WP 1998 3 12 9803779957 1 19980131 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 218 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CRACK IN MAIN CABIN SHEAR WEB AT FS 218, LBL 44.5. REPAIRED PER EA 99-154966. 2 L 7 2 4F A6WE 1998031200511 19980312 00511 WP 1998 3 12 9803789957 1 19980204 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 200 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CRACK IN FUSELAGE SKIN AT DOOR STOP ADJUST HOLE TOP AFT HOLE FS 200. REPAIRED PER EA 99-154970. 2 L 7 2 4F A6WE 1998031200512 19980312 00512 WP 1998 3 12 9803799957 1 19980131 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CRACK IN SKIN DOUBLER AT 83.5, RBL 11. REPAIRED PER EA 99-154966. 2 L 7 2 4F A6WE 1998031200513 19980312 00513 WP 1998 3 12 9803809957 1 19980131 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CRACK IN FUSELAGE SKIN INTERIOR AT THE PILOT'S WINDSHIELD WIPER MOTOR CAVITY FS 83.5 LBL 10. REPA IRED PER EA 99-154966. 2 L 7 2 4F A6WE 1998031200514 19980312 00514 WP 1998 3 12 9803819957 1 19980206 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1143-1168 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CORROSION ON INTERIOR SKIN BETWEEN CANTED FRAMES AT FS 1143 TO 1168, LONGERON 9R TO 22R. REPAIRED PER EA 99-154176. 2 L 7 2 4F A6WE 1998031200515 19980312 00515 WP 1998 3 12 9803829957 1 19980206 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1143-1168 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CORROSION ON INTERIOR SKIN BETWEEN CANTED FRAMES AT FS 1143 TO 1168, LONGERON 9L TO 22L. REPAIRED PER EA 99-154176. 2 L 7 2 4F A6WE 1998031200516 19980312 00516 WP 1998 3 12 9803839957 1 19980211 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 465 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 915RW 47139 DURING M-CHECK, FOUND CORROSION ON AFT SIDE OF FRAME AT FS 465, LONGERON 28L. REPAIRED PER EA 99-154972. 2 L 7 2 4F A6WE 1998031200517 19980312 00517 NM 1998 3 12 9803846718 1 19980127 A 5711 SPAR WEB BOEING 747 747251F 1384898 NM WS 997-1001 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR WEB AT THE LOWER CHORD FS 997 TO 1001. REPAIRED PER EA 67-153201. 2 L 7 4 4F A20WE 1998031200518 19980312 00518 NM 1998 3 12 9803856718 1 19980127 A 5711 SPAR WEB BOEING 747 747251F 1384898 NM WS 1014-1018 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR WEB AT THE LOWER CHORD FS 1014 TO 1018. REPAIRED PER EA 67-153201. 2 L 7 4 4F A20WE 1998031200519 19980312 00519 NM 1998 3 12 9803862711 1 19980117 A 5314 KEEL BEAM BOEING 727 7272S7 138407Z NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 715RC 22019 DURING M-CHECK, FOUND CORROSION ON KEEL BEAM AT STR 29R, FS 950. REPAIRED PER EA 27-154482. 2 L 7 3 4F A3WE 1998031200520 19980312 00520 WP 1998 3 12 9803879931 1 19980115 A 5312 BULKHEAD SKIN DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE UPPER DOOR CUTOUT 1.75 CEN TER LINE. REPAIRED PER EA 99-154161. 2 L 7 2 4F A6WE 1998031200521 19980312 00521 WP 1998 3 12 9803889931 1 19980214 A 5312 BULKHEAD SKIN DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACK IN THE AFT PRESSURE BULKHEAD SKIN AT THE UPPER DOOR CUTOUT 11.5 RIG HT OF CENTER LINE. REPAIRED PER EA 99-154161. 2 L 7 2 4F A6WE 1998031200522 19980312 00522 WP 1998 3 12 9803899931 1 19980214 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACKS IN THE -71 DOUBLER AT THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT. REPAIRED PER EA 99-154161. 2 L 7 2 4F A6WE 1998031200523 19980312 00523 WP 1998 3 12 9803909931 1 19980209 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACK IN THE -9 DOUBLER AT THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT. R EPAIRED PER EA 99-154161. 2 L 7 2 4F A6WE 1998031200524 19980312 00524 WP 1998 3 12 9803919931 1 19980209 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 47244 DURING AFT PRESSURE BULKHEAD INSPECTION, FOUND CRACKS IN THE AFT PRESSURE BULKHEAD UPPER DOOR CUTOUT -13 DOUBLER. REPAI RED PER EA 99-154161. 2 L 7 2 4F A6WE 1998031200525 19980312 00525 WP 1998 3 12 9803921148 1 19980202 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1521 1532 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 148US 46757 DURING PERIODIC CHECK, FOUND CORROSION ON FUSELAGE EXTERNAL SKIN AT FS 1521 TO 1532, LBL 5 TO RBL 3, LONGERON 48L AND 48 R. REPAIRED PER EA 11-154367. 2 L 7 3 4F A22WE 1998031200526 19980312 00526 WP 1998 3 12 9803931148 1 19980116 A 5320 PRESSURE WEB DOUG DC10 DC1040 3023508 WP BS 495 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 148US 46757 DURING PERIODIC CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL RIGHT PRESSURE PANEL WEB FS 495. REPAIRED PER EA 11- 153941. 2 L 7 3 4F A22WE 1998031200527 19980312 00527 NM 1998 3 12 9803946301 1 19980308 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 661US 23719 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51H- TO 9H, ROWS 51C TO 52C, ROW 66C, AND AT DOOR 3L. RECONNECTED LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998031200528 19980312 00528 WP 1998 3 12 9803959101 1 19980226 A 5210 DOUBLER DOUG DC9 DC915 3022036 WP PAX DOOR OVERSIZED A NWAA K NONE W INADEQUATE Q C UK UNKNOWN 1 GL 01 91S 47063 FORWARD CABIN DOOR WOULD NOT OPEN USING INTERIOR HANDLE. MAINTENANCE FOUND DOUBLER CONTACTING HANDLE ON OUTSIDE OF DOOR . BURNISHED DOUBLER, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998031200529 19980312 00529 NE 1998 3 12 9803969875 2 19980307 A 7261 OIL FILTER DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE DIRTY A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 784NC 48109 688294 DURING CLIMB, THE RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. CREW REDUCED POWER ON THE RIGHT ENGINE AND THE LIGH T EXTINGUISHED. THE AIRCRAFT DIVERTED TO MKE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGIN E MAIN OIL FILTER. 2 L 7 2 4F 4 F RT A6WE E2EA 1998031200530 19980312 00530 NM 1998 3 12 9803972710 1 19980307 A 7722 RESISTOR BOEING 727 727235 138408B NM PWA JT8 JT8D15A 52051 NE E/E COMPT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 820EA 22557 695247 DURING TAKEOFF ROLL AT 40 KNOTS, THE NR 2 ENGINE EGT INDICATION WAS BELOW NORMAL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 ENGINE EGT INDICATOR AND BALLAST REESISTOR. ENGINE OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998031200531 19980312 00531 WP 1998 3 12 9803989603 1 19980305 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 603NW 47101 DURING LINE MAINTENANCE INSPECTION, FOUND CABIN EMERGENCY LIGHTS BETWEEN ROWS 16 THRU 20 INOPERATIVE. REPLACED BATTERIE S IN PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031200532 19980312 00532 SO 1998 3 12 COMA9810055 1 19980304 A 5320 30005567008 TCAS TRAY EMB 120 EMB120RT SO FWD FUSE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION ZONE 100 TASK 5310-132-01I, FOUND TCAS SUPPORT TRAY CORRODED BEYOND LIMITS. REMOVED CORRODED TRAY AND BUILT UP NEW SERV TRAY IAW STC ST00075W1-D. 2 L 7 2 4T RT A31SO 1998031200533 19980312 00533 SO 1998 3 12 COMA9810056 1 19980304 A 5320 12006664005 SILL EMB 120 EMB120RT SO LT CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION, TASK 5310-131-01I, REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SI LL AND INSTALLED SERVICEABLE SILL USING EMBRAER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998031200534 19980312 00534 SO 1998 3 12 COMA9810057 1 19980304 A 5320 12004450001 SILL EMB 120 EMB120RT SO CABIN CORROSION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CABIN SILL TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED SIL L AND INSTALLED SERVICEABLE SILL USING EMBRAER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998031200535 19980312 00535 SO 1998 3 12 COMA9810058 1 19980304 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO CABIN CORROSION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED THE CROSSBEAM AT FRAME 16 TO BE CORRODED BEYOND EMBRAER CORROSION LIMIT S. REMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMBRAER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998031200536 19980312 00536 SO 1998 3 12 COMA9810059 1 19980304 A 5320 12004149001 CROSSBEAM EMB 120 EMB120RT SO CABIN CORROSION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CROSSBEAM AT FRAME 20 TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. R EMOVED CROSSBEAM AND INSTALLED SERVICEABLE CROSSBEAM USING EMBRAER 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998031200537 19980312 00537 SO 1998 3 12 COMA9810060 1 19980304 A 5320 12046158003 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORROSION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP THAT WAS CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED B UTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998031200538 19980312 00538 SO 1998 3 12 COMA9810061 1 19980304 A 5320 12046163003 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORROSION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOVED BUTT STRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998031200539 19980312 00539 SO 1998 3 12 COMA9810062 1 19980304 A 5320 12005805008 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORROSION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 120211 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTSTRAP TO BE CORRODED BEYOND EMBRAER CORROSION LIMITS. REMOV ED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMBRAER 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998031200540 19980312 00540 NE 1998 3 12 COMA9810063 2 19980306 A 7321 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 241CA 120211 TORQUE INDICATION FLUCTUATED +- 20 PERCENT DURING TAKEOFF ROLL. DEFERRED THE ELECTRONIC ENGINE CONTROL SYSTEM. 2 L 7 2 4T 4 T RT A31SO E20NE 1998031200541 19980312 00541 EA 1998 3 12 COMA9860051 1 19980306 A 3397 59465 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951CA 7091 EMERGENCY LIGHTS INOP ROWS 2 THRU 5. REPLACED EMERGENCY LIGHT POWER STRIP. 2 L 7 2 4F RT A21EA 1998031200542 19980312 00542 EA 1998 3 12 COMA9860052 1 19980306 A 3350 362624 LAMP CNDAIR CL600 CL6002B19 EA CABIN SHORTED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 964CA 7129 EMERGENCY FLOOR LIGHTING INOP ROW 2 THRU 8. REPLACED TRACK LIGHTING. 2 L 7 2 4F RT A21EA 1998031200543 19980312 00543 EA 1998 3 12 COMA9860053 1 19980308 A 3250 STEERING CNDAIR CL600 CL6002B19 EA NLG OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 917CA 7017 NOSE WHEEL STEERING FAILED DURING TAKEOFF ROLL. ADJUSTED NWS RIGGING. 2 L 7 2 4F RT A21EA 1998031200544 19980312 00544 NM 1998 3 12 SWAA980196 1 19980306 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727-908 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED SC CHECK, PERFORMED MOD TO SKIN LAP FROM BS 727 TO 908 AT S10L, 10R, 4R, AND 4L. INSTALLED REPAIR DOUB LERS PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998031200545 19980312 00545 NM 1998 3 12 SWAA980197 1 19980306 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 360-540 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED SC CHECK, PERFORMED MOD TO SKIN LAP FROM BS 360 TO 540, AT S14L, 4R, 10L AND 10R. INSTALLED REPAIR DOU BLERS PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998031200546 19980312 00546 NM 1998 3 12 SWAA980198 1 19980306 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 908-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED SC CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED AT BS 908 TO 947, AT S14 RT AND LT. REPAIRED PER SWA A CO 6717-53. 2 L 7 2 4F A16WE 1998031200547 19980312 00547 NM 1998 3 12 SWAA980199 1 19980306 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 947-1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED SC CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED AT BS 1006, 986 TO 1016, AND 908 TO 947. REPAIRED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998031200548 19980312 00548 NM 1998 3 12 SWAA980200 1 19980217 A 2782 65446519 ACTUATOR BOEING 737 7372H4 138448C NM NR 3 LE FLAP FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 74SW 22674 AFTER TAKEOFF, NR 3 L/E SLAT WOULD NOT FULLY RETRACT. AIRCRAFT RETURNED TO TPA AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 3 L/E SLAT ACTUATOR PER BOEING M/M. 2 L 7 2 4F A16WE 1998031200549 19980312 00549 NM 1998 3 12 SWAA980201 1 19980219 A 2612 896768 FIRE LOOP BOEING 737 7372H4 138448C NM APU MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 105SW 23249 IN FLIGHT, APU FIRE WARNING SOUNDED. PERFORMED FIRE PROCEDURES AND ACTIVATED FIRE BOTTLES. AIRCRAFT RETURNED TO HOU AN D MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. CONTINUED PER MEL. REMOV ED AND REPLACED APU TAILPIPE FIRE DETECTOR PER BOEING M/M. 2 L 7 2 4F A16WE 1998031200550 19980312 00550 NM 1998 3 12 SWAA980202 1 19980304 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED RON, FOUND A FUSE SKIN CRACK APPROX 8 BEHIND WING ILLUMINATION LIGHT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998031200551 19980312 00551 1998 3 12 SWAA980203 4 19980219 A 2565 D31354105 SLIDE BOEING 737 7372T4 1384492 NM CABIN LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING WALKAROUND CHECK, FOUND AFT ENTRY DOOR ESCAPE SLIDE PRESS LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1998031200552 19980312 00552 1998 3 12 SWAA980204 4 19980305 A 2565 22D22900131 SLIDE BOEING 737 7372T4 1384492 NM CABIN LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22054 DURING SC, FOUND FWD SERVICE DOOR ESCAPE SLIDE PRESS LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1998031200553 19980312 00553 NM 1998 3 12 SWAA980205 1 19980219 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 944 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702ML 22340 DURING SCHEDULED C3, FOUND FUSE SKIN CRACKED AT BS 944, AT S24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998031200554 19980312 00554 NM 1998 3 12 SWAA980206 1 19980304 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED C3, FOUND FUSE SKIN CRACKED RT SIDE ABOVE T/E FLAPS. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998031200555 19980312 00555 NM 1998 3 12 SWAA980207 1 19980219 A 5330 SKIN BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED C3, FOUND AFT GALLEY DOORWAY LOWER HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200556 19980312 00556 NM 1998 3 12 SWAA980208 1 19980304 A 5330 SKIN BOEING 737 7373H4 1384600 NM CARGO DOORWAY DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED RON, FOUND FUSELAGE DENTED BELOW AFT CARGO DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200557 19980312 00557 NM 1998 3 12 SWAA980209 1 19980305 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED SEVERAL PLACES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200558 19980312 00558 NM 1998 3 12 SWAA980210 1 19980305 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 380, S24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200559 19980312 00559 NM 1998 3 12 SWAA980211 1 19980305 A 5330 SKIN BOEING 737 7373T5 NM R1 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 26598 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER AFT R1 DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200560 19980312 00560 NM 1998 3 12 SWAA980212 1 19980219 A 5330 SKIN BOEING 737 7373T5 NM BS 470/480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 470 AND 480. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200561 19980312 00561 NM 1998 3 12 SWAA980213 1 19980216 A 5330 SKIN BOEING 737 7373T5 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN DENTED AT BS 500A, S23L AND AT BS 463. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200562 19980312 00562 NM 1998 3 12 SWAA980214 1 19980216 A 5330 SKIN BOEING 737 7373T5 NM BS 470-490 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CUTOUT CRACKED BETWEEN BS 470 AND 490. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031200563 19980312 00563 1998 3 12 SWAA980215 4 19980302 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM CABIN LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 509SW 24186 DURING RON, FOUND AFT SERVICE DOOR ESCAPE SLIDE PRESS LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998031200564 19980312 00564 NM 1998 3 12 SWAA980216 1 19980301 A 3610 1074923 REGULATOR BOEING 737 7373H4 1384600 NM NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 358SW 26595 RETURNED TO DAL DUE TO NOT BEING ABLE TO MAINTAIN CABIN PRESSURE. REPLACED NR 2 ENGINE BLEED AIR REGULATOR PER BOEING M /M. 2 L 7 2 4F RT A16WE 1998031200565 19980312 00565 NM 1998 3 12 SWAA980217 1 19980227 A 3350 20121 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED T-CHECK, FOUND AFT EMERGENCY EXIT O/B LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1998031200566 19980312 00566 NM 1998 3 12 UPS98426028 1 19980309 A 2612 FIRE WARNING BOEING 747 747123 1384873 NM CARGO COMPT ACTIVATED A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 675UP 20390 INSPECTION TYPE-N/A, WHILE AT CRUISE ALT FL 350 FLT EXPERENCED MASTER WARNING CARGO FIRE AT ZONE NR 4. SILENCED BELL TO RESET SYSTEM AND RUN CHECK LIST. A/C HAD VARIOUS HAZ MATS IN POSITION NR 14L CLOSE ENOUGH TO NR 4 TO DECLARE EMERGENCY LANDING INTO CYWC ON FINAL INTO CYWC THE CARGO AND ZONE NR 4 WENT OUT, ONCE ON GROUND EMERG CREWS FOUND NO SMOKE OR FIR E. NO ACTION TAKEN AT THIS REPORT TIME. 2 L 7 4 4F A20WE 1998031200567 19980312 00567 WP 1998 3 12 UPS98825987 1 19980126 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, FRAME CRACKED FUSELAGE STATION 220 L36 FWD FACE. REMOVED BOTTOM CRACKED PART OF FRAME, FABBED DOU BLER, FILLER AND STRAP AND INSTALLED REPAIR PIECES IAW REO 04355 AND DC8 SRM 51-1-21 AND 51-1-8. 2 L 7 4 4F RT 4A25 1998031200568 19980312 00568 WP 1998 3 12 UPS98826005 1 19980219 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1710-1730 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, FLOORBEAM INTERCOSTAL AT STA 1710 TO 1730 RBL 12 HAS CORROSION. FABRICATED SUPPORT IAW DAC DWG 57 55032, ALODINED AND PRIMED NEW SUPPORT. INSTALLED NEW SUPPORT IAW DC8 SRM 51-1-21 AND 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998031200569 19980312 00569 WP 1998 3 12 UPS98826026 1 19980226 A 5320 37502571N SPLICE DOUG DC8 DC871F 302199D WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 1040 TO 1060 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998031200570 19980312 00570 NM 1998 3 12 QXEA9800232 1 19980303 A 3260 XDN4 RELAY DHAV DHC8 DHC8202 2809007 NM RELAY PANEL MALFUNCTION A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 346PH 477 LANDING GEAR UNSAFE LIGHT ON AFTER RETRACTION. LEFT DOOR ADVISORY LIGHT WAS ALSO ON, WITH A VISUAL CONFIRMATION OF THE LEFT DOOR BEING OPEN. INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT FROM PSC TO PDX. IN PDX REPLACED THE 3261-K14 RELAY FOR THE PSEU, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998031200571 19980312 00571 NM 1998 3 12 QXEA9800234 1 19980303 A 2121 FAN DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 823PH 110 ELECTRIC SMELL NOTED IN THE COCKPIT DURING EN ROUTE AND LANDING PHASE OF FLIGHT. ALL ELECTRICAL LOADS APPEAR TO BE NORM AL, WITH NO POPPED CIRCUIT BREAKERS. INSPECTED AND FOUND HGS-DEU COOLING FAN BAD. PLACED ON MEL 34-24. AIRCRAFT RETUR NED TO SERVICE. MEL CLEARED BY RUNNING THE HGS FAN FOR SEVERAL MINUTES WITH NO ELECTRICAL SMELL NOTED. PERFORMED CAT I II CHECK OF THE HGS SYSTEM, ALL CHECKS OK. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998031200572 19980312 00572 EU 1998 3 12 QXEA9800235 1 19980303 A 2997 WIRE FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 491US 11156 BURNING SMELL NOTED IN THE COCKPIT, ALONG WITH A FLASH AND A POPPING SOUND BELOW THE FIRST OFFICER'S SMOKE MASK AREA. R EPAIRED THE SUPPLY WIRE TO THE NR 2 AC HYDRAULIC PUMP CONTROL RELAY 2MC2-142. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998031200573 19980312 00573 EU 1998 3 12 QXEA9800237 1 19980304 A 3350 5515900004 BULB GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 483US 11233 EMERGENCY EXIT SIGN AT ROW 8 HAS A BURNT BULB. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031200574 19980312 00574 EU 1998 3 12 QXEA9800238 1 19980304 A 3350 551590004 BULB GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 483US 11233 EMERGENCY EXIT SIGN AT FORWARD CLOSET HAS A BURNT OUT LAMP. REPLACED LAMP ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031200575 19980312 00575 EU 1998 3 12 QXEA9800239 1 19980304 A 3350 1315 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 COCKPIT OVERHEAD EMERGENCY EXIT SIGN HAS INOP BULBS. REPLACED BULBS, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031200576 19980312 00576 NM 1998 3 12 98FDEA00161 1 19980307 A 5754 652167224 PANEL BOEING 727 727232 1384082 NM NR 7 LE SLAT MISSING A FDEA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 499FE 21018 NR 7 LEADING EDGE SLAT ACTUATOR DOOR MISSING. * S/D* REPLACED AND ADJUSTED NR 7 SLAT ACTUATOR DOOR PER MAINTENANCE M ANUAL 27-81-32, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1998031200577 19980312 00577 NM 1998 3 12 98FDEA00162 1 19980306 A 5311 651593340 FRAME BOEING 727 727227 1384078 NM BS 600 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 CRACK IN FRAME AT FASTENER HOLE BS 600, RBL 3, WL 157. *S/D* REPAIRED FRAME AT BS 600, RBL 3, WL 157 IAW FED-EX SRM 51 -40-3. 2 L 7 3 4F A3WE 1998031200578 19980312 00578 NM 1998 3 12 98FDEA00163 1 19980306 A 5311 6516342 FRAME BOEING 727 727227 1384078 NM BS 1030 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 AFT BAY TOP OF FRAME DENTED AT BS 1030, RBL 28, WL 145. *S/D* REMOVED DAMAGED AREA AND REPAIRED FRAME AT BS 1030, RBL 28, WL 145 IAW FED-EX SRM 51-40-3. 2 L 7 3 4F A3WE 1998031200579 19980312 00579 NM 1998 3 12 98FDEA00164 1 19980306 A 5311 651593350 FRAME BOEING 727 727227 1384078 NM BS 620 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 CRACK IN FRAME AT FASTENER HOLE BS 620, RBL 3, WL 157. *S/D* REPAIRED FRAME AT BS 620, RBL 3, WL 157 IAW FED-EX SRM 51 -40-3. 2 L 7 3 4F A3WE 1998031200580 19980312 00580 NE 1998 3 12 98FDEA00165 2 19980307 A 7200 ENGINE AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 1 FLAMED OUT A FDEA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SO 25 658FE 752 DURING IDLE DESCENT PASSING FL260, NR 1 ENGINE FLAMED OUT. NO APPARENT ENGINE DAMAGE. ALL FUEL PUMPS ON, 18000 LBS OF FOB. REMAINING, FUEL DISTRIBUTION NORMAL. FOLLOWING ECAM INSTRUCTIONS, ENGINE RE-LIT WITH APPLICATION OF CONTINUOUS IG NITION. ADVISED ATC, MADE NORMAL 2 ENGINE APPROACH AND LANDING. INSPECTED NR 1 ENGINE FUEL FILTERS, FOUND SLIGHTLY DIR TY, NO DEBRIS. INSPECTED ENGINE FOR FOD DAMAGE, NONE FOUND. ALL PARAMETERS WERE NORMAL. 2 L 7 2 4F 4 F RT A35EU E13NE 1998031200581 19980312 00581 WP 1998 3 12 MWEA98290 1 19980305 A 5311 5910074 FRAME DOUG DC9 DC932 3022066 WP BS 207 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 A FRAME AT FS 207 WAS CUT TO FACILITATE OTHER MAINTENANCE. FABRICATED AND INSTALLED REPAIR SPLICES. 2 L 7 2 4F A6WE 1998031200582 19980312 00582 WP 1998 3 12 MWEA98291 1 19980305 A 5320 9910078 WEB DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 SUBFLOOR WEB AT FS 160 TO FS 200 LBL 44 TO LBL 55 WAS FOUND CORRODED. REMOVED AND REPLACED SUBFLOOR WEB. 2 L 7 2 4F A6WE 1998031200583 19980312 00583 WP 1998 3 12 MWEA98292 1 19980305 A 5320 99100787 WEB DOUG DC9 DC932 3022066 WP BS 120-160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 GALLEY SUBFLOOR WAS FOUND CORRODED IN VARIOUS AREAS. ALSO, A HOLE WAS PUNCHED IN THE FLOOR FROM FS 120 TO FS 160 LBL 8 TO RBL 55. REMOVED AND REPLACED SUBFLOOR. 2 L 7 2 4F A6WE 1998031200584 19980312 00584 WP 1998 3 12 MWEA98293 1 19980305 A 5320 9911991 JAMB DOUG DC9 DC932 3022066 WP BS 1038-1086 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 VENTRAL STAIR CUTOUT LEFT HAND JAMB HOLE L-ANGLE WAS FOUND CORRODED FROM STA 1038 TO 1086. REMOVED AND REPLACED DAMAGED SECTION OF JAMB. 2 L 7 2 4F A6WE 1998031200585 19980312 00585 WP 1998 3 12 MWEA98294 1 19980305 A 5320 5911412 DOUBLER DOUG DC9 DC932 3022066 WP BS 503 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RADAR ALTIMETER DOUBLER WAS FOUND CORRODED AT FS 503 LONGERON 30 TO 29. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 1998031200586 19980312 00586 WP 1998 3 12 MWEA98295 1 19980305 A 5320 5911412 DOUBLER DOUG DC9 DC932 3022066 WP BS 440 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RADAR ALTIMETER DOUBLER AT FS 440 LONGERON 30 TO 29L WAS FOUND CORRODED. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 1998031200587 19980312 00587 WP 1998 3 12 MWEA98296 1 19980305 A 5330 59670441 SKIN DOUG DC9 DC932 3022066 WP BS 1121/1155 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 EXTERIOR FUSELAGE SKIN WAS FOUND CORRODED AT HTE SEAMS AT FS 1121.225 AND FS 1155.225 LONGERON 18L TO 25L. REMOVED AND REPLACED SECTION OF SKIN. 2 L 7 2 4F A6WE 1998031200588 19980312 00588 WP 1998 3 12 MWEA98297 1 19980305 A 5312 5910130 BULKHEAD SKIN DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 APB SKIN WS FOUND CORRODED ON THE LOWER END FROM LONGERON 26 LEFT TO 22 RIGHT DAMAGED OUT OF LIMITS FROM LONGERON 28L TO 29R. CUT OUT DAMAGED AREAS FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998031200589 19980312 00589 WP 1998 3 12 MWEA98298 1 19980305 A 5312 1250445 BLKHD STIFFENER DOUG DC9 DC932 3022066 WP BS 1121 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 STIFFENER AT LONGERON 13L OF CANTED BULKHEAD 1121 WAS FOUND EXFOLIATED. FABRICATED AND INSTALLED REPLACEMENT STIFFENER. 2 L 7 2 4F A6WE 1998031200590 19980312 00590 WP 1998 3 12 MWEA98299 1 19980305 A 5320 9911991 JAMB DOUG DC9 DC932 3022066 WP BS 1087-1155 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 VENTRAL STAIR LEFT HAND DOOR JAMB WAS FOUND CORRODED FROM FS 1087 TO 1155. FABRICATED AND INSTALLED JAMB SECTION. 2 L 7 2 4F A6WE 1998031200591 19980312 00591 WP 1998 3 12 MWEA98316 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 598-617 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE LEFT HAND CUSP MEMBRANE WAS FOUND DAMAGED BETWEEN FS 598 TO 617. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998031200592 19980312 00592 WP 1998 3 12 MWEA98317 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 617-639 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 SUBFLOOR AT THE LT CUSP WAS FOUND DAMAGED FROM FS 617 TO FS 639. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998031200593 19980312 00593 WP 1998 3 12 MWEA98318 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 658 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND SUBFLOOR WEB AT FS 639 TO 658 WAS FOUND DAMAGED. INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998031200594 19980312 00594 WP 1998 3 12 MWEA98319 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 680 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND CUSP WEB AT STATION 680 WAS FOUND DAMAGED. INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998031200595 19980312 00595 WP 1998 3 12 MWEA98320 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 579-598 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND CUSP WEB FROM FS 579 TO 598 WAS FOUND DAMAGED. REMOVED AND REPLACED SECTION OF MEMBRANE. 2 L 7 2 4F A6WE 1998031200596 19980312 00596 WP 1998 3 12 MWEA98321 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 775-813 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND CUSP MEMBRANE WAS FOUND DAMAGED FROM FS 775 TO 813. FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998031200597 19980312 00597 WP 1998 3 12 MWEA98323 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 898-965 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND CUSP MEMBRANE WAS FOUND DAMAGED FROM FS 898 TO 965. FABRICATED AND INSTALLED REPLACEMENT WEB. 2 L 7 2 4F A6WE 1998031200598 19980312 00598 NM 1998 3 12 DL72S980523 1 19980305 A 5330 6556231 SKIN BOEING 727 727232 1384082 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 THE R1 DOOR SURROUND BEAR STRAP WAS FOUND CRACKED AT THE UPPER HINGE CUTOUT. THE SKIN AND BEAR STRAP WERE BOTH TRIMMED TO REMOVE THE CRACK. A REPAIR DOUBLER AND TRIPLER WERE INSTALLED PER THE GUIDELINES OF BAC S/B 727-53-0136 AND DOCUMENT ED PER ER/A 364187-14. 2 L 7 3 4F A3WE 1998031200599 19980312 00599 NM 1998 3 12 DL73K980524 1 19980304 A 5330 SKIN BOEING 737 737232 1384475 NM L2 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306DL 23078 THE L2 DOOR CUTOUT SURROUND SKIN, DOUBLER, AND BEAR STRAP WERE FOUND WITH A 1.375 TYPICAL CRACK IN THE LOWER, FWD CORNER . THE DAMAGE WAS REPAIRED PER THE B737 SRM 53-30-3 FIG 24 AND PER ER/A 364170-14. 2 L 7 2 4F RT A16WE 1998031200600 19980312 00600 NM 1998 3 12 DLM88980525 1 19980304 A 5320 JAMB DOUG MD88 MD88 3023688 NM CARGO DOOR CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DE 53378 THE LOWER JAMB PAN OF THE FWD CARGO DOOR CUTOUT SURROUND STRUCTURE WAS FOUND CORRODED. THE PAN SECTION BETWEEN THE FWD AND AFT CORNERS OF THE DOOR WAS REMOVED AND A NEW SECTION SPLICED IN PER THE MD-88 SRM 53-05, FIG 44 AND PER ER/A 364169 -14. 2 L 7 2 4F RT A6WE 1998031200601 19980312 00601 NM 1998 3 12 DL72S980526 1 19980306 A 5521 SPAR BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 THE LT ELEVATOR REAR SPAR WAS FOUND WITH A TYPICAL CRACK AT THE SECOND FROM THE OUTBD END HINGE. THE CRACK WAS STOP DRI LLED PER THE REQUIREMENTS OF BOEING S/B 727-55-0089 AND IS BEING TRACKED PER ER/A 364195-14AD. THE PERMANENT REPAIR WIL L MODIFY THE SPAR PER S/B 727-55-0089. 2 L 7 3 4F A3WE 1998031200602 19980312 00602 NM 1998 3 12 DL72S980527 1 19980305 A 5320 651751737 CHANNEL BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 490DA 21020 THE FS 1263 UPPER CHANNEL ON THE LT AFT VENTRAL STAIRWELL TORQUE BOX WAS FOUND WITH A 1.5 INCH CRACK IN THE TYPICAL LOCA TION PER S/B 727-53-0129. THE DAMAGED CHANNEL WAS REPLACED PER THE S/B AND DOCUMENTED PER ER/A 364193-14AD. 2 L 7 3 4F A3WE 1998031200603 19980312 00603 NM 1998 3 12 DL72S980528 1 19980306 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 FOUND AT C2 LETTER CHECK, .75 INCH CRACK IN VERT STAB S-9L, INSIDE VERT STAB CRAWLWAY, FOURTH BULKHEAD ABOVE OPENING. R EPAIRED PER M/M 55-30-0. 2 L 7 3 4F A3WE 1998031200604 19980312 00604 NM 1998 3 12 DL72S980529 1 19980306 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 FOUND AT C2 LETTER CHECK, .5 INCH CRACK IN VERT STAB S-7L, INSIDE VERT STAB CRAWLWAY THIRD BULKHEAD ABOVE OPENING. REPA IRED PER M/M 55-30-0 . 2 L 7 3 4F A3WE 1998031200605 19980312 00605 NM 1998 3 12 DLM88980530 1 19980307 A 3350 BATTERY PACK RPS1B DOUG MD88 MD88 3023688 NM CABIN DISCHARED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 994DL 8372 53346 EMERGENCY EXIT TRACK LIGHTS (FLOOR) INOP IN FIRST CLASS CABIN. REPLACED BATTERY PACK AND PWR SUPPLY, LIGHTS CK OK. 2 L 7 2 4F RT A6WE 1998031200606 19980312 00606 NM 1998 3 12 DL72S980532 1 19980307 A 3350 CONTROL RACK 334701744 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 477DA A10336 20754 ON LAYOVER CK, FOUND R2 EMERGENCY OVHD LT INOP. FOUND LIGHT CONTROL RACK BAD. REPLACED SAME, INSTALLED NEW BATTERY. 2 L 7 3 4F A3WE 1998031200607 19980312 00607 NM 1998 3 12 DL733980536 1 19980307 A 2432 BATTERY CHARGER 279202 BOEING 737 737347 1384647 NM E/E COMP DAMAGED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 304WA 1836 23345 NORMAL BLOWER POPPED CIRCUIT BREAKER. LEFT PACK TRIP TWICE. NR 1 GENERATOR VOLT/FREQUENCY ZERO. ELECTRICAL SMELL IN C ABIN. FOUND BATTERY CHARGER BURNT. REPLACED BATTERY CHARGER. 2 L 7 2 4F RT A16WE 1998031200608 19980312 00608 NM 1998 3 12 VNAA9803005 1 19980305 A 3030 0851GW PITOT HEAD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 426JS 67789 3038 PRIOR TO TAKEOFF DURING TAXI, THE CREW NOTED A NUMBER ONE PITOT HEAT FAIL WARNING MESSAGE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NUMBER ONE PITOT HEAD, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-1 1-04. OPERATION CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031200609 19980312 00609 EU 1998 3 12 HEEA0013156 1 19980303 A 6320 4638303001 BEVEL GEAR 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEVEL GEAR WORN SEAT AREA. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200610 19980312 00610 EU 1998 3 12 HEEA0013157 1 19980303 A 6320 4619303084 ROLLER BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. ROLLER BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200611 19980312 00611 EU 1998 3 12 HEEA0013158 1 19980303 A 6320 4619303083 BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200612 19980312 00612 EU 1998 3 12 HEEA0013159 1 19980303 A 6320 4619303004 ROLLER BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200613 19980312 00613 EU 1998 3 12 HEEA0013160 1 19980303 A 6320 4638305028 ROLLER BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200614 19980312 00614 EU 1998 3 12 HEEA0013161 1 19980303 A 6320 4638305001 BALL BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200615 19980312 00615 EU 1998 3 12 HEEA0013162 1 19980303 A 6320 4619305042 ROLLER BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER AND CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200616 19980312 00616 EU 1998 3 12 HEEA0013163 1 19980303 A 6320 4619306019 ROLLER BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200617 19980312 00617 EU 1998 3 12 HEEA0013164 1 19980303 A 6320 4619306020 ROLLER BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200618 19980312 00618 EU 1998 3 12 HEEA0013165 1 19980303 A 6320 4619312030 CYLINDER ROLLER 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. CORROSION ON ROLLERS. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200619 19980312 00619 EU 1998 3 12 HEEA0013166 1 19980303 A 6320 4619307023 BALL BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BALL BEARING CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200620 19980312 00620 EU 1998 3 12 HEEA0013167 1 19980303 A 6320 4619312050 BALL BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200621 19980312 00621 EU 1998 3 12 HEEA0013168 1 19980303 A 6320 4619307024 BALL BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200622 19980312 00622 EU 1998 3 12 HEEA0013169 1 19980303 A 6320 4619307025 ROLLER BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING CORROSION. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200623 19980312 00623 EU 1998 3 12 HEEA0013170 1 19980303 A 6320 4638302024 BEARING 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. BEARING ROLLOVER. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200624 19980312 00624 EU 1998 3 12 HEEA0013171 1 19980303 A 6320 4619303081 CYLINDER ROLLER 4638001004 BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 965 S737 3000 HOUR OVERHAUL DUE. ROLLER BEARING P/N 4638-302-025 RECOMMENDED. SCRAPPED PART. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998031200625 19980312 00625 EU 1998 3 12 HEEA0013172 1 19980303 A 6210 117150071 BLADE BOLKMS 117 BK117A4 5626017 EU M/R SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 2772 7092 ABRASION STRIP SEPARATED ON THE INBOARD END LOWER SIDE BEYOND LIMITS. 1 G 7 2 3U H13EU 1998031200626 19980312 00626 EU 1998 3 12 HEEA0013173 1 19980303 A 6210 117150071 BLADE BOLKMS 117 BK117A4 5626017 EU M/R SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 2772 7092 ABRASION STRIP SEPARATED ON THE INBOARD END BOTH SURFACES BEYOND LIMITS. 1 G 7 2 3U H13EU 1998031200627 19980312 00627 SW 1998 3 12 HEEA0013174 1 19980304 A 6240 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 NR2 NEEDLE STICKS IN STARTUP. NEEDLES NR1 AND NR2 HAVE EXCESSIVE SPLIT. TIME SINCE REPAIR 34:25. 1 G 7 2 4U H4SW 1998031200628 19980312 00628 1998 3 12 HEEA0013175 4 19980304 A 2310 064101600 CONTROL KCU951 BELL 212 212 1181420 SW COCKPIT HF DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736D 31135 DISPLAY HARD TO READ AND CHANNELS INTERMITTENTLY. 1 G 7 1 4U H4SW 1998031200629 19980312 00629 SW 1998 3 12 HEEA0013176 1 19980304 A 6240 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 TRIPLE TACH ALL NEEDLES READ APPROXIMATELY 3% HIGH, ALSO HAVE STICKY OPERATION BELOW 20%. 1 G 7 2 4U H4SW 1998031200630 19980312 00630 SW 1998 3 12 HEEA0013177 1 19980304 A 6240 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 TRIPLE TACH HAS MOISTURE IN GLASS. ALL NEEDLES HAVE STICKY OPERATION. 1 G 7 2 4U H4SW 1998031200631 19980312 00631 SW 1998 3 12 HEEA0013178 1 19980304 A 2435 23046313 STATOR BELL 412 412 1182202 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 CAUSING STARTER GENERATOR NOT TO COME ON LINE, CAUSES GENERATOR VOLTMETER TO PEG BACKWARDS AND FLASHING FIELD DID NOT HE LP. 1 G 7 2 4U H4SW 1998031200632 19980312 00632 EU 1998 3 12 HEEA0013179 1 19980304 A 6320 4011001 INDICATOR BOLKMS 105 BO105S 5626006 EU XMSN OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 TRIPLE OIL PRESSURE INDICATOR FAILED. TRANSMISSION PRESSURE DROPPING TO ZERO. 1 G 7 2 3U H3EU 1998031200633 19980312 00633 1998 3 12 HEEA0013180 4 19980304 A 3453 4530103 LORAN ARNAV21 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 721MB S752 WHEN SCROLLING IN AUX OR NAV MODE UNIT INTERMITTENTLY LOSES DISPLAY AND STARTS OVER. INTERMITTENT IN CDI MODE. 1 G 7 2 3U H3EU 1998031200634 19980312 00634 1998 3 12 HEEA0013182 4 19980304 A 3457 0845000000 GPS SKYNAV5000 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J S826 GPS INOPERATIVE. 1 G 7 2 3U H3EU 1998031200635 19980312 00635 1998 3 12 HEEA0013183 4 19980304 A 2312 40001452500 RECEIVER RT138F BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 DOES NOT TRANSMIT. 1 G 7 2 3U H13EU 1998031200636 19980312 00636 1998 3 12 HEEA0013184 4 19980304 A 3452 066104100 TRANSPONDER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31219 760230 TRANSPONDER WILL NOT TRANSMIT. 1 G 7 2 3U H1NE 1998031200637 19980312 00637 1998 3 12 HEEA0013185 4 19980304 A 3454 071107600 INDICATOR KDA697 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 NO. 2 VOR - GREEN NEEDLE DOESN'T POINT TO STATION BOTH SIDES. 1 G 7 2 3U H1NE 1998031200638 19980312 00638 1998 3 12 HEEA0013186 4 19980304 A 3454 071121627 CONTROL SKRSKY S76 S76A 8143006 NE COCKPIT NAV FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 NAV CONTROL WILL NOT TURN OFF WITH ON/OFF SWITCH. 1 G 7 2 3U H1NE 1998031200640 19980312 00640 SW 1998 3 12 HEEA0013188 1 19980304 A 2435 200SG119Q STARTER GEN BELL 412 412 1182202 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 142 33113 STARTER GENERATOR INOPERATIVE. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND UPPER BEARING FAILED DAMAGING FAN AND POS SIBLY ARMATURE AND STATOR. 1 G 7 2 4U H4SW 1998031200641 19980312 00641 1998 3 12 HEEA0013189 4 19980304 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 135AE S838 GPS INTERNAL BATTERY IS DEAD. 1 G 7 2 3U H3EU 1998031200642 19980312 00642 1998 3 12 HEEA0013190 4 19980304 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB S751 INNER KNOB ON GPS WILL NOT SELECT CORRECT CHOICE INTERMITTENTLY. 1 G 7 2 3U H3EU 1998031200643 19980312 00643 1998 3 12 HEEA0013191 4 19980304 A 3454 066107800 RECEIVER SKRSKY S76 S76A 8143006 NE VHF NAV INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 15460 760223 PANEL LIGHTS ILLUMINATE INTERMITTENTLY. 1 G 7 2 3U H1NE 1998031200644 19980312 00644 1998 3 12 HEEA0013192 4 19980304 A 2210 7683431 POTENTIOMETER 769000180210 SKRSKY S76 S76A 8143006 NE AUTO PILOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 384 81012190 760233 ACTUATOR DOES NOT MOVE. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND ONE EACH POTENTIOMETER CHECKED BAD, HAD NO READI NG ON TEST. 1 G 7 2 3U H1NE 1998031200645 19980312 00645 SW 1998 3 12 HEEA0013193 1 19980304 A 6210 214015300107 BLADE BELL 214 214ST 1182106 SW M/R TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 1952 28139 UPPER EROSION SHIELD TORN AND SEPARATED AT THE OUTBOARD END. 2 G 7 2 4U H10SW 1998031200646 19980312 00646 1998 3 12 HEEA0013194 4 19980304 A 3452 066106200 TRANSPONDER KT76 BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CGOFL 53130 KT76 TRANSCEIVER DRAWS EXCESSIVE CURRENT. 1 G 7 1 3U O H2SW 1998031200647 19980312 00647 1998 3 12 HEEA0013196 4 19980304 A 3421 500DCF288 HORIZON GYRO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5014V 45217 HORIZ GYRO PRECESSES. 1 G 7 1 3U H2SW 1998031200648 19980312 00648 SW 1998 3 12 HEEA0013197 1 19980304 A 6320 205040231009 RING GEAR BELL 412 412 1182202 SW M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 WORN PILOT DIA'S AND CORROSION ON UPPER AND LOWER FLANGES. 1 G 7 2 4U H4SW 1998031200649 19980312 00649 NE 1998 3 12 HEEA0013198 1 19980304 A 6730 30006773 GLAND SKRSKY S76 S76A 8143006 NE M/R SERVO GOUGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GLAND FOUND TO BE GOUGED AT LOWER OUTER END. 1 G 7 2 3U H1NE 1998031200650 19980312 00650 EU 1998 3 12 HEEA0013199 1 19980304 A 5610 1054002 WINDOW BOLKMS 105 BO105S 5626006 EU RT ROOF MIS MFG E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 SKYLIGHT WAS MANUFACTURED 3/16" TOO SHORT IN WINDOW LENGTH AND WIDTH; THAN FACTORY WIDTH. 1 G 7 2 3U H3EU 1998031200651 19980312 00651 SW 1998 3 12 HEEA0013200 1 19980304 A 3340 214175127103 POWER SUPPLY BELL 214 214ST 1182106 SW LIGHTS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 POWER SUPPLY UPPER AND LOWER LIGHT WILL NOT ILLUMINATE. 2 G 7 2 4U H10SW 1998031200652 19980312 00652 EU 1998 3 12 HEEA0013201 1 19980304 A 6410 10531980 BLADE BOLKMS 105 BO105S 5626006 EU T/R ERRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 91070 898 S145 PAINT EROSION AT BLADE TIP ON S/N 646. PAINT EROSION AND RUBBER COATING PEELED OFF AT BLADE TIP ON S/N 655. 1 G 7 2 3U H3EU 1998031200653 19980312 00653 EU 1998 3 12 HEEA0013202 1 19980304 A 6520 4619210901 GEAR HOUSING BOLKMS 105 BO105S 5626006 EU T/R HEAD DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 VERIFICATION OF "B" DIM. 1 G 7 2 3U H3EU 1998031200654 19980312 00654 SW 1998 3 12 HEEA0013204 1 19980304 A 6730 206076031017 SERVO BELL 206 206B3 1181506 SW M/R LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2756P 4533 2655 SERVO LEAKING. SERIAL NUMBERS REMOVED ARE RH1375, RH1779, AND RH1777. SENT TO HELICOPTER ACCESSORY SERVICE FOR OVERHAUL . 1 G 7 1 3U H2SW 1998031200655 19980312 00655 1998 3 12 HEEA0013205 4 19980304 A 3444 071111400 ANTENNA BOLKMS 105 BO105S 5626006 EU RADAR ALT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 137AE S851 ERRATIC ALTIMETER OPERATION. 1 G 7 2 3U H3EU 1998031200656 19980312 00656 1998 3 12 HEEA0013206 4 19980304 A 3425 066304601 INDICATOR KI525A BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2756P 2655 DEVIATION NEEDLE STICKS. 1 G 7 1 3U H2SW 1998031200657 19980312 00657 SW 1998 3 12 HEEA0013207 1 19980304 A 2611 3023131 SMOKE DETECTOR BELL 214 214ST 1182106 SW DET SYS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 6957Y 28139 SMOKE DETECTOR WILL NOT TEST. 2 G 7 2 4U H10SW 1998031200658 19980312 00658 SW 1998 3 12 HEEA0013208 1 19980304 A 6210 204011121009 GRIP BELL 212 212 1181420 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736D 11359 31135 DRAG BRACE BUSHINGS AND PITCH HORN BORES WORN BEYOND LIMITS. 1 G 7 1 4U H4SW 1998031200659 19980312 00659 SW 1998 3 12 HEEA0013209 1 19980304 A 2432 214175379103 BATTERY CHARGER BELL 214 214ST 1182106 SW DC SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 BATTERY SWITCH LIGHT REMAINS ON. 2 G 7 2 4U H10SW 1998031200660 19980312 00660 SW 1998 3 12 HEEA0013210 1 19980304 A 2430 214175132103 RELAY BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 BATTERY VOLTAGE DROPS DURING START. 2 G 7 2 4U H10SW 1998031200661 19980312 00661 SW 1998 3 12 HEEA0013211 1 19980304 A 2430 214175171103 RELAY BELL 214 214ST 1182106 SW BATTERY SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 CAUSING VOLTAGE TO DROP DURING ENGINE START. 2 G 7 2 4U H10SW 1998031200662 19980312 00662 SW 1998 3 12 HEEA0013212 1 19980304 A 3020 206062625003 ACTUATOR BELL 206 206B3 1181506 SW ENG ANTI ICE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3181J 3771 ACTUATOR INOPERATIVE. 1 G 7 1 3U H2SW 1998031200663 19980312 00663 SW 1998 3 12 HEEA0013213 1 19980304 A 2160 212073927001 MOTOR BELL 412 412 1182202 SW TEMP CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 TEMP CONTROL MOTOR INOPERATIVE. 1 G 7 2 4U H4SW 1998031200664 19980312 00664 SW 1998 3 12 HEEA0013214 1 19980304 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6160Y 51609 ACTUATOR INOPERATIVE AND WILL NOT MOTOR. 1 G 7 1 3U H2SW 1998031200665 19980312 00665 SW 1998 3 12 HEEA0013215 1 19980304 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 513EH 45421 ACTUATOR INOPERATIVE AND WILL NOT MOTOR. 1 G 7 1 3U H2SW 1998031200666 19980312 00666 SW 1998 3 12 HEEA0013216 1 19980304 A 7714 22A690 TACH GENERATOR BELL 412 412 1182202 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 TACH GENERATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998031200667 19980312 00667 SW 1998 3 12 HEEA0013217 1 19980304 A 7714 GEU7A GENERATOR BELL 412 412 1182202 SW ENG TACH MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 TACH GENERATOR INTERMITTENT LIGHT. 1 G 7 2 4U H4SW 1998031200668 19980312 00668 1998 3 12 HEEA0013218 4 19980304 A 3421 222375033103 INDICATOR BELL 214 214ST 1182106 SW COCKPIT PRECESSES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 59806 28140 ATTITUDE INDICATOR PRECESSES DURING FLIGHT. 2 G 7 2 4U H10SW 1998031200669 19980312 00669 1998 3 12 HEEA0013219 4 19980304 A 3421 222375033103 INDICATOR BELL 412 412 1182202 SW COCKPIT PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 ATTITUDE INDICATOR EXCESSIVE PRECESSING IN PITCH AND ROLL. 1 G 7 2 4U H4SW 1998031200671 19980312 00671 1998 3 12 HEEA0013221 4 19980304 A 3425 1258103 HSI BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 HSI HEADING SET INOPERATIVE. 1 G 7 2 4U H4SW 1998031200672 19980312 00672 1998 3 12 HEEA0013222 4 19980304 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 HSI INDICATOR COURSE SET INOPERATIVE. 1 G 7 2 4U H4SW 1998031200673 19980312 00673 1998 3 12 HEEA0013223 4 19980304 A 3425 1113025 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 HSI INDICATOR COURSE WINDOW DOES NOT MATCH YELLOW NEEDLE. 1 G 7 2 3U H1NE 1998031200674 19980312 00674 NE 1998 3 12 HEEA0013226 1 19980304 A 6500 7635805127101 BUSHING SKRSKY S76 S76A 8143006 NE T/R OVERSIZE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 T/R DRIVE BUSHING OVERSIZED. 1 G 7 2 3U H1NE 1998031200675 19980312 00675 1998 3 12 HEEA0013229 4 19980304 A 3416 59341 ALTIMETER BELL 206 206L1 1182107 SW COCKPIT STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5742N 45477 ALTIMETER NEEDLE STUCK AT 54,000 FEET. 1 G 7 1 3U H2SW 1998031200677 19980312 00677 1998 3 12 HEEA0013231 4 19980304 A 3421 7660002113102 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 VERT GYRO MALFUNCTION. TAKES 5 TO 7 MINUTES TO PULL FLAG ON ADI. 1 G 7 2 3U H1NE 1998031200678 19980312 00678 1998 3 12 HEEA0013232 4 19980304 A 3421 7660002113102 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 ADI WILL FALL 90 DEGREES. 1 G 7 2 3U H1NE 1998031200679 19980312 00679 SW 1998 3 12 HEEA0013233 1 19980304 A 2930 124043 INDICATOR BELL 412 412 1182202 SW HYD PRESS/TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 HYD PRESSURE/ TEMP LIGHT IN INOPERATIVE. 1 G 7 2 4U H4SW 1998031200680 19980312 00680 EU 1998 3 12 HEEA0013234 1 19980304 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4294R S860 EXH TEMP INDICATOR STATIC READING 50 DEGREES HIGH. 1 G 7 2 3U H3EU 1998031200681 19980312 00681 1998 3 12 HEEA0013235 4 19980304 A 3424 A593002 INDICATOR BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251Y 51556 TURN & BANK INDICATOR NEEDLE DOES NOT DEFLECT IN EITHER DIRECTION. 1 G 7 1 3U H2SW 1998031200682 19980312 00682 SW 1998 3 12 HEEA0013236 1 19980304 A 2841 214175257103 INDICATOR BELL 214 214ST 1182106 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 ADC DOES NOT COUNT DOWN AS FUEL IS BURNT. 2 G 7 2 4U H10SW 1998031200683 19980312 00683 SW 1998 3 12 HEEA0013237 1 19980304 A 2840 206075186003 DUAL INDICATOR BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39122 3312 DUAL INDICATOR LOADMETER IS INOPERATIVE. 1 G 7 1 3U H2SW 1998031200684 19980312 00684 SW 1998 3 12 HEEA0013238 1 19980304 A 7722 206375006101 INDICATOR BELL 206 206L1 1182107 SW COCKPIT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21240 45647 EXH TEMP INTERMITTENTLY READS UP TO 200 DEGREES LOW. 1 G 7 1 3U H2SW 1998031200685 19980312 00685 EU 1998 3 12 HEEA0013239 1 19980304 A 6240 10594576 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4573B S673 MAST MOMENT INDICATOR NO INDICATION IN FLIGHT. 1 G 7 2 3U H3EU 1998031200686 19980312 00686 EU 1998 3 12 HEEA0013240 1 19980304 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 4573B S673 MAST MOMENT INDICATOR HAS NO INDICATION IN FLIGHT. 1 G 7 2 3U H3EU 1998031200687 19980312 00687 1998 3 12 HEEA0013241 4 19980304 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 NARCO ELT TRANSMITS SIGNAL INADVERTANTLY. 1 G 7 2 3U H3EU 1998031200688 19980312 00688 1998 3 12 HEEA0013242 4 19980304 A 2562 ELT910 ELT NARCO SNIAS 350 AS350B2 8680813 EU COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 350BZ 2653 ELT FAILED "G" SWITCH TEST. 1 G 7 1 3U H9EU 1998031200689 19980312 00689 SW 1998 3 12 HEEA0013243 1 19980304 A 2432 214175379103 BATTERY CHARGER BELL 214 214ST 1182106 SW DC SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 BATTERY CHARGER VOLT SPIKES. 2 G 7 2 4U H10SW 1998031200690 19980312 00690 SW 1998 3 12 HEEA0013244 1 19980304 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 ROTARY ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998031200691 19980312 00691 SW 1998 3 12 HEEA0013245 1 19980304 A 7714 212075037101 INDICATOR BELL 412 412 1182202 SW ENG N1 STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 ENG N1 NEEDLE HAS STICKY OPERATION THROUGHOUT SCALE. 1 G 7 2 4U H4SW 1998031200692 19980312 00692 SW 1998 3 12 HEEA0013246 1 19980304 A 2436 214175153105 REGULATOR BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 VOLTAGE REGULATOR UNABLE TO ADJUST VOLTAGE. 2 G 7 2 4U H10SW 1998031200693 19980312 00693 1998 3 12 HEEA0013247 4 19980304 A 3414 214074152101 TRANSDUCER BELL 214 214ST 1182106 SW AIRSPEED FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 AIRSPEED TRANSDUCER INOPERATIVE. 2 G 7 2 4U H10SW 1998031200694 19980312 00694 SW 1998 3 12 HEEA0013248 1 19980304 A 2611 302319 SMOKE DETECTOR BELL 412 412 1182202 SW CABIN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 SMOKE DET CAUTION LIGHT DOES NOT ILLUMINATE. 1 G 7 2 4U H4SW 1998031200695 19980312 00695 NE 1998 3 12 HEEA0013249 1 19980304 A 7600 7690001880106 AMPLIFIER SKRSKY S76 S76A 8143006 NE DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 DROOP COMPENSATOR FAILED DCA TEST. 1 G 7 2 3U H1NE 1998031200696 19980312 00696 SW 1998 3 12 HEEA0013250 1 19980304 A 2822 205060606003 PUMP BELL 212 212 1181420 SW FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 BOOST PUMP POPPING CIRCUIT BREAKER. 1 G 7 1 4U H4SW 1998031200697 19980312 00697 EU 1998 3 12 HEEA0013251 1 19980304 A 7931 6607190A INDICATOR WARN BOLKMS 105 BO105S 5626006 EU OIL PRESS FAILED E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 911DD S830 OIL PRESS INDICATOR HAS NO "T" OIL LIGHT INDICATION. 1 G 7 2 3U H3EU 1998031200698 19980312 00698 EU 1998 3 12 HEEA0013252 1 19980304 A 2612 10593951 FIRE CONT UNIT BOLKMS 105 BO105S 5626006 EU LT ENG MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 91070 S145 L/H ENGINE FIRE LIGHT INTERMITTENTLY STICKS ON. 1 G 7 2 3U H3EU 1998031200699 19980312 00699 SW 1998 3 12 HEEA0013253 1 19980304 A 2823 L88010501 VALVE BELL 412 412 1182202 SW FUEL SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 FUEL VALVE HAS LOUD SQUEALING NOISE. 1 G 7 2 4U H4SW 1998031200700 19980312 00700 SW 1998 3 12 HEEA0013254 1 19980304 A 3340 A490A POWER SUPPLY BELL 206 206L1 1182107 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W 45386 STROBE POWER SUPPLY PRODUCES WEAK FLASH. 1 G 7 1 3U H2SW 1998031200701 19980312 00701 1998 3 12 HEEA0013255 4 19980304 A 3454 066303800 RMI KING KI229 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 818SH S753 RMI INOPERATIVE. 1 G 7 2 3U H3EU 1998031200702 19980312 00702 SW 1998 3 12 HEEA0013256 1 19980304 A 5510 206023119151 STABILIZER ASSY BELL 206 206L1 1182107 SW HORIZ STAB SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3892R 45594 STAB ASSY DOUBLER IS SEPARATED NEAR LEADING EDGE. 1 G 7 1 3U H2SW 1998031200703 19980312 00703 1998 3 12 HEEA0013257 4 19980304 A 3422 2891ESR DIRECTION GYRO BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078C 45392 DIR GYRO LIGHTING IS OUT. 1 G 7 1 3U H2SW 1998031200704 19980312 00704 1998 3 12 HEEA0013258 4 19980304 A 3422 2891ESR DIRECTION GYRO BELL 206 206L1 1182107 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5745N 45489 DIR GYRO INTERMITTENTLY GETS FLAG INDICATOR. 1 G 7 1 3U H2SW 1998031200705 19980312 00705 1998 3 12 HEEA0013259 4 19980304 A 3422 2891ESR DIRECTION GYRO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1073W 45386 DG LOCKS UP; DOES NOT MOVE. 1 G 7 1 3U H2SW 1998031200724 19980312 00724 CE 1998 3 12 98ZZZX1035 1 19980227 A 3222 6642000850 NOSE GEAR CESSNA 500 560CESSNA 2076750 CE DAMPER STEERING MALFUNCTION A DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 351QS 21 5600451 LITTLE TO NO NOSE WHEEL MOVEMENT WHEN RUDDER PEDALS ARE PUSHED. FOUND RESISTANCE EXCESSIVE IN SHIMMY DAMPENER AND NOSE STRUT. REPLACED GEAR. 2 L 7 2 4F RT A22CE 1998031200735 19980312 00735 NM 1998 3 12 ANCF9801 1 19980209 A 2934 TRANSMITTER BOEING 757 75723A 1384967 NM C-HYD QTY SYS DEFECTIVE W ANCF C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 23 987AN 25494 BOG/CCS - FLT 078 - INITIATING TAKEOFF ROLL, C-SYSTEM HYDRAULIC QUANTITY INDICATOR, ZERO. REJECTED TAKEOFF AT 65 KNOTS. HYDRAULIC OIL LEVEL WAS CHECKED, FOUND NORMAL. FOUND DEFECTIVE TRANSMITTER CONNECTOR. (X) 2 L 7 2 4F RT A2NM 1998031200839 19980312 00839 WP 1998 3 12 VJ9800039 1 19980306 A 5320 591486523 WEB DOUG DC9 DC932 3022066 WP BS 597 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 909VJ 47322 TWO FASTENER HEADS POPPED OFF AND BULGING UNDER PRESSURE DOME AT FS STA 597, RBL 18. REMOVED BULKHEAD PRESSURE PANEL AT FS STA 597, DRILLED NEW PANEL, FABRICATED THREE FINGER DOUBLERS PLUS TWO ADDITIONAL DOUBLERS IAW DC9 SRM 51-10-2. TRE ATED AND PRIMED PARTS IAW DC9 SRM 51-10-3. INSTALLED NEW PRESSURE BULKHEAD PANEL, FINGER DOUBLERS AND DOUBLERS IAW DC9 SRM 51-30-2, RES 1 03655 AND AERO EO 98-798. 2 L 7 2 4F A6WE 1998031200840 19980312 00840 NE 1998 3 12 MALA976031 2 19980307 A 7320 6055T19P004 HMU SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 991XJ 091 ON CLIMBOUT, THE RIGHT ENGINE SURGES WITH CTOT ON AND OFF. COMPLIED WITH QRH AND RETURNED TO DTW. MAINTENANCE REPLACED RIGHT ENGINE HMU, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998031200841 19980312 00841 NM 1998 3 12 MALA976032 1 19980308 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 864MA 363 DURING INSPECTION, EMERGENCY EXIT LIGHT ASSEMBLY ON CABIN SIDEWALL AT SEAT 1E NEEDS TO BE RESECURED. MAINTENANCE RELAMP ED AND RESECURED EMERGENCY EXIT LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998031200842 19980312 00842 NM 1998 3 12 MALA976033 1 19980306 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 848MA 346 DURING INSPECTION, FLOOR TRACK LIGHT AT 1C INOP AND EXIT SIGN AT 4D IS LOOSE. MAINTENANCE RELAMPED FLOOR TRACK LIGHT AN D REPLACED EMERGENCY EXIT IDENTIFER ASSEMBLY AT SEAT 4D, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998031200843 19980312 00843 EU 1998 3 12 MALA976034 1 19980306 A 3350 LENS BAC 146 AVRO146RJ85A 1500097 EU CABIN BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 DURING INSPECTION, BROKEN LENS ON EXIT SIGN NEAR MAIN PASSENGER DOOR. MAINTENACE REPAIRED LENS ON EXIT SIGN, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998031200844 19980312 00844 EU 1998 3 12 MALA976035 1 19980307 A 3350 1317 LAMP SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 109XJ 340A109 DURING INSPECTION, ROW 4 OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998031200845 19980312 00845 EU 1998 3 12 MALA976036 1 19980308 A 3020 DE-ICE LIGHT SAAB SF340 340B 7860101 EU RT ENGINE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 412XJ 340B412 DURING CLIMB, RIGHT ENGINE INTAKE CAUTION LIGHT ILLUMINATED. COMPLIED WITH QRH AND RETURNED TO MSP. MAINTENANCE TROUBL ESHOT SYSTEM IAW SAAB AMM 30-20-00, NO FAULT FOUND. 2 L 7 2 4T RT A52EU 1998031200846 19980312 00846 EU 1998 3 12 MALA976037 1 19980308 A 3350 6104789 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 595MA 340B216 DURING INSPECTION, THREE FLOOR TRACK AND ONE COVE LIGHT INOP. MAINTENANCE REPLACED BATTERY PACK 22LN, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998031200847 19980312 00847 EU 1998 3 12 MALA976038 1 19980306 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING INSPECTION, TWO EMERGENCY LIGHTS INOP AT SEATS 4A AND 9A. MAINTENANCE RELAMPED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998031200848 19980312 00848 EU 1998 3 12 MALA976039 1 19980306 A 3260 AIR123782 STRIKER SAAB SF340 SF340A 7850100 EU RT MLG FAILED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 103XJ 340A103 ON APPROACH, THE RIGHT MAIN LIGHT NOT ILLUMINATED WITH GEAR DOWN SELECTION, GEAR IN TRANSIT LIGHT REMAINED ON. EMERGENC Y GEAR HANDLE PULLED. AIRCRAFT LANDING WITHOUT INCIDENT. MAINTENACE REPLACED STRIKER PLATE ON RIGHT MAIN LANGING GEAR DOWN AND LOCKED SWITCH AND SEPARATION BOLTS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998031200849 19980312 00849 EU 1998 3 12 MALA976040 1 19980306 A 3350 1317 LAMP SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 112XJ 340A112 DURING INSPECTION, OVERHEAD EMERGENCY LIGHT AT 6 C/D INOP. MAITNENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998031200850 19980312 00850 NM 1998 3 12 K3HA980023 1 19980307 A 3350 3071BPEGPL BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 ROW NR 2 EMERGENCY EXIT LIGHT ON FLOOR INOP. RELAMPED AND RESECURED TO FLOOR TRACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998031200851 19980312 00851 NM 1998 3 12 K3HA980024 1 19980307 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 AISLE LIGHTED EXIT SIGN CENTER INOP. REMOVED AND REPLACED AISLE (CENTER) LIGHTED EXIT SIGN BATTERY PACK REF MM33-50-71, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998031200852 19980312 00852 NM 1998 3 12 K3HA980025 1 19980307 A 3350 S106S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 FORWARD AISLE CEILING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY'S AISLE EMERGENCY FORWARD CEILING LIGHT REF 33 -50-01, OPS CHECK OK. 2 L 7 3 4F A3WE 1998031200853 19980312 00853 NM 1998 3 12 K3HA980026 1 19980308 A 3350 3071BPEGPL BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 AT ROW 18DEF 1ST RED EMERGENCY PATH LIGHTING OUT. REMOVED AND REPLACED LIGHT BULB, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998031200854 19980312 00854 NM 1998 3 12 K3HA980027 1 19980308 A 3350 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 L2 DOOR LOWER EMERGENCY EXIT SIGN 1/2 LIGHTS OUT. REMOVED AND REPLACED LIGHT BULB, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998031200855 19980312 00855 NM 1998 3 12 K3HA980028 1 19980305 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 AFT VENTRAL AIRSTAIR EMEGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY'S, OPS CHECK OK. 2 L 7 3 4F A3WE 1998031200856 19980312 00856 NM 1998 3 12 K3HA980029 1 19980306 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 LEFT HAND OVERWING EMERGENCY LIGHT BATTERY PACK LOW CHARGE. REMOVED AND REPLACED BATTERY PACK IAW 33-50-22, OPS CHECK O K. 2 L 7 3 4F A3WE 1998031200857 19980312 00857 SW 1998 3 12 PNSA980201 1 19980226 A 7603 CLEVIS PIN SWRNGN SA227 SA227AC 8780603 SW LT POWER LEVER LOOSE A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 2719H AC713B LT POWER LEVER BECAME DISCONNECTED DURING START. RESECURED CLEVIS PIN, OPS CHECK OK. 2 L 7 2 4T RT A8SW 1998031200858 19980312 00858 SW 1998 3 12 PNSA980202 1 19980226 A 2130 CONTROL LINE SWRNGN SA227 SA227AC 8780603 SW PRESSURE SYST ICED UP A PNSA O OTHER J WARNING INDICATION CL CLIMB 1 AL 03 41NE AC741B PRESSURIZATION UNCONTROLLABLE IN AUTO DURING CLIMB. THAWED ICE IN CONTROL LINE AND PURGED OPS CHECK OK. 2 L 7 2 4T RT A8SW 1998031200859 19980312 00859 CE 1998 3 12 PNSA980203 1 19980218 A 3230 TURNBARREL CESSNA 441 441 2076020 CE LANDING GEAR JAMMED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 544AL 4410120 GEAR WOULD NOT RETRACT FULLY. STEERING CABLE TURN BARREL BECAME JAMMED IN NOSE WELL. REPLACE TURNBARRLE, GEAR SWING CH ECKED OK. 1 L 7 2 3T RT A28CE 1998031200860 19980312 00860 NE 1998 3 12 PNSA980204 2 19980220 A 8530 CYLINDER GRUMAV G21 G21A 3951204 SO PWA R985 R985* 52008 NE LT ENGINE SEPARATED A PNSA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 741 B97 22989 LT ENGINE STARTED RUNNING ROUGH AND LOST POWER, RETURNED TO BASE. FOUND CYLINDER SEPARATED FROM CASE. REPLACED ENGINE . 1 H 7 2 3R 3 R TC654 5E1 1998031200861 19980312 00861 SO 1998 3 12 PNSA980205 1 19980208 A 3260 DNLOCK SWITCH PIPER PA31 PA31350 7103110 SO RT MLG LACK OF LUBE A PNSA O OTHER N FALSE WARNING DE DESCENT 1 AL 03 3588Z 318052130 RT MAIN WOULD NOT INDICATE DOWN AND LOCKED. UNEVENTFUL LANDING WAS MADE. CLEANED AND LUBED GEAR AND SWITCHES. NO FURT HER PROBLEMS NOTED. 1 L 7 2 3O A20SO 1998031200862 19980312 00862 1998 3 12 PNSA980206 4 19980205 A 3425 52D1372335 HSI CARD CESSNA 441 441 2076020 CE LEFT FAILED A PNSA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 441LL 364 441139 CAPTAINS HSI CARD DID NOT TURN DURING TAXI. REPLACED HSI, OPS CHECK OK. 1 L 7 2 3T RT A28CE 1998031200863 19980312 00863 CE 1998 3 12 PNSA980207 1 19980210 A 3297 WIRE CESSNA 441 441 2076020 CE SQUAT SWITCH LOOSE A PNSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 441LL 441139 ENGINES WOULD NOT CRANK. SECURED WIRE AT SQUAT SWITCH, OPS CHECK OK. 1 L 7 2 3T RT A28CE 1998031200864 19980312 00864 SO 1998 3 12 PNSA980208 1 19980211 A 3222 STRUT PIPER PA32 PA32301 7103207 SO NLG REQD SERVICE A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 AL 03 8004N 328206014 NOSE GEAR SHIMMY WAS EXCESSIVE DURING TAKEOFF RUN. RETURNED TO HANGER SERVICED NOSE GEAR STRUT, OPS CHECK OK. 1 L 7 1 3O A3SO 1998031200865 19980312 00865 1998 3 12 PNSA980209 3 19980204 A 6114 ZERK PIPER PA32 PA32301 7103207 SO PROP HUB LEAKING A PNSA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 AL 03 8470Y 328206012 DURING CRUISE, A FILM OF GREASE DEVELOPED ON WINDSHIELD. RETURNED TO BASE. REPLACED LEAKING GREASE ZERK, OPS CHECK OK . 1 L 7 1 3O A3SO 1998031200866 19980312 00866 SO 1998 3 12 PNSA980210 1 19980207 A 3230 UPLOCK ROLLERS PIPER PA31 PA31350 7103110 SO NLG LACK OF LUBE A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 15PR 318052011 NOSE GEAR WOULD NOT LOCK UP. CLEANED AND LUBED DIRTY NOSE GEAR UPLOCK ROLLER, OPS CHECK OK. 1 L 7 2 3O A20SO 1998031200867 19980312 00867 NM 1998 3 12 RAAA98B2012 1 19980306 A 3350 900835A BATTERY PACK GRIMES 1000679LB BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT FWD AND RT AFT EXTERNAL OVERWING EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 3 4F A3WE 1998031200868 19980312 00868 NM 1998 3 12 RAAA98B2013 1 19980306 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998031200869 19980312 00869 NM 1998 3 12 RAAA98B2014 1 19980306 A 3350 8621014 BATTERY PACK. INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 12 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998031200870 19980312 00870 SO 1998 3 12 RAAA98E4006 1 19980306 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 PAX ROW 13 AND 22 FLOOR PROXIMITY EGRESS LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 4 4T 4A22 1998031200871 19980312 00871 SO 1998 3 12 RAAA98E4007 1 19980306 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 RT OVERWING EMERGENCY EXIT AND AFT LT EMERGENCY EXIT EGRESS IDENTIFIER LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PAC KS DUE DISCHARGED. 2 L 7 4 4T 4A22 1998031200872 19980312 00872 WP 1998 3 12 CALA9800397 1 19980306 A 2560 59536131 COVER DOUG DC9 DC982 3022082 WP LT EXCAPE ROPE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 49491 THE LT OVERWING ESCAPE ROPE COVER WAS FOUND BROKEN FROM ITS MOUNTS. THE COVER WAS REPLACED IAW MM 25-61-00. 2 L 7 2 4F A6WE 1998031200873 19980312 00873 NM 1998 3 12 CALA9800398 1 19980307 A 3231 RETRACT MECH BOEING 727 727224 1384076 NM NLG DOORS OUT OF RIG A CALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 79746 22449 THE NOSE GEAR DOORS CAME OPEN ACCOMPANIED BY ILLUMINATION OF THE RED NOSE GEAR DOORS LIGHT WITH THE GEAR HANDLE IN UP OR OFF POSITION WHILE AT CRUISE. VIBRATION WAS FELT AND NOISE LEVEL HAD INCREASED. MAINTENANCE FOUND THE NOSE GEAR DOORS OUT OF RIG. THE DOORS WERE RIGGED IAW MM 32-22-1 AND OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1998031200874 19980312 00874 WP 1998 3 12 CALA9800399 1 19980308 A 3260 BOLT DOUG DC9 DC982 3022082 WP NLG LOOSE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 18835 49439 THE GROUND SHIFT SWITCH FAILED TO MOVE TO THE FLIGHT MODE AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT RAISE. THE AIRCRAFT WAS RETURNED TO LAX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOLT BACKED OUT OF NOSE GEAR OLEO SWITCH. REP LACED HARDWARE IAW IPC 32-60-00, FIGURE 1A AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998031200875 19980312 00875 WP 1998 3 12 CALA9800400 1 19980304 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 555 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 2 INCH CRACK IN LONGERON 32R AT STA 555 UNDER CIRCUMFERENTIAL. THE CRACKED SECTION WAS REMOVED AND A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-10-00. 2 L 7 3 4F A22WE 1998031200876 19980312 00876 WP 1998 3 12 CALA9800401 1 19980304 A 5311 RIB DOUG DC10 DC1010 3022110 WP BS 555 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND TWO 1.5 INCH CRACKS IN NR 3 PACK COMPARTMENT RIB AT STA 555 BETWEEN LONGERON 30 AND 31. A REPAIR WAS F ABRICATED AND INSTALLED IAW SRM 53-30-0. 2 L 7 3 4F A22WE 1998031200877 19980312 00877 WP 1998 3 12 CALA9800402 1 19980304 A 3350 EMBS13922 CHARGER ENGMAGNETICS DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68044 46903 THE L-4 DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-50-1. 2 L 7 3 4F A22WE 1998031200878 19980312 00878 NM 1998 3 12 CALA9800403 1 19980306 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312 FROM LBL 20 TO RBL 20. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-10-51, PA GE 220-223. 2 L 7 2 4F RT A16WE 1998031200879 19980312 00879 NM 1998 3 12 CALA9800404 1 19980307 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14337 23575 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 5 TO LBL 40. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51, FIGURE 20 5. 2 L 7 2 4F RT A16WE 1998031200880 19980312 00880 WP 1998 3 12 CALA9800405 1 19980308 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND LT FLOOR SUPPORT CHANNEL CORRODED AT STA 1887. THE FLOOR SUPPORT CHANNEL WAS REPLACED IAW GMM 10-900-0 1. 2 L 7 3 4F A22WE 1998031200881 19980312 00881 WP 1998 3 12 CALA9800406 1 19980308 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 420-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND FLOOR SUPPORT BEAM CORRODED AT STA 420 TO 440. THE CORRODED SECTION OF FLOOR SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01, PAGE 1. 2 L 7 3 4F A22WE 1998031200882 19980312 00882 WP 1998 3 12 CALA9800407 1 19980308 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP LAVATORY A CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND LAV A INBOARD SUPPORT BEAM CORRODED. THE CORRODED BEAM WAS REMOVED, A NEW SECTION WAS FABRICATED AND I NSTALLED IAW GMM 10-900-01, PAGE 1. 2 L 7 3 4F A22WE 1998031200883 19980312 00883 WP 1998 3 12 CALA9800408 1 19980308 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP LAVATORY B CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND LAV B INBOARD SUPPORT BEAM FORWARD END CORRODED. THE SUPPORT BEAM WAS REPLACED IAW GMM 10-900-01, PAGE 1. 2 L 7 3 4F A22WE 1998031200884 19980312 00884 1998 3 12 9803991232 4 19980303 A 3417 HG280D80 ADC DOUG DC10 DC1030 3023501 WP NR 1/2 MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 232NW 35047 21480 46961 AFTER TAKEOFF, RECEIVED FULL WINDSHEAR WARNING WITH DECREASE IN AIRSPEED ON CAPTAIN'S SIDE. ALL THREE ENGINES FIRWALLED FOR APPROXIMATELY ONE MINUTE WITH SUBSEQUENT FAILURE OF ALL CAPTIAN'S INSTRUMENTS. AFTER SWITCH TO CADC 2 RECOVERED SO ME OF CAPTAIN'S INSTRUMENTS BUT SOME OF FIRST OFFICER'S INSTRUMENTS BECAME UNRELIABLE. FLIGHT RETURNED TO EWR AND LANDE D WITHOUT INCIDENT. REPLACED CAPTAIN'S AIRSPEED INDICATOR AND NR 1 AND NR 2 AIR DATA COMPUTERS. INSPECTED ALL ENGINES AND FOUND WITHIN TOLERANCES PER MM, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998031200885 19980312 00885 WP 1998 3 12 9804001221 1 19980308 A 7930 21SN0434 BY PASS SWITCH DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 221NW 50993 4248 46579 455499 WHILE AT CRUISE, THE NR 3 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE CREW FOLLOWED THE COM 2.72.72 AND SHUT DOWN THE ENGINE. THERE WERE NO OTHER ABNORMAL INDICATIONS. THE AIRCRAFT RETURNED TO HNL AND LANDED WITHOUT DIFFICULTY. MAINTE NANCE REPLACED THE OIL FILTER BYPASS SWITCH AND THE MAIN ENGINE OIL FILTER. THE FILTER APPEARED CLEAN WITH NO EVIDENCE OF ENGINE DISTRESS. THE AIR 2 L 7 3 4F 4 F A22WE A23EA 1998031200886 19980312 00886 WP 1998 3 12 9804019611 1 19980308 A 2450 TERMINAL DOUG DC9 DC932 3022066 WP LT AC BUS LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 611NA 47435 DURING CRUISE FLIGHT AT 35,000 FT EN ROUTE, NUMEROUS SYSTEMS FAILED WITH MULTIPLE FLAGS AND ANNUNCIATOR LIGHTS. THESE S YSTEMS INCLUDED ACARS, TCAS, RADIO RACK FAN, PRIMARY LONGERON TRIM, NR 1 COMM, NR 1 NAV, GPWS, ADI FLAGS FOR SPEED, RUNW AY, STEER, AND FLIGHT RECORDER. AFTER APPROXIMATELY 10 MINUTES, ALL SYSTEMS RETURNED TO NORMAL. SHORTLY THEREAFTER, FU EL BOOST PUMP CIRCUIT BREAKERS POPPED. FLIGHT DIVERTED TO TUL. MAINTENANCE COULD NOT DUPLICATE MALFUNCTION ON GROUND. SUSPECT LOSS OCCURRED IN A PHASE OF THE LEFT AC ELECT SYSTEM. MAINTENANCE TIGHTENED SCREW AT WIRE TO LEFT A PHASE AC B US TERMINAL. REPLACED CIRCUIT BREAKER B1-273, LEFT GEN AC PWR RELAY AND LEFT GEN CONT PANEL, CHECKED OK. 2 L 7 2 4F A6WE 1998031200887 19980312 00887 WP 1998 3 12 9804039877 1 19980307 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECTION, FOUND AFT SECTION OF SEAT MOUNTED EMERGENCY LIGHTS AND AFT EMERGENCY EXIT SIGN INOPE RATIVE. REPLACED BLOWN FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998031200888 19980312 00888 WP 1998 3 12 9804049916 1 19980307 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN FAILED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 949N 47566 DURING PERIODIC CHECK, FOUND TAIL CONE CATWALK AND HANDLE EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031200890 19980312 00890 WP 1998 3 12 9804069928 1 19980307 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CAIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 8921E 45836 FORWARD GALLEY AND CABIN EMERGENCY LIGHTS ILLUMINATED IN FLIGHT AND COULD NOT BE EXTINGUISHED. MAINTENANCE REPLACED GAL LEY DOOR PACK AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031200891 19980312 00891 WP 1998 3 12 9804079986 1 19980307 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK NOR MAL. 2 L 7 2 4F A6WE 1998031200892 19980312 00892 WP 1998 3 12 9804089755 1 19980307 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 755NW 47179 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD FLIGHT ATTENDANT LOWER FLASHLIGHT INOPERATIVE. REPLACED BATTERY, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031200893 19980312 00893 WP 1998 3 12 9804091228 1 19980309 A 3610 BLEED DUCT DOUG DC10 DC1030 3023501 WP NR 1 ENGINE LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 228NW 46578 DURING CLIMB AND CRUISE, NR 1 NACELLE TEMPERATURE WAS 200C WITH PNEUMATIC TEMPERATURE INDICATOR AT 20C AND PNEUMATIC PRE SSURE AT 10 PSI. NACELLE TEMPERATURE WAS REDUCED BY REDUCING N1 TO 80 PERCENT. SHUTTING NR 1 PNEUMATIC SUPPLY OFF HAD NO EFFECT ON NACELLE TEMPERATURE. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND EVIDENCE OF LE AKAGE FROM 8TH STAGE BLEED DUCT. REPOSITIONED DUCT, LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998031200894 19980312 00894 WP 1998 3 12 9804109928 1 19980309 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 8921E 45836 FORWARD CABIN EMERGENCY EXIT LIGHTS ILLUMINATED AT GATE AND WOULD NOT SHUT OFF. REPLACED POWER SUPPLY AND BOTH BATTERIE S, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031200895 19980312 00895 WP 1998 3 12 9804119967 1 19980309 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9331 47263 DURING LINE MAINTENANCE INSPECITON, FOUND EMERGENCY LIGHTS ON TAIL CONE WALKWAY AND RIGHT RELEASE HANDLE INOPERATIVE. R EPAIRED TWO BROKEN WIRES IN TAIL CONE AND REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031200896 19980312 00896 EU 1998 3 12 WWMA9800045 1 19980307 A 7603 C821453 CABLE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE BROKEN A WWMA D E RETURN TO BLOCK ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 WP 15 253AE 340B253 LEFT ENGINE FAILED ON TAKEOFF AT APPROXIMATELY 300 FEET ABOVE GROUND. TAKEOFF WAS AT 100 PERCENT POWER AND THE CTOT WA S ON. THE ENGINE AUTOFEATHERED AND THE RIGHT ENGINE TORQUE INCREASED TO 107 PERCENT. ALL OTHER INDICATIONS WERE NORMAL . THE AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE FOUND THE CONDITION LEVER CABLE BETWEEN THE HMU GEARBOX AND THE PCU BROKEN 4 INCHES FROM THE HMU CONNECTOR. RELACED THE CABLE, PERFORMED A BORESCOPE INSPECTION AND GROUND RUN S. 2 L 7 2 4T 4 T RT A52EU E8NE 1998031200897 19980312 00897 EU 1998 3 12 WWMA9800044 1 19980307 A 2611 72111211002 DETECTOR SAAB SF340 340B 7860101 EU LAVATORY NO TEST A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 306AE 340B306 DURING PREFLIGHT, THE LAVATORY SMOKE DETECTOR WOULD NOT TEST. REPLACED THE LAVATORY SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998031200898 19980312 00898 EU 1998 3 12 WWMA9800048 1 19980307 A 3320 BA006281 BALLAST SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 15 326AE 340B326 APPROXIMATELY 2 MINUTES AFTER THE NR 2 ENGINE WAS STARTED AND THE NR 2 GENERATOR WAS SWITCHED ON. CREW REPORTED A VERY STRONG ELECTRICAL SMOKE ODOR IN THE PASSENGER AND CARGO COMPARTMENTS. MAINTENANCE FOUND THE ODOR TO BE COMING FROM OVER HEAD LIGHT AND WINDOW LIGHT BALLASTS AT SEATS 3, 4 AND 5A, REPLACED BOTH BALLASTS. 2 L 7 2 4T RT A52EU 1998031200899 19980312 00899 EU 1998 3 12 WWMA9800047 1 19980306 A 3320 BA006281 BALLAST SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 326AE 340B326 CREW REPORTED, WINDOW LIGHTS OVER SEAT 5BC SEEMED TO BE GETTING HOT AND EMITTING A HOT PLASTIC SMELL. MAINTENANCE ISOLA TED PROBLEM TO READING LIGHT AT 3A, LIGHT WAS DEFERRED. SMELL REOCCURED ON FLIGHT 5086 ON 4-7-98, MAINTENANCE FOUND OV ERHEAD AND WINDOW LIGHT BALLASTS FOR SEATS 3,4 AND 5A TO BE CAUSING THE SMELL. REPLACED BOTH BALLASTS. 2 L 7 2 4T RT A52EU 1998031200900 19980312 00900 EU 1998 3 12 WWMA9800046 1 19980307 A 3350 SIGN SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE O OTHER TX TAXI/GRND HDL 1 WP 15 345SB 340B345 DURING PREFLIGHT CREW, FOUND THE EMERGENCY EXIT SIGN AT ROW 8A HAD FALLEN OFF. MAINTENANCE RESECURED THE EMERGENCY EXIT SIGN. 2 L 7 2 4T RT A52EU 1998031200901 19980312 00901 EU 1998 3 12 QXEA9800247 1 19980309 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 RIGHT HAND FORWARD EMERGENCY LIGHT INOPERATIVE. RELAMPED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031200902 19980312 00902 NM 1998 3 12 98FDEA00166 1 19980310 A 7933 OIL TEMP BULB BOEING 727 72725 1384006 NM NR 3 ENGINE FAILED A FDEA E ENGINE SHUTDOWN N FALSE WARNING UK UNKNOWN 1 SO 25 508FE 18279 SHUT DOWN NR 3, HIGH OIL TEMPERATURE, PREFLIGHT INDICATION LOW OIL QUANTITY ON NR 3, 1.7 GALLON. SERVICED TO 2.2 AFTER MOTORING. ON TAKEOFF NOTICED QUANTITY 4.2, IN FLIGHT TEMPERATURE WENT TO EDGE OF RED BAND, SHUT DOWN AS TEMPERATURE CLI MBED INTO RED BAND. POST FLIGHT QUANTITY 4.2. DESERVICED OIL DUE TO OVER SERVICE. REMOVED AND REPLACED OIL TEMPERATUR E BULB PRECAUTIONARY REFERENCE MAINTENANCE MANUAL 79-34-21. 2 L 7 3 4F A3WE 1998031200903 19980312 00903 NM 1998 3 12 98FDEA00167 1 19980310 A 2612 FIRE WARN LIGHT BOEING 727 727277 138408S NM APU MALFUNCTION A FDEA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 240FE 20978 BOTH MASTER FIRE WARNING LIGHTS ILLUMINATE INTERMITTENTLY. ALL FIRE WARNING LIGHTS OFF PRIOR TO TAKEOFF. ONCE AIRBORNE APU FIRE LIGHT CAME ON STEADY. MASTER FIRE WARNING LIGHTS STARTED FLICKERING. REPLACED APU FIRE BOTTLE. FOUND CORROS ION ON PLUG D-4858P FOR R421 BLOCKING RECTIFIER. CLEANED SAME, ALSO REPLACED AURAL WARNING BOX. FIRE SYSTEM TESTS OK. RAN APU, NORMAL OPERATION. 2 L 7 3 4F RT A3WE 1998031200904 19980312 00904 EU 1998 3 12 98FDEA00168 1 19980310 A 2130 82010B040901 CPC AIRBUS 310 A310203 EU NR 1/2 DEFECTIVE A FDEA A UNSCHED LANDING L NO TEST CL CLIMB 1 SO 25 404FE 233 ON DEPARTURE, A/C WOULD NOT PRESSURIZE. PERFORMED BITE CHECKS ON CPC 1 AND 2 NO DEFECTS NOTED. PREFORMED MANUAL CPC OP ERATION, OPS CHECKS NORMAL. REMOVED AND REPLACED CPC NR 2 PRECAUTIONARY PER M/M 21-31-11. OPS CHECKS NORMAL PER M/M 21 -31-00. 2 L 7 2 4F RT A35EU 1998031200905 19980312 00905 WP 1998 3 12 98FDEA00152 1 19980304 A 5312 BULKHEAD DOUG DC10 DC1010F 3022111 WP BS 1501 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 CENTER WHEEL WELL COMPARTMENT RIGHT HAND VERTICAL BULKHEAD CRACKED AT UPPER AFT CORNER, APPROX FUS STA 1501. *S/D* INS TALLED DOUBLER AS PER SRM 53-00-01. N/R N00355. 2 L 7 3 4F A22WE 1998031200906 19980312 00906 NM 1998 3 12 98FDEA00169 1 19980310 A 5330 654237052 SKIN BOEING 727 72721C 138400M NM BS 460-4180 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 NR 0874 060 WHILE WORKING NR 0449, FOUND SKIN DAMAGED BS 460-480, STR 4 RT. SKIN AND STR 4 RT SLAP WILL BE REPAIRED ON NR 0842 2 L 7 3 4F A3WE 1998031200907 19980312 00907 NM 1998 3 12 98UAL900041 1 19980128 A 5320 65B0793785 PANEL BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NLG WW MISSING A UALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 29 158UA 21054 NOSE GEAR OPENED AT 310KTS AND FL 320. SLOWED TO 270KTS GEAR HANDLE UP, NO HELP. LESS VIBRATION WITH GEAR HANDLE UP. * S/D* FOUND PANEL 65B07937-85 MISSING. ABSENCE OF PANEL ALLOWED PRESSURIZATION OF NOSE GEAR WHEEL WELL TO ALLOW GEAR DO ORS TO MOVE OFF SENSORS. PANEL WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1998031200908 19980312 00908 NM 1998 3 12 98UAL900063 1 19980214 A 3810 HANDLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE POTABLE WATER NOT CLOSED A UALA A UNSCHED LANDING W INADEQUATE Q C NR NOT REPORTED 1 WP 29 584UA 26706 NO WATER PRESSURE AND LOUD NOISE FROM REAR OF AIRCRAFT. RETURNED TO FIELD. *S/D* THE POTABLE WATER SERVICE FILL VALVE HANDLE HAD BEEN LEFT IN THE OPEN POSITION DURING SERVICING. POTABLE WATER SERVICE FILL HANDLE WAS CLOSED. NO DEFECTS WERE FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 1998031200909 19980312 00909 WP 1998 3 12 98UAL900064 1 19980215 A 4900 APU DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL APU COMPT MALFUNCTIONED A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 1816U 46615 NR 2 PNEUMATIC INOP AC OIL SMELL IN CABIN. *S/D* BURNED OUT NR 2 PACK. REPLACED COALESCER BAG. ALSO, REPLACED APU AS PRECAUTIONARY MEASURE. 2 L 7 3 4F 4 F A22WE E23EA 1998031200910 19980312 00910 WP 1998 3 12 98UAL900069 1 19980217 A 2170 COALESCER BAG DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DIRTY A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 1849U 46939 STRONG PUNGENT ODOR REPORTED BY CABIN CREW NEAR FORWARD GALLEY AREA. *S/D* REPLACED ALL THREE COALESCER BAGS, NO RECUR RENCE. 2 L 7 3 4F 4 F A22WE E23EA 1998031200911 19980312 00911 NM 1998 3 12 98UAL900083 1 19980222 A 3213 161N16253 AXLE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT MLG CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 503UA 24624 AIRCRAFT AT MAINTENANCE BASE FOR GEAR CHANGE. NEW RT MLG AFT INBD AXLE SHEARED AFTER DE-JACKING OF AIRCRAFT. *S/D* HE AT DAMAGE INDUCED BY OEM FINISH GRINDING ON THE OD CHROME PLATE, 19.25 INCHES FROM AXLE THREADED END. REPLACED AXLE AND INSPECTED REMAINING LOT AT BOEING AND MENASCO. 2 L 7 2 4F 4 F RT A2NM E17NE 1998031200912 19980312 00912 NM 1998 3 12 98UAL900087 1 19980223 A 3350 1060091102 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7945U 21899 EMERGENCY EXIT LIGHT ABOVE DOOR 1L INOPERATIVE. *S/D* BATTERY FAILED. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1998031200913 19980312 00913 NM 1998 3 12 98UAL900091 1 19980225 A 3350 90035A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7290U 21568 EMERGENCY WING ILLUMINATING LIGHT ON FUSELAGE FOUR WINDOWS AFT OF LEFT OVERWING EXIT IS INOPERATIVE. *S/D* REPLACED B ATTERY PACK DUE TO FAILURE. 2 L 7 3 4F 4 F A3WE E2EA 1998031200914 19980312 00914 NE 1998 3 12 98UAL900093 2 19980301 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE OVERHEAT A UALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 29 7466U 49237 21920 700494 NR 3 ENGINE FIRE WARNING ILLUMINATED AFTER TAKEOFF AT 1000 FEET. RETURNED TO LAX. ALSO, HAD VIBRATION ON FINAL. *S/D* CREW REPORTED EGT AT 650 AND OIL TEMPERATURE AT 130 DEGREES. REPLACED ENGINE DUE TO OVERHEAT. 2 L 7 3 4F 4 F A3WE E2EA 1998031200915 19980312 00915 NM 1998 3 12 98UAL900094 1 19980301 A 3610 10610651 DUCT AIR RESEARCH 320115601U BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7451U 21905 NR 1 ENGINE STRUT OVERHEAT LIGHT GOES OUT WHEN BLEED SHUT OFF. *S/D* THE SHORT FLEX DUCT WAS LEAKING. REPLACED FLEX D UCT. ALSO, REPLACED THE ANTI-ICE VALVE PER PRECAUTIONARY. 2 L 7 3 4F 4 F A3WE E2EA 1998031200917 19980312 00917 NM 1998 3 12 98UAL900096 1 19980227 A 5753 BOLT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE TE FLAP FAIRING MISSING A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 104UA 26902 LEFT SIDE INBOARD FLAP FAIRING WAS DANGLING AFTER FLAP RETRACTION. *S/D* THE NUT AND BOLT COMBINATION THAT SECURES THE CANOE FAIRING DRIVE ROD TO THE INBOARD MIDFLAP DISLODGED. ONCE THE BOLT AND NUT DISLODGED, THE FAIRING WAS ABLE TO DRO P DOWN. THE CORRECTIVE ACTION WAS TO REPLACE THE BOLT, NUT AND COTTER PIN COMBINATION THAT ATTACHES THE FAIRING CONTROL DRIVE TO THE MIDFLAP. 2 L 7 4 4F 4 F RT A20WE E24NE 1998031200918 19980312 00918 WP 1998 3 12 98UAL900097 1 19980303 A 3350 LIGHTS DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1817U 46616 SMALL RECTANGULAR LIGHTS ARE 1L AND 1R NOT OPERATIONAL DURING CHECK. *S/D* REPLACED EEL STRIP AT RIGHT GALLEY FORWARD OF CROSS AISLE 2 AND PUSHED BACK SOCKET AT DOOR IL EXIT SIGN PLUG. ALL EEL LIGHTS CHECK OK. 2 L 7 3 4F 4 F A22WE E23EA 1998031200919 19980312 00919 NM 1998 3 12 98UAL900099 1 19980303 A 3350 10617844 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7459U 21913 LEFT AFT OVERWING WALKWAY EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED POWER SUPPLY BASE ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1998031200920 19980312 00920 NM 1998 3 12 98UAL900100 1 19980305 A 3350 5106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA O OTHER L NO TEST IN INSP/MAINT 1 WP 29 7293U 21571 FORWARD AISLE OVERWING EXIT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE BY ROW 21 AND 8 CEILING LIGHTS BATTERY WILL NOT HOL D A CHARGE. *S/D* CLEANED BATTERY CONTACTS. LIGHT WORKS OK WITH OLD BATTERIES, BUT REPLACED BATTERIES AS PRECAUTIONAR Y. 2 L 7 3 4F 4 F A3WE E2EA 1998031200921 19980312 00921 NM 1998 3 12 98UAL900101 1 19980303 A 2421 IDG SUNSTRAND MR24114 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT ENGINE DISCONNECTED A UALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 29 660UA G0573 27115 RIGHT GENERATOR EICAS MESSAGE DISPLAYED. GENERATOR DRIVE LIGHT ILLUMINATED. GENERATOR DRIVE DISCONNECTED. *S/D* MEC HANICS PERFORMED BPCU BIT TEST, INLET TEMP SENSOR-WIRING RIGHT IDG MESSAGE WAS DISPLAYED. DURING IDG INSPECTION FOUND T 2 POWER CABLE TERMINAL STUD LOOSE DUE TO OVERHEAT. THE IDG WAS REPLACED. SYSTEM OPERATIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 1998031200922 19980312 00922 NM 1998 3 12 98UAL900102 1 19980305 A 3230 273T63015 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE MLG UPLOCK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 644UA 25094 LEFT MAIN LANDING GEAR REMAINED DOWN AFTER TAKEOFF. RETURNED TO FIELD. *S/D* MLG DRAG BRACE LOCK ACTUATOR FAILED. IN TERNAL PISTON RETENTION NUT WAS NOT INSTALLED CORRECTLY. REPLACED ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 1998031200923 19980312 00923 NM 1998 3 12 98UAL900103 1 19980305 A 3610 BLEED AIR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE INOPERATIVE A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 770UA 26925 FLIGHT RETURNED TO IAD DUE TO AFTER TAKEOFF, RIGHT ENGINE BLEED INOPERATIVE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998031200924 19980312 00924 WP 1998 3 12 ABXA9800153 1 19980309 A 5330 5910228120 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 1038 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND CRACKED FUSELAGE SKIN AT STATION 1038 AND LONGERON 14L. REPAIRED SKIN IAW DC9 SRM 53-04. 2 L 7 2 4F A6WE 1998031200925 19980312 00925 WP 1998 3 12 ABXA9800154 1 19980309 A 5753 99558223N ANGLE DOUG DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND ATTACH ANGLE INSIDE LEFT FLAP CRACKED, ACCESS THROUGH PANEL 1548. REPLACED ATTACH ANGLE IAW DC9 S RM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998031200926 19980312 00926 WP 1998 3 12 ABXA9800155 1 19980309 A 5320 39248461 ANGLE DOUG DOUG DC9 DC941 302207N WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND EXFOLIATION CORROSION ON L-ANGLE AT OUTBOARD, FORWARD CORNER OF WHEEL WELL AT SLANT PANEL. REPLAC ED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998031200927 19980312 00927 WP 1998 3 12 ABXA9800156 1 19980309 A 5320 99234359 BRACKET DOUG DOUG DC9 DC941 302207N WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND ATTACH BRACKET CRACKED AT TOP EDGE OF TRAPEZOIDAL PANEL IN LEFT WHEEL WELL. REPLACED ANGLE IAW DC 9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998031200928 19980312 00928 WP 1998 3 12 ABXA9800157 1 19980309 A 5400 995819128 STIFFENER DOUG DOUG DC9 DC941 302207N WP NR 1 ENG PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND NR 1 ENGINE PYLON STIFFENER CRACKED, (6 ABOVE FUEL SHROUD). REPLACED STIFFENER IAW DC9 SRM 51-30- 2 AND 51-30-5. 2 L 7 2 4F A6WE 1998031200929 19980312 00929 WP 1998 3 12 ABXA9800158 1 19980309 A 5320 9957739IN SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 1021 BETWEEN LONGERON 14R AND 16R. REPLACED SHEAR TIE IAW DC9 SRM 51 -30-2. 2 L 7 2 4F A6WE 1998031200930 19980312 00930 WP 1998 3 12 ABXA9800159 1 19980309 A 5510 4911390503 LOCKING TANG DOUG DOUG DC9 DC941 302207N WP RT HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND FORWARD LOCKING TANGS CRACKED AND LOCKING PLATE SHIFTED ON THE HORIZONTAL STABILIZER MAIN ATTACH B OLT, RIGHT SIDE WHERE STABILIZER ATTACHES TO CENTER SECTION. REPLACED BOLT, SLEEVE, AND RETAINER IAW DC9 MM 55-10-0. 2 L 7 2 4F A6WE 1998031200931 19980312 00931 WP 1998 3 12 ABXA9800170 1 19980309 A 3260 189915 SWITCH DOUG DC8 DC863 302198A WP LT MLG DAMAGED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 811AX 46113 ON GEAR RETRACTION RED LIGHT EXTINGUISHED BUT CAME BACK ON DURING UPLATCH CHECK. RECYCLED GEAR, WHEN GEAR WAS RETRACTED , RED INTRANSIT LIGHT REMAINED ON. REPLACED LEFT UPLATCH PROXIMITY SWITCH, OPS CHECKED GOOD IAW DC8 MM 32-60-00. 2 L 7 4 4F 4A25 1998031200932 19980312 00932 WP 1998 3 12 MWEA98324 1 19980309 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 389-427 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE RIGHT HAND CUSP WEB WAS FOUND CORRODED FROM FS 389 TO 427. REMOVED AND REPLACED SECTION OF CUSP WEB. 2 L 7 2 4F A6WE 1998031200933 19980312 00933 WP 1998 3 12 MWEA98325 1 19980309 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 457-489 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE CUSP WEB FROM FS 457 TO 489 RBL 54 HAS CORROSION. CORROSION BLENDED OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLE R. 2 L 7 2 4F A6WE 1998031200934 19980312 00934 WP 1998 3 12 MWEA98326 1 19980309 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 951-965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CUSP MEMBRANE AT LONGERON 18R FS 951 TO 965 WAS FOUND CORRODED. FABRICATED AND INSTALLED REPLACEMENT SECTION AND SPLICE S. 2 L 7 2 4F A6WE 1998031200935 19980312 00935 WP 1998 3 12 MWEA98327 1 19980309 A 5320 991040 WEB DOUG DC9 DC932 3022066 WP BS 759 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE SUB FLOOR CUSP WEB WAS FOUND CRACKED AT FS 759 RBL 48. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998031200936 19980312 00936 WP 1998 3 12 MWEA98328 1 19980309 A 5347 5916814 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 880-965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RT OUTBOARD SEAT TRACK WAS FOUND CORRODED OUT OF LIMITS FROM FS 880 TO FS 965. REMOVED AND REPLACED SECTION OF TRACK. 2 L 7 2 4F A6WE 1998031200937 19980312 00937 WP 1998 3 12 MWEA98329 1 19980309 A 5347 5910152 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 531-965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND INBOARD SEAT TRACK WAS FOUND CORRODED OUT OF LIMITS FROM FS 531 TO FS 965. REMOVED AND REPLACED SEAT TRACK. 2 L 7 2 4F A6WE 1998031200938 19980312 00938 WP 1998 3 12 MWEA98330 1 19980309 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 203ME 47673 DURING SERVICE CHECK, FOUND LT NACELLE EMERGENCY LIGHT INOPERATIVE. MTC REMOVED AND REPLACED LT NACELLE BATTERY PACK. 2 L 7 2 4F A6WE 1998031200939 19980312 00939 WP 1998 3 12 MWEA98331 1 19980308 A 3350 60030431 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 400ME 45727 THE EMERGENCY LIGHT ABOVE AFT FLIGHT ATTENDANT SEAT CAME ON WITH SWITCH IN ARMED POSITION. MTC REMOVED AND REPLACED EME RGENCY BATTERY PACK IN LT LAV. 2 L 7 2 4F A6WE 1998031200940 19980312 00940 WP 1998 3 12 MWEA98332 1 19980308 A 2560 591769037 SLIDE COVER DOUG DC9 DC914 3022034 WP FWD GALLEY FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 THE GALLEY SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998031200941 19980312 00941 WP 1998 3 12 MWEA98333 1 19980309 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP PAX DOOR LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 602ME 48133 PAX DOOR EMERGENCY SLIDE COVER LOOSE. RESECURED SLIDE COVER. 2 L 7 2 4F A6WE 1998031200942 19980312 00942 NM 1998 3 12 MWEA98334 1 19980307 A 5730 SKIN DOUG MD88 MD88 3023688 NM RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 49760 TEMPORARY REPAIR INSTALLED ON OUTBOARD LEADING EDGE OF FUEL DOOR CUTOUT ON RT WING. INSTALLED PERMANENT DOUBLER REPAIR IAW DOUGLAS TELEX. 2 L 7 2 4F RT A6WE 1998031200943 19980312 00943 WP 1998 3 12 MWEA98335 1 19980308 A 2560 113313 DOOR SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 209ME 47730 THE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1998031200944 19980312 00944 WP 1998 3 12 RRXA98066 1 19980306 A 2450 BUS POWER LIGHT DOUG DC8 DC863 302198A WP NR 1 ILLUMINATED A RRXA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 WP 15 797AL 46163 EN ROUTE, NR 1 ELECTRICAL BUSS POWER FAIL LIGHT ILLUMINATED, NR 1 BUSS DEFERRED TO KDEN. RESET NR1 BUSS, PERFORMED ENG RUN ON ALL 4 ENGS UNDER VARIOUS ELECTRICAL LOADS, SYS OPS CK GOOD. 2 L 7 4 4F 4A25 1998031200945 19980312 00945 NM 1998 3 12 VNAA9803008 1 19980306 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 422JS 39698 7602 3018 PRIOR TO TAXI, ON ENGINE STARTUP AND SUBSEQUENT TEST, THE EMERGENCY FLOOR LIGHTS AT ROW 4, 5 AND 6, WERE FOUND TO BE INO PERATIVE. MAINTENANCE INSPECTED AND REPLACED THE 5 LK EMERGENCY BATTERY PACK IN ACCORDANCE WITH DORNIER MAINTENANCE MAN UAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031200946 19980312 00946 WP 1998 3 12 CKSA98085 1 19980306 A 3260 CONNECTOR DOUG DC8 DC861 3021952 WP RT MLG DOOR DIRTY A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 812CK 45890 DURING CLIMB, DOOR NOT LATCHED LIGHT CAME ON AND THE RIGHT DOOR UNSAFE LIGHT. GEAR UPLATCH CHECK WAS NORMAL. CLEANED R IGHT GEAR DOOR SWITCH ELECTRICAL CONNECTOR PER MM 32. 2 L 7 4 4F 4A25 1998031200952 19980312 00952 NM 1998 3 12 MZZA98035 1 19980109 A 5753 6521796103 FAIRING BOEING 727 7272F9 138407D NM TE FLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 KUL - NR 7 FLAP TRACK MID FAIRING FOUND CRACKED AND DELAMINATED AT FWD EDGE OF O/BOARD SKIN. TYPICAL SRM DOUBLER REPAIR IAW ECRA 5720-01628. (M) 2 L 7 3 4F RT A3WE 1998031200961 19980312 00961 NM 1998 3 12 USSABB98012 1 19980204 A 3350 427303 TRANS-RECTIFIER BOEING 757 7572B7 1384964 NM E/E COMPT FAILED A USAA K NONE L NO TEST CR CRUISE 1 EA 19 612AU 27124 LGA - SEVERAL REPORTS OF THE EMRGENCY LIGHTS INTERMITTENTLY ILLUMINATING WHILE IN FLIGHT. LGA MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT CONTROL MODULES AND AN AFT AISLE LIGHT ASSEMBLY. SUBSEQUENTLY, PIT MAINTENANCE REPLACED THE RIGHT TRANSFORMER-RECTIFIER UNIT. (M) 2 L 7 2 4F RT A2NM 1998031200962 19980312 00962 WP 1998 3 12 USAAD98021 1 19980119 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 PHL - CABIN LOW LEVEL LIGHTS FAILED TEST. MAINTENANCE REPLACED BATTERIES. (M) 2 L 7 2 4F A6WE 1998031200963 19980312 00963 EU 1998 3 12 USAAF98010 1 19980130 A 3620 66072105 SWITCH FOKKER F28 F28MK0100 4990807 EU PNEUMATIC SYS FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 854US 11282 FLT 1275 - PIT-MSP - ON CLIMB-OUT FROM PIT WITH CLIMB POWER SET, 'WING ANTI-ICE LOW CAPACITY' MESSAGE ANNUNCIATED ON MUL TI FUNCTION DISPLAY. DUE TO WEATHER CONDITIONS IN MSP, FLIGHT DIVERTED TO PHL FOR MAINTENANCE AND SCHEDULING CONVENIENC E. FLIGHT LANDED PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE WING LOW PRESSURE WARNING SWITCH AND ADJUSTED BOTH PNEUMTIC SYSTEM PRESSURE REGULATING SHUTOFF VALVES. (M) 2 L 7 2 4F RT 1998031200964 19980312 00964 NM 1998 3 12 USAASB98029 1 19980127 A 3350 6013211 POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 276AU 22888 ROA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998031200965 19980312 00965 NM 1998 3 12 98ZZZM290 1 19980127 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 276AU 22888 ROA - MAINTENANCE FOUND THE LEFT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998031200966 19980312 00966 NM 1998 3 12 USAASB98026 1 19980131 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 270AU 22882 CLE - MAINTENANCE FOUND THE FORWARD ENTRY DOOR AND THE FORWARD SERVICE DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998031200967 19980312 00967 EU 1998 3 12 USAAF98011 1 19980202 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 867US 11312 IND - EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1998031200968 19980312 00968 1998 3 12 USAAD98022 4 19980130 A 2565 1133169 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR PUNCTURED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 925VJ 48145 PIT - THE GALLEY SERVICE DOOR EMERGENCY SLIDE INFLATION BOTTLE PUNCTURED THE SLIDE DURING INFLATION. MAINTENANCE REPLAC ED THE SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998031200969 19980312 00969 NM 1998 3 12 USAABB98013 1 19980207 A 3397 WIRE BOEING 757 7572B7 1384964 NM CABIN SHORTED A USAA O OTHER L NO TEST CR CRUISE 1 EA 19 612AU 27124 PIT - CONTINUED REPORTS OF THE EMERGENCY LIGHTS INTERMITTENTLY ILLUMINATING WHILE IN FLIGHT. PIT MAINTENANCE FOUDN A WI RE SHORTED TO A TV MONITOR BRACE. WIRE WAS REPAIRED AND THE BRACE REPOSITIONED. (M) 2 L 7 2 4F RT A2NM 1998031200970 19980312 00970 NM 1998 3 12 USAASB98033 1 19980202 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 508AU 23383 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE AFT ENTRY DOOR, THE BULLNOSE LIGHT AT ROW 25 RIGHT SIDE AND THE ESCAPE SLIDE LIGHT AFT OF AFT RIGHT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE RIGHT SIDE OF AFT ENTRY LIGHT CEILING. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998031200971 19980312 00971 NM 1998 3 12 USAASB98031 1 19980206 A 3230 BACR13CG2AB SAFETY RELAY BOEING 737 737301 1384611 NM E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 591US 23936 BWI - FLT 141, DURING CLIMB-OUT FROM BWI, CAPTAIN TRIED TO LIFT THE GEAR HANDLE TO STOW THE GEAR BUT THE HANDLE WOULD NO T MOVE PAST THE OFF POSITION. AFTER SEVERAL ATTEMPTS TO RAISE THE GEAR FAILED, CAPTAIN DECIDED TO RETURN TO FIELD AT BW I. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. OVERRIDE TRIGGER ON LANDING GEAR CONTROL LEVER WAS NOT USED. MAINTENANCE REPAIRED WIRING AT THE LANDING GEAR LOGIC SHELF E11 AND REPLACED THE R276 SAFETY RELAY. SYSTEM OPERA TIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1998031200972 19980312 00972 NM 1998 3 12 USAASB98034 1 19980206 A 5414 PANEL BOEING 737 7373B7 1384580 NM LT PYLON LOOSE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 533AU 24515 MCI - FLT 150, DURING CRUISE, PASSENGER NOTIFIED FLIGHT CREW THAT A PANEL ON TOP OF THE LEFT ENGINE PYLON FAIRING WAS LO OSE AND BLOWING IN THE WIND. NINE SCREWS APPEARED TO BE MISSING IN THE PANEL. FLIGHT DIVERTED TO MCI AND LANDED WITHOU T INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE INSTALLED SCREWS AND SECURED PANEL ON TOP OF THE LEFT ENGINE PYLON FAIRING. (M) 2 L 7 2 4F RT A16WE 1998031200973 19980312 00973 NM 1998 3 12 USAASB98027 1 19980131 A 5210 DOOR BOEING 737 737301 1384611 NM PAX COMPT NOT LATCHED A A USAA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 19 300AU 23228 PIT - FLT 1026 - UPON CLIMB-OUT FROM PIT, AIRCRAFT WAS UNABLE TO PRESSURIZE. FLT LEVELED OFF AT 7,000 FT. FLT ATTENDAN T REPORTED THAT THE AFT LEFT ENTRY DOOR DID NOT APPEAR TO BE CLOSED PROPERLY. NO DOOR WARNING LIGHTS WERE ILLUMINATED I N THE COCKPIT. CAPTAIN DECIDED TO RETURN TO FIELD AT PIT WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENC Y WAS DECLARED. MAINTENANCE FOUND THE AFT LEFT ENTRY DOOR NOT PROPERLY CLOSED AND LOCKED EVEN THOUGH DOOR WARNING LIGHT WAS NOT ILLUMINATED. CLOSED DOOR PROPERLY. AIRCRAF TOK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A16WE 1998031200974 19980312 00974 NM 1998 3 12 USAASB98032 1 19980206 A 2751 1817389 TRANSMITTER BOEING 737 737301 1384611 NM RT TE FLAP FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 342US 23511 PIT - FLT 544 - AFTER TAKEOFF AND DURING FLAP RETRACTION, CAPTAIN REPORTED THAT THE TRAILING EDGE FLAPS WOULD NOT RETRAC T TO THE UP POSITION BUT WOULD RETRACT TO BETWEEN FLAP POSITION 1 AND 2. CAPTAIN ACCOMPLISHED ALTERNATE FLAP EXTENSION PROCEDURE TO EXTEND FLAPS AND RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLA RED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FLAP POSITION TRANSMITTER PER MM 27-58-12. OPERATIONAL CHECK NORMAL. ( M) 2 L 7 2 4F RT A16WE 1998031200975 19980312 00975 WP 1998 3 12 USAAD98023 1 19980209 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 960VJ 47505 IND - THE EMERGENCY LIGHTS FOR THE AFT OVERWING EXIT SIGNS WERE INOPERATIVE, AND TEH FORWARD REMOVAVLE EMERGENCY LIGHT D ID NOT SHOW CHARGING AND THE LIGHT DID NOT OPERATE. MAINTENANCE REPLACED THE BATTERY FOR THE OVERWING EXIT SIGNS AND RE PLACED THE REMOVABLE LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998031200976 19980312 00976 WP 1998 3 12 98ZZZM291 1 19980209 A 3350 1001191 LIGHT DOUG DC9 DC931 3022065 WP CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 960VJ 47505 IND - THE EMERGENCY LIGHTS FOR THE AFT OVERWING EXIT SIGNS WERE INOPERATIVE, AND TEH FORWARD REMOVAVLE EMERGENCY LIGHT D ID NOT SHOW CHARGING AND THE LIGHT DID NOT OPERATE. MAINTENANCE REPLACED THE BATTERY FOR THE OVERWING EXIT SIGNS AND RE PLACED THE REMOVABLE LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998031200977 19980312 00977 EU 1998 3 12 USAAF98012 1 19980206 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU NLG FAILED A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 854US 11282 FLT 1158 - RIC-PHL - ON FINAL APPROACH TO PHL, NOSE GEAR DOWN AND LOCKED GREEN INDICATOR DID NOT ILLUMINATE. CREW RECYC LED GEAR AND ALL INDICATORS ILLUMINATED NORMALLY. FLIGHT LANDED PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED BOT H LAMPS IN NOSE GEAR UNSAFE INDICATOR MODULE. (M) 2 L 7 2 4F RT 1998031200978 19980312 00978 EU 1998 3 12 USAAF98013 1 19980207 A 3234 715381 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU NLG FAILED A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 854US 11282 FLT 775 - PIT-MCI - DURING FINAL APPROACH TO MCI WHEN LANDING GEAR SELECTED DOWN, CREW DID NOT RECEIVE A GREEN 'NOSE GEA R DOWN AND LOCKED' INDICATION. CREW RECYCLED LANDING GEAR AND ALL INDICATIONS WERE NORMAL. FLIGHT LANDED MCI WITHOUT F URTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR SELECTOR VALVE AND RIGGED THE SYSTEM. (M) 2 L 7 2 4F RT 1998031200979 19980312 00979 WP 1998 3 12 TWAA9802102 1 19980208 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 918TW 49367 STL - FLT 518 - DURING PREFLIGHT, THE EGRESS LIGHTS WERE FOUND INOPERATIVE FROM ROWS 29 THROUGH 33. ALSO, THE AFT EXIT SIGN WAS INOP. REPAIRED BROKEN FEEDER WIRE TO EGRESS LIGHT STRIP, AND REPLACED POWER SUPPLY FOR THE SIGN. (M) 2 L 7 2 4F A6WE 1998031200980 19980312 00980 NM 1998 3 12 TWAA9802101 1 19980209 A 8012 1757441 PRESSURE SWITCH BOEING 727 727231 1384079 NM NR 3 ENGINE WORN A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 54352 21984 SLC - FLT 146 - NR 3 ENGINE START VALVE LIGHT CAME ON IN FLIGHT. SHUT ENGINE DOWN AND RETURNED TO SLC. FOUND BAD PRESS SWITCH ON START VALVE. REPLACED SWITCH AND START VALVE. (M) 2 L 7 3 4F A3WE 1998031200981 19980312 00981 WP 1998 3 12 TWAA9802002 1 19980207 A 3230 HANDLE DOUG DC9 DC983 3022083 WP MAIN GEAR OUT OF POSITION A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 9406W 53126 STL - FLT 347 - DURING TAKEOFF STL, THE LANDING GEAR FAILED TO RETRACT. RETURNED TO STL. MAIN GEAR BYPASS HANDLE WAS R EPOSITIONED FROM THE BYPASS TO THE NORMAL POSITION. (M) 2 L 7 2 4F RT A6WE 1998031200982 19980312 00982 WP 1998 3 12 TWAA9802001 1 19980202 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1366 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 902TW 49153 STL - DURING OP-9 MAINTENANCE CHECK, THE LOWER LONGERON LEG WAS FOUND DAMAGED AT L23 STATION 1366 AT APU AREA. REPAIRED L23 PER ARA 12000. (M) 2 L 7 2 4F A6WE 1998031200983 19980312 00983 NM 1998 3 12 TAOA029804 1 19980209 A 3260 106122615 FLT/GND SENSOR BOEING 727 727225 1384077 NM LT MLG FAILED A TAOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 922TS 20415 FLT 6081 - BOS-LGA - AIRCRAFT AT GATE SMOKE IN CABIN BEFORE DEPARTURE, BOTH AIRCRAFT PACKS OVERHEATED WITH PACK GROUND C OOLING FAN DOORS FULL OPEN. SMOKE IN CABIN, PASSENGERS DEPLANED. REPLACED FLT/GROUND SHIFT SENSOR ON LEFT MAIN LANDING EAR PER MM 32-31-0. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998031200984 19980312 00984 NM 1998 3 12 TSAA9853078 1 19980202 A 5313 STRINGERS BOEING 737 7372M6C 1384708 NM FUSELAGE CUT A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 CUT STRINGERS 23 AND 24R TO FACILITATE AFT OUTFLOW VALVE DOUBLER INSTALLATION. REPAIRS STRINGERS PER SRM 53-10-3 USING NEW DOULBER. (M) 2 L 7 2 4F RT A16WE 1998031200985 19980312 00985 NM 1998 3 12 TSAA9857079 1 19980202 A 5753 SKIN BOEING 737 7372M6C 1384708 NM TE FLAP CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DURING CPC CHECK, FOUND SKIN CRACK ON UNDERSIDE OF INBOARD AFT TRAILING EDGE FLAP AT WLB 157. REPAIRED PER SRM 57-50-4. (M) 2 L 7 2 4F RT A16WE 1998031200986 19980312 00986 EU 1998 3 12 RAIA980119 1 19980119 A 7332 1103P0645 PRESSURE SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 872AE 872 FLT 4714 - FAT - LEFT ENGINE FUEL LOW PRESSURE CAPTION ILLUMINATED ON TAKEOFF. MAINTENANCE REPLACED LEFT ENGINE FUEL LO W PRESSURE SWITCH. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998031200987 19980312 00987 NE 1998 3 12 REXA98025 2 19980122 A 7320 CLAMP SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE LT P3 PIPE LOOSE A REXA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 107PX 340A010 LEFT ENGINE WOULD NOT EXCEED 60 PERCENT TORQUE AND RAN 100-150 DEGREES HOTTER THAN RIGHT. FOUND HP P-3 PIPE CLAMP OFF. REINSTALLED CLAMP AND RUN CHECKS GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998031200988 19980312 00988 WP 1998 3 12 WTAA980022 2 19980205 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT LOW POWER A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 401UE 729 FAT - LEFT ENGINE FAILED TO MAKE TAKEOFF TORQUE. TAKEOFF ABORTED. MAINTENANCE PERFORMED GROUND RUNS AND HIGH SPPED TAX I. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998031200989 19980312 00989 WP 1998 3 12 VTZA98026 2 19980125 A 7320 8974575 TTL VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 495UE 818 FLT 6391 - IAD-CHO - DURING CRUISE, EXPERIENCED A FLUCTUATION OF THE RT EGT AND TQ INDICATIONS. AIRCRAFT RETURNED TO IA D WITH NO PROBLEM. AIRCRAFT TAXIED TO THE GATE WHERE MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCHED TO T HE AIRCRAFT AND REMOVED AND REPLACED THE RT ENGINE TTL VALVE. ALL REQUIRED CHECKS WERE ACCOMPLISHED AND THE AIRCRAFT WA S RELEASED FOR SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998031200990 19980312 00990 NE 1998 3 12 USAAD98014 2 19980122 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT VIBRATION A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 EA 19 822US 49139 708117 CLT-BUF - FLT 825 - DURING CRUISE THE FLIGHT CREW NOTICED VIBRATION FROM THE LEFT ENGINE. THE CREW REDUCED THE POWER TO IDLE, AND THE ENGINE STAYED WITHIN NORMAL PARAMETERS. THE AIRCRAFT THEN DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED THE ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998031200991 19980312 00991 NE 1998 3 12 TSAA9880077 1 19980127 A 7711 ACCESSORY UNIT BOEING 737 7372Q9 138448M NM PWA JT8 JT8D9A 52048 NE ENGINE FAILED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL M00748 21719 FLT 302 - HNL-OGG - ON ENGINE RUN UP FOR TAKEOFF, BOTH EPR CIRCUIT BREAKERS POPPED GAUGES FROZE. GROUND RAN BOTH ENGINE S. OPS CHECKED OK FOR SERVICE. REPLACED ENGINE ACCESSORY UNIT FOR PRECAUTIONARY REASON. OPS CHECK OK. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998031200992 19980312 00992 WP 1998 3 12 VTZA98016 2 19980115 A 7320 8974575 TTL BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 27 495UE 818 FLT 6362 - SYR-IAD - DURING TAKEOFF EXPERIENCED A DISCREPANCY WITH THE RT ENGINE ONLY MAKING 90 PERCENT TAKEOFF TORQUE. THE AIRCRAFT RETURED TO SYR AND MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE REMOVED AND REPLACED THE TTL BYPASS VALV E ON THE RT SIDE IAW MM PROCEDURES. ALL REQUIRED CHECKS COMPLETED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998031200995 19980312 00995 NE 1998 3 12 SIMA980312 2 19980201 A 7200 ENGINE AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE RIGHT SEIZED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 21 142DD 040 PCE121172 ORD - FLT 4309 - AFTER TAKEOFF, NR 2 ENGINE LOST OIL PRESSURE. CREW SHUT DOWN ENGINE AND RETURNED TO ORD. RAI NR 2 ENG INE. PERFORMED GROUND RUNS SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998031200996 19980312 00996 WP 1998 3 12 WTAA980030 2 19980208 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT LOW POWER A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 17 425UE 798 MOD - LEFT ENGINE FAILED TO ACHIEVE MINIMUM STATIC TORQUE ON TAKEOFF ROLL. TAKEOFF ABORTED. UNABLE TO DUPLICATE REPORT ED DISCREPANCY ON SUBSEQUENT ENGINE RUN. ALL ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998031200997 19980312 00997 WP 1998 3 12 WTAA980023B 2 19980205 A 7210 31015351 IDLER GEAR BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT RED GEARBOX FAILED A A WTAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 17 426UE 774 P63305 LAX - LEFT ENGINE POWER LOSS FOLLOWED BY AUTO SHUT DOWN REPORTED ON CLIMB-OUT. CREW COMPLETED CHECKLIST PROCEDURES AND DECLARED EMERGENCY. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE. AIRC RAFT RETURNED TO SERVICE. ON SUBSEQUENT ENGINE DISASSEMBLY FOUND DIAPHRAGM FIRST IDLER GEAR AND GEARCASE FIRST ACCESSOR Y IDLER GEAR TO HAVE EXPERIENCED GEAR TOOTH FAILURE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998031200998 19980312 00998 WP 1998 3 12 WTAA980023A 2 19980205 A 7210 31022861 IDLER GEAR BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT RED GEARBOX FAILED A A WTAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 17 426UE 774 P63305 LAX - LEFT ENGINE POWER LOSS FOLLOWED BY AUTO SHUT DOWN REPORTED ON CLIMB-OUT. CREW COMPLETED CHECKLIST PROCEDURES AND DECLARED EMERGENCY. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE. AIRC RAFT RETURNED TO SERVICE. ON SUBSEQUENT ENGINE DISASSEMBLY FOUND DIAPHRAGM FIRST IDLER GEAR AND GEARCASE FIRST ACCESSOR Y IDLER GEAR TO HAVE EXPERIENCED GEAR TOOTH FAILURE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998031700003 19980317 00003 NM 1998 3 17 CALA9800390 1 19980305 A 3320 1000401 SIGN BOEING 737 737222 1384473 NM CABIN SHORTED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 10236 19937 THE CREW REPORTED SMOKE APPEARED MOMENTARILY IN CABIN AT PUSH TIME. MAINTENANCE FOUND THE NO SMOKING FASTEN SEAT BELT S YSTEM INOPERATIVE WITH THE ROW 6 ABC OVERHEAD PSU BASE ASSEMBLY SHORTED OUT. THE WIRES FOR PSU AT ROW 6 ABC WERE CUT AN D STOWED AND THE SYSTEM WAS PLACARDED INOPERATIVE. 2 L 7 2 4F A16WE 1998031700004 19980317 00004 WP 1998 3 17 MWEA98322 1 19980306 A 5320 9910140 WEB DOUG DC9 DC932 3022066 WP BS 889-894 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND CUSP MEMBRANE WAS FOUND DAMAGED FROM FS 889 TO 894. FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998031700005 19980317 00005 NE 1998 3 17 DLL19980534 2 19980307 A 7230 RB211524B4I COMPRESSOR AC101MK13 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 3 ENGINE STALLED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 SO 27 759DA 747 193Y1176 014733 JUST AFTER LEVEL OFF AT FL 370, NR 3 ENGINE HAD A PRESUMED COMPRESSOR STALL AND THE TGT WENT TO 850. ENGINE SHUTDOWN PE RPOM. ESTIMATE TIME AT 850 TGT AT 5 SECONDS. REPLACED VIGV CONTROLLER. BOROSCOPES REVEALED NO DAMAGE. 2 L 7 3 4F 4 F A23WE E12EU 1998031700006 19980317 00006 NM 1998 3 17 DL757980535 1 19980307 A 3350 LIGHT 767GE BOEING 757 757232 1384965 NM RROYCE RB211 RB211524B4 54555 NE CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 643DL 23997 014733 L3 EMER SLIDE LT INOP. REPLACED SAME, CKS GOOD. 2 L 7 2 4F 4 F RT A2NM E12EU 1998031700007 19980317 00007 1998 3 17 HEEA0013181 4 19980304 A 3444 066304400 ALTIMETER BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 RADAR ALTIMETER NEEDLE WON'T REVOLVE IN REVOLVE MODE. 1 G 7 2 3U H3EU 1998031700008 19980317 00008 1998 3 17 HEEA0013195 4 19980304 A 2211 11788292 COMPUTER BOLKMS 117 BK117B1 5626012 EU SPAS SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7059J 7151 SPAS COMPUTER POT IS STRIPPED OUT. 1 G 7 2 3U H13EU 1998031700009 19980317 00009 NE 1998 3 17 HEEA0013203 2 19980304 A 7250 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE POWER SECT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 21498 15882 36003 OIL LEAKING FROM COMPRESSOR AREA AND FORWARD COMBUSTION DRAIN. 1 G 7 2 4U 4 U H4SW E22EA 1998031700011 19980317 00011 1998 3 17 JBXA980033 4 19980211 A 2230 3A2203B PLA TRANSMITTER FOKKER F28 F28MK0100 4990807 EU RT ENGINE OUT OF ADJUST A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SO 05 106ML 11477 RDU - FLT 931 - ON TAKEOFF ROLL, AUTOTHROTTLES ARMED AND ENGAGED. INSUFFICIENT POWER AND NO AUTOTHROTTLE MOVEMENT. TAK EOFF ABORTED AT APPROX 70 KTS. RDU MX ADJUSTED NR 2 PLA TRANSMITTER GROUND RAN A/C. OPS CHECK GOOD. PERFORMED AFCAS T EST OF NR 1 AT AND NR 2 AT. ALL OPS CHECK GOOD IAW F-100 MM 22-11-00. (M) 2 L 7 2 4F RT 1998031700013 19980317 00013 NM 1998 3 17 P5CA9800488 1 19980307 A 5320 STANCHION BOEING 747 747122 1384872 NM BS 640 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BS 460 RBL 20 STANCHION CRACKED AND BROKEN AT CANON HOLES. REMOVED AND REPAIRED STANCHION 51-10-01. 2 L 7 4 4F A20WE 1998031900001 19980319 00001 NE 1998 3 19 CALA9800410 2 19980308 A 7311 FUEL OIL COOLER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE RUPTURED A CALA D E RETURN TO BLOCK ENGINE SHUTDOWN A FLAME/FIRE TX TAXI/GRND HDL 1 SW 09 68065 46590 455800 FUEL SMELL REPORTED IN COCKPIT AND CABIN DURING TAXI OUT. RETURN TO GATE, FIRE DEPART REPORTED FIRE COMING FROM NR 2 EN G. NR 2 ENG WAS SHUT DOWN. EMERG EVAC SLIDES WERE DEPLOYED AND PAX EXITED A/C VIA SLIDES. FIRE DEPART EXTINGUISHED EN G FIRE. L-3 DOOR SLIDE DID NOT FULLY DEPLOY. NR 2 ENG WILL BE REPLACED. PRELIMINARY INVESTIGATION FOUND FUEL MIGRATED INTO OIL SYS WHICH WOULD EXPLAIN REPORTED FIRE IN EXHAUST AREA. FURTHER INVESTIGATION, THE FUEL OIL HEAT EXCHANGER FAI LED INTERNALLY. ALLOWING FUEL, THAT OPERATES AT SIGNIFICANTLY HIGHER PRESS THAN OIL, TO MIGRATE INTO OIL SYS. DISASSEM BLY OF FUEL OIL HEAT EXCHANGER REVEALED CRACKED OIL DIVIDER PLATE WHICH HAD BEEN DISPLACED AND CAUSED FRETTING OF FUEL T 2 L 7 3 4F 4 F A22WE E23EA 1998031900002 19980319 00002 NE 1998 3 19 CALA9800411 2 19980308 A 7200 ENGINE PICO DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 FIRE A CALA D E RETURN TO BLOCK ENGINE SHUTDOWN B A P SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE NO WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 68065 2748 810 46590 A FUEL SMELL WAS REPORTED IN THE COCKPIT AND CABIN DURING TAXI OUT AT MAN. WHILE RETURNING TO THE GATE THE FIRE DEPARTM ENT REPORTED FIRE COMING FROM THE NR 2 ENGINE. THE NR 2 ENGINE WAS SHUT DOWN. EMERGENCY EVACUATION SLIDES WERE DEPLOYE D AND PASSENGERS EXITED THE AIRCRAFT VIA THE SLIDES. THE FIRE DEPARTMENT EXTINGUISHED THE ENGINE FIRE. THE L-3 DOOR SL IDE DID NOT FULLY DEPLOY. THE NR 2 ENGINE WILL BE REPLACED. THE SDR WILL REMAIN OPEN FOR FINDINGS ON L-3 DOOR SLIDE. 2 L 7 3 4F 4 F A22WE E23EA 1998031900003 19980319 00003 NM 1998 3 19 9804126305 1 19980205 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT DOOR 4R. REPAIRED WIRING, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998031900004 19980319 00004 WP 1998 3 19 9804139304 1 19980310 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG CONTAMINATED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 931MC 48057 AIRCRAFT FAILED TO SHIFT FROM GROUND MODE TO FLIGHT MODE AFTER TAKEOFF. FLIGHT WAS RETURNED TO MCI AND LANDED WITHOUT I NCIDENT. MAINTENANCE CONFIRMED CONTAMINATION OF ICE CRYSTALS IN NOSE STRUT FLUID. HEATED AND RESERVICED STRUT TO PROPE R LEVELS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900005 19980319 00005 WP 1998 3 19 9804149854 1 19980308 A 3230 RETRACT MECH DOUG DC9 DC951 3022051 WP LANDING GEAR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 763NC 47716 DURING APPROACH, LANDING GEAR HANDLE WOULD NOT COME DOWN FOR GEAR EXTENSION. EMERGENCY GEAR EXTENSION PROCEDURES WERE U TILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE OPERATED GEAR THROUGH SEVERAL CYCLES. DISCREPANCY COULD NOT BE DUPLICATED. ADJUSTED GEAR DOOR SENSOR. ALSO, REPAIRED MAIN GEAR DOORS DUE TO DAMAGE INCURRED ON LANDING. 2 L 7 2 4F RT A6WE 1998031900006 19980319 00006 WP 1998 3 19 9804159607 1 19980311 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 607NW 47232 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD ATTENDANT UPPER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PA CK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900007 19980319 00007 WP 1998 3 19 9804169851 1 19980310 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 EMERGENCY LIGHTS AT OVERWING EXITS INOPERATIVE. REPLACED BLOWN FUSE AT GALLEY DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998031900008 19980319 00008 WP 1998 3 19 9804179869 1 19980310 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 778NC 48100 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS AT ROWS 10 AND 14 INOPERATIVE. REPAIRED BATTERY CON TACT AT POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998031900009 19980319 00009 WP 1998 3 19 9804189928 1 19980310 A 3350 BA50661001 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 8921E 45836 FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN AND AT GALLEY DOOR ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED POW ER SUPPLY AND LIGHT ASSEMBLY AT FORWARD GALLEY DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900010 19980319 00010 WP 1998 3 19 9804199928 1 19980310 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 01 8921E 45836 FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN AND AT GALLEY DOOR ILLUMINATED IN FLIGHT AND WOULD NOT EXTINGUISH. RE PLACED BATTERIES AT GALLEY DOOR EXIT SIGN, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900011 19980319 00011 WP 1998 3 19 9804209928 1 19980310 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8921E 45836 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT RIGHT GALLEY AND FORWARD CABIN SEAT TRACK INOPERATIVE. RE PLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900012 19980319 00012 WP 1998 3 19 9804219301 1 19980311 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 301RC 48054 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SU PPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900013 19980319 00013 WP 1998 3 19 9804229851 1 19980311 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT GALLEY, FORWARD CABIN AND AT GALLEY SERVICE DOOR EXIT SIGN INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998031900014 19980319 00014 WP 1998 3 19 9804239928 1 19980311 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN PINCHED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8921E 45836 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS AND LIGHTS AT GALLEY DOOR REMAI NING ON WITH SWITCH IN OFF POSITION. FOUND WIRES PINCHED AT SEAT 3C. REPAIRED WIRES AND REPOSITIONED. ALSO, REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900015 19980319 00015 SO 1998 3 19 COMA9810064 1 19980311 A 3320 BC10047005 LIGHT ASSY EMB 120 EMB120RT SO CABIN OVERHEATED A COMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 269CA 120263 SMOKE IN CABIN DURING TAXI OPERATIONS. REPLACED OVERHEATED FLUORESCENT LIGHT ASSY AT SEAT 4B. 2 L 7 2 4T RT A31SO 1998031900016 19980319 00016 EA 1998 3 19 COMA9860054 1 19980311 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA K NONE O OTHER AP APPROACH 1 SO 01 981CA 5654 2164 7163 FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1998031900017 19980319 00017 EA 1998 3 19 COMA9860055 1 19980310 A 3250 16900107 ECU CNDAIR CL600 CL6002B19 EA NLG STEERING MALFUNCTION A COMA K NONE O OTHER AP APPROACH 1 SO 01 978CA 2917 7158 NOSE WHEEL STEERING MESSAGE ON EICAS. REPLACED THE ECU. 2 L 7 2 4F RT A21EA 1998031900018 19980319 00018 NM 1998 3 19 UPS98226084 1 19980311 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN MISSING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, INSTALL GRIMES LIGHT ABOVE FLIGHT STATION DOOR. INSTALLED EMERGENCY LIGHTS AS REQUIRED. 2 L 7 3 4F A3WE 1998031900019 19980319 00019 WP 1998 3 19 UPS98826076 1 19980127 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, MAIN CABIN STA 150 AT RIGHT HAND CUSP, INSIDE R-1 DOOR, FRAME BOTTOM FWD CORNER CORRODED. REMOVE D ANGLE, DRILLED UP REPAIR ANGLE IAW3 DC8 SRM 53-30 AND INSTALLED IAW DC8 SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998031900020 19980319 00020 WP 1998 3 19 UPS98826077 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1010-1030 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, MAIN CARGO SEAT TRACK ALONG LEFT SIDE, STA 1010 TO 1030 CRACKED AND CORRODED. REMOVED TRACK STA 1 010 TO 1090, FABBED AND INSTALLED NEW STICK IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998031900021 19980319 00021 WP 1998 3 19 UPS98826078 1 19980302 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, SEAT TRACK F FUSELAGE STATION 1440 CORRODED. REMOVED SEAT TRACK SECTION FUSELAGE STATION 1430 TO 1450, CUT AND DRILLED NEW SECTION AND INSTALLED SECTION IAW DC8 SRM 51-1-8, 51-3-0, 53-1-2 AND EO DC8 5320 5167. 2 L 7 4 4F RT 4A25 1998031900022 19980319 00022 WP 1998 3 19 UPS98826079 1 19980124 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1610-1620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, AFT ACCESORY SECTION LONGERON CRACKED AND CORRODED STA 1610 TO 1620 AND LONG 24L. REMOVED SECTI ON OF LONGERON AND REPLACED WITH NEW IAW DC8 SRM 53-2-2 AND 51-1-20D, INSTALLED SKIN DOUBLER ON FUSELAGE IAW DC8 SRM 53- 2-1 FIG 7. 2 L 7 4 4F RT 4A25 1998031900023 19980319 00023 WP 1998 3 19 UPS98826080 1 19980127 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 1320-1340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, UPPER CARGO SEAT TRACK REPAIR SPLICE CORRODED, MISSING STRAP OPEN HOLES AND 1 STRAP STA 1320 TO 13 40 LBL 52. FABBED NEW STRAP, ALODINED, PRIMED AND INSTALLED IAW DC8 SRM 53-2-3 AND 51-1-8. 2 L 7 4 4F RT 4A25 1998031900024 19980319 00024 WP 1998 3 19 UPS98826081 1 19980126 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1130-1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, AFT 6 PIT FLOOR TRACK STA 1130 TO 1140 AT BL 45L CORRODED. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED NEW SECTION IN IAW DC8 SRM 53-2-3 AND 51-1-8. 2 L 7 4 4F RT 4A25 1998031900025 19980319 00025 WP 1998 3 19 UPS98826082 1 19980123 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1685 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, STA 1685 BATHTUB FITTING CRACKED AT LONGERON 26L. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51- 1-4, 51-1-20D. INSTALLED IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998031900026 19980319 00026 WP 1998 3 19 UPS98826083 1 19980120 A 5330 SKIN DOUG DC8 DC871F 302199D WP RT WING TORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-D/CK, RIGHT WING TOP EXTERIOR SURFACE REAR SPAR AT NR 5 SPOILER SKIN IS TORN. CUT OUT DAMAGED SKIN AREA , FABRICATED FILLER AND DOUBLER IAW REO DC8 5720 7767 APPENDIX A AND INSTALLED IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998031900027 19980319 00027 WP 1998 3 19 UPS98826085 1 19980302 A 5320 4646163501 SPLICE DOUG DC8 DC871F 302199D WP BS 1350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, SPLICE FITTING AT LONG 24L FS 1350 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IAW SRM 51 -1-20D AND DWG 4646163. 2 L 7 4 4F RT 4A25 1998031900028 19980319 00028 WP 1998 3 19 UPS98826086 1 19980227 A 5320 4646163501 SPLICE DOUG DC8 DC871F 302199D WP BS 1350 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, AFT PIT FS 1350 LONG, 28L SPLICE FITTING CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED R EPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4646163. 2 L 7 4 4F RT 4A25 1998031900029 19980319 00029 1998 3 19 QXEA9800240 4 19980306 A 2565 S130508 SLIDE SWITLIK FOKKER F28 F28MK4000 4990810 EU CABIN LOW PRESS A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 480AU 11229 EMERGENCY ESCAPE SLIDE READS BELOW 2600 PSI AT 70 DEGREES F. FERRIED AIRCRAFT FROM SJC TO GEG. REPLACED ESCAPE SLIDE. 2 L 7 2 4F RT A20EU 1998031900030 19980319 00030 NM 1998 3 19 QXEA9800241 1 19980306 A 6120 YD4N RELAY DHAV 82410314015 DHAV DHC8 DHC8102 2809003 NM RELAY PNL MALFUNCTION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 813PH 32 AUTOFEATHER FAILED TO ARM. INSPECTED AND CLEANED POWER LEVER SWITCHES AND REPLACED 6121-K2 RELAY, OPERATIONAL CHECKS GO OD. 2 H 7 2 4T RT A13NM 1998031900031 19980319 00031 1998 3 19 QXEA9800243 4 19980308 A 2565 S130508 SLIDE SWITLIK FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTION A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 499US 615 11182 ESCAPE SLIDE HAS UNLASHED CORDS AND THE LANYARD IS NOT ATTACHED TO THE AIRCRAFT STRUCTURE. REPLACED SLIDE. 2 L 7 2 4F RT A20EU 1998031900032 19980319 00032 EU 1998 3 19 QXEA9800244 1 19980308 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 482US 11231 EMERGENCY LIGHTS AT ROW 8 ARE INOP. RELAMPED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031900033 19980319 00033 EU 1998 3 19 QXEA9800245 1 19980308 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 482US 11231 EMERGENCY LIGHTS OVER THE COCKPIT DOOR ARE BURNT OUT. REPLACED LAMPS, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031900034 19980319 00034 EU 1998 3 19 QXEA9800246 1 19980308 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 EMERGENCY EXIT SIGN AT CENTER CABIN IS INOP. REPLACED LAMPS, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031900035 19980319 00035 WP 1998 3 19 98FDEA00172 1 19980307 A 5511 SPAR DOUG DC10 DC1010F 3022111 WP LT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 LEFT HORIZ STAB REAR SPAR CAP FWD BARREL NUT HOLE HAS A 1.75 CRACK IND, START .25 FROM TOP SURF AND GOING DOWN PAST BARR EL NUT ON REAR WALL. REMOVED AND REPLACED NR 9 HORIZ H11 BOLT, 8 WASHERS, NUMEROUS HI-LOCK FOR CLEARANCE OF TOOLING AT NR 9 H11 BOLT AREA PER 8-551036 004. 2 L 7 3 4F A22WE 1998031900036 19980319 00036 NM 1998 3 19 98FDEA00174 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 560 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 FWD LWR CARGO FRAME DENTED BS 560, STR 24L TO 25L. REMOVED DAMAGE, INSTALLED BELTFRAME DOUBLER REPAIR PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900037 19980319 00037 NM 1998 3 19 98FDEA00175 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 1130 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 UPPER LOBE BS 1130, BETWEEN STR 13L AND 14L BELL FRAME HAS DAMAGED AREA AND BARE METAL. REMOVED DAMAGED AREA OF BELL FR AME. ACCOMPLISHED BELL FRAME REPAIR PER SRM 53-10-4 PG 7-11. 2 L 7 3 4F RT A3WE 1998031900038 19980319 00038 NM 1998 3 19 98FDEA00176 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 FWD CARGO BS 700, STR 23 TO 24 LT BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME PER SRM 51-40-3. ALODINED AND PRIMED PER M/M 51-20-0. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900039 19980319 00039 NM 1998 3 19 98FDEA00177 1 19980312 A 5330 SKIN BOEING 727 727233 138408A NM BS 700-720 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 FWD CARGO AFTER REMOVAL OF INTERCOSTAL (PER CARD 7-5330-7-2352 P2 SECTION B/2) SKIN INNER SURFACE, WAS FOUND TO BE GOUGE D IN SEVERAL AREAS BS 700 TO 720 O/B OF STR 28L. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1998031900040 19980319 00040 NM 1998 3 19 98FDEA00178 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 FWD CARGO, BS 700, STR 23 TO 24 RT BELL FRAME DENTED. CUT OUT DAMAGED AREA OF BELL FRAME PER SRM 53-10-7 PAGE 1. ALODI NED AND PRIMED PER M/M 51-20-0. INSTALLED BELL FRAME REPAIR PER SRM 51-40-3 FIG 1. 2 L 7 3 4F RT A3WE 1998031900041 19980319 00041 NM 1998 3 19 98FDEA00179 1 19980311 A 5311 FRAME BOEING 727 727233 138408A NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 FWD LWR CARGO FRAME DENTED BS 660, STR 22 TO STR 23. REMOVED DAMAGE FROM FRAME, PREPARED DOUBLER, ALODINED, PRIMED AND INSTALLED DOUBLER PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1998031900042 19980319 00042 WP 1998 3 19 ABXA9800160 1 19980214 A 5712 57694666 RIB DOUG DOUG DC8 DC863F 302198F WP WS 566.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 566.25 CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51 -1-8. 2 L 7 4 4F 4A25 1998031900043 19980319 00043 WP 1998 3 19 ABXA9800161 1 19980214 A 5712 57694666 RIB DOUG DOUG DC8 DC863F 302198F WP WS 578.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 578.75 CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51 -1-8. 2 L 7 4 4F 4A25 1998031900044 19980319 00044 WP 1998 3 19 ABXA9800162 1 19980214 A 5712 576946644 RIB DOUG DOUG DC8 DC863F 302198F WP WS 697.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 697.5 CRACKED AT UPPER AFT END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51 -1-8. 2 L 7 4 4F 4A25 1998031900045 19980319 00045 WP 1998 3 19 ABXA9800164 1 19980214 A 5712 576946646 RIB DOUG DOUG DC8 DC863F 302198F WP WS 703.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 703.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998031900046 19980319 00046 WP 1998 3 19 ABXA9800165 1 19980214 A 5712 576946642 RIB DOUG DOUG DC8 DC863F 302198F WP WS 691.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 691.25 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG 05056-7001 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998031900047 19980319 00047 WP 1998 3 19 ABXA9800166 1 19980208 A 5712 576947048 RIB DOUG DOUG DC8 DC863F 302198F WP WS 853.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION 853.75 CRACKED AT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998031900048 19980319 00048 WP 1998 3 19 ABXA9800167 1 19980214 A 5712 576947040 RIB DOUG DOUG DC8 DC863F 302198F WP WS 828.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 828.75 CRACKED AT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 . 2 L 7 4 4F 4A25 1998031900049 19980319 00049 WP 1998 3 19 ABXA9800168 1 19980214 A 5712 576947042 RIB DOUG DOUG DC8 DC863F 302198F WP WS 835 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB CRACKED AT UPPER END STATION XFS 835.0. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998031900050 19980319 00050 WP 1998 3 19 ABXA9800169 1 19980215 A 5720 56139017 ANGLE DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE INBOARD END, UPPER CORNER OF THE AFT LEADING EDGE ATTACH ANGLE IS CRACKED. REPAIRED ANGLE IAW DW G 5613901 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998031900051 19980319 00051 WP 1998 3 19 ABXA9800171 1 19980219 A 5712 576947020 RIB DOUG DOUG DC8 DC863F 302198F WP WS 766.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 766.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900052 19980319 00052 WP 1998 3 19 ABXA9800172 1 19980219 A 5712 576947136 RIB DOUG DOUG DC8 DC863F 302198F WP WS 822.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 822.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900053 19980319 00053 WP 1998 3 19 ABXA9800173 1 19980219 A 5712 576946635 RIB DOUG DOUG DC8 DC863F 302198F WP WS 272.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END AT XFS 272.5. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998031900054 19980319 00054 WP 1998 3 19 ABXA9800174 1 19980219 A 5712 576947140 RIB DOUG DOUG DC8 DC863F 302198F WP WS 828.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 828.75 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900055 19980319 00055 WP 1998 3 19 ABXA9800175 1 19980219 A 5712 576947110 RIB DOUG DOUG DC8 DC863F 302198F WP WS 735 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 735.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900056 19980319 00056 WP 1998 3 19 ABXA9800176 1 19980219 A 5712 576947112 RIB DOUG DOUG DC8 DC863F 302198F WP WS 741.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900057 19980319 00057 WP 1998 3 19 ABXA9800177 1 19980217 A 5712 5769589 RIB DOUG DOUG DC8 DC863F 302198F WP WS 410.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 410.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998031900058 19980319 00058 WP 1998 3 19 ABXA9800178 1 19980216 A 5712 576946644 RIB DOUG DOUG DC8 DC863F 302198F WP WS 454.976 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 454.976 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-31-1. 2 L 7 4 4F 4A25 1998031900059 19980319 00059 WP 1998 3 19 ABXA9800179 1 19980216 A 5313 57501981 LONGERON DOUG DOUG DC8 DC863F 302198F WP BS 946 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LONGERON 24L STATION 946 HAS A CRACK EXTENDING UNDER VERTICAL FITTING. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1998031900060 19980319 00060 WP 1998 3 19 ABXA9800180 1 19980215 A 5720 56139018 ANGLE DOUG DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING INBOARD LEADING EDGE AT THE WING ROOT UPPER AFT CORNER, THE ATTACH ANGLE IS CRACKED. REPAIRED ANGLE IAW DWG 5613901 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998031900061 19980319 00061 WP 1998 3 19 ABXA9800181 1 19980222 A 5720 5769859125 SUPPORT DOUG DOUG DC8 DC863F 302198F WP NR 2 STUB WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 NR 2 STUB WING INBOARD SUPPORT LEG CRACKED. REPAIRED IAW DWG 5769859 AND SRM 51-1-29. 2 L 7 4 4F 4A25 1998031900062 19980319 00062 WP 1998 3 19 ABXA9800182 1 19980220 A 5712 5770038 RIB DOUG DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB UPPER ARM CRACKED 7TH RIB INBOARD FROM OUTBOARD EDGE OF OUTBOARD SLOT. REPAIRED IAW SRM 57- 20 AND DWG K05056. 2 L 7 4 4F 4A25 1998031900063 19980319 00063 WP 1998 3 19 ABXA9800183 1 19980219 A 5313 57501981 LONGERON DOUG DOUG DC8 DC863F 302198F WP BS 860 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LONGERON 24L AT STATION 860 HAS CRACK. REPAIRED IAW SRM 53-2-2. 2 L 7 4 4F 4A25 1998031900064 19980319 00064 WP 1998 3 19 ABXA9800184 1 19980219 A 5313 57501981 LONGERON DOUG DOUG DC8 DC863F 302198F WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LONGERON 24 HAS A CRACK EXTENDING UNDER VERTICAL FITTING ON TORQUE BOX, RIGHT WHEEL WELL AT STATION 960. REPAIRED IAW S RM 53-2-2, 51-1-20D AND 51-1-21. 2 L 7 4 4F 4A25 1998031900065 19980319 00065 WP 1998 3 19 ABXA9800185 1 19980219 A 5712 576946916 RIB DOUG DOUG DC8 DC863F 302198F WP WS 610 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 610.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0, 51-1-8 AND 5 1-1-21. 2 L 7 4 4F 4A25 1998031900066 19980319 00066 WP 1998 3 19 ABXA9800186 1 19980219 A 5712 576947140 RIB DOUG DOUG DC8 DC863F 302198F WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 772.50 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 1998031900067 19980319 00067 WP 1998 3 19 ABXA9800187 1 19980219 A 5712 576947121 RIB DOUG DOUG DC8 DC863F 302198F WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE RIB AT STATION XFS 7725 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056-7001 AND SRM 51 -1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900068 19980319 00068 WP 1998 3 19 ABXA9800188 1 19980219 A 5712 576947037 RIB DOUG DOUG DC8 DC863F 302198F WP WS 862.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE RIB AT STATION XFS 826.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 5 1-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900069 19980319 00069 WP 1998 3 19 ABXA9800189 1 19980219 A 5712 576947035 RIB DOUG DOUG DC8 DC863F 302198F WP WS 820.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE RIB AT STATION XFS 820.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900070 19980319 00070 WP 1998 3 19 ABXA9800190 1 19980219 A 5712 57694716 RIB DOUG DOUG DC8 DC863F 302198F WP WS 722.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 722.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998031900071 19980319 00071 WP 1998 3 19 MWEA98336 1 19980111 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1066 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CRACK IN FUSELAGE SKIN UNDER RT UPPER PYLON TO FUSELAGE ATTACH ANGLE AT STA 1066 BELOW LONG 15R. MTC REPAIRED WIT H DOUBLER. 2 L 7 2 4F A6WE 1998031900072 19980319 00072 WP 1998 3 19 MWEA98337 1 19980311 A 2560 LANYARD DOUG DC9 DC915 3022036 WP GALLEY DOOR FRAYED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 GALLEY SERVICE DOOR EVACUATION SLIDE GIRT BAR LANYARD FRAYED. FABRICATED AND INSTALLED GIRT BAR LANYARD. 2 L 7 2 4F A6WE 1998031900073 19980319 00073 NE 1998 3 19 MWEA98338 2 19980309 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RIGHT FAILED A MWEA O OTHER E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 GL 31 204ME 47680 CREW REPORTS RT ENGINE MAKING EXCESSIVE NOISE AND VIBRATION THROUGHOUT CABIN. FOUND METAL SHAVINGS IN FILTER. REMOVED AND REPLACED ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1998031900074 19980319 00074 WP 1998 3 19 MWEA98339 1 19980311 A 5347 5910152 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 579-965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT HAND INBOARD SEAT TRACK WAS FOUND CORRODED FROM FS 579 TO 965. REMOVED AND REPLACED SEAT TRACK. 2 L 7 2 4F A6WE 1998031900075 19980319 00075 WP 1998 3 19 MWEA98340 1 19980311 A 5320 9910501 WEB DOUG DC9 DC932 3022066 WP BS 227-351 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE LT CUSP WEB WAS FOUND CORRODED FROM FS 227 TO 351. REMOVED AND REPLACED WEB SECTION. 2 L 7 2 4F A6WE 1998031900076 19980319 00076 WP 1998 3 19 MWEA98341 1 19980311 A 5347 5910820 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-584 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT HAND INBOARD SEAT TRACK WAS FOUND TO HAVE CORROSION FROM FS 200 TO 584. REMOVED AND REPLACED SEAT TRACK SECTION. 2 L 7 2 4F A6WE 1998031900077 19980319 00077 WP 1998 3 19 MWEA98342 1 19980311 A 5347 5910814 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 570-965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND OUTBOARD SEAT TRACK WAS FOUND CORRODED OUT OF SERVICEABLE LIMITS FROM FS 570 TO 965. REMOVED AND REPLACED SEC TION OF TRACK. 2 L 7 2 4F A6WE 1998031900078 19980319 00078 WP 1998 3 19 MWEA98343 1 19980311 A 5720 9919346 WEB DOUG DC9 DC932 3022066 WP WS 20 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER FUEL TANK WEB AT XCW 20 LEFT SIDE WAS FOUND WITH PIECE MISSING. FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998031900080 19980319 00080 WP 1998 3 19 MWEA98345 1 19980311 A 5330 5911412191 SKIN DOUG DC9 DC932 3022066 WP BS 229-589 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 NUMEROUS AREAS OF CORROSION WERE FOUND ON THE EXTERNAL FUSELAGE SKIN LONG 26L TO 26R FS 229 TO 589. REMOVED AND REPLACE D SKIN. 2 L 7 2 4F A6WE 1998031900081 19980319 00081 SO 1998 3 19 SWIA971093 1 19980204 A 3231 DOORS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT/RT MLG ICED UP A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 186SW 120034 RIGHT MAIN LANDING FAILED TO EXTEND UPON DOWN SELECTIONS. RIGHT MAIN WOULD ALSO NOT EXTEND DURING EMERGENCY EXTENSION P ROCEDURE. INDICATIONS IN BOTH CASES, 2 RED TRANSIT LIGHTS ONLY ON RIGHT MAIN. RIGHT EVENTUALLY EXTENDED DURING A NORMA L SELECTION CYCLE. FOUND ICE ON RIGHT AND LEFT LANDING GEAR AND DOORS. REMOVED ALL ICE AND EXTENDED LANDING GEAR FOUR TIMES AND TWO EMERGENCY. ALL GEAR OPS CHECKS GOOD, IAW MM 32-30-30. 2 L 7 2 4T 4 T RT A31SO E20NE 1998031900082 19980319 00082 SO 1998 3 19 SWIA971094 1 19980309 A 3231 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG DOOR FAILED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 204SW 120243 WHEN LEFT GEAR CYCLED UP A AND B INTRANSIT LIGHTS REMAIN ON. FOUND LEFT OUTBOARD GEAR DOOR SEQUENCE VALVE BLEEDING PRES SURE BY. REPLACED SEQUENCE VALVE AND CYCLED GEAR SEVERAL TIMES. ALL CHECKS GOOD ON GROUND WITH NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998031900083 19980319 00083 1998 3 19 SWIA971095 4 19980309 A 2210 YAW DAMPER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 2 FAILED A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 408SW 7055 YAW DAMPER 2 FAILS INFLIGHT, BUT WOULD RESET AFTER SEVERAL SECONDS. RETURNED TO SLC. REPLACED NR 2 FCC 4000 IAW MM 22. OPS CHECKS GOOD FOR CATII. 2 L 7 2 4F 4 F RT A21EA E15NE 1998031900084 19980319 00084 SO 1998 3 19 SWIA971096 1 19980309 A 3297 WIRE HARNESS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NM 07 188SW 120039 LANDING GEAR FAILED TO EXTEND AFTER SEVERAL ATTEMPTS WITH LANDING GEAR CONTROL LEVER. HYDRAULIC PRESSURE NORMAL. USED ELECTRIC OVERRIDE TO EXTEND GEAR. RETURNED TO LAX. REPLACED RIGHT GEAR PROXIMITY SENSOR HARNESS AND CYCLED GEAR SEVERA L TIMES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998031900085 19980319 00085 EA 1998 3 19 SWIA971097 1 19980309 A 3610 CLAMP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT BLEED DUCT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 406SW 7030 RIGHT 14TH STAGE BLEED AIR DUCT LEAK MSG OUT OF 18000 FT ON CLIMBOUT. SYNOPTIC PAGE SHOWED RED INSIDE OF VALVE. FOLLOW ED QRH CLOSING 14TH STAGE VALVE, MSG WENT OUT. RETURNED TO SLC. SECURED AND SEALED RIGHT 14TH STAGE SHUT OFF VALVE THE RMAL BLANKET. SECURED V-BAND CLAMP ON 14TH STAGE SHUTOFF VALVE IAW MM 36. OPERATED 14TH STAGE AIR WITH ENGINES AT TAKE OFF POWER AND OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1998031900086 19980319 00086 NM 1998 3 19 VNAA9803010 1 19980310 A 3030 0851GW PITOT HEAT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 457PS 49984 3048 DURING THE TAXI OUT FOR TAKEOFF, A STANDBY PITOT HEAT FAIL WARNING MESSAGE WAS DISPLAYED. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT, FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT WAS COND UCTED WITHOUT INCIDENT. PIT MAINTENANCE INSPECTED AND REPLACED THE STANDBY PITOT HEAD IN ACCORDANCE WITH DORNIER MAINTE NANCE MANUAL 34-11-04. OPERATION CHECKS WERE COMPLIED WITH. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031900087 19980319 00087 SW 1998 3 19 HEEA0013262 1 19980304 A 7810 212061201011 EJECTOR ASSY BELL 412 412 1182202 SW EXH BRACKET BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141PH 33197 LT EJECTOR ASSY AFT BRACKETS BROKEN. 1 G 7 2 4U H4SW 1998031900088 19980319 00088 1998 3 19 HEEA0013264 4 19980304 A 3421 222375033107 INDICATOR BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 ATTITUDE INDICATOR ROLL ERECTION RATE SLOW. TIME SINCE REPAIR 0:00. 2 G 7 2 4U H10SW 1998031900089 19980319 00089 NE 1998 3 19 HEEA0013265 1 19980304 A 2422 PC173 INVERTER SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 INVERTER DROPS OFF LINE AFTER ONE HOUR. TIME SINCE REPAIR 11:10. 1 G 7 2 3U H1NE 1998031900090 19980319 00090 NE 1998 3 19 HEEA0013266 1 19980304 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 M/R DAMPER IS WEAK. 1 G 7 2 3U H1NE 1998031900091 19980319 00091 NE 1998 3 19 HEEA0013267 1 19980304 A 6730 7630103902102 ACTUATOR SKRSKY S76 S76A 8143006 NE SERVO SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 ACTUATOR WILL ONLY RUN IN ONE DIRECTION. 1 G 7 2 3U H1NE 1998031900092 19980319 00092 SW 1998 3 19 HEEA0013268 1 19980304 A 2841 4814815 INDICATOR BELL 412 412 1182202 SW FUEL QTY ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 INDICATOR LEFT FUEL QTY. NEEDLE ERRATIC. 1 G 7 2 4U H4SW 1998031900093 19980319 00093 1998 3 19 HEEA0013269 4 19980304 A 3424 71252 GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 GYRO DEFECTIVE . WON'T PULL NEEDLE ON SLIP AND TURN INDICATOR. 1 G 7 2 4U H4SW 1998031900094 19980319 00094 1998 3 19 HEEA0013270 4 19980304 A 2211 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 COMPUTER WILL NOT RELEASE LATERAL AXIS BRAKE MOTOR. 1 G 7 2 4U H4SW 1998031900095 19980319 00095 1998 3 19 HEEA0013271 4 19980304 A 2211 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141PH 33197 NR2 HP WILL NOT ENGAGE. 1 G 7 2 4U H4SW 1998031900096 19980319 00096 1998 3 19 HEEA0013273 4 19980304 A 3414 214175299107 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 AIR SPEED INDICATOR READING HIGH. 2 G 7 2 4U H10SW 1998031900097 19980319 00097 1998 3 19 HEEA0013274 4 19980304 A 3420 412074030101 ISOLATION AMP BELL 412 412 1182202 SW COCKPIT INST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 ISOLATION AMPLIFIER SMOKING. 1 G 7 2 4U H4SW 1998031900098 19980319 00098 SW 1998 3 19 HEEA0013275 1 19980304 A 2841 393008047 INDICATOR BELL 412 412 1182202 SW FUEL QTY INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 DROPPING TO ZERO INTERMITTENTLY. 1 G 7 2 4U H4SW 1998031900099 19980319 00099 SW 1998 3 19 HEEA0013276 1 19980304 A 2822 9A1746 CARTRIDGE BELL 214 214ST 1182106 SW FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 360 28102 INOPERATIVE/ POPS CIRCUIT BREAKER. 2 G 7 2 4U H10SW 1998031900100 19980319 00100 1998 3 19 HEEA0013277 4 19980304 A 3414 2002011293 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 AIR SPEED INDICATOR NEEDLE STICKS BELOW 20 KTS. 1 G 7 2 3U H1NE 1998031900101 19980319 00101 1998 3 19 HEEA0013278 4 19980304 A 3416 212070238003 INDICATOR BELL 412 412 1182202 SW COCKPIT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 NEEDLE INTERMITTENT WHEN CARD IS TURNED. 1 G 7 2 4U H4SW 1998031900102 19980319 00102 EU 1998 3 19 HEEA0013279 1 19980304 A 6320 4638201003 CENTER CASE BOLKMS 105 BO105S 5626006 EU M/R XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K S859 CENTER CASE WORN. TAIL ROTOR BORE 91.90MM. 1 G 7 2 3U H3EU 1998031900103 19980319 00103 1998 3 19 HEEA0013280 4 19980304 A 3414 8502CS20LW INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 AIR SPEED INDICATOR 10 KNOTS HIGH. 1 G 7 2 3U H1NE 1998031900104 19980319 00104 NE 1998 3 19 HEEA0013281 1 19980304 A 2422 7655003007105 INVERTER SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 INVERTER CYCLES ON AND OFF. 1 G 7 2 3U H1NE 1998031900105 19980319 00105 EU 1998 3 19 HEEA0013282 1 19980304 A 7714 DL41239 INDICATOR BOLKMS 105 BO105S 5626006 EU ENG RPM HANGS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 SINGLE RPM NEEDLE HANGS 10% WHEN MOTORING ENGINE. 1 G 7 2 3U H3EU 1998031900106 19980319 00106 SW 1998 3 19 HEEA0013283 1 19980304 A 2437 209070263003 INDICATOR BELL 412 412 1182202 SW DC VOLTS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 DUAL VOLTAGE INDICATOR READS HIGH ON LOW END. 1 G 7 2 4U H4SW 1998031900107 19980319 00107 SW 1998 3 19 HEEA0013284 1 19980304 A 2425 209070263003 INDICATOR BELL 412 412 1182202 SW DUAL VOLTS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 AC NEEDLE STICKS AND DC READS HIGH. 1 G 7 2 4U H4SW 1998031900108 19980319 00108 SW 1998 3 19 HEEA0013285 1 19980304 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW ENG TORQ STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 NR1 TORQUE NEEDLE STICKS INTERMITTENTLY. 1 G 7 2 4U H4SW 1998031900109 19980319 00109 SW 1998 3 19 HEEA0013286 1 19980304 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW TORQUE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 CURSER READS HIGHER THAN NR1 AND NR2 NEEDLE. 1 G 7 2 4U H4SW 1998031900110 19980319 00110 1998 3 19 HEEA0013288 4 19980304 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 33020 HSI INOPERATIVE. STAYS AT 270 DEGREES AND NR2 PITCH HARD OVER. TIME SINCE REPAIR 50:30. 1 G 7 2 4U H4SW 1998031900111 19980319 00111 1998 3 19 HEEA0013289 4 19980304 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 FAILED TEST 1.1 ON SST. NO DG VALID. 1 G 7 2 4U H4SW 1998031900112 19980319 00112 1998 3 19 HEEA0013290 4 19980304 A 2210 2593996444 TARSYN BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 FAILED TEST 1.1 ON SST. NO DG VALID. TIME SINCE REPAIR 28:35. 1 G 7 2 4U H4SW 1998031900113 19980319 00113 SW 1998 3 19 HEEA0013291 1 19980304 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW M/R INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 ROTARY ACTUATOR INTERMITTENT OPERATION. 1 G 7 2 4U H4SW 1998031900114 19980319 00114 SW 1998 3 19 HEEA0013292 1 19980304 A 5260 SYLC502283 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998031900115 19980319 00115 SW 1998 3 19 HEEA0013293 1 19980304 A 6710 206062721113 ACTUATOR BELL 206 206B3 1181506 SW M/R STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39122 3312 ACTUATOR STUCK ON HIGH SIDE. 1 G 7 1 3U H2SW 1998031900116 19980319 00116 SW 1998 3 19 HEEA0013294 1 19980304 A 3340 7028521 LIGHT BELL 412 412 1182202 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 STROBE LIGHT NO OFF AND ON OPERATION. 1 G 7 2 4U H4SW 1998031900117 19980319 00117 SW 1998 3 19 HEEA0013295 1 19980304 A 3340 7028521 LIGHT BELL 412 412 1182202 SW STROBE INOPERATIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 STROBE LIGHT INOPERATIVE. 1 G 7 2 4U H4SW 1998031900118 19980319 00118 SW 1998 3 19 HEEA0013296 1 19980305 A 7722 212075067105 INDICATOR BELL 412 412 1182202 SW COCKPIT ITT FLUCTUATES E HEEA K NONE O OTHER CR CRUISE 1 SW 03 33008 36004 ITT INDICATOR FLUCTUATES IN CRUISE FLIGHT. 1 G 7 2 4U H4SW 1998031900119 19980319 00119 EU 1998 3 19 HEEA0013297 1 19980305 A 7714 DL43638 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X S808 TRIPLE TACH ALL NEEDLES HAVE STICKY OPERATION. 1 G 7 2 3U H3EU 1998031900120 19980319 00120 1998 3 19 HEEA0013298 4 19980305 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 TURN RATE GYRO INDICATES 6 DEGREES LEFT. 1 G 7 2 4U H4SW 1998031900121 19980319 00121 SW 1998 3 19 HEEA0013299 1 19980305 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 NR1 NEEDLE LAGS AND NR2 NEEDLE OFF MORE THAN 2%. 1 G 7 2 4U H4SW 1998031900122 19980319 00122 SW 1998 3 19 HEEA0013300 1 19980305 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 TRIPLE TACH READS 1% LOW. 1 G 7 2 4U H4SW 1998031900123 19980319 00123 1998 3 19 HEEA0013301 4 19980305 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 TURN NEEDLE IS ERRATIC AND DOESN'T INDICATE PROPER RATE OF TURN. 1 G 7 2 4U H4SW 1998031900124 19980319 00124 1998 3 19 HEEA0013302 4 19980305 A 3421 5040017901 INDICATOR BOLKMS 105 BO105S 5626006 EU COCKPIT PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 ATTITUDE INDICATOR PRECESSES AND SLOW ERECTION RATES. 1 G 7 2 3U H3EU 1998031900125 19980319 00125 1998 3 19 HEEA0013303 4 19980305 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 NARCO ELT TRANSMITS SIGNAL INADVERTANTLY. 1 G 7 2 3U H3EU 1998031900126 19980319 00126 1998 3 19 HEEA0013304 4 19980305 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4302G S853 NARCO ELT INTERMITTENT IN ARM POSITION. 1 G 7 2 3U H3EU 1998031900127 19980319 00127 1998 3 19 HEEA0013305 4 19980305 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4302G S853 NARCO ELT TRANSMITTER COMES ON DURING FLIGHT. 1 G 7 2 3U H3EU 1998031900128 19980319 00128 SW 1998 3 19 HEEA0013306 1 19980305 A 2730 214001970107 ACTUATOR ASSY BELL 214 214ST 1182106 SW ELEV DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 ELEVATOR FALLS OFF LINE. 2 G 7 2 4U H10SW 1998031900129 19980319 00129 SW 1998 3 19 HEEA0013307 1 19980305 A 7714 214175249101 INDICATOR BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 RPM NEEDLE STUCK AT ZERO. 2 G 7 2 4U H10SW 1998031900130 19980319 00130 SW 1998 3 19 HEEA0013308 1 19980305 A 6340 214074280107 LIMIT DETECTOR BELL 412 412 1182202 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 CYCLIC CENTERING DOES NOT FUNCTION. RPM LIMIT DETECTOR FAULT. 1 G 7 2 4U H4SW 1998031900131 19980319 00131 SW 1998 3 19 HEEA0013309 1 19980305 A 7714 214175251107 INDICATOR BELL 214 214ST 1182106 SW TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 NR2 NEEDLE 2% ABOVE OTHER NEEDLES. 2 G 7 2 4U H10SW 1998031900132 19980319 00132 1998 3 19 HEEA0013310 4 19980305 A 3421 5040006914 INDICATOR BELL 206 206B3 1181506 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2753F 2729 ATTITUDE INDICATOR SLOW TO REACT TO MOVEMENT. 1 G 7 1 3U H2SW 1998031900133 19980319 00133 1998 3 19 HEEA0013311 4 19980305 A 2210 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE AFCS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 INTERMITTENT RADAR. AFCS VERT GYRO FAULT 1 G 7 2 3U H1NE 1998031900134 19980319 00134 EU 1998 3 19 HEEA0013312 1 19980305 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 724MB S756 VALVE WILL NOT OPEN. INOPERATIVE. 1 G 7 2 3U H3EU 1998031900135 19980319 00135 NE 1998 3 19 HEEA0013313 1 19980305 A 2842 AT2062 INDICATOR SKRSKY S76 S76A 8143006 NE FUEL TOTALIZER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 UPPER R/H DIGIT BUTTON WILL NOT SET. 1 G 7 2 3U H1NE 1998031900136 19980319 00136 1998 3 19 HEEA0013314 4 19980305 A 3416 A30 ENCODER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8587X 51464 NO VALID OUTPUT FROM ENCODER. 1 G 7 1 3U H2SW 1998031900137 19980319 00137 SW 1998 3 19 HEEA0013315 1 19980305 A 6330 214031614128 PLATE ASSY BELL 214 214ST 1182106 SW M/R XMSN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 A/C EXPERIENCING EXCESSIVE BOUNCE IN LET DOWN. 2 G 7 2 4U H10SW 1998031900138 19980319 00138 SW 1998 3 19 HEEA0013316 1 19980305 A 6330 214031614128 PLATE ASSY BELL 214 214ST 1182106 SW XMSN TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 PLATE ASSY TORN. 2 G 7 2 4U H10SW 1998031900139 19980319 00139 EU 1998 3 19 HEEA0013317 1 19980305 A 2841 1179405401 INDICATOR BOLKMS 117 BK117A3 5626015 EU FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 NR1 SUPPLY INOPERATIVE. 1 G 7 2 3U H13EU 1998031900140 19980319 00140 NE 1998 3 19 HEEA0013318 1 19980305 A 2810 20C00212 FILLER VALVE SKRSKY S76 S76A 8143006 NE FUEL SYS LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 31219 760230 FILLER VALVE LEAKS OUT OF VALVE. 1 G 7 2 3U H1NE 1998031900141 19980319 00141 1998 3 19 HEEA0013319 4 19980305 A 2210 214074305105 AMPLIFIER ASSY BELL 214 214ST 1182106 SW AUTOPILOT FBWE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 DROPS OFF LINE. TIME SINCE REPAIR 0:00. 2 G 7 2 4U H10SW 1998031900142 19980319 00142 1998 3 19 HEEA0013320 4 19980305 A 3417 214175421101 AIR DATA COMPT BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 VNC LIGHT COMES ON ON CO-PILOTS SIDE. 2 G 7 2 4U H10SW 1998031900143 19980319 00143 SW 1998 3 19 HEEA0013321 1 19980305 A 3020 214175396101 CONTROL UNIT BELL 214 214ST 1182106 SW ENG INLET FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 ENGINE INLET WILL NOT HEAT. 2 G 7 2 4U H10SW 1998031900144 19980319 00144 SW 1998 3 19 HEEA0013322 1 19980305 A 2434 214175150105 GENERATOR BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 GENERATOR FAILED. 2 G 7 2 4U H10SW 1998031900145 19980319 00145 SW 1998 3 19 HEEA0013323 1 19980305 A 3340 7028501 LIGHT BELL 214 214ST 1182106 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 STROBE LIGHT POPS CIRCUIT BREAKER. 2 G 7 2 4U H10SW 1998031900146 19980319 00146 1998 3 19 HEEA0013324 4 19980305 A 3421 222375033107 INDICATOR BELL 214 214ST 1182106 SW COCKPIT PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 PRECESSES ABOUT 8 DEGREES ON FLIGHT LINE DURING GROUND CHECK. TIME SINCE REPAIR 0:00. 2 G 7 2 4U H10SW 1998031900147 19980319 00147 1998 3 19 HEEA0013325 4 19980305 A 2562 ACRRLB21 EPIRB BELL 212 212 1181420 SW EMERG LOCATOR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 EPIRB CASE IS SWOLLEN. CORROSION IN ANTENNA MOUNT. 1 G 7 1 4U H4SW 1998031900148 19980319 00148 SW 1998 3 19 HEEA0013326 1 19980305 A 2932 205076044009 SWITCH BELL 214 214ST 1182106 SW HYD PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 HYD PRESSURE SWITCH INOPERATIVE. 2 G 7 2 4U H10SW 1998031900149 19980319 00149 SW 1998 3 19 HEEA0013327 1 19980305 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141PH 33197 STEP ACTUATOR POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1998031900150 19980319 00150 SW 1998 3 19 HEEA0013328 1 19980305 A 3213 412030437103 CAP ASSY BELL 412 412 1182202 SW SKID AFT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CAP ASSY AFT RUBBER IS WORN. 1 G 7 2 4U H4SW 1998031900151 19980319 00151 SW 1998 3 19 HEEA0013329 1 19980305 A 3213 412030437103 CAP ASSY BELL 412 412 1182202 SW SKID AFT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 CAP ASSY AFT RUBBER WORN. 1 G 7 2 4U H4SW 1998031900152 19980319 00152 GL 1998 3 19 HEEA0013330 2 19980305 A 7230 23038162 SHROUD HOUSING BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENGINE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 1076Y CAC90437 45380 CAE895111 RECEIVED SHROUD HOUSING AND UNABLE TO OBTAIN THROAT CLEARANCE BETWEEN SHROUD AND IMPELLER. NOTE: TRIED ON SEVERAL IMPE LLERS. INSTALLED A DALLAS AIRMOTIVE OVERHAULED SHROUD ASSY. 1 G 7 1 3U 3 U H2SW E1GL 1998031900276 19980319 00276 EU 1998 3 19 GXPA98001 1 19980201 A 5230 DOOR AMD FALC20 FALCON 2720302 EU CARGO OPENED A A GXPA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 617GA 88 CARGO DOOR OPENED AFTER TAKEOFF. CARGO NET WAS ATTACHED TO DOOR PREVENTING IT FROM OPENING BEYOND APPROXIMATELY 12 INCH ES. SOME MATERIAL FROM CABIN FODED THE LEFT ENGINE, BUT IT REMAINED RUNNING. AIRCRAFT RETURNED TO SDF. UPON INVESTIGA TION, FOUND DOOR TO BE OPERATING NORMALLY WITH NO DAMAGE. DETERMINED DOOR WAS NOT LOCKED PRIOR TO DEPARTURE. (X) 2 L 7 2 4F A7EU 1998031900281 19980319 00281 NM 1998 3 19 VJ9800040 1 19980310 A 3350 6013211 POWER SUPPLY BOEING 737 7372L9 1384497 NM CARGO COMPT INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 11 737Q 21279 EXTERIOR EMERGENCY LIGHT AT L2 DOOR INOP. REPLACED POWER SUPPLY; OPS CHECKED GOOD IAW MM 33-51-11. 2 L 7 2 4F RT A16WE 1998031900282 19980319 00282 NM 1998 3 19 VJ9800041 1 19980312 A 3350 6104789 BATTERY BOEING 737 737297 1384480 NM CARGO COMPT DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 11 462AT 22631 BOTH EMERGENCY EXIT LIGHTS AT AFT ENTRY SERVICE DOOR INOP. REPLACED BATTERY PACK. 2 L 7 2 4F A16WE 1998031900283 19980319 00283 WP 1998 3 19 VJ9800042 1 19980311 A 3231 5910086501 DOOR LINKAGE DOUG DC9 DC932 3022066 WP NLG OUT OF ADJUST A VJ6A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 11 914VV 47486 AFTER GEAR RETRACTION, EXPERIENCED VIBRATION AND CREW ELECTED AS A PRECAUTIONARY MEASURE TO RETURN TO MAINTENANCE BASE. UPON LANDING DETERMINED THAT LEFT NOSE LANDING GEAR DOOR WAS NOT FULLY CLOSED. ADJUSTED LT NOSE GEAR DOOR LINK ROD ASS EMBLY; OPS CHECKED GOOD IAW MM32-22-01. RETRACTION TEST PERFORMED SATISFACTORILY. 2 L 7 2 4F A6WE 1998031900284 19980319 00284 NM 1998 3 19 K3HA980030 1 19980311 A 3350 90052 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 LEFT CENTER OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK OK REF MM 33-50-01. 2 L 7 3 4F A3WE 1998031900285 19980319 00285 NM 1998 3 19 K3HA980031 1 19980311 A 3350 90052 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 RIGHT CENTER OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK OK REF MM 33-50-01. 2 L 7 3 4F A3WE 1998031900286 19980319 00286 NM 1998 3 19 K3HA980032 1 19980311 A 3350 90052 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 LEFT FORWARD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY, OPS CHECK OK, REF MM 33-50-01. 2 L 7 3 4F A3WE 1998031900287 19980319 00287 NM 1998 3 19 K3HA980033 1 19980311 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 LEFT OVERWING CENTER EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK, REF MM 33-50-2. 2 L 7 3 4F A3WE 1998031900288 19980319 00288 NM 1998 3 19 K3HA980034 1 19980311 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 LEFT OVERWING FORWARD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK, REF MM 33-50-2. 2 L 7 3 4F A3WE 1998031900289 19980319 00289 NM 1998 3 19 K3HA980035 1 19980311 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 RIGHT OVERWING CENTER EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK, REF MM 33-50-2. 2 L 7 3 4F A3WE 1998031900290 19980319 00290 NM 1998 3 19 K3HA980036 1 19980311 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 RIGHT OVERWING FORWARD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK, REF MM 33-50-2. 2 L 7 3 4F A3WE 1998031900291 19980319 00291 SO 1998 3 19 LR7A9801 1 19980107 A 7922 8A1006X THERMOSTAT LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 3 ENGINE FAILED A LR7A E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 AL 03 401LC 732 4606 550035 PRECAUTIONARY SHUTDOWN NR 3 ENGINE AT 0400Z DUE TO HIGH OIL TEMP. FERRIED AIRCRAFT TO ANC, REPLACED NR 3 ENGINE OIL COO LER THERMOSTAT PER LOCKHEED MM CHAPTER 79-20, PAGE 203. GROUND RUNS ACCOMPLISHED, SYSTEM OPERATIONALLY TESTS OK. 2 H 7 4 4T 4 T A1SO E282 1998031900292 19980319 00292 GL 1998 3 19 LR7A9802 2 19980116 A 7200 ENGINE LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 2 FAILED A LR7A E ENGINE SHUTDOWN R C PARTIAL RPM/PWR LOSS F.O.D. DE DESCENT 1 AL 03 289F 1110 NR 2 ENGINE LOSS OF HP WITH UNCONTROLLABLE RISE IN TIT. ENGINE SHUTDOWN AT 1305Z.PROBABLE CAUSE: FOD 2 L 7 4 4T 4 T 4A22 E282 1998031900293 19980319 00293 NE 1998 3 19 LR7A9803 3 19980304 A 6114 SEAL LKHEED 382 382G 526414U SO HAMSTD 54H 54H60117 NE NR 2 PROP LEAKING A LR7A E ENGINE SHUTDOWN K FLUID LOSS CL CLIMB 1 AL 03 403LC 497 4590 N214603 NR 2 PROP LOW OIL LIGHT FEATHERED IN FLIGHT. REMOVED PROPELLER, HUB RESEALED BY PACIFIC PROPELLER, REINSTALLED AND TEST ED PER HN6101. 2 H 7 4 4T A1SO 6 C P906 1998031900294 19980319 00294 GL 1998 3 19 LR7A9804 2 19980307 A 7230 COMPRESSOR LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 3 ENGINE WORN A LR7A E ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 AL 03 285F 15261 1107 500520 NR 3 ENGINE AUTO FEATHERED ON T/O. PULLED EMERGENCY SHUTDOWN HANDLE AT 0038Z. REPLACED NR 3 SPEED SENSE VALVE IAW MM75 -10-1, NO HELP. INSPECTED COMPRESSOR THROUGH 5TH AND 10TH STAGE BLEED VALVES AND FOUND COMPRESSOR WORN. 2 L 7 4 4T 4 T 4A22 E282 1998031900295 19980319 00295 NE 1998 3 19 LR7A9805 3 19980310 A 6111 BLADE LKHEED 382 382G 526414U SO HAMSTD 54H 54H60117 NE NR 2 PROP LEAKING A LR7A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 403LC 500 4590 N214603 NR 2 PROP LOW OIL LIGHT FOLLOWED BY FLUX. SHUTDOWN IAW AFM. INSPECTED AND FOUND NR 2 BLADE LEAKING. PROP REMOVED FOR DETAILED INSPECTION BY VENDOR. 2 H 7 4 4T A1SO 6 C P906 1998031900296 19980319 00296 EU 1998 3 19 AWXA9800073 1 19980305 A 3231 201122008 UPLOCK ASSY AIRBUS 320 A320231 3930325 EU RT MLG DOOR FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 643AW 315 LANDING GEAR NOT CLOSED ECAM INDICATION, RIGHT MAIN GEAR. AIRCRAFT RETURNED TO CMH, EMERGENCY DECLARED. REMOVED AND RE PLACED RIGHT MAIN LANDING GEAR DOOR UPLOCK ASSY IAW AMM 32-31-33. 2 L 7 2 4F RT A28NM 1998031900297 19980319 00297 WP 1998 3 19 CALA9800412 1 19980311 A 5320 BEAM DOUG DC9 DC982 3022082 WP BAGGAGE COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 938AS 49365 INSPECTION FOUND MID BAGGAGE BIN Z-ANGLE BEAM CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998031900298 19980319 00298 NM 1998 3 19 CALA9800413 1 19980311 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND FLOORBEAM CORRODED AROUND NUT PLATE HOLE AT BS 947 BETWEEN RBL 12 AND LBL 12. THE FLOORBEAM WAS REPAIR ED IAW SRM 51-00-51. 2 L 7 2 4F RT A16WE 1998031900299 19980319 00299 WP 1998 3 19 CALA9800414 1 19980312 A 7120 BOLTS DOUG DC10 DC1030 3023501 WP NR 3 ENGINE LOOSE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND NR 3 ENGINE FORWARD ENGINE MOUNT TRUSS BOLTS LOOSE AT TRUSS TO PYLON BOX INTERSECTION LOWER SURFACE. T HE BOLTS WERE RETORQUED IAW SERVICE BULLETIN A54-99. 2 L 7 3 4F A22WE 1998031900300 19980319 00300 NM 1998 3 19 CALA9800415 1 19980312 A 3234 CIRCUIT BREAKER BOEING 737 7372C0 1384488 NM COCKPIT INOPERATIVE A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 14245 20074 THE LANDING GEAR HANDLE COULD NOT BE RAISED PAST THE OFF POSITION AFTER TAKEOFF FROM MSY. THE GEAR LIGHTS CIRCUIT BREAK ER WAS FOUND POPPED. THE CIRCUIT BREAKER WAS RESET AND THE GEAR RAISED NORMALLY. A FEW MINUTES LATER THE LIGHTS CIRCUI T BREAKER POPPED AGAIN. THE CIRCUIT BREAKER WAS RESET TO EXTEND THE GEAR FOR LANDING AND THE CIRCUIT BREAKER POPPED AGA IN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE CIRCUIT BREAKER EXTREMELY WEAK. THE LIGHTS CIRCUIT BR EAKER WAS REPLACED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A16WE 1998031900301 19980319 00301 WP 1998 3 19 CALA9800416 1 19980312 A 5730 SKIN DOUG DC10 DC1010 3022110 WP WS 538 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT XORS 538. THE CORROSION WAS REMOVED. A DOUBLER WAS FABRIC ATED AND INSTALLED IAW SRM 57-10. 2 L 7 3 4F A22WE 1998031900302 19980319 00302 WP 1998 3 19 CALA9800417 1 19980312 A 5711 ANGLE DOUG DC10 DC1010 3022110 WP FRONT SPAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON LEADING EDGE LOWER SPAR CAP ANGLE LOCATED ABOVE AND JUST OUTBOARD OF NR 3 ENGINE PYLON OUT BOARD SIDE. SECTION OF SACRIFICIAL DOUBLER WAS CUT OUT AND AREA WAS REPAIRED IAW DOUGLAS DRAWING 26752-6204. 2 L 7 3 4F A22WE 1998031900303 19980319 00303 WP 1998 3 19 CALA9800418 1 19980312 A 5711 ANGLE DOUG DC10 DC1010 3022110 WP FRONT SPAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND RT WING LEADING EDGE LOWER FRONT SPAR CAP ANGLE CORRODED NINE INCHES INBOARD OF FUEL VALVE. THE CORROS ION WAS REMOVED IAW SRM 51-21-00. A METAL STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-0. 2 L 7 3 4F A22WE 1998031900304 19980319 00304 WP 1998 3 19 CALA9800419 1 19980312 A 5720 DOUBLER DOUG DC10 DC1010 3022110 WP FRONT SPAR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION ON RT WING LOWER LEADING EDGE SACRIFICIAL DOUBLER JUST INSIDE PANEL NR 617 AB FRONT SPAR AREA . THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-21-0 1 AND ECRA 5720-01643, FIGURE 2. 2 L 7 3 4F A22WE 1998031900305 19980319 00305 WP 1998 3 19 CALA9800420 1 19980312 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP R-2 DOORWAY TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND ANGLE TORN AT BOLT HOLES FOR CABLE PULLEY BRACKET AT AFT UPPER CORNER OF R-2 DOOR CUTOUT. THE SUPPORT CHANNEL WAS REMOVED. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-31-1, 51-40-00, 51-21-1, AND 51-90-00. 2 L 7 3 4F A22WE 1998031900306 19980319 00306 NM 1998 3 19 CALA9800421 1 19980312 A 5320 INTERCOSTAL BOEING 727 727243 138408D NM BS 1030-1050 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 1.25 CRACK IN SUPPORT INTERCOSTAL AT AFT BAGGAGE COMPARTMENT BETWEEN BS 1030 AND 1050 ABOVE STRINGER 25L. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998031900307 19980319 00307 NM 1998 3 19 CALA9800422 1 19980313 A 5347 FLOOR TRACK BOEING 727 727243 138408D NM BS 1100 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1100, BL 45R. THE CORRODED SECTION OF FLOOR TRACK WAS REMOVED AND RE PLACED IAW SRM 53-10-5. 2 L 7 3 4F RT A3WE 1998031900308 19980319 00308 NM 1998 3 19 CALA9800423 1 19980313 A 5347 FLOOR TRACK BOEING 727 727243 138408D NM BS 1050-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND CABIN FLOOR TRACK CORRODED AT STA 1050 TO 1130, BL 25R. THE CORRODED SECTION OF FLOOR TRACK WAS REPLAC ED IAW SRM 53-10-5 AND 51-10-1. 2 L 7 3 4F RT A3WE 1998031900309 19980319 00309 NM 1998 3 19 CALA9800424 1 19980313 A 5330 SKIN BOEING 727 727243 138408D NM FUSELAGE BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND RT FUSELAGE SKIN BULGED JUST AFT AND BELOW FORWARD LAV SERVICE PANEL. THE BULGED AREA WAS REMOVED. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-2. 2 L 7 3 4F RT A3WE 1998031900310 19980319 00310 NM 1998 3 19 CALA9800425 1 19980313 A 5320 WEB BOEING 727 727243 138408D NM BS 1176 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 7 CRACK JUST BELOW DRAIN CHUTE IN LT AFT LAV FLOOR WEB AT BS 1176, LBL 50. THE CRACKED SECTION OF WE B WAS REMOVED. A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-20-01. 2 L 7 3 4F RT A3WE 1998031900311 19980319 00311 NM 1998 3 19 CALA9800426 1 19980313 A 5320 GUSSET BOEING 727 727243 138408D NM BS 825 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 2 CRACK IN GUSSET ON FORWARD SIDE OF RT FUSELAGE FRAME AT STA 825, RBL 70. THE GUSSET WAS REMOVED AN D A NEW ONE WAS INSTALLED IAW EA SA012-5310-01870. 2 L 7 3 4F RT A3WE 1998031900312 19980319 00312 WP 1998 3 19 9804029935 1 19980305 A 3230 LATCH MECHANISM DOUG DC9 DC931 3022065 WP LT MLG DOOR LACK OF LUBE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 1332U 47404 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW PERFORMED UPLATCH CHECK AND GEAR DOOR OPEN LIGHT ILLUMINATED. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBED LEFT MAIN GEA R DOOR LATCH MECHANISM AND UPPER DOOR SEQUENCE CABLE. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SER VICE. 2 L 7 2 4F A6WE 1998031900313 19980319 00313 NM 1998 3 19 9804246740 1 19980308 A 3610 PNEUMATIC SYST BOEING 747 747251F 1384898 NM NR 4 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 640US 640US DURING TAKEOFF, THE NR 4 ENGINE DID NOT REACH TAKEOFF POWER AND PNEUMATIC HIGH STAGE LIGHT DID NOT EXTINGUISH WHEN POWER WAS SET FOR TAKEOFF. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE HIGH STAGE VALVE, HIGH STAGE CON TROL, AND PNEUMATIC LINE. EXACT PART CAUSING FAULT TO BE DETERMINED. 2 L 7 4 4F A20WE 1998031900315 19980319 00315 NM 1998 3 19 UPS98226093 1 19980312 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 OVERWING EMERGENCY LIGHTS AND AFT STAIR EMERGENCY LIGHTS ARE WEAK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS. LIGHTS OPS CHECK NORMAL IAW M/M 33-50-11, P\N'S ON 96-21015 S\N'S ON NSN P\N'S OFF 96-2-1015 S\N OFF NSN. 2 L 7 3 4F A3WE 1998031900316 19980319 00316 WP 1998 3 19 UPS98826088 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 693 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C RT WING L/E RIB AT STA. XFS693.00 IS CRACKED ON THE UPPER AFT END. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 1998031900317 19980319 00317 WP 1998 3 19 UPS98826089 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 629 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C RT WING L/E UPPER RIB AT STA XFS629.00 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900318 19980319 00318 WP 1998 3 19 UPS98826090 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 672 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C RT WING L/E RIB (UPPER) AT STA XFS672.00 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED I AW SRM 57-2-0 FIG.2. 2 L 7 4 4F RT 4A25 1998031900319 19980319 00319 WP 1998 3 19 UPS98826091 1 19980226 A 5313 5753744501 LONGERON DOUG DC8 DC871F 302199D WP BS 1280-1300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C F/S 1280-1300 STR 31L IS CRACKED BTWN 5 FASTENERS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LON GERON IAW SRM 51-1-21 AND DWG 5753744. 2 L 7 4 4F RT 4A25 1998031900320 19980319 00320 WP 1998 3 19 UPS98826092 1 19980305 A 5320 4641324N FITTING DOUG DC8 DC871F 302199D WP BS 1690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE:C F/S 1690 LONGERON 28L. LONGERON TO FRAME FITTING IS EXFOLIATED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998031900321 19980319 00321 EU 1998 3 19 98FDEA00180 1 19980312 A 2612 FIRE WARN AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE MALFUNCTION A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 654FE 738 98-0067, AT APPROX 11000 FT ON CLIMB-OUT GOT A MOMENTARY FIRE WARN IN THE NR 2 ENG AS POWER WAS REDUCED WARN WENT OUT. A LL ENG INSTRUMENTS WERE NORMAL. PERFORM FIRE TEST ON NR 2 ENG PLUS IT WAS NORM BROUGHT PWR BK TO CLIMB TO CLIMB SET WIT H NO REOCCURENCE. INSP ENG, AND ALL BLEED CONN AND CLAMP RAN ENG FOR 5 MIN PER A300 JRH SYS CKD GOOD. SPRAY ALL CLAMPS , CONN AND VALVES W/LEAK DEVELOPER/DETECTOR FOUND NO LEAKS AFTER PERFORM ENG RUN. SYS NORM. 2 L 7 2 4F RT A35EU 1998031900322 19980319 00322 NM 1998 3 19 98FDEA00181 1 19980312 A 5320 65159784 STRAP BOEING 727 72722 1384002 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 CORROSION (C53-132-02-1, 2) ON LOAD TENSION STRAP BS 870, RBL 35 TO 50. *S/D* REPAIRED BS 870 LOAD TENSION STRAP AT RB L 30 TO 60 IAW FED-EX EA 7-5310-37605. 2 L 7 3 4F A3WE 1998031900323 19980319 00323 NM 1998 3 19 98FDEA00182 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0258 FWD CARGO, BELT FRAME DENTED BS 700, STR 24 R. REMOVED DAMAGE. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900324 19980319 00324 NM 1998 3 19 98FDEA00183 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0256 FWD CARGO, BELT FRAME DENTED BS 680, STR 25 R. REMOVED DAMAGE. FABRICATED AND DRILLED DOUBLER AND PRIMED ALL B ARE METAL. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900325 19980319 00325 NM 1998 3 19 98FDEA00184 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0257 FWD CARGO, BELT FRAME DENTED ( 2 PLACES) BS 680, AT STR 23 AND STR 22 R. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900326 19980319 00326 NM 1998 3 19 98FDEA00185 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 700 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0253 FWD CARGO, BELT FRAME DENTED BS 700, STR 22 R. REMOVED DAMAGE. INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900327 19980319 00327 NM 1998 3 19 98FDEA00186 1 19980312 A 5751 RIB BOEING 727 727233 138408A NM RT AILERON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0905 RT OUTBD AILERON HAS .25 DIA CHERRY MAX FASTENER IN UPPER SKIN, RIB IS .600 WIDE, ORIGINAL FASTENERS WERE .125 D IA COUNTER SINK INTO RIB WILL HAVE DAMAGED RIB AND MINIMUM ED IS LOST IN RIB. REMOVED AND REPLACED RIB PER SRM 51-10-1. SKIN REPAIR ACCOMPLISHED ON NR 0906 AILERON BALANCE ACCOMPLISHED ON NR 0324. 2 L 7 3 4F RT A3WE 1998031900328 19980319 00328 NM 1998 3 19 98FDEA00187 1 19980312 A 5313 STRINGER BOEING 727 727233 138408A NM BS 560 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0263 71C203-02 FWD CARGO BS 560, STR 24 LT, STRINGER CRACKED UPPER FLANGE. STOP DRILLED CRACK PER SRM 51-10-1. ALOD INED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 53-10-3. 2 L 7 3 4F RT A3WE 1998031900329 19980319 00329 NM 1998 3 19 98FDEA00188 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0267 FWD CARGO, BELT FRAME DENTED (2 PLACES) AT BS 520 BETWEEN STRS 23 - 25 L. REMOVED DAMAGE. INSTALLED REPAIR DOU BLER ON BELT FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900330 19980319 00330 NM 1998 3 19 98FDEA00189 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0268 FWD CARGO, BELT FRAME DENTED ( 2 PLACES ) AT BS 500 BETWEEN STRS 22 - 24 L. REMOVED DAMAGE. INSTALLED DOUBLER AT BS 500 BETWEEN STRS 22 - 24 L PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900331 19980319 00331 NM 1998 3 19 98FDEA00190 1 19980312 A 5330 SKIN BOEING 727 727233 138408A NM PAX DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0271 7-5330-7-2345 P1-3, SKIN CRACKED AT LOWER HINGE AT FWD ENTRY DOOR. ROUTED OUT CRACK. VERIFIED BY NDT. INSTALL ED DOUBLER PER EO 7-5330-7-2345 C2. 2 L 7 3 4F RT A3WE 1998031900332 19980319 00332 NM 1998 3 19 98FDEA00191 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 560 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0260, FWD CARGO, BELT FRAME DENTED AT BS 560 BETWEEN STRS 22 - 25 L. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER ON BE LT FRAME PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900333 19980319 00333 NM 1998 3 19 98FDEA00192 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0259, FWD CARGO BELT FRAME DENTED AT BS 580 BETWEEN STRS 23 - 25 L. REMOVED DAMAGE. INSTALLED DOUBLER BS 580 BETWEE N STRS 23 - 25 L PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998031900334 19980319 00334 NM 1998 3 19 98FDEA00193 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 NR 0917, FWD LOWER CARGO COMPT: FRAME DENTED AT BS 520, STR 23 - 24 RT. REMOVED DAMAGED FRAME SECTION LOWER FORWARD CA RGO BS 520, STR 23 - 24 RT. INSTALLED DOUBLER AND NEW STRINGER CLIPS PER SRM 51-40-3 FIG 1 (SHEET 4) AND SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998031900335 19980319 00335 NM 1998 3 19 98FDEA00194 1 19980312 A 5311 FRAME BOEING 727 727233 138408A NM BS 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 NR 0775, FWD LOWER CARGO COMPT, FRAME DENTED BS 600 AT STR 24 - 25 LT. REMOVED DAMAGED AREA, FABRICATED, ALODINED AND P RIMED REPAIR DOUBLER AND INSTALLED DOUBLER PER SRM 53-10-4 FIGURE 1 (SHEET 3). 2 L 7 3 4F RT A3WE 1998031900336 19980319 00336 NM 1998 3 19 98FDEA00195 1 19980312 A 5313 STRINGER BOEING 727 727233 138408A NM BS 550 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 NR 0591, FWD CARGO, STRINGER CORRODED UNDER STAND, OFF NUTPLATE BS 550 L AT STRINGER 27L. REMOVED DAMAGED AREA OF STRIN GER PER SRM 53-10-3 FIG 1 SHEET 1. MADE DOUBLER AND FILLER FROM BAC1498-108 AND BAC1498-133 MATERIAL PER SRM 53-10-3 FI G 1 SHEET 2. ALODINED AND PRIMED AFFECTED AREAS PER M/M 51-20-0. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 1 SHEET 4 AND SRM 53-10-3 FIG 1 SHEET 1 WITH 870-B2 SEALANT. REINSTALLED STAND OFF PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998031900337 19980319 00337 NM 1998 3 19 98FDEA00196 1 19980312 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720B CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 NR 0578 AFT OF BS 720B, R STR 15, AT LEADING EDGE LIGHT CRACKED. REPAIRED STRINGER, CUT OUT DAMAGED AREA INSTALLED U C HANNEL AND FILLER PER SRM 53-10-5 FIG 5. 2 L 7 3 4F RT A3WE 1998031900338 19980319 00338 WP 1998 3 19 ABXA9800192 1 19980311 A 5312 5910130391N1 BULKHEAD TEE DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD NR 6 TEE CRACKED. REPLACED TEE IAW ABX EA 53-12-3. 2 L 7 2 4F A6WE 1998031900339 19980319 00339 WP 1998 3 19 ABXA9800193 1 19980311 A 5400 591326243N ANGLE DOUG DOUG DC9 DC941 302207N WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 977AX 47513 DURING C-CHECK, FOUND THE LEFT UPPER PYLON ATTACH ANGLE CRACKED BETWEEN STATION 1054 AND 1064. REPAIRED ANGLE IAW DC9 S RM 54-04. 2 L 7 2 4F A6WE 1998031900340 19980319 00340 WP 1998 3 19 ABXA9800194 1 19980311 A 7830 5958782503 TR LINK DOUG DOUG DC9 DC931 3022065 WP NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND THE UPPER RIGHT THRUST REVERSER LINK CRACKED. REPLACED LINK IAW DC9 MM 78-31-5. 2 L 7 2 4F A6WE 1998031900341 19980319 00341 WP 1998 3 19 ABXA9800195 1 19980311 A 7830 5958782503 TR LINK DOUG DOUG DC9 DC931 3022065 WP NR 1 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND THE LOWER RIGHT THRUST REVERSER LINK CRACKED. REPLACED LINK IAW DC9 MM 78-31-5. 2 L 7 2 4F A6WE 1998031900342 19980319 00342 WP 1998 3 19 ABXA9800196 1 19980311 A 5320 995773925N SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND SHEAR TIE BETWEEN LONGERON 14L AND 16L STATION 945 CRACKED. REPLACED SHEAR TIE IAW DC9 SRM 51-30- 5. 2 L 7 2 4F A6WE 1998031900343 19980319 00343 WP 1998 3 19 ABXA9800197 1 19980311 A 5320 991050315 WEB DOUG DOUG DC9 DC931 3022065 WP BS 963 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND 2 CRACKS IN CUSP WEB AT STATION 963, RIGHT SIDE. REPAIRED WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998031900344 19980319 00344 WP 1998 3 19 ABXA9800198 1 19980311 A 5313 59114279 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND LONGERON 17L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998031900345 19980319 00345 WP 1998 3 19 ABXA9800199 1 19980311 A 5315 991224357 FLOORBEAM DOUG DOUG DC9 DC931 3022065 WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND EXFOLIATION CORROSION BETWEEN ANGLE AND FLOORBEAM LOWER FLANGE ON BEAM AT STATION 965 RBL 8. REPA IRED FLOORBEAM IAW ABX REA D953-22983-MR. 2 L 7 2 4F A6WE 1998031900346 19980319 00346 WP 1998 3 19 ABXA9800200 1 19980312 A 5313 591141513 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND LONGERON 5R CRACKED AT STATION 718. REPAIRED LONGERON IAW DC9 SERVICE REWORK DWG SR09530128. 2 L 7 2 4F A6WE 1998031900347 19980319 00347 WP 1998 3 19 ABXA9800201 1 19980312 A 5313 591144555 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 690 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND LONGERON 7L CRACKED AT STATION 690. REPAIRED LONGERON IAW DC9 SERVICE REWORK DWG SR09530128. 2 L 7 2 4F A6WE 1998031900348 19980319 00348 WP 1998 3 19 ABXA9800202 1 19980312 A 5400 99582208 STIFFENER DOUG DOUG DC9 DC931 3022065 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 DURING C-CHECK, FOUND STIFFENER CRACKED ON NR 2 PYLON WHERE THROTTLE CABLE PASSES THROUGH OUTBOARD SIDE OF PYLON. REPLA CED STIFFENER IAW DACO DWG 9958220 AND DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998031900349 19980319 00349 NM 1998 3 19 DL72S980547 1 19980310 A 3230 ACTUATOR ROD 65404674 BOEING 727 727232 1384082 NM NLG FAILED A DALA K NONE O OTHER TO TAKEOFF 1 SO 27 418DA 283 21271 NOSE LANDING FAILED TO RETRACT ON CLIMB-OUT OF LEX. C/W POM CONTINUED TO CVG. LUBED NOSE GEAR AND FOUND NOSE GEAR DOWN LOCK ACTUATOR ROD FAILED. REPLACED N OSE GEAR DOWNLOCK ACTUATOR ASSY 324003683 S/N ON 1255 S/N OFF 283. 2 L 7 3 4F A3WE 1998031900350 19980319 00350 WP 1998 3 19 DLL19980548 1 19980310 A 5311 1506088106 FRAME LKHEED 1011 10113853 5265020 WP BS 1083/1103 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 753DA 193W1189 REFERENCE N/R CARDS 274 AND 275 FRAME CRACK RT SIDE STA 1083 AND STA 1103 AT WATERLINE 200 AT FLOOR LONGERON ATTACH. R EPAIRED PER EO764076-3. 2 L 7 3 4F A23WE 1998031900351 19980319 00351 NM 1998 3 19 DL72L980552 1 19980310 A 5313 SRINGER BOEING 727 727232 1384082 NM BS 945 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 STRINGER 18A LT CRACKED 1 INCH THROUGH HORIZ FLANGE AT STA 945. REPAIRED PER M/M 53-12-0 LEVEL 1 TIME LIMITED REPAIR. 2 L 7 3 4F A3WE 1998031900352 19980319 00352 WP 1998 3 19 DLL10980554 1 19980306 A 5330 1503542107 SKIN LKHEED 1011 10113851 5265010 WP BS 1655 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 719DA 193C1135 FUSELAGE/SKIN, FS 1645-1665, STRG 38-39. REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED BETWEEN FS 1645 AND 1665 AND BETWEEN STRINGERS 38 AND 39. THE CORROSION DAMAGE WAS CUTOUT AND AN EXTERNAL REPAIR DOUBLER AND TRIPL ER WERE INSTALLED PER ER/A 364158-14, REV A. 2 L 7 3 4F A23WE 1998031900353 19980319 00353 NM 1998 3 19 DL72W980555 1 19980311 A 5320 WEB BOEING 727 727247 138408F NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 FOUND ON A1 LETTER CK .25 IN CRACK AT LIGHTENING HOLE VERTICAL WEB STA 1233R IN 48 SECTION. ROUTED OUT DAMAGED AREA PER MM 53-11-0. 2 L 7 3 4F A3WE 1998031900354 19980319 00354 NM 1998 3 19 DL72W980556 1 19980311 A 5720 AUX SPAR BOEING 727 727247 138408F NM LT WING CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 MLG AUX SPAR CHAFED AT INBD FWD END LT SIDE. REPAIRED PER MM 57-43-0 P 801. 2 L 7 3 4F A3WE 1998031900355 19980319 00355 NM 1998 3 19 DL72S980557 1 19980224 A 5311 FRAME BOEING 727 727232 1384082 NM BS 930 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 ITEM: FRAME CRACKED STA 930 ABOVE 14 LT MARKED. REPAIRED PER SRM 53-10-4 FIG 25. 2 L 7 3 4F A3WE 1998031900356 19980319 00356 1998 3 19 DL73K980559 4 19980311 A 2562 6076905 ELT LOCATOR BOEING 737 737232 1384475 NM COCKPIT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 312DL 23084 DURING L/O CHECK, FOUND ELT BEACON DAMAGED. REPLACED BEACON. 2 L 7 2 4F RT A16WE 1998031900357 19980319 00357 WP 1998 3 19 DLL10980560 1 19980311 A 3350 BATTERY PACK 516574 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 721DA 37237 193C1139 EMERGENCY LIGHTS DO NOT ILLUMINATE 16A/B AND 22H/J/ RT GALLEY LIFT AND LOWER GALLEY. REPLACED BATTERY PACK CHECKS OK. 2 L 7 3 4F A23WE 1998031900358 19980319 00358 WP 1998 3 19 DLL10980561 1 19980311 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 721DA 62845 193C1139 EMERGENCY EXIT SIGN AT 3-R DOOR STOP ILLUMINATION AFTER TWO MINUTES. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 3 4F A23WE 1998031900359 19980319 00359 NM 1998 3 19 DL72S980562 1 19980311 A 3350 BATTERIES S106 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA 22076 EMERGENCY LIGHTS ABOVE AIRSTAIRS INOP. REPLACED BATTERIES. CKS GOOD. 2 L 7 3 4F A3WE 1998031900360 19980319 00360 NM 1998 3 19 DL72L980563 1 19980311 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 514DA 21430 BOTH F/C DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998031900361 19980319 00361 NM 1998 3 19 DL72E980565 1 19980220 A 5520 TIP BOEING 727 727247 138408F NM LT ELEVATOR MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 OB AFT TIP IS MISSING ON THE LT ELEVATOR. REMOVED DAMAGED SKIN. FABRICATED REPAIR PER M/M 55-20-0 PG 801. OK TO INSTA LL. INSTALLED REPAIR PER M/M 55-20-0 PG 801. 2 L 7 3 4F A3WE 1998031900362 19980319 00362 NM 1998 3 19 SCNA98023 1 19980307 A 2910 HYDRAULIC LINE BOEING 727 727225 1384077 NM CARGO COMPT LEAKING A SCNA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 15 282SC 22558 FUMES EXIST IN PASSENGER CABIN. FOUND TAILSKID HYDRAULIC LINE IN AFT WALL OF AFT CARGO COMPARTMENT LEAKING FLUID ON A P NEUMATIC DUCT. INSTALLED A TEMPORARY REPAIR TO THE HYDRAULIC LINE AND FUNCTIONALLY CHECKED GOOD. 2 L 7 3 4F A3WE 1998031900363 19980319 00363 NM 1998 3 19 VNAA9803013 1 19980311 A 3620 3280071AMENDC PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT OVHEAD FAILED A VNAA D RETURN TO BLOCK N L FALSE WARNING NO TEST TX TAXI/GRND HDL 1 GL 07 440JS 67659 21795 3058 A LEFT HIGH PRESSURE BLEED FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENTS. MAINTENANCE INSPECTED AND REPLACED THE 16 VE OVERHEAD PANEL IN ACCORDANCE WITH DORN IER MAINTENANCE MANUAL 31-12-12. OPERATION CHECKS WERE GOOD, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031900364 19980319 00364 WP 1998 3 19 CKSA98088 1 19980308 A 3260 H2024B SWITCH DOUG DC8 DC861 3021952 WP RT MLG DOOR MALFUNCTION A CKSA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 812CK 45890 RT DOOR UNSAFE LIGHT AND DOORS NOT LATCHED LIGHT ON DURING FLIGHT, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED R T MAIN GEAR DOOR LIGHT SWITCH AND ADJUSTED STRIKER PLATE. OPS CHECKS GOOD ON GROUND AT THIS TIME. 2 L 7 4 4F 4A25 1998031900365 19980319 00365 WP 1998 3 19 CKSA98089 1 19980217 A 5347 SEAT TRACK DOUG DC8 DC8F55 3021928 WP BS 660 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161C 45856 DURING NON-ROUTINE MAINTENANCE FOUND, CENTER SEAT TRACK IN MAIN CARGO REQUIRES SPLICE AT FS 660. REMOVED AND REPLACED C ENTER SEAT TRACK IAW DC8 SRM 53-2-3. NON-ROUTINE ITEM NUMBER 30. 2 L 7 4 4F 4A25 1998031900366 19980319 00366 WP 1998 3 19 CKSA98090 1 19980307 A 3260 BULB DOUG DC8 DC861 3021952 WP MLG DOORS FAILED A CKSA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 812CK 45890 DURING FLIGHT DOOR NOT LATCH LIGHT AND RT DOOR UNSAFE LIGHT CAME ON. ALL ELSE NORMAL. CLEANED UPLATCH C/P, REPLACED BA DLY MUSHROOMED DOOR LIGHT BULB, OPS CHECKS OK PER DC-8 MM 32-12-1. 2 L 7 4 4F 4A25 1998031900367 19980319 00367 WP 1998 3 19 TWAA9802906 1 19980124 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 978Z 47250 STL - DURING OP 15 MAINTENCE CHECK, LONGERON 3L BELT RING WAS FOUND WITH A .25 INCH CRACK AT STA 160. REPLACED LONGERON FROM STA 148 END FITTING TO FACTORY SPLICE PER SRM 51-10. ACFT TT: 70,351 HOURS. ACFT TC: 83,824. (X) 2 L 7 2 4F A6WE 1998031900368 19980319 00368 WP 1998 3 19 TWAA9802905 1 19980124 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 978Z 47250 STL - DURING OP 15, A .25 INCH CRACK WAS FOUND AT STA 160 LONGERON 4L BELT RING. REPLACED LONGERON FROM STA 148 END FIT TING TO FACTORY SPLICE PER SRM 51-10. ACFT TT: 70,351 HOURS. ACFT TC: 83,824. (X) 2 L 7 2 4F A6WE 1998031900369 19980319 00369 WP 1998 3 19 TWAA9802904 1 19980124 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 978Z 47250 STL - DURING OP 15 MAINTENANCE CHECK, A CRACK WAS FOUND AT STA 200 LONGERON 4L. REPLACED LONGERON FROM STA 148 END FITT ING TO FACTORY SPLICE PER SRM 51-10. ACFT TT: 70,351 HOURS. ACFT TC: 83,824. (X) 2 L 7 2 4F A6WE 1998031900370 19980319 00370 WP 1998 3 19 TWAA9802903 1 19980126 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 958-972 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 978Z 47250 STL - DURING OP 16 MAINTENANCE CHECK, THE LOWER ATTACH LEG OF LONGERON 12 RT STA 965 WAS FOUND CRACKED .25 INCH. SPLICE D IN NEW LONGERON SECTION FROM STA 958 TO STA 972 RT SIDE OF FUSELAGE LONGERON 12 RT. LONGERON SPLICED IN PER SRM 53-02 FIG 18. ACFT TT: 70,351 HOURS. ACFT TC: 83,824. (X) 2 L 7 2 4F A6WE 1998031900371 19980319 00371 WP 1998 3 19 TWAA9802902 1 19980219 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 STL - DURING OP 9 MAINTENANCE CHECK, LONGERON 5L WAS FOUND CRACKED AT CABIN FUSELAGE STA 718. REPLACED LONGERON 5L CRAC KED SECTION PER SRM 53-02 FIG 18. ACFT TT: 75,771 HOURS. ACFT TC: 82,773. (X) 2 L 7 2 4F A6WE 1998031900372 19980319 00372 WP 1998 3 19 TWAA9802901 1 19980219 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 STL - DURING OP 9 MAINTENANCE CHECK, LONGERON 5L WAS FOUND CRACKED AT CABIN FUSELAGE STA 756. REPLACED LONGERON 5L CRAC KED SECTION PER SRM 53-02 FIG 18. ACFT TT: 75,771 HOURS. ACFT TC: 82,773. (X) 2 L 7 2 4F A6WE 1998031900373 19980319 00373 EU 1998 3 19 PLGA980228A 1 19980228 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU RT TAIL PIPE DIRTY A PLGA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 NE 05 343BE 340A101 SYR - FLT 4723 - AFTER TAKEOFF WHILE CLIMBING THROUGH 2,000 FEET, THE RT TAIL PIPE HOT LIGHT WARNING ILLUMINATED. CREW FOLLOWED PROCEDURE AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT RETURNED TO SYR AND LANDED WIHOUT INCIDENT. MAINTENANCE FO UND MOISTURE AND OIL IN RT DETECTOR CONNECTOR. THE CONNECTOR WAS CLEANED AND SYSTEM TESTED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998031900374 19980319 00374 EU 1998 3 19 PLGA980227A 1 19980227 A 7931 8543 SWITCH SAAB SF340 340B 7860101 EU RIGHT MALFUNCTIONED A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NE 05 349BE 0305W 340B196 BOS - FLT 4276 - DURING TAKEOFF, THE RT OIL PRESSURE WARNING ILLUMINATED. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE RT PGB OIL PRESSURE SWITCH. ENGINE WAS GROUND RUN AND SYSTEM TESTED GOOD. (X) 2 L 7 2 4T RT A52EU 1998031900375 19980319 00375 EU 1998 3 19 PLGA980220A 1 19980220 A 3020 NH24668081 INLET DUCT SAAB SF340 SF340A 7850100 EU RT ENGINE BURNED A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 05 346BE L155700 340A150 MHT - FLT 4386 - WHILE EN ROUTE FROM BOS TO SYP, CREW NOTICED SPARKS COMING FROM RT ENGINE INTAKE DUCT HEAT. SYSTEM WAS SHUT DOWN AND AIRCRAFT LANDED AT MHT WITHOUT INCIDENT. MAINTENANCE INSPECTED RT ENGINE INTAKE AND FOUND A HOLE BURNED IN THE LOWER DUCT. DUCT REPLACED AND SYSTEM TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998031900376 19980319 00376 SO 1998 3 19 MASA98043 1 19980227 A 3350 FO2A250V1A FUSE MS265721 EMB 120 EMB120RT SO CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 287UE 120183 CLT/GNV - FLT 5593 - PILOT REPORTED BOTH AFT EXTERIOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND RE PLACED THE FUSE. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998031900377 19980319 00377 CE 1998 3 19 MASA98044 1 19980205 A 5511 10162000061 SPAR BEECH 1900 1900D 1154162 CE HORIZONTAL STAB CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 46YV UE46 DURING NIGHT MAINTENANCE, FOUND THE HORIZONTAL STABILON SPAR CRACKED AROUND THE DEICE HOSE. MAINTENANCE REPAIRED THE CR ACKED WEBBING IN THE HORIZONTAL STABILIZER MAIN SPAR CENTER WEB IAW RO NR B1900D-55-0001. ACFT TT: 11,800 HOURS. ACFT TC: 18,212. (X) 2 L 7 2 4T RT A24CE 1998031900378 19980319 00378 NM 1998 3 19 MZZA98069 1 19980202 A 2810 10614212 GASKET BOEING 727 727264 138408M NM LT/RT WING TANKS MISSING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHK - FOLLOWING REMOVAL OF ALL NON-STRESSED WING FUEL TANK ACCESS PANELS FOUND NO PANELS HAD ALUMINUM KNITTED GA SKETS FITTED. BONDING GASKET REINSTALLED PRIOR TO PANEL REPLACEMENT. FUEL LEAK CHECK CARRIED OUT. (X) 2 L 7 3 4F A3WE 1998031900379 19980319 00379 NM 1998 3 19 MZZA98078 1 19980126 A 2782 651627537 ANGLE BOEING 727 727264 138408M NM RT LE FLAP ACT CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHK - NR 6 KRUEGER LEADING EDGE FLAP ACTUATOR TRUNNION MOUNTING BOX IS CRACKED AT LOWER INBOARD CORNER. FORMED SECTION FABRICATED IAW BOEING DRAWING AND INSTALLED IAW SRM 51-30-2. ACTUATOR REINSTALLED AND FUNCTIONAL CHECK CARRIED OUT. (X) 2 L 7 3 4F A3WE 1998031900380 19980319 00380 NM 1998 3 19 MZZA98077 1 19980129 A 5712 69174548 RIB BOEING 727 727264 138408M NM RT WING CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHECK - RIGHT WING OUTBOARD F/FLAP CENTER STABILIZING TRACK - SUPPORT FITTING INBOARD AND OUTBOARD TRACK RIBS - OUTBOARD RIB HAS .50 INCH CRACK AT FORWARD RIVET HOLE AND INBOARD RIB HAS EXCESSIVE WEAR IN LUG RADIUS. BOTH FITTINGS R EPLACED IAW SRM 51-30-2. F/FLAP REFITTED AND TESTED IAW MM 27-51-11. REF: OPERATOR CONTROL NR 98ZZZX1074. (X) 2 L 7 3 4F A3WE 1998031900381 19980319 00381 NM 1998 3 19 98ZZZX1074 1 19980129 A 5712 69174758 RIB BOEING 727 727264 138408M NM RT WING CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHECK - RIGHT WING OUTBOARD F/FLAP CENTER STABILIZING TRACK - SUPPORT FITTING INBOARD AND OUTBOARD TRACK RIBS - OUTBOARD RIB HAS .50 INCH CRACK AT FORWARD RIVET HOLE AND INBOARD RIB HAS EXCESSIVE WEAR IN LUG RADIUS. BOTH FITTINGS R EPLACED IAW SRM 51-30-2. F/FLAP REFITTED AND TESTED IAW MM 27-51-11. REF: OPERATOR CONTROL NR MZZA98077. 2 L 7 3 4F A3WE 1998031900382 19980319 00382 NM 1998 3 19 MZZA98076 1 19980209 A 2710 65256232 PCU COVER BOEING 727 727264 138408M NM AILERON CONTROL CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHECK - DURING REASSEMBLY OF AILERON PCU LINKAGE ASSEMBLY, LOWER COVER WAS FOUND CRACKED AT LOWER RIG PIN HOLE. REPAIR TO LOWER COVER CUT-OUT IAW ECRA 5270C072. PLEASE REFER TO ROUTINE CARD NR 552 FOR REASSEMBLY OF PCU LINKAGES. ( X) 2 L 7 3 4F A3WE 1998031900383 19980319 00383 NM 1998 3 19 MZZA98075 1 19980209 A 2710 69258822 BRACKET BOEING 727 727264 138408M NM RT WING DAMAGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHECK - DURING REPLACEMENT OF RT AILERON BUS CABLE, FOUND RT AILERON BUS CABLE TURNAROUND PULLEY BRACKET DAMAGED . PLATES FABRICATED AND INSTALLED IAW BOEING DRAWING 69-25882. REFER HNRC 869821 FOR CABLE REPLACEMENT. (X) 2 L 7 3 4F A3WE 1998031900384 19980319 00384 NM 1998 3 19 MZZA98074 1 19980121 A 5720 651620054 STIFFENER BOEING 727 727264 138408M NM WS 251 CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - C-CHECK - CORROSION FOUND AT RT WING SPAR STIFFENER OF FRONT SPAR NR 2 FROM WS 251 (NR 5 KRUGER FLAP AREA). CORRO SION REMOVED AND FOUND BEYOND LIMIT IAW SRM 57-10-1 AREA 3 INCHES BY 1.5 INCHES BY 0.024 INCH. STIFFENER REPLACED IAW S RM 51-30-2. HYDRAULIC PIPING AND BONDING REINSTALLED. FOR FUEL LEAK CHECK OF FASTENERS REFER HNRC 869988. (X) 2 L 7 3 4F A3WE 1998031900385 19980319 00385 NM 1998 3 19 MZZA98073 1 19980126 A 5754 ANGLE BOEING 727 727264 138408M NM NR 2 LE SLAT CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHECK - NR 2 SLAT LOWER SKIN ATTACH ANGLE FOUND WITH TWO CRACKS AT TAI DUCT CUT-OUT AT SLAT STA 271. FORMED SEC TION REPAIR CUT-OUT IAW ECRA 5750-02901. (X) 2 L 7 3 4F A3WE 1998031900386 19980319 00386 NM 1998 3 19 MZZA98072 1 19980125 A 5751 65192745 RIB BOEING 727 727264 138408M NM RT AILERON CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 622DH 20896 RIGHT OUTBOARD AILERON INBOARD HINGE SUPPORT AT WBL 498.4 - UPPER AFT FLANGE OF CHORD IS CRACKED. FORMED SECTION REPAIR CUT-OUT IAW ECRA EC 5720-00196. (X) 2 L 7 3 4F A3WE 1998031900387 19980319 00387 NM 1998 3 19 MZZA98071 1 19980202 A 2780 PIN BOEING 727 727264 138408M NM FLAP CONTL VALVE MISSING A MZZA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHECK - LEADING EDGE SLAT/FLAP CONTROL VALVE FOUND TO HAVE MISSING SPLIT PIN IN INPUT LEVER BOLT AND NUT INSTALL ED FINGER TIGHT. BOLT AND NUT TORQUED AND SPLIT PINNED IAW MM 27-81-81. (X) 2 L 7 3 4F A3WE 1998031900388 19980319 00388 NM 1998 3 19 MZZA98070 1 19980125 A 5741 NUT BOEING 727 727264 138408M NM RT WING MISSING A A MZZA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 622DH 20896 KUL - Q-CHECK - DURING INSPECTION OF RT WING HIP TANK, FOUND A BOLT MIGRATED AND BOTH NUTS MISSING OFF SUPPORT STRUT AT WBL 74 THAT SECURES RT AFT WING TERMINAL BOTTLE PIN FITTING. MIGRATED BOLT INSPECTED AND REINSTALLED. BOTH NUTS REPLAC ED IAW SRM 51-30-2. EXHAUSTIVE SEARCH CUT-OUT FOR MISSING NUTS, BUT WERE NOT FOUND. IT IS CONSIDERED THAT THE NUTS WER E NEVER INITIALLY INSTALLED. 2 L 7 3 4F A3WE 1998031900389 19980319 00389 WP 1998 3 19 HALA9800047 1 19980216 A 3350 41B004A07G3 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 661HA 47796 HNL - LOG PAGE NR A136850 - CAPTAIN'S OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BATTERIES AND T HE OPERATIONAL CHECK WAS OK. (X) 2 L 7 2 4F RT A6WE 1998031900390 19980319 00390 WP 1998 3 19 HALA9800046 1 19980214 A 3350 60030431 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 47654 HNL - FLT 533 - LOG PAGE NR A137965 - WITH EMERGENCY LIGHT SWITCH ON, ONE SECTION OF CABIN OVERHEAD LIGHTS DOES NOT ILLU MINATE. REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERIES. THE OPERATIONAL CHECK WAS GOOD. (X) 2 L 7 2 4F RT A6WE 1998031900391 19980319 00391 WP 1998 3 19 HALA9800044 1 19980212 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN BROKEN A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 47654 ITO - FLT 361 - LOG PAGE NR A137957 - EMERGENCY FLOOR LIGHT WIRE IS BROKEN ROW 23 EDF. REPLACED BROKEN RIBBON CABLE. O PS CHECK OKAY. (X) 2 L 7 2 4F RT A6WE 1998031900392 19980319 00392 WP 1998 3 19 HALA9800053 1 19980224 A 5755 CHAFE STRIPS DOUG DC9 DC951 3022051 WP LT/RT SPOILERS FAILED A HALA K NONE E VIBRATION/BUFFET CR CRUISE 1 WP 13 661HA 47796 HNL - FLT 177 - LOG PAGE NR A137992 - FLUTTER/VIBRATION AND RUMBLE FELT AT .75 MACH AND ABOVE. (FEELS AERODYNAMICALLY G ENERATED). REMOVED AND REPLACED TWO CHAFE STRIPS ON BOTH THE LEFT AND THE RIGHT SPOILERS. (X) 2 L 7 2 4F RT A6WE 1998031900393 19980319 00393 NM 1998 3 19 GAIA9826 1 19980227 A 3350 1000679 LIGHT BOEING 727 727251 138408H NM L1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278US 21157 UPON ARRIVAL AT TOL, CREW NOTED CREW EMERGENCY EXIT LIGHT BATTERY DEAD. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW B 727 MM 33-50. OPERATIONS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998031900394 19980319 00394 NM 1998 3 19 GAIA9825 1 19980227 A 3231 LINKAGE BOEING 727 727251 138408H NM NLG OUT OF ADJUST A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 264US 19983 TOL - AFTER DEPARTING, FLIGHT CREW IDENTIFIED THE 'NOSE GEAR DOOR LIGHT ON' AFTER GEAR RETRACTION. AIRCRAFT MADE AN UN EVENTFUL RETURN TO TOL. ADJUSTED AND TESTED NOSE GEAR DOOR LINKAGE IAW B-727 MM 32-22-01. AIRCRAFT RETURNED TO SERVICE . (X) 2 L 7 3 4F A3WE 1998031900395 19980319 00395 NM 1998 3 19 GAIA9823 1 19980228 A 5753 FLAP ROLLER BOEING 727 727223 1384074 NM LT TE FLAP OUT OF ADJUST A A GAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 6809 19484 WSSS - AFTER DEPARTING AT FL 250, THE FLIGHT CREW REPORTED THE AIRCRAFT AS FOLLOWS: THE PLANE STARTED EXPERIENCING UNCOM MANDED YAWING MOMENTS. THE AIRCRAFT MADE AN UNEVENTFUL RETURN TO WSSS. OPERATIONALLY CHECKED THE RUDDER, YAW DAMPENER, AILERON, AND SPOILER SYSTEMS AND FOUND NO DEFECTS. OPERATIONALY CHECKED THE FLAP SYSTEM AND ADJUSTED THE LT INBD FLAP TRACK ROLLER ECCENTRIC PER MM. (X) 2 L 7 3 4F A3WE 1998031900396 19980319 00396 NM 1998 3 19 TWRA9810 1 19980228 A 2120 AIR DISTRIBUTION BOEING 747 747136 1384883 NM CABIN ODOR A TWRA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 606FF 20273 PASSENGERS AND FLIGHT ATTENDANTS REPORTED A SMELL OF ELECTRICAL BURNING AROUND L2 AND R2. TURNED OFF ALL RECIRCULATING FANS AND GASPER FAN, SMELL STOPPED. INSPECTED ALL RECIR AND GASPER FANS FOR DEFECTS AND OPS, ALL NORMAL. PERFORMED PAC K BURN OUT, ALL PACKS AND ENGINES, NO ODOR NOTED AFTER BURN OUT. (X) 2 L 7 4 4F A20WE 1998031900397 19980319 00397 1998 3 19 TWRA9809 4 19980221 A 2350 24451 PSS SWITCH EATON 24451 BOEING 747 747131 1384881 NM R3 AUDIO CTRL P SHORTED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 608FF 19672 DURING CRUISE, R-3 AUDIO CONTROL PANEL (PSS PWR) SWITCH SHORTED OUT CAUSING SMOKE. REMOVED THE UNIT. STORED UNIT IN CO CKPIT. FOUND PSS SWITCH CONTACT BURNED. REMOVED AND REPLACED PSS SWITCH. CHECKED WIRING PER WDW 23-30-12. WIRING OK A ND OPS CHECK PSS OK PER MM 23-34-00. ALL FUNCTIONS NORMAL. (X) 2 L 7 4 4F A20WE 1998031900398 19980319 00398 WP 1998 3 19 ASAA9880028 1 19980215 A 5210 4928806503 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP L1 DOOR BENT A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 969AS 53063 ONT - FLT 595 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE. REPLACED THE DOOR HOLD OPEN HOOK AND OPE RATED NORMALLY. AIRCRAFT TT: 21,095 HOURS. AIRCRAFT TC: 10,731.(X) 2 L 7 2 4F RT A6WE 1998031900399 19980319 00399 WP 1998 3 19 ASAA9880034 1 19980223 A 5610 MECHANISM DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 937AS 49364 PDX - FLT 725 - AFTER ARRIVAL, CREW REPORTED THE FLIGHT COMPARTMENT LT SLIDING WINDOWS WERE DIFFICULT TO OPEN. ADJUSTED THE FLIGHT COMPARTMENT LT SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. AIRCRAFT TT: 35,988 HOURS. AIRCRAFT TC: 2 3,773. (X) 2 L 7 2 4F A6WE 1998031900400 19980319 00400 WP 1998 3 19 ASAA9880031 1 19980222 A 5240 MECHANISM DOUG DC9 DC983 3022083 WP SERVICE DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 SEA - FLT 601 - AFTER ARRIVAL, CREW REPORTED THE R1 DOOR WAS DIFFICULT TO OPEN AND CLOSE. LUBED THE R1 DOOR MECHANISM A ND OPERATED NORMALLY. AIRCRAFT TT: 23,499 HOURS. AIRCRAFT TC: 13,628. (X) 2 L 7 2 4F RT A6WE 1998031900401 19980319 00401 WP 1998 3 19 ASAA9880029 1 19980216 A 5210 5910081167 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 54199 ASA0033 48079 SEA - FLT 722 - AFTER ARRIVAL, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. FOUND THE L1 DOOR AND MECHANISM DAMAGED , POSSIBLE CONTACT BY JETWAY. REMOVED AND REPLACED THE L1 DOOR PER MM 52-11-00-4 AND MM 52-11-00-5, AND OPERATED NORMAL LY. PART TC: 28,996. (X) 2 L 7 2 4F A6WE 1998031900402 19980319 00402 WP 1998 3 19 ASAA9880030 1 19980220 A 2923 414470 HYDRAULIC PUMP VICKERS DOUG DC9 DC983 3022083 WP RT MLG WW FAILED A ASAA H DEACTIVATE SYST/CIRCUITS B K J SMOKE/FUMES/ODORS/SPARKS FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 01 943AS 16443 8698 MX380234 53018 SEA - FLT 570 - PRIOR TO DEPARTURE, CREW REPORTED ODOR AND FUMES IN CABIN. FOUND AUXILIARY HYDRAULIC PUMP LEAKING. REP LACED AUXILIARY HYDRAULIC PUMP, REPLACED RECIRCULATION FAN FILTER, CLEANED LOWER FUSELAGE AND ACCOMPLISHED PNEUMATIC DUC T BURN-OUT PROCEDURE. OPERATED AIR CONDITIONING SYSTEM AND NO ODOR NOTED. PART TC: 9,569. (X) 2 L 7 2 4F RT A6WE 1998031900403 19980319 00403 NM 1998 3 19 TSAA9833131 1 19980215 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND FORWARD DOOR EMERGENCY EXIT LIGHT INOPERABLE. REPLACED IDENTIFIER. OPS CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. TAT: 33,777:16 HOURS. TAC: 40,326. (X) 2 L 7 2 4F RT A16WE 1998031900405 19980319 00405 NM 1998 3 19 TSAA9833134 1 19980215 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 ON SERVICE CHECK FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,807:02 HOURS. TAC: 29,525. (X) 2 L 7 2 4F RT A16WE 1998031900406 19980319 00406 NM 1998 3 19 TSAA9833135 1 19980215 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. TAT: 28,807:02 HOURS. TAC: 29,525. (X) 2 L 7 2 4F RT A16WE 1998031900407 19980319 00407 NM 1998 3 19 TSAA9833136 1 19980215 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM PASSENGER CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. TAT: 28,807:02 HOURS. TAC: 29,525. (X) 2 L 7 2 4F RT A16WE 1998031900408 19980319 00408 NM 1998 3 19 TSAA9833137 1 19980216 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 DURING SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 32,706:08 HOURS. TAC: 61,407. (X) 2 L 7 2 4F RT A16WE 1998031900409 19980319 00409 NM 1998 3 19 TSAA9833138 1 19980216 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 DURING SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 32,706:08 HOURS. TAC: 61,407. (X) 2 L 7 2 4F RT A16WE 1998031900410 19980319 00410 NM 1998 3 19 TSAA9833139 1 19980216 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 DURING SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 32,706:08 HOURS. TAC: 61,407. (X) 2 L 7 2 4F RT A16WE 1998031900411 19980319 00411 NM 1998 3 19 TSAA9833140 1 19980216 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 DURING SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOPERABLE. AIRCRAFT RETURNED TO SERVICE. TAT: 32,706 :08 HOURS. TAC: 61,407. (X) 2 L 7 2 4F RT A16WE 1998031900412 19980319 00412 NM 1998 3 19 TSAA9833141 1 19980216 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. TAT: 44,483:42 HOURS. TAC: 57,958. (X) 2 L 7 2 4F A16WE 1998031900413 19980319 00413 NM 1998 3 19 TSAA9833142 1 19980216 A 3350 963100211 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 30,719:11 HOURS. TAC: 36,568. (X) 2 L 7 2 4F RT A16WE 1998031900414 19980319 00414 NM 1998 3 19 TSAA9833143 1 19980217 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. TAT: 39,502:35 HOURS. TAC: 50,012. (X) 2 L 7 2 4F RT A16WE 1998031900415 19980319 00415 NM 1998 3 19 TSAA9833126 1 19980212 A 3350 963100211 LIGHT BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED LIGHT ASSY AND BATTERY PACK. OPS CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 28,317:22 HOURS. TAC: 24,021. (X) 2 L 7 2 4F RT A16WE 1998031900416 19980319 00416 NM 1998 3 19 TSAA9833127 1 19980213 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. TAT: 44,466:22 HOURS. TAC: 57,918. (X) 2 L 7 2 4F A16WE 1998031900417 19980319 00417 NM 1998 3 19 TSAA9833128 1 19980213 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 DURING SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 32,688:40 HOURS. TAC: 61,367. (X) 2 L 7 2 4F RT A16WE 1998031900418 19980319 00418 NM 1998 3 19 TSAA9833129 1 19980213 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 DURING SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. TAT: 32,688:40 HOURS. TAC: 61,367. (X) 2 L 7 2 4F RT A16WE 1998031900419 19980319 00419 NM 1998 3 19 TSAA9851115 1 19980211 A 2920 RAM AIR INLET BOEING 737 737230C 1384472 NM RIGHT CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 DURING CPCP VISIT, FOUND CRACK AT RT RAM AIR DUCT INLET; LT CORNER AT RADIUS. REPAIRED CRACK PER SRM 51-40-00 AND INSTA LLED REPLACEMENT WEB. TAT: 35,050.9 HOURS. TAC: 39,058. (X) 2 L 7 2 4F A16WE 1998031900420 19980319 00420 NM 1998 3 19 TSAA9851114 1 19980211 A 2920 RAM AIR INLET BOEING 737 737230C 1384472 NM LEFT CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 DURING CPCP VISIT, FOUND CRACK AT LT RAM AIR DUCT INLET; RT CORNER AT RADIUS. REPAIRED CRACK PER SRM 51-40-00 AND INSTA LLED REPLACEMENT WEB. TAT: 35,050.9 HOURS. TAC: 39,058. (X) 2 L 7 2 4F A16WE 1998031900421 19980319 00421 NM 1998 3 19 TSAA9833116 1 19980210 A 5730 SKIN BOEING 737 7372Q9 138448M NM WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 DURING A CPC VISIT, CORROSION WAS FOUND ON THE OUTBOARD WING MAIN WING BOX LOWER SKIN. CORRECT REWORK ACCOMPLISHED PER ALOHA ECO 1684. AIRCRAFT RETURNED TO SERVICE. TAT: 46,314:38 HOURS. TAC: 59,862. (X) 2 L 7 2 4F A16WE 1998031900422 19980319 00422 NM 1998 3 19 TSAA9833118 1 19980210 A 5314 KEEL BEAM BOEING 737 7372Q9 138448M NM BS 727 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 809AL 21720 DURING A CPC VISIT, CORROSION WAS FOUND AT BS 727 KEEL BEAM AREA. REPAIR ACCOMPLISHED PER ALOHA ECO 2454. AIRCRAFT RET URNED TO SERVICE. TAT: 46,314:38 HOURS. TAC: 59,862. 2 L 7 2 4F A16WE 1998031900423 19980319 00423 NM 1998 3 19 TSAA9833130 1 19980215 A 2910 HYDRAULIC LINE BOEING 737 7372X6C 1384552 NM MLG FAILED A TSAA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 816AL 23122 FLT - 283 - PILOT REPORT ON TAXI OUT, AIRCRAFT LOST 'A' HYDRAULICS. UPON RETURN, REPLACED THE HYDRAULIC PRESSURE LINE O N THE MAIN LANDING GEAR ACTUATOR. SERVICED HYDRAULICS TO FULL AND CYCLED GEAR SEVERAL TIMES WITH GEAR PINS INSTALLED, N O LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. TAT: 30,711:25 HOURS. TAC: 36,561. (X) 2 L 7 2 4F RT A16WE 1998031900424 19980319 00424 NM 1998 3 19 TSAA9833144 1 19980219 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 DURING SERVICE CHECK, POSITIONS NR 1, NR 2, AND NR 3 EMERGENCY FLOOR LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PA CK FOR POSITION NR 1. ALL POSITIONS OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAC: 59,963. (X) 2 L 7 2 4F A16WE 1998031900426 19980319 00426 NM 1998 3 19 AALA980140 1 19980116 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON SHEAR TIE BETWEEN STR 28R AND STR 28L, AFT SIDE STA 700 FRAME. REMOVED OLD SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED PER SRM 53-10-4, PAGES 54-56, FIG 14, SHEETS 1-3. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900427 19980319 00427 NM 1998 3 19 AALA980154 1 19980116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - STR 29L, CORROSION FOUND AT STA 1166. INSTALLED STRINGER SPLICE PER SRM 53-10-3, PAGE 4B. TST: 56,192 HOURS. C YCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900428 19980319 00428 NM 1998 3 19 AALA980153 1 19980116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - SKIN BULGED AND FASTENER HEADS DISHED AT STA 1148 AND STR 26L. INSTALLED STRINGER SPLICE AT STR 26L AND STA 1148 PER SRM 53-10-3, PAGES 3-4B. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900429 19980319 00429 NM 1998 3 19 AALA980152 1 19980116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION AT FASTENER OUTBOARD FLANGE STR 28L STA 720F + 15 INCHES. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 1-2-98. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900430 19980319 00430 NM 1998 3 19 AALA980151 1 19980116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 688 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION IN STR 28R STA 688 - STA 692. INSTALLED NEW SECTION OF STR AT HAT CHANNEL PER SRM 53-10-3 PAGES 1 AND 2 , ESO 11647 DATED 1-8-98. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900431 19980319 00431 NM 1998 3 19 AALA980150 1 19980116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - FLOORBEAM UPPER CHORD CORRODED FROM LBL 10 TO LBL 14. REMOVED CORROSION PER SRM 51-10-06. CUT AND REMOVED DAMAGE D SECTION OF FLOORBEAM. ALODINED AND PRIMED, INSTALLED DOUBLER PER SRM 53-10-8. FIGURES 1-4. TST: 56,187 HOURS. CYCL ES: 34,681. (X) 2 L 7 3 4F A3WE 1998031900432 19980319 00432 NM 1998 3 19 AALA980149 1 19980116 A 5321 FLOORBOARD BOEING 727 727223 1384074 NM BS 1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON BOTTOM OF TOP FLANGE OF FLOORBOARD STA 1110, LBL 27 TO LBL 30. REMOVED CORROSION ON BOTTOM SIDE OF F LOORBOARD STA 1110 LBL 27 TO LBL 30 PER SRM 51-10-6. CUT AND REMOVED SECTION OF FLOORBOARD HAT WAS BEYOND LIMITS, ALODI NED AND PRIMED AREA. INSTALLED DOUBLER PER SRM 53-10-8. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900433 19980319 00433 NM 1998 3 19 AALA980148 1 19980116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 685 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - SKIN CORRODED OUTBOARD OF STR 28L. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3A. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900434 19980319 00434 NM 1998 3 19 AALA980147 1 19980116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON FLOORBEAM AT STA 380 FROM RBL 45 TO RBL 65. REMOVED CORRODED SECTION AND INSTALLED NEW PART AND DOUB LER PER SRM 53-10-8. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900435 19980319 00435 NM 1998 3 19 AALA980145 1 19980116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON TOP OF FLOORBEAM LBL 42 - RBL 25 STA 344. REMOVED AND REPLACED UPPER 'T' CAP OF FLOORBEAM STA 344 LB L 32 - RBL 60. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900436 19980319 00436 NM 1998 3 19 AALA980272 1 19980204 A 5330 SKIN BOEING 727 727223 1384074 NM BS 303 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FUSELAGE SKIN CRACKED AT FORWARD ENTRY DOOR LOWER HINGE CUT-OUT. INSTALLED REPAIR DOUBLER PER SB 727-53-0198. TS T: 48,140 HOURS. CYCLES: 23,835. (X) 2 L 7 3 4F A3WE 1998031900437 19980319 00437 WP 1998 3 19 AALA980404 1 19980224 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 234AA 49181 TUL - NR 5 SEAT TRACK CORRODED STA 200 - STA 202 AND STA 218. BLENDED CORROSION BEYOND LIMITS. REMOVED AND REPLACED NR 5 SEAT TRACK STA 200 - STA 218 PER SRM 51-30. TST: 44,152 HOURS. CYCLES: 24,579. (X) 2 L 7 2 4F A6WE 1998031900438 19980319 00438 NM 1998 3 19 AALA980328 1 19980217 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 843AA 20984 TUL - STA 580 ABOVE STR 27L - BULGE IN SKIN. REMOVED/REPLACED SHEAR TIE, SRM 51-10-1. TST: 58,400 HOURS. CYCLES: 37 ,776. (X) 2 L 7 3 4F A3WE 1998031900439 19980319 00439 NM 1998 3 19 AALA980311 1 19980212 A 5330 SKIN BOEING 727 727223 1384074 NM BS 512 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 843AA 20984 TUL - SKIN BULGED STA 512 AT STR 27R. INSTALLED SKIN REPAIR PER SRM 53-30-3 FIG 3 AND INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 7. TST: 58,400 HOURS. CYCLES: 37,776. (X) 2 L 7 3 4F A3WE 1998031900440 19980319 00440 NM 1998 3 19 AALA980310 1 19980212 A 5330 SKIN BOEING 727 727223 1384074 NM BS 513 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION ON SKIN STA 513 INBOARD SIDE OF STR 26R. INSTALLED EXTERNAL DOUBLER 10 INCHES BY 12 INCHES PER SRM 53-3 0-3. TST: 54,870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998031900441 19980319 00441 NM 1998 3 19 AALA980309 1 19980212 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION ON TOP OF FLOORBEAM AND EXTENDING UNDER LAVATORY FLOOR PAN. REPAIRED FLOORBEAM AT STA 1130 RBL 20 TO RB L 26 PER ESO 11697 DATED 2-6-98. TST: 54,870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998031900442 19980319 00442 NM 1998 3 19 AALA980143 1 19980116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON FLOORBEAM FROM RBL 24 TO RBL 45 AT STA 380. REMOVED CORRODED SECTION, INSTALLED NEW PART AND DOUBLER PER SRM 53-10-8. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900443 19980319 00443 NM 1998 3 19 AALA980142 1 19980116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON TOP AND BOTTOM OF FLOORBEAM AND CRACK IN FLOORBEAM STA 344, LBL 36 APPROXIMATELY. REMOVED AND REPLAC ED FLOORBEAM CAP AT STA 344 FROM LBL 34 THROUGH RBL 67 PER ESO 11697 DATED 12-15-97. TST: 56,192 HOURS. CYCLES: 34,6 65. (X) 2 L 7 3 4F A3WE 1998031900444 19980319 00444 NM 1998 3 19 AALA980141 1 19980116 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON SHEAR TIE AFT SIDE OF STA 720A ABOVE STR 26R. REMOVED AND REPLACED SHEAR TIE AT STA 720A ABOVE STR 2 6R PER SRM 51-10-1. TST: 56,192. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900445 19980319 00445 NM 1998 3 19 AALA980168 1 19980116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - LOWER SIDE OF UPPER FLANGE HAS CORROSION AROUND FASTENER HOLE. FLOORBEAM STA 480, BL ZERO. INSTALLED STRAP REPAI R ON FLOORBEAM PER AARD 52-10-7-2. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900446 19980319 00446 NM 1998 3 19 AALA980167 1 19980116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - SKIN BULDGED AND FASTENER HEADS DISHED STA 480 STR 26R. INSTALLED DOUBLER REPAIR ON STR FORWARD AND AFT OF STA 48 0. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900447 19980319 00447 NM 1998 3 19 AALA980166 1 19980116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1270 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - BELL FRAME CRACKED AT STR 19R ATTACH INSIDE RT LOWER TORQUE BOX AT STA 1270. STOP DRILLED CRACKS AND FABRICATED A ND INSTALLED DOUBLER PER SRM 57-10-21. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900448 19980319 00448 NM 1998 3 19 AALA980165 1 19980116 A 5532 SKIN BOEING 727 727223 1384074 NM V STAB BS 1213 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - VISUAL INDICATION OF CRACK ON VERTICAL STABILIZER SKIN RT SIDE AT FRONT SPAR WHERE STABILIZER AND FUSELAGE MEET. S TOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER ESO 11697 DATED 6-23-95. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900449 19980319 00449 NM 1998 3 19 AALA980164 1 19980116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - BELL FRAMES DENTED AND CRACKED STA 1090 STR 27R, STA 1090 STR 27L 950B, STR 26L 1050, STR 27L 1050, STR 27R 1070, STR 27L 1110, STR 26R 1110, STR 26L 1030, STR 27L 1030, STR 27R. DOUBLERS INSTALLED PER SRM 53-10-4 PAGES 3-6. TST: 5 6,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900450 19980319 00450 NM 1998 3 19 AALA980163 1 19980116 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 686 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - STRINGER CRACKED AT WS 686.50, SECOND RIB FORWARD OF AFT SPAR, RT WING. INSTALLED DOUBLER REPAIR PER SB 727-57A 1 59. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900452 19980319 00452 NM 1998 3 19 AALA980161 1 19980116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 910 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - STA 910 BOTTOM SIDE OF STR 18A LT BADLY GOUGED. INSTALLED STRAP PER ESO 11697 DATED 1-5-98. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900453 19980319 00453 WP 1998 3 19 AALA980282 1 19980224 A 2150 ACM DOUG DC9 DC982 3022082 WP ACM BAY DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 228AA 1142556 49178 DFW - FLT 2076 - IAH-DFW - SHORTLY AFTER TAKEOFF A BURNING SMELL LIKE A DIRTY PACK SOCK WAS IN COCKPIT AND AFT CABIN. C AIBN FROM MID TO AFT HAD A HAZE IN IT. HAZE AND SMELL QUICKLY DISSIPATED. APU WAS OFF. NO FURTHER SMELL OR HAZE FOR R EST OF FLIGHT. LANDED DFW WITHOUT INCIDENT. REPLACED BOTH LEFT AND RIGHT ACMS AND PRIMARY AND SECONDARY HEAT EXCHANGER S. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900454 19980319 00454 NM 1998 3 19 AALA0175 1 19980119 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION INSIDE STR 28R STA 990. BLENDED OUT CORROSION AND INSTALLED STRAP DOUBLER REPAIR PER ESO 11697 DATED 1- 19-98. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998031900455 19980319 00455 NM 1998 3 19 AALA980208 1 19980119 A 5330 SKIN BOEING 727 727223 1384074 NM BS 310 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 865AA 21370 TUL - SKIN CRACKED AT FOWARD ENTRY DOOR LOWER HINGE CUT OUT. CUT OUT CRACK, INSTALLED FILLERS AND DOUBLER IAW SB 727-53 -0198. TST: 57,178 HOURS. CYCLES: 35,293. (X) 2 L 7 3 4F A3WE 1998031900456 19980319 00456 NM 1998 3 19 AALA980287 1 19980209 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - STR 25L CORRODED AFT OF 720F. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3 PAGES 1-11. TST: 51,688 HOURS. C YCLES: 31,372. 9X) 2 L 7 3 4F A3WE 1998031900457 19980319 00457 NM 1998 3 19 AALA980286 1 19980209 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION ON FLOORBEAM AT BS 1130 RBL 25. REMOVED CORROSION, INSTALLED REPAIR STRAP ON TOP OF FLOORBEAM PER ESO 1 1697 DATED 2-4-98 AND AARD 53-10-07-1. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900458 19980319 00458 NM 1998 3 19 AALA980285 1 19980209 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION ON STR 24R AT STA 1166. REMOVED CORRODED STRINGER SECTION AND REPAIRED WITH STRINGER SPLICE AND DOUBLER PER SRM 53-10-3 PAGES 3-4B. TST: 51,688.24 HOURS. CYCLES: 31,370. (X) 2 L 7 3 4F A3WE 1998031900459 19980319 00459 NM 1998 3 19 AALA980284 1 19980209 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1053 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - STA 1053 TO STA 1063, STR 30, SKIN BULGING (AS SEEN FROM OUTSIDE). CUT OUT EXISTING DAMAGE ON SKIN (ALL CORROSION REMOVED). REMOVED LIGHT CORROSION ON STRINGER, INSTALLED REPAIR DOUBLER PER SRM 53-30-3 PAGE 14. TST: 51,688.24 HOUR S. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900460 19980319 00460 NM 1998 3 19 AALA0283 1 19980209 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1140 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION INSIDE STR 25R AT FS 1145. INSTALLED STRINGER SPLICE REPAIR (STA 1140 TO STA 1158) PER SRM 53-10-3. TS T: 51,688.24 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900461 19980319 00461 NM 1998 3 19 AALA980289 1 19980209 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 804 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - BELL FRAME CRACKED AT OUTBOARD SIDE CHORD ANGLE AT RIVET ATTACH POINT TO STR 14R. REPLACED FAILSAFE CHORD ANGLE A TTACHED TO OUTBOARD SIDE OF BELL FRAME FRM STR 13R TO TOP OF FUEL TANK PER SRM 51-10-1. TST: 51,688 HOURS. CYCLES: 3 1,372. (X) 2 L 7 3 4F A3WE 1998031900462 19980319 00462 NM 1998 3 19 AALA980288 1 19980209 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION AROUND CLIP NUTS ON BOTTOM FLANGE OF FLOOR BEAM AT BS 1130 FROM ZERO BL TO LBL 45. REPAIRED FLOORBEAM S TA 1130, LBL ZERO TO LBL 45 AS OUTLINED IN SRM 51-10-6 AND ESO 11697 DATED 2-6-98. ALODINED, TREATED, AND PRIMED. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900463 19980319 00463 NM 1998 3 19 AALA980325 1 19980213 A 5330 SKIN BOEING 727 727223 1384074 NM BS 515 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - STA 515 - STA 520, SKIN CORRODED OUTBOARD OF STR 27L UNDER LEVELING COMPOUND. INSTALLED DOUBLER REPAIR 53-30-3 PG 105. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900464 19980319 00464 NM 1998 3 19 AALA980324 1 19980213 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - STR 15L CRACKED AFT OF WING ICE LIGHT FORWARD OF BS 720. REPAIRED STR 15L PER SRM 53-10-3. TST: 51,688 HOURS. C YCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900465 19980319 00465 NM 1998 3 19 AALA980323 1 19980213 A 5330 SKIN BOEING 727 727223 1384074 NM BS 992 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION OUTBOARD SIDE STR 28R AFT SIDE BS 992. REMOVED CORROSION PER SRM 51-20-0, REPAIRED EXTERNAL FUSELAGE SK IN PER SRM 53-30-3 PAGE 1. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900466 19980319 00466 NM 1998 3 19 AALA980321 1 19980213 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - STRINGER CRACKED IN RADIUS STR 4R STA 560. REPAIRED STR 4R BS 560 PER SRM 53-10-3 FIG 2. TST: 51,688 HOURS. CYC LES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900467 19980319 00467 NM 1998 3 19 AALA980322 1 19980213 A 5320 SILL BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION AROUND FASTENER HOLE OF DOOR SILL AREA OUTBOARD OF STR 27R AT FS 950E +8. REMOVED CORROSION AROUND FAST ENER HOLE PER SRM 51-10-6. REPAIRED DAMAGE PER ESO 11697 DATED 2-3-98. TST: 51,688.24 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900468 19980319 00468 NM 1998 3 19 AALA980355 1 19980218 A 5711 SPAR BOEING 727 727223 1384074 NM WS 358 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - HEAVY CORROSION ON LOWER FRONT SPAR CHORD FROM FSS 358 - FSS 370 ON BOTTOM OF CHORD RT WING. REMOVED CORROSION, T REATED AND PRIMED. INSTALLED DOUBLER REPAIR PER B727 AARD/DC 57-30-00-2. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900469 19980319 00469 NM 1998 3 19 AALA980356 1 19980218 A 5330 SKIN BOEING 727 727223 1384074 NM BS 500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - FUSELAGE SKIN CORRODED ABOVE STR 27L AFT OF STA 500 THROUGH TO EXTERIOR OF SKIN. CUT OUT DAMAGED AREA AND INSTALL ED DOUBLER PER SRM 53-30-3. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900470 19980319 00470 NM 1998 3 19 AALA980357 1 19980218 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION ON BOTTOM OF SHEAR TIE ABOVE STR 26L AT FS 950E. INSTALLED NEW SHEAR TIE PER SRM 51-10-1. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998031900474 19980319 00474 NM 1998 3 19 AALA980349 1 19980217 A 5720 STIFFENER BOEING 727 727223 1384074 NM WS 230 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - VERTICAL STIFFENER CORRODED RT WING FRONT SPAR STA 230. (ABOVE NR 5 L/E FLAP ACTUATOR.) REMOVED AND REPLACED COR RODED VERTICAL STIFFENER AT STA 230 ABOVE NR 5 L/E FLAP ACTUATOR. PRIMED, PAINTED, AND SEALED IAW SRM 53-10-01. TST: 4 9,071 HOURS. CYCLES: 24,653. (X) 2 L 7 3 4F A3WE 1998031900475 19980319 00475 NM 1998 3 19 AALA980358 1 19980218 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 303 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 893AA 22009 TUL - FORWARD ENTRY DOOR SILL INBOARD CHORD ANGLE HORIZONTAL AND VERTICAL FLANGES HAVE INTERGRANULAR CORROSION. INSTAL LED NEW CHORD ANGLE STA 303 - STA 460. TST: 49,071 HOURS. CYCLES: 24,653. (X) 2 L 7 3 4F A3WE 1998031900476 19980319 00476 NM 1998 3 19 AALA980185 1 19980120 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 594 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - STR 28L CORRODED INSIDE HAT SECTION STA 594 TO STA 596. REMOVED CORRODED SECTION OF STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998031900477 19980319 00477 NM 1998 3 19 AALA980184 1 19980120 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - OUTBOARD FLANGE OF STR 29L HAS CORROSION. INSTALLED REPAIR PER ESO 11697 DATED 1-13-98. TST: 54,792. CYCLES: 3 3,779. (X) 2 L 7 3 4F A3WE 1998031900478 19980319 00478 NM 1998 3 19 AALA980223 1 19980127 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 595 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - STR 28L CORROSION INSIDE HAT SECTION STA 595. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B AT STA 595 STR 28 L. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998031900479 19980319 00479 NM 1998 3 19 AALA980222 1 19980127 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - OUTBOARD FLANGE OF STR 29L HAS CORROSION. INSTALLED REPAIR PER ESO 11697 DATED 1-13-98. TST: 54,792 HOURS. CYC LES: 33,779. (X) 2 L 7 3 4F A3WE 1998031900480 19980319 00480 NM 1998 3 19 AALA980221 1 19980127 A 5711 SPAR BOEING 727 727223 1384074 NM WS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON BOTTOM FLANGE OF FRONT SPAR CHORD ANGLE OUTBOARD OF NR 1 SLAT INBOARD TRACK OPENING. REMOVED CORROSI ON, INSTALLED REPAIR STRAP PER ESO 11697 DATED 1-10-98. (X) 2 L 7 3 4F A3WE 1998031900481 19980319 00481 NM 1998 3 19 AALA980291 1 19980209 A 5311 FRAME BOEING 727 727223 1384074 NM BS 970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - STA 970 FRAME AND SHEAR TIE CORRODED BETWEEN STR 29R AND STR 36. INSTALLED DOUBLER PER SRM 53-10-4 FIG 12. TST: 46,991 HOURS. CYCLES: 24,531. (X) 2 L 7 3 4F A3WE 1998031900482 19980319 00482 NM 1998 3 19 AALA980290 1 19980209 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - CORROSION AT STR 29L AT STA 971. REMOVED CORROSION PER SRM 51-10-6. TREATED AND PRIMED PER 51-10-6. ACCOMPLISHE D REPAIR PER ECO 11697 DATED 2-2-98. TST: 46,991. CYCLES: 24,531. (X) 2 L 7 3 4F A3WE 1998031900483 19980319 00483 NM 1998 3 19 AALA980230 1 19980128 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - CORROSION INSIDE STR 17R STA 560 - STA 563 INBOARD SIDE. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED STRIN GER REPAIR SPLICE IAW SRM 53-10-3 FIG 1. TST: 48,697 HOURS. CYCLES: 24,206. (X) 2 L 7 3 4F A3WE 1998031900484 19980319 00484 NM 1998 3 19 AALA980302 1 19980211 A 5320 WEB BOEING 727 727223 1384074 NM BS 826 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - THREE INCH CRACK AT AFT WEB TO CENTER TANK. STOP DRILLED, BUT NO REPAIR STA 826. STOP DRILLED AND INSTALLED DOUB LER PER SRM 57-10-6 PAGES 1-4. TST: 54,870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998031900599 19980319 00599 NM 1998 3 19 MALA976041 1 19980312 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DURING INSPECTION, EMERGENCY LIGHTS WILL NOT SHUT OFF WHEN SELECTED. MAINTENANCE REPLACED EMERGENCY LIGHT CONTROL BOX, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998031900600 19980319 00600 EU 1998 3 19 MALA976042 1 19980309 A 5270 SWITCH SAAB SF340 SF340A 7850100 EU PAX DOOR LACK OF LUBE A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 98XJ 098 AFTER DEPARTURE, MAIN CABIN DOOR HANDLE LIGHT ILLUMINATED ALONG WITH DOORS LIGHT. PERFORMED QRH, MADE A VISUAL CHECK OF DOOR INDEXES, TOP INDEX WAS ALIGNED, BOTTOM INDEX WAS NOT. FOLLOWED QRH, DECLARED EMERGENCY AND RETURNED TO CAK, LANDE D WITH OUT FURTHER PROBLEMS. MAINTENANCE CLEANED AND LUBED DOOR PINS AND MICROSWITCHES. PERFORMED SWITCH CHECK IN ACCO RDANCE WITH 52-70-00 OF MAINTENANCE MANUAL. ALL CHECKS SATISFACTORY ON SWITCHES, LIGHTS, AND ALIGNMENT MARKS LINE UP. 2 L 7 2 4T RT A52EU 1998031900601 19980319 00601 EU 1998 3 19 MALA976043 1 19980311 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 DURING INSPECTION, OVERHEAD LIGHTS INOP AT SEATS 2A, 6 C/D, AND 8 C/D. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998031900602 19980319 00602 EU 1998 3 19 MALA976044 1 19980308 A 5330 SKIN SAAB SF340 SF340A 7850100 EU BS 313 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 119 DURING HEAVY CHECK 4000 HOUR, DENTS ON FUSELAGE SKIN UNDER ICE SHIELD BEYOND LIMITS, STA 312.0 BETWEEN WL 84.0 AND 82.0 AND STA 313.0 BETWEEN WL 73.0 AND 71.0. REMOVED ICE SHIELDS FROM STA 308 TO STA 348 AND FROM WL 90 TO WL 67.5. REMOVED DAMAGED AREAS FROM FUSELAGE SKIN, FABRICATED AND INSTALL REPAIR DOUBLER AND FAY SEALED IAW SAAB 340 SRM 53-70-10 PG 201 -203, 53-70-10 PAGE 221 FIGURE 213. DAMAGE IS ON RIGHT SIDE OF AIRCRAFT. 2 L 7 2 4T RT A52EU 1998031900603 19980319 00603 EU 1998 3 19 MALA976045 1 19980309 A 5330 SKIN SAAB SF340 SF340A 7850100 EU BS 677 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 119XJ 119 DURING HEAVY CHECK 4000 HOUR, MAINTENANCE LOCATED DENT IN RIGHT SIDE OF FUSELAGE AT STA 677 AT WL 96, NOT WITHIN LIMITS IAW SAAB 340 SRM 51-10-10 FIGURE 10. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SAAB 340 SRM 53-80-10 PAGE 203 AND 204. 2 L 7 2 4T RT A52EU 1998031900604 19980319 00604 EU 1998 3 19 MALA976046 1 19980312 A 3350 7239410802 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 109XJ 340A109 DURING INSPECTION, FLOOR TRACK EMERGECNY LIGHT AT 4C INOP. MAINTENANCE RELAMPED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998031900605 19980319 00605 NM 1998 3 19 K3HA980037 1 19980312 A 3350 3071BPEGPL LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 FLOOR LIGHT OUT ACROSS FROM FORWARD GALLEY. RELAMPED FLOOR LIGHT (EMERGENCY E-PATH) REF 33-59-00, OPS CHECK OK. 2 L 7 3 4F A3WE 1998031900606 19980319 00606 NM 1998 3 19 K3HA980038 1 19980314 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CARGO COMPT DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 AFT CARGO DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED AFT CARGO DOOR BATTERY PACK REF MM 33-50-22, OP CHECK OK. 2 L 7 3 4F A3WE 1998031900607 19980319 00607 WP 1998 3 19 IXXA9800017 1 19980312 A 7110 COWL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE LT ENGINE DAMAGED A IXXA K NONE O OTHER LD LANDING 1 GL 23 828BX 31700 3672 45993 692334 DURING LANDING, THE NUMBER ONE ENGINE SUSTAINED A GROUND STRIKE WITH MINOR DAMAGE TO THE FORWARD FAN COWLINGS, DRAIN MAS T AND THE ACCESSORY GEARBOX COVER. A MANUFACTURER SUPPORT TEAM WAS CALLED IN TO PERFORM AN ENGINE BORESCOPE AND GEARBOX FPI INSPECTION, WHICH REVEALED NO DISCREPANCIES. A MAX POWER ASSURANCE CHECK WAS ACCOMPLISHED. RECOMMENDED CHIP DETEC TOR INSPECTION EVERY FIFTY HOURS FOR THE NEXT TWO HUNDRED HOURS WAS SCHEDULED. THE AIRCRAFT IS WILL RETURN TO SERVICE F OLLLOWING FAN COWL REPLACEMENT. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998031900608 19980319 00608 NM 1998 3 19 CALA9800427 1 19980313 A 5530 STRINGERS BOEING 727 727243 138408D NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 6 RT NR 3 STRINGER AND NR 5 STRINGER CRACKED 1 BEHIND ATTAC H BOLT. REMOVED FASTENERS IAW SRM 51-30-2. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5 . 2 L 7 3 4F RT A3WE 1998031900609 19980319 00609 NM 1998 3 19 CALA9800428 1 19980313 A 5530 STRINGER BOEING 727 727243 138408D NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND VERTICAL STABILIZER INTERNAL COMPARTMENT NR 9 RT NR 3 STRINGER CRACKED 1 BEHIND ATTACH BOLT. REMOVED F ASTENERS IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-2, AND 51-40-5. 2 L 7 3 4F RT A3WE 1998031900610 19980319 00610 NM 1998 3 19 CALA9800429 1 19980313 A 5520 HINGE BOEING 727 727243 138408D NM RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR BALANCE PANEL NR 9214 FORWARD HINGE. THE HINGE WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F RT A3WE 1998031900611 19980319 00611 NM 1998 3 19 CALA9800430 1 19980313 A 5755 ANGLE BOEING 727 727243 138408D NM NR 7 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A .5 INCH CRACK IN FALSE SPAR LOWER ANGLE BELOW AND INBOARD OF NR 7 SPOILER ACTUATOR INBOARD COVE AREA. REPAIRED FALSE SPAR LOWER ANGLE IAW EA NR 26865-5182 AND REINSTALLED ADJACENT STRUCTURE IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998031900612 19980319 00612 NM 1998 3 19 CALA9800431 1 19980313 A 5755 SKIN BOEING 727 727243 138408D NM NR 2 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A .0937 INCH CRACK AT LT WING UPPER SKIN CUTOUT FOR NR 2 SPOILER. THE FASTENERS WERE REMOVED AND A DOU BLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, 51-10-2, AND 57-30-2. 2 L 7 3 4F RT A3WE 1998031900613 19980319 00613 NM 1998 3 19 CALA9800432 1 19980313 A 5320 ANGLE BOEING 727 727243 138408D NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL UPPER SUPPORT ANGLE BETWEEN FLOORBEAM SUPPORT, STA 720 AND 720A. THE INT ERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998031900614 19980319 00614 NM 1998 3 19 CALA9800433 1 19980313 A 5330 SKIN BOEING 727 727243 138408D NM BS 1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND CORROSION IN SKIN ATTACH LEG AT FORWARD SIDE OF CIRCUMFERENTIAL, BS 1148, STRINGER 28L AND 29L. THE CO RROSION WAS CUT OUT IAW SRM 51-10-6. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-6. 2 L 7 3 4F RT A3WE 1998031900615 19980319 00615 NM 1998 3 19 CALA9800434 1 19980313 A 5320 ANGLE BOEING 727 727243 138408D NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 1.6 INCH CRACK AT BOTTOM OF LEFT CURVED SIDEWALL SUPPORT ANGLE MOUNTED TO FORWARD SIDE OF CIRCUMFEREN TIAL STA 950D. A NEW SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-3. 2 L 7 3 4F RT A3WE 1998031900616 19980319 00616 NM 1998 3 19 CALA9800435 1 19980313 A 5753 6521630174 SKIN BOEING 727 727243 138408D NM RT TE FOREFLAP DISBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND RT TRAILING EDGE INBOARD FOREFLAP DISBONDED IN TWO AREAS. THE FOREFLAP WAS REMOVED AND REPLACED. 2 L 7 3 4F RT A3WE 1998031900617 19980319 00617 NM 1998 3 19 CALA9800436 1 19980313 A 5754 BRACKET BOEING 727 727243 138408D NM NR 1 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 1 SLAT LOWER LEADING EDGE SKIN TO INBOARD TRACK ATTACH BRACKET. THE BRACK ET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998031900618 19980319 00618 NM 1998 3 19 CALA9800437 1 19980313 A 5720 ANGLE BOEING 727 727243 138408D NM WS 330 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A .5 INCH CRACK THROUGH AFT FASTENER HOLE AT REPAIR ANGLE INSIDE LT WING LEADING EDGE RIB, WS 330, AFT OF NR 4 SLAT, INBOARD END. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6. 2 L 7 3 4F RT A3WE 1998031900619 19980319 00619 NM 1998 3 19 CALA9800438 1 19980313 A 5720 BRACKET BOEING 727 727243 138408D NM LT MLG BEAM CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 2 INCH CRACK IN BRACKET AT AFT FACE OF LT GEAR BEAM WHERE HYDRAULIC LINES PASS THROUGH ACCESS DOOR 84 05. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 51-10-2, AND 51-30-2. 2 L 7 3 4F RT A3WE 1998031900620 19980319 00620 NM 1998 3 19 CALA9800439 1 19980313 A 5720 SPLICE BOEING 727 727243 138408D NM WS 224 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 3 INCH CRACK AT SPLICE PLATE ON LOWER SURFACE OF LT WING UPPER LEADING EDGE SKIN DIRECTLY ABOVE NR 2 LEADING EDGE FLAP ACTUATOR, FSS 224. THE SPLICE PLATE WAS CUT OUT, A NEW PLATE WAS FABRICATED AND INSTALLED IAW SRM 51- 40-2 AND 51-10-2. 2 L 7 3 4F RT A3WE 1998031900621 19980319 00621 NM 1998 3 19 CALA9800440 1 19980313 A 5754 SKIN BOEING 727 727243 138408D NM NR 2 SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A DENT 19.5 INCHES FROM OUTBOARD END IN LT WING NR 2 LEADING EDGE SLAT UPPER SKIN. A REPAIR WAS INSTAL LED IAW SRM 57-50-3. 2 L 7 3 4F RT A3WE 1998031900622 19980319 00622 NM 1998 3 19 CALA9800441 1 19980313 A 5730 SKIN BOEING 727 727243 138408D NM NR 3 SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A .375 INCH CRACK IN LT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT OUTBOARD TRACK AREA. A SKIN FLU SH REPAIR WAS INSTALLED IAW SRM 57-30-4. 2 L 7 3 4F RT A3WE 1998031900623 19980319 00623 NM 1998 3 19 CALA9800442 1 19980313 A 5751 SKIN BOEING 727 727243 138408D NM LT AILERON DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND LT OUTBOARD AILERON OUTBOARD UPPER TRAILING EDGE HAD A PREVIOUSLY FILLED SMALL DENT WITH FILLER BREAKIN G OUT. THE DENTED AREA WAS CUT OUT AND A HOT BONDED REPAIR WAS INSTALLED IAW SRM 51-40-6. 2 L 7 3 4F RT A3WE 1998031900624 19980319 00624 NM 1998 3 19 9804266306 1 19980313 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51HJK TO 66HJK. RECONNECTED ELECTRICAL PIN, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998031900625 19980319 00625 WP 1998 3 19 9804279302 1 19980314 A 8012 39279621 START VALVE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 302RC 36010 13377 48055 708407 DURING CRUISE AT 20,000 FEET, THE RIGHT ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW SHUT DOWN THE RIGHT ENGINE, DIV ERTED TO RST, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE START VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E9NE 1998031900626 19980319 00626 WP 1998 3 19 9804289611 1 19980312 A 3260 RETRACT MECH DOUG DC9 DC932 3022066 WP LANDING GEAR LACK OF LUBE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 611NA 47435 DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR AND NOSE GEAR UNSAFE LIGTHS REMAINED ON AFTER GEAR RETRACTION. CREW RECYCL ED GEAR WITH SAME RESULTS. FLIGHT WAS CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPER ATION OF ALL GEARS. DISCREPANCY COULD NOT BE DUPLICATED. LUBRICATED ALL MAIN GEAR PIVOT POINTS AS A PRECAUTION. 2 L 7 2 4F A6WE 1998031900627 19980319 00627 WP 1998 3 19 9804299854 1 19980311 A 3231 591078387 MECHANISM DOUG DC9 DC951 3022051 WP LT MLG DOOR OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 763NC 7528 47716 LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED AND RIGGED LEFT MAIN GEAR DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998031900628 19980319 00628 WP 1998 3 19 9804309935 1 19980314 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1332U 47404 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT AFT FLIGHT ATTENDANT JUMPSEAT AND AT CATWALK SIDEWALLS INO PERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900629 19980319 00629 WP 1998 3 19 9804319991 1 19980313 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8957E 47215 DURING LINE MAINTENANCE INSPECTION, FOUND FLASHLIGHT AT FORWARD FLIGHT ATTENDANT JUMPSEAT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900630 19980319 00630 WP 1998 3 19 9804329608 1 19980314 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 608NW 47233 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTS BETWEEN ROWS 11 THRU 13 INOPERATIVE. REPLACED BA TTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900631 19980319 00631 WP 1998 3 19 9804339608 1 19980313 A 3350 CONNECTION DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 608NW 47233 DURING PERIODIC CHECK, FOUND EMERGNECY LIGHTS BETWEEN ROWS 11 THRU 13 INOPERATIVE. TIGHTENED CONNECTION UNDER SEATS, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900632 19980319 00632 WP 1998 3 19 9804349615 1 19980314 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 615NW 47129 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHTS INOPERATIVE. REPLACED BAT TERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900633 19980319 00633 WP 1998 3 19 9804359995 1 19980310 A 3240 CHECK VALVE DOUG DC9 DC931 3022065 WP LT BRAKE FAILED A NWAA D RETURN TO BLOCK P NO WARNING INDICATION TX TAXI/GRND HDL 1 GL 01 8978E 47327 BRAKES LOCKED UP DURING TAXI. MAINTENANCE REPLACED CHECK VALVE AT LEFT BRAKE CONTROL VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900634 19980319 00634 WP 1998 3 19 9804369301 1 19980312 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 301RC 48054 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 24 THRU 29 INOPERATIVE. REPLACED BATTE RIES IN POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998031900635 19980319 00635 1998 3 19 9804379912 4 19980312 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP PAX DOOR FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 962N 5033 2559 47406 DURING PERIODIC CHECK, FOUND MAIN CABIN DOOR EVACUATION SLIDE BATTERY LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998031900636 19980319 00636 1998 3 19 9804389921 4 19980313 A 2565 13621228 SLIDE DOUG DC9 DC932 3022066 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 943N 39306 1757 47647 DURNG MAINTENANCE INSPECTION, FOUND TAIL CONE EVACUATION SLIDE BOTTLE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998031900637 19980319 00637 NM 1998 3 19 SWA980192 1 19980211 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED ON LT SIDE OF A/C BETWEEN NR 11 AND NR 12 PASSENGER WINDOWS AT BS 520. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900638 19980319 00638 NM 1998 3 19 SWA980193 1 19980211 A 5730 SKIN BOEING 737 7373T5 NM WS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED C-3 CHECK, FOUND CRACK INBD WS 213 BETWEEN KRUEGER FLAPS. REPAIRED PER SWA RA 1-357-0503. 2 L 7 2 4F RT A16WE 1998031900639 19980319 00639 NM 1998 3 19 SWA980194 1 19980210 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED LOWER AFT CORNER OF R1 DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900640 19980319 00640 NM 1998 3 19 SWA980195 1 19980210 A 3350 300432 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED RON CHECK, FOUND FWD EMERGENCY TRACK LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998031900641 19980319 00641 NM 1998 3 19 SWA980218 1 19980227 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND RT 18 A WEB AT BS 727 HAS CRACK AT I/B FASTENER HOLE. REPAIRED PER SWA RA 1-353-176 7. 2 L 7 2 4F RT A16WE 1998031900642 19980319 00642 NM 1998 3 19 SWA980219 1 19980301 A 2121 6454051 FAN BOEING 737 7373G7 1384595 NM AC BAY FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 RETURNED TO GATE DUE TO A SMOKE AND BURNING SMELL AT AFT CABIN AREA. INSPECTED AND FOUND SMELL COMING FROM RECIRCULATIN G FAN. REMOVED AND REPLACED RECIRCULATING FAN PER BOEING M/M. RETURNED TO GATE A SECOND TIME DUE TO A BURNING SMELL. R EMOVED AND REPLACED WATER SEPARATOR BAGS, AND LT AND RT HEPA FILTERS. RAN BOTH PACKS AND NR 2 ENGINE, NO DEFECTS NOTED . 2 L 7 2 4F RT A16WE 1998031900643 19980319 00643 NM 1998 3 19 SWA980220 1 19980227 A 5330 SKIN BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED C1 CHECK, FOUND UPPER HINGE CUTOUT HAS .25 INCH CRACK AT CORNER. REPAIRED PER SWA RA 1-353-1780. 2 L 7 2 4F RT A16WE 1998031900644 19980319 00644 NM 1998 3 19 SWA980221 1 19980228 A 5730 SKIN BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND .25 INCH CRACK AT L/E STATION 213, RT WING. REPAIRED PER SWA RA 1-357-0493. 2 L 7 2 4F RT A16WE 1998031900645 19980319 00645 NM 1998 3 19 SWA980222 1 19980228 A 5730 SKIN BOEING 737 7373H4 1384600 NM WS 213 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED SERVICE CHECK, FOUND 1/4 CRACK AT L/E STATION 213, LT WING. REPAIRED PER SWA RA 1-357-0493. 2 L 7 2 4F RT A16WE 1998031900646 19980319 00646 NM 1998 3 19 SWA980224 1 19980306 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 863 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN IS GOUGED AT BS 863, STR 1. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900647 19980319 00647 1998 3 19 SWA980225 4 19980309 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM CABIN LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 631SW 27706 DURING WALKAROUND CHECK, FOUND AFT SERVICE DOOR EMERGENCY SLIDE PRESSURE LOW. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998031900648 19980319 00648 NM 1998 3 19 SWA980226 1 19980309 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SERVICE CHECK, FOUND SKIN HAS A 2 DEGREE INCH CRACK AT FS 727A JUST BELOW STR 18L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998031900649 19980319 00649 NM 1998 3 19 SWA980227 1 19980310 A 5730 SKIN BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING TERMINAL CHECK, FOUND UPPER WING SKIN CRACKED AFT OF UPPER WING PANEL. REPAIRED PER SWA RA 1-257-0537. 2 L 7 2 4F A16WE 1998031900650 19980319 00650 NM 1998 3 19 SWA980228 1 19980310 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 980 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED RON CHECK, FOUND CRACK IN LT AFT FUSELAGE SKIN AT BS 980, STR 24. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998031900651 19980319 00651 NM 1998 3 19 SWA980229 1 19980310 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 722 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED TERMINAL CHECK, FOUND CRACK IN PRIOR REPAIR AT BS 722 BLEND TO CEILING ANGLE. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998031900652 19980319 00652 NM 1998 3 19 SWA980230 1 19980310 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EGRESS LIGHT AT AFT GALLEY DOOR FRAME IS INOP. REPLACED LIGHT ASSEMBLY PER B OEING MM. 2 L 7 2 4F A16WE 1998031900653 19980319 00653 NM 1998 3 19 SWA980231 1 19980310 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EGRESS LIGHT AT AFT ENTRY DOOR IS INOP. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998031900654 19980319 00654 NM 1998 3 19 SWA980232 1 19980310 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND CORROSION ON AFT BULKHEAD SUPPORT ANGLE AT BS 947.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900655 19980319 00655 NM 1998 3 19 SWA980233 1 19980310 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 727D+5 TO 860, LBL 12.75. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900656 19980319 00656 NM 1998 3 19 SWA980234 1 19980310 A 5312 BULKHEAD PANEL BOEING 737 7373H4 1384600 NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND AT BS 727 BULKHEAD PANEL IS DAMAGED. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998031900657 19980319 00657 NM 1998 3 19 SWA980235 1 19980310 A 3233 WEB BOEING 737 7373H4 1384600 NM BS 248 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND NLG RETRACT ACTUATOR SUPPORT BEAM HAS CRACKED WEB AT BS 248. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998031900658 19980319 00658 NM 1998 3 19 SWA980236 1 19980310 A 5330 PANEL BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED C4 CHECK, FOUND LWR FUSELAGE FIXED PANEL BELOW KEEL BEAM CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900659 19980319 00659 NM 1998 3 19 SWA980237 1 19980310 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 24408 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 727D+5 TO 860, LBL 7.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900660 19980319 00660 NM 1998 3 19 SWA980238 1 19980310 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 385 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED RON CHECK, FOUND DENT AT FUSELAGE RT SIDE BS 385. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900661 19980319 00661 NM 1998 3 19 SWA980239 1 19980311 A 2612 6937307153 CONTROL PNL BOEING 737 7373H4 1384600 NM COCKPIT MALFUNCTIONED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 361SW 26572 IN POSITION TO TAKEOFF, APU FIRE WARNING CAME ON. PULLED APU FIRE WARNING SWITCH. EMERGENCY FIRE TRUCK ESCORTED TO GAT E. NO FIRE EVIDENT. APU SWITCH OFF. INSPECTED AND FOUND NO EVIDENCE OF FIRE. REMOVED AND REPLACED FIRE WARNING CONTR OL PANEL AND APU BOTTLE AS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998031900662 19980319 00662 NM 1998 3 19 SWA980240 1 19980311 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 179, WL 208, RBL 28. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900663 19980319 00663 NM 1998 3 19 SWA980241 1 19980311 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 727D+5 RBL 3 WL 152. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900664 19980319 00664 NM 1998 3 19 SWA980242 1 19980311 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 1104 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CRACK IN FRAME AT BS 1104, RBL 10, 1 INCH O/B OF STRINGER 2R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900665 19980319 00665 NM 1998 3 19 SWA980243 1 19980311 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 1139 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND LOWER SPLICE STRAP AT BS 1139, WL 258, LBL 40 WAS CRACKED PASSED LIGHTENING HOLE ABOUT 1 .5 INCH FROM EDGE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900666 19980319 00666 NM 1998 3 19 SWA980244 1 19980311 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND UPON REMOVAL OF SIDE SKIN AT BS 907, CIRCUMFERENTIAL STRAP TO BE CRACKED AT 220R. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900667 19980319 00667 NM 1998 3 19 SWA980245 1 19980311 A 5314 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 706-727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND SEVEN WORKING FASTENERS IN KEEL BEAM LOWER FLANGE UPPER SURFACE AT BS 706 TO 727, RBL 7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900668 19980319 00668 NM 1998 3 19 SWA980246 1 19980311 A 5330 SKIN BOEING 737 7373H4 1384600 NM DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND AFT SERVICE DOORWAY UPPER HINGE CUTOUT FED UPPER CORNER HAS 3 INCH CRACK. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900669 19980319 00669 NM 1998 3 19 SWA980247 1 19980311 A 5247 DOOR BOEING 737 7373H4 1384600 NM BS 1121 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND APU DOOR OUTER SKIN DENTED AT BS 1121 WL 224 RBL 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900670 19980319 00670 NM 1998 3 19 SWA980248 1 19980311 A 5730 SKIN BOEING 737 7373H4 1384600 NM WINGS CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND BOOST PUMP CUTOUT UPPER SURFACE OF LOWER SKIN HAS CORROSION DAMAGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900671 19980319 00671 NM 1998 3 19 SWA980249 1 19980312 A 2910 B-NUT BOEING 737 737317 138447P NM AC BAY LEAK A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 698SW 23176 AFTER PUSH BACK FROM GATE, SMOKE FILLED CABIN AND COCKPIT IMMEDIATELY AFTER TURNING PACKS ON. RETURNED TO GATE, CLEARED CABIN AIR, INSPECTED AND CONTINUED PER MEL. AFTER TAKEOFF, CREW EXPERIENCED SMOKE IN THE CABIN AGAIN AIRCRAFT RETURN TO TUL AND MADE AN UNEVENFUL LANDING. RETORQUED B-NUT ON HYD FUSE ABOVE AFT HEAT EXCHANGER. REMOVED AND REPLACED WAT ER SEPARATOR AND BAGS. LEAK AND OPS CHECKED ALL PER BOEING MM. 2 L 7 2 4F RT A16WE 1998031900672 19980319 00672 NM 1998 3 19 SWA980251 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CRACKED AT HAT FITTING AT BS 727B, STR 8R AND 9R. REPAIRED PER TRAMCO EWO 98-0042. 2 L 7 2 4F RT A16WE 1998031900673 19980319 00673 NM 1998 3 19 SWA980252 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CRACKED AT HAT FITTING AT BS 787, STR 8L AND 9L. REPAIRED PER TRAMCO EWO 98-0042. 2 L 7 2 4F RT A16WE 1998031900674 19980319 00674 NM 1998 3 19 SWA980253 1 19980312 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 680 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED D 1/4 CHECK, FOUND LT WHEEL FRAME BS 680 HAS CRACK IN FRAME APPROX 65 FROM CENTER TO LBL JUST BELOW ROD ATTACH POINT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998031900675 19980319 00675 NM 1998 3 19 SWA980254 1 19980312 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM BS 1139 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND AT BS 1139 WL 262.5, LBL 35 FWD SIDE OF THE DOUBLER CRACKED. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998031900676 19980319 00676 NM 1998 3 19 SWA980255 1 19980312 A 5312 BULKHEAD SHROUD BOEING 737 7373H4 1384600 NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND AT BS 727 BULKHEAD CEILING TO BULKHEAD APU DUCT SHROUD DAMAGED. REPAIRED PER BOEING MM . 2 L 7 2 4F RT A16WE 1998031900677 19980319 00677 NM 1998 3 19 SWA980256 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND IS CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 500A, STR 8 TO 9 RT. REPAIRED PER BO EING PER SRM. 2 L 7 2 4F RT A16WE 1998031900678 19980319 00678 NM 1998 3 19 SWA980250 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FRAME IS CRACKED AT BS 400 BETWEEN STR 8 TO 9 LT. REPAIRED PER TRAMCO EWO 98-0042. 2 L 7 2 4F RT A16WE 1998031900679 19980319 00679 NM 1998 3 19 SWA980257 1 19980312 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 860, RBL 3, WL 154 ON FLOOR SUPPORT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900680 19980319 00680 NM 1998 3 19 SWA980258 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 747/787/827 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT FITTING AT BS 747 STR 8-9R, BS 787 STR 8-9R, BS 827 STR 8-9L, BS 82 7 STR 8-9R, BS 867 STR 8-9R, BS 747 STR 8-9L. REPAIRED PER TRAMCO 98-0042. 2 L 7 2 4F RT A16WE 1998031900681 19980319 00681 NM 1998 3 19 SWA980259 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 616 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 616, LBL 63, WL 200. REPAIRED PER SWA T1-A53-026. 2 L 7 2 4F RT A16WE 1998031900682 19980319 00682 NM 1998 3 19 SWA980260 1 19980312 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 435-400 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR/SIDEWALL SUPPORT AT BS 435 TO 400, RBL 24, WL 158.5. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998031900683 19980319 00683 NM 1998 3 19 SWA980261 1 19980312 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 969 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AND GOUGED AT BS 969, WL 188, LBL 64. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900684 19980319 00684 NM 1998 3 19 SWA980262 1 19980312 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907 STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900685 19980319 00685 NM 1998 3 19 SWA980263 1 19980312 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 500D CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 500D STR 26L TO 26R LOWER CENTER BULKHEAD SUPPORT ANGLE. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998031900686 19980319 00686 NM 1998 3 19 SWA980264 1 19980312 A 5320 CLIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 787 STR 22L, BS 787 STR 23L, BS 767 STR 23 LT, BS 747 STR 22 L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900687 19980319 00687 NM 1998 3 19 SWA980265 1 19980312 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 785 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND SKIN DAMAGE AT BS 785, WL 214, RBL 71, BELOW STR 16R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900688 19980319 00688 NM 1998 3 19 SWA980266 1 19980312 A 5400 ANGLE BOEING 737 7373H4 1384600 NM RT PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND R/W PYLON L-ANGLE STIFFENER CRACKED AT I/B SIDE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998031900689 19980319 00689 NM 1998 3 19 SWA980267 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440/500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 440, STR 8-9 RT, BS 500A STR 8-9 RT. REPAIRED PER TRAMCO EWO 98-004 2. 2 L 7 2 4F RT A16WE 1998031900690 19980319 00690 NM 1998 3 19 SWA980268 1 19980312 A 5311 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 520 STR 8-9 RT, BS 500C STR 8-9 RT, BS 440 STR 8-9 LT, BS 400 STR 8- 9 RT. REPAIRED PER TRAMCO EWO 98-0042. 2 L 7 2 4F RT A16WE 1998031900691 19980319 00691 NM 1998 3 19 SWA980269 1 19980312 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND EMERGENCY EXIT OVERHEAD TRACT LIGHT AT ROW 7 ABC, BROKEN OFF AT LIGHT HOUSING. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998031900692 19980319 00692 NM 1998 3 19 UPS98226109 1 19980309 A 5320 651633511 ANGLE BOEING 727 72725C 138400H NM BS 915 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-C, CORROSION ON ANGLE AT BS 915, LBL 68, WL 190. REMOVED AND REPLACED ANGLE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998031900693 19980319 00693 NM 1998 3 19 UPS98226111 1 19980225 A 5320 SPLICE BOEING 727 72731C 1384011 NM BS 520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 522 BETWEEN S1R AND 2R. CORROSION ON SKIN FOUND TO BE WITHIN LIMI TS. CORROSION ON BUTT SPLICE STRAP REMOVED AND REPAIRED IAW SRS ENGINEEIRNG ORDER 98-06-002R1, UPS ENGINEERING FILE NUM BER 727-53-2007. 2 L 7 3 4F A3WE 1998031900694 19980319 00694 WP 1998 3 19 UPS98826094 1 19980226 A 5320 37558422N SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1161 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 1161 BTWN STR 27L-28L SHEAR TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998031900695 19980319 00695 WP 1998 3 19 UPS98826095 1 19980225 A 5320 3750330505 SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 440 TO 460 STR 34L SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1998031900696 19980319 00696 WP 1998 3 19 UPS98826096 1 19980312 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 378 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS 378.00. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900697 19980319 00697 WP 1998 3 19 UPS98826097 1 19980307 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 74.8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, RT WING TOP AT STA XRS.74.5 AND WING STRINGER 9, THE SKIN IS CRACKED IN 2 PLACES. CUT OUT DAMAGED AR EA AND REPAIRED IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 1998031900698 19980319 00698 WP 1998 3 19 UPS98826098 1 19980312 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 828.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.828.750. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900699 19980319 00699 WP 1998 3 19 UPS98826099 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.772.500. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900700 19980319 00700 WP 1998 3 19 UPS98826100 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED AT THE AFT FASTENER AT STA XFS.622.500. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900701 19980319 00701 WP 1998 3 19 UPS98826101 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.785.00. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900702 19980319 00702 WP 1998 3 19 UPS98826102 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.778.750. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900703 19980319 00703 WP 1998 3 19 UPS98826103 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 822.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.822.500. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900704 19980319 00704 WP 1998 3 19 UPS98826104 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 747.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.747.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900705 19980319 00705 WP 1998 3 19 UPS98826105 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.616.250. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900706 19980319 00706 WP 1998 3 19 UPS98826106 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.653.750. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900707 19980319 00707 WP 1998 3 19 UPS98826107 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 791.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA XFS.791.250. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998031900708 19980319 00708 WP 1998 3 19 UPS98826108 1 19980310 A 5720 576958975 CLIP DOUG DC8 DC873F 302199F WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB IS CRACKED AT STA XOLDI6.225. REMOVED FABRICATED AND REPLACED CLIP IAW DWG 5769589. 2 L 7 4 4F RT 4A25 1998031900709 19980319 00709 WP 1998 3 19 UPS98826110 1 19980308 A 3233 4771392501 PIN DOUG DC8 DC873F 302199F WP LT MLG ACT CRACKED A IPXA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 812UP 46112 INSPECTION TYPE-N/A, NO LEFT GREEN GEAR DOWN LIGHT AND LOUD NOISE. CREW PERFORMED FLY-BY TO CONFIRM LT GEAR DOWN. FOUN D GEAR RETRACT ACTUATOR PIN (LWR) SHEARED, IPC 32-10-05 FIG 10. ALSO, FWD/LWR DOWN LOCK LINK BROKEN IPC 32-30-01. REPLA CED LOWER RETRACT CYL ATTACHMENT PIN. REPLACED FWD AND AFT LOWER DOWN LOCK LINKS PERFORMED GEAR SWING, ALL CHECKED OK. 2 L 7 4 4F RT 4A25 1998031900710 19980319 00710 WP 1998 3 19 UPS98826112 1 19980314 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-WKD, DURING WEEKEND INSPECTION FOUND EMERGENCY LIGHTS DID NOT TEST. SWITCH WAS FOUND IN ON POSITION PRI OR TO TEST. REMOVED, REPLACED AND TESTS EMERGENCY LIGHT BATTERY PACK IAW MM 33-5 0-1. (P/N 5708458-503) ON, (P/N 60-122 3-5) OFF, (S/N 404) OFF. 2 L 7 4 4F RT 4A25 1998031900711 19980319 00711 WP 1998 3 19 UPS98826113 1 19980301 A 5320 3755843502N FITTING DOUG DC8 DC871F 302199D WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, CORROSION BETWEEN BATHTUB FITTING AND SKIN AT STA 1160 BETWEEN STR 34R AND 35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998031900712 19980319 00712 WP 1998 3 19 UPS98826114 1 19980302 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 640 BETWEEN LONG 35R AND 35L INTERNAL DOUBLER IS CRACKED. REPAIRED IAW DHC SK-707-712. 2 L 7 4 4F RT 4A25 1998031900713 19980319 00713 WP 1998 3 19 UPS98826115 1 19980304 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 1480 LWR FRAME CORRODED BEYOND LIMITS BETWEEN LONG 35R TO 36. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998031900714 19980319 00714 WP 1998 3 19 UPS98826116 1 19980226 A 5320 37592582N SPLICE DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 1260 TO 1280 STR 35R SPLICE FITTING HAS 4 INCH CRACK. REMOVED, FABRICATED, AND REPLACED FITTING I AW SRM 51-1-20D AND DWG 3759258. 2 L 7 4 4F RT 4A25 1998031900715 19980319 00715 WP 1998 3 19 UPS98826117 1 19980302 A 5330 564932975N2 SKIN DOUG DC8 DC871F 302199D WP BS 1690-1890 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 1690 TO 1890 REMOVE AND REPLACE TAIL SKID LWR SKIN DUE TO CORROSION. REMOVED AND REPLACED SKIN IA W SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998031900716 19980319 00716 WP 1998 3 19 UPS98826118 1 19980304 A 5320 37508661 FITTING DOUG DC8 DC871F 302199D WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, BOTH TAIL SKID BACKUP FITTINGS CRACKED AT FS 1766. REMOVED, FABRICATED, AND REPLACED FITTINGS IAW SR M 51-3-0 AND DWG 3750866. 2 L 7 4 4F RT 4A25 1998031900717 19980319 00717 EU 1998 3 19 QXEA9800248 1 19980312 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 478US 11227 EMERGENCY EXIT SIGN AT ROW 9E IS OUT. RELAMPED SIGN, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031900718 19980319 00718 EU 1998 3 19 QXEA9800249 1 19980312 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 EMERGENCY EXIT SIGN IN THE CENTER OF THE CABIN HAS INOP BULBS. REPLACED BULBS, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998031900719 19980319 00719 NM 1998 3 19 98FDEA00197 1 19980314 A 5720 65249662 AUX SPAR BOEING 727 727227 1384078 NM WS 120 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 489FE 21492 AUX SPAR IS CRACKED, FWD OF NR 8 SPOILER FITTING. *S/D* REPAIRED AUX SPAR CHORD FWD OF NR 8 SPOILER FITTING, ALL WORK DONE IAW FED-EX EA 7-5710-38120. 2 L 7 3 4F A3WE 1998031900720 19980319 00720 EU 1998 3 19 98FDEA00199 1 19980312 A 2720 CONTROLS AIRBUS 310 A310203 EU RUDDER ICED UP A A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 SO 25 414FE 400 ON T/O ROLL, UNABLE TO GET FULL RUDDER TRAVEL, RT RUDDER TRAVEL STOPPED BETWEEN 1/2 TO 2/3 TRAVEL. ABORTED T/O. SUBSEQ UENT CONTROL CHS WITH 20 FLAPS WERE NORMAL. WHILE TAXI BACK RUDDER TRAVEL STOP AT 2/3 TRAVEL RUDDER INPUT. A/C WAS DE- ICED AT INDY WITH 55 PERCENT TYPE NR 1. DE-ICED RUDDER AND TAIL SURFACES PRECAUTIONARY CK'D LINKAGES AND CABLES FOR BIN DING, NONE FOUND. OPERATED RUDDERS THRU FULL RANGE OF TRAVEL SEVERAL TIMES CKS OK. 2 L 7 2 4F RT A35EU 1998031900721 19980319 00721 NE 1998 3 19 98FDEA00200 2 19980313 A 7200 ENGINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FOD A FDEA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL C F.O.D. CL CLIMB 1 SO 25 222FE 20933 ON CLIMBOUT AT ABOUT 4500 FT MSL (3000' AG) A LARGE BIRD FLEW RIGHT OVER COCKPIT AND INTO NR 2 ENGINE. AIRCRAFT HAD BAD VIBRATION, EVEN AT IDLE, SHUTDOWN NR 2 ENGINE. EGT DID NOT EXCEED LIMITS. NUMBER 2 ENGINE REPLACED PER FEDEX B727 ENG INE REPLACEMENT WORK CARD NUMBER 70T0002. ACCOMPLISHED ENGINE OPERATIONAL TEST PER JET RUN HANDBOOK B727 AND ALL WORK P ROPERLY. 2 L 7 3 4F 4 F RT A3WE E2EA 1998031900722 19980319 00722 NM 1998 3 19 98FDEA00170 1 19980311 A 7312 577957 MANIFOLD BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 2 FUEL HEAT RUPTURED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 503FE 18273 NR 2 ENGINE FIRE LIGHT IN FLIGHT APPROXIMATELY 11,000 FEET AFTER TAKEOFF. CHECKLIST FOLLOWED AND FIRE LIGHT EXTINGUISHE D WHEN THROTTLE RETARDED TO IDLE. ENGINE INDICATIONS WERE NORMAL. REMOVED AND REPLACED FUEL HEAT MANIFOLD, LEAK CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998031900723 19980319 00723 NM 1998 3 19 98FDEA00171 1 19980311 A 2410 700842A CSD BOEING 727 727227 1384078 NM NR 3 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 483FE 21465 AFTER TAKEOFF, NR 3 GENERATOR LOW OIL PRESS LIGHT CAME ON. FOLLOWED ALL STEPS IN RED TABS, CONSTANT SPEED DRIVE WOULD N OT DISCONNECT. AFTER THE 10TH TRY IT DISCONNECTED. CONSTANT SPEED DRIVE RISE WAS OUT OF LIMITS. CONSTANT SPEED DRIVE DID NOT DISCONNECT UNTIL WELL ON OUR WAY BACK TO DFW. REMOVED AND REPLACED NR 3 CONSTANT SPEED DRIVE, COOLER AND FLUSHE D LINES. RAN ENGINE AND SYSTEM OPERATIONAL CHECKS AND LEAK CHECKS OK PER MAINTENANCE MANUAL 24-00. RESET CIRCUIT BREAK ER FOR COOLING FAN AND RESAFTIED DISCONNECT. 2 L 7 3 4F A3WE 1998031900724 19980319 00724 EU 1998 3 19 98FDEA00198 1 19980312 A 7830 TR UNIT AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE MALFUNCTION A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 672FE 779 WHEN ACTIVATING AUTO THROTTLES FOR T/O, LEFT ECAM ANNUNCIATED ENG 1 REV PRESSURIZER AND MASTER CAUTION LIGHT REJECTED TA KEOFF.LOCKED OUT NR 1 T/R PER MEL 78-1 AND MX PROCEDURES 78-1 COMPLIED WITH. IN ADDITION, DISCONNECTED & PLUGGED BOTH D U SUPPLY LINES PER M/M 78-31-00 PAGE 901, DEFERRED PER MEL 78-1 CAT C. CONTROL # 31373, EXP 22 MAR 98. 2 L 7 2 4F RT A35EU 1998031900725 19980319 00725 WP 1998 3 19 ABXA9800203 1 19980304 A 5320 3759222IN FITTING DOUG DOUG DC8 DC863F 302198F WP BS 1260-1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STATION 1260 TO 1280 STRINGER 36 SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998031900726 19980319 00726 WP 1998 3 19 ABXA9800204 1 19980304 A 5312 56498927 BULKHEAD WEB DOUG DOUG DC8 DC863F 302198F WP BS 857 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FUSELAGE STA 857 LBL 16 THE MAIN LANDING GEAR FORWARD BULKHEAD WEB IS CRACKED AT THE ADF ANTENNA LEAD ACCESS PANEL. REP AIRED IAW DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1998031900727 19980319 00727 WP 1998 3 19 ABXA9800205 1 19980304 A 5720 5769857613 FITTING DOUG DOUG DC8 DC863F 302198F WP LT WING BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEADING EDGE OUTBOARD INTERNAL STRUCTURE FITTING BROKEN BETWEEN NR 1 AND NR 2 PYLON. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998031900728 19980319 00728 WP 1998 3 19 ABXA9800206 1 19980218 A 5712 576947011 RIB DOUG DOUG DC8 DC863F 302198F WP WS 741.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE RIB CRACKED AT STA XFS 741.25. REPAIRED IAW ABX DRAWING K0506 AND SRM 51-1-20D. 2 L 7 4 4F 4A25 1998031900729 19980319 00729 WP 1998 3 19 ABXA9800207 1 19980226 A 5320 5610326216 INTERCOSTAL DOUG DOUG DC8 DC863F 302198F WP BS 520/540 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 INTERCOSTAL ATTACH ANGLE CRACKED AT STATION 520 AND STATION 540, RBL 10. REPAIRED IAW SRM 51-1-21, SRM 53-2-0, AND SRM 51-1-20. 2 L 7 4 4F 4A25 1998031900730 19980319 00730 WP 1998 3 19 ABXA9800208 1 19980218 A 5712 576947024 RIB DOUG DOUG DC8 DC863F 302198F WP WS 760 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB CRACKED AT STA XFS 760. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K0506. 2 L 7 4 4F 4A25 1998031900731 19980319 00731 WP 1998 3 19 ABXA9800209 1 19980218 A 5712 5770138 RIB DOUG DOUG DC8 DC863F 302198F WP WS 201.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB CRACKED AT STA 201.25. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506. 2 L 7 4 4F 4A25 1998031900732 19980319 00732 WP 1998 3 19 ABXA9800210 1 19980218 A 5712 576947033 RIB DOUG DOUG DC8 DC863F 302198F WP WS 814 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE RIB CRACKED AT STA XFS 814. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506. 2 L 7 4 4F 4A25 1998031900733 19980319 00733 WP 1998 3 19 ABXA9800211 1 19980225 A 5712 576947054 RIB DOUG DOUG DC8 DC863F 302198F WP WS 697 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB CRACKED AT STA XFS 697. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506. 2 L 7 4 4F 4A25 1998031900734 19980319 00734 WP 1998 3 19 ABXA9800212 1 19980218 A 5712 57694707 RIB DOUG DOUG DC8 DC863F 302198F WP WS 728.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE RIB CRACKED AT STA XFS 728.75. REPAIRED IAW DC8 SRM 51-1-20D AND DWG K 0506. 2 L 7 4 4F 4A25 1998031900735 19980319 00735 WP 1998 3 19 ABXA9800213 1 19980304 A 5311 5750143501 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 540 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FUSELAGE TO FRAME 540 FORMER BETWEEN LONG 35R-36R IS CRACKED. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998031900736 19980319 00736 WP 1998 3 19 ABXA9800214 1 19980212 A 5320 4613574 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 460-480 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STATION 460 TO 480 STRINGER 35R SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 4613574. 2 L 7 4 4F 4A25 1998031900737 19980319 00737 WP 1998 3 19 RRXA98067 1 19980311 A 3260 CONNECTOR DOUG DC8 DC862 3021970 WP LT MLG DN LOCK FAILED A RRXA O OTHER N FALSE WARNING AP APPROACH 1 WP 15 994CF 45956 LEFT MAIN LANDING GEAR GREEN SAFE LIGHT WOULD NOT COME ON WHEN LANDING GEAR EXTENDED. REPLACED PLUG ON LEFT DOWN LOCK S WITCH, OP CHECKS GOOD. 2 L 7 4 4F 4A25 1998031900738 19980319 00738 WP 1998 3 19 RRXA98068 1 19980312 A 3260 SWITCH DOUG DC8 DC871F 302199D WP LT MLG OUT OF ADJUST A RRXA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 15 8087U 45977 ON FINAL APPROACH, LT MAIN GEAR LIGHTS DIDN'T COME ON. RECYCLED GEAR NO LIGHTS, REPLACED BULBS, STILL NO LIGHTS, RECYCL ED GEAR NO LIGHTS, REPLACED BULBS A SECOND TIME AND LT MAIN GEAR LIGHTS WORKED. EMERGENCY EQUIPMENT STANDING BY. ON GR OUND TEST OF OLD BULBS, CHECKS OK. REMOVED LT MLG DOWN LOCK SWITCH. CK'ED OK WITH OHM METER. ADJUSTED SWITCH POSITION AS RE-INSTALLED SAME SWITCH. CYCLED GEAR 3 TIMES PER M/M 32-60-0, OPS NOW NORMAL. 2 L 7 4 4F RT 4A25 1998031900739 19980319 00739 WP 1998 3 19 RRXA98069 1 19980313 A 2710 CONTROLS DOUG DC8 DC871F 302199D WP AILERONS MALFUNCTIONED A A RRXA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 15 8084U 45974 IN FLIGHT THERE WAS A LARGE DEAD SPOT IN THE AILERONS IN THE CENTER/NEUTRAL POSITION. IN FLIGHT THE AIRPLANE ROLLS LEFT AND RIGHT. TO STOP OR CONTROL THE ROLL YOU HAVE TO DO A DUTCH ROLL TYPE OF MANUVER TO CONTROL THE ROLL. INSPECTED CON TROL SURFACES, CABLES, PULLEYS, LINKAGES, ALL ATTACH FITTINGS. CHECKED CABLE TENSIONS, RAN AILERONS THROUGH MANY CYCLES . NO DEFECTS FOUND. OPS CK GOOD ON GRND. INSPECTED OPERATION OF FLT SPOILERS, ALLS OPS CK GOOD ON GRND. MAINTENANCE REQUESTED TEST FLIGHT. TEST FLIGHT SATISFACTORY. 2 L 7 4 4F RT 4A25 1998031900740 19980319 00740 NE 1998 3 19 VNAA9803015 3 19980311 A 6112 B6444 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP BOOT BROKEN A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 426JS 3038 DURING TAXI FOR TAKEOFF, THE LEFT HAND PROPELLER HEAT FAILED TO OPERATE. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATIO N MAINTENANCE INSPECTED AND REPAIRED A BROKEN PROPELLER DE-ICE BOOT LEAD WIRE IN ACCORDANCE WITH HARTZELL MAINTENANCE MA NUAL 61-00-60. OPERATION CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998031900741 19980319 00741 NM 1998 3 19 PCAA9800712 1 19980201 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 837EX 217 FIRST RED EMERGENCY FLOOR PROXIMITY LIGHT AT PASSENGER ENTRANCE IS INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900742 19980319 00742 NM 1998 3 19 PCAA9800711 1 19980201 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 814EX 318 EMERGENCY PATH LIGHT INOPERATIVE AT SEAT 3DF. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED T O SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900743 19980319 00743 NM 1998 3 19 PCAA9800710 1 19980201 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 FIRST FOUR ROWS OF FLOOR EMERGENCY PROXIMITY LIGHTING NOT ILLUMINATING WHEN TESTED. RESECURED CANNON PLUG AT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900744 19980319 00744 NM 1998 3 19 PCAA9800720 1 19980203 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 EICHP 258 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPALCED BULB. OPERATIONAL TEST NORMAL . AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900745 19980319 00745 NM 1998 3 19 98ZZZX1090 1 19980202 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 EICBJ 215 ONE LIGHT AT ROW 4 INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TE ST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900746 19980319 00746 NM 1998 3 19 PCAA9800718 1 19980208 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 835EX 289 TWO LIGHTS INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REPAIRED BROKEN WIRE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REPAIRED BROKEN WIRE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM CIRCUIT. OPERATIONAL TEST NORMAL. A IRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900747 19980319 00747 NM 1998 3 19 PCAA9800717 1 19980205 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 829EX 12015 10699 060756 146 COCKPIT PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBL Y AND LIGHT RECEPTICAL. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900748 19980319 00748 NM 1998 3 19 PCAA9800716 1 19980206 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 825EX 388 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900749 19980319 00749 NM 1998 3 19 PCAA9800715 1 19980202 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 821EX 173 FORWARD CENTER CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETU RNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900750 19980319 00750 NM 1998 3 19 PCAA9800714 1 19980208 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 818EX 235 FORWARD CABIN EMERGENCY EXIT SIGN HAS ONE INOPERATIVE BULB. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. AIRCR AFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900751 19980319 00751 NM 1998 3 19 PCAA9800713 1 19980205 A 3350 6038443 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 808EX 16319 1702 299 LEFT AFT EMERGENCY EXIT EGRESS LIGHT AND AFT CEILING AISLE LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATT ERY PACK AT POSITION 3351/PS3. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900752 19980319 00752 NM 1998 3 19 PCAA9800725 1 19980210 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 EMERGENCY FLOOR LIGHTING INOPERATIVE RIGHT CENTER FLOOR. REPAIRED OPEN CIRCUIT AT CONNECTOR, OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900753 19980319 00753 NM 1998 3 19 PCAA9800728 1 19980216 A 3350 SWITCH DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 817EX 191 LEVER FOR EMERGENCY LIGHT SWITCH BROKEN OFF. REPLACED SWITCH, PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHT SYSTEM. OP ERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900754 19980319 00754 NM 1998 3 19 PCAA9800729 1 19980216 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 SEVERAL LIGHTS INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. FOUND SEVERAL LIGHT STRIPS UNPLUGGED. SECURED CONNECTORS. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900755 19980319 00755 NM 1998 3 19 PCAA9800732 1 19980215 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTIONED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 829EX 10784 060467 146 OVERHEAD PORTABLE EMERGENCY LIGHT REMAINS ILLUMINATED DURING NORMAL OPERATIONS. REPLACED OVERHEAD PORTABLE EMERGENCY LI GHT WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900756 19980319 00756 NM 1998 3 19 PCAA9800723 1 19980209 A 7931 GAUGE DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE MALFUNCTIONED A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 820EX 019 ON CLIMB-OUT FROM SWF AFTER SELECTION OF GEAR UP, NR 2 OIL PSI LIGHT ILLUMINATED AND NR 2 OIL PSI GAUGE INDICATED 20 PSI , 5 SECONDS LATER, BOTH INDICATED NORMAL. CREW REDUCED POWER AND RETURNED TO FIELD. MAINTENANCE TROUBLESHOT NR 2 ENGIN E OIL PRESSURE SYSTEM IAW PWC MANUAL, GROUND RAN AIRCRAFT, PERFORMED A TEST FLIGHT, NO DEFECTS NOTED. AIRCRAFT RETURNE D TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900757 19980319 00757 NM 1998 3 19 PCAA9800730 1 19980213 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 831EX 160 LEFT AFT EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BULB AND CLEANED SOCKET. OPERATION TEST NOR MAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900758 19980319 00758 NM 1998 3 19 PCAA9800731 1 19980212 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 832EX 280 CENTER EMERGENCY CABIN LIGHT HAS INOPERATIVE BULBS. REMOVED AND REPLACED INOPERATIVE BULBS IN CENTER EMERGENCY CABIN LI GHT. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900759 19980319 00759 NM 1998 3 19 PCAA9800736 1 19980224 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 815EX 0007PA 321 RIGHT AFT FUSELAGE EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT POSTION NR 600. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERIVCE. (X) 2 H 7 2 4T RT A13NM 1998031900760 19980319 00760 NM 1998 3 19 PCAA9800735 1 19980222 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 RIGHT FLOOR EMERGENCY LIGHTS HAVE NUMEROUS INOPERATIVE BULBS. SECURED CONNECTOR ON RIGHT FLOOR EMERGENCY LIGHT STRIP. O PERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900761 19980319 00761 NM 1998 3 19 PCAA9800734 1 19980224 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 810EX 547 0133PA 308 FORWARD CABIN OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT POSITION NR 200. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900762 19980319 00762 NM 1998 3 19 PCAA9800733 1 19980221 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGH T BULB. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900763 19980319 00763 NM 1998 3 19 PCAA9800737 1 19980225 A 2910 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM NR 2 SYSTEM FAILED A PCAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 13 819EX 016 ON FINAL INTO PIT WHEN THE LANDING GEAR WAS SELECTED DOWN, THE NR 2 HYDRAULIC CONTENTS WERE DEPLETED. AIRCRAFT LANDED W ITHOUT INCIDENT. MAINTENANCE INSPECTED HYDRAULIC SYSTEM AND FOUND A-HYDRAULIC LINE UNDER THE LEFT INBD FLAP SPLIT. PER FORMED A REPAIR TO THE LINE IAW DHC PROCEDURES. SYSTEM WAS REPLENISHED, CHECKED OUT FOR LEAKS AND OPERATION. DHC PROCE DURES FOR LOSS OF HYDRAULIC SYSTEM C/W. GEAR RETRACTION TEST PERFORMED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X ) 2 H 7 2 4T RT A13NM 1998031900764 19980319 00764 NM 1998 3 19 PCAA9800738 1 19980226 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 SEVERAL EMERGENCY FLOOR PROXIMITY LIGHTS INOPERATIVE. SECURED SEVERAL LOOSE JUMPER WIRES, REPAIRED WIRING IN EMERGENCY PROXIMITY LIGHTING CIRCUIT AND REPLACED FORWARD AND AFT BATTERY PACK FUSES. OPERATIONAL TEST OF SYSTEM NORMAL. AIRCRAF T RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900765 19980319 00765 NM 1998 3 19 PCAA9800739 1 19980226 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 5579 060567 016 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGH T ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1998031900766 19980319 00766 WP 1998 3 19 TWAA9803101 1 19980303 A 3350 58222 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A TWAA K NONE O OTHER DE DESCENT 1 CE 05 922L 47108 STL - FLT 625 - AFT CABIN EGRESS LIGHTS AND TAIL CONE EXIT LIGHTS WERE BLINKING ON AND OFF IN DESCENT. REPLACED POWER S UPPLY FOR AFT CABIN EGRESS LIGHT SYSTEM. CHECK-C 11-15-97 MCI. (X) 2 L 7 2 4F A6WE 1998031900767 19980319 00767 WP 1998 3 19 TWAA9802801 1 19980225 A 3350 CONNECTORS DOUG DC9 DC931 3022065 WP CABIN WET A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 984Z 47412 STL - DURING OVERNIGHT MAINTENANCE, THE FIRST CLASS SECTION OF THE EGRESS LIGHTS WERE FOUND INOPERATIVE. DRIED ALL MOIS TURE ON LAMP CONNECTORS AND IN TRACKS. CHECK-C 12-13-97 AT STL. (X) 2 L 7 2 4F A6WE 1998031900768 19980319 00768 NE 1998 3 19 TAOA029811 2 19980226 A 7421 MS9386214 SEAL PARKER BOEING 727 727254 138408L NM PWA JT8 JT8D7B 52053 NE RT ENG IGN PLUG MISSING A TAOA K NONE J WARNING INDICATION DE DESCENT 1 EA 15 913TS 20250 649622 DCA/LGA - FLT 6411 - AT 3,000 FEET ON DESCENT, NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AND COCKPIT BELL SOUNDED. RET ARDED THROTTLE AND LIGHT EXTINGUISHED. FOUND CSD EJECTOR PIPE GASKET AND 8TH STAGE CHECK VALVE GASKET BLOWN, REPLACED G ASKETS. FOUND SEAL ON RIGHT HAND IGNITER PLUG MISSING, INSTALLED NEW SEAL. RAN NR 1 ENGINE AND LEAKED CHECK. FIRE WAR NING SYSTEM OPERATIONAL CHECK PER MM 26-21-0. (X) 2 L 7 3 4F 4 F A3WE E2EA 1998031900769 19980319 00769 NM 1998 3 19 TAOA029812 1 19980227 A 2612 FIRE LOOP BOEING 727 727254 138408L NM NR 1 ENGINE CHAFED A TAOA O OTHER N FALSE WARNING DE DESCENT 1 EA 15 913TS 20250 LGA/BOS - FLT 6102 - NR 1 FIRE LIGHT AND BELL WENT OFF WHEN POWER WAS ADVANCED FOR LEVEL-OFF DURING DESCENT. THROTTLE W AS RETARDED AND LIGHT AND BELL SILENCED, SYSTEM OPERATED NORMALLY. RAN NR 1 ENGINE AT DIFFERENT POWER SETTINGS. ALL PN EUMATIC DUCTS AND CLAMPS CHECKED FOR LEAKS AND SECURITY. FOUND FIRE DETECTOR LOOP WIRING AT PYLON CHAFING AT CLAMP, REP OSITIONED HARNESS, OPERATION CHECK NORMAL PER MM 26-21-0. (X) 2 L 7 3 4F A3WE 1998031900770 19980319 00770 EU 1998 3 19 SIMA980551 1 19980224 A 2930 M880507032 SWITCH KLIXON SAAB SF340 340B 7860101 EU NLG WW SHORTED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 344SB 340B344 TXK - FLT 3924 - DURING FLIGHT, CREW NOTED EMERGENCY HYDRAULIC LOW LIGHT CAME ON. CREW BLEW GEAR AND DIVERTED INTO TXK. NO FURTHER INCIDENTS WERE REPORTED. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND INSTALLED L/G DOOR EXPLOSIVE BOL TS, CHECKED HYDRAULIC LOW LIGHT, AND FERRIED AIRCRAFT TO DFW FOR REPLACEMENT OF 5GB MICROSWITCH. PERFORMED ROTATION TES T SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998031900771 19980319 00771 EU 1998 3 19 SIMA980531 1 19980222 A 3230 M835366022L RELAY SAAB SF340 340B 7860101 EU LT MLG CONTAMINATED A SIMA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 21 396AE 340B396 LAW - FLT 3509 - THE CREW NOTICED A STRONG ELECTRIAL SMOKE SMELL AND THE C/B F7 POPPED DURING APPROACH. THE CREW RESET THE C/B AND SELECTED THE GEAR DOWN. THE NOSE GEAR SHOWED DOWN AND LOCKED, MAIN GEARS SHOWED UNLOCKED. ON LANDING THE R T GEAR LOCKED, THE LT GEAR COLLAPSED AND THE LT PROP STRUCK THE GROUND. THE A/C SLID OFF THE EDGE OF THE RUNWAY. MX US ED AIR BAGS TO RAISE A/C. LOWERED LT GEAR DOWN INTO LOCKED POSITION. R/I'D LT/RT ENG. PROPELLER ASSY AND NOSE LT/RT M LG ASSY FOR DETAILED INSPECTIONS. REPLACED LT FLAP AND AILERON DUE TO MINOR DAMAGE AND REPAIRED OUTBOARD WING LEADING E DGE. ALSO, MINOR DAMAGE. REPLACED RELAY 15GA AND RECEPTACLE DUE TO LIQUID CONTAMINATION THROUGH COCKPIT FLOOR AREA. P 2 L 7 2 4T RT A52EU 1998031900772 19980319 00772 EU 1998 3 19 SIMA980562 1 19980225 A 5320 S5337129320201 SILL AEROSP ATR42 ATR42300 8680920 EU CARGO COMPT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE CARGO DOOR SILL SUPPORT PLATE CORRODED BETWEEN FRAMES 14 AND 18 . MAINTENANCE REMOVED AND REPLACED THE SUPPORT PLATE IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998031900773 19980319 00773 EU 1998 3 19 SIMA980561 1 19980225 A 5347 S53678001232 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CARGO COMPT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RT AFT CARGO SEAT TRACK GOUGED OUT OF LIMITS. MAINTENANCE REMO VED AND REPLACED THE SEAT TRACK IAW SRM 51-24-04. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998031900774 19980319 00774 EU 1998 3 19 SIMA980571 1 19980225 A 5315 S5317215820401 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 37AE 037 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RT SIDE OF FLOORBEAM 7 WAS CORRODED. MAINTENANCE SPLICED IN A NEW SECTION OF FLOORBEAM 7 IAW ATR DRAWING NR 115631R0158...1112 ISSUE A). AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998031900775 19980319 00775 EU 1998 3 19 SIMA980591 1 19980228 A 3350 330151 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 383AE 1087 340B383 DFW - FLT 3661 - EXIT SIGN ABOVE F/A JUMP SEAT NOT ILLUMINATING. REPLACED EMERGENCY BATTERY FORWARD PACK. OPS CHECK GO OD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998031900776 19980319 00776 EU 1998 3 19 RAIA980219 1 19980227 A 5730 S5391007501200 PANEL AEROSP ATR42 ATR42300 8680920 EU FWD WING BOX LOOSE A A RAIA B EMER. DESCENT E VIBRATION/BUFFET DE DESCENT 1 CE 03 424TE 20892 124 STL - FLT 7417 - AIRCRAFT ENCOUNTERED TURBULENCE IN-FLIGHT, AIRFRAME VIBRATION AFTER ENCOUNTER ON DESCENT. MAINTENANCE INSPECTED, FOUND FORWARD WING BOX PANEL 291BL LIFTED, INSPECTED AREA, REPLACED PANEL. (X) 2 H 7 2 4T RT A53EU 1998031900777 19980319 00777 EU 1998 3 19 RAIA980301 1 19980301 A 7332 1103P0645 PRESSURE SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 864AE 9031 864 LAX - FLT 4794 - RIGHT ENGINE LOW FUEL PRESSURE CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT FUEL LO W PRESSURE SWITCH. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1998031900778 19980319 00778 1998 3 19 RAIA980218 4 19980226 A 3416 4016341905 ALTIMETER JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 551HK 1875 18 41040 STL - FLT 7067 - CAPTAIN'S ALTIMETER FLAGGED ON CLIMB-OUT. MAINTENANCE REPLACED CAPTAIN'S ALTIMETER. (X) 2 L 7 2 4T RT A41NM 1998031900779 19980319 00779 EU 1998 3 19 RAIA980302 1 19980302 A 7931 1103P0645 PRESSURE SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3312UA 01514 WP RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 423AM 30 858 BRL - FLT 7541 - RIGHT ENGINE FUEL LOW PRESSURE CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT ENGINE FUEL LOW PRESSURE SWITCH. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1998031900780 19980319 00780 EU 1998 3 19 REXA98062 1 19980226 A 2842 SENSOR BAG JETSTM JETSTM3101 1500215 EU LEFT MALFUNCTIONED A REXA D RETURN TO BLOCK O OTHER CL CLIMB 1 SO 25 317PX 688 LEFT HAND FUEL QUANTITY IS INOPERABLE. APPLIED PRIST TO LEFT HAND FUEL TANK. SUMPED 3 GALLONS FROM LEFT HAND FUEL TANK . GAUGE READS SAME AS MAG STICK. (X) 2 L 7 2 4T RT A21EU 1998031900781 19980319 00781 EU 1998 3 19 REXA98061 1 19980226 A 5350 RADOME SAAB SF340 SF340A 7850100 EU FWD FUSELAGE CONTAMINATED A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 112PX 340A025 WEATHER RADAR PAINT DOTS, INOPERATIVE. CLEANED WATER OUT OF RADOME. OPS CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998031900782 19980319 00782 EU 1998 3 19 REXA98060 1 19980225 A 2434 23079009 GENERATOR BAG JETSTM JETSTM3101 1500215 EU RT ENGINE FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 316PX 4792 687 IN-FLIGHT, AMMETER SHOWED 150-200 AMPS ON LEFT SIDE AND ZERO - 10 AMPS ON RIGHT. REMOVED AND REPLACED RIGHT HAND DC GEN ERATOR. GENERATORS PARALLELED. OK FOR SERVICE. (X) 2 L 7 2 4T RT A21EU 1998031900783 19980319 00783 EU 1998 3 19 REXA98059 1 19980224 A 3297 WIRE BAG JETSTM JETSTM3101 1500215 EU NLG DAMAGED A REXA B EMER. DESCENT N FALSE WARNING LD LANDING 1 SO 25 332PX 702 NOSE GEAR NOT INDICATING GREEN. REPAIRED BROKEN AND DAMAGED WIRE AT NOSE DOWNLOCK MICROSWITCH. (X) 2 L 7 2 4T RT A21EU 1998031900784 19980319 00784 EU 1998 3 19 REXA98056 1 19980217 A 2612 51653120 FIRE CONTROL BOX BAG JETSTM JETSTM3101 1500215 EU RIGHT FAILED A REXA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 25 318PX 536 689 RIGHT ENGINE FIRE INDICATION ON RUNWAY. REMOVED AND REPLACED RIGHT FIRE CONTROL BOX. (X) 2 L 7 2 4T RT A21EU 1998031900785 19980319 00785 NE 1998 3 19 REXA98055 2 19980217 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LEFT FAILED A REXA O OTHER O OTHER NR NOT REPORTED 1 SO 25 406BH 340A074 GEE367165DKU LOUD SQUEAL LT ENGINE. REMOVED AND REPLACED LT ENGINE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1998031900786 19980319 00786 EU 1998 3 19 REXA98054 1 19980213 A 3020 ND00751940 LOAD MONITOR SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 407BH L240517 340A078 LEFT INTAKE LIGHT COMES ON CONTINUOUSLY DURING FLIGHT. REMOVED AND REPLACED LOAD MONITOR. (X) 2 L 7 2 4T RT A52EU 1998031900787 19980319 00787 EU 1998 3 19 REXA98057 1 19980219 A 6120 PROP OVERSPEED SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A REXA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 25 401BH 340A057 RIGHT HAND PROPELLER OVERSPEED WILL NOT TEST. CREW SHUT DOWN RIGHT ENGINE, RESTARTED AND TESTED AGAIN WITH NO DEFECTS. (X) 2 L 7 2 4T RT A52EU 1998031900788 19980319 00788 NE 1998 3 19 REXA98058 2 19980223 A 7510 VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE FAILED A REXA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 25 366PX 340B267 785276 RIGHT ENGINE VIBRATES AND SOUNDS SIMILAR TO COMPRESSOR STALL. ALL OTHER INDICATIONS NORMAL. AFTER INSPECTION OF RIGHT ENGINE AND GROUND RUNS IN SEVERAL DIFFERENT POWER SETTINGS, NO DEFECTS NOTED. SWAPPED ANTI-ICING BLEED VALVE FOR TROUBL ESHOOTING GROUND RUNS AND CHECKS. FOUND NO DEFECTS. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1998031900789 19980319 00789 WP 1998 3 19 NOCA0608 1 19980228 A 3350 60030431 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 COCKPIT OVERHEAD EMERGENCY LIGHT DOES NOT STAY ILLUMINATED WHEN TESTED. REPLACED FORWARD BATTERY POWER SUPPLY. OPS CHE CKS NORMAL. (X) 2 L 7 2 4F RT A6WE 1998031900790 19980319 00790 1998 3 19 98ZZZX1091 4 19980225 A 6122 30849601 PROP GOVERNOR WOODWARD BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A JJBA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 01 861CA 1068 2457383 UE164 AFTER TAKEOFF, PROPELLER RPM WENT TO 1,800. CREW ABLE TO REDUCE RPM TO 1,450, AND RETURNED TO FIELD. PROPELLER GOVERNO R FAILURE. REMOVED AND REPLACED PROPELLER GOVERNOR. 2 L 7 2 4T RT A24CE 1998031900794 19980319 00794 SO 1998 3 19 WTAA980036 1 19980220 A 2612 8005577 AURAL WARN UNIT EMB 120 EMB120RT SO COCKPIT FAILED A WTAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 201YW 120201 SFO - FIRE BELL AND 'SMOKE' AURAL WARNING WHEN STARTING RIGHT ENGINE. MAINTENANCE REPLACED AURAL WARNING UNIT. OPERATI ONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998031900795 19980319 00795 SO 1998 3 19 WTAA980040 1 19980301 A 5101 STRUCTURE EMB 120 EMB120RT SO AIRFRAME BIRD STRIKE A WTAA K NONE C F.O.D. LD LANDING 1 WP 17 193YV 120193 SBA - BIRD STRIKE ON LANDING REPORTED. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998031900796 19980319 00796 SO 1998 3 19 WTAA980039 1 19980301 A 7921 1602825 OIL COOLER EMB 120 EMB120RT SO LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 455UE 120163 SBA - LEFT ENGINE LOST OIL PRESSURE ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE REPLACED LEFT ENGINE OIL COOLER AND SERVI CED. PERFORMED ENGINE RUN. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998031900797 19980319 00797 EU 1998 3 19 WTAA980032 1 19980214 A 7712 TQ INDICATION BAG JETSTM JETSTM3101 1500215 EU LEFT MALFUNCTIONED A WTAA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 17 422UE 782 SNA - LEFT TORQUE INDICATION FLUCTUATION REPORTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE COULD NOT DUPLICATE DISCREPA NCY. PERFORMED HIGH POWER GROUND RUN, NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1998031900798 19980319 00798 WP 1998 3 19 WTAA980033 2 19980216 A 7320 8974573 BYPASS VALVE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE FAILED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 425UE 798 SBP - LEFT ENGINE FAILED TO MAKE TAKEOFF TORQUE. TAKEOFF ABORTED. MAINTENANCE DEFERRED TTL PER MEL 76-2. AIRCRAFT RET URNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLOSED DEFERRAL BY REPLACING LEFT TTL BYPASS VALVE. OPERATIONAL AND LEAK CH ECK SATISFACTORY. (X) 2 L 7 2 4T 4 T RT A21EU E4WE 1998031900799 19980319 00799 EU 1998 3 19 WTAA980037 1 19980223 A 3260 DOWNLOCK LIGHT BAG JETSTM JETSTM3101 1500215 EU LANDING GEAR MALFUNCTIONED A WTAA O OTHER P NO WARNING INDICATION DE DESCENT 1 WP 17 429UE 807 LAX - LANDING GEAR DOWN AND LOCK FAILED TO ILLUMINATE WHEN GEAR SELECTED DOWN. MAINTENANCE PERFORMED OPERATIONAL CHECK OF LANDING GEAR. GEAR INDICATIONS NORMAL. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 1998031900800 19980319 00800 WP 1998 3 19 TWAA9803102 1 19980303 A 5270 2052005T1 TARGET DOUG DC9 DC982 3022082 WP CARGO COMPT MISSING A TWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 919TW 49368 OMA - FLT 38 - AFT CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO OMA. DOOR INDICATION PLACARDED PER MEL. ON ACFT LAYOVER, THE DOOR SENSOR WAS REPLACED AND THE MISSING DOOR SENSOR TARGET WAS INSTALLED. SENSOR PART NR 8-340-02. CHECK-C 8-9-97 MCI. (X) 2 L 7 2 4F A6WE 1998031900917 19980319 00917 SW 1998 3 19 HEEA0013260 1 19980304 A 6330 214031617113 HELPER SPRING BELL 214 214ST 1182106 SW NODAL BEAM DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 NODAL BOUNCE. FOUND HELPER SPRING DEFECTIVE 2 G 7 2 4U H10SW 1998031900918 19980319 00918 SW 1998 3 19 HEEA0013261 1 19980304 A 6330 214031617113 HELPER SPRING BELL 214 214ST 1182106 SW NODAL BEAM DELAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 DELAMINATED. 2 G 7 2 4U H10SW 1998031900919 19980319 00919 NE 1998 3 19 HEEA0013263 1 19980304 A 7810 7630507001044 EXHAUST COVER SKRSKY S76 S76A 8143006 NE ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 EXHAUST COVER CRACKED IN SEVERAL SPOTS. 1 G 7 2 3U H1NE 1998031900920 19980319 00920 1998 3 19 HEEA0013287 4 19980304 A 2210 574074140003 PANEL ASSY BELL 212 212 1181420 SW SCAS SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 SCAS LIGHT GOES OUT. CHANNEL LOW. 1 G 7 1 4U H4SW 1998031900921 19980319 00921 SO 1998 3 19 C2XA98IA029 1 19980212 A 3350 D36604001 POWER SUPPLY EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 51726 120174 IAH - FLT 3950 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAIN TENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A31SO 1998031900922 19980319 00922 SO 1998 3 19 C2XA98IA028 1 19980212 A 3350 BS2197 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 51726 7897 120174 IAH - FLT 3950 - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAIN TENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A31SO 1998031900923 19980319 00923 EU 1998 3 19 C2XA98BT013 1 19980217 A 3240 140071 TRANSDUCER AEROSP ATR42 ATR42320 8680930 EU LT MLG INOPERATIVE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 09 21837 202 ON LANDING IN EWR, TOWER OBSERVED SMOKE FROM LEFT LANDING GEAR ON LANDING ROLL. TOWER CALLED TRUCKS AND NOTIFIED CAPTAI N. REMOVED AND REPLACED WHEEL AND WHEEL SPEED TRANSDUCER. (M) 2 H 7 2 4T RT A53EU 1998031900924 19980319 00924 EU 1998 3 19 C2XA98BT012 1 19980216 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 AIRCRAFT ARRIVED AT HANGAR FOR LINE CHECK WITH LOG SQUAWK 'RT FWD AND AFT EXTERIOR EMERGENCY EXIT LIGHTS INOP'. REMOVED AND REPLACED LIGHT BULBS. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998031900925 19980319 00925 EU 1998 3 19 C2XA98BT011 1 19980216 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 AIRCRAFT ARRIVED AT HANGAR FOR A LINE CHECK WITH A LOG SQUAWK OF 'LEFT REAR EXTERIOR EMERGNCY EXIT LIGHT INOP'. REMOVED AND REPLACED LIGHT BULB. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998031900926 19980319 00926 NE 1998 3 19 C2XA98IA009 2 19980130 A 7200 3047600 ENGINE AEROSP ATR42 ATR42500 EU PWA PW120 PW127 NE LEFT FAILED A C2XA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER UK UNKNOWN 1 SW 09 33449 3573 507 AM0015 MEM - FLT 3857 - THE PILOT REPORTED THE NR 1 ENGINE HAD INDICATION FLUCTUATIONS, LOUD BANGS, AND VISUAL INDICATION OF SP ARKS COMING OUT OF THE TAIL PIPE. THE CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO MEM, LANDED WITHOUT INCIDENT. MAINTEN ANCE REMOVED AND REPLACED THE NR 1 ENGINE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998031900927 19980319 00927 SO 1998 3 19 C2XA98IA010 1 19980201 A 5280 12012939002 DOOR EMB 120 EMB120RT SO RT MLG CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17728 120182 IAH - DURING C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR INBOARD FORWARD DOOR ACTUATOR FORWARD ATTACH BRACKET WAS FO UND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT FORWARD INBOARD DOOR IAW EMB-120 MM 32-12-00, AND THE AIR CRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998031900928 19980319 00928 WP 1998 3 19 AALA980178 1 19980119 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1982 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON SHEAR TIE STATION 1982. FABRICATED NEW SHEAR TIE TREATED PRIMED AND PAINTED NEW PART. INSTALL ED SHEAR SRM VOL 1 53-30-00 FIGURE NR 1. (M) 2 L 7 3 4F A22WE 1998031900929 19980319 00929 WP 1998 3 19 AALA980180 1 19980117 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 1781 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON LWR SIDE OF CHANNEL AT ATTACH POINTS. PART WAS FABRICATED AND INSTALLED PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998031900930 19980319 00930 WP 1998 3 19 AALA980179 1 19980119 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1977 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON FUSELAGE SKIN AT STATION 1977, STRINGER 51R. REPAIR FABRICATED AND INSTALLED PER ESO 7349, DAT ED 1-19-98. (M) 2 L 7 3 4F A22WE 1998031900931 19980319 00931 WP 1998 3 19 AALA98134 1 19980116 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - SMALL SECTION OF FLOOR SUPPORT CORRODED TOP AND BOTTOM SIDES, BETWEEN TRAY NR 5 AND NR 6. REMOVED PART AND REPLAC ED WITH NEW PART PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998031900932 19980319 00932 WP 1998 3 19 AALA98138 1 19980116 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FLOORBOARD SUPPORT CORRODED BETWEEN TRAYS. REMOVED PART, INSTALLED NEW PART PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998031900933 19980319 00933 WP 1998 3 19 AALA980174 1 19980116 A 5347 TRACK DOUG DC10 DC1030 3023501 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FORWARD END OF TRACK CORRODED AT WEB ATTACHMENT STATION 1841 RT. NEW TRACK FABRICATED AND INSTALLED PER AARD/SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998031900934 19980319 00934 WP 1998 3 19 AALA980173 1 19980116 A 5347 TRACK DOUG DC10 DC1030 3023501 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FORWARD END OF TRACK CORRODED AT WEB ATTACHMENT STATION 1841 LEFT. NEW TRACK WAS FABRICATED AND INSTALLED PER AAR D/SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998031900935 19980319 00935 WP 1998 3 19 AALA980127 1 19980114 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1952 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND SHEAR TIE CORRODED BEYOND LIMITS. REPLACED SHEAR TIE PER SRM 53-30-00. (M) 2 L 7 3 4F A22WE 1998031900936 19980319 00936 WP 1998 3 19 AALA980209 1 19980119 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1772 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON FRAME AND SHEAR TIES AFT CARGO. FABRICATED AND INSTALLED NEW SHEAR TIE PER SRM 53-30-00 FIGURE 10. (M) 2 L 7 3 4F A22WE 1998031900937 19980319 00937 WP 1998 3 19 AALA980210 1 19980119 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1962 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON BOTTOM FRAME ANGLE ATTACHMENT TO SKIN. INSTALLED NEW SHEAR TIE PER SRM 53-30-00 FIG 10. (M) 2 L 7 3 4F A22WE 1998031900938 19980319 00938 EU 1998 3 19 AALA980200 1 19980122 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7082A 643 TUL - FOUND SEAT TRACK NR 9 CORRODED. REPLACED TRACK NR 9 BETWEEN FRAME 30 TO 32 PER SRM 51-22-10-0, ALODINED, PRIMED, PAINTED PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998031900939 19980319 00939 EU 1998 3 19 AALA980202 1 19980122 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7082A 643 TUL - FOUND CORROSION ALONG FLOOR SUPPORT FWD OF SEAT TRACK NR 9 BETWEEN FRAMES 14-16. REMOVED AND REPLACED FLOOR SUPPO RT, INBOARD OF R1 DOOR FWD OF SEAT TRACK NR 9 BETWEEN FRAMES 14 AND 16, SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998031900940 19980319 00940 EU 1998 3 19 AALA980201 1 19980122 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7082A 643 TUL - FLOOR SUPPORT END OF TRACK NR 7, BETWEEN FRAME 14 TO 17 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10-2, ALOD INED, PRIMED AND PAINTED PER SRM 51-21-00-0. ACCOMPLISHED REPAIR PER AARD 51-10-00-3. (M) 2 L 7 2 4F RT A35EU 1998031900941 19980319 00941 EU 1998 3 19 AALA980217 1 19980126 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7082A 643 TUL - FOUND SEAT TRACK NR 10 CORRODED AT FASTENER HOLES BETWEEN FRAMES 28 AND 30 AND R2 DOOR THRESHOLD AREA. REPAIRED C ORROSION PER ESO30595, DATED 26 JAN 98. (M) 2 L 7 2 4F RT A35EU 1998031900942 19980319 00942 WP 1998 3 19 AALA980250 1 19980204 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT AIRSTAIR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 287AA 49299 DFW - DURING OVERNIGHT CHECK, AFT AIRSTAIR EMERGENCY LIGHT SIGN INOPERATIVE. REPLACED AFT AIRSTAIR EMERGENCY LIGHT SIGN WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900943 19980319 00943 WP 1998 3 19 AALA980257 1 19980205 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICING A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 581AA 53158 ORD - FLT 267 - ON TAKEOFF ORD, NOSE GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. SER VICED STRUT, LUBRICATED GEAR. ACCOMPLISHED GEAR RETRACTION CHECK SEVERAL CYCLED WITH NO DEFECTS, COULD NOT DUPLICATE. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900944 19980319 00944 1998 3 19 AALA980237 4 19980202 A 2565 D29984119 SLIDE DOUG DC9 DC982 3022082 WP TAILCONE DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 469AA 49599 ORD - DURING OVERNIGHT MAINTENANCE CHECK, FOUND TAIL CONE EVACUATION SLIDE PRESSURE INDICATOR IN THE RED BAND. REPLACED TAIL CONE EVACUATION SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900945 19980319 00945 NE 1998 3 19 AALA980195 2 19980121 A 7200 ENGINE AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 1 DEFECTIVE A AALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 14056 463 690327 JFK - FLT 657 - WHEN CLIMB RATE WAS SELECTED, NR 1 ENGINE WOULD NOT DEVELOP CLIMB POWER. RETURNED TO JFK AND LANDED WIT HOUT INCIDENT. REPLACED NR 1 ENGINE. ACCOMPLISHED ENGINE RUN AND LEAK CHECKED NORMAL. SYSTEM GROUND CHECKED NORMAL OP ERATION. OPERATIONAL CHECKED WITH NO DEFECTS. (M) 2 L 7 2 4F 4 F RT A35EU E13NE 1998031900946 19980319 00946 NE 1998 3 19 AALA980244 2 19980203 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE RIGHT FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 501AA 49738 DFW - FLT 225 - AFTER TAKEOFF, SMOKE IN CABIN. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT, NOT OVERWEIGHT. R EPLACED RT ENGINE. ACCOMPLISHED ENGINE RUN WITH NO DEFECTS. SYSTEM GROUND CHECKED NORMAL OPERATION. SYSTEM FUNCTIONAL CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998031900947 19980319 00947 WP 1998 3 19 AALA980281 1 19980209 A 3350 SPLICE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 241AA 49254 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE FLOOD LIGHTS WERE INOPERATIVE. REPLACED LOOSE WIRE SPLICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900948 19980319 00948 WP 1998 3 19 AALA980274 1 19980209 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 279AA 49295 PHX - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED PORTABLE LIGH T AT FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900949 19980319 00949 WP 1998 3 19 AALA980269 1 19980207 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 422AA 49334 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHT STRIPS WERE INOPERATIVE. REPLACED LIGHT STRIPS AT FIRST CLASS EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900950 19980319 00950 WP 1998 3 19 AALA980280 1 19980209 A 3260 D128 SENSOR DOUG DC9 DC983 3022083 WP LT MLG DEFECTIVE A AALA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 564AA 49346 SFO - FLT 1041 - DURING APPROACH SFO, GEAR WAS EXTENDED AND THE LEFT MAIN GEAR INDICATED IT WAS NOT DOWN AND LOCKED. CR EW ACCOMPLISHED ALTERNATE GEAR EXTENSION AND LANDED SFO WITHOUT FURTHER INCIDENT. AIRCRAFT GEAR WAS PINNED AND THE AIRC RAFT WAS TOWED TO THE GATE. MAINTENANCE PERFORMED A BITE CHECK OF THE PROXIMITY BOX WITH NO FAULTS NOTED. AS A PRECAUT IONARY, THE LEFT DOWN LOCK SENSOR WAS CHANGED AND THE GEAR OPERATED NORMALLY WHEN CYCLED SEVERAL TIMES. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998031900951 19980319 00951 NM 1998 3 19 AALA980308 1 19980212 A 3350 1721651 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 360AA 24041 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 24HJ WOULD NOT ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT ROW 24HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998031900952 19980319 00952 NM 1998 3 19 AALA980305 1 19980211 A 3350 7002403 MODULE GRIMES BOEING 767 767323 1385205 NM CABIN MISSING A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380AN 1834 25449 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EVACUATION ALERT MODULE WAS MISSING AT FLIGHT ATTENDANT STATION RIGHT SIDE NEAR MID GALLEY. REPLACED MISSING EMERGENCY EVACUATION ALERT MODULE AT FLT ATTENDANT STATION RIGHT SIDE NEAR MID GALLE Y. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998031900953 19980319 00953 NM 1998 3 19 AALA980249 1 19980204 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621AM 24579 DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT LIGHT STRIP INOPERATIVE. REPLACED AFT EMERGENCY LIGHT STRIP. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998031900954 19980319 00954 NM 1998 3 19 AALA980255 1 19980205 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 647AM 24605 DFW - DURING OVERNIGHT CHECK, FORWARD GALLEY EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FORWARD GA LLEY EMERGENCY EXIT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998031900955 19980319 00955 NM 1998 3 19 AALA980268 1 19980207 A 3350 SOCKET BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388AA 27448 SFO - DURING OVERNIGHT MAINTENANCE, AFT SLIDE GROUND EMERGENCY EXIT LIGHT ON LEFT FUSELAGE WAS INOPERATIVE. CLEANED COR RODED LIGHT SOCKET AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998031900956 19980319 00956 NM 1998 3 19 AALA980171 1 19980119 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 381AN 25450 SFO - DURING MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 34H INOPERATIVE. REPAIRED BROKEN WIRE AND REPLACED PIN AND C ONNECTOR FOR EMERGENCY EXIT LIGHT AT PAX SEAT 34H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998031900957 19980319 00957 NM 1998 3 19 AALA980234 1 19980201 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 668AA 25333 SNA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST AND COACH CLASS WERE INOPERATIVE. REPLACED EMERGENCY FLOOR PATH LIGHTING FORWARD AND AFT MODULES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998031900958 19980319 00958 NM 1998 3 19 AALA980225 1 19980127 A 3350 0201804001 LIGHT BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352AA 24033 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 40H INOPERATIVE. REPLACED BROKEN EMERGENCY E XIT LIGHT ASSEMBLY AT PASSENGER SEAT 40H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998031900959 19980319 00959 NM 1998 3 19 AALA980231 1 19980129 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 612AA 24488 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998031900960 19980319 00960 NM 1998 3 19 AALA980205 1 19980124 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372AA 25199 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 24H INOPERATIVE. REPLACED BROKEN PINS IN EME RGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998031900961 19980319 00961 NM 1998 3 19 AALA980219 1 19980127 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 32HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CO NNECTOR AT PAX SEAT 32HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998031900962 19980319 00962 EU 1998 3 19 AALA980226 1 19980128 A 2913 862536 HYD PUMP FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 1414D HG24578 11377 DFW - FLT 504 - DURING CLIMB-OUT FROM DFW, HYDRAULIC SYSTEM NR 1 INDICATED OVERHEAT CONDITION. CREW FOLLOWED ALTERNATE PROCEDURES TURNING OFF SYSTEM NR 1 PUMPS ON ENGINES ONE AND TWO. AFTER A FEW MINUTES THE OVERHEAT INDICATION STOPPED AN D THE AIRCRAFT AIR INTERRUPTED, RETURNED AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED ENGINE DRIVEN HYDRAULIC PUMP (SYSTEM NR 1) ON NR 1 ENGINE, CHECKS OK WITH NO OVERHEATING. SYSTEM GROUND/LEAK CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998031900963 19980319 00963 WP 1998 3 19 AALA980312 1 19980216 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446AA 49472 DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN TAIL COMPARTMENT INOPERATIVE. REPLACED BROKEN EMERGENCY LIGHT WIRE AT TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998031900965 19980319 00965 EU 1998 3 19 UF6A980130 1 19980128 A 3350 GE1317 BULB BAG ATP ATP EU COCKPIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 12926 2028 FLIGHT DECK EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED FLIGHT DECK EMERGENCY LIGHT. SYSTEM OPS CHECKED GOO D. (M) 2 L 7 2 4T RT A27NM 1998031900966 19980319 00966 EU 1998 3 19 UF6A980108 1 19980105 A 3020 9TC425 CIRCUIT BREAKER BAG ATP ATP EU LT/RT ENGINE TRIPPED A UF6A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 856AW 12104 2032 ORD - FLT 5712 - DE-ICING FAULT ON BOTH ENGINES WITH THE MASTER PBSI DEPRESSED. WHEN PBSI IS RELEASED, GET LIP ON NORMA L INDICATION. MAINTENANCE RESET CIRCUIT BREAKER 1HK37 AND 2HK37. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900967 19980319 00967 EU 1998 3 19 UF6A980109 1 19980108 A 3350 LIGHTS BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 858AW 2035 SBN - FLT 5751 - EMERGENCY LIGHTS ARE OUT OVER ROW 11. MAINTENANCE INSPECTED, NO DEFECTS NOTED. SYSTEM OPS CHECKED GOO D. (M) 2 L 7 2 4T RT A27NM 1998031900968 19980319 00968 EU 1998 3 19 UF6A980206 1 19980212 A 3150 T/O WARNING BAG ATP ATP EU COCKPIT ILLUMINATED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 857AW 2034 ORD - FLT 5717 - TAKEOFF CONFIGURATION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK OF SY STEM. SYSTEM OPS CHECKED GOOD, NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1998031900969 19980319 00969 EU 1998 3 19 UF6A980208 1 19980213 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 SBN - LEFT AFT EMERGENCY FUSELAGE LIGHT BURNED OUT. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. ( M) 2 L 7 2 4T RT A27NM 1998031900970 19980319 00970 EU 1998 3 19 UF6A980209 1 19980216 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - EMERGENCY LIGHT IN AFT GALLEY OVERHEAD POSITION INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998031900971 19980319 00971 NE 1998 3 19 UF6A980205 2 19980211 A 7532 311171202 BLEED VALVE BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE FAILED A UF6A A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 31 852AW 11155 9W574 2021 124403 ORD - FLT 5708 - IN CLIMB, ITT AND NH WERE APPROACHING RED LINE ON LEFT ENGINE. PULLED POWER LEVERS BACK AS TO NTO EXCE ED LIMITS. MAINTENANCE INSPECTED SYSTEM AND FOUND HANDLING BLEED VALVE AT FAULT. REMOVED AND REPLACED HANDLING BLEED V ALVE AND SERVO VALVE. POWER ASSURANCE RUNS OPS CHECKED SATISFACTORY. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998031900972 19980319 00972 1998 3 19 UF6A980210 4 19980217 A 2565 2077000 SLIDE BAG ATP ATP EU PAX DOOR FAILED TEST A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 12467 121 2021 SBN - FORWARD PASSENGER DOOR EVACUATION SLIDE FAILED BATTERY FUNCTION TEST. MAINTENANCE REMOVED AND REPLACED EVACUATION SLIDE. (M) 2 L 7 2 4T RT A27NM 1998031900973 19980319 00973 EU 1998 3 19 UF6A980207 1 19980213 A 3250 STEERING BAG ATP ATP EU CABIN MALFUNCTIONED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 31 858AW 2035 PIA - FLT 5745 - ON TAKEOFF AT ABOUT 60 KNOTS, THE NOSEWHEEL STEERING STOPPED WORKING. STARTED OPERATING AFTER ABORT. M AINTENANCE INSPECTED AND PERFORMED OPS CHECK OF SYSTEM. SYSTEM OPS CHECKED GOOD. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1998031900974 19980319 00974 EU 1998 3 19 UF6A980211 1 19980218 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 12226 2034 SBN - AFT OVERHEAD GALLEY EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998031900975 19980319 00975 EU 1998 3 19 UF6A980131 1 19980131 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 9887 16361 2032 SBN - NR 4 EMERGENCY BATTERY PACK INOP. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY BATTERY PACK. SYSTEM OPS CHECK ED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900976 19980319 00976 EU 1998 3 19 UF6A980202 1 19980207 A 3350 GE718 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 13666 2021 SBN - EMERGENCY EXIT LIGHT INOP AT AFT PASSENGER DOOR. MAINTENANCE REMOVED AND REPLACED LIGHT BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900977 19980319 00977 EU 1998 3 19 UF6A980129 1 19980128 A 3350 GE1317 BULB BAG ATP ATP EU PAX DOOR FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 12926 2028 SBN - ENTRY WAY OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED ENTRY WAY OVERHEAD EMERGENCY LIGHT. SY STEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900978 19980319 00978 EU 1998 3 19 UF6A980128 1 19980126 A 5270 9EN4081BT1BB2 SWITCH BAG ATP ATP EU PAX DOOR DIRTY A UF6A K NONE N FALSE WARNING UK UNKNOWN 1 GL 31 855AW 12407 2029 AZO - FLT 5707 - AFT RIGHT FUSELAGE DOOR EXIT CWP ILLUMINATED IN FLIGHT INTERMITTENTLY. MAINTENANCE CLEANED MICROSWITCH AND PERFORMED OPS CHECK OF DOOR. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900982 19980319 00982 EU 1998 3 19 UF6A980116 1 19980112 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 13520 2021 SBN - LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT IS OUT. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOO D. (M) 2 L 7 2 4T RT A27NM 1998031900983 19980319 00983 EU 1998 3 19 UF6A980117 1 19980113 A 3350 LIGHT BAG ATP ATP EU CABIN NO TEST A UF6A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 858AW 2035 CWA - FLT 5732 - EMERGENCY LIGHTING WILL NOT TEST. MAINTENANCE PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTING. SYSTE M OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900984 19980319 00984 EU 1998 3 19 UF6A980120 1 19980115 A 3350 362624 LAMP BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 851AW 13722 2020 ORD - FLT 5766 - EMERGENCY FLOOR LIGHTING BETWEEN ROWS 2 AND 4 IS INOP. MAINTENANCE REMOVED AND REPLACED FLOOR PROXIMIT Y STRIP. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900985 19980319 00985 EU 1998 3 19 UF6A980106 1 19980105 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 13657 2020 SBN - RIGHT AFT EXTERIOR EMERGENCY LIGHT IS OUT. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900986 19980319 00986 EU 1998 3 19 UF6A980107 1 19980105 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 13657 2020 SBN - LEFT AFT OVERWING EXTERIOR EMERGENCY LIGHT IS OUT. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOO D. (M) 2 L 7 2 4T RT A27NM 1998031900987 19980319 00987 EU 1998 3 19 UF6A980104 1 19980103 A 6120 PROP FEATHER SYS BAG ATP ATP EU NR 2 ENGINE INOP A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 859AW 2036 ORD - FLT 5736 - NR 2 PROP DID NOT FULLY FEATHER WHEN ENGINE WAS SHUTDOWN. MAINTENANCE INSPECTED AND RAN NR 2 ENGINE. S YSTEM OPS CHECKED WITHIN LIMITS. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1998031900988 19980319 00988 EU 1998 3 19 UF6A980110 1 19980108 A 3350 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 858AW 2035 SBN - FLT 5751 - FLOOR EMERGENCY LIGHTS ARE INOP AT ROW 9. MAINTENANCE INSPECTED, NO DEFECTS NOTED. SYSTEM OPS CHECED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900989 19980319 00989 1998 3 19 UF6A980111 4 19980108 A 3425 EFIS BAG ATP ATP EU COCKPIT ILLUMINATED A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 857AW 2034 ORD - FLT 5735 - ON TAKEOFF ROLL EFIS CWP ILLUMINATED AND X-MON WAS DISPLAYED. MAINTENANCE INSPECTED AND PERFORMED OPS CHECK. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900990 19980319 00990 EU 1998 3 19 UF6A980105 1 19980104 A 3350 58786 LIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 11966 2034 ORD - FLOOR EMERGENCY LIGHTING AT ROW 4 AND 6 C/D INOP. MAINTENANCE REMOVED AND REPLACED FLOOR LIGHT STRIPS AT ROW 3, 4 , 5, 6. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900991 19980319 00991 EU 1998 3 19 UF6A980112 1 19980108 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 9684 2021 ORD - EMERGENCY EXIT LIGHT AT ROW 16CD INOP. MAINTENANCE REMOVED AND REPLACED NR 6 EMERGENCY LIGHT POWER SUPPLY. SYSTE M OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900992 19980319 00992 EU 1998 3 19 UF6A980113 1 19980107 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 9684 2021 ORD - ROW 13-14CD EMERGENCY FLOOR LIGHTING INOP. MAINTENANCE REMOVED AND REPLACED NR 6 EMERGENCY LIGHT POWER SUPPLY. S YSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900993 19980319 00993 EU 1998 3 19 UF6A980123 1 19980119 A 3350 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 854AW 2028 FWA - FLT 5722 - EMERGENCY FLOOR LIGHTING IMMEDIATELY BEHIND ORANGE STRIP INOP. MAINTENANCE INSPECTED, NO DEFECTS NOTED . SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998031900999 19980319 00999 1998 3 19 ARWA980305 4 19980318 A 3414 O-RING DOUG DC8 DC863F 302198F WP AIR SPEED IND FAILED A ARWA O OTHER O OTHER TO TAKEOFF 1 SO 19 661AV 45969 AFTER T/O, CAPTAIN AIRSPEED DECREASING AND ALTIMETER READING LOW, BOTH UNREALIABLE. FOUND DAMAGED O-RING ON STATIC SIDE OF CAPTAIN A/S INDICATOR. REMOVED AND REPLACED O-RIGN, OPS CK. SYSTEM OK IAW MM 34-12-0. 2 L 7 4 4F 4A25 1998032400001 19980324 00001 WP 1998 3 24 AALA980175 1 19980119 A 5320 PAN DOUG DC10 DC1030 3023501 WP BS 1972 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 164AA 46950 TUL - FOUND CORROSION ON LAVATORY WASTE BOX PAN. INSTALLED NEW LAVATORY WASTE PAN PER SRM 51-01-00-5. (M) 2 L 7 3 4F A22WE 1998032400002 19980324 00002 EU 1998 3 24 SIMA980532 1 19980222 A 3350 167006 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 427MQ 091 ORD - FLT 4005 - A COUPLE OF EMERGENCY EXIT (PATH LIGHTS) ON FLOOR OUT. REPLACED BULBS, OPS CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998032500002 19980325 00002 SO 1998 3 25 SWIA971092 1 19980201 A 3010 DE-ICE SYST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT/RT SYST MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION CL CLIMB 1 NM 07 293SW 120320 OUTBOARD LEFT AND OUTBOARD RIGHT DE-ICE BOOTS AND ENGINE INLET ON RIGHT SIDE WENT INOP WHEN ACTUATED. RETURNED TO LAX. PERFORMED FUNCTIONAL CHECK OF ALL EJECTOR VALVES AND CLEANED CANNON PLUGS ON DE-ICE MONITOR. ALL CHECKS GOOD AT THIS T IME. 2 L 7 2 4T 4 T RT A31SO E20NE 1998032500003 19980325 00003 1998 3 25 HEEA0013272 4 19980304 A 2562 ELT910 ELT NARCO BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 513EH 45421 NARCO ELT BATTERY WEAK. 1 G 7 1 3U H2SW 1998032500005 19980325 00005 NM 1998 3 25 AWXA9800072 1 19980307 A 3350 900835A BATTERY BOEING 737 7372U9 1384498 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 D-EMERGENCY EXIT LIGHTS ALONG SIDE DOORS L1 R1 AND RT OVERWING INOP. REMOVED AND REPLACED BATTERY CARTRIDGE ASSY. OPS GOOD AT THIS TIME. 2 L 7 2 4F RT A16WE 1998032500006 19980325 00006 WP 1998 3 25 ABXA9800191 1 19980311 A 5320 99577397N SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND SHEAR TIE CRACKED IN RADIUS AT STATION 945 BETWEEN LONGERON 15R AND 16R. REPLACED SHEAR-TIE IAW D C9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998032500007 19980325 00007 NM 1998 3 25 98ZZZX1075 1 19980213 A 2910 65445101387 HYDRAULIC TUBE BOEING 737 7372H5 138448E NM WS 260 CHAFED A E9WA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SO 05 220US 20453 FLT 992/23 NCO - LOST A-HYDRAULIC SYSTEM PRESSURE AND QUANTITY AFTER TAKEOFF CLIMBING THROUGH APPROX 3,500 FEET. COMPLE TED EMERGENCY CHECK LIST. BURNED OFF EXCESS FUEL AND LANDED WITH AIRCRAFT WEIGHT AT 96,100 POUNDS. GEAR PINS INSTALLED FOR TOWING. INSPECTED ACFT, FOUND A-SYSTEM PRESSURE LINE RUPTURED DUE TO CHAFING ON LOWER WING ACCESS PANEL. DAMAGED LINE REMOVED AND A TEMPORARY HIGH PRESSURE FLEX LINE INSTALLED, ENGINES NR 1 AND NR 2 CASE DRAIN FILTERS REMOVED AND INS PECTED FOR DEBRIS. NONE FOUND, NEW FILTERS INSTALLED. HYDRAULIC SYSTEM REPLENISHED. OPERATIONAL CHECK DONE. OPS CHEC K GOOD. ALL WORK DONE IAW BOEING MM CHAP 29-00. TEMPORARY LINE TO BE REPAIRED. 2 L 7 2 4F A16WE 1998032500010 19980325 00010 NM 1998 3 25 98UAL900112 1 19980304 A 5101 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AIRFRAME VIBRATIONS A UALA O OTHER E VIBRATION/BUFFET TX TAXI/GRND HDL 1 WP 29 7449U 21903 UPON LANDING ROLLOUT CREW REPORTED VIBRATIONS IN THE AIRFRAME. UPON TAXIING CREW NOTICED CONDITION GETTING WORSE AND EL ECTED TO STOP. PASSENGERS DEPLANED AND AIRCRAFT TOWED TO HANGER. 2 L 7 3 4F 4 F A3WE E2EA 1998032600001 19980326 00001 WP 1998 3 26 VJ9800050 1 19980228 A 5330 1A309911A30992 SKIN DOUG DC9 DC932 3022066 WP BS 980 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 909VJ 47322 AFT CARGO FUSELAGE SKIN AND FRAME ARE CORRODED HEAVILY ON AFT SIDE AT FRAME STA 980 BETWEEN LONG 28 R AND 27R. CUT OUT AREA OF PLATING BETWEEN L27R AND 28R. FABBED FILLER 2024 T3 .50, FABBED DOUBLER 2024 T3 .025. FABBED FINGER DOUBLER 20 24 T3 IAW DC-9 SRM 51-10-2. TREATED AND PRIMED IAW DC-9 SRM 51-10-3, INSTALLED IAW AERO EO 98-802. 2 L 7 2 4F A6WE 1998032600002 19980326 00002 WP 1998 3 26 VJ9800051 1 19980318 A 3350 110049 BATTERY CHARGER DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 921VV 47284 EMERGENCY LIGHTS INOP FROM ROWS 24 BACK INTO TAIL COMPARTMENT. REPLACED AFT CEILING BATTERY CHARGER. 2 L 7 2 4F A6WE 1998032600003 19980326 00003 SO 1998 3 26 RAAA98E9009 1 19980220 A 6120 6526175 ADAPTER ALLSN 6503835 LKHEED 188 188C 5262604 SO ALLSN A6441 A6441FN606 GL NR 1 PROPELLER WORN A RAAA E ENGINE SHUTDOWN E VIBRATION/BUFFET IN INSP/MAINT 1 AL 03 1968R 4336 F12273 188C2007 P395 AFTER COMPLETION OF NR 4 PROPELLER INSTALLATION GROUND RUN WITH ENGINES IN HIGH SPEED GROUND IDLE AND POWER LEVERS IN GR OUND RANGE MAINT PERSONNEL NOTED HEAVY, ABNORMAL VIBRATION. SHUTDOWN NR 4 ENGINE WITH EMERGENCY HANDLE AND VIBRATION CO NTINUED. VIBRATION CHANGE NOTED WITH NR 1 ENGINE POWER LEVER MOVEMENT. SHUTDOWN NR 1 ENGINE WITH EMERGENCY HANDLE AND VIBRATION CEASED. FOUND NR 1SPINNER HAD DEPARTED AIRCRAFT, DAMAGING 2 NR 1 PROPELLER BLADE CUFFS, DUE EXCESSIVELY WORN RESERVOIR ADAPTER THREADS. REPLACED NR 1 PROPELLER, SPINNER AND RESERVOIR ADAPTER. INITIATED FLEET CAMPAIGN ITEM TO CH ECK RESERVOIR ADAPTER THREADS FOR EXCESSIVE WEAR. 2 L 7 4 4T 4A22 6 C P898 1998032600004 19980326 00004 NM 1998 3 26 RAAA98B2015 1 19980317 A 5712 RIB BOEING 727 72722C 138400F NM WS 601.5 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-127 FOUND LEFT WS 601.5 RIB LOWER CHORD CRACKED APPROX 1.5 INCHES AT S-6 ATTACH. REPAIRED PER SRM 57-10-5, FIG 1 M-54 NR 2. 2 L 7 3 4F A3WE 1998032600005 19980326 00005 NM 1998 3 26 RAAA98B2016 1 19980317 A 5712 RIB BOEING 727 72722C 138400F NM WS 601.5 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-127, FOUND LEFT WS 601.5 RIB UPPPER CHORD CRACKED APPROX 1.0 IN A T S-14 ATTACH. REPAIRED PER SRM 57-10-5, FIG 1 M-54 NR 1. 2 L 7 3 4F A3WE 1998032600006 19980326 00006 NM 1998 3 26 CALA9800471 1 19980317 A 3610 BLEED LINES BOEING 737 7373T0 1384582 NM RIGHT LOOSE A CALA B G EMER. DESCENT O2 MASK DEPLOYED O OTHER CR CRUISE 1 SW 09 14347 23585 CABIN PRESSURE WAS LOST WHILE EN ROUTE FROM IAH TO CZM. THE RIGHT PACK OUTPUT WENT TO ZERO. AN EMERGENCY DESCENT WAS P ERFORMED AND THE O2 MASKS WERE DEPLOYED. THE AIRCRAFT LANDED AT CZM WITHOUT FURTHER EVENT. MAINTENANCE FOUND HIGH BLEE D REGULATOR LINES LOOSE. THE LINES WERE REPOSITIONED AND TIGHTENED AND OPERATIONAL CHECKS WERE GOOD. IN ADDITION, THE O2 GENERATORS WERE REMOVED AND REPLACED. THE O2 MASKS WERE REPACKED AND LATCH SYSTEMS CHECKED IAW MM 35-22-11. 2 L 7 2 4F RT A16WE 1998032600007 19980326 00007 NM 1998 3 26 CALA9800472 1 19980317 A 2913 6507506 HYD PUMP BOEING 727 727232 1384082 NM NR 2 ENGINE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 10791 2801 20645 THE 'A' SYSTEM HYDRAULIC RESERVOIR QUANTITY WENT TO ZERO AND LOW PRESSURE LIGHTS ILLUMINATED WHILE EN ROUTE FROM MSY TO IAH. THE HYDRAULIC QUANTITY LOSS AND HYDRAULIC SYSTEM FAILURE CHECKLISTS WERE COMPLETED. THE LANDING GEAR WAS CRANKED DOWN AND THE FLAPS WERE LOWERED ELECTRICALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP CASE LEAKING. BOTH THE NR 1 AND NR 2 HYDRAULIC PUMPS WERE REMOVED AND REPLACED. THE HYDRAULIC SY STEMS WERE SERVICED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1998032600008 19980326 00008 NM 1998 3 26 CALA9800473 1 19980317 A 3233 273N10045 ACTUATOR BOEING 757 757224 1384958 NM NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 18119 27561 THE EICAS GEAR DISAGREE AND GEAR AMBER LIGHT ILLUMINATED AFTER GEAR RETRACTION WITH GEAR HANDLE IN THE UP POSITION. MOV ING THE GEAR HANDLE TO THE OFF POSITION REMOVED BOTH WARNINGS. NOSE GEAR RETRACTION SEEMED LONGER THAN NORMAL. THE FLI GHT CONTINUED TO EWR WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR RETRACT ACTUATOR IAW MM 32 -34-01. AN ADJUSTMENT/TEST OF THE NOSE GEAR WAS PERFORMED IAW MM 32-34-00. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A2NM 1998032600009 19980326 00009 WP 1998 3 26 CALA9800474 1 19980317 A 5320 FLANGE DOUG DC10 DC1030 3023501 WP BS 1781 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1781, STRINGER 47-48R. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED, THE AREA REWORKED AND REINFORCED WITH SPLICE AND RIVETED IAW SRM 53-15-01 , FIGURE 12, 53-30-00, FIGURE 5, 53-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600010 19980326 00010 WP 1998 3 26 CALA9800475 1 19980317 A 5320 CHORD DOUG DC10 DC1030 3023501 WP BS 1781 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LOWER CHORD IN CENTER CARGO AREA CORRODED AT STA 1781, STRINGER 51. THE CORRODED AREA WAS REMOVED AND THE AREA WAS REWORKED. A NEW PART WAS INSTALLED USING RIVETS AND REINFORCED WITH SHEAR CLIP IAW SRM 53-30-00, FIGURE 9, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600011 19980326 00011 WP 1998 3 26 CALA9800476 1 19980317 A 5320 CHORD DOUG DC10 DC1030 3023501 WP BS 1761 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LOWER CHORD IN CENTER CARGO AREA CORRODED AT STA 1761, STRINGER 51 TO 47L. THE CORRODED AREA WAS REMOV ED. A NEW PART AND SHEAR CLIP WERE FABRICATED IAW SRM 51-20-00. THE AREA WAS REWORKED, REINFORCED, AND RIVETED IAW 53- 30-00, FIGURE 9 AND 51-31-01. 2 L 7 3 4F A22WE 1998032600012 19980326 00012 WP 1998 3 26 CALA9800477 1 19980317 A 5320 FLANGE DOUG DC10 DC1030 3023501 WP BS 1761 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1761, STRINGER 48. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED IAW SRM 53-15-01, FIGURE 12. THE AREA WAS REWORKED AND REINFORCED WITH A SPLI CE AND RIVETED IN PLACE IAW SRM 53-30-00, FIGURE 5, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600013 19980326 00013 WP 1998 3 26 CALA9800478 1 19980317 A 5320 FLANGE DOUG DC10 DC1030 3023501 WP BS 1741 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1741, STRINGER 48. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. A NEW CHORD WAS FABRICATED IAW SRM 53-15-01, FIGURE. THE AREA WAS REWORKED, REINFORCED WITH SPLICE, AND INSTALLED USING RIVETS IAW SRM 53-30-00, FIGURE 5, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600014 19980326 00014 WP 1998 3 26 CALA9800479 1 19980317 A 5320 FLANGE DOUG DC10 DC1030 3023501 WP BS 1821 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LOWER FLANGE IN CENTER CARGO AREA CORRODED AT STA 1821, STRINGER 51. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT, REWORKED, AND REINFORCED WITH SHEAR CLIP IAW SRM 53-30-00, FIGURE 9. NEW PARTS WERE FABRICATED AND INSTAL LED USING RIVETS IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998032600015 19980326 00015 WP 1998 3 26 CALA9800480 1 19980317 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1521-1541 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LONGERON 48L CORRODED IN CENTER CARGO AREA AT STA 1521-1541. THE CORRODED AREA WAS CLEANED AND BLENDED OUT. A NEW ANGLE WAS FABRICATED, THE AREA WAS REWORKED, AND REPAIR WAS INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998032600016 19980326 00016 WP 1998 3 26 CALA9800481 1 19980317 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1581-1601 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND STRINGER 52 CORRODED IN CENTER CARGO AREA AT STA 1581-1601. THE STRINGER WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 51-21-01. 2 L 7 3 4F A22WE 1998032600017 19980326 00017 WP 1998 3 26 CALA9800482 1 19980318 A 3260 SWITCH DOUG DC9 DC932 3022066 WP LT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 18513 48112 THE LEFT GEAR UNSAFE LIGHT ILLUMINATED AFTER TAKEOFF FROM ABQ. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. THE FLI GHT WAS CONTINUED TO IAH WITH PUMPS IN HIGH AND WHEN GEAR WAS EXTENDED INDICATIONS WERE NORMAL. MAINTENANCE REPLACED TH E OVERLINK SWITCH. THE GEAR WAS SIMULATED UP AND DOWN AND ALL INDICATIONS WERE NORMAL. 2 L 7 2 4F A6WE 1998032600018 19980326 00018 WP 1998 3 26 CALA9800483 1 19980318 A 2910 S7931874L40200 HYD HOSE DOUG DC10 DC1030 3023501 WP NR 2 HYD SYST PUNCTURED A CALA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 13066 46591 THE NR 2 HYDRAULIC SYSTEM QUANTITY WAS LOST WHILE EN ROUTE FROM IAH TO LGW. THE AIRCRAFT LANDED AT LGW WITHOUT INCIDENT . MAINTENANCE FOUND HYDRAULIC LINE FROM 2-3 REVERSIBLE MOTOR PUMP PUNCTURED AND THE FORWARD SHUTOFF VALVE OF 2-3 REVERS IBLE MOTOR PUMP WAS INOPERATIVE. THE SHUTOFF VALVE WAS REMOVED AND REPLACED. THE HYDRAULIC LINE WAS REPLACED USING FLEX HOSE AND A DIP WAS ISSUED TO REPLACE THE HOSE WITHIN 500 FLIGHTS OR 1200 FLIGHT HOURS. IN ADDITION, BOTH THE LT AND RT HYDRAULIC PUMPS WERE REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1998032600019 19980326 00019 WP 1998 3 26 CALA9800484 1 19980317 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1293 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND INTERIOR UPPER LOBE CABIN FLOORBEAM BROKEN AT STA 1293, RBL 103. THE FLOORBEAM WAS REPAIRED IAW ECRA 5 320-01511 AND ENGINEERING ORDER MF MAN D10-53-896798. 2 L 7 3 4F A22WE 1998032600020 19980326 00020 WP 1998 3 26 CALA9800485 1 19980317 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1275 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND INTERIOR UPPER LOBE CABIN FLOORBEAM BROKEN AT STA 1275, RBL 103. THE FLOORBEAM WAS REPAIRED IAW ECRA 5 320-01511 AND ENGINEERING ORDER MF MAN D10-53-896798. 2 L 7 3 4F A22WE 1998032600021 19980326 00021 WP 1998 3 26 CALA9800486 1 19980318 A 5210 21182008 ACTUATOR DOUG DC10 DC1030 3023501 WP PAX DOOR FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15069 46584 INSPECTION FOUND PASSENGER DOOR MID LEFT INOPERATIVE. THE ROTARY ACTUATOR WAS REMOVED AND REPLACED AND OPERATION CHECKE D GOOD. 2 L 7 3 4F A22WE 1998032600022 19980326 00022 WP 1998 3 26 CALA9800487 1 19980318 A 5321 FLOOR WEB DOUG DC10 DC1030 3023501 WP BS 879 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 5 INCH CRACK ON FORWARD CARGO LOWER FLANGE OF FLOOR WEB AT STA 879 LBL 50. THE FLANGE WAS TRIMMED AN D BLENDED OUT AND THE AREA WAS REWORKED. TWO ANGLES WERE INSTALLED IAW SRM 53-00-01, FIGURE 3, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600023 19980326 00023 WP 1998 3 26 CALA9800488 1 19980318 A 5320 FLOOR POST DOUG DC10 DC1030 3023501 WP BS 1100 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND CABIN FLOOR POST BROKEN IN FORWARD CARGO AREA AT STA 1100. THE AREA WAS TRIMMED AND BLENDED OUT. A RE PAIR CHANNEL, ANGLE, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-20-00 AND ENGINEERING ORDER MF MAN D10-53-86801 . 2 L 7 3 4F A22WE 1998032600024 19980326 00024 WP 1998 3 26 CALA9800489 1 19980318 A 5350 MOUNT DOUG DC10 DC1030 3023501 WP TAIL CONE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND TAILCONE UPPER SECTION RT WORK PLATFORM FORWARD MOUNT RIVETS LOOSE AND CRACKED. THE MOUNT WAS REMOVED AND A NEW MOUNT WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-52-01, FIGURE 2. 2 L 7 3 4F A22WE 1998032600025 19980326 00025 WP 1998 3 26 CALA9800490 1 19980318 A 5510 T-PROFILE DOUG DC10 DC1030 3023501 WP RT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND SEVERAL 1 CRACKS IN INBOARD AND OUTBOARD ATTACH FLANGES OF RT HORIZONTAL STABILIZER NR 3 LEADING EDGE T -PROFILE. THE STRAP AND T-PROFILE WERE REMOVED. A NEW T-PROFILE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00 AND 51-3 1-01. 2 L 7 3 4F A22WE 1998032600026 19980326 00026 WP 1998 3 26 CALA9800491 1 19980318 A 5320 JAMB DOUG DC10 DC1030 3023501 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND LOWER AFT CARGO DOOR JAMB CORRODED BETWEEN STA 1921 AND 1942. THE CORRODED AREA WAS REMOVED. REPAIR P ARTS WERE FABRICATED AND INSTALLED IAW SRM 51-21-01, 53-50-00, FIGURE 15A, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600027 19980326 00027 WP 1998 3 26 9804571225 1 19980303 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1501-1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING M CHECK, FOUND CORROSION ON BELLY SKIN AT FS 1501-1531, LONGERON 48L-48R. REPAIRED PER EA 12-154586. 2 L 7 3 4F A22WE 1998032600028 19980326 00028 WP 1998 3 26 9804589947 1 19980207 A 5711 SPAR WEB DOUG DC9 DC931 3022065 WP WS 58 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8938E 47161 DURING H CHECK, FOUND A CRACK IN THE UPPER AFT SPAR IN THE CENTER TANK ACROSS THE VERTICAL LEG RADIUS AT WS 58. REPAIRE D PER EA 99-153041. 2 L 7 2 4F A6WE 1998032600029 19980326 00029 WP 1998 3 26 9804599974 1 19980307 A 5320 JAMB DOUG DC9 DC931 3022065 WP BS 996 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING M CHECK, FOUND CRACK IN THE AFT ENTRY DOOR JAMB WEB FS 996 AT RIGHT LOWER DOOR STOP PLATE. REPAIRED PER EA 99-15 4754. 2 L 7 2 4F A6WE 1998032600030 19980326 00030 WP 1998 3 26 9804609103 1 19980212 A 5330 SKIN DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 93S 47078 DURING LINE CHECK, FOUND CRACK IN FUSELAGE SKIN AROUND WINDOW 5L FRAME. REPAIRED PER EA 91-154696. 2 L 7 2 4F A6WE 1998032600031 19980326 00031 1998 3 26 COMA9810069 4 19980317 A 2210 AUTO PILOT EMB 120 EMB120RT SO E/E COMPT MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 179CA 120179 AUTOPILOT AND TRIM FAIL WARNING DURING TAKEOFF. DEFERRED AUTOPILOT SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1998032600032 19980326 00032 SO 1998 3 26 COMA9810070 1 19980318 A 7712 TQ SIGNAL COND EMB 120 EMB120RT SO LT ENGINE MALFUNCTION A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 161CA 13120 28 120143 AUTO FEATHER SYSTEM DOES NOT TEST. REPLACED THE LEFT ENGINE TORQUE SIGNAL CONDITIONER. 2 L 7 2 4T RT A31SO 1998032600033 19980326 00033 EA 1998 3 26 COMA9860062 1 19980318 A 5610 NP1393212 WINDSHIELD CNDAIR CL600 CL6002B19 EA RT COCKPIT SHATTERED A COMA K NONE O OTHER CR CRUISE 1 SO 01 979CA 2684 7159 CO-PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1998032600034 19980326 00034 EA 1998 3 26 COMA9860063 1 19980317 A 3010 14463102 DUCT CNDAIR CL600 CL6002B19 EA RT WING CRACKED A COMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 929CA 7035 WING ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED THE RIGHT WING BLEED AIR PICCOLO TUBE. 2 L 7 2 4F RT A21EA 1998032600035 19980326 00035 NM 1998 3 26 SWAA980318 1 19980317 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 332 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED 1/4D CHECK, FOUND SUPPORT ANGLE CRACK AT BS 332, LBL 62 BELOW CREASE BEAM. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F A16WE 1998032600036 19980326 00036 NM 1998 3 26 SWAA980319 1 19980317 A 5311 STUB FRAME BOEING 737 7373T5 NM BS 299 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D CHECK, FOUND CRACKED STUB FRAME AT BS 299, WL 210, RBL 55. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998032600037 19980326 00037 NM 1998 3 26 SWAA980320 1 19980317 A 5320 WEB BOEING 737 7373T5 NM BS 704-885 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D CHECK, FOUND CORROSION ON WEB AT BS 828 TO 830, WL 208, LBL 70; BS 704, WL 208, RBL 65; BS 878 TO 885 , RBL 70, WL 208;BS 901, WL 208, RBL 65. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998032600038 19980326 00038 NM 1998 3 26 SWAA980321 1 19980317 A 5315 FLOORBEAM BOEING 737 7373T5 NM BS 986 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM UPPER AND LOWER AT BS 986, RBL 44, WL 208. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998032600039 19980326 00039 NM 1998 3 26 SWAA980322 1 19980317 A 5320 SUPPORT BOEING 737 7373T5 NM BS 993 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT FITTING AT NAT 993, WL 208, LBL 34. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998032600040 19980326 00040 NM 1998 3 26 SWAA980323 1 19980317 A 3350 P4010021 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 59SW 21811 DURING WALK AROUND CHECK, FOUND FWD F/A POSITION INBD EMERGENCY FLASH LIGHT SEAL BROKEN TO DMAL. REMOVED AND REPLACED F WD INBD F/A LIGHT BATTERY PER BOEING MM. 2 L 7 2 4F A16WE 1998032600041 19980326 00041 NM 1998 3 26 SWAA980324 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 847, STR 8-9 RT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600042 19980326 00042 NM 1998 3 26 SWAA980325 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 887, STR 8-9 RT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600043 19980326 00043 NM 1998 3 26 SWAA980326 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 907, STR 8-9 RT. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998032600044 19980326 00044 NM 1998 3 26 SWAA980327 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKET AT A/C OUTLET ASSY ATTACH BRACKET AT BS 787, STR 8-9 LT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600045 19980326 00045 NM 1998 3 26 SWAA980328 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 807, STR 8-9 LT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600046 19980326 00046 NM 1998 3 26 SWAA980329 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 827, STR 8-9 LT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600047 19980326 00047 NM 1998 3 26 SWAA980330 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 847, STR 8-9 LT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600048 19980326 00048 NM 1998 3 26 SWAA980331 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 867, STR 8-9 LT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600049 19980326 00049 NM 1998 3 26 SWAA980332 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 887, STR 8-9 LT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600050 19980326 00050 NM 1998 3 26 SWAA980333 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 907, STR 8-9 LT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600051 19980326 00051 NM 1998 3 26 SWAA980290 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT A/C OUTLET ASSY ATTACH BRACKET AT BS 827, STR 8-9 RT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998032600052 19980326 00052 NM 1998 3 26 UPS98226151 1 19980317 A 5320 STRAP BOEING 727 72725C 138400H NM BS 328 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:C BROKEN TENSION STRAP UNDER MAIN CABIN FLOOR AT BS 328 BL 0, WL 200. REMOVED, FABRICATED REPAIR SPLICE AND INSTALLED IAW SRM 51-40-1, 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1998032600053 19980326 00053 NM 1998 3 26 UPS98526141 1 19980318 A 3350 BULB BOEING 757 75724APF 1384969 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 469UP 25485 INSPECTION TYPE:DAIL EXTERIOR EMERGENCY EXIT LIGHT BELOW CREW ENTRY DOOR INOP. RELAMPED, FUNCTION CHECK NORMAL. 2 L 7 2 4F RT A2NM 1998032600054 19980326 00054 WP 1998 3 26 UPS98826139 1 19980309 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C EXTERIOR FUSELAGE CENTER TANK AT STA 860 BLB 60 SUPPORT ANGLE IS CRACKED. STOP DRILLED CRACK AND REPA IRED IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1998032600055 19980326 00055 WP 1998 3 26 UPS98826140 1 19980310 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 510 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C STA 510 TO 550 BL 0, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED DAMAGED SECTION OF SEAT TRACK AND SP LICED REPLACEMENT SECTION FROM STA 430 TO 550 BL O IAW 53-2-3 FIG. 14. 2 L 7 4 4F RT 4A25 1998032600056 19980326 00056 WP 1998 3 26 UPS98826142 1 19980310 A 5347 3657503501 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C 2ND OBSERVERS FWD SEAT TRACK HAS HEAVY CORROSION, AROUND THE MOUNTING SCREWS. REMOVED AND REPLACED SE AT TRACK IAW SRM 51-3-1. 2 L 7 4 4F RT 4A25 1998032600057 19980326 00057 WP 1998 3 26 UPS98826143 1 19980312 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C STA.300, RBL59, THE SEAT TRACK IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK FROM STA 28 0-330 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998032600058 19980326 00058 WP 1998 3 26 UPS98826144 1 19980314 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C STA 1070 AT BL0 THE SEAT TRACK IS CORRODED. REMOVED, FABRICATED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998032600059 19980326 00059 WP 1998 3 26 UPS98826145 1 19980310 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1045 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C STA 1045 AT BLO, THE SEAT TRACK HAS HEAVY CORROSION, THE LOCK TANG ON RT SIDE IS CRACKING. REMOVED FA BRICATED REPLACEMENT SECTION OF TRACK FROM STA 990-1070 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998032600060 19980326 00060 WP 1998 3 26 UPS98826146 1 19980310 A 5753 37701441 FITTING DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C RT O/B SLOT TORQUE TUBE END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998032600061 19980326 00061 WP 1998 3 26 UPS98826147 1 19980310 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C STA 580 AT LBL 59, THE SEAT TRACK IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998032600062 19980326 00062 WP 1998 3 26 UPS98826148 1 19980314 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C LT WING L/E RIB ABOVE NR 1 ENGINE IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998032600063 19980326 00063 WP 1998 3 26 UPS98826149 1 19980310 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1230 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C STA 1230 AT LBL 59, THE SEAT TRACK IS CORRODED ALSO AT STA 1290. REMOVED, FABRICATED AND INSTALLED RE PLACEMENT SECTION OF TRACK FROM STA 1130 TO 1270 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998032600064 19980326 00064 WP 1998 3 26 UPS98826150 1 19980314 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1070-950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C STA 950 TO 1070 LBL 59, THE SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACE MENT SECTION OF TRACK FROM STA 930 TO 1070 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998032600065 19980326 00065 NM 1998 3 26 QXEA9800329 1 19980317 A 3350 6038441 POWER SUPPLY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 824PH 157 SEA - FORWARD TWO FLOOR PROXIMITY EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED RIGHT FORWARD POWER SUPPLY (3352-P2), OPE RATIONAL TEST IS GOOD. 2 H 7 2 4T RT A13NM 1998032600066 19980326 00066 WP 1998 3 26 98FDEA00206 1 19980318 A 5230 FRAME DOUG DC10 DC1010F 3022111 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 LOWER CENTER CARGO DOOR, FWD DOOR FRAME IS CRACKED AT STRIKER PLATE FOR ROLLER BEARING OF DOOR JAMS. *S/D* REMOVED DAM AGED SECTION OF FRAME UNDER STRINGER PLATE AS PER SRM 52-10-00 FIG 3 PG 12. FAB, REPAIR PARTS IN REF TO SRM 52-10-00. I NSTALLED PER SRM 52-10-00 8, PAINTED. 2 L 7 3 4F A22WE 1998032600067 19980326 00067 WP 1998 3 26 98FDEA00207 1 19980319 A 5320 SILL DOUG DC10 DC1010F 3022111 WP CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 SNRM N00923 - DOOR SILL FITTING CRACKED AFT CORNER, CENTER LOWER CARGO DOOR. REMOVED AND REPLACED CENTER CARGO DOOR, RE AR DOOR SILL FITTING AS NEEDED PER M/M 53-40-00. 2 L 7 3 4F A22WE 1998032600068 19980326 00068 NM 1998 3 26 98FDEA00205 1 19980318 A 3244 657276193 TIRE BOEING 727 72722 1384002 NM NR 4 MLG WHEEL MISSING A FDEA A UNSCHED LANDING E J D VIBRATION/BUFFET WARNING INDICATION INFLIGHT SEPARATION CL CLIMB 1 SO 25 193FE 19142 RIGHT OUTBOARD ANTI-SKID LIGHT BEGAN TO FLICKER DURING TAKEOFF ROLL, CAME ON SOLID AFTER ROTATION. ROC REPORTED, LOST T HE RIGHT MAIN TIRE (OUTBOARD). FOUND NR 4 TIRE MISSING. REMOVED BRAKE TO INSPECT AXLE SLEEVE. REMOVED AND REPLACED AX LE SLEEVE AND INSPECTED AXLE PER MAINTENANCE MANUAL 5-51-12 AND OVERHAUL MANUAL 32-12-01. REMOVED AND REPLACED NR 3 MA IN TIRE ASSEMBLY PER M/M 32-41-00 AND INSPECTED AXLE SLEEVE AND BEARINGS. REMOVED AND REPLACED NR 3 MAIN DUE TO NR 4 TI RE MISSING. REPLACED NR 4 BRAKE PER M/M. 2 L 7 3 4F A3WE 1998032600069 19980326 00069 WP 1998 3 26 ABXA9800225 1 19980228 A 5320 4645517502 TIE FITTING DOUG DOUG DC8 DC863F 302198F WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FLOORBEAM STA 680 RBL-24 TO WING BOX TIE FITTING CRACKED. REPAIRED IAW DWG 4645517 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998032600070 19980326 00070 WP 1998 3 26 ABXA9800226 1 19980218 A 5712 576946617 RIB DOUG DOUG DC8 DC863F 302198F WP WS 622.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 622.25. REPAIRED IAW DWG K 05056 AND DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998032600071 19980326 00071 WP 1998 3 26 ABXA9800227 1 19980220 A 5712 576946627 RIB DOUG DOUG DC8 DC863F 302198F WP WS 647.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 647.5. REPAIRED IAW DWG K 05056 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998032600072 19980326 00072 WP 1998 3 26 ABXA9800228 1 19980218 A 5712 576946631 RIB DOUG DOUG DC8 DC863F 302198F WP WS 660 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 660. REPAIRED IAW DWG K 05056 AND DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998032600073 19980326 00073 WP 1998 3 26 ABXA9800229 1 19980218 A 5712 57694667 RIB DOUG DOUG DC8 DC863F 302198F WP WS 585 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 585. REPAIRED IAW DWG K 05056 AND DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998032600074 19980326 00074 WP 1998 3 26 ABXA9800230 1 19980218 A 5712 576947024 RIB DOUG DOUG DC8 DC863F 302198F WP WS 772 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT XFS 772 CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056-7001 AND DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998032600075 19980326 00075 WP 1998 3 26 ABXA9800231 1 19980226 A 5320 5717333263 INTERCOSTAL DOUG DOUG DC8 DC863F 302198F WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 INTERCOSTAL CRACKED AT RBL 40 BETWEEN STATION 980 AND 1000. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998032600076 19980326 00076 WP 1998 3 26 ABXA9800232 1 19980224 A 5320 37504971 TIE FITTING DOUG DOUG DC8 DC863F 302198F WP BS 660 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FORWARD ACCESSORY COMPARTMENT STA 660 LEFT FRAME TO LONGERON 36, TIE FITTING IS CRACKED. REPAIRED IAW DOUGLAS DWG 37504 97 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998032600077 19980326 00077 WP 1998 3 26 ABXA9800233 1 19980223 A 5720 97532938 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 250.089 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE STA XS 250.089 THE OUTBOARD AFT VERTICAL STIFFENER FOR THE INBOARD SLOT IS CRACKED AT THE LOWER END. REPAIRED IAW DWG 9753293 AND DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1998032600078 19980326 00078 WP 1998 3 26 ABXA9800234 1 19980222 A 5712 577012423 RIB DOUG DOUG DC8 DC863F 302198F WP WS 245 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 NR 2 STUB WING LOWER RIB CRACKED AT XFS 245.0. REPAIRED IAW DWG K05056-7005 AND DC8 SRM 51-1-21D. 2 L 7 4 4F 4A25 1998032600079 19980326 00079 WP 1998 3 26 ABXA9800235 1 19980316 A 5730 5613917 PANEL DOUG DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 SKIN PANEL ON RIGHT WING HAS CRACK INDICATIONS AT 7 LOCATIONS. REPAIRED IAW REA D857-21983MR. 2 L 7 4 4F 4A25 1998032600080 19980326 00080 WP 1998 3 26 ABXA9800236 1 19980316 A 5311 5751784 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 1400 BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 STA 1400 MAIN FRAME ABOVE LONGERON 35R HAS BOTTOM LEG BROKEN OUT. REPAIRED IAW REA D853-21958MR. 2 L 7 4 4F 4A25 1998032600081 19980326 00081 WP 1998 3 26 ABXA9800237 1 19980316 A 5720 5751784 TEE CAP DOUG DOUG DC8 DC863F 302198F WP WS 45 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 LEFT AUX TANK TEE CAP CORRODED AT WING STA XFS 45.00 TO XFS 107.50. REPAIRED IAW REA D857-21955 MR. 2 L 7 4 4F 4A25 1998032600082 19980326 00082 WP 1998 3 26 ABXA9800238 1 19980316 A 5730 5613917523 PANEL DOUG DOUG DC8 DC863F 302198F WP WS 69.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 LEFT WING LOWER 69.5 SKIN PANEL HAS CRACK INDICATIONS IN FIVE PLACES. REPAIRED IAW ABX REA D857-21963 MR. 2 L 7 4 4F 4A25 1998032600083 19980326 00083 WP 1998 3 26 ABXA9800239 1 19980302 A 5712 576946618 RIB DOUG DOUG DC8 DC863F 302198F WP WS 616.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 616.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 51-2-0 AND DWG K 05 056. 2 L 7 4 4F 4A25 1998032600084 19980326 00084 WP 1998 3 26 ABXA9800240 1 19980214 A 5712 576946920 RIB DOUG DOUG DC8 DC863F 302198F WP WS 622.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 622.50 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05 056. 2 L 7 4 4F 4A25 1998032600085 19980326 00085 WP 1998 3 26 ABXA9800241 1 19980214 A 5712 576946614 RIB DOUG DOUG DC8 DC863F 302198F WP WS 603.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 603.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 0505 6. 2 L 7 4 4F 4A25 1998032600086 19980326 00086 WP 1998 3 26 ABXA9800242 1 19980303 A 5320 9755569503 WEB DOUG DOUG DC8 DC863F 302198F WP WS 510-520 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 WEB CRACKED AT STATION 510 - 520 RIGHT, JUST AFT OF SERVICE DOOR AT FLOOR LEVEL. REPLACED WEB IAW DC8 SRM 51-1-20 AND D OUG DWG 9755569. 2 L 7 4 4F 4A25 1998032600087 19980326 00087 WP 1998 3 26 ABXA9800243 1 19980212 A 5320 37502751 FITTING DOUG DOUG DC8 DC863F 302198F WP WS 620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STATION 610 TO 620 STRINGER 31L SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-11 AND 51-1-20D. 2 L 7 4 4F 4A25 1998032600088 19980326 00088 WP 1998 3 26 ABXA9800244 1 19980302 A 5320 37502571N FITTING DOUG DOUG DC8 DC863F 302198F WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STATION 1040 - 1060 STRINGER 31R SPLICE FITTING IS CRACKED. REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F 4A25 1998032600089 19980326 00089 WP 1998 3 26 ABXA9800245 1 19980302 A 5712 576947124 RIB DOUG DOUG DC8 DC863F 302198F WP WS 778.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0 AND DWG K 05056. 2 L 7 4 4F 4A25 1998032600090 19980326 00090 WP 1998 3 26 ABXA9800246 1 19980302 A 5712 576947026 RIB DOUG DOUG DC8 DC863F 302198F WP WS 785 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 785.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0 AND DWG K 050 56. 2 L 7 4 4F 4A25 1998032600091 19980326 00091 WP 1998 3 26 ABXA9800247 1 19980302 A 5712 576947136 RIB DOUG DOUG DC8 DC863F 302198F WP WS 816.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 816.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05 056. 2 L 7 4 4F 4A25 1998032600092 19980326 00092 WP 1998 3 26 ABXA9800248 1 19980312 A 5712 576947128 RIB DOUG DOUG DC8 DC863F 302198F WP WS 791.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STATION XFS 791.25 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW SRM 57-2-0 AND DWG K 05 056. 2 L 7 4 4F 4A25 1998032600093 19980326 00093 WP 1998 3 26 ABXA9800252 1 19980317 A 3260 0080004003 PROXIMITY BOX DOUG DC8 DC863F 302198F WP LT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 812AX 46126 DURING APPROACH LEFT LANDING GEAR INDICATION LIGHT WOULD NOT ILLUMINATE AFTER GEAR RETRACTION. RECYCLED GEAR, LIGHT CAM E ON AFTER 10 MINUTES OF FLIGHT. REPLACED LEFT MAIN LANDING GEAR PROXIMITY BOX. ACCOMPLISHED GEAR SWING IAW DC8 MM 32- 60-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998032600094 19980326 00094 WP 1998 3 26 ABXA9800253 1 19980317 A 5610 5613217507 WINDOW DOUG DC9 DC933F 302207A WP LT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT ) WOULD NOT OPEN. RELEASED UPPER LOCK BAR, CLEANED AND LUBRICATED LINKAGE. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998032600095 19980326 00095 WP 1998 3 26 MWEA98363 1 19980315 A 5320 CLIP DOUG DC9 DC914 3022034 WP BS 762 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FOUND CRACKED SHEAR CLIP AT FS 762 BOTTOM LONGERON 16 AND 15. MAINTENANCE REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 1998032600096 19980326 00096 WP 1998 3 26 MWEA98364 1 19980315 A 5720 VANE DOUG DC9 DC914 3022034 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FOUND CHAFE MARK ON RIGHT WING INBOARD FIXED VANE LEADING EDGE. MAINTENANCE BLENDED MARK. 2 L 7 2 4F A6WE 1998032600097 19980326 00097 WP 1998 3 26 MWEA98365 1 19980315 A 5720 VANE DOUG DC9 DC914 3022034 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FOUND 2 CHAFE MARKS ON LEADING EDGE OF RIGHT WING MIDDLE FIXED VANE. MAINTENANCE REPAIRED FIXED VAN BY BLENDING CHAFE M ARKS. 2 L 7 2 4F A6WE 1998032600098 19980326 00098 WP 1998 3 26 MWEA98366 1 19980315 A 5320 ANGLE DOUG DC9 DC914 3022034 WP BS 840 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FOUND 2 CRACKS EXTENDING FROM 1 FASTENER HOLE AT STATION 840 ON RT UPPER PYLON TO FUSELAGE ATTACH ANGLE. MAINTENANCE R EPAIRED WITH DOUBLER. 2 L 7 2 4F A6WE 1998032600099 19980326 00099 NM 1998 3 26 VNAA9803017 1 19980313 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 07 436JS 43721 701 3052 DURING PRE-TAXI CHECKS, THE CREW NOTED THAT A SECTION OF EMERGENCY PATHWAY LIGHTING WAS INOPERATIVE. MAINTENANCE INSPEC TED AND REPLACED THE 5LK EMERGENCY BATTERY, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-50-00. OPERATION CHECKS WE RE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998032600100 19980326 00100 NM 1998 3 26 VNAA9803019 1 19980317 A 2913 42086 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT HYD SYST FAILED A VNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 459PS 35784 3070 DURING THE FLIGHT TO PIT, A MAIN HYDRAULIC FAIL WARNING MESSAGE WAS NOTED BY THE CREW. THE FLIGHT CREW DECLARED AN EMER GENCY, AND CONTINUED INTO PIT. THE AIRCRAFT LANDED IN PIT WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPL ACED THE MAIN HYDRAULIC PUMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-00-00. OPERATION AND LEAK CHECKS WERE COM PLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998032600101 19980326 00101 NM 1998 3 26 MALA976055 1 19980317 A 3230 11300103 UPLOCK ACTUATOR DHAV DHC8 DHC8102 2809003 NM RT MLG FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 866MA 366 EN ROUTE THE LANDING GEAR HANDLE TRANSIT FLICKERED ON AND OFF AS WELL THE RED TRANSIT LIGHT. AIRCRAFT LANDED WITHOUT IN CIDENT. MAINTENANCE REPLACED THE RIGHT UPLOCK ACTUATOR. PERFORMED GEAR EXTENSION AND RETRACTION ALONG WITH EMERGENCY E XTENSION, SERVICED HYDRAULIC SYSTEMS AND BLED SYSTEM. OPS AND SECURITY CHECK GOOD. 2 H 7 2 4T RT A13NM 1998032600102 19980326 00102 EU 1998 3 26 MALA976056 1 19980317 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 586MA 340B165 DURING INSPECTION, 2 OVERHEAD EMERGENCY LIGHT INOP AT 10C AND 11A. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998032600103 19980326 00103 EU 1998 3 26 MALA976057 1 19980317 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 103XJ 340A103 DURING INSPECTION, RIGHT SIDE FORWARD EMERGENCY EXIT DOOR LIGHTS AND OVERHEAD LIGHTS AT ROWS 1 AND 2. MAINTENANCE RELAM PED OVERHEAD LIGHTS (PN 1317) AND INSTALLED BATTERY PACK. 2 L 7 2 4T RT A52EU 1998032600104 19980326 00104 SO 1998 3 26 RAAA98E8006 1 19980319 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT RT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998032600105 19980326 00105 NM 1998 3 26 CALA9800492 1 19980317 A 3231 BACB30LJ4U42 BOLT BOEING 757 757224 1384958 NM DOOR SEQ VLV SHEARED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 29124 27565 WHEN GEAR UP WAS SELECTED AFTER TAKEOFF, THE GEAR AND GEAR DOOR LIGHTS REMAINED ON WITH EICAS MESSAGE OF GEAR DOORS AND GEAR DISAGREE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A SHEARED BOLT IN NLG DOOR OPERATED SEQUENCE VALVE SUPPORT ASSEMBLY. THE BOLT HAD SHEARED DUE TO LINK BEING INSTALLED INCORRECTLY. THE BO LT, LINK, AND CARRIER WERE REPLACED IAW COMPONENT MAINTENANCE MANUAL 32-34-14, PAGE 701. OPERATION OF THE NLG WAS TESTE D IAW MM 32-34-00, PAGE 501 AND ALL CHECKED GOOD. AN INVESTIGATION IS BEING CONDUCTED BY ENGINEERING. 2 L 7 2 4F RT A2NM 1998032600106 19980326 00106 NM 1998 3 26 CALA9800493 1 19980319 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1110, RBL 12-36. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-08. 2 L 7 3 4F A3WE 1998032600107 19980326 00107 NM 1998 3 26 CALA9800494 1 19980319 A 5320 WEB BOEING 727 727227 1384078 NM BS 575 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND TWO 1 CRACKS ON PLATE AT FASTENERS TOP OF WEB STRINGER 18R, FS 575. THE CRACKED AREA WAS REMOVED. A R EPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-20-01, AND 51-10-2. 2 L 7 3 4F A3WE 1998032600108 19980326 00108 NM 1998 3 26 CALA9800495 1 19980319 A 5330 PLATE BOEING 727 727227 1384078 NM BS 605 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND TWO 1 CRACKS ON PLATE AT FASTENERS TOP OF WEB STRINGER 18R, FS 605. THE CRACKED AREA WAS REMOVED. A R EPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998032600109 19980326 00109 NM 1998 3 26 CALA9800496 1 19980319 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 754 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 2 CRACK IN FLOORBOARD ATTACH ANGLE AT FS 754, LBL 1. THE CRACKED AREA WAS CUT OUT. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-40-5, AND 51-30-2. 2 L 7 3 4F A3WE 1998032600110 19980326 00110 NM 1998 3 26 CALA9800497 1 19980319 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 CRACK IN SHEAR TIE AT LT BS 720, WL 208. THE SHEAR TIE WAS REMOVED. A NEW SHEAR TIE WAS FABRICATE D AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998032600111 19980326 00111 NM 1998 3 26 CALA9800498 1 19980319 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 CRACK IN INTERCOSTAL AT FS 312, LBL 31. THE CRACKED AREA WAS REMOVED. A NEW PART WAS FABRICATED A ND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998032600112 19980326 00112 NM 1998 3 26 CALA9800499 1 19980319 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 294-296 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 2 CRACK IN UPPER RADIUS OF INTERCOSTAL AT FS 294-296, LBL 42. THE INTERCOSTAL WAS REMOVED AND REPLAC ED IAW SRM 51-30-1 AND 51-40-3. 2 L 7 3 4F A3WE 1998032600113 19980326 00113 NM 1998 3 26 CALA9800500 1 19980319 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .5 INCH CRACK AT RIVET IN INTERCOSTAL AT FS 380, RBL 6. THE INTERCOSTAL WAS ALSO BENT IN THE MIDDLE. THE INTERCOSTAL WAS REMOVED IAW SRM 51-30-2. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51 -30-2. 2 L 7 3 4F A3WE 1998032600114 19980326 00114 NM 1998 3 26 CALA9800501 1 19980319 A 3230 SENSOR BOEING 737 7373T0 1384582 NM LANDING GEAR OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14347 23585 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE ABNORMAL CHECKLIST WAS COMPLETED AND THE AIRCRAFT WAS RE TURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AIR SAFETY SENSOR OUT OF ADJUSTMENT. THE SENSOR WAS ADJUSTED IAW MM 32-09-01. AN EXTENSION AND RETRACTION OF THE LANDING GEAR WAS PERFORMED IAW MM 32-32-00 AND OPERATI ON AND INDICATIONS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998032600115 19980326 00115 NM 1998 3 26 CALA9800502 1 19980319 A 5210 SKIN BOEING 727 727227 1384078 NM L1 DOOR BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND L-1 DOOR OUTER SKIN BENT WITH A .015625 INCH CRACK AT LOWER AFT CORNER ABOVE GATE. A PATCH WAS FABRICA TED AND INSTALLED IAW SRM 52-00-3 AND 51-10-2. 2 L 7 3 4F A3WE 1998032600116 19980326 00116 NM 1998 3 26 CALA9800503 1 19980319 A 5240 FRAME BOEING 727 727227 1384078 NM R 1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .75 INCH CRACK AT R-1 DOOR LOWER FORWARD CORNER FROM UNDER FORWARD LOWER FITTING TO FASTENER HEAD. C UT FRAME AND SPLICED IN NEW FRAME SECTION IAW DRAWING 69-69940. REINFORCED DOOR LOWER CORNER WITH DOUBLER, FILLER, AND SHIMS. STOP FITTING AND SEAL RETAINER WERE REINSTALLED IAW ECRA 5240-01227. 2 L 7 3 4F A3WE 1998032600117 19980326 00117 NM 1998 3 26 CALA9800504 1 19980319 A 5532 SKIN BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .25 INCH CRACK IN RT VERTICAL STABILIZER LOWER SECTION AT STA 1343. A REPAIR WAS INSTALLED IAW ECRA 5530-01075. 2 L 7 3 4F A3WE 1998032600118 19980326 00118 NM 1998 3 26 CALA9800505 1 19980319 A 5744 BRACKET BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 2 CRACK IN BOTH INBOARD AND OUTBOARD BRACKETS WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACHES INSIDE LEADING EDGE. NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. THE FLAP ACTUATOR WAS REMOVED AND REI NSTALLED IAW MM 27-80. 2 L 7 3 4F A3WE 1998032600119 19980326 00119 NM 1998 3 26 CALA9800506 1 19980319 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 686.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .25 INCH CRACK IN LT WING STRINGER ON TOP OF RIB (SECOND UPPER STRINGER FROM AFT SPAR) WS 686.5. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW EA 5762-01050. 2 L 7 3 4F A3WE 1998032600120 19980326 00120 NM 1998 3 26 CALA9800507 1 19980319 A 5712 RIB BOEING 727 727227 1384078 NM WS 629 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .25 INCH CRACK IN RIB AT WS 629. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW EA 5762-1050, FIGURE 8. 2 L 7 3 4F A3WE 1998032600121 19980326 00121 NM 1998 3 26 CALA9800508 1 19980319 A 5741 BOTTLE PIN BOEING 727 727227 1384078 NM RT WING/FUS CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND RT FORWARD BOTTLE PIN CORRODED AT HEAD FLANGE AND NECK AREA. THE RT FORWARD BOTTLE PIN WAS REPLACED IA W MM 57-41-1. 2 L 7 3 4F A3WE 1998032600122 19980326 00122 NM 1998 3 26 CALA9800509 1 19980319 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 1070-1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1070-1110, RBL 15. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1. 2 L 7 3 4F A3WE 1998032600123 19980326 00123 NM 1998 3 26 CALA9800510 1 19980319 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 380-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 380-440. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998032600124 19980326 00124 NM 1998 3 26 CALA9800511 1 19980318 A 5311 FRAME BOEING 737 7373T0 1384582 NM BS 847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND BELT FRAME CORRODED AT STA 847 BETWEEN STRINGERS 25 AND 26R. REPAIRED IAW SRM 53-00-07, PAGE 203 AND E CRA 5310-03693. 2 L 7 2 4F RT A16WE 1998032600125 19980326 00125 WP 1998 3 26 CALA9800512 1 19980318 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 49082 47927 INSPECTION FOUND A 1 CRACK IN STIFFENER AT LT MLG WHEEL WELL AFT WALL. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WA S FABRICATED AND INSTALLED IAW SRM 53-53-01, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600126 19980326 00126 WP 1998 3 26 CALA9800513 1 19980318 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1841 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 49082 47927 INSPECTION FOUND WEB IN AFT CARGO BILGE AREA TORN AND DISTORTED AT FLOORBEAM, STA 1841, STRINGER 44L. THE DAMAGED AREA OF WEB WAS TRIMMED AND BLENDED OUT. THE AREA WAS REINFORCED WITH DOUBLER IAW SRM 53-00-01, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600127 19980326 00127 WP 1998 3 26 CALA9800514 1 19980319 A 5313 STRINGER DOUG DC10 DC1030 3023501 WP BS 1953-1964 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 49082 47927 INSPECTION FOUND A 1 INCH CRACK WITH CORROSION ON STRINGER 51L BETWEEN STA 1953 AND 1964 IN AFT CARGO BILGE AREA. CORRO SION WAS REMOVED. THE CRACKED AREA WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, FIGURE 7, 51-2 0-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998032600128 19980326 00128 WP 1998 3 26 CALA9800515 1 19980320 A 5320 INTERCOSTAL DOUG DC10 DC1030 3023501 WP BS 1721 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17085 47957 INSPECTION FOUND A 1 INCH CRACK ON LOWER CAP OF INTERCOSTAL AT CEILING CENTER CARGO, RBL 82, STA 1721 WITH DISTORTION ON CEILING SUPPORT AT RBL 78. A REPAIR WAS ACCOMPLISHED IAW SRM 51-21-01 AND 51-33-01. 2 L 7 3 4F A22WE 1998032600129 19980326 00129 NM 1998 3 26 CALA9800516 1 19980319 A 5320 WEB BOEING 727 727227 1384078 NM BS 1110-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND SHEAR WEB CORRODED AT FS 1110-1130, STRINGER 17R. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-10-1 AND 51-30-02. 2 L 7 3 4F A3WE 1998032600130 19980326 00130 NM 1998 3 26 CALA9800517 1 19980319 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 1110-1130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND INTERCOSTAL TOP FLANGE CRACKED IN THREE PLACES AT FS 1110-1130, BBL 0. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998032600131 19980326 00131 NM 1998 3 26 CALA9800518 1 19980319 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 1080-1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND LT OUTBOARD SEAT TRACK CORRODED AT FS 1080-1110, LBL 45. THE CORRODED SECTION OF TRACK WAS CUT OUT AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998032600132 19980326 00132 NM 1998 3 26 CALA9800519 1 19980319 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 1030-1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1030-1140, RBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5, PAGES 18-22. 2 L 7 3 4F A3WE 1998032600133 19980326 00133 NM 1998 3 26 CALA9800520 1 19980319 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 1030-1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1030-1090, RBL 36. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5, PAGES 18-22. 2 L 7 3 4F A3WE 1998032600134 19980326 00134 NM 1998 3 26 CALA9800521 1 19980319 A 5720 ANGLE BOEING 727 727227 1384078 NM WS 330 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 2 INCH CRACK IN DOUBLER ANGLE INSIDE LT WING LEADING EDGE AT RIB, WS 330. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-03 AND 51-30-02. 2 L 7 3 4F A3WE 1998032600135 19980326 00135 NM 1998 3 26 CALA9800522 1 19980319 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .75 INCH CRACK IN LT WING UPPER TRAILING EDGE CUTOUT, FORWARD OF NR 4 SPOILER SECOND FROM OUTBOARD HI NGE. THE CRACK WAS STOP DRILLED. A REPAIR PLATE WAS FABRICATED AND INSTALLED IAW SRM 57-30-04. 2 L 7 3 4F A3WE 1998032600136 19980326 00136 NM 1998 3 26 CALA9800523 1 19980319 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .21875 INCH CRACK AT LT WING FIXED UPPER LEADING EDGE AT AFT END OF CUTOUT WHERE NR 4 SLAT OUTBOARD H OOK ATTACHES. THE CRACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-30-4, 51-10-2, 51-30-2. 2 L 7 3 4F A3WE 1998032600137 19980326 00137 NM 1998 3 26 CALA9800524 1 19980319 A 2761 BRACKET BOEING 727 727227 1384078 NM NR 3 SPOILER ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND LT WING LOWER TRAILING EDGE LOOSE BETWEEN NR 2 AND NR 3 SPOILER ACTUATOR. ONE AREA INBOARD OF NR 2 SPO ILER ACTUATOR WAS LOOSE/WORN. ANOTHER AREA OUTBOARD OF NR 3 SPOILER ACTUATOR HAD A RIB WITH 2 CRACK AND WORN BRACE ROD. THE BRACKETS AND BRACE ROD WERE REMOVED AND REPLACED IAW SRM 51-10-1, PARAGRAPH 4. 2 L 7 3 4F A3WE 1998032600138 19980326 00138 NM 1998 3 26 CALA9800525 1 19980319 A 5720 BRACKET BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH CRACK IN BRACKET AT OUTBOARD SIDE WHERE LT WING NR 1 SLAT LOWER SKIN ATTACHES TO INBOARD TRACK . THE BRACKET WAS REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998032600139 19980326 00139 NM 1998 3 26 CALA9800526 1 19980319 A 5730 SKIN BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 THE LT WING LOWER LEADING EDGE HAD A .15625 CRACK WITH LOOSE FASTENERS JUST INBOARD OF CUTOUT ABOVE NR 2 SLAT. THE CRAC K WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-1, AND 51-30-2. 2 L 7 3 4F A3WE 1998032600140 19980326 00140 NM 1998 3 26 CALA9800527 1 19980319 A 5720 ANGLE BOEING 727 727227 1384078 NM WS 120 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 2 CRACK IN LOWER LEADING EDGE SUPPORT ANGLE INSIDE LT WING LEADING EDGE AFT OF NR 3 LEADING EDGE FLAP AREA, FSS 120. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30- 2. 2 L 7 3 4F A3WE 1998032600141 19980326 00141 NM 1998 3 26 CALA9800528 1 19980319 A 5753 SKIN BOEING 727 727227 1384078 NM RT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND AN 8 GOUGE IN RT INBOARD FOREFLAP INBOARD END AT WING ROOT. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-50-00. 2 L 7 3 4F A3WE 1998032600142 19980326 00142 NM 1998 3 26 CALA9800529 1 19980319 A 5320 SUBFLOOR BOEING 727 727227 1384078 NM BS 294-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND FORWARD LAV OUTBOARD SUBFLOOR CORRODED AT FS 294-344, RBL 43-63. THE SUBFLOOR WAS REMOVED AND A NEW SU BFLOOR WAS INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998032600143 19980326 00143 NM 1998 3 26 CALA9800530 1 19980319 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720B CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, AND 53-10-3, PAGE 43, DETAIL 11. 2 L 7 3 4F A3WE 1998032600144 19980326 00144 NM 1998 3 26 CALA9800531 1 19980319 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 846 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT FS 846, RBL 1. THE FLOOR SUPPORT WAS REMOVED. A DOUBLER AND FLOOR SUPPORT WERE FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-1. 2 L 7 3 4F A3WE 1998032600145 19980326 00145 NM 1998 3 26 CALA9800532 1 19980319 A 5523 657279957 SKIN BOEING 727 727227 1384078 NM RT ELEV TAB SEPARATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND THE RT ELEVATOR CONTROL TAB TRAILING EDGE SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACED . 2 L 7 3 4F A3WE 1998032600146 19980326 00146 NM 1998 3 26 CALA9800533 1 19980319 A 5523 657279957 SKIN BOEING 727 727227 1384078 NM LT ELEV TAB SEPARATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND THE LT ELEVATOR CONTROL TAB INBOARD CORNER SEPARATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND REPLACE D. 2 L 7 3 4F A3WE 1998032600147 19980326 00147 NM 1998 3 26 CALA9800534 1 19980319 A 5755 SKIN BOEING 727 727227 1384078 NM NR 7 SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND BOTTOM OF LT WING NR 7 SPOILER CORRODED. THE SPOILER WAS REPAIRED BY AVIATION COMPOSITES AND IAW WORK C ARD 07-5750-1-2717.. 2 L 7 3 4F A3WE 1998032600148 19980326 00148 NM 1998 3 26 CALA9800535 1 19980319 A 5712 RIB BOEING 727 727227 1384078 NM LT WING TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .25 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL OUTBOARD SUPPORT RIB JUST INBOARD NR 4 SPOILER AC TUATOR IN FLAP COVE AREA. THE RIB AND ROD WERE REMOVED AND REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998032600149 19980326 00149 WP 1998 3 26 9804619178 1 19980318 A 5350 LATCH DOUG DC9 DC914 3022034 WP TAIL CONE WORN A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3310L 45705 DURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY THE TAILCONE AFTER HANDLE WAS REMOVE D FROM CLIPS. ALSO, FOUND THE UPPER LEFT LATCH SPADE WORN AND SEVERAL GUIDE PIN RECEPTACLES WORN. REPLACED LATCH SPADE AND GUIDE PIN RECEPTACLES AND CLEANED AND LUBRICATED LATCHES. FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998032600150 19980326 00150 WP 1998 3 26 9804629860 1 19980318 A 2424 TRANSFORMER DOUG DC9 DC951 3022051 WP E/E COMPT INOPERATIVE A NWAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 01 769NC 47757 DURING CLIMB-OUT, THE LEFT ENGINE DRIVEN GENERATOR TRIPPED OFF LINE WITH AN AC CROSSTIE LOCKOUT CONDITION. FLIGHT CREW PERFORMED COM PROCEDURES, RETURNED TO DTW, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE DIFFERENTIAL PROTECTIO N CURRENT TRANSFORMER. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998032600151 19980326 00151 NE 1998 3 26 9804633247 2 19980315 A 7200 ENGINE AIRBUS 320 A320212 EU CFMINT CFM56 CFM565A3 NE NR 1 FAILED A NWAA E ENGINE SHUTDOWN J X WARNING INDICATION ENGINE FLAMEOUT DE DESCENT 1 GL 01 347NW 16857 16857 408 731769 DURING DESCENT WITH POWER AT FLIGHT IDLE, ENG 1 FAIL ECAM MESSAGE ANNUNCIATED AND NR 1 ENGINE AUTO SHUT DOWN. ONE SUCCE SSFUL RELIGHT WAS ATTEMPTED. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND NR 1 ENGINE FUEL FILTER CONTAMINAT ED WITH BRONZE. REPLACED THE NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM E29NE 1998032600152 19980326 00152 WP 1998 3 26 9804649983 1 19980318 A 5610 WINDSHIELD DOUG DC9 DC932 3022066 WP RT COCKPIT FAILED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 983US 47282 DURING CLIMB-OUT, AN ELECTRICAL ARC OCCURRED AT FIRST OFFICER'S WINDSHIELD WITH WINDSHIELD HEAT TURNED OFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDHSIELD, HEAT CONTROLLER, AND ASSOCIATED WIRIN G. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998032600153 19980326 00153 WP 1998 3 26 9804659997 1 19980319 A 2910 LINE DOUG DC9 DC931 3022065 WP RT MLG ACTUATOR LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 8933E 47142 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT I NCIDENT. MAINTENANCE FOUND LINE TO RIGHT MAIN GEAR RETRACT ACTUATOR LEAKING. REPLACED LINE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998032600154 19980326 00154 WP 1998 3 26 9804669913 1 19980318 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 963N 47415 DURING PERIODIC CHECK, FOUND OVERHEAD EMERGENCY LIGHTS JUST AFT OF OVERWING EXIT INOPERATIVE. REPLACED BATTERY PACK. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600155 19980326 00155 WP 1998 3 26 UPS98826153 1 19980310 A 5542 5644210505 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE:C RUDDER, UPPER AFT CORNER LT SIDE HAS HEAVY CORROSION. REMOVED AND REPLACED RUDDER IAW MM 27-21-01. 2 L 7 4 4F RT 4A25 1998032600156 19980326 00156 WP 1998 3 26 UPS98826154 1 19980320 A 3350 BATT PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 874UP 46074 EMERGENCY LIGHTS ILLUMINATED DURING TAXI OUT W\SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED BATTERY PACK, EMERG L IGHT CHECK GOOD. 2 L 7 4 4F RT 4A25 1998032600157 19980326 00157 EU 1998 3 26 WWMA9800052 1 19980317 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY DEFECTIVE A WWMA K NONE N FALSE WARNING CR CRUISE 1 WP 15 234AE 340B234 LAVATORY SMOKE DETECTION LIGHT CAME ON IN FLIGHT WITH NO APPARENT PROBLEM. REPLACED THE LAVATORY SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998032600158 19980326 00158 EU 1998 3 26 WWMA9800051 1 19980317 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 324AE 340B324 FLIGHT 5004, AEX, CREW REPORTED THE EMERGENCY LIGHTS WOULD COME ON FOR A FEW SECONDS THEN GO OUT. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACKS. 2 L 7 2 4T RT A52EU 1998032600159 19980326 00159 EU 1998 3 26 WWMA9800050 1 19980316 A 3350 LIGHTS SAAB SF340 340B 7860101 EU CABIN MALFUNCTIONED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 324AE 340B324 FLIGHT 5087, DFW, CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE EMERGENCY LIGHT SYSTEM AND FOUND ALL LIGHTS TO FUNCTION CORRECTLY. 2 L 7 2 4T RT A52EU 1998032600160 19980326 00160 EU 1998 3 26 WWMA9800049 1 19980310 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT NO TEST A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 261AE 340B261 DURING PREFLIGHT, THE CARGO SMOKE DETECTOR WOULD NOT TEST. REPLACED THE AFT CARGO SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998032600161 19980326 00161 EU 1998 3 26 WWMA9800057 1 19980318 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 341SB 340B341 DURING PREFLIGHT, FOUND THE FLOOR EMERGENCY LIGHT AT ROW 5BC INOPERATIVE. REPLACED THE FLOOR LIGHT ASSY AT 5BC. 2 L 7 2 4T RT A52EU 1998032600162 19980326 00162 EU 1998 3 26 WWMA9800056 1 19980319 A 3350 FUSE SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 356SB 340B356 DURING PREFLIGHT, FLOOR EMERGENCY LIGHTS AT ROWS 6B AND 7B FAILED TO ILLUMINATE. MAINTENANCE TIGHTENED THE FUSE FOR THE EMERGENCY LIGHTS AT ROWS 6B AND 7B. 2 L 7 2 4T RT A52EU 1998032600163 19980326 00163 EU 1998 3 26 WWMA9800055 1 19980318 A 3350 192411A FUSE SAAB SF340 340B 7860101 EU CABIN BLOWN A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 341SB 340B341 DURING PREFLIGHT, THE MAIN DOOR EXIT AND EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE. REPLACED THE FUSE FOR THE EMERGENC Y EXIT LIGHTS. 2 L 7 2 4T RT A52EU 1998032600164 19980326 00164 EU 1998 3 26 WWMA9800054 1 19980318 A 3397 WIRE SAAB SF340 340B 7860101 EU CABIN LOOSE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 324AE 340B324 DURING PREFLIGHT, THE EMERGENCY FLOOR LIGHTS AT ROWS 6BC AND 7BC FAILED TO ILLUMINATE. MAINTENANCE FOUND A SOLDER CONNE CTION AT FUSE HAD WORK HARDENED, RESOLDERED WIRE AND PERFORMED OPS CHECK. 2 L 7 2 4T RT A52EU 1998032600165 19980326 00165 EU 1998 3 26 WWMA9800053 1 19980311 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN INTERMITTENT A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 332AE 340B332 DURING PREFLIGHT, THE EMERGENCY LIGHT ABOVE SEAT 10BC WAS INTERMITTENT. MAINTENANCE PERFORMED OPERATIONAL CHECK AND COU LD NOT DUPLICATE PROBLEM, THE BULB WAS REPLACED FOR PRECAUTIONARY REASONS. 2 L 7 2 4T RT A52EU 1998032600166 19980326 00166 EU 1998 3 26 QXEA9800330 1 19980204 A 7602 ARM FOKKER F28 F28MK4000 4990810 EU MIXTURE SUPPORT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - MIXTURE SUPPORT ARM IS CRACKED ON THE 9 O'CLOCK POSITION OUTBOARD APPROXIMATELY 2 INCHES FROM CENTER LINE. REPAIR ED IAW HORIZON EA 4-78-08 STEPS 1-3. 2 L 7 2 4F RT A20EU 1998032600167 19980326 00167 EU 1998 3 26 QXEA9800331 1 19980205 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - PREVIOUS DOUBLER REPAIR AT TOP SURFACE OF HORIZONTAL BEAM VI APPEARS TO BE CRACKED ON FORWARD SIDE OF FORWARD PRES SURE BULKHEAD. REPAIRED IAW HORIZON EA 4-53-370. 2 L 7 2 4F RT A20EU 1998032600168 19980326 00168 EU 1998 3 26 QXEA9800332 1 19980205 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CENTER CARGO DOOR UPPER FORWARD JAMB STRUCTURE HAS A GOUGE 2.2 INCHES IN LENGTH, 2.0 INCHES IN WIDTH AND APPROXIMA TELY .025 INCH DEPTH AT THE UPPER SECTION OF THE JAMB STRUCTURE FOR THE CENTER CARGO DOOR. REPAIRED IAW FOKKER SRM 53-0 2-16, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1998032600169 19980326 00169 EU 1998 3 26 QXEA9800333 1 19980205 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FORWARD CARGO DOOR LOWER FORWARD JAMB STRUCTURE HAS A GOUGE 1.6 INCHES IN LENTH, 1 INCH IN WIDTH AND APPROXIMATELY .015 IN DEPTH AT THE LOWER SECTION OF THE JAMB STRUCTURE FOR THE FORWARD CARGO DOOR. REPAIRED IAW FOKKER SRM 53-02-16, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1998032600170 19980326 00170 EU 1998 3 26 QXEA9800334 1 19980206 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 14755 AT STRINGER 74 AND 3. NUTPLATES ARE CORRODED SUSPECT FRAME CORROSION. REPAIRED IAW FOKKER SRM 53-02- 12 AND HORIZON EA 4-53-354. 2 L 7 2 4F RT A20EU 1998032600171 19980326 00171 EU 1998 3 26 QXEA9800335 1 19980206 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FORWARD CARGO COMPARTMENT CENTER DOOR FORWARD BOTTOM CORNER OF DOOR STRUCTURE HAS SEVERAL HEAVY DENTS. REPAIRED I AW FOKKER SRM 52-30-00, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600172 19980326 00172 EU 1998 3 26 QXEA9800336 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU CARGO COMPT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FORWARD CARGO BAY FLOOR FRAME 9305 TOP ANGLE HAS EXFOILATION TYPE CORROSION AT CENTER OF FRAME ANGLE BETWEEN STRIN GERS 1 AND 74. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 6 AND 7, SRM 51-31-01 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1998032600173 19980326 00173 EU 1998 3 26 QXEA9800337 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FORWARD CARGO COMPARTMENT FLOOR FRAME 5305 TOP ANGLE HAS HEAVY EXFOILATION TYPE CORROSION BETWEEN STRINGERS 1 AND 74. REPAIRED IAW HORIZON EA 4-53-156. 2 L 7 2 4F RT A20EU 1998032600174 19980326 00174 EU 1998 3 26 QXEA9800338 1 19980208 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LARGE DENT ON FUSELAGE EXTERIOR SKIN (LEFT SIDE, SKIN APPEARS TO BE BUCKLED) LOCATED ON FRAME 6305 APPROXIMATELY 6 INCHES BELOW TOP JOINT. FABRICATED SHEAR TIE IAW FOKKER SRM 53-02-11, FIGURE 1, SHEET 2 OF 2, PAGE 5, INSTALLED IAW FO KKER SRM 51-31-01. SHEAR TIE ONLY. 2 L 7 2 4F RT A20EU 1998032600175 19980326 00175 EU 1998 3 26 QXEA9800339 1 19980216 A 5320 SPLICE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 13815A AT STRINGER 74 HAS CORROSION VISIBLE FROM UNDERSIDE OF FRAME SPLICE. INSTALLED FRAME SPLICE IAW HORI ZON EA 4-53-365. 2 L 7 2 4F RT A20EU 1998032600176 19980326 00176 EU 1998 3 26 QXEA9800340 1 19980216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 13815B AT STRINGER 74 HAS A HEAVY CORROSION BUBBLE 1 INCH DIAMETER. DRILLED UP NEW PART AND INSTALLED WITH SOLID RIVETS IAW FOKKER SRM 51-31-01, 51-10-05. 2 L 7 2 4F RT A20EU 1998032600177 19980326 00177 EU 1998 3 26 QXEA9800341 1 19980216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE BUCKLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 14285 IS BUCKLED AT TWO LOCATIONS STRINGER 72 BETWEEN STRINGER 2 AND 3. REPAIRED IAW HORIZON EA 4-53-366. 2 L 7 2 4F RT A20EU 1998032600178 19980326 00178 EU 1998 3 26 QXEA9800342 1 19980216 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - REAR CARGO ENTRY WAY REINFORCED SKIN AT FRAME 16060 HAS BEEN BLENDED BEYOND SRM LIMITS. FABRICATED AND INSTALLED DOUBLER OF .050 2029T3 IAW FOKKER SRM 53-02-01, PAGE 6, FIGURE 4. ALODINED AND PAINTED DOUBLER IAW FOKKER SRM 51-10-04, PAGE 9 2 L 7 2 4F RT A20EU 1998032600179 19980326 00179 EU 1998 3 26 QXEA9800343 1 19980226 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CREASE IN BELLY SKIN AFT OF FRAME 16660 BETWEEN STRINGERS 2 AND 73. FABRICATED NEW CLIPS USING 2024T3 .040. INST ALLED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 1998032600180 19980326 00180 EU 1998 3 26 QXEA9800344 1 19980204 A 5320 WALL FOKKER F28 F28MK4000 4990810 EU RT ACM BUCKLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - WALL IN FRONT OF LOWER AFT MOUNT FOR RIGHT AIR CYCLE MACHINE HEAT EXCHANGER IS BUCKLED. FABRICATED AND INSTALLED DOUBLER REPAIR IAW FOKKER SRM 53-02-01, FIGURE 4. 2 L 7 2 4F RT A20EU 1998032600181 19980326 00181 EU 1998 3 26 QXEA9800345 1 19980204 A 5320 WALL FOKKER F28 F28MK4000 4990810 EU RT ACM DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - THREE DENTS ON WALL BEHIND HEAT EXCHANGER LOWER AFT CORNER, RIGHT AIR CYCLE MACHINE. FABRICATED AND INSTALLED DOU BLER REPAIR IAW FOKKER SRM 53-02-01, FIGURE 4. 2 L 7 2 4F RT A20EU 1998032600182 19980326 00182 EU 1998 3 26 QXEA9800346 1 19980205 A 5280 DOOR FOKKER F28 F28MK4000 4990810 EU RT MLG CHAFING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT MAIN LANDING GEAR INBOARD DOOR IS CHAFFING AGAINST FUSELAGE STRUCTURE AT OUTBOARD AFT EDGE OF WHEEL WELL. R EPAIRED IAW HORIZON AIR EA 4-53-372. 2 L 7 2 4F RT A20EU 1998032600183 19980326 00183 EU 1998 3 26 QXEA9800347 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 9305C AND STRINGER 34 THERE IS A CRACKED CLIP. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600184 19980326 00184 EU 1998 3 26 QXEA9800348 1 19980202 A 5220 FRAME FOKKER F28 F28MK4000 4990810 EU EMER EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT AFT OVERWING EMERGENCY EXIT DOOR FRAME TOP AFT CORNER IS CRACKED. REMOVED AND REPLACED FRAME IAW HORIZON EO 4-52-21C. 2 L 7 2 4F RT A20EU 1998032600185 19980326 00185 EU 1998 3 26 QXEA9800349 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED AND ONE IMPROPER FASTENER AT FRAME 9305A STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2. 2 L 7 2 4F RT A20EU 1998032600186 19980326 00186 EU 1998 3 26 QXEA9800350 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED FRAME 9305A STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600187 19980326 00187 EU 1998 3 26 QXEA9800351 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED FRAME 9305A AT STRINGER 38. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600188 19980326 00188 EU 1998 3 26 QXEA9800352 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED FRAME 9305 STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600189 19980326 00189 EU 1998 3 26 QXEA9800353 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED FRAME 9305 STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600190 19980326 00190 EU 1998 3 26 QXEA9800354 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACK FRAMED 9305 STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600191 19980326 00191 EU 1998 3 26 QXEA9800355 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACK FRAME 9305 STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600192 19980326 00192 EU 1998 3 26 QXEA9800356 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACK AT FRAME 8805 STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600193 19980326 00193 EU 1998 3 26 QXEA9800357 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED FRAME 6305 STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600194 19980326 00194 EU 1998 3 26 QXEA9800358 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACKED CLIP FRAME 6305 AND STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600195 19980326 00195 EU 1998 3 26 QXEA9800359 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED AT FRAME 9305A AND STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998032600196 19980326 00196 EU 1998 3 26 QXEA9800360 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CLIP CRACKED AT FRAME 9305A STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998032600197 19980326 00197 EU 1998 3 26 QXEA9800361 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - INSIDE CABIN FRAME 13815B HAS A CRACKED CLIP BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600198 19980326 00198 EU 1998 3 26 QXEA9800362 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - INSIDE CABIN FRAME 13815A HAS A CRACKED CLIP BETWEEN STRINGERS 46-47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, F IGURE 2. 2 L 7 2 4F RT A20EU 1998032600199 19980326 00199 EU 1998 3 26 QXEA9800363 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACKED CLIP AT FRAME 8305 STRINGER 17/18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600200 19980326 00200 EU 1998 3 26 QXEA9800364 1 19980209 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FLOORBEAM AT BL1120 IS CRACKED 6 INCHES AFT OF FRAME 3450. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600201 19980326 00201 EU 1998 3 26 QXEA9800365 1 19980209 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FLOORBEAM AT FRAME 3820 AND BL1120 RIGHT IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-14, PAGE 2, FIGURE 1. 2 L 7 2 4F RT A20EU 1998032600202 19980326 00202 EU 1998 3 26 QXEA9800366 1 19980215 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - DAMAGE IN SEAT TRACK SIX INCHES FORWARD OF FRAME 5805, MEASURED .289 DEEP, LEFT INBOARD SEAT TRACK. REPAIRED IAW FOKKER SRM 53-02-15, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1998032600203 19980326 00203 EU 1998 3 26 QXEA9800367 1 19980215 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT INBOARD SEAT TRACK HAS TWO GOUGES ON THE TOP FLANGE SEVEN INCHES BEHIND FRAME 10346 THAT HAVE BEEN BLENDED BE YOND LIMITS. BLENDING EXTENDS .030 TO .040 DOWN INTO RADIUS OF SEAT TRACK MOUNTING HOLE. REPAIRED IAW FOKKER SRM 53-02 -15 2 L 7 2 4F RT A20EU 1998032600204 19980326 00204 EU 1998 3 26 QXEA9800368 1 19980217 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - MAIN CABIN DOOR TWO CENTER RIVET ROWS ON OUTSIDE SKIN STRIP HAS DENTS. REPAIRED IAW HORIZON EA 4-52-119A. 2 L 7 2 4F RT A20EU 1998032600205 19980326 00205 EU 1998 3 26 QXEA9800369 1 19980222 A 5320 AUX BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACK ACROSS AUXILIARY BEAM EXTENSION OF BL1127 RT JUST FORWARD OF FRAME 3820. REPAIRED IAW FOKKER SRM 51-10-14, SRM 53-02-14, PAGE 2, FIGURE 1. 2 L 7 2 4F RT A20EU 1998032600206 19980326 00206 EU 1998 3 26 QXEA9800370 1 19980205 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - DENT IN BELLY SKIN BL0.00 SIX INCHES FORWARD OF PANEL 41A. REPAIRED IAW FOKKER SRM 51-31-01 AND HORIZON EA 4-53-2 56A. 2 L 7 2 4F RT A20EU 1998032600207 19980326 00207 EU 1998 3 26 QXEA9800371 1 19980206 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT SPEED BRAKE FLAP INTERNAL SKIN RIVETS LOOSE. REPAIRED IAW FOKKER SRM 51-31-05 AND HORIZON EA 4-53-352. 2 L 7 2 4F RT A20EU 1998032600208 19980326 00208 EU 1998 3 26 QXEA9800372 1 19980206 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - DENT IN LEFT FORWARD OF OBLIQUE FRAME 41-2, 8 INCHES BELOW RED PAINT. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1, PAGE 2, SRM 53-02-04, FIGURE 3, PAGE 5 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600209 19980326 00209 EU 1998 3 26 QXEA9800373 1 19980206 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - STIFFENER CRACKED ON RIGHT OBLIQUE FRAME 16-2 AT STRINGER 62. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600210 19980326 00210 EU 1998 3 26 QXEA9800374 1 19980212 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - DENT IN LEFT SKIN AND DAMAGE TO BONDED STRINGER. REPAIRED IAW FOKKER SRM 51-31-01, SRM AND 51-30-02. 2 L 7 2 4F RT A20EU 1998032600211 19980326 00211 EU 1998 3 26 QXEA9800375 1 19980214 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FRAME 18575 CHAFFED FROM CONTACT WITH WIRE BUNDLE AT STRINGER 58 .4 LONG BY .15 WIDTH BY .013 DEPTH. REPAIRED IA W HORIZON EA 4-53-385. 2 L 7 2 4F RT A20EU 1998032600212 19980326 00212 EU 1998 3 26 QXEA9800376 1 19980219 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT FRAME 18575 SKIN CONNECTION ANGLE CRACKED PASSED STOP DRILL. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PA GE 4. 2 L 7 2 4F RT A20EU 1998032600213 19980326 00213 EU 1998 3 26 QXEA9800377 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT OBLIQUE FRAME 16-2 CONNECTION ANGLE CRACKED AT STRINGER 25 FORWARD SIDE. REPAIRED IAW FOKKER SRM 53-01-01, 5 1-31-01. 2 L 7 2 4F RT A20EU 1998032600214 19980326 00214 EU 1998 3 26 QXEA9800378 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT OBLIQUE FRAME 16-2 CONNECTION ANGLE CRACKED AT STRINGER 26 FORWARD SIDE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600215 19980326 00215 EU 1998 3 26 QXEA9800379 1 19980211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - OBLIQUE FRAME 16-2 STRINGER 25 CLIP REPAIR. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1998032600216 19980326 00216 EU 1998 3 26 QXEA9800380 1 19980211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - OBLIQUE FRAME 16-2 STRINGER 26 CLIP REPAIR. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1998032600217 19980326 00217 EU 1998 3 26 QXEA9800381 1 19980224 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LEFT OBLIQUE FRAME 16-2 CONNECTION ANGLE REPAIR AT STRINGER 33, FORWARD SIDE. REPAIRED IAW FOKKER SRM 53-10-05, S RM 51-30-02. 2 L 7 2 4F RT A20EU 1998032600218 19980326 00218 EU 1998 3 26 QXEA9800382 1 19980207 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIB 3.4 IN VERTICAL STAB IS CRACKED AT LEFT AND RIGHT AFT CORNERS AT COVE ATTACH POINT. REPAIRED IAW HORIZON AIR EA 4-55-46. 2 L 7 2 4F RT A20EU 1998032600219 19980326 00219 EU 1998 3 26 QXEA9800383 1 19980226 A 5511 SPAR WEB FOKKER F28 F28MK4000 4990810 EU HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - HORIZONTAL STAB SPAR WEB BETWEEN RIBS 3145 AND 3800 ON LEADING EDGE. INSTALLED NUT PLATES ON LEADING EDGE TOP AND BOTTOM BETWEEN RIBS 3145 AND 3800. 2 L 7 2 4F RT A20EU 1998032600220 19980326 00220 EU 1998 3 26 QXEA9800384 1 19980221 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU CARGO COMPT MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 476US 11224 PDX - FORWARD CARGO COMPARTMENT FLOOR FRAME 4610 HAS HAD SEVERAL SHORT ANTI-CHAFE STRIPS. STRIPS WERE INSTALLED WITH MU LTIPLE CHERRY MAX RIVETS THROUGH FRAME WITH ALL NEW HOLES DRILLED. ONE NEW RIVET IS INSTALLED THROUGH PREVIOUS SOLID RI VET ON FRAME. REMOVED AND REPLACED PREVIOUS SPLICE AT FRAME 4610 IAW FOKKER SRM 51-31-01, PAGE 13-17, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1998032600221 19980326 00221 EU 1998 3 26 QXEA9800385 1 19980206 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE BUCKLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - FLOORBEAM BETWEEN FRAME 16060 AND 16660 BL 0 IS BUCKLED AT THE NUTPLATES. REPAIRED IAW HORIZON AIR EA 4-53-347. 2 L 7 2 4F RT A20EU 1998032600222 19980326 00222 EU 1998 3 26 QXEA9800386 1 19980205 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CRACKS FOUND ON ANGLE/CHANNEL INSIDE RIGHT MAIN LANDING GEAR WHEEL WELL, AT UPPER OUTBOARD, AFT CORNER, JUST FORWA RD OF FRAME 13345. REPAIRED IAW HORIZON AIR EA 4-53-344. 2 L 7 2 4F RT A20EU 1998032600223 19980326 00223 EU 1998 3 26 QXEA9800387 1 19980206 A 5280 HINGE FOKKER F28 F28MK4000 4990810 EU LT MLG DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - LIGHT CORROSION ON FUSELAGE STRUCTURE INSIDE LEFT MAIN LANDING GEAR WHEEL WELL, ALONG ATTACHING POINT OF INBOARD D OOR HINGE. REPAIRED IAW HORIZON AIR EA 4-53-359. 2 L 7 2 4F RT A20EU 1998032600224 19980326 00224 EU 1998 3 26 QXEA9800388 1 19980206 A 5720 VANE FOKKER F28 F28MK4000 4990810 EU RT WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - RIGHT WING OUTBOARD FLAP VANE INBOARD TOP SIDE DENTED DOWN AT DOUBLER FOR SHROUD PANEL. REPAIRED IAW FOKKER SRM 5 7-02-06, FIGURE 4, PAGE 6-7. 2 L 7 2 4F RT A20EU 1998032600225 19980326 00225 EU 1998 3 26 QXEA9800389 1 19980208 A 5720 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - CENTER WING LOWER SKIN 2 STRINGER TO BELLY FAIRING ATTACH CLIP IS CRACKED AT THE 7TH STRINGER BACK FROM FRONT OF C ENTER WING AND WS 1700. REPAIRED IAW FOKKER SRM 53-02-17, PAGE 10, FIGURE 6 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1998032600226 19980326 00226 EU 1998 3 26 QXEA9800390 1 19980208 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - WEB THAT TIES THE PNEUMATIC TUNNEL WALL TO THE LOWER WING SKIN IS CRACKED IN FOUR LOCATIONS AT STRINGER CUT OUTS A BOVE THE AFT END OF THE UPPER ACCUMULATOR. REPAIRED IAW HORIZON AIR EA 4-53-349. 2 L 7 2 4F RT A20EU 1998032600227 19980326 00227 EU 1998 3 26 QXEA9800391 1 19980208 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 PDX - WEB THAT TIES THE PNEUMATIC TUNNEL WALL TO THE LOWER WING SKIN IS CRACKED IN FOUR LOCATIONS AT STRINGER CUT OUT, V ISIBLE THROUGH PANEL 95D, RIGHT. REPAIRED IAW HORIZON AIR EA 4-53-349. 2 L 7 2 4F RT A20EU 1998032600228 19980326 00228 EU 1998 3 26 QXEA9800392 1 19980318 A 3350 5515900004 CIRCUIT CARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 SEA- AFT EMERGENCY EXIT SIGN IS INOP. REPLACED CIRCUIT CARD. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998032600229 19980326 00229 EU 1998 3 26 QXEA9800393 1 19980318 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 PDX- LEFT FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998032600230 19980326 00230 EU 1998 3 26 QXEA9800394 1 19980318 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 487US 11238 PDX - OVERHEAD EMERGENCY EXIT LIGHTS INOP. RELAMPED EXIT LIGHTS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC E. 2 L 7 2 4F RT A20EU 1998032600231 19980326 00231 EU 1998 3 26 QXEA9800395 1 19980318 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 493US 11161 SEA - EMERGENCY LIGHT AT ROW 9E IS BURNT OUT. RELAMPED, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998032600232 19980326 00232 NM 1998 3 26 98FDEA00208 1 19980319 A 3010 GASKET BOEING 727 72724C 1384005 NM NR 3 ENGINE LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS J M WARNING INDICATION OVER TEMP CL CLIMB 1 SO 25 114FE 19527 98-0074, DURING CLIMB-OUT, THE NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. ENG NR 3 BLEED AIR SWITCH WAS CLOSED AT THE TIME TH E LIGHT ILLUM. APPROPRIATE RED TABS WERE ACCOMPLISHED AND THE LIGHT WENT OUT PRIOR TO THE STEP REQUIRING POWER REDUCTIO N. WING ANTI-ICE WAS NOT BEING USED. RAN NR 3 ENGINE, FOUND WING ANTI-ICE HIGH PRESSURE SHUT OFF VALVE LEAKING AT GASK ET. REPLACED GASKET, VISUALLY INSP ALL DUCTS, WIRING AND NR 3 STRUT FIRE LOOP FOR INTEGRITY. RAN NR 3 ENGINE PER JET R UN HANDBOOK. LEAK CHECK GOOD NR 3 STRUT OVERHEAT CHECKS GOOD. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998032600233 19980326 00233 NM 1998 3 26 98FDEA00209 1 19980320 A 3610 652663928 DUCT BOEING 727 72724C 1384005 NM NR 3 PYLON FAILED A FDEA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 114FE 19527 DURING CLIMBOUT, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUM. BOTH NR 3 BLEED AND RIGHT PACK WERE ON AT THE TIME. AFTER RED TABS CALLED FOR CLOSING/OFF ON BOTH NR 3 BLEED AND RIGHT PACK, THE NR 3 STRUT LIGHT WENT OUT. ENGINE PARAMETERS OK . REMOVED AND REPLACED CRACKED DUCT FOUND DURING ENGINE RUN UP PER M/M 36-00-02. NEEDS LEAK AND OPERATIONAL CK. RAN E NG PER JET RUN HANDBOOK, STRUT OVERHEAT LIGHT DID NOT ILLUMINATE. DURING LEAK CK FOUND AIR LEAKING AT GASKET, (P/N 8003 47) REF ITEM NR 30 ILLUSTRATED PART CAT 36-10-00 FIGURE 5 GASKET IN STOCK PHX, REMOVED ADN REPLACED DUCT PER M/M REF 36- 00-2, LEAK CK GOOD. 2 L 7 3 4F A3WE 1998032600234 19980326 00234 NM 1998 3 26 98FDEA00210 1 19980318 A 5751 SPAR WEB BOEING 727 727233 138408A NM RT AILERON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0901, RT AILERON, OUTBOARD HAS CRACK IN SPAR WEB AT FASTENER HOLE. THIS REPAIR TIED TO REPAIR BEING PERFORMED ON NR0 324. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED REPAIR PER EA 7-5750-29411. 2 L 7 3 4F RT A3WE 1998032600235 19980326 00235 NM 1998 3 26 98FDEA00211 1 19980318 A 5751 SKIN BOEING 727 727233 138408A NM RT AILERON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0905, RT OUTBD AILERON HAS .25 INCH DIAMETER CHERRY MAX FASTENER IN UPPER SKIN, RIB IS .600 WIDE, ORIGINAL FASTENERS WERE .125 INCH DIAMETER, COUNTER SINK INTO RIB WILL HAVE DAMAGED RIB AND MINIMUM ED IS LOST IN RIB. REMOVED AND REPLACE D RIB PER SRM 51-10-1. SKIN REPAIR ACCOMPLISHED ON NR0906. AILERON BALANCE AND INSTALLATION ON NR0324. 2 L 7 3 4F RT A3WE 1998032600236 19980326 00236 NM 1998 3 26 98FDEA00212 1 19980320 A 5311 FRAME BOEING 727 727233 138408A NM BS 1148 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0978 71C 701 - LWR AFT CARGO, FUSE BS 1148, UPPER BELTFRAME FLANGE WORN IN EXCESS OF 50 PERCENT NEAR STR 22 LEFT. B LENDED OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998032600237 19980326 00237 NM 1998 3 26 98FDEA00213 1 19980312 A 3350 3005441 LIGHT BOEING 727 727233 138408A NM PAX DOOR RUSTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0407, FWD ENTRY DOOR SLIDE LIGHT HAS LENS SCREWS NUT PLATES RUSTED OFF. REMOVED AND INSTALLED SERVICEABLE SLIDE LIGH T ASSY NR 33960. 2 L 7 3 4F RT A3WE 1998032600238 19980326 00238 NM 1998 3 26 98FDEA00214 1 19980318 A 5751 RIVETS BOEING 727 727233 138408A NM RT AILERON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 NR 0324, RT WING OUTBOARD AILERON HAS APPROX 70 RIVETS WORKING AND LOOSE ALONG UPPER SKIN FRONT SPAR ATTACHMENT. REMOVE D AND REPLACED RIVETS PER EA 7-5750-29411, SRM 57-50-5 SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998032600239 19980326 00239 NM 1998 3 26 98FDEA00215 1 19980318 A 5751 SKIN BOEING 727 727233 138408A NM RT AILERON DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 268FE 21674 RT OUTBD AILERON HAS .25 INCH DIAMETER CHERRY MAX IN UPPER SKIN, COUNTER SINK IS TOO DEEP, IN SKIN .040 THICK. REMOVED DAMAGE AND INSTALLED FLUSH DOUBLER PER SRM 57-50-5 AND CUT OUT RIB AREA TO FACILITATE DOUBLER AND INSTALLED TYPICAL FORM ED SECTION REPAIR TO RIB PER SRM 51-40-3. POINT, BALANCE, INSTALLATION OF AILERON ACCOMPLISHED ON NR 0324. 2 L 7 3 4F RT A3WE 1998032600240 19980326 00240 NM 1998 3 26 98FDEA00216 1 19980319 A 5313 STRINGER BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 263FE 21625 NR 0228 71C 709-02, LOWER LOBE AFT CARGO CORROSION ON OUTBD FLANGE OF STR 29L FROM BS 950E TO BS 990. INSTALLED STRINGE R REPAIR ON STRINGER 29L 950E TO 990 PER EA 7-5310-29401 DATED MARCH 07, 1998. 2 L 7 3 4F RT A3WE 1998032600241 19980326 00241 NM 1998 3 26 98FDEA00203 1 19980318 A 5320 69139651 SPLICE BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 NR 0439 014, BS 870 LT UPPER SPLICE PLATE FOR UPPER CHORD HAS 2 CRACKED HOLES AND 1 DAMAGED HOLE AOG ACCESS REQUIRED. R EMOVED AND REPLACED BS 870 LT UPPER SPLICE PLATE PER BOEING DRAWING 64-8336. 2 L 7 3 4F A3WE 1998032600242 19980326 00242 WP 1998 3 26 MWEA98367 1 19980316 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND 3 AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK POWER SUPPLY. 2 L 7 2 4F A6WE 1998032600243 19980326 00243 WP 1998 3 26 MWEA98368 1 19980317 A 3350 6011777 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 207ME 47794 FOUND LT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK POWER SUPPLY. 2 L 7 2 4F A6WE 1998032600244 19980326 00244 WP 1998 3 26 MWEA98369 1 19980317 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 207ME 47794 THE EMERGENCY LIGHTS AT ROW 15 TO 18 COME ON WHEN POWER IS OFF AND EMERGENCY LIGHT SWITCH IS IN OFF POSITION. MAINTENAN CE REMOVED AND REPLACED BATTERY POWER SUPPLY. 2 L 7 2 4F A6WE 1998032600245 19980326 00245 WP 1998 3 26 MWEA98370 1 19980318 A 3350 100865 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHAREGD A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 301ME 47190 THE FIRST SECTION OF FLOOR TRACK LIGHTING WOULD NOT LIGHT UP. MAINTENANCE REMOVED AND REPLACED FIRST SECTION FLOOR TRAC K EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1998032600246 19980326 00246 NM 1998 3 26 DL72S980593 1 19980317 A 5320 WEB BOEING 727 727232 1384082 NM BS 1235 CRAKCED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND .375 INCH CRACK RT VERT WEB UPPER LIGHTENING HOLE STA 1235, .5 INCH CRACK RT VERT WEB UPPER LIGHTENING HOLE STA 12 43. REPAIRED PER MM 53-11-0 P 828. 2 L 7 3 4F A3WE 1998032600247 19980326 00247 NM 1998 3 26 DL72S980595 1 19980317 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FOUND .75 INCH CRACK IN VERT STAB STRINGER 8R AT THIRD BULKHEAD ABOVE CRAWLWAY OPENING FIN STA 133.8. REPAIRED PER MM 5 5-30-0 FIG 803. 2 L 7 3 4F A3WE 1998032600248 19980326 00248 NM 1998 3 26 DL72S980596 1 19980317 A 7110 COWL BOEING 727 727232 1384082 NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 FOUND .75 INCH CRACK NR 2 ENG NOSE COWL 10 INCH AFT OF NOSE RING 3.00 POS. REPAIRED PER MM 54-30-0 P 801. 2 L 7 3 4F A3WE 1998032600249 19980326 00249 WP 1998 3 26 DLL10980597 1 19980317 A 3350 305 BULB 305 LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 733DS 193C1224 EXTERIOR EMERGENCY EXIT LIGHTS AT DOOR 3L 3R AND 4R ARE INOP. 2 L 7 3 4F A23WE 1998032600250 19980326 00250 NM 1998 3 26 DL72K980598 1 19980317 A 3350 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 480DA 20860 FORWARD EMERGENCY AISLE LIGHT BURNT OUT. FWD GALLEY OVERHD, RELAMPED. 2 L 7 3 4F A3WE 1998032600251 19980326 00251 NM 1998 3 26 DL72W980602 1 19980318 A 5320 WEB BOEING 727 727247 138408F NM BS 1212 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 FOUND DURING B-2 LETTER CHECK, LWR TORQUE BOX VERT WEB CRACKED FS 1212 LT SIDE AT TOP OF WEB. REPAIRED PER M/M 53-11-0 PAR 19. 2 L 7 3 4F A3WE 1998032600252 19980326 00252 NM 1998 3 26 DL72W980603 1 19980318 A 5320 WEB BOEING 727 727247 138408F NM BS 1283 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 FOUND DURING B-2 LETTER CHECK, LWR TORQUE BOX VERT WEB CRACKED FS 1283 RT SIDE AT LIGHTENING HOLE. REPAIRED PER M/M 53- 11-0 PAR 15. 2 L 7 3 4F A3WE 1998032600253 19980326 00253 NE 1998 3 26 DLL19980604 2 19980318 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 3 MALFUNCTIONED A DALA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 SO 27 761DA 26199 193Y1208 14720 WHILE DES FROM FL310 TO FL290, NR 3 ENG VIBE LIGHT ILLUMINATED. VIBES ROSE RAPIIDLY TO 3.5 CONFIRMED BOTH A AND B SENSO RS. SHUT DOWN ENGINE PER POM. INSPECTED INLET AND EXHAUST, REMOVED AND INSPECTED CHIP DETECTORS, NO DEFECTS. LUBED FA N BLADES AND RAN ENG TO T/O POWER, ENG RUN GOOD. RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1998032600255 19980326 00255 NM 1998 3 26 DL72W980606 1 19980318 A 5320 WEB BOEING 727 727247 138408F NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 295WA 22532 14720 VERT WEB ABOVE S DUCT CRACKED .625 INCH AT STR CUT OUT STA 1303 LT. REPAIRED PER SRM 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1998032600256 19980326 00256 NM 1998 3 26 DL76L980608 1 19980318 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 179DN 932 25144 EMERGENCY ESCAPE PATH LIGHTING INOP CTR LFT COACH. REPLACED POWER SUPPLY M9009 AND BATTERY PACK OP CKS OK. 2 L 7 2 4F RT A1NM 1998032600257 19980326 00257 WP 1998 3 26 DLL14980609 1 19980318 A 3350 672320101 BATTERY PACK LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 193C1244 EMERGENCY LIGHT PWR SUPPLY STAYS ON AFTER TURNING LIGHTS OFF. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1998032600258 19980326 00258 NM 1998 3 26 DL72W980610 1 19980309 A 2782 BRACKET BOEING 727 727247 138408F NM NR 5 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 14720 FOUND .125 INCH VISIBLE CRACK AT NR 5 L/E FLAP ACTUATOR MOUNT BOX I/B LOWER CORNER MARKED. REPAIRED PER MM 57020-21 P 8 11. 2 L 7 3 4F A3WE 1998032600259 19980326 00259 NM 1998 3 26 DL72S980612 1 19980223 A 5311 FRAME BOEING 727 727232 1384082 NM LT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 14720 ITEM: AT HMV TEMPORARY REPAIR LMLG UPLOCK FITTING SUPPORT FRAME AFT WEB. REPAIRED PER MM 53-11-0 FIG 814. 2 L 7 3 4F A3WE 1998032600260 19980326 00260 NM 1998 3 26 DL72S980613 1 19980223 A 5312 BULKHEAD SKIN BOEING 727 727232 1384082 NM RT MLG WW CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 14720 AT HMV, FOUND APU BLEED AIR CUTOUT FWD BLKHD RT W/W SKIN CRACKED. REPAIRED PER SRM 53-10-9 FIG 5. 2 L 7 3 4F A3WE 1998032600261 19980326 00261 NM 1998 3 26 P5CA9800505 1 19980313 A 8012 BACC63AF243058 CONNECTOR BOEING 747 747122 1384872 NM NR 4 ENGINE CONTAMINATED A P5CA D RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 23 853FT 19753 NR 4 ENG START VALVE OPEN LIGHT ON. RETURNED TO RAMP. FAULT T/S CARRIED OUT. SHAKE CHECK OF WIRING ON ENG STRUT PLUGS AND ENG DISCONNECT PLUGS UNABLE TO REPRODUCE DEFECT. ENG DISCONNECT PLUG D0014P DISCONNECTED AND FOUND STRUT CONNECTOR D0044J BADLY CONTAMINATED AND INSULATION ROTTEN. CHANGED CONNECTOR PER WDM 20-11-11 AND SYSTEM CHECKED OK ON ENG RUN. 2 L 7 4 4F A20WE 1998032600262 19980326 00262 NM 1998 3 26 P5CA9800506 1 19980311 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LT WING UPPER TRAILING EDGE, FIXED PANEL DELAMINATED FWD OF SPOILER NR 5. SANDED AREA, REMOVED DAMAGED OUTER PANEL INST FIBERGLASS FILLER AND OVERLAY, BONDED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998032600263 19980326 00263 NM 1998 3 26 P5CA9800507 1 19980311 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LT WING TOP FIXED PANEL IN FRONT OF SPOILER NR 5 OUTER HINGE PANEL DELAMINATION. CUT OUT DAMAGED AREA. REMOVED WATER C ONTAMINATION AND APPLIED FIBERGLASS OVERLAY PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998032600264 19980326 00264 NM 1998 3 26 P5CA9800508 1 19980310 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 1590 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 AFT CARGO COMPARTMENT APPROX STA 1590 LBL 30 SUB FLOOR INTERCOSTAL BENT AND CRACKED. INSTALLED NEW FABRICATED INTERCOST AL WEB ASSY. 2 L 7 4 4F A20WE 1998032600265 19980326 00265 NM 1998 3 26 P5CA9800509 1 19980311 A 5753 PANEL BOEING 747 747122 1384872 NM RT TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 RT WING OUTBD FLAP COVE LIP PANEL HAS CRACK. REMOVED DAMAGE AREA, POTTED CRACKED HONEYCOMB, APPLIED FIBERGLASS FILLER A ND OVERLAY PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998032600266 19980326 00266 NM 1998 3 26 P5CA9800510 1 19980311 A 5755 SKIN BOEING 747 747122 1384872 NM NR 3 SPOILER MISREPAIRED A P5CA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 23 850FT 19755 NR 3 SPOILER HAS POSSIBLE INCORRECT REPAIR TO UPPER SURFACE. REPAIRED IN ACCORDANCE WITH SRM 51-40-06. 2 L 7 4 4F A20WE 1998032600267 19980326 00267 NM 1998 3 26 P5CA9800511 1 19980313 A 5280 DOOR BOEING 747 747122 1384872 NM LT MLG DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LT WING GEAR FLYING DOOR DELAMINATED OUTER AFT CORNER. REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING NEW FIBERGLASS OVE RLAYS PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998032600268 19980326 00268 NM 1998 3 26 P5CA9800512 1 19980310 A 5350 FAIRING BOEING 747 747122 1384872 NM BS 1460-1520 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FUSELAGE LT BODY FAIRING STA 1460-1520 JUST AFT LT BODY WHEEL WELL CRACKED AT 2 PLACES. REMOVED AND REPAIRED PANEL PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998032600269 19980326 00269 NM 1998 3 26 P5CA9800513 1 19980311 A 5320 SILL BOEING 747 747122 1384872 NM CARGO DOORWAY CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 AFT CARGO DOOR SERRATED PLATE 3, 4, 5 AND 8 HAS CORROSION ON DOOR SILL AREA. REMOVED CORROSION PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998032600270 19980326 00270 NM 1998 3 26 P5CA9800514 1 19980313 A 5753 PANEL BOEING 747 747122 1384872 NM LT TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LT WING OUTBD FLAP COVE LIP PANEL CRACKED. REPAIRED AND APPLIED FIBERGLASS OVERLAY PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998032600271 19980326 00271 NM 1998 3 26 P5CA9800515 1 19980312 A 5755 SKIN BOEING 747 747122 1384872 NM NR 6 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NR 6 SPOILER INBD EDGE SEPARATED AND HAS 2 AREAS OF DELAMINATION. REPAIRED WITH FIBERGLASS AND BONDED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998032600272 19980326 00272 NM 1998 3 26 P5CA9800516 1 19980312 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NR 3 INBD C/C TOP SIDE AFT END EXTERIOR SKIN CRACKED. REPAIRED PER SRM 54-10-03. 2 L 7 4 4F A20WE 1998032600273 19980326 00273 WP 1998 3 26 CKSA98092 1 19980308 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 1792 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, STRINGER 32 AT STA 1792 CRACKED. INSTALLED STRINGER REPAIR IAW L1011 SRM 53-13-00 PG 806. CORROSION TASK CARD NUMBER C53-120-04-03. NON-ROUTINE TASK CARD NUMBER 15868. 2 L 7 3 4F A23WE 1998032600274 19980326 00274 WP 1998 3 26 CKSA98093 1 19980308 A 5320 JAMB LKHEED 1011 1011385115 5265015 WP BS 1675 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION AFT PIT DOOR JAM SILL, CORROSION AT FWD LOWER CORNER. REMOVED A ND REPLACED CORRODED FILLER IAW L1011 SRM 51-40-01. CORROSION TASK CARD NUMBER C53-120-04-03. NON-ROUTINE TASK CARD NU MBER 15867. 2 L 7 3 4F A23WE 1998032600276 19980326 00276 WP 1998 3 26 CKSA98095 1 19980308 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 963/983 BULGING A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, SKIN BULGING AT LONG 30 BETWEEN FS 963 AND FS 983. REMOVED DAMA GE AND FABRICATED REPAIR DOUBLERS IAW AIA SKETCH AIA/E/2767. INSTALLED REPAIR DOUBLER IAW AIA SKETCH AIA/E/2767 REV ORI G DTD 03 MAR 98 AND EA L1-53-018 DTD 06 MAR 98. CORROSION TASK CARD NUMBER C53-130-06-00. NON-ROUTINE TASK CARD NUMBER 15882. 2 L 7 3 4F A23WE 1998032600277 19980326 00277 WP 1998 3 26 CKSA98096 1 19980308 A 5320 ANGLE LKHEED 1011 1011385115 5265015 WP BS 969 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, KEELSON SUPPORT ANGLE CORRODED RBL45 STA 969. INSTALLED REPAIR DOUBLERS IAW AIA SKETCH AIA/E/2765 REV ORIG DTD 03 MAR 98 AND EA L1-53-017 DTD 06 MAR 98. CORROSION TASK CARD NUMBER C5 3-130-06-00. NON-ROUTINE TASK CARD NUMBER 15892. 2 L 7 3 4F A23WE 1998032600278 19980326 00278 WP 1998 3 26 CKSA98097 1 19980308 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 970 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, STRINGER 32 HAS CORROSION AT STA 970. REMOVED CORRODED STRINGER DAMAGE AND FOUND OUT OF LIMITS IAW L1011 SRM 51-10-02. INSTALLED REPAIR IAW L1011 SRM 53-13-00 FIG 804. CORROSION TAS K CARD NUMBER C53-130-06. NON-ROUTINE TASK CARD NUMBER 15893. 2 L 7 3 4F A23WE 1998032600279 19980326 00279 NE 1998 3 26 TC8A98014 2 19980320 A 7230 COMPRESSOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE LT ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 181SK 45910 ABORTED TAKEOFF DUE TO LOUD NOISE LEFT SIDE OF AIRCRAFT. CHECKED TIRES, LANDING GEAR, FUSELAGE AND ALL 4 ENGINES FOR DA MAGE, NO DAMAGE NOTED. RAN ALL 4 ENGINES TO T/O POWER, NO COMPRESSOR STALL NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1998032600281 19980326 00281 CE 1998 3 26 98ZZZX1102 1 19980302 A 3252 7148876 STEERING UNIT CESSNA 750 750 2076810 CE NLG MALFUNCTIONED A I5EA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 07 710AW 161 0053 7500033 DURING TAXI AFTER LANDING, AIRCRAFT STARTED TO TURN LEFT WITHOUT INPUT TO TILLER OR RUDDER PEDALS. AIRCRAFT EXAMINED AN D NO APPARENT CAUSE WAS IDENTIFIED. CONTACTED CESSNA AND REQUESTED A REPLACEMENT STEERING UNIT. TECHNICIANS FOR ICT AN D LGB CAME TO PHX AND CHANGED OUT UNIT. JACKED AIRCRAFT AND PERFORMED RIGGING AND OPERATIONAL CHECKS. AIRCRAFT TAXI CH ECKED AND FUNCTIONAL CHECK FLIGHT PERFORMED. TC: 119. 2 L 7 2 4J RT T00007WI 1998032600282 19980326 00282 CE 1998 3 26 98ZZZX1103 1 19980303 A 2750 FL23 CURRENT LIMITER CESSNA 650 650 2076802 CE FLAPS FAILED A I5EA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 07 651JM 2119 6500241 DURING NORMAL APPROACH WHEN FLAPS WERE SELECTED FROM SEVEN DEGREE POSITION TO TWENTY DEGREES, FLAPS STARTED DOWN THEN ST OPPED. NO ADVERSE EFFECTS FELT ON THE AIRCRAFT AND NORMAL LANDING MADE. TOLEDO CITATION SERVICE CENTER HELP WAS REQUES TED AND THEY CAME TO AIRCRAFT. CHECKED AIRCRAFT AND FOUND DEFECTIVE CURRENT LIMITER. REPLACED LIMITER WITH NEW AND OPE RATIONAL CHECKED FLAP SYSTEM. AFTER SEVERAL OPERATIONS, RELEASED AIRCRAFT BACK TO SERVICE. OPERATIONAL FLIGHT CHECK PE RFORMED. FLIGHT TO TOLEDO SHOWED NO ABNORMAL OPERATION. TC 1,367. 2 L 7 2 4F A9NM 1998032600290 19980326 00290 GL 1998 3 26 98ZZZX1111 1 19980219 A 6310 ECD01413 STRUT BEARING ENSTRM F28 280C 3300505 GL M/R DRIVE CRACKED A L FSPA K NONE O OTHER IN INSP/MAINT 1 NE 05 5695B 18 1204 CAGE OF UPPER JACK STRUT BEARING WAS FOUND BROKEN DURING ANNUAL INSPECTION WHILE GREASING BEARING. THIS WAS THE SECOND BEARING FOUND IN THIS CONDITION. IT SHOULD BE NOTED THIS BEARING HAS A 600-HOUR LIFE LIMIT AND A 100-HOUR LUBE SCHEDULE . SUBMITTER STATED THIS BEARING WAS ORIGINALLY INTENDED TO BE HAND-PACKED. 1 G 7 1 3O H1CE 1998032600294 19980326 00294 NE 1998 3 26 ANCF9802 2 19980227 A 7321 GOVERNOR WOODWARD BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FUEL MALFUNCTIONED W ANCF C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 23 987AN 6094 2488758 25494 BOG/MEX - FLT 072 - LEFT EEC AND ENGINE LIMITER INOPERATIVE. LIGHT ILLUMINATED. EICAS MESSAGE. LT ENGINE EEC, LT ENGI NE LIMITER DISPLAYED, REJECTED TAKEOFF. READING CODE FAULT EEC NR 31 FOUND AND PERFORMED PROCEDURE IAW THIS CODE, FFG C ONNECTOR'S WERE CHECKED, CLEANED, AND ADJUSTED. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1998032600328 19980326 00328 EU 1998 3 26 MALA976058 1 19980319 A 5330 SKIN SAAB SF340 SF340A 7850100 EU BS 668-710 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 103XJ 340A103 DURING HEAVY CHECK FOUND DENT, EVALUATED DAMAGE AND CONTACTED SAAB ENGINEERING. MAINTENANCE REMOVED DAMAGED AREA BETWEE N STA 668 AND STA 710 ON RIGHT SIDE OF AIRCRAFT. FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW SAAB ENGINEERI NG STATEMENT 72SDS0901 TEMPORARY REPAIR, GOOD FOR UP TO 500 HOURS PENDING DAMAGE TOLERANT ANALYSIS AND SAAB 340 SRM 53-8 0-10 FIG 202. 2 L 7 2 4T RT A52EU 1998032600329 19980326 00329 NM 1998 3 26 MALA976059 1 19980321 A 2913 570347 HYDRAULIC PUMP DHAV DHC8 DHC8102 2809003 NM NR 2 HYD SYST FAILED A MALA A UNSCHED LANDING S AFFECT SYSTEMS CR CRUISE 1 GL 15 846MA 344 DURING FLIGHT, NR 2 HYDRAULIC SYSTEM FAILED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED RIGHT ED HYDRAULIC PUMP AN D NOSE GEAR ACTUATOR HOSE ASSEMBLY (PN OSC252B4-0124). LEAK CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998032600330 19980326 00330 EU 1998 3 26 MALA976060 1 19980320 A 2150 7792152 HEAT EXCHANGER SAAB SF340 340B 7860101 EU MAINTENANCE BAY FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 415XJ 340B415 DURING FLIGHT, THE RIGHT DUCT OVERTEMP LIGHT ILLUMINATED. CREW CLOSED RIGHT BLEED PUT IN AUTO MODE, REFERRED TO QRH, RE CYCLED TEMP SELECT AUTO MODE AND RIGHT BLEED CLOSED AGAIN. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT HE AT EXCHANGER AND RIGHT COMPRESSOR DISCHARGE OVERTEMP SWITCH (PN 67121-52-440) IAW SF340MM 21-61-00. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998032600331 19980326 00331 EU 1998 3 26 MALA976061 1 19980320 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 89XJ 089 DURING INSPECTION, RIGHT OVERHEAD EMERGENCY LIGHT INOP AT 9D. MAINTENANCE RELAMPED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998032600332 19980326 00332 EU 1998 3 26 MALA976062 1 19980321 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 41XJ 041 DURING INSPECTION, OVERHEAD EMERGENCY LIGHT INOP AT 9D. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998032600333 19980326 00333 EU 1998 3 26 MALA976063 1 19980323 A 3350 SWITCH BAC 146 AVRO146RJ85A 1500097 EU CABIN MALFUNCTIONED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 503XJ E2310 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHTING AFT RIGHT CABIN IS INOP. MAINTENANCE RECYCLED AIRCRAFT POWER, CYCLED EMERGENCY LIGHT SWITCH. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998032600334 19980326 00334 1998 3 26 CALA9800537 4 19980323 A 2565 5WD230600203 SLIDE DOUG DC10 DC1030 3023501 WP R-3 DOOR INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59083 89062 38 47926 INSPECTION FOUND THE R-3 DOOR SLIDE BOTTLE PRESSURE LIGHT ILLUMINATED. THE R-3 DOOR SLIDE WAS REMOVED AND REPLACED AND THE LIGHT TESTED NORMAL. 2 L 7 3 4F A22WE 1998032600335 19980326 00335 WP 1998 3 26 CALA9800538 1 19980321 A 3234 GEAR HANDLE DOUG DC9 DC982 3022082 WP LANDING GEAR MALFUNCTIONED A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 35832 49492 THE LANDING GEAR HANDLE WOULD NOT MOVE DOWN UPON INITIAL ATTEMPT TO LOWER, WHILE ON APPROACH. ALTERNATE GEAR EXTENSION WAS USED, AND THEN CREW WAS ABLE TO MOVE GEAR HANDLE DOWN AFTER EXTENSION. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE A IRCRAFT WAS JACKED IAW MM 7-11-00 AND THE GEAR HANDLE WAS CYCLED EIGHT TIMES AND ALL GEAR FUNCTIONS WERE NORMAL WITH SMO OTH GEAR HANDLE OPERATION. 2 L 7 2 4F A6WE 1998032600336 19980326 00336 NM 1998 3 26 CALA9800539 1 19980319 A 5712 RIB BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH CRACK IN LT WING LOWER TRAILING EDGE PANEL SUPPORT RIB JUST INBOARD OF NR 3 SPOILER ACTUATOR I N FLAP COVE AREA. THE RIB SUPPORT WAS REMOVED, NEW PARTS WERE INSTALLED IAW SRM 51-10-6 AND 51-10-1. 2 L 7 3 4F A3WE 1998032600337 19980326 00337 NM 1998 3 26 CALA9800540 1 19980319 A 5712 RIB BOEING 727 727227 1384078 NM WS 656.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .25 INCH CRACK FROM END OF STRINGER ON TOP OF RIB, SECOND UPPER STRINGER FROM AFT SPAR, WS 656.50, AC CESS 7217. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW EA 5762-01050. 2 L 7 3 4F A3WE 1998032600338 19980326 00338 NM 1998 3 26 CALA9800541 1 19980319 A 5350 10010021PWS RADOME BOEING 727 727227 1384078 NM FWD FUSELAGE ERODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND THE RADOME EXTERIOR SKIN HAD SOME SPOTS OF EROSION AND A SMALL HOLE. THE RADOME WAS REMOVED AND REPLAC ED IAW MM 53-15-0. 2 L 7 3 4F A3WE 1998032600339 19980326 00339 NM 1998 3 26 CALA9800542 1 19980319 A 5711 SPAR WEB BOEING 727 727227 1384078 NM CENTER WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 4 INCH CRACK IN CENTER WING SECTION AT REAR SPAR WEB UPPER RADIUS ABOVE PRODUCTION PANEL FROM RBL 0 T O RBL 4. THE AREA WAS REPAIRED IAW EA SA004-5710-01843, DRAWING 65C37620, AND SERVICE BULLETIN 727-57A0182. 2 L 7 3 4F A3WE 1998032600340 19980326 00340 NM 1998 3 26 CALA9800543 1 19980319 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1148-1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND FLOOR MOUNT FRAME CORRODED AT AFT BIN STA 1148 TO 1166 BETWEEN STRINGER 26 TO 27R. A NEW FRAME WAS FAB RICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-40-5 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998032600341 19980326 00341 NM 1998 3 26 9804676305 1 19980321 A 3350 BATTERY PACK BOEING 747 747451 1384940 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND UPPER DECK AFT FLOOR EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATION AL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998032600342 19980326 00342 NE 1998 3 26 9804689606 2 19980319 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE RIGHT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 606NW 47225 653943 AS TAKEOFF POWER WAS APPLIED, A NOISE WAS HEARD FOLLOWED BY VIBRATIONS FROM THE RIGHT ENGINE. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT ENGINE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998032600343 19980326 00343 1998 3 26 9804699106 4 19980322 A 3417 2587400176 ADC DOUG DC9 DC915 3022036 WP E/E COMPT INOPERATIVE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 96S 41495 343 47206 DURING CLIMBOUT, THE CENTRAL AIR DATA COMPUTER BECAME INOPERATIVE. FLIGHT CREW FOLLOWED COM PROCEDURES, RETURNED TO DTW , AND LANDED WITHOUT INCIDENT. AFTER TEN MINUTES ALL FLIGHT INSTRUMENTS OPERATED NORMALLY. MAINTENANCE REPLACED THE CE NTRAL AIR DATA COMPUTER, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998032600344 19980326 00344 WP 1998 3 26 9804709864 1 19980321 A 3230 39140165505 CYLINDER DOUG DC9 DC951 3022051 WP RT MLG INOPERATIVE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 773NC 22463 5701 47775 DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR RED WARNING AND DOOR OPEN INDICATIONS REMAINED ILLUMINATED AFTER LANDING GE AR RETRACTION. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR BU NGEE CYLINDER, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998032600345 19980326 00345 WP 1998 3 26 9804719859 1 19980322 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, FOUND AFT CEILING EMERGENCY LIGHTING ABOVE TAIL CONE DIM. MAINTENANCE REPLACED POWER SUPPLY, OPERATI ONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998032600346 19980326 00346 WP 1998 3 26 9804729859 1 19980321 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, FOUND AFT ESCAPE PATH FLOOR LIGHTING ABOVE TAIL CONE INTERIOR HANDLE INOPERATIVE. MAINTENANCE REPLAC ED POWER SUPPLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998032600347 19980326 00347 WP 1998 3 26 9804739852 1 19980320 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP FLIGHT DECK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 PILOT REPORTED, THE EMERGENCY EXIT LIGHTING IN THE FLIGHT COMPARTMENT INOPERATIVE. MAINTENANCE RELAMPED THE FLIGHT DECK EMERGENCY EXIT LIGHT, REPLACED THE BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998032600348 19980326 00348 WP 1998 3 26 9804749150 1 19980321 A 3397 WIRE DOUG DC9 DC914 3022034 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8908E 45749 DURING LINE CHECK, FOUND A SECTION OF WIRING FOR EMERGENCY EXIT FLOOR LIGHTING PULLED OUT AT FORWARD END OF CABIN. MAIN TENANCE INSTALLED NEW WIRE CONNECTION, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998032600349 19980326 00349 WP 1998 3 26 9804759952 1 19980321 A 3231 LINK DOUG DC9 DC931 3022065 WP NLG DOOR BROKEN A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 916RW 47144 VIBRATION AND NOISE COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT WAS RETURNED TO MCI AND LANDED WITHOUT INCIDENT. E MERGENCY WAS DECLARED DUE TO OVERWEIGHT LANDING CONDITION. MAINTENANCE FOUND LEFT NOSE GEAR DOOR LINK BROKEN. REPLACED LINK AND LEFT NOSE GEAR DOOR ASSEMBLY WHICH WAS DAMAGED. 2 L 7 2 4F A6WE 1998032600350 19980326 00350 NE 1998 3 26 9804769982 2 19980319 A 7230 COMPRESSOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE LT ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 982US 45790 696466 DURING TAKEOFF ROLL AT 80 KNOTS, THE LEFT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW ABORTED TAKEOFF AND RETURNED TO TH E GATE. MAINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998032600351 19980326 00351 WP 1998 3 26 9804779907 1 19980321 A 3244 95502672 TIRE DOUG DC9 DC931 3022065 WP NLG DAMAGED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 GL 01 957N 47253 EXCESSIVE NOSE WHEEL VIBRATION OCCURRED DURING TAKEOFF ROLL AT APPROXIMATELY 50 KNOTS. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED BOTH NOSE WHEEL ASSEMBLIES. 2 L 7 2 4F A6WE 1998032600352 19980326 00352 WP 1998 3 26 9804789925 1 19980320 A 2910 LINE DOUG DC9 DC932 3022066 WP RT HYD SYST BROKEN A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 925US 47472 LOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE OCCURRED IMMEDIATELY AFTER GEAR RETRACTION. NOSE GEAR RETRACTED NO RMALLY BUT BOTH MAIN GEARS WERE STILL EXTENDED WITH GEAR DOOR OPEN LIGHT ILLUMINATED. FLIGHT WAS RETURNED TO MSP AND LA NDED WITHOUT INCIDENT. MAINTENANCE FOUND BROKEN HYDRAULIC LINE AT AUXILIARY HYDRAULIC PUMP. REPLACED LINE, AUXILIARY P UMP, RIGHT ENGINE DRIVEN PUMP, AND ALL FILTERS. LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600353 19980326 00353 WP 1998 3 26 9804799938 1 19980321 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1798U 47369 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT LIGHT AT ENTRY DOOR AND FORWARD SECTION OF FLOOR PROXIMITY EMER GENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600354 19980326 00354 WP 1998 3 26 9804809945 1 19980322 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8925E 45840 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 12, 13, AND 14 INOPERATIVE. REP AIRED BROKEN WIRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600355 19980326 00355 WP 1998 3 26 9804819617 1 19980322 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 617NW 47235 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS AT ROWS 5, 6, AND 7 INOPERATIVE. REPAIRED BR OKEN WIRE AT ROW 7 LIGHTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600356 19980326 00356 SO 1998 3 26 COMA9810071 1 19980321 A 3010 DE-ICE BOOTS EMB 120 EMB120RT SO WINGS FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 261CA 120254 STABILIZER AND WING LEADING EDGE DE-ICE FAILED. REPAIRED LEAKS IN WING AND STABILIZER DE-ICE BOOTS. 2 L 7 2 4T RT A31SO 1998032600357 19980326 00357 1998 3 26 COMA9860064 4 19980317 A 3442 6229302003 RADAR CNDAIR CL600 CL6002B19 EA RADAR COMPT INOPERATIVE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 938CA 5687 3794 7046 WEATHER RADAR INOP. REPLACED THE RTA844. 2 L 7 2 4F RT A21EA 1998032600358 19980326 00358 EA 1998 3 26 COMA9860065 1 19980321 A 3411 PITOT CNDAIR CL600 CL6002B19 EA FWD FUSELAGE CONTAMINATED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 984CA 7171 AIRSPEED COMPARATOR WARNING DURING TAKEOFF. PURGED WATER FROM THE PITOT SYSTEM. 2 L 7 2 4F RT A21EA 1998032600359 19980326 00359 NM 1998 3 26 UPS98226166 1 19980320 A 3350 9621015 BATT PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT AT AFT ATTENDANT PANEL UPPER POSITION INOP. REMOVED AND REPLACED EMERGENCY BA TTERY PACK AT AFT ATTENDANT POSITION. 2 L 7 3 4F A3WE 1998032600360 19980326 00360 WP 1998 3 26 UPS98826156 1 19980310 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1863 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, STA 1861 TO 1873 AT STR 2R THE DOUBLER EXTENDING UNDER THE LONGERON HAS CORROSION. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK 813-380. 2 L 7 4 4F RT 4A25 1998032600361 19980326 00361 WP 1998 3 26 UPS98826157 1 19980311 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, STA 320 AT RBL 50 THE LOWER CHANNEL OF THE FLOORBEAM IS CORRODED BEYOND LIMITS. REPAIRED AREA IAW 81 10-3 APPROVED DHC SK 813-472. 2 L 7 4 4F RT 4A25 1998032600362 19980326 00362 WP 1998 3 26 UPS98826158 1 19980310 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1786 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, STA 1786 AT STR 28L THE INTERNAL DOUBLER HAS CORROSION. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK 813-379. 2 L 7 4 4F RT 4A25 1998032600363 19980326 00363 WP 1998 3 26 UPS98826159 1 19980226 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1650 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 1650 BTWN STR 28L TO 32L THE INTERNAL SKIN IS CORRODED AND EXTENDS UNDER THE TEAR STRAP AT EACH B AY. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK707-590. 2 L 7 4 4F RT 4A25 1998032600364 19980326 00364 WP 1998 3 26 UPS98826160 1 19980306 A 5320 36431112 ANGLE DOUG DC8 DC871F 302199D WP BS 780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FLOORBEAM ATTACH ANGLE AT STA 780 HAS HEAVY CORROSION AND IS CRACKED. REMOVED AND REPLACED ATTACH AN GLE AT STA 780 RBL 45 TO 69 IAW DWG 3643111 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998032600365 19980326 00365 WP 1998 3 26 UPS98826161 1 19980226 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 1160-1120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 1160 TO 1220 BTWN STR 33R TO 34L. THE INTERNAL DOUBLER HAS MANY AREAS OF MODERATE CORROSION. RE PAIRED AREA IAW 8110-3 APPROVED DHC SH 707-569. 2 L 7 4 4F RT 4A25 1998032600366 19980326 00366 WP 1998 3 26 UPS98826162 1 19980227 A 5311 57546711 FRAME DOUG DC8 DC871F 302199D WP BS 260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYP-C, STA 260 BTWN LONGERON 34R 33L, THE FWD FACE OF THE FRAME IS CORRODED. REMOVED, FABRICATED AND INSTALL ED REPLACEMENT FRAME AND ASSOCIATED PARTS IAW DWG 5754671 AND SRM 53-4-1. 2 L 7 4 4F RT 4A25 1998032600367 19980326 00367 WP 1998 3 26 UPS98826163 1 19980225 A 5330 577991421 SKIN DOUG DC8 DC871F 302199D WP BS 1346-1354 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 1346 TO 1354 STR 24L TO 31L, THE SKIN AND THE FINGER DOUBLER HAVE MODERATE CORROSION. REMOVED CO RROSION FROM SKIN, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5779914 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998032600368 19980326 00368 WP 1998 3 26 UPS98826164 1 19980225 A 5330 577991421 SKIN DOUG DC8 DC871F 302199D WP BS 1346-1354 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 1346 TO 1354 STR 24L TO 31L, THE SKIN AND THE FINGER DOUBLER HAVE MODERATE CORROSION. REMOVED CO RROSION FROM SKIN, FOUND WITHIN LIMITS IAW SRM 53-2-0. FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5779914. 2 L 7 4 4F RT 4A25 1998032600369 19980326 00369 WP 1998 3 26 UPS98826165 1 19980322 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-W/E, EMERGENCY EXIT LIGHTS INOP ON WEEKEND CHECK. REPLACED RECHARGEABLE BATTERY PACK ASSY. 2 L 7 4 4F RT 4A25 1998032600370 19980326 00370 WP 1998 3 26 UPS98826167 1 19980323 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-N/A, FOUND EMERGENCY LIGHT SWITCH IN THE ARMED POSITION WITH NO POWER ON A/C. BATT PACK DEPELETED. REM OVED AND REPLACED EMERGENCY BATT PACK PER MM33-50-01 PG 204, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1998032600371 19980326 00371 EU 1998 3 26 QXEA9800396 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FUSELAGE STRINGER 52 AT FRAME 16060 IS CRACKED AT THE WASHERED RIVET. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED ALODINED AND PRIMED, INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600372 19980326 00372 EU 1998 3 26 QXEA9800397 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FUSELAGE STRINGER 47 AT FRAME 16060 IS CRACKED AT THE WASHERED RIVET. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED ALODINED AND PRIMED, INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600373 19980326 00373 EU 1998 3 26 QXEA9800398 1 19980224 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED AT AFT SIDE OF FRAME 10346 STRINGER 32. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600374 19980326 00374 EU 1998 3 26 QXEA9800399 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FUSELAGE STRINGER 53 AT FRAME 16060 IS CRACKED AT THE WASHERED RIVET. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED ALODINED AND PAINTED, INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600375 19980326 00375 EU 1998 3 26 QXEA9800400 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED FORWARD OF FRAME 15205 AT STRINGER 25. FABRICATED REPAIR IAW FOKKER 53-02-13, FIGURE 2, ETCHED, ALODINE D AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600376 19980326 00376 EU 1998 3 26 QXEA9800401 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED FORWARD OF FRAME 15205 AT STRINGER 21. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALO DINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600377 19980326 00377 EU 1998 3 26 QXEA9800402 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 BETWEEN STRINGERS 28 AND 29. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600378 19980326 00378 EU 1998 3 26 QXEA9800403 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 BETWEEN STRINGERS 36 AND 37. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED ALODINED AND PRIMED. INSTALLED REPAIR AIW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600379 19980326 00379 EU 1998 3 26 QXEA9800404 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 AT LEFTHAND UPPER STUB WING ATTACH POINT. FABRICATED REPAIR IAW FOKKER S RM 53-02-13, FIGURE 2, ETCHED, ALODINED, PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600380 19980326 00380 EU 1998 3 26 QXEA9800405 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 AT LEFTHAND LOWER STUB WING ATTACH POINT. FABRICATED REPAIR IAW FOKKER S RM 53-02-13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600381 19980326 00381 EU 1998 3 26 QXEA9800406 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 BETWEEN STRINGERS 38 AND 39. FABRICATED REPAIR IAW FOKKER SRM 53-02-13 F IGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600382 19980326 00382 EU 1998 3 26 QXEA9800407 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 BETWEEN STRINGERS 58 AND 59. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600383 19980326 00383 EU 1998 3 26 QXEA9800408 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 BETWEEN STRINGERS 56 AND 57. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600384 19980326 00384 EU 1998 3 26 QXEA9800409 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 BETWEEN STRINGERS 54 AND 55. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600385 19980326 00385 EU 1998 3 26 QXEA9800410 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 ON BOTTOM RIGHT STUB WING ATTACH POINT. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600386 19980326 00386 EU 1998 3 26 QXEA9800411 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 ON TOP OF STUB WING ATTACH POINT. FABRICATED REPAIR IAW FOKKER SRM 53-02 -13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600387 19980326 00387 EU 1998 3 26 QXEA9800412 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON FORWARD SIDE OF FRAME 15205 AT STRINGER 50. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETC HED ALODINED AND PRIMED. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600388 19980326 00388 EU 1998 3 26 QXEA9800413 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACKED CLIP AT AFT SIDE OF FRAME 14765 AT STRINGER 25. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600389 19980326 00389 EU 1998 3 26 QXEA9800414 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACKED CLIP AT AFT SIDE OF FRAME 14755 AT STRINGER 39. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600390 19980326 00390 EU 1998 3 26 QXEA9800415 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACKED CLIP AT AFT SIDE OF FRAME 14755 AT STRINGER 56. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600391 19980326 00391 EU 1998 3 26 QXEA9800416 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED ON AFT SIDE OF FRAME 15285 AT STRINGER 36. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, AL ODINED AND PRIMED. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600392 19980326 00392 EU 1998 3 26 QXEA9800417 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED AT AFT SIDE OF FRAME 13815B AT STRINGER 28. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600393 19980326 00393 EU 1998 3 26 QXEA9800418 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED AT AFT SIDE OF FRAME 13815B AT STRINGER 44. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600394 19980326 00394 EU 1998 3 26 QXEA9800419 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED AT AFT SIDE OF FRAME 13815B AT STRINGER 47. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600395 19980326 00395 EU 1998 3 26 QXEA9800420 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED ON AFT SIDE OF FRAME 13815A AT STRINGER 28. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600396 19980326 00396 EU 1998 3 26 QXEA9800421 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON AFT SIDE FRAME 12875 AT STRINGER 37. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, AL ODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600397 19980326 00397 EU 1998 3 26 QXEA9800422 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON AFT SIDE OF FRAME 12875 AT STRINGER 29. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600398 19980326 00398 EU 1998 3 26 QXEA9800423 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK I/B STRINGER 34 FORWARD OF FRAME 13815. FABRICATED REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED IAW FOKKER SRM 51-31-01 AND SRM 53-02-06, FIGURE 6. 2 L 7 2 4F RT A20EU 1998032600399 19980326 00399 EU 1998 3 26 QXEA9800424 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK ON STRINGER 33, FORWARD OF FRAME 13815. FABRICATED REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED REPAIR IAW FOKK ER SRM 51-31-01 AND SRM 53-02-06, FIGURE 6. 2 L 7 2 4F RT A20EU 1998032600400 19980326 00400 EU 1998 3 26 QXEA9800425 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK ON STRINGER 31 FORWARD OF FRAME 13815. FABRICATED REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED REPAIR IAW FOKKE R SRM 51-31-01 AND SRM 53-02-06, FIGURE 6. 2 L 7 2 4F RT A20EU 1998032600401 19980326 00401 EU 1998 3 26 QXEA9800426 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK ON STRINGER 38 FORWARD OF FRAME 13815. FABRICATED, REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED REPAIR IAW FOKK ER SRM 51-31-01 AND SRM 53-02-06, FIGURE 1. 2 L 7 2 4F RT A20EU 1998032600402 19980326 00402 EU 1998 3 26 QXEA9800427 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK ON STRINGER 32 FORWARD OF FRAME 13815B. FABRICATED REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED REPAIR IAW FOKK ER SRM 51-31-01 AND SRM 53-02-06. 2 L 7 2 4F RT A20EU 1998032600403 19980326 00403 EU 1998 3 26 QXEA9800428 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK AFT OF FRAME 13815 ON STRINGER 35. FABRICATED REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED REPAIR IAW FOKKER SR M 51-31-01 AND SRM 53-02-06, FIGURE 6. 2 L 7 2 4F RT A20EU 1998032600404 19980326 00404 EU 1998 3 26 QXEA9800429 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED ON AFT SIDE OF FRAME 13815A AT STRINGER 45. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600405 19980326 00405 EU 1998 3 26 QXEA9800430 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED ON AFT SIDE OF FRAME 13815A AT STRINGER 27. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600406 19980326 00406 EU 1998 3 26 QXEA9800431 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK IN THE CASTELLATION ON FRAME 13815A AND BETWEEN STRINGER 72 AND 73. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600407 19980326 00407 EU 1998 3 26 QXEA9800432 1 19980225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 NICKS AND GOUGES ON LEFTHAND OUTBOARD SEAT TRACK CHANNEL APPROXIMATELY 3.5 IN LENGTH FORWARD OF FRAME 6805. REPLACED DA MAGED SEAT TRACK SECTION PER FOKKER SRM 53-02-15. 2 L 7 2 4F RT A20EU 1998032600408 19980326 00408 EU 1998 3 26 QXEA9800433 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON AFT SIDE OF FRAME 12875 AT STRINGER 46. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2, ETCHED, ALODINED, PRIMED AND INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600409 19980326 00409 EU 1998 3 26 QXEA9800434 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP IS CRACKED ON AFT SIDE OF FRAME 12875 AT STRINGER 45. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, ETCHED, ALODINED, PRIMED AND INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998032600410 19980326 00410 EU 1998 3 26 QXEA9800435 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK IN CASTELLATION BETWEEN STRINGER 1 AND 2 ON FRAME 15205. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600411 19980326 00411 EU 1998 3 26 QXEA9800436 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK AND CORROSION ON FRAME CASTELLATION BETWEEN STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998032600412 19980326 00412 EU 1998 3 26 QXEA9800437 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK IN THE CASTELLATION AT FRAME 13815A BETWEEN STRINGER 2 AND 3. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998032600413 19980326 00413 WP 1998 3 26 MWEA98371 1 19980319 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP CABIN DOOR SLIDE FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 602ME 48133 THE FORWARD ENTRANCE SLIDE POPPED OFF. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1998032600414 19980326 00414 WP 1998 3 26 MWEA98372 1 19980320 A 5210 SKIN DOUG DC9 DC932 3022066 WP CABIN DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FOUND CRACK ON FORWARD PASSENGER DOOR LOWER EDGE AFT CORNER OF OUTER SKIN. MTC INSTALLED INTERNAL DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998032600416 19980326 00416 NM 1998 3 26 DL72S980611 1 19980319 A 3350 1001141 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805EA 22436 AFT AIRSTAIR EMERG LIGHT INOP. REPLACED LIGHT ASSY AND BATTERY PACK. 2 L 7 3 4F A3WE 1998032600417 19980326 00417 NM 1998 3 26 DL76L980614 1 19980317 A 5330 SKIN BOEING 767 767332 1382001 NM BS 89 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 184DN 27111 THE FUSELAGE SKIN AT DOOR STATION 89 AND STRINGER 8L HAS A 1 X 2 CUTOUT. THE SKIN HAS BEEN REPAIRED WITH AN ALUMINUM DO UBLER PER THE GUIDELINES OF B767 SRM 53-00-01. ER/A 364286-14 WAS ISSUED TO DOCUMENT THE REPAIR AND TO ENSURE COMPLIA NCE WITH THE SRM. 2 L 7 2 4F RT A1NM 1998032600418 19980326 00418 NM 1998 3 26 DL72S980616 1 19980320 A 5312 6545975 BULKHEAD FTG BOEING 727 727232 1384082 NM BS 870 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 THE BORE OF FS 870 BLKHD LT TERMINAL FITTING WAS O/S TO 4.605 DIAMETER TO REMOVE TOOLING DAMAGE. REWORKED PER ERA 33151 7-14. 2 L 7 3 4F A3WE 1998032600419 19980326 00419 NM 1998 3 26 DL72S980617 1 19980320 A 5311 6516349127 FRAME BOEING 727 727232 1384082 NM BS 1166 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 SKIN ATTACH FLANGE AT FS 1166 FRAME WAS CORRODED BETWEEN S28 AND 29 ON THE LT SIDE. REPAIR WILL REQUIRE REACOMMPLISHMEN T OF AD92-12-03. REPAIRED PER ERA 331479-14AD. 2 L 7 3 4F A3WE 1998032600420 19980326 00420 NM 1998 3 26 DL76S980618 1 19980316 A 5754 WEDGE BOEING 767 767332 1382001 NM NR 8 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 129DL 24079 THE RT NR 8 SLAT WAS FOUND WITH A 2.5 DIAMETER AREA OF DELAMINATION ON THE UPPER SKIN OF THE TRAILING EDGE WEDGE. THE D AMAGE WAS TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364264-14AD. 2 L 7 2 4F RT A1NM 1998032600421 19980326 00421 NM 1998 3 26 DL72S980620 1 19980320 A 5720 STIFFENER BOEING 727 727232 1384082 NM LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 FOUND ON A1 LETTER CK, 1 INCH CRACK IN LOWER END OF L/E SPAR STIFFENER NR 2 SLAT O/B TRACK, INBD STIFFENER. REPAIRED PE R MM 57-20-21. 2 L 7 3 4F A3WE 1998032600422 19980326 00422 NM 1998 3 26 DL72S980621 1 19980320 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 FOUND ON A1 LETTER CK, NR 8 SLAT LOWER ATTACH ANGLE CRACKED AT THE INBD STOP PAD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998032600423 19980326 00423 NM 1998 3 26 DL72S980622 1 19980320 A 5754 WEB BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 NR 8 SLAT ACT I/B AND O/B ATTACH ANGLE CRACKED AT WEB. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998032600424 19980326 00424 NM 1998 3 26 DL72S980623 1 19980320 A 2782 ANGLE BOEING 727 727232 1384082 NM NR 7 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 NR 7 SLAT ACT O/B ATTACH ANGLE CRACKED AT UPPER LOBE. REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1998032600425 19980326 00425 NM 1998 3 26 DL72K980624 1 19980321 A 2751 POSITION IND 1812993 BOEING 727 727232 1384082 NM TE FLAPS FAILED A DALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SO 27 472DA 2174ANV 20749 TRAILING EDGE DEVICES (OUTBOARD) SPLIT BETWEEN 0 DEG AND 2 DEG. ACCOMPLISHED TRAILING EDGE FLAP ABNORMAL CHECKLIST AND DIVERTED TO JFK. REPLACED OUTBOARD FLAP POSITION IND. 2 L 7 3 4F A3WE 1998032600426 19980326 00426 NM 1998 3 26 DL72S980628 1 19980321 A 3350 276005 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z 21858 717146 RT AFT OVERWING EMERG LIGHT OUT. REPLACED BATTERY IN M956 LOCATION OPN GD. 2 L 7 3 4F A3WE 1998032600427 19980326 00427 NM 1998 3 26 SCNA98025 1 19980315 A 5610 5717623074 SLIDING WINDOW BOEING 727 7272J4 1384006 NM RT COCKPIT CRACKED A SCNA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 284SC 10595 21438 DURING CLIMB, NOTICED R2 WINDOW CRACKED. RETURNED TO STL. REMOVED AND REPLACED R2 WINDOW, FUNCTIONALLY CHECKED GOOD. 2 L 7 3 4F RT A3WE 1998032600428 19980326 00428 1998 3 26 RRXA98071 4 19980319 A 3414 A4144710024 AIRSPEED IND DOUG DC8 DC863F 302198F WP LT COCKPIT MALFUNCTIONED A RRXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 957R 46137 CAPTAINS AIRSPEED IND WENT TO ZERO ON CLIMBOUT. AFTER BEING AIRBORNE FOR 15 MINUTES A/S INDICATOR CAME UP TO 300 KTS AN D REMAINED THERE. DISCONNECTED ALL PITOT LINES FROM CAPT'S AIRSPEED IND, WATER TRAP, AND PITOT TUBE. BLEW OUT PITOT LI NES W/NITROGEN, REPLACED CAPT'S AIRSPEED IND, PITOT DRAIN AND PITOT TUBE. PERFORMED PITOT/STATIC CHECK. OPS AND LEAKS CHECKS GOOD, NO LEAKS NOTED IAW DC-8 MM CHAPT 34. ALL TAPE REMOVED. 2 L 7 4 4F 4A25 1998032600429 19980326 00429 WP 1998 3 26 RRXA98072 1 19980323 A 5730 57583869 SKIN DOUG DC8 DC873F 302199F WP WS 69.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A SCHEDULE INSPECTION, PERFORMED INSPECTION IAW SB 57-88, WINGS - PLATES/SKIN - INSPECT/REPAIR/MODIFY LOWER INBOA RD AFT WING SKIN PANEL. FOUND HOLES 1 AND A BOTTOM AFT LEFT WING SKIN AT STA 69.5 WERE FOUND CRACKED AS INDICATED BY ND T INSPECTION. REPAIRED IAW SB 57-88 AND TIMCO ENGINEERING SKETCH REO-04502. 2 L 7 4 4F RT 4A25 1998032600430 19980326 00430 WP 1998 3 26 ARWA980306 1 19980324 A 3320 BA170MODA BALLAST DOUG DC8 DC863F 302198F WP CABIN FAILED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 441J 45988 SMELL OF ELECTRICAL INSULATION BURNING AFTER LANDING. REMOVED AND REPLACED BALLAST ASSY, OPERATION CHECKED NORMAL IAW M M 33-00-0. 2 L 7 4 4F 4A25 1998032600431 19980326 00431 WP 1998 3 26 ARWA980308 1 19980324 A 5720 57541083 WINGTIP DOUG DC8 DC862 3021970 WP LT WING DAMAGED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 802BN 45909 ON RAMP, WHILE BEING MANSHALLED INTO THE RAMP, THE LEFT WING TIP MADE CONTACT WITH ANOTHER AIRCRAFT. TEMPORARY REPAIR A CCOMPLISHED IAW MM 6 PAR 5-1 TO FLY A/C BACK TO MIAMI. REMOVED AND REPLACED DAMAGED WING TIP IAW SRM 51-30-00. 2 L 7 4 4F 4A25 1998032600432 19980326 00432 NM 1998 3 26 VNAA9803020 1 19980317 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 422JS 42699 876 3018 THE EMERGENCY LIGHTS AT ROWS FIVE AND SIX FAILED TO OPERATE, DURING PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND RE PLACED THE EMERGENCY BATTERY AT POSITION 5LK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATION CHECKS WERE COMPLIED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998032600433 19980326 00433 NE 1998 3 26 TC8A98015 2 19980324 A 7230 COMPRESSOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 181SK 45910 669217 NR 2 ENGINE COMPRESSOR STALL ON TAKEOFF ROLL, ENGINE ANTI-ICE WAS ON, TEMP 0 CELCIUS. PERFORMED VISUAL INSPECTION OF EN GINE INLET AND EXHAUST, INSPECTED INTERSTAGE BLEED VALVE, NO DEFECTED NOTED. PERFORMED ENGINE RUN-UP WITH ANTI-ICE ON A ND BLEED AIR ON AT MAX T/O POWER, NO DEFECTED NOTED IAW TCA MIP VOL II. 2 L 7 4 4F 4 F 4A25 1E8 1998032600447 19980326 00447 NM 1998 3 26 CALA9800544 1 19980319 A 5230 SKIN BOEING 727 727227 1384078 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND C-2 CARGO DOOR AFT LOWER EDGE BENT AND CORRODED. THE AFT LOWER FRAME SECTION WAS REMOVED IAW SRM 51-30 -2 AND THE SKIN WAS STRAIGHTENED IAW SRM 51-40-1. THE NEW LOWER AFT FRAME SECTION WAS SEALED AND INSTALLED IAW SRM 51-1 0-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998032600448 19980326 00448 NM 1998 3 26 CALA9800545 1 19980319 A 5230 SKIN BOEING 727 727227 1384078 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .5 INCH CRACK WITH DENT IN AFT BAGGAGE COMPARTMENT DOOR SKIN 23 DOWN FROM TOP AND 16 AFT. THE DENTED AND CRACKED AREA WAS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-3. 2 L 7 3 4F A3WE 1998032600449 19980326 00449 NM 1998 3 26 CALA9800546 1 19980319 A 5312 BULKHEAD PANEL BOEING 727 727227 1384078 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND THE NLG WHEEL WELL FORWARD BULKHEAD TOP RIGHT PANEL, TOP LEFT PANEL, AND TOP CENTER PANELS CRACKED AT F ASTENER HOLES. THE CRACKS WERE .5 TO 1 IN LENGTH. THE CRACKED AREAS WERE CUTOUT IAW SRM 51-40-2. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 53-10-2. 2 L 7 3 4F A3WE 1998032600450 19980326 00450 NM 1998 3 26 CALA9800547 1 19980319 A 5532 SKIN BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 3 INCH CRACK IN LT VERTICAL STABILIZER AT STA 1253, JUST ABOVE AND AFT OF PANEL NR 9523. THREE 1 INC H CRACKS WERE FOUND IN THE LT VERTICAL STABILIZER AT STA 1264. THE CRACKED AREAS WERE CUTOUT IAW SRM 54-10-1. FILLER A ND DOUBLER REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 54-10-3, 53-30-3, 51-10-2, AND 51-30-1. 2 L 7 3 4F A3WE 1998032600451 19980326 00451 NM 1998 3 26 CALA9800548 1 19980319 A 5531 RIB BOEING 727 727227 1384078 NM VERT STAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND VERTICAL STABILIZER NR 7 RIB WORN AT STRINGER 2R. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55-30 -4, 51-10-6, AND 51-30-2. 2 L 7 3 4F A3WE 1998032600452 19980326 00452 NM 1998 3 26 CALA9800549 1 19980319 A 5531 RIB BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER NR 6 RIB AT STRINGER 3L. THE CRACK WAS STOP DRILLED, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-30-4, 51-10-6, AND 51-30-2. 2 L 7 3 4F A3WE 1998032600453 19980326 00453 NM 1998 3 26 CALA9800550 1 19980319 A 5753 FLAP TRACK BOEING 727 727227 1384078 NM RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND RT WING NR 7 FLAP TRACK FORWARD LUGS CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0. 2 L 7 3 4F A3WE 1998032600454 19980326 00454 NM 1998 3 26 CALA9800551 1 19980320 A 5753 SKIN BOEING 727 727227 1384078 NM RT TE FOREFLAP PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A HOLE IN RT OUTBOARD FOREFLAP UPPER INBOARD SURFACE. THE DAMAGED AREA WAS CUTOUT AND A HOT BONDED REP AIR WAS APPLIED IAW SRM 51-40-6 AND 51-10-6. 2 L 7 3 4F A3WE 1998032600455 19980326 00455 NM 1998 3 26 CALA9800552 1 19980320 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND FLOORBEAM TOP FLANGE UPPER AND LOWER SURFACE CORRODED AT FS 360, RBL 10 TO LBL 10. THE CORRODED AREA W AS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2. 2 L 7 3 4F A3WE 1998032600456 19980326 00456 NM 1998 3 26 CALA9800553 1 19980320 A 5720 ANGLE BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 3 INCH CRACK IN LT WING UPPER TRAILING EDGE PANEL SUPPORT T-ANGLE. THE CRACK WAS LOCATED AT INBOARD AFT END, OUTBOARD OF NR 1 FLAP JACKSCREW. THE T-ANGLE WAS REMOVED AND A NEW T-ANGLE WAS FABRICATED AND INSTALLED IAW SR M 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1998032600457 19980326 00457 NM 1998 3 26 CALA9800554 1 19980320 A 5752 SKIN BOEING 727 727227 1384078 NM RT AILERON TAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND RT OUTBOARD AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1998032600458 19980326 00458 NM 1998 3 26 CALA9800555 1 19980320 A 5754 RIB BOEING 727 727227 1384078 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH CRACK IN NR 2 LEADING EDGE SLAT FIRST RIB INBOARD OF ACTUATOR AT WS 629. A FORMED ANGLE REPAI R WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-0. 2 L 7 3 4F A3WE 1998032600459 19980326 00459 NM 1998 3 26 CALA9800556 1 19980320 A 5720 STIFFENER BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .625 INCH CRACK IN STIFFENER AT BOTTOM OF LT WING LEADING EDGE RIB, WBL 92.0. THE CRACK WAS STOP DRI LLED IAW SRM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998032600460 19980326 00460 NM 1998 3 26 CALA9800557 1 19980320 A 5720 ANGLE BOEING 727 727227 1384078 NM BS 120 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND TWO 1 INCH CRACKS AT BOLT HOLES OF LT WING LOWER LEADING EDGE SUPPORT ANGLE AT FS 120. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998032600461 19980326 00461 NM 1998 3 26 CALA9800558 1 19980320 A 5744 ATTACH FITTING BOEING 727 727227 1384078 NM RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING AT BOTTOM OF WING CORRODED AT INBOARD FACE. THE FITTING WAS REMOVED AND REPLACED IAW OVERHAUL MANUAL 20-50-01. 2 L 7 3 4F A3WE 1998032600462 19980326 00462 NM 1998 3 26 CALA9800559 1 19980320 A 5753 FLAP TRACK BOEING 727 727227 1384078 NM NR 6 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND UPPER MOUNT FLANGE OF NR 6 FLAP TRACK CORRODED AT FORWARD ATTACH CLEVIS. THE FLAP TRACK WAS REMOVED AN D REPLACED. 2 L 7 3 4F A3WE 1998032600463 19980326 00463 NM 1998 3 26 CALA9800560 1 19980320 A 5720 ANGLE BOEING 727 727227 1384078 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .5 INCH CRACK IN J-ANGLE SUPPORT ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. A REPAIR CHANNEL WAS FA BRICATED AND INSTALLED IAW ECRA 5750-02914. 2 L 7 3 4F A3WE 1998032600464 19980326 00464 NM 1998 3 26 CALA9800561 1 19980320 A 5720 ANGLE BOEING 727 727227 1384078 NM LT WINGTIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1.25 INCH CRACK IN LT WINGTIP SUPPORT ANGLE AT INBOARD END OF CLOSURE RIB. A DOUBLER WAS INSTALLED I AW SRM 51-30-02. 2 L 7 3 4F A3WE 1998032600465 19980326 00465 NM 1998 3 26 CALA9800562 1 19980320 A 5240 SKIN BOEING 727 727227 1384078 NM R1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .625 INCH CRACK THROUGH FASTENER AT R-1 DOOR OUTER SKIN LOWER FORWARD CORNER ABOVE GATE. A REPAIR DO UBLER WAS FABRICATED AND INSTALLED IAW SRM 52-40-1. 2 L 7 3 4F A3WE 1998032600466 19980326 00466 NM 1998 3 26 CALA9800563 1 19980320 A 5543 SKIN BOEING 727 727227 1384078 NM RUDDER TAB DETERIORATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND LT LOWER SIDE OF UPPER RUDDER TAB FIBERGLASS REPAIR DETERIORATED. THE FIBERGLASS REPAIR WAS SANDED, RE WORKED, AND PRIMED IAW SRM 51-40-9 AND 51-10-6. 2 L 7 3 4F A3WE 1998032600467 19980326 00467 NM 1998 3 26 CALA9800564 1 19980320 A 5532 SKIN BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A .1875 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER LOWER SECTION AT STA 1343. A REPAIR WAS INSTALLED IAW ECRA 5530-01075. 2 L 7 3 4F A3WE 1998032600468 19980326 00468 NM 1998 3 26 CALA9800565 1 19980320 A 5542 SKIN BOEING 727 727227 1384078 NM RUDDER ERODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND RT SIDE OF LOWER RUDDER SKIN EDGE ERODED JUST ABOVE PANEL NR 9901. THE AREA WAS SANDED AND A FIBERGLAS S OVERLAY WAS APPLIED IAW SRM 51-40-8. 2 L 7 3 4F A3WE 1998032600469 19980326 00469 NM 1998 3 26 CALA9800566 1 19980320 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH CRACK IN RT WING STA 656.50 STRINGER ON TOP OF CHORD RIB. THE CRACK WAS STOP DRILLED, A REPAI R WAS INSTALLED IAW EA 5762-01050. 2 L 7 3 4F A3WE 1998032600470 19980326 00470 NM 1998 3 26 CALA9800567 1 19980320 A 5311 CIRCUMFERENTIAL BOEING 727 727227 1384078 NM BS 804.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH CRACK IN CIRCUMFERENTIAL AT BS 804.5, S15R. THE CRACKED AREA WAS REMOVED, A REPAIR ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-3. 2 L 7 3 4F A3WE 1998032600471 19980326 00471 NM 1998 3 26 CALA9800568 1 19980320 A 5320 CHORD BOEING 727 727227 1384078 NM BS 310-362 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND TOP AND BOTTOM OF CHORD CORRODED AT FS 310 TO 362, LBL 56. ALSO, DOUBLER AT FS 360 HAD A .5 INCH CRACK . THE CHORD WAS REMOVED, CORROSION WAS REMOVED FROM AREA IAW SRM 51-10-6. A NEW DOUBLER AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998032600472 19980326 00472 NM 1998 3 26 CALA9800569 1 19980320 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND TOP FLANGE UPPER AND LOWER SURFACE OF FLOORBEAM CORRODED AT FS 360, RBL 10 TO LBL 18. THE CORRODED ARE A WAS CUT OUT, A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2. 2 L 7 3 4F A3WE 1998032600473 19980326 00473 NM 1998 3 26 CALA9800570 1 19980320 A 5753 FLAP TRACK BOEING 727 727227 1384078 NM TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND NR 7 FLAP TRACK AFT MOUNT CORRODED. THE FLAP TRACK WAS REPLACED IAW MM 27-51-0. 2 L 7 3 4F A3WE 1998032600474 19980326 00474 WP 1998 3 26 CALA9800571 1 19980322 A 8011 38334211 STARTER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE FAILED A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 16813 40732 48066 708479 THE A START VALVE LIGHT ILLUMINATED AFTER TAKEOFF FROM CLE. THE LIGHT EXTINGUISHED AFTER ABOUT 30 SECONDS. ENGINE POWE R WAS BEING REDUCED, CROSSFEED WAS CLOSED, AND HP BLEED WAS ON HIGH. THE FLIGHT LANDED AT EWR WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NR 1 ENGINE STARTER FAILED. THE STARTER AND STARTER VALVE WERE REMOVED AND REPLACED. THE VENDOR WAS UNABLE TO DETERMINE CAUSE OF FAILURE. THE STARTER WAS FOUND BEYOND ECONOMICAL REPAIR. THE VENDOR FOUND NO TROUBLE WITH THE STARTER SHUTOFF VALVE. IT WAS NOTED, HOWEVER, THAT THE VALVE HAD BEEN IDENTIFIED AS A CHRONIC UNIT. 2 L 7 2 4F 4 F A6WE E9NE 1998032600475 19980326 00475 NM 1998 3 26 CALA9800572 1 19980320 A 5753 6521630266 SKIN BOEING 727 727227 1384078 NM RT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND A 1 INCH GOUGE IN RT INBOARD FOREFLAP OUTBORD LEADING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1998032600476 19980326 00476 SO 1998 3 26 COMA9810072 1 19980323 A 2613 M1160140242 SENSOR EMB 120 EMB120RT SO CENTER WING MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 249CA 120230 BLEED AIR DUCT LEAK WARNING. REPLACED DEFECTIVE OVER TEMP SENSOR AT WING CENTER SECTION. 2 L 7 2 4T RT A31SO 1998032600477 19980326 00477 SO 1998 3 26 COMA9810073 1 19980323 A 5753 KRP138112VT ROLLERS EMB 120 EMB120RT SO TE FLAPS WORN A COMA L ABORTED APPROACH O OTHER AP APPROACH 1 SO 01 152CA 120152 FLAP CONTROL FAULT WHEN FLAPS SELECTED FOR LANDING APPROACH. REPLACED THE RIGHT HAND INBOARD FLAP ROLLERS. 2 L 7 2 4T RT A31SO 1998032600478 19980326 00478 EA 1998 3 26 COMA9860066 1 19980323 A 5210 LINKAGE CNDAIR CL600 CL6002B19 EA CABIN DOOR OUT OF ADJUST A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 949CA 7080 CABIN DOOR OUTER HANDLE WARNING MESSAGE. ADJUSTED DOOR HANDLE LINKAGE. 2 L 7 2 4F RT A21EA 1998032600479 19980326 00479 NM 1998 3 26 UPS98226168 1 19980320 A 5320 651633511 ANGLE BOEING 727 72725C 138400H NM BS 915 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C, CORROSION ON ANGLE AT BS 915 RBL 60 WL 190. REMOVED AND REPLACED ANGLE IAW SRM 51-30-05, 51-30-02. 2 L 7 3 4F A3WE 1998032600480 19980326 00480 NM 1998 3 26 UPS98226169 1 19980319 A 5320 BRACKET BOEING 727 727247 138408F NM BS 720 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-SI, CORROSION (C53-224-01.00-01) ON FRAME AND BRACKET AT BS 720C STR 7 LT FRAME WITHIN LIMITS, BRACKET O UT OF LIMITS. REMOVED CORROSION ON FRAME, FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-20-1, 51-10-6, 51-10-02, 51-3 0-2. 2 L 7 3 4F A3WE 1998032600481 19980326 00481 NM 1998 3 26 UPS98226170 1 19980323 A 5741 BOTTLE PIN BOEING 727 727247 138408F NM RT WING/FUS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-SI, RT WING AFT BOTTLE PIN CORRODED. REPLACED BOTTLE PIN PER 727 MM 57-41-01. 2 L 7 3 4F A3WE 1998032600482 19980326 00482 WP 1998 3 26 UPS98826172 1 19980324 A 5330 SKIN DOUG DC8 DC871F 302199D WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-N/A, FOUND SKIN BULGED AND CRACKED 2 INCHES FWD OF NR 4 PIT DOOR LOWER FWD CORNER DOUBLER. ALSO, BULGE IN SKIN WITH RIVET PULLED THROUGH AFT CORNER NR 4 PIT DOOR SCUF GAURD AREAS MARKED. NR OPENED AGAINST THIS ITEM. COMPL ETED NON ROUTINE 725601, INSTALLED NEW SKIN AS PER EO DC8-5330-10049A. 2 L 7 4 4F RT 4A25 1998032600483 19980326 00483 EU 1998 3 26 WWMA9800059 1 19980322 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST IN INSP/MAINT 1 WP 15 234AE 340B234 CABIN EMERGENCY LIGHTS FAIL TO STAY ON. REPLACED EMERGENCY BATTERY POWER PACK 20LN. 2 L 7 2 4T RT A52EU 1998032600484 19980326 00484 EU 1998 3 26 WWMA9800058 1 19980319 A 2730 6432331 SWITCH SAAB SF340 340B 7860101 EU RT COCKPIT DEFECTIVE A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 15 280AE 340B280 FIRST OFFICERS YOKE STARTED SMOKING FROM THE VERTICAL SYNC SWITCH. MAINTENANCE REPLACED THE FIRST OFFICERS VERTICAL SWI TCH. 2 L 7 2 4T RT A52EU 1998032600485 19980326 00485 WP 1998 3 26 CKSA98202 1 19980321 A 2612 FIRE WARNING DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE ILLUMINATED A CKSA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 GL 23 781AL 45926 671428 TEN MINUTES AFTER TAKEOFF, NR 2 ENGINE FIRE WARNING ILLUMINATED, SHUTDOWN ENGINE ACCOMPLISHED CHECKLIST. BOTH BOTTLES E XTINGUISHED. PERFORMED NR 2 ENGINE INSPECTION, NO DEFECTS NOTED AND RAN ENGINE FOR 30 MINUTES, 5 AT MAX POWER. OPS CHE CK NORMAL IAW MM 72-0. 2 L 7 4 4F 4 F 4A25 1E8 1998032600486 19980326 00486 WP 1998 3 26 CKSA98203 1 19980323 A 3297 WIRE DOUG DC8 DC861 3021952 WP RT MLG DOOR SW SHORTED A CKSA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 812CK 45890 RT GEAR DOOR UNSAFE LIGHT ON IN CRUISE INTERMITTENTLY. REPAIRED SHORTED WIRE ON GEAR DOOR SWITCH SYSTEM, OPS CHECKS GOO D IAW DC8 MM 32-60-0. 2 L 7 4 4F 4A25 1998032600567 19980326 00567 NM 1998 3 26 RAAA98B2017 1 19980319 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 2 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998032600568 19980326 00568 NM 1998 3 26 RAAA98B2018 1 19980319 A 3350 873100212 SIGN BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FWD LT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 3 4F A3WE 1998032600569 19980326 00569 NM 1998 3 26 RAAA98B2019 1 19980319 A 3350 873100112 LIGHT BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 14 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 3 4F A3WE 1998032600570 19980326 00570 WP 1998 3 26 9804821227 1 19980321 A 3397 WIRE DOUG DC10 DC1030 3023501 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 227NW 46969 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 22 TO 30 OUTBOARD SIDE. FOUND BROKEN WIRE AT PASSENG ER SEAT 30A. SECURED WIRE, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998032600571 19980326 00571 NE 1998 3 26 9804836718 2 19980320 A 7261 678960 BREATHER TUBE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE CRACKED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 618US 21122 689565 WHILE IN CRUISE, THE NR 1 ENGINE OIL QUANTITY WENT TO ZERO WITH THE OIL PRESSURE DROPPING RAPIDLY DOWN TO 8 TO 9 PSI. T HE ENGINE WAS SHUT DOWN PER COM PROCEDURE AND THE AIRCRAFT RETURNED TO ANC WITHOUT DIFFICULTY. MAINTENANCE INSPECTED TH E ENGINE AND REPLACED THE REAR MAIN BEARING BREATHER TUBE DUE TO A CRACK. THE FOLLOW-UP LEAK CHECK AND ENGINE WINDMILL CHECK WERE NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1998032600572 19980326 00572 NE 1998 3 26 9804841143 2 19980320 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 FAILED A NWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 133JC 46752 686128 APPROXIMATELY 30 MINUTES AFTER TAKEOFF, THE NR 1 ENGINE OIL CLOG LIGHT ILLUMINATED. THE CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE ENGINE. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO MSP WITHOUT DIFFICULTY. MAINTENANCE INSPECTED THE ENGINE AND THE AIRCRAFT WAS REMOVED FROM SERVICE TO CHANGE THE NR 1 ENGINE. 2 L 7 3 4F 4 F A22WE E20EA 1998032600574 19980326 00574 NM 1998 3 26 9804866740 1 19980225 A 7711 CONNECTORS BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 1 EPR DIRTY A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 640US 23888 662539 DURING TAKEOFF ROLL, THE NR 1 ENGINE WOULD NOT REACH TAKEOFF EPR WITHOUT EXCEEDING THE EGT REDLINE. THE MAXIMUM EPR REA CHED WAS 1.30. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CLEANED THE EPR TRANSMITTER AND INDICATOR CONNECTIONS AND PERFORMED AN ENGINE BLEED CHECK PER MM 75-32-00 WITH NO DEFECTS NOTED. 2 L 7 4 4F 4 F A20WE E20EA 1998032600576 19980326 00576 WP 1998 3 26 9804889152 1 19980324 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 FLIGHT ATTENDANT REPORTED, EMERGENCY FLASHLIGHT AT ENTRY DOOR 1L INOPERATIVE. MAINTENANCE REPLACED BATTERY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998032600577 19980326 00577 WP 1998 3 26 9804899152 1 19980323 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8911E 45825 DURING LINE CHECK, FOUND LEFT NACELLE EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998032600578 19980326 00578 WP 1998 3 26 9804909856 1 19980322 A 3231 LATCH DOUG DC9 DC951 3022051 WP LT MLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 765NC 47718 DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR UNSAFE AND DOOR OPEN LIGHTS ILLUMINATED. FLIGHT CREW FOLLOWED COM PROCEDURE S, RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT MAIN LANDING GEAR DOOR LATCH MECHANISM, O PERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998032600579 19980326 00579 NM 1998 3 26 9804915531 1 19980321 A 2750 RELAY BOEING 757 757251 1384970 NM TE FLAPS FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 01 531US 23846 ON APPROACH, THE TRAILING EDGE FLAPS FAILED TO EXTEND AND THE TRAILING EDGE FLAPS DISAGREE WARNING LIGHT ILLUMINATED. T HE FLIGHT DIVERTED TO DEN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAY K10104 WITH A NEW PART, OPERATIONAL T EST WAS SATISFACTORY. 2 L 7 2 4F RT A2NM 1998032600580 19980326 00580 WP 1998 3 26 9804929968 1 19980322 A 3260 SENSOR DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 9332 47264 DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CAPTAIN DECLARED AN EMERGENCY AND VER IFIED THROUGH PEEP HOLE THAT THE GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR PROXIMITY SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600581 19980326 00581 WP 1998 3 26 9804939993 1 19980323 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 8986E 47402 FLIGHT ATTENDANT REPORTED AFT FLASHLIGHT INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600582 19980326 00582 1998 3 26 9804949931 4 19980324 A 2565 113317 BATTERY DOUG DC9 DC931 3022065 WP PAX DOOR SLIDE DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 90S 40271 3477 47244 DURING PERIODIC CHECK, MAIN CABIN DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998032600583 19980326 00583 WP 1998 3 26 9804959936 1 19980324 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1799U 47370 LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998032600584 19980326 00584 1998 3 26 98FDEA00217 4 19980324 A 3418 30416923 STALL COMPUTER BOEING 727 72725 1384006 NM E/E COMPT FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 152FE 18285 ON ROTATION, STICK SHAKER ENABLE AND REMAINED ON THROUGHOUT FLIGHT. RETURNED TO BASE. TROUBLESHOT SYSTEM FOUND STALL C OMPUTER FAULTED. REMOVED AND REPLACED STALL COMPUTER SYSTEM, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1998032600585 19980326 00585 NM 1998 3 26 DL72W980629 1 19980322 A 3350 P2070003001 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 291WA 22109 FWD FLASHLIGHT INOP. REPLACED FLASHLIGHT ASSY. 2 L 7 3 4F A3WE 1998032600586 19980326 00586 NM 1998 3 26 DL75A980630 1 19980322 A 3350 P2070003001 LIGHT BOEING 757 757212 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 751AT 23125 FLASHLIGHT AT FWD INBD F/A JUMPSEAT USED. FOUND FLASHLIGHT BACKWARD IN HOLDER, BATTERY DEAD. INSTALLED NEW FLASHLIGHT ASSY. 2 L 7 2 4F RT A2NM 1998032600587 19980326 00587 WP 1998 3 26 DLL10980632 1 19980322 A 3350 LIGHT P20700042 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718DA 193C1097 LOWER GALLEY LEFT SIDE EMERGENCY FLASHLIGHT INOP. FOUND MAGNET MISSING FROM HOLDER CAUSING LIGHT TO REMAIN ON WHEN STOW ED. REPLACED HOLDER AND BATTERY. 2 L 7 3 4F A23WE 1998032600588 19980326 00588 WP 1998 3 26 DLL10980634 1 19980323 A 2840 724400171 MAGNA STICK LKHEED 1011 10113851 5265010 WP RT WING INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 733DS 193C1224 IN FLT HAD 2 RT BOOST PUMPS 1/2 LOW PRESS LIGHTS ON WITH CORRESPONDING LOW QTY LEVEL LIGHT. FLT DIVERTED INTO BHM FOR A DDITIONAL FUEL. DURING FUELING FOUND NR 1 MAGNA STICK READING FULL WITH EMPTY TANK. DEFUELED TANK AND METERED IN KNOW N QTY, FUEL QTY SYS OPN NORMAL. FWD NR 1 MAGNA STICK ON RT WING TO MCO AND PLACARD. 2 L 7 3 4F A23WE 1998032600589 19980326 00589 NM 1998 3 26 DL72E980637 1 19980225 A 5753 652163395A RIB BOEING 727 727247 138408F NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 14764 DURING SHOP VISIT, THE FLAP WAS FOUND WITH A CRACKED RIB AT THE LOWER AFT CORNER. THE RIB WAS REPAIRED PER 727 MM 57-52 -0 FIG 808 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998032600590 19980326 00590 NM 1998 3 26 DL72W980638 1 19980323 A 3350 1102833 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2817W 20873 ON LAYOVER 2 CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY LIGHT INOP. RELAMPED, NO HELP. REPLACED BATTERIES, NO HELP. RE PLACED LIGHT ASSEMBLY AND INSTALLED NEW BATTERIES, OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F A3WE 1998032600591 19980326 00591 NM 1998 3 26 DL72S980640 1 19980318 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 WEB CRACKED VERT STAB INTERIOR, VERTICAL WEB OVER S-DUCT IS CRACKED AT BOTH LOWER CORNERS (2 PLACES). REMOVED FASTENERS DYE PEN'D STOP DRILL, NO CRACK NOTED AFTER STOP DRILL HOLES ON BOTH SIDES, FABRICATED NEW DOUBLERS AS PER SRM 53-10-4 F IG 17. INSTALLED DOUBLER AND SHIM ON LT SIDE OF WEB. INSTALLED RT SIDE DOUBLER AS PER SRM 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1998032600592 19980326 00592 NM 1998 3 26 DL72K980641 1 19980324 A 5320 65562313 STRAP BOEING 727 727232 1384082 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 412DA 21232 A CRACK WAS FOUND IN THE BEAR STRAP AT THE R1 DOOR CUTOUT. THE CRACK WAS LOCATED IN THE FWD, LWR CORNER OF THE CUTOUT A ND PROPAGATED FROM THE EDGE OF THE PART DOWNWARD APPROX 1 INCH. REPAIRED PER ERA 331529-14. 2 L 7 3 4F A3WE 1998032600593 19980326 00593 NM 1998 3 26 DLM88980642 1 19980324 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 988DL 53339 FS 1418 FRAME WAS FOUND CRACKED AT L2L AND L2R. CRACKS WERE BOTH 1 INCH IN LENGTH. REPAIRED PER ERA 331500-14. 2 L 7 2 4F RT A6WE 1998032600594 19980326 00594 NM 1998 3 26 DLM88980643 1 19980324 A 5330 593600731 SKIN DOUG MD88 MD88 3023688 NM BS 1325 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 988DL 53339 FUSELAGE SKIN WAS FOUND DENTED AND GOUGED FROM FS 1309 TO FS 1338 AT L23R. REPAIRED PER ERA 331520-14. 2 L 7 2 4F RT A6WE 1998032600595 19980326 00595 SO 1998 3 26 SWIA971098 1 19980309 A 3230 CONTROL VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 198SW 120227 RIGHT MAIN LANDING GEAR WOULD NOT RETRACT. RETURNED TO FIELD. REPLACED LANDING GEAR CONTROL VALVE, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998032600596 19980326 00596 EA 1998 3 26 SWIA971099 1 19980301 A 5270 SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE CARGO DOOR DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 403SW 7028 DEPARTING SLC AND OUT OF ABOUT 1500 AGL, THE AMBER CARGO DOOR MESSAGE CAME ON. RETURNED TO SLC. CLEANED AND LUBED THE CARGO DOOR HANDLE MICROSWITCH, OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1998032600597 19980326 00597 SO 1998 3 26 SWIA971100 1 19980309 A 2460 FUSE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE EMERGENCY BUS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 AFTER DEPARTURE, NR 2 EHSI AND ADI FAILED WOULD NOT RESET. RETURNED TO LAX. INSTALLED NEW AGC10 FUSE FOR EMERGENCY BUS . TWO GROUND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998032600598 19980326 00598 SO 1998 3 26 SWIA971101 1 19980309 A 3230 RELAY BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 GEAR WOULD NOT RETRACT NORMALLY HAD TO USE DOWN LOCK RELEASE. AURAL WARNING KEPT GOING OFF CONTINUALLY FLAPS, TRIM, AUT O FEATHER. REMOVED AND REPLACED LANDING GEAR RELAY BOX, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998032600599 19980326 00599 SO 1998 3 26 SWIA971102 1 19980309 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 189SW 120048 ON CLIMBOUT, AURAL WARNING FLAPS, TRIM, AUTO FEATHER CAME ON. RETURNED TO SAN. CHANGED NOSE GEAR PROXIMITY SENSOR FOR AIR GROUND, NO AURAL WARNINGS NOTED. ABLE TO DUPLICATE THOSE AURAL WARNINGS BY JACKING NOSE STRUT TO SIMULATE A BAD PRO XIMITY SENSOR, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998032600601 19980326 00601 NM 1998 3 26 VNAA9803023 1 19980322 A 5610 17300010 WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT FLIGHT DECK CRACKED A VNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 07 440JS 21293 3058 THE RIGHT HAND FLIGHT DECK SIDE WINDOW, CRACKED DURING THE FLIGHT INBOUND TO CHS. THE AIRCRAFT DIVERTED TO ROA AND LAND ED WITHOUT ANY FURTHER INCIDENTS. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO CAK. THE FLIGHT WAS COMPLETED WITHOUT ANY PROBLEMS. CAK MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND SIDE WINDOW IN A CCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-12-00. OPERATION AND PRESSURIZATION CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998032600604 19980326 00604 NE 1998 3 26 98ZZZX1163 1 19980305 A 2913 7665009808102 PUMP ABEX SKRSKY S76 S76C 8143008 NE NR 1 HYD FAILED A HEEA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 03 476X 2387 K0041 760436 LOST NR 1 HYDRAULIC SYSTEM PRESSURE IN-FLIGHT. LANDED ON OFFSHORE PLATFORM WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAUL IC PUMP FAILURE (INTERNAL METAL CONTAMINATION). REF: S-76 IPC, CHAPTER 29-20-01, FIG 1, ITEM 11. 1 G 7 2 3U NC H1NE 1998032600613 19980326 00613 CE 1998 3 26 98ZZZX1171 1 19980201 A 2721 AN3166R NUT BEECH 99 99A 1154003 CE RUD TAB ACTUATOR CORRODED A S TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 955AA 28112 UI28 RUDDER TAB ACTUATOR NUT FOUND CORRODED DURING ROUTINE INSPECTION. 1 L 7 2 3T A14CE 1998032600624 19980326 00624 SW 1998 3 26 HEEA0013350 1 19980317 A 2435 206062200113 STARTER BELL 407 407 SW ENG START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 403PH 527 53177 STARTER TURNED SLOWLY AND CHATTERED. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND ALL FOUR BOTTOM BRUSHES BROKEN AND L EADS SEPARATED FROM BRUSHES AND COMMUTATOR WAS EXCESSIVELY PITTED. OVERHAULED STARTER GENERATOR AND RETURNED TO SERVICE . 1 G 7 1 3U O H2SW 1998032600625 19980326 00625 EU 1998 3 26 HEEA0013351 1 19980317 A 7714 32005008 TACH-GENERATOR BOLKMS 105 BO105S 5626006 EU ENGINE MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E S806 FROM STOCK, INSTALLED IN AIRCRAFT DURING GROUND RUN, HAD NO NEEDLE INDICATION ON TRIPLE TACH INDICATOR. INSPECTED AND TE STED BY ACCESSORY OVERHAUL SHOP AND COULD NOT FIND ANY PROBLEM WITH TACH GENERATOR, IT TESTED OK AND WAS RETURNED TO SER VICE. 1 G 7 2 3U H3EU 1998032600626 19980326 00626 EU 1998 3 26 HEEA0013352 1 19980317 A 6330 704A33633151 BEARING SNIAS 350 AS350B 8680801 EU TRANSMISSION DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 TRANSMISSION BEARING OIL SOAKED. 1 G 7 1 3U H9EU 1998032600628 19980326 00628 EU 1998 3 26 HEEA0013354 1 19980317 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B 8680801 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 247 2771 STROBE POWER SUPPLY INOPERATIVE. 1 G 7 1 3U H9EU 1998032600629 19980326 00629 EU 1998 3 26 HEEA0013355 1 19980317 A 6330 704A3363310951 SPHERICAL STOP SNIAS 350 AS350B2 8680813 EU TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1814 2820 SPHERICAL STOP ASSY WORN. SERIAL NUMBERS REMOVED ARE 10952, 10948, AND 10956. 1 G 7 1 3U H9EU 1998032600630 19980326 00630 SW 1998 3 26 HEEA0013356 1 19980317 A 3310 900044 LIGHT ASSY BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 510PH 53209 LIGHT STAYS ON. 1 G 7 1 3U O H2SW 1998032600631 19980326 00631 EU 1998 3 26 HEEA0013357 1 19980317 A 6210 355A11002012 BLADE SNIAS 350 AS350B2 8680813 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 3611 2820 M/R BLADE CRACKED. 1 G 7 1 3U H9EU 1998032600632 19980326 00632 SW 1998 3 26 HEEA0013358 1 19980317 A 6320 214040806003 PRESSURE SWITCH BELL 407 407 SW TRANSMISSION FAILED E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 510PH 77 53209 TRANS. PRESS CAUTION LIGHT WILL NOT ILLUMINATE. 1 G 7 1 3U O H2SW 1998032600633 19980326 00633 EU 1998 3 26 HEEA0013359 1 19980317 A 6410 704A33633091 BEARING 355A12004005 SNIAS 350 AS350B 8680801 EU T/R BLADE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 1233 6464 2771 LAMINATED BEARINGS SEPARATED. 1 G 7 1 3U H9EU 1998032600634 19980326 00634 1998 3 26 HEEA0013361 4 19980318 A 3442 MI5852013 INDICATOR P40001 BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 THE CONTRAST IS NOT BRIGHT ENOUGH TO READ THE SCREEN. THERE IS ONLY ONE COLOR. VERIFIED, FOUND INTENSITY KNOB TURNED DO WN, ALSO FOUND YELLOW DISPLAY PROBLEM ON MEMORY BOARD. REPLACED IC15, U1011, U1017, U1015, U1014, U1008, U1009. REPAIR ED. BENCH CHECK GOOD. 1 G 7 1 4U H4SW 1998032600635 19980326 00635 SW 1998 3 26 HEEA0013362 1 19980318 A 2841 393008047 INDICATOR BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 GAUGE DROPS TO ZERO OR DOWN 1000 POUNDS FROM TIME TO TIME. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U H4SW 1998032600636 19980326 00636 SW 1998 3 26 HEEA0013363 1 19980318 A 6400 222312712001 BEARING BELL 230 230 1182149 SW T/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 BEARING WORN AND DAMAGED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600637 19980326 00637 SW 1998 3 26 HEEA0013364 1 19980318 A 6400 222312751001 BEARING 222012711107 BELL 230 230 1182149 SW T/R CNTR WT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN NA 23009 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600638 19980326 00638 SW 1998 3 26 HEEA0013365 1 19980318 A 6710 212010782101 BEARING 222382001105 BELL 230 230 1182149 SW M/R CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 0118A 23009 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600639 19980326 00639 SW 1998 3 26 HEEA0013366 1 19980318 A 6710 212010782101 BEARING 222382001105 BELL 230 230 1182149 SW M/R CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 0100A 23009 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600640 19980326 00640 SW 1998 3 26 HEEA0013367 1 19980318 A 6710 212010782101 BEARING 222382001105 BELL 230 230 1182149 SW M/R CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 0148A 23009 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600641 19980326 00641 SW 1998 3 26 HEEA0013368 1 19980318 A 6300 230330509101 BEARING 230030535101 BELL 230 230 1182149 SW M/R DRIVE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600642 19980326 00642 SW 1998 3 26 HEEA0013369 1 19980318 A 6300 222330619101 BEARING 222331618105 BELL 230 230 1182149 SW M/R DRIVE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN LK0125 23009 BEARINGS WORN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600643 19980326 00643 SW 1998 3 26 HEEA0013370 1 19980318 A 6300 20012403528 BUSHING 222010509105 BELL 230 230 1182149 SW M/R DRIVE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN NA 23009 BUSHING DAMAGED. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600644 19980326 00644 SW 1998 3 26 HEEA0013371 1 19980318 A 6700 MS276475 BEARING 222001383101 BELL 230 230 1182149 SW FLT CONTROL ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN H3834 23009 BEARING ROUGH. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U NC H9SW 1998032600645 19980326 00645 1998 3 26 HEEA0013372 4 19980318 A 3453 071143100 ANTENNA KA83 BELL 206 206L1 1182107 SW LORAN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 513EH 45421 LORAN HAS NO SIGNAL WITH THIS ANTENNA. BAD FROM STOCK. 1 G 7 1 3U H2SW 1998032600646 19980326 00646 1998 3 26 HEEA0013373 4 19980318 A 3452 071119218 CONTROL BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 TRANSPONDER DOES NOT TEST PROPERLY AND NO LIGHTS TO SHOW MODE IT IS IN. 1 G 7 2 4U H4SW 1998032600647 19980326 00647 1998 3 26 HEEA0013374 4 19980318 A 2312 4000102000 TRANSCEIVER RT13 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 45381 NO 5 VOLTS OUT OF POWER SUPPLY AND CHECK TONES FOR PROPER OPERATION. 1 G 7 1 3U H2SW 1998032600648 19980326 00648 SW 1998 3 26 HEEA0013375 1 19980318 A 2120 212073927003 SERVO BELL 412 412 1182202 SW AIR DIST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 SERVO CONTROLLER MOTORS RUNS CONSTANTLY. 1 G 7 2 4U H4SW 1998032600649 19980326 00649 SW 1998 3 26 HEEA0013376 1 19980318 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW CYCLIC FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 SYSTEM CYLIC WOULD NOT MOVE WHEN BEEPED. 1 G 7 2 4U H4SW 1998032600650 19980326 00650 NE 1998 3 26 HEEA0013377 2 19980318 A 7210 3024780 COMBINING GRBOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 4357 33020 COMBINING GEAR BOX MAKING METAL. 1 G 7 2 4U 4 U H4SW E22EA 1998032600651 19980326 00651 NE 1998 3 26 HEEA0013378 1 19980318 A 7810 7630507003044 EJECTOR SKRSKY S76 S76A 8143006 NE EXHAUST CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 EXH EJECTOR CRACKED. 1 G 7 2 3U H1NE 1998032600652 19980326 00652 SW 1998 3 26 HEEA0013379 1 19980318 A 2810 214066255103 FUEL CELL BELL 214 214ST 1182106 SW SEAMS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 59806 28140 FUEL CELL LEAKING. DETERIORATED SEAMS. 2 G 7 2 4U H10SW 1998032600653 19980326 00653 SW 1998 3 26 HEEA0013380 1 19980318 A 6330 214031615105 BEARING BELL 214 214ST 1182106 SW CLEVIS ARM ASSY SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ELASTOMER BEARING SEPARATED. 2 G 7 2 4U H10SW 1998032600654 19980326 00654 SW 1998 3 26 HEEA0013381 1 19980318 A 2842 391046199 PROBE BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 PROBE WILL NOT TEST. 1 G 7 2 4U H4SW 1998032600655 19980326 00655 SW 1998 3 26 HEEA0013382 1 19980318 A 2842 391046200 PROBE BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 PROBE CAUSES INDICATOR TO RISE 200 LBS. 1 G 7 2 4U H4SW 1998032600656 19980326 00656 SW 1998 3 26 HEEA0013383 1 19980318 A 2841 384178103 SWITCH BELL 412 412 1182202 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 CAPACITANCE OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998032600657 19980326 00657 EU 1998 3 26 HEEA0013384 1 19980318 A 7931 4011001 INDICATOR BOLKMS 105 BO105S 5626006 EU NR 2 ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911EB S812 NR2 ENGINE OIL PRESSURE HIGH AT 100%. 1 G 7 2 3U H3EU 1998032600658 19980326 00658 1998 3 26 HEEA0013385 4 19980318 A 3416 A30 ALT ENCODER BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB S737 ALT ENCODER HAS NO VALID OUTPUT. 1 G 7 2 3U H3EU 1998032600659 19980326 00659 1998 3 26 HEEA0013386 4 19980318 A 3416 A30 ALT ENCODER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 51540 ENCODER HAS NO VALID OUTPUT. 1 G 7 1 3U H2SW 1998032600660 19980326 00660 SW 1998 3 26 HEEA0013387 1 19980318 A 2842 2003600000102 TRANSMITTER BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 WILL NOT TRANSMIT SIGNAL 1 G 7 2 4U H4SW 1998032600661 19980326 00661 SW 1998 3 26 HEEA0013388 1 19980318 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 MAG BRAKE INTERMITTENT -- AUTO TRIM NOT WORKING. 1 G 7 2 4U H4SW 1998032600662 19980326 00662 SW 1998 3 26 HEEA0013389 1 19980318 A 2436 214175153105 REGULATOR BELL 214 214ST 1182106 SW GEN VOLTAGE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 NO GENERATOR OUTPUT. VOLTAGE REG FAILED. 2 G 7 2 4U H10SW 1998032600663 19980326 00663 SW 1998 3 26 HEEA0013390 1 19980318 A 7722 212075067105 INDICATOR BELL 412 412 1182202 SW ENG ITT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 WILL NOT INDICATE. 1 G 7 2 4U H4SW 1998032600664 19980326 00664 SW 1998 3 26 HEEA0013391 1 19980318 A 7722 212075067109 INDICATOR BELL 412 412 1182202 SW ENG ITT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 WILL NOT INDICATE. 1 G 7 2 4U H4SW 1998032600665 19980326 00665 1998 3 26 HEEA0013392 4 19980318 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW COCKPIT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 RATE GYRO ERRATIC INDICATION. 1 G 7 2 4U H4SW 1998032600666 19980326 00666 1998 3 26 HEEA0013393 4 19980318 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 RATE GYRO INOPERATIVE. 1 G 7 2 4U H4SW 1998032600667 19980326 00667 SW 1998 3 26 HEEA0013394 1 19980318 A 7722 3030083 TRIM COMPENSATOR BELL 412 412 1182202 SW ENG TRIM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 READS 80 DEGREES TOO HIGH. ENGINE TRIM COMPENSATOR FAILED. 1 G 7 2 4U H4SW 1998032600668 19980326 00668 1998 3 26 HEEA0013395 4 19980318 A 3421 206075607103 ATTITUDE GYRO BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 42EA 51542 ATTITUDE GYRO PRECESSES AND WILL NOT CAGE. 1 G 7 1 3U H2SW 1998032600669 19980326 00669 1998 3 26 HEEA0013396 4 19980318 A 3424 A593002 INDICATOR BELL 206 206L1 1182107 SW COCKPIT T&B FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2251Z 45756 T&B INDICATOR IS NOT WORKING. 1 G 7 1 3U H2SW 1998032600670 19980326 00670 1998 3 26 HEEA0013397 4 19980318 A 3424 206070274005 INDICATOR BELL 206 206L3 1182108 SW COCKPIT T&B FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251V 51404 INDICATOR "DEAD" IS INOPERATIVE AND NEEDS LIGHT. 1 G 7 1 3U H2SW 1998032600671 19980326 00671 SW 1998 3 26 HEEA0013398 1 19980318 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW M/R BINDING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 ROTARY ACTUATOR BINDING. 1 G 7 2 4U H4SW 1998032600672 19980326 00672 SW 1998 3 26 HEEA0013400 1 19980318 A 2432 214175379103 CHARGER BELL 214 214ST 1182106 SW BATTERY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 CHARGER WON'T CHARGE BATTERY. 2 G 7 2 4U H10SW 1998032600673 19980326 00673 SW 1998 3 26 HEEA0013401 1 19980318 A 2432 214175379103 CHARGER BELL 214 214ST 1182106 SW BATTERY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 CHARGER INOPERATIVE. BATTERY NEVER SHOWS TOP CHARGE. 2 G 7 2 4U H10SW 1998032600674 19980326 00674 SW 1998 3 26 HEEA0013402 1 19980318 A 2932 205076044009 PRESSURE SWITCH BELL 214 214ST 1182106 SW HYD SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 PRESSURE SWITCH FAILED 2 G 7 2 4U H10SW 1998032600675 19980326 00675 SW 1998 3 26 HEEA0013403 1 19980318 A 7714 212075037101 INDICATOR BELL 412 412 1182202 SW ENGINE N1 STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 INDICATOR IS STICKING. 1 G 7 2 4U H4SW 1998032600676 19980326 00676 SW 1998 3 26 HEEA0013404 1 19980318 A 2810 206061661103 FUEL CELL BELL 206 206B3 1181506 SW FUEL SYS CRACKED E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 22751 3627 EXCESSIVE CRACKS ON SEAMS AND SEEPAGE THROUGH FABRIC. 1 G 7 1 3U H2SW 1998032600678 19980326 00678 EU 1998 3 26 HEEA0013406 1 19980318 A 6410 355A12004008 BLADES SNIAS 350 AS350B2 8680813 EU T/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4031L 509 2907 DAMAGE ON T/R BLADES LEADING EDGE NEAR ROOT IN AREA (F). 1 G 7 1 3U H9EU 1998032600679 19980326 00679 SW 1998 3 26 HEEA0013407 1 19980318 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31801 51074 BEEP RANGE WILL NOT STAY AT MAX. OR MIN. POSITION. 1 G 7 1 3U H2SW 1998032600680 19980326 00680 SW 1998 3 26 HEEA0013409 1 19980318 A 7714 214175428101 PANEL ASY BELL 214 214ST 1182106 SW ENGINE GAUGE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 ENGINE RPM WORKS INTERMITTENTLY. 2 G 7 2 4U H10SW 1998032600681 19980326 00681 SW 1998 3 26 HEEA0013410 1 19980318 A 6320 407375005101 INDICATOR BELL 407 407 SW XMSN OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 177 53142 NO PRESSURE INDICATION POWER. XMSN OIL TEMP/PRESS 1 G 7 1 3U O H2SW 1998032600742 19980326 00742 EU 1998 3 26 98ZZZX1192 1 19980117 A 4950 APU BAG BAE146 BAE146300A 1500267 EU CABIN ODOR A A6WA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 615AW E3141 LAX - FLT 676 - AFTER GALLEY SHED ELECTRICAL SMELL, CONTINUED WITH APU RUNNING APU GENERATOR ON. CHECKED GALLEY AREA, N O ABNORMALITIES NOTED. PERFORMED PACK BURN OUT PROCEDURE. ODOR DISAPPEARED. 2 H 7 4 4F RT A49EU 1998032600743 19980326 00743 EU 1998 3 26 98ZZZX1193 1 19980117 A 2450 SWITCH BAG BAE146 BAE146300A 1500267 EU GALLEY TRIPPED A A6WA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 GL 31 615AW E3141 LAX - FLT 676 - GALLEYS WILL NOT POWER UP AND F/A NOTICED ELECTRICAL SMELL IN REAR GALLEY. RESET MASTER START SWITCH, R EF BLK 2. 2 H 7 4 4F RT A49EU 1998032600746 19980326 00746 EU 1998 3 26 98ZZZX1196 1 19980117 A 3350 POWER SUPPLY BAG BAE146 BAE146300A 1500267 EU CABIN INOPERATIVE A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 612AW E3122 RIGHT REAR EMERGENCY EXIT LIGHT INOPERABLE. REMOVED AND REPAIRED EMERGENCY POWER SUPPLY. 2 H 7 4 4F RT A49EU 1998032600747 19980326 00747 NE 1998 3 26 98ZZZX1197 2 19980116 A 7200 ENGINE BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE NR 1 FAILED A A6WA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 611AW 19414 E3120 LF05224 SBA - FLT 586 - NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN - DIVERTED TO LAS. UNDER FURTHER INVESTIGATION. 2 H 7 4 4F 4 F RT A49EU E6NE 1998032600788 19980326 00788 WP 1998 3 26 SABA980016 2 19980309 A 7320 1379287L405 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UHR WP RT ENGINE LOOSE A SABA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 33 959AE 959 P66225C CLT - FLT 5167 - ON FLIGHT FROM LEX TO CLT, PILOT REPORTED TO DISPATCH THAT THE RIGHT ENGINE STARTED LOOSING POWER. THE ENGINE FINALLY SHUT ITSELF DOWN. AIRCREW DECLARED AN INFLIGHT EMERGENCY AND LANDED SAFELY AT CLT. MAINTENANCE FOUND T HE P3 LINE ON THE RT ENGINE LOOSE. P3 LINE WAS RETORQUED, RUN AND OPS CHECKED. TEST FLIGHT WAS REQUESTED. AIRCRAFT RE TURNED FROM TEST FLIGHT AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1998032600789 19980326 00789 NM 1998 3 26 GAIA9830 1 19980312 A 2612 FIRE LOOP BOEING 727 727214 138407R NM NR 2 ENGINE CHAFED A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 751US 21513 CREW REPORTED INTERMITTENT FIRE BELL AND LIGHT INDICATIONS FOR NR 2 ENGINE DURING CLIMB-OUT. ACFT MADE AN UNEVENTFUL RE TURN TO TOL. FOUND A-SYS LOOP HARNESS ON LOWER LOOP CHAFING ON ENG GENERATOR GROUND CABLE. REPAIRED WIRING ON LOOP HAR NESS. ALSO, FOUND 6TH, 8TH, AND 13TH STAGE BLEED AIR SADDLE DUCT LEAKING AND COWL ANTI-ICE VALVE AFT GASKET LEAKING. R EPLACED END CAP SHIMS AND GASKET ON ANTI-ICE VALVE. GROUND RAN ENG AT T/O POWER FOR SEVERAL MINUTES. PERFORMED TAXI CH ECK. FUNCTIONAL TEST CHECKS GOOD. ACFT COMPLETED SUCCESSFUL FLIGHT TEST WITH NR 2 ENGINE FIRE WARNING SYS OPERATING PR OPERLY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998032600790 19980326 00790 NM 1998 3 26 GAIA9829 1 19980305 A 3020 470962 DUCT BOEING 727 727214 138407R NM NR 2 ENGINE LEAKING A GAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 751US 21513 NR 2 ENGINE FIRE LIGHT CAME ON IN FLIGHT. AIRCRAFT MADE AN UNEVENTFUL RETURNED TO TOL. FOUND BLEED AIR LEAK AT INLET O F ANTI-ICE DUCTS CAUSING OVERHEAT CONDITION. REPLACED INLET ANTI-ICE BLEED AIR DUCTS AND SUPPORT HARDWARE. GROUND RAN NR 2 ENGINE AT TAKEOFF POWER SETTINGS. FUNCTIONALLY TESTED ANTI-ICE SYSTEM WITH NO LEAKS NOTED. AIRCRAFT RETURNED TO S ERVICE (M) 2 L 7 3 4F A3WE 1998032600791 19980326 00791 1998 3 26 98ZZZX1238 4 19980307 A 2210 CONTROL PANEL BOEING 727 727227 1384078 NM COCKPIT FAILED A AMTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 769AT 21998 DURING CRUISE FLIGHT, SMOKE WAS NOTED COMING FROM TOP OF CONTROL STAND UNDER AUTOPILOT PANEL. SMOKE STOPPED WHEN 'ALT' HOLD WAS SHUT OFF. ACCOMPLISHED SMOKE EVAC PER ADM, OPENED C/B. REMOVED AND REPLACED AUTOPILOT CONTROL PANEL IAW 22-11 -81. 2 L 7 3 4F A3WE 1998032600792 19980326 00792 EU 1998 3 26 VTZA98069 1 19980216 A 3260 8005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT MLG OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 484UE 899 FLT 6202 - IAD-HPN - DURING CLIMB, AIRCRAFT MADE A UNSCHEDULED LANDING AT IAD DUE TO RT MAIN GEAR GREEN INDICATOR NEVER WENT OUT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED RT DOWNLOCK MICROSWIT CH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600793 19980326 00793 1998 3 26 VTZA98068 4 19980216 A 3414 39948B2236 ASI BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILURE A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 495UE 818 FLT - 6282 - IAD-HPN - AIRCRAFT MADE A UNSCHEDULED LANDING AT IAD DUE TO FO'S ASI READING 40 KNOTS LOW. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ASI, OPS CHECK OK. AIRCRAFT WAS RE LEASED AND APPROVED FRO RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600794 19980326 00794 EU 1998 3 26 VTZA98066 1 19980216 A 5210 NAS620313D SHEAR BOLTS JETAIR JETSTM JETSTM4101 1500501 EU PASS DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 313UE 41026 FLT 6275 - BWI-BOS - DURING CLIMB, AIRCRAFT MADE A UNSCHEDULED LANDING AT BWI DUE TO PASSENGER DOOR WARNING LIGHT ILLUMI NATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBED DOOR SHEAR BOLT S. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600795 19980326 00795 EU 1998 3 26 VTZA98065 1 19980215 A 5270 91SE16 SWITCHES JETAIR JETSTM JETSTM4101 1500501 EU PAX DOOR OUT OR ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 317UE 41031 FLT 6225 - IAD-BOS - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 41886, MEL 52-2. MAINTENANCE CLOSED D MI 41886 ON 3-16-98 BY ADJUSTING PASSENGER DOOR MICROSWITCHES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600796 19980326 00796 EU 1998 3 26 VTZA98064 1 19980215 A 2450 A2105E PDU JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 312UE 41025 IAD-JFK - FLT 6305 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO ELECTRICAL PROBLEM ON THE NON ESS ENTIAL BUS POWER WAS INTERMITTENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOV ED AND REPLACED RT PDU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600797 19980326 00797 EU 1998 3 26 VTZA98063 1 19980212 A 5270 JE5 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 482UE 897 FLT 6260 - IAD-BUF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO PASSENGER DOOR WARNING LIGHT ILLUM INATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS ON DOOR AND COULD NOT DUPLCIATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600798 19980326 00798 EU 1998 3 26 VTZA98060 1 19980210 A 7921 OIL COOLER FLAP JETAIR JETSTM JETSTM4101 1500501 EU RIGHT INOPERATIVE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 307UE 41021 FLT 6190 - IAD-BDL - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT OIL COOLER FLAP INOP. AIRCRAFT RETUR NED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CYCLED POWER TO RT OIL COOLER FLAP ACTUATOR AND NO FAUL TS FOUND, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600799 19980326 00799 1998 3 26 VTZA98061 3 19980210 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 489UE 908 FLT 6250 - ABE-IAD - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT BETA WARNING LIGHT NEVER TURNED OFF. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PROB LEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600800 19980326 00800 EU 1998 3 26 VTZA98050 1 19980204 A 3020 CCT DE-ICE JETAIR JETSTM JETSTM4101 1500501 EU NR 2 ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 308UE 41023 FLT 6290 - IAD-DAY - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 2 CCT DE-ICE FAILED. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND IS STILL WORKING ON PROBLEM. (M) 2 L 7 2 4T RT A41NM 1998032600801 19980326 00801 EU 1998 3 26 VTZA98046 1 19980204 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3201 1500217 EU BAGGAGE COMPT FAILED A VTZA K NONE N FALSE WARNING CR CRUISE 1 EA 27 481UE 895 FLT 6280 - ORF-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD WITH ONE DISCREPANCY WHICH WAS AFT BAGGA GE SMOKE DETECTOR GIVING FALSE WARNING. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPEN ED DMI 50678, MEL 26-4. MAINTENANCE CLOSED DMI 50678 ON 2-6-98 BY GROUND RUNNING AIRCRAFT AND PERFORMING OPS CHECKS, AN D COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600802 19980326 00802 EU 1998 3 26 VTZA980033 1 19980119 A 2750 923FLBU TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU FLAPS OUT OF ADJUST A VTZA K NONE N FALSE WARNING AP APPROACH 1 EA 27 482UE 897 FLT 6243 - IAD-PHF - DURING APPROACH, EXPERIENCED A DISCREPANCY WITH THE FLAP SYSTEM. WHEN FLAPS WERE SELECTED TO 20 DE GREES, ACTUALLY WENT TO 45 DEGREES. AIRCRAFT LANDED WITH NO INCIDENT. MX CONTROL WAS NOTIFIED AND MX WAS DISPATCHED FR OM IAD TO TROUBLESHOOT THE DISCREPANCY. CURRENTLY AIRCRAFT IS STILL IN PHF UNDERGOING FURTHER TROUBLESHOOTING. AIRCAFT WAS FERRY FLOWN TO IAD WHER MAINTENANCE INSPECTED AND ADJUSTED FLAPS 20 DEGREE TRANSMITTER MICROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600803 19980326 00803 EU 1998 3 26 VTZA98010 1 19980112 A 2913 3849251 HYDRAULIC PUMP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE LEAKING A VTZA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 489UE 908 FLT 6606 - IAD-ROC - DURING TAXI AFTER LANDING, EXPERIENCED AN UNSAFE NOSE GEAR WARNING INDICATION. AIRCRAFT WAS STOPPE D AND NOSE GEAR WAS PINNED AND AIRCRAFT CONTINUED TO THE GATE. ALSO, UPON ARRIVAL AT THE GATE THE BRAKE SYSTEM FAILED A FTER THE AIRCRAFT WAS FULLY STOPPED. MAINTENANCE CONTROL WAS NOTIFIED AND MAINTENANCE WAS DISPATCHED. MAINTENANCE FOUN D THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. PUMP WAS REMOVED AND REPLACED IAW THE MM AND ALL CHECKS WERE PERFORME D. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600804 19980326 00804 EU 1998 3 26 VTZA98034 1 19980128 A 5270 JE5 SWITCH ARM BAG JETSTM JETSTM3201 1500217 EU PAX DOOR BROKEN A VTZA K NONE N FALSE WARNING AP APPROACH 1 EA 27 487UE 906 FLT 6257 - ALB-IAD - DURING APPROACH, EXPERIENCED A DOOR CAPTION WARNING LIGHT ILLUMINATION. CREW DECLARED AN EMERGENCY AND LANDED AT IAD WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO GATE AND MAINTENANCE CONTROL WAS NOTIFIED AND MAINTENAN CE WAS DISPATCHED. UPON ARRIVAL MAINTENANCE FOUND THAT THE LOWER (FLOOR) MICROSWITCH ARM HAD BROKEN. MAINTENANCE REMOV ED AND REPLACED THE ARM. ALL SYSTEMS WERE CHECKED WITHOUT FURTHER PROBLEM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M ) 2 L 7 2 4T RT A56EU 1998032600805 19980326 00805 EU 1998 3 26 VTZA98038 1 19980201 A 5220 EMER EXIT DOOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN NOT LATCHED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 330UE 41098 FLT 6456 - IAD-JFK - ABORTED TAKEOFF DUE TO EMERGENCY EXIT WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESEATED AFT EMERGENCY EXIT DOOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600806 19980326 00806 EU 1998 3 26 VTZA98041 1 19980202 A 5210 HANDLE BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 488UE 907 FLT 920 - EWR-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 07060, MEL 52-2. MAINTENANC E CLOSED DMI ON 2-2-98 BY ADJUSTING PASSENGER DOOR HANDLE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600807 19980326 00807 1998 3 26 VTZA98043 4 19980204 A 3417 7000700966 DADC JETAIR JETSTM JETSTM4101 1500501 EU NR 2 MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 309UE 41022 FLT 6264 - BTV-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 2 DADC AND NR 2 AHRS FAILED. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RERACKED NR 2 DADC AND NR 2 AHRS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600808 19980326 00808 1998 3 26 VTZA98044 4 19980204 A 3418 C771065 SIG SUMMING UNIT BAG JETSTM JETSTM3201 1500217 EU LT/RT OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 479UE 893 FLT 6153 - ABE-IAD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO STALL SHAKER SOUNDED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED THE R1 AND R2 POTENTIOMETERS ON THE LT AND RT SIGN AL SUMMING UNITS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600809 19980326 00809 EU 1998 3 26 VTZA98045 1 19980204 A 7600 21188408 IEC JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 315UE 41033 FLT 6508 - IAD-LGA - ABORTED TAKEOFF DUE TO RT ENGINE STARTED TO TTL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEM S. MAINTENANCE INSPECTED AND FOUND NR 2 BRIDGE INDICATION ERRONEOUS. MAINTENANCE SWITCHED TO NR 1 BRIDGE AND PERFORMED GROUND RUNS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600810 19980326 00810 1998 3 26 VTZA98048 4 19980205 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 EA 27 331UE 41099 FLT 6342 - IAD-EWR - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 2 AHRS FAILED. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 2 AHRS, OPS CHECK OK. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600811 19980326 00811 EU 1998 3 26 VTZA98047 1 19980205 A 7600 21188408 IEC JETAIR JETSTM JETSTM4101 1500501 EU RT LOOSE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 321UE 41045 FLT 6258 - IAD-ALB - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RT IEC FAILED. AIRCRAFT RETURNED TO GATE WITH NO F URTHER PROBLEMS. MAINTENANCE INSPECTED AND TIGHTENED T2 SENSOR AND GROUND RAN AIRCRAFT. OPS CHECK OK. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600812 19980326 00812 EU 1998 3 26 VTZA98039 1 19980129 A 2913 384925 HYDRAULIC PUMP BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 490UE 909 FLT 6274 - BUF-IAD - DURING APPROACH, AIRCRAFT MADE A SCHEDULED LANDING DUE FLAP INDICATIONS 10 DEGREES IN FLIGHT WITH H ANDLE AT ZERO ON LANDING PLUS TOTAL LOSS OF HYDRAULIC POWER ON LANDING. AIRCRAFT WENT TO GATE AND WITH NO FURTHER PROBL EMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PUMP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED F OR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600813 19980326 00813 EU 1998 3 26 VTZA98040 1 19980130 A 5610 1379377C405 WINDSCREEN BAG JETSTM JETSTM3201 1500217 EU COCKPIT CRACKED A VTZA A UNSCHED LANDING C F.O.D. CR CRUISE 1 EA 27 488UE 907 FLT 6194 - IAD-EWR - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CAPT'S OUTER WINDSCREEN CRACKED DUE TO B IRD STRIKE. AIRCRAFT RETURNED TO GATE AND WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WIN DSCREEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600814 19980326 00814 NM 1998 3 26 TAOA021810 1 19980225 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 918TS 20445 FLT 6181 - OVERNIGHT L/S, FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY OPERATIONAL CHECK NORMAL PER MM 33 -50. (M) 2 L 7 3 4F A3WE 1998032600815 19980326 00815 NM 1998 3 26 TWAA9802701 1 19980223 A 2530 8203110000 OVEN BOEING 757 7572Q8 1384972 NM NR 3 FAILED A TWAA H DEACTIVATE SYST/CIRCUITS O OTHER NR NOT REPORTED 1 CE 05 713TW 28173 STL - FLT 2 - AFT GALLEY NR 3 OVEN HAD ELECTRICAL SMELL WHEN POWER APPLIED. PULLED CB AND DID NOT USE OVEN. REPLACED T HE OVEN. (M) 2 L 7 2 4F RT A2NM 1998032600816 19980326 00816 NM 1998 3 26 TWAA9802501 1 19980219 A 3230 656021134 ACCESSORY BOX BOEING 727 727231 1384079 NM NLG MALFUNCTIONED A TWAA O OTHER J WARNING INDICATION TO TAKEOFF 1 CE 05 54336 20490 STL - FLT 328 - GEAR LEVER WAS LOCKED ON TAKEOFF. OVERRODE GEAR LEVER LOCK AND GEAR RETRACTED NORMALLY WITH NO HORNS. N OSE WHEEL WAS CENTERED. FOUND NOSE GEAR SAFETY SWITCH NOT MAKING. SERVICED NOSE STRUT PER MM AND REPLACED LANDING GEAR ACCESSORY BOX. (M) 2 L 7 3 4F A3WE 1998032600817 19980326 00817 NE 1998 3 26 TWAA9802604 2 19980222 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RIGHT FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 CE 05 907TW 49165 1227 PHL - FLT 561 - AT APPROX 3000 FEET, CREW HEARD LOUD POP. THE RT ENGINE EPR DROPPED OFF. CREW REPORTED ENGINE FAILED AN D SHUT DOWN. FLT RETURNED TO PHL. REPLACED THE RT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998032600818 19980326 00818 WP 1998 3 26 TWAA9802603 1 19980221 A 3320 5004WW LAMP DOUG DC9 DC932 3022066 WP FWD GALLEY FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 920L 47734 JAX - FLT 494 - FORWARD GALLEY OVERHEAD FLOURSCENT WORK LIGHT, RT OUTBOARD, WAS SMOKING SHORTLY AFTER TAKEOFF. THE LIGH T WAS TURNED OFF. AT JAX THE LIGHT WAS DEACTIVATED BY PULLING THE CIRCUIT BREAKER. CORRECTION WAS DEFERRED. ON LAYOVE R, THE WIRING AND SECURITY WAS CHECKED AND FOUND NORMAL. NO SIGNS OF OVERHEATING. RELAMPED AND OPERATED FOR SEVERAL HO URS. OPERATIONS WAS NORMAL. (M) 2 L 7 2 4F A6WE 1998032600819 19980326 00819 NM 1998 3 26 TWAA9802602 1 19980221 A 2421 736664E IDG BOEING 767 767231 1385131 NM RT ENGINE FAILED A TWAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 CE 05 605TW 22568 JFK - FLT 12 - THE RIGHT ENGINE GENERATOR FAILED. EICAS MESSAGE RT GEN OFF DISPLAYED. FLT RETURNED TO JFK. PLACARDED GEN INOP PER MEL. ON LAYOVER, THE RT IDG WAS REPLACED. (M) 2 L 7 2 4F RT A1NM 1998032600820 19980326 00820 WP 1998 3 26 TWAA9802601 1 19980222 A 2822 3980001 BOOST PUMP DOUG DC9 DC982 3022082 WP CENTER TANK WORN A TWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 05 906TW 49160 LAX - FLT 221 - AFTER ABOUT 10,000 LBS OF FUEL BURNED OUT OF CENTER TANK, CENTER TANK STOPPED FEEDING THE ENGINES, 6800 LBS REMAINED. MADE UNSCHEDULED LANDING AT LAX. CENTER TANK WAS EMPTIED USING ONLY FORWARD PUMP. REPLACED THE CENTER T ANK AFT BOOST PUMP. (M) 2 L 7 2 4F A6WE 1998032600821 19980326 00821 NE 1998 3 26 98ZZZM332 2 19980206 A 8530 327626 CYLINDER CVAC 240 24013 2422626 WP PWA R2800 R2800* 52026 NE NR 2 ENG CRACKED A TFAA A E UNSCHED LANDING ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 SO 15 91237 140 P32011 WHILE IN CRUISE, NR 2 ENGINE BEGAN BACKFIRING REPEATEDLY ENGINE SHUT DOWN AND SECURED AND LANDED MDPC WITH NO INCIDENT. FOUND NR 4 CYLINDER CRACKED. REMOVED AND REPLACED WITH SERVICEABLE CYLINDER ASSY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R 4 R A793 5E8 1998032600822 19980326 00822 NM 1998 3 26 98ZZZM333 1 19980208 A 7120 BEARING BOEING 747 747273C 1384896 NM NR 4 PYLON WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON AFT UPPER MOUNT HAS WORN ATTACH BUSHING AND SIDE PLAY. THRUST LINK END FITTING WORN. ENGINE UPPER MOUNT BUSHING REPLACED IAW OHM 20-50-03, THRUST LINK BEARING REPLACED IAW OHM 20-50-03. (M ) 2 L 7 4 4F A20WE 1998032600823 19980326 00823 NM 1998 3 26 AALA980345 1 19980217 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 617AM 24525 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS ILLUMINATED WITH SWITCH OFF. REPLACED EMERGENCY FL OOR PATH LIGHTING CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998032600825 19980326 00825 NM 1998 3 26 AALA980346 1 19980217 A 3350 1703643 PIN BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 370AA 25197 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS INOPERATIVE AT PAX SEATS 19B, 20B AND 21B. REPLACED PINS AT P AX SEATS 19B, 20B AND 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998032600826 19980326 00826 NM 1998 3 26 AALA980317 1 19980216 A 3350 1721651 CONNECTOR BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312AA 22315 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 30HJ WOULD NOT ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT ROW 30 HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998032600827 19980326 00827 NM 1998 3 26 AALA980315 1 19980216 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 40AB INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 40AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998032600828 19980326 00828 WP 1998 3 26 AALA980377 1 19980222 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 224AA 49174 PHX - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998032600829 19980326 00829 WP 1998 3 26 AALA980378 1 19980220 A 3397 WIRE DOUG DC9 DC982 3022082 WP COCKPIT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 33414 49325 DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. RESECURED LOOSE GROUND WIRE AT C OCKPIT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998032600830 19980326 00830 WP 1998 3 26 AALA980301 1 19980210 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7544A 53026 LAS - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPAIRED SHORTED WIRE IN RIGHT OVERWING EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998032600831 19980326 00831 WP 1998 3 26 AALA980293 1 19980210 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70529 49921 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPAIRED EMERGENC Y FLOOR PATH LIGHTING CHAFED WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998032600832 19980326 00832 EU 1998 3 26 RAIA980307 1 19980308 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 432AM 883 FLT 7332 - STL - LEFT ENGINE RPM WENT TO ZERO IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR. (M) 2 L 7 2 4T RT A56EU 1998032600833 19980326 00833 EU 1998 3 26 RAIA980306 1 19980307 A 2435 23079009 STARTER/GEN BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 973JX 973 FLT 4763 - PSP - LEFT ENGINE GENERATOR CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE STARTER GENERATO R. (M) 2 L 7 2 4T RT A56EU 1998032600834 19980326 00834 EU 1998 3 26 RAIA980233 1 19980226 A 5320 S53672400214 ANGLE AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 20, BETWEEN STRINGERS 21L AND 21R. MAINTENANCE REPAIRED FRAME 20 FAIL/SAFE ANGLE BETWEEN STRINGERS 21L AND 21R PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600835 19980326 00835 EU 1998 3 26 RAIA980232 1 19980225 A 5210 S5367121720402 PLATE AEROSP ATR42 ATR42300 8680920 EU PAX DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION ON PASSENGER DOOR SPRING ATTACH PLATE. MAINTENANCE REPLACED PASSENGER D OOR SPRING ATTACH PLATE PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600836 19980326 00836 EU 1998 3 26 RAIA980231 1 19980225 A 5320 S53572103200 CLIP AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 39 FOOTINGS, BETWEEN STRINGERS 20L AND 19L, 18L AND 17L. MAINT ENANCE REPAIRED FLOOR FRAME 39 FOOTINGS BETWEEN STRINGERS 20L AND 19L, 18L AND 17L PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600837 19980326 00837 EU 1998 3 26 RAIA800230 1 19980225 A 5315 S53672408202 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE FLOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FLOORBEAM 39 FRAME 39 RT SIDE. MAINTENANCE REPAIRED FLOOR FRAME 39 R IGHT SIDE PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600838 19980326 00838 EU 1998 3 26 RAIA980229 1 19980225 A 5315 S53672404206 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FLOOR BEAM 39. MAINTENANCE REPAIRED FLOORBEAM 39 PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600839 19980326 00839 EU 1998 3 26 RAIA980228 1 19980225 A 5347 S536780001000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FLIGHT ATTENDANT LEFT SEAT TRACK. MAINTENANCE REPLACED FLIGHT ATTEND ANT LEFT SEAT TRACK PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600840 19980326 00840 EU 1998 3 26 RAIA980227 1 19980225 A 5347 S536780001000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 36 SEAT TRACK. MAINTENANCE REPLACED SEAT TRACK AT FRAME 36 PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600841 19980326 00841 EU 1998 3 26 RAIA980226 1 19980225 A 5315 S53672404206 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FLOORBEAM 36. MAINTENANCE REPLACED FLOORBEAM 36 PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600842 19980326 00842 EU 1998 3 26 RAIA980225 1 19980225 A 5320 S53572103200 CLIP AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 36 FOOTINGS, BETWEEN STRINGERS 16L AND 21R. MAINTENANCE REPAIR ED FRAME 36 FOOTINGS BETWEEN STRINGERS 16L AND 21R PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600843 19980326 00843 EU 1998 3 26 RAIA980224 1 19980225 A 5347 S536780001000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSIN AT RIGHT INBOARD SEAT TRACK, BETWEEN FRAMES 30 AND 34. MAINTENANCE REPAI RED SEAT TRACK BETWEEN FRAMES 30 AND 34 PR ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600844 19980326 00844 EU 1998 3 26 RAIA980223 1 19980225 A 5320 S53572103200 CLIP AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA O OTHER O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 34 FOOTINGS BETWEEN STRINGERS 19L AND 21R. MAINTENANCE REPLACE D FLOOR FRAME 34 FOOTINGS BETWEEN STRINGERS 19L AND 21R PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600845 19980326 00845 EU 1998 3 26 RAIA980222 1 19980225 A 5320 S53572103200 CLIP AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 32 FOOTINGS, BETWEEN STRINGERS 17L AND 21L. MAINTENANCE REPLAC ED FLOOR FRAME 32 FOOTINGS BETWEEN STRINGERS 17L AND 21L PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600846 19980326 00846 EU 1998 3 26 RAIA980221 1 19980225 A 5311 S53372305222 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 32 BETWEEN STRINGERS 21L AND 21R. MAINTENANCE REPAIRED FLOOR F RAME 32 PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600847 19980326 00847 EU 1998 3 26 RAIA980220 1 19980215 A 5311 S53372305222 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 421TE 21801 102 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 31 BETWEEN STRINGERS 21L AND 21R. MAINTENANCE REPAIRED FLOOR F RAME 31 PER ATR SRM. (M) 2 H 7 2 4T RT A53EU 1998032600848 19980326 00848 EU 1998 3 26 VTZA98085 1 19980220 A 3350 6134051 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCHARGED A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 319UE 41042 FLT 6211 - IAD-PVD - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE CENTER EMERGENCY LIGHTS NOT ILLUMINATING. AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE CONTROL AND MAINTENANCE WAS NOTIFIED. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK FOR THE CENTER EMERGENCY LIGHTS IAW MX PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT W AS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600849 19980326 00849 1998 3 26 VTZA98087 3 19980223 A 6140 KPT06F835 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT PROP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 478UE 892 FLT 6363 - LYH-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO LEFT BETA LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FUR THER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BETA SWITCH CANNON PLUG. OPS CHECK OK. AIRCRAFT WAS APP ROVED AND RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600850 19980326 00850 EU 1998 3 26 VTZA98088 1 19980223 A 3297 WIRE JETAIR JETSTM JETSTM4101 1500501 EU GEAR SELECTOR BROKEN A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 321UE 41045 FLT 6309 - BWI-BOS - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LANDING GEAR WOULD NOT RETRACT. AIRCRA FT RETURNED TO GATE WITH NO FURTHER PROBLEMS. AIRCRAFT FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND REPAIRED BROKEN W IRE TO PIN M AT THE GEAR SELECTOR CONNECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A41NM 1998032600851 19980326 00851 EU 1998 3 26 VTZA98089 1 19980224 A 3350 311701 BATTERY PACKS BAG JETSTM JETSTM3201 1500217 EU CABIN DISCHARGED A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 472UE 823 FLT 6467 - PHF-IAD - DURING TAXI FLIGHT, AIRCRAFT RETURNED TO GATE DUE TO EMERGENCY EXIT LIGHT INOP. MAINTENANCE INSPEC TED AND REMOVED AND REPLACED BATTERY PACKS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A56EU 1998032600852 19980326 00852 EU 1998 3 26 VTZA98090 1 19980224 A 2611 7211121100 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU COMPT FAILED A VTZA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 324UE 41017 FLT 6479 - ORF-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO MAIN BAGGAGE BAY SMOKE DETECTOR WOULD NOT TEST. AIRC RAFT WAS FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND REMOVED AND REPLACED AFT SMOKE DETECTOR. OPS CHECK OK. AIRCRAF T WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600853 19980326 00853 1998 3 26 VTZA98091 4 19980224 A 3417 7000700966 DADC JETAIR JETSTM JETSTM4101 1500501 EU AVIONICS FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 323UE 41059 FLT 6267 - IAD-BTV - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO BOTH ASI INOP. AIRCRAFT WENT OT GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTION AND REMOVED AND REPLACED DADC. OPS CHECK OK. AIRCRAFT WAS RELEA SED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600854 19980326 00854 EU 1998 3 26 VTZA98092 1 19980224 A 3250 14132012407 STEERING SHAFT JETAIR JETSTM JETSTM4101 1500501 EU NLG LACK OF LUBE A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 316UE 41055 FLT 6510 - IAD-LGA - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO NOSE STEERING STUCK TO THE LEFT. MAINTENANCE INSPECT ED AND RERACKED PLUS LUBED RACK AND PINNION NLG STEERING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600855 19980326 00855 EU 1998 3 26 VTZA98094 1 19980225 A 5270 JE5 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 485UE 901 FLT 6598 - IAD-RDU - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT RDU DUE TO CABIN DOOR WARNING LIGHT ILLUMINAT ED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBRICATED PASSENGER DOOR MI CROSWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600856 19980326 00856 EU 1998 3 26 VTZA98097 1 19980226 A 3150 T/O WARNING JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT SOUNDED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 327UE 41080 FLT 6326 - IAD-ROC - AIRCRAFT ABORTED TAKEOFF DUE TO CWS SOUNDED DURING TAKEOFF ROLL. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PROBLEM. AIRCRAFT WAS RELEASE D AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600857 19980326 00857 1998 3 26 VTZA98101 4 19980301 A 3425 4020531574 ADI BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 480UE 894 FLT 6458 - IAD-PIT - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO CAPTS ADI WOULD NOT COME ON LINE. MAINTENANCE INSPEC TED AND REMOVED AND REPLACED CAPTAINS ADI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600858 19980326 00858 EU 1998 3 26 VTZA98100 1 19980227 A 2422 1B3501B13 INVERTER BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 490UE 909 FLT 6570 - IAD-MDT - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO LEFT INVERTER FAILED. MAINTENANCE INSPECTED AND COUL D NOT DUPLICATE PROBLEMS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600859 19980326 00859 EU 1998 3 26 VTZA98103 1 19980213 A 5210 SHOOT BOLTS BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 482UE 897 FLT 6435 - IAD-RDU - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO PASSENGER DOOR WARNING LIGHT ILLU MINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBED PASSENGER DOOR SH OOT BOLTS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600860 19980326 00860 EU 1998 3 26 VTZA98110 1 19980306 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 6392 - IAD-BOS - DURING TAKEOFF, EXPERIENCED A DISCREPANCY WITH THE BAGGAGE DOOR WARNING LIGHT ILLUMINATED ON TAKEOF F ROLL. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WHERE MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCH ED AND FOUND THAT THE AFT BAGGAGE BAY DOOR WARNING MICROSWITCH HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE AFT BAG GAGE BAY DOOR MICROSWITCH IAW ALL MAINTENANCE PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600861 19980326 00861 EU 1998 3 26 VTZA98109 1 19980305 A 3350 6134051 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCHARGED A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 307UE 41021 FLT 6356 - PWM-BOS - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE EMERGENCY LIGHTS AT THE LEFT EXIT ROW NOT ILLUMINAT ING. RETURNED TO GATE WHERE MAINTENANCE CONTROL WAS NOTIFIED. AIRCRAFT WAS FERRIED TO IAD MX FACILITY WHERE MAINTENANC E TROUBLESHOT THE DISCREPANCY AND FOUND THE NR 3 BATTERY PACK HAD DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE NR 3 BATTERY PACK IAW MX PROCEDURES. ALL CHECK WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SER VICE. (M) 2 L 7 2 4T RT A41NM 1998032600862 19980326 00862 EU 1998 3 26 VTZA98108 1 19980305 A 7722 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU T-2 SENSOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 483UE 898 FLT 6584 - BOS-SWF - DURING TAKEOFF, EXPERIENCED A LEFT ENGINE EGT FLUCTUATION WITH THE SRL ON. EGT WAS STABLE WITH THE SRL OFF. NOTIFIED MAINTENANCE CONTROL AND SRL SYSTEM WAS DEFERRED UNDER DMI 50763 MEL CODE 76-1. AIRCRAFT WAS THEN RE LEASED FOR SERVICE. AIRCRAFT ARRIVED AT IAD WHERE MAINTENANCE TROUBLESHOT SYSTEM AND FOUND ZONE 2 CANNON PLUG AND T-2 C ANNON PLUG DIRTY. CLEANED CANNON PLUGS AND PERFORMED REQUIRED CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600863 19980326 00863 EU 1998 3 26 VTZA98104 1 19980304 A 3520 17459910 OXYGEN MASKS JETAIR JETSTM JETSTM4101 1500501 EU CABIN WOULD NOT STOW A VTZA K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 302UE 41013 FLT 6543 - EWR-IAD - DURING TAXI, MADE A SCHEDULED LANDING AT IAD WITH ONE DISCREPANCY WHICH WAS OXYGEN MASKS AT ROW 5BC WILL NOT STOW. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 06992 MEL 35.1. M AINTENANCE CLOSED DMI 06992 ON 3-4-98 BY RESTOWING OXYGEN MASKS IN ROW 5BC. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600864 19980326 00864 1998 3 26 VTZA98081 3 19980302 A 6112 PROP HEAT JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 323UE 41059 IAD-BDL - FLT 6212 - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO LEFT PROP HEAT FAILED IN LONG AND SHORT CYCLES. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT PROP. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600865 19980326 00865 EU 1998 3 26 VTZA98102 1 19980213 A 5270 91SE13 SWITCHES BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 482UE 897 FLT 6384 - ROC TO IAD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT ROC DUE TO PASSENGER DOOR WARNING LIGHT IL LUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 21146 MEL 52-2. M AINTENANCE CLOSED DMI 21146 ON 2-13-98 BY ADJUSTING PAX DOOR MICROSWITCHES, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600866 19980326 00866 EU 1998 3 26 VTZA98084 1 19980219 A 6120 8974107 PROP GOV BAG JETSTM JETSTM3201 1500217 EU LT PROP OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 477UE 890 FLT 6478 - JFK-IAD EXPERIENCED AN ILLUMINATION OF THE LEFT SRL LIGHT CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAI NTENANCE CONTROL WAS NOTIFIED AND MAINTENANCE WAS DISPATCHED. MAINTENANCE DEFERRED THE LEFT SRL ON THE AIRCRAFT UNDER M EL NR 76-1 AND DMI NR 07839. MAINTENANCE ADJUSTED THE LEFT PROP GOVERNOR SPEED MONOPOLE AND CLOSED DMI 07839 ON 2-20-98 . OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600867 19980326 00867 EU 1998 3 26 VTZA98086 1 19980223 A 5270 91SE13 SWITCHES BAG JETSTM JETSTM3201 1500217 EU PASS DOOR DIRTY A VTZA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 489UE 908 FLT 6261 - IAD-EWR - DURING CRUISE, AIRCRAFT MADE A SCHEDULED FLIGHT WITH ONE DISCREPANCY WHICH WAS PASSENGER DOOR WARNI NG LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND OPENED DMI 49294 MEL 52-2. MAINTENANCE CLOSED DMI 49294 ON 2-23-98 BY CLEANING MICROSWITCHES AND SECURING BOLT ON PAX DOOR HANDLE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998032600868 19980326 00868 EU 1998 3 26 VTZA98067 1 19980216 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR DIRTY A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 6547 - IAD-ROA - AIRCRAFT ABORTED TAKEOFF DUE BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WIT H NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 53313, MEL 52-4. MAINTENANCE CLOSED DMI 53313 ON 2-24-98 B Y CLEANING MICROSWITCHES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600869 19980326 00869 EU 1998 3 26 VTZA98077 1 19980218 A 3320 1722334 SOCKET JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 27 311UE 41029 FLT 6198 - IAD-BDI - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS SMOKE SMELL FROM ROW 8 AFT OF LAV AREA. MAINTENANCE INSPECTED AND OPENED DMI 50-453, MEL 33-7 ON LIGHT SOCKET. MAINTENANCE CLOSED DMI 50453 ON 2-20-98 BY REMOVING AND REPLACING LIGHT SOCKET AT ROW 10A. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED F OR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600870 19980326 00870 EU 1998 3 26 VTZA98107 1 19980303 A 5610 14156002410 WINDSHIELD JETAIR JETSTM JETSTM4101 1500501 EU RT COCKPIT CRACKED A VTZA A G UNSCHED LANDING O2 MASK DEPLOYED O OTHER CR CRUISE 1 EA 27 309UE 41022 FLT 6388 - IAD-MHT - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT IAD DUE TO FO'S WINDSCREEN CRACKED AT OUTER PANE. AI RCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WINDSCREEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998032600871 19980326 00871 EU 1998 3 26 VTZA98106 1 19980303 A 7714 AG44AF TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 471UE 821 FLT 6480 - GSO-IAD - ABORTED TAKEOFF DUE TO LEFT ENGINE RPM FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TACH GENERATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A56EU 1998032600872 19980326 00872 WP 1998 3 26 ORJA9834 1 19980225 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 EMERGENCY SEAT TRACK LIGHT INOP AT 15 DEF. REMOVED AND REPLACED LAMP AND REPAIRED WIRING, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998032600873 19980326 00873 WP 1998 3 26 ORJA9831 1 19980208 A 3251 39346895001 STEERING CYL DOUG DC9 DC983 3022083 WP NLG FAILED A ORJA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 836RA 53046 DURING TAXI, NOSE WHEEL STEERING FAILED RIGHT HYD SYSTEM PRESSURE AND QTY TO ZERO. REMOVED AND REPLACED LEFT NOSE WHEEL STEERING CYLINDER PER MM CHAP 32-52-02. (M) 2 L 7 2 4F RT A6WE 1998032600874 19980326 00874 WP 1998 3 26 ORJA9830 1 19980223 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 EMERGENCY LIGHTS OUT AT ROWS 14, 15, 16, AND 24. REPLACED BATTERY PACKS AND LAMPS, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998032600875 19980326 00875 WP 1998 3 26 ORJA9820 1 19980223 A 3230 GROUND SENSE ROD DOUG DC9 DC983 3022083 WP NLG DISCONNECTED A ORJA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 833RA 53045 AFTER TAKEOFF, UNABLE TO RAISE GEAR NOSE WHEEL WOULD NOT LOCK IN CENTER POSITION SO GEAR NOT MANUALLY RETRACTED, GROUND SHIFT FAIL ACCOMPLISHED AND RETURNED TO LAND ON LANDING ROLL AND TAXI IN BOTH LEFT AND RIGHT REVERSER ACCUM LOW LIGHTS O N. FOUND ROD FROM GROUND SENSE TO NOSE GEAR CENTERING BELL CRANK DISCONNECTED REINSTALLED SAME BITE CHECK GROUND PROX B OX ALL PASSED AS PER RENO MM. (M) 2 L 7 2 4F RT A6WE 1998032600879 19980326 00879 NM 1998 3 26 ORJA9827 1 19980214 A 3397 00105606003 WIRE DOUG MD90 MD9030 3023690 NM CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 902RA 53490 EMERGENCY FLOOR TRACK INOP FROM AISLE 1FD TO 9DEF, 15DEF. FOUND BROKEN WIRE ROW 2 REINSTALLED, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998032600880 19980326 00880 WP 1998 3 26 ORJA9832 1 19980214 A 3241 TRANDUCER PINS DOUG DC9 DC987 3022087 WP MLG BACKED OUT A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 755RA 49727 ON TAKEOFF ROLL, APPROX 60 KNOTS WHEEL NOT TURNING LIGHT ILLUMINATED AFTER RETURNING TO TAXI SPEED THE LIGHT WENT OUT. R EMOVED NR 1 WHEEL HUB CAP FOUND TRANSDUCER PINS BACKED OUT. REPLACED PINS BIT CHECK NORMAL OF ANTI-SKID CONTROLLER. (M ) 2 L 7 2 4F RT A6WE 1998032600881 19980326 00881 WP 1998 3 26 ORJA9828 1 19980219 A 3350 6011779 POWER PACK DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 EMERGENCY EXIT LIGHT INOP AT LEFT FORWARD MIDDLE EXIT DOOR. REMOVED AND REPLACED EMERGENCY EXIT POWER PACK, OPS CHECK O K. (M) 2 L 7 2 4F RT A6WE 1998032600882 19980326 00882 WP 1998 3 26 ORJA9833 1 19980228 A 3350 6011779 POWER SUPPLY DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHTS POWER SUPPLY. OPS CEHCK GOOD PER MM. ( M) 2 L 7 2 4F RT A6WE 1998032600883 19980326 00883 WP 1998 3 26 ORJA9835 1 19980302 A 3350 59306431 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 EMERGENCY LIGHTS AT AFT AIRSTAIR WALKWAY INOP. INSTALLED NEW BATTERIES IN CHARGER, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998032600884 19980326 00884 WP 1998 3 26 ORJA9836 1 19980301 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS OUT ROW 6DEF AND 30DEF INOP. RECONNECTED BROKEN WIRES, OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1998032600885 19980326 00885 WP 1998 3 26 ORJA9837 1 19980302 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN DISCONNECTED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 EMERGENCY LIGHTS AT SEAT 9DEF WILL NOT ILLUMINATE. RECONNECTED BROKEN WIRE, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998032600886 19980326 00886 WP 1998 3 26 TWAA9803306 1 19980302 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-266 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING MAJOR MAINTENANCE CHECK, NR 4 CABIN CHAIR TRACK CORROSION WAS OUT OF LIMITS AFTER CLEAN UP. REPLACED FLOOR TRACK FROM STATION 200 TO 266 PER SRM 51-01 PAGE 1 ITEM C AND STANDARD PROCEDURES. (M) 2 L 7 2 4F A6WE 1998032600887 19980326 00887 NM 1998 3 26 TWAA9803304 1 19980308 A 3350 S106CD BATTERY BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54345 21632 STL - DURING ROUTINE OVERNIGHT MAINTENANCE, THE EMERGENCY OVERHEAD LIGHT IN AISLE AT ROW 22 WAS FOUND INOPERATIVE. REPL ACED BATTERIES. (M) 2 L 7 3 4F A3WE 1998032600888 19980326 00888 NM 1998 3 26 TWAA9803303 1 19980309 A 3350 900835A BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54345 21632 STL - DURING ROUTINE OVERNIGHT MAINTENANCE, THE EMERGENCY EXIT OVERHEAD SIGN IN FIRST CLASS, AND THE EMERGENCY EXIT SIGN AT THE FWD ENTRY WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK. (M) 2 L 7 3 4F A3WE 1998032600889 19980326 00889 WP 1998 3 26 TWAA9803302 1 19980306 A 3350 58222 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 416EA 47751 STL - FLT 651 - EGRESS LIGHTS WERE FOUND INOPERATIVE IN THE AFT SECTION OF FIRST CLASS AND THE FORWARD SECTION OF COACH. REPLACED EMERGENCY LIGHT POWER SUPPLY FOR EGRESS LIGHTS AT ROW 6. (M) 2 L 7 2 4F RT A6WE 1998032600890 19980326 00890 WP 1998 3 26 TWAA9803301 1 19980306 A 4930 3812761 APU DOUG DC9 DC982 3022082 WP APU COMP MALFUNCTIONED A TWAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 05 911TW 30281 49182 MCI - FLT 123 - THE APU QUIT IN-FLIGHT WITH THE LEFT ENGINE GENERATOR ALREADY DEFERRED INOPERATIVE PER MEL. MADE UNSCHE UDLED LANDING AT MCI. CORRECTED LT ENGINE GENERATOR BY REPLACING THE GENERATOR AND CSD. DEFERRED THE APU INOPERATIVE P ER MEL. CHECK-C 9-19-97 MCI. S/D. THE GENERATOR WAS FOUND WITH A BROKEN LEAD ON THE MAIN ROTOR. THE CSD GOVERNOR SUP PORT BUSHINGS AND SHAFT WERE FOUND WORN. THE APU TESTED NORMAL, NO PROBLEM WAS FOUND. (X) 2 L 7 2 4F A6WE 1998032600891 19980326 00891 NM 1998 3 26 TWAA9803204 1 19980305 A 3411 65594576 PITOT LINE BOEING 727 727231 1384079 NM VERT STAB BROKEN A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 54333 20460 STL - FLT 141 - ELEVATOR FEEL DIFFERENTIAL LIGHT CAME ON STEADY. RETURNED TO STL. REPLACED BROKEN PITOT LINE GOING TO ELEVATOR FEEL LOCATED IN BAY FIVE OF VERTICAL STABILIZER. (M) 2 L 7 3 4F A3WE 1998032600892 19980326 00892 WP 1998 3 26 TWAA9803203 1 19980305 A 5610 5912290502 WINDSHIELD DOUG DC9 DC931 3022065 WP RT COCKPIT SHATTERED A TWAA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 05 982PS 47251 SDF - FLT 697 - FIRST OFFICERS WINDSHIELD SHATTERED INFLIGHT. MADE UNSCHEDULED LANDING AT ADF. REPLACED WINDSHIELD AND HEAT CONTROLLER. (M) 2 L 7 2 4F A6WE 1998032600893 19980326 00893 WP 1998 3 26 TWAA9803202 1 19980305 A 3350 LIGHTS DOUG DC9 DC982 3022082 WP CABIN MALFUNCTIONED A TWAA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 05 916TW 49187 STL - FLT 98 - RETURN FROM TAXI, THE EMERGENCY LIGHTS CAME ON WITH SWITCH IN ARM POSITION. MAINTENANCE PERFORMED AN OPE RATIONAL CHECK PER MM 33-51-00. OPERATION WAS NORMAL. UNABLE TO DUPLICATE. (M) 2 L 7 2 4F A6WE 1998032600894 19980326 00894 NE 1998 3 26 TWAA9803201 2 19980305 A 7250 798172 VANE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217 52053 NE LT ENGINE DAMAGED A TWAA A UNSCHED LANDING J T Y WARNING INDICATION ENGINE CASE PENETRATION ENGINE STOPPAGE CL CLIMB 1 CE 05 9306T 49567 1222 LAX - FLT 467 - AT APPROX 2000 FT LEFT ENGINE FAILED. RETURNED LAX. MADE SMOOTH OVERWEIGHT LANDING. FOUND TURBINE FAI LURE INCLUDING LOSS OF TAIL CONE. CHANGED ENGINE. CHECK-C 3-15-97. EXAMINATION OF ENGINE FOUND ONE T2 VANE FRETTED TH ROUGH INNER SHROUD AND RUBBED ON T3 BLADES UNTIL ONE BLADE FAILED. THE DAMAGE WAS REPAIRED. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1998032600895 19980326 00895 WP 1998 3 26 USAAD98034 1 19980225 A 4990 OIL SYSTEM DOUG DC9 DC981 3022081 WP APU REQ'D SERVICE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 814US 48094 AFTER TAKEOFF, THE SMOKE DETECTORS SOUNDED AND THERE WAS A STRONG SMELL OF SMOKE, HOWEVER NO SMOKE WAS VISIBLE IN THE CA BIN. THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE APU OIL QTY LOW. THE APU WA S MEL'D AND THE AIRCRAFT DISPATCHED. LATER, AFTER SERVICING THE APU OIL AND OPERATING THE AIR CONDITIONING PACKS FROM T HE APU NO DEFECTS WERE NOTED. THERE HAVE BEEN NO FURTHER REPORTS OF ODORS IN THE CABIN. (M) 2 L 7 2 4F A6WE 1998032600896 19980326 00896 WP 1998 3 26 USAAD98036 1 19980228 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M) 2 L 7 2 4F A6WE 1998032600897 19980326 00897 WP 1998 3 26 USAAD98037 1 19980227 A 3350 8732030153 CONTROL MODULE DOUG DC9 DC981 3022081 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT CONTROL MODULE. (M ) 2 L 7 2 4F A6WE 1998032600898 19980326 00898 WP 1998 3 26 USAAD98035 1 19980228 A 3350 6011777LB POWER SUPPLY DOUG DC9 DC931 3022065 WP RT NACELLE FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 993VJ 47332 THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT POWER SUPPLY AND BATTERY. (M) 2 L 7 2 4F A6WE 1998032600899 19980326 00899 WP 1998 3 26 98ZZZM334 1 19980228 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 993VJ 47332 THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT POWER SUPPLY AND BATTERY. (M) 2 L 7 2 4F A6WE 1998032600900 19980326 00900 EU 1998 3 26 USAA980051 1 19980301 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU FUSELAGE DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 887US 15777 11349 PIT - DURING Q-1 CHECK, FOUND RT SKIN DELAMINATION AND SIGNS OF DISCOLORATION BETWEEN FRAMES 23011 AND 24611 AT STRINGER 53. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR 12 INCH BY 8 INCH PER US AIRWAYS EA 29352A. (M) 2 L 7 2 4F RT 1998032600901 19980326 00901 EU 1998 3 26 USAAF98024 1 19980228 A 2160 32898981 TEMP CNTRL VALVE FOKKER F28 F28MK0100 4990807 EU RT PACK FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 883US 16267 11337 FLT 1773 - CLT - SHORTLY AFTER TAKEOFF FROM CLT, THE AIR CONDITIONING CABIN SUPPLY TEMPERATURE REACHED 134 F. CREW CYCL ED THE PACK ON AND OFF. HIGH CABIN SUPPLY TEMP STILL EXISTED. SINCE THE LEFT AIR CONDITIONING PACK WAS ON MEL, THE FLI GHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED LEFT PRSOV AND REPLACED THE RIGHT TEMPERA TURE CONTROL VALVE. (M) 2 L 7 2 4F RT 1998032600902 19980326 00902 EU 1998 3 26 USAAF98023 1 19980228 A 3260 SENSOR FOKKER F28 F28MK0100 4990807 EU LANDING GEAR OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 866US 11310 FLT 533 - GSO - AFTER TAKEOFF FROM GSO, CREW WAS UNABLE TO RETRACT THE LANDING GEAR. MANUAL OVERRIDE GEAR RETRACTION WA S SUCCESSFUL. AT APPROXIMATELY 8000 FT THE FOLLOWING MESSAGES APPEARED ON THE MULTI-FUNCTION DISPLAY 'GND/FLT CONTROL', 'L/D FAULT', AND 'TCAS FAULT'. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO GSO. FLIGHT LANDED WITHOUT FURTHER I NCIDENT. UPON LANDING, ALL FAULT MESSAGES EXTINGUISHED. MAINTENANCE PSEU TEST REVEALED THE 3LH PROXIMITY GND/FLT SENSO R READS FAR/OFF. MAINTENANCE ADJUSTED THE 3LH SENSOR. GEAR SWING WAS NORMAL. (M) 2 L 7 2 4F RT 1998032600903 19980326 00903 WP 1998 3 26 CALA9800573 1 19980324 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG FLAT A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 34838 49634 THE NOSE GEAR INDICATED UNSAFE WITH GEAR HANDLE UP AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITH OUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT FLAT. THE NOSE STRUT WAS SERVICED WITH FLUID AND NITROGEN. IN ADDITION , THE NOSE STRUT SEALS WERE REPLACED IAW MM 32-21-02. THE NOSE GEAR WAS SWUNG SEVERAL TIMES AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998032600904 19980326 00904 NM 1998 3 26 UPS98226174 1 19980325 A 3350 1000679 BATTERY PACK BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE-N/A, INOP EMERGENCY EXIT LIGHT OVER CREW ENTRY DOOR. INSTALLED SERVICEABLE FWD ENTRY DOOR EMER EXIT LIG HT ASSY, BATTERIES TEST GOOD. 2 L 7 3 4F A3WE 1998032600905 19980326 00905 NM 1998 3 26 UPS98226176 1 19980325 A 3350 1000677 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE-N/A, FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED L1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1998032600906 19980326 00906 NM 1998 3 26 UPS98226177 1 19980325 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933UP 19857 INSPECTION TYPE-N/A, COCKPIT EMERGENCY EXIT LIGHT INOP. FOUND BOTH BATTERIES TO BE DEAD AND OUT OF DATE. REMOVED AND R EPLACED TWO BATTERIES PER MM33-50-10. SYSTEM GROUND CHECKS GOOD. 2 L 7 3 4F A3WE 1998032600907 19980326 00907 WP 1998 3 26 UPS98826173 1 19980324 A 5320 SUPPORT FRAME DOUG DC8 DC871F 302199D WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-N/A, STEP PLATE SUPPORT FRAME IS CRACKED IN 3 PLACES AT NR 4 PIT DOOR OPENED FOR OTHER MAINT, SEE CONTRO L ITEM UPS98826172. TRANS TO N\R CARD 75992. FABRICATED NEW CHANNEL SUPPORT FRAME AND INSTALLED PER SRM 53-1-0 COMPLET ED NON-ROUTINE 725592. 2 L 7 4 4F RT 4A25 1998032600908 19980326 00908 EU 1998 3 26 WWMA9800061 1 19980323 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA F ACTIVATE FIRE EXT. N FALSE WARNING LD LANDING 1 WP 15 320AE 340B320 CARGO SMOKE LIGHT CAME ON, DISCHARGED THE NR 1 CARGO FIRE BOTTLE. REPLACED THE NR 1 CARGO FIRE BOTTLE AND THE FWD AND A FT CARGO SMOKE DETECTORS. 2 L 7 2 4T RT A52EU 1998032600909 19980326 00909 EU 1998 3 26 WWMA9800060 1 19980323 A 5210 551743 COVER SAAB SF340 340B 7860101 EU CABIN DOOR DAMAGED A WWMA K NONE O OTHER TX TAXI/GRND HDL 1 WP 15 345SB 340B345 THE MAIN CABIN DOOR JAMMED IN PARTIAL OPEN/CLOSED POSITION, COULD NOT FULLY CLOSE OR OPEN THE DOOR. FOUND THE INSIDE UP PER DOOR COVER ASSY BENT AND JAMMED IN THE DOOR. REPLACED THE COVER ASSY. 2 L 7 2 4T RT A52EU 1998032600910 19980326 00910 WP 1998 3 26 MWEA98374 1 19980320 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 204ME 47680 THE GALLEY SLIDE CAME UNATTACHED UPON ARRIVAL. MTC REINSTALLED GALLEY SLIDE. 2 L 7 2 4F A6WE 1998032600911 19980326 00911 NM 1998 3 26 VNAA9803024 1 19980321 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP FAILED A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 459PS 68162 3070 THE RIGHT HAND PROPELLER FAILED TO COME OUT OF FEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE I NSPECTED AND REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. LEA K AND OPERATION CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998032600912 19980326 00912 WP 1998 3 26 CKSA98104 1 19980228 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 345 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-CHECK INSPECTION, FOUND SKIN TORN AT FS 345 LONG 30RT. REMOVED DAMAGE, FABRICATED REPAIR FILLER AND DO UBLERS. LOCATED PICKUP EXISTING ATTACHMENTS. TRIM AND COUNTERSINK REPAIR DOUBLERS AND INSTALLED DOUBLERS IAW COTNEY D WG NBR D99-R02. NON-ROUTINE NR 04432 TASK NR N0005. 2 L 7 4 4F 4A25 1998032600913 19980326 00913 WP 1998 3 26 CKSA98105 1 19980228 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 130-158 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-CHECK INSPECTION, FOUND 2 DENTS ON FUSE SKIN STA 130 TO 135 AT LONG 28 LT. SKIN DAMAGED LEFT SIDE STA 131 TO STA 158 JUST ABOVE LONG 28 LT HOLE 2.5 X 1.0 WITH GOUGE 27 EXTENDING AFT. REPAIRED TWO DENTS IAW COTNEY ENGINEER ING DWG D99-R03 REV B AT STA 130 TO 135 AT LONG 28 LT AND REPAIRED SKIN DAMAGE LT SIDE STA 131 TO STA 158 ABOVE LONG 28 LT IAW COTNEY ENG DWG D99-R03 REV B. NON ROUTINE NR 04460 AND 04428 TASK NR N0007. 2 L 7 4 4F 4A25 1998032600914 19980326 00914 WP 1998 3 26 CKSA98106 1 19980228 A 5313 STRINGER DOUG DC8 DC863F 302198F WP BS 1100 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON STRINGER FS 1100 ON TOP AT LONG 36. CORROSION RE MOVAL OUT OF LIMITS IAW DC8 SRM 53-2-0, FIG 1F. FAB REPAIR AND INSTALLED ON FRAME STA 1100 IAW DC8 SRM 53-2-0 PAGE 5/6 FIG 2. FAB REPAIR AND INSTALLED BELT FRAME AT STA 1100 IAW COTNEY DRAWING D93-R21. CORROSION TASK CARD NUMBER 5590-055 1. NON-ROUTINE NR 04618 TASK NR X0048. 2 L 7 4 4F 4A25 1998032600915 19980326 00915 WP 1998 3 26 CKSA98107 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1040 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND CORROSION AND GOUGE ON LT FRAME AT FS 1040 AT UPPER CUSP AREA. REMOVED CORROSION IAW DC8 SRM 53-20-0 FIG 1F. REMOVAL IS WITHIN (.002) LIMITS IAW DC8 SRM 53-2-0 FIG 1F. TREATED AND PRIMED IAW DC8 SRM 51-1-8 AND FABRICATED DOUBLER IAW COTNEY DWG NR D93-R05, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NR 573L-0551. NON-ROUTINE NR 04825 TASK NR X0061. 2 L 7 4 4F 4A25 1998032600916 19980326 00916 WP 1998 3 26 CKSA98108 1 19980228 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 350 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-CHECK INSPECTION, FOUND SUSPECTED CORROSION BULGE AT FS 350 BETWEEN LONG 26 TO 27 RT ON OUTER SKIN. RE MOVED CORROSION IAW DC8 SRM 51-1-8. CORROSION REMOVAL BEYOND LIMITS. REMOVED DISCREPANT SKIN PLATING. CUT OUT DAMAGED AREA, FABRICATED, TRIMMED, DRILLED, ALODINED, PRIMED, AND INSTALLED FILLERS AND DOUBLERS IAW COTNEY DWG D93-R56, DC8 SR M 51-1-8, 51-1-16, 51-1-21, 51-1-20D, 53-2-0 FIG 1F. NON-ROUTINE NR 05100 TASK NR X0075. 2 L 7 4 4F 4A25 1998032600917 19980326 00917 WP 1998 3 26 CKSA98109 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 880 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND PREVIOUS CORROSION BLEND ON RT FRAME AT FS 880 STILL SHOWS CORROSION. CORROSION B EYOND LIMITS. REMOVED AND REPLACED FRAME SEGMENT IAW DC8 SRM 53-3-0, 51-3-0 AND 51-1-20D. CORROSION TASK CARD NUMBER 5 73R-0551. NON-ROUTINE NR 04795 TASK NR Y1254. 2 L 7 4 4F 4A25 1998032600918 19980326 00918 WP 1998 3 26 CKSA98110 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1060 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1060 AT UPPER CUSP AREA. FABRICATED ANG LE AND SHIM IAW D93-R07 LT SIDE FRAME FS 1060 LT SIDE. INSTALLED ANGLE AND SHIM, FABRICATED FOR LT SIDE FRAME STA 1060 IAW COTNEY DWG D93-R07. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04826 TASK NR Y1278. 2 L 7 4 4F 4A25 1998032600919 19980326 00919 WP 1998 3 26 CKSA98111 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1580 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1580 AT UPPER CUSP AREA. PLUGGED MISDRI LLED HOLES ON FS 1580 LT AT APPROX CUSP AREA. FABRICATED REPAIR DOUBLER IAW COTNEY DWG NR D93-R13. HEAT TREATED IAW DC 8 SRM 51-1-1. TREATED AND PRIMED DOUBLER AND FILLER IAW DC8 SRM 51-1-8. INSTALLED FILLER AND DOUBLER IAW COTNEY DWG NR D93-R13 AND DC8 SRM 51-1-21 AND 51-1-20D. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04833 TASK NR Y1283. 2 L 7 4 4F 4A25 1998032600920 19980326 00920 WP 1998 3 26 CKSA98112 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 500 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 500, 5.5 ABOVE UPPER CUSP AREA. FAB AND INSTALLED REPAIR IAW COTNEY DWG NR D93-R10, FABRICATED REPAIR ANGLE, LOCATED, ADDED FAST ATTACHMENTS, PICK-UP EXISTING ATTACHMENTS. TREATED AND PRIMED REPAIR ANGLE AND FRAME AFFECTED AREA. INSTALLED REPAIR IAW COTNEY DWG NR D93-R10. COR ROSION TASK CARD NR 573R-0551. NON-ROUTINE NR 04875 TASK NR Y1296. 2 L 7 4 4F 4A25 1998032600921 19980326 00921 WP 1998 3 26 CKSA98113 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 540 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 540, 5.5 ABOVE UPPER CUSP AREA. PLUGGED HOLES, FAB AND DRILLED ANGLE DOUBLER AND SHIM IAW COTNEY SKETCH NR D93-R14 AT FS 540 RT 5.5 ABOVE UPPER CUSP. TREATED, PRIMED AND INSTALLED IAW COTNEY SKETCH NR D93-R14. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04876 TASK NR Y1297. 2 L 7 4 4F 4A25 1998032600922 19980326 00922 WP 1998 3 26 CKSA98114 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 940 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 940, 5.5 ABOVE UPPER CUSP AREA. FABRICA TED AND FORMED REPAIR ANGLES FOR REPAIR AT FS 940 RT 5.5 ABOVE UPPER CUSP AND HEAT TREATED IAW DC8 SRM 51-1-1 AND COTNEY DWG NR D93-R36. FAB 2 NEW GUSSETTS AND ANGLE, OUTER STRAP AND SHIMS. DRILLED AND DEBURRED FRAME AND PARTS, PLUGGED BA D HOLES AND SMOOTHED OUT DAMAGED AREA IAW COTNEY DWG NR D93-R36. TREATED, PRIMED, SEALED AND INSTALLED REPAIRS AT FS 94 0 LT 5.5 ABOVE UPPER CUSP AREA IAW COTNEY DWG NR D93-R36. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04878 T ASK NR Y1299. 2 L 7 4 4F 4A25 1998032600923 19980326 00923 WP 1998 3 26 CKSA98115 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 940 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 940, 5.5 ABOVE UPPER CUSP AREA. FABRICA TED AND FORMED REPAIR ANGLES FOR REPAIR AT FS 940 RT 5.5 ABOVE UPPER CUSP AND HEAT TREATED IAW DC8 SRM 51-1-1 AND COTNEY DWG NR D93-R36. FAB 2 NEW GUSSETTS AND ANGLE, OUTER STRAP AND SHIMS. DRILLED AND DEBURRED FRAME AND PARTS, PLUGGED BA D HOLES AND SMOOTHED OUT DAMAGED AREA IAW COTNEY DWG NR D93-R36. TREATED, PRIMED, SEALED AND INSTALLED REPAIRS AT FS 94 0 LT 5.5 ABOVE UPPER CUSP AREA IAW COTNEY DWG NR D93-R36. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04878 T ASK NR Y1299. 2 L 7 4 4F 4A25 1998032600924 19980326 00924 WP 1998 3 26 CKSA98116 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 980 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 980 5.5 ABOVE UPPER CUSP AREA. FABRICAT ED, DRILLED HOLES, PLUGGED HOLES, TREATED AND PRIMED AND INSTALLED DOUBLER IAW COTNEY DWG D93-R47. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04880 TASK NR Y1301. 2 L 7 4 4F 4A25 1998032600925 19980326 00925 WP 1998 3 26 CKSA98117 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1000 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1000, 5.5 ABOVE UPPER CUSP AREA. FABRIC ATED REPAIR IAW COTNEY D93-R46 FROM 7075.0 HEAT TREATED 7075-T6 .071. TREATED AND PRIMED REPAIR. INSTALLED SAME INSTAL LED INTERCOSTAL SHIM WITH CLIPS AT STA 1000, R5.5 ABOVE UPPER CUSP IAW COTNEY D93-R46, DC8 SRM 51-1-1, 51-1-21 AND 51-1- 20D. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04881 TASK NR Y1302. 2 L 7 4 4F 4A25 1998032600926 19980326 00926 WP 1998 3 26 CKSA98118 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1020 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1020, 5.5 ABOVE UPPER CUSP AREA. FABRIC ATED REPAIR SHIM AND ANGLE AS REQUIRED BY COTNEY D93-R54 AT FS 1020. HEAT TREATED TO 7075.T6 FROM 7075.0 AGED, PRIMED A ND INSTALLED IAW COTNEY D93-R54. FORMED AND HEATED PARTS IAW DC8 SRM 51-1-1, TREATED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FASTENERS IAW DC8 SRM 51-1-21 AND 51-1-20D. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE 04882 TASK NR Y 1303. 2 L 7 4 4F 4A25 1998032600927 19980326 00927 WP 1998 3 26 CKSA98119 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1140 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1140, 5.5 ABOVE UPPER CUSP AREA. PLUGGE D SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1140, 5.5 ABOVE UPPER CUSP AREA. FABRICATED, LOCATED, DRILLED, ADDED FASTEN ERS AS REQUIRED, DEBURRED, AND TREATED REPAIR ANGLE AND SHIMS. INSTALLED REPAIR ANGLE AND SHIMS IAW DC8 SRM 51-1-8, 51- 1-20D, 51-1-21 AND COTNEY ENGINEERING SKETCH NR D93-R55. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04883 TA SK NR Y1304. 2 L 7 4 4F 4A25 1998032600928 19980326 00928 WP 1998 3 26 CKSA98120 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1160 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1160, 5.5 ABOVE UPPER CUSP AREA. FABRIC ATED PARTS, HEAT TREATED, AGED, FORMED, TREATED AND PRIMED AND INSTALLED PARTS IAW COTNEY DWG NR D93-R57. FORMED AND HE AT TREATED PARTS IAW DC8 SRM 51-1-1. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FASTENERS IAW DC8 SRM 51-1-21, 5 1-1-20D. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04884 TASK NR Y1305. 2 L 7 4 4F 4A25 1998032600929 19980326 00929 WP 1998 3 26 CKSA98121 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1360 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1360, 5.5 ABOVE UPPER CUSP AREA. FABRIC ATED REPAIR ANGLE AND SHIMS DRILLED AND DEBURRED FRAME AND PARTS AND TRIMMED OUT DAMAGE IAW COTNEY DWG NR D93-R58. HEAT TREATED REPAIR ANGLE IAW DC8 SRM 51-1-1. TREATED, PRIMED, SEALED AND INSTALLED REPAIR ON FRAME AT FS 1360 RT 5.5 ABOVE UPPER CUSP AREA IAW COTNEY DWG NR D93-R58 AND 51-1-21 AND 51-1-20D. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04885 TASK NR Y1306. 2 L 7 4 4F 4A25 1998032600930 19980326 00930 WP 1998 3 26 CKSA98122 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1380 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1380, 5.5 ABOVE UPPER CUSP AREA. FABRIC ATED REPAIR ANGLE AND FILLER DOUBLER. ALODINED AND PRIMED. INSTALLED ANGLE AND FILLER IAW COTNEY DWG D93-R59 ON FRAME AT FS 1380 RT, 5.5 ABOVE CUSP. FORMED AND HEAT TREATED IAW DC8 SRM 51-1-1. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INS TALLED FASTENERS IAW DC8 SRM 51-1-21 AND 51-1-20D. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04886 TASK NR Y1307. 2 L 7 4 4F 4A25 1998032600931 19980326 00931 WP 1998 3 26 CKSA98123 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1400 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1400, 5.5 ABOVE UPPER CUSP AREA. FABRIC ATED REPAIR ANGLE AND FILLER, TREATED AND PRIMED. INSTALLED ANGLE AND FILLER IAW COTNEY DWG NR D93-R60 ON FRAME AT FS 1 400 R 5.5 ABOVE CUSP. HEAT TREATED PART IAW DC8 SRM 51-1-8, TREATED AND PAINTED IAW DC8 SRM 51-1-8, INSTALLED FASTENERS IAW DC8 SRM 51-1-21 AND 51-1-20D. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04887 TASK NR Y1308. 2 L 7 4 4F 4A25 1998032600932 19980326 00932 WP 1998 3 26 CKSA98124 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1420 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1420, 5.5 ABOVE UPPER CUSP AREA. PLUGGE D 2 HOLES IN FRAME AT FS 1420, FABRICATED ANGLE REPAIR AND NECESSARY SHIMS, LOCATED REPAIR ANGLE AND SHIMS, PICKED UP EX ISTING HOLES AND ADDED AS REQUIRED, DEBURRED, TREATED AND PRIMED REPAIR ANGLE, SHIMS, AND FRAME AS REQUIRED. INSTALLED REPAIR IAW DC8 SRM 51-1-8, 51-1-20D AND COTNEY ENGINEERING SKETCH NR D93-R45. CORROSION TASK CARD NUMBER 573R-0551. NO N-ROUTINE NR 04888 TASK NR Y1309. 2 L 7 4 4F 4A25 1998032600933 19980326 00933 WP 1998 3 26 CKSA98125 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1440 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1440, 5.5 ABOVE UPPER CUSP AREA. TRIMME D OUT MISDRILLED HOLES, FABRICATED DOUBLERS AND SHIMS IAW COTNEY DWG NBR D93-R71. TREATED AND PRIMED IAW DC8 SRM 51-1-8 , INSTALLED DOUBLER AND SHIMS IAW DC8 SRM 51-1-21. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04889 TASK NR Y1310. 2 L 7 4 4F 4A25 1998032600934 19980326 00934 WP 1998 3 26 CKSA98126 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1480 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT RADIUS AT FS 1480, 6, 12, 28, 36 AND 45 ABO VE UPPER CUSP AREA. FABRICATED AND INSTALLED REPAIRS TO FS 1480 RT FRAME IAW COTNEY DWG D93-R63, DC8 SRM 51-1-21, 51-1- 20D, 51-1-8, 51-1-16, 51-1-1. HEAT TREATED AND AGED REPAIR ANGLES. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04890 TASK NR Y1311. 2 L 7 4 4F 4A25 1998032600935 19980326 00935 WP 1998 3 26 CKSA98127 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1500 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND HOLES DRILLED ON RADIUS OF RT FRAME AT FS 1500, 20 AND 28 ABOVE UPPER CUSP AREA AN D GOUGES ON RT FRAME AT 5, 12 AND 20 ABOVE UPPER CUSP AREA. FABRICATED PARTS FOR HOLES DRILLED ON RADIUS OF RT FRAME AT FS 1500 IAW COTNEY DWG NBR D93-R53. TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED PARTS IAW COTNEY DWG NR D9 3-R53. GOUGE BURNISHED SMOOTH IAW COTNEY DWG NR D93-R53. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04891 T ASK NR Y1312. 2 L 7 4 4F 4A25 1998032600936 19980326 00936 WP 1998 3 26 CKSA98128 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1520 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1520, 5 ABOVE UPPER CUSP AREA. BLENDED OUT SHARP EDGES, TRIMMED DAMAGED HOLE FABRICATED DOUBLER AND SHIMS IAW COTNEY DWG D93-R64. TREATED AND PRIMED IAW DC8 S RM 51-1-8 AND INSTALLED REPAIR IAW COTNEY DWG D93-R64. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04892 TASK NR Y1313. 2 L 7 4 4F 4A25 1998032600937 19980326 00937 WP 1998 3 26 CKSA98129 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1560 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1560, 5, 8 AND 13 ABOVE UPPER CUSP AREA. RT FRAME REPAIRED AT FS 1560, 5, 8 AND 13 ABOVE UPPER CUSP AREA IAW COTNEY DWG NR D93-R62, DC8 SRM 51-1-20D, 51-9-0, 5 1-1-21 PG 9. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04893 TASK NR Y1314. 2 L 7 4 4F 4A25 1998032600938 19980326 00938 WP 1998 3 26 CKSA98130 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1580 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 1580, 8 ABOVE UPPER CUSP AREA. PLUGGED MISDRILLED HOLES, FABRICATED DOUBLER IAW COTNEY DWG NR D93-R61, TREATED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-21. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04894 TASK NR Y1315. 2 L 7 4 4F 4A25 1998032600939 19980326 00939 WP 1998 3 26 CKSA98131 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 500 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 500, 5 FROM UPPER CUSP AND 12 AND 20 ON RADIUS FROM UPPER CUSP AREA. REMOVED FASTENERS NECESSARY TO INSTALL REPAIR ON LT FRAME STA 500 AT CUSP. FABRICATED ANG LE REPAIR, PICKED UP EXISTING FASTENERS AND ADDED FASTENERS AS REQUIRED. TRIMMED, DEBURRED, TREATED AND PRIMED ANGLE. I NSTALLED FILLER AND REPAIR ANGLE IAW COTNEY DWG NR D93-R17 AND DC8 SRM 51-1-8, 51-1-21, 51-1-20D. CORROSION TASK CARD N UMBER 573L-0551. NON-ROUTINE NR 04895 TASK NR Y1384. 2 L 7 4 4F 4A25 1998032600940 19980326 00940 WP 1998 3 26 CKSA98132 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 520 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 520, 5 ABOVE UPPER CUSP AREA AND ON RADI US AT 12 ABOVE UPPER CUSP AREA. FABRICATED REPAIR ANGLE AND SHIMS, DRILLED, ALODINED, PRIMED, SEALED AND INSTALLED REPA IR ON LT FRAME FS 520 IAW COTNEY DWG NR D93-R18, DC8 SRM 51-1-21, 51-1-8, 51-1-16. PLUGGED 2 HOLES 5 ABOVE CUSP IAW CO TNEY DWG NR D93-R18, DC8 SRM 51-1-21. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04896 TASK NR Y1385. 2 L 7 4 4F 4A25 1998032600941 19980326 00941 WP 1998 3 26 CKSA98133 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 540 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 540, 5, 12 AND 20 ABOVE UPPER CUS P AREA. REMOVED EXISTING FASTENERS TO BE USED IN REPAIR. PLUGGED 4 MISDRILLED HOLES. FABRICATED REPAIR ANGLE AND SHI MS AS REQUIRED. LOCATED REPAIR ANGLE AND SHIMS AND DRILLED, DEBURRED, TREATED AND PRIMED REPAIR ANGLE AND SHIMS. INSTA LLED REPAIR ANGLE AND SHIMS IAW COTNEY ENGINEERING SKETCH NR D93-R03, DC8 SRM 51-1-8, 51-1-20D, 51-1-21. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04897 TASK NR Y1386. 2 L 7 4 4F 4A25 1998032600942 19980326 00942 WP 1998 3 26 CKSA98134 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 560 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED ON LT FRAME AT FS 560, 5 ABOVE UPPER CUSP AREA AND ON RADIUS OF LT FRAME, 20 ABOVE UPPER CUSP AREA. FORMED AND HEAT TREATED PARTS ANGLE -1 IAW DC8 SRM 51-1-1 AND DWG D93-R04. FAB RICATED SHIMS AND STRAP INSTALLED PLUG RIVETS IAW COTNEY DWG D93-R04. TREATED AND PRIMED PARTS FOR REPAIR IAW DC8 SRM 5 1-1-8. INSTALLED REPAIR IAW DWG D93-R04 AND DC8 SRM 51-1-21. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 048 98 TASK NR Y1387. 2 L 7 4 4F 4A25 1998032600943 19980326 00943 WP 1998 3 26 CKSA98135 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 320 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 320, 4, 8 AND 12 ABOVE UPPER CUSP AREA. FABRICATED REPAIR PARTS FOR HOLES IN FRAME AT STA 320 IAW COTNEY DWG NR D93-R19. TREATED AND PRIMED PARTS IAW D C8 SRM 51-1-8, INSTALLED PARTS IAW COTNEY DWG NR D93-R19. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04899 T ASK NR Y1388. 2 L 7 4 4F 4A25 1998032600944 19980326 00944 WP 1998 3 26 CKSA98136 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 340 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 340, 5 ABOVE UPPER CUSP AREA. INSTALLED RIVETS IN MISDRILLED HOLES IN RADIUS IAW DC8 SRM 51-1-21, FABRICATED DOUBLER AND SHIM IAW COTNEY DWG NR D93-R11, TREATE D AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED DOUBLER AND SHIM IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 573L-05 51. NON-ROUTINE NR 04900 TASK NR Y1389. 2 L 7 4 4F 4A25 1998032600945 19980326 00945 WP 1998 3 26 CKSA98137 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 360 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 360, 5 AND 10 ABOVE UPPER CUSP AR EA. INSTALLED RIVETS IN MISDRILLED HOLES IN RADIUS IAW DC8 SRM 51-1-21, FABRICATED DOUBLER AND SHIM IAW COTNEY DWG NR D 93-R08, TREATED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED DOUBLER IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 57 3L-0551. NON-ROUTINE NR 04901 TASK NR Y1390. 2 L 7 4 4F 4A25 1998032600946 19980326 00946 WP 1998 3 26 CKSA98138 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 600 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 600, 5 ABOVE UPPER CUSP AREA. PLUGGED S EVERAL HOLES DRILLED INTO LT FRAME AT FS 600 5 ABOVE UPPER CUSP AREA IAW DC8 SRM 51-1-21. FABRICATED ANGLE AND SHIM IAW COTNEY DWG D99-R16 HEAT TREAT AND AGED IAW DC8 SRM 51-1-1. DEBURRED DRILLED HOLES. TREATED AND PRIMED IAW DC8 SRM 51- 1-8. INSTALLED ANGLE AND SHIM ON LT FRAME AT FS 600, 5 ABOVE UPPER CUSP AREA IAW DC8 SRM 51-1-21, 51-1-20D AND COTNEY D WG NR D93-R16. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04903 TASK NR Y1392. 2 L 7 4 4F 4A25 1998032600947 19980326 00947 WP 1998 3 26 CKSA98139 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 620 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 620, 5 AND 12 ABOVE UPPER CUSP AR EA. REMOVED CUSP FITTING AT STA 620 LT, INSPECTED FITTING FOR DAMAGE. NICK ON FITTING WAS FOUND TO BE WITHIN LIMITS IA W DC8 SRM 53-2-0. REMOVED EXISTING FASTENER TO BE USED IN FRAME REPAIR. FABRICATED, DRILLED, DEBURRED AND TREATED FRAM E REPAIR ANGLE AND SHIMS AS REQUIRED. INSTALLED ANGLE REPAIR AND SHIMS IAW COTNEY ENGINEERING SKETCH NR D93-R69 AND DC8 SRM 51-1-8, 51-1-20D, 51-1-21. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04904 TASK NR Y1393. 2 L 7 4 4F 4A25 1998032600948 19980326 00948 WP 1998 3 26 CKSA98140 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 834 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED ON LT FRAME RADIUS AT FS 834, 5 ABOVE UPPER CUSP AREA. PLUG GED MISDRILLED HOLES, FABRICATED DOUBLER AND SHIM IAW COTNEY DWG NR D93-R68. REMOVED AND REPLACED GUSSET IAW COTNEY DWG NR D93-R65, TREATED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED DOUBLER AND SHIM IAW DC8 SRM 51-1-21 HEAT TREAT IAW 51-1-1 . CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04936 TASK NR Y1394. 2 L 7 4 4F 4A25 1998032600949 19980326 00949 WP 1998 3 26 CKSA98141 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 879 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED ON LT FRAME RADIUS AT FS 879, 5 ABOVE UPPER CUSP AREA AND GO UGE ON LT FRAME, 5 ABOVE UPPER CUSP AREA. REMOVED INTERCOSTAL AT STA 879 AND AFT ATTACH ANGLE. FORMED -1 AND -2 REPAIR ANGLES IAW DC8 SRM 51-1-1, HEAT TREATED AND AGE HARDENED REPAIR ANGLES IAW DC8 SRM 51-1-1; LOCATED AND DRILLED -1 AND - 2 REPAIR ANGLES IAW DC8 SRM 51-1-20D AND DWG NR D93-R20. INSTALLED REPAIR ANGLES (-1 AND -2). REINSTALLED INTERCOSTAL PREVIOUSLY REMOVED AND NEW ATTACH ANGLE IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 049 37 TASK NR Y1395. 2 L 7 4 4F 4A25 1998032600950 19980326 00950 WP 1998 3 26 CKSA98142 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 940 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 940, 5 AND 10 ABOVE UPPER CUSP AR EA. FAB REPAIR IAW COTNEY DRAWING NR D93-R48 AND INSTALLED IAW DC8 SRM 51-1-20D AND 51-1-21. CORROSION TASK CARD NUMBE R 573L-0551. NON-ROUTINE NR 04938 TASK NR Y1396. 2 L 7 4 4F 4A25 1998032600951 19980326 00951 WP 1998 3 26 CKSA98143 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 980 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 980, 5 ABOVE UPPER CUSP AREA. PLUGGED H OLES AND SMOOTHED CORNERS IAW COTNEY DWG NR D93-R67. FABRICATED REPAIR ANGLE AND DRILLED HOLES IAW COTNEY DWG NR D93-R6 7. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLE AT STA 980 LT IAW COTNEY DWG NR D93-R67 AND DC8 SRM 5 1-1-20D. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04940 TASK NR Y1398. 2 L 7 4 4F 4A25 1998032600952 19980326 00952 WP 1998 3 26 CKSA98144 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1000 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 1000, 5 ABOVE UPPER CUSP AREA. F AB REPAIR FROM 7075 .071 FORMED AND HEAT TREATED TO 7075.T6 IAW COTNEY D93-R42 TREAT AND PRIMED IAW COTNEY DWG NR D93-R4 2. INSTALLED REPAIR IAW COTNEY DWG NR D93-R42, DC8 SRM 51-1-21 AND 51-1-8. CORROSION TASK CARD NUMBER 573L-0551. NON- ROUTINE NR 04941 TASK NR Y1399. 2 L 7 4 4F 4A25 1998032600953 19980326 00953 WP 1998 3 26 CKSA98145 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1020 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1020, 5 ABOVE UPPER CUSP AREA AND GOUGE ON LT FRAME, 5 ABOVE UPPER CUSP AREA. FAB ANGLE, HEAT TREAT AND AGE ANGLE IAW DC8 SRM 51-1-1. DRILLED ANGLE IAW COTNEY DRAWING D93-R66 TREAT AND PRIMED. INSTALLED REPAIR IAW COTNEY DRAWING D93-R66. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04943 TASK NR Y1401. 2 L 7 4 4F 4A25 1998032600954 19980326 00954 WP 1998 3 26 CKSA98146 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1140 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1140, 5 ABOVE UPPER CUSP AREA. FORMED ( -1) REPAIR ANGLE AND AGED HARDENED PART IAW DC8 SRM 51-1-1 AND COTNEY DWG NR D93-R65. ROUTED OUT DAMAGED SECTION OF FRA ME AT FS 1140 LT IAW COTNEY DWG NR D93-R65. INSTALLED REPAIR ANGLE AT FS 1140 LT IAW DC8 SRM 51-1-20D AND COTNEY DWG NR D93-R65. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04944 TASK NR Y1402. 2 L 7 4 4F 4A25 1998032600955 19980326 00955 WP 1998 3 26 CKSA98147 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1160 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED ON LT FRAME RADIUS AT FS 1160, 5 ABOVE UPPER CUSP AREA. FAB AND INSTALLED TWO REPAIRS IAW COTNEY DWG NR D93-R49 AND 51-1-8 AND 51-1-20D WHERE SEVERAL HOLES WERE DRILLED IN FRAME A T FS 1160 LT, 5 ABOVE UPPER CUSP. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04945 TASK NR Y1403. 2 L 7 4 4F 4A25 1998032600956 19980326 00956 WP 1998 3 26 CKSA98148 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1180 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 1180, 5, 22, 30 AND 40 ABOVE UPPE R CUSP AREA. FAB REPAIR FOR LT FRAME AT STA 1180, 30 TO 40 ABOVE LOWER REPAIR IAW COTNEY DWG NR D93-R43. INSTALLED REP AIR IAW DWG NR D93-R43. FAB LOWER REPAIR FOR STA 1180 FROM 5, 22. PLUGGED ALL MISDRILLED HOLES IAW COTNEY DWG NR D93-R 43. INSTALLED REPAIR IAW COTNEY DWG NR D93-R43. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04946 TASK NR Y1 404. 2 L 7 4 4F 4A25 1998032600957 19980326 00957 WP 1998 3 26 CKSA98149 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1200 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 1200, 5 AND 10 ABOVE UPPER CUSP A REA. REMOVED CLIP, GUSSET AND INTERCOSTAL FOR ACCESS FAB. REPAIR ANGLE, DRILLED AND DEBURRED ANGLE AND FRAME. HEAT TR EATED ANGLE IAW DC8 SRM 51-1-1, PLUGGED MISDRILLED HOLES. FAB NEW CLIP AND GUSSET DRILLED AND DEBURRED TREATED AND PRIM ED NEW PARTS. SEALED AND INSTALLED REPAIR ANGLE, CLIP, GUSSET AND INTERCOSTAL FOR FRAME REPAIR AT FS 1200 LT 5 AND 10 A BOVE CUSP AREA IAW COTNEY DRAWING D93-R50. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04947 TASK NR Y1405. 2 L 7 4 4F 4A25 1998032600958 19980326 00958 WP 1998 3 26 CKSA98150 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1220 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 1220, 5 ABOVE UPPER CUSP AREA. F ABRICATED STRAP FOR HOLES IN FRAME AT STA 1220 IAW COTNEY DWG D93-R44. TREATED AND PRIMED IAW 51-1-8, INSTALLED STRAP IA W COTNEY DWG D93-R44. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04948 TASK NR Y1406. 2 L 7 4 4F 4A25 1998032600959 19980326 00959 WP 1998 3 26 CKSA98151 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1240 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1240, 5 ABOVE UPPER CUSP AREA. CUT AND FITTED STRAP FOR REPAIR OF EXTRA HOLES ON LT FRAME AT FS 1240 5 ABOVE UPPER CUSP AREA. DRILLED FRAME AND STRAP FOR REPA IR DEBURRED HOLES, PLUGGED EXTRA HOLES, TREATED, PRIMED, SEALED, AND INSTALLED STRAP IAW COTNEY DWG D93-R37. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04949 TASK NR Y1407. 2 L 7 4 4F 4A25 1998032600960 19980326 00960 WP 1998 3 26 CKSA98152 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1260 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1260, 5 ABOVE UPPER CUSP AREA. FABRICAT ED AND FORMED AND DRILLED AND HEAT TREATED IAW DC8 SRM PER COTNEY DWG NR D93-R38 AND DC8 SRM 51-1-1. TREATED AND PRIMED AND INSTALLED WITH HI LOC IAW DC8 SRM 51-1-8 AND 51-1-20D LT FRAME AT FS 1260, 5 ABOVE UPPER CUSP AREA. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04950 TASK NR Y1408. 2 L 7 4 4F 4A25 1998032600961 19980326 00961 WP 1998 3 26 CKSA98153 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1320 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED IN LT FRAME AT FS 1320, 5 ABOVE UPPER CUSP AREA AND AT LT FR AME RADIUS, 22 ABOVE UPPER CUSP AREA. REPAIRED SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1320 5 ABOVE CUSP AND LT FRAME RADIUS 22 ABOVE CUSP PER COTNEY DWG NR D93-R01. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04951 TASK NR Y1 409. 2 L 7 4 4F 4A25 1998032600962 19980326 00962 WP 1998 3 26 CKSA98154 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1340 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1340, 5 ABOVE UPPER CUSP AREA. FAB PART S FOR LT FRAME AT FS 1340 UPPER CUSP AREA IAW COTNEY DWG D93-R39 AND IAW DC8 SRM 53-2-0. TREATED AND PRIMED IAW DC8 SRM 51-1-8. PLUGGED MISDRILLED HOLES AND INSTALLED PARTS PER COTNEY DWG D93-R39 AND DC8 SRM 51-1-20 AND 51-1-20D. CORROSI ON TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04952 TASK NR Y1410. 2 L 7 4 4F 4A25 1998032600963 19980326 00963 WP 1998 3 26 CKSA98155 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1360 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1360, 5 ABOVE UPPER CUSP AREA. FABRICAT ED REPAIRS DRILLED TO FIT FRAME AT STA 1360 2 REPAIRS. PRIMED AND TREATED. INSTALLED REPAIR IAW COTNEY DRAWING D93-R34 , DC8 SRM 51-1-1 AND 51-1-8. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04953 TASK NR Y1411. 2 L 7 4 4F 4A25 1998032600964 19980326 00964 WP 1998 3 26 CKSA98156 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1380 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1380, 5 ABOVE UPPER CUSP AREA. FABRICAT ED, DRILLED, HEAT-TREATED, TREATED AND PRIMED AND INSTALLED FILLER AND SHIM ON LT FRAME AT FS 1380 IAW COTNEY DRAWING D9 3-R40 AND DC8 SRM 51-1-8 AND 51-1-21. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04954 TASK NR Y1412. 2 L 7 4 4F 4A25 1998032600965 19980326 00965 WP 1998 3 26 CKSA98157 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1420 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1420, 5 ABOVE UPPER CUSP AREA AND LT FRA ME RADIUS AT 31 AND 40 ABOVE UPPER CUSP AREA. FABRICATED 2 REPAIR FROM 7075.0 HEAT TREATED TO 7075-T6 .071 DRILL TO FIT FRAME 2 SHIM. INSTALLED DOUBLER IAW COTNEY D93-R35 - EXISTING HOLE WAS PLUGGED WITH MS20470E6-5 AT STA 1420 31 41 FRO M FLOOR IAW COTNEY D93-R35 AND DC8 SRM 51-1-21 AND 51-1-8. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04955 TASK NR Y1413. 2 L 7 4 4F 4A25 1998032600966 19980326 00966 WP 1998 3 26 CKSA98158 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1440 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1440, 5 ABOVE UPPER CUSP AREA. FABRICAT ED REPAIR PARTS FOR STA 1440 LT SIDE, 5 ABOVE CUSP AREA. DRILLED UP PARTS. TREATED AND PRIMED PARTS, INSTALLED -3 SHIM -2 ANGLE -4 SHIM -1 ANGLE -5 GUSSET IAW COTNEY DRAWING D93-R22 AND DC8 SRM 51-1-20D AND 51-1-8. CORROSION TASK CARD NUM BER 573L-0551. NON-ROUTINE NR 04956 TASK NR Y1414. 2 L 7 4 4F 4A25 1998032600967 19980326 00967 WP 1998 3 26 CKSA98159 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1460 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1460, 5 ABOVE UPPER CUSP AREA. FAB 2 RE PAIRS IAW COTNEY DWG NBR D93-R33. HEAT TREATED AND AGED REPAIR ANGLES, INSTALLED REPAIRS IAW DC8 SRM 51-1-1, 51-1-8, 51 -1-21, 51-1-20D. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04957 TASK NR Y1415. 2 L 7 4 4F 4A25 1998032600968 19980326 00968 WP 1998 3 26 CKSA98160 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1480 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1480, 5 ABOVE UPPER CUSP AREA AND ON LT FRAME RADIUS FROM 9 TO 44 ABOVE UPPER CUSP AREA. DEEP GOUGE ON LT FRAME AT FS 1480, 5 ABOVE UPPER CUSP AREA. ROUTED OU T DAMAGED AREA, DID DYE PENETRANT TEST. REMOVED FASTENERS AS NEEDED, FAB REPAIR ANGLE, SHIMS AND FILLERS DRILLED AND DE BURRED. REPAIR PARTS HEAT TREATED A, B AND C ANGLES IAW DC8 SRM 51-1-1 ON LT FRAME AT FS 1480 FROM 5 TO 44 ABOVE UPPER CUSP AREA IAW COTNEY DRAWINGS D93-R41 TREATED, PRIMED, SEALED AND INSTALLED PARTS -1 -2 AND -3 IAW COTNEY DRAWING D93-R4 1. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04958 AND 04959 TASK NR Y1416. 2 L 7 4 4F 4A25 1998032600969 19980326 00969 WP 1998 3 26 CKSA98161 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1500 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME AT FS 1500 5 ABOVE UPPER CUSP AREA. REMOVED D AMAGED AREA OF FRAME OF LT FRAME FS 1500 5 ABOVE UPPER CUSP. FAB REPAIR STRAP AND SHIM, FITTED, DRILLED, AND DEBURRED F RAME, SHIM AND STRAP IAW COTNEY DWG NR D93-R70. TREATED, PRIMED, SEALED AND INSTALLED REPAIR STRAP AND SHIM ON LT FRAME AT FS 1500 5 ABOVE CUSP IAW COTNEY DWG NR D93-R70. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04961 TASK NR Y1418. 2 L 7 4 4F 4A25 1998032600970 19980326 00970 WP 1998 3 26 CKSA98162 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1520 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED IN LT FRAME RADIUS AT FS 1520, 5 ABOVE UPPER CUSP AREA. INS TALLED RIVET IN MISDRILLED HOLE IN RADIUS IAW DC8 SRM 51-1-21, FABRICATED DOUBLER AND SHIM IAW COTNEY DRAWING NR D93-R51 , PRIME AND TREATED IAW DC8 SRM 51-1-8 AND INSTALLED DOUBLER AND SHIM IAW DC8 SRM 51-1-20D AND COTNEY DWG D93-R51. CORR OSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04962 TASK NR Y1419. 2 L 7 4 4F 4A25 1998032600971 19980326 00971 WP 1998 3 26 CKSA98163 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1540 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO LT FRAME RADIUS AT FS 1540, 5 ABOVE UPPER CUSP AREA. F ABRICATED AND INSTALLED NEW ANGLE FOR FRAME REPAIR AT FS 1540 LT, 5 ABOVE UPPER CUSP AREA PER COTNEY DRAWING D93-R72. F ABRICATED, HEAT AND AGED. TREATED AND PRIMED REPAIR PART IAW COTNEY DWG NR D93-R72, DC8 SRM 51-1-1 AND 51-1-8. INSTALL ED REPAIR IAW COTNEY DWG NR D93-R72. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04963 TASK NR Y1420. 2 L 7 4 4F 4A25 1998032600972 19980326 00972 WP 1998 3 26 CKSA98164 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 480 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND HOLE DRILLED INTO LT FRAME RADIUS AT FS 480, 20 ABOVE UPPER CUSP AREA AND GOUGE AT 12 ABOVE UPPER CUSP AREA. FABRICATED REPAIR ANGLE AND SHIMS, LOCATED, DRILLED ATTACHMENTS LOCATIONS IAW COTNEY DWG NR D93-R12. HEAT TREATED AND AGED REPAIR PART IAW DC8 SRM 51-1-1. TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW COTNEY DWG NR D93-R12. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04964 TASK NR Y1421. 2 L 7 4 4F 4A25 1998040100001 19980401 00001 WP 1998 4 1 UPS98826152 1 19980318 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 874UP 46074 EMERGENCY LIGHTS WILL NOT TURN OFF WITH SWITCH. REPLACED BATTERY PACK. 2 L 7 4 4F RT 4A25 1998040100003 19980401 00003 NM 1998 4 1 CALA9800536 1 19980320 A 7722 EGT INDICATION BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 1 ENGINE HIGH A CALA A D UNSCHED LANDING RETURN TO BLOCK M Y OVER TEMP ENGINE STOPPAGE CL CLIMB 1 SW 09 40127 28968 31533 THE LEFT EEC AND LEFT ELC EICAS MESSAGES ILLUMINATED AS THE LEFT ENGINE EGT EXCEEDED REDLINE AND AUTO SHUTDOWN WHILE CLI MBING OUT AT 16,000 FEET. THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS TAKEN OU T OF SERVICE FOR TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A2NM E12EU 1998040100004 19980401 00004 WP 1998 4 1 ARWA980304 1 19980317 A 3230 RETRACT MECH LKHEED 1011 1011385115 5265015 WP LANDING GEAR MALFUNCTIONED A ARWA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 19 306GB 1138 UNABLE TO RAISE GEARS AFTER T/O, AIRCRAFT CREW DUMPED FUEL (APPROX 5.000 LBS). RETURNED TO BLOCKS, PINS REMOVED, STOWED AIRCRAFT WAS OK FOR SERVICE, FUELED AND RELEASED FOR FLIGHT. 2 L 7 3 4F A23WE 1998040100005 19980401 00005 WP 1998 4 1 ARWA980307 1 19980324 A 7732 A24000104 MONITOR LKHEED 1011 1011385115 5265015 WP NR 1 ENGINE INOPERATIVE A ARWA D RETURN TO BLOCK J E WARNING INDICATION VIBRATION/BUFFET TX TAXI/GRND HDL 1 SO 19 307GB 193U1131 A/C BLOCK TURNBACK WITH SPOILER NR 5 INDICATION ON SPI NOT WORKING. AFTER A/C ON BLOCKS ENGINE SHUT DOWN, NR 1 ENGINE V IBRATION SHOWED 4 UNITS. ENTERED SPI FOR NR 5 SPOILER ON DMI 2. REMOVED AND REPLACED VIBRATION MONITOR AND PERFORMED E NGINE RUN UP AND TEST NR 1 PER LOCKHEED L1011 MM 77-32-0 NORMAL. 2 L 7 3 4F A23WE 1998040100007 19980401 00007 SO 1998 4 1 SWIA971104 1 19980306 A 3260 12038594501 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 292SW 120319 AFTER TAKEOFF WITH GEAR UP TAKEOFF WARNING CONTINUED TRIM, FLAPS, AUTO FEATHER. REPLACED GEAR CONTROL BOX, OPS CHECKS G OOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1998040200001 19980402 00001 EU 1998 4 2 98ZZZX1239 1 19980316 A 2913 D1331454E GUIDE ASSY 10545028 BOLKMS 105 BO105S 5626006 EU HYDRAULIC PACK REQUIRED LUBE A HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 6607K 416 S841 HYDRAULIC BLOCK LIGHT ILLUMINATED IN CRUISE FLIGHT. RETURNED TO BASE AND LANDED WITHOUT INCIDENT. MAINTENANCE LUBRICAT ED MICROSWITCH AND GUIDE ASSEMBLY. REF: BO-105 IPB, CHAPTER 2-447-001, FIGURE 447, ITEM 50. 1 G 7 2 3U H3EU 1998040200104 19980402 00104 NM 1998 4 2 CA980309011 1 19980218 A 2710 285T0015114 ACTUATOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE STAB/AIL MODULE MALFUNCTIONED W A UNSCHED LANDING O J OTHER WARNING INDICATION CL CLIMB 1 CA P709694 (CAN) SHORTLY AFTER TAKEOFF CLIMBING THROUGH 3500 FEET IN LEFT TURN RUDDER RATIO AND AILERON LOCK OUT MESSAGE APPEARED O N ENGINE INDICATION AND CREW ALERTING SYSTEM AND OVERHEAD PANEL. REPLACED STAB TRIM AND AILERON LOCKOUT MODULE. 2 L 7 2 4F 4 F RT A1NM E3NE 1998040200105 19980402 00105 WP 1998 4 2 CA980309014 1 19980227 A 2820 1612274101 LINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE CENTER TANK CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 14825 (CAN) NR 3 ALTERNATE FUEL QUANTITY INCREASING DURING REFUELING WITH NR 3 ALTERNATE FUEL SHUT-OFF VALVE CLOSED. CONNECTO R ASSY FUEL LINE CENTER TANK CRACKED. REPAIRED. 2 L 7 3 4F 4 F A23WE E12EU 1998040200107 19980402 00107 EA 1998 4 2 CA980311012 2 19980205 A 8520 ENGINE PIPER PA31 PA31325 7103105 SO LYC O540 TIO540F2BD 41532 EA NR 1 ENGINE FRICTION W K NONE O OTHER IN INSP/MAINT 1 CA RL31768A (CAN) UNKNOWN CAUSE OF FRICTION IN THE CRANKCASE. ENGINE SENT FOR INVESTIGATION AND REPAIR. 1 L 7 2 3O 3 O A20SO E14EA 1998040200108 19980402 00108 EA 1998 4 2 CA980311013 1 19980209 A 5711 C6W1056 SPAR DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA SPAR CAPS CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 24349 PCE41976 (CAN) DURING REPLACEMENT OF LEFT AND RIGHT LOWER WING SKINS, LEVEL 2 CORROSION WAS FOUND ON THE FORWARD SPAR CAPS IN THE AREAS BEHIND BOTH LEFT AND RIGHT NACELLE FIREWALLS. THESE AREAS CANNOT BE VISUALLY INSPECTED WITHOUT REMOVAL OF THE NA CELLES. LEFT SPAR CAP REPLACED. RIGHT SPAR CAP REPAIRED. PART TC: 30,073. ACFT TT: 24,348 HOURS. 1 H 7 2 3T 4 T A9EA E4EA 1998040200110 19980402 00110 NM 1998 4 2 CA980311015 1 19980224 A 2760 82950010175 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ACTUATOR PIN HOLE W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120329 (CAN) HYDRAULIC LEAK NR 1 SIDE AT OUTBOARD SPOILER ACTUATOR. HYDRAULIC FLUID HAD FLOWED TOWARDS THE NACELLE AND LEAKED ON THE MAIN WHEEL GIVING THE IMPRESSION THAT THE MID-DOOR ACTUATOR WAS LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1998040200111 19980402 00111 NM 1998 4 2 CA980311017 1 19980305 A 2760 824500102717 LINE A44700009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ACTUATOR PIN HOLE W K NONE K S FLUID LOSS AFFECT SYSTEMS AP APPROACH 1 CA 0801 TM120796 (CAN) HYDRAULIC LINE AT LEFT HAND SPOILER OUTBOARD ACTUATOR HAD A PIN HOLE LEAK AT THE BEND AT THE ACTUATOR. HYDRAULIC FLUID HAD FLOWED TO THE LEFT NACELLE GIVING AN INDICATION OF A FORWARD MLG DOOR ACTUATOR LEAK. 2 H 7 2 4T 4 T RT A13NM E20NE 1998040200112 19980402 00112 NM 1998 4 2 CA980311018 1 19980305 A 2910 82960010147 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE REGULATOR CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120804 (CAN) HYDRAULIC LINE CHAFING AGAINST REGULATOR AND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1998040200114 20010312 00114 WP 2001 3 12 CA980311023 1 19980228 A 2133 CONNECTOR LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE AFT OUTFLOW DISCONNECTED W A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 CA (CAN) AFTER TAKEOFF AND DURING CLIMB, AFT OUTFLOW VALVE STUCK IN THE OPEN POSITION, MANUAL MODE SELECTED AND STILL COULD NOT BRING THE AFT OUTFLOW VALVE IN THE GREEN BAND. AIRCRAFT RETURNED TO BLOCKS. AFT OUTFLOW VALVE CANNON PLUGS FOUN D DISCONNECTED FROM A PREVIOUS WORK, RECONNECTED. 2 L 7 3 4F 4 F A23WE E12EU 1998040200115 19980402 00115 WP 1998 4 2 CA980311024 1 19980228 A 2120 1526463105 DUCT ASSY LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE AIR DIST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10224 (CAN) CRACK FOUND AT CONNECTION OF OVER PRESSURE VALVE FLANGE ON DUCT. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1998040200116 19980402 00116 NE 1998 4 2 CA980311025 2 19980228 A 7320 101MK14 FUEL FLOW REG LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE FAULTY W E ENGINE SHUTDOWN O OTHER DE DESCENT 1 CA 10141 (CAN) DURING TOP OF DESCENT, NR 2 ENGINE WOULD NOT THROTTLE BACK BELOW 83 PERCENT N1. ALL ENGINE PARAMETERS WERE NORMAL . NR 2 ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE FUEL FLOW REGULATOR (FFR) INTERNAL DAMAGED. F FR REPLACED. AIRCRAFT GROUND RUN SERVICEABLE AND RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1998040200117 19980402 00117 WP 1998 4 2 CA980311026 1 19980301 A 2781 SLATS LKHEED 1011 1011385114 WP LT RT BRAKE INTERMITTENT W A UNSCHED LANDING O J OTHER WARNING INDICATION CL CLIMB 1 CA (CAN) FOLLOWING GEAR-UP SELECTION THE GEAR IN TRANSIT LIGHT AND GEAR DOOR LIGHT STAYED ON. ABNORMAL PROCEDURE CARRIED O UT EXCEPT THAT UPON GEAR DOWN SELECTION, THE GEAR TRUCK LIGHT CAME ON. ON RETURN ON APPROACH FLAPS SELECTION, THE FLAPS LOCKED AT 2 DEGREES, SLATS MALFUNCTION PROCEDURE CARRIED OUT, AND JUST PRIOR TO LANDING, THE TRUCK LIGHT EXTINGUISHED. LEFT AND RIGHT SLAT ASSYMETRY BRAKE RESET AND SLATS OPERATED NORMALLY. 2 L 7 3 4F A23WE 1998040200118 19980402 00118 WP 1998 4 2 CA980311027 1 19980301 A 2133 VALVE LKHEED 1011 10113853 5265020 WP OUTFLOW FAILED W H DEACTIVATE SYST/CIRCUITS O OTHER DE DESCENT 1 CA (CAN) AIRCRAFT SLOW TO PRESSURIZE, PRESSURE CONTROLLER BITE CHECK CARRIED OUT AND FWD OUTFLOW VALVE FOUND STICKING. REAR OUTFLOW VALVES NOT RESPONDING IN BOTH AUTO AND MANUAL MODES. FWD OUTFLOW VALVE AND ACTUATOR REPLACED, REAR VALVES CLEAN ED. 2 L 7 3 4F A23WE 1998040200119 19980402 00119 SW 1998 4 2 CA980311029 1 19980210 A 5610 3600431255 WINDSHIELD GULSTM 690TP 690D 3970405 SW COCKPIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA 361 (CAN) THE WINDSHIELD OUTER GLASS CRACKED WHILE ON DESCENT. ACFT TT: 9,794 HOURS. 1 H 7 2 3T 2A4 1998040200120 19980402 00120 NM 1998 4 2 CA980313007 1 19980227 A 2760 82950010223 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE IB ROLL SPOILER LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 120542 (CAN) CREW REPORTED FUEL LEAK AROUND THE NR 1 MLG WHEEL WELL. INVESTIGATION FOUND A CRACKED HYDRAULIC LINE AT THE INBOA RD ROLL SPOILER ACTUATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1998040200121 19980402 00121 SO 1998 4 2 CA980313009 1 19980224 A 7810 41200451 EDUCTOR CAMAIR 480 480 1890102 SO ALLSN 250C 250C20 03013 GL ENG EXHAUST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 107 CAE845007 (CAN) EXHAUST EDUCTOR CRACKED IN SEVERAL PLACES BOTH ON FORWARD AND AFT EDGES AROUND DOUBLERS. 1 L 7 2 3O 3 U 2A2 E4CE 1998040200122 19980402 00122 EU 1998 4 2 AWXA9800074 1 19980312 A 5347 A5NA2223 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 808 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING SCHEDULED C-3 INSPECTION, NR 4 SEAT TRACK REPLACED FROM STN 808 FR 20 TO STN 950 FR 24 DUE TO CORROSION BEYOND SR M LIMITS. SPLICED IN FLOOR TRACK PER ER 32-53-12-17. 2 L 7 2 4F RT A28NM 1998040200123 19980402 00123 EU 1998 4 2 AWXA9800075 1 19980312 A 5347 A5NA2223 FLOOR TRACK AIRBUS 320 A320231 3930325 EU BS 808 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 DURING SCHEDULED C-3 INSPECTION, REPLACED NR 2 AND NR 3 FLOOR TRACK STN 808 FR 20 DUE TO CORROSION BEYOND SRM LIMITS. S PLICED IN FLOOR TRACK PER SRM 53-00-15, PAGE 201. 2 L 7 2 4F RT A28NM 1998040200124 19980402 00124 EU 1998 4 2 AWXA9800076 1 19980226 A 5347 ASNA2223 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 808 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING SCHEDULED C-6 INSPECTION, FOUND SEAT TRACK NR 4 STN 808 AND SEAT TRACK NR 3 STN 808 CORRODED PAST SRM LIMITS 53-0 0-15. EFFECTED AREAS REPAIRED PER SRM 53-00-15, PAGE 204 USING EXTRUSION 7075-T6. 2 L 7 2 4F RT A28NM 1998040200125 19980402 00125 EU 1998 4 2 AWXA9800077 1 19980226 A 5347 ASNA2223 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 808 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 633AW 082 DURING SCHEDULED C-6 INSPECTION, FOUND CORROSION ON SEAT TRACKS AT STN 808, FR 20, TRACKS 1, 2, 3 AND 4. NR 3 TRACK REQ UIRED RE-WORK. INSTALLED EXTRUSION 7075T6 REPAIR DUE TO CORROSION BEYOND LIMITS AS PER SRM 53-00-15. 2 L 7 2 4F RT A28NM 1998040200126 19980402 00126 NM 1998 4 2 AWXA9800078 1 19980314 A 3350 864705 POWER SUPPLY BOEING 737 7372M8 1384483 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 141AW 21955 EMERG EXIT LIGHT CENTER AISLE OVERWING WON'T LIGHT WITH OTHER EXIT LIGHTS. REMOVED AND REPLACED BATTERY PWR SUPPLY UNIT , OPS CKD NORMAL. STC NR SA3432NM. 2 L 7 2 4F A16WE 1998040200127 19980402 00127 EU 1998 4 2 AWXA9800079 1 19980312 A 5347 ASNA2223 SEAT TRACK AIRBUS 320 A320231 3930325 EU BS 808 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 640AW 448 NR 4 SEAT TRACK REPLACED FROM STN 808 FRO 20 TO STN 950 FRA 24 DUE CORRODED BEYOND SRM LIMITS. SPLICED IN FLOOR TRACK A S PER ER 32-53:12-17. 2 L 7 2 4F RT A28NM 1998040200128 19980402 00128 EU 1998 4 2 AWXA9800080 1 19980314 A 5347 ASNA2223 FLOOR TRACK AIRBUS 320 A320231 3930325 EU BS 808 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 640AW 448 NR 2 AND 3 FLOOR TRACK STN 808 FR 20 REPLACED DUE CORROSION BEYOND SRM LIMITS. SPLICED IN FLOOR TRACK AS PER SRM 53-00- 15 PAGE 201. 2 L 7 2 4F RT A28NM 1998040200129 19980402 00129 NM 1998 4 2 AWXA9800081 1 19980314 A 3246 WHEEL BOEING 737 7373S3 1384711 NM MLG MISSING A A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 315AW 23734 DURING ROUTINE MAINTENANCE CHECK ON POST FLIGHT WALKAROUND, FOUND NR 1 MAIN TIRE AND WHEEL ASSEMBLY MISSING. LANDING NO RMAL, NO VIBRATION, ANTI-SKID NORMAL. REMOVED AND REPLACED LEFT MLG INNER CYLINDER PER OHM 32-11-11. 2 L 7 2 4F RT A16WE 1998040200130 19980402 00130 NM 1998 4 2 CALA9800574 1 19980320 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 400-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND TOP AND BOTTOM OF RT OUTBOARD SEAT TRACK CORRODED AT FS 400 TO 440. THE SEAT TRACK WAS REMOVED AND REP LACED IAW SRM 51-30-2, 53-10-5 AND 51-10-2. 2 L 7 3 4F A3WE 1998040200131 19980402 00131 NM 1998 4 2 CALA9800575 1 19980320 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND TOP FLANGE OF FLOORBEAM CORRODED AT FS 1110, RBL 10 TO RBL 63. THE CORRODED AREA WAS CUT OUT AND A REP AIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998040200132 19980402 00132 NM 1998 4 2 CALA9800576 1 19980320 A 5754 SKIN BOEING 727 727227 1384078 NM NR 6 LE FLAP DEBONDING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 73751 21247 INSPECTION FOUND RT WING NR 6 KRUEGER FLAP DEBONDING. A REPAIR WAS ACCOMPLISHED IAW ECRA 5720-01064. 2 L 7 3 4F A3WE 1998040200133 19980402 00133 WP 1998 4 2 CALA9800577 1 19980322 A 5400 BRACKET DOUG DC10 DC1030 3023501 WP NR 2 PYLON CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND NR 2 PYLON UPPER PYLON TRAILING EDGE ATTACH BRACKET CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IA W SRM 54-32-02, 51-38-01, FIGURE 13, 51-21-01, 51-31-01. 2 L 7 3 4F A22WE 1998040200134 19980402 00134 WP 1998 4 2 CALA9800578 1 19980322 A 5530 SUPPORT DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 809NY 49263 INSPECTION FOUND A .375 INCH CRACK AT LOWER RIVET HOLE IN FORWARD LEFT VERTICAL STABILIZER SPAR SUPPORT AT 37.3 INCHES A FT OF STA 1089.3 IN TAIL COMPARTMENT ABOVE CATWALK. THE AREA WAS REPAIRED IAW SRM 55-02, FIGURE 26. 2 L 7 2 4F A6WE 1998040200135 19980402 00135 WP 1998 4 2 CALA9800579 1 19980323 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1421-1441 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND CORROSION ON LONGERON 30L BETWEEN STA 1421 TO 1441. THE CORRODED SECTION OF LONGERON WAS REMOVED AND R EPLACEMENT LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-00, FIGURE 2. 2 L 7 3 4F A22WE 1998040200136 19980402 00136 NM 1998 4 2 CALA9800580 1 19980320 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1090, LBL 55 AND AT STA 970 TO 1130, RBL 24. THE SEAT TRACKS WERE REMOVED A ND REPLACED IAW SRM 53-10-2, 51-10-2, AND 51-20-11. 2 L 7 3 4F A3WE 1998040200137 19980402 00137 NM 1998 4 2 CALA9800581 1 19980323 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND TWO 2 CRACKS IN STA 1183 BULKHEAD WEB ON FORWARD SIDE AT WL 188, RBL 32 AND RBL 35.5. THE CRACKS WERE STOP DRILLED, A REPAIR WAS INSTALLED IAW SRM 53-00 AND BOEING DRAWING 65C31446. 2 L 7 3 4F A3WE 1998040200138 19980402 00138 NM 1998 4 2 CALA9800582 1 19980323 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1090 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND FLOORBEAM CORRODED AT FS 1090, RBL 24. THE CORRODED AREA WAS CUT OUT, TWO ANGLES WERE FABRICATED AND I NSTALLED IAW SRM 53-10-8, FIGURE 8. 2 L 7 3 4F A3WE 1998040200139 19980402 00139 NM 1998 4 2 CALA9800583 1 19980323 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND FLOORBEAM CORRODED AT FS 1166 RBL 45. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A REPAIR WAS FABR ICATED AND INSTALLED IAW SRM 53-10-8 AND 51-30-2. 2 L 7 3 4F A3WE 1998040200140 19980402 00140 SO 1998 4 2 EMB120RT 1 19980324 A 3230 MS34702833S CONNECTOR EMB 120 EMB120RT SO RT MLG SHORTED A COMA K NONE O OTHER CL CLIMB 1 SO 01 264CA 120256 LANDING GEAR WILL NOT RETRACT. REPAIRED DOWNLOCK WIRING CONNECTOR AT RIGHT HAND LANDING GEAR. 2 L 7 2 4T RT A31SO 1998040200141 19980402 00141 SO 1998 4 2 COMA9810075 1 19980324 A 3350 CONNECTOR EMB 120 EMB120RT SO CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 241CA 120211 EMERGENCY LIGHT AT ROW 2 INOPERABLE. REPAIRED LOOSE CONNECTION AT BULB. 2 L 7 2 4T RT A31SO 1998040200142 19980402 00142 SO 1998 4 2 COMA9810076 1 19980325 A 3610 S2L228 O-RINGS EMB 120 EMB120RT SO LT BLEED AIR WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 249CA 120230 LEFT HAND BLEED AIR DUCT LEAK WARNING AFTER TAKEOFF. REPLACED O-RING SEALS ON LEFT HAND BLEED AIR TUBING CONNECTIONS. 2 L 7 2 4T RT A31SO 1998040200143 19980402 00143 SO 1998 4 2 COMA9810077 1 19980324 A 3610 52L228 O-RINGS EMB 120 EMB120RT SO LT BLEED AIR WORN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 249CA 120230 LEFT HAND BLEED AIR DUCT LEAK WARNING. REPLACED WORN O-RINGS AT LEFT WING BLEED AIR DUCT JOINT. 2 L 7 2 4T RT A31SO 1998040200144 19980402 00144 SO 1998 4 2 COMA9810078 1 19980325 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO RT TE FLAP MALFUNCTUATING A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 205CA 8048 4855 120205 OUTBOARD FLAP INDICATION IS FLUCTUATING BETWEEN 2 AND 7 UNITS. COULD NOT DUPLICATE DISCREPANCY. REPLACED RIGHT HAND OU TBOARD FLAP ACTUATOR FOR TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1998040200145 19980402 00145 NM 1998 4 2 UPS98226179 1 19980325 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 990-1005 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-SI, THE SEAT TRACK AT RBL 55 HAS CORROSION AROUND NUT PLATE HOLES BETWEEN BS 990 TO 1005 WL 208. REMOVE D AND REPLACED SEAT TRACK SECTION BS 990 TO 1010 IAW SRM 51-30-2 53-10-01, 51-10-02. 2 L 7 3 4F A3WE 1998040200146 19980402 00146 NM 1998 4 2 UPS98226181 1 19980325 A 5347 694121 TRACK BOEING 727 727247 138408F NM BS 740-755 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON EXPANSION LINK LBL 45 BS 740 TO 755 WL 207 TO 208. REMOVED CORROSIO N ON EXPANSION LINK FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED EXPANSION LINK/TRACK PER SRM 51-30- 4. 2 L 7 3 4F A3WE 1998040200147 19980402 00147 WP 1998 4 2 UPS98826180 1 19980326 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATT PACK, SYSTEM OPS CHECK OK. 2 L 7 4 4F RT 4A25 1998040200148 19980402 00148 NM 1998 4 2 QXEA9800438 1 19980321 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 349PH 486 FORWARD LEFT EMERGENCY AIRSTAIR LIGHT INOP. RELAMPED, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998040200149 19980402 00149 NM 1998 4 2 QXEA9800439 1 19980321 A 3350 6104781 BATTERY DHAV 82410191011 DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 824PH 15736 22 157 FIRST 2 FLOOR PROXIMITY LIGHTS INOP. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998040200150 19980402 00150 EU 1998 4 2 QXEA9800440 1 19980322 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 486US 11237 EXIT SIGN AT SEAT 9A INOP. RELAMPED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998040200152 19980402 00152 EU 1998 4 2 QXEA9800442 1 19980324 A 3350 5515900004 CIRCUIT GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTION A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 490US 11152 EMERGENCY EXIT LIGHT IN CEILING ABOVE THE GALLEY HAS BULBS INOP. REPLACED THE CIRCUIT CARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998040200153 19980402 00153 EU 1998 4 2 QXEA9800443 1 19980324 A 3350 5515900004 CIRCUIT GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTION A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 499US 11182 FORWARD EXIT SIGN ABOVE THE COCKPIT DOOR HAS INOP BULBS. REPLACED CIRCUIT CARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998040200154 19980402 00154 WP 1998 4 2 98FDEA00218 1 19980325 A 5754 RIB DOUG DC10 DC1010F 3022111 WP NR 2 LE SLAT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 049FE 47803 LEFT WING NR 2 LEADING EDGE SLAT, INBOARD CLOSURE RIB IS BADLY CORRODED ON THE INSIDE, EXFOILATED. *S/D* COMPLIED WITH EA 8-5750-38493. 2 L 7 3 4F A22WE 1998040200155 19980402 00155 NM 1998 4 2 98FDEA00219 1 19980326 A 5320 651862014 CHANNEL BOEING 727 72722C 138400F NM BS 555.05 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 NR 0449 006 - WHILE WORKING NR 0227 FOUND CHANNEL CRACKED AT BS 555.05, WL 187 AS MARKED NR 65-18620-14. REMOVED AND RE PLACED CHANNEL (NR 1 TRANSVERSE BEAM) WL 187 IN FWD CARGO DOOR IAW FED-EX SRM 51-30-2. 2 L 7 3 4F A3WE 1998040200156 19980402 00156 NM 1998 4 2 98FDEA00220 1 19980326 A 5320 65341444 BEAM BOEING 727 72722C 138400F NM BS 765 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 NR 0170 007 - CORROSION ON LONGITUDINAL BEAM UNDER NUTPLATES AT BS 765, RBL 25, WL 208. REPAIRED LONGITUDINAL BEAM AT B S 765, RBL 25, WL 208 IAW FED-EX EA 7-5310-37471B. 2 L 7 3 4F A3WE 1998040200157 19980402 00157 WP 1998 4 2 ABXA9800254 1 19980323 A 3350 41B0048D07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941AX 47419 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED COCKPIT EMERGENCY LIGHT BATTERIES, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998040200158 19980402 00158 NM 1998 4 2 P5CA9800517 1 19980317 A 5320 SILL BOEING 747 747123 1384873 NM CARGO DOORWAY CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION FOUND ON FWD LOWER CARGO SERRATED PLATE ON DOOR SILL NR 5, 6 AND7 BOTTOM AFT HOLE NR 8 HAS CORROSION. REMOVED CORROSION FROM PLATE PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200159 19980402 00159 NM 1998 4 2 P5CA9800518 1 19980317 A 5510 FASTENER BOEING 747 747123 1384873 NM HORIZ STAB MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 RT HORIZ STAB NAV LIGHT FIXED WITH SEALANT FASTENERS MISSING. INSTALLED FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998040200160 19980402 00160 NM 1998 4 2 P5CA9800519 1 19980317 A 5230 SKIN BOEING 747 747123 1384873 NM CARGO DOOR TORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FWD CARGO DOOR TORN IN UPPER RT CORNER AT PREVIOUS REPAIR. INSTALLED DOUBLER ON FWD RT CORNER OF DOOR PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998040200161 19980402 00161 NM 1998 4 2 P5CA9800520 1 19980317 A 3230 BUMPER PAD BOEING 747 747123 1384873 NM LT MLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LT WING GEAR BOGIE BEAM TILT BUMPER CRACKED AND DAMAGED. REMOVED AND REPLACED BUMPER PAD PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200162 19980402 00162 NM 1998 4 2 P5CA9800521 1 19980317 A 5280 SKIN BOEING 747 747123 1384873 NM RT MLG DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 RT WING MLG LOWER FLYING DOOR IS DELAMINATED. REMOVED DAMAGE, APPLIED FIBERGLASS AND BONDING PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998040200163 19980402 00163 NM 1998 4 2 P5CA9800522 1 19980317 A 7110 PANEL BOEING 747 747123 1384873 NM NR 1 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 NR 1 ENGINE INLET 3 INCH CRACK AT 3 O'CLOCK POSITION ON ACCOUSTIC PANEL. REPAIRED CRACK BY CUTTING IT OUT AND APPLYING POTTING COMPOUND PER SRM 54-31-03. 2 L 7 4 4F A20WE 1998040200164 19980402 00164 NM 1998 4 2 P5CA9800523 1 19980317 A 5320 STANCHION BOEING 747 747123 1384873 NM BS 480 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 FWD CARGO COMPARTMENT STA 480 PLUG SUPPORT CHANNEL DAMAGED. REMOVED AND REPLACED BOTH RT SIDE STANCHIONS AT STA 480 PER SRM 51-30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1998040200165 19980402 00165 NM 1998 4 2 P5CA9800524 1 19980317 A 5730 PANEL BOEING 747 747123 1384873 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 RT WING TOP L/E FIXED PANEL INBD OF PYLON PREVIOUS REPAIR PEELING OFF. REMOVED PREVIOUS REPAIR, REPAIRED PER SRM 51-40- 15. 2 L 7 4 4F A20WE 1998040200166 19980402 00166 NM 1998 4 2 P5CA9800525 1 19980320 A 5321 FLOOR PANEL BOEING 747 747132 1384882 NM CARGO COMPT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FWD CARGO COMPARTMENT BS 570/600 FLOOR PANEL DAMAGED. REPAIRED DAMAGE PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998040200167 19980402 00167 NM 1998 4 2 P5CA9800526 1 19980320 A 5414 PLATE BOEING 747 747132 1384882 NM NR 2 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 DAMAGE ON NR 2 PYLON DUCT REAR LOWER PLATE. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200168 19980402 00168 NM 1998 4 2 P5CA9800527 1 19980320 A 5330 PANEL BOEING 747 747132 1384882 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LT BODY GEAR STA 1480 PANEL CRACKED. REPAIRED CRACK PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998040200169 19980402 00169 NM 1998 4 2 P5CA9800528 1 19980320 A 5320 SHEAR TIE BOEING 747 747132 1384882 NM BS 1780 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 AFT CARGO COMPARTMENT STA 1780 S47L SHEAR TIE CRACKED. REPAIRED PER 53-10-04. 2 L 7 4 4F A20WE 1998040200170 19980402 00170 NM 1998 4 2 P5CA9800529 1 19980320 A 5321 FLOOR PANEL BOEING 747 747132 1384882 NM BS 1450-1460 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 MAIN DECK BS 1450 TO 1460 FLOOR PANEL DAMAGED. REPAIRED PER SRM 53-21-02. 2 L 7 4 4F A20WE 1998040200171 19980402 00171 NM 1998 4 2 P5CA9800530 1 19980320 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2250 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BS 2250 LBL 11 SEAT TRACK WEB CRACKED. REPAIRED SEAT TRACK PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998040200172 19980402 00172 NM 1998 4 2 P5CA9800531 1 19980320 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1900-1920 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 AFT CARGO COMPARTMENT BS 1900/1920 SUPPORT ANGLE BROKEN. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200173 19980402 00173 NM 1998 4 2 P5CA9800532 1 19980320 A 5320 CHANNEL BOEING 747 747132 1384882 NM BS 560 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BS 560 FWD CARGO RT SIDE CHANNEL BROKEN. REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998040200174 19980402 00174 NM 1998 4 2 P5CA9800533 1 19980320 A 5321 FLOOR PANEL BOEING 747 747132 1384882 NM BS 520/600 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 UPPER DECK BS 520/600 RPL 9/27 FLOOR PANEL DAMAGE. REPLACED FLOOR PANEL PER SRM 53-21-02. 2 L 7 4 4F A20WE 1998040200175 19980402 00175 NM 1998 4 2 P5CA9800534 1 19980320 A 5320 TIE STRAP BOEING 747 747132 1384882 NM BS 1940/1980 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BULK CRGO BS 1940/1980 S40L TIE STRAPS DAMAGED AND CRACKED. REPLACED TIE STRAPS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200176 19980402 00176 NM 1998 4 2 P5CA9800535 1 19980320 A 5400 BRACKET BOEING 747 747132 1384882 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 1 PYLON FILTER MOUNT BRACKED CRACKED, 2 EA. REPLACED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998040200177 19980402 00177 NM 1998 4 2 P5CA9800536 1 19980320 A 5320 SPLICE BOEING 747 747132 1384882 NM BS 1350 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 MAIN DECK BS 1350 STR 13L SPLICE FITTING CRACKED. REPLACED FITTING PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200178 19980402 00178 NM 1998 4 2 P5CA9800537 1 19980320 A 5400 FASTENERS BOEING 747 747132 1384882 NM NR 4 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 PYLON INSIDE STRUT AT STA 221.9 LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998040200179 19980402 00179 NM 1998 4 2 P5CA9800538 1 19980320 A 5320 WEB BOEING 747 747132 1384882 NM BS 570 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FWD CARGO COMPARTMENT BS 570 SUPPORT WEB CRACKED. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200180 19980402 00180 NM 1998 4 2 P5CA9800539 1 19980320 A 5320 FASTENERS BOEING 747 747132 1384882 NM BS 570-600 MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FWD CARGO COMPT BS 570/600 FLOOR PANEL MISSING FASTENERS. REMOVED AND REPLACED FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998040200181 19980402 00181 NM 1998 4 2 P5CA9800540 1 19980320 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 320 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NLG BS 320, 2 CRACKED ANGLES. REMOVED AND REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200182 19980402 00182 NM 1998 4 2 P5CA9800541 1 19980320 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 400 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FWD E/E COMP BS 400 ANGLE CRACKED. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200183 19980402 00183 NM 1998 4 2 P5CA9800542 1 19980320 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT WING INBD OF NR 7 FLAP TRACK FOREFLAP DELAMINATED. REPAIRED FOREFLAP DELAMINATION PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998040200184 19980402 00184 NM 1998 4 2 P5CA9800543 1 19980320 A 5400 FAIRING BOEING 747 747132 1384882 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 PYLON, V FAIRING LEFT FWD CRACKED. REPAIRED FAIRING PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998040200185 19980402 00185 NM 1998 4 2 P5CA9800544 1 19980312 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK BS 502 THRU 530 LBL 9. REMOVED CORROSION PER SRM 51-10-01 AND TRACK REPAIRED PER SRM 51-10-05. 2 L 7 4 4F A20WE 1998040200186 19980402 00186 NM 1998 4 2 P5CA9800545 1 19980321 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 840 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 TENSION TIE CRACKED AT BS 840 WL 300. TENSION TIE REPAIRED PER SRM 53-23-71. 2 L 7 4 4F A20WE 1998040200187 19980402 00187 NM 1998 4 2 P5CA9800546 1 19980321 A 5320 CHANNEL BOEING 747 747132 1384882 NM CARGO COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FWD CARGO FLOOR SUPPORT CHANNEL CRACKED. SUPPORT REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200188 19980402 00188 NM 1998 4 2 P5CA9800547 1 19980312 A 5330 PANEL BOEING 747 747132 1384882 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LT T/E PANEL 572AB DELAMINATED. REPAIRED PANEL PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998040200189 19980402 00189 NM 1998 4 2 P5CA9800548 1 19980312 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2190 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON MAIN DECK BS 2190 LBL 11 SEAT TRACK. REPLACED TRACK PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 1998040200190 19980402 00190 NM 1998 4 2 P5CA9800549 1 19980321 A 5730 SKIN BOEING 747 747132 1384882 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LT WING UPPER SKIN FRT SPAR EXT CORRODED. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1998040200191 19980402 00191 NM 1998 4 2 P5CA9800550 1 19980321 A 7110 COWL BOEING 747 747132 1384882 NM NR 4 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 ENGINE RT COWL DELAMINATED. REPAIRED COWL BY HOT BOND PER SRM 51-40-06 FIG 17A. 2 L 7 4 4F A20WE 1998040200192 19980402 00192 NM 1998 4 2 P5CA9800551 1 19980321 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 520-530 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON SEAT TRACK BS 520 TO 530 BL L47. CORROSION REMOVED TRACK REPLACED AND REPROTECTED PER SRM 51-10-01 , 53-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998040200193 19980402 00193 NM 1998 4 2 P5CA9800552 1 19980321 A 5320 BRACKET BOEING 747 747132 1384882 NM BS 1380/1400 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FUSELAGE SUPPORT BRACKET BS 1380/1400 BROKEN. SUPPORT BRACKET REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200194 19980402 00194 NM 1998 4 2 P5CA9800553 1 19980321 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1487 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FUSELAGE SUPPORT FORGING CRACKED AT BS 1487. REPLACED FITTING PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200195 19980402 00195 NM 1998 4 2 P5CA9800554 1 19980321 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1110 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON SEAT TRACK FLANGE AT BS 1110 BL 98. CORROSION REMOVED, REPAIRED AND REPROTECTED PER SRM 51-10-01, 53-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200196 19980402 00196 NM 1998 4 2 P5CA9800555 1 19980321 A 7110 COWL BOEING 747 747132 1384882 NM NR 4 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 RT SIDE FAN COWL DELAMINATED. REPAIRED BY HOT BOND REPAIR PER SRM 51-40-06 FIG 17A. 2 L 7 4 4F A20WE 1998040200197 19980402 00197 NM 1998 4 2 P5CA9800556 1 19980321 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 2060 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FLOOR SUPPORT CHANNEL CRACKED AT BS 2060 BL 22. REPAIRED SUPPORT CHANNEL PER SRM 51-40-03 FIG 2. 2 L 7 4 4F A20WE 1998040200198 19980402 00198 NM 1998 4 2 P5CA9800557 1 19980321 A 5311 FRAME BOEING 747 747132 1384882 NM BS 860 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FRAME CRACKED AT BS 860 L 25. REPAIRED FRAME PER BACRS 53-22-33686. 2 L 7 4 4F A20WE 1998040200199 19980402 00199 NM 1998 4 2 P5CA9800558 1 19980314 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1980 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FUSELAGE SKIN DENTED AT BS 1980 S47R TO S51R. REPAIRED SKIN PER SRM 51-40-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1998040200200 19980402 00200 NM 1998 4 2 P5CA9800559 1 19980321 A 5320 WEB BOEING 747 747132 1384882 NM BS 2120 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 WEB AT BS 2120 TO 2140 STR 28R TO 29R CRACKED. REPAIRED WEB PER SRM 51-40-02 AND 51-40-03. 2 L 7 4 4F A20WE 1998040200201 19980402 00201 NM 1998 4 2 P5CA9800560 1 19980321 A 5280 DOOR BOEING 747 747132 1384882 NM LT MLG CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LT BODY GEAR DOOR CORRODED. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200202 19980402 00202 NM 1998 4 2 P5CA9800561 1 19980321 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 780 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 TENSION TIE CRACKED. TENSION TIE REPAIRED PER SB 53-2371 FIG 5. 2 L 7 4 4F A20WE 1998040200203 19980402 00203 NM 1998 4 2 P5CA9800562 1 19980321 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 820 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 TENSION TIE CRACKED AT BS 820 WL 300. TENSION TIE REPAIRED PER SB 53-2371 FIG 3. 2 L 7 4 4F A20WE 1998040200204 19980402 00204 NM 1998 4 2 P5CA9800563 1 19980321 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 860 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 TENSION TIE CRACKED AT BS 860 WL 300. TENSION TIE REPAIRED PER SB 53-2371 FIG 3. 2 L 7 4 4F A20WE 1998040200205 19980402 00205 NM 1998 4 2 P5CA9800564 1 19980321 A 5414 SKIN BOEING 747 747132 1384882 NM NR 4 PYLON HOLE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 PYLON RT HYD DOOR NR 484AR HAS HOLE. HOT BOND REPAIRED HOLE PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998040200206 19980402 00206 NM 1998 4 2 P5CA9800565 1 19980321 A 5330 SKIN BOEING 747 747132 1384882 NM APU COMPT AREA DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 APU COMPT RT DOOR RECESS CUTOUT ENLARGED. REPAIRED CUTOUT PER SRM 52-40-02 FIG 1. 2 L 7 4 4F A20WE 1998040200207 19980402 00207 NM 1998 4 2 P5CA9800566 1 19980321 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 498 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON SEAT TRACK BS 498 TO 500 LBL 99L. REPAIRED CORROSION PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200208 19980402 00208 NM 1998 4 2 P5CA9800567 1 19980323 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 920 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON SEAT TRACK STA 920 RBL 97R. REPAIRED CORROSION PER SRM 53-10-05. 2 L 7 4 4F A20WE 1998040200209 19980402 00209 NM 1998 4 2 P5CA9800568 1 19980311 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 980 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION MAIN DECK FLOORBEAM AT STA 980 RBL 70. REPAIRED PER 51-40-04 FIG 1. 2 L 7 4 4F A20WE 1998040200210 19980402 00210 NM 1998 4 2 P5CA9800569 1 19980323 A 5311 FRAME BOEING 747 747132 1384882 NM BS 540 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BS 540 S26L FRAME CRACKED. REPAIRED FRAME PER RS53-22-33687 BOEING. 2 L 7 4 4F A20WE 1998040200211 19980402 00211 NM 1998 4 2 P5CA9800570 1 19980323 A 5720 STIFFENER BOEING 747 747132 1384882 NM BS 1350 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON RT WING GEAR STA 1350 STIFFENER. REPAIRED CORROSION PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200212 19980402 00212 NM 1998 4 2 P5CA9800571 1 19980323 A 5753 FLAP BOEING 747 747132 1384882 NM NR 7 TE FLAP CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT LEADING EDGE FRONT SPAR WS 972 NR 7 FLAP. REPAIRED CORROSION PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200213 19980402 00213 NM 1998 4 2 P5CA9800572 1 19980323 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 2705 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 APU VERTICAL SUPPORT TUBE AT BS 2705 WL 364 HAS CRACK. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200214 19980402 00214 NM 1998 4 2 P5CA9800573 1 19980311 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 920 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON MAIN DECK SEAT TRACK BS 920 RBL 97R. CORROSION REMOVED AND REPAIRED PER SRM 53-10-05 FIG 14. 2 L 7 4 4F A20WE 1998040200215 19980402 00215 NM 1998 4 2 P5CA9800574 1 19980311 A 5400 FASTENERS BOEING 747 747132 1384882 NM NR 3 PYLON MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 3 PYLON AFT FIXED FAIRING 4 ANCHOR NUTS MISSING. REPLACED FASTENERS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200216 19980402 00216 NM 1998 4 2 P5CA9800575 1 19980321 A 5320 CLIP BOEING 747 747132 1384882 NM BS 1480 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT BODY GEAR CLIP DAMAGED STA 1480 ABOVE ANTI-SKID MODULE. REMOVED AND REPLACED CLIP PER MM 20-51-01. 2 L 7 4 4F A20WE 1998040200217 19980402 00217 NM 1998 4 2 P5CA9800576 1 19980311 A 5400 STRAP BOEING 747 747132 1384882 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 1 PYLON INTERNAL STRAP CRACKED AT STA 207. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200218 19980402 00218 NM 1998 4 2 P5CA9800577 1 19980311 A 5414 DOOR BOEING 747 747132 1384882 NM NR 1 PYLON DEFORMED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 1 PYLON RT TRAILING EDGE DOOR DEFORMED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200219 19980402 00219 NM 1998 4 2 P5CA9800578 1 19980311 A 5246 2024530063N DOOR BOEING 747 747132 1384882 NM BS 1840-1860 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BS1840 TO 1860 DRIP SHROUD ACCESS DOOR CRACKED. REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200220 19980402 00220 NM 1998 4 2 P5CA9800579 1 19980311 A 5400 NUT PLATE BOEING 747 747132 1384882 NM NR 3 STRUT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 3 AFT ENGINE STRUT L/R 4 DAMAGED NUT PLATES. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998040200221 19980402 00221 NM 1998 4 2 P5CA9800580 1 19980311 A 5730 PANEL BOEING 747 747132 1384882 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT WING PANEL 672DB DAMAGED ANCHOR NUTS. REMOVED AND REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200222 19980402 00222 NM 1998 4 2 P5CA9800581 1 19980311 A 5730 PLATE BOEING 747 747132 1384882 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT WING T/E ACCESS PANEL 691DB DAMAGED ANCHOR NUTS. REMOVED AND REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200223 19980402 00223 NM 1998 4 2 P5CA9800582 1 19980311 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LT WING FUELING PANEL DAMAGED LATCH. REMOVED AND REPLACED PER SRM 52-49-09. 2 L 7 4 4F A20WE 1998040200224 19980402 00224 NM 1998 4 2 P5CA9800583 1 19980311 A 5530 NUT PLATE BOEING 747 747132 1384882 NM VERT STAB DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 TWELVE DAMAGED NUT PLATE ON VERTICAL FIN. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998040200225 19980402 00225 NM 1998 4 2 VNAA9803026 1 19980324 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PCU DIRTY A VNAA D RETURN TO BLOCK J L WARNING INDICATION NO TEST TX TAXI/GRND HDL 1 GL 07 441JS 3059 THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED WHEN SELECTED, DURING TAXI CHECKS. THE AIRCRAFT RETURNED TO THE GATE. O UTSTATION MAINTENANCE INSPECTED, CLEANED AND SECURED THE RIGHT HAND OVERSPEED GOVERNOR CANNON PLUG. OPERATIONAL CHECKS W ERE COMPLETED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00-820. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998040200226 19980402 00226 WP 1998 4 2 CKSA98166 1 19980228 A 5320 SPLICE DOUG DC8 DC863F 302198F WP BS 1050 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON DOUBLER FS 1050 LONG 31LT. CLEANED CORROSION ON SPLICE PLATE IAW DC8 SRM 51-1-8. CORROSION REMOVAL OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED SPLICE PLATE IAW D C8 SRM 51-1-20D AND 51-1-21. FABRICATED REPLACEMENT SPLICE PLATE IAW DOUGLAS DWG 5779936 AND DC8 SRM 53-4-1 FIG 44 SHEE T 1 PAGE 161. TREATED AND PRIMED SPLICE PLATE IAW DC8 SRM 51-1-8. INSTALLED SPLICE PLATE IAW DC8 SRM 51-1-20D AND 51-1 -21. CORROSION TASK CARD NUMBER 5590-0551. NON-ROUTINE NR 04613 TASK NR X0043. 2 L 7 4 4F 4A25 1998040200227 19980402 00227 WP 1998 4 2 CKSA98167 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 1310 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1310, BL 24RT. REMOVED DAMAGED CARGO TRACK AT STA 1310, BL 24RT TO FIT PLUGS. CORROSION TREATED, PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNELS AND PLUGS ON TRACK STA 1310, B L 24RT IAW DC8 SRM 53-2-3 FIG 6D SHEET 1. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04474 TASK NR Y1585. 2 L 7 4 4F 4A25 1998040200228 19980402 00228 WP 1998 4 2 CKSA98168 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 870 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 870, BL 0. CUT OUT DAMAGED AREA OF SEAT TRACK 2 PLACES FOR PLUG REPAIR IAW DC8 SRM 53-2-3. TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8. INSTALLED PLUG REPAIRS IAW DC8 SRM 53- 2-3 AT STA 870. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04475 TASK NR Y1586. 2 L 7 4 4F 4A25 1998040200229 19980402 00229 WP 1998 4 2 CKSA98169 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 680 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 680, BL 0. REMOVED 2 SECTIONS OF WORN SEAT TRACK, STA 6 80, BL 0. INSTALLED TWO TRACK PLUGS IAW DC8 SRM 53-2-3 FIG 6D SHEET 1 AND DC8 SRM 51-3-0. C-CHECK WORK CARD NUMBER 006 0. NON-ROUTINE NR 04476 TASK NR Y1587. 2 L 7 4 4F 4A25 1998040200230 19980402 00230 WP 1998 4 2 CKSA98170 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 1220 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1220 BL 45 LT. REMOVED DAMAGE FROM SEAT TRACK TO FLT TR ACK PLUGGED IAW DC8 SRM 53-2-3 FIG 6D. PRIMED AND INSTALLED IAW DC8 SRM 53-2-3 FIG 6D. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04477 TASK NR Y1588. 2 L 7 4 4F 4A25 1998040200231 19980402 00231 WP 1998 4 2 CKSA98171 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP CABIN BROKEN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK LUGS BROKEN AT BEAR TRAP POSITION BETWEEN COMP 1 AND 2 BL 24RT. R OUTED OUT BROKEN LUGS AT BEAR STRAP BETWEEN COMP 1 AND 2 BL24RT TO INSTALL PLUGS. INSTALLED PLUGS WITH SCREWS IAW SRM 5 3-2-3 FIG 6D AND DC8 SRM 51-3-0. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 05801 TASK NR Y1604. 2 L 7 4 4F 4A25 1998040200232 19980402 00232 WP 1998 4 2 CKSA98172 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 1130 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1130, BL 24RT. CUT THE DAMAGED SEAT TRACK AT STA 1130 B L 24RT TO FIT PLUGS AND CHANNELS. INSTALLED THE PLUGS AND CHANNELS FIT IN TRACK STA 1130, BL 24RT IAW DC8 SRM 53-2-3 FI G 6D. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE 04473 TASK NR Y1584. 2 L 7 4 4F 4A25 1998040200233 19980402 00233 WP 1998 4 2 CKSA98173 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 770 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 770 BL 24RT. CUT WORN OUT SEAT TRACK AT STA 770, BL 24R T. INSTALLED CHANNELS AND SEAT TRACK IAW DC8 SRM 53-2-3 FIG DG. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04472 T ASK NR Y1583. 2 L 7 4 4F 4A25 1998040200234 19980402 00234 WP 1998 4 2 CKSA98174 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 860 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 860, BL 45RT. REMOVED THE DAMAGED CARGO TRACK AT STA 86 0, BL 45RT. CORROSION TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED CHANNELS AND PLUGS ON CARGO TRACK AT STA 860 BL 45RT IAW DC8 SRM 53-2-3 FIG 6D SHEET 1. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04471 TASK NR Y1582. 2 L 7 4 4F 4A25 1998040200235 19980402 00235 WP 1998 4 2 CKSA98175 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 1400 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND SEAT TRACK WORN, STA 1400, BL 45RT. CUT OUT DAMAGED AREA 2 PLACES FOR PLUG R EPAIR AT STA 1400 BL 45RT IAW DC8 SRM 53-2-3. TREATED AND PRIMED AREA OF REPAIR IAW DC8 SRM 51-1-8. INSTALLED PLUG REP AIRS IAW DC8 SRM 51-2-3 FIG 6D AT STA 1400. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 04470 TASK NR Y1581. 2 L 7 4 4F 4A25 1998040200236 19980402 00236 WP 1998 4 2 CKSA98176 1 19980228 A 5230 SKIN DOUG DC8 DC863F 302198F WP CARGO DOOR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND A PIT DOOR INNER SKIN CRACKED 2 PLACES UPPER FWD CORNER. STOP DRILLED CRACK AND FABRICATED, HEAT-TREATED, TREATED AND PRIMED AND INSTALLED DOUBLER ON CRACK A-PIT DOOR INNER SKIN IAW DC8 SRM 51-1-1 , 51-1-21, 52-4-1 PG 5. NON-ROUTINE NR 04424 TASK NR Y1557. 2 L 7 4 4F 4A25 1998040200237 19980402 00237 WP 1998 4 2 CKSA98177 1 19980228 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 902 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND FITTING CRACKED ON STA 902 FRAME RT SIDE 20 INCHES ABOVE CUSP. REMOVED DAMAGED FI TTING, FABRICATED NEW FITTING IAW DAC DWG NR 3779498. DRILLED UP NEW FITTING PER DC8 SRM 53-1-0 AND 51-1-20D. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING PER DC8 SRM 53-1-0 AND 51-1-20D. CORROSION TASK CARD NUMBER 573R-0551 . NON-ROUTINE NR 04795 TASK NR Y1254. 2 L 7 4 4F 4A25 1998040200238 19980402 00238 WP 1998 4 2 CKSA98178 1 19980228 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 857 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND FITTING CRACKED ON STA 857 FRAME RT SIDE 20 INCHES ABOVE CUSP. REMOVED FITTING FR OM STA 857 FRAME, FABRICATED FITTING IAW DAC DWG NR 3779498. LOCATE AND PICKED UP ALL ATTACHMENT LOCATIONS IAW DC8 SRM 51-1-20D. TREATED AND PRIMED FITTING IAW DC8 SRM 51-1-8. INSTALLED FITTING AT FS 857 FRAME IAW DC8 SRM 51-1-20D. CORR OSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04992 TASK NR Y1448. 2 L 7 4 4F 4A25 1998040200239 19980402 00239 WP 1998 4 2 CKSA98179 1 19980228 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 600 MISDRILLED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LT UPPER CUSP FITTING AT FS 600 DRILLED INTO. REMOVED LT UPPER CUSP FITTING AT FS 600. POSITION AND FITTED NEW CUSP FITTING IAW DC8 SRM 53-1-0. INSTALLED FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. COR ROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04902 TASK NR Y1391. 2 L 7 4 4F 4A25 1998040200240 19980402 00240 WP 1998 4 2 CKSA98180 1 19980228 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 710 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND RT WING L/E STA XFS710 LOWER SEAM SCREW HEADS PULLED THROUGH L/E SKIN. FABRI CATED FILLER PLATE FROM 7075-T6 .063 IAW SRM 57-2-1 FIG 2H PG 15 AND INSTALLED REPAIR ON RT WING L/E STA XFS710 LOWER SE AM SCREWS IAW SRM 57-2-1 FIG 2H PG 15. C-CHECK WORK CARD NUMBER 03766. NON-ROUTINE NR 04960 TASK NR Y1380. 2 L 7 4 4F 4A25 1998040200241 19980402 00241 WP 1998 4 2 CKSA98181 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 560 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 560, 5.5 ABOVE UPPER CUSP AREA. FABRICA TED REPAIR ANGLE IAW COTNEY DWG NR D93-R02. HEAT TREATED AND AGED IAW DC8 SRM 51-1-1. PERFORMED CONDUCTIVITY TEST ON H EAT TREATED ANGLE IT TEST TO 7075-0. TREATED AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-8. INSTALLED REPAIR ANGLES ON RT FRAME AT FS 560 5.5 ABOVE UPPER CUSP AREA IAW COTNEY DWG NR D93-R02. CORROSION TASK CARD NUMBER 573R-0551. NON-ROUTIN E NR 04877 TASK NR Y1298. 2 L 7 4 4F 4A25 1998040200242 19980402 00242 WP 1998 4 2 CKSA98182 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 480 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SEVERAL HOLES DRILLED INTO RT FRAME AT FS 480, 5.5 ABOVE UPPER CUSP AREA. PLUGGED HOLES, FABED SHIM, ANGLE AND DRILLED RT FRAME AT FS 480 IAW COTNEY DWG NR D93-R15 AND DC8 SRM 51-1-21 AND 51-1-8. CORR OSION TASK CARD NUMBER 573R-0551. NON-ROUTINE NR 04874 TASK NR Y1295. 2 L 7 4 4F 4A25 1998040200243 19980402 00243 WP 1998 4 2 CKSA98183 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 1560 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LT FRAME CRACKED AT FS 1560. REMOVED CUSP FITTING AND CUT OUT CRACKED FRAME SEGME NT ON LT FRAME STA 1560. FABRICATED NEW FRAME SEGMENT AND DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0 FIG 2 SHEET 4 VIEW J. HEAT TREATED 7075-0 .071 Z FRAME AND DOUBLER IAW DC8 SRM 51-1-1 PAR 1 THRU 4. TREATED AND PRIMED REPAIR PARTS Z FRAME SEGMENT, DOUBLERS AND FILLERS IAW DC8 SRM 51-1-8. INSTALLED CUSP FITTING IAW DC8 SRM 51-3-0. INSTALLED Z FRAME SEGMEN T AND DOUBLERS ALONG WITH THE FILLER IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04832 TASK NR Y1282. 2 L 7 4 4F 4A25 1998040200244 19980402 00244 WP 1998 4 2 CKSA98184 1 19980228 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 1000 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND HOLES DRILLED INTO RT UPPER CUSP FITTING AT FS 1000. REMOVED AND REPLACED CUSP FI TTING AT FS 1000 IAW DC8 SRM 51-1-20D AND 51-3-0. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04793 TASK NR Y 1252. 2 L 7 4 4F 4A25 1998040200245 19980402 00245 WP 1998 4 2 CKSA98185 1 19980228 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND LEFT WHEEL WELL BARE METAL WITH SLIGHT CORROSION ON TOP OF LONGERON 24 STA 98 0 AROUND 2 AFT BOLT HEADS. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND CRACK AT FS 980 ON LONGERON. STOP DRILLED CRAC K, FABRICATED REPAIR DOUBLER AND SHIM IAW DC8 SRM 53-2-2 FIG 5 SHEET 9. TREATED AND PRIMED REPAIR PARTS AND AFFECTED AR EA ON LONGERON 24LT IAW DC8 SRM 51-1-8. INSTALLED REPAIR AT FS 980 LONGERON 24 LT IAW DC8 SRM 53-2-2 FIG 5 SHEET 9. C- CHECK WORK CARD NUMBER 3010. NON-ROUTINE NR 02476 TASK NR Y0875. 2 L 7 4 4F 4A25 1998040200246 19980402 00246 WP 1998 4 2 CKSA98186 1 19980228 A 5311 FLANGE DOUG DC8 DC863F 302198F WP BS 420 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND FRAME FLANGE CRACKED STA Y420 ABOVE LONGERON 36. REMOVED INTERCOSTAL AT FS 420 TO ACCESS DAMAGE AREA FROM LONGERON 35 TO 36RT. REMOVED DAMAGE, FABRICATED PLUG AND 2 REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 2. HEAT TREATED AND AGED PARTS IAW DC8 SRM 51-1-1. LOCATED AND DRILLED UP PARTS. TREATED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED REPAIR AT STA 420 IAW DC8 SRM 53-2-0 PAGE 2U/2V. REINSTALLED INTERCOSTAL BETWEEN STA 400 TO 420 IAW DC8 SRM 51-1-20D AND 51-1-21. CORROSION TASK CARD NUMBER 5570-0551. NON-ROUTINE NR 03577 TASK NR Y0333. 2 L 7 4 4F 4A25 1998040200247 19980402 00247 WP 1998 4 2 CKSA98187 1 19980228 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 320-330 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND SKIN TORN DAMAGE TOP OF DOOR CUT OUT BOX FS 320 TO 330 ABOVE LONGERON 35 RT. ROUT ED OUT DAMAGED AREA AT FS 320 TO 330 LONGERON 35 RT. FABRICATED FILLER AND REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 1D. T REATED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 53-2-0 AND 51-1-21. CORROSION TASK CARD NUMBE R 5570-0551. NON-ROUTINE NR 03455 TASK NR Y0237. 2 L 7 4 4F 4A25 1998040200248 19980402 00248 WP 1998 4 2 CKSA98188 1 19980228 A 5347 36575011 SEAT TRACK DOUG DC8 DC863F 302198F WP LT COCKPIT WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND CAPT'S UPPER SEAT TRACKS WORN. REMOVED AND REPLACED BOTH FWD SEAT TRACK T'S AT CAPT'S POSITION IAW DC8 SRM 53-1-0 AND 51-1-20D. INSTALLATION OK. AFTER CAPT'S SEAT INSTALLATION SEAT TRACK AND SEA T OPERATES GOOD AT ALL LOCKING DETENTS IAW DC8 SRM 53-1-0 AND 51-1-20D AND ALSO DC8 MM 25-11-0. C-CHECK WORK CARD NUMBE R 0051. NON-ROUTINE NR 03442 TASK NR Y0225. 2 L 7 4 4F 4A25 1998040200249 19980402 00249 WP 1998 4 2 CKSA98189 1 19980228 A 5312 BULKHEAD ANGLE DOUG DC8 DC863F 302198F WP BS 1320 BROKEN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS FS 1320 HAS AREA BROKEN OUT AT TWO HOLES WHERE ATTACH ANGLE ATTACHES TO FRAME. REPAIRED BROKEN BULKHEAD ATTACH ANGLE RT SIDE BETWEEN C AND D PITS IAW DC8 SRM 53-2-0 FIG 1B AT FS 1320. CORROSION TASK CARD NUMBER 5590-0551. NON-ROUTINE NR 03382 TASK NR Y0171. 2 L 7 4 4F 4A25 1998040200250 19980402 00250 WP 1998 4 2 CKSA98190 1 19980228 A 5312 BULKHEAD WEB DOUG DC8 DC863F 302198F WP 9G BULKHEAD PUNCTURED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND NUMEROUS PUNCTURES ON LOWER END OF 9G BULKHEAD. FABRICATED REPAIR DOUBLERS T O REPAIR PUNCTURES ON LOWER END OF 9G BULKHEAD, DRILLED AND DEBURRED DOUBLERS AND BULKHEAD, TREATED, PRIMED AND INSTALLE D DOUBLERS IAW DC8 SRM 53-2-0 FIG 1B SHEET 2, 51-1-8, AND 51-1-21. C-CHECK WORK CARD NUMBER 0060. NON-ROUTINE NR 03224 TASK NR Y0026. 2 L 7 4 4F 4A25 1998040200251 19980402 00251 WP 1998 4 2 CKSA98191 1 19980228 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 285-315 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION SPOT ON LT SIDE OF LONG 34 RT AT FS Y298 INSIDE DOOR CUT OUT. CORROSION REMOVAL IS BEYOND LIMITS OF DC8 SRM 53-2-0 FIG 1F. REMOVED SECTION OF LONG 34R FROM FS 285 TO 315 INSIDE DOOR CUTOUT. ALSO, REMOVED BATHTUB FITTING BETWEEN LONG 34R AND 35R AT FS 300 DUE TO CORROSION ON FITTING. REPL ACED LONGERON AREA AND FABRICATED DOUBLERS PER DC8 SRM 53-2-2 FIG 10. REPLACED BATHTUB FITTING PER DC8 SRM 53-2-0 FIG 2 D. CORROSION TASK CARD NUMBER 5570-0551. NON-ROUTINE NR 05013 TASK NR X0064. 2 L 7 4 4F 4A25 1998040200252 19980402 00252 WP 1998 4 2 CKSA98192 1 19980228 A 5320 37509392N FITTING DOUG DC8 DC863F 302198F WP BS 1000 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION AND GOUGE MARK ON LT UPPER CUSP FITTING AT FS 1000. REMOVED OLD FITTING IAW DC8 SRM 53-1-0. DRILLED UP NEW FITTING ON LT UPPER CUSP AT FS 1000 IAW DC8 SRM 51-1-20D. INST ALLED NEW FITTING AT FS 1000 AT LT UPPER CUSP IAW DC8 SRM 51-1-21. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE N R 04823 TASK NR X0059. 2 L 7 4 4F 4A25 1998040200253 19980402 00253 WP 1998 4 2 CKSA98193 1 19980228 A 5320 4597643IN FITTING DOUG DC8 DC863F 302198F WP BS 580 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON UPPER CUSP FITTING AT FS 580 LT. REMOVED UPPER C USP FITTING AT STA 580 LT. CORROSION EVALUATION BEYOND LIMITS IAW DC8 SRM 53-2-0. TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20, 51-1-20D. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 048 16 TASK NR X0057. 2 L 7 4 4F 4A25 1998040200254 19980402 00254 WP 1998 4 2 CKSA98194 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION OF FLOOR FRAME STA 240 ABOVE LONGERON 35L A PIT. AF TER REMOVAL OF CORROSION FLOOR FRAME OUT OF LIMITS. FABRICATED REPAIR FILLER AND DOUBLERS IAW DC8 SRM 53-2-0 FIG 2. HE AT TREATED AND AGED PARTS IAW DC8 SRM 51-1-1. LOCATED AND DRILLED REPAIR PARTS. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2 ON FS 240 ABOVE LONGERON 35 LT. CORROSION TASK CARD NUMBER 5570-0551. NON- ROUTINE NR 02536 TASK NR X0029. 2 L 7 4 4F 4A25 1998040200255 19980402 00255 WP 1998 4 2 CKSA98195 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP COCKPIT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND COCKPIT FLOOR TRACK SECOND OBSERVERS SEAT FWD TRACK HAS CORROSION AROUND FAST ENERS. REMOVED AND REPLACED FWD FLOOR TRACK AT SECOND OBSERVERS SEAT IAW DC8 SRM 51-1-21. SEAT TRACK DRILLED IAW DAC D WG NR 3657504. PRIMED IAW DC8 SRM 51-1-8. C-CHECK WORK CARD NUMBER 0051. NON-ROUTINE NR 02284 TASK NR X0028. 2 L 7 4 4F 4A25 1998040200256 19980402 00256 WP 1998 4 2 CKSA98196 1 19980228 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP COCKPIT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND COCKPIT FLOOR TRACK SECOND OBSERVERS SEAT AFT TRACK HAS CORROSION AROUND FAST ENERS. REMOVED AND REPLACED AFT FLOOR TRACK AT SECOND OBSERVERS SEAT IAW DC8 SRM 51-1-21. SEAT TRACK DRILLED IAW DAC D WG NR 3657504. PRIMED TRACK IAW DC8 SRM 51-1-8 AND 51-3-0. C-CHECK WORK CARD NUMBER 0051. NON-ROUTINE NR 02258 TASK N R X0027. 2 L 7 4 4F 4A25 1998040200257 19980402 00257 WP 1998 4 2 CKSA98197 1 19980228 A 5320 3642974502 FITTING DOUG DC8 DC863F 302198F WP BS 680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON FRAME TO SPAR FITTING CENTER WING UPPER SKIN UNDER CUSP RIGHT SIDE ST A680 X=-64. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED FITTING AND REPLACED WITH NEW FITTING IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 2000-0551. NON-ROUTINE NR 02199 TASK N R X0021. 2 L 7 4 4F 4A25 1998040200258 19980402 00258 WP 1998 4 2 CKSA98198 1 19980228 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 340 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON FITTING AT FS 340 BETWEEN LONGERON 34R AND 35R. C ORROSION IS OUT OF LIMITS. REMOVED FITTING FROM STA 340 BETWEEN L34R AND 35R. CUT NEW FITTING, FABRICATED SPLICES IAW DC8 SRM 53-2-0 FIG 2D. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 5570-0551. NON-ROUTINE NR 03824 TASK NR X0016. 2 L 7 4 4F 4A25 1998040200259 19980402 00259 WP 1998 4 2 CKSA98199 1 19980228 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 288 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. NR 1 T-BOLT BACK-UP FITTING CORRODED STA Y288. REMOVED NR 1 T BOLT BACK UP FITTING AT STA Y288. CLEANED AND PRIMED AREA IAW DC8 SRM 51-1-8. DRILLED NEW FITTING AND FABRICATED REPA IR SPLICES IAW DC8 SRM 53-2-0 PG 15 AND 16. INSTALLED FITTING ON STA Y288 IAW DC8 SRM 51-1-21D. CORROSION TASK CARD NU MBER 5570-0551. NON-ROUTINE NR 03532 TASK NR X0014. 2 L 7 4 4F 4A25 1998040200260 19980402 00260 WP 1998 4 2 CKSA98200 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 180 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION ON FWD FACE OF FRAME AT FS Y180 ABOVE LONGERON 34R. CORROSION REMOVAL BEYOND DC8 SRM LIMITS IAW DC8 SRM 51-1-8 AND 53-2-0 FIG 7. HEAT TREATED AND AGED DOUBLER IAW DC8 SRM 51-1-1. LOCATED AND DRILLED UP. FABRICATED DOUBLER IAW DC8 SRM 53-2-0 FIG 2. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER AT STA Y180 ABOVE LONGERON 34R IAW DC8 SRM 53-2-0 PAGE 2U/2V FIG 2, 51-1-20D AND 51-1-21. CORROSION TASK CARD NUMBER 5570-0551. NON-ROUTINE NR 03424 TASK NR X0003. 2 L 7 4 4F 4A25 1998040200261 19980402 00261 WP 1998 4 2 CKSA98201 1 19980228 A 5230 SKIN DOUG DC8 DC863F 302198F WP CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE C-2 CHECK INSPECTION, FOUND B-PIT DOOR HAS CORROSION ON LOWER SEAL CHANNEL FWD LOWER TO AFT LOWER. REMOV ED MINOR SURFACE CORROSION ON LOWER AFT CORNER AND AREA BETWEEN FWD AND AFT CORNER. .002 METAL REMOVED IS WITHIN LIMITS IAW DC8 SRM 52-2-0 FIG 6; CORROSION ON LOWER FWD CORNER WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER, DRIL LED, DEBURRED, AND TREATED REPAIR DOUBLER. TREATED AND PRIMED ALL AFFECTED AREAS ON DOOR SEAL CHANNEL, INSTALLED REPAIR DOUBLER ON FWD LOWER CORNER IAW DC8 SRM 51-1-8, 51-1-21, 52-2-2. C-CHECK WORK CARD NUMBER 3007. NON-ROUTINE NR 05018 TASK NR X0065. 2 L 7 4 4F 4A25 1998040200262 19980402 00262 NE 1998 4 2 TC8A98016 2 19980325 A 7230 COMPRESSOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 181SK 45910 ABORTEDTAKEOFF DUE TO LOUD NOISE. RAN ENGINES 1, 2, 3, 4 WITH ANTI-ICE AND BLEED VALVES ON, BLEED VALVE OPS CHECKED NOR MAL IAW MIP CHPT 2 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1998040200263 19980402 00263 WP 1998 4 2 SABA980013 2 19980210 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UHR WP RIGHT FAILED A SABA E ENGINE SHUTDOWN P NO WARNING INDICATION CR CRUISE 1 SO 33 941AE 6052 293 941 P66299C FAY - FLT 5078 - ON FLIGHT FROM OAJ TO CLT, PILOT STATED THERE WAS A SLIGHT ENGINE SURGE AND RAPIDLY FOLLOWED BY A RT EN GINE SHUTDOWN. ALL ENGINE INDICATIONS NORMAL PRIOR TO SHUTDOWN OF RT ENGINE. AIRCREW DECLARED AN IN-FLIGHT EMERGENCY. AIRCREW ALSO TRIED TO AIRSTART. THE ENGINE WOULD NOT START WITH 30 PERCENT RPM. AIRCRAFT DIVERTED INTO FAYETTEVILLE. EMERGENCY PROCEDURES WERE USED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE DEPLOYED FROM CLT TO FAY. MAINTE NANCE REMOVED AND REPLACED THE RT ENGINE. AIRCRAFT RETURNED TO SERVICE AT 1,620 HOURS 2-12-98. PART TOTAL CYCLES: 10, 626. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1998040200264 19980402 00264 NE 1998 4 2 SABA980017 3 19980311 A 6111 PROP BLADE BAG JETSTM JETSTM3201 1500217 EU MCAULY 4HFR34 4HFR34C653 NE RT ENGINE LOOSE A SABA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 33 928AE 7170 941749 928 941749 CLT - FLT 5172 - ON FLIGHT FROM CLT TO NTS, AIRCREW REPORTED A SEVERE VIBRATION AFTER TAKEOFF. AIRCRAFT RETURNED TO CLT . NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND ONE OF THE BLADES, IN THE RIGH T PROP, HAD SLIPPED IN THE HUB. RT PROPELLER REMOVED AND REPLACED. ENGINE RUN, RIGGED, LEAK AND OPS CHECKED GOOD. AIR CRAFT RETURNED TO SERVICE. PART TOTAL CYCLES: 11,367. (X) 2 L 7 2 4T RT A56EU 6 C 3PNE 1998040200265 19980402 00265 WP 1998 4 2 SABA980019 2 19980315 A 7321 89778024 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE FAILED A SABA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 33 920AE 2170302 920 SOP - FLT 5022 - ON FLIGHT FROM CLT TO ISO, THE RT ENGINE RPM DROPPED AND FUEL CAPTION LIGHT CAME ON. AIRCREW COULD NOT REGAIN POWER, SO THE ENGINE WAS SHUT DOWN. IN-FLIGHT EMERGENCY WAS DECLARED AND EMERGENCY PROCEDURES WERE USED. AIRCR AFT DIVERTED AND LANDED AT SOP WITH NO OTHER PROBLEMS. MAINTENANCE FOUND A BAD RIGHT FUEL CONTROL. REMOVED AND REPLACE D RIGHT FUEL CONTROL. RIGGED, LEAK AND OPS CHECKED GOOD. TEST FLIGHT C/W AND RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A56EU E4WE 1998040200266 19980402 00266 NM 1998 4 2 AALA980294 1 19980210 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 580-585 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - STR 28L CORRODED STA 580 - STA 585. REMOVED CORE, INSTALLED STRINGER REPAIR IAW SRM 53-10-3. TST: 54,870.3 HOUR S. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200267 19980402 00267 NM 1998 4 2 AALA980296 1 19980210 A 5330 SKIN BOEING 727 727223 1384074 NM BS 584 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - SKIN CORRODED UNDER STR 28L. REMOVED CORROSION, INSTALLED DOUBLER REPAIR IAW SRM 53-30-10. TST: 54,870.3 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200268 19980402 00268 NM 1998 4 2 AALA980295 1 19980210 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 743 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - STR 17R CRACKED AT FORWARD END FASTENER HOLE STA 743. STOP DRILLED CRACK. INSTALLED DOUBLER IAW AARD 51-40-00-1. TST: 54,870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200269 19980402 00269 NM 1998 4 2 AALA980297 1 19980210 A 5720 SUPPORT BOEING 727 727223 1384074 NM WS 112 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CRACK IN VERTICAL STIFFENER ATTACH ANGLE AT FORWARD SPAR, STA 112 LEFT, OTBD OF FORWARD BOTTLE PIN. REPAIRED VERT ICAL STIFFENER PER SRM 51-40-3, PAGE 2. TST: 51,688.24 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998040200270 19980402 00270 NM 1998 4 2 AALA980298 1 19980210 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION INSIDE OF STR 28R AT BS 950E +2 INCHES. REMOVED CORROSION PER SRM 51-10-6, REPAIRED STR PER ESO 11697 D ATED 2-2-98. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998040200271 19980402 00271 NM 1998 4 2 AALA980299 1 19980210 A 5510 TIE CAP BOEING 727 727223 1384074 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION RT HORIZONTAL STABILIZER UPPER T/E HINGE CAP. THREE LOCATIONS ABOVE NR'S 4, 5, AND 7, ELEVATOR HINGE PO INTS. REMOVED CORROSION AND REPAIRED PER ESO 11697 DATED 2-5-98. ALL THREE LOCATIONS. TST: 51,688 HOURS. CYCLES: 3 1,372. (X) 2 L 7 3 4F A3WE 1998040200272 19980402 00272 EU 1998 4 2 AALA980359 1 19980217 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - FRAME 58 CORRODED AT LONGERON 55R TO 55L. INSTALLED DOUBLER PER SRM 53-10-13. TST: 25,415.42 HOURS. CYCLES: 9, 488. (X) 2 L 7 2 4F RT A35EU 1998040200273 19980402 00273 EU 1998 4 2 AALA980371 1 19980218 A 5320 SILL AIRBUS 300 A300B4605R 3930308 EU BS 1711-1722 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - CORROSION AROUND SEVERAL ROLLER TRAY ATTACH HOLES IN SILL BEAM AT FORWARD CARGO DOOR. REMOVED CORROSION, TREATED, PRIMED, AND PAINTED AREA THEN INSTALLED 2 EACH STRAPS AT FR 25 AND FR 25A PER ESO 30595 DATED 2-11-98. TST: 265,415.4 2 HOURS. CYCLES: 9,488. (X) 2 L 7 2 4F RT A35EU 1998040200274 19980402 00274 EU 1998 4 2 AALA980372 1 19980218 A 5754 STRUCTURE AIRBUS 300 A300B4605R 3930308 EU LE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 25071 514 TUL - CORROSION INSIDE MAIN SECTION OF KRUEGER FLAP. REPLACED MAIN KRUEGER FLAP WITH NEW SERVICEABLE FLAP. TST: 25,41 5.42 HOURS. CYCLES: 9,488. (X) 2 L 7 2 4F RT A35EU 1998040200275 19980402 00275 WP 1998 4 2 AALA980375 1 19980219 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 816-822 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON LONGERON 52 STA 816 TO STA 822 ON RT SIDE OF LONGERON. REMOVED AND REPLACED CORRODED LONGERON SECTIO N PER SRM 53-10-00. TST: 60,422 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998040200276 19980402 00276 WP 1998 4 2 AALA980376 1 19980218 A 5320 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 1781-1779 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 CORROSION IN OMNI-ROLLER TRAY AFT END OF TRAY IN CORNER STA 1781 - STA 1779 AFT. FABRICATED NEW OMNI-ROLLER TRAY TRACK, ALODINED AND PRIMED, AND PAINTED NEW TRAY. REF: SRM 53-70-00 PAGE 29 VOL 1 AND SRM 51-21-01 VOL II, AND INSTALLED NEW TRACK IN FRAME. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998040200277 19980402 00277 WP 1998 4 2 AALA980384 1 19980219 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 879-749 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - T-ANGLE FROM SLANT PANEL TO TRAY LBL 65 STA 879 TO STA 749 IS CORRODED. REPLACED CORRODED SECTION OF T-ANGLE PER SRM 51-01-00-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998040200278 19980402 00278 NM 1998 4 2 AALA980385 1 19980220 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1010-1020 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CUT OUT SKIN UNDER STR 29R AT STA 1010 TO STA 1020 FOR STRINGER REMOVAL. FABRICATED AND INSTALLED DOUBLER STA 101 0 AT STR 29R PER SRM 53-30-3. TST: 54,868.47 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200279 19980402 00279 NM 1998 4 2 AALA980386 1 19980220 A 5330 SKIN BOEING 727 727223 1384074 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - CORROSION UNDER STR 28R AFT OF STA 480. SKIN BULGED, RIVETS POPPED. INSTALLED SKIN DOUBLER AT STRINGER SPLICE PE R SRM 53-10-3 PAGE 3, 53-30-3, FIG 3, PAGE 14A. TST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998040200280 19980402 00280 NM 1998 4 2 AALA980387 1 19980220 A 5330 SKIN BOEING 727 727223 1384074 NM BS 600 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - SEVERAL DEEP GOUGES ON FUSELAGE SKIN. REMOVED SHEAR TIE, STA 600 BETWEEN STR 26 AND STR 27L. INSTALLED EXTERNAL DOUBLER IAW SRM 53-30-3. TST: 54,868 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200281 19980402 00281 NM 1998 4 2 AALA980388 1 19980220 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1010-1016 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION IN STR 26L, STA 1010 TO STA 1016. CUT CORRODED SECTION OUT. INSTALLED STR REPAIR PER SRM 53-10-3. TST : 54,868.47 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200282 19980402 00282 NM 1998 4 2 AALA980389 1 19980220 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION ON STR 29R STA 950E TO STA 950E +10 INCHES. REMOVED CORROSION, CUT OUT STRINGER, INSTALLED NEW STRINGER FROM 950D +10 INCHES TO STA 1010 PER AARD 53-10-03-1 PAGE 1. (X) 2 L 7 3 4F A3WE 1998040200283 19980402 00283 NM 1998 4 2 AALA980390 1 19980220 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION ON FLOOR BEAM STA 380 FROM RT INBD SEAT TRACK TO GALLEY DOOR THRESHOLD TOP AND BOTTOM. INSTALLED REPAIR PER AARD 53-10-07 AND TREATED AND PRIMED PER SRM 51-20-0. TST: 54,868 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200284 19980402 00284 NM 1998 4 2 AALA980391 1 19980220 A 5711 SPAR CHORD BOEING 727 727223 1384074 NM WS 512-515 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - HEAVY CORROSION ON LOWER SPAR CHORD UNDER NR 6 SLAT AT FSS 512 - FSS 515, RT WING. INSTALLED DOUBLER REPAIR PER B 727 AARD/DC 57-30-00-2. ALODINED AND PRIMED AREA PER 51-10-2 AND 51-20-14 (SRM). SEALED REPAIR PER 51-30-0 FIG 4MM. T ST: 51,688 HOURS. CYCLES: 31,372. (X) 2 L 7 3 4F A3WE 1998040200285 19980402 00285 NM 1998 4 2 AALA980392 1 19980220 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1010-1016 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - HEAVY CORROSION IN STR 27L, STA 1010 - STA 1016. REPAIRED STRINGER PER SRM 53-10-3, FIG 1. TST: 54,868 HOURS. C YCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200286 19980402 00286 NM 1998 4 2 AALA980393 1 19980220 A 5311 FRAME BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION ON 580 BOLT FRAME AND SHEAR TIE STR 26L - STR 27L. REMOVED CORROSION FROM BELT FRAME AT INSTALLED NEW S HEAR TIE. TST: 54,868 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200287 19980402 00287 1998 4 2 AALA980407 4 19980226 A 2565 CABLE BOEING 727 727223 1384074 NM DOOR SLIDE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - GIRT BAR LANYARD, CABLE BROKEN AT THE SLIDE RELEASE PAWL MECHANISM (OVERHAUL DUE 7-98). REMOVED AND REPLACED SLID E PER MM. TST: 44,584 HOURS. CYCLES: 24,187. (X) 2 L 7 3 4F A3WE 1998040200288 19980402 00288 NM 1998 4 2 AALA980408 1 19980226 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 724 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - STRINGER 27R HAS CORROSION INSIDE STA 724. REPAIRED STRINGER PER SRM 53-10-3 FIG 1. TST: 44,584 HOURS. CYCLES: 24,187. (X) 2 L 7 3 4F A3WE 1998040200289 19980402 00289 NM 1998 4 2 AALA980409 1 19980226 A 5510 BEAM BOEING 727 727223 1384074 NM LT HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - LEFT HORIZONTAL STABILIZER TRAILING EDGE BEAM HAS CORROSION ON UPPER SURFACE ABOVE NR 1 AND NR 4 ELEVATOR HINGE BE ARINGS. REMOVED CORROSION AND INSTALLED DOUBLERS PER SRM 55-10-6 FIG 1 AND ESO 11697 DATED 2-19-98. TST: 44,584 HOURS . CYCLES: 24,187. (X) 2 L 7 3 4F A3WE 1998040200290 19980402 00290 NM 1998 4 2 AALA980410 1 19980226 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 735-740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - STR 27R HAS CORROSION INSIDE AT STA 735 - STA 740. REPAIRED STRINGER PER SRM 53-10-3 FIG 1. TST: 44,584 HOURS. CYCLES: 24,187. (X) 2 L 7 3 4F A3WE 1998040200291 19980402 00291 NM 1998 4 2 AALA980411 1 19980226 A 5330 SKIN BOEING 727 727223 1384074 NM BS 405 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA 22467 TUL - STA 405 ABOVE STR 24L - DENT WITH 2 DEEP GOUGES. GOUGES HAVE BEEN WORKED, BUT HAVE IMPROPER BLEND RATIO. REMOVED DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3, PAGES 12-14A. TST: 44,584 HOURS. CYCLES: 24,187. (X) 2 L 7 3 4F A3WE 1998040200292 19980402 00292 WP 1998 4 2 AALA980425 1 19980226 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 234AA 49181 TUL - TOP OF FLOORBEAM IS CORRODED. CUT OUT CORRODED AREA, INSTALLED 2 INCH FILLER PLUG WITH 20.5 INCH DOUBLER STARTING AT 11 INCHES FROM RT SIDE OF FLOORBEAM PER SRM 53-05 FIG 20A. TST: 44,152 HOURS. CYCLES: 24,579. (X) 2 L 7 2 4F A6WE 1998040200293 19980402 00293 WP 1998 4 2 AALA980426 1 19980302 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 218 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 234AA 49181 TUL - FORWARD LAVATORY TANK FORWARD TIE-DOWN BRACKET CORRODED ON FRAME APPROXIMATELY 10 INCHES ABOVE CUSP. FRAME REPAIR ED PER SRM 53-03 FIG 2A. TST: 44,152 HOURS. CYCLES: 24,579. (X) 2 L 7 2 4F A6WE 1998040200294 19980402 00294 NM 1998 4 2 AALA980427 1 19980303 A 5510 HINGE BOEING 727 727223 1384074 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - CORROSION ON TOP OF T/E, OUTBOARD OF NR 6 ELEVATOR HINGE, HORIZONTAL STABILIZER, T/E CHORD RIGHT. REPAIRED CORROD ED AREA PER ESO 11697, TREATED, PRIMED, AND PAINTED. TST: 57,207 HOURS. CYCLES: 35,211. (X) 2 L 7 3 4F A3WE 1998040200295 19980402 00295 NM 1998 4 2 AALA980428 1 19980303 A 5510 HINGE BOEING 727 727223 1384074 NM HORIZONTAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - CORROSION ON TOP OF HORIZONTAL STABILIZER T/E INBOARD OF NR 6 HINGE (ELEV) RIGHT. REPAIRED CORRODED AREA PER ESO 11697. TREATED, PRIMED, AND PAINTED. TST: 57,207 HOURS. CYCLES: 35,211. (X) 2 L 7 3 4F A3WE 1998040200296 19980402 00296 NM 1998 4 2 AALA980430 1 19980303 A 5511 SPAR BOEING 727 727223 1384074 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - AFT SPAR OF LEFT HORIZONTAL STABILIZER CORRODED AT NR 1 HINGE, TOP SIDE. INSTALLED DOUBLER REPAIR PER ESO 11697 D ATED 2-25-98. TST: 57,207 HOURS. CYCLES: 35,211. (X) 2 L 7 3 4F A3WE 1998040200297 19980402 00297 NM 1998 4 2 AALA980431 1 19980303 A 5312 BULKHEAD BEAM BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - FORWARD SIDE 1183 BULKHEAD LBL 8, VERTICAL STIFFENER CRACKED IN RADIUS OUTBOARD SIDE ABOVE RADIUS BLOCK. STOP DRI LLED END OF CRACK AND INSTALLED REPAIR DOUBLERS IAW SB 727-53-0175, FIG 3. TST: 57,207 HOURS. CYCLES: 35,211. (X) 2 L 7 3 4F A3WE 1998040200298 19980402 00298 NM 1998 4 2 AALA980451 1 19980306 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 712AA 22468 TUL - CORROSION ON SKIN AFT OF STA 720C OUTBOARD OF STR 27L, AREA 4 INCHES BY 2.50 INCHES. AREA PREVIOUSLY REWORKED. C UT OUT CORROSION ON SHIM AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. TST: 45,340.49 HOURS. CYCLES: 24,417. (X) 2 L 7 3 4F A3WE 1998040200299 19980402 00299 NM 1998 4 2 AALA980453 1 19980304 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION IN STR 28R. REMOVED SECTION AT STR 28R AND INSTALLED NEW SECTION PER ESO 11697 DATED 2-9-98. TST: 54, 870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200300 19980402 00300 NM 1998 4 2 AALA980454 1 19980305 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION ON LOWER INSIDE ANGLE OF DELTA BEAM AT FORWARD LEFT CORNER. INSTALLED STAINLESS STEEL CAD PLATE STIFFEN ER AT FORWARD ROW OF DELTA BEAM WEB PER 51-40-4 PAGES 1-5. TST: 54,870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200301 19980402 00301 NM 1998 4 2 AALA980455 1 19980305 A 5330 SKIN BOEING 727 727223 1384074 NM BS 745 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - CORROSION ON LOWER SKIN OF DELTA BEAM FROM STA 745 TO STA 770 AND STA 780 TO STA 791. REPLACED DELTA BEAM FROM ST A 740 - STA 785 PER SRM 51-40-02. TST: 54,870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200302 19980402 00302 NM 1998 4 2 AALA980456 1 19980305 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - LEVELING COMPOUND CRACKED AND BULGED STA 680 AFT SIDE TOP SIDE OF STR 27R. REMOVED LEVELING COMPOUND, FOUND CORRO SION OUT OF LIMITS, INSTALLED DOUBLER IAW SRM 53-30-3. TST: 54,870 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200303 19980402 00303 NM 1998 4 2 AALA980457 1 19980304 A 5320 WEB BOEING 727 727223 1384074 NM BS 1255 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 879AA 21391 TUL - HORIZONTAL WEB CRACKED AT STA 1255 RBL 27 TO RBL 33. INSTALLED DOUBLER PER ESO 11697 DATED 2-19-98. TST: 54,870 .3 HOURS. CYCLES: 33,161. (X) 2 L 7 3 4F A3WE 1998040200304 19980402 00304 NM 1998 4 2 AALA980458 1 19980306 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1140-1160 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 712AA 22468 TUL - CORROSION ON STR 30 AT STA 1140 TO STA 1160. CUT OUT CORROSION AND INSTALLED REPAIR PER SRM 53-10-3, PAGE 3. TST : 45,340.49 HOURS. CYCLES: 24,417. (X) 2 L 7 3 4F A3WE 1998040200305 19980402 00305 NM 1998 4 2 AALA980467 1 19980309 A 5330 SKIN BOEING 727 727223 1384074 NM BS 430 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - SMALL CRACK IN SKIN STA 430 BETWEEN STR 20R AND STR 19R. REPAIRED PER SRM 53-30-3 FIG 13. REPAIRED INSIDE DOUBLE R PER SRM 51-20-01-5. TST: 77,619 HOURS. CYCLES: 53,030. (X) 2 L 7 3 4F A3WE 1998040200306 19980402 00306 NM 1998 4 2 USAABB98022 1 19980308 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 LAX - FLOOR EMERGENCY LIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F RT A2NM 1998040200307 19980402 00307 EU 1998 4 2 USAASB98048 2 19980224 A 7260 3353228010 COVER BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563C1 13802 EU NR 2 ENGINE LOOSE A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 419US 23986 TPA - FLT 1080 - ON CLIMB-OUT FROM TPA GOING THROUGH 10,000 FEET, THE NR 2 ENGINE OIL QUANTITY DROPPED TO ZERO FOLLOWED BY THE OIL PRESSURE DROPPING TO ZERO. CAPTAIN SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT TPA. FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 13 MINUTES. MAINTENANCE FOUND THE NR 2 ENG INE N2 ROTOR ROTATION PAD COVER ON THE ACCESSORY GEARBOX ABOVE THE STARTER LEAKING. SECURED SAME. SERVICED OIL AND RAN ENGINE. LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F RT A16WE E21EU 1998040200308 19980402 00308 NM 1998 4 2 USAA980107 1 19980228 A 5330 SKIN BOEING 737 737201 1384454 NM BS 379 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 379 BETWEEN BL ZERO AND S28L SKIN (FUSELAGE). INSTALL ED DOUBLER, REPAIRED PER TR 53-30-04. (X) 2 L 7 2 4F A16WE 1998040200309 19980402 00309 NM 1998 4 2 USAA980108 1 19980228 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 2 EACH SKIN ATTACH FASTENER HOLES 7 INCHES AND 8 INCHE S FORWARD OF BS 540 FRAME S15R STRINGER FUSELAGE. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3 FIG 1 AND EA 4 3631. (X) 2 L 7 2 4F A16WE 1998040200310 19980402 00310 NM 1998 4 2 USAA980111 1 19980228 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK BS 663 BL ZERO WL 205 FLOORBEAM WEB. INSTALLED DOUBLER, REPAIRED PER BAC DRAWING NR 65C34537. (X) 2 L 7 2 4F A16WE 1998040200311 19980402 00311 NM 1998 4 2 USAA980112 1 19980228 A 5330 SKIN BOEING 737 737201 1384454 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK FORWARD ENTRY DOOR FUSELAGE LOWER AFT CORNER WL 207, ST A 344 SKIN. INSTALLED DOUBLER, REPAIRED PER BOEING DWG 65C27257. (X) 2 L 7 2 4F A16WE 1998040200312 19980402 00312 NM 1998 4 2 USAA980113 1 19980228 A 5330 SKIN BOEING 737 737201 1384454 NM BS 304 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK BS 304 BETWEEN S9L AND S10L SKIN. (EDDY CURRENT). INS TALLED DOUBLER, REPAIRED PER EA 43634. (X) 2 L 7 2 4F A16WE 1998040200313 19980402 00313 NM 1998 4 2 USAA980114 1 19980228 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 340-360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH BY 15 INCH CORROSION ON STR 25R FROM STA 360 - STA 340. INSTAL LED NEW STRINGER, REPAIRED PER SRM 53-10-3 FIG 1. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1998040200314 19980402 00314 NM 1998 4 2 USAA980115 1 19980218 A 5314 KEEL BEAM BOEING 767 767201 1385125 NM BS 860 ERODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 41917 23899 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 6 INCH BY .035 INCH DEEP ERODED AREA 1 FOOT FORWARD OF ACCES S HOLE FOR LOWER ANTI-COLLISION WIRING IN KEEL BEAM JUST FORWARD OF BS 860. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 61191. (X) 2 L 7 2 4F RT A1NM 1998040200315 19980402 00315 NM 1998 4 2 USAA980116 1 19980219 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 470 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 37012 23311 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND EVIDENCE OF LIGHT CORROSION ON SKIN STA 470 BETWEEN STR 28R AND STR 28L. CORROSION TASK NR C 53-208-01. INSTALLED DOUBLER PER REPAIR DOCUMENT SRM 53-00-01 FIG 202. (X) 2 L 7 2 4F RT A16WE 1998040200316 19980402 00316 WP 1998 4 2 AALA980424 1 19980302 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1209 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 234AA 49181 TUL - CORROSION ON SEAT TRACK AT STA 1209, NUT PLATE MOUNT HOLE FOR GALLEY. REPLACED NR 1 SEAT TRACK STA 1174 - STA 130 9. (X) 2 L 7 2 4F A6WE 1998040200317 19980402 00317 WP 1998 4 2 AALA980383 1 19980219 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP BS 875 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 FORMED SECTION (DOOR POCKET) U-CHANNEL IS CORRODED AT STA 875 LONGERON 38L TO LONGERON 43L (SLANT PANEL WALL). REPLACED CORRODED U-CHANNEL AT STA 875 LONGERON 38L TO LONGERON 43L PER SRM 51-01-00-05. (X) 2 L 7 3 4F A22WE 1998040200318 19980402 00318 1998 4 2 HEEA0013411 4 19980318 A 3421 501125501 VERTICAL GYRO BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 VERT GYRO PRECESSES. 2 G 7 2 4U H10SW 1998040200319 19980402 00319 SW 1998 4 2 HEEA0013412 1 19980318 A 7931 206075677103 INDICATOR BELL 206 206L3 1182108 SW ENG OIL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 8588X 51486 LEAKING OIL AT FACE. PRESSURE SIDE HIGH OUT OF TOLERANCE. 1 G 7 1 3U H2SW 1998040200320 19980402 00320 SW 1998 4 2 HEEA0013413 1 19980318 A 2840 206075186005 INDICATOR BELL 206 206L1 1182107 SW COCKPIT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3892R 45594 INDICATOR LOAD SIDE ERRATIC AND HAS FRICTION. 1 G 7 1 3U H2SW 1998040200321 19980402 00321 1998 4 2 HEEA0013414 4 19980318 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW COCKPIT HSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 COCKPIT HSI RATCHETY WHEN POWER IS APPLIED. 1 G 7 2 4U H4SW 1998040200322 19980402 00322 NE 1998 4 2 HEEA0013415 2 19980318 A 7210 3017600 GEARBOX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE OIL TEMP PORT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 14364 36002 ENG HAS CRACKED GEARBOX AT OIL TEMP BULB PORT. 1 G 7 2 4U 4 U H4SW E22EA 1998040200323 19980402 00323 SW 1998 4 2 HEEA0013418 1 19980318 A 2436 51539002N CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 GENERATOR WILL NOT COME ON LINE. CONTROL UNIT FAILED 1 G 7 2 4U H4SW 1998040200324 19980402 00324 SW 1998 4 2 HEEA0013419 1 19980318 A 2436 51539002N CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 GENERATOR WILL NOT COME ON LINE. CONTROL UNIT FAILED 1 G 7 2 4U H4SW 1998040200325 19980402 00325 SW 1998 4 2 HEEA0013420 1 19980318 A 2436 51539002N CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 WILL NOT COME ON LINE. CONTROL UNIT FAILED 1 G 7 2 4U H4SW 1998040200326 19980402 00326 1998 4 2 HEEA0013421 4 19980318 A 3425 125810 HSI SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 HSI COURSE SET KNOB AND NEEDLE DOES NOT WORK. 1 G 7 2 3U H1NE 1998040200327 19980402 00327 1998 4 2 HEEA0013422 4 19980318 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141PH 33197 ATTITUDE INDICATOR PITCHBALL ERRATIC IN MOVEMENT. KNOB INTERMITTENT. 1 G 7 2 4U H4SW 1998040200328 19980402 00328 SW 1998 4 2 HEEA0013423 1 19980318 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 33020 NR 1 NEEDLE STICKS AND INDICATES LOW OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998040200329 19980402 00329 NE 1998 4 2 HEEA0013424 1 19980318 A 6210 SB7004103 BEARING SKRSKY S76 S76A 8143006 NE BLADE SPINDLE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 BEARING HAS EXCESSIVE RUBBER WEAR. 1 G 7 2 3U H1NE 1998040200330 19980402 00330 SW 1998 4 2 HEEA0013425 1 19980318 A 6710 206062721113 ACTUATOR BELL 206 206B3 1181506 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2145C 3456 ACTUATOR MOTOR DOES NOT FUNCTION. 1 G 7 1 3U H2SW 1998040200331 19980402 00331 SW 1998 4 2 HEEA0013426 1 19980318 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 STEP ACTUATOR CAUSES STEP CIRCUIRT BREAKER TO POP. 1 G 7 2 4U H4SW 1998040200332 19980402 00332 SW 1998 4 2 HEEA0013427 1 19980318 A 3340 A490ATSDF1428 POWER SUPPLY BELL 206 206B3 1181506 SW STROBE INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2145C 3456 POWER SUPPLY INTERMITTENT. 1 G 7 1 3U H2SW 1998040200333 19980402 00333 SW 1998 4 2 HEEA0013428 1 19980318 A 2400 M833830209 CIRCUIT BREAKER BELL 214 214ST 1182106 SW ELECT SYS OPEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 RELAY IS STUCK OPEN. 2 G 7 2 4U H10SW 1998040200334 19980402 00334 1998 4 2 HEEA0013430 4 19980318 A 3425 4018369902 FLIGHT DIRECTOR BEECH 200 200BEECH 1152920 CE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 789DS BB478 ALTITUDE SELECT MODE INOPERATIVE. 1 L 7 2 4T A24CE 1998040200335 19980402 00335 1998 4 2 HEEA0013431 4 19980318 A 3444 7001840913 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 TRANSCEIVER WILL NOT TEST. ERRATIC READING. 1 G 7 2 3U H1NE 1998040200336 19980402 00336 NE 1998 4 2 HEEA0013432 1 19980318 A 2424 7655009005104 GENERATOR CONT SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 A/C GEN. WILL NOT TEST IN THE OVERVOLT AND UNDERVOLT POSITION. 1 G 7 2 3U H1NE 1998040200337 19980402 00337 NE 1998 4 2 HEEA0013433 1 19980318 A 2424 7655009005108 GENERATOR CONT SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 GENERATOR WILL NOT COME ON LINE. 1 G 7 2 3U H1NE 1998040200338 19980402 00338 1998 4 2 HEEA0013434 4 19980318 A 2210 1177130501 CONVERTER BOLKMS 117 BK117B1 5626012 EU AUTO FLIGHT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 CONVERTER WORN OUT. SHAFT HAS TOO MUCH PLAY. 1 G 7 2 3U H13EU 1998040200339 19980402 00339 SW 1998 4 2 HEEA0013435 1 19980318 A 2842 206364601101 TRANSMITTER BELL 206 206L3 1182108 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8590X 51494 TRANSMITTER FLUCTUATES. 1 G 7 1 3U H2SW 1998040200340 19980402 00340 SW 1998 4 2 HEEA0013436 1 19980318 A 2840 206064636103 PROBE BELL 206 206L3 1182108 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8590X 51494 PROBE FLUCTUATES. 1 G 7 1 3U H2SW 1998040200341 19980402 00341 NE 1998 4 2 HEEA0013437 1 19980318 A 3340 A413AHDACF1428 POWER SUPPLY SKRSKY S76 S76A 8143006 NE STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 LIGHT INOPERATIVE. 1 G 7 2 3U H1NE 1998040200342 19980402 00342 SW 1998 4 2 HEEA0013438 1 19980318 A 2430 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 CONTROL UNIT FAILED. NO OUTPUT. 1 G 7 2 4U H4SW 1998040200343 19980402 00343 SW 1998 4 2 HEEA0013439 1 19980318 A 2430 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 NO OUTPUT. CONTROL UNIT FAILED 1 G 7 2 4U H4SW 1998040200345 19980402 00345 SW 1998 4 2 HEEA0013441 1 19980318 A 2430 51509002R CONTROL UNIT BELL 412 412 1182202 SW NR 1 DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 NR 1 GENERATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998040200346 19980402 00346 NE 1998 4 2 HEEA0013442 1 19980318 A 2430 7655009006105 DC CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 GENERATOR WOULD NOT COME ON LINE. 1 G 7 2 3U H1NE 1998040200347 19980402 00347 SW 1998 4 2 HEEA0013443 1 19980318 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 10 ERROR SPLIT EXCESSIVE FRICTION ERROR. 1 G 7 2 4U H4SW 1998040200348 19980402 00348 1998 4 2 HEEA0013444 4 19980318 A 2211 4033089901 COMPUTER FZ702 BELL 214 214ST 1182106 SW AUTO FLIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 COMPUTER FAILED TEST 11.10 ON SST TWICE. 2 G 7 2 4U H10SW 1998040200349 19980402 00349 SW 1998 4 2 HEEA0013445 1 19980318 A 7810 212061201011 EJECTOR BELL 412 412 1182202 SW LT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 LT EJECTOR ASSY RING CRACKED. 1 G 7 2 4U H4SW 1998040200350 19980402 00350 SW 1998 4 2 HEEA0013446 1 19980318 A 7810 212061201012 EJECTOR BELL 412 412 1182202 SW RT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 RT EJECTOR ASSY RING CRACKED. 1 G 7 2 4U H4SW 1998040200351 19980402 00351 SW 1998 4 2 HEEA0013448 1 19980318 A 6710 214001423109 ACTUATOR BELL 214 214ST 1182106 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 ACTUATOR MOTOR WEAK. 2 G 7 2 4U H10SW 1998040200352 19980402 00352 SW 1998 4 2 HEEA0013449 1 19980318 A 2841 214066212105 PROBE BELL 214 214ST 1182106 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 PROBE INOPERATIVE. 2 G 7 2 4U H10SW 1998040200353 19980402 00353 SW 1998 4 2 HEEA0013450 1 19980318 A 6240 214074280105 DETECTOR BELL 214 214ST 1182106 SW ROTOR RPM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ROTOR RPM AUDIO INOPERATIVE. 2 G 7 2 4U H10SW 1998040200354 19980402 00354 SW 1998 4 2 HEEA0013451 1 19980318 A 5530 206020113163 FIN ASSY BELL 206 206L1 1182107 SW VERT FIN DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 INSPECTED FIN, FOUND DAMAGE IN AREA WHERE NO STRUCTURAL DAMAGE ALLOWED TO VERTICAL FIN STRUCTURE AS PER BHT-206-SRM-1 SE CTION 6-3-9. SCRATCH 2 3/4" LONG DEPTH .001-.004. STINGER HOLE OVERSIZED. 1 G 7 1 3U H2SW 1998040200355 19980402 00355 SW 1998 4 2 HEEA0013452 1 19980318 A 7722 3030083 TRIM COMPENSATOR BELL 412 412 1182202 SW ENGINE ITT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 TRIM COMPENSATOR CAUSES ITT CIRCUIT BREAKER TO POP. 1 G 7 2 4U H4SW 1998040200356 19980402 00356 SW 1998 4 2 HEEA0013453 1 19980318 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW M/R FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 3893S 33022 ROTARY ACTUATOR WILL NOT TEST. 1 G 7 2 4U H4SW 1998040200357 19980402 00357 NE 1998 4 2 HEEA0013454 1 19980318 A 6210 7615009100042A BLADE SKRSKY S76 S76A 8143006 NE M/R SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 12229 760050 FIBERGLASS SEPARATED UNDERNEATH THE SLICE TITANIUM AT STATION 112.5 ON BOTH SURFACES. THE TRIM TAB HAS SOME SEPARATION ALSO. 1 G 7 2 3U H1NE 1998040200359 19980402 00359 SW 1998 4 2 HEEA0013456 1 19980319 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8590X 51494 ACTUATOR WORKS INTERMITTENTLY. 1 G 7 1 3U H2SW 1998040200360 19980402 00360 SW 1998 4 2 HEEA0013457 1 19980319 A 2820 233575 VALVE BELL 412 412 1182202 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 VALVE WILL NOT CLOSE IN NORMAL POSITION. 1 G 7 2 4U H4SW 1998040200361 19980402 00361 SW 1998 4 2 HEEA0013458 1 19980319 A 2915 212076006007 VALVE ASSY BELL 412 412 1182202 SW HYD SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 BYPASS INDICATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998040200362 19980402 00362 1998 4 2 HEEA0013459 4 19980319 A 3424 214075244001 RATE GYRO BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 INDICATES TURN WHEN STRAIGHT. RATE GYRO FAILED 2 G 7 2 4U H10SW 1998040200363 19980402 00363 1998 4 2 HEEA0013460 4 19980319 A 2200 214074104101 SENSOR DUALRATE BELL 214 214ST 1182106 SW SCAS SYS FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5748M 28102 KICKS SCAS PITCH OFF. 2 G 7 2 4U H10SW 1998040200364 19980402 00364 1998 4 2 HEEA0013461 4 19980319 A 3420 258719343 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 FAILED TEST 6.6 ON SST. 1 G 7 2 3U H1NE 1998040200365 19980402 00365 SW 1998 4 2 HEEA0013462 1 19980319 A 7712 412075205101 TRANSMITTER BELL 412 412 1182202 SW ENG TORQUE ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141PH 33197 ERRATIC TORQUE FLUCTUATION ON NR1 ENGINE. 1 G 7 2 4U H4SW 1998040200366 19980402 00366 NM 1998 4 2 MALA976064 1 19980326 A 3350 OL3071BPEGPL SIGN DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 826MA 330 DURING INSPECTION, EMERGENCY EXIT SIGN HAS BEEN BROKEN OFF, LOCATED NEXT TO SEAT 4E, UNIT STILL LIGHTS UP. MAINTENANCE REPLACED EXIT SIGN. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998040200367 19980402 00367 NM 1998 4 2 MALA976065 1 19980325 A 3350 MS25231316 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 832MA 341 DURING INSPECTION, ROW 4 EMERGENCY LIGHT INOP. MAINTENANCE REPLACED LAMP. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998040200368 19980402 00368 EU 1998 4 2 MALA976066 1 19980325 A 3350 7239410802 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 41XJ 041 DURING PREFLIGHT, FORWARD TWO FLOOR PROX EMERGENCY LIGHTS INOP. MAINTENANCE RECONNECTED CANNON PLUG TO EMERGENCY LIGHTI NG, REPLACED EMERGENCY LIGHT BULB, AND RECONNECTED WIRE. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998040200369 19980402 00369 EU 1998 4 2 MALA976067 1 19980324 A 5610 7256100501 WINDSHIELD SAAB SF340 340B 7860101 EU LT COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 407XJ 340B407 AFTER CLIMB, THE LEFT FRONT WINDSHIELD HEAT LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. AIRCRAFT RETURNED TO MSP. MAIN TENACE REPLACED THE RIGHT FRONT WINDSHIELD. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998040200370 19980402 00370 EU 1998 4 2 MALA976068 1 19980326 A 3350 SWITCH SAAB SF340 SF340A 7850100 EU CABIN DIRTY A MALA K NONE L NO TEST CR CRUISE 1 GL 15 110XJ 340A110 DURING FLIGHT, THE EMERGENCY LIGHTS CAME ON IN THE ARMED POSITION. MAINTENACE CLEANED FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH BY DOOR. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998040200371 19980402 00371 NM 1998 4 2 K3HA980039 1 19980325 A 3350 07912330711 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 FORWARD OF SEAT ROW 2ABC, RED E-PATH LIGHT LENSE AND BULB MISSING. INSTALLED LENSE AND RELAMPED, OP'S CHECK GOOD. 2 L 7 3 4F A3WE 1998040200372 19980402 00372 NE 1998 4 2 9804966613 2 19980324 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 3 MALFUNCTIONED A NWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 01 613US 20358 689562 DURING CRUISE, THE CREW NOTICED THE NR 3 ENGINE OIL CONSUMPTION TO BE UNUSUALLY HIGH. THE OIL CONSUMPTION DECREASED WIT H LOWER POWER SETTINGS SO THE AIRCRAFT DIVERTED TO MSP FOR MAINTENANCE. THE ENGINE WAS NOT SHUT DOWN AND THE FLIGHT WAS COMPLETED WITHOUT FURTHER DIFFICULTY. UPON ARRIVAL IN MSP, THE AIRCRAFT WAS REMOVED FROM SERVICE AND THE NR 3 ENGINE W AS CHANGED. EXACT PART CAUSING DIFFICULTY TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998040200373 19980402 00373 NM 1998 4 2 9804976303 1 19980326 A 3350 LIGHT BOEING 747 747451 1384940 NM CABIN INIOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 11B-14B, 23C-31C, AND AT DOOR 2R. REPAIRED W IRING. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998040200374 19980402 00374 NM 1998 4 2 9804982275 1 19980323 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 275US 21154 DURING PREFLIGHT, FOUND MAIN CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998040200375 19980402 00375 NM 1998 4 2 9804992293 1 19980321 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 293US 21504 DURING PREFLIGHT, FOUND RIGHT OVERWING EMERGENCY LIGHT FLASHES. REPLACED BATTERY AND POWER SUPPLY M655. OPERATIONAL CH ECK OK. 2 L 7 3 4F A3WE 1998040200376 19980402 00376 NM 1998 4 2 9805002288 1 19980318 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 288US 21376 DURING PREFLIGHT, FOUND ESCAPE SLIDE EMERGENCY LIGHT LEFT AFT GALLEY DOOR INOPERATIVE. REPLACED BATTERY PACK. OPERATIO NAL CHECK OK. 2 L 7 3 4F A3WE 1998040200377 19980402 00377 NM 1998 4 2 9805012204 1 19980326 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 204US 22544 DURING PREFLIGHT, FOUND LEFT CENTER EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998040200378 19980402 00378 WP 1998 4 2 UPS98826182 1 19980326 A 8011 35051542 STARTER DOUG DC8 DC873F 302199F WP CFM56 NR 1 ENGINE FAILED A IPXA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 01 818UP 46108 ENGINE NR 1 SHUTDOWN DUE TO OIL LOSS. REPLACED STARTER. FOUND STARTER SHEARED AND INTERNALLY FAILED. SHAFT AREA HAD D AMAGE ON STARTER. 2 L 7 4 4F RT 4A25 1998040200379 19980402 00379 WP 1998 4 2 98FDEA00221 1 19980326 A 3231 LATCH DOUG DC10 DC1010F 3022111 WP MLG DOOR LACK OF LUBE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 050FE 47804 98-0077 - AFTER GEAR RETRACTION ON TAKEOFF, THE RED RIGHT GEAR LIGHT STARTED FLICKERING ON BOTH PANELS. THE GEAR WAS RE CYCLED IN ACCORDANCE WITH THE RED TABS. THE LIGHT REMAINED EXTINGUISHED. FAULT CODE 32-30 APR. FOUND RIGHT MLG DOOR L ATCH ROLLER LINK BINDING, LUBED AND CLEANED. CHECKED MLG DOOR PROX SENSOR IAW M/M 32-61-03. OPS CKS NORMAL. 2 L 7 3 4F A22WE 1998040200380 19980402 00380 WP 1998 4 2 ABX9800255 1 19980326 A 5320 39151291 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 604 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 28L END FITTING CRACKED AFT OF STATION 604. REPLACED LONGERON FITTING IAW DC9 SRM 51-30- 5. 2 L 7 2 4F A6WE 1998040200381 19980402 00381 WP 1998 4 2 ABXA9800256 1 19980326 A 5320 39151291 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 604 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 26R END FITTING CRACKED AFT OF STATION 604. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998040200382 19980402 00382 WP 1998 4 2 ABXA9800257 1 19980325 A 5313 5920302509 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 869 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND CORROSION ON THE UNDERSIDE OF LONGERON 29R AT STATION 869. REPAIRED LONGERON IAW ABX REA D953-230 23-MR. 2 L 7 2 4F A6WE 1998040200383 19980402 00383 WP 1998 4 2 ABXA9800258 1 19980326 A 5320 995772815 DOUBLER DOUG DOUG DC9 DC941 302207N WP BS 737 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL UPPER PRESSURE PANEL DOUBLER AT STATION 737 RBL 42 CORRODED. R EPLACED DOUBLER IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998040200384 19980402 00384 WP 1998 4 2 ABXA9800259 1 19980326 A 5320 99234552 FITTING DOUG DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND KEEL AREA FITTING CRACKED AT STATION 737 AND RBL 8. REPLACED FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998040200385 19980402 00385 WP 1998 4 2 ABXA9800260 1 19980326 A 5512 59225761 SKIN DOUG DOUG DC9 DC941 302207N WP LT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND CORROSION ON LEFT HORIZONTAL STABILIZER UPPER SKIN FROM STATION XHS 32 - XHS 140. REPAIRED IAW AB X REA D955-2067. 2 L 7 2 4F A6WE 1998040200386 19980402 00386 WP 1998 4 2 ABXA9800261 1 19980326 A 5312 591013039INI BULKHEAD TEE DOUG DOUG DC9 DC941 302207N WP AFT PRESS BULKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD TEE-CAP SECTION NR 6 CRACKED. REPAIRED TEE-CAP IAW DWG SR09530056 AND ABX E A 53120037-006. 2 L 7 2 4F A6WE 1998040200387 19980402 00387 WP 1998 4 2 ABXA9800262 1 19980326 A 5312 9915558209 BLKHD STIFFENER DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD RADIAL STIFFENER 2ND UP FROM FLOOR, LEFT SIDE, CRACKED AT OUTBOARD END. REP AIRED STIFFENER IAW SERVICE REWORK DRAWING NR J060110.. 2 L 7 2 4F A6WE 1998040200388 19980402 00388 WP 1998 4 2 ABXA9800263 1 19980326 A 5312 9915558201 BLKHD STIFFENER DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 957AX 47759 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER 3RD UP FROM FLOOR, LEFT SIDE, CRACKED AT OUTBOARD END. REPAIRED S TIFFENER IAW SERVICE REWORK DWG J060110. 2 L 7 2 4F A6WE 1998040200389 19980402 00389 WP 1998 4 2 ABXA9800264 1 19980326 A 5313 591140617N LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 160-197 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160 AND 197. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998040200390 19980402 00390 WP 1998 4 2 ABXA9800265 1 19980326 A 5341 39164092 FITTING DOUG DOUG DC9 DC932F 3022067 WP BS 690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND RIGHT OUTBOARD T-FITTING BETWEEN FUSELAGE AND RIGHT SLANT PANEL CORRODED AT STATION 690. REPLACED T-FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998040200391 19980402 00391 NM 1998 4 2 DL72L980646 1 19980324 A 2120 AIR DISTRIBUTION BOEING 727 727232 1384082 NM CABIN SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 505DA 21307 AIR RETURN SMOKE IN AFT CABIN DURNING T/O CREW DUMPED FUEL TO 163,500 NORMAL LANDING AND STOP. RAN PACKS WITH APU AIR ALL PACKS OPERATED NORMAL. FLT CREW TAXI AND AND RAN ENGINES AT RUNUP AREA WITH MECHANIC, CHECKING PACKS WITH ENGINE AI R AT IDLE AND POWER. ALL PACKS OPERATED NORMAL, NO SMOKE IN CABIN. PERFORMED OVERWEIGHT LANDING CHECK PHASE 1, NO DAMA GE FOUND RETUNED A/C BACK TO SERVICE. 2 L 7 3 4F A3WE 1998040200392 19980402 00392 NM 1998 4 2 DL73E980648 1 19980324 A 2421 GENERATOR BOEING 737 737247 138448D NM NR 1 ENGINE TRIPPED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 239WA 23187 C ON CLIMB-OUT OF 23,000 FEET, CTR FUEL PUMPS WERE TURNED ON AND WE LOST THE NR 1 GEN IN ABOUT 2-3 SECONDS, THE NR 1 BUS O FF AND GEN OFF BUS LIGHTS ILLUM FOLLOWING POM PROCEDURES WE WERE UNABLE TO POWER NR 1 BUS BY LT GEN OR APU. GEN NR 1 VO LTS AND FREQS PEGGED TO THE LOW SIDE. CHECKED NR 1 CSD OIL SVC CHECKED GOOD, HAD MT AND LV FAULTS CLEARED FAULTS APU PO WERED BOTH LT/RT BUSSES NML. RESET NR 1 GEN, RAN BOTH ENG GEN SYS XFERS POWER SEVERAL TIMES, CKS NML LT GEN AND BUS OPN CKS NML. 2 L 7 2 4F A16WE 1998040200393 19980402 00393 NM 1998 4 2 DL73K980650 1 19980324 A 3350 BR9279108 SIGN BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 305DL 23077 2L EMERGENCY DOOR LIGHT INOP. REPLACED ASSEMBLY. 2 L 7 2 4F RT A16WE 1998040200394 19980402 00394 WP 1998 4 2 DLL19980651 1 19980324 A 3350 POWER SUPPLY RPS1B LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 6403 193H1216 ON L/O AFT RT CORNER EMERGENCY LIGHT SECTION OUT. REPLACED AFT RT POWER SUPPLY CKS OK. 2 L 7 3 4F A23WE 1998040200395 19980402 00395 NM 1998 4 2 DL76S980652 1 19980324 A 5754 114T410226A SKIN BOEING 767 767332 1382001 NM NR 11 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 123DN 23437 WINGS LEADING EDGE SLAT NR 11, TRAILING EDGE WEDGE, SKIN DELAMINATION REPAIR. THE UPPER SKIN OF THE NR 11 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 6 AREA OF DELAMINATION. THE DAMAGE WAS TRIMMED OUT AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364348-14AD. 2 L 7 2 4F RT A1NM 1998040200396 19980402 00396 NM 1998 4 2 DL76S980653 1 19980324 A 5754 114T410530A WEDGE BOEING 767 767332 1382001 NM NR 8 LE SLAT TE DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 123DN 23437 WINGS NR 8 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 5 BY 9 AREA OF DELAMINATION ON THE UPPER SKIN. THE DELAMINATION WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER /A 364347-14AD. 2 L 7 2 4F RT A1NM 1998040200397 19980402 00397 NM 1998 4 2 DL76S980654 1 19980324 A 5754 114T410225A WEDGE BOEING 767 767332 1382001 NM NR 2 LE SLAT TE DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 123DN 23437 WINGS NR 2 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 2 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 7 BY 4 .5 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 3 64346-14AD. 2 L 7 2 4F RT A1NM 1998040200398 19980402 00398 NM 1998 4 2 DL76S980655 1 19980324 A 5754 114T410131A WEDGE BOEING 767 767332 1382001 NM NR 1 LE SLAT TE DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 123DN 23437 WINGS NR 1 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 1 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 4 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 36 4345-14AD. 2 L 7 2 4F RT A1NM 1998040200399 19980402 00399 NM 1998 4 2 DL72S980656 1 19980322 A 5320 65562312 BEAR STRAP BOEING 727 727232 1384082 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 492DA 21061 FUSELAGE SKIN R1 DOOR SURROUND UPPER HINGE CUTOUT, REPAIR FOR CRACK IN DOOR SURROUND BEAR STRAP. THE INTERNAL R1 DOOR S URROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND CRACKED AT THE UPPER HINGE CUTOUT. THE SKIN WAS TRIMMED AWAY TO ACCE SS THE CRACK. THE CRACK IN THE BEAR STRAP WAS TRIMMED OUT AND THE SKIN AND BEAR STRAP, REPAIRED WITH A DOUBLER AND TRIP LER PER BAC S/B 727-53-0136 AND ER/A 364328-14. 2 L 7 3 4F A3WE 1998040200400 19980402 00400 NM 1998 4 2 DL72S980657 1 19980324 A 5521 SPAR BOEING 727 727232 1384082 NM RT ELEV REAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 541DA 22387 HORIZ STABILIZER RT ELEVATOR REAR SPAR, REPAIR FOR TYPICAL CRACKS. THE RT ELEVATOR REAR SPAR WAS FOUND WITH TWO TYPICAL CRACKS .25 OR SMALLER EXTENDING FROM UNDERNEATH THE 2ND HINGE FITTING FROM THE OUTBD END OF THE SPAR. THE CRACKS WERE STOP DRILLED PER BAC S/B 727-55-0089 AND SET-UP FOR REPEAT INSPECTION AND PERMANENT MODIFICATION PER ER/A 364338-14AD. 2 L 7 3 4F A3WE 1998040200401 19980402 00401 WP 1998 4 2 DLL10980658 1 19980319 A 3221 1543141 TRUNNION LKHEED 1011 10113851 5265010 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 723DA 193C1150 FUSELAGE FS 449 BULKHEAD LBL 21 NLG TRUNNION FITTING, REPAIR FOR CRACK. THE 1543141 NLG TRUNNION FITTING WAS FOUND WITH A TYPICAL CRACK AT THE FS 449 BULKHEAD AT LBL 21. THE CRACK IS IN THE INBD SKIN FLANGE AND EXTENDS INTO THE VERTICAL FLANGE. THE CRACK IS REPAIRED WITH A 1642622-145 AND -139 KIT PER LAC S/B 093-53-233 AND IS DOCUMENTED PER ER/A 364313 -14AD. 2 L 7 3 4F A23WE 1998040200402 19980402 00402 NM 1998 4 2 DL72S980660 1 19980325 A 5320 6516350 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 CRACKS WERE FOUND IN THE LBL AND RBL 36.83 VERT STIFFENER ON THE FWD SIDE OF THE FS 1183 BLKHD. THE CRACKS WERE LOCATED AT APPROX WL 238 AND WERE NO MORE THAN 2 IN LENGTH. REPAIRED PER ERA 331543-14. 2 L 7 3 4F A3WE 1998040200403 19980402 00403 NM 1998 4 2 DL72S980662 1 19980318 A 5530 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 SKIN CRACKED, PREVIOUSLY STOP DRILLED CRACK AT BASE OF VERTICAL STAB FRONT SPAR, RT SIDE. REMOVED FASTENERS. CUT OUT D AMAGED SECTION OF SKIN. E/C INSP OK. FABRICATED FILLER AND BEGAN FABRICATION OF DOUBLER PER SRM 55-30-3. OK TO INSTAL L DOUBLER. STARTED INSTALLING DOUBLER PER SRM 55-30-3. COMPLETED INSTALLATION OF DOUBLER PER SRM 55-30-3. 2 L 7 3 4F A3WE 1998040200404 19980402 00404 NM 1998 4 2 DLM88980663 1 19980325 A 2530 OVEN DOUG MD88 MD88 3023688 NM FWD GALLEY FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 929DL 49716 DURING TAXI OUT FROM LAX, FLT ATTENDANT REPORTED SPARKS AND SMOKE COMING FROM FWD GALLEY. C/B POPPED. REPLACED GALLEY OVEN. 2 L 7 2 4F RT A6WE 1998040200405 19980402 00405 NM 1998 4 2 DL72S980666 1 19980304 A 5753 652163261 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 DURING SHOP INSPECTION, THE FLAP WAS FOUND WITH A CRACKED REAR CHORD ANGLE. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 B Y INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998040200406 19980402 00406 NM 1998 4 2 DL72S980667 1 19980304 A 5753 652163261 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 DURING SHOP INSPECTION, THE FLAP REAR CHORD ANGLE WAS FOUND CRACKED 32 AND 37 FROM THE IB END. THE ANGLE WAS REPAIRED B Y INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1998040200407 19980402 00407 WP 1998 4 2 RRXA98038 1 19980116 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1400-1440 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND LOWER FUSELAGE SKIN CRACKED AND CORRODED AT STA 1400 TO 1440 AND LONGERONS 31R TO 36. REMOVED DAMAGED SECTION BY CUTOUT. TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AND FINGER DOUBLERS AN D INSTALLED IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04148 AND DC-8 SRM 53-4-1 FIGURE 17 ITEM B. 2 L 7 4 4F RT 4A25 1998040200408 19980402 00408 GL 1998 4 2 RRXA98043 2 19980206 A 7230 565174759 PANEL DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C5 GL NR 2 ENGINE TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND NR 2 ENGINE FAN CASE, RT SIDE, AFT THE CLOSE-OUT PANEL ATTACHED TO THE AFT END OF THE STRUT AT 3:00 POSITION WAS SNAGGED DURING ENGINE HOIST, PART WAS TORN ON UPPER FLANGE. REMOVED DAMAGED PANEL, FABRICATE D AND INSTALLED NEW PANEL IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04197. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998040200409 19980402 00409 WP 1998 4 2 RRXA98039 1 19980202 A 5320 565192744 ANGLE DOUG DC8 DC871F 302199D WP BS 1766 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND ADDITIONAL DRILLING HOLES IN THE FUSELAGE TO VERTICAL ATTACHMENT ANGLE AT STA 1766. R EMOVED DAMAGED SECTION, FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04249 AND DC-8 SRM 53-2-5 FIGURE 16A SHEET 1. 2 L 7 4 4F RT 4A25 1998040200410 19980402 00410 WP 1998 4 2 RRXA98041 1 19980205 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 290 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND LONGERON 34 RIGHT, STA 290 TO STA 310, OUTBD ANGLE IS CORRODED BEYOND LIMITATIONS IAW DC-8 SRM. CUT OUT DAMAGE SECTION BETWEEN STA 290 AND STA 310. FABRICATED AND INSTALLED REPAIR DOUBER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04251 AND DC-8 SRM 53-2-0 FIGURE 1B. 2 L 7 4 4F RT 4A25 1998040200411 19980402 00411 WP 1998 4 2 RRXA98040 1 19980202 A 5320 5616520244 JAMB DOUG DC8 DC871F 302199D WP BS 560 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND DOOR JAMB WEB AT STA 560 HAS EXFOLIATION CORROSION. CORROSION IS 100 PERCENT THROUGH WEB IN THE CORNER RADIUS. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB AND REPAIR STRAP IAW FAA APPROVED DER T IMCO ENGINEERING SKETCH REO-04250 AND 51-1-8. 2 L 7 4 4F RT 4A25 1998040200412 19980402 00412 WP 1998 4 2 RRXA98042 1 19980212 A 2750 5614376507 FITTING DOUG DC8 DC871F 302199D WP LT TE FLAP OVERSIZE HOLES A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND OVERSIZE HOLE TO LT FLAP LINK SUPPORT FITTING AT STA XF 339. REWORK TO 0.874/0.8762 B /P DAI HOLES. OPEN SUBJECT HOLES TO REMOVE MINIMUM MATERIAL, ENLARGE BOTH HOLES. FABRICATED AND INSTALLED 2 EACH BUSHI NGS IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04269. 2 L 7 4 4F RT 4A25 1998040200415 19980402 00415 EU 1998 4 2 98ZZZX1249 1 19980212 A 6710 10513122 PITCH LINK BOLKMS 105 BO105C 5626005 EU MAIN ROTOR HUB CRACKED B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 352TT S59 WHILE C/W DAILY INSPECTION OF AD 87-26-02R1, FOUND BLUE MRB PITCH LINK CRACKED AT BOTTOM END OF ROD ON SLEEVE PORTION. R EMOVED CRACKED PITCH LINK (BLUE), AND INSTALLED SERVICEABLE LINK IAW BO-105 MM. OPS FUNCTIONAL CHECK GOOD. 1 G 7 2 3U H3EU 1998040200430 19980402 00430 WP 1998 4 2 AALA980405 1 19980224 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 857 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 234AA 49181 NR 6 SEAT TRACK CORRODED AT STA 857. CORROSION BLENDED BEYOND LIMITS. AREA CUT OUT AND PLUG INSTALLED PER AARD 53-20-0 0-10. TST: 44,152 HOURS. CYCLES: 24,579. (X) 2 L 7 2 4F A6WE 1998040200432 19980402 00432 SW 1998 4 2 98ZZZX1265 1 19980121 A 6230 206010336005 DRIVE LINK BELL 206 206L1 1182107 SW PYLON WORN B L ZV1R K NONE O OTHER IN INSP/MAINT 1 SW 03 5000G 5392 45163 INSPECTION FOUND DRIVE LINK ASSY WITH EXCESSIVE PLAY AT TWO PLACES. SEE BELL MM L-3 FIG 62-21. ON TEAR DOWN, FOUND BEA RINGS AND SPACERS WORN BEYOND LIMITS. TOTAL TIME OF PARTS, LESS THAN 1,000 HRS/1 YEAR SINCE REPLACEMENT. 1 G 7 1 3U H2SW 1998040200436 19980402 00436 SW 1998 4 2 98ZZZX1269 1 19980316 A 2910 70012F000T204 HOSE BELL 412 412 1182202 SW NR 1 HYD SYSTEM LEAKING A HEEA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 03 108X 33115 IN CRUISE, LOST NR 1 HYDRAULIC SYSTEM. LANDED WITHOUT INCIDENT. (PRESSURE INDICATION). MAINTENANCE FOUND HOSE TO COLL ECTIVE SERVO LEAKING, REPLACED SAME. REF: 412 IPB, CHAPTER 29-99-00, FIG 29-3, ITEM 51. 1 G 7 2 4U H4SW 1998040200442 19980402 00442 NM 1998 4 2 K3HA980040 1 19980328 A 3350 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY EXIT LIGHT LEFT HAND MID ROW SEAT 20ABC SEVERAL LIGHT BURN OUT. INSTALLED NEW BULBS. 2 L 7 3 4F A3WE 1998040200443 19980402 00443 NM 1998 4 2 K3HA980041 1 19980329 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 AT POST FLIGHT, FOUND RIGHT HAND EMERGENCY (CENTER) LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, REF MM 33-50-21, OPS CHECK OK. 2 L 7 3 4F A3WE 1998040200444 19980402 00444 NM 1998 4 2 CALA9800584 1 19980326 A 3260 SWITCH BOEING 737 7373T0 1384582 NM GEAR LEVER INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14324 23375 WHEN GEAR WAS EXTENDED FOR LANDING AT CLE, THE NLG UNSAFE LIGHT REMAINED ILLUMINATED. THE GEAR WAS CYCLED TWICE AND ALL INDICATIONS WERE NORMAL. MAINTENANCE FOUND THE GEAR LEVER SWITCH AT FAULT. THE SWITCH WAS REPLACED AND GEAR OPERATION AND INDICATIONS WERE GOOD. 2 L 7 2 4F RT A16WE 1998040200445 19980402 00445 WP 1998 4 2 CALA9800585 1 19980328 A 3350 EMBS1392 BATT CHARGER ENGMAGNETICS DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 49082 87682 47927 THE EMERGENCY EXIT LIGHTS WOULD NOT TEST, NO GREEN WHEN BUTTON PUSHED. THE LEFT AFT BATTERY CHARGER AND PACK WERE REMOV ED AND REPLACED. 2 L 7 3 4F A22WE 1998040200446 19980402 00446 NM 1998 4 2 CALA9800586 1 19980325 A 3350 90052 BATTERY PACK GRIMES BOEING 727 727224 1384076 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND CEILING EMERGENCY EXIT LIGHT BETWEEN R-2 DOOR AND L-2 DOOR INOPERATIVE. THE BATTERY PACK WAS REMOVED A ND REPLACED. 2 L 7 3 4F A3WE 1998040200447 19980402 00447 WP 1998 4 2 CALA9800587 1 19980325 A 5510 PIVOT PLATES DOUG DC9 DC982 3022082 WP LT HOR STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12811 49265 INSPECTION FOUND LT HORIZONTAL STABILIZER INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED. THE PIVOT PLATES WERE REPL ACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998040200448 19980402 00448 WP 1998 4 2 CALA9800588 1 19980325 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12811 49265 INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR EXTERIOR SKIN AROUND HOLD OPEN HOOK CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 20A, PAGE 43. 2 L 7 2 4F A6WE 1998040200449 19980402 00449 WP 1998 4 2 CALA9800589 1 19980325 A 5210 INTERCOSTAL DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12811 49265 INSPECTION FOUND A 1 INCH CRACK IN RADIUS OF MAIN CABIN DOOR INTERCOSTAL AFT OF HANDLE TORQUE SHAFT. THE INTERCOSTAL WA S REPLACED IAW SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F A6WE 1998040200450 19980402 00450 WP 1998 4 2 CALA9800590 1 19980326 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1521-1571 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND LONGERON 46L CORRODED AROUND FASTENER HOLE ON END CAP AT SPLICE JOINT IN CENTER CARGO BAY AT STA 1521 T O 1571. A NEW END CAP WAS FITTED TO THE LONGERON IAW GMM 10-900-01. 2 L 7 3 4F A22WE 1998040200451 19980402 00451 WP 1998 4 2 CALA9800591 1 19980326 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1129 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND A 2 INCH CRACK IN LONGERON 36L AT FUSELAGE SKIN JOINT STA 1129. THE CRACKED SECTION OF LONGERON WAS RE MOVED AND A NEW SECTION WAS FITTED IAW SRM 53-10-00. 2 L 7 3 4F A22WE 1998040200452 19980402 00452 WP 1998 4 2 CALA9800592 1 19980326 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 2140 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND A 2 INCH CRACK IN FRAME AT STRINGER 2 STA 2140Y. A REPAIR WAS PERFORMED IAW SRM 53-30-00. 2 L 7 3 4F A22WE 1998040200453 19980402 00453 WP 1998 4 2 CALA9800593 1 19980326 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1571-1711 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND LONGERON 48L IN CENTER CARGO BAY CORRODED AT STA 1571 TO 1711. A NEW END CAP WAS FITTED TO LONGERON AN D A NEW SECTION OF LONGERON WAS SPLICED IN IAW GMM 10-900-01. 2 L 7 3 4F A22WE 1998040200454 19980402 00454 WP 1998 4 2 CALA9800594 1 19980326 A 5311 BELLFRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 49246 INSPECTION FOUND A 2 INCH CRACK IN BELLFRAME AT LONGERON 2R, STA 1418. THE AREA WAS REPAIRED IAW ECRA 5310-03700 AND SR M 53-03, FIGURE 32. 2 L 7 2 4F A6WE 1998040200455 19980402 00455 WP 1998 4 2 CALA9800595 1 19980326 A 5320 BRACKET DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 49246 INSPECTION FOUND ANGLE BRACKET CORRODED AT STA 1174, LONGERON 29R. A NEW ANGLE BRACKET WAS INSTALLED IAW SRM 51-10-03. 2 L 7 2 4F A6WE 1998040200456 19980402 00456 WP 1998 4 2 CALA9800596 1 19980326 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12811 49265 INSPECTION FOUND A 1 INCH CRACK AT FORWARD END AND AFT END OF NR 1 DOOR BEAM OF MAIN CABIN DOOR. A NEW NR 1 MAIN CABIN DOOR BEAM WAS INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998040200457 19980402 00457 NM 1998 4 2 CALA9800597 1 19980327 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1130-1170 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND AFT LAV LT SUB FLOOR SUPPORT CORRODED AT STA 1130 TO 1170, LBL 25 TO 60. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A NEW FLOOR SUPPORT PANEL WAS FABRICATED AND INSTALLED. 2 L 7 3 4F A3WE 1998040200458 19980402 00458 NM 1998 4 2 CALA9800598 1 19980327 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1070-1050 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1070 TO 1050, LBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, 51-30-5, AND MM 51-20-0. 2 L 7 3 4F A3WE 1998040200459 19980402 00459 NM 1998 4 2 CALA9800599 1 19980327 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 440-480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SEAT TRACK CORRODED AT STA 440 TO 480, RBL 24. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 5 1-10-5, 53-10-5, 51-30-5, 51-30-8, 51-10-2, 51-30-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998040200460 19980402 00460 NM 1998 4 2 CALA9800600 1 19980328 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND FLOORBEAM CORRODED AT STA 480, RBL 48. THE CORRODED AREA WAS REMOVED, A FLOORBEAM REPAIR WAS FABRICATE D AND INSTALLED IAW SRM 53-10-8, FIGURE 1. 2 L 7 3 4F A3WE 1998040200461 19980402 00461 NM 1998 4 2 9805026303 1 19980329 A 3350 CONNECTOR BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FORWARD OF ROW 39R AND AT DOORS 2L, 4R, AND 3L. RECONN ECTED LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998040200462 19980402 00462 WP 1998 4 2 9805039942 1 19980327 A 7711 LG80A2 TRANSMITTER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 3991C 8087 5140 47175 657545 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EPR INDICATION FROZE AT 1.7. CREW ABORTED TAKEOFF AND RETURNED TO THE GAT E. MAINTENANCE REPLACED THE LEFT ENGINE EPR TRANSMITTER, ENGINE OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998040200463 19980402 00463 WP 1998 4 2 9805049103 1 19980328 A 7931 795898011 OIL LINE DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7 52053 NE LT ENGINE CRACKED A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 93S 47078 653954 DURING CRUISE AT 33,000 FEET, THE LEFT ENGINE OIL QUANTITY BEGAN DECREASING WITH ASSOCIATED LOW OIL PRESSURE. CREW SHUT DOWN THE LEFT ENGINE AND DIVERTED TO MEM. MAINTENANCE REPLACED THE LEFT ENGINE OIL PRESSURE TRANSMITTER LINE AND OIL F ILTER, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998040200464 19980402 00464 WP 1998 4 2 9805059877 1 19980328 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS IN VENTRAL STAIR AREA INOPERATIVE. MAINTENANCE REPLACED 3 BATTERY PACKS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998040200465 19980402 00465 WP 1998 4 2 9805069302 1 19980327 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 602RC 48055 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHT PLATE BROKEN AT AT MAIN CABIN DOOR 1R. MAINTENANCE REPLACED LIGHT ASSEMBL Y, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200466 19980402 00466 WP 1998 4 2 9805079178 1 19980329 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200467 19980402 00467 WP 1998 4 2 9805089860 1 19980326 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 769NC 47757 DURING LINE CHECK, FOUND ONE SECTION OF CEILING EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998040200468 19980402 00468 WP 1998 4 2 9805099751 1 19980326 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 751NW 47115 DURING LINE CHECK, FOUND WING/NACELLE EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED RELAY R2-213, BATTERY PACKS AND RELAMPED LIGHTS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200469 19980402 00469 WP 1998 4 2 9805109307 1 19980329 A 3350 MODULE DOUG DC9 DC982 3022082 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309RC 48088 DURING LINE CHECK, FOUND FLOOR TRACK EMERGENCY EXIT PROXIMITY LIGHTING INOPERATIVE AT SEAT ROW 30. MAINTENANCE REPLACED LIGHT MODULE ASSEMBLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200470 19980402 00470 WP 1998 4 2 9805119875 1 19980329 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 784NC 48109 DURING LINE CHECK, FOUND THE FIRST SECTION OF CABIN EMERGENCY PROXIMITY LIGHTING INOPERATIVE. MAINTENANCE REPLACED POWE R SUPPLY AND BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998040200471 19980402 00471 1998 4 2 9805129953 4 19980325 A 3418 COMPUTER DOUG DC9 DC931 3022065 WP NR 2 STALL WARN FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 918RW 47158 STALL WARNING INDICATION FAILURE LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDEN T. MAINTENANCE REPLACED THE NR 2 STALL WARNING COMPUTER AND TRANSDUCER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200472 19980402 00472 WP 1998 4 2 9805139925 1 19980326 A 2750 59268805001 CONTROL VALVE DOUG DC9 DC932 3022066 WP TE FLAP SYSTEM FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 925US 24332 1303 47472 FLAPS INDICATED 5 DEGREES WITH FLAP HANDLE SELECTED UP AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INC IDENT. MAINTENANCE REPLACED FLAP CONTROL VALVE AND RIGGED SYSTEM, LEAK AND OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200473 19980402 00473 WP 1998 4 2 9805149954 1 19980325 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 921RW 47164 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY EXIT SIGN AT GALLEY DOOR INOPERATIVE. REPLACED FUSE, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1998040200474 19980402 00474 WP 1998 4 2 9805159954 1 19980326 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 921RW 47164 DURING LINE MAINTENANCE INSPECTION, FOUND GALLEY DOOR AND FORWARD CABIN FLOOR PROXIMITY EMERGENCY LIGHTS WOULD NOT TEST. REPLACED FUSE AT GALLEY DOOR AND REPAIRED CRIMPED WIRE AT ROW 2 FOOTREST, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200475 19980402 00475 WP 1998 4 2 9805169953 1 19980325 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 918RW 47158 FLIGHT ATTENDANT REPORTED FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200476 19980402 00476 WP 1998 4 2 9805179928 1 19980325 A 3397 WIRE HARNESS DOUG DC9 DC931 3022065 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8921E 45836 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT HARNESS FOR EMERGENC Y LIGHT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200477 19980402 00477 WP 1998 4 2 9805189944 1 19980327 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200478 19980402 00478 WP 1998 4 2 9805199605 1 19980329 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 605NW 47223 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS AT FORWARD GALLEY DOOR AND BETWEEN ROWS 1 THRU 4 INOPERATIVE. REPLACED FU SE IN EMERGENCY EXIT SIGN AT FORWARD GALLEY DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200479 19980402 00479 SO 1998 4 2 COMA9810079 1 19980328 A 5230 12021360001 SKIN EMB 120 EMB120RT SO CARGO DOOR BROKEN OFF A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 164D 20874 120164 DURING LEAK CHECK OF CARGO DOOR SEAL FOUND AN AREA OF CARGO DOOR SKIN MISSING (BROKEN OFF) FROM UPPER AFT CORNER, MISSI NG SKIN AREA WAS 3.75 INCH LONG AND .625 IN FROM OUTER EDGE OF SKIN. NO DAMAGE TO DOOR FRAME WAS FOUND. THE CARGO DOOR SKIN WAS REPAIRED IAW AERODESIGN REPORT NR 2699-1 DATED 03-28-98. 2 L 7 2 4T RT A31SO 1998040200480 19980402 00480 EA 1998 4 2 COMA9860067 1 19980326 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION LD LANDING 1 SO 01 975CA 3281 7150 FLAPS FAIL MESSAGE ON EICAS. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1998040200481 19980402 00481 EA 1998 4 2 COMA9860068 1 19980327 A 5210 LATCH MECH CNDAIR CL600 CL6002B19 EA PAX DOOR DIRTY A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 912CA 7011 CABIN DOOR LATCH MESSAGE ON EICAS. CLEANED EXCESS GREASE FROM DOOR LATCHES. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4F RT A21EA 1998040200482 19980402 00482 EA 1998 4 2 COMA9860069 1 19980325 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FLAP FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 949CA 3181 601 7080 FLAPS FAILED AT 17 DEGREES WHEN SELECTED FOR LANDING APPROACH. REPLACED DEFECTIVE FLAP ACTUATOR, LEFT HAND OUTBOARD FLA P. 2 L 7 2 4F RT A21EA 1998040200483 19980402 00483 NM 1998 4 2 SWAA980334 1 19980318 A 5510 BEAM BOEING 737 7373G7 1384595 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND UPPER RT HORIZONTAL STAB TRAILING EDGE BEAM CHANNEL CRACKED STUB AT BS 92. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200484 19980402 00484 NM 1998 4 2 SWAA980335 1 19980318 A 5530 WEB BOEING 737 7373G7 1384595 NM VERT STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND VERTICAL STAB WEB FIN AT BS 69.4 26 FWD OF RUDDER HINGE IS CRACKED. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200485 19980402 00485 NM 1998 4 2 SWAA980336 1 19980319 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 312 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND FLOORBOARD FASTENER HOLE DRILLED BESIDE REPAIR FASTENER IN FLOORBEAM SPLICE AT BS 312, R BL 20.5, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200486 19980402 00486 NM 1998 4 2 SWAA980337 1 19980319 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 494 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND DENT IN SKIN AT BS 494, 3 BELOW STR 15 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200487 19980402 00487 NM 1998 4 2 SWAA980338 1 19980319 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CORRISION ON Z-ANGLE CHORD AT BS 270, LBL 9 TO RBL 11, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200488 19980402 00488 NM 1998 4 2 SWAA980339 1 19980320 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME AT BS 500 CORRODED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200489 19980402 00489 NM 1998 4 2 SWAA980340 1 19980320 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CRACKED AROUND FASTENER HOLE AT BS 344, LBL 9 AND AT BS 344, LBL 7. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200490 19980402 00490 NM 1998 4 2 SWAA980341 1 19980320 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CRACKED AROUND FASTENER HOLE AT BS 344, RBL 0 AND AT BS 344, RBL 1. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200491 19980402 00491 NM 1998 4 2 SWAA980342 1 19980320 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME CRACKED AT RADIUS AND FASTENER HOLE FWD LOWER CORNER OF RT DOORWAY AT BS 294.5 , RBL 55. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200492 19980402 00492 NM 1998 4 2 SWAA980343 1 19980320 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 1 LBL 1, WL 187. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200493 19980402 00493 NM 1998 4 2 SWAA980344 1 19980320 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 196.5+0 200, LBL 4.7 AND WL 199 TO 200 LBL 6.7. REPAIRE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200494 19980402 00494 NM 1998 4 2 SWAA980345 1 19980320 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 211 TO 212, RBL 6.7 AND WL 211 TO 212.5, LBL 6.7. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200495 19980402 00495 NM 1998 4 2 SWAA980346 1 19980320 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND 178 BULKHEAD WEB CRACKED AT WL 234 RBL 11.7 AND 12.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200496 19980402 00496 NM 1998 4 2 SWAA980347 1 19980321 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1030 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION ON WEB AT BS 1030, RBL 5 - RBL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200497 19980402 00497 NM 1998 4 2 SWAA980348 1 19980321 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORRODED FASTENER HOLE AT BS 344, LBL 7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200498 19980402 00498 NM 1998 4 2 SWAA980349 1 19980321 A 5510 STRAP BOEING 737 7373G7 1384595 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACKED STABILIZER STRAP AT BS 331 LBL 46 WL 200. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200499 19980402 00499 NM 1998 4 2 SWAA980350 1 19980321 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 350 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT FWD ENTRY DOORWAY DOOR STOP FITTING NR 10 AT BS 350, WL 215, LBL 66. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200500 19980402 00500 NM 1998 4 2 SWAA980351 1 19980321 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AROUND FLOORBOARD FASTENER HOLE AT BS 967, RBL 48, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200501 19980402 00501 NM 1998 4 2 SWAA980352 1 19980321 A 5320 CREASE BEAM BOEING 737 7373G7 1384595 NM BS 576 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM OUTBOARD CHORD CRACKED AT BS 576, LBL 70, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200502 19980402 00502 NM 1998 4 2 SWAA980353 1 19980321 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT LBL 6.0, WL 198 TO 199, RBL 0, WL 188 AND RBL 1.0, WL 187. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200503 19980402 00503 NM 1998 4 2 SWAA980354 1 19980321 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 395 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND DENT SKIN AT BS 395, 1 INCH ABOVE STR 25 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200504 19980402 00504 NM 1998 4 2 SWAA980355 1 19980321 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 315 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 315 LBL 32 WL 194. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200505 19980402 00505 NM 1998 4 2 SWAA980356 1 19980321 A 5315 BEAM WEB BOEING 737 7373G7 1384595 NM BS 440-460 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 440 TO 460, WL 208, RBL 69. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200506 19980402 00506 NM 1998 4 2 SWAA980357 1 19980321 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 350 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT FWD ENTRY DOORWAY DOOR STOP FITTING NR 9 AT BS 350, WL 222, LBL 66 A ND FITTING NR 10 AT BS 350, WL 216, LBL 66. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200507 19980402 00507 NM 1998 4 2 SWAA980358 1 19980321 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 301/360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 360, WL 264.5 LBL 56 AND BS 301, WL 256, LBL 56. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200508 19980402 00508 NM 1998 4 2 SWAA980359 1 19980321 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 296 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND STRINGER CRACKED AT BS 296, WL 256, LBL 55. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200509 19980402 00509 NM 1998 4 2 SWAA980360 1 19980321 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND ANGLE STIFFENER CRACKED AT BS 290, WL 254, RBL 54 AND BS 290, WL 240, RBL 59. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200510 19980402 00510 NM 1998 4 2 SWAA980361 1 19980321 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 394/500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH L-ANGLE CRACKED AT BS 394, WL 208, BL 0 AND BS 500D+5, BL 0, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200511 19980402 00511 NM 1998 4 2 SWAA980362 1 19980321 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, RBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200512 19980402 00512 NM 1998 4 2 SWAA980364 1 19980321 A 5320 ANGLE BOEING 737 7373H4 1384600 NM RT DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND L-ANGLE CORRODED ON OUTBOARD EDGE OF RT DOORWAY Z-ANGLE. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998040200513 19980402 00513 NM 1998 4 2 SWAA980365 1 19980321 A 5320 ANGLE BOEING 737 7373H4 1384600 NM DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND RT FWD DOORWAY Z-ANGLE CORRODED UPPER AND LOWER SRFC AT BS 277 TO 344. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200514 19980402 00514 NM 1998 4 2 SWAA980366 1 19980321 A 5240 SKIN BOEING 737 7373H4 1384600 NM NOSE COMP DOOR GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND NOSE COMP DOOR HAS 2.5 INCH GOUGE ON INSIDE SKIN. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200515 19980402 00515 NM 1998 4 2 SWAA980367 1 19980321 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1005 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED WEB BETWEEN Z-ANGLE AND GALLEY TRACK AT BS 1005, RBL 41. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200516 19980402 00516 NM 1998 4 2 SWAA980363 1 19980321 A 3350 20121 CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389SW 26592 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY LIGHT ABOVE L2 DOOR INOP. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998040200517 19980402 00517 1998 4 2 SWAA980368 4 19980320 A 2565 D31354433 SLIDE BOEING 737 7373H4 1384600 NM CABIN OUT OF DATE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND L-2 EMERGENCY EVACUATION SLIDE OUT OF DATE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998040200518 19980402 00518 NM 1998 4 2 SWAA980369 1 19980320 A 5754 SKIN BOEING 737 7373H4 1384600 NM RT LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED C2 CHECK, FOUND CRACK ON L/E SKIN AT KRUEGER FLAP SEAL DOOR CUTOUT. REPAIRED PER SWA RA 1-357-0538. 2 L 7 2 4F RT A16WE 1998040200519 19980402 00519 NM 1998 4 2 SWAA980370 1 19980320 A 2910 171K1454ER0204 HYD LINE BOEING 737 7373Y0 1384671 NM NLG RUPTURE A SWAA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 699SW 23826 RETURN TO LAS DUE TO NOSE LANDING GEAR FAILING TO RETRACT AND MADE UNEVENTFUL LANDING. INSPECTED AND FOUND NOSE GEAR AC TUATOR UPLOCK HYD LINE RUPTURE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998040200520 19980402 00520 NM 1998 4 2 SWAA980372 1 19980323 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 742 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721SW 22697 DURING SCHEDULED RON CHECK, FOUND CRACK IN FUSELAGE SKIN AT BS 742 AT S16L APPROX 1.25 INCH LENGHT. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1998040200521 19980402 00521 NM 1998 4 2 SWAA980373 1 19980323 A 5320 ANGLE BOEING 737 7373H4 1384600 NM FWD DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND FWD ENTRY DOOR FRAME UPPER FWD CORNER OF FUSELAGE CRACKED L-ANGLE. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200522 19980402 00522 NM 1998 4 2 SWAA980374 1 19980324 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 881-885 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE CRACKED AT BS 881 TO 885 BETWEEN STR 24R AND 25R. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998040200523 19980402 00523 NM 1998 4 2 SWAA980375 1 19980324 A 5320 WEB BOEING 737 7373H4 1384600 NM CARGO COMPT DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO DOOR CUT-OUT, FORWARD LOWER WEB IS DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200524 19980402 00524 NM 1998 4 2 SWAA980376 1 19980325 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1136/1128 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT 2 ADJACENT FASTENERS AT BS 1136, STR 10R AND BS 1128, STR 1 0R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998040200525 19980402 00525 NM 1998 4 2 SWAA980377 1 19980325 A 5320 WEB BOEING 737 7372H4 138448C NM BS 460-480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB CRACKED RT UNDER TRANS ANGLE AT BS 460 TO 480 LBL 24. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998040200526 19980402 00526 NM 1998 4 2 SWAA980378 1 19980325 A 5312 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD SIDE CHORD (RT) CRACKED IN RADIUS AT WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200527 19980402 00527 NM 1998 4 2 SWAA980379 1 19980325 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 201 TO 202, LBL 6.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200528 19980402 00528 NM 1998 4 2 SWAA980380 1 19980325 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 1140 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND STRINGER 5L CRACKED AT BS 1140. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200529 19980402 00529 NM 1998 4 2 SWAA980381 1 19980325 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 1140 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND STRINGER 5R CRACKED AT BS 1140. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200530 19980402 00530 NM 1998 4 2 SWAA980382 1 19980325 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1107 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 1107 BETWEEN STRINGERS 2R AND 3R. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998040200531 19980402 00531 NM 1998 4 2 SWAA980383 1 19980325 A 5330 SKIN BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR CUTOUT LOWER AFT CORNER OUTER SKIN CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200532 19980402 00532 NM 1998 4 2 SWAA980384 1 19980325 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND Z-CHORD AT BS 270, WL 208 CORRODED BETWEEN LBL 11 TO RBL 11. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998040200533 19980402 00533 NM 1998 4 2 SWAA980385 1 19980325 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 270 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200534 19980402 00534 NM 1998 4 2 SWAA980386 1 19980325 A 5330 SKIN BOEING 737 7373T5 NM BS 870 PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING WALKAROUND CHECK, FOUND A SKIN PUNCTURE AND 7 CREASE AT BS 870 BETWEEN STRINGERS 25 AND 26. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200535 19980402 00535 NM 1998 4 2 SWAA980387 1 19980325 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND ATTACH ANGLE CRACKED AT BS BULKHEAD 178 WL 208 RBL 24 TO 20. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998040200536 19980402 00536 NM 1998 4 2 SWAA980388 1 19980325 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS BULKHEAD 178 TO 186 WL 208 RBL 24. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998040200537 19980402 00537 NM 1998 4 2 SWAA980389 1 19980325 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED B/C CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT AND STRAP CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998040200538 19980402 00538 WP 1998 4 2 98FDEA00222 1 19980327 A 5511 SPAR CAP DOUG DC10 DC1010F 3022111 WP LT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 052FE 47806 LT HORIZONTAL STABILIZER REAR SPAR CAP FWD BARREL NUT HOLE HAS A 1.75 INCH CRACK INDICATION, STARTING .25 FROM THE TOP S URFACE AND GOING DOWN PAST THE BARREL NUT ON THE REAR WALL. REF EO 8-5510-7-3310. REMOVED NR 9 HORZ H-11 BOLT PER EA 8 551036-004 FOR BARREL NUT HOLE INSP EDDY CURRENT INSP FOUND 1.75 CRACK. INSTALLED NEW H-11 BOLT 8 WASHERS REF EA 85510- 36002. REMOVED AND REPLACED NUMEROUS HI-LOKS FOR CLEARANCE OF TOOLING AT NR 9 H-11 BOLT AREA. 2 L 7 3 4F A22WE 1998040200539 19980402 00539 NM 1998 4 2 MWEA98375 1 19980323 A 2750 5910035 SWITCH DOUG MD88 MD88 3023688 NM COCKPIT OUT OF ADJUST A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 31 701ME 49760 ON TAKEOFF ROLL AT 90 KNOTS SLAT AURAL WARNING SOUNDED AND SLAT DISAGREEMENT LIGHT ILLUMINATED. MTC CLEANED ADJUSTED AN D TESTED FLAP SLAT HANDLE POSITION SWITCHES. 2 L 7 2 4F RT A6WE 1998040200540 19980402 00540 WP 1998 4 2 MWEA98376 1 19980324 A 3350 08199 LIGHT DOUG DC9 DC914 3022034 WP CABIN CRACKED A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 400ME 45727 THE EMERGENCY FLOOR TRACK LIGHTS HAVE A SMALL PIECE CRACKED OUT AT SEATS 7CD. MTC REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHT COVER SECTION FROM SEAT ROW 4CD TO 7CD. 2 L 7 2 4F A6WE 1998040200541 19980402 00541 WP 1998 4 2 MWEA98377 1 19980326 A 2560 5917689103 COVER DOUG DC9 DC914 3022034 WP DOOR SLIDE LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 600ME 45725 THE FORWARD ENTRY DOOR SLIDE COVER FOUND LOOSE. MTC SECURED SLIDE COVER. 2 L 7 2 4F A6WE 1998040200542 19980402 00542 NM 1998 4 2 P5CA9800706 1 19980321 A 5400 FASTENERS BOEING 747 747132 1384882 NM NR 3 PYLON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 ANCHOR NUTS SURFACE CORROSION ON NR 3 PYLON NAC STA 379 TO 417. CORROSION REMOVED AND RETREATED PER SRM 51-01-01 AND 51 -10-02. 2 L 7 4 4F A20WE 1998040200543 19980402 00543 NM 1998 4 2 P5CA9800707 1 19980321 A 7110 COWL BOEING 747 747132 1384882 NM NR 3 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 PANEL 474BL DELAMINATED TOP LT CORNER OF NR 3 ENGING COWL. HOT BOND REPAIR PER SRM 51-40-06 FIG 17. 2 L 7 4 4F A20WE 1998040200544 19980402 00544 NM 1998 4 2 P5CA9800708 1 19980321 A 5400 FASTENERS BOEING 747 747132 1384882 NM NR 3 PYLON CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON NR 3 PYLON AFT STRUT DIAG BRACE AFT END LARGE HI-LOK HEADS. SURFACE CORROSION REMOVED PER SRM 51-1 0-01. 2 L 7 4 4F A20WE 1998040200545 19980402 00545 NM 1998 4 2 P5CA9800709 1 19980321 A 7110 COWL BOEING 747 747132 1384882 NM NR 4 PYLON CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 ENG NOSE COWL SKIN SURFACE CORROSION. REMOVED SURFACE CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200546 19980402 00546 NM 1998 4 2 P5CA9800710 1 19980321 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2260 WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 SEAT TRACK BS 2260 BL 33 DEEPLY WORN. REPLACED SEAT TRACK PER SRM 53-10-05. 2 L 7 4 4F A20WE 1998040200547 19980402 00547 NM 1998 4 2 P5CA9800711 1 19980321 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 2150 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 MAIN DECK SEAT TRACK BROKEN AT BS 2150 TO 2230. SEAT TRACK REPAIRED PER SRM 53-10-08. 2 L 7 4 4F A20WE 1998040200548 19980402 00548 NM 1998 4 2 P5CA9800712 1 19980321 A 5320 REVEAL BOEING 747 747132 1384882 NM L4 DOORWAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 L4 DOOR CUTOUT LWR REVEAL CRACKED. REMOVED CRACKED AREA PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998040200549 19980402 00549 NM 1998 4 2 P5CA9800713 1 19980321 A 5320 REVEAL BOEING 747 747132 1384882 NM R1 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 R-1 DOOR FWD REVEAL PANEL CRACKED. REPAIRED PER SRM 51-40-03 FIG 3. 2 L 7 4 4F A20WE 1998040200550 19980402 00550 NM 1998 4 2 P5CA9800714 1 19980321 A 5320 TENSION TIE BOEING 747 747132 1384882 NM BS 880 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 TENSION TIE CRACKED AT FUSELAGE BS 880 WL 300. REPAIRED PER SB 53-2371 FIG 3. 2 L 7 4 4F A20WE 1998040200551 19980402 00551 NM 1998 4 2 P5CA9800715 1 19980321 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 520 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK AT BS 520 BL 9. CORROSION REMOVED, REPAIRED AND REPROTECTED PER SRM 51-10-01 , 51-10-02 AND 53-10-05. 2 L 7 4 4F A20WE 1998040200552 19980402 00552 NM 1998 4 2 P5CA9800716 1 19980321 A 5730 SKIN BOEING 747 747132 1384882 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 SURFACE CORROSION ON UPPER SPAR SKIN RT WING. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-03. 2 L 7 4 4F A20WE 1998040200553 19980402 00553 NM 1998 4 2 P5CA9800717 1 19980321 A 5347 TIE DOWN TRACK BOEING 747 747132 1384882 NM BS 1120-1170 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON MAIN DECK TIE DOWN TRACK AT BS 1120 TO 1170 BL R11. REMOVED CORROSION AND REPROTECTED PER SRM 51-1 0-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200554 19980402 00554 NM 1998 4 2 P5CA9800718 1 19980321 A 5320 REVEAL BOEING 747 747132 1384882 NM L5 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 L-5 DOOR UPPER REVEAL CRACKED. REVEAL REPAIRED PER SRM 53-10-04 FIG 9. 2 L 7 4 4F A20WE 1998040200555 19980402 00555 1998 4 2 P5CA9800719 4 19980321 A 3451 BASE BOEING 747 747132 1384882 NM NR 1 DME ANTENNA CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 1 DME ANT BASE CORRODED. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200556 19980402 00556 NM 1998 4 2 P5CA9800720 1 19980321 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LT WING INBD PANEL ABOVE LANDING LIGHT DELAMINATED. FIBERGLASS REPAIRED PER SRM 51-40-12. 2 L 7 4 4F A20WE 1998040200557 19980402 00557 NM 1998 4 2 P5CA9800721 1 19980321 A 7110 COWL BOEING 747 747132 1384882 NM NR 4 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 FAN COWL DELAMINATED. HOT BOND REPAIR PER SRM 51-20-06 FIG 17A. 2 L 7 4 4F A20WE 1998040200558 19980402 00558 NM 1998 4 2 P5CA9800722 1 19980321 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 2310 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT FLOOR SUPPORT FUSELAGE BS 2310 BL 25 TO 33. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200559 19980402 00559 NM 1998 4 2 P5CA9800723 1 19980321 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 2279 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT FLOOR SUPPORT BS 2279 TO 2200 L41. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02 . 2 L 7 4 4F A20WE 1998040200560 19980402 00560 NM 1998 4 2 P5CA9800724 1 19980321 A 5414 PANEL BOEING 747 747132 1384882 NM PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 PANEL 484AL ON PYLON SKIN WORN AND DELAMINATED. HOT BOND REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998040200561 19980402 00561 NM 1998 4 2 P5CA9800725 1 19980321 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 980 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON FLOORBEAM UPPER CHORD AT FUSELAGE BS 980 L2 TO R2. CORROSION REMOVED AND REPROTECTED PER SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200562 19980402 00562 NM 1998 4 2 P5CA9800726 1 19980321 A 5347 TIE DOWN BOEING 747 747132 1384882 NM BS 980 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON TIE DOW AT FUSELAGE BS 980 BL L11. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02 . 2 L 7 4 4F A20WE 1998040200563 19980402 00563 NM 1998 4 2 P5CA9800727 1 19980321 A 5347 TIE DOWN BOEING 747 747132 1384882 NM BS 1000 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION ON TIE DOWN AT FUSELAGE BS 1000 BL R97. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10- 02. 2 L 7 4 4F A20WE 1998040200564 19980402 00564 NM 1998 4 2 P5CA9800728 1 19980321 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1100 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT FLOOR SUPPORT AT FUSELAGE BS 1100 R80 TO R97. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 A ND 51-10-02. 2 L 7 4 4F A20WE 1998040200565 19980402 00565 NM 1998 4 2 P5CA9800729 1 19980321 A 5321 FLOOR PANEL BOEING 747 747132 1384882 NM BS 520 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT FLOOR PANEL FUSELAGE BODY STATION 520 TO 540 BL 8. CORROSION REMOVED AND PANEL REPLACED AND REPROT ECTED PER SRM 51-01-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200566 19980402 00566 NM 1998 4 2 P5CA9800730 1 19980321 A 5320 ANCHOR NUTS BOEING 747 747132 1384882 NM BS 1220 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT FLOOR SUPPORT ANCHOR NUTS. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200567 19980402 00567 NM 1998 4 2 P5CA9800731 1 19980321 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT FLOOR SUPPORT FUSELAGE BS 1220 BL 85 TO 97. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200568 19980402 00568 NM 1998 4 2 P5CA9800732 1 19980321 A 5347 TIE DOWN BOEING 747 747132 1384882 NM BS 2180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT TIE DOWN FUSELAGE BS 2180 BL 30. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200569 19980402 00569 NM 1998 4 2 P5CA9800733 1 19980321 A 5347 TIE DOWN BOEING 747 747132 1384882 NM BS 2300 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT TIE DOWN FITTING SUPPORT FUSELAGE BS 2300 BL 22. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-0 1 AND 51-10-02. 2 L 7 4 4F A20WE 1998040200570 19980402 00570 NM 1998 4 2 P5CA9800734 1 19980321 A 5320 SUPPORT BOEING 747 747132 1384882 NM CABIN CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION MAIN DECK FLOOR SUPPORT BL 22 TO 24. REPAIRED CORROSION PER SRM 51-40-04. 2 L 7 4 4F A20WE 1998040200571 19980402 00571 NM 1998 4 2 P5CA9800735 1 19980305 A 5414 DOOR BOEING 747 747238B 1384828 NM NR 1 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 1 PYLON O/B SIDE OF SAILBOAT DOOR CHAFED FWD END. SANDED OUT CHAFED AREA, APPLIED POTTING COMPOUND, SANDED AND REPAI NTED PER SRM 51-70-00. 2 L 7 4 4F A20WE 1998040200572 19980402 00572 NM 1998 4 2 P5CA9800736 1 19980305 A 5400 BRACE BOEING 747 747238B 1384828 NM NR 1 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 1 PYLON O/B SIDE DIAGONAL BRACE CHAFED FWD END. EDDY CURRENT C/W PER NDT PART 6 54-40-03 WITHIN LIMITS PER SRM 54-40 -01. BLEND OUT AREA SHOT PEENED AND TREATED PER SRM 54-40-01 AND 51-70-00. 2 L 7 4 4F A20WE 1998040200573 19980402 00573 NM 1998 4 2 VNAA9803027 1 19980325 A 5610 001A561A0000201 WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FLIGHT DECK SHATTERED A VNAA K NONE O OTHER DE DESCENT 1 GL 07 459PS 47055 3070 DURING THE DESCENT, THE RT FWD WINDSCREEN WAS STRUCK BY A BIRD. MX FOUND DAMAGE TO THE LT ENG NACELLE COWLINGS. THE FL AP HINGE FAIRING WAS DAMAGED. DAMAGE WAS FOUND ON THE LT PROPELLER SPINNER. MX INSPECTED AND REPLACED THE RT FWD COCKP IT WINDOW IAW DORNIER MM 56-11-00. THE ACFT WAS INSPECTED AND APPROVED FOR A FERRY FLT TO CAK TO COMPLETE REPAIRS. THE FERRY FLT WAS OPERATED WITHOUT ANY PROBLEMS. MX IN CAK REPLACED THE LT ENG CHIN COWLING AND REPAIRED THE SIDE COWLING, IAW DORNIER MM 71-60-03 AND DORNIER SPR 14850. THE SPINNER AND FLAP FAIRING WERE REPLACED IAW DORNIER MM 57-80-00 AND 61-10-00. OPERATION CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998040200665 19980402 00665 NM 1998 4 2 9805206310 1 19980329 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND E-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRING AT TERMINAL STRIP, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998040200666 19980402 00666 NM 1998 4 2 9805212293 1 19980316 A 3260 INDICATION BOEING 727 727251 138408H NM NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 293US 21504 DURING GEAR EXTENSION, NOSE GEAR INDICATED UNSAFE. CYCLED GEAR INCREASED AIRSPEED TO 200 KIAS. RECEIVED SAFE INDICATIO N 1.5 MINUTES LATER. VERIFIED THROUGH VISUAL INSPECTION WINDOW. AIRCRAFT LANDED WITHOUT INCIDENT. JACKED AIRCRAFT AND SWUNG GEAR SEVERAL TIMES. COULD NOT DUPLICATE. LUBRICATED NOSE LANDING GEAR. 2 L 7 3 4F A3WE 1998040200668 19980402 00668 WP 1998 4 2 9805239759 1 19980330 A 3260 SENSOR DOUG DC9 DC941 302207N WP NLG MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 759NW 47287 DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON WITH NO GREEN INDICATION AFTER GEAR EXTENSION. CREW RECYCLE D GEAR AND NORMAL INDICATIONS WERE ACHIEVED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR PROXIMIT Y SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200669 19980402 00669 WP 1998 4 2 9805249139 1 19980330 A 3397 WIRE DOUG DC9 DC914 3022034 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 948L 47049 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD CABIN EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. REPAIRED WIRING TO LIGHTING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200670 19980402 00670 WP 1998 4 2 9805259877 1 19980330 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998040200671 19980402 00671 WP 1998 4 2 9805269603 1 19980330 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 603NW 47101 FLIGHT ATTENDANT REPORTED, FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200672 19980402 00672 WP 1998 4 2 9805279615 1 19980330 A 3397 BR963150 WIRE HARNESS DOUG DC9 DC932 3022066 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 615NW 47129 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 13 INOPERATIVE. REPLACED WIRE HARNESS ASSEMBLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998040200673 19980402 00673 NM 1998 4 2 UPS98226204 1 19980324 A 2730 CLEVIS BOEING 727 72731C 1384011 NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, LT ELEVATOR HAS CRACKED LUGS AT NR 3 HINGE POINT AT ES 66.5. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-08-001, UPS FILE NUMBER 727-55-0366 AND BOEING SERVICE BULLETIN 727-55-53 REV 3FIGURE 6 AND DRAWING NUMBER 65-6 8883. 2 L 7 3 4F A3WE 1998040200674 19980402 00674 NM 1998 4 2 UPS98226205 1 19980330 A 5400 WEB BOEING 727 72731C 1384011 NM BS 1381 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, CRACK ON WEB ABOVE NUMBER 2 ENGINE HORIZONTAL FIREWALL LT SIDE AT BS 1381. NEW WEB FABRICATED AND IN STALLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1998040200675 19980402 00675 NM 1998 4 2 UPS98226206 1 19980330 A 5400 WEB BOEING 727 72731C 1384011 NM BS 1381 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1381. NEW WEB FABRICATED AND INS TALLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1998040200676 19980402 00676 NM 1998 4 2 UPS98226207 1 19980313 A 5320 65159682 FITTING BOEING 727 72731C 1384011 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, BS 740 RT FUSELAGE FITTING HAS SEVERAL CRACKS ON OUTBD FLANGE BETWEEN S18R AND 23R. FITTING REPLACED IAW UPS ENGINEEIRNG ORDER B727-5310-7477 AND SRS ENGINEERING ORDER 98-08-003, REF UPS EO B727-5310-10331-A. 2 L 7 3 4F A3WE 1998040200677 19980402 00677 NM 1998 4 2 UPS98226208 1 19980313 A 5320 65159681 FITTING BOEING 727 72731C 1384011 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, BS 740 LT FUSELAGE FITTING HAS SEVERAL CRACKS ON OUTBD FLANGE BETWEEN S18L AND 23L. FITTING REPLACED IAW UPS ENGINEERING ORDER B727-5310-7477 AND SRS EO 98-08-002, REF UPS EO B727-5310-10332-A. 2 L 7 3 4F A3WE 1998040200678 19980402 00678 NM 1998 4 2 UPS98226209 1 19980316 A 2760 65375393 ROD END BOEING 727 72731C 1384011 NM NR 6 SPOILER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, NR 6 GROUND SPOILER CASTING AND LINKAGE HAS EXCESSIVE PLAY. REPLACED WORN ACTUATOR CASTING LINKAGE R OD END AND BOLT IAW MM 27-6 2-81. 2 L 7 3 4F A3WE 1998040200679 19980402 00679 NM 1998 4 2 UPS98226210 1 19980316 A 2760 ROD END BOEING 727 72731C 1384011 NM NR 7 SPOILER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, NR 7 GROUND SPOILER CASTING AND ACTUATOR ROD END HAS EXCESSIVE PLAY. REPLACED SPOILER CASTING IAW MM 27-62-81 AND REPLACED ACTUATOR ROD END IAW OHM 27-60-01. 2 L 7 3 4F A3WE 1998040200680 19980402 00680 NM 1998 4 2 UPS98226211 1 19980316 A 2760 CASTING BOEING 727 72731C 1384011 NM NR 9 SPOILER WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, NR 9 GROUND SPOILER (ACTUATOR) CASTING HAS EXCESSIVE PLAY AT HINGE POINT. REPLACED ACTUATOR CASTING IAW MM 27-61-91. 2 L 7 3 4F A3WE 1998040200681 19980402 00681 NM 1998 4 2 UPS98226212 1 19980320 A 5754 RIB BOEING 727 72731C 1384011 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, NR 4 LE SLAT CRACK ON RIB (THIRD FROM OUTBD). DAMAGED AREA BLENDOUT IAW SRM 51-40-01. 2 L 7 3 4F A3WE 1998040200682 19980402 00682 NM 1998 4 2 UPS98226213 1 19980316 A 2810 382221 DOUBLER BOEING 727 72731C 1384011 NM NR 1 TANK CORRODED A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, FUEL LEAK AT NR 1 TANK OVERWING REFUELING AREA ON INVESTIGATION, ADAPTER FILLER AND INTERNAL DOUBLER FOUND CORRODED. REPLACED CORRODED PARTS IAW DRAWING 65-19299. 2 L 7 3 4F A3WE 1998040200683 19980402 00683 NM 1998 4 2 UPS98226214 1 19980320 A 5754 RIB BOEING 727 72731C 1384011 NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, NR 4 LE SLAT CRACK ON RIB (THIRD FROM OUTBOARD). REPAIR CARRIED OUT IAW SRM 51-40-3 FIGURE 1. 2 L 7 3 4F A3WE 1998040200684 19980402 00684 NM 1998 4 2 UPS98226215 1 19980320 A 5730 SKIN BOEING 727 72731C 1384011 NM WS 198 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, RIGHT HAND LE INNER SKIN CRACKED AT WS 198. INNER SKIN CUT OUT AND REPAIR CARRIED OUT IAW SRM 57-30- 4. 2 L 7 3 4F A3WE 1998040200685 19980402 00685 NM 1998 4 2 UPS98226216 1 19980318 A 2710 65742845 CASTING BOEING 727 72731C 1384011 NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, LT AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LOWER SUPPORT LUG FOR TAB PULLEY. CASTING REPL ACED IAW OHM 27-12-00. 2 L 7 3 4F A3WE 1998040200686 19980402 00686 NM 1998 4 2 UPS98226217 1 19980324 A 5311 FRAME BOEING 727 72731C 1384011 NM BS 360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 924UP 19234 INSPECTION TYPE-C, FRAME CRACKED AT FWD RT ST 360 RIGHT HAND SIDE AT STRINGER 25 APPROX. FRAME REPAIRED IAW SRM 51-40-3 . 2 L 7 3 4F A3WE 1998040200687 19980402 00687 WP 1998 4 2 UPS98826196 1 19980311 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 220-240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C/CK, FWD LOWER CARGO L36 CORRODED, STA 220 TO 240. REMOVED CORROSION, REMOVED LONGERON BOTH HALVES AN D LOCATED AND DRILLED NEW LONGERON HALVES IAW DC8 SRM 51-18, 53-2-0, 51-1-24, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998040200688 19980402 00688 WP 1998 4 2 UPS98826197 1 19980313 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C/CK, FUSELAGE STATION 450 LONGERON 31 LEFT TP 31 RIGHT FINGER DOUBLER CORRODED. REMOVED DOUBLER, FABB ED NEW ONE IAW DAC DWG 5755271. INSTALLED NEW DOUBLER IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998040200689 19980402 00689 WP 1998 4 2 UPS98826198 1 19980313 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C/CK, REMOVED AND REPLACED FWD INTERNAL SKIN DOUBLER. REMOVED DOUBLER, FABBED NEW ONE IAW DC8 SRM 51-1- 24. NEW DOUBLER TO BE INSTALLED ON UPS NR 522669. 2 L 7 4 4F RT 4A25 1998040200690 19980402 00690 WP 1998 4 2 UPS98826199 1 19980309 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C/CK, CRACKS AT 2 SCREW HOLES, LEFT HAND LEADING EDGE AT XFS 700, BOTTOM OF LEFT WING. FABBED REPAIR DO UBLER AND INSTALLED WITH RIVETS IAW UPS EO 5720 4082. 2 L 7 4 4F RT 4A25 1998040200691 19980402 00691 WP 1998 4 2 UPS98826201 1 19980314 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C/CK, ZEE FITTING CORRODED, STA 300, LONGERON 32-33 LEFT. REMOVED FITTING, DRILLED AND INSTALLED NEW ON E IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998040200692 19980402 00692 WP 1998 4 2 UPS98826202 1 19980314 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C/CK, ZEE FITTING STA 270, LONGERON 33-34 RIGHT CORRODED. REMOVED FITTING, DRILLED AND INSTALLED NEW ON E IAW DC8 SRM 51-3-2, 51-1-20D, AND 51-1-8. 2 L 7 4 4F RT 4A25 1998040200693 19980402 00693 WP 1998 4 2 UPS98826203 1 19980312 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1170 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C/CK, ALC C-3 DOOR LOWER JAMB BACKUP FITTING CORRODED, STA 1170. REMOVED Z-FITTING, DRILLED AND INSTALL ED IAW DC8 SRM 51-1-8, AND 51-1 20D, 2 NEW FITTING. REMOVED CORROSION FROM A THIRD FITTING, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998040200694 19980402 00694 NM 1998 4 2 98FDEA00223 1 19980331 A 2133 10328051 OUTFLOW VALVE BOEING 727 72722C 138400F NM AFT FUSELAGE FAILED A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 102FE 19193 AIRCRAFT WILL NOT PRESSURIZE IN NORMAL OR AUTOMATIC. NO AUTHORITY WITH MANUAL WITH FULL INCREASE PRESSURE. CABIN VERTI CAL SPEED INDICATOR FULL CLIMB THROUGHOUT. *S/D* REPLACED LEFT OUTFLOW VALVE PER MAINTENANCE MANUAL 21-30-51, PERFORME D SYSTEM ADJUSTMENT TEST AS PER 21-30-0. SYSTEM OPERATIONAL CHECKS GOOD ON GROUND IN MANUAL AND AUTO MODE. 2 L 7 3 4F A3WE 1998040200695 19980402 00695 NM 1998 4 2 98FDEA00224 1 19980331 A 3213 AXLE BOEING 727 727277 138408S NM NR 1 WHEEL SHEARED A A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 245FE 22016 DURING WALKAROUND INSPECTION, FOUND THE NR 1 WHEEL ASSEMBLY AXLE TO BE SHEARED AT THE AXLE NUT. TIRE AND WHEEL REMAINED INTACT ON AXLE. *S/D* REMOVED AND REPLACED MAIN LANDING GEAR INNER STRUT, NR 1 AND NR 2 TIRES AND BRAKES, NR 2 ANTI- SKID DETECTOR. SERVICED STRUT, BRAKES AND ANTI-SKID OPERATIONAL CHECK GOOD. 2 L 7 3 4F RT A3WE 1998040200696 19980402 00696 WP 1998 4 2 ABXA9800266 1 19980325 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 16L CRACKED AT HI-LOK AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998040200697 19980402 00697 WP 1998 4 2 ABXA9800267 1 19980325 A 5313 591140125 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 130-160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 25R CORRODED BETWEEN STATION 130 AND 160. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998040200698 19980402 00698 WP 1998 4 2 ABXA9800268 1 19980325 A 5311 995774011 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 637 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND FRAME AT STATION 637 CRACKED IN THE LEFT KEEL BEAM ON THE OUTBOARD END. REPAIRED FRAME IAW DC9 SR M 53-03. 2 L 7 2 4F A6WE 1998040200699 19980402 00699 WP 1998 4 2 ABXA9800269 1 19980325 A 5313 5916441507 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 408/427 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 29L CRACKED BETWEEN STATION 408 AND 427. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998040200700 19980402 00700 WP 1998 4 2 ABXA9800270 1 19980325 A 5320 4912460501 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 907 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND INTERCOSTAL CORRODED IN AFT LOWER CARGO DOOR JAMB POCKET AT STATION 907 AND LONGERON 28R. REPLACE D INTERCOSTAL TEE FITTING IAW DC9 SRM. 2 L 7 2 4F A6WE 1998040200701 19980402 00701 WP 1998 4 2 ABXA9800271 1 19980326 A 5320 39132091 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 579 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 29L FITTING CRACKED JUST FWD OF STATION 579. REPLACED END FITTING IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998040200702 19980402 00702 WP 1998 4 2 ABXA9800272 1 19980326 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 16R CORRODED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998040200703 19980402 00703 WP 1998 4 2 ABXA9800273 1 19980326 A 5330 591141247 SKIN DOUG DOUG DC9 DC932 3022066 WP BS 439 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND FUSELAGE SKIN AT STATION 439 BETWEEN LONGERON 30 AND LONGERON 29L BULGED AND CORRODED BEYOND LIMIT S. REPAIRED SKIN IAW DC9 SRM 53-04. 2 L 7 2 4F A6WE 1998040200704 19980402 00704 WP 1998 4 2 ABXA9800274 1 19980326 A 5311 995823869N FRAME DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND FRAME AT STATION 980 AND LONGERON 16L AND 17L CRACKED AT HI-LOK. REPAIRED IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998040200705 19980402 00705 WP 1998 4 2 ABXA9800275 1 19980326 A 5320 3916174501 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 604 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 29L END FITTING CRACKED AFT OF STATION 604. REPLACED END FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998040200706 19980402 00706 WP 1998 4 2 ABXA9800276 1 19980327 A 5320 39161741 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 604 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 DURING C-CHECK, FOUND LONGERON 29R FITTING CRACKED AFT OF STATION 604. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998040200707 19980402 00707 WP 1998 4 2 ABXA9800277 1 19980327 A 5313 59114268 LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LONGERON 13R CRACKED AT PYLON BULKHEAD AND STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998040200708 19980402 00708 WP 1998 4 2 ABXA9800278 1 19980327 A 5313 59114267 LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LONGERON 13L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998040200709 19980402 00709 WP 1998 4 2 MWEA98378 1 19980328 A 2560 SMOKE GOGGLE DOUG DC9 DC932 3022066 WP COCKPIT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND SMOKE GOGGLE COMPARTMENT FULL OF WATER. MTC DRAINED COMPARTMENT AND REMOVED AND REPLACED CRACKED GOGGLE. 2 L 7 2 4F A6WE 1998040200710 19980402 00710 WP 1998 4 2 MWEA98379 1 19980317 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP GALLEY DOOR LACK OF LUBE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 207ME 47794 THE RIGHT GALLEY GIRT BAR IS DIFFICULT TO PUT IN THE ARMED POSITION. MTC CLEANED AND LUBED GALLEY DOOR GIRT BAR. 2 L 7 2 4F A6WE 1998040200711 19980402 00711 WP 1998 4 2 MWEA98380 1 19980327 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 502ME 48132 THE GALLEY SLIDE COVER CAME OFF. MTC RESECURED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998040200712 19980402 00712 WP 1998 4 2 MWEA98381 1 19980328 A 7930 42D1091A BY-PASS SWITCH DOUG DC9 DC915 3022036 WP RT ENGINE DEFECTIVE A MWEA O OTHER N FALSE WARNING CR CRUISE 1 GL 31 300ME 45718 THE RIGHT OIL STRAINER CLOGGING LIGHT ILLUMINATED IN FLIGHT AND PERFORMED PRECAUTIONARY LANDING. MTC REMOVED AND REPLAC ED OIL FILTER AND ENGINE OIL PRESSURE DIFFERENTIAL SWITCH. 2 L 7 2 4F A6WE 1998040200713 19980402 00713 WP 1998 4 2 MWEA98382 1 19980328 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 301ME 47190 DURING SERVICE CHECK, FOUND CABIN EMERGENCY LIGHTS FORWARD OF EMERGENCY EXIT SEATS ON WITH POWER OFF. MTC REMOVED AND R EPLACED FORWARD EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1998040200714 19980402 00714 WP 1998 4 2 SCNA98026 1 19980323 A 5312 BULKHEAD WEB DOUG DC10 DC1010 3022110 WP BS 595 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 46977 DURING SCHEDULED MAINTENANCE, FOUR CRACKS WERE FOUND AT STA 595 LEFT HAND SIDE LONGERON 43 INBOARD OF AREA A REFERENCE NDI MANUAL 531003 FIGURE 1. AREA REPAIRED IN ACCORDNACE WITH DOUGLAS REWORK DRAWING SR105300647001. 2 L 7 3 4F A22WE 1998040200715 19980402 00715 NM 1998 4 2 DHL98724001 1 19980330 A 5753 SKIN BOEING 727 727228 NM RT TE MIDFLAP TORN A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 724DH 19862 AIRFRAME VIBRATES NOTICED DURING CLIMBOUT MAKING TURNS TO THE LEFT AND RIGHT. CHECKED ALL FLT CONTROLS VISUALLY AND OPE RATIONALLY, CHECKED FLAP ROLLER CLEARANCE. FOUND MISSING UPPER SKIN ON RT MIDFLAP TRAILING EDGE 20 X 3. INSTALLED INT ERM REPAIR PER NR 98DHL1.21RO-1 ENGINEERING DATA. 2 L 7 3 4F A3WE 1998040200716 19980402 00716 1998 4 2 DHL98741001 4 19980331 A 3442 MI585161 RT UNIT BOEING 727 7272Q9 138448M NM FWD FUSELAGE FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 741DH 21931 WEATHER RADAR WILL NOT PAINT GROUND RETURN BETWEEN 30 DEGREES LEFT AND 30 DEGREES RIGHT OF NOSE UNLESS TILT ADJUSTED 7 DEGREES NOSE DOWN. SOLID GROUND RETURN OUTSIDE OF 30 DEGREES LEFT AND RIGHT. REPLACED R/T, OPS CHECK GOOD PER BOEING M M 34-41-0. 2 L 7 3 4F RT A3WE 1998040200717 19980402 00717 NM 1998 4 2 P5CA9800738 1 19980325 A 2911 26604725 ACCUMULATOR BOEING 747 747132 1384882 NM NR 4 HYD SYST RUPTURED A P5CA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 23 857FT 20246 DURING APPROACH, AFTER GEAR DOWN LOST NR 4 HYD SYSTEM, 0 BRAKE PRESSURE ON GUAGE. HYD BRAKE ACCUMULATOR RUPTURED, DAMAG E TRIM AIR DUCT, APU FUEL DRAIN LINE, HYD LINE DAMAGE. 2 L 7 4 4F A20WE 1998040200718 19980402 00718 NM 1998 4 2 P5CA9800739 1 19980325 A 5753 FOREFLAP BOEING 747 747124 1384874 NM RT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 ON POST FLT WALKAROUND, FOUND APPROX 13 FT OF OUTBD FOREFLAP MISSING FROM RIGHT SIDE OF AIRCRAFT. REPAIRED BY BOEING PE R WORK DOCUMENT NR 6-117-RE-706. 2 L 7 4 4F A20WE 1998040200719 19980402 00719 NM 1998 4 2 P5CA9800740 1 19980325 A 2730 PCU BOEING 747 747123 1384873 NM LT ELEVATOR FAILED A P5CA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 23 858FT 20109 LOST 1.5 GALS FLUID FROM NR 1 HYDRO SYSTEM AT TOP OF DESCENT. FOUND LT OUTBOARD ELEVATOR PCU FILTER AREA LEAKING. REMO VED AND REPLACED LT ELEVATOR OUT BOARD PCU PER MM 27-31-08 SERVICED HYD FLUID. LEAK CHECK OK, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 1998040200720 19980402 00720 NM 1998 4 2 P5CA9800741 1 19980326 A 2910 HYD LINE BOEING 747 747122 1384872 NM LT MLG WW FAILED A P5CA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 854FT 19754 HYDRAULIC LEAK IN AREA OF LEFT WING ROOT, AFT PORTION OF W/W. REMOVED AND REPLACED HYD LINE PER 20-11-05 NEAR WING GEAR AFT TRUNNION. LEAK CK OK. 2 L 7 4 4F A20WE 1998040200721 19980402 00721 NM 1998 4 2 P5CA9800742 1 19980328 A 2751 98010903 POSITION IND BOEING 747 747123 1384873 NM LT TE FLAP FAILED A P5CA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 23 858FT 20109 ON CLIMB WHEN FLAPS UP SELECTED, LT INBD T/E FLAPS SHOWED 1 DEGREE, RT INBD T/E FLAPS SHOWED UP. AIRCRAFT RETURNED TO O RD. INSP FLAPS NO DEFECT NOTED, FOUND LT INBD POS IND STUCK AT 1 DEGREE POS. REPLACED INBD FLAP POS IND CHK OK PER MM 27-57-00. FLAP POS IND OP CK THRU SEVERAL CYC PER MM 27-57-00. 2 L 7 4 4F A20WE 1998040200722 19980402 00722 WP 1998 4 2 ARWA980309 1 19980330 A 5230 AE727102311 LINK DOUG DC8 DC862 3021970 WP CARGO DOOR BENT A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 1804 45896 ON OPENING OF MAIN CARGO DOOR FOUND FOUR LONG LINK ASSYS BENDING. REMOVED AND REPLACED 4 LONG LINK ASSY FOR FWD ACTUATO R END, FOUR ACT. AFT AND FWD IAW CARGO CONVERSION MM CHIP 7-08. OPS NORMAL ALL INDICATIONS NORMAL SEVERAL TIMES. 2 L 7 4 4F 4A25 1998040200723 19980402 00723 WP 1998 4 2 ARWA980310 1 19980330 A 2711 H2024B SWITCH DOUG DC8 DC863F 302198F WP AILERON TAB FAILED A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 661AV 45969 DURING TAXI AND T/O CHECK, AILERON REVERSION LIGHT DID NOT GO OUT WITH THE AILERON POWER LEVEL ON. RECYCLED, NO HELP. R EMOVED AND REPLACED AILERON MANUAL CONTROL INDICATING SWITCH, GROUND OPS CHECKED NORMAL PER MM 27-11-14. 2 L 7 4 4F 4A25 1998040200724 19980402 00724 WP 1998 4 2 ARWA980311 1 19980331 A 2110 B125B DUCT DOUG DC8 DC862 3021970 WP NR 3 TURBOCOMP FAILED A ARWA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 19 802BN 45909 AT 39,000 LOSS PRESSURIZATION, PROCED FOR EMERGENCY DESCENT. RETURNED TO MIAMI. AT ARRIVAL AIRCRAFT WILL NOT ACCEPT EX TERNAL POWER. FOUND CLAMP TO NR 3 T/C DUCT HAD FAILED, CAUSING DUCT TO COME LOOSE. RESECURED DUCT WITH NEW CLAMP AND P ERFORMED OPS CHECK OF PRESSURIZATION SYSTEM. OPS CK'D NORMAL PER MM 21-30-01. REPAIRED WIRE IAW 21-51-00 AND REMOVED A ND REPLACED EXTERNAL POWER RELAY. CHECK NORMAL IAW MM 24-40-0. 2 L 7 4 4F 4A25 1998040200725 19980402 00725 NE 1998 4 2 TC8A98017 2 19980328 A 7230 COMPRESSOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 181SK 45910 669217 REJECTED TAKEOFF AT 80 KNOTS DUE TO COMPRESSOR STALL NR 2 ENGINE. MAX THRUST WAS USED, 1.90 EPR. INSPECTED INLET AREA, EXHAUST AREA AND INNER STAGE BLEED VALVE, NO DEFECTS NOTED. RUN-UP ENGINES, ACCOMPLISHED BY CAPTAIN, BLEED VALVES OFF, BLEED VALVES ON AND ANTI-ICE VALVES ON. OPERATION OF BLEED VALVE CLOSES AT 58 PERCENT N1. RUN-UP OK, OPERATION VALVE, NO DEFECTED NOTED IAW MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1998040200727 19980402 00727 SW 1998 4 2 HEEA0013463 1 19980319 A 2910 212076006007 VALVE ASSY BELL 412 412 1182202 SW HYD SYS FAILED E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 3893L 33006 REMOTE BYPASS INDICATOR ON. 1 G 7 2 4U H4SW 1998040200728 19980402 00728 1998 4 2 HEEA0013465 4 19980319 A 2211 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 INTERMITTENTLY FAILS TEST 2.1 ON SST. 1 G 7 2 4U H4SW 1998040200729 19980402 00729 1998 4 2 HEEA0013466 4 19980319 A 3414 412075009105 INDICATOR BELL 412 412 1182202 SW AIRSPEED STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 AIRSPEED NEEDLE STICKS AND HAS ERRATIC OPERATION. 1 G 7 2 4U H4SW 1998040200730 19980402 00730 1998 4 2 HEEA0013467 4 19980319 A 3422 5223241000 GYRO COMPASS BEECH 200 200CBEECH 1152926 CE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 500PH BL29 GYRO COMPASS SLOW TO SLAVE. 1 L 7 2 4T A24CE 1998040200731 19980402 00731 EU 1998 4 2 HEEA0013468 1 19980319 A 2436 51565000R REGULATOR BOLKMS 105 BO105S 5626006 EU DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T S111 VOLTAGE WILL NOT ADJUST. 1 G 7 2 3U H3EU 1998040200732 19980402 00732 1998 4 2 HEEA0013469 4 19980319 A 3422 40205773 GYRO BOLKMS 117 BK117B2 5626013 EU COCKPIT DG FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 134AE 7237 FAILED TEST 1.1 ON SST NO VALID. 1 G 7 2 3U NC H13EU 1998040200733 19980402 00733 EU 1998 4 2 HEEA0013470 1 19980319 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 81832 S828 MAST MOMENT TRANSMITTER WILL TEST BUT WILL NOT WORK IN FLIGHT. 1 G 7 2 3U H3EU 1998040200734 19980402 00734 EU 1998 4 2 HEEA0013471 1 19980319 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 81832 S828 INDICATOR WILL TEST BUT WILL NOT WORK IN FLIGHT. 1 G 7 2 3U H3EU 1998040200735 19980402 00735 SW 1998 4 2 HEEA0013472 1 19980319 A 3340 A490ATSDF1428 POWER SUPPLY BELL 206 206L1 1182107 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5006F 45181 STROBE POWER SUPPLY INOPERATIVE. 1 G 7 1 3U H2SW 1998040200736 19980402 00736 SW 1998 4 2 HEEA0013473 1 19980319 A 7931 APTE138100G TRANSMITTER BELL 412 412 1182202 SW OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 TRANSMITS 20 PSI HIGH. 1 G 7 2 4U H4SW 1998040200737 19980402 00737 SW 1998 4 2 HEEA0013474 1 19980319 A 7931 APTE138150G TRANSMITTER BELL 212 212 1181420 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 4461 31304 TRANSMITS LOW OUT OF TOLERANCE. 1 G 7 1 4U H4SW 1998040200738 19980402 00738 SW 1998 4 2 HEEA0013475 1 19980319 A 2930 124043 INDICATOR BELL 412 412 1182202 SW HYD SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 HYD SYS TEMP. NEEDLE STICKS. PAINT RANGE MARKING. 1 G 7 2 4U H4SW 1998040200739 19980402 00739 SW 1998 4 2 HEEA0013477 1 19980319 A 7714 206075682107 GAGE BELL 206 206L3 1182108 SW GAS PRODUCER ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6603X 51412 GAS PRODUCER GAGE SMALL NEEDLE IS ERRATIC. 1 G 7 1 3U H2SW 1998040200740 19980402 00740 SW 1998 4 2 HEEA0013478 1 19980319 A 7714 206070266009 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50182 45242 INDICATOR WILL NOT INDICATE. 1 G 7 1 3U H2SW 1998040200741 19980402 00741 SW 1998 4 2 HEEA0013479 1 19980319 A 2841 393008047 INDICATOR BELL 412 412 1182202 SW FUEL QTY DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 WHEN TURNED OFF INDICATOR RISES TO 150 LBS. 1 G 7 2 4U H4SW 1998040200742 19980402 00742 SW 1998 4 2 HEEA0013480 1 19980319 A 7712 206075185001 TORQUE GAUGE BELL 206 206B3 1181506 SW ENG TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2285B 3642 TORQUE GAUGE EXCESSIVE FRICTION ERROR. 1 G 7 1 3U H2SW 1998040200743 19980402 00743 SW 1998 4 2 HEEA0013481 1 19980319 A 7712 206075739103 TORQUEMETER BELL 206 206L3 1182108 SW ENGINE STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31801 51074 TORQUEMETER NEEDLE STICKS AT 6%. 1 G 7 1 3U H2SW 1998040200744 19980402 00744 1998 4 2 HEEA0013482 4 19980319 A 3422 2594484 TRANSMITTER BELL 214 214ST 1182106 SW FLUX VALVE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 TRANSMITTER READS LOW OUT OF TOLERANCE. 2 G 7 2 4U H10SW 1998040200745 19980402 00745 1998 4 2 HEEA0013483 4 19980319 A 3422 2594484 TRANSMITTER BELL 214 214ST 1182106 SW FLUX VALVE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 TRANSMITTER EXCESSIVE READINGS. 2 G 7 2 4U H10SW 1998040200746 19980402 00746 1998 4 2 HEEA0013484 4 19980319 A 3422 2594484 TRANSMITTER BELL 212 212 1181420 SW FLUX VALVE ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 FLUX VALVE HAS ERRATIC READINGS. 1 G 7 1 4U H4SW 1998040200747 19980402 00747 EU 1998 4 2 HEEA0013485 1 19980319 A 7714 4011001 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 205UC S668 INDICATOR READS TOO LOW AT FLIGHT. 1 G 7 2 3U H3EU 1998040200748 19980402 00748 SW 1998 4 2 HEEA0013486 1 19980319 A 2437 209070264003 DUAL AMMETER BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 NR2 NEEDLE WILL NOT INDICATE. 1 G 7 2 4U H4SW 1998040200749 19980402 00749 SW 1998 4 2 HEEA0013487 1 19980319 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 STEP ACTUATOR INOPERATIVE POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1998040200750 19980402 00750 1998 4 2 HEEA0013488 3 19980319 A 6140 503890571 TACH GENERATOR BEECH 200 200BEECH 1152920 CE PROP ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30PH BB635 ERRATIC OUTPUT. 1 L 7 2 4T A24CE 1998040200751 19980402 00751 1998 4 2 HEEA0013489 3 19980319 A 6140 503890571 TACH GENERATOR BEECH 200 200BEECH 1152920 CE PROP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30PH BB635 NR1 GAUGE STAYS ON ZERO. 1 L 7 2 4T A24CE 1998040200752 19980402 00752 1998 4 2 HEEA0013490 4 19980319 A 3425 656767 COMPENSATOR BELL 212 212 1181420 SW COCKPIT HSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 COMPENSATOR WILL NOT ADJUST. 1 G 7 1 4U H4SW 1998040200753 19980402 00753 1998 4 2 HEEA0013491 4 19980319 A 3416 8800 ENCODER BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 ALTITUDE ENCODER INTERMITTENTLY CAUSES GPS TO DISPLAY NO ATTITUDE INPUT. 1 G 7 2 4U H4SW 1998040200754 19980402 00754 1998 4 2 HEEA0013492 4 19980319 A 3416 8800 ENCODER BEECH 200 200BEECH 1152920 CE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 30PH BB635 ENCORDER FAULTY NO ATTITUDE INPUT ON GPS. 1 L 7 2 4T A24CE 1998040200755 19980402 00755 EU 1998 4 2 HEEA0013493 1 19980319 A 2422 SS120 STATIC INVERTER BOLKMS 117 BK117B2 5626013 EU AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 STATIC INVERTER INTERMITTENT. 1 G 7 2 3U NC H13EU 1998040200756 19980402 00756 SW 1998 4 2 HEEA0013494 1 19980319 A 6710 206062721113 ACTUATOR BELL 206 206B3 1181506 SW DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2285B 3642 ACTUATOR STICKS AND INTERMITTENT. 1 G 7 1 3U H2SW 1998040200757 19980402 00757 SW 1998 4 2 HEEA0013495 1 19980319 A 2435 2CM272B1 STARTER BELL 214 214ST 1182106 SW START GENERATOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 141 28139 STARTER WILL NOT SPIN. 2 G 7 2 4U H10SW 1998040200758 19980402 00758 SW 1998 4 2 HEEA0013496 1 19980319 A 5310 206033099181 PANEL BELL 206 206L1 1182107 SW FUSELAGE MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5007Y 45192 INSERTS FOR FUEL CROSSOVER MISLOCATED FROM BELL. 1 G 7 1 3U H2SW 1998040200759 19980402 00759 1998 4 2 HEEA0013497 4 19980319 A 3457 0110005400 GPS 150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB S751 CANNOT ACQUIRE SATELLITES FOR 1 1/2 HOURS ON 1ST FLIGHT OF DAY. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT TO TAKE EX CESSIVELY LONG TO LOCK ON. 1 G 7 2 3U H3EU 1998040200760 19980402 00760 EU 1998 4 2 HEEA0013498 1 19980319 A 6520 350A33109100 GEARBOX 350A33020005 AEROSP AS355 AS355F1 8680810 EU T/R NOISY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 M2210 GEARBOX WAS OVERHAULED AND NEW GEARS WERE INSTALLED. STATIC PATTERNS ON GEARS MATCHED TESTER SHEET AS REQUIRED. AFTER A FLIGHT OF 15 MINUTES CREW HEARD A HIGH PITCH NOISE FROM GEARBOX. GEARBOX WAS DIASSEMBLED AND COULD NOT FIND ANY DISCR EPANCIES. NOTICED THAT PINION GEAR HAD A ZF SERIAL NUMBER AND BEVEL GEAR HAD A M AS A PREFIX WHICH IS UNCOMMON, PLEASE EVALUATE. 1 G 7 2 3U H11EU 1998040200761 19980402 00761 SW 1998 4 2 HEEA0013499 1 19980319 A 2432 30703001 BATTERY BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 INSPECTED BY SHOP. FOUND BATTERY HAS NUMEROUS BURNT CELLS AND WILL NOT PASS CAPACITY TEST. 1 G 7 2 4U H4SW 1998040200762 19980402 00762 SW 1998 4 2 HEEA0013500 1 19980319 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X 51486 UNABLE TO ADJUST STROKE TO PROPER SETTINGS. 1 G 7 1 3U H2SW 1998040200763 19980402 00763 GL 1998 4 2 HEEA0013501 2 19980319 A 7314 3944001 FUEL PUMP SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENG FUEL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 9673 760050 FUEL PUMP WORN SPLINES. 1 G 7 2 3U 3 U H1NE E1GL 1998040200764 19980402 00764 GL 1998 4 2 HEEA0013502 2 19980319 A 7314 3881005 FUEL PUMP BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENG FUEL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 42EA 5377 51542 FUEL PUMP HAS WORN SPLINES. 1 G 7 1 3U 3 U H2SW E1GL 1998040200765 19980402 00765 1998 4 2 HEEA0013503 4 19980319 A 3416 8503S20LW5V ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 ALTIMETER INDICATES OUT OF TOLERANCE AT APPROXIMATELY 18,000 FEET. ALSO UNIT HAS CLICKING NOISE WHILE BEING RUN. 1 G 7 2 3U H1NE 1998040200766 19980402 00766 SW 1998 4 2 HEEA0013504 1 19980319 A 7712 206075739103 TORQUEMETER BELL 206 206L3 1182108 SW ENG TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X 51486 TORQUE GAUGE FOR ENGINE FILLS UP WITH OIL WHEN ENGINE IS RUNNING. SEE OIL IN SIGHT GLASS FACE AND LEAKS ON PANEL. 1 G 7 1 3U H2SW 1998040200767 19980402 00767 EU 1998 4 2 HEEA0013505 1 19980319 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y 2891 S669 M/R BLADE NOSE AND NECK SHELL CRACKED AND SEPARATED. 1 G 7 2 3U H3EU 1998040200768 19980402 00768 EU 1998 4 2 HEEA0013506 1 19980319 A 6210 10515141 BLADE BOLKMS 105 BO105S 5626006 EU M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y 2891 S669 M/R BLADE NOSE AND NECK SHELL CRACKED AND SEPARATED. 1 G 7 2 3U H3EU 1998040200769 19980402 00769 SW 1998 4 2 HEEA0013507 1 19980319 A 6210 412015300106 BLADE BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 6113 BLADE WAS REPAIRED NEAR THE MIDSPAN TAB WHICH HAS CAUSED THE TIP TO EXCEED THE MAX WEIGHT LIMIT BY 161 GR. 1 G 7 2 4U H4SW 1998040200770 19980402 00770 GL 1998 4 2 HEEA0013508 2 19980323 A 7250 23008054 NOZZLE 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 513EH CAT70735 45421 CAE860213 ENGINE REMOVED DUE TO OIL BLOWING OUT OF COMP. DISCHARGE. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INS PECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR1 NOZZLE VANES, OUTERBAND AND KEYWELDS. 1 G 7 1 3U 3 U H2SW E1GL 1998040200771 19980402 00771 1998 4 2 HEEA0013509 4 19980323 A 3451 066106602 TRANSCEIVER SKRSKY S76 S76A 8143006 NE DME FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 DME OPERATED 50% OF THE TIME AND IS VERY WEAK. PERFORMED PRELIMINARY INSPECTION, VERIFIED PROBLEM. UNIT WAS HEAVILY COR RODED. CLEANED CORROSION FROM ALL BOARDS AND CHASIS. BEGAN BENCH CHECK AND UNIT DREW EXCESSIVE CURRENT AND BURNT R236, R240 ON THE MODULATOR BOARD. SENT TO 1 G 7 2 3U H1NE 1998040200772 19980402 00772 1998 4 2 HEEA0013510 4 19980323 A 3452 066106202 TRANSPONDER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 TRANSPONDER INOPERATIVE. RECEIVE INTERMITTENT. PERFORMED PRELIMINARY INSPECTION, VERIFIED PROBLEM. FOUND NO 192 VOLT L INE. TROUBLESHOT AND REPLACED Q105, REPAIRED. BEGAN BENCH CHECK AND FOUND RECEIVER SENSE WEAK AND INTERMITTENTLY RECEI VES. 1 G 7 2 3U H1NE 1998040200773 19980402 00773 1998 4 2 HEEA0013511 4 19980323 A 2312 064105430 TRANSCEIVER BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2278V 3632 24 MONTH INSPECTION DUE. PERFORMED PRELIMINARY INSPECTION AND TESTED UNIT. FOUND DISPLAY NOT DIMMING. SWAPPED OUT DS90 1 DISPLAY AND V901 PHOTOCELL. NO HELP. FOUND I509 INTEGRATED CIRCUIT (SURFACE MOUNT) BAD. 1 G 7 1 3U H2SW 1998040200774 19980402 00774 1998 4 2 HEEA0013512 4 19980323 A 3457 0845000000 GPS SKYNAV5000 BEECH 200 200CBEECH 1152926 CE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 39PH BL3 SELECTOR KNOB SKIPS DIGITS AND LETTERS WHEN TRYING TO SELECT. 1 L 7 2 4T A24CE 1998040200775 19980402 00775 EU 1998 4 2 HEEA0013514 1 19980325 A 7600 350A57149000 ROD SPRING SNIAS 350 AS350B2 8680813 EU ENG CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 RUST AND CORROSION INSIDE. 1 G 7 1 3U H9EU 1998040200776 19980402 00776 SW 1998 4 2 HEEA0013517 1 19980325 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 53 33022 STEP ACTUATOR DOESN'T RETRACT. 1 G 7 2 4U H4SW 1998040200777 19980402 00777 SW 1998 4 2 HEEA0013518 1 19980325 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 383 33006 ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998040200778 19980402 00778 SW 1998 4 2 HEEA0013519 1 19980325 A 5260 SYLC502283 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 STEP ACTUATOR WEAK, POPS CIRCUIT BREAKER AFTER TWO CYCLES. 1 G 7 2 4U H4SW 1998040200779 19980402 00779 SW 1998 4 2 HEEA0013520 1 19980325 A 5260 SYLC502281 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 ACTUATOR OCASSIONALLY GIVES LIGHTS IN UP AND DOWN POSITION WITH TEST BOX. 1 G 7 2 4U H4SW 1998040200780 19980402 00780 SW 1998 4 2 HEEA0013521 1 19980325 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 ACTUATOR WILL NOT EXTEND. OR SOMETIMES RETRACT. 1 G 7 2 4U H4SW 1998040200781 19980402 00781 SW 1998 4 2 HEEA0013522 1 19980325 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 ACTUATOR WILL NOT ACTUATE. 1 G 7 2 4U H4SW 1998040200782 19980402 00782 SW 1998 4 2 HEEA0013523 1 19980325 A 5260 SYLC502281 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 STEP ACTUATOR INOPERATIVE; DOES NOT RETRACT. 1 G 7 2 4U H4SW 1998040200783 19980402 00783 SW 1998 4 2 HEEA0013524 1 19980325 A 5260 212075418103 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998040200784 19980402 00784 SW 1998 4 2 HEEA0013525 1 19980326 A 6240 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 ROTOR NEEDLE STUCK AT 120 RPM. 1 G 7 2 4U H4SW 1998040200785 19980402 00785 SW 1998 4 2 HEEA0013526 1 19980326 A 2800 MS29561210 PACKING 209062502101 BELL 212 212 1181420 SW OIL COOLER LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 102PH 297 30899 OIL LEAKAGE CAUSED BY FAILURE OF O-RING. O-RING HAS BECOME BRITTLE AND BROKEN. THE LEAKAGE IS BEING REPORTED AT APPROX IMATELY 2 QTS. REPLACED O-RING AND RETURNED TO SERVICE. 1 G 7 1 4U H4SW 1998040200786 19980402 00786 NE 1998 4 2 HEEA0013528 1 19980326 A 2611 30231R7B SMOKE DETECTOR SKRSKY S76 S76A 8143006 NE FIRE SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 SMOKE DETECTOR WILL NOT TEST. 1 G 7 2 3U H1NE 1998040200787 19980402 00787 1998 4 2 HEEA0013529 4 19980326 A 3444 7001840913 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 TRANSCEIVER INTERMITTENT OUTPUT. 1 G 7 2 3U H1NE 1998040200788 19980402 00788 SW 1998 4 2 HEEA0013530 1 19980326 A 2840 384178091 SELECTOR BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 CAPACITANCE LOW OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998040200789 19980402 00789 SW 1998 4 2 HEEA0013531 1 19980326 A 2810 214066226103 CHECK VALVE BELL 412 412 1182202 SW MID CELL LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 CHECK VALVE FAULTY. FUEL IS LEAKING INTO MID CELL. 1 G 7 2 4U H4SW 1998040200790 19980402 00790 EU 1998 4 2 HEEA0013532 1 19980326 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXAUST TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T S539 EXH TEMP INDICATOR EXCESSIVE FRICTION AND CANNOT CALIBRATE. 1 G 7 2 3U H3EU 1998040200791 19980402 00791 EU 1998 4 2 HEEA0013533 1 19980326 A 6240 HMM02 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T S111 LIGHT FLICKERS WHEN POWER TURNED ON. 1 G 7 2 3U H3EU 1998040200792 19980402 00792 EU 1998 4 2 HEEA0013534 1 19980326 A 6240 10594576 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T S111 MAST MOMENT TRANSMITTER WILL NOT CHECK CORRECTLY. 1 G 7 2 3U H3EU 1998040200793 19980402 00793 1998 4 2 HEEA0013535 4 19980326 A 3424 A1605 INDICATIOR BOLKMS 105 BO105S 5626006 EU TURN & BANK FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3533T S111 TURN & BANK INDICATOR HAS NO INDICATION. 1 G 7 2 3U H3EU 1998040200794 19980402 00794 1998 4 2 HEEA0013536 4 19980326 A 3416 5934D1 ALTIMETER BELL 206 206L3 1182108 SW COCKPIT ERRORS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8588X 51486 ALTIMETER HAS EXCESSIVE FRICTION ERROR. 1 G 7 1 3U H2SW 1998040200795 19980402 00795 SW 1998 4 2 HEEA0013537 1 19980326 A 2436 206075447007 VOLT REGULATOR BELL 206 206L3 1182108 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251V 51404 VOLTAGE REGULATOR FAILED. GEN DROPS OFF LINE. 1 G 7 1 3U H2SW 1998040200796 19980402 00796 SW 1998 4 2 HEEA0013538 1 19980326 A 3340 7028501 STROBE BELL 412 412 1182202 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 STROBE INOPERATIVE, LIGHT WILL NOT FLASH. 1 G 7 2 4U H4SW 1998040200797 19980402 00797 SW 1998 4 2 HEEA0013539 1 19980326 A 3340 7028511 LIGHT BELL 412 412 1182202 SW STROBE SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 STROBE LIGHT SHORTED, CAUSES CIRCUIT BREAKER TO POP. 1 G 7 2 4U H4SW 1998040200798 19980402 00798 SW 1998 4 2 HEEA0013540 1 19980326 A 3340 7028501 LIGHT BELL 412 412 1182202 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 STROBE LIGHT INOPERATIVE. 1 G 7 2 4U H4SW 1998040200800 19980402 00800 SW 1998 4 2 HEEA0013542 1 19980326 A 2436 206075447007 VOLT REGULATOR BELL 206 206L3 1182108 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 210PH 51541 GENERATOR SLOW TO COME ON LINE. 1 G 7 1 3U H2SW 1998040200801 19980402 00801 SW 1998 4 2 HEEA0013543 1 19980326 A 6730 206076062003 CYLINDER BELL 206 206L1 1182107 SW CYCLIC LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1078D 14890 45397 SERVO LEAKING AND BOOT TORN. 1 G 7 1 3U H2SW 1998040200802 19980402 00802 SW 1998 4 2 HEEA0013544 1 19980326 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 ROTARY ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998040200803 19980402 00803 SW 1998 4 2 HEEA0013545 1 19980326 A 2430 214175171103 RELAY BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 GENERATOR FALLING OFF LINE. 2 G 7 2 4U H10SW 1998040200804 19980402 00804 SW 1998 4 2 HEEA0013547 1 19980326 A 2432 214175379103 BATTERY CHARGER BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 59806 28140 BATTERY LIGHT COMES ON IN FLIGHT. BATTERY CHARGER DEFECTIVE 2 G 7 2 4U H10SW 1998040200805 19980402 00805 EU 1998 4 2 HEEA0013548 1 19980326 A 6320 4638201004 LOWER HOUSING BOLKMS 105 BO105S 5626006 EU M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB S737 M/R GR BOX LINERS LOOSE. INTERNAL SHAFT SEAT WORN. CORROSION ON LOWER FLANGE. 1 G 7 2 3U H3EU 1998040200806 19980402 00806 EU 1998 4 2 HEEA0013549 1 19980326 A 6320 4619201902 CENTER CASE BOLKMS 105 BO105S 5626006 EU GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB S737 TR QUILL WORN. OIL NOZZLE SEAT WORN. ACCY FAN DRIVE QUILLS WORN AND PIN SEAT WORN. 1 G 7 2 3U H3EU 1998040200807 19980402 00807 EU 1998 4 2 HEEA0013550 1 19980326 A 7712 G555674 TRANSDUCER BOLKMS 117 BK117A4 5626017 EU TORQUE ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 PRESSURE TRANSDUCER ERRATIC INDICATION. 1 G 7 2 3U H13EU 1998040200808 19980402 00808 1998 4 2 HEEA0013551 4 19980326 A 2210 7611123 PITCH SLICE AMP SKRSKY S76 S76A 8143006 NE AUTO FLIGHT MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5426U 760167 NR 1 PITCH KICKS IN FLIGHT. 1 G 7 2 3U H1NE 1998040200809 19980402 00809 SW 1998 4 2 HEEA0013552 1 19980326 A 6710 214001423109 ACTUATOR BELL 214 214ST 1182106 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ACTUATOR DOES NOT WORK. 2 G 7 2 4U H10SW 1998040200810 19980402 00810 SW 1998 4 2 HEEA0013553 1 19980326 A 6710 214001423109 ACTUATOR BELL 214 214ST 1182106 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 ACTUATOR DOES NOT WORK. 2 G 7 2 4U H10SW 1998040200811 19980402 00811 SW 1998 4 2 HEEA0013554 1 19980326 A 2121 214073917101 BLOWER BELL 214 214ST 1182106 SW AIR DIST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 BLOWER POPS CIRCUIT BREAKER. 2 G 7 2 4U H10SW 1998040200812 19980402 00812 SW 1998 4 2 HEEA0013555 1 19980326 A 6240 206076373001 TACH GENERATOR BELL 206 206L3 1182108 SW N2 ROTOR MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31801 51074 N2 ROTOR NEEDLE BOUNCES. 1 G 7 1 3U H2SW 1998040200813 19980402 00813 SW 1998 4 2 HEEA0013556 1 19980326 A 6240 214074280105 DETECTOR BELL 214 214ST 1182106 SW M/R RPM MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 RPM DETECTOR HAS NO RPM LIGHT ILLUMINATION. 2 G 7 2 4U H10SW 1998040200814 19980402 00814 EU 1998 4 2 HEEA0013557 1 19980326 A 7931 1176131203 PRESS SWITCH BOLKMS 117 BK117B1 5626012 EU NR 2 ENG OIL FAILED E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 217UC 7152 NR 2 ENGINE OIL PRESSURE CAUTION LIGHT NOT GOING OUT. 1 G 7 2 3U H13EU 1998040200815 19980402 00815 NE 1998 4 2 HEEA0013558 2 19980326 A 7200 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE COMPRESSOR STALLS E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 108X 16721 33115 CPPS60139 COMPRESSOR STALLS. 1 G 7 2 4U 4 U H4SW E22EA 1998040200816 19980402 00816 EU 1998 4 2 HEEA0013559 1 19980326 A 6320 4638201005 UPPER HOUSING BOLKMS 105 BO105S 5626006 EU M/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB S737 UPPER BORE WORN LINER LOOSE. 1 G 7 2 3U H3EU 1998040200817 19980402 00817 NE 1998 4 2 HEEA0013560 1 19980326 A 6220 7610608000049 DAMPER SKRSKY S76 S76A 8143006 NE M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1547D 760077 M/R ROTOR DAMPER WEAK AND LEAKING. 1 G 7 2 3U H1NE 1998040200818 19980402 00818 SW 1998 4 2 HEEA0013561 1 19980326 A 7720 206075682001 GAGE BELL 206 206B3 1181506 SW GAS PROD DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22751 3627 GP GAGE NEEDLE STICKS AND PARTICLES INSIDE GLASS. 1 G 7 1 3U H2SW 1998040200819 19980402 00819 SW 1998 4 2 HEEA0013562 1 19980326 A 7712 206075739107 TORQUEMETER BELL 206 206B3 1181506 SW ENGINE MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22751 3627 SLUGGISH OPERATION AND FLUID IN GLASS. 1 G 7 1 3U H2SW 1998040200820 19980402 00820 SW 1998 4 2 HEEA0013563 1 19980326 A 2841 206075189101 INDICATOR BELL 206 206B3 1181506 SW FUEL QTY ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22751 3627 EXCESSIVE FRICTION ERROR. 1 G 7 1 3U H2SW 1998040200821 19980402 00821 SW 1998 4 2 HEEA0013564 1 19980326 A 5610 P21207601 WINDOW BELL 412 412 1182202 SW LT LOWER MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 WINDOW DOES NOT FIT CONTOUR OF AIRCRAFT AIRFRAME. DRAIN HOLES IN LOWER CORNER ARE LOCATED IN WRONG PLACE. 1 G 7 2 4U H4SW 1998040200822 19980402 00822 SW 1998 4 2 HEEA0013565 1 19980326 A 5610 P21207602 WINDOW BELL 412 412 1182202 SW RT CHIN BUBBLE MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 WINDOW DOES NOT FIT CONTOUR OF AIRCRAFT AIRFRAME. DRAIN HOLES IN LOWER CORNER ARE LOCATED IN WRONG PLACE. SENT TO NORDA M TEXAS FOR CREDIT AGAINST ORIGINAL PURCHASE. 1 G 7 2 4U H4SW 1998040200823 19980402 00823 SW 1998 4 2 HEEA0013566 1 19980326 A 3340 7028521 LIGHT WHELEN BELL 412 412 1182202 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 STROBE LIGHT INOPERATIVE. 1 G 7 2 4U H4SW 1998040200824 19980402 00824 SW 1998 4 2 HEEA0013567 1 19980326 A 7714 206070266001 INDICATOR BELL 206 206L1 1182107 SW GAS PRODUCER STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Q 45187 GAS PRODUCER NEEDLE STICKS AT START. 1 G 7 1 3U H2SW 1998040200825 19980402 00825 1998 4 2 HEEA0013568 4 19980326 A 3416 10162701696 ALTIMETER BOLKMS 105 BO105S 5626006 EU COCKPIT ENCODER MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T S539 EXCESSIVE FRICTION ERROR AND ENCODER READS LOW. 1 G 7 2 3U H3EU 1998040200826 19980402 00826 EU 1998 4 2 USAAF98022 1 19980226 A 2910 HYD SYSTEM FOKKER F28 F28MK0100 4990807 EU NR 2 SYSTEM FAILED A USAA K O NONE OTHER C J F.O.D. WARNING INDICATION AP APPROACH 1 EA 19 867US 11312 FLT 861 - BHM - EN ROUTE TO BHM AT APPROXIMATELY 11,000 FT, CAPTAIN BELIEVED AIRCRAFT SUSTAINED A LIGHTNING STRIKE. AIR CRAFT LOST SYSTEM 2 HYDRAULIC PRESSURE SHORTLY AFTERWARDS. DURING APPROACH TO BHM AFTER FLAPS AND LANDING GEAR WERE EXT ENDED THE SYSTEM 1 HYDRAULIC SYSTEM FAILED. CAPT DECLARED EMERGENCY AND LANDED. TOUCHDOWN WAS NORMAL. ON ROLLOUT, THE LEFT MAIN GEAR TIRES BLEW OUT. AIRCRAFT PULLED LEFT AND ROLLED OFF THE RUNWAY. NOSE GEAR COLLAPSED AND AIRCRAFT CAME TO REST PARTIALLY ON THE ACTIVE RUNWAY. PASSENGERS AND CREW EVACUATED THROUGH THE MAIN ENTRY DOOR. AIRCRAFT WAS REPAIR ED PER FOKKER DAMAGE AND REPAIR REPORT G100A-00-8141 FSW-S-406. (X) 2 L 7 2 4F RT 1998040200827 19980402 00827 NM 1998 4 2 USAASB98049 1 19980226 A 3397 WIRE BOEING 737 7372B7 1384560 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 529AU 24411 PIT - MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 6 THROUGH 9 INOP. MAINTENANCE REPAIRED A BROKEN WIR E NEAR SEAT ROW 9. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998040200828 19980402 00828 NM 1998 4 2 USAASB98051 1 19980303 A 5230 10608214 SEAL BOEING 737 737401 1384701 NM CARGO DOOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 418US 23985 CLT - FLT 2310 - CLIMBING THROUGH 8,000 FEET, THE FIRST OFFICER NOTICED THE CAIBN WAS CLIMBING. CREW WENT THROUGH PROCE DURES WITH NO HELP. AT 11,000 FEET, THE CREW DECIDED TO RETURN TO FIELD AT CLT BECAUSE OF THE INABILITY TO PRESSURIZE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. AFTER LANDING, THE CAPTAIN PERFORMED A WALK-AROUND INSPECTION OF THE AIRCRAFT AND FOUND THE AFT CARGO DOOR SEAL HANGING OUTSIDE THE AIRCRAFT. MAINTENANCE FOUND THE THE A FT CARGO DOOR SEAL SEPARATED FROM THE TRACK. REINSTALLED DOOR SEAL IN TRACK. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A16WE 1998040200829 19980402 00829 WP 1998 4 2 USAAD98038 1 19980304 A 7930 42D1091 SWITCH DOUG DC9 DC981 3022081 WP RT ENGINE FAILED A USAA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 EA 19 800US 48034 MCO - FLT 1866 - DURING CRUISE, THE RIGHT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE CREW SHUT DOWN THE RIGHT ENGINE AND DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED THE OIL SCREEN AND CHIP DETECTORS. NO CARBON OR APPRECIABLE CONTAMINENTS WERE NOTED. THE ENGINE WAS RUN AND THE OIL SCREEN REPLACED A SECOND TIME. AGAIN, NO CONTAMINE NTS FOUND. THE OIL FILTER CLOG LIGHT WAS OUT AT THIS TIME. THE OIL FILTER CLOG ANNUNCIATOR SYSTEM WAS MEL'D. DURING T HE MAINTENANCE RON THE OIL SCREEEN WAS REPLACED AGAIN AND FOUND TO BE CLEAN. THE OIL FILTER DIFFERENTIAL SWITCH WAS REP LACED. (M) 2 L 7 2 4F A6WE 1998040200830 19980402 00830 NM 1998 4 2 USAASB98052 1 19980304 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 442US 24841 ALB - MAINTENANCE FOUND THE MAIN ENTRY DOOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE FORWARD BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998040200831 19980402 00831 NM 1998 4 2 USAASB98050 1 19980226 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 LGA - MAINTENANCE FOUND THE MAIN ENTRY DOOR LOW LEVEL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTE RY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998040200832 19980402 00832 NM 1998 4 2 98ZZZM335 1 19980226 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 LGA - MAINTENANCE FOUND THE MAIN ENTRY DOOR LOW LEVEL EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTE RY PACK AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998040200833 19980402 00833 NM 1998 4 2 MASA98042 1 19980227 A 3397 5918891 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN DAMAGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 4604 - DEN-GJT - DURING PREFLIGHT, PILOT REPORTED THE EMERGENCY LIGHTS WERE NOT WORKING PROPERLY. MAINTENANCE REPAI RED A WIRE TO THE FLGIHT ATTENDANTS EMERGENCY LIGHT SWITCH AND REPLACED THE DIODES. AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A13NM 1998040200834 19980402 00834 NM 1998 4 2 98ZZZM336 1 19980227 A 3350 5918891 DIODES DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 4604 - DEN-GJT - DURING PREFLIGHT, PILOT REPORTED THE EMERGENCY LIGHTS WERE NOT WORKING PROPERLY. MAINTENANCE REPAI RED A WIRE TO THE FLGIHT ATTENDANTS EMERGENCY LIGHT SWITCH AND REPLACED THE DIODES. AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A13NM 1998040200835 19980402 00835 NM 1998 4 2 MASA98041 1 19980227 A 3350 40005130003 SWITCH DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 7621 - DEN-HDN - DURING PREFLIGHT, PILOT REPORTED THE EMERGENCY LIGHTS FLASHED IN FLIGHT. MAINTENANCE REMOVED AND R EPLACED THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998040200836 19980402 00836 NM 1998 4 2 MASA98040 1 19980227 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 7525 - DRO-DEN - AFTER DEBOARDING PASSENGERS IN DEN. PILOT TESTED EMERGENCY LIGHT SYSTEM, WHICH FAILED TO ILLUMINAT ED. MAINTENANCE REPAIRED A WIRE TO PIN AT DIODE AND REMOVED AND REPLACED BATTERIES. (M) 2 H 7 2 4T RT A13NM 1998040200837 19980402 00837 NM 1998 4 2 MASA98045 1 19980301 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 FLT 7622 - HDN-DEN - PILOT REPORTED, AFT EMERGENCY EXIT SIGN WOULD NOT ILLUMINATE. AIRCRAFT WAS FERRIED TO GJT. MAINTE NANCE REMOVED AND REPLACED THE POWER PACK. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998040200838 19980402 00838 NM 1998 4 2 MASA98047 1 19980305 A 3350 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 FLT 7662 - DEN-MTJ - CREW REPORTED ONE BULB BURNED OUT AT ROW 3 EMERGENCY TRACK LIGHTING. MAINTENANCE ACTION WAS DEFERR ED PER MEL 33-11. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998040200839 19980402 00839 NM 1998 4 2 MASA98049 1 19980305 A 3350 OL6839BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING A ROUTINE LINE CHECK INSPECTION, MAINTENANCE PERSONNEL FOUND THE OVERHEAD CENTER EMERGENCY EXIT LIGHT WITH SEVERA L BULBS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED BULBS, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998040200840 19980402 00840 EU 1998 4 2 SABA980015 1 19980223 A 7712 8974575 TTL VALVE BAG JETSTM JETSTM3201 1500217 EU RT ENG FAILED A SABA C ABORTED TAKEOFF S AFFECT SYSTEMS TO TAKEOFF 1 SO 33 962AE 86082651215 962 CLT - FLT 5173 - ON FLIGHT FROM CLT TO OAJ, PILOT ABORTED TAKEOFF DUE TO RIGHT ENGINE TORQUE STARTED DECREASING AND TEMP ERATURE WAS INCREASING. NO EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO PARKING RAMP. MAINTENANCE FOUND THE TTL BYPAS S VALVE BAD. REMOVED AND REPLACED VALVE. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998040200841 19980402 00841 NM 1998 4 2 SABA980014 1 19980223 A 6123 995236B35220 SWITCH ASSY DHAV DHC8 DHC8102 2809003 NM COCKPIT INTERNAL A SABA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 33 880CC 277 CLT - FLT 5107 - ON FLIGHT FROM CLT TO AGS, AIRCRAFT ABORTED TAKEOFF DUE TO AUTOFEATHER SYSTEM WOULD NOT ARM. NO EMERGE NCY WAS DELCARED. AIRCRAFT RETURNED TO PARKING RAMP. MAINTENANCE FOUND THE AUTOFEATHER SELECT SWITCH BAD. REMOVED AND REPLACED SWITCH, SYSTEM GROUND RUN AND OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998040200842 19980402 00842 EU 1998 4 2 SIMA980641 1 19980305 A 3260 141FLO1D3 SWITCH AEROSP ATR72 ATR72212 EU NLG FAILED A SIMA K NONE N FALSE WARNING LD LANDING 1 SW 21 369AT 369 HOU - FLT 3547 - INBOUND TO HOU FOR LANDING, WHEN GEAR WAS SELECTED DOWN FOR LANDING THE NOSE GEAR GREEN LIGHT FLASHED I NTERMITTENT ON THE LOWER INDICATOR PANEL. THE UPPER INDICATION PANEL INDICATED ALL GEAR DOWN AND LOCKED. PILOT CONTINU ED TO HOU AND LANDED SAFELY. MEL ITEM WAS ISSUED AGAINST THE LANDING GEAR FOR RETURN FLIGHT FOR DFW. DFW MAINTENANCE R EPLACED THE NOSE LANDING GEAR UPLOCK BOX SWITCH AND PERFORMED GEAR RETRACTION TEST SATISFACTORILY. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200843 19980402 00843 CE 1998 4 2 98ZZZM337 1 19980226 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG FAILED A JJBA K NONE N FALSE WARNING IN INSP/MAINT 1 EA 01 848CA 0499A UE53 RIGHT MAIN GEAR FAILED TO INDICATE DOWN AND LOCK. REPLACED ACTUATOR. 2 L 7 2 4T RT A24CE 1998040200844 19980402 00844 1998 4 2 F3LA98007 4 19980308 A 2565 D31591478 SLIDE BOEING 737 737317 138447P NM PAX DOOR DEPLOYED A F3LA O OTHER O OTHER NR NOT REPORTED 1 NM 03 EICHH 23177 DEN - UPON ARRIVAL FLIGHT CREW REPORTED R-1 SLIDE DEPLOYED WHEN FORWARD SERVICE DOOR WAS OPENED. MAINTENANCE REPLACED S LIDE ASSEMBLY. (M) 2 L 7 2 4F RT A16WE 1998040200845 19980402 00845 NM 1998 4 2 F3LA98006 1 19980308 A 2910 65445101470 LINE BOEING 737 737201 1384454 NM 'A' HYD SYSTEM FAILED A F3LA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 03 205AU 19421 SFO - ON INBOUND FLIGHT TO SFO, FLIGHT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID. USED ALTERNATE FL AP SYSTEM AND AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE 'A' SYSTEM HYDRAULIC PRESSURE LINE IN AFT FLAP WEL L, BOTH 'A' SYSTEM HYDRAULIC PUMPS (NR 1 P/N 65075-01, S/N 184104AK, NR 2 P/N 65075-06, S/N 183975), NR 1 AND NR 2 ENGIN E PUMP CASE DRAIN FILTERS. 'A' SYSTEM HYDRAULIC RETURN FILTER. PERFORMED LEAK AND OPERATIONAL CHECK AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998040200846 19980402 00846 WP 1998 4 2 98ZZZM338 1 19980306 A 2612 2440832 ELEMENT DOUG DC8 DC851 3021920 WP NR 2 ENGINE CHAFING A FXLA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 19 508DC 45935 DURING CRUISE NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. SHUT DOWN ENGINE AND FIRE WARNING CEASED. GROUND INSPEC TION REVEALED NO EVIDENCE OF FIRE OR OVERHEAT. FOUND FIRE SENSE ELEMENT ON AFT COWLING CONTACTING CASE. REPOSITIONED E LEMENT AND SECURED. ENGINE TESTED OK. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1998040200847 19980402 00847 WP 1998 4 2 USAAD98039 1 19980307 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 936VJ 48116 IND - THE CEILING EMERGENCY LIGHTS FOR ROWS 14-18 WERE WEAK. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998040200848 19980402 00848 WP 1998 4 2 USAAD98040 1 19980308 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959VJ 47352 IND - THE CEILING EMERGENCY LIGHTS FOR ROWS 14-18 WERE WEAK. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998040200849 19980402 00849 WP 1998 4 2 USAAD98041 1 19980309 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924VJ 48144 CMH - THE TAIL COMPARTMENT EVACUATION LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EVACUATION LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998040200850 19980402 00850 NM 1998 4 2 USAASB98058 1 19980303 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 428US 24550 ALB - MAINTENANCE FOUND THE BULLNOSE EVACUATION LIGHTS AT ROW 12 RIGHT SIDE INOP, THE SIDEWALL EXIT SIGN AT SEAT 12F INO P, THE EVACUATION LIGHTS FROM ROW 12 TO 20 INOP AND THE SEAT MOUNTED EXIT SIGN AT SEAT 12 INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE CEILING AT ROW 20 LEFT SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998040200851 19980402 00851 NM 1998 4 2 USAASB98057 1 19980302 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 262AU 22868 ROC - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR. MAINTENANCE REMOV ED AND REPLACED THE BATTERY PACK AND POWER SUPPLY IN THE FORWARD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998040200852 19980402 00852 NM 1998 4 2 98ZZZM339 1 19980302 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 262AU 22868 ROC - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND FORWARD SERVICE DOOR. MAINTENANCE REMOV ED AND REPLACED THE BATTERY PACK AND POWER SUPPLY IN THE FORWARD CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998040200853 19980402 00853 NM 1998 4 2 USAASB98055 1 19980309 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 282AU 23115 CLT - MAINTENANCE FOUND THE EMERGENCY LIGHT OVER THE FORWARD SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EM ERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998040200854 19980402 00854 NM 1998 4 2 USAASB98056 1 19980224 A 3350 3114981 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 590US 23935 ORD - WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE FORWARD RIGHT EMERGENCY EVACUA TION SLIDE LIGHT INOP. LIGHT ASSEMBLY WAS BADLY CORRODED. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPS CH ECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998040200855 19980402 00855 NM 1998 4 2 USAASB98054 1 19980308 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 19 373US 22952 ALB - MAINTENANCE FOUND THE LIGHTS FOR THE EMERGENCY EXIT SIGNS AT THE COCKPIT ENTRANCE AND OVER THE FORWARD ENTRY DOOR INOP AND THE BULLNOSE EVACUATION LIGHT AT ROWS 3 RIGHT SIDE INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE FORWARD ENTRYWAY CEILING LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998040200856 19980402 00856 EU 1998 4 2 USAAF98025 1 19980304 A 3010 SWITCH FOKKER F28 F28MK0100 4990807 EU WING ANTI-ICE FAILED A USAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 EA 19 887US 11349 CLT - FLT 1210 - ON CLIMB-OUT OF CLT AIRCRAFT HAD A WING ANTI-ICE FAULT TWICE BETWEEN 9000 FEET - 11,000 FEET. FLIGHT R ETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED WING ANTI-ICE SWITCH IN OVERHEAD PANEL. PERFORMED OPERATIONAL TEST PR MM 30-11-00, NO FAULTS. OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT 1998040200857 19980402 00857 EU 1998 4 2 USAAF98021 1 19980224 A 5280 D13312410 DOOR FOKKER F28 F28MK0100 4990807 EU RT MLG DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 883US 11337 FLT 275 - PHL-BTV - AFTER T/O, GEAR WOULD NOT RETRACT. ALT PROCEDURES PERFORMED. GEAR SUCCESSFULLY RAISED WITH MANUAL OVERRIDE. FLT PROCEEDED TO BTV. ON DESCENT TO BTV WHEN LANDING GEAR WAS LOWERED, 'R MLG UNSAFE' MESSAGE ILLUMINATED. G REEN RMLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. RECYCLED GEAR TWICE W/O SUCCESS. TOWER FLYBY CONFIRMED THAT RT MAI N GEAR WAS DOWN BUT NOT LOCKED. FLT DIVERTED TO BDL FOR LONGER RUNWAYS. EN ROUTE TO BDL, GEAR RECYCLED SEVERAL TIMES. ON SIXTH ATTEMPT, ALL THREE GREEN LIGHTS ILLUMINATED AND NO MESSAGES APPEARED ON DISPLAY. FLT CONTINUED TO BDL WITH GE AR DOWN. FLT LANDED BDL W/O FURTHER INCIDENT. MX FOUND THE RT MAIN GEAR OTBD DOOR CONNECTING ROD SEPARATED FROM DOOR. 2 L 7 2 4F RT 1998040200858 19980402 00858 EU 1998 4 2 98ZZZM340 1 19980224 A 3231 A11430410 ROD FOKKER F28 F28MK0100 4990807 EU RT MLG DOOR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 883US 11337 FLT 275 - PHL-BTV - AFTER T/O, GEAR WOULD NOT RETRACT. ALT PROCEDURES PERFORMED. GEAR SUCCESSFULLY RAISED WITH MANUAL OVERRIDE. FLT PROCEEDED TO BTV. ON DESCENT TO BTV WHEN LANDING GEAR WAS LOWERED, 'R MLG UNSAFE' MESSAGE ILLUMINATED. G REEN RMLG DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. RECYCLED GEAR TWICE W/O SUCCESS. TOWER FLYBY CONFIRMED THAT RT MAI N GEAR WAS DOWN BUT NOT LOCKED. FLT DIVERTED TO BDL FOR LONGER RUNWAYS. EN ROUTE TO BDL, GEAR RECYCLED SEVERAL TIMES. ON SIXTH ATTEMPT, ALL THREE GREEN LIGHTS ILLUMINATED AND NO MESSAGES APPEARED ON DISPLAY. FLT CONTINUED TO BDL WITH GE AR DOWN. FLT LANDED BDL W/O FURTHER INCIDENT. MX FOUND THE RT MAIN GEAR OTBD DOOR CONNECTING ROD SEPARATED FROM DOOR. 2 L 7 2 4F RT 1998040200859 19980402 00859 NM 1998 4 2 AALA980246 1 19980203 A 2421 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA K NONE H ELECT. POWER LOSS-50 PC DE DESCENT 1 SW 07 377AN 25446 MIA - FLT 920 - RT GEN DRIVE LT REMAINED ON STEADY DURING DESCENT. RT GEN DRIVE DISCONNECTED AS PER FT MANUAL, APU STAR TED. REMOVED AND REPLACE RT ENGINE IDG GEN ASSY, OPS CHECK NORMAL. LEAK CHECKS NORMAL. OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 1998040200860 19980402 00860 NM 1998 4 2 AALA980276 1 19980202 A 2421 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA K NONE H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 07 383AN 26995 LAX - FLT 999 - CHECKED AND PLACARDED LT GEN SYSTEM INOP AS PER MEL MAN ACCOMPD REQUIRED MPM AS PER MEL MAN CHECKED AND SERVICED LT. RT ENG 'IDG' AND APU IDG ENTERED IN MIC. REPLACED 1 ENG IDG ENG GROUND RUN UP OK. LEAK CHECK OK REMOVED PLACARD 2-37DC-B CLEARED MIC. (M) 2 L 7 2 4F RT A1NM 1998040200861 19980402 00861 NE 1998 4 2 AALA980216 2 19980125 A 7200 ENGINE AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 70072 515 JFK - FLT 141 - N2 ENGINE VIBRATION ECAM, NR 2 ENGINE INDICATION FLASHING. VARIED FROM 4.6 AT CRUISE POWER INCREASING T O 6.0 -6.4 WHEN THROTTLE REDUCED TO IDLE. POSSIBLE SLIGHT BUZZ LEFT IN NR 2 THROTTLE. N1 VIB AND ALL OTHER INDICATIONS NORMAL. NOTICEABLE HARMONIC VIBRATION WHEN ENGINE WINDING DOWN AT GATE. REMOVED AND REPLACED NR 2 ENGINE AS PER MCM W ORKCARD NR AE719307 AND ACCOMPLISHED ENGINE RUN UP. ENGINE OPS AND LEAK CHECKS NORMAL. (M) 2 L 7 2 4F 4 F RT A35EU E13NE 1998040200862 19980402 00862 NM 1998 4 2 AALA980159 1 19980119 A 2822 BOOST PUMP BOEING 767 767323 1385205 NM LT AFT WING FAILED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 351AA 24032 EZE - FLT 998 - DURING CLIMB-OUT, APPROACHING LEVEL OFF AT FL410, LT AFT FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED WITH EICAS MSG. APPROX 30 SECONDS LATER LT FWD FUEL BOOST PUMP LOW PRESS LIGHT ILLUMINATED WITH EICAS MSG L FUEL SYS PR ESS. OPENED FUEL CROSSFEED VALVE. LEFT FWD AND AFT FUEL BOOST PUMP LOW PRESS LIGHTS EXTINGUISHED AFTER ABOUT 1 MIN FUE L X-FEED VALVE LEFT IN OPEN POSITION. REMOVED FUEL FROM TANKS. OPENED ACCESS PANELS AND INSPECTED FUEL TANK LINES FOR OBSTRUCTIONS NO DISCREPANCIES. REPLACED LEFT AFT AND FWD FUEL BOOST PUMPS PER MM. REPLACED LEFT AFT AND FWD FUEL BOOST PUMPS PRESSURE SW PER MM. REFILLED TANKS AND CHECKED FOR LEAKS, NO LEAKS DETECTED. (M) 2 L 7 2 4F RT A1NM 1998040200863 19980402 00863 EA 1998 4 2 MASA98014 1 19980122 A 3350 GE1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 2103 - SAT-FTW - CREW REPORTED THE REAR EMERGENCY OVERHEAD LIGHT WAS INOP. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1 AND AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1998040200864 19980402 00864 EU 1998 4 2 SIMA980423 1 19980211 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 4313 211 ORD - FLT 4012 - FLOOR PROX LIGHTS INOP. RAI'D EMERGENCY LIGHT BATTERY PACKS, LOCATIONS 32L, 10WL, 18WL AND 29WL. PERF ORMED OPERATIONAL CHECK SATISFACTORILY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200865 19980402 00865 EU 1998 4 2 98ZZZM341 1 19980211 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 11730 211 ORD - FLT 4012 - FLOOR PROX LIGHTS INOP. RAI'D EMERGENCY LIGHT BATTERY PACKS, LOCATIONS 32L, 10WL, 18WL AND 29WL. PERF ORMED OPERATIONAL CHECK SATISFACTORILY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200866 19980402 00866 EU 1998 4 2 98ZZZM342 1 19980211 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 11735 211 ORD - FLT 4012 - FLOOR PROX LIGHTS INOP. RAI'D EMERGENCY LIGHT BATTERY PACKS, LOCATIONS 32L, 10WL, 18WL AND 29WL. PERF ORMED OPERATIONAL CHECK SATISFACTORILY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200867 19980402 00867 EU 1998 4 2 98ZZZM343 1 19980211 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 4457 211 ORD - FLT 4012 - FLOOR PROX LIGHTS INOP. RAI'D EMERGENCY LIGHT BATTERY PACKS, LOCATIONS 32L, 10WL, 18WL AND 29WL. PERF ORMED OPERATIONAL CHECK SATISFACTORILY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200868 19980402 00868 EU 1998 4 2 SIMA980431 1 19980212 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 12715 017 SAW - DURING PS-2 CHECK, MAINTENANCE REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS AT LOCATION 10WL AND 20WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200869 19980402 00869 EU 1998 4 2 98ZZZM344 1 19980212 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 12700 017 SAW - DURING PS-2 CHECK, MAINTENANCE REPORTED THAT SEVERAL EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACKS AT LOCATION 10WL AND 20WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200870 19980402 00870 EA 1998 4 2 VTZA98059 1 19980213 A 2750 865D1007 BPSU CNDAIR CL600 CL6002B19 EA FLAPS STUCK A VTZA O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 EA 27 622BR 7187 BNA/IAD - FLT 6701 - DURING APPROACH AT 1200 HRS ON 2-13-98, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHIC H WAS FLAPS STUCK AT ZERO DEGREES. EICAS MESSAGE READ FLAPS FAILED. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BP SU. OPS CHECK OK. AIRCRAFT RELEASED AND APROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998040200871 19980402 00871 EU 1998 4 2 98ZZZM345 1 19980220 A 3230 1867F RADIUS ROD BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 492UE 790 FLT 6221 - SWF-IAD - DURING APPROACH, EXPERIENCED A MOMENTARY LT GEAR UNSAFE WARNING LIGHT. AFTER A BRIEF MOMENT LEFT M AIN GEAR WENT GREEN BUT THE GPWS 'TO LOW GEAR' WARNING SOUNDED. A/C MADE A NORMAL LANDING BUT FOUND THE NOSE WHEEL STEE RING WAS INOPERATIVE. A/C STOPPED ON THE HIGH SPEED TAXI RAMP AND MX CONTROL WAS NOTIFIED. MX WAS NOTIFIED AND A\C WAS TOWED TO THE LINE. MX TROUBLESHOT SYSTEM AND FOUND THE LT UPLOCK MICROSWITCH WAS DEFECTIVE ALONG WITH A BROKEN WIRE ON THE NLG WEIGHT ON WHEEL MICROSWITCH. MX ALSO FOUND THE RT RADIUS ROD WAS DEFECTIVE. MX REMOVED AND REPLACED THE RT RA DIUS ROD AND THE LT UPLOCK MICROSWITCH AND REPAIRED THE WIRE TO THE NLG WEIGHT ON WHEEL MICROSWITCH. ALL FUNCTIONAL CHE 2 L 7 2 4T RT A56EU 1998040200872 19980402 00872 CE 1998 4 2 MASA98038 1 19980224 A 3246 11480012913889 WHEEL BEARINGS BEECH 1900 1900D 1154162 CE NLG FAILED A MASA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 124YV UE124 FLT 5530 - BGR-BOS - UPON ARRIVAL IN BOS, PILOTS FELT EXCESSIVE NOSE WHEEL SHIMMY DURING TAXI. AIRCRAFT STOPPED AND SEC URED ON TAXIWAY, FIRE EQUIPMENT VEHICLES ROLLED AS A PRECAUTION. IN MAINTENANCE, NOSE WHEEL ASSEMBLY AND BEARINGS WERE REMOVED AND REPLACED. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998040200873 19980402 00873 WP 1998 4 2 98ZZZM346 1 19980216 A 7120 37707451 ARM DOUG DC8 DC851 3021920 WP NR 4 ENGINE BROKEN A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 507DC 51047 45855 DURING 'A' CHECK, FOUND LEFT ARM OF NR 4 ENGINE MOUNT ASSEMBLY BROKEN IN THE THREADED AREA AND NUT MISSING, REF DACO IPC 71-20-0 FIG 16 ITEM 65 AND 30). REPLACED AFT ENGINE MOUNT ASSEMBLY AND RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1998040200874 19980402 00874 NM 1998 4 2 BJNA980202 1 19980223 A 3350 P4010020 BATTERY PACK BOEING 737 737214 138446R NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 L2 DOOR EMERGENCY SLIDE BATTERY WEAK. REMOVE AND REPLACE BATTERY PACK PER BMM 33-51-71, GROUND CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1998040200875 19980402 00875 EA 1998 4 2 98ZZZM347 1 19980218 A 7931 3024611C OIL REGULATOR DHAV DHC7 DHC7102 2802708 EA NR 3 ENGINE STICKING A CICA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 17 25AG 25 FLT 705 - FLL-PID - PILOT ABORTED AND RETURNED TO THE GATE. PILOT REPORTED NR 3 OIL PRESSURE GAUGE ERRATIC READING 80-1 50 PSI. AIRCRAFT DEPLANED 35 PASSENGERS AND TAXIED TO MX HANGAR. UPON ARRIVAL AT HANGAR THE NR 3 OIL PRESSURE TRANSMIT TER WAS CHANGED. DID NOT FIX PROBLEM. SUBSEQUENTLY, THE NR 3 ENGINE OIL PRESSURE REGULATOR WAS CHANGED IAW PW MM 79-25 -04. THE ENGINE WAS GROUND RUN AND NO FURTHER OIL PRESSURE PROBLEMS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1998040200876 19980402 00876 EA 1998 4 2 98ZZZM348 1 19980214 A 3260 MS3126E833P CONNECTOR ELDEC 805310 DHAV DHC7 DHC7102 2802708 EA LT MLG WW LOOSE A CICA A UNSCHED LANDING J WARNING INDICATION LD LANDING 1 SO 17 25AG 470 25 FLT 707 - FLL-PID - PILOT REPORTED LEFT MAIN GEAR LIGHT INDICATED TRANSIT (RED) WHEN GEAR WAS DOWN AND LOCKED. AIRCRAFT DID NOT LAND AT PID, BUT RETURNED TO FLL AND LANDED WITHOUT MISHAP. THE PASSENGERS WERE DEPLANED AND AIRCRAFT TAXIED T O MX HANGAR. INSPECTION FOUND DOWN LOCK PICK UP SENSOR CANNON PLUG LOOSE. RESECURRED CANNON PLUG, PERFORMED GEAR SWING TWO TIMES. AIRCRAFT OPERATED IAW MM. CANNON PLUG RECHECKED FOR SECURITY, CRACKS, LOOSENESS. CHECKED OK, RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1998040200877 19980402 00877 EA 1998 4 2 98ZZZM349 1 19980210 A 3260 805310 PROX SWITCH DHAV DHC7 DHC7102 2802708 EA RT MLG FAILED A CICA B EMER. DESCENT N FALSE WARNING AP APPROACH 1 SO 17 25AG 3799 25 FLT 702 - PID-FLL - PILOT REPORTED GREEN DOWN AND LOCK LIGHT ILLUMINATED IN FLIGHT WITH GEAR UP AFTER CYCLING GEAR SAME CONDITION EXISTED. CO-PILOT VERIFIED GEAR WAS DOWN AND IN LOCKED POSITION (BY SIGHT). AIRCRAFT LANDED AT FLL WITH NO I NCIDENT AFTER PASSENGERS DEPLANED. AIRCRAFT WAS TAXIED TO MX FACILITY. TROUBLESHOOTING FOUND PROXIMITY SWITCH TO BE IN OPERATIVE. THE PROXIMITY SWITCH WAS REPLACED. A GEAR RETRACTION WAS PERFORMED AND FOUND TO BE OPERATING NORMAL. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1998040200878 19980402 00878 EA 1998 4 2 98ZZZM350 2 19980221 A 7200 ENGINE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 3 MALFUNCTIONED A CICA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 SO 17 25AG 23757 25 86401 FLT 717 - FLL-PID - PILOT REPORTED NR 3 ENGINE OIL PRESSURE ERRATIC. FLUCTUATES ALL OVER FROM ABOUT 90 PSI TO 150 PSI. NR 3 ENGINE TORQUE FLUCTUATED BETWEEN 3500-3800 LBS IN FLIGHT AT THE SAME TIME THAT OIL PRESSURE FLUCTUATED. WHEN OIL PRESURE IS STEADY TORQUE IS ALSO STEADY. PILOT RETURNED TO FLL AND LANDED AND DEPLANED 28 PASSENGERS AND TAXIED TO FLL MX HANGAR NR 3 ENGINE REMOVED AND REPLACED WITH SERVICEABLE ENGINE. THE AIRCRAFT WAS RUN AND RELEASED FOR SERVICE. THE REMOVED ENGINE WILL BE SENT TO ENGINE VENDOR FOR TEARDOWN AND REPAIR. (M) 2 H 7 4 4T 4 T A20EA E4EA 1998040200879 19980402 00879 NM 1998 4 2 ASAA9840036 1 19980219 A 5753 65C2632017 SKIN BOEING 737 7374Q8 NM LT TE MID FLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING C-CHECK, THE LEFT WING OUTBOARD MID FLAP LOWER SURFACE NR 1 TRACK AFT FAIRING NYLON PADS WORN INTO WING SUR FACE. REPAIRED PER EA 5750-01185 AND BOEING TELEX ASA-SEA-95-0634RR. (M) 2 L 7 2 4F RT A16WE 1998040200880 19980402 00880 NM 1998 4 2 ASAA9840035 1 19980219 A 5730 65C363301 SKIN BOEING 737 7374Q8 NM RT WING LIGHTNING STRIKE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING C-CHECK, PREVIOUS INTERIM REPAIRED LIGHTNING STRIKE DAMAGE WAS FOUND ON THE CONDUCTIVE STRIP OF THE RT WING FIXED T/E. REPAIRED PER EA 5740-01270 AND BOEING TELEX ASA-SEA-98-0045RR. (M) 2 L 7 2 4F RT A16WE 1998040200881 19980402 00881 NM 1998 4 2 ASAA9840034 1 19980219 A 5400 FAIRINGS BOEING 737 7374Q8 NM NR 1/2 WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING C-CHECK, WEAR WAS FOUND AT VARIOUS LOCATINS ON ALL FOUR BULLNOSE FAIRINGS ON NR 1 AND NR 2 ENGINES AS A RES ULT OF THE BLOCKER DOOR HINGE FITTINGS RUBBING AGAINST THE FAIRING SURFACES. REPAIRED PER EA 5430-01029 AND BOEING TELE X ASA-SEA-98-0049RR. (M) 2 L 7 2 4F RT A16WE 1998040200882 19980402 00882 NM 1998 4 2 ASAA9840033 1 19980219 A 5230 6546921225 SKIN BOEING 737 7374Q8 NM CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 763AS 25100 SEA - DURING C-CHECK, A SERIES OF DENTS AND SCRATCHES WERE FOUND IN THE SKIN OF THE FORWARD CARGO DOOR IN THE VICINITY O F THE DOOR HANDLE. REPAIRED PER EA 5230-01079. (M) 2 L 7 2 4F RT A16WE 1998040200883 19980402 00883 WP 1998 4 2 ASAA9880033 1 19980223 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 24R AND 26L WERE INTERMITTENT. REPLACED THE BATTE RIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200884 19980402 00884 WP 1998 4 2 ASAA9880032 1 19980222 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200885 19980402 00885 WP 1998 4 2 ASAA9880026 1 19980207 A 3350 SPLICE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 940AS 49825 PDX - PRIOR TO DEPARTURE OF FLT 498, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FWD CABIN WERE INOPERATIVE. R EPLACED SPLICE IN WIRING AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998040200886 19980402 00886 WP 1998 4 2 ASAA9880025 1 19980205 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 2119 53063 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPE RATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200887 19980402 00887 NM 1998 4 2 ASAA9840040 1 19980222 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 22-25. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200889 19980402 00889 NM 1998 4 2 ASAA9840038 1 19980220 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE AFT TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNE CTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200890 19980402 00890 NM 1998 4 2 ASAA9840032 1 19980218 A 3397 WIRE BOEING 737 737490 1384715 NM CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 767AS 27081 SEA - FLT 517 - PRIOR TO FLT, THE FORWARD TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECON NECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200891 19980402 00891 NM 1998 4 2 ASAA9840037 1 19980219 A 2560 6176810D18306101 BOTTLE AIRCRUISERS BOEING 737 7374Q8 NM SLIDE DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 773AS 11862 5208 25106 SEA - DURING CREW TRAINING, THE AFT EVACUATION SLIDE FAILED TO FULLY DEPLOY, BOTTLE PRESSURE OBSERVED TO BE VERY LOW. B OTTLE PRESSURE BEFORE DEPLOYMENT READ OPERATIONAL. REMOVED AND REPLACED EVAC SLIDE BOTTLE AND REGULATOR. BOTTLE AND RE GULATOR SENT TO AIR CRUISERS FOR EVALUATION AND REPAIR AS NECESSARY. BOTTLE WAS OVERHAULED AND HYDRO TESTED ON 3/4/98 B Y AIR CRUISERS. (M) 2 L 7 2 4F RT A16WE 1998040200892 19980402 00892 NM 1998 4 2 ASAA9810012 1 19980203 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, THE INTERIOR OVERWING EMERGENCY EXIT LIGHTS WERE FLASHING WHEN ACTIVATED. REPLACED BATT ERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200893 19980402 00893 NM 1998 4 2 ASAA9810014 1 19980213 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING RECON, THE AFT SEAT PALLET EMERGENCY EXIT LIGHTS AND AFT THREE BATTERY PACKS WERE FOUND TO BE INOPERATIVE. REPLACED AFT SEAT PALLET RECEIVER AND AFT THREE BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200894 19980402 00894 NM 1998 4 2 98ZZZM351 1 19980213 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING RECON, THE AFT SEAT PALLET EMERGENCY EXIT LIGHTS AND AFT THREE BATTERY PACKS WERE FOUND TO BE INOPERATIVE. REPLACED AFT SEAT PALLET RECEIVER AND AFT THREE BATTERY PACKS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200895 19980402 00895 NM 1998 4 2 ASAA9810015 1 19980213 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING RECON, THE LEFT OVERWING EXIT IDENTIFIER, AFT ENTRY EXIT IDENTIFIER, AND THE SMOKE BARRIER EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE LEFT OVERWING EXIT IDENTIFIER BATTERY PACK, THE AFT ENTRY EXIT IDENTIFIER BATTERY PACK, AND THE SMOKE BARRIER EXIT LIGHT ASSEMBLY AND ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200896 19980402 00896 NM 1998 4 2 98ZZZM352 1 19980213 A 3350 8731002142 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING RECON, THE LEFT OVERWING EXIT IDENTIFIER, AFT ENTRY EXIT IDENTIFIER, AND THE SMOKE BARRIER EXIT LIGHT WERE FOUND TO BE INOPERATIVE. REPLACED THE LEFT OVERWING EXIT IDENTIFIER BATTERY PACK, THE AFT ENTRY EXIT IDENTIFIER BATTERY PACK, AND THE SMOKE BARRIER EXIT LIGHT ASSEMBLY AND ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200897 19980402 00897 NM 1998 4 2 ASAA9810016 1 19980220 A 3350 86210151 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 741AS 21959 ANC - FLT 30 - PRIOR TO FLT, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET POSITION 9. REPLACE D BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998040200899 19980402 00899 NM 1998 4 2 ASAA9840019 1 19980202 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 ANC - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED 3 LI GHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200900 19980402 00900 NM 1998 4 2 ASAA9840026 1 19980205 A 3350 3114981 LIGHT BOEING 737 7374Q8 NM CABIN CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 SEA - DURING MAINTENANCE CHECK, THE R-1 DOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED R1 EME RGENCY LIGHT REFLECTOR ASSY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200901 19980402 00901 NM 1998 4 2 ASAA9840027 1 19980205 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 SEA - DURING MAINTENANCE CHECK, THE AFT TWO RED EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNE CTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200902 19980402 00902 NM 1998 4 2 ASAA9840030 1 19980215 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15 AND 16 WERE FOUND TO BE INOPERATIVE. R ECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200903 19980402 00903 NM 1998 4 2 ASAA9840031 1 19980216 A 3350 20131A BATTERY BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 780AS 25112 JNU - DURING MAINTENANCE CHECK, ONE SECTION OF THE EMERGENCY EXIT FLOOR TRACK LIGHTS AISLE LOCATION L2 AND R2 DOOR EXIT WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200904 19980402 00904 SO 1998 4 2 C2XA98IA024 1 19980213 A 3221 19750 TRUNNION EMB 120 EMB120RT SO NLG CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE UPPER TRUNNION ON THE NOSE LANDING GEAR WAS FOUND TO BE CRACKED. MAINTENANCE REMOV ED AND REPLACED THE UPPER TRUNNION IAW EMB-120 MM CHAPTER 32-21-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200905 19980402 00905 SO 1998 4 2 C2XA98IA025 1 19980213 A 5753 12018355001 SUPPORT EMB 120 EMB120RT SO LT TE FLAP CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE MIDDLE FORWARD SKIN SUPPORT ON THE LEFT NACELLE FLAP WAS FOUND TO BE CRACKED. MAIN TENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM CHAPTER 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200906 19980402 00906 SO 1998 4 2 C2XA98IA026 1 19980213 A 5753 12018355002 SUPPORT EMB 120 EMB120RT SO RT TE FLAP CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE FORWARD MIDDLE SKIN SUPPORT ON THE RIGHT NACELLE FLAP WAS FOUND TO BE CRACKED. MAI NTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM CHAPTER 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200907 19980402 00907 SO 1998 4 2 C2XA98IA027 1 19980213 A 5730 12015667002 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12705 120089 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING LOWER SKIN WAS FOUND TO BE CRACKED AT ACCESS PANEL 622DB. MAINTENANCE I NSTALLED A DOUBLER REPAIR IAW EMB-120 SRM CHAPTER 57-20-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200908 19980402 00908 EU 1998 4 2 C2XA98IA031 1 19980220 A 5341 S53572804200 FITTING AEROSP ATR42 ATR42320 8680930 EU WING/FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING NDT INSPECTION OF THE AFT CENTER BOLT HOLE ON THE LEFT WING TO FUSELAGE FITTING AT FRAME 27, A CRACK INDICA TION WAS FOUND IN THE OUTER STRAP. MAINTENANCE REAMED THE AFFECTED HOLE TO SECOND OVERSIZE AND, THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE UNDER DEFERRED MAINTENANCE ITEM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIRED AUTHORI ZATION EC5340-01031. (M) 2 H 7 2 4T RT A53EU 1998040200909 19980402 00909 SO 1998 4 2 C2XA98IA032 1 19980219 A 3397 W502005620 WIRE EMB 120 EMB120RT SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16724 120171 IAH - DURING DAILY INSPECTION, THE AFT EXTERIOR EMERGENCY LIGHT ON THE LEFT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENAN CE REPAIRED WIRE NR W502-0056-20 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200910 19980402 00910 EU 1998 4 2 C2XA98IAA33 1 19980225 A 3350 3351214CF20 WIRE AEROSP ATR42 ATR42500 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING MAINTENANCE VISIT NR 14, FOUND LEFT SIDE AFT CABIN EMERGENCY EXIT SIGN/LIGHT TO BE INOPERATIVE. MAINTENANC E REPAIRED WIRE NR 3351214CF20 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200911 19980402 00911 EU 1998 4 2 C2XA98IA030 1 19980220 A 3397 3351117CF20 WIRE AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED W IRE NR 3351117CF20 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200912 19980402 00912 CE 1998 4 2 C2XA98CL015 1 19980221 A 3060 4E31971 BRUSH BLOCK BEECH 1900 1900D 1154162 CE RT PROP CHAFED WIRE A C2XA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 09 81546 UE187 CLE - FLT 3057 - CREW REPORTED THE RIGHT PROP DE-ICE WOULD NOT TEST FOR FIRST FLIGHT CHECKS IN AUTO OR MANUAL MODES. AI RCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE PROP AND REMOVED AND REPLACED A CHAFFED WIRE ON THE BRUSH BLOCK IAW B1900D MM 30-60-00. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998040200913 19980402 00913 SO 1998 4 2 C2XA98CL017 1 19980224 A 7712 30005000052 SIGNAL COND UNIT EMB 120 EMB120RT SO RT ENGINE FAILED A C2XA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 09 15732 120195 CLE - FLT 3079 - CREW REPORTED THE AUTOFEATHER SYSTEM WOULD NOT TEST, THE TORQUE WOULD RISE BUT NO ARM LIGHT OR NP CHANG E WAS NOTED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE TORQUE SIGNAL CONDITION UNIT IAW EMB-120-MM 77-11-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200914 19980402 00914 1998 4 2 C2XA98CL016 4 19980223 A 6122 78249035 PROP CONTL UNIT EMB 120 EMB120RT SO LT ENGINE MALFUNCTIONED A C2XA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SW 09 17720 120142 CLE - FLT 3216 - CREW REPORTED THE LEFT BETA LIGHT WOULD NOT WORK WITH THE POWER LEVER BELOW FLIGHT IDLE, AIRCRAFT RETUR NED TO GATE. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE PROPELLER CONTROL UNIT IAW EMB-120 MM 61-21-00, OPERATION AL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200915 19980402 00915 EU 1998 4 2 C2XA98BT014 1 19980220 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14821 160 BTV - DURING 4A INSPECTION, FOUND MAIN CABIN EMERGENCY EXIT SIGN OVER FLIGHT ATTENDANTS SEAT INOPERATIVE. REPLACED POWE R SUPPLY AND OPERATIONALLY CHECKED ITEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200916 19980402 00916 SO 1998 4 2 C2XA98CL014 1 19980219 A 2750 3069001017 ANNUNCIATOR EMB 120 EMB120RT SO COCKPIT FAILED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 15730 0055 120187 CLE - FLT 3143 - CREW REPORTED DURING CLIMB RECEIVED A FLAP FAULT, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTNENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE FLAP ANNUNCIATOR ASSEMBLE IAW EMB-120 MM 27-50-05. O PERATIONAL CHECKS WERE SATISFACTORY IAW EMB-120MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200917 19980402 00917 CE 1998 4 2 C2XA98CL006 1 19980121 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE CHAFED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 09 81536 UE152 CLE - FLT 3160 - CREW REPORTED THE LEFT FIRE WARNING SYSTEM ACTIVATED IN FLIGHT, AIRCRAFT LANDED WITHOUT FURTHER INCIDEN T. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT ENGINE FIRE LOOP IAW B1900 MM 26-10-00, OPERAT IONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998040200918 19980402 00918 EU 1998 4 2 C2XA98CL005 1 19980202 A 7312 10718DAF HEATER AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE RT ENG FUEL/OIL LEAKING A A C2XA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION LD LANDING 1 SW 09 15827 14615 510 175 CLE - CREW REPORTED THE RIGHT ENGINE CAUGHT FIRE UPON LANDING. MAINTENANCE INSPECTED THE RIGHT ENGINE AND FOUND THE FUE L/OIL HEATER TO BE LEAKING WHICH CAUSED THE FIRE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXP RESS TASK CARD NR 2272001. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998040200919 19980402 00919 EU 1998 4 2 C2XA98BT003 1 19980112 A 7170 S7171001401300 DRAIN LINE AEROSP ATR42 ATR42320 8680930 EU NR 1 ENGINE BROKEN A C2XA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 09 14830 184 BTV - DURING 3A INSPECTION, FOUND NR 1 ENGINE FUEL FLOW DIVIDER DRAIN LINE BROKEN. REMOVED AND REPLACED WITH A SERVICEA BLE LINE AND LEAK CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200920 19980402 00920 EU 1998 4 2 C2XA98BT002 1 19980112 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14830 184 BTV - DURING 3A INSPECTION, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOPERATIVE MAINTENANCE REMOVED AND REPLACED THE FUSE A T POWER SUPPLY 18WL FOR AFT RIGHT EXTERIOR EMERGENCY LIGHT. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200921 19980402 00921 EU 1998 4 2 C2XA98B1001 1 19980112 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93840 271 BTV - DURING 1A INSPECTION, FOUND FORWARD LOWER EMERGENCY EXIT LIGHT SIGNS RIGHT AND LEFT INOPERATIVE. REMOVED AND REPL ACED EMERGENCY LIGHTING POWER SUPPLY UNIT 29WL. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200922 19980402 00922 SO 1998 4 2 C2XA98IA014 1 19980204 A 3350 D43682 SPLICE EMB 120 EMB120RT SO CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15721 120160 IAH - DURING POST FLIGHT INSPECTION, THE PILOT REPORTED THREE BULBS INOPERATIVE IN THE AISLE PATH LIGHTING. MAINTENANCE REMOVED AND REPLACED WIRE SPLICE SPAH28 IAW EMB120 WIRING MANUAL 20-21-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200923 19980402 00923 SO 1998 4 2 C2XA98CL010 1 19980205 A 2910 2025000002 SWIVEL EMB 120 EMB120RT SO RT MLG LEAKING A C2XA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 27707 1397 120095 CLE - FLT 3068 - CREW REPORTED WHILE EN ROUTE TO CLE THE GREEN HYDRAULIC SYSTEM FAILED. AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A HYDRAULIC LINE SWIVEL LEAKING IN THE RIGHT MAIN LANDIN G GEAR WHEEL WELL. THE SWIVEL WAS REMOVED AND REPLACED IAW ERAM CMM 32-14-01. OPERATIONAL AND LEAK CHECKS WERE SATISFA CTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200924 19980402 00924 1998 4 2 C2XA98CL009 3 19980204 A 6140 SEL0C29DH NP GAUGE EMB 120 EMB120RT SO COCKPIT INOPERATIVE A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 09 16702 477 120078 CLE - FLT 3172 - CREW REPORTED THAT WHILE TAXIING FOR TAKEOFF THE RIGHT ENGINE NP GAUGE WAS INOPERTIVE. AIRCRAFT RETURN ED TO GATE. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT ENGINE NP GAUGE IAW EMB-120 MM 61-40 -00. OPERATIONAL CHECKS WERE SATISFACTORY AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200925 19980402 00925 SO 1998 4 2 C2XA98IA013 1 19980204 A 7921 1602824 OIL COOLER EMB 120 EMB120RT SO NR 2 NACELLE CRACKED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 09 16719 120138 BTR - FLT 3865 - PILOT REPORTED AFTER DEPARTURE, THE NR 2 OIL PRESSURE WARNING LIGHT ILLUMINATED, FOLLOWED BY A FLUCTUAT ING OIL PRESSURE GAUGE WHICH THEN DROPPED TO 0 PSI. THE CREW SHUT DOWN THE NR 2 ENGINE AND LANDED AT BTR WITHOUT INCIDE NT. MAINTENANCE FOUND THE NR 2 OIL COOLER TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 2 OIL COOLER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200926 19980402 00926 SO 1998 4 2 C2XA98C1011 1 19980208 A 3260 12041127001 PROX SWITCH EMB 120 EMB120RT SO RT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 51726 120174 CLE - FLT 3297 - CREW REPORTED THE LANDING GEAR GREEN 'B' LIGHT ILLUMINATED IN FLIGHT, AND DURING GEAR TRANSIT THE RED ' A' AND 'B' LIGHT DID NOT ILLUMINATE ON THE RIGHT MAIN LANDING GEAR. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT . MAINTENANCE INSPECTED AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR PROX SWITCH IAW EMB-120 MM 32-61 -01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200927 19980402 00927 EU 1998 4 2 C2XA98BT010 1 19980212 A 3350 301180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19812 99 EWR - IN BOUND AFTER LANDING CREW REPORTED EMERGENCY LIGHTS ON FLOOR BETWEEN ROWS FIVE THROUGH NINE, ABOVE ROW FIVE AND NINE, AND ABOVE FLIGHT ATTENDANTS PANEL TO BE INOPERATIVE. TROUBLESHOT REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPL IES AT 10WL AND 18WL LOCATIONS. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200928 19980402 00928 EU 1998 4 2 C2XA98BT009 1 19980211 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14834 193 BTV - DURING 1A INSPECTION, FOUND EMERGENCY LIGHTS FAILED TO OPERATE PROPERLY DURING TEST OF SYSTEM. REMOVED AND REPLAC ED EMERGENCY LIGHT BATTERY PACK. OPS CHECK OF SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200929 19980402 00929 EU 1998 4 2 SABA980011 1 19980207 A 3230 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU NLG DIRTY A SABA O OTHER N FALSE WARNING LD LANDING 1 SO 33 190PC 750 CLT - FLT 5214 - ON FLT FROM LEX TO CLT, ON APPROACH TO CLT, THE PILOT PUT THE LANDING GEAR DOWN. RECEIVED 3 GREEN LIGH TS AND AN UNSFE RED LIGHT, ALSO WARNING HORN ON NOSE LANDING GEAR. PILOT PUT THE FLAPS TO 35 DEGREES, BUT NO CHANGE. C YCLED GEAR WITH NO CHANGE. PILOT THEN CYCLED THE CIRCUIT BREAKER FOR THE WARNING HORN AT THE TIME THE RED LIGHT AND WAR NING HORN WENT OUT. NO EMERGENCY WAS DECLARED. AIRCRAFT MADE A SAFE LANDING WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE NOSE GEAR DOWN AND LOCK SWITCH STICKING. CLEANED AND LUBED SWITCH. GROUND CYCLED GEAR AND OPS CHECKED GOOD. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998040200930 19980402 00930 1998 4 2 SABA980010 4 19980206 A 3425 7003360941 GYRO DHAV DHC8 DHC8102 2809003 NM E/E COMPT FAILED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 883CC 86060452 162 CLT - FLT 5085 - ON FLT FROM CLT TO CVG, THE FIRST OFFICERS AHRS WENT OUT AND FLAGS WERE TRIGGERED. CREW RESET CIRCUIT BREAKERS. SYSTEM WAS STILL INOP. AIRCRAFT RETURNED TO CHALLOTTE AND LANDED WITH NO OTHER PROBLEMS. NO EMERGENCY WAS D ECLARED. MAINTENANCE FOUND A BAD AHRS GYRO. REMOVED AND REPLACED GYRO. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998040200931 19980402 00931 EU 1998 4 2 SABA980009 1 19980206 A 2130 FILTER BAG JETSTM JETSTM3201 1500217 EU CABIN DIRTY A SABA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 33 942AE 942 CLT - FLT 5222 - ON FLIGHT FROM CLT TO LEX, AFTER DEPARTING CLT PRESSURIZATION BECAME INOP IN MANUAL AND AUTO MODE. CRE W REPORTED, COULD NOT FLY TO LEX, WITH PRESENT FUEL, DUE TO FUEL CONSUMPTION AT LOWER ALTITUDE AND HAVE THE RESERVE FUEL REQUIRED. AIRCRAFT RETURNED TO CLT FOR REPAIR. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED BACK AT CLT WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE REFERENCE SCREEN. ON THE PRESSURIZATION SAFETY VALVE BLOCKED WITH DUST AND DIRTY. REF ERENCE SCREEN WAS CLEANED. AIRCRAFT WAS GROUND RUN AND OPS CHECKED GOOD. TEST FLT WAS FLOWN AND INFLIGHT CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998040200932 19980402 00932 EU 1998 4 2 REXA98066 1 19980308 A 2433 LT52A INVERTER BAG JETSTM JETSTM3101 1500215 EU LEFT FAILED A REXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 315PX 6046 685 HOT BURNING SMELL AND SMOKE IN COCKPIT ON SHORT FINAL. SMOKE STOPPED AFTER LANDING, BUT THE HOT SMELL CONTINUED. FOUND INVERTOR UNDER CAPTAINS SEAT FOR FO'S INSTRUMENT LIGHTS SMOKED. REMOVED AND REPLACED INVERTOR. (M) 2 L 7 2 4T RT A21EU 1998040200933 19980402 00933 1998 4 2 REXA98064 4 19980306 A 3442 6224022001 TR UNIT SAAB SF340 SF340A 7850100 EU FWD FUSELAGE FAILED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 406BH 3268 340A074 RADAR PAINTING FALSE ECHOS. REMOVED AND REPLACED RADAR TRANSCEIVER. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998040200934 19980402 00934 NM 1998 4 2 EISA98040 1 19980221 A 2612 182528001375 FIRE LOOP BOEING 727 727221 1384071 NM NR 2 ENGINE INOPERATIVE A EISA K NONE P NO WARNING INDICATION UK UNKNOWN 1 SW 07 366PA 58624 22538 NR 2 FIRE WARNING WILL NOT TEST. REPLACED CONNECTOR AND FIRE LOOP. (M) 2 L 7 3 4F A3WE 1998040200935 19980402 00935 NM 1998 4 2 EIAA980120 1 19980215 A 5320 SHEAR TIE BOEING 747 747273C 1384896 NM BS 1372 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, LEFT BODY LANDING GEAR WHEEL WELL BS 1372 BULKHEAD UPPER CHORD, VERTICAL FRAME SHEAR TIE CRACKED. REPAIRED IAW SRM 53-10-04 FIG 4. (M) 2 L 7 4 4F A20WE 1998040200936 19980402 00936 NM 1998 4 2 EIAA980112 1 19980202 A 5320 WEB BOEING 747 747273C 1384896 NM BS 1242 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, CORROSINO AT BS 1242 RBL 35 AND WL 180 RT MLG W/W CANTED BULKHEAD WEB CUTOUT. REPAI RED BY TRIMMING WEB, INSTALLING REPAIR DOUBLER AND FILLER IAW HAECO RS R53-48-33673. (M) 2 L 7 4 4F A20WE 1998040200937 19980402 00937 NM 1998 4 2 EIAA980113 1 19980205 A 5711 SPAR BOEING 747 747273C 1384896 NM RT WING CRACK A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, RIGHT WING FRONT SPAR CHORD HAS A FASTENER HOLE THAT IS CRACKED BEYOND LIMITS. OVER SIZED HOLE TO REMOVED CRACK AND INSTALLED NEW FASTENER IAW HAECO RS R54-52-33482. (M) 2 L 7 4 4F A20WE 1998040200938 19980402 00938 NM 1998 4 2 EIAA980114 1 19980202 A 5314 KEEL BEAM BOEING 747 747273C 1384896 NM BS 1383 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, KEEL BEAM LOWER PANEL SUPPORT STRUCTURE CORRODED AT BS 1383 LBL 16 - RBL 16. REPLAC ED 'T' SECTION IAW SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1998040200939 19980402 00939 NM 1998 4 2 EIAA980115 1 19980214 A 5320 WEB BOEING 747 747273C 1384896 NM BS 1760 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, AFT CARGO COMPARTMENT, BS 1760 AT RBL 52 FLOORBEAM VERTICAL WEB DAMAGED. REPAIRED I AW SRM 51-40-02 FIG 1. (M) 2 L 7 4 4F A20WE 1998040200941 19980402 00941 NM 1998 4 2 EIAA980117 1 19980215 A 5230 SKIN BOEING 747 747273C 1384896 NM CARGO DOOR DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, FWD CARGO DOOR AFT LOWER CORNER SKIN DAMAGED. REPAIRED IAW SRM 52-00-03 FIG 4. (M) 2 L 7 4 4F A20WE 1998040200942 19980402 00942 NM 1998 4 2 EIAA980118 1 19980215 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 1840 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, FUSELAGE BS 1840 AT STRINGER 46L - 47L, SKIN HAS A DENT. REPAIRED IAW SRM 53-30-03 FIG 1. (M) 2 L 7 4 4F A20WE 1998040200943 19980402 00943 NM 1998 4 2 EIAA980119 1 19980215 A 5711 SPAR BOEING 747 747273C 1384896 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 20651 HKG - DURING C5/D CHECK INSPECTION, RT WING SPAR UPPER CHORD FSS 688 CRACK AT FASTENER HOLE. REPAIRED IAW HAECO RS 554- 52-33482. (M) 2 L 7 4 4F A20WE 1998040200944 19980402 00944 NM 1998 4 2 GAIA9828 1 19980303 A 3260 ACCESSORY UNIT BOEING 727 727223 1384074 NM LANDING GEAR LOOSE A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6831 20184 AFTER DEPARTING MCO, CREW REPORTS, AFTER GEAR RETRACTION, ALL GEAR UNSAFE 9RED) LIGHTS REMAIN ILLUMINATED. CYCLED GEAR AND INDICATION REMAINED THE SAME. SHORTLY BEFORE RETURN TO MCO, UNSAFE LIGHT EXTINGUISHED. NORMAL INDICATION, AIRCRAFT MADE AN UNEVENTFUL RETURN TO MCO. CLEANED AND RESECURED LANDING GEAR ACCESSORY UNIT PER B727 MM. SYSTEM AND ALL INDIC ATIONS TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998040200945 19980402 00945 WP 1998 4 2 GAIA9822 1 19980224 A 3230 CONTROL CABLE DOUG DC9 DC915F 3022037 WP RT MLG WW ICED UP A GAIA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 563PC 47055 KHA - FLT 805 - SFO-SEA - ON APPROACH TO SEA THE FLIGHT CREW FOUND THE LANDING GEAR HANDLE STUCK IN THE UP POSITION. TH E CREW ELECTED TO USE ALTERNATE GEAR EXTENSION PROCEDURES AND MADE AN UNEVENTFUL LANDING. INSPECTION FOUND A BLOCK OF I CE HANGING ON THE LANDING GEAR CONTROL VALVE CABLES. THE ICE WAS REMOVED THE CABLE WERE LUBED AND A RETRACTION TEST WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998040200946 19980402 00946 NM 1998 4 2 98ZZZM353 1 19980219 A 2424 20040 GCU DORNER DO32 DO328100 2996000 NM LT ENGINE TRIPPED A EQGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 19 335PH 1154 3013 FLT 445 - DFW-CUU - APPROX 45 MINUTES INTO THE FLT, FLT WAS CLEARED TO CLIMB TO FL310. WHILE PASSING THROUGH FL280, CRE W ENCOUNTERED A RT ALT FAILURE. FO ATTEMPTED TO RESET ALT BY PRESSING THE RT ALT BUTTON TO 'OFF' AND AGAIN TO 'ON'. AL T FAIL LIGHT REMAINED ON. CREW CONSULTED QRH FOR FOLLOW PROCEDURES AND PRESSED THE AC TIE BUTTON TO 'ON' TO ALLOW THE L T ALT TO PICK UP THE LOAD. CREW ALSO TURNED OFF WINDSHIELD HEATS. AS THE FLT LEVELED OFF AT FL310, CREW ENCOUNTERED LT ALT FAILURE. FO PRESSED THE AC TIE BUTTON TO 'OFF' AND ATTEMPTED TO RESET BOTH THE LT AND RT ALT WITH NEITHER COMING B ACK ON LINE. CREW CONTACTED FLT CONTROL AND MX CONTROL AND RETURNED TO DFW. CENTER WAS BRIEFED OF THE SITUATION AND TH 2 H 7 2 4T RT A45NM 1998040200947 19980402 00947 NM 1998 4 2 98ZZZM354 1 19980219 A 2424 20040 GCU DORNER DO32 DO328100 2996000 NM RT ENGINE TRIPPED A EQGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 19 335PH 1008 3013 FLT 445 - DFW-CUU - APPROX 45 MINUTES INTO THE FLT, FLT WAS CLEARED TO CLIMB TO FL310. WHILE PASSING THROUGH FL280, CRE W ENCOUNTERED A RT ALT FAILURE. FO ATTEMPTED TO RESET ALT BY PRESSING THE RT ALT BUTTON TO 'OFF' AND AGAIN TO 'ON'. AL T FAIL LIGHT REMAINED ON. CREW CONSULTED QRH FOR FOLLOW PROCEDURES AND PRESSED THE AC TIE BUTTON TO 'ON' TO ALLOW THE L T ALT TO PICK UP THE LOAD. CREW ALSO TURNED OFF WINDSHIELD HEATS. AS THE FLT LEVELED OFF AT FL310, CREW ENCOUNTERED LT ALT FAILURE. FO PRESSED THE AC TIE BUTTON TO 'OFF' AND ATTEMPTED TO RESET BOTH THE LT AND RT ALT WITH NEITHER COMING B ACK ON LINE. CREW CONTACTED FLT CONTROL AND MX CONTROL AND RETURNED TO DFW. CENTER WAS BRIEFED OF THE SITUATION AND TH 2 H 7 2 4T RT A45NM 1998040200948 19980402 00948 NM 1998 4 2 98ZZZM355 1 19980316 A 3150 EICAS DORNER DO32 DO328100 2996000 NM COCKPIT MALFUNCTIONED A EQGA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 19 338PH 3029 DFW - FLT 193 - JUST AFTER RECEIVING CLEARANCE FOR POSITION AND HOLD AND BEFORE STARTING THE TAKEOFF ROLL HAD A MASTER C AUTION WITH EICAS MESSAGE 'PROXI SYSTEM' AND ALSO A BLUE STATUS MESSAGE 'HYD PROXI SINGLE' WITH AMBER MESSAGES ON THE HY DRAULIC SYSTEM PAGE 'PROXI LOCK FAIL' AND 'PROXI SYSTEM FAIL'. CREW CLEARED AIRCRAFT FROM RUNWAY AND PROCEEDED TO RETUR N TO GATE. ON APPROACH TO GATE. ON APPROACH TO GATE, ALL CAUTIONS EXTINGUISHED. CREW RECEIVED CLEARANCE ONCE AGAIN AN D AIRCRAFT DEPARTED WITHOUT INCIDENT. (M) 2 H 7 2 4T RT A45NM 1998040200949 19980402 00949 SW 1998 4 2 98ZZZM356 1 19980316 A 2550 CURTAIN FRCHLD SA227 SA227DC 3377521 SW BAGGAGE DOOR OUT OF POSITION A EQGA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 19 853LS DC853B BPT - FLT 1296 - DURING CLIMB, CREW HEARD A SLAPPING SOUND OUTSIDE OF THE AIRCRAFT. CREW RETURNED TO BPT FOR INVESTIGAT ION. UPON ARRIVAL AT GATE AND SHUTTING DOWN BOTH ENGINES, GROUND CREW REALIZED THAT THE FWD RT BAGGAGE DOOR HAD BEEN CL OSED WITH THE RAIN PROTECTOR CURTAIN HANGING OUTSIDE OF THE AIRCRAFT. RAIN PROTECTION CURTAIN WAS STOWED PROPERLY AND C REW PERFORMED VISUAL INSPECTION OF CARGO BAY AREA FOR SIGNS OF DAMAGE. NO DAMAGE WAS DETECTED. FLT DEPARTED WITHOUT FU RTHER INCIDENT. (M) 2 L 7 2 4T RT A18SW 1998040200950 19980402 00950 1998 4 2 HALA9800062 4 19980209 A 2565 1A23133 O-RING DOUG DC9 DC951 3022051 WP CABIN DOOR SLIDE FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 601AP 47658 FLT 158 - HNL - FORWARD SERVICE DOOR SLIDE DID NOT DEPLOY PRESS ZERO. INSPECTION OF BOTTLE REVEILED THE MAIN 'O' RING C OULD HAVE CAUSED THE PRESSURE TO LEAK OUT OF THE BOTTLE. WHEN A NEW BOTTLE WAS INSTALLED AND SLIDE TESTED, IT DEPLOYED AS ADVERTISED. REMOVED AND REPLACED RIGHT FWD DOOR SLIDE. (M) 2 L 7 2 4F RT A6WE 1998040200951 19980402 00951 EU 1998 4 2 98ZZZM357 1 19980223 A 5711 S5721058020051 SPAR AEROSP ATR42 ATR42300 8680920 EU LT WING AFT CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 973NA 065 DURING ACCOMPLISHEMENT OF SB ATR 42-57-0044R2 AD 97-26-11, FOUND CORROSION DAMAGE ON THE LEFT WING REAR SPAR LOWER EXTRU SION FOUND OUT OF LIMITS. THE MANUFACTURE WAS CONTACTED AND A TEMPORARY REPAIR WAS PROVIDED ALLOWING TO FLY THE AIRCRAF T TO A BASE WHERE THE NECCESSARY REPAIRS COULD BE PERFORMED. THE TEMPORARY REPAIR WAS ACCOMPLISHED IAW THE MANUFACTURER DRAWING AIRAMS/T/ATR/31761/98. A MECHANIC WAS ONBOARD THE AIRCRAFT TO PERFORM A VISUAL INSPECTION AFTER EACH LANDING I AW THE MANUFACTURER PROCEDURES. (M) 2 H 7 2 4T RT A53EU 1998040200952 19980402 00952 NM 1998 4 2 TAOA039802 1 19980311 A 3350 RPSIB BATTERY CHARGER BOEING 727 727227 1384078 NM CABIN FAILED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 2587 21244 FLT 6150 - LGA-BOS - AFT SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY CHARGER, OPERATIONAL CHECK NO RMAL PER MM 33-50. (M) 2 L 7 3 4F A3WE 1998040200953 19980402 00953 WP 1998 4 2 ASAA9880049 1 19980311 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200954 19980402 00954 WP 1998 4 2 ASAA9880048 1 19980310 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 940AS 49825 LAX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPAIRED CHAF FED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998040200955 19980402 00955 WP 1998 4 2 ASAA9880047 1 19980310 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT FROM ROWS 19 TO 22 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998040200956 19980402 00956 WP 1998 4 2 ASAA9880046 1 19980309 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 964AS 53078 SMF - PRIOR TO DEPARTURE OF FLT 409 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 2 FORWARD AND ROWS 25 TO 2 9 WERE INOPERATIVE. SECURED LOOSE CONNECTORS AT ROW 2 AND ROW 25 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200957 19980402 00957 WP 1998 4 2 ASAA9880042 1 19980308 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 21 TO 28 WERE FOUND INOPERATIVE. REPLACED TH E POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200958 19980402 00958 WP 1998 4 2 ASAA9880040 1 19980303 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 965AS 53079 SEA - FLT 446 - PRIOR TO DEPARTURE, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACE D THE BATTERY PACK AND REPAIRING WIRING IN PART OF SECTION, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200959 19980402 00959 WP 1998 4 2 ASAA9880039 1 19980303 A 3350 GROUND DOUG DC9 DC982 3022082 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 49925 SEA - DURING MAINTENANCE CHECK, THE R-1 DOOR OVERHEAD EMERGENCY LIGHTS FLICKERED. RESECURED LOOSE GROUND STUD AND LIGHT S OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998040200960 19980402 00960 WP 1998 4 2 ASAA9880037 1 19980301 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 949AS 53022 SEA - FLT 232 - PRIOR TO DEPARTURE, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPAIRE D FLOOR TRACK WIRING IN FIRST CLASS CABIN AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200961 19980402 00961 WP 1998 4 2 ASAA9880036 1 19980301 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REPLACED TH E BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200962 19980402 00962 WP 1998 4 2 ASAA9880035 1 19980226 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 PDX - DURING MAINTENANCE CHECK, THE FLIGHT DECK AND FORWARD ENTRY EMERGENCY LIGHTS WERE FOUND TO BE VERY DIM. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200963 19980402 00963 WP 1998 4 2 ASAA9880027 1 19980215 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 947AS 53020 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. REPLACED LIGHT ASSEMBLY AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200964 19980402 00964 NM 1998 4 2 ASAA9840046 1 19980308 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 SEA - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECT ED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200965 19980402 00965 NM 1998 4 2 ASAA9840045 1 19980306 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200966 19980402 00966 NM 1998 4 2 ASAA9840043 1 19980228 A 3350 15AT41 SWITCH BOEING 737 7374Q8 NM COCKPIT LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 774AS 25107 JNU - DURING MAINTENANCE CHECK, THE FLIGHT STATION EMERGENCY EXIT LIGHT SWITCH WOULD NOT REMAIN IN THE ON POSITION. FOU ND THAT AN UNUSED TERMINAL SCREW ON THE SWITCH WAS LOOSE WHICH WAS CAUSING INTERFERENCE WITH SWITCH TRAVEL. REMOVED SCR EW AND INSPECTED SWITCH FOR DAMAGE AND OTHER TERMINALS FOR SECURITY. NO DEFECTS NOTED. SWITCH OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200967 19980402 00967 NM 1998 4 2 ASAA9840042 1 19980227 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 SEA - DURING MAINTENANCE CHECK, THE FWD AND AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACE D LIGHT ASSEMBLIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200968 19980402 00968 NM 1998 4 2 ASAA9840029 1 19980210 A 3397 WIRE BOEING 737 737490 1384715 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 767AS 27081 PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200969 19980402 00969 NM 1998 4 2 ASAA9810020 1 19980306 A 3350 LIGHT BOEING 737 737210C 1384459 NM CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 ANC - DURING MAINTENANCE CHECK, ONE RED EMERGENCY FLOOR TRACK LIGHT WAS FOUND TO BE MISSING AT NR 6 PALLET. REPLACED LI GHT ASSEMBLY, LAMP, AND LENS. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998040200970 19980402 00970 NM 1998 4 2 ASAA9810019 1 19980303 A 3350 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING RECON, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO INOPERATVIE AT ROW 14. REPLACED BATTERY PACK AND LIGH TS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998040200971 19980402 00971 NM 1998 4 2 ASAA9810018 1 19980225 A 3350 883200312 RECEIVER BOEING 737 737210C 1384459 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE FIRST PALLET EMERGENCY EXIT LIGHT RECEIVER WAS FOUND TO BE INOPERATIVE. REPLACED RE CEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998040200972 19980402 00972 NM 1998 4 2 ASAA9810013 1 19980211 A 3350 8731002142 LIGHTS BOEING 737 7372X6C 1384552 NM R1 DOORS INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R1 AND R2 DOOR EMERGENCY IDENTIFIERS WERE FOUND TO BE INOPERATIVE. REPLACED R1 DOOR LIGHT ASSEMBLY AND THE BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200973 19980402 00973 NM 1998 4 2 98ZZZM358 1 19980211 A 3350 014997101 BATTERY PACK BOEING 737 7372X6C 1384552 NM R2 DOORS DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R1 AND R2 DOOR EMERGENCY IDENTIFIERS WERE FOUND TO BE INOPERATIVE. REPLACED R1 DOOR LIGHT ASSEMBLY AND THE BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200974 19980402 00974 WP 1998 4 2 ASAA9880041 1 19980304 A 5210 4928806503 HOOK DOUG DC9 DC983 3022083 WP L1 DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOLD OPEN HOOK WAS FOUND BENT. REPLACED THE DOOR HOLD OPEN HOOK AND OPERATE D NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998040200975 19980402 00975 WP 1998 4 2 ASAA9880038 1 19980228 A 5610 MECHANISM DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 937AS 49364 SEA - AFTER ARRIVAL OF FLT 530 - CREW REPORTED THE CAPTAINS SLIDING WINDOW WOULD NOT OPEN MORE THAN HALFWAY. ADJUSTED T HE CAPTAINS SLIDING WINDOW MECHANISM, PRESSURE CHECKED TO 3 PSI AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998040200976 19980402 00976 NM 1998 4 2 ASAA9840041 1 19980126 A 5542 65C2584151 SKIN BOEING 737 7374Q8 NM RUDDER CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 1187 25104 SEA - DURING C-CHECK, THE RUDDER LEFT AND RIGHT SIDES WERE FOUND TO HAVE ETCHED AND CRACKED PAINT. ON FURTHER EVALUATIO N IT WAS DETERMINED THAT THE OUTER PLIES OF GRAPHITE WERE FOUND TO BE PEELING AND SPLINTERING. REMOVED AND REPLACED RUD DER. REMOVED RUDDER WAS SENT TO NORDAM FOR EVALUATION AND REPAIR. THE RUDDER WAS SUBSEQUENTLY EXCHANGED BY NORDAM AND ALASKA AIRLINES RECEIVED A NEW RUDDER. (M) 2 L 7 2 4F RT A16WE 1998040200977 19980402 00977 EU 1998 4 2 AALA980413 1 19980227 A 2910 O-RING FOKKER F28 F28MK0100 4990807 EU RT ENGINE DEFECTIVE A AALA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 07 1471G 11507 SAT - FLT 249 - DURING CRUISE, NR 1 HYDRAULIC QTY DEPLETED TO ZERO. CREW FOLLOWED ALTERNATE PROCEDURES TURNING OFF SYST EM NR 1 PUMPS ON ENGINES 1 AND 2. LANDING GEAR ALTERNATE PROCEDURES WERE FOLLOWED AND THE AIRCRAFT LANDED SAT WITH NO F URTHER INCIDENT. REPLACED LEAKING O-RING ON RIGHT ENGINE DRIVEN HYDRAULIC PUMP SYSTEM NR 1. SERVICED HYDRAULIC SYSTEM AND RAN ENGIEN WITH NO FURTHER LEAKS NOTED. SYSTEM LEAK CHECKED AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998040200978 19980402 00978 EU 1998 4 2 AALA980228 1 19980301 A 2750 EAFCD8518411 CONTROL UNIT FOKKER F28 F28MK0100 4990807 EU TE FLAPS DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1438H 11428 ORD - FLT 1648 - ON TAKEOFF ORD, FLAPS WOULD NOT RETRACT, STAYED AT 8 DEGREES. RETURNED TO ORD, LANDED WITHOUT INCIDENT , FLAPS RETRACTED NORMALLY. REPLACED FLAP CONTROL UNIT. CYCLED FLAPS SEVERAL TIMES WITH NO FAULTS NOTED. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998040200979 19980402 00979 EU 1998 4 2 AALA980439 1 19980305 A 2751 WARNING FOKKER F28 F28MK0100 4990807 EU COCKPIT MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1432A 11417 COS - FLT 659 - AFTER TAKEOFF, EIGHT DEGREES FLAPS WAS SELECTED AND A FLAP ASYMMETRY MESSAGE APPEARED ON MFDU. FLIGHT C REW DECLARED AN EMERGENCY AND LANDED COS WITHOUT FURTHER INCIDENT. MAINTENANCE RESET ASYMMETRY FAULT BALL ON MAINTENANC E TEST PANEL AND CYCLED FLAPS SEVERAL TIMES UNABLE TO DUPLICATE FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998040200980 19980402 00980 NM 1998 4 2 98ZZZM359 1 19980227 A 3350 LIGHT BOEING 727 727227 1384078 NM AIRSTAIRS BROKEN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 772AT 22003 DURING P/F, FOUND THE OVERHEAD EMERGENCY LIGHT ASSY NOT WORKING PROPERLY AND LENS COVER IS BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. (M) 2 L 7 3 4F A3WE 1998040200981 19980402 00981 NM 1998 4 2 98ZZZM360 1 19980227 A 3350 LIGHT BOEING 727 727264 138408M NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 763AT 22983 DURING P/F, FOUND EMERGENCY LIGHT OVER L-1 DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT OVER L-1 DOOR. (M) 2 L 7 3 4F A3WE 1998040200982 19980402 00982 NM 1998 4 2 98ZZZM361 1 19980227 A 3350 BATTERY PACK BOEING 727 727264 138408M NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 763AT 22983 DURNG P/F, FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1998040200983 19980402 00983 NM 1998 4 2 98ZZZM362 1 19980221 A 3350 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 783AT 22000 DURING P/F, FOUND ROW TO 10 EGRESS LIGHT OUT. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998040200984 19980402 00984 EU 1998 4 2 C2XA98BT021 1 19980310 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 BTV - DURING 3A INSPECTION, FOUND FORWARD AISLE PATH EMERGENCY LIGHTS TO BE INOPERATIVE. REMOVED AND REPLACED POWER SUP PLIES AT 29WL AND 3WL AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200985 19980402 00985 EU 1998 4 2 C2XA98BT020 1 19980307 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 BTV - DURING 3A INSPECTION, FOUND CABIN AISLE PATH EMERGENCY LIGHTS DID NOT TEST PROPERLY. REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY 10WL. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200986 19980402 00986 EU 1998 4 2 C2XA98BT019 1 19980306 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15816 105 EWR - REPORTED LEFT FORWARD EMERGENCY LIGHT TO BE INOPERATIVE. REMOVED AND REPLACD BATTERY PACK FOR FORWARD EMERGENCY L IGHTS. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200987 19980402 00987 EU 1998 4 2 C2XA98BT018 1 19980306 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19812 99 EWR - AFTER ARRIVING FLIGHT 3528, REPORTED PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY LIGHT AND BATTERY PACK AT POSITION 29WL. SYSTEM WAS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200988 19980402 00988 EU 1998 4 2 98ZZZM363 1 19980306 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19812 99 EWR - AFTER ARRIVING FLIGHT 3528, REPORTED PASSENGER DOOR EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY LIGHT AND BATTERY PACK AT POSITION 29WL. SYSTEM WAS OPERATIONALLY CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200989 19980402 00989 EU 1998 4 2 C2XA98BT017 1 19980303 A 5350 RADOME AEROSP ATR42 ATR42320 8680930 EU FWD FUSELAGE LIGHTNING STRIKE A C2XA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 09 14833 188 EWR - EN ROUTE SYR AIRCRAFT STUCK BY LIGHTNING DIVERTED TO SWF. AIRCRAFT HAD LIGHTNING INSPECTION AND FERRIED TO EWR, P ERFORMED FURTHER CHECKS AND MAINTENANCE FERRIED AIRCRAFT TO BTV FOR FINAL REPAIRS. MAJOR REPAIR PERFORMED ON FORWARD PR ESSURE BULKHEAD AT UPPER LEFT SIDE, OUTBOARD OF RADOME LATCH IAW ATR 42 SRM 53-11-10 PRESSURE CHECKED AIRCRAFT AFTER REP AIR AND RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200990 19980402 00990 EU 1998 4 2 C2XA98BT016 1 19980306 A 3350 COVER AEROSP ATR72 ATR72212 EU GALLEY CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69902 385 EWR - CREW REPORTED EMERGENCY EXIT LIGHT IN FRONT OF GALLEY LOOSE AND CRACKED. MAINTENANCE FOUND GALLEY FLOOR EMERGENC Y EXIT LIGHT COVER MISSED PLACED/CRACKED, RE-INSTALLED GALLEY FLOOR EMERGENCY EXIT LIGHT AND COVER. (M) 2 H 7 2 4T RT A53EU 1998040200991 19980402 00991 EU 1998 4 2 C2XA98CL018 1 19980302 A 2612 FIRE WARNING AEROSP ATR42 ATR42320 8680930 EU RT ENGINE ACTIVATED A C2XA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 09 19812 99 EWR - DURING TAXI THE CREW RECEIVED A FIRE INDICATION WITH ALL ASSOCIATED WARNING ON THE RIGHT ENGINE. MAINTENANCE PERF ORMED A DETAILED VISUAL INSPECTION OF THE RIGHT ENGINE AND FOUND NO INDICATION OF A FIRE. THE FIRE DETECTION SYSTEM CHE CKED GOOD IAW ATR 42 JIC 26-12-00. AIRCRAFT ENGINES WERE CHECKED FOR OPERATION AND LEAKS WITH NO DEFECTS FOUND, DETERMI NED FIRE WARNINGS DUE TO HIGH WINDS BLOWING INTO TAIL PIPE OF ENGINES. AIRCRAFT RELEASED FOR SERVICE. (M) 2 H 7 2 4T RT A53EU 1998040200992 19980402 00992 EU 1998 4 2 C2XA98BT015 1 19980225 A 3350 P4010021 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 BTV - ON LINE CHECK IN BTV, FOUND EMERGENCY FLASHLIGHT BELOW FLIGHT ATTENDANTS SEAT TO BE INOPERATIVE. REMOVED AND REPL ACED EMERGENCY FLASHLIGHT BATTERY PACK. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998040200993 19980402 00993 SO 1998 4 2 C2XA98IA035 1 19980226 A 3220 20168 PIN EMB 120 EMB120RT SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK UPPER PIVOT PIN WAS FOUND TO BE CORRODED INSIDE THE A TTACH PIN HOLE. MAINTENANCE REMOVED AND REPLACED THE PIN IAW ERAM CMM 32-31-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200994 19980402 00994 SO 1998 4 2 C2XA98IA036 1 19980226 A 3220 20168 PIN EMB 120 EMB120RT SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR TORQUE LINK LOWER PIVOT PIN WAS FOUND TO BE CORRODED IN SIDE THE ATTACH PIN HOLE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PIVOT PIN IAW ERAC CMM 32-31-01 AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200995 19980402 00995 SO 1998 4 2 C2XA98IA037 1 19980226 A 3221 1975000001 TRUNNION EMB 120 EMB120RT SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR STRUT SPRING BOX UPPER TRUNNION WAS FOUND TO BE PITTED. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED TRUNNION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ALL WORK ACCOMPLISH ED IAW ERAM CMM 32-21-01. (M) 2 L 7 2 4T RT A31SO 1998040200996 19980402 00996 SO 1998 4 2 C2XA98IA038 1 19980226 A 3221 2069600001 TRUNNION EMB 120 EMB120RT SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR SPRING BOX LOWER TRUNNION WAS FOUND TO BE PITTED. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED TRUNNION IAW EMB120 CMM ERAM 32-21-01 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998040200997 19980402 00997 SO 1998 4 2 C2XA98IA041 1 19980226 A 5720 12017063609 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200998 19980402 00998 SO 1998 4 2 C2XA98IA040 1 19980226 A 5720 12017062613 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 MM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040200999 19980402 00999 NM 1998 4 2 CKSA98204 1 19980330 A 2612 FIRE CARD BOEING 747 747269B NM E/E COMPT LOOSE A CKSA O OTHER N FALSE WARNING TO TAKEOFF 1 GL 23 708CK 21543 UPON ROTATION WHEEL WELL FIRE LIGHT ILLUMINATED STEADY. TRANSFERRED TO DMI NR 76808998 PER MEL 26-6 PLACARDS INSTALLED. RESEATED LOOSE A16 CARD IN FIRE DETECT CARD BOX. OPS CHECK GOOD IAW B747 MM 26-17-00. CLEARS DMI PLACARDS REMOVED. 2 L 7 4 4F RT A20WE 1998040300001 19980403 00001 1998 4 3 UPS98626135 4 19980318 A 3420 STANDBY ATT IND BOEING 767 76734AF 1385212 NM INSTRUMENT PNL. GROUNDED A IPXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 01 312UP 27763 INSPECTION TYPE-N/A ON TAKEOFF AT 40 KTS GPWS PULL UPLIGHT AND MASTER WARN LIGHT ILLUM. WARNING LTS COME ON/OFF MOVI NG STANDBY ATT IND CAGE KNOB. REPOSITION WIRES IN AREA OF SAI BEHIND WARN LTS. REPLACED SAI, UNABLE TO GET WARN LTS ON . SUSPECT CASE GROUND, SAI OP CK NORM PER MM34-24-00. 2 L 7 2 4F RT A1NM 1998040600001 19980406 00001 EU 1998 4 6 VTZA98012 1 19980108 A 2611 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU BAGG COMPT DIRTY A VTZA K NONE N FALSE WARNING DE DESCENT 1 EA 27 481UE 895 FLT 6254 - AIB-IAD - DURING DESCENT, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS POD SMOKE DETECTIO N WARNING LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE AND WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED SMO KE DETECTOR CANNON PLUG, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998040700001 19980407 00001 1998 4 7 HEEA0013408 4 19980318 A 2210 BHL43051500 SENSOR BOLKMS 117 BK117B1 5626012 EU SPAS SYS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 7059J 7151 SPAS SYSTEM WILL NOT TEST. 1 G 7 2 3U H13EU 1998040700002 19980407 00002 EU 1998 4 7 HEEA0013447 1 19980318 A 7714 1179405303 INDICATOR BOLKMS 117 BK117B1 5626012 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7059J 7151 NR1 NEEDLE DOES NOT MOVE WITH POWER. 1 G 7 2 3U H13EU 1998040700003 19980407 00003 NE 1998 4 7 UPS98826178 2 19980325 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM56* 13802 NE NR 4 FAILED A IPXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 SO 01 798UP 45898 693280 NR 4 ENGINE FLAMEOUT AT FL350, SUCCESSFUL RESTART WITH MILD VIBRATION. FLAMEOUT WITH THROTTLE ADVANCE. FIRE TEST INDIC ATED SHORT CIRCUIT, MA N-O-TEMP(270DEG. C). NR 4 BLEED OFF, TEMP DECREASE ENG FIRE, SEVERE DAMAGE CHECKLIST ACCOMPLISHE D. DISCHARGED BOTH FIRE BOTTLES. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998040700004 19980407 00004 NE 1998 4 7 DL72S980659 2 19980325 A 7321 FUEL CONTROL 37820113 BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE FAILED A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 SO 27 544DA 82510 22493 695334 NR 3 ENG DID NOT RESPOND TO THROTTLE MOVEMENT DURING DESCENT, FLAMEOUT, FUEL FLOW WAS ZERO. EGT AND EPR WERE ZERO AND N OT RESPONDING. N1 AND N2 DISPLAYED WINDMILLING INDICATION, THIS LASTED FOR 2 TO 3 MINUTES. PRIOR TO COMMENCING THE ENG FAILURE FOLLOW UP CHECKLIST THE ENG BEGAN RESPONDING NORMALLY. REPLACED NR 3 ENGINE FUEL CONTROL AND FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 1998040700005 19980407 00005 WP 1998 4 7 RRXA98073 1 19980324 A 2612 24407332 FIRE ELEMENT DOUG DC8 DC8F54 3021926 WP NR 2 ENGINE SHORTED A RRXA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 WP 15 991CF 45801 CLIMBING THROUGH 13000 FT, NR 2 ENG FIRE WARNING CAME ON. SHUT DOWN ENGINE AND FIRE WARNING WENT OUT. TESTED FIRE WARN ING AND TEST WAS INOP, DISCHARGED AGENT AFTER APPROX 30 SEC FIRE TEST WAS GOOD. RII FOUND NR 2 ENG UPPER AFT FIRE WARNI NG ELEMENT SHORTING TO CLAMP. REMOVED AND REPLACED SAME MOW NORMAL. REMOVED AND REPLACED INBD NR 2 FIRE BOTTLE IAW MM -26-4-1, OPS NOW NORMAL ON 2 AND 3 ENG RUN. 2 L 7 4 4F 4A25 1998040700006 19980407 00006 NE 1998 4 7 P5CA9800743 2 19980324 A 7261 0979004001 OIL TANK CAP BOEING 747 747283B 1384867 NM PWA JT9 JT9D7 52054 NE NR 4 ENGINE MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 FOUND NR 4 ENGINE OIL CAP MISSING. INSPECTED ENG FOR CAP. DRAINED OIL AND SERVICED. INSTALLED NEW CAP, OPS AND LEAK C HECK OK IAW MM 79-11-00. 2 L 7 4 4F 4 F A20WE E20EA 1998040700007 19980407 00007 EU 1998 4 7 MALA976078 1 19980318 A 3350 7239410802 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 592MA 340B199 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHT AT ROW 9 INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998040700008 19980407 00008 NM 1998 4 7 AALA980429 1 19980303 A 5510 HINGE BOEING 727 727223 1384074 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 863AA 21090 TUL - CORROSION ON TOP OF HORIZONTAL STABILIZER, T/E CHORD INBOARD OF NR 7 ELEV HINGE RIGHT. REPAIRED CORRODED AREA PER ESO 11697. TREATED, PRIMED, AND PAINTED. TST: 57,207 HOURS. CYCLES: 35,211. (X) 2 L 7 3 4F A3WE 1998040700009 19980407 00009 SO 1998 4 7 C2XA98IA102 1 19980226 A 5720 12017059609 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 19 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN T SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040700010 19980407 00010 SO 1998 4 7 C2XA98IA061 1 19980226 A 5347 120159994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998040800001 19980408 00001 NM 1998 4 8 K3HA980021 1 19980301 A 3350 37069001 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY LIGHT AFT VENTRAL STAIRS INOP. INSTALLED NEW BATTERYS (P/N 370069-001) (S/N NOV-59), OPS CHECK OK. 2 L 7 3 4F A3WE 1998040800002 19980408 00002 NM 1998 4 8 QXEA00011 1 19980104 A 2130 PRESSURIZATION DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 09 347PH 480 RETURNED TO FIELD. AIRCRAFT WILL NOT PRESSURIZE IN MANUAL. AUTO PRESIOUSLY MEL'D. AIRCRAFT DOWN FOR REPAIRS. 2 H 7 2 4T RT A13NM 1998040800003 19980408 00003 NM 1998 4 8 QXEA9800031 1 19980115 A 3320 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 827PH 275 CABIN OVERHEAD LIGHT AT ROW 2 HAS ACRID SMELL. MAINTENANCE REMOVED LAMP, DISCONNECTED CONNECTOR, AND PLACED ON MEL. ME L CLEARED BY REPLACING RECEPTACLE AND LAMP, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998040800004 19980408 00004 NM 1998 4 8 QXEA9800034 1 19980119 A 3350 10126271 SIGN DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 354PH 498 RIGHT HAND FORWARD EMERGENCY EXIT SIGN INOP. REPLACED RIGHT HAND EXIT SIGN, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998040800005 19980408 00005 NM 1998 4 8 98UAL900008 1 19980109 A 2530 WIRE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY CHILLER CHAFED A UALA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 WP 29 653UA 25391 SHORT CIRCUIT IN FRONT OF P39 PANEL RESULTED IN LOCALIZED FIRE AFT OF FORWARD GALLEY CHILLER. THE I/B WIRE BUNDLE WAS F OUND WITH SEVERE DAMAGE. DIVERTED TO LHR. *S/D* ALL WIRES REPAIRED PER BOEING STANDARD WIRING PRACTICES MANUAL CH 20. BECAUSE OF THE SEVERITY OF THE DAMAGE, CAUSE OF INCIDENT INCONCLUSIVE. HOWEVER, IT IS BELIEVED TO HAVE BEEN CAUSED BY INADVERTENT CONTACT BETWEEN THE FORWARD GALLEY CHILLER AND THE BUNDLES DURING CHILLER REPLACEMENT. SUBSEQUENT INSPECTI ONS ON OTHER UAL 767 AIRCRAFT HAVE REVEALED MINOR DAMAGE TO THIS WIRING AT THESE LOCATIONS. FUTURE CHILLER CHAFING. BO EING CONSULTED FOR FUTURE PERMANENT WIRE BUNDLE/CHILLER PLACEMENT RESOLUTION. 2 L 7 2 4F 4 F RT A1NM E24NE 1998040800006 19980408 00006 1998 4 8 98UAL900009 4 19980109 A 2340 WARNING SYST BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 29 653UA 25391 UPON EVACUATION OF AIRCRAFT, AURAL WARNING SIGNAL FAILED TO OPERATE MID CABIN TO AFT CABIN. *S/D* THIS PROBLEM WAS NOT DUPLICATED. AFTER POWER WAS RESTORED, THE SYSTEM OPERATIONALLY CHECKED NORMAL. THE SYSTEM HAS ONLY ONE POWER SOURCE F OR THE FORWARD, CENTER AND AFT ZONES OF THE AIRCRAFT, MAKING IT IMPOSSIBLE FOR THE FAILURE TO BE RELATED TO LOSS OF POWE R DUE TO THE OTHER AIRCRAFT PROBLEMS. 2 L 7 2 4F 4 F RT A1NM E24NE 1998040800008 19980408 00008 NM 1998 4 8 98UAL900014 1 19980113 A 2750 7321855007 CONTROL VALVE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE TE FLAP FAILED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 658UA 27113 TRAILING EDGE LIGHT ON DURING APPROACH AT POSITION 20. EXECUTED MISSED APPROACH. NEXT APPROACH FLAPS WORKED NORMALLY. *S/D* AN INTERMITTENT INTERNAL FAILURE IN THE TRAILING EDGE FLAP POWER DRIVE UNIT HYDRAULIC CONTROL VALVE MODULE ACTIV ATED THE T/E FLAP FAILURE PROTECTION SYSTEM WHICH INHIBITS FLAP MOVEMENT. REPOSITIONING THE FLAP CONTROL LEVERS TO THE FULL RETRACT POSITION UNLATCHED THE FAILURE PROTECTION SYSTEM AND RESTORED FULL FLAP OPERATION. THE SUBJECT T/E FLAP P DU CONTROL VALVE WAS REMOVED, REPLACED, AND OPERATIONALLY CHECKED PER MM 27-51-32. ALL SYSTEMS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1998040800009 19980408 00009 NM 1998 4 8 98UAL900021 1 19980117 A 2530 OVEN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE GALLEY DIRTY A UALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 612UA 21873 STRONG SMELL OF ELECTRICAL SMOKE IN FWD GALLEY AREA. SMELL APPEARED TO DISSIPATE WHEN UTILITY BUSES WERE TURNED OFF. D IVERTED TO SLC. *S/D* AIRCRAFT WAS THOROUGHLY INSPECTED AND NO DEFECTS WERE FOUND. MECHANIC WRITE-UP FOLLOWS: CK'D P 31,P33,P36,P37 PNLS AND WIRING, RECIRCULATION FANS, ALL OVENS, CHILLERS, LIGHTS, HOT PLATES. RAN ENTERTAINMENT SYS, NO ODORS NOTED. RAN ENGS AT PWR IN GRD AND FLT MODES, FULL ELEC LOAD WITH PACKS, NO ODORS NOTED. INSPECTED AREA FWD OF P3 3 PNL, NO DEFECTS NOTED. UNABLE TO DUPLICATE SMOKE OR ODOR. FLEET ENGINEERING SUSPECTS PLASTIC OR OTHER ITEM WAS DRAWN -UP AGAINST OVEN RECIRCULATION FAN INLET CAUSING THE BURNT SMELL. 2 L 7 2 4F 4 F RT A1NM E3NE 1998040800010 19980408 00010 NM 1998 4 8 98UAL900057 1 19980209 A 2120 COOLING VALVE BOEING 10607042 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E COMPT STUCK A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7284U 21562 AT 24,000 FEET ALTITUDE COULD NOT MAINTAIN PRESSURIZATION. LESS THAN 500 FPM CABIN ALTITUDE CLIMB. DECENDED TO 15,000 FEET AND COULD ONLY MAINTAIN 9,000 FEET CABIN ALTITUDE. *S/D* THE RADIO RACK COOLING VALVE WAS STUCK OPEN. REPLACED V ALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998040800011 19980408 00011 NM 1998 4 8 98UAL900060 1 19980211 A 7933 TEMP SENSOR LEWIS ENGINE 1122514 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 364UA 24533 724850 THE NUMBER 1 ENGINE OIL TEMPERATURE WAS IN THE HIGH END OF THE YELLOW BAND. THE TEMPERATURE FOLLOWS THE THROTTLE POSITI ON. ALL OTHER INDICATION WERE NORMAL. *S/D* REPLACED OIL TEMPERATURE BULB. 2 L 7 2 4F 4 F RT A16WE E2GL 1998040800012 19980408 00012 NM 1998 4 8 98UAL900065 1 19980213 A 2820 69186128 ELBOW BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL TANK BROKEN A UALA O OTHER O OTHER CL CLIMB 1 WP 29 7446U 21900 FUEL TANK NR 3 BURNS FUEL WHILE IN ALL CONFIGURATIONS DURING CLIMB. NR 3 TANK WAS FULL AND BURNED DOWN ABOUT 700 LBS A ND THEN STOPPED. *S/D* THE VENT ELBOW IN THE TANK WAS FOUND BROKEN. REPLACED ELBOW. 2 L 7 3 4F 4 F A3WE E2EA 1998040800013 19980408 00013 NM 1998 4 8 98UAL900070 1 19980217 A 2530 COFFEEMAKER BE AEROSPACE 3520001 BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE GALLEY DIRTY A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 9052U 19933 SMOKE IN AFT CABIN FROM AFT GALLEY AREA. IT APPEARS TO BE FROM COFFEEMAKER AREA. *S/D* FOUND COFFEE POT LID UNDER GAL LEY INBOARD COFFEEMAKER. REMOVED DEBRIS. APPLIED POWER TO AFT GALLEY. NO SMOKE/ODORS DETECTED, OK TO CONTINUE. 2 L 7 2 4F 4 F A16WE E2EA 1998040800014 19980408 00014 NM 1998 4 8 98UAL900072 1 19980218 A 5210 MECHANISM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PAX DOOR LACK OF LUBE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 305UA 23666 CABIN DOOR WARNING LIGHT ILLUMINATED. *S/D* CHECKED OPERATION OF DOOR 1L. CLEANED AND LUBED LATCH ROLLERS AND OPERATI NG MECHANISMS, DOOR OP CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998040800015 19980408 00015 NM 1998 4 8 98UAL900078 1 19980221 A 2750 285N0011 FSEU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 539UA 25223 FLIGHT CREW UNABLE TO FULLY EXTEND FLAPS. DIVERTED TO LAX. *S/D* FOUND FAULTY FSEU NUMBER 1. REPLACED FSEU AND OPERA TIONALLY CHECKED GOOD. 2 L 7 2 4F 4 F RT A2NM E17NE 1998040800017 19980408 00017 NM 1998 4 8 98UAL900080 1 19980218 A 7931 OIL LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE ILLUMINATED A UALA E ENGINE SHUTDOWN N FALSE WARNING NR NOT REPORTED 1 WP 29 304UA 23665 THE NUMBER ONE ENGINE LOW OIL PRESSURE LIGHT CAME ON. AFTER AWHILE, THE OIL PRESSURE STARTED TO DROP. THE NUMBER ONE E NGINE WAS SHUTDOWN. 2 L 7 2 4F 4 F RT A16WE E2GL 1998040800018 19980408 00018 EU 1998 4 8 98UAL900081 1 19980220 A 2910 HYD FLUID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST LOSS A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 411UA 464 CREW REPORTS, LOSS OF GREEN HYDRAULIC SYSTEM FLUID QUANTITY WITH ASSOCIATED ECAM MESSAGE RSVR LO AIR PRESSURE. 2 L 7 2 4F 4 F RT A28NM E40NE 1998040800019 19980408 00019 EU 1998 4 8 98UAL900082 1 19980221 A 2910 HYD FLUID AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST LOSS A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 411UA 464 AFTER DEPARTURE CREW REPORTS INDICATED LOSS OF GREEN HYDRAULIC SYSTEM FLUID QUANTITY WITHOUT ASSOCIATED ECAM MESSAGE. T WO HOURS LATER ECAM RSVR LO AIR PRESSURE MESSAGE RECEIVED AND FLT DIVERTED FOR PRECAUTIONARY LANDING. 2 L 7 2 4F 4 F RT A28NM E40NE 1998040800020 19980408 00020 NM 1998 4 8 98UAL900084 1 19980222 A 3350 LIGHT BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 611UA 21872 EMERGENCY EXIT LIGHTS DOOR 1L DAMAGED. REPLACED EEL LIGHT TRACK AND OP CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1998040800021 19980408 00021 NM 1998 4 8 98UAL900085 1 19980222 A 2530 5468AMOD COFFEEMAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 7278U 21425 FLIGHT ATTENDANT REPORTED WHITE SMOKE FROM FORWARD GALLEY. GALLEY POWER SECURED. DIVERTED TO SAV. *S/D* FORWARD COFF EEMAKER HAD A SHORT CIRCUIT AND POPPED A CIRCUIT BREAKER. REPLACED COFFEEMAKER AND CHECKED OPERATION. 2 L 7 3 4F 4 F A3WE E2EA 1998040800023 19980408 00023 NM 1998 4 8 98UAL900088 1 19980221 A 5270 387 BULB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CARGO DOOR MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 7284U 21562 ABORTED TAKEOFF AT 70 KNOTS DUE TO FORWARD CARGO DOOR LIGHT CAME ON. RETURNED TO GATE. *S/D* CARGO DOOR OPERATION CHE CKED AND NO DISCREPANCY WAS FOUND. WARNING LIGHT SOCKET WAS CLEANED AND RELAMPED. 2 L 7 3 4F 4 F A3WE E2EA 1998040800024 19980408 00024 NM 1998 4 8 98UAL900089 1 19980221 A 2750 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS MALFUNCTIONED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 7257U 21404 USING ALTERNATE SYSTEM, OUTBOARD FLAPS WOULD NOT EXCEED BEYOND 30 DEGREES, THEN WOULD NOT RETRACT LESS THAN 5 DEGREES. R ETURNED TO PAI. 2 L 7 3 4F 4 F A3WE E2EA 1998040800025 19980408 00025 NM 1998 4 8 98UAL900090 1 19980225 A 3840 7047M3 COMPRESSOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE WATER SYST CLOGGED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7452U 21906 CREW REPORTED AN ELECTRICAL ODOR. POTABLE WATER AIR COMPRESSOR CIRCUIT BREAKER POPPED AND WOULD NOT RESET. *S/D* WATE R SYSTEM AIR COMPRESSOR FAILED. REPLACED AIR COMPRESSOR. 2 L 7 3 4F 4 F A3WE E2EA 1998040800026 19980408 00026 WP 1998 4 8 98UAL900092 1 19980226 A 2130 PRESSURIZATION DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN MALFUNCTIONED A UALA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 1845U 48261 AFTER TAKEOFF, PRESSURIZATION DID NOT OPERATE IN AUTO. SELECTED SEMI-AUTO, OK TO FL340 THEN SEMI-AUTO FAILED. SELECTED STBY, OK FOR ONE HOUR. ON CLIMB TO FL360, CABIN DEPRESSURIZED. SELECTED MANUAL BUT UNABLE TO CONTROL PRESSURIZATION. DESCENDED TO 15,000 MSL, DUMPED FUEL AND RETURNED TO HNL. 2 L 7 3 4F 4 F A22WE E23EA 1998040800092 19980408 00092 WP 1998 4 8 DLL19980497 1 19980302 A 3350 RPS1 BATTERY PACK LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 756DR 193Y1185 EMERGENCY LIGHT BATTERY PACK DEAD. NO VOLTAGE OUTPUT. 2 L 7 3 4F A23WE 1998040800093 19980408 00093 WP 1998 4 8 DLL19980498 1 19980302 A 3350 BATTERY PACK 20131A LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 756DR 15 193Y1185 BATTERY PACK DEAD DUE TO PWR SUPPLY VOLTAGE INOP. 2 L 7 3 4F A23WE 1998040800094 19980408 00094 NM 1998 4 8 DL767980499 1 19980302 A 5754 114T4104 WEDGE BOEING 767 767232 1385132 NM NR 4 TE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 101DA 22213 THE LT WING NR 4 SLAT WAS FOUND WITH A 3 INCH DIAMETER AREA OF SKIN DELAMINATION. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364149-14AD. 2 L 7 2 4F RT A1NM 1998040800095 19980408 00095 NM 1998 4 8 DLM88980502 1 19980302 A 3320 SOCKET BV04055015 DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 902DE 53379 AIRCRAFT RETURN TO BLOCK WITH ELECTRICAL SMELL AND SMOKE FROM FIRST CLASS NUMBER 4 FLUORESCENT LIGHT ARCING. REPLACED B ULB HOLDER ASSY. 2 L 7 2 4F RT A6WE 1998040800096 19980408 00096 NM 1998 4 8 DLM88980504 1 19980302 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 911DL 49542 THE FUSELAGE SKIN WAS BADLY DENTED AT FS 237 BETWEEN STR 17L AND 18L. STRINGER 17L WAS CRACKED AND THE FS 237 FORMER WA S CRACKED AND BUCKLED. THE STRINGER AND FRAME WERE REPAIRED PER THE SRM. THE SKIN DAMAGE WAS CUTOUT AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER AND INTERNAL FATIGUE DOUBLER PER ER/A 364128-14. DAMAGE WAS CAUSED BY GROUND EQUIPMENT IMPACT. 2 L 7 2 4F RT A6WE 1998040800097 19980408 00097 NM 1998 4 8 DL72S980505 1 19980227 A 5330 6518420763 SKIN BOEING 727 727232 1384082 NM BS 345 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 THE FUSELAGE SKIN AND UNDERLYING DOUBLER AND BEAR STRAP WERE FOUND WITH A 3.5 INCH CRACK IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL DOUBLER AND TRIPLER PER ER/A 364131-14, REV A. 2 L 7 3 4F A3WE 1998040800099 19980408 00099 NM 1998 4 8 DL72S980510 1 19980218 A 5753 SKIN BOEING 727 727225 1384077 NM NR 1 TE MIDFLAP WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 DURING SHOP VISIT THE LEADING EDGE SKIN WAS FOUND WORN BEYOND LIMITS AT THE I/B END OF FLAP. THE SKIN WAS REPAIRED PER 727 MM 57-52-0, FIG 803 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998040800100 19980408 00100 NM 1998 4 8 DHL9872401C 1 19980206 A 7110 COWLING BOEING 727 727228 NM NR 2 ENGINE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 2 ENGINE LT FWD COWLING HAS HOLE GOUGED NEAR AFT LINE UP PIN RECEPTACLE. REPLACED SKIN PER SRM 51-40-2, 2 X 2. N/R 6910 2 L 7 3 4F A3WE 1998040800101 19980408 00101 NM 1998 4 8 DHL9872402C 1 19980206 A 5720 ANGLE BOEING 727 727228 NM WS 568 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT WING T/E PANEL UPPER SURFACE SUPPORT ANGLE I/B SIDE HAS INTERIM REPAIR CRACKED AT WS 568 . REPLACED T/E PANEL ATTACH BRACKET PER SRM 51-30-2, N/R 2346. 2 L 7 3 4F A3WE 1998040800102 19980408 00102 NM 1998 4 8 DHL9872403C 1 19980205 A 5755 65982963 ANGLE BOEING 727 727228 NM NR 8 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT WING NR 8 SPOILER UPPER SUPPORT BRACKET IS CRACKED, AFT BOTTOM AREA. ALSO, IN SAME BRACKET, OUTBD SIDE C RACKED AT TOP. REPLACED SUPPORT BRACKET AND ANGLE PER SRM 51-10-1, N/R 2333. 2 L 7 3 4F A3WE 1998040800103 19980408 00103 NM 1998 4 8 DHL9872404C 1 19980205 A 5712 RIB BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT WING RIB CHORD AT BL 70.5 HAS HFEC CRACK INDICATION, HFEC HOLE, OVERSIZED. HFEC INSTALLED ATTACH TEE P ER SRM 51-20-2, N/R 2288. 2 L 7 3 4F A3WE 1998040800104 19980408 00104 NM 1998 4 8 DHL9872405C 1 19980205 A 5720 BRACKET BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LEFT WING T/E CAVITY FOUND LOWER PANEL SUPPORT BRACKET CRACKED AND LOOSE BELOW NR 3 FLIGHT SPOILER. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-10-1, N/R 1049. 2 L 7 3 4F A3WE 1998040800105 19980408 00105 NM 1998 4 8 DHL9872406C 1 19980205 A 5720 CLIP BOEING 727 727228 NM NR 1 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 1 SLAT OUTBD TRACK TO SLAT LOWER SKIN ATTACH CLIP IS CRACKED AT RADIUS. REPLACED CLIP PER SRM 51-30-2, N/R 1070. 2 L 7 3 4F A3WE 1998040800106 19980408 00106 NM 1998 4 8 DHL9872407C 1 19980206 A 5720 CLIP BOEING 727 727228 NM NR 2 SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 2 SLAT O/B TRACK TO SLAT LOWER SKIN ATTCH CLIP IS CRACKED. REPLACED SLIP PER SRM 51-30-2, N/R 1076. 2 L 7 3 4F A3WE 1998040800107 19980408 00107 NM 1998 4 8 DHL9872408C 1 19980206 A 5754 SKIN BOEING 727 727228 NM NR 4 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 4 SLAT LOWER SKIN IS CRACKED AT CUTOUT FOR O/B UP STOP PAD. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLE R AND INSTALLED PER SRM 51-40-2, 6 X 4.5. N/R 1086. 2 L 7 3 4F A3WE 1998040800108 19980408 00108 NM 1998 4 8 DHL9872409C 1 19980206 A 5720 652165828 ANGLE BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LT WING LOWER TRAILING EDGE COVE PANEL SUPPORT ANGLES ARE CRACKED. REMOVED AND REPLACED SUPPORT ANGLES PER SRM 51-10-1. 2 L 7 3 4F A3WE 1998040800109 19980408 00109 NM 1998 4 8 DHL9872410C 1 19980206 A 5720 WEB BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LEFT WING FIXED LEADING EDGE INTERIOR VERTICAL WEB AT WBL 92.8 CRACKED AT ATTACH FASTENERS AT AFT END. STOP DRILL, HFEC STOP DRILL. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 15 X 3. N/R 1093. 2 L 7 3 4F A3WE 1998040800110 19980408 00110 NM 1998 4 8 DHL9872411C 1 19980206 A 5720 ANGLE BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LEFT WING LOWER TRAILING EDGE COVE PANEL I/B SUPPORT ANGLE CRACKED AT ATTACH BOLTS. REPLACED LEFT WING ATT ACH BRACKET PER SRM 51-30-2. N/R 1121. 2 L 7 3 4F A3WE 1998040800111 19980408 00111 NM 1998 4 8 DHL9872412C 1 19980208 A 5330 SKIN BOEING 727 727228 NM BS 1318 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, AFT AIRSTAIR WELL CRACK AT LIGHTENING HOLE BS 1318 LEFT TORQUE BOX. STOP DRILL CRACK, INSTALLED DOUBLER REP AIR PER SRM 51-40-2, 5 X 4. N/R 3682. 2 L 7 3 4F A3WE 1998040800112 19980408 00112 NM 1998 4 8 DHL9872413C 1 19980208 A 5321 FLOOR PANELS BOEING 727 727228 NM BS 1030 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, FLOORBOARD NR 105 CRACKED AND DELAMINATING BS 1030 TO 1070 LBL 24 TO 45. REMOVED CABIN FLOOR PANELS AND REP LACED PER SRM 51-10-1, 8 X 32 AND 10 X 32. N/R 3680. 2 L 7 3 4F A3WE 1998040800113 19980408 00113 NM 1998 4 8 DHL9872414C 1 19980207 A 5313 STRINGER BOEING 727 727228 NM BS 950-970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CORROSION AT STRINGER 27L, BS 950 TO 970, IN AFT BAG BIN. CUT OUT DAMAGED AREA, INSTALLED NEW STRINGER FROM STA 950 TO 970 PER SRM 53-10-3, 45 LONG. N/R 3673. 2 L 7 3 4F A3WE 1998040800114 19980408 00114 NM 1998 4 8 DHL9872415C 1 19980207 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 1050 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, SEAT TRACK CORRODED AT BS 1050 LB 45. CUT OUT CORRODED SECTION, INSTALLED SEAT TRACK PER SRM 53-10-5. N/R 3672. 2 L 7 3 4F A3WE 1998040800115 19980408 00115 NM 1998 4 8 DHL9872416C 1 19980207 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1050 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, SEAT TRACK CORRODED AT RBL 45, BS 1050. CUT OUT DAMAGED SECTION FROM 1030 TO 1070 PER SRM 53-10-5, AND REP LACED PER THE SAME. N/R 3671. 2 L 7 3 4F A3WE 1998040800116 19980408 00116 NM 1998 4 8 DHL9872417C 1 19980207 A 5320 SUPPORT BOEING 727 727228 NM BS 620 CHANNEL A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, FWD BAGGAGE COMPARTMENT STA 620 FLOOR LEVEL SUPPORT CHANNEL 6TH FROM LEFT CENTER SKIN CRACKED. STOP DRILLED , INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 4 X 2. N/R 3658. 2 L 7 3 4F A3WE 1998040800117 19980408 00117 NM 1998 4 8 DHL9872418C 1 19980206 A 5311 FRAME BOEING 727 727228 NM BS 1030 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LEFT SIDE AFT BAGGAGE COMPT STA 1030 ABOVE STRINGER 26 FRAME CRACKED. CUT OUT DAMAGED AREA, INSTALLED DOUBL ER REPAIR PER SRM 53-10-4, 10 X 5. N/R 3626. 2 L 7 3 4F A3WE 1998040800118 19980408 00118 NM 1998 4 8 DHL9872419C 1 19980206 A 5320 RIB BOEING 727 727228 NM LT AC BAY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LEFT A/C BAY FWD PANEL SUPPORT RIB CORRODED THROUGH. REPLACED DAMAGED SECTION OF LEFT A/C BAY SUPPORT RIB P ER SRM 51-40-3, 2' X 3 X 1. N/R 3575. 2 L 7 3 4F A3WE 1998040800119 19980408 00119 NM 1998 4 8 DHL9872420C 1 19980205 A 5330 SKIN BOEING 727 727228 NM BS 420 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, FS SKIN AT STA 420 STR 24L DENTED. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 14 X 17. N/R 3487. 2 L 7 3 4F A3WE 1998040800120 19980408 00120 NM 1998 4 8 DHL9872421C 1 19980205 A 5330 SKIN BOEING 727 727228 NM BS 423 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, SKIN DENTED AT STA 423 BETWEEN STR 23L AND 24L. CUT OUT DAMAGED SECTION, INSTALLED DOUBLER PER SRM 53-30-3 . DOUBLER 14 X 17, FILLER 1 X 1. N/R 3476. 2 L 7 3 4F A3WE 1998040800121 19980408 00121 NM 1998 4 8 DHL9872422C 1 19980205 A 5320 FAIRING BOEING 727 727228 NM CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, AFT CARGO FWD DOOR CUTOUT AFT CENTER AREA FAIRING LOWER CORNER TORN. INSTALLED OVERLAY REPAIR PER SRM 51-40 -8. N/R 3468. 2 L 7 3 4F A3WE 1998040800122 19980408 00122 NM 1998 4 8 DHL9872423C 1 19980205 A 5320 FRAME BOEING 727 727228 NM NR 2 CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 2 CARGO DOOR FRAME CRACKED AT BS 990 FRAME BETWEEN STR 26R AND STR 27R. REMOVED FASTENERS, CUT OUT DAMAG ED SECTION AND INSTALLED REPAIR DOUBLER PER S/B 53A0199, 5 X 12. N/R 3458. 2 L 7 3 4F A3WE 1998040800123 19980408 00123 NM 1998 4 8 DHL9872424C 1 19980204 A 5330 SKIN BOEING 727 727228 NM BS 264 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, DENT AT STR 24R BA 264R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 13 X 7.5. N/R 342 5. 2 L 7 3 4F A3WE 1998040800124 19980408 00124 NM 1998 4 8 DHL9872425C 1 19980204 A 5330 SKIN BOEING 727 727228 NM BS 259 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, DENT AT BS 259R AT STR 24R. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-10-2, 13 X 7.5. N /R 3424. 2 L 7 3 4F A3WE 1998040800125 19980408 00125 NM 1998 4 8 DHL9872426C 1 19980207 A 5311 FRAME BOEING 727 727228 NM BS 1070 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CIRCUMFERENTIAL CRACKED AT BS 1070 STR 27L, TOP FLANGE. CUT OUT DAMAGED SECTION AND INSTALLED DOUBLER REPAI R PER SRM 53-10-4, DOUBLER 6 X 11. N/R 3650. 2 L 7 3 4F A3WE 1998040800126 19980408 00126 NM 1998 4 8 DHL9872427C 1 19980206 A 5320 ANGLE BOEING 727 727228 NM BS 1342 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, AFT AIRSTAIR STA 1342 RIGHT SIDED UNDER HYD VALVE ANGLE BRACKET CRACKED. REMOVED AND REPLACED ANGLE SUPPORT BRACKET PER SRM 51-10-1, 1.25 X 1.25 X 6. N/R 4043. 2 L 7 3 4F A3WE 1998040800127 19980408 00127 NM 1998 4 8 DHL9872428C 1 19980206 A 5720 TIP BOEING 727 727228 NM RT WING ERODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT STAB TIP FAIRING ERODED AT LEADING EDGE. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 4 X 6. N/R 4019. 2 L 7 3 4F A3WE 1998040800128 19980408 00128 NM 1998 4 8 DHL9872429C 1 19980204 A 5320 SIDE RAIL BOEING 727 727228 NM BS 530 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, MAIN CABIN RT SIDE RAIL AT BS 530 IS HEAVILY GOUGED. STOP DRILLED AND INSTALLED DOUBLER REPAIR PER SRM 51-4 0-2, 4.5 X 2.5. N/R 5039. 2 L 7 3 4F A3WE 1998040800129 19980408 00129 NM 1998 4 8 DHL9872430C 1 19980207 A 5320 CHANNEL BOEING 727 727228 NM BS 1150 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CABIN FLOOR STRUCTURE STA 1150, 25 RBL HAT CHANNEL BROKEN OFF. REPLACED HAT CHANNEL METAL STRAP PER SRM 51- 40-2, 11 X 7. N/R 5122. 2 L 7 3 4F A3WE 1998040800130 19980408 00130 NM 1998 4 8 DHL9872431C 1 19980208 A 5320 CHANNEL BOEING 727 727228 NM BS 1136 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CABIN FLOOR WL 208 STA 1136 ANGLE CHANNEL 25 FROM CENTER RIGHT TO 65 CENTER CORRODED. REMOVED AND REPLACED HAT CHANNEL PER SRM 51-10-1, N/R 5113. 2 L 7 3 4F A3WE 1998040800131 19980408 00131 NM 1998 4 8 DHL9872432C 1 19980206 A 5320 BRACKET BOEING 727 727228 NM BS 740 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CABIN FLOOR CENTER SEAT TRACK SUPPORT BRACKET CRACKED AT BS 740 BL 0. REPLACED SUPPORT BRACKET PER SRM 51-3 0-2. N/R 5111. 2 L 7 3 4F A3WE 1998040800132 19980408 00132 NM 1998 4 8 DHL9872433C 1 19980206 A 5320 CHANNEL BOEING 727 727228 NM BS 1136 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CABIN INTERIOR STA 1136 WL 208.1 25 LEFT OF CENTER, CHANNEL CORRODED. CUT OUT DAMAGED SECTION, 16 X 16 FROM 1130 TO 1150 LBL 24 AND INSTALLED PER SRM 51-10-2. N/R 5112. 2 L 7 3 4F A3WE 1998040800133 19980408 00133 NM 1998 4 8 DHL9872434C 1 19980206 A 7110 COWLING BOEING 727 727228 NM NR 2 ENGINE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 2 ENGINE LT FWD COWLING LOWER AFT CORNER GOUGED. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 54-10-3, 7 X 2.75. N/R 6908. 2 L 7 3 4F A3WE 1998040800134 19980408 00134 NM 1998 4 8 DHL9872435C 1 19980206 A 7110 COWLING BOEING 727 727228 NM NR 2 ENGINE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 2 ENGINE RT FWD COWLING LOWER AFT CORNER GOUGED. REPLACED SECTION PER SRM 51-40-3, 5 X 3. N/R 6896. 2 L 7 3 4F A3WE 1998040800135 19980408 00135 NM 1998 4 8 DHL9872436C 1 19980206 A 7110 COWLING BOEING 727 727228 NM NR 2 ENGINE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT CHECK, NR 2 ENGINE LT AFT COWLING SKIN BENT AT UPPER AFT CORNER. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR P ER SRM 54-10-3, 3.5 X 4. N/R 6895. 2 L 7 3 4F A3WE 1998040800136 19980408 00136 NM 1998 4 8 DHL9872437C 1 19980206 A 7110 COWLING BOEING 727 727228 NM NR 1 ENGINE CRACKED A A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 1 ENG TOP COWLING AFT EDGE WITH PIECE MISSING. REPAIRED PER SRM 51-40-3, 6 X 7.25. N/R 6869. 2 L 7 3 4F A3WE 1998040800137 19980408 00137 NM 1998 4 8 DHL9872438C 1 19980205 A 7110 COWLING BOEING 727 727228 NM NR 3 ENGINE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 3 LOWER ENGINE COWLING EXTERIOR CTR SECTION PREVIOUS REPAIR COMING OFF. CUT OUT DAMAGED AREA AND INSTAL LED DOUBLER REPAIR PER SRM 54-10-3, 8 X 4'. N/R 6858. 2 L 7 3 4F A3WE 1998040800138 19980408 00138 NM 1998 4 8 DHL9872439C 1 19980205 A 7110 COWLING BOEING 727 727228 NM NR 3 ENGINE SKIN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, 33 ENGINE UPPER COWLING CTR LATCH OUTER SKIN DAMAGED. STOP DRILLED, INSTALLED DOUBLER REPAIR PER SRM 51-40- 2, 2.5 X 1.125. N/R 6856. 2 L 7 3 4F A3WE 1998040800139 19980408 00139 NM 1998 4 8 DHL9872440C 1 19980116 A 5712 RIB BOEING 727 727228 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, 1 CRACK NOTED AT UPPER FLANGE AT RIB 13. STOP DRILLED CRACK, HFEC STOP DRILL, INSTALLED RIB REPAIR AT WS 60 1.5 PER SRM 57-10-5, 16 X 2 X 1. N/R 2257. 2 L 7 3 4F A3WE 1998040800140 19980408 00140 NM 1998 4 8 DHL9872441C 1 19980205 A 5720 STIFFENER BOEING 727 727228 NM WS 304 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT L/E WING STIFFENER CRACKED AT WS 304 I/B SIDE JUST ABOVE L/E FLAP ACTUATOR. CUT OUT DAMAGED AREA, INSTAL LED DOUBLER PER SRM 57-30-4, 3 X 3. N/R 2309. 2 L 7 3 4F A3WE 1998040800141 19980408 00141 NM 1998 4 8 DHL9872442C 1 19980206 A 5753 SKIN BOEING 727 727228 NM RT TE FOREFLAP CHAFFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT O/B FOREFLAP UPPER SURFACE HAS SIGNS OF CHAFING IN TWO PLACES. INSTALLED FILLER REPAIR PER SRM 51-40-1, 3 X 8 AND 4 X 5. N/R 2355. 2 L 7 3 4F A3WE 1998040800142 19980408 00142 NM 1998 4 8 DHL9872443C 1 19980207 A 5753 FLAP BOEING 727 727228 NM NR 5 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT NR 5 FLAP TRACK FAIRING IS CRACKED AT FWD END LOWER SURFACE. STOP DRILLED CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, DOUBLER 4.5 X 7. N/R 2365. 2 L 7 3 4F A3WE 1998040800143 19980408 00143 NM 1998 4 8 DHL9872444C 1 19980207 A 5753 FAIRING BOEING 727 727228 NM NR 5 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT MLG NR 5 FLAP FAIRING INNER SKIN FWD DOOR UPPER SIDE CRACKED. REMOVED CRACKED SKIN, INSTALLED NEW SKIN P ER SRM 51-40-2, 4.5 X 1.5. N/R 2377. 2 L 7 3 4F A3WE 1998040800144 19980408 00144 NM 1998 4 8 DHL9872445C 1 19980211 A 5754 TRACK BOEING 727 727228 NM NR 6LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CRACK AT R/W L/E AT NR 6 I/B TRACK. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 57-30-4, 3 X 6, FILLER 1 X 1.5. N/R 2383. 2 L 7 3 4F A3WE 1998040800145 19980408 00145 NM 1998 4 8 DHL9872446C 1 19980205 A 5312 BULKHEAD BOEING 727 727228 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, 1183 BULKHEAD RT FWD SIDE WL 237.1 I/B AND O/B SIDES OF VERTICAL STIFFENER CRACKED 37 RIGHT OF CENTER. STOP DRILL, HFEC, INSTALLED REPAIR PER S/B 53-0192, AND SRM 51-30-2. N/R 3499. 2 L 7 3 4F A3WE 1998040800146 19980408 00146 NM 1998 4 8 DHL9872447C 1 19980208 A 5320 TORQUE BOX BOEING 727 727228 NM BS 1318 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, AFT AIRSTAIR WELL, CRACK AT LIGHTENING HOLE RIGHT TORQUE BOX BS 1318. STOP DRILL CRACK, INSTALLED DOUBLER R EPAIR PER SRM 51-40-2, 5 X 4. N/R 3679. 2 L 7 3 4F A3WE 1998040800147 19980408 00147 NM 1998 4 8 DHL9872448C 1 19980206 A 5315 FLOORBEAM BOEING 727 727228 NM BS 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, EXFOLIATION CORROSION AT FLOORBEAM UPPER CHORD LEFT END OF FLOORBEAM BS 600. CUT OUT DAMAGED AREA, INSTALL ED REPAIR PER PEMCO LETTER 98-0010 1 X 5. N/R 3628. 2 L 7 3 4F A3WE 1998040800148 19980408 00148 NM 1998 4 8 DHL9872449C 1 19980205 A 5320 STOP BOEING 727 727228 NM AFT EMER EXIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LT AFT EMERGENCY EXIT CUTOUT TOP STOP CRACKED. REPLACED STOP PADS PER SRM 51-10-1. N/R 3531. 2 L 7 3 4F A3WE 1998040800149 19980408 00149 NM 1998 4 8 DHL9872450C 1 19980205 A 5320 STOP PAD BOEING 727 727228 NM RT EMER EXIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CABIN RT AFT EMERGENCY EXIT CUTOUT FORWARD BOTTOM STOP CRACKED. REPLACED STOP PAD PER SRM 51-10-1. N/R 353 2. 2 L 7 3 4F A3WE 1998040800150 19980408 00150 NM 1998 4 8 DHL9872451C 1 19980206 A 5753 FAIRING BOEING 727 727228 NM NR 8 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 8 FLAP TRACK HINGED FAIRING HAVE BOTH TRACKS CRACKED. REMOVED AND REPLACED FAIRING PER MM 27-51-11. N/R 2363. 2 L 7 3 4F A3WE 1998040800151 19980408 00151 NM 1998 4 8 DHL9872452C 1 19980205 A 2782 BRACKET BOEING 727 727228 NM NR 6 LE FLAP ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT NR 6 L/E FLAP ACTUATOR MOUNT BRACKET LOWER I/B AREA CRACKED AT WS 304. INSTALLED FABRICATED ANGLE BRACKE T PER SRM 51-40-3, 6 X 6. N/R 2310. 2 L 7 3 4F A3WE 1998040800152 19980408 00152 NM 1998 4 8 DHL9872453C 1 19980213 A 5753 FLAP BOEING 727 727228 NM RT TE MIDFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, RT O/B MIDFLAP DELAMINATED AT O/B T/E CORNER. INSTALLED BONDING REPAIR PER SRM 51-40-6, 3 X 20.5. N/R 2385 . 2 L 7 3 4F A3WE 1998040800153 19980408 00153 NM 1998 4 8 DHL9872454C 1 19980116 A 5712 RIB BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CRACK IN UPPER FLANGE OF RIB 13, R/W. STOP DRILL CRACK, HFEC, INSTALLED RIB REPAIR PER SRM 57-10-5. REPAIR 16 X 2 X 1. N/R 2257. 2 L 7 3 4F A3WE 1998040800154 19980408 00154 NM 1998 4 8 DHL9872455C 1 19980205 A 5753 SKIN BOEING 727 727228 NM LT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LEFT O/B FLAP ASSY UPPER SURFACE DELAMINATED 8 INCHES FROM O/B END, 10 FROM TRAILING EDGE. INSTALLED BONDI NG REPAIR PER SRM 51-40-6, 4 X 4. N/R 1063. 2 L 7 3 4F A3WE 1998040800155 19980408 00155 NM 1998 4 8 DHL9872456C 1 19980206 A 5720 ANGLE BOEING 727 727228 NM WS 130 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LT WING FIXED LEADING EDGE INTERIOR, LOWER SUPPORT ANGLE AT STA 130 IS CRACKED AT ATTACH HOLES. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 51-10-1, 20 X 3. N/R 1089. 2 L 7 3 4F A3WE 1998040800156 19980408 00156 NM 1998 4 8 DHL9872457C 1 19980206 A 2782 BRACKET BOEING 727 727228 NM NR 1 LE SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 1 SLAT ACTUATOR, I/B AND O/B MOUNT BRACKETS AT FRONT SPAR ARE CRACKED AT ATTACH POINTS. REMOVED CRACKED PARTS, FABRICATED REPAIR PARTS AND INSTALLED PER S/B 57-0130 AND INSTALLED REPAIR DOUBLERS PER S/B 4 X 8 AND 16 X 12. N /R 1072. 2 L 7 3 4F A3WE 1998040800157 19980408 00157 NM 1998 4 8 DHL9872458C 1 19980206 A 5754 ANGLE BOEING 727 727228 NM NR 3 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, NR 3 SLAT ACTUATOR DOOR, I/B ATTACH ANGLE ON THE UPPER SIDE CRACKED AT FWD FASTENER. REPLACED ANGLE PER SRM 51-30-2. N/R 1081. 2 L 7 3 4F A3WE 1998040800158 19980408 00158 NM 1998 4 8 DHL9872459C 1 19980114 A 5712 RIB BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, LEFT WING RIB CHORD BL 70.5 HAS CRACK INDICATION AT FWD UPPER AND FWD LOWER HOLES. HFEC, CRACK VERIFIED. S TOP DRILLED CRACK, HFEC, INSTALLED REPAIR PER S/B 57-0211. N/R 1030/1143. 2 L 7 3 4F A3WE 1998040800159 19980408 00159 NM 1998 4 8 DHL9872460C 1 19980210 A 5320 WEB BOEING 727 727228 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, PRESSURE WEB CRACK IN NOSE WW LEFT SIDE WALL. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER S/B 53-0145 AND S RM 51-30-2, 60 X 20. N/R 7821. 2 L 7 3 4F A3WE 1998040800160 19980408 00160 NM 1998 4 8 DHL9872461C 1 19980210 A 5320 WEB BOEING 727 727228 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, PRESSURE WEB CRACK IN NOSE WW. ROUTED OUT CRACK, HFEC, AND INSTALLED DOUBLER PER S/B 53-0145 AND SRM 51-40 -2, 18 X 24. N/R 7826. 2 L 7 3 4F A3WE 1998040800161 19980408 00161 NM 1998 4 8 DHL9872462C 1 19980210 A 5320 WEB BOEING 727 727228 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, PRESSURE WEB CRACK IN NOSE WW LEFT SIDE WALL JUST BELOW FWD ACCESS PANEL. CUT OUT DAMAGED AREA, INSTALLED D OUBLER REPAIR PER S/B 53-0145, 57 X 15. N/R 7822. 2 L 7 3 4F A3WE 1998040800162 19980408 00162 NM 1998 4 8 DHL9872463C 1 19980210 A 5320 WEB BOEING 727 727228 NM NLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, PRESSURE WEB IN NOSE WW LEFT SIDE CRACKED BELOW BELLCRANK. CUT OUT DAMAGED AREA, REMOVED EXISTING DOUBLER, HFEC INSTALLED DOUBLER PER SRM 51-30-2, 60 X 20. N/R 7820. 2 L 7 3 4F A3WE 1998040800163 19980408 00163 NM 1998 4 8 DHL9872464C 1 19980205 A 5741 BOTTLE PIN BOEING 727 727228 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CORROSIN BLEEDING FROM RT WING SPAR TO BODY FITTING. REMOVED CORROSION, BLENDED OUT FACE OF FITTING. FLAP PEENED FITTING, INSTALLED BUSHING AND INSTALLED BOTTLE PIN PER AVITAS EO PMSI191R0-3. N/R 7815. 2 L 7 3 4F A3WE 1998040800164 19980408 00164 NM 1998 4 8 DHL9872465C 1 19980205 A 7110 COWL BOEING 727 727228 NM NR 3 ENGINE TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, METAL TORN ON TOP FIXED COWL AT FWD ENGINE MOUNT. REPLACED SKIN PER SRM 51-30-2, 25 X 6. N/R 6835. 2 L 7 3 4F A3WE 1998040800165 19980408 00165 NM 1998 4 8 DHL9872466C 1 19980205 A 7110 COWL BOEING 727 727228 NM NR 3 ENGINE WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, 33 ENGINE HOLE WORN THROUGH FWD FIXED COWL AFT FLANGE. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR AT IN SIDE CHANNEL 6 X 6, FILLER 3 X 4. INSTALLED DOUBLER IN EXTERNAL SKIN PER SRM 54-30-1 DOUBLER 4 X 6, FILLER 1 X 2. N/R 6834. 2 L 7 3 4F A3WE 1998040800166 19980408 00166 NM 1998 4 8 DHL9872467C 1 19980220 A 5230 FRAME BOEING 727 727228 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, C-3 CARGO DOOR HAS CRACK IN LOWER FORWARD FRAME. STOP DRILLED CRACK, PERFORM HFEC, ACCOMPLISHED REPAIR PER AVITAS EO 98PMSI191D-2. N/R 4049. 2 L 7 3 4F A3WE 1998040800167 19980408 00167 NM 1998 4 8 DHL9872468C 1 19980220 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 660 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, FOUND HEAVY CORROSION ON FLOOR TRACK FLANGES AT STA 660, BL 0 TO 24L. CUT OUT DAMAGED SECTION, INSTALLED SE AT TRACK REPAIR PER SRM 53-10-5, 10.5 LONG. N/R 5157. 2 L 7 3 4F A3WE 1998040800168 19980408 00168 NM 1998 4 8 DHL9872469C 1 19980215 A 5347 BAC15201434 SEAT TRACK BOEING 727 727228 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, SEAT TRACK FLANGE CORRODED AT LBL 45 BETWEEN STA 560 AND 620. CUT OUT CORRODED AREA STA 560 TO 580. INSTA LLED NEW SECTION PER SRM 53-10-5. N/R 5143. 2 L 7 3 4F A3WE 1998040800169 19980408 00169 NM 1998 4 8 DHL9872470C 1 19980204 A 5711 SPAR BOEING 727 727228 NM WS 399 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 724DH 19862 AT C-CHECK, CORROSION ON LEFT WING FRONT SPAR LOWER CHORD O/B FLANGE UPPER SURFACE WS 399. REMOVED CORROSION, INSTALLE D CHORD REPAIR PER AVITAS EO 98PMSI191D-1, 13 X 2.75. N/R 1024. 2 L 7 3 4F A3WE 1998040800170 19980408 00170 NM 1998 4 8 CKSA98034 1 19980224 A 5753 FRAME BOEING 747 747146 NM LT TE MIDFLAP DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, TOP OF L/E JUST O/B OF O/B CARRIAGE PILLOWING. REMOVED DAMAGED UPPER ST RAP (FRAME ASSY) IAW B747 SRM 51-30-02. INSTALLED NEW FRAME ASSY IAW B747 SRM 51-30-02. REPAIR ACCOMPLISHED USING B747 SRM 51-10-1 (REPLACEMENT OF PARTS). CORROSION TASK CARD NUMBER C57-560-10 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 0 03739. 2 L 7 4 4F A20WE 1998040800171 19980408 00171 NM 1998 4 8 CKSA98035 1 19980224 A 5720 T-CHORD BOEING 747 747146 NM WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, I/B CARRIAGE FWD ACCESS HOLE AFT EDGE CORRODED BETWEEN NUT PLATES AND T- CHORD. REPAIRED CORROSION DAMAGE TO T-CHORD IAW AIA EDR NR B4-05552 DATED 11-21-97. CORROSION TASK CARD NUMBER C57-560 -10 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 003741. 2 L 7 4 4F A20WE 1998040800172 19980408 00172 NM 1998 4 8 CKSA98036 1 19980224 A 5311 FRAME BOEING 747 747146 NM BS 520 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LFT SIDEWALL AREA, BS 520, FRAME CRACKED ALONG PREVIOUS DOUBLER REPAIR (REFERENCE: BETWEEN S31L AND S32L AREA). REMOVED PREVIOUS DOUBLER IAW B747 SRM 51-30-02. PERFORMED HFEC ON WEB PER BOEING SRM 53-10-04 END OF CRACK VERIFIED AND MARKED. VERIFIED CRACK CONTAINED AFTER STOP DRILL. REPAIRED IAW SRM 53-10-04. CORROSION TASK C ARD NUMBER C53-110-01 PART 2 OF 5. NON-ROUTINE TASK CARD NUMBER 12511. 2 L 7 4 4F A20WE 1998040800173 19980408 00173 NM 1998 4 8 CKSA98037 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 1000 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, CRACK ON SEAT TRACK VERT FLANGE AT BS 1000 LBL 11.33. VERIFIED END OF C RACK WITH EDDY CURRENT. STOP DRILL END OF CRACK USING NR 10 DRILL BIT. INSTALLED REPAIR PARTS IAW DWG AIA/E/2731. COR ROSION TASK CARD NUMBER C53-210-05. NON-ROUTINE TASK CARD NUMBER 12540. 2 L 7 4 4F A20WE 1998040800174 19980408 00174 NM 1998 4 8 CKSA98038 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 1020 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION IN SEAT TRACK BS 1020 LBL 11.33. REMOVED AND REPLACED SEAT T RACK BS 1020 LBL 11.33 IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05 PART 1 OF 1. NON-ROUTINE TASK CARD NUMBER 12541. 2 L 7 4 4F A20WE 1998040800175 19980408 00175 NM 1998 4 8 CKSA98039 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 1140-1160 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON SEAT TRACK BS 1140 TO 1160 LBL 11.33. REMOVED AND REPLACE D SEAT TRACK FS 1140 TO 1160 AND LBL 11.33 IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05 PART 1 OF 1. N ON-ROUTINE TASK CARD NUMBER 12571. 2 L 7 4 4F A20WE 1998040800176 19980408 00176 NM 1998 4 8 CKSA98040 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 1180-1265 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON SEAT TRACK AND FLOOR SUPPORT FLANGES FROM BS 1180 TO 1265 LBL 11.33. REMOVED AND REPLACED SEAT TRACK FS 1180 TO 1265 LBL 11.33 IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05 PART 1 OF 1. NON-ROUTINE TASK CARD NUMBER 12572. 2 L 7 4 4F A20WE 1998040800177 19980408 00177 NM 1998 4 8 CKSA98041 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 1160-1265 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION, FOUND CORROSION ON SEAT TRACK AND FLOOR SUPPORT FLANGES FROM BS 1160 TO 1265 RBL 11.33. REMOVED DAMAGED AREA AT BS 1265 RBL 11.33 AND FABRICATED PARTS IAW AIA/E/2732. INSTALLED SEAT TRACK IAW AIA/E/SKETCH 2732. CO RROSION TASK CARD NUMBER C53-210-05 PART 1 OF 1. NON-ROUTINE TASK CARD NUMBER 12573. 2 L 7 4 4F A20WE 1998040800178 19980408 00178 NM 1998 4 8 CKSA98042 1 19980224 A 5320 INTERCOSTAL BOEING 747 747146 NM BS 1700 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON INTERCOSTAL WEB AFT OF BS 1700 AT S-30L. CORROSION OUT OF LIMITS IAW B747 SRM 53-10-1. INSTALLED REPAIR IAW B747 SRM 51-40-2. CORROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5 . NON-ROUTINE TASK CARD NUMBER 12579. 2 L 7 4 4F A20WE 1998040800179 19980408 00179 NM 1998 4 8 CKSA98043 1 19980224 A 5730 SKIN BOEING 747 747146 NM LT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, LT OVERWING SKIN AT WBL 128.45 HAS A 4 X 4 AREA OF CORROSION 2 FT 4 FWD OF MID SPAR. REMOVED CORROSION IAW B747 SRM 51-10-1. ULTRASONIC THICKNESS CHECK, MINIMUM NOMINAL THICKNESS .335 TO .34 0 IN 2 BY 2.5 AREA APPROX. REMOVED AND REPLACED BOLTS IAW B747 SRM 51-30-02 AND 51-30-04. REWORKED IAW EA B4-57-021. C ORROSION TASK CARD NUMBER C53-190-01 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 12598. 2 L 7 4 4F A20WE 1998040800180 19980408 00180 NM 1998 4 8 CKSA98044 1 19980224 A 5730 SKIN BOEING 747 747146 NM LT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, LT OVERWING SKIN AT WBL 128.45 HAS A 4 X 4 AREA OF CORROSION 2 FT FWD OF MID SPAR. REMOVED CORROSION IAW B747 SRM 51-10-1. ULTRASONIC THICKNESS CHECK, MINIMUM NOMINAL THICKNESS AT WING SKIN EDGE .195 TO .230 IN 2.5 BY 3 AREA APPROX. REMOVED AND REPLACED BOLTS IAW B747 51-30-02 AND 51-30-04. REWORKED IAW EA B4-57-021. CORROSION TASK CARD NUMBER C53-190-01 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 12599. 2 L 7 4 4F A20WE 1998040800181 19980408 00181 NM 1998 4 8 CKSA98045 1 19980224 A 5330 SKIN BOEING 747 747146 NM BS 1850 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON INTERNAL SKIN AT UPPER FWD CORNER OF C-2 DOOR CUTOUT BS 18 50. REMOVED CORROSION IAW B747 SRM 51-10-1. PERFORMED ULTRASONIC THICKNESS CHECK, MINIMUM NOMINAL THICKNESS .135. CORR OSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-30-01. INSTALLED REPAIR PARTS PER B747 SRM 51-30-02 AND AIA/E/2735. CO RROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5. NON-ROUTINE TASK CARD NUMBER 12735. 2 L 7 4 4F A20WE 1998040800182 19980408 00182 NM 1998 4 8 CKSA98046 1 19980224 A 5320 ANGLE BOEING 747 747146 NM BS 1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON ANGLES AND STRAPS ATTACHED TO TOP OF FRAME AT BS 1920 ABOV E S-41R. CORROSION ON ANGLES - 65B04866-2 AND 65B01856-80 OUT OF LIMITS IAW B747 SRM 53-10-1. REMOVED AND INSTALLED AN GLES IAW B747 SRM 51-30-2. CORROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5. NON-ROUTINE TASK CARD NUMBER 12736. 2 L 7 4 4F A20WE 1998040800183 19980408 00183 NM 1998 4 8 CKSA98047 1 19980224 A 5320 ANGLE BOEING 747 747146 NM FUSELAGE CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, LITE SURFACE CORROSION AFT OF NR 2 DME. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED AND REPLACED ATTACH ANGLE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-190-01 PART 2 OF 2. NON-ROUTINE TASK CARD NUMBER 12747. 2 L 7 4 4F A20WE 1998040800184 19980408 00184 NM 1998 4 8 CKSA98048 1 19980224 A 5720 BRACKET BOEING 747 747146 NM RT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, RT WING FWD FILLET RIB FS 840 BETWEEN STRINGER 47R AND 47L MOUNT BRACKET S HAVE CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED A ND REPLACED MOUNT BRACKET IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-190-01 PART 2 OF 2. NON-R OUTINE TASK CARD NUMBER 12748. 2 L 7 4 4F A20WE 1998040800185 19980408 00185 NM 1998 4 8 CKSA98049 1 19980224 A 5320 STIFFENER BOEING 747 747146 NM BS 1480 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 1480 AFT SIDE WEB LWR STIFFENER AT LBL 97 CORRODED FILLET AREA. REMO VED CORROSION IAW B747 SRM 51-10-01 FOUND OUT OF LIMIT. REMOVED AND REPLACED CORRODED STIFFENER IAW B747 SRM 51-10-01 A ND 51-30-02. CORROSION TASK CARD NUMBER C53-190-01 PART 1 OF 2. NON-ROUTINE TASK CARD NUMBER 12766. 2 L 7 4 4F A20WE 1998040800186 19980408 00186 NM 1998 4 8 CKSA98050 1 19980224 A 5320 DOUBLER BOEING 747 747146 NM BS 1480 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 1480 AFT WEB DOUBLER CORRODED LBL 97. REMOVED CORROSION IAW B747 SRM 51-10-01, FOUND OUT OF LIMIT. REMOVED AND REPLACED WEB DOUBLER IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CAR D NUMBER C53-190-01. NON-ROUTINE TASK CARD NUMBER 12767. 2 L 7 4 4F A20WE 1998040800187 19980408 00187 NM 1998 4 8 CKSA98051 1 19980224 A 5712 RIB BOEING 747 747146 NM WS 1010 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON RT WING RIB STA 1010 OVER SLAT CAVITY ON RT SIDE OF RIB AN D FWD TOP OF RIB. REMOVED CORROSION IAW SRM 51-10-01. CHECKED RIB THICKNESS FOUND MINIMUM NOMINAL .035 MAX NOMINAL THI CKNESS .070 OUT OF LIMITS IAW SRM 57-20-01. REPAIRED IAW AIA/E/2742 SKETCH. CORROSION TASK CARD NUMBER C57-510-01 PART 2 OF 4. NON-ROUTINE TASK CARD NUMBER 12784. 2 L 7 4 4F A20WE 1998040800188 19980408 00188 NM 1998 4 8 CKSA98052 1 19980224 A 5720 65B107831 STIFFENER BOEING 747 747146 NM WS 1516 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION RT WING NR 26 L/E FLAP STIFFENER (CTR) OTBD END BOTH SIDES. R EMOVED AND REPLACED THE 65B10783-1 HAT SECTION IAW B747 SRM 51-30-02 AND 51-10-1. CORROSION TASK CARD NUMBER C57-510-01 PART 2 OF 4. NON-ROUTINE TASK CARD NUMBER 12789. 2 L 7 4 4F A20WE 1998040800189 19980408 00189 NM 1998 4 8 CKSA98053 1 19980224 A 5320 ANGLE BOEING 747 747146 NM BS 2380 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 2380 LT SIDE FLOORBOARD ATTACH ANGLE HAS AREAS OF CORROSION. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS AS PER B747 SRM 53-10-01. INSTALLED ATTACH ANGLE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12793. 2 L 7 4 4F A20WE 1998040800190 19980408 00190 NM 1998 4 8 CKSA98054 1 19980224 A 5320 INTERCOSTAL BOEING 747 747146 NM BS 2345 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 2345 INTERCOSTAL HAS CORROSION RBL45. REMOVED CORROSION FS 2345 INTE RCOSTAL BL 45 IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REMOVED AND REPLACED INTERCOSTAL IAW B747 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12795. 2 L 7 4 4F A20WE 1998040800191 19980408 00191 NM 1998 4 8 CKSA98055 1 19980224 A 5320 ANGLE BOEING 747 747146 NM BS 2350 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 2350 FLOOR SUPPORT ATTACH ANGLE HAS CORROSION LBL 10. REMOVED CORROS ION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS AS PER B747 SRM 53-10-01. REPLACED IAW SRM 51-10-01. CORROSION T ASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12796. 2 L 7 4 4F A20WE 1998040800192 19980408 00192 NM 1998 4 8 CKSA98056 1 19980224 A 5320 ANGLE BOEING 747 747146 NM BS 2330 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 2330 LBL15 LAV DRAIN TUBE ATTACH ANGLE UNDERSIDE CORRODED. REMOVED C ORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED AND REPLACED ANGLE IAW B747 S RM 51-10-01. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12797. 2 L 7 4 4F A20WE 1998040800193 19980408 00193 NM 1998 4 8 CKSA98057 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 2280-2345 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FLOORBOARD SUPPORT FROM FS 2280 TO 2345 RBL 40 HAS CORROSION. REMOVED C ORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED AND REPLACED FLOORBOARD SUPPO RT IAW B747 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12799. 2 L 7 4 4F A20WE 1998040800194 19980408 00194 NM 1998 4 8 CKSA98058 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 2320 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 2320 AT FLOORBOARD SUPPORT HAS SEVERAL AREAS OF CORROSION. REMOVED C ORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. INSTALLED REPAIR PARTS IAW B747 SRM 5 1-40-04. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12801. 2 L 7 4 4F A20WE 1998040800195 19980408 00195 NM 1998 4 8 CKSA98059 1 19980224 A 5320 ANGLE BOEING 747 747146 NM BS 2300-2320 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FLOORBOARD ATTACH ANGLE RBL 70 BETWEEN FS 2300 AND 2320 HAS CORROSION. R EMOVED AND REPLACED ATTACH ANGLE IAW B747 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12806. 2 L 7 4 4F A20WE 1998040800196 19980408 00196 NM 1998 4 8 CKSA98060 1 19980224 A 5320 603127 SUPPORT BOEING 747 747146 NM BS 2280-2300 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FLOORBOARD SUPPORT AT RBL 64 BETWEEN 2280 AND 2300. REMOVED CORROSION I AW B747 SRM 51-10-01. FOUND OUT OF LIMITS AS PER SRM 53-10-01. REMOVED AND REPLACED SUPPORT WITH EXTRUSION IAW SRM 51- 10-01. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TASK CARD NUMBER 12807. 2 L 7 4 4F A20WE 1998040800197 19980408 00197 NM 1998 4 8 CKSA98061 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 810-854 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION UNDER MAIN CARGO FLOOR ON FLOOR SUPPORT AND SEAT TRACK AT FS 810 TO 854 APPROX 78 FROM RT SIDEWALL. REMOVED HAT CHANNEL BS 810 TO 854 RBL 35 IAW SRM 51-30-02. REPLACED HAT CHANNEL IAW B747 SRM 51-10-01 AND 51-30-02. REMOVED SEAT TRACK IAW B747 SRM 51-10-01 BS 810 TO 854. REPLACED SEAT TRACK IAW S RM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-01 PART 3 OF 8. NON-ROUTINE TASK CARD NUMBER 12824. 2 L 7 4 4F A20WE 1998040800198 19980408 00198 NM 1998 4 8 CKSA98062 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 855 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION UNDER FLOOR PANELS AT FS 855 RBL 11 TO 33 APPROX 84 TO 105 FR OM RT SIDE WALL ON FLOOR SUPPORTS. REMOVED AND REPLACED CORRODED FLOOR SUPPORTS IAW B747 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-210-01 PART 3 OF 8. NON-ROUTINE TASK CARD NUMBER 12828. 2 L 7 4 4F A20WE 1998040800199 19980408 00199 NM 1998 4 8 CKSA98063 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 855 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION UNDER MAIN CARGO FLOOR SUPPORTS FS 855 10 TO RT OF FLOOR CENT ER LINE AND FWD. REMOVED AND REPLACED CORRODED FLOOR SUPPORT IAW B747 SRM 51-10-01. CORROSION TASK CARD NUMBER C53-210 -01 PART 3 OF 8. NON-ROUTINE TASK CARD NUMBER 12829. 2 L 7 4 4F A20WE 1998040800200 19980408 00200 NM 1998 4 8 CKSA98064 1 19980224 A 5320 BRACKETS BOEING 747 747146 NM BS 855 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, MAIN CARGO FLOOR FS 855 LBL 11 TO 33 HAS CORRODED FLOOR SUPPORT BRACKETS 10 TO RT OF FLOOR CTR LINE RBL 10. REMOVED CORRODED FLOOR SUPPORT BRACKETS IAW B747 SRM 51-10-01. REPLACED FLOOR SUPP ORTS IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-01 PART 3 OF 8. NON-ROUTINE TASK CARD NUMB ER 12830. 2 L 7 4 4F A20WE 1998040800201 19980408 00201 NM 1998 4 8 CKSA98065 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 1620-1660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, BETWEEN FS 1620 AND FS 1660 LBL 10 SEAT TRACK HAS CORROSION. REMOVED SE AT TRACK IAW B747 SRM 51-30-02. INSTALLED REPAIR SPLICE IAW SRM 53-10-05 FIG 1A. CORROSION TASK CARD NUMBER C53-210-01 PART 3 OF 8. NON-ROUTINE TASK CARD NUMBER 12851. 2 L 7 4 4F A20WE 1998040800202 19980408 00202 NM 1998 4 8 CKSA98066 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 1820 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FS 1820 RBL 32 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRAC K FS 1820 RBL 32 IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-01 PART 4 OF 8. NON-ROUTINE TA SK CARD NUMBER 12859. 2 L 7 4 4F A20WE 1998040800203 19980408 00203 NM 1998 4 8 CKSA98067 1 19980224 A 5315 FLOORBEAM BOEING 747 747146 NM BS 1394 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, FLOORBEAM WEB CRACKED AT BS 1394 RBL 125. REMOVED AND REPLACED CRACKED WEB IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-06. NON-ROUTINE TASK CARD NUMBER 12863. 2 L 7 4 4F A20WE 1998040800204 19980408 00204 NM 1998 4 8 CKSA98068 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 1283-1335 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON SEAT TRACK FLANGES AT RBL 11 BS 1283 TO 1335. REMOVED SEA T TRACK BS 1283 TO 1335 RBL 11 IAW SRM 51-30-02. REPLACED SEAT TRACK IAW B747 SRM 51-30-02 AND 51-10-01. CORROSION TAS K CARD NUMBER C53-210-06 PART 1 OF 1. NON-ROUTINE TASK CARD NUMBER 12876. 2 L 7 4 4F A20WE 1998040800205 19980408 00205 NM 1998 4 8 CKSA98069 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 620-660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, BETWEEN BS 620 AND BS 660, FROM RBL-10 TO RBL-40, BOTH SEAT TRACKS CORRO DED. REMOVED SEAT TRACK BS 620 TO 660 RBL-40 BOTH SEAT TRACKS IAW B747 SRM 51-30-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. INSTALLED NEW SEAT TRACK IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-03 PART 3 O F 4. NON-ROUTINE TASK CARD NUMBER 12889. 2 L 7 4 4F A20WE 1998040800206 19980408 00206 NM 1998 4 8 CKSA98070 1 19980224 A 5315 FLOORBEAM BOEING 747 747146 NM BS 580/760 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, BETWEEN BS 580 AND BS 760 AT FLOOR CENTER AREA, FLOORBEAM PLUS TWO FLOOR AUXILIARY CHANNEL SUPPORTS PLUS WATER CONNECTOR FITTINGS AND FRAME SUPPORTS CORRODED. REMOVED CORROSION ON FLOORBEAM F S 660 AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-01 AND 53-10-01. REPAIRED FLOORBEAM IAW B747 SRM 53-10-07. SEEM M40' S 14767 AND 14768 FOR AUXILIARY CHANNEL SUPPORTS WATER FITTINGS AND FRAME SUPPORTS. CORROSION TASK CARD NUMBER C53-210- 03 PART 3 OF 4. NON-ROUTINE TASK CARD NUMBER 12891. 2 L 7 4 4F A20WE 1998040800207 19980408 00207 NM 1998 4 8 CKSA98071 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 640/660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, BETWEEN BS 640 AND BS 660, RBL 36, AUXILIARY CHANNEL FLOOR SUPPORT CORRO DED. REMOVED CORROSION IAW B747 SRM 51-10-01. INSTALLED IAW B747 SRM 51-03-02. CORROSION TASK CARD NUMBER C53-210-01 PART 2 OF 8. NON-ROUTINE TASK CARD NUMBER 12895. 2 L 7 4 4F A20WE 1998040800208 19980408 00208 NM 1998 4 8 CKSA98072 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 640-740 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, BETWEEN BS 640 AND BS 740, LBL 20, FIRST LFT SEAT TRACK CORRODED AT FOUR DIFFERENT LOCATIONS. REMOVED SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02 AND 53-10-01. REPLACED SEAT TRACK IAW SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-01 PART 2 OF 8. NON-ROUTINE TASK CARD NUMBER 12896. 2 L 7 4 4F A20WE 1998040800209 19980408 00209 NM 1998 4 8 CKSA98073 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 520-600 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, BETWEEN BS 520 AND BS 600, AT RBL 50, THIRD RT SEAT TRACK CORRODED. RE MOVED SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW B747 SRM 51-30-02 AND SRM 53-10-01. REPLACED SEAT TRACK IAW SRM 51-10-0 1 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-01 PART 2 OF 8. NON-ROUTINE TASK CARD NUMBER 12903. 2 L 7 4 4F A20WE 1998040800210 19980408 00210 NM 1998 4 8 CKSA98074 1 19980224 A 5512 PLATE BOEING 747 747146 NM RT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING LINE MAINTENANCE INSPECTION FOUND PANEL O/B OF O/B ELEV ON LOWER SURFACE HAS SMALL AREA OF CORROSION. REMOVED AN D INSTALLED CORRODED FILLER PLATE IAW B747 SRM 51-10-01 AND 51-30-02 W/O 210-674. NON-ROUTINE TASK CARD NUMBER 12915. 2 L 7 4 4F A20WE 1998040800211 19980408 00211 NM 1998 4 8 CKSA98075 1 19980224 A 5330 SKIN BOEING 747 747146 NM BS 2360 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING WALKAROUND INSPECTION FOUND LEVEL 2 CORROSION, LWR SKIN DAMAGED AND DRAIN BROKEN AT FS 2360 RBL 12 STR 49. CUT O UT DAMAGE AND MADE FILLER AND DOUBLER IAW AIA/E/2739 SKETCH. INSTALLED REPAIR IAW AIA/E/2739 SKETCH. NON-ROUTINE TASK CARD NUMBER 12917. 2 L 7 4 4F A20WE 1998040800212 19980408 00212 NM 1998 4 8 CKSA98076 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 660-780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, SEAT TRACK CORRODED BS 660 TO 780 RBL34. REMOVED AND INSTALLED SEAT TRA CK IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-03 PART 3 OF 4. NON-ROUTINE TASK CARD NUMBER 14721. 2 L 7 4 4F A20WE 1998040800213 19980408 00213 NM 1998 4 8 CKSA98077 1 19980224 A 5347 SEAT TRACK BOEING 747 747146 NM BS 660-780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, SEAT TRACK CORRODED BS 660 TO 780 RBL11. REMOVED AND INSTALLED SEAT TRA CK IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-03 PART 3 OF 4. NON-ROUTINE TASK CARD NUMBER 14722. 2 L 7 4 4F A20WE 1998040800214 19980408 00214 NM 1998 4 8 CKSA98078 1 19980224 A 5320 T-ANGLE BOEING 747 747146 NM BS 1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION ON T-ANGLE BS 1920 ON TOP OF FLOORBEAM FROM RBL 40 TO LBL 53. CORROSION FOUND TO BE OUT OF LIMITS AT RBL 10 TO 42 AND LBL 20 TO 23 IAW B747 SRM 53-10-1. CUTOUT CORRODED T-ANGLE IAW B747 SRM 51-40-4. INSTALLED REPAIR PARTS IAW B747 SRM 51-40-04. CORROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5. N ON-ROUTINE TASK CARD NUMBER 14753. 2 L 7 4 4F A20WE 1998040800215 19980408 00215 NM 1998 4 8 CKSA98079 1 19980224 A 5315 FLOORBEAM BOEING 747 747146 NM BS 1660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON FLOORBEAM UPPER CHORD AT STA 1660 LBL 15. REMOVED CORROSI ON ON FLOORBEAM UPPER CHORD AT BS 1660 LBL 15 IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. CUT OU T DAMAGED AREA IAW B747 SRM 53-10-07 FIG 9. INSTALLED REPAIR SPLICES IAW SRM 53-10-07 FIG 9. CORROSION TASK CARD NUMBE R C53-210-01. NON-ROUTINE TASK CARD NUMBER 14755. 2 L 7 4 4F A20WE 1998040800216 19980408 00216 NM 1998 4 8 CKSA98080 1 19980224 A 5311 FRAME BOEING 747 747146 NM BS 400-420 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION. CORROSION ON LOWER INNER SIDE WINDOW FRAME RT SIDE STA 400 TO 420. REM OVED FRAME AS PER SRM 51-30-02. FOUND CORROSION OUT OF LIMITS. REPLACED NEW WINDOW FRAME BETWEEN STA 400 TO 420 RT SID E IAW B747 SRM 51-10-06, 51-30-02, 51-10-1. CORROSION TASK CARD NUMBER C53-210-03. NON-ROUTINE TASK CARD NUMBER 14758. 2 L 7 4 4F A20WE 1998040800217 19980408 00217 NM 1998 4 8 CKSA98081 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, BS 1920 LBL 23 FLOOR SUPPORT CORRODED. CORROSION FOUND TO BE OUT OF LIM ITS IAW B747 SRM 53-10-1. CUT OUT DAMAGED SECTION OF FLOOR SUPPORT IAW B747 SRM 51-40-4 FIG 2. INSTALLED FLOOR SUPPORT AND SPLICES IAW B747 SRM 51-40-4. CORROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5. NON-ROUTINE TASK CARD NUMBER 147 60. 2 L 7 4 4F A20WE 1998040800218 19980408 00218 NM 1998 4 8 CKSA98082 1 19980224 A 5320 ANGLE BOEING 747 747146 NM BS 500-520 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION, FOUND BS 500 TO 520 RBL 5 FLOOR SUPPORT ANGLE CRACKED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-01. NON-ROUTINE TASK CARD NUMBER 14770. 2 L 7 4 4F A20WE 1998040800219 19980408 00219 NM 1998 4 8 CKSA98084 1 19980224 A 5320 SUPPORT BOEING 747 747146 NM BS 1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 703CK 19727 DURING CPCP INSPECTION FOUND LEVEL 2 CORROSION, INTERGRAN CORROSION ON FLOOR SUPPORT (ATTACHED TO T-ANGLE) AT FS 1920 RB L 30.5. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUT OUT CORRODED FLOOR SUPPORT SECTION IAW B747 SRM 51-40-3. INSTALLED FLOOR SUPPORT AND SPLICE IAW B747 SRM 51-40-3. CORROSION TASK CARD NUMBER C53-110-01 PART 3 OF 5. N ON-ROUTINE TASK CARD NUMBER 14782. 2 L 7 4 4F A20WE 1998041000003 19980410 00003 SO 1998 4 10 98ZZZX1323 2 19980301 A 7310 636113 TUBE CESSNA 421 421B 2076014 CE CONT O520 GTSIO520* 17032 SO NR 2 CYL INJ FAILED A DYVA K NONE O OTHER NR NOT REPORTED 1 NM 07 5943M 897 421B0316 A FUEL DISCHARGE TUBE ASSY FROM THE FUEL MANIFOLD VALVE TO THE NR 2 CYLINDER FUEL INJECTOR NOZZLE WAS FOUND BROKEN AT TH E BALL END FITTING INSIDE OF THE BRASS RETAINING NUT ON THE FUEL MANIFOLD END. SUBMITTER STATED NO OBVIOUS CAUSE OF FAI LURE, HOWEVER, AGE FATIGUE, AND/OR VIBRATION MAY BE FACTORS. 1 L 7 2 3O 3 O A7CE E7CE 1998041000004 19980410 00004 CE 1998 4 10 98ZZZX1324 1 19980304 A 3710 1H59 CHECK VALVE CESSNA 421 421C 2076016 CE VACUUM MANIFOLD FAILED A MOGA K NONE O OTHER IN INSP/MAINT 1 GL 25 98437 5917 421C0040 DURING ENGINE RUNS FOR PHASE INSPECTION, LT ENGINE STARTED AND BOTH VACUUM FAIL BUTTONS PULLED ON GAUGE. VACUUM PRESSUR E NORMAL. RT ENGINE WAS NOT RUNNING. RT ENGINE STARTED, ALL INDICATIONS NORMAL. LT ENGINE SHUT DOWN WITH RT ENGINE RU NNING AND BOTH BUTTONS REMAINED PULLED, BUT VACUUM FELL TO 1 INCH. TROUBLESHOOTING REVEALED CHECK VALVE DEFECTIVE IN VA CUUM MANIFOLD. REMOVED AND REPLACED MANIFOLD, AIRBORNE TECHNICAL SERVICE INSTRUCTION CALLS FOR 1 YEAR INSPECTION AND 10 YEAR REPLACEMENT. THIS UNIT MANUFACTURED 10-75. 1 L 7 2 3O A7CE 1998041000005 19980410 00005 CE 1998 4 10 98ZZZX1325 1 19980303 A 7120 505402019 BEAM ASSY 505402019 CESSNA 421 421C 2076016 CE LT NAC MOUNT LOOSE A MOGA K NONE O OTHER IN INSP/MAINT 1 GL 25 98737 5917 421C0040 DURING PHASE INSPECTION, SEVERAL LOOSE AND WORKING RIVETS WERE FOUND IN TOP OF INBOARD ENGINE MOUNT BEAM APPROXIMATELY 6 INCHES AFT OF AFT ENGINE MOUNT BRACKET. SUBMITTER STATED POSSIBLY CAUSED BY HARD LANDING OR TURBULENCE. 1 L 7 2 3O A7CE 1998041000007 19980410 00007 CE 1998 4 10 98ZZZX1327 1 19980303 A 3250 59420011 BELLCRANK CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO NLG STEERING CRACKED A MOGA K NONE O OTHER IN INSP/MAINT 1 GL 25 98437 5917 421C0040 272428R DURING PHASE INSPECTION, NOSE STEERING BELLCRANK WAS FOUND CRACKED ON BOTH SIDES OF CENTER PIVOT BOLT. FAILURE WOULD RE SULT IN LOSS OF STEERING. NO IMPACT MARKS FOUND. AIRCRFAT HAS HISTORY OF NOSE GEAR COLLAPSE. 1 L 7 2 3O 3 O A7CE E7CE 1998041000008 19980410 00008 CE 1998 4 10 98ZZZX1328 1 19980303 A 8120 51550117 BRACKET CESSNA 421 421C 2076016 CE LT ENGINE TURBO CRACKED A S MOGA K NONE O OTHER IN INSP/MAINT 1 GL 25 98437 5917 421C0040 DURING PHASE INSPECTION, LT TURBOCHARGER MOUNTING BRACKET WAS FOUND CRACKED ALONG WELD JOINING FLAT PLATE AND TUBE PORTI ON. 1 L 7 2 3O A7CE 1998041000009 19980410 00009 CE 1998 4 10 98ZZZX1329 1 19980303 A 7120 50540303 BEAM ASSY CESSNA 421 421C 2076016 CE CONT O520 GTSIO520L 17032 SO LT/RT NACELLE CRACKED A MOGA K NONE O OTHER IN INSP/MAINT 1 GL 25 98437 5917 421C0040 272428R DURING PHASE INSPECTION, UPPER OUTBOARD AFT VERTICAL WEB MEMBERS OF AFT BEAM ASSEMBLIES WERE FOUND CRACKED. THIS AFFECT ED BEAMS IN BOTH NACELLES. SUBMITTER SUSPECTS CAUSE WAS HARD LANDING. AIRCRAFT REMOVED FROM SERVICE PENDING REPAIRS. 1 L 7 2 3O 3 O A7CE E7CE 1998041000026 19980410 00026 SW 1998 4 10 98ZZZX1346 1 19980323 A 2910 10648BHI11 SWITCH BELL 230 230 1182149 SW NR 1 HYD SYSTEM FAILED A HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 236X 23015 IN CRUISE FLIGHT, NR 1 HYDRAULIC SYSTEM PRESSURE DROPPED TO ZERO, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND ON/OFF SWI TCH FAILED. REPLACED SWITCH DUE TO WEAK LOCK IN THE ON POSITION. REF: IPC, CHAPTER 96-99-00, PAGE 80, ITEM 16, FIGURE 96-1022. 1 G 7 2 3U NC H9SW 1998041000063 19980410 00063 CE 1998 4 10 98ZZZX1310 1 19980324 A 3230 504501032 TORQUE TUBE CESSNA 402 402B 207590P CE RT MLG FAILED A OEZA O OTHER J WARNING INDICATION CL CLIMB 1 WP 19 773EA 11396 402B0544 PILOT REPORTED RT MAIN GEAR WOULD NOT RETRACT. MECHANICS FOUND TORQUE TUBE 504501032 PEELED LIKE A PILLSBURY CAN OF BIS CUITS. 1 L 7 2 3O A7CE 1998041000069 19980410 00069 CE 1998 4 10 98ZZZX1316 1 19980213 A 3231 52130389 BRACKET ASSY CESSNA 402 402C 207590R CE LT NLG DOOR ROD FAILED A A GNXA O OTHER J WARNING INDICATION AP APPROACH 1 SW 01 38CJ 402C0023 PILOT REPORTED NOSE GEAR WOULD NOT COME DOWN AND LOCK. A NOSE GEAR UP LANDING WAS MADE. INVESTIGATION REVEALED THE FOR WARD LT NOSE GEAR GOOD RETRACTION ROD BRACKET ASSY FAILED ALLOWING THE NOSE GEAR TO IMPACT DOOR ON RETRACTION AND JAMMIN G NOSE GEAR IN WHEEL WELL. REASON FOR BRACKET FAILURE IS NOT CONCLUSIVE AT THIS TIME. 1 L 7 2 3O A7CE 1998041000074 19980410 00074 WP 1998 4 10 9805471225 1 19980318 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING M-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT FS 459 LBL 62. REPAIRED PER EA 12-150786. 2 L 7 3 4F A22WE 1998041000075 19980410 00075 WP 1998 4 10 9805481225 1 19980318 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING M-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME AT FS 459, RBL 62. REPAIRED PER EA 12-150786. 2 L 7 3 4F A22WE 1998041000076 19980410 00076 WP 1998 4 10 9805491225 1 19980316 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 895 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING M-CHECK, FOUND CORROSION ON FORWARD CARGO DOOR JAMB FRAME AT FS 895, STR 42R. REPAIRED PER EA 12-190781. 2 L 7 3 4F A22WE 1998041000077 19980410 00077 WP 1998 4 10 9805501152 1 19980310 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING L-CHECK, FOUND CRACK IN FRAME AT FS 459, RBL 62 IN FORWARD AVIONICS COMPARTMENT. REPAIRED PER EA 11-150785. 2 L 7 3 4F A22WE 1998041000078 19980410 00078 WP 1998 4 10 9805511152 1 19980301 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 895 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING L-CHECK, FOUND CRACK IN FORWARD CARGO DOOR JAMB FS 895. REPAIRED PER EA 11-154993. 2 L 7 3 4F A22WE 1998041000079 19980410 00079 WP 1998 4 10 9805521152 1 19980301 A 5320 WEB DOUG DC10 DC1040 3023508 WP BS 476 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING L-CHECK, FOUND A CRACK IN THE NOSE GEAR SUPPORT BEAM RIGHT WEB AT FS 476. REPAIRED PER EA 11-156156. 2 L 7 3 4F A22WE 1998041000080 19980410 00080 WP 1998 4 10 9805531152 1 19980311 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING L-CHECK, FOUND CRACK IN FRAME AT FS 459, LBL 62 IN THE FORWARD AVIONICS COMPARTMENT. REPAIRED PER EA 11-150785. 2 L 7 3 4F A22WE 1998041000081 19980410 00081 NM 1998 4 10 9805542706 1 19980325 A 5320 ANGLE BOEING 727 727225 1384077 NM CARGO DOORWAY CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 815EA 22552 DURING H-CHECK, FOUND CORROSION ON SKIN SUPPORT ANGLE AT THE FORWARD CARGO DOOR AFT JAMB. REPAIRED PER EA 27-156539. 2 L 7 3 4F A3WE 1998041000082 19980410 00082 EU 1998 4 10 QXEA9800450 1 19980328 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 AFT LEFT AND RIGHT EXIT EVACUATION LIGHTS INOP. MAINTENANCE TIGHTENED LT AND RT EVACUATION LIGHT SOCKETS, CLEANED GROUN D CONNECTIONS, AND REMOVED AND REPLACED LAMPS. EVACUATION LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1998041000083 19980410 00083 EU 1998 4 10 QXEA9800451 1 19980331 A 3350 1012721 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 EMERGENCY EXIT LIGHT COVER ON SEAT 8B MISSING. THE LIGHT ASSEMBLY WAS REPLACED, CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998041000084 19980410 00084 EU 1998 4 10 QXEA9800452 1 19980331 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 10. MAINTENANCE REPLACED SAME, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998041000095 19980410 00095 NM 1998 4 10 98UAL900001 1 19980103 A 2133 27406502 OUT FLOW VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 778UA 26940 AIRCRAFT RETURNED TO MIA, UNABLE TO PRESSURIZE CABIN AND LANDED OVERWEIGHT. *S/D* AFT OUTFLOW VALVE REPLACED TWO DAYS LATER. THERE WAS NO FURTHER PRESSURIZATION PROBLEMS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998041000096 19980410 00096 EU 1998 4 10 98UAL900002 1 19980102 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 417UA 483 EEL LIGHT INOP AT 12C. REPLACE LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A28NM E40NE 1998041000097 19980410 00097 NE 1998 4 10 98UAL900003 2 19980106 A 7200 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 4 BIRD STRIKE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 WP 29 188UA 26877 724699 ON TAKEOFF ROLL CREW REPORTED BIRD STRIKE AND ABORTED TAKEOFF AT 130 KNOTS. *S/D* FOUND EVIDENCE OF BIRD STRIKE ON NR 4 ENGINE. INSPECTED ENGINE NO DAMAGE FOUND. 2 L 7 4 4F 4 F RT A20WE E24NE 1998041000098 19980410 00098 WP 1998 4 10 98UAL900004 1 19980105 A 5712 RIB DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CTR WING CRACKED A UALA K NONE O OTHER UK UNKNOWN 1 WP 29 1837U 47969 A CRACK WAS FOUND ON THE CENTER WING SECTION RIBS LOCATED AT RBL 29.0. THE CRACK RUNS FWD AND AFT DIAGONALLY AND MEASU RES APPROXIMATELY 4.00 INCHES IN LENGTH. A DOUBLER WAS INSTALLED IN THE AREA. 2 L 7 3 4F 4 F A22WE E23EA 1998041000099 19980410 00099 EU 1998 4 10 98UAL900005 1 19980108 A 3220 TORQUE LINKS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG DISCONNECTED A UALA K NONE O OTHER LD LANDING 1 WP 29 441UA 751 NLG TORQUE LINKS DISCONNECTED UPON LANDING. NLG TIRES ROTATED 180 DEGREES DURING A SLOW LEFT TURN FOLLOWING LANDING ROL L-OUT. 2 L 7 2 4F 4 F RT A28NM E40NE 1998041000101 19980410 00101 NM 1998 4 10 98UAL900106 1 19980308 A 3260 841602 PSEU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG DEFECTIVE A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 567UA 26673 RETURNED TO FIELD AT LAX UNDER AMBER ALERT DUE TO A NOSE GEAR INDICATION PROBLEM. *S/D* PSEU WAS GIVING FALSE SIGNALS. NOSE DOWN LOCK SYSTEM 1 AND 2 WAS OUT OF ADJUSTMENT. READJUSTED NOSE DOWN LOCK SYSTEM 1 AND 2. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041000102 19980410 00102 NM 1998 4 10 98UAL900119 1 19980321 A 2440 DH7BC RELAY BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE GROUND SERVICE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 368UA 24537 GROUND SERVICE BUS CIRCUIT BREAKER POPPED, LOST GENERATOR. *S/D* INSPECTED WIRING BEHIND THE P-6 PANEL AND ALL LOOKED GOOD. REPLACED GROUND SERVICE RELAY, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041000103 19980410 00103 NM 1998 4 10 98UAL900121 1 19980324 A 2722 3800022107 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RUDDER ACTUATOR FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 521UA 24891 FLIGHT DIVERTED TO LAX AND LANDED UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. *S/D* RUDDER RATIO CHANGE AC TUATOR ROD SEAL FAILED. REPLACED RRCA AND SERVICED LEFT SYSTEM. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041000105 19980410 00105 NM 1998 4 10 98UAL900115 1 19980314 A 2133 SWITCH HAMILTON STD 711003X BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE OUTFLOW VALVE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 926UA 107417 26648 DIVERTED TO SACRAMENTO DUE TO THE LOSS OF CABIN PRESSURIZATION. *S/D* PROBLEM CAUSED BY FAILURE OF THE SWITCH ON THE O UTFLOW VALVE. THIS SWITCH ALSO CONTROLS THE FORWARD OUTFLOW VALVE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041000107 19980410 00107 NM 1998 4 10 98UAL900117 1 19980317 A 3350 1315 LAMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7456U 21910 EMERGENCY EXIT LIGHT ON LEFT FUSELAGE AFT OF WING IS INOPERATIVE. RELAMPED. 2 L 7 3 4F 4 F A3WE E2EA 1998041000108 19980410 00108 NE 1998 4 10 98UAL900118 2 19980318 A 7532 BLEED AIR VALVE AIR RESEARCH 8981261 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 7287U 21565 AIRCRAFT EXPERIENCED BLEED TRIP RESULTING IN CABIN ALTITUDE RISING ABOVE 10,000 FEET. AIRCRAFT WAS IN CRUISE AT 31,000 FEET. CAPTAIN DECLARED AN EMERGENCY FOR IMMEDIATE DESCENT. DESCENDED TO 20,000 FEET AND PRESSURE RETURNED TO NORMAL. C ONTINUED TO DESCEND INTO LGA. *S/D* REPLACED NR 3 ENGINE PNEUMATIC BLEED AIR VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998041000109 19980410 00109 WP 1998 4 10 ABXA9800279 1 19980306 A 5320 561386255 DOUBLER DOUG DOUG DC8 DC863F 302198F WP BS 20-25 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FINGER DOUBLER HAS HEAVY CORROSION AT FS 20 TO 25, STRINGER 31R. REPAIRED IAW DC8 SRM 53-1-0 AND 51-1-20. 2 L 7 4 4F 4A25 1998041000110 19980410 00110 WP 1998 4 10 ABXA9800280 1 19980210 A 5712 576947023 RIB DOUG DOUG DC8 DC863F 302198F WP WS 778.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE UPPER RIB CRACKED AT AFT END XFS 778.75. REPAIRED IAW ABX DWG K05056 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998041000111 19980410 00111 WP 1998 4 10 ABXA9800281 1 19980212 A 5320 561032617 INTERCOSTAL DOUG DOUG DC8 DC863F 302198F WP BS 340 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 INTERCOASTAL JUST AFT OF MAIN DECK FLOORBEAM STATION 340 LBL10 CRACKED. REPAIRED IAW DC8 SRM 53-20 AND 51-1-20D. 2 L 7 4 4F 4A25 1998041000112 19980410 00112 WP 1998 4 10 ABXA9800282 1 19980223 A 5712 RIB DOUG DOUG DC8 DC863F 302198F WP WS 220.0 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 AT XFS 220.0, NR 2 STUB WING RIB (UPPER) IS CRACKED. REPAIRED IAW DWG K05056. 2 L 7 4 4F 4A25 1998041000113 19980410 00113 WP 1998 4 10 ABXA9800283 1 19980222 A 5320 561032617 INTERCOSTAL DOUG DOUG DC8 DC863F 302198F WP BS 520 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STATION 520 RBL 10 ON CEILING INTERCOSTAL ATTACH ANGLE IS CRACKED. REPAIRED IAW DC8 SRM 53-7-7 AND 51-1-21D. 2 L 7 4 4F 4A25 1998041000114 19980410 00114 WP 1998 4 10 ABXA9800284 1 19980212 A 5320 3750330523 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STATION 440 TO 460 STRINGER 33R SPLICE FITTING IS CRACKED AT FWD END. REPAIRED IAW DC8 SRM 51-1-21D. 2 L 7 4 4F 4A25 1998041000115 19980410 00115 WP 1998 4 10 ABXA9800285 1 19980215 A 5320 3640887N FITTING DOUG DOUG DC8 DC863F 302198F WP BS 960-980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 HORIZONTAL FITTING CORRODED AT LBL 48 BETWEEN FUSELAGE STATION 980 AND 960. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F 4A25 1998041000116 19980410 00116 WP 1998 4 10 ABXA9800286 1 19980222 A 5712 K050567 RIB DOUG DOUG DC8 DC863F 302198F WP WS 270 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 NR 3 STUB WING RIB IS CRACKED AT STA 270 (UPPER RIB). REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998041000117 19980410 00117 WP 1998 4 10 ABXA9800287 1 19980215 A 5311 5645332617 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 902 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 BULGING CORROSION AND POPPED RIVETS RBL 64 STATION 902. REPAIRED IAW DWG 5645332 AND DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998041000118 19980410 00118 WP 1998 4 10 ABXA9800288 1 19980214 A 5712 5770024 RIB DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT LEADING EDGE SECTION BETWEEN PYLONS, LOWER LEADING EDGE RIB JUST INBOARD OF SLOT ACTUATOR IS CRACKED AT THE AFT END . REPAIRED IAW DWG K05056-7001 AND DC8 SRM 51-1-11. 2 L 7 4 4F 4A25 1998041000119 19980410 00119 WP 1998 4 10 ABXA9800289 1 19980331 A 2510 5925379502 SEAT DOUG DC9 DC932 3022066 WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 905AX 732 47147 FIRST OFFICER'S SEAT WAS DIFFICULT TO LOCK IN FULL FORWARD POSITION. SEAT SLID BACK ON INITIATION OF TAKEOFF ROLL. SEA T UNLOCKED ON FINAL APPROACH INTO ILN WITH FIRST OFFICER FLYING AIRCRAFT. LUBRICATED FIRST OFFICER'S SEAT LINKAGE. SEA T OPERATES NORMALLY. LOCKS IN ALL POSITIONS IAW DC 9 MM. 2 L 7 2 4F A6WE 1998041000120 19980410 00120 WP 1998 4 10 ABXA9800290 1 19980331 A 3260 UNSAFE LIGHT DOUG DC9 DC932 3022066 WP RT MLG ILLUMINATED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 980AX 47176 AFTER GEAR RETRACTION, THE RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. IN THE GEAR UP-LATCH CHECK POSITION, THE GEAR DOOR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR DOWN AND UP, NORMAL OPERATION. PERFORMED ADJUSTMENT/TEST IAW DC9 MM 32-31 -4, FOUND NO DEFECTS. OPERATED LANDING GEAR SEVERAL TIMES, PERFORMED UP-LATCH CHECK. OPS CHECKED NORMAL. NO DEFECTS N OTED. 2 L 7 2 4F A6WE 1998041000121 19980410 00121 WP 1998 4 10 MWEA98383 1 19980401 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP CABIN DOOR SLIDE FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 207ME 47794 THE MAIN CABIN DOOR EVACUATION SLIDE COVER SEPARATED FROM DOOR. MTC REINSTALLED MAIN CABIN DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998041000122 19980410 00122 WP 1998 4 10 MWEA98384 1 19980330 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP GALLEY DR SLIDE FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 204ME 47680 THE GALLEY SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998041000123 19980410 00123 NM 1998 4 10 SCNA98028 1 19980401 A 2932 ST7R PRESS SENSOR BOEING 727 7272J4 1384006 NM A-HYD SYSTEM INOPERATIVE A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 290SC 20764 ON TAKEOFF ROLL, A-SYSTEM HYDRAULICS PRESSURE LOW CIRCUIT BREAKER POPPED, TAKEOFF ABORTED AT 80 KNOTS. REMOVED AND REPL ACED A-SYSTEM PRESSURE TRANSMITTER IN ACCORDANCE WITH MAINTENANCE MANUAL 293101. FUNCTIONAL AND LEAK CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998041000129 19980410 00129 NM 1998 4 10 98ZZZX1352 1 19980313 A 6710 900C3820021105 SERVO ACTUATOR DOUG MD900 MD900 3027375 NM M/R LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 67 0066400082 90000012 HYDRAULIC SERVO ACTUATOR LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998041000130 19980410 00130 NM 1998 4 10 98ZZZX1353 1 19980313 A 6320 381860710012 BYPASS INDICATOR DOUG MD900 MD900 3027375 NM MGB OIL FAILED A R7MA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 11 901CF 1971 0009 90000012 MGB FILTER BYPASS INDICATOR UNIT INOPERATIVE. EVEN WITH FRESH FILTERS INSTALLED, UNIT 'POPS'. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998041000131 19980410 00131 1998 4 10 98ZZZX1354 4 19980317 A 2210 105860291 CONTROL UNIT BOLKMS 105 BO105LSA3 5626020 EU AUTOFLIGHT MALFUNCTIONED A R7MA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 NM 11 202LF 503 1191028 2014 CONTROL MALFUNCTION, ROLL FEEDBACK DURING FLIGHT AND PITCH INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998041000132 19980410 00132 EU 1998 4 10 98ZZZX1355 1 19980126 A 6410 11731743 BLADE BOLKMS 117 BK117A3 5626015 EU T/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 70 394 7063 T/R BLADE PAINT BEGINNING TO PEEL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998041000133 19980410 00133 EU 1998 4 10 98ZZZX1356 1 19980126 A 6410 11731743 BLADE BOLKMS 117 BK117A3 5626015 EU T/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 70 386 7063 T/R BLADE PAINT BEGINNING TO PEEL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998041000134 19980410 00134 EU 1998 4 10 98ZZZX1357 1 19980127 A 6410 11731743 BLADE BOLKMS 117 BK117A4 5626017 EU T/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 155 412 7127 T/R BLADE PAINT BEGINNING TO PEEL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998041000135 19980410 00135 EU 1998 4 10 98ZZZX1358 1 19980127 A 6410 11731743 BLADE BOLKMS 117 BK117A4 5626017 EU T/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 155 409 7127 T/R BLADE PAINT BEGINNING TO PEEL. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998041000137 19980410 00137 NE 1998 4 10 98ZZZX1360 2 19980302 A 7250 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURBINE BLADES PITTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 1156 SC17231 7230 LE45987EF TURBINE ROTOR ASSY UPGRADED TO -11, SOME PITTING ON BLADES. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCL ES: 6,310.5. 1 G 7 2 3U 3 U H13EU E5NE10 1998041000138 19980410 00138 NM 1998 4 10 98ZZZX1361 1 19980313 A 6322 900D1400526101 BLOWER DRIVE DOUG MD900 MD900 3027375 NM M/R LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 1971 0062190038 90000012 BLOWER DRIVE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998041000139 19980410 00139 NM 1998 4 10 K3HA980042 1 19980330 A 3350 387 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 R-2 EMERGENCY EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK FOR R-2 EMERGENCY DOOR. OPS CHECK GOOD PER MM 33-50-71. 2 L 7 3 4F A3WE 1998041000140 19980410 00140 NM 1998 4 10 K3HA980043 1 19980330 A 3350 900835A LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 LEFT OVERWING AFT EXIT DOOR EMERGENCY LIGHT INOP. RELAMPED FIXED EXIT LIGHT. OPS CHECK OK. 2 L 7 3 4F A3WE 1998041000141 19980410 00141 NM 1998 4 10 K3HA980044 1 19980330 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 LEFT WING EMERGENCY LIGHT AFT OUT EMERGENCY EXIT. REMOVED AND REPLACED BATTERY PACK REF MM 33-50-71. 2 L 7 3 4F A3WE 1998041000142 19980410 00142 NM 1998 4 10 K3HA980045 1 19980330 A 3350 079123 LENSE BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHT AND LENSE MISSING REF MM 33-50. INSTALLED SERVICEABLE LENSE AND BULB P/N 30711, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998041000143 19980410 00143 WP 1998 4 10 CALA9800608 1 19980401 A 5743 FITTING DOUG DC10 DC1030 3023501 WP LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 41068 47867 INSPECTION FOUND LT MLG FITTING ATTACHMENT TO LOWER SUPPORT DOUBLER CORRODED AROUND FASTENER HOLE AT INNER SURFACE. THE CORROSION WAS REMOVED IAW SRM 51-21-01. THE AREA WAS REPAIRED IAW ECRA 5740-01831. 2 L 7 3 4F A22WE 1998041000144 19980410 00144 WP 1998 4 10 CALA9800609 1 19980402 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 THE TAILCONE PULL FORCE FROM THE OUTSIDE, INSIDE, AND AFT ENTRY DOOR HANDLES WAS EXCESSIVE. THE TAILCONE CABLES WERE RI GGED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998041000145 19980410 00145 NM 1998 4 10 CALA9800610 1 19980402 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND FLOOR SUPPORT CORRODED UNDER NUT PLATES IN FORWARD CARGO COMPARTMENT AT STA 640, STRINGER 28R. THE COR RODED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-4-4, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998041000146 19980410 00146 NM 1998 4 10 CALA9800611 1 19980402 A 5320 WEB BOEING 727 727227 1384078 NM BS 1150/1170 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND RT AFT LAV FLOOR WEB CORRODED AT STA 1150 AND 1170. THE CORRODED SECTION OF FLOOR WAS CUT OUT IAW SRM 51-40-2. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-2. 2 L 7 3 4F A3WE 1998041000147 19980410 00147 NM 1998 4 10 CALA9800612 1 19980402 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 722 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 1 CRACK IN ANGLE AT FS 722, BBL 0. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-6, AND 51-40-1. 2 L 7 3 4F A3WE 1998041000148 19980410 00148 NM 1998 4 10 CALA9800613 1 19980402 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 471 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT FS 471, BBL 0. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTA LLED IAW SRM 51-10-1, 51-10-2, AND 51-40-5. 2 L 7 3 4F A3WE 1998041000149 19980410 00149 NM 1998 4 10 CALA9800614 1 19980402 A 5320 INTERCOSTAL BOEING 727 727227 1384078 NM BS 380 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT UPPER FLANGE RIVET, FS 380, LBL 12. THE CRACK WAS STOP DRILLED IAW S RM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998041000150 19980410 00150 NM 1998 4 10 CALA9800615 1 19980402 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 380-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND CORROSION ON TOP AND BOTTOM OF CHORD AT FS 380-420, RBL 64. THE CORROSION AND CORRODED SPLICE ANGLE WE RE REMOVED. A NEW SPLICE ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-6, AND 51-10-1. 2 L 7 3 4F A3WE 1998041000151 19980410 00151 NM 1998 4 10 CALA9800616 1 19980402 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND SEAT TRACK CORRODED IN FLOOR PANEL NR 97 INBOARD AFT AREA. THE SEAT TRACK WAS REMOVED. A NEW SEAT TRA CK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998041000152 19980410 00152 NM 1998 4 10 CALA9800617 1 19980402 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND SEAT TRACK CORRODED AT FLOOR PANEL NR 104 AREA. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FA BRICATED AND INSTALLED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998041000153 19980410 00153 NM 1998 4 10 CALA9800618 1 19980402 A 5320 DOUBLER BOEING 727 727227 1384078 NM BS 1263 KINKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND DOUBLER KINKED AND TORQUE BOX WEB CRACKED 1 AT STA 1263R BELOW AIRSTAIR ACTUATOR. THE CRACK WAS STOP D RILLED IAW SRM 51-10-1. THE DOUBLER WAS REMOVED IAW SRM 51-30-2. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51- 10-1, 51-30-2, AND 51-40-2. 2 L 7 3 4F A3WE 1998041000154 19980410 00154 WP 1998 4 10 9805559908 1 19980326 A 5320 591235019 DOUBLER DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING L CHECK, FOUND CRACK IN COCKPIT WINDOW SILL DOUBLER (P/N 5912350-19) AT FS 83.5. REPAIRED PER EA 99-156262. 2 L 7 2 4F A6WE 1998041000155 19980410 00155 WP 1998 4 10 9805569908 1 19980326 A 5320 591235020 DOUBLER DOUG DC9 DC931 3022065 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 958N 47254 DURING L CHECK, FOUND CRACK IN COCKPIT WINDOW SILL DOUBLER (P/N 5912350-20) AT FS 83.5. REPAIRED PER EA 99-556262. 2 L 7 2 4F A6WE 1998041000156 19980410 00156 WP 1998 4 10 9805579920 1 19980314 A 5312 DOUBLER DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 942N 47459 DURING L CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD VENTRAL DOOR CUTOUT LEFT -9 DOUBLER. REPAIRED PER EA 99-1562620. 2 L 7 2 4F A6WE 1998041000157 19980410 00157 WP 1998 4 10 9805589956 1 19980323 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 695 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING M CHECK, FOUND CRACK IN KEEL ATTACH FITTING LOCATED UNDER DOOR ACTUATOR FITTING AT FS 695. REPLACED FITTING (391 5784-1) PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998041000158 19980410 00158 WP 1998 4 10 9805599956 1 19980324 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 699 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING M CHECK, FOUND CRACK KEEL ATTACH FITTING BELOW MAIN LANDING GEAR ACTIVATOR FITTING AT FS 699. REPLACED FITTING ( P/N 3915784-505) PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998041000159 19980410 00159 NM 1998 4 10 9805602705 1 19980303 A 5313 LONGERON BOEING 727 727225 1384077 NM BS 1168 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 802EA 22433 DURING H CHECK, FOUND CORROSION ON STR 27L AT FS 1168. REPAIRED PER EA 27-156099. 2 L 7 3 4F A3WE 1998041000160 19980410 00160 NM 1998 4 10 9805612705 1 19980216 A 5313 LONGERON BOEING 727 727225 1384077 NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 802EA 22433 DURING H CHECK, FOUND CORROSION ON STR 29R AT FS 950. REPAIRED PER EA 27-154490. 2 L 7 3 4F A3WE 1998041000161 19980410 00161 NM 1998 4 10 9805622705 1 19980226 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 802EA 22433 DURING H CHECK, FOUND CORROSION ON UPPER CHORD OF FLOORBEAM AT FS 1130, RBL 16-27, WL 208. REPAIRED PER EA 27-154488. 2 L 7 3 4F A3WE 1998041000162 19980410 00162 NM 1998 4 10 9805636719 1 19980302 A 5711 SPAR BOEING 747 747251F 1384898 NM WS 1383 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING PERIODIC CHECK, FOUND CORROSION ON FRONT SPAR LOWER CHORD NEAR SUPPORT FITTING AT FSS 1383. REPAIRED PER EA 67-1 53232. 2 L 7 4 4F A20WE 1998041000163 19980410 00163 NM 1998 4 10 9805646719 1 19980302 A 5311 FRAME BOEING 747 747251F 1384898 NM BS 380 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 619US 21321 DURING PERIODIC CHECK, FOUND CRACK IN FRAME 380 AT STR 23L. REPAIRED PER EA 67-155568. 2 L 7 4 4F A20WE 1998041000164 19980410 00164 WP 1998 4 10 9805659992 1 19980203 A 5320 PRESSURE WEB DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 DURING L CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 110, LEFT SIDE AT THE OUTBOA RD VERTICAL BEAM ATTACH. REPAIRED PER EA 99-154771. 2 L 7 2 4F A6WE 1998041000165 19980410 00165 WP 1998 4 10 9805669992 1 19980310 A 5320 PRESSURE WEB DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 DURING L CHECK, FOUND CRACKS IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL AT FS 110 AT THE INBOARD AND OUTB OARD VERTICAL BEAMS, RIGHT SIDE. REPAIRED PER EA 99-154771. 2 L 7 2 4F A6WE 1998041000166 19980410 00166 WP 1998 4 10 9805679996 1 19980330 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 83 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M CHECK, FOUND CORROSION DOUBLER (P/N 5912350-20) AT STR 83, RBL 10. REPAIRED PER EA 99-156261. 2 L 7 2 4F A6WE 1998041000167 19980410 00167 WP 1998 4 10 9805689996 1 19980330 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 82 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M CHECK, FOUND CRACK IN DOUBLER (P/N 5912350-19) AT STR 82, LBL 10. REPAIRED DOUBLER PER EA 99-156261. 2 L 7 2 4F A6WE 1998041000168 19980410 00168 WP 1998 4 10 9805699996 1 19980314 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 313 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M CHECK, CORROSION AROUND FASTENERS IN FRAME 313 AND LONGERON 28R. REPAIRED PER EA 99-156259. 2 L 7 2 4F A6WE 1998041000169 19980410 00169 WP 1998 4 10 9805709163 1 19980401 A 7312 320115 HEAT VALVE DOUG DC9 DC914 3022034 WP PWA JT8 JT8D9 52048 NE LT ENGINE INOPERATIVE A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 8906E 45747 666806 DURING DESCENT AT 23,000 FEET, THE LEFT ENGINE FUEL HEAT VALVE FAILED TO CLOSE. OIL TEMPERATURE CLIMBED TO THE CAUTION RANGE. CREW PERFORMED A PRECAUTIONARY SHUTDOWN OF THE LEFT ENGINE. AIRCRAFT DIVERTED TO CMH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL HEAT VALVE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1998041000170 19980410 00170 WP 1998 4 10 9805719852 2 19980331 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LEFT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 761NC 47709 696669 DURING TAKEOFF ROLL AT 60 KNOTS, THE LEFT ENGINE EPR AND N1 INDICATIONS BEGAN DECREASING. CREW ABORTED TAKEOFF AND RETU RNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 1998041000172 19980410 00172 NE 1998 4 10 9805731154 2 19980330 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN O OTHER LD LANDING 1 GL 01 154US 46763 686165 DURING THE LANDING ROLLOUT AT APPROXIMATELY 80 KNOTS WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE E NGINE WAS SHUT DOWN AT APPROXIMATELY 40 KNOTS WITH THE EGT AT MAXIMUM FOR 10 SECONDS. THE ENGINE WAS BOROSCOPED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE AND FERRIED TO MSP FOR AN ENGINE CHANGE. EXACT REASON FOR THE EN GINE STALLS TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998041000173 19980410 00173 WP 1998 4 10 9805749751 1 19980402 A 3010 420115 PRESS SWITCH DOUG DC9 DC941 302207N WP WING ANTI-ICE ERRATIC A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 751NW 41640 13 47115 DURING CLIMB-OUT FROM DTW, AIRFOIL ICE PROTECTION PRESSURE ABNORMAL LIGHT ILLUMINATED UPON SELECTION OF WING ANTI-ICE. F LIGHT WAS DIVERTED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WING ICE PROTECTION AIR PRESSURE SWITCH. OP ERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998041000174 19980410 00174 WP 1998 4 10 9805759878 1 19980402 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP TAIL COMPT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041000175 19980410 00175 WP 1998 4 10 9805769995 1 19980401 A 3397 WIRE DOUG DC9 DC931 3022065 WP TAIL CONE BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8978E 47327 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS IN TAILCONE INOPERATIVE. REPAIRED BROKEN WIRE. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000176 19980410 00176 WP 1998 4 10 9805779758 1 19980402 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS IN AFT TAIL COMPARTMENT AND IN VENTRAL STAIR AREA INOPERATIVE . REPAIRED WIRING AT S3-156. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000177 19980410 00177 WP 1998 4 10 9805789930 1 19980402 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 OVERWING EMERGENCY EXIT LIGHT AT SEAT 12D INOPERATIVE. RESEATED CONNECTOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000178 19980410 00178 WP 1998 4 10 9805799930 1 19980402 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 EMERGENCY LIGHTS ON BOTH SIDES OF CATWALK INOPERATIVE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000179 19980410 00179 WP 1998 4 10 9805809944 1 19980401 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP TAIL CONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS IN TAILCONE AREA INOPERATIVE. REPLACED POWER SUPPLY. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000180 19980410 00180 SO 1998 4 10 COMA9810080 1 19980401 A 3260 922AA2YAVZ722 SENSOR EMB 120 EMB120 3260201 SO RT MLG MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 267CA 120259 RT MLG, GREEN DOWN INDICATION, CAME ON WITH GEAR RETRACTED. REPLACED THE RT MLG DOWNLOCK SENSOR. 2 L 7 2 4T RT A31SO 1998041000181 19980410 00181 SO 1998 4 10 COMA9810081 1 19980401 A 2434 30081001 GENERATOR EMB 120 EMB120 3260201 SO LT ENGINE FAILED A COMA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 259CA 9949 120252 UNUSUAL AND STRONG VIBRATION BETWEEN 12,500 AND 13,000 FEET. INSPECTED AIRCRAFT FOR CAUSE OF VIBRATION AND FOUND NO DEF ECTS. REPLACED LT ENGINE AUX GENERATOR FOR TROUBLE SHOOTING. 2 L 7 2 4T RT A31SO 1998041000182 19980410 00182 SO 1998 4 10 COMA9810082 1 19980331 A 3350 1011103 SIGN EMB 120 EMB120 3260201 SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 120233 EMERGENCY EXIT SIGN AT SEAT 5A IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998041000183 19980410 00183 SO 1998 4 10 COMA9810083 1 19980330 A 3260 SENSOR EMB 120 EMB120 3260201 SO LT MLG DIRTY A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 255CA 120238 THE LT MLG INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTION. LANDING GEAR WAS CYCLED AND 2ND RETRACTION WAS NORMAL. C OULD NOT DUPLICATE DISCREPANCY. CLEANED INDICATION SENSORS AND CONNECTIONS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1998041000184 19980410 00184 EA 1998 4 10 COMA9860070 1 19980331 A 3350 363782 LAMP CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951CA 7091 EMERGENCY FLOOR LIGHTING, ROW 2 IS INOP. REPLACED LIGHT STRIP. 2 L 7 2 4F RT A21EA 1998041000185 19980410 00185 EU 1998 4 10 WWMA9800065 1 19980402 A 2612 72111211000 DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 329AE 340B329 FLIGHT NR 5042 -BTR-DFW - CARGO SMOKE LIGHT ON CWP ILLUMINATED IN FLIGHT. CARGO EXTINGUISHER NR 1 WAS DISCHARGED. DIVE RTED TO AEX. REPLACE NR 1 CARGO FIRE BOTTLE AND FORWARD AND AFT FIRE DETECTORS. 2 L 7 2 4T RT A52EU 1998041000186 19980410 00186 EU 1998 4 10 WWMA9800064 1 19980329 A 2611 72111211000 DETECTOR SAAB SF340 340B 7860101 EU LAVATORY NO TEST A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 231AE 340B231 LAV SMOKE TEST IS INOPERATIVE. REPLACED LAV SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998041000187 19980410 00187 EU 1998 4 10 WWMA9800063 1 19980401 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 319AE 340B319 DURING PREFLIGHT, THE EMERGENCY LIGHT OVER SEAT 9A FAILED TO ILLUMINATE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A52EU 1998041000188 19980410 00188 EU 1998 4 10 WWMA9800062 1 19980325 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 339SB 340B339 DURING PREFLIGHT, THE EMERGENCY LIGHT OVER SEAT 11A FAILED TO ILLUMINATE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A52EU 1998041000189 19980410 00189 EU 1998 4 10 WWMA9800066 1 19980327 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 280AE 340B280 DURING PREFLIGHT, EMERGENCY FLOOR LIGHTS AT ROWS 6, 7, 8 AND OVERHEAD LIGHTS AT ROWS 8 AND 10 FAILED TO ILLUMINATE. REP LACED EMERGENCY POWER SUPPLY 22LN. 2 L 7 2 4T RT A52EU 1998041000190 19980410 00190 NM 1998 4 10 98FDEA00228 1 19980401 A 3610 DUCT DOUG MD11 MD11F 3023600 NM NR 1 PYLON CRACKED A FDEA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 25 613FE 48749 98-0083 - ON CLIMB-OUT FROM ANC THROUGH FL 400 ENG 1 FIRE ALERT CAME ON. FOLLOWED EMERGENCY PROCEDURE AND RETURNED TO A NC. ALL ENGINE, HYDRAULIC, PNEUMATIC AND ELECTRICAL SYSTEMS NORMAL. SUSPECT BLEED AIR LEAK IN ENG NR 1. FOUND DUCT IN PYLON CHAFFED BY T/R INTERLOCK HYD LINE ALSO CRACKS IN DUCT ADJACENT TO FLANGE ON IPC REF 36-14-80-01 FIG 220. REMOVED AND REPLACED BOTH DAMAGED DUCT ASSY LEAK AND OPS CKS GOOD ON ENG RUN. ALL COWLINGS SECURED. A/C OK FOR SERVICE. PART S REPLACED: DUCT ASSY, P/N BUM7011-537 DUCT ASSY, P/N 88033-1. 2 L 7 3 4F RT A22WE 1998041000191 19980410 00191 NM 1998 4 10 98FDEA00229 1 19980402 A 3610 CLAMP BOEING 727 727225 1384077 NM NR 3 ENGINE INOPERATIVE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 462FE 22550 ON CLIMBOUT WITH AIRCRAFT CLEAN AND CLIMB POWER SET AT APPROXIMATELY 7,000 FEET THE ENGINE NR 3 STRUT OVERHEAT LIGHT ILL UMINATED. COMPLIED WITH RED TAB PROCEDURE AND LIGHT WENT OUT AND STAYED OUT FOR REMAINING 30 MINUTE OF FLIGHT. FOUND 6 TH STAGE DUCT LEAKING AT CLAMP DOWNSTREAM OF CHECK VALVE. REMOVED AND REPLACED CLAMP, OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 3 4F A3WE 1998041000192 19980410 00192 NM 1998 4 10 98FDEA00225 1 19980331 A 2781 106081918 SWITCH BOEING 727 727227 1384078 NM NR 3 LE FLAP FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 494FE 21532 98-0080 CDG - AFTER TAKEOFF DURING FLAP RETRACTION TO 0 HAD FAILURE NR 3 LED FAILED TO RETRACT. PERFORMED APPROPRIATE C HECK LIST WITH NO RESOLUTION OF PROBLEM. DUMPED FUEL TO MAXIMUM LAND WEIGHT. NORMAL LANDING AT CDG. INSTALLED JUMPER CABLE ON NR 3 LEADING EDGE FLAP POSITION SWITCH AS PER MAINTENANCE MANUAL 27-82-0. OPERATION OF FLAPS AND SLATS PERFORM ED, ALL INDICATION NORMAL. NR 3 LEADING EDGE FLAP POSITION INDICATION SWITCH REPLACED PER MAINTENANCE MANUAL 27-82-1 AD JUSTMENT AND TEST PER SAME. ALL INDICATIONS NORMAL. 2 L 7 3 4F A3WE 1998041000193 19980410 00193 WP 1998 4 10 98FDEA00230 1 19980119 A 2621 89524002 FIRE BOTTLE DOUG DC10 DC1030F 3023504 WP NR 3 ENGINE BLOWN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 DURING B CHECK, FOUND NUMBER 2 LEFT ENGINE FIRE BOTTLE NUMBER 2 CARTRIDGE BLOWN DURING REMOVAL AND REPLACEMENT OF EXPIRE D CARTRIDGE. REMOVED AND REPLACED NR 2 ENGINE LEFT FIRE BOTTLE AND CARTRIDGES PER M/M 26-21-02 AND M/M 26-21-01. 2 L 7 3 4F RT A22WE 1998041000194 19980410 00194 WP 1998 4 10 ABXA9800291 1 19980309 A 5320 577991711 DOUBLER DOUG DOUG DC8 DC863F 302198F WP BS 105 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 INTERNAL FINGER DOUBLER CORRODED AND CRACKED AT STATION 105, LONGERON 31R. REPAIRED IAW ABX REA D853-22748 MR. 2 L 7 4 4F 4A25 1998041000195 19980410 00195 WP 1998 4 10 ABXA9800292 1 19980307 A 5320 9753785 CUSP DOUG DOUG DC8 DC863F 302198F WP BS 460-560 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 MAIN CABIN LOWER CUSP CORRODED BEYOND LIMITS AT STATION 460 TO STATION 560 RIGHT SIDE. REPAIRED IAW DC8 SRM 53-2-5. 2 L 7 4 4F 4A25 1998041000196 19980410 00196 WP 1998 4 10 ABXA9800293 1 19980223 A 5720 5769600 DOUBLER DOUG DOUG DC8 DC863F 302198F WP WS 597-603 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE SKIN INTERNAL DOUBLER BETWEEN STA XFS 597 AND XFS 603 IS CRACKED AT THE TAI EXHAUST HOLES. REPA IRED IAW DWG 5769600 AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998041000197 19980410 00197 WP 1998 4 10 ABXA9800294 1 19980228 A 5320 5613327105 ANGLE DOUG DOUG DC8 DC863F 302198F WP BS 25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 COCKPIT SUB FLOOR AT STATION -25 RBL 8, INTERCOSTAL IS CRACKED AT FWD END (FLOOR SUPPORT ANGLE). REPAIRED IAW DWG 56133 27 AND DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998041000198 19980410 00198 WP 1998 4 10 ABXA9800295 1 19980402 A 5320 991075521 WEB DOUG DOUG DC9 DC932F 3022067 WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 920, 921, 925, 940, AND 945 AT RBL 54. REPAIRED CUSP WEB IAW DC9 SRM 51-30-13, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998041000199 19980410 00199 WP 1998 4 10 ABXA9800296 1 19980402 A 5320 59560655 SLANT PANEL DOUG DOUG DC9 DC932F 3022067 WP BS 690 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND RIGHT SLANT PANEL STATION 690 CORRODED UNDER POTTED CAPS, AROUND THE FLOATING NUT-PLATES, BETWEEN RBL 22 AND RBL 44. REPLACED SLANT PANEL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041000200 19980410 00200 WP 1998 4 10 ABXA9800297 1 19980402 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041000201 19980410 00201 WP 1998 4 10 ABXA9800298 1 19980402 A 5313 59114269 LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LONGERON 12R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041000202 19980410 00202 WP 1998 4 10 ABXA9800299 1 19980402 A 5313 591140615 LONGERON DOUG DOUG DC9 DC932F 3022067 WP BS 180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LONGERON 3L CRACKED JUST AFT OF STATION 180. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041000203 19980410 00203 WP 1998 4 10 ABXA9800300 1 19980402 A 5280 59175331 PAN DOUG DOUG DC9 DC932F 3022067 WP LT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING C-CHECK, FOUND LEFT MAIN LANDING GEAR DOOR PAN CRACKED AT FORWARD SIDE. REPAIRED DOOR PAN IAW DC9 SRM 52-05. 2 L 7 2 4F A6WE 1998041000204 19980410 00204 SO 1998 4 10 SWIA971105 1 19980304 A 5350 FAIRING EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE WING/FUSELAGE DEPARTED A SWIA K NONE D INFLIGHT SEPARATION CR CRUISE 1 NM 07 204SW 120243 BOTTOM CENTER PANEL OF FUSELAGE (MID WING), FWD OF LEFT AIR CONDITIONING PACK, DEPARTED THE AIRCRAFT. (FERRIED FROM PIH TO SLC). INSTALLED NEW WING CENTER FAIRING PANEL, IAW MM 57-11-01. ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041000205 19980410 00205 SO 1998 4 10 SWIA971106 1 19980304 A 3610 BLEED LINE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT PACK RUPTURED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 194SW 120120 AFTER TAKEOFF, THE DUCT LEAK LIGHT ILLUMINATED, RETURNED TO LAX. MEL 32-21-1. REPLACED RUPTURED BLEED LINE AT RIGHT PAC K SHUT OFF VALVE. LEAK AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041000206 19980410 00206 SO 1998 4 10 SWIA971107 1 19980304 A 3020 DE-ICE EJECTORS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE DIRTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 227SW 120304 LEFT ENGINE INLET INOP LIGHT ILLUMINATED,RETURNED TO SBA. CLEANED LEFT ENGINE INLET EJECTORS. RAN ENGINES AND DE-ICE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041000208 19980410 00208 SO 1998 4 10 SWIA971109 1 19980308 A 3020 INLET DE-ICE EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 227SW 120304 RIGHT ENGINE AIR INLET DE-ICE FAILED IN FLIGHT. RETURNED TO LAX. OPERATED RIGHT ENGINE AIR INLET EXTENSIVELY, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041000209 19980410 00209 EA 1998 4 10 SWIA971110 1 19980309 A 3411 PITOT SYST CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT NOISE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 405SW 7029 IMMEDIATELY AFTER TAKEOFF FROM SLC, LEFT AND RIGHT IAS MESSAGES APPEARED FOLLOWED BY STALL FAIL, MACH TRIM ALSO HIGH PIT CH NOISE FOLLOWED BY VERY UNRELIABLE AIRSPEED INDICATION FROM CO-PILOTS AIRSPEED INDICATOR. AS AIRCRAFT SLOWED DOWN, LO UD NOISE WENT AWAY. RETURNED TO SLC. PITOT STATIC OPS CHECKS PITOT STATIC SYSTEM IAW MM 34-11-00. VERIFIED PITOT STAT IC DRAINS CONTAINED NO WATER. UNABLE TO DUPLICATE SYSTEM FAILURE OR HAVE ANY HIGH PITCHED NOISES. 2 L 7 2 4F 4 F RT A21EA E15NE 1998041000210 19980410 00210 NE 1998 4 10 SWIA971111 2 19980309 A 7261 OIL CAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE LEAKING A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 407SW 7034 LEFT ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE. DIVERTED TO CPR. ENGINE SHUT DOWN IAW QRH PROCEDURES. AFTER ARRIVAL IN CPR OIL LEVEL WAS CHECKED IN SHOW REFILL. ON SHUT DOWN THE PREVIOUS NIGHT IN CPR OIL LEVEL CHECKED NORMAL. RAN ENGINE FOUND LEFT ENGINE OIL RESERVOIR CAP TO BE LEAKING. REMOVED AND REPLACED RESERVOIR CAP. RAN ENGINE FOR 20 PLUS MINUTES AND ENGINE LEAK CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1998041000211 19980410 00211 NM 1998 4 10 P5CA9800745 1 19980331 A 5314 KEEL BEAM BOEING 747 747132 1384882 NM BS 1380 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 SHEET METAL DAMAGE TO UPPER KEEL BEAM WEB AT STATION 1380 IN THE RIGHT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CUT TING DOUBLERS AND TRIPLERS PER PAC MA 5310-24:01. 2 L 7 4 4F A20WE 1998041000212 19980410 00212 NM 1998 4 10 P5CA9800746 1 19980331 A 2911 26604725 ACCUMULATOR BOEING 747 747132 1384882 NM BS 1380 FAILED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 BRAKE ACCUMULATOR LOWER CAP BROKEN OFF COMPLETELY. REMOVED AND REPAIRED BRAKE ACCUMULATOR PER MM 32-41-09. PRECHARGED ACCUMULATOR PER MM 12-15-09. SYSTEM TESTS NORMAL PER MM 32-41-00. 2 L 7 4 4F A20WE 1998041000213 19980410 00213 NM 1998 4 10 P5CA9800747 1 19980331 A 5314 KEEL BEAM BOEING 747 747132 1384882 NM BS 1380 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 SHEET METAL DAMAGE TO LOWER KEEL BEAM AREA AND LOWER WEB AT STA 1380 RT BODY WHEEL WELL. REPAIRED DAMAGED SECTION BY CU TTING OUT DAMAGE AND FABRICATION FILLERS, DOUBLERS AND TRIPLERS AND REPLACING PER PAC MA NR 5310-24:10. 2 L 7 4 4F A20WE 1998041000214 19980410 00214 NM 1998 4 10 P5CA9800748 1 19980331 A 3610 39831021 ISOLATION VALVE BOEING 747 747122 1384872 NM LEFT INOPERATIVE A P5CA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 23 850FT 19755 LOW DUCT PRESS ON LEFT WING DURING START. ISOLATION VALVE DOES NOT CLOSE. REMOVE AND REPLACED ISOLATION VALVE. OPS CH ECK GOOD IAW MM 36-11-07. 2 L 7 4 4F A20WE 1998041000215 19980410 00215 WP 1998 4 10 RRXA98075 1 19980327 A 2420 RESISTOR DOUG DC8 DC871F 302199D WP NR 4 OVERHEATED A RRXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 WP 15 8087U 45977 ON LANDING, NR 4 GEN UNPARL'D LIGHT AND BUS POWER FAIL LIGHT ON, SMOKE IN COCKPIT. FOUND NR 4 25 WATT RESISTOR OVERHEAT ED, ENTERED AS DMI NR 803339 IAW MEL 24-1 CAT C DUE DATE 4-6-98 PLACARD INSTALLED. *S/D* SERVICED OIL CAVITIES ON NR 4 CSD/GEN ASSY. RESET CSD RAN ALL ENG'S. NR 4 GEN OPS CKS GOOD. PREFERENTIAL CK CKS GOOD. THIS CLEARS DMI NR 803339. 2 L 7 4 4F RT 4A25 1998041000216 19980410 00216 NM 1998 4 10 VNAA9803034 1 19980331 A 2121 011389502 FAN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT AC PACK FAILED A VNAA D RETURN TO BLOCK J M WARNING INDICATION OVER TEMP TX TAXI/GRND HDL 1 GL 07 426JS 58772 6356 3038 A LEFT HAND AIRCONDITIONING PACK OVERHEAT WARNING MESSAGE ILLUMINATED, DURING TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED T O THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND GROUND COOLING FAN IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-51-23. FUNCTIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998041000217 19980410 00217 NM 1998 4 10 CKSA98205 1 19980331 A 5320 SILL BOEING 727 727223 1384074 NM CARGO DOOR DAMAGED A CKSA B EMER. DESCENT O OTHER CR CRUISE 1 GL 23 729CK 19482 AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION AT FL310. CABIN ALTITUDE CONTINUED TO CLIMB 150 TO 300 FPM AT CRUISE. CARGO HEAT OUTFLOW VALVE CLOSED AND CABIN RATE INCREASED TO 1500 FPM UNCONTROLLABLY. AIRCRAFT DESCENDED FROM FL310 TO FL240, CABIN PRESSURE BEGAN TO RESPOND BELOW FL290, FLIGHT CONTINUED AT FL240, PRESSURIZATION CONTROL MANUAL. TRANSFERRED TO DMI LIST NR 88109098 IAW MEL 21-16-1A, PLACARDS INSTALLED. AUTO CONTROL IS WORKING FINE AFTER MAIN CARGO DOOR SILL REPA IR. CLEARED DMI NR 88109098 AUTO PRESSURIZATION PER FLT CREW INFORMATION ON PRESSURIZATION SATISFACTORY. 2 L 7 3 4F A3WE 1998041000229 19980410 00229 EU 1998 4 10 98ZZZX1373 1 19980126 A 3210 SHIM BRAERO DH125 BAE125800A 1500285 EU LT SIDESTAY WRONG PART A S JGVA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 09 961JC 4081 258062 DURING REPLACEMENT OF LT FAIRING STRUT PLATE, FOUND AN OLD SHIM INSTALLED BETWEEN BEARING ITEM 145 AND PLATE ITEM 135 ON THE LOWER LEG OF THE LT SIDESTAY LOOKING IN HAWKER ILLUSTRATED PARTS LISTING 32-10-00-30, PAGE 0. THERE SHOULD NOT BE A SHIM INSTALLED BETWEEN ITEM 145 AND ITEM 135. DURING THE INVESTIGATING OF THE .060 INCH SHIM, FOUND SHIM TO HAVE DEEP BRINELLING FROM RIDING ON BEARING. IN LOOKING IN THE IPC, WAS NOT ABLE TO FIND .060 INCH SHIM LISTED. THE ONLY SHIMS LISTED WERE .040 INCH, .020 INCH, .050 INCH, AND .010 INCH SHIMS; THEREFORE, AN IMPROPER SHIM WAS INSTALLED ON THE LT SI DESTAY. THIS AREA OF THE SIDESTAY SHOULD BE INSPECTED DURING THE REMOVAL OF SIDESTAY OR AT 48-MONTH INSPECTION. 2 L 7 2 4F RT A3EU 1998041000274 19980410 00274 NM 1998 4 10 USAA980109 1 19980228 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 540 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT 2 SKIN ATTACH FASTENER HOLES 5 INCHES TO 11 INCHES F OWARD OF BS 540 FRAME S15L STRINGER (FUSELAGE). INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1 AND EA 43631. (X) 2 L 7 2 4F A16WE 1998041000275 19980410 00275 NM 1998 4 10 USAA980110 1 19980228 A 5311 FRAME BOEING 737 737201 1384454 NM BS 294.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 46595 22273 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK IN BODY FRAME RADIUS BS 294.5, 5 INCHES BELOW S26R. IN STALLED FRAME REPAIR, REPAIRED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1998041000276 19980410 00276 NM 1998 4 10 AALA980109 1 19980113 A 5315 FLOOR BEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - CORROSION ON TOP OF FLOOR BEAM STA 380 RBL 5 - RBL 25. REMOVED CORROSION PER SRM 51-10-6. REPAIRED PER SRM 53-10 -8, PAGES 9-A AND 9-B. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998041000277 19980410 00277 NM 1998 4 10 AALA980110 1 19980113 A 5320 SILL BOEING 727 727223 1384074 NM BS 1176 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 872AA 21384 TUL - WEB AND CHORD ANGLE CORRODED 1 INCH IN DIAMETER, AREA BOTTOM SIDE 1176 CHORD ANGLE BL 6, VAULT DOOR LOWER SILL. R EMOVED CORROSION PER SRM 51-10-6. INSTALLED DOUBLER IAW SRM 51-40-2. TST: 54,792 HOURS. CYCLES: 33,779. (X) 2 L 7 3 4F A3WE 1998041000278 19980410 00278 NM 1998 4 10 F3LA98003 1 19980215 A 2780 NAS11048 BOLT BOEING 737 73736Q 1384409 NM LE FLAPS MISSING A A F3LA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 NM 03 307FL 28760 SEA - FLT 640 - AIR TURN BACK. FLIGHT CREW REPORTED LEADING EDGE FLAPS/SLATS WOULD NOT FULLY RETRACT WHEN TRAILING EDGE FLAPS SELECTED TO '0' DEGREES. MAINTENANCE FOUND BOLT (P/N NAS1104-8), NUT (P/N NAS6794W), AND WASHER (P/N 960D416) MI SSING FROM THE LEADING EDGE CONTROL VALVE (REF: BOEING 737-300 PARTS CATALOG 27-81-81-01). REPLACED NUT AND BOLT ASSEM BLY, RAN OPERATIONAL CHECK PER MM 27-81-00, PAGE 501, AND SYSTEM CHECKED OKAY. NOTE: 'THE BOLT IN QUESTION WAS LYING L OOSE IN THE PANEL AREA OF THE CONTROL VALVE WITH NO NUT OR WASHER IN SIGHT. THE BOLT CAME OUT OF THE ACTUATOR. TIME ON THE AIRCRAFT - LESS THAN 100 HOURS OUT OF BOEING, A NEW ONE. AEG, MIDO SAF5-300 ALERTED.....'. (X) 2 L 7 2 4F RT A16WE 1998041000279 19980410 00279 1998 4 10 VTZA98052 4 19980208 A 3418 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA RT STALL VANE TRIPPED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 624BR 7211 IAD/TPA - FLT 6681 - DURING CRUISE AT 0720 HOURS ON 2-8-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT AOA STALL VAN E HEAT FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET RT AOA CIRCUIT BREA KER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998041000280 19980410 00280 EA 1998 4 10 VTZA98029 1 19980127 A 5610 601R330339 WINDSCREEN CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A VTZA B EMER. DESCENT O OTHER DE DESCENT 1 EA 27 624BR 7211 IAD/RSW - FLT 6677 - DURING CRUISE ON 1-27-98 AT 1310 HOURS, EXPERIENCED A SHATTERING OF THE CAPTAIN'S WINDSCREEN. AIRC RAFT DECLARED AN EMERGENCY AND LANDED AT RSW WITH NO FURTHER PROBLEMS. MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE W AS DISPATCHED TO THE AIRCRAFT AND REMOVED AND REPLACED THE CAPTAIN'S WINDSCREEN. ALL REQUIRED CHECKS WERE ACCOMPLISHED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1998041000282 19980410 00282 EU 1998 4 10 MALA976074 1 19980403 A 7603 STOP HANDLE SAAB SF340 340B 7860101 EU FLIGHT IDLE PULLED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 420XJ 420 DURING CLIMB, FLIGHT IDLE LIGHT ILLUMINATED. MAINTENANCE INSPECTED, FOUND FLIGHT IDLE STOP HANDLE PULLED. RESET KNOB, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998041000283 19980410 00283 EU 1998 4 10 MALA976075 1 19980331 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, SEAT 1D EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998041000284 19980410 00284 1998 4 10 MALA976076 4 19980331 A 3425 6226342022 EHSI SAAB SF340 SF340A 7850100 EU RT COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 DURING FLIGHT, RIGHT HSI INOP. SCREEN IS BLACK. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED RIGHT EHSI, SYSTEM OPS GOOD. 2 L 7 2 4T RT A52EU 1998041000285 19980410 00285 EU 1998 4 10 MALA976077 1 19980331 A 2613 OVERHEAT LIGHT SAAB SF340 SF340A 7850100 EU LT TAILPIPE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 107XJ 340A107 ON CLIMB, LEFT TAILPIPE HOT WARNING LIGHT ILLUMINATED, COMPLETED QRH AND WARNING LIGHT EXTINGUISHED AFTER CLOSING BLEED VALVE. AIRCRAFT RETURNED TO ATW. MAINTENANCE PERFORMED 20 MIN RUN WITH BLEEDS ON-CND, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998041000286 19980410 00286 NM 1998 4 10 RAAA98B2020 1 19980327 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998041000287 19980410 00287 SO 1998 4 10 RAAA98E4008 1 19980326 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 PAX ROW 10 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998041000288 19980410 00288 SO 1998 4 10 RAAA98E4009 1 19980331 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 LT AND RT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHTS DUE FAILED. 2 L 7 4 4T 4A22 1998041000289 19980410 00289 SO 1998 4 10 RAAA98E8007 1 19980327 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FWD LT AND AFT LT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHTS DU E FAILED. 2 L 7 4 4T 4A22 1998041000290 19980410 00290 SO 1998 4 10 RAAA98E8008 1 19980327 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 PAX ROW 17 EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998041000291 19980410 00291 NM 1998 4 10 CALA9800619 1 19980402 A 5754 RIB BOEING 727 727227 1384078 NM NR 4 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 4 SLAT INBOARD END RIB. THE CRACKED AREA WAS REMOVED IAW SRM 51-30-2. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-40-2, AND 51-10-2. 2 L 7 3 4F A3WE 1998041000292 19980410 00292 NM 1998 4 10 CALA9800620 1 19980402 A 5720 ANGLE BOEING 727 727227 1384078 NM WS 130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 1 INCH CRACK IN CURVED ANGLE INSIDE LT WING INBOARD FIXED LEADING EDGE AT STA 130. A DOUBLER WAS INS TALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998041000293 19980410 00293 NM 1998 4 10 CALA9800621 1 19980402 A 5712 RIB BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A .75 INCH CRACK AT STIFFENER ON INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0. A DOUBLER WAS INS TALLED IAW SRM 51-40-4 AND 51-30-2. 2 L 7 3 4F A3WE 1998041000294 19980410 00294 NM 1998 4 10 CALA9800622 1 19980402 A 2782 ANGLE BOEING 727 727227 1384078 NM NR 2 SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 1.5 INCH CRACK IN INBOARD SUPPORT ANGLE AT UPPER SURFACE OF COVER BELOW LT WING NR 2 SLAT ACTUATOR. T HE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998041000295 19980410 00295 NM 1998 4 10 CALA9800623 1 19980402 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1049 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 2 INCH CRACK IN FLOOR SUPPORT FRAME IN AFT BAGGAGE BIN AT STA 1049, SRTINGER 27R. THE FLOOR SUPPORT FRAME WAS REMOVED, AN INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998041000296 19980410 00296 WP 1998 4 10 CALA9800624 1 19980402 A 5320 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 INSPECTION FOUND FORWARD BAGGAGE BIN DOOR PAN CORRODED. A LOWER PAN SPLICE REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 4 4. 2 L 7 2 4F A6WE 1998041000297 19980410 00297 WP 1998 4 10 CALA9800625 1 19980404 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 INSPECTION FOUND A 1.25 INCH CRACK AT FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. A NR 4 BEAM WAS INSTALLED IAW EA 5 240-01192. 2 L 7 2 4F A6WE 1998041000298 19980410 00298 WP 1998 4 10 CALA9800626 1 19980403 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 370 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71828 49488 INSPECTION FOUND FUSELAGE SKIN TORN AND MISSING A 1 X 1.5 SECTION JUST FORWARD OF FORWARD BAGGAGE BIN DOOR AT STA 370, L ONGERON 26R. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND ECRA 533 1-01020. 2 L 7 2 4F A6WE 1998041000299 19980410 00299 NM 1998 4 10 CALA9800627 1 19980403 A 5730 SKIN BOEING 727 727232 1384082 NM WS 250 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SCREW HOLE ON TOP OF LT WING FIXED LEADING EDGE CORRODED AT WS 250. THE CORROSION WAS REMOVED IAW SRM 57-20-1. THE CORRODED AREA OF SKIN WAS CUT OUT. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW AEROCORP ENGINEERING OR DER 04884. 2 L 7 3 4F A3WE 1998041000300 19980410 00300 NM 1998 4 10 CALA9800628 1 19980405 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND LOWER CHORD OF FLOORBEAM CORRODED AT STA 1130, RBL 0 TO RBL 60. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5310-03707. 2 L 7 3 4F A3WE 1998041000301 19980410 00301 WP 1998 4 10 CALA9800629 1 19980406 A 3350 EMBS1392 CHARGER DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND ZONE-A EMERGENCY LIGHT BATTERY PACK INOPERATIVE. THE EMERGENCY LIGHT CHARGER WAS REPLACED AND OPERATIO N CHECKED GOOD IAW MM 33-50-00. 2 L 7 3 4F A22WE 1998041000302 19980410 00302 NE 1998 4 10 9805819975 2 19980404 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE LEFT FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 9339 47382 649148 AFTER LIFTOFF, THE LEFT ENGINE N1 INDICATION DECREASED WITH ASSOCIATED VIBRATION. CREW SHUT DOWN THE LEFT ENGINE, RETUR NED TO DTW, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1998041000303 19980410 00303 NE 1998 4 10 9805829915 2 19980404 A 7532 658385 PRBC DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 965N 53683 6643 47417 666959 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EXPERIENCED AN UNKNOWN NOISE. CREW ABORTED TAKEOFF AND RETURNED TO THE GA TE. MAINTENANCE REPLACED THE LEFT ENGINE PRBC, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998041000304 19980410 00304 NE 1998 4 10 9805836603 2 19980401 A 7321 7591001 FUEL CONTROL BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE FAILED A NWAA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 GL 01 603US 70856 10023 19780 662452 DURING FINAL APPROACH AT 4000 MSL, THE NR 1 ENGINE FLAMED OUT. ONE RAPID RESTART WAS ATTEMPTED BUT WAS UNSUCCESSFUL. T HE APPROACH AND LANDING WAS COMPLETED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE INLET AND EXHAUST WITH NO TROUBLE FOU ND. THE FUEL CONTROL AND 8TH STAGE PNEUMATIC CHECK VALVE WERE CHANGED. THE FOLLOW-UP ENGINE RUN WAS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1998041000305 19980410 00305 EU 1998 4 10 9805843244 1 19980403 A 3350 321454 POWER SUPPLY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 344NW 13211 6345 388 TEST OF EMERGENCY LIGHT SYSTEM REVEALED EMERGENCY POWER SUPPLY 13WL INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPE RATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998041000306 19980410 00306 NM 1998 4 10 9805852284 1 19980403 A 3350 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 284US 21323 DURING PREFLIGHT, FOUND LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY AND CHARGER, OPERATIONAL CH ECK OK. 2 L 7 3 4F A3WE 1998041000307 19980410 00307 NM 1998 4 10 9805862715 1 19980405 A 3350 POWER SUPPLY BOEING 727 7272S7 138407Z NM CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 719RC 22490 DURING PREFLIGHT, FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY H9930, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998041000308 19980410 00308 NM 1998 4 10 9805872710 1 19980404 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 820EA 22557 DURING PREFLIGHT, FOUND CENTER MID CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY AND POWER SUPPLY, OPERATIONAL CH ECK OK. 2 L 7 3 4F A3WE 1998041000309 19980410 00309 WP 1998 4 10 9805889942 1 19980327 A 7711 JG298H1 EPR INDICATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D15 52051 NE LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 3991C 34506 5829 47175 657545 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE EPR INDICATION FROZE AT 1.5. CREW ABORTED TAKEOFF AND RETURNED TO THE GAT E. MAINTENANCE REPLACED THE LEFT ENGINE EPR INDICATOR, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998041000310 19980410 00310 WP 1998 4 10 9805899880 1 19980405 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 675MC 47651 PILOT REPORTED EMERGENCY AISLE LIGHTS REMAINED ILLUMINATED FROM SEAT ROW 20, AFT REGARDLESS OF FLIGHT DECK LIGHT SWITCH POSITION. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AT SEAT 15D, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041000311 19980410 00311 WP 1998 4 10 9805909877 1 19980405 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE TAIL COMPARTMENT POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041000312 19980410 00312 WP 1998 4 10 9805919872 1 19980405 A 3350 CONNECTOR DOUG DC9 DC951 3022051 WP CABIN DISCONNECTED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, FOUND FLOOR PROXIMITY EMERGENCY LIGHT INOPERATIVE AT SEAT ROW 6. MAINTENANCE RECONNECTED CONNECTOR L OCATED UNDER SEAT ROW 6, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041000313 19980410 00313 1998 4 10 9805929988 4 19980404 A 2565 13621224 SLIDE BOTTLE DOUG DC9 DC931 3022065 WP CABIN LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8944E 47964 2488 47167 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EVACUATION SLIDE BOTTLE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998041000314 19980410 00314 WP 1998 4 10 9805939925 1 19980404 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000315 19980410 00315 NM 1998 4 10 QXEA9800446 1 19980330 A 3350 6038443 BATTERY DHAV 82410191011 DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 347PH 14596 457 480 SEVERAL FLOOR EMERGENCY LIGHTS AND ONE EXIT SIGN AT THE LEFT EMERGENCY EXIT HATCH ARE INOP. REPLACED BATTERY POWER SUPP LY AT 3352 PS2 POSITION, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998041000316 19980410 00316 NM 1998 4 10 QXEA9800447 1 19980330 A 3350 10005511 LIGHT DHAV 82510202001 DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 828PH 7588 1027 287 COCKPIT EMERGENCY LANTERN INOP. REPLACED LANTERN, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998041000317 19980410 00317 NM 1998 4 10 QXEA9800448 1 19980329 A 5210 SCREW DHAV DHC8 DHC8102 2809003 NM PAX DOOR LOOSE A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 816PH 54 MAIN CABIN DOOR IS DIFFICULT TO OPEN. INSPECTED AND FOUND A LOOSE SCREW AT THE FORWARD HANDRAIL WHICH WAS BLOCKING THE DOOR FROM EXTENDING FULLY. TIGHTENED SCREW, OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998041000318 19980410 00318 EU 1998 4 10 QXEA9800449 1 19980330 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 491US 11156 WING EMERGENCY EXIT HANDLE LIGHT ON THE LEFT SIDE OF THE AIRCRAFT IS INOP (BOTH LAMPS). RELAMPED, OPERATIONAL CHECKS GO OD. 2 L 7 2 4F RT A20EU 1998041000319 19980410 00319 NM 1998 4 10 QXEA9800453 1 19980331 A 3260 841005 PSEU DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTION A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 814PH 9786 1474 43 AFTER TAKEOFF, WHEN THE LANDING GEAR WAS SELECTED UP, ALL GEAR INDICATION LIGHTS WENT OUT NORMALLY. AFTER ABOUT 5 SECON DS THE LEFT GEAR DOOR LIGHT ILLUMINATED. VISUAL INSPECTION CONFIRMED THE GEAR DOOR TO BE OPEN. CYCLED LANDING GEAR AND THE GEAR DOOR CLOSED. INSPECTED AIRCRAFT AND FOUND SAFE FOR A FERRY FLIGHT TO PDX. REPLACED THE PSEU, OPERATIONAL CHE CKS GOOD. 2 H 7 2 4T RT A13NM 1998041000320 19980410 00320 EU 1998 4 10 QXEA9800454 1 19980331 A 3350 CONNECTOR GRIMES 1012721 FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 ALL EMERGENCY LIGHTS ON THE PASSENGER SEAT SIDES ARE INOP. FOUND CORRODED WIRE SPLICES AT SEAT ROWS 1, 9 AND 14. REPAI RED WIRING AND CONNECTIONS, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998041000321 19980410 00321 EU 1998 4 10 QXEA9800455 1 19980331 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 OVERHEAD EMERGENCY LIGHT AT ROW 10 HAS AN INOP 28 VOLT BULB. RELAMPED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998041000322 19980410 00322 NM 1998 4 10 QXEA9800456 1 19980403 A 3350 6038443 BATTERY DHAV 82410191011 DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 349PH 486 FORWARD LEFT EXTERNAL EMERGENCY LIGHT IS INOP. REPLACED PS1 BATTERY PACK, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998041000323 19980410 00323 NM 1998 4 10 98FDEA00231 1 19980403 A 5320 65159752 FORGING BOEING 727 72722 1384002 NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 189FE 19082 WHILE WORKING NR 0441, FOUND CORROSION ON BS 870 FORGING, RBL 57, WL 168. *S/D* REMOVED AND REPLACED RIGHT HAND BS 870 FITTING STR 9 TO WL 156 IAW FED-EX NR 7-5310-38683. 2 L 7 3 4F A3WE 1998041000324 19980410 00324 NM 1998 4 10 98FDEA00232 1 19980403 A 5411 652076127 RIB BOEING 727 727232 1384082 NM BS 1283 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 499FE 21018 RIB CRACKED AT BS 1283 AT 7 O'CLOCK POSITION ON S-DUCT. *S/D* REPAIRED RIB AT BS 1283 AT 7 O'CLOCK POSITION ON 5 DUCT IAW FED-EX SRM 54-10-3. 2 L 7 3 4F A3WE 1998041000325 19980410 00325 NM 1998 4 10 98FDEA00234 1 19980403 A 3610 CLAMP BOEING 727 727225 1384077 NM NR 3 ENGINE LOOSE A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 462FE 22550 ON CLIMBOUT PASSING APPROXIMATELY FLIGHT LEVEL 270, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. LIGHT WENT OUT WHEN NR 3 POWER LEVER PULLED TO IDLE. RESTORED POWER AND LIGHT DID NOT COME BACK ON. FOUND ONE CLAMP LEAKING AT CHECK VALVE GOIN G TO AIR CLEANER. REPOSITIONED CLAMP AND TIGHTENED UP LEAK CHECKED GOOD. NOT IN LOG BOOK BUT LEAK AT CLAMP GOING TO PE RCOOLER, NOT AIR CLEANER ON 8TH STAGE BLEED AIR LINE. 2 L 7 3 4F A3WE 1998041000326 19980410 00326 NM 1998 4 10 98FDEA00235 1 19980404 A 3610 VALVE BOEING 727 727225 1384077 NM NR 3 ENGINE LEAKING A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 462FE 22550 ON CLIMBOUT, ENGINE NR 3 STRUT OVERHEAT LIGHT CAME ON. COMPLETION OF RED TABS EXTINGUISHED LIGHT. OPERATED NR 3 ENGINE WITH NO FURTHER ILLUMINATION OF LIGHT. NR 3 BLEED AND NR 2 PACK TURNED OFF AND LEFT OFF PER RED TABS. REMOVED PYLON P ANELS 5501-5502 FROM RIGHT SIDE FOUND 8TH STAGE BLEED CHECK VALVE LEAKING DOWN STEAM SIDE OF VALVE. INSTALLED 2 NEW GAS KETS IN BLEED CHECK VALVE LEAK CHECKS GOOD RAN NR 3 ENGINE PER JET RUN HANDBOOK OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1998041000327 19980410 00327 NM 1998 4 10 98FDEA00236 1 19980330 A 5311 FRAME BOEING 727 727227 1384078 NM BS 680 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 483FE 21465 FWD CARGO BS 680, STR 23L FRAME HAS DAMAGED (DENT). INSTALLED 7075-T6 DOUBLER (15 INCHES) IN FWD CARGO BS 680, STR 23L FRAME PER SRM 53-10-4. 2 L 7 3 4F A3WE 1998041000328 19980410 00328 NM 1998 4 10 98FDEA00237 1 19980330 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 483FE 21465 BS 720, STRINGER 28L, CORROSION ON FUSELAGE SKIN AROUND NUT PLATE AND AREA WHERE SEALANT IS POURED ON ACFT SKIN. REMOVE D DAMAGED AREA, ALODINED AND PRIMED AREA, INSTALLED EXTERNAL REPAIR DOUBLER FROM .071 2024T3 MATERIAL, AS PER SRM 53-30- 3 PAGE 8 AND 53-30-3 PAGE 14 TABLE I AND II. 2 L 7 3 4F A3WE 1998041000329 19980410 00329 NM 1998 4 10 98FDEA00238 1 19980330 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1010 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 483FE 21465 BS 1010, STR 27L CORRODED. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-3 AT BS 1010, STR 27L. 2 L 7 3 4F A3WE 1998041000330 19980410 00330 NM 1998 4 10 98FDEA00239 1 19980402 A 5311 FRAME BOEING 727 727227 1384078 NM BS 490 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 483FE 21465 AFT LWR CARGO BELL FRAME DENTED AND BENT AT BS 490 BETWEEN STR 25 AND 26L. FABRICATED AND INSTALLED DOUBLER PER SRM 53- 10-4. 2 L 7 3 4F A3WE 1998041000331 19980410 00331 NM 1998 4 10 98FDEA00240 1 19980327 A 5311 FRAME BOEING 727 727233 138408A NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 UPPER LOBE, BELTFRAME AT BS 520, RBL 65 DENTED OUT OF LIMITS. REMOVED DAMAGE AT BELTFRAME BS 520, RBL 65 AND INSTALLED DOUBLER AS PER SRM 51-40-3 PG 1-6 AND EA 7531028295. 2 L 7 3 4F RT A3WE 1998041000332 19980410 00332 NM 1998 4 10 98FDEA00241 1 19980327 A 5311 FRAME BOEING 727 727233 138408A NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 UPPER LOBE BELTFRAME AT BS 500, RBL 65 DENTED OUT OF LIMITS PER EA 7531028295. REMOVED DAMAGE AT BELTFRAME BS 500, RBL 65 AND INSTALLED DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7531028295. 2 L 7 3 4F RT A3WE 1998041000333 19980410 00333 NM 1998 4 10 98FDEA00242 1 19980402 A 5330 SKIN BOEING 727 727233 138408A NM BS 660 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 FUSE SKIN CORRODED AT BS 660 BETWEEN STR 28L TO W8R. REMOVED CORROSION. REMOVED SECTION OF FUSE SKIN I/B OF STR 28R. I NSTALLED REPAIR DOUBLER PER SRM 53-30-3. 2 L 7 3 4F RT A3WE 1998041000334 19980410 00334 NM 1998 4 10 98FDEA00243 1 19980402 A 5311 FRAME BOEING 727 727233 138408A NM BS 540 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 UPPER LOBE BS 540, RBL 65, BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-30. 2 L 7 3 4F RT A3WE 1998041000335 19980410 00335 NM 1998 4 10 98FDEA00244 1 19980402 A 5311 FRAME BOEING 727 727233 138408A NM BS 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 UPPER LOBE, BS 600, RBL 65 BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-3. 2 L 7 3 4F RT A3WE 1998041000336 19980410 00336 NM 1998 4 10 98FDEA00245 1 19980402 A 5311 FRAME BOEING 727 727233 138408A NM BS 580 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 UPPER LOBE BS 580, RBL 65 BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 A ND SRM 53-40-3. 2 L 7 3 4F RT A3WE 1998041000337 19980410 00337 NM 1998 4 10 98FDEA00246 1 19980401 A 5320 BEAM BOEING 727 727233 138408A NM BS 743 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 A/C BAY, BS 743 CHORD ABOVE DELTA BEAM, UPPER SURFACE CORRODED LBL - RBL 12. REMOVED CHORD ANGLE AND REINSTALLED WITH N EW CHORD ANGLE PER SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998041000338 19980410 00338 NM 1998 4 10 98FDEA00247 1 19980402 A 5320 BEAM BOEING 727 727233 138408A NM BS 743 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 A/C BAY, BS 743, RBL 8 HEAVY CORROSION ABOVE DELTA BEAM, LWR SURFACE OF PLATE AT FWD ROW OF FASTENERS. REMOVED CORROSIO N, TREATED, INSTALLED DOUBLER PER SRM 51-40-02 OVER DAMAGED AREA. 2 L 7 3 4F RT A3WE 1998041000339 19980410 00339 NM 1998 4 10 98FDEA00248 1 19980402 A 5320 BEAM BOEING 727 727233 138408A NM BS 750 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 A/C BAY CORROSION ABOVE DELTA BEAM BS 750, RBL 6, AROUND ACCESS PLATE 3210. REMOVED CORROSION, TREATED, INSTALLED DOUBL ER OVER AREA PER SRM 51-40-2. 2 L 7 3 4F RT A3WE 1998041000340 19980410 00340 WP 1998 4 10 ABXA9800301 1 19980316 A 5730 5769857 SKIN DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE BETWEEN PYLONS INTERNAL UPPER DOUBLER IS CRACKED ABOVE SLOT ACTUATOR. REPAIRED IAW DC8 SRM 51-3- 0 AND 51-1-20D. 2 L 7 4 4F 4A25 1998041000341 19980410 00341 WP 1998 4 10 ABXA9800302 1 19980315 A 5320 577991711 DOUBLER DOUG DOUG DC8 DC863F 302198F WP BS 450 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FINGER DOUBLER CRACKED AT STATION 450, LONGERON 31L. CORROSION OUT OF LIMITS. REPAIRED IAW ABX REA D853-22748. 2 L 7 4 4F 4A25 1998041000342 19980410 00342 WP 1998 4 10 ABXA9800303 1 19980314 A 5320 3649114N FITTING DOUG DOUG DC8 DC863F 302198F WP BS 920 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 CORRODED VERTICAL FITTING RBL 65 STATION 920. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998041000343 19980410 00343 WP 1998 4 10 ABXA9800304 1 19980315 A 5320 97558851 SHEAR TIE DOUG DOUG DC8 DC863F 302198F WP BS 1000 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FORWARD SHEAR TIE AT STATION 1000 HAS HEAVY CORROSION AT LONGERON 33R. REPAIRED IAW DC8 SRM 53-20-0 AND DWG 9755888. 2 L 7 4 4F 4A25 1998041000344 19980410 00344 WP 1998 4 10 ABXA9800305 1 19980313 A 5313 56138627 LONGERON DOUG DOUG DC8 DC863F 302198F WP BS 25 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LONGERON 31R AT STATION 25 HAS HEAVY CORROSION. REPAIRED IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1998041000345 19980410 00345 WP 1998 4 10 ABXA9800306 1 19980307 A 5320 3750257IN SPLICE DOUG DOUG DC8 DC863F 302198F WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LONGERON 31L SPLICE FITTING CRACKED BETWEEN STATION 440 TO 460. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998041000346 19980410 00346 WP 1998 4 10 ABXA9800307 1 19980312 A 5712 RIB DOUG DOUG DC8 DC863F 302198F WP WS 354 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE RIB CRACKED AT WS 354 UPPER AFT. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998041000347 19980410 00347 WP 1998 4 10 ABXA9800308 1 19980220 A 5313 1415997 LONGERON DOUG DOUG DC8 DC863F 302198F WP BS 1746 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LONGERON 32L CORRODED BEYOND LIMITS AT STATION 1746 TO 1756. REPAIRED IAW DC8 SRM 53-22. 2 L 7 4 4F 4A25 1998041000348 19980410 00348 WP 1998 4 10 ABXA9800309 1 19980211 A 5711 5597841502 SPAR DOUG DOUG DC8 DC863F 302198F WP WS 555 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING REAR SPAR UPPER CHORD AT STATION XRS 555 HAS EXFOLIATION CORROSION. REPAIRED IAW ABX REA D857-22332. 2 L 7 4 4F 4A25 1998041000349 19980410 00349 WP 1998 4 10 ABXA9800310 1 19980312 A 5313 52641520 STRINGER DOUG DOUG DC8 DC863F 302198F WP BS 1460 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STRINGERS 34R AND 34L AT STATION 1460 CORRODED BEYOND LIMITS. REPAIRED IAW DC8 SRM 53-2-0 AND 51-1-20. 2 L 7 4 4F 4A25 1998041000350 19980410 00350 WP 1998 4 10 ABXA9800311 1 19980401 A 3260 59151695512 UPLATCH DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A ABXA K NONE N FALSE WARNING TO TAKEOFF 1 GL 23 980AX 47176 AFTER GEAR RETRACTION ON TAKEOFF, THE RIGHT GEAR UNSAFE LIGHT REMAINED ON. RECYCLED GEAR AND PERFORMED UPLATCH CHECK WI TH NORMAL INDICATION. REPLACED RIGHT MAIN LANDING GEAR DOOR UPLATCH ASSEMBLY IAW DC9 MM 32-31-4. 2 L 7 2 4F A6WE 1998041000351 19980410 00351 WP 1998 4 10 SCNA98029 1 19980226 A 5530 FASTENER DOUG DC10 DC1015 3022118 WP VERT STAB SHEARED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A SCHEDULED MAINTENANCE INSPECTION, THE AFT LOWER RIGHT HAND FASTENER WAS FOUND SHEARED OFF ON THE NUT SIDE FOR T HE NUMBER FOUR BANJO FITTING ATTACHMENT. THE AREA WAS REWORKED IN ACCORDANCE WITH SERVICE BULLETIN DC10-55-023 REVISION TWO. 2 L 7 3 4F A22WE 1998041000352 19980410 00352 1998 4 10 ARWA980401 4 19980331 A 3441 452080052141 INU LKHEED 1011 1011385115 5265015 WP NR 2 INOPERATIVE A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 307GB 193U1131 F/O ADI FAILED FULL NOSE UP. AFTER T/O WINDSHEER ALERT WARNING ON AT 50 FT ANGLE AND 1000 ON APPROACH. FLAP ASSEMETRY DET FOULT LIGHT ON DURING FLAP RETRACTION. DURING CLIMBOUT L 5, 6 AND R 5, 6 SPOILER AND ROLL SPOILER LIGHT ON, PUSH L IGHT ON. REMOVED AND REPLACED NR 2 INU CHECKED ON GROUND NORMAL IAW 34-43-00. FOUND EXCELENOMETER LOOSE SECURED SYSTEM CHECKED NORMAL MANY TIMES IAW MM 34-62-00. CYCLED FLAPS UNABLE TO DUPLICATE FOULT. I.A.W. 27-51-00. COMPARATOR RESE T. CYCLE SPOILER UNABLE TO DUPLICATE FAULT IAW MM 27-62-00. 2 L 7 3 4F A23WE 1998041000353 19980410 00353 1998 4 10 ARWA980402 4 19980402 A 3418 2299006010 AOA SENSOR LKHEED 1011 1011385115 5265015 WP E/E COMPT MALFUNCTIONED A ARWA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 307GB 055 193U131 WINDSHEAR WARNING COMES ON SHORTLY AFTER TAKEOFF AND AT APPROX 1.000 DURING LANDING APPROACH. REMOVED AND REPLACED AOA SENSORS. REMOVED AND REPLACED LONGITUDINAL ACCELEROMETERS. OPS CHECK NORMAL AS PER MM 34-62-00 AND WINDSHEAR 060-4033. (M) 2 L 7 3 4F A23WE 1998041000354 19980410 00354 NM 1998 4 10 VNAA9804004 1 19980405 A 2913 42086 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BLUE HYD SYST FAILED A VNAA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 427JS 3039 EN ROUTE, THE AIRCRAFT DISPLAYED A BLUE MAIN HYDRAULIC PUMP AND AN AMBER EMERGENCY PARK BRAKE ACCUMULATOR WARNING MESSAG E. THE AIRCRAFT LANDED IN PIT AS SCHEDULED. MAINTENANCE INSPECTED AND REPLACED THE MAIN HYDRAULIC MOTOR AND PUMP ASSEM BLY IAW DORNIER MM 29-11-04. OPERATION AND LEAK CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998041000356 19980410 00356 EU 1998 4 10 CA980325047 1 19980324 A 5330 HC537H12100 SKIN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FRAME 12 & 14 WRINKLED W K NONE O OTHER IN INSP/MAINT 1 CA 30524 5099 (CAN) SEVERAL AREAS OF WRINKLES OR OIL CANNING WERE FOUND. THE FUSELAGE ROOF CANOPY SKIN BETWEEN FRAMES 12 AND 14. NO HEAVY LANDINGS REPORTED. NO OTHER ADDITIONAL DAMAGE FOUND. ROOF CANOPY SKIN REPLACED. PART TC: 38,948. AIRCRAFT TT: 29,849 HOURS. 2 H 7 4 4F 4 F RT A49EU E6NE 1998041000357 19980410 00357 EU 1998 4 10 CA980325046 1 19980324 A 2510 HC251H0177000 BRACKET HC251H0078 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE O/H ELECT PANEL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 30524 5099 (CAN) ON REMOVAL OF COCKPIT OVERHEAD PANEL TO FACILITATE STRUCTURAL REPAIR, BOTH THE LEFT AND RIGHT AFT SUPPORT MOUNTING BRACKETS FOR THE OVERHEAD ELECTRICAL PANEL WERE FOUND CRACKED. IPC 25-10-71-01, FIG.1, ITEMS 55 AND 60. 2 H 7 4 4F 4 F RT A49EU E6NE 1998041000358 19980410 00358 WP 1998 4 10 CA980325042 1 19980307 A 3610 LJ28020 DUCT LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENG NAC DETACHED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA 10059 (CAN) DURING CRUISE, NR 2 ENG NACELLE PYLON OVERHEAT LIGHTS CAME ON BOTH A AND B CHANNELS. PLUS CAWP AND THRUST REVERSER LIGHT ON. ENG USED UNDER REDUCED POWER. AFT DUCTING CONNECTING TO PRESSURE REGULATING AND SHUT OFF FOUND COMPLETELY D ETACHED. RECONNECTED, SERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 1998041000359 19980410 00359 EU 1998 4 10 CA980325041 1 19980224 A 2916 1Q2398 RESEVOIR 1Q2398 BRAERO 748 HS7482B 1500248 EU HYD SYS CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 8592 R3749265873 (CAN) HYDRAULIC RESERVOIR CRACKED AT FOOT WELD AREA. REPLACED. PART TC: 11,438. 2 L 7 2 3T A24EU 1998041000360 19980410 00360 SW 1998 4 10 CA980325038 1 19980319 A 2740 2743052003 TRUNNION BOLT FRCHLD SA227 SA227CC SW MAIN PIVOT LOOSE W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 7766 (CAN) PILOT COMPLAINED OF VIBRATIONS IN THE TAIL WHEN PITCH TRIMMING AT HIGHER SPEEDS. INSPECTION FOUND THAT THE STABIL IZER HAD MORE THAN ACCEPTABLE PLAY. THE MAIN PIVOT INNER AND OUTER BOLTS WERE FOUND FAR BELOW THE SPECIFIED TORQUE AS O UTLINED IN THE FAIRCHILD MM. PART TC: 9,934. 2 L 7 2 4T RT A18SW 1998041000361 19980410 00361 NM 1998 4 10 CA980325013 1 19980324 A 3411 PITOT HEAD BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE LT ELEV FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 707367 (CAN) AIRCRAFT RETURNED TO BLOCKS DUE LT ELEVATOR PITOT PROBE HEAT INOP, REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998041000362 19980410 00362 NM 1998 4 10 CA980325012 1 19980324 A 2150 6806404 ACM ALLIED 6806404 BOEING 767 767375 NM LT PACK SEIZED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 35304 371046 (CAN) A/C RETURNED TO GATE DUE LT PACK TEMP EICAS MESSAGE AND LT PACK INOP LIGHT ON. LT ACM REPLACED. 2 L 7 2 4F RT A1NM 1998041000363 19980410 00363 NM 1998 4 10 CA980325010 1 19980323 A 2430 GENERATOR BOEING 747 7474F6 NM NR 4 WIRING W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) HISTORY OF NR 4 GEN AND BUS NR 4 FAULT PROBLEMS. MANY UNITS CHANGED, NO FIX, HIGH RESISTANCE BETWEEN NR 4 GCU AND CURRENT LIMITER, ONGOING. 2 L 7 4 4F RT A20WE 1998041000364 19980410 00364 EA 1998 4 10 CA980325005 1 19980210 A 5343 TUBING DHAV DHC2 DHC2MK1 2800102 EA LT MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 25282 (CAN) FORWARD LEFT HAND LANDING GEAR ATTACH POINT WAS FOUND CORRODED OUT BEHIND THE FLOAT FITTING TUBE AND ATTACH FITTIN G HAD LITTLE OR NO METAL LEFT. SB 2/49 WAS COMPLIED WITH AND 'BIRD CAGE' WAS REPAIRED IN OTHER AREAS. THIS AREA NOT CA LLED UP IN SB. THIS IS SECOND FINDING. AIRCRAFT TT: 24,651 HOURS. 1 H 7 1 3R A806 1998041000365 19980410 00365 EA 1998 4 10 CA980325004 1 19980119 A 5343 TUBING DHAV DHC2 DHC2MK1 2800102 EA GEAR ATTACH CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 22603 (CAN) FORWARD LEFT HAND LANDING GEAR ATTACH POINT FOUND CORRODED OUT BEHIND THE FLOAT FITTING. TUBE AND FITTING ATTACHIN G POINT HAD LITTLE OR NO METAL LEFT. SB 2/49 WAS COMPLIED WITH BUT THIS AREA IS NOT INSPECTED IN THE SB. AIRCRAFT TT: 21,704 HOURS. 1 H 7 1 3R A806 1998041000366 19980410 00366 WP 1998 4 10 CA980318054 1 19980310 A 5280 1530924187 DOORS LKHEED 1011 1011385114 WP MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING WALK AROUND, A 5 INCH CRACK WAS FOUND IN THE AFT LOWER CORNER OF ONE OF THE MAIN GEAR FIXED DOORS, THE OTHE R DOOR ALSO CRACKED. BOTH REPAIRED PER SB093/SK52-208. ACFT TT: 46,948 HOURS. 2 L 7 3 4F A23WE 1998041000367 19980410 00367 EU 1998 4 10 CA980318051 1 19980305 A 5412 PANEL AIRBUS 310 A310304 EU LT WHEEL WELL DAMAGED W K NONE D INFLIGHT SEPARATION LD LANDING 1 CA (CAN) LEFT HAND WHEEL WELL BULK HEAD PANEL FELL OFF AND DAMAGED. PANEL REPLACED. AIRCRAFT TT: 41,402 HOURS. 2 L 7 2 4F RT A35EU 1998041000368 19980410 00368 EU 1998 4 10 CA980318050 1 19980227 A 2810 DOOR AIRBUS 310 A310304 EU FUEL PANEL MISSING W K NONE D INFLIGHT SEPARATION LD LANDING 1 CA (CAN) FUEL PANEL DOOR FOUND MISSING AFTER A/C LANDED. NEW PANEL INSTALLED ON RETURN TO HOME BASE. 2 L 7 2 4F RT A35EU 1998041000369 19980410 00369 EU 1998 4 10 CA980318049 1 19980308 A 3230 664700500A4G SENSOR AIRBUS 320 A320212 EU GEAR OUT OF ADJUST W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) LGCIU 1 AND 2 FAULT INDICATION UPON SELECTING LANDING GEAR UP. GRAVITY EXTENSION CARRIED OUT SUCCESSFULLY. MAINT ENANCE ACTION INVOLVED ADJUSTING PROXIMITY SENSOR 35GA AND REPLACING LGCIU NR 1. 2 L 7 2 4F RT A28NM 1998041000370 19980410 00370 NM 1998 4 10 CA980317046 1 19980203 A 2913 6507406 PUMP ABEX 6507506 BOEING 707 727100 1384036 NM PWA JT8 JT8D7B 52053 NE NR 2 ENG HYD FAILED W O OTHER K FLUID LOSS DE DESCENT 1 CA 152173K 655044 (CAN) AT TOP OF DESCENT, AIRCRAFT BEGAN TO LOSE A-SYSTEM HYDRAULIC FLUID, A-SYSTEM PRESS FLUCTUATING BETWEEN 3,000 AND 2 ,500 PSI. ACFT STOPPED ON RUNWAY AND T OWED TO RAMP. FOUND HEAVY LEAK AT NR 2 ENG HYDRAULIC PUMP AND NR 1 CASE DRAIN H AD CARBON RUBBER CONTAMINANTS. BOTH PUMPS AND CASE DRAIN FILTER REPLACED. SYSTEM SERVICED AND LEAK CHECK CARRIED OUT, A/C SERVICEABLE. 2 L 7 3 4F 4 F RT A3WE E2EA 1998041000371 19980410 00371 NM 1998 4 10 CA980317039 1 19980316 A 2133 7110033 VALVE HAMSTD 7110033 BOEING 737 7372T7 NM PWA JT8 JT8D17 52049 NE OUT FLOW DIRTY W O OTHER J WARNING INDICATION TO TAKEOFF 1 CA 35906 165687 708808 (CAN) AT TAKEOFF, PRESSURIZATION SYSTEM AUTO FAIL LIGHT CAME ON. THROUGH 5,000 FEET, RESET SYSTEM AND OPERATED NORMALLY FOR REST OF FLIGHT. OUTFLOW VALVE REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1998041000372 19980410 00372 WP 1998 4 10 CA980317038 1 19980313 A 5244 H2024B SWITCH DOUG DC10 DC1030 3023501 WP ASSORY DOOR INTERMITTENT W A D UNSCHED LANDING RETURN TO BLOCK P NO WARNING INDICATION CL CLIMB 1 CA (CAN) UNABLE TO PRESSURIZE A/C AFTER TAKEOFF WITH OUTFLOW VALVE CLOSED. ON RETURN TO DEPARTURE DOCK, FOUND CENTER ACCES SORY DOOR OPEN. DOOR SWITCH WAS INTERMITTENT AND GAVE NO WARNING INDICATION. SWITCH REPLACED. 2 L 7 3 4F A22WE 1998041000373 19980410 00373 1998 4 10 CA980317036 4 19980312 A 2565 5WD26010040 SLIDE DOUG DC10 DC1030 3023501 WP LOWER GIRT TORN W K NONE L NO TEST IN INSP/MAINT 1 CA (CAN) SLIDE DEPLOYED AS PART OF SAMPLING PROGRAM. DEPLOYMENT NORMAL UNTIL TIE BACK SEPARATION. PRESSURE LOST IN LOWER TUBE DUE TO 14 INCH TEAR AT RT EDGE OF LOWER GIRT ASSY. 2 L 7 3 4F A22WE 1998041000374 19980410 00374 NM 1998 4 10 CA980317035 1 19980313 A 2750 MS172272 WASHER 65502535 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE TABS WORN W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 2592 148 687733 (CAN) AIRCRAFT RETURNED DUE FLAPS WOULD NOT LOWER PAST 10 UNITS ON APPROACH. RETAINING WASHERS BACKED OFF OF DRIVE SHAF T. TR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998041000375 19980410 00375 NM 1998 4 10 CA980317034 1 19980309 A 2910 6544510192 LINES 6544510192 BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE LT MLG LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 709378 (CAN) A/C RETURNED DUE LT MLG WOULD NOT RETRACT. HEAVY HYD FLUID LOSS ON RETURN. REPLACED HYD LINES, LEAK CHECK. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1998041000376 19980410 00376 NM 1998 4 10 CA980317033 1 19980309 A 7931 65544761 SWITCH 65544761 BOEING 737 7372L9 1384497 NM PWA JT8 JT8D17 52049 NE NR 2 ENG OIL FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) NR 2 ENGINE OIL FILTER LIGHT CAME ON. POWER REDUCED, BUT SETTING TOO LOW TO CONTINUE. RETURNED TO GATE. REPLACE D OIL PRESS DIFFERENTIAL SWITCH. 2 L 7 2 4F 4 F RT A16WE E2EA 1998041000377 19980410 00377 EU 1998 4 10 CA980317031 1 19980309 A 3231 D52880165001 DOOR AIRBUS 320 A320211 3930320 EU RT MLG OUT OF RIGGING W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND RT MAIN LANDING GEAR DOOR OUT OF RIG. MAIN LANDING GEAR DOOR RIGGED. 2 L 7 2 4F RT A28NM 1998041000378 19980410 00378 NM 1998 4 10 CA980317029 1 19980209 A 3220 SEALS 654620042 BOEING 737 7372T2 1384491 NM PWA JT8 JT8D17 52049 NE NLG WORN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 66554 17842 B0203P418 702737 (CAN) AFTER TAKEOFF, NLG WOULD NOT RETRACT. A/C RETURNED TO BLOCKS. NLG FLAT. SERVICED. NLG SEALS REPLACED ON OVERNI GHT. PART TC: 14,169. 2 L 7 2 4F 4 F RT A16WE E2EA 1998041000379 19980410 00379 NM 1998 4 10 CA980317028 1 19980209 A 2421 739515C IDG SUNDSTRAND 739515C BOEING 767 767375 NM FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA F0987 (CAN) ABORTED TAKEOFF DUE EICAS MESSAGE. RT GENERATOR DRIVE FOLLOWED BY RR GEN AND LT AND RT UTIL BUSSES. RT GENERATO R DRIVE MESSAGE DISSAPPEARED DURING TAXI IN. SERVICED IDG WITH 3 QUARTS OIL. A/C OPERATED MEL WITH RT IDG DISCONNECTED . IDG REPLACED. 2 L 7 2 4F RT A1NM 1998041000380 19980410 00380 WP 1998 4 10 CA980317027 1 19980209 A 3230 ACG7083503 ROD DOUG DC10 DC1030 3023501 WP NOSE LDG DAMAGED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) A/C RETURNED TO BLOCKS, UNABLE TO RETRACT NOSE LANDING GEAR. FOUND GROUND SHIFT ROD END DAMAGED. REPLACED GROUND SHIFT ROD AND SHIFT BRACKET. RETRACTION TESTS CARRIED OUT. CHECKED SERVICEABLE. 2 L 7 3 4F A22WE 1998041000381 19980410 00381 1998 4 10 CA980317026 4 19980209 A 3417 HG480B20 AIR DATA COMPUTE HG480B20 BOEING 737 737275 1384485 NM PWA JT8 JT8D17 52049 NE COCKPIT FAILED W A D UNSCHED LANDING RETURN TO BLOCK I FLT. ATTITUDE INST. CL CLIMB 1 CA P539 702661 (CAN) AIRCRAFT RETURNED TO BLOCKS DUE TO CAPT'S ALTIMETER FLAG, MACK TRIM FAIL FLAG. C.A.D.C REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998041000382 19980410 00382 1998 4 10 CA980317025 4 19980209 A 3413 457400WA0811 IVSI TELEDYNE 457400WA0811 BOEING 737 737275 1384485 NM COCKPIT FAILED W A D UNSCHED LANDING RETURN TO BLOCK I FLT. ATTITUDE INST. CL CLIMB 1 CA 2820 (CAN) AIRCRAFT RETUREND TO GATE DUE TO CAPTAIN'S IVSI FAILURE ON CLIMB OUT. REPLACED. 2 L 7 2 4F A16WE 1998041000383 19980410 00383 WP 1998 4 10 CA980317024 1 19980206 A 7120 LH121005T12 NUT DOUG DC10 DC1030 3023501 WP LT RT MOUNTS LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 1979 (CAN) DURING INSPECTION, FOUND FORWARD MOUNT BOLTS WITH BROKEN LOCKWIRE. LOW TORQUE VALUES WERE CONFIRMED. REPLACED RT AND LT MOUNT BOLTS AND NUTS. PART TT: 65,430 HOURS. 2 L 7 3 4F A22WE 1998041000384 19980410 00384 EU 1998 4 10 CA980317023 1 19980206 A 2400 PANEL 123VU AIRBUS 320 A320211 3930320 EU CB PANEL SHORTED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 21235 (CAN) CIRCUIT BREAKER PANEL 123VU DROPPED, CABLE SHORTED AGAINST STRUCTURE. LOOP WAS TOO LARGE AND CHAFED. 2 L 7 2 4F RT A28NM 1998041000385 19980410 00385 NM 1998 4 10 CA980317011 1 19980227 A 2910 829700185 HYDRAULIC TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FIREWALL CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 23562 120156 (CAN) RIGHT HAND ENGINE HYDRAULIC PUMP PRESSURE LINE FOUND CHAFED WHERE IT PASSES THROUGH THE NACELLE HORIZ. FIREWALL. T HE BULKHEAD 45 DEGREE FITTING RETAINING NUT WAS LOOSE ALLOWING FITTING TO MOVE IN BRACKET. BRACKET FOUND CRACKED AT BOT TOM OF FINGERS. LOOSE BULKHEAD FITTING AND DAMAGED BRACKET ALLOWED TUBE TO WEAR ON FIREWALL. SB 8-29-17 AND SB 8-29-19 ARE RELEVANT. PART TC: 32,973. 2 H 7 2 4T 4 T RT A13NM E20NE 1998041000386 19980410 00386 NM 1998 4 10 CA980317007 1 19980210 A 2760 82940010107 PRESS TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ROLL SPOILER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120322 (CAN) DURING WALK-AROUND, NR 1 SYSTEM HYDRAULIC QUANTITY LOW. HYDRAULIC FLUID LEAKING FROM WING ROOT AREA. ROLL SPOIL ER PRESSURE LINE LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1998041000387 19980410 00387 EA 1998 4 10 CA980317006 1 19980207 A 3234 574205 GEAR SELECT DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 HYD LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 15133 519 123150 (CAN) AFTER LANDING, LOST NR 2 HYDRAULIC FLUID. LANDING GEAR SELECTOR VALVE FOUND LEAKING. PART TC: 15,133. 2 H 7 2 4T 4 T RT A13NM E20NE 1998041000388 19980410 00388 NM 1998 4 10 CA980317004 1 19980107 A 5415 RIVETS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT NAC BRACKET SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 18462 120833 (CAN) RIGHT HAND NACELLE SURGE DAMPER ATTACH BRACKET RIVETS SHEARED. AIRCRAFT TT: 18,688 HOURS. 2 H 7 2 4T 4 T RT A13NM E20NE 1998041000389 19980410 00389 EA 1998 4 10 CA980317002 1 19980104 A 3320 BV033000220 LAMP HOLDER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE CABIN MELTED W K NONE O OTHER IN INSP/MAINT 1 CA 123116 (CAN) CABIN FLUORESCENT LIGHTING FOUND NOT WORKING ON ROW 4. FORWARD TUBE SOCKET FOUND MELTED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998041000390 19980410 00390 WP 1998 4 10 CA980305013 1 19980219 A 2160 97852011 CONTROL VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LEFT PACK TEMP INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 71159 P657363D (CAN) AIRCRAFT RETURNED DUE TO PRESSSURIZATION FAULT. CABIN CONTINUED TO CLIMB PAST 11,000 FEET, OXYGEN MASKS DEPLOYED. LEFT PACK WATER SEPARATOR TEMPERATURE CONTROL VALVE FOUND INOPERATIVE WHEN PACK IN OPERATION. VALVE REPLACED AND CHEC KED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998041000391 19980410 00391 EU 1998 4 10 CA980305012 1 19980127 A 2740 D2747001200000 CHAIN AIRBUS 320 A320211 3930320 EU HORZ STAB TRIM SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 20530 (CAN) TRIMMABLE HORIZONTAL STABILIZER CABLE ASSY CHAIN AT ACTUATOR FOUND WITH SEVERAL LINKS KINKED. CABLE CHAIN REPLACE D. AIRCRAFT TT: 20,340 HOURS. 2 L 7 2 4F RT A28NM 1998041000392 19980410 00392 EU 1998 4 10 CA980305010 1 19980127 A 5753 D757007420600 BEARING LINER AIRBUS 320 A320211 3930320 EU NR 3 FLAP BRNG MIGRATED W K NONE O OTHER IN INSP/MAINT 1 CA 19564 (CAN) NR 3 FLAP SUPPORT BEARING (JOINT) LINER MIGRATING. BEARING LINER MIGRATED COMPLETELY OUT OF HOUSING. BEARING REP LACED. 2 L 7 2 4F RT A28NM 1998041000395 20010312 00395 SW 2001 3 12 CA980305001 1 19980213 A 7931 206075787101 TUBE BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL COLLECTIVE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 3515 (CAN) VERTICAL TUNNEL AND FORWARD PILOT AND COPILOT SEAT AREAS OPENED, AND THEN WHILE MOVING COLLECTIVE, LEVER WAS FOUND CONTACTING BOTH OIL PRESSURE AND TORQUE PRESSURE LINES. TUBES WERE WORN AND PROTECTIVE PAINT WAS WORN OFF OF LEVER. T UBES ADJUSTED FOR CLEARANCE. 1 G 7 1 3U 3 U NC H2SW E1GL 1998041000396 20010312 00396 SW 2001 3 12 CA980303005 1 19980211 A 2821 222366621101 FILTER BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL FUEL SYSTEM BROKEN W O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA (CAN) ON GROUND RUN THE AIRCRAFT ENGINE QUIT. FURTHER INVESTIGATION FOUND THAT THE FUEL FILTER BOWL HAD BROKEN APART FRO M THE HEAD ASSY.BY WAY OF THE CAST ASSY., WHICH HOLDS THE HELICOIL FOR THE BOWL.ONCE THE BOWL BROKE AWAY FUEL TO THE ENG INE WAS LOST. 1 G 7 1 3U 3 U H2SW E4CE 1998041000397 19980410 00397 CE 1998 4 10 CA980303003 1 19980128 A 7603 66001511 THROTTLE CABLE LEAR 24 24B 5170306 CE GE CJ610 CJ6106 30006 NE LT ENGINE STIFF W K NONE O OTHER CR CRUISE 1 CA E251181A (CAN) LEFT ENGINE POWER LEVER WAS DIFFICULT TO MOVE WHILE IN CRUISE. 2 L 7 2 4J 4 J A10CE 1E16 1998041000398 19980410 00398 SW 1998 4 10 CA980302005 1 19980115 A 2720 NAS6204190 BOLT K950002001 KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE RUDDER CONTROL WORN W K NONE O OTHER IN INSP/MAINT 1 CA 3031 LE81008 (CAN) PLAY IN RUDDER CONTROL SYSTEM TRACED TO THE CONTROL BOLT CONNECTING THE CONTROL SPRING STRUT ASSY. TO THE PEDAL SY STEM CONTROL TUBE. BOLT FOUND TO HAVE DEEP GROOVES-ABOUT 25 PERCENT WORN INTO THE SHANK, WHERE THE SPRING STRUT CLEVIS END CONTACTS THE BOLT. SECOND AIRCRAFT FOUND WITH SIMILAR PROBLEM. 1 G 7 1 4F 4 U NT TR7BO E17EA 1998041000399 19980410 00399 NM 1998 4 10 CA980225019 1 19980216 A 2131 CONTROLLER BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE NR 2 PACK INTERMITTENT W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 700814 (CAN) UNABLE TO PRESSURIZE USING LEFT PACK ONLY. REPLACED NR 2 PACK COOLING FAN AND DOOR ACTUATOR AND PRESSURIZATION CO NTROLLER. 2 L 7 3 4F 4 F RT A3WE E2EA 1998041000400 20010312 00400 NM 2001 3 12 CA980225015 1 19980210 A 3242 AHM9100 STATOR BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E437 54555 NE BRAKES DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) TWO STATORS FOUND DELAMINATED AND BROKEN. BRAKE DISC WAS IMPROPERLY ASSEMBLED INTO THE HEAT PACK. THE ANTIVIBRATIO N GROOVES AROUND THE DRIVE TENIONS SHOULD FACE THE ROTOR, ON THIS ASSY THEY WERE ASSEMBLED FACING THE THRUST PLATE. REPA IRED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998041000402 19980410 00402 EU 1998 4 10 CA980225003 1 19980207 A 3230 DRG156869 ROD ROTOL 200429005 FOKKER F28 F28MK1000 4990808 EU NLG DWNLOCK REQ ADJUSTMENT W K NONE J WARNING INDICATION CL CLIMB 1 CA DRG156869 (CAN) AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT, AIRCRAFT RETURNED. NLG DOWNLOCK ACTUATING ROD WAS SLIGHTLY OUT OF ADJUSTMENT, WOULD NOT RETRACT WITH AIR LOADS AGAINST IT. ADJUSTED PER THE MM. 2 L 7 2 4F RT A20EU 1998041000403 19980410 00403 NM 1998 4 10 CA980220013 1 19980208 A 5280 BOLT BOEING 767 767233 NM LT MLG DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON WALKAROUND, FOUND LT MLG FIXED DOOR AND TRUNNION DOOR DAMAGED; ALSO, LARGE PANEL AFT OF GEAR 8 INCH BY 6 FEET D AMAGED PLUS SMALL PANEL INBOARD OF LARGE PANEL FORWARD MID-ATTACHMENT BOLT ON FIXED DOOR BROKEN CAUSING DAMAGE. BOLT RE PLACED AND DOOR REPAIRED. AIRCRAFT TT: 40,372 HOURS. 2 L 7 2 4F RT A1NM 1998041000404 19980410 00404 SW 1998 4 10 CA980220001 1 19980205 A 6210 206010200033 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL BOLT BORE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 3344 CS613 CAE820197 (CAN) MAIN ROTOR BLADES REMOVED FROM HUB FOR MAINTENANCE. BLADE BORES WERE FOUND CORRODED BEYOND LIMITS. THIS 4TH TIME AFTER BORE BUSHING CHANGES THE CORROSION HAS REAPPEARED. 1 G 7 1 3U 3 U H2SW E4CE 1998041000441 19980410 00441 CE 1998 4 10 CA971219006 1 19980326 A 3246 16294 WHEEL HALF CLEVELAND 40169 CESSNA 441 441 2076020 CE BOLT HOLE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) OUTBOARD WHEEL HALF CRACKED FROM BASE OF THE BOLT HOLE COUNTER BORE TO INSIDE OF WHEEL HALF ABOVE THE AIR SEAL. C RACK ALLOWED TUBELESS TIRE TO SLOWLY DEFLATE, ONLY WITH WEIGHT OF AIRCRAFT ON WHEELS. 1 L 7 2 3T RT A28CE 1998041000448 19980410 00448 NM 1998 4 10 CA971216069 1 19980317 A 2612 FIRE LOOP BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 1 ENG INTERMITTANT W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 700329 (CAN) ON DEPARTURE AT FL 200, CREW OBSERVED FIRE WARNING. NR 1 ENG SHUT DOWN AND A/C RETURNED. UNABLE TO DETECT FAULT. TWO FIRE LOOPS AND CONTROL UNIT RELACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1998041000455 19980410 00455 EU 1998 4 10 AALA980490 1 19980312 A 3222 C231098102 STRUT AIRBUS 300 A300B4605R 3930308 EU NLG DEFECTIVE A AALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SW 07 25071 514 JFK - FLT 107 - DURING APPROACH, THE NOSE LANDING GEAR RED UNLOCK LIGHT ILLUMINATED ON GEAR EXTENSION. CREW MISSED THE APPROACH, GEAR WAS CYCLED WITH THREE GREEN GEAR SAFE LIGHT ILLUMINATED. AIRCRAFT LANDED JFK WITHOUT FURTHER INCIDENT. R EPLACED NOSE GEAR TELESCOPING DRAG STRUT. ACCOMPLISHED NOSE LANDING GEAR RETRACTION AND ALTERNATE EXTEND CHECKS WITH NO RMAL INDICATION. SYSTEM LEAKED AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998041000456 19980410 00456 NM 1998 4 10 AALA980459 1 19980307 A 3260 2314143 SWITCH BOEING 727 727223 1384074 NM LT MLG DOOR DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 872AA 21384 MIA - FLT 617 - AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED AND THE MAIN LEFT GEAR DOOR WARNING LIGHT ILLUMINATED. AI RCRAFT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. REPLACE LEFT MAIN LANDING GEAR DOOR LIM IT SWITCH AND CYCLED GEAR SEVERAL TIME WITH NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000457 19980410 00457 NM 1998 4 10 AALA980122 1 19980112 A 2613 04A35548004255 ELEMENT BOEING 727 727223 1384074 NM NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 6822 19700 MIA - FLT 1746 - AFTER TAKEOFF MIA DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. AIRCRAFT AIR INTERRUPTED MI A AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE STRUT OVERHEAT DETECTION ELEMENT. NR 1 STRUT OVERHEAT DETECTION TE STS OK. NO LEAKS FOUND IN STRUT AREA AND NO OVERHEAT WARNING ON ENGINE RUN. SYSTEM LEAK AND GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 3 4F A3WE 1998041000458 19980410 00458 NM 1998 4 10 AALA980212 1 19980124 A 3230 AAP2448A UNIT BOEING 727 727223 1384074 NM E/E COMPT DEFECTIVE A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 6823 R00041 19701 DFW - FLT 885 - DURING TAKEOFF ATL-DFW WHEN LANDING GEAR RETRACTED, GEAR DID NOT RETRACT. OVERRIDE TRIGGER WAS USED AND GEAR RETRACTED NORMALLY. ABNORMAL PROCEDURES FOLLOWED FOR ENTIRE FLIGHT AND AIRCRAFT LANDED DFW WITHOUT INCIDENT. REP LACED LANDING GEAR ASSY UNIT. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000459 19980410 00459 NM 1998 4 10 AALA980227 1 19980128 A 2822 2580005 BOOST PUMP BOEING 727 727223 1384074 NM NR 1 DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 712AA 22468 MIA - FLT 489 - DURING CRUISE, NR 1 FWD BOOST PUMP CIRCUIT BREAKER TRIPPED. NR 1 AFT BOOST PUMP WAS ON MEL, FLIGHT CREW DECIDED TO RETURN TO MIA. AIRCRAFT LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED FWD AND AFT FUEL BOOST PUMPS PER MM PROCEDURES. SYSTEM LEAK AND OPERATED NORMALLY WITHOUT POPPING CIRCUIT BREAKERS. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 3 4F A3WE 1998041000460 19980410 00460 NM 1998 4 10 AALA980199 1 19980122 A 2822 8905K935 SWITCH BOEING 727 727223 1384074 NM COCKPIT DEFECTIVE A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 712AA 22468 BNA - FLT 2017 - DURING TAKEOFF, NR 2 FUEL TANK LEFT AFT BOOST PUMP CIRCUIT BREAKER POPPED. NO RESET ATTEMPTED. AIRCRA FT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. REPLACED LEFT AFT BOOST PUMP SWITCH. DEFUELED, REFUELDED AND SUMPED AL L FUEL TANKS. GROUND RUNUP CHECK OF FUEL SYSTEMS CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000461 19980410 00461 WP 1998 4 10 AALA980441 1 19980304 A 3350 P4010051111 MODULE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 493AA 49731 EWR - DURING OVERNIGHT MAINTENANCE, HALF OF THE FLOOR EMERGENCY LIGHT WOULD NOT ILLUMINATE. REPLACED TWO EMERGENCY PATH LIGHTING MODULES IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041000462 19980410 00462 NM 1998 4 10 AALA980125 1 19980115 A 3610 65234941 DUCT BOEING 727 727223 1384074 NM NR 3 ENGINE RUPTURED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 702AA 22460 DFW - FLT 271 - AFTER TAKEOFF TUL DURING CLIMB-OUT, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. BLEED AIR SWITCH CLOSED AND THROTTLE RETARDED TO IDLE PER EMERGENCY PROCEDURES. AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RU PTURED DUCT AND ACCOMPLISHED REQUIRED CHECKS PER MM. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000463 19980410 00463 NM 1998 4 10 AALA980278 1 19980207 A 2780 RETRACT MECH BOEING 727 727227 1384078 NM RT LE SLAT REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 721AA 20729 MCI - FLT 1675 - AFTER TAKEOFF MCI, FLAPS WERE RETRACTED AND NR 7 FLAP DID NOT RETRACT. AIRCRAFT RETURNED TO MCI AND LA NDED WITHOUT INCIDENT. MAINTENANCE SERVICED SYSTEM AND CYCLED FLAPS SEVERAL TIMES WITH NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000464 19980410 00464 NM 1998 4 10 AALA980267 1 19980206 A 2913 MPEV305610A PUMP BOEING 727 727223 1384074 NM 'B' HYD SYSTEM DEFECTIVE A AALA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 SW 07 848AA 20989 JFK - FLT 1195 - AFTER TAKEFF JFK, HYDRAULIC SYSTEM 'B' INDICATED A QUANTITY LOSS. AIRCRAFT AIR INTERRUPTED AND RETURNE D TO JFK AND LANDED WITHOUT FURTHER INCIDENT. FOUND SYSTEM 'B' ELECTRIC PUMP LEAKING FROM SHAFT. REPLACED PUMP, CHANGE D FILTERS AND SERVICED SYSTEM. SYSTEM GROUND AND LEAKED CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000465 19980410 00465 1998 4 10 AALA980157 4 19980118 A 2210 2588880901 COUPLER BOEING 727 727223 1384074 NM TAIL DEFECTIVE A A AALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 708AA 22465 MIA - FLT 1017 - ON TAKEOFF MIA EXPERIENCED RUDDER PROBLEMS, INTERMITTENT YAW IN FLIGHT. DECLARED EMERGENCY AND RETURNE D TO MAI. LANDED MIA WITHOUT INCIDENT. REPLACED UPPER AND LOWER YAW DAMPER COUPLERS. ACCOMPLISHED ALL REQUIRED TESTS PER MM. ACCOMPLISHED LMP TESTS WITH NORMAL RESULTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000466 19980410 00466 WP 1998 4 10 AALA980417 1 19980302 A 3230 39370335503 CYLINDER DOUG DC9 DC982 3022082 WP RT MLG DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 581AA MAL439 53158 SFO - FLT 1917 - UPON ARRIVAL SFO, NECESSARY TO RECYCLE GEAR THREE TIMES TO GET DOWN AND LOCKED INDICATION. REPLACED RI GHT MAIN LANDING GEAR BUNGEE CYLINDER. ACCOMPLISHED GEAR SWING WITH NO PROBLEMS NOTED. LEAK CHECKED OK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041000467 19980410 00467 NM 1998 4 10 AALA980183 1 19980120 A 3260 106122629 SENSOR BOEING 727 727223 1384074 NM RT MLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 889AA 21527 MIA - FLT 1193 - AFTER GEAR RETRACTION, THE RIGHT GEAR RED AND GREEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MIA AND LA NDED WITHOUT INCIDENT. REPLACED RIGHT MAIN GEAR DOWNLOCK SENSOR. PERFORMED GEAR RETRACTION WITH NO DEFECTS. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000468 19980410 00468 NM 1998 4 10 AALA980156 1 19980116 A 3610 CLAMP BOEING 727 727223 1384074 NM NR 3 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 702AA 22460 DFW - FLT 919 - AFTER TAKEOFF DFW NR 3 STRUT OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY CHECKLIST, RETARDED THR OTTLE AND LIGHT EXTINGUISHED. DUMPED FUEL AND RETURNED TO LAND DFW WITHOUT INCIDENT. REMOVED AND REPLACED BOTH CLAMPS. RAN NR 3 ENGINE, NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000469 19980410 00469 NM 1998 4 10 AALA980124 1 19980113 A 2751 ABB2042B ACTUATOR BOEING 727 727223 1384074 NM LT TE FLAP DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 878AA 21390 ORD - FLT 1920 - AFTER TAKEOFF DURING CLIMB, FLAPS WERE RETRACTED AND A AMBER LEADING EDGE FLAP LGIHT ILLUMINATED ALONG WITH AN AMBER NR 7 SLAT LIGHT ILLUMINATED. FLAPS WERE RETURNED TO 2 DEGREES AND RESELECTED TO 0 DEGREES, LEADING EDGE F LAP AMBER LIGHT ALONG WITH A GREEN EXTENDED LIGHT ILLUMINATED ON TEST PANEL. ALTERNATE CHECKLIST WAS FOLLOWED. AIRCRAF T LANDED ORD WITHOUT INCIDENT WITH NORMAL FLAP CONFIGURATION. REPLACED NR 7 SLAT ACTUATOR. OPS CHECK NORMAL. SYSTEM L EAKED AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998041000470 19980410 00470 WP 1998 4 10 AALA980381 1 19980221 A 2913 6304106 PUMP DOUG DC10 DC1010 3022110 WP NR 3 HYD SYSTEM DEFECTIVE A AALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 130AA 250827 46989 HNL - FLT 162 - DURING CLIMB-OUT, NR 3 HYDRAULIC ELEVATOR LIGHT CAME ON WITH SYSTEM QUANTITY AND PRESSURE REDUCING TO ZE RO. AIRCRAFT AIR INTERRUPTED AND RETURNED AND LANDED HNL OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTI ON WITH NO DEFECTS FOUND. REPLACED REVERSIBLE HYDRAULIC PUMP ON NR 3 SYSTEM. SYSTEM OPERATES NORMAL WITH NO LEAKS. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1998041000471 19980410 00471 EU 1998 4 10 AALA980348 1 19980216 A 4990 A0007022500462 APU AIRBUS 300 A300B4605R 3930308 EU APU COMP LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 41063 P1077 506 ORD - FLT 921 - AFTER TAKEOFF SMOKE WAS DETECTED IN THE CABIN WITH NO ABNORMAL INDICATIONS. AIRCRAFT RETURNED TO ORD AN D LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED BOTH AIR CYCLE MACHINE COALESCER BAGS. ACCOMPLISHED PACK BURNOUT PROCED URE AND OVERWEIGHT LANDING INSPECTION WIHT NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FERR Y FLIGHT ORD-JFK. OPERATIONAL CHECKED NORMAL WITH NO DEFECTS. MAINTENANCE ENTRY ON 2/17 STATED THE THE SMOKE IN CABIN WAS CAUSED BY APU INLET CHAMBER OIL FILLED FROM APU. REPLACED APU. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998041000472 19980410 00472 WP 1998 4 10 AALA980433 1 19980303 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 292AA 49304 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR LIGHTING AT FORWARD GALLEY WAS INOPERTIVE. REPAIRED BROKEN WIRE AT EMERGENCY FLOOR LIGHT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041000473 19980410 00473 WP 1998 4 10 AALA980421 1 19980301 A 3350 2620441050 MODULE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 498AA 49736 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT R2 DOOR LOWER MARKER INOPERATIVE. REPLACED FORWARD MODULE AND BATTE RY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041000474 19980410 00474 NM 1998 4 10 AALA980369 1 19980219 A 2421 IDG BOEING 757 757223 1384957 NM NR 1 ENGINE REQ'D SERVICE A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 687AA 25695 DFW - FLT 70 - REPEAT ITEM 33 LEFT GEN CONTROL TRIPPED OFF AND CSD DRIVE LIGHT FLICKERED CONTINUOUSLY. DISCONNECTED LEF T IDG. CHECKED AND SERVICED NR 1 ENG IDG OIL. RECONNECTED IDG. RAN ENGINE. IDG OPS CHECK OK. NO LEAKS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A2NM 1998041000475 19980410 00475 NM 1998 4 10 AALA980382 1 19980219 A 2424 GCU BOEING 757 757223 1384957 NM LEFT FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 687AA 25695 TAD - FLT 36 - LEFT GEN DRIVE EICAS ILLUMINATED 3 HR INTO FLIGHT LEFT GEN CON DROPPED OFF. INITIATED PROCEDURE IDG DISC ONNECTED APU STARTED FINE AT FL410 CONTINUED FLIGHT WITH RIGHT GEN AND APU GEN. REPLACED LEFT GENERATOR CONTROL UNIT SE RVICED IDG RAN ENGINE. ELEC OPS NORMAL. (M) 2 L 7 2 4F RT A2NM 1998041000476 19980410 00476 NM 1998 4 10 AALA980478 1 19980305 A 2421 IDG BOEING 767 767323 1385205 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 355AA 24036 JFK - FLT 950 - APPROX 45 MINUTES INTO FLIGHT GOT L GEN DRIVE LIGHT ON STEADY COMPLETED PROCEDURE PER OPS MANUAL AND DIS CONNECTED L GEN DRIVE. REPLACED LT IDG. OPS CHECK AND LEAK CHECK OK. REMOVED MEL 2401 AUTH 03-67DC-B CLEARED MIC SHEE T 3552409CE/0954.05MAR.JFK. (M) 2 L 7 2 4F RT A1NM 1998041000477 19980410 00477 1998 4 10 AALA980479 4 19980306 A 3425 EFIS PANEL BOEING 767 767323 1385205 NM LT COCKPIT MALFUNCTIONED A AALA K NONE O OTHER CR CRUISE 1 SW 07 371AA 25198 BOS - FLT 70 - CAPTAINS EFIS CONTROL PANEL CIRCUIT BREAKER POPS IN FLIGHT. ONE RESET WAS ATTEMPTED. REMOVED AND REPLAC ED EFIS CONTROL PANEL OPERATIONAL CHECKS NORMAL. (M) 2 L 7 2 4F RT A1NM 1998041000478 19980410 00478 NM 1998 4 10 AALA980438 1 19980302 A 3610 DUCT BOEING 767 767223 1385123 NM RIGHT FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 335AA 22333 SFO - FLT 59 - DUCK LEAK LIGHT RT SIDE ILLUMINATES INTERMITTENTLY THROUGHOUT THE FLT. CLOSING RIGHT ENGINE BLEED. RIGH T ISOLATION VALVE AND RETARDING RIGHT THROTTLE HAD NO EFFECT. LIGHT CONTINUED TO FLICKER ON AND OFF. FOUND DUCT 404822 7 LEAKING AIR, DUE TO CRACKED WELD. REPLACED DUCT. NEW DUCT LEAK AND OPS CHECK OK. ACCOMPLISHED HI-POWER RUN. NO PRO BLEMS NOTED. SYSTEMS NOW OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A1NM 1998041000479 19980410 00479 NM 1998 4 10 AALA980432 1 19980303 A 2421 IDG BOEING 767 767223 1385123 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 323AA 22324 RT GEN DRIVE LIGHT FLICKERED FOR 25 MINUTES. DRIVE LIGHT THEN CAME ON STEADY ENOUGH TO GIVE ICAS R GEN DRIVE INDICATION STEADY. RT IDG SHUT DOWN PER OPERATION MANUAL PROCEDURE APU STARTED, AT 41,000 FT, CARRIED TO RT BUS. INSPECTED FOUND DEBRIS IDG FILL COUPLING SEAT. REMOVED DEBRIS SERVICED IDG. RAN UP ENG, LEAK CHECK GOOD OP CHECK GOOD. DELAY INCURRE D DUE RT GEN DRIVE LIGHT ILLUMINATED. IDG WAS DISCONNECTED. (M) 2 L 7 2 4F RT A1NM 1998041000480 19980410 00480 NM 1998 4 10 AALA980414 1 19980224 A 2612 FIRE DETECTOR BOEING 767 767323 1385205 NM LT ENGINE MALFUNCTIONED A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 351AA 24032 LGW - 50 - LT ENG OH LP 1 STATUS MESSGE ANNUNCIATED ON LOWER EICAS. PERFORMED TROUBLESHOOTING AS PER MM 26-11-00-1 OH L OOP 1 FOUND INOPERATIVE NIL SPARES LGW ITEM DEF PER MEL 26-02B AU 2-364D-A ENT IN MICS PLACARDED RAISED. TROUBLESHOT SY STEM AND REPLACED FAULTY L ENG OVERHEAD LOOP DETECTOR ASSY PER MM 26-11-02-4 OVERHEAT DET TEST OK ON EICAS. REMOVED PLA C 2-364D-A. CLEARED MIC SHEET. (M) 2 L 7 2 4F RT A1NM 1998041000481 19980410 00481 NM 1998 4 10 AALA980435 1 19980304 A 2421 IDG BOEING 767 767223 1385123 NM LT ENGINE INOPERATIVE A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 338AA 22335 ORD - FLT 95 - STEADY EICAS MSG L GEN DRIVE 'DRIVE' LIGHT ON STEADY OH GEN DRIVE DISC. PLACARDED LT IDG INOP PER MEL EN TERED IN MIC SHEET CHECKED LT AND RT IDG OILS AND APU OIL. REMOVED AND REPLACED LT IDG, LEAK CHECK GOOD. OPS CHECK GOO D. REMOVED PLACARD. (M) 2 L 7 2 4F RT A1NM 1998041000503 19980410 00503 SO 1998 4 10 C2XA98CL022 1 19980301 A 2170 44E221A WATER SEPARATOR EMB 120 EMB120RT SO NR 2 FAULTED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 31711 120107 CLE - FLT 3116 - CREW REPORTED A DUCT LEAK LIGHT ON THE RIGHT ENGINE DURING DEPARTURE, CREW PERFORMED QRH ITEMS AND LIGH T EXTINGUISHED AT THE 3 MINUTE MARK. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPL ACED THE NR 2 WATER SEPARATOR IAW EMB-120 MM 30-10-02, OPERATIONAL CHECK OF BLEED AIR SYSTEM WAS SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041000504 19980410 00504 CE 1998 4 10 98ZZZM385 1 19980301 A 2120 AIR DISTRIBUTION BEECH 1900 1900D 1154162 CE COCKPIT ODOR A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 87551 UE206 CLE - FLT 3165 - CREW REPORTED A VERY STRONG BURNING SMELL/SULPHUR SMELL IMMEDIATELY AFTER GEAR UP, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, ALSO OPERATIONAL CHECKS WERE PERFORMED WITH ENGINES RU NNING AT DIFFERENT POWER SETTINGS AND ENVIROMENTALS ON USING DIFFERENT SETTINGS AND LOADS WITH NO DEFECTS NOTED ON ANY S YSTEM. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998041000505 19980410 00505 SO 1998 4 10 C2XA98CL020 1 19980228 A 3242 21585 BRAKE STATOR EMB 120 EMB120RT SO LT MLG BROKEN A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 09 26714 0755 120118 CLE - FLT 3355 - CREW REPORTED FEELING THE BRAKES GRABBING ON TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED T HEN REMOVED AND REPLACED THE LEFT OUTBOARD BRAKE ASSEMBLY DUE TO A BROKEN STATOR, IAW EMB-120 MM 32-41-05. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041000506 19980410 00506 1998 4 10 RAIA980303 4 19980305 A 6113 664005300 O-RING BAG JETSTM JETSTM3201 1500217 EU LT SPINNER WORN A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 434AM 12952 887 FLT 7486 - STL - LEFT PROPELLER SPINNER WOBBLES IN FLT. MAINTENANCE INSPECTED AND REPLACED LEFT PROPELLER SPINNER O-RIN G. (M) 2 L 7 2 4T RT A56EU 1998041000507 19980410 00507 EU 1998 4 10 RAIA980304 1 19980305 A 7921 L86023281 OIL COOLER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 551HK 41040 FLT 7517 - GRR - LEFT ENGINE LOST OIL PRESSURE, CREW PEFORMED INFLIGHT SHUTDOWN. MAINTENANCE REPLACED LEFT OIL COOLER A SSEMBLY. (M) 2 L 7 2 4T RT A41NM 1998041000508 19980410 00508 1998 4 10 RAIA980309 4 19980310 A 3417 7000700951 ADC AEROSP ATR72 ATR72202 8680940 EU E/E COMPT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 723TE 14051 283 FLT 7166 - STL - CAPTAINS AIRSPEED INDICATOR WENT TO ZERO AND CAPTAINS ALTIMETER FELL TO 500 FEET. MAINTENANCE REPLACED CAPTAINS AIR DATA COMPUTER (ADC). (M) 2 H 7 2 4T RT A53EU 1998041000509 19980410 00509 1998 4 10 RAIA980308 3 19980308 A 6112 DE-ICE BOOT JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 558HK 41071 FLT 7219 - STL - RIGHT PROPELLER DE-ICE FAILED LONG AND SHORT CYCLES. MAINTENANCE REPLACED RIGHT PROPELLER ASSEMBLY. ( M) 2 L 7 2 4T RT A41NM 1998041000510 19980410 00510 SW 1998 4 10 98ZZZM386 1 19980305 A 2150 20475546 ACM SWRNGN SA227 SA227AC 8780603 SW LEFT INOPERATIVE A EQGA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 19 459AM AC700 AUT - FLT 1280 - DURING SHORT FINAL INTO AUS, SMOKE BEGAN COMING OUT OF THE LEFT BLEED. UPON LANDING AND DURING ROLL OU T, FO SHUT OFF BOTH BLEEDS. RESIDUAL SMOKE CONTINUED TO ENTER COCKPIT THROUGH LEFT BLEED DURING TAXI TO GATE. AIRCRAFT ARRIVED AT GATE WITHOUT INCIDENT AND BOTH ENGINES WERE SHUT DOWN. MAINTENANCE CONTROL WAS NOTIFIED AND CONTACTED TO IN SPECT AIRCRAFT. UPON INSPECTION, THE LEFT AIR CYCLE MACHINE WAS FOUND TO BE DEFECTIVE. LEFT AIR CYCLE MACHINE/AIRCONDI TIONING WAS DEFERRED PER MEL 21-4-0. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998041000511 19980410 00511 WP 1998 4 10 VTZA98093 2 19980225 A 7320 89778025 FCU BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 482UE 897 FLT 6468 - IAD-BWI - AIRCRAFT ABORTED TAKEOFF DUE TO TORQUE FLUCTUATION ON LT AND RT ENGINES. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED X-SCREW ON LT FCU AND NO FLUX DEFECTS NOTED ON RT ENGINE DURING GROUND RUN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998041000513 19980410 00513 NE 1998 4 10 TSAA9872040 2 19980106 A 7260 GEARBOX BOEING 737 7372Y5 1384554 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LEAKING A TSAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 810AL 24031 FLT 247 - ITO-HNL - SHUT DOWN NR 1 ENGINE DUE TO LOW OIL PRESSURE. ENGINE WAS SHUT DOWN FOR APPROXIMATELY 12 MINUTES. D IVERTED TO OGG. SERVICED OIL (4 QTS). PULLED ENGINE OIL FILTER. CHECK OK. INSTALLED NEW OIL FILTER PER ENGINE MANUAL 72-61-00, PAGE 1005-1006. REINSTALLED COMBUSTION CHAMBER FUEL DRAG LINE. NO OIL IN LINE. REMOVED OIL PRESSURE DIFFER ENTIAL LINE. MOTORED ENGINE. POSITIVE FLOW FROM OIL PUMP. OIL PRESSURE RISE AND OIL TEMP RISE. QIL QTY READS ZERO. REPLACED NR 1 ENGINE GEARBOX ASSY PER PWA MM 72-60. REPLACED OIL COOLER. PRECAUTIONARY LOW OIL QTY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U 4 F RT A16WE E2EA 1998041000514 19980410 00514 WP 1998 4 10 VTZA98051 2 19980209 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 310UE 41028 FLT 6302 - IAD-BOS - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT OIL CONTAMINATION WARNING LIGHT ILLUM INATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND VERY SMALL AMOUNT OF METAL LIC MATERIAL ON CHIP DETECTOR. MAINTENANCE CLEANED AND REINSTALLED CHIP DETECTOR AND GROUND RAN AIRCRAFT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1998041000515 19980410 00515 WP 1998 4 10 VTZA98049 2 19980205 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RIGHT LOW POWER A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 305UE 41019 FLT 6502 - IAD-LGA - ABORTED TAKEOFF DUE TO RT ENGINE WOULD NOT MAKE TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND FOUND NO DEFECTS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1998041000516 19980410 00516 WP 1998 4 10 VTZA98053 2 19980209 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE DIRTY A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 310UE 41028 FLT 6602 - IAD-BWI - AIRCRAFT RETURNED TO GATE DUE TO RT OIL CONTAMINATION WARNING LIGHT ILLUMINATED. MAINTENANCE INSPE CTED AND FOUND SMALL CHIP ON DETECTOR AND REMOVED AND REINSTALLED CHIP DETECTOR. OPS CHECK OK. AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1998041000517 19980410 00517 NE 1998 4 10 SIMA980411 2 19980210 A 7320 311325201 VALVE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENGINE FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 407AT 374 407 ORD - FLT 4123 - FLT CREW REPORTED SMOKE SMELL IN THE CABIN AND COCKPIT. MAINTENANCE R/I'D P2.5/P3 SWITCHING VALVE AND NL PROBE IAW PWA MM 72-01-60. PERFORMED GROUND ENGINE RUNS SATISFACTORILY. RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998041000518 19980410 00518 NE 1998 4 10 98ZZZM387 2 19980210 A 7320 3033509 PROBE AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENGINE FAILED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 407AT CH4310 407 ORD - FLT 4123 - FLT CREW REPORTED SMOKE SMELL IN THE CABIN AND COCKPIT. MAINTENANCE R/I'D P2.5/P3 SWITCHING VALVE AND NL PROBE IAW PWA MM 72-01-60. PERFORMED GROUND ENGINE RUNS SATISFACTORILY. RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998041000519 19980410 00519 EU 1998 4 10 RAIA980211 1 19980211 A 7332 CM6839 LAMP BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LEFT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 425AM 500 870 FLT 7440 - STL - LEFT FUEL LOW PRESSURE CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED BULBS IN LEFT FUEL CA PTION. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998041000520 19980410 00520 WP 1998 4 10 RAIA980210 2 19980211 A 7310 1379305A73 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE KINKED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 423AM 14432 858 FLT 7456 - STL - RIGHT FUEL LOW PRESSURE CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED LEFT FUEL SUPPLY LIN E. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998041000521 19980410 00521 EU 1998 4 10 RAIA980216 1 19980224 A 7332 1103P0645 SWITCH BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 423AM 858 FLT 7437 - CMI - RIGHT ENGINE FUEL PRESSURE CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT ENGINE FUEL PRESSURE SWITCH. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998041000522 19980410 00522 NE 1998 4 10 PLGA980204A 2 19980204 A 7320 PCU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE OUT OF ADJUST A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 NE 05 742BA 340A092 PWM - FLT 4277 - DURING TAKEOFF, WHEN THE CTOT WAS SWITCHED ON THE RIGHT TORQUE INCREASED BUT THE LEFT DID NOT. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RIGGED THE LEFT ENGINE PCU. SYSTEM GROUND CHECKED GOOD. ( M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998041000523 19980410 00523 WP 1998 4 10 VTZA98076 2 19980218 A 7320 89778025 FCU BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 489UE 908 FLT 6348 - IAD-GSO - AIRCRAFT ABORTED TAKEOFF DUE TO LEFT RPM 103 PERCENT AT 80 KNOTS. AIRCRAFT RETURNED TO GATE WITH N O FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED X-SCREW ON FCU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVE D FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998041000525 19980410 00525 NE 1998 4 10 REXA98067 2 19980309 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RIGHT OVERTEMP A REXA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 25 347AM 340A039 RIGHT ENGINE OVERTEMP ON TAKEOFF ROLL. PERFORMED LP-1 INSPECTION ON RIGHT ENGINE. GROUND RUNS NORMAL, NO DEFECTS NOTED . (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998041000526 19980410 00526 NE 1998 4 10 REXA98065 2 19980308 A 7321 7086M60G11 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE SURGE A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 406BH ECDE5330 340A074 RIGHT ENGINE HAD A ITT SURGE ON TAKEOFF. REMOVED AND REPLACED RIGHT ENGINE ECU. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998041000527 19980410 00527 NE 1998 4 10 REXA98063 2 19980304 A 7321 7086M60G010 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE MALFUNCTIONED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 403BH 340A060 RT ITT GAUGE DROPPED TO ZERO INFLIGHT. REMOVED AND REPLACED RT ECU. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998041000528 19980410 00528 NM 1998 4 10 98ZZZM388 1 19980121 A 5753 SKIN BOEING 727 727212 138407G NM RT TE AFT FLAP DENTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 A DENT ON RT INBOARD AFT FLAP UPPER SKIN 2 INCHES DIAMETER AT WBL 123 RT INBOARD AFT FLAP. TRIMMED OUT THE DENTED AREA OF SKIN. PERFORMED FIBERGLASS CLOTH OVERLAY REPAIR. (M) 2 L 7 3 4F A3WE 1998041000529 19980410 00529 NE 1998 4 10 RAIA980305 2 19980306 A 7320 32448555 HMU AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 723TE 283 FLT 7126 - STL - RIGHT ENGINE WAS SLOW TO ACHIEVE TAKEOFF TORQUE. MAINTENANCE REPLACED RIGHT FUEL HYDROMECHANICAL UNIT. (M) 2 H 7 2 4T 4 T RT A53EU E2ONE 1998041000530 19980410 00530 NE 1998 4 10 AALA980491 2 19980227 A 7314 GASKET AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 2 ENGINE DETERIORATED A A AALA A F UNSCHED LANDING ACTIVATE FIRE EXT. J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 07 70074 517 LHR - FLT 105 - AIRCRAFT MADE AN UNSCHEDULED LANDING AT BOS DUE TO CREW NOTING RIGHT INNER, FUEL TANK QUANTITY FLUCTUATI ON. UPON LANDING BOS, AIRCRAFT BEHIND US ON TAXIWAY REPORTED 'FUEL POURING FROM NR 2 ENGINE' PULLED NR 2 FIRE HANDLE AN D FIRED AGENT 1. TROUBLESHOT NR 2 ENGINE FUEL SYSTEM. FOUND FUEL PUMP INLET HOSE GASKET DETERIORATED. REPLACED GASKET PERFORMED MAINTENANCE CHECKS IAW MM. CHECKS NORMAL. NO DEFECTS NOTED. OK FOR SERVICE, NO LEAKS NOTED. REPLACED RT E NGINE NR 1 AND NR 2 FIRE BOTTLES PER MM. ACCOMPLISHED REQUIRED CHECKS OK. RESAFETIED RT ENGINE FIRE HANDLE. (M) 2 L 7 2 4F 4 F RT A35EU E13NE 1998041000531 19980410 00531 NE 1998 4 10 AALA980326 2 19980214 A 7314 3782018 FUEL PUMP BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 713AA 7103 22469 MIA - FLT 2181 - AFTER TAKEOFF MIA, NR 1 ENGINE FAILURE. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACE D NR 1 ENGINE FUEL CONTROL AND FUEL PUMP. ACCOMPLISHED LEAK CHECK AND ALL REQUIRED RUN UP CHECKS WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998041000532 19980410 00532 NE 1998 4 10 AALA980420 2 19980301 A 7321 658385 FUEL CONTROL BOEING 727 727223 1384074 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE DEFECTIVE A AALA A UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 SW 07 898AA 22014 MIA - FLT 929 - WHILE PASSING THROUGH 2000 FT, NR 1 ENGINE FLAMED OUT WITH NO PRIOR ABNORMAL INDICATIONS. AIRCRAFT RETU RNED TO MIAMI AND LANDED WITHOUT INCIDENT, NOT OVERWEIGHT. REPLACED FUEL PUMP AND FUEL CONTROL. LEAK CHECKED WITH NO L EAKS FOUND. GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998041000533 19980410 00533 NM 1998 4 10 TWAA9804010 1 19980122 A 5754 SKIN BOEING 767 767231 1385131 NM NR 8 LE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 LAX - DURING C-CHECK MAINTENANCE, FOUND THE RT WING NR 8 LE SLAT REPAIR DELAMINATED AT INBOARD UPPER EDGE. INSTALLED HO T BOND REPAIR PER SRM 51-70-10 PAGE 23. (M) 2 L 7 2 4F RT A1NM 1998041000534 19980410 00534 NM 1998 4 10 TWAA9804009 1 19980217 A 5754 SKIN BOEING 767 767231 1385131 NM NR 6 LE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 LAX - DURING C-CHECK MAINTENANCE, NR 6 LE SLAT INBAORD TOP SIDE WAS DELAMINATED AT TOP CENTER, 9 INCH BY 2 INCH, 36 INCH FROM INBOARD END. REPAIRED DELAMINATED AREA PER 51-70-10 AND SEALED EDGES. (M) 2 L 7 2 4F RT A1NM 1998041000535 19980410 00535 NM 1998 4 10 TWAA9804008 1 19980211 A 5755 SKIN BOEING 767 767231 1385131 NM NR 12 SPOILER CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING C-CHECK MAINTENANCE, NR 12 SPOILER UPPER SURFACE HAD A SMALL 1.24 INCH CRACK AT INBOARD FORWARD CORNER. RE PAIRED SPOILER BY HOTBONDING PER SRM 51-70-05 PAGE 23. (M) 2 L 7 2 4F RT A1NM 1998041000536 19980410 00536 NM 1998 4 10 TWAA9804007 1 19980220 A 5753 SKIN BOEING 767 767231 1385131 NM LT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 609TW 22572 LAX - DURING C-CHECK MAINTENANCE, THE LEFT OUTBOARD FLAP WEDGE HAD 14 INCH HORIZONTAL CRACK, 17 INCH FROM INBOARD END AN D 19 INCH FROM BOTTOM TRAILING EDGE. REPAIRED AREA PER 767 SRM 51-70-05. (M) 2 L 7 2 4F RT A1NM 1998041000543 19980410 00543 WP 1998 4 10 TWAA9804101 1 19980319 A 3260 H146 SWITCH DOUG DC9 DC931 3022065 WP NLG INTERMITTENT A TWAA O OTHER N FALSE WARNING DE DESCENT 1 CE 05 984Z 47412 SGF - FLT 363 - ON GEAR EXTENSION, THE NOSE GEAR DOWN LIGHT WAS INOPERATIVE. CYCLED LANDING GEAR AND GOT CORRECT INDICA TION. MADE TWO FLYBYS. FOUND UPLIMIT SWITCH INTERMITTENT. REPLACED SWITCH. (M 2 L 7 2 4F A6WE 1998041000544 19980410 00544 NM 1998 4 10 TWAA9804102 1 19980319 A 3350 6104781 BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 84355 21987 STL - DURING OVERNIGHT MAINTENANCE, FOUND THE EMERGENCY SLIDE LIGHTS INOPERATIVE AT THE L2 AND R2 DOORS. REPLACED THE B ATTERY PACK. (M) 2 L 7 3 4F A3WE 1998041000545 19980410 00545 WP 1998 4 10 TWAA9804103 1 19980319 A 2421 976J2528 GENERATOR DOUG DC9 DC982 3022082 WP APU WORN A TWAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 05 951U 49245 JFK - FLT 8703 - THE LEFT GEN FAILED, NO VOLTS OR FREQS. APU STARTED AND RAN NORMALLY FOR 30 MINUTES THEN APU GEN FAILE D, NO VOLTS OR FREQS RETURNED TO JFK. THE LEFT GEN WAS DEFERRED PER MEL, AND THE APU GENERATOR CONTROL UNIT WAS REPLACE D. IN FLIGHT, THE APU GENERATOR RAN NORMAL FOR AWHILE THEN FAILED. FLT AGAIN RETURNED TO JFK. REPLACED THE LEFT CSD M FG PN 696233B, AND THE APU GENERATOR. (M) 2 L 7 2 4F A6WE 1998041000554 19980410 00554 NM 1998 4 10 TSAA9753169 1 19980305 A 5311 6546538551 FRAME BOEING 737 737297 1384480 NM BS 597 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING LAP JOINT INSPECTION, FOUND CRACKED FRAME AT STATION 597 BETWEEN 16L AND 17L. REMOVED AND REPLACED FRAME SECTION PER SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1998041000555 19980410 00555 NM 1998 4 10 TSAA9757168 1 19980305 A 5711 SPAR BOEING 737 737297 1384480 NM LT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING LAP JOINT INSPECTION, FOUND WBL 92 LEFT WING L/E SPAR LEVEL 2 CORROSION 2 INCH BY 3 INCH ARUOND BOOST PUMP ATTACH MENT TO SPAR. REMOVED CORROSION IAW 57-10-01 AND 51-10-6. LIMITS FOUND TO BE ACCEPTABLE TO BOEING. REPAIRED IAW DRAWI NGS SBX-SBA-98-0010TR AND SBX-SBA-98-0011RR AND APPROVED BY 8110-3 DATED 2/25/98. (M) 2 L 7 2 4F A16WE 1998041000556 19980410 00556 NM 1998 4 10 TSAA9753166 1 19980220 A 5320 SCUFF PLATE BOEING 737 737297 1384480 NM BS 465 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING LAP JOINT INSPECTION, FOUND FORWARD CARGO DOOR SCUFF PLATE STRUCTURE CRACKED 1.5 INCH LONG ON BOTTOM LEFT SIDE AT STATION 465. REMOVED CRACKED AREA AND REPAIRED IAW SRM 51-40-3, FIGURE 1 AND SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1998041000557 19980410 00557 NM 1998 4 10 TSAA9753165 1 19980220 A 5320 SCUFF PLATE BOEING 737 737297 1384480 NM BS 450 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING LAP JOINT INSPECTION, FOUND FORWARD CARGO DOOR SCUFF PLATE STRUCTURE CRACKED 2 INCH ON BOTTOM LEFT SIDE AT STATIO N 450. REMOVED CRACKED AREA AND REPAIRED IAW SRM 51-40-3, FIGURE 1, AND SRM 51-30-02. (M) 2 L 7 2 4F A16WE 1998041000558 19980410 00558 NM 1998 4 10 TSAA9753164 1 19980225 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 645 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING LAP JOINT INSPECTION, CRACK WAS FOUND ON FLOORBEAM BS 645, LBL 40. REMOVED ANGLE FABRICATED REPAIR ANGLE PER SRM 51-10-1, ALODINED PART PER SRM 51-30-5, PRIMED REPAIR ANGLE PER SRM 51-10-2. INSTALLED REPAIR ANGLE AND FASTENERS PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998041000559 19980410 00559 NM 1998 4 10 TSAA9751163 1 19980220 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 706 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 DURING LAP JOINT INSPECTION, CRACK WAS FOUND ON CENTER LONGITUDINAL FLOORBEAM STATION 706, BL 0. REPAIRED IAW WITH SRM 51-40-02. (M) 2 L 7 2 4F A16WE 1998041000560 19980410 00560 EU 1998 4 10 SIMA980764 1 19980317 A 5320 S53678008216 ZEE CHANNEL AEROSP ATR42 ATR42300 8680920 EU CARGO COMPT CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT AFT CARGO Z-CHANNEL WAS CORRODED. MAINTENANCE REMOVED AND REPL ACED THE Z-CHANNEL IAW SRM 52-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000561 19980410 00561 EU 1998 4 10 SIMA980763 1 19980317 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 38 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAM 38 IAW SRM 53-25-03. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000562 19980410 00562 EU 1998 4 10 SIMA980753 1 19980316 A 5311 S53671310200 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED FRAME 37 WAS CORRODED AT FLOOR LEVEL. MAINTENANCE REPAIRED FRAME 37 IAW SRM 53-67-70, FIGURE 402. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000563 19980410 00563 EU 1998 4 10 SIMA980752 1 19980316 A 5311 S5376131024251 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED FRAME 36 WAS CORRODED AT SILL PLATE. MAINTENANCE REPAIRED FRAME 36 IAW SRM 53-61-40. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000564 19980410 00564 EU 1998 4 10 SIMA980751 1 19980316 A 5313 S53671000203 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED STRINGER 17 RIGHT CORRODED BETWEEN FRAMES 30 AND 35. MAINTENANCE R EPAIRED STRINGER 17R IAW SRM 53-00-00, FIGURE 427. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000565 19980410 00565 EU 1998 4 10 SIMA980761 1 19980317 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 0209 ORD - FORWARD EMERGENCY LIGHTING INOP. REPLACED EMERGENCY BATTERY PACKS AND POWER SUPPLIES FOR 3WL AND 27WL IAW ATR-42 JIC 33-51-21. OPERATIONAL CHECKS GOOD AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000566 19980410 00566 EU 1998 4 10 SIMA980762 1 19980317 A 3350 8G500542405 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344SB 340B344 BULB TO EMERGENCY LIGHTING AT ROW 7 NOT WORKING. RAI LIGHT BULB FOR EMERGENCY LIGHTING AT ROW 7. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998041000567 19980410 00567 1998 4 10 REXA98070 4 19980316 A 3425 6226190113 AHARS COMPUTER SAAB SF340 SF340A 7850100 EU LEFT FAILED A REXA K NONE O OTHER CR CRUISE 1 SO 25 326PX 388 340A054 CAPTAINS HEADING FAILED 40 DEGREES OFF. TRY HDL SLAVE NUMEROUS TIMES NO RESULTS. REMOVED AND REPLACED AHARS COMPUTER O N CAPTAINS SIDE. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998041000568 19980410 00568 EU 1998 4 10 REXA98069 1 19980313 A 3251 3810009104 ACTUATOR SAAB SF340 SF340A 7850100 EU NLG STEERING FAILED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 406BH 61 340A074 DURING TAXI STEERING TILLER BECAME DIFFICULT TO TURN. NOSE WHEEL WAS UNCONTROLLABLE. HYD PUMP RAN NORMALLY WHEN DEPRES SED AND HYD WAS OK. AFTER EXCERSIZING TILLER IT BEGAN WORKING FOR A SHORT TIME. REMOVED AND REPLACED NOSE WHEEL STEERI NG SERVO ACTUATOR IAW 32-50-25. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998041000569 19980410 00569 1998 4 10 REXA98071 4 19980316 A 3422 258719343 DIRECTIONAL GYRO BAG JETSTM JETSTM3101 1500215 EU NR 1 INOP A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 317PX 86059544 688 NR 1 COMPASS INOP DURING TAXI. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998041000570 19980410 00570 CE 1998 4 10 98ZZZM390 1 19980225 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG LEAKING A JJBA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 EA 01 853CA FAH0052A UE56 LANDING GEAR FAILED TO EXTEND IN NORMAL MODE. (M) 2 L 7 2 4T RT A24CE 1998041000571 19980410 00571 NM 1998 4 10 F3LA98008 1 19980318 A 3350 6104789 BATTERY PACK BOEING 737 7372L9 1384497 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 270FL 22733 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY LIGHTS INOPERATIVE AT RIGHT OVERWING AND AFT OF RIGHT WING PO SITIONS. REPLACED BATTERY PACK AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1998041000572 19980410 00572 NM 1998 4 10 F3LA98009 1 19980317 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN LOOSE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 205AU 19421 PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 4 A, B, C INOPERATIVE. MAINTENANCE REP AIRED WIRING AND SECURED WIRING HARNESS AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998041000573 19980410 00573 EU 1998 4 10 C2XA98IA075 1 19980310 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING A-CHECK INSPECTION, THE EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY 3WL DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE ASSOCIATED POWER SUPPLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 H 7 2 4T RT A53EU 1998041000574 19980410 00574 EU 1998 4 10 C2XA98IA074 1 19980310 A 3350 3011157 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING A-CHECK INSPECTION, THE EMERGENCY LIGHTS ASSOCIATED WITH POWER SUPPLY 10WL WOULD NOT ILLUMINATE. MAINTENAN CE REMOVED AND REPLACED THE BATTERY PACK IN THE POWER SUPPLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000575 19980410 00575 SO 1998 4 10 C2XA98IA070 1 19980310 A 3350 D43682 CONNECTOR EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16724 120171 IAH - DURING PRE-FLIGHT INSPECTION, THE PILOT REPORTED THAT ONE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE RELEASED T HE AIRCRAFT UNDER MEL, AND SUBSEQUENTLY REPAIRED WIRE CONNECTOR SPANAQ IAW EMB-120 WIRING MANUAL 20-00-03 AND REMOVED TH E ITEM FROM MEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041000576 19980410 00576 SO 1998 4 10 C2XA98CL025 1 19980312 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO RT MLG OUT OF ADJUST A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 27707 120095 DAY - FLT 3233 - CREW REPORTED THE RIGHT MAIN LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS MAINTENANC E FERRIED TO CLE. MAINTENANCE INSPECTED THE LANDING GEAR THEN CLEANED AND ADJUSTED THE RIGHT MAIN LANDING GEAR RETRACT AND EXTENDED ACTUATOR IAW EMB-120 MM 32-32-10. OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-120 MM 32-30-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041000577 19980410 00577 SO 1998 4 10 C2XA98CL24 1 19980312 A 2916 3182001003 RESERVOIR EMB 120 EMB120RT SO LT HYD SYSTEM MOISTURE CONTAM A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 16723 18127 120169 CLE - FLT 3349 - CREW REPORTED THE MAIN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON TAKEOFF, ON THE GREEN SIDE. SI MULTANEOUSLY THE HYDRAULIC LOW PRESSURE RESERVOIR LIGHT ILLUMINATED, AND THE BLUE SYSTEM PRESSURE FLUCTUATED. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE DRAINED MOISTURE FROM THE NR 1 RESERVOIR, OPERATIONAL CHECKS OF BOTH SYSTEM WERE SATISFACTORY IAW EMB-120-MM 29-10-03. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041000578 19980410 00578 GL 1998 4 10 C2XA98CL023 2 19980309 A 7530 23058911 ACTUATOR EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LT ENGINE FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15926 145005 310025 EWR - FLT 4023 - CREW REPORTED DURING CLIMB-OUT, RECEIVED A LOW N1 WARNING ON THE LEFT ENGINE. THE ENGINE WAS SHUT DOWN AS A PRECAUTION AND THE AIRCRAFT RETURN TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT E NGINE COMPRESSOR VARIABLE GUIDE VANE ACTUATOR IAW EMB-145 MM 75-33-01. OPERATIONAL CHECKS WERE SATISFACTORY, FEDEC 1A W AS ALSO REMOVED AND REPLACED FOR PRECAUTIONARY MEASURES. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1998041000579 19980410 00579 GL 1998 4 10 C2XA98CL027 2 19980315 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 15932 145015 CAE310020 CLE - FLT 9500 - CREW REPORTED DURING TAKEOFF, THE LEFT ENGINE OIL PRESSURE EXCEEDED MANUFACTURES LIMITS. AIRCRAFT LAND ED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPERSS TASK CARD NR 6271 001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1998041000580 19980410 00580 NE 1998 4 10 C2XA98CL028 2 19980315 A 7250 TURBINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 81536 UE152 CLE - DURING A SCHEDULED INSPECTION, THE RIGHT ENGINE WAS FOUND TO HAVE A BLADE TIP MISSING ON THE 2ND STAGE POWER TURBI NE. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 4272003. OPERATIONAL AND LE AK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1998041000581 19980410 00581 NM 1998 4 10 C8GA982102 1 19980321 A 2130 PRESSURIZATION BOEING 727 727230 1384080 NM CABIN MALFUNCTIONED A C8GA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 15 357KP 20675 FLT CCI104 - DAY/TPA - AT FL330, A/C PRESSURIZATION (CABIN) BEGAN TO CLIMB. UPON DESCENT TO 10,000 FT MSL, THE CABIN WA S RE-PRESSURIZED AT APPROXIMATELY 17,000 FT MSL BY RECYCLING THE BLEED SW'S. PSI DIFF WAS 8.5. DIVERTED TO CAE FOR PRE CAUTION. C/W MM 21-31-0. OPERATION PRESSURIZATION SYSTEM CARRIED OUT IAW MM 21-31-0. SYSTEM CHECKS GOOD. (M) 2 L 7 3 4F A3WE 1998041000582 19980410 00582 NM 1998 4 10 TWRA9814 1 19980320 A 3350 LIGHT BOEING 747 747282B 1384860 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 15 610FF 20501 PRIOR TO DEPARTURE, FORWARD OF 'E' ZONE RT SIDE 'E' PATH LIGHT INOP. FOUND RT 'E' ZONE LIGHTS EGRESS CONNECTION TO GALL EY WET, DRIED CONNECTION. OPS CHECK OK PER MM 33-59-00 PAGE 501. (M) 2 L 7 4 4F A20WE 1998041000594 19980410 00594 WP 1998 4 10 TWAA9803809 1 19980316 A 2160 SRL92G INDICATOR DOUG DC9 DC982 3022082 WP COCKPIT WORN A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 913TW 49184 STL - FLT 715 - OVERHEAT ODOR IN CABIN AND COCKPIT WHILE ON APPROACH. NO OVERHEAT INDICATION. WING AND ENGINE ANTI-ICE ON. GAUGES DID NOT INDICATE HOT, SOME SMOKE IN CABIN. TURNED OFF ALL SYSTEMS. REPLACED LEFT TEMP CONTROL VALVE POSN IND AND RESEATED CONNECTOR FOR THE TEMP CONTROL VALVE. (M) 2 L 7 2 4F A6WE 1998041000604 19980410 00604 NM 1998 4 10 TWAA9803706 1 19980313 A 5330 SKIN BOEING 767 767231 1385131 NM BS 1285 BULGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 LAX - DURING C-CHECK, FOUND FUSELAGE STRINGER 35L WITH A BULGE IN THE SKIN BETWEEN RIVETS, FUSELAGE STATION 1285. REMOV ED FOREIGN OBJECT FROM BENEATH SKIN AND STRINGER. INSTALLED REPAIR DUE TO CRACK PER SRM 53-00-01. (M) 2 L 7 2 4F RT A1NM 1998041000605 19980410 00605 WP 1998 4 10 TWA9803704 1 19980315 A 3350 14597101 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 924L 47324 STL - FLT 218 - DURING PREFLIGHT, ONE SECTION OF OVERHEAD EMERGENCY LIGHTS IN COACH WERE FOUND INOPERATIVE. REPLACED BA TTERIES IN POWER PACK B-2. CHECK-C 8-6-97 MCI. (M) 2 L 7 2 4F A6WE 1998041000606 19980410 00606 NM 1998 4 10 TWAA9803703 1 19980314 A 3350 1102837 LIGHT BOEING 727 727231 1384079 NM AIRSTAIR INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54351 21983 MCO - DURING OVERNIGHT MAINTENANCE, THE VENTRAL AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND INOPERATIVE. PLACARDED INOPERATI VE PER MEL. AT THE NEXT STATION THE LIGHT ASSEMBLY WAS REPLACED. CHECK-C 10-31-97. (M) 2 L 7 3 4F A3WE 1998041000607 19980410 00607 WP 1998 4 10 TWAA9803702 1 19980315 A 5350 591009113 RADOME DOUG DC9 DC932 3022066 WP FWD FUSELAGE PUNCTURED A TWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 CE 05 923L 47109 MSY - FLT 8689 - CREW REPORTED LOUD BANG FROM NOSE OF AIRCRAFT, MADE UNSCHEDULED LANDING AT MSY. FOUND BIRD STRIKE TO R ADOME AT 9 O'CLOCK POSITION. REPLACED RADOME AND REPAIRED METAL DAMAGE AT THE JOINT BETWEEN RADOME AND FUSELAGE. CHECK -C 2-11-98 STL. (M) 2 L 7 2 4F A6WE 1998041000608 19980410 00608 WP 1998 4 10 TWAA9803701 1 19980314 A 3350 CIRCUIT BREAKER DOUG DC9 DC983 3022083 WP CABIN TRIPPED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9404V 53140 MCI - DURING OVERNIGHT MAINTENANCE, THE FIRST CLASS EGRESS LIGHTS WERE FOUND INOPERATIVE. RESET CIRCUIT BREAKER. CHECK -C 1-31-98 LAX. (M) 2 L 7 2 4F RT A6WE 1998041000609 19980410 00609 NM 1998 4 10 TWRA9813 1 19980318 A 2433 RECTIFIER BOEING 747 747131 1384881 NM E/E COMPT NOT CONNECTED A TWRA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 EA 15 608FF 19672 AT ROTATE, ALL DC POWER WAS LOST. ONLY BATTERY POWER WAS NORMAL. FLIGHT DIVERTED IN VMC TO BGR. NORMAL LANDING. RERA CKED NR 1, NR 2, NR 3 AND ESS TR, FOUND ALL TR WERE DISCONNECTED FROM RACK. RAN ALL ENGINE IAW WITH MM 71-00-00. STEP 3, ALL SYSTEM CHECKED OK. (M) 2 L 7 4 4F A20WE 1998041000610 19980410 00610 1998 4 10 USAASB98045 4 19980218 A 3454 DMN426 VOR ANTENNA BOEING 737 737301 1384611 NM FUSELAGE MALFUNCTIONED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 300AU 23228 PIT - FLT 8051 - ON APPROACH TO PIT ON LOC INTERCEPT, CREW LOST SIGNAL ON BOTH SIDES WITH FLIGHT DIERECTOR AND AUTOPILOT COUPLED. AFTER ACCOMPLISHING GO-AROUND, CREW DID THE APPROACH HAND FLOWN WITHOUT THE FLIGHT DIRECTOR AND EVERYTHING SE EMED NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD VOR ANTENNA AND THE NR 1 VOR/ILS NV RECEIVER. OPERATIONAL TEST NORMAL. (M) 2 L 7 2 4F RT A16WE 1998041000611 19980410 00611 1998 4 10 98ZZZM391 4 19980218 A 3454 20412343422 NAV RECEIVER BOEING 737 737301 1384611 NM E/E COMPT MALFUNCTIONED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 300AU 23228 PIT - FLT 8051 - ON APPROACH TO PIT ON LOC INTERCEPT, CREW LOST SIGNAL ON BOTH SIDES WITH FLIGHT DIERECTOR AND AUTOPILOT COUPLED. AFTER ACCOMPLISHING GO-AROUND, CREW DID THE APPROACH HAND FLOWN WITHOUT THE FLIGHT DIRECTOR AND EVERYTHING SE EMED NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FORWARD VOR ANTENNA AND THE NR 1 VOR/ILS NV RECEIVER. OPERATIONAL TEST NORMAL. (M) 2 L 7 2 4F RT A16WE 1998041000612 19980410 00612 1998 4 10 USAASB98044 4 19980217 A 3454 20412343422 NAV RECEIVER BOEING 737 737301 1384611 NM E/E COMPT MALFUNCTIONED A USAA L A ABORTED APPROACH UNSCHED LANDING O OTHER AP APPROACH 1 EA 19 300AU 23228 IAD - FLT 826 - ON APPROACH INTO DCA, BOTH LOCALIZERS WERE REPORTED TO BE INTERMITTENT AT 109.9 TWO ATTEMPTS WERE MADE W ITH THE SAME RESULT. FLIGHT DIVERTED TO IAD WHEREAS BOTH LOCALIZERS WERE INTERMITTENT AT 109.3. RECEIVED ALTITUDE ALER T FROM TOWER ON APPROACH. BOTH ALTIMETERS READ 700 FEET. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 VOR/ILS NAV RECEIVER, FLIGHT INSTRUMENT ACCESSORY UNIT AND THE NR 1 ILS RELAY. PERFORMED OPERATIO NAL CHECK OF NAV SYSTEM PER MM 34-31-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998041000613 19980410 00613 1998 4 10 98ZZZM392 4 19980217 A 3454 6552805379 ACCESSORY UNIT BOEING 737 737301 1384611 NM E/E COMPT MALFUNCTIONED A USAA L A ABORTED APPROACH UNSCHED LANDING O OTHER AP APPROACH 1 EA 19 300AU 23228 IAD - FLT 826 - ON APPROACH INTO DCA, BOTH LOCALIZERS WERE REPORTED TO BE INTERMITTENT AT 109.9 TWO ATTEMPTS WERE MADE W ITH THE SAME RESULT. FLIGHT DIVERTED TO IAD WHEREAS BOTH LOCALIZERS WERE INTERMITTENT AT 109.3. RECEIVED ALTITUDE ALER T FROM TOWER ON APPROACH. BOTH ALTIMETERS READ 700 FEET. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 VOR/ILS NAV RECEIVER, FLIGHT INSTRUMENT ACCESSORY UNIT AND THE NR 1 ILS RELAY. PERFORMED OPERATIO NAL CHECK OF NAV SYSTEM PER MM 34-31-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998041000614 19980410 00614 1998 4 10 98ZZZM393 4 19980217 A 3451 D2723Q1 ILS RELAY BOEING 737 737301 1384611 NM E/E COMPT MALFUNCTIONED A USAA L A ABORTED APPROACH UNSCHED LANDING O OTHER AP APPROACH 1 EA 19 300AU 23228 IAD - FLT 826 - ON APPROACH INTO DCA, BOTH LOCALIZERS WERE REPORTED TO BE INTERMITTENT AT 109.9 TWO ATTEMPTS WERE MADE W ITH THE SAME RESULT. FLIGHT DIVERTED TO IAD WHEREAS BOTH LOCALIZERS WERE INTERMITTENT AT 109.3. RECEIVED ALTITUDE ALER T FROM TOWER ON APPROACH. BOTH ALTIMETERS READ 700 FEET. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 VOR/ILS NAV RECEIVER, FLIGHT INSTRUMENT ACCESSORY UNIT AND THE NR 1 ILS RELAY. PERFORMED OPERATIO NAL CHECK OF NAV SYSTEM PER MM 34-31-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998041000615 19980410 00615 NM 1998 4 10 USAASB98053 1 19980306 A 2120 AIR DISTRIBUTION BOEING 737 737301 1384611 NM CABIN ODOR A USAA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 354US 23557 BDL - FLT 331 - EN ROUTE FROM PIT TO BDL, A PASSENGER COMPLAINED OF A SMOKEY SMELL IN THE CABIN. PACKS WERE RUN ON HIGH . NO SOURCE COULD BE FOUND AND SMELL DISSIPATED. APU MASTER CAUTION CAME ON THREE MINUTES PRIOR TO REPORT OF ODOR. SM ELL RETURNED ON GROUND. BOTH PACKS NORMAL. APU WAS INOP PER MEL. MAINTENANCE INSPECTED AIR CONDITION SYSTEM INCLUDING ACM OIL AND WATER SEPARATOR CONDITION. CHECKED E/E COMPARTMENT AND CARGO BAYS. CHECKED ENGINE OIL LEVELS. TAXIED TO RUNUP AREA AND RAN ENGINES AT CRUISE POWER WITH BOTH PACKS ON. NO FAULTS NOTED. COULD NOT DUPLICATE SMELL. (M) 2 L 7 2 4F RT A16WE 1998041000616 19980410 00616 WP 1998 4 10 USAA980117 1 19980307 A 5720 59373291 DOUBLER DOUG DC9 DC981 3022081 WP MLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805US 45431 48053 PIT - DURING Q-1 CHECK, FOUND 1.5 INCH CRACK TOPWING MLG BEAVER TAIL DOUBLER. MADE INTERIM REPAIR, TRIM OUT CRACK PER S RM 57-03 FIG 27 AND EA 49160. (M) 2 L 7 2 4F A6WE 1998041000617 19980410 00617 EU 1998 4 10 USAAF98026 1 19980311 A 3230 RETRACT MECH FOKKER F28 F28MK0100 4990807 EU NLG LACK OF LUBE A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 866US 11310 PIT - 1221 - DURING APPROACH INTOP PIT CREW RECEIVED A NOSE GEAR UNSAFE INDICATION WHEN LOWERING THE LANDING GEAR. CREW ADVISED ATC, EXECUTED A GO-AROUND AND RECYCLED THE GEAR. AFTER RECYCLING THE GEAR ALL INDICATIONS WERE NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE LUBRICATED THE NOSE GEAR AND ASSOCIATED COMPONENTS. GEAR SWING WAS GOOD. (M) 2 L 7 2 4F RT 1998041000618 19980410 00618 EU 1998 4 10 USAAF98027 1 19980311 A 3230 D76351001 CABLE FOKKER F28 F28MK0100 4990807 EU LANDING GEAR DAMAGED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 853US 11281 MSP - FLT 1756 - ON SHORT FINAL APPROACH AT MSP, WAS UNABLE TO MOVE THE LANDING GEAR HANDLE TO THE DOWN POSITION. THE ALTERNATE LANDING GEAR EXTENSION PROCEDURE WAS USED TO LOWER THE LANDING GEAR. GEAR FELL AND THREE GREENS WERE ILLUMINA TED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. GEAR WAS PINNED AND AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE CLEANED LANDING GEAR VALVE AND LUBED SAME AT NOSE GEAR WHEEL WELL. OPS CHECK HANDLE SEVERAL TIMES. RESET ALTERNATE GEAR EXTENS ION HANDLE, REMOVED GEAR PINS. AIRCRAFT OK FOR FERRY FLIGHT TO PIT. AT PIT, MAINTENANCE REPLACED THE TELEFLEX CABLE TH AT ATTACHES TO THE GEAR HANDLE ROD ASSEMBLY AND THE FORWARD TUBE ASSEMBLY. (M) 2 L 7 2 4F RT 1998041000619 19980410 00619 EU 1998 4 10 98ZZZM394 1 19980311 A 3230 D76395401 TUBE FOKKER F28 F28MK0100 4990807 EU LANDING GEAR DAMAGED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 853US 11281 MSP - FLT 1756 - ON SHORT FINAL APPROACH AT MSP, CAPTAIN WAS UNABLE TO MOVE THE LANDING GEAR HANDLE TO THE DOWN POSITION . THE ALTERNATE LANDING GEAR EXTENSION PROCEDURE WAS USED TO LOWER THE LANDING GEAR. GEAR FELL AND THREE GREENS WERE I LLUMINATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. GEAR WAS PINNED AND AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE C LEANED LANDING GEAR VALVE AND LUBED SAME AT NOSE GEAR WHEEL WELL. OPS CHECK HANDLE SEVERAL TIMES. RESET ALTERNATE GEAR EXTENSION HANDLE, REMOVED GEAR PINS. AIRCRAFT OK FOR FERRY FLIGHT TO PIT. AT PIT, MAINTENANCE REPLACED THE TELEFLEX C ABLE THAT ATTACHES TO THE GEAR HANDLE ROD ASSEMBLY AND THE FORWARD TUBE ASSEMBLY. (M) 2 L 7 2 4F RT 1998041000620 19980410 00620 EU 1998 4 10 WTAA980045 1 19980311 A 7603 1379079E409 SPEED LEVER BAG JETSTM JETSTM3101 1500215 EU LT ENGINE OUT OF ADJUST A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 431UE 813 SMF - LEFT ENGINE SPEED LEVER DOES NOT HOLD POSITION WITH FRICTION LOCK APPLIED DURING TAKEOFF ROLL. TAKEOFF ABORTED. A IRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE CLEANED AND ADJUSTED SPEED LEVER FRICTION LOCK. SYSTEM OPERATIONAL CHE CK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998041000621 19980410 00621 SO 1998 4 10 WTAA980046 1 19980313 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG FAILED A WTAA K NONE J WARNING INDICATION CL CLIMB 1 WP 17 453UE 120148 LAX - LANDING GEAR WOULD NOT RETRACT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR RETRACTION ACTUATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041000622 19980410 00622 SO 1998 4 10 WTAA980047 1 19980314 A 3260 922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO NLG INTERMITTENT A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 216YV 120216 FAT - GEAR WOULD NOT RETRACT ALONG WITH NOSE RED INTRANSIT LIGHTS. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAIN TENANCE SWAPPED PROXIMITY SENSORS AND DEFERRED PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING NOSE LANDING GEAR 'A' UPLOCK PROXIMITY SENSOR. OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1998041000623 19980410 00623 EU 1998 4 10 WTAA980042 1 19980304 A 7712 TQ INDICATION BAG JETSTM JETSTM3101 1500215 EU LT/RT ENGINE DROPPED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 431UE 813 FAT - LEFT ENGINE TORQUE DROPPED TO 80 PERCENT ON TAKEOFF. TAKEOFF ABORTED. MAINTENANCE PERFORMED TWO POINT RUN OF LEF T AND RIGHT ENGINES. UNABLE TO DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998041000624 19980410 00624 SO 1998 4 10 WTAA980041 1 19980304 A 2120 AIR DISTRIBUTION EMB 120 EMB120RT SO CABIN ODOR A WTAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 17 284YV 120284 LAX - SMOKE SMELL IN CABIN REPORTED. MAINTENANCE DEFERRED COOLING SYSTEM PER MEL 21-51-2. AIRCRAFT RETURNED TO SERVICE . MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY PERFORMING OPERATIONAL CHECK. UNABLE TO DUPLICATE DISCREPANCY. SWAPPED GROUND COOLING FANS FOR TROUBLESHOOTING. (M) 2 L 7 2 4T RT A31SO 1998041000625 19980410 00625 WP 1998 4 10 VJ9800052 1 19980321 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 948VV 47559 MAIN CABIN DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY, OPS CHECKED GOOD IAW MM 33-50. (M) 2 L 7 2 4F A6WE 1998041000626 19980410 00626 NM 1998 4 10 TSAA9853160 1 19980304 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 850 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 ON SERVICE CHECK, FUOND A FUSELAGE SKIN CRACK AT BS 850 STRINGER 21R. REPAIRED PER SRM 53-30-3 FIG 6. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041000627 19980410 00627 NM 1998 4 10 TSAA9832162 1 19980308 A 3240 26066724 BRAKE BOEING 737 7372T4 1384492 NM NR 3 LEAKING A TSAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 WP 13 808AL 23445 FLT 90 - HNL-KOA - AFTER TAKEOFF WITH GEARS AND FLAPS COMING UP, SYSTEM 'A' HYDRAULIC QUANTITY WAS DECREASING'. LANDED 26R WITHOUT INCIDENT. TOWED TO GATE. MAINTENANCE FOUND NR 3 BRAKE LEAKING. REPLACED NR 3 BRAKE ASSY AND REPLENISHED H YDRAULIC FLUID, OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041000628 19980410 00628 NM 1998 4 10 TWRA9811 1 19980304 A 3350 PRS1B BATTERY CHARGER BOEING 747 747212B 1384886 NM CABIN TRIPPED A TWRA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 EA 15 616FF 21939 AFTER PUSH BACK, 'E' ZONE EMERGENCY LIGHTS ON, UNABLE TO RESET. REMOVED AND REPLACED BATTERY CHARGER 'E' ZONE LEFT REAR . OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1998041000629 19980410 00629 NM 1998 4 10 TWRA9812 1 19980315 A 2820 2172005 CHECK VALVE BOEING 747 747238B 1384828 NM NR 2 MAIN TANK STUCK OPEN A TWRA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 607PE 20011 IN CRUISE, ON CENTER TANK TO ALL ENGINE FUEL FEED, FUEL MIGRATED INTO NR 2 MAIN TANK AT RATE OF 1800 LBS PER HR, ALL FOU R CROSS FEEDS OPEN, 1 AND 4 MAIN BOOST PUMPS OFF, 2 AND 3 CENTER WING PUMPS ON FOR TROUBLESHOOTING. TURNED OFF NR 2 MAI N FORWARD AND AFT PUMPS ONE AT A TIME. THE NR 2 MAIN FORWARD 'PRESS' LIGHT DOES NOT COME ON WITH THE PUMP SWITCH OFF. A LL OTHER INDICATIONS NORMAL. AIR TURN BACK TO JED. REMOVED AND REPLACED NR 2 FORWARD BOOST PUMP DISCHARGE PORT CHECK V ALVE IAW MM 28-22-03. OPS CHECK AND LEAK CHECK OK. (M) 2 L 7 4 4F A20WE 1998041000630 19980410 00630 EU 1998 4 10 SIMA980722 1 19980313 A 3397 WIRE AEROSP ATR72 ATR72212 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 274AT 238 274 ONE FLORO PROX LIGHT INOP BY GALLEY DUE TO BROKEN WIRE. ISSUED MEL 33-22 AND RETURNED A/C TO SERVICE. REPAIRED BROKEN WIRE IN ACC WITH STD PRACTICES. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000631 19980410 00631 EU 1998 4 10 SIMA980721 1 19980313 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 425MJ 238 425 HOUR - EMERGENCY LIGHT BATTERY PACK GALLEY EXIT LIGHT DEAD POSITION 62WL. RAI'D BATTERY PACK 62WL, OPS CHECKED GOOD. A /C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000632 19980410 00632 NM 1998 4 10 MASA98052 1 19980310 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 DURING A-CHECK INSPECTION, MAINTENANCE FOUND THE CENTER AFT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BULB, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998041000633 19980410 00633 SO 1998 4 10 ASOA98019 1 19980209 A 2150 PACK EMB 120 EMB120RT SO LEFT MALFUNCTIONED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 227AS 120023 LEFT AIR CONDITIONING PACK FILLED THE AIRCRAFT WITH A BURNING ODOR AND FAILED. RESET NORMALLY BUT THE ODOR REMAINED. D FW, MAINTENANCE INSPECTED LEFT PACK, NO DEFECTS NOTED. GROUND OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASE D FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041000634 19980410 00634 EU 1998 4 10 98ZZZM395 1 19980222 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 634AS 370 SAW - DURNG C-CHECK INSPECTION, MAINTENANCE REPORTED RT FA SEAT TRACK CORRODED. INSTALLED NEW RT FA SEAT TRACK IAW ASA EO 72-53-0043. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000635 19980410 00635 EU 1998 4 10 98ZZZM396 1 19980220 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 634AS 370 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LEFT OUTBOARD AFT SEAT TRACK CORRODED. INSTALLED NEW LEFT OUTBOAR D AFT SEAT TRACK IAW ASA EO 72-53-0044. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000636 19980410 00636 EU 1998 4 10 98ZZZM397 1 19980222 A 5347 S5357020320002 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 634AS 370 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT INBOARD MIDDLE SEAT TRACK CORRODED. INSTALLED NEW RT INBOARD M IDDLE SEAT TRACK IAW ASA SRM 51-25-04 AND EO 72-53-0044. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000637 19980410 00637 EU 1998 4 10 98ZZZM398 1 19980222 A 5347 S536780011210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 634AS 370 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LEFT FA SEAT TRACK CORRODED. INSTALLED NEW LEFT FA SEAT TRACK IAW ASA EO 72-53-0043. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000638 19980410 00638 EU 1998 4 10 98ZZZM399 1 19980222 A 5347 S5357020320202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 634AS 370 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT MIDDLE OUTBOARD SEAT TRACK CORRODED. INSTALLED NEW RT MIDDLE O UTBOARD SEAT TRACK IAW ASA EO 72-53-0044. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000639 19980410 00639 EU 1998 4 10 98ZZZM400 1 19980224 A 5320 S53572405211 FITTING AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 634AS 370 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED STRINGER NR 16 RT END FITTING CORRODED AT FRAME 27 RT. INSTALLED NEW STRINGER END FITTING IAW ASA EO 72-53-0046. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041000640 19980410 00640 NM 1998 4 10 98ZZZM401 1 19980226 A 3350 320559 SPLICE BOEING 737 7372H5 138448E NM CABIN BROKEN A E9WA K NONE L NO TEST IN INSP/MAINT 1 SO 05 221US 20454 ON OVERNIGHT CHECK, FOUND ROW 2 EMERGENCY LIGHT INOP. FOUND BUTT SPLICE BROKEN. REINSTALLED NEW SPLICE, OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1998041000641 19980410 00641 NM 1998 4 10 98ZZZM402 1 19980222 A 3350 MS1557081 LAMP BOEING 737 737247 138448D NM CABIN FAILED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 487GS 19600 RIGHT EXTERIOR EMERGENCY EXIT LIGHTS INOP. FOUND ON AMPLIFIED PREFLIGHT. RELAMPED EMERGENCY LIGHT IAW BOEING MM 33-51- 22. (M) 2 L 7 2 4F A16WE 1998041000642 19980410 00642 NM 1998 4 10 98ZZZM403 1 19980222 A 3350 PIN BOEING 737 737247 138448D NM CABIN BENT A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 487GS 19600 RIGHT EXTERIOR EMERGENCY EXIT LIGHT INOP. FOUND ON AMPLIFIED PREFLIGHT. STRAIGHTENED PINS ON RT BATTERY PACK CHARGER. (M) 2 L 7 2 4F A16WE 1998041000643 19980410 00643 WP 1998 4 10 98ZZZM404 1 19980318 A 2910 1530501249 HYD LINE LKHEED 1011 10113851 5265010 WP LT WING LEAKING A WRNA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 05 311EA 193A1012 SYSTEM 'C' HYD RSVR QTY LOW AND DECREASING. SWITCHING PUMP OFF DID NOT STOP FLUID LOSS. REF MANUAL GEAR EXTENSION, ATM TURNED OFF FLUID LOSS STOPPED AT AROUND THREE-EIGHTHS TANK QTY. AIRCRAFT LANDING NORMAL. FOUND PIN HOLE LEAK IN HYD C -CHECK SYSTEM RETURN LINE IN LEFT WING. LINE REPAIRED BY 'PERMASWAGE' COUPLING IAW 20-29-04 LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 1998041000644 19980410 00644 NM 1998 4 10 98ZZZM405 1 19980221 A 3350 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 783AT 22000 ROW 1 TO 10 EGRESS LIGHTS OUT. REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1998041000645 19980410 00645 NM 1998 4 10 98ZZZM406 1 19980107 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 783AT 22000 DURING PREFLIGHT, THE EGRESS LIGHT WAS FOUND INOP, AT ROW 28 ABC. REPAIRED BY REPLACING EGRESS LIGHT HOLDER. 2 L 7 3 4F A3WE 1998041000646 19980410 00646 NM 1998 4 10 98ZZZM407 1 19980104 A 3350 LIGHT BOEING 727 727264 138408M NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 765AT 23014 IND - DURING PRE-FLIGHT, THE AFT ENTRY FOR AIRSTAIR EGRESS LIGHT IS INOP. REMOVED AND REPLACED LIGHT ASSY AND OPS CHEC K NORMAL. (M) 2 L 7 3 4F A3WE 1998041000647 19980410 00647 WP 1998 4 10 98ZZZM408 1 19980102 A 3350 LIGHT PANEL LKHEED 1011 10113851 5265010 WP EXTERIOR FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 188AT 193C1078 CLE - WHEN REMOVING POWER FROM AIRCRAFT ALL EMERGENCY LIGHTS (INSIDE AND OUT) CAME ON. WOULD NOT TURN OFF UNTIL POWER W AS REAPPLIED TO AIRCRAFT. INSTALLED NEW EXTERIOR LIGHTS PANEL PER MM 33-51-01. EMERGNCY LIGHTS CHECKED NORMAL. (M) 2 L 7 3 4F A23WE 1998041000648 19980410 00648 NM 1998 4 10 98ZZZM409 1 19980205 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN MISSING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 767AT 22001 DURING P/F FOUND THE FORWARD EMERGENCY CEILING AREA LIGHT MISSING (NEAR ROW 11). REPLACED MISSING AREA LIGHT AS REQUIRE D, OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1998041000649 19980410 00649 NM 1998 4 10 98ZZZM410 1 19980207 A 3350 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 773AT 22004 DURING P/F FOUND THE EMERGENCY EXIT LIGHT ON AFT CARGO DOOR INOP. REPLACED BATTERY PACK FOR EMERGENCY LIGHT ON AFT CARG O DOOR. (M) 2 L 7 3 4F A3WE 1998041000650 19980410 00650 NM 1998 4 10 98ZZZM411 1 19980213 A 3350 BATTERY PACK BOEING 727 7272B7 138407L NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 762AT 22162 DURING P/F FOUND LEFT FORWARD EMERGENCY EGRESS LIGHT INOP (EXTERIOR). REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1998041000651 19980410 00651 NM 1998 4 10 98ZZZM412 1 19980218 A 3350 FUSE BOEING 727 7272B7 138407L NM CABIN BLOWN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 760AT 21954 DURING P/F FOUND MULTIPLE FLOOR AISLE LIGHTS INOP, FORWARD SECTION EGRESS. REMOVED AND REPLACED FUSE IN FORWARD EGRESS POWER PACK, OPS CHECKED OK PER MM. (M) 2 L 7 3 4F A3WE 1998041000652 19980410 00652 NM 1998 4 10 98ZZZM413 1 19980217 A 3397 WIRE BOEING 727 727290 138408W NM CABIN LOOSE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 774AT 21510 DURING P/F, FOUND EGRESS TRACK LIGHTING BETWEEN R2-L2 DOORS TORN UP, PIGTAILS RIPPED FROM SPLICES. REMOVED AND REPLACED TRACK AND REPLACED PIGTAIL, EGRESS LIGHTS, OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1998041000653 19980410 00653 NM 1998 4 10 98ZZZM414 1 19980218 A 3350 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 773AT 22004 RIGHT AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY. (M) 2 L 7 3 4F A3WE 1998041000655 19980410 00655 EU 1998 4 10 AALA980477 1 19980311 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FLOOR SUPPORT FRAME HAS CORROSION FROM DOOR TO NR 5 ROLLER TRAY AT FRAME 63. REMOVED AND REPLACED FLOOR SUPPORT P ER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998041000656 19980410 00656 EU 1998 4 10 AALA980492 1 19980311 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FLOOR BOARD SUPPORT AT FRAME 66 HAS CORROSION AROUND FASTENER HOLES TOP AND BOTTOM. INSTALLED DOUBLER ON FLOOR SU PPORT AT OUT OF LIMIT AREA PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1998041000657 19980410 00657 NM 1998 4 10 AALA980482 1 19980310 A 5330 SKIN BOEING 727 727223 1384074 NM BS 390-405 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6835 20188 TUL - SMALL CRACKS IN FUSE STATION 390 TO 405 STRINGER 19R AND 20R. CUTOUT DAMAGED AREA (CRACKS) FAB 2024-T3 .040 FILLE TS FOR CUT OUTS. INSTALL LARGER FILLET OVER DAMAGED AREA, LAP SEAM REPAIR SRM 53-30-3 FIG 24. (M) 2 L 7 3 4F A3WE 1998041000658 19980410 00658 EU 1998 4 10 AALA980447 1 19980306 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - NR 7 FLOOR SUPPORT CORRODED AT FRAME 13. INSTALLED STRAP ON FLOOR SUPPORT PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998041000659 19980410 00659 EU 1998 4 10 AALA980448 1 19980304 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU R1 DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - FLOOR BOARD SUPPORT CORRODED AT FORWARD GIRT BAR PAD R-1 DOOR. REMOVED AND REPLACD PART FLOOR BOARD SUPPORT. (M) 2 L 7 2 4F RT A35EU 1998041000660 19980410 00660 1998 4 10 HEEA0013569 4 19980326 A 3421 23501069 GYRO BEECH 200 200BEECH 1152920 CE ARTIFICIAL HORIZ UNKNOWN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 789DS BB478 GYRO SLOW TO ERECT. 1 L 7 2 4T A24CE 1998041000661 19980410 00661 1998 4 10 HEEA0013571 4 19980326 A 2210 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 AFCS COMPUTER INOPERATIVE. 1 G 7 2 4U H4SW 1998041000662 19980410 00662 SW 1998 4 10 HEEA0013572 1 19980326 A 2842 391046199 PROBE BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 INDICATES HIGH OUT OF TOLERANCE AND WIRE BURNT. 1 G 7 2 4U H4SW 1998041000663 19980410 00663 1998 4 10 HEEA0013573 4 19980326 A 3416 D120P2T ANEROID SNIAS 350 AS350B2 8680813 EU ALTIMETER DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 2873 READS 160 FEET OFF. BAROMETRIC ANEROID DEFECTIVE 1 G 7 1 3U H9EU 1998041000664 19980410 00664 1998 4 10 HEEA0013574 4 19980326 A 3416 5035P2P13 ALTIMETER BELL 412 412 1182202 SW ENCODER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 ENCODING ALTIMETER CARD TURNS WHEN KNOB IS TURNED. 1 G 7 2 4U H4SW 1998041000665 19980410 00665 SW 1998 4 10 HEEA0013575 1 19980326 A 6710 214001347005 ACTUATOR ROTARY BELL 412 412 1182202 SW CYCLIC MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 CYCLIC DOES NOT TEST LATERAL. 1 G 7 2 4U H4SW 1998041000666 19980410 00666 NE 1998 4 10 HEEA0013576 1 19980326 A 2436 7655009006105 CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 GENERATOR WILL NOT COME ON LINE. 1 G 7 2 3U H1NE 1998041000667 19980410 00667 NE 1998 4 10 HEEA0013577 2 19980326 A 7261 1742500 FILTER ASSY BOLKMS 117 BK117B2 5626013 EU LYC LTS101 LTS101650B1 41560 NE ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 OIL FILTER ASSY INOPERATIVE. 1 G 7 2 3U 3 U NC H13EU E5NE 1998041000668 19980410 00668 SW 1998 4 10 HEEA0013578 1 19980326 A 6510 407040325101 SHAFT BELL 407 407 SW T/R AFT DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 53114 T/R AFT SHAFT IS DAMAGED. 1 G 7 1 3U O H2SW 1998041000669 19980410 00669 1998 4 10 HEEA0013579 4 19980326 A 2312 4000103000 TRANSCEIVER BOLKMS 117 BK117B1 5626012 EU COCKPIT INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 RECEIVES INTERMITTENT AND MIKE GAIN DEVIATION INTERMITTENT. 1 G 7 2 3U H13EU 1998041000670 19980410 00670 1998 4 10 HEEA0013580 4 19980326 A 3421 5208130004 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 HORIZ INDICATOR FLAG STICKS, RESET BUTTON INTERMITTENT. GLIDE SLOPE FLAG STICKS AND PINS 52 AND 59 WILL NOT LOCK UP. 1 G 7 1 3U H2SW 1998041000672 19980410 00672 EU 1998 4 10 HEEA0013583 1 19980326 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J S826 TORQUE TRANSMITTER INOPERATIVE. 1 G 7 2 3U H3EU 1998041000673 19980410 00673 EU 1998 4 10 HEEA0013584 1 19980326 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J S826 INDICATOR INOPERATIVE. 1 G 7 2 3U H3EU 1998041000674 19980410 00674 1998 4 10 HEEA0013585 4 19980326 A 3416 1003511326 ALTIMETER SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 ALTIMETER HAS EXCESSIVE FRICTION ERROR. 1 G 7 2 3U H1NE 1998041000675 19980410 00675 NE 1998 4 10 HEEA0013586 1 19980326 A 6220 7610608000045 DAMPER SKRSKY S76 S76A 8143006 NE M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 706AE 760275 M/R DAMPER LEAKING. 1 G 7 2 3U H1NE 1998041000676 19980410 00676 NE 1998 4 10 HEEA0013587 1 19980326 A 6220 7610608000050 DAMPER SKRSKY S76 S76A 8143006 NE M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 22342 760096 M/R DAMPER LEAKING AND FLAT SPOT. 1 G 7 2 3U H1NE 1998041000677 19980410 00677 SW 1998 4 10 HEEA0013588 1 19980326 A 6720 7001483 ROLL CONTROL ROD BELL 412 412 1182202 SW T/R CONTROL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 ROLL KICKS IN FLIGHT. 1 G 7 2 4U H4SW 1998041000678 19980410 00678 1998 4 10 HEEA0013589 4 19980326 A 3425 5222638006 INDICATOR BEECH 200 200BEECH 1152920 CE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 789DS BB478 INDICATOR INTERNAL LIGHT IS INOPERATIVE. 1 L 7 2 4T A24CE 1998041000679 19980410 00679 EU 1998 4 10 HEEA0013590 1 19980326 A 7334 BSE20660G1 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4294R S860 TRANSMITS HIGH OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1998041000680 19980410 00680 EU 1998 4 10 HEEA0013591 1 19980326 A 7930 6607190A WARNING SYS BOLKMS 105 BO105S 5626006 EU OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J S826 OIL PRESS WARN WOULD NOT ILLUMINATE "T" OIL LIGHT. 1 G 7 2 3U H3EU 1998041000681 19980410 00681 1998 4 10 HEEA0013592 4 19980326 A 3416 214175278101 ALTIMETER BELL 412 412 1182202 SW COCKPIT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 WHEN ADJUSTING KNOB, ENCODER GIVES ERRATIC READING. TIME SINCE REPAIR 240:10. 1 G 7 2 4U H4SW 1998041000682 19980410 00682 EU 1998 4 10 HEEA0013593 1 19980326 A 7714 DL40438 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 TRIPLE TACH NR 1 NEEDLE DOES NOT WORK. 1 G 7 2 3U H3EU 1998041000683 19980410 00683 EU 1998 4 10 HEEA0013594 1 19980326 A 7714 DL43638 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 S827 TRIPLE TACH HAS NO INDICATION. 1 G 7 2 3U H3EU 1998041000684 19980410 00684 EU 1998 4 10 HEEA0013595 1 19980326 A 7714 DL43638 INDICATOR BOLKMS 105 BO105S 5626006 EU TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB S751 NR2 NEEDLE DOESN'T MOVE WHEN POWER IS APPLIED. 1 G 7 2 3U H3EU 1998041000685 19980410 00685 SW 1998 4 10 HEEA0013596 1 19980326 A 7714 212070108007 INDICATOR BELL 212 212 1181420 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 NR 2 NEEDLE READING HIGH. 1 G 7 1 4U H4SW 1998041000686 19980410 00686 SW 1998 4 10 HEEA0013597 1 19980326 A 2422 PS2701 INVERTER BELL 212 212 1181420 SW AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 INVERTER INOPERATIVE. 1 G 7 1 4U H4SW 1998041000687 19980410 00687 EU 1998 4 10 HEEA0013598 1 19980326 A 6320 7631955115 OIL PUMP BOLKMS 105 BO105S 5626006 EU M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 5310 S737 OIL PUMP OUTER LINER BREAKING DOWN. 1 G 7 2 3U H3EU 1998041000688 19980410 00688 NE 1998 4 10 HEEA0013599 1 19980326 A 2612 473205 DETECTOR SKRSKY S76 S76A 8143006 NE FIRE DET SYS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5426U 760167 FLAME DETECTOR WOULD NOT TEST CORRECTLY. 1 G 7 2 3U H1NE 1998041000689 19980410 00689 EU 1998 4 10 HEEA0013600 1 19980326 A 3340 A413AHDADF28V POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 ANTI COLLISION LIGHT INOPERATIVE. 1 G 7 2 3U H3EU 1998041000690 19980410 00690 1998 4 10 HEEA0013601 4 19980326 A 3451 6221233001 RECEIVER DME40 BEECH 200 200CBEECH 1152926 CE DME FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 500PH BL29 DME WILL NOT RECEIVE ON 110 FREQUENCIES. 1 L 7 2 4T A24CE 1998041000691 19980410 00691 NE 1998 4 10 HEEA0013602 1 19980326 A 7600 7690001880106 AMPLIFIER SKRSKY S76 S76A 8143006 NE DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE 760275 DROOP COMPENSATOR AMPLIFIER CAUSES INTERMITTENT OSCILLATION ENGINE. 1 G 7 2 3U H1NE 1998041000692 19980410 00692 1998 4 10 HEEA0013603 4 19980326 A 3414 8000 AIRSPEED IND BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2764F 45279 EXCESSIVE LEAKAGE AND INDICATOR OUT OF TOLERANCE. 1 G 7 1 3U H2SW 1998041000693 19980410 00693 1998 4 10 HEEA0013604 4 19980326 A 3422 2891ESR GYRO BELL 206 206L1 1182107 SW COCKPIT DG PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5017G 45228 DIR GYRO PRECESSES EXCESSIVELY. 1 G 7 1 3U H2SW 1998041000694 19980410 00694 SW 1998 4 10 HEEA0013605 1 19980326 A 2436 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 GENERATOR KICKS OFF. 1 G 7 2 4U H4SW 1998041000695 19980410 00695 SW 1998 4 10 HEEA0013606 1 19980326 A 2437 209070263003 INDICATOR BELL 412 412 1182202 SW DUAL VOLTS STICKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 INDICATOR HANDS STICKING AND OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998041000696 19980410 00696 1998 4 10 HEEA0013607 4 19980326 A 2210 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 ROLL CHANNEL SWEEPS LEFT AND RIGHT ON SYSTEM 1 AND 2. 1 G 7 2 4U H4SW 1998041000697 19980410 00697 SW 1998 4 10 HEEA0013608 1 19980326 A 2841 412375001105 INDICATOR BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 NR2 SIDE DROPS TO ZERO. 1 G 7 2 4U H4SW 1998041000698 19980410 00698 NE 1998 4 10 HEEA0013609 1 19980326 A 2611 30326E7 AMPLIFIER SKRSKY S76 S76A 8143006 NE SMOKE DET FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31217 760229 SMOKE DETECTOR WOULD NOT TEST. 1 G 7 2 3U H1NE 1998041000699 19980410 00699 SW 1998 4 10 HEEA0013610 1 19980326 A 2425 209070263003 INDICATOR BELL 412 412 1182202 SW DUAL VOLT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 HL923 33150 A/C VOLT NEEDLE DOES NOT MOVE WITH POWER APPLIED. 1 G 7 2 4U H4SW 1998041000700 19980410 00700 SW 1998 4 10 HEEA0013611 1 19980326 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 NR1 NEEDLE LAGS AND NR2 ROTOR NEEDLE READS HIGH. 1 G 7 2 4U H4SW 1998041000702 19980410 00702 SW 1998 4 10 HEEA0013615 1 19980326 A 7100 4068T96P01 PRESSURE SWITCH BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 5748M 28102 PRESSURE SWITCH CAUSES LIGHT TO STAY ON. 2 G 7 2 4U H10SW 1998041000703 19980410 00703 EU 1998 4 10 HEEA0013616 1 19980326 A 7714 645500051 TRANSMITTER SNIAS 350 AS350B 8680801 EU NG TACH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 2653 TACH TRANSMITTER CAUSES FLUCTUATING NG INDICATOR. 1 G 7 1 3U H9EU 1998041000704 19980410 00704 NE 1998 4 10 HEEA0013617 2 19980326 A 7313 4046T78P05 NOZZLE BELL 214 214ST 1182106 SW GE CT7TS CT72A 30030 NE ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 NOZZLE LEAKING AND WORN. ENGINE SLOW TO START. 2 G 7 2 4U 4 U H10SW E8NE 1998041000705 19980410 00705 EU 1998 4 10 HEEA0013618 1 19980326 A 2610 0301037070 HARNESS SNIAS 350 AS350B2 8680813 EU FIRE DET DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 2862 PROBE RETAINING NUT NOT SECURED. 1 G 7 1 3U H9EU 1998041000706 19980410 00706 1998 4 10 HEEA0013619 4 19980326 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 21498 4469 36003 CVR WON'T TEST. 1 G 7 2 4U H4SW 1998041000707 19980410 00707 1998 4 10 HEEA0013620 4 19980326 A 2562 DK100 BEACON BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 1330 36003 REMOVED WITH CVR S/N 379 DUE TO WON'T TEST. 1 G 7 2 4U H4SW 1998041000708 19980410 00708 1998 4 10 HEEA0013621 4 19980326 A 2370 9806019001 CVR BEECH 200 200CBEECH 1152926 CE COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 500PH 4512 BL29 CVR WILL NOT TEST IN AIRCRAFT. 1 L 7 2 4T A24CE 1998041000709 19980410 00709 1998 4 10 HEEA0013622 4 19980326 A 2562 DK100 BEACON BEECH 200 200CBEECH 1152926 CE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 500PH 833 BL29 REMOVED WITH CVR S/N 288 FOR WILL NOT TEST IN AIRCRAFT. 1 L 7 2 4T A24CE 1998041000710 19980410 00710 SW 1998 4 10 HEEA0013623 1 19980326 A 2422 ASH4501 INVERTER BELL 412 412 1182202 SW AC SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 INVERTER CAUSES FULL GAUGE TO FLUCTUATE. 1 G 7 2 4U H4SW 1998041000711 19980410 00711 SW 1998 4 10 HEEA0013624 1 19980326 A 7714 206075681117 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 210PH 51541 NOT INDICATING PROPERLY BELOW 30%, BOTH NEEDLES. 1 G 7 1 3U H2SW 1998041000712 19980410 00712 SW 1998 4 10 HEEA0013625 1 19980326 A 6720 7001484 YAW CONTROL BELL 412 412 1182202 SW AUTO FLIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 YAW CONTROL INOPERATIVE. 1 G 7 2 4U H4SW 1998041000713 19980410 00713 1998 4 10 HEEA0013626 4 19980326 A 3424 9551 INDICATOR BEECH 200 200BEECH 1152920 CE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 789DS BB478 TURN & SLIP INDICATOR MAKING EXCESSIVE NOISE. 1 L 7 2 4T A24CE 1998041000714 19980410 00714 NE 1998 4 10 HEEA0013627 2 19980326 A 7200 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE POWER SECT FAILED E HEEA K NONE R PARTIAL RPM/PWR LOSS LD LANDING 1 SW 03 5759N 11978 33002 N2 POWER SECTION DROPPED OFF LINE UPON LANDING, CANNOT ROTATE N2; N1 TURNS FREELY. 1 G 7 2 4U 4 U H4SW E22EA 1998041000715 19980410 00715 SW 1998 4 10 HEEA0013628 1 19980326 A 6240 206075681105 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6610Y 51419 DUAL TACH ROTOR NEEDLE INOPERATIVE. 1 G 7 1 3U H2SW 1998041000716 19980410 00716 SW 1998 4 10 HEEA0013630 1 19980326 A 6220 204010937009 DAMPER ASSY BELL 212 212 1181420 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1082G 31109 DAMPER ASSY SIGHT GLASS CLOUDY AND LEAKING. SERIAL NUMBERS REMOVED ARE A1187 AND R19-11869. 1 G 7 1 4U H4SW 1998041000717 19980410 00717 SW 1998 4 10 HEEA0013631 1 19980326 A 7714 206075681105 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH MIS MARKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205FC 51130 DUAL TACH HAS WRONG RANGE MARKINGS. NEEDS YELLOW BAND FROM 100% TO 103%. 1 G 7 1 3U H2SW 1998041000718 19980410 00718 EU 1998 4 10 HEEA0013632 1 19980326 A 7714 DL41239 INDICATOR BOLKMS 105 BO105S 5626006 EU SINGLE RPM STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 137AE S851 RPM INDICATOR NEEDLE HAS STICKY OPERATION. 1 G 7 2 3U H3EU 1998041000719 19980410 00719 EU 1998 4 10 HEEA0013633 1 19980326 A 7714 DL41239 INDICATOR BOLKMS 105 BO105S 5626006 EU SINGLE RPM STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205UC S668 RPM INDICATOR NEEDLE HAS STICKY OPERATION. 1 G 7 2 3U H3EU 1998041000720 19980410 00720 1998 4 10 HEEA0013634 4 19980326 A 3425 1113025 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 HSI CDI NEEDLE STICKS. 1 G 7 2 3U H1NE 1998041000721 19980410 00721 1998 4 10 HEEA0013635 4 19980326 A 3425 1113025 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 HSI FLAG DOESN'T PULL (STICKS) 1 G 7 2 3U H1NE 1998041000722 19980410 00722 1998 4 10 HEEA0013636 4 19980326 A 3421 1113034 INDICATOR BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 ATTITUDE INDICATOR LEFT KNOB WILL NOT ADJUST. 1 G 7 1 4U H4SW 1998041000723 19980410 00723 1998 4 10 HEEA0013637 4 19980326 A 2210 7000299901 CONTROL BELL 412 412 1182202 SW AUTOPILOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 NR2 AP TRIPS ON LINE. 1 G 7 2 4U H4SW 1998041000724 19980410 00724 1998 4 10 HEEA0013638 4 19980326 A 3421 1113034 INDICATOR BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 ATTITUDE INDICATOR INOPERATIVE. 2 G 7 2 4U H10SW 1998041000725 19980410 00725 1998 4 10 HEEA0013639 4 19980326 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21498 36003 HSI CDI NEEDLE DEFLECTS FULL SCALE WHILE ON COURSE. 1 G 7 2 4U H4SW 1998041000726 19980410 00726 1998 4 10 HEEA0013640 4 19980326 A 2210 412001304101 SERVO ASSY BELL 412 412 1182202 SW AUTO FLIGHT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 HP NR2 INOPERATIVE SIDE, HP NR1 GOOD SIDE. 1 G 7 2 4U H4SW 1998041000727 19980410 00727 SW 1998 4 10 HEEA0013641 1 19980326 A 6240 214074280103 DETECTOR BELL 412 412 1182202 SW RPM LIMIT FAILED E HEEA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 03 108X 33115 RPM WARNING LIGHT AND CYCLIC CENTERING LIGHT FLASH OFF AND ON IN FLIGHT. 1 G 7 2 4U H4SW 1998041000728 19980410 00728 SW 1998 4 10 HEEA0013642 1 19980326 A 6240 206076373001 TACH GEN BELL 206 206L3 1182108 SW ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 32041 51539 TRIPS LOW ROTOR WARNING HORN AFTER MUTED. 1 G 7 1 3U H2SW 1998041000729 19980410 00729 EU 1998 4 10 HEEA0013643 1 19980326 A 7930 6607190A WARN SYS BOLKMS 105 BO105S 5626006 EU OIL PRESS FAILED E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 50293 S677 T-OIL LIGHT WILL NOT GO OUT. 1 G 7 2 3U H3EU 1998041000730 19980410 00730 1998 4 10 HEEA0013644 4 19980326 A 3424 206070274005 INDICATOR BELL 206 206L1 1182107 SW COCKPIT T&B FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2133X 45634 NEEDLE ON INDICATOR INOPERATIVE. MAKING NOISE. 1 G 7 1 3U H2SW 1998041000731 19980410 00731 1998 4 10 HEEA0013645 4 19980326 A 3424 TS4001AL INDICATOR BOLKMS 117 BK117B2 5626013 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 7234 TURN AND SLIP NEEDLE WOULD NOT OPERATE. 1 G 7 2 3U NC H13EU 1998041000732 19980410 00732 EU 1998 4 10 HEEA0013646 1 19980326 A 7722 TM42739 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 9190Y S669 EXH TEMP INDICATOR NON LINEAR THROUGHOUT SCALE. 1 G 7 2 3U H3EU 1998041000734 19980410 00734 SW 1998 4 10 HEEA0013648 1 19980326 A 2820 2C271 CARTRIDGE BELL 206 206L1 1182107 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5000K 45167 FUEL CARTRIDGE INOPERATIVE. 1 G 7 1 3U H2SW 1998041000735 19980410 00735 EU 1998 4 10 HEEA0013649 1 19980326 A 3610 97914211 VALVE BOLKMS 105 BO105S 5626006 EU BLEED SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 VALVE INOPERATIVE, PIECES BROKEN ON INSIDE. 1 G 7 2 3U H3EU 1998041000736 19980410 00736 EU 1998 4 10 HEEA0013651 1 19980326 A 3610 97914211 VALVE BOLKMS 105 BO105S 5626006 EU BLEED SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 VALVE FAILED. PIECES BROKEN INSIDE. 1 G 7 2 3U H3EU 1998041000737 19980410 00737 NE 1998 4 10 HEEA0013652 1 19980326 A 6220 7640002900102 DAMPER SKRSKY S76 S76A 8143006 NE M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1545X 760050 VISCIOUS DAMPER LEAKING AND WEAK. 1 G 7 2 3U H1NE 1998041000738 19980410 00738 1998 4 10 HEEA0013653 4 19980326 A 3421 7660002113103 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 VERT GYRO INOPERATIVE. 1 G 7 2 3U H1NE 1998041000739 19980410 00739 1998 4 10 HEEA0013654 4 19980326 A 3442 MI5851345V INDICATOR P40 SKRSKY S76 S76A 8143006 NE RADAR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 INDICATOR WILL NOT SHOW A PICTURE IN ANY MODE AFTER WARM UP. ANTENNA WILL NOT SWEEP. TRIED SAME INDICATOR IN N1545X AN D HAD SAME PROBLEM. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT CAUSING ANTENNA NOT TO SCAN. SWAPPED BOARDS. FOUND LO GIC #2 BOARD BAD. TROUBLESHOT BOARD. FOUND BAD PULSES AT SEVERAL IC'S. REPLACED U1301,U1325,U1363,U1337,U1347,U1345,U 1341,U1343. NO HELP.TROUBLESHOT FURTHER. FOUND PIN 8 OF U1366 BEING LOADED DOWN. REPLACED U1366. REPAIRED. BENCH CH ECK GOOD. 1 G 7 2 3U H1NE 1998041000740 19980410 00740 NE 1998 4 10 HEEA0013655 1 19980326 A 6410 7610105101042 BLADE SKRSKY S76 S76A 8143006 NE T/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 4082 760181 TIP WEIGHT POCKET COVER IS UNBONDED ON PADDLE "A". 1 G 7 2 3U H1NE 1998041000741 19980410 00741 NE 1998 4 10 HEEA0013656 1 19980326 A 6210 7615009043050 TIP CAP SKRSKY S76 S76A 8143006 NE M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 BOTH INTERNAL DOUBLERS HAVE RIVETS INSTALLED. 1 G 7 2 3U H1NE 1998041000742 19980410 00742 SW 1998 4 10 HEEA0013657 1 19980326 A 6220 204011121009 GRIP 204012101153 BELL 212 212 1181420 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 13748 ADA53562 30899 POSSIBLE REPAIR PITCH HORN MOUNT BORE, AND REPLACEMENT OF THE BLADE BOLT BUSHINGS, DRAG BRACE BUSHINGS AND BEARING LINER S. 1 G 7 1 4U H4SW 1998041000743 19980410 00743 1998 4 10 HEEA0013658 4 19980326 A 2200 214074301105 AMPLIFIER BELL 214 214ST 1182106 SW SCAS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 SCAS SYSTEM WILL NOT MONITOR TEST PROPERLY. (STOPS AT PITCH FUNCTION) ALSO, PITCH CHANNEL WON'T STAY ENGAGED. 2 G 7 2 4U H10SW 1998041000744 19980410 00744 1998 4 10 HEEA0013659 4 19980326 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 133AE S800 KNOBS DON'T CHANGE ANYTHING. PERFORMED PRELIMINARY INSPECTION. ALSO FOUND ENT BUTTON UNREADABLE. 1 G 7 2 3U H3EU 1998041000745 19980410 00745 1998 4 10 HEEA0013660 4 19980326 A 2312 064101902 TRANSCEIVER KY196 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007N 45184 RECEIVES BUT WILL NOT TRANSMIT 118 MHZ RANGE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT TRANSMITTING ON CORRECT FREQUENCY FROM 118MHZ TO 129MHZ. REPLACED TRANSISTORS Q307 AND Q308 IN VCO SECTION. REPAIRED PROBLEM. FOUND UNIT TO H AVE VERY WEAK RECEIVE. ADJUSTED VCO AND ALIGNEDRECEIVER SEVERAL TIMES. NO HELP. 1 G 7 1 3U H2SW 1998041000746 19980410 00746 1998 4 10 HEEA0013661 4 19980326 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 51134 INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT NOT RECEIVING. REPLACED V101 CAVITY TUBE. REPAIRED, BUT FOU ND UNIT OFF FREQUENCY. ADJUSTED V101 CAVITY TUBE, NO HELP. REPLACED V101 AGAIN, NO HELP. SWAPPED OUT HALVES OF UNIT, FOUND PROBLEM ON PRESELECTOR SIDE. 1 G 7 1 3U H2SW 1998041000747 19980410 00747 1998 4 10 HEEA0013662 4 19980326 A 2312 064105430 TRANSCEIVER BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2277A 3630 NO POWER INDICATED. SMELLED BURNT. PERFORMED PRELIMINARY INSPECTION. FOUND OPEN FUSE, SHORTED TRANSISTOR Q507 AND BURN SPOT ON DISPLAY BOARD. 1 G 7 1 3U H2SW 1998041000748 19980410 00748 1998 4 10 HEEA0013663 4 19980326 A 3444 066106103 ALTIMETER BOLKMS 105 BO105S 5626006 EU RADAR ALT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4294R S860 LOW POWER OUT, BELOW SPECS. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT OUT OF SPECS. ALIGNED UNIT TO SPECS, WHILE TE STING UNIT, FOUND POWER OUT WEAK (23MW). TROUBLESHOT UNIT AND CHECKED VOLTAGE ON OSCILLATOR CURRENT REGULATOR BOARD. V OLTAGE CHECKS GOOD. CONTINUEDTROUBLESHOOTING AND FOUND STRIPLINE CAUSING PROBLEM. 1 G 7 2 3U H3EU 1998041000749 19980410 00749 1998 4 10 HEEA0013664 4 19980326 A 3457 13824120234 RECEIVER BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5014Y 45219 COCKPIT GPS RECEIVER NO POWER. FOUND UNIT DOES NOT HAVE A DISPLAY. 1 G 7 1 3U H2SW 1998041000750 19980410 00750 1998 4 10 HEEA0013665 4 19980326 A 3416 212070238007 INDICATOR BELL 412 412 1182202 SW COCKPIT ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 INDICATES 1500 FEET OFF. READJUSTED TO ZERO. BENCH CHECK GOOD. 1 G 7 2 4U H4SW 1998041000751 19980410 00751 GL 1998 4 10 HEEA0013668 2 19980330 A 7250 23008054 NOZZLE VANE 23033185 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL NR 1 CRACKED E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 2124Z CAT70467 45646 CAE860564 ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF TURBINE PARTS NOTED: NR 1 NOZZLE VANE CRACKED AND BURNT BEYOND SERV ICEABLE LIMITS. 1 G 7 1 3U 3 U H2SW E1GL 1998041000752 19980410 00752 1998 4 10 HEEA0013669 4 19980330 A 3457 0845000000 GPS SKYNAV5000 BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27805 230 31106 WILL NOT ACCEPT PRESENT POSITION. PERFORMED PRELIMINARY INSPECITON. FOUND UNIT INTERMITTENTLY DOES NOT POWER UP AND ALS O INTERMITTENTLY LOSES PRESENT POSITION AND USER WAYPOINTS AFTER SHUTDOWN. 1 G 7 1 4U H4SW 1998041000753 19980410 00753 SW 1998 4 10 HEEA0013670 1 19980331 A 5321 2H6031313115 FLOOR PANEL BELL 206 206B3 1181506 SW RT OUTBOARD MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 FLOOR PANEL EDGE DISTANCE TOO SHORT RIGHT HAND OUTBOARD SIDE. 1 G 7 1 3U H2SW 1998041000754 19980410 00754 1998 4 10 HEEA0013671 4 19980331 A 3425 1113025 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT HSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 COURSE SET NEEDLE ROTATES BY ITSELF. 1 G 7 2 3U H1NE 1998041000755 19980410 00755 SW 1998 4 10 HEEA0013672 1 19980331 A 2842 206063656001 TRANSMITTER BELL 206 206L1 1182107 SW FUEL QTY FAILED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 50034 45169 RECEIVED FOR TROUBLESHOOTING FUEL QUANTITY PROBLEMS. PROBE DID NOT WORK AT ALL. (NO OUTPUT) 1 G 7 1 3U H2SW 1998041000756 19980410 00756 SW 1998 4 10 HEEA0013673 1 19980401 A 6420 214011819101 BEARING 214011801117 BELL 214 214ST 1182106 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 1281 A387 28102 4 EACH BLADE FEATHER BEARINGS WORN BEYOND LIMITS. 2 G 7 2 4U H10SW 1998041000757 19980410 00757 SW 1998 4 10 HEEA0013674 1 19980401 A 6510 406040339105 BEARING 406040320101 BELL 407 407 SW UNKNOWN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 510PH AFS972 53209 ROUGH BEARINGS. SERIAL NUMBERS REMOVED ARE K96-2176 AND K96-2157. 1 G 7 1 3U O H2SW 1998041000758 19980410 00758 NM 1998 4 10 AALA980444 1 19980306 A 3350 STRIP BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 616AA 24524 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY FLOOR PATH LIGHT WOULD NOT ILLUMINATE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998041000759 19980410 00759 NM 1998 4 10 98ZZZX1419 1 19980306 A 4950 SEAL BOEING 757 75723N 1384973 NM APU FAILED A AMTA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 514AT 27971 AT FL 410, CABIN BEGAN TO FILL WITH WHAT APPEARED TO BE (AIR CONDITIONING) AC SMOKE. CREW FOLLOWED AOM SMOKE CLEARING A ND AC SMOKE PROCEDURES. AIRCRAFT DIVERTED TO MCO. THE APU'S OIL/AIR SEALS WERE FAILING AFTER RUN-UP. APU WAS DEFERRED PER MEL. (APU WOULD REQUIRE REPLACING). 2 L 7 2 4F RT A2NM 1998041000760 19980410 00760 NM 1998 4 10 ASAA9840028 1 19980209 A 5610 ROLLER BOEING 737 7374Q8 NM LT COCKPIT LOOSE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 785AS 27628 SEA - FLT 84 - PRIOR TO FLIGHT, THE CAPTAIN'S SLIDING WINDOW COULD NOT BE CLOSED. SECURED LOOSE ROLLER AT BOTTOM AFT SI DE OF WINDOW AND WINDOW OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1998041000762 19980410 00762 EU 1998 4 10 C2XA98IA015 1 19980208 A 2424 243230 GCU AEROSP ATR42 ATR42500 EU NR 1 SMOKING A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 17448 506 IAH - FLT 3969 - PILOT REPORTED THAT SMOKE WAS NOTED FROM THE 90VU RACK FOLLOWED BY THE LOSS OF THE NR 1 ACW GENERATOR. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ACW GENERATOR CONTROL UNIT. T HE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998041000763 19980410 00763 EU 1998 4 10 98ZZZX1420 1 19980221 A 2752 791A000007 ACTUATOR LUCAS AIRBUS 320 A320231 3930325 EU TE FLAPS BINDING A P9RA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 EITLJ 16262 L585 257 FLAP SYSTEM FAULT - ON INBOUND TRIP TO ZIH FROM DTW RECYCLED FLAPS ACCORDING TO ECAM PROCEDURE. EXECUTED NO FLAPS LANDI NG. RESET WING TIP BRAKES, SLATS AND FLAPS. CHECKED SYSTEM, OPERATION OK. FLAP AND SLATS EXTENDED AND RETRACTED NORMA LLY. (FLAP ROTARY ACTUATOR CHANGED . OTW FOUND TORQUE LIMITER POPPED). 2 L 7 2 4F RT A28NM 1998041000764 19980410 00764 EA 1998 4 10 MASA98051 1 19980308 A 3350 GE1317 BULB BRUCE BM10006002 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27185 7185 WHILE PERFORMING ROUTINE MAINTENANCE INSPECTION, FOUND RT TOP CENTER EXTERNAL EMERGENCY LIGHT INOPERABLE. MAINTENANCE R EMOVED AND REPLACED BULB. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A21EA 1998041000765 19980410 00765 EA 1998 4 10 MASA98048 1 19980305 A 5210 601R386461 HANDLE 601R319003 CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF ADJUST A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 17217 7217 CLT/TLH - FLT 5789 - BEFORE DEPARTURE TO TLH, CREW REPORTED THE PASSENGER DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MA INTENANCE TROUBLESHOT AND ADJUSTED THE INTERNAL HANDLE ROLLER. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. ACFT TT H RS: 301. ACFT TT CYCLES: 215. (X) 2 L 7 2 4F RT A21EA 1998041000766 19980410 00766 CE 1998 4 10 MASA98046 1 19980303 A 5270 MS250081 SWITCH BEECH 1900 1900D 1154162 CE PAX DOOR OUT OF ADJUST A MASA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 190YV UE190 FLT 5989 - MBS-PIT - EN ROUTE FROM SAGINAW TO PIT, PILOT REPORTED THE PAX DOOR ANNUNC ILLUMINATED. CREW DECLARED AN EME RGENCY AND DIVERTED TO DTW. THE DOOR WAS INSPECTED TO INSURE THAT IT WAS PROPERLY CLOSED AND LOCKED. MAINTENANCE ACTIO N WAS DEFERRED ON THE ANNUNC PER MEL 52-01. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE DOOR AJAR SWITCH WAS ADJUSTED AS NEEDED, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1998041000767 19980410 00767 EU 1998 4 10 VTZA98057 1 19980130 A 3040 327310 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU RT WINDSHIELD MISWIRED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 496UE 900 IAD/ALB - FLT 6258 - DURING CRUISE AT 1837 HOURS ON 1-30-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FO'S WINDSCREEN HEAT WENT TO WARM-UP AFTER TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SWA PPED LEADS TO ALTERNATE HEAT SENSOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998041000768 19980410 00768 EU 1998 4 10 SIMA980521 1 19980221 A 3260 MS3476W1419AX CONNECTOR SAAB SF340 340B 7860101 EU LT MLG LOOSE A SIMA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 21 387AE 340B387 ACT - FLT 3549 - NOSE GEAR AND LEFT MAIN GEAR DOWNLOCK INDICATION INOPERABLE. AIRCRAFT RETURNED TO DFW AND LANDED SAFEL Y. FOUND CANNON PLUG 5GPI IN LEFT WHEEL WELL NOT LOCKED. REMOVED, CLEANED, AND LOCKED CANNON PLUG SYSTEM. OPS CHECK G OOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998041000770 19980410 00770 SO 1998 4 10 C2XA98CL012 1 19980212 A 3010 M832481226 O-RING EMB 145 EMB145 SO VERTICAL STAB WORN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15941 145035 CLE - FLT 4043 - CREW REPORTED WHILE CLIMBING THROUGH 5,000 FEET WITH ANTI-ICE ON, THEY RECEIVED A LEFT HAND ENGINE BLEE D LEAK ON EICAS AND A RED LEAK MESSAGE IN BLEED SWITCH ON OVERHEAD PANEL. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER IN CIDENT. MAINTENANCE REMOVED AND REPLACED AN O-RING IN THE VERTICAL STAB DEICE DUCT COUPLING IAW EMB-145 MM 30-12-07, OP ERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. ACFT TT: 406.6 HOURS. TOTAL CYCLES: 294 . (X) 2 L 7 2 4F RT T00011AT 1998041000771 19980410 00771 EA 1998 4 10 JBXA980032 1 19980203 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY MALFUNCTIONED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 571ML 7209 PHL - FLT 754 - AFTER TAKEOFF, EICAS INDICATED LAVATORY SMOKE. RETURNED TO BASE, PHL. INSPECTED LAVATORY TRASH CONTAIN ER AND FIRE BOTTLE, ALL NORMAL. ALL VISIBLE WIRING AND ELEC CONNECTORS ALL NORMAL. CHECKED AFT CARGO AND APU COMPTS, A LL NORMAL. RAN APU, AIR COND, ENGS, ALL NORMAL. EICAS AND SMOKE DETECTOR SYSTEM OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A21EA 1998041000772 19980410 00772 NM 1998 4 10 UIEA9801 1 19980128 A 2120 AIR DISTRIBUTION BOEING 747 7472D7B 1384803 NM COCKPIT ODOR A UIEA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 522MC 21783 FRA/SHJ - FLT TG891 - AFTER TOP OF DESCENT, A STRONG ELECTRICAL SMELL WAS NOTED. FLIGHT DECK FAN WAS ON AT THE TIME FOR APPROX 10 MINUTES. FAN SWITCHED OFF. P6 CIRCUIT BREAKER PANEL (FRONT, BACK, AND UNDER F/E TABLE) WERE CHECKED FOR SMO KE AND ODORS. THE SMELL SEEMED PREDOMINANTLY TO COME FROM F/O SIDE, MORE FROM TOP OF HIS GLARESHIELD THAN UNDER. SMELL DISSIPATED APPROX 5 MINUTES AFTER TURNING FLT DECK FAN OFF. FAN RAN ON GROUND FOR APPROX 10 MINUTES WITH NO RECURRENCE . (X) 2 L 7 4 4F RT A20WE 1998041000773 19980410 00773 WP 1998 4 10 TWAA9803305 1 19980205 A 5753 SKIN DOUG DC9 DC982 3022082 WP LT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 924TW 49100 MCI - DURING MAINTENANCE CHECK, THE LEFT WING OTBD FLAP SECTION 65 INCHES TO 76 INCHES, INBD OF THE OTBD END, ON THE TRA ILING EDGE, WAS FOUND DELAMINATED. ACCOMPLISHED FIBERGLASS LAY-UP REPAIR PER SRM 51-70-1A FIG 49 PAGE 112. (X) 2 L 7 2 4F A6WE 1998041000774 19980410 00774 EU 1998 4 10 VTZA98105 1 19980303 A 2435 23095002D STARTER GEN JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 27 333UE 41101 IAD/PWM - FLT 6578 - DURING CRUISE AT 1930 HRS ON 3-3-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO LT GENERATO R WENT OFF-LINE SEVERAL TIMES. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND LOO SE LEAD ON STARTER GENERATOR, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998041000776 19980410 00776 EA 1998 4 10 VTZA98056 1 19980214 A 2750 601R93106101 DRIVE SHAFT CNDAIR CL600 CL6002B19 EA TE FLAPS LACK OF LUBE A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 622BR 7187 BNA/IAD - FLT 6701 - DURING APPROACH AT 1120 HRS ON 2-14-98, AIRCRAFT MADE A SCHEDULED LANDING AT IAD WITH ONE DISCREPAN CY WHICH WAS FLAPS FAILED MESSAGE ON EICAS. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBED FLAP DRIVE SHAFT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998041000777 19980410 00777 EA 1998 4 10 VTZA980054 1 19980212 A 2750 601R930503 FECU CNDAIR CL600 CL6002B19 EA FLAPS FALSE READING A VTZA K NONE F FLT CONT AFFECTED AP APPROACH 1 EA 27 622BR 7187 IAD/ATL - FLT 6715 - DURING APPROACH AT 0930 HRS ON 2-12-98, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHIC H WAS FLAPS STUCK AT ZERO DEGREES. EICAS MESSAGE READ FLAPS FAILED. MAINTENANCE INSPECTED RESET FLAP CIRCUIT BREAKER. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998041000778 19980410 00778 EA 1998 4 10 VTZA98037 1 19980131 A 2750 865D1007 PDU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILURE A VTZA O OTHER J WARNING INDICATION DE DESCENT 1 EA 27 622BR 7187 RSW/IAD - FLT 6676 - DURING DESCENT AT 0915 HRS ON 1-31-98, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS THE FLAPS FAILED, EICAS CAUTION MESSAGE ZERO POSITION. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANC E INSPECTED AND REMOVED AND REPLACED FLAP PDU, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998041000779 19980410 00779 EA 1998 4 10 VTZA98095 1 19980220 A 2750 601R93106101 DRIVE SHAFT CNDAIR CL600 CL6002B19 EA TE FLAPS CORROSION A VTZA K NONE J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 EA 27 622BR 7187 BNA/IAD - FLT 6705 - DURING APPROACH AT 2055 HRS ON 2-20-98, AIRCRAFT EXPERIENCED A FLAP FAIL FAULT WARNING. AIRCRAFT L ANDED AT IAD WITH ZERO FLAPS AFTER DECLARING AN EMERGENCY. MAINTENANCE CONTROL NOTIFIED AND MAINTENANCE DISPATCHED TO A CFT. AIRCRAFT TOWED TO THE MAINTENANCE HANGAR WHERE IT IS STILL UNDERGOING TROUBLESHOOTING BY BOTH ACA MAINTENANCE TECH NICIANS AND BOMBARDIER TECHNICAL REPS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BOTH FLAP ACTUATORS AND FLAP DRIV E SHAFTS. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: OPERATOR CONTROL NR 98ZZZX1422. (X) 2 L 7 2 4F RT A21EA 1998041000780 19980410 00780 EA 1998 4 10 98ZZZX1422 1 19980220 A 2752 854D10011 ACTUATORS CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A VTZA K NONE J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 EA 27 622BR 7187 BNA/IAD - FLT 6705 - DURING APPROACH AT 2055 HRS ON 2-20-98, AIRCRAFT EXPERIENCED A FLAP FAIL FAULT WARNING. AIRCRAFT L ANDED AT IAD WITH ZERO FLAPS AFTER DECLARING AN EMERGENCY. MAINTENANCE CONTROL NOTIFIED AND MAINTENANCE DISPATCHED TO A CFT. AIRCRAFT TOWED TO THE MAINTENANCE HANGAR WHERE IT IS STILL UNDERGOING TROUBLESHOOTING BY BOTH ACA MAINTENANCE TECH NICIANS AND BOMBARDIER TECHNICAL REPS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BOTH FLAP ACTUATORS AND FLAP DRIV E SHAFTS. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: OPERATOR CONTROL VTZA98095. (X) 2 L 7 2 4F RT A21EA 1998041000781 19980410 00781 EU 1998 4 10 VTZA98042 1 19980202 A 7712 TORQUE GAUGE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 497UE 904 IAD/ROA - FLT 6591 - DURING TAXI AT 1645 HOURS ON 2-2-98, AIRCRAFT RETURNED TO GATE DUE TO LT TORQUE GAUGE FAILED. MAIN TENANCE INSPECTED AND SWITCHED TO NR 2 BRIDGE ON THE LT TORQUE SIGNAL CONDITIONER. AIRCRAFT GROUND RUN, OPS CHECK OK. A IRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998041000782 19980410 00782 EU 1998 4 10 VTZA98096 1 19980226 A 7712 1246432 TORQUE GAUGE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 497UE 904 IAD/MKT - FLT 6570 - DURING TAKEOFF AT 1710 HRS ON 2-26-98, AIRCRAFT ABORTED TAKEOFF DUE TO LT TORQUE GAUGE FAILED. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TORQUE GAUGE. AIRCRAFT WAS GROUND RUN, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998041000784 19980410 00784 1998 4 10 98ZZZX1424 4 19980130 A 2564 D30170535 SLIDE/RAFT LKHEED 1011 10113851 5265010 WP L1 DOOR MISMANUFACTURED A WRNA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 05 826CR 193A1141 WHEN ATTEMPTING TO EXECUTE MINI-EVAC DRILL, L-1 DOOR OPENED PARTIALLY AND L-1 SLIDE/RAFT FAILED TO DEPLOY. DRILL CALLED OFF AND L-2 DOOR SLIDE/RAFT REMOVED FOR RE-INSPECTION. L-1 DOOR SLIDE/RAFT REMOVED FOR INSPECTION. FOUND GIRT BAR STR AP TOO SHORT TO ALLOW RELEASE CABLE TO PULL PINS ON COVER. RETURNED TO VENDOR FOR FURTHER EVALUATION AND TEAR DOWN REPO RT. 2 L 7 3 4F A23WE 1998041000785 19980410 00785 WP 1998 4 10 98ZZZX1425 1 19980223 A 3350 516574 POWER PACK LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A WRNA K NONE L NO TEST IN INSP/MAINT 1 SO 05 826CR 193A1141 EMERGENCY EXIT LIGHTS INOPERABLE AT L-3 DOOR. REMOVED AND REPLACED EMERGENCY POWER PACK IAW 33-21-19. OPS CHECK SATISF ACTORY. (X) 2 L 7 3 4F A23WE 1998041000786 19980410 00786 EU 1998 4 10 SABA980018 1 19980310 A 2161 7252C000 TEMP CONTROL BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A SABA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 33 966AE 966 RDU - FLT 5187 - ON FLIGHT FROM RDU/CHS, AIRCREW TURNED ON RT FLOW PACK AND SMOKE AND A BURNING SMELL WAS NOTED. EMERGE NCY PROCEDURES WERE FOLLOWED AND IN-FLIGHT EMERGENCY DECLARED. AIRCRAFT RETURNED TO RDU AND LANDED WITH NO PROBLEMS. M AINTENANCE DEPLOYED FROM CLT/RDU AND FOUND RT AUTOTEMP CONTROLLER BAD, TEMP CONTROLLER DEFERRED TO MSL NR 03059802C. A IRCRAFT WAS RESTRICTED TO LT FLOW PACK ONLY. AIRCRAFT WAS REPOSITIONED TO CLT FOR MAINTENANCE. (X) 2 L 7 2 4T RT A56EU 1998041000789 19980410 00789 SW 1998 4 10 98ZZZX1428 1 19980210 A 6330 214031458102 FITTING 214031810105 BELL 214 214ST 1182106 SW RT LOWER TRANS WORN B ALGR K NONE O OTHER IN INSP/MAINT 1 SW 03 214EV 28117 DURING 100-HOUR INSPECTION, FOUND EXCESSIVE WEAR ON UPPER AND LOWER SIDES OF RESTRAINT AT ATTACHMENT POINT ON TRANSMISSI ON SUPPORT. 2 G 7 2 4U H10SW 1998041000794 19980410 00794 SW 1998 4 10 PNSA980301 1 19980303 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A PNSA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 175SW AC621 NOSE GEAR WOULD NOT EXTEND. EMERGENCY EXTENTION PERFORMED LANDING UNEVENTFUL. LUBED AND ADJUSTED NOSE GEAR, OPS CHECK OK. 2 L 7 2 4T RT A8SW 1998041000795 19980410 00795 SO 1998 4 10 PNSA980302 1 19980316 A 8011 STARTER PIPER PA32 PA32301 7103207 SO ENGINE FAILED A PNSA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 8361Q 11316 328106055 ENGINE WOULD NOT TURN OVER. REPLACED STARTER, OPS CHECKED OK. 1 L 7 1 3O A3SO 1998041000796 19980410 00796 SO 1998 4 10 PNSA980303 1 19980312 A 2434 ALY6421 ALTERNATOR PIPER PA32 PA32301 7103207 SO ENGINE INTERMITTENT A PNSA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 03 82455 328006079 LOW BATTERY, ENGINE WOULD NOT START. REPLACED INTERMITTENT ALTERNATOR, OPS CHECK OK. 1 L 7 1 3O A3SO 1998041000797 19980410 00797 SW 1998 4 10 PNSA980304 1 19980318 A 5230 DOOR SWRNGN SA227 SA227AC 8780603 SW CARGO COMPT NOT LOCKED A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 2719H AC713B CARGO DOOR WARNING LIGHT CAME ON DURING CLIMB. DEPRESSURIZED RETURNED TO ANC, LANDING WAS UNEVENTFUL. FOUND CARGO DOOR HANDLE NOT FULLY IN CLOSED DETENT. DOOR SECURED, NEXT FLIGHT OK. 2 L 7 2 4T RT A8SW 1998041000798 19980410 00798 SO 1998 4 10 PNSA980305 1 19980318 A 3260 SENSORS PIPER PA31 PA31 7103102 SO NLG LACK OF LUBE A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 AL 03 27987 317912054 GEAR WARNING HORN SOUNDED DURING TAKEOFF ROLL. ABORTED TAKEOFF, TAXI BACK TO HANGER UNEVENTFUL. CLEANED AND LUBED NOSE GEAR, OPS CHECK OK. 1 L 7 2 3O A20SO 1998041000799 19980410 00799 SO 1998 4 10 RAAA98E8009 1 19980401 A 3397 WIRE LKHEED 188 188C 5262604 SO BS 390 CHAFED A RAAA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 178RV 188C2010 DURING CLIMBOUT, EMERGENCY EVAC LIGHTS CB TRIPPED. RESET ONCE AND TRIPPED AGAIN AFTER SEVEN MINUTES. RETURNED TO ANC A ND LANDED OVERWEIGHT WITHOUT INCIDENT. FOUND EMERGENCY LIGHT WIRE NR N54Q20 CHAFED AT FS 390. REPAIRED WIRE SYSTEM, OP S CHECK GOOD PER RAA DOC 86-26. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION PER 42-11-09. 2 L 7 4 4T 4A22 1998041000800 19980410 00800 NM 1998 4 10 CALA9800630 1 19980406 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND LOWER CAP OF FLOORBEAM CORRODED AT FS 1070 FROM LBL 39 TO RBL 48. THE LOWER CAP WAS CUT OUT, L-ANGLES, FILLER AND A STRAP WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 8. 2 L 7 3 4F A3WE 1998041000801 19980410 00801 NM 1998 4 10 CALA9800631 1 19980406 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1110-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SEAT TRACK CORRODED FROM STA 1110 TO 1130, LBL 45. A NEW SECTION OF SEAT TRACK WAS FABRICATED AND INST ALLED IAW SRM 53-10-2, 51-10-2 AND MM 51-20-0. 2 L 7 3 4F A3WE 1998041000802 19980410 00802 NM 1998 4 10 CALA9800632 1 19980407 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 970-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SEAT TRACK CORRODED AT FS 970 TO 1130, RBL 24. A SEAT TRACK REPAIR WAS FABRICATED AND INSTALLED IAW SR M 53-10-05, FIGURE 7, 51-10-2 AND MM 51-30-11. 2 L 7 3 4F A3WE 1998041000803 19980410 00803 WP 1998 4 10 CALA9800633 1 19980407 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 486-490 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14831 49491 INSPECTION FOUND LONGERON 30 IN FORWARD CARGO COMPARTMENT CORRODED FROM STA 486 TO 490. A NEW LONGERON WAS FABRICATED A ND INSTALLED IAW SRM 53-02. 2 L 7 2 4F A6WE 1998041000804 19980410 00804 WP 1998 4 10 CALA9800634 1 19980407 A 5210 AIR BOTTLE DOUG DC10 DC1030 3023501 WP L3 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND L-3 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06. 2 L 7 3 4F A22WE 1998041000805 19980410 00805 WP 1998 4 10 CALA9800635 1 19980407 A 5210 AIR BOTTLE DOUG DC10 DC1030 3023501 WP L2 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND L-2 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-12-06. 2 L 7 3 4F A22WE 1998041000806 19980410 00806 WP 1998 4 10 CALA9800636 1 19980407 A 5210 AIR BOTTLE DOUG DC10 DC1030 3023501 WP R1 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND R-1 DOOR AIR BOTTLE PRESSURE LOW. THE AIR BOTTLE WAS FILLED IAW MM 52-11-06. 2 L 7 3 4F A22WE 1998041000807 19980410 00807 NM 1998 4 10 9805942275 1 19980324 A 3260 656021132 ACCESSORY UNIT BOEING 727 727251 138408H NM E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 275US 22376 1972 21154 DURING GEAR RETRACTION, THE NOSE GEAR INDICATION DID NOT MATCH OPERATION OF NOSE GEAR. RECYCLED GEAR WITH SAME RESULTS. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR LOCK SWITCH AND LANDING GEAR ACCESSORY UNIT. PERFORMED GEAR SWING AND OPERATIONAL CHECK. 2 L 7 3 4F A3WE 1998041000808 19980410 00808 NM 1998 4 10 9805956307 1 19980404 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 2AB TO 4AB. REPAIRED WIRING, OPERATIONAL CHE CK GOOD. 2 L 7 4 4F RT A20WE 1998041000809 19980410 00809 WP 1998 4 10 9805969922 1 19980406 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 945N 47664 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000810 19980410 00810 WP 1998 4 10 9805979913 1 19980406 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 963N 47415 DURING PERIODIC CHECK, FOUND RIGHT NACELLE AND RIGHT TAIL CONE EMERGENCY EVACUATION SLIDE LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000811 19980410 00811 1998 4 10 9805989913 4 19980406 A 2565 113317 SLIDE BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 963N 14130 1208 47415 DURING PERIODIC CHECK, FORWARD GALLEY DOOR EVACUATION SLIDE FAILED BATTERY TEST. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998041000812 19980410 00812 NM 1998 4 10 9805995517 1 19980311 A 2910 HYD LINE BOEING 757 757251 1384970 NM LT HYD SYST DAMAGED A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 517US 23205 ON DESCENT, LEFT HYDRAULIC SYSTEM LOST FLUID SUPPLY. ALTERNATE SYSTEMS WERE USED, AIRCRAFT LANDED IN SFO WITHOUT INCIDE NT. MAINTENANCE FOUND THE ENGINE DRIVEN PUMP LINE DAMAGED. THE ENGINE DRIVEN PUMP, LINE AND FILTERS WERE REPLACED. RU N-UP, LEAK CHECK AND FUNCTIONAL TEST WERE SATISFACTORY. 2 L 7 2 4F RT A2NM 1998041000813 19980410 00813 WP 1998 4 10 9806009854 1 19980403 A 2780 DUCT DOUG DC9 DC951 3022051 WP LT LE SLAT INOPERATIVE A NWAA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 01 763NC 47716 DURING DESCENT AND SLAT EXTENSION, THE SLAT EXTEND BLUE INDICATION LIGHT DID NOT ILLUMINATE. THE FLIGHT CREW CYCLED THE SLATS, PERFORMED COM PROCEDURES, CONTACTED MAINTENANCE CONTROL, DECLARED AN EMERGENCY, AND LANDED AT MEM WITHOUT INCIDE NT. MAINTENANCE REPLACED THE LEFT WING TELESCOPE DUCT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041000814 19980410 00814 NM 1998 4 10 9806012204 1 19980319 A 3030 HEATER BOEING 727 727251 138408H NM LT STATIC PORT INOPERATIVE A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 204US 22544 AT FL350, THE LEFT STATIC PORT HEATER INDICATION LIGHT ILLUMINATED. RESET CIRCUIT BREAKER, NO HELP. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. REPLACED THE LEFT STATIC PORT HEATER, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998041000815 19980410 00815 SO 1998 4 10 COMA9810084 1 19980405 A 3397 WIRE EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 261CA 120254 EMERGENCY EXIT SIGN AT ROW 8 DOES NOT ILLUMINATE. REPAIRED BROKEN WIRE AT EXIT SIGN. 2 L 7 2 4T RT A31SO 1998041000816 19980410 00816 EA 1998 4 10 COMA9860071 1 19980405 A 3230 PIN CNDAIR CL600 CL6002B19 EA NLG INSTALLED A COMA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 01 978CA 7158 NLG FAILED TO RETRACT. REMOVED DOWN LOCK SAFETY PIN AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1998041000817 19980410 00817 EA 1998 4 10 COMA9860072 1 19980403 A 3244 50105711 TIRE 50105711 CNDAIR CL600 CL6002B19 EA LT MLG FAILED A COMA K NONE O OTHER LD LANDING 1 SO 01 926CA 2532 252 NOV961174 7027 THE LEFT HAND TIRES BURST DURING LANDING. REPLACED THE LEFT MLG WHEEL ASSY AND COMPLIED WITH BURST TIRE INSP. 2 L 7 2 4F RT A21EA 1998041000818 19980410 00818 EA 1998 4 10 COMA9860073 1 19980403 A 3350 LIGHTS CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 988CA 7204 ONE SECTION OF EMERGENCY FLOOR LIGHTING IS INOP. DEFERRED PER MEL. 2 L 7 2 4F RT A21EA 1998041000819 19980410 00819 EU 1998 4 10 WWMA9800068 1 19980405 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 340RC 340B340 EMERGENCY LIGHT AT ROW 3A FAILED TO ILLUMINATE DURING TEST. REPLACED BULB. 2 L 7 2 4T RT A52EU 1998041000820 19980410 00820 EU 1998 4 10 WWMA9800067 1 19980403 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 352SB 340B352 OVERHEAD EMERGENCY LIGHT AT ROW 11A FAILED TO ILLUMINATE. REPLACED BULB. 2 L 7 2 4T RT A52EU 1998041000821 19980410 00821 EU 1998 4 10 QXEA9800457 1 19980227 A 5320 WINDOW POST FOKKER F28 F28MK4000 4990810 EU NR 2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 RIGHTHAND NR 2 WINDOW POST HAS A .1875 INCH CRACK. REPAIRED IAW HORIZON EA 4-53-376. 2 L 7 2 4F RT A20EU 1998041000822 19980410 00822 EU 1998 4 10 QXEA9800458 1 19980304 A 5320 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 COCKPIT PEDESTAL HAS CORROSION AT RT SIDE IN NUMEROUS LOCATIONS ALONG LOWER MOUNTING STRUCTURE. REPAIRED IAW HORIZON ZI R EA 4-53-377. 2 L 7 2 4F RT A20EU 1998041000823 19980410 00823 EU 1998 4 10 QXEA9800459 1 19980304 A 5320 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 COCKPIT PEDESTAL HAS CORROSION AT LT SIDE IN NUMEROUS LOCATIONS. REPAIRED IAW HORIZON AIR EA 4-53-377. 2 L 7 2 4F RT A20EU 1998041000824 19980410 00824 EU 1998 4 10 QXEA9800460 1 19980225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 MINOR NICKS AND GOUGES IN LUG OF LT OB SEAT TRACK BETWEEN FRAME 13815A AND 15205. REPAIRED IAW FOKKER SRM 53-02-15. 2 L 7 2 4F RT A20EU 1998041000825 19980410 00825 EU 1998 4 10 QXEA9800461 1 19980227 A 5220 FLANGES FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 SERVICE/EMERGENCY DOOR INTERNAL LOWER CENTER AND LOWER AFT OVAL LIGHTENING HOLES HAVE CRACKS ON FLANGES. REPAIRED IAW F OKKER SRM 53-02-01 PAGE 10 FIGURE 8. 2 L 7 2 4F RT A20EU 1998041000826 19980410 00826 EU 1998 4 10 QXEA9800462 1 19980227 A 5220 DOOR FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 SERVICE/EMERGENCY DOOR INTERNAL UPPER INBD EDGE IS CHAFED IN SIX PLACES. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998041000827 19980410 00827 EU 1998 4 10 QXEA9800463 1 19980304 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 RT INBD SEAT TRACK HAS GOUGES AND NICKS IN TRACK AT TOP SURFACE. REMOVED AND REPLACED SEAT TRACK IAW FOKKER SRM 53-02-1 5. 2 L 7 2 4F RT A20EU 1998041000828 19980410 00828 EU 1998 4 10 QXEA9800464 1 19980306 A 5720 FITTING FOKKER F28 F28MK4000 4990810 EU REAR SPAR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 RIGHT REAR SPAR END FITTING HOLE HAS CRACK INDICATIONS AT LOWER END. REPAIRED IAW HORIZON AIR EA 4-53-387. 2 L 7 2 4F RT A20EU 1998041000829 19980410 00829 EU 1998 4 10 QXEA9800465 1 19980225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 DEEP GOUGE ON LEFTHAND INBOARD SEAT TRACK. INSTALLED NEW SECTION OF SEAT TRACK AND SPLICE SECTION IAW FOKKER SRM 53-02- 15, PAGE 3. 2 L 7 2 4F RT A20EU 1998041000830 19980410 00830 EU 1998 4 10 QXEA9800466 1 19980228 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACKS AT BOTH ENDS OF TRANSVERSE ANGLE AT FWD BASE OF VERT STAB. REPAIRED IAW FOKKER SRM 51-10-05 PAGE 601. 2 L 7 2 4F RT A20EU 1998041000831 19980410 00831 EU 1998 4 10 QXEA9800467 1 19980301 A 5510 MOUNT FOKKER F28 F28MK4000 4990810 EU HORIZ STAB FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 THE ELEVATOR BOOSTER TO HORIZONTAL STAB MOUNTS HAVE .010 TO .015 RADIAL PLAY AND THE LOWER LEFT MOUNT IS FRETTING. REPA IRED IAW HORIZON AIR EA 4-55-51. 2 L 7 2 4F RT A20EU 1998041000832 19980410 00832 EU 1998 4 10 QXEA9800468 1 19980226 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CRACK BETWEEN TWO RIVETS AS SEEN FROM INSIDE LIGHTENING HOLE, ON LEFTHAND WING, INSIDE INBOARD FLAP WELL AT ATTACH POINT OF OUTBOARD SPRING STRUT. REPAIRED IAW HORIZON AIR EA 4-57-97. 2 L 7 2 4F RT A20EU 1998041000833 19980410 00833 EU 1998 4 10 QXEA9800569 1 19980225 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 THERE IS A GOUGE ON TOP OF THE SEAT TRACK BETWEEN FRAMES 9305 AND 9305A ON LEFTHAND INBOARD SIDE. REPAIRED IAW FOKKER S RM 53-02-15 FIGURE 1. 2 L 7 2 4F RT A20EU 1998041000834 19980410 00834 WP 1998 4 10 98FDEA00249 1 19980402 A 3260 CONTROL UNIT DOUG DC10 DC1030F 3023504 WP LANDING GEAR FAILED A FDEA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 25 302FE 46801 ON FINAL LANDING GEAR CAME DOWN BUT NO GREEN GEAR LIGHT DOWN LIGHT. RECYCLED LANDING GEAR UP AND THAN DOWN AND THAN REC EIVED 4 GREEN LIGHTS. REMOVED AND REPLACED CONTROL UNIT PER M/M 32-61-01, BITE TEST GOOD. 2 L 7 3 4F RT A22WE 1998041000835 19980410 00835 WP 1998 4 10 98FDEA00250 1 19980405 A 5230 SLIDER DOUG DC10 DC1030F 3023504 WP CARGO DOOR BROKEN A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 322FE 47908 SHORT FINAL, LEFT AFT CARGO DOOR LIGHT ON F/E PANEL ILLUM FOLLOWED BY IMMEDIATE PRESSURE DROP IN CABIN. ACFT WAS ALREAD Y CONFIGURED FOR LANDING, LANDED SUCCESSFULLY, NO FURTHER PROBLEMS. DOOR 4L SWITCH NOT WORKING DUE TO TRACK CAM AND SLI DER BROKEN. REPLACED TRACK CAM AND SLIDER, OPS OK. C/B'S DO NOT POP. 2 L 7 3 4F RT A22WE 1998041000836 19980410 00836 NM 1998 4 10 98FDEA00251 1 19980406 A 3234 SOLENOID BOEING 727 72725C 138400H NM GEAR HANDLE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 116FE 19298 LANDING GEAR HANDLE FAILED TO GO UP BEYOND OFF POSITION. COMPLETED LANDING GEAR LEVER LATCH FAIL TO RELEASE CHECK LIST THROUGH STEP 7. DETERMINE LEVER LATCH SOLENOID IS INOPERATIVE. REMOVED AND REPLACED MAIN LANDING GEAR SAFETY SWITCH PE R MAINTENANCE MANUAL 32-09-211, NO HELP. REMOVED AND REPLACED LANDING GEAR HANDLE LOCK SOLENOID PER MAINTENANCE MANUAL 32-31-12 PAGE 401-403, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1998041000837 19980410 00837 NE 1998 4 10 98FDEA00252 2 19980404 A 7200 ENGINE BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 2 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 154FE 18287 NR 2 ENGINE OIL PRESSURE EXCEEDED RED RADIAL DURING DEPARTURE AT ALL POWER SETTINGS ABOVE IDLE. OIL TEMPERATURE 118C, P RESS 60 PSI PRESS 52 PSI AT IDLE. FOUND BREATHER PRESSURE AT 5.6 PSI OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE F OR HIGH BREATHER PRESSURE PER WORK CARD 70T0502. 2 L 7 3 4F 4 F A3WE E2EA 1998041000838 19980410 00838 NM 1998 4 10 98FDEA00253 1 19980407 A 7933 56B17C OIL TEMP BULB BOEING 727 727277 138408S NM NR 3 ENGINE INOPERATIVE A FDEA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 25 241FE 20979 NR 3 OIL TEMPERATURE GAUGE INOPERATIVE. NEEDLE HANGS STRAIGHT DOWN TWITCHES OCCASIONALLY. REMOVED AND REPLACED NR 3 OI L TEMPERATURE BULB PER MAINTENANCE MANUAL 79-32-01. 2 L 7 3 4F RT A3WE 1998041000839 19980410 00839 WP 1998 4 10 98FDEA00254 1 19980402 A 3260 SWITCH DOUG DC10 DC1030F 3023504 WP LANDING GEAR FAILED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 302FE 46801 LANDING GEAR HANDLE WAS PLACED DOWN, ALL INDICATORS REMAINED RED. LANDING GEAR HANDLE WAS CYCLED TWICE, NO JOY. ALTERN ATE EXTENSION HANDLES WERE ACTUATED IN ACCORDANCE WITH ED TAB PROCEDURES. ALL INDICATORS WENT GREEN. REPEAT. INSTALLE D GEAR PINS, REPLACED LANDING GEAR CONTROL SWITCH PER M/M 32-61-04-2 PG 201-203.98743. OPERATED GEAR HANDLE SEVERAL TIM ES. GEAR LIGHT WERE RED WITH HANDLE UP AND GREEN WITH HANDLE DOWN. OK FOR SERVICE. REMOVED GEAR PINS. 2 L 7 3 4F RT A22WE 1998041000841 19980410 00841 NM 1998 4 10 98UAL900031 1 19980125 A 2612 649302 FIRE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 585UA 26709 LEFT ENGINE HAD FIRE LP2 INDICATION. *S/D* FOUND LOWER CORE NUMBER 2 LOOP FAULTED. REPLACED THE DETECTOR ASSEMBLY AND THE SYSTEM OPERATIONALLY CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041000842 19980410 00842 NE 1998 4 10 98UAL900039 2 19980125 A 7200 3F13513501 SWITCH BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE FAILED A UALA K NONE O OTHER LD LANDING 1 WP 29 4728U 19925 663086 ENGINE BACKFIRE, POP DURING LANDING ROLL WITH ACCOMPANYING FLASH NOTICED FROM CABIN. NO ABNORMAL ENGINE INDICATIONS. * S/D* WHEN THE STALL IN REVERSE OCCURRED THE NR 4 ENGINE REVERSER WAS LOCKED AND DEACTIVATED SO IT WAS NOT USED FOR REVE RSE AND COULD NOT HAVE STALLED IN REVERSE. HOWEVER, HNL ACCOMPLISHED STALL CHECKS ON ALL THE ENGINES NR 1, 2 AND 4 ENGI NES CHECKED OK. NR 3 ENGINE FAILED THE RABS CHECK. FOUND THE RABS SWITCH FAULTY AND REPLACED SWITCH. 2 L 7 4 4F 4 F A20WE E20EA 1998041000843 19980410 00843 NM 1998 4 10 98UAL900073 1 19980219 A 2932 SR2C7PL02 TRANSMITTER AMATEK ST107R BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE B-HYD SYST FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 363UA 8363A 24532 AFTER THE GEAR WAS RAISED, THERE WAS A 'B' SYSTEM HYDRAULIC PRESSURE LOSS. *S/D* REPLACED 'B' SYSTEM PRESSURE TRANSMI TTER. HYDRAULIC SYSTEM CHECKS NORMAL AFTER REPLACEMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041000844 19980410 00844 NM 1998 4 10 98UAL900076 1 19980218 A 3350 BATTERY PACK BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 165UA 21658 PER CREW, EMERGENCY LIGHTS ILLUMINATED ROWS 13 TO 17. CYCLING CIRCUIT BREAKER AND FLIGHT DECK SWITCH, NO HELP. *S/D* P ROBLEM WAS RESOLVED WHEN THE BATTERY PACK WAS REPLACED. PROBABLE CAUSE WAS DEGRADATION OF THE NICAD BATTERIES. 2 L 7 4 4F 4 F A20WE E20EA 1998041000845 19980410 00845 NM 1998 4 10 98UAL900077 1 19980218 A 3350 BATTERY PACK BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 4732U 19927 EMERGENCY LIGHTS AT 4 LEFT AND RIGHT ARE ON WHEN SWITCH IS ARMED. *S/D* PROBLEM WAS RESOLVED WHEN THE BATTERY PACK WAS REPLACED. PROBABLE CAUSE WAS DEGRADATION OF THE NICAD BATTERIES. 2 L 7 4 4F 4 F A20WE E20EA 1998041000846 19980410 00846 NM 1998 4 10 98UAL900124 1 19980326 A 7830 REVERSER LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 ENGINE ILLUMINATED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 194UA 26892 663090 ON TAKEOFF AT 138 KTS, AMBER NR 2 REVERSER CAME ON. ABORTED TAKEOFF. 2 L 7 4 4F 4 F RT A20WE E24NE 1998041000847 19980410 00847 NM 1998 4 10 98UAL900125 1 19980327 A 3231 141N09362 ROD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NLG DOOR BROKEN A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 539UA 25223 RETURNED TO ORD DUE TO NOISE IN NOSE GEAR AREA WHEN GEAR WAS RETRACTED. *S/D* RIGHT NOSE GEAR STRUT DOOR AND OPERATIN G ROD WAS DAMAGED FROM POSSIBLE DOOR IMPACT WITH BAGGAGE CART. REPLACED ROD AND DOOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041000848 19980410 00848 NE 1998 4 10 98UAL900126 2 19980328 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE DAMAGED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 583UA 17234 26705 RETURNED TO SEA UNDER AMBER ALERT DUE TO NR 1 ENGINE COMPRESSOR STALL. *S/D* THE NR 1 ENGINE INGESTED ICE AND SUSTAINE D DAMAGE TO THE HIGH PRESSURE COMPRESSOR. THE 6TH STAGE BLADES WERE FOUND TORN. THE DAMAGED BLADES WERE REPLACED. AS A PRECAUTIONARY, THE NR 2 ENGINE WAS INSPECTED AND COMPRESSOR DAMAGE WAS FOUND. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041000849 19980410 00849 NM 1998 4 10 98UAL900127 1 19980328 A 2782 LEFDU ALLIED SIGNA 126344 BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE LE FLAPS FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 157UA 119P799 20106 LEADING EDGE FLAP LIGHTS STAYED ON DURING FLIGHT UNTIL CREW WENT FROM POSITION ONE, TO FLAP POSITION FIVE. GREEN LIGHT THEN CAME ON AND STAYED ON THROUGH LANDING. *S/D* LEADING EDGE FLAP DRIVE UNIT AT POSITION NR 1 LT FAILED. REPLACED L EFDU AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1998041000850 19980410 00850 NM 1998 4 10 98UAL900128 1 19980328 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7449U 21903 AIRSTAIR EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED BATTERY. 2 L 7 3 4F 4 F A3WE E2EA 1998041000851 19980410 00851 NE 1998 4 10 98UAL900129 2 19980328 A 7310 SEAL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 7268U 21415 DURING CLIMB 800-1000, NR 3 ENGINE LOST THRUST. EPR DROPPED TO APPROXIMATELY 1.0 EGT, OIL PRESSURE, OIL QUANTITY NORMAL . ENGINE CONTINUED TO RUN. FUEL FLOW APPROXIMATELY 3000 PPH WITH NO THROTTLE RESPONSE. RETURNED TO SFO. THE ENGINE L OST THRUST DUE A FAILED FUEL SEAL. THE FUEL CONTROL AND FUEL PUMP WERE ALSO REPLACED FOR PRECAUTIONARY REASONS. 2 L 7 3 4F 4 F A3WE E2EA 1998041000852 19980410 00852 1998 4 10 98UAL900130 4 19980323 A 2565 SLIDE BF GOODRICH 7A14693 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 177UA GO55 24384 DURING THE SHOP OVERHAUL OF A SLIDE/RAFT REMOVED FOR TIME EXPIRATION THE RIGHT HAND GIRT ATTACHMENT, PART NUMBER 5A22883 -2, WAS FOUND TO BE TEARING LOOSE FROM THE BOTTOM TUBE. SLIDE/RAFT SENT TO VENDOR FOR REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 1998041000854 19980410 00854 NM 1998 4 10 98UAL900132 1 19980322 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7284U 21562 CORROSION FOUND BETWEEN RAM AIR DOOR ACTUATOR EXTERNAL ACCESS PANEL AND FUSELAGE SKIN. REMOVED CORROSION FROM SKIN AND PERFORMED EXTERNAL SKIN REPAIR PER 727 SRM 53-30-3. 2 L 7 3 4F 4 F A3WE E2EA 1998041000855 19980410 00855 NM 1998 4 10 98UAL900133 1 19980331 A 7830 21L12 EAU FORK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E3 RACK FRACTURED A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 345UA 24249 BOTH THRUST REVERSER UNLOCK LIGHTS ILLUMINATED AFTER TAKEOFF. *S/D* FOUND ENGINE ACCESS UNIT RETAINING FORK ON RADIO R ACK FRACTURED AND MISSING PIN. EAU WAS LOOSE IN RACK. REPLACED FORK AND PERFORMED EAU OPS CHECK, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041000856 19980410 00856 WP 1998 4 10 98UAL900134 1 19980401 A 3230 RETRACT MECH DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LT MLG LACK OF LUBE A UALA K NONE J WARNING INDICATION CR CRUISE 1 WP 29 1838U 46632 AFTER TAKEOFF, LEFT MAIN GEAR DID NOT RETRACT. DURING FLIGHT GEAR CAME UP. NORMAL LANDING AT ORD. *S/D* LEFT MAIN LA NDING GEAR WAS FOUND WITH INADEQUATE LUBRICANT. THE GEAR WAS LUBED AND WAS OPERATED SEVERAL TIMES TO CONFIRM A NORMAL O PERATION. 2 L 7 3 4F 4 F A22WE E23EA 1998041000857 19980410 00857 NM 1998 4 10 98UAL900135 1 19980401 A 3350 CONNECTOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 656UA 25394 EEL FLOOR PATH LIGHTS ARE INOP ON RIGHT HAND SIDE FROM DOOR 1 RIGHT TO SEAT 6E. PROBLEM ORIGINATES AT CONNECTOR AT SEAT 1E. REPLACED EEL FEEDER STRIP FROM WALL AT 1 E AND F. 2 L 7 2 4F 4 F RT A1NM E24NE 1998041000858 19980410 00858 WP 1998 4 10 ABXA9800312 1 19980328 A 5320 57500421 ANGLE DOUG DOUG DC8 DC863F 302198F WP BS 930-935 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 KEEL BEAM AREA AT APPROXIMATELY STATION 930 TO 935 RIGHT SIDE, THE KEEL ANGLE HAS A 5 INCH CRACK. REPAIRED IAW ABX REA D853-22758 AND DC8 SRM 52-2-0. 2 L 7 4 4F 4A25 1998041000859 19980410 00859 WP 1998 4 10 ABXA9800313 1 19980305 A 5720 36468741 FITTING DOUG DOUG DC8 DC863F 302198F WP WS 23 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WHEEL WELL FITTING CRACKED AT STATION XCW 23 BELOW PRESSURE PANEL. REPAIRED IAW DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998041000860 19980410 00860 WP 1998 4 10 ABXA9800314 1 19980312 A 5320 3755847501 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 1150 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 SHEAR TIE AT STATION 1150 BETWEEN LONGERON 30R AND 33R HAS 6 INCH CRACK. REPAIRED IAW SRM 51-1-20D. 2 L 7 4 4F 4A25 1998041000861 19980410 00861 WP 1998 4 10 ABXA9800315 1 19980313 A 5320 3755843502N SHEAR TIE DOUG DOUG DC8 DC863F 302198F WP BS 1160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 SHEAR TIE CRACKED, STATION 1160 BETWEEN LONGERON 34R TO 35R. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998041000862 19980410 00862 WP 1998 4 10 ABXA9800316 1 19980212 A 5320 3750496 SPLICE DOUG DOUG DC8 DC863F 302198F WP BS 620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 STATION 620 BETWEEN STRINGERS 35R AND 35L FRAME SPLICE HAS 8 INCH CRACK. REPAIRED IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1998041000863 19980410 00863 WP 1998 4 10 ABXA9800317 1 19980311 A 5711 5597830501 SPAR DOUG DOUG DC8 DC863F 302198F WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WHEEL WELL AT FWD LOWER OUTBOARD END, REAR SPAR LOWER CHORD HAS NUMEROUS CRACKS. REPAIRED IAW ABX REA D857-22747 MR. 2 L 7 4 4F 4A25 1998041000864 19980410 00864 WP 1998 4 10 ABXA9800318 1 19980406 A 5753 995760016 ANGLE DOUG DOUG DC9 DC931 3022065 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE BRACKET INTERNAL ANGLE CRACKED AT OUTBOARD SIDE. REPLACED ANGLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041000865 19980410 00865 WP 1998 4 10 ABXA9800319 1 19980406 A 5320 49125401 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND FLOORBEAM VERTICAL SUPPORT FITTING BELOW PYLON BULKHEAD CRACKED, STATION 965. REPLACED FITTING IA W DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998041000866 19980410 00866 WP 1998 4 10 ABXA9800320 1 19980406 A 5510 591802011 BRACKET DOUG DOUG DC9 DC931 3022065 WP HORIZ STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND THE BRACKET BELOW AND INBOARD OF NR 1 LEFT ELEVATOR HINGED BEARING CRACKED. REPLACED BRACKET IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041000867 19980410 00867 WP 1998 4 10 ABXA9800321 1 19980406 A 5313 59364369 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND LONGERON 13R AT STATION 965 CRACKED. REPLACED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041000868 19980410 00868 WP 1998 4 10 ABXA9800322 1 19980406 A 5313 59114082 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LONGERON 6R CRACKED AT STATION 680. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041000869 19980410 00869 WP 1998 4 10 ABXA9800323 1 19980406 A 5313 59114082 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LONGERON 6R CRACKED AT STATION 617. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041000870 19980410 00870 WP 1998 4 10 MWEA98385 1 19980402 A 7110 59586564 SKIN DOUG DC9 DC914 3022034 WP RT COWL TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 THE RIGHT HAND UPPER COWL APRON LATCH AREA HAS TORN SKIN. MTC FABRICATED AND INSTALLED REPAIR SKIN. 2 L 7 2 4F A6WE 1998041000871 19980410 00871 WP 1998 4 10 MWEA98386 1 19980402 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP PAX DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 301ME 47190 THE PASSENGER ENTRANCE DOOR SLIDE COVER CAME OFF WHEN OPENED. MTC REINSTALLED PASSENGER DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998041000872 19980410 00872 NM 1998 4 10 DL76L980671 1 19980327 A 2520 RDAX4406 SEAT ELECT BOX BOEING 767 767332 1382001 NM CABIN FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 173DN 24800 PROBLEM OCCURED 7 HRS INTO FLT, A SMOKE ODOR WAS OBSERVED COMING FROM THE CAPTS SIDE OF THE ACFT NEAR ROW 24. C/B' S WE RE NORMAL. THE F/A WERE DIRECTED TO SHUT OFF POWER TO THE MID GALLEY AND PAX ENTERTAINMENT SYSTEM. THE ODOR DISSIPATED SHORTLY THEREAFTER. REPLACED SEB AT SEAT 22AB. 2 L 7 2 4F RT A1NM 1998041000873 19980410 00873 WP 1998 4 10 DLL10980672 1 19980327 A 5240 COUNTERBALANCE 527001348 LKHEED 1011 10113851 5265010 WP R4 DOOR BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 720DA 439 193C1136 R-4 DOOR DOES NOT OPEN WHEN USING EMERGENCY HANDLE. ITEM FOUND DURING E-LETTER CHECK INITIAL INSP, OPN 58131. ITEM CLE ARED BY REPLACING DR COUNTERBALANCE. OPS CK GOOD OPN 68115 ITEM REPLACED ON N/R CARD 149. 2 L 7 3 4F A23WE 1998041000874 19980410 00874 NM 1998 4 10 DL72S980673 1 19980327 A 3310 INDICATOR BOEING 727 727232 1384082 NM COCKPIT SHORTED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 536DA 22049 AT FL 310 HAD STRONG ELECT SMELL LIKE PLASTIC BURNING. INDICATOR LTS MASTER SECT 1 C/B POPPED. ODOR SLOWLY SUBSIDED, F OUND COCKPIT INDICATOR SHORTING TO GROUND. REPOSITIONED TERMINALS, CKS OK. 2 L 7 3 4F A3WE 1998041000875 19980410 00875 NM 1998 4 10 DL76L980674 1 19980327 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DN 24763 24759 EMERGENCY AISLE LIGHTS ROWS 24 TO 27 RIGHT AND LEFT SIDES INOP. REPLACED POWER SUPPLY, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1998041000876 19980410 00876 NM 1998 4 10 DL72K980675 1 19980328 A 3260 656021132 ACCESSORY UNIT BOEING 727 727232 1384082 NM LANDING GEAR FAILED A DALA O OTHER B P SMOKE/FUMES/ODORS/SPARKS NO WARNING INDICATION AP APPROACH 1 SO 27 481DA 20861 WHEN GEAR HANDLE SELECTED DOWN GEAR LIGHTS DID NOT ILLUM. GEAR HANDLE WAS SELECTED UP BUT WOULD NOT GO PAST OFF. POM A BNML PROCEDURE WAS C/W. FOUND LEVER LATCH CB POPPED. RESET CB GEAR, LIGHTS ILLUMINATED, GEAR WAS VISUALLY CONFIRMED DO WN. FOUND LEVER LATCH C/B POPPED. FOUND LDG GEAR ACCY UNIT WITH HEAVY ELECT SMELL. REPLACED LDG ACCY UNIT. REPLACED LEVER LATCH C/B. REPLACED R92 LDG SAFETY RELAY. PERFORMED GEAR SWING PER MM. PERFORMED LDG GEAR ELECT MODULE ADJ TEST PER MM. ALL CHKS NML. RESTORED A/C TO NML. 2 L 7 3 4F A3WE 1998041000877 19980410 00877 NM 1998 4 10 DL76L980679 1 19980328 A 3242 26088127 BRAKE BOEING 767 767332 1382001 NM NR 4 BURNED A DALA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 181DN 25986 A/C ARRIVED GATE WITH NR 4 BRAKE ON FIRE. EXTINGUISHED FIRE COOLED BRAKE AND REPLACED BRAKE AND WHEEL ASSY PER M/M. RE PLACED WHEEL AND BRAKE, SYSTEM NORMAL. 2 L 7 2 4F RT A1NM 1998041000878 19980410 00878 NM 1998 4 10 DLM90980680 1 19980328 A 3350 BULB 081691 DOUG MD90 MD9030 3023690 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DN 53392 EMERGENCY TRACK LIGHT 2C INOP. REPLACED SOCKET BULB AND LENS, OPS CHKS GOOD. REMOVED MCO AND PLAC. 2 L 7 2 4F RT A6WE 1998041000879 19980410 00879 NM 1998 4 10 DL76L980681 1 19980328 A 3350 BATTERY 20131A BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DN 2377 25061 OUTSIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY, SYSTEM OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1998041000880 19980410 00880 WP 1998 4 10 DLL17980682 1 19980329 A 5220 COUNTERBALANCE 1282T10019 LKHEED 1011 10113853 5265020 WP L3 DOOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 765DA 1817RW 193H1206 AIRCRAFT ARRIVED WITH L3 EMERGENCY HANDLE PARTIALLY OPEN. REPLACED COUNTERBALANCE AND RIGGED DOOR. 2 L 7 3 4F A23WE 1998041000881 19980410 00881 WP 1998 4 10 DLL10980683 1 19980328 A 5330 1503140147 SKIN LKHEED 1011 10113851 5265010 WP BS 759 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE FUSELAGE SKIN AT FS 759 AND STRINGER 38 WAS FOUND CRACKED DUE TO CORROSION. THE CORRODED AREA WAS TRIMMED OUT AND A N EXTERNAL ALUMINUM DOUBLER WAS INSTALLED PER ER/A 364366-14, REV A. 2 L 7 3 4F A23WE 1998041000882 19980410 00882 NM 1998 4 10 DL757980684 1 19980327 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 646DL 24217 THE UPPER CAP OF THE STA 1681.8 FLOORBEAM WAS FOUND CORRODED ALONG ITS ENTIRE LENGTH LBL 61.95 TO RBL 61.95. THE UPPER CAP WAS TRIMMED OFF AND AN EXTRUDED CAP INSTALLED IN ITS PLACE PER ER/A 364222-14, REV B. 2 L 7 2 4F RT A2NM 1998041000883 19980410 00883 WP 1998 4 10 DLL10980685 1 19980327 A 5730 1527139107 SKIN LKHEED 1011 10113851 5265010 WP WS 477 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 720DA 193C1136 THE LT LOWER WING SKIN WAS FOUND CRACKED AT IWS 477 AND STRINGER 17. THE CRACK IS SUBJECT TO THE SID AD 95-20-04. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A DOUBLER AND TRIPLER PER ER/A 364365-14AD, REV A. THE ER/A WAS GRANTED AMOC A PPROVAL. 2 L 7 3 4F A23WE 1998041000884 19980410 00884 NM 1998 4 10 DL72S980686 1 19980322 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 303 PART A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 ANGLE CRACKED STA 303.9 FWD CABIN LBL 28. REPLACED ANGLE PER SRM 51- 00. 2 L 7 3 4F A3WE 1998041000885 19980410 00885 NM 1998 4 10 DL72S980689 1 19980330 A 5320 WEB BOEING 727 727232 1384082 NM BS 1237 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 FOUND ON D1 LETTER CK, LT VERT TORQUE BOX WEB CRACKED AT UPPER END AT STA 1237 LT. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998041000886 19980410 00886 NM 1998 4 10 DL76L980691 1 19980329 A 2560 60231002 ACTUATOR BOEING 767 767332 1382001 NM RT WING FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 199DN 28456 RT OVERWING SQUIB TEST INOP. FOUND BLOW DOWN ACTUATOR BLOWN AND 2 SECOND RELAY ON RIGHT WING BAD. REPLACED ACTUATOR AN D WAITING ON 2 SECOND RELAY. 2 L 7 2 4F RT A1NM 1998041000887 19980410 00887 WP 1998 4 10 DLL17980694 1 19980331 A 5220 COUNTERBALANCE 1282T10019 LKHEED 1011 10113853 5265020 WP L3 D00R WEAK A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 767DA 181TRW 193H1209 L3 DOOR FAILED OPN 68116, EMERGENCY DOOR OPERATIONAL. OPS TIME GREATER THAN 7 SECONDS. REPLACED COUNTERBALANCE. 2 L 7 3 4F A23WE 1998041000888 19980410 00888 NM 1998 4 10 DL72S980696 1 19980324 A 5510 BUSHING BOEING 727 727232 1384082 NM RT HORZ STAB WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 BUSHINGS WORN RT HORZ STAB. NR 1 HINGE ATTACH PT FOR ELEV FITTING BUSHINGS ARE WORN. ALSO, HARDWARE IS WORN AND FITTIN G LUGS ARE WORN. SPOTFACED .013 ON D/B FACE OF I/B LUG AND .010 ON I/B FACE OF O/B LUG. REMOVED BUSHINGS AND CLEANED L UGS WITHIN LIMITS PER MM 55-50-0 FIG 801. ROTOPEENED PER PS 900-4-01005 TREAT AND PAINTED FACES AND BORES. TURNED BUSH INGS LENGTHEN LUGS. INSTALLED BUSHINGS PER MM 55-58-0 PG 802. REPLACED HARDWARE, OK TO ROTOPEEN. OK TO TREAT AND PAIN T. 2 L 7 3 4F A3WE 1998041000889 19980410 00889 NM 1998 4 10 DL72S980697 1 19980328 A 5510 BUSHING BOEING 727 727232 1384082 NM LT HORIZ STAB WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 LT HORIZ STAB NR 1 HINGE ATT PT FUS ELEV, FITTING AND BUSHINGS ARE WORN. SPOTFACE I/B FACE OF O/B LUG .012 REMOVED BUSH INGS, CLEANED LUG WITHIN LIMITS PER MM 55-50-0 FIG 801. ROTOPEENED PER PS900-4 TREAT FACES AND BORES. PAINTED FACES AN D BORES. TURNED BUSHNGS TO LENGTH OF LUG THICKNESS. INSTALLED BUSHINGS PER M/M 55-50-0 PG 802. OK TO ROTOPEEN, TO TRE AT/PAINT, OK TO INSTL BUSHINGS. 2 L 7 3 4F A3WE 1998041000890 19980410 00890 NM 1998 4 10 DL72S980700 1 19980326 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 ON UPPER SURFACE OF FLOORBEAM STA 344 FROM LT O/B SEAT TRACK TO DOOR SILL FOUND CORROSION. INSTALLED NEW FLOORBEAM PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1998041000891 19980410 00891 NM 1998 4 10 DLM88980701 1 19980331 A 5320 THRESHOLD DOUG MD88 MD88 3023688 NM C1 DOOR CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 904DE 53409 CORROSION ALONG C-1 DOOR THRESHOLD SEVERAL PLACES. CLEANED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-01. REMOVED DAMAGED SECTION AND FABRICATED REPAIR DOUBLERS AND REPLACEMENT SECTION PER ERA 364414-14. FINISHED INSTALLATION PER ER A 364414-14. 2 L 7 2 4F RT A6WE 1998041000892 19980410 00892 NM 1998 4 10 DLM88980704 1 19980401 A 2170 COALESCER V1211 DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 911DL 49542 AFT LAV SMOKE DETECTOR ACTIVATED ON SHORT FINAL. ENG AND AIRFOIL A/I HAD BEEN TURNED ON PASSING 15,000 FT AND TURNED OFF PASSING 2,000 FT. BURNING ODOR WAS NOTICED BUT NO SMOKE. REPLACED WATER BAGS, OPERATED PACKS NO ODORS NOTICED. 2 L 7 2 4F RT A6WE 1998041000893 19980410 00893 NM 1998 4 10 DL72E980707 1 19980401 A 5320 WEB BOEING 727 727247 138408F NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 FOUND ON F1 LETTER CK, .125 INCH CRACK AT LIGHTENING HOLE IN LT TORQUE BOX VERTICLE WEB STA 1223. ROUTED OUT DAMAGED AR EA PER MM 53-11-0. 2 L 7 3 4F A3WE 1998041000894 19980410 00894 NM 1998 4 10 DL72E980709 1 19980401 A 5411 RIB BOEING 727 727247 138408F NM BS 1342 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 HOLE WORN THROUGH LIP OF NR 2 ENGINE CUTOUT AT 9 O'CLOCK POSITION. FOUND ON LETTER CHECK F-1. INSTALLED DOUBLER PER M/ M 53-11-0 PG 801. 2 L 7 3 4F A3WE 1998041000895 19980410 00895 NM 1998 4 10 DL72E980710 1 19980401 A 5754 STIFFENER BOEING 727 727247 138408F NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 A 2 INCH CRACK WING L/E VERT STIFFENER AFT OF NR 3 SLAT I/B TRACK. REPAIRED PER MM 57-20-21 PG 813. 2 L 7 3 4F A3WE 1998041000896 19980410 00896 NM 1998 4 10 DL76G980712 1 19980401 A 3350 SIGN S283TO143 BOEING 767 7673P6 1385105 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 152DL 18448 24984 ON L/O, FOUND RT AFT EMERGENCY EXIT SIGN INOP. REPLACED PWR SUPPLY. 2 L 7 2 4F RT A1NM 1998041000897 19980410 00897 NM 1998 4 10 DL757980713 1 19980401 A 5754 WEDGE 114N3002119 BOEING 757 757232 1384965 NM NR 5 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 628DL A10104 22918 NR 5 L/E SLAT T/E WEDGE IS DELAMINATED AT I/B END APPROX 4 BY 6. REMOVED AND REPLACED SLAT. 2 L 7 2 4F RT A2NM 1998041000898 19980410 00898 WP 1998 4 10 DLL10980716 1 19980402 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 760 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 CORROSION WAS FOUND ON THE FWD BELLY SKIN BETWEEN FS 539 AND 983. REPAIRED PER ERA 331516-14. 2 L 7 3 4F A23WE 1998041000899 19980410 00899 NM 1998 4 10 DL73K980717 1 19980402 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 306DL 23078 EMERGENCY LIGHTS SEAT ROW 5 TO 20 WILL NOT EXTINGUISH. REPLACED M9013 BATTERY PACK AND POWER SUPPLY, OPN NML. 2 L 7 2 4F RT A16WE 1998041000900 19980410 00900 NM 1998 4 10 DLM88980719 1 19980402 A 4990 CHIP DETECTOR DOUG MD88 MD88 3023688 NM APU LEAKING A DALA A UNSCHED LANDING B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CL CLIMB 1 SO 27 990DL 53342 SMOKE IN CABIN IMMEDIATELY AFTER T/O. RTB FWD AND AFT SMOKE DETECTORS WENT OFF. FOUND APU CHIP DETECTOR LEAKING OIL. R EPLACED PACKING, PERFORMED DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1998041000901 19980410 00901 NE 1998 4 10 DL73E980720 2 19980402 A 7510 ANTI-ICE BOEING 737 7372S3 NM PWA JT8 JT8D15 52051 NE ENGINE ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 369DL 21776 AT 25,000, AN ELECTRICAL SMELL WAS NOTED IN ENTIRE AIRCRAFT WHEN ENGINE ANTI-ICE WAS TURNED ON. SMELL WENT AWAY WHEN EN GINE ANTI-ICE TURNED OFF. RAN ENGINES AND PACKS, INSPECTED FOR SOURCE, NO TROUBLE FOUND. 2 L 7 2 4F 4 F RT A16WE E2EA 1998041000902 19980410 00902 WP 1998 4 10 DLL14980721 1 19980403 A 3350 BULB LKHEED 1011 1011385115 5265015 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 193C1244 DURING L/O, FOUND EXTERIOR EMERGENCY LIGHTS OUT AT L1 AND L3 DOORS. RELAMPED, OPS CK GOOD. 2 L 7 3 4F A23WE 1998041000903 19980410 00903 NM 1998 4 10 DL72K980722 1 19980402 A 3350 BATTERY 900835A BOEING 727 727232 1384082 NM BS 950 DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 471DA 8225 20748 CARGO DOOR EMERGENCY LIGHT BATTERY PACK FAILED ON TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998041000904 19980410 00904 NM 1998 4 10 DL757980726 1 19980403 A 2530 831610403M0DA OVEN BOEING 757 757232 1384965 NM GALLEY BURNED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 654DL 24394 MID GALLEY OVEN SMOKING. REPLACED OVEN. 2 L 7 2 4F RT A2NM 1998041000905 19980410 00905 NM 1998 4 10 DL72S980727 1 19980325 A 5311 FRAME BOEING 727 727232 1384082 NM BS 930 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 AT HMV, FOUND FS 930 LT SIDE FRAME IS CRACKED 10 INCH BELOW CABIN WINDOW. FABRICATED NEW PARTS SRM 53-10-4, PAINTED/INS TLD COMPLETED PER SAME. 2 L 7 3 4F A3WE 1998041000906 19980410 00906 NM 1998 4 10 DL72S980728 1 19980103 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 497DA 25125 21077 LEFT OVERWING EMERGENCY LIGHT WAS INOP. FOUND THAT BATTERY PACK WAS DEAD. REPLACED BATTERY PACK WITH NEW, OPS NML. 2 L 7 3 4F A3WE 1998041000907 19980410 00907 WP 1998 4 10 DLL13980729 1 19980304 A 2842 287701043 TRANSMITTER LKHEED 1011 10113851 5265010 WP LT WING LOOSE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK K FLUID LOSS TO TAKEOFF 1 SO 27 790DL 193A1143 ON T/O, TOWER REPORTED ACFT HAD SOMETHING STREAMING FROM THE OUTBD LEFT WING. VISUAL INSPECTION NOTED FUEL WAS COMING F ROM TOP OF WING. RETURNED TO SFO. MAINT FOUND NR 5 FUEL QTY TRANSMITTER FOR 2 LT INBD FUEL TANK LOOSE IN ITS HOUSING A ND 4 OF THE 5 SCREWS MISSING. PROBE WAS SECURED AND NEW FASTENERS INSTALLED. AERODYNAMIC SEALER REQUIRED BUT WAS FORWA RDED TO MCO TO AVOID FURTHER DELAY. ACCOUNT SEALER CURE TIME AND OVERWEIGHT INSPECTION WAS PERFORMED PER MM. ACFT LAND ED OVERWEIGHT. 2 L 7 3 4F A23WE 1998041000908 19980410 00908 NM 1998 4 10 DLM88980730 1 19980403 A 2560 LIGHT P20700020 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST CR CRUISE 1 SO 27 901DL 49532 EMERGENCY FLASHLIGHT AFT GALLY INOP. REPLACED FLASHLIGHT WITH SERVICEABLE FLASHLIGHT. 2 L 7 2 4F RT A6WE 1998041000909 19980410 00909 NM 1998 4 10 DL76L980731 1 19980403 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 193DN 28450 F/C AND B/C SEAT MOUNTED EMERGENCY LIGHTS ALL INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 1998041000910 19980410 00910 NM 1998 4 10 DL76L980732 1 19980403 A 3350 0L3071BPEGPL BULB BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 193DN 28450 EMERGENCY LIGHTS AT 1D AND 2B INOP. REBULBED. 2 L 7 2 4F RT A1NM 1998041000911 19980410 00911 NM 1998 4 10 DLM88980733 1 19980404 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM RT ENGINE FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 997DL 53364 NR 2 HYD QTY FELL TO 3 QTS IN FLT. TURNED SYS OFF. TURNED SYS BACK ON FOR FLAP AND GEAR EXT AND QTY DROPPED TO 1 QT. R EPLACED NR 2 ENGINE PRESSURE LINE. 2 L 7 2 4F RT A6WE 1998041000917 19980410 00917 WP 1998 4 10 VJ9800061 1 19980204 A 2730 5957119503 BRACKET DOUG DC9 DC932 3022066 WP ELEVATOR CONTL CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FOUND CRANK BRACKET CORRODED BEYOND LIMITS ON ELEVATOR SERVO CABLE ATTACH. REPLACED CRANK ASSY AND HARDWARE IAW DC9 MM 22-10-5, RIGGED AND OPS CHECKED GOOD IAW DC9 MM 27-40-0. 2 L 7 2 4F A6WE 1998041000918 19980410 00918 WP 1998 4 10 VJ9800062 1 19980205 A 2540 79556527514 TUBE DOUG DC9 DC932 3022066 WP RT AFT LAV CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 CORROSION FOUND ON RT AFT LAV PRESSURE PLUMBING. REPLACED CORRODED SECTION OF PLUMBING IAW DC9 MM 25-41-0. 2 L 7 2 4F A6WE 1998041000919 19980410 00919 WP 1998 4 10 VJ9800063 1 19980205 A 5330 591970731 SKIN DOUG DC9 DC932 3022066 WP BS 900-935 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 AFT PIT LOWER DOOR JAMB CORRODED OUTSIDE AND INSIDE OF BOX FRAME FS 900 TO FS 935. CUTOUT CORRODED AREA FS 908 TO FS 92 5, FABRICATED FILLER, DOUBLER, TRIPLER IAW REA 981127 BCAG DATA FAX FILE MISC 2302, ACTION 3 360129, FILE 98-02-17-021 D TD 20 FEB 98. INSTALLED IAW DC9 SRM 53-05, FIG 106. TREATED AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1998041000920 19980410 00920 WP 1998 4 10 VJ9800064 1 19980205 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 AFT PIT DOOR JAMB BOX FRAME PANEL CORRODED BEYOND LIMITS BETWEEN LONGERONS 25 RT AND 26 RT. FABRICATED NEW PANEL IAW DC 9 SRM 51-10-2 AND 53-11-3 FIG 3 PG 11. TREATED AND PRIMED IAW DC9 SRM 51-10-3, INSTALLED PANEL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041000921 19980410 00921 WP 1998 4 10 VJ9800065 1 19980206 A 5321 FLOOR DOUG DC9 DC932 3022066 WP AFT GALLEY CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 TOP SIDE, BOTTOM EDGE AND BOTTOM SUPPORT RIBS AFT GALLEY CENTER FLOOR PANEL CORRODED BEYOND LIMITS. FABRICATED AND INST ALLED NEW SKIN IAW DC9 SRM 51-10-2. SEALED AND ASSEMBLED PANEL IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041000922 19980410 00922 WP 1998 4 10 VJ9800066 1 19980206 A 5321 FLOOR DOUG DC9 DC932 3022066 WP FLT STATION CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 PILOTS FLOOR BOARD AND ATTACHED PARTS CORRODED BEYOND LIMITS. REMOVED CORROSION AND INSTALLED NEW STIFFENERS AND SKIN I AW DC9 SRM 53-01, FIG 1 AND DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041000923 19980410 00923 WP 1998 4 10 VJ9800067 1 19980206 A 2760 5913879507 BRACKET DOUG DC9 DC932 3022066 WP WS 300 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 RT OUTBOARD SPOILER PULLEY BRACKET CORRODED. REPLACED BRACKET IAW DC9 MM 27-60-0. 2 L 7 2 4F A6WE 1998041000924 19980410 00924 WP 1998 4 10 VJ9800068 1 19980210 A 5321 99101551 FLOOR DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 CENTER FLOOR PANEL AT FS 351 TO FS 446 CORRODED BEYOND LIMITS AT TOP SIDE AND BOTTOM EDGES OF SCREW HOLES. FABRICATED N EW FLOOR PANEL IAW DC9 SRM 51-10-4 AND 53-05, FIG 1. 2 L 7 2 4F A6WE 1998041000925 19980410 00925 WP 1998 4 10 VJ9800069 1 19980210 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 CENTER OF END BRACKET AT FS 218 FROM LONGERON 28L TO 27R CORRODED. FABRICATED NEW BRACKET. HEAT TREATED, DRILLED AND IN STALLED IAW DC9 SRM 51-10-2A, PG 1-24 AND 51-10-1-4, PG 1-24. 2 L 7 2 4F A6WE 1998041000926 19980410 00926 WP 1998 4 10 VJ9800070 1 19980221 A 5320 2777896 ANGLE DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT FS 980, BL46 LT CORRODED BEYOND LIMITS. REMOVED CORROSION, FABRICATED, TREATED AND PRIMED ANGLE, FILLER A NDS SHIM IAW DC9 SRM 53-05, PG 31. 2 L 7 2 4F A6WE 1998041000927 19980410 00927 WP 1998 4 10 VJ9800071 1 19980221 A 5320 2777896 ANGLE DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT FS 980, BL 42 RT CORRODED BEYOND LIMITS. REMOVED CORROSION AND NUT PLATES IAW DC9 SRM 53-05, PG 31, FIG 2 0A AND FABRICATED REPAIR ANGLE AND SHIM PER FIG 20A, VIEW AA. 2 L 7 2 4F A6WE 1998041000928 19980410 00928 WP 1998 4 10 VJ9800073 1 19980223 A 5320 2912758 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT AT FS 996, BL 32 LT, CORRODED BEYOND LIMITS. REMOVED CORROSION IAW DC9 SRM 51-10-3. FABRICATED AND TREAT ED SHIM AND ANGLE IAW DC9 SRM 53-05, FIG 20A. 2 L 7 2 4F A6WE 1998041000929 19980410 00929 WP 1998 4 10 VJ9800074 1 19980228 A 5321 99578022 FLOOR DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR PANEL 4410A CORRODED BEYOND LIMITS ON BOTTOM SIDE IAW DC9 SRM 51-10-3 AND SRM 53-01, FIG 1. REMOVED CORROSION AND FABRICATED PANEL IAW DC9 SRM 51-10-2. BONDED NEW PART IAW DC9 SRM 51-70-3. 2 L 7 2 4F A6WE 1998041000930 19980410 00930 WP 1998 4 10 VJ9800075 1 19980301 A 5315 99581881 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR BEAM AFT LAV FS 965, BL 22R, CORRODED. REMOVED SECTION FLOORBEAM FROM BL 0 TO BL 50R, FABRICATED AND SPLICED NEW SECTION IAW DC9 SRM 53-05, FIG 20A. TREATED AND PRIMED IAW DC9 SRM 51-10-3 AND 51-30-0. 2 L 7 2 4F A6WE 1998041000931 19980410 00931 WP 1998 4 10 VJ9800076 1 19980304 A 5321 99578665 FLOOR DOUG DC9 DC932 3022066 WP BS 130 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR PANEL, FS 130, CORRODED BEYOND LIMITS DC9 SRM 53-01, FIG 1. REMOVED CORROSION IAW DC9 SRM 51-10-3. INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-2 AND 51-30-1. 2 L 7 2 4F A6WE 1998041000932 19980410 00932 WP 1998 4 10 VJ9800077 1 19980311 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 AFT BAGGAGE FLOOR SUPPORT, LT SIDE, BETWEEN LONGERON 28L AND 27L, FS 935, CORRODED. FABRICATED NEW FLOOR SUPPORT IAW DC 9 SRM 51-10-4, 51-30-2, AND 53-01, FIG 2. INSTALLED NEW SUPPORT IAW DC9 SRM 51-30-0 AND 51-30-2. 2 L 7 2 4F A6WE 1998041000933 19980410 00933 WP 1998 4 10 VJ9800078 1 19980318 A 5347 S2772660 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SEAT TRACK FS 200 TO 220, BL 22L, CORRODED. REPLACED SEAT TRACK FROM FS 200 TO 325 IAW DC9 SRM 51-30-1 AND 53-05. 2 L 7 2 4F A6WE 1998041000934 19980410 00934 WP 1998 4 10 VJ9800079 1 19980318 A 5347 S2772660 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-245 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SEAT TRACK FS 200 TO 245, BL 44.5R, CORRODED. REPLACED SEAT TRACK FROM FS 200 TO 245, BL 44.5R, IAW DC9 SRM 51-30-1, 51 -30-2 AND 53-05. 2 L 7 2 4F A6WE 1998041000935 19980410 00935 WP 1998 4 10 VJ9800080 1 19980318 A 5347 ACA74133 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 245 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SEAT TRACK FS 245, BL 44.5R, CORRODED. REPLACED SEAT TRACK SPLICE IAW DC9 SRM 51-30-1, 51-30-2 AND 53-05. 2 L 7 2 4F A6WE 1998041000936 19980410 00936 WP 1998 4 10 VJ9800081 1 19980318 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-230 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SEAT TRACK, FS 200 TO 230, BL 45L, CORRODED. REPLACED SEAT TRACK FROM FS 200 TO 230, BL 45L IAW DC9 SRM 53-05, FIG 4D, 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998041000937 19980410 00937 WP 1998 4 10 VJ9800082 1 19980318 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 168 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR WEB AT FS 168, X54R, Z0, CORRODED. FABRICATED, TREATED AND PRIMED NEW SUB FLOOR IAW DC9 SRM 51-10-2, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998041000938 19980410 00938 WP 1998 4 10 VJ9800083 1 19980318 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR FS 200, X46-53R, CORRODED. FABRICATED, TREATED AND PRIMED NEW SUB FLOOR IAW DC9 SRM 51-10-2, 51-10-3 AND 51-3 0-2. 2 L 7 2 4F A6WE 1998041000939 19980410 00939 WP 1998 4 10 VJ9800085 1 19980318 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR BULGED AT FS 200, X48L, Z=0. REMOVED, TREATED, PRIMED AND INSTALLED SUB FLOOR IAW DC9 SRM 51-10-2, 51-10-3, A ND 51-30-2. 2 L 7 2 4F A6WE 1998041000940 19980410 00940 WP 1998 4 10 VJ9800086 1 19980318 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 160-175 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR FS 160 TO 175, X20L, Z=0, CORRODED. FABRICATED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, 5 1-30-2. 2 L 7 2 4F A6WE 1998041000941 19980410 00941 WP 1998 4 10 VJ9800087 1 19980322 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 160-220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOORBOARD ATTACH ANGLES FS 160 TO 220, BL 55L - BL55R, Z=0, CORRODED BEYOND LIMITS. FABRICATED NEW ANGLES, TREATED, PR IMED AND INSTALLED NEW ANGLES IAW DC9 SRM 51-10-3, 51-30-1, 51-30-2 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1998041000942 19980410 00942 WP 1998 4 10 VJ9800088 1 19980322 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 148-160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR UNDER GALLEY WATER LINE DRAIN FS 148 TO 160, BL 43R-58R, CORRODED BEYOND LIMITS IAW DC9 SRM 53-01, FIG 1. FAB RICATED SUB FLOOR PANEL, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998041000943 19980410 00943 WP 1998 4 10 VJ9800089 1 19980322 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 LOWER LEG OF INTERCOSTAL AT FS 980, L28R, CORRODED. FABRICATED, DRILLED AND INSTALLED NEW INTERCOSTAL IAW DC9 SRM 51-30 -1, 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998041000944 19980410 00944 WP 1998 4 10 VJ9800090 1 19980324 A 5320 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 AFT PIT LOWER DOOR JAMB FRAME PANEL CORRODED BEYOND LIMITS IAW DC9 SRM 53-01 FIG 1 SHEET 3. FABRICATED, TREATED, PRIMED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998041000945 19980410 00945 WP 1998 4 10 VJ9800091 1 19980324 A 5320 991007813 CUSP DOUG DC9 DC932 3022066 WP BS 195 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 CUSP FITTING AT AFT END OF R1 DOOR, FS 195 TO 205, BL 55 TO 61R, CORRODED. REMOVED CORRODED SECTION CUSP FS 165 TO 229, FABRICATED SPLICE DOUBLER AND SPLICED NEW SECTION OF CUSP IAW DC9 SRM 53-05 FIG 55 SHEET 4. 2 L 7 2 4F A6WE 1998041000946 19980410 00946 WP 1998 4 10 VJ9800092 1 19980324 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SKIN UNDER FWD ADF LOOP ANTENNA CORRODED BEYOND LIMITS. REMOVED DAMAGED AREA, FABRICATED FINGER DOUBLER, EXTERNAL DOUBL ER, AND FILLERS IAW EO 12-5311-29B1190. PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3B, 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998041000947 19980410 00947 WP 1998 4 10 VJ9800093 1 19980324 A 5320 PLATE DOUG DC9 DC932 3022066 WP GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 INBOARD SIDE OF LIFE VEST PLATE AT NR 4 GALLEY CORRODED BEYOND LIMIT IAW DC9 SRM 53-01 FIG 1. FABRICATED AND INSTALLED NEW PLATE IAW DC9 SRM 51-10-2 AND 51-30-1. 2 L 7 2 4F A6WE 1998041000948 19980410 00948 WP 1998 4 10 VJ9800094 1 19980324 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 180-183 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR PANEL AT FS 180 TO 183, X32-42R, CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW DC9 SR M 51-10-2, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998041000949 19980410 00949 WP 1998 4 10 VJ9800095 1 19980324 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 190 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 STRESS CRACK CORROSION FOUND AROUND RIVET ON SUB FLOOR AT FS 190, X22R. FABRICATED A NEW PANEL, TREATED, PRIMED AND INS TALLED IAW DC9 SRM 551-10-2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000950 19980410 00950 WP 1998 4 10 VJ9800096 1 19980325 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 220-240 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR UNDER G2 GALLEY CRACKED AND CORRODED STA Y220-240, X47-57. FABRICATED, TREATED AND INSTALLED NEW SECTION IAW DC9 SRM 51-10-2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000951 19980410 00951 WP 1998 4 10 VJ9800097 1 19980325 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT ATTACH ANGLE AT STA Y200, X46-56R, CORRODED. FABRICATED, TREATED AND INSTALLED SUPPORT IAW DC9 SRM 51-10- 2, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998041000952 19980410 00952 WP 1998 4 10 VJ9800098 1 19980325 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR WEBB CORRODED AT STA Y200, X 0-22R, CORRODED. FABRICATED, TREATED, INSTALLED REPLACEMENT IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998041000953 19980410 00953 WP 1998 4 10 VJ9800099 1 19980325 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT STA Y200, X56R, CORRODED. FABRICATED, TREATED AND INSTALLED NEW SECTION IAW DC9 SRM 51-10-1, 51-10-3, 51- 10-4, 51-30-2. 2 L 7 2 4F A6WE 1998041000954 19980410 00954 WP 1998 4 10 VJ9800100 1 19980325 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 200-220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR WEB STA 200 TO 220, X44-54R, CORRODED. FABRICATED, TREATED, AND INSTALLED REPLACEMENT IAW DC9 SRM 51-10-2, 51 -10-3, 51-30-2. 2 L 7 2 4F A6WE 1998041000955 19980410 00955 WP 1998 4 10 VJ9800101 1 19980325 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT ANGLE FS Y220, X0, CORRODED. FABRICATED AND INSTALLED NEW SUPPORT IAW DC9 SRM 51-10-1, 51-10-3, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000956 19980410 00956 WP 1998 4 10 VJ9800102 1 19980302 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT UPPER FLANGE FS Y200-220, X15L, CORRODED. FABRICATED, TREATED, AND INSTALLED NEW SUPPORT IAW DC9 SRM 51-1 0-1, 51-10-3, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000957 19980410 00957 WP 1998 4 10 VJ9800103 1 19980326 A 5320 2931860 FITTING DOUG DC9 DC932 3022066 WP BS 317/325 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 LONGERON 30 SPLICE FITTING FS 317 AND FS 325 CORRODED. REMOVED AND REPLACED FITTING IAW DC9 SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1998041000958 19980410 00958 WP 1998 4 10 VJ9800105 1 19980326 A 5320 5912528501 JAMB DOUG DC9 DC932 3022066 WP BS 900-934 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 AFT CARGO DOOR JAMB BETWEEN FS Y900-934, L28R, CORRODED. LOCATED, DRILLED, TREATED AND INSTALLED NEW SECTION DOOR PAN I AW DC9 SRM 51-30-1, 51-30-2, 53-04, FIG 44, AND 51-10-4. 2 L 7 2 4F A6WE 1998041000959 19980410 00959 WP 1998 4 10 VJ9800106 1 19980326 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 317/325 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 LONGERON 30 UNDER SPLICE FITTING AT FS 317 AND FS 325 CORRODED. REMOVED AND REPLACED IAW DC9 SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1998041000960 19980410 00960 WP 1998 4 10 VJ9800107 1 19980326 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 160-220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FWD LAV SUB FLOOR AT FS 160 TO 220, 55L TO 55R, CORRODED. FABRICATED AND INSTALLED NEW SUB FLOOR IAW DC9 SRM 51-10-2, 5 1-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998041000961 19980410 00961 WP 1998 4 10 VJ9800108 1 19980326 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 CHIPNUT FS 200, BL X0, CORRODED. REMOVED DAMAGED FLOOR SUPPORT, FABRICATED, TREATED AND INSTALLED REPLACEMENT IAW DC9 S RM 51-10-2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000962 19980410 00962 WP 1998 4 10 VJ9800109 1 19980326 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 160-220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR FS 160 TO 220, 55L TO 55R, FWD LAV CORRODED. FABRICATED AND INSTALED NEW SUB FLOOR IAW DC9 SRM 51-10-2, 51-10 -3, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000963 19980410 00963 WP 1998 4 10 VJ9800110 1 19980326 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR WEB SKIN CORRODED FS Y220, X8L. REMOVED, FABRICATED, TREATED AND INSTALLED REPLACEMENT WEB IAW DC9 SRM 51-10- 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000964 19980410 00964 WP 1998 4 10 VJ9800111 1 19980326 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 196 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT UPPER AND LOWER FLANGE FS Y196, X0-44L, CORRODED. REMOVED, FABRICATED, TREATED AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998041000965 19980410 00965 WP 1998 4 10 VJ9800112 1 19980326 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR WEB FS Y200, X0-22L, CORRODED. REMOVED DAMAGED SECTION, FABRICATED, TREATED AND INSTALLED REPLACEMENT IAW DC9 SRM 51-10-2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000966 19980410 00966 WP 1998 4 10 VJ9800113 1 19980326 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR SUPPORT UPPER FLANGE FS Y160-Y200, X0, CORRODED. REMOVED, FABRICATED, TREATED AND INSTALLED REPLACEMENT IAW DC9 S RM 51-10-1, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998041000967 19980410 00967 WP 1998 4 10 VJ9800114 1 19980326 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 119-148 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 SUB FLOOR FS Y119-Y148, X12R-58R, Z=0, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. FABRICATED, TREATED AND INSTALLE D SUB FLOOR IAW DC9 SRM 51-10-2, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998041000968 19980410 00968 WP 1998 4 10 VJ9800115 1 19980407 A 2560 591769637 SLIDE COVER DOUG DC9 DC932 3022066 WP L1 DOOR LOOSE A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 11 916VV 47445 FORWARD ENTRY DOOR SLIDE COVER DISLODGED. RESEATED SLIDE IAW MM 25-60, PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998041000969 19980410 00969 NM 1998 4 10 K3HA980046 1 19980404 A 3350 37067001 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 ON POST FLIGHT, FOUND OVERHEAD EMERGENCY LIGHT DIM. REMOVED AND REPLACED BATTERY'S, OPS CHECK OK REF MM 33-50-77. 2 L 7 3 4F A3WE 1998041000970 19980410 00970 1998 4 10 K3HA980047 4 19980404 A 2564 4600107 LIFE RAFT BOEING 727 727225 1384077 NM CABIN LOW PRESSURE A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 354PA 20624 RIGHT HAND OVERWING LIFE RAFT LOW BOTTLE CHARGE. REMOVED AND REPLACED LIFE RAFT IAW MM 25-60-0. 2 L 7 3 4F A3WE 1998041000971 19980410 00971 WP 1998 4 10 IXXA9800034 1 19980405 A 2121 X207256C FAN DOUG DC8 DC862 3021970 WP E/E COMPT FAILED A IXXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 728PL 1294 45918 ENROUTE, A BURNT ELECTRICAL ODOR WAS SENSED IN THE COCKPIT WITH THE RIGHT RECIRCULATION FAN OPERATING. THE FAN WAS SHUT OFF FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED AND FOUND THE FAN DEFECTIVE. MAINTENANCE DEFERRED THE RIGH T RECIRCULATION FAN. 2 L 7 4 4F 4A25 1998041000972 19980410 00972 WP 1998 4 10 IXXA9800035 1 19980402 A 3260 H146 SWITCH DOUG DC8 DC862 3021970 WP LT MLG DEFECTIVE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 728PL 45918 ENROUTE, GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED WARNING LIGHT ILLUMINATED. THE FLIGHT CREW CYCLED THE GEA R EXTINGUSHING THE WARNING LIGHT. GROUND INSPECTION FOUND THE LEFT MAIN GEAR UPLATCH SWITCH INTERMITTENT AND ELECTRICAL CONNECTOR DAMAGED. MAINTENANCE REPLACED THE SWITCH AND REPAIRED THE CONNECTOR IAW MAINTENANCE MANUAL 32-60-0 AND ACCOM PLISHED A GEAR SWING. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER DISCREPANCIES NOTED. 2 L 7 4 4F 4A25 1998041000973 19980410 00973 NM 1998 4 10 CALA9800637 1 19980407 A 2432 425404 CHARGER BOEING 757 757224 1384958 NM APU INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14115 11324 27557 THE APU LOW OIL QUANTITY LIGHT AND APU DOOR EICAS MESSAGE ACTIVATED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR. M AINTENANCE FOUND THE APU BATTERY CHARGER CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET AND APU DOOR CLOSED. MA INTENANCE CHECKED THE APU OIL QUANTITY AND DOOR OPERATION, BOTH CHECKED GOOD. THE APU BATTERY CHARGER WAS REMOVED AND R EPLACED. THE APU WAS RUN AND OPERATION CHECKED GOOD WITH NO LEAKS NOTED. 2 L 7 2 4F RT A2NM 1998041000974 19980410 00974 NM 1998 4 10 CALA9800638 1 19980407 A 5320 FRAME BOEING 727 727227 1384078 NM L-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 1 INCH CRACK IN LOWER SIDE CORNER OF L-2 DOOR FRAME UPPER HINGE CUTOUT. THE L-2 DOOR FRAME WAS REPLA CED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998041000975 19980410 00975 NM 1998 4 10 CALA9800639 1 19980407 A 5320 DOOR FRAME BOEING 727 727227 1384078 NM C-2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND A 1 INCH CRACK IN FORWARD LOWER EDGE OF C-2 DOOR FRAME. A NEW CORNER WAS INSTALLED ON FORWARD LOWER A REA OF C-2 DOOR IAW SRM 51-30-2 AND 51-10-2. 2 L 7 3 4F A3WE 1998041000976 19980410 00976 NM 1998 4 10 CALA9800640 1 19980407 A 5751 HINGES BOEING 727 727227 1384078 NM LT AILERON DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15774 21242 INSPECTION FOUND LEFT OUTBOARD AILERON HINGES DAMAGED. THE HINGES WERE REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998041000977 19980410 00977 NM 1998 4 10 CALA9800641 1 19980407 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1130-1150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1130 TO 1150, LBL 12. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR S UPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. 2 L 7 3 4F A3WE 1998041000978 19980410 00978 NM 1998 4 10 CALA9800642 1 19980407 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1110-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1110 TO 1130, LBL 12. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-4 AND 51-30-2. 2 L 7 3 4F A3WE 1998041000979 19980410 00979 1998 4 10 9806025647 4 19980311 A 2350 MICROPHONE BOEING 757 757251 1384970 NM LT COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 547US 26494 RADIOS UNUSEABLE WITH CAPTAIN'S MIC SELECTED. AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC ED THE CAPTAIN'S HAND MIC WITH A SERVICEABLE UNIT. 2 L 7 2 4F RT A2NM 1998041000980 19980410 00980 NM 1998 4 10 9806035639 1 19980313 A 2121 6067723 FAN BOEING 757 757251 1384970 NM E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 539US 26486 FLIGHT ATTENDANT REPORTED ELECTRICAL ODOR IN THE FORWARD GALLEY AREA. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT INCIDEN T. MAINTENANCE REPLACED THE RIGHT RECIRCULATION FAN WITH A SERVICEABLE UNIT. 2 L 7 2 4F RT A2NM 1998041000981 19980410 00981 WP 1998 4 10 9806049880 1 19980405 A 3260 PROX SENSOR DOUG DC9 DC951 3022051 WP NLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 675NC 47651 DURING FLIGHT, THE NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED. THE FLIGHT CREW PERFORMED COM PROCEDURES, DIVERTED FLIGH T TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR LOCK SENSOR AND PROXIMITY ELECTRONICS UNIT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041000982 19980410 00982 1998 4 10 9806059155 4 19980406 A 3442 20671570153 TR UNIT DOUG DC9 DC914 3022034 WP E/E COMPT INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8914E 2444 583 45831 DURING CLIMBOUT, THE RADAR SYSTEM WAS UNRELIABLE. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPL ACED THE RADAR TRANSCEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000983 19980410 00983 1998 4 10 9806066719 4 19980406 A 3197 WIRE BOEING 747 747251F 1384898 NM J-BOX 41 FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 619US 21321 DURING TAKEOFF, THE AURAL WARNING HORN SOUNDED. AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. REPAIRED WIRING IN J-BOX 41, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998041000984 19980410 00984 WP 1998 4 10 9806079974 1 19980404 A 5350 TAIL CONE DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY THE TAIL CONE. ALSO, FOUND THE BAY ONET CABLES RUSTY AND THE LATCHES WOULD NOT RETURN TO THE CLOSED POSITION. REPLACED THE CABLES, LUBRICATED THE LATCHES, AND RIGGED THE DEPLOYMENT SYSTEM, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998041000985 19980410 00985 1998 4 10 9806085503 4 19980405 A 3414 4039891903 AIRSPEED IND BOEING 757 757251 1384970 NM LT COCKPIT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 503US 42653 42653 23192 LOST CAPTAIN'S AIRSPEED INDICATION ON TAKEOFF ROLL. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTEN ANCE REPLACED THE CAPTAIN'S AIRSPEED INDICATOR WITH A SERVICEABLE UNIT. 2 L 7 2 4F RT A2NM 1998041000986 19980410 00986 WP 1998 4 10 9806099950 1 19980405 A 2611 SMOKE DETECTOR DOUG DC9 DC932 3022066 WP LAVATORY ACTIVATED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 9346 47376 FORWARD LAVATORY SMOKE DETECTOR ACTIVATED ON APPROACH. FLIGHT CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT IN CIDENT. MAINTENANCE INSPECTED WIRING AND ELECTRICAL SYSTEMS. ALL SYSTEMS CHECKED NORMAL. DISCREPANCY COULD NOT BE DUP LICATED. 2 L 7 2 4F A6WE 1998041000987 19980410 00987 WP 1998 4 10 9806109990 1 19980406 A 3260 PROX SENSOR DOUG DC9 DC931 3022065 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 8950E 47186 DURING APPROACH, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW VERIFIED VISUALLY THROUGH PEEP HOLE THAT GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR PROXIM ITY SENSOR BROKEN. REPLACED SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000988 19980410 00988 WP 1998 4 10 9806119609 1 19980406 A 3260 PROX SENSOR DOUG DC9 DC932 3022066 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 609NW 47234 DURING APPROACH, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. EMERGENCY GEAR EXTENSI ON PROCEDURES WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR PROXIMITY SENSOR BROKEN A T OVERCENTER LINK. REPLACED SENSOR. ALSO, REPLACED MAIN GEAR DOOR SKID PLATES DUE TO DAMAGE INCURRED ON LANDING. 2 L 7 2 4F A6WE 1998041000989 19980410 00989 WP 1998 4 10 9806129986 1 19980406 A 2133 54447222 ACTUATOR DOUG DC9 DC932 3022066 WP OUTFLOW VALVE BINDING A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 986US 50572 39325 47480 LOSS OF CABIN PRESSURIZATION OCCURRED DURING CRUISE FLIGHT AND COULD NOT BE CONTROLLED MANUALLY. CREW ACCOMPLISHED EMER GENCY DESCENT TO 10,000 FEET AND CONTINUED TO DESTINATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OUTFLOW VALVE ACTUATOR BINDING. REPLACED ACTUATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000990 19980410 00990 WP 1998 4 10 9806139102 1 19980407 A 2170 COALESCER BAG DOUG DC9 DC915 3022036 WP CABIN CONTAMINATED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 92S 47064 DURING CLIMBOUT, FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE REAR CABIN. FLIGHT RETURNED TO MSP AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED BOTH NR 1 AND NR 2 WATER SEPARATOR COALESCER BAGS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000991 19980410 00991 1998 4 10 9806149967 4 19980407 A 2565 13621224 SLIDE DOUG DC9 DC931 3022065 WP TAIL CONE LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9331 43994 2000 47263 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EVACUATION SLIDE BOTTLE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998041000992 19980410 00992 WP 1998 4 10 9806159619 1 19980407 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 619NW 47518 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD PASSENGER DOOR EMERGENCY EXIT SIGN INOPERATIVE. CONNECTOR AT LIGHT AS SEMBLY WAS FOUND TO BE DISCONNECTED. REPAIRED AND REASSEMBLED CONNECTOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000993 19980410 00993 WP 1998 4 10 9806169924 1 19980407 A 2910 LINE DOUG DC9 DC932 3022066 WP RT HYD SYST LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 GL 01 926RC 47473 RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO EN ROUTE. CREW DECLARED AN EMERGENCY AND CONTINUED TO DEST INATION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLEX LINE LEAKING AT ELECTRIC PUMP OUTLET. REPLACED LINE , OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998041000994 19980410 00994 1998 4 10 9806179989 4 19980407 A 3442 20671570153 TR UNIT DOUG DC9 DC931 3022065 WP E/E COMPT MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8945E 7351 1 47181 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE D RADAR TRANSCEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041000995 19980410 00995 NM 1998 4 10 SWAA980492 1 19980403 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, RBL 1 TO LBL 1, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998041000996 19980410 00996 NM 1998 4 10 SWAA980493 1 19980403 A 5730 SKIN BOEING 737 7373H4 1384600 NM LT WING GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND LEFT WING FIXED L/E SKIN INTERNAL SURFACE GOUGED AT NR 1 SLAT I/B AUX TRACK CUTOUT. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998041000997 19980410 00997 NM 1998 4 10 SWAA980494 1 19980403 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND A 1 INCH CRACK AT BS 178 BULKHEAD AT WL 187, RBL 1. REPAIRED PER BOEING SRM AND TYPICAL REPAIR T1-353-057. 2 L 7 2 4F RT A16WE 1998041000998 19980410 00998 NM 1998 4 10 SWAA980495 1 19980403 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 948 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND AFT CARGO FLOORBEAM ANGLE CORRODED AT BS 948. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998041000999 19980410 00999 WP 1998 4 10 CKSA98207 1 19980304 A 3231 LOCKS DOUG DC8 DC861 3021952 WP MLG DOOR LACK OF LUBE A CKSA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 812CK 45890 AFTER CLIMB CHECKLIST COMPLETE, DOOR NOT LATCHED LIGHT CAME ON. ALSO, RT DOOR UNSAFE LIGHT ON, ALL ELSE NORMAL. LUBED GEAR DOOR ROLLOVER LOCKS, OPS CHECKS NORMAL PER MM 52-0. 2 L 7 4 4F 4A25 1998041500004 19980415 00004 NE 1998 4 15 98UAL900120 2 19980320 A 7200 ENGINE BOEING 747 747451 1384940 NM PWA 4056 PW4056 NE NR 2 FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 105UA 26473 724382 APPROXIMATELY THREE HOURS AFTER TAKEOFF, NR 2 ENGINE OIL QUANTITY SHOWED 5 QUARTS SLOWLY GOING TO ZERO, 30-45 MINUTES LA TER OIL PRESSURE STARTED DECREASING. ENGINE SHUTDOWN AT 72 PSI OIL PRESSURE. WIND MILLING OIL PRESSURE 6 PSI OIL TEMP 47 DEGREES. 2 L 7 4 4F 4 F RT A20WE E24NE 1998041500005 19980415 00005 NM 1998 4 15 98UAL900123 1 19980326 A 2133 OUT FLOW VALVE BOEING 777 777222 1385219 NM PWA 4084 PW4084 NE CABIN FAILED A UALA B G EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 WP 29 783UA 26950 AT FL350 FLIGHT CREW GOT EICAS MESSAGE: 'FWD OUTFLOW VALVE'. AIRCRAFT DESCENDED DUE CLIMBING CABIN. CREW COULD NOT CON TROL CABIN PRESSURE. CAPTAIN DECLARED AN EMERGENCY AT FL240. FLIGHT CLEARED TO 10,000 FEET. DURING DESCENT, ALL OXYGE N MASKS DEPLOYED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998041500006 19980415 00006 WP 1998 4 15 VJ9800060 1 19980324 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 917VV 47323 EXTERIOR FUSELAGE SKIN AT AFT UPPER ADF ANTENNA CORRODED. BLENDED CORROSION AND REMOVED OUT OF LIMITS AREA. FABRICATED , DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR PARTS AT UPPER FWD AND AFT ADF LOOP ANTENNA IAW DC9 SRM 53-04 , FIG 29, AND AERO EO 98-790. 2 L 7 2 4F A6WE 1998041500007 19980415 00007 SO 1998 4 15 SWIA971112 1 19980330 A 3233 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 237SW 120314 DURING GEAR RETRACTION, AFTER GEAR UP LIGHTS ARE OUT MOMENTARILY, LEFT MAIN INTRANSIT LIGHT CAME BACK ON. CYCLED GEAR A ND ALL STAYED OUT NORMAL. RETURNED TO SLC, REPLACED LEFT MLG ACTUATOR PER MM 32-32-10. CYCLED GEAR AND INDICATION AND OPERATION CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041500008 19980415 00008 NM 1998 4 15 P5CA9800744 1 19980328 A 2780 126344151 FLAP DRIVE BOEING 747 747249F 1384849 NM NR 2 LE FLAP INOPERATIVE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 888KH 21827 NR 2 LT LEADING EDGE FLAP SEGMENT WILL NOT RETRACT PNEUMATICALLY OR ELECTRICALLY. REMOVED AND REPLACED NR 2 LT LEADING EDGE FLAP DRIVE AND OPS CHECK NORMAL PER MM 72-81-07. 2 L 7 4 4F A20WE 1998041500010 19980415 00010 NM 1998 4 15 98FDEA00233 1 19980402 A 3610 AIR SUPPLY DOUG MD11 MD11F 3023600 NM NR 1 ENGINE BROKEN A FDEA A B E UNSCHED LANDING EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 613FE 48749 ON CLIMBOUT, ENG NR 1 FIRE WARNING CAME ON. WARNING WENT OUT UPON ENG SHUTDOWN. RETURNED TO RAMP. FOUND TUBE-RS HP RE COUP AIR SUPPLY WAS BROKEN AND MANIFOLD-HPT ACTIVE CLEARANCE CONTROL WAS CRACKED. ALSO, CLAMP JAW WAS BROKEN. REPLACED ABOVE PARTS AND RAN NR 1 ENG ABOUT 15 MINUTES, FOUND NO FIRE WARNING AND ALL INDICATIONS WERE NORMAL PER MD-11 JRH. FD CU HAD NO CURRENT FAULT AND R-T-S TEST PASSED. 2 L 7 3 4F RT A22WE 1998041500011 19980415 00011 1998 4 15 HEEA0013629 4 19980326 A 2210 7000299908 AUTOPILOT PC700 BOLKMS 117 BK117B1 5626012 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7040U 7180 API WORKS INTERMITTENTLY, SAS/ATT DOES NOT WORK. 1 G 7 2 3U H13EU 1998041500012 19980415 00012 GL 1998 4 15 HEEA0013667 2 19980330 A 7260 23055464 GEARBOX COVER 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL AFT TM BORE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 86CH CAG37520 S557 CAE830990 ENGINE REMOVED DUE TO AFT T/M LEAK. INSPECTION REVEALED: LEAKING AT COVER AFT T/M BORE. 1 G 7 2 3U 3 U H3EU E4CE 1998041500013 19980415 00013 NM 1998 4 15 DL72S980690 1 19980330 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 536DA 22049 FOUND ON D1 LETTER CK, NR 2 L/E FLAP ACTUATOR O/B MOUNT BRACKET CRACKED LOWER RADIUS. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998041500014 19980415 00014 WP 1998 4 15 VJ9800072 1 19980222 A 5347 FLOOR TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 AFT PIT FLOOR TRACK, TOP AND BOTTOM, CORRODED BEYOND LIMITS. REPLACED FLOOR TRACK IAW DC9 SRM 51-10-4 AND 51-30-1. 2 L 7 2 4F A6WE 1998041500015 19980415 00015 WP 1998 4 15 VJ9800084 1 19980318 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR ATTACH UPPER FLANGE FS200, X 0-22R, CORRODED. FABRICATED FLOOR SUPPORT IAW DC9 SRM 51-10-1 AND 51-10-4. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1998041700001 19980417 00001 EU 1998 4 17 HEEA0013650 1 19980326 A 3610 97914211 VALVE BOLKMS 105 BO105S 5626006 EU PNEU SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 VALVE HAS PIECES BROKEN INSIDE. 1 G 7 2 3U H3EU 1998041700002 19980417 00002 SW 1998 4 17 HEEA0013666 1 19980330 A 2430 SM20ACD200A21 RELAY BELL 206 206L3 1182108 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 6 51529 COIL AND CONTACTOR ARE BURNT. COIL IS BURNT. 1 G 7 1 3U H2SW 1998041700003 19980417 00003 SW 1998 4 17 HEEA0013675 1 19980401 A 6500 406040339111 BEARING 406040320101 BELL 407 407 SW T/R ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM AFS755 53060 ROUGH BEARINGS. SERIAL NUMBERS REMOVED ARE C97-1825 AND C97-1883. 1 G 7 1 3U O H2SW 1998041700004 19980417 00004 SW 1998 4 17 HEEA0013676 1 19980401 A 6310 406340102101 CARBON SEAL 406040500123 BELL 407 407 SW FREEWHEEL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 427PH A3392 53059 CARBON SEAL LEAKING. 1 G 7 1 3U O H2SW 1998041700005 19980417 00005 SW 1998 4 17 HEEA0013677 1 19980401 A 6420 407312100101 BEARING 407012101105 BELL 407 407 SW YOKE LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 196 53006 53059 ON POST FLIGHT FOUND CLICKING NOISE EMINATING FROM TRUNNION CLAMP RING AREA. SUSPECT TRUNNION BEARING LOOSE IN YOKE, CA USING NOISE WHEN BLADES ARE FLAPPED. MORE NOTICEABLE AFTER FLIGHT WHEN WARM, NOISE DIMINISHES AS YOKE COOLS. REPAIRED A ND INSPECTED BY OVERHAUL SHOP. 1 G 7 1 3U O H2SW 1998041700006 19980417 00006 SW 1998 4 17 HEEA0013678 1 19980401 A 5210 205030220010 TRACK BELL 412 412 1182202 SW RT DOOR MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 22608 33075 REMOVE AND REPLACE MISMANUFACTURED UPPER R/H DOOR TRACK ON AIRFRAME FWD SECTION. 1 G 7 2 4U H4SW 1998041700007 19980417 00007 EU 1998 4 17 HEEA0013679 1 19980402 A 2435 150SG122Q GENERATOR SNIAS 350 AS350B2 8680813 EU START/GEN NOISY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 381 3004 RADIO INTERFERENCE. INSPECTED BY ACCESSORY OVERHAUL SHOP AND FOUND BRUSHES EXCESSIVELY WORN, COMMUTATOR PITTED AND ARMA TURE IS SHORTED. 1 G 7 1 3U H9EU 1998041700008 19980417 00008 SW 1998 4 17 HEEA0013681 1 19980402 A 7712 212070160007 INDICATOR BELL 212 212 1181420 SW TORQUEMETER STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 31122 INDICATOR NEEDLE STUCK AT ZERO. 1 G 7 1 4U H4SW 1998041700009 19980417 00009 1998 4 17 HEEA0013682 4 19980402 A 3416 212070238003 INDICATOR BELL 412 412 1182202 SW ALTIMETER LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 INDICATOR HAS EXCESSIVE CASE LEAK. 1 G 7 2 4U H4SW 1998041700010 19980417 00010 1998 4 17 HEEA0013683 4 19980402 A 3423 CB212528A COMPASS SKRSKY S76 S76A 8143006 NE COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 COMPASS FLUID LEVEL IS LOW. 1 G 7 2 3U H1NE 1998041700011 19980417 00011 SW 1998 4 17 HEEA0013684 1 19980402 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW ENG TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 ENGINE INPUT BLOWS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1998041700012 19980417 00012 1998 4 17 HEEA0013685 4 19980402 A 3416 59341 ALTIMETER BELL 206 206L1 1182107 SW COCKPIT LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406EH 45183 ALTIMETER LEAKED DURING 12 MONTH INSPECTION. 1 G 7 1 3U H2SW 1998041700013 19980417 00013 EU 1998 4 17 HEEA0013686 1 19980402 A 6520 4638201003 CENTER CASE BOLKMS 105 BO105S 5626006 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 133AE S800 T/R BORE NOZZLE RING SEAT AND SUPPORT PIN SEAT DUE TO WEAR. 1 G 7 2 3U H3EU 1998041700014 19980417 00014 SW 1998 4 17 HEEA0013687 1 19980402 A 2810 206064611001 CELL BELL 206 206L1 1182107 SW FUEL SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 10761 45381 FUEL CELL BLISTERS AND LEAKAGE AS MARKED AND POSSIBLE FUEL SEEPAGE THROUGH FABRIC. 1 G 7 1 3U H2SW 1998041700015 19980417 00015 SW 1998 4 17 HEEA0013688 1 19980402 A 2810 206064611001 CELL BELL 206 206L1 1182107 SW FUEL SYS LEAK E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 FUEL CELL POROUS FABRIC. NEEDS INSIDE COATING DUE TO POSSIBLE PIN HOLE LEAK. 1 G 7 1 3U H2SW 1998041700016 19980417 00016 1998 4 17 HEEA0013689 4 19980402 A 3413 RC30VIL INDICATOR BELL 412 412 1182202 SW RATE OF CLIMB DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 SMALL SCREW LOOSE INSIDE RATE OF CLIMB GAUGE. 1 G 7 2 4U H4SW 1998041700017 19980417 00017 SW 1998 4 17 HEEA0013690 1 19980402 A 7722 212075067105 INDICATOR BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 ITT INDICATOR DOES NOT WORK. 1 G 7 1 4U H4SW 1998041700018 19980417 00018 1998 4 17 HEEA0013691 4 19980402 A 3424 214075244001 GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 TURN NEEDLE DOESN'T WORK. RATE GYRO FAILED 1 G 7 2 4U H4SW 1998041700019 19980417 00019 NE 1998 4 17 HEEA0013692 1 19980402 A 2932 7645001078121 TRANSMITTER SKRSKY S76 S76A 8143006 NE HYD SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 HYD TRANSMITTER OCCASSIONALLY INDICATES MIN. 1 G 7 2 3U H1NE 1998041700020 19980417 00020 SW 1998 4 17 HEEA0013693 1 19980402 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R SERVO LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6610C 14929 51425 M/R SERVO LEAKING. 1 G 7 1 3U H2SW 1998041700021 19980417 00021 SW 1998 4 17 HEEA0013694 1 19980402 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R SERVO LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6610C 18137 51425 M/R SERVO LEAKING. 1 G 7 1 3U H2SW 1998041700022 19980417 00022 SW 1998 4 17 HEEA0013695 1 19980402 A 6730 206076062003 CYLINDER BELL 206 206L3 1182108 SW M/R SERVO LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6610C 16623 51425 M/R SERVO LEAKING. 1 G 7 1 3U H2SW 1998041700023 19980417 00023 SW 1998 4 17 HEEA0013696 1 19980402 A 2840 473203003 SIGNAL COND BELL 412 412 1182202 SW FUEL SYS FAILS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 INTERMITTENTLY NEEDLE GOES TO ZERO. 1 G 7 2 4U H4SW 1998041700024 19980417 00024 SW 1998 4 17 HEEA0013697 1 19980402 A 6710 C4264215 SLIDE AND SLEEVE BELL 206 206L3 1182108 SW M/R CONTROL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 LEAKING INTERNALLY FROM INNER SPOOLS. 1 G 7 1 3U H2SW 1998041700025 19980417 00025 SW 1998 4 17 HEEA0013698 1 19980402 A 2400 214175171103 RELAY BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 DRAW DOWN DURING BATTERY START. 2 G 7 2 4U H10SW 1998041700026 19980417 00026 SW 1998 4 17 HEEA0013699 1 19980402 A 6710 214001970111 ACTUATOR ASSY BELL 214 214ST 1182106 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 ACTUATOR INOPERATIVE. 2 G 7 2 4U H10SW 1998041700027 19980417 00027 SW 1998 4 17 HEEA0013700 1 19980402 A 3340 DK100 BEACON BELL 212 212 1181420 SW STROBE WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1079U 947 31122 BEACON IS WEAK. 1 G 7 1 4U H4SW 1998041700028 19980417 00028 EU 1998 4 17 HEEA0013701 1 19980402 A 3340 A413A POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 POWER SUPPLY INOPERATIVE. 1 G 7 2 3U H3EU 1998041700029 19980417 00029 EU 1998 4 17 HEEA0013702 1 19980402 A 2844 BSE206150G3 TRANSDUCER BOLKMS 105 BO105S 5626006 EU FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911EB S812 TRANSDUCER HIGH OUT OF TOLERANCE THROUGHOUT. 1 G 7 2 3U H3EU 1998041700031 19980417 00031 1998 4 17 HEEA0013705 4 19980402 A 3421 501145301 GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 VERT GYRO WILL NOT SPOOL UP. 1 G 7 2 3U H1NE 1998041700032 19980417 00032 SW 1998 4 17 HEEA0013707 1 19980402 A 2822 164A1681 PUMP BELL 412 412 1182202 SW FUEL BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 BOOST PUMP INOPERATIVE. 1 G 7 2 4U H4SW 1998041700033 19980417 00033 EU 1998 4 17 HEEA0013708 1 19980402 A 7722 10590947 INDICATOR BOLKMS 105 BO105S 5626006 EU TOT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 TOT INDICATOR WILL NOT CALIBRATE AND POINTER NEEDS REFACING. 1 G 7 2 3U H3EU 1998041700034 19980417 00034 1998 4 17 HEEA0013709 4 19980402 A 3421 206075607103 GYRO BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 ATTITUDE GYRO SPINS AND WILL NOT CAGE. 1 G 7 1 3U H2SW 1998041700035 19980417 00035 1998 4 17 HEEA0013710 4 19980402 A 3452 066107100 TRANSPONDER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 TRANSPONDER INOPERATIVE ALSO CAPACITY C507 IS BAD. 1 G 7 2 3U H1NE 1998041700036 19980417 00036 NE 1998 4 17 HEEA0013711 2 19980402 A 7200 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE POWER SECT FAILED E HEEA K NONE R PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 SW 03 3893P 13424 33012 COMPRESSOR STALLS. INSPECT FOR CORROSION ON ACCESSORY GEARBOX. 1 G 7 2 4U 4 U H4SW E22EA 1998041700037 19980417 00037 1998 4 17 HEEA0013712 4 19980402 A 2562 569880101 SWITCH BOLKMS 105 BO105S 5626006 EU ELT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 SWITCH CAUSES ELT TO GO OFF ALL THE TIME. 1 G 7 2 3U H3EU 1998041700038 19980417 00038 SW 1998 4 17 HEEA0013713 1 19980402 A 6330 214031614127 PLATE ASSY BELL 214 214ST 1182106 SW M/R XMSN CRACKED E HEEA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 03 6957Y 28139 PLATE ASSY HAS CRACKED RUBBER CAUSING M/R VIBRATION. 2 G 7 2 4U H10SW 1998041700039 19980417 00039 SW 1998 4 17 HEEA0013714 1 19980402 A 6330 214031614128 PLATE ASSY BELL 214 214ST 1182106 SW M/R XMSN CRACKED E HEEA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 SW 03 6957Y 28139 PLATE ASSY CRACKED RUBBER CAUSING M/R VIBRATION. 2 G 7 2 4U H10SW 1998041700040 19980417 00040 SW 1998 4 17 HEEA0013716 1 19980402 A 6710 206062721113 ACTUATOR BELL 206 206B3 1181506 SW DROOP COMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2275Y 3626 ACTUATOR DOES NOT MOVE WHEN POWER IS APPLIED. 1 G 7 1 3U H2SW 1998041700041 19980417 00041 SW 1998 4 17 HEEA0013717 1 19980402 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8592X 51508 ACTUATOR INOPERATIVE. 1 G 7 1 3U H2SW 1998041700042 19980417 00042 SW 1998 4 17 HEEA0013718 1 19980402 A 2400 M833830207 CIRCUIT BREAKER BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 CIRCUIT BREAKER INOPERATIVE. 2 G 7 2 4U H10SW 1998041700043 19980417 00043 NE 1998 4 17 HEEA0013719 1 19980402 A 2611 30231R7B DETECTOR SKRSKY S76 S76A 8143006 NE SMOKE DET INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 SMOKE DET INTERMITTENT WARNING LIGHTS. 1 G 7 2 3U H1NE 1998041700044 19980417 00044 SW 1998 4 17 HEEA0013720 1 19980402 A 2432 39563001 BATTERY BELL 412 412 1182202 SW STANDBY DC FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 BATTERY UNIT FAILED CAPACITY TEST. 1 G 7 2 4U H4SW 1998041700045 19980417 00045 SW 1998 4 17 HEEA0013721 1 19980402 A 6720 7001483 ROLL CONTROL BELL 412 412 1182202 SW T/R CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA ROLL CONTROL KICKS IN BOTH CHANNEL IN ATT. MODE AND SAS MODE. 1 G 7 2 4U H4SW 1998041700046 19980417 00046 SW 1998 4 17 HEEA0013722 1 19980402 A 2841 393008047 INDICATOR BELL 412 412 1182202 SW FUEL QTY STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA INDICATOR STICKS AT 1000. 1 G 7 2 4U H4SW 1998041700047 19980417 00047 EU 1998 4 17 HEEA0013723 1 19980402 A 6240 10594564 INDICATOR BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 818SH S753 MAST MOMENT INDICATOR INDICATES ZERO. 1 G 7 2 3U H3EU 1998041700048 19980417 00048 EU 1998 4 17 HEEA0013724 1 19980402 A 6240 10594575 TRANSMITTER BOLKMS 105 BO105S 5626006 EU MAST MOMENT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 818SH S753 MAST MOMENT INDICATES ZERO. 1 G 7 2 3U H3EU 1998041700049 19980417 00049 SW 1998 4 17 HEEA0013725 1 19980402 A 2436 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 GENERATOR WOULD NOT COME ON LINE. 1 G 7 2 4U H4SW 1998041700050 19980417 00050 SW 1998 4 17 HEEA0013726 1 19980402 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS NOISY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 450VA INVERTER VERY NOISY. 1 G 7 2 4U H4SW 1998041700051 19980417 00051 EU 1998 4 17 HEEA0013727 1 19980402 A 7714 DL41239 INDICATOR BOLKMS 105 BO105S 5626006 EU SINGLE RPM STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E S806 INDICATOR INTERMITTENTLY STICKS AT ZERO. 1 G 7 2 3U H3EU 1998041700052 19980417 00052 SW 1998 4 17 HEEA0013728 1 19980402 A 7714 206076373001 TACH GEN BELL 206 206L1 1182107 SW SPLINE AREA WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1077A 45382 TACH GEN HAS WORN SPLINE AND CRACKS IN MOUNT PLATE AT BOLT HOLES. 1 G 7 1 3U H2SW 1998041700053 19980417 00053 SW 1998 4 17 HEEA0013729 1 19980402 A 7714 206076373001 TACH GEN BELL 206 206L1 1182107 SW SPLINE AREA WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50046 45173 WORN SPLINE AND CRACKS IN MOUNT PLATE AT BOLT HOLES. 1 G 7 1 3U H2SW 1998041700054 19980417 00054 SW 1998 4 17 HEEA0013730 1 19980402 A 7714 206076373001 TACH GEN BELL 206 206L1 1182107 SW SPLINE AREA WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Y 45192 TACH GEN WORN SPLINE. 1 G 7 1 3U H2SW 1998041700055 19980417 00055 1998 4 17 HEEA0013732 4 19980402 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW ROLL COMMAND STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 ROLL COMMAND BAR STICKS IN CENTER POSITION. 1 G 7 2 4U H4SW 1998041700056 19980417 00056 1998 4 17 HEEA0013733 4 19980402 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW ROLL AXIS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 INDICATOR CHATTER IN ROLL AXIS. 1 G 7 2 4U H4SW 1998041700057 19980417 00057 EU 1998 4 17 HEEA0013734 1 19980402 A 7714 DL41239 INDICATOR BOLKMS 105 BO105S 5626006 EU SINGLE RPM ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5421E S806 ERRATIC ON STARTUP AND SHUTDOWN. 1 G 7 2 3U H3EU 1998041700058 19980417 00058 EU 1998 4 17 HEEA0013735 1 19980402 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 EXH TEMP INDICATOR FAILS CALIBRATION CHECK. 1 G 7 2 3U H3EU 1998041700059 19980417 00059 NE 1998 4 17 HEEA0013736 1 19980402 A 7931 7645001078101 INDICATOR SKRSKY S76 S76A 8143006 NE ENG OIL FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 NEEDLE FLUCTUATES AT 50' INTERMITTENTLY. 1 G 7 2 3U H1NE 1998041700060 19980417 00060 EU 1998 4 17 HEEA0013737 1 19980402 A 7722 50061036 INDICATOR BOLKMS 105 BO105S 5626006 EU EXH TEMP STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB S751 EXH TEMP NEEDLE STICKS ON HIGH SIDE. 1 G 7 2 3U H3EU 1998041700061 19980417 00061 SW 1998 4 17 HEEA0013738 1 19980402 A 2820 2C271 CARTRIDGE BELL 206 206L1 1182107 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2761N 45277 CARTRIDGE INTERMITTENT OPERATION. 1 G 7 1 3U H2SW 1998041700062 19980417 00062 SW 1998 4 17 HEEA0013739 1 19980402 A 3340 A490A POWER SUPPLY BELL 206 206L3 1182108 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 51540 POWER SUPPLY HAS NO OUTPUT. 1 G 7 1 3U H2SW 1998041700063 19980417 00063 1998 4 17 HEEA0013740 4 19980402 A 2562 ELT910 ELT NARCO SKRSKY S76 S76A 8143006 NE COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 ELT TRANSMITS INTERMITTENTLY WHEN OFF ON ARM. 1 G 7 2 3U H1NE 1998041700064 19980417 00064 1998 4 17 HEEA0013741 4 19980402 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 INADVERTENT ACTIVATION FOR UNKNOWN PERIODS OF TIME. 1 G 7 2 3U H3EU 1998041700065 19980417 00065 1998 4 17 HEEA0013742 4 19980402 A 3444 7001840913 TRANSCEIVER SKRSKY S76 S76A 8143006 NE RADAR ALT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 FAILED TEST 1.1 (NOT VALID) 1 G 7 2 3U H1NE 1998041700066 19980417 00066 EU 1998 4 17 HEEA0013743 1 19980402 A 2844 BSE206150G3 TRANSDUCER BOLKMS 105 BO105S 5626006 EU FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 TRANSDUCER READS HIGH OUT OF TOLERANCE. 1 G 7 2 3U H3EU 1998041700067 19980417 00067 1998 4 17 HEEA0013745 4 19980402 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 STARTED TUMBLING IN FLIGHT. 1 G 7 2 3U H1NE 1998041700068 19980417 00068 1998 4 17 HEEA0013746 4 19980402 A 3414 8502CS20LW AIRSPEED IND SKRSKY S76 S76A 8143006 NE COCKPIT CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 AIRSPEED INDICATOR INLET POTS CRACKED. 1 G 7 2 3U H1NE 1998041700069 19980417 00069 1998 4 17 HEEA0013747 4 19980402 A 3414 412075009105 AIRSPEED IND BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 AIRSPEED INDICATOR DOES NOT INDICATE BELOW 25 KNOTS. 1 G 7 2 4U H4SW 1998041700070 19980417 00070 1998 4 17 HEEA0013748 4 19980402 A 3414 412075009105 AIRSPEED IND BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 AIRSPEED INDICATES LOW OUT OF TOLERANCE THROUGHOUT SCALE. 1 G 7 2 4U H4SW 1998041700071 19980417 00071 1998 4 17 HEEA0013749 4 19980402 A 2210 7690001812102 MAGNETIC BRAKE SKRSKY S76 S76A 8143006 NE AUTOFLIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 LATERAL FORCE TRIM INOPERATIVE. 1 G 7 2 3U H1NE 1998041700072 19980417 00072 1998 4 17 HEEA0013750 4 19980402 A 3421 222375033103 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 ATTITUDE INDICATOR EXCESSIVE ROLL IN PITCH ERECTION RATES. 1 G 7 2 4U H4SW 1998041700073 19980417 00073 1998 4 17 HEEA0013751 4 19980402 A 3414 412075009105 AIRSPEED IND BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 AIRSPEED INDICATOR NEEDLE DOES NOT RETURN TO ZERO. 1 G 7 2 4U H4SW 1998041700074 19980417 00074 EU 1998 4 17 HEEA0013752 1 19980402 A 6520 4638201003 CENTER CASE BOLKMS 105 BO105S 5626006 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 T/R BORE WORN AND LOOSE LINERS (3 EACH). 1 G 7 2 3U H3EU 1998041700075 19980417 00075 1998 4 17 HEEA0013753 4 19980402 A 3454 071121701 NAV UNIT KDA692 BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 NAV UNIT DOES NOT DRIVE POINTER. 2 G 7 2 4U H10SW 1998041700076 19980417 00076 SW 1998 4 17 HEEA0013754 1 19980402 A 7714 206062627003 TACH GEN BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 TACH GENERATOR FLUCTUATES 4% TO 10%. 1 G 7 1 3U H2SW 1998041700077 19980417 00077 SW 1998 4 17 HEEA0013755 1 19980402 A 7714 206070266009 INDICATOR BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2272J 3620 INDICATOR INTERMITTENTLY STICKS AT ZERO. 1 G 7 1 3U H2SW 1998041700078 19980417 00078 NE 1998 4 17 HEEA0013756 1 19980402 A 3610 7650007903102 VALVE SKRSKY S76 S76A 8143006 NE BLEED SOV FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 BLEED SOV INOPERATIVE. 1 G 7 2 3U H1NE 1998041700079 19980417 00079 SW 1998 4 17 HEEA0013757 1 19980402 A 2435 23081018 STARTER BELL 407 407 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 403PH 555 53177 STARTER TURNS SLOWLY AND CHATTERS. OVERHAULED BY ACCESSORY OVERHAUL SHOP DUE TO ALL FOUR BOTTOM BRUSH LEADS SEPARATING F ROM BRUSHES, BRUSHES BURNT AND COMMUTATOR WAS SEVERELY PITTED. 1 G 7 1 3U O H2SW 1998041700080 19980417 00080 SW 1998 4 17 HEEA0013758 1 19980402 A 5522 206023119157 ELEVATOR BELL 206 206L1 1182107 SW LT ELEV CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 LT ELEV ASSY CORRODED THROUGH SKIN. 1 G 7 1 3U H2SW 1998041700081 19980417 00081 SW 1998 4 17 HEEA0013759 1 19980402 A 5522 206023119159S SKIN BELL 206 206L1 1182107 SW ELEV CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 ELEV CORRODED THROUGH SKIN. 1 G 7 1 3U H2SW 1998041700082 19980417 00082 EU 1998 4 17 HEEA0013760 1 19980402 A 6320 4638201004 LOWER HOUSING BOLKMS 105 BO105S 5626006 EU M/R XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 M/R GR BOX LOWER HOUSING SEAT WORN, LOOSE INSIDE LINERS. 1 G 7 2 3U H3EU 1998041700083 19980417 00083 1998 4 17 HEEA0013761 4 19980402 A 3422 RCA15BK1 GYRO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2777D 45299 DIR GYRO CAGING SHAFT STICKS. PRECESSES AND GLASS FOGS. 1 G 7 1 3U H2SW 1998041700084 19980417 00084 SW 1998 4 17 HEEA0013762 1 19980402 A 6240 206070265101 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G 45398 INDICATOR ROTOR NEEDLE INOPERATIVE. 1 G 7 1 3U H2SW 1998041700101 19980417 00101 SO 1998 4 17 98ZZZX1453 1 19980301 A 5280 4752932 HINGE 4752930 PIPER PA31 PA31350 7103110 SO LT INB GR DOOR FAILED A JIKA K NONE O OTHER IN INSP/MAINT 1 WP 01 45004 318052163 LEFT MAIN GEAR INBOARD DOOR FORWARD HINGE WAS FOUND BROKEN. SUBMITTER STATED THIS IS THE 8TH FOUND IN RECENT HISTORY. T HIS HINGE IS THE 'NEW STYLE' SPECIFIED IN AD 80-26-05. THIS HINGE NEEDS TO BE RE-DESIGNED TO PREVENT THIS TYPE OF CRACK ING, AND POSSIBLE GEAR FOULING. 1 L 7 2 3O A20SO 1998041700104 19980417 00104 NE 1998 4 17 98ZZZX1455 2 19980307 A 7323 25249994 GOVERNOR BENDIX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE NR 2 ENGINE FAILED A HEEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 108X 1550 A9348 33115 CPPS62029 PILOT EXPERIENCED LOW SIDE GOVERNOR FAILURE SHORTLY AFTER TAKEOFF. RETURNED TO BASE AND LANDED WITHOUT INCIDENT. MAINT ENANCE REPLACED NR 2 ENGINE POWER TURBINE GOVENROR. REF: P&W IPC, CHAPTER 72-10-03, FIG 1, ITEM NR 10. 1 G 7 2 4U 4 U H4SW E22EA 1998041700105 19980417 00105 EU 1998 4 17 MALA976079 1 19980408 A 2910 CAUTION LIGHT SAAB SF340 SF340A 7850100 EU HYD SYST ILLUMINATED A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 107XJ 340A107 ON DESCENT INTO MSP WHEN LOWERING GEAR, THE HYDRAULIC CAUTION LIGHT ILLUMINATED AND NOSE GEAR LIGHT WAS THE ONLY ONE TO ILLUMINATE. HYDRAULIC PUMP WAS SELECTED OFF AND REFERENCE THE QRH, SELECTED OVERRIDE AND EVERYTHING WAS NORMAL. AIRCRA FT LANDED WITHOUT INCIDENT. MAINTENACE PULLED AND RESET AUTO PUMP CIRCUIT BREAKER. AUTO PUMP CONTROL SYSTEM, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998041700106 19980417 00106 EU 1998 4 17 MALA976080 1 19980408 A 3350 AML9ILA85 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 31XJ 031 DURING INSPECTION, THE EMERGENCY BUTTON ON FLIGHT ATTENDANTS PANEL INOP. MAINTNENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998041700107 19980417 00107 EU 1998 4 17 MALA976081 1 19980405 A 3350 60207 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, EMERGENCY EXIT LIGHT 1D INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998041700108 19980417 00108 EU 1998 4 17 MALA976082 1 19980405 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 423XJ 423 DURING INSPECTION, EMERGENCY LIGHT INOP AT 6A. MAINTENANCE RESECURED LIGHT STRIP CONNECTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998041700109 19980417 00109 EU 1998 4 17 MALA976083 1 19980403 A 3350 3071BPEGPL BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 99XJ 099 DURING INSPECTION, 6D EXIT LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998041700110 19980417 00110 NM 1998 4 17 MALA976084 1 19980403 A 3350 MS25231316 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DURING INSPECTION, EMERGENCY LIGHT 1E INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998041700111 19980417 00111 EU 1998 4 17 MALA976085 1 19980406 A 3350 MS1557081 BULB SAAB SF340 340B 7860101 EU FUSELAGE FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 430XJ 430 DURING INSPECTION, THE LEFT EXTERNAL EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998041700112 19980417 00112 NM 1998 4 17 MALA976086 1 19980405 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 846MA 344 DURING INSPECTION, EMERGENCY EXIT DOOR ROW 4 SEAT A AND B NEEDS TO BE RESECURED. MAINTENACE RESECURED LIGHT. ALL CHECK S GOOD. 2 H 7 2 4T RT A13NM 1998041700113 19980417 00113 EU 1998 4 17 MALA976087 1 19980402 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG IND LOOSE A MALA O OTHER N FALSE WARNING DE DESCENT 1 GL 15 426XJ 426 INBOUND TO DTW PUT GEAR DOWN, NO LEFT HAND LANDING GEAR INDICATION. MAINTENANCE RESECURED LOOSE CANNON PLUG IN LEFT GEAR WHEEL WELL. ALL INDICATIONS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 1998041700114 19980417 00114 EU 1998 4 17 MALA976088 1 19980405 A 5347 7553799387 SEAT TRACK SAAB SF340 SF340A 7850100 EU CABIN CORRODED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 98XJ 098 DURING HEAVY CHECK, CENTER SEAT TRACK BETWEEN STA 297-378 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED DAMA GED SEAT TRACK BETWEE STA 297-378 IAW SAAB 340 SRM 53-70-60. 2 L 7 2 4T RT A52EU 1998041700115 19980417 00115 NM 1998 4 17 AWXA9800082 1 19980318 A 3350 S106 BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 150AW 23218 CABIN OVERWING EMERGENCY EXIT SIGN FAILS 4 MIN, BATTERY OPS CHECK. REMOVED AND REPLACED CABIN OVERWING EMERGENCY EXIT S IGN BATTERY, SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 1998041700116 19980417 00116 NM 1998 4 17 AWXA9800083 1 19980320 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 EXIT LIGHTS FLICKER ON/OFF LT ROW 1-4. REMOVED AND REPLACED BATTERY CARTRIDGE ASSY, DUE TO PWR SUPPLY CHANGE. TEST OK. 2 L 7 2 4F RT A16WE 1998041700117 19980417 00117 NM 1998 4 17 AWXA9800084 1 19980320 A 3350 900542 POWER SUPPLY BOEING 737 737277 1384570 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 EMERG EXIT LIGHTS IN FIRST CLASS ILLUMINATE INTERMIT. REMOVED AND REPLACED ROW NR 3 BATTERY SUPPLY. OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1998041700118 19980417 00118 NM 1998 4 17 AWXA9800085 1 19980321 A 3350 849029 BATTERY BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 DURING ROUTINE MAINTENANCE CHECK, FOUND BULLNOSE EMERGENCY LIGHTS AT 3L, 4L AND 7L INOP. CHARGED EMERGENCY LIGHT BATTER Y. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998041700119 19980417 00119 EU 1998 4 17 AWXA9800087 1 19980322 A 5347 ASNA2223 FLOOR TRACK AIRBUS 320 A320231 3930325 EU BS 800 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 646AW 271 DURING SCHEDULED C-5 INSPECTION, FOUND NR 4 TRACK CORRODED STATION 800. TRACK REPLACED AS PER SRM 53-11-15, PAGE 217 AN D 218. 2 L 7 2 4F RT A28NM 1998041700120 19980417 00120 NM 1998 4 17 AWXA9800090 1 19980403 A 7110 1731010513 COWLING BOEING 737 737277 1384570 NM LT ENGINE FELL OFF A A AWXA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 WP 28 189AW 22656 LEFT ENGINE COWLING FELL OFF AFTER TAKOFF. RENISTALLED COWLS PER R5M78001 AND THRUST REVERSER ASSY. 2 L 7 2 4F RT A16WE 1998041700121 19980417 00121 EU 1998 4 17 AWXA9800091 1 19980324 A 5347 ASNA2223 FLOOR TRACK AIRBUS 320 A320231 3930325 EU BS 800 CORRODED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 631AW 077 NR 4 FLOOR TRACK, STATION 800, AT FRAME 20 CORRODED NR 4 FLOOR TRACK, STATION 800, AT FRAME 20 CORRODED. REPAIRED PER S RM 53-00-15, FIG 201 PG 204 NR 4 FLOOR TRACK, STATION 800, AT FRAME 20 CORRODED, REPAIRED PER SRM 53-00-15, FIG 201 PG. 204. 2 L 7 2 4F RT A28NM 1998041700122 19980417 00122 WP 1998 4 17 9806189878 1 19980408 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5 THROUGH 9. MAINTENANCE REPLACED BATTERIES IN BATTERY PACK B5-40. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041700123 19980417 00123 WP 1998 4 17 9806199921 1 19980408 A 3260 PROX SENSOR DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 943N 47647 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW VERIFIED VISUALLY THROUGH PEEP HOLE THAT GEAR WA S DOWN AND LOCKED. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR PROXIMITY SE NSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998041700124 19980417 00124 WP 1998 4 17 9806209614 1 19980408 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 614NW 47128 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700125 19980417 00125 WP 1998 4 17 9806219931 1 19980408 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 90S 47244 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIE S. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700126 19980417 00126 WP 1998 4 17 9806229942 1 19980407 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 3991C 47175 FLIGHT ATTENDANT REPORTED FORWARD FLASHLIGHT INDICATOR NOT FLASHING. REPLACED BATTERY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700127 19980417 00127 SO 1998 4 17 COMA9810085 1 19980406 A 5320 12034416001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 196CA 120196 CREW PREFLIGHT INSPECTION FOUND ONE RIVET HEAD BROKEN OFF IN FUSELAGE SKIN, LEFT HAND SIDE, FRAME NR 9, JUST BELOW CAPTA IN'S DV WINDOW. FURTHER INVESTIGATION REVEALED A CRACKED SKIN SUPPORT AT THAT LOCATION. THE SUPPORT WAS REPLACED PER A ERODESIGN REPORT NR 660-1, IR, 2-16-93. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1998041700128 19980417 00128 SO 1998 4 17 COMA9810086 1 19980407 A 3020 CONNECTOR EMB 120 EMB120RT SO RT ENGINE CORRODED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 189CA 120189 RIGHT ENGINE INLET ANTI-ICE SYSTEM FAILED. REPAIRED CORROSION ON WIRING CONNECTIONS AT THE EJECTOR FLOW VALVE. 2 L 7 2 4T RT A31SO 1998041700129 19980417 00129 SO 1998 4 17 COMA9810087 1 19980408 A 5270 SWITCH EMB 120 EMB120RT SO RT FUEL DOOR OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 261CA 120254 SERVICE DOOR WARNING CAME ON DURING TAKEOFF. ADJUSTED MICROSWITCHES AT THE FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998041700130 19980417 00130 EA 1998 4 17 COMA980074 1 19980408 A 8012 8989308 START VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 979CA 1733 7159 RIGHT ENGINE START MESSAGE CAME ON AFTER TAKEOFF. REPLACED THE ENGINE AIR START VALVE. 2 L 7 2 4F RT A21EA 1998041700131 19980417 00131 NM 1998 4 17 UPS98226340 1 19980402 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 657 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:C CORROSION ON SEAT TRACK BS 657. REMOVED AND REPLACED TRACK PER SRM 53-10-5. 2 L 7 3 4F A3WE 1998041700132 19980417 00132 NM 1998 4 17 UPS98226341 1 19980402 A 5347 SEAT TRACK BOEING 727 72725C 138400H NM BS 657-662/720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE:C CORROSION (C53-224-03.00-01) ON SEAT TRACK BS 657 TO BS 662 AND AT BS 720 LBL 65 WL 208. CORROSION RE MOVAL OUT OF LIMITS PER SRM 53-10-1. REMOVED AND REPLACED SECTION OF SEAT TRACK THAT ENCOMPASSES BS 657 TO BS 720 IAW S RM 53-10-5. 2 L 7 3 4F A3WE 1998041700133 19980417 00133 NM 1998 4 17 UPS98226342 1 19980409 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 FOWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY OPS IS INTERMINT AND BACK COVER IS MISSING. REMOVED AND REPLACED FWD ENTRY DOOR EMERG EXIT LIGHT ASSY PER M/M 33-50-01. OPS CHECK GOOD. OK FOR SERVICE. P/N : 10-0067-9,S/N OFF UNKNOWN S/N :ON 1 3697. 2 L 7 3 4F A3WE 1998041700134 19980417 00134 NM 1998 4 17 UPS98226343 1 19980409 A 3350 BULB BOEING 727 72721C 138400M NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 934UP 19135 CABIN ENTRY DOOR EMERGENCY EXIT 1 LIGHT INOP. RELAMPED, GROUND CHECKS OK. 2 L 7 3 4F A3WE 1998041700135 19980417 00135 WP 1998 4 17 UPS98826331 1 19980328 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP WS 539.635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C RT WING L/E AT STA XFS.539.635, DIRECTLY ABOVE NR 3PYLON, THE WING DOUBLER PLATE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER AND INTERNAL DOUBLER IAW SRM 57-2-1A FIG 1. 2 L 7 4 4F RT 4A25 1998041700136 19980417 00136 WP 1998 4 17 UPS98826332 1 19980402 A 5720 576954541 DOUBLER DOUG DC8 DC873F 302199F WP WS 850 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C LT O/B L/E SECTION O/B END, THE EXTERIOR L/E SKIN IS CKACKED AND THE INTERNAL, DOUBLER/STRAP IS ALSO C RACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER AND REPAIRED SKIN IAW SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7. 2 L 7 4 4F RT 4A25 1998041700137 19980417 00137 WP 1998 4 17 UPS98826333 1 19980329 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C STA 460 FRAME AT STR 36 FWD SIDE OF FRAME IS CORRODED JUST BELOW FLOORBOARD SUPPORT. REPAIRED AREA IA W SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998041700138 19980417 00138 WP 1998 4 17 UPS98826334 1 19980329 A 5320 37558242 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C SHEAR TIE FITTING AT STA 280 STRINGERS 33R AND 34R IS CORRODED. REMOVED, FABRICATED AND INSTALLED REP LACEMENT FITTING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1998041700139 19980417 00139 WP 1998 4 17 UPS98826335 1 19980325 A 5320 5649982 CLIP DOUG DC8 DC873F 302199F WP BS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C STA 55.00 AT STR 31R, THE SHEAR CLIP IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 53-3-1 FIG 3. 2 L 7 4 4F RT 4A25 1998041700140 19980417 00140 WP 1998 4 17 UPS98826336 1 19980327 A 5320 5649982 CLIP DOUG DC8 DC873F 302199F WP BS 25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C STA 25 AT STR 31R, THE SHEAR CLIP IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 53-3-1 FIG 3. 2 L 7 4 4F RT 4A25 1998041700141 19980417 00141 WP 1998 4 17 UPS98826337 1 19980325 A 5320 56499982 CLIP DOUG DC8 DC873F 302199F WP BS 35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C STA 35 AT STR 31R, THE SHEAR TIE FITTING IS CORRODED. REMOVED, FABRICATED INSTALLED REPLACEMENT FITTI NG IAW SRM 53-3-1 FIG 3. 2 L 7 4 4F RT 4A25 1998041700142 19980417 00142 WP 1998 4 17 UPS98826338 1 19980329 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 704 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C LOWER EXTERIOR FUSELAGE AT STA 704 LBL6 FRAME ANGLE IS CRACKED. REPAIRED AREA IAW DWG 5750365 AND SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1998041700143 19980417 00143 WP 1998 4 17 UPS98826344 1 19980401 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 672.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C RT WING L/E O/B NR 4 ENG RIB IS CRACKED AT STA XFS.672.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 5 7-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998041700144 19980417 00144 WP 1998 4 17 UPS98826345 1 19980401 A 5320 564932963 TIE CLIP DOUG DC8 DC873F 302199F WP BS 1725 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C STA 1725, BETWEEN STR 32R-33R, INTERCOSTAL FRAME TIE CLIP IS CRACKED. REMOVED, FABRICATED AND INSTALL ED REPLACEMENT CLIP IAW DWG 5649329 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041700145 19980417 00145 WP 1998 4 17 UPS98826346 1 19980331 A 5320 37799781 FITTING DOUG DC8 DC873F 302199F WP BS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C MAIN CABIN AT STA 700, STR 13L, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DW G 3779978 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041700146 19980417 00146 WP 1998 4 17 UPS98826347 1 19980331 A 5320 37799781 FITTING DOUG DC8 DC873F 302199F WP BS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C MAIN CABIN AT STA 700, STR 18R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DW G 3779978 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041700147 19980417 00147 WP 1998 4 17 UPS98826348 1 19980401 A 5712 RIB DOUG DC8 DC873F 302199F WP BS 347.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS 347.750. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998041700148 19980417 00148 WP 1998 4 17 UPS98826349 1 19980326 A 5730 SKIN DOUG DC8 DC873F 302199F WP BS 282.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C RT WING L/E SKIN ON TOP AT STA XFS 282.500 HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED AREA IAW S RM 57-3-0. 2 L 7 4 4F RT 4A25 1998041700149 19980417 00149 WP 1998 4 17 UPS98826350 1 19980401 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 497.491 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS 497.491. STOP DRILLED CRACK AND R EPAIRED IAW SRR57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998041700150 19980417 00150 WP 1998 4 17 UPS98826351 1 19980326 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 250.089 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C LT WING LWR SURFACE OF I/B STUB WING HAS HEAVY CORROSION AROUND FASTENER XS 250.089. REPAIRED AREA IA W SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998041700151 19980417 00151 WP 1998 4 17 UPS98826352 1 19980403 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 227.333 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C LT WING L/E SKIN AS STA XS 227.333 ON TOP HAS HEAVY CORROSION AROUND FASTENER HOLE. REPAIRED AREA IAW SRM 57-3-3 AND ADD 5720-7767. 2 L 7 4 4F RT 4A25 1998041700152 19980417 00152 NM 1998 4 17 98FDEA00258 1 19980407 A 5320 SPLICE BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR 0789 70C079-00, BS 720D - 720E, STR 21R IN SNAKE PIT AREA CORRODED. CUTOUT CORRODED AREA AND INSTALLED STR SPLICE PE R SRM 53-10-3, PAGE 3. 2 L 7 3 4F RT A3WE 1998041700153 19980417 00153 NM 1998 4 17 98FDEA00259 1 19980403 A 5320 SPLICE BOEING 727 727227 1384078 NM BS 680-686 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 483FE 21465 FWD CARGO STRINGER 27LT, BS 680 PLUS 6, LEVELING COMPOUND CRACKED AND LIFTED AT STRINGER SPLICE. REMOVED LEVELING COMPO UND, FOUND CORROSION. REMOVED CORROSION BY CUTTING OUT DAMAGED SECTION. INSTALLED STRINGER SPLICE PER SRM 53-10-3 PAGE 4A, FIG 1, TABLE II AND SRM 53-10-3 PAG 4B. 2 L 7 3 4F A3WE 1998041700154 19980417 00154 NM 1998 4 17 98FDEA00260 1 19980403 A 5311 BELL FRAME BOEING 727 727227 1384078 NM BS 660 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 483FE 21465 NR 0867 FWD CARGO BS 660 BELL FRAME IS DAMAGED ABOVE STRINGER 24 LT. REMOVED DAMAGED AREA, INSTALLED DOUBLER ON BELL FR AME PER SRM 51-40-3. SPLICE INSTALLED AT STRINGER 25 PER EA NR75310-29332. 2 L 7 3 4F A3WE 1998041700155 19980417 00155 WP 1998 4 17 ABXA9800324 1 19980408 A 5610 TRIM DOUG DOUG DC9 DC933F 302207A WP COCKPIT OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. REPOSITIONED WINDOW TRIM. 2 L 7 2 4F A6WE 1998041700156 19980417 00156 WP 1998 4 17 ABXA9800325 1 19980407 A 3260 7000010101 UPLATCH SWITCH DOUG DC8 DC863 302198A WP LT MLG DOOR DEFECTIVE A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 815AX 46097 GEAR UNSAFE LIGHT ILLUMINATED DURING GEAR UPLATCH CHECK. LEFT LANDING GEAR DOOR INDICATED UNLATCHED ON FLIGHT ENGINEERS PANEL. RECYCLED GEAR, SAME RESULT. *S/D* REPLACED LEFT MAIN LANDING GEAR UPLATCH SWITCH IAW DC8 MM 32-60-00, OPS CHE CKED GOOD. 2 L 7 4 4F 4A25 1998041700157 19980417 00157 WP 1998 4 17 ABXA9800326 1 19980406 A 3260 7000010101 SWITCH DOUG DC9 DC933F 302207A WP LT MLG DOOR DEFECTIVE A ABXA O OTHER N FALSE WARNING UK UNKNOWN 1 GL 23 930AX 47363 GEAR DOOR OPEN LIGHT ILLUMINATED DURING UPLATCH CHECK. RECYCLED GEAR, LIGHT EXTINGUISHED. UPLATCH CHECK OK. REPLACED THE LEFT MAIN LANDING GEAR DOOR POSITION SWITCH. 2 L 7 2 4F A6WE 1998041700158 19980417 00158 WP 1998 4 17 MWEA98394 1 19980331 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 786 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FOUND CRACK ON LONGERON 17R AT STATION 786 ATTACH BOLTS. MAINTENANCE REMOVED LONGERON SECTION FABRICATED AND INSTALLED NEW SECTION. 2 L 7 2 4F A6WE 1998041700159 19980417 00159 NM 1998 4 17 VNAA9804005 1 19980405 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 436JS 3052 DURING THE PREFLIGHT INSPECTION, A SECTION OF EMERGENCY LIGHTS WAS NOTES TO BE INOPERATIVE. MAINTENANCE INSPECTED AND R EPLACED THE 6LK EMERGENCY BATTERY PACK, IN ACCORDANCE WITH DORNER MM 33-51-01. OPERATIONAL CHECKS WERE COMPLETED AND TH E ACFT RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 1998041700160 19980417 00160 SW 1998 4 17 HEEA0013464 1 19980319 A 6340 214074280107 DETECTOR BELL 412 412 1182202 SW RPM LIMIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 RPM LIMIT DETECTOR FAILED. CYCLE COUNTER TIME STAYS ON AT ALL TIMES. 1 G 7 2 4U H4SW 1998041700161 19980417 00161 SW 1998 4 17 HEEA0013527 1 19980326 A 5320 212030155001 BOLT ASSY BELL 212 212 1181420 SW LIFT LINK FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27805 1692 31106 ON POSTFLIGHT INSPECTION FOUND HEAD END OF LOWER LIFT LINK BOLT LYING IN THE BOTTOM OF THE SERVO COMPARTMENT. BOLT FAIL ED 1 AND 5/8" FROM THE END. THE THREADED END OF THE BOLT REMAINED ENGAGED IN THE LIFT LINK. REPLACED WITH SERVICEABLE B OLT. 1 G 7 1 4U H4SW 1998041700162 19980417 00162 SW 1998 4 17 HEEA0013570 1 19980326 A 6340 214074280107 DETECTOR BELL 412 412 1182202 SW RPM LIMIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 LIGHTS INTERMITTENT FLASHING. 1 G 7 2 4U H4SW 1998041700163 19980417 00163 SW 1998 4 17 HEEA0013581 1 19980326 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11027 45411 CAUSES STARTER TO RUN AFTER SHUTDOWN. 1 G 7 1 3U H2SW 1998041700164 19980417 00164 NE 1998 4 17 HEEA0013614 2 19980326 A 7210 9560137520 MAGNETIC SEAL SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4034Q 2918 MAGNETIC LEAKING. 1 G 7 1 3U 3 U H9EU E19EU 1998041700165 19980417 00165 SW 1998 4 17 HEEA0013715 1 19980402 A 6710 206062721109 ACTUATOR BELL 206 206L4 1182110 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7077F 52038 INOPERATIVE. 1 G 7 1 3U NC H2SW 1998041700166 19980417 00166 SW 1998 4 17 HEEA0013763 1 19980402 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 450VA ALTERNATER CAUSES CYCLIC TO BECOME ERRATIC. 1 G 7 2 4U H4SW 1998041700167 19980417 00167 1998 4 17 HEEA0013764 4 19980402 A 3424 206070274005 INDICATOR BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 INDICATOR STAYS 1/2 BALL OFF. 1 G 7 1 3U H2SW 1998041700168 19980417 00168 SW 1998 4 17 HEEA0013765 1 19980402 A 7332 206075676003 INDICATOR BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL DUAL FUEL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2250U 45754 FUEL PRESSURE INDICATOR READS LOW. 1 G 7 1 3U 3 U H2SW E1GL 1998041700169 19980417 00169 SW 1998 4 17 HEEA0013766 1 19980402 A 7931 206075677103 INDICATOR BELL 206 206L3 1182108 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54641 51184 PSI HIGH ON UPPER SCALE. 1 G 7 1 3U H2SW 1998041700170 19980417 00170 SW 1998 4 17 HEEA0013767 1 19980402 A 7714 206070265011 INDICATOR BELL 206 206L1 1182107 SW DUAL TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G 45398 TURBINE NEEDLE HAS STICKY OPERATION. 1 G 7 1 3U H2SW 1998041700171 19980417 00171 SW 1998 4 17 HEEA0013768 1 19980402 A 7714 206075682107 INDICATOR BELL 206 206L3 1182108 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251Y 51556 GAS PRODUCER INDICATOR NEEDLE STICKS AND DOES NOT INDICATE 10%. 1 G 7 1 3U H2SW 1998041700172 19980417 00172 SW 1998 4 17 HEEA0013769 1 19980402 A 2822 164A199 BOOST PUMP BELL 206 206L1 1182107 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5017G 45228 RH BOOST PUMP QUITS AFTER 10 MINUTES OF OPERATION. 1 G 7 1 3U H2SW 1998041700173 19980417 00173 SW 1998 4 17 HEEA0013770 1 19980402 A 2822 164A199 BOOST PUMP BELL 206 206L1 1182107 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10778 45391 FUEL BOOST PUMP RPM MOTOR WILL NOT RUN. 1 G 7 1 3U H2SW 1998041700174 19980417 00174 SW 1998 4 17 HEEA0013771 1 19980402 A 3340 A490A POWER SUPPLY BELL 206 206L3 1182108 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 363BH 51345 STROBE LIGHT INOPERATIVE. 1 G 7 1 3U H2SW 1998041700175 19980417 00175 1998 4 17 HEEA0013772 4 19980402 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE NR 1 PITCH MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5426U 760167 NR 1 PITCH KICKS IN LEVEL FLIGHT. 1 G 7 2 3U H1NE 1998041700176 19980417 00176 1998 4 17 HEEA0013773 4 19980402 A 3416 59341 ALTIMETER BELL 206 206L1 1182107 SW COCKPIT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3892R 45594 ALTIMETER LEAKING AT KNOB. 1 G 7 1 3U H2SW 1998041700177 19980417 00177 1998 4 17 HEEA0013774 4 19980402 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW AUTO FLIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 TARSYN WILL NOT SLAVE TO CONVERT HEADINGS. 1 G 7 2 4U H4SW 1998041700179 19980417 00179 EU 1998 4 17 HEEA0013776 1 19980402 A 3213 10550103 SKID BOLKMS 105 BO105S 5626006 EU END CAP CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 CORROSION PITS INSIDE OF TUBE AT FWD. END CAP. 1 G 7 2 3U H3EU 1998041700180 19980417 00180 SW 1998 4 17 HEEA0013777 1 19980402 A 7714 214175251103 INDICATOR BELL 214 214ST 1182106 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 TRIPLE TACH INDICATOR INTERMITTENT. 2 G 7 2 4U H10SW 1998041700181 19980417 00181 SW 1998 4 17 HEEA0013778 1 19980402 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2758N 45267 ACTUATOR INOPERATIVE. 1 G 7 1 3U H2SW 1998041700182 19980417 00182 SW 1998 4 17 HEEA0013779 1 19980402 A 6240 206076373001 TACH GENERATOR BELL 206 206L3 1182108 SW ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 205FC 51130 TACH GENERATOR FAILED. NO ROTOR INDICATION. 1 G 7 1 3U H2SW 1998041700183 19980417 00183 SW 1998 4 17 HEEA0013785 1 19980402 A 2842 391046200 PROBE BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 FUEL QTY PROBE INACCURATE READINGS. 1 G 7 2 4U H4SW 1998041700184 19980417 00184 SW 1998 4 17 HEEA0013786 1 19980402 A 3340 A490ATSDF1428 POWER SUPPLY BELL 206 206L3 1182108 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 STROBE POWER SUPPLY INOPERATIVE. 1 G 7 1 3U H2SW 1998041700185 19980417 00185 EU 1998 4 17 HEEA0013787 1 19980402 A 3340 A413AHDADF28V POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K S859 STROBE POWER SUPPLY INOPERATIVE. 1 G 7 2 3U H3EU 1998041700186 19980417 00186 SW 1998 4 17 HEEA0013788 1 19980402 A 3340 A490ATSDF1428 POWER SUPPLY BELL 206 206L3 1182108 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116P 51530 STROBE POWER SUPPLY INOPERATIVE. 1 G 7 1 3U H2SW 1998041700187 19980417 00187 SW 1998 4 17 HEEA0013789 1 19980402 A 7921 209062501005 OIL COOLER BELL 412 412 1182202 SW ENG OIL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2298Z 33077 UNIT IS LEAKING. 1 G 7 2 4U H4SW 1998041700188 19980417 00188 SW 1998 4 17 HEEA0013790 1 19980402 A 6220 212030437007 CAP ASSY BELL 212 212 1181420 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3131S 30953 RUBBER CUSHION WORN AND CRACKED. 1 G 7 1 4U H4SW 1998041700189 19980417 00189 SW 1998 4 17 HEEA0013791 1 19980402 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5014V 45217 ACTUATOR INOPERATIVE. 1 G 7 1 3U H2SW 1998041700190 19980417 00190 1998 4 17 HEEA0013792 2 19980402 A 7412 103815501 EXCITER BELL 412 412 1182202 SW ENG ING FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 EXCITER INTERMITTENT. CAUSED ENGINE TO FLAME OUT AT START, 40 N1. 1 G 7 2 4U H4SW 1998041700191 19980417 00191 SW 1998 4 17 HEEA0013793 1 19980402 A 6340 214074280107 DETECTOR BELL 412 412 1182202 SW RPM LIMIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 RPM AUDIO INOPERATIVE CAUSES CYCLIC CENTER LIGHT TO COME ON. 1 G 7 2 4U H4SW 1998041700192 19980417 00192 SW 1998 4 17 HEEA0013794 1 19980402 A 2842 214066212105 PROBE BELL 214 214ST 1182106 SW FUEL SYS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59805 28141 PROBE WILL NOT TEST. 2 G 7 2 4U H10SW 1998041700193 19980417 00193 SW 1998 4 17 HEEA0013795 1 19980402 A 3040 214075186001 CONTROL UNIT BELL 214 214ST 1182106 SW WINDSHIELD FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 WINDSHIELD HEAT INOPERATIVE; DOES NOT COME ON. 2 G 7 2 4U H10SW 1998041700194 19980417 00194 SW 1998 4 17 HEEA0013797 1 19980402 A 6320 206040190005 PUMP BELL 206 206L1 1182107 SW M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5000K 45167 SHAFT BUSHING WORN. 1 G 7 1 3U H2SW 1998041700195 19980417 00195 SW 1998 4 17 HEEA0013798 1 19980402 A 6320 206040190005 PUMP BELL 206 206L1 1182107 SW GEAR BOX OIL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 SHAFT BUSHING WORN. 1 G 7 1 3U H2SW 1998041700196 19980417 00196 SW 1998 4 17 HEEA0013799 1 19980402 A 6230 412040101127 MAST ASSY BELL 412 412 1182202 SW M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 3091 33112 3100 HOUR INSPECTION. UNBONDED WEAR SLEEVE AND INSPECT T/D CORROSION ON UPPER MAST. 1 G 7 2 4U H4SW 1998041700197 19980417 00197 1998 4 17 HEEA0013800 4 19980402 A 2210 4025008918 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 COMPUTER AFCS WILL NOT TEST PROPERLY. 1 G 7 2 4U H4SW 1998041700198 19980417 00198 SW 1998 4 17 HEEA0013801 1 19980402 A 7931 209070262101 INDICATOR BELL 412 412 1182202 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 OIL TEMP/PRESS INDICATOR FAILED. 1 G 7 2 4U H4SW 1998041700199 19980417 00199 SW 1998 4 17 HEEA0013802 1 19980402 A 7931 209070262101 INDICATOR BELL 412 412 1182202 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 OIL PRESSURE IS HIGH. 1 G 7 2 4U H4SW 1998041700202 19980417 00202 SW 1998 4 17 HEEA0013805 1 19980402 A 6240 206075681105 INDICATOR BELL 206 206L3 1182108 SW DUAL TACH FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108PH 51334 DUAL TACH N2 NEEDLE FLUCTUATES. 1 G 7 1 3U H2SW 1998041700203 19980417 00203 SW 1998 4 17 HEEA0013806 1 19980402 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 450VA INVERTER CAUSES FUEL GAUGE TO FLUCTUATE. 1 G 7 2 4U H4SW 1998041700204 19980417 00204 NE 1998 4 17 HEEA0013807 1 19980402 A 6220 7610608000049 DAMPER SKRSKY S76 S76A 8143006 NE M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1546G 760076 DAMPER IS WEAK AND LEAKING. 1 G 7 2 3U H1NE 1998041700205 19980417 00205 SW 1998 4 17 HEEA0013808 1 19980402 A 3340 A490A POWER SUPPLY BELL 206 206L3 1182108 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3207Q 51540 POWER SUPPLY INOPERATIVE AND HAS NO OUTPUT. 1 G 7 1 3U H2SW 1998041700206 19980417 00206 SW 1998 4 17 HEEA0013809 1 19980402 A 3340 A490A POWER SUPPLY BELL 206 206L3 1182108 SW STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 363BH 51345 POWER SUPPLY INOPERATIVE AND HAS NO OUTPUT. 1 G 7 1 3U H2SW 1998041700207 19980417 00207 1998 4 17 HEEA0013810 4 19980402 A 2210 214074301105 AMPLIFIER BELL 214 214ST 1182106 SW SCAS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 PITCH CHANNEL KICKS OFF WITH CONTROL INPUT. 2 G 7 2 4U H10SW 1998041700208 19980417 00208 SW 1998 4 17 HEEA0013811 1 19980402 A 2435 214175150105 GENERATOR BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 2232 28139 GENERATOR TRIPS BREAKER. 2 G 7 2 4U H10SW 1998041700209 19980417 00209 SW 1998 4 17 HEEA0013812 1 19980402 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 21497 51518 ACTUATOR INOPERATIVE. 1 G 7 1 3U H2SW 1998041700210 19980417 00210 SW 1998 4 17 HEEA0013813 1 19980402 A 6320 206040190005 PUMP BELL 206 206L3 1182108 SW GEAR BOX LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4282Z 51499 SEAL LEAKING-SHAFT WORN. 1 G 7 1 3U H2SW 1998041700211 19980417 00211 SW 1998 4 17 HEEA0013815 1 19980402 A 2915 212076006007 VALVE ASSY BELL 412 412 1182202 SW HYD PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 BYPASS BUTTON WILL NOT RESET. 1 G 7 2 4U H4SW 1998041700212 19980417 00212 NE 1998 4 17 HEEA0013816 1 19980402 A 2420 7655009005108 GENERATOR CONTRO SKRSKY S76 S76A 8143006 NE AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 A/C GENERATOR WOULD NOT COME ON BY ITSELF. 1 G 7 2 3U H1NE 1998041700213 19980417 00213 SW 1998 4 17 HEEA0013818 1 19980402 A 7921 8543909 OIL COOLER BELL 206 206L1 1182107 SW ENGINE LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 5014V 45217 OIL COOLER LEAKING. 1 G 7 1 3U H2SW 1998041700214 19980417 00214 NE 1998 4 17 HEEA0013819 1 19980402 A 2913 7665009808101 HYD PUMP SKRSKY S76 S76A 8143006 NE HYD SYS WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122H 760233 SPLINE WORN ON INTERNAL AND EXTERNAL DRIVE SHAFTS. 1 G 7 2 3U H1NE 1998041700215 19980417 00215 1998 4 17 HEEA0013821 4 19980402 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW COCKPIT PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 ATTITUDE INDICATOR PRECESSES. 1 G 7 2 4U H4SW 1998041700216 19980417 00216 1998 4 17 HEEA0013822 4 19980402 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 RATE TURN INDICATOR NO TURN NEEDLE MOVEMENT. 1 G 7 2 4U H4SW 1998041700217 19980417 00217 1998 4 17 HEEA0013825 4 19980402 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW AUTO FLIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 HEADING PRECESSES AND FAILS TEST 8.5 ON SST. 1 G 7 2 4U H4SW 1998041700219 19980417 00219 SW 1998 4 17 HEEA0013830 1 19980402 A 6710 204060762005 LINEAR ACTUATOR BELL 412 412 1182202 SW M/R BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 LINEAR ACTUATOR TERMINAL STUD IS BROKEN. 1 G 7 2 4U H4SW 1998041700220 19980417 00220 1998 4 17 HEEA0013831 4 19980402 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 33076 ATTITUDE INDICATOR POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1998041700221 19980417 00221 SW 1998 4 17 HEEA0013832 1 19980402 A 5260 206331102 STEP BELL 206 206L3 1182108 SW RT STEP CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 STEP HAS EXCESSIVE CORROSION AT MOUNT POINTS. 1 G 7 1 3U H2SW 1998041700222 19980417 00222 GL 1998 4 17 HEEA0013833 2 19980402 A 7314 3881005 FUEL PUMP BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL FUEL SYS WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8591X 51495 WORN DRIVE SHAFT SPLINES AND GEAR SPLINES. 1 G 7 1 3U 3 U H2SW E1GL 1998041700223 19980417 00223 1998 4 17 HEEA0013834 4 19980402 A 3457 1624811 ANTENNA BOLKMS 105 BO105S 5626006 EU GPS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 GPS INDICATES ANTENNA FAILED AND SHOWS 1.0 VOLTS. 1 G 7 2 3U H3EU 1998041700224 19980417 00224 1998 4 17 HEEA0013835 4 19980402 A 3453 071143100 ANTENNA KA83 BELL 206 206L3 1182108 SW LORAN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41791 51465 LORAN UNIT NOT RECEIVING SIGNAL. 1 G 7 1 3U H2SW 1998041700225 19980417 00225 1998 4 17 HEEA0013837 4 19980403 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 S818 DUE 2 YEAR INSPECTION. PERFORMED PRELIMINARY INSPECTION AND FOUND GPS HAS SEVERAL BUTTONS TO BE UNREADABLE AND ALSO BA CKUP BATTERY IS DEAD. 1 G 7 2 3U H3EU 1998041700226 19980417 00226 1998 4 17 HEEA0013839 4 19980403 A 3120 811B DIGITAL CLOCK SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 CLOCK WILL NOT KEEP CORRECT TIME. 1 G 7 2 3U H1NE 1998041700227 19980417 00227 SW 1998 4 17 HEEA0013840 1 19980403 A 2621 A352T EXTINGUISHER BELL 412 412 1182202 SW FIRE EXT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 FIRE EXT OUT OF GREEN AT 10C. 1 G 7 2 4U H4SW 1998041700228 19980417 00228 1998 4 17 HEEA0013841 4 19980403 A 3120 811B DIGITAL CLOCK BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 COATING ON FACE IS MISSING AND BATTERY IS DEAD. 1 G 7 1 4U H4SW 1998041700229 19980417 00229 SW 1998 4 17 HEEA0013842 1 19980403 A 2824 L88010491 VALVE BELL 412 412 1182202 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 VALVE DOES NOT CYCLE. 1 G 7 2 4U H4SW 1998041700230 19980417 00230 SW 1998 4 17 HEEA0013843 1 19980403 A 7722 206375007103 INDICATOR BELL 206 206L1 1182107 SW TOT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007N 45184 TOT NEEDLE STICKS AT 500 WHEN HEATED. 1 G 7 1 3U H2SW 1998041700231 19980417 00231 1998 4 17 HEEA0013844 4 19980403 A 3416 212070238007 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT LEAKAGE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 ALTIMETER EXCESSIVE CASE LEAKAGE. 1 G 7 2 3U H1NE 1998041700232 19980417 00232 SW 1998 4 17 HEEA0013845 1 19980403 A 7714 206075682001 GAS PROD GAGE BELL 206 206L1 1182107 SW COCKPIT ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5005F 45176 GAS PROD GAGE ERRATIC ON STARTUP. 1 G 7 1 3U H2SW 1998041700233 19980417 00233 1998 4 17 HEEA0013846 4 19980403 A 3416 212070238003 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 760167 INDICATOR IS OUT OF TOLERANCE AT 18,000 FEET. FAILED BEFORE AND AFTER TEST. 1 G 7 2 3U H1NE 1998041700234 19980417 00234 SW 1998 4 17 HEEA0013847 1 19980403 A 7712 212070160007 INDICATOR BELL 212 212 1181420 SW TORQUEMETER FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102PH 30899 NR 2 NEEDLE WILL NOT INDICATE. 1 G 7 1 4U H4SW 1998041700235 19980417 00235 SW 1998 4 17 HEEA0013848 1 19980403 A 6310 214040840101 SEAL 214040019101 BELL 214 214ST 1182106 SW XMSN LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6957Y NA 28139 SEAL LEAKING. 2 G 7 2 4U H10SW 1998041700236 19980417 00236 NM 1998 4 17 K3HA980048 1 19980408 A 2782 IU11032 ACTUATOR BOEING 727 727225 1384077 NM NR 6 LE SLAT LEAKING A K3HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 25 8881Z 21578 LOSS A SYSTEM HYDRAULIC FLUID, RETURNED TO BLOCK. TROUBLESHOT NR 6 SLAT ACTUATOR, INSTALLED NR 6 SLAT ACTUATOR IAWMM 27 -81-32 OPS CHECK OK. ALSO, CHECK A AND B SYSTEM CASE DRAIN FILTERS NO DEFECTS NOTED. REF MM 29-11-0 AND 29-12-0. 2 L 7 3 4F A3WE 1998041700237 19980417 00237 NM 1998 4 17 K3HA980049 1 19980407 A 3350 BAC1522339556 TRACK BOEING 727 727225 1384077 NM CABIN LOOSE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 LAST SET OF TRACK LIGHT EMERGENCY BY AFT LAV TAPED DOWN NEED TO REPLACE TRACK. REPLACED TRACK COVER SECTION. OPS CHECK OK REF MM 33-59-00. 2 L 7 3 4F A3WE 1998041700238 19980417 00238 NM 1998 4 17 K3HA980050 1 19980406 A 3350 SIGN BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 AFT AIRSTAIR DOOR EMEGENCY EXIT SIGN BELOW AFT FLIGHT ATTENDANT HAND MIKE HAS SOME LIGHT OUT. RELAMPED, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998041700239 19980417 00239 NE 1998 4 17 CALA9800643 2 19980404 A 7260 STARTER GEAR 3353001100 BOEING 737 7373T0 1384582 NM GE CFM56 CFM563B1 13802 NE NR 1 GEARBOX FAILED A CALA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 09 14320 23371 858653 THE NR 1 ENGINE STOPPED WHILE EN ROUTE FROM SAL TO IAH. THE AIRCRAFT WAS DIVERTED TO MID WHERE IT LANDED WITHOUT INCIDE NT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. ACCESSORY GEARBOX DISASSEMBLY REVEALED STARTER GEAR FAILURE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041700240 19980417 00240 WP 1998 4 17 CALA9800644 1 19980407 A 5320 JAMB DOUG DC10 DC1030 3023501 WP BS 1964 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND CORROSION ON ENTRY LOWER AFT CARGO JAMB BOX AT STA 1964 BETWEEN STRINGER 40-46. THE CORRODED AREAS WERE REMOVED. A STRAP, DOUBLERS, PLUG, ANGLE, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-50-00, FIGURE 14. 2 L 7 3 4F A22WE 1998041700241 19980417 00241 WP 1998 4 17 CALA9800645 1 19980408 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 455 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND CORROSION ON FLOOR OMEGA SUPPORT AT STA 455, RBL 45. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-70-00, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998041700242 19980417 00242 WP 1998 4 17 9806239996 1 19980403 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 1003-1038 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND CORROSION ON LEFT INTERCOSTAL MOUNT T-ANGLE IN THE APU BAY FS 1003 TO 1038. REPAIRED PER EA 99-15 6160. 2 L 7 2 4F A6WE 1998041700243 19980417 00243 WP 1998 4 17 9806249974 1 19980325 A 5711 SPAR DOUG DC9 DC931 3022065 WP WS 691 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9338 47347 DURING M-CHECK, FOUND CORROSION ON REAR SPAR UPPER CAP AND ADJOINING WING SKIN AT WS 691. REPAIRED PER EA 99-154768. 2 L 7 2 4F A6WE 1998041700244 19980417 00244 WP 1998 4 17 9806259933 1 19980413 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 589 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING M-CHECK, FOUND CORROSION OF END FITTING FOR LONGERON 26L AT FS 589. REPLACED FITTING (P/N 3920334-1N) PER SRM 51 -30-2. 2 L 7 2 4F A6WE 1998041700245 19980417 00245 WP 1998 4 17 9806269933 1 19980413 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 589 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1134U 47280 DURING M-CHECK, FOUND CRACK IN END FITTING FOR LONGERON 30 AT FS 589. REPLACED FITTING (P/N 5920331-1N) PER SRM 51-30-2 . 2 L 7 2 4F A6WE 1998041700246 19980417 00246 WP 1998 4 17 9806279933 1 19980413 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 589 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING M-CHECK, FOUND CRACK IN END FITTING FOR LONGERON 28L AT FS 589. REPLACED FITTING (P/N 5920332-1N) PER SRM 51-30- 2. 2 L 7 2 4F A6WE 1998041700247 19980417 00247 WP 1998 4 17 9806289941 1 19980122 A 5312 BULKHEAD DOUBLER DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M-CHECK, FOUND CRACK IN AFT PRESSURE BULKHEAD SUPPORT CHANNEL -11 DOUBLER AT THE TOP RIGHT SIDE. REPAIRED PER EA 99-154621. 2 L 7 2 4F A6WE 1998041700248 19980417 00248 NM 1998 4 17 9806296608 1 19980407 A 5711 SPAR CHORD BOEING 747 747151 1384891 NM WS 1471 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PERIODIC CHECK, FOUND CORROSION ON LOWER CHORD OF FRONT SPAR FS 1471. REPAIRED PER EA 66-153315. 2 L 7 4 4F A20WE 1998041700249 19980417 00249 WP 1998 4 17 9806301162 1 19980314 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING L-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME RIGHT SIDE, FS 459, RBL 61. REPAIRED PER EA 11-155559. 2 L 7 3 4F A22WE 1998041700250 19980417 00250 WP 1998 4 17 9806311162 1 19980314 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING L-CHECK, FOUND CRACK IN LOWER NOSE FUSELAGE FRAME LEFT SIDE, FS 459, LBL 61. REPAIRED PER EA 11-155558. 2 L 7 3 4F A22WE 1998041700251 19980417 00251 WP 1998 4 17 9806321162 1 19980329 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 1009 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 162US 46771 DURING L-CHECK, FOUND CORROSION ON ANGLE AT FORWARD CARGO DOOR LOWER AFT JAMB FS 1009, RBL 75. REPAIRED PER EA 11-15622 1. 2 L 7 3 4F A22WE 1998041700252 19980417 00252 WP 1998 4 17 UPS98826353 1 19980312 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 190-220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK FWD LOWER CARGO, LONG 35 R CORRODED STA 190 TO 220. REMOVED I/B AND O/B SECTIONS OF LONGERON 35 RI GHT, LONGERON CORRODED BEYOND LIMITS IAW DC8 SRM 53 2 0. LOCATED DRILLED AND DEBURRED LONGERON IAW DC8 SSRM 51 1 24 AND INSTALLED IAW DC8 SRM, 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700253 19980417 00253 WP 1998 4 17 UPS98826354 1 19980317 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 190-380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, LONGERON 35 LEFT STA 190 380 CORRODED. REMOVED L35L. FOUND TO BE CORRODED BEYOND LIMITS, RECEIVE D NEW LONGERON PART 9754913 324 LOCATED AND DRILLED LONGERONS IAW DC8 SRM 51 3 2. INSTALLED WITH HI-LOKS IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700254 19980417 00254 WP 1998 4 17 UPS98826355 1 19980312 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 370 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, FWD LOWER CARGO SKIN BULGED AND CORRODED AT STA 270 RIGHT OF L36. REMOVED LOWER BELLY SKIN STA 19 0 450 AND DOUBLERS DRILLED COUNTER SUNK AND INSTALLED NEW SKIN AND DOUBLERS IAW DC8 SMR 51 1 4, 51 1 20, 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700255 19980417 00255 WP 1998 4 17 UPS98826356 1 19980314 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, Z FITTING CORRODED STA 340, LONGERON 35L TO 36. REMOVED OLD FITTING IAW DC8 SRM 51 1 20D. RECEIV ED NEW PART PN 37558 2201N, LOCATED AND DRILLED NEW PART, IAW DC8 SRM 51 3 2 ALODINED AND PRIMED HOLE IN NEW PART IAW D C8 SR, 51 1 8, INSTALLED NEW PART IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700256 19980417 00256 WP 1998 4 17 UPS98826357 1 19980317 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, Z FITTING AT L34R L33R AT FUSELAGE STATION 1160 HAS EXTENSIVE CORROSION. REMOVED Z FITTING CUT NE W 2 FITTINGS AND FABBED REPAIR ANGLES IAW DC8 SRM 53 2 0. TRANSFER EXISTING HOLES TO NEW 2 FITTINGS IAW DC8 SRM 51 3 2. ALODINED AND PRIMED REPAIR ANGLES IAW DC8 SRM 51 1 8. INSTALLED 2 FITTING AND REPAIR ANGLES IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700257 19980417 00257 WP 1998 4 17 UPS98826358 1 19980315 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, Z FITTING CORRODED AT FUSELAGE STATION 280 34R- 35R. REMOVED OLD FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51 1 20D. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700258 19980417 00258 WP 1998 4 17 UPS98826359 1 19980314 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, STA 1050, L31R SPLICE CRACKED. REMOVED SPLICE IAW DC8 SRM 51 1 20D AND DC8 SRM 51 3 1, MATERIAL I D 3750257-1 FITTING IAW DAC DWG 5750322, ALODINED AND PRIMED MATING AR EA IAW DC8 SRM 51 1 8. INSTALLED FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700259 19980417 00259 WP 1998 4 17 UPS98826360 1 19980317 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1228 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, Z FITTING STA L35R L34R FS 1228 IS CRACKED AND CORRODED. REMOVED OLD FITTING HOLES IN NEW FITTING IAW DC8 SRM 51 1 24. ALODINED AND PRIMED HOLES IAW DC8 SRM 51 1 8. INSTALLED NEW FITTING IAW DC 8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998041700260 19980417 00260 WP 1998 4 17 UPS98826362 1 19980328 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 74.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C RT WING TOP SKIN AT STA XRS.74.5 AND WING UPPER STR 9 HAS STRESS CORROSION CRACKING AT ONE FASTENER. REPAIRED AREA IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 1998041700261 19980417 00261 NE 1998 4 17 98FDEA00262 2 19980410 A 7200 ENGINE BOEING 727 727277 138408S NM PWA JT8 JT8D9A 52048 NE RIGHT SPARKS A FDEA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 25 241FE 20979 ATA: 05-50 98-0098, AFTER TAKEOFF FROM PHL 9L- TOWER REPORTED THAT SEVERAL AIRCRAFT SAW SPARKS FROM RIGHT SIDE OF AIRCR AFT. RETURNED TO PHL FOR INSPECTION. ALL AIRCRAFT SYSTEMS NORMAL, ENGINE PARAMETERS NORMAL, NO PRESSURE PROBLEMS. INS PECTED ALL 3 ENGINE INLETS AND EXHAUSTS NO DEFECTS FOUND. INSPECTED AIRCRAFT AND GEAR ALL CHECKS GOOD. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 1998041700262 19980417 00262 NM 1998 4 17 98FDEA00263 1 19980410 A 3260 PROX SENSOR DOUG MD11 MD11F 3023600 NM LT MLG FAILED A FDEA O OTHER N FALSE WARNING LD LANDING 1 SO 25 582FE 48420 98-0099 NRT:LEFT GEAR UNSAFE INDICATION ON LANDING. RECYCLED GEAR ARM SAME ON LANDING CONFIGURATION PAGE INDICATION GE AR DOWN WITH FLOOR VIEW. REMOVED AND REPLACED DOWN LOCK PROXIMITY SENSOR PER M/M 32-61-15 RETURN TO SERVICE TEST CHECK GOOD. 2 L 7 3 4F RT A22WE 1998041700263 19980417 00263 EU 1998 4 17 98FDEA00264 1 19980411 A 2611 CONTROL UNIT AIRBUS 310 A310203 EU MAIN DECK MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 415FE 349 98-0100, AT FL290 CREW RECEIVED AN ECAM WARNING OF MAIN DECK SMOKE WARNING. CREW DONNED 02 MASK AND FOLLOWED AFM PROCED URES. NEVER DID SMELL SMOKE. DECLARED PRECAUTIONARY AND RETURNED TO AIRPORT. T/S SYSTEM PER TSM, ALL DETECTORS TESTED GOOD. BITE TEST OF ALL THREE MAIN DECK SMOKE DET CTL UNITS, CHKS GOOD. RAN NR 2 ENG AND NR 2 PACK, OPS CHK NORMAL. N O INDICATION OF SMOKE OR FIRE DAMAGE NOTED. ACFT RETURNED TO SERVICE. REMOVAL AND REPLACEMENT OF ALL THREE MAIN DECK C ARGO COMPT. SMOKE DETECTOR CONTROL UNITS PRECAUTIONARY. 2 L 7 2 4F RT A35EU 1998041700264 19980417 00264 SO 1998 4 17 SWIA971149 1 19980309 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LAVATORY CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 RIGHT FORWARD BUTT STRAP UNDER LAVATORY AREA HAS CORROSION. REMOVED AND REPLACED RIGHT FORWARD BUTT STRAP UNDER LAVATOR Y AREA IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041700265 19980417 00265 SO 1998 4 17 SWIA971150 1 19980309 A 5320 TEE SECTION EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE FRAME 16 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 RIGHT T-SECTION BETWEEN CENTER AND RIGHT BUTT STRAPS AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED RIGHT T-SECTION AT FRAME 16 IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041700266 19980417 00266 SO 1998 4 17 SWIA971151 1 19980303 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 LEFT FLOOR SEAT TRACK LONG SECTION UNDER GALLEY AREA HAS CORROSION. REMOVED AND REPLACED LEFT SEAT TRACK WITH A NEW SEA T TRACK IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041700267 19980417 00267 SO 1998 4 17 SWIA971152 1 19980306 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 FORWARD LONG SECTION OF CABIN SEAT TRACK, RIGHT SIDE FLOOR LEVEL HAS NUMEROUS AREAS OF CORROSION. REPLACED RIGHT SIDE F LOOR LEVEL SEAT TRACK WITH NEW SEAT TRACK IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041700268 19980417 00268 SO 1998 4 17 SWIA971153 1 19980306 A 5320 CROSS BEAM EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 209SW 120269 LEFT FLOOR CROSSBEAM AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED LEFT FLOOR CROSS BEAM AT FRAME 16 IAW SRM 51-40-02 . 2 L 7 2 4T 4 T RT A31SO E20NE 1998041700269 19980417 00269 WP 1998 4 17 CKSA98208 1 19980407 A 2710 57147155508 POWER CONTL VLV DOUG DC8 DC861 3021952 WP RT AILERON FAILED A CKSA O OTHER J WARNING INDICATION CR CRUISE 1 GL 23 817CK 45887 MAN RUDDER AND AILERON LIGHTS CAME ON IN FLIGHT ALONG WITH RES PRESS LOW LIGHT HYD QTY DROPPED DOWN 1/3 FROM FULL. LOST ALL HYD PRESS. PERFORMED ABNORMAL HYDRAULICS THEN EMERGENCY HYDRAULIC CHECKLIST ACCORDING TO FOM. MADE 0 FLAP LANDING SFO. REMOVED AND REPLACED RT INBD AILERON PCV ASSY PER MM 27-10, OPS AND LEAK CHECK OK. HYDRAULICS SERVICED AND BLED. 2 L 7 4 4F 4A25 1998041700270 19980417 00270 NM 1998 4 17 CKSA98209 1 19980307 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6834 20187 BEFORE FLIGHT, FOUND DAMAGE PUNCTURED SKIN AFT OF EXTERIOR POWER HOOK-UP AND BELOW FWD LAV SERVICE DOOR. INSTALLED BLIN D RIVET REPAIR IAW B727 SRM 53-30-3 PAGES 2-6. 2 L 7 3 4F A3WE 1998041700437 19980417 00437 SO 1998 4 17 CA971021003 1 19980326 A 3213 40327000 HOUSING 4041302 PIPER PA31 PA31 7103102 SO LT MLG STRUT CRACKED W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 10073 (CAN) AFTER LANDING, PILOT REPORTED LT LANDING STRUT WAS FLAT AND LEAKING FLUID. MAINTENANCE INSPECTION REVEALED STRUT HOUSING HAD A 16 INCH VERTICAL CRACK. HOUSING REPLACED. 1 L 7 2 3O A20SO 1998041700439 19980417 00439 CE 1998 4 17 CA971024004 1 19980326 A 2520 NAS1329C4K80 RIVNUT BEECH 5053448627 BEECH 90 65A90 1152908 CE SEAT FRAME LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUNTINE INSPECTION AND IN A CCW CAMPAIGN NOTICE 651-006, INSPECTION OF CABIN SEAT FOUND LOOSE RIVNUTS. SE AT REPAIRED. 1 L 7 2 3T 3A20 1998041700464 19980417 00464 NM 1998 4 17 CA971208008 1 19980317 A 3244 323000210 TIRE BOEING 747 747233B NM PWA JT9 JT9D7 52054 NE MLG NR 10 BLOWN W K NONE O OTHER LD LANDING 1 CA P685935 (CAN) NR 10 TIRE BLEW ON LANDING. TIRE REPLACED. 2 L 7 4 4F 4 F RT A20WE E20EA 1998041700465 19980417 00465 NM 1998 4 17 CA971208010 1 19980317 A 2530 86010000 OVEN BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE NR 3 GALLEY BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P709649 (CAN) ON TAXI, CABIN CREW REPORTED SMOKE COMING FROM REAR GALLEY. UTILITY BUS SELECTED OFF. A/C TAXIED CLEAR OF RUNWAY AND ENGINES SHUT DOWN. NR 3 GALLEY INSPECTED AND OVEN REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998041700469 19980417 00469 NM 1998 4 17 CA971216018 1 19980317 A 3510 FITTING BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE OBS OXY PANEL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 708810 (CAN) SECOND OBSERVER OXYGEN CONTROL PANEL FITTING CRACKED. PANEL REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998041700470 19980417 00470 NM 1998 4 17 CA971216021 1 19980317 A 2751 1817381 TRANSMITTER 1817381 BOEING 737 737296 1384486 NM PWA JT8 JT8D9A 52048 NE FLAP POSITION FAILED W A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 CA 7381 707412 (CAN) AIR TURN BACK TO BLOCKS DUE TO STICK SHAKER STALL WARNING AT TAKEOFF. REPLACED FLAP POSITION TRANSMITTER. 2 L 7 2 4F 4 F RT A16WE E2EA 1998041700471 19980417 00471 NM 1998 4 17 CA971216022 1 19980317 A 3244 TIRE BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NLG WHEEL RIM DETACHED W K NONE O OTHER IN INSP/MAINT 1 CA 688478 (CAN) AIRCRAFT ARRIVED WITH LT NOSE WHEEL OFF RIM. REPLACED BOTH NOSE WHEELS. 2 L 7 2 4F 4 F A16WE E2EA 1998041700472 19980417 00472 NM 1998 4 17 CA971216025 1 19980317 A 3260 188915 SENSOR ELDEC 188915 BOEING 737 737217 1384464 NM RT MLG INTERMITTENT W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AIRCRAFT RETURNED TO RAMP DUE TO RT MAIN GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. RT UPLOCK REPLACED. 2 L 7 2 4F A16WE 1998041700473 19980417 00473 NM 1998 4 17 CA971216028 1 19980317 A 5512 6575564508 PLATE 65737824 BOEING 737 737242C 1384478 NM PWA JT8 JT8D9A 52048 NE HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 53787 654788 (CAN) TRAILING EDGE OF HORIZONTAL STABILIZER BEAM ASSY CRACKED ON FORWARD EDGE OF THE COVER PLATE ALONG THE RADIUS IN 4 LOCATIONS. THE LONGEST CRACK WAS APPROX 2 INCHES LONG. BEAM LENGTH IS 12 FEET. THE RADIUS SHOULD BE .25 INCH RADII AN D WAS ONLY.10 INCH RADII ON MANUFACTURE. THE DEFECT OF PLATE (BEAM ASSY) IS ATTACHING POINT FOR LOWER HORIZ STAB ACCESS PANEL. REPLACED. PART TC: 46,379. AIRCRAFT TT: 50,989 HOURS. 2 L 7 2 4F 4 F A16WE E2EA 1998041700474 19980417 00474 NM 1998 4 17 CA971216029 1 19980317 A 2822 6072101 IMPELLER BOEING 747 747475 NM BOOST PUMP WORN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) OVERRIDE JETTISON PUMP IMPELLER SHROUD WORN FROM CONTACT WITH THEIR RESPECTIVE INLET CHECK VALVES. SHROUD HAD BEE N WORN DOWN ENOUGH TO CAUSE IMPELLER DAMAGE. ALSO, THE DISCHARGE CHECK VALVE WAS WORN INTO THE ATTACHED FUEL PIPES. AL L REPLACED. 2 L 7 4 4F RT A20WE 1998041700475 19980417 00475 NM 1998 4 17 CA971216031 1 19980317 A 2720 2588880901 COUPLER SPERRY 2588880901 BOEING 737 737248C NM PWA JT8 JT8D9A 52048 NE YAW DAMPER MALFUNCTION W A H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CR CRUISE 1 CA 30914 0991007 674215 (CAN) IN CRUISE DURING LIGHT CHOP, AIRCRAFT BEGAN TO EXPERIENCE A 10 DEGREE DUTCH ROLL ACCOMPANIED BY YAW, GPS INPUT, YA W DAMPER AND AUTOPILOT CONTROL WERE DEACTIVATED IN ATTEMPT TO REDUCE THE CONDITION. YAW DAMPER WAS THEN RE-ACTIVATED AN D THE CONDITION SUBSIDED. PRECAUTIONARY RUDDER PCU SLIDE CHECK CARRIED OUT, NO FAULT FOUND. YAW DAMPER COUPLER REPLACE D. PART TC: 29,003. 2 L 7 2 4F 4 F A16WE E2EA 1998041700481 19980417 00481 NE 1998 4 17 K3HA980051 2 19980409 A 7314 878200 FUEL PUMP BOEING 727 727225 1384077 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A A K3HA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 25 8880Z 21453 666859 NR 1 ENGINE FAILED IMMEDIATELY AFTER LIFT OFF. SECURED FAILED ENGINE. ATTEMPTED RESTART AS PER PROCEDURES. NO FUEL FL OW, NO START. ENGINE WINDMILLED 24 MINUTES WITH OIL PRESSURE AT 15 TO 18 PSI. REPLACED NR 1 ENGINE FUEL PUMP PER MM MA NUAL 73-11-011. LEAK CHECK, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998041700482 19980417 00482 NM 1998 4 17 CALA9800646 1 19980408 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1010-1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1010 TO 1030, RBL 48. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, FIGURE 1, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998041700483 19980417 00483 NM 1998 4 17 CALA9800647 1 19980407 A 5320 FITTING BOEING 737 737130 1384435 NM BS 706 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14206 19023 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE FRAME TRUNNION BEAM SUPPORT FITTING IN RT WHEEL WELL AT BS 706. THE BEAM WAS REPLACED IAW ECRA 5311-01045. 2 L 7 2 4F A16WE 1998041700484 19980417 00484 NM 1998 4 17 CALA9800648 1 19980408 A 5311 FRAME BOEING 737 737130 1384435 NM BS 707 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14206 19023 INSPECTION FOUND BS 706L FRAME LUG HOLE CORRODED AT LT MLG. AN OUTER BUSHING FOR BEAM AND TWO EACH HAT BUSHINGS FOR FRA ME LUG WERE FABRICATED AND INSTALLED IAW ECRA 5310-03713. 2 L 7 2 4F A16WE 1998041700485 19980417 00485 NM 1998 4 17 CALA9800649 1 19980410 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1090-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND RT AFT LAV SEAT TRACK CORRODED BETWEEN STA 1090 TO 1130, RBL 24. A NEW SECTION OF SEAT TRACK WAS FABRI CATED AND INSTALLED IAW SRM 53-10-5, PAGE 1 FIGURE 1, 51-10-2 AND MM 51-20-0. 2 L 7 3 4F A3WE 1998041700486 19980417 00486 NM 1998 4 17 CALA9800650 1 19980412 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1110, RBL 0 TO 60. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FI GURE 3. 2 L 7 3 4F A3WE 1998041700487 19980417 00487 NM 1998 4 17 CALA9800651 1 19980412 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1070, RBL 20 TO 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3. 2 L 7 3 4F A3WE 1998041700488 19980417 00488 NM 1998 4 17 CALA9800652 1 19980412 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1130, LBL 24. THE SEAT TRACK WAS REMOVED. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998041700489 19980417 00489 WP 1998 4 17 CALA9800653 1 19980408 A 5311 FRAME DOUG DC10 DC1030 3023501 WP LT MLG BROKEN A CALA A D UNSCHED LANDING RETURN TO BLOCK K FLUID LOSS CR CRUISE 1 SW 09 19072 46576 THE AIRCRAFT LOST NR 3 HYDRAULIC SYSTEM FLUID WHILE EN ROUTE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. INITIAL FINDINGS REVEALED THE LT MLG SUPPORT FRAME ASSEMBLY WAS BROKEN. *S/D* FAILURE OF THE SUPPORT FRAME ASSEMBLY RESULTED IN DAMAGE TO THE HYDRAULIC LINES AND SUBSEQUENT LOSS OF HYDRAULIC FLUID FROM THE NR 3 SYSTEM. THE HYD RAULIC LINES AND LT MLG RETRACT ACTUATOR WERE REPLACED. THE LT MLG SUPPORT FRAME ASSEMBLY, SUPPORT FITTING, AND ASSOCIA TED DAMAGED HARDWARE WERE REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1998041700490 19980417 00490 EU 1998 4 17 98FDEA00261 1 19980409 A 7600 COMPUTER AIRBUS 300 A300F4605R 3930327 EU NR1 THRUST CONTL FAILED A FDEA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 667FE 771 NR 2 THROTTLE CONTINUES TO ROLL BACK ON ROTATION APPZ 1 THROTTLE WIDTH OK REST OF FLIGHT. TROUBLESHOT PER TSM 73-00-30 PG 105 FIG 103 NO THROTTLE VALID FAULT CODE CHECKED THROTTLE CONTROL EFFORT IAW M/M 76-11-00, DISPLACEMENT EFFORT NORMAL . REMOVED AND REPLACED NR 1 THRUST CONTROL COMPUTER PER M/M 22-36-34-4 AFS AND LAND TEST GOOD. 2 L 7 2 4F RT A35EU 1998041700491 19980417 00491 NM 1998 4 17 98FDEA00265 1 19980413 A 5320 DOUBLERS DOUG MD11 MD11F 3023600 NM BS 1458 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 609FE 48549 SNRM N 00345, CENTER GEAR WELL, LEFT TRUNNION SUPPORT ANGLE DOUBLER IS CRACKED AT UPPER AND LOWER FWD SECTIONS AT BS 145 8. REMOVED SUPT ANGLE DOUBLERS EDDY CURENT INSP'D PER EA 1-5310-38499 NO DEFECT NOTED, INSTALLED ANGLE DOUBLER PER EA 1 -5310-38499. 2 L 7 3 4F RT A22WE 1998041700492 19980417 00492 WP 1998 4 17 ABXA9800327 1 19980409 A 5250 AR25291GR41 LATCH DOUG DC9 DC932 3022066 WP COCKPIT DOOR BENT A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 928AX 47392 COCKPIT DOOR WAS STUCK CLOSED. WOULD NOT OPEN. FOUND LATCH TO BE BINDING. REPAIRED AND REASSEMBLED HANDLE. 2 L 7 2 4F A6WE 1998041700493 19980417 00493 WP 1998 4 17 ABXA9800343 1 19980412 A 7830 AE246000E0480 HOSE DOUG DC8 DC863 302198A WP NR 2 TR UNIT LEAKING A ABXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 825AX 46115 LOSS OF HYDRAULIC FLUID DOWN TO STANDPIPE LEVEL. AILERON CONTROL MANUAL LIGHT ILLUMINATED, HYDRAULIC PRESSURE VERY LOW AND NR 2 THRUST REVERSER LIGHT WAS FLASHING. REPLACED LEAKING HYDRAULIC HOSE TO THE THRUST REVERSER PUMP. RESERVICED HYDRAULIC SYSTEM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998041700494 19980417 00494 WP 1998 4 17 ABXA9800344 1 19980410 A 3260 0080004003 PROX SWITCH DOUG DC8 DC862 3021970 WP RT MLG WW OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 804AX 45987 RED GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. DOOR NOT LATCHED LIGHT WAS ILLUMINATED. RECYCLED GEA R TWICE, UPLATCH CHECKED GOOD. PERFORMED ADJUST/TEST OF MAIN LANDING GEAR IAW DC8 MM 32-6. SYSTEM OPS CHECKED GOOD AFT ER ADJUSTMENT. 2 L 7 4 4F 4A25 1998041700495 19980417 00495 WP 1998 4 17 MWEA98395 1 19980404 A 5730 39171801 SKIN DOUG DC9 DC914 3022034 WP WS 137 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 THE LEFT HAND LOWER WING PLATING AT XRS 137 REAR SPAR HAS A FASTENER HOLE DAMAGE. MTC REPLACED AND REPAIRED DAMAGE AND INSTALLED REPAIR BUSHING. 2 L 7 2 4F A6WE 1998041700496 19980417 00496 WP 1998 4 17 MWEA98396 1 19980404 A 5512 59180021 SKIN DOUG DC9 DC914 3022034 WP LT HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FOUND CRACK IN LEFT HAND HORIZONTAL STABILIZER UPPER AFT SKIN PANEL AT STATION XH8. MTC REMOVED AND REPLACED SKIN PANEL . 2 L 7 2 4F A6WE 1998041700497 19980417 00497 WP 1998 4 17 MWEA98397 1 19980409 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 THE GALLEY SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998041700498 19980417 00498 NM 1998 4 17 SCNA98032 1 19980408 A 3020 320115 ANTI-ICE VALVE BOEING 727 7272J4 1384006 NM NR 2 ENGINE COWL LEAKING A SCNA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 GL 15 285SC 8425 21676 ON DESCENT, TURNED ON ENGINE ANTI-ICE AND APPROXIMATELY TWO MINUTES LATER GOT ENGINE NUMBER TWO FIRE WARNING. SHUT DOWN NUMBER TWO ENGINE AND BLEW BOTH FIRE BOTTLES. FOUND NUMBER TWO COWL ANTI-ICE VALVE LEAKING. REMOVED AND REPLACED NUMB ER TWO COWL ANTI-ICE VALVE AND BOTH ENGINE FIRE BOTTLES AND SQUIBS. 2 L 7 3 4F RT A3WE 1998041700507 19980417 00507 GL 1998 4 17 CA970421038 2 19980107 A 7230 RING GROOVES 6876667 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FRONT SEAL WORN W K NONE O OTHER IN INSP/MAINT 1 CA CAE820180B (CAN) FRONT SEAL RING GROOVES WORN BEYOND LIMITS. 1 G 7 1 3U 3 U H2SW E4CE 1998041700515 19980417 00515 GL 1998 4 17 CA970421049 2 19980211 A 7313 6898735 NOZZLE 6898735 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAT30215F CAE831824 (CAN) FUEL NOZZLE CRACKED BEYOND LIMITS. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998041700516 19980417 00516 GL 1998 4 17 CA970421050 2 19980211 A 7260 68760300 STUD 68760300 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENG ASSORY DRV LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA CAE831824 (CAN) LOOSE STUD ON ENGINE ACCESSORY DRIVE GEARBOX. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998041700517 19980417 00517 GL 1998 4 17 CA970421051 2 19980211 A 7420 6870855 LEAD 6870855 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL THREADS STRIPPED W K NONE O OTHER IN INSP/MAINT 1 CA A0453 CAE831824 (CAN) STRIPPED THREADS ON LEAD CONNECTOR, CORROSION MAY BE CAUSE. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998041700518 19980417 00518 GL 1998 4 17 CA970421052 2 19980211 A 7420 106149501 EXCITER UNISON 106149501 BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL ENG IGN STRIPPED W K NONE O OTHER IN INSP/MAINT 1 CA 8346 CAE831824 (CAN) STRIPPED THREADS ON CONNECTIONS, POSSIBLY CORROSION. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998041700560 19980417 00560 GL 1998 4 17 CA970513023 2 19980319 A 7261 41291023 SHAFT ENSTRM F28 ENSTROM480 GL ALLSN 250C 250C20 03013 GL OIL COOLER CRACKED W A E UNSCHED LANDING ENGINE SHUTDOWN O J M OTHER WARNING INDICATION OVER TEMP CR CRUISE 1 CA 33 CAE845007 (CAN) IN-FLIGHT FAILURE OF OIL COOLER CONNECTING SHAFT. 1 G 7 1 3O 3 U NC H1CE E4CE 1998041700616 19980417 00616 1998 4 17 98ZZZX1474 4 19980405 A 3425 2589210902 COMPASS BOEING 727 727227 1384078 NM HSI NR 1 FAILED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 308AS 8079264 22002 CAPTAIN'S HSI HAS COMPASS FLAG. COPILOT'S RMI OFF FLAG IN VIEW. REMOVED AND REPLACED NR 1 COMPASS. 2 L 7 3 4F A3WE 1998041700623 19980417 00623 NM 1998 4 17 CA980402011 1 19980221 A 2530 HEATER PAD BOEING 767 767233 NM FWD GALLEY SHORTED W K NONE O OTHER CR CRUISE 1 CA (CAN) FLIGHT ATTENDANT RECEIVED AN ELECTRICAL SHOCK FROM A CONTROL SWITCH ON THE FORWARD GALLEY HEATER PAD. WARMER PAD AND LIGHT LENS REPLACED. 2 L 7 2 4F RT A1NM 1998041700624 19980417 00624 NM 1998 4 17 CA980402010 1 19980217 A 2750 285T0049127 ELECT UNIT 285T00495312 BOEING 767 767233 NM LE FLAP INTERMITTENT W L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) LEADING EDGE FLAP DISAGREE MESSAGE DISPLAYED. NECESSARY TO DO GO-AROUND AND ALTERNATE EXTENSION USED PRIOR TO LAN DING. REPLACED FLAP/SLAT ELECTRONIC UNIT. BITE CHECK AND SYSTEM OPERATION CARRIED OUT SERVICEABLE. 2 L 7 2 4F RT A1NM 1998041700625 19980417 00625 NM 1998 4 17 CA980402006 1 19980310 A 2530 OVEN FAN BOEING 767 767233 NM NR 3 AFT GALLEY BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) SMOKE EMANATING FROM BEHIND OVEN NR 3 AFT GALLEY. FIRE EXTINGUISHER DIRECTED INTO AREA. GALLEY SBS PULLED. OVEN REPLACED. 2 L 7 2 4F RT A1NM 1998041700628 19980417 00628 NM 1998 4 17 CA980331019 1 19980324 A 2781 18196914 TRANSMITTER BOEING 757 757236 NM LE SLAT CRACKED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA (CAN) AFTER TAKEOFF HAD TO RETURN DUE TO LEADING EDGE SLAT LOCKED BETWEEN UP AND NR 1 POSITION. LANDED OVERWEIGHT. OVE RWEIGHT LANDING CHECK CARRIED OUT OK AND SLAT PDU POSITION REPLACED. 2 L 7 2 4F RT A2NM 1998041700629 19980417 00629 WP 1998 4 17 CA980331017 1 19980321 A 2750 1562416109 LINK ASSEMBLY LKHEED 1011 1011385114 WP NR 1 FLAP VANE BROKEN W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) AFTER LANDING, DURING FLAP RETRACTION,THE FLAP POSITION INDICATOR SHOWED OFF, CIRCUITBREAKER CHECKED OK. DAMAGE T O NR 1 INBOARD FLAP VANE CAUSED BY THE BREAKING OF THE INBD FLAP VANE LINK. FLAP VANE, LINK AND FLAP ACTUATOR REPLACED. 2 L 7 3 4F A23WE 1998041700630 19980417 00630 WP 1998 4 17 CA980331016 1 19980320 A 2912 1515680103 PLUG LKHEED 1011 1011385114 WP B SYS HYD BROKEN W D RETURN TO BLOCK K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING PUSHBACK NR 2 ENG START, THE B-SYSTEM HYDRAULIC DROPPED TO ZERO. AIRCRAFT RETURNED TO GATE. THE PLUG CARTR IDGE CAVITY ON THE HIGH PRESSURE SYSTEM FILTER MODULE ASSY BROKEN. PLUG REPLACED. 2 L 7 3 4F A23WE 1998041700635 19980417 00635 EU 1998 4 17 CA980330025 1 19980319 A 2810 9001EN6 SWITCH BAG BAE146 BAE146200A 1500266 EU REFUEL PANEL SHORTED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) DURING REFUELING OPERATION, REFUELER COULD NOT PRESSURE REFUEL. CIRCUIT BREAKER E1 'QUANTITY AUX POWER WAS TRIPPE D. BREAKER RESET AND WHEN REFUEL DOOR PANEL SWITCH WAS ACTIVIATED SPARKS AND SMOKE CAME FROM WIRING AT POINT IT ENTERE D SWITCH. 2 H 7 4 4F RT A49EU 1998041700639 19980417 00639 EU 1998 4 17 CA980317032 1 19980309 A 5101 FUSELAGE AIRBUS 320 A320211 3930320 EU LOUD BANG W A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CA (CAN) A/C EXPERIENCED A LOUD BANG AND SHUDDER DURING CLIMB IN CLEAN AIR AND CLEAN CONFIGURATION. AFTER RETURN TO BLOCKS , A/C INSPECTED FOR BIRD STRIKE AND INSPECTION OF AIR CONDITIONING PACKS AND BORESCOPE CHECK OF ENGINES CARRIED OUT. NO DEFECTS FOUND. AIRCRAFT TT: 20,608 HOURS. 2 L 7 2 4F RT A28NM 1998041700718 19980417 00718 EU 1998 4 17 98ZZZX1499 1 19980301 A 3310 1179203103 CONTROL UNIT BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED A RMXA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 05 118LL 7097 INTERNAL MALFUNCTION OF COPILOT INSTRUMENT LIGHTING CONTROL UNIT. WHEN CONTROL UNIT FAILED, IT PRODUCED SMOKE AND ELECT RICAL FUMES ACCORDING TO PILOT. 1 G 7 2 3U H13EU 1998041700719 19980417 00719 EU 1998 4 17 98ZZZX1500 1 19980325 A 6410 11731743 BLADE BOLKMS 117 BK117B1 5626012 EU T/R ERODED A BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 213AE 567 377 7219 EXCESSIVE EROSION OF T/R BLADES SURFACE PROTECTION. THE PAINT HAS COME OFF IN LARGE STRIPS AND THEN THE RUBBERIZED EROS ION PROTECTION STARTS FLAKING OFF. 1 G 7 2 3U H13EU 1998041700720 19980417 00720 EU 1998 4 17 98ZZZX1501 1 19980325 A 6410 11731743 BLADE BOLKMS 117 BK117B1 5626012 EU T/R ERODED A BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 213AE 567 378 7219 EXCESSIVE EROSION OF T/R BLADES SURFACE PROTECTION. THE PAINT HAS COME OFF IN LARGE STRIPS AND THEN THE RUBBERIZED EROS ION PROTECTION STARTS FLAKING OFF. 1 G 7 2 3U H13EU 1998041700721 19980417 00721 1998 4 17 98ZZZX1502 4 19980310 A 3160 900A3720002107 DISPLAY DOUG MD900 MD900 3027375 NM COCKPIT FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 344 008251113 90000012 DISPLAY SYSTEM UNIT INOPERATIVE. LOWER HALF OF DISPLAY IS DIMMER (APPROXIMATELY BY HALF) THAN THE UPPER HALF. REPLACED WITH REPAIRED UNIT. CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998041700722 19980417 00722 GL 1998 4 17 98ZZZX1503 2 19980327 A 7320 1564T1005 ACTUATOR BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 ENG CONTROL FAILED A RMXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 05 911LF S663 834838 FOLLOWING TAKEOFF, RPM WARNING LIGHT, ATTEMPTED TO BEEP ENGINES DOWN - ONLY NR 1 RESPONDED. RETURNED AND EMERGENCY LAND ING MADE. FOUND NR 2 ACTUATOR INOPERABLE. PARTS ON ORDER. 1 G 7 2 3U 3 U H3EU E4CE 1998041700723 19980417 00723 SW 1998 4 17 98ZZZX1504 1 19980127 A 6220 222031613101 LIFT LINK BELL 230 230 1182149 SW M/R WORN A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 4UV LK0414 23019 LIFT LINK BEARING WORN OUT OF LIMITS. REMOVED AND REPLACED. 1 G 7 2 3U NC H9SW 1998041700724 19980417 00724 1998 4 17 98ZZZX1505 4 19980226 A 2312 40001452500 TRANSCEIVER RT138F BOLKMS 117 BK117B1 5626012 EU COCKPIT DEFECTIVE A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 217MC 294 7195 TRANSCEIVER PL TONE MODULATION IS INDICATING 1.8 HKZ TO 2.1 KHZ. CHECKED SPECS - SHOULD BE AROUND .75 TO .8 KHZ. REMOV ED AND REPLACED. 1 G 7 2 3U H13EU 1998041700725 19980417 00725 1998 4 17 98ZZZX1506 4 19980207 A 3421 5040017901 GYRO BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 105NG 5429 S632 ATTITUDE GYRO FAILED ON OPS CHECK. SPINS LIKE A TOP. REMOVED AND REPLACED. 1 G 7 2 3U H3EU 1998041700726 19980417 00726 1998 4 17 98ZZZX1507 4 19980213 A 3421 4021541671 ARTIFICAL HORIZ BOLKMS 117 BK117B1 5626012 EU COCKPIT MALFUNCTIONED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 214AE 82070915 7206 ARTIFICAL HORIZON PITCH AND ROLL CSAS WILL NOT ENGAGE. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 1998041700727 19980417 00727 1998 4 17 98ZZZX1508 4 19980214 A 2211 7004206901 COMPUTER BOLKMS 117 BK117B1 5626012 EU CSAS FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 214AE 89110252 7206 CSAS COMPUTER PITCH AND ROLL LIGHT STAYS ON. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 1998041700728 19980417 00728 1998 4 17 98ZZZX1509 4 19980206 A 2211 7004206901 COMPUTER 88030204 BOLKMS BK117 BK117C1 5626025 EU CSAS FAILED A RMXA K NONE J WARNING INDICATION CR CRUISE 1 SW 05 117NC 7509 CSAS COMPUTER PITCH LIGHT ILLUMINATED INTERMITTENTLY IN-FLIGHT. REMOVED AND REPLACED. 1 G 7 2 3U NC H13EU 1998041700729 19980417 00729 EU 1998 4 17 98ZZZX1510 1 19980109 A 2810 P401 VALVE BOLKMS BK117 BK117C1 5626025 EU FUEL VENT FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 117NC 7509 VENT VALVE FAILURE. ALLOWS FUEL TO VENT. REMOVED AND REPLACED. 1 G 7 2 3U NC H13EU 1998041700730 19980417 00730 EU 1998 4 17 98ZZZX1511 1 19980109 A 2810 P401 VALVE BOLKMS BK117 BK117C1 5626025 EU FUEL VENT FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 117NC 472 NA1 7509 VENT VALVE FAILED. REMOVED AND REPLACED. 1 G 7 2 3U NC H13EU 1998041700731 19980417 00731 1998 4 17 98ZZZX1512 4 19980129 A 2350 AA95726 AUDIO PANEL BOLKMS 105 BO105LSA3 5626020 EU COCKPIT DEFECTIVE A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 911SV 2800 2033 AUDIO PANEL SELECT KNOB INOPERATIVE. REMOVED AND REPLACED. 1 G 7 2 3U H3AU 1998041700732 19980417 00732 1998 4 17 98ZZZX1513 4 19980130 A 2211 7004206901 COMPUTER BOLKMS BK117 BK117C1 5626025 EU COCKPIT FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 117NC 85010121 7509 CSAS COMPUTER INTERMITTENT. ROLL AND PITCH CHANNELS BOTH DROP OFF-LINE AND CANNOT BE RESET OR JUST WILL NOT COME ON-LIN E. REMOVED AND REPLACED. 1 G 7 2 3U NC H13EU 1998041700735 19980417 00735 EU 1998 4 17 98ZZZX1516 1 19980111 A 6410 11731743 BLADE BOLKMS 117 BK117B1 5626012 EU T/R DEBONDED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 170MC 292 294 7217 TAIL ROTOR BLADE DEBONDING. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 1998041700736 19980417 00736 EU 1998 4 17 98ZZZX1517 1 19980205 A 3340 30050423 LIGHT BOLKMS 117 BK117B1 5626012 EU ANTI COLLISION FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 117LU 15 1278320 7144 ANTI-COLLISION STROBE INOPERATIVE. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 1998041700745 19980417 00745 CE 1998 4 17 98ZZZX1486 1 19980401 A 3230 AN17520 BOLT CESSNA 402 402C 207590R CE LT MLG TORQ LINK FAILED A A BR0A O OTHER O OTHER LD LANDING 1 WP 19 2616D 402C0115 PILOT WAS LANDING ACFT WITH A CROSSWIND FROM THE RIGHT. PILOT TOUCHED DOWN ON RIGHT MAIN GEAR FIRST, AND THEN ON THE LE FT. AS ACFT DECELERATED WITH LITTLE OR NO APPLIED BRAKING ACTION, IT STARTED TO WOBBLE AND VEERED TO THE LEFT COMING TO A STOP OFF OF THE LEFT HAND SIDE OF THE RUNWAY. APPARENTLY, THE LEFT HAND TORQUE LINKS ON THE MAIN GEAR HAD SEPARATED CAUSING THE ACFT TO VEER TO THE LEFT. THE BOLT FOR THE TORQUE LINKS WAS STILL IN THE LOWER LINK, AND THE NUT WAS FOUND CLOSE TO THE TOUCHDOWN SPOT. THE THREADS OF THE NUT WERE STTRIPPED AND PIECES OF THE COTTER PIN WERE STILL IN THE HOLE ON THE BOLT. 1 L 7 2 3O A7CE 1998041700747 19980417 00747 EA 1998 4 17 98ZZZX1488 2 19980210 A 7200 ENGINE DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA LEFT FAILED A GCNA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 19 177GC 23907 11918 263 PCE42149 LEFT ENGINE TORQUE PRESSURE DROPPED TO ZERO AFTER SLIGHT POWER REDUCTION, CAME BACK UP TO ABOUT 4 PSI, POWER INCREASED T O 15 PSI. AFTER ANOTHER SLIGHT POWER REDUCTION, TORQUE DROPPED TO ZERO AND OIL PRESSURE DROPPED BELOW 40 PSI. FEATHERE D AND SECURED ENGINE. ONCE ON GROUND, MAINTENANCE PERSONNEL RESTARTED ENGINE AND PERFORMED A THOROUGH GROUND RUN, AND C OULD NOT DUPLICATE PROBLEM OR FIND ANY DISCREPANCIES. REPLACED THE FUEL CONTROL UNIT AS A PRECAUTIONARY MEASURE BECAUSE NO DISCREPANCIES IN THE ENGINE, ENGINE ACCESSORIES, OR ENGINE SYSTEMS COULD BE FOUND. 1 H 7 2 3T 4 T A9EA E4EA 1998041700755 19980417 00755 EU 1998 4 17 98ZZZX1496 1 19980402 A 2820 FUEL FILTER BOLKMS 117 BK117B2 5626013 EU NR 2 ENG FILTER WARNING LIGHT A HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 132AE 7238 ON APRIL 2, 1998 AT 1236 IN CRUISE FLIGHT, NR 2 ENGINE FUEL FILTER LIGHT ILLUMINATED. RETURNED TO GLENDALE AIRPORT. TR OUBLESHOOTING IN PROGRESS. 1 G 7 2 3U NC H13EU 1998041700756 19980417 00756 EU 1998 4 17 98ZZZX1497 1 19980330 A 2821 430129501 FUEL FILTER BOLKMS 117 BK117B2 5626013 EU FUEL 1-2 CONTAMINATED A HEEA A UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS CR CRUISE 1 SW 03 132AE AFF1176 7238 ON MARCH 30, 1998 DURING CRUISE FLIGHT, NR 2 FUEL FILTER LIGHT CAME ON. PILOT TURNED A/C TO RETURN TO BASE. APPROXIMAT ELY 5 MINUTES LATER, THE NR 1 FUEL FILTER LIGHT ILLUMINATED. LANDED IN THE DESERT ONE MILE SOUTH OF WITTMAN, AZ. MAINT ENANCE SAMPLED FUEL, REPLACED FILTER ELEMENTS. NO ABNORMALITIES NOTED. REPLACED NR 1 ENGINE FUEL FILTER ASSY AND FUEL PUMP. SUSPECT ROOT CAUSE WAS MOISTURE IN BOTH ENGINE FUEL FILTER SWITCHES. (THERE HAD BEEN RECORD RAINFALL IN THE PREC EDING DAYS). 1 G 7 2 3U NC H13EU 1998041700758 19980417 00758 WP 1998 4 17 VJ9800116 1 19980410 A 3231 59149842 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG DOOR MALFUNCTIONED A ZZDA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 11 902VJ 47177 UPON RETRACTION OF LANDING GEAR AFTER TAKEOFF, EXPERIENCED AIRFRAME VIBRATION. AS PRECAUTIONARY MEASURE FLIGHT CREW ELE CTED TO RETURN TO IAD. ON ARRIVAL AT GATE FOUND RT NOSE GEAR DOOR OPEN. INSPECTED NOSE WHEEL AREA AND FOUND NO DAMAGE. CLOSED AND SECURED DOOR OPERATION IAW MM 32-22-1. 2 L 7 2 4F A6WE 1998041700759 19980417 00759 WP 1998 4 17 VJ9800117 1 19980411 A 5330 1A2680012IA26 SKIN DOUG DC9 DC932 3022066 WP BS 522 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 967VV 47170 DENT 2.5 X 6 X .0110 IN FUSELAGE AT FS 522, L29R. CUT OUT SKIN, FABRICATED DOUBLER, TREATED AND PRIMED DOUBLER REPAIR A ND FINGER DOUBLERS FROM 7075T6 .025 MATERIAL IAW DC9 SRM 51-30-2, 51-30-5 AND EO 98-845. 2 L 7 2 4F A6WE 1998041700760 19980417 00760 WP 1998 4 17 VJ9800118 1 19980203 A 5330 S293198330A06 SKIN DOUG DC9 DC932 3022066 WP BS 579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 CORROSION BULGE AT DOUBLER OF FUSELAGE BETWEEN L29R AND L30R, FS 579. REMOVED FASTENERS AND SKIN CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 53004, FIG 43. 2 L 7 2 4F A6WE 1998041700761 19980417 00761 WP 1998 4 17 VJ9800119 1 19980204 A 5321 59108209 FLOOR DOUG DC9 DC932 3022066 WP FS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 NUT PLATE ATTACH PLATE CORRODED BOTTOM SIDE CABIN FLOOR FS 218, BL 35. REMOVED AND REPLACED NUT PLATE IAW DC9 SRM 51-30 -2. FABRICATED DOUBLER IAW DC9 SRM 51-10-2. 2 L 7 2 4F A6WE 1998041700762 19980417 00762 WP 1998 4 17 VJ9800120 1 19980204 A 5320 591082011 NUT PLATE STRIP DOUG DC9 DC932 3022066 WP BS 446 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 NUT PLATE CONNECTOR STRIP CENTER FLOOR PANEL AT FS 446 CORRODED BEYOND LIMITS. REMOVED AND REPLACED NUT PLATE CONNECTOR STRIP IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041700763 19980417 00763 WP 1998 4 17 VJ9800121 1 19980204 A 5320 STRAP DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 BOTTOM OF LT AFT LINER STRAP IN AFT CARGO PIT CORRODED BEYOND LIMITS IAW DC9 SRM 53-01, FIG 1. FABRICATED, TREATED, PRI MED AND INSTALLED STRAP IAW DC9 SRM 51-10-3, 53-01 FIG 1, 51-30-0 AND 51-30-2. 2 L 7 2 4F A6WE 1998041700764 19980417 00764 WP 1998 4 17 VJ9800122 1 19980205 A 5320 BRACKET DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 TOP AND BOTTOM NUT PLATE CHANNEL LT ADF ANTENNA, SUPPORT BRACKET CORRODED BEYOND LIMITS IAW DC9 SRM 51-01, FIG 1. FABRI CATED SUPPORT BRACKET, TREATED, PRIMED AND INSTALLED NEW BRACKET IAW DC9 SRM 51-10-2 AND 51-30-1. 2 L 7 2 4F A6WE 1998041700765 19980417 00765 WP 1998 4 17 VJ9800123 1 19980205 A 2530 LID DOUG DC9 DC932 3022066 WP NR 4 GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 LID AND TOP EDGE FOOD CARRIER AT NR 4 GALLEY CORRODED. FABRICATED LID AND REPLACED FASTENERS IN LID IAW DC9 SRM 51-10-2 AND 51-30-0. 2 L 7 2 4F A6WE 1998041700766 19980417 00766 WP 1998 4 17 VJ9800124 1 19980206 A 5311 2652479 FRAME DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FASTENER HOLE IN FLOOR SUPPORT BEAM FS 160 BL 45R. Z=0, CORRODED BEYOND LIMITS IAW DC9 SRM 53-01, FIG 1. FABRICATED REP AIR ANGLE, INSTALLED ANGLE AND SHIMS IAW DC9 SRM 53-05, FIG 20A, 51-10-3, 51-10-2. 2 L 7 2 4F A6WE 1998041700767 19980417 00767 WP 1998 4 17 VJ9800125 1 19980208 A 5347 59108201 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-250 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 NR 2 SEAT TRACK, FS 200 TO 250, CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC9 SRM 51-30-1 AND 53-05, FIG 4. 2 L 7 2 4F A6WE 1998041700768 19980417 00768 WP 1998 4 17 VJ9800126 1 19980208 A 5347 59108201 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 275-325 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 NR 2 SEAT TRACK, FS 275 TO 325, BL 22L, CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED SEAT TRACK IAW DC9 SRM 51-30-1 AND 53-05, FIG 4. 2 L 7 2 4F A6WE 1998041700769 19980417 00769 WP 1998 4 17 VJ9800127 1 19980209 A 5320 7075T6 ANGLE DOUG DC9 DC932 3022066 WP BS 160-220 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOORBOARD ATTACH ANGLES, FS 160 TO 220, BL 55L, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. FABRICATED AND INSTALL ED ATTACH ANGLE IAW DC9 SRM 51-10-2, 51-30-1, 51-30-2. TREATED AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1998041700770 19980417 00770 WP 1998 4 17 VJ9800128 1 19980210 A 5320 5917579179 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 LT DOOR JAMB ANGLE, AFT PSGR DOOR, FS 996, BL 20L, CORRODED. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998041700771 19980417 00771 WP 1998 4 17 VJ9800129 1 19980213 A 5321 5910079 FLOOR DOUG DC9 DC932 3022066 WP COCKPIT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 BOTTOM FLOOR PANEL 4410 CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. FABRICATED AND BONDED NEW PART IAW DC9 SRM 51-1 0-2 AND 51-70-3. 2 L 7 2 4F A6WE 1998041700772 19980417 00772 WP 1998 4 17 VJ9800130 1 19980223 A 5321 59100801 FLOOR DOUG DC9 DC932 3022066 WP BS 130 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 11 905VV 47378 FLOOR PANEL, FS 130 CORRODED BEYOND LIMIT IAW DC9 SRM 53-01. REMOVED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-2 AND 51- 30-1. 2 L 7 2 4F A6WE 1998041700773 19980417 00773 NM 1998 4 17 RAAA98B2021 1 19980410 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998041700774 19980417 00774 SO 1998 4 17 RAAA98E4010 1 19980408 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 AFT RT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998041700775 19980417 00775 GL 1998 4 17 9806331228 2 19980406 A 7230 COMPRESSOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 3 ENGINE STALLED A NWAA E A F J ENGINE SHUTDOWN UNSCHED LANDING ACTIVATE FIRE EXT. DUMP FUEL R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 228NW 46578 455962 DURING TAKEOFF AT ROTATION, THE NR 3 ENGINE COMPRESSOR STALLED SEVERAL TIMES WITH VISIBLE FIRE REPORTED BY THE TOWER AND FLIGHT ATTENDANT. NOTICEABLE FUEL FLOW DECREASE AND POWER LOSS OCCURRED. BOTH FIRE BOTTLES FOR THE NR 3 ENGINE WERE D ISCHARGED AND THE ENGINE WAS SHUT DOWN. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO BOM AND LANDED WITHOUT FURTHER DIF FICUTLY. MAINTENANCE REPLACED THE ENGINE AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE A23EA 1998041700776 19980417 00776 WP 1998 4 17 9806349962 1 19980409 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 914RW 47362 DURING LINE CHECK, FOUND SERVICE DOOR AND FIRST CLASS EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BLOWN F USE AND TIGHTENED BATTERY PACK CONNECTIONS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700777 19980417 00777 WP 1998 4 17 9806359980 1 19980409 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE CHECK, FOUND EMERGENCY LIGHTS ABOVE BOTH FORWARD OVERWING EXITS WEAK. MAINTENANCE REPAIRED THE LEFT EMERGEN CY LIGHT AND REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700778 19980417 00778 WP 1998 4 17 9806369610 1 19980409 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 610NW 47432 DURING LINE CHECK, FOUND AFT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMA L. 2 L 7 2 4F A6WE 1998041700779 19980417 00779 EU 1998 4 17 9806373209 1 19980409 A 3350 CONNECTOR AIRBUS 320 A320211 3930320 EU CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309US 118 DURING TEST OF EMERGENCY LIGHTS, FOUND LIGHTS INOPERATIVE AT SEAT ROWS 19 TO 21ABC. MAINTENANCE SECURED CANNON PLUG AT SIDEWALL BELOW SEAT 19ABC, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998041700780 19980417 00780 EU 1998 4 17 9806383223 1 19980410 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 323US 23908 516 272 DURING TEST OF EMERGENCY LIGHT SYSTEM, RECEIVED FAULT RT OVERWING. MAINTENANCE REPLACED RIGHT OVERWING POLWER SUPPLY A ND BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998041700781 19980417 00781 NE 1998 4 17 9806391155 2 19980408 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 155US 46764 686175 AT TOP OF DESCENT, THE NR 3 ENGINE COMPRESSOR STALLED WHEN THE POWER LEVER WAS RETARDED. THE ENGINE ROLLED BACK AND THE EGT BEGAN TO RISE. EGT CLIMBED TO 810C AND THE ENGINE WAS SHUT DOWN. THE COM PROCEDURE WAS FOLLOWED AND A SUCCESSFUL RESTART WAS ACCOMPLISHED. THE ENGINE PERFORMED NORMALLY FOR THE REMAINDER OF THE FLIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE AND THE NR 3 ENGINE WAS CHANGED. 2 L 7 3 4F 4 F A22WE E20EA 1998041700782 19980417 00782 NM 1998 4 17 9806405516 1 19980411 A 7110 COWLING BOEING 757 757251 1384970 NM NR 1 ENGINE MISSING A NWAA A UNSCHED LANDING D E INFLIGHT SEPARATION VIBRATION/BUFFET CL CLIMB 1 GL 01 516US 23204 DURING CLIMB, CREW NOTICED A VIBRATION WHICH INCREASED IN INTENSITY COMING FROM THE LEFT SIDE OF THE AIRCRAFT. CREW ELE CTED TO RETURN TO DEPARTURE AIRPORT. GROUND MAINTENANCE FOUND A PORTION OF NR 1 ENIGNE INBOARD AFT COWL HAD LIBERATED F ROM AIRCRAFT. 2 L 7 2 4F RT A2NM 1998041700783 19980417 00783 WP 1998 4 17 9806411148 1 19980409 A 7830 TR UNIT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 148US 46757 686129 WHEN ENGINE POWER WAS ADVANCED TO THE TAKEOFF SETTING, THE NR 2 ENGINE THRUST REVERESER UNLOCK INDICATION ILLUMINATED. T HE TAKEOFF WAS ABORTED AT APPROXIMATELY 30 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER O N MEL 78-1A. 2 L 7 3 4F 4 F A22WE E20EA 1998041700784 19980417 00784 NE 1998 4 17 9806421143 2 19980409 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 133JC 46752 686171 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 980C FOR THREE SECO NDS BEFORE THE ENGINE WAS SHUT DOWN. A BORESCOPE WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS REMOVED FROM SE RVICE AND FERRIED TO MSP DUE TO SIMULTANEOUS STALL ON THE NR 3 ENGINE. 2 L 7 3 4F 4 F A22WE E20EA 1998041700785 19980417 00785 NE 1998 4 17 9806431143 2 19980409 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 133JC 46752 686167 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 980C FOR THREE SECO NDS BEFORE THE ENGINE WAS SHUT DOWN. A BORESCOPE WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS REMOVED FROM SE RVICE AND FERRIED TO MSP DUE TO SIMULTANEOUS STALL ON THE NR 1 ENGINE. 2 L 7 3 4F 4 F A22WE E20EA 1998041700786 19980417 00786 WP 1998 4 17 9806449154 1 19980410 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8913E 45830 DURING LINE CHECK, FOUND FORWARD CEILING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1998041700787 19980417 00787 WP 1998 4 17 9806459997 1 19980412 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 PILOT REPORTED FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F A6WE 1998041700788 19980417 00788 WP 1998 4 17 9806469986 1 19980412 A 3350 LIGHT DOUG DC9 DC932 3022066 WP TAIL CONE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE CHECK, FOUND ONE EMERGENCY LIGHT OUT AT TAIL CONE WALKWAY. MAINTENANCE REPLACED THE LIGHT ASSEMBLY MOUNT, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700789 19980417 00789 WP 1998 4 17 9806479930 1 19980411 A 3350 SOCKET DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 89S 47042 DURING LINE CHECK, FOUND SEAT ROW 12 RIGHT SIDE EMERGENCY PATHWAY LIGHTING INOPERATIVE. MAINTENANCE REPLACED LIGHT SOCK ET, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700790 19980417 00790 WP 1998 4 17 9806489917 1 19980412 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE CHECK, FOUND CATWALK EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1998041700791 19980417 00791 WP 1998 4 17 9806499877 1 19980411 A 3350 CHARGER DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND CATWALK EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGER, OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F RT A6WE 1998041700792 19980417 00792 WP 1998 4 17 9806509859 1 19980410 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS IN LAST 4 SEAT ROWS AND AN EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED F USE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041700793 19980417 00793 WP 1998 4 17 9806519851 1 19980410 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS AT SEAT ROWS 16 THRU 20 INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041700794 19980417 00794 WP 1998 4 17 9806529310 1 19980411 A 3350 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 313RC 48091 FLIGHT ATTENDANT REPORTED THE FORWARD FLASHLIGHT AT THE AFT FLIGHT ATTENDANT STATION INOPERAITVE. MAINTENANCE REPLACED THE FLASHLIGHT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041700795 19980417 00795 SO 1998 4 17 COMA9810088 1 19980402 A 5320 12005805003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST CENTER BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED P ART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700796 19980417 00796 SO 1998 4 17 COMA9810089 1 19980402 A 5320 12046963001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/01I, FOUND FIRST LEFT HAND BUTT STRAP CORRODED BEYOND EMB-LIMITS. REMOVED DAMAGED PA RT AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700797 19980417 00797 SO 1998 4 17 COMA9810090 1 19980402 A 5320 12005803001 SILL EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132 O1I, FOUND FIRST RIGHT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PAR T AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700798 19980417 00798 SO 1998 4 17 COMA9810091 1 19980402 A 5320 12046156001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST RIGHT BUTT STRAP CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PA RT AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700799 19980417 00799 SO 1998 4 17 COMA9810092 1 19980402 A 5320 12004149002 SUPPORT EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16R CORRODED BEYOND EMB LIMITS. REMOVED DAMA GED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700800 19980417 00800 SO 1998 4 17 COMA9810093 1 19980402 A 5320 12009846001 SUPPORT EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 16L CORRODED BEYOND EMB LIMITS. REMOVED DAMA GED PART AND INSTALLED SERV PART IAW EMB-120 SRM CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700801 19980417 00801 SO 1998 4 17 COMA9810094 1 19980402 A 5320 12006158002 SILL EMB 120 EMB120RT SO CARGO COMPT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 161/162-01Z, FOUND RIGHT CARGO FORWARD FLOOR SILL CORRODED BEYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700802 19980417 00802 SO 1998 4 17 COMA9810095 1 19980402 A 5320 12005802001 SILL EMB 120 EMB120RT SO CABIN DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FIRST LEFT FLOOR SILL CORRODED BYOND EMB LIMITS. REMOVED DAMAGED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700803 19980417 00803 SO 1998 4 17 COMA9810096 1 19980402 A 5320 12004149002 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132 01I, FOUND FLOOR SUPPORT-T AT FRAME 20L CORRODED BEYOND EMB LIMITS. REMOVED DAMA GED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700804 19980417 00804 SO 1998 4 17 COMA9810097 1 19980402 A 5320 12039724001 SILL EMB 120 EMB120RT SO EMERGENCY EXIT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 151/152-01Z, FOUND AFT EMERGENCY EXIT SILL AND PIN RECEPTACLES CORRODED BEYOND EMB LIMITS. RE MOVED DAMAGED PARTS AND INSTALLED SERV PARTS IAW EMB-120 SRM, CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700805 19980417 00805 SO 1998 4 17 COMA9810098 1 19980402 A 5320 12004149001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 244CA 120217 DURING 2C INSPECTION TASK 5310-131/132-01I, FOUND FLOOR SUPPORT-T AT FRAME 20R CORRODED BEYOND EMB LIMITS. REMOVED DAMA GED PART AND INSTALLED SERV PART IAW EMB-120 SRM, CHAPTER 51. 2 L 7 2 4T RT A31SO 1998041700806 19980417 00806 SO 1998 4 17 COMA9810099 1 19980409 A 3260 INTRANSIT LIGHT EMB 120 EMB120RT SO LT MLG ILLUMINATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 244CA 120217 LEFT HAND MLG INTRANSIT LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. ENTERED DISCREPANCY IN DEFERRED MAINTENANCE L OG PER MEL. 2 L 7 2 4T RT A31SO 1998041700807 19980417 00807 1998 4 17 COMA9810100 2 19980409 A 7510 38E966A VALVE EMB 120 EMB120RT SO LT ENG DE-ICE LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 249CA 120230 LEFT HAND BLEED AIR DUCT LEAK WARNING DURING FLIGHT. REPLACED LEAKING DE-ICE PRESSURE REGULATOR VALVE. 2 L 7 2 4T RT A31SO 1998041700808 19980417 00808 SO 1998 4 17 COMA9810101 1 19980408 A 2797 WIRE EMB 120 EMB120RT SO ELEV TRIM FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 257CA 120248 TAKEOFF TRIM WARNING DURING TAKEOFF. REPAIRED WIRE SPLICE IN ELEVATOR TRIM POSITION SENSOR SYSTEM. 2 L 7 2 4T RT A31SO 1998041700809 19980417 00809 EA 1998 4 17 COMA9860075 1 19980412 A 2820 7366438 COMPUTER CNDAIR CL600 CL6002B19 EA FUEL SYST MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 952CA 420 3743 7092 FUEL IMBALANCE MESSAGE DURING FLIGHT. REPLACED THE FUEL COMPUTER. 2 L 7 2 4F RT A21EA 1998041700810 19980417 00810 WP 1998 4 17 UPS98826387 1 19980402 A 5320 5779936 CLIP DOUG DC8 DC873F 302199F WP BS 1540 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, INTERCOSTAL TIE CLIP IS CRACKED AT STA 1540 AND STR 10. REMOVED FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 51-1-21 AND DWG 5779936. 2 L 7 4 4F RT 4A25 1998041700811 19980417 00811 WP 1998 4 17 UPS98826388 1 19980325 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 126.5-107.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, LT WING L/E UPPER SURFACE HAS HEAVY CORROSION AROUND FASTENERS AT FRONT SPAR BTWN STA'S XFS126.250 TO XFS107.500. REPAIRED AREA IAW SRKM 57-2-1 FIG 37. 2 L 7 4 4F RT 4A25 1998041700812 19980417 00812 WP 1998 4 17 UPS98826389 1 19980326 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 1.25-7.50 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, RT WING L/E AUX TANK I/B END ON TOP SKIN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED THE AREA IA W SRM 57-2-1 FIG 37. 2 L 7 4 4F RT 4A25 1998041700813 19980417 00813 WP 1998 4 17 UPS98826390 1 19980328 A 5320 4705211 FITTING DOUG DC8 DC873F 302199F WP BS 680-700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN STA 680 TO 700 AT STR 1, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND DWG 4750521. 2 L 7 4 4F RT 4A25 1998041700814 19980417 00814 WP 1998 4 17 UPS98826391 1 19980408 A 5320 975187951 ANGLE DOUG DC8 DC873F 302199F WP BS 310-330 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, WEB SUPPORT ANGLE IS CRACKED IN 2 PLCS AT STA 310 AND 330 STR 26L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLES IAW DWG 9751879 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041700815 19980417 00815 WP 1998 4 17 UPS98826392 1 19980325 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 20-45 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, LT WING L/E UPPER SURFACE HAS HEAVY CORROSION AROUND FASTENERS AT FRONT SPAR BTWN STA XFS20 TO XFS45. REPAIRED AREA IAW SRM 57-2-1 FIG 37. 2 L 7 4 4F RT 4A25 1998041700816 19980417 00816 WP 1998 4 17 UPS98826393 1 19980330 A 5320 47723591 FITTING DOUG DC8 DC873F 302199F WP BS 1520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1520 ON PIT CEILING AT BL 0, THE SEAT TRACK SUPPORT-T FITTING IS CRACKED. REMOVED, FABRICATED AN D INSTALLED REPLACEMENT FITTING IAW DWG 4772359 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041700817 19980417 00817 WP 1998 4 17 UPS98826394 1 19980326 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 735.00 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, RT WING L/E AT STA XFS.735.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998041700818 19980417 00818 WP 1998 4 17 UPS98826395 1 19980330 A 5320 5649028 DOUBLER DOUG DC8 DC873F 302199F WP BS 40-60 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, A/C INTERNAL DOUBLER STA 40 TO 60 AT STR 27R IS CORRODED. REMOVED FABRICATED AND INSTALLED REPLACEME NT DOUBLER IAW 8110-3 APPROVED DHC SK867-872. 2 L 7 4 4F RT 4A25 1998041700819 19980417 00819 WP 1998 4 17 UPS98826396 1 19980329 A 5714 47507182 FITTING DOUG DC8 DC873F 302199F WP BS 704 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, LOWER FUSELAGE EXTERIOR CENTER WING BOX AT STA 704, RBL 3, THE FITTING IS CRACKED. REMOVED, FABRICAT ED AND INSTALLED REPLACEMENT FITTING IAW DWG 4750718. 2 L 7 4 4F RT 4A25 1998041700820 19980417 00820 WP 1998 4 17 UPS98826397 1 19980329 A 5714 564667488 WEB DOUG DC8 DC873F 302199F WP BS 850 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, UPPER WING BOX AREA AT STA 850 RBL 65, BULKHEAD TO FUSELAGE WEB HAS A 3 INCH CRACK. REMOVED PRESSURE PANEL, FABRICATED REPLACEMENT PANEL AND INSTALLED IAW DWG 5646674. 2 L 7 4 4F RT 4A25 1998041700821 19980417 00821 WP 1998 4 17 UPS98826398 1 19980325 A 5320 4611067N FITTING DOUG DC8 DC873F 302199F WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, STA 70, LONGERON 30L END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041700822 19980417 00822 WP 1998 4 17 UPS98826399 1 19980331 A 5320 37799782 FITTING DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN AT STA 781 STR 18L, THE FRAME TO STR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INST ALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3779978. 2 L 7 4 4F RT 4A25 1998041700823 19980417 00823 WP 1998 4 17 UPS98826400 1 19980330 A 5320 37558471N FITTING DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1220 AT STR 33R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND DWG 3755847. 2 L 7 4 4F RT 4A25 1998041700824 19980417 00824 WP 1998 4 17 UPS98826401 1 19980331 A 5320 47504192 FITTING DOUG DC8 DC873F 302199F WP BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1140 AT STR 22R, SHEAR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FIT TING IAW DWG 4750419 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041700825 19980417 00825 WP 1998 4 17 UPS98826402 1 19980331 A 5320 37798742 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN AT STA 759 AND STR 13R, FRAME TO STR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INST ALLED REPLACEMENT FITTING IAW DWG 37798874 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041700826 19980417 00826 WP 1998 4 17 UPS98826403 1 19980330 A 5320 37558541 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1220 AT STR 27L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLAC EMENT FITTING IAW DWG 3755854-1. 2 L 7 4 4F RT 4A25 1998041700827 19980417 00827 WP 1998 4 17 UPS98826404 1 19980330 A 5313 561537757 LONGERON DOUG DC8 DC873F 302199F WP BS 1500-1520 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1500 TO 1520, STR 29L TOP FLANGE IS PART MISSING. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW DWG 5615377 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041700828 19980417 00828 WP 1998 4 17 UPS98826405 1 19980330 A 5320 3773077510 FITTING DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1300 AT STR 27R, THE FLOORBEAM SUPPORT FITTING HAS HEAVY CORROSION, CRACKING. REMOVED, FABRICATE D AND INSTALLED REPLACEMENT FITTING IAW DWG 3773077 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041700829 19980417 00829 WP 1998 4 17 UPS98826406 1 19980330 A 5320 37799782 FITTING DOUG DC8 DC873F 302199F WP BS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN AT STA 700, STR 13R, FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 5 1-1-21 AND DWG 3779978. 2 L 7 4 4F RT 4A25 1998041700830 19980417 00830 WP 1998 4 17 UPS98826407 1 19980403 A 5320 3641125501N FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN AT STA 759 LBL 47, ON TOP OF CENTER WING BOX, TIE FITTING IS CRACKED. REMOVED AND REPLACE D FITTING IAW DWG 3641125 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041700831 19980417 00831 WP 1998 4 17 UPS98826408 1 19980404 A 5320 37534882 FITTING DOUG DC8 DC873F 302199F WP BS 560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN AT STA 560 AND STR 21R, THE FRAME TO CUSP TIE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND DWG 3753488. 2 L 7 4 4F RT 4A25 1998041700832 19980417 00832 EU 1998 4 17 WWMA9800071 1 19980411 A 2611 72111211000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY DIRTY A WWMA O OTHER N FALSE WARNING CR CRUISE 1 WP 15 352SB 340B352 LAV SMOKE CWP LIGHT CAME ON FOR 5 MIN IN FLIGHT. FOLLOWED QRH PROCEDURES. CLEANED LAV SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998041700833 19980417 00833 1998 4 17 WWMA9800070 2 19980410 A 7200 ENGINE SAAB SF340 340B 7860101 EU NR 2 FIRE A WWMA F ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 WP 15 286AE 340B286 DURING START OF NR 2 ENGINE, THE RAMPER OBSERVED FLAMES COMING FROM THE ENGINE TAILPIPE. START WAS ABORTED AND FIRE HAN DLE WAS PULLED. RIGHT ENGINE FIRE BOTTLE WAS REPLACED AND SYSTEM CHECKED. 2 L 7 2 4T RT A52EU 1998041700834 19980417 00834 NE 1998 4 17 WWMA9800069 2 19980408 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT SMOKING A WWMA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 15 320AE 340B320 AIRCRAFT RETURNED TO THE GATE DUE TO REPORTS FROM RAMP PERSONNEL OF SMOKE COMIN G FROM THE RIGHT ENGINE COWLING. MAINTE NANCE INSPECTED THE RIGHT ENGINE, FOUND NO EVIDENCE OF SMOKE OR LEAKING FLUIDS. PERFORMED GROUND RUNS AND RELEASED THE AIRCRAFT FOR SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4T 4 T RT A52EU E8NE 1998041700835 19980417 00835 EU 1998 4 17 QXEA900499 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 13815 HAS A CRACKED CLIP AT STRINGER 33. COMPLIED WITH REPAIR IAW FOKKER SRM 53-02-13 PA GE 6 FIGURE 2 AND SRM 51-31-01 FOR SOLID FASTENERS. 2 L 7 2 4F RT A20EU 1998041700836 19980417 00836 EU 1998 4 17 QXEA9800472 1 19980226 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY CRUSHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 ABOVE REAR CARGO BAY ENTRANCE THE SUPPORT STRUCTURE HAS BEEN CRUSHED. REPAIRED IAW HORIZON AIR EA 4-53-374. 2 L 7 2 4F RT A20EU 1998041700837 19980417 00837 EU 1998 4 17 QXEA9800473 1 19980303 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 THERE WAS A CRACK AND LIGHT SURFACE CORROSION AT STRINGER 1 FRAME 15205 ON CASTELLATION (CLIP). REPAIRED CRACK AND REMO VED CORROSION IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998041700838 19980417 00838 EU 1998 4 17 QXEA9800474 1 19980302 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISSING A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 488US 11240 REWORK OF CLIP REPAIR REQUIRES RIVETS INSTALL INTO CLIP REPAIR. INSTALLED THREE MISSING RIVETS IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998041700839 19980417 00839 EU 1998 4 17 QXEA9800475 1 19980304 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CORROSION ON RIGHTHAND INBOARD SEAT TRACK AT FRAME 4610 APPROXIMATELY 5 INCH LENGTH. REMOVED AND REPLACED SEAT TRACK PE R FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998041700840 19980417 00840 EU 1998 4 17 QXEA9800476 1 19980302 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED AT FRAME 10346 BETWEEN STRINGER 36 AND 37. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 AND FOKKER SRM 51-31- 01. 2 L 7 2 4F RT A20EU 1998041700841 19980417 00841 EU 1998 4 17 QXEA9800477 1 19980224 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED ON AFT SIDE OF FRAME 10346 AT STRINGER 443. INSTALLED REPAIR IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998041700842 19980417 00842 EU 1998 4 17 QXEA9800478 1 19980224 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 CLIP CRACKED AT AFT SIDE OF FRAME 10346 STRINGER 43. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998041700843 19980417 00843 EU 1998 4 17 QXEA9800479 1 19980303 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 22293 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FUSELAGE FRAME 22293 IS CRACKED AT STRINGER 54. REPAIRED IAW HORIZON AIR EA 4-53-388. 2 L 7 2 4F RT A20EU 1998041700844 19980417 00844 EU 1998 4 17 QXEA9800480 1 19980305 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 BORE FOR LOWER BUSHING IN LEFTHAND SPEED BRAKE SUPPORT LINK IS WORN OVERSIZE. BUSHING IS ALSO WORN OVERSIZE AND REQUIRE S REPLACEMENT. REPAIRED LOWER BUSHING BORE IAW HORIZON AIR EA 4-27-29, STEP 1 AND 3. 2 L 7 2 4F RT A20EU 1998041700845 19980417 00845 EU 1998 4 17 QXEA9800481 1 19980305 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 BORE FOR UPPER BUSHING IN LEFTHAND SPEED BRAKE SUPPORT LINK IS STEP-WORN AND WILL REQUIRE REPAIR TO RE-BUSH. BUSHING IS ALSO WORN OVERSIZE. REPAIRED UPPER BUSHING BORE IAW HORIZON AIR EA 4-27-29, STEP 1 AND 3. 2 L 7 2 4F RT A20EU 1998041700846 19980417 00846 EU 1998 4 17 QXEA9800482 1 19980315 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FLANGE CRACKED ON FRAME CLIP THROUGH STOP DRILL AT FRAME 17565 STRINGER 23. INSTALLED SOLID RIVETS IAW FOKKER SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1998041700847 19980417 00847 EU 1998 4 17 QXEA9800483 1 19980315 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FLANGE CRACKED ON FRAME CLIP THROUGH STOP DRILL, AT FRAME 17565 STRINGER 24. INSTALLED SOLID RIVETS IAW FOKKER SRM 51-3 1-01. 2 L 7 2 4F RT A20EU 1998041700848 19980417 00848 EU 1998 4 17 QXEA9800484 1 19980315 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FLANGE CRACKED ON FRAME CLIP THROUGH STOP DRILL AT FRAME 17565 STRINGER 25. INSTALLED SOLID RIVETS IAW SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998041700849 19980417 00849 EU 1998 4 17 QXEA9800485 1 19980315 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 FLANGE CRACKED THROUGH STOP DRILL ON FRAME 17565 STRINGER 26. INSTALLED SOLID RIVETS IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998041700850 19980417 00850 EU 1998 4 17 QXEA9800486 1 19980226 A 5311 RIB FOKKER F28 F28MK4000 4990810 EU BS 4790 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 WING TAILBOX RIB AT STATION 4790 IS CRACKED THROUGH TWO RIVETS ATTACHING SPRING STRUT BRACKET TO RIB SEEN THROUGH LOWER TAIL SKIN LIGHTNING HOLE. INSTALLED NEW PLATE AND CRACK CONTAINMENT IAW HORIZON AIR EA 4-57-96. 2 L 7 2 4F RT A20EU 1998041700851 19980417 00851 EU 1998 4 17 QXEA9800487 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12875 HAS A CRACKED CLIP AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGUR E 2. 2 L 7 2 4F RT A20EU 1998041700852 19980417 00852 EU 1998 4 17 QXEA9800488 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12875 HAS A CRACKED CLIP AT STRINGER 42. INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700853 19980417 00853 EU 1998 4 17 QXEA9800489 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12875 HAS CRACKED CLIP AT STRINGER 43. INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-13, PA GE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700854 19980417 00854 EU 1998 4 17 QXEA9800490 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12875 HAS A CRACKED CLIP AT STRINGER 46. INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4 AND FOKKER SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998041700855 19980417 00855 EU 1998 4 17 QXEA9800491 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12405 HAS A CRACKED CLIP AT STRINGER 31. INSTALLED REPAIR CLIP AIW FOKKER SRM 53-02-13, FIGURE 2 PAGE 4. 2 L 7 2 4F RT A20EU 1998041700856 19980417 00856 EU 1998 4 17 QXEA9800492 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12405 HAS CRACKED CLIP AT STRINGER 33. INSTALLED REPAIR IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700857 19980417 00857 EU 1998 4 17 QXEA9800493 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12405 HAS A CRACKED CLIP AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700858 19980417 00858 EU 1998 4 17 QXEA9800494 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 12405 HAS A CRACKED CLIP AT STRINGER 42. INSTALLED REPAIR ANGLE IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700859 19980417 00859 EU 1998 4 17 QXEA9800495 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 11405 HAS A CRACKED CLIP AT STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700860 19980417 00860 EU 1998 4 17 QXEA9800496 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 11405 HAS A CRACKED CLIP AT STRINGER 32. FABRICATED REPAIR CLIP ETCHED, ALODINED, PRIMED AND INSTALLED IAW FOKKER SRM 53-02-13, PAGE 4 FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700861 19980417 00861 EU 1998 4 17 QXEA9800497 1 19980321 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 13815A HAS A CRACKED CLIP AT STRINGER 46. INSTALLED SOLID RIVETS IAW FOKKER SRM 51-31-01 . 2 L 7 2 4F RT A20EU 1998041700862 19980417 00862 EU 1998 4 17 QXEA9800498 1 19980320 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 13815 HAS A CRACKED CLIP AT STRINGER 43. COMPLIED WITH REPAIR AIW FOKKER 53-02-13, PAGE 6, FIGURE 2 AND FOKKER 51-31-01 FOR SOLID FASTENERS. 2 L 7 2 4F RT A20EU 1998041700863 19980417 00863 EU 1998 4 17 QXEA9800500 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER FUSELAGE FRAME 9305 HAS A CRACKED CASTELLATION AT STRINGER 47. INSTALLED REPAIR CLIP AIW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998041700864 19980417 00864 EU 1998 4 17 QXEA9800501 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE I FLT. ATTITUDE INST. IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER FUSELAGE FRAME 9305 HAS A CRACKED CASTELLATION AT STRINGER 45. INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-123 , PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700865 19980417 00865 EU 1998 4 17 QXEA9800502 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 8805 HAS A CRACKED CASTELLATION AT STRINGER 48. INSTALLED REPAIR CLIP IAW FOKKER SRM 53- 02-13, PAGE 4, FIG 2. 2 L 7 2 4F RT A20EU 1998041700866 19980417 00866 EU 1998 4 17 QXEA9800503 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 6305 HAS A CRACKED CASTELLATION AT STRINGER 39. MANUFACTURED AND INSTALLED REPAIR CLIP I AW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700867 19980417 00867 EU 1998 4 17 QXEA9800504 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 6305 HAS A CRACKED CASTELLATION AT STRINGER 40. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 , FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700868 19980417 00868 EU 1998 4 17 QXEA9800505 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 6305 HAS A CRACKED CASTELLATION AT STRINGER 41. REPAIRED IAW FOKKER SRM 51-02-13, PAGE 4 , FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700869 19980417 00869 EU 1998 4 17 QXEA9800506 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 6305 HAS A CRACKED CASTELLATION AT STRINGER 43. MANUFACTURED AND INSTALLED REPAIR CLIP I AW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700870 19980417 00870 EU 1998 4 17 QXEA9800507 1 19980321 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 5305 HAS A CRACKED CASTELLATION AT STRINGER 43. COMPLETED REPAIRS IAW FOKKER SRM 53-02-1 3, PAGE 6, FIGURE 2 AND FOKKER SRM 51-31-01 FOR SOLID RIVETS. 2 L 7 2 4F RT A20EU 1998041700871 19980417 00871 EU 1998 4 17 QXEA9800508 1 19980322 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 10346 HAS A CRACKED CASTELLATION AT STRINGER 44. FABRICATED AND INSTALLED REPAIR CLIP IA W FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700872 19980417 00872 EU 1998 4 17 QXEA9800509 1 19980322 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 10346 HAS A CRACKED CASTELLATION AT STRINGER 43. FABRICATED AND INSTALLED REPAIR CLIP IA W FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700873 19980417 00873 EU 1998 4 17 QXEA9800510 1 19980322 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10364 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 10346 HAS A CRACKED CASTELLATION AT STRINGER 32. FABRICATED AND INSTALLED CABIN CLIP IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700874 19980417 00874 EU 1998 4 17 QXEA9800511 1 19980322 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 10346 HAS A CRACKED CASTELLATION AT STRINGER 31. FABRICATED AND INSTALLED CABIN CLIP IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700875 19980417 00875 EU 1998 4 17 QXEA9800512 1 19980322 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER FUSELAGE FRAME 9305A HAS A CRACKED CASTELLATION AT STRINGER 47. INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-13 , PAGE 4, FIGURE 2 AND MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998041700876 19980417 00876 EU 1998 4 17 QXEA9800513 1 19980322 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PASSENGER CABIN FUSELAGE FRAME 9305A HAS A CRACKED CASTELLATION AT STRINGER 34. REPAIRED CASTELLATION IAW FOKKER SRM 53 -02-13, FIGURE 2, PAGE 6. 2 L 7 2 4F RT A20EU 1998041700877 19980417 00877 EU 1998 4 17 QXEA9800514 1 19980327 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 FRAME CLIP AT FRAME 6305 STRINGER 15 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998041700878 19980417 00878 EU 1998 4 17 QXEA9800515 1 19980327 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 FRAME CLIP AT FRAME 5805 STRINGER 15 CRACKED. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, PAGE 4. 2 L 7 2 4F RT A20EU 1998041700879 19980417 00879 EU 1998 4 17 QXEA9800516 1 19980323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 58.5-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 CLIP IS CRACKED BACKSIDE FRAME 58.5-2 ABOVE STRINGER 44. INSTALLED CLIP IAW FOKKER SRM 53-02-13, FIGURE 6 WITH FASTENER S IAW MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998041700880 19980417 00880 EU 1998 4 17 QXEA9800517 1 19980323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 58.5-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 PREVIOUS CLIP REPAIR CRACKED BACKSIDE FRAME 58.5-2 ABOVE STRINGER 31. INSTALLED CLIP IAW FOKKER SRM 53-02-13, FIGURE 6 WITH FASTENERS IAW MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998041700881 19980417 00881 EU 1998 4 17 QXEA9800518 1 19980323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 CLIP CRACKED BACKSIDE FRAME 50-2 ABOVE STRINGER 40. PERFORMED CLIP REPAIR IAW FOKKER SRM 53-02-13, FIGURE 4. 2 L 7 2 4F RT A20EU 1998041700882 19980417 00882 EU 1998 4 17 QXEA9800519 1 19980323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 CLIP IS CRACKED IN RADIUS FRAME 50-2 STRINGER 29. INSTALLED CLIP IAW FOKKER SRM 53-02-13, FIGURE 6. 2 L 7 2 4F RT A20EU 1998041700883 19980417 00883 EU 1998 4 17 QXEA9800520 1 19980323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 CLIP HAS 2 CRACKS ONE IN RADIUS BACKSIDE FRAME 41-2 STRINGER 31. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 8, FIGURE 6. 2 L 7 2 4F RT A20EU 1998041700884 19980417 00884 EU 1998 4 17 QXEA9800521 1 19980323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 CLIP CRACKED PAST STOP DRILL BACKSIDE OF FRAME 41-2 STRINGER 39. INSTALLED ANGLE IAW FOKKER SRM 53-02-13, FIGURE 6, PAG E 8 WITH FASTENERS IAW MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998041700885 19980417 00885 EU 1998 4 17 QXEA9800522 1 19980323 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 477AU 11226 CLIP CRACKED FRONTSIDE FRAME 50-2 STRINGER 47. INSTALLED REPAIR ANGLE IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998041700886 19980417 00886 WP 1998 4 17 RRXA98076 1 19980409 A 3230 47783031 PIN DOUG DC8 DC862 3021970 WP LT MLG BROKEN A RRXA O OTHER J WARNING INDICATION CL CLIMB 1 WP 15 990CF 46068 DOORS AND LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER GEAR HANDLE WAS PLACED IN THE UP POSITION. TOWER REPORT ED LEFT MAIN LANDING GEAR DOWN. HYDRAULIC PRESSURE AND QUANTITY GOOD, THREE GEAR PINS ON BOARD. AIRCRAFT GEAR CYCLED O NCE TOWER REPORTED GEAR (LEFT) STILL DOWN. REMOVED AND REPLACED LMLG BOSS PIN IAW UAL DC-8 M/M 32-11-62 AND PERFORMED L MG OPS CHK IAW DC-8 M/M 32-32-2. 2 L 7 4 4F 4A25 1998041700887 19980417 00887 1998 4 17 VNAA9804008 4 19980410 A 3418 861EF1 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE MALFUNCTIONED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 442JS 3060 DURING THE TAKEOFF ROLL, AN ANGLE OF ATTACK MISCOMPARE WARNING MESSAGE ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AI RCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND PERFORMED A SYSTEMS OPERATIONAL CHECK, IN ACCORDANCE WITH DORNIE R MAINTENANCE MANUAL 27-33-00. NO PROBLEMS WERE NOTED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998041700888 19980417 00888 NM 1998 4 17 TSAA9833176 1 19980314 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041700889 19980417 00889 NM 1998 4 17 TSAA9833177 1 19980314 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041700890 19980417 00890 NM 1998 4 17 TSAA9833178 1 19980314 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041700891 19980417 00891 NM 1998 4 17 TSAA9833179 1 19980314 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041700892 19980417 00892 NM 1998 4 17 TSAA9833180 1 19980314 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041700893 19980417 00893 NM 1998 4 17 TSAA9833181 1 19980314 A 3397 WIRE BOEING 737 737297 1384480 NM CABIN BROKEN A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT IDENTIFIER INOP. WIRE FOUND BROKEN AT CONNECTOR, RECONNECTED WIRE SYSTEM CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998041700894 19980417 00894 NM 1998 4 17 TSAA9833185 1 19980320 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 DURING SERVICE CHECK, FOUND POSITION NR 4 EMEREGNCY FLOOR LIGHT WEAK. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998041700895 19980417 00895 EU 1998 4 17 VTZA98138 4 19980319 A 3425 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 325UE 41063 FLT 6236 - BOS-BWI - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FO'S EFIS SCREENS WENT BLANK. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SYMBOL GENERATOR, OPS CHECK O K. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998041700896 19980417 00896 EU 1998 4 17 VTZA98126 1 19980310 A 2150 1718D000 ACM JETAIR JETSTM JETSTM4101 1500501 EU AFT FUSELAGE FAILURE A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 332UE 41100 FLT 6392 - IAD-BOS - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO DUCT OVERTEMP WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND OPENED DMI 46505, MEL 21-1 ON RT PACK. MAINTENANCE CLOSED DMI 46505 ON 3-14-98 BY REMOVING AND REPLACING RT ACM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998041700897 19980417 00897 1998 4 17 VTZA9139 4 19980320 A 3442 6227337001 RADAR RT BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 470UE 814 FLT 6357 - IAD-RDU - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RADAR FAILURE. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RADAR RT, OPS CHECK OK. AIRCRAFT WAS RELEAS ED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998041700898 19980417 00898 1998 4 17 VTZA98141 4 19980324 A 6122 8210263 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 471UE 821 IAD/CLE - FLT 6551 - DURING CLIMB AT 1740 HOURS ON 3-24-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE TORQUE AND RPM FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLAC ED PROPELLER GOVERNOR, OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998041700899 19980417 00899 EA 1998 4 17 VTZA98140 1 19980320 A 5350 6003303881 RADOME CNDAIR CL600 CL6002B19 EA FWD FUSELAGE DAMAGED A VTZA O OTHER C F.O.D. CR CRUISE 1 EA 27 624BR 7211 FLT 6718 - ATL-IAD - DURING CRUISE, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH AIRCRAFT WAS DAMAGED B Y HAIL AND A/C HAD A ENGINE SHUTDOWN DUE TO FLAMEOUT. ENGINE WAS RESTARTED WITH NO PROBLEMS INDICATING. AIRCRAFT LANDE D AT IAD AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND MAINTENANCE REMOVED AND REPLACED RADOME, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998041700900 19980417 00900 WP 1998 4 17 TWAA9804603 1 19980327 A 2170 COALESCER DOUG DC9 DC983 3022083 WP CABIN DIRTY A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 9305N 49395 LGA - FLT 293 - AFTER TAKEOFF SMOKE FILLED CABIN AND COCKPIT WITH ODOR AND LIGHT HAZY SMOKE. FLIGHT RETURNED TO LGA. F OUND AIR COND PACK COALESCER BAGS CLOGGED BY DEBRIS FROM BIRD INJESTION. PERFORMED PACK BURNOUT AND REPLACED BOTH COALE SCER BAGS. PERFORMED ECS HEALTH CHECK. (M) 2 L 7 2 4F RT A6WE 1998041700901 19980417 00901 NM 1998 4 17 TWAA9804602 1 19980329 A 2530 OVEN BOEING 727 727231 1384079 NM GALLEY DIRTY A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 54345 21632 STL - FLT 492 - SMOKE WAS COMING FROM FWD LEFT OVEN IN FWD GALLEY. CREW TURNED OVEN OFF AND PULLED CB. FOUND FOOD STUC K ON OVEN RACK. REPLACED OVEN RACK. CHECK-C 6-1-97 MCI. (M) 2 L 7 3 4F A3WE 1998041700902 19980417 00902 NE 1998 4 17 TWAA9804601 2 19980327 A 7314 3782017 FUEL PUMP BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A TWAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 CE 05 54333 20460 4020 DFW - FLT 178 - NR 1 ENGINE FAILED AT APPROX 1200 FEET DURING TAKEOFF. ENGINE SPOOLED DOWN. RETURNED TO DFW. FUEL PUM P FAILURE. REPLACED FUEL PUMP AND JFC. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998041700909 19980417 00909 SO 1998 4 17 WTAA980052 1 19980325 A 3260 922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO NLG INTERMITTENT A WTAA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 17 221YV 120221 BFL - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURN TO STATION WITHOUT INCIDENT. MAINTENANCE REPLACED RT MAIN LANDING GEAR 'A' SYSTEM UPLOCK PROXIMITY SENSOR. LANDING GEAR OPERATIONAL NORMAL DURING GROUND CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041700910 19980417 00910 SO 1998 4 17 WTAA980048 1 19980318 A 3260 922FS2A6NZ735 PROX SENSOR EMB 120 EMB120RT SO NLG FAILED A WTAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 17 284YV 120284 SBA - LANDING GEAR FAILED TO RETRACT ON DEPARTURE. AIRCRAFT RETURN TO STATION WITHOUT INCIDENT. MAINTENANCE REMOVED AN D REPLACED NOSE GEAR SHOCK ABSORBER PROXIMITY SENSOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041700911 19980417 00911 SO 1998 4 17 WTAA980050 1 19980320 A 3260 922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO NLG INTERMITTENT A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 250YV 120250 LAX - LANDING GEAR FAILED TO EXTEND ON INITIAL ATTEMPT. CREW ACCOMPLISHED GEAR EXTENSION USING ELECTRICAL OVERRIDE PROC EDURES. AIRCRAFT LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE LANDING GEAR 'A' SYSTEM UPLOCK PROXIMITY SENSOR. LANDING GEAR EXTENSION AND RETRACTION OPERATIONAL CHECK NORMAL DURING GEAR SWING. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041700912 19980417 00912 SO 1998 4 17 WTAA980051 1 19980321 A 3260 922AA2YA6PZ722 PROX SENSOR EMB 120 EMB120RT SO NLG INTERMITTENT A WTAA O OTHER N FALSE WARNING AP APPROACH 1 WP 17 250YV 120250 LAX - LANDING GEAR FAILED TO EXTEND ON INITIAL ATTEMPT. GEAR SELECTED DOWN USING OVERRIDE PROCEDURES. MAINTENANCE REPL ACED NOSE LANDING GEAR 'A' SYSTEM DOWN LOCK PROXIMITY SENSOR. LANDING GEAR OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998041700913 19980417 00913 EU 1998 4 17 WTAA980049 1 19980320 A 3230 1847F RADIUS ROD BAG JETSTM JETSTM3101 1500215 EU LT MLG WORN A WTAA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 17 425UE 798 SFO - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINS ILLUMINATED AFTER GEAR RETRACTION. MAINTENANCE REMOVED AND REPLAC ED LEFT MAIN RADIUS ROD. LANDING GEAR OPERATIONAL CHECK NORMAL. AIRCRAFT RETURN TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998041700914 19980417 00914 SO 1998 4 17 WTAA980053 1 19980325 A 3260 12038594001 CONTROL MODULE EMB 120 EMB120RT SO COCKPIT FAILED A WTAA K NONE N FALSE WARNING TO TAKEOFF 1 WP 17 221YV 120221 SFO - RIGHT MAIN LANDING GEAR 'B' SYSTEM INTRANSIT LIGHT REMAINS ILLUMINATED FOLLOWING GEAR RETRACTION. MAINTENANCE DEF ERRED 'B' SYSTEM GEAR POSITION INDICATION PER MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEA RED DEFERRAL BY REPLACING LANDING GEAR CONTROL MODULE. PERFORMED GEAR SWING. OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1998041700915 19980417 00915 NE 1998 4 17 TWRA9815 2 19980328 A 7230 COMPRESSOR BOEING 747 747282B 1384860 NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE STALLED A A TWRA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 15 611FF 20502 662217 IN CRUISE, SUSPECT COMPRESSOR STALL NR 3 ENGINE FOLLOWED BY POWER LOSS AND FLAME OUT. VIBRATION REPORTED BY FLIGHT ATTE NDANTS AT TIME OF POWER LOSS. NO EGT OR ENGINE PARAMETERS EXCEEDED. ENGINE SHUT DOWN 1540Z. RELIGHT AT 1545Z, OPS NOR MAL REMAINDER OF FLT. REMOVED AND REPLACED MAIN FUEL FILTERS, CONDUCTED BOROSCOPE INSPECTION. NO DISCREPANCY NOTED. I NSPECTED INLET AND EXHAUST SECTIONS, LEAK CHECK PERFORMED, NONE NOTED MM REF 71-00-00 AND 72-00-00. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998041700916 19980417 00916 NM 1998 4 17 TAOA039803 1 19980316 A 3350 07912 LAMP BOEING 727 727225 1384077 NM CABIN MISSING A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 20447 FLT 6030 - LGA-BOS - ONE WHITE ELP LIGHT INOPERATIVE AT ROW 5. REPAIRED BROKEN WIRE, REPLACED BULB AND CAPSULE, OPERATI ONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998041700917 19980417 00917 NM 1998 4 17 TAOA039804 1 19980316 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 924TS 21041 FLT 6141 - BOS-LGA - RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK AND BASE ASSEMBLY, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998041700918 19980417 00918 NM 1998 4 17 TAOA039807 1 19980325 A 3350 110049 BATTERY CHARGER BOEING 727 727225 1384077 NM CABIN FAILED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 919TS 6299 20447 FLT 6140 - BOS, OVERNIGHT L/S CHECK, FORWARD SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY CHARGER, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998041700919 19980417 00919 NM 1998 4 17 TAOA039808 1 19980325 A 3350 20131A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS 20441 FLT 6530 - OVERNIGHT LGA, L/S CHECK, AFT SECTION OF EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK, OPERATI ONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998041700920 19980417 00920 NM 1998 4 17 NOCA0798 1 19980313 A 5210 RESERVOIR BOEING 757 75723A 1384967 NM PAX DOOR MALFUNCTIONED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 757NA 24567 R-4 DOOR SLIDE INADVERTENTLY DEPLOYED ON GROUND AT JFK. SLIDE/RAFT OPERATION NORMAL. INSPECTED AREA AND REPLACED R-4 D OOR SLIDE/RAFT. REPLACED DOOR ASSIST RESERVOIR. PERFORMED REQUIRED INSPECTION FUNCTIONS ON DOOR SLIDE/RAFT AND DOOR AS SIST RESERVOIR, CHECKED OK. (M) 2 L 7 2 4F RT A2NM 1998041700921 19980417 00921 NM 1998 4 17 MZZA98095 1 19980217 A 5720 6516275 ANGLE BOEING 727 727264 138408M NM RT WING CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - NR 6 KRUEGER LEADING EDGE FLAP ACTUATOR TRUNNION MOUNTING BOX STRUCTURE FOUND CRACKED AT INBOARD LOWER AND OUTBOAR D UPPER CORNERS. INBOARD AND OUTBOARD ANGLES FABRICATED IAW BOEING DRAWING 65-16275 AND INSTALLED IAW SRM 51-30-2. ACT UATOR REINSTALLED AND FUNCTIONAL CHECK CUTOUT. (M) 2 L 7 3 4F A3WE 1998041700922 19980417 00922 NM 1998 4 17 MZZA98096 1 19980218 A 2810 10614212 GASKET BOEING 727 727264 138408M NM LT/RT WING MISSING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - ALL LEFT AND RT NON STRESSED WING FUEL TANK PANELS FOUND WITH MISSING KNITTED BONDING GASKETS, FOLLOWING PANEL REM OVAL. NEW KNITTED GASKETS INSTALLED IAW MM 28-11-21. (M) 2 L 7 3 4F A3WE 1998041700923 19980417 00923 NM 1998 4 17 MZZA98097 1 19980223 A 2750 69139082 SPRING BOEING 727 727264 138408M NM RT TE FLAP BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - RIGHT INBOARD FOREFLAP INBOARD SEQUENCE CARRIAGE TOGGLE DETENT SPRING BROKEN. SPRING REPLACED IAW MM 27-51-4. FU NCTIONAL CHECK CUTOUT SATISFACTORY. (M) 2 L 7 3 4F A3WE 1998041700924 19980417 00924 NM 1998 4 17 MZZA98098 1 19980221 A 3211 65821531 BUSHING BOEING 727 727264 138408M NM LT MLG CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - LEFT MLG AFT RUNNION BUSHING FOUND, HAS SIGN OF CORROSION. LEFT MLG AFT TRUNNION BUSHING REPLACED IAW SRM 20-50-0 3. (M) 2 L 7 3 4F A3WE 1998041700925 19980417 00925 NM 1998 4 17 MZZA98099 1 19980218 A 5713 STRINGER BOEING 727 727264 138408M NM WS 656.5 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - CRACK AT 'Z' SECTION AT WS 656.5 AT AFT OF VENT BOX, MOUNTING POINT BETWEEN 'Z' SECTION AND WEB LT WING. FABRICAT ED EXTRUSION IAW EA 5762-01050. ALODINED AND PRIME IAW 51-20-2. INSTALLED EXTRUSION IAW EA 5762-01050. (M) 2 L 7 3 4F A3WE 1998041700926 19980417 00926 NM 1998 4 17 MZZA98100 1 19980218 A 5713 STRINGER BOEING 727 727264 138408M NM WS 686.5 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - CRACK AT 'Z' SECTION AT WS 686.5 AT AFT OF VENT BOX, MOUNTING POINT BETWEEN 'Z' SECTION AND WEB LEFT WING. FABRIC ATED EXTRUSION IAW EA 5762-01050. ALODINED AND PRIME IAW 51-20-2. INSTALLED EXTRUSION IAW EA 5762-01050. (M) 2 L 7 3 4F A3WE 1998041700927 19980417 00927 NM 1998 4 17 MZZA98101 1 19980302 A 2710 CONTROL CABLE BOEING 727 727264 138408M NM RT WING MISINSTALLED A MZZA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 623DH 20895 KUL - RT AILERON BODY CABLE SYSTEM, AFT QUADRANT ABOVE RT WHEEL WELL FOUND TO HAVE CABLES INSTALLED ON WRONG GROOVES IAW MM 27-61-11, PARA 71 PLS NOTE THAT RETAINERS STILL HAD ORIGINAL BOEING TAMPER PROOF SEALANT. CABLES SWAPPED IN GROOVES IAW MM 27-62-11, BODY RIGGED AND SYSTEM TESTED IAW MM 27-61-11. (M) 2 L 7 3 4F A3WE 1998041700928 19980417 00928 NM 1998 4 17 MZZA98102 1 19980220 A 2710 65247338 DRUM BOEING 727 727264 138408M NM AILERON CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - LOST MOTION DEVICE UPPR CABLE DRUM FOUND CRACKED AT CABLE RETAINER SLOT. DRUM REPLACED IN LOST MOTION DEVICE IAW OHM 27-10-03. (M) 2 L 7 3 4F A3WE 1998041700929 19980417 00929 NM 1998 4 17 MZZA98103 1 19980223 A 2782 6516275 MOUNTING BOX BOEING 727 727264 138408M NM NR 2 LE FLAP ACT CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - CRACK ON NR 2 KRUEGER FLAP ACTUATOR MOUNTING BOX ON LOWER OUTBOARD SIDE. LEFT WING NR 2 LE FLAP ACTUATOR MOUNTING BOX OUTBOARD WEB FABRICATED IAW 727 DWG 65-16275. ALODINED AND PRIMED IAW MM 51-20-2. REMOVED AND INSTALLED WITH NEW WEB IAW SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998041700930 19980417 00930 NM 1998 4 17 MZZA98104 1 19980217 A 5754 651729326 RIB BOEING 727 727264 138408M NM NR 6 LE SLAT CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - NR 6 SLAT HAS CRACKING IN THE FOLLOWING PLACES UPPER SKIN AT OUTBOARD HOOK AFT FASTENER HOLE (2 CRACKS), EYE END A TTACH INBOARD RIB AT UPPER FWD CORNER AND LOWER AFT CORNER. REPAIR CARRIED OUT TO THE UPPER SKIN OF OUTBOARD HOOK AS PE R SRM 57-50-3. REPLACED RIB AS PER DWG REF NR 65-17294. (M) 2 L 7 3 4F A3WE 1998041700931 19980417 00931 NM 1998 4 17 MZZA98105 1 19980219 A 5320 WEB BOEING 727 727264 138408M NM BS 620 FAILED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - WEB BUCKLED BETWEEN STA 28L AND 28R AT FS 620 FWD CARGO. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998041700932 19980417 00932 NM 1998 4 17 MZZA98108 1 19980219 A 5320 SILL BOEING 727 727264 138408M NM CARGO DOOR CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - AFT CARGO DOOR LOWER SILL T-CHORD BADLY CORRODED ON PREVIOUS BLENDED OUT AREAS. REPAIR CARRYOUT PER ECRA EC 5310- 02509. (M) 2 L 7 3 4F A3WE 1998041700933 19980417 00933 NM 1998 4 17 MZZA98111 1 19980217 A 5320 6556129 SILL BOEING 727 727264 138408M NM CARGO DOOR CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - AFT CARGO SILL FWD CORNER AREA BADLY CORRODED. WEB REPAIR CARRYOUT PER SRM 53-10-1. (M) 2 L 7 3 4F A3WE 1998041700934 19980417 00934 NM 1998 4 17 MZZA98110 1 19980215 A 5510 652298771 BEAM BOEING 727 727264 138408M NM LT HORIZ STAB CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 623DH 20895 KUL - LEFT HORIZONTAL STAB TRAILING EDGE UPPER BEAM IS CORRODED EXFOLIATED AT FWD H/CHANNEL. CORROSION REMOVED IAW SRM 51-10-6 FOUND OUT OF LIMITS SRM 51-10-1 PAGE 1 FLANGE THICKNESS LIMIT. LEFT H/STAB, TRAILING EDGE UPPER REPLACED, NEW R OWS OF RIVET INSTALLED IAW SRM 51-10-3. (M) 2 L 7 3 4F A3WE 1998041700935 19980417 00935 WP 1998 4 17 HALA9800073 1 19980326 A 3350 60030431 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 47654 HNL - FLT 113 - EMERGENCY LIGHTS CEILING ROW 12-18 DOES NOT TEST 'ON' PREFLIGHT. REMOVED AND REPLACED EMERGENCY BATTERI ES. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998041700936 19980417 00936 WP 1998 4 17 HALA9800074 1 19980326 A 2913 AS66411LS666 PUMP DOUG DC9 DC951 3022051 WP RT HYD SYSTEM FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 669HA MX294444U 47654 HNL - FLT 113 - RIGHT HYDRAULIC PUMP FAILED IN FLIGHT. A/C MADE AN UNEVENTFUL LANDING IN HNL. REMOVED AND REPLACED RT HYDRAULIC PUMP. (M) 2 L 7 2 4F RT A6WE 1998041700937 19980417 00937 CE 1998 4 17 98ZZZM416 1 19980321 A 3260 UPLOCK SWITCH BEECH 1900 1900C 1154161 CE RT MLG OUT OF ADJUST A GUUA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 105GL UC105 FLT 7427 - MIA/MCO - LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER TAKEOFF. AIRCRAFT RETURNED TO MIA. ADJUST ED RIGHT MAIN LANDING GEAR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A24CE 1998041700938 19980417 00938 CE 1998 4 17 98ZZZM417 1 19980321 A 2781 SWITCH BEECH 1900 1900 1154160 CE TE FLAPS OUT OF ADJUST A GUUA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 189GA UB9 FLT 7475 - MIA-MCO - LANDING GEAR WARNING HORN AND INTRANSIT LIGHT REMAIN ON AFTER GEAR RETRACTION. A/C RETURNED TO MIA . STRAIGHTENED MICROSWITCH ACTUATOR ON FLAP SWITCH. (M) 2 L 7 2 4T RT A24CE 1998041700939 19980417 00939 WP 1998 4 17 AALA980554 1 19980320 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7538A 49992 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS IN AFT STAIR AREA INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT WIRE AND SPLICE IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041700940 19980417 00940 WP 1998 4 17 AALA980523 1 19980318 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 276AA 49273 DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT FOR TAIL CONE RELEASE HANDLE WAS INOPERATIVE. REPLACE SPLICES FOR LIGHT O N TAIL CONE RELEASE HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041700941 19980417 00941 WP 1998 4 17 AALA980513 1 19980316 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7508 49802 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT IN MID AND AFT CABIN INOPERATIVE. REPAIRED SHORTED WIRE I N TAIL COMPARTMENT. REPLACED FORWARD/AFT MODULES AND BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041700942 19980417 00942 EU 1998 4 17 AALA980506 1 19980414 A 5320 INTERCOSTAL AIRBUS 300 A300B4605R 3930308 EU FRAME 38-38.1 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON INTERCOSTAL BELOW NR 6 ROLLER TRAY NEXT TO STRINGER 44R (ON OUTBOARD SIDE) BETWEEN FRAME 38 AND 38.1. REPLACED INTERCOSTAL WITH NEW ONE AND INSTALLED DOUBLER IAW SRM 51-71-30. (M) 2 L 7 2 4F RT A35EU 1998041700943 19980417 00943 WP 1998 4 17 AALA980493 1 19980315 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 293AA 49305 DFW - DURING OVERNIGHT CHECK, MID CABIN EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PAT H LIGHT CONNECTORS AT MID GALLEY. SYSTEM GROUD CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998041700944 19980417 00944 NM 1998 4 17 AALA980559 1 19980323 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 638AA 24596 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR PATH LIGHT IN FORWARD COACH CABIN INOPERATIVE. REPLACED EMERGENCY FLOOR P ATH LIGHT STRIP FORWARD COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998041700945 19980417 00945 NM 1998 4 17 AALA980557 1 19980322 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636AM 24594 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT CENTER CABIN L2/R2 DOOR AREA INOPERATIVE. R EPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT CENTER CABIN L2/R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998041700946 19980417 00946 NM 1998 4 17 AALA980548 1 19980320 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380AN 25449 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 21H INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LI GHT CONNECTOR AT PAX SEAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998041700947 19980417 00947 NM 1998 4 17 AALA980549 1 19980322 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 334AA 22332 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 20 HJ INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT L IGHT CONNECTOR AT PAX SEAT 20 HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998041700948 19980417 00948 NM 1998 4 17 AALA980495 1 19980314 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 625AA 24583 DFW - DUIRNG OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. REPAIRED SHORTED EMERGENCY E XIT FLOOR PATH LIGHT CONNECTOR IN MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998041700949 19980417 00949 NM 1998 4 17 AALA980496 1 19980313 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373AA 25200 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 28B INOPERATIVE. REPAIRED BROKEN EMERGENCY E XIT LIGHT WIRE AT PASSENGER SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998041700950 19980417 00950 WP 1998 4 17 AALA980505 1 19980414 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1977 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - LONGERON 38L CORRODED AT STATION 1977. REPLACED SECTION OF LONGERON PER SRM 53-10-00. (M) 2 L 7 3 4F A22WE 1998041700951 19980417 00951 NM 1998 4 17 AALA980525 1 19980318 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 641AA 24599 MIA - FLT 442 - DURING OVERNIGHT MAINTENANCE SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 19A INOPERATIVE. R EPLACED SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROW 19A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998041700952 19980417 00952 EU 1998 4 17 AALA980515 1 19980316 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FRAME 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGE R56L SPLICE AT FRAME 65. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998041700953 19980417 00953 WP 1998 4 17 AALA980502 1 19980315 A 3260 DT2RA7 SWITCH DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 07 7508 49802 DFW - FLT 2225 - DURING APPROACH DFW, GEAR WAS EXTENDED AND GREEN DOWN AND LOCK LIGHS DID NOT ILLUMINATE. GEAR WAS RECY CLED PER CHECKLIST AND THREE GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. R EPLACED LANDING GEAR HANDLE SWITCH. ACCOMPLISHED GEAR SWING WITH NO PROBLEMS NOTED. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F A6WE 1998041700954 19980417 00954 WP 1998 4 17 AALA980367 1 19980218 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 226AA 49176 TUL - FLT 1744 - AFTER TAKEOFF SMOKE WAS DETECTED IN THE CABIN WITH NO ABNORMAL INDICATIONS. AIRCRAFT RETURNED TO TUL A ND LANDED WITHOUT INCIDENT. REPLACED BOTH AIR CYCLE MACHINE COALESCER BAGS. ACCOMPLISHED PACK BURNOUT PROCEDURE WITH N O DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. ACCOMPLISHED FERRY FLIGHT TUL-ORD. OPERATIONAL CHECKED NORMA L WITH NO DEFECTS FOUND. (M) 2 L 7 2 4F A6WE 1998041700955 19980417 00955 WP 1998 4 17 G60A018 1 19980325 A 5510 AVB7021503 FAIRING DOUG DC10 DC1030F 3023504 WP LT HORIZ STAB CRACKED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 600GC 46965 GROUND MAINTENANCE FOUND PART OF THE LEFT AFT HORIZONTAL STABILIZER TRAILING EDGE UPPER SIDE MISSING. GROUND MAINTENANC E PERFORMED AN INTERIM REPAIR IAW BOEING TELEX SEQUENCE 9809446. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998041700956 19980417 00956 NM 1998 4 17 WRLA98075 1 19980323 A 7110 2215125581 COWLING DOUG MD11 MD11F 3023600 NM NR 3 ENGINE PUNCTURED A WRLA K NONE O OTHER TX TAXI/GRND HDL 1 EA 27 274WA 48633 DURING OFF LOADING OF CARGO, 'BAGGAGE TUG' OPERATOR STRUCK THE RIGHT SIDE OF THE NR 3 ENGINE FAN COWLING, DAMAGING ITS S KIN. MAINTENANCE PERSONNEL REPAIRED SKIN PER PWA NACELLE STRUCTURAL REPAIR MANUAL 54-20-00. REPAIR REQUIRES REINSPECTI ON AT EACH A CHECK, AND REQUIRES SKIN REPLACEMENT AT NEXT C-CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998041700957 19980417 00957 NM 1998 4 17 WRLA98076 1 19980306 A 2150 35J32600 CLAMP DOUG MD11 MD11 3023602 NM NR 3 PACK BROKEN A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 271WA 48518 DURING INITIAL CLIMB-OUT, PASSING THOUGH 18,000 FT, FLT CREW RECEIVED LEVEL 3 ALERT ON NR 3 PNEUMATIC MANIFOLD FAILED WA RNING. FLIGHT CREW ELECTED TO RETURN TO POINT OF DEPARTURE FOR MAINTENANCE. AIRCRAFT RETURNED TO POINT OF DEPARTURE, A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND BROKEN CLAMP ON NR 3 REFRIGERATION UNIT. CLAMP WAS REP LACED, GROUND RUNS PERFORMED WITH NO MALFUNCTIONS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998041700958 19980417 00958 EU 1998 4 17 SIMA980781 1 19980319 A 5347 S53570201202 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT MID OUTBOARD, THE RIGHT AFT OUTBOARD, RIGHT AFT INBOARD, LEFT AFT OUTBOARD, LEFT AFT INBOARD, RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700959 19980417 00959 EU 1998 4 17 98ZZZM418 1 19980319 A 5347 S53678001200 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT MID OUTBOARD, THE RIGHT AFT OUTBOARD, RIGHT AFT INBOARD, LEFT AFT OUTBOARD, LEFT AFT INBOARD, RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700960 19980417 00960 EU 1998 4 17 98ZZZM419 1 19980319 A 5347 S53678001202 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT MID OUTBOARD, THE RIGHT AFT OUTBOARD, RIGHT AFT INBOARD, LEFT AFT OUTBOARD, LEFT AFT INBOARD, RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700961 19980417 00961 EU 1998 4 17 98ZZZM420 1 19980319 A 5347 S53678001210 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 251AE 250 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT MID OUTBOARD, THE RIGHT AFT OUTBOARD, RIGHT AFT INBOARD, LEFT AFT OUTBOARD, LEFT AFT INBOARD, RIGHT FLIGHT ATTENDANT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700962 19980417 00962 EU 1998 4 17 SIMA980851 1 19980326 A 3234 1005383Y00 SELECTOR VALVE AEROSP ATR42 ATR42300 8680920 EU LANDING GEAR INOPERATIVE A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 422MQ 46 0028 ORD - FLT 4351 - DURING CLIMB-OUT, CREW WAS NOT ABLE TO RETRACT GEAR. CREW RETURNED TO ORD SAFELY. NO FURTHER INCIDENT S WAS REPORTED. RAI'D L/G SELECTOR VALVE. PERFORMED RETRACTION CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700963 19980417 00963 EU 1998 4 17 REXA98077 1 19980319 A 3411 PITOT BAG JETSTM JETSTM3101 1500215 EU FWD FUSELAGE WATER CONTAM A REXA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 317PX 688 AIRSPEED INDICATORS ARE OFF BY 60 KNOTS. DRAINED PITOT WATER TRAPS. (M) 2 L 7 2 4T RT A21EU 1998041700964 19980417 00964 EU 1998 4 17 REXA98076 1 19980323 A 3610 CLAMP SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A A REXA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 403BH 340A060 LEFT ENGINE LOST TORQUE AFTER TAKEOFF TEMP WENT TO 915 DEGREES. LEFT ENGINE SHUT DOWN AND RETURNED TO MEM. FOUND LEFT ENGINE HIGH PRESSURE BLEED PIPE CLAMP BOLT SHEARERD. REMOVED AND REPLACED CLAMP AND PERFORMED ENGINE. RUNS HELD AT 60, 70, 80, 90, 100 PERCENT. ALL GROUND RUNS OP CHECKED GOOD. (M) 2 L 7 2 4T RT A52EU 1998041700965 19980417 00965 EU 1998 4 17 REXA98075 1 19980322 A 3243 MASTER CYLINDER BAG JETSTM JETSTM3101 1500215 EU RT COCKPIT NO PRESSURE A REXA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 315PX 685 FO LEFT BRAKE PEDAL NO PRESSURE. SERVICED FO'S BRAKE MASTER CYLINDER. (M) 2 L 7 2 4T RT A21EU 1998041700966 19980417 00966 1998 4 17 REXA98074 4 19980319 A 3442 6222504001 ANTENNA SAAB SF340 340B 7860101 EU RADAR FAILED A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 367PX 1864 340B271 WEATHER RADAR POINTS ECHOES ON OPPOSITE SIDE OF DISPLAY KNOWN. ECHOES TO RIGHT OF AIRCRAFT PAINT ON LEFT SIDE OF DISPLA Y. REMOVED AND REPLACED THE WEATHER RADAR ANTENNA. (M) 2 L 7 2 4T RT A52EU 1998041700967 19980417 00967 EU 1998 4 17 REXA98073 1 19980317 A 3233 AIR134736 BOLT SAAB SF340 340B 7860101 EU LT MLG ACT FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 363PX 340B260 UPON LANDING GEAR RETRACTION GOT A GEAR HANDLE LIGHT AND THE HYDRAULIC PUMP KEPT RUNNING. PUT LANDING GEAR BACK DOWN, A ND THE LEFT HAND MAIN WOULD NOT LOCK DOWN. RAN EMERGENCY CHECKLIST, PULLED T-HANDLE WITH NO CHANGE. LANDED WITH NO FUR THER INCIDENT. REMOVED AND REPLACED MAIN LANDING GEAR RETRACT ACTUATOR BRACKET RETAINING BOLT. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998041700968 19980417 00968 EU 1998 4 17 REXA98072 1 19980318 A 7712 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU RIGHT MALFUCNTIONED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 333PX 704 RIGHT TORQUE FLUX ON TAKEOFF. SWAPPED CANNON PLUG ON RIGHT ENGINE TORQUE SIGNAL CONDITIONER FROM BRIDGE 1 TO BRIDGE 2. GROUND RUN AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998041700969 19980417 00969 EU 1998 4 17 C2XA98IA082 1 19980320 A 5230 S52376519216 HINGE AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING C-CHECK INSPECTION, FOUND FORWARD CARGO DOOR, DOOR SIDE HINGE CRACKED AT FORWARD LUG. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR IAW ATR 42 MM JIC 52-31-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700970 19980417 00970 EU 1998 4 17 C2XA98IA081 1 19980320 A 5230 S52376104204 FRAME AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING C-CHECK INSPECTION, FOUND FORWARD CARGO DOOR FRAME CRACKED AFT OF THE ACTUATOR ATTACHMENT FITTING. MAINTEN ANCE REMOVED AND REPLACED THE CARGO DOOR IAW ATR42MM JIC 52-31-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 1998041700971 19980417 00971 EU 1998 4 17 C2XA98IA080 1 19980320 A 3350 0341516 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700972 19980417 00972 EU 1998 4 17 C2XA98IA079 1 19980320 A 5315 S5317320620000 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING C-CHECK INSPECTION, FOUND CAPTAINS SIDE FLOOR CORRODED AT SEAT ATTACHMENT AREA. MAINTENANCE REMOVED AND RE PLACED THE FLOORBEAM IAW ATR-42 SRM 53-17-70/51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700973 19980417 00973 EU 1998 4 17 C2XA98IA078 1 19980320 A 5610 S53171123204 WINDSHIELD AEROSP ATR42 ATR42320 8680930 EU COCKPIT DEFECTIVE HOLE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING C-CHECK INSPECTION, FOUND DEFECT INDICATIONS ON WINDSHIELD NODE NR 5 FASTENER LOCATIONS DURING ACCOMPLISHME NT OF SSI 53-11-27. MAINTENANCE REAMED THE DEFECTIVE HOLES UNTIL DEFECT WAS REMOVED AND INSTALLED OVERSIZE FASTENERS IA W CONTINENTAL EXPRESS ECRA 5310-01086. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700974 19980417 00974 EU 1998 4 17 C2XA98IA077 1 19980320 A 5320 S53671406202 STIFFENER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14819 156 IAH - DURING C-CHECK INSPECTION, FOUND VHF 2 FUSELAGE STIFFENER CRACKED. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998041700975 19980417 00975 EU 1998 4 17 C2XA98BT022 1 19980314 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14834 193 DURING LINE CHECK, FOUND MAIN CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED ENTRY DOOR EXIT LIGHT. OPS CHECK GO OD. (M) 2 H 7 2 4T RT A53EU 1998041700976 19980417 00976 EA 1998 4 17 98ZZZM421 1 19980224 A 7711 7700P4 CONNECTOR DHAV DHC7 DHC7102 2802708 EA NR 1 ENGINE BROKEN A CICA K NONE J WARNING INDICATION CR CRUISE 1 SO 17 4860J 19 FLT 204 - PID-MIA - PILOT REPORTED NR 1 T5 GAUGE HAD IMPROPER INDICATION, 100-200 DEGREE TOO LOW. THE AIRCRAFT WAS INSP ECTED AND FOUND SAFE FOR FERRY FLIGHT TO FLL MAINTENANCE. INSPECTION FOUND LOOSE WIRE ON CANNON PLUG ON T5 LINE IN WING ROOT. REPLACED PIN AND SECURED WIRE. RAN ENGINE AND FOUND T5 OPERATED NORMAL IAW MM. AIRCRAFT RETURNED TO SERVICE. ( M) 2 H 7 4 4T A20EA 1998041700977 19980417 00977 EA 1998 4 17 98ZZZM422 2 19980117 A 7320 324475315 LINKAGE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 2 ENGINE OUT OF ADJUST A CICA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 17 4860J 19 86354 PRIOR TO FLT 9486, PILOT REPORTED NR 2 ENGINE LOSES FUEL PRESSURE WHEN CONDITION LEVER IS BROUGHT TO START FEATHER POSIT ION. THE AIRCRAFT WAS INSPECTED AND FOUND TO BE SAFE FOR FERRY FLIGHT, WITH NR 2 ENGINE SHUT DOWN, TO FLL MX BASE. INS PECTION FOUND FCU LINKAGE OUT OF ADJUSTMENT. READJUSTED LINKAGE, SAFETIED, TEST RUN OK. AIRCRAFT WAS RELEASED FOR FLIG HT. (M) 2 H 7 4 4T 4 T A20EA E4EA 1998041700978 19980417 00978 EA 1998 4 17 98ZZZM423 1 19980305 A 5510 12206020 SPEED TAPE DHAV DHC7 DHC7102 2802708 EA HORIZ STAB TORN A CICA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER IN INSP/MAINT 1 SO 17 25AG 25 FLT 9051 - CANCELLED DUE TO SPEED TAPE COMING OFF FROM HORIZONTAL STABILIZER. THE AIRCRAFT WAS INSPECTED AND FOUND TO B E SAFE FOR FERRY FLIGHT TO FLL. MAINTENANCE REMOVED TORN TAPE AND REPLACED TAPE OVER LIGHTNING HOLE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 4 4T A20EA 1998041700979 19980417 00979 EU 1998 4 17 98ZZZM424 1 19980302 A 2120 1379258L403 Y-DUCT BAG JETSTM JETSTM3101 1500215 EU BS 220 CRACKED A CX7A A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 03 828JS 708 FLT 280 - MDW-GRR - LIGHT SMOKE AND ODOR EMANATED. CREW SHUT OFF FLOWS SMOKE SUBSIDED. ATC WAS NOTIFIED. AIRCRAFT RET URNED TO MDW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS THEN FERRIED TO GRR. FLOWS DEFERRED. INSPECTION FOUND CRACKED Y-D UCT BLOWING AIR ON RESIDUAL HYDRAULIC FLUID BELOW BELLY OF AIRCRAFT. REPLACED DUCT AND CLEANED UP FLUID. AIRCRAFT RETU RNED TO SERVICE. AIRCRAFT TOTAL TIME HOURS 19165.5. (M) 2 L 7 2 4T RT A21EU 1998041700980 19980417 00980 NM 1998 4 17 98ZZZM425 1 19980126 A 7110 COWL BOEING 757 75723APF 1384966 NM NR 1 ENGINE CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND NR 1 ENGINE OUTBOARD FAN COWL UPPER EDGE STRIP HAS A .375 INCH CRACK AND .75 INCH CRACK AT AFT HIN GE. REPLACED METAL STRIP IAW MM 71-11-04. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998041700981 19980417 00981 NM 1998 4 17 98ZZZM426 1 19980126 A 7110 COWL BOEING 757 75723APF 1384966 NM NR 1 ENGINE CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND NR 1 ENGINE INBOARD FAN COWL HAS A 1.5 INCH CRACK UPPER EDGE, AFT HINGE AND .375 INCH CRACK ON STR IP FWD OF 2ND HINGE. REPLACED METAL STRIP IAW MM 71-11-04. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998041700982 19980417 00982 NM 1998 4 17 98ZZZM427 1 19980126 A 7110 LJ76156 SEAL BOEING 757 75723APF 1384966 NM NR 2 ENG COWL CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND NR 2 ENGINE LEFT FAN COWL UPPER METAL SEAL CRACKED. REPLACED SEAL IAW MM 71-11-04. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998041700983 19980417 00983 NM 1998 4 17 98ZZZM428 1 19980126 A 7110 STIFFENERS BOEING 757 75723APF 1384966 NM NR 2 ENGINE CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND NR 2 ENGINE INBOARD FAN COWL START VALVE ACCESS DOOR INBOARD SKIN STIFFENERS CRACKED. REPAIRED ST IFFENERS IAW SRM 51-70-00. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998041700984 19980417 00984 NM 1998 4 17 98ZZZM429 1 19980126 A 5347 SEAT TRACK BOEING 757 75723APF 1384966 NM BS 780-800 CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND CRACK ON SEAT TRACK STATION 780-800 LEFT SIDE. REPLACED CRACKED SEAT TRACK IAW SRM 53-00-52 AND B OEING MESSAGE HAR-98-0013RR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A2NM 1998041700985 19980417 00985 NM 1998 4 17 98ZZZM430 1 19980126 A 5230 GUIDE BLOCK BOEING 757 75723APF 1384966 NM CARGO DOOR CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND MAIN CARGO DOOR LOWER FWD CORNER GUIDE BLOCK CRACKED. CRACKED BLENDED OUT PER BOEING MESSAGE STS- HAR-98-0005RR. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998041700986 19980417 00986 NM 1998 4 17 98ZZZM431 1 19980126 A 5320 INTERCOSTAL BOEING 757 75723APF 1384966 NM BS 839-859 CRACKED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 571CA 24456 DURING C-CHECK, FOUND FUSELAGE INTERCOSTAL CRACKED AT STATION 839-859, 51 INCHES B/L, LEFT SIDE AND RIGHT SIDE. REMOVED FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-10-00, 51-40-02 AND 53-30-51. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998041700987 19980417 00987 1998 4 17 98ZZZM432 4 19980317 A 2210 187491A COUPLER BOEING 707 707330C 138367G NM E/E COMPT DEFECTIVE A A CLCA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 19 707HE 1832 20124 ON CAC FLT 47 MIA/SAL, A/C ENCOUNTERED 'DUTCH ROLLS' PASSING 28,000 FEET. TURNING YOKE TO RIGHT ALLOWED CONTROL OF ROLL TO SOME DEGREE. YOKE IN NEUTRAL AND CLOSING INBOARD SPOILER SWITCH DAMPENED THE OSCILLATION, BUT NOT COMPLETELY. A/C DUMPED FUEL AND AIR RETURNED TO MIA. ON GROUND MAINTENANCE REPLACED YAW DAMPER COUPLER AND OPS CHECKED PER MM 22-6-00. ALSO, REMOVED AND REPLACED RUDDER POWER CONTROL UNIT. OPS CHECKED PER ADJUSTMENT TEST, MM 27-12-121. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 4 4F 4A26 1998041700988 19980417 00988 NM 1998 4 17 98ZZZM433 1 19980322 A 3260 PROX SWITCH BOEING 757 75723APF 1384966 NM NLG FAILED A CLCA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 571CA 24456 ON CAC FLT 95, MIA/GYE, AFTER TAKEOFF STATUS MESSAGE A/G NOSE DISAGREE ILLUMINATED. A/C ACCOMPLISHED AIR RETURN BACK TO MIA. ON GROUND MAINTENANCE REMOVED AND REPLACED PSEU PER MM 32-09-04, MESSAGE CLEARED AND A/C RELEASED INTO SERVICE. A FTER SECOND TAKEOFF STATUS MESSAGE NOSE A/G DISAGREE ILLUMINATED ONCE AGAIN. A/C ACCOMPLISHED SECOND AIR RETURN BACK TO MIA. ON GROUND MAINTENANCE REMOVED AND REPLACED NLG PROX SWITCH IAW MM 32-09-02. PERFORMED RETRACT CHECK AND OPS CHEC KED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998041700989 19980417 00989 CE 1998 4 17 98ZZZM434 1 19980117 A 5753 SKIN BEECH 1900 1900D 1154162 CE RT TE FLAP LOOSE A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 474 UE176 IN ICT AT OVERNIGHT DETAIL NR 1 INSPECTION, MAINTENANCE FOUND SEVERAL RIVETS LOOSE AND PULLED THROUGH THE SKIN ON THE BO TTOM SKIN OF RT INBOARD FLAP. REPAIRED IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998041700990 19980417 00990 CE 1998 4 17 98ZZZM435 1 19980228 A 3240 ACCUMULATOR BEECH 1900 1900D 1154162 CE LT BRAKE SYSTEM REQ'D SERVICE A AMWA K NONE O OTHER LD LANDING 1 CE 07 166YV 6452 UE166 FLT 5657 - AIRCRAFT LOST BRAKING FORCE ON LEFT SIDE AFTER LANDING IN ICT. ICT MAINTENANCE BLED BRAKE SYSTEM AND RETURNE D THE AIRCRAFT TO SERVICE WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4T RT A24CE 1998041700991 19980417 00991 CE 1998 4 17 98ZZZM436 1 19980217 A 5753 SKIN BEECH 1900 1900D 1154162 CE LT TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 62ZV UE62 DURING AIRCRAFT ACCEPTANCE INSPECTION MAINTENANCE FOUND ATTACH BRACKETS WORN, A 6 INCH CRACK ON BOTTOM TE NEAR INBOARD E ND AND A 6 INCH CRACK ON TOP TE NEAR INBOARD END. REPAIRED CRACK IN TOP SKIN IAW SRM 57-00 AND BOTTOM SKIN IAW AIR MIDW EST TO 1900-27-00-0001. REPLACED BRACKETS IAW SRM 57-00. (M) 2 L 7 2 4T RT A24CE 1998041700992 19980417 00992 WP 1998 4 17 USAAD98057 1 19980326 A 5610 WINDOW DOUG DC9 DC982 3022082 WP RT COCKPIT OUT OF ADJUST A A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 818US 48098 PHL - FLT 1484 - THE FLIGHT WAS AIRBORNE FOR JUST A FEW MINUTES WHEN THE FIRST OFFICERS WINDOW LATCHED INTO THE OPEN POS ITION AND COULD NOT BE CLOSED. THE FLIGHT RETURNED TO PHL WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUN D THE WINDOW FRAME COMPOUND WAS NOT SMOOTH AND THE LOCK HANDLE OUT OF ADJUSTMENT. SMOOTHED COMPOUND AND ADJUSTED LOCK. (M) 2 L 7 2 4F A6WE 1998041700993 19980417 00993 WP 1998 4 17 USAA98054 1 19980328 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 931VJ 47188 CMH - THE LEFT NACELLE EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998041700994 19980417 00994 WP 1998 4 17 USAAD98051 1 19980324 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 920VJ 48140 ORF - THE AFT CABIN FLOOR AND TAIL COMPARTMENT CATWALK LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE FLOOR LIGHTING BATTERY CHARGER ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998041700995 19980417 00995 WP 1998 4 17 USAAD98052 1 19980328 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 938VJ 48119 IND - EMERGENCY LIGHTS IN THE AFT FUSELAGE ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998041700996 19980417 00996 WP 1998 4 17 USAAD98053 1 19980329 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 926VJ 48146 IND - THE CABIN CEILING EMERGENCY LIGHTS FOR ROWS 10-14 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTE RY. (M) 2 L 7 2 4F A6WE 1998041700997 19980417 00997 WP 1998 4 17 USAAD98055 1 19980328 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 977VJ 48155 CMH - THE RIGHT NACELLE EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE POWER SUPPLY FOR THE R IGHT NACELLE EMERGENCY LIGHT. (M) 2 L 7 2 4F A6WE 1998041700998 19980417 00998 WP 1998 4 17 98ZZZM437 1 19980328 A 3350 6011777LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CARGO COMPT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 977VJ 48155 CMH - THE RIGHT NACELLE EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE POWER SUPPLY FOR THE R IGHT NACELLE EMERGENCY LIGHT. (M) 2 L 7 2 4F A6WE 1998041700999 19980417 00999 NM 1998 4 17 USAABB98023 1 19980329 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 MCO - FOUND L4 AND R1 DOOR EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLIES. (M) 2 L 7 2 4F RT A2NM 1998041701000 19980417 01000 NM 1998 4 17 USAASB98066 1 19980316 A 2420 941D3352 CIRCUIT BREAKER BOEING 737 737201 1384454 NM COCKPIT FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 243US 22445 CLT - FLT 1503 - ON CLIMB-OUT FROM CLT, THE NR 1 GENERATOR WAS LOST AT APPROXIMATELY 6,000 FEET. CREW PUT THE APU GENER ATOR ON LINE AND IT CEASED AT 11,000 FEET. WITH ONLY ONE POWER SOURCE LEFT, CREW RETURNED TO FIELD AT CLT AND LANDED WIT HOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 BUS TIE CIRCUIT BREAKER RE LAY C804. RAN ENGINES AND APU. ALL GENERATOR OPERATIONAL CHECKS SATISFACTORY. FOUND NR 1 ENGINE CSD OVERSERVICED. DR AINED CSD TO PROPER LEVEL. (M) 2 L 7 2 4F A16WE 1998041701001 19980417 01001 WP 1998 4 17 USAAD98045 1 19980319 A 3230 59516395001 CYLINDER DOUG DC9 DC982 3022082 WP NLG FAILED A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 824US 49143 PBI - FLT 1753 - ON APPROACH INTO PBI, AS CREW ATTEMPTED TO EXTEND THE LANDING GEAR, DID NOT GET THREE GREENS. THE NOSE GEAR DID NOT APPEAR TO EXTEND NORMALLY. ON DOWNWIND THE TOWER ADVISED THE CAPTAIN THAT THE NOSE GEAR WAS NOT EXTENDED. CAPTAIN DID A MANUAL GEAR EXTENSION PROCEDURE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR BUNGEE CYLINDER ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998041701002 19980417 01002 WP 1998 4 17 USAAD98046 1 19980320 A 2420 976J2544 CONTROL PANEL DOUG DC9 DC931 3022065 WP E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 946VJ 47026 CMH - FLT 920 - ON TAKEOFF THE AC CROSSTIE LOCKOUT AND RIGHT GENERATOR OFF LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GENERATOR CONTROL PANEL. (M) 2 L 7 2 4F A6WE 1998041701003 19980417 01003 WP 1998 4 17 USAAD98044 1 19980318 A 2130 DUCT DOUG DC9 DC982 3022082 WP RIGHT FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 830US 49443 RSW - FLT 932 - EN ROUTE AT 31,000 FEET THE FLOW LIGH TILLUMINATED ON THE PRESSURE CONTROLLER AND THE CABIN STARTED TO C LIMB AT 1000 FT/MIN. THE CREW SWITCHED TO THE STANDBY PRESSURIZATION SYSTEM BUT THE CABIN CONTINUED TO CLIMB AT THE MAX RATE, THE OUTFLOW VALVE WAS FULLY CLOSED. THE CAPTAIN INITIATED A DESCENT TO 10,000 FT AND THE FLOW LIGHT WENT OUT. T HE FLIGHT CONTINUED TO ITS DESTINATION. MAINTENANCE SECURED THE RIGHT RAM AIR DUCT AT THE HEAT EXCHANGER PLENUM. (M) 2 L 7 2 4F A6WE 1998041701004 19980417 01004 NM 1998 4 17 USAASB98070 1 19980319 A 5610 5893543109 WINDSHIELD BOEING 737 7374B7 1384702 NM LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 428US 11663 24550 IND - FLT 797 - AT CRUISE ALTITUDE, CAPTAINS WINDSHIELD BEGAN ARCING. WINDSHIELD HEAT WAS TURNED OFF. SHORTLY THEREAFT ER, THE CAPTAINS WINDSHIELD CRACKED. A DECISION WAS MADE TO DIVERT TO IND. FLIGHT LANDED WITHOUT FURTHER INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS L1 WINDSHIELD. ALSO, REPLACED L1 WINDSHIEL D HEAT CONTROLLER (P/N 83000-05602) AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998041701005 19980417 01005 WP 1998 4 17 USAA980121 1 19980319 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 160 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805US 45571 48053 PIT - DURING Q-1 CHECK, FOUND TWO CRACKS, .25 INCH IN TOP SKIN, 1 INCH CRACK IN MID SKIN AT STATION 160, TOP FWD CORNER OF MAIN ENTRANCE DOOR OPENING. INSTALLED DOUBLERS PER SRM 53-05 FIG 26. (M) 2 L 7 2 4F A6WE 1998041701006 19980417 01006 WP 1998 4 17 USAA980124 1 19980319 A 5320 591014211 WEB DOUG DC9 DC981 3022081 WP BS 636 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805US 45571 48053 PIT - DURING Q-1 CHECK, FOUND CORROSION UNDERSIDE OF DOOR FRAME WEB AT MID CARGO DOOR STATION 636 AND 28R. SPLICED NEW FORWARD SECTION OF WEB PER EA 49301. CORROSION TASK NR C51-53300, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1998041701007 19980417 01007 WP 1998 4 17 USAA980123 1 19980319 A 5320 BEAM DOUG DC9 DC981 3022081 WP BS 1155 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805US 45571 48053 PIT - DURING Q-1 CHECK, FOUND CORROSION AT SCREW HOLE AT STATION 1155 LONGERON 29R BEAM. REMOVED CORROSION AND INSTALLE D DOUBLER STRAP PER EA 49231. CORROSION TASK NR C57-5330, CORROSION LEVEL 1. (M) 2 L 7 2 4F A6WE 1998041701008 19980417 01008 WP 1998 4 17 USAA980122 1 19980319 A 5530 DRAG ANGLE DOUG DC9 DC981 3022081 WP VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805US 45571 48053 PIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK AT VERTICAL LEG OF LT VERTICAL STAB DRAG ANGLE AT STATION 1288 CANTED. INST ALLED NESTED ANGLE PER SRM 53-05 FIG 23B. (M) 2 L 7 2 4F A6WE 1998041701009 19980417 01009 NM 1998 4 17 VJ09800053 1 19980322 A 3350 3114981 DEFLECTOR BOEING 737 7372E1 138448F NM L1 DOOR INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 461AT 20976 DURING LAYOVER CHECK, FOUND L-1 DOOR EMERGENCY EXIT ESCAPE SLIDE LIGHT INOP. REPLACED LIGHT DEFLECTOR ASSY. (M) 2 L 7 2 4F A16WE 1998041701010 19980417 01010 NM 1998 4 17 TWAA9804408 1 19980313 A 5280 DOOR BOEING 727 727231 1384079 NM NLG CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54352 21984 MCI - DURING C-CHECK MAINTENANCE, THE LEFT NOSE LANDING GEAR DOOR, INBOARD EDGE OF DOOR, SEAL RETAINER AND LOWER EDGE OF GEAR DOOR WAS CORRODED. REPLACED DOOR ASSY AND RIGGED PER MM 32-22-1. (M) 2 L 7 3 4F A3WE 1998041701011 19980417 01011 NM 1998 4 17 TWAA9804407 1 19980210 A 5320 INTERCOSTAL BOEING 727 727231 1384079 NM BS 1034 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 84355 21987 MCI - DURING C-CHECK MAINTENANCE, FOUND CORROSION AT INTERCOSTAL STATION 1034 LBL 12. REPLACED INTERCOSTAL PER SRM 51-1 0-01. (M) 2 L 7 3 4F A3WE 1998041701012 19980417 01012 NM 1998 4 17 TWAA9804406 1 19980201 A 5320 ANGLE BOEING 727 727231 1384079 NM BS 344 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 24343 21630 MCI - DURING C-CHECK MAINTENANCE, FOUND FORMER CAP WITH CORROSION AT FS 344, RBL 46 TO 63. REPLACED FORMER CAP ANGLE PE R SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998041701013 19980417 01013 NM 1998 4 17 TWAA9804405 1 19980205 A 5320 SUPPORT BOEING 727 727231 1384079 NM CABIN FLOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 24343 21630 MCI - DURING C-CHECK MAINTENANCE AT CABIN FLOOR PANEL INBOARD OF FWD ENTRY DOORWAY, THE FLOOR SUPPORT HAD CORROSION. RE MOVED CORROSION BY REPLACEMENT OF SUPPORT. INSTALLED NEW PART SRM 51-10-01. (M) 2 L 7 3 4F A3WE 1998041701014 19980417 01014 NM 1998 4 17 TWAA9804404 1 19980312 A 5730 SKIN BOEING 767 767231 1385131 NM LT WING DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 LAX - DURING C-CHECK MAINTENANCE, ON TOP OF LEFT WING, TOP SURFACE OF LE BULL NOSE PANEL AFT OF NR 5 SLAT, OUTER SURFACE OF COMPOSIT MATERIAL WAS CRACKED IN TEN DIFFERENT PLACES. INSTALLED WEB LAYUPS REPAIR PER SRM 57-41-01. (M) 2 L 7 2 4F RT A1NM 1998041701015 19980417 01015 NM 1998 4 17 TWAA9804403 1 19980210 A 5730 PANEL BOEING 767 767231 1385131 NM RT WING DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING C-CHECK MAINTENANCE, ON TOP OF RT WING FWD OF OUTBOARD FLAP CANOE, OUTBOARD OF NR 12 SPOILER, A PANEL IS DE LAMINATING. INSTALLED HOT BOND REPAIR PER SRM 51-70-07. (M) 2 L 7 2 4F RT A1NM 1998041701019 19980417 01019 NE 1998 4 17 TWAA9804303 2 19980324 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE STALLED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 CE 05 902TW 49153 3259 RNO - FLT 224 - ABORTED TAKEOFF AT 100 KTS DUE TO COMPRESSOR STALLS ON RT ENGINE. FOUND COMPRESSOR BLADES DAMAGED FROM APPARENT ICE INGESTION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998041701020 19980417 01020 WP 1998 4 17 TWAA9804302 1 19980324 A 2133 2021941 ACTUATOR DOUG DC9 DC983 3022083 WP FUSELAGE FAILED A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 9407R 49400 JFK 0 FLT 187 - AFTER TAKEOFF, OUTFLOW VALVE REMAINED OPEN. AIRCRAFT WOULD NOT PRESSURIZE. RETURND TO JFK. PLACARDED AUTO CABIN PRESSURIZATION CONTROL INOP PER MEL. CHECK C 4-17-97 MCI. REPLACED THE OUTFLOW VALVE ACT WHICH HAD FAILED I N THE OPEN POSITION CAUSING THE CIRCUIT BREAKER TO POP. (M) 2 L 7 2 4F RT A6WE 1998041701021 19980417 01021 WP 1998 4 17 TWAA9804301 1 19980323 A 3350 0105607001 LENS DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9402W 53138 STL - FLT 467 - DURING PREFLIGHT, CREW REPORTED RED EGRESS LIGHT STRIP INOP AT ROW 22. REPLACED LENS. (M) 2 L 7 2 4F RT A6WE 1998041701022 19980417 01022 NE 1998 4 17 TWAA9804206 2 19980320 A 7250 798404 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE LT ENGINE CRACKED A TWAA C D ABORTED TAKEOFF RETURN TO BLOCK Y ENGINE STOPPAGE TO TAKEOFF 1 CE 05 9420D 49824 1422 STL - FLT 173 - DURING TAKEOFF ROLL AT 80 KNOTS, LT ENGINE OIL QUANTITY AND PRESSURE FELL TO ZERO. ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED ENGINE. CHECK-C 12-9-97 MCI. S/D - FOURTH STAGE TURBINE BLADE AIRFOIL FAILED FROM FATI GUE CRACK AT BASE OF AIRFOIL ORIGINATING AT LEADING EDGE. DAMAGE WAS REPAIRED. (X) 2 L 7 2 4F 4 F A6WE E9NE 1998041701023 19980417 01023 NM 1998 4 17 TWAA9804203 1 19980318 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 1275 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 LAX - DURING CHECK-C MAINTENANCE, FOUND CORROSION AT STRINGER 34L, FS 1275 IN AFT CARGO COMPARTMENT. REPAIRED STRINGER 34L PER SRM 53-30-03. (M) 2 L 7 2 4F RT A1NM 1998041701024 19980417 01024 NM 1998 4 17 TWAA9804202 1 19980317 A 5320 GUSSETT BOEING 727 727231 1384079 NM BS 825.95 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54352 21984 MCI - DURING C-CHECK MAINTENANCE, FOUND GUSSETT CRACKED AT FS 825.95 BELOW FLOOR AT FUSELAGE FRAME LEFT SIDE WALL AREA. REPAIRED PER M071T68 PHASE E. INSTALLED GUSSET PER SRM 51-10-1 AND SB 727-53-0197. (M) 2 L 7 3 4F A3WE 1998041701026 19980417 01026 WP 1998 4 17 VJ9800057 1 19980228 A 5330 1A30991 SKIN DOUG DC9 DC932 3022066 WP BS 980 CORRODED A VJ6A O OTHER O OTHER IN INSP/MAINT 1 SO 11 909VJ 47322 AFT CARGO FUSELAGE SKIN AND FRAME CORRODED AT FRAME STATION 980 BETWEEN L27R AND L28R ON AFT SIDE. CUT OUT PLATING BETW EEN L27R AND L28R, FABRICATED FILLER USING T2024T3 OF .050 AND .025 THICKNESS, FABRICATED FINGER DOUBLER USING 2024 T3, .025 IAW DC9 SRM 51-10-23. TREATED AND PRIMED IAW DC9 SRM 51-10-3, INSTALLED IAW AERO EO 98-802. (M) 2 L 7 2 4F A6WE 1998041701027 19980417 01027 WP 1998 4 17 98ZZZM438 1 19980228 A 5330 1A30992 SKIN DOUG DC9 DC932 3022066 WP BS 980 CORRODED A VJ6A O OTHER O OTHER IN INSP/MAINT 1 SO 11 909VJ 47322 AFT CARGO FUSELAGE SKIN AND FRAME CORRODED AT FRAME STATION 980 BETWEEN L27R AND L28R ON AFT SIDE. CUT OUT PLATING BETW EEN L27R AND L28R, FABRICATED FILLER USING T2024T3 OF .050 AND .025 THICKNESS, FABRICATED FINGER DOUBLER USING 2024 T3, .025 IAW DC9 SRM 51-10-23. TREATED AND PRIMED IAW DC9 SRM 51-10-3, INSTALLED IAW AERO EO 98-802. (M) 2 L 7 2 4F A6WE 1998041701028 19980417 01028 WP 1998 4 17 VJ9800059 1 19980327 A 3350 6100928 BULB DOUG DC9 DC932 3022066 WP CABIN FAILED A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 939VV 47089 EMERGENCY FLOOR PATH LIGHTS BURNED OUT IN SEVERAL LOCATIONS. RELAMPED, OPS CHECKED GOOD IAE MM 33-50. (M) 2 L 7 2 4F A6WE 1998041701029 19980417 01029 WP 1998 4 17 VJ9800058 1 19980320 A 5754 FITTING DOUG DC9 DC932 3022066 WP NR 1 SLAT TRACK GOUGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 917VV 47323 ATTACH FITTING RT WING, NR 1 SLAT MAIN TRACK (CENTER), GOUGED. BLENDED AREA IAW DC9 SRM 53-01, FIG 1. BLEND DEPTHS WIT HIN LIMITS PER RES 1 1668, TREATED AREA IAW SRM 51-10-3 AND AERO EO 98-822, COMPLETED FORM 8110-3. (M) 2 L 7 2 4F A6WE 1998041701030 19980417 01030 EU 1998 4 17 Y2PA98014 1 19980318 A 3411 STATIC LINE AMD FALC20 FALCOND 2720304 EU LT COCKPIT DAMAGED A Y2PA O OTHER O OTHER LD LANDING 1 GL 23 817AA 233 CAPTAINS ALTIMETER SEVERALLY LAGS BEHIND CO-PILOTS. AFTER TOUCH DOWN ALTIMETER READ 1400 FEET THEN SLOWLY RETURNED TO 7 80 FEET. NO EMERGENCY PROCEDURES WERE NECESSARY AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AT YIP. MAINTENANCE DI SCOVERED THAT THE CAPTAIN'S STATIC LINE WAS KINKED. THE LINE WAS REROUTED AND A PITOT-STATIC SYSTEM CHECK WAS PERFORMED IAW DA-20 MM 34-10-1 WITH NO DEFECTS NOTED. (M) 2 L 7 2 4F A7EU 1998041701031 19980417 01031 EU 1998 4 17 WTAA980044 1 19980305 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA K NONE N FALSE WARNING CR CRUISE 1 WP 17 423UE 799 FAT - RIGHT GEAR INTRANSIT RED INDICATION FAILS TO ILLUMINATE. MAINTENANCE REPLACED RIGHT DOWNLOCK MICROSWITCH. OPERAT IONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998041701032 19980417 01032 1998 4 17 USAASB98064 4 19980315 A 3417 LINE BOEING 737 737301 1384611 NM NR 2 ADC LOOSE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 342US 23511 IAH - FLT1840 - SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 400 FEET, THE FIRST OFFICERS AIRSPEED INDICATOR AND ALTIMETER BE CAME UNRELIABLE. CAPTAINS SIDE WAS OPERATIONAL ALONG WITH THE STANDBY INSTRUMENTS. FLIGHT RETURNED TO FIELD AT IAH AND LANDED WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT A16WE 1998041701033 19980417 01033 NM 1998 4 17 USAASB98059 1 19980310 A 3260 189929 SENSOR BOEING 737 7373B7 1384580 NM LT MLG FAILED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 375US 22954 PIT - FLT 335 - EN ROUTE FROM DFW TO PIT, CREW REPORTED THAT THE LT MLG UNSAFE LIGHT ILLUMINATES INTERMITTENTLY DURING F LIGHT. RECYCLED GEAR WITH NO POSITIVE RESULTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX TESTED GEAR INDICATION PER MM 32-61-00. INSPECTED AND CLEANED LEFT GEAR UPLOCK SENSOR. REPLACED M988 GEAR LOGIC CARD (P/N 8-060-02) AS PRECAUTION ARY AND TESTED PER MM 32-20-00. ALL INDICATIONS NORMAL. MCO - FLT 2238 - DURING CLIMB-OUT FROM LGA, THE LT MLG UNSAFE LIGHT ILLUMINATED 3 MINUTES AFTER NORMAL GEAR RETRACTION. GEAR LEVER WAS POSITIONED TO UP AND LIGHT EXTINGUISHED 2 MINU TES LATER. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT AT MCO. MX REMOVED AND REPLACED LT MLG UPLOCK SENSOR. 2 L 7 2 4F RT A16WE 1998041701034 19980417 01034 NM 1998 4 17 USAASB98060 1 19980311 A 3350 1000679 LIGHT ASSY BOEING 737 737201 1384454 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 248US 22755 LGA - FLT 956 - PRIOR TO DEPARTURE, MAINTENANCE WAS CALLED TO FIX AND INOP AFT EMERGENCY LIGHT. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998041701035 19980417 01035 NM 1998 4 17 USAASB98061 1 19980313 A 3350 1000679 LIGHT ASSY BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 285AU 23132 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE AFT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EX IT LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998041701036 19980417 01036 NM 1998 4 17 USAASB98062 1 19980313 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 518AU 23704 IAH - MAINTENANCE FOUND THE LEFT CENTER OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998041701037 19980417 01037 NM 1998 4 17 USAASB98063 1 19980312 A 2410 CSD BOEING 737 737201 1384454 NM NR 2 GENERATOR OUT OF ADJUST A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 246US 22753 BOS - FLT 1683 - AT 5,000 FEET, THE NR 2 GENERATOR DROPPED OFF LINE. CAPTAIN HAD A BRAND NEW FIRST OFFICER ON BOARD AND WAS NOT CERTAIN ABOUT THE RELIABILITY OF THE APU. CAPTAIN ELECTED TO RETURN TO FIELD AT BOS AFTER STARTING APU AND PLA CING APU'S GENERATOR ON LINE. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE AD JUSTED THE FREQUENCY ON THE NR 2 CSD. SYSTEM OPS CHECK GOOD ON GROUND RUN. (M) 2 L 7 2 4F A16WE 1998041701038 19980417 01038 EU 1998 4 17 USAAF98028 1 19980312 A 3234 715381 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAILED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 899US 11399 FLT 743 - PWM - ON APPROACH TO PWM THE LANDING GEAR SELECTOR HANDLE WOULD NOT MOVE FROM THE 'UP' POSITION. CREW PERFORM ED A GO AROUND AND LOWERED THE LANDING GEAR WITH THE ALTERNATE PROCEDURE. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND WA S TOWED TO THE GATE. MAINTENANCE CHECKED AIRCRAFT AND FOUND IT SAFE FOR MAINTENANCE FERRY FLIGHT TO CLT. CLT MAINTENAN CE REPLACED THE LANDING GEAR SELECTOR VALVE. (M) 2 L 7 2 4F RT 1998041701039 19980417 01039 EU 1998 4 17 USAAF98029 1 19980316 A 3620 FAULT LIGHT FOKKER F28 F28MK0100 4990807 EU BLEED SYSTEM ILLUMINATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 865US 11308 PIT - FLT 540 - AIRCRAFT WAS CLIMBING TO FL250 OUT OF PIT WHEN A BLEED FAULT 1 LIGHT ILLUMINATED. CAPTAIN DESCENDED TO FL240 AND TRIED TO RESET WITHOUT SUCCESS. FLIGHT RETURNED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENAN CE PERFORMED BLEED SYSTEM CHECKOUT AND FOUND NO DISCREPANCIES. (M) 2 L 7 2 4F RT 1998041701040 19980417 01040 WP 1998 4 17 USAAD98042 1 19980313 A 2130 1718561 HOSE DOUG DC9 DC931 3022065 WP LT ACM FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 923VJ 48143 BUF - FLT 2101 - DURING CLIMB-OUT, THE FLIGHT CREW WAS NOT ABLE TO MAINTAIN THE PROPER PRESSURIZATION SCHEDULED. THE AI RCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED A TORN FLEXIBLE DUCT AT THE LEFT ACM. T HE RIGHT AIR CONDITIONING PACK WAS ON MEL AT THE TIME. (M) 2 L 7 2 4F A6WE 1998041701041 19980417 01041 NE 1998 4 17 98ZZZM439 2 19980225 A 7250 TURBINE BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE DAMAGED A A RYNA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 07 421EX 19099 649670 FLT 613 - IND-CLT - HAD AN AIR TURN BACK TO IND. ON DEPARTURE FROM IND FELT VIBRATION IN RUDDER PEDAL'S AND FLOOR. NR 2 ENGINE HAD LOW N1 AND LOW EPR AND HIGH EGT. REMOVED AND REPLACED NR 2 ENGINE DUE TO TURBINE DAMAGE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998041701042 19980417 01042 NM 1998 4 17 98ZZZM440 1 19980315 A 2121 5007024620 FAN BOEING 727 72722C 138400F NM COCKPIT FAILED A RYNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 428EX 19097 FLT 707 - DEN-IND - SMELLED SMOKE IN COCKPIT AT FLT LEVEL 33,000 FT. GASPER FAN CIRCUIT BREAKER POPPED. DIVERTED TO MC I, DECLARED AN EMERGENCY. REMOVED AND REPLACED GASPER FAN. (M) 2 L 7 3 4F A3WE 1998041701043 19980417 01043 WP 1998 4 17 ORJA9848 1 19980313 A 3350 EM1267 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 880RA 53186 ROW 12-16 EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN LT FORWARD PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998041701044 19980417 01044 WP 1998 4 17 ORJA9852 1 19980316 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 FLOOR TRACK IS OUT ROW 14-17. REMOVED AND REPLACED EMERGENCY FLOOR PATH WAY LIGHTING BATTERY CHARGER AND OPS CHECK GOOD . (M) 2 L 7 2 4F RT A6WE 1998041701045 19980417 01045 WP 1998 4 17 HALA9800069 1 19980321 A 3244 TIRE DOUG DC9 DC951 3022051 WP RT MLG BLOWN A HALA K NONE O OTHER LD LANDING 1 WP 13 603DC 47784 OGG - FLT 548 - NR 4 MAIN TIRE BLEW OUT ON LANDING, IN OGG RT MLG DOOR BENT ON TRAILING EDGE, RT FLAP T/E AREA DAMAGED, AFT OF MLG IN TWO PLACES. AIRCRAFT WAS FERRIED TO HNL, DUE TO DAMAGE OF RT MLG OUTBOARD DOOR. REMOVED AND REPLACED NR 3 AND NR 4 MLG TIRES AND RIGHT MLG FLY DOOR ASSY. REPLACED DAMAGED AREA ON T/E OF FLAP. GEAR SWING AND DOOR FIT CHECK, ALL OK. (M) 2 L 7 2 4F RT A6WE 1998041701046 19980417 01046 WP 1998 4 17 HALA9800071 1 19980324 A 3350 600304031 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 661HA 47796 HNL - FLT 512 - EMERGENCY LIGHT CEILING ROW 6-12 DOES NOT COME ON DURING PREFLIGHT TEST. REPLACED BATTERY FOR EMERGENCY LIGHTS FOR ROW 6-12, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998041701047 19980417 01047 NM 1998 4 17 GAIA9827 1 19980227 A 2612 894120 FIRE LOOP BOEING 727 727214 138407R NM NR 2 ENGINE SHORTED A GAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 751US 8194 21513 NR 2 ENGINE FIRE INDICATIONS IN FLIGHT, LIGHT AND BELL. AIRCRAFT MADE AN UNEVENTFUL RETURN TO TOL. REMOVED AND REPLACE D NR 2 ENGINE LOWER FIRE DETECTION LOOP IAW B-727 MM 26-10. OPERATIONAL CHECKS GOOD ON GROUND. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 3 4F A3WE 1998041701048 19980417 01048 NM 1998 4 17 GAIA9824 1 19980225 A 2611 302842 SMOKE DETECTOR BOEING 727 727223 1384074 NM CARGO COMPT FAILED A GAIA K NONE N FALSE WARNING LD LANDING 1 SW 07 854AA 20995 CARGO SMOKE LIGHT CAME ON LANDING IN TOL. NO SMOKE IN THE AIRPLANE. THE TAXI TO THE GATE WAS UNEVENTFUL. FOUND NR 5 S MOKE DETECTOR NOT OPERATING PROPERLY. REMOVED AND REPLACED NR 5 DETECTOR IAW B-727 MM, CHAPTER 26-10. FUNCTIONALLY CHE CKS GOOD. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER DISCREPANCIES. (M) 2 L 7 3 4F A3WE 1998041701049 19980417 01049 WP 1998 4 17 98ZZZM441 1 19980312 A 3610 37771641 DUCT DOUG DC8 DC861 3021952 WP NR 2 ENGINE LOOSE A FXLA O OTHER J M WARNING INDICATION OVER TEMP CR CRUISE 1 SO 19 30UA 54700 45888 DURING CRUISE MASTER FIRE WARNING LIGHT CAME ON. VERIFIED NR 2 ENGINE AT FAULT. REDUCED POWER AND LIGHT WENT OUT. TES TED FIRE WARNING SYSTEM WHICH WAS SATISFACTORY. RESTORED POWER AND NO FURTHER INDICATION. GROUND INSPECTION REVEALED L OW PRESS PNEUMATIC DUCT LOOSE. TIGHTENED AND SECURED GLAND NUT. RAN ENGINE FOR 20 MINUTES AND SYSTEM CHECKED NORMAL. R ETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1998041701050 19980417 01050 WP 1998 4 17 98ZZZM442 1 19980321 A 2730 4644177 CRANK ASSY DOUG DC8 DC851 3021920 WP RT ELEVATOR CRACKED A A FXLA O OTHER F FLT CONT AFFECTED TO TAKEOFF 1 SO 19 507DC 69023 45855 ON ARRIVAL MIA PILOT REPORTED LEFT WING VERY HEAVY ON TAKEOFF AND LANDING. GROUND INSPECTION REVEALED A BROKEN CRANK AS SEMBLY AT THE RIGHT ELEVATOR BUS TORQUE TUBE. THE BREAK OCCURRED AT THE LARGE DIAMETER HOLE WHERE THE CRANK ASSY MOUNTS ON THE ELEVATOR BUS TORQUE TUBE. IT APPEARS A CRACK EMANATED FROM THE THROUGH BOLT RETAINING HOLE OF THE CRANK CAUSING THE CRANK TO SEPARATE FROM THE BUS TORQUE TUBE. THE CRANK ASSY WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1998041701051 19980417 01051 NM 1998 4 17 EISA98056 1 19980319 A 3297 WIRE BOEING 727 7272M7 138407S NM LANDING GEAR BROKEN A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 742RW 21952 ON TAKEOFF IN MSP, THE GEAR FAILED TO RETRACT, PERFORMED CHECKLIST AND RETRACTED GEAR BY PULLING THE OVERRIDE RELEASE LA TCH, FLIGHT CONTINUED TO FINAL DESTINATION CANCUN. TROUBLESHOT ELECTRICAL CIRCUIT. ONE BROKEN WIRE WAS FOUND IN SOLENO ID CONNECTOR. REPAIRED AND TESTED OK IAW MM 32-31-11. (M) 2 L 7 3 4F A3WE 1998041701052 19980417 01052 SO 1998 4 17 98ZZZM443 1 19980112 A 5510 11014110731 BRACKET EMB 110 EMB110P1 3260122 SO HORIZ STAB CRACKED A BQTA K NONE O OTHER IN INSP/MAINT 1 NE 05 101TN 15771 110271 AT FRAME STATION 33, LEFT FORWARD UPPR SUPPORT BRACKET, P/N 110-1411-07-31, FOUND CRACKED DURING DYE PENETRANT INSPECTIO N PER AD 83-14-09. CRACK EXTENDED APPROXIMATELY .125 INCH THROUGH .1875 INCH FROM BOLT HOLE. BRACKET WAS REPLACED. 1 L 7 2 4T A21SO 1998041701053 19980417 01053 SO 1998 4 17 98ZZZM444 1 19980131 A 2731 110321004 BRACKET EMB 110 EMB110P1 3260122 SO TRIM ACTUATOR CRACKED A BQTA K NONE O OTHER IN INSP/MAINT 1 NE 05 790RA 11464 11027B ELEVATOR TRIM TAB ACTUATOR SUPPORT, PART NR 110-3210-04, FOUND CRACKED DURING INSPECTION PER AD 91-25-09. BRACKET WAS R EPLACED. (M) 1 L 7 2 4T A21SO 1998041701054 19980417 01054 WP 1998 4 17 ORJA9853 1 19980317 A 3350 EM1267 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 EMERGENCY LAMPS INOP O/H ROWS 6-9. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998041701058 19980417 01058 WP 1998 4 17 ORJA9854 1 19980318 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 OVERWING FORWARD LEFT EMERGENCY FLOOR LIGHTS POWER SUPPLY WON'T SHUT OFF EMERGENCY LIGHTS REMAIN ON UNTIL BATTERY EXHAUS TION. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 1998041701059 19980417 01059 WP 1998 4 17 ORJA9844 1 19980313 A 2913 AS66411LS666 HYD PUMP DOUG DC9 DC983 3022083 WP NR 2 ENGINE INOPERATIVE A ORJA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 876RA 53183 NO HYDRAULIC PRESSURE ON RIGHT ENGINE START RETURNED TO GATE. REMOVED AND REPLACED NR 2 ENGINE DRIVEN HYD PUMP IAW MM 2 9-10-05 LEAK AND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998041701060 19980417 01060 WP 1998 4 17 ORJA9838 1 19980310 A 4920 P839 APU DOUG DC9 DC987 3022087 WP APU COMPT INOPERATIVE A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 755RA 49727 AT PUSH BACK, FOUND APU TO BE INOP RETURNED TO GATE, REF DMI NR 13018. (M) 2 L 7 2 4F RT A6WE 1998041701061 19980417 01061 WP 1998 4 17 ORJA9842 1 19980313 A 7711 CIRCUIT BREAKER DOUG DC9 DC982 3022082 WP NR 1 EPR TRIPPED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 11 824RA 53017 ABORTED TAKEOFF DUE TO NO EPR ON LEFT ENGINE AT POWER UP. CHECKED INLET AND EXHAUST RESET NR 1 EPR AND NR 1 DFGC CIRCUI T BREAKERS, OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998041701062 19980417 01062 WP 1998 4 17 ORJA9839 1 19980311 A 3350 PIN DOUG DC9 DC983 3022083 WP CABIN NOT SECURED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 ROW 7D EMERGENCY AISLE LIGHT OUT. FOUND RECESSED PIN AT SIDE WALL, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998041701063 19980417 01063 WP 1998 4 17 ORJA9843 1 19980313 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC987 3022087 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 ROWS 15-18 AIRCRAFT RIGHT EMERGENCY LIGHTS STAY ON IN ARMED POSITION 18, REST OF THE SYSTEM WORKS NORMALLY. REMOVED AND REPLACED BATTERY CHARGER AT SEAT 18A, SYSTEM OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998041701064 19980417 01064 WP 1998 4 17 ORJA9841 1 19980309 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS INOP FROM ROW 12 THROUGH 16. REMOVED AND REPLACED BATTERY CHARGER ASSY AT LEFT MID EXIT, OPS CHECK GOO D. (M) 2 L 7 2 4F RT A6WE 1998041701065 19980417 01065 WP 1998 4 17 ASAA9880057 1 19980321 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 964AS 53078 SEA - PRIOR TO DEPARTURE FO FLT 722, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998041701066 19980417 01066 WP 1998 4 17 ASAA9880056 1 19980320 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 2167 49126 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998041701067 19980417 01067 WP 1998 4 17 ASAA9880055 1 19980320 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 23 AFT WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998041701068 19980417 01068 WP 1998 4 17 ASAA9880054 1 19980316 A 3350 0105606005 LAMP DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 33 AFT WERE FOUND INOPERATIVE. REPLACED LAMP MODULE AT ROW 33 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998041701069 19980417 01069 WP 1998 4 17 ASAA9880053 1 19980315 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 17 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998041701070 19980417 01070 WP 1998 4 17 ASAA9880052 1 19980315 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP COCKPIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND INOPERATIVE. REPLACE D THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998041701071 19980417 01071 NM 1998 4 17 ASAA9840055 1 19980316 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 17 AND THE AFT FOUR LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998041701073 19980417 01073 NM 1998 4 17 ASAA9840053 1 19980310 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998041701074 19980417 01074 NM 1998 4 17 ASAA9810021 1 19980306 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING RECON, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT PALLET NR 4-8 WERE FOUND TO BE INOPERATIVE. REPLACED BATTE RY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998041701075 19980417 01075 SW 1998 4 17 HEEA0013476 1 19980319 A 7933 214175253103 INDICATOR BELL 214 214ST 1182106 SW OIL TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 INDICATOR READS LOW ON TEMP SIDE. 2 G 7 2 4U H10SW 1998041701076 19980417 01076 SW 1998 4 17 HEEA0013546 1 19980326 A 2400 214175132103 RELAY BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 CONTACT BALL NR2 TO 24V OPEN IN REST POSITION. 2 G 7 2 4U H10SW 1998041701077 19980417 01077 SW 1998 4 17 HEEA0013704 1 19980402 A 2840 391046197 PROBE BELL 412 412 1182202 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 INDICATES HIGH OUT OF TOLERANCE; WIRE CRUSHED. 1 G 7 2 4U H4SW 1998041701078 19980417 01078 1998 4 17 HEEA0013780 4 19980402 A 2210 214074305105 AMPLIFIER BELL 214 214ST 1182106 SW AUTO FLIGHT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59805 28141 AMPLIFIER FAILED MONITOR TEST. 2 G 7 2 4U H10SW 1998041701079 19980417 01079 SW 1998 4 17 HEEA0013781 1 19980402 A 2931 214175252101 INDICATOR BELL 214 214ST 1182106 SW HYD SYS ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 HYD PRESS INDICATOR ERRATIC READINGS. 2 G 7 2 4U H10SW 1998041701080 19980417 01080 1998 4 17 HEEA0013782 4 19980402 A 3420 214074300107 AFCS BELL 214 214ST 1182106 SW ANNUN PANEL INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 AFCS ENGAGE INTERMITTENT. 2 G 7 2 4U H10SW 1998041701081 19980417 01081 1998 4 17 HEEA0013783 4 19980402 A 2210 214074305105 AMPLIFIER BELL 214 214ST 1182106 SW AUTOFLIGHT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 59805 28141 AMPLIFIER FAILED MONITOR TEST. 2 G 7 2 4U H10SW 1998041701082 19980417 01082 SW 1998 4 17 HEEA0013784 1 19980402 A 2400 M833830207 CIRCUIT BREAKER BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 CHARGES MOTION OUTPUT NOT CHARGING BATTERY. 2 G 7 2 4U H10SW 1998041701083 19980417 01083 SW 1998 4 17 HEEA0013796 1 19980402 A 7931 209062002001 INDICATOR BELL 412 412 1182202 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 INDICATOR ALWAYS POPPED. 1 G 7 2 4U H4SW 1998041701084 19980417 01084 SW 1998 4 17 HEEA0013814 1 19980402 A 2430 214175133103 RELAY BELL 214 214ST 1182106 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 INOPERATIVE. 2 G 7 2 4U H10SW 1998041701085 19980417 01085 SW 1998 4 17 HEEA0013817 1 19980402 A 6320 8538100 OIL COOLER BELL 412 412 1182202 SW XMSN LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 2261D 33076 OIL COOLER LEAKING. 1 G 7 2 4U H4SW 1998041701086 19980417 01086 1998 4 17 HEEA0013827 4 19980402 A 2210 11788810 TRANSDUCER BOLKMS 117 BK117B2 5626013 EU CSAS MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 134AE 7237 TRANSDUCER CAUSES ERRATIC READINGS. 1 G 7 2 3U NC H13EU 1998041701087 19980417 01087 WP 1998 4 17 9806531141 1 19980414 A 3251 ACG74405505 CYLINDER DOUG DC10 DC1040 3023508 WP NLG STEERING FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 01 141US 47096 6446 46750 DURING TAKEOFF ROLL, LOST NR 1 HYDRAULIC SYSTEM. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE FOUND THE LEFT NOSE WHEEL STEERING CYLINDER LEAKING. REPLACED THE STEERING CYLINDER, CHECKED FILTERS, AND REFILLED SYSTEM. LEAK AND O PERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998041701089 19980417 01089 NE 1998 4 17 9806552298 2 19980413 A 7321 FUEL CONTROL BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE CENTER ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 298US 22152 700623 AS TAKEOFF POWER WAS APPLIED, THE CENTER ENGINE EPR INDICATION WOULD NOT REACH TARGET EPR SETTING. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE CENTER ENGINE FUEL CONTROL UNIT, OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998041701090 19980417 01090 EU 1998 4 17 9806563240 1 19980410 A 3310 EO05301 LIGHT AIRBUS 320 A320212 EU COCKPIT INOPERATIVE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 340NW 372 FOLLOWING TAKEOFF, SMOKE WAS OBSERVED IN THE COCKPIT AND A COCKPIT LIGHTING CIRCUIT BREAKER POPPED. CREW DONNED OXYGEN MASKS, DECLARED AN EMERGENCY, RETURNED TO DTW, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FIRST OFFICER'S FL OOR LIGHT ASSEMBLIES AND MAP LIGHT ASSEMBLY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998041701091 19980417 01091 EU 1998 4 17 9806573209 1 19980410 A 2150 PACK AIRBUS 320 A320211 3930320 EU NR 1 OVERHEAT A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 309US 118 FOLLOWING TAKEOFF, GRAY SMOKE WITH AN OILY SMELL WAS OBSERVED IN THE COCKPIT AND CABIN. CREW PERFORMED THE AIR CONDITION ING SMOKE PROCEDURE PER COCKPIT OPERATING MANUAL AND DECLARED AN EMERGENCY, RETURNED TO DTW, AND LANDED WITHOUT INCIDEN T. NR 1 PACK WAS PLACED ON DEFERRAL PER MEL 21-52-01A. SUBSEQUENT MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIE S. NR 1 PACK OPERATIONALLY CHECKED OK. 2 L 7 2 4F RT A28NM 1998041701092 19980417 01092 1998 4 17 9806589602 4 19980414 A 3442 G1519 CONTROL PANEL DOUG DC9 DC932 3022066 WP FLIGHT DECK INOPERATIVE A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 602NW 5115 5115 47046 DURING CLIMBOUT, THE WEATHER RADAR WOULD NOT MAP IN ANY POSITION. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED THE RADAR CONTROL PANEL, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041701093 19980417 01093 WP 1998 4 17 9806599957 1 19980412 A 2720 RUDDER VALVE DOUG DC9 DC931 3022065 WP TAIL OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 915RW 47139 DURING CLIMBOUT, THE FLAP/RUDDER STOP INOPERATIVE INDICATION ILLUMINATED. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INC IDENT. THE FLIGHT CREW NOTED THAT THE RUDDER/STOP INDICATION LIGHT EXTINGUISHED WHEN FLAPS WERE EXTENDED FOR LANDING. M AINTENANCE ADJUSTED AND TESTED THE AUXILIARY RUDDER THROW LIMITER CONTROL VALVE IN ACCORDANCE WITH MAINTENANCE MANUAL SP ECIFICATIONS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041701094 19980417 01094 WP 1998 4 17 9806609910 1 19980411 A 3150 T/O WARNING DOUG DC9 DC931 3022065 WP COCKPIT SOUNDED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 960N 47256 ON DEPARTURE, THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. FLIGHT CREW RESET FLAPS, MOVED TRIM, AND RESET SP EEDBRAKE HANDLE WITH NO FURTHER OCCURRANCE OF WARNING. MAINTENANCE PERFORMED TAKEOFF WARNING SYSTEM TEST PER MAINTENANC E MANUAL PROCEDURES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041701095 19980417 01095 WP 1998 4 17 9806619965 1 19980413 A 3350 LIGHT DOUG DC9 DC931 3022065 WP TAIL COMPT INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 911RW 47149 DURING LINE CHECK, FOUND EMERGENCY LIGHT IN TAIL COMPARTMENT WALKWAY INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMB LY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998041701096 19980417 01096 WP 1998 4 17 9806629863 1 19980414 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, FOUND TAIL AREA EMERGENCY EXIT LIGHT DIM. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES, OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998041701097 19980417 01097 WP 1998 4 17 9806639919 1 19980414 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 941N 47450 DURING LINE CHECK, FOUND ESCAPE PATH LIGHTING AT SEAT ROWS 8 THRU 10 INOPERATIVE. MAINTENANCE REPLACED FUSE, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1998041701098 19980417 01098 WP 1998 4 17 9806649954 1 19980414 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 921RW 47164 DURING LINE CHECK, FOUND SEAT 2C EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F A6WE 1998041701099 19980417 01099 WP 1998 4 17 9806659958 1 19980414 A 3260 SENSOR DOUG DC9 DC931 3022065 WP RT MLG DOOR INOPERATIVE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 917RW 47145 DURING TAKEOFF, THE MAIN LANDING GEAR DOOR OPEN INDICATION ILLUMINATED. THE FLIGHT CREW ABORTED THE TAKEOFF AND RETURNE D TO BOARDING GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOOR SENSOR AND PERFORMED A TEST OF PROXIMITY SENSOR ELECTRONICS UNIT IN ACCORDANCE WITH MAINTENANCE MANUAL PROCEDURES. OPERATIONAL TEST NORMAL. 2 L 7 2 4F A6WE 1998041701100 19980417 01100 NM 1998 4 17 UPS98226420 1 19980410 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 420 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 942UP 19101 INSPECTION TYPE-C, WHILE WORKING NRC FUSELAGE 70 CUSTOMER NR 677615 DISCOVERED STRINGER AND STRINGER TIE CORRODED BS 420 STR 23R. REPAIRED STRINGER FROM BS 416 TO 440 PER 727 SRM 53-10-3 AND REPAIRED STRINGER TIE PER SRM 53-10-3, 51-30-2 A ND 53-10-1. 2 L 7 3 4F A3WE 1998041701101 19980417 01101 WP 1998 4 17 UPS98826409 1 19980329 A 5320 3779659501 FITTING DOUG DC8 DC873F 302199F WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN AT STA 902 AND LONG 6L, THE LONG END FITTING IS CRACKED AND HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998041701102 19980417 01102 WP 1998 4 17 UPS98826410 1 19980401 A 5311 97549199 FRAME DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1180 FRAME AT STR 9R HAS A SMALL CRACK. REPAIRED AREA IAW DWG 9754919 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041701103 19980417 01103 WP 1998 4 17 UPS98826411 1 19980404 A 5320 37558472N FITTING DOUG DC8 DC873F 302199F WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1160 JUST ABOVE STR 33R, THE SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041701104 19980417 01104 WP 1998 4 17 UPS98826412 1 19980331 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 25-60 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 25 TO 60 RBL36 TO 48, THE DOUBLER UNDER THE LAV FLOOR IS CORRODED. REMOVED, FABRICATED AND INSTA LLED REPLACEMENT DOUBLER IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998041701105 19980417 01105 WP 1998 4 17 UPS98826413 1 19980331 A 5320 5612298339 DOUBLER DOUG DC8 DC873F 302199F WP BS 10-30 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, COCKPIT SUB FLOOR AT STA -30 TO -10, RBL 24 TO 29, THE FINGER DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5612298 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041701106 19980417 01106 WP 1998 4 17 UPS98826414 1 19980402 A 5320 561229877 DOUBLER DOUG DC8 DC873F 302199F WP BS 10-30 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, COCKPIT SUB FLOOR AT STA -30 TO -10 LBL 16 TO 24, THE FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMO VED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5612298-77 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041701107 19980417 01107 WP 1998 4 17 UPS98826415 1 19980405 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 858 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, RT WING L/E O/B SECTION AT STA XFS858.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998041701108 19980417 01108 WP 1998 4 17 UPS98826416 1 19980331 A 5720 561378521 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, COCKPIT SUB FLOOR AT STA -80, LBL 59, THE VERTICAL INTERCOSTAL IS CRACKED AT THE LWR END. REMOVED, F ABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5613785 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998041701109 19980417 01109 WP 1998 4 17 UPS98826417 1 19980325 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 74 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, LT WING UPPER SURFACE IS CRACKED AT STA XRS 74 JUST FWD OF STR 9. REPAIRED AREA IAW SRM 57-2-1 FIG 1 0. 2 L 7 4 4F RT 4A25 1998041701110 19980417 01110 WP 1998 4 17 UPS98826418 1 19980403 A 5320 46401622 FITTING DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1540 AT STR 21L, THE FLOOR TO CUSP TIE FITTING IS CORRODED BEYOND LIMITS. REMOVE AND REPLACE D FITTING IAW DWG 4640162 AND SRM 53-2-0 FIG 20. 2 L 7 4 4F RT 4A25 1998041701111 19980417 01111 WP 1998 4 17 UPS98826419 1 19980327 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 709.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, LT WING L/E SKIN AT STA XFS 709.5 HAS INTERGRANNULAR CORROSION AROUND 2 FASTENERS. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998041701112 19980417 01112 WP 1998 4 17 UPS98826421 1 19980326 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 622.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998041701113 19980417 01113 WP 1998 4 17 UPS98826422 1 19980329 A 5320 FRAME DOUG DC8 DC873F 302199F WP LT COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, FRAME CRACKED IN RADIUS, JUST FWD OF CAPT'S WINDSHIELD. INSIDE RAIN REMOVAL PLENUM ACCESS PLATE #94L , UPPER INBD CORNER. REPAIRED IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1998041701114 19980417 01114 WP 1998 4 17 UPS98826423 1 19980325 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, RT SIDE FWD SERVICE DOOR UPPER FWD CORNER CRACKED. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998041701115 19980417 01115 WP 1998 4 17 UPS98826424 1 19980327 A 5542 5644210505 SKIN DOUG DC8 DC873F 302199F WP RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, RUDDER UPPER RT SIDE T/E BETWEEN UPPER STATIC WICKS IS A SMALL AREA OF CORROSION. REMOVED AND REPLAC ED RUDDER IAW M/M 27-21-01. 2 L 7 4 4F RT 4A25 1998041701116 19980417 01116 WP 1998 4 17 UPS98826425 1 19980328 A 2780 37701441 FITTING DOUG DC8 DC873F 302199F WP RT LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, RT O/B SLOT TORQUE TUBE I/B END FITTING IS CRACKED IN RADIUS. REMOVED AND REPLACED FITTING IAW M/M 2 7-80-05. 2 L 7 4 4F RT 4A25 1998041701117 19980417 01117 WP 1998 4 17 UPS98826426 1 19980329 A 5512 SKIN DOUG DC8 DC873F 302199F WP LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, LT HORZ STAB INBD L/E HAS FILLIFORM CORROSION OUTBD END L/E XFS 197.5. REPAIRED IAW SRM 55-2-1. 2 L 7 4 4F RT 4A25 1998041701118 19980417 01118 WP 1998 4 17 UPS98826427 1 19980401 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, RT WING I/B STUB WING I/B RIB FWD LWR CORNER HAS CRACK IN RADIUS. REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998041701119 19980417 01119 WP 1998 4 17 UPS98826428 1 19980328 A 5313 3648667 LONGERON DOUG DC8 DC873F 302199F WP BS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-D, FS 55 LONGERON 30R WAS FOUND WITH CORROSION REMOVAL BEYOND SRM LIMITS. REMOVED AND REPLACED LONGERON IAW SRM 51-3-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998041701120 19980417 01120 WP 1998 4 17 UPS98826429 1 19980313 A 5720 CLIP DOUG DC8 DC873F 302199F WP BS 855 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE-C, CORROSION ON CENTER WING SPAR FITTINGS FS 855 INSIDE LT W/W BELOW UPPER CORNER. REMOVED CLIP, DRILLE D AND INSTALLED IAW DC8 SRM 57-2-3. 2 L 7 4 4F RT 4A25 1998041701121 19980417 01121 EU 1998 4 17 QXEA9800524 1 19980410 A 3350 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 EMERGENCY EXIT SIGN ON SIDEWALL BY SEAT 9A/B INOP. REMOVED AND REPLACED EMERGENCY EXIT SIGN, OPERATIONAL TESTS GOOD. 2 L 7 2 4F RT A20EU 1998041701122 19980417 01122 EU 1998 4 17 QXEA9800525 1 19980410 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED EXIT LIGHT ASSEMBLY, OPERATIONAL TEST IS GOOD. 2 L 7 2 4F RT A20EU 1998041701123 19980417 01123 EU 1998 4 17 QXEA9800526 1 19980412 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 TOP EMERGENCY EXIT LIGHT AT GALLEY SERVICE DOOR INOP. RELAMPED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998041701124 19980417 01124 EU 1998 4 17 QXEA9800527 1 19980412 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 EXIT LIGHT OVER DOOR, ROW 8 INOP. RELAMPED, OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A20EU 1998041701125 19980417 01125 EU 1998 4 17 QXEA9800528 1 19980413 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 EXIT LIGHT OUT AT 9A. REPLACED BULB, OPERATIONAL TEST GOOD. 2 L 7 2 4F RT A20EU 1998041701126 19980417 01126 EU 1998 4 17 QXEA9800529 1 19980414 A 3350 CONNECTION FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 SEAT EVACUATION LIGHTS ON FRONT 6 ROWS ARE ON WITH THE EMERGENCY LIGHT SWITCH IN ARM POSITION. MAINTENANCE INSPECTED AN D FOUND LOOSE CONNECTION AT SEAT ROW 1AB. SECURED CONNECTION, OPERATIONAL TEST IS GOOD. 2 L 7 2 4F RT A20EU 1998041701127 19980417 01127 WP 1998 4 17 98FDEA00266 1 19980413 A 5270 WARNING SYST DOUG DC10 DC1030F 3023504 WP CABIN DOOR MALFUNCTION A FDEA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 25 317FE 46835 AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. DISCOVERED 6 FT AFT CABIN DOOR OPEN APPROX 2.5 INCHES. DUMPED FUEL AND L ANDED VCP WITHOUT INCIDENT. RESET DOOR PER M/M 52-10-01-2 ARMS OK. CHECKED FOR ELECTRICAL ANOMOLIES TO LOCK PIN RELEAS E AND ACTUATOR. FOUND NO POWER COMING OUT OF AFT DOOR LIMIT SWITCH IN THE DOOR STOW POSITION. OK TO CONTINUE ON PREVIO US DEFERRED. INSTALLED DOOR WARNING LIGHT STRIKER PLATE, POSITION SWITCH PER M/M 52-70-00, DOOR INDICATION OPS CHECK GO OD PER M/M 52-70-00. 2 L 7 3 4F RT A22WE 1998041701128 19980417 01128 NM 1998 4 17 98UAL900105 1 19980307 A 2750 DISAGREE LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 572UA 26682 AIRCRAFT DIVERTED TO SLC DUE TO TE FLAPS DISAGREEMENT INDICATION. *S/D* AIRCRAFT OPERATIONALLY CHECKED GOOD, NO DISCRE PANCIES FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041701129 19980417 01129 NM 1998 4 17 98UAL900108 1 19980306 A 2410 CSD SUNDSTRAND 705117E BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE FAILED A A UALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 154UA 1422 20103 APPROXIMATELY ONE HOUR PRIOR TO ARRIVAL AT HNL NR 4 ENGINE CSD OVER TEMPERATURE. PROCEDURES 733 AND 734 INEFFECTIVE IN DISCONNECTING THE CSD. SHUT DOWN NR 4 ENGINE. LANDED UNDER AMBER ALERT. *S/D* ROOT CAUSE CANNOT BE DETERMINED DUE TO EXTENSIVE DAMAGE TO CSD. THE UNIT WILL BE SCRAPPED. THE SOLDER FOR THE DISCONNECT SOLENOID WIRES WAS MELTED AND IT C ANNOT BE DETERMINED WHEN IT OCCURRED. THE CSD WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1998041701130 19980417 01130 NE 1998 4 17 98UAL900136 2 19980403 A 7230 COMPRESSOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 9 RT ENGINE STALLED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 555UA 26647 RETURNED TO FIELD AFTER HEARING LOUD NOISE AND SEEING A FLASH FROM THE RIGHT SIDE OF AIRCRAFT. ENGINES OPERATED NORMALL Y UPON RETURN. *S/D* AUTOTHROTTLES ON, NO ABNORMAL INDICATIONS ON ANY ENG INSTRUMENT, NO EICAS MESSAGES. RETURNED TO ORD WITH NO FURTHER PROBLEMS- ENGINES OPERATED NORMALLY DURING RETURN. ACCOMPLISHED FIM 71-05-00 PG104-105. NO DEFECTS ON BORESCOPE, CHIP DETECTORS, OR MESSAGES. REPLACED OIL FILTER MM 79-21-05. NO LEAKS NOTED AFTER ENGINE RUNUP. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041701131 19980417 01131 NM 1998 4 17 98UAL900137 1 19980312 A 5210 AW6VCRG BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2L WORN A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 508UA 24744 UPON ARRIVAL, AGENT COULD NOT FULLY OPEN DOOR 2L. DOOR ONLY SWINGS TO THREE QUARTERS OF FULL TRAVEL. *S/D* REPLACED D OOR 2L ROTARY SNUBBER AND UPPER AND LOWER HINGE LINK BEARINGS, OPS CHECKED NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998041701132 19980417 01132 NM 1998 4 17 98UAL900138 1 19980404 A 3230 PIN BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT MLG INSTALLED A UALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C TO TAKEOFF 1 WP 29 378UA 24653 DURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED WITH THE THROTTLES ADVANCED. PULLING THE AIR-GROUND CIRCUIT BREAKER SI LENCED THE HORN. *S/D* DURING PROBLEM IDENTIFICATION AND TROUBLESHOOTING, MAINTENANCE FOUND THE RIGHT HAND MAIN LANDIN G GEAR SAFETY SENSOR WITH RIG PINS INSTALLED AND THE TELEFLEX CABLE OUT OF RIG. REMOVED RIG PINS, RIGGED SAFETY SENSOR AND CONDUCTED OPERATIONAL CHECK PER AURAL WARNING SYSTEM TEST PROCEDURE, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041701133 19980417 01133 NM 1998 4 17 98UAL900139 1 19980406 A 3350 582233 POWER SUPPLY BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 174UA 24381 EMERGENCY EXIT LIGHTS INTERMITTENT ROWS 51 TO 59 LEFT HAND SIDE E-ZONE. *S/D* DEFECTIVE BATTERY PACK WAS REMOVED AND R EPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 1998041701134 19980417 01134 1998 4 17 98UAL900140 4 19980403 A 3422 GYRO SPERRY 25883024MOD BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 977UA 21508 THE FIRST OFFICER'S HSI AND THE CAPTAIN'S RMI HAD GYRO FLAGS DURING TURNS. *S/D* UNIT SLIP RINGS WERE A LITTLE LOOSE. REPLACED NUMBER TWO DIRECTIONAL GYRO, OPS CHECK GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1998041701135 19980417 01135 WP 1998 4 17 ABXA9800328 1 19980410 A 5313 59114279 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND LONGERON 17L AT STATION 945 CRACKED. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041701136 19980417 01136 WP 1998 4 17 ABXA9800329 1 19980410 A 5320 3917624511 FITTING DOUG DOUG DC9 DC931 3022065 WP CARGO DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND THE VERTICAL DOOR JAMB SUPPORT FITTING CRACKED AT RIGHT SIDE, BEHIND LOWER STOP PLATE. REPLACED F ITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041701137 19980417 01137 WP 1998 4 17 ABXA9800330 1 19980410 A 5320 991050311 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND A CRACKED ANGLE AT STATION 996 AND LONGERON 18R. REPLACED ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998041701138 19980417 01138 WP 1998 4 17 ABXA9800331 1 19980408 A 2760 3923257501N FITTING DOUG DOUG DC9 DC931 3022065 WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND THE RIGHT INBOARD SPOILER TORQUE TUBE CENTER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SR M 51-10-4. 2 L 7 2 4F A6WE 1998041701139 19980417 01139 WP 1998 4 17 ABXA9800332 1 19980410 A 5320 991555411 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND INTERCOSTAL ANGLE CRACKED AT STATION 237 BETWEEN LONGERONS 27R AND 28R. REPLACED ANGLE IAW DC9 SR M 51-30-2, 51-30-5 AND DACO DWG 9915554. 2 L 7 2 4F A6WE 1998041701140 19980417 01140 WP 1998 4 17 ABXA9800333 1 19980410 A 5320 99155547 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND INTERCOSTAL ANGLE CRACKED AT STATION 237 BETWEEN LONGERONS 27L AND 28L. REPLACED ANGLE IAW DC9 SR M 51-30-2 AND DACO DWG 9915554. 2 L 7 2 4F A6WE 1998041701141 19980417 01141 WP 1998 4 17 ABXA9800334 1 19980408 A 5320 991050313 WEB DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 965 RIGHT SIDE RBL 44. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998041701142 19980417 01142 WP 1998 4 17 ABXA9800335 1 19980408 A 5320 39571751 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 1121 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND FITTING JUST FWD OF CANTED FRAME STATION 1121 AT VENTRAL STAIR LEFT JAMB CRACKED. REPLACED FITTIN G IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998041701143 19980417 01143 WP 1998 4 17 ABXA9800336 1 19980408 A 5320 9912243225 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND A CRACKED ATTACH ANGLE AT STATION 965 LONGERON 17L FWD PYLON BULKHEAD. REPLACED ANGLE IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998041701144 19980417 01144 WP 1998 4 17 ABXA9800337 1 19980408 A 5312 9912243225 BULKHEAD ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND THE PYLON BULKHEAD TO LONGERON 17R SHEAR CLIP ANGLE CRACKED AT STA 965. REPLACED ANGLE IAW DC9 SR M 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998041701145 19980417 01145 WP 1998 4 17 ABXA9800338 1 19980408 A 5320 3916209502 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND STATION 680 FLOOR SUPPORT BEAM TO CENTER TANK VERTICAL SUPPORT LEG CRACKED IN 3 PLACES. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-3. 2 L 7 2 4F A6WE 1998041701146 19980417 01146 WP 1998 4 17 ABXA9800339 1 19980408 A 5312 3917624511 BULKHEAD FITTING DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND THE LOWER AFT PRESSURE BULKHEAD DOOR FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998041701147 19980417 01147 WP 1998 4 17 ABXA9800340 1 19980408 A 5320 3917285503 FITTING DOUG DOUG DC9 DC941 302207N WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 958AX 47760 DURING C-CHECK, FOUND THE LEFT FLOOR TO KEEL ATTACH FITTING AT STATION 737 CRACKED. REPLACED CRACKED FITTING IAW DC9 SR M 51-30-1. 2 L 7 2 4F A6WE 1998041701148 19980417 01148 WP 1998 4 17 ABXA9800341 1 19980408 A 5313 591141555 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 756 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LONGERON 7L CRACKED AT STATION 756. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998041701149 19980417 01149 WP 1998 4 17 ABXA9800342 1 19980406 A 5311 991183913 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 1104 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND CANTED FRAME STATION 1104 CRACKED AT LONGERON 13R. REPLACED CANTED FRAME IAW DC9 SRM 51-30-52. 2 L 7 2 4F A6WE 1998041701150 19980417 01150 WP 1998 4 17 MWEA98398 1 19980413 A 5712 9919353 RIB DOUG DC9 DC932 3022066 WP WS 164 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION WAS FOUND ALONG THE UPPER SURFACE OF THE LOWER CUP OF THE RIB AT WING STATION XRS 164 LEFT SIDE. CLEANED CORR OSION AND INSTALLED STRAP REPAIR USING APPROVED DATA. 2 L 7 2 4F A6WE 1998041701151 19980417 01151 WP 1998 4 17 MWEA98399 1 19980413 A 5311 995791739 FRAME DOUG DC9 DC932 3022066 WP BS 937 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION AND EXCESSIVE DRILL MARKS WERE FOUND ON FRAME AT FUSELAGE STATION 937. REMOVED CORROSION AND DAMAGED AREA FAB RICATED AND INSTALLED REPAIR PARTS USING APPROVED DATA. 2 L 7 2 4F A6WE 1998041701152 19980417 01152 WP 1998 4 17 MWEA98400 1 19980413 A 5720 4912003 CLIP DOUG DC9 DC932 3022066 WP WS 111 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING FUEL TANK STRINGER 22 LEFT HAS A CRACKED CLIP A STATION XRS 111. REMOVED OLD CLIP FABRICATED AND INSTALLED RE PLACEMENT CLIP. 2 L 7 2 4F A6WE 1998041701153 19980417 01153 WP 1998 4 17 MWEA98401 1 19980413 A 5720 4913188 CLIP DOUG DC9 DC932 3022066 WP WS 111 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING FUEL TANK STRINGER 22 LEFT HAS A CRACKED CLIP AT XRS111. REMOVED OLD CLIP FABRICATED AND INSTALLED REPLACEMEN T CLIP. 2 L 7 2 4F A6WE 1998041701154 19980417 01154 WP 1998 4 17 MWEA98402 1 19980413 A 5720 3919256 SPLICE DOUG DC9 DC932 3022066 WP CENTER WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER WING TANK STRINGER SPLICE NUMBER 13 HAS PREVIOUS BLEND OUT REPAIR THAT IS BEYOND LIMITS. FABRICATED AND INSTALLE D REPLACEMENT SPLICE. 2 L 7 2 4F A6WE 1998041701155 19980417 01155 WP 1998 4 17 MWEA98403 1 19980413 A 5720 3919256 SPLICE DOUG DC9 DC932 3022066 WP CENTER WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 STRINGER 13 SPLICE IN CENTER WING TANK HAS CORROSION. REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998041701156 19980417 01156 WP 1998 4 17 MWEA98404 1 19980413 A 5720 3919256 SPLICE DOUG DC9 DC932 3022066 WP CENTER WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER WING TANK STRINGER SPLICE ON STRINGER 15 WAS FOUND CORRODED. REMOVED OLD PART FABRICATED AND INSTALLED REPLACEME NT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998041701157 19980417 01157 WP 1998 4 17 MWEA98405 1 19980413 A 5720 3919256 SPLICE DOUG DC9 DC932 3022066 WP CENTER WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER WING TANK STRINGER 14 SPLICE WAS FOUND CORRODED. REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART USIN G APPROVED DATA. 2 L 7 2 4F A6WE 1998041701158 19980417 01158 WP 1998 4 17 MWEA98406 1 19980413 A 5320 SPLICE DOUG DC9 DC932 3022066 WP CENTER WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER WING TANK STRINGER 11 SPLICE HAS SEVERAL LOCATIONS OF DAMAGE. FABRICATED REPLACEMENT REPAIR SPLICE USING APPROVE D DATA. 2 L 7 2 4F A6WE 1998041701159 19980417 01159 WP 1998 4 17 MWEA98428 1 19980414 A 5720 3919256 SPLICE DOUG DC9 DC932 3022066 WP CENTER WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER WING TANK SPLICE FOR STRINGER NR 14 HAS TOOLING MARKS. MTC REMOVED DAMAGED PART FABRICATED AND INSTALLED REPLACE MENT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998041701160 19980417 01160 WP 1998 4 17 MWEA98429 1 19980414 A 5720 3919256 SPLICE DOUG DC9 DC932 3022066 WP CENTER WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CENTER WING TANK SPLICE ON STRINGER NR 15 HAS TOOLING DAMAGE. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART. 2 L 7 2 4F A6WE 1998041701161 19980417 01161 WP 1998 4 17 MWEA98430 1 19980414 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 980 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 16 RIGHT WAS FOUND CRACKED AT FS 980. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPAIR SECTION OF LONGERON . 2 L 7 2 4F A6WE 1998041701162 19980417 01162 WP 1998 4 17 MWEA98431 1 19980414 A 5315 9911544 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE FLOORBEAM AT FUSELAGE STATION 237 RIGHT BOTTLINE 41 WAS FOUND CORRODED. MTC REMOVED CORROSION AND REPAIRED FLOORBEA M. 2 L 7 2 4F A6WE 1998041701163 19980417 01163 WP 1998 4 17 MWEA98432 1 19980414 A 5330 5911427 SKIN DOUG DC9 DC932 3022066 WP BS 978 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FUSELAGE SKIN IS DENTED AND GOUGED AT FS 978. ALSO, A CRACK WAS FOUND IN SKIN. REPAIRED FUSELAGE SKIN USING APPROVED D ATA. 2 L 7 2 4F A6WE 1998041701164 19980417 01164 WP 1998 4 17 MWEA98433 1 19980414 A 5711 5919153 SPAR DOUG DC9 DC932 3022066 WP RT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE RIGHT WING FORWARD LOWER SPAR CAP HAS AN UNDOCUMENTED REPAIR. MTC REPAIRED SPAR CAP USING APPROVED DATA. 2 L 7 2 4F A6WE 1998041701165 19980417 01165 WP 1998 4 17 MWEA98434 1 19980414 A 5311 9911842 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE CANTED FRAME AT FUSELAGE STATION 1143 HAD AN IMPROPER REPAIR. REPAIRED FRAME USING APPROVED DATA. 2 L 7 2 4F A6WE 1998041701166 19980417 01166 WP 1998 4 17 MWEA98435 1 19980414 A 2810 5912369 FUEL PANEL DOUG DC9 DC932 3022066 WP RT WING CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING LOWER FUEL PANEL NR 1456 HAS CORROSION AROUND AND INSIDE COUNTERSUNK HOLES AND ON BOTTOM SIDE. MTC REMOVED A ND REPLACED FUEL PANEL WITH SERVICEABLE UNIT. 2 L 7 2 4F A6WE 1998041701167 19980417 01167 NE 1998 4 17 DLL10980740 2 19980405 A 7260 RB21122B02 GEARBOX LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 720DA 38963 010656 193C1136 010656 BEGINNING DESCENT, -A- SYSTEM PRESSURE 0, QUANTITY REMAINED. IDG LOW OIL PRESSURE LIGHT ON, GEN DISCONNECTED. DISCONNE CTED IDG. ON APPROACH NR 1 OIL QTY DROPPED, QTY BELOW 10. NR 1 ENG SHUTDOWN. AT GATE NR 1 ENG OIL QTY 0. REPLACED NR 1 ENG MAIN GEARBOX ON ROUTINE CHECK. PERFORMED TESTS 1-3-9-16 PER PFHB, ALL TEST OK. 2 L 7 3 4F 4 F A23WE E12EU 1998041701168 19980417 01168 WP 1998 4 17 DLL14980745 1 19980406 A 5210 1282T10019 COUNTERBALACE LKHEED 1011 1011385115 5265015 WP PAX DOOR FAILED TEST A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 527001348 193C1237 L3 DOOR FAILED EMERGENCY TIMED TEST WITH INSIDE HANDLE REF R/C 923 OPN 68116. REPLACING DOOR COUNTERBALNCE ASSY CO (P/N 527001348). 2 L 7 3 4F A23WE 1998041701169 19980417 01169 NE 1998 4 17 DLM88980762 2 19980407 A 7261 LUBRICATION DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE OVERSERVICED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 967DL 16549 53116 725995 ON CLIMBOUT, NR 2 ENG OIL TEMP REACHED 165 DEG AND PRESS WAS 55 PSI. TEMP FLUX FROM 155 TO 165 DEG UNTIL DESCENT PWR RE TARDED. GRADUAL DECREASE TO NML ON TAXI IN. OIL TANK OVER SERVICED. DRAINED TANK TO PROPER LEVEL, RAN ENG PRESS AND T EMP NORMAL. 2 L 7 2 4F 4 F RT A6WE E9NE 1998041701170 19980417 01170 NM 1998 4 17 DL72W980764 1 19980407 A 2782 BRACKET BOEING 727 727247 138408F NM NR 1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON E1 LETTER CK, .25 INCH VISIBLE CRACK INBD MOUNT BRACKET NR 1 L/E FLAP ACTUATOR. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998041701171 19980417 01171 NM 1998 4 17 DL72E980765 1 19980407 A 7931 OIL PRESS VALVE BOEING 727 727247 138408F NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 282WA 21484 700710 ON CLIMBOUT, NR 3 ENG OIL PRESS INDICATED IN THE RED, AT IDLE OIL PRESS IN THE GREEN. ANY ATTEMPT TO GO OVER 55 PERCENT . PRESSURE WOULD CLIMB TOWARDS THE RED. REPLACED OIL PRESSURE RELIEF VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998041701172 19980417 01172 NM 1998 4 17 DL72W980766 1 19980407 A 5320 ANGLE BOEING 727 727247 138408F NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON E1 LETTER CK, LT KEEL BEAM ANGLE CRACKED I/B OF APU MOUNT STA 870. REPLACED ANGLE PER SRM 53-10-9. 2 L 7 3 4F A3WE 1998041701173 19980417 01173 NM 1998 4 17 DL72W980767 1 19980407 A 5754 RIB BOEING 727 727247 138408F NM NR 7 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON E1 LETTER CK, 1 INCH CRACK AT NR 7 SLAT ACTUATOR ATTACH RIB I/B SIDE. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998041701174 19980417 01174 NM 1998 4 17 DL72W980768 1 19980407 A 2782 BRACKET BOEING 727 727247 138408F NM NR 8 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2810W 20648 FOUND ON E1 LETTER CK, NR 8 SLAT ACTUATOR I/B MOUNT BRACKET IS CRACKED. REPAIR PER MM 57-20-21. 2 L 7 3 4F A3WE 1998041701175 19980417 01175 WP 1998 4 17 DLL10980769 1 19980407 A 3350 305 BULB LKHEED 1011 10113851 5265010 WP R3 DOOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 727DA 193C1167 R3 SLIDE LGT INOP. RELAMPED, CK'S GOOD. 2 L 7 3 4F A23WE 1998041701176 19980417 01176 WP 1998 4 17 DLL19980770 1 19980407 A 3350 BULB 305 LKHEED 1011 10113853 5265020 WP EXTERIOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 193H1202 2L EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED, OPS OK. 2 L 7 3 4F A23WE 1998041701178 19980417 01178 NM 1998 4 17 DL72S980775 1 19980327 A 5753 652163262 DOUBLER BOEING 727 727232 1384082 NM NR 3 MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 AFT SPAR CHORD DOULBER CRACKED TWO PLACES 34 FROM I/B END OF NR 3 MIDFLAP. REPLACED DOULBER PER BOEING M/M 57-52-0 FIG 802. . 2 L 7 3 4F A3WE 1998041701179 19980417 01179 NM 1998 4 17 DL72S980773 1 19980408 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 405DA 21149 AFT AIRSTAIR EMER LIGHT INOP. REPL BATT, OPS CK OK. 2 L 7 3 4F A3WE 1998041701180 19980417 01180 NM 1998 4 17 DLM88980774 1 19980408 A 3350 LIGHTS DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DE 49997 LT AND RT EMERGENCY WING EXTERIOR LIGHTS INOP. 2 L 7 2 4F RT A6WE 1998041701181 19980417 01181 WP 1998 4 17 DLL13980776 1 19980408 A 2150 PACK LKHEED 1011 10113851 5265010 WP NR 2 SMOKING A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 790DL 193A1143 FLIGHT ATTENDANT NOTIFIED CREW OF LIGHT SMOKE IN CABIN. CHECKLIST FOLLOWED AND ISOLATED NR 2 A/C PACK. SMOKE CLEARED. DRAINED AND REFILLED ACM. REPLACED WATER SEPARATOR BAG, INSPECTED ENGINE AND ALL CHECKS NORMAL. 2 L 7 3 4F A23WE 1998041701182 19980417 01182 NM 1998 4 17 DL72S980778 1 19980409 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 FOUND ON B2 LETTER CHECK, .125 INCH CRACK IN LIGHTENING HOLE LT SIDE STA 1223. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998041701183 19980417 01183 NM 1998 4 17 DL72L980780 1 19980409 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM BS 950 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 509DA 21311 AFT LT OVERWING EMER SLIDE LIGHT INOP. REPLACED BATT, OPS OK. 2 L 7 3 4F A3WE 1998041701184 19980417 01184 NM 1998 4 17 DL76S980782 1 19980410 A 5754 114T410131A WEDGE BOEING 767 767332 1382001 NM NR 1 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 125DL 24075 DELAMINATION WAS FOUND ON THE NR 1 L/E SLAT TRAILING EDGE WEDGE NEAR THE INB'D END. DELAM WAS APPROX 3 BY 6. REPAIRED PER ERA 364501-14AD. 2 L 7 2 4F RT A1NM 1998041701185 19980417 01185 WP 1998 4 17 DLL14980783 1 19980408 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 912 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 THE FUSELAGE SKIN AT FS 912 BETWEEN STRINGERS 32 AND 33 WAS FOUND WITH A 2 INCH LONG CRACK DUE TO CORROSION. AN EXISTIN G SKIN DOUBLER REPAIR WAS ADJACENT TO THE DAMAGE. THE CRACK WAS CUTOUT AND AN EXTERNAL DOUBLER WAS INSTALLED TO REPAIR THE CUTOUT AND TO TIE-IN TO THE EXISTING REPAIR. THE REPAIR WAS ACCOMPLISHED PER ER/A 364475-14, REV A AND IS TIME- LI MITED. 2 L 7 3 4F A23WE 1998041701186 19980417 01186 NM 1998 4 17 DL73K980784 1 19980408 A 5312 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 THE FS 178 BULKHEAD WEB WAS FOUND WITH SEVERAL CRACKS IN THE AREA OF RBL 5.7 AND LBL 5.7 BETWEEN WL 190 AND 210. THE WE B STRAP AT RBL 5.7 WAS ALSO CRACKED. THE CRACKS WERE CUT OUT AND A SINGLE WEB DOUBLER INSTALLED TO ENCOMPASS ALL OF THE CUT OUTS. THE STRAP WAS REPAIRED WITH AN ALUMINUM STRAP DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 331603-14, REV A. 2 L 7 2 4F RT A16WE 1998041701187 19980417 01187 NM 1998 4 17 DL72S980785 1 19980407 A 5315 652083724 FLOORBEAM BOEING 727 727225 1384077 NM BS 1110 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 THE UPPER CAP OF THE FS 1110 PASSENGER FLOORBEAM WAS FOUND CORRODED. A SECTION OF THE CAP WAS CUT OUT BETWEEN RBL 12 AN D LBL 12. THE CAP WAS REPAIRED WITH A FILLER SECTION AND FOUR SPLICE ANGLES PER ER/A 364205-14, REV A. 2 L 7 3 4F A3WE 1998041701188 19980417 01188 NM 1998 4 17 DL73K980786 1 19980408 A 5330 654577319 SKIN BOEING 737 737232 1384475 NM BS 727-777 LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 THE WINDOW BELT SKIN BETWEEN FS 727 AND 777 WAS FOUND WITH SIX LIGHTNING STRIKE DAMAGE LOCATIONS. TWO OF THE LOCATIONS WERE REPAIRED BY DRILLING OUT AND INSTALLING .25 INCH DIA RIVETS PER THE B737 SRM. THE REMAINING LOCATIONS WERE BLENDE D OR CUT OUT AND REPAIRED WITH CONTINUOUS DOUBLER AND TRIPLER PER ER/A 331583-14, REV A. 2 L 7 2 4F RT A16WE 1998041701189 19980417 01189 NM 1998 4 17 DL76G980787 1 19980407 A 5330 143T32114 SKIN BOEING 767 7673P6 1385105 NM BS 620 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1501P 24983 THE FUSELAGE SKIN AND STRINGERS BETWEEN FS 610 TO 63 AND STRINGERS 35L TO 37L WERE BADLY DENT AND TORN BY A GROUND EQUIP MENT IMPACT. THE DAMAGED SKIN AND STRINGERS WERE CUT OUT. THE STRINGERS WERE REPAIRED PER THE B767 SRM. THE SKIN WAS REPAIRED WITH AN EXTERNAL SKIN DOUBLER PER ER/A 364451-14, REV B. 2 L 7 2 4F RT A1NM 1998041701190 19980417 01190 WP 1998 4 17 DLL13980792 1 19980412 A 3350 5165741 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 784DA AC982 193A1038 L1 DOOR EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998041701191 19980417 01191 NM 1998 4 17 DL76L980793 1 19980411 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 180DN 25985 EMERG LIGHTS INOP ROW 24 THRU 28FG. REPLACED POWER SUPPLY, OPS CHECK NORMAL. 2 L 7 2 4F RT A1NM 1998041701192 19980417 01192 NM 1998 4 17 DL72L980794 1 19980412 A 3350 BATTERY 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 502DA 3674 21304 FOUND L-2 UPPER EMERG LIGHT INOP. REPLACED BATTERY. FOUND L-2 LOWER EMERG LIGHT INOP. REPAIRED GND WIRE. 2 L 7 3 4F A3WE 1998041701193 19980417 01193 NM 1998 4 17 DL72S980795 1 19980412 A 3350 1000677 RACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 468DA 20745 EMERGENCY LIGHT OVER AFT LEFT DOOR INOP. REPLACED RACK, OPN GOOD. 2 L 7 3 4F A3WE 1998041701194 19980417 01194 NM 1998 4 17 DL72S980796 1 19980401 A 5330 SKIN BOEING 727 727232 1384082 NM R-1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 DURING INSPECTION OF FWD SVC DOOR UPPER HINGE CUTOUT REF SI 4-72762-12 ME 02, .25 INCH VISIBLE CRACK FOUND IN BEAR STRAP . REPAIRED PER ER/A 364433-14 CODE 4-53-31-20. 2 L 7 3 4F A3WE 1998041701195 19980417 01195 NM 1998 4 17 DL72S980797 1 19980410 A 5320 69678811 ANGLE BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 THE GUSSET ANGLE AT FS 1273 ON THE RT VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A TYPICAL CRACK. THE GUSSET ANGLE WAS REPLACED WITH A NEW PART PER BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 364503-14AD. 2 L 7 3 4F A3WE 1998041701196 19980417 01196 NM 1998 4 17 DL72S980798 1 19980410 A 5330 651753058 SKIN BOEING 727 727225 1384077 NM BS 1207 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 AN EXISTING REPAIR WAS REMOVED FROM THE LOWER SKIN PANEL NEAR THE STRINGER 20R LAP SPLICE. THE UNDERLYING SKIN CUTOUT W AS 3.5 X 4. THE SKIN CUTOUT AND SURROUNDING AREA WAS DYE PENETRANT INSPECTED TO ENSURE NO CRACKS AND AN EXTERNAL ALUMIN UM DOUBLER INSTALLED PER ER/A 364319-14, REV B. 2 L 7 3 4F A3WE 1998041701197 19980417 01197 NM 1998 4 17 DL767980799 1 19980411 A 5310 141T3001 STRUCTURE BOEING 767 767232 1385132 NM BS 430 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 106DA 22218 FUSELAGE STRINGERS 36L TO 33R WERE FOUND CORRODED BETWEEN FS 412 AND 456. NEW SECTIONS OF STRINGER WERE SPLICED IN PER SRM OR LONGER BLUEPRINT STRINGER SPLICES WERE INSTALLED. A SMALL SECTION OF SKIN WAS CORRODED AND CUTOUT. THE SKIN WAS REPAIRED PER THE B767 SRM. THE OVERALL REPAIR WAS DOCUMENTED AND INSTALLED PER ER/A 364467-14, REV A. LIAISON ENG R'G DETERMINED THAT SPILL IN B/B WAS CAUSE AND THEREFORE AN ISOLATED INCIDENT. 2 L 7 2 4F RT A1NM 1998041701198 19980417 01198 NM 1998 4 17 DLM88980800 1 19980413 A 3241 4062575 TRANSDUCER DOUG MD88 MD88 3023688 NM NR 1 MLG SHEARED A DALA O OTHER O OTHER LD LANDING 1 SO 27 986DL 53313 A/C OVERRAN RUNWAY. FOUND NR 1 MAIN ANTI-SKID TRANSDUCER PIN SHEARED. REPLACED TRANSDUCER. 2 L 7 2 4F RT A6WE 1998041701199 19980417 01199 NM 1998 4 17 DLM88980804 1 19980413 A 3350 BATTERY 339001283 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 913DE 661 49956 ON L/O, FOUND AFT EXTERIOR EMERGENCY LIGHT INOP. REPLACED EMERGENCY LIGHTS BATTERY, OKS CKS GOOD. 2 L 7 2 4F RT A6WE 1998041701200 19980417 01200 NM 1998 4 17 DL72S980808 1 19980403 A 5320 534201871 ANGLE BOEING 727 727232 1384082 NM BS 740 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 DURING MV1 CHECK TASK C53-113-01, CORROSION FOUND ON SKIN SUPPORT ANGLE AT STA 740 STR 27R. REPLACED SUPPORT ANGLE PER M/M 53-11-0 PG 858. 2 L 7 3 4F A3WE 1998041701201 19980417 01201 NM 1998 4 17 DL72S980809 1 19980327 A 5312 BLKHD ANGLE BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 DURING MV1 CHECK, FOUND KEEL BEAM SUPPORT ANGLE CRACKED 3.5 INCHES, FWD SIDE OF STA 870 BULKHEAD, RT SIDE OF KEEL BEAM. REPLACED ANGLE PER SRM 53-10-9 FIG 13. 2 L 7 3 4F A3WE 1998041701202 19980417 01202 NM 1998 4 17 SCNA98033 1 19980408 A 7830 TR LIGHT BOEING 727 727227 1384078 NM NR 3 ENGINE ILLUMINATED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 275AF 22092 ON TAKEOFF ROLL, NUMBER THREE REVERSER LIGHT ILLUMINATED. ABORTED TAKEOFF. MEGGED WIRES BACK TO THRUST REVERSER SWITCH AND FUNCTIONALLY TESTED GOOD. SYSTEM OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F A3WE 1998042400001 19980424 00001 EU 1998 4 24 MALA976089 1 19980410 A 2611 SMOKE WARNING SAAB SF340 340B 7860101 EU E/E COMPT ACTIVATED A MALA O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 15 595MA 340B216 AVIONICS SMOKE MASTER WARNING ILLUMINATED FOR 3 TO 5 SECONDS THEN WENT OFF. MAINTENANCE INSPECTED AVIONICS BAY AREA FOR SIGNS OF SMOKE OR BURNING, NONE FOUND. INSPECTED CANNON PLUGS ON DETECTOR ALL CHECKS GOOD. RERACKED WEU FOR TROUBLESH OOTING PURPOSES. ALL OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400002 19980424 00002 EU 1998 4 24 MALA976090 1 19980410 A 3350 4970114010 CRADLE SAAB SF340 SF340A 7850100 EU FLIGHT DECK FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 27XJ 027 CABIN EMERGENCY LIGHT AND FLIGHT DECK EMERGENCY BUTTON WHEN PRESSED ONLY GET ONE CHIME. MAINTENANCE REPLACED FLIGHT DEC K CRADLE, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400003 19980424 00003 1998 4 24 MALA976091 4 19980409 A 3425 RELAY SAAB SF340 SF340A 7850100 EU E/E COMPT FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 41XJ 041 AFTER TAKEOFF, CAPAIN'S HSI AND ADI GOES DARK WHEN HYD PUMP CYCLES IN FLIGHT. MAINTENANCE REPLACED 69PC RELAY, OPS CHEC KS GOOD. 2 L 7 2 4T RT A52EU 1998042400004 19980424 00004 EU 1998 4 24 MALA976092 1 19980409 A 2613 OVERTEMP SENSOR SAAB SF340 340B 7860101 EU RT TAILPIPE DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 407XJ 340B407 AFTER TAKEOFF, RIGHT TAILPIPE HOT LIGHT CAME ON. MAINTENANCE CLEANED AND RESEALED TAILPIPE SENSORS, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400005 19980424 00005 EU 1998 4 24 MALA976093 1 19980409 A 2613 OVERTEMP SENSOR SAAB SF340 340B 7860101 EU RT TAILPIPE DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 418XJ 418 AFTER TAKEOFF, RIGHT TAILPIPE HOT LIGHT CAME ON. MAINTENANCE CLEANED AND RESEALED TAILPIPE SENSORS, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400006 19980424 00006 EU 1998 4 24 MALA976094 1 19980409 A 7722 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 991XJ 091 AFTER TAKEOFF, RIGHT ITT TEMP WAS 100 DEGRESS HOTTER THAN THE LEFT(605-711). MAINTENANCE VERIFIED PROBLEM THROUGH ITT C ALIBRATION, CLEANED AND RESECURED CANNON PLUG ON T4.5 TRIMMER, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400007 19980424 00007 NM 1998 4 24 K3HA980052 1 19980414 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 LEFT OVERWING LOWER EMERGENCY LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK PER MM 33-50-00 . 2 L 7 3 4F A3WE 1998042400008 19980424 00008 NM 1998 4 24 K3HA980053 1 19980414 A 3350 387 BULB BOEING 727 727225 1384077 NM R1 DOOR FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 R1 DOOR HAS SOME LIGHTS OUT ON THE LOWER EXIT LIGHT. REBULBED TWO LIGHTS CHECK OK PER MM 33-50-01. 2 L 7 3 4F A3WE 1998042400009 19980424 00009 NM 1998 4 24 K3HA980054 1 19980414 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY LIGHT IN AFT STAIRWAY DID NOT ILLUMINATE. REMOVED AND REPLACED NICAD BATTERIES (P/N S-106, S/N MAR-1), OPS CH ECK OK PER MM 33-50-0. 2 L 7 3 4F A3WE 1998042400010 19980424 00010 SO 1998 4 24 RAAA98E9011 1 19980415 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD RT AND AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISC HARGED. 2 L 7 4 4T 4A22 1998042400011 19980424 00011 NM 1998 4 24 SWA980554 1 19980409 A 5730 SKIN BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 329SW 23693 DURING SCHEDULED C2 CHECK, FOUND NR 1 SLAT I/B AUX TRACK CUTOUT CRACKED IN 2 PLACES AT AFT EDGE. REPAIRED PER SWA RA NR 1-357-0545. 2 L 7 2 4F RT A16WE 1998042400012 19980424 00012 NM 1998 4 24 SWA980555 1 19980409 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 500D, STR 19 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400013 19980424 00013 NM 1998 4 24 SWA980556 1 19980409 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 271 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AROUND NUT PLATE AT BS 271, RBL 1, WL 208. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400014 19980424 00014 NM 1998 4 24 SWA980557 1 19980409 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 289/302/380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 289, WL 253, ABOVE STR 11 RT, BS 302 WL 256 ABOVE STR 10 L/H AND BS 380 TO 400 LBL 1 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400015 19980424 00015 NM 1998 4 24 SWA980558 1 19980409 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED SERVICE CHECK, FOUND R-2 EXTERIOR EMERGENCY LIGHT AND L-2 INTERIOR EMERGENCY LIGHT INOP. REPLACED BATT ERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042400016 19980424 00016 NM 1998 4 24 SWA980559 1 19980409 A 5320 ANGLE BOEING 737 7373T5 NM BS 301.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 301.9, LBL 54, WL 257.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400017 19980424 00017 NM 1998 4 24 SWA980560 1 19980409 A 5311 FRAME BOEING 737 7373T5 NM BS 301.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE ON FRAME AT BS 294, LBL 50, WL 267. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998042400018 19980424 00018 NM 1998 4 24 SWA980561 1 19980409 A 5320 ANGLE BOEING 737 7373T5 NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 290, RBL 54, WL 240 AND BS 290, RBL 25, WL 254. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400019 19980424 00019 NM 1998 4 24 SWA980562 1 19980409 A 5320 WEB BOEING 737 7373T5 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 277, RBL 56, WL 231. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400020 19980424 00020 NM 1998 4 24 SWA980563 1 19980409 A 5311 FRAME BOEING 737 7373T5 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 500, LBL 63 WL 215. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400021 19980424 00021 NM 1998 4 24 SWA980564 1 19980409 A 5320 WEB BOEING 737 7373T5 NM BS 390/424/454 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 390 RBL 70 WL 208, BS 424 TO 438 RBL 70 WL 208 AND BS 454 RBL 70 WL 2 08. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400022 19980424 00022 NM 1998 4 24 SWA980565 1 19980409 A 5320 WEB BOEING 737 7373T5 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 500+11 AND 18, RBL 70 WL 208, BS 500 A+7 RBL 70 WL 208 AND BS 500 C+1 0 TO 18 RBL 70 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400023 19980424 00023 NM 1998 4 24 SWA980566 1 19980409 A 5320 WEB BOEING 737 7373T5 NM BS 381-389 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 381 TO 389, LBL 70, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400024 19980424 00024 NM 1998 4 24 SWA980567 1 19980409 A 5320 SUPPORT BOEING 737 7373T5 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED CHANNEL SUPPORT AT BS 328, LBL 44.5, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400025 19980424 00025 NM 1998 4 24 SWA980568 1 19980409 A 5315 FLOORBEAM BOEING 737 7373T5 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM L-ANGLE AT BS 328 LBL 45 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400026 19980424 00026 NM 1998 4 24 SWA980569 1 19980409 A 5315 FLOORBEAM BOEING 737 7373T5 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM STIFFENER AT BS 328, RBL 33, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400027 19980424 00027 NM 1998 4 24 SWA980570 1 19980409 A 5320 ANGLE BOEING 737 7373T5 NM BS 519 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 519 RBL 25 WL 206, BS 519 LBL 25 WL 205 AND BS 519 LBL 45 WL 206. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400028 19980424 00028 NM 1998 4 24 SWA980571 1 19980409 A 5320 WEB BOEING 737 7373T5 NM BS 519-500 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR WEB AT BS 519 LBL 25 WL 205, BS 500 D+11 BL 0 WL 208 AND BS 380 TO 400 WL 207 BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400029 19980424 00029 NM 1998 4 24 SWA980572 1 19980409 A 5320 SUPPORT BOEING 737 7373T5 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540 LBL 28 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400030 19980424 00030 NM 1998 4 24 SWA980573 1 19980409 A 5315 FLOORBEAM BOEING 737 7373T5 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, WL 207, LBL 14. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400031 19980424 00031 NM 1998 4 24 SWA980574 1 19980409 A 5320 CHORD BOEING 737 7373T5 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORRODED Z-CHORD AT BS 270, WL 207, RBL 9 TO LBL 9. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998042400032 19980424 00032 NM 1998 4 24 SWA980575 1 19980410 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN APPROX 2.75 AT BS 500 D AND S10R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400033 19980424 00033 NM 1998 4 24 SWA980576 1 19980410 A 3350 6127421 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND EVACUATION EMERGENCY LIGHT INOP AT THE AFT SERVICE AREA. REMOVED AND REPLACED PAC K ASSY FOR THE AFT SLIDE DOOR EMERGENCY LIGHTS, CKS GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998042400034 19980424 00034 NM 1998 4 24 SWA980577 1 19980410 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400/867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN STR 8 LT AND 9 LT AT BS 867 AND BS 400, S TR 8 RT AND 9 RT. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042400035 19980424 00035 NM 1998 4 24 SWA980578 1 19980410 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT DOOR STOP NR 9, BS 348 LBL 65 WL 223. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998042400036 19980424 00036 NM 1998 4 24 SWA980579 1 19980410 A 5330 SKIN BOEING 737 7373T5 NM BS 316/996/1007 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 316, 2 BELOW STR 2 LT AND BS 996 AND 1007, 4 ABOVE STR 14 LT. REPAIRE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400037 19980424 00037 NM 1998 4 24 SWA980580 1 19980410 A 5311 FRAME BOEING 737 7373T5 NM BS 847/400/360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET AT BS 847 STR 9 RT, BS 400 STR 9 LT AND BS 360 STR 9 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400038 19980424 00038 NM 1998 4 24 SWA980581 1 19980410 A 5311 FRAME BOEING 737 7373T5 NM BS 887/827/887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET AT BS 887, STR 9 LT BS 827 STR 9 LT AND BS 887 STR 9 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400039 19980424 00039 NM 1998 4 24 SWA980582 1 19980410 A 5320 WEB BOEING 737 7373T5 NM BS 519 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR WEB AT BS 519, RBL 25, WL 206. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400040 19980424 00040 NM 1998 4 24 SWA980583 1 19980410 A 5320 ANGLE BOEING 737 7373T5 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 294, WL 208.5, RBL 55. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400041 19980424 00041 NM 1998 4 24 SWA980584 1 19980410 A 5320 STIFFENER BOEING 737 7373T5 NM BS 520 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED MECHANICAL DAMAGE IN STIFFENER ANGLE AT BS 520, RBL 25, WL 200. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998042400042 19980424 00042 NM 1998 4 24 SWA980585 1 19980410 A 5320 WEB BOEING 737 7373T5 NM BS 1032-1034 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 1034, LBL 2 WL 209, BS 1033 LBL 9.5 WL 209 AND BS 1032 LBL 18 WL 209. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400043 19980424 00043 NM 1998 4 24 SWA980586 1 19980410 A 5320 WEB BOEING 737 7373T5 NM BS 1032 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 1032 RBL 16 WL 209. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400044 19980424 00044 NM 1998 4 24 SWA980587 1 19980410 A 5320 SUPPORT BOEING 737 7373T5 NM BS 964-978 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORRODED THRESHOLD Z-SUPPORT ANGLES AFT SERVICE DOOR AT BS 964 TO 978 RBL 55 WL 209. RE MOVED AND REPLACED PER BOEING SRM, DAMAGE OUT OF LIMITS. 2 L 7 2 4F RT A16WE 1998042400045 19980424 00045 NM 1998 4 24 SWA980588 1 19980410 A 5320 INTERCOSTAL BOEING 737 7373T5 NM BS 747-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 747 TO 767 RBL 20, WL 155. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998042400046 19980424 00046 NM 1998 4 24 SWA980589 1 19980411 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 886/930 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED A2 CHECK, FOUND CRACKED SKIN AT BS 930, STR 23R, BS 930 STR 21R AND BS 860 STR 23R. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400047 19980424 00047 NM 1998 4 24 SWA980590 1 19980411 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 930/880 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED A2 CHECK, FOUND CRACKED SKIN AT BS 930, STR 25R, BS 880 STR 24R AND BS 880 STR 25R. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400048 19980424 00048 NM 1998 4 24 SWA980591 1 19980412 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998042400049 19980424 00049 NM 1998 4 24 SWA980592 1 19980412 A 3350 900835A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND CENTER EMERGENCY EXIT LIGHT BATTERY AND BASE CHECK BAD. REMOVED AND REPLACED BASE SYSTEM AND BATTERY PER BOEING MM. 2 L 7 2 4F A16WE 1998042400050 19980424 00050 NM 1998 4 24 SWA980593 1 19980412 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED STRINGER 3L AT BS 380 UNDER STRINGER TIE CLIP. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042400051 19980424 00051 NM 1998 4 24 SWA980594 1 19980412 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1010 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED STRINGER 4L AT BS 1010. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042400052 19980424 00052 NM 1998 4 24 SWA980595 1 19980412 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 360-540 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SERVICE VISIT, REPAIRED SKIN LAP AT BS 360 TO 540, STR 14L, BS 360 TO 540 STR 10L, BS 360 TO 540 STR 4L, BS 360 T O 540 STR 4R AND BS 360 TO 540 STR 10R. REPAIRED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998042400053 19980424 00053 NM 1998 4 24 SWA980596 1 19980412 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 360-540 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SERVICE VISIT, REPAIRED SKIN LAP AT BS 360 TO 540 STR 14R, BS 540 TO 727 STR 4L, BS 540 TO 727 STR 4R, BS 727 TO 908 STR 10L AND BS 727 TO 908 STR 4L. REPAIRED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998042400054 19980424 00054 NM 1998 4 24 SWA980597 1 19980412 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727-908 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 57SW 21722 DURING SERVICE VISIT, REPAIRED SKIN LAP AT BS 727 TO 908 STR 4R AND BS 727 TO 908, STR 10R. REPAIRED PER SWA ACO 6717-5 3. 2 L 7 2 4F A16WE 1998042400055 19980424 00055 NM 1998 4 24 UPS98226430 1 19980410 A 2761 ANGLE BOEING 727 72722C 138400F NM NR SPOILER ACT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, NR 2 SPOILER ACTUATOR SUPPORT CASTING, ATTACH ANGLE ON REAR SPAR I/B CRACKED. ATTACH ANGLE REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998042400056 19980424 00056 NM 1998 4 24 UPS98226431 1 19980410 A 5330 SKIN BOEING 727 72722C 138400F NM BS 251.6 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK FOUND ON FUSELAGE SKIN BS 251.6, WL 221.5. SKIN REPAIRED IAW SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1998042400057 19980424 00057 NM 1998 4 24 UPS98226432 1 19980407 A 5400 WEB BOEING 727 72722C 138400F NM BS 1380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, SUSPECT CRACK ON WEB ABOVE NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1380. NEW WEB FABRICATED AN D INSTALLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1998042400058 19980424 00058 NM 1998 4 24 UPS98226433 1 19980415 A 2710 HINGE BOEING 727 72722C 138400F NM RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, RT OUTBD AILERON HINGE IS CRACKED, SECOND FROM INBD HINGE FITTING. REPLACED IAW 65-19275. 2 L 7 3 4F A3WE 1998042400059 19980424 00059 NM 1998 4 24 UPS98226434 1 19980410 A 5330 SKIN BOEING 727 72722C 138400F NM BS 530 SCRATCHED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, FOUND SCRATCH 3 INCHES LONG NEAR OF FWD CARGO COMPARTMENT, RT SIDE STN 530 WL 188 SECTION 43. REMOVE D SCRATCH AND REPAIRED IAW SRM 53-30-3, FIG 3. 2 L 7 3 4F A3WE 1998042400060 19980424 00060 NM 1998 4 24 UPS98226435 1 19980415 A 3211 QF71210053 FITTING BOEING 727 72722C 138400F NM NR 3 TRUNNION DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, NR 3 TRUNNION FITTING FOUND TO HAVE A SURFACE IRREGULARITY DURING NDT PROCESS (FLUORESCENT DYE PENETR ANT). NR 3 TRUNNION FITTING REPLACED IAW MM 71-21-01. 2 L 7 3 4F A3WE 1998042400061 19980424 00061 WP 1998 4 24 UPS98826436 1 19980327 A 5320 9759429 SUPPORT DOUG DC8 DC873F 302199F WP BS 1445-1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, CARGO PIT RT AFT FLOOR SUPPORT ANGLE HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEM ENT SUPPORT IAW SRM 51-1-21 AND DWG 9759429. 2 L 7 4 4F RT 4A25 1998042400062 19980424 00062 WP 1998 4 24 UPS98826437 1 19980327 A 5320 9759429 SUPPORT DOUG DC8 DC873F 302199F WP BS 1420-1480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, CARGO PIT LT FLOOR SUPPORT ANGLE HAS MODERATE CORROSION FS 1420 TO 1480. REMOVED, FABRICATED AND INS TALLED REPLACEMENT SUPPORT IAW SRM 51-1-21 AND DWG 9759429. 2 L 7 4 4F RT 4A25 1998042400063 19980424 00063 WP 1998 4 24 UPS98826438 1 19980328 A 5320 9759429 SUPPORT DOUG DC8 DC873F 302199F WP BS 440-460 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-C, FLOORBOARD SUPPORT BETWEEN FS 440 TO 460 STR 33L CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACE MENT SUPPORT IAW SRM 51-1-21 AND DWG 9759429. 2 L 7 4 4F RT 4A25 1998042400064 19980424 00064 NM 1998 4 24 QXEA9800523 1 19980412 A 7712 3039232 TSCU DHAV DHC8 DHC8102 2809003 NM ENGINE MALFUNCTION A QXEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 09 813PH 14100 4100 32 AUTOFEATHER SYSTEM DOES NOT ARM. ABORTED TAKEOFF AND RETURNED TO THE GATE. SYSTEM ARMED AND TESTED NORMALLY ON THE GRO UND DURING TEST MODE. REPLACED POWER LEVER SWITCHES 6121-S12 AND 6121-S13. ALSO, REPLACED NR 1 AND NR 2 TORQUE SIGNAL CONDITIONERS (TSEU). OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042400065 19980424 00065 EU 1998 4 24 98FDEA00267 1 19980414 A 5210 DOOR AIRBUS 300 A300F4605R 3930327 EU PAX COMPT NOT SEALED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 657FE 748 PASSING FL 330 IN THE CLIMB MAIN DECK DOOR LIGHT ILLUMINATED. CABIN BEGAN TO DEPRESSURIZE. PASSING FL 190 IN THE DESCE NT DOOR INDICATED NORMAL. ALL CABIN DOORS, OPENED AND INSPECTED MAIN CARGO DOOR SEALS, FOUND OK. CLOSED INDICATOR LIGH TS OK. NO DAMAGE FOUND. PRESSURIZED A/C TO .2 DIFFERENTIAL. NO DOOR WARNING INDICATION. 2 L 7 2 4F RT A35EU 1998042400066 19980424 00066 NM 1998 4 24 98FDEA00268 1 19980415 A 5320 55184175 CHORD BOEING 727 727225 1384077 NM BS 309.24 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 465FE 21289 H-CHORD CORRODED AT END LBL 11, BS 309.24, WL 178. *S/D* REMOVED AND REPLACED H-CHORD AT LBL 11, BS 309.24, WL 178. 2 L 7 3 4F A3WE 1998042400067 19980424 00067 NM 1998 4 24 98FDEA00269 1 19980415 A 5313 652353529 STRINGER BOEING 727 72721C 138400M NM BS 470 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 WHILE WORKING NR 0842 FOUND CORROSION ON STRINGER 2 RT, BS 470. *S/D* REMOVED DAMAGED SECTION OF STRINGER AND REPLACED WITH NEW SECTION OF STRINGER AT BS 430 TO 470, STR 2 RT PER FED-EX SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1998042400068 19980424 00068 NM 1998 4 24 98FDEA00270 1 19980415 A 5320 652353530 STRINGER BOEING 727 72721C 138400M NM BS 470-450 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 WHILE WORKING NR 0842 FOUND CORROSION ON STRINGER 3 RT ON FLANGE BS 470 TO 450. *S/D* REMOVED DAMAGED SECTION OF STRIN GER AND REPLACED WITH NEW SECTION OF STRINGER AT BS 430 TO 470, STR 3 RT PER FED-EX SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1998042400069 19980424 00069 NM 1998 4 24 98FDEA00271 1 19980415 A 5313 652353520 STRINGER BOEING 727 72721C 138400M NM BS 520-740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 WHILE WORKING NR 0842, FOUND CORROSION ON STRINGER 1, BS 520 TO 740. *S/D* REMOVED CORROSION ON STRINGER, EVALUATED DA MAGE. REMOVED 2 DAMAGED SECTIONS AND INSTALLED 2 NEW SECTIONS OF STRINGER AT STR 1, BS 440 TO 570 AND BS 650 TO 740 IAW FED-EX SRM 53-10-3 FIG 3. 2 L 7 3 4F A3WE 1998042400070 19980424 00070 WP 1998 4 24 98FDEA00272 1 19980415 A 5411 RIB DOUG DC10 DC1010F 3022111 WP NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 049FE 47803 NR 2 ENG INLET INTERNAL 7TH RIB AFT OF FWD WEB CRACKED, UPPER CAP APPROX 7 LONG, 5:00 POSITION. * S/D* REPAIRED RIB CA P WITH ANGLE DOUBLER IN REF TO SRM 54-10-00. INSTALLED REPAIRED RIB CAP REF SRM 54-10-00. 4-16-98. 2 L 7 3 4F A22WE 1998042400071 19980424 00071 WP 1998 4 24 98FDEA00273 1 19980415 A 5400 WEB DOUG DC10 DC1010F 3022111 WP NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 049FE 47803 NR 2 ENG INLET INTERNAL WEB BETWEEN 7TH AND 9TH RIB AFT OF FWD WEB CRACKED, 7:00 POSITION. *S/D* REMOVED RIB AND FABRI CATED NEW RIB REF SRM 51-00-01. INSTALLED NEW RIB REF SRM 54-10-00. 4-16-98. 2 L 7 3 4F A22WE 1998042400072 19980424 00072 WP 1998 4 24 98FDEA00274 1 19980415 A 5400 STIFFENER DOUG DC10 DC1010F 3022111 WP NR 2 NACELLE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 049FE 47803 NR 2 INLET INTERNAL 7TH RIB AFT OF FWD WEB ANGLE STIFFENER CRACK, 7:00 POSITION. *S/D* REMOVED ANGLE STIFFENER AND FAB RICATED NEW STIFFENER IN REF SRM 51-00-01. INSTALLED STIFFENER REF SRM 54-10-00. 4-16-98. 2 L 7 3 4F A22WE 1998042400073 19980424 00073 WP 1998 4 24 ABXA9800345 1 19980413 A 3610 711737525D CONNECTOR DOUG DC8 DC861 3021952 WP COCKPIT FAILED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 842AX 46015 LOUD AIR NOISE IN FWD COCKPIT AREA. HOT ODOR NOTICED IN COCKPIT. CREW EXPERIENCED BURNING EYES AND HEADACHE. NOISE WA S ELIMINATED BY TURNING OFF NR 3 CTC. REPLACED PNEUMATIC DUCT CONNECTOR, LEAK CHECKED GOOD. 2 L 7 4 4F 4A25 1998042400074 19980424 00074 WP 1998 4 24 ABXA9800355 1 19980414 A 5610 5613217507 WINDOW DOUG DC9 DC932 3022066 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 901AX 47381 UNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT). WINDOW OPENED AFTER SEVERAL ATTEMPTS. WHEN RECLOSED, WINDOW WO ULD NOT REOPEN. LUBRICATED TRACK AND ROLLERS, WINDOW OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998042400075 19980424 00075 WP 1998 4 24 ABXA9800356 1 19980415 A 5610 5613217507 WINDOW DOUG DC9 DC932 3022066 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 901AX 47381 CAPTAIN'S SLIDING CLEAR VIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEAR VIEW WINDOW IAW DC9 MM. 2 L 7 2 4F A6WE 1998042400076 19980424 00076 WP 1998 4 24 MWEA98436 1 19980415 A 5720 4919285 CLIP DOUG DC9 DC932 3022066 WP WS 69 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING UPPER ATTACH CLIP CRACKED AT STATION XRS 69 WEB BETWEEN 31 AND 32 STRINGERS. MTC REMOVED OLD CLIP FABRICATED AND INSTALLED REPLACEMENT USING SERVICEABLE DATA. 2 L 7 2 4F A6WE 1998042400077 19980424 00077 WP 1998 4 24 MWEA98437 1 19980415 A 5720 5509570003 FITTING DOUG DC9 DC932 3022066 WP WS 240 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INBOARD SLAT TRACK FITTING AT XRS 240 RT WING WAS FOUND CORRODED. MTC REMOVED AND REPLACED INBOARD FITTING USING APPROV ED DATA. 2 L 7 2 4F A6WE 1998042400078 19980424 00078 WP 1998 4 24 MWEA98438 1 19980415 A 5720 5509570003 FITTING DOUG DC9 DC932 3022066 WP WS 240 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 OUTBOARD SLAT TRACK FITTING CORRODED AT WING STATION 240 RIGHT WING. MTC REMOVED AND REPLACED SLAT TRACK FITTING USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400079 19980424 00079 WP 1998 4 24 MWEA98439 1 19980415 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 208 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FUSELAGE SKIN WAS FOUND GOUGED AT FUSELAGE STATION 208 LONG 18 RIGHT. MTC BLENDED GOUGE AND REPAIRED AREA USING APPROVE D DATA. 2 L 7 2 4F A6WE 1998042400080 19980424 00080 WP 1998 4 24 MWEA98440 1 19980415 A 5720 59342167 DOUBLER DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 EXFOLIATION WAS FOUND ON A DOUBLER BETWEEN FUEL DRAIN VALVE AND BOTTOM OF LEFT WING. REMOVED CORRODED DOUBLER FABRICATE D AND INSTALLED REPLACEMENT DOUBLER USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400081 19980424 00081 WP 1998 4 24 MWEA98441 1 19980415 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AN INTERNAL DOUBLER WAS FOUND CORRODED AT FUSELAGE STATION 996 LONGERON 23 LEFT. MTC REMOVED OLD DOUBLER FABRICATED AND INSTALLED REPLACEMENT DOUBLER USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400082 19980424 00082 WP 1998 4 24 MWEA98442 1 19980415 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE FUSELAGE SKIN WAS FOUND CORRODED, BULGING AND HAS RIVETS WITH PULLING HEADS. MTC BLENDED CORROSION AND FOUND SKIN O UT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400083 19980424 00083 WP 1998 4 24 MWEA98443 1 19980415 A 5311 9912246115 FRAME DOUG DC9 DC932 3022066 WP BS 1038 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 EXTERIOR FUSELAGE THE FRAME FUSELAGE STATION 1038 WAS FOUND DEEPLY CHAFED AND CORRODED. BLENDED CORROSION, FABRICATED A ND INSTALLED REPAIR STRAP USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400084 19980424 00084 WP 1998 4 24 MWEA98444 1 19980415 A 5330 59114273 SKIN DOUG DC9 DC932 3022066 WP BS 980 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AT FUSELAGE STATION 980 LONGERON 16 RIGHT A SMALL CRACK WAS FOUND IN THE FUSELAGE SKIN. REPAIRED SKIN USING APPROVED DA TA. 2 L 7 2 4F A6WE 1998042400085 19980424 00085 WP 1998 4 24 MWEA98445 1 19980415 A 5330 5911412191 SKIN DOUG DC9 DC932 3022066 WP BS 229-265 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FORWARD LOWER BELLY SKIN WAS DAMAGED DURING MAINTENANCE. THE SKIN WAS REMOVED FROM FS 229 TO FS 265 LONGERON 26L TO 26R , A REPLACEMENT SKIN WAS SPLICED IN USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400086 19980424 00086 NM 1998 4 24 VNAA9804010 1 19980412 A 3246 26104851 WHEEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG OUT OF BALANCE A VNAA O OTHER E VIBRATION/BUFFET TO TAKEOFF 1 GL 07 424JS 4518 151 3033 DURING THE TAKEOFF, THE CREW NOTED SOME VIBRATIONS FROM THE NOSE LANDING GEAR. WHEN THE FLIGHT WAS IN RANGE OF BTV, THE CREW ADVISED TOWER THAT THEY MAY HAVE A FLAT, OR OUT OF BALANCE NOSE TIRE. THE TOWER DECLARED AN EMERGENCY, AND DISPAT CHED EQUIPMENT. THE FLIGHT LANDED WITHOUT INCIDENT IN BTV, AND TAXIED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NOSEWHEELS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-41-01. THE AIRCRAFT WAS RETURNED TO SERVICE. PART SERI AL NUMBER B-0266 TOTAL TIME 3958.8, TOTAL LANDINGS 3617, TIME SINCE OVERHAUL 15.1, SERIAL NUMBER B-0394 STATS GIVEN BELO W. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998042400100 19980424 00100 NM 1998 4 24 VJ9800131 1 19980408 A 3350 6013211 CHARGER BOEING 737 7372L9 1384497 NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 LT EMERGECY OVERWING LIGHT INOP. REPLACED BATTERY CHARGER IAW MM 33-51-31; OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 1998042400101 19980424 00101 EU 1998 4 24 MALA976095 1 19980405 A 3350 3071BPEGPL BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, EXIT LIGHT INOP NEXT TO SEAT 1D. MAINTENANCE RELAMPED EXIT LIGHT AT SEAT 1D. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400102 19980424 00102 EU 1998 4 24 MALA976096 1 19980406 A 3350 GUARD SAAB SF340 SF340A 7850100 EU COCKPIT LOOSE A MALA K NONE O OTHER CR CRUISE 1 GL 15 27XJ 027 IN FLIGHT, THE CREW REPORTED GUARD OVER THE EMERGENCY LIGHTS SWITCH IS LOOSE. MAINTENANCE TIGHTENED THE EMERGENCY LIGHT SWITCH GUARD. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400103 19980424 00103 EU 1998 4 24 MALA976097 1 19980407 A 5270 G6669 LOCK SWITCH SAAB SF340 SF340A 7850100 EU CARGO DOOR INTERNAL FAULT A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 107XJ 340A107 DURING CLIMB, CARGO DOOR WARNING LIGHT ILLUMINATED. MAINTENANCE REPLACED DOOR LOCK SWITCH. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042400104 19980424 00104 EU 1998 4 24 MALA976099 1 19980412 A 3350 313 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 99XJ 099 DURING INSPECTION, EMERGENCY LIGHTS SEAT 3CD AND RIGHT FORWARD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED LIGHTS. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400105 19980424 00105 EU 1998 4 24 MALA976100 1 19980412 A 3320 BALLAST SAAB SF340 340B 7860101 EU LAVATORY FAILED A MALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 GL 15 403XJ 340B403 INBOUND FOUND LAV SMOKE LIGHT ILLUMINATED. MAINTENANCE REPLACED LAV LIGHT BALLAST. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400106 19980424 00106 NM 1998 4 24 MALA976101 1 19980410 A 2720 2379003001 PRESS REGULATOR DHAV DHC8 DHC8102 2809003 NM RUDDER FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 833MA 343 ON CLIMB-OUT, RUDDER PRESSURE, RUDDER FULL PRESSURE AND NR 2 RUDDER HYD LIGHTS ILLUMINATED. MAINTENANCE REPLACED DUAL P RESSURE REGULATOR. OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042400107 19980424 00107 NM 1998 4 24 MALA976102 1 19980409 A 2720 570347 PUMP DHAV DHC8 DHC8102 2809003 NM RUDDER CONTROL FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 833MA 343 DURING CLIMB-OUT, RUDDER PRESSURE, RUDDER FULL PRESSURE AND NR 2 RUDDER HYD PRESSURE LIGHT ILLUMINATED. MAINTENANCE REP LACED NR 2 HYD PUMP. OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042400108 19980424 00108 EU 1998 4 24 MALA976103 1 19980414 A 3350 SWITCH SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE O OTHER CR CRUISE 1 GL 15 31XJ 031 DURING FLIGHT, FA'S EMERGENCY ARM LIGHT SWITCH INOP. MAINTENANCE RELAMPED LIGHT. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042400109 19980424 00109 NM 1998 4 24 K3HA980055 1 19980415 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 AT POST FLIGHT, FOUND AFT AIRSTAIR EMERGENCY LIGHT BATTERY DEPLETED. REMOVED AND REPLACED BATTERY, REF MM 33-51-01, OPS CHECK OK. 2 L 7 3 4F A3WE 1998042400110 19980424 00110 WP 1998 4 24 CALA9800659 1 19980415 A 3260 SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 72821 49481 THE AIRCRAFT HAD A BRIEF HISTORY OF THE NOSE GEAR UNSAFE LIGHT REMAINING ILLUMINATED AFTER TAKEOFF. CYCLING THE GEAR WO ULD EXTINGUISH THE LIGHT. THE NOSE GEAR LOCK SENSOR WAS REMOVED AND REPLACED IAW MM 32-60-05, PAGES 216-220. THE NOSE G EAR WAS SWUNG WITH OPERATION AND INDICATIONS CHECKING NORMAL. 2 L 7 2 4F A6WE 1998042400111 19980424 00111 NM 1998 4 24 CALA9800660 1 19980304 A 5330 SKIN BOEING 737 737130 1384435 NM BS 262-274 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14209 19206 INSPECTION FOUND AN 8 INCH CRACK IN LT FUSELAGE SKIN AT STA 262-274, STRINGER 9L. THE CRACKED AREA OF SKIN WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-21-31. 2 L 7 2 4F A16WE 1998042400112 19980424 00112 WP 1998 4 24 CALA9800661 1 19980414 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 370-427 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND A 3 INCH CRACK IN FORWARD BAG BIN LOWER DOOR JAMB BEAM AT STA 370-427. A BEAM WAS INSTALLED IAW SRM 51 -30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998042400113 19980424 00113 WP 1998 4 24 CALA9800662 1 19980414 A 5240 BEAM DOUG DC9 DC932 3022066 WP R-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17543 45789 INSPECTION FOUND A 4 CRACK IN R-1 DOOR INTERIOR FORWARD NR 2 BEAM. THE CRACK WAS STOP DRILLED IAW SRM 52-05, FIGURE 25. A J-ANGLE, FITTING, AND SHIMS WERE FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 25 AND 51-10-3. 2 L 7 2 4F A6WE 1998042400114 19980424 00114 WP 1998 4 24 CALA9800663 1 19980414 A 5320 JAMB DOUG DC9 DC982 3022082 WP BAGGAGE DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND MID BAG BIN LOWER DOOR JAMB CORRODED. REPAIRED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998042400115 19980424 00115 WP 1998 4 24 CALA9800664 1 19980415 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND TWO 1 INCH CRACKS IN BELTFRAME AT STA 1418, LONGERON 2L AND 2R. AN UPPER FRAME SPLICE REPAIR WAS INSTA LLED IAW SRM 53-03, FIGURE 32. 2 L 7 2 4F A6WE 1998042400116 19980424 00116 WP 1998 4 24 CALA9800665 1 19980415 A 5240 ANGLE DOUG DC9 DC982 3022082 WP SERVICE DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND ATTACH ANGLE AT TOP OF SLIDE ON FORWARD SERVICE DOOR CORRODED. THE ANGLE WAS REPLACED IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1998042400117 19980424 00117 WP 1998 4 24 CALA9800666 1 19980417 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND AFT CARGO COMPARTMENT BELTFRAME CORRODED AT STA 1231, LONGERON 29L - 29R. THE CORRODED AREA WAS REMOVE D AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 24. 2 L 7 2 4F A6WE 1998042400118 19980424 00118 WP 1998 4 24 CALA9800667 1 19980417 A 5320 JAMB DOUG DC9 DC982 3022082 WP BAGGAGE DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND AFT BAG BIN LOWER DOOR JAMB CORRODED. REPLACED WITH A NEW Z-ANGLE BEAM IAW SRM 51-30-2 AND 51-30-3. 2 L 7 2 4F A6WE 1998042400119 19980424 00119 WP 1998 4 24 CALA9800668 1 19980415 A 5320 PAN DOUG DC9 DC982 3022082 WP STA 370-427 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND LOWER PAN SECTION OF FORWARD BAG BIN DOOR OPENING CORRODED AT STA 370-427. A LOWER PAN SPLICE REPAIR WA S INSTALLED IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 1998042400120 19980424 00120 WP 1998 4 24 CALA9800669 1 19980415 A 5240 DOOR BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND A 1.4 CRACK IN FORWARD END OF NR 4 FORWARD SERVICE DOOR BEAM. THE BEAM WAS REMOVED AND A NEW ONE WAS I NSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998042400121 19980424 00121 WP 1998 4 24 CALA9800670 1 19980415 A 5350 LATCHES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 THE FORCE REQUIRED TO RELEASE TAILCONE USING THE AFT ENTRANCE DOOR AND INTERIOR RELEASE HANDLES DURING DROP TEST, WAS EX CESSIVE. THE TAILCONE LATCHES WERE ADJUSTED AND LUBRICATED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998042400122 19980424 00122 WP 1998 4 24 CALA9800671 1 19980416 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 THE FUSELAGE SKIN WAS FOUND CRACKED AT FORWARD LOWER VHF ANTENNA RT MOUNT HOLE. A REPAIR WAS INSTALLED IAW ECRA 5330-05 230 AND A DIP WAS ISSUED TO INSTALL A PERMANENT REPAIR WITHIN 3600 FLIGHT CYCLES OR ONE YEAR, WHICHEVER COMES FIRST. 2 L 7 2 4F A6WE 1998042400123 19980424 00123 WP 1998 4 24 CALA9800672 1 19980416 A 5210 BRACKET DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND A .5 INCH CRACK IN MAIN CABIN DOOR BRACKET FORWARD OF DOOR HANDLE MECHANISM. THE BRACKET WAS REMOVED A ND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-1, -2, AND -5. 2 L 7 2 4F A6WE 1998042400124 19980424 00124 NE 1998 4 24 9806663209 2 19980415 A 7261 OIL SYST AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 ENGINE LEAKING A NWAA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 309US 118 731477 SHORTLY AFTER TAKEOFF, FLIGHT CREW NOTICED A BURNING SMELL AND LIGHT SMOKE HAZE THROUGHOUT THE AIRCRAFT. AIRCRAFT RETUR NED TO DEPARTURE AIRPORT. MAINTENANCE FOUND INTERNAL OIL LEAK IN NR 1 ENGINE. REPLACED THE NR 1 ENGINE. 2 L 7 2 4F 4 F RT A28NM E29NE 1998042400125 19980424 00125 WP 1998 4 24 9806679949 1 19980416 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8928E 45865 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHTS IN TAILCONE AREA INOPERATIVE. RE PLACED POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400126 19980424 00126 WP 1998 4 24 9906689986 1 19980415 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE OVERHEAD EMERGENCY LIGHT DIM. REPLACED BATTERY PACK. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1998042400127 19980424 00127 WP 1998 4 24 9806699756 1 19980415 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 756NW 47180 FLIGHT ATTENDANT REPORTED THE EMERGENCY FLASHLIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400128 19980424 00128 WP 1998 4 24 9806709865 1 19980415 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 774NC 47776 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE IN COCKPIT AND AT FORWARD ENTRANCE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042400129 19980424 00129 WP 1998 4 24 9806719163 1 19980416 A 3350 BATTERY PACK DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8906E 45747 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE IN MID CABIN. MAINTENANCE REPLACED BATTERY PACK. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400130 19980424 00130 WP 1998 4 24 9806729859 1 19980416 A 3350 CONNECTOR DOUG DC9 DC951 3022051 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, FOUND EMERGENCY LIGHTING REMAINED ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN THE 'OFF' POSITION. MAI NTENANCE RECONNECTED CONNECTOR AT FORWARD SERVICE DOOR BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042400131 19980424 00131 NM 1998 4 24 UPS98226443 1 19980401 A 5320 FITTING BOEING 727 72722C 138400F NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE:C CRACKS FOUND ON BS 740 FITTING OUTBD FLANGE BETWEEN S18R AND S20R AND LOWER END OF FITTING. FITTING R EPAIRED IAW UPS ENGINEERING ORDER B727-5310-7497. 2 L 7 3 4F A3WE 1998042400132 19980424 00132 WP 1998 4 24 UPS98826440 1 19980313 A 5720 FITTING DOUG DC8 DC873F 302199F WP CENTER WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK CORROSION ON CENTER WING SPAR FITTING FUSELAGE STATION 855 INSIDE LEFT HAND WHEEL WELL BELOW UPPER CORNER. REMOVED CLIP, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 57 2 3, THIS CLIP INSTALLED WITH -3 DOUBLER AFTER CORR OSION REMOVAL IAW DC8 SRM 51 1 8, 51 1 20D, AND 51 3 0. 2 L 7 4 4F RT 4A25 1998042400133 19980424 00133 WP 1998 4 24 UPS98826441 1 19980311 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 220-240 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE:C/CK, FWD LOWER CARGO L36 CORRODED, STA 220 TO 240. REMOVED CORROSION, REMOVED LONGERON BOTH HALVES AN D LOCATED AND DRILLED NEW LONGERON HALVES IAW DC8 SRM 51 1 8, 53 2 0, 51 1 24, AND INSTALLED IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998042400134 19980424 00134 WP 1998 4 24 UPS98826442 1 19980327 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE:C LT WING L/E SKIN DOUBLER ABOVE THE NR 1 PYLON IS CRACKED. REMOVED AND REPLACED INTERNAL AND EXTERNAL REPAIR DOUBLERS IAW SRM 57-2-1A AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998042400135 19980424 00135 EU 1998 4 24 WWMA9800074 1 19980415 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E COMPT DIRTY A WWMA K NONE N FALSE WARNING CR CRUISE 1 WP 15 306AE 340B306 FLIGHT 3224, SBP, AVIONICS SMOKE LIGHT ILLUMINATED ONCE THEN EXTINGUISHED. CLEANED THE SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998042400136 19980424 00136 EU 1998 4 24 WWMA9800073 1 19980415 A 2611 72111211000 SMOKEDETECTOR SAAB SF340 340B 7860101 EU E/E COMPT DEFECTIVE A WWMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 338SB 340B338 FLIGHT 5034, BTR, AVIONICS SMOKE LIGHT ILLUMINATED. REPLACED THE SMOKE DETECTOR. 2 L 7 2 4T RT A52EU 1998042400137 19980424 00137 EU 1998 4 24 WWMA9800072 1 19980412 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA C D F ABORTED TAKEOFF RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING TO TAKEOFF 1 WP 15 343SB 340B343 FLIGHT 3221, LAX, CARGO SMOKE LIGHT CAME ON. ABORTED TAKEOFF AND FIRED NR 1 FIRE BOTTLE. REPLACED FWD AND AFT CARGO SM OKE DETECTORS. 2 L 7 2 4T RT A52EU 1998042400138 19980424 00138 EU 1998 4 24 QXEA98 530 1 19980414 A 2150 PACK FOKKER F28 F28MK4000 4990810 EU CABIN SMOKE A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 482US 11231 GEG - FLIGHT ATTENDANT REPORTED SMOKE AND HAZY CONDITIONS IN CABIN AND LAV SMOKE DETECTOR ACTIVATED. TURNED BOTH PACKS OFF AND RETURNED TO GEG. MAINTANENCE ISOLATED PROBLEM TO CABIN PACK. DEFERRED PER MEL 21-1. AIRCRAFT RELEASED FOR TEST FLIGHT. TEST FLIGHT SATISFACTORY. 2 L 7 2 4F RT A20EU 1998042400139 19980424 00139 EU 1998 4 24 QXEA9800531 1 19980414 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 GEG - EMERGENCY EXIT LIGHT OVER COCKPIT DOOR WAS NOT ILLUMINATED WITH EMERGENCY LIGHTS IN ARM OR ON. MAINTANENCE REPLAC ED EXIT SIGN, CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998042400140 19980424 00140 WP 1998 4 24 ABXA9800346 1 19980414 A 5311 9919619506N FRAME DOUG DOUG DC9 DC931 3022065 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND FUSELAGE MAIN FRAME STATION 737 RIGHT SIDE CRACKED AT THE INBOARD FLANGE AFT SIDE AT THE TRACK ZEE CLIP ATTACHMENT. REPAIRED FRAME IAW ABX REA D953-23210 MR. 2 L 7 2 4F A6WE 1998042400141 19980424 00141 WP 1998 4 24 ABXA9800347 1 19980414 A 5330 59114273 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND SKIN CRACKED ABOVE LONGERON 17L STATION 980. REPAIRED SKIN IAW ABX REA D953-23222 MR. 2 L 7 2 4F A6WE 1998042400142 19980424 00142 WP 1998 4 24 ABXA9800348 1 19980414 A 5311 9919617501N FRAME DOUG DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND FUSELAGE MAIN FRAME STATION 699 LEFT SIDE CRACKED AT UPPER INBOARD AFT FLANGE AT THE TRACK ZEE CLI P ATTACHMENT. REPAIRED FRAME IAW ABX REA D953-23208-MR. 2 L 7 2 4F A6WE 1998042400143 19980424 00143 WP 1998 4 24 ABXA9800349 1 19980414 A 5311 9919617502N FRAME DOUG DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND FUSELAGE MAIN FRAME STATION 699 RIGHT SIDE CRACKED AT UPPER INBOARD FORWARD AND AFT FLANGES AT THE TRACK ZEE CLIPS ATTACHMENTS. REPLACED MAIN FRAME IAW DC9 SB 53-131 AND ABX REA D953-23181-MR. 2 L 7 2 4F A6WE 1998042400144 19980424 00144 WP 1998 4 24 ABXA9800350 1 19980414 A 5320 991008711 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 1168 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C- CHECK, FOUND INTERCOSTAL ANGLE CRACKED AT CANTED FRAME STATION 1168, 6 O'CLOCK POSITION. REPLACED INTERCOSTAL ANGLE IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998042400145 19980424 00145 WP 1998 4 24 ABXA9800351 1 19980414 A 5320 99101516 WEB DOUG DOUG DC9 DC931 3022065 WP BS 617-639 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND THE UNDERSIDE OF CUSP WEB AT STA 617-639 RT SIDE CORRODED BEYOND LIMITS. REPLACED CUSP WEB IAW DC 9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998042400146 19980424 00146 WP 1998 4 24 ABX9800352 1 19980414 A 5320 99577099N INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP BS 945-965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND INTERCOSTAL CORRODED AT STATION 945-965 AND LONGERON 29R. REPLACED INTERCOSTAL IAW DC9 SRM 51-30- 52. 2 L 7 2 4F A6WE 1998042400147 19980424 00147 WP 1998 4 24 ABXA9800353 1 19980414 A 5320 591141253 DOUBLER DOUG DOUG DC9 DC931 3022065 WP BS 389 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND ANTENNA INTERNAL DOUBLER STATION 389 CORRODED BEYOND LIMITS. REPLACED DOUBLER IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998042400148 19980424 00148 WP 1998 4 24 ABXA9800354 1 19980414 A 5313 591141585 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 699/718/737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND LONGERON 5R CRACKED AT STATION 699, 718 AND 737. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998042400149 19980424 00149 NM 1998 4 24 DLM90980803 1 19980414 A 3246 BEARING DOUG MD90 MD9030 3023690 NM MLG WHEEL LOOSE A DALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 27 915DN 53395 ON DEPARTURE PUSHBACK, GROUND CREW HEARD LOUD NOISE FROM THE RIGHT MAIN GEAR. FOUND NR 4 MAIN WHEEL INNER BEARING RACE LOOSE IN WHEEL CASTING. REPLACED WHEEL ASSY. 2 L 7 2 4F RT A6WE 1998042400150 19980424 00150 NM 1998 4 24 DLM88980805 1 19980414 A 3350 LENS DOUG MD88 MD88 3023688 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 919DE 53422 SEAT 23 EMERGENCY TRACK LIGHT HAS BULB COVER MISSING. REPLACED LENS AND BULB. 2 L 7 2 4F RT A6WE 1998042400151 19980424 00151 NM 1998 4 24 DL72S980806 1 19980414 A 5522 ACCESS PANEL BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 FOUND ON B2 LETTER CK, 4 INCH CRACK ON BALANCE BOARD ACCESS PANEL 9114. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1998042400152 19980424 00152 NM 1998 4 24 DL72S980807 1 19980414 A 5320 65872607 FITTING BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 498DA 21142 FOUND ON B2 LETTER CK, LT INBD VERTICAL STAB TIE BOLT FITTING CRACKED 1 INCH AT THE FIRST FASTENER HOLE AFT OF THE TIE B OLT. REPLACED FITTING PER BOEING DRAWING 65-17509. 2 L 7 3 4F A3WE 1998042400153 19980424 00153 NM 1998 4 24 DL72S980810 1 19980414 A 3350 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 546DA 22677 ON L/O, FOUND L1 DOOR EMERGENCY LIGHT OUT. RE-LAMPED, OPS CK-OK. 2 L 7 3 4F A3WE 1998042400154 19980424 00154 NM 1998 4 24 DL767980813 1 19980115 A 3350 BATTERY 61020 BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 113DA 22225 JUMPSEAT TWO CENTER FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY AND BULB ASSY. 2 L 7 2 4F RT A1NM 1998042400155 19980424 00155 NM 1998 4 24 DL72S980817 1 19980323 A 5330 SKIN BOEING 727 727232 1384082 NM FWD FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 .5 INCH CRACK IN FUSELAGE SKIN AT LOWER INBD CORNER L-4 WINDSHIELD, FROM ATTACH SCREW TO CUTOUT-MARKED. REPAIRED PER SR M 53-30-3 AND ER/A 364469-14. 2 L 7 3 4F A3WE 1998042400156 19980424 00156 NM 1998 4 24 DL733980819 1 19980416 A 5330 SKIN BOEING 737 7373L9 1384470 NM BS 227 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 231DN 23717 TWO DENTS EXIST IN THE FUSE SKIN AT APPROX BS227 BETWEEN S17R AND S19R. PRIOR TO ENTERING REVENUE SERVICE; REPAIR PER E RA 331623-14. 2 L 7 2 4F RT A16WE 1998042400157 19980424 00157 NM 1998 4 24 DL72S980820 1 19980319 A 5753 652163387 RIB BOEING 727 727232 1384082 NM NR 1 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 DURING SHOP VISIT, THE NR 1 MIDFLAP WAS FOUND WITH IB AFT CLOSEOUT RIB CRACKED AT LOWER AFT CORNER. THE RIB WAS REPAIRE D BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER PER 727 MM 57-52-0,FIG. 808. 2 L 7 3 4F A3WE 1998042400158 19980424 00158 NM 1998 4 24 DL72S980829 1 19980326 A 5320 FRAME BOEING 727 727232 1384082 NM CABIN DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 .75 INCH CRACK BEYOND STOP DRILL AT MAIN ENTRY DOOR UPPER DOOR UPPER FRAME, AFT END PREVIOUS REPAIR. REMOVED UPPER LINE R AND GATE. REMOVED UPPER FRAME. DRILLED REPLACEMENT FRAME. BEGAN INSTALLING FRAME. INST FRAME CLOSED UPPER LINER. P ER M/M 52-11-01. 2 L 7 3 4F A3WE 1998042400159 19980424 00159 NM 1998 4 24 SCNA98034 1 19980408 A 7830 TR LIGHT BOEING 727 727227 1384078 NM NR 3 ENGINE ILLUMINATED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 275AF 22092 ON TAKEOFF ROLL, NUMBER THREE REVERSER LIGHT ILLUMINATED, ABORTED TAKEOFF. MEGGED WIRES BACK TO THRUST REVERSER SWITCH AND FUNCTIONALLY TESTED GOOD. SYSTEM OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F A3WE 1998042400160 19980424 00160 1998 4 24 RRXA98077 4 19980414 A 3442 RADAR DOUG DC8 DC862F 3021972 WP COCKPIT MALFUNCTIONED A RRXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 15 997CF 46154 WEATHER RADAR WILL NOT PAINT GROUND SHOWS ONLY SPOKE PATTERN. PERFORMED OPERATIONAL CHECK OF WEATHER RADAR SYSTEM, OPER ATIONAL CHECKS GOOD IAW M/M 34. 2 L 7 4 4F 4A25 1998042400161 19980424 00161 1998 4 24 VNAA9804011 4 19980413 A 2312 7510764902 TRANSCEIVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AVIONICS RACK FAILED A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 422JS 70264 3018 DURING TAXI, THE NUMBER ONE COMM UNIT FAILED TO OPERATE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NUMBER ONE COMM UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 23-10-00. OPERATIONAL CHECKS WERE COMP LETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998042400162 19980424 00162 NE 1998 4 24 TC8A98019 2 19980417 A 7532 PRBC VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE DIRTY A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 181SK 45910 669217 NR 2 ENGINECOMPRESSOR STALL DURING TAKEOFF, REJECTED TAKEOFF AT 95 KTS. INSPECTED, CLEANED AND LUBED NR 2 PRBC VALVE. P ERFORMED HIGH POWER RUN IAW 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1998042400163 19980424 00163 EU 1998 4 24 AWXA9800089 1 19980402 A 2920 E0245115B0 RELAY AIRBUS 320 A320231 3930325 EU RAM AIR TURBINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 628AW 67 RAM AIR TURBINE DEPLOYED ON ITS OWN ON CLIMBOUT. FOUND BOTH RELAYS 17XE AND 18 XE BAD, REPLACED BOTH. PERFORMED RAT AU TO DEPLOYMENT AND INSPECTION PER AWA TASK CARD NR F2C29301, STEP 3, FUNCTION TEST GOOD. 2 L 7 2 4F RT A28NM 1998042400164 19980424 00164 NM 1998 4 24 AWXA9800092 1 19980407 A 3350 900835A BATTERY BOEING 737 7372U9 1384498 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 149AW 22575 EMERGENCY EXIT LIGHTS ALONG SIDE DOORS L1 AND R1 AND RT OVERWING INOP. REMOVED AND REPLACED BATTERY CARTRIDGE ASSY, OPS CK GOOD AT THIS TIME. 2 L 7 2 4F RT A16WE 1998042400165 19980424 00165 NM 1998 4 24 AWXA9800094 1 19980408 A 3350 864705 FUSE BOEING 737 73733A 1384673 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 168AW 23629 EMERGENCY LIGHTS ON SEAT ROWS 6 TO 18 INOP. REPLACED FUSE IN EMERGENCY LIGHT POWER SUPPLY, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1998042400166 19980424 00166 NM 1998 4 24 AWXA9800095 1 19980414 A 5330 SKIN BOEING 737 737277 1384570 NM L2 DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 L2 DOOR LOWER HINGE CUTOUT HAS FUSLAGE CRACK. FABRICATED DOUBLER FROM 301 1/2 HARD FAB FILLER DOUBLER FROM .071 202473 INSTALLED IAW SRM 53-30-03 FIG 34. 2 L 7 2 4F RT A16WE 1998042400167 19980424 00167 NM 1998 4 24 AWXA9800096 1 19980310 A 5330 SKIN BOEING 737 737277 1384570 NM R2 DOORWAY CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 R2 DOOR CUTOUT HAS CRACK AT LOWER HINGE IN FUSELAGE, APPROXIMATELY 1.75 INCHES LONG/CRACK IN FUSELAGE SKIN RT WING TO BO DY AREA (2 CRACKS). REPAIRED PER PRELIMINARY CIR 3-53-35-AB AND SRM 53-30-31 PAGE 28 RESPECTIVELY. 2 L 7 2 4F RT A16WE 1998042400168 19980424 00168 NM 1998 4 24 AWXA9800097 1 19980226 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181 22648 DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN CRACKED AT STA 727B + 10 BELOW STR 17R. TEMP REPAIR PER SRM 53-30 -03. 2 L 7 2 4F RT A16WE 1998042400169 19980424 00169 NM 1998 4 24 AWXA9800103 1 19980417 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 150AW 23218 EVIDENCE OF FUSELAGE SKIN CRACK LT SIDE OF AIRCRAFT, AFT OF WING TO BODY FAIRING APPROX STRINGERS 21, 22, 23, 1ST STRING ER ABOVE EXISTING PATCH. BLIND FASTENERS INSTALLED PER SRM 53-00-01 FIG 202. REINSPECT EVERY 2500 CYCLES, TERMINATE AT 20000 CYCLES. EVIDENCE OF FUSELAGE SKIN CRACK RT SIDE OF AIRCRAFT, AT STRINGER 23 STA 727A, 1 STRINGER BELOW EMERGENCY EXIT LIGHT. 2 L 7 2 4F RT A16WE 1998042400170 19980424 00170 SO 1998 4 24 RAAA98E9012 1 19980417 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998042400171 19980424 00171 NM 1998 4 24 CALA9800673 1 19980418 A 3260 SENSOR BOEING 737 7373T0 1384582 NM RT MLG OUT OF ADJUST A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 47332 23570 THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. WHEN OFF POSITION WAS SELECTED, BOT H RED AND GREEN LIGHTS WERE ILLUMINATED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC E ADJUSTED THE RT MLG UPLOCK SENSOR TARGET. A RETRACTION TEST WAS PERFORMED AND ALL INDICATIONS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 1998042400172 19980424 00172 NM 1998 4 24 CALA9800674 1 19980415 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND UPPER CAP OF FLOORBEAM CORRODED AT FS 1130, LBL 60 TO RBL 60. THE FLOORBEAM WAS CORRODED IAW ECRA 5310 -03707. 2 L 7 3 4F A3WE 1998042400173 19980424 00173 NM 1998 4 24 CALA9800675 1 19980415 A 5320 CHORD BOEING 727 727232 1384082 NM BS 1179 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND CHORD CORRODED AT FS 1179, LBL 20. THE CHORD WAS REMOVED AND A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 53-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1998042400174 19980424 00174 NM 1998 4 24 CALA9800676 1 19980415 A 5320 CHORD BOEING 727 727232 1384082 NM BS 950-1010 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND AFT CARGO THRESHOLD LOWER CHORD CORRODED AT FS 950E TO 1010. THE AREA WAS REPAIRED IAW ECRA 5310-03710 . 2 L 7 3 4F A3WE 1998042400175 19980424 00175 NM 1998 4 24 CALA9800677 1 19980417 A 5531 SPAR BOEING 727 727232 1384082 NM VERT STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND VERTICAL STABILIZER FRONT SPAR FIN STA 87 TO 100 CORRODED ON RT SIDE. THE CORRODED AREA WAS CUT OUT, A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW ENGINEERING ORDER 98-833. 2 L 7 3 4F A3WE 1998042400176 19980424 00176 WP 1998 4 24 CALA9800678 1 19980417 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND A 1 INCH CRACK IN LONGERON 2R AND 2L AT STA 1418. THE AREAS WERE REPAIRED IAW SRM 53-02-18. 2 L 7 2 4F A6WE 1998042400177 19980424 00177 WP 1998 4 24 CALA9800679 1 19980417 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 470-480 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND LOWER FUSELAGE SKIN CRACKED FROM STA 470 TO 480 BETWEEN LONGERON 30 AND 29L. THE SKIN WAS REPAIRED IAW ECRA 5330-02655. 2 L 7 2 4F A6WE 1998042400178 19980424 00178 SO 1998 4 24 COMA9810102 1 19980415 A 3620 LEAK WARNING EMB 120 EMB120RT SO RIGHT ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 263CA 120255 RIGHT HAND DUCT LEAK WARNING DURING TAKEOFF. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T RT A31SO 1998042400179 19980424 00179 SO 1998 4 24 COMA9810103 1 19980418 A 5415 12003976001 FITTING EMB 120 EMB120RT SO LT NACELLE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 254CA 1233 DURING LEFT ENGINE CHANGE, FOUND THE MOST AFT, INBOARD NACELLE SUPPORT ROD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLA CED THE FITTING. 2 L 7 2 4T RT A31SO 1998042400180 19980424 00180 SO 1998 4 24 COMA9810104 1 19980418 A 5415 12030973001 FITTING EMB 120 EMB120RT SO LT NACELLE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 254CA 1233 DURING LEFT ENGINE CHANGE, FOUND THE SECOND FROM AFT NACELLE SUPPORT ROD ATTACH FITTING ON THE INBOARD SIDE TO HAVE EXCE SSIVE PLAY AT THE BEARING. REPLACED THE FITTING. 2 L 7 2 4T RT A31SO 1998042400181 19980424 00181 SO 1998 4 24 COMA9810105 1 19980418 A 5415 12030573601 FITTING EMB 120 EMB120RT SO LT NACELLE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 254CA 1233 DURING LEFT ENGINE CHANGE, FOUND PLAY IN ONE BEARING OF THE INBOARD NACELLE SUPPORT ROD CLUSTER FITTING. REPLACED INBOA RD NACELLE SUPPORT ROD CLUSTER FITTING. 2 L 7 2 4T RT A31SO 1998042400182 19980424 00182 SO 1998 4 24 COMA9810106 1 19980418 A 5415 12000361602 FITTING EMB 120 EMB120RT SO LT NACELLE WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 254CA 1233 DURING LEFT ENGINE CHANGE, FOUND THE INBOARD, FORWARD SUPPORT ROD, FORWARD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLA CED INBOARD, FORWARD NACELLE SUPPORT ROD FORWARD FITTING. 2 L 7 2 4T RT A31SO 1998042400183 19980424 00183 EA 1998 4 24 COMA9860076 1 19980314 A 5320 45820651 FITTING CNDAIR CL600 CL6002B19 EA LAVATORY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 DURING C-1 INSPECTION, FOUND LAV FLOOR ENCLOSURE CLOSE OUT COVER FITTING (P/N 4582065-1) CRACKED. REPLACED CLOSE OUT CO VER IN ACCORDANCE WITH CONCESSION LETTER C095-774. 2 L 7 2 4F RT A21EA 1998042400184 19980424 00184 EA 1998 4 24 COMA9860077 1 19980315 A 3350 P4010021 BATTERY PACK CNDAIR CL600 CL6002B19 EA COCKPIT DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 966CA 7132 DURING C-1 INSPECTION, FOUND CO-PILOTS EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK IN ACCORDANCE WITH AIRCRAFT MAI NTENANCE MANUAL 25-61-02. 2 L 7 2 4F RT A21EA 1998042400185 19980424 00185 EA 1998 4 24 COMA9860078 1 19980314 A 5753 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 966CA 7132 DURING C-1 INSPECTION, FOUND LEFT INBOARD FLAP TO BE CHAFED. REPLACED LEFT INBOARD FLAP. 2 L 7 2 4F RT A21EA 1998042400186 19980424 00186 EA 1998 4 24 COMA9860079 1 19980404 A 5320 6013501251 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 ANGLE (P/N 601-35012-51) IN AFT EQUIPMENT BAY, LEFT HAND SIDE OF FS 621 BULKHEAD CRACKED. REPLACED ANGLE AS PER REO 601 R-53-61. 2 L 7 2 4F RT A21EA 1998042400187 19980424 00187 EA 1998 4 24 COMA9860080 1 19980228 A 4980 601R9720419 SHIELD CNDAIR CL600 CL6002B19 EA APU CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 967CA 7134 DURING C-1 INSPECTION, FOUND APU EXHAUST SHIELD ASSEMBLY CRACKED. REPLACED EXHAUST SHIELD. 2 L 7 2 4F RT A21EA 1998042400188 19980424 00188 EA 1998 4 24 COMA9860081 1 19980418 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION CL CLIMB 1 SO 01 976CA 8595 7151 FLAPS FAILED AT ZERO AFTER TAKEOFF. REPLACED THE LEFT AND RIGHT FLAP BPSU. 2 L 7 2 4F RT A21EA 1998042400189 19980424 00189 EA 1998 4 24 COMA9860082 1 19980418 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 999CA 7230 LANDING GEAR WILL NOT RETRACT. COULD NOT DUPLICATE DISCREPANCY. REPLACED GEAR SELECTOR FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1998042400190 19980424 00190 EA 1998 4 24 COMA9860083 1 19980418 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 999CA 7230 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO THE FIELD AND THEN WAS FERRIED TO CVG GEAR DOWN. C VG MAINT COULD NOT DUPLICATE THE PROBLEM BUT DID FIND A DI11 OFF CODE. THE LANDING GEAR CONTROL HANDLE WAS REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F RT A21EA 1998042400191 19980424 00191 NM 1998 4 24 UPS98226444 1 19980410 A 5320 SILL BOEING 727 72722C 138400F NM BS 480-600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, TO AID IN CORROSION REMOVAL PLEASE DISPLACE DOOR SILL WEB BS 480 TO 600 DOOR SILL WEB DERIVETED, INSPECTED AND FOUND CRACKED AND CORRODED. NEW WEB FABRICATED IN TWO SECTIONS IAW SRM 53-10-2, FIG 3 AND SPLICED AT BS 5 25 IAW SRM 51-40-2 FIG 1. WEB INSTALLED IAW DRAWING 65-40507. 2 L 7 3 4F A3WE 1998042400192 19980424 00192 NM 1998 4 24 UPS98226445 1 19980407 A 5753 SKIN BOEING 727 72722C 138400F NM LT TE FLAP DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, LT INBD AFT FLAP HAS DELAMINATION OUTBD LOWER SURFACE. REPAIRED IAW SRM 51-40-9. 2 L 7 3 4F A3WE 1998042400193 19980424 00193 NM 1998 4 24 UPS98226446 1 19980408 A 2730 BRACKET BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, RT ELEVATOR TRAILING EDGE CAVITY BRACKET CRACKED A FS 60 (ABOVE TAB ROD). BRACKET REPLACED IAW DRAWI NG NR 69-19144. 2 L 7 3 4F A3WE 1998042400194 19980424 00194 NM 1998 4 24 UPS98226447 1 19980409 A 5311 FRAME BOEING 727 72722C 138400F NM BS 481 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK FOUND ON FUSELAGE FRAME AT BS 481 AT SEAT TRACK ATTACH HOLE LBL 62. CRACK REMOVED PER SRM 51-1 0-6 AND REPAIR CARRIED OUT IAW SRS EO 98-10-007. 2 L 7 3 4F A3WE 1998042400195 19980424 00195 NM 1998 4 24 UPS98226448 1 19980408 A 5311 FRAME BOEING 727 72722C 138400F NM BS 490 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, TOE ON FRAME AT BS 490 FWD SIDE CRACKED AT LATCH SUPPORT FITTING OF MAIN CARGO DOOR. FRAME REPAIRED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1998042400196 19980424 00196 NM 1998 4 24 UPS98226449 1 19980406 A 5311 FRAME BOEING 727 72722C 138400F NM BS 580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK IN TOE OF FRAME AT BS 580 LEFT HAND AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4 F IGURE 11. 2 L 7 3 4F A3WE 1998042400197 19980424 00197 NM 1998 4 24 UPS98226450 1 19980404 A 5320 EXTRUSION BOEING 727 72722C 138400F NM BS 480-600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CORROSION UNDER REMOVED TEFLON STRIP. ALL CORROSION REMOVED IAW SRM 51-10-6, ALL AREAS INSPECTED AND REPAIRED IAW SRS ENGINEERING ORDER 98-10-005, UPS FILE NUMBER 727-53-2017. 2 L 7 3 4F A3WE 1998042400198 19980424 00198 NM 1998 4 24 UPS98226451 1 19980406 A 5311 FRAME BOEING 727 72722C 138400F NM BS 490 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK IN TOE OF FRAME AT STATION 490 LT AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4 FIG URE 11. 2 L 7 3 4F A3WE 1998042400199 19980424 00199 NM 1998 4 24 UPS98226452 1 19980408 A 5320 WEB BOEING 727 72722C 138400F NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK FOUND ON RT WHEEL WELL, FWD WALL BS 870. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998042400200 19980424 00200 NM 1998 4 24 UPS98226454 1 19980408 A 5320 65405124 FITTING BOEING 727 72722C 138400F NM BS 487 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, ON REMOVAL OF BS 487 MAIN CARGO DOOR LATCH SUPPORT FITTING, CORROSION FOUND ON FITTING. NEW MAIN CAR GO DOOR LATCH SUPPORT FITTING REAPLACED IAW EO B727-5310 -0437 APPENDIX 8.6 AND 8.7. 2 L 7 3 4F A3WE 1998042400201 19980424 00201 NM 1998 4 24 UPS98226455 1 19980409 A 5320 65405122 FITTING BOEING 727 72722C 138400F NM BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, ON REMOVAL OF MAIN CARGO DOOR LATCH SUPPORT FITTING, FITTING FOUND CRACKED. NEW MAIN CARGO DOOR FITT ING REPLACED IAW EO B727-5310-0437. 2 L 7 3 4F A3WE 1998042400202 19980424 00202 NM 1998 4 24 UPS98226457 1 19980401 A 2710 652011811 CASTING BOEING 727 72722C 138400F NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, LT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. REPLACED CASTI NG WITH NEW ONE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998042400203 19980424 00203 NM 1998 4 24 UPS98226458 1 19980401 A 2710 652611812 CASTING BOEING 727 72722C 138400F NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, RT INBD AILERON TURNAROUND PULLEY CASTING HAS CORROSION ON LUG FOR TURNAROUND PULLEY. CASTING REPLAC ED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998042400204 19980424 00204 NM 1998 4 24 UPS98226459 1 19980417 A 3350 9621019 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, FWD ENTRY OVERHEAD EMER LIGHT INOP. REPLACED BATTERY, CHECKS OK. 2 L 7 3 4F A3WE 1998042400205 19980424 00205 NM 1998 4 24 UPS98226461 1 19980417 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, EMER LIGHT AT SEAT 6C INOP. REMOVED AND REPLACED BATTERY, CHECKS OK. 2 L 7 3 4F A3WE 1998042400206 19980424 00206 NM 1998 4 24 UPS98226462 1 19980417 A 3350 9621019 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE MAIN ENTRY DOOR INOP. REMOVED AND REPLACED BATTERY PACK, CHECKS GOOD. 2 L 7 3 4F A3WE 1998042400207 19980424 00207 NM 1998 4 24 UPS98226463 1 19980417 A 3350 BATTERY PACK BOEING 727 727185C 138406N NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-N/A, BOTH EMERGENCY LIGHTS OUT AT COCKPIT DOOR AND L1 DOOR. REMOVED AND REPLACED BATTERY PACK FOR COCKP IT DOOR AND L1 DOOR, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998042400208 19980424 00208 NM 1998 4 24 UPS98526456 1 19980417 A 3350 233N3219300 LIGHT PANEL BOEING 757 75724APF 1384969 NM COCKPIT MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 466UP 25482 INSPECTION TYPE-P/F, EXIT LIGHTS COME ON WHEN SWITCH IS IN THE OFF POSITION. NO GROUND PWR ON A/C AND BATTERY SWITCH IS OFF. REMOVED AND REPLACED EMERGENCY LIGHT PANEL. 2 L 7 2 4F RT A2NM 1998042400209 19980424 00209 EU 1998 4 24 WWMA9800075 1 19980416 A 3350 6013211 BATTERIES SAAB SF340 340B 7860101 EU CABIN DISCHARGED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 324AE 340B324 ADJACENT FLOOR PROXIMITY LIGHTS INOP AT ROWS 8B/10B AND TWO ADJACENT OVERHEAD EMER LIGHTS INOP AT 9A/11A. REPLACED BATT ERIES 22LN AND 23LN. 2 L 7 2 4T RT A52EU 1998042400210 19980424 00210 NM 1998 4 24 QXEA9800532 1 19980416 A 3350 LIGHTS DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 824PH 157 TWO FORWARD EMERGENCY ESCAPE FLOOR PATH LIGHTS ARE INOP. RESTORED WIRING TO ORIGINAL CONDITION IAW DHC MAINTENANCE MANU AL. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998042400211 19980424 00211 WP 1998 4 24 ABXA9800357 1 19980415 A 3260 0080004002 SWITCH DOUG DC8 DC863F 302198F WP LT MLG DEFECTIVE A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 LANDING GEAR UPLATCH CHECK FAILED. RED GEAR UNSAFE LIGHT AND LEFT MAIN\NGEAR DOOR UNLATCHED LIGHT ILLUMINATED. RECYCLE D GEAR, NO CHANGE. PERFORMED ALTERNATE UPLATCH CHECK. REPLACED LEFT MAIN LANDING GEAR PROXIMITY SWITCH IAW DC8 MM 32-6 0-0, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998042400212 19980424 00212 WP 1998 4 24 ABXA9800358 1 19980417 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP LT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 982AX 47317 WHEN LANDING GEAR WAS PLACED DOWN, THREE GREEN LIGHTS AND THE GEAR DOOR OPEN LIGHT REMAINED ON. REPLACED MAIN LANDING G EAR DOOR POSITION SWITCH. 2 L 7 2 4F A6WE 1998042400213 19980424 00213 WP 1998 4 24 ABXA9800359 1 19980419 A 5610 5613217507 WINDOW DOUG DC9 DC932 3022066 WP LT COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 901AX 47381 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. LUBRICATED WINDOW, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998042400214 19980424 00214 WP 1998 4 24 ABXA9800360 1 19980415 A 2910 LINE DOUG DC9 DC933F 302207A WP RT MLG WW RUPTURED A ABXA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 930AX 47363 RIGHT HYDRAULIC FLUID QUANTITY DROPPED TO 0. REPAIRED HYDRAULIC LINE AT THE AUXILIARY PUMP FILTER, OPS CHECKED GOOD IAW DC9 MM. 2 L 7 2 4F A6WE 1998042400215 19980424 00215 WP 1998 4 24 MWEA98457 1 19980417 A 5320 39148671 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 DURING SKIN REPLACEMENT LONGERON 25 RIGHTS END FITTING AT FUSELAGE STATION 996 WAS FOUND CORRODED. REMOVED AND REPLACED FITTING. 2 L 7 2 4F A6WE 1998042400216 19980424 00216 WP 1998 4 24 MWEA98458 1 19980417 A 5320 5914558 DOUBLER DOUG DC9 DC932 3022066 WP BS 965 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE DOUBLER LOCATED AT LONGERON 22 LEFT JUST FORWARD OF FRAME STATION 965 IS CORRODED. REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 1998042400217 19980424 00217 WP 1998 4 24 MWEA98459 1 19980417 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 945-996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 23 RIGHT WAS FOUND CORRODED FROM FUSELAGE STATION 945 TO 996. MTC REMOVED OLD PART FABRICATED AND INSTALLED RE PLACEMENT LONGERON. 2 L 7 2 4F A6WE 1998042400218 19980424 00218 WP 1998 4 24 MWEA98460 1 19980417 A 5312 991556117 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 22ME 47701 THE 996 BULKHEAD LOWER TEE ANGLE WAS FOUND CORRODED. REMOVED AND REPLACED TEE ANGLE. 2 L 7 2 4F A6WE 1998042400219 19980424 00219 WP 1998 4 24 MWEA98461 1 19980417 A 5320 9915561 FITTING DOUG DC9 DC932 3022066 WP AFT FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE AFT JACK POINT FITTING IS CORRODED. REMOVED AND REPLACED AFT JACK FITTING. 2 L 7 2 4F A6WE 1998042400220 19980424 00220 WP 1998 4 24 MWEA98462 1 19980417 A 5320 5910130 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 A SHEAR TIE WAS FOUND CRACKED AT FUSELAGE STATION 996. MTC REMOVED OLD SHEAR TIE AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 1998042400221 19980424 00221 WP 1998 4 24 MWEA98463 1 19980417 A 5320 9915561 SPLICE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE WEB SPLICE AT FUSELAGE STATION 996 IS CORRODED THROUGH. MTC REMOVED OLD SPLICE OBTAINED NEW SPLICE AND INSTALLED SP LICE. 2 L 7 2 4F A6WE 1998042400222 19980424 00222 WP 1998 4 24 MWEA98464 1 19980417 A 5320 5912528 JAMB PAN DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE AFT CARGO DOOR CUTOUT JAMB PAN WAS FOUND CORRODED AROUND THE LOWER AREA. MTC REMOVED DAMAGED SECTION INSTALLED REPA IR SECTION USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400223 19980424 00223 WP 1998 4 24 MWEA98465 1 19980417 A 5320 9958232 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 962 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE INTERCOSTAL AT FS 926 BETWEEN LONGERON 28R AND 29R HAS ELONGATED FASTENER HOLES. MTC REMOVED OLD PART FABRICATED AN D INSTALLED REPLACEMENT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400224 19980424 00224 WP 1998 4 24 MWEA98466 1 19980417 A 5320 9958227 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 907 MISMANUFACTURED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL AT FUSELAGE STATION 907 FROM LONGERON 29R TO 28R IS OF THE WRONG INTERCOSTAL THICKNESS. REMOVED OLD PART FA BRICATED AND INSTALLED REPLACEMENT PART USING APPROACH DATA. 2 L 7 2 4F A6WE 1998042400225 19980424 00225 WP 1998 4 24 MWEA98467 1 19980417 A 5320 9958231 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 897-937 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE INTERCOSTAL LOCATED ON LONGERON 29 RIGHT FROM FUSELAGE STATION 897 TO 937 WAS IMPROPERLY MADE. MTC REMOVED OLD PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400226 19980424 00226 WP 1998 4 24 MWEA98468 1 19980417 A 5320 9958232 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 889-897 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AN INTERCOSTAL AT LONGERON 25R AT FUSELAGE STATION 889 TO 897 HAS DOUBLE DRILLED HOLES. REMOVED DAMAGED PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400227 19980424 00227 WP 1998 4 24 MWEA98469 1 19980417 A 5320 9958232 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 937--945 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AN INTERCOSTAL AT LONGERON 25 RIGHT AT FUSELAGE STATION 937 TO 945 HAS DOUBLE DRILLED HOLES. REMOVED DAMAGED PART FABRI CATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400228 19980424 00228 WP 1998 4 24 MWEA98470 1 19980417 A 5320 9958232 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 937-945 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 AN INTERCOSTAL AT LONGERON 26 RIGHT LOCATED FROM FUSELAGE STATION 937 TO 945 HAS DOUBLE DRILLED HOLES. MTC REMOVED DAMA GED PART FABRICATED AND INSTALLED REPLACEMENT PART USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400229 19980424 00229 NM 1998 4 24 DL72S980816 1 19980416 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 0560 21020 FOUND EMERGENCY LIGHT SECTION IN CABIN INOP. REPLACED PWR SUPPLY, SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 1998042400230 19980424 00230 NM 1998 4 24 DL733980822 1 19980416 A 5330 6545772188 SKIN BOEING 737 737347 1384647 NM BS 870 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 THE FUSE SKIN WAS REPORTED TO BE WORN FROM BS 860 TO BS 885 TO A MAX DEPTH OF 0.013. REPAIRED PER ERA 331634-14. 2 L 7 2 4F RT A16WE 1998042400231 19980424 00231 NM 1998 4 24 DL72W980823 1 19980416 A 5320 ANGLE BOEING 727 727247 138408F NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON C2 LETTER CK, AFT GUSSET ANGLE CRACKED STA 1263 LOWER RT TORQUE BOX. REPLACED ANGLE PER SRM 53-10-10. 2 L 7 3 4F A3WE 1998042400232 19980424 00232 NM 1998 4 24 DL72W980824 1 19980416 A 5320 WEB BOEING 727 727247 138408F NM BS 1277 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON C2 LETTER CK, LT LOWER VERTICAL TORQUE BOX WEB CRACKED AT LIGHTENING HOLE STA 1277. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998042400233 19980424 00233 NM 1998 4 24 DL72W980825 1 19980416 A 5320 WEB BOEING 727 727247 138408F NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON C2 LETTER CK, VERTICAL WEB CRACKED ABOVE 'S' DUCT LOWER RT SIDE STA 1303. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1998042400234 19980424 00234 NM 1998 4 24 DL72W980826 1 19980416 A 5311 FRAME BOEING 727 727247 138408F NM BS 910 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON C2 LETTER CHECK, 1.25 INCH CRACK MLG UPLOCK FRAME STA 910. INSTALLED TEMP, REPAIR PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998042400235 19980424 00235 NM 1998 4 24 DL72W980827 1 19980416 A 2782 BRACKET BOEING 727 727247 138408F NM LE FLAP ACTUATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON C-2 LETTER CHECK, INBD ATTACH BRACKET CRACKED NR 1 L/E FLAP ACTUATOR. REPAIR PER MM 57-20-21. 2 L 7 3 4F A3WE 1998042400236 19980424 00236 NM 1998 4 24 DLM88980830 1 19980417 A 7603 THROTTLE CABLES DOUG MD88 MD88 3023688 NM NR 2 ENGINE JAMMED A DALA O OTHER O OTHER CL CLIMB 1 SO 27 980DL 53267 ON LEVEL OFF AT 5,000 FEET, THE NR 2 THROTTLE JAMMED. PUSHED BACK AND CONSIDERABLE FORCE WAS REQUIRED TO PUSH THE THROT TLE FORWARD AGAIN. FOUND RT ENGINE ANTI-ICE DUCT BLOWN AND ENGINE CONTROL CABLES DAMAGED. REPLACED DUCT AND CABLES AND REPAIRED DAMAGED COWL. 2 L 7 2 4F RT A6WE 1998042400237 19980424 00237 NM 1998 4 24 DL72S980832 1 19980417 A 5754 STIFFENER BOEING 727 727232 1384082 NM RT LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 475DA 20752 FOUND ON A1 LETTER CK, 2 SPAR STIFFENERS CRACKED AT NR 7 SLAT INBD AND OUTBD STIFFENERS AT THE OUTBD TRACK. REPLACED ST IFFENERS PER MM 57-20-21. 2 L 7 3 4F A3WE 1998042400238 19980424 00238 NM 1998 4 24 DL72S980833 1 19980417 A 5720 AUX SPAR BOEING 727 727232 1384082 NM LT WING CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 475DA 20752 FOUND ON A1 LTR CHECK, MLG CHAFING FWD SURFACE OF AUX SPAR I/B END. REPAIRED PER M/M 57-43-0. 2 L 7 3 4F A3WE 1998042400239 19980424 00239 NM 1998 4 24 DL72K980834 1 19980417 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 472DA 1286 20749 LT OVRWING EXIT IDENT EMERG LIGHTS INOP. REPLACED BATT PACK M1090, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1998042400240 19980424 00240 NM 1998 4 24 DL72S980835 1 19980417 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 475DA 20752 FOUND ON A1 LTR CHECK, NR 4 SLAT NOSE RIB CRACKED 1.5 INCH O/B SIDE OF ACTUATOR ROD END. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998042400241 19980424 00241 NM 1998 4 24 DL72S980836 1 19980417 A 5320 FITTING BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 475DA 20752 FOUND ON A1 LETTER CK, UPPER FLANGE OF LT INBD TENSION TIE FITTING CRACKED. REPLACED FITTING PER BOEING DWG NR 65-17509 REV M. 2 L 7 3 4F A3WE 1998042400242 19980424 00242 WP 1998 4 24 DLL10980837 1 19980417 A 3350 2232 BULB LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 712DA 193C1088 RELAMPED R4 EXTERIOR EMERGENCY LIGHT. 2 L 7 3 4F A23WE 1998042400243 19980424 00243 NM 1998 4 24 DL72S980838 1 19980418 A 3350 BATTERY PACK 1060091102 BOEING 727 727232 1384082 NM COCKPIT DISCHARGE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 416DA 2867 21258 EMERG LIGHT IN THE COCKPIT IS INOP. REPLACED BATTERY PACK ASSY AND THE BATTERIES CK OK. 2 L 7 3 4F A3WE 1998042400244 19980424 00244 NM 1998 4 24 DL72S980839 1 19980418 A 2530 OVEN 5316OVS175 BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 478DA 479 20755 ELECTRICAL ODOR IN F/C REPORTED BY F/A. REPLACED FIRST CLASS OVEN. 2 L 7 3 4F A3WE 1998042400245 19980424 00245 NM 1998 4 24 DL76S980840 1 19980417 A 2781 PROX TARGET BOEING 767 767332 1382001 NM NR 12 LE SLAT MISSING A DALA O OTHER N FALSE WARNING DE DESCENT 1 SO 27 125DL 24075 ON APPROACH WHEN FLAPS 15 SELECTED GOT LEADING EDGE LIGHT WITH L/E SLAT ASSYM EICAS MSG. LANDED WITH FLAPS 20 USING ALT FLAP POSITION/SELECTOR. DUE TO LDG FLAPS 20 AT 170K, LT MAIN GEAR BRAKE TEMP WAS 5 AND RT MAIN GEAR WAS 6. LDG WT 290 K LBS. HAD BDL EMERG TRUCKS CALLED OUT FOR HOT LDG, POS WHEEL/BRAKE FIRES. NOT NEEDED. PERF HIGH ENERGY STOP/HEAT DMG INSP, NO DAMAGE FOUND. FOUND MID EXTEND PROX TARGET FOR NR 12 SLAT SW S300 MISSING REF IPC 27-81-02-01 FIG 1, SHT 3, DE TAIL D. REPLACED TARGET. 2 L 7 2 4F RT A1NM 1998042400246 19980424 00246 NM 1998 4 24 DL73E980842 1 19980418 A 5753 SPINDLE BOEING 737 737247 138448D NM RT TE FLAP BROKEN A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 238WA 23186 WITH A/C FULLY CONFIGURED FOR LANDING, 30 DEGREES FLAPS, GEAR DOWN, THE AILERONS REQUIRED 12 DEGREES LEFT TRIM FOR LEVEL FLIGHT. NO CROSSWIND. EACH PROGRESSIVE FLAP SETTING REQUIRED MORE AILERON INPUT. FOUND RT O/B FLAP CARRIAGE SPINDLE B ROKEN, REPLACED. 2 L 7 2 4F A16WE 1998042400247 19980424 00247 NM 1998 4 24 DL73K980843 1 19980418 A 3350 FUSE BOEING 737 737232 1384475 NM CABIN BLOWN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 316DL 23088 ON SERVICE CK DURING TEST OF EMERGENCY LIGHT SYTEM, FOUND AFT SECTION OF SEAT LIGHTS INOP. FOUND BLOWN FUSE ON PWR SUPP LY CKD FOR SHORTS, NONE FOUND. REPLACED PWR SUPPLY LIGHTS, CK NORMAL. 2 L 7 2 4F RT A16WE 1998042400248 19980424 00248 NM 1998 4 24 SCNA98035 1 19980415 A 7830 65379135 TR VALVE BOEING 727 727227 1384078 NM NR 3 ENGINE FAILED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 275AF 22092 NUMBER THREE THRUST REVERSER OPERATION LIGHT ILLUMINATED AT APPROXIMATELY 1.95 EPR ON TAKEOFF ROLL. TAKEOFF ABORTED AT 60 KNOTS. REMOVED AND REPLACED THRUST REVERSER DIRECTIONAL VALVE PER MAINTENANCE MANUAL CHAPTER 783015, OPERATIONAL CHE CK GOOD. 2 L 7 3 4F A3WE 1998042400249 19980424 00249 1998 4 24 VNAA9804015 4 19980417 A 3418 861EF1 AOA SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT FUSELAGE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 328JS 78524 3030 DURING TAXI FOR TAKEOFF, A STICK PUSHER AND ANGLE OF ATTACK FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT INTO PIT. THE FERRY FLIGHT WAS CARRIED OUT WITHOUT ANY INCIDENT. PIT MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND ANGLE OF ATTACK SENSOR, IN ACCO RDANCE WITH DORNIER MAINTENANCE MANUAL 27-33-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SER VICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998042400250 19980424 00250 WP 1998 4 24 CKSA98259 1 19980414 A 3310 6426 TRANSFORMER DOUG DC8 DC863F 302198F WP FLOOD LIGHT MALFUNCTION A CKSA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 GL 23 870BX 46036 ON LANDING F/E'S PANEL BEHIND LIGHT SWITCH'S BEGAN TO ARC AND SMOKE. ON INSPECTION OF LIGHT SWITCHES FOUND DAMAGE ON FL OOD LIGHT SWITCHES PULLED BREAKERS AS REQUIRED AND TIED OFF CONTINUE DMI NR 8230998 IAW DC8 MM 33-1. REMOVED AND REPLAC ED RHEOSTAT TRANSFORMER OPS CHECK NORMAL IAW MM 33-01. THIS CLEARS DMI 8230998 PLACARDS REMOVED. 2 L 7 4 4F 4A25 1998042400251 19980424 00251 WP 1998 4 24 CKSA98260 1 19980416 A 2130 COUPLING DOUG DC8 DC862 3021970 WP RT MLG WW LOOSE A CKSA B EMER. DESCENT O OTHER CR CRUISE 1 GL 23 801MG 45986 WHILE CLIMBING OUT OF FL290, A LOUD RUMBLING NOISE CAME FROM UNDER PILOTS FEET THAT LASTED FOR ABOUT 10 SEC. UPON REACH ING FL350, CABIN ALT WAS RISING AND DIFF PRESS WAS DECREASING. COULD NOT MAINTAIN A CABIN ALT BELOW 10,000 FT. DESCEND ED TO FL240 CABIN ALT 8700 FT DIFF PRESS OF 5.0 PSI. FOUND DUCT IN RT WHEEL WELL TO NASI SYSTEM COUPLING LOOSE. SECURE D AND SAFETIED COUPLING. LEAK AND OPS CHECKS GOOD. 2 L 7 4 4F 4A25 1998042400252 19980424 00252 NE 1998 4 24 CKSA98261 2 19980416 A 7200 ENGINE DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 2 FIRE A CKSA F ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 GL 23 809CK 45803 NR 2 ENG FIRE WARNING CAME ON DURING DESCENT. AFTER SHUTDOWN LIGHT WENT OUT, THEN CAME BACK ON WITH BELL SEVERAL MINUTE S LATER. DISCHARGED ONE FIRE BOTTLE, LIGHT REMAINED ON. FIRED REMAINING BOTTLE, LIGHT REMAINED ON UNTIL AFTER LANDING THEN WENT OUT. REMOVED AND REPLACED BOTH FIRE BOTTLES ON LEFT WING IAW MM 26-4-1, OPS CHECK GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1998042400253 19980424 00253 WP 1998 4 24 CKSA98262 1 19980414 A 3610 CLAMP LKHEED 1011 1011385115 5265015 WP NR 3 ENGINE LOOSE A CKSA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 103CK 293C1212 ENG 3 FIRE DETECTION AT 7,000 FT WITH LIGHT ILLUMINATED AND RED T-HANDLE ILLUMINATED AND HYD BARRIER LIGHTS ON. TIGHTEN ED LOOSE DUCT CLAMP AT NR 3 ENGINE MIXING EJECTOR SYSTEM OPS AND LEAK CHECK GOOD WITHOUT FIRE LOOP LIGHT DETECTION IAW L 1011 MM CH 36-11-08. 2 L 7 3 4F A23WE 1998042400293 19980424 00293 1998 4 24 HEEA0013849 4 19980406 A 3414 214175299105 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 AIRSPEED INDICATOR NEEDS TO BE BENCH CHECKED AND CERTIFIED. (PER ASB 214ST-97-79) SERIAL NUMBERS REMOVED ARE 230241 AN D 230259. 2 G 7 2 4U H10SW 1998042400294 19980424 00294 1998 4 24 HEEA0013850 4 19980406 A 3414 214175299105 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 AIRSPEED INDICATOR NEEDS TO BE BENCH CHECKED AND CERTIFIED. (PER ASB 214ST-97-79) SERIAL NUMBERS REMOVED ARE 230245 AN D 230242. 2 G 7 2 4U H10SW 1998042400295 19980424 00295 1998 4 24 HEEA0013851 4 19980406 A 3414 214175299105 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 AIRSPEED INDICATOR NEEDS TO BE BENCH CHECKED AND CERTIFIED. (PER ASB 214ST-97-79) 2 G 7 2 4U H10SW 1998042400296 19980424 00296 SW 1998 4 24 HEEA0013852 1 19980406 A 6310 406040500125 FREEWHEEL UNIT BELL 407 407 SW SEALS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 417PH 1283 53038 SEALS LEAKING AND WORN SEAL SLEEVE. PARTS AND LABOR WILL BE INVOICED ON PM#2497. REPLACEMENT SEAL P/N 406-340-102-101 R ECEIVED ON 3-11-98 AGAINST OUR PO#407-285, INVOICE# I100514582. REPLACEMENT SEAL P/N 214-040-841-101 AND SLEEVE P/N 214 -040-814-103 WERE RECEIVED 1 G 7 1 3U O H2SW 1998042400297 19980424 00297 SW 1998 4 24 HEEA0013853 1 19980406 A 6500 406040339111 BEARING 406040320101 BELL 407 407 SW T/R ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH AFS932 53114 ROUGH BEARINGS. SERIAL NUMBERS REMOVED ARE K97-0737 AND A98-0536. 1 G 7 1 3U O H2SW 1998042400298 19980424 00298 SW 1998 4 24 HEEA0013854 1 19980406 A 6420 406312100101 BEARING 407012101105 BELL 407 407 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 183 53005 53142 BEARINGS WORN. SCRAPPED BEARINGS. 1 G 7 1 3U O H2SW 1998042400299 19980424 00299 SW 1998 4 24 HEEA0013855 1 19980406 A 6500 406040339105 BEARING 407040303101 BELL 407 407 SW T/R ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 288 AFS932 53198 ROUGH BEARINGS. SERIAL NUMBERS REMOVED ARE C97-2195 AND C97-2206. PARTS AND LABOR WILL BE INVOICED...WO#9800152-99. 1 G 7 1 3U O H2SW 1998042400300 19980424 00300 SW 1998 4 24 HEEA0013856 1 19980406 A 6220 407010100103 HUB BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM 1234 53060 4 EACH GRIPS P/N 406-010-108-109, S/N A3310, A3331, A3324, A3312 (ALL TOTAL TIME 1234:35) DUE RETIREMENT. 1 EACH LOWER CONE SEAT P/N 407-010-107-101, S/N A80 (TOTAL TIME 1234:35) DUE RETIREMENT. PARTS AND LABOR WILL BE INVOICED...WO#980019 7-99. 1 G 7 1 3U O H2SW 1998042400301 19980424 00301 SW 1998 4 24 HEEA0013857 1 19980406 A 6310 406040500123 FREEWHEEL UNIT BELL 407 407 SW SEAL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 1167G 564 53067 FREEWHEEL UNIT FORWARD SEAL LEAKING. 1 G 7 1 3U O H2SW 1998042400302 19980424 00302 SW 1998 4 24 HEEA0013860 1 19980406 A 6230 214010500117 SWASHPLATE BELL 214 214ST 1182106 SW M/R LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 385 28106 SWASHPLATE LOOSE SLEEVE NUT. 2 G 7 2 4U H10SW 1998042400303 19980424 00303 SW 1998 4 24 HEEA0013861 1 19980406 A 6520 406040400115 GEARBOX BELL 407 407 SW T/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 427PH 1111 53059 INPUT AND OUTPUT SEALS LEAKING. 1 G 7 1 3U O H2SW 1998042400304 19980424 00304 SW 1998 4 24 HEEA0013862 1 19980407 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 23 28140 START KICKS OFF AND DISENGAGES. 2 G 7 2 4U H10SW 1998042400305 19980424 00305 1998 4 24 HEEA0013863 4 19980407 A 3120 212075514001 CLOCK BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 CLOCK INOPERATIVE. 2 G 7 2 4U H10SW 1998042400306 19980424 00306 1998 4 24 HEEA0013864 4 19980407 A 2330 ACS1278 AUDIO CONTROL BOLKMS 117 BK117A4 5626017 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 AUDIO CONTROL INTERNAL LIGHTING INOPERATIVE. 1 G 7 2 3U H13EU 1998042400307 19980424 00307 1998 4 24 HEEA0013865 4 19980407 A 3421 2360041902 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2777D 45299 ATTITUDE INDICATOR BAD BEARINGS. 1 G 7 1 3U H2SW 1998042400308 19980424 00308 SW 1998 4 24 HEEA0013866 1 19980407 A 6240 2360016901 INDICATOR BELL 206 206L1 1182107 SW ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2759U 45272 BEARINGS EXCESSIVELY NOISY. 1 G 7 1 3U H2SW 1998042400309 19980424 00309 1998 4 24 HEEA0013867 4 19980407 A 3421 2360041902 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 ATTITUDE INDICATOR BAD BEARINGS. 1 G 7 2 4U H4SW 1998042400310 19980424 00310 1998 4 24 HEEA0013868 4 19980407 A 3421 2360041902 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5012V 45200 ATTITUDE INDICATOR BAD BEARINGS. 1 G 7 1 3U H2SW 1998042400311 19980424 00311 1998 4 24 HEEA0013869 4 19980407 A 2340 ACS775SL AUDIO CONTROL BOLKMS 117 BK117A4 5626017 EU COCKPIT NOISY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 ICS HAD LOUD STATIC WHEN ON. 1 G 7 2 3U H13EU 1998042400312 19980424 00312 1998 4 24 HEEA0013870 4 19980407 A 3455 6223586001 ANTENNA BELL 206 206L3 1182108 SW ADF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 515KA 51048 ADF IS UNRELIABLE. 1 G 7 1 3U H2SW 1998042400313 19980424 00313 SW 1998 4 24 HEEA0013871 1 19980407 A 2842 214066212107 PROBE BELL 214 214ST 1182106 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 PROBE WILL NOT TEST. 2 G 7 2 4U H10SW 1998042400314 19980424 00314 1998 4 24 HEEA0013872 4 19980407 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW HSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 HSI INDICATOR DOES NOT INDICATE PROPERLY. 1 G 7 2 4U H4SW 1998042400315 19980424 00315 SW 1998 4 24 HEEA0013873 1 19980408 A 6230 214040003105 TRANSMISSION BELL 214 214ST 1182106 SW M/R MAST MAKING METAL E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 7120 28106 M/R MAST ASSY HAS METAL IN OIL. 2 G 7 2 4U H10SW 1998042400316 19980424 00316 EU 1998 4 24 HEEA0013874 1 19980408 A 6420 579063 BEARING 355A12004008 SNIAS 350 AS350B2 8680813 EU T/R HEAD SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 543 6663 3004 RUBBER SEPARATION. 1 G 7 1 3U H9EU 1998042400317 19980424 00317 SW 1998 4 24 HEEA0013875 1 19980408 A 6220 407010111101 CONE SET BELL 407 407 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 1235 53016 CONE SET TEFLON LINER COMING OFF. 1 G 7 1 3U O H2SW 1998042400318 19980424 00318 SW 1998 4 24 HEEA0013876 1 19980408 A 6230 406010427109 GIMBAL RING BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 1168 53038 EXCESSIVE PLAY ON AIRCRAFT AND WORN BUSHINGS. 1 G 7 1 3U O H2SW 1998042400319 19980424 00319 SW 1998 4 24 HEEA0013877 1 19980408 A 6230 406010428109 HUB SET BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 1168 53038 EXCESSIVE PLAY ON AIRCRAFT AND WORN BUSHINGS. 1 G 7 1 3U O H2SW 1998042400320 19980424 00320 SW 1998 4 24 HEEA0013878 1 19980408 A 6230 406010425107 LEVER ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 1168 53038 EXCESSIVE PLAY ON AIRCRAFT AND WORN BUSHINGS. 1 G 7 1 3U O H2SW 1998042400321 19980424 00321 SW 1998 4 24 HEEA0013879 1 19980408 A 6230 406010425107 LEVER ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 1168 53038 EXCESSIVE PLAY ON AIRCRAFT AND WORN BUSHINGS. 1 G 7 1 3U O H2SW 1998042400322 19980424 00322 SW 1998 4 24 HEEA0013880 1 19980408 A 6230 406010426101 LINK ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 1168 53038 EXCESSIVE PLAY ON AIRCRAFT AND WORN BUSHINGS. 1 G 7 1 3U O H2SW 1998042400323 19980424 00323 SW 1998 4 24 HEEA0013881 1 19980408 A 6230 406010426101 LINK ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 1168 53038 EXCESSIVE PLAY ON AIRCRAFT AND WORN BUSHINGS. 1 G 7 1 3U O H2SW 1998042400347 19980424 00347 SO 1998 4 24 98ZZZX1553 2 19980301 A 8520 537750 BOLT CESSNA 404 404 2075901 CE CONT O520 GTSIO520M 17032 SO NR 6 INT ROCKER FAILED A A GNBA A UNSCHED LANDING E K VIBRATION/BUFFET FLUID LOSS CL CLIMB 1 SW 01 5388J 1113 4040666 276144R SHORTLY AFTER TAKEOFF, PILOT FELT MINOR SHAKE IN LT ENGINE. A VISUAL INSPECTION (IN-FLIGHT) REVEALED SMALL AMOUNT OF OI L STREAMING BACK. PILOT RETURNED TO AIRPORT. MAINTENANCE PERSONNEL NOTED NR 6 INTAKE ROCKER BOX HAD A HOLE FROM THE IN SIDE OUT. REPLACED BOLT, GROUND CHECK OK. 1 L 7 2 3O 3 O RT A25CE E7CE 1998042400355 19980424 00355 EU 1998 4 24 98ZZZX1562 1 19980130 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT INBOARD AFT SEAT TRACK TO BE CORRODED. REPLACED RIGHT AFT INBOARD SEAT TRACK IAW ASA E.O. 72-53-0036. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400356 19980424 00356 EU 1998 4 24 98ZZZX1563 1 19980130 A 5320 S5367800826801 CHANNEL AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED PASSENGER DOOR FLOOR SUPPORT CORRODED FRAMES 38 - 39. REPLACED FL OOR SUPPORT AT PASSENGER DOOR BETWEEN FRAMES 38 AND 39 IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400357 19980424 00357 EU 1998 4 24 98ZZZX1564 1 19980131 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING '4 C' CHECK INSPECTION, MAINTENANCE REPORTED LT FA SEAT TRACK CORRODED. INSTALLED NEW LT FA SEAT TRACK IAW ASA EO 72-53-0035. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400358 19980424 00358 EU 1998 4 24 98ZZZX1565 1 19980131 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING '4 C' CHECK INSPECTION, MAINTENANCE REPORTED RT FA SEAT TRACK CORRODED. INSTALLED NEW RT FA SEAT TRACK IAW ASA EO 72-53-0035. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400359 19980424 00359 EU 1998 4 24 98ZZZX1566 1 19980131 A 5347 S5367801212 SEAT TRACK AEROSP ATR72 ATR72212 EU CARGO COMPT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING '4 C' CHECK INSPECTION, MAITNENANCE REPORTED RT AFT CARGO SEAT TRACK CORRODED BEYOND LIMITS. INSTALLED NEW RT AFT CARGO SEAT TRACK IAW ASA EO 72-53-0036. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400360 19980424 00360 EU 1998 4 24 98ZZZX1567 1 19980131 A 5320 FILLER AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FILLER PLATE ON SILL PLATE CORRODED. FABRICATED AND INSTALLED NEW PLATE IAW BASIC SHEET METAL PRACTICES AND INSTALLED IAW ASA EO 72-43-011. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400361 19980424 00361 EU 1998 4 24 98ZZZX1568 1 19980125 A 5320 S5367131831605 SILL AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR SILL PLATE CORRODED. INSTALLED SERVICE DOOR SILL PLA TE KIT A01 IAW EO 72-53-0011 AND SB ATR 72-53-1048. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400362 19980424 00362 EU 1998 4 24 98ZZZX1569 1 19980130 A 5320 S5367131821600 SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR FLOOR SUPPORT CORRODED FRAMES 38-39. REPLACED FLOOR SUPPORT IAW ATR 72 SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400363 19980424 00363 EU 1998 4 24 98ZZZX1570 1 19980131 A 5320 S5367800821602 SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 635AS 372 DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT Z-MEMBER CORRODED AT FRAMES 39-41. INSTALLED NEW RT Z-MEMBER IAW ATR 72 SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998042400364 19980424 00364 GL 1998 4 24 WTAA980054 3 19980325 A 6114 7503503AF DOME SEAL BAG JETSTM JETSTM3101 1500215 EU ROTOL R333 R333482F12 GL RT PROPELLER FAILED A WTAA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 WP 17 424UE 796 SNA - SMOKE ODOR REPORTED IN CABIN DURING TAXI OUT. RIGHT ENGINE OIL CAPTION LIGHT ILLUMINATED SUBSEQUENT TO REPORTED O DOR. CREW SHUT ENGINES DOWN AND DEPLANED PASSENGERS. MAINTENANCE DISCOVERED OIL SOURCE OF SMOKE ODOR TO BE FROM FAILE D RT PROPELLER DOME SEAL. REPLACED SEAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A21EU 6 C P61GL 1998042400367 19980424 00367 EU 1998 4 24 98ZZZX1573 1 19980108 A 6420 1053170023 BEARING BOLKMS 105 BO105LSA3 5626020 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 219 2015 TAIL ROTOR BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998042400368 19980424 00368 EU 1998 4 24 98ZZZX1574 1 19980226 A 7931 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU OIL PRESS WARN FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 134 T16992 2015 OIL PRESSURE WARNING SWITCH HAS ERRATIC OPERATION. CAUSES LOW PRESSURE WARNING LIGHT AT 100 PERCENT NR FLAT PITCH. REP LACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998042400369 19980424 00369 EU 1998 4 24 98ZZZX1575 1 19980105 A 7931 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU OIL PRESS WARN FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 450 V24679 2015 OIL PRESSURE WARNING SWITCH UNIT IS INOPERATIVE. INTERMITTENTLY LIGHT GOES 'ON' THEN 'OFF' DURING FLIGHT. REPLACED WIT H NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998042400370 19980424 00370 EU 1998 4 24 98ZZZX1576 1 19980316 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105LSA3 5626020 EU ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 203LF 208 12715 2015 FUEL PRESSURE TRANSMITTER IS ERRATIC. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998042400371 19980424 00371 EU 1998 4 24 98ZZZX1577 1 19980216 A 7120 10560387 BUSHING BOLKMS 105 BO105LSA3 5626020 EU ENGINE MOUNT WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 433 68 2014 ENGINE MOUNT BUSHING'S ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998042400470 19980424 00470 NM 1998 4 24 K3HA980056 1 19980419 A 3350 BULB BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 AFT GALLEY FLOOR LIGHTING IS MISSING (2 RED BULBS). RELAMPED, OPS CHECK OK. REF MM 33-59-00. 2 L 7 3 4F A3WE 1998042400471 19980424 00471 NM 1998 4 24 K3HA980057 1 19980420 A 3350 S106S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 AFT AIRSTAIR EMERGENCY PATH LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES PER MM 33-50-00. OPS CHECK OK. 2 L 7 3 4F A3WE 1998042400472 19980424 00472 NM 1998 4 24 CALA9800680 1 19980419 A 2750 TORQUE TUBE BOEING 737 737130 1384435 NM RT TE FLAP DAMAGED A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 14206 19023 WHEN FLAPS WERE EXTENDED ON APPROACH, THE FLAP INDICATOR DID NOT MOVE. THE FLAPS WERE LOWERED MANUALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. TROUBLESHOOTING FOUND THE RT INBOARD FLAP TORQUE TUBE DAMAGED. THE TORQUE WAS REMOVED AND RE PLACED IAW MM 27-51-251. IN ADDITION, MAINTENANCE FOUND A BAD FLAP POSITION INDICATOR. THE FLAP POSITION INDICATOR WAS REMOVED AND REPLACED IAW MM 27-58-41. FLAP OPERATION AND INDICATIONS CHECKED GOOD. 2 L 7 2 4F A16WE 1998042400473 19980424 00473 WP 1998 4 24 CALA9800681 1 19980417 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72830 49490 INSPECTION FOUND A 1 INCH CRACK IN NR 1 BEAM OF MAIN CABIN DOOR. THE MAIN CABIN DOOR NR 1 BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998042400474 19980424 00474 WP 1998 4 24 CALA9800682 1 19980418 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 2 INCH CRACK ON LT MLG WHEEL WELL AFT WEB VERTICAL STIFFENER. THE STIFFENER WAS REMOVED AND A NEW ST IFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998042400475 19980424 00475 WP 1998 4 24 CALA9800683 1 19980418 A 5210 FITTING DOUG DC10 DC1030 3023501 WP R-3 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND A 2 INCH CRACK IN R-3 DOOR LOWER FITTING. THE LOWER FITTING WAS REMOVED, A NEW BEAM AND FASTENERS WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998042400476 19980424 00476 1998 4 24 CALA9800684 4 19980421 A 2565 SLIDE BOEING 737 737217 1384464 NM R-2 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12231 19885 INSPECTION FOUND R-2 DOOR SLIDE PRESSURE AT ZERO. THE R-2 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-311. 2 L 7 2 4F A16WE 1998042400477 19980424 00477 WP 1998 4 24 9806739880 1 19980416 A 5210 SEAL DOUG DC9 DC951 3022051 WP DOOR 1R LOOSE A NWAA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 GL 01 670MC 47651 DURING TAKEOFF, HEARD NOISE AND FELT VIBRATION FROM GALLEY DOOR. AIRCRAFT RETURNED OT MSP AND LANDED WITHOUT INCIDENT. UPON MAINTENANCE INSPECTION, FOUND 8 INCHES OF WHITE RUBBER INTERIOR DOOR LINING TRIM LOOSE AND PROTRUDING FROM THE TOP OF DOOR 1R. INSPECTED AND FOUND NO DAMAGE TO AIRCRAFT. REMOVED LOOSE TRIM, OK TO CONTINUE SERVICE. 2 L 7 2 4F RT A6WE 1998042400478 19980424 00478 NE 1998 4 24 9806741154 2 19980415 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION LD LANDING 1 GL 01 154US 46763 686159 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. EGT REACHED 930C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER MAINTENANCE MANUAL AND RAN ENGINE TO TAKEOFF POWER WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE WITH THE BORESCOPE DEFERRED FOR FIVE CYCLES. 2 L 7 3 4F 4 F A22WE E20EA 1998042400479 19980424 00479 NE 1998 4 24 9806751144 2 19980415 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 144JC 46752 686138 AFTER LANDING WHILE CREW WAS ATTEMPTING TO RESTOW THE NR 3 ENGINE THRUST REVERSER, THE NR 3 ENGINE COMPRESSOR STALLED. E GT CLIMBED TO 820C AND THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER THE TAFI MANUAL WITH NO DEFECTS N OTED. THE ENGINE WAS RUN WITH NO PROBLEMS AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1998042400480 19980424 00480 NE 1998 4 24 9806761155 2 19980415 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 155US 46764 686158 WHILE CLIMBING THRU 9500 FEET, THE NR 1 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN PER COM AND THE AIRCRAFT RE TURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE PER MAINTENANCE AND TAFI MANUALS INCLUDING A BORESCOPE WITH NO TROUBLE FOUND. 2 L 7 3 4F 4 F A22WE E20EA 1998042400481 19980424 00481 NE 1998 4 24 9806779763 2 19980418 A 7321 7436024 FUEL CONTROL DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE LT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 763NW 36183 1 47396 676228 DURING CLIMB TO MAINTAIN EQUAL POWER SETTINGS, THE POWER LEVERS WERE SPLIT WITH THE LEFT FORWARD OF THE RIGHT. CREW ELE CTED TO RETURN TO DTW. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL UNIT. ENGINE OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998042400482 19980424 00482 WP 1998 4 24 9806789611 1 19980419 A 4930 SEAL DOUG DC9 DC932 3022066 WP APU LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 611NA 41621 995 47435 DURING CRUISE FLIGHT, APU OIL PRESSURE LOW LIGHT CAME ON AND APU SHUT DOWN. CROSSTIE RELAY WAS ON MEL. FLIGHT CREW RET URNED TO DEPARTURE AIRPORT. MAINTENANCE FOUND OIL LEAK AT FUEL CONTROL GARLOCK SEAL AND REPLACED SEAL. MAINTENANCE ALS O REPLACED AC BUS CONTROL PANEL. GROUND RUN AND CROSSTIE OPERATION NORMAL AND NO OIL LEAKS NOTED. 2 L 7 2 4F A6WE 1998042400483 19980424 00483 NM 1998 4 24 9806795635 1 19980414 A 2421 729825H IDG BOEING 757 757251 1384970 NM LT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 535US 18419 1629 26482 LEFT ENGINE GENERATOR DRIVE LIGHT ILLUMINATED ON TAKEOFF. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTE NANCE REPLACED THE LEFT IDG WITH A SERVICEABLE UNIT. RUN-UP AND LEAK CHECK SATISFACTORY. 2 L 7 2 4F RT A2NM 1998042400484 19980424 00484 NM 1998 4 24 9806806303 1 19980419 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AROUND ROW 31H AND DOOR 3R. RECONNECTED WIRE CONNECTOR , OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998042400485 19980424 00485 NM 1998 4 24 9806816611 1 19980419 A 2782 126344171 ACTUATOR BOEING 747 747251B 1384892 NM NR 3 LE FLAP MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 611US 69559 20556 20356 DURING CLIMB, THE NR 3 LEADING EDGE FLAP WOULD NOT RETRACT. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPL ACED THE NR 3 LEADING EDGE FLAP ACTUATOR, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998042400486 19980424 00486 WP 1998 4 24 9806829969 1 19980419 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD SECTION OF MID CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400487 19980424 00487 WP 1998 4 24 9806839969 1 19980419 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH VENTRAL STAIR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES IN POWE R SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400488 19980424 00488 WP 1998 4 24 9806849611 1 19980419 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611NA 47435 DURING LINE MAINTENANCE INSPECTION, FOUND AFT CABIN EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400489 19980424 00489 WP 1998 4 24 9806859882 1 19980419 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670MC 47659 DURING LINE CHECK, FOUND LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTER IES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042400490 19980424 00490 WP 1998 4 24 9806869880 1 19980418 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675MC 47651 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS AT SEAT ROWS 21 AND 23 INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK , OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042400491 19980424 00491 WP 1998 4 24 9806879311 1 19980419 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 314RC 49110 DURING LINE CHECK, FOUND BOTH AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400492 19980424 00492 EA 1998 4 24 COMA9860084 1 19980420 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 957CA 10813 5080 7109 FLAPS FAILED AT 30 DEGREES. REPLACED THE LEFT HAND FLAP BPSU. 2 L 7 2 4F RT A21EA 1998042400493 19980424 00493 NM 1998 4 24 SWAA980619 1 19980415 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 294/986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294.5, 986.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400494 19980424 00494 NM 1998 4 24 SWAA980620 1 19980415 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 332.1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND ANGLE CRACKED AT BS 332.1 AT S8R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400495 19980424 00495 NM 1998 4 24 SWAA980621 1 19980415 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT RBL 4.7, WL 200.5 TO 201.25. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400496 19980424 00496 NM 1998 4 24 SWAA980622 1 19980415 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT RBL 4.7, WL 198 198.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400497 19980424 00497 NM 1998 4 24 SWAA980623 1 19980415 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT LBL 6.7, WL 211.5 TO 213.25. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400498 19980424 00498 NM 1998 4 24 SWAA980624 1 19980415 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND BULKHEAD 178 CRACKED AT LBL 4.7, WL 198 TO 198.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400499 19980424 00499 NM 1998 4 24 SWAA980625 1 19980415 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 400 AND S27L, AND AT BS 663.75. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400500 19980424 00500 NM 1998 4 24 SWAA980626 1 19980415 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND RT CHORD CRACKED AT BS 178, WL 207, RBL 29 AND LBL 29. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400501 19980424 00501 NM 1998 4 24 SWAA980627 1 19980415 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400/747/867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 400, 747, AND 867. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042400502 19980424 00502 NM 1998 4 24 SWAA980628 1 19980415 A 2910 HYD SYST BOEING 737 7373H4 1384600 NM A-HYD SYST OVERSERVICED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 647SW 27717 ON TAKEOFF, CREW NOTED A RUBBER TYPE BURN SMELL COMING THROUGH DUCT SYSTEM. NO VISIBLE SMOKE. ODOR DISSIPATED AT LOWER THRUST SETTING. AIRCRAFT RETURNED TO MDW AND MADE AN UNEVENTFUL LANDING. INSPECTED AIRCRAFT, FOUND A SYSTEM HYD RESER VOIR OVERSERVICED. DESERVICED TO PROPER LEVEL AND PERFORMED ENGINE POWER ASSURANCE RUN PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042400503 19980424 00503 NM 1998 4 24 SWAA980629 1 19980415 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED 1/4 D-CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED BELOW S15R AT BS 291.5. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042400504 19980424 00504 NM 1998 4 24 SWAA980630 1 19980415 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED 1/4 D-CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED ABOVE S12R AT BS 295. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042400505 19980424 00505 NM 1998 4 24 SWAA980631 1 19980414 A 3350 P4010021 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355SW 25250 DURING PREFLIGHT CHECK, FOUND FWD EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042400506 19980424 00506 NM 1998 4 24 SWAA980632 1 19980415 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727, S6R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042400507 19980424 00507 EU 1998 4 24 WWMA9800076 1 19980418 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 261AE 340B261 FLIGHT ATTENTANTS EMERGENCY LIGHT ARM LIGHT INOP. RELAMPED. 2 L 7 2 4T RT A52EU 1998042400508 19980424 00508 NM 1998 4 24 QXEA9800533 1 19980419 A 3350 10005511 LIGHT DHAV 82510202001 DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTION A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 830PH 16113 2562 05000IN 314 COCKPIT EMERGENCY LIGHT INOP OVER JUMPSEAT. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042400509 19980424 00509 NM 1998 4 24 QXEA9800534 1 19980417 A 3231 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 814PH 43 LEFT MAIN FORWARD GEAR DOOR REMAINS OPEN AFTER TAKEOFF. GEAR WAS CYCLED, AND THE DOOR CLOSED. INSPECTED FORWARD GEAR D OOR ACTUATION MECHANISM, NO DEFECTS NOTED. CLEANED BOTH RESTRICTORS AT THE FORWARD GEAR DOOR ACTUATOR, OPERATIONAL CHEC KS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998042400510 19980424 00510 EU 1998 4 24 QXEA9800535 1 19980417 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 EMERGENCY LIGHT ON OVERHEAD AISLE AT ROW 1 INOP. RELAMPED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998042400511 19980424 00511 EU 1998 4 24 QXEA9800536 1 19980417 A 3350 5515900004 SIGN GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 EMERGENCY EXIT SIGN ON SIDE WALL AT ROW 9 INOP. REPLACED SIGN, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998042400512 19980424 00512 EU 1998 4 24 QXEA9800537 1 19980417 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 484US 11234 SEAT LIGHTING ON ROWS 11, 12, AND 14 GO ON AND OFF INTERMITTENTLY DURING TAXI AND FLIGHT. TIGHTENED CONNECTION AT ROW 9 AB, OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998042400513 19980424 00513 EU 1998 4 24 QXEA9800538 1 19980417 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 484US 11234 SEAT MOUNTED FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS ON THE LAST 4 SEAT ROWS ARE INTERMITTANTLY ON. FOUND 2 BROKEN WIRES UNDER ROW 11. REPAIRED WIRING. OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998042400514 19980424 00514 NM 1998 4 24 98UAL900075 1 19980219 A 8011 505422 BEARING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE STARTER DRIVE FAILED A A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 29 7260U 5909 21407 NR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE INDICATED ZERO. SHUT DOWN ENGINE AND DIVERTED TO OMA. *S/D * THE STARTER DRIVE BALL BEARING CAGE FAILED. ONE BALL WAS INGESTED INTO THE MAIN OIL PUMP RESULTING IN A SHEARED SHAF T AND ZERO OIL PRESSURE. BEARING THRESHOLD LIMITS HAVE BEEN IMPLEMENTED TO PREVENT SUCH FAILURES IN THE FUTURE. 2 L 7 3 4F 4 F A3WE E2EA 1998042400515 19980424 00515 NM 1998 4 24 98UAL900142 1 19980411 A 3230 FUSE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT MLG BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 611UA 21872 RIGHT MAIN LANDING GEAR FAILED TO RETRACT. RECYCLED, GEAR RETRACTED BUT LANDING GEAR DOOR REMAINED OPEN. GEAR DISAGREE LIGHT ILLUMINATED. RETURNED TO FIELD. *S/D* FOUND RT MLG TRUCK POSITIONING FLOW FUSE BROKEN AND WOULD NOT RESET. RE PLACED FUSE. 2 L 7 2 4F 4 F RT A1NM E3NE 1998042400516 19980424 00516 NM 1998 4 24 98UAL900143 1 19980412 A 2613 SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING/BODY OUT OF POSITION A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 351UA 24319 RIGHT WING BODY OVERHEAT DETECTION SYSTEM LIGHT ON. *S/D* SENSOR IN PYLON WAS IN CLOSE PROXIMITY TO DUCT. REPOSITIONE D SENSOR AND RAN THE ENGINE AT POWER FOR TWENTY MINUTES WITH NO INDICATIONS, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998042400517 19980424 00517 NM 1998 4 24 98UAL900145 1 19980401 A 3610 8102081 HEAT EXCHANGER BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT PACK FAILED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 766UA 26917 L BLEED PRSOV SHOWS CLOSED ON AIR SUPPLY MAIN T, BLEED LOSS WING L, BODY L, BLEED LEAK L STATUS MSG'S AND L PACK INOP. C REW HEARD POP JUST BEFORE MESSAGES APPEARED. RETURNED TO IAD AND LANDED OVERWEIGHT. *S/D* FOUND LT HEAT EXCHANGER TOR N OPEN AT PRIMARY INLET DUCT SEAM WELD. REPLACED LT HEAT EXCHANGER PART NUMBER 810208-1. UNDER INVESTIGATION BY THE MA NUFACTURER. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998042400518 19980424 00518 NM 1998 4 24 98UAL900146 1 19980317 A 5321 173821 FLOOR BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GALLEY CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 777UA 26916 FOUND MID GALLEY FLOOR PANELS (REF IPC 25-31-01-075) WHICH HAD HEAVY CORROSION ON THE AFT EDGE OF THE FORWARD PANEL AND THE FORWARD EDGE OF THE REAR PANEL. THERE WAS NO SEALANT BETWEEN THE THRESHOLD PLATE AND THE GALLEY FLOOR PAN. THIS CO NDITION ALLOWED MOISTURE TO BE TRAPPED BETWEEN THE THRESHOLD PLATE AND THE FOOD CART RAMP AREA OF THE PALLET CAUSING COR ROSION. INTERIM REPAIRED PER EVA MOC1-7614. PALLET AND THRESHOLD PLATE TO BE REPLACED AT NEXT 'C' CHECK. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998042400519 19980424 00519 NM 1998 4 24 98UAL900147 1 19980412 A 3397 58782 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7257U 21404 EEL FLOOR LIGHTS INOP ROW 19 TO 26. *S/D* REPLACED POWER STRIP. 2 L 7 3 4F 4 F A3WE E2EA 1998042400520 19980424 00520 NM 1998 4 24 98UAL900148 1 19980413 A 3232 1U11935 ACTUATOR BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE MLG DOOR MALFUNCTIONED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 165UA 21658 AFTER GEAR RETRACTION AND PLACING THE GEAR HANDLE IN THE OFF POSITION THE RIGHT BODY DOOR LIGHT CAME ON, BOTH PRI AND AL T. NECESSARY TO RECYCLE GEAR TO PUT LIGHT OUT. *S/D* FOUND LEVER LOCK CONTACTING RELEASE CAM. CONTACT PREVENTED INTE RNAL LOCK FROM ACTUATING. REPLACED BODY GEAR DOOR ACTUATOR PER MM 32-33-27. ADJUSTED TO PROVIDE CLEARANCE. 2 L 7 4 4F 4 F A20WE E20EA 1998042400521 19980424 00521 1998 4 24 98UAL900149 4 19980414 A 2565 TUBE AIR CRUISERS 62772292 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SLIDE/RAFT TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 770UA 0018 26925 DURING SHOP OVERHAUL, THE SLIDE/RAFT DEVELOPED A TWO INCH TEAR IN THE LOWER TUBE UNDER THE GIRT AFTER THE FLAT FIRE TEST . SLIDE/RAFT SENT TO VENDOR FOR WARRANTY REPAIR. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998042400522 19980424 00522 NM 1998 4 24 98UAL900150 1 19980416 A 3350 BULB BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 506UA 24627 EMERGENCY SLIDE LIGHT INOP, DOOR 4L. LAMP BURNED OUT. REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998042400523 19980424 00523 WP 1998 4 24 ABXA9800361 1 19980420 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC933F 302207A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 930AX 47363 COCKPIT EMERGENCY LIGHTS WERE DIM. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998042400524 19980424 00524 WP 1998 4 24 ABXA9800362 1 19980420 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 965AX 47498 EMERGENCY LIGHTS WERE WEAK. REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998042400525 19980424 00525 1998 4 24 ABXA9800363 4 19980416 A 3421 36143091006 EADI DOUG DC8 DC863 302198A WP COCKPIT DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 820AX 5500 46155 FIRST OFFICER'S EADI FAILED. DISPLAY UNIT WENT BLANK, ELECTRICAL SMELL/FUMES WERE NOTED IN THE COCKPIT. REPLACED FIRST OFFICER'S EADI IAW DC8 MM 34-21-0, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998042400526 19980424 00526 WP 1998 4 24 ABXA9800364 1 19980417 A 2110 5614845517 TURBOCOMPRESSOR DOUG DC8 DC861 3021952 WP NR 1 DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 844AX 5952 45848 NR 1 CTC DEVELOPED LOUD SQUEALING NOISE WITH METALLIC SMELL FROM AIR DUCTS INTO COCKPIT. REPLACED NR 1 CTC IAW DC8 MM 2 1-10-1, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998042400527 19980424 00527 WP 1998 4 24 ABXA9800365 1 19980417 A 2110 5614845517 TURBOCOMPRESSOR DOUG DC8 DC863 302198A WP NR 1 DEFECTIVE A ABXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 824AX 55689 46141 NR 1 CTC BEARING FAILED. LOUD SQUEALING NOISE, VIBRATION AND BURNING SMELL IN COCKPIT. REPLACED NR 1 CTC IAW DC8 MM 21 -10-1, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998042400528 19980424 00528 WP 1998 4 24 MWEA98486 1 19980417 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 502ME 48132 THE GALLEY DOOR EMERGENCY DOOR SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998042400529 19980424 00529 WP 1998 4 24 MWEA98487 1 19980417 A 2560 591769037 DOOR SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 209ME 47730 THE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1998042400530 19980424 00530 WP 1998 4 24 MWEA98488 1 19980420 A 5512 5912481 PLATE DOUG DC9 DC932 3022066 WP HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 HORIZONTAL STABILIZE STRESSED PLATE SHOWS EVIDENCE OF CORROSION AND CHAFING. REMOVED OLD PLATE AND INSTALLED FABRICATED REPLACEMENT. 2 L 7 2 4F A6WE 1998042400531 19980424 00531 WP 1998 4 24 MWEA98489 1 19980420 A 5400 99581399 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT PYLON VERTICAL STIFFENER CRACKED FORWARD INBOARD CORNER OF ELECTRICAL CONNECTOR PANEL. MTC REMOVED CRACKED ANGLE F ABRICATED AND INSTALLED REPLACEMENT ANGLE. 2 L 7 2 4F A6WE 1998042400532 19980424 00532 WP 1998 4 24 MWEA98490 1 19980420 A 5313 5911415 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 3 RIGHT HAS A SECTION TRIMMED OFF BY UPPER ANTI COLLISION LIGHT MOUNT. MTC REMOVED DAMAGED SECTION OF LONGERON FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION. 2 L 7 2 4F A6WE 1998042400533 19980424 00533 WP 1998 4 24 MWEA98491 1 19980420 A 5313 5911415 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 2 RIGHT HAS A SECTION TRIMMED OFF BY UPPER ANTI COLLISION MOUNT. MTC REMOVED DAMAGED SECTION OF LONGERON FABRI CATED AND INSTALLED REPLACEMENT LONGERON SECTION. 2 L 7 2 4F A6WE 1998042400534 19980424 00534 WP 1998 4 24 MWEA98492 1 19980420 A 5711 5911301501 SPAR DOUG DC9 DC932 3022066 WP WS 360 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LT WING STATION XRS 360 LOWER AFT SPAR HAS INTERGRANULAR CORROSION ON UPPER SIDE OF LOWER SPAR CAP. MTC REMOVED CORROSI ON AND REPAIRED SPAR USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400535 19980424 00535 WP 1998 4 24 MWEA98493 1 19980420 A 5712 99193533 RIB DOUG DC9 DC932 3022066 WP WS 164 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LOWER CAP ON THE WING RIB AT STATION XRS 164. MTC REMOVED CORROSION AND INSTALLED REPAIR STRAP TO THE LOWER CAP. 2 L 7 2 4F A6WE 1998042400536 19980424 00536 WP 1998 4 24 MWEA98494 1 19980420 A 5712 9919314 RIB DOUG DC9 DC932 3022066 WP WS 481 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEADING EDGE RIB AT STATION XRS 481 ON LEFT WING WAS FOUND DEEPLY GOUGED. MTC REMOVED AND REPLACED SUPPORT RIB ON LEADI NG EDGE. 2 L 7 2 4F A6WE 1998042400537 19980424 00537 WP 1998 4 24 MWEA98495 1 19980420 A 5754 9919449 SKIN DOUG DC9 DC932 3022066 WP NR 4 LE SLAT TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RT NR 4 SLAT HAS TORN METAL SKIN AT FASTENER HOLES ON THE OUTBOARD EDGE. MTC REPAIRED SKIN USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400538 19980424 00538 WP 1998 4 24 MWEA98496 1 19980420 A 5711 599191532 SPAR CAP DOUG DC9 DC932 3022066 WP WS 200 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING LEADING EDGE STATION 200 FORWARD SPAR LOWER CAP HAS A PREVIOUS REPAIR ON THE FORWARD SIDE OF THE CAP. REMOVE D PREVIOUS REPAIR BLENDED CORROSION INSTALLED REPAIR STRAPS USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400539 19980424 00539 WP 1998 4 24 MWEA98497 1 19980420 A 5711 59191532 SPAR CAP DOUG DC9 DC932 3022066 WP WS 330 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING LEADING EDGE STATION 330 FORWARD LOWER SPAR HAS CORROSION. MTC REMOVED CORROSION AND INSTALLED REPAIR STRAP USING APPROVED DATA. 2 L 7 2 4F A6WE 1998042400540 19980424 00540 WP 1998 4 24 MWEA98498 1 19980420 A 5712 99193534 RIB DOUG DC9 DC932 3022066 WP WS 164 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION FOUND ON WING RIB AT STATION XRS 164 RT WING UPPER SURFACE OF LOWER RIB CAP. MTC BLENDED AREA AND INSTALLED STRAP REPAIR. 2 L 7 2 4F A6WE 1998042400541 19980424 00541 WP 1998 4 24 MWEA98499 1 19980420 A 5720 4911462 CLIP DOUG DC9 DC932 3022066 WP WS 137 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION ON THE LOWER OUTBOARD RIB ATTACH CLIP AT XRS 137 BETWEEN STRINGER 11 AND LOWER CHORD LT WING. MTC REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 1998042400542 19980424 00542 WP 1998 4 24 MWEA98500 1 19980420 A 5720 91200751H BRACKET DOUG DC9 DC932 3022066 WP WS 111.5 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 ANGLE BRACKET HAS A CRACK NEAR STRINGER 1 CONNECTING TO REAR SPAR AT XRS 111.5 LEFT WING. MTC REMOVED AND REPLACED BRAC KET. 2 L 7 2 4F A6WE 1998042400543 19980424 00543 WP 1998 4 24 ARWA980407 1 19980420 A 2910 1140450600 HYD LINE DOUG DC8 DC862 3021970 WP NR 4 LEAKING A ARWA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 19 1804 45896 LOST HYDRAULIC FLUID TO STAND PIPE LEVEL, HYDRAULIC LOSS OF FLUID, EMERGENCY CHECKLIST WAS PERFORMED. PRESSURE CHECK OK . ABNORMAL CHECKLIST WAS FOLLOWED TO AND BEFORE LANDING CHECKS. LANDING AND ROLL-OUT WERE UNEVENTFUL. PRECAUTIONARY A /C TOW IN WAS REQUESTED AFTER CLEARING RUNWAY. FLAPS WERE MAINTAINED AT LANDING CONFIGURATION TO AVOID FURTHER LOSS OF FLUID. AFTER MECHANICS CHECKED FOR LEAKS IT APPEARED LIKE FLEX HYDRAULIC LINE (NR 4) HAD SPLIT OPEN AT THE RUDDER PUMP LOCATION. REMOVED AND REPLACED LINE, RAN NR 2 AND 3 ENGINES AND CYCLED ALL SYSTEMS THROUGH SEVERAL TIMES TO BLEED AIROU T SERVICED HYD QTY. AS REQUIRED, NO LEAKS NOTED AT THIS TIME, IAW DC-8 MM 27-20-02. 2 L 7 4 4F 4A25 1998042400544 19980424 00544 WP 1998 4 24 ARWA980408 1 19980419 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 640 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 ON PREFLIGHT, FOUND EVIDENCE OF CORROSION AT APPROXIMATELY FS 640 L 33R AND 34R. REMOVED CORROSION, FOUND BEYOND LIMITS IAW SRM 53-2-0. REFER TO DOUGLAS MESSAGE MISC 546/JCT. 2 L 7 4 4F 4A25 1998042400545 19980424 00545 WP 1998 4 24 ASAA9880043 1 19980308 A 5610 MECHANISM DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 SFO - PRIOR TO DEPARTURE OF FLT 349, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. LUBRICATE D THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998042400546 19980424 00546 WP 1998 4 24 ASAA9880044 1 19980308 A 5610 MECHANISM DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 SEA - AFTER ARRIVAL OF FLT 349, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED THE F LIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998042400547 19980424 00547 WP 1998 4 24 ASAA9880045 1 19980308 A 5610 MECHANISM DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 SEAT - PRIOR TO DEPARTURE OF FLT, 539, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WAS DIFFICULT TO OPEN. A DJUSTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998042400548 19980424 00548 EU 1998 4 24 ASOA98022 1 19980305 A 3350 CONNECTOR AEROSP ATR72 ATR72212 EU CABIN LOOSE A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 631AS 362 EXTERIOR EMERGENCY LIGHT AT SERVICE DOOR THAT ILLUMINATES EXIT AREA INOPERATIVE. ATL MAINTENANCE RESEATED CANNON PLUG O N LIGHT POWER SUPPLY. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400550 19980424 00550 EU 1998 4 24 VTZA98119 1 19980307 A 5270 JE5 SWITCH BAG JETSTM JETSTM3201 1500217 EU PASSENGER DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 489UE 908 IAD/ROC - FLT 6452 - DURING CRUISE AT 1430 HOURS ON 3-7-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR W ARNING LIGHT ILLUMINATED. AIRCRAFT LANDED AT IAD AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBED PASSENGER DOOR HANDLE MECHANISM AND MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998042400551 19980424 00551 EU 1998 4 24 VTZA98111 1 19980309 A 3060 ES3023 PROP TEST BOX JETAIR JETSTM JETSTM4101 1500501 EU RT PROP FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 324UE 41017 FLT 6500 - IAD-LGA - TAKEOFF ABORTED DUE TO RT PROP DE-ICE FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED PROP TEST BOX, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RET URN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400552 19980424 00552 WP 1998 4 24 VTZA98122 2 19980309 A 7200 310349016 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 314UE 41027 P76099 FLT 6199 - BDL-IAD - AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RE TURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ENGINE, AND GROUND RAN AIRCRAFT . OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E4WE 1998042400553 19980424 00553 1998 4 24 VTZA98124 4 19980310 A 3425 7003110901 EADI JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 310UE 41028 FLT 6214 - IAD-ORF - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO FO'S EADI SCREEN WENT BLANK. MAINTENANCE INSPECTED A ND REMOVED AND REPLACED EADI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400554 19980424 00554 1998 4 24 VTZA98125 3 19980310 A 6140 8659566 PRESS SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 370MT 800 FLT 6151 - IAD-PHF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO RT BETA WARNIGN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT PRESSURE SWITCH . OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400555 19980424 00555 EU 1998 4 24 VTZA98120 1 19980308 A 3240 S214149 PRESS IND BAG JETSTM JETSTM3201 1500217 EU LT BRAKE FAILED A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 490UE 909 FLT 6564 - GSO-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LEFT BRAKE PRESS URE GAUGE INDICATED 200 PSI WITH NO PRESSURE APPLIED, AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTE NANCE INSPECTED AND OPENED DMI 55808, MEL 32-1 ON GAUGE. MAINTENANCE CLOSED DMI 55808 ON 3-9-98 BY REMOVING AND REPLACI NG GAUGE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400556 19980424 00556 EU 1998 4 24 VTZA98121 1 19980308 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 309UE 41022 FLT 903 - IAD-RIC - AIRCRAFT ABORTED TAKEOFF DUE TO BAGGAGE DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETUEND TO GATE WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 51989, MEL 52-3. MAINTENANCE CLOSED DMI 51989 ON 3-9-98 B Y ADJUSTING MICROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400557 19980424 00557 EU 1998 4 24 VTZA98127 1 19980311 A 3260 ATG135704 DOWNLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NLG DIRTY A VTZA O OTHER N FALSE WARNING LD LANDING 1 EA 27 324UE 41017 FLT 6267 - IAD-BTV - DURING LANDING, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS NLG UNSAFE LIGHT (RED LIGHT) STAYED ON WHEN GEAR EXTENDED. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE I NSPECTED AND CLEANED NOSE GEAR DOWNLOCK MICROSWITCH AND PERFORMED GEAR SWING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400558 19980424 00558 EU 1998 4 24 VTZA98098 1 19980227 A 7722 6100144A INDICATOR BAG JETSTM JETSTM3201 1500217 EU LT ENG EGT FAILURE A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 493UE 805 FLT 6272 - IAD-BUF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT EGT GAUGE FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EGT INDICATOR, OPS CHECK OK. AIRCRAF T WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400559 19980424 00559 1998 4 24 VTZA98118 4 19980308 A 3445 066500012704 TCAS BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 494UE 810 FLT 6377 - IAD-CRW - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO VIS SCREEN WENT BLANK. MAINTENANCE INSPECTED AND REM OVED AND REPLACED TCAS/VSI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400560 19980424 00560 EU 1998 4 24 VTZA98117 1 19980308 A 5270 JE5 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 489UE 908 FLT 6357 - IAD-RDU - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED . AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBED LOWER MICROSWITCH. O PS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400561 19980424 00561 1998 4 24 VTZA98116 4 19980308 A 3425 4020531574 ADI BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 474UE 849 FLT 6312 - IAD-JFK - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO LEFT ADI WOULD NOT COME ON LINE. MAINTENANCE INSPECT ED AND REMOVED AND REPLACED ADI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400562 19980424 00562 EU 1998 4 24 VTZA98115 1 19980308 A 2913 PV304426 PUMP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 475UE 850 FLT 6330 - IAD-PIT - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO RIGHT HYDRAULIC PUMP PRESSURE DROPPED TO ZERO. MAINT ENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PUMP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400563 19980424 00563 1998 4 24 VTZA98114 4 19980308 A 3442 6224022001 RT UNIT BAG JETSTM JETSTM3201 1500217 EU FWD FUSELAGE FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 471UE 821 FLT 6379 - IAD-SYR - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO WEATHER RADAR WENT INOP DURING TAXI. MAINTENANCE INS PECTED AND REMOVED AND REPLACED RADAR RT AND RADAR SCREEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400564 19980424 00564 1998 4 24 98ZZZM445 4 19980308 A 3442 6225941001 INDICATOR BAG JETSTM JETSTM3201 1500217 EU FUSELAGE FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 471UE 821 FLT 6379 - IAD-SYR - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO WEATHER RADAR WENT INOP DURING TAXI. MAINTENANCE INS PECTED AND REMOVED AND REPLACED RADAR RT AND RADAR SCREEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400565 19980424 00565 EU 1998 4 24 VTZA98113 1 19980308 A 6120 31058993 NTS TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 310UE 41028 FLT 6416 - IAD-CHS - AIRCRAFT ABORTED TAKEOFF DUE TO GREEN APR ARM WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NTS TRANSDUCER, AND GROUND RAN AIRCRAFT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400566 19980424 00566 EU 1998 4 24 VTZA98112 1 19980309 A 2611 7211121100 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE COMPT FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 325UE 41063 FLT 6371 - EWR-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO BAGGAGE BAY SMOKE DETECTOR INOP, WOULD NOT TEST. AIR CRAFT WAS FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND REMOVED AND REPLACED SMOKE DETECTOR, OPS CHECK OK. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400567 19980424 00567 EA 1998 4 24 VTZA98133 1 19980312 A 2611 PU90421R3 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA LAVATORY FAILED A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 623BR 7192 FLT 6718 - ATL-IAD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LAV SMOKE WARNIGN LIGHT ILLUMINATED. A IRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FERRIED AIRCRAFT TO IAD WHERE MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998042400568 19980424 00568 EA 1998 4 24 VTZA98132 1 19980312 A 2170 7536893 FILTERS CNDAIR CL600 CL6002B19 EA CABIN DIRTY A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 623BR 7192 FLT 6693 - IAD-JAX - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LAV SMOKE WARNING LIGHT ILLUMINATED. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED ACM'S COALESAR BAGS AND DUCTING FOR EVIDENCE OF OIL AND REMOVED AND REPLACED ACM WATER FILTERS. MAINTENANCE GROUND RAN AIRCRAFT OPS CHECK OK. AIRCRAFT WAS RELEASED AN D APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998042400569 19980424 00569 EU 1998 4 24 VTZA98131 1 19980311 A 3250 190600 CONTROL CABLE JETAIR JETSTM JETSTM4101 1500501 EU NLG STEERING FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 301UE 41012 FLT 6225 - IAD-BOS - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO NOSE WHEEL STEERING INOP. MAINTENANCE INSPECTED AND REMOVED AND REPLACED STEERING CABLE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400570 19980424 00570 EU 1998 4 24 VTZA98130 1 19980313 A 2497 XB157 WIRE BAG JETSTM JETSTM3201 1500217 EU TERMINAL BLOCK LOOSE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 475UE 850 FLT 6350 - IAD-EWR - AIRCRAFT ABORTED TAKEOFF DUE TO LT RED INVERTER AND RT AC MAIN CAPTION WARNING LIGHT ILLUMINATED. A IRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPAIRED WIRE NEAR TERMINAL BLOCK T2BC, OP S CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400571 19980424 00571 EU 1998 4 24 VTZA98129 1 19980313 A 2422 IR3501B12 STATIC INVERTER BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 475UE 850 FLT 6350 - IAD-EWR - ABORTED TAKEOFF DUE TO LEFT RED INVERTER AND RT AC MAIN CAPTION WARNIGN LIGHT ILLUMINATED. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT STATIC INVERTER, OPS CHE CK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400572 19980424 00572 EU 1998 4 24 VTZA98128 1 19980313 A 3244 TIRE BAG JETSTM JETSTM3201 1500217 EU NLG REQ'D SERVICE A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 490UE 909 FLT 6564 - GSO-IAD - ABORTED TAKEOFF DUE TO EXTREME PULL TO LEFT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. M AINTENANCE INSPECTED AND SERVICED NOSE TIRE AND PERFORMED HIGH SPEED TAXI. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042400573 19980424 00573 EU 1998 4 24 VTZA98134 4 19980313 A 3160 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 331UE 41099 FLT 6625 - IAD-ILM - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE FO'S RMU FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 2 SYMBOL GENERATOR, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998042400574 19980424 00574 EU 1998 4 24 VTZA98135 1 19980318 A 3060 666000218 BRUSH BLOCK BAG JETSTM JETSTM3101 1500215 EU LT PROP FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 473UE 828 FLT 6261 - IAD-EWR - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT PROP HEAT FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT PROP BRUSH BLOCK, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998042400575 19980424 00575 EU 1998 4 24 VTZA98136 1 19980318 A 3350 6047051 POWER SUPPLY JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 319UE 41042 DURING MAINTENANCE INSPECTION, AIRCRAFT HAD ONE DISCREPANCY WHICH WAS THE EMERGENCY TRACK LIGHTING WAS INOP. MAINTENANC E REMOVED AND REPLACED THREE POWER SUPPLIED. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A41NM 1998042400577 19980424 00577 NM 1998 4 24 TWAA9804013 1 19980216 A 5311 FRAME BOEING 727 727231 1384079 NM BS 783.95 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54344 21631 JFK - DURING C-CHECK, FOND CRACK INDICATION ON LEFT FRAME AT BS 783.95, FIRST HOLE ABOVE FLOORBEAM. REAMED HOLE TO .312 BUT CRACK INDICATION STILL EXISTED. STOP DRILLED CRACK PER 51-10-01 AND INSTALLED DOUBLERS PER MO 71T68-C AND SERVICE BULLETIN 727-53-0197. (M) 2 L 7 3 4F A3WE 1998042400578 19980424 00578 NM 1998 4 24 TWAA9804012 1 19980227 A 5330 SKIN BOEING 727 727231 1384079 NM PAX DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 84357 21989 MCI - DURNG C-CHECK, FOUND CRACK IN FUSELAGE SKIN 1.125 INCH LONG GOING FORWARD FROM BOTTOM HINGE POCKET FOR FWD MAIN EN TRY DOOR. CONFIRMED WITH HIGH FREQ EDDY CURRENT. REPAIRED PER SRM 53-10-219 FIG 202, TWA STD PRACTICES, AND SERVICE BU LLETIN 727-53-1098, ADDED STAINLESS DOUBLER. (M) 2 L 7 3 4F A3WE 1998042400580 19980424 00580 EU 1998 4 24 AALA980446 1 19980306 A 5320 SILL AIRBUS 300 A300B4605R 3930308 EU CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - FOUND CORROSION ON FORWARD AND LOWER DOOR SILL BULK CARGO DOOR CUTOUT. REMOVED AND REPLACED LOWER FORWARD DOOR ST RAP PER SRM 53-13-13 PAGE 202. (M) 2 L 7 2 4F RT A35EU 1998042400581 19980424 00581 EU 1998 4 24 AALA980445 1 19980305 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - DURING C-CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT NR 9 BETWEEN FRAMES NR 13 AND NR 15 TWO FEET INBOARD OF R1 DOOR. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-10, AND SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998042400582 19980424 00582 EU 1998 4 24 AALA980462 1 19980307 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRINGER SPLICE AND STRINGER 51L FORWARD SIDE OF FRAME 65 HAS CORROSION. REMOVED AND REPLACED STRINGER END SPLICE WITH NEW PART PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998042400583 19980424 00583 EU 1998 4 24 AALA980461 1 19980307 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 1938-4040 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 55RT BETWEEN FRAME 59 TO FRAME 61. FABRICATED AND DRILLED SPLICE PIECES (DOUBLER) AND INSTALLED PER SRM 53-10-14-2 TREATED PRIMED AND PAINTED. (M) 2 L 7 2 4F RT A35EU 1998042400584 19980424 00584 EU 1998 4 24 AALA980460 1 19980306 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - STRINGER 56 RT HAS CORROSION LOWER FLANGE AROUND FASTENER. REMOVED CORROSION, INSTALLED SPLICES PER SRM 53-10-14- 2. (M) 2 L 7 2 4F RT A35EU 1998042400585 19980424 00585 EU 1998 4 24 AALA980466 1 19980306 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - NR 7 SEAT TRACK CORRODED BETWEEN FRAME 15 AND 16. NR 7 SEAT TRACK CORRODED BETWEEN FRAME 16 AND 16A. REPLACED NR 7 SEAT TRACK FROM FRAME 15A TO FRAME 19 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998042400586 19980424 00586 EU 1998 4 24 AALA980465 1 19980306 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - DURING C-CHECK, FOUND GOUGE IN NR 8 SEAT TRACK AT FRAME NR 31 IN FORWARD CABIN. BLENDED OUT DAMAGED AREA AND REPA IRED PER ESO 30595 DATED 3-4-98. (M) 2 L 7 2 4F RT A35EU 1998042400587 19980424 00587 EU 1998 4 24 AALA980464 1 19980307 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - R-4 DOOR FLOORBOARD SUPPORT INBOARD CORNER EXFOLIATED AROUND FASTENER HOLE BETWEEN FRAMES 75 AND 76 AS VIEWED FROM BOTTOM. REPLACED FLOORBOARD SUPPORT BETWEEN FRAME 75 AND 76 PR SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998042400588 19980424 00588 EU 1998 4 24 AALA980463 1 19980307 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRINGER SPLICE 51L FORWARD OF FRAME 65 HAS CORROSION. REMOVED AND REPLACED STRINGER SPLICE 51L PER SRM 51- 72-10-0. (M) 2 L 7 2 4F RT A35EU 1998042400589 19980424 00589 EU 1998 4 24 AALA980473 1 19980309 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOND CORROSION NR 10 SEAT TRACK BETWEEN FRAME 27 AND 28. INSTALLED NEW SEAT TRACK PER AARD 51-10-00-3 AND 51-20-0 0-1 AND SRM 51-10-00-0 AND 53-10-16-2 AND 51-10-00-1 AND 51-22-00. (M) 2 L 7 2 4F RT A35EU 1998042400590 19980424 00590 EU 1998 4 24 AALA980481 1 19980309 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION UNDER LAV 'M' SUPPORT, CENTER BEAM AT FRAME 31 AND 32. REPLACED CORRODED SEAT TRACK STRUCTURE PER SRM 51-10-00-0, 53-10-16-2, 53-10-00-1, 51-22-00. (M) 2 L 7 2 4F RT A35EU 1998042400591 19980424 00591 EU 1998 4 24 AALA980486 1 19980310 A 5320 END CAP AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 57 END CAP BETWEEN FRAME 65 AND 66. REMOVED AND REPLACED STRINGER END CAP PER SRM 51- 72-20. (M) 2 L 7 2 4F RT A35EU 1998042400592 19980424 00592 EU 1998 4 24 AALA980487 1 19980310 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON FLOORBEAM AT FRAME 58 UNDER NR 3 AND NR 4 ROLLER TRAYS. SPLICE IN NEW SECTION OF FLOORBEAM PER SRM 53-10-15-2. (M) 2 L 7 2 4F RT A35EU 1998042400593 19980424 00593 EU 1998 4 24 AALA980488 1 19980310 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND SEAT TRACK NR 3 BETWEEN FRAME 31 AND 32 HAS DEEP CORROSION. INSTALLED NEW SEAT TRACK FROM FRAME 25 - FRAME 33 PER AARD 51-10-00-3 AND 51-70-00-1 AND 51-40-00-1 AND SRM 51-21-20 AND 51-22-00 AND 51-24-00 AND 51-72-10-0 AND 51-40 -30 AND 53-10-16-2. (M) 2 L 7 2 4F RT A35EU 1998042400594 19980424 00594 EU 1998 4 24 AALA980485 1 19980310 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - FOUND CORROSION ON SEAT TRACK 6 INCH AFT OF FRAME 15A, 18 INCHES RT OF CENTER LINE. REPAIRED PER ESO30595, DATED 3-9-98, INSTALLED STAINLESS STRAP. (M) 2 L 7 2 4F RT A35EU 1998042400595 19980424 00595 EU 1998 4 24 AALA980484 1 19980310 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 1163-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - DURING C-CHECK, FOUND CORROSION ON NR 6 FLOOR SUPPORT AT FRAME 15 IN FORWARD CABIN. REMOVED CORROSION AND INSTALL ED REPAIR STRAPS PER AARD 53-20-00-2 AND ESO 30595 DATED 3-9-98. (M) 2 L 7 2 4F RT A35EU 1998042400596 19980424 00596 EU 1998 4 24 AALA980483 1 19980310 A 5347 FLOOR TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1153-1163 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - DURING C-CHECK, FOUND CORROSION FLOOR TRACK NR 4 AT FRAME 14 IN FORWARD CABIN. REMOVED CORROSION AND INSTALLED RE PAIR STRAPS PER AARD 53-20-00-2 AND ESO 30595, DATED 3-9-98. (M) 2 L 7 2 4F RT A35EU 1998042400597 19980424 00597 NM 1998 4 24 AALA980468 1 19980309 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 TUL - FRAME SHEER TIE CORRODED BEHIND THE SHEER CLIP (FWD SIDE OF FRAME). INST ALLED BELTFRAME REPAIR PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998042400598 19980424 00598 NM 1998 4 24 AALA980469 1 19980309 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 TUL - STATION 1148, STRINGER 29R, SHEER TIE CORRODED AFT SIDE OF FRAME. REMOVED AND REPLACED SHEER TIE PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998042400599 19980424 00599 NM 1998 4 24 AALA980470 1 19980309 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1060 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 TUL - TWO INCH AREA OF STRINGER 30 CORRODED BETWEEN STATION 1050 AND 1070. STRINGER SPLICE SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998042400600 19980424 00600 NM 1998 4 24 AALA980471 1 19980309 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1060 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 TUL - SKIN AT STATION 1060 AT STRINGER 30 CORRODED THROUGH APPROX DAMAGE AREA IS 1 INCH BY 1 INCH. REMOVED CORRODED SKI N AND INSTALLED REPAIR PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998042400601 19980424 00601 NM 1998 4 24 AALA980472 1 19980309 A 5330 SKIN BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 708AA 22465 TUL - FOUND SKIN CORRODED OUTBOARD OF STRINGER 28L BETWEEN 950E AND 950F. INSTALLED DOUBLER PR SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998042400602 19980424 00602 NM 1998 4 24 AALA980474 1 19980309 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CORROSION ON SHEAR TIE BETWEEN STRINGER 26R-27R STATION 660. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-1 . (M) 2 L 7 3 4F A3WE 1998042400603 19980424 00603 NM 1998 4 24 AALA980475 1 19980309 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 804.95 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - AT FUSELAGE STATION 804.95 FRAME OUTBOARD SIDE STIFFENER ANGLE CRACKED AT STRINGER 14R ATTACH POINT. REMOVED AND REPLACED OUTBOARD SIDE SECTION OF FRAME CHORD ANGLE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998042400604 19980424 00604 NM 1998 4 24 TWRA9807 1 19980204 A 2530 OVEN BOEING 747 747131 1384881 NM GALLEY ODOR A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 15 608FF 19672 DURING CLIMB ACRID SMELL PERMEATED COCKPIT, NO SMOKE OBSERVED ADN NO SOURCE COULD BE FOUND. DURING THAT TIME NOTED OVEN IN NR 2 GALLEY POPPED CIRCUIT BREAKER. RESTORED ELECTRICAL POWER, OPERATED NORMALLY UNTIL APPROXIMATELY 45 MINUTES BEF ORE LANDING WHEN SMELL RETURNED. FOUND C/B'S NR 2 GALLEY OVENS SET, RAN OVENS FOR 2 HOURS PER MM 25-31-00. OPS CHECK O K. (M) 2 L 7 4 4F A20WE 1998042400605 19980424 00605 NM 1998 4 24 TAOA039801 1 19980303 A 3350 37067001 BATTERY PACK BOEING 727 727254 138408L NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 916TS 20437 FLT 6443 - DCA - RIGHT FORWARD OVERWING INTERIOR EMERGENCY LIGHT INOPERATIVE. BATTERY PACK REPLACED, OPERATIONAL CHECK NORMAL PER MM 33-50. (M) 2 L 7 3 4F A3WE 1998042400606 19980424 00606 EU 1998 4 24 SIMA980701 1 19980311 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AT 434 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT INBOARD, LEFT AFT OUTBOARD AND THE LEFT AFT FLIGHT ATT ENDANT SEAT TRACKS WERE CORRODED. MAINTENANCE REMOVED AND REPLACED THE THREE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400607 19980424 00607 EU 1998 4 24 98ZZZM446 1 19980311 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AT 434 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT INBOARD, LEFT AFT OUTBOARD AND THE LEFT AFT FLIGHT ATT ENDANT SEAT TRACKS WERE CORRODED. MAINTENANCE REMOVED AND REPLACED THE THREE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400608 19980424 00608 EU 1998 4 24 98ZZZM447 1 19980311 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 434AT 434 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT INBOARD, LEFT AFT OUTBOARD AND THE LEFT AFT FLIGHT ATT ENDANT SEAT TRACKS WERE CORRODED. MAINTENANCE REMOVED AND REPLACED THE THREE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400609 19980424 00609 WP 1998 4 24 98ZZZM448 2 19980223 A 7320 FUEL CONTROL FRCHLD SA227 SA227DC 3377521 SW GARRTT TPE331 TPE3311U 01514 WP LT ENGINE OUT OT ADJUST A EQGA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 19 854LS DC854B DFW - FLT 1235 - ON TAKEOFF ROLL, LEFT ENGINE PRODUCED ONLY 97 PERCENT RPM. CREW ABORTED TAKEOFF AND RETURNED TO GATE A REA. MAINTENANCE INSPECTED THE AIRCRAFT AND ADJUSTED SCREW 'X' ON THE LEFT ENGINE ONE AND ONE-HALF TURNS. MAINTENANCE PERFORMED GROUND RUNS. ALL RUNS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A18SW E3WE 1998042400610 19980424 00610 NM 1998 4 24 AALA980621 1 19980326 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - BELL FRAME CORRODED AROUND HOLE FOR WIRES STATION 1070 ABOVE STRINGER 10L. INSTALLED DOUBLER ON CUTOUT OF DOOR FR AME IAW 55-10-1 AND 51-40-2 PAGE 3. (M) 2 L 7 3 4F A3WE 1998042400611 19980424 00611 NM 1998 4 24 AALA980622 1 19980326 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - SHEAR TIE CORRODED BETWEEN STRINGER 27 AND 28R. REMOVED AND REPLACED CORRODED SHEAR TIE PER SRM 53-10-4 ALODINED AND PRIMED PART AND APPLIED SEALANT TO REPAIR AREA. (M) 2 L 7 3 4F A3WE 1998042400612 19980424 00612 NM 1998 4 24 AALA980623 1 19980326 A 5311 FRAME BOEING 727 727227 1384078 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FUSELAGE FRAME CRACKED AT FRAME STATION 930 STRINGER 14L. REPAIRED CRACK FRAME IAW BOEING SERVICE BULLETIN 727-53 -0162 FIG 3. (M) 2 L 7 3 4F A3WE 1998042400613 19980424 00613 NM 1998 4 24 AALA980624 1 19980326 A 5330 SKIN BOEING 727 727227 1384078 NM BS 307 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - SKIN HAS DEEP WEAR BEHIND FUSELAGE TORQUE TUBE IN CENTER SECTION. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53 -30-3. (M) 2 L 7 3 4F A3WE 1998042400614 19980424 00614 NM 1998 4 24 MASA98061 1 19980321 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 DURING ROUTINE MAINTENANCE, FOUND SEVERAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED NR 2 POSITION EMERGENCY LIGHT BATTERY. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998042400615 19980424 00615 NM 1998 4 24 MASA98059 1 19980320 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING A ROUTINE INSPECTION, MAINTENANCE FOUND THE EMERGENCY LIGHT SWITCH NORMAL LIGHT WOULD ILLUMINATE. MAINTENANCE RE PLACED THE BULBS IN THE SWITCH, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998042400616 19980424 00616 NM 1998 4 24 MASA98056 1 19980313 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 DURING ROUTINE LIGHTING CHECK, MAINTENANCE FOUND THE THE SECOND CABIN OVERHEAD CENTER AISLE EMERGENCY LIGHT WOULD NOT IL LUMINATE. MAINTENANCE REMOVED AND REPLACED THE BULB. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998042400617 19980424 00617 NM 1998 4 24 MASA98067 1 19980401 A 3350 0L3071BAEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING NIGHT MAINTENANCE, FOUND CENTER OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BULBS, OPS CHEC K GOOD. (M) 2 H 7 2 4T RT A13NM 1998042400618 19980424 00618 NM 1998 4 24 MASA98068 1 19980402 A 3350 L03071BPEGPC BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 DURING ROUTINE MAINTENANCE, FOUND THE CENTE ROVERHEAD EMERGENCY EXIT LIGHT HAD FIVE INOPERATIVE BULBS. MAINTENANCE REMO VED AND REPLACED THE FIVE BULBS, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998042400619 19980424 00619 NM 1998 4 24 MASA98064 1 19980330 A 3350 S6R3S62LAE BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 DURING ROUTINE MAINTENANCE, FOUND ONE RED EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED LAMP, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998042400620 19980424 00620 NM 1998 4 24 MASA98065 1 19980330 A 3350 PR2 BULB DHAV DHC8 DHC8202 2809007 NM CABIN OUT OF POSITION A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE DURING PRE-MAINTENANCE RUN-UP. FOUND BULB OUT OF POSITION, REPOSITIONED BULB. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998042400621 19980424 00621 EU 1998 4 24 SIMA980883 1 19980329 A 5320 S5367121729801 DRAIN TRACK AEROSP ATR72 ATR72212 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR DRAIN TRACK AND THE SERVICE DOOR DRAIN TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH DRAIN TRACK IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400622 19980424 00622 EU 1998 4 24 98ZZZM449 1 19980329 A 5320 S5367121729801 DRAIN TRACK AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR DRAIN TRACK AND THE SERVICE DOOR DRAIN TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH DRAIN TRACK IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400623 19980424 00623 EU 1998 4 24 SIMA980882 1 19980329 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND THE CARGO DOOR SILL PLATE WERE CORR ODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED BOTH SILL PLATES IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 1998042400624 19980424 00624 EU 1998 4 24 98ZZZM450 1 19980329 A 5320 S5367131828001 SILL AEROSP ATR72 ATR72212 EU CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND THE CARGO DOOR SILL PLATE WERE CORR ODED OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED BOTH SILL PLATES IAW SRM 51-25-03. AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A53EU 1998042400625 19980424 00625 EU 1998 4 24 SIMA980903 1 19980331 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THAT THE FLOORBEAM 38 WAS CORRODED OUT OF LIMITS. MAINTENANCE REPA IRED FLOORBEAM 38 IAW SRM 53-00-00 PAGE 498. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400626 19980424 00626 EU 1998 4 24 SIMA980771 1 19980318 A 2424 243211 GCU AEROSP ATR42 ATR42300 8680920 EU NR 2 MALFUNCTIONED A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 21 233RM 235 MSN - FLT 4117 - AIRCRAFT RETURNED TO AIRPORT AFTER BURNING SMELL AND ELEC WARNIG ON CAP. AIRCRAFT LANDED OVERWEIGHT. R EPLACED NR 2 ACW GENERATOR GCU AND PERFORMED OVERWEIGHT INSPECTION. NR 2 AC GEN SYSTEM CHECKED GOOD AND NO DISCREPANCIE S WERE NOTED ON OVERWEIGHT INSPECTION. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400627 19980424 00627 EU 1998 4 24 SIMA9807402 1 19980315 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 223 ORD - FLT 4147 - EMERGENCY ESCAPE PATH LIGHT INOP AT SEAT POSITION 3A. ITEM DEFERRED MEL 33-22. SPLICED BROKEN WIRE AN D REPLACED BULB IAW STANDARD PRACTICE. OPS CHECK GOOD AT THIS TIME MEL CLEARED AND A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400628 19980424 00628 EU 1998 4 24 SIMA980881 1 19980329 A 3350 167006 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423MQ 030 MKE - FLOOR PROX LIGHTS ROW 5 INOP. ISSUED MEL'D AND RETURNED A/C TO SERVICE. REINSTALLED LIGHT BULB IN SOCKET. PERFO RMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400629 19980424 00629 EU 1998 4 24 SIMA980904 1 19980331 A 5320 S5367800920102 CHANNEL AEROSP ATR72 ATR72212 EU FRAME 36-38 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR CHANNEL BETWEEN FRAME 36 AND 38 CORRODED AND THE F LOOR CHANNEL BETWEEN FRAME 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOOR CHANNELS IAW SRM 51-25-02. A /C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400630 19980424 00630 EU 1998 4 24 98ZZZM451 1 19980331 A 5320 S5367800826901 CHANNEL AEROSP ATR72 ATR72212 EU FRAME 38-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR CHANNEL BETWEEN FRAME 36 AND 38 CORRODED AND THE F LOOR CHANNEL BETWEEN FRAME 38 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLOOR CHANNELS IAW SRM 51-25-02. A /C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400631 19980424 00631 EU 1998 4 24 SIMA980902 1 19980331 A 5330 S5317210100264 SKIN AEROSP ATR72 ATR72212 EU FRAME 5/6 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE NOTED DENT IN FUSELAGE. LEFT SIDE 36 INCHES BELOW STATIC PORT BETWEEN FRAME 5 AND 6. MAINTENANCE INSTALLED A PATCH IAW SRM 53-00-00 PAGE 410. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400632 19980424 00632 EU 1998 4 24 SIMA980901 1 19980331 A 5330 S5317210100264 SKIN AEROSP ATR72 ATR72212 EU FRAME DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 369AT 369 SAW - DURING CPCP-1 INSPECTION, MAINTENANCE NOTED DENT IN FUSELAGE. LEFT SIDE AT FRAME 2 AND STRINGER 11. MAINTENANCE REPAIRED THE DENT IAW SRM 53-00-00 FIGURE 422. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400633 19980424 00633 WP 1998 4 24 AALA980641 1 19980329 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 291AA 49303 DFW - DURING OVERNIGHT MAINTENANCE, THE FORWARD FLIGHT ATTENDANT STATION PORTABLE EMERGENCY FLASHLIGHT WAS INOPERATIVE. REPLACED PORTABLE EMERGENCY FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 1998042400634 19980424 00634 NM 1998 4 24 AALA980598 1 19980323 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 727AA 20734 MIA - DURING OVERNIGHT MAINTENANCE CEHCK, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT COACH INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN AFT COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400635 19980424 00635 NM 1998 4 24 AALA980524 1 19980318 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 703AA 22461 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHTING EXIT SIGN IN FIRST CLASS INOPERATIVE. REPLACED THREE EMERGE NCY EXIT FLOOR LIGHT SEGMENTS UNDER EXIT SIGN IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400636 19980424 00636 NM 1998 4 24 AALA980639 1 19980329 A 3350 A3060720201 CONDUCTOR BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 706AA 22463 ATL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND COACH CABIN INOPERATIVE. R EPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONDUCTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400638 19980424 00638 NM 1998 4 24 AALA980450 1 19980308 A 3350 CLIP BOEING 727 727223 1384074 NM CABIN OUT OF ADJUST A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 707AA 22464 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN VENTRAL STAIR INOPERATIVE. ADJUSTED CLIPS ON EMERGENCY EXIT CHARGER FOR VENTRAL STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400639 19980424 00639 NM 1998 4 24 AALA980600 1 19980325 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT PASSENGER SEAT ROW 19 INOPERATIVE. REPAIRED EMER GENCY EXIT FLOOR PATH LIGHT STRIP AT PASSENGER SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400640 19980424 00640 NM 1998 4 24 AALA980418 1 19980301 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 859AA 21086 RDU - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY LIGHT IN AIRSTAIR INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN A IRSTAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400641 19980424 00641 NM 1998 4 24 AALA980449 1 19980307 A 3350 SPLICE BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 861AA 21088 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTING WAS INOPERATIVE FROM SEAT ROWS 8 THROUGH 18. REPAIRED FAULTY SPLICES IN EMERGENCY FLOOR LIGHTING SYSTEM SEAT ROWS 8 THROUGH 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400642 19980424 00642 NM 1998 4 24 AALA980514 1 19980317 A 3350 1001141 LIGHT BOEING 727 727233 138408A NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 866AA 21371 DFW - DURING OVERNIGHT CHECK, AFT STAIRWAY EMERGENCY LIGHT ASSEMBLY WAS INOPERATIVE. REPLACED AFT STAIRWAY EMERGENCY LI GHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A3WE 1998042400643 19980424 00643 NM 1998 4 24 AALA980406 1 19980225 A 3397 WIRE BOEING 727 727223 1384074 NM GALLEY SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 871AA 21383 BNA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING WOULD NOT ILLUMINATE. REPAIRED SHORTED WIRE IN EMERGENCY FLOOR L IGHTING AT FORWARD GALLEY SIDEWALL LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400644 19980424 00644 NM 1998 4 24 AALA980602 1 19980325 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 887AA 21526 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY LIGHT ASSE MBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400645 19980424 00645 NM 1998 4 24 AALA980540 1 19980318 A 3350 PIN BOEING 727 727223 1384074 NM L1 DOOR PUSHED OUT A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6818 19493 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EVACUATION DOOR MOUNTED SLIDE LIGHT ON FORWARD L1 DOOR INOPERATIVE. INSTA LLED PIN ON LIGHT ASSEMBLY WIRE TO SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400646 19980424 00646 NM 1998 4 24 AALA980553 1 19980321 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 21387 DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT SIGN HAD TWO BULBS INOPERATIVE. REPLACED AFT EMERGENCY EXIT SIGN LIGHT STRIP ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998042400647 19980424 00647 EU 1998 4 24 AALA980270 1 19980208 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14077 612 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACT LIGHTING AT R4 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400648 19980424 00648 WP 1998 4 24 AALA980271 1 19980207 A 2430 DISCONNECT DOUG DC10 DC1010 3022110 WP LT BATTERY LOOSE A AALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SW 07 130AA 46989 LAX - FLT 606 - ON CLIMB-OUT, BATTERY AND LEFT EMERGENCY AC INDICATED ZERO VOLTS AND ZERO AMPS. AIRCRAFT AIR INTERRUPTE D AND RETURNED TO LAX WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEFT BATTERY QUICK DISCONNECT LOOSE. SECURED LEFT BA TTERY QUICK DISCONNECT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1998042400649 19980424 00649 EU 1998 4 24 AALA980304 1 19980211 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7083A 645 MIA - FLT 988 - DURING PREFLIGHT, CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTING PULLED LOOSE AND INOPERATIVE AT SEAT ROW 23 THROUGH 26. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT SEAT ROWS 23 THROUGH 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400650 19980424 00650 EU 1998 4 24 AALA980256 1 19980225 A 3350 KD4A017 RELAY AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70074 517 JFK - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS DISARM ANNUNCIATOR ON WITH SWITCH IN ARM POSITION. REPLACED RELAY 1 XX. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400651 19980424 00651 EU 1998 4 24 AALA980316 1 19980214 A 2611 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU AFT LAVATORY LOOSE A AALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 07 18066 509 JFK - DURING OVERNIGHT CHECK, AFT LAVATORY SMOKE DETECTOR RED WARNING LIGHT INOPERATIVE. RESECURED LOOSE CONNECTOR FOR AFT LAVATORY SMOKE DETECTOR RED WARNING LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400652 19980424 00652 NM 1998 4 24 AALA980442 1 19980304 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT MANTENANCE, EMERGENCY EXIT LIGHTS IN CABIN WOULD NOT ILLUMINATE. REPAIRED TWO OPEN CIRCUITS IN E MERGENCY EXIT LIGHT SYSTEM ZONE 'A'. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998042400653 19980424 00653 EU 1998 4 24 AALA980558 1 19980323 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80058 466 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 15B AND AFT TO MID CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT ROW 15B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400654 19980424 00654 EU 1998 4 24 AALA980551 1 19980321 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 40064 507 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT L4 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400655 19980424 00655 NM 1998 4 24 AALA980550 1 19980320 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS IN CABIN ZONE 'B' WOULD NOT ILLUMINATE. REPLACED EMERGENCY EX IT LIGHT CONNECTOR IN ZONE 'B'. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998042400656 19980424 00656 NM 1998 4 24 AALA980555 1 19980322 A 3350 CONNECTORS DOUG MD11 MD11 3023602 NM CABIN LOOSE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 1766A 48597 LHR - FLT 86 - DURING FLIGHT, EMERGENCY FLOOR PATH LIGHTS ILLUMINATED AND WOULD NOT EXTINGUISH WHEN COCKPIT EMERGENCY LI GHT SWITCH TURNED TO OFF. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTORS IN FIRST CLASS AND AS A PRECAUTIONARY, RE PLACED FORWARD RIGHT POWER PACK ASSEMBLY. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998042400657 19980424 00657 NM 1998 4 24 AALA980539 1 19980313 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1756 48491 DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS EMERGENCY EXIT FLOOR LIGHT TRACKING INOPERATIVE. REPAIRED SPLICE BETWEEN R2 LIGHTS. GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998042400658 19980424 00658 EU 1998 4 24 AALA980494 1 19980314 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN DAMAGED A AALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 7083A 645 MIA - FLT 1819 - DURING GROUND OPERATIONS THE OUTBOUND CREW REPORTED THE EMERGENCY EXIT FLOOR PATH LIGHTING FORWARD OF P ASSENGER SEAT 3R WAS MISSING. REPLACED EMERGENCY EXIT FLOOR PATH LIGHTING STRIP FROM PASSENGER SEAT 3R FORWARD DUE TO 2 0 FEET OF WIRE BEING DAMAGED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400659 19980424 00659 WP 1998 4 24 AALA980504 1 19980315 A 3350 P2010031303 LIGHT DOUG DC10 DC1030 3023501 WP L4 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 164AA 46950 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L4 DOOR LOWER HALF WAS INOPERATIVE. REPLACED L4 DOOR LOWER EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1998042400660 19980424 00660 NM 1998 4 24 AALA980601 1 19980324 A 3350 L204961 LIGHT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT AISLE LIGHT ASSEMBLY ABOVE SEAT 7H INOPERATIVE. REPLACED OV ERHEAD EMERGENCY EXIT AISLE LIGHT ASSEMBLY ABOVE SEAT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998042400661 19980424 00661 EU 1998 4 24 AALA980604 1 19980326 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE SEAT ROWS 21H THROUGH 25H. REPLACED FLAT WIRE FROM WALL CONNECTOR TO EMERGENCY ESCAPE PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998042400662 19980424 00662 NM 1998 4 24 AALA980632 1 19980325 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1764B 48554 DFW - DURING OVERNIGHT MAINTENANCE, THE R1 FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT WAS INOPERATIVE. REPLACED R1 F LIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998042400663 19980424 00663 WP 1998 4 24 AALA980643 1 19980330 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447AA 49473 BOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM PASSENGER SEAT ROWS 20 THROUGH 26 INOPERATIV E. RESECURED DISCONNECTED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP SEAT ROW 20. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F A6WE 1998042400664 19980424 00664 EU 1998 4 24 AALA980489 1 19980311 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1411G 11369 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTING AT OVERWING EXITS WOULD NOT ILLUMINATE. REPLACED EMERGENCY EXIT F LOOR LIGHTING STRIP AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998042400665 19980424 00665 EU 1998 4 24 AALA980541 1 19980318 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1460A 11480 DFW - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT AISLE LIGHT AT ROW 13 INOPERATIVE. REPAIRED WIRE ON ELECTRI CAL CONTACT SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998042400666 19980424 00666 EU 1998 4 24 AALA980379 1 19980221 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1402K 11353 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT FORWARD SERVICE DOOR WERE INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT GROUND WIRE LOCATED OVER COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998042400667 19980424 00667 NM 1998 4 24 AALA980609 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 410-491 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FASTENERS AND SKIN HAVE CORROSION AT STRINGER 8 LOWER SURFACE OF RT WING FROM WING STATION 410 TO 491.5. REMOVED CORRODED FASTENERS AND CORROSION PER SRM 51-30-1, ALODINED AND PRIMED AREA. INSTALLED REPAIR STRAP AT STATION 418 AND 4 88 PER ESO 11697 AND INSTALLED FASTENERS PER ESO 11697 3-17-98. (M) 2 L 7 3 4F A3WE 1998042400668 19980424 00668 NM 1998 4 24 AALA980610 1 19980326 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND STATION 720A BELL FRAME SHEAR TIE HAS CORROSION FWD AND AFT SIDES BETWEEN STRINGER 27L AND 28L. REPAIRED WI TH DOUBLER, REMOVED CORRODED SECTION. REPAIR PER SRM 53-10-4 PAGE 49-51. (M) 2 L 7 3 4F A3WE 1998042400669 19980424 00669 NM 1998 4 24 AALA980611 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 417-456 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FASTENERS AND LOWER WING SKIN CORRODED AT STRINGER 6 RIGHT WING FROM STATION 410.0 TO WS 491.5. REPAIRED AREA PER ESO 11697, DATED 3-17-98. (M) 2 L 7 3 4F A3WE 1998042400670 19980424 00670 NM 1998 4 24 AALA980612 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 491-574 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FASTENERS AND SKIN HAS CORROSION AT STRINGER 6 ON LOWER SURFACE OF RIGHT WING FOR WS 491.5 TO STATION 574. REMOVE D CORRODED FASTENERS AND CORROSION PER SRM 57-30-1, ALODINED AND PRIMED INSTALLED REPAIR STRAP AT STATION 496 PER ESO 11 697 AND INSTALLED NEW FASTENERS PER ESO 11697 DATED 3-17-98. (M) 2 L 7 3 4F A3WE 1998042400671 19980424 00671 NM 1998 4 24 AALA980613 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 330-410 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FASTENERS AND SKIN HAVE CORROSION AT STRINGER 8 ON LOWER SURFACE OF RT WING FROM WING STATION 330.5-410. REMOVED CORRODED FASTENERS, REMOVED CORROSION IAW SRM 57-30-1, ALODINED AND PRIMED. INSTALLED REPAIR STRAP IAW ESO 11697 WITH N EW FASTENERS. (M) 2 L 7 3 4F A3WE 1998042400672 19980424 00672 NM 1998 4 24 AALA980614 1 19980326 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - PREVIOUS REPAIR CORRODING ON TOP OF FLOORBEAM AT STATION 400 RBL 10 TO 14 INCH. REMOVED DAMAGED AREA AND REPAIRED PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998042400673 19980424 00673 NM 1998 4 24 AALA980615 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 251-330 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FASTENERS AND SKIN HAVE CORROSION AT STRINGER 6 LOWER SURFACE OF RIGHT WING, WING STATION 251 TO 330.5. ALODINED AND PRIMED AREA, INSTALLED REPAIR STRAP IAW ESO 11697 DATED 3-17-98 AND INSTALLED NEW FASTENERS IAW ESO 11697, DATED 3-1 7-98. (M) 2 L 7 3 4F A3WE 1998042400674 19980424 00674 NM 1998 4 24 AALA980616 1 19980326 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 344 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND STRINGER CRACK AT RIVETS ATTACHING WALL SUPPORT BRACKET AT STRINGER 5 RIGHT FORWARD SIDE OF STATION 344. RE PAIRED WITH 'J' ANGLE REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998042400675 19980424 00675 NM 1998 4 24 AALA980617 1 19980326 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND SHEAR TIE BETWEEN STRINGER 27-28L AT STATION 720E HAS CORROSION. REMOVED AND REPLACED SHEAR TIE PER 52-10-4 PAGE 12-17. (M) 2 L 7 3 4F A3WE 1998042400676 19980424 00676 NM 1998 4 24 AALA980618 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 474-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND CORROSION AROUND 9 FASTENERS ON LOWER WING SKIN STRINGER 6, WS 474-500. REMOVED CORROSION AND INSTALLED REP AIR STRAP AS PER ESO 11697, DATED 3/17/98. (M) 2 L 7 3 4F A3WE 1998042400677 19980424 00677 NM 1998 4 24 AALA980619 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 474-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - LOWER WING SKIN HAS CORROSION AROUND 26 EACH FASTENERS STRINGER 8 WS 474-500. REMOVED CORROSION AND INSTALLED REP AIR STRAP AS PER ESO 11697, DATED 3/17/98. (M) 2 L 7 3 4F A3WE 1998042400678 19980424 00678 EU 1998 4 24 AALA980588 1 19980324 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 28 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON TRACK NR 10, 4 INCHES FORWARD OF FRAME 28. INSTALLED TRACK NR 10 FROM FRAME 26-30 PER SRM 51-7 2-10-0. (M) 2 L 7 2 4F RT A35EU 1998042400679 19980424 00679 EU 1998 4 24 AALA980587 1 19980323 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - TRACK 3A LAV SUPPORT TRACK HAS CORROSION IN AROUND 3 LAVATORY BOLT HOLES AND ON TOP OF TRACK. REMOVED CORRODED TR ACK AND LAVATORY SUPPORT BOLT HOLE BLOCKS AND REPLACED WITH NEW PER SRM 51-72-10-0 AND 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998042400680 19980424 00680 EU 1998 4 24 AALA980586 1 19980323 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FLOOR SUPPORT CORRODED FWD FRAME 74 BETWEEN TRACKS 6 AND 7. BLENDED OUT CORROSION AND REPAIRED DAMAGE ON FRAME 74 BETWEEN TRACKS 6 AND 7 PER SRM 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998042400681 19980424 00681 EU 1998 4 24 AALA980585 1 19980323 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 78 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION AROUND FLOORBOARD MOUNT HOLE ON NR 7 TRACK JUST AFT OF FRAME 78. BLENDED OUT CORROSION AND INSTAL LED STRAP DOUBLER PER AARD 53-20-00-02. (M) 2 L 7 2 4F RT A35EU 1998042400682 19980424 00682 EU 1998 4 24 AALA980565 1 19980320 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FLOORBOARD SUPPORT IS CORRODED BETWEEN FRAME 71 AND 72 AT TRACK NR 7. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP PER AARD 53-20-00-02. (M) 2 L 7 2 4F RT A35EU 1998042400683 19980424 00683 EU 1998 4 24 AALA980564 1 19980320 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 73-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - THE SMALL SEAT TRACK INBOARD OF R-4 DOOR IS CORRODED BETWEEN 73 FRAME AND 74 FRAME TRACK 9. REMOVED AND REPLACED SEAT TRACK LOCATED AT TRACK 9 BETWEEN FRAME 73 AND 74 PER SRM 51-77-10-0. (M) 2 L 7 2 4F RT A35EU 1998042400684 19980424 00684 EU 1998 4 24 AALA980563 1 19980320 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FLOOR SUPPORT CORRODED AT TRACK NR 6 BETWEEN FRAME 72 AND 73. BLENDED OUT CORROSION AND INSTALLED STRAP REPAIR PE R AARD 53-20-00-02. (M) 2 L 7 2 4F RT A35EU 1998042400685 19980424 00685 EU 1998 4 24 AALA980562 1 19980319 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FLOOR SUPPORT CORRODED AT FRAME 72 BY TRACK NR 7. FABRICATED AND INSTALLED STRAP REPAIR PER AARD 53-20-00-02. (M ) 2 L 7 2 4F RT A35EU 1998042400686 19980424 00686 EU 1998 4 24 AALA980561 1 19980320 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 67 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON FLOORBEAM AT FRAME 67 BETWEEN TRAYS NR 1 AND NR 2. REMOVED AND REPLACED FLOORBEAM AT FRAME 67 BULK CARGO FLOOR BETWEEN TRAYS 1 AND 2 PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1998042400687 19980424 00687 EU 1998 4 24 AALA980560 1 19980320 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 66-69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - LARGE AREAS OF CORROSION BETWEEN FRAME 66 AND FRAME 69 LEFT SIDE OF BULK CARGO FLOORBEAM. REMOVED AND REPLACED BU LK CARGO FLOORBEAM BETWEEN FRAME 66 AND 69 LEFT SIDE PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1998042400688 19980424 00688 EU 1998 4 24 AALA980547 1 19980320 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 14-18 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORRODED SEAT TRACK NR 6. REMOVED AND REPLACED THE SECTION OF SEAT TRACK NR 6 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998042400689 19980424 00689 EU 1998 4 24 AALA980526 1 19980319 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 15 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION OF LAST 19 INCHES OF SECTION. INSTALLED STRAP ON FLOORBOARD SUPPORT PER AARD 53-20-00-2 PAGE 1. ( M) 2 L 7 2 4F RT A35EU 1998042400690 19980424 00690 NM 1998 4 24 AALA980398 1 19980220 A 5230 SKIN DOUG MD11 MD11 3023602 NM CARGO DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - CENTER CARGO DOOR FWD LOWER CORNER HAS SUSTAINED IMPACT DAMAGE. INSTALLED REPAIR DOUBLER PER ESO 41000 DATED 2/20 /98. (M) 2 L 7 3 4F RT A22WE 1998042400691 19980424 00691 NM 1998 4 24 AALA98363 1 19980215 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 911 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1764B 48554 TUL - FOUND CORROSION ON SEAT TRACK. REMOVED AND REPLACED SECTION OF TRACK STANDARD SEAT TRACK REPAIR PER 53-70-00-0 VO L I. (M) 2 L 7 3 4F RT A22WE 1998042400692 19980424 00692 NM 1998 4 24 AALA980239 1 19980130 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 911 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - FOUND SEAT TRACK NR 3 CORRODED AT STATION 911. REMOVED CORRODED AREA AND INSTALLED A SEAT TRACK PLUG PER SRM 53-7 0-00-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1998042400693 19980424 00693 NM 1998 4 24 AALA980238 1 19980130 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 911 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1765B 48596 TUL - FOUND SEAT TRACK NR 4 AT STATION 911 CORRODED ON TOP OF TRACK. REMOVED CORRODED AREA AND INSTALLED A SEAT TRACK P LUG PER SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1998042400694 19980424 00694 NM 1998 4 24 AALA98139 1 19980116 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 900-905 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 TUL - FOUND CORROSION ON SEAT TRACK NR 6 UNDER LAVS AFT OF GALLEY NR 5. REMOVED AND REPLACED SEAT TRACK SECTION ACCOMPL ISHED STANDARD SEAT TRACK REPAIR PER SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1998042400695 19980424 00695 NM 1998 4 24 AALA98423 1 19980228 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 909 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - FOUND CORROSION AT TIE DOWN POINT FOR LAV 2 TRACK NR 4 ABOUT STATION 909. REMOVED DAMAGED AREA AND PLUGGED SEAT T RACK PER SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1998042400696 19980424 00696 EU 1998 4 24 AALA980576 1 19980321 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 54 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRINGER 56L UNDER FRAME 54.2 HAS CORROSION. REMOVED CORROSION PRIMED AND TREATED. INSTALLED DOUBLER IAW S RM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998042400697 19980424 00697 WP 1998 4 24 AALA980596 1 19980323 A 5313 STRINGER DOUG DC10 DC1010 3022110 WP BS 1119 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - AFT END OF STRINGER 52 AT STATION 1119 EXFOLIATED. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998042400698 19980424 00698 WP 1998 4 24 AALA980597 1 19980323 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1099-1119 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - BULDGE IN SKIN STRINGER 52 JUST FWD OF CAC DOOR. INSTALLED DOUBLER PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998042400699 19980424 00699 WP 1998 4 24 AALA980527 1 19980319 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 840-879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - SEAT TRACK NR 6 CORRODED UNDER GALLEY 840-850. REPLACED SECTION OF SEAT TRACK FROM STATION 735-879 PER SRM 53-70- 00. (M) 2 L 7 3 4F A22WE 1998042400700 19980424 00700 WP 1998 4 24 AALA980528 1 19980319 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP BS 830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - INTERCOSTAL FRAME CORRODED JUST OUTBOARD OF SEAT TRACK NR 6 UNDER GALLEY. REPLACED INTERCOSTAL AT STATION830 PER AARD 51-10-00-1. (M) 2 L 7 3 4F A22WE 1998042400701 19980424 00701 WP 1998 4 24 AALA980529 1 19980319 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - LEFT INBOARD LAV SUPPORT 'HOCKEY STICK' HAS CORROSION AROUND AFT MOUNT HOLE. REPLACED LEFT INBOARD LAV SUPPORT PE R AARD 51-10-00 PAGE 1. (M) 2 L 7 3 4F A22WE 1998042400702 19980424 00702 WP 1998 4 24 AALA980530 1 19980319 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1391 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND CORROSION AROUND BELLY DRAIN HOLES AT APPROX FUSE STATION 1391. INSTALLED REPAIR DOUBLER PER SRM 53-40-00 A REA CORROSION REMOVAL PER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1998042400703 19980424 00703 WP 1998 4 24 AALA980531 1 19980318 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1331 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND CORROSION AROUND BELLY DRAIN AT APPROX STATION 1331. REMOVED CORROSION PER SRM 51-21-01 AND INSTALLED REPAI R DOUBLER PER SRM 53-40-00. (M) 2 L 7 3 4F A22WE 1998042400704 19980424 00704 WP 1998 4 24 AALA980533 1 19980318 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 800-879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND SEVERAL AREAS OF CORROSION ON LEFT OUTBOARD ROLLER TRAY. INSTALLED NEW TRAY PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998042400705 19980424 00705 WP 1998 4 24 AALA980532 1 19980319 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND CORROSION BETWEEN STATION 1701 FLOORBOARD AND FLOORBOARDS SUPPORT ON TOP OF FLOORBEAM BETWEEN NR 3 ROLLER TR AY AND NR 5 ROLLER TRAY. TREATED PRIMED AND PAINTED AREA PER SRM 51-21-01 VOL II. INSTALLED DOUBLER TO TOP FO FLOORBEA M PER SRM 53-00-01 VOL 1. (M) 2 L 7 3 4F A22WE 1998042400706 19980424 00706 WP 1998 4 24 AALA980543 1 19980319 A 5320 WEB DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - LOWER LOBE GALLEY FIRE DOOR TRACK LOWER WEB IS CORRODED THROUGH AFT OF THE C-LIFT DOOR SUPPORT POST. REMOVED, MAN UFACTURED AND REINSTALLED NEW WEB SECTION PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998042400707 19980424 00707 WP 1998 4 24 AALA980544 1 19980319 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 879-715 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - RIGHT INBOARD L/L GALLEY ROLLER TRAY HAS SEVERAL AREAS OF CORROSION. INSTALLED NEW SECTION OF TRACK FROM STATION 725 TO STATION 879 PER SRM 53-70-00 FIG NR 8. (M) 2 L 7 3 4F A22WE 1998042400708 19980424 00708 WP 1998 4 24 AALA980581 1 19980320 A 5730 SKIN DOUG DC10 DC1010 3022110 WP WS 126.3 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - 10 INCHES INBOARD OF FUSE SKIN (XW108) STATION 1116.3 FASTENER INTO NR 2 TANK (TOP) HAS INTERGRANULAR CORROSION. I NSTALLED FASTENER, ALODINED, PRIMED AND APPLIED DINOL AV30 FER ESO 7349 DATED MAR 19, 1998. (M) 2 L 7 3 4F A22WE 1998042400709 19980424 00709 WP 1998 4 24 AALA980500 1 19980313 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1910 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FLOORBOARD SUPPORT HAS CORROSON AROUND HOLES FOR CLIP NUTS UNDER RT COFFEEBAR. REMOVED AND REPLACED SUPPORT PER A ARD 51-10-00-1 PAGE 1. (M) 2 L 7 3 4F A22WE 1998042400710 19980424 00710 WP 1998 4 24 AALA980501 1 19980313 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1910 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - GALLEY SUPPORT HAS CORROSION ON FLOORBOARD SUPPORT LEG STATION 1910 UNDER RT COFFEEBAR. REMOVED AND REPLACED SUPP ORT PER AARD 51-10-00-1 PAGE 1. (M) 2 L 7 3 4F A22WE 1998042400711 19980424 00711 WP 1998 4 24 AALA980635 1 19980325 A 5320 SPLICE DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FRAME LOWER 'J' ANGLE SPLICE IS CORRODED. REPLACED CORRODED 'J' ANGLE PER SRM 53-30-00 FIG 5. (M) 2 L 7 3 4F A22WE 1998042400712 19980424 00712 WP 1998 4 24 AALA980636 1 19980325 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND CORROSION IN FRAME LOWER 'J' ANGLE, UPPER AND LOWER SURFACES. REPLACED CORRODED 'J' ANGLE PER SRM 53-30-00 FIG 5. (M) 2 L 7 3 4F A22WE 1998042400713 19980424 00713 WP 1998 4 24 AALA980626 1 19980326 A 5320 DOUBLER DOUG DC10 DC1010 3022110 WP BS 1999 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - INTERNAL SKIN DOUBLER AT STATION 1999 IS CORRODED FROM STRINGER 42L TO 43L. TRIMMED OUT CORRODED AREA AND INST FI LLER WITH INTERNAL DOUBLER. 2 EXT DOUBLERS (STACKED ) BELOW SKIN SPLICE AND 1 EXT DOUBLER STRAP ABOVE SKIN SPLICE PER E SO 7349 DATED 3-25-98. (M) 2 L 7 3 4F A22WE 1998042400714 19980424 00714 WP 1998 4 24 AALA980637 1 19980320 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 835 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND CORROSION ON GALLEY SUPPORT TRACK. INSTALLED DOUBLER AND REPAIR PLUG IN GALLEY SUPPORT PER SRM 53-70-00. ( M) 2 L 7 3 4F A22WE 1998042400715 19980424 00715 NM 1998 4 24 AALA984057 1 19980327 A 5730 SKIN BOEING 767 767223 1385123 NM BS 956 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 320AA 22321 AFW - FOUND CORROSION ON CENTER WING UPPER SKIN AT AFT DRAIN LOCATION. REMOVED CORROSION, BLENDED AREA, PRIMED, PAINTED AND SEALED PER ENGINEERING MRB 767-1593. (M) 2 L 7 2 4F RT A1NM 1998042400716 19980424 00716 EU 1998 4 24 AALA980631 1 19980326 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FRAME 56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - NR 6 ROLLER TRAY AT FRAME 56, FORWARD TRAY CORRODED AT FASTENER AT FRAME 56. ROLLER TRAY REPLACED, REF AARD 51-10 -00-3, TREATED PRIMED AND PAINTED TRAY REF SRM 51-21-00-01. (M) 2 L 7 2 4F RT A35EU 1998042400717 19980424 00717 EU 1998 4 24 AALA980630 1 19980326 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - NR 6 FORWARD ROLLER TRAY SEGMENT CORRODED FRAME 58 SPLICE. REPLACED ROLLER TRAY SECTION REF AARD 51-10-00-3, TREA TED, PRIMED AND PAINTED REF SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998042400718 19980424 00718 EU 1998 4 24 AALA980629 1 19980325 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON LOWER ANGLE OF STRINGER 55 FROM FRAME 72-73. REPAIRED STRINGER PER E20 30575, DATED 3-24-98. ( M) 2 L 7 2 4F RT A35EU 1998042400719 19980424 00719 EU 1998 4 24 AALA980634 1 19980326 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON SEAT TRACK NR 8 BETWEEN FRAME 29 AND 33. REMOVED CORRODED SECTION OF TRACK NR 8 AND FABRICATED NEW SECTION AND INSTALLED DOUBLERS PER SRM 51-72-10-0 AND ESO 30595 DATED 3/25/98. (M) 2 L 7 2 4F RT A35EU 1998042400720 19980424 00720 EU 1998 4 24 AALA980627 1 19980324 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FRAME 28 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON TOP OF FRAME 28 BETWEEN SEAT TRACK NR 9 AND NR 10. INSTALLED DOUBLER ANGLE PER SRM 51-71-50, A LODINED, PRIMED AND PAINTED, BLENDED AREA AND DOUBLER PER SRM 51-22-00. (M) 2 L 7 2 4F RT A35EU 1998042400721 19980424 00721 EU 1998 4 24 AALA980628 1 19980325 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND STRINGER 49L HAS CORROSION AT FRAME 69. REMOVED CORRODED SECTION OF STRINGER. INSTALLED NEW SECTION AND DO UBLER TO STRINGER 49L PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998042400722 19980424 00722 NM 1998 4 24 AALA984060 1 19980330 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 933 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 328AA 22328 AFW - WHILE IN FOR MBV MAINTENANCE FOUND TWO AREA OF CORROSION ON THE UPPER SURFACE OF THE UPPER FLANGE OF THE FLOORBEAM AT STATION 933 LBL 11. AFTER BLENDING, THE AREAS WERE DYE CHECKED SHOT/ROTO PEENED PER SRM 51-20-06. REFINISHED PER S RM AND FILLED WITH BMS5-95 SEALANT. (M) 2 L 7 2 4F RT A1NM 1998042400723 19980424 00723 NM 1998 4 24 AALA980606 1 19980326 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - STRINGER IS LEFT CRACKED FORWARD OF ICE LIGHT BETWEEN STATION 720B AND 720C. REPAIRED WITH STRINGER SPLICE PER SR M 53-10-3. (M) 2 L 7 3 4F A3WE 1998042400724 19980424 00724 NM 1998 4 24 AALA980607 1 19980326 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 420 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND CORROSION ON TOP FLANGE OF FLOORBEAM STATION 420 RBL 55 TO RBL 60. REMOVED DAMAGE AND REPAIRED PER SRM 53-1 0-8. (M) 2 L 7 3 4F A3WE 1998042400725 19980424 00725 NM 1998 4 24 AALA980608 1 19980326 A 5730 SKIN BOEING 727 727227 1384078 NM WS 491-574 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FASTENERS AND SKIN HAS CORROSION AT STRINGER 8 ON LOWER SURFACE OF RT WING FROM WS 491.5 TO WS 574. REMOVED CORRO DED FASTENERS AND CORROSION PER SRM 57-30-1 ALODINED AND PRIMED AREAS. INSTALLED REPAIR STRAP AT STATION 496 PER ESO 11 697 AND INSTALLED NEW FASTENERS PER ESO 11697 DATED 3-7-98. (M) 2 L 7 3 4F A3WE 1998042400726 19980424 00726 EU 1998 4 24 SIMA980862 1 19980327 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 301AE 340B301 DFW - FLT 3935 - WHITE FLOOR LIGHT NEAR ROW 10 INOP MEL'D PER 33-15-2. RETURNED A/C TO SERVICE. RAID BULB AT ROW 10 ON THE FLOOR PROX LIGHTING. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998042400727 19980424 00727 1998 4 24 SIMA9806861 4 19980327 A 3442 M158535505 R/T UNIT AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 407AT 2531 407 CRP - FLT 3716 - DURING FLT TO DFW FROM HRL CREW NOTED SMOKE IN FLIGHT CABIN. CREW DIVERTED INTO CRP. CFR FOLLOW A/C T O GATE. A/C LANDED SAFELY. NOTE SMOKE OCCURED WHEN WX RADAR WAS RESET. RAI RADAR R/T. PERFORMED OPS CHECK GOOD. RET URNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042400728 19980424 00728 WP 1998 4 24 GAIA9831 1 19980322 A 5311 99582022 FRAME DOUG DC9 DC915F 3022037 WP BS 544 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING B-CHECK INSPECTION FOR AD 73-09-02 A CRACK WAS DISCOVERED ON THE RIGHT FUSELAGE FRAME AT STATION 544 JUST BELOW T HE FLOOR LINE. FRAME WAS REPAIRED IAW DC-9 SB 53-117. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998042400729 19980424 00729 WP 1998 4 24 GAIA9832 1 19980331 A 5347 S2914913 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 237 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING INSPECTION OF CORROSION TASK 58-53302 WHILE AIRCRAFT WAS IN C-CHECK LEVEL 2 CORRSION WAS FOUND ON A FLOOR SEAT TR ACK AT FUSELAGE STATION 237 LBL 0. THE SEAT TRACK WAS REPAIRED IAW DC-9 SRM 53-05 FIG 4F. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998042400730 19980424 00730 WP 1998 4 24 GAIA9834 1 19980327 A 5330 5920323 SKIN DOUG DC9 DC915F 3022037 WP BS 285-307 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR ON THE FUSELAGE SKIN BETWEEN LONGERON 22R AND 18R FROM FUSELAGE STAT ION 285 TO 307. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-054. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998042400731 19980424 00731 WP 1998 4 24 GAIA9835 1 19980327 A 5330 5911411 SKIN DOUG DC9 DC915F 3022037 WP BS 185-200 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR ON THE FUSELAGE SKIN BETWEEN LONGERON 20R AND 22R FROM FUSELAGE STAT ION 185 TO 200. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-055. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998042400732 19980424 00732 WP 1998 4 24 GAIA9836 1 19980327 A 5330 5921764 SKIN DOUG DC9 DC915F 3022037 WP BS 332-408 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING C-CHECK INSPECTION, FOUND 2 TEMPORARY REPAIRS ON THE FUSELAGE SKIN BELOW THE MAIN CARGO DOOR BETWEEN LONGERON 18L AND 19L FROM FUSELAGE STATION 332 TO 408. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-056. THE AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998042400733 19980424 00733 WP 1998 4 24 GAIA9833 1 19980327 A 5330 99211601 SKIN DOUG DC9 DC915F 3022037 WP BS 389-408 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING INSPECTION OF PSE 53.09.021 WHILE AIRCRAFT WAS IN C-CHECK A CRACK WAS FOUND AT THE WINDOW CUTOUT BETWEEN STATION 389 AND 408 AND TWO CRACKS WERE FOUND AT THE WINDOW CUTOUT BETWEEN STATION 604 AND 623. A TEMPORARY REPAIR WAS PERFORME D ON THE SKIN IAW BOEING LETTER SEQUENCE 9808139 DATED MARCH 11, 1998. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998042400734 19980424 00734 WP 1998 4 24 98ZZZM452 1 19980327 A 5330 99115351 SKIN DOUG DC9 DC915F 3022037 WP BS 604-623 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 562PC 47012 DURING INSPECTION OF PSE 53.09.021 WHILE AIRCRAFT WAS IN C-CHECK A CRACK WAS FOUND AT THE WINDOW CUTOUT BETWEEN STATION 389 AND 408 AND TWO CRACKS WERE FOUND AT THE WINDOW CUTOUT BETWEEN STATION 604 AND 623. A TEMPORARY REPAIR WAS PERFORME D ON THE SKIN IAW BOEING LETTER SEQUENCE 9808139 DATED MARCH 11, 1998. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998042400735 19980424 00735 NM 1998 4 24 GAIA9837 1 19980403 A 2751 10607916 INDICATOR BOEING 727 727224 1384076 NM TE FLAPS LOOSE A GAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 69740 20668 AFTER DEPARTURE FROM IAH-TOL, THE INBOARD FLAPS FROZE AT 2 DEGREES. AIRCRAFT RETURNED TO IAH. AFTER 10 MINUTES FLAPS W ENT TO 30 DEGREES, BUT ON TAXI IN FLAPS FROZE AT 2 DEGREES AGAIN. THE FLT CREW DECLARED AN EMERGENCY INTO IAH AND MADE AN UNEVENTFUL LANDING. CLEANED AND RE-SEATED CANNON PLUG ON FLAP GAUGE, OPS AND GROUND CHECKED OK PER B727 MM 27-50. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998042400736 19980424 00736 NM 1998 4 24 WRLA98078 1 19980330 A 2822 608473 BOOST PUMP DOUG MD11 MD11 3023602 NM NR 3 FUEL TANK FAILED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 275WA 48631 DURING TAXI-OUT, FLT CREW NOTED NR 3 TANK AFT BOOST PUMP ALERT. FLIGHT CREW ELECTED TO RETURN TO GATE WITHOUT FURTHER I NCIDENT. MAINTENANCE PERSONNEL CONFIRMED FUEL BOOST PUMP FAILURE. PART WAS NO STOCK AT STATION. ASSIGNED DEFERRAL TO MALFUNCTION. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998042400737 19980424 00737 NM 1998 4 24 WRLA98079 1 19980330 A 2612 61071800 FIRE LOOP DOUG MD11 MD11 3023602 NM NR 2 ENGINE FAILED A WRLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 275WA 48631 DURING INITIAL CLIMB, FLT CREW RECEIVED A NR 2 ENGINE FIRE WARNING. FLT CREW RETARDED THE THROTTLE AND WARNIGN WENT OUT . FLT CREW ELECTED TO RETURN TO POINT OF DEPARTURE FOR MAINTENANCE. MAINTENANCE PERSONNEL FOND 'B' FIRE LOOP HARNESS B AD. PART WAS REPLACED. GROUND RUNS WERE COMPLETED WITH NO MALFUNCTIONS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998042400738 19980424 00738 NM 1998 4 24 TSAA9853197 1 19980307 A 5313 STRINGER BOEING 737 737297 1384480 NM BS 351 DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 TEAR STRAP AT STATION 351 AND STRINGER 24R HAS EDGE DISTANCE OF .30 INCH. REPAIRED STRAP BY INSTALLING A DOUBLER PER SB A-SBX-SEA-980002RR AND APPROVED BY 8110-3 DATED MARCH 9, 1998. (M) 2 L 7 2 4F A16WE 1998042400739 19980424 00739 NM 1998 4 24 TSAA9853196 1 19980306 A 5313 STRINGER BOEING 737 737297 1384480 NM BS 896 DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 TEAR STRAP AT STATION 896 AND STRINGER 20R HAS EDGE DISTANCE OF .5 DIAMETER (MINIMUM OF 1.5 DIA IS REQUIRED). REPAIRED STRAP BY INSTALLING A DOUBLER PER SBA-SBX-SEA-98-0002RR AND APPROVED BY 8110-3 DATED MAR9, 1998. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F A16WE 1998042400740 19980424 00740 NM 1998 4 24 TSAA9853194 1 19980301 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 520 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 STATION 520 AND STRINGER 27L TO 20L AFT BULKHEAD LEFT 'L' ANGLE HAS LEVEL 2 CORROSION. FABRICATED, TREATED, PRIMED AND INSTALLED ANGLE PER SRM 51-10-1, 51-10-2 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1998042400741 19980424 00741 NM 1998 4 24 TSAA9825193 1 19980228 A 5320 SUPPORT BOEING 737 737297 1384480 NM BS 440-460 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 FLOOR SUPPORT STRUCTURE WEB AT STATION 440 TO 460 AND STRINGER 28L HAS LEVEL 2 CORROSION. FABRICATED REPAIR PART PER SR M 51-10-1. INSTALLED NEW PART PER SRM 51-10-6. (M) 2 L 7 2 4F A16WE 1998042400742 19980424 00742 NM 1998 4 24 TSAA9833198 1 19980402 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 ON SERVICE CHECK, FOUND NR 1 POSITION EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998042400743 19980424 00743 NM 1998 4 24 TWRA9816 1 19980322 A 2810 FUEL TANK BOEING 747 747130 1384880 NM NR 2/3 LEAKING A TWRA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 15 603FF 19746 AFTER TAKEOFF, AFTER NR 1 A/C PACK TURNED ON, REPORT OF HEAVY SMELL OF FUEL FUMES IN CABIN AS WELL AS IN COCKPIT AS A/C ROTATED. AFTER ALL PACKS WERE TURNED ON FUEL SMELL DISSIPATED. ON FUEL LEAK CHECK OF NR 3 MAIN FUEL TANK, STATIC FUEL LEAK FROM WING ROOT SPLICE AT SPANWISE NR 2 AND NR 3, ALSO FUEL LEAKS FROM WING ROOT SPLICE AREA SPANWISE NR 3 AND SPANW ISE NR 2. AFTER TANK ENTRY, RESEALED NR 3 MAIN FUEL TANK WING ROOT SPLICE AT SPANWISE NR 2 AND NR 3 AND SEALED LOWER SE AM STRINGER AT WING ROOT AREA SPANWISE NR 3 AND NR 2. LEAK CHECKED OK PER REF MM 28-11-00. (M) 2 L 7 4 4F A20WE 1998042400744 19980424 00744 EU 1998 4 24 REXA98082 1 19980331 A 2613 OVERHEAT SENSOR SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A REXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 111PX 340A024 RIGHT TAIL PIPE HOT LIGHT IN FLIGHT. CLEANED AND INSPECTED TAILPIPE SENSORS. NO DEFECTS NOTED ON GROUND RUN-UP. OK FO R SERVICE. (M) 2 L 7 2 4T RT A52EU 1998042400745 19980424 00745 EU 1998 4 24 REXA98080 1 19980325 A 7712 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU LT TQ GAUGE DIRTY A REXA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 25 315PX 685 LEFT TORQUE GAUGE SPIKED WHILE TAXIING. CLEANED TORQUE BRIDGE CANNON PLUG GROUND. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998042400746 19980424 00746 EU 1998 4 24 REXA98079 1 19980324 A 7712 TQ SIGNAL COND BAG JETSTM JETSTM3101 1500215 EU RT ENGINE OUT OF ADJUST A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 315PX 685 RIGHT TORQUE GAUGE SPIKES WITH NO POWER ADVANCEMENT. CALIBRATED TORQUE SIGNAL CONDITIONER. PERFORMED GROUND RUNS, NO D EFECT NOTED. (M) 2 L 7 2 4T RT A21EU 1998042400747 19980424 00747 WP 1998 4 24 HALA9800076 1 19980331 A 3350 60030451 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 674MC 47735 FLT 113 - HNL - EMERGENCY LIGHT CEILING ROW 3-4 OUT. REMOVED AND REPLACED BATTERIES, POWER SUPPLY, OPERATIONAL CHECK GO OD. (M) 2 L 7 2 4F RT A6WE 1998042400748 19980424 00748 WP 1998 4 24 HALA9800080 1 19980401 A 3350 CONTROL BOX DOUG DC10 DC1010 3022110 WP CABIN FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 119AA 46519 HNL - FLT 10 - EMERGENCY LIGHT TEST INOP (GREEN LT) AND 2L AND 4L FAULT LIGHT CAME ON DURING TEST. REPLACED EMERGENCY L IGHT CONTROL BOX ON 2L AND 4L DOOR, OPS CHECK GOOD. (M) 2 L 7 3 4F A22WE 1998042400749 19980424 00749 WP 1998 4 24 HALA9800072 1 19980325 A 3230 GRD SHIFT CONTL DOUG DC9 DC951 3022051 WP LANDING GEAR OUT OF ADJUST A HALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 13 673MC 47726 FLT 530 - HNL - A/C WAS UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. SUSPECT GROUND SHIFT FAILURE. A/C MADE AN UNEVEN TFUL LANDING IN HNL. ADJUSTED GROUND SHIFT CONTROL MECHANISM, PER M/M 32-231. (M) 2 L 7 2 4F RT A6WE 1998042400750 19980424 00750 WP 1998 4 24 HALA9800085 1 19980405 A 2131 10256852 CONTROLLER DOUG DC9 DC951 3022051 WP COCKPIT FAILED A HALA O OTHER O OTHER LD LANDING 1 WP 13 420EA 47689 FLT 561 - HNL - CABIN ALTITUDE INDICATES BELOW SEA LEVEL WHEN CABIN PRESSURE CONTROL IS SET TO SEA LEVEL. CABIN PRESSUR E CLIMB RAPIDLY ON TOUCH DOWN. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER, PRESSURIZATION AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998042400751 19980424 00751 WP 1998 4 24 HALA980089 1 19980405 A 3260 PROX SENSOR DOUG DC9 DC951 3022051 WP NLG FAILED A HALA O OTHER N FALSE WARNING CR CRUISE 1 WP 13 674MC 47735 FLT 564 - HNL - NOSE GEAR UNSAFE LIGHT CAME ON DURING CRUISE (UPLATCH CHECK OK RT HYD PUMP ON HIGH OR LOW HAD NO CHANGE) . UPON LOWERING GEAR, LIGHT (RED) STAYED ON AND NO GREEN NOSE LANDING GEAR LIGHT CAME ON. CYCLED GEAR HAD ON CHANGE. THEN AFTER APPROX 15 SECONDS GREEN LIGHT CAME ON WITH NO RED. REMOVED AND REPLACED NOSE GEAR SENSOR. OPS CHECK OK PER MM 32-00, GEAR SWING, INDICATION CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998042400752 19980424 00752 WP 1998 4 24 GTIA9800037 1 19980402 A 2560 SLIDE DOUG DC9 DC931 3022065 WP RT EMER EXIT DR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 934ML 47526 THE RIGHT EXIT DOOR ESCAPE SLIDE FELL OUT OF THE CASING. INSTALLED COVERS ON RIGHT EMERGENCY ESCAPE SLIDE IAW DC-9 MM 2 5-61-0. (M) 2 L 7 2 4F A6WE 1998042400753 19980424 00753 WP 1998 4 24 GTIA9800038 1 19980331 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 699 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 969ML 47268 OKC - AIRCRAFT UNDERGOING A C-CHECK INSPECTION, THE FRAME AT STATION 699 RIGHT SIDE OF FUSELAGE WAS FOUND CRACKED IN THE LOWER POCKET OF THE FITTING. (M) 2 L 7 2 4F A6WE 1998042400754 19980424 00754 WP 1998 4 24 GTIA9800039 1 19980331 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 737 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 969ML 47268 OKC - AIRCRAFT UNDERGOING A C-CHECK INSPECTION, THE FRAME AT STATION 737 WAS FOUND CRACKED IN THE LOWER POCKET OF THE FI TTING. (M) 2 L 7 2 4F A6WE 1998042400755 19980424 00755 WP 1998 4 24 GTIA9800040 1 19980331 A 5530 TIE FITTING DOUG DC9 DC931 3022065 WP VERT STAB CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 969ML 47268 OKC - AIRCRAFT UNDERGOING A C-CHECK INSPECTION, THE VERTICAL TIE FITTING ATTACHING THE VERTICAL TO THE FUSELAGE WAS FOUN D CRACKED IN HALF. (M) 2 L 7 2 4F A6WE 1998042400756 19980424 00756 WP 1998 4 24 GTIA9800041 1 19980331 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 737 CRACKED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 969ML 47268 OKC - AIRCRAFT UNDERGOING A C-CHECK INSPECTION, THE FRAME AT STATION 737 RIGHT SIDE WAS FOUND CRACKED IN THE LOWER POCKE T OF THE FITTING. (M) 2 L 7 2 4F A6WE 1998042400757 19980424 00757 WP 1998 4 24 G6OA019 1 19980329 A 7810 131M55G01 EXHAUST FAIRING DOUG DC10 DC1030F 3023504 WP NR 1 ENGINE MISSING A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 603GC 47922 ON PREFLIGHT INSPECTION, GROUND MAINTENANCE NOTED THE NR 1 ENGINE AFT CENTER BODY EXHAUST NOZZLE FAIRING MISSING. GROUN D MAINTENANCE REPLACED THE NR 1 ENGINE AFT CENTER BODY EXHAUST NOZZLE PER MM 78-11-02. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 3 4F RT A22WE 1998042400758 19980424 00758 1998 4 24 NOCA0898 4 19980326 A 2562 EB2BW ELT BOEING 757 75723A 1384967 NM BS 400 MALFUNCTIONED A NOCA K NONE N FALSE WARNING DE DESCENT 1 EA 15 757NA 24567 EMERGENCY LOCATOR TRANSMITTER SIGNAL ACTIVATED ON DESCENT, SIGNAL CAN BE ON 121.5. REMOVED AND REPLACED ELT TRANSMITTER . OPERATIONAL CHECK OF ELT OK. (M) 2 L 7 2 4F RT A2NM 1998042400759 19980424 00759 NM 1998 4 24 TAOA039806 1 19980326 A 4900 38067811 APU BOEING 727 727227 1384078 NM CABIN OVERHEATING A TAOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 15 924TS 21041 LGA-BOS - FLT 6080 - SMOKE IN CABIN WITH BOTH PACKS AND GASPER FAN ON. PACKS WERE NOT OVERHEATED, BEFORE DEPARTURE LGA AIRCRAFT SWAP. REPLACED AUXILIARY POWER UNIT ASSEMBLY PER FORM 14MT-4914A LEAK AND OPERATIONAL CHECK NORMAL. RAN BOTH PACKS NO SMOKE OR FUMES NOTED. (M) 2 L 7 3 4F A3WE 1998042400760 19980424 00760 EU 1998 4 24 RAIA980313 1 19980319 A 7600 31058691 IEC JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 565HK 41082 FLT 7724 - JFK - RIGHT IEC FAILED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT DELTA P/P TRANSDUCER. (M) 2 L 7 2 4T RT A41NM 1998042400761 19980424 00761 EU 1998 4 24 RAIA980310 1 19980317 A 5411 S5421039000751 FRAME AEROSP ATR42 ATR42300 8680920 EU RT ENGINE CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 119 STL - DURING INSPECTION, FOUND RIGHT ENGINE INTERMEDIATE FRAME CRACKED AT INBOARD VERTICAL MEMBER ABOVE ENGINE ISOLATOR MOUNT. MAINTENANCE REPLACED RIGHT ENGINE INTERMEDIATE FRAME. (M) 2 H 7 2 4T RT A53EU 1998042400762 19980424 00762 EU 1998 4 24 RAIA980314 1 19980323 A 5320 S53971002243 FITTING AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CRACKED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 722TE 220 STL - DURING LANDING GEAR CHANGE MAINTENANCE FOUND RIGHT SIDE FRAME 27 FUSELAGE FAIRING ATTACH FITTING CRACKED AT STRING ER 14. MAINTENANCE REPLACED RIGHT SIDE FRAME 27 ATTACH FITTING AT STRINGER 14. (M) 2 H 7 2 4T RT A53EU 1998042400763 19980424 00763 1998 4 24 RAIA980317 4 19980326 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 551HK 41040 FLT 7490 - STL - CAPTAINS ALTIMETER FLAGGED ON TAKEOFF ROLL. MAINTENANCE REPLACED LEFT AIR DATA COMPUTER. (M) 2 L 7 2 4T RT A41NM 1998042400764 19980424 00764 EU 1998 4 24 RAIA980316 1 19980324 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGG DOOR OUT OF ADJUST A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 554HK 6371 41067 FLT 7745 - JFK - CARGO DOR CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE ADJUSTED AFT BAGGAGE DOOR MICROSWITCH. (M) 2 L 7 2 4T RT A41NM 1998042400765 19980424 00765 EU 1998 4 24 RAIA980315 1 19980324 A 2150 38650 DUCT AEROSP ATR72 ATR72202 8680940 EU RT PACK FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 721TE 217 FLT 7170 - STL - RIGHT PACK FAULTED, CREW SMELLED SMOKE. MAINTENANCE REPLACED RIGHT HEAT EXCHANGER BLEED AIR DUCT. (M) 2 H 7 2 4T RT A53EU 1998042400800 19980424 00800 NM 1998 4 24 98ZZZX1613 1 19980409 A 6220 900R2100001103 DROOP STOP DOUG MD900 MD900 3027375 NM M/R HEAD CRACKED A L A EGRA K NONE O OTHER IN INSP/MAINT 1 EA 17 900LF 778 90000022 DURING 100-HOUR SPECIAL INSPECTION OF MAIN ROTOR HEAD, 4 EACH, DROOP STOP SUPPORT BRACKETS WERE FOUND CRACKED COMPLETELY THROUGH AT BOLT ATTACHMENT POINT SECURING BRACKET TO MAIN ROTOR HEAD. IF DROOP STOP SUPPORT WERE TO DEPART AIRCRAFT, M AIN ROTOR BLADE WOULD CONTACT TAIL BOOM. MANUFACTURER SHOULD NOTIFY OPERATOR OF POSSIBLE CRACKING AND INCREASE INSPECTI ON INTERVAL. 1 G 7 2 3U NC H19NM 1998042400822 19980424 00822 WP 1998 4 24 IXXA9800029 1 19980318 A 3610 39216041 REGULATOR VALVE DOUG DC8 DC862 3021970 WP NR 1 ENGINE DEFECTIVE A IXXA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 GL 23 61CX 46142 DURING CLIMBOUT, THE NUMBER ONE AND TWO ENGINE PNEUMATIC MANIFOLD OVER TEMPERATURE INDICATING LIGHTS ILLUMINATED, VERIFI ED BY TEMPERATURE INDICATOR. THE FLIGHT ENGINEER SECURED THE NUMBER ONE AND TWO ENGINE BLEED SYSTEMS FOLLOWING COMPANY EMERGENCY PROCEDURES. THE FLIGHT RETURNED TO TOL FOR AN UNEVENFUL LANDING. MAINTENANCE PERFORMED A GROUND RUN IN ACCO RDANCE WITH COMPANY JRH WHICH REVEALED THE NUMBER ONE BLEED REGULATOR VALVE DEFECTIVE, WHICH WAS REPLACED. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL TEST. 2 L 7 4 4F 4A25 1998042400823 19980424 00823 WP 1998 4 24 IXXA9800031 1 19980115 A 2560 3705474503 FITTING DOUG DC8 DC871F 302199D WP CARGO DR SLIDE CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTINE C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FORWARD DOOR LEFT FRONT SLIDE SUPPORT FITTNIG TO BE CRAC KED. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW SLIDE SUPPORT FITTING IN ACC ORDANCE WITH FAA PER APPROVED DRAWING COO-8-52-121-98 AND ENGINEERING ORDER 52-DC8-817. 2 L 7 4 4F RT 4A25 1998042400824 19980424 00824 WP 1998 4 24 IXXA9800032 1 19980115 A 5330 PLATING DOUG DC8 DC871F 302199D WP BS 650-780 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 650 TO 78 0, LONGERONS 32 LEFT AND 32 RIGHT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION A NEW SECTION OF SKIN, INTERNAL AND EXTERNAL REPAIR DOUBLERS AND A EXTERNAL REPAIR TRIPLER IN ACCORDANCE WITH FAA PER APPROVED DRAWING COO-8-53-057-98 AND ENGINEERING ORDER 53-DC8-793. 2 L 7 4 4F RT 4A25 1998042400826 19980424 00826 WP 1998 4 24 IXXA9800036 1 19980114 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON LONGERON SPLICE 27 RIGHT BETWEEN FUSELAGE STATIONS 440.0 TO 460.0. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION A NEW LONGERON SPLICE FITTING IN A CCORDANCE WITH FAA PER APPROVED DRAWING COO-8-069-98 AND ENGINEERING ORDER 53-DC8-810. 2 L 7 4 4F RT 4A25 1998042400827 19980424 00827 WP 1998 4 24 IXXA9800037 1 19980115 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1160 WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTINE C-CHECK INSPECTION, FOUND EXCESS WEAR WAS DETECTED ALONG THE LOWER AFT CARGO COMPARTMENT CUT OUT, ALONG F RAME AT FUSELAGE STATION 1160 BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. REPAIR ACCOMPLISHED BY FABRICATION AND INSTALLATI ON A REPAIR DOUBLER IN ACCORDANCE WITH FAA PER APPROVED DRAWING COO-8-53-049098 AND ENGINEEERING ORDER 53-DC8-789. 2 L 7 4 4F RT 4A25 1998042400828 19980424 00828 WP 1998 4 24 IXXA9800038 1 19980204 A 5730 PLATING DOUG DC8 DC871F 302199D WP WS 415-422 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LEFT WING LOWER LEADING EDGE BETWEEN STATIONS XS415 AND 422. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION AN INTERNAL FILLER AND AN EXTERNAL REPLAIR DOUBLER IN ACCORDANCE WITH FAA PER APPROVED DRAWING C00-8-070-98 AND ENGINEERING ORDER 57-DC8-805. 2 L 7 4 4F RT 4A25 1998042400829 19980424 00829 WP 1998 4 24 IXXA9800039 1 19980204 A 5720 36540733 FITTING DOUG DC8 DC871F 302199D WP LT WING DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTINE C-CHECK INSPECTION, FOUND LEFT WING NUMBER FIVE SPOILER HINGE FITTING CRACKED. REPAIR ACCOMPLISHED BY RE MOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION NEW HINGE FITTING IN ACCORDANCE WITH DAC DRAWING 3654073 AND ENGI NEERING ORDER 27-DC8-799. 2 L 7 4 4F RT 4A25 1998042400830 19980424 00830 WP 1998 4 24 IXXA9800040 1 19980128 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 1350 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTINE C-CHECK INSPECTION, A CRACK LOCATED ON LONERGON SPLICE FITTING 32 RIGHT AT FUSELAGE STATION 1350. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION AN NEW SPLICE FITTING IN ACCORDANCE WITH FAA P ER APPROVED DRAWING C00-8-53-061-98 AND ENGINEERING ORDER 53-DC8-797. 2 L 7 4 4F RT 4A25 1998042400832 19980424 00832 WP 1998 4 24 9806889993 1 19980417 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8986E 47402 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. RIGGED TAIL CONE DEPLOY MENT SYSTEM, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998042400833 19980424 00833 NE 1998 4 24 9806896740 2 19980416 A 7200 ENGINE BOEING 747 747251F 1384898 NM PWA JT9 JT9D7J 52054 NE NR 1 OVERTEMP A NWAA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION LD LANDING 1 GL 01 640US 23888 662539 AFTER LANDING AND SLOWING TO TAXI SPEED, THE NR 1 ENGINE COMPRESSOR STALLED WITH THE TOWER REPORTING FLAMES FROM THE TAI LPIPE. THE ENGINE WAS SHUT DOWN, MAXIMUM EGT WAS 1089C FOR 35 SECONDS. MAINTENANCE CHANGED THE ENGINE DUE TO THE OVERT EMP. 2 L 7 4 4F 4 F A20WE E20EA 1998042400834 19980424 00834 NE 1998 4 24 9806901162 2 19980417 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA K NONE R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 162US 46771 686151 DURING LANDING ROLLOUT WHILE COMING OUT OF REVERSE THRUST AT 80 KTS, THE NR 3 ENGINE COMPRESSOR STALLED. EGT PEAKED AT 1000C BEFORE THE ENGINE WAS SHUT DOWN AND THE COM COMPLIED WITH. MAINTENANCE INSPECTED THE ENGINE PER MAINTENANCE MANUA L INCLUDING A BORESCOPE. NO PROBLEMS WERE FOUND. 2 L 7 3 4F 4 F A22WE E20EA 1998042400835 19980424 00835 WP 1998 4 24 9806911148 1 19980416 A 7830 TR UNIT DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 148US 46757 686129 DURING TAKEOFF ROLL, THE NR 2 ENGINE REVERSER UNLOCKED LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETU RNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A. 2 L 7 3 4F 4 F A22WE E20EA 1998042400836 19980424 00836 WP 1998 4 24 9806929931 1 19980420 A 3010 T-DUCT DOUG DC9 DC931 3022065 WP RT WING CRACKED A NWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 90S 47244 DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH ROLL TO THE RIGHT. CREW RECYCLED SLATS WITH SAME RESULTS. FL IGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT USING FLAPS ONLY. MAINTENANCE FOUND THE RIGHT SLAT BINDING DUE TO RIGHT ANTI-ICE T-DUCT CRACKED. REPLACED THE DUCT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400837 19980424 00837 WP 1998 4 24 9806989976 1 19980420 A 3510 292617EA1 OXYGEN PANEL DOUG DC9 DC931 3022065 WP COCKPIT OVERHEATED A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 9340 45308 2587 47389 DURING CLIMBOUT AT 12,000 FEET, A LOUD POP WAS HEARD FOLLOWED BY SMOKE COMING FROM OVERHEAD OF COCKPIT JUMPSEAT AT OXYGE N CONTROL PANEL. FLIGHT CREW DECLARED AN EMERGENCY AND THE AIRCRAFT WAS RETURNED TO DLH. LANDING WAS UNEVENTFUL. MAIN TENANCE FOUND OBSERVER'S OXYGEN CONTROL PANEL LIGHT PLATE OVERHEATED. REPLACED PANEL, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400838 19980424 00838 NE 1998 4 24 9806943209 2 19980417 A 7261 OIL LINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 1 ENGINE CRACKED A NWAA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 GL 01 309US 118 DURING CRUISE, AFT CARGO SMOKE INDICATION ILLUMINATED. CREW DISCHARGED CARGO FIRE EXTINGUISHER, DECLARED AN EMERGENCY, DIVERTED TO JAX, AND LANDED WITHOUT INCIDENT. NO INDICATION OF FIRE OR SMOKE IN AFT CARGO COMPARTMENT UPON INSPECTION B Y FIRE FIGHTING CREW. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. THE NR 1 ENGINE WAS PREVIOUSLY REPLACED D UE TO A CRACKED OIL LINE INDUCING OIL INTO THE PNEUMATIC SYSTEM CONSEQUENTLY CREATING SMOKE IN THE CABIN. 2 L 7 2 4F 4 F RT A28NM E29NE 1998042400839 19980424 00839 WP 1998 4 24 9806959756 1 19980420 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 756NW 47180 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS IN FIRST CLASS CABIN AREA DIM WHEN OPERATED. MAINTENANCE REPLAC ED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400840 19980424 00840 NM 1998 4 24 UPS98226470 1 19980404 A 5320 PRESSURE WEB BOEING 727 72722C 138400F NM BS 938 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK DETECTED IN CEILING OF RT WHEEL WELL AT BS 938 RBL 36. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIR COMPLETED PER EO B727-5 310-0460-L. 2 L 7 3 4F A3WE 1998042400841 19980424 00841 NM 1998 4 24 UPS98226471 1 19980404 A 5320 PRESSURE WEB BOEING 727 72722C 138400F NM BS 938 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK DETECTED IN CEILING OF LT WHEEL WELL AT BS 938 LBL 55. CRACK STOP DRILLED IAW SRM 51-10-1 AND REPAIR CARRIED OUT IAW EO B72 7-5310-0460, APPENDIX C. 2 L 7 3 4F A3WE 1998042400842 19980424 00842 NM 1998 4 24 UPS98226472 1 19980407 A 5521 RIB BOEING 727 72722C 138400F NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, RESULTS OF X-RAY ON LT ELEVATOR SHOWS CRACK IN LOWER RIB AREA BETWEEN ES 66.79 AND ES 71.79, 23 INCHE S FWD OF TRAILING EDGE. DAMAGE TRIMMED OUT IAW SRM 55-20-1 AND REPAIR CARRIED IAW SRS ENGINEERING ORDER 98-10-006, REF UPS ENGINEERING FILE NUMBER 727-55-0369. 2 L 7 3 4F A3WE 1998042400843 19980424 00843 NM 1998 4 24 UPS98226473 1 19980416 A 5522 SKIN BOEING 727 72722C 138400F NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, LT ELEVATOR TRAILING EDGE FASTENER HOLES FOUND CRACKED AND DAMAGED. DAMAGE BLENDED OUT AND REPAIR CA RRIED OUT IAW SRM 55-20-3, FIG 2. 2 L 7 3 4F A3WE 1998042400844 19980424 00844 NM 1998 4 24 UPS98226474 1 19980406 A 5311 FRAME BOEING 727 72722C 138400F NM BS 500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, CRACK IN TOE OF FRAME AT BS 500 LT AT LATCH SUPPORT FITTING. FRAME REPAIRED IAW SRM 53-10-4, FIG 11. 2 L 7 3 4F A3WE 1998042400845 19980424 00845 NM 1998 4 24 UPS98226475 1 19980407 A 5521 RIB BOEING 727 72722C 138400F NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-C, RESULTS OF X-RAY INSPECTION ON LT ELEVATOR SHOWS CRACK IN LOWER RIB REPAIR AREA BETWEEN ES 66.79 AND 69.79 AT 23 INCHES FWD OF TRAILING EDGE. DAMAGED AREA OF RIB TRIMMED OUT AND REPAIR CARRIED OUT IAW SRS ENGINEERING ORD ER 98-10-006, UPS ENGINEERING FILE NUMBER 727-55-0369. 2 L 7 3 4F A3WE 1998042400846 19980424 00846 WP 1998 4 24 UPS98826465 1 19980401 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, SKIN CRACKED AND CORRODED AT SHEAR TIE UNDER FRAME FS 1600 BTWN LONG 25R AND 24R AFT ACCY COMPT. REP AIRED IAW DHC SK-803-679. 2 L 7 4 4F RT 4A25 1998042400847 19980424 00847 WP 1998 4 24 UPS98826466 1 19980320 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, FS 1520 FLOORBEAM FWD SIDE HAS HEAVY CORROSION ON TANG LBL 59. REPAIRED IAW DHC SK-803-070. 2 L 7 4 4F RT 4A25 1998042400848 19980424 00848 WP 1998 4 24 UPS98826467 1 19980330 A 5320 3755872505 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 320 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, SHEAR TIE FITTING FS 320 BETWEEN STR 30L TO 29L HAS CORROSION. REMOVED AND REPLACED FITTING IAW SRM 52-2-0. 2 L 7 4 4F RT 4A25 1998042400849 19980424 00849 WP 1998 4 24 UPS98826468 1 19980404 A 5320 3755822501 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, SHEAR TIE FITTING AT FS 300 BETWEEN L36 AND L-35L IS CRACKED AND CORRODED. REMOVED, FABRICATED AND I NSTALLED REPLACEMENT FITTING IAW SRM 53-2- 0. 2 L 7 4 4F RT 4A25 1998042400850 19980424 00850 WP 1998 4 24 UPS98826469 1 19980414 A 5313 3648666 LONGERON DOUG DC8 DC873F 302199F WP BS 35-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, LONGERON 27R EXFOLIATED FS 35 TO 70. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998042400851 19980424 00851 EU 1998 4 24 WWMA9800078 1 19980421 A 2611 72111211000A SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DEFECTIVE A WWMA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 WP 15 356SB 340B356 CARGO SMOKE DETECTOR DOES NOT TEST. REMOVED AND REPLACED CARGO FWD SMOKE DETECTOR, OPS CK OK. 2 L 7 2 4T RT A52EU 1998042400852 19980424 00852 EU 1998 4 24 WWMA9800077 1 19980420 A 2611 SMOKE LIGHT SAAB SF340 340B 7860101 EU CARGO COMPT ILLUMINATED A WWMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 341SB 340B341 RETURN TO FIELD, THE CARGO SMOKE LIGHT CAME ON 10 MINUTES AFTER DEPARTURE. VISUAL INSPECTED CARGO COMPARTMENT, SMOKE SE NSOR ASSEMBLIES. SENSORS FOUND CLEAN. 2 L 7 2 4T RT A52EU 1998042400853 19980424 00853 WP 1998 4 24 ABXA9800366 1 19980417 A 5210 MECHANISM DOUG DOUG DC8 DC863 302198A WP CABIN DOOR BINDING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824AX 46141 FORWARD CABIN DOOR WOULD NOT OPEN FROM THE OUTSIDE. REPLACED FORWARD CABIN DOOR IAW DC8 MM 52-11-1, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998042400854 19980424 00854 WP 1998 4 24 ABXA9800367 1 19980421 A 3231 DOOR SPRING DOUG DC8 DC863F 302198F WP LT MLG DOOR OUT OF ADJUST A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 814AX 46041 LANDING GEAR UNSAFE LIGHT ILLUMINATED DURING CRUISE FLIGHT WITH LEFT MAIN LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINA TED. RECYCLED GEAR, NO CHANGE. ADJUSTED LEFT MAIN LANDING GEAR PROXIMITY SWITCH TARGET STOP. REPLACED LEFT GEAR DOOR SPRING IAW DC8 MM 32-31-5. PERFORMED TEST IAW DC8 MM 32-6, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998042400855 19980424 00855 WP 1998 4 24 DLL19980844 1 19980419 A 7830 TR LIGHT LKHEED 1011 10113853 5265020 WP NR 2 ENGINE ILLUMINATED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 762DA 69299 193Y1210 14625 REVERSER PRESSURE LIGHT ON IN FLT POM. FOUND REVERSER STOWED AND REPLACED PRSOV WITH NO HELP. SUSPECT WIR ING. 2 L 7 3 4F A23WE 1998042400856 19980424 00856 NM 1998 4 24 DLM90980846 1 19980419 A 2730 SENSOR 4073400902 DOUG MD90 MD9030 3023690 NM RT ELEVATOR MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 915DN 95030205 53395 AT 31,000 FT GOT PYLON FLAP MESSAGE FOLLOWED BY ELEVATOR SPLIT MESSAGE THEN PYLON FLAP MESSAGE WENT OUT. AIRCRAFT RETUR NED TO DFW. REPLACED ACU AND RT ELEV POS SENSOR . 2 L 7 2 4F RT A6WE 1998042400857 19980424 00857 NM 1998 4 24 DLM88980847 1 19980419 A 3260 INDICATOR 387 DOUG MD88 MD88 3023688 NM RT MLG FAILDED A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 923DL 49705 RT MLG GREEN DOWN AND LOCK LIGHT INOP. VERIFIED GEAR DOWN AND LOCKED. RELAMPED GEAR INDICATOR. GEAR INDICATION CKS NM L NOW. 2 L 7 2 4F RT A6WE 1998042400858 19980424 00858 NM 1998 4 24 DL72S980850 1 19980420 A 5311 65561014 FRAME BOEING 727 727225 1384077 NM BS 620 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 INBD CHORD OF THE FS 620 FRAME WAS FOUND CORRODED APPROX 2 INCHES OUTBD OF S26R. CORROSION WAS ON THE INBD CHORD ONLY. REPAIRED PER ERA 331533-14. 2 L 7 3 4F A3WE 1998042400859 19980424 00859 NM 1998 4 24 DL733980851 1 19980420 A 5314 65621257 KEEL BEAM BOEING 737 737347 1384647 NM BS 500 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 S28L KEEL BEAM WAS CORRODED AT FS 500D THRU FS 520. THE CORROSION REQUIRED CUTTING AND REMOVING A SECTION FROM FS 500D+ 10 FWD TO FS 500C+10. REPAIRED PER ERA 331606-14 . 2 L 7 2 4F RT A16WE 1998042400860 19980424 00860 NM 1998 4 24 DL733980852 1 19980420 A 5312 6546568187 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 1016 CORROEDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 AFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT APPROX BL 0.0. THE CORROSION INCLUDED SURFACES 0 THE DO ME WEB (GORE) AND BOTH THE LT AND RT 'C' CHANNEL STIFFENERS. AN ACCESS HOLE WAS CUT INTO THE FUSESLAGE SKIN TO FACILITA TE THE GORE REPAIR. REPAIRED PER ERA331614-14 . 2 L 7 2 4F RT A16WE 1998042400861 19980424 00861 NM 1998 4 24 DL733980853 1 19980420 A 5330 SKIN BOEING 737 737347 1384647 NM CARGO DOORWAY DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 3301 23181 FUSELAGE SKIN BELOW C1 DOOR CUTOUT WAS FOUND DENTED AND CREASED IN TWO PLACES. THE DAMAGE IS BETWEEN S26R AND S27R. RE PAIRED PER ERA 331629-14. 2 L 7 2 4F RT A16WE 1998042400862 19980424 00862 NM 1998 4 24 DL73S980856 1 19980420 A 3350 BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 328DL 23100 ON TEST L2 DOOR EXTERIOR EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY PACK POWER SUPPLY. 2 L 7 2 4F RT A16WE 1998042400863 19980424 00863 NM 1998 4 24 VNAA9804017 1 19980416 A 3241 AE20768 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ANTI-SKID SYST MALFUNCTIONED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 458PS 46231 3068 AN ANTI-SKID FAIL WARNING MESSAGE ILLUMINATED, DURING TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE CYCLED ELECTRICAL POWER AND RE-RACKED THE ANTI-SKID CONTROL UNIT. OPERATIONAL CHECKS WERE COMPLETED IN ACCORDANCE WITH DORNIER MANTENANCE MANUAL 32-40-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998042900001 19980429 00001 1998 4 29 HEEA0013680 4 19980402 A 2340 ACS1278 SWITCH BOLKMS 117 BK117A4 5626017 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 ICS/PVT SWITCH VIBRATES TO THE OFF POSITION IN FLIGHT. 1 G 7 2 3U H13EU 1998042900002 19980429 00002 1998 4 29 HEEA0013706 4 19980402 A 2210 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 FAILED PART 9.3 AND 9.4 ON SST PITCH. 1 G 7 2 4U H4SW 1998042900003 19980429 00003 EU 1998 4 29 HEEA0013731 1 19980402 A 6240 DL40438 INDICATOR BOLKMS 105 BO105S 5626006 EU ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 ROTOR NEEDLE READS ABOUT 3% HIGHER THAN N2 NEEDLES. 1 G 7 2 3U H3EU 1998042900004 19980429 00004 EU 1998 4 29 HEEA0013744 1 19980402 A 2422 SS120 STATIC INVERTER BOLKMS 117 BK117B1 5626012 EU AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 109 7198 STATIC INVERTER INOPERATIVE. 1 G 7 2 3U H13EU 1998042900005 19980429 00005 EU 1998 4 29 HEEA0013820 1 19980402 A 6240 KDW02 RPM WARNING BOX BOLKMS 105 BO105S 5626006 EU M/R MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 AUDIO HORN BEEPS LOW. 1 G 7 2 3U H3EU 1998042900006 19980429 00006 EU 1998 4 29 HEEA0013823 1 19980402 A 6240 KDW021 RPM WARNING BOX BOLKMS 105 BO105S 5626006 EU ROTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 ROTOR LIGHTS INOPERATIVE. 1 G 7 2 3U H3EU 1998042900007 19980429 00007 EU 1998 4 29 HEEA0013824 1 19980402 A 3340 A413AHDADF1428 POWER SUPPLY BOLKMS 105 BO105S 5626006 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 86CH S557 STROBE LIGHT INOPERATIVE. 1 G 7 2 3U H3EU 1998042900008 19980429 00008 EU 1998 4 29 HEEA0013828 1 19980402 A 3340 1179203903 POWER SUPPLY BOLKMS 117 BK117B1 5626012 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 217UC 7152 POWER SUPPLY INOPERATIVE. 1 G 7 2 3U H13EU 1998042900009 19980429 00009 1998 4 29 HEEA0013829 4 19980402 A 3414 58023060 INDICATOR BOLKMS 117 BK117A3 5626015 EU AIRSPEED INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 AIRSPEED INDICATOR LIGHTS INTERMITTENT. 1 G 7 2 3U H13EU 1998042900010 19980429 00010 1998 4 29 HEEA0013838 4 19980403 A 3457 0845000000 GPS SKYNAV5000 BOLKMS 117 BK117B1 5626012 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 GPS INOPERATIVE. FOUND UNIT NOT PICKING UP ANY SIGNALS; ALSO ENT BUTTON IS VERY INTERMITTENT. 1 G 7 2 3U H13EU 1998042900011 19980429 00011 WP 1998 4 29 UPS98826361 1 19980404 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 CORROSION ON INNER DOUBLER BELOW EXT AIR CONDITIONING RECEPTACLE ON RT SIDE ABOVE FWD E/E COMP. REMOVED CORROSION ON IN NER DOUBLER. ACCOMPLISHED EO DC8-5330-8942-D INTERM REPAIR. 2 L 7 4 4F RT 4A25 1998042900012 19980429 00012 SO 1998 4 29 SWIA971146 1 19980309 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LAVATORY CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 CENTER CABIN FLOOR BUTT STRAP FRAME 38 AFT (NEAR LAVATORY) HAS CORROSION. REMOVED AND REPLACED CENTER CABIN FLOOR BUTT STRAP AT FRAME 38, IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998042900013 19980429 00013 SO 1998 4 29 SWIA971147 1 19980309 A 5210 BOLT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE PAX DOOR LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 CORROSION AND LOOSENESS IN ATTACH BOLT, LOWER END OF LOWER AFT HANDRAIL SUPPORT ARM. REPLACED HARDWARE, IAW MM 52-10-00 . 2 L 7 2 4T 4 T RT A31SO E20NE 1998042900024 19980429 00024 EU 1998 4 29 JBXA980035 1 19980328 A 2720 703853 MANIFOLD FOKKER F28 F28MK0100 4990807 EU RUDDER FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 106ML 2914 11477 RDU - FLT 375 - SYSTEM NR 2 RUDDER FAULTED. REMOVED AND REPLACED RUDDER MANIFOLD IAW F-100 MM 27-22-01, OPS CHECK GOOD. (M) 2 L 7 2 4F RT 1998042900025 19980429 00025 NM 1998 4 29 98UAL900141 1 19980407 A 5101 STRUCTURE BOEING 777 777222 1385219 NM PWA 4084 PW4084 NE AIRFRAME VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 786UA 26938 AIRCRAFT HAD AIRFRAME VIBRATION AT FL220, 320K IAS. FLIG HT RETURNED TO MAI AND LANDED OVER WEIGHT. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998042900026 19980429 00026 WP 1998 4 29 AALA980580 1 19980321 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 959 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FLOORBOARD SUPPORT BRACKET CORRODED AT STATION 959. REMOVED AND REPLACED BRACKET PER SRM 51-00-05. (M) 2 L 7 3 4F A22WE 1998042900419 19980429 00419 SW 1998 4 29 HEEA0012517 1 19980106 A 6710 206062721109 ACTUATOR BELL 206 206L1 1182107 SW M/R CONT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5737T 45454 ACTUATOR WORKS INTERMITTENTLY, WILL NOT ADJUST. 1 G 7 1 3U H2SW 1998042900420 19980429 00420 SW 1998 4 29 HEEA0012518 1 19980106 A 3340 A490A POWER SUPPLY WHELEN BELL 206 206L1 1182107 SW STROBE WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 16938 45157 POWER SUPPLY VERY WEAK. 1 G 7 1 3U H2SW 1998042900421 19980429 00421 NE 1998 4 29 HEEA0012519 1 19980106 A 3150 7655001001103 CAUTION PANEL SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 31217 760229 CAUTION PANEL NO OUTPUT ON PIN "S" ON TEST (LANDING GEAR PANEL LIGHTS WILL NOT PUSH TO TEST) 1 G 7 2 3U H1NE 1998042900422 19980429 00422 1998 4 29 HEEA0012520 4 19980106 A 2210 7611113 AMPLIFIER SKRSKY S76 S76A 8143006 NE YAW SLICE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S 760035 YAW SLICE AMP CAUSING ACTUATOR TO DEFLECT FULL RIGHT. 1 G 7 2 3U H1NE 1998042900423 19980429 00423 NE 1998 4 29 HEEA0012521 1 19980106 A 7712 7645001078106 INDICATOR SKRSKY S76 S76A 8143006 NE DUAL TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 DUAL TORQUE INDICATOR WILL NOT ADJUST DOWN. 1 G 7 2 3U H1NE 1998042900424 19980429 00424 1998 4 29 HEEA0012522 4 19980106 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 COPILOT ATTITUDE INDICATOR PRECESSES. 1 G 7 2 3U H1NE 1998042900425 19980429 00425 1998 4 29 HEEA0012523 4 19980106 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 760077 VG CAUSES 10 ROLL TO RIGHT. 1 G 7 2 3U H1NE 1998042900426 19980429 00426 SW 1998 4 29 HEEA0012524 1 19980106 A 6320 205040231009 RING GEAR BELL 412 412 1182202 SW M/R GR BOX CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 FRETTING CORROSION ON FLANGE SURFACE AND PILOT DIAMETERS (UPPER AND LOWER) 1 G 7 2 4U H4SW 1998042900427 19980429 00427 1998 4 29 HEEA0012525 4 19980106 A 2200 2593996333 TARSYN 333 BELL 412 412 1182202 SW AUTO FLIGHT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 2258F 33073 FAILED TEST 3.1 ON SST BENCH. 1 G 7 2 4U H4SW 1998042900428 19980429 00428 1998 4 29 HEEA0012526 4 19980106 A 3420 4020936903 GYRO BELL 412 412 1182202 SW 3 AXIS IND FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 GYRO BLEW CIRCUIT BREAKER ON SST. 1 G 7 2 4U H4SW 1998042900429 19980429 00429 1998 4 29 HEEA0012527 4 19980106 A 3425 066304604 INDICATOR KI525A HUGHES 269 269C 4470504 WP COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 102LU S1548 HSI CARD INTERMITTENTLY STICKS IN SLAVE MODE. 1 G 7 1 3O 4H12 1998042900430 19980429 00430 SW 1998 4 29 HEEA0012528 1 19980106 A 7810 212061201011 EJECTOR BELL 412 412 1182202 SW LT EXH CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 LT EJECTOR ASSY HAS CRACK AROUND SUPPORTS. 1 G 7 2 4U H4SW 1998042900431 19980429 00431 SW 1998 4 29 HEEA0012529 1 19980106 A 2432 214175379103 CHARGER BELL 214 214ST 1182106 SW BATTERY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 BATTERY SYSTEM LIGHT REMAINS ON. 2 G 7 2 4U H10SW 1998042900432 19980429 00432 1998 4 29 HEEA0012530 4 19980106 A 3424 214075244001 RATE GYRO BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 RATE GYRO SHOWS FULL LEFT TURN ALL THE TIME. 2 G 7 2 4U H10SW 1998042900433 19980429 00433 SW 1998 4 29 HEEA0012531 1 19980106 A 2822 164A1681 PUMP BELL 412 412 1182202 SW FUEL BOOST FAILED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 141PH 33197 NR 2 FUEL TRANSFER LIGHT ON WOULD NOT GO OUT. 1 G 7 2 4U H4SW 1998042900434 19980429 00434 SW 1998 4 29 HEEA0012532 1 19980106 A 2432 214175379103 CHARGER BELL 214 214ST 1182106 SW BATTERY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 BATTERY NOT CHARGING. 2 G 7 2 4U H10SW 1998042900435 19980429 00435 NE 1998 4 29 HEEA0012533 1 19980106 A 2430 6013211 EMERGENCY POWER SKRSKY S76 S76A 8143006 NE DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 707AE 760276 EMERGENCY POWER FAILED. LIGHTS DO NOT COME ON. DEFECTIVE CELLS. 1 G 7 2 3U H1NE 1998042900436 19980429 00436 NE 1998 4 29 HEEA0012534 1 19980106 A 3340 A413AHDACF1428 POWER SUPPLY SKRSKY S76 S76A 8143006 NE STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 POWER SUPPLY INOPERATIVE. 1 G 7 2 3U H1NE 1998042900437 19980429 00437 SW 1998 4 29 HEEA0012535 1 19980106 A 6710 204060762103 ACTUATOR BELL 412 412 1182202 SW M/R CONTROL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6559Z 36019 ACTUATOR WILL NOT HOLD BEEP RANGE ADJUSTMENT. 1 G 7 2 4U H4SW 1998042900438 19980429 00438 SW 1998 4 29 HEEA0012536 1 19980106 A 2822 205060606003 PUMP BELL 412 412 1182202 SW FUEL BOOST FAILED E HEEA K NONE J WARNING INDICATION NR NOT REPORTED 1 SW 03 141PH 33197 BOOST PUMP LIGHT COMES ON IN FLIGHT. 1 G 7 2 4U H4SW 1998042900439 19980429 00439 SW 1998 4 29 HEEA0012537 1 19980106 A 6320 222375077111 TRANSMITTER BELL 214 214ST 1182106 SW M/R GR BOX FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 INDICATES HIGH AND ALSO SHOWS 10-20 PSI STATIC. 2 G 7 2 4U H10SW 1998042900440 19980429 00440 SW 1998 4 29 HEEA0012538 1 19980106 A 7722 212075067105 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 ITT INDICATOR READS LOW THROUGHOUT SCALE. 1 G 7 2 4U H4SW 1998042900441 19980429 00441 1998 4 29 HEEA0012539 4 19980106 A 3420 4020936903 GYRO BELL 412 412 1182202 SW 3 AXIS INDICATOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 3 AXIS GYRO INDICATOR CAUSES KICKS IN PITCH AND ROLL IN AIRCRAFT. 1 G 7 2 4U H4SW 1998042900442 19980429 00442 SW 1998 4 29 HEEA0012540 1 19980106 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893P 33012 TRIPLE TACH INDICATOR HAS LOOSE PARTS INSIDE. 1 G 7 2 4U H4SW 1998042900443 19980429 00443 1998 4 29 HEEA0012541 4 19980106 A 2210 7000299901 AUTOPILOT CONTRO BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 AUTOPILOT CONTROL HP1 AND HP2 LIGHTS ARE TOO DIM WHEN INSTRUMENT LIGHTS ARE DIMMED. 1 G 7 2 4U H4SW 1998042900444 19980429 00444 1998 4 29 HEEA0012542 4 19980106 A 2211 4025008918 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5759N 33002 AFCS COMPUTER FAILED TEST 8.3 ON SST BENCH TWICE. 1 G 7 2 4U H4SW 1998042900446 19980429 00446 SW 1998 4 29 HEEA0012545 1 19980109 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 53038 FOUND DISC PACK CRACKED ON DAILY INSPECTION. 1 G 7 1 3U O H2SW 1998042900447 19980429 00447 SW 1998 4 29 HEEA0012546 1 19980109 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 DISC COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998042900448 19980429 00448 SW 1998 4 29 HEEA0012547 1 19980109 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 DISC COUPLING CORROSION BEYOND LIMITS. 1 G 7 1 3U O H2SW 1998042900449 19980429 00449 SW 1998 4 29 HEEA0012548 1 19980109 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 DISC COUPLING HAS GAP BETWEEN DISCS BEYOND LIMITS. 1 G 7 1 3U O H2SW 1998042900450 19980429 00450 SW 1998 4 29 HEEA0012549 1 19980109 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DISK COUPLING HAS CORROSION AND PITS CAUSING DISCS TO SPREAD (GAPS BETWEEN DISC STACK) 1 G 7 1 3U O H2SW 1998042900451 19980429 00451 SW 1998 4 29 HEEA0012550 1 19980109 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 53038 DISC COUPLING HAS CRACKED DISC ON THE FRONT AND REAR BETWEEN BOLT HOLES 1 G 7 1 3U O H2SW 1998042900452 19980429 00452 SW 1998 4 29 HEEA0012551 1 19980109 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 NR 1 TAIL ROTOR DRIVESHAFT COUPLING DISC CRACKED. 1 G 7 1 3U O H2SW 1998042900453 19980429 00453 SW 1998 4 29 HEEA0012552 1 19980109 A 6400 222012130001 IDLER BELL 230 230 1182149 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 IDLER BEARING HAS PLAY. 1 G 7 2 3U NC H9SW 1998042900454 19980429 00454 SW 1998 4 29 HEEA0012555 1 19980109 A 6220 222310117105 SPRING BELL 230 230 1182149 SW M/R FLAP DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 M/R FLAPPING ELASTOMER CRACKING AND DETERIORATED. SERIAL NUMBERS REMOVED LK0092 AND LK0067. 1 G 7 2 3U NC H9SW 1998042900455 19980429 00455 EU 1998 4 29 HEEA0012556 1 19980109 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 ANTI COLL LIGHT INOPERATIVE. 1 G 7 1 3U H9EU 1998042900456 19980429 00456 SW 1998 4 29 HEEA0012557 1 19980109 A 3212 206050247131 FLOAT COVER BELL 407 407 SW FLOAT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FLOAT COVER ASSY END CAPS WORN. 1 G 7 1 3U O H2SW 1998042900457 19980429 00457 SW 1998 4 29 HEEA0012558 1 19980109 A 3212 206050247137 FLOAT COVER BELL 407 407 SW FLOAT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FLOAT ASSY END CAPS WORN. 1 G 7 1 3U O H2SW 1998042900458 19980429 00458 1998 4 29 HEEA0012559 4 19980112 A 3413 212070239003 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. 2 G 7 2 4U H10SW 1998042900459 19980429 00459 1998 4 29 HEEA0012560 4 19980112 A 3413 212070239003 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. 2 G 7 2 4U H10SW 1998042900460 19980429 00460 1998 4 29 HEEA0012561 4 19980112 A 3413 212070239003 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. 2 G 7 2 4U H10SW 1998042900461 19980429 00461 1998 4 29 HEEA0012562 4 19980112 A 3413 212070239003 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. 2 G 7 2 4U H10SW 1998042900462 19980429 00462 1998 4 29 HEEA0012563 4 19980112 A 3413 RC30VIL2 INDICATOR BELL 214 214ST 1182106 SW VERT SPEED DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 VERT SPEED INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. TIME SINCE REPAIR 0:00. 2 G 7 2 4U H10SW 1998042900463 19980429 00463 1998 4 29 HEEA0012564 4 19980112 A 3413 RC30VIL2 INDICATOR BELL 214 214ST 1182106 SW VERT SPEED DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 VERT SPEED INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. TIME SINCE REPAIR 0:00. 2 G 7 2 4U H10SW 1998042900464 19980429 00464 1998 4 29 HEEA0012565 4 19980112 A 3413 RC30VIL2 INDICATOR BELL 214 214ST 1182106 SW VERT SPEED DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. 2 G 7 2 4U H10SW 1998042900465 19980429 00465 1998 4 29 HEEA0012566 4 19980112 A 3413 RC30VIL2 INDICATOR BELL 214 214ST 1182106 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 INDICATOR NEEDS TO MODIFIED PER S/B 214-97-79. 2 G 7 2 4U H10SW 1998042900466 19980429 00466 SW 1998 4 29 HEEA0012567 1 19980113 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 65 53072 NR 1 T/R DRIVE SHAFT COUPLING DISC CRACKED. 1 G 7 1 3U O H2SW 1998042900467 19980429 00467 SW 1998 4 29 HEEA0012568 1 19980113 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FOUND DISC PACK CRACKED ON DAILY INSPECTION. 1 G 7 1 3U O H2SW 1998042900468 19980429 00468 SW 1998 4 29 HEEA0012569 1 19980113 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 ON DAILY INSPECTION FOUND NR1 DISC PACK CRACKED. 1 G 7 1 3U O H2SW 1998042900469 19980429 00469 SW 1998 4 29 HEEA0012570 1 19980113 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 326 53003 NR 7 (2ND FROM REAR) THOMAS COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998042900470 19980429 00470 SW 1998 4 29 HEEA0012571 1 19980113 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 CRACKED DISC ON OUTER DISC, 2ND FROM LAST PACK. 1 G 7 1 3U O H2SW 1998042900471 19980429 00471 SW 1998 4 29 HEEA0012572 1 19980113 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 CRACKED DISC ON OUTER DISC. LAST DISC PACK NEAR T/R GEARBOX. 1 G 7 1 3U O H2SW 1998042900472 19980429 00472 EU 1998 4 29 HEEA0012573 1 19980113 A 2930 806966 ELEMENT SNIAS 350 AS350B2 8680813 EU HYD SYS DIRTY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 HYD FILTER ELEMENT NEEDS TO BE CLEANED. 1 G 7 1 3U H9EU 1998042900473 19980429 00473 EU 1998 4 29 HEEA0012574 1 19980113 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 92 3004 PITCH CONTROL ROD BEARING HAS WEAR. 1 G 7 1 3U H9EU 1998042900474 19980429 00474 EU 1998 4 29 HEEA0012575 1 19980113 A 6220 117775P STARFLEX SNIAS 350 AS350B2 8680813 EU M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 STARFLEX BALL JOINT WORN TEFLON AND SEAL UNBONDED. 1 G 7 1 3U H9EU 1998042900475 19980429 00475 SW 1998 4 29 HEEA0012576 1 19980113 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2014K 7147 33020 UNABLE TO TRACK AND BALANCE BLADE. 1 G 7 2 4U H4SW 1998042900476 19980429 00476 SW 1998 4 29 HEEA0012577 1 19980113 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 8411 33022 BLADE HAS SKIN CRACK NEAR THE INBOARD TRIM TAB ON THE LOWER SURFACE WHERE A REPAIR WAS DONE PREVIOUSLY AT COMPOSITE TECH NICS WITH A TOTAL TIME OF 7978:15. 1 G 7 2 4U H4SW 1998042900477 19980429 00477 GL 1998 4 29 HEEA0012578 2 19980113 A 7250 23038218 NOZZLE 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE CAT33006 S787 CAE822541F ENGINE REMOVED DUE TO OIL STARVATION. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR1 NOZZLE INNER BAND THROUGH DIAPHRAGM BRONZE FILLET AS MARKED. 1 G 7 2 3U 3 U H3EU E4CE 1998042900478 19980429 00478 GL 1998 4 29 HEEA0012579 2 19980113 A 7250 23055438 NOZZLE 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 615 CAT90562 760181 CAE890607S ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR 2 NOZZLE VANES AND KEY WELDS. 1 G 7 2 3U 3 U H1NE E1GL 1998042900479 19980429 00479 SW 1998 4 29 HEEA0012581 1 19980114 A 6320 412040111103 SEAL BELL 412 412 1182202 SW M/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 MAGNETIC RING HAS NO MAGNETISM. 1 G 7 2 4U H4SW 1998042900480 19980429 00480 NM 1998 4 29 CALA9800086 1 19980118 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14341 23579 INSPECTION FOUND FLOORBEAM CORRODED AROUND SCREW HOLES AT STA 947, LBL 6. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1998042900481 19980429 00481 NM 1998 4 29 CALA9800087 1 19980118 A 3350 38931002 BATTERIES MARATHON BOEING 727 727232 1384082 NM AFT AIRSTAIR DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 511PE 20634 INSPECTION FOUND AFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1998042900482 19980429 00482 EU 1998 4 29 9801073204 1 19980116 A 2750 RETRACT MECH AIRBUS 320 A320211 3930320 EU TE FLAPS MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 304US 40 DURING APPROACH WHEN FLAPS POSITION ONE SELECTED, RECEIVED F/CTL FLAPS LOCKED MESSAGE. DIVERTED TO IAD AND LANDED WITHO UT INCIDENT. MAINTENANCE RIGGED FLAP SYSTEM, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998042900483 19980429 00483 WP 1998 4 29 9801089916 1 19980119 A 7312 FUEL HEAT LIGHT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LT ENGINE ILLUMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 949N 47566 666365 DURING TAKEOFF ROLL AT 80 KNOTS, THE LEFT ENGINE FUEL HEAT LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE TESTED THE LEFT ENGINE FUEL HEAT SYSTEM, OPERATIONAL CHECK WAS NORMAL. PROBLEM COULD NOT BE DUPLICAT ED. 2 L 7 2 4F 4 F A6WE E2EA 1998042900484 19980429 00484 NE 1998 4 29 9801091145 2 19980115 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 OVER TEMP A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 145US 46754 686117 DURING THE LANDING ROLLOUT WHILE COMING OUT OF REVERSE THRUST, THE NR 3 ENGINE REACHED AN EGT OF 940C FOR ONE SECOND. T HE ENGINE WAS SHUT DOWN. MAINTENANCE PERFORMED AN OVERTEMP INSPECTION PER MM 72-00-00, PG 233 WITH NO DEFECTS. THE BOR ESCOPE WAS DEFERRED FOR 80 HOURS AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1998042900485 19980429 00485 NE 1998 4 29 9801101152 2 19980118 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 01 152US 46761 686159 AT TOP OF DESCENT WITH POWER REDUCTION, THE NR 1 ENGINE AUDIBLY COMPRESSOR STALLED. THERE WAS A SLIGHT VIBRATION AND RI SING EGT. THE ENGINE WAS SHUT DOWN WITH A MAXIMUM EGT OF 690C. RESTART ATTEMPT WAS SUCCESSFUL AND THE ENGINE OPERATION WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER MM 71-00-00 FOR A TYPE A STALL WITH N O DEFECTS. ENGINE RUN WAS NORMAL. THE AIRCRAFT RETURNED TO SERVICE WITH A FIVE CYCLE BORESCOPE DEFERRAL. 2 L 7 3 4F 4 F A22WE E20EA 1998042900486 19980429 00486 WP 1998 4 29 9801119877 1 19980116 A 3222 STRUT DOUG DC9 DC951 3022051 WP NLG LOW PRESSURE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 786NC 48148 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION ACCOMPANIED BY TAKEOFF WARNING HORN AND LOSS OF PRESSUR IZATION. CREW RECYCLED GEAR AND GEAR INDICATION AND SYSTEM FUNCTIONS RETURNED TO NORMAL. FLIGHT WAS CONTINUED TO DESTI NATION AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NOSE GEAR STRUT SCHRADER VALVE AND SERVICED STRUT TO PROPER LEVEL. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042900487 19980429 00487 1998 4 29 9801129923 4 19980119 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 927RC 38360 5872 47469 DURING LINE MAINTENANCE INSPECTION, FOUND GALLEY DOOR EVACUATION SLIDE BOTTLE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998042900488 19980429 00488 WP 1998 4 29 9801139944 1 19980118 A 3310 LIGHT DOUG DC9 DC931 3022065 WP RT COCKPIT FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 01 1309T 47316 DURING TAXI-OUT, AN ACRID ELECTRICAL SMOKE DEVELOPED IN COCKPIT. FLUORESCENT LIGHT CIRCUIT BREAKER L-20 POPPED. AIRCRA FT RETURNED TO GATE. MAINTENANCE SUSPECTED SHORT IN BALLAST OR WIRING TO FIRST OFFICER'S FLUORESCENT LIGHTS. DEFERRED LIGHTS PER MEL 33-1. 2 L 7 2 4F A6WE 1998042900489 19980429 00489 1998 4 29 9801149902 4 19980119 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP PAX DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 38451 3669 47073 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EVACUATION SLIDE LOW ON PRESSURE. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998042900490 19980429 00490 WP 1998 4 29 9801159965 1 19980103 A 5320 PRESS PANEL DOUG DC9 DC931 3022065 WP BS 83 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 911RW 47149 DURING L-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 83. REPAIRED PER EA 99-153474. 2 L 7 2 4F A6WE 1998042900491 19980429 00491 WP 1998 4 29 9801169885 1 19980107 A 5320 JAMB DOUG DC9 DC951 3022051 WP BS 1167 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 401EA 47682 DURING H-CHECK, FOUND CRACK IN AFT VENTRAL DOOR JAMB WEB UNDER SCUFF PLATE FS 1167. REPAIRED PER EA 98-153442. 2 L 7 2 4F RT A6WE 1998042900492 19980429 00492 WP 1998 4 29 9801179154 1 19980103 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 69.55 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8913E 45830 DURING PERIODIC CHECK, FOUND FUSELAGE SKIN CRACKED AT FS 69.55, RBL 14 TO 20. REPAIRED PER EA 91-154152. 2 L 7 2 4F A6WE 1998042900493 19980429 00493 NM 1998 4 29 9801186718 1 19980117 A 5320 FITTING BOEING 747 747251F 1384898 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR LONGERONS 38R, 42R, 44R, 46R, 48R, 49R, 50R, AND 51R AT FS 23 60. REPLACED FITTINGS PER BOEING DRAWING 65B02699. 2 L 7 4 4F A20WE 1998042900494 19980429 00494 NM 1998 4 29 9801196718 1 19980117 A 5320 FITTING BOEING 747 747251F 1384898 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND CORROSION ON END FITTINGS FOR LONGERONS 38L, 40L, 42L, 44L, 46, 48L, 49L, 50L, AND 51L AT F S 2360. REPLACED FITTINGS PER BOEING DRAWING 65B02699. 2 L 7 4 4F A20WE 1998042900500 19980429 00500 SO 1998 4 29 COMA9810025 1 19980116 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR TORN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 248CA 120228 AIRCRAFT WOULD NOT PRESURIZE AFTER TAKEOFF. REPLACED CARGO DOOR SEAL. 2 L 7 2 4T RT A31SO 1998042900501 19980429 00501 EA 1998 4 29 COMA9860015 1 19980117 A 2613 356024310 ELEMENT CNDAIR CL600 CL6002B19 EA LT PYLON FALSE WARN A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 929CA 7035 ANTI-ICE DUCT LEAK WARNING MESSAGE. REPLACED THE LEFT ENGINE PYLON SENSING ELEMENT. 2 L 7 2 4F RT A21EA 1998042900502 19980429 00502 EA 1998 4 29 COMA9860016 1 19980117 A 3230 16215103 BRACKET CNDAIR CL600 CL6002B19 EA NLG WOW SWITCH BENT A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 931CA 7037 NLG DID NOT RETRACT. REPLACED BENT WEIGHT ON WHEELS PROXIMITY SENSOR BRACKET. 2 L 7 2 4F RT A21EA 1998042900503 19980429 00503 EA 1998 4 29 COMA9860017 1 19980118 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 947CA 7077 NLG DID NOT RETRACT. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 1998042900504 19980429 00504 EA 1998 4 29 COMA9860018 1 19980118 A 2613 356024310 OVERHEAT ELEMENT CNDAIR CL600 CL6002B19 EA LT PYLON FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 929CA 5 7035 LEFT 14TH STAGE DUCT LEAK MESSAGE. REPLACED THE LEFT HAND ENGINE PYLON BLEED LEAK SENSING ELEMENT. 2 L 7 2 4F RT A21EA 1998042900505 19980429 00505 EA 1998 4 29 COMA9860019 1 19980116 A 5610 NP1393221 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 946CA 4501 7072 PILOTS SIDE WINDSHIELD SHATTERED. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 1998042900506 19980429 00506 NM 1998 4 29 SWAA980031 1 19980102 A 2910 LINE BOEING 737 7373H4 1384600 NM B-HYD SYST RUPTURED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 675AA 23253 EN ROUTE, EXPERIENCED B-SYSTEM HYDRAULIC QUANTITY LOSS. AIRCRAFT DIVERTED TO ONT AND MADE AN UNEVENTFUL LANDING. REMOV ED AND REPLACED RUPTURED LINE TO B-ACOUSTIC MUFFLER, CHECKED CASE DRAIN FILTERS AND OP CHECKED PUMP PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042900507 19980429 00507 NM 1998 4 29 SWAA980032 1 19980103 A 2997 WIRE BOEING 737 7373H4 1384600 NM B-HYD SYST CHAFED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 349SW 24408 EN ROUTE, EXPERIENCED B-SYSTEM HYDRAULIC OVERHEAT WARNING LIGHT. AIRCRAFT DIVERTED TO DAL AND MADE AN UNEVENTFUL LANDIN G. REPAIRED CHAFED TEMP SENSOR WIRING AT SUPPLY LINE. 2 L 7 2 4F RT A16WE 1998042900508 19980429 00508 NM 1998 4 29 SWAA980033 1 19980104 A 2424 948F4582 GCU BOEING 737 7373Q8 1384670 NM NR 1 ENGINE INOPERATIVE A SWAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 SW 07 687SW 23388 EN ROUTE, NR 1 ENGINE GENERATOR DROPPED OFF LINE. APU GEN WAS ALREADY ON MEL. AIRCRAFT DIVERTED TO PHX AND MADE AN UNE VENTFUL LANDING. REMOVED AND REPLACED NR 1 GENERATOR CONTROL UNIT PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042900509 19980429 00509 NM 1998 4 29 SWAA980034 1 19980111 A 5610 5893543109 WINDOW BOEING 737 737317 138447P NM LT COCKPIT NOT SEALED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 698SW 23176 DURING CLIMBOUT, NOTED VERY LARGE AIR LEAK AT CAPT NR 1 WINDOW. AIRCRAFT RETURNED TO LAS AND MADE AN UNEVENTFUL LANDING . REMOVED AND REPLACED WINDOW ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042900510 19980429 00510 NM 1998 4 29 SWAA980035 1 19980112 A 3350 6104781 BATTERY BOEING 737 7373Q8 1384670 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED TERMINAL CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED CHARGER AND BAT TERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042900511 19980429 00511 1998 4 29 SWAA980036 4 19980112 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM R1 DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 AT GATE, FWD SERVICE DOOR SLIDE ACCIDENTALLY DEPLOYED. REMOVED AND REPLACED SLIDE ASSEMBLY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042900512 19980429 00512 NM 1998 4 29 SWAA980037 1 19980114 A 3350 A3061095102 LIGHT BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 512SW 24189 DURING ROUTINE SLIDE DISASSEMBLY AND CHECK, FOUND ONE EMERGENCY SLIDE LIGHT INOP ON LIGHT STRIP. REMOVED AND REPLACED L IGHT PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042900513 19980429 00513 NM 1998 4 29 QXEA9800032 1 19980117 A 5280 85420006001 BUSHINGS DHAV DHC8 DHC8102 2809003 NM MLG DOOR WORN A QXEA K NONE O OTHER CR CRUISE 1 NM 09 840PH 12755 2289 74 NR 1 FORWARD MAIN LANDING GEAR DOOR REMAINED OPEN 3 DURING FLIGHT. DOOR IS LOOSE ON THE GROUND. MAINTENANCE FOUND FORW ARD LANDING DOOR BUSHINGS WORN. REPLACED DOOR. EXTENSION AND RETRACTION CHECK GOOD. 2 H 7 2 4T RT A13NM 1998042900514 19980429 00514 EU 1998 4 29 QXEA9800035 1 19980119 A 2120 AIR DISTRIBUTION FOKKER F28 F28MK4000 4990810 EU CABIN ODOR A QXEA K NONE O OTHER CR CRUISE 1 NM 09 491US 11156 WHEN TURNING UP COCKPIT PACK HEAT YOU GET AN OILY SMELL. FLIGHT ATTENDANT REPORTED SLIGHT HAZE IN CABIN. TURNED HEAT D OWN PROBLEM WENT AWAY. MAINTENANCE OPERATED PACK ON FULL WARM FOR THIRTY MINUTES. NO PROBLEMS NOTED. NO PARTS REPLACE D. 2 L 7 2 4F RT A20EU 1998042900515 19980429 00515 EU 1998 4 29 QXEA9800036 1 19980119 A 3350 1820 BULB GRIMES A42052 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 THE 28V OVERHEAD EMERGENCY LIGHT AT ROW 14 INOP. REPLACED BULB, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998042900516 19980429 00516 WP 1998 4 29 ABXA9800028 1 19980120 A 5320 991075521 CUSP WEB DOUG DOUG DC9 DC933F 302207A WP BS 955 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND RIGHT CUSP WEB AT FS 955 CRACKED APPROX 4 LONG. REPAIRED CUSP WEB IAW ABX REA D953-22256. 2 L 7 2 4F A6WE 1998042900517 19980429 00517 WP 1998 4 29 ABXA9800029 1 19980120 A 5312 99155581417 BLKHD STIFFENER DOUG DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT 996 AND LONGERON 14L LOWER FLANGE CRACKED. REPAIRED STIFFENER IAW DC9 S/B 53-166, SERVICE REWORK DWG J060110 VIEW V-V AND DACO DWG PL 9915558. 2 L 7 2 4F A6WE 1998042900518 19980429 00518 WP 1998 4 29 ABXA9800030 1 19980120 A 5312 9915558148 BLKHD STIFFENER DOUG DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT STA 996 AND LONGERON 14R LOWER FLANGE CRACKED. REPAIRED STIFFE NER IAW DC9 S/B 53-166, SERVICE REWORK DWG J060110 VIEW V-V AND DACO DWG PL 9915558. 2 L 7 2 4F A6WE 1998042900519 19980429 00519 WP 1998 4 29 ABXA9800031 1 19980119 A 5315 9922397501 FLOORBEAM DOUG DOUG DC9 DC933F 302207A WP BS 937 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND FLOORBEAM LOWER FLANGE CORRODED AT STA 937, BL 0.0. REPAIRED FLOORBEAM IAW ABX REA D53-22192MR. 2 L 7 2 4F A6WE 1998042900520 19980429 00520 WP 1998 4 29 ABXA9800032 1 19980119 A 5743 9955840505 FITTING DOUG DOUG DC9 DC933F 302207A WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND THE LEFT PORK-CHOP FITTING CORRODED. REPLACED FITTING IAW DC9 S/B 53-182 AND DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998042900521 19980429 00521 WP 1998 4 29 ABXA9800033 1 19980119 A 5720 9955840511 TRAP PANEL DOUG DOUG DC9 DC933F 302207A WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 DURING C-CHECK, FOUND LEFT TRAPEZODIAL PANEL UPPER HORIZONTAL FLANGE EXFOLIATED AND CRACKED. REPLACED TRAPEZODIAL PANEL IAW DC9 S/B 53-182 AND DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998042900522 19980429 00522 WP 1998 4 29 ABXA9800027 1 19980119 A 5610 1335096 SPRING DOUG DOUG DC8 DC861 3021952 WP RT COCKPIT BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 DURING PREFLIGHT, FOUND THAT THE FIRST OFFICER'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. REPLACED BROKEN AFT SPRING, WINDOW OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998042900523 19980429 00523 WP 1998 4 29 ABXA9800026 1 19980117 A 3350 60030431 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 944AX 4771 47550 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1998042900524 19980429 00524 NE 1998 4 29 ABXA9800034 2 19980118 A 7261 581167 FILTER DOUG DC8 DC863F 302198F WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 23 826AX 46061 DURING DESCENT WITH THROTTLE AT IDLE, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WITH AN OIL PRESSURE READING OF 25 PSI. SECURED NR 2 ENGINE. WINDMILLING OIL PRESS 7 PSI, N2-23 PERCENT, N1-14 PERCENT, EGT-70 DEG, AND EPR-1.00. REPLA CED MAIN OIL FILTER AND OIL PRESSURE RELIEF VALVE. CHECKED BREATHER PRESSURE IAW PRATT AND WHITNEY MANUAL 72-00 AND JT3 D OHM 72-00. OPS AND LEAK CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1998042900525 19980429 00525 WP 1998 4 29 MWEA98026 1 19980118 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200-256 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING C-CHECK, FOUND NR 4 CABIN SEAT TRACK CORRODED TO EXCESS AT FWD FS 200 TO 256. MTC REPAIRED IAW SRM 53-05 FIG 4F. 2 L 7 2 4F A6WE 1998042900526 19980429 00526 WP 1998 4 29 MWEA98027 1 19980118 A 5280 FASTENER DOUG DC9 DC932 3022066 WP NLG DOOR MISINSTALLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING C-CHECK, FOUND IMPROPER FASTENERS ON AFT NOSE GEAR DOOR. MTC REPAIRED IAW SRM 53-05 FIG 62 AND SRM 51-30-5. 2 L 7 2 4F A6WE 1998042900527 19980429 00527 WP 1998 4 29 MWEA98028 1 19980118 A 5400 ANGLE DOUG DC9 DC932 3022066 WP BS 1019 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING C-CHECK, FOUND 2 SMALL CRACKS THROUGH 2 RIVET HOLES ON RIGHT UPPER PYLON TO FUSELAGE ATTACH ANGLE AT FS 1019. MT C REPAIRED IAW 54-04 FIG 10. 2 L 7 2 4F A6WE 1998042900528 19980429 00528 WP 1998 4 29 MWEA98029 1 19980118 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 150 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING C-CHECK, FOUND FUSELAGE DENTED AT STATION 150 LONGERON 26L. MTC REPAIRED IAW SRM 53-04 FIG 38 SHEET 18 SRM 51-10 -3 AND SRM 51-30-2. 2 L 7 2 4F A6WE 1998042900529 19980429 00529 WP 1998 4 29 MWEA98030 1 19980118 A 5542 SKIN DOUG DC9 DC932 3022066 WP RUDDER DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 DURING C-CHECK, FOUND TWO DENTS ON RUDDER LEFT SIDE CENTER AFT. MTC REPAIRED IAW SRM 55-03 FIG 11 AND 55-40-1. 2 L 7 2 4F A6WE 1998042900530 19980429 00530 WP 1998 4 29 MWEA98031 1 19980119 A 5313 27778221 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, LONGERON 3R WAS FOUND CRACKED AT FS 756. REMOVED DAMAGED SECTION, FABRICATED REPAIR SEC IAW 53-02 FIG 1 8. INSTALLED REPAIR SEC IAW 51-30. 2 L 7 2 4F A6WE 1998042900531 19980429 00531 WP 1998 4 29 MWEA98032 1 19980119 A 5313 27779221 LONGERON DOUG DC9 DC932 3022066 WP CABIN CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 D-CHECK, LONGERON 2R AT FS 756 FOUND CRACKED. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SEC IAW 53-02, INS TALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998042900532 19980429 00532 WP 1998 4 29 MWEA98033 1 19980119 A 5313 S2912099 LONGERON DOUG DC9 DC932 3022066 WP CABIN DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, THE LONGERON 10 LEFT AT FS 965 HAS A DRILL STRIKE. REMOVED DAMAGED SECTION, FABRICATED REPAIR SECTIONS IAW SRM 53-02 FIG 18, INSTALLED REPAIR SECTIONS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998042900533 19980429 00533 WP 1998 4 29 MWEA98034 1 19980119 A 5311 S2777930 FRAME DOUG DC9 DC932 3022066 WP BS 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, CABIN FRAME AT STA 218 BETWEEN LONGERON 17L-18L CORRODED AND GROUND OUT. REMOVED DAMAGED SECTION OF FRA ME, FABRICATED AND INSTALLED REPAIR PER SRM 53-03 FIG 32. 2 L 7 2 4F A6WE 1998042900534 19980429 00534 WP 1998 4 29 MWEA98035 1 19980119 A 5320 7075T6063 SHEAR CLIP DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, THE AFT ACCESS COMP LEFT HAND CANTED FRAME 1089 BETWEEN LONG 7 AND 8 TIE BRACKET CRACKED AND CORRODED. R EMOVED CRACKED BRACKET AND FABRICATED SHEAR TIE IAW SRM 53-11-4. INSTALLED SHEAR TIE IAW SRM 51-30. 2 L 7 2 4F A6WE 1998042900535 19980429 00535 WP 1998 4 29 MWEA98036 1 19980107 A 5320 39203221 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, CORROSION WAS FOUND ON END CAP AT FS 996 LONGERON 28L. REMOVED, ORDERED AND INSTALLED NEW END CAP IAW S RM 51-30. 2 L 7 2 4F A6WE 1998042900536 19980429 00536 WP 1998 4 29 MWEA98037 1 19980107 A 5320 7075T6080 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 851-889 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, THE INTERCOSTAL AT LONGERON 29R FS 851 TO 889 WAS FOUND CORRODED. REMOVED AND FABRICATED INTERCOSTAL IA W SRM 53-11-3, INSTALLED INTERCOSTAL IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998042900537 19980429 00537 WP 1998 4 29 MWEA98038 1 19980119 A 5330 49125309 ACCESS PLATE DOUG DC9 DC932 3022066 WP FUSELAGE NOSE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, THE CAPTAINS WINDSHIELD WIPER MOTOR ACCESS PANEL IS CORRODED AROUND STEEL FASTENERS. REMOVED OLD ACCESS PLATE, ORDERED NEW PART AND DRILLED UP NEW PART, INSTALLED NEW ACCESS PLATE. 2 L 7 2 4F A6WE 1998042900538 19980429 00538 WP 1998 4 29 MWEA98039 1 19980119 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 851-889 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, AN INTERCOSTAL AT LONGERON 28R FS 851 TO FS 889 WAS FOUND CORRODED. REMOVED OLD INTERCOSTAL AND FABRICA TED REPLACEMENT INTERCOSTAL IAW 53-11-3, INSTALLED INTERCOSTAL IAW 51-30. 2 L 7 2 4F A6WE 1998042900539 19980429 00539 WP 1998 4 29 MWEA98040 1 19980119 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 851 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, A FRAME AT FS 851 LONGERON 26L TO 26R WAS FOUND CORRODED. REMOVED DAMAGED SECTION, FABRICATED REPAIR SE CTIONS IAW SRM 53-03 FIG 2A, INSTALLED REPAIR SECTIONS IAW SRM 51-30-5 AND RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998042900540 19980429 00540 WP 1998 4 29 MWEA98041 1 19980119 A 5320 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 408 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, THE SHEAR TIE ON FRAME AT FS 408 HAS CORROSION BETWEEN LONGERON 29L AND 29R. REMOVED DAMAGED SECTION, F ABRICATED REPLACEMENT SECTION OF SHEAR TIE IAW SRM 53-03 FIG 2A, INSTALLED SHEAR TIE IAW 51-30-2. 2 L 7 2 4F A6WE 1998042900541 19980429 00541 WP 1998 4 29 MWEA98042 1 19980119 A 5311 991961502 FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, FRAME AT FS 699 WAS FOUND CRACKED IN THE LWR OUTBD AFT POCKET RT SIDE. REMOVED DAMAGED FRAME AT STA 699 RT SIDE ORDERED AND INSTALLED NEW FRAME IAW DOUGLAS SB53-131. 2 L 7 2 4F A6WE 1998042900542 19980429 00542 WP 1998 4 29 MWEA98043 1 19980119 A 5320 9936579 BEAM DOUG DC9 DC932 3022066 WP BS 389 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, THE LWR FLANGE OF FLOORBEAM AT FS 389 FOUND TO BE CHAFFED, LOCATED RT ABOVE FWD CARGO DOOR. REMOVED DAM AGED AREA, FABRICATED REPAIR SEC IAW SRM 53-05 FIG 86, INSTALLED REPAIR SEC IAW SRM 53-05 AND 51-30. 2 L 7 2 4F A6WE 1998042900543 19980429 00543 WP 1998 4 29 MWEA98044 1 19980119 A 5330 59114023 SKIN DOUG DC9 DC932 3022066 WP L1 DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, FUSELAGE SKIN IS CRACKED AND GOUGED AT CUTOUT FOR L1 DOOR HOLD OPEN LOCK. STOP DRILLED CRACK IN CUTOUT, FABRICATED REPAIR DOUBLERS IAW SRM 53-04 FIG 24, INSTALLED REPAIR DOUBLERS IAW SRM 51-30. 2 L 7 2 4F A6WE 1998042900544 19980429 00544 WP 1998 4 29 MWEA98045 1 19980119 A 5330 5911427 SKIN DOUG DC9 DC932 3022066 WP BS 935 GROOVED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING D-CHECK, FUSELAGE SKIN FOUND TO BE GROOVED AT FS 935 LONGERON 15R WHERE RT PYLON LEADING EDGE ATTACHES. BLENDED AREA, OUT OF LIMITS. FAB REPAIR DOUBLERS IAW SRM 53-04 FIG 3A. INSTALLED REPAIR DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 1998042900545 19980429 00545 WP 1998 4 29 MWEA98066 1 19980119 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 980 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE LONGERON AT FS 980 17L WAS FOUND WITH ELONGATED HOLES. REMOVED DAMAGED SECTION OF LONGERON, FABRICATED REPAIR SECTI ON IAW SRM 53-02 FIG 18, INSTALLED REPAIR SECTION IAW 51-30. 2 L 7 2 4F A6WE 1998042900546 19980429 00546 WP 1998 4 29 MWEA98067 1 19980119 A 5210 WEB DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 A CRACK WAS FOUND ON THE FWD ENTRY DOOR VERTICAL WEB BETWEEN BEAM 4 AND 5. REMOVED DAMAGED PART, FABRICATED REPAIR PART PER DRAWING 9955763, INSTALLED REPAIR PART IAW SRM 51-30. 2 L 7 2 4F A6WE 1998042900547 19980429 00547 WP 1998 4 29 MWEA98068 1 19980119 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LONGERON 4L WAS FOUND CRACKED AT FUSELAGE STATION 160 AND FUSELAGE STATION 200. REMOVED DAMAGED LONGERON, ORDERED NEW P ART, INSTALLED NEW LONGERON IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998042900548 19980429 00548 WP 1998 4 29 MWEA98069 1 19980117 A 5210 BEAM DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 DURING C-CHECK, FOUND FWD ENTRY DOOR UPPER BEAM CRACKED ON FWD END IN RADIUS. MTC INSTALLED ANGLE REPAIR IAW SRM 52-05 FIG 31. 2 L 7 2 4F A6WE 1998042900549 19980429 00549 WP 1998 4 29 MWEA98070 1 19980118 A 5712 RIB DOUG DC9 DC932 3022066 WP WS 394 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 DURING C-CHECK, FOUND LEFT WING LEADING EDGE RIB AT STA XRS 394 CRACKED ON AFT LOWER LEG APPROX 2 .625 IN. MTC INSTALLE D ANGLE REPAIR IAW TELEX MISC DG 28/GLP. 2 L 7 2 4F A6WE 1998042900550 19980429 00550 WP 1998 4 29 MWEA98071 1 19980119 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 203ME 47673 CREW REPORTS, GALLEY DOOR SLIDE COVER FELL OFF. MTC INSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1998042900551 19980429 00551 WP 1998 4 29 MWEA98072 1 19980119 A 5720 INTERCOSTAL DOUG DC9 DC932 3022066 WP RT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 DURING C-CHECK, FOUND RT WING TRAILING EDGE WEB AND INTERCOSTAL ASSY CRACKED AFT OF OUTBD SPOILER PANEL REACTION ARM. M TC INSTALLED DOUBLER REPAIR IAW SRM 57-01 FIG 3 SHEET 2. 2 L 7 2 4F A6WE 1998042900552 19980429 00552 WP 1998 4 29 MWEA98073 1 19980119 A 5210 SKIN DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 DURING C-CHECK, FOUND FWD ENTRANCE DOOR HAS A .5 INCH CRACK ON SKIN ON OUTER LOWER EDGE. MTC INSTALLED DOUBLER REPAIR I AW SRM 52-05 FIG 32. 2 L 7 2 4F A6WE 1998042900553 19980429 00553 WP 1998 4 29 MWEA98074 1 19980120 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 817 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DURING INSPECTION, FOUND .0625 INCH CRACK ON FUSELAGE SKIN AT STATION 817 ABOVE LONGERON 13L. MTC INSTALLED INTERIM REP AIR PER JO60143 AND PLACED ON C/O 3142 FOR PERMANENT REPAIR. 2 L 7 2 4F A6WE 1998042900554 19980429 00554 WP 1998 4 29 MWEA98075 1 19980119 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 203ME 47673 THE GALLEY SLIDE COVER CAME OFF. MTC RESECURED THE SLIDE AND COVER. 2 L 7 2 4F A6WE 1998042900555 19980429 00555 WP 1998 4 29 MWEA98076 1 19980120 A 5330 SKIN DOUG DC9 DC914 3022034 WP BS 817 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 DURING INSPECTION, FOUND SKIN CRACK .0625 INCH IN LENGTH AT STA 817 LONGERON 13L FWD ROW OF APB. MTC INSTALLED DOUBLER REPAIR IAW SB 53-147R7 INTERIM SERVICE REWORK DRAWING JO60143. 2 L 7 2 4F A6WE 1998042900556 19980429 00556 NM 1998 4 29 DLM88980148 1 19980119 A 5350 530698500 RADOME DOUG MD88 MD88 3023688 NM FWD FUSELAGE COLLAPSED A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 918DE 49959 A/C EXPERIENCED LOUD POP AND THEN LOUD RUSH OF AIR NEAR COCKPIT EXTERIOR. PRESSURIZATION OK. RTB ATL WHERE TWR NOTIFIE D THE CREW THE RADOME HAD COLLAPSED. REMOVED AND REPLACED RADOME. INSPECTED BOTH ENGS FOR FOD AND AIRFRAME FOR DAMA GE, NONE NOTED. TESTED WX RADAR ALL CKS OK. ALL MTC COMPLETED PER M/M. 2 L 7 2 4F RT A6WE 1998042900557 19980429 00557 NM 1998 4 29 DLM88980152 1 19980119 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM RT HYD SYST CHAFED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 968DL 53161 LOST RT HYS SYSTEM IN FLT. FOUND PRESSURE FLEX LINE CHAFED THRU GOING TO HYD PRESSURE FILTER MODULE. REPLACED LINE, LE AK CHECK GOOD. 2 L 7 2 4F RT A6WE 1998042900558 19980429 00558 NM 1998 4 29 DLM88980158 1 19980119 A 2130 PRESSURIZATION DOUG MD88 MD88 3023688 NM CABIN MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 937DL 49810 ACFT WOULD NOT HOLD PRESSURIZATION ON TAKEOFF. CLIMBED TO 8,000 AUTO CONTROLLERS WERE NOT ILLUMINATED. RESEATED ALL DO ORS, RAN AUG VALVE CK PER PFHB PRESSURIZED A/C. NO LEAKS FOUND. 2 L 7 2 4F RT A6WE 1998042900559 19980429 00559 NM 1998 4 29 DL72S980159 1 19980119 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FOUND ON D1 LETTER CK, .25 INCH CRACK RT TORQUE BOX VERTICAL WEB LIGHTENING HOLE STA 1303. ROUTED OUT DAMAGED AREA PER MM 53-11-0. 2 L 7 3 4F A3WE 1998042900560 19980429 00560 NM 1998 4 29 DL72S980160 1 19980119 A 5320 WEB BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 533DA 22046 FOUND ON D1 LETTER CK, .5 INCH CRACK AT LT TORQUE BOX VERICAL WEB LIGHTENING HOLE STA 1263. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998042900561 19980429 00561 NM 1998 4 29 DL72W980162 1 19980119 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2821W 21059 AFT OVERHEAD LIGHTED SIGN EMERG LIGHT INOP. REPLACED RACK AND BATT PACK, OPN CK GOOD. 2 L 7 3 4F A3WE 1998042900562 19980429 00562 NM 1998 4 29 DL72W980163 1 19980119 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2821W 21059 AFT AISLE OVERHEAD LIGHTED SIGN EMERG LIGHT INOP. REPLACED RACK AND BATT PACK, OPN CK GOOD. 2 L 7 3 4F A3WE 1998042900563 19980429 00563 NM 1998 4 29 P5CA9800017 1 19980117 A 5755 PANEL BOEING 747 747124 1384874 NM NR 6 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 6 SPOILER PANEL DELAMINATED AT I/B AND O/B EDGE BAND. REMOVED DELAMINATION UPPER SKIN, FABRICATED AND BONDED REPAIR SKIN AND DOUBLER IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998042900564 19980429 00564 NM 1998 4 29 P5CA9800018 1 19980117 A 5755 PANEL BOEING 747 747124 1384874 NM NR 4 SPOILER SPLIT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 4 SPOILER PANEL, T/E HAS SPLIT IN REPAIR. CLEANED DAMAGED AREA APPLIED FILLER, BONDED CURED SANDED SMOOTH IAW SRM 51 -40-06. 2 L 7 4 4F A20WE 1998042900565 19980429 00565 NM 1998 4 29 P5CA9800019 1 19980117 A 5755 PANEL BOEING 747 747124 1384874 NM NR 11 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 11 SPOILER PANEL, UPPER SURFACE DELAMINATED. REMOVED DAMAGED AREA, APPLIED FILLER AND DOUBLED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998042900566 19980429 00566 NM 1998 4 29 P5CA9800020 1 19980117 A 5730 PANEL BOEING 747 747124 1384874 NM LT WING LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 L/W FLYING PANEL Z572 I/B BRACKET, O/B FASTENER HOLE DRILLED OVERSIZED FITTING. FITTING REPLACED IAW 51-10-01, HFEC CHE CK OK. 2 L 7 4 4F A20WE 1998042900567 19980429 00567 NM 1998 4 29 P5CA9800021 1 19980117 A 5755 PANEL BOEING 747 747124 1384874 NM NR 6 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 R/W PANEL FORWARD OF NR 6 SPOILER DELAMINATED. REPAIRED PANEL IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998042900568 19980429 00568 NM 1998 4 29 P5CA9800022 1 19980117 A 5753 FASTENERS BOEING 747 747124 1384874 NM LT TE MID FLAP MISINSTALLED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEFT WING INBOARD TRAILING EDGE MIDFLAP HAS BLIND FASTENER INSTALLED IN STRESS PANEL. REMOVED AND REPAIRED FASTENER IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998042900569 19980429 00569 NM 1998 4 29 P5CA9800023 1 19980118 A 5400 BRACE BOEING 747 747122 1384872 NM NR 1 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT SIDE OF DIAGONAL BRACE CHAFED FWD END OF NR 1 ENGINE PYLON. BLENDED OUT CHAFED AREA PER SRM 54-40-01. 2 L 7 4 4F A20WE 1998042900570 19980429 00570 NM 1998 4 29 P5CA9800024 1 19980116 A 5400 BRACE BOEING 747 747283B 1384867 NM NR 1 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 1 ENGINE PYLON SAIL PLANE AREA DIAGONAL BRACE CHAFED FWD RT SIDE. CHAFE OF DIAGONAL BRACE WITHIN LIMITS PER ZONE 3 S RM 54-40-01. EDDY CURRENT C/W PER NDT 54-40-08 PART 6, NO CRACKS FOUND. BLENDED OUT CHAFED AREA AND TREATED AREA PER S RM 54-40-01. 2 L 7 4 4F A20WE 1998042900571 19980429 00571 NM 1998 4 29 P5CA9800025 1 19980116 A 5400 BRACE BOEING 747 747238B 1384828 NM NR 1 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 1 ENGINE PYLON SAIL PLANE AREA DIAGONAL BRACE CHAFED 2 PLACES LT SIDE. CHAFE WITHIN LIMITS ZONE 3 PER SRM 54-40-01. EDDY CURRENT C/W PER NDT 54-40-08 PART 6. BLENDED OVER CHAFE AREA SHOT PEENED AND TREATED PER SRM 54-40-01. 2 L 7 4 4F A20WE 1998042900572 19980429 00572 NM 1998 4 29 P5CA9800026 1 19980116 A 5400 BRACE BOEING 747 747238B 1384828 NM NR 4 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 4 ENGINE PYLON SAIL AREA DIAGONAL BRACED CHAFED FWD END LT SIDE. CHAFE OF DIAGONAL BRACE WITHIN LIMITS PER 54-40-01 ZONE 3. EDDY CURRENT C/W, NO CRACKS NOTED PER NDT 54-40-08 PART 6. BLENDED OUT CHAFED AREA, SHOT PEENED AND TREATED PE R SRM 54-40-01. 2 L 7 4 4F A20WE 1998042900573 19980429 00573 NM 1998 4 29 P5CA9800027 1 19980119 A 3230 2670296 SEQUENCE VALVE BOEING 747 747123 1384873 NM NLG CRACKED A P5CA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 23 859FT 20326 ON MAINTENANCE WALK AROUND, FOUND NOSE LANDING GEAR OPEN DOOR SEQUENCE VALVE ASSEMBLY LEAKING. VALVE FOUND TO BE CRACKE D. REMOVED AND REPLACED NOSE GEAR, OPERATED DOOR SEQUENCE VALVE IAW BOEING M/M 32-34-07, LEAK AND OPERATIONAL CHECK OK. 2 L 7 4 4F A20WE 1998042900591 19980429 00591 EU 1998 4 29 VTZA98001 1 19980101 A 2424 51539002A GCU BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 EA 27 478UE 892 FLT 6372 - IAD-HLB - DURING TAXI, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT GENERATOR FELL OFF LINE AND WOULD NOT RESET. AIRCRAFT RETURNED TO GATE AND WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED GCU, OP S CHECK OK. AIRCRAFT WAS RELEASED AND RETUREND TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998042900638 19980429 00638 NM 1998 4 29 AALA984007 1 19980106 A 5320 FITTING BOEING 767 767223 1385123 NM BS 632 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 315AA 22317 AFW - FRAME SPLICE FITTING AT STA 632 RBL 48 HAD GOUGE BLENDED BEYOND SRM LIMITS. REPAIRED IAW MRB 767-1553. TST: 4,1 72 HOURS. CYCLES: 673. (X) 2 L 7 2 4F RT A1NM 1998042900657 19980429 00657 WP 1998 4 29 AALA980001 1 19980101 A 3350 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 451AA 49477 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS AND COACH WERE FOUND INOPERABLE. REPAIRED EMERGENCY FLOOR PATH LIGHTING WIRES AT SEAT ROWS 3E, 7D, AND 29D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998042900662 19980429 00662 SO 1998 4 29 ASOA98003 1 19980106 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A ASOA K NONE L NO TEST IN INSP/MAINT 1 SO 11 504AS 120278 ATL - UPON INSPECTION FOUND 4 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PAC K. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900663 19980429 00663 EU 1998 4 29 ASOA98004 1 19980107 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 8378 413 DURING SCHEDULED MAINTENANCE, FOUND SEAT TRACKS RIGHT CENTER AND RIGHT OUTER BETWEEN FRAMES 29 TO 36 UNSERVICEABLE DUE T O CORROSION. REMOVED AND REPLACED SEAT TRACKS IAW EO72-53-0029 AND SRMS 53-53-00, 51-21-17, 27, 31, 51-22-02 AND 51-25- 01, 02 (M) 2 H 7 2 4T RT A53EU 1998042900664 19980429 00664 EU 1998 4 29 98ZZZM174 1 19980107 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 8378 413 DURING SCHEDULED MAINTENANCE, FOUND SEAT TRACKS RIGHT CENTER AND RIGHT OUTER BETWEEN FRAMES 29 TO 36 UNSERVICEABLE DUE T O CORROSION. REMOVED AND REPLACED SEAT TRACKS IAW EO72-53-0029 AND SRMS 53-53-00, 51-21-17, 27, 31, 51-22-02 AND 51-25- 01, 02 (M) 2 H 7 2 4T RT A53EU 1998042900665 19980429 00665 EU 1998 4 29 MALA975925 1 19980129 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 99XJ 099 DURING INSPECTION, EMERGENCY OVERHEAD LIGHT INOP AT SEAT 2C. MAINTENANCE RELAMPED EMERGENCY LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900666 19980429 00666 NM 1998 4 29 MALA975926 1 19980202 A 3350 SIGN DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 864MA 363 DURING INSPECTION, FOUND EMERGENCY EXIT SIGN HAD FALLEN. MAINTENANCE RESECURED EMERGENCY EXIT SIGN, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042900667 19980429 00667 NM 1998 4 29 MALA975927 1 19980128 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 861MA 362 DURING INSPECTION, ONE FLOOR TRACK EMERGENCY LIGHTING INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998042900668 19980429 00668 NM 1998 4 29 MALA975928 1 19980201 A 3350 1317 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DURING INSPECTION, EMERGENCY LIGHTS IN ROW 3 AND 6 INOP. MAINTENANCE RELAMPED EMERGENCY LIGHTS, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042900669 19980429 00669 NM 1998 4 29 MALA975929 1 19980202 A 3350 1013073 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 830MA 337 DURING INSPECTION, ONE FLOOR TRACK LIGHT INOP. MAINTENANCE RELAMPED FLOOR TRACK LIGHT, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042900670 19980429 00670 NM 1998 4 29 MALA975930 1 19980201 A 3350 10126271 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 827MA 331 DURING INSPECTION, 1E CABIN SIDEWALL EMERGENCY EXIT LIGHT IS BROKEN. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998042900671 19980429 00671 NM 1998 4 29 MALA975931 1 19980202 A 3350 10126271 LENS DHAV DHC8 DHC8102 2809003 NM CABIN MISSING A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 827MA 331 DURING INSPECTION, EMERGENCY EXIT SIGN MISSING IN CABIN FROM LOWER WALL PANEL AT SEAT 4A. MAINTENANCE REPLACED LENS COV ER AT SEAT 4A, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998042900672 19980429 00672 NM 1998 4 29 MALA975932 1 19980202 A 3350 MS25231316 LAMP DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 826MA 330 DURING INSPECTION, EMERGENCY LIGHTS AT ROWS 1 AND 4 INOP. MAINTENANCE RELAMPED EMERGENCY LIGHTS, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998042900673 19980429 00673 EU 1998 4 29 MALA975933 1 19980131 A 3350 OL307115 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 98XJ 098 DURING INSPECTION, PASSENGER DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY EXIT LIGHT, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900674 19980429 00674 EU 1998 4 29 MALA975934 1 19980131 A 3697 WIRE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT AIR VLV BROKEN A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 27XJ 027 LEFT AIR VALVE LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPAIRED BROKEN WIRE AT CANNON P LUG ON SHUT OFF VALVE AT PIN NR 1, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998042900675 19980429 00675 EU 1998 4 29 MALA975935 1 19980131 A 3350 6104789 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 590MA 340B181 DURING INSPECTION EMERGENCY EXIT LIGHT TEST FAILED. MAINTENANCE REPLACED ALL 5 BATTERY PACKS FOR EMERGENCY LIGHTS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900676 19980429 00676 1998 4 29 MALA975936 4 19980131 A 3420 SWITCH SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 590MA 340B181 AFTER TAKEOFF, NR 2 EHSI AND EADI BOTH WENT BLANK, UNABLE TO RESET. MAINTENANCE REPLACED RIGHT AVIONICS SWITCH. NR 2 E HSI AND EADI OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900677 19980429 00677 EU 1998 4 29 MALA975937 1 19980201 A 3020 ND00752200 THERMAL CONTROL SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 590MA 340B181 DURING FLIGHT, RIGHT ENGINE INTAKE HEAT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THERMAL CONT ROL, RIGHT INTAKE OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900678 19980429 00678 EU 1998 4 29 MALA975938 1 19980201 A 7810 NF24668057 NOZZLE SAAB SF340 340B 7860101 EU LEFT EXHAUST FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 404XJ 340B404 DURING FLIGHT, THE LEFT INTAKE LIGHT CYCLES ON AND OFF, DUE TO WEATHER CONDITIONS. MAINTENANCE REPLACED LEFT EXHAUST NO ZZLE, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900679 19980429 00679 EU 1998 4 29 MALA975939 1 19980129 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119XJ 119 DURING INSPECTION, ONE EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED EMERGENCY LIGHT, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042900680 19980429 00680 EU 1998 4 29 MALA975940 1 19980126 A 2613 M250381209 HARNESS SAAB SF340 SF340A 7850100 EU RT TAIL PIPE FAILED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 114XJ 340A114 DURING INSPECTION, RIGHT TAIL PIPE HOT LIGHT IS BROKE. MAINTENANCE REWIRED THE RIGHT I/B DETECTORS, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042900681 19980429 00681 EU 1998 4 29 MALA975941 1 19980129 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 107XJ 340A107 DURING INSPECTION, EMERGENCY LIGHT INOP OVER SEATS 1 C/D AND 3 C/D. MAINTENANCE REPLACED POSITION 20LN BATTERY PACK, OP S CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900682 19980429 00682 EU 1998 4 29 MALA975942 1 19980128 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 107XJ 340A107 DURING INSPECTION, SEVERAL EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED ALL EMERGENCY LIGHT BATTERY PACKS, OPS CHECK GOO D. 2 L 7 2 4T RT A52EU 1998042900683 19980429 00683 NM 1998 4 29 MALA975943 1 19980201 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 827MA 331 DURING INSPECTION, EMERGENCY LIGHTING INOP. MAINTENACE RELAMPED EMERGENCY LIGHTING, ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998042900684 19980429 00684 NM 1998 4 29 MALA975944 1 19980129 A 2612 FIRE LOOP DHAV DHC8 DHC8102 2809003 NM APU MALFUNCTIONED A MALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 861MA 362 DURING POSTFLIGHT TAXI, AUTO SHUTDOWN OF APU, THE FIRE DETECTION LIGHT CAME ON. MAINTENANCE OPENED APU BAY, INSPECTED F OR OVERHEAT OR FIRE, NONE FOUND. APU FIRE DETECTION SYSTEM DEFERRED AS PER MEL 26-60. 2 H 7 2 4T RT A13NM 1998042900685 19980429 00685 EU 1998 4 29 MALA975945 1 19980130 A 2910 HYD SYST SAAB SF340 340B 7860101 EU MAIN HYD SYST REQD SERVICE A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 592MA 340B199 AFTER TAKEOFF, HYDRAULIC LIGHT CAME ON, QUANTITY WAS 0, CHECKED ACCUMULATORS, MAIN LOW, EMERGENCY NORMAL. HYDRAULIC PUM P CONTINUED TO RUN UNTIL TURNED OFF. DUE TO WEATHER FLIGHT WAS DIVERTED TO CWA. MAINTENANCE SERVICED HYDRAULIC SYSTEM, PERFORMED GEAR SWINGS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900686 19980429 00686 EU 1998 4 29 MALA975946 1 19980130 A 2910 SWIVEL ASSY SAAB SF340 SF340A 7850100 EU LT MLG BRAKE FAILED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 48XJ 048 CREW REPORTED THE HYDRAULICS FAILED DURING TAXI OUT TO THE RUNWAY. AIRCRAFT WAS PARTIALLY OFF RUNWAY, AIRCRAFT TOWED BA CK TO GATE. MAINTENANCE REPLACE THE LEFT OUT BOARD BRAKE SWIVEL ASSEMBLY. SERVICED SYSTEM, BLED BRAKE, ALL CHECKS GOOD . 2 L 7 2 4T RT A52EU 1998042900687 19980429 00687 NM 1998 4 29 K3HA980010 1 19980131 A 3350 07912 COVER BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 354PA 20624 EMERGENCY PATH LIGHTING SEAT ROW 5 LIGHT COVER IS MISSING. REINSTALLED SEAT COVER AT ROW 5. 2 L 7 3 4F A3WE 1998042900688 19980429 00688 NM 1998 4 29 SRAA98A0201 1 19980202 A 3350 LIGHT BOEING 747 747246F NM UPPER DECK BROKEN A SRAA K NONE L NO TEST IN INSP/MAINT 1 GL 23 744SJ 22245 DURING POST FLIGHT INSPECTION, FOUND EMERGENCY FLASH LIGHT SEAL BROKEN. RESAFETY UPPER DECK EMERGENCY FLASH LIGHT IAW A TA 25-00-00. 2 L 7 4 4F A20WE 1998042900689 19980429 00689 SO 1998 4 29 RAAA98E4005 1 19980204 A 5320 DOUBLER LKHEED 188 188C 5262604 SO BS 478-492 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 1 CHECK, FOUND STR 40 DOUBLER CORRODED FS 478 TO 492. REPLACED STRINGER DOUBLER PER SRM 53-2-2. M- 54 NR 5. 2 L 7 4 4T 4A22 1998042900690 19980429 00690 WP 1998 4 29 CALA9800166 1 19980202 A 5522 SKIN DOUG DC10 DC1010 3022110 WP LT ELEV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND LT INBOARD ELEVATOR UPPER TRAILING EDGE SKIN CORRODED. THE CORRODED AREA WAS CUT OUT, DOUBLERS, SPLICE S, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 55-10-00, 51-21-01, 51-31-01, AND 51-35-02. 2 L 7 3 4F A22WE 1998042900691 19980429 00691 WP 1998 4 29 CALA9800167 1 19980202 A 5522 SKIN DOUG DC10 DC1010 3022110 WP LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 2 INCH CRACK IN LT ELEVATOR SKIN AT PANEL NR 335FB. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRIC ATED AND INSTALLED IAW SRM 55-10-00 AND 51-21-01. 2 L 7 3 4F A22WE 1998042900692 19980429 00692 WP 1998 4 29 CALA9800168 1 19980202 A 5400 WEB DOUG DC10 DC1010 3022110 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL WEB UNDER REV INTERLOCK VALVE/CYLINDER ON TOP OF NR 1 PYLON. THE WEB WAS REMOVED IAW SRM 51-31-01. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-20-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998042900693 19980429 00693 WP 1998 4 29 CALA9800169 1 19980202 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP BS 1841 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13086 46917 INSPECTION FOUND A 2 X 1 CRACK AT FASTENER HOLE OF STIFFENER ON AFT SIDE OF FRAME IN CENTER CARGO COMPARTMENT AT STA 184 1, RBL 42. THE STIFFENER WAS REMOVED IAW SRM 51-30-00. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 53-16-01 A ND 51-30-00. 2 L 7 3 4F A22WE 1998042900694 19980429 00694 WP 1998 4 29 CALA9800170 1 19980202 A 5720 FLANGE DOUG DC10 DC1010 3022110 WP WS 794-799 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND CORROSION AT AFT ANCHOR NUTS OF LT WING LOWER LEADING EDGE FLANGE, XORS 794-799. A PLATE WAS FABRICATE D AND INSTALLED IAW SRM 57-10-00 AND 51-20-00. 2 L 7 3 4F A22WE 1998042900695 19980429 00695 WP 1998 4 29 CALA9800171 1 19980202 A 5712 RIB DOUG DC10 DC1010 3022110 WP WS 885 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 2 INCH CRACK AT LOWER OUTBOARD FLANGE AFT END, OF LT WING LEADING EGDE RIB, XORS 885. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-00-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998042900696 19980429 00696 WP 1998 4 29 CALA9800172 1 19980202 A 5720 DOUBLER DOUG DC10 DC1010 3022110 WP WS 445 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A 1 INCH CRACK IN DOUBLER INBOARD OF NR 3 SLAT OUTBOARD TRACK ON RT WING LOWER LEADING EDGE, XORS 445. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-00-01 AND 51-21-01. 2 L 7 3 4F A22WE 1998042900697 19980429 00697 NM 1998 4 29 9801985529 1 19980130 A 2421 IDG BOEING 757 757251 1384970 NM NR 1 GENERATOR REQD SERVICE A NWAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 01 529US 23844 NR 1 GENERATOR OFF LIGHT ILLUMINATED ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE FLIGHT RETURNED TO THE GATE. MAI NTENANCE INSPECTED AND SERVICED THE NR 1 IDG. SUBSEQUENT RUN-UP WAS SATISFACTORY. 2 L 7 2 4F RT A2NM 1998042900698 19980429 00698 1998 4 29 9801999981 4 19980201 A 3442 20671570153 TRANSCEIVER DOUG DC9 DC931 3022065 WP RADAR SYSTEM MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 994Z 10046 1523 47097 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE D RADAR TRANSCEIVER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900699 19980429 00699 WP 1998 4 29 9802009854 1 19980129 A 2432 WIRE DOUG DC9 DC951 3022051 WP BATTERY COMP BROKEN A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 01 763NC 47716 SMOKE WAS COMING FROM BATTERY COMPARTMENT AND INTO COCKPIT WHILE AIRCRAFT WAS PARKED AT THE GATE. ALL PASSENGERS WERE S AFELY EVACUATED THROUGH MAIN CABIN DOOR. MAINTENANCE FOUND BROKEN WIRE P100A24N. REPLACED WIRING, BATTERIES, BATTERY C HARGER, AND TEMPERATURE SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042900700 19980429 00700 WP 1998 4 29 9802019951 1 19980201 A 3260 BULB DOUG DC9 DC932 3022066 WP LT MLG BURNED OUT A NWAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 01 9347 45827 LEFT MAIN LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW ABORTED APPROACH AND NORMAL INDICATION S WERE ACHIEVED DURING GO-AROUND. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RELAMPED LEFT MAIN LANDING GEAR GREEN DOWNLOCK LIGHT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900701 19980429 00701 WP 1998 4 29 9802029852 1 19980201 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 761NC 47709 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042900702 19980429 00702 WP 1998 4 29 9802039857 1 19980201 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 766NC 47739 DURING LINE MAINTENANCE INSPECTION, FOUND AFT INTERIOR EMERGENCY LIGHTING INOPERATIVE. REPLACED BATTERY PACK, OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998042900703 19980429 00703 WP 1998 4 29 9802049909 1 19980130 A 3350 6011779 BATTERY PACK DOUG DC9 DC931 3022065 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900704 19980429 00704 WP 1998 4 29 980205994 1 19980130 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE MAINTENANCE INSPECITON, FOUND LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900705 19980429 00705 WP 1998 4 29 9802069964 1 19980201 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 912RW 47150 FLIGHT ATTENDANT REPORTED, FORWARD EMERGENCY FLASHLIGHT NOT BLINKING. REPLACED BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900706 19980429 00706 WP 1998 4 29 9802079965 1 19980201 A 3350 6014113 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 911RW 47149 FLOOR PROXIMITY EMERGENCY LIGHTS AT OVERWING EMERGENCY EXIT FLICKERED ON AND OFF DURING FLIGHT. REPLACED BATTERY PACK A ND BATTERIES AT ROW 12A, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900707 19980429 00707 WP 1998 4 29 9802089975 1 19980130 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9339 47382 DURING PERIODIC CHECK, FOUND FORWARD CABIN, GALLEY DOOR, COCKPIT OVERHEAD, AND FORWARD ENTRY DOOR EMERGENCY LIGHTS INOPE RATIVE AND/OR FAILED TEN MINUTE TEST. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900708 19980429 00708 WP 1998 4 29 9802099867 1 19980202 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 776NC 47786 DURING INSPECTION, THE AFT CABIN FLOOR PROXIMITY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENC Y LIGHTS BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998042900709 19980429 00709 WP 1998 4 29 9802109103 1 19980202 A 3350 BATTERY PACK DOUG DC9 DC915 3022036 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 93S 47078 DURING INSPECTION, THE LEFT NACELLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIG HTS BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998042900710 19980429 00710 WP 1998 4 29 9802119878 1 19980202 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING INSPECTION, THE FORWARD OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGEN CY LIGHTS BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998042900711 19980429 00711 WP 1998 4 29 9802129857 1 19980202 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 766NC 47739 DURING INSPECTION, THE AFT CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGH TS BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998042900712 19980429 00712 WP 1998 4 29 9802059944 1 19980130 A 3350 60030451 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1309T 47316 DURING LINE MAINTENANCE INSPECITON, FOUND LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900713 19980429 00713 WP 1998 4 29 9802139875 1 19980130 A 7711 611424 PT7 LINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE CRACKED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 784NC 48109 688816 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED CRACKED PT7 LINE ON THE LEFT ENGINE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1998042900714 19980429 00714 WP 1998 4 29 9802149862 1 19980130 A 7711 EPR TRANSMITTER DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 771NC 47769 695275 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE LEFT ENGINE EPR TRANSMITTER AND INDICATOR, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1998042900715 19980429 00715 WP 1998 4 29 9802159952 1 19980203 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 916RW 47144 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT RIGHT FORWARD SERVICE DOOR INOPERATIVE. REPLACED POWER SUP PLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900716 19980429 00716 WP 1998 4 29 9802169940 1 19980203 A 3260 PROX SENSOR DOUG DC9 DC932 3022066 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 3322L 47031 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW PERFORMED COCKPIT OPERATING MANUAL PROCEDURES AN D FLIGHT CONTINUED TO DESTINATION. ON GEAR EXTENSION, NOSE UNSAFE LIGHT REMAINED ILLUMINATED. GO-AROUND PROCEDURES WER E EXECUTED AND EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PROXIMITY SENSOR BRACKET BROKEN. REPLACED SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900717 19980429 00717 SO 1998 4 29 COMA9810034 1 19980130 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHAGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 156CA 14879 1000 120156 EMERGENCY FLOOR LIGHTING IS INOP. REPLACED EMERGENCY BATTERIES. 2 L 7 2 4T RT A31SO 1998042900718 19980429 00718 SO 1998 4 29 COMA9810035 1 19980130 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTION A COMA D RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 137H 4462 120137 FLAP CONTROL FAULT WARNING. REPLACED THE LEFT HAND INBOARD FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1998042900719 19980429 00719 EA 1998 4 29 COMA9860029 1 19980130 A 5210 LATCH MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR CONTAMINATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 924CA 7026 CABIN DOOR OUTER HANDLE CAUTION MESSAGE AFTER TAKEOFF. REMOVED EXCESS GREASE FROM LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1998042900720 19980429 00720 EA 1998 4 29 COMA9860030 1 19980130 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 966CA 7132 CABIN DOOR WARNING AT 17,000 FT. INSPECTED CABIN DOOR AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 1998042900721 19980429 00721 EA 1998 4 29 COMA9860031 1 19980130 A 4990 1603662 OIL COOLER CNDAIR CL600 CL6002B19 EA APU FAILED A COMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 01 946CA 7072 APU OIL TEMP CAUTION INDICATION. REPLACED THE OIL COOLER. 2 L 7 2 4F RT A21EA 1998042900722 19980429 00722 EA 1998 4 29 COMA9860032 1 19980201 A 3350 64645 LIGHT CNDAIR CL600 CL6002B19 EA CABIN DIM A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 945CA 7069 EMERGENCY FLOOR LIGHTING IS DIM, AFT CABIN AREA. REPLACED AFT TRACK LIGHT ASSY. 2 L 7 2 4F RT A21EA 1998042900723 19980429 00723 EA 1998 4 29 COMA9860033 1 19980202 A 3250 17300231 HARNESS CNDAIR CL600 CL6002B19 EA NLG DEFECTIVE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 912CA 7011 NOSE WHEEL STEERING INOP. REPLACED THE NLG STEERING HARNESS. 2 L 7 2 4F RT A21EA 1998042900724 19980429 00724 1998 4 29 COMA9860034 4 19980202 A 3417 8220372115 ADC CNDAIR CL600 CL6002B19 EA NR 2 MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 960CA 9373 130 7117 COPILOTS AIRSPEED INDICATION IS ERRATIC. REPLACED THE NR 2 ADC. 2 L 7 2 4F RT A21EA 1998042900725 19980429 00725 EA 1998 4 29 COMA9860035 1 19980130 A 3260 600332101 TARGET FITTING CNDAIR CL600 CL6002B19 EA NLG DOOR MISSING A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 918CA 7018 DURING GEAR RETRACTION NOSE DOOR LIGHT CAME ON. REPLACED RIGHT HAND NLG DOOR FITTING ASSY. 2 L 7 2 4F RT A21EA 1998042900726 19980429 00726 NM 1998 4 29 UPS98225703 1 19980126 A 5280 FRAME BOEING 727 72722C 138400F NM NLG DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 943UP 19102 INSPECTION TYPE-D, CORROSION FOUND ON INBOARD SKIN FRAME LT DOOR OF NOSE WHEEL WELL. LT NLG FWD WHEEL DOOR I/B FRAME RE PLACED PER SRM 52-80-1 FIG 1 SRM 51-10-1 AND DRAWING 65-17563. 2 L 7 3 4F A3WE 1998042900727 19980429 00727 NM 1998 4 29 UPS98225706 1 19980131 A 3350 BATTERY PACK BOEING 727 72751C 1384015 NM COCKPIT LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 903UP 18945 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS FLICKERED ON TWICE DURING FLIGHT. SWITCH IN ARMED POSITION. RESEATED AND SE CURED COCKPIT EMERGENCY EXIT LIGHT BATTERY PACK. EMERGENCY LIGHTS OPS CKD NORMAL PER MM33-50-01. 2 L 7 3 4F A3WE 1998042900728 19980429 00728 WP 1998 4 29 UPS98825689 1 19980120 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, C-3 CARGO FS 1160 RT FLOORBEAM SUPPORT FITTING IS CRACKED ON LWR END. REMOVED, FABRICATED, AND INSTA LLED REPLACEMENT FITTING IAW SRM51-3-0 AND DWG 9754024. 2 L 7 4 4F RT 4A25 1998042900729 19980429 00729 WP 1998 4 29 UPS98825690 1 19980119 A 5712 RIB DOUG DC8 DC871F 302199D WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, RT WING L/E AT STA XOLDI 6.225 UPPER RIB CRACKED 4. REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998042900730 19980429 00730 WP 1998 4 29 UPS98825691 1 19980120 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, FS 1690 L-28L CORROSION REMOVAL BEYOND LIMITS. INSTALLED EXTERNAL SKIN REPAIR DOUBLER IAW SRM 53-2-1 . 2 L 7 4 4F RT 4A25 1998042900731 19980429 00731 WP 1998 4 29 UPS98825692 1 19980128 A 5712 RIB DOUG DC8 DC871F 302199D WP BS 385.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, LT WING L/E RIB CRACKED LWR ARM STA 385.250. REPAIRED IAW SRM 57-3-1. 2 L 7 4 4F RT 4A25 1998042900732 19980429 00732 WP 1998 4 29 UPS98825693 1 19980120 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 35-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, FUSELAGE DOUBLER ABOVE L30R BETWEEN FS 35 TO 55 CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INS TALLED REPLACEMENT DOUBLER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998042900733 19980429 00733 WP 1998 4 29 UPS98825694 1 19980119 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 490-530 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, SEAT TRACK AT FS 490 TO 530 LBL 59.5 HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACE MENT TRACK IAW SRM ADDN DC8-5320-5167C. 2 L 7 4 4F RT 4A25 1998042900734 19980429 00734 WP 1998 4 29 UPS98825695 1 19980120 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, FS 70 LONG-33L SKIN CORRODED OUT OF LIMITS. REPAIRED IAW DHC SK-750-649. 2 L 7 4 4F RT 4A25 1998042900735 19980429 00735 WP 1998 4 29 UPS98825696 1 19980120 A 5320 37558451 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, FS 1200 BTWN STR 35R TO 36 TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1998042900736 19980429 00736 WP 1998 4 29 UPS98825697 1 19980120 A 5320 37558451 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-C, FS 1200 BTWN STR 34L TO 35L TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1998042900737 19980429 00737 EU 1998 4 29 QXEA9800058 1 19980202 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 EMERGENCY EXIT LIGHT AT SEAT 8E INOP. RELAMPED, OPERATIONAL TEST POSITIVE. 2 L 7 2 4F RT A20EU 1998042900738 19980429 00738 NM 1998 4 29 98FDEA00081 1 19980203 A 2751 18129952 INDICATOR BOEING 727 7272S2F 1384O81 NM TE FLAPS INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 215FE 22936 INBOARD INDICATED ASYMMETRIC AT 1 DEGREE UPON RETRACT. REPLACED INBOARD FLAP POSITION INDICATOR. REMOVED AND CLEANED B YPASS VALVE CANNON PLUG THEN REINSTALLED. LUBED JACK SCREWS, VISUALLY CHECKED JACK SCREWS FLAP TRACKS AND ROLLERS OPERA TED WITH HYDRAULICS SEVERAL TIMES THROUGH FULL TRAVEL FLAPS OPERATE NORMAL OK FOR FLIGHT. 2 L 7 3 4F A3WE 1998042900739 19980429 00739 WP 1998 4 29 ABX9800044 1 19980203 A 5311 9912246115 FRAME DOUG DOUG DC9 DC941 302207N WP BS 1114 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND FUSELAGE FRAME AT STA 1114 HEAVILY CORRODED BETWEEN LONGERON 24L AND 24R. REPLACED FRAME IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998042900740 19980429 00740 WP 1998 4 29 ABXA9800045 1 19980203 A 5320 991555965 DOOR JAMB DOUG DOUG DC9 DC941 302207N WP BS 1135 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE AFT VENTRAL DOOR AFT JAMB WEB FS 1135 FRAME CORRODED, LONGERON 24L TO 24R. REPLACED WEB I AW DC9 SRM 51-30-2, AND DACO DWG 9915559. 2 L 7 2 4F A6WE 1998042900741 19980429 00741 WP 1998 4 29 ABXA9800046 1 19980203 A 5320 991966017 FITTING DOUG DOUG DC9 DC941 302207N WP ACCESS COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND LEFT SUPPORT BRACKET FITTING IN AFT ACCESSORY COMPARTMENT CORRODED AND CRACKED. REPLACED BRAC KET FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998042900742 19980429 00742 WP 1998 4 29 ABXA9800047 1 19980203 A 5320 991966018 FITTING DOUG DOUG DC9 DC941 302207N WP ACCESS COMPT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND SUPPORT BRACKET FITTING IN AFT ACCESSORY COMPARTMENT CORRODED AND CRACKED. REPLACED BRACKET FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998042900743 19980429 00743 WP 1998 4 29 ABXA9800048 1 19980203 A 5320 9911839120 STIFFENER DOUG DOUG DC9 DC941 302207N WP BS 1197 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND STIFFENER CORRODED AT AFT SIDES OF STA 1197 AND LONGERON 13R. REPLACED STIFFENER IAW DC9 SRM 51-30-5 AND DACO DWG 9911839. 2 L 7 2 4F A6WE 1998042900744 19980429 00744 WP 1998 4 29 ABXA9800049 1 19980203 A 5311 9912246115 FRAME DOUG DOUG DC9 DC941 302207N WP BS 1114 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND FRAME AT STA 1114 CORRODED FROM LONGERON 24L TO 24R. REPLACED FRAME T-CAP IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998042900745 19980429 00745 WP 1998 4 29 ABXA9800050 1 19980203 A 5320 991199115 ANGLE DOUG DOUG DC9 DC941 302207N WP VENTRAL DOORWAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE AFT VENTRAL STAIR DOOR JAMB ANGLE CORRODED. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30- 5. ADDITIONAL PARTS JAMB, (P/N 991190-401), ANGLE (P/N 9919662-12). 2 L 7 2 4F A6WE 1998042900746 19980429 00746 WP 1998 4 29 ABXA9800051 1 19980203 A 5320 49174271 BRACKET DOUG DOUG DC9 DC941 302207N WP VENTRAL DOORWAY CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 DURING MOD/D-CHECK, FOUND THE AFT VENTRAL STAIR DOOR JAMB BRACKET CORRODED. REPLACED BRACKET IAW DC9 SRM 51-30-2 AND 51 -30-5. 2 L 7 2 4F A6WE 1998042900747 19980429 00747 WP 1998 4 29 ABXA9800052 1 19980203 A 5320 991555049 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED AT STA 980 BETWEEN LONGERON 27L AND 28L. REPLACED ANGLE IAW DACO DWG 9915550 AND DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998042900748 19980429 00748 WP 1998 4 29 ABXA9800053 1 19980203 A 5320 591395185 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 186 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND FORWARD LT ENTRY DOOR DRAIN PAN SUPPORT ANGLE CRACKED AT LBL 55 AND STATION 186. REPLACED ANGLE I AW DC9 SRM 51-30-8. 2 L 7 2 4F A6WE 1998042900749 19980429 00749 1998 4 29 DHL98801001 4 19980203 A 3417 2587400176 ADC DOUG DC8 DC873F 302199F WP E/E COMPT FAILED A DHLA A J UNSCHED LANDING DUMP FUEL O OTHER CR CRUISE 1 SO 01 801DH 46033 AUTOPILOT HOLD FUNCTION UNUSABLE, NR 2 ALTIMETER TOTALLY UNRELIABLE, FLUCTUATIONS OF 500 FEET. REMOVED AND REPLACED ADC , OPS CHECK GOOD PER MM 34-11-0 AND 34-12-0. 2 L 7 4 4F RT 4A25 1998042900756 19980429 00756 NM 1998 4 29 B4MR98001 1 19980201 A 5230 FRAME BOEING 727 727243 138408D NM CARGO DOOR CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ACCOMPLISHMENT OF RYAN EO RN 727-53-28, FOUND NR 2 CARGO DOOR FRAME AFT EDGE LOWER CORNER CORRODED. REMOVED CORR OSION IAW B727 SRM 51-10-6. ULTRASONIC THICKNESS CHECK - INITIAL THICKNESS READINGS FRAME FLANGE AREA .044 TO .121, HAS NOMINAL THICKNESS .145, FRAME WEB THICKNESS .066 TO .070. INSTALLED REPAIR IAW AIA/E/2729. NON-ROUTINE TASK CARD NUMBE R 14983. 2 L 7 3 4F RT A3WE 1998042900757 19980429 00757 NM 1998 4 29 B4MR98002 1 19980201 A 5720 STIFFENER BOEING 727 727243 138408D NM LT WING CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND LT WING REAR SPAR STIFFENER IS CORRODED (TOP AND BOTTOM) AT WBL 108 (INBD SIDE OF LANDING GEAR TRUNNION). REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 57-10-1. INSTA LLED REPAIR IAW B727 SRM 51-30-2. CORROSION TASK CARD NUMBER C57-581-03. NON-ROUTINE TASK CARD NUMBER 14373. 2 L 7 3 4F RT A3WE 1998042900758 19980429 00758 NM 1998 4 29 B4MR98003 1 19980201 A 5314 KEEL BEAM BOEING 727 727243 138408D NM BS 950-990 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ACCOMPLISHMENT OF AD 92-12-03, FOUND CORROSION ON KEEL BEAM BETWEEN FS 950E TO FS 990. REMOVED CORROSION IAW B72 7 SB 53-0179. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW SB 727 53-0179 N5C2 AND 727/E/2718 AIA SKETCH. NON-ROUTINE TASK CARD NUMBER 14917. 2 L 7 3 4F RT A3WE 1998042900759 19980429 00759 NM 1998 4 29 B4MR98004 1 19980201 A 5330 SKIN BOEING 727 727243 138408D NM BS 950-970 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ACCOMPLISHMENT OF AD 92-12-03, FOUND CORROSION ON SKIN UNDER WEB NEXT TO STR 27L STA 950 TO 970 IN C-2 PIT. CORR OSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-30-1. INSTALLED REPAIR DOUBLER AND FILLER IAW B727 SRM 53-30-3 FIG 3. N ON-ROUTINE TASK CARD NUMBER 14835. 2 L 7 3 4F RT A3WE 1998042900760 19980429 00760 NM 1998 4 29 B4MR98005 1 19980201 A 5311 FRAME BOEING 727 727243 138408D NM BS 1030 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND FS 1030 LT SIDE CIRCUM HAS SMALL AREA OF CORROSION JUST UNDER FLOORBEAM. REMOVED CORROSION IAW SRM 51-10-6. ULTRASONIC THICKNESS CHECK MINIMUM NOMINAL: .045 MAX NOMINAL: .075. FOUND TO BE OUT OF LIMIT S IAW B727 SRM 53-10-1. INSTALLED REPAIR IAW B727 SRM 51-40-3 FIG 1. CORROSION TASK CARD NUMBER C53-224-06. NON-ROUTI NE TASK CARD NUMBER 11995. 2 L 7 3 4F RT A3WE 1998042900761 19980429 00761 NM 1998 4 29 B4MR98006 1 19980201 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 680 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 FS 680 RBL 25 TO LBL 25 HAS CORROSION (FLOORBEAM). REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS I AW B727 SRM 53-10-1. INSTALLED IAW B727 SRM 53-10-8 FIG 3. CORROSION TASK CARD NUMBER C53-224-03. NON-ROUTINE TASK CA RD NUMBER 11977. 2 L 7 3 4F RT A3WE 1998042900762 19980429 00762 NM 1998 4 29 B4MR98007 1 19980201 A 5313 STRINGER BOEING 727 727243 138408D NM BS 950 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ACCOMPLISHMENT OF AD 92-12-03, FOUND STR 28L AT FS 950A HAS CORROSION AFT OF BEAM. U/T THICKNESS CK .124 REMAINI NG AFTER CORROSION REMOVED. REMOVED CORROSION IAW B727 SRM 51-10-1. INSTALLED REPAIR STRAP WITH FILLER IAW B727 SB 727 -53-179. NON-ROUTINE TASK CARD NUMBER 14856. 2 L 7 3 4F RT A3WE 1998042900763 19980429 00763 NM 1998 4 29 B4MR98008 1 19980201 A 5230 FRAME BOEING 727 727243 138408D NM BS 950 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ACCOMPLISHMENT OF RYAN EO RN 727-53-28, FOUND FS 950E NR 2 LWR CARGO FWD FRAME LWR CORNER HAS CORROSION UNDER LWR DOOR STOP. CORROSION REMOVED IAW B727 SRM 51-10-6. ULTRASONIC THICKNESS CHECK - INITIAL THICKNESS READINGS MINIMUM NO MINAL THICKNESS .028 TO .056 MAX NOMINAL THICKNESS .074 FRAME WEB AREA. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SR M 53-10-1 MADE REPAIR DOUBLER IAW SB 727-53A0199 AND AIA EOR B2-05613. INSTALLED REPAIR IAW SB 727-53A0199. NON-ROUTIN E TASK CARD NUMBER 14963. 2 L 7 3 4F RT A3WE 1998042900764 19980429 00764 NM 1998 4 29 B4MR98009 1 19980201 A 5313 STRINGER BOEING 727 727243 138408D NM BS 950 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ACCOMPLISHMENT OF AD 92-12-03, FOUND STR 28L AT FS 950A HAS CORROSION FWD OF BEAM. REMOVED CORROSION IAW B727 SR M 51-10-1. ULTRASONIC THICKNESS CHECK, INTERGRANULAR CORROSION DETECTED REINSPECT U/T THICKNESS CK .116 NO FURTHER COR ROSION NOTED. MADE AND INSTALLED REPAIR STRAP WITH FILLER IAW B727 SB 727-53-0179. NON-ROUTINE TASK CARD NUMBER 14823. 2 L 7 3 4F RT A3WE 1998042900765 19980429 00765 NM 1998 4 29 B4MR98010 1 19980201 A 5311 FRAME BOEING 727 727243 138408D NM BS 783.95 MISDRILLED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ACCOMPLISHMENT OF AD 94-02-04, FOUND FRAME AT BS 783.95 LT SIDE HAS MISDRILLED HOLE, JUST ABOVE CENTER WING TANK UPPER SKIN. INSTALLED FREEZE PLUG IAW B727 SRM 51-10-7 AND EA B2-53-016. NON-ROUTINE TASK CARD NUMBER 15287. 2 L 7 3 4F RT A3WE 1998042900766 19980429 00766 NM 1998 4 29 B4MR98011 1 19980201 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 1110 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 521DB 21266 DURING ROUTINE CPCP INSPECTION, FOUND FS 1110 RBL 10 PREVIOUS FLOORBEAM REPAIR HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-6. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED DAMAGED UPPER PORTION OF FLOORBEAM AND FABRICAT ED REPAIR PARTS IAW SRM 53-10-8. INSTALLED REPAIR IAW B727 SRM 51-30-2. CORROSION TASK CARD NUMBER C53-224-03. NON-RO UTINE TASK CARD NUMBER 11971. 2 L 7 3 4F RT A3WE 1998042900767 19980429 00767 NE 1998 4 29 TC8A98007 2 19980203 A 7261 OIL SYST DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE REQD SERVICE A TC8A E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 182SK 45817 SHUTDOWN NR 3 ENGINE AT 1130Z IN FLIGHT DUE TO LOW OIL PRESSURE INDICATION AND LOW OIL PRESSURE LIGHT. WINDMILLING OIL PRESSURE 10 PSI. ADDED 5 QTS TO FILL OIL TANK TO FULL. INSPECTED OIL FILTER, FOUND IT CLOGGED AND BYPASSED. CLEANED F ILTER IAW PWA MANUAL 72-0 PG 660. CHECKED PRESSURE LOSS PER 79-4-0. RAN-UP ENGINE AND FOUND NO LEAKS. 2 L 7 4 4F 4 F 4A25 1E8 1998042900772 19980429 00772 NM 1998 4 29 P5CA9800737 1 19980305 A 5414 DOOR BOEING 747 747238B 1384828 NM NR 4 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 4 PYLON O/B SAILBOAT DOOR CHAFED. SANDED DOWN CHAFED AREA, APPLIED POTTING COMPOUND, SANDED DOWN AND PRIMED/PAINTED PER SRM 51-70-00. 2 L 7 4 4F A20WE 1998042900773 19980429 00773 WP 1998 4 29 RRXA98074 1 19980212 A 5711 3641823502 SPAR WEB DOUG DC8 DC871F 302199D WP WS 879 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8177U 45983 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE BEYOND LIMITATIONS TO RIGHT WING, AUX SPAR WEB AT STA 879 TO STA 902. AUX SPAR WEB CORROSION REMOVED MATERIAL LOSS WAS MINIMAL USING DC-8 SRM 57-2-0 FIGURE 6 SHEET 1. THE MAJOR MATERIAL R EMOVED WAS AT THE EDGE OF THE PART LEAVING IN EXCESS OF 2D EDGE DISTANCE FROM THE SUROUNDING FASTENER HOLES WHICH IS ACC EPTABLE PER DC-8 SRM 57-2-0 FIGURE 6 SHEET 1, AND IAW FAA APPRROVED DER TIMCO ENGINEERING SKETCH REO-04167. 2 L 7 4 4F RT 4A25 1998042900774 19980429 00774 SO 1998 4 29 C2XA98IA039 1 19980226 A 5720 12017063609 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 20 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120MM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900775 19980429 00775 SO 1998 4 29 C2XA98IA042 1 19980226 A 5720 12017063609 BRACKET EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NR 3 UPPER SKIN SUPPORT ON RIB 21 OF THE RIGHT WING WAS FOUND TO BE CRACKED. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-4--02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900776 19980429 00776 SO 1998 4 29 C2XA98IA043 1 19980226 A 5720 12017062613 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 21 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900777 19980429 00777 SO 1998 4 29 C2XA98IA044 1 19980226 A 5320 12004149001 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900778 19980429 00778 SO 1998 4 29 C2XA98IA045 1 19980226 A 5320 12004170004 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE CENTER T-PROFILE AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900779 19980429 00779 SO 1998 4 29 C2XA98IA046 1 19980226 A 5712 12017062015 RIB EMB 120 EMB120RT SO LEFT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 21 WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01020, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900780 19980429 00780 SO 1998 4 29 C2XA98IA047 1 19980226 A 5320 12002616001 BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 40. MAINTENANCE R EPAIRED THE AFFECTED AREA IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01043 AND THE AIRCR AFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900781 19980429 00781 SO 1998 4 29 C2XA98IA048 1 19980226 A 5320 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE AT FRAME 15 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED T-PROFILER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900782 19980429 00782 SO 1998 4 29 C2XA98IA049 1 19980226 A 5320 12004449001 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 38 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900783 19980429 00783 SO 1998 4 29 C2XA98IA050 1 19980226 A 5320 12004449001 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900784 19980429 00784 SO 1998 4 29 C2XA98IA051 1 19980226 A 5320 12027929001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 34 TO FRAME 39. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1998042900785 19980429 00785 SO 1998 4 29 C2XA98IA052 1 19980226 A 5313 12017417006 STRINGER EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 41 AND 42. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SECTION OF STRINGER IAW EMB120 SRM 53-00-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4T RT A31SO 1998042900786 19980429 00786 SO 1998 4 29 C2XA98IA053 1 19980226 A 5320 12027929001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900787 19980429 00787 SO 1998 4 29 C2XA98IA054 1 19980226 A 5320 12006158001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO FRAME 40. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900788 19980429 00788 SO 1998 4 29 C2XA98IA055 1 19980226 A 5320 12006159001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 34 AND 39. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900789 19980429 00789 SO 1998 4 29 C2XA98IA056 1 19980226 A 5320 S12006519001 CREASE BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 TO 44. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900790 19980429 00790 SO 1998 4 29 C2XA98IA057 1 19980226 A 5320 12005779001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900791 19980429 00791 SO 1998 4 29 C2XA98IA058 1 19980226 A 5320 12004449001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900792 19980429 00792 SO 1998 4 29 C2XA98IA059 1 19980226 A 5720 12017060609 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, THE NR 1 UPPER SKIN SUPPORT ON RIB 20 FO THE LEFT WING WAS FOUND TO BE CRACKED. MAINTE NANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900793 19980429 00793 SO 1998 4 29 C2XA98IA060 1 19980226 A 5720 12017063609 BRACKET EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURNG C-CHECK INSPECTION, THE NR 2 UPPER SKIN SUPPORT ON RIB 20 OF THE LEFT WING WAS FOUND TO BE CRACKED. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900794 19980429 00794 SO 1998 4 29 C2XA98IA034 1 19980225 A 3233 2060500005 ACTUATOR EMB 120 EMB120RT SO NLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 SW 09 22727 120177 IAH - DURING FLT 3794 - FROM LRD, THE PILOT REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO LRD WITHOUT INCIDENT, AND WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR RETRACT ACTUAT OR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900795 19980429 00795 SO 1998 4 29 C2XA98IA068 1 19980226 A 5347 12015996005 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEA T TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900796 19980429 00796 EU 1998 4 29 C2XA98IA069 1 19980302 A 5311 S53971402294 FRAME AEROSP ATR42 ATR42500 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14445 503 IAH - DURING C-CHECK INSPECTION, FOUND BELLY FAIRING SUPPORT FRAME NR 27A CRACKED ON RIGHT SIDE. MAINTENANCE STOP DRILL ED THE CRACK AND INSTALLED A REPAIR DOUBELR IAW ATR42-500 SRM 51-70-00 AND 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998042900797 19980429 00797 SO 1998 4 29 C2XA98IA062 1 19980226 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEA T TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900798 19980429 00798 SO 1998 4 29 C2XA98IA063 1 19980226 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SE AT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900799 19980429 00799 SO 1998 4 29 C2XA98IA064 1 19980226 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FORWARD SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900800 19980429 00800 SO 1998 4 29 C2XA98IA065 1 19980226 A 5347 12026863007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT SIDEWALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900801 19980429 00801 SO 1998 4 29 C2XA98IA066 1 19980226 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TR ACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900802 19980429 00802 SO 1998 4 29 C2XA98IA067 1 19980226 A 5347 12026865009 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT T RACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998042900803 19980429 00803 EU 1998 4 29 AALA980218 1 19980127 A 3230 296801 REDUCER VLV FOKKER F28 F28MK0100 4990807 EU WW DEFECTIVE A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 1472B 368 11514 ORD - FLT 247 - DURING APPROACH ORD, LANDING GEAR SELECTED DOWN, LEFT AND RIGHT MAIN GEAR EXTENDED SLOWLY CAUSING A LAND ING GEAR UNSAFE MESSAGE TO ILLUMINATE. BEFORE LANDING CREW GOT THREE GREEN DOWN AND LOCK LIGHTS AND THE AIRCRAFT LANDED ORD WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED LANDING GEAR REDUCER VALVE, SERVICED HYDRAULIC SYSTEM, AND SWUNG GE AR SEVERAL TIMES WITH NORMAL OPERATION. SYSTEM GROUND CHECKED AND LEAKED CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998042900804 19980429 00804 NM 1998 4 29 AALA980434 1 19980303 A 3350 P4010051 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607AM 27058 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS ILLUMINATED INTERMITTENTLY. REPLACED EMERGENCY FLOOR LIGHT MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998042900805 19980429 00805 NM 1998 4 29 AALA980437 1 19980302 A 3397 0201922001 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388AA 27448 LHR - DURING MAINTENANCE, EMERGENCY PATH LIGHT AT SEAT 21B INOPERATIVE. REPLACED EMERGENCY PATH LIGHT CABLE ASSEMBLY AT SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998042900806 19980429 00806 NM 1998 4 29 AALA980436 1 19980302 A 3350 0201820001 LIGHT BOEING 767 767323 1385205 NM FWD GALLEY BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 376AN 25445 LHR - DURING MAINTENANCE, FORWARD GALLEY RIGHT ESCAPE PATH LIGHT BROKEN. REPLACED LAMP HOLDER AND EMERGENCY LIGHT COVER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998042900807 19980429 00807 NM 1998 4 29 AALA980415 1 19980302 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 620AA 24578 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. REPAIRED EMERGENCY FLOOR PATH WIRE AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998042900808 19980429 00808 NM 1998 4 29 AALA980443 1 19980305 A 3350 3020442 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 641AA 24599 DFW - DURING OVERNIGHT CHECK, R2 AFT EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REPLACED R2 AFT EMERGENCY EXIT LIGHT AS SEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998042900809 19980429 00809 NM 1998 4 29 AALA980440 1 19980304 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607AM 27058 DFW - FLT 2328 - DURIGN CRUISE, THE FLOOR EMERGENCY LIGHT ILLUMINATED FOR APPROXIMATELY 35 MINUTES. REPAIRED LOOSE EMER GENCY AISLE PATH LIGHTING GROUND WIRE AND REPLACED CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998042900810 19980429 00810 NM 1998 4 29 AALA980476 1 19980309 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 39B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CON NECTOR AT PAX SEAT 39B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998042900811 19980429 00811 NM 1998 4 29 AALA980480 1 19980310 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635AA 24593 DFW - DURING OVERNIGHT CHECK, CENTER CABIN EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT STRIP AT CENTER CABIN FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998042900812 19980429 00812 EU 1998 4 29 MALA976069 1 19980328 A 2913 4018502 HYD PUMP SAAB SF340 340B 7860101 EU NLG WW FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 427XJ 427 ON APPROACH, SELECTED GEAR HANDLE DOWN, PUMP RAN, GEAR UNSAFE LIGHT ILLUMINATED, GEAR DOORS DID NOT OPEN, RECYCLED GEAR AND STILL UNSAFE. CONTACTED MAINTENANCE CONTROL AND PULLED THE T-HANDLE AND PUMPED THE GEAR DOWN, GEAR CAME DOWN WITH T HREE GREENS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC PUMP, RELAY 15GA (PN M83536/6-022L) AND SOCKET 15GA-31 (PN RSE120060). ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998042900813 19980429 00813 EU 1998 4 29 MALA976070 1 19980327 A 3350 6104789 BATTERY PACKS SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 68XJ 068 DURING INSPECTION EMERGENCY LIGHTS INOP. MAINTENANCE FOUND EMERGENCY PACKS DEAD. REMOVED AND REPLACED EMERGENCY BATTER Y PACKS, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900814 19980429 00814 EU 1998 4 29 MALA976071 1 19980327 A 3350 LENS SAAB SF340 SF340A 7850100 EU CABIN BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 68XJ 068 DURING INSPECTION, FLIGHT ATTENDANT'S EMERGENCY LIGHT LENSE COVER BUTTON IS BROKEN. MAINTENANCE REPLACED EMERGENCY LIGH T LENS COVER, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900815 19980429 00815 EU 1998 4 29 MALA976072 1 19980322 A 3350 7239025502 PANEL SAAB SF340 SF340A 7850100 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 41XJ 041 DURING INSPECTION, EMERGENCY LIGHT ON OVERHEAD PANEL WILL NOT STAY SECURED. MAINTENANCE REPLACED EMERGENCY OVERHEAD PAN EL, OP'S CHECK GOOD. 2 L 7 2 4T RT A52EU 1998042900816 19980429 00816 NM 1998 4 29 MALA976073 1 19980329 A 3350 6104789 BATTERY PACK DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 824MA 327 DURING INSPECTION, EMERGENCY FLOOR TRACK LIGHTING IS INOP. MAINTENANCE REPLACED 6 EMERGENCY LIGHT BATTERY PACKS, OPS CH ECK GOOD. 2 H 7 2 4T RT A13NM 1998042900817 19980429 00817 WP 1998 4 29 CALA9800601 1 19980330 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16804 49246 TAIL CONE PULL FROM INTERIOR RELEASE HANDLE WAS LOW AT SIX POUNDS. AN ADJUSTMENT/TEST WAS PERFORMED IAW WORK CARD 08-53 50-1-0008 AND PULL TEST WAS WITHIN SPECIFICATIONS AT 20 POUNDS. 2 L 7 2 4F A6WE 1998042900818 19980429 00818 NM 1998 4 29 CALA9800602 1 19980330 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND A 6 INCH CRACK ON AFT SIDE OF STA 1183 BULKHEAD AT RBL 7, WL 192 JUST ABOVE TAIL SKID ATTACH UPPER L-AN GLE TO LOWER L-ANGLE. THE CRACK WAS ROUTED OUT IAW ECRA 5310-01473. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 53 10-01473, SRM 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1998042900819 19980429 00819 NM 1998 4 29 CALA9800603 1 19980330 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND A 3 INCH CRACK AROUND FASTENERS ON STA 1183 BULKHEAD AT RBL 7, WL 192 ABOVE TAIL SKID AT SECOND ANGLE F ROM TOP. THE CRACK WAS ROUTED OUT IAW ECRA 5310-01473. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01473, SRM 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1998042900820 19980429 00820 NM 1998 4 29 CALA9800604 1 19980330 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND SEAT TRACK CORRODED AT STA 480, RBL 48. A SEAT TRACK REPAIR WAS FABRICATED AND INSTALLED IAW 53-10-5, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998042900821 19980429 00821 WP 1998 4 29 CALA9800605 1 19980330 A 5754 RIBS DOUG DC10 DC1030 3023501 WP NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 1 INCH CRACK IN THREE RIBS OF NR 1 LT SLAT. THE CRACKED RIBS WERE REMOVED. NEW RIBS WERE FABRICATED AND INSTALLED IAW SRM 57-55-01 FIGURE 2 51-20-00 AND 51-31-01. 2 L 7 3 4F A22WE 1998042900822 19980429 00822 NM 1998 4 29 CALA9800606 1 19980330 A 5754 SKIN BOEING 727 727232 1384082 NM NR 1 LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND A DENT IN LT WING LEADING EDGE NR 1 SLAT. THE DENTED AREA WAS REMOVED. THE AREA WAS REINFORCED WITH A NEW DOUBLER WHICH WAS FABRICATED AND INSTALLED IAW SRM 57-10-00 FIGURE 18A 51-20-00 AND 51-31-01. 2 L 7 3 4F A3WE 1998042900823 19980429 00823 WP 1998 4 29 CALA9800607 1 19980331 A 5754 SKIN DOUG DC10 DC1010 3022110 WP NR 4 LE SLAT PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND A 1 INCH DIAMETER HOLE IN NR 4 LEADING EDGE SLAT JUST OUTBOARD OF CENTER TRACK. THE DAMAGED AREA WAS C UT OUT, FILLER, DOUBLER, BAFFLE AND SPLICE PLATE WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, PAGE 27 AND ECRA 5752-0 1022. 2 L 7 3 4F A22WE 1998042900824 19980429 00824 WP 1998 4 29 9805289945 1 19980304 A 5320 BRACKET DOUG DC9 DC931 3022065 WP BS 639 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8925E 45841 DURING H-CHECK, FOUND SHEAR TIE FITTING CRACKED AT FS 639 AT LONGERON 29L. REPLACED SHEAR TIE FITTING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998042900825 19980429 00825 WP 1998 4 29 9805299996 1 19980311 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 945 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND CORROSION ON END FITTING FOR LONGERON 21R AT FS 945. REPLACED FITTING (P/N 4912798-501) PER SRM 5 3-01. 2 L 7 2 4F A6WE 1998042900826 19980429 00826 WP 1998 4 29 9805309996 1 19980318 A 5320 FITTING DOUG DC9 DC931 3022065 WP BS 998 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND CORROSION ON END FITTING FOR LONGERON 22L AT FS 998. REPLACED FITTING (P/N 4912515-1) PER SRM 53- 01. 2 L 7 2 4F A6WE 1998042900827 19980429 00827 NE 1998 4 29 9805313214 2 19980330 A 7320 30179000101 T12 SENSOR AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 314US 17418 17418 160 731201 DURING CLIMB, NR 2 ENGINE N1, FUEL FLOW, AND EGT BEGAN TO FLUCTUATE. FLUCTUATION CONTINUED DESPITE VARIOUS POWER SETTIN GS OR IN A CONSTANT POWER SETTING. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED THE FUEL FILTER, FU EL PUMP, HMU, AND T12 SENSOR. ENGINE HAD A BORESCOPE INSPECTION AND WAS FOUND OK. AIRCRAFT GROUND RUN AND LEAK CHECK O K. 2 L 7 2 4F 4 F RT A28NM E29NE 1998042900828 19980429 00828 WP 1998 4 29 9805329924 1 19980331 A 5350 SPRING DOUG DC9 DC932 3022066 WP TAIL CONE MISINSTALLED A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 926RC 47473 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO DEPLOY TAIL CONE. ALSO, FOUND THAT TAIL C ONE RELEASE HANDLE CABLE WAS NOT INSTALLED IN SWITCH PLUNGER. MAINTENANCE FOUND THE LATCH SPRINGS IMPROPERLY INSTALLED. REPLACED LATCH SPRINGS AND PROPERLY INSTALLED RELEASE HANDLE CABLE, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998042900829 19980429 00829 WP 1998 4 29 9805339981 1 19980328 A 5270 STRIKER PLATE DOUG DC9 DC931 3022065 WP CARGO DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 994Z 47097 DURING CLIMB, AFT CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. DURING LAN DING LIGHT WENT OUT. MAINTENANCE ADJUSTED STRIKER PLATE AT CARGO DOOR, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998042900830 19980429 00830 NM 1998 4 29 9805342293 1 19980321 A 3260 SWITCH BOEING 727 727251 138408H NM NLG FAILED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 293US 21504 ON LANDING GEAR EXTENSION, RECEIVED NO INDICATION FOR NOSE GEAR DOWN AND LOCKED. RECYCLED GEAR AFTER THREE TO FOUR MINU TES. RECEIVED NOSE GEAR INDICATION AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR LOCK SWTICH S96, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998042900831 19980429 00831 NM 1998 4 29 9805352293 1 19980321 A 3260 SWITCH BOEING 727 727251 138408H NM NLG FAILED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 293US 21504 DURING GEAR EXTENSION, RECEIVED NO NOSE GEAR INDICATION DOWN AND LOCKED. CYCLED GEAR WITH NO INDICATION. AFTER TWO MIN UTES, GREEN DOWN AND LOCKED INDICATION LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED POSITION SWITCH S 93, OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1998042900832 19980429 00832 WP 1998 4 29 9805369753 1 19980331 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 753NW 47117 DURING LINE CHECK, FOUND COCKPIT FORWARD AISLE, LEFT FORWARD ENTRY AND GALLEY SERVICE OVERHEAD EMERGENCY LIGHTS INOPERAT IVE. MAINTENANCE REPLACED BATTERY PACK B5-23 AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900833 19980429 00833 EU 1998 4 29 9805373225 1 19980314 A 3350 POWER PACK AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 325US 281 DURING TEST OF EMERGENCY LIGHTS VIA CIDS, THE LEFT CENTER EMERGENCY POWER PACK FAILED. MAINTENANCE REPLACED POWER SUPPL Y PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998042900834 19980429 00834 EU 1998 4 29 9805383242 1 19980302 A 3350 BULB AIRBUS 320 A320212 EU CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 342NW 381 DURING TEST OF EMERGENCY LIGHTS, FOUND ALL FOUR OVERWING EMERGENCY EXIT HANDLE ILLUMINATION LIGHTS INOPERATIVE. MAINTEN ANCE REPLACED BULBS AT ALL FOUR POSITIONS, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998042900835 19980429 00835 EU 1998 4 29 9805393227 1 19980310 A 3350 321430 BATTERY AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 327NW 297 DURING TEST OF EMERGENCY LIGHT SYSTEM, FORWARD LEFT EMERGENCY LIGHT BATTERY FAILED. MAINTENANCE REPLACED BATTERY, OPERA TIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998042900836 19980429 00836 EU 1998 4 29 9805403240 1 19980317 A 3350 BULBS AIRBUS 320 A320212 EU CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 340NW 372 DURING TEST OF EMERGENCY LIGHT SYSTEM, FOUND ALL FOUR OVERWING EMERGENCY EXIT HANDLE ILLUMINATION LIGHTS INOPERATIVE. M AINTENANCE REPLACED BULBS, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998042900837 19980429 00837 WP 1998 4 29 9805419925 1 19980331 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK AND POWER SU PPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900838 19980429 00838 WP 1998 4 29 9805429998 1 19980331 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8934E 47143 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY ESCAPE PATH LIGHTING BETWEEN SEATS 18 THRU 21 AND AT LEFT LAVATORY E XIT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900839 19980429 00839 WP 1998 4 29 9805439920 1 19980331 A 3610 FITTING DOUG DC9 DC932 3022066 WP AUG VALVE LEAKING A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 942N 47459 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDE NT. MAINTENANCE REPLACED LEAKING FITTING AT AUGMENTATION VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900840 19980429 00840 1998 4 29 9805449941 4 19980331 A 3442 RADAR PANEL DOUG DC9 DC932 3022066 WP COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 3324L 47103 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTE D RADAR STABILIZATION AND REPLACED RADAR CONTROL PANEL DUE TO FAULTY MODE SELECTION, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042900841 19980429 00841 WP 1998 4 29 9805459614 1 19980331 A 3260 PSEU PROCESSOR DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 614NW 47128 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDEN T. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND. REPLACED PSEU PROCESSOR AS A PRECAUTION. 2 L 7 2 4F A6WE 1998042900842 19980429 00842 WP 1998 4 29 9805469920 1 19980329 A 3610 17945022 HEAT EXCHANGER DOUG DC9 DC932 3022066 WP TAIL COMPT CRACKED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 942N 48758 9888 47459 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDE NT. MAINTENANCE REPLACED CRACKED HEAT EXCHANGER, LEAK AND OPERATIONAL CHECK WAS NORMAL. 2 L 7 2 4F A6WE 1998042900843 19980429 00843 NM 1998 4 29 SWAA980390 1 19980324 A 2910 LINE BOEING 737 7373H4 1384600 NM A-HYD SYSTEM BROKEN A SWAA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 07 654SW 28399 AFTER LANDING FOUND HYDRAULIC LEAK RT SIDE OF A/C IN RIGHT WING AREA BEHIND NR 2 ENGINE. SUSPECT A-SYSTEM. INSTALLED LINE, SVC'D A-HYDRAULIC SYSTEM. LEAK CHECK GOOD, PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900844 19980429 00844 NM 1998 4 29 SWAA980391 1 19980324 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND STR 11L CRACKED FWD ENTRY DOOR AT BS 312. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900845 19980429 00845 NM 1998 4 29 SWAA980392 1 19980326 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORROSION ON FLOORBEAM AT BS 947, RBL 48.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042900846 19980429 00846 NM 1998 4 29 SWAA980393 1 19980326 A 5330 SKIN BOEING 737 7372H4 138448C NM VERT STAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND SKIN BELOW LT STAB. REAR SPAR ATTACH CUTOUT IS WORN. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042900847 19980429 00847 NM 1998 4 29 SWAA980394 1 19980326 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 312-348 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOORWAY LOWER SILL I/B SUPPORT ANGLE CORRODED AT BS 312 TO 348, WL 209, LBL 61 . REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900848 19980429 00848 NM 1998 4 29 SWAA980395 1 19980326 A 5320 ANGLE BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND AFT GALLEY DOORWAY LOWER SILL SUPPORT Z-ANGLES CORRODED. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998042900849 19980429 00849 NM 1998 4 29 SWAA980396 1 19980326 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 947.5, WL 208, LBL 53 CRACKED AT FASTENER HOLE. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998042900850 19980429 00850 NM 1998 4 29 SWAA980397 1 19980326 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 986.5, LBL 45 TO RBL 50, WL 208 CORRODED ON UPPER AND LOWER SURFACES. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900851 19980429 00851 NM 1998 4 29 SWAA980398 1 19980326 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT 328, RBL 30, WL 208 CORRODED AT FASTENER HOLE LOWER SURFACE. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900852 19980429 00852 NM 1998 4 29 SWAA980399 1 19980326 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND SUPPORT BEAM AT BS 1010 LBL 34 WL 208, BS 959 RBL 18 WL 208, BS 995 LBL 18 TO BS 1004 LB L 7 WL 208 AND BS 957 RBL 25 WL 208 CORRODED AT FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900853 19980429 00853 NM 1998 4 29 SWAA980400 1 19980326 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND RT FRAME AT BS 6616, RBL 60, WL 201 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900854 19980429 00854 NM 1998 4 29 SWAA980401 1 19980326 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 28, WL 208 ON UPPER AND LOWER SURFACE. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998042900855 19980429 00855 NM 1998 4 29 SWAA980402 1 19980326 A 5320 FRAME BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND GALLEY DOORWAY UPPER FWD STUB FRAME CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900856 19980429 00856 NM 1998 4 29 SWAA980403 1 19980326 A 2613 SENSOR BOEING 737 7372H4 138448C NM LT AC DUCT OUT OF POSITION A SWAA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 53SW 21534 DURING FLIGHT, LEFT WING BODY OVERHEAT ILLUMINATED AT APPROXIMATELY 8,000 FT. LIGHT EXTINGUISHED SHORTLY AFTER CLOSING ISOLATION AND NR 1 ENG BLEED VALVES. REPOSITIONED SENSOR AT LEFT A/C DUCT, OPS CHECKS OK PER BOEING MM. 2 L 7 2 4F A16WE 1998042900857 19980429 00857 NM 1998 4 29 SWAA980407 1 19980327 A 3233 DRAIN PLUG BOEING 737 7373H4 1384600 NM LT MLG ACT LEAKING A SWAA A UNSCHED LANDING K FLUID LOSS IN INSP/MAINT 1 SW 07 620SW 28036 FLIGHT DIVERTER INTO OAK DUE TO A ENG LOW PRESSURE LIGHT ILLUMINATED. A-SYSTEM WAS DECREASING RAPIDLY. LDG GEAR SELEC TOR MOVED TO OFF. A-SYS QUANTITY STABILIZED JUST UNDER 1/4 TANK. INSPECTED AND FOUND LEFT MLG ACTUATOR DRAIN PLUG NOT SAFETIED. RETORQUED AND RESAFETIED DRAIN PLUG. REMOVED AND REPLACED A-SYS CASE DRAIN FILTERS. LEAKS CHECK GOOD PER B OEING MM. REPOSITIONED SENSOR AT LEFT A/C DUCT, OPS CHECKS OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900858 19980429 00858 NM 1998 4 29 SWAA980408 1 19980327 A 2913 PUMP BOEING 737 7373H4 1384600 NM B-HYD SYST FAILED A SWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SW 07 603SW 27954 RETURNED TO PHX DUE TO B-SYS HYD FAILURE AND LEFT WING TO BODY OVERHEAT. REMOVED AND REPLACED CRACKED HEAT EXCHANGER DU CT AND B-SYS ELECTRIC PUMP. 2 L 7 2 4F RT A16WE 1998042900859 19980429 00859 NM 1998 4 29 SWAA980404 1 19980326 A 5320 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 177 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 177 STR 17 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900860 19980429 00860 NM 1998 4 29 SWAA980405 1 19980326 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND 1 INCH CRACK AT BS 178 BULKHEAD, WL 187, RBL 1. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900861 19980429 00861 NM 1998 4 29 SWAA980406 1 19980326 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 372 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED TERMINAL CHECK, FOUND 4 INCH CRACK AT BS 372, 14 ABOVE FLOOR LINE ON LT SIDE OF A/C. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998042900862 19980429 00862 NE 1998 4 29 SWAA980409 2 19980328 A 7230 FAN BLADES BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE DAMAGED A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 357SW 26594 RETURNED TO MSY AND MADE AN UNEVENTFUL LANDING DUE TO BIRD STRIKE TO RADOME AND NR 1 ENGINE. PERFORMED BIRD STRIKE INSP ECTION, FOUND 8 ENGINE FAN BLADES BENT. REMOVED AND REPLACED 8 FAN BLADES PER BOEING MM, WITH A BORESCOPE SCHEDULED WIT HIN 10 CYCLES. 2 L 7 2 4F 4 F RT A16WE E2GL 1998042900863 19980429 00863 NM 1998 4 29 SWAA980410 1 19980329 A 2410 CSD SEAL BOEING 737 7373Y0 1384671 NM NR 1 ENGINE LEAKING A SWAA E ENGINE SHUTDOWN O OTHER CL CLIMB 1 SW 07 682SW 23496 DIVERTED TO MSY DUE TO INFLT SHUTDOWN OF NR 1 ENGINE, WHEN OIL PRESSURE DROPPED BELOW RED LINE, DUE TO CSD CARBON SEAL L EAKING. LANDED WITHOUT INCIDENT. REMOVED THE CSD FOR ENGINEERING EVALUATION OF THE GEARBOX. REPLACED NR 1 ENGINE CSD GARLOC SEAL AND RETAINING RING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900864 19980429 00864 NM 1998 4 29 SWAA980411 1 19980327 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND L-ANGLE FWD BOTTOM DOORWAY FRAME CRACKED AT BS 291.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042900865 19980429 00865 NM 1998 4 29 SWAA980412 1 19980327 A 5320 ANGLE BOEING 737 7372H4 138448C NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND Z-ANGLE AT AFT SERVICE DOOR CORRODED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042900866 19980429 00866 NM 1998 4 29 SWAA980413 1 19980327 A 5320 WEB BOEING 737 7372H4 138448C NM BS 440/490 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB LOWER END FWD OF DOOR CUTOUT CRACKED AT BS 440 AND AT BS 490. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998042900867 19980429 00867 NM 1998 4 29 SWAA980414 1 19980327 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 429 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORROSION UNDERNEATH FLOORBEAM NUT PLATE AT BS 429 RBL 8.5. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1998042900868 19980429 00868 NM 1998 4 29 SWAA980415 1 19980327 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 269 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND ANGLE AND NUT PLATES CORRODED AT BS 269, RBL 11 THRU LBL 10. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1998042900869 19980429 00869 NM 1998 4 29 SWAA980416 1 19980327 A 5330 SKIN BOEING 737 7373H4 1384600 NM R2 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 326SW 23690 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED, .75 LENGTH AT UPPER HINGE CUTOUT AT R2 DOOR. REPAIRED PER SWA R A 1-353-1794. 2 L 7 2 4F RT A16WE 1998042900870 19980429 00870 NM 1998 4 29 SWAA980417 1 19980327 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 911-927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 26L CORRODED AT BS 911 TO 927. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900871 19980429 00871 NM 1998 4 29 SWAA980418 1 19980328 A 5712 RIB BOEING 737 7372H4 138448C NM LT WING GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND DOUBLER REPAIR SPLICE SEALANT MISSING FWD AT BS 540 ALONG STR 3L. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998042900872 19980429 00872 NM 1998 4 29 SWAA980419 1 19980328 A 3244 TIRES BOEING 737 7373H4 1384600 NM MLG FLAT A SWAA K NONE O OTHER LD LANDING 1 SW 07 650SW 27720 AFTER LANDING, FOUND NR 3 AND NR 4 WHEEL TIRES FLAT, WITH NR 3 WHEEL TIRE MISSING A 3 X 6 INCH PIECE OF TREAD. INSPECTE D AND REPLACED NR 3 AND NR 4 WHEEL TIRE ASSY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900873 19980429 00873 NM 1998 4 29 SWAA980420 1 19980327 A 2910 LINE BOEING 737 7373H4 1384600 NM A-HYD SYST LEAKING A SWAA K NONE O OTHER LD LANDING 1 SW 07 654SW 28399 AFTER LANDING, TOWER REPORTED SMOKE IN NR 2 ENGINE AREA. POST FLIGHT INSPECTION REVEALED HYDRAULIC LEAK RT SIDE OF A/C IN RIGHT WING AREA BEHIND NR 2 ENG. INSPECTED AND FOUND HYD LINE BROKEN AT NR 2 ENG AFT PYLON. REMOVED AND REPLACED F IXED TUBE ASSY, SVC'D A-HYD SYSTEM, NO LEAKS CHECKED NORMAL AS PER BOEING MM. INSPECTED AND REPLACED NR 3 AND NR 4 WHEE L TIRE ASSY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900874 19980429 00874 NM 1998 4 29 SWAA980421 1 19980327 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 1 LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 360SW 26571 DURING SCHEDULED C4 CHECK, FOUND NR 1 KRUEGER DEFLECTOR DOOR CUTOUT CRACKED .25 AT RADIUS. REPAIRED PER SWA RA 1-357-0 540. 2 L 7 2 4F RT A16WE 1998042900875 19980429 00875 NM 1998 4 29 SWAA980422 1 19980327 A 5413 LONGERON BOEING 737 7373H4 1384600 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON LONGERON CRACKED JUST FWD OF BUBBLE FAIRING. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900876 19980429 00876 NM 1998 4 29 SWAA980423 1 19980327 A 5320 CROSS MEMBER BOEING 737 7372H4 138448C NM BS 998-999-1001 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR CROSS MEMBER CORRODED AT BS 998 LBL 13.5, BS 999 LBL 11.5 AND BS 1001 LBL 12. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042900877 19980429 00877 NM 1998 4 29 SWAA980424 1 19980327 A 5320 CROSS MEMBER BOEING 737 7372H4 138448C NM BS1008-1010-1011 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR CROSS MEMBER CORRODED AT BS 1008.5 LBL 7.5, BS 1010 LBL 8.5 AND 1011 LBL 6.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042900878 19980429 00878 NM 1998 4 29 SWAA980425 1 19980327 A 5320 CROSS MEMBER BOEING 737 7372H4 138448C NM BS 1011-1013 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR CROSS MEMBER CORRODED AT BS 1011 LBL 6.5, BS 1011 LBL 7.5 AND BS 1013 LBL 6. R EMOVE AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998042900879 19980429 00879 NM 1998 4 29 SWAA980426 1 19980328 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 358 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 358 RBL 63 WL 201. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900880 19980429 00880 NM 1998 4 29 SWAA980427 1 19980328 A 5320 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP FWD CARGO BAY AT BS 400 STR 28L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900881 19980429 00881 NM 1998 4 29 SWAA980428 1 19980328 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 787/807 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND WEB CRACKED BETWEEN BS 787 AND 807, STR 24L WL 161. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900882 19980429 00882 NM 1998 4 29 SWAA980429 1 19980328 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 500 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY DOOR CUTOUT AFT FRAME CLOSEOUT WEB IS GOUGED AND OIL CANNED AT BS 500, WL 156 TO 159, RBL 24 TO 28. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900883 19980429 00883 NM 1998 4 29 SWAA980430 1 19980328 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 727 BONDED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND SKIN BONDED DOUBLER DELAMINATED AT BS 727+18, STR 20 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900884 19980429 00884 NM 1998 4 29 SWAA980431 1 19980328 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 727/767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 727C LT BETWEEN STR 8 AND 9, BS 727D LT BETWEEN STR 8 AND 9 AND BS 767 LT BETWEEN 8 AND 9. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900885 19980429 00885 NM 1998 4 29 SWAA980432 1 19980328 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 787 LT BETWEEN STR 8 AND 9 AT A/C VENT ATTACH BRACKET FASTENER. RE MOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900886 19980429 00886 NM 1998 4 29 SWAA980433 1 19980329 A 5330 SKIN BOEING 737 7373G7 1384595 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 382SW 23783 DURING SCHEDULED C4 CHECK, FOUND DOORWAY SKIN INSIDE FWD LOWER CORNER OF DOOR DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900887 19980429 00887 NM 1998 4 29 SWAA980434 1 19980329 A 5320 WEB BOEING 737 737317 138447P NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED C2 CHECK, FOUND WEB BETWEEN FLOORBEAMS CRACKED AT BS 520 LBL 24.75 AND BS 520 ALONG LBL 45.50 (CRACK IS 1.5 LONG, LOCATED AT THE UPPER AFT CORNER). REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900888 19980429 00888 NM 1998 4 29 SWAA980435 1 19980329 A 5315 FLOORBEAM BOEING 737 737317 138447P NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED C2 CHECK, FOUND FLOORBEAM AT BS 520 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900889 19980429 00889 NM 1998 4 29 SWAA980436 1 19980329 A 5311 FRAME BOEING 737 7373Q8 1384670 NM BS 1064 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED C4 CHECK, FOUND Z-FRAME AT BS 1064 APU BLEED CUTOUT HOLE, DAMAGED 7 AROUND RADIUS. REPAIRED PER SWA RA 1-353-1797. 2 L 7 2 4F RT A16WE 1998042900890 19980429 00890 NM 1998 4 29 SWAA980437 1 19980329 A 5320 ANGLE BOEING 737 737317 138447P NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED BC2 CHECK, FOUND SHEAR WEB AND ANGLE CRACKED AT BS 520, LBL 24.75. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998042900891 19980429 00891 NM 1998 4 29 SWAA980438 1 19980329 A 5330 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED RON CHECK, FOUND A SECTION WITH EMERGENCY TRACK LIGHTING INOP. INSTALLED AND RECONNECTED LIGHT ASSEMBL IES AND OP CHECKED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900892 19980429 00892 NM 1998 4 29 SWAA980439 1 19980329 A 5400 ANGLE BOEING 737 737317 138447P NM LT PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED C2 CHECK, FOUND PANEL ATTACH ANGLE ON TOP OF PYLON CRACKED, INBD SIDE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900893 19980429 00893 NM 1998 4 29 SWAA980440 1 19980329 A 3350 SIGN BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351SW 24572 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT SIGN RT SIDE BROKEN AT OVERWING EXIT DOOR. REMOVED AND REPLACED EXIT SIGN , OPS CHECKED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900894 19980429 00894 NM 1998 4 29 SWAA980441 1 19980329 A 3241 AV24E1144 VALVE BOEING 737 7372H4 138448C NM LANDING GEAR INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 86SW 22827 DIVERTED TO HOU DUE TO ANTI-SKID INOP GEAR DOWN. COULD NOT GO TO AUS DUE TO WET RUNWAYS. LANDED WITHOUT INCIDENT. REM OVED AND REPLACED PARKING BRAKE VALVE, NO LEAKS OPS CHECKED GOOD PER BOEING MM. REMOVED AND REPLACED EXIT SIGN, OPS CHE CKED PER BOEING MM. 2 L 7 2 4F A16WE 1998042900895 19980429 00895 1998 4 29 SWAA980442 4 19980330 A 2565 61621469 SLIDE BOEING 737 7375H4 138449D NM CABIN OUT OF DATE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED CHECK, FOUND L-2 EMERGENCY EVACUATION SLIDE OUT OF DATE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998042900896 19980429 00896 NM 1998 4 29 SWAA980443 1 19980330 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED SERVICE CHECK, FOUND SKIN CRACKED AT BS 767 RT SIDE 5 INCHES BELOW WHITE STRIPE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998042900897 19980429 00897 NM 1998 4 29 98FDEA00226 1 19980401 A 5270 SWITCH BOEING 727 72722 1384002 NM CARGO DOOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 190FE 19083 MAIN CARGO DOOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. REPLACED LOCK ROD SWITCH AND ADJUSTED PER MAINTENANCE MANUAL 52-70 -09, OPERATIONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1998042900898 19980429 00898 WP 1998 4 29 98FDEA00227 1 19980331 A 2910 500134160356 HOSE ASSY DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE BROKEN A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 306FE 48298 APPROXIMATELY 20 MIN INTO FLIGHT, NR 2 HYD QUANTITY AND PRESSURE WENT TO ZERO. ENGINE RAN APPROXIMATELY 55 MINUTES BEFO RE SHUTING DOWN. T/S FOUND NR 2 ENG FIRE-RESISTANT HOSE ASSY BROKEN. REPLACED NEW HOSE ASSY AND REPLACED BOTH ENG DRIV E PUMP AND FILTERS CHECKED, NO CONTAMINATION. REPLACED FILTERS AND LEAK CHK BY ENG RAN NML PER M/M 29-11-02-2, 29-12-0 2-2 ENG RAN BY 136501, 252482. 2 L 7 3 4F RT A22WE 1998042900899 19980429 00899 WP 1998 4 29 SCNA98027 1 19980105 A 2170 COALESCER BAG DOUG DC10 DC1010 3022110 WP NR 1 PACK CONTAMINATED A SCNA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 15 572SC 46977 WHILE WARMING THE COCKPIT TEMPERATURE ZONE TWO HAZY FOG POURED IN VENTS THROUGHOUT THE AIRCRAFT. FOUND NUMBER ONE PACK WATER SEPARATOR DIFFERENTIAL PRESSURE INDICATOR POPPED. RESET INDICATOR AND REPLACED WATER SEPARATOR BAG PER MAINTENAN CE MANUAL CHAPTER 215100. 2 L 7 3 4F A22WE 1998042900900 19980429 00900 1998 4 29 DHL98741002 4 19980331 A 3442 MI585164 ANTENNA BOEING 727 7272Q9 138448M NM FWD FUSELAGE FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 741DH 21931 WEATHER RADAR WILL NOT PAINT GROUND RETURN BETWEEN 30 DEGREES LEFT AND 30 DEGREES RIGHT OF NOSE UNLESS TILT ADJUSTED 7 DEGREES NOSE DOWN. SOLID GROUND RETURN OUTSIDE OF 30 DEGREES LEFT AND RIGHT. FOUND ANTENNA SUPPORT SPRINGS SHEARED AND JAMMED IN MECHANISM. ALSO, FOUND PITCH STAB INOP. REMOVED AND REPLACED ANTENNA. REPAIRED BROKEN WIRE AT D4375 . STAB CHECKS OK PER MM 34-17. 2 L 7 3 4F RT A3WE 1998042900901 19980429 00901 NM 1998 4 29 VNAA9803032 1 19980326 A 3240 AC69963 METERING UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG BRAKES FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 438JS 59092 811 3056 THE RIGHT HAND BRAKE PEDALS ON THE PILOT AND FIRST OFFICERS POSITIONS, PULSATED WHEN BRAKES WERE COMMANDED. THE AIRCRAF T RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE BRAKE METERING UNIT IN ACCORDANCE WITH DORNIER MAINTENAN CE MANUAL 32-42-03. OPERATION AND LEAK CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998042900902 19980429 00902 1998 4 29 TC8A98018 4 19980331 A 3422 25883025 DIRECTIONAL GYRO DOUG DC8 DC862 3021970 WP E/E COMPT REPLACED A TC8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 181SK 6330 45910 SHORTLY AFTER TAKEOFF, F/O COMPASS SYSTEM SPUN AND FROZEN. REMOVED AND REPLACED NR 1 DIRECTIONAL GYRO IAW MM 34-22-00, ALL OPERATIONS OK. 2 L 7 4 4F 4A25 1998042900904 19980429 00904 NM 1998 4 29 SCNA98030 1 19980406 A 7830 62102 SWITCH BOEING 727 7272J4 1384006 NM NR 3 ENG TR INOPERATIVE A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 275AF 20764 AT TAKEOFF, ENGINE NUMBER THREE REVERSE OPERATING LIGHT ILLUMINATED. TAKEOFF ABORTED AT 60 KNOTS. REMOVED AND REPLACED NUMBER THREE ENGINE THRUST REVERSER UNLOCK SWITCH, FUNCTIONALLY CHECK GOOD. 2 L 7 3 4F RT A3WE 1998042900905 19980429 00905 NM 1998 4 29 SWAA980496 1 19980404 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 770 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 770, AT RBL 3. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900906 19980429 00906 NM 1998 4 29 SWAA980497 1 19980404 A 5315 FLOORBEAM BOEING 737 7373T5 NM BS 770 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23064 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 770, AT RBL 3. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900907 19980429 00907 NM 1998 4 29 SWAA980498 1 19980404 A 5320 INTERCOSTAL BOEING 737 7373T5 NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CRACKED AT BS 179, RBL 25 AND LBL 25. REPLACED BOTH PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998042900908 19980429 00908 NM 1998 4 29 SWAA980499 1 19980405 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 332SW 23696 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 22DEF. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998042900909 19980429 00909 NM 1998 4 29 SWAA980500 1 19980405 A 5313 STRINGER BOEING 737 7373H4 1384600 NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED BC3 CHECK, FOUND STRINGER 18A IN RT W/W CRACKED. REPAIRED PER ACO 1-353-1800. 2 L 7 2 4F RT A16WE 1998042900910 19980429 00910 NM 1998 4 29 UPS98226322 1 19980403 A 5320 65C132495 FORGING BOEING 727 72725C 138400H NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-C WHILE WORKING EO#B727-5310-5474B, FOUND CORROSION ON BS 740 FORGING AFT FLANGE COMMON TO FLOORBEAM WL 206 LBL 63. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REPLACED FORGING IAW EO B727-5310-7477, ER 98-2312. 2 L 7 3 4F A3WE 1998042900911 19980429 00911 NM 1998 4 29 UPS98226323 1 19980316 A 5347 BAC1520792 SEAT TRACK BOEING 727 727247 138408F NM BS 870-960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, CORROSION ON SEAT TRACK FLANGE, AS MARKED, IN MAIN DECK BS 870 TO 960 RBL 45 WL 208. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED WITH NEWLY FABRICATED ITEM PER SRM 53-10-5, 51-30-2 AND 51-30-0. 2 L 7 3 4F A3WE 1998042900912 19980429 00912 NM 1998 4 29 UPS98226324 1 19980402 A 5753 65192507 FLAP TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-C, CORROSION (C57-581-05.00-04) NR 7 FLAP TRACK AFT CENTER MOUNT HOLE HAS CORROSION. REMOVED CORROSION ON MOUNT HOLE PER UPS EO NO 727-57-1964. 2 L 7 3 4F A3WE 1998042900913 19980429 00913 NM 1998 4 29 UPS98226325 1 19980402 A 5753 65192507 FLAP TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-SI, CORROSION (C57-581-05.00-04) NR 8 FLAP TRACK CENTER AFT MOUNT HOLE HAS CORROSION. REMOVED CORROSION IN MOUNT HOLE PER UPS EO NR 727-57-1963. 2 L 7 3 4F A3WE 1998042900914 19980429 00914 NM 1998 4 29 UPS98226326 1 19980402 A 5753 65192507 FLAP TRACK BOEING 727 727247 138408F NM TE FLAPS CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 207UP 21699 INSPECTION TYPE-SI, CORROSION (C57-581-05.00-04) NR 7 FLAP TRACK FORWARD MOUNT CENTER HOLE IS CORRODED. REMOVED CORROSI ON IN MOUNT HOLE PER UPS EO NR 727-57-1964. 2 L 7 3 4F A3WE 1998042900915 19980429 00915 WP 1998 4 29 UPS98826327 1 19980401 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, RT WING L/E O/B OF NR 4 ENG, XFS610.00, THE L/E RIB IS CRACKED FWD LWR FLANGE. STOP DRILLED CRACK AN D REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998042900916 19980429 00916 WP 1998 4 29 UPS98826328 1 19980401 A 5720 57698596 DOUBLER DOUG DC8 DC873F 302199F WP WS 230.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, RT I/B STUB WING DOUBLER AT STA XS230.089 IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5769859 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998042900917 19980429 00917 WP 1998 4 29 UPS98826329 1 19980326 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 772.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, RT WING L/E SKIN ON TOP AT STA XFS 772.500 HAS HEAVY CORROSION UNDER THE SURFACE AT 2 SCREWS. REMOVE D DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998042900918 19980429 00918 WP 1998 4 29 UPS98826330 1 19980402 A 5320 57044081 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1480-1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, MAIN CABIN AT STA 1480 TO 1500 AT STR 2R, THE INTERCOSTAL AND ATTACH CLIP BOTH ARE CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL AND ATTACH CLIP IAW DWG 5704408 AND SRM 53-4-1 FIG 49. 2 L 7 4 4F RT 4A25 1998042900919 19980429 00919 NM 1998 4 29 QXEA9800470 1 19980406 A 3350 6038441 POWER SUPPLY GRIMES 82410191011 DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 824PH 157 FORWARD 2 EMERGENGY FLOOR LIGHTS INOP. THE POWER SUPPLY AT 3352 PS 2 WAS REMOVED AND REPLACED, OPERATIONAL CHECK IS GOO D. 2 H 7 2 4T RT A13NM 1998042900920 19980429 00920 EU 1998 4 29 QXEA9800471 1 19980406 A 3350 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 ROW 9E OVERWING EXIT LIGHT INOP. MAINTENANCE RELAMPED SAME, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998042900921 19980429 00921 NM 1998 4 29 98FDEA00255 1 19980407 A 3230 656021132 ACCESSORY UNIT BOEING 727 727277 138408S NM E/E COMPT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 245FE 22016 LANDING GEAR LEVER FAILED TO RELEASE AFTER TAKEOFF. AIRCRAFT STUCK IN GROUND FLIGHT MODE. REMOVED AND REPLACED R92. C OOLING FAN WORKED BUT LEVER LATCH WOULD NOT PULL. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT PER 32-09-122, OPERA TIONAL CHECK NORMAL. LEVER LATCH PULLS FOR LANDING GEAR CONTROL. 2 L 7 3 4F RT A3WE 1998042900922 19980429 00922 NE 1998 4 29 98FDEA00256 2 19980408 A 7321 ECU AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 ENGINE MALFUNCTIONED A FDEA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 25 667FE 771 AT ROTATION, NR 2 ENGINE AND THROTTLE BEGAN TO ROLL BACK. NOTICED FLUX BUT ON PUSHING NR 2 THROTTLE BACK UP, ENGINE RET URNED TO NORMAL. REMOVED AND REPLACED NR 2 ENGINE ECU PER M/M 73-21-01-4. RAN NR 2 ENGINE PER JRH AND M/M 71-00-00-5. POWER ASSURANCE CHECK, ALL PARAMETERS NORMAL. 2 L 7 2 4F 4 F RT A35EU E13NE 1998042900923 19980429 00923 WP 1998 4 29 98FDEA00257 1 19980407 A 3234 GEAR HANDLE DOUG DC10 DC1030F 3023504 WP COCKPIT LACK OF LUBE A FDEA O OTHER J WARNING INDICATION AP APPROACH 1 SO 25 302FE 46801 LANDING GEAR HANDLE WAS PLACED IN DOWN POS. ALL 8 LANDING GEAR POSITION INDICATORS STAYED RED. RECYCLED LANDING GEAR H ANDLE, NO HELP. RED TAB PROCEDURE FOLLOWED. ATL LANDING GEAR EXTENSION HANDLE WAS PULLED. ALL 8 GEAR POSITION INDICAT ORS WENT GREEN. CLEANED AND LUBED HANDLE ASSY PER M/M 32-31-02-7. FOUND PUSH PULL CABLES OUT OF ADJ. RIGGED CABLES PE R MM 32-31-02-2, OPS CKS GOOD. 2 L 7 3 4F RT A22WE 1998042900924 19980429 00924 WP 1998 4 29 MWEA98390 1 19980403 A 5220 591036715 DOUBLER DOUG DC9 DC914 3022034 WP EMER EXIT DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FOUND TWO CRACKS ON THE PLUG DOOR DOUBLERS ON BOTTOM. MTC REMOVED AND REPLACED DOUBLERS. 2 L 7 2 4F A6WE 1998042900925 19980429 00925 NM 1998 4 29 MWEA98391 1 19980406 A 2560 5956953503 SLIDE COVER DOUG MD88 MD88 3023688 NM GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 601ME 49762 THE AFT GALLEY SERVICE DOOR EVACUATION SLIDE COVER DISENGAGED. MTC REINSTALLED AFT GALLEY SLIDE COVER. 2 L 7 2 4F RT A6WE 1998042900926 19980429 00926 NM 1998 4 29 DL757980738 1 19980405 A 3350 POWER SUPPLY BOEING 757 757232 1384965 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 607DL 22814 FLOOR PROXIMITY EMERGENCY ESCAPE PATH MARKING SYSTEM FLOOR WIRING EXPOSED, SOME LIGHTS INOP. REPAIRED FLOOR PROX EMERG ESCAPE PATH TRACK WIRING AND REPLACED F/C POWER SUPPLY MODULE, ALL OPN NOW NORMAL. 2 L 7 2 4F RT A2NM 1998042900927 19980429 00927 NM 1998 4 29 DL76L980739 1 19980405 A 2530 OVEN 828450405 BOEING 767 767332 1382001 NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 185DN 42 27961 F/C GALLEY LOWER OVEN HAD ELECTRICAL HEAT SMELL. OVEN TURNED OFF, SMELL DISSIPATED. REPLACED OVEN AND INSPECTED WIRING , CKS OK. 2 L 7 2 4F RT A1NM 1998042900928 19980429 00928 NM 1998 4 29 DL72E980743 1 19980402 A 5320 CHANNEL BOEING 727 727247 138408F NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 282WA 21484 THE AFT CHANNEL OF THE VENTRAL STAIRWAY TORQUE BOX AT FS 1263 WAS FOUND WITH A TYPICAL CRACK. THE DAMAGED PART WAS REMO VED AND REPLACED WITH A NEW PART PER THE REQUIREMENTS OF BAC S/B 727-53-0129 AND DOCUMENTED PER ER/A 364426-14AD. 2 L 7 3 4F A3WE 1998042900929 19980429 00929 NM 1998 4 29 DLM90980744 1 19980329 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 812/793/775 LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 LIGHTNING STRIKE DAMAGE WAS FOUND ON THE WINDOW BELT SKIN PANEL SURROUNDING WINDOWS 29, 30 AND 31. THE DAMAGE WAS BLEND ED OUT. THE DAMAGE AT WINDOW 30 WAS FOUND TO BE ACCEPTABLE AND THE DAMAGE AT WINDOW 29 AND 31 WAS REPAIRED PER DAC REWO RK DWG SRO9530053. THE REPAIR WAS DOCUMENTED PER ER/A 364363-14 AND APPROVED PER FAA 8110-3. 2 L 7 2 4F RT A6WE 1998042900930 19980429 00930 NM 1998 4 29 DLM88980746 1 19980401 A 5320 JAMB DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 904DE 53409 THE LOWER JAMB PAN OF THE C1 DOOR SURROUND LOWER SILL WAS FOUND CORRODED AND REQUIRED SPLICING. THE CORRODED SECTION WA S CUTOUT AND A NEW SECTION WAS SPLICED IN PER THE GUIDLINES OF THE MD-88 SRM 53-05, FIG 44 AND ER/A 364414-14. 2 L 7 2 4F RT A6WE 1998042900931 19980429 00931 NM 1998 4 29 DL76S980747 1 19980331 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1197-1307 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 135DL 25145 THE FUSELAGE SKIN AT FS 1197+110 WAS BADLY DAMAGED BY AN IMPACT FROM GROUND EQUIPMENT. THE SKIN WAS CUTOUT BETWEEN STR 35R AND 39L RESULTING IN A 15.5 X 19.5 CUTOUT. THE DAMAGED SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER INSTALLED PE R ER/A 364390-14, REV A. 2 L 7 2 4F RT A1NM 1998042900932 19980429 00932 NM 1998 4 29 DL72S980748 1 19980320 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 DURING SHOP INSPECTION, THE NR 3 MIDFLAP WAS FOUND WITH A CRACK IN THE AFT LOWER CLOSEOUT ANGLE, 18 FROM I/B END. THE A NGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998042900933 19980429 00933 NM 1998 4 29 DL72S980749 1 19980320 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 DURING SHOP INSPECTION, A DOUBLER ON THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED ANGLE, 32 FROM I/B END. THE ANGLE WAS R EPAIRED PER 727 MM 57-52-0 FIG 802 BY INSTALLING/REPLACING THE REPAIR DOUBLER. 2 L 7 3 4F A3WE 1998042900934 19980429 00934 NM 1998 4 29 DL72S980750 1 19980221 A 5753 ANGLE BOEING 727 727232 1384082 NM LT TE MID FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 AFT LOWER CHORD ANGLE IS DAMAGED 29 FROM O/B END OF NR 2 MIDFLAP. REPAIRED PER M/M 57-52-0 FIG 802, INSTALLED DOULBER. 2 L 7 3 4F A3WE 1998042900935 19980429 00935 WP 1998 4 29 DLL10980751 1 19980403 A 5320 1512169101102 FITTING LKHEED 1011 10113851 5265010 WP BS 901 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 TWO OF THE LWR DOOR SILL INBD CAP FITTINGS LOCATED AT FS 901 USED ON BOTH RT AND LT SIDES WERE FOUND CORRODED AND REQUIR ED REPLACEMENT. REPAIRED PER ERA 331465-14. 2 L 7 3 4F A23WE 1998042900936 19980429 00936 WP 1998 4 29 DLL10980752 1 19980403 A 5712 1527032308 RIB LKHEED 1011 10113851 5265010 WP WS 529 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 RT WING IWS 529 RIB, UPPER CAP WAS FOUND CRACKED. PART REPLACED PER ERA 331467-14. 2 L 7 3 4F A23WE 1998042900937 19980429 00937 WP 1998 4 29 DLL10980753 1 19980403 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 718 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 DENTS FOUND ON FUSE SKIN FROM 709 TO 730 BETWEEN S22-24. REPAIRED PER ERA 331484-14. 2 L 7 3 4F A23WE 1998042900938 19980429 00938 WP 1998 4 29 DLL10980754 1 19980403 A 5320 PRESSURE DECK LKHEED 1011 10113851 5265010 WP BS 395-437 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 NLG PRESSURE DECK WAS FOUND CRACKED IN FIVE LOCATIONS. ALL WERE AT THE EDGES OF PAD UP AREAS IN THE PANEL WHERE THE NLG VERT WALL STIFFENERS TIE INTO THE PRESSURE DECK. REPAIRED PER ERA 331507-14. 2 L 7 3 4F A23WE 1998042900939 19980429 00939 NM 1998 4 29 DL72S980755 1 19980402 A 5330 65562312 BEAR STRAP BOEING 727 727232 1384082 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 THE R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRA CK WAS STOP DRILLED AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED PER THE DIRECTION OF BAC S/B 727-53-0136 AND ER/A 364433-14. 2 L 7 3 4F A3WE 1998042900940 19980429 00940 WP 1998 4 29 DLL10980756 1 19980403 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 1615 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 MULTI ELEMENT CORROSION WAS FOUND IN THE AFT LT SIDE OF THE C2 CARGO COMPT BETWEEN FS 1585 AND FS 1665. DAMAGE INCLUDES SKIN, STRINGERS, FRAME AND SKIN CLIP. REPAIRED PER ERA 331474-14. 2 L 7 3 4F A23WE 1998042900941 19980429 00941 WP 1998 4 29 DLL10980757 1 19980403 A 5310 LS13112 PANEL LKHEED 1011 10113851 5265010 WP FS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 FUSE HORIZ PRESSURE DECK PANEL WAS FOUND WITH APPROX 0.75 INCH CRACK. THE CRACK IS LOCATED AT RBL 102 JUST AFT OF FS 37 8. REPAIRED PER ERA 331483-14. 2 L 7 3 4F A23WE 1998042900942 19980429 00942 WP 1998 4 29 DLL10980758 1 19980403 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FS 328 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 AT HMV, FS 328 BLKHD EXTRNL SKIN DOUBLERS WERE FOUND CORRODED BETWEEN THE FUSE SKIN AND SKIN DOUBLER. ADDITIONAL INSPEC TION FOUND TWO CRACKS IN THE FUSE SKIN AND ORIGNAL INTERNAL DOUBLER. REPAIRED PER ERA 331542-14AD. 2 L 7 3 4F A23WE 1998042900943 19980429 00943 WP 1998 4 29 DLL10980759 1 19980403 A 5730 1527140106 SKIN LKHEED 1011 10113851 5265010 WP WS 477 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 WHILE ACCOMPLISHING INSPECTION PER SI7-70953-12AD, A CRACK INDICATION WAS FOUND ON THE RT WING LWR SURFACE AT IWS 477, S 17. REPAIRED PER ERA 331493-14AD. 2 L 7 3 4F A23WE 1998042900944 19980429 00944 WP 1998 4 29 DLL10980760 1 19980403 A 5730 1527139107 SKIN LKHEED 1011 10113851 5265010 WP WS 570 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 WHILE ACCOMPLISHING INSPECTIONS PER SI 7-70958-12AD, A CRACK INDICATION WAS FOUND ON THE LT WING LWR SURFACE AT IWS 570, S10. REPAIRED PER ERA 331492-14AD. 2 L 7 3 4F A23WE 1998042900945 19980429 00945 WP 1998 4 29 DLL10980761 1 19980403 A 3221 FITTING LKHEED 1011 10113851 5265010 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 DURING RTN INSPECTION OF THE FS 449 BLKHD WALL, TYP DAMAGE WAS FOUND TO THE RT NLG TRUNNION FITTING. REPAIRED PER ERA 3 31464-14AD. 2 L 7 3 4F A23WE 1998042900946 19980429 00946 WP 1998 4 29 SCNA98031 1 19980402 A 2611 SMOKE DETECTOR DOUG DC10 DC1015 3022118 WP LAVATORY MALFUNCTIONED A SCNA K NONE P NO WARNING INDICATION UK UNKNOWN 1 GL 15 151SY 48295 TWO PASSENGERS WERE CAUGHT SMOKING IN THE LAVATORIES AND THE SMOKE DETECTORS FAILED TO GO OFF. ALL LAVATORY SMOKE DETEC TORS SUBJECTED TO LIVE SMOKE TEST WITH NO FAULT FOUND. SMOKE DETECTORS INSPECTED FOR TAMPERING AND NO DEFECTS NOTED. 2 L 7 3 4F A22WE 1998042900947 19980429 00947 WP 1998 4 29 DHL98801003 1 19980407 A 3246 26014112 WHEEL DOUG DC8 DC873 302199C WP NR 2 MLG MISSING A A DHLA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 801DH 46033 WHILE RETURNING TO RAMP, AIRCRAFT GROUND HANDLING BECAME ABNORMAL. INSPECTION REVEALED NUMBER 2 TIRE MISSING AND NUMBER 1 TIRE FAILED. REMOVED AND REPLACED NUMBER 1 AND NUMBER 2 MAIN WHEEL ASSY AND NR 2 WHEEL TRANSDUCER. 2 L 7 4 4F RT 4A25 1998042900948 19980429 00948 WP 1998 4 29 CKSA98206 1 19980326 A 3350 POWER PACK LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 DURING TERMINATION OF SERVICE CHECK, FOUND EMERGENCY FLOOR LIGHT 15DE WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIG HT POWER PACK, OPS CHECK GOOD IAW 33-51-03. 2 L 7 3 4F A23WE 1998043000009 19980430 00009 NM 1998 4 30 DL76L980298 1 19980203 A 2750 SENSOR BOEING 767 767332 1382001 NM TE FLAPS MISWIRED A DALA O OTHER J WARNING INDICATION CR CRUISE 1 SO 27 179DN 25144 FLAP INDICATOR JUMPS FROM 0 TO 1/2 AND L/E SLAT ASYM CAUSING MSG ALONG WITH LEADING EDGE LIGHT. THIS HAPPENED SEVERAL T IMES ON DESCENT. L/E SLATS WERE VISUALLY CHECKED FLAPS WOULD NOT EXTEND NORMALLY OR VIA PRM PROC FOR ALT FLAP EXT. NO FLAP LANDING DONE AT ATL. REWIRED NR 12 O/B SENSOR (S294) AND NR 11 O/B SENSOR (S295) FROM SENSORS TO WING ROOT (D4628) . SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A1NM 1998043000010 19980430 00010 NM 1998 4 30 DLM11980313 1 19980205 A 2520 PROJECTOR DOUG MD11 MD11 3023602 NM RROYCE RB211 RB21122B02 54555 NE CABIN SMOKING A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 809DE 48480 010517 SMOKE AND ELECTRIC SMELL FROM B/C PROJECTOR DURING TAXI OUT. DISABLED B/C PROJECTOR. INSPECTED AREA, NO TROUBLE FOUND. 2 L 7 3 4F 4 F RT A22WE E12EU 1998043000011 19980430 00011 NM 1998 4 30 DL72W980318 1 19980205 A 3350 LIGHT 1000677 BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 295WA 5289 22532 DURING L/O, FOUND EMER EXIT LIGHT ASSY AT THE AFT OVERHEAD LIGHT ASSY INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1998043000012 19980430 00012 NM 1998 4 30 DL72S980320 1 19980203 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1030 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 CORROSION ON FLOORBEAM STA 1030 AT BOLT HOLES AT BL 0, LBL 9 AND RBL 10.5. CORROSION WITHIN LIMITS AT BL 0 AND RBL 10.5 . CORROSION OUT OF LIMIT AT STA LB 9 PER SRM 53-10-1. INSTALLED REPAIR PER M/M 53-20-11. 2 L 7 3 4F A3WE 1998043000013 19980430 00013 NM 1998 4 30 DL72L980321 1 19980205 A 3230 TORQUE TUBE 324704052 BOEING 727 727232 1384082 NM RT MLG FAILED A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 508DA DL603R 21310 UPON T/O, AFTER GEAR RETRACTION (DOORS LIGHT REMAINED ILLUMINATED AND RT GEAR DOOR LIGHT ON S/O PNL WAS ON. ADDITIONALL Y RT GEAR AND GREEN GEAR LIGHTS REMAINED ILL.VISUAL INSP CONFIRMED RMLG WAS DWN. ACCOMPLISHED POM WITH GEAR HANDLE UP P OS THE LIGHTS REMAINED THE SAME. REPLACED UP-LOCK TORQUE TUBE DUE SHEARED RIVITS. GEAR RETRACTION PER MM CK NML. 2 L 7 3 4F A3WE 1998043000014 19980430 00014 NM 1998 4 30 DL72S980323 1 19980206 A 3610 04301512150 CLAMP BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE BROKEN A DALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 468DA 66166 20745 687403 AT CRUISE, GOT NR 1 ENG FIRE WARNING. SHUTDOWN ENGINE. REPLACED CLAMP ON 13TH STG DUCT AND REPAIRED BURNED WIRES. 2 L 7 3 4F 4 F A3WE E2EA 1998043000016 19980430 00016 NM 1998 4 30 DL72W980325 1 19980206 A 5330 SKIN BOEING 727 727247 138408F NM FS 580 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 A 1 X 1 CUTOUT WAS MADE IN THE FUSELAGE SKIN AT FS 580 JUST ABOVE STRINGER 27L. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 363961-14, REV A. 2 L 7 3 4F A3WE 1998043000017 19980430 00017 NM 1998 4 30 DL72S980326 1 19980204 A 5330 65545831 SKIN BOEING 727 727225 1384077 NM BS 1160 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 WHILE ACCOMPLISHING MODIFICATIONS AROUND THE AFT LAV SERVICE PANEL CUTOUT IN THE SKIN, THE BONDED INTERNAL DOUBLER WAS T ORN IN SEVERAL LOCATIONS. THE SKIN AND BONDED DOUBLER WERE CUTOUT AND REMOVED BETWEEN FS 1158 AND 1183 AND BETWEEN STR 20L AND 23L. A NEW SECTION OF SKIN WAS SPLICED IN PER ER/A 363813-14, REV B. 2 L 7 3 4F A3WE 1998043000018 19980430 00018 NM 1998 4 30 DLM88980327 1 19980207 A 3230 STRUT DOUG MD88 MD88 3023688 NM NLG REQD SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 926DL 49713 DURING GEAR RETRACTION, NOSE GEAR DID NOT STOW IN WELL PROPERLY. NOSE GEAR UNSAFE LIGHT ON. FOUND NOSE STRUT UNDERSERV ICED. SERVICED STRUT PER MM. 2 L 7 2 4F RT A6WE 1998043000019 19980430 00019 NM 1998 4 30 DL767980328 1 19980207 A 3350 BPS73 POWER SUPPLY BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 102DA 22214 SECTIONS OF SEAT MOUNTED EMERGENCY LIGHTING INOP. FOUND ON PREFLIGHT. REPLACED POWER SUPPLY, SYSTEM CKS GOOD. 2 L 7 2 4F RT A1NM 1998043000020 19980430 00020 NM 1998 4 30 DL72S980332 1 19980208 A 2560 MV10 MEGAPHONE BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 478DA 20755 FOUNDED FWD MEGA PHONE INOP. REPLACED SAME, CKS OK. 2 L 7 3 4F A3WE 1998043000021 19980430 00021 NE 1998 4 30 DL76S980333 2 19980208 A 7320 FUEL LINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 1 ENGINE LOOSE A A DALA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 27 128DL 24239 24078 ON DESCENT AT FL200 WITH ENGINE ANTI-ICE TURNED ON AND AUTO THROTTLES ENGAGED RT ENGINE ADV TO FULL POWER AND LT ENGINE REMAINED AT IDLE. N1 COMMAND BUG SHOWED FULL POWER REQUESTED ENGINE STAYED AT IDLE. MAINT FOUND FUEL LINE CONN AT FUEL FLOW METER LOOSE AND LEAKING. REINSTALLED MOUNT BOLTS AND SAFETIED PER M/M. MOTORED ENG NO FURTHER LEAKS RAN ENG PER PFHB IND NORM. 2 L 7 2 4F 4 F RT A1NM E13NE 1998043000022 19980430 00022 NM 1998 4 30 DL72K980334 1 19980209 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 472DA 20749 SEVERAL OF THE FASTENER HOLES ON THE S18A STRINGER AT FS 940 OF BOTH RT AND LT SIDES WERE FOUND TO HAVE CRACKS AND OR CO RROSION IN THEM. REPAIRED PER ERA 331316-14. 2 L 7 3 4F A3WE 1998043000023 19980430 00023 WP 1998 4 30 DLL19980335 1 19980209 A 5711 SPAR LKHEED 1011 10113853 5265020 WP LT/RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 753DA 193W1189 DURING INSPECTION OF THE LT AND RT WING REAR SPAR UPPER CAP FASTENER HOLES PER EO 7-59089-3 SEVERAL CRACK INDICATIONS WE RE FOUND ON THE RT REAR SPAR. ALL NON CRACKED HOLES WERE COLD WORKED. THE AREA WAS THEN REPETITIVELY INSPECTED. ALL C OVERED BY PREVIOUS ERA 304992-14. A DECISION WAS MADE TO ACCOMPLISH REAR SPAR MOD DUE TO REPETITIVE INSPECTION REQ. RE PAIR PER ERA 331265-14AD WHICH TERMINATES ACTION FOR SI7-71067-12AD. 2 L 7 3 4F A23WE 1998043000024 19980430 00024 NM 1998 4 30 DL73S980336 1 19980209 A 5320 INTERCOSTAL BOEING 737 737232 1384475 NM BS 338 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 DURING INSPECTION, THE R1 DOOR INTERCOSTALS WERE FOUND CRACKED AT 3 LOCATIONS BETWEEN BS 332 AND 344. THE DAMAGED INTER COASTALS WERE LOCATED AT S8A, 10A AND 11. REPAIRED PER ERA 331341-14AD. 2 L 7 2 4F RT A16WE 1998043000025 19980430 00025 NM 1998 4 30 DL73S980337 1 19980209 A 5330 SKIN BOEING 737 737232 1384475 NM BS 380 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 DURING INSPECTION, A DENT WAS FOUND IN THE FUSELAGE SKIN AT APPROX STA 380 AND S18L. REPAIRED PER ERA 331346-14. 2 L 7 2 4F RT A16WE 1998043000026 19980430 00026 NM 1998 4 30 DLM88980338 1 19980209 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 984DL 53311 FS 1418 WAS CRACKED AT L2L ON, WHICH IS ONE OF THE TYP LOCATIONS. REPAIRED PER ERA 331297-14. 2 L 7 2 4F RT A6WE 1998043000027 19980430 00027 NM 1998 4 30 DL73S980339 1 19980209 A 5312 65163007 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 DURING INSPECTION, SERVERAL CRACKS WERE FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS WERE LOCATED AT WL 192 TO 202 AND LBL 5 AND RBL 5. REPAIRED PER ERA 331313-14. 2 L 7 2 4F RT A16WE 1998043000028 19980430 00028 NM 1998 4 30 DL73S980340 1 19980209 A 5743 654948832 FITTING BOEING 737 737232 1384475 NM RT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 328DL 23100 DURING INSPECTION PER SI3-66022-12, THE RT MLG BEAM AFT SUPPORT FITTING ON THE REAR SPAR WAS FOUND WITH CRACKS. THE CRA CKS WERE IN THE FITTING AND THE SPAR CAP AND WEB. THE DISCREPANT HOLES WERE OVERSIZED. REPAIR PER ERA 331333-14. 2 L 7 2 4F RT A16WE 1998043000029 19980430 00029 NM 1998 4 30 DL72W980341 1 19980209 A 5312 6516350314 BULKHEAD BEAM BOEING 727 727247 138408F NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 MTC FOUND A .1875 INCH CRACK IN THE OUTBD AFT FLANGE OF THE RBL 8 VERT BEAM IN THE FS 1183 BLKHD, WHICH BEGINS AT WL 182 . REPAIRED PER ERA 362891-14, REV A. 2 L 7 3 4F A3WE 1998043000030 19980430 00030 NM 1998 4 30 DLM88980342 1 19980209 A 5520 39226095 BRACKET DOUG MD88 MD88 3023688 NM LT HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 984DL 53311 THE XE204.114 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORIZ STAB WAS FOUND TO HAVE CORROSION. REPAIRED AND RE WORKED PER ERA 331309-14. 2 L 7 2 4F RT A6WE 1998043000031 19980430 00031 NM 1998 4 30 DLM88980343 1 19980209 A 5520 49180195 BRACKET DOUG MD88 MD88 3023688 NM LT HORIZ STAB CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 984DL 53311 XE225.834 ELEVATOR HINGE SUPPORT BRACKET ATTACHED TO THE LT HORIZ STAB WAS FOUND TO CONTAIN CORROSION. REPAIRED AND REW ORKED PER ERA 331301-14. 2 L 7 2 4F RT A6WE 1998043000032 19980430 00032 NM 1998 4 30 DL72W980345 1 19980127 A 5320 BOX BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 WING ICE LIGHT BOX BETWEEN STA 720B AND 720C AT STR 15L IS CORRODED. REPAIRED PER SRM 53-30-3 FIG 22. 2 L 7 3 4F A3WE 1998043000033 19980430 00033 NM 1998 4 30 DL72W980346 1 19980204 A 5741 FITTING BOEING 727 727247 138408F NM RT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 CORROSION RT AFT WING TERMINAL FITTING AFT BUSHING BORE. BORED FITTING BORE TO 4.500 PER SRM 53-40-01 TO REMOVE CORROSI ON. TURNED BUSHING TO PROPER FIT. TREATED BUSHING. OK TO TREAT FITTING BORE. TREATED BORE, OK TO INST SLEEVE. INSTA LLED SLEEVE PER SRM 53-40-0. BUSHING AND TERMINAL PIN INSTALLED ON NR 1119. 2 L 7 3 4F A3WE 1998043000077 19980430 00077 NM 1998 4 30 P2EA98005 1 19980126 A 5311 FRAME BOEING 737 737222 1384473 NM BS 500 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - DURING C-CHECK, FUSELAGE FRAME, UPPER FLANGE CRACKED, IN FORWARD CARGO COMPARTMENT AT BS 500, BETWEEN STRINGER 19L AND 21L, CRACK SIZE 11 INCH BY 4 INCH. REPAIRED FUSELAGE FRAME CRACK, PER SRM 53-10-4 FIG 1. (M) 2 L 7 2 4F A16WE 1998043000079 19980430 00079 NM 1998 4 30 98ZZZM209 1 19980118 A 3310 1041021 LIGHT SOCKET BOEING 727 72751C 1384015 NM COCKPIT BURNED A RYNA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 07 436EX 19289 FLT 6704 - IND-SEA - AIR RETURN TO IND, CLIMBING OUT OF IND CREW EXPERIENCED A STRONG ELECTRICAL ODOR AND SMOKE WAS CLEA RLY VISIBLE UNDER CAPTAINS GLARESHIELD. REMOVED AND REPLACED BOTH INBOARD FLOURESCENT LIGHT SOCKETS. (M) 2 L 7 3 4F A3WE 1998043000083 19980430 00083 CE 1998 4 30 98ZZZM213 1 19980118 A 3233 114380041 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG FAILED A JJBA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 01 854CA 9417 UE60 GEAR WOULD NOT EXTEND. MLG ACTUATOR LEAKING. REMOVED AND REPLACED LT MLG ACTUATOR. (M) 2 L 7 2 4T RT A24CE 1998043000084 19980430 00084 WP 1998 4 30 HALA9800033 1 19980203 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN BROKEN A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 603DC 47784 HNL - FLT 508 - FOUR ROWS OF EMERGENCY LIGHTS INOP. REPAIRED BROKEN WIRES. (M) 2 L 7 2 4F RT A6WE 1998043000085 19980430 00085 WP 1998 4 30 HALA9800030 1 19980202 A 3350 POWER PACK DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 152AA 46707 HNL - FLT 9 - EMERGENCY LIGHT TEST FAIL, INOP. EMERGENCY LIGHT PANEL FAIL ON OVERWING LIGHT. REMOVED AND REPLACED EMER GENCY LIGHTS POWER PACK AT 3R AND 3L DOORS. OPS CHECK OK, OK FOR SERVICE. (M) 2 L 7 3 4F A22WE 1998043000086 19980430 00086 1998 4 30 HALA9800031 4 19980202 A 2360 STATIC WICK DOUG DC9 DC951 3022051 WP LT ELEVATOR DAMAGED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 669HA 47654 HNL - EVIDENCE OF LIGHTING STRIKE ON LEFT ELEVATOR TRAILING EDGE NEAR OUTBOARD STATIC WICK UNDERSIDE. PERFORMED LIGHTIN G STRIKE INSPECTION PER MM 5-53-0, TOP OF FUSELAGE FROM LEFT WINDOW BELT TO RT WINDOW BELT PEND AND 2B, 5 AND 6. COMPLE TED LIGHTING STRIKE INSPECTION PER MM 5-53-0. FOUND STATIC WICK BAD. REPLACED STATIC WICK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998043000087 19980430 00087 WP 1998 4 30 HALA9800028 1 19980130 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 673MC 47726 HNL - FLT 128 - EMERGENCY LIGHTS MID CABIN ON CEILING, DO NOT COME ON. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998043000088 19980430 00088 WP 1998 4 30 GTIA9800008 1 19980109 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12505 45788 ACY - FLT 119 - CABIN FLOOR LIGHTING REAR EMERGENCY EXIT ROW NEEDS FIXING. REPAIRED WIRING AT SEAT TRACK SEAT 11 IAW W/ D 33-51-03. GROUND OPS CHECK OK. (M) 2 L 7 2 4F A6WE 1998043000089 19980430 00089 WP 1998 4 30 GTIA9800009 1 19980113 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - CEILING EMERGENCY LIGHTS ON LEFT SIDE BETWEEN ROWS 15-21 ARE OUT. REMOVED AND REPLACED BATTERY POWER SUPPLY WITH SERVICEABLE BATTERY POWER SUPPLY IAW DC-9 MM CH 33-58-0. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998043000090 19980430 00090 WP 1998 4 30 GTIA9800010 1 19980114 A 3350 RPSIB BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - EMERGENCY LIGHTS IN AFT CABIN STAY ON AT ALL TIMES. FOUND EMERGENCY LIGHTS BATTERY PACK B35-39, STATION 1000 FAUL TY. REPLACED BATTERY PACK B5-39 AND FUNCTIONALLY TESTED SYSTEM IAW DC-9 MM 33-53-0. (M) 2 L 7 2 4F A6WE 1998043000091 19980430 00091 WP 1998 4 30 GTIA9800011 1 19980114 A 3350 60030431 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - EMERGENCY LIGHTS IN CENTER CABIN INTERMITTENT. FOUND EMERGENCY LIGHT BATTERY PACK B5-25, STATION 639R, FAULTY. R EPLACED B5-25 BATTERY PACK IAW DC9 MM 33-53-0. SYSTEM OPS CHECK NORMAL IAW DC-9 MM 33-53-0. (M) 2 L 7 2 4F A6WE 1998043000092 19980430 00092 WP 1998 4 30 GTIA9800012 1 19980114 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - EMERGENCY LIGHTS COME ON WITH BATTERY SWITCH IN OFF POSITION. FOUND NR 2 WIRE ON EMERGENCY LIGHT BATTERY PACK B5- 5 BROKEN. REPAIRED WIRE, EMERGENCY LIGHT SYSTEM. OPS CHECK NORMAL ON GRUOND 33-53-0. (M) 2 L 7 2 4F A6WE 1998043000093 19980430 00093 WP 1998 4 30 GTIA9800013 1 19980110 A 3350 P207001101 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 DTW - FLT 617 - AFT UPPER PORTABLE FLASHLIGHT INOP. REMOVED AND REPLACED PORTABLE FLASHLIGHT IAW DC-9 MM 33-50-0. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998043000094 19980430 00094 WP 1998 4 30 GTIA9800014 1 19980118 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 ACY - FLT 119 - FORWARD EMERGENCY FLASHLIGHT INOP NOT FLASHING. REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT, OPS CHECK GOOD ON GROUND. (M) 2 L 7 2 4F A6WE 1998043000096 19980430 00096 CE 1998 4 30 98ZZZM214 1 19980129 A 3234 1013841377 CONTROL HANDLE BEECH 1900 1900 1154160 CE LANDING GEAR FAILED A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 192GA 409 UB17 FLT 7448 - TPA-EYW - LANDING GEAR WILL NOT RETRACT. AIRCRAFT RETURNED TO TPA AND WITHOUT INCIDENT. AIRCRAFT WAS FERRIE D TO MIA WERE MAINTENANCE REPLACED THE LANDING GEAR CONTROL HANDLE ASSY. (M) 2 L 7 2 4T RT A24CE 1998043000097 19980430 00097 CE 1998 4 30 98ZZZM215 1 19980123 A 2150 ACM BEECH 1900 1900C 1154161 CE CABIN CONTAMINATED A GUUA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 11ZR UB11 FLT 7391 - EYW-MCO - SMOKE IN COCKPIT DUE TO ENVIROMENTAL VALVE. AIRCRAFT RETURNED TO EYW AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO MIA. MAINTENANCE CLEANED OFF RESIDUAL SOAP IN ACM ORFICE. (M) 2 L 7 2 4T RT A24CE 1998043000098 19980430 00098 CE 1998 4 30 98ZZZM216 1 19980126 A 3260 1013810061 SWITCH BEECH 1900 1900C 1154161 CE NLG FAILED A GUUA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 11ZR UB11 FLT 7177 - FLL-MCO - THE LANDING GEAR FAILED TO RETRACT FULLY AFTER TAKEOFF. EXTENDED GEAR, RETURNED TO FLL, AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO MIA. MAINTENANCE REPLACED THE NOSE LANDING GEAR UPLOCK SWITCH. SATISFACTOR Y CHECKS ON JACKS. (M) 2 L 7 2 4T RT A24CE 1998043000099 19980430 00099 CE 1998 4 30 98ZZZM217 1 19980123 A 5521 10162001445 SPAR CAP BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 198GA UB5 AT SCHEDULED EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS TO HAVE INTERGRANULAR CORROSION THE LAST FOUR INCHES OUTBOARD. REPLACED LEFT ELEVATOR UPPER AND LOWER SPAR CAPS, P/N'S 101-920014-45, AND 101-620014-47. ( M) 2 L 7 2 4T RT A24CE 1998043000100 19980430 00100 CE 1998 4 30 98ZZZM218 1 19980123 A 5510 1016200111 HINGE BEECH 1900 1900C 1154161 CE LT ELEVATOR CORRODED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 198GA UB5 AT SCHEDULED EMPENNAGE INSPECTION DETERMINED LEFT ELEVATOR, OUTBOARD AND CENTER HINGE ATTACH BRACKETS TO HAVE INTERGRANU LAR CORROSION. REMOVED AND REPLACED OUTBOARD AND CENTER HINGE, ATTACH BRACKETS. (M) 2 L 7 2 4T RT A24CE 1998043000105 19980430 00105 EU 1998 4 30 RAIA980113 1 19980113 A 7797 310465701 WIRE HARNESS AEROSP ATR42 ATR42300 8680920 EU LT ENGINE SHORTED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 424TE 20639 124 FLT 7138 - STL - LEFT ENGINE TORQUE SURGES IN FLIGHT. MAINTENANCE REPAIRED WIRING ON LEFT ENGINE WIRING HARNESS. (M) 2 H 7 2 4T RT A53EU 1998043000106 19980430 00106 EU 1998 4 30 RAIA980116 1 19980116 A 3234 F96GA0102 GEAR HANDLE AEROSP ATR72 ATR72202 8680940 EU INST PANEL FAILED A RAIA B EMER. DESCENT O OTHER LD LANDING 1 CE 03 721TE 217 FLT 7019 - STL - LANDING GEAR WOULD NOT RETRACT. GEAR REMAINED DOWN AND LOCKED. MAINTENANCE REPLACED LANDING GEAR HAND LE. (M) 2 H 7 2 4T RT A53EU 1998043000107 19980430 00107 EU 1998 4 30 RAIA980117 1 19980116 A 3040 327310 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU LT WINDSHIELD FAILED A RAIA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 CE 03 433AM 885 FLT 7512 - STL - LEFT FORWARD COCKPIT WINDSCREEN HEATING ELEMENTS BEGAN GLOWING, CREW TURNED WINDSCREEN HEAT OFF. MAINT ENANCE FOUND LEFT WINDSCREEN HEAT CONTROLLER FAULTY. REPLACED LEFT CONTROLLER AND WINDSCREEN. (M) 2 L 7 2 4T RT A56EU 1998043000108 19980430 00108 EU 1998 4 30 RAIA980118 1 19980118 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 867AE 13844 867 FLT 4737 - SFO - LEFT ENGINE FIRE CAPTION ILLUMINATED DURING TAXI. MAINTENANCE INSPECTED FOUND LEFT ENGINE FIRE LOOP TO BE FAULTY. NO INDICATION OF FIRE. REPLACED LEFT ENGINE FIRE LOOP. (M) 2 L 7 2 4T RT A56EU 1998043000109 19980430 00109 EU 1998 4 30 RAIA980120 1 19980119 A 3297 WIRE AEROSP ATR72 ATR72202 8680940 EU LT MLG BROKEN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 721TE 12178 217 FLT 7141 - MEM - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPAIRED BROKEN WIRE AT LEFT MAIN LANDING GE AR WEIGHT ON WHEELS PROXIMITY SWITCH. (M) 2 H 7 2 4T RT A53EU 1998043000110 19980430 00110 EU 1998 4 30 RAIA980121 1 19980121 A 7720 31055016 INLET TEMP SENSR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 559HK 5168 41075 FLT 7478 - STL - LEFT ENGINE INTEGRATED ELECTRONIC CONTROL FAULT ILLUMINATED ACCOMPANIED BY LEFT ENGINE ANTI-ICE FAULT. MAINTENANCE REPLACED LEFT ENGINE INLET TEMPERATURE SENSOR. (M) 2 L 7 2 4T RT A41NM 1998043000111 19980430 00111 EU 1998 4 30 RAIA980128 1 19980125 A 3230 7445B RELEASE VALVE BAG JETSTM JETSTM3201 1500217 EU HYD BAY TRIPPED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 433AM 13803 885 STL - FLT 7372 - GEAR WOULD NOT RETRACT WHEN SELECTED UP. RESET LANDING GEAR CONTROL RELEASE VALVE. (M) 2 L 7 2 4T RT A56EU 1998043000112 19980430 00112 EU 1998 4 30 RAIA980124 1 19980122 A 2612 3039870 FIRE LOOP AEROSP ATR72 ATR72202 8680940 EU NR 2 ENGINE FAILED A RAIA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 CE 03 721TE 11516 217 PIA - FLT 7130 - NR 2 ENGINE FIRE WARNING ON APPROACH. DISCHARGED FIRE EXTINGUISHERS. REMOVED AND REPLACED PIPE/LOOP A SSY. INSPECTION REVEALED NO EVIDENCE OF FIRE. (M) 2 H 7 2 4T RT A53EU 1998043000113 19980430 00113 EU 1998 4 30 RAIA980123 1 19980122 A 2932 MS287786 SEAL BAG JETSTM JETSTM3201 1500217 EU TRANSMITTER LEAKING A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 424AM 865 STL - FLT 7446 - HYDRAULIC PRESSURE DROPPED IN FLIGHT. REPLACE SEAL ON FITTING OF PRESSURE TRANSMITTER. (M) 2 L 7 2 4T RT A56EU 1998043000114 19980430 00114 EU 1998 4 30 RAIA980122 1 19980122 A 2424 51539002 GCU BAG JETSTM JETSTM3201 1500217 EU NR 1 FAILED A RAIA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CE 03 423AM 10048 858 STL - FLT 7203 - LEFT GENERATOR DROPPED OFF LINE. REPLACED GENERATOR CONTROL UNIT. (M) 2 L 7 2 4T RT A56EU 1998043000115 19980430 00115 WP 1998 4 30 CALA9800255 1 19980213 A 5210 BEAM DOUG DC9 DC981 3022081 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND A 1.25 INCH CRACK AT AFT END OF MAIN CABIN DOOR NR 7 BEAM AND A 1 INCH CRACK WAS LOCATED AT FORWARD END OF NR 7 BEAM. A 1 INCH CRACK WAS FOUND AT FORWARD END OF MAIN CABIN DOOR NR 8 BEAM. A .75 INCH CRACK WAS FOUND AT FOR WARD END OF MAIN CABIN DOOR NR 2 BEAM. THE BEAMS WERE REPAIRED IAW SRM 52-05, FIGURE 31 AND ECRA 5211-01022. 2 L 7 2 4F A6WE 1998043000116 19980430 00116 WP 1998 4 30 CALA9800256 1 19980213 A 5210 ANGLE DOUG DC9 DC981 3022081 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND A .125 INCH CRACK IN MAIN CABIN DOOR ANGLE AT BAYONET CUTOUT. REPAIRED IAW SRM 52-05, FIGURE 33. 2 L 7 2 4F A6WE 1998043000117 19980430 00117 WP 1998 4 30 CALA9800257 1 19980216 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 218-256 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND FUSELAGE SKIN DENTED AT FLOOR LEVEL AFT OF L-1 DOOR, STA 218 TO 256, LONGERON 18L. THE SKIN WAS REPAIR ED IAW ECRA 5330-01204. 2 L 7 2 4F A6WE 1998043000118 19980430 00118 WP 1998 4 30 CALA9800258 1 19980211 A 5347 TRACK DOUG DC10 DC1030 3023501 WP BS 1841 HOLE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A HOLE ON FLOOR TRACK IN AFT CARGO BILGE AREA AT STA 1841, RBL 25. A NEW SPLICE ANGLE AND STRAP WERE F ABRICATED AND INSTALLED IAW MF MAN D10-53-86784. 2 L 7 3 4F A22WE 1998043000119 19980430 00119 WP 1998 4 30 CALA9800259 1 19980211 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1275 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A 1 INCH CRACK ON FLOORBEAM UNDER LOWER JAMB OF R-3 DOOR AT STA 1275. A REPAIR WAS FABRICATED AND INST ALLED IAW ECRA 5320-01500. 2 L 7 3 4F A22WE 1998043000120 19980430 00120 WP 1998 4 30 CALA9800260 1 19980215 A 5754 RIVETS DOUG DC10 DC1030 3023501 WP NR 1 LE FLAP SHEARED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A ROW OF SHEARED RIVETS AND A BROKEN BRACKET ON LT WING NR 1 LEADING EDGE SLAT LOWER EDGE INBOARD SKIN SURFACE. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998043000121 19980430 00121 WP 1998 4 30 CALA9800261 1 19980215 A 5512 ALC7270502 PANEL DOUG DC10 DC1030 3023501 WP RT HORZ STAB DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 THE RT HORIZONTAL STABILIZER LEADING EDGE PANEL SUSTAINED DAMAGE ON FOUR CORNERS WHEN IT WAS DROPPED DURING REMOVAL. TH E PANEL WAS REPAIRED IAW SRM 55-12-01 AND ECRA 5510-01390. 2 L 7 3 4F A22WE 1998043000122 19980430 00122 WP 1998 4 30 CALA9800262 1 19980214 A 5530 FITTING DOUG DC10 DC1030 3023501 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A 0.160 INCH CRACK ON VERTICAL STABILIZER NR 4 BANJO FITTING. A REPAIR WAS PERFORMED IAW SRM 55-20-00, FIGURE2, PAGE 28-29 AND 55-20-00, FIGURE 7, PAGE 40. 2 L 7 3 4F A22WE 1998043000123 19980430 00123 WP 1998 4 30 CALA9800263 1 19980215 A 7830 TR PANEL DOUG DC10 DC1030 3023501 WP NR 2 ENGINE DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13088 46850 INSPECTION FOUND A 10 INCH AREA OF DELAMINATION AT NR 2 ENGINE LEFT THRUST REVERSER LOWER SIDEWALL PANEL (FAN AIR BYPASS AREA). THE C-DUCT ASSEMBLY WAS REPLACED IAW MM 78-32-11. 2 L 7 3 4F A22WE 1998043000124 19980430 00124 NM 1998 4 30 CALA9800264 1 19980213 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 400 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 21363 INSPECTION FOUND FLOORBEAM CORRODED AT STA 400, RBL 0 TO 25. A FLOORBEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53 -10-08, FIGURE 3. 2 L 7 3 4F A3WE 1998043000125 19980430 00125 NM 1998 4 30 CALA9800265 1 19980214 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79754 21363 INSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 0 TO 65. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-08, FI GURE 3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998043000126 19980430 00126 WP 1998 4 30 CALA9800266 1 19980216 A 5311 BELTFRAME DOUG DC9 DC981 3022081 WP BS 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 37882 48027 INSPECTION FOUND BELTFRAME CORRODED ACROSS BOTTOM ON FRONT CENTER AND LOWER CHANNEL AT STA 1322 FROM LONGERON 28L TO 28R . A REPAIR WAS INSTALLED IAW SRM 53-03. 2 L 7 2 4F A6WE 1998043000127 19980430 00127 WP 1998 4 30 CALA9800267 1 19980216 A 5320 JAMB DOUG DC10 DC1030 3023501 WP AC DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12061 47851 INSPECTION FOUND TWO, 2 INCH CRACKS AT UPPER SIDE OF FORWARD VERTICAL DOOR JAMB OF LT FORWARD AIR CONDITIONING COMPARTME NT. ONE AREA WAS TRIMMED AND BLENDED OUT. THE OTHER AREA WAS REWORKED AND REINFORCED WITH A DOUBLER IAW SRM 53-30-00, FIGURE 4. NEW RIVETS WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998043000128 19980430 00128 EU 1998 4 30 98FDEA00110 1 19980217 A 2840 2NSN04333 PRESS SWITCH AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 1 POSITION FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 650FE 726 FUEL PRESSURE LIGHT ILLUMINATED ON CLIMBOUT. NR 1 FUEL FILTER CLOGGED LIGHT ON. FOUND FUEL FILTER OK. FOUND PRESSURE DIFFERENTIAL SWITCH BAD. REMOVED AND REPLACED SWITCH, OPS NORMAL PER AML 73-34-11. ENGINE LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT A35EU E13NE 1998043000144 19980430 00144 WP 1998 4 30 MWEA98159 1 19980216 A 5754 5910437 PANEL DOUG DC9 DC932 3022066 WP LT LE FLAP CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT HAND WING SLAT ACCESS PANEL NR 1136A FOUND PITTING CORROSION ON THE OUTER SURFACE. REPAIRED IAW SRM 57-01 FIG 3. 2 L 7 2 4F A6WE 1998043000145 19980430 00145 WP 1998 4 30 MWEA98160 1 19980216 A 5311 2777930 FRAME DOUG DC9 DC932 3022066 WP BS 389 MISREPAIRED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 PREVIOUS REPAIR WAS ON AT FS STA 389 BETWEEN LONGERON 28L AND 29R NOT IAW SRM. FABRICATED REPAIR FILLER AND DOUBLERS IA W SRM 53-03 FIG 2A. 2 L 7 2 4F A6WE 1998043000146 19980430 00146 WP 1998 4 30 MWEA98161 1 19980216 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 511 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 INTERCOSTAL AT BS 511 FOUND HOLE AND TOOLING MARKS. FABRICATED REPAIR ANGLES IAW 53-01. 2 L 7 2 4F A6WE 1998043000147 19980430 00147 WP 1998 4 30 MWEA98162 1 19980216 A 5311 5910668 FRAME DOUG DC9 DC932 3022066 WP BS 370 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FRAME AT FS 370 WAS FOUND TO HAVE A TOOLING MARK IN THE UPPER RADIUS BETWEEN LONGERON 29L AND 30. FABRICATED REPAIR ANG LE IAW SRM 53-01 FIG 1 AND FIG 2. 2 L 7 2 4F A6WE 1998043000148 19980430 00148 WP 1998 4 30 MWEA98163 1 19980216 A 5320 3913291 SPLICE DOUG DC9 DC932 3022066 WP BS 813-823 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 SPLICE FITTING ON LONGERON 28L BETWEEN FS 813 AND 832 WAS FOUND CRACKED. FABRICATED REPLACEMENT SPLICE PER PRINT 391329 1. 2 L 7 2 4F A6WE 1998043000149 19980430 00149 WP 1998 4 30 MWEA98164 1 19980216 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 945-965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON SPLICE AT LONGERON 30 BETWEEN FS 945 AND 965 WAS FOUND CRACKED. FABRICATED REPAIR SPLICE IAW PRINT 3913291. 2 L 7 2 4F A6WE 1998043000150 19980430 00150 WP 1998 4 30 MWEA98165 1 19980216 A 5313 5914468 LONGERON DOUG DC9 DC932 3022066 WP BS 1087-1121 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LONGERON 25 LEFT WAS FOUND CRACKED FROM FS 1087 TO 1121. FABRICATED REPLACEMENT SECTION PER PRINT NR 5914468. 2 L 7 2 4F A6WE 1998043000151 19980430 00151 WP 1998 4 30 MWEA98166 1 19980216 A 5400 49198642 BRACKET DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORNER BRACKET JUST FORWARD OF THE NR 2 PYLON AFT UPPER SPAR STRAP WAS FOUND CRACKED. INSTALLED REPLACEMENT PART IAW SR M 51-30. 2 L 7 2 4F A6WE 1998043000152 19980430 00152 NM 1998 4 30 DL72L980376 1 19980211 A 5313 65564414 STRINGER BOEING 727 727232 1384082 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 STRINGER 29R WAS FOUND CORRODED NEAR FS 950E+10. THE STRINGER WAS CUT AT FS 950D+10 AND THE AFT SECTION REMOVED. A NEW SECTION OF STRINGER WAS SPLICED IN PER ER/A 363710-14, REV B. 2 L 7 3 4F A3WE 1998043000153 19980430 00153 NM 1998 4 30 DL733980378 1 19980213 A 3350 BATTERY PACK BOEING 737 737347 1384647 NM GALLEY DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 312WA 23598 ON PREFLIGHT FOUND LAST SECTION OF EMERGENCY TRACK LIGHTING INOP. FOUND BATTERY PACK BAD AND WIRE SHORTED ABOVE AFT GAL LEY. REPLACED PACK AND SECTION OF WIRE CHECKS GOOD. ALSO, REPLACED BATTERY. 2 L 7 2 4F RT A16WE 1998043000154 19980430 00154 NM 1998 4 30 DL72L980379 1 19980211 A 5320 655612910 SILL BOEING 727 727232 1384082 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 THE OUTBOARD CAP (EXTRUDED TEE) OF THE C2 DOOR SURROUND LOWER SILL WAS FOUND BADLY CORRODED ON THE OUTBD FLANGE. THE FL ANGE WAS CUT AWAY TO REMOVE THE CORROSION. THE CUT FLANGE WAS REPAIRED WITH A SHEET METAL ANGLE REPAIR PER ER/A 363872- 14, REV A. 2 L 7 3 4F A3WE 1998043000155 19980430 00155 NM 1998 4 30 DL767980380 1 19980210 A 5330 146T35311 SKIN BOEING 767 767232 1385132 NM BS 1351 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 108DL 22220 THE FUSELAGE SKIN WAS BADLY DENTED AT FS 1351 NEAR STRINGER 31R (JUST AFT OF THE C2 DOOR CUTOUT). THE UNDERLYING FRAME WAS ALSO DENTED. THE DAMAGED FRAME WAS REPAIRED PER THE B767 SRM 71-70-11. THE DENTED SKIN WAS CUTOUT AND REPAIRED WIT H AN ALUMINUM DOUBLER AND TRIPLER PER ER/A 363959-14, REV A. 2 L 7 2 4F RT A1NM 1998043000156 19980430 00156 NM 1998 4 30 DL72S980381 1 19980213 A 5720 SUPPORT BEAM BOEING 727 727232 1384082 NM LT MLG CHAFFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 FOUND DURING F-1 LETTER CHECK, MLG SIDE BRACE NUT CHAFING MLG SUPPORT BEAM. REPAIRED PER M/M 57-43-0. 2 L 7 3 4F A3WE 1998043000157 19980430 00157 NM 1998 4 30 DL72S980382 1 19980210 A 3350 20131A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 416DA 21258 ON S/C, FOUND AFT SECTION OF EMERGENCY ESCAPE LIGHTS INOP. REPLACED BATTER, OPS NORMAL. 2 L 7 3 4F A3WE 1998043000158 19980430 00158 NM 1998 4 30 DL73K980385 1 19980214 A 2910 651782119 PRESS PACK BOEING 737 737232 1384475 NM LT MLG WW MALFUNCTIONED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 305DL 3174 23077 LOST PRESSURE ON BOTH A-SYS HYD PUMPS, HYD QTY NML. MTC HAS FOUND NO FLUID LOSS. MOTORED ENG'S AT GATE HAD PRESSURE. C KD CASE DRAIN AND PRESS FILTERS, NO CONTAMINATION FOUND. REPLACED A-SYS HYD PRESS PACKAGE AND CASE DRAIN FILTERS, RAN B OTH ENG'S AND EXERCISED ALL FLIGHT CONTROLS. ALL PRESSURES WERE NORMAL. 2 L 7 2 4F RT A16WE 1998043000159 19980430 00159 NM 1998 4 30 DL72W980387 1 19980214 A 3350 BATTERY PACK 900835A BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2820W A9738 21058 ON L/O, CHECK FOUND LT FIXED OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OF LT FIXED OVERWING EMERGENCY. 2 L 7 3 4F A3WE 1998043000160 19980430 00160 NM 1998 4 30 DL72W980390 1 19980215 A 3350 LIGHT 1001141 BOEING 727 727247 138408F NM AFT STAIRWAY INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 291WA 8966 22109 AFT STAIRWAY EMER EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS NML. 2 L 7 3 4F A3WE 1998043000161 19980430 00161 WP 1998 4 30 DLL14980391 1 19980215 A 2710 ACTUATOR 21770001DLM LKHEED 1011 1011385115 5265015 WP LT AILERON BROKEN A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 740DA 1603 193C1244 HYD SYS-A FLUID LEVEL DROPPED TO 1/4 DURING CRUISE FLT. UNLATCHED ENG PUMP S/O SWITCH FOR HYD SYS-A AND FLUID LOSS STOP PED. FOUND LT OUTBD ACTUATOR OF INBD AILERON BROKEN AND HYD LINE AT ACT BROKEN. REPLACED SAME PER MM, ALL CKS OK. CKD A-PUMP HYD FILTERS FOR METAL, ALL OK. 2 L 7 3 4F A23WE 1998043000162 19980430 00162 NM 1998 4 30 VNAA9802013 1 19980216 A 2730 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE STICK PUSHER DIRTY A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 436JS 3052 DURING THE TAKEOFF ROLL, A STICK PUSHER FAIL WARNING MESSAGE OCCURED. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNE D TO THE GATE. MAINTENANCE CLEANED AND INSPECTED THE STICK PUSHER CANNON PLUG AND PERFORMED OPERATIONAL CHECKS IN ACCO RDANCE WITH DORNIER MAINTENANCE MANUAL 27-33-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998043000163 19980430 00163 WP 1998 4 30 CKSA98013 1 19980106 A 3260 SWITCH DOUG DC8 DC855 3021927 WP RT MLG DOWNLOCK FAILED A CKSA K NONE N FALSE WARNING CR CRUISE 1 GL 23 801CK 45816 THIRTY MINS AFTER T/O, RIGHT LANDING GEAR LIGHT ILLUMINATED (GOOD UPLATCH CHECK PRIOR TO THIS). FOUND PUSH PIN AT RIGHT GEAR DOWN AND LOCK SWITCH. REPAIRED AND SYSTEM OPS CHECKS GOOD IAW MM CHAPTER 32-7-0. 2 L 7 4 4F 4A25 1998043000164 19980430 00164 WP 1998 4 30 CKSA98014 1 19980130 A 3350 516574 POWER PACK LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 109CK 193N1205 L-4 DOOR EMERGENCY EXIT LIGHT INOP. ASSIGNED DMI NR 128030 IAW AIA MEL 33-51-02-1 ALL SPECIAL PROCEDURES COMPLIED WITH. REMOVED AND REPLACED L-4 POWER PACK. OPS CHECK GOOD IAW 33-60. THIS CLEARS DMI NR 128030. 2 L 7 3 4F A23WE 1998043000165 19980430 00165 WP 1998 4 30 VJ9800014 1 19980130 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 69.5 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 THREE FASTENER HOLES HAVE CRACKS EMANATING FROM THEM AT FUSELAGE STATION 69.5 LBL 16.0 (TWO CRACKS), 17.10 (2 CRACKS) AN D 18.0 (1 CRACK). ACCESSED AREA FOR REPAIR IAW DC9 MM. REPAIRED AREA IAW REQUIREMENTS CONTAINED IN AD 96-11-11 AND EO 12-5330-29-B1048. REINSTALLED ACCESS ITEMS IAW DC9 MM AND DPS 3.40-1. LEAK CHECKS GOOD IAW DC9 MM 34-10-0 PG 209. REF NR 027VI-0005/112778. 2 L 7 2 4F A6WE 1998043000166 19980430 00166 WP 1998 4 30 VJ9800015 1 19980131 A 5320 SUB FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 922VV 47274 REPAIR ON SUB-FLOOR PLATE CORRODED AT STA Y200, X54. CUT OUT CORRODED AREA, FABRICATED REPAIR DOUBLER, DRILLED, TREATED AND INSTALLED IAW DC9 SRM 51-10-3, 51-10-4 AND EO 98-773. REFERENCE NR 0271X1-0351/113687. 2 L 7 2 4F A6WE 1998043000167 19980430 00167 EU 1998 4 30 MAL975972 1 19980212 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 112XJ 340A112 DURING INSPECTION, EMERGENCY LIGHT AT ROW 2 AND 3 INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998043000168 19980430 00168 EU 1998 4 30 MALA975971 1 19980212 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING INSPECTION, SEAT 6A OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998043000169 19980430 00169 EU 1998 4 30 MALA975973 1 19980211 A 3240 5010488 TIRE SAAB SF340 340B 7860101 EU RT MLG INTERNAL FAULT A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 429XJ 429 ON LANDING ROLL OUT, THE TOWER INDICATED SMOKE OR SIGNS OF HOT BRAKE ON RIGHT SIDE. ALSO, LOSS OF TOTAL BRAKE EFFECTIVE NESS AND ANTI-SKID WARNING. MAINTENANCE REPLACED RIGHT TIRES AND INSPECTED BRAKES. HIGH SPEED TAXI CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998043000170 19980430 00170 EU 1998 4 30 MALA975974 1 19980214 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 592MA 340B199 DURING INSPECTION, EMERGENCY LIGHT ROW 3CD INOP. MAINTENANCE RESECURED PANEL, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998043000171 19980430 00171 EU 1998 4 30 MALA975975 1 19980216 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 435XJ 435 DURING INSPECTION, EMERGENCY EXIT SIGN ABOVE FLIGHT ATTENDANT INOP. MAINTENANCE RESECURED CANNON PLUG, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998043000172 19980430 00172 EU 1998 4 30 MALA975976 1 19980205 A 3260 CONNECTOR SAAB SF340 SF340A 7850100 EU RT WOW SW CONTAMINATED A MALA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 GL 15 68XJ 068 ON APPROACH, WHEN GEAR SELECTED DOWN, THREE GREEN ANTI-SKID CAUTION LIGHTS ILLUMINATED. AIRCRAFT WAS DIVERTED TO DTW. M AINTENANCE FOUND OIL RESIDUE IN RIGHT INBOARD WOW HARNESS CONNECTOR IN GEARWELL, CLEANED CANNON PLUG. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998043000173 19980430 00173 NM 1998 4 30 MALA975977 1 19980208 A 2750 745583A CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM RT TE FLAP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 846MA 344 AFTER DEPARTURE, FLAP DRIVE FAULT LIGHT ILLUMINATED AND FLAPS STUCK A 5 DEGREES. AIRCRAFT DIVERTED TO MSP. MAINTENANCE REPLACED THE RIGHT SECONDARY FLAP DRIVE CABLES AND NR 1 STANDBY HYDRAULIC PUMP (P/N 731840), (S/N MX-519012). ALL CHEC KS GOOD. 2 H 7 2 4T RT A13NM 1998043000174 19980430 00174 NM 1998 4 30 MALA975978 1 19980214 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 831MA 339 DURING INSPECTION, EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998043000175 19980430 00175 EU 1998 4 30 MALA975979 1 19980211 A 3241 39647 CONTROL VALVE SAAB SF340 SF340A 7850100 EU ANTI-SKID SYST FAILED A MALA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 GL 15 68XJ 068 ON APPROACH, ANTI-SKID LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE ANTI-SKID CONTROL VALVE A ND CONTROL BOX (P/N 42-683-3), (S/N 566). ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998043000176 19980430 00176 NM 1998 4 30 MALA975980 1 19980212 A 3350 LP010 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 826MA 330 DURING INSPECTION, EMERGENCY EXIT LIGHT INOP AT FORWARD EMERGENCY DOOR EXIT. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998043000177 19980430 00177 EU 1998 4 30 MALA975981 1 19980212 A 7603 SOLENOID SAAB SF340 SF340A 7850100 EU FLIGHT IDLE SYST LACK OF LUBE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 98XJ 098 AFTER TAKEOFF, FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE COMPLETED OPS CHECK OF F LIGHT IDLE STOP SOLENOID, LUBRICATED SOLENOID. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998043000178 19980430 00178 WP 1998 4 30 9802721148 1 19980214 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 148US 46757 DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM DOOR 2 TO DOOR 3. REPLACED POWER SUPPLY AND BATT ERY, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998043000179 19980430 00179 NM 1998 4 30 9802736642 1 19980213 A 7603 COUPLING SCREW BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE BROKEN A A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 642NW 21942 702134 AT START OF TAKEOFF ROLL, THE NR 4 ENGINE DID NOT ACCELERATE OR RESPOND TO POWER LEVER INPUTS. THE TAKEOFF WAS ABORTED AND RETURNED TO THE GATE. MAINTENANCE FOUND A BROKEN COUPLING SCREW IN THE STRUT AREA. REPLACED THE SCREW AND A FUNCTI ONAL TEST OF THE THRUST LEVER SYSTEM PER MM 76-11-06 WAS NORMAL. 2 L 7 4 4F 4 F A20WE E3NE 1998043000180 19980430 00180 NE 1998 4 30 9802742293 2 19980214 A 7200 ENGINE BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE LEFT FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 01 293US 21504 700540 DURING CRUISE, THE LEFT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. CREW SHUT DOWN THE LEFT ENGINE, DIVERTED TO MEM, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998043000181 19980430 00181 EU 1998 4 30 9802753213 1 19980209 A 2120 VFT300A1AMDTA SKIN VALVE AIRBUS 320 A320211 3930320 EU E/E COMPT INOPERATIVE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 313US 13428 135 153 FOLLOWING TAKEOFF, CREW UNABLE TO PRESSURIZE THE AIRCRAFT. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE RE PLACED THE AVIONICS EQUIPMENT COOLING SKIN AIR OUTLET VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998043000182 19980430 00182 WP 1998 4 30 9802769882 1 19980216 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST NR NOT REPORTED 1 GL 01 670MC 47659 FLIGHT ATTENDANT REPORTED, THE AFT MOUNTED EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY, OPERATIO NAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043000183 19980430 00183 WP 1998 4 30 9802779885 1 19980216 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 401EA 47682 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS AT SEAT ROWS 16 THRU 19 INOPERATIVE IN THE CEILING AREA. MAINTENANCE REP LACED POWER SUPPLY B5-26, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043000184 19980430 00184 WP 1998 4 30 9802789868 1 19980216 A 3350 FUSE DOUG DC9 DC951 3022051 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE CHECK, FOUND RIGHT AND LEFT SIDE OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED FUSE, OPE RATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043000185 19980430 00185 NM 1998 4 30 UPS98225766 1 19980216 A 5744 FITTING BOEING 727 72722C 138400F NM WS 224.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, EXCESSIVE CORROSION ON NR 4 FLAP TRACK, WING ATTACH FITTING. BUSHING MANUFACTURED AND THEN INSTALLED PER OHM 57-40-01. FITTING THEN REINSTALLED PER OHM 20-50-01. 2 L 7 3 4F A3WE 1998043000186 19980430 00186 NM 1998 4 30 UPS98225767 1 19980216 A 5744 FITTING BOEING 727 72722C 138400F NM WS 224.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, EXCESSIVE CORROSION ON NR 5 FLAP TRACK ON WING ATTACH FITTING. BUSHING MANUFACTURED AND THEN INSTALL ED PER OHM 57-40-01. FITTING THEN REINSTALLED PER OHM 20-50-01. 2 L 7 3 4F A3WE 1998043000187 19980430 00187 NM 1998 4 30 UPS98225768 1 19980216 A 3211 651620610 FITTING BOEING 727 72722C 138400F NM RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, RIGHT HAND MLG FWD TRUNNION BEARING SUPPORT FITTING HAS CORROSION ON INNER AND OUTER LUGS THAT CONTAC T REAR SPAR FITTING BEARING. SUPPORT FITTING REPLACED IAW MM 32-11-51. 2 L 7 3 4F A3WE 1998043000188 19980430 00188 NM 1998 4 30 UPS98225771 1 19980216 A 3211 65192961 FITTING BOEING 727 72722C 138400F NM LT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION ON LEFT HAND FWD TRUNNION BEARING SUPPORT ATTACH FITTING ON REAR SPAR. BEARING SUPPORT FIT TING REPLACED IAW DRAWING 65-19297. 2 L 7 3 4F A3WE 1998043000189 19980430 00189 NM 1998 4 30 UPS98225772 1 19980216 A 3211 69192962 FITTING BOEING 727 72722C 138400F NM RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, FITTING IN REAR SPAR OF RIGHT HAND WING FOR ATTACHING RT MLG FWD TRUNNION BEARING SUPPORT HAS EVIDENC E OF CORROSION. BEARING SUPPORT FITTING ATTACH FITTING REPLACED PER DRAWING 65-19297. 2 L 7 3 4F A3WE 1998043000190 19980430 00190 NM 1998 4 30 UPS98225773 1 19980216 A 3221 TRUNNION FITTING BOEING 727 72722C 138400F NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION ON TRUNNION FITTING ON RIGHT HAND SIDE FOR NOSE LANDING GEAR. CORROSION REMOVED AND AREA R EPROTECTED PER SRM 53-40-1 FIG 2. 2 L 7 3 4F A3WE 1998043000191 19980430 00191 NM 1998 4 30 UPS98225775 1 19980216 A 3221 FITTING BOEING 727 72722C 138400F NM NLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-C, CORROSION ON LEFT HAND TRUNNION FITTING FOR NOSE LANDING GEAR. CORROSION REMOVED AND AREA REPROTECTE D PER SRM 53-40-1 FIG 2. 2 L 7 3 4F A3WE 1998043000192 19980430 00192 NM 1998 4 30 UPS98225780 1 19980216 A 5713 STRINGER BOEING 727 72751C 1384015 NM WS 629 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, WHILE WORKING NRC 465706 WINGS 329, FOUND STRINGER 14 TAB TO BE CRACKED AT R/W STA 629.0. REPAIRED STR 14 AT RWS 629.0 IAW UPS EO B727-5710-0314F. 2 L 7 3 4F A3WE 1998043000193 19980430 00193 NM 1998 4 30 UPS98225781 1 19980216 A 5712 RIB BOEING 727 72751C 1384015 NM WS 629 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI ,RWS 629 RIB IS CRACKED IN RADIUS AT S-11 LOWER ATTACH BOLT HOLE. REPAIRED 629 RIB (RWS) IAW UPS EO B727-5710-1325H. 2 L 7 3 4F A3WE 1998043000194 19980430 00194 NM 1998 4 30 UPS98225782 1 19980216 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION BS 680 FRAME LBL 24 WL 154 UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLER PER SRM 51-40-3, HEAT TREATED AND THEN INSTALLED PER SRM 51-20-04 SRM 53-10-2 AND SRM 51-40-3. 2 L 7 3 4F A3WE 1998043000195 19980430 00195 NM 1998 4 30 UPS98225783 1 19980203 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 370-380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION ON STR 26 LT BS 370 TO 380. REMOVED DAMAGED SECTION, INSTALLED NEW STRINGER AND STRINGER SPLICE PER SRM 53-10-3 WITH FASTENER BS 360 TO 380. 2 L 7 3 4F A3WE 1998043000196 19980430 00196 NM 1998 4 30 UPS98225784 1 19980203 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 251 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION AROUND FASTENERS ON FRAME BS 251 RBL 24 WL 162. REMOVED DAMAGED SECTION AND INSTALLED FIL LER AND DOUBLER IAW SRM 51-10-2, 51-40-2 AND MM 51-20-15. 2 L 7 3 4F A3WE 1998043000197 19980430 00197 NM 1998 4 30 UPS98225785 1 19980216 A 5320 65189553 FITTING BOEING 727 72751C 1384015 NM BS 365 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STRINGER TIE OF STR 26 LT BS 365. REMOVED AND REPLACED STRINGER TIE IAW SRM 51-30-2, 53-10-1, 51-30-4. 2 L 7 3 4F A3WE 1998043000198 19980430 00198 NM 1998 4 30 UPS98225786 1 19980216 A 5320 WEB BOEING 727 72751C 1384015 NM BS 307-314 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION ON VERTICAL WEB OF DOGHOUSE BS 307 TO 314, LBL 13.5, WL 157 TO 161. CUT OUT DAMAGED AREA OF WEB AND INSTALLED DOUBLER IAW SRM 53-10-9, 51-40-2. 2 L 7 3 4F A3WE 1998043000199 19980430 00199 NM 1998 4 30 UPS98225787 1 19980203 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 329 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON FRAME BS 328, RBL 43, WL 169 (AREA MARKED). CORROSION FOUND TO BE O UT OF LIMITS PER SRM 53-10-1, INSTALLED STANDARD FRAME DOUBLER REPAIR IAW SRM 51-40-3, AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998043000200 19980430 00200 NM 1998 4 30 UPS98225789 1 19980203 A 5347 BAC15201430 SEAT TRACK BOEING 727 72751C 1384015 NM BS 1010-1110 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 904UP 18946 INSPECTION TYPE-SI, CORROSION (44-53-12) IN SEAT TRACK WELL AND AROUND NUT PLATES BS 1010 TO 1110, RBL 62, WL 208. CORR OSION FOUND OUT OF LIMITS PER SRM 51-30-2, REPLACED SEAT TRACK WITH NEW ITEM PER SRM 51-30-2, SRM 51-10-2 AND SRM 51-20- 151. 2 L 7 3 4F A3WE 1998043000201 19980430 00201 WP 1998 4 30 UPS98825778 1 19980205 A 5320 37508342N FITTING DOUG DC8 DC873F 302199F WP BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-C, FWD ACC COMP FS 640 - THE KEEL BEAM TIE FITTING TO BULKHEAD FRAME IS CRACKED (TOP/INSIDE) AND BOTTOM. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000202 19980430 00202 WP 1998 4 30 UPS98825779 1 19980205 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-C, FWD ACC COMP AT FS 660 - KEEL BEAM TIE FITTING TO STRINGER 35R IS CRACKED IN UPPER RADIUS. REMOVED A ND REPLACED FITTING IAW SRM 51-3-1 AND 53-1-0. 2 L 7 4 4F RT 4A25 1998043000203 19980430 00203 WP 1998 4 30 UPS98825788 1 19980211 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, FS 440 TO 460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000204 19980430 00204 WP 1998 4 30 UPS98825790 1 19980211 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, FS 440 TO 460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1998043000205 19980430 00205 WP 1998 4 30 UPS98825791 1 19980209 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 572.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998043000206 19980430 00206 WP 1998 4 30 UPS98825792 1 19980209 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 600-620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, NR 1 PIT AT STA 600 TO 620 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1998043000207 19980430 00207 WP 1998 4 30 UPS98825793 1 19980211 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 274 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LONGERON END FITTING AT FS 274 STR 31R HAS HEAVY CORROSION AROUND FASTENERS. REMOVED AND REPLACED FI TTING IAW SRM 51-1-210D. 2 L 7 4 4F RT 4A25 1998043000208 19980430 00208 WP 1998 4 30 UPS98825795 1 19980209 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 35-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, HEAVY CORROSION BETWEEN INTERNAL DOUBLER AND SKIN AT LONGERON 31R AND BETWEEN FS 35 AND 55. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 53-3-1 AND 51-1-21. 2 L 7 4 4F RT 4A25 1998043000209 19980430 00209 WP 1998 4 30 UPS98825796 1 19980211 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 600-620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, FS 600 TO 620 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000210 19980430 00210 WP 1998 4 30 UPS98825797 1 19980209 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT STA XFS 635.000. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998043000211 19980430 00211 WP 1998 4 30 UPS98825798 1 19980209 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 822.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FSTR STA XFS 822.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998043000212 19980430 00212 WP 1998 4 30 UPS98825799 1 19980210 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 678.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, RT WING L/E AT STA XFS 678.750 - THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2- 0. 2 L 7 4 4F RT 4A25 1998043000213 19980430 00213 NM 1998 4 30 QXEA9800066 1 19980213 A 3260 INDICATION DHAV DHC8 DHC8102 2809003 NM LANDING GEAR MALFUNCTIONED A QXEA O OTHER N FALSE WARNING LD LANDING 1 NM 09 830PH 314 ATTEMPTED NORMAL GEAR EXTENSION GOT THREE RED LIGHTS ONLY. ATTEMPTED SECOND EXTENSION AND GOT SAME INDICATION. PERFORM ED ALTERNATE GEAR EXTENSION AND GOT THREE GREEN. LANDED NORMALLY. MAINTENANCE INSPECTED LANDING GEAR, NO DISCREPANCIES NOTED. PERFORMED INSPECTION OF PSEU AND RACK, NO DISCREPANCIES NOTED. PERFORMED BITE TEST, NO DISCREPANCIES NOTED. A IRCRAFT WAS TEST FLOWN, TEST FLIGHT SATISFACTORY. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998043000214 19980430 00214 EU 1998 4 30 QXEA9800067 1 19980213 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 EXIT SIGN ABOVE COCKPIT DOOR HAS ALL LIGHTS INOP. MAINTENANCE RELAMPED WITH 28 VOLT BULBS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998043000215 19980430 00215 EU 1998 4 30 QXEA9800068 1 19980213 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 FORWARD EMERGENCY EXIT SIGN HAS INOP BULBS. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998043000216 19980430 00216 EU 1998 4 30 QXEA9800070 1 19980214 A 3350 551590004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTION A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 OVERHEAD EMERGENCY EXIT SIGN ROW 8 IS ONLY PARTIALLY ILLUMINATED. MAINTENANCE REPLACED CIRCUIT BOARD, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998043000217 19980430 00217 EU 1998 4 30 QXEA9800071 1 19980216 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 EXIT LIGHT OUT AT SEAT 8A. MAINTENANCE RELAMPED EXIT SIGN AT SEAT 8A, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998043000218 19980430 00218 NM 1998 4 30 98FDEA00111 1 19980218 A 5311 BELLFRAME BOEING 727 727227 1384078 NM BS 660 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 BS 660L, STR 23L, 22L, 24L AND 25L IS DENTED (BELLFRAME) AND HOLES DRILLED IN RADIUS. REMOVED DAMAGED AREA AND INSTALLE D DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998043000219 19980430 00219 NM 1998 4 30 98FDEA00112 1 19980218 A 5311 BELLFRAME BOEING 727 727227 1384078 NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 BS 520L BETWEEN STR 22 TO 25L BELL FRAME DENTED SEVERAL PLACES. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-4 0-3. 2 L 7 3 4F A3WE 1998043000220 19980430 00220 NM 1998 4 30 98FDEA00113 1 19980217 A 5311 FRAME BOEING 727 727227 1384078 NM BS 930 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 INSPECTED FRAME AT BS 930, STR 14R, CRACK FOUND. INSTALLED DOUBLER AS PER EO 7-5310-7-4330. 2 L 7 3 4F A3WE 1998043000221 19980430 00221 NM 1998 4 30 98FDEA00114 1 19980217 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1148 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 477FE 21394 LWR FUSE SKIN BULGE BETWEEN STR 26R AND STR 25R, BS 1148R. REMOVED ALL CORROSION AND INSTALLED FRAME SHEAR TIE REPAIR A T SKIN ATTACHMENT PER SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 1998043000222 19980430 00222 NM 1998 4 30 98FDEA00115 1 19980218 A 5243 DOOR BOEING 727 72725C 138400H NM HYD SERVICE BLOWN OFF A FDEA K NONE O OTHER UK UNKNOWN 1 SO 25 133FE 19851 AIRCRAFT HYDRAULIC SERVICE ACCESS DOOR BLOWN OFF IN FLIGHT. CANNIBALIZED DOOR FROM AIRCRAFT 146 AND INSTALLED ON AIRCRA FT 133, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998043000223 19980430 00223 WP 1998 4 30 ABXA9800080 1 19980216 A 5320 59145581N DOUBLER DOUG DOUG DC9 DC931 3022065 WP AFT FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 945AX 47551 DURING C-CHECK, FOUND CORROSION AT THE AFT END OF THE PRESSURIZATION OUTFLOW VALVE SCOOP. REPLACED DOUBLER IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998043000224 19980430 00224 WP 1998 4 30 ABXA9800081 1 19980216 A 5312 591013013 BLKHD DOUBLER DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BULKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK COMPLIANCE WITH S/B 53-137, FOUND DOUBLER CRACKED RADIALLY IN UPPER RIGHT AND UPPER LEFT CORNERS. REPAIR ED DOUBLER IAW ABX REA D953-22492-MR AND DC9 S/B 53-137. 2 L 7 2 4F A6WE 1998043000225 19980430 00225 WP 1998 4 30 ABXA9800082 1 19980216 A 5320 99101515 WEB DOUG DOUG DC9 DC931 3022065 WP BS 617-639 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND THE LEFT CUSP WEB CRACKED AT STA 617, 639 AND 658. REPLACED CUSP WEB IAW DC9 SRM 51-10-04. 2 L 7 2 4F A6WE 1998043000226 19980430 00226 WP 1998 4 30 ABXA9800083 1 19980216 A 5320 3916209501 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 DURING C-CHECK, FOUND FLOORBEAM VERTICAL SUPPORT FITTING AT STA 680 AND LBL 44 CRACKED. REPLACED FITTING IAW DC9 SRM 51 -10-4. 2 L 7 2 4F A6WE 1998043000227 19980430 00227 WP 1998 4 30 ABXA9800084 1 19980108 A 5320 561537275 DOUBLER DOUG DOUG DC8 DC861 3021952 WP BS 1350 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 FINGER DOUBLER CORRODED AND CRACKED BEYOND LIMITS AT STATION 1350 BETWEEN LONGERON 34R-34L. REPAIRED IAW DACO DWG 56153 72 AND SRM 51-1-21. 2 L 7 4 4F 4A25 1998043000228 19980430 00228 WP 1998 4 30 ABXA9800085 1 19980108 A 5320 5758571517 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1500 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 STA 1500 ABOVE STR 33L TRACK SUPPORT FITTING IS CRACKED HORIZONTALLY ON UPPER FLANGE. REPAIRED IAW SRM 51-1-20D. 2 L 7 4 4F 4A25 1998043000229 19980430 00229 WP 1998 4 30 ABXA9800086 1 19980201 A 5320 97537841 SUPPORT DOUG DOUG DC8 DC861 3021952 WP BS 70 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 FWD CARGO COMPARTMENT, STA 70 AT LONGERON 33R TO 35R, FLOOR SUPPORT ANGLE HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998043000230 19980430 00230 WP 1998 4 30 ABXA9800087 1 19980201 A 5347 4929147 SEAT TRACK DOUG DOUG DC8 DC861 3021952 WP BS 200 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 846AX 46158 MAIN CABIN SEAT TRACK CORRODED BEYOND LIMITS AT FS 200 LBL 25. REPAIRED IAW SRM 53-2-3. 2 L 7 4 4F 4A25 1998043000231 19980430 00231 WP 1998 4 30 ABXA9800088 1 19980216 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928AX 47392 EMERGENCY EXIT LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHTS BATTERIES. 2 L 7 2 4F A6WE 1998043000232 19980430 00232 NM 1998 4 30 P5CA9800230 1 19980213 A 5280 65B109571 HINGE BOEING 747 747132 1384882 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LT WING GEAR DOOR HINGE FWD POSITION FAILURE, FOUND AFTER BLOCK-IN. FOUND NO OTHER DAMAGE. REMOVED AND REPLACED FWD HI NGE PER MM 32-12-01. 2 L 7 4 4F A20WE 1998043000233 19980430 00233 NM 1998 4 30 P5CA9800231 1 19980213 A 5755 SKIN BOEING 747 747249F 1384849 NM NR 8 SPOILER DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 NR 8 SPOILER HAS DENTS IN UPPER SURFACE. CUTOUT DAMAGED AREA, APPLIED FILLER AND DOUBLER AND PAINTED AREA PER SRM 51-40 -06 AND 51-24-11. 2 L 7 4 4F A20WE 1998043000234 19980430 00234 NM 1998 4 30 P5CA9800232 1 19980211 A 5753 PANEL BOEING 747 747249F 1384849 NM LT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LT MIDFLAP COVE LIP PANEL INBD HAS CRACK. CLEANED/SMOOTHED DAMAGED AREA. STOP DRILLED CRACK, APPLIED FIBERGLASS OVERLA Y AND PAINTED PER SRM 51-40-15 AND 51-24-11. 2 L 7 4 4F A20WE 1998043000235 19980430 00235 NM 1998 4 30 P5CA9800233 1 19980212 A 5751 SKIN BOEING 747 747249F 1384849 NM LT AILERON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LT OUTBD LWR T/E AILERON HAS DAMAGE. REPAIRED AILERON T/E IAW MM 51-40-15. PAINTED REPAIRED AREA IAW MM 51-24-11. 2 L 7 4 4F A20WE 1998043000236 19980430 00236 NM 1998 4 30 P5CA9800235 1 19980211 A 5321 FLOOR PANELS BOEING 747 747249F 1384849 NM CABIN DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 MAIN CABIN FLOOR PANELS UNDER UPPER DECK ACCESS LADDER INBD LEG DAMAGED DUE TO LADDER RESTING ON THE PANEL. FABRICATED AND INSTALLED NEW FLOOR PANEL PER SRM 51-30-02 AND 51-0-01. 2 L 7 4 4F A20WE 1998043000237 19980430 00237 NM 1998 4 30 P5CA9800236 1 19980210 A 5320 JAMB BOEING 747 747249F 1384849 NM CORGO DOORWAY GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 FWD LOWER CARGO DOOR JAMB AFT LOWER SIDE LATCH PIN HOUSING IS GOUGED. BLENDED OUT GOUGE. NDT HFEC FOR CRACKS, NONE FOU ND. TREATED AND PRIMED PER SRM 53-40-01 AND 51-00-02. NDT MANUAL 51-00-00. 2 L 7 4 4F A20WE 1998043000238 19980430 00238 NM 1998 4 30 P5CA9800237 1 19980210 A 5246 PANEL BOEING 747 747249F 1384849 NM LAV SERVICE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 LAV SERVICE PANEL AREA HAS LIGHT CORROSION AND BARE METAL. REMOVED CORROSION, CLEANED, TREATED AND PRIMED PER SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F A20WE 1998043000239 19980430 00239 NM 1998 4 30 P5CA9800238 1 19980213 A 5751 SKIN BOEING 747 747249F 1384849 NM RT AILERON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 920FT 22237 RT OUTBD AILERON LOWER T/E HAS DAMAGE AT CONDUCTIVE STRIP. REMOVED DAMAGED SECTION OF CONDUCTIVE STRIP AND STATIC WICK. REPAIRED CONDUCTIVE STRIP, REPLACED WICK. OHM CHECKED PER MM 57-51-03 AND 23-61-00. 2 L 7 4 4F A20WE 1998043000240 19980430 00240 NM 1998 4 30 CKSA98015 1 19980213 A 5330 65921444 SKIN BOEING 727 727223 1384074 NM BS 950-1183 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 856AA 20997 ACCOMPLISHMENT OF AD 90-06-09. REPLACE AFT BELLY SKIN PANELS IAW S/B 727-53-0159. REMOVED AND REPLACED AFT BELLY SKIN PANELS IAW SB 727-53-0159 AND AD 90-06-09. REPAIR ORDER NUMBER 856-291. 2 L 7 3 4F A3WE 1998043000266 19980430 00266 NM 1998 4 30 98ZZZX778 1 19980121 A 3350 1000679 LIGHT BOEING 727 727222 1384073 NM CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 7640U 19913 DURING PRE-FLIGHT IN DAY, DISCOVERED EMERGENCY EXIT LIGHT ABOVE L-1 DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY EX IT LIGHT (L-1 DOOR). 2 L 7 3 4F A3WE 1998043000274 19980430 00274 EU 1998 4 30 98ZZZX786 2 19980112 A 7260 3353001030 GEARBOX BOEING 737 7374Q8 NM CFMINT CFM56 CFM563C1 13802 EU ENGINE FAILED A RIVA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 17 405KW 24704 726393 JFK/FLL - FLT 87 AT 21:00 IFSD - WHILE IN STABLE-STATE CRUISE, NR 1 ENGINE SHUT DOWN WITH NO ABNORMAL INDICATIONS. DIVE RTED TO ILM. NO RE-LIGHT WAS ATTEMPTED DUE TO NO N2 INDICATION. TROUBLESHOT ENGINE, FOUND BEARING HOUSING IN THE ACCES SORY DRIVE GEARBOX FOR THE HORIZONTAL DRIVE SHAFT FAILED, THE DRIVE SHAFT BACKED OUT. REPLACED ACCESSORY DRIVE GEARBOX (ADBG) AND THE TRANSFER GEARBOX (TGB). 2 L 7 2 4F 4 F RT A16WE E21EU 1998043000275 19980430 00275 EA 1998 4 30 VTZA98003 1 19980105 A 7714 CONNECTOR CNDAIR CL600 CL6002B16 1900305 EA NR 1 ENGINE DIRTY A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 621BR 7186 IAD/BNA - FLT 6704 - DURING CRUISE AT 1755 HRS ON 1-5-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 ENGINE N2 IND ICATION WENT TO ZERO. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED ALTERNATOR CANNON PLUG, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998043000276 19980430 00276 NM 1998 4 30 NOCA03/98 1 19980106 A 3350 767 LAMP BOEING 757 75728A 1384976 NM CABIN FAILED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 751NA 28164 EXTERIOR EMERGENCY LIGHT INOPERATIVE AT L4 DOOR. RELAMPED, CHECKED NORMAL ON TEST. (X) 2 L 7 2 4F RT A2NM 1998043000278 19980430 00278 NM 1998 4 30 98ZZZX787 1 19980103 A 5610 001A561A0000207 WINDOW DORNER DO32 DO328100 2996000 NM RT COCKPIT DELAMINATED A EQGA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 19 340PH 2413 596 3064 DFW/ASE - FLT 175 - APPROXIMATELY 10-15 MINUTES AFTER TAKEOFF FROM DFW, COPILOT'S SIDE WINDOW BEGAN TO DELAMINATE. CAPT AIN CONTACTED DISPATCH AND MAINTENANCE CONTROL AND WAS ADVISED TO RETURN TO DFW. AIRCRAFT WAS RETURNED TO DFW WITHOUT I NCIDENT. UPON INSPECTION, MAINTENANCE IDENTIFIED SMALL AREA OF DELAMINATION ON COPILOT'S SIDE WINDOW. DELAMINATION WAS DETERMINED TO BE WITHIN THE LIMITATIONS ESTABLISHED IN DORNIER MM 56-12-00. DELAMINATED WINDOW WAS ENTERED IN MAINTENA NCE CARRY OVER WITH DAILY INSPECTION AND AIRCRAFT RELEASED TO SERVICE. PART TOTAL CYCLES 2667. 2 H 7 2 4T RT A45NM 1998043000279 19980430 00279 WP 1998 4 30 DHL9880650C 1 19980102 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1699-1703 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FUSE STA 1700, NR 5 FLOOR TRACK DAMAGED. CUT OUT DAMAGED SECTION OF TRACK FROM 1699 TO 1703, FABRICATED REP AIR CHANNEL AND INSTALLED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000280 19980430 00280 WP 1998 4 30 DHL9880651C 1 19980123 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1530 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1530 LINE 5 FLOOR TRACK DAMAGED. REMOVED AND REPLACED DAMAGED TRACK PER SRM 53-21-2. 2 L 7 4 4F RT 4A25 1998043000281 19980430 00281 WP 1998 4 30 DHL9880652C 1 19980116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1300 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FUS SAT 1300 LINE NR 5 FLOOR TRACK CHIPPED. REMOVED AND INSTALLED 2 DAMAGED PLUG AT STA 1298 PER SRM 53-2-3 . 2 L 7 4 4F RT 4A25 1998043000282 19980430 00282 WP 1998 4 30 DHL9880653C 1 19980109 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 860 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, STA 860 LINE NR 5 FLOOR TRACK WORN. CUT OUT DAMAGED SECTION OF TRACK, INSTALLED SEAT TRACK AND SPLICE. REP AIRED PER SRM 53-2-3, 25 LONG. 2 L 7 4 4F RT 4A25 1998043000283 19980430 00283 WP 1998 4 30 DHL9880654C 1 19980102 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 150 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C CHECK, STA 150 LINE NR 5 FLOOR TRACK CHIPPED. CUT OUT DAMAGED SECTION AND INSTALLED PLUGS, SPLICES AND TRACK PER S RM 53-2-3, FS 145 TO 149 AND 153 TO 157. 2 L 7 4 4F RT 4A25 1998043000284 19980430 00284 WP 1998 4 30 DHL9880655C 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 330 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 330 LINE NR 5 FLOOR TRACK WORN. CUT OUT DAMAGED SECTION AND INSTALLED PLUG PER SRM 53-2-3, FS 335 TO 339 . 2 L 7 4 4F RT 4A25 1998043000285 19980430 00285 WP 1998 4 30 DHL9880656C 1 19980127 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 60 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 60 LINE NR 5 FLOOR TRACK CHIPPED. REMOVED FLOOR PLANK, CUT OUT DAMAGED SECTION AND INSTALLED REPAIR PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000286 19980430 00286 WP 1998 4 30 DHL9880657C 1 19980118 A 5753 DOOR DOUG DC8 DC873F 302199F WP LT TE FLAP BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FLAP, ICE BREAKER AT I/B OBSERVED BEND. REMOVED DAMAGED DOOR AND INSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998043000287 19980430 00287 WP 1998 4 30 DHL9880658C 1 19980116 A 5712 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING FILLET FAIRING RIB CRACKED. REMOVED DAMAGED RIB, FABRICATED REPAIR AND INSTALLED PER SRM 51-1-21, 1 X 1 X 9. 2 L 7 4 4F RT 4A25 1998043000288 19980430 00288 WP 1998 4 30 DHL9880659C 1 19980122 A 7110 STRIP DOUG DC8 DC873F 302199F WP NR 3 COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 3 ENGINE COWL RT AFT REVERSER RUB STRIP CRACKED. REMOVED AND REPLACED STRIP CFM MM 78-32-0. 2 L 7 4 4F RT 4A25 1998043000289 19980430 00289 WP 1998 4 30 DHL9880660C 1 19980211 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT BAGGAGE COMPT RT SIDE TUNNEL AT STA 1300 FLOORBEAM CORRODED. CUT OUT BEAM, FABRICATED PER EO MMC382N038 6 AND INSTALLED AT STA 1300, RBL 51. ANGLE 1.25 X 1.25 X 2.5 X 9.75. 2 L 7 4 4F RT 4A25 1998043000290 19980430 00290 WP 1998 4 30 DHL9880661C 1 19980211 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1340 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT BAGGAGE COMPT RT TUNNEL AT STA 1340, FLOORBEAM CORRODED. CUT OUT DAMAGED SECTION OF FLOORBEAM AND FABRI CATED FILLER AND ANGLE PER EO MMC382N0367. INSTALLED REPAIR PARTS PER THE EO, FILLER 1 X 1 ANGLE, 25 X 7.5. 2 L 7 4 4F RT 4A25 1998043000291 19980430 00291 WP 1998 4 30 DHL9880662C 1 19980211 A 5320 CIRCUMFERENTIAL DOUG DC8 DC873F 302199F WP BS 1240 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT BAGGAGE COMPT RT SIDE FLOOR AREA STA 1240 CORROSION ON CIRCUMFERENTIAL. FABRICATED REPAIR ANGLE AND STR AP PER SRM 51-1-21 AND EO MMC38N0374. 9 X 1 X 2.25 AT FS 1240 BETWEEN STR 6R. 2 L 7 4 4F RT 4A25 1998043000292 19980430 00292 WP 1998 4 30 DHL9880663C 1 19980213 A 5752 TAB DOUG DC8 DC873F 302199F WP LT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, LT AILERON TAB DELAMINATED. REMOVED AND REPAIRED TAB. 2 L 7 4 4F RT 4A25 1998043000293 19980430 00293 WP 1998 4 30 DHL9880664C 1 19980110 A 5512 5640807505 PANEL DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, COMPLY WITH DHL MSI 806-0913-1001, REMOVE AND REPLACE HORIZONTAL STAB CENTER SECTION, DUE TO CRACKED FASTENE R HOLE. REMOVED AND REPLACED AFT UPPER PANEL PER S/B 55-15. 2 L 7 4 4F RT 4A25 1998043000294 19980430 00294 WP 1998 4 30 DHL9880665C 1 19980211 A 5210 DOOR DOUG DC8 DC873F 302199F WP PAX DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN ENTRY DOOR TEMPORARY REPAIR INSTALLED ON UPPER FWD CORNER. REMOVED PREVIOUS DOUBLER AND FABRICATED NEW DOUBLER, 27 X 26 AND TRIPLER 22.25 X 19 PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998043000295 19980430 00295 WP 1998 4 30 DHL9880666C 1 19980130 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 150 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN CARGO COMPT FUS STA 150 LINE NR 3 FLOOR TRACK CHIPPED. REMOVED TRACK SECTION AND INSTALLED SPLICED AND TRACKS PER SRM 52-2-3, 40 LONG. 2 L 7 4 4F RT 4A25 1998043000296 19980430 00296 WP 1998 4 30 DHL9880667C 1 19980116 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 330 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN CARGO COMPT STQ 300 LINE NR 4 TRACK DAMAGED. REMOVED PREVIOIUSLY INSTALLED PLUG FROM STA 329 TO 333 AN D INSTALLED NEW PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000297 19980430 00297 WP 1998 4 30 DHL9880668C 1 19980113 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 3 ENG AFT REVERSER COWL I/B AREA MID SURFACE HEAT SHIELD COVER DAMAGED. TRIMMED AREA AND FABRICATED REPA IR PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998043000298 19980430 00298 WP 1998 4 30 DHL9880669C 1 19980113 A 5347 TRACK DOUG DC8 DC873F 302199F WP BS 1680 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN CARGO COMPT FS 1680 LINE NR 3 TRACK WORN. CUT OUT DAMAGED SECTION AND INSTALLED REPAIR PLUG PER SRM 51 -3-0. 2 L 7 4 4F RT 4A25 1998043000299 19980430 00299 WP 1998 4 30 DHL9880670C 1 19980112 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 860 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN CARGO COMPT FS 860 NR 3 FLOOR TRACK CHIPPED. CUT OUT DAMAGED SECTION AND INSTALLED PLUG PER SRM 51-1-8 FROM STA 859 TO 863. 2 L 7 4 4F RT 4A25 1998043000300 19980430 00300 WP 1998 4 30 DHL9880671C 1 19980104 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 680 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, MAIN CARGO COMPT FS 680 LINE NR 3 FLOOR TRACK CHIPPED. REMOVED DAMAGED PLUG AND FABRICATED NEW PER SRM 53-2 -3. 2 L 7 4 4F RT 4A25 1998043000301 19980430 00301 WP 1998 4 30 DHL9880672C 1 19980112 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 650 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 650 LINE NR 3 TRACK IS CHIPPED. CUT OUT DAMAGED SECTION AND REPLACED PER SRM 53-2-3 FROM STA 648 TO 652. 2 L 7 4 4F RT 4A25 1998043000302 19980430 00302 WP 1998 4 30 DHL9880674C 1 19980114 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 460 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 460 LINE NR 3 FLOOR TRACK CHIPPED. CUT OUT DAMAGED AREA AND FABRICATED REPAIRPLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000303 19980430 00303 WP 1998 4 30 DHL9880675C 1 19980102 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 420 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 420 LINE NR 3, FLOOR TRACK DAMAGED. CUT OUT DAMAGED SECTION AND INSTALLED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000304 19980430 00304 WP 1998 4 30 DHL9880676C 1 19980112 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 780 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 780 LINE NR 7 FLOOR TRACK WORN. CUT OUT DAMAGED SECTION OF TRACK AND INSTALLED PER SRM 53-2-3, 40 LONG. 2 L 7 4 4F RT 4A25 1998043000305 19980430 00305 WP 1998 4 30 DHL9880677C 1 19980123 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 230 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 230 LINE NR 7 FLOOR TRACK WORN. REMOVED AND REPLACED TRACK PER SRM 53-2-3, FROM FS 205. 2 L 7 4 4F RT 4A25 1998043000306 19980430 00306 WP 1998 4 30 DHL9880678C 1 19980123 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 180 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 180 LINE NR 7 FLOOR TRACK DAMAGED. CUT OUT DAMAGED SECTION FROM 178 TO 183. INSTALLED REPAIR PLUG PER S RM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000307 19980430 00307 WP 1998 4 30 DHL9880679C 1 19980123 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 160 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 160 LINE 7 FLOOR TRACK DAMAGED. CUT OUT DAMAGED SECTION FROM FS 158 TO 163, FABRICATED REPAIR PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000308 19980430 00308 WP 1998 4 30 DHL9880680C 1 19980124 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 180 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 180 LINE NR 6 FLOOR TRACK WORN. CUT OUT DAMAGED SECTION AND FABRICATED 4 HOLE. REPAIRED PLUG PER SRM 53 -2-3, FROM 178 TO 182. 2 L 7 4 4F RT 4A25 1998043000309 19980430 00309 WP 1998 4 30 DHL9880681C 1 19980124 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 160 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 160 LINE NR 6 FLOOR TRACK WORN. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR PLUG PER SRM 53-2-3, FS 1 60 TO 164. 2 L 7 4 4F RT 4A25 1998043000310 19980430 00310 WP 1998 4 30 DHL9880682C 1 19980125 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 200 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 200 LINE NR 6 FLOOR TRACK WORN. CUT OUT DAMAGED SECTION PER SRM 53-2-3. INSTALLED REPAIR PLUG FROM STA 200 TO 205. 2 L 7 4 4F RT 4A25 1998043000311 19980430 00311 WP 1998 4 30 DHL9880683C 1 19980114 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 420 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 420 LINE NR 6 FLOOR TRACK WORN. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PLUG PER SRM 5 3-2-3 FROM FS 414 TO 418 AND FROM 421 TO 425. 2 L 7 4 4F RT 4A25 1998043000312 19980430 00312 WP 1998 4 30 DHL9880684C 1 19980102 A 5330 PANEL DOUG DC8 DC873F 302199F WP BS 650 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, AFT OF REAR SPAR BETWEEN STA 650 AND SKIN PANEL DELAMINATED. REMOVED AND INSTALLED NEW PANEL PER SRM 51-3-0 . 2 L 7 4 4F RT 4A25 1998043000313 19980430 00313 WP 1998 4 30 DHL9880685C 1 19980114 A 7110 BRACKET DOUG DC8 DC873F 302199F WP NR 4 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, ENG NR 4 TURBINE CASE COOLING AIR INTAKE TUBE AFT MOUNT BRACKET CRACKED, 10 O'CLOCK. REMOVED AND REPLACED P ER MM 20-16-0. 2 L 7 4 4F RT 4A25 1998043000314 19980430 00314 WP 1998 4 30 DHL9880686C 1 19980114 A 7110 BRACKET DOUG DC8 DC873F 302199F WP NR 4 ENGINECOWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, NR 4 ENGINE HAS COOLING TUBE AFT MOUNT BRACKET CRACKED AT 5 O'CLOCK POSITION. REMOVED AND REPLACED BRACKET PER MM 20-16-0. 2 L 7 4 4F RT 4A25 1998043000315 19980430 00315 WP 1998 4 30 DHL9880687C 1 19980109 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 870 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 870 LINE NR 4 FLOOR TRACK CHIPPED. CUT OUT DAMAGED SECTION, FABRICATED REPAIR AND INSTALLED PER SRM 53-2 -3. 2 L 7 4 4F RT 4A25 1998043000316 19980430 00316 WP 1998 4 30 DHL9880688C 1 19980109 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1130 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1130 LINE NR 4 FLOOR TRACK WORN/CHIPPED. CUT OUT DAMAGED SECTION, FABRICATED REPAIR AND INSTALLED PER SR M 53-2-3. 2 L 7 4 4F RT 4A25 1998043000317 19980430 00317 WP 1998 4 30 DHL9880689C 1 19980120 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1330 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1330 LINE NR 4 FLOOR TRACK CHIPPED. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED REPAIR PER SRM 53-2-3 FROM FS 1330 TO 1334. 2 L 7 4 4F RT 4A25 1998043000318 19980430 00318 WP 1998 4 30 DHL9880690C 1 19980122 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1490 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1490 LINE NR 4 FLOOR TRACK CHIPPED. REMOVED 2 DAMAGED PLUGS, FABRICATED NEW PER SRM 53-2-3, FROM FS 1480 TO 1484 AND 1487 TO 1491. 2 L 7 4 4F RT 4A25 1998043000319 19980430 00319 WP 1998 4 30 DHL9880691C 1 19980117 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1580 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1580 LINE NR 4 FLOOR TRACK WORN. REMOVED PREVIOUSLY INSTALLED PLUG AND INSTALLED FABRICATED PLUG PER SRM 53-2-3 FROM STA 1578 TO 1602. 2 L 7 4 4F RT 4A25 1998043000320 19980430 00320 WP 1998 4 30 DHL9880692C 1 19980109 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1120 CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1120 LINE NR 2 TRACK CHIPPED. CUT OUT DAMAGED SECTION AND FABRICATED REPAIR PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000321 19980430 00321 WP 1998 4 30 DHL9880693C 1 19980128 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1600 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1600 LINE NR 2 FLOOR TRACK DAMAGED. REMOVED DAMAGED SECTION, INSTALLED PER SRM 53-2-3, 70 LONG. 2 L 7 4 4F RT 4A25 1998043000322 19980430 00322 WP 1998 4 30 DHL9880694C 1 19980128 A 5347 FLOOR TRACK DOUG DC8 DC873F 302199F WP BS 1660 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, FS 1660 LINE NR 2 TRACK DAMAGED. TRACKED REPLACED FROM 1590 TO FS 1660 PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998043000323 19980430 00323 WP 1998 4 30 DHL9880695C 1 19980211 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 1 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING NR 1 FLAP VANE DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-50-0. 2 L 7 4 4F RT 4A25 1998043000324 19980430 00324 WP 1998 4 30 DHL9880696C 1 19980211 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 2 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RIGHT WING NR 2 FLAP VANE DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-50-00. 2 L 7 4 4F RT 4A25 1998043000325 19980430 00325 WP 1998 4 30 DHL9880697C 1 19980211 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 3 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING NR 3 FLAP VANE DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-50-00. 2 L 7 4 4F RT 4A25 1998043000326 19980430 00326 WP 1998 4 30 DHL9880698C 1 19980211 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 2 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, RT WING GROUND SPOILER DELAMINATED. REMOVED, REPAIRED AND REPLACED PER MM 27-61-1. 2 L 7 4 4F RT 4A25 1998043000327 19980430 00327 WP 1998 4 30 DHL9880699C 1 19980202 A 5350 56535681 FAIRING DOUG DC8 DC873F 302199F WP WING CHIPPED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 806DH 46002 AT C-CHECK, UNDER WING FAIRING HAS EDGE PANEL CHIPPED OFF. REMOVED AND REPLACED DAMAGED PANEL PER SRM 51-1-15. 2 L 7 4 4F RT 4A25 1998043000328 19980430 00328 WP 1998 4 30 RRXA98019 1 19980106 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND INTERIOR SKIN CORRODED BEYOND LIMITATIONS IAW DC-8 SRM AT, STA 660 AND BETWEEN LONGERO NS 32 RIGHT AND 33 RIGHT. REMOVED ALL CORROSION AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND DOUBLER REPAIR IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH D85-R01, DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998043000329 19980430 00329 WP 1998 4 30 RRXA98021 1 19980127 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 312 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 961R 46133 DURING A MAINTENANCE VISIT, FOUND CORROSION ON EXTERIOR SKIN BEYOND LIMITATIONS IAW DC-8 SRM AT, STA 312 LONGERON 36. R EMOVED ALL CORROSION IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILL IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH D85-R03 AND DC-8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998043000330 19980430 00330 WP 1998 4 30 98ZZZM278 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 585 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998043000331 19980430 00331 WP 1998 4 30 98ZZZM279 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 680 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998043000332 19980430 00332 WP 1998 4 30 98ZZZM280 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 764 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998043000333 19980430 00333 WP 1998 4 30 98ZZZM281 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 519 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998043000334 19980430 00334 WP 1998 4 30 98ZZZM282 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 606 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998043000335 19980430 00335 WP 1998 4 30 98ZZZM283 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 675 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998043000336 19980430 00336 WP 1998 4 30 98ZZZM284 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 784 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REF GAIA9815. 2 L 7 2 4F A6WE 1998043000337 19980430 00337 WP 1998 4 30 98ZZZM285 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 604 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REFERENCE GAIA9815. 2 L 7 2 4F A6WE 1998043000338 19980430 00338 WP 1998 4 30 98ZZZM286 1 19980209 A 5347 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 694 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AB BS 383. SEAT TRACK WAS REPAIRED IAW KIT TY HAWK EA D9-53-051. REFERENCE GAIA9815. 2 L 7 2 4F A6WE 1998043000339 19980430 00339 WP 1998 4 30 GAIA9814 1 19980209 A 5330 591422 SKIN DOUG DC9 DC915F 3022037 WP BS 817 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 50014 47055 DURING INSPECTION OF THE FUSELAGE SKIN PER AD 81-26-03R1 SIX CRACKS WERE FOUND AT STATION 817. FOUR CRACKS BETWEEN L2R ANDL3R AND TWO CRACKS BETWEEN L1 AND L2L. THE SKIN WAS REPAIRED IAW SERVICE REWORK DRAWING J060143. (M) 2 L 7 2 4F A6WE 1998043000340 19980430 00340 1998 4 30 GAIA9818 4 19980209 A 2210 YAW DAMPER BOEING 727 727223 1384074 NM AUTOPILOT MALFUNCTIONED A A GAIA B EMER. DESCENT F FLT CONT AFFECTED CR CRUISE 1 SW 07 855AA 20996 EN ROUTE FROM MSP TO TOL, FLT CREW REPORTES AT FL 370 AIRCRAFT YAWED BACK AND FORTH. CONTINUED YAWING UNITL DESCENT TO FL 210. NO WARNING LIGHTS ILLUMINATED. APPEARED TO BE YAW DAMPER PROBLEM. POSSIBLE LOOSE RUDDER LINKAGE DECLARED IFE. PERFORMED YAW DAMPER CHECK AND TEST. BOTH YAW DAMPER UNITS TEST NORMAL. CHECKED UPPER AND LOWER RUDDER FOR FAIR IN S LIP STREAM. CHECKED FOR LOOSE LINKAGE, WITH NO DEFECTS FOUND. RUDDER SYSTEM CHECKS NORMAL AND AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 3 4F A3WE 1998043000341 19980430 00341 WP 1998 4 30 GAIA9812 1 19980209 A 5712 99193691 BLKHD T-CAP DOUG DC9 DC915F 3022037 WP WS 58.5 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 50014 47055 DURING INSPECTION OF CORROSION TASK 13-57301 WHILE AIRCRAFT WAS IN C-CHECK LEVEL 2 CORROSION WAS FOUND ON THE SURFACE OF THE WING BULKHEAD LOWER T-CAP AT STATION 58.5 OF THE LEFT WING BETWEEN STRINGER 11 THROUGH 17. THE T-CAP WAS REPAIRED IAW WITH DC-9 SB 57-98 SB 57-98. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998043000342 19980430 00342 WP 1998 4 30 GAIA9811 1 19980209 A 5712 99193692 BLKHD T-CAP DOUG DC9 DC915F 3022037 WP WS 58.5 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 47055 DURING INSPECTION OF CORROSION TASK 14-57301 WHILE AIRCRAFT WAS IN C-CHECK LEVEL 2 CORROSION WAS FOUND ON THE SURFACE OF THE WING BULKHEAD LOWER T-CAP AT STATION 58.5 OF THE RIGHT WING BETWEEN STRINGERS 11 THROUGH 16. THE T-CAP WAS REPAIRE D IAW THE DC-9 SB 57-98. THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998043000343 19980430 00343 WP 1998 4 30 GAIA9813 1 19980209 A 5330 59114011 SKIN DOUG DC9 DC915F 3022037 WP BS 211 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 50014 47055 DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR AND DENT ON THE FUSELAGE SKIN JUST BELOW THE FORWARD ENTRANCE DOOR B ETWEEN LONGRON 20L AND 18L AT FUSELAGE STATION 211. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-049. (M) 2 L 7 2 4F A6WE 1998043000344 19980430 00344 NM 1998 4 30 ASAA9840012 1 19980122 A 5320 6978602 BRACKET BOEING 737 7374Q8 NM BS 729.35 WORN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - DURING C-CHECK, EXCESSIVE WEAR WAS FOUND AROUND FASTENER HOLE ON THE LEFT MLG FAIRING BRACKET AT STATION 729.35. R EPAIRED PER EA 5320-01333. (M) 2 L 7 2 4F RT A16WE 1998043000345 19980430 00345 NM 1998 4 30 ASAA9840013 1 19980122 A 5330 6546881 SKIN BOEING 737 7374Q8 NM BS 1064 PUNCTURED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - DURING C-CHECK, A PUNCTURE WAS FOUND IN THE FUSELAGE SKIN AT FS 1064 AND STRINGER 24. REPAIRED PER EA 5330-01311 AND BOEING TELEX ASA-SEA-98-00012RR. (M) 2 L 7 2 4F RT A16WE 1998043000346 19980430 00346 NM 1998 4 30 ASAA9840014 1 19980122 A 5347 654795734 TRACK BOEING 737 7374Q8 NM BS 803-809 CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - DURING C-CHECK, MINOR SURFACE CORROSION WAS FOUND AT TWO LOCATIONS ON THE UPPER SURFACE ON THE OUTBOARD FLANGE OF THE TIE DOWN TRACK IN THE AFT CARGO COMPARTMENT. REPAIRED PER EA 5360-01015. (M) 2 L 7 2 4F RT A16WE 1998043000347 19980430 00347 NM 1998 4 30 ASAA9840015 1 19980122 A 5522 65C25746141 SKIN BOEING 737 7374Q8 NM LT ELEVATOR PEELING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - DURING C-CHECK, A SMALL SECTION OF THE OUTER CARBON LAYER WAS FOUND PEELING ON THE LEFT ELEVATOR LOWER SURFACE NEX T TO THE 3RD HINGE CUTOUT FROM INBOARD END. REPAIRED PER EA 5520-01051 AND BOEING TELEX ASA-SEA-98-0010RR. (M) 2 L 7 2 4F RT A16WE 1998043000348 19980430 00348 WP 1998 4 30 ASAA9880023 1 19980203 A 5320 FRAME DOUG DC9 DC982 3022082 WP CARGO DOORWAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 OAK - DURING 30K CHECK, CRACK WAS FOUND IN FORWARD CARGO COMPARTMENT DOOR FRAME IN RADIUS AT FORWARD UPPER STRIKER. STO P DRILLED CRACK AND INSTALLED DOUBLER IAW ASA EA 5320-01334. (M) 2 L 7 2 4F A6WE 1998043000349 19980430 00349 WP 1998 4 30 ASAA9880024 1 19980203 A 5230 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 OAK - DURING 30K CHECK, CRACKS WERE FOUND IN FORWARD CARGO COMPARTMENT DOOR INNER FRAME SUPPORT 'T' ANGLE AND FORWARD LO WER STRIKER FITTING. STOP DRILLED CRACKS AND INSTALLED NEW INTERCOSTAL, TEE FITTING, 'L' ANGLE AND SHIMS IAW DC9 SRM 51 -30-02 AND INSTALLED DOUBLER IAW DC9 SRM 52-03, FIG 1, PAGE 2. (M) 2 L 7 2 4F A6WE 1998043000350 19980430 00350 NM 1998 4 30 ASAA9840020 1 19980204 A 5520 69560273 FITTING BOEING 737 7374Q8 NM RT ELEVATOR CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING C-CHECK, FOUND CORROSION IN THE TWO AFT HOLES OF THE RT OUTBOARD ELEVATOR HINGE FITTING. REPAIRED PER EA 5 520-01052 AND BOEING TELEX ASA-SEA-98-0029RR. (M) 2 L 7 2 4F RT A16WE 1998043000351 19980430 00351 NM 1998 4 30 ASAA9840021 1 19980204 A 5320 6517688175 ANGLE BOEING 737 7374Q8 NM L1 DOOR SILL CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING C-CHECK, FOUND CORROSION IN THE UPPER SURFACE OF THE L1 DOOR SILL ANGLE. REPAIRED PER EA 5310-01569 AND BO EING TELEX ASA-SEA-98-0030RR. (M) 2 L 7 2 4F RT A16WE 1998043000352 19980430 00352 NM 1998 4 30 ASAA9840023 1 19980204 A 7830 315A1508507 TR UNIT BOEING 737 7374Q8 NM NR 2 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING C-CHECK, THE NR 2 ENGINE INBOARD T/R BULLNOSE SECTION WAS FOUND GOUGED AT THE 10 AND 11 O'CLOCK POSITIONS. REPAIRED PER EA 5430-01027 AND BOEING TELEX ASA-SEA-98-0028RR. (M) 2 L 7 2 4F RT A16WE 1998043000353 19980430 00353 NM 1998 4 30 ASAA9840022 1 19980204 A 7830 315A1508507 TR UNIT BOEING 737 7374Q8 NM NR 1 ENGINE GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING C-CHECK, THE NR 1 ENGINE INBOARD T/R BLOCKER DOORS WERE FOUND RIDING THE BULLNOSE IN SEVERAL PLACES. REPAI RED PER EA 5430-01027 AND BOEING TELEX ASA-SEA-98-0028RR. (M) 2 L 7 2 4F RT A16WE 1998043000354 19980430 00354 NM 1998 4 30 ASAA9840024 1 19980204 A 5753 65C2630933 STIFFENER BOEING 737 7374Q8 NM LT TE FLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING C-CHECK, FOUND WEAR ON A STIFFENER ON THE LEFT WING NR 3 FLAP TRACK FAIRING INBOARD SKIN. REPAIRED PER EA 5720-01134. (M) 2 L 7 2 4F RT A16WE 1998043000355 19980430 00355 NM 1998 4 30 ASAA9840025 1 19980204 A 5753 65C353181 FAIRING BOEING 737 7374Q8 NM RT TE FLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 771AS 25104 SEA - DURING C-CHECK, THE RT WING NR 6 FLAP TRACK FAIRING TAILCONE WAS FOUND TO HAVE LOOSE RIVETS. REPAIRED PER EA 5750 -01212 ADN BOEING TELEX ASA-SEA-96-0203RR. (M) 2 L 7 2 4F RT A16WE 1998043000356 19980430 00356 NM 1998 4 30 ASAA9810011 1 19980125 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM PALLET 9-2 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET POSITIONS 9-2 AND 10-6. REPLACED BOTH BATTERY PACKS AND THE RECEIVER ON PALLET 9-2 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998043000357 19980430 00357 NM 1998 4 30 98ZZZM287 1 19980125 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM PALLET 10-6 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT PALLET POSITIONS 9-2 AND 10-6. REPLACED BOTH BATTERY PACKS AND THE RECEIVER ON PALLET 9-2 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998043000358 19980430 00358 NM 1998 4 30 ASAA9840018 1 19980127 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 776AS 25109 PDX - FLT 424 - PRIOR TO FLT, THE EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 22-25. RECONNECTED LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998043000359 19980430 00359 WP 1998 4 30 ASAA9880019 1 19980130 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 979AS 53471 PDX - PRIOR TO DEPARTURE OF FLT 520, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. SECURED LOOSE CONNECTOR TO LIGHT ASSY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998043000360 19980430 00360 WP 1998 4 30 ASAA9880020 1 19980131 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 28 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE MID POWER SUPPLY AND REPLACED THE AFT POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998043000361 19980430 00361 WP 1998 4 30 98ZZZM288 1 19980131 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 955AS 48080 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 19 TO 28 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE MID POWER SUPPLY AND REPLACED THE AFT POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998043000362 19980430 00362 WP 1998 4 30 ASAA9880021 1 19980201 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS AND THE OVERHEAD EMERGENCY LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998043000363 19980430 00363 WP 1998 4 30 ASAA9880022 1 19980203 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 2814 49103 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPE RATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998043000364 19980430 00364 WP 1998 4 30 ASAA9880010 1 19980114 A 5210 TRIM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 955AS 48080 SEA - AFTER ARRIVAL OF FLT 547 - CREW REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. TRIMMED UPPER DOOR TRIM TO ALLOW FOR SEAL DEFLECTION AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998043000365 19980430 00365 WP 1998 4 30 ASAA9880011 1 19980117 A 5210 TRIM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 SEA - AFTER ARRIVAL OF FLT 196, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN. TRIMMED FORWARD UPPER CORNER OF DOOR T RIM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998043000366 19980430 00366 1998 4 30 ASAA9880012 4 19980118 A 2565 D37013115 BOTTLE DOUG DC9 DC982 3022082 WP R1 DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 937AS ALT2261604A 49364 PDX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998043000367 19980430 00367 WP 1998 4 30 ASAA9880018 1 19980127 A 5210 591473023 LINK DOUG DC9 DC983 3022083 WP L1 DOOR BENT A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 943AS 53018 ONT - PRIOR TO DEPARTURE OF FLT 595, CREW REPORTED, THE L1 DOOR WOULD NOT LATCH OPEN. REPLACED THE DOOR HOLD OPEN MECHA NISM LINK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998043000368 19980430 00368 NM 1998 4 30 PCAA9800682 1 19980104 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 829EX 146 COCKPIT PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVI CEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000369 19980430 00369 NM 1998 4 30 PCAA9800681 1 19980103 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 821EX 173 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000370 19980430 00370 NM 1998 4 30 PCAA9800679 1 19980101 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 812EX 312 BOTH CABIN CEILING AND LEFT AFT EXTERIOR EMERGENCY LIGHTS INOPERATIVE FROM FLIGHT ATTENDANTS SWITCH. REMOVED AND REPLAC ED BATTERY PACK AT POSITION 3351-P3. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000371 19980430 00371 NM 1998 4 30 PCAA9800686 1 19980106 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 833EX 282 COCKPIT PORTABLE EMERGENCY LIGHT COMES ON IN FLIGHT. REMOVED AND REPLACED COCKPIT PORTABLE EMERGENY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000372 19980430 00372 NM 1998 4 30 PCAA9800683 1 19980106 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 813AW 247 THREE LIGHTS INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULBS. OPERATIONAL TEST NO RMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000373 19980430 00373 NM 1998 4 30 PCAA9800684 1 19980107 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 COCKPIT PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SER VICE. (M) 2 H 7 2 4T RT A13NM 1998043000374 19980430 00374 NM 1998 4 30 PCAA9800677 1 19980104 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 13 808EX 299 UPON APPROACH INTO BTV, THE LANDING GEAR WOULD NOT EXTEND NORMALLY. ALTERNATE GEAR EXTENSION PERFORMED. MAINTENANCE TR OUBLESHOT SYSTEM. FOUND THE LANDING GEAR SELECTOR VALVE AT FAULT. REMOVED AND REPLACED VALVE IAW DHC MANUAL, SYSTEM OP ERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000375 19980430 00375 NM 1998 4 30 PCAA980687 1 19980108 A 2750 CONNECTOR DHAV DHC8 DHC8102 2809003 NM TE FLAPS CORRODED A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 811AW 201 DURING CLIMB-OUT FROM LGA, THE FLAP DRIVE CAUTION LIGHT ILLUMINATED. A/C RETURNED TO FIELD. MAINTENANCE TROUBLESHOT SY STEM. FOUND MOISTURE AT 2752-P4 TORQUE SENSOR CANNON PLUG CLEANED. ALSO, FOUND SLIGHT CORRSION AT 2752-P5. REPLACED C ANNON PLUG. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000376 19980430 00376 NM 1998 4 30 PCAA9800688 1 19980108 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 809EX 302 FORWARD CENTER AISLE CABIN FLOOR EMERGENCY PROXIMITY LIGHTS INOPERATIVE. REPAIRED FORWARD CENTER AISLE FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM WIRING. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000377 19980430 00377 NM 1998 4 30 PCAA9800689 1 19980110 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 814EX 318 FORWARD RED EMERGENCY FLOOR PROXIMITY SYSTEM LIGHTS INOPERATIVE. SECURED UNDERFLOOR CONNECTOR. OPERATIONAL TEST NORMAL . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000378 19980430 00378 NM 1998 4 30 PCAA9800690 1 19980113 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 813AW 247 FORWARD CABIN EMERGENCY SIGN HAS ONE INOPERATIVE BULB. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000379 19980430 00379 NM 1998 4 30 PCAA9800691 1 19980113 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 824EX 387 LEFT AFT EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNE D TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000380 19980430 00380 NM 1998 4 30 PCAA9800692 1 19980113 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 824EX 387 RIGHT AFT EXTERIOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURN ED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000381 19980430 00381 NM 1998 4 30 PCAA9800693 1 19980114 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 826EX 389 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPER ATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000382 19980430 00382 NM 1998 4 30 PCAA9800694 1 19980119 A 3230 PSEU DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 13 821EX 173 EN ROUTE TO PHL, UPON SELECTING THE LANDING GEAR DOWN THE GEAR DID NOT EXTEND. CAUTION LIGHT ILLUMINATED MOMENTARILY TH EN EXTINGUISHED. THE CONTROL CIRCUIT BREAKER POPPED. AN ALTERNATE EXTENSION WAS PERFORMED AND THE A/C LANDED SAFELY. M AINTENANCE TROUBLESHOT SYSTEM, INSPECTED WIRING AT SELECTOR VALVES, CHECKED INTEGRITY OF DIODED CR1, CR2 AT THE NR 1 REL AY PANEL, ALL CHECKED GOOD. REPLACED RELAYS 3261K5, 3261K6, 3261K7, AND PSEU. CYCLED GEAR SEVERAL TIMES. NO DEFECTS N OTED. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000383 19980430 00383 NM 1998 4 30 PCAA9800695 1 19980116 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 808EX 299 LIGHT IN FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH IS INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A /C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000384 19980430 00384 NM 1998 4 30 PCAA9800696 1 19980116 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000385 19980430 00385 NM 1998 4 30 PCAA9800697 1 19980119 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 838EX 220 FORWARD AIRSTAIR DOOR EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY. OPERATION AL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000386 19980430 00386 NM 1998 4 30 PCAA9800698 1 19980118 A 3397 WIRE DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 EICHP 258 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REPAIRED OPEN CIRCUIT IN FLOOR EMERGENCY PROXIMITY LIGHT SYSTEM WIRING. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000387 19980430 00387 NM 1998 4 30 PCAA9800699 1 19980120 A 5610 17180003 WINDOW DHAV DHC8 DHC8102 2809003 NM LT COCKPIT CRACKED A PCAA O OTHER O OTHER CR CRUISE 1 EA 13 EICBJ 215 DURING CRUISE FLIGHT EN ROUTE TO ALB, THE CAPTAIN'S SIDE WINDOW CRACKED. A/C LANDED WITHOUT INCIDENT. REMOVED AND REPL ACED LEFT SIDE WINDOW IAW DHC MM. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000388 19980430 00388 NM 1998 4 30 PCAA9800700 1 19980121 A 3234 574205 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA K NONE O OTHER AP APPROACH 1 EA 13 819EX 016 UPON APPROACH INTO ROC, THE LANDING GEAR WOULD NOT EXTEND NORMALLY. ALTERNATE EXTENSION PERFORMED, LANDED A/C WITHOUT I NCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, FOUND THE LANDING GEAR SELECTOR VALVE AT FAULT. REMOVED AND REPLACED IAW DHC MAINTENANCE PROCEDURES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000389 19980430 00389 NM 1998 4 30 PCAA9800701 1 19980122 A 3230 PSEU DHAV DHC8 DHC8102 2809003 NM LANDING MALFUNCTIONED A PCAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 13 815EX 321 UPON APPROACH INTO PHL, THE LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. CREW PERFORMED GO AROUND AND THEN GEAR EXTE NDED NORMALLY. MAINTENANCE TROUBLESHOT SYSTEM, COULD NOT DUPLICATE PROBLEM. REMOVED AND REPLACED PSEU AS A PRECAUTION. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000390 19980430 00390 NM 1998 4 30 PCAA9800702 1 19980123 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 813AW 247 ONE LIGHT INOPERATIVE IN FLOOR EMEREGNCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000391 19980430 00391 NM 1998 4 30 PCAA9800703 1 19980122 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 815EX 321 EMERGENCY LIGHT SWITCH AT FLIGHT ATTENDANT PANEL HAS INDICATOR LIGHT INOPERATIVE. REMOVED AND REPLACED BULB. OPERATION AL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000392 19980430 00392 NM 1998 4 30 PCAA9800704 1 19980124 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 817EX 191 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000393 19980430 00393 NM 1998 4 30 PCAA9800705 1 19980121 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000394 19980430 00394 NM 1998 4 30 PCAA9800706 1 19980125 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 EICHP 258 TWO LIGHTS INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED ONE BULB AND REPLACED ONE LIG HT SOCKET. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000395 19980430 00395 NM 1998 4 30 PCAA9800708 1 19980126 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 OVERHEAD EMERGENCY LIGHT AT ROW FIVE INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000401 19980430 00401 NM 1998 4 30 MZZA98052 1 19980102 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP SEPARATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING T/E OUTBOARD AFT FLAP UPPER S KIN AFT EDGE AT WBL 388. THE DAMAGED SKIN 8 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF H ANGAR NON ROUTINE REPAIR ITEM CARD NR 841155 (SEQ NR 06055). (M) 2 L 7 3 4F A3WE 1998043000402 19980430 00402 NM 1998 4 30 MZZA98051 1 19980102 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP SEPARATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING T/E OUTBOARD AFT FLAP UPPER S KIN AFT EDGE AT WBL 342. THE DAMAGED SKIN 7 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 841154 (SEQ NR 06054). (M) 2 L 7 3 4F A3WE 1998043000403 19980430 00403 NM 1998 4 30 MZZA98050 1 19980102 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP DISBONDED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DISBONDED WAS FOUND ON RT WING T/E OUTBOARD AFT FLAP UPPER SU RFACE EXISTING REPAIR DOUBLER AT WBL 468. THE DAMAGED EXISTING REPAIR DOUBLER WAS REMOVED AND REPAIRED PER B727 SRM 51- 40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 841153 (SEQ NR 06053). (M) 2 L 7 3 4F A3WE 1998043000404 19980430 00404 NM 1998 4 30 MZZA98049 1 19980102 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP SEPARATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING T/E INBOARD AFT FLAP UPPER SK IN AT WBL 127. THE DAMAGED SKIN 7 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 841150 (SEQ NR 06050). (M) 2 L 7 3 4F A3WE 1998043000405 19980430 00405 NM 1998 4 30 MZZA98048 1 19980112 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP SEPARATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEPARATION WAS FOUND ON RT WING INBOARD T/E AFT FLAP UPPER SK IN AT WBL 208. THE DAMAGED SKIN 3 INCH BY .5 INCH IN SIZE WAS REPAIRED PER B727 SRM 51-40-6 FIGURE 26. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 841149 (SEQ NR 06049). (M) 2 L 7 3 4F A3WE 1998043000406 19980430 00406 NM 1998 4 30 MZZA98047 1 19980112 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING T/E INBOARD AFT FLAP T/E UP PER SKIN AT WBL 182. THE DAMAGED SKIN 11.5 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. R EF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 841148 (SEQ NR 06048). (M) 2 L 7 3 4F A3WE 1998043000407 19980430 00407 NM 1998 4 30 MZZA98046 1 19980102 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING T/E INBOARD AFT FLAP AT WBL 234. THE DAMAGED SKIN 4 INCHES BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRD PER B727 SRM 51-40-6. REF, HANGAR NON RO UTINE REPAIR ITEM CARD NR 841147 (SEQ NR 06047). (M) 2 L 7 3 4F A3WE 1998043000408 19980430 00408 NM 1998 4 30 MZZA98045 1 19980102 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP DISBONDED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DISBONDED WAS FOUND ON RT WING INBOARD AFT FLAP OUTBOARD AFT CORNER. THE DAMAGED SKIN 5 INCH BY 5.5 INCH WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 841164 (SEQ NR 06046). (M) 2 L 7 3 4F A3WE 1998043000409 19980430 00409 NM 1998 4 30 MZZA98044 1 19980105 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WS FOUND ON LEFT WING OUTBOARD T/E AFT FLAP LOWE R SURFACE AT WBL 450. THE DAMAGED SKIN 6 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF , HANGAR NON ROUTINE REPAIR ITEM CARD NR 806449 (SEQ NR 05027). (M) 2 L 7 3 4F A3WE 1998043000410 19980430 00410 NM 1998 4 30 MZZA98043 1 19980105 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIR, DELAMINATION WERE FOUND ON LEFT WING OUTBOARD AFT FLAP UPPER SURFACE AT THE FOLLOWING LOCATION, WBL 301, WBL 359, WBL 363 AND WBL 492. THE DAMAGED SKIN WERE TRIMMED AND REPAIRED PE R B727 SRM 51-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 806448 (SEQ NR 05026). (M) 2 L 7 3 4F A3WE 1998043000411 19980430 00411 NM 1998 4 30 MZZA98042 1 19980105 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING INBOARD T/E AFT FLAP UPPE R SURFACE BETWEEN WBL 86 AND WBL 96. THE DAMAGED SKIN 10 INCH BY 2 INCH IN SIZE WAS TRIMMED AND REPAIRED PER B727 SRM 5 1-40-6. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 806447 (SEQ NR 05025). (M) 2 L 7 3 4F A3WE 1998043000414 19980430 00414 NM 1998 4 30 MZZA98039 1 19980105 A 5311 FRAME BOEING 727 727224 1384076 NM BS 580 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1 INCH LONG CRACK WAS FOUND ON FORWARD CARGO COMPRTMENT FRAME UPPER CHORD AT BS 580, RBL 3. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-3 FIGURE 1. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 839630 (SEQ NR 01092). (M) 2 L 7 3 4F A3WE 1998043000415 19980430 00415 NM 1998 4 30 MZZA98038 1 19980105 A 5320 69439473 SUPPORT FITTING BOEING 727 727224 1384076 NM NLG W/W CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WERE FOUND ON NLG W/W AFT MOUNT SUPPORT FITT ING PLATES AT BS 337 RBL 17.5 AND LBL 17.5. THE CORRODED MOUNT SUPPORT FITTING PLATES WERE REMOVED AND REPLACED PER B72 7 SRM 51-30-2. REF, HANGAR NON ROUTINE REPAIR ITEM CARD NR 839628 (SEQ NR 01091). (M) 2 L 7 3 4F A3WE 1998043000416 19980430 00416 WP 1998 4 30 UPS98825895 1 19980210 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1024 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:C F/S 1024 LBL 59 - SEAT TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SECT ION OF TRACK IAW SRM ADDN DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 1998043000419 19980430 00419 NE 1998 4 30 98ZZZX956 2 19980119 A 7414 101536421 MAGNETO DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE RT ENG LT MAG FAILED A VLLA O OTHER E VIBRATION/BUFFET CR CRUISE 1 GL 05 36AP 2037 EA035049 13439 BP307288 IN CRUISE POWER, PILOT REPORTED RIGHT ENGINE SHAKING. WHEN ON GROUND, MAGNETO CHECK SHOWED LEFT MAGNETO RUNNING VERY RO UGH. REMOVED MAGNETO AND FOUND IT SPARKING INTERMITTENTLY. 2 L 7 2 4R 4 R A669 5E4 1998043000451 19980430 00451 SO 1998 4 30 98ZZZX988 2 19980210 A 8530 637837 VALVE SPRING CESSNA 402 402C 207590R CE CONT O520 TSIO520UB 17040 SO ENGINE EXHAUST BROKEN A HYIA K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 NE 01 6875D 1100 402C0511 811011R RIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS. 1 L 7 2 3O 3 O A7CE E8CE 1998043000452 19980430 00452 SO 1998 4 30 98ZZZX989 2 19980210 A 8530 631521 VALVE SPRING CESSNA 402 402C 207590R CE CONT O520 TSIO520UB 17040 SO ENGINE INTAKE BROKEN A HYIA K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS IN INSP/MAINT 1 NE 01 6875D 1100 402C0511 811011R RIGHT ENGINE RUNNING ROUGH. FOUND 8 OF 12 VALVE SPRINGS BROKEN. REMOVED AND REPLACED ALL VALVE SPRINGS. 1 L 7 2 3O 3 O A7CE E8CE 1998043000461 19980430 00461 EU 1998 4 30 USAAF98008 2 19980119 A 7510 40E183 SHUTOFF VALVE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU RT ENGINE INOPERATIVE A A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 863US 11303 GSO - FLT 875 - FLT EN ROUTE RIC TO CLT, WHEN NR 2 ENGINE ANTI-ICE FAILURE OCCURRED. CREW RESET CIRCUIT BREAKER AND IT POPPED. DUE TO WEATHER CONDITIONS IN CLT, FLIGHT DIVERTED TO GSO. FLT LANDED GSO WITHOUT FURTHER INCIDENT. MAINTENANC E REPLACED RIGHT ENGINE ANTI-ICE VALVE. OPS AND LEAK CHECK OK PER MM 30-21-01 400-814-A. (M) 2 L 7 2 4F 4 F RT 1998043000462 19980430 00462 NE 1998 4 30 GAIA9819 2 19980212 A 7261 STUD BOEING 727 7272J0 138407E NM PWA JT8 JT8D15 52051 NE GEARBOX LOOSE A GAIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 281KH 21105 ON DEPARTURE OUT OF TOL, RAPIDLY LOST OIL QTY NR 3 ENGINE DURING CLIMB-OUT, TEMPS AND PRESSURES OK. SHUT DOWN ENGINE AT 1.5 GALLONS REMAINING. ON POST FLIGHT FOUND STUD PULLED FROM OIL FILTER HOUSING. REPAIRED LOOSE STUD AND REMOVED AND REPLACED OIL FILTER IAW 79-20-06. OPS CHECK GOOD, NO LEAKS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A3WE E2EA 1998043000463 19980430 00463 EU 1998 4 30 RAIA980202 1 19980203 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 428AM 877 FLT 7336 - STL - LEFT ENGINE RPM WENT TO ZERO DURING CLIMB. MAINTENANCE REPLACED LEFT ENGINE TACH GENERATOR. (M) 2 L 7 2 4T RT A56EU 1998043000464 19980430 00464 EU 1998 4 30 RAIA980208 1 19980205 A 3234 DN1076ZMK4 HANDLE BAG JETSTM JETSTM3201 1500217 EU INST PANEL FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 864AE 864 FLT 4784 - LAX - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE REPLACED LANDING GEAR HANDLE. (M) 2 L 7 2 4T RT A56EU 1998043000465 19980430 00465 1998 4 30 RAIA980209 3 19980205 A 6112 B5JFR36C1104D BOOT JETAIR JETSTM JETSTM4101 1500501 EU LT PROPELLER FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 553HK 2747 41066 FLT 7706 - LEFT PROPELLER DE-ICE FAILED IN FLIGHT. MAINTENANCE REPLACED LEFT PROPELLER ASSEMBLY DUE TO FAILED DE-ICE BO OT. (M) 2 L 7 2 4T RT A41NM 1998043000466 19980430 00466 1998 4 30 RAIA980207 4 19980205 A 3418 45150561 AOA VANE AEROSP ATR42 ATR42300 8680920 EU LT FUSELAGE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 426TE 228 FLT 7140 - STL - CAPTAINS STICK PUSHER FAULTED IN FLIGHT. MAINTENANCE REPLACED LEFT ANGLE OF ATTACK VANE. (M) 2 H 7 2 4T RT A53EU 1998043000467 19980430 00467 1998 4 30 RAIA980206 4 19980205 A 3418 45150560 AOA VANE AEROSP ATR42 ATR42300 8680920 EU RT FUSELAGE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 426TE 228 FLT 7136 - STIL - STICK PUSHER FAULTED AFTER TAKEOFF. MAINTENANCE REPLACED RIGHT ANGLE OF ATTACK VANE. (M) 2 H 7 2 4T RT A53EU 1998043000468 19980430 00468 EU 1998 4 30 RAIA980203 1 19980205 A 3620 6411343 SWITCH AEROSP ATR72 ATR72202 8680940 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 723TE 283 FLT 7158 - STL - LEFT ENGINE AIR BLEED FAULT ILLUMINATED. MAINTENANCE REPLACED LEFT ENGINE BLEED OVER TEMPERATURE SWITC H. (M) 2 H 7 2 4T RT A53EU 1998043000469 19980430 00469 EU 1998 4 30 RAIA980204 1 19980204 A 3060 D45081B TIMER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 550HK 41039 FLT 7650 - JFK - LEFT PROPELLER DE-ICE FAILED. MAINTENANCE REPLACED LEFT PROPELLER DE-ICE TIMER. (M) 2 L 7 2 4T RT A41NM 1998043000470 19980430 00470 1998 4 30 RAIA980205 4 19980105 A 3418 350A23008314 COMPUTER AEROSP ATR42 ATR42300 8680920 EU E/E COMPT FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 426TE 228 FLT 7136 - STL - STICK PUSHER FAULTED IN FLIGHT. MAINTENANCE REPLACED CREW ALERTING COMPUTER. (M) 2 H 7 2 4T RT A53EU 1998043000473 19980430 00473 NM 1998 4 30 MASA98025 1 19980210 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING MAINTENANCE INSPECTION, PORTABLE EMERGENCY LIGHT STAYED ILLUMINATED AFTER TESTING. MAINTENANCE REPLACED THE PORT ABLE EMERGENCY LIGHT ASSEMBLY. (M) 2 H 7 2 4T RT A13NM 1998043000474 19980430 00474 SO 1998 4 30 MASA98022 1 19980208 A 3350 1149053 LENS ASSY EMB 120 EMB120RT SO CABIN MISSING A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 287UE 120183 FLT 5595 - JAX-FLL - CREW REPORTED THE COVER MISSING ON THE EMERGENCY EXIT SIGN OVER THE JUMP SEAT. MAINTENANCE REPLACE D LENS ASSEMBLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998043000475 19980430 00475 EA 1998 4 30 MASA98023 1 19980116 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA SERVICE DOOR FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 DURING NIGHT MAINTENANCE, FOUND EMERGENCY LIGHT AFT OF SERVICE DOOR WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLA CED THE BULB. (M) 2 L 7 2 4F RT A21EA 1998043000476 19980430 00476 CE 1998 4 30 MASA98020 1 19980206 A 3260 GE327 BULB BEECH 1900 1900D 1154162 CE LT MLG FAILED A MASA B EMER. DESCENT P NO WARNING INDICATION AP APPROACH 1 SW 07 146ZV UE146 FLT 407 - ROW-ABQ - CREW REPORTED, NO LEFT MAIN GEAR INDICATION. CREW VISUALLY VERIFIED GEAR WAS DOWN. CAPTAIN PUMPED GEAR DOWN UNTIL FELT RESISTANCE. CREW DECLARED AN EMERGENCY AND PROCEEDED TO LAND. AIRCRAFT LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE REMOVED AND REPLACED THE BULB IN THE MAIN LANDING GEAR ANNUNCIATOR ASSY. AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000477 19980430 00477 CE 1998 4 30 MASA98024 1 19980209 A 3260 1003810061 SWITCH BEECH 1900 1900D 1154162 CE NLG OUT OF ADJUST A MASA B EMER. DESCENT P NO WARNING INDICATION AP APPROACH 1 SW 07 146ZV UE146 FLT 551 - ALM-ABQ - CREW REPORTED WITH THE LNDING GEAR HANDLE IN DOWN POSITION, PILOT COULD NOT GET NOSE GREEN DOWN AND LOCKED INDICATION. RED GEAR HANDLE LIGHT WAS ILLUMINATED, BUT THERE WAS NO AUDIBLE WARNING. PILOT HAND PUMPED GEAR BUT DID NOT RECEIVE A GREEN LIGHT. CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED TH E NOSE UPLOCK SWITCH AND PERFORMED A GEAR RETRACTION. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000478 19980430 00478 CE 1998 4 30 MASA98021 1 19980206 A 1100 1293800061 PLACARD BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR OUT OF POSITION A MASA K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 SW 07 220YV UE220 FLT 7685 - MTJ-DEN - CREW REPORTED THAT THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN AND THE LOCK MECHANISM WAS BINDING. T HE PUSH BUTTON WAS RUBBING AGAINST THE INSIDE DOOR PLACARD. MAINTENANCE REPOSITIONED THE PLACARD. OPS CHECKED GOOD. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000479 19980430 00479 NM 1998 4 30 MASA98009 1 19980114 A 5210 85210127051 CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR OUT OF ADJ A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 436YV 436 FLT 7573 - GCC-SHR- AIRCRAFT LANDED IN SHR AND THE CREW HAD TROUBLE OPENING THE AIRSTAIR DOOR. MAINTENANCE LUBED CABLES AND PULLEYS. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000480 19980430 00480 NM 1998 4 30 MASA98011 1 19980120 A 5210 85210181101 CABLE DHAV DHC8 DHC8202 2809007 NM PAX DOOR WORN A MASA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 07 436YV 436 FLT 7561 - SHR-DEN - UPON ARRIVAL IN DEN, THE AIRSTAIR DOOR WOULD NOT OPEN DUE TO THE CABLE BINDING. MAINTENANCE REMOVE D AND REPLACED THE DOOR CABLE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000481 19980430 00481 CE 1998 4 30 MASA98027 1 19980211 A 3260 1003810061 DOWNLOCK SWITCH BEECH 1900 1900D 1154162 CE NLG FAILED A MASA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SW 07 146ZV UE146 FLT 407 - ROW-ABQ - ON APPROACH TO ABQ WITH GEAR SELECTED DOWN, PILOT DID NOT HAVE GREEN NOSE INDICATION AND RED HANDLE WAS STILL ILLUMINATED. CREW DECLARED EMERGENCY, PERFORMED FLYBY OF TOWER TO VERIFY GEAR WAS DOWN, AND LANDED WITHOUT IN CIDENT. MAINTENANCE REMOVED AND REPLACED NOSE DOWNLOCK SWITCH. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000482 19980430 00482 WP 1998 4 30 ORJA9819 1 19980206 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 ROWS 18-21 EMERGENCY LIGHTS RIGHT SIDE ON CONTINUOUSLY. REMOVED AND REPLACED RIGHT AFT EXIT ROW IDENTIFIER BATTERY PACK PER MM CH 25-00-01, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998043000483 19980430 00483 WP 1998 4 30 ORJA9817 1 19980205 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 SEVERAL EMERGENCY EXIT ROW LIGHTS ILLUMINATED IN FLIGHT. REMOVED AND REPLACED RIGHT AFT EMERGENCY EXIT ROWS BATTERY PAC K, OPS NORMAL OF EMERGENCY LIGHT SYSTEM. (M) 2 L 7 2 4F RT A6WE 1998043000484 19980430 00484 WP 1998 4 30 ORJA9818 1 19980205 A 3350 EM1267 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS SEAT ROWS 21-24 INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998043000485 19980430 00485 WP 1998 4 30 ORJA9814 1 19980128 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 873RA 53093 EMPENNAGE CAT WALK EMERGENCY LIGHTS 33A INOP. FOUND POWER PACK BATTERY DEFECTIVE RELAMPED BOTH, OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1998043000486 19980430 00486 WP 1998 4 30 ORJA9816 1 19980130 A 3397 00105606003 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 EMERGENCY LIGHT INOP AT ROW 1. REMOVED AND REPLACED ASSY AT ROW 1, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998043000487 19980430 00487 EU 1998 4 30 WTAA980029 1 19980208 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3101 1500215 EU CABIN DISCHARGED A WTAA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 17 403UE 743 SFO - EMERGENCY EXIT LIGHTS REPORTED INOPERATIONAL. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CH ECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998043000488 19980430 00488 EU 1998 4 30 WTAA980027 1 19980207 A 2612 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU LT/RT SYSTEM DIRTY A WTAA D RETURN TO BLOCK L NO TEST NR NOT REPORTED 1 WP 17 402UE 734 LAX - LEFT AND RIGHT FIRE DETECTION SYSTEM ACTIVATED ON TAXI. AIRCRAFT RETURNED TO GATE. MAINTENANCE WAS UNABLE TO DUP LICATE REPORTED DISCREPANCY. SYSTEM OPERATIONAL CHECK NORMAL. CLEANED ELECTRICAL CONNECTIONS AS PRECAUTION. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998043000489 19980430 00489 CE 1998 4 30 98ZZZM292 1 19980123 A 5610 1143240206 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 847CA UE52 CO-PILOTS WINDSHIELD HEAT INOP OVER 2/3 OF WINDSHIELD. WINDSHIELD HEATER FAILURE. REMOVED AND REPLACED CO-PILOTS WINDS HIELD. (M) 2 L 7 2 4T RT A24CE 1998043000490 19980430 00490 CE 1998 4 30 98ZZZM293 1 19980130 A 3251 114388018 ACTUATOR BEECH 1900 1900D 1154162 CE NLG STEERING BINDING A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 832CA 8181 DD0313 UE22 NOSE GEAR HARD TO CASTER. REPLACED POWER STEERING ACTUATOR. (M) 2 L 7 2 4T RT A24CE 1998043000491 19980430 00491 CE 1998 4 30 98ZZZM294 1 19980131 A 2620 1143200523 FIRE SWITCH BEECH 1900 1900D 1154162 CE COCKPIT STUCK A JJBA O OTHER J WARNING INDICATION IN INSP/MAINT 1 EA 01 836CA 9073 790 UE32 LT ENGINE FIRE EXTINGUISHER ANNUNCIATOR INOPERATIVE. REPLACED SWITCHED. (M) 2 L 7 2 4T RT A24CE 1998043000492 19980430 00492 CE 1998 4 30 98ZZZM295 1 19980129 A 3233 11438004113 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG LEAKING A JJBA O OTHER K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 EA 01 845CA 9825 0042A UE47 WHEN GEAR SELECTED DOWN, GEAR CIRCUIT BREAKER OPENED AND HYD PUMP CYCLED. RESET C/B, GEAR EXTENDED NORMALLY. REPLACED LEFT MAIN GEAR ACTUATOR. (M) 2 L 7 2 4T RT A24CE 1998043000493 19980430 00493 NM 1998 4 30 GAIA9820 1 19980216 A 5610 A1098206C WINDSHIELD BOEING 727 727223 1384074 NM RT COCKPIT CRACKED A GAIA B EMER. DESCENT O OTHER CR CRUISE 1 SW 07 6831 20184 FLT 718 - EN ROUTE TO BSM, CREW REPORTED R-1 WINDOW CRACKED. CREW DECLARED EMERGENCY AND DIVERTED TO DFW. AN UNEVENTFU L LANDING WAS MADE. DFW, REMOVED AND REPLACED R-1 WINDOW. REF B-727 MM 56-11-11. (M) 2 L 7 3 4F A3WE 1998043000494 19980430 00494 1998 4 30 GLBA98004 4 19980105 A 3497 WIRE BEECH 1900 1900D 1154162 CE RT COCKPIT CHAFED A GLBA O OTHER O OTHER CR CRUISE 1 CE 01 97UX UE97 CO-PILOT EADI BEGAN JUMPING AND FLICKERING. REPAIRED CHAFED WIRE IN AVIONICS BAY. (M) 2 L 7 2 4T RT A24CE 1998043000495 19980430 00495 CE 1998 4 30 GLBA98002 1 19980105 A 2910 1145800501 LINE BEECH 1900 1900D 1154162 CE HYD SYSTEM CRACKED A GLBA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 01 202ZK UE202 LOW HYDRO LIGHT WHEN GEAR CAME UP. BROKEN HYDRO LINE REPLACED. (M) 2 L 7 2 4T RT A24CE 1998043000496 19980430 00496 NM 1998 4 30 98ZZZM296 1 19980206 A 2130 PRESSURIZATION BOEING 727 727251 138408H NM CABIN MALFUNCTIONED A FX7A A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 19 266US 19985 FLT 758 - DURING CLIMB-OUT, LOST PRESSURIZATION, AFTER DUMPING FUEL RETURNED TO KMIA, LANDED WITHOUT INCIDENT. AIRCRAFT WAS INSPECTED FOR OPEN DOORS AND COMPARTMENTS, NONE FOUND, DOOR SEAL INSPECTED FOUND NORMAL. ACCOMPLISHED GROUND PRESS URIZATION CHECK, NORMAL, NO LEAKS FOUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998043000497 19980430 00497 WP 1998 4 30 98ZZZM297 1 19980212 A 5743 5611425501 TRUNNION DOUG DC8 DC851 3021920 WP LT MLG CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 508DC 63576 45935 MIA - DURING C-CHECK INSPECTION, FOUND LEFT MAIN GEAR TRUNNION CRACKED, REMOVED AND REPLACED LEFT GEAR TRUNNION PER DOUG LAS DC-8 MAIN GEAR FITTING REPLACEMENT GUIDE AND RECOVERY AND MOD SERVICE DEPARTMENT CI-735. (M) 2 L 7 4 4F 4A25 1998043000499 19980430 00499 NM 1998 4 30 MZZA98023 1 19980101 A 5330 SKIN BOEING 727 7272F9 138407D NM BS 1166 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 KUL - SEVERAL PREVIOUS CORROSION BELNDOUTS ON FUSELAGE SKIN FORWARD OF BS 1166 AND BETWEEN STRINGER 23L AND 25L FOUND BE YOND SRM ALLOWABLE LIMITS. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F RT A3WE 1998043000508 19980430 00508 NM 1998 4 30 MZZA98014 1 19980102 A 5315 651631526 FLOORBEAM BOEING 727 7272F9 138407D NM BS 328 CORROSION A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 KUL - FLOORBEAM AT STATION 328 AT LBL 30 HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-6. FOUND BEYOND LIMIT IAW ECRA 5310-03651. CARRY OUT REPAIR IAW SRM 53-10-8. (M) 2 L 7 3 4F RT A3WE 1998043000517 19980430 00517 EU 1998 4 30 C2XA98BT008 1 19980211 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 09 19812 99 EWR - FLT 3440 - ARRIVED NEWARK REPORTING THA MAIN CABIN DOOR AND CARGO DOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED BOTH THE MAIN CABIN DOOR AND CARGO DOOR EMERGENCY LIGHT BULBS, AND OPERATIONALLY CHECKED THE I TEMS GOOD. (M) 2 H 7 2 4T RT A53EU 1998043000518 19980430 00518 EU 1998 4 30 C2XA98BT007 1 19980211 A 3350 44 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST UK UNKNOWN 1 SW 09 42836 200 EWR - FLT 3685 - ARRIVED NEWARK, REPORTING THAT BOTH THE EMERGENCY LIGHT ON THE MAIN CABIN DOOR STEP AND THE EMERGENCY L IGHT FOR THE SERVICE DOOR WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE MAIN DOOR STEP BULB AND THE SERVICE DO OR EMERGENCY LIGHT BULB, AND OPERATIONALLY CHECKED THE SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998043000519 19980430 00519 NM 1998 4 30 USAASB98041 1 19980214 A 2433 1032575 TR UNIT BOEING 737 7372B7 1384560 NM E/E COMPT INOP A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 284AU 37539 23131 MCO - FLT 508, EN ROUTE FROM FLL TO PIT, THE NR 1 GEN SHOWED OVERLOAD WITH A HIGH AMP READING OF 90 AMPS. THE NR 2 GEN WAS 50 AMPS. WHEN THE CREW TRIED TO DOWNLOAD, THE NR 1 GENERATOR DROPPED OFF LINE ALONG WITH FOUR CIRCUIT BREAKERS IN S EQUENCE. NR 1 MAIN FUEL BOOST PUMP, OVERHEAD 5 VOLT, NR 1 TR AND THE EQUIPMENT COOLING BLOWER. AT THIS POINT NOTICED N R 2 GENERATOR HAD A HIGH TEMPERATURE. FLT DIVERTED TO MCO AND LANDED WITHOUT FURTHER INCIDENT. MX VERIFIED THE NR 1 GE NERATOR DRAWS A LOAD OF 85 AMPS AT HIGH POWER AND WITH THE APU GENERATOR ON LINE AMP LOAD IS NORMAL AT 55 AMPS. AFTER T /S, MX REMOVED AND REPLACED THE NR 1 TRU. OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998043000520 19980430 00520 NM 1998 4 30 USAA980069 1 19980214 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 345 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 42456 22198 CLT - DURING A CHECK VISUAL INSPECTION, FOUND A 217 INCH CORROSION ON FLOORBEAM UPPER CHORD FROM LBL 62 TO RBL 62 STATIO N 345. INSTALLED T-CAP PER REPAIR DOCUMENT SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1998043000521 19980430 00521 NM 1998 4 30 USAA980068 1 19980213 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM BS 365 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 42456 22198 CLT - DURING A VISUAL CHECK INSPECTION, FOUND A 61.24 INCH OF CORROSION ON THE FLOORBEAM UPPER CHORD AT STATION 365 FROM BL 0 TO RBL 45.5. INSTALLED T-CAP PER REPAIR DOCUMENT SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1998043000522 19980430 00522 NM 1998 4 30 USAA980067 1 19980213 A 5315 FLOORBEAM BOEING 757 757225 1384959 NM CABIN CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 42456 22198 CLT - DURING A VISUAL CHECK INSPECTION, FOUND A 126 INCH AREA OF CORROSION ON UPPER CHORD OF FLOORBEAM 377 FROM RBL 10 T O LBL 62. REPAIRED T-CAP PER REPAIR DOCUMENT SRM 53-00-51 AND EA 61271. (M) 2 L 7 2 4F RT A2NM 1998043000523 19980430 00523 NM 1998 4 30 USAA980066 1 19980213 A 5315 141N5150 FLOORBEAM BOEING 757 757225 1384959 NM BS 324 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 42456 22198 DURING A VISUAL CHECK INSPECTION, FOUND A 35 INCH AREA OF CORROSION ON FLOORBEAM UPPER CHORD AT STATION 324 FROM RBL 42 TO RBL 62. UPPER T-CAP REMOVED AND REPLACED BETWEEN LBL 6.0 TO RBL 70.0. REPAIR ANGLE INSTALLED PER EA 61274 AND SRM 5 1-70-12. (M) 2 L 7 2 4F RT A2NM 1998043000524 19980430 00524 NM 1998 4 30 USAA980065 1 19980217 A 5315 141N51131 FLOORBEAM BOEING 757 757225 1384959 NM BS 377.7 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 37365 22210 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 24 INCHES BY 1 INCH ON FLOORBEAM STATION 377.7 BL 0 TO LBL 24 UPPER FLANGE. REPAIR T-CAP PER REPAIR DOCUMENT SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1998043000525 19980430 00525 NM 1998 4 30 USAA980060 1 19980217 A 5315 141T511379 FLOORBEAM BOEING 767 767201 1385125 NM BS 325 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 647US 41917 23899 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A CORRODED AREA AT FLOORBEAM BOARD 1 INCH BY 78 INCHES TOP SURFACE BETWE EN STATION 325 RBL 24-RBL 54. REPAIR T-CAP PER REPAIR DOCUMENT SRM 53-00-51 AND EA 61283. (M) 2 L 7 2 4F RT A1NM 1998043000526 19980430 00526 NM 1998 4 30 USAA980061 1 19980217 A 5320 BAC1515553 CREASE BEAM BOEING 757 757225 1384959 NM BS 365-395 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 37365 22210 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND INTERCOSTAL CORROSION AT RBL 60 STATION 365-395 CREASE BEAM INNER CHORD. REPLACED ONE-THIRD CHORD PER REPAIR DOCUMENT SRM 53-10-51. (M) 2 L 7 2 4F RT A2NM 1998043000527 19980430 00527 NM 1998 4 30 USAA980062 1 19980217 A 5320 BAC1515553 SILL BOEING 757 757225 1384959 NM BS 395-418 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 22210 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION ON R1 DOOR LOWER SILL RBL 60 STATION 395-418. INSTALLED DOUBL ER, REPAIR ACCOMPLISHED ON JL 45-53500-023 PER REPAIR DOCUMENT SRM 53-10-51. (M) 2 L 7 2 4F RT A2NM 1998043000528 19980430 00528 WP 1998 4 30 USAAD98033 1 19980222 A 3244 3910063507 TIRE DOUG DC9 DC931 3022065 WP LT MLG BLOWN A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 929VJ 48118 IND - FL 277 - ON TAKEOFF THERE WAS A STRONG VIBRATION AND A LEFT GEAR RED UNSAFE LIGHT WITH THE GEAR STILL DOWN. THE G EAR WAS LEFT IN THE DOWN POSITION AND THE CAPTAIN VERIFIED THE GEAR WAS DOWN AND LOCKED. THE A/C RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MX REPLACED BOTH LEFT MAIN TIRES DUE TO THE LEFT MAIN INBOARD TIRE BEING FLAT AND THE CAP BLOWN OFF. THE LEFT MAIN LANDING GEAR DOWN SENSOR AND CONDUIT BRACKET WERE REPLACED. THE A/C WAS THEN FERRIED TO THE M AIN MAINTENANCE BASE FOR FLAP REPAIRS. (M) 2 L 7 2 4F A6WE 1998043000529 19980430 00529 NM 1998 4 30 USAA980063 1 19980217 A 5315 141N51111 FLOORBEAM BOEING 757 757225 1384959 NM BS 345 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 37365 22210 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 46 INCH BY 1 INCH CORROSION AREA ON FLOORBEAM STATION 345 BL 0 TO RBL 46 UPPER FLANGE. REPAIR T-CAP PER REPAIR DOCUMENT SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1998043000530 19980430 00530 NM 1998 4 30 USAA980064 1 19980217 A 5315 141N51121 FLOORBEAM BOEING 757 757225 1384959 NM BS 365 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 37365 22210 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 46 INCH BY 1 INCH CORROSION AREA ON FLOORBEAM STATION 365 BL 0 TO RBL 46 UPPER FLANGE. REPAIR T-CAP PER REPAIR DOCUMENT SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1998043000531 19980430 00531 WP 1998 4 30 USAA980080 1 19980220 A 5315 LONGERON DOUG DC9 DC981 3022081 WP BS 160 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 45819 48035 PIT - DURING Q-4/C-3 INSPECTION, FOUND .5 INCH CRACK AT STATION 160 LONGERON 4 LEFT. SPLICED IN NEW SECTION OF LONGERON AND REPLACED END FITTING PER SRM 53-02 FIG 18 SHEET 1-6. (M) 2 L 7 2 4F A6WE 1998043000532 19980430 00532 NM 1998 4 30 USAA980079 1 19980219 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373B7 1384580 NM CABIN CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 389US 37012 23311 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CORROSION AREA AROUND FASTENERS AND SCREW HOLES AT UPPER CHORD 328 FLOORBEAM. CORROSION TASK CARD NR C53-107-02. REPAIRED FLOORBEAM UPPER T-CAP SECTION BETWEEN LBL 32 AND RBL 36 PER TYPICAL REPAIR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998043000533 19980430 00533 NM 1998 4 30 USAA980054 1 19980107 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 230AU 48323 21975 ROA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK BS 727A PLUS 8 STRINGER 18L FUSELAGE SKIN. STOPPED DRILL ED CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998043000534 19980430 00534 WP 1998 4 30 USAAD98025 1 19980214 A 3231 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG DOORS MALFUNCTIONED A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 824US 49143 GSO - FLT 8001 - AFTER TAKEOFF AND GEAR RETRACTION THERE WAS A LOUD NOISE AND VIBRATION FROM THE FRONT OF THE AIRCRAFT. DURING RECYCLING OF THE GEAR, WHEN THE GEAR WAS DOWN THERE WAS NO VIBRATION, BUT WHEN THE WAS RETRACTED THE VIBRATION A ND NOISE RETURNED. GEAR INDICATION WAS NORMAL. THE AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE FOUND BOTH NOSE GEAR D OORS OPEN. THE DOORS WERE CLOSED AND SECURED. THE NOSE GEAR WAS THEN RETRACTED SEVERAL TIMES AND ALL OPERATIONS WERE N ORMAL. (M) 2 L 7 2 4F A6WE 1998043000535 19980430 00535 WP 1998 4 30 USAAD98028 1 19980218 A 3620 SRL92F INDICATOR DOUG DC9 DC931 3022065 WP FLT DECK FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 941VJ 47054 DCA - FLT 8011 - DURING TAKEOFF THE PNEUMATIC PRESSURE INDICATED 60 PSI. ON INITIAL REDUCTION OF POWER THE PRESSURE FOL LOWED THE THROTTLE. ON SUBSEQUENT POWER CHANGES THE SAME THING HAPPENED. AFTER RETURNING TO THE FIELD THE PNEUMATIC PR ESSURE INDICATED 6 TO 8 PSI WITH THE ENGINES SHUTDOWN AND NO PRESSURE IN THE SYSTEM. MAINTENANCE REPLACED THE PRESSURE INDICATOR AND THE APU LOAD CONTROL VALVE. (M) 2 L 7 2 4F A6WE 1998043000536 19980430 00536 WP 1998 4 30 98ZZZM298 1 19980218 A 3610 10947881 VALVE DOUG DC9 DC931 3022065 WP APU BYPASSING A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 941VJ 47054 DCA - FLT 8011 - DURING TAKEOFF THE PNEUMATIC PRESSURE INDICATED 60 PSI. ON INITIAL REDUCTION OF POWER THE PRESSURE FOL LOWED THE THROTTLE. ON SUBSEQUENT POWER CHANGES THE SAME THING HAPPENED. AFTER RETURNING TO THE FIELD THE PNEUMATIC PR ESSURE INDICATED 6 TO 8 PSI WITH THE ENGINES SHUTDOWN AND NO PRESSURE IN THE SYSTEM. MAINTENANCE REPLACED THE PRESSURE INDICATOR AND THE APU LOAD CONTROL VALVE. (M) 2 L 7 2 4F A6WE 1998043000537 19980430 00537 WP 1998 4 30 USAAD98029 1 19980219 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 981VJ 48157 CMH - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F A6WE 1998043000538 19980430 00538 WP 1998 4 30 USAAD98030 1 19980219 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 933VJ 47216 ROC - THE AFT CABIN CEILING MOUNTED EMERGENCY LIGHTS WERE INTERMITTENT. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998043000539 19980430 00539 EU 1998 4 30 USAAF98018 1 19980218 A 3230 DNLOCK PLUNGER FOKKER F28 F28MK0100 4990807 EU NLG LACK OF LUBE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 864US 11306 FLT 1672 - PIT-MDT - AFTER TAKEOFF FROM PIT, NOSE GEAR ALERT ILLUMINATED ON MFDU. THE BLUE INTRANSIT LIGHT REMAINED LIT IN GEAR HANDLE. CREW RECYCLED GEAR WITH SAME RESULT. CAPTAIN DECLARED AND EMERGENCY AND FLIGHT RETURNED TO PIT. FLIG HT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED, LUBRICATED AND RIGGED THE NOSE GEAR DOWN LOCK PLUNGER MECHANIS M. (M) 2 L 7 2 4F RT 1998043000540 19980430 00540 1998 4 30 USAAF98015 4 19980213 A 3418 2566A27 TRANSDUCER FOKKER F28 F28MK0100 4990807 EU LT FUSELAGE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 860US 11295 FLT 864 - PIT-DTW - AT ROTATION THE STICK SHAKER WARNING SYSTEM ACTIVATED ALONG WITH A STALL WARNING LIGHT. IT WAS TOO LATE FOR AN ABORTED TAKEOFF, SO CAPTAIN CONTINUED WITH A CLIMB-OUT FROM PIT. STICK SHAKER CONTINUED TO OPERATE. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. STICK SHAKER STOPPED AND STALL WARNING LIGHT EXTINGUISHED UPON LA NDING. MAINTENANCE REPLACED THE LEFT ANGLE OF ATTACK TRANSDUCER. (M) 2 L 7 2 4F RT 1998043000541 19980430 00541 NM 1998 4 30 USAASB98035 1 19980210 A 3020 655812310 ANTI-ICE DUCT BOEING 737 737201 1384454 NM NR 2 ENGINE LEAKING A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 236US 22352 TPA - FLT 1874 - THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMB-OUT APPROXIMATELY 25 MILES NORTH OF TPA. CREW FOLLOWED EMERGENCY PROCEDURES FOR OVERHEAT PROBLEM. WHEN THRUST LEVER WAS BROUGHT TO IDLE, THE LIGHT WENT OUT. FLIGHT RETURNED TO FIELD AT TPA WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. THE NR 2 ENGINE WAS NOT SHUT DOWN IN FLI GHT. MAINTENANCE FOUND A LEAK IN THE NR 2 ENGINE NOSE COWL ANTI-ICE DUCT. REPLACED DUCT. OPS CHECK AND LEAK CHECK GOO D. (M) 2 L 7 2 4F A16WE 1998043000542 19980430 00542 NM 1998 4 30 USAASB98043 1 19980217 A 3350 S106 BATTERY BOEING 737 737201 1384454 NM COCKPIT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 227AU 21816 ALB - MAINTENANCE FOUND THE COCKPIT EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES. OPS CH ECK GOOD. (M) 2 L 7 2 4F A16WE 1998043000543 19980430 00543 WP 1998 4 30 USAAD98027 1 19980218 A 3350 LIGHTING DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 930VJ 45868 CMH - AFT CABIN AND TAILCONE CATWALK FLOOR PATH LIGHTING INOP. MAINTENANCE FOUND ONE CATWALK SOCKET WITH MOISTURE CONTA MINATION FROM THE LEFT WATER SEPARATOR UNION DRIPPING. DRIED AND CLEARED AREA AND REPLACED SOCKET. (M) 2 L 7 2 4F A6WE 1998043000544 19980430 00544 WP 1998 4 30 USAAD98026 1 19980210 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 973VJ 47099 PIT - FLOOR PATH LIGHTING INOPERATIVE FROM ROW 16 TO TAILCONE CATWALK. MAINTENANCE REPLACED FUSE IN THE FLOOR PATH BATT ERY PACK. (M) 2 L 7 2 4F A6WE 1998043000545 19980430 00545 EU 1998 4 30 USAAF98017 1 19980217 A 2934 QTY TRANSMITTER FOKKER F28 F28MK1000 4990808 EU NR 1 HYD SYSTEM MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 868US 11313 PIT - CAPTAIN ADVISED VIA ACARS THE THE NR 1 HYD QTY WAS LOW AND LOST NOSE WHEEL STEERING. AN EMERGENCY WAS DECLARED AN D THE A/C LANDED WITHOUT FURTHER INCIDENT. THE A/C WAS CHECKED, NO LEAKS WERE NOTED. SERVICED HYD NR 1 AND NR 2 SYSTEM . FOUND NR 1 HYDRO QTY TRANSMITTER CAUSING ERRATIC INDICATION. MAINTENANCE CLEANED THE ELECTRICAL CONNECTOR ON THE NR 1 HYDRAULIC SYSTEM QTY TRANSMITTER. (M) 2 L 7 2 4F RT A20EU 1998043000546 19980430 00546 EU 1998 4 30 USAAF98016 1 19980217 A 5230 HANDLE FOKKER F28 F28MK0100 4990807 EU CARGO DOOR LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 857US 11289 CLE - FLT 598 - ON CLIMB-OUT OF CLE, CAPTAIN RECEIVED A MID CABIN DOOR WARNING LIGHT. FLIGHT RETURNED TO CLE WHERE LAND ING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND MID CARGO HANDLE OPEN. CLOSED HANDLE. WARNING LIGHTS OPS NORMAL. (M) 2 L 7 2 4F RT 1998043000547 19980430 00547 EU 1998 4 30 REXA98045 1 19980204 A 7603 CONDITION LEVER SAAB SF340 340B 7860101 EU LT ENGINE OUT OF ADJUST A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 370PX 340B300 LEFT PROP RPM BELOW 1000, AND TORQUE VERY SLOW TO RISE ON TAKEOFF ROLL. RERIGGED LEFT CONDITION LEVER AT SECTOR PULLEY. GROUND RUN AND CTOT CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1998043000548 19980430 00548 EU 1998 4 30 REXA98046 1 19980208 A 3297 WIRE BAG JETSTM JETSTM3101 1500215 EU LT MLG OPEN A REXA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 317PX 688 LEFT MAIN GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION. RE-BUTT SPLICED UPLOCK SWITCH WIRES ON LEFT MAIN LAND ING GEAR. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998043000549 19980430 00549 EU 1998 4 30 REXA98047 1 19980210 A 2613 TAILPIPE SAAB SF340 SF340A 7850100 EU RT ENGINE DIRTY A REXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 407BH 340A078 RIGHT ENGINE TAIL PIPE HOT LIGHT ON IN FLIGHT. REMOVED RIGHT TAILPIPE ASSY. INSPECTED, CLEANED, AND SEALED CONNECTORS. REINSTALED GROUND RUN CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1998043000550 19980430 00550 EU 1998 4 30 REXA98048 1 19980210 A 3020 ND00752200 THERMAL CONTROL SAAB SF340 SF340A 7850100 EU RT FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 111PX L242088 340A024 RIGHT INTAKE LIGHT COMES ON 5 SECONDS AFTER SWITCHED ON IN FLIGHT. REMOVED AND REPLACED RIGHT ENGINE INTAKE HEAT THERMA L CONTROLLER. (M) 2 L 7 2 4T RT A52EU 1998043000551 19980430 00551 EU 1998 4 30 REXA98049 1 19980210 A 3020 CONNECTOR SAAB SF340 SF340A 7850100 EU RIGHT DIRTY A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 325PX 340A051 RIGHT INTAKE OFF AND ON. CLEANED ALL INTAKE CANNON PLUGS. PERFORMED GROUND RUN. COULD NOT DUPLICATE DISC. (M) 2 L 7 2 4T RT A52EU 1998043000552 19980430 00552 EU 1998 4 30 REXA98050 1 19980211 A 3411 PITOT TUBE SAAB SF340 SF340A 7850100 EU LEFT DIRTY A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 326PX 340A054 CAPTAINS AIRSPEED INDICATOR READ 40 KNOTS ON TAKEOFF. CAPTAIN CLEARED LEFT PITOT TUBE AND STATIC PORT. (M) 2 L 7 2 4T RT A52EU 1998043000553 19980430 00553 EU 1998 4 30 REXA98051 1 19980212 A 3412 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU COCKPIT TRIPPED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 370PX 340B300 OUTSIDE AIR TEMP INOP. LIGHT CAME ON IN FLIGHT. RESET CIRCUIT BREAKER, NO FIX. PERFORMED GROUND RUNS AT HIGH POWER SE TTINGS FOR 15 MIN. COULD NOT DUPLICATE. (M) 2 L 7 2 4T RT A52EU 1998043000554 19980430 00554 EU 1998 4 30 REXA98052 1 19980211 A 3020 CONNECTOR SAAB SF340 340B 7860101 EU RT INTAKE DIRTY A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 360PX 340B220 RIGHT INTAKE LIGHT CYCLES ON AND OFF 10 - 20 SECONDS. CLEANED RT INTAKE HEAT CANNON PLUGS. GROUND RUN FOR 15 MINUTES. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998043000555 19980430 00555 WP 1998 4 30 REXA98053 2 19980210 A 7261 86504610 SCAVENGE PUMP BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE3311 01514 WP RIGHT INOP A REXA E ENGINE SHUTDOWN K P FLUID LOSS NO WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 332PX 702 P63081 OIL CAP LIGHT ACCOMPANIES BY NO OIL PRESSURE AND NO BETA LIGHT. REPLACED TURBINE SCAVENGE PUMP. (M) 2 L 7 2 4T 3 T RT A21EU E3WE 1998043000556 19980430 00556 NM 1998 4 30 MZZA98068 1 19980116 A 5343 651467639 FITTING BOEING 727 727212 138407G NM NLG CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PITTING CORROSION WAS FOUND ON NLG RT AND LT TRUNNING SUPPORT FITTING. THE CORRODED TRUNNION SUPPOR T FITTING WAS CLEANED UP AND BEARING HALVES REPLACED PER B727 SRM 53-40-1 FIGURE 2. (M) 2 L 7 3 4F A3WE 1998043000557 19980430 00557 NM 1998 4 30 MZZA9867 1 19980115 A 5240 65C199014 LATCH ASSY BOEING 727 727212 138407G NM R2 SERVICE DOOR BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, EXCESSIVE BROKEN WIRES WERE FOUND ON R2 SERVICE DOOR ESCAPE S LIDE LATCH CABLE. THE DAMAGED ESCAPE SLIDE LATCH ASSEMBLY WAS REMOVED AND REPLACED PER B727 MM 25-60-16. (M) 2 L 7 3 4F A3WE 1998043000558 19980430 00558 NM 1998 4 30 MZZA98066 1 19980115 A 3231 BACB10B131 ROLLER BOEING 727 727212 138407G NM LT/RT MLG DOOR FROZEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, ROLLERS FROZEN WERE FOUND ON RT AND LEFT MLG DOOR EMERGENCY M ANUAL RELEASE CRANK. THE DEFECTED ROLLERS WERE REMOVED AND REPLACED NEW ROLLERS PER BOEING SRM 20-50-03. (M) 2 L 7 3 4F A3WE 1998043000559 19980430 00559 NM 1998 4 30 MZZA98065 1 19980115 A 5753 SKIN BOEING 727 727212 138407G NM LT TE AFT FLAP DENT A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DENT WAS FOUND ON RT WING T/E INBOARD AFT FLAP UPPER SKIN AT WBL 123. THE DAMAGED SKIN 2 INCH DIAMETER WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998043000560 19980430 00560 NM 1998 4 30 MZZA98064 1 19980116 A 5754 RIB BOEING 727 727212 138407G NM NR 6 LE SLAT CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 2 SUB-STANDARD REPAIR WERE FOUND IN RT WING L/E NR 6 SLAT ACT UATOR OUTBOARD RIB. THE DAMAGED SLAT ACTUATOR OUTBOARD RIB WAS REMOVED AND REPLACED WITH NEW RIB PER B727 SRM 57-50-2 A ND 51-30-2. (M) 2 L 7 3 4F A3WE 1998043000561 19980430 00561 NM 1998 4 30 MZZA98063 1 19980113 A 5754 SKIN BOEING 727 727212 138407G NM NR 6 LE SLAT CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A SUB-STANDARD EXTERNAL REPAIR WAS FOUND ON RT WING NR 6 SLAT NOSE AREA AT SS 122. THE EXISTING EXTERNAL REPAIR WAS REMOVED AND REPLACED WITH NEW STANDARD EXTERNAL REPAIR PER B727 SRM 57-50-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 1998043000562 19980430 00562 NM 1998 4 30 MZZA98060 1 19980114 A 5321 FLOOR PANEL BOEING 727 727212 138407G NM BS 1136 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RT AFT LAVATORY FLOOR PANEL AT BS 1136, RBL 26. THE CORRODED FLOOR PANEL 3 INCH BY 4 INCH IN SIZE WAS CUTOUT AND INBOARD PARTITION LOWER SUPPORT CHANN EL WERE REPAIRED PER B727 SRM 53-20-2 AND 51-40-4 RESPECTIVELY. (M) 2 L 7 3 4F A3WE 1998043000563 19980430 00563 NM 1998 4 30 MZZA98059 1 19980114 A 5753 SKIN BOEING 727 727212 138407G NM LT TE FOREFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP LOW ER SKIN BETWEEN WBL 93 AND WBL 103. THE DAMAGED SKIN 10 INCH BY 8 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SR M 51-40-6. (M) 2 L 7 3 4F A3WE 1998043000564 19980430 00564 NM 1998 4 30 MZZA98058 1 19980114 A 5753 SKIN BOEING 727 727212 138407G NM LT TE FOREFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP T/E LOWER SKIN AT WBL 117. THE DAMAGED SKIN 10 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. ( M) 2 L 7 3 4F A3WE 1998043000565 19980430 00565 NM 1998 4 30 MZZA98057 1 19980114 A 5753 SKIN BOEING 727 727212 138407G NM LT TE FOREFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP T/ E LOWER SKIN AT WBL 187. THE DAMAGED SKIN 9.5 INCHES BY 4 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-4 0-6. (M) 2 L 7 3 4F A3WE 1998043000566 19980430 00566 NM 1998 4 30 MZZA98056 1 19980114 A 5753 SKIN BOEING 727 727212 138407G NM LT TE FOREFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP UPP ER SKIN AT WBL 88 JUST ABOVE FLAP FRONT SPAR CAP. THE DAMAGED SKIN 2.5 INCH BY 1.5 INCH IN SIZE WAS TRIMMED OUT AND REP AIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998043000567 19980430 00567 NM 1998 4 30 MZZA98055 1 19980114 A 5753 SKIN BOEING 727 727227 1384078 NM LT TE FOREFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86426 21364 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP UPP ER SKIN AT WBL 164. THE DAMAGED SKIN 4 INCH BY 3 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998043000568 19980430 00568 NM 1998 4 30 MZZA98054 1 19980114 A 5753 SKIN BOEING 727 727212 138407G NM LT TE MIDFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING INBOARD T/E MIDFLAP T/E L OWER SKIN AT WBL 133. THE DAMAGED SKIN 5 INCH BY 4.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. ( M) 2 L 7 3 4F A3WE 1998043000569 19980430 00569 NM 1998 4 30 MZZA98061 1 19980115 A 5753 SKIN BOEING 727 727212 138407G NM LT TE AFTFLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION AND DENT WAS FOUND ON LEFT WING T/E INBOARD AFTFLAP UPPER SKIN AT WBL 90 AND WBL 94 RESPECTIVELY. THE DAMAGED SKIN 1.5 INCH DIAMETER AND 2.5 INCHES DIAMETER WERE TRIMMED OUT AND REPAIRED PER B727 RM 51-40-6. (M) 2 L 7 3 4F A3WE 1998043000570 19980430 00570 NM 1998 4 30 MZZA98053 1 19980114 A 5753 SKIN BOEING 727 727212 138407G NM LT TE MIDFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 86425 21459 TNN - DURING 'S' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING INBOARD T/E MIDFLAP T/E S KIN LOWER SURFACE AT WBL 181. THE DAMAGED SKIN 5.5 INCH BY 4.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 5 1-40-6. (M) 2 L 7 3 4F A3WE 1998043000571 19980430 00571 NM 1998 4 30 P2EA98023 1 19980131 A 5753 SUPPORT BOEING 737 737222 1384473 NM RT TE FLAP GOUGE A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 DURING INSPECTION, FOUND A GOUGE AT THE RIGHT WING OUTBOARD FLAP OUTBOARD TRACK GIMBLE SUPPORT. BLENDED OUT GOUGED AREA ON SUPPORT FITTING IAW BOEING TELEX NR C00-SJO-98-0063RR. (M) 2 L 7 2 4F A16WE 1998043000572 19980430 00572 NM 1998 4 30 P2EA98024 1 19980129 A 5320 SUPPORT BOEING 737 737222 1384473 NM VHF ANTENNA CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 DURING MAINTENANCE FOUND A CRACK AT THE UPPER VHF ANTENNA SUPPORT BASE. REPAIRED IAW COOPESA EO-C00-3-53-047-98. (M) 2 L 7 2 4F A16WE 1998043000573 19980430 00573 NM 1998 4 30 P2EA98025 1 19980203 A 5330 SKIN BOEING 737 737244 138448U NM BS 890 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - DURING C-CHECK, FOUND UPPER FUSELAGE DENTED SKIN SECTION OUT OF LIMITS AT BS 890 BELOW STRINGER 21R. REPAIRED DAM AGED SECTION IAW SRM 53-30-3 FIG 5. (M) 2 L 7 2 4F A16WE 1998043000574 19980430 00574 NM 1998 4 30 P2EA98027 1 19980204 A 5311 FRAME BOEING 737 737244 138448U NM BS 1040 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - DURING C-CHECK, FOUND TAIL COMPARTMENT STATION 1040, STRINGER 8R, FRAME HAS CRACKS. REPAIRED FRAME AT STATION 104 0, BETWEEN STRINGE 8 AND 10 RT, PER SRM 53-10-4, FIG 4. (M) 2 L 7 2 4F A16WE 1998043000575 19980430 00575 NM 1998 4 30 P2EA98028 1 19980203 A 5312 RIB BOEING 737 737244 138448U NM WS 695 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - DURING C-CHECK, FOUND RT W/W AT STATION 695, W/L 196, RIB WITH OUTBOARD CHORD CRACKED. REPAIRED OUTBOARD CHORD PE R SRM 51-40-3. FIG1. (M) 2 L 7 2 4F A16WE 1998043000576 19980430 00576 NM 1998 4 30 P2EA98029 1 19980205 A 5330 SKIN BOEING 737 737244 138448U NM BS 397 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - DURING C-CHECK, UPPER FUSELAGE DENTED SKIN SECTION OUT OF LIMITS AT STATION 397, BETWEEN STRINGERS 2 AND 3 LEFT. R EPAIRED DAMAGED SECTION PER SRM 53-30-3, FIG 7. (M) 2 L 7 2 4F A16WE 1998043000577 19980430 00577 NM 1998 4 30 P2EA98030 1 19980203 A 5330 SKIN BOEING 737 737244 138448U NM BS 434 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - DURING C-CHECK ITEM, UPPER FUSELAGE, DENTED SKIN SECTION OUT OF LIMITS AT BS 434 BETWEEN STRINGERS 1 AND 2L. REPA IRED DAMAGED SECTION IAW SRM 53-30-3 FIG 5. (M) 2 L 7 2 4F A16WE 1998043000578 19980430 00578 NM 1998 4 30 P2EA98031 1 19980203 A 5751 SKIN BOEING 737 737244 138448U NM RT AILERON DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - DURING C-CHECK, RT AILERON UPPER AND LOWER SURFACES DELAMINATED AT SEVERAL PLACES. REPAIRED PER SRM 51-40-6, FIG 11. AILERON BALANCED PER SRM 51-80-1. AILERON REMOVED AND INSTALLED PER MM 27-11-11. (M) 2 L 7 2 4F A16WE 1998043000579 19980430 00579 NM 1998 4 30 P2EA98032 1 19980203 A 5542 SKIN BOEING 737 737244 138448U NM RUDDER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - DURING C-CHECK, FOUND RUDDER UPPER AFT TRAILING EDGE DELAMINATED. REPAIRED PER SRM 51-40-6, FIG 2, BALANCE OK PER SRM 51-80-1, POINT 2, FIG 8. (M) 2 L 7 2 4F A16WE 1998043000580 19980430 00580 NM 1998 4 30 P2EA98033 1 19980218 A 3230 SENSOR BOEING 737 737297 1384480 NM RT MLG OUT OF ADJUST A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 5WM 22629 FLT 421 - DFW - AIR RETURN NO EMERGENCY DECLARED LANDING UNEVENTFUL. LANDING GEAR WOULD NOT RETRACT NORMALLY. ADJUSTED AIR SAFETY SENSOR, RT MLG, PER MM 32-09-200. PERFORMED GEAR SWING PER MM 7-11-11. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998043000581 19980430 00581 NM 1998 4 30 NOCA0598 1 19980213 A 3350 767 LAMP BOEING 757 75728A 1384976 NM CABIN FAILED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE AT DOOR R4. RELAMPED EXTERIOR EMERGENCY LIGHT AT DOOR R4. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 1998043000582 19980430 00582 NM 1998 4 30 MASA98026 1 19980211 A 3350 GE1619 LAMP DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 436YV 436 FLT 7529 - DRO-DEN - UPON ARRIVAL IN DEN, CREW NOTICED LEFT FORWARD EMERGENCY EXIT LIGHT INOP. MAINTENANCE RESET LAMP, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000583 19980430 00583 1998 4 30 98ZZZM299 4 19980205 A 6122 311849601 GOVERNOR BEECH 1900 1900D 1154162 CE RT ENGINE MALFUNCTIONED A JJBA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 01 857CA 10021833 UE71 TAKEOFF ABORTED, RIGHT PROP BEGAN TO FEATHER DURING APPLICATION OF T/O POWER. REPLACED GOVERNOR. (M) 2 L 7 2 4T RT A24CE 1998043000584 19980430 00584 CE 1998 4 30 98ZZZM300 1 19980206 A 2752 1295210501 ACTUATOR BEECH 1900 1900D 1154162 CE TE FLAP BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 861CA UE164 FLAP SYSTEM INOPERATIVE. LEFT INBOARD FLAP ACTUATOR BROKEN. (M) 2 L 7 2 4T RT A24CE 1998043000585 19980430 00585 NM 1998 4 30 GAIA9821 1 19980220 A 2133 OUTFLOW VALVE BOEING 727 727223 1384074 NM CABIN DIRTY A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 854AA 20995 AFTER DEPARTING OKC, CREW REPORTED AIRCRAFT DEPRESSURIZATION AT FL 260. NO DOOR INDICATIONS. CREW WAS UNABLE TO CONTRO L CABIN IN MANUAL OR AUTO. INSPECTED OUTFLOW VALVES. REMOVED DEBRIS. CLEANED OUTFLOW VALVES, REINSTALLED AND FUNCTION ALLY TESTED. PRESSURIZATION SYSTEMS LEAK AND FUNCTIONALLY TESTED GOOD. (M) 2 L 7 3 4F A3WE 1998043000586 19980430 00586 WP 1998 4 30 98ZZZM301 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 428 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998043000587 19980430 00587 WP 1998 4 30 98ZZZM302 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 516 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998043000588 19980430 00588 WP 1998 4 30 98ZZZM303 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 602 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998043000589 19980430 00589 WP 1998 4 30 98ZZZM304 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 634 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998043000590 19980430 00590 WP 1998 4 30 98ZZZM305 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 695 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 695 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998043000591 19980430 00591 WP 1998 4 30 98ZZZM306 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 517 LBL 22. (M) 2 L 7 2 4F A6WE 1998043000592 19980430 00592 WP 1998 4 30 98ZZZM307 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 568 LBL 22. (M) 2 L 7 2 4F A6WE 1998043000593 19980430 00593 WP 1998 4 30 98ZZZM308 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 585 LBL 22. (M) 2 L 7 2 4F A6WE 1998043000594 19980430 00594 WP 1998 4 30 98ZZZM309 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 680 LBL 22. (M) 2 L 7 2 4F A6WE 1998043000595 19980430 00595 WP 1998 4 30 98ZZZM310 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS. (M) 2 L 7 2 4F A6WE 1998043000596 19980430 00596 WP 1998 4 30 98ZZZM311 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 764 LBL 22. (M) 2 L 7 2 4F A6WE 1998043000597 19980430 00597 WP 1998 4 30 98ZZZM312 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSLAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 519 RBL 22. (M) 2 L 7 2 4F A6WE 1998043000598 19980430 00598 WP 1998 4 30 98ZZZM313 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 674 RBL 22. (M) 2 L 7 2 4F A6WE 1998043000599 19980430 00599 WP 1998 4 30 98ZZZM314 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 675 RBL 22. (M) 2 L 7 2 4F A6WE 1998043000601 19980430 00601 WP 1998 4 30 98ZZZM316 1 19980209 A 5347 4924374 TRACK DOUG DC9 DC915F 3022037 WP BS 694 MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 604 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998043000602 19980430 00602 WP 1998 4 30 GAIA9817 1 19980211 A 5241 99115793 BEAM DOUG DC9 DC915F 3022037 WP BS 178 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 563PC 50014 47055 DURING INSPECTION FOR AD 81-10-10 A 1 INCH CRACK WAS FOUND ON THE NR 1 BEAM IN THE UPPER FORWARD CORNER OF THE FORWARD G ALLEY SERVICE DOOR. THE BEAM WAS REPAIRED IAW THE DOUGLAS SRM CHAPTER 52 FIG 25. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998043000603 19980430 00603 WP 1998 4 30 GTIA9800020 1 19980204 A 2560 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR FELL OFF A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 17535 47111 MAIN CABIN DOOR SLIDE PACK FELL OFF. REINSTALLED MAIN CABIN DOOR SLIDE IAW DC-9 MM 25-62-0, INSTALLATION CHECKS GOOD. R II ACCOMPLISHED. (M) 2 L 7 2 4F A6WE 1998043000604 19980430 00604 WP 1998 4 30 GTIA9800022 1 19980212 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 DTW - FLT 417 - ONE OF THE TWO COCKPIT EMERGENCY LIGHTS IS INOP. REMOVED AND REPLACED LAMPS AS REQUIRED IAW DC-9 MM. ( M) 2 L 7 2 4F A6WE 1998043000605 19980430 00605 NM 1998 4 30 F3LA98005 1 19980223 A 2450 915F2132 BUS PROTECT PNL BOEING 737 737301 1384611 NM COCKPIT FAILED A F3LA A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 578US 23257 SFO-DEN - FLIGHT CREW REPORTED SMOKE IN COCKPIT COMING FROM FIRST OFFICERS ELECTRICAL PANEL. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO SLC. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED GENERATOR CONTROL UNIT AND BU S PROTECTION PANEL AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1998043000606 19980430 00606 NM 1998 4 30 98ZZZM317 1 19980223 A 2424 915F2125 GCU BOEING 737 737301 1384611 NM COCKPIT FAILED A F3LA A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 578US 23257 SFO-DEN - FLIGHT CREW REPORTED SMOKE IN COCKPIT COMING FROM FIRST OFFICERS ELECTRICAL PANEL. AN EMERGENCY WAS DECLARED AND AIRCRAFT WAS DIVERTED TO SLC. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED GENERATOR CONTROL UNIT AND BU S PROTECTION PANEL AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1998043000607 19980430 00607 WP 1998 4 30 98ZZZM318 1 19980220 A 3210 5778946 BOGIE BEAM DOUG DC8 DC8F54 3021926 WP LT MLG CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 44UA 45800 ON TRANSIT CHECK, FOUND FORWARD SWIVEL BOGIE BEAM CRACKED AT LOWER SWIVEL PIN AFT LUG REF S/B32-182. REMOVED AND REPLAC ED BOGIE BEAM. 2 L 7 4 4F 4A25 1998043000608 19980430 00608 SO 1998 4 30 C2XA98IA016 1 19980427 A 3350 30043221 LIGHT EMB 120 EMB120RT SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16724 120171 IAH - FLT 3798 - PILOT REPORTED THAT THE FORWARD LEFT AND AFT RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIV E. MAINTENANCE REPLACED THE BULBS AND RELEASED THE AIRCRAFT. THE DISCREPANCY REPEATED ON FLIGHT 210B, CLL 1-7-99 WHERE MAINTENANCE PLACED THE LIGHTING SYSTEM ON MEL. THE MEL WAS CLEARED ON 1-11-99, FLIGHT 3481, WHEN MAINTENANCE REMOVED A ND REPLACED THE RIGHT AFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998043000609 19980430 00609 CE 1998 4 30 C2XA98IA017 1 19980427 A 3350 MDA5 FUSE BEECH 1900 1900D 1154162 CE PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17534 UE141 IAH - FLT 3659 - PILOT REPORTED THAT ALL EMERGENCY/COURTESY LIGHTS ON THE MAIN PASSENGER DOOR WERE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE EMERGENCY LIGHT FUSE LOCATED IN THE MAIN BATTERY BOX. THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000610 19980430 00610 EU 1998 4 30 C2XA98IA018 1 19980427 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14451 512 IAH - FLT 3440 - PILOT REPORTED THAT THE EMERGENCY LIGHT POWER SUPPLY WAS BAD. MAINTENANCE REMOVED AND REPLACED THE EME RGENCY LIGHT POWER SUPPLY BATTERY AT 43WL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998043000611 19980430 00611 EU 1998 4 30 C2XA98IA019 1 19980211 A 5312 S53572801207 BULKHEAD AEROSP ATR42 ATR42500 EU RT MLG WW CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING C-CHECK INSPECTION, THE MAIN LANDING GEAR WHEEL WELL AFT BULKHEAD WAS FOUND TO BE CRACKED. MAINTENANCE STO P DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR OVER THE AFFECTED AREA IAW ATR42-500 SRM 51-70-00, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998043000612 19980430 00612 EU 1998 4 30 C2XA98IA020 1 19980211 A 5210 S5217661200200 HANDLE AEROSP ATR42 ATR42500 EU PAX DOOR OUT OF ADJUST A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR FAILED THE FUNCTIONAL CHECK OF DOOR HANDLE OPEN/CLOSE FORCE. MAINTE NANCE CLEANED AND ADJUSTED THE PASSENGERS DOOR EXTERNAL HANDLE IAW ATR42-500 MM CH52-11-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998043000613 19980430 00613 EU 1998 4 30 C2XA98IA021 1 19980211 A 3350 3012701 LIGHT AEROSP ATR42 ATR42500 EU PAX DOOR INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT ON THE PASSENGER DOOR STEP STRUCTURE WAS FOUND TO BE INOPERATIVE. M AINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998043000614 19980430 00614 CE 1998 4 30 C2XA98CL013 1 19980217 A 3233 11238002223 ACTUATOR BEECH 1900 1900D 1154162 CE NLG FAILED A C2XA K NONE O OTHER AP APPROACH 1 SW 09 81538 UE199 CLE - FLT 3280 - CREW REPORTED THE NOSE GEAR LIGHT BARELY ILLUMINATES IN THE AIR BUT COMES TO FULL BRIGHTENSS ON THE GRO UND. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE NOSE GEAR ACTUATOR IAW B1900D MM 32-30-14. OPERA TIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000615 19980430 00615 NM 1998 4 30 AWXA9800068 1 19980217 A 2120 AIR DISTRIBUTION BOEING 737 737277 1384570 NM CABIN SMOKE A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 183AW 22650 SMOKE IN THE CABIN, RETURNED TO AIRPORT. CHECKED PACKS RAN A/C, RECIRC FAN, EYEBALL VENTS, COULD NOT DUPLICATE. 2 L 7 2 4F RT A16WE 1998043000617 19980430 00617 EU 1998 4 30 AWXA9800071 1 19980225 A 3232 MS172271 KEY WASHER AIRBUS 320 A320231 3930325 EU GEAR DOOR ACT MISSING A AWXA A UNSCHED LANDING J O WARNING INDICATION OTHER CL CLIMB 1 WP 28 636AW 098 AFTER GEAR RETRACTION, UNUSUAL NOISE HEARD, ECAM DISPLAYED LANDING GEAR DOOR UNLOCKED, LGCIU 1 AND 2 FAIL. GRAVITY EXTE NDED GEAR SUCCESFULLY, UNEVENTFUL LANDING KLAS. EMERGENCY WAS DECLARED. REPLACED ALL MISSING HARDWARE, INCLUDING KEY W ASHER. 2 L 7 2 4F RT A28NM 1998043000618 19980430 00618 WP 1998 4 30 CALA9800409 1 19980310 A 3260 DNLOCK SWITCH DOUG DC9 DC932 3022066 WP LT MLG INOPERATIVE A CALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 09 12538 47218 WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH, THE LEFT MLG GREEN LIGHT DID NOT ILLUMINATE. THE GEAR WAS CYCLED SEVERA L TIMES, BUT THE LIGHT DID NOT COME ON. THE EMERGENCY GEAR EXTENSION HANDLE WAS PULLED BUT THE LEVER WAS JAMMED. THE L EFT MLG GREEN LIGHT FINALLY CAME ON. A TOWER FLY-BY WAS PERFORMED AND THE GEAR WAS VISUALLY CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LT MLG DOWNLOCK SWITCH IAW MM 32-60-1. THE GEAR WAS SW UNG AND ALL INDICATIONS WERE GOOD. OPERATION OF THE ALTERNATE EXTENSION CONTROL LEVER WAS CHECKED IAW MM 32-31-2 AND OP ERATION CHECKED GOOD WITH THE GEAR EXTENDING AND LOCKING INTO POSITION. 2 L 7 2 4F A6WE 1998043000619 19980430 00619 NM 1998 4 30 UPS98226075 1 19980309 A 5751 CASTING BOEING 727 72731C 1384011 NM RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 926UP 19233 INSPECTION TYPE-C, CRACK ON RIGHT HAND AILERON LOCKOUT CASTING. CASTING REPLACED IAW DRAWING 65-21779 AND SRS ENGINEERI NG ORDER 98-0 6-005. 2 L 7 3 4F A3WE 1998043000620 19980430 00620 WP 1998 4 30 UPS98826057 1 19980224 A 5744 56422051 FITTING DOUG DC8 DC871F 302199D WP WS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, LT WING T/E, THE LWR REAR SPAR TO AUX SPAR TIE FITTING AT THE STA 98 FLAP HINGE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-3-0 AND DWG 5642205. 2 L 7 4 4F RT 4A25 1998043000621 19980430 00621 WP 1998 4 30 UPS98826058 1 19980225 A 5320 CUSP DOUG DC8 DC871F 302199D WP BS 240-260 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, FS 240 TO 260 RT CUSP UPPER SURFACE HAS SEVERE CORROSION. REPAIRED IAW SRM 53-2-5. 2 L 7 4 4F RT 4A25 1998043000622 19980430 00622 WP 1998 4 30 UPS98826059 1 19980131 A 5720 36445462 FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, FWD OF ACCESS 560-B, 30 FT INBD OF XW408 CRACKED IN STRINGER END FITTING. REMOVED CRACKED FITTING, D RILLED NEW FITTING IAW DC8 SRM 51-3-2 AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000623 19980430 00623 WP 1998 4 30 UPS98826060 1 19980202 A 5751 WEB DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, RT I/B AILERON, O/B END WEB CRACKED (CLOSURE RIB). REMOVED CLOSURE RIB, FABBED REPAIR DOUBLER FOR IT AND INSTALLED IAW REO 0429A REVA, DC8-SRM 51-1-8 AND DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998043000624 19980430 00624 WP 1998 4 30 UPS98826061 1 19980301 A 5320 3755843501N FITTING DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, BATHTUB FITTING IS CRACKED AT FS 1200 BETWEEN STR 34R AND 35R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000625 19980430 00625 WP 1998 4 30 UPS98826062 1 19980226 A 5320 37048412 FITTING DOUG DC8 DC871F 302199D WP LT WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, 505-E XRS 74.9. STRINGER 51 END FITTING HAS ELONGATED HOLE THROUGH FITTING'S WING SKIN. INSTALLED BU SHING IAW DC8-SRM 51-1-25 AND REO 04389. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED NEW FITTING IAW 51-1-20D, DC8 SRM 51-1-11 AND DC8 SRM 51-3-0 AND REO-04389. 2 L 7 4 4F RT 4A25 1998043000626 19980430 00626 WP 1998 4 30 UPS98826063 1 19980127 A 5220 BRACKET DOUG DC8 DC871F 302199D WP EMER EXIT DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LT AFT OVERWING EXIT DOOR HAS 2 CRACK IN WINDOW FRAME TEE AT FWD LWR CORNER. REMOVED CRACKED BRACKET AND INSTALLED NEW ONE IAW DC8 SRM 51-1-2- AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000627 19980430 00627 WP 1998 4 30 UPS98826064 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 575 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, CABIN SEAT TRACK H GOUGED AND CRACKED AT STA 575. REMOVED DAMAGE OUT IAW DC8 SRM 53-2-3. ALODINED A ND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PLUG AT STA 575 SEAT TRACK H IAW DC8- SRM 51-30. 2 L 7 4 4F RT 4A25 1998043000628 19980430 00628 WP 1998 4 30 UPS98826065 1 19980127 A 5230 FITTING DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, PIT DOOR CLOSE OUT FITTING CRACKED AT FS 1420 BL 0. REMOVED DOOR BARRIER CLOSE OUT. FABRICATED DOUB LER IAW DC8 SRM 53-2- 0. ALODINED AND PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-8, 51-1-20. FABRICATED FITTING IAW 5616673. ALODINED/PRIMED AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-20. INSTALLED CLOSEOUT IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998043000629 19980430 00629 WP 1998 4 30 UPS98826066 1 19980121 A 5320 ANGLE DOUG DC8 DC871F 302199D WP FWD FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LT RAIN REMOVAL PLENUM HAS 1 CRACK ON SUPPORT ANGLE (I/B SIDE OF CHAMBER). FABBED, INSTALLED REPAIR ANGLE IAW REO04273. 2 L 7 4 4F RT 4A25 1998043000630 19980430 00630 WP 1998 4 30 UPS98826067 1 19980122 A 5230 DOUBLER DOUG DC8 DC871F 302199D WP CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LT SIDE FUSELAGE, FWD LT CORNER OF MAIN CARGO DOOR, REPAIR DOUBLER DAMAGED. BLENDED OUT DAMAGED EDGE OF LOWER SKIN IAW SRM 53-2-0 FIG 1F SHT 3 PG 2P. REPAIRED PER REO04323 REV B BY INSTALLING DOUBLER. 2 L 7 4 4F RT 4A25 1998043000631 19980430 00631 WP 1998 4 30 UPS98826068 1 19980301 A 5320 564932949 DOUBLER DOUG DC8 DC871F 302199D WP BS 1766 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, LWR INTERNAL DOUBLER CORRODED FS 1766 LBL 3. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER I AW SRM 51-1-21 AND DWG 5649329. 2 L 7 4 4F RT 4A25 1998043000632 19980430 00632 WP 1998 4 30 UPS98826069 1 19980124 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, LWR FWD CARGO COMPT STN 300.00, LONG 33L AND 32L CORRODED BATH TUB FITTING. REMOVED OLD FITTING IAW DC8 SRM 51-1-20D. RECEIVED NEW PART 3755822- 505. LOCATED AND DRILLED NEW PART IAW DC8 SRM 51-3-2. REMOVED CORROSION, ALODINED AND PRIMED IAW DC8 SRMK 51-1-8. INSTALLED IAW SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1998043000633 19980430 00633 WP 1998 4 30 UPS98826070 1 19980127 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP CARGO COMPT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 703UP 45939 INSPECTION TYPE-C, UPPER CARGO SEAT TRACK (LOWER SIDE) CORRODED AT STA 1400, RBL 60. REMOVED SEAT TRACK FS 1370 TO 1430 IAW SRM 53-4-1. DRILLED UP NEW TRACK AND SPLICES IAW DC8 SRM 53-4-1 AND 53-2-3. ALODINED AND PRIMED AS REQUIRED IAW D C8 SRM 51-1-8. INSTALLED NEW TRACK IAW 51-3-0 AND 51-1-17. 2 L 7 4 4F RT 4A25 1998043000634 19980430 00634 WP 1998 4 30 UPS98826071 1 19980304 A 5320 3755841501 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, SHEAR TIE CRACKED FS 1200 STR 33R TO 34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000635 19980430 00635 WP 1998 4 30 UPS98826072 1 19980223 A 5712 576953053 RIB DOUG DC8 DC871F 302199D WP WS 360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, LT WING L/E LWR RIB AT STA XFS 360.25 IS CRACKED AT AFT DOUBLER FSTR HOLE. REMOVED, FABRICATED AND I NSTALLED REPLACEMENT RIB IAW SRM 51-1-21 AND DWG 5769530. 2 L 7 4 4F RT 4A25 1998043000636 19980430 00636 WP 1998 4 30 UPS98826073 1 19980302 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, AFT PIT FS 1520 SHEAR TIE BETWEEN LONGERONS 31L TO 32L LEFT SIDE IS CRACKED. REPAIRED IAW SRM 53-2-0 . 2 L 7 4 4F RT 4A25 1998043000637 19980430 00637 NM 1998 4 30 DL73S980537 1 19980309 A 5320 INTERCOSTAL BOEING 737 737232 1384475 NM BS 337 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 330DL 23102 DURING INSPECTION PER SI 3-55852-12, THE R1 DOOR AFT FRAME INTERCOSTALS BETWEEN FS 332 AND 344 WERE FOUND CRACKED AT 3 L OCATIONS S8A, 10A, AND 11A. REPAIRED PER ERA 331432-14AD. 2 L 7 2 4F RT A16WE 1998043000638 19980430 00638 NM 1998 4 30 DL73S980538 1 19980309 A 5330 6545768279280 SKIN BOEING 737 737232 1384475 NM BS 489 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 330DL 23102 SEVERAL GOUGES AND NICKS WERE FOUND IN THE EDGE OF THE SKIN O THE AFT SIDE OF THE C1 DOOR CUTOUT AT APPROX FS 489, BETWE EN S21R AND S23R. REPAIRED PER ERA 331462-14. 2 L 7 2 4F RT A16WE 1998043000639 19980430 00639 NM 1998 4 30 DLM88980540 1 19980309 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 987DL 53338 FS 1418 CRACKED AT L2L AND L2R AT THE TYP LOCATIONS. REPAIRED PER ERA 331436-14. 2 L 7 2 4F RT A6WE 1998043000640 19980430 00640 NM 1998 4 30 DL72S980541 1 19980309 A 5320 6516350 STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 A CRACK WAS FOUND IN THE RBL 36.83 VERT STIFFENER ON THE FWD SIDE FO THE FS 1183 BLKHD. THE CRACK WAS LOCATED AT APPROX WL 238 AND WAS APPROX 2. REPAIRED PER ERA 331448-14AD. 2 L 7 3 4F A3WE 1998043000641 19980430 00641 WP 1998 4 30 DLL10980542 1 19980309 A 5343 FITTING LKHEED 1011 10113851 5265010 WP BS 449 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 DURING RTN INSPECTION OF THE FS 449 BLKHD, TYP DAMAGE WAS FOUND TO THE RT NLG TRUNNION FITTING. THE FITTING HAD A CRACK IN THE INBD FLANGE. THIS CRACK IS TYP PER SB 093-53-233. THIS AC WAS PREVIOUSLY REPAIRED USING THE 1642622-101/-102 P REVENATIVE MOD PER SAME SB. REPAIRED PER ERA 331464 14AD. 2 L 7 3 4F A23WE 1998043000643 19980430 00643 WP 1998 4 30 DLL10980544 1 19980309 A 5330 SKIN LKHEED 1011 10113851 5265010 WP PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1731D 193C1200 A TYP CRACK WAS FOUND AT THE UPPER AFT CORNER OF THE R1 DOOR PASSENGER DOOR. REPAIRED PER ERA 331475-14. 2 L 7 3 4F A23WE 1998043000644 19980430 00644 NM 1998 4 30 DL72E980545 1 19980309 A 5330 SKIN BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 EXISTING REPAIR AT L1 DOOR LWR HINGE WAS INSTALLED PER B727 MM 53-30-00. REPAIR PER ERA 304060-14, REV B. 2 L 7 3 4F A3WE 1998043000645 19980430 00645 NM 1998 4 30 DL72S980546 1 19980309 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 523DA 21583 ON L/O, FOUND LEFT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED BATT PACK, OPS CK NML. 2 L 7 3 4F A3WE 1998043000646 19980430 00646 WP 1998 4 30 DLL10980549 1 19980306 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 328 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 719DA 193C1135 THE SKIN AT FS 328 AND LBL 22 WAS FOUND CORRODED NEAR THE CORNER OF THE NOSE LANDING GEAR DOOR CUTOUT. THE EXISTING AD MANDATED MOD DOUBLERS WERE ALSO FOUND CORRODED. THE SKIN WAS TRIMMED AWAY TO REMOVE THE CORROSION AND THE MOD DOUBLERS WERE REMADE TO ENCOMPASS THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 364164-14AD, REV A. 2 L 7 3 4F A23WE 1998043000647 19980430 00647 NM 1998 4 30 DL72W980550 1 19980307 A 5313 65564228 STRINGER BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 THE FUSELAGE STRINGER AND SKIN AT S-29R WERE FOUND BADLY CORRODED BETWEEN FS 720A+10 AND 720C+10. THE SKIN DAMAGE WAS C UTOUT AND A DOUBLER AND TRIPLER INSTALLED. THE DAMAGED AREA OF STIFFENER WAS REMOVED AND A NEW SECTION SPLICED IN. THE REPAIR WAS ACCOMPLISHED PER ER/A 364137-14, REV A. 2 L 7 3 4F A3WE 1998043000648 19980430 00648 WP 1998 4 30 DHL98801002 1 19980308 A 2697 WIRE DOUG DC8 DC873F 302199F WP NR 1 ENGINE CHAFED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 801DH 46033 NR 1 FIRE BELL SOUNDED INTERMITTENTLY, FIRE HANDLE GLARESHIELD LIGHT AND FIRE BELL ILLUMINATED AND SOUNDED WITH B-LOOP S ELECTED. FIRE BELL AND FIRE WARNING CANCELLED BY ITSELF AND NR 1 ENG SHORT CIRCUIT LIGHT ILLUMINATED TWICE. DEFERRED PER MEL 26-2-3. FOUND AND REPAIRED WIRE W5124A16, CHAFED AT 1 O'CLOCK POSITION FAN CASE. OPS CHECK GOOD PER MM 26-10-0 . 2 L 7 4 4F RT 4A25 1998043000649 19980430 00649 NM 1998 4 30 P5CA9800454 1 19980302 A 5400 BRACKET BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACKED INBOARD AND OUTBOARD SUPPORT BRACKETS ON NR 4 PYLON LOWER FIREWALL RIB. REPLACED SUPPORT BRACKETS PER BAC SRM 5 1-30-02. 2 L 7 4 4F A20WE 1998043000650 19980430 00650 NM 1998 4 30 P5CA9800455 1 19980302 A 5753 FAIRING BOEING 747 747122 1384872 NM LT TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DELAMINATION ON LEFT OUTBOARD FLAP OUTBOARD HINGE FAIRING PANEL. REPAIRED PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000651 19980430 00651 NM 1998 4 30 P5CA9800456 1 19980302 A 5532 PANEL BOEING 747 747122 1384872 NM VERT STAB DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DEBONDING AND EROSION ON PREVIOUS REPAIR ON RIGHT EXTERIOR PANEL ON VERTICAL STABLIZER. REPAIRED PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000652 19980430 00652 NM 1998 4 30 P5CA9800457 1 19980303 A 5414 DOOR SKIN BOEING 747 747122 1384872 NM NR 2 PYLON PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 HOLE IN LEFT HYDRAULIC SERVICE DOOR (SAILBOAT) ON NR 2 PYLON. REPAIRED PER BAC SRM 51-40-06. 2 L 7 4 4F A20WE 1998043000653 19980430 00653 NM 1998 4 30 P5CA9800458 1 19980303 A 5414 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACKED SKIN ON NR 2 PYLON ADJACENT TO PANEL 463EL. REPAIRED PER BAC SRM 54-30-03. 2 L 7 4 4F A20WE 1998043000654 19980430 00654 NM 1998 4 30 P5CA9800459 1 19980303 A 5400 ANGLE BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 CRACK ON LEADING EDGE UPPER HORIZONTAL WEB INBOARD ATTACH ANGLE. REPAIRED PER BAC SRM 51-30-03. 2 L 7 4 4F A20WE 1998043000655 19980430 00655 NM 1998 4 30 P5CA9800460 1 19980303 A 5330 PANEL BOEING 747 747122 1384872 NM BS 1054 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 TWO CRACKS ON UPPER SURFACE OF PANEL 191A AT BS 1054. REPAIRED PER BAC SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000656 19980430 00656 NM 1998 4 30 P5CA9800461 1 19980303 A 5330 PANEL BOEING 747 747122 1384872 NM BS 1012 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DELAMINATION ON FUSELAGE PANEL 192HR AT BS 11012, BL 9. REPAIRED PER BAC SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000657 19980430 00657 NM 1998 4 30 P5CA9800462 1 19980303 A 5330 PANEL BOEING 747 747122 1384872 NM BS 1240 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEVEL 1 CORROSION UNDER HINGE PANELS ON FUSELAGE PANEL 192A AT BS 1240. REMOVED CORROSION AND TREATED PER BAC SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F A20WE 1998043000658 19980430 00658 NM 1998 4 30 P5CA9800463 1 19980303 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1260 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 DAMAGED FUSELAGE SKIN PANEL IN RIGHT WING GEAR WHEEL WELL AT BS 1260. REPAIRED DAMAGE AND REPLACED FASTENERS PER BAC SR M 53-30-02 AND 53-30-03. 2 L 7 4 4F A20WE 1998043000659 19980430 00659 NM 1998 4 30 P5CA9800464 1 19980307 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT WING T/E O/B OR I/B AFT FLAP DELAMINATED I/B OF O/B TRACK. REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000660 19980430 00660 NM 1998 4 30 P5CA9800465 1 19980307 A 5350 FAIRING BOEING 747 747122 1384872 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT FUSELAGE LWR FAIRING FWD OF W/GEAR W/W DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000661 19980430 00661 NM 1998 4 30 P5CA9800466 1 19980307 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT WING T/E FLAP O/B AFT FLAP DELAMINATED. REPAIRED PER MM 27-51-00. 2 L 7 4 4F A20WE 1998043000662 19980430 00662 NM 1998 4 30 P5CA9800467 1 19980308 A 5330 PANEL BOEING 747 747122 1384872 NM BS 1000 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE BS 1000 PANEL 191AL AND SKIN ON INSIDE DELAMINATED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000663 19980430 00663 NM 1998 4 30 P5CA9800468 1 19980308 A 5330 PANEL BOEING 747 747122 1384872 NM BS 1000 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE BS 1000 PANEL 191AR FORWARD CORNER DAMAGED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000664 19980430 00664 NM 1998 4 30 P5CA9800469 1 19980307 A 5330 TRIM STRIP BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE PANEL 191ER TRIM STRIP CRACKED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000665 19980430 00665 NM 1998 4 30 P5CA9800470 1 19980307 A 5320 BRACKET BOEING 747 747122 1384872 NM AC DOORWAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 AIR CONDITIONING DOORS LOWER FUSELAGE LATCH BRACKET CORRODED. REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998043000666 19980430 00666 NM 1998 4 30 P5CA9800471 1 19980308 A 5330 SKIN BOEING 747 747122 1384872 NM RT MLG WW CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT BODY GEAR CUT OUT WEB FOR OLEO STRUT CLOSURE SKIN CRACKED ON I/B SIDE. REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998043000667 19980430 00667 NM 1998 4 30 P5CA9800472 1 19980307 A 5320 CLIP BOEING 747 747122 1384872 NM RT MLG WW CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RIGHT BODY GEAR WHEEL WELL CRACKED ANGLE CLIP. REPLACED ANGLE CLIP PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998043000668 19980430 00668 NM 1998 4 30 P5CA9800473 1 19980307 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 R/WING AFT FLAP LOWER SKIN L/E DELAMINATED. REPAIRED DELAMINATION BY REMOVING DELAM, POTTING CORE AND PUTTING ON FIBERG LASS OVERLAYS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000669 19980430 00669 NM 1998 4 30 P5CA9800474 1 19980310 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE FOREFLAP DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT WING T/E OUTBD FOREFLAP LEADING EDGE DENTED O/B OF O/B LINK. REMOVED DAMAGE PLYS, REMOVED CORD AND REPLACED. FABRIC ATED FIBERGLASS FILLER AND OVERLAYS AND BONDED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000670 19980430 00670 NM 1998 4 30 P5CA9800475 1 19980307 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE PANEL 191NL INBD CORNER CRACKED. FOUND PAINT BUILDUP TO BE CRACKED. SANDED AND INSP AREA NO CRACK FOUND IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000671 19980430 00671 NM 1998 4 30 P5CA9800476 1 19980307 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 PANEL 192MR DELAMINATED AND WITH A HOLE. PANEL REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000672 19980430 00672 NM 1998 4 30 P5CA9800477 1 19980307 A 5245 HINGE BOEING 747 747122 1384872 NM AC BAY DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 A/C PANEL 192HR LOWER FUSELAGE HINGE CORRODED. REMOVED LIGHT SURFACE CORROSION FROM A/C BAY DOOR IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998043000673 19980430 00673 NM 1998 4 30 P5CA9800478 1 19980307 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE LOWER PANEL 191A 2 CRACKS IN UPPER SURFACE. REPAIRED DAMAGED PANEL IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000674 19980430 00674 NM 1998 4 30 P5CA9800479 1 19980307 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LOWER FUSELAGE AIR COND PANEL 192A CRACKED ON PREVIOUS REPAIR ON UPPER SURFACE. FOUND AND REMOVED OIL AND WATER. CUT O UT DAMAGED AREA AND REPLACED DAMAGED FIBERGLAS IAW 51-40-15. 2 L 7 4 4F A20WE 1998043000675 19980430 00675 NM 1998 4 30 P5CA9800480 1 19980307 A 5311 FRAME BOEING 747 747122 1384872 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 AIR CONDITIONING PANEL 191A CORRODED FRAME UNDERNEATH. REMOVED MINOR SURFACE CORROSION IAW 51-10-02. 2 L 7 4 4F A20WE 1998043000676 19980430 00676 NM 1998 4 30 P5CA9800481 1 19980307 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT WING INBD T/E UPPER SURFACE PANEL JUST FORWARD OF FLYING PANEL IS CRACKED. SANDED PANEL REMOVED DAMAGE SKIN, FABRICA TED REPAIR IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000677 19980430 00677 NM 1998 4 30 P5CA9800482 1 19980307 A 5320 STANCHIONS BOEING 747 747122 1384872 NM E/E COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 BS 460 RBL 55 LBL 55 E AND E COMPT STANCHIONS CRACKED AND BROKEN BY CANON PLUG ATTACHMENTS. INSTALLED NEW STANCHIONS IA W SRM 51-10-01. 2 L 7 4 4F A20WE 1998043000678 19980430 00678 NM 1998 4 30 P5CA9800483 1 19980307 A 5414 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON HOLE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 PYLON HYD DOOR LT INBOARD SKIN HAS HOLE. REPAIRED HOLE IN DOOR PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998043000679 19980430 00679 NM 1998 4 30 P5CA9800484 1 19980307 A 5330 SKIN BOEING 747 747122 1384872 NM BS 680 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FUSELAGE BS 680 WORKING FASTENERS BETWEEN CORNER LAP SEAMS. REPAIRED WORKING FASTENERS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998043000680 19980430 00680 NM 1998 4 30 P5CA9800485 1 19980307 A 5243 HYD DOOR BOEING 747 747122 1384872 NM NR 2 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 NR 2 PYLON LT HYDRAULIC DOOR CHAFED ON FWD INBOARD SKIN. REMOVED PRIMER FROM CHAFED AREA, FABRICATED DOUBLER THEN BONDE D DOUBLER TO REPAIR AREA IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998043000681 19980430 00681 NM 1998 4 30 P5CA9800486 1 19980307 A 5330 SKIN BOEING 747 747122 1384872 NM BS 640 WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 FUSELAGE FWD LOWER EXTERNAL SKIN BS 640 HAS LOOSE FASTENERS AT LOWER LAP SEAMS. REMOVED AND REPLACED FASTENERS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998043000682 19980430 00682 NM 1998 4 30 P5CA9800487 1 19980307 A 5245 BRACKET BOEING 747 747122 1384872 NM AC COMPT DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 PANEL 191A HOLD OPEN BRACKET CORRODED AND GOUGED. REPAIRED BRACKET PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998043000683 19980430 00683 NM 1998 4 30 P5CA9800489 1 19980307 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT WING FLYING PANEL PULLED FASTENERS. REMOVED AND REPLACED FASTENERS IAW SRM 51-30-02 AND 51-32-03. 2 L 7 4 4F A20WE 1998043000684 19980430 00684 NM 1998 4 30 P5CA9800490 1 19980310 A 5247 DOOR BOEING 747 747122 1384872 NM APU COMPT DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 APU BATTERY COMPARTMENT DOOR DAMAGED AT AFT CORNER ON AFT FLANGE. REPAIRED DAMAGE AT APU ACCESS DOOR IAW SRM 51-40-02, 51-30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1998043000685 19980430 00685 NM 1998 4 30 P5CA9800491 1 19980307 A 5730 SKIN BOEING 747 747122 1384872 NM WS 1196 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT WING T/E UPPER SKIN PANEL WS 1196 DELAMINATED ON BOTTOM SURFACE. FABRICATED FIBERGLASS FILLERS AND OVERLAYS AND BOND ED NEW REPAIR PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000686 19980430 00686 NM 1998 4 30 P5CA9800492 1 19980310 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 RT WING T/E INBD FOREFLAP LEADING EDGE SKIN DELAMINATED. SANDED DAMAGED AREA, SMOOTH AND REMOVED DELAMINATED AREA. APP LIED FILLER WITH FIBERGLASS OVERLAYS IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998043000687 19980430 00687 NM 1998 4 30 P5CA9800493 1 19980310 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT WING T/E INBD FLAP MIDFLAP DELAMINATED ON LEADING EDGE AREA. REPAIRED FLAP SKIN IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000688 19980430 00688 NM 1998 4 30 P5CA9800494 1 19980310 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT WING FLYING PANEL WBL 197 CRACKED BY FITTING. REMOVED AND REPLACED FLYING PANEL IAW 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998043000689 19980430 00689 NM 1998 4 30 P5CA9800495 1 19980310 A 5730 PANEL BOEING 747 747122 1384872 NM LT TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT WING T/E FLAP FIXED PANEL JUST INBOARD OF NR 1 PYLON DELAMINATED. REMOVED DAMAGE, APPLIED FILLERS AND DOUBLERS IAW S RM 51-40-09. 2 L 7 4 4F A20WE 1998043000690 19980430 00690 NM 1998 4 30 P5CA9800496 1 19980310 A 5753 FLAP BOEING 747 747122 1384872 NM LT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT WING OTBD T/E MIDFLAP HAS 3 FT CRACK ON TRAILING EDGE. PREPARED AREA OF REPAIR, INJECTED CORE ALONG CRACK AND APPLIE D FIBERGLASS LAYERS IAW 747 SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000691 19980430 00691 NM 1998 4 30 P5CA9800497 1 19980310 A 5753 FLAP BOEING 747 747122 1384872 NM LT TE MIDFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LT WING I/B T/E MIDFLAP LEADING EDGE DELAMINATED. REPAIRED DELAMINATED AREA BY CUTTING OUT DAMAGE, POTTING CORE AND APP LYING FIBERGLASS OVERLAYS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000692 19980430 00692 NM 1998 4 30 P5CA9800498 1 19980310 A 5522 SKIN BOEING 747 747122 1384872 NM LE ELEV CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 LEFT INBOARD ELEVATOR LOWER SKIN CRACKED. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000693 19980430 00693 NM 1998 4 30 P5CA9800499 1 19980310 A 3810 PANEL BOEING 747 747122 1384872 NM WATER SERVICE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 WATER SERVICE PANEL DELAMINATED. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000694 19980430 00694 NM 1998 4 30 P5CA9800500 1 19980310 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 PANEL 191H CRACKED AND DELAMINATED. REPAIRED PER BOEING SRM 51-40-09. 2 L 7 4 4F A20WE 1998043000695 19980430 00695 NM 1998 4 30 VNAA9803009 1 19980306 A 3241 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ANTI-SKID VALVE DIRTY A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 432JS 3045 A ANTI-SKID FAIL WARNING MESSAGE ILLUMINATED, ON THE TAXI OUT PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MA INTENANCE INSPECTED AND CLEANED THE ANTI-SKID VALVE CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-03. OPERATION CHECKS WERE SATISFACTORY. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998043000696 19980430 00696 NM 1998 4 30 CKSA98086 1 19980307 A 2697 WIRE BOEING 747 747269B NM PWA JT9 JT9D7J 52054 NE NR 2 ENGINE BROKEN A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 708CK 21543 685900 AFTER T/O, NR 2 ENGINE FIRE WARNING SOUNDED. FIRED BOTH BOTTLES, NACELLE TEMP REMAINED AT TOP OF SCALE A-LOOP (DMI'ED) INOP. INFLIGHT MECHANICS VIEWED NR 2 ENGINE AFTER FIRE WARNING AND OBSERVED NO ABNORMAL INDICATIONS. ENGINE SHUTDOWN B Y CREW ACCORDING TO QRH PROCEDURES. POST FLIGHT INSPECTION BY CREW REVEALED NO INDICATION OF FIRE OR OTHER ABNORMALITIE S TO NR 2 ENGINE. REPAIRED BROKEN WIRE CONNECTION AT LOOP 2 ENGINE B-LOOP, OPS CHECKED GOOD. REPLACED BOTH FIRE BOTTLE S WITH SERVICEABLE UNITS. TESTED SQUIB CIRCUITS AND REPLACED BOTH SQUIBS. RETURNED ACFT TO NORMAL IAW BMM 26-11-00 AND 26-00-00. 2 L 7 4 4F 4 F RT A20WE E20EA 1998043000697 19980430 00697 NM 1998 4 30 CKSA98087 1 19980308 A 3610 65B912641 DUCT BOEING 747 747269B NM PWA JT9 JT9D7J 52054 NE NR 2 ENGINE DAMAGED A CKSA O OTHER J WARNING INDICATION TO TAKEOFF 1 GL 23 708CK 21543 685900 NR 2 ENG FIRE WARNING SOUNDED ON TAKEOFF AND THRUST LEVER WAS RETARDED TO IDLE. WHEN THRUST LEVER WAS RETARDED, FIRE WA RNING CEASED. SHUT ENG NR 2 DOWN AS B-LOOP NACELLE TEMP HAD INCREASED NEAR BOTTOM OF RED ZONE AND A-LOOP STAYED NEAR BO TTOM OF YELLOW ZONE. TOTAL WINDMILLING TIME WAS :35 (MINUTES) WITH FIRE SWITCH IN. UPON 1ST NR 2 ENG INSPECTION, FOUND 15TH STAGE BLEED DUCT HAD FAILED. CLAMP FAILURE. REMOVED AND REPLACED AFFECTED DUCTS INCLUDING ADJACENT DUCTS THAT HA D SUSTAINED DAMAGE. PERFORMED LEAK CHECK DURING IDLE RUN, GOOD. HIGH STAGE VALVE OPS CHECK GOOD. RAN ENGINE TO T/O PW R SETTING (1.51 EPR AT 2 MIN) OPS NORMAL IAW BMM 75-32-15, 75-32-00 AND 71-00-00. 2 L 7 4 4F 4 F RT A20WE E20EA 1998043000720 19980430 00720 SO 1998 4 30 WTAA980035 1 19980219 A 3340 TAXI LIGHT EMB 120 EMB120RT SO NLG CRACKED A WTAA K NONE C F.O.D. TO TAKEOFF 1 WP 17 284UE 120145 SMF - BIRD STRIKE AT NOSE GEAR AREA ON TAKEOFF. NO ADVERSE INDICATIONS EN ROUTE TO SFO. MAINTENANCE INSPECTED AREA FOR DAMAGE. REPLACED CRACKED LEFT TAXI LIGHT. NO OTHER DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998043000721 19980430 00721 SO 1998 4 30 WTAA980034 1 19980218 A 3260 MS3470L106S CONNECTOR EMB 120 EMB120RT SO RT MLG FAILED A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 221YV 120221 SFO - LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED CANNON PLUG J0318 AT RIGHT LANDING GEAR FOR SQUAT SWITCH. PERFORMED GEAR SWING. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998043000722 19980430 00722 EU 1998 4 30 WTAA980038 1 19980224 A 3350 995918 LAMP BAG JETSTM JETSTM3101 1500215 EU COCKPIT INOPERATIVE A WTAA K NONE O OTHER AP APPROACH 1 WP 17 428UE 806 LAX - LEFT MAIN LANDING GEAR DOWN AND LOCK FAILED TO ILLUMINATE WHEN GEAR SELECTED DOWN. MAINTENANCE RELAMPED GEAR POSI TION INDICATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998043000723 19980430 00723 NM 1998 4 30 USAA980098 1 19980223 A 5711 SPAR WEB BOEING 737 737201 1384454 NM BS 200.5 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND CRACK .25 INCH LONG LT HORIZONTAL STABILIZER AT STATION 200.5 FRONT SPAR WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 55-10-5. (M) 2 L 7 2 4F A16WE 1998043000725 19980430 00725 NM 1998 4 30 USAA980095 1 19980223 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD UNDER RADAR DISH MOUNT, INBOARD SIDE OF RT LOWER HAT SECTION LEG. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11-1, SRM 53-10-11. (M) 2 L 7 2 4F A16WE 1998043000726 19980430 00726 NM 1998 4 30 USAA980094 1 19980223 A 5311 FRAME BOEING 737 737201 1384454 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND, .75 INCH CRACK STATION 616 FRAME INBOARD CHORD, LBL 62.5 WL 202 FRAME. F ABRICATED AND INSTALLED REPAIR ANGLE, REPAIRED PER EA 43552. (M) 2 L 7 2 4F A16WE 1998043000727 19980430 00727 NM 1998 4 30 USAA980093 1 19980223 A 5311 FRAME BOEING 737 737201 1384454 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 616 FRAME INBOARD CHORD RBL 62.5, WL 202 FRAME. F ABRICATED AND INSTALLED DOUBLER, REPAIRED PER EA 43551. (M) 2 L 7 2 4F A16WE 1998043000728 19980430 00728 NM 1998 4 30 USAA980092 1 19980223 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 664 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 3 INCHES STATION 664 BL 0 WL 207.5 TO WL 204 FLOORBEAM WEB. REMOV ED DAMAGED AREA INSTALLED WEB REPAIR, REPAIRED PER BOEING DRAWING 65-C34537. (M) 2 L 7 2 4F A16WE 1998043000729 19980430 00729 NM 1998 4 30 USAA980091 1 19980223 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 22796 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 727 LBL 25 INCH FLOORBEAM LOWER CHORD. REPLA CED SECTION OF LOWER CHORD, REPAIRED PER SRM 51-40-4. (M) 2 L 7 2 4F A16WE 1998043000730 19980430 00730 NM 1998 4 30 USAA980090 1 19980223 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 707-714 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 22796 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND SEVERAL .25 INCH CRACK LBL 25 LONGITUDINAL FLOORBEAM LOWER WEB STATION 70 7 TO STATION 714, WL 203.5. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-2, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998043000731 19980430 00731 NM 1998 4 30 USAA980089 1 19980223 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 707-714 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 707 TO STATION 714 RBL 25 LONG FLOORBEAM WEB. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998043000732 19980430 00732 NM 1998 4 30 USAA980087 1 19980223 A 5330 SKIN BOEING 737 737201 1384454 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION FOUND .5 INCH CRACK FORWARD ENTRY DOORWAY UPPER HINGE CUTOUT SKIN. CUTOUT CRAC K AND INSTALLED FILLER AND DOUBLER, REPAIRED PER SRM 51-10-1, SRM 53-30-3, AND EA 43555. (M) 2 L 7 2 4F A16WE 1998043000733 19980430 00733 NM 1998 4 30 USAA980086 1 19980223 A 5311 FRAME BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH AT STATION 328 STRINGER 20R FRAME. INSTALLED REPAIR DOUBL ER, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1998043000734 19980430 00734 NM 1998 4 30 USAA980085 1 19980223 A 5311 FRAME BOEING 737 737201 1384454 NM BS 947 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1.25 INCH LONG AFT ENTRANCE DOOR FRAME STATION 947 STRINGER 11L WE B (FRAME). INSTALLED DOUBLER ON EXISTING WEB, REPAIRED PR TR 53-30-07. (M) 2 L 7 2 4F A16WE 1998043000735 19980430 00735 NM 1998 4 30 USAA980084 1 19980223 A 5312 BLKHD STIFFENER BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BS 178 LBL 5.75 AT WL 183.5 STIFFENER, BULKHEAD. DOUBLER AND STIFFENERS INSTALLED, REPAIRED PER TR 53-10-17. (M) 2 L 7 2 4F A16WE 1998043000736 19980430 00736 NM 1998 4 30 USAA980083 1 19980223 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 178 BULKHEAD LBL 5, WL 199. INSTALLED DOUBLER RE PAIRED PER SRM 53-10-11. (M) 2 L 7 2 4F A16WE 1998043000737 19980430 00737 NM 1998 4 30 USAA980082 1 19980223 A 5314 KEEL BEAM BOEING 737 737201 1384454 NM BS 695-727 WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND WORN HOLES, HOLES ELONGATED IN CHORD .09375 INCH STATION 695 TO STATION 727 LOWER CHORD (KEEL BEAM). SPOT FACED SCREW HOLES, HFEC INSPECTION INSTALLED STRAP, REPAIRED PER EA 43618 SRM 51-30-6 . (M) 2 L 7 2 4F A16WE 1998043000738 19980430 00738 NM 1998 4 30 USAA980081 1 19980223 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40152 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AND .75 INCH CRACK BS 727 LEFT OUTBOARD CHORD STRINGER 18A L/S. CUTOUT AND SPLICED IN NEW SECTION OF STRINGER, REPAIRED EO 5394G068. (M) 2 L 7 2 4F A16WE 1998043000739 19980430 00739 NM 1998 4 30 USAA980078 1 19980219 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 660 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 660 LBL 24 FLOORBEAM. INSTALLED DOUBLER, REPAIRED PER E O 5791G632. (M) 2 L 7 2 4F A16WE 1998043000740 19980430 00740 NM 1998 4 30 USAA980077 1 19980219 A 5312 BULKHEAD SKIN BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2.5 INCH CRACK BS 178 BULKHEAD AT UPPER LEFT RADAR MOUNT BULKHEAD SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-10-11, FIG 1. (M) 2 L 7 2 4F A16WE 1998043000741 19980430 00741 NM 1998 4 30 USAA980076 1 19980219 A 5330 SKIN BOEING 737 737201 1384454 NM BS 963 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 963, STRINGER 17R SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 AND BOEING DRAWING 65C27287. (M) 2 L 7 2 4F A16WE 1998043000742 19980430 00742 NM 1998 4 30 USAA980075 1 19980219 A 5311 FRAME BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION FOUND 1.7 INCH CRACK IN WEB OF FRAME BS 328 BETWEEN S20R AND S21R WEB AREAS OF FRAME. INSTALLED DOUBLER OVER STOP DRILLED CRACKED AREA IN WEB, REPAIRED PER AIW SRM 51-40-2 AND BOEING PRING NR 65-458 12. (M) 2 L 7 2 4F A16WE 1998043000743 19980430 00743 NM 1998 4 30 USAA980074 1 19980219 A 5330 SKIN BOEING 737 737201 1384454 NM BS 328 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT STATION 328 ST RINGER 17 SKIN AND BARE STRAP. INSTALLED DOUBLERS PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998043000744 19980430 00744 NM 1998 4 30 USAA980073 1 19980219 A 5320 DRAG ANGLE BOEING 737 737201 1384454 NM BS 1090 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 1090 BETWEEN S2R AND S3L DRAG ANGLE. INSTALLED REPAIR S TRAP AND REPAIRED PER EA 43571. (M) 2 L 7 2 4F A16WE 1998043000745 19980430 00745 NM 1998 4 30 USAA980072 1 19980219 A 5240 SKIN BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK IN SKIN AT WINDOW FORWARD SERVICE DOOR. INSTALLED DOUBL ER, REPAIRED PER T/R 52-10-01 A. (M) 2 L 7 2 4F A16WE 1998043000746 19980430 00746 NM 1998 4 30 USAA980070 1 19980219 A 5320 FLANGE BOEING 737 737201 1384454 NM BS 727 STR 18A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK NDT INSPECTION, FOUND .25 INCH CRACK BS 727 STRINGER 18A LEFT OUTBOARD FORWARD FLANGE. INSTALLED REPAIR ANGLES, REPAIRED PER EO 5394G068. (M) 2 L 7 2 4F A16WE 1998043000747 19980430 00747 NM 1998 4 30 USAA980105 1 19980223 A 5330 SKIN BOEING 737 737201 1384454 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 259AU 39110 22806 INT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK ON EXTERNAL FUSELAGE SKIN AT FORWARD RT SERVICE DO OR LOWER HINGE CUTOUT FORWARD EDGE SKIN. REMOVED SECTION OF SKIN AND INSTALLED REPAIR DOUBLER. REPAIRED PER SB 737-53- 1074 FIG 3 AND SRM 53-30-3 FIG 32. (M) 2 L 7 2 4F A16WE 1998043000748 19980430 00748 NM 1998 4 30 USAA980102 1 19980223 A 5311 FRAME BOEING 737 737201 1384454 NM BS 286 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 259AU 39110 22806 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 3 INCH BY 4 INCH CORROSION BS 286, STRINGER 28L FRAME WEB. CUTOUT CORRO DED SECTION OF FRAME WEB AND INSTALLED NEW SECTION, REPAIRED PER SRM 51-40-02. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998043000749 19980430 00749 NM 1998 4 30 USAA980101 1 19980223 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 333 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 259AU 39110 22806 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK IN STRINGER, S18R BS 333. SPLICED STRINGER 65-45800-189, REPAIRED PER EA 43633. (M) 2 L 7 2 4F A16WE 1998043000750 19980430 00750 NM 1998 4 30 USAA980100 1 19980223 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1138 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 259AU 39110 22806 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK STRINGER 15 LT AT STATION 1138, STRINGER. REPLACED SECTI ON OF STRINGER AND SPLICED TOGETHER, REPAIRED PER SRM 53-10-7. (M) 2 L 7 2 4F A16WE 1998043000751 19980430 00751 NM 1998 4 30 USAA980059 1 19980213 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967-1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 279AU 39892 22891 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 40 INCH CORROSION BS 967 TO 1006 STRINGER 27L. REMOVED CORRO DED STRINGER AND INSTALLED STRINGER SPLICE, REPAIRED PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998043000752 19980430 00752 NM 1998 4 30 USAA980103 1 19980223 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 967/987 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 259AU 39110 22806 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 12 INCH SECTION OF CORROSION STRINGER 27L, BS 967 AND BS 987 S TRINGERS. CUTOUT STRINGER, FABRICATED REPAIR SECTIONS AND SPLICED AND INSTALLED ON A/C BS 947 PLUS 10 INCHES TO BS 1016 , REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998043000753 19980430 00753 NM 1998 4 30 USAA980071 1 19980219 A 5330 SKIN BOEING 737 737201 1384454 NM BS 764 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 223US 51546 21665 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 764 AT STRINGER 19L SKIN. INSTALLED DOUBLER, REPAIRED P ER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998043000754 19980430 00754 NM 1998 4 30 USAA980097 1 19980223 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCH LONG STATION 727 A STRINGER 18R SKIN. INSTALLED REPAIR DOU BLER, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998043000755 19980430 00755 NM 1998 4 30 USAA980099 1 19980223 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FUOND CRACK 2 INCHES LONG STATION 727A PLUS 4 INCH STRINGER 18R SKIN. INSTALL ED REPAIR DOUBLER, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998043000756 19980430 00756 NM 1998 4 30 USAA980104 1 19980223 A 5311 FRAME BOEING 737 737201 1384454 NM BS 787 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 259AU 39110 22806 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 6 INCH CORROSION BS 787 BETWEEN STRINGER 26R AND STRINGER 27R. CUTOUT CORRODED AREA AND INSTALLED REPAIR SKIN ATTACH ANGLE, REPAIRED PER SRM 53-10-4 FIG 7. CORROSION TASK NR C53-20 8-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998043000757 19980430 00757 NM 1998 4 30 USAA980088 1 19980223 A 5330 SKIN BOEING 737 737201 1384454 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK AFT ENTRY GALLEY DOOR UPPER HINGE CUT OUT SKIN EXTERIOR. CUT OUT CRACK AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998043000758 19980430 00758 NM 1998 4 30 USAA980106 1 19980226 A 5330 SKIN BOEING 737 7372B7 1384560 NM PAX DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 278AU 40163 22890 ROA - DURING 'CX-2' CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND .25 INCH CRACK FORWARD ENTRY DOOR CUT OUT LOWER HINGE CU T OUT FUSELAGE SKIN. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3, FIG 31. (M) 2 L 7 2 4F A16WE 1998043000759 19980430 00759 NM 1998 4 30 USAASB98042 1 19980202 A 3350 110049 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 507AU 23382 ORD - MAINTENANCE FOUND A SECTION OF LOW LEVEL EMERGENCY LIGHTS INOP IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPL ACED THE FORWARD BATTERY CHARGER ASSEMBLY FOR THE LOW LEVEL EMERGENCY LIGHTS. ALSO, REPLACED BROKEN LIGHT SOCKET (P/N 0 8169-1), AND LENS (P/N 07912) AT ROW 3. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998043000760 19980430 00760 NM 1998 4 30 USAASB98039 1 19980215 A 3350 AD20131A BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 411US 23880 EWR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS ON SEAT ROWS 20 THROUGH 24 AND THE AFT DOORS INOP. MAINTENANCE REMOVE D AND REPLACED THE AFT RIGHT BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998043000761 19980430 00761 NM 1998 4 30 USAASB98037 1 19980211 A 7931 697902E PRESS SWITCH BOEING 737 737201 1384454 NM NR 1 ENG CSD FAILED A USAA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 252AU 22758 CLT - FLT 764 - WHILE EN ROUTE TO CLT, THE NR 1 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED. CREW DISCONNECTED CSD PE R CHECKLIST AND DECLARED AN EMERGENCY. THE APU WAS ALREADY ON MEL, SO THE AIRCRAFT OPERATED ON ONE GENERATOR THE REMAIN DER OF THE FLIGHT TO CLT. THE FLIGHT WAS LOCATED 50 MILES NORTHWEST OF CLT WHEN THE INCIDENT OCCURRED. THE FLIGHT LAND ED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE CSD LOW OIL PRESSU RE SWITCH. PERFORMED ENGINE RUN. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998043000762 19980430 00762 NM 1998 4 30 USAASB98036 1 19980211 A 3260 189929 UPLOCK SENSOR BOEING 737 7372B7 1384560 NM LT MLG FAILED A USAA K NONE O OTHER CL CLIMB 1 EA 19 287AU 23134 ATL - FLT 1243 - AFTER TAKEOFF FROM PHL, THE LEFT MAIN LANDING GEAR TRANSIT LIGHT REMAINED ILLUMINATED. CREW CYCLED GEA R AND LIGHT WENT OUT, THEN IT FLICKERED FOR REMAINDER OF FLIGHT. FLIGHT LANDED IN ATL WITHOUT FURTHER INCIDENT. MAINTE NANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR UPLOCK SENSOR PER MM. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998043000763 19980430 00763 EU 1998 4 30 USAAF98020 1 19980221 A 3350 59257 INVERTER FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 854US 11282 PIT - FORWARD FLOOR PROXIMITY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED THE FLOOR PROXIMITY INVERTER. (M) 2 L 7 2 4F RT 1998043000764 19980430 00764 NM 1998 4 30 USAABB98020 1 19980219 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AU 22198 LAX - EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE REPLACED ALL OF THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998043000765 19980430 00765 NM 1998 4 30 USAAB98021 1 19980219 A 3350 873203193REV4 CONTROL MODULE BOEING 757 757225 1384959 NM CABIN INTERMITTENT A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AU 22198 LAX - AFT EMERGENCY LIGHT CONTROL MODULE INTERMITTENT. MAINTENANCE REPLACED THE MODULE. (M) 2 L 7 2 4F RT A2NM 1998043000766 19980430 00766 NM 1998 4 30 USAASB98047 1 19980224 A 3350 1011143 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 351US 23554 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EME RGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT S IGN, BATTERY PACK AND CHARGER ASSEMBLY FOR SEAT ROW 10ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998043000767 19980430 00767 NM 1998 4 30 98ZZZM319 1 19980224 A 3350 1012623 SIGN BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 351US 23554 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EME RGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT S IGN, BATTERY PACK AND CHARGER ASSEMBLY FOR SEAT ROW 10ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998043000768 19980430 00768 NM 1998 4 30 98ZZZM320 1 19980224 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 351US 23554 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EME RGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT S IGN, BATTERY PACK AND CHARGER ASSEMBLY FOR SEAT ROW 10ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998043000769 19980430 00769 NM 1998 4 30 98ZZZM321 1 19980224 A 3350 20121 CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 351US 23554 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER SEAT ROW 10ABC WOULD NOT ILLUMINATE DURING OPERATIONAL TEST OF EME RGENCY LIGHTS. MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT WAS SHORTED. REMOVED AND REPLACED THE LIGHT ASSEMBLY, EXIT S IGN, BATTERY PACK AND CHARGER ASSEMBLY FOR SEAT ROW 10ABC. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998043000770 19980430 00770 1998 4 30 USAASB98046 4 19980222 A 3425 7725005009 ADI BOEING 737 737401 1384701 NM COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 420US 19335 23987 CLT - FLT 1699 - SHORTLY AFTER TAKEOFF FROM CLT, THE FIRST OFFICERS ADI FLAG CAME INTO VIEW AND BECAME UNRELIABLE. THE DECISION WAS MADE TO RETURN TO FIELD AT CLT FOR MAINTENANCE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE FIRST OFFICERS ADI. OPERATIONAL CHECK AND FUNCTIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998043000771 19980430 00771 WP 1998 4 30 TWAA9803003 1 19980302 A 3397 WIRE DOUG DC9 DC934 302207E WP CABIN BROKEN A TWAA O OTHER O OTHER NR NOT REPORTED 1 CE 05 927L 48123 STL - FLT 433 - A BURNING SMELL WAS DETECTED IN REAR OF CABIN AT 300 FT AGL. REPAIRED BROKEN WIRE AT WIRE BUNDLE FOR LI GHTING BALLAST, ROW 19 RT SIDE. (M) 2 L 7 2 4F RT A6WE 1998043000772 19980430 00772 1998 4 30 TWAA9803002 4 19980302 A 2340 H200792 SWITCH DOUG DC9 DC982 3022082 WP COCKPIT LOOSE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 955U 49427 PBI - FLT 268 - DURING PREFLIGHT, WHEN PA BUTTON IN COCKPIT WAS PUSHED THE BUTTON ARCED AND SPARKED. SECURED LOOSE SWIT CH. (M) 2 L 7 2 4F A6WE 1998043000773 19980430 00773 WP 1998 4 30 TWAA9803001 1 19980226 A 2752 BRACE DOUG DC9 DC982 3022082 WP TE FLAP ACT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 916TW 49187 DURING C-CHECK, FOUND APPROX 2 INCH CRACK, OUTBOARD SIDE UPPER AFT CORNER OF X-BRACE. LOCATED INBOARD OF NR 2 FLAP ACTU ATOR. REPAIRED PER ARA 15061. (M) 2 L 7 2 4F A6WE 1998043000774 19980430 00774 NM 1998 4 30 TWAA9802907 1 19980301 A 3230 1U10851 SEQUENCE VALVE BOEING 727 727231 1384079 NM LT MLG RUPTURED A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 54329 20307 MCO - FLT 653 - AT GEAR RETRACTION THE 'A' HYD SYSTEM QTY AND PRESSURE DROPPED. BOTH ENGINE PUMPS WERE DEPRESSURIZED AN D FLIGHT RETURNED TO MCO. REPLACED THE LEFT MAIN LANDING GEAR LOCK SEQUENCE VALVE. (M) 2 L 7 3 4F A3WE 1998043000775 19980430 00775 EU 1998 4 30 SIMA980501 1 19980219 A 3246 50092361 WHEEL SAAB SF340 340B 7860101 EU NR 1 WHEEL BROKEN A SIMA K NONE O OTHER LD LANDING 1 SW 21 388AE DEC930937 340B388 DFW - FLT 3804 - NR 1 MAIN WHEEL, ONE-THIRD OF RIN BROKEN OFF, CAUSING THE TIRE TO LOOSE PRESSURE. RAI'D TIRE SHEEL ASS Y, RAI'D NR 2 TIRE WHEEL ASSY AS PRECAUTIONARY. PERFORMED VISUAL INSPECTION FOR EXTERIOR DAMAGE TO SKIN, NO DISCREPANCI ES NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998043000776 19980430 00776 EU 1998 4 30 SIMA980471 1 19980216 A 3350 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 414WF 414 DFW - FLT 3541 - AFT SECTION OF EMERGENCY FLOOR LIGHTING SYSTEM IN CABIN WILL NOT EXTINGUISH. REMOVED AND REPLACED BATT ERY PACK IAW JIC 33-51-71 SYSTEM TESTED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998043000777 19980430 00777 EU 1998 4 30 SIMA980502 1 19980219 A 3350 3012000 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 431AT 503 431 DFW - FLT 3716 - FORWARD CABIN EMERGENCY SIGNS INOP AND FLOOR PROX LIGHTING WILL NOT TURN OFF. RAI'D BATTERY PACK AT SE AT 1AB AND POWER SUPPLY FOR SIGNS AT SAME LOC. PERFORMED OPS CHECK SATISFACTORILY. AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998043000778 19980430 00778 EU 1998 4 30 98ZZZM322 1 19980219 A 3350 AQS1000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 431AT 11542 431 DFW - FLT 3716 - FORWARD CABIN EMERGENCY SIGNS INOP AND FLOOR PROX LIGHTING WILL NOT TURN OFF. RAI'D BATTERY PACK AT SE AT 1AB AND POWER SUPPLY FOR SIGNS AT SAME LOC. PERFORMED OPS CHECK SATISFACTORILY. AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998043000779 19980430 00779 EU 1998 4 30 SIMA980503 1 19980219 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AT 798 345 DFW - FLT 3504 - AFT EMERGENCY EXIT LIGHT WILL NOT TEST. RAI'D BATTERY PACK AT 62WL. OPS CHECK GOOD. AIRCRAFT WAS RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998043000780 19980430 00780 NM 1998 4 30 98ZZZM323 1 19980213 A 2612 1011B FIRE DETECTOR BOEING 727 72721 1384003 NM ENGINE MALFUNCTIONED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 356QS 19258 FLT 247 - SYR-DAY - HAD AN AIR TURNBACK TO SYR. FIRE WARNING WENT OFF DURING CLIMB, BELL BUT NO FIRE WARNING LIGHT. RE MOVED AND REPLACED ALL THREE ENGINE FIRE DETECTOR'S. (M) 2 L 7 3 4F A3WE 1998043000781 19980430 00781 NM 1998 4 30 98ZZZM324 1 19980214 A 2612 W19807918 FIRE WIRE BOEING 727 72721 1384003 NM NR 1 ENGINE BROKEN A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 356QS 19258 FLT 247 - SYR-DAY - HAD AN AIR TURNBACK TO SYR. ON CLIMB-OUT FROM SYR FIRE WARNING BELL SOUNDED WITH NO ASSOCIATED LIGH T. BELL WAS SILENCED BUT IMMEDIATELY WENT OF AGAIN. REPLACED WIRE HARNESS TO NR 1 ENGINE. (M) 2 L 7 3 4F A3WE 1998043000782 19980430 00782 NM 1998 4 30 98ZZZM325 1 19980220 A 3350 LIGHT BOEING 727 727222 1384073 NM CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 7635U 19908 DURING PREFLIGHT IN DAY, EMERGENCY EXIT LIGHT OVER FORWARD ENTRY INOPERATIVE. RESET EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 1998043000783 19980430 00783 NM 1998 4 30 98ZZZM326 1 19980204 A 3397 WIRE BOEING 727 72789 1384028 NM CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 511DB 19139 DURING SCHEDULED MAINTENANCE IN TUS, RIGHT AFT EMERGENCY EXIT LIGHT STAYS ON WITH POWER ON. REPAIRED WIRING TO TERMINAL LUG CONNECTION. (M) 2 L 7 3 4F A3WE 1998043000784 19980430 00784 NM 1998 4 30 98ZZZM327 1 19980210 A 2612 FIRE WARNING BOEING 727 727222 1384073 NM ENGINE ACTIVATED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 7645U 20039 FLT 546 - DAY-ELP - HAD AN AIR RETURN TO DAY. DURING CLIMB FIRE WARNING BELL SOUNDED WITH NO OTHER INDICATIONS. PERFOR MED ENGINE, WHEEL WELL, FIRE WALL FIRE TEST ALL NORMAL, RAN ENGINES AT 85 PERCENT N2. NO FIRE WARNING OR OTHER ABNORMAL ITIES NOTED. 2 L 7 3 4F A3WE 1998043000785 19980430 00785 EU 1998 4 30 RAIA980213 1 19980215 A 3241 428891 CONTROLLER JETAIR JETSTM JETSTM4101 1500501 EU ANTI-SKID SYSTEM FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 571HK 4094 41090 FLT 7779 - DCA - ANTI-SKID SYSTEM FAILED ON TAKEOFF. MAINTENANCE REPLACED ANTI-SKID CONTROL UNIT. (M) 2 L 7 2 4T RT A41NM 1998043000786 19980430 00786 EU 1998 4 30 RAIA980212 1 19980212 A 2910 HYDRAULIC SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU MAIN HYD SYSTEM REQ'D SERVICE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 561HK 41077 FLT 7792 - JFK - HYDRAULIC QTY INDICATOR DROPPED BELOW RED LINE ON TAKEOFF ROLL. MAINTENANCE BLED HYDRAULIC ACCUMULATOR S AND SERVICED HYDRAULIC SYSTEM. QTY OPERATES NORMALLY. (M) 2 L 7 2 4T RT A41NM 1998043000787 19980430 00787 1998 4 30 RAIA980215 4 19980224 A 3416 4016341905 ALTIMETER JETAIR JETSTM JETSTM4101 1500501 EU LT INST PNL FLAGGED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 551HK 41040 FLT 7482 - STL - CAPTAINS ALTIMETER FLAGGED ON CLIMB-OUT. MAINTENANCE REPLACED CAPTAINS ALTIMETER. (M) 2 L 7 2 4T RT A41NM 1998043000788 19980430 00788 EU 1998 4 30 RAIA980214 4 19980224 A 3160 7011672111 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU RIGHT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 550HK 7203 41039 FLT 7720 - JFK - RIGHT EFIS SYMBOL GENERATOR FAILED. MAINTENANCE REPLACED RIGHT EFIS SYMBOL GENERATOR. (M) 2 L 7 2 4T RT A41NM 1998043000789 19980430 00789 1998 4 30 RAIA980217 4 19980225 A 3425 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU E/E COMP FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 567HK 4814 41085 FLT 7714 - JFK - CAPTAINS EHSI SHOWING 10 TO 15 DEGREE HEADING SPLIT AND HSI WAS ERRATIC. MAINTENANCE REPLACED NR 1 AHR S COMPUTER. (M) 2 L 7 2 4T RT A41NM 1998043000790 19980430 00790 EU 1998 4 30 PLGA980218D 1 19980218 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU RT TAILPIPE WATER CONTAM A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 341BE 340A063 PWM - FLT 4327 - AFTER TAKEOFF, THE RIGHT TAIL PIPE HOT LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURES AND LIGHT DID NOT E XTINGUISH. THE RIGHT ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO PWM. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WATER IN DETECTOR CONNECTOR. UNIT WAS CLEANED AND SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998043000791 19980430 00791 EU 1998 4 30 PLGA980218A 1 19980218 A 3610 5056T88P01 VALVE SAAB SF340 SF340A 7850100 EU RIGHT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 743BA AEX10724 340A093 BGR - FLT 4411 - AFTER TAKEOFF, THE RIGHT AIR VALVE FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BGR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GARRETT VALVE. SYSTEM CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998043000792 19980430 00792 EU 1998 4 30 PLGA980218B 1 19980218 A 3020 NH24668083 IPD SAAB SF340 340B 7860101 EU LT ENGINE FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 364BE 305 340B294 BOS - FLT 4232 - AFTER TAKEOFF, THE LEFT ENGINE INTAKE HEAT FAILED. AIRCRAFT RETURNED TO BOS DUE TO WEATHER CONDITIONS. MAINTENANCE FOUND THE LEFT INLET PROTECTION DEVICE HAD FAILED. UNIT WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A52EU 1998043000793 19980430 00793 EU 1998 4 30 PLGA980218C 1 19980218 A 2613 CONNECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE WATER CONTAM A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 743BA 340A093 BOS - FLT 4319 - AFTER TAKEOFF, THE RIGHT ENGINE TAIL PIPE HOT LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURES AND LIGHT EX TINGUISHED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND WATER IN DETECTOR CONNECTOR. UNIT WAS CLEANED AND SYSTEM TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998043000794 19980430 00794 EU 1998 4 30 PLGA980208B 1 19980208 A 7722 522861 ITT INDICATOR SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A PLGA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 NE 05 745BA 12862005 340A111 BOS - FLT 4428 - AFTER TAKEOFF, THE RIGHT ITT INDICATOR STARTED FLUCTUATING BETWEEN 800-900 DEGREES. ENGINE WAS SHUT DO WN. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ITT INDICATOR. SYSTEM CHECKED GO OD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998043000795 19980430 00795 EU 1998 4 30 PLGA980208A 1 19980208 A 6120 AUTOCOARSEN SAAB SF340 SF340A 7850100 EU E/E COMPT MALFUNCTIONED A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NE 05 345BE 340A108 PWM - FLT 4385 - DURING TAKEOFF, THE AUTOCOARSEN FAILED TO ARM. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RAN AIRCRAFT AND FOUND SYSTEM TO BE OPERATING NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998043000796 19980430 00796 EU 1998 4 30 PLGA980204C 1 19980204 A 3020 ND00752208 CONTROL SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 346BE L243326 340A150 BOS - FLT 4308 - AFTER TAKEOFF, THE LEFT ENGINE INTAKE HEAT FAILED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDEN T. MAINTENANCE REPLACED THE LEFT THERMAL CONTROL. SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998043000797 19980430 00797 EU 1998 4 30 PLGA980204B 1 19980204 A 3020 M8535362024L RELAY SAAB SF340 SF340A 7850100 EU RT ENGINE FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 744BA 340A105 BOS - FLT 4289 - SHORTLY AFTER DEPARTURE, THE RIGHT ENGINE INTAKE HEAT FAILED. AIRCRAFT RETURNED TO BOS AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED THE RIGHT HEAT DRIVER RELAY. SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998043000798 19980430 00798 WP 1998 4 30 ORJA9823 1 19980210 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 873RA 53093 EMERGENCY LIGHT ON SEAT 8D INOP. INSTALLED LIGHT ASSY, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998043000799 19980430 00799 WP 1998 4 30 ORJA9825 1 19980213 A 3350 PPSIB CHARGER DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY ESCAPE PATH LIGHTS IN ROWS 19, 20, 21, AND 22 ILLUMINATED WOULD NOT SHUT OFF UNTIL BATTERY PACK WAS DISCHARGED . INSTALLED NEW EMERGENCY PATH LIGHT BATTERY PACK CHARGER ROWS 19-22. OPS CHECK NORMAL IAW MM 33-00-00. (M) 2 L 7 2 4F RT A6WE 1998043000800 19980430 00800 WP 1998 4 30 ORJA9826 1 19980217 A 3350 EM1267 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 842RA 49604 CEILING EMERGENCY LIGHTS AT ROWS 33 THROUGH 26 INOP. REPLACED BATTERIES IN O/H BIN 25, OPS NORMAL. (M) 2 L 7 2 4F A6WE 1998043000801 19980430 00801 WP 1998 4 30 ORJA9821 1 19980211 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY TRACK LIGHTING WILL NOT EXTINGUISH AT ROW 21-24 DEF. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER AT LEFT AFT OVERWING DOOR SYSTEM, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998043000802 19980430 00802 WP 1998 4 30 ORJA9822 1 19980210 A 3350 59306431 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 873RA 53093 ROW 25 THROUGH 28 D, E, F EMERGENCY LIGHTS INOP. REPLACED BATTERIES TO EMERGENCY EXIT AFT GALLEY, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998043000803 19980430 00803 WP 1998 4 30 ORJA9815 1 19980130 A 7931 201EDP11 SYS DISPLAY PNL DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A ORJA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 11 821RA 49931 RETURN TO GATE, ENGINE DISPLAY PANEL SHOWED INCORRECT OIL PRESSURE FOR BOTH ENGINES AFTER ENGINE START DISPLAYED OIL PRE SSURE OF 36 LEFT AND 27 RIGHT OAP LOW OIL PRESSURE ANNUNCIATION DID NOT ILLUMINATE. REMOVED AND REPLACED SYSTEM DISPLAY PANEL, RAN MOTORS SYSTEMS OPS CHECK GOOD AT THIS TIME. (M) 2 L 7 2 4F A6WE 1998043000804 19980430 00804 NE 1998 4 30 98ZZZM328 2 19980206 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT OVERTEMPED A NVEA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 SO 03 204NE 340B204 785213 FLT 5747 - APF - ON APPROACH LEFT ENGINE OVERTEMPED AND THE NG ROLLED BACK. THE CREW ELECTED TO SHUT DOWN THE ENGINE AN D LANDED WITHOUT PROBLEMS. REPLACED ENGINE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998043000805 19980430 00805 SO 1998 4 30 MASA98039 1 19980225 A 3397 WIRE EMB 120 EMB120RT SO CABIN SHORTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 340JS 120172 FLT 5508 - MIA-TLH - ON START UP IN MIA, CREW NOTICED THE EMERGENCY TRACK LIGHTS IN THE MIDDLE FLOOR SECTION WOULD NOT I LLUMINATE. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-51-1. IN SUBSEQUENT MAINTENANCE, A SHORTED WIRE WAS REPAIRED. ( M) 2 L 7 2 4T RT A31SO 1998043000806 19980430 00806 NM 1998 4 30 MASA98029 1 19980217 A 3350 MS25237327 BULB DHAV DHC8 DHC8202 2809007 NM COCKPIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 FLT 7622 - HDN-DEN - IN DEN, CREW REPORTED THE PORTABLE EMERGENCY LIGHT WAS INOP. MAINTENANCE REMOVED AND REPLACED THE BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000807 19980430 00807 NM 1998 4 30 MASA98030 1 19980218 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 7592 - DEN-GJT - DURING DEN PREFLIGHT CHECK, PILOT NOTICED TWO FLOOR TRACK LIGHTS WERE INOP. MAINTENANCE REMOVED AN D REPLACED THE BATTERIES AND TRACK LIGHTING STRIP. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000808 19980430 00808 NM 1998 4 30 98ZZZM329 1 19980218 A 3350 6519035 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 7592 - DEN-GJT - DURING DEN PREFLIGHT CHECK, PILOT NOTICED TWO FLOOR TRACK LIGHTS WERE INOP. MAINTENANCE REMOVED AN D REPLACED THE BATTERIES AND TRACK LIGHTING STRIP. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000809 19980430 00809 NM 1998 4 30 MASA98033 1 19980219 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 DURING LINE CHECK INSPECTION, MAINTENANCE FOUND THE CENTER AISLE EMERGENCY EXIT SIGN WAS DIM. REMOVED AND REPLACED BURN ED OUT LIGHT BULBS, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998043000810 19980430 00810 NM 1998 4 30 MASA98034 1 19980219 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 DURING LINE CHECK INSPECTION, MAINTENANCE FOUND THE AFT CENTER AISLE EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED THE BULB IN THE LIGH ASSY, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998043000811 19980430 00811 NM 1998 4 30 MASA98035 1 19980222 A 3350 MS252313H BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 DURING ROUTINE LINE INSPECTION, THE NR 2 OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACE D THE BULB, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000812 19980430 00812 NM 1998 4 30 MASA98036 1 19980222 A 3350 AML91LA5 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 DURING ROUTINE LINE CHECK INSPECTION, THE F/A EMERGENCY LIGHT SWITCH WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPL ACED THE SWITCH BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998043000816 19980430 00816 CE 1998 4 30 MASA98028 1 19980216 A 5210 129400371 SEAL BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR FAILED A A MASA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 5YV UE5 FLT 5288 - PBI-TLH - AT APPROXIMATELY 20,000 FEET, THE CREW HEAR A SHORT BURST FOLLOWED BY IMMEDIATE DECOMPRESSION. THE CREW DECLARED AN EMERGENCY AND EXECUTED A DESCENT TO 10,000 FEET. DURING THE DESCENT THE CREW COULD NOT GET OXYGEN TO FLOW TO THE MASKS UNTIL REACHING 10,000 FT. AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE FOUND THE PASSENGER DOOR SEAL FROM THE TOP TO APPROXIMATELY HALF WAY DOWN HAD FAILED. MAINTENANCE REPLACED THE DOOR SEAL. THE OXYGEN SYSTEM WAS TROU BLESHOT, NO DISCREPANCIES WERE NOTED. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000817 19980430 00817 CE 1998 4 30 MASA98031 1 19980218 A 5210 10151404715 CAMS BEECH 1900 1900D 1154162 CE PAX DOOR OUT OF ADJUST A MASA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 37YV UE37 FLT 7476 - CYS-DEN - IN DEN, CREW REPORTED THE CABIN DOOR WAS DIFFICULT TO OPEN AND CLOSE. MAINTENANCE RIGGED THE DOOR CAMS. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998043000818 19980430 00818 EU 1998 4 30 VTZA98083 1 19980220 A 2820 9409019 MOTIVE FLOW DRV JETAIR JETSTM JETSTM4101 1500501 EU LT FUEL SYSTEM FAILED A VTZA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 306UE 41020 FLT 6517 - LGA-IAD - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE FUEL CROSSFEED NOT FUNCTIONING PROPERLY. AIRCRAFT RETURNED TO GATE WHERE MAINTENANCE CONTROL AND MAINTENANCE WAS NOTIFIED. AIRCRAFT WAS FERRIED TO IAD MAINTENANCE FACILI TY WHERE MAINTENANCE TROUBLESHOT THE DISCREPANCY AND FOUND THE MOTIVE FLOW DRIVE TO BE MALFUNCTIONING. MAINTENANCE REMO VED AND REPLACED THE MOTIVE FLOW DRIVE IAW MX PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998043000819 19980430 00819 1998 4 30 VTZA98082 4 19980220 A 3414 39948B2236 AIRSPEED IND BAG JETSTM JETSTM3201 1500217 EU LT COCKPIT FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 480UE 894 FLT 6152 - BGM-IAD - DURING TAKEOFF, EXPERIENCED 20 KTS DIFFERENCE BETWEEN THE CAPT'S AND F/O'S ASI. CREW ABORTED TAKEO FF AND RETURNED TO THE GATE AND NOTIFIED MAINTENANCE CONTROL. IAD MAINTENANCE WAS DISPATCHED WITH REPLACEMENT COMPONENT S TO BGM. UPON ARRIVAL AT BGM MAINTENANCE FOUND THAT THE CAPT'S ASI WAS DEFECTIVE. MAINTENANCE REMOVED AND REPLACED TH E CAPT'S ASI AND PERFORMED ALL REQUIRED CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998043000820 19980430 00820 EU 1998 4 30 VTZA98080 1 19980217 A 2612 51653151 DETECTION BOX JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 319UE 41042 FLT 949 - EWR-PIT - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO LT ENGINE FIRE WARNING ILLUMINATED. MAINTENANCE INSPE CTED AND REMOVED AND REPLACED FIRE DETECTION BOX AND FIRE LOOP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998043000821 19980430 00821 EU 1998 4 30 98ZZZM330 1 19980217 A 2612 51228532 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 319UE 41042 FLT 949 - EWR-PIT - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO LT ENGINE FIRE WARNING ILLUMINATED. MAINTENANCE INSPE CTED AND REMOVED AND REPLACED FIRE DETECTION BOX AND FIRE LOOP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998043000822 19980430 00822 EU 1998 4 30 VTZA98019 1 19980218 A 3350 FU248 FUSE JETAIR JETSTM JETSTM4101 1500501 EU CABIN BLOWN A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 320UE 41043 FLT 6254 - AIB-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO EMERGENCY TRACK LIGHTING AND OVERWING LIGHTS INOP. M AINTENANCE INSPECTION AND REMOVED AND REPLACED FUSE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A41NM 1998043000823 19980430 00823 1998 4 30 VTZA98078 3 19980217 A 6112 PROP HEAT JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 302UE 41013 FLT 6547 - IAD-ROA - DURING CRUISE, AIRCRAFT MADE A UNSCHEDULED LANDING AT IAD DUE TO LEFT PROP HEAT FAILED. AIRCRAFT W ENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT PROP ASSY. OPS CHECK OK. AI RCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998043000824 19980430 00824 1998 4 30 VTZA98075 3 19980216 A 6112 B4018317 DE-ICE BOOT JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 305UE 41019 FLT 6454 - IAD-DET - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO LEFT PROP HEAT FAILED IN ICING CO NDITIONS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT NR 4 PROP DE-ICE BOOT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998043000825 19980430 00825 EU 1998 4 30 VTZA98074 1 19980217 A 5210 JE5 ACTUATOR BAG JETSTM JETSTM3201 1500217 EU PAX DOOR DIRTY A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 479UE 893 FLT 6600- IAD-DAY - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO PASSENGER DOOR WARNING LIGHT ILLUMI NATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBED MICROSWITCH DRA W BOLT ACTUATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998043000826 19980430 00826 EU 1998 4 30 VTZA98073 1 19980217 A 7712 3102476211 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 494UE 810 FLT 6261 - IAD-EWR - AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE EGT FLUCTUATION. AIRCRAFT RETURNED TO GATE W ITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEAN CANNON PLUG AND REMOVED AND REPLACED TORQUE SIGNAL CONDITIONER , OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998043000827 19980430 00827 EU 1998 4 30 VTZA98072 1 19980217 A 3244 31485 MAIN TIRE BAG JETSTM JETSTM3201 1500217 EU RT MLG BLOWN A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 481UE 895 FLT 6414 - IAD-GSO - DURING TAXI FLT, AIRCRAFT RETURNED TO GATE DUE TO A/C WOULD NOT MOVE FORWARD ON TAXIWAY. MAINTENAN CE INSPECTED AND FOUND RT MAIN TIRE BLOWN. MAINTENANCE REMOVED AND REPLACED RT MAIN TIRE AND BRAKE ASSEMBLY. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998043000828 19980430 00828 EU 1998 4 30 98ZZZM331 1 19980217 A 3240 215221 BRAKE ASSY BAG JETSTM JETSTM3201 1500217 EU RT MLG DAMAGED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 481UE 895 FLT 6414 - IAD-GSO - DURING TAXI FLT, AIRCRAFT RETURNED TO GATE DUE TO A/C WOULD NOT MOVE FORWARD ON TAXIWAY. MAINTENAN CE INSPECTED AND FOUND RT MAIN TIRE BLOWN. MAINTENANCE REMOVED AND REPLACED RT MAIN TIRE AND BRAKE ASSEMBLY. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998043000829 19980430 00829 EU 1998 4 30 VTZA98071 1 19980217 A 3040 2311M511 WIPER MOTOR BAG JETSTM JETSTM3201 1500217 EU LT WINDSHIELD FAILED A VTZA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 476UE 884 FLT 6325 - IAD-GSO - DURING TAXI FLT, AIRCRAFT RETURNED TO GATE DUE TO CAPTAINS WIPER MOTOR CIRCUIT BREAKER POPPED AND S MOKE SMELL IN COCKPIT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WIPER MOTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998043000830 19980430 00830 EU 1998 4 30 VTZA98070 1 19980217 A 2910 13791231157 HYD LINE BAG JETSTM JETSTM3201 1500217 EU RIGHT LEAKING A VTZA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 484UE 899 FLT 6200 - IAD-ROA - DURING TAXI, RETURNED TO GATE DUE TO LOST OF HYDRAULICS AND BRAKES ON TAXIWAY. MAINTENANCE INSPECT ED AND FOUND HYDRAULIC LINE LEAKING AND REMOVED AND REPLACED LINE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998043000831 19980430 00831 SO 1998 4 30 RAAA98E9010 1 19980314 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD LT AND AFT LT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISC HARGED. 2 L 7 4 4T 4A22 1998043000832 19980430 00832 WP 1998 4 30 VJ9800043 1 19980305 A 5310 1A28762 STRUCTURE DOUG DC9 DC932 3022066 WP FS 607 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 909VJ 47322 LOWER END CAP CORRODED AND 6 RIVET POPPED IN CARGO COMAPARTMENT BELOW CENTER FUEL TANK PRESSURE BULKHEAD. REMOVED DUCT SEAL CONTAINER, DOUBLER AROUND DUCT CUT OUT AND WEB PLUS CORRODED T-CHORD. INSTALLED T-CHORD IAW DC9 SRM, FIG 53-03, PG 15, AND DOUBLER IAW DC9 SRM 51-10-2, AND REINSTALLED DUCT SEAL REATINER IAW DC9 SRM 51-30-1. REPAIR ACCOMPLISHED IAW A EROCORP EO 98-798. 2 L 7 2 4F A6WE 1998043000833 19980430 00833 WP 1998 4 30 VJ9800044 1 19980306 A 5312 591486523 BULKHEAD DOUG DC9 DC932 3022066 WP BS 597 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 909VJ 47322 TWO FASTENER HEADS POPPED AND BULGING UNDER PRESSURE DOME AT STA 597, RBL 18. DRILLED NEW PANEL, FABRICATED FINGER DOU BLERS PLUS 2 ADDITIONAL DOUBLERS IAW DC9 SRM 51-10-2. TREATED AND PRIMED AREAS IAW DC9 SRM 51-10-3, INSTALLED NEW PRESS URE BULKHEAD PANEL, FINGER DOUBLERS AND DOUBLERS IAW DC9 SRM 51-30-2, RES 1 03655 AND AEROCORP EO 98-798. 2 L 7 2 4F A6WE 1998043000834 19980430 00834 WP 1998 4 30 VJ9800045 1 19980312 A 5711 5911305504 SPAR CHORD DOUG DC9 DC932 3022066 WP WS 80 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 909VJ 47322 VISUAL INSPECTION OF BLEND AREA AT XRS80 PER AIRTRAN WO 30343, CORROSION WAS NOTED IN THE BLEND AREA AND AROUND 1 FASTEN ER NEXT TO TO THE BLENDED AREA ON THE RIGHT WING REAR SPAR LOWER CHORD. REMOVED CORROSION IAW DC9 SRM 51-10-3, BLENDED AREA TO MINIMUM OF 1 INCH RADIUS PER EO 98-813, SHOTPEENED AND REWORKED AREA, APPLIED CORROSION PROTECTION IAW DC9 SRM 5 1-10-3, EO 98-813 AND REINSTALLED FASTENERS IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998043000835 19980430 00835 NM 1998 4 30 VJ9800046 1 19980314 A 3230 65445815 ISOLATION VALVE BOEING 737 7372L9 1384497 NM RT MLG FAILED A ZZDA O OTHER K FLUID LOSS LD LANDING 1 SO 11 465AT 21528 DURING ROLLOUT ON LANDING, NOSE WHEELS AND RT MAIN GEAR WHEELS DEPARTED HARD SURFACE OF RUNWAY. LINE MAINTENANCE INSPE CTED AIRCRAFT AND DETERMINED AIRCRAFT COULD BE SAFELY RESTORED TO RUNWAY. PINNED GEAR AND SUBSEQUENTLY AIRCRAFT WAS TOW ED TO GATE TO DEPLANE PASSENGERS AND FURTHER INSPECT AIRCRAFT LANDING GEAR SYSTEM. FOUND LANDING GEAR ISOLATION VALVE H AD FAILED. REPLACED ISOLATION VALVE, REPLACED HYDRAULIC FILTERS, PERFORMED HARD LANDING INSPECTION AND NO DAMAGE FOUND. 2 L 7 2 4F RT A16WE 1998043000836 19980430 00836 WP 1998 4 30 VJ9800047 1 19980313 A 2560 5928730503 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR DISLODGED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 918VV 47320 MAIN CABIN PASSENGER EMERGENCY DOOR SLIDE DISLODGED. REINSTALLED SLIDE COVER IAW DC9 MM 25-60, ACCOMPLISHED REQUIRED IN SPECTIONS. 2 L 7 2 4F A6WE 1998043000837 19980430 00837 WP 1998 4 30 VJ9800048 1 19980315 A 3350 110049 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 939VV 47089 EMERGENCY FLOOR PATH LIGHTING, SECTION 3, INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51, OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998043000838 19980430 00838 NM 1998 4 30 CALA9800443 1 19980314 A 5347 TIE DOWN BOEING 737 7373T0 1384582 NM BS 794-847 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14336 23574 INSPECTION FOUND RT TIE DOWN STRIP CORRODED AT STA 794.3 TO 847. THE RT CARGO TRACK WAS CUT AND SPLICED IAW SRM 53-00-5 3, FIGURE 202. 2 L 7 2 4F RT A16WE 1998043000839 19980430 00839 WP 1998 4 30 CALA9800444 1 19980314 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 586 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68044 46903 INSPECTION FOUND A .75 INCH CRACK THROUGH INNER AND OUTER SKIN OF CUTOUT FOR AFT PACK HOT AIR EXHAUST AT FORWARD LOWER C ORNER, FS 586. DOUBLERS AND FILLER WERE INSTALLED IAW ENGINEERING ORDER COM NR 26752-1616I/R. 2 L 7 3 4F A22WE 1998043000840 19980430 00840 WP 1998 4 30 CALA9800445 1 19980314 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14890 49114 INSPECTION FOUND A .375 INCH CRACK IN VERTICAL STABILIZER FORWARD RIGHT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. THE ANGLE WAS REPAIRED IAW SRM 55-02, FIGURE 26. 2 L 7 2 4F A6WE 1998043000841 19980430 00841 WP 1998 4 30 CALA9800446 1 19980315 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83872 49120 INSPECTION FOUND A .5 INCH CRACK IN VERTICAL STABILIZER FORWARD LEFT SPAR SUPPORT ANGLE AT APPROXIMATELY 37.5 INCHES AFT OF STA 1089.5 IN TAIL COMPARTMENT ABOVE CATWALK. REPAIRED ANGLE IAW SRM 55-02, FIGURE 26. 2 L 7 2 4F A6WE 1998043000842 19980430 00842 WP 1998 4 30 CALA9800447 1 19980315 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT ANGLE AT STA 2007 BETWEEN LBL 56 AND 63. TH E CORROSION WAS TRIMMED AND BLENDED OUT. A SPLICE ANGLE AND U-SPLICE CHANNEL WERE FABRICATED AND INSTALLED IAW SRM 51-2 0-00, 53-40-00, FIGURE 16, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000843 19980430 00843 WP 1998 4 30 CALA9800448 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1964 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT AT STA 1964, RBL 20. THE FLOOR SUPPORT WAS REMOVE D. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26 AND 51-31-01. 2 L 7 3 4F A22WE 1998043000844 19980430 00844 WP 1998 4 30 CALA9800449 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1884-1997 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT BETWEEN STA 1884 AND 1997, LBL 25. THE FLOO R SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-20-00, AN D 51-31-01. 2 L 7 3 4F A22WE 1998043000845 19980430 00845 WP 1998 4 30 CALA9800450 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1942 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY 1 CRACK ON FLOOR SUPPORT ABOVE STA 1942 AT RBL 3. THE FLOOR SUPPORT WA S REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-21-00, 51-31-01, AND 53-16-01. 2 L 7 3 4F A22WE 1998043000846 19980430 00846 WP 1998 4 30 CALA9800451 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION AND A 1 CRACK ON FLOOR SUPPORT ABOVE FLOORBEAM AT STA 1986 AT RBL 4. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AN D 53-16-01. 2 L 7 3 4F A22WE 1998043000847 19980430 00847 WP 1998 4 30 CALA9800452 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1841-1884 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT BETWEEN STA 1841 AND 1884 AT RBL 34. THE FL OOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000848 19980430 00848 WP 1998 4 30 CALA9800453 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1841-1884 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT BETWEEN STA 1841 AND 1884, BL 0 TO LBL 8. T HE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-20 -00, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000849 19980430 00849 WP 1998 4 30 CALA9800454 1 19980315 A 5311 FRAME DOUG DC10 DC1030 3023501 WP TAIL CONE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 1 INCH CRACK IN TAIL CONE UPPER SECTION LT SIDE RIB NR 8. THE RIB AND SPLICE WERE REMOVED. A NEW FR AME AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-30-00, FIGURE 1, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000850 19980430 00850 WP 1998 4 30 CALA9800455 1 19980315 A 5330 PANEL DOUG DC10 DC1030 3023501 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 2 INCH CRACK IN LT NR 4 BANJO FITTING INNER ACCESS PANEL. THE PANEL WAS REMOVED AND A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-20-00 AND 51-31-01. 2 L 7 3 4F A22WE 1998043000851 19980430 00851 WP 1998 4 30 CALA9800456 1 19980315 A 5347 FLOOR TRACK DOUG DC10 DC1030 3023501 WP BS 840 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR TRACK AT STA 840, RBL 27. THE FLOOR TRACK WAS REMOV ED, A NEW TRACK WAS INSTALLED IAW SRM 53-70-00, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000852 19980430 00852 WP 1998 4 30 CALA9800457 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 824-879 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INTERIOR UPPER LOBE CABIN UNDER FLOOR LAV/GALLEY CORROSION ON FLOOR SUPPORT BETWEEN STA 824 AND 879, RBL 73. THE FLOOR SUPPORT WAS REMOVED. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000853 19980430 00853 WP 1998 4 30 CALA9800458 1 19980315 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1381 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1381, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A N EW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-53-01, FIGURE 3, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000854 19980430 00854 WP 1998 4 30 CALA9800459 1 19980315 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1421 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND A 1 INCH CRACK ON FAIRING SUPPORT ANGLE AT STA 1421, STRINGER 32R. THE SUPPORT ANGLE WAS REMOVED. A N EW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-53-01, FIGURE 3. 2 L 7 3 4F A22WE 1998043000855 19980430 00855 WP 1998 4 30 CALA9800460 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 492 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 492, RBL 30. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS F ABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998043000856 19980430 00856 WP 1998 4 30 CALA9800461 1 19980315 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 455 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 455, LBL 60. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS F ABRICATED AND INSTALLED IAW SRM 53-12-15, FIGURE 1 AND 26, 51-31-01, AND 51-20-00. 2 L 7 3 4F A22WE 1998043000857 19980430 00857 WP 1998 4 30 CALA9800462 1 19980315 A 5320 VENT BOX DOUG DC10 DC1030 3023501 WP BS 1480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14063 47864 INSPECTION FOUND CORROSION ON VENT BOX AT STA 1480 AT ATTACHMENT TO LONGERON 27R. CORRODED TRUSS WAS REMOVED. A NEW PA RT WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-31-01, AND 53-14-01, FIGURE 5, ITEM 42. 2 L 7 3 4F A22WE 1998043000858 19980430 00858 1998 4 30 9804391161 4 19980314 A 3417 CADC DOUG DC10 DC1040 3023508 WP NR 1 FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 161US 46770 ON TAKEOFF ROLL, CAPTAIN'S AIRSPEED INDICATOR INDICATED 20 KTS BELOW FIRST OFFICER'S. ABORTED TAKEOFF AT 140 KTS AND RE TURNED TO THE GATE. REPLACED THE NR 1 CADC, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998043000859 19980430 00859 WP 1998 4 30 9804409877 1 19980314 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND CATWALK AND EXIT HANDLE EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES, O PERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043000860 19980430 00860 WP 1998 4 30 9804419302 1 19980315 A 8097 WIRE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE DAMAGED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 302RC 48055 708407 DURING CLIMB, THE RIGHT ENGINE START VALVE OPEN LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPAIRED THE RIGHT ENGINE WIRE HARNESS. ENGINE OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E9NE 1998043000861 19980430 00861 WP 1998 4 30 9804429870 1 19980315 A 3350 FLASHLIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 779NC 48101 FLIGHT ATTENDANT REPORTED AN INOPERATIVE EMERGENCY FLASHLIGHT AT THE FORWARD FLIGHT ATTENDANT SEAT. MAINTENANCE REPLACE D THE EMERGENCY FLASHLIGHT, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043000862 19980430 00862 WP 1998 4 30 9804439851 1 19980313 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 01 760NC 47708 DURING TAXI OUT, THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS SECTION AND THE LOCATOR LIGHT OVER THE GALLEY DOOR RE MAINED ILLUMINATED. AIRCRAFT RETURNED TO THE GATE AREA. MAINTENANCE REPAIRED SHORTED WIRING AT THE AIRPHONE BRACKET AT SEAT ROW 2C AND REPLACED THE POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043000863 19980430 00863 WP 1998 4 30 9804449150 1 19980315 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8908E 45749 DURING LINE CHECK, FOUND ONE EACH FORWARD EMERGENCY FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED THE B ATTERY, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998043000864 19980430 00864 1998 4 30 9804459930 4 19980313 A 2210 COMPUTER DOUG DC9 DC931 3022065 WP E/E COMPT FAILED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 89S 47042 RUDDER OSCILLATION WITH AIRCRAFT YAW OCCURRED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED STABILIZATION AUGMENTATION COMPUTER AND RUDDER YAW DAMPER ACTUATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998043000865 19980430 00865 SO 1998 4 30 COMA9810065 1 19980314 A 2121 EVAC523C2 FAN EMB 120 EMB120RT SO CABIN OVERHEATED A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 266CA 15259 120258 STRONG ELECTRICAL SMELL IN COCKPIT. RIGHT HAND RECIRCULATION FAN CIRCUIT BREAKER TRIPPED. REPLACED THE RIGHT HAND RECI RCULATION FAN. 2 L 7 2 4T RT A31SO 1998043000866 19980430 00866 SO 1998 4 30 COMA9810066 1 19980313 A 3097 WIRE EMB 120 EMB120RT SO WING DE-ICE BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 268CA 120262 STABILIZER AND WING DE-ICE BOOTS INDICATE INOPERABLE DURING FLIGHT. REPAIRED BROKEN WIRE AT DE-ICE SYSTEM EJECTOR VALVE S. 2 L 7 2 4T RT A31SO 1998043000867 19980430 00867 SO 1998 4 30 COMA9810067 1 19980312 A 3260 12043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR FAILED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 269CA 16537 112 120263 TAKEOFF AURAL WARNING SOUNDED AFTER TAKEOFF. REPLACED THE LANDING GEAR RELAY BOX. 2 L 7 2 4T RT A31SO 1998043000868 19980430 00868 SO 1998 4 30 COMA9810068 1 19980310 A 5230 12032772041 CABLE EMB 120 EMB120RT 3260202 SO CARGO DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 200CD 18374 120200 DURING 2C INSPECTION TASK 813-01A, FOUND CARGO DOOR FORWARD INNER CABLE TO BE CORRODED. REMOVED CORRODED CABLE AND INST ALLED SERV CABLE IAW EMB120 MM. 2 L 7 2 4T RT A31SO 1998043000869 19980430 00869 EA 1998 4 30 COMA9860056 1 19980315 A 3350 64643 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912CA 7011 EMERGENCY FLOOR LIGHTING FRONT HALF OF CABIN IS INOPERABLE. REPLACED LIGHT STRIP ROWS 2 THRU 5. 2 L 7 2 4F RT A21EA 1998043000870 19980430 00870 EA 1998 4 30 COMA9860057 1 19980314 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTION A COMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 982CA 7168 CARGO SMOKE WARNING DURING FLIGHT. REPLACED CARGO SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 1998043000871 19980430 00871 EA 1998 4 30 COMA9860058 1 19980309 A 5710 601R108001 WING EXTENSION CNDAIR CL600 CL6002B19 EA WS 353 DAMAGED A COMA O OTHER C F.O.D. TX TAXI/GRND HDL 1 SO 01 937CA 7044 DURING AIRCRAFT DE-ICING, GROUND EQUIPMENT STRUCK THE LEFT HAND OUTBOARD WING. REPLACED THE LEFT HAND WING EXTENSION AS SY FROM WS 353 OUTBOARD. 2 L 7 2 4F RT A21EA 1998043000872 19980430 00872 EA 1998 4 30 COMA9860059 1 19980312 A 3230 864806 PSEU CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 989CA 7215 LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN FOR LANDING. MANUAL RELEASE SYSTEM USED TO EXTEND GEAR. REPLACED THE PS EU. 2 L 7 2 4F RT A21EA 1998043000873 19980430 00873 EA 1998 4 30 COMA9860060 1 19980312 A 2751 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 931CA 7037 FLAPS FAIL CAUTION MESSAGE DURING LANDING APPROACH. COULD NOT DUPLICATE DISCREPANCY. FLAPS FUNCTIONAL NORMALLY. 2 L 7 2 4F RT A21EA 1998043000874 19980430 00874 NM 1998 4 30 UPS98226119 1 19980317 A 3520 OXY MASK BOEING 727 72725C 138400H NM CABIN DEPLOYED A IPXA G O2 MASK DEPLOYED O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, ROW 19 O2 MASK DEPLOYED. REPLACED O2 MASK AS REQUIRED PER B727 PAX SUP 35-20-00. 2 L 7 3 4F A3WE 1998043000875 19980430 00875 WP 1998 4 30 UPS98826120 1 19980304 A 5320 37508651N FITTING DOUG DC8 DC871F 302199D WP BS 1750 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, AFT FUSELAGE TAIL SKID FITTING IS CRACKED AT BOTH END BOLT HOLES AT STA 1750 BL 0. REMOVED AND REPLA CED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000876 19980430 00876 WP 1998 4 30 UPS98826121 1 19980223 A 5712 576958963 RIB DOUG DC8 DC871F 302199D WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, LT WING RIB AT STA.XOLDI 6.225 I/B SIDE IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 F IG 2. 2 L 7 4 4F RT 4A25 1998043000877 19980430 00877 WP 1998 4 30 UPS98826122 1 19980304 A 5320 37558412 FITTING DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 1160 AND STR 33R AND 34R SHEAR TIE IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2 D. 2 L 7 4 4F RT 4A25 1998043000878 19980430 00878 WP 1998 4 30 UPS98826123 1 19980226 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 99 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, NOSE SECTION LT SIDE AT STA 99 FRAME IS CRACKED IN TWO PLACES UPPER AND LWR SECTION OF SPLICE. STOP DRILLED CRACK ON UPPER FLANGE AND REMOVED DAMAGE ON LWR FLANGE AND REPAIRED IAW DHC SK 707-600 AND REFERENCE TO EO DC8 5 310- 10296. 2 L 7 4 4F RT 4A25 1998043000879 19980430 00879 WP 1998 4 30 UPS98826124 1 19980225 A 5320 3754041501 FITTING DOUG DC8 DC871F 302199D WP BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 320 AT STR 26L, DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D . 2 L 7 4 4F RT 4A25 1998043000880 19980430 00880 WP 1998 4 30 UPS98826125 1 19980225 A 5320 3754041501 FITTING DOUG DC8 DC871F 302199D WP BS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 300 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 1998043000881 19980430 00881 WP 1998 4 30 UPS98826126 1 19980225 A 5320 37558541 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 1200 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1998043000882 19980430 00882 WP 1998 4 30 UPS98826127 1 19980225 A 5320 3755854502 FITTING DOUG DC8 DC871F 302199D WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 707UP 45907 INSPECTION TYPE-C, STA 1180 AT STR 26L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998043000883 19980430 00883 WP 1998 4 30 UPS98826128 1 19980310 A 5712 RIB DOUG DC8 DC873F 302199F WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM IS CRACKED BY THE AFT FASTENER AT STA 660. STOP DRILLED CRACK AND REPAIRED I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998043000884 19980430 00884 WP 1998 4 30 UPS98826129 1 19980313 A 5320 577384444 CLIP DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LONG 5R AFT BULKHEAD CLIP IS CRACKED AT STA 1766. REMOVED AND REPLACED CLIP IAW DWG 5773844. 2 L 7 4 4F RT 4A25 1998043000885 19980430 00885 WP 1998 4 30 UPS98826130 1 19980312 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM REPAIR DOUBLER IS CRACKED AT STA XFS.304. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998043000886 19980430 00886 WP 1998 4 30 UPS98826131 1 19980312 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING LWR SKIN DOUBLER ON NR 2 ENG STUB WING JUST FWD OF CUTOUT IS CRACKED. REMOVED DOUBLER AND ST OP DRILLED CRACK AND REPAIRED IAW SRM 57-2- 1A. 2 L 7 4 4F RT 4A25 1998043000887 19980430 00887 WP 1998 4 30 UPS98826132 1 19980309 A 5730 5769857613 PANEL DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING O/B SLOT O/B PANEL LAND IS CRACKED. REMOVED AND REPLACED ANGLE FITTING IAW DWG 5769857-613. 2 L 7 4 4F RT 4A25 1998043000888 19980430 00888 WP 1998 4 30 UPS98826133 1 19980310 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 422.750 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-C, LT WING LWR L/E SURFACE IS CRACKED JUST FWD OF EXISTING DOUBLER AT STA 422.750. STOP DRILLED CRACK A ND REPAIRED IAW DC8-5720-4087. 2 L 7 4 4F RT 4A25 1998043000889 19980430 00889 EU 1998 4 30 QXEA9800250 1 19980206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CLIP CRACKED FRAME 13815A STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998043000890 19980430 00890 EU 1998 4 30 QXEA9800251 1 19980206 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 476US 11224 REAR CARGO DOOR APERTURE HAS A NUT PLATE HOLE CONNECTING THE RIVET HOLE, AT INNER SKIN FORWARD SIDE. REPAIRED IAW FOKKE R SRM 53-02-16, PAGE 2, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000891 19980430 00891 EU 1998 4 30 QXEA9800255 1 19980206 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU CARGO COMPT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FLOORBEAM ON REAR CARGO CEILING BETWEEN FRAME 16060 AND 16660 BL 600R IS DENTED UP .5 INCH BUCKLED AND POSSIBLY CRACKED. REPAIRED FLOORBEAM IAW HORIZON AIR EA 4-53-346. 2 L 7 2 4F RT A20EU 1998043000892 19980430 00892 EU 1998 4 30 QXEA9800256 1 19980206 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT FRAME 16660 STRINGER 62 CARGO APERTURE SKIN PANEL IS DENTED AT .065 DEEP. DRILLED OUT AND CUT DAMAGE, AND REPAIRED I AW FOKKER SRM 53-02-16, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000893 19980430 00893 EU 1998 4 30 QXEA9800257 1 19980206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED CLIP AT FRAME 13815B STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000894 19980430 00894 EU 1998 4 30 QXEA9800258 1 19980206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED CLIP AT FRAME 13815A STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-4. 2 L 7 2 4F RT A20EU 1998043000895 19980430 00895 EU 1998 4 30 QXEA9800259 1 19980206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED CLIP FRAME 13815A STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998043000896 19980430 00896 EU 1998 4 30 QXEA9800260 1 19980206 A 5320 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FORWARD CARGO COMPARTMENT FORWARD DOOR AFT SIDE OF DOOR APERTURE AT LOWER SIDE NEXT TO CORNER HAS TWO DENTS. REPAIRED I AW FOKKER SRM 53-02-16, FIGURE 1. 2 L 7 2 4F RT A20EU 1998043000897 19980430 00897 EU 1998 4 30 QXEA9800261 1 19980206 A 5230 DOOR FOKKER F28 F28MK4000 4990810 EU CARGO GOMPT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FORWARD CARGO COMPARTMENT FORWARD DOOR AFT BOTTOM CORNER OF DOOR STRUCTURE HAS SEVERAL DEEP DENTS. REPAIRED IAW FOKKER SRM 52-30-00, FIGURE 1 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998043000898 19980430 00898 EU 1998 4 30 QXEA9800262 1 19980206 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FORWARD CARGO COMPARTMENT FORWARD DOOR INNER STRUCTURE SKIN HAS SEVERAL DEEP DENTS. REPAIRED IAW EA 4-52-117. 2 L 7 2 4F RT A20EU 1998043000899 19980430 00899 EU 1998 4 30 QXEA9800263 1 19980208 A 5230 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED FRAME CLIP AT THE 3RD FROM AFT FRAME AT THE BOTTOM HINGE END OF AFT CARGO DOOR. DRILLED OUT DAMAGED FRAME CLIP AND REPAIRED IAW FOKKER SRM 51-10-5. 2 L 7 2 4F RT A20EU 1998043000900 19980430 00900 EU 1998 4 30 QXEA9800264 1 19980208 A 5230 INTERCOSTAL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THE 2ND INTRCOSTAL FROM THE HINGE ON THE FORWARD SIDE OF THE AFT CARGO DOOR BETWEEN THE FORWARD AND THE 2ND FROM FORWARD FRAMES IS CRACKED. REPAIRED INTERCOSTAL IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998043000901 19980430 00901 EU 1998 4 30 QXEA9800265 1 19980208 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THE FORWARD FRAME OF THE AFT CARGO DOOR HAS CORROSION ON IT IN AN AREA 8 TO 18 INCHES FROM THE HINGE. REPAIRED IAW FOKK ER 51-31-01. 2 L 7 2 4F RT A20EU 1998043000902 19980430 00902 EU 1998 4 30 QXEA9800266 1 19980207 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 CRACK INDICATION ON LOWER SIDE OF BEAM 2 AT LOCATION BL 550L. CRACK INDICATION IS APPROXIMATELY .375 TO .5 INCH LONG. R EPAIRED IAW FOKKER SRM 53-02-18, PAGE 33, FIGURE 13. 2 L 7 2 4F RT A20EU 1998043000903 19980430 00903 EU 1998 4 30 QXEA9800267 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CLIP CRACKED FRAME 5805 AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000904 19980430 00904 EU 1998 4 30 QXEA9800268 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED CLIP AT FRAME 9305C STRINGER 58 AT 2 RIVETS. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000905 19980430 00905 EU 1998 4 30 QXEA9800269 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED CLIP AT FRAME 5805 STRINGER 473. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000906 19980430 00906 EU 1998 4 30 QXEA9800270 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED CLIP AT FRAME 9305 AT STRINGER 49. REPAIRED DAMAGE IAW FOKKER SRM 53-02-12, PAGE 4, FIGURE 1. 2 L 7 2 4F RT A20EU 1998043000907 19980430 00907 EU 1998 4 30 QXEA9800271 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CRACKED CLIP AT FRAME 9305 STRINGER 48. COMPLETED REPAIR IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000908 19980430 00908 EU 1998 4 30 QXEA9800272 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CLIP CRACKED AT FRAME 5805 AT STRINGER 16. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000909 19980430 00909 EU 1998 4 30 QXEA9800273 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CLIP CRACKED FRAME 6305 AT STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000910 19980430 00910 EU 1998 4 30 QXEA9800274 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CLIP CRACKED FRAME 8305 AT STRINGER 17. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000911 19980430 00911 EU 1998 4 30 QXEA9800275 1 19980202 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A CLIP CRACKED FRAME 8205 AT STRINGER 28. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000912 19980430 00912 EU 1998 4 30 QXEA9800276 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 13815A HAS A CRACKED CLIP BETWEEN STRINGER 48-49. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000913 19980430 00913 EU 1998 4 30 QXEA9800277 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 13815A HAS CRACKED CLIP BETWEEN STRINGER 41-42. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000914 19980430 00914 EU 1998 4 30 QXEA9800278 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 13815A HAS A CRACKED CLIP BETWEEN STRINGERS 26-273. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000915 19980430 00915 EU 1998 4 30 QXEA9800279 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 13345 HAS A CRACKED CLIP BETWEEN STRINGERS 33-34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000916 19980430 00916 EU 1998 4 30 QXEA9800280 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12875 HAS CRACKED CLIP BETWEEN STRINGERS 29-30. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000917 19980430 00917 EU 1998 4 30 QXEA9800281 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12875 HAS CRACKED CLIP BETWEEN STRINGER 35-36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000918 19980430 00918 EU 1998 4 30 QXEA9800282 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12875 HAS A CRACKED CLIP BETWEEN STRINGERS 33-34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000919 19980430 00919 EU 1998 4 30 QXEA9800283 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12875 HAS A CRACKED CLIP BETWEEN STRINGERS 41-42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000920 19980430 00920 EU 1998 4 30 QXEA9800284 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12875 HAS A CRACKED CLIP BETWEEN STRINGERS 42-43. REPAIRED IAW FOKKER 53-02-13 PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000921 19980430 00921 EU 1998 4 30 QXEA9800286 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12405 HAS CRACKED CLIP BETWEEN STRINGERS 31-32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000922 19980430 00922 EU 1998 4 30 QXEA9800287 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12405 HAS A CRACKED CLIP BETWEEN STRINGERS 33-34. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000923 19980430 00923 EU 1998 4 30 QXEA9800288 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 12405 HAS A CRACKED CLIP BETWEEN STRINGERS 41-42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000924 19980430 00924 EU 1998 4 30 QXEA9800289 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 10966 HAS A CRACKED CLIP BETWEEN STRINGERS 43-44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000925 19980430 00925 EU 1998 4 30 QXEA9800290 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 10966 HAS A CRACKED CLIP BETWEEN STRINGERS 42-43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000926 19980430 00926 EU 1998 4 30 QXEA9800291 1 19980203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 INSIDE CABIN FRAME 10346 HAS A CRACKED CLIP BETWEEN STRINGERS 31-32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998043000927 19980430 00927 EU 1998 4 30 QXEA9800292 1 19980203 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 476US 11224 THERE IS A ELIPICAL HOLE IN FRAME 9035A AT STRINGER 27-28. REPAIRED IAW FOKKER SRM 51-10-3, PAGE 2, TABLE I AND SRM 53- 02-12 AND EA 4-53-343. 2 L 7 2 4F RT A20EU 1998043000928 19980430 00928 EU 1998 4 30 QXEA9800293 1 19980203 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT FRAME 12405 NEAR STRINGER 27-28 DUCT STANDOFF HOLE IN FRAME CAP IS ENLARGED. REPAIRED IAW EA 4-53-343. 2 L 7 2 4F RT A20EU 1998043000929 19980430 00929 EU 1998 4 30 QXEA9800294 1 19980203 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FRAME CAP AT FRAME 9035A BETWEEN STRINGER 47-48 DUCT STANDOFF HOLE IS ENLARGED. REPAIRED IAW FOKKER SRM 51-10-03, PAGE 2, TABLE I, SRM 53-02-12 AND EA 4-53-343. 2 L 7 2 4F RT A20EU 1998043000930 19980430 00930 EU 1998 4 30 QXEA9800295 1 19980203 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FRAME CAP 10346 BETWEEM STRINGER 47-48 DUCT STANDOFF HOLE IS ELONGATED. REPAIRED IAW HORIZON AIR EA 4-53-343. 2 L 7 2 4F RT A20EU 1998043000931 19980430 00931 EU 1998 4 30 QXEA9800296 1 19980202 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FRAME CAP AT 15205 BETWEEN STRINGER 47-48 DUCT STANDOFF HOLE IS ELONGATED. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 9, FI GURE 3. 2 L 7 2 4F RT A20EU 1998043000932 19980430 00932 EU 1998 4 30 QXEA9800297 1 19980202 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 FRAME CAP AT 14285 BETWEEN STRINGER 47-48 DUCT STAND OFF MOUNT HOLE IS ELONGATED. REPAIRED IAW HORIZON AIR EA 4-53-343. 2 L 7 2 4F RT A20EU 1998043000933 19980430 00933 EU 1998 4 30 QXEA9800298 1 19980207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU LAVATORY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LAV AREA FRAME, 16660 CASTELLATION IS CRACKED AT STRINGER 25. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000934 19980430 00934 EU 1998 4 30 QXEA9800299 1 19980207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU LAVATORY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LAV AREA FRAME 16060 CASTELLATION IS CRACKED AT STRINGER 26. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000935 19980430 00935 EU 1998 4 30 QXEA9800300 1 19980207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU LAVATORY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LAV AREA FRAME 16660 CASTELLATION IS CRACKED AT STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000936 19980430 00936 EU 1998 4 30 QXEA9800301 1 19980207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU LAVATORY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LAV AREA FRAME 16660 CASTELLATION IS CRACKED AT STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000937 19980430 00937 EU 1998 4 30 QXEA9800302 1 19980207 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU LAVATORY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LAV AREA FRAME 16660 CASTELLATION IS CRACKED AT STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998043000938 19980430 00938 EU 1998 4 30 QXEA9800303 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LEFTHAND OBLIQUE FRAME 32-2 CONNECTION ANGLE CRACKED PASSED STOP DRILL AT STRINGER 30 AFT SIDE. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 53-02-13, FIGURE 4, PAGE 6. 2 L 7 2 4F RT A20EU 1998043000939 19980430 00939 EU 1998 4 30 QXEA9800304 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LEFTHAND OBLIQUE FRAME 41-2 CONNECTION ANGLE CRACKED PASSED STOP DRILL AT STRINGER 30 INBOARD AFT. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 8. 2 L 7 2 4F RT A20EU 1998043000940 19980430 00940 EU 1998 4 30 QXEA9800305 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LEFTHAND OBLIQUE FRAME 41-2 CONNECTION ANGLE CRACKED AT STRINGER 20 AFT SIDE. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 7. 2 L 7 2 4F RT A20EU 1998043000941 19980430 00941 EU 1998 4 30 QXEA9800306 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LEFTHAND OBLIQUE FRAME 50-2 CONNECTION ANGLE IS CRACKED IN 2 PLACES AT STRINGER 27. REPAIRED IAW FOKKER SRM 53-02-13, P AGE 6, FIGURE 4 REPAIR SCHEME 2. 2 L 7 2 4F RT A20EU 1998043000942 19980430 00942 EU 1998 4 30 QXEA9800307 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LEFTHAND SIDE OBLIQUE FRAME 32-2 CONNECTION ANGLE IS CRACKED PASSED STOP DRILL AT STRINGER 30 INBOARD. REPAIRED IAW FOK KER SRM 51-31-01, 51-30-02 AND SRM 53-02-13, FIGURE 4, PAGE 6. 2 L 7 2 4F RT A20EU 1998043000943 19980430 00943 EU 1998 4 30 QXEA9800308 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 LEFTHAND OBLIQUE FRAME 32-2 CONNECTION ANGLE HAS CRACKED PASSED STOP DRILL ON AFT SIDE AT STRINGER 27. REPAIRED IAW FOK KER SRM 51-31-01 AND 51-30-02 AND 53-02-13, FIGURE 4, PAGE 6. 2 L 7 2 4F RT A20EU 1998043000944 19980430 00944 EU 1998 4 30 QXEA9800309 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 RIGHTHAND OBLIQUE FRAME 50-2 CONNECTION ANGLE HAS CRACKED PASSED STOP DRILL FORWARD SIDE AT STRINGER 48. REPAIRED IAW F OKKER SRM 51-30-02 AND 51-31-01. 2 L 7 2 4F RT A20EU 1998043000945 19980430 00945 EU 1998 4 30 QXEA9800310 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 RIGHTHAND OBLIQUE FRAME 41-2 CONNECTION ANGLE REPAIR CRACKED AT TOP AFT ATTACH AREA. REPAIRED IAW FOKKER SRM 53-02-13, 51-10-4 AND 53-10-05. 2 L 7 2 4F RT A20EU 1998043000946 19980430 00946 EU 1998 4 30 QXEA9800311 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 RIGHTHAND OBLIQUE FRAME 32-2 CONNECTION ANGLE CRACKED AFT SIDE AT STRINGER 44-43. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6, FIGURE 4. 2 L 7 2 4F RT A20EU 1998043000947 19980430 00947 EU 1998 4 30 QXEA9800312 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 RIGHTHAND OBLIQUE FRAME 32-2 CONNECTION ANGLE CRACKED ON AFT SIDE AT STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, FIG URE 4, PAGE 6. 2 L 7 2 4F RT A20EU 1998043000948 19980430 00948 EU 1998 4 30 QXEA9800313 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 RIGHTHAND CONNECTION ANGLE CRACKED AT RIGHTHAND OBLIQUE FRAME 16-2 AT STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13, PA GE 6, FIGURE 4. 2 L 7 2 4F RT A20EU 1998043000949 19980430 00949 EU 1998 4 30 QXEA9800314 1 19980207 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 RIGHTHAND OBLIQUE FRAME 16-2 HAS CONNECTION ANGLE CRACKED AT STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6, FIG URE 4. 2 L 7 2 4F RT A20EU 1998043000950 19980430 00950 EU 1998 4 30 QXEA9800315 1 19980206 A 5532 PANEL FOKKER F28 F28MK4000 4990810 EU VERT STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 VERTICAL STAB COVE PANEL LEFTHAND AND RIGHTHAND FLAGS HAS LOOSE RIVETS ALMOST ENTIRE LENGTH. REPAIRED IAW FOKKER SRM 51 -31-01, 51-31-05, 55-31-01, FIGURE 1. 2 L 7 2 4F RT A20EU 1998043000951 19980430 00951 EU 1998 4 30 QXEA9800316 1 19980207 A 5532 PANEL FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 RIB 3.4 IN VERTICAL STAB IS CRACKED AT LEFTHAND AND RIGHTHAND AFT CORNERS AT COVE ATTACH POINT. SPLICED FLANGE ON NOTED RIB PER EA 4-55-46. 2 L 7 2 4F RT A20EU 1998043000952 19980430 00952 EU 1998 4 30 QXEA9800317 1 19980215 A 5530 FAIRING FOKKER F28 F28MK4000 4990810 EU VERT STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 VERTICAL STAB BULLET FAIRING HAS HOLE IN SKIN APPROXIMATELY 20 FORWARD OF STAY 26400, LEFTHAND SIDE MANUFACTURED DOUBLE. STOP DRILLED REPAIRED IAW FOKKER SRM 51-31-01, 55-02-03, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1998043000953 19980430 00953 EU 1998 4 30 QXEA9800318 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGER 2.15 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31- 01. 2 L 7 2 4F RT A20EU 1998043000954 19980430 00954 EU 1998 4 30 QXEA9800319 1 19980205 A 5720 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGER 2.17 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31- 01. 2 L 7 2 4F RT A20EU 1998043000955 19980430 00955 EU 1998 4 30 QXEA9800320 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGER 2.18 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31- 01. 2 L 7 2 4F RT A20EU 1998043000956 19980430 00956 EU 1998 4 30 QXEA9800321 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGER 2.19 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31- 01. 2 L 7 2 4F RT A20EU 1998043000957 19980430 00957 EU 1998 4 30 QXEA9800322 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGER 2.20 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31- 01. 2 L 7 2 4F RT A20EU 1998043000958 19980430 00958 EU 1998 4 30 QXEA9800323 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGER 2-21 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31- 01. 2 L 7 2 4F RT A20EU 1998043000959 19980430 00959 EU 1998 4 30 QXEA9800324 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGERR 2-22 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1998043000960 19980430 00960 EU 1998 4 30 QXEA9800325 1 19980205 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT THE WS 1700 AND STRINGER 2.23 THERE IS A CRACK IN THE ATTACH ANGLE CLIP. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51 -31-01. 2 L 7 2 4F RT A20EU 1998043000961 19980430 00961 EU 1998 4 30 QXEA9800326 1 19980205 A 5320 CLIPS FOKKER F28 F28MK4000 4990810 EU WS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 476US 11224 AT WS 1700 AND STRINGER 2.24 THERE IS A CRACK IN THE ANGLE ATTACH CLIPS. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1998043000962 19980430 00962 GL 1998 4 30 98FDEA00201 2 19980315 A 7200 ENGINE DOUG DC10 DC1010F 3022111 WP GE CF6 CF650C 30018 GL NR 3 FAILED A A FDEA E ENGINE SHUTDOWN R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CR CRUISE 1 SO 25 053FE 47807 IN LEVEL CRUISE AT FL350 AND APPROX M.83 NR 3 ENG APPEARED TO FLAMEOUT. ENG INDICATORS STABILIZED AT APPROX N1 33 PERCE NT, EGT 530, NR 65 PERCENT, F/F 600. RED TAB CK LIST ACCOMPLISHED AND ENG RESTARTED AT FL 280. INSP INT AND EXH BOTH C K'D GOOD. FOUND VSV FEEDBACK CABLE OUT OF LIMITS. REMOVED AND REPLACED SAME PER M/M 75-31-01. CK'D CDP LINES FOR BLOC KAGE AND PERFORMED MAX PWR RUN PER JRH. ALL PARAMETERS NORMAL. 2 L 7 3 4F 4 F A22WE A23EA 1998043000963 19980430 00963 WP 1998 4 30 ABXA9800215 1 19980302 A 5712 576946624 RIB DOUG DOUG DC8 DC863F 302198F WP WS 635 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 635.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 050 56. 2 L 7 4 4F 4A25 1998043000964 19980430 00964 WP 1998 4 30 ABXA9800216 1 19980312 A 5712 576946622 RIB DOUG DOUG DC8 DC863F 302198F WP WS 628.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX RIGHT WING LEADING EDGE RIB AT STA XFS 628.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05 056. 2 L 7 4 4F 4A25 1998043000965 19980430 00965 WP 1998 4 30 ABXA9800217 1 19980312 A 5712 5769471 RIB DOUG DOUG DC8 DC863F 302198F WP WS 747.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 747.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 050 56. 2 L 7 4 4F 4A25 1998043000966 19980430 00966 WP 1998 4 30 ABXA980218 1 19980214 A 5712 576947134 RIB DOUG DOUG DC8 DC863F 302198F WP WS 810 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 810.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 050 56. 2 L 7 4 4F 4A25 1998043000967 19980430 00967 WP 1998 4 30 ABXA9800219 1 19980312 A 5712 576947140 RIB DOUG DOUG DC8 DC863F 302198F WP WS 822.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 822.50 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DC8 SRM 57-2-0 AND DWG K 05 056. 2 L 7 4 4F 4A25 1998043000968 19980430 00968 WP 1998 4 30 ABXA9800220 1 19980302 A 5712 576935035 RIB DOUG DOUG DC8 DC863F 302198F WP WS 728.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE RIB AT STA XFS 728.25 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACKED RIB IAW SRM 57-2-0. 2 L 7 4 4F 4A25 1998043000969 19980430 00969 WP 1998 4 30 ABXA980021 1 19980302 A 5320 3754946 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 1220 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 FLOORBEAM END FITTING IS CRACKED AT STA 1220 AND STR 21R. REPAIRED IAW DWG 3754946 AND DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1998043000970 19980430 00970 WP 1998 4 30 ABXA980022 1 19980222 A 5320 5750726176 INTERCOSTAL DOUG DOUG DC8 DC863F 302198F WP BS 400 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 INTERCOSTAL UPPER FLANGE CRACKED AT LONGERON 33R JUST AFT OF FUSE STA 400. REPAIRED IAW DWG 5750726 AND DC8 SRM 51-1-21 . 2 L 7 4 4F 4A25 1998043000971 19980430 00971 WP 1998 4 30 ABXA980023 1 19980222 A 5720 576958339 DOUBLER DOUG DOUG DC8 DC863F 302198F WP WS 330 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 RIGHT WING LEADING EDGE INTERNAL DOUBLER AT STA XFS 330 IS CRACKED. REPAIRED IAW DWG 5769589 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998043000972 19980430 00972 WP 1998 4 30 ABXA9800224 1 19980222 A 5712 576935035 RIB DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 814AX 46041 LEFT WING LEADING EDGE BETWEEN THE NR 1 AND NR 2 PYLONS HAS 3 UPPER RIBS CRACKED. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F 4A25 1998043000973 19980430 00973 WP 1998 4 30 ABXA9800249 1 19980316 A 5610 5613217508 WINDOW DOUG DOUG DC8 DC861 3021952 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 DURING POST FLIGHT, FOUND FIRST OFFICER'S WINDOW (EMERG EXIT) BINDING AND WOULD ONLY OPEN PARTIALLY. LUBRICATED WINDOW IAW DC8 MAINT MANUAL, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998043000974 19980430 00974 WP 1998 4 30 MWEA98346 1 19980313 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 209ME 47730 GALLEY SERVICE DOOR EVACUATION SLIDE FELL OFF. REINSTALLED GALLEY SERVICE DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1998043000975 19980430 00975 NM 1998 4 30 DL72S980564 1 19980312 A 3350 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 21074 EMERGENCY TRACK LIGHTING INOP IN AFT SECTION OF CABIN. 2 L 7 3 4F A3WE 1998043000976 19980430 00976 NM 1998 4 30 DL76L980566 1 19980312 A 2131 211080116 CONTROLLER BOEING 767 767332 1382001 NM NR 1/2 FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 180DN 25985 DURING CLIMB PASSING 17,500 AUTO PRESSURE CONTROL 1 AND 2 FAILED. MANUAL CONTROL WAS ERRATIC PLUS AND MINUS 1000 FT PER MM. REPLACED OUTFLOW VALVE AND BOTH NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS, SYSTEM CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1998043000977 19980430 00977 WP 1998 4 30 DLL10980567 1 19980312 A 3350 516574 POWER PACK LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 193C1180 4R LARGE EXIT SIGN DOES NOT ILLUM WITH EMERG LTS. REPLACED EMERG POWER PACK AT 4R LOCATION. 2 L 7 3 4F A23WE 1998043000978 19980430 00978 NM 1998 4 30 DL72E980570 1 19980313 A 3350 CONNECTOR 900542 BOEING 727 727247 138408F NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W T4167 21481 ON LAYOVER CK, FOUND 2 AFT LEFT OVERWING EMERG EXIT LIGHTS INOP. FOUND CONNECTOR PLUG OFF OF BATTERY PACK FOR AFT O/W B ATTERY PACK. REINSTALLED CONNECTOR CHECKS GOOD. REPLACED BATTERY FOR MIDDLE O/W EXIT LIGHT, NO HELP. REPLACED BATTERY PACK, OPS CKS GOOD. 2 L 7 3 4F A3WE 1998043000979 19980430 00979 NM 1998 4 30 DL72E980571 1 19980220 A 5720 FALSE SPAR BOEING 727 727247 138408F NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 JUST O/B OF NR 5 FLAP TRACK MOUNT, LOWER CAP OF FALSE SPAR IS CRACKED. REPAIRED PER MM 57-55-0 FIG 805. 2 L 7 3 4F A3WE 1998043000980 19980430 00980 NM 1998 4 30 DL72E980572 1 19980220 A 5320 BRACKET BOEING 727 727247 138408F NM BS 930 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 MAIN CABIN STA 930 STRINGER S-14-L BRACKET CRACKED IN RADIUS. TRIMMED OFF DAMGED SECTION OF FRAME AND BEGAN DRILLING RE PAIR PER SRM 53-10-4 FIG 25. DRILLED UP REPAIR PER SRM 53-10-4 FIG 25. INSTALLED REPAIR PER SRM 53-10-4 FIG 25. 2 L 7 3 4F A3WE 1998043000981 19980430 00981 NM 1998 4 30 DL72E980573 1 19980220 A 5311 FRAME BOEING 727 727247 138408F NM BS 930 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 MAIN CABIN STA 930 STRINGER S-13-R FRAME CRACKED. REPAIRED PER 53-10-4 FIG 25 AND ERA 331494. 2 L 7 3 4F A3WE 1998043000982 19980430 00982 NM 1998 4 30 DL757980574 1 19980314 A 3350 BPS73 BATTERY CHARGER BOEING 757 757232 1384965 NM BS 985 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 637DL 23760 DURING L/O CHECK, FOUND LT EMERGENCY OVERWING EXIT LIGHTS OUT. ALSO, FOUND FWD EXTERIOR LIGHT FOR OFF-WING OUT. REPLAC ED LT CHARGER FOR BATTERY PACK M10567 LOCATED ON PSU SPACER PANEL STA 985 LBL 49. 2 L 7 2 4F RT A2NM 1998043000983 19980430 00983 WP 1998 4 30 DLL10980577 1 19980314 A 2840 10648LD2591 BULB LKHEED 1011 10113851 5265010 WP NR 3 ENGINE FAILED A DALA K NONE P NO WARNING INDICATION CL CLIMB 1 SO 27 1732D 193C1213 10113 WHILE CLIMBING THROUGH FL 35.5 NR 3 ENG FLAMED OUT. IT APPEARS THE NR 3 ENG TANK VLV BECAME UNLATCHED. RELATCHED THE N R 3 ENG TANK VLV SWITCH LIGHT AND RESTARTED ENG, BOTH LIGHT BULBS IN FLOW BAR WERE BURNED OUT. REPLACED NR 3 ENG TANK V LV SWITCH LENS ASSY VALVE AND LIGHT LENS OPERATES GOOD. COMPLETED LOST THRUST REPORT AND INSPECTED ENG INLET, EXHAUST A ND CHIP DETECTORS, ALL CKS GOOD. GOOD OIL PRESSURE MAINTAINED DURING EVENT. 2 L 7 3 4F A23WE 1998043000986 19980430 00986 NM 1998 4 30 P5CA9800502 1 19980313 A 8012 START VALVE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE MALFUNCTIONED A P5CA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 WP 23 853FT 19753 685956 ON INITIATING DESCENT, NR 4 ENG START VALVE LIGHT ILLUMINATED STEADY. WHEN HIGH STAGE LIGHT WAS OUT, START VALVE LIGHT WOULD EXTINGUISH. VALVE LIGHT ON STEADY ACCOMPANIED BY HIGH STAGE LIGHT ON. ENG SHUT DOWN ACCOMPLISHED. INSPECTED ALL COMPONENTS, NO DAMAGE TO STARTER OR VALVE. LOCKED OUT THE NR 4 ENG HI-STAGE VALVE PER DDPG 36-01-1. 2 L 7 4 4F 4 F A20WE E20EA 1998043000988 19980430 00988 NM 1998 4 30 P5CA9800504 1 19980316 A 2613 OVERHEAT LIGHT BOEING 747 747123 1384873 NM RT WING ILLUMINATED A P5CA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 23 859FT 20326 ON CLIMBOUT, RT WING OVERHEAT LIGHT CAME ON. APPLIED CHECKLIST AND RETURNED TO JFK. INSPECTED LEADING EDGE DUCT AREA F OR LEAKS AND FAULTY WIRE CONNECTIONS. FOUND LEADING EDGE DUCT BLANKET TORN AND SHORTING WIRES. REPAIRED WIRE AND REPLA CED BLANKET, OPERATIONAL CHECK GOOD PER MM 71-00-00. 2 L 7 4 4F A20WE 1998043000989 19980430 00989 1998 4 30 VNAA9803016 4 19980314 A 2210 7015327901 PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT FAILED A VNAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 07 432JS 48452 6604 3045 WHEN ELECTRICAL POWER WAS APPLIED TO THE AIRCRAFT, THE CREW NOTICED A TRICKLE OF SMOKE COMING FROM THE FLIGHT GUIDANCE C ONTROL PANEL. THE CREW REMOVED ELECTRICAL POWER FROM THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE FLIGHT GUIDA NCE CONTROL PANEL IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 22-11-00. OPERATION CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998043000990 19980430 00990 EU 1998 4 30 AALA980373 1 19980218 A 3230 38000300 CONTROL CABLE FOKKER F28 F28MK0100 4990807 EU MLG BROKEN A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 1417D 11396 COS - FLT 0659 - ON APPROACH COS, LANDING GEAR FAILED TO EXTEND. CYCLED GEAR AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO TUL FOR REPAIR. REPLACED TELEFLEX CABLE AND RIGGED. PERFORMED GEAR EXTENSION AND RETRACTION PROCEDURES WIT H NO DEFECTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998043000991 19980430 00991 WP 1998 4 30 AALA980396 1 19980222 A 4950 B NUT DOUG DC9 DC983 3022083 WP APU LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 566AA 49348 ORD - FLT 0447 - AFTER TAKEOFF, FLIGHT CREW SMELLED AND SAW SMOKE IN COCKPIT. FLIGHT ATTENDANT CONFIRMED THE SAME IN TH E FORWARD CABIN. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED APU AND FOUND A LOOSE B-NUT AT TEE FITTING. TIGHTENED B-NUT AT TEE FITTING WITH NO FURTHER LEAK NOTED. RAN PACKS AND ACCOMPLISHED BURN-OUT WITH N O SMOKE NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998043000992 19980430 00992 WP 1998 4 30 AALA980374 1 19980219 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 581AA 53158 ORD - FLT 1025 - AFTER TAKEOFF, HAD TO CYCLE GEAR TO GET NOSE LANDING GEAR LIGHT TO EXTINGUISH. SERVICED GEAR WITH FLUI D AND NITROGEN. ACCOMPLISHED LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERAT ION. (X) 2 L 7 2 4F A6WE 1998043000993 19980430 00993 EU 1998 4 30 AALA980327 1 19980216 A 3230 201218006 ACTUATOR ROTOL FOKKER F28 F28MK0100 4990807 EU MLG DOWNLOCK DEFECTIVE A AALA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 1404D 11355 ORD - FLT 1721 - UPON GEAR EXTENSION, RECEIVED LEFT AND RIGHT LANDING GEAR UNSAFE INDICATION WITH ASSOCIATED DOORS UNSAF E INDICATION. RECYCLED GEAR WITH NORMAL INDICATIONS. REPLACED LEFT AND RIGHT MAIN GEAR DOWNLOCK ACTUATORS. LEAK CHECK ED WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998043000994 19980430 00994 EU 1998 4 30 AALA980248 1 19980204 A 2750 EAFCD8518411 FLAP CONTL UNIT FOKKER F28 F28MK0100 4990807 EU TE FLAPS DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1433B FBE0219 11418 YYZ - FLT 1611 - AFTER TAKEOFF YYZ, TRAILING EDGE FLAPS WOULD ONLY RETRACT TO 5 DEGREES. AIRCRAFT RETURNED TO YYZ AND L ANDED WITHOUT INCIDENT. REPLACED FLAP CONTROL DATA UNIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. FUNCTIONAL CHECK FL IGHT ACCOMPLISHED WITH NO DEFECTS NOTED. (X) 2 L 7 2 4F RT 1998043000995 19980430 00995 EU 1998 4 30 AALA980240 1 19980130 A 2910 CDK2638 COUPLER FOKKER F28 F28MK0100 4990807 EU NR 2 HYD SYS DEFECTIVE A AALA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 07 1407D 11360 OKC - FLT 1537 - EN ROUTE ORD/OKC, MFDU DISPLAYED HYDRAULIC SYSTEM TWO QUANTITY MESSAGE. FLIGHT CREW VERIFIED QUANTITY ON OVERHEAD PANEL AND TURNED OFF SYSTEM TWO PUMPS. AIRCRAFT CONTINUED TO OKC AIRPORT AND LANDED WITHOUT INCIDENT. REPL ACED LEAKING QUICK DISCONNECT COUPLING ON SYSTEM TWO HYDRAULIC PUMP AND SERVICED SYSTEM TO FULL. SYSTEM OPERATED NORMAL LY WITH NO LEAKAGE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998043000996 19980430 00996 EU 1998 4 30 AALA980103 1 19980113 A 2750 A83235417 SYNCRO FOKKER F28 F28MK0100 4990807 EU RT WING DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1407D A59152173 11360 DFW - FLT 0432 - AFTER TAKEOFF, FLAPS WERE SELECTED UP AND THE CREW RECEIVED A FLAP ASYMMETRY MESSAGE ON MFDU. AIRCRAFT RETURNED AND LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT HAND MIDDLE FLAP SYNCRO AND CYCLED FLAPS WITH NO FAULTS. SYS TEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998043000997 19980430 00997 EU 1998 4 30 AALA980395 1 19980222 A 2150 9787344 VALVE GARRTT P657 AIRBUS 300 A300B4605R 3930308 EU NR 1 ENGINE DEFECTIVE A AALA A G B UNSCHED LANDING O2 MASK DEPLOYED EMER. DESCENT O OTHER CL CLIMB 1 SW 07 50051 459 SJU - FLT 1915 - DURING CLIMB-OUT, NR 2 PACK FAILED AT 25,000 FEET AND CABIN ALTITUDE CONTINUED TO CLIMB AT 1,000 FEET P ER MINUTE. NR 1 PACK FAILED AND BOTH PACKS UNABLE TO BE RESET. OXYGEN MASKS DEPLOYED AT 14,000 CABIN ALTITUDE DURING E MERGENCY DESCENT. AIRCRAFT AIR INTERRUPTED AND RETURNED SJU AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE FAN AIR VALVE AND RESECURED CLAMPS AT RIGHT SIDE OF PACK. ACCOMPLISHED LEAK AND OPERATIONAL CHECKS OF SYSTEM WITH NO FAULTS NOT ED. PASSENGER OXYGEN MASKS WERE REPACKED ADN OXYGEN BOTTLES REPLACED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998043000998 19980430 00998 NM 1998 4 30 AALA980403 1 19980224 A 3350 44MY232796 SWITCH GRAYHILL BOEING 767 767323 1385205 NM L4 DOOR SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379AA 25448 LAX - DURING OVERNIGHT CHECK, CABIN EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED SHORTED EMERGENCY LIGHT SWITCH AT L 4 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998043000999 19980430 00999 NM 1998 4 30 AALA980380 1 19980221 A 3350 P4010051 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 640A 24598 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPLACED EMERGENC Y DOOR PATH LIGHTING MODULES AT SEAT ROWS 3 AND 9. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998043001000 19980430 01000 WP 1998 4 30 AALA980399 1 19980223 A 3260 5543151 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A AALA K NONE P NO WARNING INDICATION AP APPROACH 1 SW 07 298AA 49310 ORD - FLT 1418 - DURING APPROACH TO ORD WITH THROTTLES AT IDLE, NOSE LANDING GEAR UNSAFE LIGHT DID NOT ILLUMINATE. AIRC RAFT LANDED ORD WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR UP SENSOR AND TARGET OUT OF LIMITS. ADJUSTED NOS E LANDING GEAR UP SENSOR AND TARGET PER MM LIMITS. ACCOMPLISHED NOSE LANDING GEAR RETRACTION CHECK CYCLING GEAR SEVERAL TIMES WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998043001001 19980430 01001 NM 1998 4 30 AALA980397 1 19980223 A 3397 WIRE BOEING 767 767223 1385123 NM L1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 322AA 22323 SFO - FLT 0041 - DURING MAINTENANCE, EMERGENCY EXIT SIGN AT L1 DOOR FOUND INOPERATIVE. REPAIRED EMERGENCY EXIT SIGN BRO KEN WIRE AT L1 FLIGHT ATTANDANT SEAT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998043001002 19980430 01002 NM 1998 4 30 AALA980401 1 19980224 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 607AM 27058 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS WERE INOPERATIVE. REPLACED EMERGENC Y FLOOR PATH LIGHTING FORWARD MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998043001003 19980430 01003 WP 1998 4 30 AALA980412 1 19980226 A 3260 SS092200017019 SWITCH UNIT DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 07 7530 49922 49922 ORD - FLT 0424 - AFTER TAKEOFF WITH NORMAL GEAR RETRACTION, THE GEAR UNSAFE LIGHTS ILLUMINATED WITH GEAR HANDLE UP ON AL L THREE GEARS. AIRCRAFT CONTINUED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED RIGHT THROTTLE SWITCH SYSTEM AND CYCLED GEAR SEVERAL TIMES WITH NO FURTHER FAULTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998043001004 19980430 01004 WP 1998 4 30 AALA980394 1 19980222 A 2130 1500P0228 SWITCH DOUG DC9 DC982 3022082 WP LT PACK DEFECTIVE A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 492AA 2267 49730 ATL - FLT 1491 - DURING CRUISE, BOTH AIRFLOW METERS WENT TO ZERO FLOW AND LIGHT ILLUMINATED. CABIN CONTINUED TO CLIMB W ITH OUTFLOW VALVE CLOSED. PERFORMED ALTERNATE PROCEDURE, MIXING VALVES WOULD NOT MOVE. BEGAN DESCENT AND CABIN AND AIR PLANE MET AT 10,000 FEET. AIR INTERRUPTED AND LANDED ATL WITHOUT FURTHER INCIDENT. REPLACED LEFT HAND PRESSURE DIFFERE NTIAL SWITCH. ACCOMPLISHED SYSTEM FUNCTIONAL CHECK OF PACK. SHUTDOWN PRESSURE SWITCH WITH NORMAL OPERATION. SYSTEM G ROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998043001005 19980430 01005 NM 1998 4 30 AALA980318 1 19980215 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6823 19701 ORD - DURING OVERNIGHT MAINTENANCE, RIGHT AFT CARGO DOOR EMERGENCY LIGHTS ILLUMINATED WHEN ALL POWER WAS REMOVED FROM TH E AIRCRAFT. LIGHTS WENT OUT WHEN POWER WAS APPLIED. DURING TROUBLESHOOTING, COULD NOT DUPLICATE PROBLEM. SYSTEM GROUN D CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998043001006 19980430 01006 NM 1998 4 30 AALA980365 1 19980218 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 725AA 20732 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS OVER AFT SERVICE DOOR INOPERATIVE. RESECURED LIGHT ASSEMBLY FOR EM ERGENCY LIGHTS OVER AFT SERVICE DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998043001007 19980430 01007 EU 1998 4 30 AALA980254 1 19980205 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1413A 11376 ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT AISLE LIGHTS LEFT SIDE INOPERATIVE. REPLACED WIRE AT EMERGENCY EXIT AISLE, LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998043001008 19980430 01008 NM 1998 4 30 AALA980364 1 19980218 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 725AA 20732 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS OVER FORWARD GALLEY DOOR INOPERATIVE. RESEATED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS OVER FORWARD GALLEY DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998043001009 19980430 01009 NM 1998 4 30 AALA980354 1 19980218 A 2421 GENERATOR BOEING 767 767223 1385123 NM RT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 338AA 22335 RDU - FLT 0173 - RIGHT DRIVE CAME ON DURING CLIMB-OUT FL 280. DISCONNECT PROCEDURE WAS DONE IAW MANUAL. PLACARDED RIGH T ENGINE GENERATOR INOPERABLE PER MEL RF NR 24-1 AUTH 2-280DC-B. TRANSFERRED TO MIC SHEET. SERVICED BOTH IDGS AND APU OIL. GENERATOR DISCONNECTED. REMOVED AND REPLACED RIGHT ENGINE GENERATOR PER MM. OPS CHECKED AND LEAK CHECK GOOD. RE MOVED MEL PLACARD 24-1 AUTH NR 2-28-0DC-B. CLEARED MIC SHEET. 33824FA00/1627.17FEB.RDU. (X) 2 L 7 2 4F RT A1NM 1998043001010 19980430 01010 NM 1998 4 30 AALA980347 1 19980217 A 2421 IDG BOEING 757 757223 1384957 NM LT ENGINE FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 687AA 25695 ORD - FLT 2228 - GENERATOR DRIVE LIGHT CAME ON WITH EICAS MESSAGE. GENERATOR DRIVE DISCONNECTED. RAN ENGINES TO CONFIR M LEFT IDG HAD PROBLEM. PLACARDED LT IDG INOP PER MEL. REF 24-1 AUTH 2-303-DC-B. CHECKED AND SERVICED BOTH IDG'S AND A PU PER MEL, ALL FULL. ENTERED IN MIC SHEET. INSTALLED SERVICEABLE LEFT ENGINE IDG. OPS CHECK NORMAL, MEL 24-1. AUTH 2-303DC-B. CLEARED MIC, CLEARED 5DE24C6F1/1426.14FEB.ORD. (X) 2 L 7 2 4F RT A2NM 1998043001011 19980430 01011 NM 1998 4 30 AALA980368 1 19980219 A 2421 IDG BOEING 767 767323 1385205 NM RIGHT FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 386AA 27060 JFK - FLT 0016 - DURING CRUISE AT FL 370, RIGHT GENERATOR DRIVE LIGHT BEGAN FLICKERING. A FEW MINUTES LATER, THE GENERA TOR DRIVE MESSAGE ON THE EICAS CAME ON AND CREW DISCONNECTED THE IDG PER PROCEDURES. REPLACED RT IDG, RAN NR 2 ENGINE. ALL PARAMETERS NORMAL. LEAK CHECK OK. OK FOR SERVICE. 386242DC4/2155.18FEB.JFK. (X) 2 L 7 2 4F RT A1NM 1998043001012 19980430 01012 NM 1998 4 30 AALA980144 1 19980116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - CORROSION ON FLOOR BEAM STA 380 FROM RBL 12 TO RBL 24. REMOVED CORRODED SECTION, INSTALLED NEW PART AND DOUBLER P ER SRM 53-10-8. TST: 56,192 HOURS. CYCLES: 34,665. X) 2 L 7 3 4F A3WE 1998043001013 19980430 01013 WP 1998 4 30 AALA980307 1 19980210 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON BELL FRAME FROM STR 50R TO STR 49L AT STA 879. REMOVED CORROSION, INSTALLED DOUBLER. REPAIRED IAW S RM 53-30-00. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001014 19980430 01014 WP 1998 4 30 AALA980251 1 19980204 A 5311 LONGERON DOUG DC10 DC1010 3022110 WP BS 1139 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 BELL FRAME HAS CORROSION BETWEEN 50L AND 50R STA 775. INSTALLED REPAIR ANGLE PER SRM 53-30-00 PAGE 31. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001015 19980430 01015 WP 1998 4 30 AALA980344 1 19980212 A 5320 INTERCOSTAL DOUG DC10 DC1010 3022110 WP BS 859 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON INTERCOSTAL ABOVE STR 43L FROM STA 859 - STA 879. REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW PER IAW CHAP 51 OF SRM AND AARRD 51-01-00-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001016 19980430 01016 WP 1998 4 30 AALA980343 1 19980212 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1781 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON ANGLE AT STA 1781 TRACKS 1 AND 2, TERMINATING END OF CARGO COMPARTMENT FLOOR AT BULKHEAD. REMOVED AN D REPLACED ANGLE FITTING PER SRM 51-21-00 VOL II. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001017 19980430 01017 WP 1998 4 30 AALA980342 1 19980212 A 5320 DOOR FRAME DOUG DC10 DC1010 3022110 WP BS 869 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION AT LEFT CARGO/GALLEY DOOR FRAME BOTTOM INSIDE, STA 869 AND STR 48L. REMOVED CORRODED ANGLE FRAME AND IN STALLED NEW FRAME PER IAW CHAPTER 51 OF SRM AND AARD 51-02-00-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001018 19980430 01018 WP 1998 4 30 AALA980306 1 19980211 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 825 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - FLOORBOARD SUPPORT HAS CORROSION AT STA 825 BETWEEN ROLLER TRAYS AND 1 AND 2. REMOVED CORROSION, FABRICATED NEW S UPPORT AND INSTALLED IAW AARD 51-10-00-21. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001019 19980430 01019 WP 1998 4 30 AALA980263 1 19980205 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 623 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - NR 1 ROLLER TRAY HAS CORROSION ON FWD ATTACH ANGLE CLIP STA 623. FABRICATED NEW CLIP ANGLE AND INSTALLED IAW AARD 51-10-00-1. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001020 19980430 01020 WP 1998 4 30 AALA980259 1 19980204 A 5320 GUIDE RAIL DOUG DC10 DC1010 3022110 WP BS 1561 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CENTER CARGO LT SIDE GUIDE RAIL HAS CORROSION FROM STA 1561 - STA 1621. REMOVED AND REPLACED GUIDE RAIL PER AARD 51-00-00-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001021 19980430 01021 WP 1998 4 30 AALA980331 1 19980216 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1781 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION AT STA 1781 AFT LOWER WALL SUPPORT. REMOVED AND REPLACED MANUFACTURED SUPPORT PER AARD 51-01-00-05. TS T: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001022 19980430 01022 WP 1998 4 30 AALA980332 1 19980216 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ALONG SLANT PANEL TO FLOOR ATTACH ANGLE. REMOVED AND REPLACED PER 51-21-01. TST: 60,422.53 HOURS. CY CLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001023 19980430 01023 WP 1998 4 30 AALA980333 1 19980216 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1967 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON AFT LOWER FLOORBOARD TO BULKHEAD ATTACH ANGLE IN AFT CARGO. REMOVED AND REPLACED PART PER 51-10-01. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001024 19980430 01024 NM 1998 4 30 AALA980160 1 19980116 A 5320 DOOR FRAME BOEING 727 727223 1384074 NM BS 1030 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - RIGHT AFT SERVICE DOOR FRAME CORRODED - HINGE CASTING AREA. REPLACED LOWER STOP PAD CASTING. REMOVED CORROSION F ROM FRAME AND INSTALLED REPAIR DOUBLER PER 51-40-3 FIG 1 PAGES 1-6. (X) 2 L 7 3 4F A3WE 1998043001025 19980430 01025 WP 1998 4 30 AALA980319 1 19980213 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 BLENDED CORROSION FROM FLOOR BEAM - OUT OF LIMITS. MADE AND INSTALLED FLOORBEAM END AND SPLICE, ALODINED AND PRIMED. S RM VOL II 51-21-01, SRM VOL I 53-60-01-3. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001026 19980430 01026 NM 1998 4 30 AALA980146 1 19980116 A 5320 DOOR FRAME BOEING 727 727223 1384074 NM BS 376 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - TWO AREAS OF CORROSION ON FORWARD LIP OF DOOR FRAME, STR 15R TO STR 16R. BLENDED OUT CORROSION (TWO AREAS) AND IN STALLED REPAIR DOUBLER PER ESO 11697 DATED 1-6-98. TST: 56,192 HOURS. CYCLES: 34,665. (X) 2 L 7 3 4F A3WE 1998043001027 19980430 01027 WP 1998 4 30 AALA980330 1 19980213 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 770 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - AREAS OF CORROSION ON ROLLER TRAY NR 1 FROM STA 770 - STA 879. SPLICED IN NEW TRACK PER SRM 53-70-00. TST: 60,4 22.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001028 19980430 01028 WP 1998 4 30 AALA980336 1 19980215 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - NR 4 ROLLER TRAY HAS NUMEROUS SPOTS OF CORROSION FROM STA 760 TO STA 595. REMOVED CORRODED TRACK, FABRICATED NEW TRACK AND REINSTALLED PER SRM 51-01-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001029 19980430 01029 WP 1998 4 30 AALA980335 1 19980215 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 800 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - NUMEROUS SPOTS OF CORROSION IN ROLLER TRAY NR 4 BETWEEN STA 879 AND STA 769. REMOVED CORRODED SECTION OF TRACK, F ABRICATED NEW AND INSTALLED PER SRM 51-01-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001030 19980430 01030 WP 1998 4 30 AALA980334 1 19980215 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 862 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION IN ROLLER TRAY NR 4 STA 859 TO STA 865. REMOVED CORRODED SECTION OF TRACK, FABRICATED NEW AND INSTALLED PER SRM 51-01-05. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001031 19980430 01031 WP 1998 4 30 AALA980341 1 19980214 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 745 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - NR 2 ROLLER TRAY HAS NUMEROUS AREAS OF CORROSION STA 745 - STA 875. SPLICED IN NEW TRAY FROM STA 840 - STA 875 PE R SRM 53-70-00 VOL I. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001032 19980430 01032 WP 1998 4 30 AALA980360 1 19980217 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 595 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - NR 2 ROLLER TRAY HAS CORROSION FROM STA 595 - STA 745. SPLICED IN NEW TRAY SECTION PER SRM 53-70-00. TST: 60,42 2.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001033 19980430 01033 WP 1998 4 30 AALA980361 1 19980217 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 879 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 CORROSION ON ROLLER TRAY NR 5 JUST FORWARD OF STA 879 (X +66). CORRODED SECTION OF TRAY REPLACED PER AARD 51-10-00-05 A ND ALODINED, TREATED, PRIMED, AND PAINTED PER SRM 51-21-01 VOL II. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001034 19980430 01034 WP 1998 4 30 AALA980362 1 19980217 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 859 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 ROLLER TRAY NR 5 HAS CORROSION ON LOWER SURFACE AFT OF STA 859 (X +166). CORRODED SECTION OF TRAY REPLACED PER AARD 51- 01-00-5 AND ALODINED, TREATED, PRIMED AND PAINTED PER SRM 51-21-01 VOL II. TST: 60,422.53 HOURS. CYCLES: 20,166. (X ) 2 L 7 3 4F A22WE 1998043001035 19980430 01035 WP 1998 4 30 AALA980260 1 19980204 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 1661 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - NR 1 ROLLER TRAY HAS CORROSION STA 1661. REMOVED AND REPLACED TRAY PER AARD 51-01-00-05. SPLICED PER SRM 53-70-0 0 FIG 7. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001036 19980430 01036 WP 1998 4 30 AALA980265 1 19980205 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 1601 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - NR 4 ROLLER TRAY HAS CORROSION FROM STA 1601 - STA 1701. REMOVED CORROSION AND SPLICED TRAY STA 1641 PER SRM 53-7 0-00 VOL I. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001037 19980430 01037 WP 1998 4 30 AALA980261 1 19980204 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 1561 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - ROLLER TRAY NR 1 HAS CORROSION AT STA 1621 - STA 1561. REMOVED AND REPLACED TRAY TRACK PER SRM 53-70-00 FIG 7. T ST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001038 19980430 01038 WP 1998 4 30 AALA980320 1 19980213 A 5320 SILL DOUG DC10 DC1010 3022110 WP CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 CORROSION AROUND RIV-NUT ON AFT SIDE DOOR SILL FACET. TREATED, PAINTED, AND PRIMED AREA PER SRM 51-21 VOL II. DAMAGED AREA OK FOR SERVICE PER ESO 7349 DATED 2-10-98. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001039 19980430 01039 WP 1998 4 30 AALA980340 1 19980304 A 5320 POST DOUG DC10 DC1010 3022110 WP BS 875 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON ANGLE PANEL AND CASTING AROUND WALL POST AT FLOORING FOR AIRCRAFT C-LIFT DOOR ATTACH POINT STA 875. I NSTALLED NEW ANGLE WEB. SPLICED TOGETHER PER IAW 51-01-00-05, AARD CHAPTER 51, AND 53-00-01 - ESO 7349 DATED 2-12-98. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001040 19980430 01040 WP 1998 4 30 AALA980339 1 19980215 A 2530 TRACK DOUG DC10 DC1010 3022110 WP GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - REMOVED CORRODED GALLEY TRACK SECTION, FABRICATED NEW PIECE, AND INSTALLED IAW 51-10-00-01 AND 51-01-00-05 OF AARD CHAPT 51 OF SRM. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001041 19980430 01041 WP 1998 4 30 AALA980338 1 19980215 A 2530 TRACK DOUG DC10 DC1010 3022110 WP GALLEY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON LT SLIDING DOOR FORWARD TRACK AT STA 879. REMOVED CORRODED PIECE, FABRICATED NEW AND INSTALLED IAW S RM 51-10-00-01 AND 51-01-00-05 OF AARD 53-00-01 SRM. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001042 19980430 01042 WP 1998 4 30 AALA980337 1 19980215 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 876 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION UNDER LT SLIDING DOOR AFT SIDE ANGLE STA 876 FORWARD AND INBOARD OF ROLLER TRAY NR 2 IN CARGO. REMOVED C ORRODED PIECE, FABRICATED NEW AND INSTALLED PER SRM 51-10-00-01 AND 51-01-00-05 OF AARD AND SRM CHAPTER 51. TST: 60,42 2.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001043 19980430 01043 WP 1998 4 30 AALA980266 1 19980205 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1900 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - CORROSION ON FLOOR SUPPORT. REMOVED AND REPLACED SUPPORT SRM AND AARD 51-01-00. ALODINED, PRIMED AND PAINTED PER SRM 51-21-01. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001044 19980430 01044 WP 1998 4 30 AALA980262 1 19980205 A 2550 SPROCKET BOX DOUG DC10 DC1010 3022110 WP BS 1781 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - RIGHT LOAD SYSTEM SPROCKET BOX HAS CORROSION AROUND NUT PLATES AND FITTING LOCATED ABOVE STR 47R. DRILLED OUT HOL ES, INSTALLED NEW SPROCKET BOX PER 51-21-02 AND 51-01-00-01. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001045 19980430 01045 NM 1998 4 30 AALA980229 1 19980128 A 5310 STRUCTURE BOEING 727 727223 1384074 NM BS 580-600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - CORROSION ON SKIN STR 28L AND INTERCOSTAL STA 580 - STA 600. REMOVED CORROSION AND INSTALLED SKIN DOUBLER PER SRM 53-30-3 FIG 3 AND SPLICED IN NEW SECTION FO STR 28L PER SRM 53-10-3 FIG 1 AND REPLACED INTERCOSTAL. TST: 60,422.53 HO URS. CYCLES: 20,166. (X) 2 L 7 3 4F A3WE 1998043001046 19980430 01046 WP 1998 4 30 AALA980292 1 19980207 A 2550 SIDE RAIL DOUG DC10 DC1010 3022110 WP BS 1063-1102 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - RIGHT PALLET SIDE RAIL HAS CORROSION FROM STA 1063 TO STA 1102. INSTALLED/SPLICED IN FABRICATED PIECE PER SRM 51- 00-00. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001047 19980430 01047 NM 1998 4 30 AALA980241 1 19980130 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FLOOR TRACK LIGHTING INOPERABLE. INSTALLED NEW EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROW 5 AND ROW 6. INSTALLED NEW CONNECTOR ON EMERGENCY FLOOR TRACK POWER WIRES AT ROW 30. OPS CHECKED OK. TST: 70,613 HOURS. CYCLES: 47,995. ( X) 2 L 7 3 4F A3WE 1998043001048 19980430 01048 NM 1998 4 30 AALA980155 1 19980116 A 5530 STRINGER BOEING 727 727223 1384074 NM VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - STRINGER CRACKED AT BOLT HOLE INSIDE VERTICAL STABILIZER, BAY NR 10, RT SIDE, 4TH STRINGER FROM BOTTOM. INSTALLED DOUBLER ON CRACKED AREA OF STRINGER PER SRM 55-30-4 FIG 1 AND ESO 11697 DATED 1-14-98. TST: 56,192 HOURS. CYCLES: 3 4,665. (X) 2 L 7 3 4F A3WE 1998043001049 19980430 01049 WP 1998 4 30 AALA980264 1 19980205 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1139 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 131AA 46994 TUL - LONGERON 52 CORRODED AT STA 1139. REPLACED STR 52 FROM 1156 TO 1139, REINSTALLED BELL FRAMES AND SHEAR TIES PER S RM AARD 51-01-00-05. TREATED, PRIMED AND PAINTED PER SRM 51-21-01 VOL 4. TST: 60,422.53 HOURS. CYCLES: 20,166. (X) 2 L 7 3 4F A22WE 1998043001050 19980430 01050 WP 1998 4 30 VJ9800049 1 19980318 A 3350 CO030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A VJ6A K NONE L NO TEST IN INSP/MAINT 1 SO 11 939VV 47089 FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPS CHECKED NORMAL IAW MM 33-50-0. 2 L 7 2 4F A6WE 1998043001051 19980430 01051 EU 1998 4 30 MALA976053 1 19980315 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 595MA 340B216 ON DEPARTURE, THE LANDING GEAR DID NOT RETRACT WITH PROPER PRESSURE ON HYDRAULIC GAUGE. CREW RECYCLED AS PER QRH AND TH E GEAR DID RETRACT. AIRCRAFT LANDING IN DTW WITHOUT INCIDENT. MAINTENANCE PERFORMED SEVERAL OPS CHECKS, BLED AND SEVIC ED HYDRAULIC SYSTEM. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998043001052 19980430 01052 EU 1998 4 30 MALA976054 1 19980315 A 3350 CONNECTOR BAC 146 AVRO146RJ85A 1500097 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 506XJ E2314 DURING INSPECTION FLIGHT ATTENDANT REPORTED, NUMEROUS EMERGENCY LIGHTS INOP. MAINTENANCE FOUND LOOSE CANNON PLUG ON AFT BATTERY PACK. RESECURED PLUG, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998043001053 19980430 01053 NM 1998 4 30 CALA9800463 1 19980316 A 5330 SKIN BOEING 727 727243 138408D NM BS 417 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A 2 INCH CRACK IN R-1 DOOR CUTOUT AT FS 417. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5307-01141. 2 L 7 3 4F RT A3WE 1998043001054 19980430 01054 NM 1998 4 30 CALA9800464 1 19980316 A 5753 652163091 FOREFLAP BOEING 727 727243 138408D NM LT TE FLAP DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND LT INBOARD FOREFLAP CRUSHED (4 AREA) AT INBOARD END. THE FOREFLAP WAS REMOVED AND REPLACED. 2 L 7 3 4F RT A3WE 1998043001055 19980430 01055 NM 1998 4 30 CALA9800465 1 19980316 A 5720 BEAM BOEING 727 727243 138408D NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A .5 INCH CRACK IN J-BEAM ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE J-BEAM WAS REPAIRED IAW ECRA 5750-02193 AND EA 26865-5075. 2 L 7 3 4F RT A3WE 1998043001056 19980430 01056 NM 1998 4 30 CALA9800466 1 19980316 A 5610 WINDOW BOEING 727 727243 138408D NM R-1 POSITION DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A BURNED SPOT AND A DELAMINATION BUBBLE IN R-1 WINDOW UPPER EDGE. THE R-1 WINDOW WAS REMOVED AND REPLA CED IAW MM 56-11-11. 2 L 7 3 4F RT A3WE 1998043001057 19980430 01057 NM 1998 4 30 CALA9800467 1 19980316 A 5755 SKIN BOEING 727 727243 138408D NM NR 7 SPOILER WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A GROOVE WORN ON BOTTOM OF LT WING NR 7 SPOILER. THE NR 7 SPOILER WAS REMOVED AND REPLACED. 2 L 7 3 4F RT A3WE 1998043001058 19980430 01058 NM 1998 4 30 CALA9800468 1 19980316 A 5347 FLOOR TRACK BOEING 727 727243 138408D NM BS 380-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND FLOOR TRACK CORRODED AT STA 380 TO 420, RBL 25. THE TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED A ND INSTALLED IAW SRM 53-05-01 AND 51-10-01. 2 L 7 3 4F RT A3WE 1998043001059 19980430 01059 NM 1998 4 30 CALA9800469 1 19980317 A 5720 STIFFENER BOEING 727 727243 138408D NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17410 21663 INSPECTION FOUND A .1562 INCH CRACK THROUGH FASTENER HOLE AT BOTTOM OF STIFFENER AT INBOARD SIDE OF LT WING LEADING EDGE RIB, WBL 92.0, ACCESS CUTOUT 6303. A REPAIR WAS INSTALLED IAW SRM 51-14-1. 2 L 7 3 4F RT A3WE 1998043001060 19980430 01060 NM 1998 4 30 CALA9800470 1 19980317 A 3350 20131A BATTERY RADIANT BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14337 23575 THE FORWARD SERVICE DOOR EXIT SIGN FAILED TEN MINUTE BURN DURATION TEST. THE BATTERY WAS REPLACED AND A WIRE WAS RECONN ECTED, OPERATIONAL TEST WAS GOOD. 2 L 7 2 4F RT A16WE 1998043001061 19980430 01061 NE 1998 4 30 9804466603 2 19980316 A 7200 ENGINE BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 4 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 01 603US 19780 662615 AFTER REACHING CRUISE AT FL350, THE NR 4 ENGINE FLAMED OUT. WHILE DESCENDING, THE CREW ATTEMPTED THREE RESTARTS OF THE NR 4 ENGINE WITH THE LAST ONE SUCCESSFUL AT FL250. ALL ENGINE PARAMETERS INDICATED NORMAL AFTER THE RESTART SO THE AIRC RAFT CLIMBED BACK TO FL350 AND CONTINUED TO NRT WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED. THE FUEL FILTER AND PH FILTER WERE REPLACED AND THE AIRCRAFT CONTINUED IN SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1998043001062 19980430 01062 EU 1998 4 30 9804473231 1 19980316 A 3350 100865 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 331NW 318 DURING TEST OF EMERGENCY FLOOR PATH LIGHTING, FOUND LIGHTS INOPERATIVE AT SEAT ROWS 19-21 AND 25-27. MAINTENANCE REPLAC ED THE BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998043001063 19980430 01063 WP 1998 4 30 9804489860 1 19980317 A 2780 59268805501 VALVE DOUG DC9 DC951 3022051 WP LE FLAPS INOPERATIVE A NWAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 01 769NC 42481 42461 47757 DURING DESCENT, THE SLAT DISAGREEMENT INDICATION ILLUMINATED WHEN LEADING EDGE SLAT DE-VICES WERE EXTENDED. FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARED EMERGENCY AND LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE SLAT CONTROL VALVE, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043001064 19980430 01064 WP 1998 4 30 9804499615 1 19980316 A 2130 CONNECTOR DOUG DC9 DC932 3022066 WP E/E COMPT DAMAGED A NWAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 01 615NW 47129 LOSS OF CABIN PRESSURE OCCURRED DURING CRUISE FLIGHT AT 31,000 FEET. CABIN PRESSURE WARNING LIGHT ILLUMINATED WITH DROP IN DIFFERENTIAL PRESSURE. CREW INITIATED RAPID DESCENT TO 15,000 FEET AND FLIGHT WAS CONTINUED TO DESTINATION. CABIN RPESSURE STABILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED DAMAGED AIR/GROUND CHECK VALVE CONNECTOR , OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998043001065 19980430 01065 WP 1998 4 30 9804509860 1 19980318 A 2420 GEN CONTL PNL DOUG DC9 DC951 3022051 WP FLIGHT DECK MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 769NC 47757 DURING CLIMBOUT, THE LEFT ENGINE DRIVEN GENERATOR TRIPPED OFF LINE TOGETHER WITH AN AC CROSSTIE LOCKOUT. THE FLIGHT CRE W SUCCESSFULLY RESET THE LEFT ENGINE DRIVEN GENERATOR. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAC ED THE GENERATOR CONTROL PANEL AND AC BUS CONTROL UNIT, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998043001066 19980430 01066 WP 1998 4 30 9804519308 1 19980316 A 3350 SWITCH DOUG DC9 DC982 3022082 WP FLIGHT DECK INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 311RC 48089 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS WOULD NOT EXTINGUISH WITH OFF SWITCH. MAINTENANCE REPLACED FLIGHT DECK E MERGENCY EXIT LIGHT SWITCH, OPERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998043001067 19980430 01067 WP 1998 4 30 9804529163 1 19980316 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8906E 45747 DURING LINE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES, OP ERATIONAL CHECK OK. 2 L 7 2 4F A6WE 1998043001068 19980430 01068 WP 1998 4 30 9804539601 1 19980317 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 601NW 47038 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTE RY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998043001069 19980430 01069 WP 1998 4 30 9804549978 1 19980317 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING PERIODIC CHECK, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998043001070 19980430 01070 WP 1998 4 30 9804559914 1 19980316 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 964N 47416 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 18 THRU 20 INOPERATIVE. REPLACED BROKEN WIRE UN DER SEATS 19DEF, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998043001071 19980430 01071 WP 1998 4 30 9804569989 1 19980316 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY PATH LIGHTS IN TAIL CONE CATWALK AREA INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998043001072 19980430 01072 EA 1998 4 30 COMA9860061 1 19980316 A 3230 PIN CNDAIR CL600 CL6002B19 EA NOSE GEAR INSTALLED A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 971CA 7145 NLG WILL NOT RETRACT. REMOVED NLG, DOWN LOCK SAFETY PIN. 2 L 7 2 4F RT A21EA 1998043001073 19980430 01073 NM 1998 4 30 SWAA980271 1 19980313 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 774-857 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND VERTICAL SUPPORT WEB TIE STRAP CORRODED AT BS 774 TO 857, RBL 19 WL 164. REMOVED AND RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001074 19980430 01074 NM 1998 4 30 SWAA980272 1 19980313 A 3350 A3060195102 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 503SW 24180 DURING EMERGENCY ESCAPE SLIDE TEARDOWN IN SHOP, FOUND ONE LIGHT STRIP LAMP INOP. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998043001075 19980430 01075 NM 1998 4 30 SWAA980273 1 19980313 A 5320 ANGLE BOEING 737 7372H4 138448C NM AFT LAV CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND L-ANGLE ON TOP OF AFT LAV DOOR SUPPORT INTERCOSTAL HAS CORRODED. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001076 19980430 01076 NM 1998 4 30 SWAA980274 1 19980313 A 5247 DOUBLER BOEING 737 7372H4 138448C NM APU DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED C3 CHECK, FOUND APU DOOR FWD HINGE AFT ANGLE BRACKET DOUBLER CRACKED IN RADIUS. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1998043001077 19980430 01077 NM 1998 4 30 SWAA980275 1 19980313 A 5320 FITTING BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT FITTING AT BS 867, STR 8L AND 9L. REPAIRED PER TRAMCO EWO 98-0042. 2 L 7 2 4F RT A16WE 1998043001078 19980430 01078 NM 1998 4 30 SWAA980276 1 19980313 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907, STR 4L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001079 19980430 01079 NM 1998 4 30 SWAA980277 1 19980313 A 5400 ANGLE BOEING 737 7373H4 1384600 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON AFT LOWER L STIFFENER CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001080 19980430 01080 NM 1998 4 30 SWAA980278 1 19980313 A 5400 ANGLE BOEING 737 7373H4 1384600 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON UPPER AFT I/B L-CLIP CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001081 19980430 01081 NM 1998 4 30 SWAA980279 1 19980313 A 5400 SUPPORT BOEING 737 7373H4 1384600 NM LT PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED D-CHECK, FOUND L/W PYLON I/B T/E SUPPORT LONGERON UNDER SPRING DOOR ASSY IS CRACKED. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998043001082 19980430 01082 NM 1998 4 30 SWAA980280 1 19980313 A 5730 PANEL BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED C4 CHECK, FOUND LEFT WING UPPER SURFACE TRAILING EDGE PANEL HAS TWO CRACKS. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001083 19980430 01083 NM 1998 4 30 SWAA980281 1 19980313 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 524 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND DENT IN SKIN AT BS 524, 3 ABOVE STR 26 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001084 19980430 01084 NM 1998 4 30 SWAA980282 1 19980313 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORROSION AT BS 727 TO 947 LBL 3 WL 159, BS 727 TO 947 RBL 3 WL 159, BS 727 TO 947 RBL 8 WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001085 19980430 01085 NM 1998 4 30 SWAA980283 1 19980313 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 700 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND LT WHEEL WELL ATTACH ANGLE AT BS 700 WL 152 TO 172, LBL 57 HAS MECHANICAL DAMAGE ON THE OUTBOARD FLANGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001086 19980430 01086 NM 1998 4 30 SWAA980284 1 19980313 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACKED SUPPORT ANGLE AT BS 727+2, RBL 3 WL 162. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001087 19980430 01087 NM 1998 4 30 SWAA980285 1 19980313 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND DENT IN FRAME AT BS 727D, RBL 30 WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001088 19980430 01088 NM 1998 4 30 SWAA980286 1 19980313 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 949 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 949 RBL 66.5 WL 230. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001089 19980430 01089 NM 1998 4 30 SWAA980287 1 19980313 A 5320 STRINGER CLIP BOEING 737 7373G7 1384595 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663 STR 10 LT, BS 663 STR 10 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001090 19980430 01090 NM 1998 4 30 SWAA980288 1 19980313 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947 LBL 53 WL 208, BS 947 RBL 4.5 WL 208, BS 986.5 LBL 39.5 WL 2 08, BS 967 LBL 43 WL 207, BS 964 LBL 42 WL 207, BS 294 LBL 39 TO 59 WL 207, BS 307 RBL 12 WL 208. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998043001091 19980430 01091 NM 1998 4 30 SWAA980289 1 19980313 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 329 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACK IN SKIN AT FWD SERVICE DOOR AFT LOWER CUTOUT AT BS 329 WL 211. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998043001092 19980430 01092 NM 1998 4 30 SWAA980291 1 19980313 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 1016/1028 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CORROSION ON LAV FLOOR SHEAR WEB AT BS 1016 LBL 14 WL 33, BS 1028 LBL 6 WL 18.5. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001093 19980430 01093 NM 1998 4 30 SWAA980292 1 19980313 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 993.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS 993.5 LBL 17 WL 208, BS 993.5 LBL 24 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001094 19980430 01094 NM 1998 4 30 SWAA980293 1 19980313 A 5320 WEB BOEING 737 7373T5 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND WEB CRACK AT BS 178 BL 0 WL 188. REMOVED AND REPLACED PER SWA T1-353-057. 2 L 7 2 4F RT A16WE 1998043001095 19980430 01095 NM 1998 4 30 SWAA980294 1 19980313 A 5330 SKIN BOEING 737 7373T5 NM BS 940.5 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND DENT IN SKIN AT BS 940.5, BELOW STR 23 RT, BS 348, 1 BELOW STR 22 RT, BS 362 TO 374 2-6 ABOVE STR 19 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001096 19980430 01096 NM 1998 4 30 SWAA980295 1 19980313 A 5320 ANGLE BOEING 737 7373T5 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 696SW 23064 DURING SCHEDULED D-CHECK, FOUND CRACKED SUPPORT ANGLE BS 727+2 LBL 1, WL 169. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001097 19980430 01097 NM 1998 4 30 SWAA980297 1 19980314 A 5320 NUT PLATE BOEING 737 7373H4 1384600 NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORROSION AROUND NUT PLATE HOLE AT BS 520, RBL 25. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001098 19980430 01098 NM 1998 4 30 SWAA980298 1 19980314 A 5320 SKIN BOEING 737 7373H4 1384600 NM RT LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACK ON RT KRUEGER FLAP I/B END. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998043001099 19980430 01099 NM 1998 4 30 SWAA980299 1 19980314 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 383.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 4 LT AT BS 383.5 HAS CRACK. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001100 19980430 01100 NM 1998 4 30 SWAA980300 1 19980314 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 727-905 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND BS 727 TO 905 STRINGER 4L DAMAGED IN 4 PLACES AT BS 979, 817, 837 AND 857. REPAIR ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001101 19980430 01101 NM 1998 4 30 SWAA980301 1 19980314 A 5313 STRINGER BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND NUMEROUS FASTENER HOLES CRACKED AT BS 1006 TO 1016 STR 10R, BS 908 TO 947 STR 10R, BS 908 TO 947 STR 14R, BS 1006 TO 1016 STR 14R, BS 908 TO 947 STR 10L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001102 19980430 01102 NM 1998 4 30 SWAA980302 1 19980314 A 5312 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND SKIN 6 FASTENER HOLES CRACKED AT BS 947 STR 4L, 3 FASTENER HOLES CRACKED AT BS 100 6 STR 4L AND 5 FASTENER HOLES CRACKED AT BS 1006 TO 1016 STR 10L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001103 19980430 01103 NM 1998 4 30 SWAA980303 1 19980314 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND APPROX 5 SKIN CRACK AT FUSELAGE LAP JOINT BS 727B S10L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001104 19980430 01104 NM 1998 4 30 SWAA980305 1 19980314 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 370SW 26597 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CORROSION AT BS 947.5 RBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001105 19980430 01105 NM 1998 4 30 SWAA980306 1 19980314 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 568 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND SKATE ANGLE CRACKED AT BS 568 LBL 55 WL 178. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001106 19980430 01106 NM 1998 4 30 SWAA980307 1 19980314 A 5320 SHROUD BOEING 737 7373G7 1384595 NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND TOOLING MARK ON SIDEWALL SHROUD ATTACH BRACKET AT BS 500A RBL 57 WL 181. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001107 19980430 01107 NM 1998 4 30 SWAA980308 1 19980314 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CORROSION AROUND NUTPLATE ON FRAME AT BS 500 RBL 25 WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001108 19980430 01108 NM 1998 4 30 SWAA980309 1 19980314 A 5320 CLIP BOEING 737 7373G7 1384595 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D STR 19 RT, BS 500D STR 19 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001109 19980430 01109 NM 1998 4 30 SWAA980311 1 19980314 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION NOTED AT BS 178 BULKHEAD WEB AT LBL 57 WL 201.5 TO 202.75, LBL 5.7 WL 1 97.5 TO 198.75, LBL 5.7 WL 210.5-212.75, LBL 6 WL 200.5-201, LBL 9.75 TO 10.5 WL 218, RBL 5.0 WL 217 TO 218.75, RBL 5.0 WL 200.75 TO 201.5, RBL 5.0 WL 197.5 TP 198.25, RBL 6.0 WL 212 TO 212.75, RBL 6.0 WL 226.5 TO 227, RBL 8.5 TO 16 WL 218. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001110 19980430 01110 NM 1998 4 30 SWAA980312 1 19980314 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 294 RBL 54.5 WL 208.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001111 19980430 01111 NM 1998 4 30 SWAA980313 1 19980314 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM AT BS 328 LBL 45 WL 206, BS 328.5 LBL 45 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001112 19980430 01112 NM 1998 4 30 SWAA980314 1 19980314 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328/344 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344 LBL 25, 20.5, 17, 14, 7, RBL 8.5, WL 207 AND 208, BS 328 R BL 15 AND 28.5 WL 208, 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001113 19980430 01113 NM 1998 4 30 SWAA980315 1 19980314 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 691SW 23781 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOORBEAM STIFFENER AT BS 328 RBL 32.5, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998043001114 19980430 01114 NM 1998 4 30 SWAA980296 1 19980315 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 305 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED D-CHECK, FOUND STRINGER 4L CRACKED AT BS 305 ABOVE AND FWD OF FWD ENTRY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001115 19980430 01115 NM 1998 4 30 SWAA980304 1 19980315 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED D-CHECK, FOUND CORROSION UNDER STRINGER SPLICE AT BS 907, STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001116 19980430 01116 NM 1998 4 30 SWAA980310 1 19980315 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 56SW 21721 DURING SERVICE VISIT, REPAIRED SKIN LAP AT BS 360 TO 540 STR 14L, STR 10L, 4L, 4R, 10R, 14R; BS 540 TO 727 STR 4L, 4R; B S 727 TO 908 STR 10L, 4L, 4R, 10R. REPAIRED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998043001117 19980430 01117 NM 1998 4 30 SWAA980316 1 19980316 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND BELT FRAME ATTACH ANGLE CRACKED AT BS 380 STR 26L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001118 19980430 01118 NM 1998 4 30 SWAA980317 1 19980316 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 834 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 55SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED BELT FRAME AT BS 834 STR 27R AT SHEAR TIE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998043001119 19980430 01119 NM 1998 4 30 UPS98626134 1 19980317 A 3350 LIGHT BOEING 767 76734AF 1385212 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 303UP 27241 INSPECTION TYPE-N/A, HALF OF THE LIGHTS ON EMER LIGHT PLATE INOP. RELAMPED EMER LIGHT PLATE PANEL. 2 L 7 2 4F RT A1NM 1998043001120 19980430 01120 WP 1998 4 30 UPS98826138 1 19980318 A 3350 5708458503 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 880UP 46080 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING BITE CHECK. REMOVED AND REPLACED EMERGENCY LIGHT B ATTERY PACK, OPS CHECK OK. 2 L 7 4 4F RT 4A25 1998043001121 19980430 01121 EU 1998 4 30 QXEA9800327 1 19980316 A 3350 5515900004 CIRCUIT CARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTION A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 484US 11234 EXIT SIGN AT ROW 8 OUT. REPLACED CIRCUIT CARD, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998043001122 19980430 01122 EU 1998 4 30 QXEA9800328 1 19980316 A 3350 5515900004 CIRCUIT CARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU CABIN MALFUNCTION A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 477AU 11226 LIGHTS DIM AT THE EXIT SIGN IN THE CEILING AT ROW 8 AND 9. REPLACED CIRCUIT CARDS, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998043001123 19980430 01123 NE 1998 4 30 98FDEA00202 2 19980317 A 7230 COMPRESSOR AIRBUS 300 A300F4605R 3930327 EU GE CF6 CF680C2A5 NE NR 2 ENGINE BURNED A FDEA C F D ABORTED TAKEOFF ACTIVATE FIRE EXT. RETURN TO BLOCK A J FLAME/FIRE WARNING INDICATION TO TAKEOFF 1 SO 25 654FE 738 REJECTED T/O AT APPROX 120 KTS, (18R MEM) DUE TO FIRE ON NR 2 ENGINE. AFTER BOTH BOTTLES WERE FIRED THE FIRE WENT OUT. A/C NOT EVACUATED EMERGENCY CREW CONFIRMED NO FURTHER SMOKE. FOUND HOLE BURNED THROUGH REAR COMPRESSOR STAGE AT 8 O'CL OCK FUEL NOZZLE POSITION. *S/D* INSPECTED WHEELS AS PER 32-41-00-6, NO DEFECTS NOTED SKS 197864. FOUND HOLE BURNED TH ROUGH REAR COMPRESSOR STAGE AT EIGHT O'CLOCK FUEL NOZZLE POSITION. JOB PROGRESS FORM STARTED. REMOVED AND REPLACED NR 2 ENG IAW W/C 64T0700. LEAK AND OPS CHECK GOOD IAW SNRD NR 390843. REMOVED AND REPLACED FAN AIR VALVE IAW M/M 36-11-16 -4. 2 L 7 2 4F 4 F RT A35EU E13NE 1998043001124 19980430 01124 WP 1998 4 30 98FDEA00204 1 19980217 A 5311 FRAME DOUG DC10 DC1010F 3022111 WP BS 459 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 391FE 46625 STA 459 Z=-78, X=-63 A CRACK WAS FOUND ON THE FRAME LT SIDE. REF NRC NR N 2064. REPAIRED FRAME IAW SRM 53-30-00 FIG 5. 2 L 7 3 4F A22WE 1998043001125 19980430 01125 NM 1998 4 30 98UAL900013 1 19980108 A 2131 7638101 CONTROLLER HONEYWELL HG180Y742 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 7256U 21403 CREW REPORTED, CABIN PRESSURE AT 9.2 DIFFERENTIAL AT FLT 330. SWITCHING TO AUTO AND STANDBY WOULD NOT LOWER CABIN PRESS URE DIFFERENTIAL. OUTFLOW VALVE WOULD NOT WORK IN MANUAL AC OR DC. HAD TO CHANGE ALTITUDE TO LOWER CABIN PRESSURE. RE PLACED NR 1 AIR DATA COMPUTER AND THE AUTO PRESSURE CONTROLLER PANEL. 2 L 7 3 4F 4 F A3WE E2EA 1998043001126 19980430 01126 NM 1998 4 30 98UAL900033 1 19980125 A 3350 767 LAMP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN FAILED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 541UA 25253 EMERGENCY SLIDE LIGHT FOR RIGHT-HAND OVERWING SLIDE IS INOP. *S/D* RELAMPED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998043001127 19980430 01127 NM 1998 4 30 98UAL900040 1 19980129 A 2121 732591E FAN SUNDSTRAND 732591E BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 174UA 4329 24381 ELECTRICAL SMELL AND SMOKE IN CABIN CONCENTRATED BETWEEN GALLEY 402 AND LAV 111-112. LEFT AND RIGHT UTILITY BUSES TRIPPE D. SMOKE REMOVAL PROCEDURE, CLEARED CABIN. *S/D* UPPER NR 2 RECIRCULATION FAN BEARING FAILURE. REPLACED FAN. 2 L 7 4 4F 4 F RT A20WE E24NE 1998043001128 19980430 01128 NM 1998 4 30 98UAL900048 1 19980207 A 3260 BCREF7817 LIGHT BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG DEFECTIVE A UALA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 29 534UA 25129 LEFT MAIN GEAR, NO GREEN LIGHT WITH GEAR DOWN. EXTENDED GEAR BY ALTERNATE METHOD. LANDED UNDER AMBER ALERT. *S/D* RE PLACED THE LEFT GEAR INDICATION LIGHT ASSEMBLY. 2 L 7 2 4F 4 F RT A2NM E17NE 1998043001129 19980430 01129 NM 1998 4 30 98UAL900107 1 19980306 A 2611 SMOKE ALARM BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LAVATORY ACTIVATED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 927UA 26649 LAVATORY SMOKE DETECTOR ALARM WENT OFF AND WOULD NOT SILENCE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998043001130 19980430 01130 NM 1998 4 30 98UAL900109 1 19980309 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7441U 21895 AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1998043001131 19980430 01131 GL 1998 4 30 98UAL900110 2 19980309 A 7230 MID SHAFT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 ENGINE FAILED A UALA E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 1843U 46636 451295 SHUT DOWN NR 3 ENGINE DUE TO AIRCRAFT VIBRATION AND HIGH TEMPERATURE INDICATION. DIVERTED TO HNL LANDED UNDER AMBER ALE RT. *S/D* THE FAN MID-SHAFT IN THE ENGINE SEPARATED. THE PRIMARY CAUSE OF FAILURE IS STILL UNDER INVESTIGATION BY GEN ERAL ELECTRIC. 2 L 7 3 4F 4 F A22WE E23EA 1998043001132 19980430 01132 NM 1998 4 30 98UAL900111 1 19980310 A 3350 CIRCUIY BREAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN TRIPPED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7252U 21399 RIGHT HAND EMERGENCY LIGHT CONTROL CIRCUIT BREAKER POPPED AND WOULD NOT RESET. 2 L 7 3 4F 4 F A3WE E2EA 1998043001133 19980430 01133 NM 1998 4 30 98UAL900113 1 19980311 A 5270 WARNING LIGHT BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CARGO DOOR ACTIVATED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 770UA 26925 CREW ABORTED TAKEOFF DUE TO FORWARD CARGO DOOR WARNING LIGHT CAME ON. ABORTED TAKEOFF AT 90 KNOTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998043001134 19980430 01134 NM 1998 4 30 98UAL900114 1 19980311 A 2913 623337 HYD PUMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A UALA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 306UA 23667 THE NUMBER ONE ENGINE HYDRAULIC PUMP FAILED. CREW FELT VIBRATION IN CABIN WITH 'A' HYDRAULIC SYSTEM PRESSURE FLUCTUATIN G AND THEN VIBRATION AND FLUCTUATION STOPPED, BUT THE PUMP LOW PRESSURE LIGHT CAME ON. *S/D* REPLACED THE NUMBER ONE E NGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F 4 F RT A16WE E2GL 1998043001135 19980430 01135 WP 1998 4 30 ABXA9800250 1 19980317 A 3260 DC26A1415S CONNECTOR DOUG DC8 DC863 302198A WP RT MLG DIRTY A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 824AX 46141 GEAR RECYCLE WAS REQUIRED TO GET THE RIGHT MAIN LANDING GEAR LIGHT TO INDICATE DOWN AND LOCKED. RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH CONNECTOR WAS FOUND TO BE DIRTY. CLEANED AND REINSTALLED CANNON PLUG. LANDING GEAR OPS CHECKED GOOD I AW DC8 MM 32-60-0. 2 L 7 4 4F 4A25 1998043001136 19980430 01136 WP 1998 4 30 ABXA9800251 1 19980316 A 3260 0080004003 CONTROL BOX DOUG DC8 DC863F 302198F WP NLG WW DEFECTIVE A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 812AX 46126 LANDING GEAR UNSAFE LIGHT WAS ON WITH NOSE LANDING GEAR UNLATCHED INDICATION. RECYCLED GEAR, NO HELP. REPLACED PROXIMI TY CONTROL BOX AND NOSE LANDING GEAR UPLIMIT SWITCH IAW DC8 MM 32-60-0. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998043001137 19980430 01137 WP 1998 4 30 MWEA98347 1 19980313 A 2560 11320 GIRT BAR DOUG DC9 DC914 3022034 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 700ME 2560 THE GALLEY DOOR ESCAPE SLIDE ASSEMBLY DETACHED. MTC REINSTALLED R-1 GIRT BAR SLIDE CLIP. 2 L 7 2 4F A6WE 1998043001138 19980430 01138 WP 1998 4 30 MWEA98348 1 19980313 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 THE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1998043001139 19980430 01139 WP 1998 4 30 MWEA98349 1 19980316 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 502ME 48132 THE GALLEY SERVICE DOOR SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998043001140 19980430 01140 WP 1998 4 30 MWEA98350 1 19980318 A 5312 JAMB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACK ON AFT VENTRAL DOOR JAMB WEB LEFT SIDE. MTC SPLICED IN NEW SECTION WITH DOUBLER AND FILLER. 2 L 7 2 4F A6WE 1998043001141 19980430 01141 WP 1998 4 30 MWEA98351 1 19980318 A 5312 JAMB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACK IN AFT PRESSURE BULKHEAD FORWARD SIDE UPPER LEFT CORNER OF DOOR JAMB ON JAMB FLANGE. MTC SPLICED NEW JAMB S ECTION. 2 L 7 2 4F A6WE 1998043001142 19980430 01142 WP 1998 4 30 MWEA98352 1 19980318 A 5312 BLKHD SKIN DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND VERTICAL CRACK ON AFT PRESSURE BULKHEAD UPPER LEFT CORNER OF VENTRAL DOOR JAMB ON 3 WEB SKIN. MTC SPLICED NEW 3 S ECTION SKIN. 2 L 7 2 4F A6WE 1998043001143 19980430 01143 WP 1998 4 30 MWEA98353 1 19980318 A 5312 BLKHD DOUBLER DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND A RADIAL CRACK ON AFT PRESSURE BULKHEAD DOOR JAMB UPPER LEFT CORNER OF -13 DOUBLER. MTC REMOVED AND REPLACED -13 DOUBLER. 2 L 7 2 4F A6WE 1998043001144 19980430 01144 WP 1998 4 30 MWEA98354 1 19980318 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1130 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND MODERATE CORROSION ON LT SIDE AFT ACCESSORY COMPARTMENT FUSE SKIN STA 1130. MTC REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998043001145 19980430 01145 WP 1998 4 30 MWEA98355 1 19980318 A 5210 99915565159 ANGLE DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACK ON NR 3 BEAM ON RT SIDE OF AFT VENTRAL DOOR. MTC REMOVED AND REPLACED ANGLE. 2 L 7 2 4F A6WE 1998043001146 19980430 01146 WP 1998 4 30 MWEA98356 1 19980318 A 5210 9915565133 PAN DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACK AROUND UPPER LT DOOR STOP ON AFT VENTRAL DOOR. MTC REMOVED AND REPLACED PAN. 2 L 7 2 4F A6WE 1998043001147 19980430 01147 WP 1998 4 30 MWEA98357 1 19980318 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 1132.6 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND CRACK ON INTERCOSTAL BOTTOM FLANGE LT SIDE FUSE STA 1132.60 TO 1143.01. MTC FABRICATED DOUBLER AND INSTALLED. 2 L 7 2 4F A6WE 1998043001148 19980430 01148 WP 1998 4 30 MWEA98358 1 19980318 A 5220 DOOR PAN DOUG DC9 DC932 3022066 WP LT/RT EMER EXIT GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND THE LT AND RT AFT OVERWING EXIT DOOR FRAME PANS GOUGED AT TOP CENTER AREA. MTC BLENDED GOUGES AND FABRICATED REPA IR DOUBLERS AND INSTALLED. 2 L 7 2 4F A6WE 1998043001149 19980430 01149 WP 1998 4 30 MWEA98359 1 19980318 A 5312 9915558143 CLIPS DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 FOUND THE AFT PRESSURE BULKHEAD RT RADIAL FORMER CRACKED ON OUTBOARD END. MTC TRIMMED OUT FORMER AND FITTED WITH NEW CL IPS. 2 L 7 2 4F A6WE 1998043001150 19980430 01150 WP 1998 4 30 MWEA98360 1 19980318 A 5320 INTERCOSTAL DOUG DC9 DC981 3022081 WP LT EMER EXIT DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 THE INTERCOSTAL DAMAGED BY DRILL JUST BELOW LT FORWARD OVERWING EXIT JAMB. MTC REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 1998043001151 19980430 01151 WP 1998 4 30 MWEA98361 1 19980318 A 5210 BEAM DOUG DC9 DC981 3022081 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CRACK IN RADIUS OF NR 6 BEAM AFT END OF FORWARD PASSENGER DOOR. MTC REPAIRED WITH REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998043001152 19980430 01152 WP 1998 4 30 MWEA98362 1 19980318 A 5210 J06021313 DOUBLER DOUG DC9 DC981 3022081 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CRACK IN RADIUS OF NR 2 BEAM FORWARD END OF FORWARD PASSENGER DOOR. MTC REPAIRED WITH DOUBLER. 2 L 7 2 4F A6WE 1998043001153 19980430 01153 WP 1998 4 30 DLL19980580 1 19980315 A 5312 1554194101 BULKHEAD CAP LKHEED 1011 10113853 5265020 WP FS 983 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 753DA 193W1189 THE LOWER CAP OF THE FS 983 BULKHEAD WAS FOUND CORRODED NEAR RBL 42.5 STR 28. THE LOWER FLANGE OF THE CAP WAS CUTOUT TO REMOVE THE DAMAGE. TWO REPAIR ANGLES WERE INSTALLED PER ER/A 364233-14, REV C TO REPAIR THE DAMAGE. 2 L 7 3 4F A23WE 1998043001154 19980430 01154 NM 1998 4 30 DL767980581 1 19980313 A 5754 WEDGE BOEING 767 767232 1385132 NM NR 7 LE SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 109DL 22221 THE RT WING NR 7 SLAT WAS FOUND WITH A 5 X 2.5 X .025 DENT ON THE LOWER SURFACE THE TRAILING EDGE WEDGE. THE DENT WAS R EPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A364235-14AD. 2 L 7 2 4F RT A1NM 1998043001155 19980430 01155 NM 1998 4 30 DL76L980582 1 19980313 A 5754 WEDGE BOEING 767 767332 1382001 NM NR 7 LE SLAT GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 172DN 24775 THE LT WING NR 7 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 1INCH LONG GOUGE THROUGH THE LOWER SKIN. THE DAMAGE WAS REPA IRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364249-14AD. 2 L 7 2 4F RT A1NM 1998043001156 19980430 01156 NM 1998 4 30 DL72W980583 1 19980313 A 5330 65C139132 SKIN BOEING 727 727247 138408F NM BS 1060 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 THE SKIN WAS FOUND CORRODED AT STRINGER 28R BETWEEN FS 1050 AND 1070. THE DAMAGE WAS CUTOUT OVER A 3 X 16 AREA. THE SK IN WAS REPAIRED WITH A DOUBLER PER THE GUIDLINES OF B727 SRM 53-30-3 AND DOCUMENTED PER ER/A 364236-14. 2 L 7 3 4F A3WE 1998043001157 19980430 01157 NM 1998 4 30 DL72W980584 1 19980311 A 5320 65562312 STRAP BOEING 727 727247 138408F NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 THE R1 DOOR CUTOUT REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK IN UPPER HINGE CUTOUT. THE SKIN WAS CUT TO ACCESS THE CRACK AND THE BEAR STRAP WAS CUT TO REMOVE THE CRACK. THE CUTOUTS WERE REPAIRED WITH A DOUBLER AND TR IPLER PER THE GUIDLINES OF BOEING S/B 727-53-0136 AND ER/A 364227-14. 2 L 7 3 4F A3WE 1998043001158 19980430 01158 NM 1998 4 30 DL72E980585 1 19980316 A 5714 64083358 WEB BOEING 727 727247 138408F NM CTR WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 THE CENTER WING FUEL TANK SPANWISE BEAM NR 1 WEB WAS FOUND CRACKED AT APPROX LBL 3, JUST BELOW THE CHEM-MILL RADIUS. TH E RESULTING CUTOUT IS 2.9 (INB'D-OUTB'D) BY 0.5. REPAIRED PER ERA 331472-14. 2 L 7 3 4F A3WE 1998043001159 19980430 01159 WP 1998 4 30 DLL15980587 1 19980316 A 3350 516574 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 15725 193Y1184 BATTERY PACK WOULD NOT LIGHT CABIN OVERHEAD, AFT GALLEY OR OUTSIDE ESCAPE SLIDE LIGHTS DURING TEST. 2 L 7 3 4F A23WE 1998043001160 19980430 01160 WP 1998 4 30 DLL15980589 1 19980316 A 3350 20131A BATTERY PACK LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 61428 193Y1184 BATTERY DISCHARGED RAPIDLY BY DEFECTIVE BATTERY CHARGER/ POWER SUPPLY. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1998043001161 19980430 01161 WP 1998 4 30 DLL15980590 1 19980316 A 3350 RPS1B POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 193Y1184 AFT CABIN FLOOR EMERGENCY LIGHTS ON BOTH SIDES INOP. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998043001162 19980430 01162 WP 1998 4 30 DLL15980591 1 19980316 A 3350 20131A BATTERY PACK LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 755DL 193Y1184 AFT CABIN EMERGENCY FLOOR LIGHTS INOP BOTH SIDES. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1998043001163 19980430 01163 NM 1998 4 30 DL72S980592 1 19980305 A 5320 FITTING BOEING 727 727232 1384082 NM FUS FITTING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 522DA 21582 CORROSION ON BORE OF BODY FITTING LT AFT BTL PIN. ALSO, SOME CORROSION ON EDGE OF FITTING BETWEEN WING AND BODY FITTING . REMOVED CORROSION PER 53-40-1 FIG 4. REWORKED NR 1214 BORE, REPAIRED ON NR 1214 AS PER ERA 331517-14. 2 L 7 3 4F A3WE 1998043001164 19980430 01164 NM 1998 4 30 DHL98712001 1 19980317 A 5230 LINE BOEING 727 72729 1384007 NM CARGO DOOR LOOSE A DHLA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 01 712DH 19401 MAIN CARGO DOOR LIGHT CAME ON AT FL 310. PERFORMED EMERGENCY CHECK LIST AND LANDED AT TYS. ALSO, DOOR UNSAFE RED AND L ATCH UNLOCK AMBER LIGHTS ILLUMINATED. FOUND SMALL HYDRAULIC LEAK ON SLIDING LOCK BAR ACTUATOR LINE. TIGHTENED, OPS CHE CK GOOD. 2 L 7 3 4F A3WE 1998043001165 19980430 01165 NM 1998 4 30 DHL98712002 1 19980317 A 5230 STRIKER PLATE BOEING 727 72729 1384007 NM CARGO DOOR SLIPPED A DHLA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 SO 01 712DH 19401 MAIN CARGO DOOR LIGHT CAME ON AT FL 230. DOOR UNSAFE LIGHT AND LATCH UNLOCK LIGHTS CAME ON. FOUND STRIKER PLATE SLIPPI NG OFF TORQUE TUBE LOCK SWITCH PLUNGER. RESHIMMED, SWITCH OPS CHECKED OK. PRESSURIZED AND UNPRESSURIZED PER MM 52-34- 01. 2 L 7 3 4F A3WE 1998043001166 19980430 01166 NM 1998 4 30 DHL98740001 1 19980318 A 2131 7110025 CONTROLLER BOEING 727 7272Q9 138448M NM CABIN MALFUNCTIONED A DHLA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 740DH 21930 AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE. REMOVED AND REPLACED PRESSURE CONTROLLER, RAN AIRCRAFT, PRESSURIZED OK. 2 L 7 3 4F RT A3WE 1998043001167 19980430 01167 NE 1998 4 30 CKSA98091 2 19980212 A 7230 BLADE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 2 ENGINE DAMAGED A A CKSA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 23 103CK 293C1212 14542 AFTER TAKEOFF, NR 2 ENG HAD A LARGE COMPRESSOR STALL WITH A 40 FT TO 50 FT. REPORTED FLAME OUT THE TAIL, OBSERVED BY TO WER, OTHER ACFT AND GROUND PERSONNEL. TGT = 860, ALL OTHER PARAMETERS WITHIN LIMITS. FIRM 71-23-17-02. PERFORMED BOR ESCOPE INSPECTION ON ENGINE NR 2. LP COMPRESSOR HAS MANY BLADE TIPS DAMAGED ALL WITHIN LIMITS. HP COMPRESSOR HAS FEW B LADE TIPS DAMAGED ALL WITHIN LIMITS. COMBUSTION CAN AND HPT BLADES HAVE NO OBVIOUS DAMAGE IAW MM 72-00-00. 2 L 7 3 4F 4 F A23WE E12EU 1998050100004 19980501 00004 CE 1998 5 1 98ZZZX1617 1 19980411 A 2612 302158 SENSOR BEECH 99 C99 1154006 CE RT ENGINE MALFUNCTIONED A AJZA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 19 388AV U188 APPROXIMATELY 10 MINUTES AFTER TAKEOFF, THE RT ENGINE FIRE WARNING LIGHT CAME ON. THeRE WAS NO OTHER INDICATION OF FIRE AND THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO L15 WITH NO PROBLEMS. THE LIGHTS WENT OUT AFTER AIRCRAFT WAS P ARKED. INVESTIGATED RECORDS AND NOTICED THE AIRCRAFT WAS WASHED THE NIGHT BEFORE, DRIED AND SEALED LOWER DETECTOR. SYS TEM OPERATIONALLY CHECKED GOOD. 1 L 7 2 3T A14CE 1998050100018 19980501 00018 WP 1998 5 1 VJ9800133 1 19980203 A 5330 5911402 PLATING DOUG DC9 DC932 3022066 WP BS 110-118 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 15 905VJ 47378 DENTS AND CRACK IN LT SIDE OF FUSELAGE FROM FS 110 TO 118, BETWEEN LONGERON 17L TO 19L. FABRICATED AND INSTALLED FLUSH REPAIR IAW DC9 SRM 53-04, FIG 4 AND FIG 38, REFERENCE RFTS 98-109 AND 98-124. TREATED AND PRIMED PARTS IAW DC9 SRM 51-1 0-3. 2 L 7 2 4F A6WE 1998050100019 19980501 00019 WP 1998 5 1 VJ9800134 1 19980210 A 5230 PLATING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 15 905VJ 47378 FWD EDGE OF AFT CARGO DOOR DAMAGED AT SEAL RETAINER. TRIMMED CRACK AND COLD WORKED WRINKLE IAW REA 98131. FABRICATED T WO DOUBLERS FROM .063 T3 AL AND ONE FROM .032 TITANIUM. INSTALLED IAW BOEING SKETCH 98-03-02-011, SHEET 1, AND DC9 SRM 52-03, FIG 8, SHEET 2, AND INNER SKIN IAW DC9 SRM 52-01, FIG 2, SHEET 3. 2 L 7 2 4F A6WE 1998050100020 19980501 00020 WP 1998 5 1 VJ9800135 1 19980306 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 164 CRACKED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 15 905VJ 47378 LT CUSP AT FS 164, APPROX Z=0 CRACKED. TRIMMED DAMAGED AREA AND FABRICATED REPAIR DOUBLER AND FILLER IAW DRAWING SK9812 8. TREATED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998050100021 19980501 00021 WP 1998 5 1 VJ9800136 1 19980325 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS Y200 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 15 905VJ 47378 FLOOR SUPPORT CORRODED AT STA Y200, X56RH. REMOVED, FABRICATED, TREATED AND INSTALLED IAW DC9 SRM 51-10-1, 51-10-4, 51- 10-3 AND 51-3-2. 2 L 7 2 4F A6WE 1998050100022 19980501 00022 WP 1998 5 1 VJ9800137 1 19980326 A 5311 2777930 FRAME DOUG DC9 DC932 3022066 WP BS 220 CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 15 905VJ 47378 BULKHEAD FLANGE ABOVE FS 220, LONGERON 30, CORRODED. REPAIRED IAW DC9 SRM 53-03, FIG 2A, SHEET 5, AND 51-10-2A. 2 L 7 2 4F A6WE 1998050100023 19980501 00023 WP 1998 5 1 VJ9800138 1 19980404 A 3810 5707638511 WATER HEATER DOUG DC9 DC932 3022066 WP FWD LAVATORY CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 15 905VJ 47378 TOP OF FRESH WATER TANK UNDER FORWARD LAV SINK CORRODED. REPLACED TANK IAW DC9 MM 38-11-4. LEAK AND OPS CHECKED GOOD I AW DC9 MM 38-11-4. 2 L 7 2 4F A6WE 1998050100024 19980501 00024 WP 1998 5 1 VJ9800139 1 19980422 A 2560 591769637 COVER DOUG DC9 DC932 3022066 WP L1 DOOR SLIDE DISLODGED A VJ6A K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 936VV 47397 MAIN CABIN ENTRANCE DOOR EMERGENCY SLIDE PACK DISLODGED WHILE CLOSING. RESECURED SLIDE AND ACCOMPLISHED REQUIRED INSPEC TION. 2 L 7 2 4F A6WE 1998050100025 19980501 00025 EU 1998 5 1 MALA976104 1 19980421 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 417XJ 340B417 DURING INSPECTION EMERGENCY EXIT LIGHT ADJACENT TO MAIN DOOR INOP. MAINTENANCE RECONNECTED CANNON PLUG ON SWING OUT GAL LEY. ALL EMERGENCY LIGHTS OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998050100026 19980501 00026 EU 1998 5 1 MALA976105 1 19980420 A 3350 6122751 BATTERY PACK BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 502XJ E2307 DURING INSPECTION FORWARD CABIN'S EMERGENCY FLOOR TRACK LIGHT AND EMERGENCY EXIT SIGNS INOP. MAINTENANCE INSTALLED NEW BATTERY PACKS, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998050100027 19980501 00027 NM 1998 5 1 AWXA9800098 1 19980307 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 DURING ROUTINE MAINTENANCE CHECK, FOUND LT FUSELAGE CRACK AT STA 727. REPAIR PER SRM 53-30-03. 2 L 7 2 4F RT A16WE 1998050100028 19980501 00028 NM 1998 5 1 AWXA9800099 1 19980311 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN CRACK AT STA 727B STR 18. TEMP REPAIR PER SRM 53-30-03. 2 L 7 2 4F RT A16WE 1998050100029 19980501 00029 NM 1998 5 1 AWXA9800100 1 19980201 A 5330 SKIN BOEING 737 737277 1384570 NM BS 760 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE CRACK AT STA 760 STR 18. REPAIR PER SRM 53-30-03 FIG 6 AND PLACE ON AW M106 NR 980149. 2 L 7 2 4F RT A16WE 1998050100030 19980501 00030 NM 1998 5 1 AWXA9800101 1 19980414 A 5330 SKIN BOEING 737 737277 1384570 NM BS 825 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE CRACK AT STA 825 BETWEEN STR 15R AND 16R. REPAIR PER 53-30-03. 2 L 7 2 4F RT A16WE 1998050100031 19980501 00031 NM 1998 5 1 AWXA9800102 1 19980201 A 5330 SKIN BOEING 737 7372A6 138448B NM BS 350 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 145AW 20194 LOWER FUSELAGE SKIN BULGING AROUND FASTENERS AT THE E AND E DOOR AND THE NLG W/W AREA AS FOLLOWS: BS 358 RT OF ANTENNA BL 3 AFT LT CORNER OF E AND E DOOR CUTOUT LT SIDE STA 350 STR 26 AND STR 27. AFT AND LT AREA OF THE E AND E DOOR, STA 3 50, 320 STR 26 AND STR 27 SKIN BULGING, STA 294 STR 25 SKIN BULGING, AND BULGING SKIN AROUND THE NOSE. INSTALLED FASTEN ERS PER 2-53-43-22B SR 737-53-1076 PART 4 STEP D AND TRANSFERRED TO AWM 106 NR 980141 SCHEDULED TO TERMINATE AT C-CHECK. 2 L 7 2 4F A16WE 1998050100032 19980501 00032 NM 1998 5 1 AWXA9800104 1 19980130 A 5330 SKIN BOEING 737 737277 1384570 NM BS 747 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN CRACK STA 747A STR 17R. REPAIR PER SRM 53-30-03. 2 L 7 2 4F RT A16WE 1998050100033 19980501 00033 NM 1998 5 1 AWXA9800105 1 19980415 A 5330 SKIN BOEING 737 737277 1384570 NM BS 747 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 DURING ROUTINE MAINTENANCE CHECK, FOUND FUSELAGE SKIN CRACK LT SIDE STR 17L STA 747. REPAIR PER SRM 53-30-03 FIG 1. 2 L 7 2 4F RT A16WE 1998050100034 19980501 00034 NM 1998 5 1 AWXA9800106 1 19980204 A 5330 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 178AW 22645 DURING ROUTINE MAINTENANCE CHECK, FOUND CRACK IN FUSELAGE SKIN 2 INCHES LONG LT FWD WING TO BODY. REPAIRED PER SRM 53-3 0-03 FIG 1. 2 L 7 2 4F RT A16WE 1998050100035 19980501 00035 NM 1998 5 1 AWXA9800107 1 19980417 A 3350 900542 BATTERY PACK BOEING 737 7372E3 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 DURING ROUTINE MAINTENANCE CHECK, FOUND BOTH L2 AND R2 EXTERIOR EMERG EXIT LIGHTS FAIL 4 MIN CAP TEST. REMOVED AND REP LACED BATTERY PACK FOR L2 AND R2 EXTERIOR EMERG EXIT LGHTS, SYSTEM OPS CHECKS GOOD. 2 L 7 2 4F RT A16WE 1998050100036 19980501 00036 NM 1998 5 1 AWXA9800108 1 19980419 A 4950 0007352 APU BOEING 737 737301 1384611 NM AFT FUSELAGE FAILED A AWXA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 326AW 23258 AFTER TAKEOFF FUMES SMELLED IN FLT DECK AND CABIN. LATER IN FLIGHT FUMES DID NOT DIMINISH MUCH AND APPEARED TO BE COMIN G FROM ATR CONDITIONING SYSTEM, DEFFERED. REMOVED AND REPLACE L AND R PACK COALESCER BAGS. PLACARDED APU INOPERATIVE P ER MEL 49-01 C/N 90788. ENGINE OPS AND EXTENDED PACK RUNS ELIMINATED RESIDUAL AROMA FROM ECS. VERIFIED APU BLEED WAS S OURCE AFTER ISOLATION. REMOVED AND REPLACED APU PER R6D49004, OPS GOOD MEL CLEARED. 2 L 7 2 4F RT A16WE 1998050100037 19980501 00037 NM 1998 5 1 AWXA9800109 1 19980314 A 5330 SKIN BOEING 757 7572S7 1384962 NM BS 405 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 904AW 23566 DURING SCHEDULED C-5 INSPECTION, FOUND LOWER FUSELAGE SKIN CRACKED AT STA 405, STR 276 (LBL 14). FOUND BY HFEC. INSTAL LED RIVET REPAIR PER SRM 53-00-01. 2 L 7 2 4F RT A2NM 1998050100038 19980501 00038 NM 1998 5 1 RAAA98B2022 1 19980422 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 MID CABIN DOOR EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998050100039 19980501 00039 NM 1998 5 1 CALA9800685 1 19980421 A 3260 TARGET BOEING 737 737524 1384721 NM RT MLG OUT OF ADJUST A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 33608 27321 THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED ON APPROACH. THE GEAR WAS CYCLED AND THE RED LI GHT EXTINGUISHED. MAINTENANCE FOUND THE RT MLG DOWNLOCK SENSOR TARGET GAP OUT OF LIMITS. THE SENSOR GAP WAS ADJUSTED I AW MM 32-61-31, PAGE 403. A GEAR SWING WAS PERFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F RT A16WE 1998050100040 19980501 00040 WP 1998 5 1 CALA9800686 1 19980421 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG FLAT A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 809NY 49263 THE NLG WOULD NOT RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANC E FOUND THE NLG STRUT FLAT. A NEW GLAND NUT WAS INSTALLED AND THE STRUT WAS REPACKED. 2 L 7 2 4F A6WE 1998050100041 19980501 00041 NM 1998 5 1 CALA9800687 1 19980422 A 3260 LOGIC CARDS BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 69311 23362 THE NOSE GEAR RED UNSAFE AND GREEN LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING CLE. THE GEAR WAS LOWERE D AND NORMAL INDICATIONS WERE SHOWN. THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RE MOVED AND REPLACED THE M1215 AND M983 LANDING GEAR LOGIC CARDS. IN ADDITION, THE NLG LOCK SENSOR WAS ADJUSTED IAW MM 32 -61-41, PAGES 401-406. THE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F RT A16WE 1998050100042 19980501 00042 WP 1998 5 1 CALA9800688 1 19980423 A 5753 SKIN DOUG DC10 DC1030 3023501 WP LT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13066 46591 INSPECTION FOUND LT WING INBOARD FLAP SKIN TORN AND CORRODED AT OUTBOARD EDGE CLOSURE RIB. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-21-01, 51-31-01, AND ECRA 5752-01023. 2 L 7 3 4F A22WE 1998050100043 19980501 00043 EU 1998 5 1 9806963202 1 19980417 A 2820 FUEL TANK AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE RT WING LEAKING A NWAA A UNSCHED LANDING K X FLUID LOSS ENGINE FLAMEOUT CL CLIMB 1 GL 01 302US 32 731237 DURING CLIMB, A FUEL LEAK FROM THE RIGHT WING WAS REPORTED. FLIGHT CREW DIVERTED TO MSP. DURING DESCENT INTO MSP WHILE FOLLOWING COM FOR A FUEL LEAK, NR 2 ENGINE FLAMED OUT AT 5000 FEET. A SUCCESSFUL RELIGHT WAS ACCOMPLISHED, AN UNEVENTF UL LANDING WAS PERFORMED. 2 L 7 2 4F 4 F RT A28NM E29NE 1998050100044 19980501 00044 NM 1998 5 1 9806976718 1 19980419 A 7714 TACHOMETER BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 618US 21122 662614 DURING TAKEOFF ROLL AT APPROXIMATELY 115 KTS, THE NR 4 ENGINE N1 RPM INDICATION MALFUNCTIONED. THE TAKEOFF WAS ABORTED. MAINTENANCE PLACED THE NR 4 ENGINE N1 INDICATION SYSTEM ON MEL AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1998050100045 19980501 00045 NE 1998 5 1 9806981152 2 19980420 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 GL 01 152US 46760 686116 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN WITH THE E GT REACHING A MAXIMUM OF 940C. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A22WE E20EA 1998050100046 19980501 00046 WP 1998 5 1 9806999759 1 19980421 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, FOUND FIRST CLASS SECTION OF FLOOR LIGHTING WOULD NOT EXTINGUISH WITHOUT RECYCLING POWER SWITCH. MAI NTENANCE REPLACED BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100047 19980501 00047 WP 1998 5 1 9807009759 1 19980421 A 3350 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, FOUND EMERGENCY LIGHT IN TAIL COMPARTMENT INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100048 19980501 00048 WP 1998 5 1 9807019302 1 19980421 A 3350 BATTERY DOUG DC9 DC982 3022082 WP AFT CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302RC 48055 PILOT REPORTED ONE FLASHLIGHT IN THE AFT SECTION OF THE AIRCRAFT HAD AN INOPERATIVE TEST LIGHT. MAINTENANCE REPLACED FL ASHLIGHT AND BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100049 19980501 00049 SO 1998 5 1 COMA9810107 1 19980420 A 3246 3006041 WHEEL 314461 EMB 120 EMB120RT SO LT MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 241CA 64 1211 MAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APPROXIMATELY 12 INCHES LONG. WHEEL ASSEMBLY (P/N 3-1446-1) WHEEL ASSEMBLY HAS GO NE THROUGH 45 TIRE CHANGES SINCE NEW. WHEEL ASSEMBLY HAS BEEN REMOVED FROM SERVICE. 2 L 7 2 4T RT A31SO 1998050100050 19980501 00050 SO 1998 5 1 COMA9810108 1 19980422 A 3150 80055711 T/O WARNING EMB 120 EMB120RT SO E/E COMPT MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 205CA 13801 120205 'TRIM' AURAL WARNING DURING TAKEOFF. REPLACED THE AUDIO WARNING UNIT. 2 L 7 2 4T RT A31SO 1998050100051 19980501 00051 SO 1998 5 1 COMA9810109 1 19980421 A 3010 3D237606 CONTROL VALVE EMB 120 EMB120RT SO WING DE-ICE MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 249CA 19095 876 120230 LEFT AND RIGHT OUTBOARD WING DE-ICE CAUTION WARNINGS AFTER TAKEOFF. REPLACED THE DE-ICE EJECTOR CONTROL VALVE. 2 L 7 2 4T RT A31SO 1998050100052 19980501 00052 EA 1998 5 1 COMA9860085 1 19980419 A 3350 58728 COVER CNDAIR CL600 CL6002B19 EA CABIN CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 A 24 AND 48 MONTH INSPECTION. THE AFT 3 FOOT SECTION OF EMERGENCY FLOOR PATH LIGHTING, TRACK COVER IS CRACKED. REPLACE D TRACK COVER. 2 L 7 2 4F RT A21EA 1998050100053 19980501 00053 EA 1998 5 1 COMA9860086 1 19980419 A 5347 601R3103215 SEAT TRACK CNDAIR CL600 CL6002B19 EA BS 349 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 932CA 7038 A 24 AND 48 MONTH INSPECTION. LEFT FORWARD FLOOR SEAT RAIL IS CORRODED FS 349 AND 409+32. REPLACED SEAT RAIL. 2 L 7 2 4F RT A21EA 1998050100054 19980501 00054 NM 1998 5 1 UPS98226476 1 19980423 A 3350 51356B37 LIGHT BOEING 727 72722C 138400F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT ABOVE STAIR TO COCKPIT INOP (UPPER DECK). REMOVED AND REPLACED COCKPIT STAIR EMERGENCY LIGHT, OPS CHECK GOOD (P/N 51356B37) ON, (S/N 18149) ON, (S/N 33648) OFF. 2 L 7 3 4F A3WE 1998050100055 19980501 00055 NM 1998 5 1 UPS98226478 1 19980423 A 3350 BATTERY BOEING 727 72722C 138400F NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 929UP 19092 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS LIGHTS, COCKPIT FWD ENTRY DOOR INOP. REMOVED AND REPLACED BOTH SETS OF BATTE RIES OUT OF THE EMERGENCY EXIT LIGHT UNITS PER MM 25-60-00, OPS CHECK NORMAL AT THIS TIME. 2 L 7 3 4F A3WE 1998050100056 19980501 00056 WP 1998 5 1 98FDEA00275 1 19980417 A 2497 WIRE DOUG DC10 DC1010F 3022111 WP BS 1800 SHORTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 049FE 47803 SNRM NR N01247, AFT ENGINE INLET DUCT ACCESS PANEL NR 364GR POWER FEEDER CABLES SHORTED AT ADEL CLAMP CENTER FRAME. SPL ICED NEW CABLE 3X3 BO CAL FWD OF PRESSURE BULKHEAD, STA 1880 (SPLICED IN MAIN CABLE) PER MM 20-10-03. OPS CK ON ENG RUN CK'D NORMAL PER JRH 8-2. 2 L 7 3 4F A22WE 1998050100057 19980501 00057 NM 1998 5 1 DHL98726001 1 19980421 A 3040 656021130 CONNECTOR 512776 BOEING 727 727228 NM WINDOW HEAT SHORTED A DHLA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 01 726DH 266 20409 AURAL WARNING BOX ELECTRICAL SHORT, ALSO BOTH R-1 AND R-2 WINDOW HEAT CONTROLLERS ARE SHORTED OUT. REPLACED CANNON CON NECTOR 4774 AND AURAL WARNING BOX AND BOTH WINDOW HEAT CONTROLLERS. 2 L 7 3 4F A3WE 1998050100058 19980501 00058 NM 1998 5 1 VNAA9804019 1 19980416 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROP DIRTY A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 430JS 3044 DURING THE TAXI FOR TAKEOFF, THE RIGHT HAND PROPELLER OVERSPEED TEST, FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RET URNED TO THE GATE. MAINTENANCE CLEANED AND INSPECTED THE RIGHT HAND PROPELLER OVERSPEED GOVERNOR CANNON PLUG. OPERATIO NAL CHECKS WERE COMPLIED WITH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998050100059 19980501 00059 WP 1998 5 1 CKSA98263 1 19980418 A 7830 TR ACTUATOR DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE FAILED A CKSA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION DE DESCENT 1 GL 23 809CK 45803 643333 DURING DESCENT, NR 2 ENGINE FIRE WARNING CAME ON. PROCEDURES FOLLOWED IAW AIA FOM. ENGINE SHUTDOWN AND NR 2 BOTTLE FIR ED. NR 2 BOTTLE PRESS LOW LIGHT DID NOT COME ON NR 1 BOTTLE FIRED AND PRESS LOW LIGHT CAME ON. FOUND T/R ACTUATOR LEAK ING BADLY WHICH CAUSED THE FIRE WARNING TO GO OFF. REMOVED AND REPLACED T/R ACTUATOR ON ENGINE NR 2 OPS CHECK ON ENG RU N UP GOOD IAW DC8 MM 78-7-0. ALSO, REMOVED AND REPLACED NR 1 AND NR 2 FIRE BOTTLES. TEST GOOD IAW DC8 MM 26-4-1. 2 L 7 4 4F 4 F 4A25 1E8 1998050100060 19980501 00060 NM 1998 5 1 CKSA98264 1 19980417 A 2120 AIR DISTR BOEING 727 727223 1384074 NM COCKPIT ODOR A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 729CK 19482 PRIOR TO DESCENT, FUMES PRESENT ON FLT DECK. CAPT AND F/E EXPERIENCED IRRITATIONS. A/C HAD HAZMAT ABOARD NOT PREVIOUSL Y IDENTIFIED BY SHIPPER. A/C WAS DOWN LOADED AND SECURED FOR SHUTDOWN. CHECKED AREA WITH GAS ANALYZER PROBE, NO SIGN O F CONTAMINATION. ALL CARGO THAT WAS ON BOARD WAS CHECKED BY BDL FIRE DEPARTMENT, NO CONTAMINATION. COULD NOT DUPLICATE . DEFERRED PER MEL 30-7 CAT D DMI NR 88110798. INSPECTED REPELLANT SYSTEM FOR LEAKAGE, NO LEAKS FOUND. PLACARDS INSTA LLED, OPS CHECKED GOOD. THIS CLEARS DMI NR 88110798, PLACARDS REMOVED. 2 L 7 3 4F A3WE 1998050100256 19980501 00256 WP 1998 5 1 VJ9800140 1 19980423 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 LONGERON 17LT LOWER FLANGE CRACKED .5 INCH FROM LOWER EDGE AT FS 965 MAIN FRAME ATTACH HOLE AND CORRODED. REMOVED LONGE RON FROM FS 960 - 996. CUT, DRILLED DEBURRED NEW SECTION OF LONGERON AND INSTALLED FROM FS 956 - 996 IAW DC9 SRM 51010- 4, TRAVELER 1A-30766-1, CUT NEW SPLICE, DRILLED AND DEBURRED IAW DC9 SRM 53-02, FIG 18, TRAVELER 1A-30767-1. LONGERON A ND SPLICE TREATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED IAW DC9 SRM 53-02, FIG 18, 51-30-2. 2 L 7 2 4F A6WE 1998050100257 19980501 00257 WP 1998 5 1 VJ9800141 1 19980423 A 5720 59124371 DOUBLER DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 LT WING LOWER MAIN LANDING GEAR DOUBLER HAS SEVERAL BLEND OUTS BEYOND LIMITS. REMOVED LT LWR MLG DOUBLER IAW DC9 SRM 51 -30-5. DRILLED, COUNTERSUNK AND DEBURRED NEW DOUBLER IAW DC9 SRM 51-10-4. TREATED HOLES IAW DC9 SRM 51-10-3, INSTALLED AND SEALED DOUBLER IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998050100258 19980501 00258 WP 1998 5 1 VJ9800142 1 19980423 A 5313 S277792251A306 STRINGER DOUG DC9 DC932 3022066 WP BS 370-389 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 FWD CARGO PIT AT FS 380, 28L, CORRODED BEYOND LIMIT BETWEEN FS 370 - 389. REMOVED LONGERON 28L FROM FS 345 - 398. DRIL LED AND DEBURRED NEW LONGERON 28L. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-2, 51-10-4, AND 51-30-2. SHEAR TIE CRACKED AT FS 351. FABRICATED, DRILLED, DEBURRED SHEAR TIE. REPAIRED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3 AND 5 1-30-2 AFTER TREATING AND PRIMING. 2 L 7 2 4F A6WE 1998050100259 19980501 00259 WP 1998 5 1 VJ9800143 1 19980423 A 5320 1A20920130921 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 FUSELAGE SKIN AT ADF ANTENNA CORRODED BEYOND LIMIT AFTER REMOVAL OF CORROSION IAW SRM 51-01. REMOVED OVERHEAD CEILING P ANELS AND AIR CONDITIONING DUCTS FOR ACCESS. REPAIRED FUSELAGE SKIN IAW DC9 SRM 53-04, FIG 29, REINSTALLED DUCTS AND PA NELS IAW DC9 MM 25-22-0, 25-28-0 AND 20-11-0. DOUBLER 28.5 BY 16 INCHES AND FINGER DOUBLERS 28.5 BY 3 INCHES. 2 L 7 2 4F A6WE 1998050100260 19980501 00260 WP 1998 5 1 VJ9800144 1 19980423 A 5320 59124372 DOUBLER DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 LT WING LOWER MAIN LANDING GEAR DOUBLER HAS SEVERAL BLEND OUTS BEYOND LIMIT. REMOVED, REPLACED, DRILLED, COUNTER SUNK A ND DEBURRED NEW DOUBLER. TREATED AND PRIMED IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998050100261 19980501 00261 NM 1998 5 1 MALA976106 1 19980422 A 2910 O-RING DHAV DHC8 DHC8102 2809003 NM NR 1 HYD LINE LEAKING A MALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 831MA 339 DURING CRUISE FLIGHT, THE NR 1 HYDRAULIC QUANTITY VERY LOW. EMERGENCY LANDING IN MBS WITH QUANTITY INDICATING NEAR ZERO . LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED O-RING ON PRESSURE SUPPLY LINE NIPPLE FITTING. ALL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998050100262 19980501 00262 EU 1998 5 1 MALA976107 1 19980403 A 5320 FRAME BAC 146 AVRO146RJ85A 1500097 EU NLG DOORWAY CRACKED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 502XJ E2307 DAMAGE WAS NOTED ON THE LEFT NOSE LANDING GEAR DOOR FRAME. IN THE RETURN FLANGE COMMON TO THE OUTER SKIN PANEL, A 3.5 I NCH LONG CRACK WAS NOTED STARTING FROM THE FORWARD END GOING AFT. ALSO APPROXIMATELY 4 AFT OF THE FIRST CRACK, A 1.5 LO NG CRACK WAS NOTED. MAINTENANCE STOP DRILLED THE CRACKS ENDS AND DISASSEMBLED AS REQUIRED. FABRICATED A NESTED REPAIR ANGLE, DRILLED 2 ROWS OF FASTENERS IN THE VERTICAL FLANGE. ALODINE AND PRIME ALL TRIMMED AND FABRICATED PARTS IN ACCORD ANCE WITH AVRO STANDARD PROCEDURES. 2 H 7 4 4F RT A49EU 1998050100263 19980501 00263 NM 1998 5 1 K3HA980058 1 19980420 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 RIGHT AFT OVER WING EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-0. NO HELP, FOUND LOOSE P IN ON PLUG D2098 PER WD 33-51-02 (PIN NR 5) RESECURED, OPS CHECK OK PER MM 33-50-0. 2 L 7 3 4F A3WE 1998050100264 19980501 00264 NM 1998 5 1 K3HA980059 1 19980422 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 R-1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT, OPS CHECK GOOD REF MM 33-50-71. 2 L 7 3 4F A3WE 1998050100265 19980501 00265 NM 1998 5 1 K3HA980060 1 19980423 A 3350 07912 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 EMERGENCY PATH LIGHT, LIGHT MODULE COMING OUT THE TRACK COVER BETWEEN ROW SEAT 20ABCDEF. REPLACED TRACK (P/N 08163-000 1-08) AND LIGHT MANUAL IN ROW SEAT 20 ABCDEF. 2 L 7 3 4F A3WE 1998050100266 19980501 00266 NM 1998 5 1 K3HA980061 1 19980423 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 AFT OUTSIDE EMEGENCY LIGHT INOP ON LEFT SIDE. REMOVED AND REPLACED BATTERY PACK IAW 33-50-22, OPS CHECK OK. 2 L 7 3 4F A3WE 1998050100267 19980501 00267 WP 1998 5 1 CALA9800689 1 19980423 A 3222 STRUT DOUG DC9 DC982 3022082 WP NLG REQUIRED SERVICE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16808 49262 THE NOSE GEAR DID NOT RETRACT AFTER TAKEOFF FROM ORD. THE CHECKLIST WAS PERFORMED AND WHEN THE GEAR WAS PUT DOWN IT EXT ENDED WITH A BANG. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR STRUT FLAT. A FULL SERVICE WAS PERFORMED ON THE NOSE STRUT IAW MM 32-21-02. STRUT LEAK CHECK WAS GOOD. 2 L 7 2 4F A6WE 1998050100268 19980501 00268 NE 1998 5 1 9807022298 2 19980422 A 7320 MOISTURE TRAP BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE LT FUEL CONTL CONTAMINATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 298US 22152 696617 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENIGNE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE DRAINED FUEL CONTROL MOISTURE TRAP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998050100269 19980501 00269 WP 1998 5 1 9807039752 1 19980422 A 3260 301350201 PROCESSOR UNIT DOUG DC9 DC941 302207N WP E/E COMPT INOPERATIVE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 752NW 552 552 47116 DURING CLIMB-OUT, THE RIGHT MAIN INBOARD BRAKE ASSEMBLY INDICATED AN OVERTEMP CONDITION. THE FLIGHT CREW LOWERED THE LA NDING GEAR HANDLE PER COM PROCEDURES RESULTING IN A LANDING GEAR UNSAFE LIGHT ILLUMINATION. LANDING GEAR WAS RECYCLED W ITH A CONTINUAL ILLUMINATION OF THE LEFT LANDING GEAR UNSAFE LIGHT. FLIGHT LANDED AT DESTINATION WITHOUT INCIDENT. MAI NTENANCE REPLACED THE LANDING GEAR INDICATION PROCESSOR UNIT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100270 19980501 00270 WP 1998 5 1 9807049856 1 19980422 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE CHECK, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050100271 19980501 00271 WP 1998 5 1 9807059865 1 19980422 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 774NC 47776 DURING LINE CHECK, FOUND FIRST CLASS COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050100272 19980501 00272 WP 1998 5 1 9807069753 1 19980422 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 753NW 47117 DURING LINE CHECK, FOUND EMERGENCY LIGHTING INOPERATIVE AT FORWARD ENTRY DOOR, FORWARD SERVICE DOOR, AND NR 2 GALLEY. 2 L 7 2 4F A6WE 1998050100273 19980501 00273 NM 1998 5 1 9807076302 1 19980422 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM DOOR 3L-4L AND FROM 3R-4R. RECONNECTED WIRES. OP ERATIONAL CHECK OK 2 L 7 4 4F RT A20WE 1998050100274 19980501 00274 EU 1998 5 1 9807083244 1 19980421 A 3350 10103585 LIGHT AIRBUS 320 A320212 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 344NW 388 DURING LINE CHECK, EMERGENCY LIGHT TEST FAULTS UNIT EMER R. MAINTENANCE REPLACED LIGHT ASSEMBLY AT RIGHT FORWARD OVERWI NG EXIT. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998050100275 19980501 00275 1998 5 1 9807099603 4 19980423 A 3417 ADC DOUG DC9 DC932 3022066 WP E/E COMPT MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 603NW 47101 CAPTAIN'S ALTIMETER FLAG APPEARED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED AT APPROXIMATELY 120 KNOTS. MAINTENANCE COU LD NOT DUPLICATE DISCREPANCY. REPLACED AIR DATA COMPUTER AS A PRECAUTION. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998050100276 19980501 00276 WP 1998 5 1 9807109605 1 19980423 A 4990 APU DOUG DC9 DC932 3022066 WP PNEUMATIC SYST OIL LEAK A NWAA A UNSCHED LANDING K J B FLUID LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 605NW 47223 LEFT AFT LAVATORY SMOKE ALARM ACTIVATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. PROBLEM COULD NOT BE DUPLICATED ON GROUND. IT IS SUSPECTED THAT RESIDUAL OIL FROM THE APU LEAKED INTO THE PNEUMATIC SYSTEM. A IRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998050100277 19980501 00277 1998 5 1 9807119603 4 19980423 A 3416 4019953904 ALTIMITER DOUG DC9 DC932 3022066 WP LT COCKPIT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 603NW 34839 4400 47101 CAPTAIN'S ALTIMETER FLAPG APPEARED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED AT APPROXIMATELY 90 TO 95 KNOTS. MAINTENAN CE REPLACED THE ALTIMETER. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998050100278 19980501 00278 WP 1998 5 1 9807129969 1 19980422 A 2420 CONTROL PANEL DOUG DC9 DC931 3022065 WP RT GENERATOR MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 9333 47246 SHORTLY AFTER TAKEOFF, THE RIGHT GENERATOR CYCLED ON AND OFF FOUR TIMES THEN DROPPED OFF LINE. FLIGHT WAS RETURNED TO D TW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT GENERATOR CONTROL PANEL, VOLTAGE REGULATOR, GENERATOR, A ND CSD. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998050100279 19980501 00279 WP 1998 5 1 9807139906 1 19980421 A 2780 BRACKET DOUG DC9 DC931 3022065 WP NR 1 SLAT BROKEN A NWAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 01 956N 47252 DURING APPROACH INTO DTW, SLATS WOULD NOT EXTEND AND AIRCRAFT ROLLED TO THE RIGHT. CREW DECLARED AN EMERGENCY AND AIRCR AFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 SLAT INBOARD IDLER PULLEY BRACKET BROKEN LOOSE FROM FORWARD SPAR BR ACKET. AIRCRAFT WAS FERRIED TO ATL AND IS CURRENTLY BEING REPAIRED. 2 L 7 2 4F A6WE 1998050100280 19980501 00280 WP 1998 5 1 9807149924 1 19980421 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926RC 47473 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100281 19980501 00281 WP 1998 5 1 9807159938 1 19980422 A 3350 POWER SUPPY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1798U 47369 DURING LINE CHECK, FOUND THE LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. 2 L 7 2 4F A6WE 1998050100282 19980501 00282 WP 1998 5 1 9807169989 1 19980422 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8945E 47181 DURING LINE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE IN TAIL COMPARTMENT CATWALK. MAINTENANCE REPLACED THE POWER SUPPL Y. 2 L 7 2 4F A6WE 1998050100283 19980501 00283 WP 1998 5 1 9807179947 1 19980422 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN MISINSTALLED A NWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 01 8938E 47161 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHT INBOARD OF FORWARD LAVATORY INOPERATIVE. MAINTENANCE CORRECTED LIGHTIN G WIRING. OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F A6WE 1998050100284 19980501 00284 WP 1998 5 1 9807189990 1 19980422 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8950E 47186 DURING LINE CHECK, FOUND EMERGENCY OVERHEAD LIGHTING IN FIRST CLASS SECTION DIM. MAINTNANCE REPLACED BATTERIES AND POWE R SUPPLY. 2 L 7 2 4F A6WE 1998050100285 19980501 00285 WP 1998 5 1 9807199762 1 19980423 A 2410 CSD DOUG DC9 DC941 302207N WP LT ENGINE INOPERATIVE A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 762NW 47395 DURING FLIGHT, THE LEFT ENGINE DRIVEN GENERATOR SYSTEM BECAME INOPERATIVE. FLIGHT CREW FOLLOWED COM PROCEDURES. DIVERT ED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE CONSTANT SPEED DRIVE UNIT AND THE LEFT ENGI NE DRIVEN GENERATOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100286 19980501 00286 EU 1998 5 1 QXEA9800539 1 19980421 A 2170 DRAIN FOKKER F28 F28MK4000 4990810 EU COALESCER BAG PLUGGED A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 482US 11231 GEG - AIRCRAFT RETURNED TO FIELD DUE TO SMOKE IN THE CABIN. MAINTENANCE FOUND THE WATER SOCK DRAIN PLUGGED FOR THE CABI N PACK. THE DRAIN WAS UNPLUGGED AND THE WATER SOCK WAS CLEANED, IT WAS FULL OF WATER MIXED WITH OIL. SYSTEM WAS OPERAT IONALLY TESTED AND A TEST FLIGHT ACCOMPLISHED, TESTS NORMAL. THE APU WAS SUSPECTED OF PUTTING THE OIL IN THE BLEED AIR SYSTEM AND IS CURRENTLY ON MEL. 2 L 7 2 4F RT A20EU 1998050100287 19980501 00287 EU 1998 5 1 QXEA980540 1 19980421 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 SEA - SEVERAL EXIT LIGHTS INOP BY GALLEY SERVICE DOOR. MAINTENANCE RELAMPED, EXIT LIGHTS OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1998050100288 19980501 00288 1998 5 1 98FDEA00276 4 19980417 A 3417 CADC DOUG MD11 MD11F 3023600 NM E/E COMPT MALFUNCTIONED A FDEA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SO 25 613FE 48749 SNRM N01247 AT NRT: DURING CLIMB-OUT OF KIX GOT A GPWS TERRAIN WARNING AT 10,000 FT. ESCAPE MANUVER BEGAN FOLLOWED W/W INDSHEAR ALERT. CREW THEN GOT THE STICK SHAKER AND PITCH LIMIT IND. A/C DIVERTED, DUMPED FUEL AND LANDED IN NRT. REM OVED AND REPLACED THE NR 1 RADIO ALT, AND THE NR 2 CADC SWITCHING UNIT. PERFORMED PITOT-STATIC LEAK CK OPS CK'D OK. 2 L 7 3 4F RT A22WE 1998050100289 19980501 00289 NM 1998 5 1 98FDEA00277 1 19980417 A 5330 65545664 SKIN BOEING 727 727233 138408A NM BS 663 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 NR-0402, LWR FUSELAGE SKIN CORRODED ON UPPER SURFACE AT BS 663 BL0, WL 138. 2 L 7 3 4F RT A3WE 1998050100290 19980501 00290 NE 1998 5 1 98FDEA00278 2 19980420 A 7510 470926 ANTI-ICE DUCT BOEING 727 72725C 138400H NM PWA JT8 JT8D7 52053 NE NR 2 ENGINE DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 135FE 19853 NR 2 ENG LEFT HAND ENGINE INLET A/I DUCT DAMAGED, LOCATED JUST FWD OF THE A/I VALVE. *S/D* REMOVED AND REPLACED ANTI-I CE DUCT PER FED-EX M/M 75-10-14. 2 L 7 3 4F 4 F A3WE E2EA 1998050100291 19980501 00291 NM 1998 5 1 98FDEA00279 1 19980420 A 5320 651758866 SUPPORT BOEING 727 727233 138408A NM BS 266 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 NR 0577: WHILE WORKING NR-0573 FOUND 25 G-BEAM TO BE CORRODED AT BS 266 LBL 8 WL 208. REMOVED AND REPLACED 25 G-BEAM B S 266 LBL 8 - RBL 21.5 W 208 IAW FEDEX SRM 53-10-1, 51-30-2, FEDEX MM 57-20-21. 2 L 7 3 4F RT A3WE 1998050100292 19980501 00292 NM 1998 5 1 98FDEA00280 1 19980420 A 5320 691541610 SHEAR TIE BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 NR0573: WHILE WORKING NR0450 FOUND SHEAR TIE AT BS 720, LBL 5 - RBL 5 BETWEEN 28L-R WL 138 TO BE CORRODED AND OUT OF LI MITS. REMOVED CORRODED SHEAR TIE AND FABRICATED NEW AND INSTALLED IAW BAC DRW 65-15939 AND FEDEX SRM 51-20-1 AND 51-20- 2. 2 L 7 3 4F RT A3WE 1998050100293 19980501 00293 NM 1998 5 1 98FDEA00281 1 19980420 A 5330 655457721 SKIN BOEING 727 727233 138408A NM BS 683 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 WHILE WORKING ON NR0518, FOUND CORROSION ON SKIN AT BS 683 LBL 12 WL 138, BET 27L TO 28L. *S/D* REPAIRED SKIN AT BS 68 3, LBL 12, WL 138, BETWEEN STR 27L AND 28L PER FED-EX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1998050100294 19980501 00294 NM 1998 5 1 98FDEA00282 1 19980420 A 5330 655457721 SKIN BOEING 727 727233 138408A NM BS 700-720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION ON SKIN FWD CARGO BAY BS 700 TO 720 RBL 10 WL 138 NEXT TO STR 28R. *S/D* REMOVED CORRODED SKIN AT BS 700 TO 720, WL 138, RBL 10 AND INSTALLED INTERNAL DOUBLER. INSTALLED ALL ITEMS REMOVED FOR ACCESS IAW FED-EX SRM 53-30-3. 2 L 7 3 4F RT A3WE 1998050100295 19980501 00295 NM 1998 5 1 98FDEA00283 1 19980420 A 5320 65162794 BEAM BOEING 727 727233 138408A NM BS 760-790 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION (C53-224-01, 2) ON LONGITUDINAL BEAM FLANGES AT RBL 24 BS 760 TO 790 WL 208. *S/D* REMOVED AND REPLACED LONG ITUDINAL BEAM UPPER CHORD BS 740 TO 850, RBL 25 AND SEAT TRACK BS 760 TO 850, RBL 25, WL 208 PER FED-EX SRM 51-30-2 AND FED-EX DRAWING 65-16279. 2 L 7 3 4F RT A3WE 1998050100296 19980501 00296 NM 1998 5 1 98FDEA00284 1 19980420 A 5313 655623622 STRINGER BOEING 727 727233 138408A NM BS 710 CORROSION A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION ON STR 28R BS 710 WL 140. *S/D* REMOVED CORRODED STRINGER 28 RT, BS 710 TO 720 AND INSTALLED NEW SECTION AND REPAIR CAP AT BS 710 IAW FED-EX SRM 53-10-3. 2 L 7 3 4F RT A3WE 1998050100297 19980501 00297 NM 1998 5 1 98FDEA00285 1 19980420 A 5315 6516338171 FLOORBEAM BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION (C53-224-01, 2) ON UPPER CHORD OF BS 950 FLOORBEAM LBL 16 TO 19 WL 208. *S/D* REPAIRED CORROSION AREAS OF UP PER CHORD BS 950 FLOORBEAM FROM LBL 16 TO 19, WL 208 PER EA NR 7-5310-38742. 2 L 7 3 4F RT A3WE 1998050100298 19980501 00298 NM 1998 5 1 98FDEA00286 1 19980420 A 5320 65585373 CLIP BOEING 727 727233 138408A NM BS 681 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 LWR FRAME TO WEB CLIP CORRODED AT BS 681 LBL 3 WL 156. *S/D* CORRODED LOWER FRAME TO WEB CLIP AT BS 681, LBL 3, WL 15 6. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPLACED CORRODED LOWER FRAME TO WEB CLIP AND REINSTALLED PARTS R EMOVED FOR ACCESS IAW FED-EX SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998050100299 19980501 00299 WP 1998 5 1 ABXA9800375 1 19980422 A 5320 56144389 DOUBLER DOUG DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 INTERNAL DOUBLER AT GROUND AIR CONNECTION IS CRACKED. REPAIRED PER ABX REA D853-22653 MR. 2 L 7 4 4F 4A25 1998050100300 19980501 00300 WP 1998 5 1 ABXA9800376 1 19980422 A 5753 5652796 RIB DOUG DOUG DC8 DC862 3021970 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 WEB OF INBOARD RIB OF LEFT INBOARD FLAP IS CRACKED. REPAIRED IAW ABX REA D857-22657 MR. 2 L 7 4 4F 4A25 1998050100301 19980501 00301 WP 1998 5 1 ABXA9800377 1 19980328 A 5712 576949615 RIB DOUG DOUG DC8 DC862 3021970 WP WS 785 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 785.000. REPAIRED RIB IAW DWG K05056 AND DC 8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998050100302 19980501 00302 WP 1998 5 1 ABXA9800378 1 19980328 A 5712 576949615 RIB DOUG DOUG DC8 DC862 3021970 WP WS 578.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 578.750. REPAIRED IAW DWG K 05056 AND DC8 S RM 51-1-20D. 2 L 7 4 4F 4A25 1998050100303 19980501 00303 WP 1998 5 1 ABXA9800379 1 19980328 A 5712 576949613 RIB DOUG DOUG DC8 DC862 3021970 WP WS 785 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT WING LEADING EDGE RIB LOWER ARM CRACKED AT STATION XFS 785. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998050100304 19980501 00304 WP 1998 5 1 ABXA9800380 1 19980329 A 5320 37502571 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 620-640 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STATION 620-640 STRINGER 31R SPLICE FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998050100305 19980501 00305 WP 1998 5 1 ABXA9800381 1 19980329 A 5320 564660832 ANGLE DOUG DOUG DC8 DC862 3021970 WP BS 1380 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STATION 1380 BULKHEAD RIGHT, FORWARD SIDE, LOWER INTERCOSTAL, OUTBOARD FORWARD IS CRACKED ON UNDERSIDE. REPAIRED IAW DA CO DWG 5646608 AND DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998050100306 19980501 00306 WP 1998 5 1 ABXA9800382 1 19980329 A 5712 576949615 RIB DOUG DOUG DC8 DC862 3021970 WP WS 747.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 747.500. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998050100307 19980501 00307 WP 1998 5 1 ABXA9800383 1 19980329 A 5712 5769470 RIB DOUG DOUG DC8 DC862 3021970 WP WS 735 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 735.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998050100308 19980501 00308 WP 1998 5 1 ABXA9800384 1 19980329 A 5712 K05056 RIB DOUG DOUG DC8 DC862 3021970 WP WS 810 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 810.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998050100309 19980501 00309 WP 1998 5 1 ABXA9800368 1 19980421 A 3260 0080004003 PROX BOX DOUG DC9 DC931 3022065 WP E/E COMPT DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 944AX 47550 DURING FINAL APPROACH, GEAR DOOR OPEN LIGHT FAILED TO EXTINGUISH AFTER GEAR EXTENSION. RECYCLED GEAR AND LIGHT EXTINGUIS HED. REPLACED LANDING GEAR PROXIMITY BOX IAW DC9 MM 32-00. 2 L 7 2 4F A6WE 1998050100310 19980501 00310 WP 1998 5 1 ABXA9800369 1 19980421 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 941AX 47419 EMERGENCY EXIT LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1998050100311 19980501 00311 WP 1998 5 1 ABXA9800370 1 19980421 A 3231 RIVETS DOUG DC9 DC931 3022065 WP MLG DR TQ TUBE SHEARED A ABXA L ABORTED APPROACH O OTHER AP APPROACH 1 GL 23 923AX 47165 AFTER EXTENDING LANDING GEAR, GEAR DOOR OPEN LIGHT ILLUMINATED. ABORTED APPROACH AND RECYCLED GEAR. LEFT GEAR RED LIGH T AND GEAR DOOR OPEN LIGHT ILLUMINATED. CREW INITIATED EMERGENCY GEAR EXTENSION PROCEDURES AND LANDED WITH THE LEVER UP . LANDING WAS UNEVENTFUL. REPLACED SHEARED RIVETS IN THE TORQUE TUBE SEQUENCE AFM. 2 L 7 2 4F A6WE 1998050100312 19980501 00312 EA 1998 5 1 SWIA971157 1 19980404 A 5101 STRUCTURE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE AIRFRAME LIGHTNING STRIKE A SWIA A UNSCHED LANDING C F.O.D. CL CLIMB 1 NM 07 407SW 7034 DURING DEPARTURE CLIMB, INCURRED A LIGHTNING STRIKE. RETURNED TO AIRPORT. COMPLIED WITH LIGHTING INSPECTION AT MAINTEN ANCE BASE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998050100313 19980501 00313 WP 1998 5 1 CKSA98265 1 19980421 A 2612 FIRE LOOP DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE CHAFED A CKSA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 809CK 45803 643333 UPON INITIAL DESCENT NR 2 ENGINE FIRE WARNING CAME ON. COMPANY PROCEDURES FOLLOWED AND ENGINE WAS SECURED. FOUND WIRE CHAFFING AT RT FWD MAIN WIRE BUNDLE AT 3 O'CLOCK POSITION. WHEN MOVING BUNDLE, FIRE WARNING WOULD GO ON AND OFF DEPENDI NG ON THE POSITION OF BUNDLE. REPLACED WIRE. FIRE WARNING SYSTEM OPS CHECK NORMAL IAW MM 26. 2 L 7 4 4F 4 F 4A25 1E8 1998050100314 19980501 00314 SO 1998 5 1 98ZZZX1631 1 19980215 A 5210 1159SCB1001 SEAL GULSTM G1159 G1159B 3953535 SO CABIN DOOR TORN A BUEA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION NR NOT REPORTED 1 GL 23 36PN 42 'LOST PRESSURIZATION AT FL 390. COULD NOT CONTROL CABIN. MADE EMERGENCY DESCENT AND RETURNED TO PONTIAC'. REPLACED CA BIN DOOR SEAL AND DOOR SEAL CHECK VALVE. GROUND TEST AND FLIGHT TEST OF PRESSURIZATION SYSTEM NORMAL. 2 L 7 2 4F RT A12EA 1998050100315 19980501 00315 EU 1998 5 1 SABA980008 1 19980204 A 2612 D2370120 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE CHAFED A SABA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 33 964AE 964 OAJ - FLT 5114 - ON FLIGHT FROM LAJ/CLT AFTER TAKEOFF AND AT 6,000 FEET DURING CLIMB-OUT, NR 2 ENGINE FIRE BELL AND FIRE LIGHT CAME ON. AIRCREW FIRED BOTH FIRE BOTTLES ON NR 2 ENGINE. NR 2 ENGINE SHUT DOWN. AIRCRAFT RETURNED TO OAJ. AIR CREW DECLARED, IN-FLIGHT EMERGENCY. EMERGENCY PROCEDURES WERE USED. EMERGENCY VEHICLES WERE CALLED OUT. AIRCRAFT LAND ED AT OAJ WITH NO OTHER PROBLEMS. MAINTENANCE DEPLOYED FROM CLT/OAJ. MAINTENANCE FOUND THE FORWARD FIRE LOOP ON NR 2 E NGINE CHAFED AND SHORTED OUT. REMOVED AND REPLACED THE FORWARD FIRE LOOP. REPLACED LEFT AND RIGHT FIRE BOTTLES AND SQU IBS. ENGINE RUN COMPLETED. FIRE WARNING SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE AT 1,558 HOURS. (X) 2 L 7 2 4T RT A56EU 1998050100316 19980501 00316 EU 1998 5 1 SIMA980642 1 19980305 A 3320 6500111 LIGHT SOCKET SAAB SF340 340B 7860101 EU LAVATORY BURNED A SIMA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 21 397AE 340B397 ABI - FLT 3812 - CREW DIVERTED TO ABI WHILE EN ROUTE TO DFW WITH A LAV SMOKE LIGHT AND SMELL. MTX FOUND A LIGHT SOCKET IN LAV THAT WAS GETTING HOT. REPLACED FLUORESCENT LAMP SOCKET AND C/W WITH SB 340-33-047. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998050100317 19980501 00317 WP 1998 5 1 TWAA9804204 1 19980317 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1267-1278 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 924TW 49100 MCI - DURING OP 16 MAINTENANCE CHECK, INNER GRANULAR CORROSION WAS FOUND AT INBD SIDE OF NR 2 CHAIR TRACK, FS 1267 - FS 1278. REPLACED NR 2 CHAIR TRACK FS 1220 - FS 1309 PER SRM 53-08. (X) 2 L 7 2 4F A6WE 1998050100318 19980501 00318 WP 1998 5 1 TWAA9804205 1 19980316 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1140 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 924TW 49100 MCI - DURING OP 16 MAINTENANCE CHECK, INNER GRANULAR CORROSION WAS FOUND ON NR 1 CHAIR TRACK ON OTBD RADIUS STA 1140. R EPLACED CHAIR TRACK SECTION FS 1126 - FS 1145 OF NR 1 TRACK PER SRM 53-05 FIG 4. (X) 2 L 7 2 4F A6WE 1998050100319 19980501 00319 WP 1998 5 1 TWAA9804501 1 19980318 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 237-256 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 924TW 49100 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND NR 1 CHAIR TRACK CORRODED BEYOND LIMITS FS 237 TO FS 256. REPLACED CHAIR TR ACK SECTION PER SRM 51-01. (X) 2 L 7 2 4F A6WE 1998050100320 19980501 00320 WP 1998 5 1 TWAA9803705 1 19980313 A 2740 846D1003 MOTOR DOUG DC9 DC983 3022083 WP HORIZ STAB WORN A TWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CE 05 9619V 53566 STL - FLT 263 - PRIMARY LONGITUDINAL TRIM FAILED. FLIGHT RETURNED TO STL. REPLACED PRIMARY TRIM MOTOR. (X) 2 L 7 2 4F RT A6WE 1998050100321 19980501 00321 GL 1998 5 1 C2XA98CL026 2 19980312 A 7320 23069253 FADEC EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 1 ENGINE FAILED A C2XA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 SW 09 14942 490 BX46088 145037 SAV - FLT 4020 - CREW REPORTED DURING DESCENT, THE NR 1 ENGINE CONTROL 'B' FAILED AND THE ENGINE WAS SHUT DOWN. AIRCRAF T LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED FADEC 1A IAW EMB-145 MM 73-22-0 1. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1998050100322 19980501 00322 EU 1998 5 1 C2XA98IA071 1 19980309 A 3260 E0052R10B6SNE CONNECTOR AEROSP ATR42 ATR42500 EU LT MLG DIRTY A C2XA K NONE N FALSE WARNING CL CLIMB 1 SW 09 17448 506 IAH - FLT 3853 - DURING FLIGHT, CREW REPORTED THE LANDING GEAR CYCLED BEFORE IT WOULD RETRACT. MAINTENANCE CLEANED THE LEFT MAIN LANDING GEAR UPLOCK BOX CANNON PLUG AND THE AIRCRAFT WAS RELEASED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998050100323 19980501 00323 EU 1998 5 1 C2XA98IA072 1 19980309 A 3297 32316040CF24 WIRE AEROSP ATR42 ATR42500 EU LT MLG CHAFED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 17448 506 IAH - FLT 3857 - DURING FLIGHT, CREW REPORTED THE LEFT MAIN LANDING GEAR NR 1 SYSTEM UNLOCK LIGHT ILLUMINATED IN-FLIGHT. MAINTENANCE REPAIRED A CHAFED WIRE ON THE LEFT MAIN LANDING GEAR UPLOCK BOX AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (X) 2 H 7 2 4T RT A53EU 1998050100324 19980501 00324 EU 1998 5 1 C2XA98IA073 1 19980310 A 3260 D228830001 SWITCH AEROSP ATR42 ATR42500 EU LT MLG INOPERATIVE A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 09 17448 506 IAH - FLT 3876 - DURING FLIGHT IN BPT, THE CREW REPORTED THE LEFT MAIN LANDING GEAR SYSTEM NR 2 UNLOCK LIGHT ILLUMINATED IN-FLIGHT. THE AIRCRAFT WAS RELEASED TO SERVICE UNDER MEL. MAINTENANCE AT IAH SUBSEQUENTLY REMOVED AND REPLACED THE L EFT MAIN LANDING GEAR SYSTEM 2 PROXIMITY SWITCH AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998050100325 19980501 00325 SW 1998 5 1 HEEA0013858 1 19980406 A 6322 407040303101 FAN SHAFT BELL 407 407 SW BEARINGS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 343 53142 FAN SHAFT HAS ROUGH BEARINGS. 1 G 7 1 3U O H2SW 1998050100326 19980501 00326 EU 1998 5 1 HEEA0013884 1 19980413 A 3340 356H28 BULB SNIAS 350 AS350B2 8680813 EU STROBE LIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 72 2820 BULB BURNT OUT. 1 G 7 1 3U H9EU 1998050100327 19980501 00327 EU 1998 5 1 HEEA0013885 1 19980413 A 3340 356H28 BULB SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 79 2820 ONLY FLASHES ABOUT ONE MINUTE, THEN QUITS. 1 G 7 1 3U H9EU 1998050100328 19980501 00328 EU 1998 5 1 HEEA0013886 1 19980413 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 677 2771 STROBE WILL NOT FLASH. 1 G 7 1 3U H9EU 1998050100329 19980501 00329 EU 1998 5 1 HEEA0013887 1 19980413 A 3340 356H2802 POWER SUPPLY SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 149 2771 STROB WILL NOT FLASH. 1 G 7 1 3U H9EU 1998050100330 19980501 00330 EU 1998 5 1 HEEA0013888 1 19980413 A 7933 646600251 TEMP PROBE SNIAS 350 AS350B2 8680813 EU OIL SYS BROKEN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 105 2771 TEMP PROBE BROKEN. 1 G 7 1 3U H9EU 1998050100331 19980501 00331 EU 1998 5 1 HEEA0013889 1 19980413 A 7714 56337078012 INDICATOR SNIAS 350 AS350B2 8680813 EU ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 2653 SOME OF THE LIGHTS DO NOT LIGHT UP. REPLACEMENT PART S/N 453 TAKEN FROM CONSIGNMENT KIT. 1 G 7 1 3U H9EU 1998050100332 19980501 00332 EU 1998 5 1 HEEA0013890 1 19980413 A 5412 350A58011113 FIREWALL SNIAS 350 AS350B2 8680813 EU ENGINE DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 3859 2820 FIREWALL COMING APART. 1 G 7 1 3U H9EU 1998050100333 19980501 00333 EU 1998 5 1 HEEA0013891 1 19980413 A 6330 579065H MEMBER SNIAS 350 AS350B2 8680813 EU TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 1579 2873 RUBBER WORN. REPLACEMENT TAKEN FROM CONSIGNMENT KIT. S 1 G 7 1 3U H9EU 1998050100334 19980501 00334 EU 1998 5 1 HEEA0013892 1 19980413 A 6230 350A37112701 LINK SCISSORS SNIAS 350 AS350B2 8680813 EU M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 1551 2873 REMOVED AS SCISSOR ASSEMBLY. 1 G 7 1 3U H9EU 1998050100335 19980501 00335 EU 1998 5 1 HEEA0013893 1 19980413 A 6230 350A58101921 MOUNT SNIAS 350 AS350B2 8680813 EU M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 1551 2873 REMOVED AS SCISSOR ASSEMBLY. 1 G 7 1 3U H9EU 1998050100336 19980501 00336 EU 1998 5 1 HEEA0013894 1 19980413 A 7160 350A54108004 INTAKE SNIAS 350 AS350B2 8680813 EU ENG AIR CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 1551 2873 ENG AIR INTAKE CRACKED. 1 G 7 1 3U H9EU 1998050100337 19980501 00337 EU 1998 5 1 HEEA0013895 1 19980413 A 6730 AC67246 SERVO SNIAS 350 AS350B2 8680813 EU M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 4000L 1551 2873 FRONT SERVO CONTROL LEAKING. 1 G 7 1 3U H9EU 1998050100338 19980501 00338 1998 5 1 HEEA0013896 4 19980415 A 2210 214074301105 AMPLIFIER BELL 214 214ST 1182106 SW SCAS MALFUNCTION E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 59806 28140 PITCH CHANNEL KICKS IN FLIGHT. 2 G 7 2 4U H10SW 1998050100339 19980501 00339 SW 1998 5 1 HEEA0013897 1 19980415 A 5210 205030220010 TRACK ASSY BELL 212 212 1181420 SW RT UPPER DOOR DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 R/H UPPER DOOR TRACK NOT WIDE ENOUGH TO ALLOW ROLLER TO PASS WITHOUT JAMMING IN CHANNEL. 1 G 7 1 4U H4SW 1998050100340 19980501 00340 SW 1998 5 1 HEEA0013898 1 19980415 A 2810 206064611001 FUEL CELL BELL 206 206L1 1182107 SW FUEL SYS LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 3892R 45594 FUEL CELL LEAKING. 1 G 7 1 3U H2SW 1998050100341 19980501 00341 SW 1998 5 1 HEEA0013899 1 19980415 A 6220 412010182101 BEARING BELL 412 412 1182202 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2261D 248 33076 BEARING INNER RACE SHOULDER WORN ON ONE SIDE DUE TO LOST TORQUE OF NUT P/N MS14145L5 WHICH WAS CAUSED BY THE LACK OF THR EADS ON THIS NUT OR WASHER P/N AN960-516 NOT CONTACTING THE PITCH HORN FULLY. AS NOTED IN ASB 412-98-92. 1 G 7 2 4U H4SW 1998050100342 19980501 00342 SW 1998 5 1 HEEA0013902 1 19980415 A 6310 406340102101 CARBON SEAL 406040500123 BELL 407 407 SW FREEWHEEL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 2490 A2882 53003 FREEWHEEL CARBON SEAL LEAKING. (2500 HOUR OVERHAUL DUE) 1 G 7 1 3U O H2SW 1998050100343 19980501 00343 SW 1998 5 1 HEEA0013903 1 19980415 A 6230 206010451005 RING ASSY 206010450113 BELL 206 206L1 1182107 SW M/R MAST WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5737T JIJG09229 45454 SEAL RIDE WORN BEYOND LIMITS. 1 G 7 1 3U H2SW 1998050100344 19980501 00344 SW 1998 5 1 HEEA0013910 1 19980415 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DISC CRACKED ON INSIDE HOLE. 1 G 7 1 3U O H2SW 1998050100345 19980501 00345 SW 1998 5 1 HEEA0013911 1 19980415 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 DISC COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998050100346 19980501 00346 SW 1998 5 1 HEEA0013912 1 19980415 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998050100347 19980501 00347 EU 1998 5 1 HEEA0013913 1 19980415 A 7933 646600251 TEMP PROBE SNIAS 350 AS350B2 8680813 EU OIL TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2771 TEMP PROBE FAILED. GAUGE READING ERRATIC. 1 G 7 1 3U H9EU 1998050100348 19980501 00348 1998 5 1 HEEA0013914 4 19980415 A 3416 214175278101 INDICATOR BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1167G 53067 ENCODER TRANSPONDER READS 200 FEET OFF. 1 G 7 1 3U O H2SW 1998050100349 19980501 00349 EU 1998 5 1 HEEA0013915 1 19980415 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 169 2820 PITCH CONTROL ROD BEARING WORN. 1 G 7 1 3U H9EU 1998050100350 19980501 00350 EU 1998 5 1 HEEA0013916 1 19980415 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 281 2862 PITCH CONTROL ROD AXIAL WEAR, SPHERICAL BEARINGS. 1 G 7 1 3U H9EU 1998050100351 19980501 00351 EU 1998 5 1 HEEA0013917 1 19980415 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 171 2771 PITCH CONTROL ROD BEARINGS WORN. 1 G 7 1 3U H9EU 1998050100352 19980501 00352 EU 1998 5 1 HEEA0013918 1 19980415 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 101 2820 PITCH CONTROL WEAR INSIDE ID OF RUBBER BUSHING. 1 G 7 1 3U H9EU 1998050100353 19980501 00353 EU 1998 5 1 HEEA0013919 1 19980415 A 6220 117775P BALL JOINT SNIAS 350 AS350B2 8680813 EU STARFLEX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 2873 STARFLEX BALL JOINT EFLON WORN. 1 G 7 1 3U H9EU 1998050100354 19980501 00354 1998 5 1 HEEA0013920 4 19980415 A 2312 064105430 TRANSCEIVER SNIAS 350 AS350B2 8680813 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 3004 DISPLAY GOES OUT IN FLIGHT. "USE" DISPLAY IS INCORRECT. VERIFIED. "USE" DISPLAY INCORRECT. REPLACED I901 I.C. CHIP - NO HELP. REPLACED I505 AND I506 I.C. CHIPS - REPAIRED. TESTED UNIT. ADJUSTED SIDETONE. BENCH CHECK GOOD. 1 G 7 1 3U H9EU 1998050100355 19980501 00355 1998 5 1 HEEA0013921 4 19980416 A 3452 066106200 TRANSCEIVER KT76 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2249Z 45753 PULSE WIDTH OUT OF SPECS. UNABLE TO CHANGE PULSE WIDTH DUE IT BEING A SURFACE MOUNT COMPONENT. 1 G 7 1 3U H2SW 1998050100356 19980501 00356 1998 5 1 HEEA0013922 4 19980416 A 2312 069102405 TRANSCEIVER KX155 BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 104PH 3622 RADIO POWERS OFF BY ITSELF. (NO DISPLAY) VERIFIED COMPLAINT. PERFORMED PRELIMINARY INSPECTION AND FOUND UNIT TO HAVE N O DISPLAY DUE TO BURNT SPOT ON DISPLAY BOARD. 1 G 7 1 3U H2SW 1998050100357 19980501 00357 SW 1998 5 1 HEEA0013923 1 19980416 A 7930 1740352 INDICATOR 174000101 BELL 206 206L3 1182108 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3116L 4841 51529 INDICATOR WILL NOT INDICATE. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998050100358 19980501 00358 SW 1998 5 1 HEEA0013924 1 19980416 A 7930 174035201 INDICATOR 174000103 BELL 206 206L1 1182107 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2775A 4178 45297 INDICATOR WILL NOT INDICATE. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998050100359 19980501 00359 SW 1998 5 1 HEEA0013925 1 19980416 A 7930 174035201 INDICATOR 174000103 BELL 206 206L1 1182107 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2135V 4181 45657 WILL NOT INDICATE. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998050100360 19980501 00360 SW 1998 5 1 HEEA0013926 1 19980416 A 7930 174035201 INDICATOR 174000103 BELL 206 206L3 1182108 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 41128 3969 51134 INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 1 3U H2SW 1998050100361 19980501 00361 1998 5 1 HEEA0013927 4 19980416 A 3457 0110010600 GPS GPS165 BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 SEVERAL LED INOPERATIVE, LOWER DISPLAY. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT DISPLAYING STRANGE CHARACTERS, AND WILL NOT LOCK ON. 1 G 7 2 4U H4SW 1998050100362 19980501 00362 SW 1998 5 1 HEEA0013928 1 19980416 A 7714 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2149S 36002 TRIPLE TACH NR2 NEEDLE AND ROTOR NEEDLE ARE INOPERATIVE. 1 G 7 2 4U H4SW 1998050100363 19980501 00363 1998 5 1 HEEA0013929 4 19980416 A 3421 5040017901 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 321 2873 ATTITUDE INDICATOR HAS LOOSE SCREW INSIDE OF UNIT. 1 G 7 1 3U H9EU 1998050100364 19980501 00364 1998 5 1 HEEA0013930 4 19980416 A 2312 064101902 TRANSCEIVER KY196 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81832 S828 HEAVY STATIC AND NO SIDETONE. PERFORMED PRELIMINARY INSPECTION. ADJUSTED C/N SQUELCH AND SIDETONE. REPAIRED. ALSO ADJ USTED CARRIER SQUELCH. FOUND TRANSMIT POWER OUT LOW. REPLACED C623 AND C624 CAPACITORS. NO HELP. REPLACED T604 TRANS FORMER. REPAIRED BUT FOUND MODULATIONDISTORTED AT 85% MODULATION. REPLACED Q120, Q121, Q122, Q125 AND Q126 TRANSISTORS . MODULATION STILL DISTORTED. 1 G 7 2 3U H3EU 1998050100365 19980501 00365 1998 5 1 HEEA0013931 4 19980416 A 3457 0845000000 GPS SKYNAV5000 BOLKMS 117 BK117A3 5626015 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911NC 7026 GPS NOT PICKING UP SATELLITES. 1 G 7 2 3U H13EU 1998050100366 19980501 00366 EU 1998 5 1 HEEA0013932 1 19980416 A 7930 1740352 INDICATOR 174000101 BOLKMS 105 BO105S 5626006 EU ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 967MB 463 S737 INDICATOR WILL NOT INDICATE. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 2 3U H3EU 1998050100367 19980501 00367 EU 1998 5 1 HEEA0013933 1 19980416 A 7930 174035201 INDICATOR 174000103 BOLKMS 105 BO105S 5626006 EU ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K 4164 S859 INDICATOR WILL NOT INDICATE. INDICATOR WAS REMOVED FROM BOWL AND CLEANED. INSTALLED INDICATOR BACK ON BOWL, TESTED AND INDICATOR STILL DIDN'T WORK. 1 G 7 2 3U H3EU 1998050100368 19980501 00368 EU 1998 5 1 HEEA0013934 1 19980416 A 2435 230321825 STATOR 23032048 BOLKMS 117 BK117B2 5626013 EU START/GEN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 136AE 23685 7234 STATOR DEFECTIVE CAUSING VERY HIGH FIELD CURRENT AND BRUSH LEADS ARE TOO LONG. 1 G 7 2 3U NC H13EU 1998050100369 19980501 00369 1998 5 1 HEEA0013935 4 19980416 A 3434 066104400 RECEIVER KMR675 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 OUTER MARKER INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND WHITE INNER MARKER LIGHT TO BE INOPERATIVE. REPLACED TRANSISTOR Q106. NO HELP. FOUND AGC NOT WORKING. REPLACED INTEGRATED CIRCUIT I105, CAPACITOR C120, RESISTORS R125, R 122, AND R128 AND TRANSISTOR Q103.NO HELP. 1 G 7 2 3U H1NE 1998050100370 19980501 00370 1998 5 1 HEEA0013936 4 19980416 A 3451 066106600 TRANSCEIVER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 TRANSCEIVER WILL NOT COME UP ON LINE. (DOES NOT TRANSMIT OR RECEIVE) PERFORMED PRELIMINARY INSPECTION. TROUBLESHOT AND FOUND VCO BUFFER, RVTTS, AND IF/AGC BOARDS BAD. 1 G 7 2 3U H1NE 1998050100371 19980501 00371 1998 5 1 HEEA0013937 4 19980416 A 2312 40001278500 TRANSCEIVER RT40 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911MJ 760231 NO TRANSMIT OR RECEIVE (400 MHZ RT INOPERATIVE ON FM RADIO) FOUND K1 RELAY CORRODED. SYNTHESIZER BOARD CAUSES NON-LINEA R POWER. 1 G 7 2 3U H1NE 1998050100372 19980501 00372 NE 1998 5 1 HEEA0013938 1 19980416 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 12525 760229 T/R BLADE TRAILING EDGE ON PADDLE "A" SPLIT OPEN. 1 G 7 2 3U H1NE 1998050100373 19980501 00373 NE 1998 5 1 HEEA0013939 1 19980416 A 2436 7655009005104 GENERATOR CONTRO SKRSKY S76 S76A 8143006 NE DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 CAUSING A/C GENERATOR TO KICK OFF LINE. 1 G 7 2 3U H1NE 1998050100374 19980501 00374 SW 1998 5 1 HEEA0013940 1 19980416 A 7714 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 TRIPLE TACH READS HIGH AND NEEDLES 1 AND 2 HAVE EXCESSIVE FRICTION ERROR. 1 G 7 2 4U H4SW 1998050100375 19980501 00375 NE 1998 5 1 HEEA0013941 1 19980416 A 2421 7655009005105 GENERATOR SKRSKY S76 S76A 8143006 NE AC SYS WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1545X 760050 A/C GEN WORN AND DRY DRIVESHAFT AND ROTOR SPLINES. 1 G 7 2 3U H1NE 1998050100376 19980501 00376 GL 1998 5 1 HEEA0013942 2 19980416 A 7314 3944001 FUEL PUMP SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 792CH 760193 FUEL PUMP WORN DRIVE SHAFT SPLINES AND GEAR SPLINES. 1 G 7 2 3U 3 U H1NE E1GL 1998050100377 19980501 00377 1998 5 1 HEEA0013943 4 19980416 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 137AE S851 2 YEAR INSPECTION DUE. PERFORMED PRELIMINARY INSPECTION. FOUND BACKUP BATTERY TO BE DEAD AND ALSO FOUND PLASTIC ON SID E OF UNIT TO BE CRACKED. 1 G 7 2 3U H3EU 1998050100378 19980501 00378 SW 1998 5 1 HEEA0013944 1 19980416 A 6720 206001188001 PLATE ASSY BELL 206 206L1 1182107 SW MIXING LEVER ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 BEARING ROUGH, RATCHETY AND CANNOT BE REPLACED. SCRAPPED BEARING AND REPLACED WITH SERVICEABLE BEARING. 1 G 7 1 3U H2SW 1998050100379 19980501 00379 SW 1998 5 1 HEEA0013945 1 19980416 A 6700 206001328007 SLEEVE BELL 206 206L1 1182107 SW FLT CONTROL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 CORROSION BEYOND LIMITS ON INSIDE DIAMETER OF RETAINER RING. SCRAPPED REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1998050100380 19980501 00380 SW 1998 5 1 HEEA0013946 1 19980416 A 6710 206001343001 ELBOW BELL 206 206L1 1182107 SW M/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078D 45397 CORROSION BEYOND LIMITS AROUND BOLT HOLE AND AROUND SHOULDER AREA. SCRAPPED LOCALLY. REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1998050100381 19980501 00381 EU 1998 5 1 HEEA0013947 1 19980416 A 6710 10541121 BELLCRANK BOLKMS 105 BO105S 5626006 EU FLT CONT CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5029H S670 CORROSION AND PITTING IN BEARING MOUNTING BORE. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H3EU 1998050100382 19980501 00382 1998 5 1 HEEA0013948 4 19980416 A 2312 4000106010 CONTROL UNIT C10 SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 707AE 760276 LED DISPLAY WON'T DIM. PERFORMED PRELIMINARY INSPECTION. REPLACED PHOTOCELL RT1. REPAIRED PROBLEM. ALSO FOUND THUMBWH EEL INTERMITTENT. CLEANED THUMBWHEEL AND RESOLDERED CONTACTS ON THUMBWHEEL. NO HELP. REPLACED THUMBWHEEL S1. REPAIRE D PROBLEM. TOUCHED UP FACEPLATE.BENCH CHECK GOOD. 1 G 7 2 3U H1NE 1998050100383 19980501 00383 1998 5 1 HEEA0013949 4 19980416 A 3444 7001840903 TRANSCEIVER BELL 212 212 1181420 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 TRANSCEIVER DISPLAY 50,250,400 AND 1200 LED'S GO OUT. 1 G 7 1 4U H4SW 1998050100384 19980501 00384 1998 5 1 HEEA0013950 4 19980416 A 3424 214075244001 RATE GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 RATE GYRO TURN NEEDLE STICKS. 1 G 7 2 4U H4SW 1998050100385 19980501 00385 1998 5 1 HEEA0013951 4 19980416 A 3120 M811B DIGITAL CLOCK BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 CLOCK GOES OFF AND ON. 1 G 7 2 4U H4SW 1998050100386 19980501 00386 SW 1998 5 1 HEEA0013952 1 19980416 A 2435 23032048 GENERATOR BELL 206 206B3 1181506 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22743 11484 3624 DROPS OFF LINE IN FLIGHT. COMES BACK ON WITH RESET FIELD SWITCH. 1 G 7 1 3U H2SW 1998050100387 19980501 00387 1998 5 1 HEEA0013953 4 19980416 A 3440 066304550 DISPLAY KP1553A BOLKMS 117 BK117B2 5626013 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 132AE 7238 DIGITAL DISPLAY IS INOPERATIVE. 1 G 7 2 3U NC H13EU 1998050100388 19980501 00388 1998 5 1 HEEA0013954 4 19980416 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 ELT WOULD NOT GO OFF POSITION. 1 G 7 2 3U H3EU 1998050100389 19980501 00389 1998 5 1 HEEA0013955 4 19980416 A 2562 ELT910 ELT NARCO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 ELT INOPERATIVE. 1 G 7 2 4U H4SW 1998050100390 19980501 00390 1998 5 1 HEEA0013956 4 19980416 A 2562 ELT910 ELT NARCO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5742N 45477 ELT WILL NOT TURN OFF. 1 G 7 1 3U H2SW 1998050100391 19980501 00391 1998 5 1 HEEA0013957 4 19980416 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 NR2 REEL PITCH CHATTERS. 1 G 7 2 3U H1NE 1998050100392 19980501 00392 SW 1998 5 1 HEEA0013958 1 19980416 A 2622 MODEL344 FIRE EXTINGUISHE BELL 206 206L1 1182107 SW CABIN DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5007Y 45192 PRESSURE AND WEIGHT ARE LOW. 1 G 7 1 3U H2SW 1998050100393 19980501 00393 1998 5 1 HEEA0013959 4 19980416 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW COCKPIT NOISY E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 TARSYN NOISY BEARING. 1 G 7 2 4U H4SW 1998050100394 19980501 00394 1998 5 1 HEEA0013960 4 19980416 A 2564 214070943108 LIFE RAFT BELL 214 214ST 1182106 SW EMERG EQUIP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 WILL NOT FIT IN THE AIRCRAFT. 2 G 7 2 4U H10SW 1998050100395 19980501 00395 SW 1998 5 1 HEEA0013961 1 19980416 A 7714 65023046 DUAL TACH BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078G 45398 DUAL TACHNEEDLE SPLIT. 1 G 7 1 3U H2SW 1998050100396 19980501 00396 SW 1998 5 1 HEEA0013962 1 19980416 A 7712 412075008111 INDICATOR BELL 412 412 1182202 SW NR 1 ENG TORQ FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 33023 NR1 ENGINE SIDE POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1998050100397 19980501 00397 SW 1998 5 1 HEEA0013963 1 19980416 A 2841 206075189001 INDICATOR BELL 206 206B3 1181506 SW FUEL QTY STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107PH 2789 FUEL QTY INDICATOR NEEDLE STUCK BETWEEN 55 AND 60 GALLONS. 1 G 7 1 3U H2SW 1998050100398 19980501 00398 1998 5 1 HEEA0013964 4 19980416 A 3421 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22342 760096 NR1 ROLL KICKS. VERT GYRO FAULTY 1 G 7 2 3U H1NE 1998050100399 19980501 00399 1998 5 1 HEEA0013965 4 19980416 A 3416 066306401 ENCODER SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 760181 ENCODER INDICATES OUT OF TOLERANCE. 1 G 7 2 3U H1NE 1998050100400 19980501 00400 1998 5 1 HEEA0013966 4 19980416 A 2211 4008519916 COMPUTER BEECH 200 200BEECH 1152920 CE AUTO FLIGHT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 789DS BB478 VERTICAL ATITUDE FUNCTION INOPERATIVE. 1 L 7 2 4T A24CE 1998050100401 19980501 00401 1998 5 1 HEEA0013967 4 19980416 A 3421 2360041902 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1078C 45392 ATTITUDE INDICATOR HAS BAD BEARINGS. 1 G 7 1 3U H2SW 1998050100402 19980501 00402 1998 5 1 HEEA0013968 4 19980416 A 3421 2360041902 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2250U 45754 ATTITUDE INDICATOR HAS BAD BEARINGS. 1 G 7 1 3U H2SW 1998050100403 19980501 00403 1998 5 1 HEEA0013969 4 19980416 A 3421 2360041902 INDICATOR BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1072T 45385 INDICATOR ROTOR BEARINGS FROZEN. 1 G 7 1 3U H2SW 1998050100404 19980501 00404 1998 5 1 HEEA0013970 4 19980416 A 3454 066302440 INDICATOR KPI552 BOLKMS 117 BK117A4 5626017 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 COMPASS CARD PRECESSES AND SLOW LOCALIZER. 1 G 7 2 3U H13EU 1998050100405 19980501 00405 EU 1998 5 1 HEEA0013971 1 19980416 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU OIL SYS STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8197X S808 VALVE STICKS INTERMITTENTLY. 1 G 7 2 3U H3EU 1998050100406 19980501 00406 GL 1998 5 1 HEEA0013972 2 19980416 A 7250 6851531 NOZZLE 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL NR 4 DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22718 CAT40270 3618 CAE834218 RECEIVED NR4 NOZZLE AND ATTEMPTED TO MACHINE TIP PATHS. NOTED: COATING LIFTING AND FLAKING DURING MACHINING. 1 G 7 1 3U 3 U H2SW E4CE 1998050100407 19980501 00407 NE 1998 5 1 HEEA0013973 2 19980416 A 7320 324473513 FUEL CONTROL BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 AFCU BROKEN. FOUND PX-PY ADAPTER BROKEN. REPLACED WITH SERVICEABLE PART. 1 G 7 2 4U 4 U H4SW E22EA 1998050100408 19980501 00408 1998 5 1 HEEA0013974 4 19980416 A 2562 ELT910 ELT NARCO BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 ELT COMES ON INTERMITTENTLY. 1 G 7 2 3U H3EU 1998050100409 19980501 00409 SW 1998 5 1 HEEA0013975 1 19980416 A 3340 212075139001 LANDING LIGHT BELL 412 412 1182202 SW MOTOR CONTACTS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 LANDING LIGHT WOULD NOT TURN OFF WHEN LIGHT IS HOT. REPLACED GEAR, CLEANED MOTOR CONTACTS. UNIT MEETS MFG SPECS. 1 G 7 2 4U H4SW 1998050100510 19980501 00510 WP 1998 5 1 VJ9800145 1 19980427 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 AFT FRAME CORRODED, LT SIDE 6 INCHES ABOVE FLOOR, AT FS 996. FABRICATED SPLICE, 15 BY 2 BY 1 INCHES IAW DC9 SRM 53-03, FIG 14 AND FRAME, 15 BY 2 BY 1 INCHES, IAW DAC DWG 5910163 AND RES 1 05439. INSTALLED REPAIR PARTS IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998050100511 19980501 00511 NM 1998 5 1 MALA976108 1 19980426 A 2422 DH103024600C INVERTER DHAV DHC8 DHC8102 2809003 NM LT COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 824MA 327 DURING FLIGHT, THE PRIMARY INVERTER CIRCUIT BREAKER POPPED. CREW RAN QRH ITEMS, RESET CIRCUIT BREAKER PER MAINTENANCE C ONTROL, CIRCUIT BREAKER IMMEDIATELY POPPED AGAIN. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE PRIMARY INVERTER. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998050100512 19980501 00512 NM 1998 5 1 CALA9800691 1 19980425 A 3260 SWITCH BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 69311 23362 THE AIRCRAFT HAD A HISTORY OF THE NOSE GEAR RED UNSAFE LIGHT ILLUMINATING IN FLIGHT. MAINTENANCE REMOVED AND REPLACED T HE NOSE GEAR LOCK SWITCH IAW MM 32-61-41. THE NOSE GEAR DOWN SENSOR WAS REPLACED IAW MM 32-61-51. IN ADDITION, THE LAN DING GEAR LOGIC CARDFILE UNIT WAS REPLACED AND TESTED IAW MM 32-09-20, PAGES 401-424. ALL CHECKS WERE NORMAL. THE AIRC RAFT HAS FLOWN FIVE FLIGHTS WITHOUT REPEAT OF THE PROBLEM SINCE THIS CORRECTIVE ACTION WAS IMPLEMENTED. 2 L 7 2 4F RT A16WE 1998050100513 19980501 00513 NM 1998 5 1 CALA9800692 1 19980423 A 5753 SKIN BOEING 757 757224 1384958 NM RT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17122 27564 INSPECTION FOUND A 1.3 CRACK ON NR 4 FLAP LOWER SURFACE OUTBOARD SECTION AND TWO EACH RIVETS POPPED ON UPPER SURFACE OF FLAP, RT WING. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW ECRA 5750-02940. 2 L 7 2 4F RT A2NM 1998050100514 19980501 00514 WP 1998 5 1 CALA9800693 1 19980423 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND A 1 CRACK AT AFT END OF FORWARD ENTRY DOOR NR 2 BEAM. THE BEAM WAS REPAIRED IAW SRM 52-05, PAGE 179. 2 L 7 2 4F A6WE 1998050100515 19980501 00515 WP 1998 5 1 CALA9800694 1 19980423 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND A .75 INCH CRACK AT AFT END OF FORWARD ENTRY DOOR NR 7 BEAM. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-05-31. 2 L 7 2 4F A6WE 1998050100516 19980501 00516 NM 1998 5 1 CALA9800695 1 19980423 A 5230 FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39340 23578 INSPECTION FOUND A 6 CRACK AT LOWER FORWARD CORNER OF FORWARD CARGO DOOR SIDE FRAME WEB. A REPAIR WAS INSTALLED IAW ECR A 5234-01003. 2 L 7 2 4F RT A16WE 1998050100517 19980501 00517 NM 1998 5 1 CALA9800696 1 19980330 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 714 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15781 20636 INSPECTION FOUND CRACKS IN FORWARD PIT FLOOR SUPPORT AT STA 714, LBL 2. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1, P AGE 6. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-3. 2 L 7 3 4F A3WE 1998050100518 19980501 00518 NM 1998 5 1 CALA9800697 1 19980424 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND STRINGER 28L CORRODED AT STA 720D. THE CORRODED AREA OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3. 2 L 7 3 4F A3WE 1998050100519 19980501 00519 NM 1998 5 1 CALA9800698 1 19980424 A 5311 FRAME BOEING 727 727232 1384082 NM BS 560 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A .375 INCH CRACK WITH CORROSION IN FRAME 560 TO SKIN ATTACH FLANGE, BBL 0 TO LBL 6. THE CORRODED AREA OF FLANGE WAS CUT OFF IAW SRM 53-10-4. A NEW FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1998050100520 19980501 00520 NM 1998 5 1 CALA9800699 1 19980424 A 5311 FRAME BOEING 727 727232 1384082 NM BS 640 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A 1 CRACK IN UPPER FLANGE RADIUS OF FRAME 640, RBL 8, FORWARD BAGGAGE BIN. THE CRACKED AREA WAS CUT OU T IAW SRM 51-40-3. A DOUBLER AND FITTING WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1, SHEET A, SRM 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998050100521 19980501 00521 NM 1998 5 1 CALA9800700 1 19980424 A 5530 SUPPORT BOEING 727 727232 1384082 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A 1 CRACK IN VERTICAL STABILIZER SUPPORT WEB AT STRINGER 3L AND STRINGER 3R. THE LT AND RT SUPPORT WEB WAS REMOVED. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998050100522 19980501 00522 NM 1998 5 1 CALA9800701 1 19980424 A 5530 SUPPORT BOEING 727 727232 1384082 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 INSPECTION FOUND A 2.5 CRACK IN VERTICAL STABILIZER STRINGER 4L SUPPORT WEB. THE SUPPORT WEB WAS REMOVED IAW SRM 51-30- 2. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998050100523 19980501 00523 WP 1998 5 1 9807209605 1 19980422 A 4990 GTCP8598D APU DOUG DC9 DC932 3022066 WP TAIL FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 01 605NW 48431 4864 47223 AFTER ENGINE START SMOKE BEGAN TO ENTER CABIN. PLANE WAS AT THE GATE AND PASSENGERS WERE DEPLANED THROUGH THE GATEWAY. MAINTENANCE ISOLATED SOURCE OF SMOKE TO OIL IN PNEUMATIC SYSTEM FROM THE APU. PLACED APU ON MEL AND REPLACED WATER SEP ARATORS. 2 L 7 2 4F A6WE 1998050100524 19980501 00524 NE 1998 5 1 9807219869 2 19980425 A 7321 7436024 FUEL CONTROL DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 778NC 36854 3872 48100 696730 DURING TAKEOFF ROLL AT 130 KNOTS, THE LEFT ENGINE EXPERIENCED COMPRESSOR STALLS. CREW COMPLETED TAKEOFF THEN RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL CONTROL UNIT. OPERATIONAL CHECK OK . AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 1998050100525 19980501 00525 NM 1998 5 1 9807222298 1 19980424 A 7711 EPR SYST BOEING 727 727251 138408H NM PWA JT8 JT8D15A 52051 NE LT ENGINE MALFUNCTIONED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 298US 22152 696617 AS TAKEOFF POWER WAS APPLIED, THE LEFT ENGINE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE MEL'D EPR SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998050100526 19980501 00526 EU 1998 5 1 9807233206 1 19980423 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 360US 60 DURING TEST OF THE EMERGENCY LIGHT SYSTEM, INT LOAD EMERG L FAULT WAS DISPLAYED. MAINTENANCE REPLACED BATTERY PACK AND POWER SUPPLY 11WL. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998050100527 19980501 00527 GL 1998 5 1 9807241227 2 19980424 A 7260 PACKING DOUG DC10 DC1030 3023501 WP GE CF6 CF650C 30018 GL NR 2 ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 227NW 46969 455929 WHILD CLIMBING THROUGH FL200 (TPE), THE NR 2 ENGINE OIL QUANTITY INDICATION DROPPED TO ZERO WITH THE INDICATED OIL PRESS URE DOWN TO 10 PSI. THE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED ONE MINUTE LATER. THE CREW THEN FOLLOWED COM PROCED URES AND SHUT DOWN THE ENGINE. THE AIRCRAFT RETURNED TO TPE AND LANDED WITHOUT FURTHER DIFFICULTY. MAINTENANCE REPLACE D THE PACKING ON THE MASTER CHIP DETECTOR. FOLLOW-UP ENGINE RUN WAS NORMAL WITH NO LEAKS NOTED. 2 L 7 3 4F 4 F A22WE A23EA 1998050100528 19980501 00528 WP 1998 5 1 9807259860 1 19980424 A 2822 BOOST PUMP DOUG DC9 DC951 3022051 WP LT WING LEAKING A NWAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 GL 01 769NC 47757 DURING CLIMB-OUT, THE FLIGHT CREW NOTICED A STREAM OF FLUID LEAKING FROM THE LEFT WING. FLIGHT CREW DECLARED AN EMERGEN CY, FOLLOWED COM PROCEDURES, RETURNED TO DFW, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT SIDE AFT BOOS T PUMP VOLUTE. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050100529 19980501 00529 SO 1998 5 1 COMA9810110 1 19980424 A 4950 GTCP36150AA APU EMB 120 EMB120RT SO EMPENNAGE SMOKING A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 189CA 6968 120189 FLIGHT DECK FILLED WITH SMOKE DURING PRE-FLIGHT INSPECTIONS, APU WAS OPERATING, NO PASSENGERS ON BOARD. DEFERRED APU PE R MEL 49-00-1. 2 L 7 2 4T RT A31SO 1998050100530 19980501 00530 EA 1998 5 1 COMA9860087 1 19980425 A 5320 MS20426ADS RIVET CNDAIR CL600 CL6002B19 EA BS 333 BURNED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 960CA 4932 7117 DURING LIGHTNING STRIKE INSPECTION, FOUND A DEEP BURN ON AIRCRAFT BELLY AT FUSELAGE STATION 333.00. UPON FURTHER INVEST IGATION, FOUND BURN TO BE IN A RIVET HEAD. REMOVED THE RIVET AND INSTALLED A NEW ONE IN ACCORDANCE WITH CANADAIR STRUCT URAL REPAIR MANUAL CHAPTER 51-42-06. 2 L 7 2 4F RT A21EA 1998050100531 19980501 00531 EA 1998 5 1 COMA9860088 1 19980424 A 2612 21804100 FIRE LOOP CNDAIR CL600 CL6002B19 EA LT PYLON DEFECTIVE A COMA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 918CA 7018 LEFT 14TH STAGE BLEED DUCT WARNING MESSAGE ILLUMINATED DURING CRUISE FLIGHT AND WOULD NOT EXTINQUISH WITH REDUCED POWER. LEFT ENGINE WAS SHUTDOWN AND AIRCRAFT DIVERTED TO CMH. REPLACED THE LEFT ENGINE 14TH STAGE FIRE DETECTION LOOP. 2 L 7 2 4F RT A21EA 1998050100532 19980501 00532 EA 1998 5 1 COMA9860089 1 19980424 A 3230 G601R1011031 PIN CNDAIR CL600 CL6002B19 EA MLG INSTALLED A COMA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 991CA 7216 LANDING GEAR WOULD NOT RETRACT DURING CLIMB OUT, AIRCRAFT RETURNED TO THE FIELD. REMOVED GEAR DOWN LOCK PINS FROM MLG. 2 L 7 2 4F RT A21EA 1998050100533 19980501 00533 NM 1998 5 1 UPS98226492 1 19980422 A 5220 5079784 FRAME BOEING 727 7271A7C 13840X2 NM EMER EXIT DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C CORROSION LT AFT OVERWING EXIT BOTTOM OF DOOR UNDER PRESSURE SEAL ON FRAME REMOVED AND REPLACED LO WER FORWARD FRAME SECTION IAW SRM 51-30-02, 51-10-1, 53-10-1. 2 L 7 3 4F A3WE 1998050100534 19980501 00534 NM 1998 5 1 UPS98226493 1 19980422 A 5240 651844265 DOOR SEAL BOEING 727 7271A7C 13840X2 NM GALLEY DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C CORROSION ON MID GALLEY DOOR SEAL DEPRESSOR, UPPER FWD AND AFT, VERTICAL SIDE UPPER AND LOWER. REMOVE D AND REPLACED 4 (EA) SEAL DEPRESSORS AT MID GALLEY DOOR CUTOUT STRUCTURE. 2 L 7 3 4F A3WE 1998050100535 19980501 00535 NM 1998 5 1 UPS98226494 1 19980422 A 5311 FRAME BOEING 727 7271A7C 13840X2 NM BS 275 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C CORROSION ON WEB IN FRONT OF DRAG BRACE SHELF BS 275 WL 149-152 RBL 14 TO LBL 14. REMOVED DAMAGED SEC TION AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-03. 2 L 7 3 4F A3WE 1998050100536 19980501 00536 NM 1998 5 1 UPS98226495 1 19980424 A 3411 503FAD11 PITOT BOEING 727 72727C 138400J NM LT FUSELAGE CONTAMINATED A IPXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 909UP 19115 LOST CAPTAINS AIRSPEED INDICATOR ON TAKEOFF ROLL CONTINUED TAKEOFF NOTICED STBY AIRSPEED INDICATOR INOP AT 10,000 FT, WI NDSHEAR/GRD PRX CAME ON THROUGH 500 FT. AFTER TAKEOFF LOST EPR 3, 2, 1 ABOUT 10 SECONDS APART THROUGH 12,000. FOUND NU MEROUS WORMS AND WATER IN CAPT'S PITOT SYS, FLUSHED SYS WITH NITROGEN, ALL DEBRIS REMOVED. PERFORMED PITOT/STATIC TEST PER MM 34-12 -06 . SYS OPS CHK OK. REMOVED AND REPLACED NR 1 ADC PRECAUTIONARY DUE TO WATER IN PITOT LINE P/N ON AND O FF 503FAD1-1, S/N ON 1881 OFF 1702. 2 L 7 3 4F A3WE 1998050100537 19980501 00537 NM 1998 5 1 UPS98526508 1 19980424 A 2612 285N002836 CARD BOEING 757 75724APF 1384969 NM FIRE WARNING MALFUNCTIONED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 426UP 25457 FIRE WARNING LIGHT ILLUMINATED W/NO OTHER AURAL WARNING. UNABLE TO GET LIGHT TO EXTINGUISH. REMOVED AND REPLACED AFLOT S CARD NR 3, NR M10400 IAW MM 26-10-01 PG 401. OPS CHECK OK, S/N OFF DO9521 ON D10064 P/N ON AND OFF 285N0028-36. 2 L 7 2 4F RT A2NM 1998050100538 19980501 00538 WP 1998 5 1 UPS98826484 1 19980414 A 5320 46143971N FITTING DOUG DC8 DC873F 302199F WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C, INBD LONGERON TO BULKHEAD FITTING IS CRACKED F/S 70 L-31R. REMOVED AND REPLACED FITTING IAW SRM 51-1 -21. 2 L 7 4 4F RT 4A25 1998050100539 19980501 00539 WP 1998 5 1 UPS98826485 1 19980326 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 193 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C, RT WING L/E AUX TANK UPPER AFT SKIN ON O/B END IS PULLING THROUGH (INTERNAL CORROSION) XFS 193.00. R EPAIRED IAW DHC SK 803-363. 2 L 7 4 4F RT 4A25 1998050100540 19980501 00540 WP 1998 5 1 UPS98826486 1 19980401 A 5320 38896211 SPLICE DOUG DC8 DC873F 302199F WP BS 1580-1600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:C, SEAT TRACK SPLICE CORRODED BEYOND LIMITS F/S 1580-1600 RBL 48 AFT ACCY COMP. REMOVED, FABRICATED, AN D INSTALLED REPLACEMENT SPLICE IAW SRM 51-3-0 AND DWG 3889621. 2 L 7 4 4F RT 4A25 1998050100541 19980501 00541 WP 1998 5 1 UPS98826487 1 19980330 A 5320 3773159501 FITTING DOUG DC8 DC873F 302199F WP BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, F/S 1480 ABOVE STR 27L - FLOORBEAM SUPPORT FITTING HAS HEAVY CORROSION/CRACKING ON BOTTOM. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050100542 19980501 00542 WP 1998 5 1 UPS98826488 1 19980326 A 5320 56422051 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, LT WING T/E THE LWR REAR SPAR TO AUX SPAR TIE FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DHC SK- 803-491 WITH REF TO UPS EO DC8-5720-10228-E. 2 L 7 4 4F RT 4A25 1998050100543 19980501 00543 WP 1998 5 1 UPS98826489 1 19980402 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, F/S 880 FLOORBEAM NUT PLATE HOLES CORRODED RBL 5 TO RBL 35. REPAIRED IAW DHC SK-803-780. 2 L 7 4 4F RT 4A25 1998050100544 19980501 00544 WP 1998 5 1 UPS98826491 1 19980320 A 5312 5612149108 BULKHEAD FITTING DOUG DC8 DC873F 302199F WP BS 1818 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, F/S 1818 CANTED BULKHEAD FITTING AT LONGERON 1R CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEM ENT FITTING IAW SRM 51-1-21 AND DWG 5612149. 2 L 7 4 4F RT 4A25 1998050100545 19980501 00545 WP 1998 5 1 UPS98826496 1 19980401 A 5720 57698955 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, LT WING IB STUB WING INNER DOUBLER AROUND SLOT PANEL CRACKED BTWN RIBS JUST OB OF SLOT PANEL. REMOVE D, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5769895. REMOVED AND REPLACED FITTING P/N 4640 162- 502 IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998050100546 19980501 00546 WP 1998 5 1 UPS98826497 1 19980402 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 59 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D LT NOSE W/W TUNNEL HAS CORROSION OUT OF LIMITS ON SUB FRAME ATTACH DOUBLER F/S -59 L 22L-23L. REMOVED , FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1- 20D AND 53-3-0. 2 L 7 4 4F RT 4A25 1998050100547 19980501 00547 WP 1998 5 1 UPS98826498 1 19980407 A 5720 975329424 ANGLE DOUG DC8 DC873F 302199F WP WS 252 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, RIB SUPPORT ANGLE CRACKED AT RT STUB WING XFS 252.00. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 D AND 9753294. 2 L 7 4 4F RT 4A25 1998050100548 19980501 00548 WP 1998 5 1 UPS98826499 1 19980401 A 5720 5739859 ANGLE DOUG DC8 DC873F 302199F WP WS 240.126 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D RT I/B STUB WING ATTACH ANGLE XS 240.126 LWR O/B END HAS CRACK IN RADIUS. REMOVED, FABRICATED, AND IN STALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 5739859. 2 L 7 4 4F RT 4A25 1998050100549 19980501 00549 WP 1998 5 1 UPS98826500 1 19980406 A 5320 47731471 FITTING DOUG DC8 DC873F 302199F WP BS 1600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, RT AFT SERVICE DOOR F/S 1600 AT CUSP AREA THE FRAME TO CUSP ATTACH ANGLE IS HEAVILY CORRODED. REMOVE D AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050100550 19980501 00550 WP 1998 5 1 UPS98826501 1 19980402 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 717 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, F/S 717 FLOORBEAM RT SIDE RBL 35 UPPER CAP CORROSION REMOVAL BEYOND LIMITS. REPAIRED IAW DHC SK-803- 786. 2 L 7 4 4F RT 4A25 1998050100551 19980501 00551 WP 1998 5 1 UPS98826502 1 19980401 A 5320 PRESURE WEB DOUG DC8 DC873F 302199F WP BS 52-67 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, RT NOSE W/W TUNNEL PRESSURE WEB HAS HEAVY CORROSION FROM F/S -52 TO -67. REPAIRED IAW DHC SK 803-610 . 2 L 7 4 4F RT 4A25 1998050100552 19980501 00552 WP 1998 5 1 UPS98826503 1 19980416 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 25-35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, FUSELAGE SKIN EXFOLIATED BELOW EXISTING CUTOUT AT LG 27R BETWEEN F/S 25-35. REPAIRED IAW DHC SK-803- 047. 2 L 7 4 4F RT 4A25 1998050100553 19980501 00553 WP 1998 5 1 UPS98826504 1 19980415 A 5320 449950341 FORMER DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D F/S 55 FRAME FORMER CRACKED BETWEEN LONGERON 27-28 RT. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998050100554 19980501 00554 WP 1998 5 1 UPS98826505 1 19980414 A 5313 561386110 LONGERON DOUG DC8 DC873F 302199F WP BS 8-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, CORROSION REMOVAL BEYOND LIMITS LONGERON 31R F/S 8-70. REMOVED, FABRICATED, AND INSTALLED REPLACEMEN T LONGERON IAW SRM 51-1-21 AND DWG 5613861. 2 L 7 4 4F RT 4A25 1998050100555 19980501 00555 WP 1998 5 1 UPS98826506 1 19980413 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 35-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D, F/S 35-55 A/C DOUBLER HAS HEAVY CORROSION UNDER NUTPLATES UNDER O/B FLANGE OF LONGERON 30R. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 51-1-20D AND DWG 5649028. 2 L 7 4 4F RT 4A25 1998050100556 19980501 00556 WP 1998 5 1 UPS98826507 1 19980401 A 5320 PRESURE WEB DOUG DC8 DC873F 302199F WP BS 12 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE:D RT NOSE W/W TUNNEL PRESSURE WEB HAS HEAVY CORROSION AT F/S -12 UNDER STIFFENER RBL 35-46. REPAIRED IA W DHC SK-803-617. 2 L 7 4 4F RT 4A25 1998050100557 19980501 00557 WP 1998 5 1 UPS98826509 1 19980427 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 748UP 45948 EMERG EXIT LIGHTS ILLUMINATED AT ALL TIMES REGARDLESS OF CONTROL POSITION. REMOVED AND REPLACED EMER BATT PACK. OPS CH ECK NORMAL (P/N ON 5708458-503 S/N FTL 010 ), (P/N OFF 60-1223-5 S/N 337). 2 L 7 4 4F RT 4A25 1998050100558 19980501 00558 EU 1998 5 1 QXEA9800541 1 19980225 A 2510 BOLTS FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - THE COCKPIT CENTER PEDESTAL HAS OBVIOUS CORROSION AT TWO MOUNT BOLTS AT THE AFT END OF THE CO-PILOTS LEFT FOOT RES T. REPAIRED IAW HORIZON AIR EA 4-53-377. 2 L 7 2 4F RT A20EU 1998050100559 19980501 00559 EU 1998 5 1 QXEA9800542 1 19980227 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - THERE IS A CRACK IN CASTELLATION AT FRAME 13815B AND BETWEEN STRINGERS 3 AND 2. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998050100560 19980501 00560 EU 1998 5 1 QXEA9800543 1 19980227 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CRACK IN CASTELLATION AT FRAME 13815B AND BETWEEN STRINGERS 72 AND 73. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 . 2 L 7 2 4F RT A20EU 1998050100561 19980501 00561 EU 1998 5 1 QXEA9800544 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - POSSIBLE CRACKED CLIP AFT OF FRAME 12405 AT STRINGER 20. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2. ET CHED ALODINED AND PRIMED, INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998050100562 19980501 00562 EU 1998 5 1 QXEA9800545 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CRACK ON STRINGER 32 AFT OF FRAME 12405. FABRICATED REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED IAW FOKKER SRM 53-02-06, FIGURE 6 AND FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998050100563 19980501 00563 EU 1998 5 1 QXEA9800546 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CRACK ON STRINGER 34 AFT OF FRAME 12405. FABRICATED, REPAIR ETCHED, ALDOINED, PRIMED AND INSTALLED REPAIR IAW FOK KER SRM 51-31-01 AND FOKKER SRM 53-02-06, FIGURE 6. 2 L 7 2 4F RT A20EU 1998050100564 19980501 00564 EU 1998 5 1 QXEA9800547 1 19980223 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CRACK ON STRINGER 36 AFT OF FRAME 12405. FABRICATED REPAIR, ETCHED, ALODINED, PRIMED AND INSTALLED REPAIR IAW FOK KER SRM 51-31-01 AND FOKKER SRM 53-02-06, FIGURE 6. 2 L 7 2 4F RT A20EU 1998050100565 19980501 00565 EU 1998 5 1 QXEA9800548 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - POSSIBLE CRACKED CLIP ON AFT SIDE OF FRAME 12405 AT STRINGER 37. FABRICATED REPAIR IAW FOKKER SRM 53-02-13 FIGURE 2. ETCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998050100566 19980501 00566 EU 1998 5 1 QXEA9800549 1 19980223 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - CLIP IS CRACKED ON AFT SIDE OF FRAME 12405 AT STRINGER 43. FABRICATED REPAIR IAW FOKKER SRM 53-02-13, FIGURE 2. E TCHED, ALODINED AND PRIMED. INSTALLED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998050100567 19980501 00567 EU 1998 5 1 QXEA9800550 1 19980316 A 5302 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - THERE IS A CRACKED FRAME CASTELLATION AT FRAME 6305 AND STRINGER 32. REPAIRED CRACK IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998050100568 19980501 00568 EU 1998 5 1 QXEA9800551 1 19980409 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 PDX - FORWARD GALLEY EMERGENCY EXIT LIGHTS DO NOT OPERATE. INSERTED WIRE PIN INTO MATRIX BLOCK. 2 L 7 2 4F RT A20EU 1998050100569 19980501 00569 EU 1998 5 1 QXEA9800552 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FLANGE CRACKED COMPLETELY AROUND RIVET, FRAME 17565 AT STRINGER 57. FABRICATED DOUBLER, ALODINED, PRIMED AND ATTA CHED RIVETS IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1998050100570 19980501 00570 EU 1998 5 1 QXEA9800553 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME 17565 HAS CRACK IN PREVIOUS REPAIR THAT IS OUT OF LIMITS JUST BELOW STRINGER 23. REMOVED OLD REPAIR. FABRI CATED NEW DOUBLER. REMOVED DAMAGED MATERIAL AND INSTALLED NEW DOUBLER IAW FOKKER SRM 51-10-00, 51-10-05, 51-31-01 AND 5 3-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1998050100571 19980501 00571 EU 1998 5 1 QXEA9800554 1 19980227 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - OBLIQUE FRAME 61-2 HAS CRACK IN REPAIR CLIP AT STIRNGER 43. REMOVED DAMAGED CLIP AND INSTALLED NEW CLIP IAW FOKKE R SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998050100572 19980501 00572 EU 1998 5 1 QXEA9800555 1 19980227 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - OBLIQUE FRAME 16-2 HAS 0.7 CRACK IN REPAIR CLIP AT STRINGER 32. INSTALLED REPAIR CLIP IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998050100573 19980501 00573 EU 1998 5 1 QXEA9800556 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME 32-2 HAS CRACK RUNNING THROUGH STOP DRILL AT STRINGER 68, FORWARD SIDE OF FRAME. FABRICATED DOUBLER, ALODIN ED, PRIMED AND ATTACHED DOUBLER WITH MS20426AD RIVETS WET IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1998050100574 19980501 00574 EU 1998 5 1 QXEA9800557 1 19980227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FRAME 32-2 HAS CRACK AT STRINGER 48. FABRICATED FRAME CLIP AND ATTACHED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998050100575 19980501 00575 EU 1998 5 1 QXEA9800558 1 19980319 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - REPAIR MISSING FRAME CLIP 41-2 ABOVE STRINGER 44. REPAIRED MISSING FRAME CLIP IAW FOKKER SRM 53-02-13, PAGE 7 FIG URE 5. ATTACHING RIVETS TO SKIN IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998050100576 19980501 00576 EU 1998 5 1 QXEA9800559 1 19980303 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU FUEL TANK CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 PDX - FUEL TANK ACCESS PANEL REBATE 71A, ONE CRACK INDICATION .375 IN LENGTH, AFT OUTBOARD CORNER. REFERENCE ATTACHED H ORIZON AIR EA 4-57-99 FOR AUTHORIZATION TO CONTINUE IN-SERVICE WITH INDICATED CRACK. 2 L 7 2 4F RT A20EU 1998050100577 19980501 00577 NM 1998 5 1 98FDEA00287 1 19980423 A 8011 97907821 STARTER BOEING 727 7272S2F 1384O81 NM NR 3 ENGINE FAILED A FDEA A UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 SO 25 212FE 22934 WHEN TURNING ON NR 3 BLEED ON CLIMB-OUT, NR 3 FIRE LIGHT AND FIRE WARNING CAME ON. TURNING OFF THE BLEED, THE FIRE LIG HT AND HORN WENT OFF. FOUND STARTER CONTROL VALVE STUCK 25 PERCENT OPEN AND STARTER IN TOO MANY PIECES. REPLACED ST ARTER AND CONTROL VALVE PER MAINTENANCE MANUAL 80-10-02. STARTER AND VALVE OPERATIONALLY CHECKED NORMAL. 2 L 7 3 4F A3WE 1998050100578 19980501 00578 WP 1998 5 1 ABXA9800385 1 19980416 A 5712 596953046 RIB DOUG DOUG DC8 DC862 3021970 WP WS 347.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 347.75 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DC8 SRM 51-1-21 AND DRAWING K05056. 2 L 7 4 4F 4A25 1998050100579 19980501 00579 WP 1998 5 1 ABXA9800387 1 19980416 A 5320 3750330523 SPLICE DOUG DOUG DC8 DC862 3021970 WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STRINGER 27R, SPLICE BETWEEN STATION 600 AND STATION 620 IS CRACKED. REPLACED STRINGER SPLICE IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998050100580 19980501 00580 WP 1998 5 1 ABXA9800388 1 19980413 A 5320 37546251 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1180-1200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STATION 1180-1200 STRINGER 36 SPLICE FITTING IS CRACKED. REPAIRED IAW ABX REA D853-22883 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998050100581 19980501 00581 WP 1998 5 1 ABXA9800389 1 19980413 A 5313 S2641455 LONGERON DOUG DOUG DC8 DC862 3021970 WP BS 1190 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LONGERON 36 SEVERELY CORRODED AT F/S 1190. REPAIRED IAW ABX REA D853-22883 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998050100582 19980501 00582 WP 1998 5 1 ABXA9800390 1 19980416 A 5312 5910163113 BLKHD STIFFENER DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 923AX 47165 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD STIFFENER AT LONGERON 30 CORRODED. REPAIRED STIFFENER IAW ABX REA D953-2325 3-MR AND DC9 SRM 53-05. 2 L 7 2 4F A6WE 1998050100583 19980501 00583 WP 1998 5 1 ABXA9800391 1 19980416 A 5311 9912243105 FRAME DOUG DOUG DC9 DC931 3022065 WP FRAME 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND FRAME 965 AND LONGERON 30 CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998050100584 19980501 00584 WP 1998 5 1 ABXA9800392 1 19980416 A 5313 59114277 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND LONGERON 16L CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998050100585 19980501 00585 WP 1998 5 1 ABXA9800393 1 19980416 A 5311 5912285515 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 641 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 944AX 47550 DURING C-CHECK, FOUND THE RIGHT CABIN WINDOW FRAME STATION 641 CRACKED. REPAIRED FRAME IAW DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 1998050100586 19980501 00586 WP 1998 5 1 ABXA9800394 1 19980424 A 5230 5649820 DOOR DOUG DOUG DC8 DC862 3021970 WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 AFT LOWER CARGO DOOR LOWER SIDE HAS 2 CRACKS. REPAIRED PER DC8 SRM 52-4-2 AND 52-2-0. 2 L 7 4 4F 4A25 1998050100587 19980501 00587 WP 1998 5 1 ABXA9800371 1 19980423 A 3260 UP LATCH SWITCH DOUG DC8 DC863F 302198F WP LANDING GEAR OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 814AX 46041 IN CRUISE FLIGHT, LANDING GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED LANDING GEAR. LANDING GEAR DOOR 'NOT LATCHED' LIGHT ILLUMINATED. SLOW FLEW AIRCRAFT AT 220 KNOTS. ADJUSTED LEFT GEAR DOOR UPLATCH IAW DC8 MM 32-31-4. 2 L 7 4 4F 4A25 1998050100588 19980501 00588 WP 1998 5 1 ABXA9800372 1 19980422 A 3260 UP LATCH LIGHT DOUG DC9 DC941 302207N WP NLG ILLUMINATED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 958AX 47760 NOSE GEAR UNSAFE LIGHT ILLUMINATED AFTER UP-LATCH CHECK WITH HANDLE IN THE UP POSITION. RECYCLED GEAR, LIGHT EXTINGUISH ED. INSPECTED UPLOCK PROXIMITY SWITCH AND TARGET. NO DEFECTS NOTED. CYCLED NOSE GEAR 5 TIMES. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998050100589 19980501 00589 NE 1998 5 1 DLM88980860 2 19980421 A 7510 ANTI-ICE DUCT DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE BLOWN A DALA A UNSCHED LANDING X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 907DL 49538 ON TAKEOFF AT 8000FL, RT ENG FLAME OUT FOLLOWED POM. PLACED FUEL CONTROL TO OFF AND LANDED. REPLACED LEFT FRAME ANTI-I CE DUCT RAN ENGINE CKS OK. 2 L 7 2 4F 4 F RT A6WE E9NE 1998050100590 19980501 00590 WP 1998 5 1 DLL19980861 1 19980421 A 3350 BULB 305 LKHEED 1011 10113853 5265020 WP EXTERIOR FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 193H1202 R2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED. 2 L 7 3 4F A23WE 1998050100591 19980501 00591 NM 1998 5 1 DL757980868 1 19980421 A 5330 141N33313 SKIN BOEING 757 757232 1384965 NM BS 400 LIGHTNING STRIKE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 662DN 24991 FUSELAGE/WINDOW BELT SKIN, LT, NR 1 WINDOW, STA 400. REPAIR FOR LIGHTNING STRIKES. THE LT WINDOW BELT SKIN AT STA 400 SUFFERED A LIGHTNING STRIKE ON THE FWD SIDE AND THE AFT SIDE OF THE NR 1 WINDOW CUTOUT. BOTH DAMAGED AREAS WERE CLEANED UP WITH .50 HOLES. ALUMINUM BUSHINGS WERE INSTALLED IN THE HOLES AND AN ALUMINUM DOUBLER WAS INSTALLED AROUND THE WIND OW PER ER/A 364571-14, REV B. 2 L 7 2 4F RT A2NM 1998050100592 19980501 00592 NM 1998 5 1 DLM90980869 1 19980418 A 5342 591214185 ANGLE DOUG MD90 MD9030 3023690 NM BS 937 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 FUSELAGE/ATTACH FITTING, VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE: REPAIR FOR CRACK. THE VERTICAL STABILIZER TO FUS ELAGE ATTACH ANGLE ON THE LT SIDE OF THE AIRCRAFT WAS FOUND WITH A .90 CRACK AT FS 937. THE CRACKED FLANGE WAS TRIMMED OUT AND A .080 THICK A-286 STEEL REPAIR ANGLE WAS INSTALLED PER ER/A 364553-14. 2 L 7 2 4F RT A6WE 1998050100593 19980501 00593 NM 1998 5 1 DL757980870 1 19980422 A 5754 114N4004178A TE WEDGE BOEING 757 757232 1384965 NM NR 8 LE SLAT DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 686DA 27589 WING RT, NR 8 SLAT, TRAILING EDGE WEDGE REPAIRED FOR DENT. THE TRAILING EDGE WEDGE ON THE RT WING NR 8 SLAT WAS FOUND W ITH A 4 BY .875 BY .040 DEEP DENT. THE DAMAGED AREA WAS REPAIRED PER B757 SRM 57-43-02, FIG. 201. BECAUSE THE SLAT WED GES ARE THE SUBJECT OF AD 91-22-51, ER/A 364600-14AD WAS ISSUED TO DOCUMENT THE REPAIR. 2 L 7 2 4F RT A2NM 1998050100594 19980501 00594 NM 1998 5 1 DL72E980871 1 19980422 A 5754 BRACKET BOEING 727 727247 138408F NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON F1 LETTER CHK, NR 1 SLAT ACT IB MOUNT BRACKET CRACKED AT WEB. REPAIR PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998050100595 19980501 00595 NM 1998 5 1 DL72E980874 1 19980422 A 5330 SKIN BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND F1 LETTER CHECK, FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED APPROX .25 IN. REPAIR PER M/M 53-30-03. 2 L 7 3 4F A3WE 1998050100596 19980501 00596 NM 1998 5 1 DL757980876 1 19980423 A 3350 20131A BATTERY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 625DL 22915 F/C EMERGENCY TRACK LIGHTING INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A2NM 1998050100597 19980501 00597 NM 1998 5 1 DL72S980879 1 19980424 A 5754 RIB BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 FOUND ON E2 LETTER CK, 2 CRACKS IN NR 7 SLAT NOSE RIB AT THE OUTBD SIDE OF THE ACTUATOR. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998050100598 19980501 00598 WP 1998 5 1 DLL19980881 1 19980424 A 2612 CONNECTOR LKHEED 1011 10113853 5265020 WP NR 3 ENGINE DIRTY A DALA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 27 753DA 193W1189 DURING CLIMB, NR 3 ENG FIRE WARNING FIRE HANDLE LT, DETECTOR AND BELL CAME ON WITH LOOP -A- SELECTED -B- LOOP INOP. SHU T DOWN ENG, DISCHARGED BOTTLES. CLEANED CONNECTORS ON NR 3 ENG -A- AND -B-. REPLACED BOTTLES, RAN ENG W/BLDS ON AND OF F AT ALL DIFF PWR SETTINGS PER PFHB. ALL INDS NORM. A/C OK FOR SERVICE. 2 L 7 3 4F A23WE 1998050100599 19980501 00599 NE 1998 5 1 DL72S980883 2 19980425 A 7314 37820113 PUMP 37820113 BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING X ENGINE FLAMEOUT TO TAKEOFF 1 SO 27 470DA 64097 SN0468 20747 687410 NR 1 ENG FLAMED OUT AFTER T/O. REPLACED NUMBER ONE FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 1998050100600 19980501 00600 NM 1998 5 1 DL76L980885 1 19980425 A 2120 AIR DISTRIBUYION BOEING 767 767332 1382001 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 190DN 28447 SHORTLY AFTER TAKEOFF, FLT ATTENDENT IN AFT CABIN REPORTED SMELL OF BURNING PLASTIC, ON DESCENT ODOR CHANGED TO OILY SME LL. SMELL ALSO NOTICED IN COCKPIT. CHECKED ALL C/B'S IN COCKPIT AND LOWER E/E. ALL OK, RAN PACKS AND RELATED EQUIPMEN T FOR 4 HOURS. ALL OK. RAN BOTH ENGINES AT HIGH POWER, NO ODORS DETECTED. CHECKED APU INLET AND RAN APU, SYSTEM OK. A /C LATER DISPATCHED ON DOMESTIC FLIGHT, NO TROUBLES NOTED, NO ABNORMAL OIL USEAGE. 2 L 7 2 4F RT A1NM 1998050100601 19980501 00601 NM 1998 5 1 DL76S980886 1 19980425 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 116DL 23275 EMERGENCY EXIT IDENTIFIER LIGHTS AT L-2 AND R-2 INOP. REPLACED POWER SUPPLY, SYSTEM OPS GOOD. 2 L 7 2 4F RT A1NM 1998050100602 19980501 00602 NM 1998 5 1 DL72K980887 1 19980425 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 472DA 12769 20749 FWD OVERWING EXTERNAL EMERG LIGHT INOP LT SIDE. REPLACED BATT PACK M654, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1998050100603 19980501 00603 EU 1998 5 1 RAIA980322 1 19980331 A 3260 9005EN8 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 425AM 870 FLT 7058 - STL - LEFT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTION. MAINTENANCE REPLACED LEFT MA IN LANDING GEAR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A56EU 1998050100604 19980501 00604 1998 5 1 RAIA980320 4 19980331 A 3442 7008470822 RT UNIT JETAIR JETSTM JETSTM4101 1500501 EU RADOME FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 564HK 3878 41081 FLT 7460 - STL - WEATHER RADAR FAILED IN FLIGHT. MAINTENANCE REPLACED WEATHER RADAR RECEIVER TRANSMITTER. (M) 2 L 7 2 4T RT A41NM 1998050100605 19980501 00605 EU 1998 5 1 RAIA980321 1 19980331 A 2612 23VU DIODE AEROSP ATR42 ATR42300 8680920 EU FIRE PANEL FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 426TE 228 FLT 7136 - STL - BOTH BOOST PUMP INDICATORS SHOWING OPEN AND CLOSED, LEFT ENGINE FIRE DETECTION A/B LOOPS FAULTED. MAIN TENANCE INSPECTED AND REPLACED PANEL 23VU DUE TO DIODE FAILURE. (M) 2 H 7 2 4T RT A53EU 1998050100606 19980501 00606 NM 1998 5 1 TSAA9833182 1 19980318 A 3350 20131A BATTERY BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 ON SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998050100607 19980501 00607 NM 1998 5 1 TSAA9832183 1 19980319 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998050100608 19980501 00608 NM 1998 5 1 TSAA9833184 1 19980319 A 3350 6013211 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 ON SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998050100609 19980501 00609 NM 1998 5 1 TSAA9833174 1 19980313 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998050100610 19980501 00610 NM 1998 5 1 TSAA9833175 1 19980314 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHTING BATTERY LOW. REPLACED BATTERY PACK. OPS CHECK GOOD. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998050100611 19980501 00611 EU 1998 5 1 AALA980589 1 19980324 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU FRAME 21-26 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND TWO AREAS OF CORROSION AND MECHANICAL DAMAGE ON NR 10 TRACK. INSTALLED TRACK NR 10 BETWEEN FRAMES 21-26 PER SRM 51-72-10-0, ALODINED, PRIMED AND PAINTED TRACK PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998050100612 19980501 00612 NM 1998 5 1 AALA98422 1 19980302 A 5347 TRACK DOUG MD11 MD11 3023602 NM BS 457 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1766A 48597 TUL - FOUND CORROSION TO TRACK NR 1 AT STATION 457 AT THE LAV TIEDOWN, BEYOND LIMITS. REMOVED AND REPLACED NR 1 TRACK F ROM PRODUCTION SPLICE TO L1 DOOR STATION 410, PER SRM AARD 51-10-00-1 PAGE 1. (M) 2 L 7 3 4F RT A22WE 1998050100613 19980501 00613 WP 1998 5 1 AALA980545 1 19980319 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 228AA 49178 TUL - FOUND CORROSION IN L29L, STATION 370 TO 427. INSTALLED STRAP DOUBLER PER ESO 80559. (M) 2 L 7 2 4F A6WE 1998050100614 19980501 00614 EU 1998 5 1 AALA980572 1 19980321 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 60-61 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRINGER 52L HAS CORROSION BETWEEN FRAME 60 AND FRAME 61 AFT CARGO. REPAIRED STRINGER 52L PER SRM 53-10-14. REMOVED CORROSION PER SRM 51-74-10-2. (M) 2 L 7 2 4F RT A35EU 1998050100615 19980501 00615 EU 1998 5 1 AALA980573 1 19980321 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 54 57-58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - STRINGERS 54L AND 55L HAVE CORROSION AFT CARGO BETWEEN FRAME 57.3 AND 58. REMOVED CORROSION PER SRM 51-74-10-2. R EPAIRED PER ESO 30595 DATED 3-18-98 AND SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100616 19980501 00616 EU 1998 5 1 AALA980574 1 19980321 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FLOORBEAM IN AFT CARGO AT FRAME 56 HAS CORROSION BELOW ROLLER TRAY NR 6. REMOVED CORROSION PER SRM 51-74-10-2. R EPAIRED PER ESO 30595 STEP A DATED 3-19-98. (M) 2 L 7 2 4F RT A35EU 1998050100617 19980501 00617 EU 1998 5 1 AALA980575 1 19980321 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 64-65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRINGER 54R BETWEEN FRAMES 64 AND 65 HAS CORROSION. REMOVED CORROSION PER SRM 51-74-10-2. REPAIRED PER ES O 30595, DATED 3-18-98. (M) 2 L 7 2 4F RT A35EU 1998050100618 19980501 00618 NM 1998 5 1 AALA980661 1 19980401 A 5240 SKIN BOEING 727 727223 1384074 NM FUSELAGE MISREPAIRED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 878AA 21390 TUL - LARGE ROUT OUT AREA OF FWD GALLEY DOOR EXIT SKIN AT UPPER HINGE ARM CUTOUT AT UPPER AFT CORNER. REPAIRED AREA WIT H DOUBLER PER SRM 52-00-3. (M) 2 L 7 3 4F A3WE 1998050100619 19980501 00619 NM 1998 5 1 AALA980674 1 19980401 A 5330 SKIN BOEING 727 727223 1384074 NM BS 385 MISINSTALLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 878AA 21390 TUL - P/A REPAIR NOT PROPERLY INSTALLED, NO RADIUS IN FILLER. NO E/D ON FILLER AND NUMEROUS FASTENERS HEADS ARE TO HIGH AND PIECE OF WOOD JAMMED UNDER EDGE OF DOUBLER. REMOVED PREVIOUS REPAIR AND INSTALLED NEW DOUBLER PER SRM 53-30-3. (M ) 2 L 7 3 4F A3WE 1998050100620 19980501 00620 NM 1998 5 1 AALA984058 1 19980330 A 5743 TRUNNION BOEING 767 767223 1385123 NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 323AA 22324 AFW - FOUND SMALL AREA OF CORROSION IN THE LT MLG SUPPORT BEAM AFT TRUNNION BEARING BORE. REMOVED PITTING AND GOUGING B Y BLENDING THE AREA. (M) 2 L 7 2 4F RT A1NM 1998050100621 19980501 00621 NM 1998 5 1 AALA984059 1 19980327 A 5330 SKIN BOEING 767 767223 1385123 NM BS 440 LIGHTNING STRIKE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 320AA 22321 AFW - FOUND AND BLENDED OUT AN ARE OF LIGHTNING STRIKE DAMAGE ON THE EXTERNAL FUSELAGE SKIN. THE BLENDOUT EXCEEDS SRM L IMITS. NDT CHECKED BLENDED AREA. NO CRACKS INDICATED. REFINISHED PER SRM. APPROVED FOR CONTINUED SERVICE BY ENGINEER ING PER MRB 767-1589. (M) 2 L 7 2 4F RT A1NM 1998050100622 19980501 00622 NM 1998 5 1 AALA980662 1 19980401 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1213 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND STATION 1213 CHORD BELOW LOWER FIXED STEP, CENTER SECTION CORRODED ON END AT RBL 15 AND LBL 15 UNDER SPLICES . REPAIRED PER ESO 11697, DATED 3/10/97. (M) 2 L 7 3 4F A3WE 1998050100623 19980501 00623 NM 1998 5 1 AALA980666 1 19980401 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1213 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CHORD ANGLE CRACKED STATION 1213 BELOW 4TH FIXED STEP, RBL 16. REMOVED AND REPLACED CHORD ANGLE. (M) 2 L 7 3 4F A3WE 1998050100624 19980501 00624 NM 1998 5 1 AALA980620 1 19980326 A 5230 WEB BOEING 727 727227 1384078 NM BS 560 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FORWARD CARGO DOOR WEB CRACKED 4 PLACED UNDER THE SEAL RETAINER. CUT OUT DAMAGED SECTION OF WEB AND REPAIRED PER SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 1998050100625 19980501 00625 NM 1998 5 1 AALA980663 1 19980401 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1213 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND STATION 1213 CHORD BELOW LOWER FIXED STEP CORRODED ON RT SECTION UNDER SPLICE AT RBL 18-22. REPAIRED PER ES O 11697, DATED 3/10/98. (M) 2 L 7 3 4F A3WE 1998050100626 19980501 00626 NM 1998 5 1 AALA980665 1 19980401 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1213 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND STATION 1213 LOWER CHORD BELOW LOWER FIXED STEP CORRODED ON LEFT SIDE UNDER SPLICE LBL 18-22. REMOVED AND R EPLACED LEFT CHORD ANGLE. (M) 2 L 7 3 4F A3WE 1998050100627 19980501 00627 NM 1998 5 1 AALA984062 1 19980327 A 5320 SILL BOEING 767 767223 1385123 NM BS 542 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 320AA 22321 AFW - FOUND AND BLENDED CORROSION ON THE OUER CHORD OF THE FWD CARGO DOOR LOWER SILL. THE BLENDOUT IS ON THE UPPER SURF ACE OF THE OUTBOARD LOWER FLANGE OF THE CHORD. THE BLEND OUT EXCEEDS SRM LIMITS. REFINISHED THE BLENDOUT PER SRM. APP ROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1587. (M) 2 L 7 2 4F RT A1NM 1998050100628 19980501 00628 EU 1998 5 1 AALA980497 1 19980313 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FLOORBOARD SUPPORT AT FRAME 60 BETWEEN ROLLER TRAYS 2 AND 3 HAS CORROSION AROUND FASTENER HOLES TOP AND BOTTOM. R EMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-10-0, SPLICED PER SRM 53-10-15-2. (M) 2 L 7 2 4F RT A35EU 1998050100629 19980501 00629 EU 1998 5 1 AALA980517 1 19980316 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FRAME 64-65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER SPLICE AT STRINGER 51L, 53L 54L AND 55L BETWEEN FRAME 64 AND 65. REMOVED AND REPLACED STRINGER SPLICED AT 51L, 53L, 54L, AND 55L PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100630 19980501 00630 EU 1998 5 1 AALA980518 1 19980317 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 54-54.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 53L BETWEEN FRAME 54 AND 54.2. INSTALLED STRINGER SPLICE AT 53L AND INSTALLED NEW STR INGER 53L BETWEEN FRAME 54 AND FRAME 54.2 IAW SRM 53-10-14.2. (M) 2 L 7 2 4F RT A35EU 1998050100631 19980501 00631 EU 1998 5 1 AALA980519 1 19980317 A 5347 TIE DOWN AIRBUS 300 A300B4605R 3930308 EU FRAME 68-69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CARGO FLOOR, THIRD TIE DOWN FROM DOOR FLOOR BRACKET HAS CORROSION. SPLICED IN REPAIR PER SRM 53-10-15-2. ( M) 2 L 7 2 4F RT A35EU 1998050100632 19980501 00632 EU 1998 5 1 AALA980520 1 19980317 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 71 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 54L AT FRAME 71. INSTALLED NEW SECTION OF STRINGER PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100633 19980501 00633 EU 1998 5 1 AALA980522 1 19980318 A 7120 MOUNT AIRBUS 300 A300B4605R 3930308 EU RT ENGINE DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND LIGHT DAMAGE ON RT ENGINE PYLON FORWARD ATTACH FITTING LOWER FWD RT SIDE. BLENDED PER ESO 30595, DATED 3-16 -98 AND FLAPPER PEENED WORK AREA PER SRM 51-29-00 (AA SPECIFICATION PAGE 16-19) PRIMED AND PAINTED. (M) 2 L 7 2 4F RT A35EU 1998050100634 19980501 00634 EU 1998 5 1 AALA980507 1 19980316 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - RIGHT PICKUP ANGLE CRACKED. REPAIRED PICKUP ANGLE PER ESO 30595, DATED 3-11-98. (M) 2 L 7 2 4F RT A35EU 1998050100635 19980501 00635 EU 1998 5 1 AALA980508 1 19980316 A 5720 BRACKET AIRBUS 300 A300B4605R 3930308 EU LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - KRUEGER FLAP BRACKET EXFOLIATED AT LOWR OUTBOARD MOUNT BORE, OUTBOARD MOUNT PAD AND FLAP TO ARM ATTACH POINT. INS TALLED NEW MOUNT PER MM 27-87-11, OPS CHECK OK. (M) 2 L 7 2 4F RT A35EU 1998050100636 19980501 00636 EU 1998 5 1 AALA980509 1 19980316 A 2550 TRAY AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CENTER CARGO NR 6 ROLLER TRAY HAS CORROSION DAMAGE. REMOVED AND REPLACED SECTION OF ROLLER TRAY PER SRM 51- 72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100637 19980501 00637 EU 1998 5 1 AALA980510 1 19980314 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 4044 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND GOUGE IN AIRCRAFT, CROWN SKIN STATION 4044 BETWEEN STRINGER 5 AND 6 LEFT SIDE. REPAIRED DAMAGED SKIN PER SR M 53-10-12 FIG 203, INSTALLED DOUBLER. (M) 2 L 7 2 4F RT A35EU 1998050100638 19980501 00638 EU 1998 5 1 AALA980511 1 19980314 A 5230 DOOR AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND NUT PLATE HOLES CORRODED AROUND FORWARD LOWER CORNER OF FORWARD CARGO DORO, DOOR INNER STRUCTURE. REMOVED A ND REPLACED DOUBLER PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998050100639 19980501 00639 EU 1998 5 1 AALA980512 1 19980316 A 5230 DOOR AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND NUT PLATE HOLES CORRODED AROUND FWD LOWER CORNER OF FORWARD CARGO DOOR, DOOR INNER STRUCTURE. REMOVED AND R EPLACED DOUBLER PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998050100640 19980501 00640 EU 1998 5 1 AALA980503 1 19980313 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON FLOORBEAM SUPPORT AT FRAME 60 FROM ROLLER TRAY NR 4 TO THE CARGO DOOR SILL. REMOVED AND REPLAC ED FLOOR CROSSBEAM PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100641 19980501 00641 EU 1998 5 1 AALA980499 1 19980313 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND FLOOR SUPPORT AROUND FRAME 60 BETWEEN NR 1 AND NR 2 ROLLER TRAYS HAS CORROSION. REMOVED AND REPLACED CROSSB EAM PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100642 19980501 00642 NM 1998 5 1 AALA984049 1 19980316 A 5730 SKIN BOEING 767 767223 1385123 NM WS 234 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 317AA 22319 AFW - FOUND CORROSION ON LEFT WING UPPER SKIN PANEL LANDING. BLENDED OUT CORROSION, ALODINED AND PRIMED AREA PER MM INS TRUCTIONS. (M) 2 L 7 2 4F RT A1NM 1998050100643 19980501 00643 EU 1998 5 1 AALA980571 1 19980321 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON FLOORBEAM IN AFT CARGO AT FRAME 58 BELOW NR 6 ROLLER TRAY. REPAIRED PER ESO 30595 DATED 3-18-9 8, AFTER CORROSION REMOVED PER SRM 51-74-10-2. (M) 2 L 7 2 4F RT A35EU 1998050100644 19980501 00644 EU 1998 5 1 AALA980570 1 19980321 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 64 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND FLOORBEAM IN BULK CARGO HAS CORROSION AT FRAME 64 RT SIDE WALL TO NR 5 ROLLER TRAY. REPAIRED PER ESO 30595, DATED 3-18-98, AFTER CORROSION REMOVED PER SRM 51-74-10-2. (M) 2 L 7 2 4F RT A35EU 1998050100645 19980501 00645 EU 1998 5 1 AALA980569 1 19980320 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 58-64 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 54L FROM FRAME 58 TO 64. REMOVED AND REPLACED STRINGER 54L FROM FRAME 58 TO FRAME 64 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100646 19980501 00646 EU 1998 5 1 AALA980568 1 19980320 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 57 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON INBOARD FLANGE OF STRINGER 56R BETWEEN FRAME 57.2 AND 57.3. INSTALLED DOUBLER ON STRINGER PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998050100647 19980501 00647 EU 1998 5 1 AALA980566 1 19980320 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU FRAME 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER SPLICE ON STRINGER 55L AT FRAME 65. REMOVED AND REPLACED STRINGER SPLICE ON STRINGER 55L AT FRAME 65 PER SRM 51-72-00-10. (M) 2 L 7 2 4F RT A35EU 1998050100648 19980501 00648 EU 1998 5 1 AALA980534 1 19980318 A 5320 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON SHEAR TIE AT FRAME 58 BETWEEN STRINGER 52R AND 53R. REMOVED AND REPLACED SHEAR TIE PER SRM 51- 72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100649 19980501 00649 EU 1998 5 1 AALA980535 1 19980318 A 5320 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON SHEAR TIE AT FRAME 58 BETWEEN STRINGER 54R AND 55R. REMOVED AND REPLACED SHEAR TIE PER SRM 51- 72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100650 19980501 00650 EU 1998 5 1 AALA980536 1 19980318 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 57.3-58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 49L BETWEEN FRAME 57.3 AND 58. REMOVED SECTION OF STRINGER AND REPAIRED WITH SPLICE I AW SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998050100651 19980501 00651 EU 1998 5 1 AALA980537 1 19980318 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 58-59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRINGER 49L HAS CORROSION LOWER FLANGE AT FASTENERS BETWEEN FRAMES 58 AND 59. REMOVED SECTION OF STRINGER AND REPAIRED WITH SPLICE IAW SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998050100652 19980501 00652 EU 1998 5 1 AALA980538 1 19980318 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU FRAME 61 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON FLOORBEAM END FITTING RT SIDE AT FRAME 61. REMOVED AND REPLACED FLOORBEAM END FITTING PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100653 19980501 00653 EU 1998 5 1 AALA980579 1 19980321 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 54.1 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORRODED LONGERON AROUND FRAME 54.1. REMOVED CORRODED SECTION OF LONGERON, SPLICED IN NEW PIECE PER SRM 53- 10-14. (M) 2 L 7 2 4F RT A35EU 1998050100654 19980501 00654 EU 1998 5 1 AALA980578 1 19980321 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 54 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 56L BETWEEN FRAME 54 AND 54.1. REMOVED CORRODED MATERIAL PER 51-74-10-2 AND INSTALLED DOUBLER PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998050100655 19980501 00655 EU 1998 5 1 AALA980577 1 19980321 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 58-59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND LONGERON 56R BETWEEN FRAMES 58 AND 59 HAS CORROSION ON THE LOWER SIDE. REMOVED CORRODED LONGERON SECTION AN D INSTALLED NEW PIECE PER SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998050100656 19980501 00656 EU 1998 5 1 AALA980594 1 19980323 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND STRINGER 55R HAS SURFACE CORROSION ON SHEAR TIE AND STRINGER. INSTALLED NEW STRINGER SECTION PER SRM 53-10- 1A PAGE 210. (M) 2 L 7 2 4F RT A35EU 1998050100657 19980501 00657 EU 1998 5 1 AALA980593 1 19980323 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 70-71 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 57 BETWEEN FRAME 70 AND 71. INSTALLED DOUBLER ON STRINGER PER SRM 53-10-14 AFTER CORR OSION WAS REMOVED. (M) 2 L 7 2 4F RT A35EU 1998050100658 19980501 00658 EU 1998 5 1 AALA980592 1 19980323 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 54.54.1 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 53R BETWEEN FRAME 54 AND 54.1. CUT OUT SECTION OF STRINGER 53R AND SPLICED IN NEW SEC TION PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998050100659 19980501 00659 EU 1998 5 1 AALA980591 1 19980323 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 72-73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 56L. INSTALLED DOUBLER REPAIR PER SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998050100660 19980501 00660 EU 1998 5 1 AALA980590 1 19980323 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 57 BETWEEN FRAME 54 AND 54.1. INSTALLED STRINGER SPLICE AND DOUBLERS PER SRM 53-10-14 . (M) 2 L 7 2 4F RT A35EU 1998050100661 19980501 00661 EU 1998 5 1 AALA980595 1 19980323 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 71/72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION AROUND LOWER ANGLE OF STRINGER 56L BETWEEN FRAME 71 AND 72. INSTALLED DOUBLER REPAIR PER SRM 53-1 0-14-2. (M) 2 L 7 2 4F RT A35EU 1998050100662 19980501 00662 EU 1998 5 1 AALA980521 1 19980318 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORRODED FLOORBOARD SUPPORT IN CABIN. REMOVED AND REPLACED FLOORBOARD SUPPORT FROM FRAME 71 TO 73 PER SRM 5 1-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050100663 19980501 00663 EU 1998 5 1 AALA980498 1 19980313 A 5320 41A5451534501 SHIM AIRBUS 300 A300B4605R 3930308 EU FAIRING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 59081 639 TUL - FAIRING SHIM CORRODED. REPLACED SHIM PER SRM REF 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998050100664 19980501 00664 WP 1998 5 1 AALA980582 1 19980320 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 168 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70425 49337 TUL - CUSP FRAME AT STATION 168 HAS CORROSION, JUST FORWARD OF FORWARD SERVICE DOOR AT CABIN FLOOR LEVEL. REMOVED CORRO SION PER SRM 53-10-3. INSTALLED DOUBLER AFTER TREATING AND PRIMING PER SRM 53-20-00-14. (M) 2 L 7 2 4F A6WE 1998050100665 19980501 00665 WP 1998 5 1 AALA980583 1 19980323 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1304 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70425 49337 TUL - FOUND CORROSION IN NR 2 SEAT TRACK AT STATION 1304. CORROSION REMOVAL WENT BEYOND LIMITS. REPLACED SEAT TRACK NR 2 FROM STATION 1260 TO 1309 AND SPLICE PER SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 1998050100666 19980501 00666 WP 1998 5 1 AALA980584 1 19980319 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 228AA 49178 TUL - FOUND L30 HAS CORROSION STATION 370 TO 427. INSTALLED DOUBLER STRAP PER ESO 80559, DATED 3/19/98. (M) 2 L 7 2 4F A6WE 1998050100667 19980501 00667 EU 1998 5 1 AALA980599 1 19980325 A 5320 CROSS FRAME AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - FOUND CORROSION ON CABIN CROSS FRAME. INSTALLED DOUBLER ANGLE PER ESO 30595 DATED 3-20-98. (M) 2 L 7 2 4F RT A35EU 1998050100668 19980501 00668 SO 1998 5 1 C2XA98IA088 1 19980329 A 5320 12017066037 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 25 NR 5 UPPER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REM OVED AND REPLACED THE AFFECTED SUPPORT IAW THE EMB SRM 51-70-00 AND 51-25-02. (M) 2 L 7 2 4T RT A31SO 1998050100669 19980501 00669 SO 1998 5 1 C2XA98IA089 1 19980329 A 5311 12005020003 FRAME EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, FRAME 43 WAS FOUND TO BE CORRODED. THE AFFECTED FRAME SECTION WAS REMOVED AND THE FRAM E REPAIRED UTILIZING A SPLICE IAW THE EMB SRM 53-00-04. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100670 19980501 00670 SO 1998 5 1 C2XA98IA090 1 19980329 A 5315 12004170004 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, FRAME 38 FLOORBEAM WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED F LOORBEAM IAW THE EMB SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100671 19980501 00671 SO 1998 5 1 C2XA98IA091 1 19980329 A 5320 12002591002 ANGLE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM ATTACH ANGLE AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED ANGLE IAW THE EMB SRM 51-21-42, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100672 19980501 00672 SO 1998 5 1 C2XA98IA092 1 19980329 A 5315 12006451001 FLOORBEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE FLOORBEAM USING A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5310-01032. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100673 19980501 00673 SO 1998 5 1 C2XA98IA093 1 19980329 A 5320 12006914001 ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, FRAME 13 FLOOR SUPPORT ANGLES WERE FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLES IN ACCORDANCE WITH THE EMB SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100674 19980501 00674 SO 1998 5 1 C2XA98IA094 1 19980329 A 5313 12017417006 STRINGER EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, STRINGER 21L WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE AFFECTED PORTION OF STR INGER AND PERFORMED A SPLICE REPAIR IAW EMB SRM 51-10-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100675 19980501 00675 SO 1998 5 1 C2XA98IA095 1 19980329 A 5713 12016079002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER NR 8 WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE A FFECTED PORTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100676 19980501 00676 SO 1998 5 1 C2XA98IA096 1 19980329 A 5720 12016037013 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING RIB 7 NR 3 LOWER SKIN SUPPORT WAS FOUND CRACKED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED SKIN SUPPORT IAW EMB SRM 51-40-02. THE AIRCRAFT WAS THE APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100677 19980501 00677 SO 1998 5 1 C2XA98IA097 1 19980329 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACE D THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100678 19980501 00678 SO 1998 5 1 C2XA98IA098 1 19980329 A 5347 12026865009 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100679 19980501 00679 SO 1998 5 1 C2XA98IA099 1 19980329 A 5713 12016086001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER NR 10 WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE A FFECTED PORTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050100680 19980501 00680 SO 1998 5 1 C2XA98IA100 1 19980329 A 5730 12015668001 SKIN EMB 120 EMB120RT SO LEFT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT WING INBOARD FORWARD SKIN WAS FOUND TO BE CRACKED. MAINTENANCE REPAIRED THE A FFECTED SKIN PANEL WITH A DOUBLER REPAIR IAW THE EMB SRM 57-20-01. (M) 2 L 7 2 4T RT A31SO 1998050100681 19980501 00681 SO 1998 5 1 C2XA98IA101 1 19980329 A 5730 12015668002 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING INBOARD FORWARD SKIN PANEL WAS FOUND CRACKED. MAINTENANCE REPAIRED THE SKIN PANEL USING A DOUBLER REPAIR IAW THE EMB SRM 57-20-01. (M) 2 L 7 2 4T RT A31SO 1998050100682 19980501 00682 CE 1998 5 1 C2XA98CL035 1 19980405 A 2612 101910523 BRACKET BEECH 1900 1900D 1154162 CE LT ENGINE BROKEN A C2XA E F D ENGINE SHUTDOWN ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 09 69548 UE193 CLE - FLT 3041 - CREW REPORTED THAT DURING TAXI THE LEFT ENGINE FIRE DETECTOR ACTIVATED, CREW PERFORMED QRH ITEMS. AIRC RAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ENGINE AND FOUND THE FORWARD FIRE LOOP ATTACHMENT BRACKET BROKEN ALLOWING LOOP TO CONTACT EXHAUST STACK, NO INDICATION OF FIRE WAS EVIDENT. MAINTENANCE REMOVED AND REPL ACED THE LEFT ENGINE FORWARD FIRE LOOP EXHAUST ATTACHMENT BRACKET IAW B1900D SRM 51-40-10, AIRCRAFT RELEASED FOR SERVICE . (M) 2 L 7 2 4T RT A24CE 1998050100683 19980501 00683 EU 1998 5 1 C2XA98IA108 1 19980404 A 5315 S53672215202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE FLOORBEAM IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100684 19980501 00684 EU 1998 5 1 C2XA98IA107 1 19980404 A 5347 S53678001222 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 36 TO FRAME 40. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK IAW ATR42 SRM 51-25-02 AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100685 19980501 00685 EU 1998 5 1 C2XA98IA106 1 19980404 A 5320 S53672408216 ANGLE AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE THRESHOLD ATTACH ANGLE AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED ANGLE IAW ATR42 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100686 19980501 00686 EU 1998 5 1 C2XA98IA105 1 19980404 A 5347 S536780012000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE RT OUTBOARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 36. MAINTEN ANCE REMOVED AND REPLACED THE AFFECTED SECTION OF SEAT TRACK IAW ATR24 SRM 51-25-02 AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100687 19980501 00687 EU 1998 5 1 C2XA98IA104 1 19980404 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 38 WAS FOUND TO BE CORRODED ON THE RIGHT SIDE. MAINTENANCE REPA IRED THE AFFECTED PORTION OF FLOORBEAM USING A SPLICE REPAIR IAW ATR42 SRM 53-61-40, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100688 19980501 00688 EU 1998 5 1 C2XA98IA103 1 19980404 A 5315 S53172218200 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16824 166 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM UNDER PANEL 211JF WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED FLOORBEAM IAW ATR 42 SRM 51-25-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100689 19980501 00689 EU 1998 5 1 WTAA980057 1 19980331 A 7921 INTAKE BAG JETSTM JETSTM3101 1500215 EU RT ENGINE BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 402UE 734 LAX - BIRD STRIKE TO RIGHT ENGINE OIL COOLER INTAKE REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998050100690 19980501 00690 EU 1998 5 1 WTAA980056 1 19980328 A 3260 1373015SK401 SWITCH BAG JETSTM JETSTM3101 1500215 EU COCKPIT DIRTY A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 402UE 734 SFO - CAP PANEL GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND ALL INDICATION LIGHTS EXTINGUISHED. AIRCRAFT RETURNED TO STATION AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE UNABLE TO DUPLICATE REPORTED DISCREPANCY. AS PREC AUTION CLEANED THROTTLE SYNCHRO MICROSWITCHES. SYSTEM OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A21EU 1998050100691 19980501 00691 EU 1998 5 1 WTAA980061 1 19980401 A 6120 10147 OVERSPEED SWITCH BAG JETSTM JETSTM3101 1500215 EU COCKPIT FAILED A WTAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 426UE 774 FAT - ON CLIMB-OUT AT 140 KNOTS OVERSPEED HORN SOUNDED. AIRCRAFT RETURNED TO STATION. MAINTENANCE REPLACED OVERSPEED S WITCH. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998050100692 19980501 00692 EU 1998 5 1 WTAA980058 1 19980331 A 3350 311701 BATTERY PACK BAG JETSTM JETSTM3101 1500215 EU CABIN DISCHARGED A WTAA K NONE O OTHER IN INSP/MAINT 1 WP 17 403UE 743 FAT - EMERGENCY LIGHT AT ESCAPE HATCH SIGN INOPERATIONAL. MAINTENANCE REPLACED BATTERY PACK FOR EMERGENCY EXIT SIGN. O PERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998050100693 19980501 00693 EU 1998 5 1 WTAA980059 1 19980331 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA O OTHER N FALSE WARNING CR CRUISE 1 WP 17 423UE 799 FAT - 3 GREEN DOWN AND LOCK INDICATION AND RIGHT INTRANSIT LIGHT REPORTED ILLUMINATED AT THE SAME TIME. MAINTENANCE REP LACED RIGHT MAN GEAR DOWNLOCK MICROSWITCH. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998050100694 19980501 00694 EU 1998 5 1 WTAA980060 1 19980331 A 3040 XW20173M1 WIPER MOTOR BAG JETSTM JETSTM3101 1500215 EU COCKPIT FAILED A WTAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 425UE 798 LAX - LEFT WIPER MOTOR INOPERATIONAL. AIRCRAFT RETURNED TO STATION. MAINTENANCE REPLACED LEFT WIPER MOTOR. OPERATIONA L CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998050100695 19980501 00695 1998 5 1 WTAA980055 4 19980328 A 3418 C818061 COMPUTER EMB 120 EMB120ER 3260203 SO E/E COMPT MALFUNCTIONED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 301YV 120301 RDD - STALL WARNING ON LEFT SIDE ILLUMINATED ON MAP ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE DEFERRED LEFT STALL WARNING PER MEL 27-36-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY RERACKING STALL W ARNING COMPUTER. OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1998050100696 19980501 00696 SO 1998 5 1 WTAA980031 1 19980209 A 2121 EVAC2322C2 FAN EMB 120 EMB120RT SO CABIN FAILED A WTAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 17 284YV 120284 FAT - ELECTRICAL ODOR REPORTED FROM RIGHT PACK. MAINTENANCE DEFERRED RIGHT PACK PER MEL 21-51-2. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING RIGHT GROUND COOLING FAN. OPERATIONAL CHECK SATISFACTO RY. (M) 2 L 7 2 4T RT A31SO 1998050100697 19980501 00697 NM 1998 5 1 TSAA9827195 1 19980305 A 5753 SKIN BOEING 737 737297 1384480 NM RT TE MIDFLAP DENTED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 RT WING INBOARD MIDFLAP LE DENT .57 INCH DEEP BY .60 INCH WIDE AT INBOARD TRACK CUTOUT OUTBOARD CORNER. REPAIRED PER SB A-SBX-98-0024 AND APPROVED BY 8110-3 DATED 3-5-98. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998050100698 19980501 00698 EU 1998 5 1 AS0A98025 1 19980326 A 3240 AHA1653 BRAKE AEROSP ATR72 ATR72212 EU RT MLG FIRE A ASOA F ACTIVATE FIRE EXT. A P FLAME/FIRE NO WARNING INDICATION IN INSP/MAINT 1 SO 11 640AS 405 WHILE AT ATL, MAINTENANCE WAS TAXIING THE AIRCRAFT TO A HANGAR, THE RIGHT MAIN BRAKE OVERHEATED AND CAUGHT ON FIRE. THE RE WERE NO WARNING INDICATIONS IN THE FLIGHT DECK. ATL MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN INBOARD AND OUTB OARD BRAKE ASSEMBLIES, TIRE ASSEMBLIES, BRAKE TRANSMITTERS AND TEMP BULBS. THE AIRCRAFT WAS INSPECTED FOR FIRE DAMAGE, NONE FOUND. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100699 19980501 00699 SO 1998 5 1 ASOA98024 1 19980319 A 5320 12003039001 WINDOW POST EMB 120 EMB120RT SO LT COCKPIT CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 217AS 120011 DURING C-CHECK INSPECTION, FOUND CRACKS IN THE LEFT LATERAL DV WINDOW POST. REQUIRES INSPECTION WITHIN 75 FLIGHT HOURS AND REPLACEMENT WITHIN 150 FLIGHTS HOURS IAW EAC FAX NR SST0468/98 AND EO120-53-0068. (M) 2 L 7 2 4T RT A31SO 1998050100700 19980501 00700 NM 1998 5 1 USAA980B1 1 19980323 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 847 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 35831 23380 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 4 INCH LONG BY 1 INCH WIDE CORROSION BS 847 OVER STRINGER 26R TO STRINGE R 25R FRAME. INSTALLED REPAIR DOUBLER, REPAIRED PER SRM 53-00-51 FIG 203. CORROSION LEVEL 2, CORROSION TASK NR C53-208 -01. (M) 2 L 7 2 4F RT A16WE 1998050100701 19980501 00701 NM 1998 5 1 USAA980129 1 19980323 A 5314 KEEL BEAM BOEING 737 7373B7 1384580 NM BS 707-727 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 35831 23380 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FASTENERS HOLES .5 INCH BY .1875 INCH BS 707-727 LT KEE L BEAM. INSTALLED REPAIR STRAPS, REPAIRED PER EA 43725A. CORROSION TASK NR C53-212-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1998050100702 19980501 00702 NM 1998 5 1 USAA980130 1 19980323 A 5314 KEEL BEAM BOEING 737 7373B7 1384580 NM BS 707 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 505AU 23380 INT - DUIRNG Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FASTENER HOLES .5 INCH BY .5 INCH BS 707-727 RT KEEL BE AM. INSTALLED REPAIR ANGLE, REPAIRED PER EA 43726A. CORROSION TASK NR C53-212-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1998050100703 19980501 00703 NM 1998 5 1 USAA980128 1 19980320 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1016 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 36948 23312 CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES STATION 1016 BEAM IN LEFT LAV AREA. INSTALLED REPAIR STRAP REPAIR DOCUMENT SRM 53-00-51 FIG 203. (M) 2 L 7 2 4F RT A16WE 1998050100704 19980501 00704 NM 1998 5 1 USAA980127 1 19980320 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 986 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 36948 23312 CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES THE ENTIRE LENGTH STATION 986 FLOORBEAM. REPLACED T- CAP PER TYPICAL REPAIR NR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1998050100705 19980501 00705 NM 1998 5 1 USAA980126 1 19980320 A 5315 6545810 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 36948 23312 CLT - DURING Q-6 VISUAL INSPECTION, FOUND CORROSION ON THE UPPER SURFACE OF FLOORBEAM AT STATION 312 LBBL 11.0. CORROSI ON TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998050100706 19980501 00706 NM 1998 5 1 USAA980125 1 19980320 A 5320 ANGLE BOEING 737 7373B7 1384580 NM BS 312 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 36948 23312 CLT - DURING Q-6 VISUAL INSPECTION, FOUND A 17 INCH AREA OF CORROSION AT THE REPAIR ANGLE T-CAP STATION 312 FLOORBEAM LB BL 6 TO RBBL 11. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998050100707 19980501 00707 NM 1998 5 1 USAA980118 1 19980320 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 36948 23312 CLT - DURING Q-6 AND HFEC CHECK VISUAL INSPECTION, FOUND TWO 2 INCH LONG CRACKS IN THE SKIN AT STATION 727D PLUS 6 BL 2L AND BL 2R. INSTALLED DOUBLER PER REPAIR DOCUMENT SRM 53-60-01. (M) 2 L 7 2 4F RT A16WE 1998050100708 19980501 00708 NM 1998 5 1 USAA980119 1 19980320 A 5320 SILL BOEING 737 7373B7 1384580 NM BS 296 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 36948 23312 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT RIVET HOLE FORWARD SERVICE DOOR SILL STATION 296 RBBL 55.0. WEB REPAIR, DOUBLER INSTALLED PER REPAIR DOCUMENT SRM 51-70-13. (M) 2 L 7 2 4F RT A16WE 1998050100709 19980501 00709 NM 1998 5 1 USAA980120 1 19980320 A 5320 FORMER BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 390US 36948 23312 CLT - DURING Q-6 HFEC AND VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT STATION 727D FORMER. FRAME REPAIRED AT STATION 7 27D BL 1L PER REPAIR DOCUMENT SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F RT A16WE 1998050100710 19980501 00710 NM 1998 5 1 USAASB98075 1 19980324 A 2121 65771 FAN BOEING 737 737301 1384611 NM E/E COMPT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 585US 21911 23930 STL - FLT 133 - FLIGHT DIVERTED TO STL DUE TO ELECTRICAL SMELL IN THE CABIN. CAPTAINS STATED DURING THAT DURING CRUISE, AND ELECTRICAL SMELL WAS NOTED COMING FROM THE MID CABIN. GALLEY POWER WAS TURNED OFF AND SMELL SEEMED TO DISSIPATE ON LY TO RETURN A SHORT TIME LATER. THE FIRST OFFICER CHECKED THE CABIN FIRST, THEN THE CAPTAIN TO SEE IF THEY COULD DETER MINE SOURCE. NO SOURCE WAS FOUND AND NO SMOKE WAS PRESENT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS D ECLARED. MAINTENANCE FOUND THE NORMAL EQUIPMENT COOLING FAN CAUSING SMELL. REPLACED SAME. OPERATIONAL CHECK GOOD. (M ) 2 L 7 2 4F RT A16WE 1998050100711 19980501 00711 NM 1998 5 1 USAASB98068 1 19980318 A 2131 7102048 CONTROLLER BOEING 737 7373B7 1384580 NM E/E COMPT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 517AU 58413 23703 CLT - FLT 122 - AT FL230, CAPTAIN STATED HE LOST CABIN PRESSURIZATION. SYSTEM DID NOT AUTO SWITCH TO STANDBY. MANUAL A C WAS SELECTED AND CONTROL WAS REGAINED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. AN EMERG ENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER PER MM. SYSTEM CHECKS GOOD IN AUTO A ND STANDBY. (M) 2 L 7 2 4F RT A16WE 1998050100712 19980501 00712 NM 1998 5 1 USAASB98072 1 19980320 A 2121 6454051 FAN BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 391US 36886 23313 CLT - FLT 703 - AFTER TAKEOFF, PASSING THROUGH 1,700 FEET, CREW BEGAN TO SMELL A BURNING ELECTRICAL ODOR. SMEL APPEARED TO BE STRONGER IN REAR OF AIRCRAFT THAN THE COCKPIT AND FRONT GALLEY. FLIGHT RETURNED TO FIELD AT CLT. ON APPROACH TO CLT, CREW SHUT DOWN THE RECIRCULATION FAN AND THE APU AND THE ODOR SUBSIDED BEFORE TOUCHDOWN. FLIGHT LANDED WITHOUT IN CIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FAN PER MM 21-21-22. OPERATIONA L CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100713 19980501 00713 NM 1998 5 1 USAASB98074 1 19980322 A 2170 V1211 SEPARATOR BAG BOEING 737 7373B7 1384580 NM RT PACK CLOGGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 520AU 23706 PHL - FLT 1486 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF. DUCT PRESSURE WAS GOOD AT 40 PSI AND OUTFLOW VAL VE WAS FULL CLOSED. THE LEFT PACK WAS ON MEL. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT PACK WATER SEPARATOR BAG CLOGGED. REPLACED SAME. OPERATIONAL CHE CK OF RIGHT PACK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100714 19980501 00714 NM 1998 5 1 USAASB98087 1 19980402 A 5242 DOOR BOEING 737 737301 1384611 NM E/E COMPT OPEN A USAA A UNSCHED LANDING P W NO WARNING INDICATION INADEQUATE Q C CL CLIMB 1 EA 19 577US 23742 CLT - FLT 84 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE AND THE COCKPIT WAS EXTREMELY NOISY. FLIGHT RETURNED TO FIE LD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE E/E DOOR OPEN AND ALSO FOUND THE DOOR INDICATION IN THE COCKPIT WAS INOP. DOOR WAS CLOSED AND THE FLIGHT WAS DISPATCHED WITH THE E/E DOOR LGI HT INDICATION ON MEL. MAINTENANCE ADJUSTED THE E/E DOOR PROXIMITY SWITCH. DOOR INDICATION CHECK GOOD. REMOVED MEL. ( M) 2 L 7 2 4F RT A16WE 1998050100715 19980501 00715 NM 1998 5 1 USAASB98067 1 19980317 A 3350 30043229 LIGHT BOEING 737 7374B7 1384702 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 PHL - PILOT REPORTED THE EMERGENCY PATH LIGHTING WAS INOP AT SEAT ROWS 24 AND 25ABC. MAINTENANCE REMOVED AND REPLACED T HE LEFT AFT ESCAPE SLIDE LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100716 19980501 00716 1998 5 1 USAASB98069 4 19980319 A 3425 329B8J ADI BOEING 737 737401 1384701 NM FLIGHT COMPT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 411US 32132 23880 PIT - FLT 1498 - UPON CLIMB-OUT FROM PIT, CAPTAINS ATTITUDE INDICATOR FAILED. DECISION WAS MADE TO RETURN TO FIELD AT P IT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS ATTITUDE DIRECTION INDICATOR. SYSTEM FUNCTIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100717 19980501 00717 NM 1998 5 1 USAASB98080 1 19980328 A 2120 AIR DISTR BOEING 737 737401 1384701 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 420US 23987 EWR - FLT 7003 - AFTER TAKEOFF, AT APPROX 10,000 FT, THE CABIN FILLED WITH SMOKE. CAPTAIN DUMPED PRESSURE, OPENED OUTFL OW VALVE AND PLACED RECIRCULATION FAN ON HIGH. CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TO EWR. DURNG DESCENT, CABIN CLEARED WITH MINOR SMELL OF SMOKE. FLIGHT LANDED NORMAL WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. MAINTENANCE CHECKED BOTH ENGINES AND AIR CONDITION BAYS FOR DUCT SECURITY AND LEAKS. FOUND OK. CHECKED AIRCRAFT FOR SKYDROL LEAKS. NONE FOUND. CHECKED LAVS AND GALLEY EQUIPMENT. FOUND NORMAL. RAN EACH PACK OFF OF APU AND ENGINES. NO SMOKE NOTED. COULD NOT DUPLICATE SMOKE OR SMELL. (M) 2 L 7 2 4F RT A16WE 1998050100718 19980501 00718 NM 1998 5 1 USAASB98065 1 19980315 A 5610 5717623115 WINDOW BOEING 737 737301 1384611 NM FLIGHT COMPT OUT OF ADJUST A USAA A UNSCHED LANDING O OTHER DE DESCENT 1 EA 19 559AU 23513 OAK - FLT 81 - FLIGHT DIVERTED TO OAK DUE TO CAPTAINS SLIDING WINDOW WOULD NOT CLOSE. FLIGHT LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE ADJUSTED THE CAPTAINS L2 SLIDING WINDOW PER MM 56-12-11. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100719 19980501 00719 NM 1998 5 1 EISA98041 1 19980216 A 5543 TAB BOEING 727 727223 1384074 NM RUDDER MOISTURE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK, X-RAY INSPECTION OF RUDDER MOISTURE IN HONEYCOMB AS SHOWN IN SHOTS NR 5C, 9C AND 9D. CUT OUT PORTION OF RUDDER TAB TO REMOVE WATER. REMOVED WATER FROM HONEYCOMB PER SRM 51-40-09 USING VAC BAG METHOD. POTTED HONEY CORE PER SRM 51-40-06. FABRICATED NEW SKIN REPLACEMENT PARTS PER SRM 51-10-1 AND INSTALLED WITH FIBERGLASS OVER LAY PER SRM, 51 -40-08 AND 51-40-09. (M) 2 L 7 3 4F A3WE 1998050100720 19980501 00720 NM 1998 5 1 EISA98042 1 19980218 A 5520 ANGLE BOEING 727 727223 1384074 NM LT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, X-RAY OF LEFT ELEVATOR REVEALED ANGLE MATERIAL MISSING AND 1.5 INCH CRACK AS SHOWN IN SHOTS N R 1 AND NR 2. PULLED BACK SKIN TO ACCESS AREA, REMOVED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 55-20-3 AND 55 -20-4 BALANCE CHECKED PER SRM 51-80- P-1 PARA 3. (M) 2 L 7 3 4F A3WE 1998050100721 19980501 00721 NM 1998 5 1 EISA98043 1 19980218 A 5230 WEB BOEING 727 727223 1384074 NM CARGO DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND 2.5 INCH CRACK IN FORWARD CARGO DOOR WEB AT FS 575, BOTTOM AFT, LOWER SIDE OF DOOR. ST OPPED DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-02. (M) 2 L 7 3 4F A3WE 1998050100722 19980501 00722 NM 1998 5 1 EISA98044 1 19980218 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM BS 720 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND INTERCOSTAL CRACKED IN 5 PLACES AT FS 720-720A. REMOVED ANGLE, FABRICATED NEW ANGLE PE R SRM 51-40-03 AND INSTALLED PER SRM 53-10-08. (M) 2 L 7 3 4F A3WE 1998050100723 19980501 00723 NM 1998 5 1 EISA98045 1 19980218 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 312 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND STIFFENER CRACKED IN E/E BAY, FS 312, LBL 32, WL 208. REMOVED STIFFENER AND FABRICATED NEW PART PER SRM 51-40-03, INSTALLED SRM 51-10-08. (M) 2 L 7 3 4F A3WE 1998050100724 19980501 00724 NM 1998 5 1 EISA98046 1 19980218 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 303 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND ANGLE CRACKED IN E/E BAY, FS 303, LBL 10. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE PER SRM 51-40-03 AND INSTALLED PER SRM 51-10-03. (M) 2 L 7 3 4F A3WE 1998050100725 19980501 00725 NM 1998 5 1 EISA98047 1 19980218 A 5712 RIB BOEING 727 727223 1384074 NM WS 171 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND LEFT WING RIB CRACKED AT TOP OF RIB, WS 171 AS MARKED. REMOVED STIFFENER, FABRICATED A NGLES OF 7075-0 AND HEAT TREATED TO 7075-T6 PER BAC DRAWING 53-98012-5. INSTALLED ANGLES PER DWG 53-98012-5 INSTALLED S TIFFENER PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998050100726 19980501 00726 NM 1998 5 1 EISA98048 1 19980218 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 303 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND .25 INCH CRACK ON STRINGER 6L AT FS 303.9. STOP DRILLED CRACK. FABRICATED AND INSTALL ED DOUBLER PER SRM 53-30-01. (M) 2 L 7 3 4F A3WE 1998050100727 19980501 00727 NM 1998 5 1 EISA98049 1 19980218 A 5712 RIB BOEING 727 727223 1384074 NM WS 171 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND 3 CRACKS IN WING RIB AT RT WING STATION 171, TOP SIDE OF RIB. REMOVED STIFFENER, FABRI CATED ANGLES OF 7075-0 AND HEAT TREATED TO 7075-T6. INSTALLED ANGLES PER BAC DWG 53-98012-5. INSTALLED STIFFENER PER S RM 51-30-02. (M) 2 L 7 3 4F A3WE 1998050100728 19980501 00728 NM 1998 5 1 EISA98050 1 19980218 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM BS 720-740 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, FOUND INTERCOSTAL CRACKED AT FS 720F-740 AFT END, LEFT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 57-40-03. (M) 2 L 7 3 4F A3WE 1998050100729 19980501 00729 NM 1998 5 1 EISA98053 1 19980218 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 FOUND DURING CARGO MOD, DURING D-CHECK INSPECTION, FOUND CRACK IN FRAME AT FS 700, AT STRINGER 20L-21L. FABRICATED AND INSTALLED DOUBLER PER SRM 53-10-04. (M) 2 L 7 3 4F A3WE 1998050100730 19980501 00730 NM 1998 5 1 EISA98054 1 19980218 A 5752 HINGE BOEING 727 727223 1384074 NM RT AILERON BROKEN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 DURING D-CHECK INSPECTION, REMOVED RIGHT OUTBOARD OUTBOARD AILERON TAB TO FOM AND FOUND NR 3 HINGE BROKEN. REMOVED AND REPLACED NR 3 HINGE. REINSTALLED AILERON TAB PER MM 27-10-0. (M) 2 L 7 3 4F A3WE 1998050100731 19980501 00731 NM 1998 5 1 EISA98060 1 19980325 A 3350 COVER BOEING 727 7272M7 138407S NM CABIN LOOSE A EISA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 721RW 21200 FOUND R2 EMERGENCY LIGHT COVER IS LOOSE DURING CREW MEMBER WALKAROUND (PILOT REPORT P-49). RESECURED R2 EMERGENCY LIGHT COVER AS REQUIRED. (M) 2 L 7 3 4F A3WE 1998050100732 19980501 00732 NM 1998 5 1 EISA98061 1 19980322 A 3350 LIGHTS BOEING 727 7272M7 138407S NM CABIN LOOSE A EISA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 721RW 21200 FOUND FLOOR LIGHTING ON ROW 32D LOOSE DURING CREW MEMBER WALKAROUND (PILOT REPORT P-25). RESECURED AS REQUIRED. OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 1998050100733 19980501 00733 NM 1998 5 1 EISA98068 1 19980311 A 3350 BULB BOEING 727 7272M7 138407S NM CABIN FAILED A EISA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 721RW 21200 LIGHT BULB INOPERATIVE IN EXIT SIGN ROW 20. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED LIGHT BULBS ON OVERWING EXIT SIGN. (M) 2 L 7 3 4F A3WE 1998050100734 19980501 00734 NM 1998 5 1 EISA98051 1 19980218 A 5320 FLOOR PAN BOEING 727 727223 1384074 NM BS 1178 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6819 19494 FOUND DURING CARGO COMPT MOD, DURING D-CHECK INSPECTION, FOUND CORROSION ON FLOOR PAN AT FS 1178 LT SIDE. CUT OUT DAMAG E. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-02. (M) 2 L 7 3 4F A3WE 1998050100735 19980501 00735 NM 1998 5 1 EISA98057 1 19980320 A 3230 SPLICE BOEING 727 72731 1384010 NM LANDING GEAR FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 240NE 18906 ON TAKEOFF OUT OF CLE, UNABLE TO RETRACT LANDING GEAR, TRIED CYCLING HANDLE SEVERAL TIMES, WOULD GO TO OFF POSITION ONLY . WHEN POSITION BACK DOWN HAD BOTH ANTI-SKID RELEASE LIGHTS ILLUMINATED. PILOT HAD AIR TURN BACK TO CLE. REPAIRED FAU LTY SPLICED TO LANDING GEAR LEVER SAFETY SOLENOID, GEAR HANDLE OPS NORMAL. (M) 2 L 7 3 4F A3WE 1998050100736 19980501 00736 1998 5 1 EISA98069 4 19980405 A 3425 2589201902 COMPASS RACK BOEING 727 727227 1384078 NM COMPT INOP A EISA A UNSCHED LANDING G MULTIPLE FAILURE TO TAKEOFF 1 SW 07 308AS 8070264 22002 DEPARTING BRUSSELS CAPTAINS HSI HAS COMPASS FLAG IN VIEW AND CO-PILOT RMI OFF FLAG IN VIEW. AIR TURNBACK TO BRUSSELS. G ENERATED FROM PILORT REPORT. REMOVED AND REPLACED NR 1 COMPASS RACK IAW MM 34-00. OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998050100737 19980501 00737 NM 1998 5 1 USAASB98084 1 19980330 A 3397 WIRE BOEING 737 7374B7 1384702 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 442US 24841 MCI - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY LIGHTS ILLUMINATE WITH SWITCH IN THE OFF POSITION. MAINTENANCE FOUN D A BROKEN WIRE AT PIN NR 2 OF THE SWITCH. REPAIRED SAME. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100738 19980501 00738 NM 1998 5 1 USAASB98085 1 19980402 A 3350 210310005 FUSE BOEING 737 737401 1384701 NM CABIN BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 422US 23989 ROC - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS INOP DURING THE OVERNIGHT CHECK, LEFT OVERWING HATCH SIGN L751, R IGHT EXTERIOR AFT OVERWING FLOOD LIGHT L548 AND THE AISLE LOW LEVEL LIGHTING AT SEAT ROWS 6 THROUGH 9. MAINTENANCE RELA MPED THE EXTERIOR AFT OVERWING FLOOD LIGHT L548 AND REMOVED AND REPLACED THE FUSE IN THE POWER SUPPLY FOR OVERWING HATCH SIGN L751 AND THE AISLE LOW LEVEL LIGHTING AT SEAT ROWS 6 THROUGH 9. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100739 19980501 00739 NM 1998 5 1 USAASB98083 1 19980329 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 442US 24841 ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS THROUGHOUT THE CABIN INOP, ROW 1 AND 2 SEAT MOUNTED EVACUATION LI GHTS, FORWARD ENTRY CEILING EXIT SIGN, ROW 2 LEFT AND ROW 4 RIGHT BULLNOSE LIGHTS, AFT ENTRY AND AFT SERVICE DOOR EXIT S IGNS, AFT PASSENGER DOOR SIDEWALL AND BULLNOSE EXIT SIGNS, ROWS 20 THROUGH 23 SEAT MOUNTED EVACUATION LIGHTS AND ROW 25 RIGHT BULLNOSE LIGHTS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS IN THE FORWARD AND AFT ENTRY CEILINGS, LEFT S IDE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050100740 19980501 00740 NM 1998 5 1 USAABB98025 1 19980331 A 3350 9221009 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 LAX - R2 DOOR IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998050100741 19980501 00741 EU 1998 5 1 SIMA980791 1 19980320 A 3610 32149602 VALVE AEROSP ATR72 ATR72212 EU NR 1 PACK INOPERATIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 425MJ 140 425 DFW - FLT 3620 - UPON ARRIVAL TO DFW, CREW SMELLED SMOKE AND CALLED FOR CFR. PAX AND CREW DEPLANED RAPIDLY. NO EMERGEN CY EVACUATION ON THE TAXIWAY. NO FIRE DETECTED. CREW THEN BROUGHT A/C BACK TO GATE. NO FURTHER INCIDENTS REPORTED. A /C RETURNED TO SERVICE. CREW REPORTED SMOKE IN COCKPIT FROM ACM. NR 1 PAC VALVE CIRCUIT BREAKER POPPED JUST PRIOR TO S MOKE. MAINTENANCE R/I'D THE NR 1 PAC VALVE PER ATR72 JIC'S. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/ C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050100742 19980501 00742 NM 1998 5 1 TWAA9805103 1 19980403 A 2560 582243 BATTERY PACK BOEING 767 767231 1385131 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 607TW 22570 JFK - FLT 904 - DURING PREFLIGHT CHECK, THE NR 2 LEFT OVERWING SLIDE SQUIBB DID NOT TEST CORRECTLY. PLACARDEDPER MEL. T HE NEXT DAY THE BATTERY PACK WAS REPLACED. (M) 2 L 7 2 4F RT A1NM 1998050100743 19980501 00743 NM 1998 5 1 TWAA9805102 1 19980405 A 2530 888011 CART BOEING 767 767231 1385131 NM GALLEY WORN A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 CE 05 601TW 343 22564 JFK - FLT 841 - SERVING CART 343 POPPED NR 2 CIRCUIT BREAKER. THERE WAS SMELL OF BURNED ELECTRICAL WIRING IN OR NEAR CA RT. CREW DID NOT RESET CIRCUIT BREAKER. REPLACED CART. (M) 2 L 7 2 4F RT A1NM 1998050100744 19980501 00744 NM 1998 5 1 TWAA9805101 1 19980403 A 2613 OVERHEAT LOOP BOEING 727 727231 1384079 NM AFT BODY OUT OF POSITION A TWAA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CE 05 54340 20845 STL - FLT 5039 - ON TAKEOFF, THE LOWER AFT BODY OVERHEAT LIGHT CAME ON. SWITCHED BLEED SOURCES BUT LIGHT INTERMITTENT. REPOSITIONED LOOP PER MM 26-1401 AND REPLACED LAMP ASY FOR AFT BODY OVERHEAT. OP 17 MAINTENANCE CHECK 9-15-97. (M) 2 L 7 3 4F A3WE 1998050100745 19980501 00745 WP 1998 5 1 TWAA9805003 1 19980323 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945-950 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON LONGERON 23L, STATION 945 TO 950. REMOVED CORROSION PER SRM 51 -10-03. INSTALLED NEW PART PER SRM 51-01 PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998050100746 19980501 00746 WP 1998 5 1 TWAA9805002 1 19980401 A 3230 39281375001 RETRACT CYL DOUG DC9 DC982 3022082 WP NLG WORN A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 904TW 49156 STL - FLT 714 - AFTER CHECK-C MAINTENANCE FLT 714 RETURNED TO STL DUE TO NOSE GEAR DOOR UNSAFE LIGHT ON WITH GEAR RETRAC TED. FOUND LOWER BUNGEE BOLT FOR NOSE GEAR TOO LONG MFG NAS1106-23D. HIT STRUCTURE AT DOUBLER. INSTALLED SHORTER BOLT . AIRCRAFT OPERATED OUT OF STL ON FLT 10, BUT LANDING GEAR WOULD NOT RETRACT. RETURNED TO STL. FOUND GROUND BYPASS HA NDLE OUT. REPLACED LATCH ON GROUND BYPASS HANDLE, THE NLG RETRACT CYL, AND THE RETRACT CYCL LOWER BUSHING. LATCH MFG H 5000-2-125-218. BUSHING MFG S22103780H8-050. (M) 2 L 7 2 4F A6WE 1998050100748 19980501 00748 WP 1998 5 1 TWAA9804901 1 19980401 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 990Z 47136 FLT STL - FLT 314 - ONE SECTION OF OVERHEAD COACH EMERGENCY LIGHTS WERE REPORTED INOP. REPLACED CEILING POWER SUPPLY IN FORWARF CABIN. (M) 2 L 7 2 4F A6WE 1998050100749 19980501 00749 WP 1998 5 1 TWAA9804803 1 19980330 A 2130 94840213 AMPLIFIER DOUG DC9 DC931 3022065 WP PRESSURE CONTROL WORN A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 992Z 47095 ORD - FLT 1394 - AT FL 270 LOST CABIN PRESSURE. MANUAL PRESSURIZATION DID NOT CONTROL CABIN. PASSENGER OXY COMPT DOORS OPENED AUTOMATICALLY. FLIGHT DIVERTED TO ORD. AIRCRAFT FERRIED TO STL FOR CORRECTION. CHANGED CABIN PRESSURE CONTROL AMPLIFIER, RESEALED SEVERAL SMALL LEAKS IN AIRCRAFT FUSELAGE, AND REPLACED SPLIT FLEX HOSE BETWEEN PRESSURIZATION CONTR OLLER AND FILTER. (M) 2 L 7 2 4F A6WE 1998050100750 19980501 00750 1998 5 1 TWAA9804802 4 19980331 A 2210 258668911 CONTROL HEAD DOUG DC9 DC932 3022066 WP COCKPIT WORN A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 922L 47108 STL - FLT 541 - THE AUTOPILOT CONTROL HEAD WAS REPORTED SMOKING AND BURNING. REPLACED AUTOPILOT CONTROL HEAD. (M) 2 L 7 2 4F A6WE 1998050100751 19980501 00751 NM 1998 5 1 TWAA9804801 1 19980331 A 2422 7077603 INVERTER BOEING 767 767231 1385131 NM STANDBY WORN A TWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 05 605TW 22568 YQX - FLT 818 - BOTH FLIGHT MANAGEMENT COMPUTER SYSTEMS MALFUNCTIONED, STANDBY INSTRUCTIONS LIGHTING BECAME INOP, AND EI CAS MESSAGE STANDBY INVERTER DISPLAYED. DIVERTED TO YQX. REPLACED THE STANDBY INVERTER AND K105. (M) 2 L 7 2 4F RT A1NM 1998050100752 19980501 00752 NM 1998 5 1 MASA98062 1 19980324 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 DURING A ROUTINE INSPECTION, MAINTENANCE PERSONNEL FOUND THE LEFT OVERHEAD EMERGENCY EXIT SIGN WAS DIM. MAINTENANCE REM OVED AND REPLACED BURNED OUT BULBS. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998050100753 19980501 00753 NM 1998 5 1 AALA980625 1 19980326 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1060 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND NICK WITH CRACK IN FORWARD SKIN AT STATION 30, STATION 1060. REMOVED OK AND INSTALLED DOUBLER REPAIR PER SR M 53-30-3 PAGE 1. (M) 2 L 7 3 4F A3WE 1998050100754 19980501 00754 NM 1998 5 1 AALA980676 1 19980401 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - FOUND TOP FLANGE OF FLOORBEAM CORRODED, (PREVIOUSLY REPAIRED) STATION 380. REMOVED AND REPLACED TO TOP CAP OF (PR EVIOUSLY REPAIRED) UPPER FLANGE REPAIR PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998050100755 19980501 00755 NM 1998 5 1 AALA980677 1 19980401 A 5311 FRAME BOEING 727 727223 1384074 NM BS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FORWARD GALLEY DOOR FORWARD FRAME AT DOOR CUTOUT CRACKED JUST ABOVE STRINGER 9R, STATION 380 IN SEAL LAND FLANGE. INSTALLED NEW PIECE IN FORWARD GALLEY DOOR FRAME STRINGER 9R, STATION 380 PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998050100756 19980501 00756 NM 1998 5 1 AALA980672 1 19980401 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - BELLFRAME BENT ABOVE STRINGER 25L AT STATION 1110. INSTALLED BELLFRAME REPAIR PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998050100757 19980501 00757 NM 1998 5 1 AALA980673 1 19980401 A 5320 WEB BOEING 727 727223 1384074 NM BS 1163 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND SHEAR WEB CORRODED AT STATION 1163 LBL 45 IN LEFT AFT LAV. INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-2. ( M) 2 L 7 3 4F A3WE 1998050100758 19980501 00758 NM 1998 5 1 AALA980675 1 19980401 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CARGO CEILING FLOORBEAM CORRODED LBL 24 TO LBL 48 AT STATION 1070. INSTALLED LOWER CHORD REPAIR ANGLE AND S TRAPS, TWO LOCATIONS LBL 24 PER SRM 53-10-8 AND STRAP LBL 45 PER ESO. (M) 2 L 7 3 4F A3WE 1998050100759 19980501 00759 NM 1998 5 1 AALA980667 1 19980401 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 344 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND STRINGER 5R CRACKED AT STATION 344. REPAIRED STRINGER 5R, STATION 344 PER ESO DATED 3/17/98 ESO 11697. (M) 2 L 7 3 4F A3WE 1998050100760 19980501 00760 NM 1998 5 1 AALA980668 1 19980401 A 5330 SKIN BOEING 727 727223 1384074 NM BS 581 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CORROSION BLISTERING THROUGH BELLY SKIN AT STATION 581 STRINGER 27L. REPAIRED PER ESO 11697, DATED 3-11-98. (M) 2 L 7 3 4F A3WE 1998050100761 19980501 00761 NM 1998 5 1 AALA980669 1 19980401 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1097 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CROWN SKIN CRACKED FROM RIVET APPROX .25 INCH LONG STATION 1097, 1ST RIVET TO THE RIGHT. INSTALLED DOUBLER PER S/B 727-53A0204. (M) 2 L 7 3 4F A3WE 1998050100762 19980501 00762 NM 1998 5 1 AALA980670 1 19980401 A 5320 WEB BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - SHEAR WEB CORRODED AT STATION 1148 LBL 45 INCH LEFT AFT LAV. INSTALLED TYPICAL WEB REPAIR PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998050100763 19980501 00763 NM 1998 5 1 AALA980671 1 19980401 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CORROSION ON TOP OF FLOORBEAM STATION 380 RBL 29-RBL 42 AND CORROSION ON TOP OF AND ON BOTTOM OF TOP FLANGE STATION 380 RBL 45 TO RBL 63. REPAIRED PER SRM 53-10-08 PAGES 9A AND 9B. (M) 2 L 7 3 4F A3WE 1998050100764 19980501 00764 NM 1998 5 1 AALA980660 1 19980401 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CORROSION ON BELLFRAME REPAIR STATION 990 BETWEEN STA 25A TO STRINGER 30. REMOVED DOUBLERS, REMOVED CORROSI ON, TREAT AND PRIMED, REINSTALLED DOUBLERS. (M) 2 L 7 3 4F A3WE 1998050100765 19980501 00765 NM 1998 5 1 AALA980664 1 19980401 A 5320 INTERCOSTAL BOEING 727 727223 1384074 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CORROSION ON INTERCOSTAL FROM FS 1050 TO FS 1070 BETWEEN STRINGER 26R AND 27R. REMOVED CORROSION, INSTALLED DOUBLER AND NEW TOP ANGLE. (M) 2 L 7 3 4F A3WE 1998050100766 19980501 00766 NM 1998 5 1 AALA980659 1 19980401 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 987-996 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 878AA 21390 TUL - FOUND CORROSION ON STRINGER 30 BETWEEN STATION 987 TO STATION 996. REPAIRED STRINGER PER ESO 11697. (M) 2 L 7 3 4F A3WE 1998050100767 19980501 00767 WP 1998 5 1 AALA980647 1 19980329 A 5347 ROLLER TRAY DOUG DC10 DC1010 3022110 WP BS 1778 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND LEFT LOAD CHAIN TRAY UPPER SURFACE CORRODED AT FASTENERS HOLES, STATION 1778. INSTALLED NEW ROLLER TRAY PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998050100768 19980501 00768 WP 1998 5 1 AALA980642 1 19980328 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 129AA 46996 TUL - FOUND CORROSION ARUOND NUMEROUS NUT PLATES ON BOTTOM OF FLOORBOARD FRAME ANGLES BOTH FORWARD AND AFT SIDES FROM 43 L TO 43R AT STATION 1841. REMOVED DAMAGED AREAS AND INSTALLED REPAIR ANGLES PER SRM 53-00-01 VOL 1. (M) 2 L 7 3 4F A22WE 1998050100769 19980501 00769 NE 1998 5 1 USAABB98026 2 19980403 A 7260 M06622AA GEARBOX BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE FAILED A USAA A UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 EA 19 600AU 27155 22192 30524 ABQ - FLT 28 - EN ROUTE LAX-PIT, AT FL370 CREW NOTE LEFT ENGINE SPOOL DOWN, ACCOMPANIED BY EICAS MESSAGE 'L ENG LP PUMP' . FLIGHT DIVERTED TO ABQ AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE GEARBOX. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1998050100770 19980501 00770 WP 1998 5 1 IXXA9800044 1 19980302 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 830BX 2907 45973 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON FUSELAGE FRAME AT FUSELAGE STATION 70 BETWEEN LONGERONS 32 AND 33 RIGHT. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF A NESTED ANGLE REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING E27-R04 AND ENGINEERING ORDER 53-DC8-820. 2 L 7 4 4F RT 4A25 1998050100771 19980501 00771 WP 1998 5 1 IXXA9800045 1 19980301 A 5330 PLATING DOUG DC8 DC871F 302199D WP BS 340 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 830BX 2907 45973 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 340 LONGERON 31 LEFT. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN A CCORDANCE WITH FAA DER APPROVED DRAWING E27-R05 AND ENGINEERING ORDER 53-DC8-821. 2 L 7 4 4F RT 4A25 1998050100772 19980501 00772 WP 1998 5 1 IXXA9800046 1 19980301 A 5330 PLATING DOUG DC8 DC871F 302199D WP BS 418 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 830BX 2907 45973 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED AT THE LEFT FORWARD EMERGENCY EXIT DOOR LOWER AFT JAMB CORNER AT FUSELAGE STATION 418. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND A TRIPLER IN ACCORDANCE WITH DOUGLAS FAX FILE ACTION 362047, FILE 98-03-05-005 AND ENGINEERING ORDER 53-DC8-822. 2 L 7 4 4F RT 4A25 1998050100773 19980501 00773 WP 1998 5 1 IXXA9800047 1 19980301 A 5330 PLATING DOUG DC8 DC871F 302199D WP BS 30 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 830BX 2907 45973 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 30 AND 61 LONGERON 34 RIGHT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER A ND REPAIR DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED DRAWING E27-R03 AND ENGINEERING ORDER 53-DC8-825. 2 L 7 4 4F RT 4A25 1998050100774 19980501 00774 WP 1998 5 1 IXXA9800042 1 19980204 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 450 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823BX 2851 46064 DURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON LONGERON 35 LEFT SPLICE FITTING AT FUSELAGE STATION 450. REP AIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW SPLICE FITTING IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-8-53-059-98 AND ENGINEERING ORDER 53-DC8-796. 2 L 7 4 4F RT 4A25 1998050100775 19980501 00775 WP 1998 5 1 IXXA9800043 1 19980422 A 3310 BA170 BALLAST DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 821BX 45811 EN ROUTE, A BURNING ODOR WAS SENSED IN THE COCKPIT WHEN THE GLARESHIELD FLUORESCENT LIGHTING WAS ILLUMINATED. THE LIGHT ING SYSTEM WAS TURNED OFF AND THE ODOR SUBSIDED AND THE FLIGHT CONTINUED TO TOL. MAINTENANCE INSPECTED AND FOUND THE GL ARESHIELD LIGHT BALLAST DEFECTIVE. THE GLARESHIELD LIGHTING WAS PLACED ON DEFERRAL AND THE AIRCRAFT WAS RETURNED TO SER VICE. 2 L 7 4 4F RT 4A25 1998050100776 19980501 00776 WP 1998 5 1 9807269884 1 19980426 A 3150 SWITCH DOUG DC9 DC951 3022051 WP E/E COMPT STICKING A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 677MC 47756 DURING TAKEOFF ROLL, THE TAKEOFF AURAL WARNING HORN SOUNDED. FLIGHT CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHO UT INCIDENT. MAINTENANCE CLEANED AND LUBRICATED THE HORIZONTAL STABILIZER WARNING SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050100777 19980501 00777 WP 1998 5 1 9807279104 1 19980424 A 3350 SOCKET DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 94S 47204 DURING LINE CHECK, FOUND 2 RED EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED 2 SOCKET ASSEMBLIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100778 19980501 00778 WP 1998 5 1 9807289304 1 19980425 A 3350 SPLICE DOUG DC9 DC982 3022082 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 931MC 48057 DURING LINE CHECK, FOUND FLOOR TRACK LIGHT AFT OF SEAT ROW 1CD WITH BROKEN WIRE SPLICE. MAINTENANCE REPAIRED WIRING, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100779 19980501 00779 WP 1998 5 1 9807299876 1 19980425 A 3350 CHARGER DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 785NC 48110 DURING LINE CHECK, FOUND LEFT AND RIGHT EMERGENCY EXIT EXTERIOR LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY CHARGE R, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050100780 19980501 00780 WP 1998 5 1 9807309866 1 19980427 A 3397 WIRE DOUG DC9 DC951 3022051 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 3C INOPERATIVE. MAINTENANCE INSTALLED WIRING SPLICE AND REPOSITIONED W IRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050100781 19980501 00781 WP 1998 5 1 9807319305 1 19980427 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 307RC 48086 DURING LINE CHECK, FOUND COCKPIT EMERGENCY LIGHTS DIM. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100782 19980501 00782 WP 1998 5 1 9807329983 1 19980424 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 983US 47282 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 12 THRU 14 INOPERATIVE. REPLACED BATTE RY PACK AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100783 19980501 00783 1998 5 1 9807339952 4 19980426 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP CABIN DOOR LOW RPESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 916RW 37100 90 47144 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998050100784 19980501 00784 WP 1998 5 1 9807349921 1 19980426 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 943N 47647 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERHEAD EMERGENCY LIGHTS DIM. REPLACED BATTERIES IN POWER SUPPLY AT FS 9 84, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100785 19980501 00785 WP 1998 5 1 9807359918 1 19980426 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 940N 47572 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT TAIL CONE HANDLE INOPERATIVE. SOCKET WAS CORRODED THROUGH LEGS OF LAMP. REPLACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100786 19980501 00786 WP 1998 5 1 9807369907 1 19980424 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 957N 47253 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS BETWEEN ROWS 5 THRU 7 INOPERATIVE. REPLACED FUSE, OPERATIONA L CHECK NORMAL. 2 L 7 2 4F A6WE 1998050100787 19980501 00787 WP 1998 5 1 9807591225 1 19980425 A 2420 976J86217 CONTROL DOUG DC10 DC1030 3023501 WP NR 1 GENERATOR FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 GL 01 225NW 269 100 46582 NR 1 GENERATOR OFF LIGHT ILLUMINATED AND NR 1 GENERATOR DROPPED OFF LINE. ON TAKEOFF ROLL, THE NR 1 GENERATOR OFF LIGHT ILLUMINATED AGAIN. RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 1 GENERATOR CONTROL, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A22WE 1998050100788 19980501 00788 WP 1998 5 1 9807601156 1 19980426 A 2450 RCCB DOUG DC10 DC1040 3023508 WP CABIN INOPERATIVE A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 GL 01 156US 46765 DURING CRUISE, LOST GROUND SERVICE BUS, VIDEO SYSTEM BECAME INOPERATIVE AND ALSO TOILETS. WATER QUANTITY INDICATED ZERO AND WATER PRESSURE INDICATED LOW. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RCCB BI-33 9, OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A22WE 1998050100789 19980501 00789 1998 5 1 9807611229 4 19980424 A 2216 37570217 COMPUTER DOUG DC10 DC1030 3023501 WP E/E COMPT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 229NW 8525 8525 46551 AFTER DEPARTING, THE NR 1 AUTO PILOT OR ATS WOULD NOT ENGAGE. NR 2 AUTO PILOT WOULD ENGAGE BUT WOULD NOT TRIM. FLIGHT RETURNED TO AMS AND LANDED WITHOUT INCIDENT. REPLACED AUTO PITCH TRIM COMPUTER AND ACCELEROMETER, OPERATIONAL CHECK NOR MAL. 2 L 7 3 4F A22WE 1998050100790 19980501 00790 EU 1998 5 1 QXEA9800620 1 19980425 A 3350 1315 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TEST IS GOOD. 2 L 7 2 4F RT A20EU 1998050100791 19980501 00791 EU 1998 5 1 QXEA9800621 1 19980424 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 SEVERAL OVERHEAD EVACUATION LIGHTS INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998050100792 19980501 00792 EU 1998 5 1 QXEA9800622 1 19980426 A 3350 XB864041 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU INOPERATIVE INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 SEAT FLOOR PROXIMITY EXIT SIGN MISSING AT ROW 8. MAINTENANCE INSTALLED NEW FLOOR PROXIMITY SEAT SIGN AT ROW 8, FUNCTION TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998050100793 19980501 00793 EU 1998 5 1 98FDEA00296 1 19980425 A 3411 STATIC LINE AIRBUS 300 A300F4605R 3930327 EU LEFT DIRTY A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 667FE 771 ABORTED TAKEOFF FOR LOSS OF AIRSPEED INDICATION ON THE CAPTAINS SIDE. ABORTED AT 120 KNOTS. CHECKED NUMBER 1 ADC, BLEW OUT STATIC LINE WITH NITROGEN, PITOT/STATIC CK OK. 2 L 7 2 4F RT A35EU 1998050100794 19980501 00794 NM 1998 5 1 98FDEA00297 1 19980427 A 5315 65208353 FLOORBEAM BOEING 727 727233 138408A NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION (C53-111-01) ON FLOORBEAM LOWER CHORD AT BS 1070, LBL 42, RBL 50, WL 200. *S/D* REPAIRED LOWER CHORD ON FLOO RBEAM BS 1070, LBL 42 TO RBL 50, WL 200 IAW FED-EX SRM 53-10-8, 53-10-1. 2 L 7 3 4F RT A3WE 1998050100795 19980501 00795 NM 1998 5 1 98FDEA00298 1 19980427 A 5315 65163141 FLOORBEAM BOEING 727 727233 138408A NM BS 312 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION (C53-224-01) ON FLOORBEAM AT BS 312, LBL 4, WL 208. *S/D* REPAIRED FLOORBEAM AT BS 312, LBL 4, WL 208 IAW FE D-EX SRM 53-10-8, 53-10-1, BAC DRAWING 65-16314. 2 L 7 3 4F RT A3WE 1998050100796 19980501 00796 NM 1998 5 1 98FDEA00299 1 19980427 A 5320 691541610 SHEAR TIE BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 WHILE WORKING NR0450 FOUND SHEAR TIE AT BS 720, LBL 5 TO RBL 5 BETWEEN 28L AND 28R, WL 138 TO BE CORRODED AND OUT OF LIM ITS. 2 L 7 3 4F RT A3WE 1998050100797 19980501 00797 NE 1998 5 1 98FDEA00302 2 19980420 A 7510 577957 ANTI-ICE DUCT BOEING 727 72725C 138400H NM PWA JT8 JT8D7 52053 NE NR 2 ENGINE BROKEN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 135FE 19853 NR 2 ENGINE LEFT HAND ENGINE INLET ANTI-ICE DUCT BROKEN IN HALF. LOCATED JUST AFT OF ANTI-ICE VALVE. REMOVED AND REPLA CED ANTI-ICE DUCT IAW FED-EX M/M 75-10-00. 2 L 7 3 4F 4 F A3WE E2EA 1998050100798 19980501 00798 NM 1998 5 1 98UAL900144 1 19980411 A 5270 SENSOR ELDEC 834403 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E/E DOOR OUT OF ADJUST A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 659UA 27114 TAKEOFF ABORTED AT 110 KNOTS. *S/D* E AND E COMPARTMENT DOOR WARNING ILLUMINATED. REPLACED AND ADJUSTED E AND E DOOR CLOSED SENSOR S201 PER MM, GROUND OPS CHECKS OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1998050100799 19980501 00799 NM 1998 5 1 98UAL900151 1 19980417 A 2121 FAN ALLIED SIGNA 6066223 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN FAILED A UALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 WP 29 610UA UA00155756 21871 STRONG ELECTRICAL SMELL IN CABIN AND FLIGHT DECK ON APPROACH. LANDED UNDER AMBER ALERT. *S/D* RT CABIN AIR RECIRCULA TION FAN EXPERIENCED BEARING FAILURE. SHOP FINDINGS CONFIRMED FAILURE MODE. NO PRIOR HISTORY. 2 L 7 2 4F 4 F RT A1NM E3NE 1998050100800 19980501 00800 NE 1998 5 1 98UAL900152 2 19980418 A 7530 6A3322 VSV LEVER ARM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J Y M WARNING INDICATION ENGINE STOPPAGE OVER TEMP CR CRUISE 1 WP 29 434UA 492 V10171 ENGINE NR 2 FAILED. ENGINE SEIZED IN FLIGHT, FL 28, MAX EGT AT 790 DEGREES. FLIGHT DIVERTED TO IAD AND LANDED UNDER AM BER ALERT. *S/D* ONE STAGE 3 VSV LEVER ARM FAILED FROM FATIGUE AND CAUSED SUBSEQUENT FAILURE OF STAGE 4 COMPRESSOR BLA DE AND FURTHER DOWNSTREAM DAMAGE. CAUSE OF VSV LEVER ARM FATIGUE FAILURE IS STILL UNDER INVESTIGATION. INSTRUMENTED EN GINE TESTING IS SCHEDULED TO BEGIN IN LATE OCTOBER 1998. 2 L 7 2 4F 4 F RT A28NM E40NE 1998050100801 19980501 00801 NM 1998 5 1 98UAL900153 1 19980421 A 2131 CONTROLLER HAMILTON STA 7638101 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 7275U 21422 UNABLE TO CONTROL CABIN PRESSURE AT 29,000 FEET IN AUTO, MANUAL OR STANDBY. ALTITUDE WARNING HORN SOUNDED. DESCENDED T O 25,000 FEET AND SYSTEM STARTED OPERATING OK. *S/D* REPLACED PRESSURE CONTROLLER. 2 L 7 3 4F 4 F A3WE E2EA 1998050100802 19980501 00802 NM 1998 5 1 98UAL900154 1 19980421 A 3260 INDICATION BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LANDING GEAR MALFUNCTIONED A UALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 29 663UA 27160 AFTER LANDING GEAR EXTENSION, EICAS GEAR DISAGREE AND TAIL SKID WARNINGS. GEAR AND TAIL SKID WARNING LIGHTS ILLUMINATED ON LANDING GEAR INDICATION PANEL BUT HAD ALL GEAR DOWN LIGHTS GREEN. RECYCLED LANDING GEAR AND GOT ALL NORMAL INDICATI ONS WITH NO ABNORMAL EICAS OR GEAR WARNINGS. 2 L 7 2 4F 4 F RT A1NM E24NE 1998050100803 19980501 00803 NM 1998 5 1 98UAL900155 1 19980421 A 7931 332A104122 TUBE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE CRACKED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 202UA 2483 24717 724290 NUMBER TWO ENGINE OIL FILTER BYPASS LIGHT CAME ON. REDUCED THRUST AND LIGHT WENT OUT. *S/D* FOUND NR 2 ENGINE OIL PRE SSURE LINE GOING TO OIL FILTER DIFFERENTIAL PRESSURE SWITCH, CRACKED. REPLACED LINE, OPS CHECK OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998050100804 19980501 00804 NM 1998 5 1 98UAL900156 1 19980422 A 5240 RESERVOIR BOEING 143N61003 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 2L BLOWN A UALA K NONE W INADEQUATE Q C NR NOT REPORTED 1 WP 29 515UA 24840 DOOR 2L HARD TO OPEN ON ARRIVAL AT GATE. *S/D* FOUND 2L DOOR OUT OF SEQUENCE AFTER DOOR OPENED PARTIALLY FROM OUTSIDE WHILE STILL ARMED. FOUND EMERGENCY POWER RESERVOIR BLOWN. REPLACED RESERVOIR AND RESEQUENCED DOOR, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998050100805 19980501 00805 NM 1998 5 1 98UAL900157 1 19980419 A 5312 BULKHEAD SEAL BOEING 10327431 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE PRESS BLKHD FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 348UA 24252 UNABLE TO MAINTAIN CABIN PRESSURIZATION. OUTFLOW VALVE INDICATED FULL CLOSED IN THE AUTO MODE. *S/D* ACCOMPLISHED FUS ELAGE LEAK CHECK AND FOUND THAT THE FLEXIBLE PRESSURE SEAL AT THE PRESSURE BULKHEAD HAD BLOWN. THE FLEXIBLE RUBBER BOOT WAS REPLACED. PRESSURIZATION WAS NORMAL AFTER THE BOOT REPLACEMENT. 2 L 7 2 4F 4 F RT A16WE E2GL 1998050100806 19980501 00806 NM 1998 5 1 98UAL900158 1 19980423 A 2797 WIRE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 LE SLAT FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 375UA 24640 NUMBER TWO LEADING EDGE SLAT INTRANSIT LIGHT ILLUMINATED ON OVERHEAD AND INTRANSIT ON FORWARD PANEL. *S/D* THE NR 2 SL AT LOCK SWITCH AND ASSOCIATED WIRING WERE CHECKED FOR AN INTERMITTENT OPEN. BOTH THE SWITCH AND THE WIRE CHECKED GOOD. THEY WERE PREVIOUSLY REPLACED ON APRIL 16,1998. ALL THE OTHER WIRES AND SLAT LOCK SWITCHES WERE CHECKED FOR INTERMITTE NT OPENS. AN INTERMITTENT OPEN WAS FOUND AT THE CONDUIT ON THE NR 1 SLAT LOCK SWITCH WIRING. THE WIRE WILL BE REPLACED . 2 L 7 2 4F 4 F RT A16WE E2GL 1998050100807 19980501 00807 WP 1998 5 1 ABXA9800403 1 19980423 A 3260 32802651 TARGET DOUG DOUG DC8 DC862 3021970 WP RT MLG WW OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 804AX 45987 GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH THE GEAR UP, RIGHT GEAR DOOR INDICATED 'NOT LATCHED'. CYCLED GEAR TWICE, NO CHANGE. ACCOMPLISHED ALTERNATE UPLATCH PROCEDURES. LIGHTS REMAINED ON THROUGHOUT FLIGHT. ADJUSTED RIGHT MAIN LANDING GEAR DOOR SENSOR TARGET STOP IAW DC8 MM 32-60-00, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998050100808 19980501 00808 WP 1998 5 1 ABXA9800404 1 19980424 A 3260 H141003 SWITCH DOUG DC8 DC863 302198A WP LT MLG CORRODED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 DURING GEAR UPLATCH CHECK, LEFT MAIN GEAR LIGHT ILLUMINATED WITH RED GEAR UNSAFE LIGHT. REPLACED LEFT MAIN LANDING GEAR DOWNLOCK SWITCH IAW DC8 MM 32-60-0. ALL INDICATIONS NORMAL. 2 L 7 4 4F 4A25 1998050100809 19980501 00809 WP 1998 5 1 ABXA9800405 1 19980422 A 5250 AR25291GR41 LATCH DOUG DC9 DC914 3022034 WP COCKPIT DOOR LOOSE A ABXA K NONE O OTHER CR CRUISE 1 GL 23 925AX 45728 COCKPIT DOOR EXTREMELY DIFFICULT TO OPEN FROM CABIN. TIGHTENED DOOR HANDLE/LATCH ASSEMBLY, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998050100810 19980501 00810 WP 1998 5 1 ABXA9800406 1 19980426 A 3260 H141005 SWITCH DOUG DC9 DC941 302207N WP NLG DEFECTIVE A ABXA L ABORTED APPROACH P NO WARNING INDICATION DE DESCENT 1 GL 23 977AX 47513 NOSE GEAR UNSAFE LIGHT FAILED TO ILLUMINATE WITH THROTTLES AT IDLE AND GEAR IN THE UP POSITION. REPLACED NOSE LANDING G EAR UP AND DOWN LIMIT SWITCHES. 2 L 7 2 4F A6WE 1998050100811 19980501 00811 WP 1998 5 1 ABXA9800407 1 19980427 A 5610 5613217507 WINDOW DOUG DC9 DC933F 302207A WP LT COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. ADJUSTED FORWARD WINDOW AFT ADJUSTMENT ON CAPTAIN'S CLEARVIEW WINDOW. 2 L 7 2 4F A6WE 1998050100812 19980501 00812 WP 1998 5 1 CKSA98266 1 19980420 A 5313 STRINGER DOUG DC8 DC863F 302198F WP BS 1700 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. STRINGER 26 POSSIBLE INDICATION OF CRACK. COMPLIED WITH HFEC INSPECTION, DETERMINED CRACK TO RUN FWD TO APPROX .0625 FROM 2ND FASTENER. FITTING CRACKED DUE TO CORROSION STRESS AT B OLT ATTACH POINT. REMOVED CRACKED STR FITTING S26R IAW DC-8 SRM 51-1-21. DRILLED NEW FITTING IAW DC-8 SRM 51-1-21. IN STALLED STRINGER FITTING IAW DC-8 SRM 51-1-21. CORROSION TASK CARD NUMBER 5600-0551. NON-ROUTINE TASK CARD NUMBER 2328 5. 2 L 7 4 4F 4A25 1998050100813 19980501 00813 WP 1998 5 1 CKSA98267 1 19980420 A 5313 STRINGER DOUG DC8 DC863F 302198F WP BS 1700 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 811CK 46147 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS 1700 STRINGER 29R CRACKED AT END. STRESS CRACK (CORROSION) .0625 TO END OF STRINGER 29R FROM LAST FASTENER. REPAIRED STRINGER IAW EDR NO D805818 AND AIA/E/2808 DTD APRIL 18, 1998 . CORROSION TASK CARD NUMBER 5600-0551. NON-ROUTINE TASK CARD NUMBER 23341. 2 L 7 4 4F 4A25 1998050200001 19980502 00001 WP 1998 5 2 IH981432001 1 19980417 A 3260 801801 SWITCH DOUG DC9 DC931 3022065 WP NLG FAILED B IH3R B EMER. DESCENT N FALSE WARNING AP APPROACH 1 WP 07 212ME 47701 DURING EVALUATION FLIGHT THERE WAS A NOSE GEAR UNSAFE INDICATION AFTER LANDING GEAR EXTENSION. REMOVED AND REPLACED NOS E LANDING GEAR DOWNLOCK SWITCH, OPS CHECK NORMAL. 2 L 7 2 4F A6WE 1998050200006 19980502 00006 WP 1998 5 2 VJ9800132 1 19980408 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 1074 CRACKED A VJ6A O OTHER O OTHER IN INSP/MAINT 1 SO 11 917VV 47323 CRACK FOUND EMANATING APPROX .25 INCH BOTH SIDES OF FASTENER HOLE CANTED BULKHEAD AT FS 1074, L3. FABRICATED AND INSTAL LED REPAIR DOUBLERS IAW AEROCORP RES-1 04577 AND DC9 SRM 51-10-04, 51-10-03 AND MM 53-10-0, FIG 811. 2 L 7 2 4F A6WE 1998050200007 19980502 00007 EU 1998 5 2 AALA980552 1 19980322 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1470K 11506 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING WOULD NOT ILLUMINATE. REPLACED EMERG ENCY EXIT FLOOR PATH LIGHTING CONNECTOR AT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998050200008 19980502 00008 EU 1998 5 2 RAIA980312 1 19980318 A 3320 BL10072001 SOCKET JETAIR JETSTM JETSTM4101 1500501 EU CABIN SHORTED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 574HK 41093 FLT 7144 - STL - CREW REPORTED SMOKE IN PASSENGER CABIN. MAINTENANCE INSPECTED AND FOUND OVERHEAD LIGHT SOCKET SHORTED AT SEAT 4A. MAINTENANCE REPLACED LIGHT SOCKET ASSEMBLY AT SEAT 4A. (M) 2 L 7 2 4T RT A41NM 1998050600001 19980506 00001 EU 1998 5 6 AALA980567 1 19980320 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 TUL - FOUND CORROSION ON STRINGER 55L BETWEEN FRAME 58 AND 64. REMOVED AND REPLACED STRINGER 55L BETWEEN FRAME 58 AND 6 4 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998050600004 19980506 00004 NM 1998 5 6 UPS98426477 1 19980423 A 5210 DOOR BOEING 747 747123 1384873 NM CABIN DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-N/A, R-4 ENTRY DOOR LOWER FWD CORNER SEPARATED FROM A/C. REMOVED AND REPLACED R4 ENTRY DOOR IAW MM 52-1 1-01. 2 L 7 4 4F A20WE 1998050600009 19980506 00009 NM 1998 5 6 CALA9800690 1 19980423 A 2910 LINE BOEING 737 737222 1384473 NM NR 5 LE SLAT LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 10236 19937 THE B SYSTEM HYDRAULIC QUANTITY DECREASED TO 1.8 GALLONS IN FLIGHT AND WAS ACCOMPANIED BY ILLUMINATION OF THE B SYSTEM L OW QUANTITY LIGHT. THE ABNORMAL CHECKLIST WAS ACCOMPLISHED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 5 LEADING EDGE SLAT ACTUATOR LINE LEAKING. THE LINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1998050600010 19980506 00010 SO 1998 5 6 SWIA971158 1 19980401 A 3230 12025262501 RELAY BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 189SW 120048 LANDING GEAR WILL NOT RETRACT WHEN GEAR HANDLE IS MOVED TO UP POSITION. CYCLED HANDLE SEVERAL TIMES WITH SAME RESULTS. RETURNED TO EKO. FERRIED TO SLC. REMOVED AND REPLACED RELAY BOX. OPS CHECKS OF GEAR WAS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998050600011 19980506 00011 SO 1998 5 6 SWIA971159 1 19980404 A 3260 PROX SENSOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LANDING GEAR MALFUNCTIONED A SWIA O OTHER P NO WARNING INDICATION DE DESCENT 1 NM 07 186SW 120034 LEFT MAIN LANDING GEAR DOES NOT INDICATE GREEN WHEN SELECTED DOWN. REPAIRED LEFT A SYSTEM DOWN LOCK PROX SENSOR IAW MM 32-61-01. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998050600012 19980506 00012 WP 1998 5 6 ABXA9800386 1 19980416 A 5320 3750330523 SPLICE DOUG DOUG DC8 DC862 3021970 WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STRINGER 26R SPLICE BETWEEN STATION 600 AND STATION 620 IS CRACKED. REPLACED STRINGER SPLICE IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998050800018 19980508 00018 EU 1998 5 8 MALA976109 1 19980427 A 3350 MS1557081 BULB SAAB SF340 340B 7860101 EU FUSELAGE FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 403XJ 340B403 DURING INSPECTION, LEFT EXTERNAL EMERGENCY LIGHT INOP. MAINTENANCE RELAMPED. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998050800019 19980508 00019 EU 1998 5 8 MALA976110 1 19980426 A 2613 HOT LIGHT SAAB SF340 SF340A 7850100 EU LT TAIL PIPE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 27XJ 027 AFTER DEPARTURE, THE LEFT TAIL PIPE HOT LIGHT ILLUMINATED. CREW PERFORMED QRH, LIGHT EXTINGUISHED WITH REDUCED POWER, L IGHT ILLUMINATED AT 5000 FEET, 83 PERCENT TORQUE, AND ITT'S NORMAL. AIRCRAFT RETURNED TO SCE. MAINTENANCE INSPECTED S YSTEM FOR DEFECTS, NONE FOUND, OBSERVED CREW WHILE PERFORMING RUNS AND SYSTEM CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998050800020 19980508 00020 NM 1998 5 8 CALA9800702 1 19980427 A 2910 HYD LINES BOEING 737 737130 1384435 NM LT ELEV PCU PUNCTURED A CALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 09 14208 19025 THE A SYSTEM HYDRAULIC FLUID LEVEL DROPPED TO ZERO WHILE ON DESCENT INTO PHL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MA INTENANCE FOUND TWO HYDRAULIC FLEX LINES AT LT ELEVATOR PCU PUNCTURED. THE FLEX LINES WERE REMOVED AND REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1998050800021 19980508 00021 NM 1998 5 8 CALA9800703 1 19980427 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1166, RBL 16. THE CORRODED AREA WAS CUT OUT. A CHANNEL AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800022 19980508 00022 NM 1998 5 8 CALA9800704 1 19980427 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT LBL 12 AND LBL 4, STA 1166. THE CORRODED SECTIONS OF FLOOR SUPPORT WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-30-5, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800023 19980508 00023 NM 1998 5 8 CALA9800705 1 19980427 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND A 5 CRACK WITH CORROSION IN INTERCOSTAL FOOT BETWEEN STRINGERS 29R AND 28R AT STA 950E. THE CRACKED AN D CORRODED AREA WAS CUT OFF IAW SRM 53-10-4. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-10-2, 51-30-2, A ND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800024 19980508 00024 NM 1998 5 8 CALA9800706 1 19980427 A 5320 CLIP BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND STRINGER TIE CLIP CORRODED AT FS 950E. THE CLIP WAS REMOVED AND A NEW CLIP WAS FABRICATED AND INSTALLE D IAW SRM 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800025 19980508 00025 NM 1998 5 8 CALA9800707 1 19980427 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 535 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND FLOOR SUPPORTS AT RBL 2 AND LBL 2, STA 535 CORRODED. THE CORRODED AREAS WERE CUT OUT. REPAIR ANGLES W ERE FABRICATED AND INSTALLED IAW SRM 51-40-36, 51-10-2, 51-30-2, 51-40-3, FIGURE 1, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800026 19980508 00026 NM 1998 5 8 CALA9800708 1 19980427 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 535 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT RBL 8 AND LBL 13, STA 535. THE CORRODED AREAS WERE CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800027 19980508 00027 NM 1998 5 8 CALA9800709 1 19980427 A 5320 FLOOR SUPPORT BOEING 727 727224 1384076 NM STA 680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND A 10.75 CRACK IN FLOOR SUPPORT AT STA 680, RBL 24. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICA TED AND INSTALLED IAW SRM 51-40-4, FIGURE 1, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800028 19980508 00028 NM 1998 5 8 CALA9800710 1 19980427 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 485 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND A 6.5 CRACK IN FLOOR SUPPORT AT STA 485, LBL 12. THE CRACKED SECTION WAS CUT OUT. A REPAIR WAS FABRIC ATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800029 19980508 00029 WP 1998 5 8 CALA9800711 1 19980427 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 240 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 INSPECTION FOUND A DENT IN FUSELAGE SKIN AT STA 240 BETWEEN LONGERON 17 AND 18L. A REPAIR WAS INSTALLED IAW ECRA 5330-0 2445. 2 L 7 2 4F A6WE 1998050800030 19980508 00030 NM 1998 5 8 CALA9800712 1 19980428 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND STRINGER 28L AND STRINGER TIE CORRODED AT FS 950. THE STRINGER TIE AND CORRODED END OF STRINGER WERE R EMOVED. REPAIR WAS INSTALLED IAW SRM 51-10-2, 53-10-3, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800031 19980508 00031 NM 1998 5 8 CALA9800713 1 19980428 A 5320 CHORD BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 INSPECTION FOUND LOWER RT T-CHORD CORRODED AT FS 950. THE CHORD WAS REMOVED. A NEW CHORD WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, PAGE 4, PARAGRAPH 4 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998050800032 19980508 00032 WP 1998 5 8 9807371225 1 19980311 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 568-587 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING M CHECK, FOUND CORRODED LONGERON IN THE NR 1 AC COMPARTMENT AT THE EXHAUST FS 568-587. REPAIRED PER EA 12-155546 . 2 L 7 3 4F A22WE 1998050800033 19980508 00033 WP 1998 5 8 9807389605 1 19980416 A 5312 BULKHEAD DOUBLER DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 605NW 47223 DURING LINE CHECK, FOUND A CRACK IN THE AFT PRESSURE BULKHEAD -13 DOUBLER ABOVE THE LEFT DOOR STOP FITTING. REPAIRED PE R EA 96-156476. 2 L 7 2 4F A6WE 1998050800034 19980508 00034 NM 1998 5 8 9807396718 1 19980403 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM BS 500 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND A CRACK IN 2 UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLES AT THE FUSELAGE FRAME FS 500, RIGHT SIDE. REPAIRED PER EA 67-121410. 2 L 7 4 4F A20WE 1998050800035 19980508 00035 NM 1998 5 8 9807406718 1 19980403 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM BS 380 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND A CRACK IN A UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLE AT THE FUSELAGE FRAME FS 380, R IGHT SIDE. REPAIRED PER EA 67-121410. 2 L 7 4 4F A20WE 1998050800036 19980508 00036 NM 1998 5 8 9807416718 1 19980403 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM BS 340 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND A CRACK IN 2 UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLES AT THE FUSELAGE FRAME FS 340, LEFT SIDE. REPAIRED PER EA 67-121410. 2 L 7 4 4F A20WE 1998050800037 19980508 00037 NM 1998 5 8 9807426718 1 19980403 A 5315 FLOORBEAM BOEING 747 747251F 1384898 NM BS 360 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 618US 21122 DURING PERIODIC CHECK, FOUND A CRACK IN A UPPER DECK FLOORBEAM UPPER CHORD FASTENER HOLE AT THE FUSELAGE FRAME FS 360, R IGHT SIDE. REPAIRED PER EA 67-121410. 2 L 7 4 4F A20WE 1998050800038 19980508 00038 WP 1998 5 8 9807449933 1 19980314 A 5312 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 37 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING M CHECK, FOUND A CRACK IN THE WEB OF THE FS 37 BULKHEAD AS VIEWED THROUGH ACCESS HOLE ABOVE THE LEFT UPPER RADOME GUIDE PIN HOLE. REPAIRED PER EA 99-154843. 2 L 7 2 4F A6WE 1998050800039 19980508 00039 WP 1998 5 8 9807459941 1 19980314 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 321 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3324L 47103 DURING M CHECK, FOUND CRACK IN FLOORBEAM UPPER FLANGE AT FS 321 JUST OUTBOARD OF CENTERLINE. REPAIRED PER EA 99-154774. 2 L 7 2 4F A6WE 1998050800040 19980508 00040 WP 1998 5 8 9807469956 1 19980407 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 560 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 923RW 47183 DURING M-CHECK, FOUND CORROSION ON FRAME AT AFT LOWER HANDLE FS 560, LONGERON 19R. REPAIRED PER EA 99-154790. 2 L 7 2 4F A6WE 1998050800041 19980508 00041 WP 1998 5 8 9807471225 1 19980320 A 5320 WEB DOUG DC10 DC1030 3023501 WP RT MLG WW CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 225NW 46582 DURING M CHECK, FOUND CRACK IN AFT WEB IN THE RIGHT WHEEL WELL. REPAIRED PER EA 12-156163. 2 L 7 3 4F A22WE 1998050800042 19980508 00042 WP 1998 5 8 9807481152 1 19980311 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1801-1821 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 152US 46761 DURING L CHECK, FOUND CORROSION ON EXTERIOR SKIN AT FASTENERS FS 1801-1821, LONGERON 43R. REPAIRED PER EA 11-155549. 2 L 7 3 4F A22WE 1998050800043 19980508 00043 NM 1998 5 8 9807496612 1 19980117 A 5320 FORGING BOEING 747 747251B 1384892 NM BS 2060-2080 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M CHECK, FOUND CORROSION ON WINDOW FORGING LEFT FS 2060-2080, STR 18L. REPLACED FORGING PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998050800044 19980508 00044 NM 1998 5 8 9807506612 1 19980127 A 5320 FORGING BOEING 747 747251B 1384892 NM BS 2140 2160 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M CHECK, FOUND CORROSION ON WINDOW FORGING LEFT FS 2140-2160, STR 22L. REPLACED FORGING PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998050800045 19980508 00045 NM 1998 5 8 9807546612 1 19980127 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M CHECK, FOUND CORROSION ON AFT END FITTINGS FOR STR 26L, 36L, 38L, 40L, 42L, 44L, 46L, 48L, 49L, 50L, AND 51L AT FS 2360. REPLACED FITTINGS PER DWG 65B02697 AND 65B02699. 2 L 7 4 4F A20WE 1998050800046 19980508 00046 NM 1998 5 8 9807536612 1 19980127 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M CHECK, FOUND CORROSION ON THE FORWARD FITTINGS FOR STR 26L, 36L, 40L, 42L, 44L, 46L, 49L, 50L, 51 AT FS 2360. R EPLACED FITTINGS PER DWG 65B04159, 65B04160, AND 65B04161. 2 L 7 4 4F A20WE 1998050800047 19980508 00047 NM 1998 5 8 9807516612 1 19980127 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M CHECK, FOUND CORROSION ON THE FORWARD FITTINGS FOR STR 26R, 36R, 38R, 40R, 42R, 44R, AND 46R AT FS 2360. REPLA CED FITTINGS PER DWG 65B04160. 2 L 7 4 4F A20WE 1998050800048 19980508 00048 NM 1998 5 8 9807526612 1 19980127 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M CHECK, FOUND CORROSION ON THE AFT FITTINGS FOR STR 26R, 36R, 38R, 40R, 42R, 44R, 46R, 48R, 49R, 50R, AND 51R AT FS 2360. REPLACED FITTINGS PER DWG 65B02697 AND 65B02699. 2 L 7 4 4F A20WE 1998050800049 19980508 00049 WP 1998 5 8 9807559996 1 19980408 A 5330 SKIN DOUG DC9 DC931 3022065 WP CARGO DOORWAY CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE UPPER FORWARD CORNER OF THE FORWARD CARGO DOOR CUTOUT. REPAIR ED PER EA 99-123570. 2 L 7 2 4F A6WE 1998050800050 19980508 00050 WP 1998 5 8 9807569996 1 19980417 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 579 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M CHECK, FOUND CORROSION ON AFT SIDE OF FS 579 FRAME AT LONGERON 17L. REPAIRED PER EA 99-156478. 2 L 7 2 4F A6WE 1998050800051 19980508 00051 WP 1998 5 8 9807579996 1 19980303 A 5312 BULKHEAD CHORD DOUG DC9 DC931 3022065 WP BS 110 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M CHECK, FOUND CORROSION ON UPPER SURFACE OF LOWER FORWARD FLANGE OF FS 110 BULKHEAD T CHORD OUTBOARD OF RIGHT TR UNNION SUPPORT BEAM IN THE NOSE LANDING GEAR WHEEL WELL. REPAIRED PER EA 99-156582. 2 L 7 2 4F A6WE 1998050800052 19980508 00052 NM 1998 5 8 9807586608 1 19980309 A 5313 LONGERON BOEING 747 747151 1384891 NM BS 1941-1944 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 608US 19785 DURING PERIODIC CHECK, FOUND CORROSION OF STR 37L FROM FS 1941-1944. REPAIRED PER EA 66-155605. 2 L 7 4 4F A20WE 1998050800053 19980508 00053 WP 1998 5 8 9807439933 1 19980314 A 5312 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 37 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING M CHECK, FOUND CRACK IN THE WEB OF FS 37 BULKHEAD AS VIEWED THROUGH THE ACCESS HOLE ABOVE THE RIGHT UPPER RADOME GUIDE PIN. REPAIRED PER EA 99-154843. 2 L 7 2 4F A6WE 1998050800054 19980508 00054 EA 1998 5 8 COMA9860090 1 19980427 A 2750 7805013 SELECTOR LEVER CNDAIR CL600 CL6002B19 EA COCKPIT FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 973CA 1120 7146 DURING APPROACH INTO MCO, FLAP CAUTION WARNING ACTIVATED AT 8 DEGREE FLAP SETTING. REPLACED THE FLAP SELECTOR LEVER ASS EMBLY. 2 L 7 2 4F RT A21EA 1998050800055 19980508 00055 EU 1998 5 8 WWMA9800080 1 19980417 A 3350 5225280527 PANEL SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 350CF 340B350 FLIGHT 3235, LAX, EMERGENCY ARM LIGHT ON F/A'S PANEL INOP. REPLACED FLT ATT PANEL. 2 L 7 2 4T RT A52EU 1998050800056 19980508 00056 EU 1998 5 8 WWMA9800079 1 19980417 A 3350 LAMP SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 348SB 340B348 FLIGHT 3319, LAX, AFT FLOOR PROXIMITY EMERG LIGHT INOP. REINSTALLED LAMP ON FLOOR EMERGENCY LIGHT AT SEATS 12BC. 2 L 7 2 4T RT A52EU 1998050800057 19980508 00057 NM 1998 5 8 QXEA9800619 1 19980424 A 5210 85210200103 GUIDE STOP DHAV 85210192005 DHAV DHC8 DHC8202 2809007 NM CABIN DOOR MALFUNCTION A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 351PH 490 BOI- MAIN CABIN DOOR EXTERIOR RELEASE HANDLE RECESSES TOO FAR INTO THE INDENT. CAN NOT OPEN MAIN CABIN DOOR FROM THE OU TSIDE. REMOVED AND REPLACED THE EXTERIOR DOOR HANDLE BUMPER UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVI CE. 2 H 7 2 4T RT A13NM 1998050800058 19980508 00058 NM 1998 5 8 QXEA9800623 1 19980427 A 6120 78249017 CONTROL UNIT DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE MALFUNCTION A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 824PH 7240 7240 157 SEA - WHILE TAXIING TO PARKING, THE NR 2 ENGINE FEATHERED, THEN CAME OUT OF FEATHER WITHOUT ANY INPUT FROM THE CREW. TH E POWER LEVER WAS SLIGHTLY AFT OF THE FLIGHT IDLE GATE. THE CONDITION LEVER WAS AT MIN. REPLACED NR 2 PROPELLER CONTRO L UNIT (PCU). RIGGED PCU AND PERFORMED ENGINE RUN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998050800059 19980508 00059 1998 5 8 98FDEA00300 4 19980428 A 3417 4045053903 ADC AIRBUS 300 A300F4605R 3930327 EU NR 1 MALFUNCTION A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 667FE 771 98-0107 - WRI 34-14-2231:CAPTAINS PFD DISPLAY HAS NO AIRSPEED INDICATION DURING TAKEOFF ROLL. T/O ABORTED. ALL OTHER A IRSPEED INDICATORS WERE NORMAL. REMOVED AND REPLACED THE NR 1 ADC. SWAPPED NR 1 AND NR 3 EFIS SGU'S. A/C DOWNGRADED T O CHECK CAT 2. NR 3 EFIS SGU DEFERRED PER DMI 34-7. 2 L 7 2 4F RT A35EU 1998050800060 19980508 00060 EU 1998 5 8 98FDEA00301 1 19980428 A 3411 PITOT TUBE AIRBUS 300 A300F4605R 3930327 EU LEFT MALFUNCTION A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 667FE 771 98-0108 - WRI 34-14-02232: CAPTAINS PFD AIRSPEED INDICATOR DOES NOT OPERATE. NO INDICATION ON T/O ROLL. TAKEOFF ABORTE D. REMOVED AND REPLACED CAPTAINS PITOT TUBE, PITOT LEAK CHECK OK. NR 3 EFIS CONTROL SYS OK. CLEARED MEL 34-7. 2 L 7 2 4F RT A35EU 1998050800061 19980508 00061 WP 1998 5 8 ABXA9800408 1 19980428 A 7120 37707451 MOUNT DOUG DC8 DC863F 302198F WP NR 3 ENGINE SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 DURING C-CHECK, FOUND NR 3 ENGINE REAR INBOARD MOUNT ARM SHEARED AT THREADED PORTION. *S/D* REPLACED NR 3 LEFT AFT ENG INE MOUNT IAW DC8 MM 71-20-02. 2 L 7 4 4F 4A25 1998050800062 19980508 00062 WP 1998 5 8 DLL19980890 1 19980426 A 3350 LIGHT 1008951 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 193H1216 FIRST CLASS RT SIDE INBD OF R1 DOOR EMER EXIT AISLE LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A23WE 1998050800063 19980508 00063 NM 1998 5 8 DL72S980891 1 19980426 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM LT WING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 21074 LEFT WING EMERGENCY LIGHT DID NOT ILLUMINATE ON TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998050800064 19980508 00064 NM 1998 5 8 DLM88980892 1 19980426 A 2410 CSD DOUG MD88 MD88 3023688 NM LT ENGINE FAILED A DALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION AP APPROACH 1 SO 27 925DL UH60481281 49712 ON FINAL GOT L GEN OFF AND A/C X-TIE LOCKOUT. REPLACED LT CSD AND GEN PERF ELECTICAL SYS CHK, PER PFHB. CROSS TIE OPN NORMAL. 2 L 7 2 4F RT A6WE 1998050800065 19980508 00065 NM 1998 5 8 DL76L980893 1 19980427 A 5754 WEDGE BOEING 767 767332 1382001 NM NR 1 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 173DN 24800 WING, NR1 LEADING EDGE SLAT, TRAILING EDGE WEDGE. DELAMINATION REPAIR A 1.5 BY 1.2 AREA OF DELAMINATION WAS FOUND ON TH E UPPER SURFACE OF THE TRAILING EDGE WEDGE ON THE NR 1 SLAT. THE DELAMINATION WAS REPAIRED PER THE B676 SRM 57-43-0 2 AND DOCUMENTED PER ER/A 364635-14AD. 2 L 7 2 4F RT A1NM 1998050800066 19980508 00066 NM 1998 5 8 DL72K980894 1 19980426 A 5320 65562313 BEAR STRAP BOEING 727 727232 1384082 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FUSELAGE/SKIN ASSY, R1 DOOR SURROUND DOUBLER, UPPER HINGE CUTOU. REPAIR FOR CRACK IN REINFORCING DOUBLER. THE R1 DOOR SURROUND REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK IN THE UPPER HINGE CUTOUT. THE CRACK WAS IDEN TIFIED AS BEING IN REGION 'E' PER BAC S/B 727-53-0136. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DOUBLER PER S/B 727 -53-0136 AND ER/A 364614-14, REV A. 2 L 7 3 4F A3WE 1998050800067 19980508 00067 NM 1998 5 8 DL76S980895 1 19980424 A 5330 SKIN BOEING 767 767332 1382001 NM BS 450 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 FUSELAGE/SKIN, FS 434-500, STRG 32R-38R, SKIN SPLICE REPAIR. THE FUSELAGE SKIN BETWEEN FS 434 AND 500 AND BETWEEN STRIN GERS 32R AND 38R WAS BADLY DENTED OR TORN FROM A GROUND EQUIPMENT IMPACT. THE DAMAGED SECTION OF SKIN WAS TRIMMED AWAY AND A NEW SECTION OF SKIN WAS SPLICED IN PER ER/A 364572-14, REV B. 2 L 7 2 4F RT A1NM 1998050800068 19980508 00068 WP 1998 5 8 DLL10980896 1 19980424 A 5711 1527095429 SPAR WEB LKHEED 1011 10113851 5265010 WP WS 77 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 WING LT, REAR SPAR WEB, OWS 77 LOWER CAP ATTACHMENT, REPAIR FOR WEB CRACK. THE LT WING REAR SPAR WEB WAS FOUND WITH A . 50 LONG CRACK EMANATING FROM A FASTENER HOLE ATTACHING THE WEB TO THE LOWER SPAR CAP AT OWS 77. THE WEB CRACK WAS ROUT ED OUT AND AN ALUMINUM DOUBLER AND TRIPLER INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 364580-14, REV A. 2 L 7 3 4F A23WE 1998050800069 19980508 00069 NM 1998 5 8 DLM88980897 1 19980426 A 2750 LINKAGE 59359731 DOUG MD88 MD88 3023688 NM LT TE FLAP BROKEN A DALA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SO 27 959DL 49978 LEFT INBOARD FLAP I/B ACTUATOR LINKAGE ARM AND WELD ASSY BROKE ON GEAR DOOR. REPLACED ARM AND WELD ASSY. INSPECTED W/ W AND OPERATED FLAPS SEVERAL TIMESM, OPS CKS NORMAL. 2 L 7 2 4F RT A6WE 1998050800070 19980508 00070 NM 1998 5 8 DL72K980898 1 19980420 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FOUND ON MV2 CORROSION VISIT, NR 1 L/E FLAP ACTUATOR INBD ATTACH BRACKET CRACKED, UPPER AND LOWER CORNERS. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998050800071 19980508 00071 NM 1998 5 8 DL72K980899 1 19980420 A 2782 BRACKET BOEING 727 727232 1384082 NM LT LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998050800072 19980508 00072 NM 1998 5 8 DL72K980900 1 19980420 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FOUND ON MV2 CORROSION VISIT, NR 2 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED, LOWER END. REPAIRED PER 57-20-21. 2 L 7 3 4F A3WE 1998050800073 19980508 00073 NM 1998 5 8 DL72K980902 1 19980420 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FOUND ON MV2 CORROSION VISIT, 1 VISABLE CRACK STR 18A RT, AFT OF STA 940 FITTING UPPER AFT ATTACH BOLT. REPAIRED PER M/ M 53-12-0. 2 L 7 3 4F A3WE 1998050800074 19980508 00074 NM 1998 5 8 DL72S980903 1 19980427 A 2780 BRACKET BOEING 727 727225 1384077 NM NR 8 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 1 INCH CRACK NR 8 SLAT INBD MOUNT BRKT. REPAIRED PER M/M 57-20-21 P. 812. 2 L 7 3 4F A3WE 1998050800075 19980508 00075 NM 1998 5 8 DLM88980904 1 19980407 A 3350 BULB DOUG MD88 MD88 3023688 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DE 49997 EMERGENCY TRACK WHITE LIGHT AT 21 ED MISSING. REPLACED MISSING BULB AND LENS CHECKS FINE. 2 L 7 2 4F RT A6WE 1998050800076 19980508 00076 NM 1998 5 8 DLM88980905 1 19980427 A 3350 SOCKET DOUG MD88 MD88 3023688 NM EXTERIOR CORRODED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DE 49997 EXTERIOR EMERGENCY RT OFF WING LIGHT INOP. CLEANED SOCKET CHECKS FINE. 2 L 7 2 4F RT A6WE 1998050800077 19980508 00077 NM 1998 5 8 DL757980906 1 19980427 A 5210 SCREW BOEING 757 757232 1384965 NM R2 DOOR HANDLE SHEARED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 622DL 22912 R2 DOOR WOULD NOT ARM. REPLACD SHEARED SCREW ON OUTSIDE DOOR HANDLE. 2 L 7 2 4F RT A2NM 1998050800078 19980508 00078 NM 1998 5 8 DL76S980907 1 19980428 A 5315 FLOORBEAM BOEING 767 767332 1382001 NM BS 610 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 131DN 24852 STA 610 FLOORBEAM WAS FOUND WITH DAMAGE TO THE LWR CHORD AND WEB BETWEEN APPROX LBL14 AND RBL 13. THE DAMAGE APPEARS TO HAVE BEEN CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 331621-14. 2 L 7 2 4F RT A1NM 1998050800079 19980508 00079 NM 1998 5 8 DLM88980908 1 19980428 A 5330 5953050 SKIN DOUG MD88 MD88 3023688 NM BS 235 CREASED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 989DL 53341 THE FUSELAGE SKIN AFT OF THE L1 DOOR WAS FOUND WITH A CREASEFROM STA 230 TO 240 BETWEEN L18 AND 19L. REPAIRED PER ERA 3 31647-14. 2 L 7 2 4F RT A6WE 1998050800080 19980508 00080 NM 1998 5 8 DLM88980909 1 19980428 A 5330 5911401 SKIN DOUG MD88 MD88 3023688 NM BS 221 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 989DL 53341 SEVERAL DENTS WERE FOUND IN THE FUSE SKIN AT FS 216 TO 229 BETWEEN L17 AND 18L. REPAIRED PER ERA 331653-14. 2 L 7 2 4F RT A6WE 1998050800081 19980508 00081 NM 1998 5 8 DLM88980910 1 19980428 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 989DL 53341 FS 1418 FRAME WAS CRACKED AT L2R. CRACK WAS APPROX 1 IN LENGTH. REPAIRED PER ERA 331637-14. 2 L 7 2 4F RT A6WE 1998050800082 19980508 00082 NM 1998 5 8 DLM88980911 1 19980428 A 5330 5911401 SKIN DOUG MD88 MD88 3023688 NM BS 219 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 989DL 53341 DENT WAS FOUND AT STA 218 BETWEEN L18L AND L19L. REPAIRED PER ERA 331654-14. 2 L 7 2 4F RT A6WE 1998050800083 19980508 00083 NM 1998 5 8 DL72K980914 1 19980421 A 5320 BEAR STRAP BOEING 727 727232 1384082 NM R1 DOOR CUTOUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 FOUND ON MV2 CORROSION VISIT, CRACK IN EDGE OF BEARSTRAP AT RT FWD SERVICE DOOR UPPER HINGE CUTOUT UPPER FWD CORNER. RE FERENCE SUPPLEMENTAL CARD FOR SI 4-72762-12 ME-02. REPAIRED PER ERA 364614-14 REV A. 2 L 7 3 4F A3WE 1998050800084 19980508 00084 NM 1998 5 8 DHL9872601D 1 19980303 A 5320 ANGLE BOEING 727 727228 NM BS 330 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D-CHECK, CORROSION AT LT MOUNTING FLANGE FOR LOWER FUSELAGE ACCESS PANEL 1104 INTERIOR AND EXTERIOR. CUT OUT DAMAGE D TIE ANGLE SKIN ATTACHMENT. INSTALLED NEW CHORD ANGLE PER SRM 51-10-4. REPLACED TIE ANGLES AT FRAMES BS 330, 320 AND 300 PER SRM 53-10-4, 4 BY 1 BY 5. N/R 3444. 2 L 7 3 4F A3WE 1998050800085 19980508 00085 NM 1998 5 8 DHL9872602D 1 19980302 A 5311 FRAME BOEING 727 727228 NM BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT BS 940 FRAME CRACKED BELOW CABIN FLOOR AT FASTENER HOLE. STOP DRILL CRACK PER S/B 53-190. ACCOMPLISHED REPAIR PER S/B 53-190. N/R 3400. 2 L 7 3 4F A3WE 1998050800086 19980508 00086 NM 1998 5 8 DHL9872603D 1 19980308 A 5720 FAIRING BOEING 727 727228 NM NR 8 FLAP TRACK DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 8 FLAP TRACK FAIRING 10 FROM FWD EDGE INTERM REPAIR. CUT OUT DAMAGED SECTION. INSTALLED DOUBLER REPAIR PER SRM 51-40-2 FILLER 2 BY 1.5, DOUBLER 6 BY 6. N/R 2513. 2 L 7 3 4F A3WE 1998050800087 19980508 00087 NM 1998 5 8 DHL9872604D 1 19980308 A 5720 FAIRING BOEING 727 727228 NM NR 8 FLAP TRACK DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 8 FLAP TRACK FAIRING FORWARD EDGE CENTER SECTION INTERM REPAIR. INSTALLED DOUBLER ON FAIRING PER SRM 51- 40-2 2.5 BY 1, N/R 2514. 2 L 7 3 4F A3WE 1998050800088 19980508 00088 NM 1998 5 8 DHL9872605D 1 19980308 A 5730 SKIN BOEING 727 727228 NM RT WING REPAIRED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT WING O/B FORE FLAP O/B FOLLOW UP LINK CUTOUT HAS INTERM REPAIR. INSTALLED PERMANENT REPAIR PER SRM 57-30 -4, 6 BY 4.5. N/R 2478. 2 L 7 3 4F A3WE 1998050800089 19980508 00089 NM 1998 5 8 DHL9872606D 1 19980308 A 5753 SKIN BOEING 727 727228 NM RT TE FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT WING OUTBD AFT FLAP 40 FROM INBD EDGE LOWER SKIN BULGED. INSTALLED FILLER REPAIR PER SRM 51-40-1. N/R 2 463. 2 L 7 3 4F A3WE 1998050800090 19980508 00090 NM 1998 5 8 DHL9872607D 1 19980304 A 5753 SKIN BOEING 727 727228 NM RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT WING OUTBD AFT FLAP 20 FROM OUTBD EDGE UPPER AND LOWER SKIN EPOXY REPAIR CRACKED AND DETERIORATED. INST ALLED FILLER REPAIR PER SRM 51-40-1. N/R 2461. 2 L 7 3 4F A3WE 1998050800091 19980508 00091 NM 1998 5 8 DHL9872608D 1 19980304 A 5730 SKIN BOEING 727 727228 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT WING TRAILING EDGE LOWER SKIN PANEL DELAMINATED UNDERNEATH NR 13 SPOILER. INSTALLED BONDING REPAIR PER S RM 51-40-5, 23.5 BY 9.5 AT RT T/E LOWER SKIN PANEL. INSTALLED OVERLAY REPAIR PER SRM 51-40-8 AT UPPER SURFACE. N/R 241 3. 2 L 7 3 4F A3WE 1998050800092 19980508 00092 NM 1998 5 8 DHL9872609D 1 19980304 A 5730 SKIN BOEING 727 727228 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT WING TRAILING EDGE LOWER SKIN PANEL DELAMINATED. REMOVED PANEL, INSTALLED BONDING REPAIR PER SRM 51-40-5 . N/R 2400. 2 L 7 3 4F A3WE 1998050800093 19980508 00093 NM 1998 5 8 DHL98726100 1 19980304 A 5730 SKIN BOEING 727 727228 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 11 SPOILER PANEL LOWER SKIN CENTER SECTION DELAMINATED. INSTALLED BONDING REPAIR PER SRM 51-40-6, 34 BY 9.5. N/R 2397. 2 L 7 3 4F A3WE 1998050800094 19980508 00094 NM 1998 5 8 DHL98726101 1 19980306 A 5230 RETAINER BOEING 727 727228 NM NR 2 CARGO DOOR LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 2 AFT CARGO DOOR CUTOUT SEAL RETAINER HAS METAL JOINT PLATE LOOSE. REMOVED AND REPLACED DOUBLER PER SRM 51-40-2. N/R 3673. 2 L 7 3 4F A3WE 1998050800095 19980508 00095 NM 1998 5 8 DHL98726102 1 19980305 A 5320 CLIP BOEING 727 727228 NM BS 460 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CRACKS IN STRINGER TIE CLIP FS 460 STR 5LT. REMOVED AND REPLACED TIE CLIP PER SRM 53-10-1, 4 BY 3. N/R 3 655. 2 L 7 3 4F A3WE 1998050800096 19980508 00096 NM 1998 5 8 DHL98726103 1 19980305 A 5320 CLIP BOEING 727 727228 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, STR TIE CLIP AT STR 2 RT CRACKED, FS 480. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-1. N/R 3652. 2 L 7 3 4F A3WE 1998050800097 19980508 00097 NM 1998 5 8 DHL98726104 1 19980305 A 5311 FRAME BOEING 727 727228 NM BS 540 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, 2 DENT S IN FRAME FS 540, STR 6 R. INSTALLED FRAME REPAIR PER SRM 53-10-4. N/R 3651. 2 L 7 3 4F A3WE 1998050800098 19980508 00098 NM 1998 5 8 DHL98726105 1 19980305 A 5320 WEB BOEING 727 727228 NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD PIT BILGE Z WEB IS CRACKED AT NUTPLATE HOLE JUST FWD OF STA 720C STR 26R. INSTALLED DOUBLER REPAIR PER SRM 51-402, 1.5 BY 3 N/R 3639. 2 L 7 3 4F A3WE 1998050800099 19980508 00099 NM 1998 5 8 DHL98726106 1 19980306 A 5320 STIFFENER BOEING 727 727228 NM BS 920 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CORROSION ON STIFFENER IN LEFT WHEEL BS 920 ABOVE GEAR DOOR. INSTALL ANGLE REPAIR PER SRM 51-40-4, 7.5 LONG . N/R 7300. 2 L 7 3 4F A3WE 1998050800100 19980508 00100 NM 1998 5 8 DHL98726107 1 19980304 A 5314 PANEL BOEING 727 727228 NM KEEL BEAM TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, KEEL BEAM ACCESS PANEL AT APU CUTOUT LOWER SECTION HAS SKIN TORN AT O/B EDGE. REPLACED PANEL PER SRM 51-40- 2, 30 BY 12. N/R 7297. 2 L 7 3 4F A3WE 1998050800101 19980508 00101 NM 1998 5 8 DHL98726108 1 19980304 A 5314 PANEL BOEING 727 727228 NM KEEL BEAM TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, KEEL BEAM ACCESS PANEL AT APU CUTOUT UPPER SECTION HAS TORN EDGE. REPLACED PANEL PER SRM 51-40-2, 35 BY 10. 5. N/R 7269. 2 L 7 3 4F A3WE 1998050800102 19980508 00102 NM 1998 5 8 DHL98726109 1 19980305 A 3213 657276137 STRUT BOEING 727 727228 NM LT MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT MLG SHOCK STRUT THREADS HAVE CORROSION AND PITTING. INSTALLED SERVICABLE STRUT PER MM 32-11-0. N/R 7301 . 2 L 7 3 4F A3WE 1998050800103 19980508 00103 NM 1998 5 8 DHL9872610D 1 19980306 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO FLOOR SUPPORT INTERCOSTAL IS CORRODED ALONG THE UPPER FLANGE FROM BS 1148 TO 1166, LB 24. REPLACE D SUPPORT INTERCOSTAL PER SRM 51-40-4 20 LONG. N/R 3675. 2 L 7 3 4F A3WE 1998050800104 19980508 00104 NM 1998 5 8 DHL98726110 1 19980305 A 3213 657276138 STRUT BOEING 727 727228 NM RT MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT MLG SHOCK STRUT THREADS HAVE CORROSION AND PITTING. INSTALLED SERVICABLE STRUT PER MM 32-11-0. N/R 7302 . 2 L 7 3 4F A3WE 1998050800105 19980508 00105 NM 1998 5 8 DHL98726111 1 19980311 A 3230 65284107 BRACKET BOEING 727 727228 NM RT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT MLG CABLE PULLEY CLUSTER AT AFT OUTBD SIDE OF RT WW CRACKED. REMOVED AND REPLACED CRACKED BRACKET PER M M 20-20-4. N/R 7304. 2 L 7 3 4F A3WE 1998050800106 19980508 00106 NM 1998 5 8 DHL98726112 1 19980302 A 5330 SKIN BOEING 727 727228 NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NUMEROUS RIVETS WORKING LOOSE LT LOWER WING TRAILING EDGE AT ACCESS PANEL JUST OUTBD OF NR 4 TRAILING EDGE T RACK. REMOVED AND REPLACED NEW SKIN AT WING T/E ACCESS PANEL PER SRM 51-40-6, N/R 1334. 2 L 7 3 4F A3WE 1998050800107 19980508 00107 NM 1998 5 8 DHL98726113 1 19980227 A 5320 COVER BOEING 727 727228 NM NR 7 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT UPPER WING AND NR 7 GROUND SPOILER CTR HINGE COVER I/B LEG IS CRACKED. INSTALLED BONDING REPAIR ON PAN EL AT HINGE PER SRM 51-40-6. N/R 1352. 2 L 7 3 4F A3WE 1998050800108 19980508 00108 NM 1998 5 8 DHL98726114 1 19980309 A 5341 651621813 FITTING BOEING 727 727228 NM LT WING/FUS CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, WING FITTING CRACKED IN BORE FOR LEFT FWD BOTTLE PIN. CUT OUT SECTION OF FRONT SPAR LOWER CHORD AND SPAR WE B. REMOVED FASTENERS AND TERMINAL FITTING PER SRM. REMOVED FWD SECTION OF BL 70.5 WEB PER SRM. HFEC OF ALL HOLES. I NSTALLED TERMINAL FITTING, SPAR WEB REPAIR, LOWER CHORD ANGLE REPAIR PER BOEING DRAWING 65C36584. DOUBLER S 2 X 2' X 19 , 2 X 2 X 17, 2 X 2 X 12. N/R 1474. 2 L 7 3 4F A3WE 1998050800109 19980508 00109 NM 1998 5 8 DHL98726115 1 19980301 A 7603 CRANK BOEING 727 727228 NM NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, 33 ENGINE PYLON THROTTLE CRANK CRACKED. REMOVED AND REPLACED CRANK PER MM 76-12-41. N/R 6342. 2 L 7 3 4F A3WE 1998050800110 19980508 00110 NM 1998 5 8 DHL98726116 1 19980303 A 5330 SKIN BOEING 727 727228 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, JUST OUTBD OF APU EXHAUST TOP COVE PANEL HAS BULGE. INSTALLED BONDED REPAIR PER SRM 51-40-6, 10 BY 6'. N/R 2373. 2 L 7 3 4F A3WE 1998050800111 19980508 00111 NM 1998 5 8 DHL98726117 1 19980227 A 7110 COWL BOEING 727 727228 NM NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 3 ENGINE LOWER COWL INBD SIDE 3RD LATCH OUT FROM OUTBD END, INBD GUSSETT CRACKED. REPLACED GUSSETT PER S RM 51-40-03, 9 BY 6. N/R 6263. 2 L 7 3 4F A3WE 1998050800112 19980508 00112 NM 1998 5 8 DHL98726119 1 19980224 A 5400 INLET BOEING 727 727228 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 2 ENGINE INLET INNER SKIN HAS CRACKS END AT RIVETS AT 2 O'CLOCK POSITION. INSTALLED DOUBLER REPAIR PER S RM 54-10-3, 13 BY 6. N/R 6364. 2 L 7 3 4F A3WE 1998050800113 19980508 00113 NM 1998 5 8 DHL9872611D 1 19980303 A 5730 SKIN BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, TOP SKIN JUST FWD OF NR 12 SPOILER INBD HINGE BENT UP AND CRACKED. STOP DRILLED CRACK, HFEC, INSTALLED REP AIR PER SRM 57-30-4, 4 BY 7. N/R 2367. 2 L 7 3 4F A3WE 1998050800114 19980508 00114 NM 1998 5 8 DHL98726120 1 19980228 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 1 ENG UPPER COWL DAMAGED LOWER FWD OUTBD CORNER. REPLACED ANGLE PER SRM 51-40-3, 2' BY 3. N/R 6299. 2 L 7 3 4F A3WE 1998050800115 19980508 00115 NM 1998 5 8 DHL98726121 1 19980228 A 7110 COWL BOEING 727 727228 NM NR 2 ENGINE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 2 ENG FLT FWD COWL LOWER FRAME DAMAGED AT AFT ALIGNMENT PIN RECEPATACLE. CUT OUT DAMAGED SECTION, INSTAL LED FORMED ANGLE REPAIR PER SRM 51-40-3, 28 BY 4. N/R 6301. 2 L 7 3 4F A3WE 1998050800116 19980508 00116 NM 1998 5 8 DHL98726122 1 19980228 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, 31 UPPER COWL WEB DAMAGED, CRACKED AT FWD END OUTBD SIDE. CUT OUT DAMAGED AREA FABRICATED DOUBLER REPAIR PE R SRM 54-10-3, 1 BY 6 N/R 6298. 2 L 7 3 4F A3WE 1998050800117 19980508 00117 NM 1998 5 8 DHL9872612D 1 19980303 A 5730 SKIN BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, TOP FILLET PANEL OUTBD OF NR 14 SPOILER, INBD EDGE, SCREW HOLE HAS CRACK. INSTALLED BONDING REPAIR PER SRM 51-40-6 . N/R 2366. 2 L 7 3 4F A3WE 1998050800118 19980508 00118 NM 1998 5 8 DHL9872613D 1 19980227 A 5720 TIP BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, R/W TIP LIGHT FAIRING CRACKED AT BOTTOM. REMOVED FAIRING, CUT OUT DAMAGED AREA. INSTALLED WING TIP REPAIR PER SRM 57-20-5. 3 BY 2 AND 3.5 BY 2. N/R 2266. 2 L 7 3 4F A3WE 1998050800120 19980508 00120 NM 1998 5 8 DHL9872615D 1 19980301 A 5720 FAIRING BOEING 727 727228 NM NR 5 JACKSCREW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, 5 JACKSCREW FAIRING HAS SEVERAL CRACKS AT AFT MOUNT POINT. INSTALLED SERVICABLE FAIRING PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998050800121 19980508 00121 NM 1998 5 8 DHL9872616D 1 19980311 A 5720 652165830 BRACKET BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT WING TRAILING EDGE PANEL BRACKET I/B OF NR 13 SPOILER CRACKED ON RADIUS. INSTALLED BRACKET SUPPORT PER S RM 51-10-1, N/R 2516. 2 L 7 3 4F A3WE 1998050800122 19980508 00122 NM 1998 5 8 DHL9872617D 1 19980317 A 5730 PANEL BOEING 727 727228 NM LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT TRAILING EDGE PANEL 8105 IS DELAMINATED. INSTALLED BONDING REPAIR PER SRM 51-40-6. N/R 1485. 2 L 7 3 4F A3WE 1998050800123 19980508 00123 NM 1998 5 8 DHL9872618D 1 19980305 A 5320 ANGLE BOEING 727 727228 NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT WING FWD VENT HAS FWD RIB ATTACH EAR CRACKED AT WS 656.5. STOP DRILLED END OF CRACK, HFEC. INSTALLE D VENT STRINGER TO RIB ATTACHEMNT PER S/B 57A159, 2 BY 2. N/R 1439. 2 L 7 3 4F A3WE 1998050800124 19980508 00124 NM 1998 5 8 DHL9872619D 1 19980303 A 5730 PANEL BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT WING FILLET PANEL 3505 BOTTOM AREA HAS A CRACKED HOLE. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, 3 BY 3. N/R 1448. 2 L 7 3 4F A3WE 1998050800125 19980508 00125 NM 1998 5 8 DHL9872620D 1 19980303 A 5350 FILLET BOEING 727 727228 NM LT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT WING FILLET PANEL 3505 HAS NUMEROUS ELONGATED HOLES. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8, 4 BY 4. N/R 1447. 2 L 7 3 4F A3WE 1998050800126 19980508 00126 NM 1998 5 8 DHL9872621D 1 19980303 A 5350 FILLET BOEING 727 727228 NM LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT WING PANEL 3505 INNER SKIN BOTTOM AREA IS DELAMINATED. INSTALLED REPAIR PER SRM 51-40-8, 4 BY 6. N/R 1444. 2 L 7 3 4F A3WE 1998050800127 19980508 00127 NM 1998 5 8 DHL9872622D 1 19980303 A 5750 FILLET BOEING 727 727228 NM LT WING MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT WING FILLET PANEL NR 3505 BOTTOM EDGE HAS MISSING FILLER IN SEVERAL AREAS. INSTALLED REPAIR PER SRM 51 -40-1 .75 BY 36, N/R 1442. 2 L 7 3 4F A3WE 1998050800128 19980508 00128 NM 1998 5 8 DHL9872623D 1 19980305 A 5753 SKIN BOEING 727 727228 NM LT TE AFT FLAP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT OB AFT FLAP LOWER SKIN SURFACE BULGED AND WORN. INSTALLED REPAIR PER SRM 51-40-8, 12 BY 12. N/R 1435. 2 L 7 3 4F A3WE 1998050800130 19980508 00130 NM 1998 5 8 DHL9872625D 1 19980304 A 5753 SKIN BOEING 727 727228 NM LT TE FORE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT O/B FORE FLAP MID AREA OF TRAILING EDGE IS DELMINATED. INSTALLED REPAIR PER SRM 51-40-6, 17 BY 8. N/R 1 402. 2 L 7 3 4F A3WE 1998050800131 19980508 00131 NM 1998 5 8 DHL9872626D 1 19980227 A 5730 SKIN BOEING 727 727228 NM WS 519 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT WING UPPER SURFACE L/E STATION 519 NR 3 L/E SLAT O/B HOOK CUTOUT HAS A .5 CRACK AT UPPER O/B CORNER. S TOP DRILLED CRACK, HFEC. INSTALLED DOUBLER REPAIR PER SRM 57-30-4 DOUBLER 6 BY 8 AND FILLER 1 BY 6. N/R 1361. 2 L 7 3 4F A3WE 1998050800132 19980508 00132 NM 1998 5 8 DHL9872627D 1 19980302 A 5751 SKIN BOEING 727 727228 NM LT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT WING OUTBD AILERON OUTBD TRAILING EDGE IS DELAMINATED. INSTALLED REPAIR PER SRM 51-40-6, 45 BY 7.25. R EBALANCED ON N/R 1337. N/R 1338. 2 L 7 3 4F A3WE 1998050800133 19980508 00133 NM 1998 5 8 DHL9872628D 1 19980302 A 5720 CHANNEL BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, SUPPORT CHANNEL FOR ACCESS PANEL 8405L IS CRACKED. REPLACED SUPPORT CHANNEL PER SRM 51-40-3, 38 BY 1.75 BY 1.25. N/R 1335. 2 L 7 3 4F A3WE 1998050800134 19980508 00134 NM 1998 5 8 DHL9872629D 1 19980228 A 5730 SKIN BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, TOP OF WING CRACKS AT NR 2 SPOILER HINGES NR 2 AND NR 4. CUT OUT DAMAGED SECTION OF LEFT WING. INSTALLED REPAIR PER SRM 57-30-04 7.75 BY 3.25 BY 6 BY 3. N/R 1309. 2 L 7 3 4F A3WE 1998050800135 19980508 00135 NM 1998 5 8 DHL9872630C 1 19980228 A 5720 ANGLE BOEING 727 727228 NM WS 130 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEADING EDGE PANEL SUPPORT ANGLE CRACKED AT LEADING EDGE STATION 130. REPLACED SUPPORT ANGLE PER SRM 51-40- 3, 18 BY 1 BY 1. 2 L 7 3 4F A3WE 1998050800136 19980508 00136 NM 1998 5 8 DHL9872631C 1 19980228 A 5754 CHORD BOEING 727 727228 NM NR 3 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 3 SLAT HAS CRACKS IN CHORD BELOW TAI DUCT INSIDE SLAT. STOP DRILLED CRACK. NDT CRACK, INSTALLED REPAIR PER SRM 51-40-4. N/R 1294. 2 L 7 3 4F A3WE 1998050800137 19980508 00137 NM 1998 5 8 DHL9872632D 1 19980227 A 5720 ANGLE BOEING 727 727228 NM WS 70.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, WS 70.5 OUTBD SIDE L/E COVE AREA CRACK IN ANGLE 11 DOWN FROM TOP OF WING. REPLACED ATTACH ANGLE PER SRM 57- 20-3 36 BY 4. N/R 1278. 2 L 7 3 4F A3WE 1998050800138 19980508 00138 NM 1998 5 8 DHL9872633D 1 19980227 A 5730 SKIN BOEING 727 727228 NM LE WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 3 SLAT INBD TRACK CUTOUT IN WING LEADING EDGE CRACKED. TRIMMED OUT DAMAGED AREA . INSTALLED DOUBLER REP AIR PER SRM 57-30-4 6 BY 8 DOUBLER, FILLER 1 BY 1. N/R 1277. 2 L 7 3 4F A3WE 1998050800139 19980508 00139 NM 1998 5 8 DHL9872634D 1 19980227 A 2782 BRACKET BOEING 727 727228 NM NR 3 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, 3 SLAT ACTUATOR FAIRING INBD ATTACH ANGLE IS CRACKED. REPLACED ANGLE PER SRM 51-30-2. N/R 1272. 2 L 7 3 4F A3WE 1998050800140 19980508 00140 NM 1998 5 8 DHL9872635D 1 19980227 A 2782 ANGLE BOEING 727 727228 NM NR 2 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 2 SLAT ACTUATOR FAIRING OUTBD ATTACH ANGLES IS CRACKED. REMOVED AND INSTALLED NEW ANGLE PER SRM 51-40-4. ANGLE 10 BY .75 BY .75. N/R 1271. 2 L 7 3 4F A3WE 1998050800141 19980508 00141 NM 1998 5 8 DHL9872636D 1 19980227 A 5730 PANEL BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, OUTBD TAI EXHAUST PANEL IS CRACKED ON TOPSIDE. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 1268. 2 L 7 3 4F A3WE 1998050800142 19980508 00142 NM 1998 5 8 DHL9872637D 1 19980227 A 5720 TIP BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, WING TIP IS CRACKED BELOW OUTBD STATIC WICK. CUT OUT CRACK AND INSTALLED REPAIR PER SRM 57-20-5, 10 BY 3. N /R 1266. 2 L 7 3 4F A3WE 1998050800143 19980508 00143 NM 1998 5 8 DHL9872638D 1 19980304 A 5753 652962525 CASTING BOEING 727 727228 NM LT TE FOREFLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT OUTBD FORE FLAP I/B UPPER SURFACE SIDE CASTING CRACKED. HFEC CRACK, REPLACED CASTING PER SRM 51-10-1. N /R 1412. 2 L 7 3 4F A3WE 1998050800144 19980508 00144 NM 1998 5 8 DHL9872639D 1 19980303 A 5320 WEB BOEING 727 727228 NM BS 268 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NOSE WW LT SIDEWALL PRESSURE WEB CRACKED AT FASTENER HOLES ABOVE ACCESS PANEL BS 268 WL 190. HFEC, CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 5 BY 4. N/R 3552. 2 L 7 3 4F A3WE 1998050800145 19980508 00145 NM 1998 5 8 DHL9872640D 1 19980304 A 5320 CLIP BOEING 727 727228 NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD PIT A/C COMPT VERTICAL ANGLE SUPPORT CLIP CRACKED AT STA 720E FLOORBEAM RBL 51. REPLACED CLIP PER SRM 5 1-30-2, 3.5 BY .5. N/R 3535. 2 L 7 3 4F A3WE 1998050800146 19980508 00146 NM 1998 5 8 DHL9872641D 1 19980304 A 5320 SHEAR TIE BOEING 727 727228 NM BS 540 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD PIT LEFT SIDEWALL STA 540 FRAME SHEARTIE CRACKED BET STR 22L AND 21L. CUT OUT DAMAGED AREA, INSTALLED S HEARTIE PER SRM 53-10-4, 6 BY 4.5, FILLER 5.5 BY 4.5. N/R 3528. 2 L 7 3 4F A3WE 1998050800147 19980508 00147 NM 1998 5 8 DHL9872642D 1 19980304 A 5320 ANGLE BOEING 727 727228 NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LOWER FUSELAGE SKIN ATTACH ANGLE TO INTERCOSTAL WEB IS CRACKED AT RADIUS BS 720F LBL 6. ATTACHED ANGLE PER SRM 51-30-2, 21 BY 1 BY 1. N/R 3475. 2 L 7 3 4F A3WE 1998050800148 19980508 00148 NM 1998 5 8 DHL9872643D 1 19980303 A 5320 SUPPORT BOEING 727 727228 NM LT BODY FAIRING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CORROSION PRESENT AT SUPPORT RIBS FOR LT BODY FAIRING 3337. REPALCED BRACKETS PER SRM 51-40-3, 3 BY 3 AND 3 BY 2. N/R 3455. 2 L 7 3 4F A3WE 1998050800149 19980508 00149 NM 1998 5 8 DHL9872644D 1 19980303 A 5350 FAIRING BOEING 727 727228 NM RT FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RT FUSELAGE BODY FAIRING 3621 IS CRACKED AT FASTENER HOLE AND L/E. INSTALLED OVERLAY REPAIR PER SRM 51-40-8 . N/R 3451. 2 L 7 3 4F A3WE 1998050800150 19980508 00150 NM 1998 5 8 DHL9872645D 1 19980302 A 5320 WEB BOEING 727 727228 NM BS 1330 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CRACK AT LIGHTENING HOLE AT WEB ON RIGHT SIDE OF VENTRAL STAIRWELL BS 1330 RBL 20. STOP DRILL CRACK, HFEC, INSTALLED WEB REPAIR PER SRM 51-40-2, 3 BY 3. N/R 3414. 2 L 7 3 4F A3WE 1998050800151 19980508 00151 NM 1998 5 8 DHL9872646D 1 19980301 A 5330 SKIN BOEING 727 727228 NM BS 234 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FUSELAGE SKIN CRACKED AT BS 243.7 WL 220. CUT OUT DAMAGED AREA, HFEC, INSTALLED DOUBLER REPAIR PER SRM 53-3 0-3, 11 BY 11.5. N/R 3384. 2 L 7 3 4F A3WE 1998050800152 19980508 00152 NM 1998 5 8 DHL9872647D 1 19980301 A 5330 SKIN BOEING 727 727228 NM BS 243 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FUSE SKIN CRACKED TWO FASTENERS HOLES RT SIDE BS 243.7 WL 215. CUT OUT DAMAGED AREA, HFEC, INSTALLED DOUBLE R REPAIR PER SRM 53-30-3, 10 BY 10. N/R 3383. 2 L 7 3 4F A3WE 1998050800153 19980508 00153 NM 1998 5 8 DHL9872648D 1 19980301 A 5330 SKIN BOEING 727 727228 NM BS 211 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FUSELAGE SKIN CRACKS AT FOUR FASTENERS RT SIDE BS 211.8 WL 215. CUT OUT DAMAGED AREA, HFEC, INSTALLED DOUBL ER REPAIR PER SRM 53-30-3, 10 BY 14. N/R 3382. 2 L 7 3 4F A3WE 1998050800154 19980508 00154 NM 1998 5 8 DHL9872649D 1 19980225 A 5320 ANGLE BOEING 727 727228 NM AFT AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CHANNEL CRACKED AT UPPER CORNER, BELOW AFT AIRSTAIR HAND PUMP. INSTALLED NEW CHANNEL SUPPORT PER SRM 51-40- 2, 9 BY 2.5 BY 2.5, N/R 3342. 2 L 7 3 4F A3WE 1998050800155 19980508 00155 NM 1998 5 8 DHL9872650D 1 19980227 A 5320 CHORD BOEING 727 727228 NM BS 360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CHORD ANGLE NOSE WHEEL WELL CUTOUT AREA STA 360 LEFT FASTENERS PULLING. REMOVED CORRODED CHORD. INSTALLED NEW CHORD PER SRM 51-30-2. N/R 3326. 2 L 7 3 4F A3WE 1998050800156 19980508 00156 NM 1998 5 8 DHL9872651D 1 19980227 A 5320 JAMB BOEING 727 727228 NM ELECT SVC PANEL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, ELECT GROUND SERVICE PANEL LOWER DOOR JAMB CRACKED. REMOVED ANGLE. INSTALLED NEW ANGLE PER SRM 51-40-3, 2 BY 1' BY 9.5. N/R 3308. 2 L 7 3 4F A3WE 1998050800157 19980508 00157 NM 1998 5 8 DHL9872652C 1 19980227 A 5330 SKIN BOEING 727 727228 NM EXT PWR DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, EXT POWER ACCESS DOOR CUTOUT HAS ANGLE CRACKED AT LOWER EDGE OF CUTOUT. REMOVED AND INSTALLED NEW ANGLE PER SRM 51-40-3, 2 BY 1 BY 9.5, N/R 3270. 2 L 7 3 4F A3WE 1998050800158 19980508 00158 NM 1998 5 8 DHL9872653D 1 19980303 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1166 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 5 SEAT TRACK LOCK FLANGES WORN AND GOUGED FROM STA 1166 TO 1176. REMOVED AND REPLACED DAMAGED SEAT TRAC K. N/R 5150. 2 L 7 3 4F A3WE 1998050800159 19980508 00159 NM 1998 5 8 DHL9872654D 1 19980303 A 5347 BAC1520792 SEAT TRACK BOEING 727 727228 NM BS 560 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 5 SEAT TRACK LOCK FLANGE WORN AT STA 600. REMOVED DAMAGED SECTION. REPLACED DAMAGED SECTION FROM STA 56 0 TO 600 PER SRM 53-10-5. N/R 5156. 2 L 7 3 4F A3WE 1998050800160 19980508 00160 NM 1998 5 8 DHL9872655D 1 19980303 A 5347 SEAT TRACK BOEING 727 727228 NM BS 600 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 3 SEAT TRACK WORN AT STA 600. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5 FROM STA 560 TO 690. N/R 5147. 2 L 7 3 4F A3WE 1998050800161 19980508 00161 NM 1998 5 8 DHL9872656D 1 19980305 A 5311 FRAME BOEING 727 727228 NM BS 890 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LEFT FUSELAGE FRAME GOUGED AT I/B FWD EDGE STA 890, 13 IN FROM FLOOR. INSTALLED FRAME REPAIR PER SRM 53-10- 4, 7 BY 2.5' BY 1. N/R 5193. 2 L 7 3 4F A3WE 1998050800162 19980508 00162 NM 1998 5 8 DHL9872657D 1 19980304 A 5320 CLIP BOEING 727 727228 NM BS 1070 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FUSELAGE UPPER LOBE INTERIOR BS 1070 HAS FRAME TO STR 4 RT CHANNEL CLIP CRACKED. REPLACED CHANNEL CLIP PER SRM 51-40-3, 4 BY 4. N/R 5203. 2 L 7 3 4F A3WE 1998050800163 19980508 00163 NM 1998 5 8 DHL9872658D 1 19980303 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1080 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 6 SEAT TRACK LOCK FLANGES GOUGES AT STA 1080. INSTALLED NEW SECTION PER SRM 53-10-5. 30 LONG, N/R 5145. 2 L 7 3 4F A3WE 1998050800164 19980508 00164 NM 1998 5 8 DHL9872659D 1 19980305 A 5320 WEB BOEING 727 727228 NM BS 640 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD PIT BILGE Z WEB IS CRACKED AT NUTPLATE HOLE AND CORROSION AT LOWER SURFACE BET STA 640-660 STR 26R. CUT OUT DAMAGED AREA AT FLOOR SUPPORT AND INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 8 BY 4. N/R 3628. 2 L 7 3 4F A3WE 1998050800165 19980508 00165 NM 1998 5 8 DHL9872660D 1 19980305 A 5320 WEB BOEING 727 727228 NM BS 600-620 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD PIT BILGE WEB CHANNEL HAS SURFACE CORROSION ABOVE AND BELOW AT DOOR CUTOUT BET STA 600-620. CUT OUT DAM AGED AREA AND INSTALLED REPAIR PER SRM 51-40-2, 14 BY 2.5. N/R 3627. 2 L 7 3 4F A3WE 1998050800166 19980508 00166 NM 1998 5 8 DHL9872661D 1 19980305 A 5320 ANGLE BOEING 727 727228 NM BS 520 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD BILGE FLOOR SUPPORT Z ANGLE CRACKED AT RADIUS AT STA 520 STR 27R. CUT OUT DAMAGED AREA AND INSTALLED PE R SRM 51-40-3, 2', N/R 3620. 2 L 7 3 4F A3WE 1998050800167 19980508 00167 NM 1998 5 8 DHL9872662D 1 19980305 A 5320 WEB BOEING 727 727228 NM BS 520 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD PIT RT Z WEB IS CRACKED AT NUT PLATE HOLE JUST FWD OF STA 5290 STR 26R. INSTALLED DOUBLER REPAIR PER SR M 51-40-2, 6 BY 4 N/R 3619. 2 L 7 3 4F A3WE 1998050800168 19980508 00168 NM 1998 5 8 DHL9872663D 1 19980305 A 5347 SUPPORT BOEING 727 727228 NM BS 870 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, SEAT TRACK ASSY AT LBL 45 BS 870 IS LOOSE AND WORN AT ATACH BOLT. REPLACED SEAT TRACK SUPPORT PER SRM 51-10 -1. N/R 3600. 2 L 7 3 4F A3WE 1998050800169 19980508 00169 NM 1998 5 8 DHL9872664D 1 19980306 A 5320 FITTING BOEING 727 727228 NM BS 1033 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, BS 1033 RT AFT LOWER SERVICE DOOR FWD HINGE SUPPORT CASTING CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-30-2, N/R 3726. 2 L 7 3 4F A3WE 1998050800170 19980508 00170 NM 1998 5 8 DHL9872665D 1 19980306 A 5311 FRAME BOEING 727 727228 NM BS 1148 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO BS 1148 FRAME CORRODED ALONG ATTACH ANGLE FROM STRINGER 28R TO 26R. CUT OUT DAMAGED SECTION. INS TALLED FRAME REPAIR PER SRM 51-40-3, 23 BY 6. N/R 3696. 2 L 7 3 4F A3WE 1998050800171 19980508 00171 NM 1998 5 8 DHL9872666D 1 19980306 A 5312 BULKHEAD ANGLE BOEING 727 727228 NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO BS 1166 BULKHEAD CEILING ATTACH ANGLE CORRODED ON UPPER AND LOWER SURFACES FROM RBL 53 TO 23. RE PLACED ATTACH ANGLE PER SRM 51-30-2. N/R 3694. 2 L 7 3 4F A3WE 1998050800172 19980508 00172 NM 1998 5 8 DHL9872667D 1 19980306 A 5313 STRINGER BOEING 727 727228 NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, BS 1166 FRAME ATTACH ANGLE AND AFT SIDE FRAME CORRODED BETWEEN STR 21R AND 22R. REPLACED ATTACH ANGLE PER S RM 51-40-3, 5 BY 2 BY 1. NR 3692. 2 L 7 3 4F A3WE 1998050800173 19980508 00173 NM 1998 5 8 DHL9872668D 1 19980308 A 5313 STRINGER BOEING 727 727228 NM BS 974 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO STRINGER 22L IS CORRODED AT BS 974. CUT OUT DAMAGED SECTION AND INSTALLED NEW SECTION PER SRM 53- 10-3, 24 LONG N/R 3805. 2 L 7 3 4F A3WE 1998050800174 19980508 00174 NM 1998 5 8 DHL9872669D 1 19980308 A 5320 SUPPORT BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO FLOOR SUPPORT CHANNNEL ALONG OUTBD RADIUS, CORRODED FROM BS 950F GOING AFT FOR 4.5. REMOVED AND REPLACED FLOOR SUPPORT CHANNEL PER SRM 53-10-1, 68.5. N/R 3807. 2 L 7 3 4F A3WE 1998050800176 19980508 00176 NM 1998 5 8 DHL9872671D 1 19980306 A 5315 FLOORBEAM BOEING 727 727228 NM BS 312 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FUSELAGE INT UPPER LOBE STA 312 CORROSION FLOORBEAM BL 4L TO 45L. CUT OUT DAMAGED AREA. INSTALLED REPAIR P ER SRM 51-40-4 12 LONG, N/R 3778. 2 L 7 3 4F A3WE 1998050800177 19980508 00177 NM 1998 5 8 DHL9872672D 1 19980306 A 5341 BOTTLE PIN BOEING 727 727228 NM RT WING /FUS SCRATCHED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, RIGHT AFT BOTTLE PIN FORGING IS SCRATCHED. REMOVED CORROSION AND REBORED TO 4.5 PER SRM 57-10-7, N/R 3735. 2 L 7 3 4F A3WE 1998050800178 19980508 00178 NM 1998 5 8 DHL9872673D 1 19980330 A 5320 SUPPORT BOEING 727 727228 NM BS 1090 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO BS 1090 RBL 16 SUPPORT FOR DOOR UP STOP IS BROKEN. REPLACED SUPPORT ANGLE PER SRM 51-30-2. N/R 3 924. 2 L 7 3 4F A3WE 1998050800179 19980508 00179 NM 1998 5 8 DHL9872674D 1 19980312 A 3270 FITTING BOEING 727 727228 NM TAIL SKID CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, L TAIL SKID RT HINGE FITTING CRACKED AT FWD LOWER END. REMOVED FITTING, INSTALLED NEW SKIN FITTING PER SRM 51-10-1. N/R 3867. 2 L 7 3 4F A3WE 1998050800180 19980508 00180 NM 1998 5 8 DHL9872675D 1 19980310 A 5313 STRINGER BOEING 727 727228 NM BS 280 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, STRINGER 24L STA 280 CORRODED. CUT OUT DAMAGED SECTION FROM BS 281 TO BS 306. INSTALLED REPAIR PER SRM 53- 10-3, 22 LONG. N/R 3863. 2 L 7 3 4F A3WE 1998050800181 19980508 00181 NM 1998 5 8 DHL9872676D 1 19980306 A 5313 STRINGER BOEING 727 727228 NM BS 469 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, BS 469 ABOVE STR 19 RT CORROSION FOUND ON RT PRESS AIR EXHAUST FLANGE. CUT OUT DAMAGED SECTION, INSTALLED S TRINGER REPAIR PER SRM 53-10-3, 20. N/R 3864. 2 L 7 3 4F A3WE 1998050800182 19980508 00182 NM 1998 5 8 DHL9872677D 1 19980309 A 5313 STRINGER BOEING 727 727228 NM BS 480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, FWD PIT BILGE STR 29R SPLICE HAS CORROSION JUST AFT OF STR 480. CUT OUT DAMAGED SECTION. INSTALLED STRINGE R REPAIR PER SRM 53-10-3 48. N/R 3885. 2 L 7 3 4F A3WE 1998050800183 19980508 00183 NM 1998 5 8 DHL9872678D 1 19980308 A 5312 BULKHEAD ANGLE BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO BS 950 VERTICAL BULKHEAD WALL SUPPORT ANGLE IS CRACKED AT FLOOR LEVEL ATTACH POINT. INSTALLED AN GLE REPAIR PER SRM 51-40-4, 3 BY 2. N/R 3886. 2 L 7 3 4F A3WE 1998050800184 19980508 00184 NM 1998 5 8 DHL9872679D 1 19980308 A 5320 ANGLE BOEING 727 727228 NM BS 294 CORROSION A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, MAIN CABIN FLOOR COMP SUPPORT ANGLE LOWER SECTION ACCESS THROUGHOUT E/E COMPT, BETWEEN 294 AND 312 LBL 12 S HOWS CORROSION. REMOVED AND REPLACED SUPPORT ANGLE, 3 BY 2. N/R 3897. 2 L 7 3 4F A3WE 1998050800185 19980508 00185 NM 1998 5 8 DHL9872680D 1 19980308 A 5320 BRACKET BOEING 727 727228 NM BS 294 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CABIN FLOOR SUPPORT CHORD LOWER SECTION COMPT ACCESS BETWEEN BS 294 AND 312 RBL 12 SUPPORT BRACKET SHOWS CO RROSION AND CRACKING. REMOVED AND REPLACED ANGLE BRACKET PER SRM 51-40-3, 3 BY 2. N/R 3898. 2 L 7 3 4F A3WE 1998050800186 19980508 00186 NM 1998 5 8 DHL9872681D 1 19980228 A 5330 SKIN BOEING 727 727228 NM BS 260-360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, BULGING LAP SEAM STR 24L STA 260 TO 360 LEFT. CUT OUT DAMAGED SKIN AT LAP CROWN STR 24LT FROM BS 218 TO 30 7 PER SRM 53-30-3 8.625 BY 2.625. N/R 3346. 2 L 7 3 4F A3WE 1998050800187 19980508 00187 NM 1998 5 8 DHL9872682D 1 19980228 A 5330 SKIN BOEING 727 727228 NM BS 440 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, BULGING SKIN STA 440 STR 20R. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 53-30-3, 12 BY 12. N/R 3351. 2 L 7 3 4F A3WE 1998050800188 19980508 00188 NM 1998 5 8 DHL9872683D 1 19980302 A 5311 FRAME BOEING 727 727228 NM BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT BS 940 FRAME CRACKED BELOW CABIN FLOOR AT FASTNER HOLE. ACCOMPLISHED REPAIR PER S/B 53-0190. N/R 3399. 2 L 7 3 4F A3WE 1998050800189 19980508 00189 NM 1998 5 8 DHL9872684D 1 19980303 A 5343 75463421 TRUNNION BOEING 727 727228 NM NLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT TRUNNION SUPPORT FITTING AFT FLANGE CRACKED. REPLACED FITTING PER SRM 51-10-1. N/R 3550. 2 L 7 3 4F A3WE 1998050800190 19980508 00190 NM 1998 5 8 DHL9872685D 1 19980323 A 5320 ANGLE BOEING 727 727228 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, CORROSION AT LT MOUNTING FLANGE FOR LOWER FUSELAGE ACCESS PANEL NR 1104 INTERIOR AND EXTERIOR. REPLACED CHO RD ANGLE PER SRM 51-30-2, 52. N/R 3917. 2 L 7 3 4F A3WE 1998050800191 19980508 00191 NM 1998 5 8 DHL9872686D 1 19980402 A 5330 SKIN BOEING 727 727228 NM BS 178 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, SKIN DAMAGE STA 178 UPPER SURFACE BL 1 LEFT TO BL 6. CUT OUT DAMAGED SECTION, INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 15 BY 9. N/R 4348. 2 L 7 3 4F A3WE 1998050800192 19980508 00192 NM 1998 5 8 DHL9872687D 1 19980308 A 5532 PANEL BOEING 727 727228 NM VERT STAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, VERTICAL STABILIZER ACCEESS PANEL 4608 DAMAGED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 4341. 2 L 7 3 4F A3WE 1998050800193 19980508 00193 NM 1998 5 8 DHL9872688D 1 19980308 A 5532 PANEL BOEING 727 727228 NM VERT STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, VERTICAL STABILIZER ACCESS PANEL 9607 INTERM REPAIR CRACKED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N /R 4340. 2 L 7 3 4F A3WE 1998050800194 19980508 00194 NM 1998 5 8 DHL9872689D 1 19980308 A 5532 PANEL BOEING 727 727228 NM VERT STAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, VERTICAL STAB PANEL 9607 DAMAGED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 4339. 2 L 7 3 4F A3WE 1998050800195 19980508 00195 NM 1998 5 8 DHL9872690D 1 19980306 A 5542 PANEL BOEING 727 727228 NM RUDER DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LOWER RUDDER LT SIDE SECOND PANEL FROM BOTTOM INTERM REPAIR. INSTALLED BONDED REPAIR PER SRM 51-40-6. N/R 4321. 2 L 7 3 4F A3WE 1998050800196 19980508 00196 NM 1998 5 8 DHL9872691D 1 19980306 A 5542 SKIN BOEING 727 727228 NM RUDDER CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LOWER RUDDER LT SIDE CORNER SECTION FROM LE TO TE SKIN BULGE AND INTERM REPAIR. INSTALLED BONDING REPAIR PE R SRM 51-40-6. N/R 4320. 2 L 7 3 4F A3WE 1998050800197 19980508 00197 NM 1998 5 8 DHL9872692D 1 19980306 A 5350 TAIL CONE BOEING 727 727228 NM VERT STAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, VERT STAB TAIL CONE HAS DELAMINATION AFT OF LT ACCESSS. INSTALLED OVERLAY REPAIR PER SRM 51-40-8. N/R 431 5. 2 L 7 3 4F A3WE 1998050800198 19980508 00198 NM 1998 5 8 DHL9872693D 1 19980304 A 5522 RIVETS BOEING 727 727228 NM LT ELEVATOR LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, LT ELEVATOR LOWER SKIN HAS LOOSE RIVETS JUST AFT OF LOWER ACCESS PANEL. REPLACED ANGLE PER SRM 51-40-3, 1.2 5 BY 1.25 BY 18. N/R 4261. 2 L 7 3 4F A3WE 1998050800199 19980508 00199 NM 1998 5 8 DHL9872694D 1 19980301 A 5532 PANEL BOEING 727 727228 NM VERT STAB DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, PANEL 9604 HAS ELONGATED SCREW HOLES. INSTALLED FIBERGLASS OVERLAY PER SRM 51-40-8, N/R 4238. 2 L 7 3 4F A3WE 1998050800200 19980508 00200 NM 1998 5 8 DHL9872695D 1 19980301 A 5532 PANEL BOEING 727 727228 NM VERT STAB DISBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, PANEL 9606 HAS DISBONDING AT SCREW HOLES. INSTALLED FIBERGLASS REPAIR PER SRM 51-40-8. N/R 4237. 2 L 7 3 4F A3WE 1998050800201 19980508 00201 NM 1998 5 8 DHL9872696D 1 19980301 A 5532 PANEL BOEING 727 727228 NM VERT STAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, ACCESS PANEL 9505 IS DELAMINATING. INSTALLED OVERLAY REPAIR PER SRM 51-40-8 2 L 7 3 4F A3WE 1998050800202 19980508 00202 NM 1998 5 8 DHL9872697D 1 19980308 A 5311 FRAME BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO BS 950 FRAME IS CRACKED AT TOP FLANGE RBL 17. HFEC, STOP DRILLED, HFEC OF STOP DRILL. INSTALLED FRAME REPAIR PER SRM 51-10-1 5 BY 3. N/R 3848. 2 L 7 3 4F A3WE 1998050800203 19980508 00203 NM 1998 5 8 DHL9872698D 1 19980306 A 5320 SUPPORT BOEING 727 727228 NM BS 1166 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO AFT BULKHEAD HORIZ WALL SUPPORTS AT BL 0, 19 ABOVE FLOOR IS CORRODED FROM BS 1166 TO 1174. REPLAC ED SUPPORT ANGLE PER SRM 51-30-2, 6. N/R 3682. 2 L 7 3 4F A3WE 1998050800204 19980508 00204 NM 1998 5 8 DHL9872699D 1 19980306 A 5320 ANGLE BOEING 727 727228 NM BS 1145 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, AFT CARGO SUPPORT ANGLE AT LBL 16 IS CORRODED FROM BS 1166 TO 1145. CUT OUT DAMAGED SECTION AND INSTALLED A NGLE REPAIR PER SRM 51-40-4, FILLER 8 LONG. N/R 3676. 2 L 7 3 4F A3WE 1998050800205 19980508 00205 NM 1998 5 8 DHL98726002 1 19980423 A 3260 MS242266R CONNECTOR BOEING 727 727228 NM E/E BAY FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 726DH 20409 UPON GEAR RETRACTION, LEFT GEAR UNSAFE LIGHT ILLUMINATED AND GREEN GEAR LIGHT ILLUMINATED. REPLACED CONNECTOR D-4774 A ND REPINNED NR 2 AND NR 10. 2 L 7 3 4F A3WE 1998050800206 19980508 00206 WP 1998 5 8 RRXA98078 1 19980417 A 2910 HYD LINE DOUG DC8 DC8F54 3021926 WP NR 3 ENGINE FAILED A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 992CF 45884 AT FL 35.0 LOST HYD FLUID TO STAND PIPE AUX LEVEL. PERFORMED HYD FLUID OR PRESS LOSS CHECKLIST. FOUND PRESSURE LINE ON NR 3 ENGINE RUPTURED. REMOVED AND REPLACED SAID LINE. ALSO, REPLACED SUCTION LINE AS PRECAUTIONARY. LEAK CK'D SYSTEM CHECKED GOOD. HYD PUMPS PRESS CKS GOOD. 2 L 7 4 4F 4A25 1998050800207 19980508 00207 WP 1998 5 8 RRXA98080 1 19980422 A 3231 RETRACT MECH DOUG DC8 DC873F 302199F WP NLG DOORS LACK OF LUBE A RRXA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 WP 15 602AL 45991 ON GEAR UPLATCH CHECK, GEAR FAILED CHECK IN COMPLIANCE WITH GEAR UPLATCH FAILURE CHECK LIST GEAR CONTINUED TO FAIL UPLAT CH CHECK AND SOUNDED AS THOUGH NOSE GEAR DOORS WERE OPEN AND/OR NOSE GEAR EXTENDED WHILE IN THE GEAR UP POSITION. IN CO MPLIANCE WITH THE QRH DOMESTIC RESTRICTIONS RETURN WAS MANDATORY. INTERNATIONAL DESTINATION WAS MMGL. LUBED GEAR UPLAT CH MECHANISMS ON ALL GEAR. FLIGHT TEST REQUESTED BY MANAGER OF M/C FOR FURTHER EVALUATION PER MR/P CHAP 4 ITEM XX PG 16 4 AND 165. 2 L 7 4 4F RT 4A25 1998050800208 19980508 00208 WP 1998 5 8 RRXA98081 1 19980428 A 2110 6F8157509 CHECK VALVE DOUG DC8 DC862F 3021972 WP NR 1 TURBO COMP CRACKED A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 15 996CF 46162 INBOUND TO DAY, ODOR OF BURNING OIL AROUND CAPT AND FO AREA, ALSO NO AIR FLOW FROM OUTLETS. SHUTOFF NR 1 TC THEN NR 2 T C AND ODOR DISSIPATED. NOTED LOUD RUMBLING WHEN EITHER NR 1 OR NR 2 T/C WAS OPERATING ALONE. FOUND NR 1 T/C CHECK VALV E CRACKED. REMOVED AND REPLACED NR 1 T/C CHECK VALVE OPS CK GOOD. OPERATED NR 1 AND NR 2 TC'S, NO RUMBLING OR ODORS OF OIL NOTICED ON GROUND. 2 L 7 4 4F 4A25 1998050800209 19980508 00209 WP 1998 5 8 ARWA980409 1 19980427 A 7110 57141901 COWLING DOUG DC8 DC862 3021970 WP NR 2 ENGINE DAMAGED A ARWA K NONE O OTHER TX TAXI/GRND HDL 1 SO 19 802BN 45909 DURING GROUND HANDLING, NR 2 ENGINE COWLING DAMAGED BY BELT LOADER, LT AND RT FWD COWLINGS. LT AND RT AFT COWLINGS AND T/R LOWER STRINGER, REMOVED AND REPLACED NR 2 ENGINE. FWD AND AFT COWLINGS AND T/R LOWER STRINGER AS PER DC-8 MM 71-10- 2 AND 78-30-0. 2 L 7 4 4F 4A25 1998050800210 19980508 00210 WP 1998 5 8 ARWA980410 1 19980427 A 5310 STRUCTURE DOUG DC8 DC862 3021970 WP BS 380-400 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 DURING PRE-FLIGHT, FOUND STRUCTURAL DAMAGED AT RIGHT SIDE OF FUSELAGE BETWEEN STR 380, 400 AND LONGERON 25-26, SIZE OF D AMAGE FROM 4.5 INCHES TO 4.0 INCHES REPAIRED RIGHT SIDE OF FUSELAGE BETWEEN STA 380R-400 R AND LONG 25-26 IAW REO-04635 REVISION 1R DATED 4/24/98. 2 L 7 4 4F 4A25 1998050800211 19980508 00211 NM 1998 5 8 VNAA9804020 1 19980428 A 7931 IPTE75GF100070D TRANSDUCER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 426JS 74774 3038 DURING TAXI,THE LEFT ENGINE OIL PRESSURE WAS INDICATING BELOW LIMITS. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAIN TENANCE TROUBLE SHOT AND FOUND THE LEFT OIL PRESSURE TRANSDUCER TO BE DEFECTIVE. OUTSTATION MAINTENANCE INSPECTED AND A PPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO DCA FOR REPAIR. THE FERRY FLIGHT TOOK PLACE WITHOUT INCIDENT. PSA MAINTENAN CE WAS DISPATCHED TO DCA ,WITH PARTS FOR THE REPAIR. MAINTENANCE INSPECTED AND REPLACED THE LEFT OIL PRESSURE TRANSDUCE R, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-71-03. OPERATION AND LEAK CHECKS WERE SATISFACTORY, AND THE AIRCRAF T WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998050800212 19980508 00212 1998 5 8 VNAA9804021 4 19980417 A 3418 861EF1 AOA SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT FUSELAGE FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 432JS 65221 41286 3045 DURING TAXI PRIOR TO TAKEOFF, A STICK PUSHER FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. OUTS TATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT WAS EXECUTED WITHOUT ANY PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE LEFT ANGLE OF ATTACK SENSOR, IN ACCORDANCE WITH DORNIER MAINT ENANCE MANUAL 27-33-01. OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998050800312 19980508 00312 WP 1998 5 8 VJ9800146 1 19980428 A 3350 110049 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A VJ6A K NONE L NO TEST TX TAXI/GRND HDL 1 SO 15 910VJ 47277 SEVERAL EMERGENCY EXIT LIGHTS INOP IN FORWARD CABIN. REPLACED BATTERY PACK AND CHARGER. 2 L 7 2 4F A6WE 1998050800313 19980508 00313 WP 1998 5 8 VJ9800147 1 19980313 A 2571 1A306501 BATTERY TRAY DOUG DC9 DC932 3022066 WP E/E COMPT CORRODED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 BATTERY TRAY, LT SIDE, IN E/E COMPARTMENT CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. REMOVED CORROSION IAW DC9 SRM 51-10-3. FABRICATED DOUBLER REPAIR FROM 2024T3, 7/8 BY 13/8 BY 35/8 INCHES, IAW DC9 SRM 53-01, FIG 2. TREATED, PRIME D AND INSTALLED IAW DC9 SRM 51-10-3 AND 51-10-2. 2 L 7 2 4F A6WE 1998050800314 19980508 00314 NM 1998 5 8 K3HA980062 1 19980424 A 3350 1102533 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 ASSIGNED RIP 33-04-01 EMERGENCY AFT AIRSTAIR LIGHT DOES NOT ILLUMINATE CHECK LIGHT ASSY AND BATTERIES. REPLACED LIGHT A SSEMBLY AND BATTERIES (2XP/N S106). OPS CHK OK. 2 L 7 3 4F A3WE 1998050800315 19980508 00315 NM 1998 5 8 AWXA9800111 1 19980421 A 5310 FUSELAGE BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 D-CRACK IN FUSELAGE 1 AT STA 727 STR 16R. C/W REPAIR PER 53-30-03 PAGE11. 2 L 7 2 4F RT A16WE 1998050800316 19980508 00316 NM 1998 5 8 AWXA9800115 1 19980422 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 277 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 156AW 23778 2 BY 3 HOLE IN FUSELAGE SKIN FROM JET WAY STRIKE, NO STRINGER OR FRAME DAMAGE. HOLE LOCATED 1 AFT OF BULKHEAD 277, HALF BELOW WATER LINE. REPAIRED IAW SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A16WE 1998050800317 19980508 00317 NM 1998 5 8 AWXA9800117 1 19980326 A 5320 FLOOR PAN BOEING 757 7572G7 1384963 NM BS 1681 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 910AW 24523 DURING SCHEDULED C-7 INSPECTION, FOUND CABIN FLOOR PAN/WEB AT STA 1681 HAS CORROSION AT FWD EDGE ALONG ENTIRE EDGE. REP AIRED PER SRM 53-60-51, FIGURE 203. 2 L 7 2 4F RT A2NM 1998050800318 19980508 00318 NM 1998 5 8 AWXA9800118 1 19980423 A 3350 0013395 BATTERY PACK BOEING 737 737112 1384412 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 DURING ROUTINE MAINTENANCE CHECK, FOUND D-RT AND LTE XT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS. 2 L 7 2 4F A16WE 1998050800319 19980508 00319 NM 1998 5 8 AWXA9800119 1 19980424 A 5315 BAC1518338 FLOORBEAM BOEING 757 757225 1384959 NM BS 1640 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 907AW 22691 DURING SCHEDULED C-3 INSPECTION, FOUND STA 1640 BL0 CABIN FLOORBEAM UPPER CHORD CORRODED. NEW SECTION OF FLOORBEAM SPLI CED IN IAW, SRM 53-00-51. 2 L 7 2 4F RT A2NM 1998050800320 19980508 00320 EU 1998 5 8 AWXA9800121 1 19980428 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU LT CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 621AW 053 DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT HAND OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY LI GHT BATTERY. PACK OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1998050800321 19980508 00321 SO 1998 5 8 RAAA98E8010 1 19980428 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT RT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT DUE FAILED. 2 L 7 4 4T 4A22 1998050800322 19980508 00322 NM 1998 5 8 RAAA98B2023 1 19980428 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 10 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998050800323 19980508 00323 NM 1998 5 8 RAAA98B2024 1 19980428 A 3350 873100112 LIGHT BOEING 727 72722C 138400F NM CABIN BROKEN A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 2 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK DUE BROKEN LAMP ASSY. CHANGED PROXIMITY LIGHT ASSY. 2 L 7 3 4F A3WE 1998050800324 19980508 00324 SO 1998 5 8 RAAA98E9013 1 19980429 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD RT AND AFT LT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISC HARGED. 2 L 7 4 4T 4A22 1998050800325 19980508 00325 NM 1998 5 8 CALA9800715 1 19980128 A 3397 WIRE BOEING 727 727243 138408D NM CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 578PE 21661 INSPECTION FOUND FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A DAMAGED WIRE AT CONNECTOR. THE WIRE WAS REPAIRED, THE LIGHT WAS RELAMPED, AND THE BATTERY PACK WAS RECHARGED. OPERATION CHECKED GOOD IAW MM 33-50. 2 L 7 3 4F RT A3WE 1998050800326 19980508 00326 NM 1998 5 8 CALA9800716 1 19980214 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79754 21363 INSPECTION FOUND CENTER AISLE EMERGENCY EXIT LIGHT BETWEEN L-2 AND R-2 DOORS INOPERATIVE. THE BATTERY PACK FOR EMERGENC Y EXIT LIGHT WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-11. 2 L 7 3 4F A3WE 1998050800327 19980508 00327 NM 1998 5 8 CALA9800717 1 19980430 A 3350 900835A BATTERY PACK GRIMES BOEING 727 727227 1384078 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79754 21363 INSPECTION FOUND THE LT ESCAPE HATCH OVERWING EXIT SIGN WOULD NOT ILLUMINATE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1998050800328 19980508 00328 NM 1998 5 8 CALA9800718 1 19980312 A 3350 BATTERY PACK BOEING 727 727243 138408D NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17410 21663 THE EMERGENCY EXIT SIGN IVER COCKPIT DOOR FELL OUT AND WAS FOUND INOPERATIVE. THE EMERGENCY LIGHT BATTERY PACK AND LENS E ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 3 4F RT A3WE 1998050800329 19980508 00329 WP 1998 5 8 CALA9800719 1 19980114 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP LT REAR SPAR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12510 47799 INSPECTION FOUND CRACK INDICATIONS IN LT REAR SPAR LOWER CAP AFT TANG. A REPAIR WAS PERFORMED IAW ECRA 5710-01878. 2 L 7 2 4F A6WE 1998050800330 19980508 00330 WP 1998 5 8 CALA9800720 1 19980114 A 7830 STIFFENER DOUG DC9 DC932 3022066 WP NR 1 ENG TR GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12510 47799 INSPECTION FOUND THE NR 1 ENGINE THRUST REVERSER PANEL NR 7519DS GOUGED ON FORWARD UPPER CORNER. THE STIFFENER WAS REMO VED AND THE GOUGE WAS BLENDED OUT IAW SRM 53-01. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW DOUGLAS DRAWING NR 59 58762, SRM 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998050800331 19980508 00331 NE 1998 5 8 9807629869 2 19980427 A 7230 COMPRESSOR DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE STALLED A NWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 01 778NC 48100 696732 AFTER LIFTOFF, THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALLS. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCI DENT. MAINTENANCE REPLACED THE RIGHT ENGINE. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 1998050800332 19980508 00332 EU 1998 5 8 9807633226 1 19980427 A 3350 321430 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 326US 282 DURING EMERGENCY LIGHT TEST, INT LOADS EMER R FAULT DISPLAYED. MAINTENANCE REPLACED PSEU BATTERY PACK. OPERATIONAL CHE CK OK. 2 L 7 2 4F RT A28NM 1998050800333 19980508 00333 NM 1998 5 8 9807646305 1 19980427 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 665US 23820 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT 43C, 9J, AND L1 LAV. REPAIRED WIRING. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998050800334 19980508 00334 NE 1998 5 8 9807656729 2 19980426 A 7230 COMPRESSOR BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 629US 22388 689562 DURING LANDING ROLLOUT, WHILE IN REVERSE THRUST, THE NR 3 ENGINE EXPERIENCED A MINOR COMPRESSOR STALL. EGT REACHED MAXI MUM OF 740C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED AND THE AIRCRAFT WA S RETURNED TO SERVICE. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998050800335 19980508 00335 WP 1998 5 8 9807669760 1 19980428 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NW 47288 DURING LINE MAINTENANCE INSPECTION, FOUND MID CABIN OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 19 THROUGH 21 INOPERATIVE. R EPLACED BATTERIES IN BATTERY PACK AT FS 825. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050800336 19980508 00336 WP 1998 5 8 9807679951 1 19980428 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9347 45827 DURING LINE MAINTENANCE INSPECTION, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050800337 19980508 00337 WP 1998 5 8 9807689851 1 19980428 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 16 THROUGH 20 INOPERATIVE. REPLACED BA TTERIES IN BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050800338 19980508 00338 WP 1998 5 8 9807699877 1 19980428 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE MAINTENANCE INSPECITON, FOUND TAILCONE CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050800339 19980508 00339 WP 1998 5 8 9807709752 1 19980428 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 752NW 47116 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES IN POW ER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050800340 19980508 00340 WP 1998 5 8 9807719993 1 19980427 A 3350 SOCKET DOUG DC9 DC931 3022065 WP CABIN BAD A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8986E 47402 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT AFT CENTER CATWALK INOPERATIVE. REPLACED LIGHT SOCKET. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050800341 19980508 00341 WP 1998 5 8 9807729931 1 19980429 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 90S 47244 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERIES. OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050800342 19980508 00342 WP 1998 5 8 9807739955 1 19980429 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 922RW 47182 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK . OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050800343 19980508 00343 SO 1998 5 8 COMA9810111 1 19980429 A 3020 2957D513541 DE-ICE BOOT EMB 120 EMB120RT SO RT ENGINE INLET WORN A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 152CA 120152 RIGHT ENGINE INLET DE-ICE SYSTEM FAILURE DURING CRUISE FLIGHT. REPLACED LEFT AND RIGHT ENGINE INLET DE-ICE BOOTS. 2 L 7 2 4T RT A31SO 1998050800344 19980508 00344 EA 1998 5 8 COMA9860091 1 19980428 A 3080 871BN32 ICE DETECTOR CNDAIR CL600 CL6002B19 EA NOSE SECTION DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 986CA 2181 7174 DURING T/O ROLL AT STL ICE DETECTOR NR 1 WARNING ACTIVATED. REPLACED THE NR 1 ICE DETECTOR. 2 L 7 2 4F RT A21EA 1998050800345 19980508 00345 NM 1998 5 8 SWA980598 1 19980413 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 747 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED, D-CHECK, FOUND DENTED FRAME AT 747, LBL 35, WL 160. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800346 19980508 00346 NM 1998 5 8 SWA980599 1 19980413 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN STR 8 LT AND 9 LT; BS 827, STR 8 LT AND 9 LT; AND BS 787, STR 8 LT AND 9 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800347 19980508 00347 NM 1998 5 8 SWA980600 1 19980413 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN BS 520, STR 8 RT AND 9 RT; AND BS 727D, STR 8 RT AND 9 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800348 19980508 00348 NM 1998 5 8 SWA980601 1 19980413 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500-520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL ANGLE AT BS 500D- 520, LBL 1, WL 208. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998050800349 19980508 00349 NM 1998 5 8 SWA980602 1 19980413 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 640 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 640, WL 221, LBL 65. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800350 19980508 00350 NM 1998 5 8 SWA980603 1 19980413 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 794-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT BS 794-847, RBL 19, WL 160. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998050800351 19980508 00351 NM 1998 5 8 SWA980604 1 19980413 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 787-794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED INTERCOSTAL AT BS 787-794, RBL 23, WL 158. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998050800352 19980508 00352 NM 1998 5 8 SWA980605 1 19980413 A 5320 TIE STRAP BOEING 737 7373H4 1384600 NM BS 781-802 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED TIE STRAP UNDERNEATH PRIMARY STILL WEB AT BS 781-802, RBL 19.5, WL 156; BS 839- 855, RBL 19, WL162; AND 847, RBL 19, WL 161. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800353 19980508 00353 NM 1998 5 8 SWA980606 1 19980413 A 5320 TIE STRAP BOEING 737 7373H4 1384600 NM BS 787/774-858 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED TIE STRAP UNDERNEATH PRIMARY STILL WEB AT BS 787, RBL 21, WL 157; BS 774-858, R BL 19, WL 163. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800354 19980508 00354 NM 1998 5 8 SWA980607 1 19980413 A 5320 BEAM BOEING 737 7373H4 1384600 NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED CREASE BEAM AT BS 179, RBL 29, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800355 19980508 00355 NM 1998 5 8 SWA980608 1 19980413 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 269 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 269, WL 207, RBL 11. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800356 19980508 00356 NM 1998 5 8 SWA980609 1 19980414 A 5320 MOUNTING BOEING 737 7373G7 1384595 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D CHECK, FOUND CORRODED FWD ENTRY DOORWAY GIRT BAR MOUNTING PAD AT BS 344, WL 208, LBL 60. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800357 19980508 00357 NM 1998 5 8 SWA980610 1 19980414 A 5320 THRESHOLD BOEING 737 7373G7 1384595 NM BS 303-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D CHECK, FOUND CORRODED FWD ENTRY THRESHOLD INBOARD SUPPORT ANGLE AT BS 303-344, WL 208, LBL 61. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800358 19980508 00358 NM 1998 5 8 SWA980611 1 19980414 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 312-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D CHECK, FOUND CORRODED WEB AT BS 312-344, LBL 60, WL 208. RREMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800359 19980508 00359 NM 1998 5 8 SWA980612 1 19980414 A 5754 SKIN BOEING 737 7373G7 1384595 NM NR 5 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D CHECK, FOUND CRACKED NR 5 SLAT LOWER SKIN AT WBL 167.5, AFT ROW. REMOVED AND REPLACED PER DRAWING 65 C30133 BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800360 19980508 00360 NM 1998 5 8 SWA980613 1 19980414 A 5754 SKIN BOEING 737 7373G7 1384595 NM NR 5 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D CHECK, FOUND CRACKED NR 5 SLAT LOWER SKIN AT FS 172, AFT ROW. REMOVED AND REPLACED PER DRAWING 65C30 133 BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800361 19980508 00361 NM 1998 5 8 SWA980614 1 19980414 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD WEB AT WL 197 TO 201, RBL 4.7. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800362 19980508 00362 NM 1998 5 8 SWA980615 1 19980414 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 727D PLUS 6, LBL 17, WL 156. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998050800363 19980508 00363 NM 1998 5 8 SWA980616 1 19980414 A 5320 SHEAR WEB BOEING 737 7373G7 1384595 NM BS 927-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR WEB UPPER ATTACH ANGLE AT BS 927 TO 947 BL0, WL 208. CRACK LOCATION AT BS 930. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800364 19980508 00364 NM 1998 5 8 SWA980617 1 19980414 A 5320 CREASE WEB BOEING 737 7373G7 1384595 NM BS 877 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND CORRODED CREASE BEAM AT BS 877, LT 65, WL 208 AROUND FASTENER HOLE. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800365 19980508 00365 NM 1998 5 8 SWA980618 1 19980414 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 867-886 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CHAFFED AT BS 867-886 BETWEEN STR 1 AND 2 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800366 19980508 00366 NM 1998 5 8 SWA980633 1 19980416 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 965 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 80SW 22675 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED BS 965, STRINGER 26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998050800367 19980508 00367 NM 1998 5 8 SWA980634 1 19980416 A 3350 6104781 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 96SW 23055 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING BATTERY PACK INOP. REPLACED FLOOR TRACK LIGHTING B ATTERY PACK PER BOEING MM. 2 L 7 2 4F A16WE 1998050800368 19980508 00368 NM 1998 5 8 SWA980635 1 19980416 A 5310 FUSELAGE BOEING 737 7372K6 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE RT SIDE, BS 727, STR 6. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800369 19980508 00369 NM 1998 5 8 SWA980636 1 19980416 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 615 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 615 WL 221 LBL 65. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800370 19980508 00370 NM 1998 5 8 SWA980637 1 19980416 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 302 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 302, WL 236, 6.5 ABOVE STR 14 LT. REMOVED AND RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800371 19980508 00371 NM 1998 5 8 SWA980638 1 19980416 A 5242 SKIN BOEING 737 7373H4 1384600 NM E/E DOOR GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND E/E DOOR OUTER SKIN, HAS NUMEROUS GOUGES AND DENTS. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998050800372 19980508 00372 NM 1998 5 8 SWA980639 1 19980416 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 727C, RBL 48, WL 169. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800373 19980508 00373 NM 1998 5 8 SWA980640 1 19980416 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 767-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT BS 767-787, RBL 20, WL 156. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998050800374 19980508 00374 NM 1998 5 8 SWA980641 1 19980416 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED BRACKET AT BS 328, LBL 53, WL 181. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800375 19980508 00375 NM 1998 5 8 SWA980642 1 19980416 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED BS 178 BULKHEAD WEB AT LBL 6.7, WL 200 TO WL 198. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998050800376 19980508 00376 NM 1998 5 8 SWA980643 1 19980416 A 5320 FLOOR WEB BOEING 737 7373H4 1384600 NM BS 179-188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR WEB AT BS 179-188, RBL 25-29, WL 207; AND BS 179-188, LBL 25-29, WL 207. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800377 19980508 00377 NM 1998 5 8 SWA980644 1 19980416 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 967-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED WEB AT BS 967-986, RBL 46-48, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800378 19980508 00378 NM 1998 5 8 SWA980645 1 19980416 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED SUPPORT ANGLE AT 178 BULKHEAD, LBL 27, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800379 19980508 00379 NM 1998 5 8 SWA980646 1 19980416 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 277 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 277, RBL 41, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800380 19980508 00380 NM 1998 5 8 SWA980647 1 19980416 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1002 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED WEB AT BS 1002, RBL 45.5, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800381 19980508 00381 NM 1998 5 8 SWA980648 1 19980416 A 5320 CHANNEL BOEING 737 7373H4 1384600 NM BS 334 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED U-CHANNEL AT BS 334, LBL 60 AND 354, LBL 61, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800382 19980508 00382 NM 1998 5 8 SWA980649 1 19980416 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROED BELT FRAME LEG AT BS 500 C, RBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800383 19980508 00383 NM 1998 5 8 SWA980650 1 19980416 A 5320 WEB BOEING 737 7373H4 1384600 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2 D CHECK, FOUND DAMAGED WEB AT FWD SIDE OF DOOR CUT-OUT 8 UP FROM LOWER END. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998050800384 19980508 00384 NM 1998 5 8 SWA980651 1 19980416 A 5320 FRAME BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED FWD GALLEY DOOR AT FWD LWR CORNER BS 294.5 AT Z-ANGLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800385 19980508 00385 NM 1998 5 8 SWA980652 1 19980416 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 904/938 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SCHEDULED TRAN CHECK, FOUND DENTED SKIN AT BS 904 2 ABOVE STR 21 RT; AND BS 938 3.5 ABOVE STR 24 RT. REPAIRED PE R BOEING SRM. 2 L 7 2 4F A16WE 1998050800386 19980508 00386 NM 1998 5 8 SWA980653 1 19980417 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 515 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED A2 CHECK, FOUND CRACKED APPROX 4 FEET LONG AT BS 515, STR 14, ABOVE NR 9 WINDOW RT SIDE OF A/C. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800387 19980508 00387 NM 1998 5 8 SWA980654 1 19980417 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FLOORBEAM AT BS 787 RBL 14. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800388 19980508 00388 NM 1998 5 8 SWA980655 1 19980418 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM PAX DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 57SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND FWD PASSENGER DOOR EMERGENCY EXIT LIGHT CHARGING BASE BAD. REPLACED FWD PASSENGE R DOOR EMERGENCY EXIT LIGHT PER PER BOEING MM. 2 L 7 2 4F A16WE 1998050800389 19980508 00389 NM 1998 5 8 SWA980656 1 19980418 A 5320 SKIN BOEING 737 7373H4 1384600 NM R2 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED BC1 CHECK, FOUND R2 DOOR UPPER FUSELAGE HINGE CUT-OUT HAS .250 LONG CRACK IN RADIUS. REPAIRED PER SWA RA NR 1-353-1807. 2 L 7 2 4F RT A16WE 1998050800390 19980508 00390 NM 1998 5 8 SWA980657 1 19980418 A 5330 SKIN BOEING 737 7373H4 1384600 NM L1 DOORWAY GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED RON CHECK, FOUND GOUGE BELOW L-1 DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800391 19980508 00391 NM 1998 5 8 SWA980658 1 19980418 A 5310 FUSELAGE BOEING 737 7373H4 1384600 NM BS 980 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED RON CHECK, FOUND CRACKED FUSELAGE AT BS 980 STR 21 ABOUT 2 LONG HFEC. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800392 19980508 00392 NM 1998 5 8 SWA980659 1 19980418 A 5330 SKIN BOEING 737 7373H4 1384600 NM PAX DOORWAY GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED TERMINAL CHECK, FOUND GOUGED BELOW FWD ENTRY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800393 19980508 00393 NM 1998 5 8 SWA980660 1 19980418 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2 D-CHECK, FOUND LT INTERCOSTAL AT BS 500-500A UNDER TRANSITION ANGLE DAMAGED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800394 19980508 00394 NM 1998 5 8 SWA980661 1 19980419 A 3230 RETRACT MECH BOEING 737 7375H4 138449D NM LANDING GEAR LACK OF LUBE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 511SW 24188 AFTER TAKEOFF GEAR WOULD NOT COME UP, PULLED TRIGGER LOCK OVERRIDE TO RISE AFTER GEAR RETRACTED, TAKEOFF WARNING HORN AN D CDU STUCK. USED QRH PULLED P62 CB HORN OFF, AND CDU OK. AIR RETURN TO PHX, AND MADE AN UNEVENTFUL LANDING. ADJUSTED GROUND SENSE CABLE AIR SENSOR AND LUBE CABLE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998050800395 19980508 00395 NM 1998 5 8 SWA980662 1 19980420 A 5330 SKIN BOEING 737 7373H4 1384600 NM PAX DOORWAY GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED A2 CHECK, FOUND GOUGED SKIN BELOW AFT ENTRY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800396 19980508 00396 NM 1998 5 8 SWA980663 1 19980420 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED RON CHECK, FOUND CRACKED FUSELAGE SKIN 1.25 AT BS 927, RT SIDE AFT OF AFT CARGO DOOR. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1998050800397 19980508 00397 NM 1998 5 8 SWA980664 1 19980421 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 PLUS 8 = 947, LBL 3, WL 155. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800398 19980508 00398 NM 1998 5 8 SWA980665 1 19980421 A 5314 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CORRODED KEEL BEAM OB FLANGE AT BS 500 D PLUS 500 D PLUS, LBL 6, WL 149. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998050800399 19980508 00399 NM 1998 5 8 SWA980666 1 19980421 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 380/440/747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH ANGLE BETWEEN STR 8 LT AND 9 LT AT BS 747; STR 8 LT AND 9 LT AT BS 440; AND STR 8 RT AND 9 RT AT BS 380. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800400 19980508 00400 NM 1998 5 8 SWA980667 1 19980421 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907, STR 4 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800401 19980508 00401 NM 1998 5 8 SWA980668 1 19980421 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CORRODED Z CHORD AT BS 270, WL 207, RBL 5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800402 19980508 00402 NM 1998 5 8 SWA980669 1 19980421 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 327 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 327, RBL 66, WL 210.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800403 19980508 00403 NM 1998 5 8 SWA980670 1 19980421 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 955 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CORRODED LOWER STUB FRAME AT BS 955, RBL 54, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800404 19980508 00404 NM 1998 5 8 SWA980671 1 19980421 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 827, LBL 45, WL 171. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800405 19980508 00405 NM 1998 5 8 SWA980672 1 19980421 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 295, LBL 59, WL 223; AND BS 295, LBL 58, WL 216. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800406 19980508 00406 NM 1998 5 8 SWA980673 1 19980421 A 5320 BEAM BOEING 737 7373H4 1384600 NM BS 947 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND DAMAGED CREASE BEAM WEB AND OUTBOARD CHORD AT BS 947, LBL 59, WL 208. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800407 19980508 00407 NM 1998 5 8 SWA980674 1 19980421 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 358 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 358, LBL 65, WL 216. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800408 19980508 00408 NM 1998 5 8 SWA980675 1 19980421 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED STUB FRAME AT BS 294.5, WL 209, RBL 54. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800409 19980508 00409 NM 1998 5 8 SWA980676 1 19980421 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800410 19980508 00410 NM 1998 5 8 SWA980677 1 19980422 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 970 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 970, STR 21L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998050800411 19980508 00411 NM 1998 5 8 SWA980678 1 19980422 A 5310 FUSELAGE BOEING 737 7372T4 1384492 NM BS 787/727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702SW 22054 DURING SCHEDULED TERMINAL CHECK, FOUND CRACKED 1 S-17 AT BS 787; AND 3 S-16 AT BS 727B. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998050800412 19980508 00412 NM 1998 5 8 SWA980679 1 19980422 A 5320 SHEAR TIE BOEING 737 7375H4 138449D NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED RON CHECK, FOUND CRACKED SHEAR TIE AT BS 907 INBD OF STRINGER 26L; AND BS 907 OTBD, STR 26L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800413 19980508 00413 NM 1998 5 8 SWA980680 1 19980422 A 5313 STRINGER BOEING 737 7375H4 138449D NM BS 907 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED SERVICE CHECK, FOUND GOUGED/DENTED AT BS 907 BETWEEN STRINGERS 25R AND 26R APPROX 4 LONG BY .375 DEEP. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800414 19980508 00414 NM 1998 5 8 SWA980681 1 19980422 A 5330 SKIN BOEING 737 7375H4 138449D NM BS 907 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 527SW 26569 DURING SCHEDULED SERVICE CHECK, FOUND GOUGED/DENTED SKIN LAP AFT AT BS 907 STRINGER 25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800415 19980508 00415 NM 1998 5 8 SWA980682 1 19980423 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO DOOR UPLOCK BRACKET INTERCOSTAL. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998050800416 19980508 00416 1998 5 8 SWA980683 4 19980423 A 2565 61620468 SLIDE BOTTLE BOEING 737 7373T5 NM CABIN DOOR LOW A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 667SW 23063 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EVAC, FWD SLIDE BOTTLE LOW. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998050800417 19980508 00417 NM 1998 5 8 SWA980684 1 19980423 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SCHEDULED CHECK, FOUND DENTED SKIN AT BS 500BT17, LBL 41, WL161. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800418 19980508 00418 NM 1998 5 8 SWAA980685 1 19980424 A 5753 DOOR BOEING 737 7373H4 1384600 NM LT TE FLAP JAMMED A SWAA K NONE O OTHER AP APPROACH 1 SW 07 626SW 27702 ON APPROACH TO FLL FLAPS WILL NOT EXTEND PAST 10 DEG LEADING EDGE FLAPS AND SLATS ARE ALSO IN FULL EXT. PERFORMED NORMA L LANDING AT 10 DEG (ALT FLAP EXT, NO HELP). FOUND LT INBD TE FLAP CLEARANCE DOOR JAMMED. REMOVED DOOR PER CDL. RAN F LAPS FULL UP- FULL DOWN. 2 L 7 2 4F RT A16WE 1998050800419 19980508 00419 NM 1998 5 8 SWAA980686 1 19980424 A 5310 STRUCTURE BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED RON CHECK, FOUND CRACKED AFT FUSELAGE (APPROX 3) BEHIND DOOR AND IN FRONT OF PREVIOUS REPAIR. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998050800420 19980508 00420 NM 1998 5 8 SWAA980687 1 19980424 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 519 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 519, ABOVE STR 22 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800421 19980508 00421 NM 1998 5 8 SWAA980688 1 19980424 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 PLUS 4, 947, LBL 12, WL 155; AND BS 727 PLUS 4 TO 947 , RBL 7.5, WL 155. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800422 19980508 00422 NM 1998 5 8 SWAA980689 1 19980424 A 2751 CONNECTOR BOEING 737 7375H4 138449D NM TE FLAPS DIRTY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 521SW 25320 AFTER TAKEOFF, GEAR RETRACTION FLAPS POSITIONED FROM 5 TO 1 BUT THEY DID NOT MOVE. TRIED RECYCLING LEVER BUT NOTHING HA PPENED. LOWERED FLAPS USING ALTERNATE FLAP SWITCH. AIRCRAFT RETURNED AND MADE UNEVENTFUL LANDING. RESET THE TRANSFER VALVE, CLEANED FLAP POSITION INDICATOR CANNON PLUG, SERVICED B SYS. OPS CHECK ON GRD FOR FLAPS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998050800423 19980508 00423 NM 1998 5 8 SWAA980690 1 19980424 A 5330 SKIN BOEING 737 7375H4 138449D NM BS 868-873 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN AT BS 868-873 ABOVE STR 24 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800424 19980508 00424 NM 1998 5 8 SWAA980691 1 19980424 A 5330 SKIN BOEING 737 7375H4 138449D NM BS 887 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 887, 7 BELOW STR 18R; AND BS 903, 5 BELOW STR 14L. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800425 19980508 00425 NM 1998 5 8 SWAA980692 1 19980424 A 2613 655280915 OVERHEAT LIGHT BOEING 737 7372H4 138448C NM NR 1 ENG ILLUMINATED A SWAA K NONE N FALSE WARNING AP APPROACH 1 SW 07 103SW 23109 ON FINAL APPROACH NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED FOR ABOUT 5 SECONDS THEN WENT OUT. ALL ENGINE INDICATIONS WERE NORMAL. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED ENGINE FOR LEAKS, INSPECTED LOOPS, WIRING AND CONNECTORS, NO A BNORMALITIES NOTED. REPLACED ENGINE OVERHEAT DETECTOR UNIT AND OPERATED NR 1 ENG PER AMM. 2 L 7 2 4F A16WE 1998050800426 19980508 00426 NM 1998 5 8 SWAA980693 1 19980424 A 5310 STRUCTURE BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED RON CHECK, FOUND CRACKED AFT FUSELAGE (APPROX 3) BEHIND CARGO DOOR AND IN FRONT OF PREVIOUS REPAIR. R EPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998050800427 19980508 00427 NM 1998 5 8 SWAA980694 1 19980424 A 3350 FLOOR LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357SW 26594 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT FLOOR LIGHTS ROW 14-16 INOP. RESECURED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998050800428 19980508 00428 NM 1998 5 8 SWAA980695 1 19980425 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AFT CABIN. FOUND WIRES LOOSE AND DISCONNECTED AT 3 LOCATIONS. RECONNECTED WIRES AND OPS CHK GOOD. 2 L 7 2 4F RT A16WE 1998050800429 19980508 00429 NM 1998 5 8 SWAA980697 1 19980427 A 5330 SKIN BOEING 737 7372K6 NM BS 880 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 880, 520R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800430 19980508 00430 NM 1998 5 8 SWAA980698 1 19980427 A 5330 SKIN BOEING 737 7372K6 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 727A PLUS 2 S 17R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800431 19980508 00431 NM 1998 5 8 SWAA980699 1 19980427 A 5320 DOOR FRAME BOEING 737 7373H4 1384600 NM BS 493-496 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 22938 DURING SCHEDULED D-CHECK, FOUND CORRODED DOOR FRAME COVER PLATE AT BS 493-496, RBL 25-30, WL 157. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800432 19980508 00432 NM 1998 5 8 SWAA980700 1 19980427 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 318 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 22938 DURING SCHEDULED D-CHECK, FOUND SKIN GOUGED ABOVE FWD ENTRY DOOR CUTOUT AT BS 318, WL 296 YTO WL 291, LBL 40. REMOVED A ND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800433 19980508 00433 NM 1998 5 8 SWAA980701 1 19980427 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 181 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 22938 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 181, RBL 17.5, WL 182. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800434 19980508 00434 NM 1998 5 8 SWAA980702 1 19980427 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 22938 DURING SCHEDULED D-CHECK, FOUND GOUGED INNER SURFACE OF SKIN UNDER VHF ANTENNA AT BS 500 PLUS 5, WL 149, LBL 01. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800435 19980508 00435 NM 1998 5 8 SWAA980703 1 19980427 A 5530 SKATE ANGLE BOEING 737 7373H4 1384600 NM VERT STAB CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 22938 DURING SCHEDULED D-CHECK, FOUND CHAFED RIGHT VERTICAL STAB CLOSURE SKATE ANGLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800436 19980508 00436 NM 1998 5 8 SWAA980704 1 19980427 A 5512 SKIN BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN RT HORIZ STAB-FIXED L/E. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800437 19980508 00437 NM 1998 5 8 SWAA980705 1 19980427 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 820 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND GOUGED FUSELAGE SKIN AT BS 820, STR 26R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998050800438 19980508 00438 NM 1998 5 8 UPS98226517 1 19980429 A 5330 SKIN BOEING 727 727247 138408F NM BS 823 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:SI CORROSION (C53-224-05.00-01) ON UPPER SKIN OF FUEL CELL BS 823 LBL 34 WL 196. REMOVED CORROSION BLEN DED AND REFINISHED PER ER NR 98-2375. 2 L 7 3 4F A3WE 1998050800439 19980508 00439 NM 1998 5 8 UPS98226518 1 19980429 A 5753 65327347 FITTING BOEING 727 727247 138408F NM TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:SI CORROSION (C57-581-06.00-03) NR 1 FORWARD TRACK FITTING ON ONE LUG FACE AND THE LARGE FASTENER ATTACH HOLES. REMOVED FITTING, REWORKED PER ER NR98-2405, REINSTALLED SERVICABLE FITTING. 2 L 7 3 4F A3WE 1998050800440 19980508 00440 NM 1998 5 8 UPS98226519 1 19980413 A 5347 BAC1520792 SEAT TRACK BOEING 727 727247 138408F NM BS 520-683 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:SI MAIN DECK SEAT TRACK BS 520-683 RBL 45 WL 208 HAS CORROSION ON FLANGE AND IN WELL AREA, AS MARKED. C ORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. NEW SEAT TRACK FABRICATED PER SRM 53-10-5 AND INSTALLED PER SRM 51- 10-2. 2 L 7 3 4F A3WE 1998050800441 19980508 00441 NM 1998 5 8 UPS98226520 1 19980420 A 5320 CLIP BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:SI CORROSION (C53-224-01.00-01) ON FRAME AND STRINGER CLIPS AT STA 720B STR CLIPS 5-8 RT FRAME AT STR 2- 10 RT STR CLIPS 4-9 LT CORROSION ON STRINGER CLIPS AT BS 720B STR 5 AND 6 RIGHT, 9 RIGHT AND STR 5 AND 6 LEFT WERE F OUND OUT OF LIMITS PER SRM 51-10-6. NEW CLIPS WERE INSTALLED PER SRM 53-30-2 AND MM 51-20-21. 2 L 7 3 4F A3WE 1998050800442 19980508 00442 NM 1998 5 8 UPS98226521 1 19980413 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE:SI CORROSION (C53-111-01.00-02)FWD CARGO BAY BS 720 LOWER FLANGE OF FLOORBEAM IN AND AROUND NUT PLATE HO LES LBL 45 TO RBL 25 WL 200, A 2.2 BY .9 BY .125 AREA OF THE LOWER FLANGE AT LBL 16 WAS FOUND TO BE OUT OF LIMITS PER SR M 53-10-1. A STANDARD FLOORBEAM L ANGLE EXTRUSION REPAIR WAS INSTALLED PER SRM 53-10-8, MM 51-20-151 AND MM 51-20-31. 2 L 7 3 4F A3WE 1998050800443 19980508 00443 EU 1998 5 8 QXEA9800625 1 19980428 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 BOI - EMERGENCY LIGHTS REMAIN ON IN ENTRANCE WAY. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY IN OVERHEAD OF ENTR YWAY. SYSTEM CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998050800444 19980508 00444 EU 1998 5 8 QXEA9800626 1 19980428 A 2170 COALESCER DUCT FOKKER F28 F28MK4000 4990810 EU FWD PACK FAILED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 482US 11231 SEA - BURNING SMELL AND LOUD SQUEAL COMING FROM COCKPIT PACK. STOPPED WHEN COCKPIT PACK WAS TURNED OFF. MAINTENANCE IN SPECTED AND PLACED ON MEL. LATER THAT DAY AT GEG MAINTENANCE FOUND THE INLET DUCT TO WATER SEPARATOR COLLAPSED. THE WA TER SOCK WAS INSPECTED AND LOOKED GOOD, MAINTENANCE THEN INSTALLED WATER SEPARATOR AND DUCT, PERFORMED A GROUND RUN, OPE RATIONAL CHECKS WERE NORMAL. CLEARED THE MEL. AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1998050800445 19980508 00445 NM 1998 5 8 98FDEA00303 1 19980424 A 5310 STRUCTURE BOEING 727 727225 1384077 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 1175 - 71-C209-02, HEAVY CORROSION UNDER SEALER AND STRINGER IN AREA OF STATION 720 TO 720A, TOP SIDE AFT OF CENTER B AY TO STA 720A. REMOVED CORRODED SECTION OF STRINGER AND SKIN. INSTALLED EXTERNAL SKIN DOUBLER SRM 53-30-3 AND STRINGE R AND STRINGER SPLICE PER SRM 53-10-3. 2 L 7 3 4F A3WE 1998050800446 19980508 00446 NM 1998 5 8 98FDEA00304 1 19980425 A 5311 BELLFRAME BOEING 727 727233 138408A NM BS 804 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 NR NR 0211 - 72-C236-02, BS 804, STR 14L, BELLFRAME ANGLE IS CRACKED AT FASTENER UPPER LOBE. REMOVED DAMAGED AREA OF BE LLFRAME DYE CHECKED FOR VERIFICATION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-40-3 PG 3. 2 L 7 3 4F RT A3WE 1998050800447 19980508 00447 NM 1998 5 8 98FDEA00305 1 19980425 A 5320 STRAP BOEING 727 727233 138408A NM PAX DOORWAY GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 NR 0960 BEAR STRAP AT LOWER HINGE CUTOUT FOR FWD ENTRY DOOR IS DEEPLY GOUGED. GOUGE DAMAGE WAS BLENDED OUT PER SRM 51-1 0-1, AREA WAS EDDY CURRENT INSP, NO CRACKS WERE FOUND. SKIN WAS THEN REPAIRED PER EA 7-5330-29483, DATED 4-22-98. BASE D ON S/B 727-53-198, REVISION 1 DATED 7-25-91. 2 L 7 3 4F RT A3WE 1998050800448 19980508 00448 NM 1998 5 8 98FDEA00306 1 19980423 A 5314 KEEL BEAM BOEING 727 727233 138408A NM BS 875 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 NR 0638, NR 71-C304-02, KEEL BEAM AREA LWR RT KEEL BEAM CRACKED, JUST ABOVE LWR RT FITTING APPROX BS 875. TRIMMED THE U PPER FLANGE OF KEEL BEAM CHORD, REMOVING CRACKED AREA. TREATED AND PRIMED METAL. INSTALLED REPAIR DOUBLER PER BOEING S ERVICE BULLETIN 727-53-0208 PG 45 DETAIL II DATED JAN 18, 1996. 2 L 7 3 4F RT A3WE 1998050800449 19980508 00449 NM 1998 5 8 98FDEA00307 1 19980422 A 5311 FRAME BOEING 727 727233 138408A NM BS 380 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 227FE 21673 NR 0227, BS 380, BELOW STR 5L, FRAME GOUGED ON INBD SIDE OF INBD LEG OF FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1998050800450 19980508 00450 NM 1998 5 8 98FDEA00308 1 19980420 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 0902, 72-C235-02, UPPER LOBE CORROSION ON FLOORBEAM BS 680, BLO - RBL 24. REMOVED CORROSION OUT OF LIMITS. INSTALLE D REPAIR PER SRM 53-10-8. TREATED AND PRIMED. 2 L 7 3 4F A3WE 1998050800451 19980508 00451 NM 1998 5 8 98FDEA00309 1 19980421 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 560 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 0894, 72-C235-02, UPPER LOBE, CORROSION ON FLOORBEAM, BS 560, BLO - RBL 24. REMOVED CORROSION FOUND TO BE OUT OF LIM ITS. REPAIRED PER SRM 53-10-8, 51-20-4, AND 51-30-2. 2 L 7 3 4F A3WE 1998050800452 19980508 00452 NM 1998 5 8 98FDEA00310 1 19980428 A 5313 STRINGER BOEING 727 727233 138408A NM BS 720 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 NR 0200, 72-C235-02, MAIN CARGO - 2 CRACKS TO STR 15R, BS 720B + 6 JUST FWD OF WING LIGHTS. REPAIRED STRINGER AT WING S CANNING LIGHT PER SRM 53-10-3 FIG 5. 2 L 7 3 4F RT A3WE 1998050800453 19980508 00453 NE 1998 5 8 98FDEA00311 2 19980418 A 7230 804541 COMP BLADE AIRBUS 310 A310222 3930315 EU PWA JT9 JT9D7R4E 52054 NE NR 1 ENGINE DAMAGED A FDEA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SO 25 417FE 333 98-0110 - STA-DFW - AFTER ROTATION AND DURING CLIMB, EXPERIENCED A SEVERE VIBRATION FROM NR 1 ENG. WHEN POWER PULLED BA CK BELOW 1.2 EPR, VIBRATION WOULD STOP, NO ABNORMAL READING NOTED ON VIBRATION METER. NOTICED NEED FOR RUDDER TRIM DURI NG CLIMB. REMOVED NR 1 ENG NOSE COWL, FAN BLADES, FRONT CASE PER M/M 71-11-00, 72,23-00, 72-10-00 SEE LOG 01039388 FOR NOSE COWL INSTALLATION. INSTALLED FRONT FAN CASE PER JTPD-7R4 SEC 72-33-00 RUB WEAR CHECKED OK AFTER RUN PW INSPECT XC3 74 EVM ON ENG RUN 0.4 RAN ENG PER JRH INSTALLED FAN BLADES PER PW SEC 72-31-00. 2 L 7 2 4F 4 F RT A35EU E3NE 1998050800454 19980508 00454 NM 1998 5 8 98FDEA00312 1 19980428 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 NR 0891, 72-C235-02, BS 344 FLOORBEAM LBL 60 TO RBL 25 HAS CORROSION AROUND NUTCLIP HOLES. INSTALLED REPAIR STRAPS IAW SRM 53-10-07-2 P 1-3. 2 L 7 3 4F RT A3WE 1998050800455 19980508 00455 NM 1998 5 8 98FDEA00313 1 19980428 A 5313 STRINGER BOEING 727 727233 138408A NM BS 520 DAMGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 267FE 21673 NR 1028, HOLE IN RADIUS OF STR 25L, BS 520 IN LWR FWD CARGO. CUT OUT DAMAGE AND INSTALLED 2 SPLICE REPAIRS PER 53-10-3. 2 L 7 3 4F RT A3WE 1998050800456 19980508 00456 NM 1998 5 8 98FDEA00314 1 19980428 A 5330 SKIN BOEING 727 727225 1384077 NM BS 660-668 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 0504, CORROSION ON BELLY SKIN IN LWR FWD CARGO BS 660 TO 668, STR 28R TO STR 28L. CUTOUT SKIN AND INSTALLED .080 202 4T3 DOUBLER PER 53-30-3. 2 L 7 3 4F A3WE 1998050800457 19980508 00457 NM 1998 5 8 98FDEA00315 1 19980428 A 5330 SKIN BOEING 727 727225 1384077 NM BS 685-690 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 0616, 71-C209-02, CORROSION ON BELLY SKIN BS 685-690 BLO IN FWD LOWER CARGO. CUTOUT CORROSION AND INSTALLED .080 202 4T3 DOUBLER PER 53-30-3 FIG 1 PG 8. 2 L 7 3 4F A3WE 1998050800458 19980508 00458 NM 1998 5 8 98FDEA00316 1 19980428 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 0980, 72-C235-02, UPPER LOBE, BS 720D, LBL 5, CORROSION ON FLOORBEAM AT FASTENER HOLES. REMOVED CORROSION. INSTALLE D FLOORBEAM REPAIR PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998050800459 19980508 00459 NM 1998 5 8 98FDEA00317 1 19980428 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 CORROSION ON FLOORBEAM BS 620, BL O LBL 24. CORROSION REMOVAL OUT OF LIMITS AT LBL 4. REPAIRED FLOORBEAM PER SRM 53-10 -8. REPAIRED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998050800460 19980508 00460 NM 1998 5 8 98FDEA00318 1 19980428 A 5311 FRAME BOEING 727 727225 1384077 NM BS 600 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR 0220, DENTS IN BELLFRAME (6 TOTAL) BS 600, STR 23L TO 25L DEFORMING WEB. CUT OUT DAMAGE AND INSTALLED TYP BELL FRAME REPAIR 51-40-3 W/EXCEPTION OF EA 7-5310-29458. 2 L 7 3 4F A3WE 1998050800461 19980508 00461 WP 1998 5 8 98FDEA00319 1 19980429 A 3260 SWITCH DOUG DC10 DC1010F 3022111 WP LT MLG FAILED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 058FE 46705 98-0109, PILOTS PANEL RED LEFT GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. S/O PANEL LEFT GEAR LIGHT EXTINGU ISHED. PERFORMED RECYCLE OF GEAR AND LIGHT REMAINED ILLUMINATED ON PILOTS PANEL FOR LEFT GEAR. FEF1 32-30 AF-L.T/S AND FOUND LT MLG DOOR UPLATCH PROX SWITCH BAD 274911. WIRED PROX SWITCH AT TERMINAL STRIP EMPLOYEE NR 44389 OPS CHECK LMLG DOOR UPLOCK PROX SWITCH M/M 32-61-03 STEPS 13 A,B,C CHECKS GOOD. EMPLOY NR 31716 VERIFIED INSTALLATION EMPLOY NR 30089 2 PER 31-61-03. 2 L 7 3 4F A22WE 1998050800462 19980508 00462 WP 1998 5 8 ABXA9800373 1 19980427 A 5720 57696015 DOUBLER DOUG DOUG DC8 DC862 3021970 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 805AX 45906 LEFT STAB WING ABOVE NR 2 PYLON CRACKED JUST OUTBOARD OF AUX TANK MOUNTING SURFACE. REPAIRED IAW ABX REA D857-22682-MR. 2 L 7 4 4F 4A25 1998050800463 19980508 00463 WP 1998 5 8 ABXA9800374 1 19980427 A 5400 991550030 ANGLE DOUG DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND THE RIGHT PYLON INTERIOR ATTACH ANGLE CRACKED AT THE AFT ENGINE MOUNT UPPER SPAR LUG. REPLACED AN GLE IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998050800464 19980508 00464 WP 1998 5 8 ABXA9800395 1 19980427 A 5230 3914025502 FITTING DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT DOOR INTERIOR FITTING P/N 3914025-502 CRACKED AT DOOR LEADING EDGE NEX T TO UPLATCH MECHANISM. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998050800465 19980508 00465 WP 1998 5 8 ABXA9800396 1 19980427 A 5230 39140252 FITTING DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND AFT LOWER CARGO COMPARTMENT DOOR INTERIOR FITTING P/N 3914025-2 CRACKED. REMOVED AND REPLACED FIT TING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998050800466 19980508 00466 WP 1998 5 8 ABXA9800397 1 19980427 A 5230 39140251 FITTING DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND AFT LOWER CARGO DOOR FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998050800467 19980508 00467 WP 1998 5 8 ABXA9800398 1 19980427 A 5320 49113831 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 313 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND FRAME MOUNT FITTING AT STATION 313, RIGHT SIDE CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998050800468 19980508 00468 WP 1998 5 8 ABXA9800399 1 19980427 A 5320 995773925 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP FRAME 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND SHEAR-TIE CRACKED BETWEEN LONGERONS 14L AND 16L AT FRAME 945. REPLACED SHEAR-TIE IAW DC9 SRM 51-3 0-2. 2 L 7 2 4F A6WE 1998050800469 19980508 00469 WP 1998 5 8 ABXA9800400 1 19980427 A 5320 99577397 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP FRAME 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 902AX 47426 DURING C-CHECK, FOUND SHEAR-TIE CRACKED BETWEEN LONGERONS 14R AND 16R AT FRAME 945. REPLACED SHEAR-TIE IAW DC9 SRM 51-3 0-2. 2 L 7 2 4F A6WE 1998050800470 19980508 00470 WP 1998 5 8 ABXA9800401 1 19980427 A 5320 49125401 FITTING DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 DURING C-CHECK, FOUND FRAME VERTICAL SUPPORT FITTING CRACKED AT STATION 1041 AND LBL 30. REPLACED FITTING IAW DC9 SRM 5 1-30-5. 2 L 7 2 4F A6WE 1998050800471 19980508 00471 WP 1998 5 8 ABXA9800402 1 19980329 A 5712 5769470 RIB DOUG DOUG DC8 DC862 3021970 WP WS 797.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 797.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998050800472 19980508 00472 WP 1998 5 8 ABXA9800409 1 19980416 A 5712 57696001 RIB DOUG DOUG DC8 DC862 3021970 WP WS 635 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT WING LEADING EDGE RIB AT STATION XFS 635.00 CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DC8 SRM 51-1-21, 51-1-2 0D AND DRAWING K05056. 2 L 7 4 4F 4A25 1998050800474 19980508 00474 WP 1998 5 8 ABXA9800411 1 19980428 A 5320 3917624513N FITTING DOUG DOUG DC9 DC933F 302207A WP PAX DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, FOUND FITTING CRACKED IN AFT ENTRY DOOR, RIGHT JAMB, FWD SIDE, 36 ABOVE FLOOR LINE. REPLACED FITTING IA W DC9 SRM 51-30-22 AND 51-30-5. 2 L 7 2 4F A6WE 1998050800475 19980508 00475 WP 1998 5 8 ABXA9800412 1 19980429 A 5530 591212379 ANGLE DOUG DOUG DC9 DC941 302207N WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 DURING C-CHECK, FOUND VERTICAL STABILIZER AFT SPAR LEFT VERTICAL Z ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AN D DACO DWG 5912123. 2 L 7 2 4F A6WE 1998050800476 19980508 00476 WP 1998 5 8 ABXA9800413 1 19980428 A 5320 995773925 SHEAR TIE DOUG DOUG DC9 DC933F 302207A WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 945 BELOW LONGERONS 14L AND 15L. REPLACED SHEAR-TIE IAW DC9 SRM 51-3 0-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998050800477 19980508 00477 WP 1998 5 8 ABXA9800414 1 19980429 A 5530 591212380 ANGLE DOUG DOUG DC9 DC941 302207N WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 DURING C-CHECK, FOUND VERTICAL STABILIZER AFT SPAR, RIGHT VERTICAL Z ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND DACO DWG 5912123. 2 L 7 2 4F A6WE 1998050800478 19980508 00478 WP 1998 5 8 ABXA9800415 1 19980429 A 5320 992343512 ANGLE DOUG DOUG DC9 DC941 302207N WP BS 776 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 DURING C-CHECK, FOUND ATTACH ANGLE CRACKED STATION 776, RIGHT WHEEL WELL AT LONGERON 20R. REPLACED ANGLE IAW DC9 SRM 51 -30-5, 51-30-1 AND DACO DWG 9923435. 2 L 7 2 4F A6WE 1998050800479 19980508 00479 WP 1998 5 8 ABXA9800416 1 19980429 A 5320 9911840166 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1171 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 990AX 47493 DURING C-CHECK, FOUND SHEAR-TIE CRACKED AT STATION 1171 BETWEEN LONGERONS 2R AND 3R. REPLACED SHEAR-TIE IAW DC9 SRM 51- 30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998050800480 19980508 00480 WP 1998 5 8 ABX9800417 1 19980429 A 5712 576990316 RIB DOUG DOUG DC8 DC861 3021952 WP WS 195 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 851AX 45940 RIGHT WING LEADING EDGE, LOWER RIB CRACKED AT STATION XFS 195.0. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998050800481 19980508 00481 WP 1998 5 8 ABXA9800418 1 19980429 A 5315 591013712 FLOORBEAM DOUG DOUG DC9 DC933F 302207A WP BS 370-427 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 934AX 47462 DURING C-CHECK, FOUND LONGITUDINAL FLOORBEAM EXFOLIATED AT STATION 370-371 AND 426-427, RBL 42 ABOVE THE FLC DOOR CUTOUT . REPLACED FLOORBEAM IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998050800482 19980508 00482 WP 1998 5 8 ABXA9800419 1 19980428 A 5610 5613217507 WINDOW DOUG DC9 DC933F 302207A WP LT COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED LINKAGE ON CAPTAIN'S CLEARVIEW WINDOW. 2 L 7 2 4F A6WE 1998050800483 19980508 00483 WP 1998 5 8 ABXA9800420 1 19980428 A 5610 36407341 WINDOW DOUG DC9 DC933F 302207A WP LT COCKPIT STICKING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. LUBRICATED UPPER HINGE LOCK. 2 L 7 2 4F A6WE 1998050800484 19980508 00484 WP 1998 5 8 ABXA9800431 1 19980428 A 5753 47544201 BOLT DOUG DC8 DC863 302198A WP LT TE FLAP SHEARED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 DURING PREFLIGHT, FOUND LEFT INBOARD FLAP SUPPORT BEARING BOLT SHEARED. REPLACED BOLT IAW DC8 MM 27-51-3. 2 L 7 4 4F 4A25 1998050800485 19980508 00485 NM 1998 5 8 SCNA98036 1 19980421 A 3397 WIRE BOEING 727 7272A1 138407F NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 EMERGENCY TRACK LIGHT AT ROW 18C IS INOPERATIVE. REPAIRED BROKEN WIRING AND FUNCTIONALLY CHECKED GOOD. 2 L 7 3 4F A3WE 1998050800486 19980508 00486 1998 5 8 DHL98742001 4 19980430 A 3442 RADAR BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 742DH 21290 WITH STAB ON 0 DEGREE TILT, 0 BANK IN LEVEL FLT GROUND RETURN ON LEFT ONE-THIRD OF SCREEN. WITH 30 DEGREE BANK RIGHT, LE FT HALF OF SCREEN FILLED WITH GROUND RETURN. IN RIGHT TURN, LEFT HALF OF SCREEN FILLED WITH GROUND RETURN. FOUND ROLL GAIN AT 2-3 DEGREE HIGH. ADJUSTED ROLL GAIN. INSPECTED RADAR FOR MOISTURE. NONE FOUND, OPS CHECK PER MM. 2 L 7 3 4F A3WE 1998050800487 19980508 00487 NM 1998 5 8 VNAA9804024 1 19980424 A 3244 26107012 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG FLAT A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 437JS 28818 1708 3055 DURING THE POST FLIGHT INSPECTION, THE RIGHT HAND OUTBOARD TIRE WAS NOTED TO BE FLAT. THE INSPECTION REVEALED A POSSIBL E OVERHEAT CONDITION HAD OCCURED. AS A PRECAUTION, MAINTENANCE REPLACED ALL MAIN LANDING GEAR WHEELS AND BRAKES, AND PE RFORMED AN OPERATIONAL CHECK OF THE ANTI-SKID SYSTEM, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-41-10, 32-42-07,3 2-42-10. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998050800488 19980508 00488 NM 1998 5 8 TWAA9803901 1 19980317 A 2120 AIR DISTRIBUTION BOEING 767 7673Q8 NM CABIN ODOR A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 634TW 28132 JFK - FLT 840 - DURING FIRST REVENUE FLIGHT OF ACFT, TWO FLIGHT ATTENDANTS AND SEVERAL PASSENGERS REPORTED SICK DUE TO P LASTIC SMELL IN THE AIRCRAFT. ACCOMPLISHED PACK BURN-OUT, CHECKED OVENS AND INTERIOR LIGHTS. NO PROBLEM OR ODOR DETECT ED. (X) 2 L 7 2 4F RT A1NM 1998050800491 19980508 00491 EU 1998 5 8 USAAF98036 1 19980411 A 3234 7115381 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAILED A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 866US 18492 11310 PIT - ON APPROACH, GREEN 'NOSE' GEAR INDICATION DID NOT ILLUMINATE. CREW DID A GO-AROUND PROCEDURE AND RECYCLED THE LAN DING GEAR. ALL THREE GREEN GEAR INDICATORS ILLUMINATED PROPERLY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR SELECTOR VALVE AND RIGGED THE VALVE. THEY ALSO LUBRICATED THE NOSE GEAR ASSEMBLY. (X) 2 L 7 2 4F RT 1998050800492 19980508 00492 NE 1998 5 8 USAASB98090 2 19980406 A 7261 3051157040 SEAL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 523AU 23858 MEM - FL 175 - AT 28,000 FEET, 138 MILES WEST OF MEM, THE NR 1 ENGINE HAD A LOSS OF OIL AS INDICATED ON THE OIL QUANTITY INDICATOR. FLIGHT DIVERTED INTO MEM AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. THE NR 1 ENGINE WAS NOT SHUT DOWN IN-FLIGHT. MAINTENANCE FOUND THE NR 1 ENGINE CSD GARLOCK SEAL LEAKING. REPLACED SAME. SERVICED ENGINE O IL. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F RT A16WE E2GL 1998050800493 19980508 00493 NM 1998 5 8 USAA980160 1 19980412 A 5330 SKIN BOEING 737 737201 1384454 NM BS 740 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 226US 49824 21815 ROA - DURING C-5 CHECK, FOUND 2 INCH CRACK AT STA 740, S17R FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER EA 5 1596. (X) 2 L 7 2 4F A16WE 1998050800494 19980508 00494 NE 1998 5 8 USAASB98091 2 19980407 A 7314 378200 FUEL PUMP BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE DEFECTIVE A A USAA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 268AU 22880 BWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPON D TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WIT HOUT INCIDENT. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE CHECKED THROTTLE CABLE S FOR FREEDOM OF MOVEMENT. CABLE REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP AND FUEL CONTROL UNIT. ENGINE RUN, OPE RATION CHECK AND LEAK CHECK GOOD. REF: OPERATOR CONTROL NR 98ZZZX1641. (X) 2 L 7 2 4F 4 F A16WE E2EA 1998050800496 19980508 00496 NE 1998 5 8 USAASB98092 2 19980408 A 7261 3051157040 SEAL BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 523AU 23858 IND - FL 1588 - DURING CRUISE, CREW NOTICED THE NR 1 ENGINE OIL QUANTITY HAD DECREASED FROM 4 GALLONS TO 1-3/4 GALLONS D URING FLIGHT. THE ONLY INDICATION THE CREW HAD WAS LOW OIL QUANTITY. FLIGHT DIVERTED TO IND DUE TO OIL LOSS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE ENGINE WAS NOT SHUT DOWN. MAINTENANCE FOUND A DAMAGED SEA L AT THE CSD/GEARBOX SPLINE ON THE NR 1 ENGINE. REPLACED SEAL PER MM 72-60-00. SERVICED ENGINE OIL AND PERFORMED ENGIN E GROUND RUN AT HIGH POWER SETTINGS. NO LEAKS NOTED. (X) 2 L 7 2 4F 4 F RT A16WE E2GL 1998050800497 19980508 00497 EU 1998 5 8 RAIA980401 1 19980401 A 3060 C40543 BRUSH BLOCK BAG JETSTM JETSTM3201 1500217 EU LT PROPELLER FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 875JX 12903 500 875 STL - FLT 7466 - LEFT PROPELLER DEICE FAILED IN-FLIGHT. MAINTENANCE REPLACED LEFT PROPELLER DEICE BRUSH BLOCK. ACFT TT : 12,902.7 HOURS. (X) 2 L 7 2 4T RT A56EU 1998050800498 19980508 00498 EU 1998 5 8 RAIA980402 1 19980401 A 2910 1379007D479 LINE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA B O EMER. DESCENT OTHER K FLUID LOSS CR CRUISE 1 CE 03 430AM 14466 880 STL - FLT 7479 - LOST HYDRAULIC PRESSURE, MANUALLY PUMPED GEAR DOWN. MAINTENANCE INSPECTED AND REPLACED HYDRAULIC PRESS URE LINE AT LEFT ENGINE ZONE TWO. (X) 2 L 7 2 4T RT A56EU 1998050800499 19980508 00499 NE 1998 5 8 PIVA11079 2 19980407 A 7200 ENGINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A65AR 52043 NE NR 1 FAILED A PIVA E ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION UK UNKNOWN 1 WP 13 711PK 2682 SH3696 97044 SHUT DOWN OF ONE ENGINE IN-FLIGHT PER FOLLOWING PILOT REPORT IN PIVA AFML PAGE 102793, NR 1 ENGINE FAILED IN-FLIGHT. NO TED COMPRESSOR STALL FOLLOWED BY 3 LARGE EXPLOSIONS AND FIRE ON RIGHT SIDE OF ENGINE. ENGINE SECURED AND EMERGENCY DECL ARED. THE SPECIFIC CAUSE OF ENGINE FAILURE HAS NOT YET BEEN ESTABLISHED. NO FIRE DAMAGE TO ENGINE NACELLE OR AIRCRAFT WAS DETERMINED. (X) 2 H 7 2 4T 4 T A41EU E4EA 1998050800500 19980508 00500 NM 1998 5 8 EIAA980140 1 19980204 A 5415 FITTING BOEING 747 747273C 1384896 NM PYLON WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 DURING 'C5/D' CHECK INSPECTION, ALL PYLON WING UPPER LINK FITTING OUTER LUG FACES FOUND CORRODED. PYLON NR 1 AND NR 4, CORROSION BLENDED OUT. BUSHINGS FABRICATED AND INSTALLED IAW SB 54-2164 AND HAECO RS R57-04-33646. PYLON NR 2 AND NR 3 , CORROSION BLENDED OUT AND REPAIRED IAW SB 54-2164, AND HAECO RS R57-04-33621. (X) 2 L 7 4 4F A20WE 1998050800501 19980508 00501 NM 1998 5 8 EIAA980135 1 19980219 A 5347 TRACK BOEING 747 747273C 1384896 NM BS 570 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 DURING 'C5/D' CHECK INSPECTION, FORWARD CARGO COMPARTMENT TIE-DOWN TRACK FOUND CRACKED AT BS 570 RBL 25. REPAIRED TRACK IAW SRM 53-10-05 FIG 5. (X) 2 L 7 4 4F A20WE 1998050800502 19980508 00502 NM 1998 5 8 EIAA980136 1 19980219 A 5210 FITTING BOEING 747 747273C 1384896 NM CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, FORWARD CARGO COMPARTMENT NR 4 DOOR SILL LATCH CAM TRUSS FITTING CORRODED. REPLAC ED IAW SRM 51-10-01. (X) 2 L 7 4 4F A20WE 1998050800503 19980508 00503 NM 1998 5 8 EIAA980150 1 19980319 A 5320 GUIDE BOEING 747 747132 1384882 NM BS 850 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 DURING 'B' CHECK INSPECTION, FORWARD CARGO COMPARTMENT, CENTER GUIDE UNDER FLOOR PANELS CRACKED AT STATION 850. REPAIRE D IAW SRM 51-40-02 FIG 1. (M) 2 L 7 4 4F A20WE 1998050800504 19980508 00504 NM 1998 5 8 EIAA980121 1 19980215 A 5315 FLOOR BEAM BOEING 747 747273C 1384896 NM BS 1760 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1760 FLOOR BEAM UPPER CHORD DAMAGED LBL 15 - LBL 22. (X) 2 L 7 4 4F A20WE 1998050800506 19980508 00506 SO 1998 5 8 ASOA98026 1 19980407 A 2910 HYDRAULIC LINE EMB 120 EMB120RT SO RT MLG WW SPLIT A ASOA O OTHER K J F FLUID LOSS WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 SO 11 235AS 120047 HKG - FLT 7468 - INBOUND DFW, CREW DECLARED AN EMERGENCY DUE TO LOSS OF BLUE HYDRAULIC SYSTEM. A ZERO-FLAP LANDING WAS MADE AND AIRCRAFT WAS A TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. DFW MAINTENANCE F0UND THE RIGHT ENGINE HYDRAULIC P UMP PRESSURE LINE SPLIT. FABRICATED NEW SECTION OF PRESSURE LINE AND PERMASWEGED IN. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (X) 2 L 7 2 4T RT A31SO 1998050800507 19980508 00507 NM 1998 5 8 EIAA980127 1 19980217 A 5411 FRAME BOEING 747 747273C 1384896 NM NR 1 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FRAME CRACKED AT NAC 163. REPAIRED IAW SRM 51-10-01. (X) 2 L 7 4 4F A20WE 1998050800508 19980508 00508 EU 1998 5 8 GAIA9839 2 19980410 A 7200 ENGINE CVAC 240 240D 2422660 WP RROYCE DART DART5424 54522 EU LEFT FAILED A GAIA E A ENGINE SHUTDOWN UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 07 94279 18638 3071 101 DURING CLIMB AND APPROACHING 11,500 FEET TO LEVEL OFF AT 12,000 FEET, THERE WAS A FLASH AND THE LEFT ENGINE AUTOFEATHERE D. ALL INDICATIONS WERE NORMAL. AN EMERGENCY WAS DECLARED, THE ACFT LANDED AT IND (WHICH WAS THE POINT OF DEPARTURE) W ITH NO DIFFICULTY. THE ENGINE HAS BEEN INSPECTED AND DETERMINED THERE WAS AN INTERNAL FAILURE IN THE ENGINE NOSE SECTIO N. THE ENGINE WAS REMOVED AND REPLACED WITH A SERVICEABLE ENGINE. THE DAMAGED ENGINE WILL BE SENT OUT FOR REPAIR. (X) 2 L 7 2 4R 4 T RT A793 E5EU 1998050800509 19980508 00509 NM 1998 5 8 EIAA980123 1 19980210 A 5400 BRACE BOEING 747 747273C 1384896 NM NR 1 PYLON WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON FORWARD DIAGONAL BRACE FITTING HAS THREE SLOTTED HOLES. REPAIRED IAW H AECO RS R54-54-33605. (X) 2 L 7 4 4F A20WE 1998050800510 19980508 00510 NM 1998 5 8 EIAA980126 1 19980217 A 5413 STRINGER BOEING 747 747273C 1384896 NM NR 1 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON, CRACKED STRINGER AT NAC 166 OUTBOARD SIDE OF PYLON. REPAIRED IAW SRM 52-40-04 FIG 2. (X) 2 L 7 4 4F A20WE 1998050800511 19980508 00511 NM 1998 5 8 EIAA980138 1 19980219 A 5400 FITTING BOEING 747 747273C 1384896 NM WS 669 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, RT WS 669.5 BULKHEAD PYLON SUPPORT FORWARD INBOARD BACK-UP FITTING CRACKED AT STR 24. BACK-UP FITTING REPLACED IAW SB 54A2159. (X) 2 L 7 4 4F A20WE 1998050800512 19980508 00512 NM 1998 5 8 EIAA980133 1 19980114 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 370 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, RT SIDE BS 370 STR NR 6 SKIN CRACKED AT ONE TOP ROW COUNTERSUNK FASTENER HOLE OF L AP SPLICE APPROX .0625 INCH IN LENGTH RUNNING AFT. CUT OUT SKIN LAP, REPAIRED IAW EV EO 53-747-1032-90 REV B AND BOEING DWG 65B28215 SHEET 1. (X) 2 L 7 4 4F A20WE 1998050800513 19980508 00513 NM 1998 5 8 EIAA980132 1 19980115 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 370 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LT SIDE BS 370 STR NR 6 SKIN CRACKED AT TWO TOP ROW COUNTERSUNK FASTENER HOLES OF THE LAP SPLICE, BOTH RUNNING FORWARD AND AFT APROXIMATELY .0624 INCH IN LENGTH. CUT OUT SKIN SLAP, REPAIRED IAW SRM 53- 30-03 FIG 26. (X) 2 L 7 4 4F A20WE 1998050800514 19980508 00514 NM 1998 5 8 EIAA980134 1 19980219 A 5311 FRAME BOEING 747 747273C 1384896 NM BS 438 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, BS 438 BETWEEN STR 25 - STR 26 FRAME WEB CRACKED. REPAIRED FRAME WEB IAW HAECO RS 53-11-33658. (X) 2 L 7 4 4F A20WE 1998050800515 19980508 00515 NM 1998 5 8 TWAA9805402 1 19980410 A 3350 582243 BATTERY PACK BOEING 767 767205 1385121 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 651TW 23058 JFK - DURING MAINTENANCE CHECK OF THE AIRCRAFT, THE EGRESS LIGHTS WERE FOUND FLASHING FROM ROW 30 TO ROW 35 AFT RT SIDE OF CABIN. REPLACED BATTERY PACK. CHECK-C 3-27-98 LAX. (X) 2 L 7 2 4F RT A1NM 1998050800516 19980508 00516 1998 5 8 SABA980023 4 19980331 A 6122 89741016 GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 962AE 962 CLT/AHN - FLT 5166 - SHORTLY AFTER DEPARTING CLT, THE RIGHT ENGINE BETA WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO CLT WITH NO OTHER PROBLEMS. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED AT CLT. MAINTENANCE REMOVED AND REPLACED THE RIGHT PROP GOVERNOR. AIRCRAFT TEST FLIGHT COMPLETED. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A56EU 1998050800517 19980508 00517 WP 1998 5 8 TWAA9805401 1 19980411 A 2530 4110001143 COFEE MAKER DOUG DC9 DC931 3022065 WP GALLEY SHORTED A TWAA H DEACTIVATE SYST/CIRCUITS A B FLAME/FIRE SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 979Z 24 47343 STL - FLT 531 - NR 2 COFFEE MAKER SHOT FLAMES AND SMOKE. TURNED OFF COFFEE MAKER. REPLACED COFFEE MAKER. CHECK-C 12-3 -97 STL. (X) 2 L 7 2 4F A6WE 1998050800518 19980508 00518 WP 1998 5 8 TWAA9805301 1 19980407 A 2913 314195 PUMP DOUG DC9 DC932 3022066 WP LT ENGINE FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 922L 47108 STL - FLT 599 - DURING CRUISE, THE LEFT HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. THE SYSTEM PRESSURE FLUCTUATED BETWEE N 1800 - 2800 PSI REGARDLESS OF PUMP SELECTION, HI-LOW-OFF. REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP MFG PN 31419 5. OP-15 11-15-97 MCI. (X) 2 L 7 2 4F A6WE 1998050800519 19980508 00519 NM 1998 5 8 EIAA980146 1 19980312 A 5315 FLOOR BEAM BOEING 747 747132 1384882 NM BS 500 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 89285 19896 MZJ - DURING 'C4' CHECK INSPECTION, FLOOR BEAM AT STA 500 RLB 46 UPPER CHORD CRACKED. REPAIRED FLOOR BEAM UPPER CHORD I AW SRM 53-10-07 FIG 8. (X) 2 L 7 4 4F A20WE 1998050800520 19980508 00520 NM 1998 5 8 EIAA980143 1 19980228 A 5320 WEB BOEING 747 747SR46 NM BS 1480 LT CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 53618 21033 MZJ - DURING 'C6' CHECK INSPECTION, LT BODY GEAR WHEEL WELL BULKHEAD BS 1480 HAS EXFOLIATION CORROSION BEHIND BRAKE SHUT TLE VALVE. REPAIRED IAW ECRA 478-53-080-02. (X) 2 L 7 4 4F A20WE 1998050800521 19980508 00521 NM 1998 5 8 EIAA980142 1 19980228 A 5320 WEB BOEING 747 747SR46 NM BS 1480 RT CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 53618 21033 MZJ - DURING 'C6' CHECK INSPECTION, RT BODY GEAR WHEEL WELL BULKHEAD BS 1480 HAS CORROSION BEHIND BRAKE SHUTTLE VALVE. R EPAIRED IAW ECRA 478-53-081-2. (X) 2 L 7 4 4F A20WE 1998050800522 19980508 00522 NM 1998 5 8 EIAA980141 1 19980228 A 5320 STIFFENER BOEING 747 747SR46 NM BS 1241 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 53618 21033 MZJ - DURING 'C6' CHECK INSPECTION, RT WING GEAR WHEEL WELL VERTICAL STIFFENER ON BS 1241 BULKHEAD FOURTH FROM OUTBOARD HAS CORROSION OUT OF LIMITS. REPLACED STIFFENER IAW SRM 51-10-01. (X) 2 L 7 4 4F A20WE 1998050800523 19980508 00523 NM 1998 5 8 EIAA980130 1 19980219 A 5315 FLOOR BEAM BOEING 747 747273C 1384896 NM BS 1880 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1880 FLOOR BEAM UPPER CHORD DAMAGED AT LBL 48. REPAIRED IAW SRM 51-40-03 FIG 2. (X) 2 L 7 4 4F A20WE 1998050800524 19980508 00524 NM 1998 5 8 EIAA980131 1 19980219 A 5320 PANEL BOEING 747 747273C 1384896 NM BS 1241 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, LT WING WHEEL WELL BS 1241 CANTED B/K CRACKED AT LT UPPER CORNER LBL 90 AT TRIM AI R DUCT CUT-OUT. PANEL REPLACED IAW SB 747-53-2329. (X) 2 L 7 4 4F A20WE 1998050800525 19980508 00525 NM 1998 5 8 EIAA980124 1 19980210 A 5400 BRACE BOEING 747 747273C 1384896 NM NR 4 PYLON WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DRUING 'C5/D' CHECK INSPECTION, NR 4 PYLON FORWARD DIAGONAL BRACE FITTING HAS THREE SLOTTED HOLES. REPAIRED IAW H AECO RS R54-54-33605. (X) 2 L 7 4 4F A20WE 1998050800526 19980508 00526 NM 1998 5 8 EIAA980129 1 19980217 A 5414 SKIN BOEING 747 747273C 1384896 NM NR 4 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 4 PYLON INBOARD SKIN CRACKED AT NAC STA 180. REPAIRED IAW HAECO RS R54-51-3360 9. (X) 2 L 7 4 4F A20WE 1998050800527 19980508 00527 NM 1998 5 8 EIAA980128 1 19980217 A 5414 SKIN BOEING 747 747273C 1384896 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 3 PYLON LT OUTER SKIN CRACKED AT NAC STATION 180. REPAIRED IAW HAECO RS R54-51 -33636. (X) 2 L 7 4 4F A20WE 1998050800528 19980508 00528 NM 1998 5 8 EIAA980145 1 19980228 A 5711 SPAR CAP BOEING 747 747SR46 NM WS 934 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 53618 21033 MZJ - DURING 'C6' CHECK INSPECTION, RT WING LOWER SPAR CAP HAS CORROSION AT WS 934. REPAIRED IAW ECRA 478-57-084-02. (X ) 2 L 7 4 4F A20WE 1998050800529 19980508 00529 NM 1998 5 8 EIAA980149 1 19980319 A 5414 SKIN BOEING 747 747132 1384882 NM NR 4 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 82743 19898 HKG - DURING B-CHECK INSPECTION, NR 4 ENGINE PYLON RT SKIN LOWER EDGE, DOUBLER AND SKIN CRACKED. REPAIRED IAW SRM 54-30 -03 FIG 35 AND FIG 36. (X) 2 L 7 4 4F A20WE 1998050800530 19980508 00530 NM 1998 5 8 EIAA980144 1 19980228 A 5720 CHORD BOEING 747 747SR46 NM WS 499 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 478EV 53618 21033 MZJ - DURING 'C6' CHECK INSPECTION, LT WING TRAILING EDGE UPER T-CHORD AT WS 499 IS CRACKED. REPAIRED IAW ECRA 478-57-0 83-02. (X) 2 L 7 4 4F A20WE 1998050800531 19980508 00531 NM 1998 5 8 EIAA980137 1 19980219 A 5720 SHEAR TIE BOEING 747 747273C 1384896 NM WS 669 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, RT WS 669.5 UPPER FORWARD MOST SHEAR TIE CAP CRACKED. REPAIRED IAW SB 57-2273 FIG 8 AND FIG 9. (X) 2 L 7 4 4F A20WE 1998050800532 19980508 00532 NM 1998 5 8 EIAA980122 1 19980215 A 5315 FLOOR BEAM BOEING 747 747273C 1384896 NM BS 1720 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, AFT CARGO COMPARTMENT BS 1720 FLOOR BEAM UPPER CHORD DAMAGED BL ZERO - RBL 12. WE B REPAIRED IAW SRM 51-40-02, FIG 1, AND ANGLE REPLACED IAW SRM 51-10-01. (X) 2 L 7 4 4F A20WE 1998050800533 19980508 00533 1998 5 8 SABA980021 4 19980331 A 3421 258719343 GYRO BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILED A SABA A UNSCHED LANDING O OTHER AP APPROACH 1 SO 33 928AE 928 CLT/HKY - FLT 5092 - ON APPROACH TO HKY, THE PILOT'S ARTIFICIAL HORIZON WENT BLANK. DUE TO HEAVY RAIN, PILOT HAD TO ABO RT APPROACH TO HKY. AIRCRAFT RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE NR 1 DG. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998050800534 19980508 00534 WP 1998 5 8 SABA980024 2 19980402 A 7320 8961153 GASKET BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE TORN A SABA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 SO 33 170PC 717 P63234 CLT/GSP - FLT 9101 - THE LEFT ENGINE WAS SHUT DOWN IN-FLIGHT BY THE AIRCREW. THE LEFT ENGINE WAS HAVING SEVERE TORQUE F LUCTUATION BETWEEN ZERO PERCENT AND 70 PERCENT. THE AIRCRAFT WAS 12 MILES OUT, ON DESCENT TO GSP. IN-FLIGHT EMERGENCY DECLARED. EMERGENCY PROCEDURES USED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FROM CLT, FOUND THE P-3 LINE LOOSE. RE-SECURED THE P-3 LINE AND REPLACED THE P-3 GASKET. (X) 2 L 7 2 4T 4 T RT A21EU E4WE 1998050800535 19980508 00535 CE 1998 5 8 S2YA98009 1 19980318 A 3060 4E31961 BRUSH BLOCK BEECH 1900 1900D 1154162 CE RT PROPELLER WORN A S2YA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 13 92SK 572 UE92 MKE/MQT - FLT 1233 - WHILE IN CRUISE FLIGHT, CREW NOTICED THE RT PROP HEAT INDICATING ONLY 8 AMPS IN AUTO OR MANUAL MODE S. THE WEATHER IN THE MQT AREA INDICATED ICING CONDITIONS, SO THE CREW ELECTED TO RETURN TO MKE AFTER CONSULATION WITH MAINTENANCE. AFTER AN UNEVENTFUL LANDING, MAINTENANCE FOUND THE RT PROP DE-ICE BRUSH BLOCK WITH WORN BRUSHES. THE BRUS H BLOCK WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998050800536 19980508 00536 1998 5 8 TWAA9805201 4 19980407 A 3418 9650041027 COMPUTER DOUG DC9 DC941 302207N WP E/E COMPT FAILED A TWAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 933L 299 47617 SAT - FLT 656 - DURING TAXI, THE STALL INDICATION FAILURE LIGHT CAME ON. SYSTEM NR 2 WOULD NOT RESET. REPLACED THE NR 2 ANGLE OF ATTACK TRANSDUCER MFG P/N 800987-17 AND NR 2 STALL WARNING COMPUTER MFG P/N 965-0041-027. OP-15 12-08-96 STL . REF: OPERATOR CONTROL NR 98ZZZX1642. (X) 2 L 7 2 4F A6WE 1998050800537 19980508 00537 1998 5 8 98ZZZX1642 4 19980407 A 3418 80098717 TRANSDUCER DOUG DC9 DC941 302207N WP E/E COMPT FAILED A TWAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CE 05 933L 47617 SAT - FLT 656 - DURING TAXI, THE STALL INDICATION FAILURE LIGHT CAME ON. SYSTEM NR 2 WOULD NOT RESET. REPLACED THE NR 2 ANGLE OF ATTACK TRANSDUCER MFG P/N 800987-17 AND NR 2 STALL WARNING COMPUTER MFG P/N 965-0041-027. OP-15 12-08-96 STL . REF: OPERATOR CONTROL NR TWAA9805201. 2 L 7 2 4F A6WE 1998050800541 19980508 00541 WP 1998 5 8 TWAA9805604 1 19980404 A 5240 FITTING DOUG DC9 DC951 3022051 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 406EA 47686 STL - DURING OP 9 MAINTENANCE CHECK, FOUND FITTING CRACKED AT FORWARD SERVICE DOOR JUST ABOVE BAYONET NR 3 BEAM, HAS .25 INCH CRACK. INSTALLED NEW FITTING PER SRM 51-30-2/4/5/6. (X) 2 L 7 2 4F RT A6WE 1998050800547 19980508 00547 NM 1998 5 8 EIAA980125 1 19980217 A 5400 WEB BOEING 747 747273C 1384896 NM NR 1 PYLON MISINSTALLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING 'C5/D' CHECK INSPECTION, NR 1 PYLON MID-SPAR WEB CUT-OUT AREA ON REWORK HAS AS EXTRA ROW OF FASTENERS. REP AIRED IAW HAECO RS R54-53-33608. (X) 2 L 7 4 4F A20WE 1998050800548 19980508 00548 EU 1998 5 8 MALA976098 1 19980411 A 3233 AIR124110 BOLT SAAB SF340 340B 7860101 EU NLG ACTUATOR BENT A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 595MA 340B216 DURING GEAR RETRACTION THE INTRANSIT LIGHT WOULD NOT EXTINGUISH. MAINTENANCE REPLACED ACTUATOR BOLT ON NOSE LANDING GEA R, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998050800549 19980508 00549 NM 1998 5 8 MALA976111 1 19980429 A 3350 1013075 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 832MA 341 DURING INSPECTION, 3 RED FLOOR TRACK LIGHTS INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998050800550 19980508 00550 1998 5 8 MALA976112 4 19980430 A 3442 071131900 RT UNIT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 826MA 330 DURING FLIGHT, THE WEATHER RADAR INOP, OCCASIONALLY PAINTS SPOKES. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RADAR R/T, SYSTEM TESTS IAW DHC-8 MM 34. 2 H 7 2 4T RT A13NM 1998050800551 19980508 00551 EU 1998 5 8 MALA976113 1 19980429 A 3020 INTAKE LIGHT SAAB SF340 340B 7860101 EU RT ENGINE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 426XJ 426 DURING FLIGHT, THE RIGHT INTAKE LIGHT ILLUMINATED, IT APPEARED TO CYCLE IN OVER TEMP MODE. AIRCRAFT RETURNED TO DTW. M AINTENANCE SWITCHED TO SPARE THERMISTOR T1 TO T4 AND T3 TO T5. RAN AIRCRAFT FOR 25 MINUTES ALL IAW SAAB 340 MM CHECKS G OOD AT THIS TIME. 2 L 7 2 4T RT A52EU 1998050800552 19980508 00552 NM 1998 5 8 CALA9800721 1 19980429 A 2530 8103010000 OVEN BOEING 737 7373T0 1384582 NM AFT GALLEY DIRTY A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 69348 23341 23586 THE CREW REPORTED SMOKE COMING FROM NR 1 AND NR 2 AFT GALLEY OVENS IN FLIGHT. THE SMOKE WAS MOMENTARY. THE FLIGHT WAS CONTINUED TO DEN WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. FOOD RESIDUE WAS FOUND ON THE HEATING ELEMENTS OF BOTH OVENS. THE ELEMENTS WERE CLEANED AND BOTH OVENS WERE OPERATED WITH NO SMOKE DETECTED. 2 L 7 2 4F RT A16WE 1998050800553 19980508 00553 WP 1998 5 8 CALA9800722 1 19980429 A 3233 ARG73765509 ACTUATOR DOUG DC10 DC1030 3023501 WP LT MLG FAILED A CALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION TO TAKEOFF 1 SW 09 13066 14101 46591 THE LT MLG WOULD NOT RETRACT AFTER TAKEOFF. CYCLING THE GEAR DID NOT HELP. FUEL WAS DUMPED AND THE GEAR WAS VISUALLY C ONFIRMED DOWN BY TOWER. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG THE LANDI NG GEAR SEVERAL TIMES, BUT COULD NOT DUPLICATE THE PROBLEM. THE LT GEAR RETRACT CYLINDER AND LT GEAR DOWNLOCK BUNGEE CY LINDER WERE REMOVED AND REPLACED IAW MM 32-33-01 AS A PRECAUTIONARY MEASURE. THE LANDING GEAR WAS SWUNG FOUR MORE TIMES AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1998050800554 19980508 00554 WP 1998 5 8 CALA9800723 1 19980429 A 2910 B-NUT DOUG DC9 DC982 3022082 WP BRAKE CON VLV LOOSE A CALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 478AC 48063 WHEN HYDRAULICS WERE SWITCHED TO LOW DURING CLIMBOUT. THE LEFT HYDRAULIC SYSTEM PRESSURE AND QUANTITY WENT TO ZERO. TH E LEFT SWITCHES WERE TURNED TO OFF AND THE LEFT HYDRAULIC QUANTITY SLOWLY INCREASED TO 16 QUARTS. THE FLIGHT WAS CONTIN UED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A LOOSE B-NUT ON LT DUAL BRAKE CONTROL VALVE. THE B-NUT WAS TIGHTENED. THE LT ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE LT HYDRAU LIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998050800555 19980508 00555 NM 1998 5 8 CALA9800724 1 19980429 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69333 23571 THE EMERGENCY TRACK LIGHTS AT LAST FIVE ROWS OF AIRCRAFT WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE F OUND A WIRE BROKEN AT SEAT 21. THE WIRE WAS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED. 2 L 7 2 4F RT A16WE 1998050800556 19980508 00556 NM 1998 5 8 UPS98226339 1 19980408 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 INSPECTION, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY OPERATION IS INTERMITTENT AND BACK COVER IS MISSING. REMOVED A ND REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT ASSEMBLY AS PER M/M 33-50-01, OP'S CHECKS GOOD. 2 L 7 3 4F A3WE 1998050800557 19980508 00557 NM 1998 5 8 UPS98226479 1 19980423 A 5320 SHEAR TIE BOEING 727 727247 138408F NM BS 660 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-02) FWD CARGO BAY SHEAR TIE AT BS 660 AT STR 26 RT ON FWD FACE. CORROSION OUT OF LIMITS. REMOVED SHEAR TIE AND INSTALLED NEW SHEAR TIE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998050800558 19980508 00558 NM 1998 5 8 UPS98226480 1 19980422 A 5753 651920812 TRACK BOEING 727 727247 138408F NM NR 2 TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) IN NR 2 FLAP TRACK CENTER MOUNT HOLE. FLAP TRACK REMOVED, REPAIRED AND RETURNED TO SERVICEABLE CONDITION BY NEWELL CORP JOB NR 11804 TRACK TO BE INSTALLED ON TC NR C57-581-04-3D. 2 L 7 3 4F A3WE 1998050800559 19980508 00559 NM 1998 5 8 UPS98226481 1 19980422 A 5753 651920812 TRACK BOEING 727 727247 138408F NM NR 1 TE FLAP CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE-SI, CORROSION (C57-581-06.00-03) NR 1 FLAP TRACK FWD LUG INTERFACE. FLAP TRACK REMOVED, REPAIRED AND RE TURNED TO SERVICEABLE CONDITION AT MACHINE SHOP TO BE INSTALLED ON TC NR C57-581-04-3D. 2 L 7 3 4F A3WE 1998050800560 19980508 00560 NM 1998 5 8 UPS98226482 1 19980421 A 5330 SKIN BOEING 727 727247 138408F NM BS 470 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE-SI, CORROSION (6-53-20) AT ANTENNA CUT OUT BOTTOM OF FUSELAGE 20 AFT OF E-BAY DOOR, BS 470 WL 138.5 BL 0 . REMOVED CORROSION, FABRICATED DOUBLER AND INSTALLED IAW SRM 53-30-1, 51-10-6, 53-30-3, 51-30-5. 2 L 7 3 4F A3WE 1998050800561 19980508 00561 WP 1998 5 8 UPS98826522 1 19980413 A 5320 56449315 DOUBLER DOUG DC8 DC873F 302199F WP BS 8-70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, FINGER DOUBLER IS SPLIT IN HALF FROM STA 8 TO STA 70 AT STR 31R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5644931 AND SRM 53-3-3 FIG 1. 2 L 7 4 4F RT 4A25 1998050800562 19980508 00562 WP 1998 5 8 UPS98826524 1 19980420 A 5320 9887940507 ANGLE DOUG DC8 DC873F 302199F WP BS 1320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, STA 1320 LWR FWD FLANGE OF FLOORBEAM HAS EXFOLIATION CORROSION BL 0 TO RBL 36. REMOVED, FABRICATED A ND INSTALLED REPLACEMENT ANGLE IAW DWG 9887940 AND SRM 51-9-0. 2 L 7 4 4F RT 4A25 1998050800563 19980508 00563 WP 1998 5 8 UPS98826526 1 19980402 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 80 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, LT NOSE W/W TUNNEL PRESSURE WEB AT STA -80 AND LBL 36 TO 48 IS CORR. REPAIRED AREA IAW SRM 53-3-3 FI G 6 AND 52-2-0 FIG 23. 2 L 7 4 4F RT 4A25 1998050800564 19980508 00564 NM 1998 5 8 98FDEA00320 1 19980430 A 3610 SHUTOFF VALVE BOEING 727 727233 138408A NM NR 3 BLEED AIR INOPERATIVE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 222FE 20933 REPEAT WRITE-UP FROM DISCREPANCY NR 01199454 ENGINE NR 3 STRUT OVERHEAT LIGHT ON. OVERHEAT LIGHT CAME ON PASSING FLIGHT LEVEL 250 AND APPROXIMATELY 20 MINUTES INTO FLIGHT. BOTH PACKS ON NR 1 BLEED OFF, NR 2 OPEN NR 3 OPEN CLIMB POWER WITH IN PARAMETERS. ADMINISTERED RED TABS CHECKLIST AND THE LIGHT WENT OUT. CONTINUED FLIGHT ON ONE PACK FOR REST OF FLIGHT . PULLED NR 3 STRUT PANELS AND RAN ENGINE TO CHECK FOR BLEED LEAKS. NO LEAKS FOUND BUT NR 3 BLEED AIR SHUTOFF VALVE FOU ND TO BE INOPERATIVE. REMOVED AND REPLACED NR 3 SHUTOFF VALVE AND OPERATIONAL CHECKED AND LEAK CHECKED NORMAL. RAN NR 3 ENGINE AT HIGH POWER AND STRUT OVERHEAT CHECKS NORMAL. REINSTALLED PANELS, OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998050800565 19980508 00565 NM 1998 5 8 98FDEA00321 1 19980501 A 5320 69473751 CLIP BOEING 727 727233 138408A NM BS 698 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 STRINGER 26R CLIP AT BS 698 CORRODED. *S/D* FOUND STRINGER CLIP AT BS 698, STR 26R TO BE OUT OF LIMITS. INSTALLED NEW STR CLIP IAW FED-EX SRM 53-10-1 AND SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998050800566 19980508 00566 NM 1998 5 8 98FDEA00322 1 19980501 A 5320 66222231 SPLICE BOEING 727 72721C 138400M NM BS 480 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 WHILE WORKING NR 0990, FOUND BS 480 SPLICE PLATE CRACKED BETWEEN STRINGER 2 RT AND 3 RT. *S/D* REMOVED DAMAGED SPLICE PLATE, AND INSTALLED NEW SPLICE PLATE IAW FED-EX SRM 51-30-2, 51-30-5. 2 L 7 3 4F A3WE 1998050800568 19980508 00568 WP 1998 5 8 ABXA9800421 1 19980329 A 5755 56551681 SPOILER DOUG DOUG DC8 DC862 3021970 WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT SPOILER HAD WIDESPREAD CORROSION AND DELAMINATION. REPLACED ALL HONEYCOMB CORE, DOUBLERS AND SKIN. 2 L 7 4 4F 4A25 1998050800569 19980508 00569 WP 1998 5 8 ABXA9800422 1 19980325 A 5753 5701446502 VANE DOUG DOUG DC8 DC861 3021952 WP RT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 845AX 46157 RIGHT VANE HAD WIDESPREAD DELAMINATION AND CORROSION. REPLACED ALL HONEYCOMB CORE DOUBLERS AND SKIN. 2 L 7 4 4F 4A25 1998050800570 19980508 00570 WP 1998 5 8 ABXA9800423 1 19980416 A 5712 576949015 RIB DOUG DOUG DC8 DC862 3021970 WP WS 628.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT WING LEADING EDGE RIB AT STATION XFS 628.750 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DC8 SRM 51-1-21 AND 51-1-20D AND DRAWING K05056. 2 L 7 4 4F 4A25 1998050800571 19980508 00571 WP 1998 5 8 ABXA9800424 1 19980416 A 5320 2537717 CUSP DOUG DOUG DC8 DC862 3021970 WP BS 320-340 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT HAND CUSP BETWEEN STATION 320 TO 340 IS CRACKED. REPAIRED CUSP IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998050800572 19980508 00572 WP 1998 5 8 ABXA9800425 1 19980416 A 5311 5640234 FRAME DOUG DOUG DC8 DC862 3021970 WP BS 1360 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STATION 1360 FRAME FORWARD SIDE OF STRINGER 36 IS CORRODED. REPAIRED FRAME IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998050800573 19980508 00573 WP 1998 5 8 ABXA9800426 1 19980416 A 5320 97540221 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 500 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STATION 500 RIGHT HAND FLOORBEAM END FITTING IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21 AND DRAWING 9754022. 2 L 7 4 4F 4A25 1998050800574 19980508 00574 WP 1998 5 8 ABXA9800427 1 19980416 A 5712 57703756 RIB DOUG DOUG DC8 DC862 3021970 WP WS 297.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 297.5 IS CRACKED AT THE AFT, UPPER END. REPAIRED RIB IAW DC8 SRM 51-1-20D AN D DRAWING K05056. 2 L 7 4 4F 4A25 1998050800575 19980508 00575 WP 1998 5 8 ABXA9800428 1 19980416 A 5313 7549121509 LONGERON DOUG DOUG DC8 DC862 3021970 WP BS 550-560 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LONGERON 36 AT STATION 550 TO 560 HAS CORROSION. REPLACED LONGERON IAW DC8 SRM 53-2-2 AND 53-2-0. 2 L 7 4 4F 4A25 1998050800576 19980508 00576 WP 1998 5 8 ABXA9800429 1 19980416 A 5320 3755822511 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 570 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 SHEAR TIE FITTING AT STATION 570 BETWEEN LONGERONS 36R AND 35R IS CRACKED. REPLACED SHEAR TIE FITTING IAW DC8 SRM 53-2- 0. 2 L 7 4 4F 4A25 1998050800577 19980508 00577 WP 1998 5 8 ABXA9800430 1 19980416 A 5320 37546251 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1180-1200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STATION 1180 TO 1200 LONGERON 34R SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D AND ABX REA D 853-22783. 2 L 7 4 4F 4A25 1998050800578 19980508 00578 WP 1998 5 8 ABXA9800432 1 19980428 A 2612 D5020 LOOP DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 812AX 46126 670969 FIRE WARNING ON NR 4 ENGINE. SECURED ENGINE AND DISCHARGED FIRE BOTTLE. MASTER FIRE WARNING CAME ON MOMENTARILY WITH N O LIGHT IN ANY LEVER OR ON FLIGHT ENGINEER PANEL. TESTED EACH ENGINE FIRE WARNING SYSTEM, NR 4 ENGINE WOULD NOT TEST. M ASTER WARNING FLASHED ON AND OFF. AFTER ENGINE WAS SECURED FIRE WARNING TESTED OK. FOUND BROKEN PIN IN NR 4 LOWER LOOP CONNECTOR. REPLACED LOWER LOOP. FIRE WARNING TESTED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1998050800579 19980508 00579 NM 1998 5 8 DL72S980915 1 19980428 A 5320 WEB BOEING 727 727232 1384082 NM BS 1240 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 FOUND ON D1 LETTER CHK, .25 INCH CRACK IN VENTRAL STAIR TORQUE BOX AT LWR LIGHTENING HOLE STA 1240. ROUTE OUT CRACK PER MM 53-11-0. 2 L 7 3 4F A3WE 1998050800580 19980508 00580 NM 1998 5 8 DL72S980916 1 19980428 A 5320 WEB BOEING 727 727232 1384082 NM BS 1313 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 FOUND ON D1 LETTER CHK, .25 INCH CRACK IN VENTRAL STAIR TORQUE BOX UPPER LIGHTENING HOLE STA 1313 LT. ROUTE OUT CRACK P ER MM 53-11-0. 2 L 7 3 4F A3WE 1998050800581 19980508 00581 NM 1998 5 8 DL72S980917 1 19980428 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR SEPARATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 FOUND ON D1 LETTER CHK, TRAILING EDGE OF RT ELEVATOR SEPARATED JUST O/B OF TRIM TAB. INSTALLED FASTENERS PER MM 55-20-0 . 2 L 7 3 4F A3WE 1998050800582 19980508 00582 NM 1998 5 8 DL72S980918 1 19980428 A 5520 FASTENERS BOEING 727 727232 1384082 NM LT ELEVATOR FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 LT ELEVATOR TRAILING EDGE SEPARATED/FASTENERS SHEARED AT SEVERAL LOCATIONS ALONG TRAILING EDGE. INSTALLED FASTENERS PER MM 55-20-0. 2 L 7 3 4F A3WE 1998050800583 19980508 00583 NM 1998 5 8 DL757980919 1 19980428 A 3246 WHEEL BOEING 757 757232 1384965 NM LT MLG DAMAGED A DALA K NONE O OTHER LD LANDING 1 SO 27 639DL 23993 NR 5 MAIN DEPARTED A/C ON LDG. REPLACED WHEEL ASSY. 2 L 7 2 4F RT A2NM 1998050800584 19980508 00584 NM 1998 5 8 DL72K980920 1 19980428 A 3350 BATTERY NS996 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA 21232 EMERGENCY EXIT LIGHT O/H AISLE ROW 4 INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998050800585 19980508 00585 WP 1998 5 8 DLL10980921 1 19980424 A 5730 SKIN LKHEED 1011 10113851 5265010 WP WS 477 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 FOUR FASTENER HOLES IN THE LOWER WING SKIN AT IWS 477 AND STRINGER 17 WERE FOUND CRACKED ON BOTH WINGS. THE CRACKS ARE THE SUBJECT OF SID AD 95-20-04, R1 (SID NR 57-3-2). THE CRACKED HOLES WERE OVERSIZED TO REMOVE THE CRACKS AND ALUMINU M BUSHINGS WERE INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 364606-14AD, REV B. 2 L 7 3 4F A23WE 1998050800586 19980508 00586 NM 1998 5 8 DL73S980922 1 19980423 A 5330 655298892 SKIN BOEING 737 737232 1384475 NM BS 935 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 THE FUSELAGE SKIN AT STRINGER 21L AND BETWEEN FS 927 AND 947.8 WAS DAMAGED BY GROUND EQUIPMENT. THE DAMAGED SKIN WAS CU TOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 364605-14. THE UNDERLYING STRINGER WAS REPAIRED PER B737 SRM 53-10-3. 2 L 7 2 4F RT A16WE 1998050800587 19980508 00587 NM 1998 5 8 DL72S980923 1 19980429 A 3350 POWER PACK 90052 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 538DA VA6447 22076 ON L/O, FOUND F/C OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY POWER PACK AND POWER PACK RACK. CKS NML AS PER M/M. 2 L 7 3 4F A3WE 1998050800588 19980508 00588 NM 1998 5 8 DL72S980924 1 19980422 A 5320 COWL BOEING 727 727232 1384082 NM LT ENGINE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LT FWD ENG COWL SUPPORT RING LIP WORN AT AFT FWD COWL SUPPORT MATING SURFACE, AFT LT EMPENNAGE 6-11 O'CLOCK. REMOVED DA MAGED AREA, WITHIN LIMITS PER SRM 53-10-1 FIG 1 SECTION AT 6:00 AND 7:00 OUT OF LIMITS. FABRICATED REPAIR PER M/M 53-11 -0 PG 801 SECTION 7:00 TO 11:00 WITHIN LIMITS PER M/M 53-11-0 PG 801. OK TO TREAT, PAINT, INSTL 6-7 O'CLOCK. DOUBLER TR EATED AND PAINTED, INSTALLED REPAIR ANGLE PER M/M 53-11-0 PG 801. 2 L 7 3 4F A3WE 1998050800589 19980508 00589 NM 1998 5 8 DL76P980925 1 19980429 A 2761 ACTUATOR 252T13013 BOEING 767 767332 1382001 NM NR 8 SPOILER FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION LD LANDING 1 SO 27 1402A 2501A 25989 NUMBER 8 SPOILER CASTING FAILED AT FILTER. REPLACED NUMBER 8 SPOILER ACTUATOR. 2 L 7 2 4F RT A1NM 1998050800590 19980508 00590 NM 1998 5 8 DL72S980926 1 19980430 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 FOUND ON C1 LETTER CK, .75 INCH CRACK FUSE SKIN UPPER AFT CORNER OF R-5 WINDOW CUTOUT. REPAIR PER MM 53-30-3. 2 L 7 3 4F A3WE 1998050800591 19980508 00591 WP 1998 5 8 DLL19980927 1 19980430 A 3350 337001090 BATTERY PACK LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 760DH 193Y1194 EMERG LT BATTERY PACK INOP. WOULD NOT CHARGE. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1998050800592 19980508 00592 NM 1998 5 8 DL72S980931 1 19980318 A 5753 652163261 DOUBLER BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 REPAIR DOULBERS CRACKED IN THREE PLACES 19, 32 AND 37 FROM I/B END OF LOWER AFT CHORD ANGLE NR 2 MIDFLAP. REPAIRED BY R EPLACING DOUBLERS PER BOEING M/M 57-52-0 FIG 802. ON NON-ROUTINE CARDS NR 005932 AND 005933. 2 L 7 3 4F A3WE 1998050800593 19980508 00593 NM 1998 5 8 DLM11980936 1 19980430 A 2910 HYD LINE DOUG MD11 MD11 3023602 NM RT LE SLAT ACT LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 810DE 48565 LOST NUMBER 3 HYDRAULIC SYSTEM, DIVERTED TO NRT. FOUND OUTBOARD SLAT ACTUATOR PRESSURE LINE LEAKING. SWAGGED SLEEVE ON LINE PER M/M 20-10-01-2. 2 L 7 3 4F RT A22WE 1998050800594 19980508 00594 SO 1998 5 8 SWIA971160 1 19980403 A 5522 SKIN EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ELEVATOR LIGHTNING STRIKE A SWIA O OTHER C F.O.D. CL CLIMB 1 NM 07 295UX 120295 AIRCRAFT TOOK A LIGHTNING STRIKE WHILE AIRBORNE. RETURNED TO RDM. RDM, INSPECTED AIRCRAFT PER MM 05-50-01 AND FOUND LI GHTNING STRIKE TO LEFT ELEVATOR. NO OTHER DAMAGE FOUND. RELEASED AIRCRAFT FOR SPECIAL FLIGHT. 2 L 7 2 4T 4 T RT A31SO E20NE 1998050800595 19980508 00595 EA 1998 5 8 SWIA971161 1 19980403 A 3260 PSEU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE E/E COMPT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 408SW 7055 AFTER DEPARTURE THE FOLLOWING CAUTION MESSAGES APPEARED: L AOA HEAT, L STATIC, L PITOT, PITOT BASE HEAT, FOLLOWED QRH EL ECTED TO RETURN TO SLC AIRPORT. REMOVED AND REPLACED PSEU. OPS CHECKS GOOD IAW MM 33-00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 1998050800596 19980508 00596 EA 1998 5 8 SWIA971164 1 19980407 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE CARGO COMPT MALFUNCTIONED A SWIA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 407SW 7034 SMOKE CARGO WARNING CAME ON INFLIGHT. PERFORMED EMERGENCY PROCEDURE AND RETURNED TO SLC. BOTH FIRE BOTTLES WERE FIRED. REPLACED FAULTY SMOKE DETECTOR AND REPLACED CARGO BAY FIRE BOTTLE WITH SERVICEABLE UNIT . 2 L 7 2 4F 4 F RT A21EA E15NE 1998050800597 19980508 00597 NE 1998 5 8 RRXA98082 2 19980428 A 7200 ENGINE DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE FAILED A RRXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 15 991CF 45801 NR 4 ENG LOUD BANG, HEAVY VIBRATION, DECAYING N1, N2 AND INCREASING EGT, ACCOMPANIED BY VIOLENT YAW TO THE RIGHT. HEAVY VIBRATION FELT WITH THROTTLE ADVANCEMENT. PREPARED AIRCRAFT FOR THREE ENGINE FERRY, INSPECTED AIRCRAFT AND FOUND IT SA FE FOR THE FLIGHT INTENDED. WRITE-UP STILL OPEN TILL ENGINE CHANGE. 2 L 7 4 4F 4 F 4A25 1E8 1998050800598 19980508 00598 WP 1998 5 8 RRXA98083 1 19980429 A 5242 DOOR DOUG DC8 DC871 302199A WP A/E COMPT NOT LATCHED A RRXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 15 811AL 46099 UNABLE TO PRESSURIZE AIRCRAFT. RESECURE A AND E DOOR FWD, OPS CHECKS GOOD NO DEFECTS NOTED. 2 L 7 4 4F 4A25 1998050800599 19980508 00599 NM 1998 5 8 VNAA9804025 1 19980428 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 436JS 49238 637 3052 DURING THE PREFLIGHT INSPECTION, THE EMERGENCY FLOOR LIGHTING AT ROWS FOUR, FIVE AND SIX, WERE FOUND TO BE INOPERATIVE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT, TO FACILITATE REPAIR. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY INCIDENT. PIT MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY BATTERY PACK IN ACCORD ANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998050800600 19980508 00600 NE 1998 5 8 TC8A98020 2 19980430 A 7260 COVER PLATE DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE LT ENG GEAR BOX LOOSE A TC8A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 23 184SK 45981 669604 PRECAUTIONARY SHUTDOWN NR 3 ENGINE ON SHORT FINAL. OIL PRESSURE STARTED FLUCTUATING BETWEEN 45 PSI AND YELLOW ARC. SHU T IT DOWN WHEN ITWENT BELOW THE RED LINE. REMOVED, INSPECTED AND REPLACED OIL FILTER PER MM 79-20-7, NO METAL FOUND IN FILTER, LEAK CHECKS OK. ON ENGINE RUN FOUND OIL LEAKING AT GEARBOX COVER PLATE FWD OF P AND D VALVE. 16 QUARTS OF OIL ADDED AT ARRIVAL. TIGHTENED LOOSE BOLTS AND RESAFETIED COVER PLATE. ENGINE RUN UP CHECKS AND LEAK CHECKS OK PER MM 71- 00. 2 L 7 4 4F 4 F 4A25 1E8 1998050800601 19980508 00601 WP 1998 5 8 MWEA98501 1 19980420 A 5720 4912001 CLIP DOUG DC9 DC932 3022066 WP WS 111 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING LOWER STRINGER CLIP CRACKED AT STRINGER 17 STATION XRS 111. MTC REMOVED AND REPLACED CLIP. 2 L 7 2 4F A6WE 1998050800602 19980508 00602 WP 1998 5 8 MWEA98502 1 19980420 A 5720 4911462 CLIP DOUG DC9 DC932 3022066 WP WS 137 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION ON LOWER OUTBOARD RIB ATTACH CLIP AT XRS 137 BETWEEN STRINGER 11 AND LOWER CHORD OF LEFT WING. REMOVED FABRIC ATED AND REPLACED CLIP. 2 L 7 2 4F A6WE 1998050800603 19980508 00603 WP 1998 5 8 MWEA98503 1 19980420 A 5730 5911280 PLATE DOUG DC9 DC932 3022066 WP WS 111.5 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING STRINGER 22 AT XRS 111.5 HAS A CRACKED REINFORCEMENT PLATE. REMOVED FABRICATED AND REPLACED REINFORCEMENT PLA TE. 2 L 7 2 4F A6WE 1998050800604 19980508 00604 WP 1998 5 8 MWEA98504 1 19980420 A 5720 4912003 CLIP DOUG DC9 DC932 3022066 WP WS 111 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING ATTACH CLIP AT STATION XEW 111 BETWEEN STRINGER 21 AND 22 WAS FOUND CORRODED. MTC REMOVED FABRICATED AND INST ALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 1998050800605 19980508 00605 WP 1998 5 8 MWEA98505 1 19980420 A 5720 4911499 CLIP DOUG DC9 DC932 3022066 WP WS 111 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING RIB ATTACH CLIP AT XRS 111 BETWEEN STRINGER 19 AND 20 WAS FOUND CORRODED. REMOVED OLD CLIP, FABRICATED AND IN STALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 1998050800606 19980508 00606 WP 1998 5 8 MWEA98506 1 19980420 A 5720 4911393 FITTING DOUG DC9 DC932 3022066 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 OUTBOARD FLAP ATTACH FITTING ON FWD SIDE OF AFT SPAR HAS A CRACKED BOLT HOLE. MTC REMOVED OLD FITTING FABRICATED AND IN STALLED REPLACEMENT FITTING. 2 L 7 2 4F A6WE 1998050800607 19980508 00607 WP 1998 5 8 MWEA98507 1 19980420 A 5730 9919348 PLATE DOUG DC9 DC932 3022066 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT WING CORROSION ON T-CAP TO AFT SPAR SPLICE PLATE. MTC REMOVED OLD PLATE FABRICATED AND INSTALLED REPLACEMENT PLATE . 2 L 7 2 4F A6WE 1998050800608 19980508 00608 WP 1998 5 8 MWEA98508 1 19980420 A 5720 9919348 SPLICE DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 DURING D-CHECK, CORROSION WAS FOUND ON RT WING T-CAP TO AFT SPAR SPLICE PLATE. MTC REMOVED OLD SPLICE FABRICATED AND IN STALLED REPLACEMENT SPLICE PLATE. 2 L 7 2 4F A6WE 1998050800609 19980508 00609 WP 1998 5 8 MWEA98509 1 19980420 A 5720 491207 CLIP DOUG DC9 DC932 3022066 WP WS 20 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING STATION XCW 20 TIE CLIP IS GOUGED AND HAS AN OVERSIZED HOLE. REMOVED OLD CLIP AND FABRICATED AND INSTALLED R EPLACEMENT CLIP. 2 L 7 2 4F A6WE 1998050800610 19980508 00610 WP 1998 5 8 MWEA98510 1 19980420 A 5720 4912014 CLIP DOUG DC9 DC932 3022066 WP WS 20 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RT WING STATION XCW 20.0 RT TIE CLIP R20-14 IS DENTED. MTC REMOVED DAMAGED CLIP FABRICATED AND INSTALLED REPLACEMENT CL IP. 2 L 7 2 4F A6WE 1998050800611 19980508 00611 WP 1998 5 8 MWEA98511 1 19980420 A 5713 5919236 STRINGER DOUG DC9 DC932 3022066 WP WS 69-111.5 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 CORROSION ON AFT LOWER LEG OF STRINGER 14 XRS 69 TO XRS 111.5 RT WING. REMOVED CORROSION AND FABRICATED REPAIR STRAP, I NSTALLED STRAP. 2 L 7 2 4F A6WE 1998050800612 19980508 00612 WP 1998 5 8 MWEA98512 1 19980420 A 5713 5919238 STRINGER DOUG DC9 DC932 3022066 WP WS 69 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING STRINGER 16 AT STATION XRS 69 WAS FOUND TO HAVE CORROSION. MTC REMOVED CORROSION FABRICATED AND INSTALLED RE PAIR STRAP ON STRINGER. 2 L 7 2 4F A6WE 1998050800613 19980508 00613 WP 1998 5 8 MWEA98513 1 19980420 A 5720 3919251 CLIP DOUG DC9 DC932 3022066 WP WS 164 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 RIGHT WING CORROSION ON OUTBOARD RIB ATTACH CLIP AT XRS 164 STRINGER 11 TO AFT SPAR. MTC REMOVED OLD CLIP FABRICATED AN D INSTALLED REPLACEMENT CLIP. 2 L 7 2 4F A6WE 1998050800614 19980508 00614 WP 1998 5 8 MWEA98514 1 19980420 A 5330 5911426 SKIN DOUG DC9 DC932 3022066 WP BS 996 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 OUTER FUSELAGE SKIN HAS TWO DRILL MARKS AT FS 996 LONGERON 6L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998050800615 19980508 00615 WP 1998 5 8 MWEA98515 1 19980420 A 5315 99115451 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 408 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 212ME 47701 FLOORBEAM AT FS 408 HAS AN IMPROPER REPAIR DOUBLER ON THE RIGHT HAND END OF BEAM. MTC REMOVED IMPROPER REPAIR, FABRICAT ED PROPER REPAIR DOUBLER AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998050800616 19980508 00616 WP 1998 5 8 MWEA98516 1 19980420 A 5313 3925966503 LONGERON DOUG DC9 DC932 3022066 WP BS 585 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 FORWARD CARGO COMPARTMENT LONGERON 2R FS 585 HAS DRILL STARTS ON INBOARD RADIOS. MTC REMOVED AND REPLACED LONGERON 25R. 2 L 7 2 4F A6WE 1998050800617 19980508 00617 WP 1998 5 8 MWEA98517 1 19980420 A 5330 5910228 SKIN DOUG DC9 DC932 3022066 WP BS 1087-1121 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 LEFT FUSELAGE SKIN FROM FS 1087 TO FS 1121 WAS FOUND GOUGED AND DENTED. MTC REMOVED SKIN, FABRICATED AND INSTALLED REPL ACEMENT SKIN. 2 L 7 2 4F A6WE 1998050800618 19980508 00618 EU 1998 5 8 HEEA0013977 1 19980420 A 6321 350A32050002 BRAKE SNIAS 350 AS350B2 8680813 EU ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 533 3004 ROTOR BRAKE OIL SOAKED AND WORN. 1 G 7 1 3U H9EU 1998050800620 19980508 00620 EU 1998 5 8 HEEA0013979 1 19980420 A 6420 350A33211905 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 965 2873 T/R HEAD BEARINGS WORN. 1 G 7 1 3U H9EU 1998050800621 19980508 00621 GL 1998 5 8 HEEA0013980 2 19980420 A 7250 23001967 TURBINE WHEEL 23038241 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 3RD STAGE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J 1738 CAT25228 S826 CAE836370 ENGINE REMOVED DUE TO TURBINE 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED: SEVERE SULFIDATION ON ALL NR3 WHEEL BLADES. SCRAPPED NR3 WHEEL AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U H3EU E4CE 1998050800622 19980508 00622 GL 1998 5 8 HEEA0013981 2 19980420 A 7250 6886407 TURBINE WHEEL 23038241 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J 1738 CAT25228 S826 CAE836370 ENGINE REMOVED DUE TO TURBINE 1750 HOUR INSPECTION. UPON INSPECTION OF TURBINE PARTS NOTED: CATASTROPHIC SULFIDATION O N ALL NR1 WHEEL BLADES. SCRAPPED NR1 WHEEL AND REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U 3 U H3EU E4CE 1998050800623 19980508 00623 SW 1998 5 8 HEEA0013982 1 19980420 A 2435 206062200123 BRUSH BELL 407 407 SW START/GEN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 1817 53003 PERFORMED 300 HOUR INSPECTION AND FOUND BRUSHES EXCESSIVELY WORN. REPLACED BRUSHES AND PACKING. 1 G 7 1 3U O H2SW 1998050800624 19980508 00624 SW 1998 5 8 HEEA0013984 1 19980420 A 6230 214010500105 SWASHPLATE BELL 214 214ST 1182106 SW M/R LOOSE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 2911 28101 SWASHPLATE LOWER HUB NUT FOUND UNDER TORQUE. 2 G 7 2 4U H10SW 1998050800625 19980508 00625 1998 5 8 HEEA0013985 4 19980420 A 3457 0845000000 GPS SKYNAV5000 BOLKMS 117 BK117B1 5626012 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 INTERMITTENTLY LOSING POWER AND SHUTTING DOWN. NOT AIRCRAFT WIRING. DOES SAME WHEN POWERED UP ON BENCH. FOUND UNIT TO LOCK UP AND CHANGES MODES WITHOUT PRESSING ANY KEYS. 1 G 7 2 3U H13EU 1998050800626 19980508 00626 1998 5 8 HEEA0013986 4 19980420 A 3414 412075009105 INDICATOR BELL 412 412 1182202 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 AIRSPEED IND EXCESSIVE CASE LEAKAGE AND READ OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998050800627 19980508 00627 SW 1998 5 8 HEEA0013987 1 19980420 A 2611 302319 SMOKE DETECTOR BELL 412 412 1182202 SW FUSELAGE FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 SMOKE DET FAILS FUNCTION TEST. 1 G 7 2 4U H4SW 1998050800628 19980508 00628 1998 5 8 HEEA0013988 4 19980420 A 2210 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2148K 36001 AFCS COMPUTER FAILED. ROLL ACTUATOR HUNTS BOTH DIRECTIONS. 1 G 7 2 4U H4SW 1998050800629 19980508 00629 1998 5 8 HEEA0013989 4 19980420 A 3425 4018369902 FLIGHT DIRECTOR BEECH 200 200BEECH 1152920 CE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 789DS BB478 FLT DIR INOPERATIVE. 1 L 7 2 4T A24CE 1998050800630 19980508 00630 SW 1998 5 8 HEEA0013990 1 19980420 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 1305 28140 STARTER WILL NOT DISENGAGE WHEN APPROPRIATE NG% IS ACHIEVED. MUST BE MANUALLY DISENGAGED. 2 G 7 2 4U H10SW 1998050800631 19980508 00631 SW 1998 5 8 HEEA0013993 1 19980421 A 6520 206040440103 PINION BELL 206 206L1 1182107 SW T/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 SILVER COATING FLAKING FROM GEAR TOOTH. 1 G 7 1 3U H2SW 1998050800632 19980508 00632 GL 1998 5 8 HEEA0013994 2 19980421 A 7250 6890040 NOZZLE SHIELD 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE 665 CAT30033F S787 CAE834699 ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR1 NOZZLE SHIELD INNER BAND AS MARKED AND CRACK AT POSITIONING LUGS AS MARKED. 1 G 7 2 3U 3 U H3EU E4CE 1998050800633 19980508 00633 GL 1998 5 8 HEEA0013995 2 19980421 A 7250 23062752 NOZZLE SHIELD 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 677 CAT95295 760167 CAE890014S ENGINE REMOVED DUE TO NR1 AND NR2 WHEEL CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIM ITS ON NR1 NOZZLE SHIELD OUTER BAND. 1 G 7 2 3U 3 U H1NE E1GL 1998050800634 19980508 00634 SW 1998 5 8 HEEA0013996 1 19980421 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP STRIPPED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 365 33005 ACTUATOR INTERNAL GEAR SEEMS TO BE STRIPPED. 1 G 7 2 4U H4SW 1998050800635 19980508 00635 SW 1998 5 8 HEEA0013997 1 19980421 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 8 33005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998050800636 19980508 00636 SW 1998 5 8 HEEA0013998 1 19980421 A 5260 212075418105 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 11 33005 STEP ACTUATOR INOPERATIVE. 1 G 7 2 4U H4SW 1998050800637 19980508 00637 SW 1998 5 8 HEEA0013999 1 19980421 A 6340 214074280107 DETECTOR BELL 412 412 1182202 SW RPM LIMIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 RPM LIMIT AUDIO DISABLED. 1 G 7 2 4U H4SW 1998050800638 19980508 00638 EU 1998 5 8 HEEA0014000 1 19980421 A 2842 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL IND FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 4 S827 TRANSMITS HIGH OUT OF TOLERANCE THROUGHOUT. 1 G 7 2 3U H3EU 1998050800639 19980508 00639 GL 1998 5 8 HEEA0014001 2 19980421 A 7250 6898782 TURBINE WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 2ND STAGE PITTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911EB CAT40380 S812 CAE836073 RECEIVING INSPECTION REVEALED: PITS BEYOND SERVICEABLE LIMITS ON NR2 WHEEL BLENDED AREA E (AFT) AS MARKED. NOTE: BLEN DING OF THESE PITS WOULD EXCEED OVERHAUL LIMITS OF .050 DEEP. INSTALLED A NEW NR2 WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 1998050800640 19980508 00640 GL 1998 5 8 HEEA0014002 2 19980421 A 7250 6898977 COUPLING 6898735 BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL ENGINE N1 WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 104PH 697 CAT33145 3622 CAE834363 ENGINE REMOVED DUE TO TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED: N1 COUPLING FAILED NO-GO GAUGE. INSTAL LED A NEW N1 COUPLING. 1 G 7 1 3U 3 U H2SW E4CE 1998050800641 19980508 00641 GL 1998 5 8 HEEA0014003 2 19980421 A 7250 23062750 NOZZLE SHIELD 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 133AE 753 CAT33440 S800 CAE833901 ENGINE REMOVED DUE TO 3500 HOUR TURBINE OVERHAUL. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE L IMITS ON NR1 NOZZLE SHIELD DOME AREA ABOUT 45% AROUND. 1 G 7 2 3U 3 U H3EU E4CE 1998050800643 19980508 00643 GL 1998 5 8 HEEA0014005 2 19980421 A 7230 23004513 CARBON SEAL 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG COMP WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50046 358 CAC70260 45173 CAE860400 ENGINE REMOVED DUE TO TURBINE OVERHAUL. INSPECTION OF COMPRESSOR PARTS REVEALED: WORN BEYOND SERVICEABLE LIMITS ON SEA L HOUSING TANGS. INSTALLED A NEW SEAL. 1 G 7 1 3U 3 U H2SW E1GL 1998050800644 19980508 00644 GL 1998 5 8 HEEA0014006 2 19980421 A 7230 23004513 CARBON SEAL 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG COMP WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2772A 352 CAC70120 45311 CAE860357 ENGINE REMOVED DUE TO CRACKED SCROLL. INSPECTION OF COMPRESSOR PARTS REVEALED: WORN BEYOND SERVICEABLE LIMITS ON SEAL TANGS AND TANG SLOTS. INSTALLED A NEW SEAL. 1 G 7 1 3U 3 U H2SW E1GL 1998050800645 19980508 00645 GL 1998 5 8 HEEA0014007 2 19980421 A 7230 23004513 CARBON SEAL 23051643 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENG COMP WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8592X 928 CAC90059 51508 CAE895719 ENGINE REMOVED DUE TO CRACKED SCROLL. INSPECTION OF COMPRESSOR PARTS REVEALED: WORN BEYOND SERVICEABLE LIMITS ON SEAL TANGS AND TANG SLOTS. INSTALLED A NEW SEAL. 1 G 7 1 3U 3 U H2SW E1GL 1998050800646 19980508 00646 GL 1998 5 8 HEEA0014008 2 19980421 A 7230 23004513 CARBON SEAL 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG COMP WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2764F 368 CAC70230 45279 CAE860050 ENGINE REMOVED DUE TO COMPRESSOR HIGH TIME IMPELLER. INSPECTION OF COMPRESSOR PARTS REVEALED: WORN BEYOND SERVICEABLE LIMITS ON SEAL TANGS AND TANG SLOTS. INSTALLED A NEW SEAL. 1 G 7 1 3U 3 U H2SW E1GL 1998050800647 19980508 00647 GL 1998 5 8 HEEA0014009 2 19980421 A 7230 23056634 GEAR 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL SPUR ADAPTER WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 630 CAC70540 45291 CAE860387 ENGINE REMOVED DUE TO TURBINE OVERHAUL. INSPECTION OF COMPRESSOR PARTS REVEALED: STEP WEAR BEYOND SERVICEABLE LIMITS ON SPUR GEARSHAFT AFT SPLINES (FAILED NO-GO GAUGE) INSTALLED A NEW SPUR GEAR. 1 G 7 1 3U 3 U H2SW E1GL 1998050800648 19980508 00648 GL 1998 5 8 HEEA0014010 2 19980421 A 7260 6876925A TUBE ASSY 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENG GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8199J 1719 CAG23058 S826 CAE836369 ENGINE REMOVED DUE TO METAL. INSPECTION OF GEARBOX PARTS REVEALED: TUBE ASSY. FAILED DIMENSIONAL CHECK PER CEB1307. INS TALLED A NEW TUBE. 1 G 7 2 3U 3 U H3EU E4CE 1998050800649 19980508 00649 GL 1998 5 8 HEEA0014011 2 19980421 A 7260 6876925 TUBE ASSY 6894171 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL ENG GR BOX WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 131AE CAG35231 S787 CAE822541F ENGINE REMOVED DUE TO METAL. INSPECTION OF GEARBOX PARTS REVEALED: TUBE ASSY. FAILED DIMENSIONAL CHECK PER CEB1307. INS TALLED A NEW TUBE. 1 G 7 2 3U 3 U H3EU E4CE 1998050800650 19980508 00650 1998 5 8 HEEA0014012 4 19980422 A 2370 9806019001 CVR BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 3885 33077 CVR NEEDS EVALUATION. 1 G 7 2 4U H4SW 1998050800651 19980508 00651 1998 5 8 HEEA0014013 4 19980422 A 2312 069102435 RECEIVER KX155 BELL 206 206L3 1182108 SW NAV/COMM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 NAV COMM RECEIVER NO DISPLAY. 1 G 7 1 3U H2SW 1998050800652 19980508 00652 SW 1998 5 8 HEEA0014015 1 19980422 A 2435 200SGL1008 START/GEN 200SGL132Q BELL 206 206L1 1182107 SW END BELL CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50182 475 3051 45242 EXCESSIVE CORROSION FOUND ON END BELL DURING IT'S FIRST 500 HOUR INSPECTION WHICH CORRODED THROUGH ONE OF THE SCREW HOLE S. NOTE: THIS SEEMS TO HAVE HAPPENED DUE TO THE TYPE FINISH THESE END BELL ASSEMBLIES HAVE. THEY DON'T HAVE ANY PAINT OR PRIMER. 1 G 7 1 3U H2SW 1998050800653 19980508 00653 NE 1998 5 8 HEEA0014016 1 19980422 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R ERODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 11725 760076 BOTH PRIMARY RUBBER ERRODED THROUGH AND PITCH HORN "A" IS DUE RETIREMENT. 1 G 7 2 3U H1NE 1998050800654 19980508 00654 1998 5 8 HEEA0014017 4 19980422 A 2330 066105552 AUDIO PANEL BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 206LS 51070 PA CHANNEL INOPERATIVE AND DUAL SINGLE SWITCH LOOSE. 1 G 7 1 3U H2SW 1998050800655 19980508 00655 SW 1998 5 8 HEEA0014018 1 19980422 A 2822 205060606003 PUMP BELL 412 412 1182202 SW BOOST FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 107X 33113 TURNS AT VERY SLOW SPEED AND THEN POPS CIRCUIT BREAKER. 1 G 7 2 4U H4SW 1998050800656 19980508 00656 SW 1998 5 8 HEEA0014019 1 19980422 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 EXCESSIVE CORROSION. SCRAPPED LOCALLY. 2 G 7 2 4U H10SW 1998050800657 19980508 00657 SW 1998 5 8 HEEA0014020 1 19980422 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 EXCESSIVE CORROSION. SCRAPPED LOCALLY. 2 G 7 2 4U H10SW 1998050800658 19980508 00658 SW 1998 5 8 HEEA0014021 1 19980422 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 EXCESSIVE CORROSION. SCRAPPED LOCALLY. 2 G 7 2 4U H10SW 1998050800659 19980508 00659 SW 1998 5 8 HEEA0014022 1 19980422 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 28101 EXCESSIVE CORROSION. SCRAPPED LOCALLY. 2 G 7 2 4U H10SW 1998050800660 19980508 00660 SW 1998 5 8 HEEA0014023 1 19980422 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 EXCESSIVE CORROSION. SCRAPPED LOCALLY. 2 G 7 2 4U H10SW 1998050800661 19980508 00661 SW 1998 5 8 HEEA0014024 1 19980422 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 EXCESSIVE CORROSION. SCRAPPED LOCALLY. 2 G 7 2 4U H10SW 1998050800662 19980508 00662 GL 1998 5 8 HEEA0014025 2 19980422 A 7250 6892824 NOZZLE SHIELD 23035128 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 615 CAT90562 760181 CAE890607S ENGINE REMOVED DUE TO TURBINE CYCLES. UPON INSPECTION OF TURBINE PARTS NOTED: CRACKED BEYOND SERVICEABLE LIMITS ON NR1 NOZZLE SHIELD DOME AS MARKED. 1 G 7 2 3U 3 U H1NE E1GL 1998050800663 19980508 00663 1998 5 8 HEEA0014026 4 19980422 A 2562 ELT10 ELT NARCO BOLKMS 105 BO105S 5626006 EU BATTERY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 54191 S804 BATTERY INOPERATIVE. TIME SINCE REPAIR 0:00. 1 G 7 2 3U H3EU 1998050800664 19980508 00664 NE 1998 5 8 HEEA0014027 1 19980422 A 2430 6153A TRANSFORMER SKRSKY S76 S76A 8143006 NE DC SYS FAILED E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 5435V 760158 BURNING SMELL COMING FROM UNIT AND CAUSES TONE IN HEADSET. 1 G 7 2 3U H1NE 1998050800665 19980508 00665 SW 1998 5 8 HEEA0014028 1 19980422 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 STARTER KICKS OFF EARLY ON START UP. 2 G 7 2 4U H10SW 1998050800666 19980508 00666 1998 5 8 HEEA0014029 4 19980422 A 3423 C2300DL4B COMPASS BELL 206 206L1 1182107 SW COCKPIT LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 22425 45743 COMPASS LEAKING. 1 G 7 1 3U H2SW 1998050800667 19980508 00667 EU 1998 5 8 HEEA0014030 1 19980422 A 6240 KDW021A WARNING BOX BOLKMS 105 BO105S 5626006 EU ROTOR RPM FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3520T S539 INTERMITTENT LIGHT AND AUDIO AT 100% RPM. 1 G 7 2 3U H3EU 1998050800668 19980508 00668 EU 1998 5 8 MALA976114 1 19980502 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 991XJ 091 DURING INSPECTION, EMERGENCY LIGHT FLOOR TRACK OUT ROW 4 AND AFT. MAINTENANCE FOUND MOST AFT EMERGENCY BATTERY PACK LOW . REPLACED BATTERY PACK, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998050800669 19980508 00669 EU 1998 5 8 MALA976115 1 19980502 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 115XJ 340A115 DURING INSPECTION, EMERGENCY LIGHT AT SEAT 3CD INOP. MAINTENANCE REPLACED BULB, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998050800670 19980508 00670 EU 1998 5 8 MALA976116 1 19980501 A 3350 6122751 BATTERY PACKS BAC 146 AVRO146RJ85A 1500097 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 507XJ E2316 DURING INSPECTION, SEVERAL EMERGENCY LIGHTS AFT ARE INOP. MAINTENANCE REPLACED AFT BATTERY PACKS, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998050800671 19980508 00671 NE 1998 5 8 MALA976117 2 19980502 A 7532 7858023 BLEED VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 428XJ 428 DURING FLIGHT, THE RIGHT BLEED FAILED TO OPEN WHEN BLEED SWITCH SELECTED TO AUTO POSITION, WILL OPEN AT LOW POWER SETTIN G BUT AUTO COARSEN WHEN POWER ADVANCED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT BLEED VALVE. RAN AC AND OPS AND SECURITY CHECKS GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998050800672 19980508 00672 NM 1998 5 8 K3HA980063 1 19980428 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 FORWARD TRACK SECTION FORWARD LIGHT INOP. FOUND BROKEN WIRE ON FORWARD LIGHT SOCKET FORWARD SECTION TRACK LIGHTS. REPA IRED WIRE, CHECKS NORMAL. 2 L 7 3 4F A3WE 1998050800673 19980508 00673 NM 1998 5 8 K3HA980064 1 19980429 A 3350 ML3071BPE LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 AFT AIRSTAIR ARROW SIGN HAS LIGHT OUT. RELAMPED, OPS CHECK OK. 2 L 7 3 4F A3WE 1998050800674 19980508 00674 NM 1998 5 8 K3HA980065 1 19980429 A 2611 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 FORWARD LAV SMOKE DETECTOR NEEDS BATTERY. INSTALLED BATTERY, TESTS OK. 2 L 7 3 4F A3WE 1998050800675 19980508 00675 NM 1998 5 8 K3HA980066 1 19980430 A 3350 387 LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 R1 DOOR EMERGENCY EXIT ARROW SIGN HAS SOME LIGHT OUT. RELAMPED R1 DOOR EMERGENCY EXIT LOWER ARROW SIGN LIGHTS, OPS CHEC KED OK. 2 L 7 3 4F A3WE 1998050800676 19980508 00676 NM 1998 5 8 K3HA980067 1 19980503 A 3350 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 AISLE EMERGENCY LIGHT AT ROW 27 ONE BULB INOP. RELAMPED PER MM 33-50-00, OPS CHECKS OK. 2 L 7 3 4F A3WE 1998050800677 19980508 00677 NM 1998 5 8 K3HA980068 1 19980503 A 3350 BULB BOEING 727 727225 1384077 NM CARGO COMPT FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 AFT CARGO DOOR EMERGENCY LIGHT, ONE BULB INOP. RELAMPED PER MM 33-50-11, OPS CHECK OK. 2 L 7 3 4F A3WE 1998050800678 19980508 00678 NE 1998 5 8 9807741160 2 19980429 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 01 160US 46769 686110 AT TOP OF DESCENT FL330, THE NR 3 ENGINE FLAMED OUT. THE ENGINE WAS SUCCESSFULLY RESTARTED ON THE SECOND ATTEMPT. THE DESCENT AND LANDING WAS WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE ENGINE PER TAFI 71-00-00 AND PERFORMED A HIGH POW ER ENGINE RUN, ALL WITH NO TROUBLE FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. EXACT PART CAUSING DIFFICULTY TO BE DE TERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998050800679 19980508 00679 EU 1998 5 8 9807753212 1 19980430 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 312US 7292 7251 152 DURING TEST OF EMERGENCY LIGHT SYSTEM, EXIT LIGHT ABOVE DOOR 2L WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGEN CY POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998050800680 19980508 00680 NM 1998 5 8 9807766608 1 19980501 A 3350 POWER SUPPLY BOEING 747 747151 1384891 NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 608US 19785 DURING LINE CHECK, FOUND UPPER DECK B-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998050800681 19980508 00681 NM 1998 5 8 9807776308 1 19980501 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 668US 24223 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE BETWEEN DOOR 1L AND 2L. RECONNECTED ELECTRICAL PINS, O PERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998050800682 19980508 00682 NM 1998 5 8 9807786304 1 19980429 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 664US 23819 DURING LINE CHECK, FOUND THREE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT ROW 43 AND 2 IN THE UPPER DECK. REPAIRED WIRI NG AND RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998050800683 19980508 00683 SO 1998 5 8 COMA9810112 1 19980420 A 3246 3006041 WHEEL 314461 EMB 120 EMB120RT SO LT MLG CRACKED A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 241CA 14982 64 1211 MAIN WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT BY MECHANIC DUE TO LOW PRESSURE. TIRE SHOP FOUND INBOARD (P/N 300-604-1) WAS MISSING A SECTION OF WHEEL FLANGE APPROXIMATELY 12 INCHES LONG. WHEEL ASSEMBLY HAS GONE THRU 45 TIRE CHANGES SINCE NEW. WHEEL ASSEMBLY HAS BEEN REMOVED FROM SERVICE. 2 L 7 2 4T RT A31SO 1998050800684 19980508 00684 EA 1998 5 8 COMA9860092 1 19980503 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946CA 7072 AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERABLE. REPLACED BULB. 2 L 7 2 4F RT A21EA 1998050800685 19980508 00685 EA 1998 5 8 COMA9860093 1 19980501 A 5270 DOOR WARNING CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 914CA 7012 CARGO DOOR WARNING MESSAGE AFTER TAKEOFF. PLACED CARGO DOOR WARNING SYSTEM ON DEFERRED MAINTENANCE LIST. 2 L 7 2 4F RT A21EA 1998050800686 19980508 00686 EA 1998 5 8 COMA9860094 1 19980501 A 2710 272953 LINK CNDAIR CL600 CL6002B19 EA RT AILERON CRACKED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 924CA 7026 RIGHT AILERON WILL NOT TEST WITH SYSTEM 2 PRESSURE VERIFIED AT 2900 PSI. FOUND PCU OUTPUT LINK FOR SYSTEM 2 (INBOARD) B ROKEN FORWARD OF AILERON ATTACH. REMOVED AND REPLACED OUTPUT LINK (P/N 27295-3) WITH SERVICEABLE (P/N 27295-5) IAW CANA DAIR MM 27-14-15-400-801. 2 L 7 2 4F RT A21EA 1998050800687 19980508 00687 WP 1998 5 8 98FDEA00324 1 19980503 A 5400 AUB7000 FITTING DOUG DC10 DC1010 3022110 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 STA-LAX - NR 3 PYLON HAS A HIGH FREQUENCY EDDY CURRENT CRACK INDICATION IN THE OUTBOARD ENGINE TRUSS FITTING AS PER FED- EX EO 8-5410-7-3323 PT W. COMPLIED WITH REPAIR AND TERMINATING MOD EO 8-5410-7-3323 PT 4. 2 L 7 3 4F A22WE 1998050800688 19980508 00688 WP 1998 5 8 ABXA9800441 1 19980107 A 5320 99105013 WEB DOUG DOUG DC9 DC941 302207N WP BS 256 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 968AX 47499 DURING C-CHECK, FOUND THE LEFT CUSP WEB CORRODED AT STATION 256. REPAIRED CUSP WEB IAW ABX REA D953-22186MR. 2 L 7 2 4F A6WE 1998050800689 19980508 00689 WP 1998 5 8 ABXA9800433 1 19980410 A 5320 3643697 FITTING DOUG DOUG DC8 DC862 3021970 WP FRAME 880 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 FRAME 880 UPPER FITTING HAS HEAVY CORROSION AND CRACKED RIGHT WHEEL WELL CEILING, BL 0. *S/D* REPAIRED IAW ABX REA D85 3-2280MR. 2 L 7 4 4F 4A25 1998050800690 19980508 00690 WP 1998 5 8 ABXA9800434 1 19980412 A 5320 576949615 INTERCOSTAL DOUG DOUG DC8 DC862 3021970 WP BS 1480 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 INTERCOSTAL CRACKED LOWER FWD END FASTENER HOLE FS 1480 LONGERON 35L. REPAIRED IAW DC8 SRM 53-4-1. 2 L 7 4 4F 4A25 1998050800691 19980508 00691 WP 1998 5 8 ABXA9800435 1 19980326 A 5712 5769470 RIB DOUG DOUG DC8 DC862 3021970 WP WS 778.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 778.75 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DC8 SRM 51-1-20D AND AB X DWG K05056. 2 L 7 4 4F 4A25 1998050800692 19980508 00692 WP 1998 5 8 ABXA9800436 1 19980405 A 5320 5711283516 WEB DOUG DOUG DC8 DC862 3021970 WP BS 1164 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 STATION 1164 AT STRINGER 32R, TORQUE BOX WEB IS CRACKED. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998050800693 19980508 00693 WP 1998 5 8 ABXA9800437 1 19980331 A 5712 57703756 RIB DOUG DOUG DC8 DC862 3021970 WP WS 466.651 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056. 2 L 7 4 4F 4A25 1998050800694 19980508 00694 WP 1998 5 8 ABXA9800438 1 19980331 A 5712 RIB DOUG DOUG DC8 DC862 3021970 WP WS 603.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 603.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DC8 SRM 51-1-8 AND DWG K05056. 2 L 7 4 4F 4A25 1998050800695 19980508 00695 WP 1998 5 8 ABXA9800439 1 19980331 A 5730 5769589 SKIN DOUG DOUG DC8 DC862 3021970 WP WS 258 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE UPPER SKIN AT STATION XW 258 APPROXIMATELY 7 FWD OF THE SPAR IS CRACKED. REPAIRED IAW DC8 SRM 5 7-2-1. 2 L 7 4 4F 4A25 1998050800696 19980508 00696 WP 1998 5 8 ABXA9800440 1 19980329 A 5712 576949615 RIB DOUG DOUG DC8 DC862 3021970 WP WS 622.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENERS AT STATION XFS 622.500. REPAIRED IAW DC8 SRM 51-1-21 AND ABX DWG K05056. 2 L 7 4 4F 4A25 1998050800697 19980508 00697 WP 1998 5 8 ABXA9800442 1 19980430 A 2530 HOTCUP DOUG DC8 DC863 302198A WP GALLEY DEFECTIVE A ABXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 817AX 45928 OVERHEATING ELECTRICAL SMELL COMING FROM HOT CUP AREA. HOT CUP WAS IN USE AT THE TIME. TURNED HOT CUP OFF AND PULLED C IRCUIT BREAKER, SMELL WENT AWAY. REPLACED HOT CUP. 2 L 7 4 4F 4A25 1998050800698 19980508 00698 WP 1998 5 8 MWEA98557 1 19980425 A 5320 99118757 ANGLE DOUG DC9 DC932 3022066 WP FRAME 1168 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACKED AFT ACCESSORY COMPARTMENT CANTED FRAME 1168 RIGHT SIDE LOWER SUPPORT ANGLE. MTC REMOVED AND REPLACED ANGL E. 2 L 7 2 4F A6WE 1998050800699 19980508 00699 WP 1998 5 8 MWEA98558 1 19980425 A 5320 99115025 CLIP DOUG DC9 DC932 3022066 WP BS 69 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACKED BEAM END CLIP AT FS 69 IN UPPER LEFT HAND SIDE OF FORWARD ACCESSORY. MTC REMOVED AND REPLACED BEAM END CL IP. 2 L 7 2 4F A6WE 1998050800700 19980508 00700 WP 1998 5 8 MWEA98559 1 19980426 A 5532 591216612N SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND VERTICAL STABILIZER CANOE SKIN ON RIGHT AFT SIDE CHAFED BEYOND LIMITS. MTC REPAIRED WITH DOUBLER. 2 L 7 2 4F A6WE 1998050800701 19980508 00701 WP 1998 5 8 MWEA98560 1 19980426 A 5530 591216611N FAIRING DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND THE BLEND OUT OF CHAFING ON UPPER VERTICAL STABILIZER FAIRING OUT OF LIMITS. MTC REPAIRED WITH DOUBLER. 2 L 7 2 4F A6WE 1998050800702 19980508 00702 NM 1998 5 8 DL72S980928 1 19980430 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 406DA 3801 21150 ON INSP, FOUND AFT EMERGENCY EXIT SIGN NO TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998050800703 19980508 00703 NM 1998 5 8 DL76P980930 1 19980501 A 2750 RETRACT MECH BOEING 767 767332 1382001 NM TE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 SO 27 1402A 25989 ON FINAL WITH FLAPS POSTIONED TO 30 DEG, THEY RETRACTED TO 20 DEG. FLAP HANDLE MOVED TO MATCH FLAP POS. STATUS MSG T/E FLAP SHUT DOWN. DIVERTED TO JFK. INSP AND OPS CHECKED FLAPS ALL NORMAL. NO FAULTS ON FLAP/SLAT ECU. ADP ON M CO. 2 L 7 2 4F RT A1NM 1998050800704 19980508 00704 NM 1998 5 8 DL757980932 1 19980427 A 5314 146N35601 KEEL BEAM BOEING 757 757232 1384965 NM BS 1390 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 617DL 22907 THE STRG 29L KEEL CHORD WAS FOUND CORRODED BETWEEN STA 1390 AND 1400. THE CHORD WAS CUT AT STA 1390 AND THE AFT END REM OVED. A NEW SECTION OF CHORD WAS SPLICE IN WITH STEEL REPAIR ANGLES PER ER/A 364526-14, REV C. 2 L 7 2 4F RT A2NM 1998050800705 19980508 00705 NM 1998 5 8 DL73E980933 1 19980428 A 5330 654577882 SKIN BOEING 737 737247 138448D NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 236WA 23184 THE R2 DOOR OPENING SURROUND SKIN WAS FOUND WITH A .75 INCH LONG CRACK AT THE CUTOUT FOR THE LOWER HINGE. THE SKIN AND BONDED DOUBLERS WERE CUTOUT TO REMOVE THE CRACK. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TR IPLER PER ER/A 364647-14, REV A. 2 L 7 2 4F A16WE 1998050800706 19980508 00706 NM 1998 5 8 DL757980934 1 19980429 A 5330 SKIN BOEING 757 757232 1384965 NM BS 840 PUNCTURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 648DL 24372 A SMALL PUNCTURE WAS FOUND IN THE FUSELAGE SKIN AT STA 840 AND STRINGER 16L JUST FWD OF A LIGHT CUTOUT. THE PUNCTURE WA S TRIMMED OUT TO A SMOOTH HOLE AND AN EXTERNAL DOUBLER AND TRIPLER WERE INSTALLED PER ER/A 364662-14. 2 L 7 2 4F RT A2NM 1998050800707 19980508 00707 NM 1998 5 8 DL73E980935 1 19980429 A 5753 BOLT BOEING 737 7372S3 NM NR 3 TE FLAP LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 369DL 21776 DURING AD MANDATED INSPECTION, THE OUTBD BOLT ON THE NR 3 FLAP OUTBD TRACK AFT ATTACH FITTING WAS FOUND LOOSE. THE COND ITION WAS CORRECTED BY INSTALLING THE TRACK MODIFICATION PER BAC S/B 737-57A1130. THE MODIFICATION WAS DOCUMENTED PER ER/A 364643-14AD. 2 L 7 2 4F RT A16WE 1998050800708 19980508 00708 NM 1998 5 8 DL72K980937 1 19980421 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1030 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 CORROSION FLOORBEAM STA 1030 BL 0. REMOVED CORROSION, FOUND OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 53-20-11. 2 L 7 3 4F A3WE 1998050800709 19980508 00709 NM 1998 5 8 DL72L980939 1 19980501 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT FIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 FOUND ON C2 LETTER CHECK, VERTICAL FIN STRINGER CRACKED AT RIB ATTACH BOLT S-8 AT STA 157.200 RT SIDE. REPAIR PER M/M 5 3-30-0. 2 L 7 3 4F A3WE 1998050800710 19980508 00710 NM 1998 5 8 DL72K980941 1 19980430 A 5330 SKIN BOEING 727 727232 1384082 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 491DA 21060 DURING L/O CHECK, EO 4-727622-12 INSPECTION FOUND A CRACK IN THE R-1 DOORWAY UPPER HINGE CUTOUT. A REPAIR WAS MADE TO S ATISFY THIS EO PER M/M 53-30-0. 2 L 7 3 4F A3WE 1998050800711 19980508 00711 NE 1998 5 8 DLL14980943 2 19980502 A 7250 TURBINE BLABE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENGINE DAMAGED A DALA E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 SO 27 740DA 22884 193C1244 14715 NR 3 ENGINE HIGH VIBRATION ON CLIMB. ENGINE SHUTDOWN AND RTN TO TPA. BORESCOPED ENGINE FOUND HPT BLADE DAMAGE. REPLAC ED ENGINE. 2 L 7 3 4F 4 F A23WE E12EU 1998050800712 19980508 00712 WP 1998 5 8 DLL10980944 1 19980502 A 2150 ACTUATOR LKHEED 1011 10113851 5265010 WP NR 3 PACK INOPERATIVE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 728DA 193C1173 ON TAKEOFF, NR 3 PACK OVERHEATED CAUSING A GREAT DEAL OF SMOKE IN THE CABIN. FOUND NUMBER 3 PACK RAM AIR DOOR ACTUATOR STUCK. REPLACED ACTUATOR. 2 L 7 3 4F A23WE 1998050800713 19980508 00713 WP 1998 5 8 DLL14980946 1 19980502 A 3350 BULB LKHEED 1011 1011385115 5265015 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 741DA 193C1245 EXTERIOR EMERGENCY LIGHT AT R-4 DOOR INOP. RELAMPED. 2 L 7 3 4F A23WE 1998050800714 19980508 00714 NM 1998 5 8 DL72W980947 1 19980502 A 3350 900542 RACK BOEING 727 727247 138408F NM BS 800 INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2819W 21057 RT AFT OVERWING EMER EXIT LIGHT INOP. REPLACED BATT RACK, OPS NOW NML. 2 L 7 3 4F A3WE 1998050800715 19980508 00715 WP 1998 5 8 DLL13980948 1 19980503 A 3260 PROX SWITCH 801813 LKHEED 1011 10113851 5265010 WP LT MLG DOOR FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 790DL 193A1143 AFTER T/O, LDG GEAR RAISED GREEN LIGHTS EXT RED DOOR AND INTRANSIT LIGHT REMAINED ON ALONG WITH LT GEAR OR DOOR LIGHT ON S/O PNL. GEAR PLACED DOWN AND GEAR EXTENDED WITH 3 GREENS BUT RED DOOR AND INTRANSIT LIGHT REMAINED ON ALONG WITH AMBE R LIGHT ON S/O PANEL. REPLACED LT GEAR DOOR PROX SWT DOOR IND NOW NORMAL. 2 L 7 3 4F A23WE 1998050800716 19980508 00716 WP 1998 5 8 DLL19980949 1 19980503 A 3240 2136720PT1AD BRAKE HOUSING LKHEED 1011 10113853 5265020 WP NR 1 MLG FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 753DA 193W1189 ON L/O, FOUND NR 1F BRAKE HOUSING DAMAGED CAUSING THE DAMAGE TO THE WHEEL ASSY. THIS COULD HAVE CAUSED THE WHEEL TO SEI ZE. 2 L 7 3 4F A23WE 1998050800717 19980508 00717 WP 1998 5 8 SCNA98037 1 19980426 A 5210 ADA3418401 SUPPORT DOUG DC10 DC1015 3022118 WP L4 DOOR BROKEN A SCNA K NONE O OTHER DE DESCENT 1 GL 15 152SY 48289 DURING DESCENT, PRESSURIZATION WOULD NOT START A NORMAL DESCENT IN THE AUTO/SEMI MODES. UPON LANDING FLIGHT ATTENDANT R EPORTED LOUD CONTINUOUS HISS COMING FROM THE L4 DOOR. FOUND LOWER TELEFLEX SUPPORT BROKEN. REPLACED SUPPORT AND OPERAT IONALLY CHECKED GOOD PER MAINTENANCE MANUAL CHAPTER 521200. 2 L 7 3 4F A22WE 1998050800718 19980508 00718 NM 1998 5 8 DHL98726124 1 19980303 A 5720 ANGLE BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D-CHECK, LT WING TRAILING EDGE COVE PANEL SUPPORT FRAME IS CRACKLED AT FASTENER RECEPTACLE ANGLE LOCATED JUST BEL OW NR 5 SPOILER OUTBD END. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-30-2. N/R 1369. 2 L 7 3 4F A3WE 1998050800719 19980508 00719 GL 1998 5 8 DHL98807003 2 19980502 A 7200 ENGINE DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL NR 2 FAILED A DHLA O OTHER E VIBRATION/BUFFET CR CRUISE 1 SO 01 807DH 45990 ENG NR 2 ROLLED BACK TO IDLE THEN FAILED AT FL 330. DECENDED AND ATTEMPTED RESTART. RESTART SUCCESSFUL AND NO ABNORMAL ITIES FOR THE REST OF THE FLIGHT. VISUALLY INSPECTED INLET AND EXHAUST. PERFORMED N1 ROTOR CHECK, ENGINE CHECK, AND SP ECIFIC GRAVITY FOR PROPER FUEL USED. ENGINE RAN 83 PERCENT PRESSURE WAS WITHIN LIMITS WITH BOOST PUMPS OFF. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998050800720 19980508 00720 WP 1998 5 8 ARWA980411 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 300 BENT A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND FS 300, RIB BENT, CUSP ANGLE AREA. CUT OUT DAMAGED SECTION OF FRAME. INSTALLED NEW SE CTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WOR K ORDER 970101, ITEM NR 0014, CONTROL NR 5009. 2 L 7 4 4F 4A25 1998050800721 19980508 00721 WP 1998 5 8 ARWA980412 1 19980424 A 3810 FILL PORT DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE EXT RIGHT FOWARD, WATER FILL PORT, CORROSION INSIDE. REMOVED CORROSION, FABRICATED FILLE R AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0169, CONTROL NR 5025. 2 L 7 4 4F 4A25 1998050800722 19980508 00722 WP 1998 5 8 ARWA980413 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 640 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FRAME AT FS 640 AT CUSP AREA HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED AND INS TALLED SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0132, CONTROL NR 5034. 2 L 7 4 4F 4A25 1998050800723 19980508 00723 WP 1998 5 8 ARWA980414 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1120 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FRAME AT FS 1120 AT CUSP AREA HAS CORROSION. CUT OUT DAMAGE SECTION OF FRAME. FABRICATED AND INS TALLED NEW SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR F ORM JW3B, WORK ORDER 970101, ITEM NR 0145, CONTROL NR 5047. 2 L 7 4 4F 4A25 1998050800724 19980508 00724 WP 1998 5 8 ARWA980415 1 19980424 A 5320 CUSP DOUG DC8 DC862 3021970 WP BS 1200 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT HAND CUSP AT FS 1200 HAS CORROSION. CUT OUT DAMAGED SECTION OF CUSP. FABRICATED AND INSTALL ED NEW SECTION OF CUPS IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-5. WORK ACCOMPLISHED UNDER ARROW AIR FORM J W3B, WORK ORDER 970101, ITEM NR 0160, CONTROL NR 5062. 2 L 7 4 4F 4A25 1998050800725 19980508 00725 WP 1998 5 8 ARWA980416 1 19980424 A 5320 CUSP DOUG DC8 DC862 3021970 WP BS 1140-1160 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND CUSP AT FS 1140 TO 1160 HAS CORROSION. CUT OUT DAMAGED SECTION OF CUSP. FABRICATED AN D INSTALLED NEW SECTION OF CUSP IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-5. WORK ACCOMPLISHED UNDER ARROW A IR FORM JW3B, WORK ORDER 970101, ITEM NR 0106, CONTROL NR 5089. 2 L 7 4 4F 4A25 1998050800726 19980508 00726 WP 1998 5 8 ARWA980417 1 19980424 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 680-710 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LONGERON 31 LEFT HAS CORROSION AT FS 680 TO 710. CUT OUT DAMAGED SECTION OF LONGERON. LOCATED DR ILLED AND INSTALLED NEW SECTION OF LONGERON IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 51-1-20D AND 53-4-1 39A. WO RK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2996, CONTROL NR 5105A. 2 L 7 4 4F 4A25 1998050800727 19980508 00727 WP 1998 5 8 ARWA980418 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 540 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FRAME AT FS 540 HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED NEW SE CTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WOR K ORDER 970101, ITEM NR 799, CONTROL NR 5394. 2 L 7 4 4F 4A25 1998050800728 19980508 00728 WP 1998 5 8 ARWA980419 1 19980424 A 5313 LONGERON DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND LONGERON 24 HAS A CRACK. REMOVED DAMAGED LONGERON. LOCATED, DRILLED AND INSTALLED NEW LONGERON 24 IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5753508 AND SRM 51-1-24, 51-1-20D AND 51-3-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2191, CONTROL NR 5809. 2 L 7 4 4F 4A25 1998050800729 19980508 00729 WP 1998 5 8 ARWA980420 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1240 CUT OUT A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND CUT OUT CIRCUMFERENTIAL AT FS 1240 FOR REMOVAL OF CUSP SECTION. CUT FRAME SECTION. FABRICATED SP LICES AND INSTALLED FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FOR M M3A, WORK ORDER 970101, ITEM NR 2487, CONTROL NR 5988. 2 L 7 4 4F 4A25 1998050800730 19980508 00730 WP 1998 5 8 ARWA980421 1 19980424 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1450 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSLAGE EXT SKIN FS 1450 HOOK TO LOCK REAR SERVICE DOOR HAS CORROSION. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED DOUBLER, FILLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.020D-0339. WORK ACCOM PLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0339, CONTROL NR 5188. 2 L 7 4 4F 4A25 1998050800731 19980508 00731 WP 1998 5 8 ARWA980422 1 19980424 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1230 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURINGD CHECK, FOUND LEFT HAND FS 1230 LONGERON 21 FLOORBEAM FITTING HAS CORROSION. REMOVED DAMAGED FITTING. FABRICATE D AND INSTALLED NEW FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING 9754064 AND SRM 51-1-20D. WORK ACCOMPL ISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2362, CONTROL NR 5814. 2 L 7 4 4F 4A25 1998050800732 19980508 00732 WP 1998 5 8 ARWA980423 1 19980424 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1140-1170 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN AT LONGERON 11 LEFT, WEB HAS CORROSION FROM FS 1140 TO 1170. FABRICATED STRAP AND INST ALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW97010-2916. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970 101, ITEM NR 2916, CONTROL NR 5095A. 2 L 7 4 4F 4A25 1998050800733 19980508 00733 WP 1998 5 8 ARWA980424 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1563 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN, FRAME AT FS 1563 HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED NEW SEC TION OF FRAME AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-0135. WORK ACCOMPLISHED UNDER ARROW AIR F ORM JW3B, WORK ORDER 970101, ITEM NR 0135, CONTROL NR 5037. 2 L 7 4 4F 4A25 1998050800734 19980508 00734 WP 1998 5 8 ARWA980425 1 19980424 A 5230 DOOR DOUG DC8 DC862 3021970 WP BS 158 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND AFT LOWER FUSELAGE DOOR AT FS 1586 HAS CORROSION. CLEANED CORROSION FABRICATED DOULBER AND INSTAL LED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-0198. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 9701 01, ITEM NR 0198, CONTROL NR 5126. 2 L 7 4 4F 4A25 1998050800735 19980508 00735 WP 1998 5 8 ARWA980426 1 19980424 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 255 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND CABIN FLOORBEAM AT FS 255 HAS CORROSION. CUT OUT DAMAGED SECTION OF FLOORBEAM. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-2896. WORK ACCOMPLISHED UNDER ARROW AIR FORM J W3B, WORK ORDER 970101, ITEM NR 2896, CONTROL NR 5090A. 2 L 7 4 4F 4A25 1998050800736 19980508 00736 WP 1998 5 8 ARWA980427 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1542 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN FRAME IS CRACKED AT FS 1542. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED NEW FRAME S ECTION AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3020. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3 B, WORK ORDER 970101, ITEM NR 3020, CONTROL NR 5119A. 2 L 7 4 4F 4A25 1998050800737 19980508 00737 WP 1998 5 8 ARWA980428 1 19980424 A 5240 SKIN DOUG DC8 DC862 3021970 WP SERVICE DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND FWD SERVICE DOOR HAS DENT AND A CRACK. STOP DRILLED CRACK, FABRICATED DOUBLER AND INST ALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98030806. WORK ACCOMPLISHED UNDER A RROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2439, CONTROL NR 5976. 2 L 7 4 4F 4A25 1998050800738 19980508 00738 WP 1998 5 8 ARWA980429 1 19980424 A 5320 STIFFENER DOUG DC8 DC862 3021970 WP BS 980 CUT A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND MAIN WHEEL WELL, CUT HORIZONTAL STIFFENER AT FS 980 TO FACILITATE LONGERON 24 REPLACEME NT. CUT STIFFENER AND FABRICATED REPAIR BLOCK AND ANGLES AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.97010 1-3043. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM 3043, CONTROL NR 5134A. 2 L 7 4 4F 4A25 1998050800739 19980508 00739 WP 1998 5 8 ARWA980430 1 19980424 A 5280 SKIN DOUG DC8 DC862 3021970 WP RT MLG DOOR CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT MAIN LANDING GEAR DOOR INTERIOR AREA HAS CORROSION. REMOVED DOOR SKIN. FABRICATED NEW SKIN AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 52-6-2 AND 51-3-2. WORK ACCOMPLISHED UNDER ARROW AIR FOR M JW3B, WORK ORDER 970101, ITEM NR 2406, CONTROL NR 5940. 2 L 7 4 4F 4A25 1998050800740 19980508 00740 WP 1998 5 8 ARWA980431 1 19980424 A 5240 ACCESS DOOR DOUG DC8 DC862 3021970 WP BS 1586 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE LOWER ACCESS DOOR NR 60 AT FS 1586 IS DAMAGED. FABRICATED AND INSTALLED REPAIR DOUBLER I N ACCORDANCE WITH JOSSAIR COMPANY, EO ARW970101-0198. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, IT EM NR 0198, CONTROL NR 5126. 2 L 7 4 4F 4A25 1998050800741 19980508 00741 WP 1998 5 8 ARWA980432 1 19980424 A 5320 WEB DOUG DC8 DC862 3021970 WP CABIN TORN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN 9G BULKHEAD SUB FLOOR WEB IS TORN. REMOVED SUB FLOOR WEB. FABRICATED AND INSTALLED NE W SUB FLOOR WEB IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-007. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 980010, ITEM NR 007. 2 L 7 4 4F 4A25 1998050800742 19980508 00742 WP 1998 5 8 ARWA980433 1 19980424 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP COCKPIT CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN, COCKPIT FORWARD OF RUDDER PEDALS, FINGER DOUBLER HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.112D-2726. WORK A CCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2726, CONTROL NR 4406. 2 L 7 4 4F 4A25 1998050800743 19980508 00743 WP 1998 5 8 ARWA980434 1 19980424 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 74.125 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND INSTALL TWO DOUBLERS AT FS 74.125 LEFT HAND FOR TEMPERATURE PROBES. FABRICATED AND INSTALLED TWO TEMPERATURE PROBES DOUBLERS IN ACCORDANCE WITH NEW SYSTEMS DRAWING 229-92-100 AND 229-921110. WORK ACCOMPLISHED UNDER A RROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3131, CONTROL NR 4497. 2 L 7 4 4F 4A25 1998050800744 19980508 00744 WP 1998 5 8 ARWA980435 1 19980424 A 5320 SUB FLOOR DOUG DC8 DC862 3021970 WP BS 224 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND ACCESSORY COMPARTMENT SUB FLOOR AT FS 224 HAS CORROSION. REMOVED SUB FLOOR. FABRICATED AND INSTA LLED NEW SUB FLOOR IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-0007. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1650, CONTROL NR 4132. 2 L 7 4 4F 4A25 1998050800745 19980508 00745 WP 1998 5 8 ARWA980436 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 228 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND ACCESSORY COMPARTMENT AT FS 228, CIRCUMFERENTIAL HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-0, 51-1-20D AND 51-3-0. WORK ACCOMPLI SHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1690, CONTROL NR 4188. 2 L 7 4 4F 4A25 1998050800746 19980508 00746 WP 1998 5 8 ARWA980437 1 19980424 A 5312 BULKHEAD SKIN DOUG DC8 DC862 3021970 WP BS 1400 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND AFT LOWER CARGO COMPARTMENT FS 1400 BULKHEAD ACCESS PANEL IS CRACKED. REMOVED SKIN, FABRICATED NE W SKIN AND INSTALLED IN ACCORDANDE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98022303. WORK ACCOM PLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM 0324, CONTROL NR 5151. 2 L 7 4 4F 4A25 1998050800747 19980508 00747 WP 1998 5 8 ARWA980438 1 19980424 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE FORWARD TOPSIDE INSTALL DOUBLERS WHERE EXISTING OMEGA ANTENNAS WERE MOUNTED. FABRICATED FILLER AND DOUBLERS AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3136, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3136, CONTROL NR 5166A. 2 L 7 4 4F 4A25 1998050800748 19980508 00748 WP 1998 5 8 ARWA980439 1 19980424 A 5312 BULKHEAD WEB DOUG DC8 DC862 3021970 WP BS 35 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE AT FS 35.0 BULKHEAD HAS TWO BIG HOLES AT CENTER SECTION. REMOVED BULKHEAD WEB. INSTALLE D NEW SECTION OF WEB IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.980010-0031. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A , WORK ORDER 980010, ITEM NR 0031, CONTROL NR 0031. 2 L 7 4 4F 4A25 1998050800749 19980508 00749 WP 1998 5 8 ARWA980440 1 19980424 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 1500 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN FLOORBEAM AT FS 1500 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND REPAI R ANGLE AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING EO 98AROW.021D-2478. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1478, CONTROL NR 5599. 2 L 7 4 4F 4A25 1998050800750 19980508 00750 WP 1998 5 8 ARWA980441 1 19980424 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 260 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN FLOORBEAM AT FS 260 LEFT HAND HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND REPAIR ANGLE AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-3128. WORK ACCOMPLISHED UNDER ARR OW AIR FORM JW3B, WORK ORDER, 970101, ITEM NR 3128, CONTROL NR 5162A. 2 L 7 4 4F 4A25 1998050800751 19980508 00751 WP 1998 5 8 ARWA980442 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP RT MLG WW CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT WHEEL WELL, FORWARD RIGHT LOWER CORNER FRAME HAS CORROSION AND IS CRACKED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3113. W ORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 3113, CONTROL NR 5158A. 2 L 7 4 4F 4A25 1998050800752 19980508 00752 WP 1998 5 8 ARWA980443 1 19980424 A 5320 SPLICE DOUG DC8 DC862 3021970 WP BS 660-680 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MIDSHIP ACCESSORY COMPARTMENT LONGERON 25 RIGHT SPLICE HAS CORROSION, FS 660 TO 680. REMOVED LONG ERON SPLICE, CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO A RW.970101.2418. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2418, CONTROL NR 5921. 2 L 7 4 4F 4A25 1998050800753 19980508 00753 WP 1998 5 8 ARWA980445 1 19980424 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 857-879 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN LONGERON NR 1 AT FS 857 TO 879 HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR BL OCK AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98012905. WORK ACCOMPLI SHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0845, CONTROL NR 5433. 2 L 7 4 4F 4A25 1998050800754 19980508 00754 WP 1998 5 8 ARWA980446 1 19980424 A 5314 KEEL BEAM DOUG DC8 DC862 3021970 WP BS 680-720 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE CENTER SECTION KEEL BEAM FROM FS 680 TO 720 HAS CORROSION. CUT OUT DAMAGED SECTION OF KE EL BEAM. MACHINED NEW SECTION OF KEEL BEAM AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 561377 9 AND ACTION NR 358456, 358745, FILE NR 98-01-30-004/98-02-03-005. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK OR DER 970101, ITEM NR 2997, CONTROL NR 5107A. 2 L 7 4 4F 4A25 1998050800755 19980508 00755 WP 1998 5 8 ARWA980447 1 19980424 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 1420 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND AFT LOWER CARGO LEFT SIDE FS 1420, FLOORBEAM HAS CORROSION. REMOVED CORROSION. FABRICATED REPAIR ANGLE AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2436. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2436, CONTROL NR 5236. 2 L 7 4 4F 4A25 1998050800756 19980508 00756 WP 1998 5 8 ARWA980448 1 19980424 A 5320 TRAP FITTING DOUG DC8 DC862 3021970 WP RIGHT CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND TRAPEZOID FITTING HAS FOUR CRACKS. REMOVED CRACKED TRAP, FITTING AND INSTALLED NEW TRA P FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5616481 AND SRM 51-1-20D, 51-3-0. WORK ACCOMPLISHED U NDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3067, CONTROL NR 5142A. 2 L 7 4 4F 4A25 1998050800757 19980508 00757 WP 1998 5 8 ARWA980449 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 680 CRACK A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MIDSHIP ACCESSORY COMPARTMENT, CIRCUMFERENTIAL FRAME HAS A 2 INCH CRACK AT STATION 680, BETWEEN LO NGERON 35R AND 36. STOP DRILLED CRACK AND REMOVED DAMAGED EXISTING SPLICE. FABRICATED NEW SPLICE AND INSTALLED IN ACCO RDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-3029. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITE M NR 3029, CONTROL NR 5123A. 2 L 7 4 4F 4A25 1998050800758 19980508 00758 WP 1998 5 8 ARWA980450 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 400 GOUGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN LONGERON NR 12 AT STATION 400 FRAME HAS GOUGE. CUT OUT DAMAGED SECTION OF FRAME. FABR ICATED FILLER AND REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2994. WORK ACCOMPL ISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2994, CONTROL NR 5113A. 2 L 7 4 4F 4A25 1998050800759 19980508 00759 WP 1998 5 8 ARWA980451 1 19980424 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1400 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE EXTERIOR SKIN HAS A HOLE AT FS 1400. CUT OUT DAMAGED SECTION OF SKIN. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1 AND 51-1-20D AND 51-1-2. WORK ACCOMP LISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2952, CONTROL NR 5112A. 2 L 7 4 4F 4A25 1998050800760 19980508 00760 WP 1998 5 8 ARWA980452 1 19980424 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 680-720 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE CENTER SECTION, LONGERON 32L HAS CORROSION AT FS 680 TO 720. CUT OUT DAMAGED SECTION OF LONGERON. LOCATED, DRILLED, AND INSTALLED NEW SECTION OF LONGERON IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2 -0 AND 51-1-20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2947, CONTROL NR 5106A. 2 L 7 4 4F 4A25 1998050800761 19980508 00761 WP 1998 5 8 ARWA980453 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 660 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN FRAME AT STATION 660 HAS CORROSION. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED REPA IR SPLICES AND INSTALLED NEW SECTION OF FRAME IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1. WORK ACCOMPLISHE D UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 3094, CONTROL NR 5152A. 2 L 7 4 4F 4A25 1998050800762 19980508 00762 WP 1998 5 8 ARWA980454 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1420 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN LEFT SIDE STATION 1420 FRAME IS CRACKED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED NEW SECTION OF FRAME AND REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1 AND 51-1- 20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3125, CONTROL NR 5159A. 2 L 7 4 4F 4A25 1998050800763 19980508 00763 WP 1998 5 8 ARWA980455 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1400 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN RIGHT SIDE STATION 1400 FRAME IS CRACKED. CUT OUT DAMAGED SECTION OF FRAME. FABRICATE D NEW SECTION OF FRAME AND REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-1 AND 51-1 -20D. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2928, CONTROL NR 5100A. 2 L 7 4 4F 4A25 1998050800764 19980508 00764 WP 1998 5 8 ARWA980456 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 400 DENTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN RIGHT SIDE STATION 400 FRAME HAS A DENT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED REPAIR DOUBLER AND INSTALLED NEW SECTION OF FRAME IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2926. WORK ACC OMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2926 CONTROL NR 5099A. 2 L 7 4 4F 4A25 1998050800765 19980508 00765 WP 1998 5 8 ARWA980457 1 19980424 A 5350 FAIRING DOUG DC8 DC862 3021970 WP RT WING/FUS DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND FUSELAGE RIGHT SIDE FORWARD OF WING, FAIRING SUPPORT HOLE IS ELONGATED. REAMED HOLE TO .375 DIAME TER AND FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS, AND PAR TS, EO 98012104. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2914, CONTROL NR 5093A. 2 L 7 4 4F 4A25 1998050800766 19980508 00766 WP 1998 5 8 ARWA980458 1 19980424 A 5311 FRAME DOUG DC8 DC862 3021970 WP CABIN CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CABIN AT RIGHT HAND CUSP, CIRCUMFERENTIAL HAS CORROSION. CUT DAMAGED SECTION OF FRAME. FABR ICATED NEW SECTION OF FRAME AND REPAIR SPLICES AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 53-2-3 AND 51-1-20. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0100, CONTROL NR 5083. 2 L 7 4 4F 4A25 1998050800767 19980508 00767 WP 1998 5 8 ARWA980459 1 19980424 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 350 DENTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND MAIN CARGO DOOR CUTOUT, EXTERIOR SKIN AT FS 350, LOWER CORNER AREA HAS SEVERAL DENTS AND CORROSION . REMOVED CORROSION AND TRIMMED OUT AREA IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, ACTION NR 360499, FILE NR 98-02-0 10. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2508, CONTROL NR 5007A. 2 L 7 4 4F 4A25 1998050800768 19980508 00768 WP 1998 5 8 ARWA980460 1 19980424 A 2530 OVEN DOUG DC8 DC862 3021970 WP GALLEY REPLACED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND REMOVED OVEN AND INSTALLED MICROWAVE SYSTEM FOR COMPANY CONVINIENCE. REMOVED OVEN. FABRICATED MI CROWAVE MOUNT AND INSTALLED MICROWAVE SYSTEM IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98032301. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3147, CONTROL NR 4500. 2 L 7 4 4F 4A25 1998050800769 19980508 00769 WP 1998 5 8 ARWA980461 1 19980424 A 5330 ACCESS PANEL DOUG DC8 DC862 3021970 WP RT MLG MISSING A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND MAIN LANDING GEAR, KEEL BEAM INSPECTION ACCESS PANEL MISSING. FABRICATED AND INSTALLED NEW ACCESS PANEL IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW970101-3180. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WO RK ORDER 970101, ITEM NR 3180, CONTROL NR 5172A. 2 L 7 4 4F 4A25 1998050800770 19980508 00770 WP 1998 5 8 ARWA980462 1 19980424 A 5330 SKIN DOUG DC8 DC862 3021970 WP FUSELAGE PUNCTURED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT SIDE FUSELAGE JUST FORWARD OF AFT PRESSURE BULKHEAD, BETWEEN LONGERON 26R AND 28R, SKIN IS P UNCTURED. CUT OUT DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.970101-3236, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 3236, CONTROL NR 5180. 2 L 7 4 4F 4A25 1998050800771 19980508 00771 WP 1998 5 8 ARWA980463 1 19980424 A 2710 CABLE GUIDE DOUG DC8 DC862 3021970 WP WS 422 BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING FRONT SPAR AT STATION XFS 422.0 HAS A PHENOLIC CABLE GUIDE BROKEN. FABRICATED REPAIR SP LICES AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-0705. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0705, CONTROL NR 1214. 2 L 7 4 4F 4A25 1998050800772 19980508 00772 WP 1998 5 8 ARWA980464 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 710-885 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING LEADING EDGE HAS CORROSION FORM STATION XFS 710 TO 885. REMOVED DAMAGED SECTION OF SKIN . FABRICATED DOUBLER, FILLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98ROW.021D-2372. WORK ACCOMPLISHE D UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2372, CONTROL NR 5929. 2 L 7 4 4F 4A25 1998050800773 19980508 00773 WP 1998 5 8 ARWA980465 1 19980424 A 5320 TRAP PANEL DOUG DC8 DC862 3021970 WP LT MLG WW CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT HAND WHEEL WELL, TRAPEZOID FITTING HAS A 7 INCH CRACK. REMOVED CRACKED TRAPEZOID, LOCATED, D RILLED AND INSTALLED NEW TRAPEZOID FITTING IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5616481 AND SRM 51-1- 20D, 51-3-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1379, CONTROL NR 1534. 2 L 7 4 4F 4A25 1998050800774 19980508 00774 WP 1998 5 8 ARWA980466 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 485-710 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT HAND WING LEADING EDGE FROM STATION XFS 485 TO 710 HAS CORROSION. CUT OUT DAMAGED AREA. FAB RICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-2-1. WORK ACCOMPLISHED UND ER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1378, CONTROL NR 1533. 2 L 7 4 4F 4A25 1998050800775 19980508 00775 WP 1998 5 8 ARWA980467 1 19980424 A 5753 SKIN DOUG DC8 DC862 3021970 WP LT TE FLAP CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING, INBOARD FLAP SKIN HAS CORROSION. REMOVED SECTION OF SKIN. FABRICATED AND INSTALLED NE W SECTION OF SKIN IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-1525. WORK ACCOMPLISHED UNDER ARROW AIR FORM J W3B, WORK ORDER 970101, ITEM NR 1525, CONTROL NR 1538. 2 L 7 4 4F 4A25 1998050800776 19980508 00776 WP 1998 5 8 ARWA980468 1 19980424 A 5753 SKIN DOUG DC8 DC862 3021970 WP LT TE FLAP DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING, INBOARD FLAP, LOWER SURFACE HAS A TEMPORARY REPAIR. REMOVED SECTION OF SKIN. FABRICAT ED AND INSTALLED NEW SECTION IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021RO-1388. WORK ACCOMPLISHED UNDER ARROW FORM M3A, WORK ORDER 970101, ITEM NR 1388, CONTROL NR 1547. 2 L 7 4 4F 4A25 1998050800777 19980508 00777 WP 1998 5 8 ARWA980469 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 710-885 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING LEADING EDGE EXTERNAL SURFACE HAS CORROSION FROM STATION 710 TO 885. CUT OUT DAMAGED SE CTION. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1201. WORK AC COMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1201, CONTROL NR 1422. 2 L 7 4 4F 4A25 1998050800778 19980508 00778 WP 1998 5 8 ARWA980470 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 291 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING UPPER LEADING EDGE SKIN HAS CORROSION AT STATION XFS 291.00. CUT OUT DAMAGED AREA. FAB RICATED FILLER AND DOULBER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1285. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1285, CONTROL NR 1448. 2 L 7 4 4F 4A25 1998050800779 19980508 00779 WP 1998 5 8 ARWA980471 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 329 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING LEADING EDGE SKIN HAS CORROSION AT STATION XFS 329.00. CUT OUT DAMAGED AREA. FABRICATE D FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1285. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1286, CONTROL NR 1449. 2 L 7 4 4F 4A25 1998050800780 19980508 00780 WP 1998 5 8 ARWA980472 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING NR 1 STUB LEADING EDGE MATING SURFACE HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-1522. WORK ACCOMPLISHED UNDER AR ROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1522, CONTROL NR 1469. 2 L 7 4 4F 4A25 1998050800781 19980508 00781 WP 1998 5 8 ARWA980473 1 19980424 A 5720 T-CAP DOUG DC8 DC862 3021970 WP LT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING AUX TANK UPPER CAP HAS CORROSION AT ATTACHMENT HOLES. REMOVED DAMAGED T-CAP, AND INSTAL LED NEW T-CAP FROM DOUGLAS AIRCRAFT COMPANY. INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 51-1-20 AND 51- 1-21. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1209, CONTROL NR 1437. 2 L 7 4 4F 4A25 1998050800782 19980508 00782 WP 1998 5 8 ARWA980474 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING NR 1 STUB LEADING EDGE HAS A TEMPORARY REPAIR. FABRICATED AND INSTALLED NEW DOUBLER IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS AND PARTS, EO 98012105. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2833, CONTROL NR 1900. 2 L 7 4 4F 4A25 1998050800783 19980508 00783 WP 1998 5 8 ARWA980475 1 19980424 A 5720 CAP DOUG DC8 DC862 3021970 WP LT WING MISDRILLED A ARWA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING AUX TANK UPPER T-CAP HAS SOME MISDRILLED HOLES. PLUGED MISDRILLED HOLES FABRICATED REPA IR STRAP AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2933. WORK ACCOMPLISHED UNDER ARROW AIR FO RM M3A, WORK ORDER 970101, ITEM NR 2933, CONTROL NR 1941. 2 L 7 4 4F 4A25 1998050800784 19980508 00784 WP 1998 5 8 ARWA980476 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING CENTER LEADING EDGE LOWER SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANDE WITH AVITAS ENGINEERING, EO 98AROW.021D-3007. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 3007, CONTROL NR 1953. 2 L 7 4 4F 4A25 1998050800785 19980508 00785 WP 1998 5 8 ARWA980477 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING OUTBOARD LEADING EDGE, INBOARD SECTION HAS CORROSION. CUT OUT DAMAGED AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2497, CONTROL NR 1836. 2 L 7 4 4F 4A25 1998050800786 19980508 00786 WP 1998 5 8 ARWA980478 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING OUTBOARD LEADING EDGE LOWER SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLE R AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2845. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2845, CONTROL NR 1902. 2 L 7 4 4F 4A25 1998050800787 19980508 00787 WP 1998 5 8 ARWA980479 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING OUTBOARD LEADING EDGE, INBOARD SECTION LOWER SKIN HAS CORROSION AND A CRACK. CUT OUT DA MAGED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2846 AND DOUGLAS AIRCRAFT COMPANY, SRM 51-1-21. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2846, CO NTROL NR 1903. 2 L 7 4 4F 4A25 1998050800788 19980508 00788 WP 1998 5 8 ARWA980480 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP LT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING INBOARD STUB LEADING EDGE SKIN UPPER SURFACE HAS CORROSION. CUT OUT DAMAGED AREA. FABR ICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2855. WORK ACCOMPLISHED U NDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2855, CONTROL NR 1916. 2 L 7 4 4F 4A25 1998050800789 19980508 00789 WP 1998 5 8 ARWA980481 1 19980424 A 5400 STRAP DOUG DC8 DC862 3021970 WP NR 1 PYLON CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND NR 1 ENGINE PYLON, UPPER SUPPORT STRAP HAS A CRACK. REMOVED SUPPORT STRAP. FABRICATED NEW STRAP AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY DRAWING NR 5753033, 5753000 AND SRM 51-1-20D. WORK ACCOMPLISH ED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0581, CONTROL NR 8012. 2 L 7 4 4F 4A25 1998050800790 19980508 00790 WP 1998 5 8 ARWA980482 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 423-525 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN HAS CORROSION FROM STATION XFS 423 TO 525. REMOVED DAMAG ED SKIN. FABRICATED NEW SKIN AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-3-2-, 51-1-21 AND 51-1-2 1D. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2939, CONTROL NR 5103A. 2 L 7 4 4F 4A25 1998050800791 19980508 00791 WP 1998 5 8 ARWA980483 1 19980424 A 5720 ANGLE DOUG DC8 DC862 3021970 WP LT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT WING FUEL DUMP SHROUD COVER ATTACH ANGLE IS CRACKED. REMOVED CRACKED ANGLE. FABRICATED NEW ANGLE AND INSTALLED IN ACCORDANCE WITH JOSSAIR COMPANY EO ARW.970101.3065. WORK ACCOMPLISHED UNDER ARROW AIR, INC FORM M3A, WORK ORDER 970101, ITEM NR 3065, CONTROL NR 1970. 2 L 7 4 4F 4A25 1998050800792 19980508 00792 WP 1998 5 8 ARWA980484 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 0-74 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT WING UPPER SURFACE SKIN HAS CORROSION FROM STATION XWO TO XRS 74. CUT OUT DAMAGED AREA. FA BRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 57-2-1. WORK ACCOMPLISHED UN DER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 1589, CONTROL NR 1562. 2 L 7 4 4F 4A25 1998050800793 19980508 00793 WP 1998 5 8 ARWA980485 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT WING NR 4 STUB LEADING EDGE SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FILLER AN D DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW-021D-1495. WORK ACCOMPLISHED UNDER ARROW AIR F ORM JW3B, WORK ORDER 970101, ITEM NR 1495, CONTROL NR 1496. 2 L 7 4 4F 4A25 1998050800794 19980508 00794 WP 1998 5 8 ARWA980486 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP RT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT WING NR 3 STUB LEADING EDGE UPPER SKIN HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED FIL LER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH AVITAS ENGINEERING, EO 98AROW.021D-2616. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2616, CONTROL NR 1886. 2 L 7 4 4F 4A25 1998050800795 19980508 00795 WP 1998 5 8 ARWA980487 1 19980424 A 5720 SUPPORT DOUG DC8 DC862 3021970 WP RT WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT WING CENTER SECTION OF LEADING HAS A SUPPORT CRACKED. REMOVED CRACKED SUPPORT. FABRICATED NEW SUPPORT AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5770409 AND SRM 53-01-0. WORK ACCOMPL ISHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 1721, CONTROL NR 1689. 2 L 7 4 4F 4A25 1998050800796 19980508 00796 WP 1998 5 8 ARWA980488 1 19980424 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 50 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT WING SURFACE AT STATION XRS 50 HAS CORROSION AND A CRACK. REMOVED CORROSION AND CUT OUT CRA CKED AREA. FABRICATED FILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH INTERNATIONAL AVIATION ADVISORS, CONSULTANTS, AND PARTS, EO 98012103. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2892, CONTROL NR 1926. 2 L 7 4 4F 4A25 1998050800797 19980508 00797 WP 1998 5 8 ARWA980489 1 19980424 A 7110 BLOWOUT PANEL DOUG DC8 DC862 3021970 WP NR 3 ENGINE MISSING A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND REMOVED FROM NR 3 ENGINE INBOARD COWLING BLOW OUT PANEL FOR AIRCRAFT 802. FABRICATED AND INSTALLE D NEW BLOW OUT PANEL FOR NR 3 ENGINE IN ACCORDANCE WITH JOSSAIR COMPANY, EO ARW.95141-0103, REV C, WORK ACCOMPLISHED UND ER ARROW AIR FORM M3A, WORK ORDER, 970101, ITEM NR 3152, CONTROL NR 7194. 2 L 7 4 4F 4A25 1998050800798 19980508 00798 WP 1998 5 8 ARWA980490 1 19980424 A 5531 SPAR CAP DOUG DC8 DC862 3021970 WP VERT STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND VERTICAL STABILIZER REAR SPAR CAP LEFT HAND HAS CORROSION. REMOVED SECTION OF SPAR CAP. MACHINED NEW SECTION OF SPAR CAP AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, DRAWING NR 5611409 AND SRM 51-1-21. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 0526, CONTROL NR 6019. 2 L 7 4 4F 4A25 1998050800799 19980508 00799 WP 1998 5 8 ARWA980491 1 19980424 A 5532 SKIN DOUG DC8 DC862 3021970 WP VERT STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE LOWER SECTION HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED F ILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW A IR FORM JW3B, WORK ORDER 970101, ITEM NR 0542, CONTROL NR 6034. 2 L 7 4 4F 4A25 1998050800800 19980508 00800 WP 1998 5 8 ARWA980492 1 19980424 A 5532 SKIN DOUG DC8 DC862 3021970 WP VERT STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND VERTICAL STABILIZER LEADING EDGE UPPER SECTION HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED F ILLER AND DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2856, CONTROL NR 6086. 2 L 7 4 4F 4A25 1998050800801 19980508 00801 WP 1998 5 8 ARWA980493 1 19980424 A 5531 SPAR CAP DOUG DC8 DC862 3021970 WP VERT STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND VERTICAL STABILIZER, REAR SPAR CAP, LEFT AND RIGHT SIDE HAS CORROSION AT STATION 161. REMVOED COR ROSION IN AREA. FABRICATED REPAIR DOUBLERS AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, ACTION NR 35887, FILE NR 98-01-005. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B, WORK ORDER 970101, ITEM NR 2514, CONTROL NR 3086. 2 L 7 4 4F 4A25 1998050800802 19980508 00802 WP 1998 5 8 ARWA980494 1 19980424 A 5512 SKIN DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND RIGHT HAND HORIZONTAL STABILIZER, INBOARD LEADING EDGE HAS CORROSION. REMOVED CORROSION. FABRICA TED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1 AND 51-1-20. WORK ACCOMPLISHED UNDER ARROW AIR JW3B, WORK ORDER 970101, ITEM NR 2464, CONTROL NR 3083. 2 L 7 4 4F 4A25 1998050800803 19980508 00803 WP 1998 5 8 ARWA980495 1 19980424 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS A CRACK ON SKIN. STOP DRILLED CRACK. FA BRICATED REPAIR DOUBLER AND INSTALLED IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1, WORK ACCOMPLISHED UNDER A RROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0261, CONTROL NR 3015. 2 L 7 4 4F 4A25 1998050800804 19980508 00804 WP 1998 5 8 ARWA980496 1 19980424 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER INBOARD LEADING EDGE HAS TEMPORARY REPAIR. REMOVED EXISTING REPAI R. FABRICATED AND INSTALLED REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY SRM 55-2-1. WORK ACCOMPLISHED U NDER ARROW AIR FORM M3A, WORK ORDER, 970101, ITEM NR 0268, CONTROL NR 3022. 2 L 7 4 4F 4A25 1998050800805 19980508 00805 WP 1998 5 8 ARWA980497 1 19980424 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND LEFT HAND HORIZONTAL STABILIZER OUTBOARD LEADING EDGE HAS TEMPORARY REPAIR. REMOVED EXISTING REPA IR. FABRICATED AND INSTALLED NEW REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS AIRCRAFT COMPANY, SRM 55-2-1. WORK ACCOMPLI SHED UNDER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 0062, CONTROL NR 3014. 2 L 7 4 4F 4A25 1998050800806 19980508 00806 WP 1998 5 8 ARWA980498 1 19980424 A 5313 LONGERON DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND INSPECTED LEFT AND RIGHT HAND LONGERON 24 FOR CRACK GROWTH, FOUND CRACK UNDER RT MAIN BOLT. REPLA CED LONGERON 24R HAND PER ARROW AIR FORM M3A, WORK ORDER 970101, ITEM NR 2191, CONTROL NR 5809 AND RED BORDER NR 8064. 2 L 7 4 4F 4A25 1998050800807 19980508 00807 WP 1998 5 8 ARWA980499 1 19980424 A 5754 SKIN DOUG DC8 DC862 3021970 WP LT LE FLAP DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 DURING D-CHECK, FOUND REMOVED TEMPORARY REPAIR LEFT WING LEADING EDGE SLOT AT STA XFS 526. PERFORMED REPAIR OF LEFT HAN D WING LEADING EDGE SLOT AT XFS=526 AS APER EO 98012105 AND ARROW AIR RED BORDER NR 8071. 2 L 7 4 4F 4A25 1998050800808 19980508 00808 NM 1998 5 8 RAAA98B2025 1 19980501 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FWD LT AND AFT LT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISC HARGED. 2 L 7 3 4F A3WE 1998050800809 19980508 00809 SO 1998 5 8 RAAA98E4011 1 19980502 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 AFT LT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998050800810 19980508 00810 SO 1998 5 8 RAAA98E9014 1 19980502 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998050800811 19980508 00811 SO 1998 5 8 RAAA98E9015 1 19980502 A 3350 873100212 SIGN LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED EXIT IDENTIFIER LIGHT ASSY DUE FAI LED. 2 L 7 4 4T 4A22 1998050800812 19980508 00812 1998 5 8 CALA9800725 4 19980501 A 3417 1903925 CADC BOEING 747 747238B 1384828 NM NUMBER 1 FAILED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14024 23608 20534 AFTER DEPARTURE, NUMBER ONE CADC FAILED CAPTAINS FD AND MACH INDICATOR HAD WARNING FLAGS AND NO WIND READ OUT ON INS 1 A ND 3. AIR RETURNED. REMOVED AND REPLACED NUMBER 1 CADC PER MM 34-12-01 AND PERFORMED STATIC LEAK TEST. 2 L 7 4 4F A20WE 1998050800814 19980508 00814 NM 1998 5 8 CALA9800727 1 19980502 A 3246 69564572 WHEEL BOEING 737 7372C0 1384488 NM MLG MISSING A CALA K NONE O OTHER LD LANDING 1 SW 09 10242 20071 THE NUMBER THREE TIRE ASSY DEPARTED THE AIRCRAFT ON LANDING. INSPECTED AXLE, NO DAMAGE. INSTALLED NR 3 TIRE AND WHEEL ASSY WITH NEW SPRING RETAINER AND AXLE NUT PER MM 32-45-11. 2 L 7 2 4F A16WE 1998050800815 19980508 00815 NM 1998 5 8 CALA9800728 1 19980430 A 5753 65464431280A SKIN BOEING 737 7373T0 1384582 NM RT TE FOREFLAP WRINKLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 71314 28863 23365 RIGHT WING O/B FOREFLAP HAS WRINKLED SKIN. REPLACED RIGHT WING O/B FOREFLAP PER MM 27-51-37. 2 L 7 2 4F RT A16WE 1998050800816 19980508 00816 NM 1998 5 8 CALA9800729 1 19980503 A 5315 BAC1505100246 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 23588 MAIN CABIN FLOORBEAM CORRODED STA 312 RBL 10 TO LBL 10 UPPER T ON BEAM AROUND NUT PLATES FORWARD AND AFT SIDES OF BEAM. INSTALLED REPAIR PER SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998050800817 19980508 00817 NM 1998 5 8 CALA9800730 1 19980429 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT PIT STA 1166 FLOOR SUPPORT IS OUT OF LIMITS AT RBL 5. CUT OUT AREA. FABRICATED REPAIR, TREATED, PRIMED AND INSTALL ED PER SRM 53-10-5, 51-10-2, 51-30-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050800818 19980508 00818 NM 1998 5 8 CALA9800731 1 19980502 A 5320 69133833 FITTING BOEING 727 727224 1384076 NM BS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT PIT FS 1183 STR 30 AFT JACK PAD MOUNT CORRODED BEYOND LIMITS. DRILLED, DEBURRED, TREATED, AND PRIMED NEW MOUNT AND NEW INTERCOSTAL PER SRM 51-30-5, 51-10-2, AND MM 51-20-11. INSTALLED NEW MOUNT AND INTERCOSTAL PER SRM 51-30-2. INSTALL ED E/Q BAFFLE PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998050800819 19980508 00819 NM 1998 5 8 CALA9800732 1 19980430 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1007 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT CARGO PIT FLOOR SUPPORT GOUGE AT STA 1007 LBL 15. REMOVED GOUGED AREA, FABRICATED NEW PART AND DOUBLERS AND INSTALL ED PER SRM 51-40-4. 2 L 7 3 4F A3WE 1998050800820 19980508 00820 NM 1998 5 8 CALA9800733 1 19980501 A 7120 ISOLATOR BOEING 727 727224 1384076 NM NR 2 ENGINE SLIPPED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 NUMBER 2 ENGINE FORWARD MOUNTS HAVE EVIDENCE OF SLIPPAGE AND DISBONDING. REPLACED NUMBER 2 ENGINE FORWARD ISOLATORS PER MM 71-21-1. 2 L 7 3 4F A3WE 1998050800821 19980508 00821 NM 1998 5 8 CALA9800734 1 19980504 A 3350 LIGHT BOEING 727 727224 1384076 NM R1 DOOR INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 R1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED R1 EMERGENCY LIGHT ASSY PER MM 33-50-91. 2 L 7 3 4F A3WE 1998050800822 19980508 00822 NM 1998 5 8 CALA9800735 1 19980504 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1166 CORROSION A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT PIT STA 1166 FLOOR SUPPORT IS OUT OF LIMITS AT RBL 5. CUT OUT AREA, FABRICATED REPAIR, TREATED, PRIMED AND INSTALLE D PER SRM 53-105, 51-10-2, 51-30-2 AND 51-20-11. 2 L 7 3 4F A3WE 1998050800823 19980508 00823 NM 1998 5 8 CALA9800736 1 19980503 A 2910 97860B04NN0216 HYD LINE BOEING 727 727227 1384078 NM TAIL SKID LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 76752 21248 LOSS OF A-SYSTEM HYDRAULIC FLUID UPON RETRACTING THE LANDING GEAR. REMOVED AND REPLACED TAIL SKID RIGHT HYDRAULIC LINE PER MM 32-71-12. 2 L 7 3 4F A3WE 1998050800824 19980508 00824 NE 1998 5 8 CALA9800737 2 19980503 A 7230 COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE STALLED A CALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 09 15781 20636 AS AIRCRAFT LEVELING AT FL 350 THE POWER REDUCTION CAUSED HEAVY COMPRESSOR STALLS IN THE NUMBER ONE ENGINE. LARGE FLUCT UATION IN N1, EGT, N2, AND FUEL FLOW. RAN NR 1 ENGINE PER MM 71-00-87 TO TAKEOFF POWER FOR THREE MINUTES, REDUCED POWER . NO STALLS NOTICED. CHECKED BLEED SCHEDULE. TESTS PERFORMED SEVERAL TIMES WITHOUT FAULTS. 2 L 7 3 4F 4 F A3WE E2EA 1998050800825 19980508 00825 NM 1998 5 8 CALA9800738 1 19980503 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10791 20645 ESCAPE PATH LIGHTS INOP ROW 24 TO 29. REPAIRED BROKEN WIRE GOING TO SEATS PER MM 33-50-00. 2 L 7 3 4F A3WE 1998050800826 19980508 00826 NM 1998 5 8 CALA9800739 1 19980503 A 5330 SKIN BOEING 727 727232 1384082 NM BS 693 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 FUSELAGE SKIN IN FORWARD BAG BIN FS 695.700 AT RBL HAS SURFACE CORROSION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PE R SRM 53-30-03. 2 L 7 3 4F A3WE 1998050800827 19980508 00827 NM 1998 5 8 CALA9800740 1 19980503 A 5311 FLANGE BOEING 727 727232 1384082 NM FRAME 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 A 1 INCH CRACK AT FRAME 500 TOP FLANGE RADIUS ABOVE 24 L. FABRICATED NEW DOUBLER AND INSTALLED IN ACCORDANCE WITH SRM 5 1-40-3. HEAT TREATED PER BAC 5602. 2 L 7 3 4F A3WE 1998050800828 19980508 00828 NM 1998 5 8 CALA9800741 1 19980503 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10791 20645 LT EXIT LIGHT INOP OVER EXIT IN CABIN. REPAIRED BROKEN WIRE AT EXIT IDENTIFIER, OPS CHECK PER 33-50-00. 2 L 7 3 4F A3WE 1998050800829 19980508 00829 NM 1998 5 8 CALA9800742 1 19980503 A 5320 FLANGE BOEING 727 727232 1384082 NM BS 700 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 TOP FLANGE RADIUS FS 700 ABOVE 24 L HAS 1.5 INCH CRACK. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2 AND 51-40-3. 2 L 7 3 4F A3WE 1998050800830 19980508 00830 NM 1998 5 8 CALA9800743 1 19980503 A 5320 65595943 JAMB BOEING 727 727232 1384082 NM C1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 C-1 DOOR JAMB BENT/TORN AT TWO PLACES. REMOVED AND REPLACED DOOR JAMB AS REQUIRED PER SRM 51-10-1. 2 L 7 3 4F A3WE 1998050800831 19980508 00831 NM 1998 5 8 CALA9800744 1 19980503 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 VERT STAB INNER COMPARTMENT NR 7 STRINGER NR 2 AND NR 3 CRACKED (2) AT ATTACH BOLT. REPAIRED NR 7 RT STRINGER NR 2 AND NR 3 ON VERTICAL STAB PER SRM 55-30-4. 2 L 7 3 4F A3WE 1998050800832 19980508 00832 NM 1998 5 8 CALA9800745 1 19980503 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 VERT STAB INNER COMPARTMENT NR 1 CANTED STATION 1303 HAS CRACK (2.5) AT RT LOWER CORNER. ALSO, CRACK (1) AT RT UPPER CO RNER. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLERS PER SRM 51-40-2. 2 L 7 3 4F A3WE 1998050800833 19980508 00833 NM 1998 5 8 CALA9800746 1 19980503 A 3520 225057 OXY CONTL UNIT BOEING 727 727232 1384082 NM PAX COMPT FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10791 20645 FWD OXYGEN PASSENGER DROP FAILED FUNCTIONAL TEST. REPLACED OXYGEN CONTROL UNIT AND PERFORMED PNEUMATIC OXYGEN DROP PER MM 35-21-00. 2 L 7 3 4F A3WE 1998050800834 19980508 00834 NM 1998 5 8 CALA9800747 1 19980503 A 5311 FRAME BOEING 727 727232 1384082 NM FRAME 520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10791 20645 TOP FLANGE AT FRAME 520 HAS .5 INCH CRACK ABOVE STR 26R. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-6. HEAT TREAT PER BAC 5602. 2 L 7 3 4F A3WE 1998050800835 19980508 00835 NM 1998 5 8 CALA9800748 1 19980501 A 3350 1102837 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59792 20646 AFT AIRSTAIR EMERGENCY LIGHT O/H INOP. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F A3WE 1998050800836 19980508 00836 WP 1998 5 8 CALA9800749 1 19980502 A 5320 991158221 BEAM DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 F/S/D NR 4 BEAM IS CRACKED AT FORWARD END APPROX 1. REMOVED CRACKED BEAM AND INSTALLED SERVICEABLE PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998050800837 19980508 00837 WP 1998 5 8 CALA9800750 1 19980501 A 5210 995576311 INTERCOSTAL DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 MAIN CABIN DOOR INTERCOSTAL AFT OF DOOR LOCK MECHANISM IS CRACKED (1) WHERE IT ATTACHES TO OUTSIDE HANDLE RECESS. INSTA LLED NEW INTERCOSTAL PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998050800838 19980508 00838 NM 1998 5 8 UPS98426530 1 19980504 A 3350 LIGHT BOEING 747 747123F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 677UP 20391 INSPECTION TYPE-N/A, NR 1 LT DOOR EMERG LIGHT INOP (REF ITEM M 150853). FOUND PIN 9 PUSHED BACK INTO CONECTOR D1561J. R EINSTALLED PIN PER 33-51-12, CHECKED NORMAL CLEARING M 150853. 2 L 7 4 4F A20WE 1998050800839 19980508 00839 WP 1998 5 8 UPS98826525 1 19980409 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-C, THE FUSELAGE SKIN AT STA 850 AND STR 24L JUST ABOVE THE WING HAS HEAVY CORROSION. REPAIRED AREA IAW 8110-3 APPROVED DHC SK803-975. 2 L 7 4 4F RT 4A25 1998050800840 19980508 00840 WP 1998 5 8 UPS98826528 1 19980330 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, FLOORBEAM SUPPORT FITTING FS 100 L-27R LWR I/B FLANGE HAS HEAVY EXFOLIATION CORROSION. REMOVED, FABR ICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3773077. 2 L 7 4 4F RT 4A25 1998050800841 19980508 00841 WP 1998 5 8 UPS98826529 1 19980325 A 5730 SKIN DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-D, LT WING L/E UPPER SURFACE CRACKED AT FASTENER HOLE BTWN REPAIR DOUBLERS ON SECTION JUST O/B OF NR 1 E NG. SUSPECT HEAVY CORROSION UNDER SKIN. CUT OUT CORRODED AND DAMAGED AREA AND REPAIRED IAW DHC SK-803-156. WITH REF TO UPS EO DC8-5720-10402-A. 2 L 7 4 4F RT 4A25 1998050800842 19980508 00842 WP 1998 5 8 UPS98826532 1 19980426 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RIB CRACKED ON RT WING L/E AT APPROX STA XS 225 NR 3 ENG STUB WING. REPAIRED IAW SRM 57-3-1. 2 L 7 4 4F RT 4A25 1998050800843 19980508 00843 WP 1998 5 8 UPS98826533 1 19980422 A 5320 45976431 FITTING DOUG DC8 DC871F 302199D WP BS 20 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, HEAVY CORROSION ON RT CUSP TO FRAME FITTING FS 20. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050800844 19980508 00844 WP 1998 5 8 UPS98826534 1 19980422 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 978 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, LONGERON 24R CRACKED IN HORIZONTAL FLANGE AT AFT END FS 978. REPAIRED IAW SRM 53-2-2. 2 L 7 4 4F RT 4A25 1998050800845 19980508 00845 WP 1998 5 8 UPS98826535 1 19980427 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 85-90 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, LONGERON 29R BETWEEN FS 85 AND 90 CORROSION REMOVAL IS BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 FIG 10 . 2 L 7 4 4F RT 4A25 1998050800846 19980508 00846 WP 1998 5 8 UPS98826536 1 19980424 A 5720 97532978 ANGLE DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, VERT ANGLE CRACKED BTWN RIBS ON RT WING L/E AT STA XS 250.089. REMOVED, FABRICATED AND INSTALLED REP LACEMENT ANGLE IAW SRM 51-1-21 AND DWG 9752397. 2 L 7 4 4F RT 4A25 1998050800847 19980508 00847 WP 1998 5 8 UPS98826537 1 19980425 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, LONG 28R O/B FLANGE CRACKED AT FRAME 180 ATTACH BOLT. REPAIRED IAW SRM 53-4-1. 2 L 7 4 4F RT 4A25 1998050800848 19980508 00848 WP 1998 5 8 UPS98826538 1 19980425 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 360-380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, INTERCOSTAL CRACKED BTWN FS 360 TO 380 AT LONG-33R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT IA W SRM 51-1-20D AND DWG 5750726. 2 L 7 4 4F RT 4A25 1998050800849 19980508 00849 WP 1998 5 8 UPS98826540 1 19980422 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 766.250 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING L/E AT XFS 766.250 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998050800850 19980508 00850 WP 1998 5 8 UPS98826541 1 19980422 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 697.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING L/E AT STA XFS 697.5 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998050800851 19980508 00851 WP 1998 5 8 UPS98826542 1 19980422 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 710 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING L/E AT STA XFS 710 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998050800852 19980508 00852 EU 1998 5 8 QXEA9800627 1 19980501 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 EMERGENCY LIGHT AT THE OVERWING EXIT, AT SEAT 9E IS OUT. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1998050800853 19980508 00853 EU 1998 5 8 QXEA9800628 1 19980503 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 EMERGENCY LIGHT AT SEAT 8B REPORTED INOPERATIVE. MAINTENANCE RELAMPED AND SECURED WITH BREAKAWAY SAFETY WIRE, OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A20EU 1998050800854 19980508 00854 EU 1998 5 8 QXEA9800629 1 19980502 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 EMERGENCY EVACUATION LIGHT ON ROWS 5, 6, 9 AND 10 ARE INTERMITTENTLY ON. MAINTENANCE REPAIRED A CANNON PLUG ON THE EMER GENCE BATTERY PACK AT 9AB, OPERATIONAL CHECKS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998050800855 19980508 00855 EU 1998 5 8 QXEA9800630 1 19980504 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 THE EMERGENCY LIGHT AT ROW 9A WAS FOUND INOPERATIVE. MAINTENANCE RELAMPED AND FUNCTION CHECKED WORK, CHECKED GOOD. 2 L 7 2 4F RT A20EU 1998050800856 19980508 00856 EU 1998 5 8 QXEA9800631 1 19980430 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 THE FORWARD CABIN EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE SIGN AND TESTED, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998050800857 19980508 00857 EU 1998 5 8 QXEA9800632 1 19980501 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 THE EMERGENCY EVACUATION LIGHT AT SEAT 4B WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKED WIRE AT THE LIGHT. SYSTEM TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998050800858 19980508 00858 EU 1998 5 8 QXEA9800633 1 19980503 A 3350 6008905 BATTERY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 THE EMERGENCY EVACUATION LIGHTS ON THE RIGHT ESCAPE HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK LOCATED ABOVE SEAT ROW 7. SYSTEM WAS TESTED AND OPERATED NORMAL. 2 L 7 2 4F RT A20EU 1998050800859 19980508 00859 WP 1998 5 8 ABXA9800443 1 19980503 A 7931 1G1741A SWITCH DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 853AX 46037 669202 NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED ON CLIMBOUT. OIL QUANTITY, TEMPERATURE AND PRESSURE WERE NORMAL. PERFOR MED ABNORMAL PROCEDURE. LIGHT REMAINED ON. PRECAUTIONARY ENGINE SHUTDOWN. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITC H. OPS CHECKED NORMAL IAW DC8 MM 79-32-2. 2 L 7 4 4F 4 F 4A25 1E8 1998050800860 19980508 00860 WP 1998 5 8 MWEA98561 1 19980426 A 4900 38025611 APU DOUG DC9 DC932 3022066 WP AFT FUSELAGE DEFECTIVE A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 502ME 48132 AFTER COMPLETING BEFORE START CHECKLIST EXTERNAL POWER WENT OFF LINE AND CABIN FILLED WITH SMOKE. MTC DEFERRED ENTIRE A PU. 2 L 7 2 4F A6WE 1998050800861 19980508 00861 WP 1998 5 8 MWEA98562 1 19980503 A 5312 59174637N BULKHEAD DOOR DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FOUND CRACK ON VENTRAL DOOR JAMB UPPER RIGHT CORNER. MTC REPAIRED WITH 5 DOUBLERS. 2 L 7 2 4F A6WE 1998050800862 19980508 00862 WP 1998 5 8 MWEA98563 1 19980503 A 5320 59164411 SPLICE DOUG DC9 DC915 3022036 WP BS 237 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FOUND CRACK ON FORWARD CARGO LONGERON 2L AT STATION 237 ON LEFT VERTICAL LEG. MTC FABRICATED AND INSTALLED LONGERON AND SPLICE. 2 L 7 2 4F A6WE 1998050800863 19980508 00863 WP 1998 5 8 MWEA98564 1 19980503 A 5312 5917579123 STRAP DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD MISINSTALLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 900ME 45841 THE AFT VENTRAL DOOR JAMB UPPER LEFT AND RIGHT CORNER STRAPS HAVE BEEN TRIMMED INCORRECTLY. MTC FABRICATED AND INSTALLE D STRAPS. 2 L 7 2 4F A6WE 1998050800864 19980508 00864 WP 1998 5 8 MWEA98565 1 19980503 A 5713 59112761N STRINGER DOUG DC9 DC915 3022036 WP WS 67 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FOUND CORROSION ON LEFT WING STRINGER 12 AFT LEG AT STATION XRS 67. MTC FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 1998050800865 19980508 00865 NE 1998 5 8 P5CA9800765 2 19980430 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 2 MALFUNCTIONED A P5CA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 WP 23 857FT 20246 662652 VIBRATION ON TAKEOFF. RETARDED AND ADVANCED NR 2 ENG THROTTLE. VIBRATION FOLLOWED THROTTLE MOVEMENT. A/C PACKS WERE O FF. REMOVED AND REPLACED NR 2 ENGINE PER MM 71-00-00. OPS CHECK, LEAK CHECK ALL NORMAL ON ENG RUN-UP PER MM 71-00-00. 2 L 7 4 4F 4 F A20WE E20EA 1998050800866 19980508 00866 NE 1998 5 8 P5CA9800766 2 19980501 A 7320 63030000 ACTUATOR BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE INOPERATIVE A P5CA A UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 WP 23 853FT 19753 662991 NR 4 ENG FAILED IN CRUISE. TRIED TO RELIGHT 2 TIMES AT 2 DIFFERENT ALTITUDES AND WOULD NOT RELIGHT. REMOVED ENGINE FUE L CONDITION MOTOR ACTUATOR PER MM 76-11-04 PG 401 TO 404. GROUND CHECK OK STATICALLY. INSPECTED FUEL PUMP FILTER, NO C ONTAMINATION FOUND. LEAK CHECK OK. FIREWALL C/PS CLEANED AND CHECKED. OP CHECK FUEL CONDITION MOTOR ACTUATOR GOOD. 2 L 7 4 4F 4 F A20WE E20EA 1998050800867 19980508 00867 NM 1998 5 8 P5CA9800767 1 19980430 A 5751 65B081269 FITTING BOEING 747 747132 1384882 NM LT AILERON GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT I/B AILERON I/B PRIMARY HINGE WING FITTING LT SIDE IS GOUGED BY RETAINER BOLT HOLE AREA. BLENDED GOUGE LESS THAN 1 0 PERCENT MATERIAL LOSS PER SRM 57-50-01. 2 L 7 4 4F A20WE 1998050800873 19980508 00873 CE 1998 5 8 98ZZZX1652 1 19980403 A 8120 8797 GEAR BEECH 18 G18S 1151010 CE REAR SECTION FAILED A KVJA K NONE O OTHER IN INSP/MAINT 1 SW 05 621KE 91 BA556 SUPERCHARGER INPUT GEAR FAILED. CAUSE UNKNOWN. 1 L 7 2 3R A765 1998050800882 19980508 00882 CE 1998 5 8 98ZZZX1661 1 19980403 A 8120 C1650060107 VALVE CESSNA 402 402C 207590R CE WASTEGATE LEAKING A GNXA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SW 01 38CJ 682 402C0023 DURING FLIGHT AT 10,000 MSL, PILOT NOTICED THAT OIL PRESSURE ON RIGHT ENGINE WAS DROPPING SLOWLY AND OIL TEMP WAS RISING SLOWLY FOLLOWED SHORTLY BY A COMPLETE LOSS OF MANIFOLD PRESSURE. THE PILOT TOOK PRECAUTIONARY MEASURES AND SHUT DOWN E NGINE. HE CONTINUED ON AND MADE AN UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE PERSONNEL FOUND THE WASTEGATE ACTUATO R FAILED AND ALL THE ENGINE OIL WAS DUMPED. INSPECTION REVEALED THE SEAL INSIDE THE ACTUATOR WAS BAD. AN OVERHAUL OF T HE COMPLETE ASSY REPAIRED THE PROBLEMS. NO KNOWN CAUSE FOR SEAL FAILURE. 1 L 7 2 3O A7CE 1998050800905 19980508 00905 NE 1998 5 8 98ZZZX1684 2 19980416 A 7320 430110212 ACTUATOR AVP1 BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE FLOW FENCE FAILED A BAQA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 EA 03 967LS 181 7067 LE45224 INTERNAL BREAKDOWN OF AIR FLOW MODULATOR (FLOW FENCE ACTUATOR) CAUSED THE OCCURRENCE OF COMPRESSOR STALLS DURING APPROAC H TO LANDING. 1 G 7 2 3U 3 U H13EU E5NE 1998050800908 19980508 00908 CE 1998 5 8 98ZZZX1687 1 19980401 A 3310 10901VM21L2000 FLOODLIGHT LEAR 35 35A 5170602 CE INST PANEL BURNED A IJDA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 01 110FT 471 SMOKE NOTED AT INSTRUMENT GLARESHIELD DETERMINED TO BE FROM FLUORESCENT FLOODLIGHT. PORTION OF FLOODLIGHT LENS (PLASTIC ) WAS OVERHEATED. PLASTIC SHEATH AROUND COLD CATHODE TUBE AT POWER INPUT END WAS CHARRED/OVERHEATED. ASSY REMOVED FROM AIRCRAFT. 2 L 7 2 4F A10CE 1998050800911 19980508 00911 CE 1998 5 8 98ZZZX1689 1 19980406 A 3231 15810038 CAM 1158100366 BEECH 99 99 1154002 CE RT OTBD MLG DOOR BENT A JDWA O OTHER J WARNING INDICATION AP APPROACH 1 CE 09 118SF U32 PIC REPORTED THE INABILITY TO EXTEND THE LANDING GEAR ELECTRICALLY, WITH A LOUD BANG NOTED IMMEDIATELY UPON EXTENSION. T HE LANDING GEAR WAS EXTENDED MANUALLY, AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. SUBSEQUENT INVESTIGATION DISCL OSED A TRIPPED LANDING GEAR CIRCUIT BREAKER, AND A BENT RT OUTBOARD MLG DOOR ACTUATING CAM. THE GEAR DOOR ROLLER ASSY S TRUCK THE UNDERSIDE OF THE LANDING GEAR ACTUATING CAM CAUSING THE GEAR TO BIND IN THE WHEEL WELL. INVESTIGATION FAILED TO DETERMINE A CAUSE. THE CAM ASSY MAY HAVE BEEN MIS-RIGGED, OR FAILED TO SNAP OVERCENTER DUE TO WEAK RETURN SPRINGS. 1 L 7 2 3T A14CE 1998050800921 19980508 00921 NE 1998 5 8 98ZZZX1699 2 19980329 A 7200 ENGINE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE NR 1 MALFUNCTIONED A HDNA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 03 914ET 178 BB0022 TWO MINUTES AFTER TAKEOFF, POWER DECREASED TO 20 - 40 PERCENT OF NORMAL ON NR 1 ENGINE. RETURNED FOR PRECAUTIONARY LAND ING. ENGINE APPEARED TO FUNCTION NORMALLY BELOW 50 PERCENT TORQUE, ABOVE 50 PERCENT, TORQUE WOULD DECREASE. NO FURTHER INCIDENT OCCURRED. AIRCRAFT SHUT DOWN. ELECTRICAL CONNECTIONS CHECKED. OPERATIONAL CHECK FLIGHT PERFORMED AND RETURN ED TO SERVICE. 1 G 7 2 3U 3 U O H88EU E42NE 1998050800923 19980508 00923 NM 1998 5 8 USAA980132 1 19980327 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 294-325 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 43087 22444 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 30 INCH STATION 294 TO 325 STRINGER 24L. SPLICED I N NEW STRINGER SECTION, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01. CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800924 19980508 00924 EU 1998 5 8 USAA980150 1 19980221 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU BS 3870 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 889US 11358 PIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT, FOUND BL 0 CORRODED AT STATION 3870 TO AFT OF 5305. MANUFACTURED NE W BEAM AND INSTALLED PER SRM 53-12-10 FIG 8 ITEM 390. (M) 2 L 7 2 4F RT 1998050800925 19980508 00925 EU 1998 5 8 USAA980149 1 19980221 A 5320 WEB FOKKER F28 F28MK0100 4990807 EU BS 5305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 889US 11358 PIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT, FOUND BL 0 SUPPORT WEB CORRODED AT STATION 5305. MANUFACTURED AND I NSTALLED NEW WEB PER SRM 53-12-10 FIG 8 ITEM 840. (M) 2 L 7 2 4F RT 1998050800926 19980508 00926 NM 1998 5 8 USAA980148 1 19980420 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 237 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 49556 21816 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH CORRODED AREA AND OTHER SMALLER AREAS AT BS 237 LBL 24 TO RBL 24 NOSE WHEEL WELL UPPER CHORD ANGLE. FABRICATED NEW ANGLE AND INSTALLED, REPAIRED PER DRW 65-45819 SRM 51-10-1. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800927 19980508 00927 NM 1998 5 8 USAA980147 1 19980402 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 920-932 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 21816 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 10 INCH CORRODED AREA BS 920 TO BS 932 STRINGER 25L STRINGER. REMOVED CORRODED AREA, INSTALLED REPAIR PARTS, REPAIRED PER T/R 53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800928 19980508 00928 NM 1998 5 8 USAA980146 1 19980402 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 49556 21816 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 663 RBL 25 WL 202 UPPER CHORD ANGLE. INSTALLED DO UBLER, REPAIRED PER DRAWING 65C37732. (M) 2 L 7 2 4F A16WE 1998050800929 19980508 00929 NM 1998 5 8 USAA980144 1 19980402 A 5330 SKIN BOEING 737 737201 1384454 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 49556 21816 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CRACK .125 INCH SKIN RT AFT SERVICE DOOR CUTOUT FORWARD LOWER CORNER. C UTOUT CRACK FABRICATED AND INSTALLED DOUBLER, REPAIRED PER BOEING DRWING 65C27287. (M) 2 L 7 2 4F A16WE 1998050800930 19980508 00930 NM 1998 5 8 USAA980143 1 19980402 A 5311 FRAME BOEING 737 737201 1384454 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 49556 21816 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK STATION 520 INBOARD OF CHORD LBL 21 FRAME. INSTALLED DOUB LER, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1998050800931 19980508 00931 NM 1998 5 8 USAA980141 1 19980402 A 5311 FRAME BOEING 737 737201 1384454 NM BS 360 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 49556 21816 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 6 INCH AREA CORRODED AT STATION 360, BETWEEN S28L AND STRINGER 28R FRAME. INSTALLED FRAME REPAIR SECTION AND REPAIRED PER SRM 53-10-04 FIG 10. CORROSION TASK NR C53-202-01, CORROSI ON LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800932 19980508 00932 NM 1998 5 8 USAA980155 1 19980404 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 41923 22878 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON BULKHEAD SUPPORT ANGLE 3 INCH BY 1.5 INCH BS 1016 BULKHEAD (FORWARD FACE) JUST ABOVE DRAIN HOLE BBL '0'0. INSTALLED CHANNEL REPAIR AND SKIN REPAIR, REPAIRED PER SRM 51-40-3 FIG 1 AND SRM 53-10-4 FIG 3. CORROSION TASK NR C53-208-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800933 19980508 00933 NM 1998 5 8 USAA980154 1 19980404 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 953 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 41923 22878 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CRACK .125 INCH AFT ENTRY DOOR CUTOUT UPPER HINGE STATION 953 SKIN. INS TALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 21A. (M) 2 L 7 2 4F A16WE 1998050800934 19980508 00934 NM 1998 5 8 USAA980153 1 19980404 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 927-947 CREASE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 41923 22878 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1.5 INCH BY 5 INCH CREASE IN SKIN BS 927-947 AND 933-943, STRINGER 17L-1 9L. REMOVED PREVIOUS DOUBLER AND CUTOUT DAMAGED AREA, INSTALLED DOUBLER AND FILLERS, REPAIRED PER SRM 53-30-3 FIG 6. ( M) 2 L 7 2 4F A16WE 1998050800935 19980508 00935 NM 1998 5 8 USAA980152 1 19980404 A 5320 STRAP BOEING 737 7372B7 1384560 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 22878 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND TWO .25 INCH CRACKS, BS 312 LOWER CHORD STABILIZER STRAP. INSTALLED REP AIR DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998050800936 19980508 00936 NM 1998 5 8 USAA980151 1 19980404 A 5314 KEEL BEAM BOEING 737 7372B7 1384560 NM BS 727/722 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 266AU 41923 22878 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH CORRODED AREA TWO LEFT KEEL BEAMS BS 727 AND 722. IN STALLED REPAIR STRAP, REPAIRED PER EA 43828. (M) 2 L 7 2 4F A16WE 1998050800937 19980508 00937 NM 1998 5 8 USAA980142 1 19980402 A 5330 SKIN BOEING 737 737201 1384454 NM BS 759 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 49556 21816 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND CRACK AT STA 759 S17R, 3 INCH LONG SKIN. REMOVED PRE-DOUBLER AND BLIN D FASTENERS, FABRICATED DOUBLER AND INSTALLED PER SRM 53-30-3 FIG 25 AND EA 30778. (X) 2 L 7 2 4F A16WE 1998050800938 19980508 00938 NM 1998 5 8 USAA980145 1 19980402 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 227AU 49556 21816 INT - DURING 'Q-2' CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STA 727 A PLUS 10 INCHES BELOW S17R SKIN. REMOVED TWO PR EVIOUS DOUBLERS, CUT OUT DAMAGED SKIN. FABRICATED FILLER AND INSTALLED. REPAIRED PER SRM 53-30-3 FIG 6. (X) 2 L 7 2 4F A16WE 1998050800939 19980508 00939 NM 1998 5 8 USAA980133 1 19980327 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 42937 22444 INT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND 1 INCH BY 8 INCH CORROSION STA 1006 STR 26L. INSTALLED REPAIR ANGLES, REPAIRED PER SRM 53-10-3. CORROSION TAKE NR: C53-202-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1998050800940 19980508 00940 NM 1998 5 8 USAA980137 1 19980327 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 908 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 42937 22444 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 4 INCH BY 4 INCH STATION 908, STRINGER 21L. CUT OUT DAMAGE AN D INSTALLED STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800941 19980508 00941 NM 1998 5 8 USAA980135 1 19980327 A 5320 BEAM BOEING 737 737201 1384454 NM BS 235 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 42937 22444 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AROUND NUT PLATES STATION 235 BL '0' TO RBL 1 5 NOSE W/W CEILING TRANSVERSER BEAM. REMOVED AND INSTALLED NEW PREFAB TRANSVERSER BEAM, FABRICATED AND INSTALLED ZEE ST RAPS. REPAIRED PER SRM 51-10-1 DRAWING 69-37989. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800942 19980508 00942 NM 1998 5 8 USAA980134 1 19980327 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 494-325 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 42937 22444 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 2 INCH BY 30 INCH CORRODED AREAS CORROSION ON STRINGER 24L FROM BS 294.5 TO BS 325.3 STRINGER. INSTALLED DOUBLER REPAIR ANGLE, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-202-01, CORROSI ON LEVEL 2. (M) 2 L 7 2 4F A16WE 1998050800943 19980508 00943 WP 1998 5 8 USAA980157 1 19980405 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 984 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807US 45745 48039 PIT - DURNIG C-2 CHECK, FOUND .5 INCH CRACK AT STATION 984 LONGERON 20 LEFT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10 -28. (M) 2 L 7 2 4F A6WE 1998050800944 19980508 00944 WP 1998 5 8 USAA980156 1 19980405 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 984 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 807US 45745 48039 PIT - DURING C-2 CHECK, FOUND .5 INCH CRACK IN SKIN AT STATION 984 LONGERON 20 RIGHT. INSTALLED DOUBLER PER TYPICAL REP AIR 53-10-28. (M) 2 L 7 2 4F A6WE 1998050800945 19980508 00945 NM 1998 5 8 USAA980136 1 19980327 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 967-987 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 242US 42937 22444 INT - DURING 'Q-4' CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 20 INCHES, STA 967 TO STA 987, STR 25R. INSTALLED REPAIR ANGLES AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1998050800946 19980508 00946 WP 1998 5 8 USAA980140 1 19980327 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 976VJ 39490 48147 PIT - DURING C-5 CHECK, FOUND .25 INCH CRACK IN SKIN AFT OF STATION 1087 BETWEEN LONGERON 3R AND 4R. REPAIRED DOUBLER 2 024T3 .080 FILLER 2014T6 .063 PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1998050800947 19980508 00947 WP 1998 5 8 USAA980138 1 19980327 A 5320 591214129 ANGLE DOUG DC9 DC931 3022065 WP BS 942 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 976VJ 39490 48147 PIT - DURING C-5 CHECK, FOUND .375 INCH CRACK AT RT DRAG ANGLE AT STATION 942. REPAIRED MFG STRAP 7075T6 .125 AND SPLIC E 7075T6 .190 PER SRM 53-05 FIG 23A SHEET NR 2 CONF 502. (M) 2 L 7 2 4F A6WE 1998050800948 19980508 00948 WP 1998 5 8 USAA980139 1 19980331 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 976VJ 39490 48147 PIT - DURING C-5 CHECK, FOUND .625 INCH CRACK AT STATION 965 BELOW LONGERON 13 RT. REPAIRED FINGER DOUBLER .032 RITANIU M AND PLUG 2024T3 .063 PER SRM 53-04 FIG 32 AND FIG 18. (M) 2 L 7 2 4F A6WE 1998050800949 19980508 00949 EU 1998 5 8 980407 1 19980407 A 5315 D28254001 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU BS 6030 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 888AU 11357 PIT - DURING Q-1 CHECK, FOUND CORROSION 8 FT LONGERON FLOORBEAM ON SEAT TRACK BL 600R JUST AFT OF P-SPLICE STATION 6030. REPAIRED BEAM, BEYOND PRODUCTION SPLICE, EXTENDED 39 IN AFT TO STATION 7300 WHERE NEW PRODUCTION SPLICE WAS MADE PER E 0 49367. MODIFIED PART INSTALLED WAS D28254-001 (NOTE) USED RAW STOCK BEAM D95166-001, 115-7546. (M) 2 L 7 2 4F RT 1998050800950 19980508 00950 EU 1998 5 8 USAAF98034 1 19980401 A 2131 21185264 CONTROLLER FOKKER F28 F28MK0100 4990807 EU CABIN MALFUNCTIONED A USAA B EMER. DESCENT J WARNING INDICATION DE DESCENT 1 EA 19 886US 11346 CLT - FLT 1079 - EN ROUTE FROM MDT TO CLT WHILE DESCENDING FROM 350 TO 310, AIRCRAFT EXPERIENCED A LOSS OF CABIN PRESSUR E. A RAPID DESCENT TO 10,000 FEET WAS MADE. MASKS DID NOT DROP. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AUTO PRESSURE CONTROLLER, PRIMARY AND SECONDARY OUTFLOW VALVES AND PERFORMED A HULL LEAK CHECK. (M) 2 L 7 2 4F RT 1998050800951 19980508 00951 EU 1998 5 8 USAAF98035 1 19980404 A 3260 EAADL8529403 DIMMING UNIT FOKKER F28 F28MK0100 4990807 EU E/E COMPT INOPERATIVE A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 862US 11300 PVD - FLT 396 - ON APPROACH TO PVD WHEN LANDING GEAR WAS SELECTED DOWN, NO GREEN GEAR SAFE LIGHTS ILLUMINATED. NO FAULT MESSAGES WERE ILLUMINATED. TOWER FLYBY INDICATED THAT GEAR APPEARED DOWN AND LOCKED. FLIGHT LANDED PVD WITHOUT FURTHE R INCIDENT. MAINTENANCE REPLACED THE NR 5 DIMMING AND SUPPLY UNIT. (M) 2 L 7 2 4F RT 1998050800952 19980508 00952 WP 1998 5 8 USAAD98065 1 19980407 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 DCA - FOUR LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. ( X) 2 L 7 2 4F A6WE 1998050800953 19980508 00953 WP 1998 5 8 USAAD98066 1 19980408 A 3350 081691 SOCKET DOUG DC9 DC931 3022065 WP CABIN CORRODED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 931VJ 47188 CMH - THE AFT SECTION OF THE CABIN FLOOR TRACK EMERGENCY LIGHTS AND THE CATWALK LIGHTS WERE INOPERATIVE. MAINTENANCE RE PLACED A LIGHT SOCKET FOR THE CATWALK LIGHTS AND REPAIRED A SHORTED WIRE NEAR THE TAIL CONE RELEASE HANDLE. (M) 2 L 7 2 4F A6WE 1998050800954 19980508 00954 WP 1998 5 8 USAAD98059 1 19980401 A 2410 696233B CSD DOUG DC9 DC931 3022065 WP LT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 966VJ 47420 PIT - FL 992 - DURING CRUISE, THE LEFT GENERATOR FAILED WITH NO VOLTS OR FREQS. THE APU WAS ALREADY ON MEL. THE AIRCRA FT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT CSD AND GENERATOR. (M) 2 L 7 2 4F A6WE 1998050800955 19980508 00955 WP 1998 5 8 USAAD98063 1 19980404 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 959VJ 47352 IND - AFT CABIN CEILING EMERGENCY LIGHTS DIM. MAINTENANCE REPLACED THE AFT CABIN CEILING EMERGENCY LIGHTS BATTERIES. ( M) 2 L 7 2 4F A6WE 1998050800956 19980508 00956 WP 1998 5 8 USAAD98062 1 19980404 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 991VJ 47310 CMH - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY SUPPLY. (M) 2 L 7 2 4F A6WE 1998050800957 19980508 00957 WP 1998 5 8 USAAD98061 1 19980324 A 3350 110049 CHARGER DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 920VJ 48140 ORF - THE AFT CABIN FLOOR AND TAIL COMPARTMENT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LI GHT CHARGER ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998050800958 19980508 00958 WP 1998 5 8 USAAD98060 1 19980402 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 991VJ 47310 IND - THE SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998050800959 19980508 00959 NM 1998 5 8 USAABB98024 1 19980329 A 2560 140N2766 BAR LOCK 146N6150 BOEING 757 757225 1384959 NM R4 DOOR MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 618AU 22210 PHL - DURING RON MAINTENANCE, THE R4 DOOR WAS OPENED BY UTILITY PERSONNEL. THE INDICATIONS ON THE DOOR SHOWED THAT THE SLIDE HAD BEEN DISARMED, BUT THE SLIDE DEPLOYED. MAINTENANCE FOUND THAT THE GIRT BAR ON THE SLIDE WAS MISSING A SLIDER (BAR LOCK). IT IS BELIEVED THAT THE GIRT BAR HUNG UP IN THE DOOR THRESHOLD/FLOOR FITTING, THEREBY DEPLOYING THE SLIDE W HEN THE DOOR WAS OPENED. THE FLIGHT CREW HAD NOT REPORTED THE INOPERATIVE DOOR SLIDE LIGHT ON THE PREVIOUS FLIGHT. (M) 2 L 7 2 4F RT A2NM 1998050800960 19980508 00960 NM 1998 5 8 USAASB98073 1 19980321 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 576US 23741 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT SEAT ROWS 2, 3, AND 4. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998050800961 19980508 00961 NM 1998 5 8 USAASB98071 1 19980320 A 3260 189929 UPLOCK SENSOR BOEING 737 737301 1384611 NM RT MLG FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 558AU 23512 BOS - FLT 945 - FOLLOWING TAKEOFF ROTATION FROM BOS, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED WITH GEAR HANDLE IN THE UP OR OFF POSITION. CREW DECIDED TO RETURNED TO FIELD AT BOS WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLOCK SENSOR. OPE RATIONAL CHECK GOOD PER MM 32-61. (M) 2 L 7 2 4F RT A16WE 1998050800962 19980508 00962 NM 1998 5 8 USAASB98086 1 19980401 A 3350 CONNECTOR BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 284AU 23131 CLT - MAINTENANCE FOUND 50 PERCENT OF THE EMERGENCY LOW LEVEL LIGHTING INOP. MAINTENANCE FOUND A LOW LEVEL LIGHTING CAN NON PLUG BAD. WHEN CANNON PLUG WAS HANDLED AND SHAKEN, LIGHTS FLICKERED. WIRES WERE PULLED AND APPEARED TO BE OVERCRIM PED WHEN INSTALLED. REPLACED CANNON PLUG. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998050800963 19980508 00963 NM 1998 5 8 USAASB98089 1 19980407 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 283AU 23116 ALB - MAINTENANCE FOUND FOUR ROWS OF LOW LEVEL LIGHTING, AFT OF THE OVERWING EXIT IN THE MID CABIN, INOP. MAINTENANCE R EMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998050800964 19980508 00964 EU 1998 5 8 USAAF98031 1 19980325 A 3231 STOP FOKKER F28 F28MK0100 4990807 EU LT MLG DOOR OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 889US 11358 CLT 1856 - CREW RECEIVED LEFT MAIN LANDING GEAR WARNING MESSAGE DURING RETRACTION ON THE MFDU. CREW LOWERED THE GEAR AN D RECEIVED A NORMAL DOWN AND LOCKED INDICATION. THE FLIGHT THEN RETURNED TO CLT WHERE LANDING WAS WITHOUT FURTHER INCID ENT. MAINTENANCE FOUND LEFT GEAR DOOR STOP OUT OF ADJUSTMENT. ADJUSTED THE DOOR STOP. (M) 2 L 7 2 4F RT 1998050800965 19980508 00965 EU 1998 5 8 USAAF98032 1 19980325 A 3230 DOWNLOCK PIN FOKKER F28 F28MK0100 4990807 EU NLG NOT ENGAGED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 887US 11349 PWM - FLT 1824 - ON APPROACH, NOSE GEAR WAS SHOWING AN UNSAFE NOSE LIGHT. AIRCRAFT DID A GO-AROUND. CAPTAIN DECIDED TO FREE FALL THE NOSE GEAR AND GOT A GREEN LIGHT. AN EMERGENCY WAS DECLARED AND CABIN WAS PREPARED FOR AN EMERGENCY LANDI NG. FLIGHT HAD NO PROBLEMS DURING LANDING. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PIN NOT FULLY ENGAGED. REMOVED FOREIG N OBJECT FROM LOCK PIN. GEAR SWING CHECKED GOOD. (M) 2 L 7 2 4F RT 1998050800966 19980508 00966 NM 1998 5 8 USAASB98079 1 19980327 A 3350 15AT17 SWITCH BOEING 737 7372B7 1384560 NM FLIGHT COMPT DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 284AU 23131 LGA - UPON TESTING EMERGENCY LIGHTING SYSTEM, WITH SWITCH IN ARMED POSITION, ALL LIGHTS BEGAN TO ILLUMINATE INTERMITTENT LY OFF AND ON, ON THEIR OWN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT SWITCH IN THE FLIGHT DECK. OPERATION AL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998050800967 19980508 00967 EU 1998 5 8 USAAF98033 1 19980317 A 3350 LIGHTS FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 881US 11333 PIT - DURING OVERNIGHT MAINTENANCE VISIT, FOUND LOW LEVEL LIGHTING IN AFT CABIN INOPERATIVE. MAINTENANCE REPAIRED WIRIN G IN AFT LOW LEVEL LIGHTING CIRCUIT. (M) 2 L 7 2 4F RT 1998050800968 19980508 00968 EU 1998 5 8 USAAF98030 1 19980322 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 850US 11276 IND - MAINTENANCE FOUND TWO INOPERATIVE CEILING EMERGENCY LIGHTS IN MID CABIN. MAINTENANCE REPLACED THE BATTERY PACK. ( M) 2 L 7 2 4F RT 1998050800969 19980508 00969 1998 5 8 USAAD98056 4 19980309 A 2565 13621224 SLIDE DOUG DC9 DC931 3022065 WP AFT FUSELAGE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919VJ 48139 PIT - AFT ESCAPE SLIDE FAILED TO DEPLOY DURING OPERATIONAL TEST. MAINTENANCE REPLACED THE SLDIE ASSEMBLY. TWO ADDITION AL OPERATIONAL TESTS WERE SCHEDULED. (M) 2 L 7 2 4F A6WE 1998050800970 19980508 00970 WP 1998 5 8 USAAD98050 1 19980323 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG DOOR MALFUNCTIONED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 982VJ 48158 IND - FLT 942 - AFTER TAKEOFF AND THE LANDING GEAR RETRACTED, THE FLIGHT CREW EXPERIENCED SEVERE VIBRATION FROM THE NOSE GEAR AREA. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT NOSE GEAR DOOR OPEN. THE NOSE GEAR DOOR MECHANISM WAS INSPECTED AND NO DISCREPANCIES WERE FOUND. THE NOSE GEAR DOOR WAS CLOSED AND TH E AIRCRAFT DISPATCHED. (M) 2 L 7 2 4F A6WE 1998050800971 19980508 00971 WP 1998 5 8 USAAD98047 1 19980320 A 5610 5912290505 WINDSHIELD DOUG DC9 DC931 3022065 WP LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 933VJ 47216 PIT - FLT 1237 - THE CAPTAINS OUTER WINDSHIELD PANE CRACKED DURING CRUISE ABOUT 20 MINUTES AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE CAPTAINS WINDSHIELD. (M) 2 L 7 2 4F A6WE 1998050800972 19980508 00972 1998 5 8 USAAD98043 4 19980317 A 2350 G5302 CONTROL PANEL DOUG DC9 DC931 3022065 WP COCKPIT FAILED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 970VJ 47050 IND - FLT 1120 - AFTER ROTATION WHILE CLIMBING OUT OF IND EN ROUTE TO PHL, CREW HAD TOTAL RADIO FAILURE. CREW WAS ABLE TO GET THE NR 3 RADIO TO PICK UP DELTA FLIGHT IN THE AREA AND ALTITUDE AND ROUTING INSTRUCTIONS WERE PASSED ALONG. FLIG HT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 NAV COMM CONTROL PANEL DUE TO DEAD SPOT IN COMM CONTROL ON/OFF VOLUME KNOB. REPLACED NR 1 AND NR 2 COMM TRANSCEIVERS. COCKPIT MICROPHONES ALSO REPLA CED. (M) 2 L 7 2 4F A6WE 1998050800973 19980508 00973 NM 1998 5 8 USAASB98082 1 19980328 A 3350 900835A POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 22888 CMH - MAINTENANCE FOUND ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE FOUND ALL EMERGENCY LIGHT BATTERIE S DEAD. CHARGED ALL BATTERIES FOR FIVE HOURS, THEN REMOVED AND REPLACED BATTERY PACKS FOR THE INTERIOR LIGHTS ABOVE THE MAIN ENTRANCE DOOR AND FORWARD SERVICE DOOR AND FOR THE EXTERIOR LIGHTS AT THE MAIN ENTRANCE DOOR, FORWARD SERVICE DOOR , LEFT OVERWING AND LEFT FUSELAGE FAIRING. ALSO, REPLACED BATTERY PACK FOR UPPER AISLE LIGHT AT SEAT ROW 2. OPERATIONA L CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998050800974 19980508 00974 SO 1998 5 8 MASA98072 1 19980406 A 3350 LIGHTS EMB 120 EMB120RT SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 289UE 120191 DURING PREFLIGHT INSPECTION, PILOT FOUND AFT SECTION OF EMERGENCY LIGHTS INOP. HOWEVER, BEFORE MAINTENANCE ARRIVED, LIG HTS WERE AGAIN WORKING. MAINTENANCE T/S, NO DISCREPANCIES WERE NOTED. AIRCRAFT WS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050800975 19980508 00975 NM 1998 5 8 MASA98071 1 19980405 A 3350 PR2 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 DURING ROUTINE MAINTENANCE, FOUND PORTABLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHECK G OOD. (M) 2 H 7 2 4T RT A13NM 1998050800976 19980508 00976 NM 1998 5 8 MASA98075 1 19980409 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 DURING ROUTINE MAINTENANCE INSPECTION, MAINTENANCE PERSONNEL FOUND THE CENTER OVERHEAD EMERGENCY EXIT SIGN DIM. THE BUR NED OUT BULBS WERE REPLACED, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998050800977 19980508 00977 NM 1998 5 8 MASA98076 1 19980409 A 3350 BATTERIES DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 FLT 7525 - DRO-DEN - IN DEN PILOT REPORTED, THE EMERGENCY LIGHT BATTERIES WEAK. MAINTENANCE REMOVED AND REPLACED THE BA TTERIES. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998050800978 19980508 00978 SO 1998 5 8 MASA98081 1 19980412 A 3350 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 289UE 120191 DURING PRE-FLIGHT INSPECTION, CREW FOUND AFT SECTION OF EMERGENCY FLOOR PATH LIGHTING WOULD ONLY STAY ILLUMINATED FOR 15 SECONDS. MAINTENANCE INSTRUCTED PILOT TO RUN THE APU AND POSITION EMERGENCY LIGHTING SWITCH TO THE ARM POSITION. IN 1 0 MINUTES, THE BATTERY PACK RECHARGED, SYSTEM OPERATED NORMALL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998050800979 19980508 00979 SO 1998 5 8 MASA98078 1 19980411 A 3397 WIRE EMB 120 EMB120RT SO CABIN CHAFED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 287UE 120183 DURING ROUTINE MAINTENANCE, AFT LEFT AND RIGHT LIGHTED EMERGENCY EXIT LIGHTS FAILED ILLUMINATE. TROUBLESHOT SYSTEM, FOU ND FUSE TO BE BAD AND CHAFFED WIRE THAT SHORTED TO GROUND. REPAIRED WIRE AND REPLACED FUSE. OPERATIONAL CHECK WAS SATI SFACTORY. (M) 2 L 7 2 4T RT A31SO 1998050800980 19980508 00980 CE 1998 5 8 MASA98077 1 19980331 A 7120 MS2000618 TRUSS BOLTS BEECH 1900 1900D 1154162 CE RT ENGINE LOOSE A A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 59YV UE59 FLT 5330 - JAX-PBI - IN FLIGHT, CREW NOTICED THE RIGHT COWLING WAS LOOSE. CREW REDUCED POWER TO THE RT ENGINE AND RETUR NED TO THE GATE WITHOUT INCIDENT. MAINTENANCE FOUND THE UPPER INBOARD TRUSS BOLT WAS LOOSE. REMOVED AND REPLACED THE E NGINE TRUSS AND BOLTS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998050800981 19980508 00981 CE 1998 5 8 MASA98074 1 19980408 A 3230 11438800013 HYD POWER PACK BEECH 1900 1900D 1154162 CE NLG CAVITATED A MASA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SW 07 86YV UE86 FLT 5069 - FMN-GUP - AFTER DEPARTURE GEAR WOULD NOT FULLY RETRACT. PILOT SELECTED GEAR DOWN AND THE NOSE GEAR WOULD NOT FULLY EXTEND. PILOT ATTEMPTED TO PUMP GEAR DOWN AND DID RECEIVE DOWN AND LOCKED INDICATION. CREW DECLARED AN EMERGENC Y AND PERFORMED A FLYBY TO VERIFY GEAR DOWN. THE GEAR WAS VERIFIED DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAIN TENANCE PERFORMED A PRESSURE BLEEDING OF THE SYSTEM AND SEVERAL RETRACTIONS AND EXTENSIONS. OPS CHECK GOOD. AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998050800982 19980508 00982 CE 1998 5 8 MASA98069 1 19980403 A 5210 1015141641 CABLE DRUM BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR OUT OF ADJUST A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 17YV UE17 FLT 5983 - PIT-MBS - CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. THE DOOR WAS INSPECTED AND THE AIRCRAFT W AS FERRIED TO DUJ. DUJ MAINTENANCE RIGGED THE DOOR CABLE DRUM, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998050800983 19980508 00983 CE 1998 5 8 MASA98079 1 19980411 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 29YV UE29 DURING ROUTINE MAINTENANCE, DISCOVERED A SKIN CRACK APPROXIMTELY 1.5 INCHES LONG AT FORWARD OUTBOARD LEFT SIDE OF NR 2 V HF ANTENNA. COMPLETED REPAIR BY STOP DRILLING CRACK AND INSTALLING A REINFORCEMENT DOUBLER TO SKIN CRACK IAW BEECHCRAFT STRUCTUAL REPAIR MANUAL CHAPTER 53-90-00 PP 10-11. REFERENCE RO NR B1900D-53-0005 JAX. (M) 2 L 7 2 4T RT A24CE 1998050800984 19980508 00984 CE 1998 5 8 MASA98080 1 19980411 A 5330 SKIN BEECH 1900 1900D 1154162 CE FUSELAGE CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 29YV UE29 DURING ROUTINE MAINTENANCE, DISCOVERED SKIN CRACK APPROXIMATELY 2 INCHES LONG ON LOWER RIGHT FUSELAGE IN SPAR AREA. REP AIR WAS COMPLETED BY STOP DRILLING CRACK AND INSTALLING REINFORCEMENT DOUBLER TO AFFECTED AREA IAW BEECH STRUCTURAL REPA IR MANUAL CHAPTER 53-00-06, PP 40-41. REFERENCE RO NR B1900D-53-0006 JAX. INSPECTED FOR HIDDEN DAMAGE, FOUND NO DISCRE PANCIES. (M) 2 L 7 2 4T RT A24CE 1998050800985 19980508 00985 EU 1998 5 8 SIMA980981 1 19980408 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 399AT 399 SAW - DURNG CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT OUTBOARD AND THE LEFT AFT INBOARD SEAT TRACKS WERE CORR ODED. MAINTENANCE REMOVED AND REPLACED BOTH SEAT TRACKS IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998050800986 19980508 00986 1998 5 8 JBXA980036 4 19980407 A 2230 AUTO THROTTLE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU LT/RT ENGINE MALFUNCTIONED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 108ML 11484 BOTH AUTO THROTTLES FAULTED ON T/O ROLL, ABORTED AT 20 KNTS. INDICATED BOTH AUTO THROTTLES RESET AND NO AUTOLAND MESSA GE APPEARED ON THE MFDU. PERFORMED TEST OF FCC1 AND FCC2 IAW 22-11-00. PERFORMED TEST OF AUTO THROTTLES 1 AND 2 IAW 22 -31-00, COULD NOT DUPLICATE ANY FAULT. 2 L 7 2 4F 4 F RT 1998050800987 19980508 00987 EU 1998 5 8 JBXA980037 1 19980408 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A JBXA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 05 304ML 373 RDU - FLT 27 - ABORTED TAKEOFF RIGHT FORWARD EMERGENCY EXIT OPEN LIGHT. INSPECTED AND FOUND RT FORWARD OVERWING EMERGEN CY EXIT ARM COVER OFF. REINSTALLED COVER IAW 52-21-11. (M) 2 L 7 2 4F RT A28NM 1998050800988 19980508 00988 NM 1998 5 8 GAIA9838 1 19980408 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM L-1 DOOR INOPERATIVE A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6827 20180 DURING MAINTENANCE AT OKC, FOUND EMERGENCY LIGHT ABOVE L-1 DOOR FAILED TO ILLUMINATE. REMOVED AND REPLACED EMERGENCY LI GHT ASSEMBLY. SYSTEM OPERATIONALLY CHECKS GOOD. (M) 2 L 7 3 4F A3WE 1998050800989 19980508 00989 WP 1998 5 8 GTIA9800047 1 19980410 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942ML 47478 COCKPIT EMERGENCY LIGHT (BOTH BULBS) WILL NOT TEST WHEN CABIN EMERGENCY LIGHT SWITCH PULLED IN ON POSITION. RESET BATTE RY PACKS OPERATIONAL GOOD AIW MM 33-50. (M) 2 L 7 2 4F A6WE 1998050800990 19980508 00990 WP 1998 5 8 GTIA9800046 1 19980412 A 3350 CONNECTORS DOUG DC9 DC941 302207N WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 FORWARD ENTRANCE WALKWAY EMERGENCY LIGHTS INOPERATIVE. PULLED LIGHT STRIP OUT AND TRIED AT THE AISLE. LIGHT STRIP WORK ED. FOLLOWED WIRES BACK AND FOUND TWO BAD CONNECTIONS, REPAIRED TWO CONNECTIONS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998050800991 19980508 00991 WP 1998 5 8 GTIA9800042 1 19980404 A 3350 60060431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942ML 1941 47478 FOUND EMERGENCY LIGHT OVER OBSERVERS SEAT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998050800992 19980508 00992 NM 1998 5 8 F3LA98014 1 19980409 A 5330 SKIN BOEING 737 737201 1384454 NM BS 895/901 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 DEN - FLT 43 - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD92-25-09), INSPECTION REPORTED BULGING OF S KIN (CORROSION) AT STATION 901, S23R AND S24R, AND STATION 895, STRINGER 25R. MAINTENANCE REPAIRED CORRODED AREAS PER S RM 53-30-1, PAGE 3 (FIG 1) AND PAGE 5. (M) 2 L 7 2 4F A16WE 1998050800993 19980508 00993 NM 1998 5 8 F3LA98013 1 19980409 A 5330 SKIN BOEING 737 737201 1384454 NM L1 DOORWAY CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 DEN - DURING CIRCUMFERENTIAL SPLICE INSPECTION, WORK CARD 7-0126 (AD 92-25-09, INSPECTION REPORTED .625 INCH CRACK SIX I NCHES FORWARD OF L-1 DOOR IN FUSELAGE SKIN AT STRINGER 7. MAINTENANCE REPAIRED CRACK PER SRM 53-30-3, PAGES 7 AND 8. ( M) 2 L 7 2 4F A16WE 1998050800994 19980508 00994 NM 1998 5 8 F3LA98012 1 19980401 A 5730 SKIN BOEING 737 737201 1384454 NM LT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 DEN - PRIOR TO DEPARTURE, MAINTENANCE REPORTED ONE .25 INCH CRACK IN LEFT WING LEADING EGE SKIN AT WBL 165.0. MAINTENAN CE REPAIRED DAMAGED AREA PER SRM 57-30-4, PAGE 4. (M) 2 L 7 2 4F A16WE 1998050800995 19980508 00995 NM 1998 5 8 F3LA98011 1 19980403 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 DURING C-CHECK, MAINTENANCE REPORTED CORROSION ON UPPER CHORD BS 328 FLOORBEAM, LBL 30-4, WL 208. MAINTENANCE REMOVED D AMAGED SECTION OF BS 328 BEAM UPPER CHORD FROM LBL 28 TO LBL 65. FABRICATED REPAIR PARTS AND INSTALLED WET WITH FASTENE RS PER SRM 53-10-9, FIG 5 AND SRM 53-10-1. (M) 2 L 7 2 4F A16WE 1998050800996 19980508 00996 NM 1998 5 8 F3LA98015 1 19980407 A 5754 SKIN BOEING 737 737201 1384454 NM NR 4 LE FLAP DELAMINATED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, MAINTENANCE REPORTED DISBONDING ON NR 4 SLAT TRAILING EDGE WEDGE OUTBOARD UPPER END. MAINTENANCE REMOVED 52.0 INCHE OF DELAMINATED SKIN FROM OUTBOARD LOWER SURFACE, 13 INCHES OF DELAMINATED SKIN FROM OUTBOARD UPPER SU RFACE AND 15 INCHES OF DAMAGED HONEYCOMB CORE, FABRICATED REPAIR PARTS AND APPLIED BONDING PRIMER PER SRM 51-40-6, PAGES 8 TO 8H. (M) 2 L 7 2 4F A16WE 1998050800997 19980508 00997 NM 1998 5 8 EISA98039 1 19980208 A 3350 1000679 BATTERIES BOEING 727 727223 1384074 NM CABIN DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6815 19490 EMERGENCY LIGHT BATTERY DEAD. INSTALLED NEW BATTERIES. (M) 2 L 7 3 4F A3WE 1998050800998 19980508 00998 NM 1998 5 8 EISA98038 1 19980209 A 5754 GUIDE BOEING 727 727223 1384074 NM WS 620 CHIPPED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND NR 2 SLAT GUIDE CHIPPED AT WS 620 LT TOP OF FLAT TRAILING EDGE. INSTALLED SLAT TRAILING EDGE DOUB LER PER SRM 57-50-03. (M) 2 L 7 3 4F A3WE 1998050800999 19980508 00999 NM 1998 5 8 EISA98037 1 19980209 A 5400 S-DUCT BOEING 727 727223 1384074 NM NR 2 ENGINE TORN A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND NR 2 ENGINE INTAKE 12 O'CLOCK POSITION HAS A TEAR IN SKIN AT OPENING NEXT TO ENGINE RING FLANGE. R EMOVED DAMAGED AREA, FABRICATED REPAIR FILLER AND DOUBLER PER SRM 54-10-03. INSTALLED REPAIR PER SRM 54-10-03. (M) 2 L 7 3 4F A3WE 1998050801000 19980508 01000 NM 1998 5 8 EISA98036 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM LT TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND TORN AND DELAMINATED LEFT INBOARD AFT FLAP TRAILING EDGE. REPAIR DELAMINATION ON LEFT INBOARD AFT FLAP BY INJECTION METHOD PR SRM 51-40-06. (M) 2 L 7 3 4F A3WE 1998050801001 19980508 01001 NM 1998 5 8 EISA98035 1 19980209 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 850 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND 50 INCH CRACK IN SUPPORT ANGLE FOR LEFT MAIN GEAR DOOR UPSTOP, FS 850. STOP DRILLED CRACK, FABRIC ATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1998050801002 19980508 01002 NM 1998 5 8 EISA98034 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM RT TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND RT INBOARD AFT FLAP DELAMINATED TRAILING EDGE. REPAIR DELAMINATION BY INJECTION METHOD PER SRM 51 -40-06. (M) 2 L 7 3 4F A3WE 1998050801003 19980508 01003 NM 1998 5 8 EISA98033 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM LT TE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND LEFT INBOARD AFT FLAP BOTTOM SKIN WITH CRACKS AND DENTS IN AREA 18 INCHES BY 24 INCHES. ACCOMPLIS HED POTTING REPAIR PER SRM 51-40-06 AND INSTALLED FIBERGLASS OVERLAY PER SRM 51-40-08. (M) 2 L 7 3 4F A3WE 1998050801004 19980508 01004 NM 1998 5 8 EISA98032 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM RT TE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURIGN C-CHECK, FOUND RT INBOARD AFT FLAP BOTTOM SKIN WITH CRACKS AND DENTS IN AREA 18 INCHES BY 24 INCHES. ACCOMPLISHE D POTTING REPAIR PER SRM 51-40-06 AND INSTALLED FIBERGLASS OVERLAY PER SRM 51-40-08. (M) 2 L 7 3 4F A3WE 1998050801005 19980508 01005 NM 1998 5 8 EISA98031 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM RT TE FLAP HOLE A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND CRACK AND HOLE, RT INBOARD AFT FLAP. REPAIRED HOLE WITH POTTING REPAIR PER SRM 51-40-06 FIBERGLAS S OVERLAY APPLIED PER SRM 51-40-08. (M) 2 L 7 3 4F A3WE 1998050801006 19980508 01006 NM 1998 5 8 EISA98030 1 19980209 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 750-950 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND CORROSION ON SEAT TRACK, LEFT SIDE FROM FS 750 TO 950E ON MAIN CARGO DECK. REMOVED TRACK AND INST ALLED NEW SEAT TRACK IAW SRM 53-10-05. (M) 2 L 7 3 4F A3WE 1998050801007 19980508 01007 NM 1998 5 8 EISA98029 1 19980209 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 178 CORROSION A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND FS 178 BULKHEAD, FIRST ANGLE FROM BOTTOM HAS CORROSION. REMOVED ANGLE, FABRICATED ANGLE FROM 7075 -T6 AND INSTALLED PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998050801008 19980508 01008 NM 1998 5 8 EISA98028 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM LT TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND LEFT INBOARD AFT FLAP DELAMINATED AT TRAILING EDGE. REPAIRED DELAMINATION BY INJECTION METHOD PER SRM 51-40-06. (M) 2 L 7 3 4F A3WE 1998050801009 19980508 01009 NM 1998 5 8 EISA98027 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM LT TE FLAP DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND LEFT INBOARD AFT FLAP HAS HOLE AND DENT ON BOTTOM SKIN. REPAIRED HOLE AND DENT IN BOTTOM SKIN WIT H POTTING REPAIR PER SRM 51-40-06 AND MADE FIBERGLASS OVERLAY PER SRM 51-40-08. (M) 2 L 7 3 4F A3WE 1998050801010 19980508 01010 NM 1998 5 8 EISA98026 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM LT TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND TRAILING EDGE DELAMINATION ON LEFT INBOARD AFT FLAP. REPAIRED DELAMINATION WITH FIBERGLASS OVERLA Y PER SRM 51-40-08. (M) 2 L 7 3 4F A3WE 1998050801011 19980508 01011 NM 1998 5 8 EISA98025 1 19980209 A 5753 SKIN BOEING 727 727223 1384074 NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND INBOARD FLAP, AFT FLAP TRAILING EDGE DELAMINATED. REPAIRED DELAMINATION ON TRAILING EDGE WITH FIB ERGLASS OVERLAY PER SRM 51-40-08. (M) 2 L 7 3 4F A3WE 1998050801012 19980508 01012 NM 1998 5 8 EISA98024 1 19980209 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 560-580 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND CORROSION ON FLOORBEAM AND SEAT TRACK AT FS 560-580. SURFACE CORROSION REMOVED ON FLOORBEAM. FOU ND IN LIMITS PER SRM 53-10-1. INSTALLED NEW SECTION OF SEAT TRACK. (M) 2 L 7 3 4F A3WE 1998050801013 19980508 01013 NM 1998 5 8 EISA98023 1 19980209 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 580-620 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND FS 580 RT AND 620 CORROSION ON CENTER BEAM AND SIDE OF SEAT TRACK. REMOVED SURFACE CORROSION ON F LOORBEAM AND FOUND TO BE IN LIMITS. REMOVED AND REPLACED SEAT TRACK PER 53-10-1 DUE TO CORROSION OUT OF LIMITS. (M) 2 L 7 3 4F A3WE 1998050801014 19980508 01014 NM 1998 5 8 EISA98022 1 19980209 A 5320 DOUBLER BOEING 727 727223 1384074 NM BS 253L CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND CORROSION ON COCKPIT SHEER DOUBLER JUST BELOW PILOTS WINDOW FS 253 LT. REMOVED CORROSION, FABRICA TED DOUBLER AND INSTALLED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998050801015 19980508 01015 NM 1998 5 8 EISA98021 1 19980209 A 2820 VENT BOX BOEING 727 727223 1384074 NM WS 171.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND WING STATION 171.5 RT WING, FUEL VENT BOX HAS CRACKED FLANGE AT UPPER CHORD. FABRICATED REPAIR PA RTS PER SRM 57-10-4 AND INSTALLED REPAIR PER SRM 51-10-4 FIG 8. (M) 2 L 7 3 4F A3WE 1998050801016 19980508 01016 NM 1998 5 8 EISA98020 1 19980209 A 2810 FUEL TANK BOEING 727 727223 1384074 NM RT WING LEAK A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FUOND FUEL LEAK NR 3 SLAT ACTUATOR CAN ON RT WING. REMOVED OLD SEALER AND RESEALED AT LEAK SOURCE PER 7 27 MM 28-11-0, PAGE 801. (M) 2 L 7 3 4F A3WE 1998050801017 19980508 01017 NM 1998 5 8 EISA98019 1 19980209 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 629 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND LEFT WING STATION 629, CRACK ON UPPER STRINGER ATTACHMENT TO RIB, 7TH FROM FWD SPAR. DRILLED REPA IR ANGLES AND RADIUS BLOCKS AND INSTALLED REPAIR PER BOEING SB 727-57A-159. (M) 2 L 7 3 4F A3WE 1998050801018 19980508 01018 NM 1998 5 8 EISA98018 1 19980209 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 519 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND LEFT WING STATION 519, 10TH STRINGER AFT OF FRONT SPAR HAS CRACK AT STRINGER TO RIB ATTACHMENT (UP PER STRINGER). DRILLED REPAIR ANGLES AND RADIUS BLOCKS AND INSTALLED PER BOEING SB 727-57A-159. (M) 2 L 7 3 4F A3WE 1998050801019 19980508 01019 NM 1998 5 8 EISA98017 1 19980209 A 5522 SKIN BOEING 727 727223 1384074 NM RT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND RIGHT ELEVATOR HAS CRACK AND HOLE IN BOTTOM SKIN, OUTBOARD END. FABRICATED DOUBLER PER SRM 55-20- 03. (M) 2 L 7 3 4F A3WE 1998050801020 19980508 01020 NM 1998 5 8 EISA98016 1 19980209 A 5520 ANGLE BOEING 727 727223 1384074 NM RT ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND X-RAY INSPECTION OF RT ELEVATOR SHOWS A CRACK INDICATION AS SHOWN IN SHOTS R7, R1 AND R4. REMOVED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1998050801021 19980508 01021 NM 1998 5 8 EISA98015 1 19980209 A 5320 GUSSET BOEING 727 727223 1384074 NM BS 356 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND FS 356, STRINGER 17L, GUSSET AND STRINGER CRACKED AT WIRE BUNDLE. FABRICATED PART PER SAMPLE AND INSTALLED PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998050801022 19980508 01022 NM 1998 5 8 EISA98014 1 19980209 A 5311 FRAME BOEING 727 727223 1384074 NM BS 360 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 6826 19704 DURING C-CHECK, FOUND FS 360, STRINGER 17L FRAME CRACKED AND BROKEN. FABRICATED DOUBLER AND INSTALLED PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998050801023 19980508 01023 NM 1998 5 8 EISA98074 1 19980411 A 3350 1000879 LIGHT BOEING 727 727223 1384074 NM COCKPIT LOOSE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312NE 5530 20193 ON SERVICE CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE IN THE ARMED POSITION. GENERATED FROM MAINTENANCE REPO RT. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. (M) 2 L 7 3 4F A3WE 1998050801024 19980508 01024 NM 1998 5 8 EISA98073 1 19980404 A 3350 STRIP BOEING 727 7272M7 138407S NM CABIN LOOSE A EISA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 721RW 21200 ESCAPE PATH LIGHTING STRIP LOOSE BEHIND SEAT 22D, STRIP IS CAUSING PASSENGERS TO TRIP. GENERATED BY PILOT REPORT. SECU RED AS REQUIRED, GOOD FOR SERVICE MM 33-00. (M) 2 L 7 3 4F A3WE 1998050801025 19980508 01025 NM 1998 5 8 EISA98072 1 19980404 A 3350 BULB BOEING 727 7272M7 138407S NM L1 DOOR FAILED A EISA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 721RW 21200 L-1 DOOR EMERGENCY EXIT LIGHT BULB INOPERATIVE. GENERATED BY PILOT REPORT. RELAMPED AS REQUIRED IAW MM 33-00. (M) 2 L 7 3 4F A3WE 1998050801026 19980508 01026 NM 1998 5 8 EISA98071 1 19980407 A 5230 SEAL BOEING 727 727223 1384074 NM CARGO DOOR TORN A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 312NE 20193 AFTER DEPARTURE FROM LAX, HAD NO CONTROL OF PRESSURIZATION. PEGGED AT 2000 FPM CLIMB. CLOSED CARGO OUT FLOW VALVE, STI LL 1300-1400 FPM CLIMB, NO CONTROL MANUALLY EITHER. ATB TO LAX FOR TROUBLESHOOTING. REPAIRED TEARS IN FWD BOTTOM CARGO DOOR SEAL, AFT BOTTOM CARGO DOOR SEAL, UPPER MAIN CARGO DOOR SEAL, PRESSURIZED AIRCRAFT WITH APU CHECKED FOR LEAKS, AND OUTFLOW VALVE OPERATION. CHECKS GOOD, NO LEAKS NOTED. (M) 2 L 7 3 4F A3WE 1998050801027 19980508 01027 1998 5 8 EISA98066 4 19980323 A 2312 064100514 VHF COM BOEING 727 727277 138408S NM E/E BAY INTERMITTENT A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 275WC 6935 20549 AFTER TAKEOFF FROM BRU, NR 1 COM WORKED INTERMITTENTLY. AIR TURN BACK TO BRU. PERFORMED NR 1 VHF ANTENNA BONDING CHECK PER MM 23. NO DEFECTS FOUND. ANTENNA COAX AND ANTENNA RESISTANCE NORMAL. REMOVED AND REPLACED NR 1 VHF. (M) 2 L 7 3 4F RT A3WE 1998050801028 19980508 01028 NM 1998 5 8 EISA98065 1 19980322 A 3232 731411 ACTUATOR BOEING 727 72731 1384010 NM RT MLG DOOR MALFUNCTIONED A EISA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 240NE 18906 DURING TAKEOFF FROM IND, RIGHT MAIN GEAR SLOW TO RETRACT. CYCLED THREE TIMES PER MAINTENANCE REQUEST. NO HELP. RETURN ED TO IND PER MAINTENANCE REQUEST. FOUND RIGHT MAIN GEAR WHEEL WELL DOOR ACTUATOR BYPASSING. REMOVED AND REPLACED RIGH T MAIN GEAR WHEEL WELL DOOR ACTUATOR IAW MM 32-32-81, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998050801029 19980508 01029 NM 1998 5 8 EISA98064 1 19980322 A 3350 1000679 LIGHT BOEING 727 727231 1384079 NM CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 74318 3701 20051 DURING SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED CABIN EMERGENCY EXIT LIGHT IAW 33-00 . OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998050801030 19980508 01030 NM 1998 5 8 EISA98063 1 19980322 A 2150 6075102 CONTROL BOEING 727 727221 1384071 NM RT PACK MALFUNCTIONED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366PA 31C4961 22538 DURING ASCENT OUT OF DFW, NOTICED LOUD RUMBLE FROM RIGHT PACK, PACK WAS SHUT DOWN. AIRCRAFT WOULD NOT MAINTAIN CABIN PR ESSURE WITH LEFT PACK. REMOVED AND REPLACED RIGHT 35 DEGREE CONTROL IAW 21-60-00, REPAIRED AND SECURED CONNECTOR TO LEF T PACK AIR CYCLE MACHINE IAW 21-50-00. (M) 2 L 7 3 4F A3WE 1998050801031 19980508 01031 NM 1998 5 8 EISA98062 1 19980321 A 5210 DOOR BOEING 727 727223 1384074 NM CABIN UNLOCKED A EISA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SW 07 312NE 20193 DEPARTING SJU, AFT ENTRY DOOR LIGHT CAME ON AFTER TAKEOFF COULD NOT PRESSURIZE SMOOTH LANDING 155 LBS. AIRCRAFT RETURNE D TO SJU. FOUND AFT ENTRY CARGO DOOR UNLOCKED REMOVED CONTAINERS ANDCLOSED. WORKS OK. PERFORMED OVERWEIGHT LANDING IN SPECTION PER MM CHAPTER 5. (M) 2 L 7 3 4F A3WE 1998050801032 19980508 01032 NM 1998 5 8 EISA98059 1 19980321 A 3350 1000679 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721RW 21200 DURING SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOPERATIVE OVER MAIN ENTRY DOOR. REMOVED AND REPLACED EMERGENCY EXIT LIGHT OVER MAIN ENTRY DOOR MM 33-00. (M) 2 L 7 3 4F A3WE 1998050801033 19980508 01033 NM 1998 5 8 EISA98058 1 19980311 A 2780 CONNECTOR BOEING 727 727223 1384074 NM NR 2 SLAT LOOSE A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 AFTER TAKEOFF OUT OF MIA, NR 2 SLAT LEADING EDGE DEVICE WOULD NTO RETRACT. FOLLOWED EMERGENCY PROCEDURES PER AOM. PILO T DID AIR TURN BACK TO MAI. FOUND CANNON PLUG OFF OF NR 2 SLAT ACTUATOR, CLEANED AND RECONNECTED CANNON PLUG. OPS CHEC K OK PER MM 27-81-0. (M) 2 L 7 3 4F A3WE 1998050801034 19980508 01034 WP 1998 5 8 ORJA9867 1 19980331 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 873RA 53093 EMERGENCY LIGHT INOP AT ROW 7 DEF AND 8 DEF. REPAIRED WIRING. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998050801035 19980508 01035 WP 1998 5 8 ORJA9866 1 19980331 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 EMERGENCY LIGHT INOP AT ROW 9 DEF AND 19 DEF. REPAIRED WIRING. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998050801036 19980508 01036 WP 1998 5 8 ORJA9868 1 19980402 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 821RA 49931 EMERGENCY EXIT LIGHTS IN O/H FROM COCKPIT TO ROW 1 INOP. REPLACED BATTERY PACK IN O/H AT FORWARD LAV. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998050801037 19980508 01037 NM 1998 5 8 ORJA9862 1 19980324 A 3241 CONNECTOR DOUG MD90 MD9030 3023690 NM ANTI-SKID SYSTEM LOOSE A ORJA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 11 902RA 53490 RETURNED TO GATE, ANTI-SKID FAULT DURING TAXI OUT. FOUND 70 PERCENT BRAKE PEDAL SWITCHES AT FAULT CLEANED AND RESEATED CANNON PLUGS ANTI-SKID SYSTEM TEST PASS IAW MM CHAP 32-00. (M) 2 L 7 2 4F RT A6WE 1998050801038 19980508 01038 WP 1998 5 8 ORJA9863 1 19980327 A 2913 AS66411LS666 HYD PUMP DOUG DC9 DC983 3022083 WP NR 1 ENGINE FAILED A ORJA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 11 873RA 53093 RETURNED TO GATE, LEFT ENGINE HYDRAULIC PUMP INOP. REMOVED NR 1 EDP HYD INSTALLED SERVICEABLE EDP HYD IN NR 1 ENG PER M M REF 29-10-05 RAN ENGINE PERFORMED LEAK CHECK, CHECKS OK GOOD PUMP PRESS COWL AND ASSOCIATED PANELS CLOSED. (M) 2 L 7 2 4F RT A6WE 1998050801039 19980508 01039 WP 1998 5 8 ORJA9860 1 19980320 A 2760 WARNING DOUG DC9 DC983 3022083 WP SPOILER SYSTEM ACTIVATED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 11 834RA 53124 ABORTED TAKEOFF DUE TO SPOILER DEPLOYED ANNUNCIATION ON OAP. ASSIGNED TO DMI NR 13132 REF TO LOP PAGE 156711. SPOILER SYSTEM OPS CHECK NORMAL IAW MM 27-60-00. NO DISCREPANCIES NOTED CLEARS DMI NR 13132. (M) 2 L 7 2 4F RT A6WE 1998050801040 19980508 01040 WP 1998 5 8 ORJA9861 1 19980325 A 5610 5887275501 WINDSHIELD DOUG DC9 DC982 3022082 WP CTR COCKPIT FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 822RA 49932 AIR RETURN TO LAS, CLIMBING THROUGH 12,000 MSL CENTER WINDSHIELD POPPED AND STARTED LEAKING AT SEAMS. REMOVED AND REPLA CED WINDSHIELD IAW MM 56-10-01 PRESSURED A/C TO 7 PSI AND NO LEAKS NOTED, ANTI-ICE AND ANIT-FOG OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998050801041 19980508 01041 WP 1998 5 8 ORJA9859 1 19980323 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTING SYSTEM INOP. REPLACED FUSE, BATTERIES, AND BATTERY PACK IN CABIN ROWS 4-7, 17-25 LEFT AND RT AFT EME RGENCY O/W EXIT IDENTIFIER. (M) 2 L 7 2 4F RT A6WE 1998050801042 19980508 01042 NM 1998 5 8 ORJA9856 1 19980321 A 3350 CONNECTOR DOUG MD90 MD9030 3023690 NM CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 902RA 53490 MID SECTION EMERGENCY LIGHT O/H OUT. FOUND CONNECTOR LOOSE AT BATTERY PACK SECURED AS REQUIRED, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998050801043 19980508 01043 WP 1998 5 8 ORJA9855 1 19980321 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 RETURNED TO GATE DURING PUSH BACK EMERGENCY LIGHTING AT ROWS 16, 17, 18, 19 CAME ON COULD NOT BE EXTINGUISHED ALSO EMERG ENCY EXIT LIGHT AT ROW 20 A/C LEFT CAME ON AND COULD NOT BE EXTINGUISHED. REPLACED LEFT FORWARD EMERGENCY EXIT SIGN BAT TERY PACK ASSY AND REPAIRED SHORTED WIRING AT SEAT O/B LEGS AT ROW 17-19 RIGHT SIDE, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998050801044 19980508 01044 WP 1998 5 8 ORJA9847 1 19980312 A 3350 59306431 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DIRTY A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 EMERGENCY LIGHTS ROW 12-17 ON A/C RIGHT SIDE ON IN FLT. REMOVED EMERGENCY BATTERIES FROM PACK CLEARED CONTACTS RESEATED CYCLED EMERGENCY POWER SWITCH SYSTEM F/C OK. (M) 2 L 7 2 4F RT A6WE 1998050801045 19980508 01045 WP 1998 5 8 ORJA9846 1 19980313 A 3350 CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 EMERGENCY SEAT LIGHTS FROM ROW 12 TO 16 INOP. REMOVED AND REPLACED CHARGER AT ROW 20 NR 1 SIDE, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998050801046 19980508 01046 WP 1998 5 8 ORJA9845 1 19980313 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 EMERGENCY EXIT LIGHT NR 1 SIDE FORWARD INOP. REMOVED AND REPLACED AT ROW 20 NR 1 SIDE, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998050801047 19980508 01047 WP 1998 5 8 ORJA9858 1 19980321 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 PRE-FLIGHT RNO, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED LEFT FORWARD OVERWING BATTERY PACK ASSY, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998050801048 19980508 01048 WP 1998 5 8 ASAA9880068 1 19980404 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 PDX - DURING MAINTENANCE CHECK, THE L1 DOOR BAYONET DID NOT LOCK THE HINGE FROM ROTATING. ADJUSTED THE L1 DOOR ROTATION ROD AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998050801049 19980508 01049 NM 1998 5 8 ASAA9840057 1 19980331 A 2150 6938766 RAM AIR DOOR BOEING 737 7374Q8 NM PIN MIGRATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 SEA - DURING C-CHECK, THE LEFT RAM AIR DOOR HINGE PIN WAS FOUND TO HAVE MIGRATED CAUSING DAMAGE TO THE WING TO BODY FAIR ING. REPAIRED PER EA 2150-01007 AND BOEING SERVICE LETTER 737-SL-21-037. (M) 2 L 7 2 4F RT A16WE 1998050801050 19980508 01050 NM 1998 5 8 ASAA9840058 1 19980331 A 5753 65C2632030 DOUBLER BOEING 737 7374Q8 NM RT TE MIDFLAP WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 762AS 25099 SEAT - DURING C-CHECK, THE RT WING OUTBOARD MID FLAP WAS FOUND TO BE WORN ON THE INBOARD LEADING EDGE. REPAIRED PER EA 5750-01166 AND BOEING TELEX ASA-SEA-94-0483TR. (M) 2 L 7 2 4F RT A16WE 1998050801051 19980508 01051 NM 1998 5 8 ASAA9840059 1 19980331 A 5751 65C2591128A SKIN BOEING 737 7374Q8 NM RT AILERON DELAMINATED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 1341 25099 SEA - DURING C-CHECK, THE RT AILERON LOWER SKIN WAS FOUND TO BE DELAMINATED. REPAIRED PER EA 5760-01010 AND BOEING TELE X ASA-SEA-98-0063RR. (M) 2 L 7 2 4F RT A16WE 1998050801052 19980508 01052 WP 1998 5 8 ASAA9880067 1 19980404 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 934AS 49235 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998050801053 19980508 01053 WP 1998 5 8 ASAA9880059 1 19980325 A 3350 LAMP DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 949AS 53022 SEA - AFTER ARRIVAL OF FLIGHT 349, CREW REPORTED THE EMERGENCY FLOOR TRACK IN THE FORWARD CABIN WERE INOPERATIVE. REPLA CED DEFECTIVE LAMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998050801054 19980508 01054 WP 1998 5 8 ASAA9880058 1 19980325 A 3350 276005 FUSE DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE FUSE IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998050801058 19980508 01058 NM 1998 5 8 ASAA9810023 1 19980324 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 10 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998050801059 19980508 01059 NM 1998 5 8 ASAA9810022 1 19980321 A 3350 8731002142 LIGHT BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED SMOKE BARR IER EMERGENCY EXIT LIGHT ASSEMBLY AND BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998050801060 19980508 01060 WP 1998 5 8 ASAA9880066 1 19980402 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 950AS 53023 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 30 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLYS AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998050801061 19980508 01061 WP 1998 5 8 ASAA9880065 1 19980401 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998050801062 19980508 01062 WP 1998 5 8 ASAA9880064 1 19980401 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 935AS 49236 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998050801063 19980508 01063 WP 1998 5 8 ASAA9880062 1 19980326 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 969AS 53063 ONT - PRIOR TO DEPARTURE OF FLT 531, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998050801064 19980508 01064 WP 1998 5 8 ASAA988061 1 19980325 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 940AS 49825 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT IN THE FORWARD ENTRY WAS FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998050801065 19980508 01065 WP 1998 5 8 ASAA9880060 1 19980325 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 940AS 49825 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998050801066 19980508 01066 NM 1998 5 8 ASAA9840060 1 19980401 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 PDX - DURING MAINTENANCE CHECK, THE AFT 3 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED W IRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998050801067 19980508 01067 NM 1998 5 8 ASAA9810026 1 19980401 A 3350 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. ( M) 2 L 7 2 4F A16WE 1998050801068 19980508 01068 NM 1998 5 8 ASAA9810025 1 19980331 A 3350 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER AND ROW 14 EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLAC ED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998050801069 19980508 01069 NM 1998 5 8 ASAA9810024 1 19980331 A 3350 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 746AS 23123 ANC - PRIOR TO FLIGHT, THE R2 EMERGENCY EXIT TRACK LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHT OPERAT ED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998050801070 19980508 01070 1998 5 8 HEEA0014031 4 19980422 A 3120 212075514001 CLOCK BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 CLOCK LOSES TIMES. 1 G 7 2 4U H4SW 1998050801071 19980508 01071 1998 5 8 HEEA0014032 4 19980422 A 3420 4021541671 INDICATOR BOLKMS 117 BK117B2 5626013 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 134AE 7237 ARTIFICIAL HORIZ INDICATOR INTERNAL LIGHTS SHORTED. 1 G 7 2 3U NC H13EU 1998050801072 19980508 01072 SW 1998 5 8 HEEA0014033 1 19980422 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6161A 51611 ACTUATOR INOPERATIVE. 1 G 7 1 3U H2SW 1998050801073 19980508 01073 SW 1998 5 8 HEEA0014034 1 19980427 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 762 28101 DURING 250 HOUR INSPECTION FOUND CLUTCH FAILED TORQUE SLIPPAGE TEST WAS AT 250 IN. LBS. AND END PLAY WAS AT .014 LIMITS ARE .004-.010. 2 G 7 2 4U H10SW 1998050801074 19980508 01074 SW 1998 5 8 HEEA0014035 1 19980427 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 75 28140 KICKS OUT DURING START AND HIGH VOLTAGE DRAW. 2 G 7 2 4U H10SW 1998050801075 19980508 01075 SW 1998 5 8 HEEA0014036 1 19980428 A 5532 206020113229 FIN ASSEMBLY BELL 407 407 SW VERT FIN DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 INSPECTED VERTICAL FIN AS PER ASB407-98-17 FOR CUTS AND SCRATCHES. THE ALLOWABLE DEPTH WAS .020. THE TWO CUTS FOUND WE RE .017 AND .024 DEEP. SCRAPPED PART. 1 G 7 1 3U O H2SW 1998050801076 19980508 01076 SW 1998 5 8 HEEA0014037 1 19980428 A 2435 2CM272B1 STARTER BELL 214 214ST 1182106 SW ENGINE MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 DRAWS HIGH VOLTAGE DURING START UP. 2 G 7 2 4U H10SW 1998050801077 19980508 01077 SW 1998 5 8 HEEA0014038 1 19980429 A 2432 RG380E44 BATTERY BELL 222 222U 1182140 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6992 16 47521 BATTERY WAS FOUND AT 6 VOLTS ON 3-11-98. BATTERY WAS CHARGED TO 22.5 VOLTS. WHILE DISCONNECTED FROM AIRCRAFT, VOLTAGE DROPPED FROM 22.5 VOLTS TO 18 VOLTS IN ONE HOUR. VOLTAGE WAS MEASURED AT 15.4 VOLTS AFTER 5 HOURS. AIRCRAFT BATTERY WA S INSTALLED NEW AT 4469:05 AIRCRAFT HOURS ON 1-30-98. REPLACED WITH SERVICEABLE AIRCRAFT BATTERY. 1 G 7 2 3U H9SW 1998050801078 19980508 01078 EU 1998 5 8 HEEA0014040 1 19980429 A 6710 1054537110 BEARING 10545371 BOLKMS 105 BO105S 5626006 EU MIXING LEVER UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5031U S678 TEFLON UNBONDING FROM BEARING. REPLACED WITH NEW BEARING. 1 G 7 2 3U H3EU 1998050801079 19980508 01079 EU 1998 5 8 HEEA0014041 1 19980429 A 6710 1054537110 BEARING 10545371 BOLKMS 105 BO105S 5626006 EU MIXING LEVER UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 133AE S800 TEFLON UNBONDING FROM BEARING. REPLACED WITH NEW BEARING. 1 G 7 2 3U H3EU 1998050801080 19980508 01080 EU 1998 5 8 HEEA0014042 1 19980429 A 6710 1054537110 BEARING 10545371 BOLKMS 105 BO105S 5626006 EU MIXING LEVER UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 135AE S838 TEFLON UNBONDING FROM BEARING. REPLACED WITH NEW BEARING. 1 G 7 2 3U H3EU 1998050801081 19980508 01081 EU 1998 5 8 HEEA0014043 1 19980429 A 6710 1054537110 BEARING 10545371 BOLKMS 105 BO105S 5626006 EU MIXING LEVER UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81992 S827 TEFLON LINER UNBONDED AND BEARING VERY STIFF. UNABLE TO MOVE INNER RACE. REPLACED WITH NEW BEARING. 1 G 7 2 3U H3EU 1998050801082 19980508 01082 EU 1998 5 8 HEEA0014044 1 19980429 A 6710 1054537110 BEARING 10545371 BOLKMS 105 BO105S 5626006 EU MIXING LEVER UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 S677 TEFLON LINER UNBONDED AND BEARING VERY STIFF. UNABLE TO MOVE INNER RACE. REPLACED WITH NEW BEARING. 1 G 7 2 3U H3EU 1998050801083 19980508 01083 EU 1998 5 8 HEEA0014045 1 19980429 A 6710 1054537110 BEARING 10545371 BOLKMS 117 BK117A4 5626017 EU MIXING LEVER UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911RZ 7092 TEFLON LINER UNBONDED AND BEARING VERY STIFF. UNABLE TO MOVE INNER RACE. REPLACED WITH NEW BEARING. 1 G 7 2 3U H13EU 1998050801085 19980508 01085 GL 1998 5 8 HEEA0014047 2 19980429 A 7261 23063144 FILTER ELEMENT BELL 407 407 SW ALLSN 250C 250C47B GL ENG OIL CLOGGED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 407MM 53060 ON DAILY INSPECTION FOUND OIL FILTER BYPASS BUTTON POPPED. REPLACED WITH SERVICEABLE FILTER. 1 G 7 1 3U 3 U O H2SW E1GL 1998050801087 19980508 01087 SW 1998 5 8 HEEA0014049 1 19980429 A 6720 206001763001 BELLCRANK ASSY BELL 206 206L1 1182107 SW ANTI TORQUE CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 45598 BELLCRANK CHAFFED AT ROD END ATTACH AREA. REPLACED BELLCRANK WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1998050801088 19980508 01088 SW 1998 5 8 HEEA0014050 1 19980429 A 7170 70031A202000 HOSE ASSY BELL 206 206L1 1182107 SW EXH DRAIN CLOGGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 45598 CLOGGED EXH COLLECTOR DRAIN HOSE. REPLACED WITH NEW HOSE. 1 G 7 1 3U H2SW 1998050801089 19980508 01089 GL 1998 5 8 HEEA0014051 2 19980429 A 7322 25490925 FUEL CONTROL SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL ENGINE MALFUNCTIONED E HEEA K NONE R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 03 706AE 760275 FUEL CONTROL MALFUNCTION. WILL NOT TOP. DROOPS AT 90 PERCENT TORQUE. UNIT HAS EXPERIENCED STARTING PROBLEMS 1 G 7 2 3U 3 U H1NE E1GL 1998050801090 19980508 01090 SW 1998 5 8 HEEA0014052 1 19980429 A 5260 206310110 STEP BELL 206 206L3 1182108 SW ENTRY CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6251X 51552 STEP CORRODED BEYOND LIMITS. 1 G 7 1 3U H2SW 1998050801091 19980508 01091 1998 5 8 HEEA0014053 4 19980429 A 3452 066106200 TRANSPONDER KT76 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER CR CRUISE 1 SW 03 21497 51518 MODE "C" REPORTED INOPERATIVE BY ATC. PERFORMED PRELIMINARY INSPECTION. FOUND PULSE WIDTH TO BE OUT OF SPECS AND REPLY LIGHT TO CONSTANTLY BLINK. 1 G 7 1 3U H2SW 1998050801092 19980508 01092 1998 5 8 HEEA0014054 4 19980429 A 2370 9806020023 CVR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 CVR CAUSES THE "TEST" LIGHT TO STAY ILLUMINATED CONSTANTLY. 1 G 7 2 4U H4SW 1998050801093 19980508 01093 1998 5 8 HEEA0014055 4 19980429 A 3457 0110005400 GPS GPS150 BELL 206 206L1 1182107 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 GPS NO LONGER NEEDED ON AIRCRAFT. BENCH CHECK REQUIRED. PERFORMED PRELIMINARY INSPECTION. FOUND DIRECT TO BUTTON UNREA DABLE. 1 G 7 1 3U H2SW 1998050801094 19980508 01094 1998 5 8 HEEA0014056 4 19980429 A 3457 0110005400 GPS GPS150 BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22425 45743 GPS TAKES 30 MINUTES TO COME ON. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT TO HAVE UNREADABLE ENTRY AND CRSR BUTTONS . 1 G 7 1 3U H2SW 1998050801095 19980508 01095 1998 5 8 HEEA0014057 4 19980429 A 3452 066106200 TRANSPONDER KT76 BELL 206 206B3 1181506 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3181Y 3772 NUMBERS ON THE DIAL, DO NOT MATCH DECODER NUMBER TRANSMITTING. FOUND UNIT SHOWING FALSE PULSES. CLEANED WAFER SWITCHES. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY TO SPECS. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1998050801096 19980508 01096 1998 5 8 HEEA0014058 4 19980429 A 3455 066104701 RECEIVER BELL 212 212 1181420 SW COCKPIT ADF FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5736J 31140 ADF RECEIVER WEAK RECEIVE AND NOT POINTING CORRECTLY IN ADF MODE. INSPECTED AND FOUND ADF MODE SIGNAL WEAK AND NOT POINT ING. TRIED ALIGNING RECEIVER. NO HELP. 1 G 7 1 4U H4SW 1998050801097 19980508 01097 NE 1998 5 8 HEEA0014059 1 19980429 A 2430 A1077D RELAY SKRSKY S76 S76A 8143006 NE DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 RELAY CONTACTS STUCK. REPLACED WITH SERVICEABLE RELAY. 1 G 7 2 3U H1NE 1998050801098 19980508 01098 SW 1998 5 8 HEEA0014060 1 19980429 A 2430 A1077 RELAY BELL 206 206L3 1182108 SW DC SYS STUCK E HEEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 03 4282Z 51499 STUCK CLOSED AFTER INSTALLATION. RESET RELAY AND TRIED AGAIN, UNIT THEN STARTED SMOKING. REPLACED WITH SERVICEABLE REL AY SYSTEM. 1 G 7 1 3U H2SW 1998050801099 19980508 01099 NE 1998 5 8 HEEA0014061 1 19980429 A 6510 S613764329002 TUBE ASSY 763610400704 SKRSKY S76 S76A 8143006 NE T/R DRIVE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4253S A248PHI0056 760035 T/R DRIVE TUBE SEPARATED BEYOND LIMITS. REPLACED WITH NEW TUBE ASSEMBLY. 1 G 7 2 3U H1NE 1998050801100 19980508 01100 EU 1998 5 8 HEEA0014062 1 19980429 A 6310 4638302002 INPUT PINION 4638001004 BOLKMS 105 BO105S 5626006 EU FREEWHEEL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3071K 1078 S859 INPUT PINION BEARING JOURNAL WORN BEYOND LIMITS. REPLACED WITH NEW PINION. 1 G 7 2 3U H3EU 1998050801101 19980508 01101 EU 1998 5 8 HEEA0014063 1 19980429 A 6520 4639311010 COVER 4639003007 BOLKMS 117 BK117B1 5626012 EU T/R XMSN WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 3102 384 7198 FORWARD BORE WORN FROM BEARING SPINNING. REPLACED WITH NEW COVER. 1 G 7 2 3U H13EU 1998050801102 19980508 01102 SW 1998 5 8 HEEA0014064 1 19980429 A 6420 212011701101 HUB ASSY BELL 412 412 1182202 SW T/R FEATHER BRG WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1202T 33112 T/R HUB ASSY WORN FEATHERING BEARING. REPLACED BEARINGS AND RETURNED TO SERVICE. 1 G 7 2 4U H4SW 1998050801103 19980508 01103 EU 1998 5 8 HEEA0014065 1 19980429 A 6330 579063 BEARING 355A12004008 SNIAS 350 AS350B2 8680813 EU M/R XMSN MT SEPARATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 6452 2862 RUBBER SEPARATION ON 4 EACH BEARINGS. 1 G 7 1 3U H9EU 1998050801104 19980508 01104 EU 1998 5 8 HEEA0014066 1 19980429 A 2823 857A1641 VALVE SNIAS 350 AS350B2 8680813 EU FUEL SYS STUCK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 350BZ 839 2653 VALVE STUCK. 1 G 7 1 3U H9EU 1998050801105 19980508 01105 SW 1998 5 8 HEEA0014067 1 19980429 A 3212 212073905001 GAUGE BELL 407 407 SW FLOAT PRESS CONTAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 MOISTURE IN GAUGE. 1 G 7 1 3U O H2SW 1998050801106 19980508 01106 SW 1998 5 8 HEEA0014068 1 19980429 A 3212 212073905001 GAUGE BELL 407 407 SW FLOAT PRESS CONTAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM 53060 MOISTURE IN GAUGE 1 G 7 1 3U O H2SW 1998050801107 19980508 01107 SW 1998 5 8 HEEA0014069 1 19980429 A 2820 233565 VALVE BELL 412 412 1182202 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 VALVE INOPERATIVE. 1 G 7 2 4U H4SW 1998050801108 19980508 01108 EU 1998 5 8 HEEA0014070 1 19980429 A 2435 23032048 STARTER BOLKMS 105 BO105S 5626006 EU ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 6825 S818 STARTER WILL NOT ENGAGE. 1 G 7 2 3U H3EU 1998050801109 19980508 01109 1998 5 8 HEEA0014071 4 19980429 A 2210 2593996333 TARSYN BELL 412 412 1182202 SW AUTO FLIGHT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 23023 33080 FAILS TEST 6.2 ON SST. COMPASS CARD WILL NOT MOVE. 1 G 7 2 4U H4SW 1998050801110 19980508 01110 1998 5 8 HEEA0014072 4 19980429 A 3421 258719343 GYRO BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 GYRO WILL NOT BECOME VALID. 2 G 7 2 4U H10SW 1998050801111 19980508 01111 SW 1998 5 8 HEEA0014073 1 19980429 A 7931 1179405807 INDICATOR BELL 214 214ST 1182106 SW ENG OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 PRESSURE NEEDLE FLUCTUATES WHEN VIBRATED. 2 G 7 2 4U H10SW 1998050801112 19980508 01112 SW 1998 5 8 HEEA0014074 1 19980429 A 6320 90093013 INDICATOR BELL 206 206L1 1182107 SW XMSN TEMP/PRESS FLUCTUATES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 45291 OIL PRESS NEEDLE FLUCTUATES. 1 G 7 1 3U H2SW 1998050801113 19980508 01113 EU 1998 5 8 HEEA0014075 1 19980429 A 6240 206075681117 INDICATOR BOLKMS 105 BO105S 5626006 EU ROTOR INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 ROTOR NEEDLE IS INTERMITTENT AND NOISY. 1 G 7 2 3U H3EU 1998050801114 19980508 01114 NE 1998 5 8 HEEA0014076 1 19980429 A 7714 7645001076101 INDICATOR SKRSKY S76 S76A 8143006 NE GAS GEN TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 GAS GEN TACH NO INDICATION ON DISPLAY OR ANALOG. 1 G 7 2 3U H1NE 1998050801115 19980508 01115 SW 1998 5 8 HEEA0014077 1 19980429 A 7712 206075739103 TORQUEMETER BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 20898 45721 TORQUEMETER NEEDLE DOESN'T RETURN TO ZERO. 1 G 7 1 3U H2SW 1998050801116 19980508 01116 1998 5 8 HEEA0014078 4 19980429 A 2312 7001840913 TRANSCEIVER BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141PH 33197 TRANSCEIVER POWER OUT FLUCTUATES WHEN VIBRATED. 1 G 7 2 4U H4SW 1998050801117 19980508 01117 1998 5 8 HEEA0014079 4 19980429 A 2312 7001840913 TRANSCEIVER BELL 412 412 1182202 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 TRANSCEIVER POWER OUT FLUCTUATES WHEN VIBRATED. 1 G 7 2 4U H4SW 1998050801118 19980508 01118 1998 5 8 HEEA0014080 4 19980429 A 3444 7000839904 INDICATOR BELL 412 412 1182202 SW RADAR ALT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 RADAR ALT NEEDLE STICKS AT 210 FEET. 1 G 7 2 4U H4SW 1998050801119 19980508 01119 1998 5 8 HEEA0014081 4 19980429 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW COCKPIT STICKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 36005 HSI INDICATOR HEADING SET POINTER STICKS INTERMITTENTLY. 1 G 7 2 4U H4SW 1998050801120 19980508 01120 1998 5 8 HEEA0014082 4 19980429 A 3416 5035P2P44 ALTIMETER BELL 412 412 1182202 SW COCKPIT ENCODE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 ENCODER READS OUT OF TOLERANCE AT 10,000 FEET AND ABOVE. 1 G 7 2 4U H4SW 1998050801121 19980508 01121 1998 5 8 HEEA0014083 4 19980429 A 3416 5035P2P44 ALTIMETER BELL 412 412 1182202 SW COCKPIT ENCODE ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 ENCODING ALT INDICATES 200 FEET LOW OUT OF TOLERANCE. 1 G 7 2 4U H4SW 1998050801122 19980508 01122 SW 1998 5 8 HEEA0014084 1 19980429 A 2842 391046199 PROBE BELL 412 412 1182202 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 FUEL QTY SENSOR CHAFED WIRE AND TROUBLESHOOTING. 1 G 7 2 4U H4SW 1998050801123 19980508 01123 1998 5 8 HEEA0014085 4 19980429 A 2210 214175259103 INDICATOR BELL 214 214ST 1182106 SW ELEV POSITION FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 ELEV POSITION INDICATOR INOPERATIVE. 2 G 7 2 4U H10SW 1998050801124 19980508 01124 1998 5 8 HEEA0014086 4 19980429 A 2562 ELT10 ELT NARCO BELL 206 206L3 1182108 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6610E 51424 ELT RESET BUTTON WILL NOT SPRING BACK. 1 G 7 1 3U H2SW 1998050801125 19980508 01125 1998 5 8 HEEA0014087 4 19980429 A 2312 7001840913 TRANSCEIVER BELL 412 412 1182202 SW COCKPIT DISPLAY DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 50,250,400, AND 1200 LEDS WILL NOT LIGHT. 1 G 7 2 4U H4SW 1998050801126 19980508 01126 1998 5 8 HEEA0014088 4 19980429 A 2312 071121540 CONTROL BELL 214 214ST 1182106 SW COMM SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59806 28140 25K PULL TUNING KNOB COMES OUT OF CONTROL HEAD WHEN PULLED. PERFORMED PRELIMINARY INSPECTION. FOUND LOOSE LOCK RING IN UNIT. REINSTALLED LOCK RING, REPAIRED. TESTED UNIT. BENCH CHECK GOOD. 2 G 7 2 4U H10SW 1998050801127 19980508 01127 SW 1998 5 8 HEEA0014089 1 19980429 A 6220 214010103115 SPINDLE 214010100207 BELL 214 214ST 1182106 SW M/R CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8045T 2945 A368 28101 EAR CRACKED IN MOUNT AREA APPROX. 2 INCHES ON BOTH SIDES, ON LOWER SIDE OF TRAILING EDGE OF WHITE BLADE. SCRAPPED PART. 2 G 7 2 4U H10SW 1998050801128 19980508 01128 SW 1998 5 8 HEEA0014090 1 19980430 A 5313 206031314123S LONGERON BELL 206 206L1 1182107 SW FUSELAGE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 TOOLING HOLES NOT IN ALIGNMENT WITH ORIGINAL, CAUSING BOW ALONG CENTER OF LONGERON. 1 G 7 1 3U H2SW 1998050801130 19980508 01130 GL 1998 5 8 HEEA0014092 2 19980430 A 7230 230052711 SPLINE ADAPTER 23051643 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE MIS MFG E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 792CH CAC90538 760193 CAE890532S RECEIVING INSPECTION REVEALED: O.D. MEASURED (.9853) .0002 UNDER SPECS ON SPLINE ADAPTER O.D. INSTALLED A NEW SPLINE AD APTER. 1 G 7 2 3U 3 U H1NE E1GL 1998050801131 19980508 01131 SW 1998 5 8 HEEA0014093 1 19980430 A 2821 206061634003 VALVE BELL 407 407 SW FUEL FILTER LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 53003 VALVE LEAKS. 1 G 7 1 3U O H2SW 1998050801132 19980508 01132 EU 1998 5 8 HEEA0014094 1 19980430 A 6230 350A37112601 LINK SNIAS 350 AS350B2 8680813 EU M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 1612 2873 SISSORS LINK BUSHING WORN. 1 G 7 1 3U H9EU 1998050801133 19980508 01133 EU 1998 5 8 HEEA0014095 1 19980430 A 7933 646600251 TEMP PROBE SNIAS 350 AS350B2 8680813 EU ENG OIL TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 2620 2777 TEMP PROBE INOPERATIVE. 1 G 7 1 3U H9EU 1998050801134 19980508 01134 SW 1998 5 8 HEEA0014096 1 19980430 A 6320 222375077113 TRANSMITTER BELL 407 407 SW GEARBOX OIL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 GAUGE READS ZERO OIL PRESSURE. 1 G 7 1 3U O H2SW 1998050801135 19980508 01135 SW 1998 5 8 HEEA0014097 1 19980430 A 6720 406312103101 LINK BELL 407 407 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM 53060 TAIL ROTOR PITCH CHANGE LINK HAS EXCESSIVE MECHANICAL WEAR. 1 G 7 1 3U O H2SW 1998050801136 19980508 01136 SW 1998 5 8 HEEA0014098 1 19980430 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CGOFL 53130 ONE DISK CRACKED ON NR7 THOMAS COUPLING PACK. 1 G 7 1 3U O H2SW 1998050801137 19980508 01137 SW 1998 5 8 HEEA0014099 1 19980430 A 7714 407375002103 INDICATOR BELL 407 407 SW ENG NG INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1167G 53067 NG INDICATOR INTERMITTENT INOPERATIVE. 1 G 7 1 3U O H2SW 1998050801138 19980508 01138 SW 1998 5 8 HEEA0014100 1 19980430 A 3213 206030104001 FITTING ASSY BELL 206 206B3 1181506 SW CROSSTUBE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22751 3627 FITTING ASSY WORN AND GOUGED. SCRAPPED FITTINGS AND REPLACED WITH SERVICEABLE FITTINGS. 1 G 7 1 3U H2SW 1998050801139 19980508 01139 1998 5 8 HEEA0014101 4 19980501 A 3441 6222898012 PROCESSOR UNIT BEECH 200 200BEECH 1152920 CE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 500PH BL29 RNAV PROCESSOR UNIT HAS SOME SEGMENTS THAT ARE INOPERATIVE. 1 L 7 2 4T A24CE 1998050801140 19980508 01140 1998 5 8 HEEA0014102 4 19980501 A 3414 8502CS20LW INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31217 760229 AIRSPEED INDICATOR INDICATES HIGH OUT OF TOLERANCE. 1 G 7 2 3U H1NE 1998050801141 19980508 01141 NE 1998 5 8 HEEA0014103 1 19980501 A 2611 30231R7B SMOKE DETECTOR SKRSKY S76 S76A 8143006 NE ENGINE MALFUNCTION E HEEA K NONE N FALSE WARNING NR NOT REPORTED 1 SW 03 1546K 760082 SMOKE DETECTOR GAVE INDICATION OF FIRE ONCE IN FLIGHT. 1 G 7 2 3U H1NE 1998050801142 19980508 01142 SW 1998 5 8 HEEA0014104 1 19980501 A 6710 206062721109 ACTUATOR BELL 206 206L3 1182108 SW M/R CONTROL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 49EA 51507 ACTUATOR WILL NOT ADJUST. 1 G 7 1 3U H2SW 1998050801143 19980508 01143 SW 1998 5 8 HEEA0014105 1 19980501 A 5320 206033410040S INTERCOSTAL BELL 206 206L1 1182107 SW FUSELAGE DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 MECHANICAL DAMAGE ON LOWER FORWARD BEND RADIUS. 1 G 7 1 3U H2SW 1998050801144 19980508 01144 SW 1998 5 8 HEEA0014106 1 19980501 A 2436 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 33080 GENERATOR WOULD NOT COME ON LINE. 1 G 7 2 4U H4SW 1998050801145 19980508 01145 1998 5 8 HEEA0014107 4 19980501 A 3421 125780 INDICATOR SKRSKY S76 S76A 8143006 NE COCKPIT ADI PRECESSES E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 1547D 760077 ADI INDICATOR PRECESSING IN FLIGHT. 1 G 7 2 3U H1NE 1998050801146 19980508 01146 1998 5 8 HEEA0014108 4 19980501 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW FLT DIRECTOR FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893N 33010 FD FLAG NOT RETRACTING WHEN POWER IS ON. 1 G 7 2 4U H4SW 1998050801147 19980508 01147 1998 5 8 HEEA0014109 4 19980501 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 108X 33115 ATTITUDE INDICATOR WILL NOT OPERATE IN PITCH. 1 G 7 2 4U H4SW 1998050801148 19980508 01148 1998 5 8 HEEA0014110 4 19980501 A 3421 2360041905 ROTOR ASSY BELL 206 206L1 1182107 SW INDICATOR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11027 45411 ROTOR ASSY BEARINGS ARE BAD. 1 G 7 1 3U H2SW 1998050801149 19980508 01149 1998 5 8 HEEA0014111 4 19980501 A 2562 ELT910 ELT NARCO BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 513EH 45421 ELT UNIT FOUND IN ON POSITION FOR UNKNOWN TIME. 1 G 7 1 3U H2SW 1998050801150 19980508 01150 WP 1998 5 8 TWAA9805403 1 19980409 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9412W 53187 STL - DURING MAINTENANCE CHECK OF AIRCRAFT, FOUND EGRESS LIGHTS INOPERATIVE ROW 3 TO ROW 7 IN CABIN, AND RED EGRESS BULB INOPERATIVE AT AFT OVERWING EXIT AND L2 DOOR. SECURED LOOSE CONNECTION AT ROW 3, AND REPLACED LAMPS AT L2 DOOR AND AFT OVERWING EXIT. CHECK-C 9-6-97 LAX. (X) 2 L 7 2 4F RT A6WE 1998050801151 19980508 01151 WP 1998 5 8 G6OA020 1 19980402 A 2830 107796A108 ACTUATAOR DOUG DC10 DC1030 3023501 WP LT FUEL DUMP FAILED A G6OA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 27 606GC 47929 ORD/BSL - DURING FLIGHT, CREW IDENTIFIED A PROBLEM WITH NR 1 AC BUS AND ELECTED TO DIVERT TO JFK. PRIOR TO LANDING DURI NG FUEL DUMP, THE LEFT FUEL DUMP VALVE CONTROL CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER, AFTER 90 SECONDS CIR CUIT BREAKER TRIPPED AGAIN. GROUND MAINTENANCE REPLACED LEFT FUEL DUMP ACTUATOR PER MM 28-30-02. NO LEAKS FOUND. OPER ATIONAL CHECK NORMAL. OK FOR SERVICE. (X) 2 L 7 3 4F A22WE 1998050801152 19980508 01152 WP 1998 5 8 SABA980020 2 19980330 A 7320 8961153 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE TORN A SABA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 33 963AE 963 ISO - FLT 5022 - ON FLIGHT FROM ISO/CLT, PILOT ABORTED TAKEOFF FOR LEFT ENGINE BARELY MAKING 92 PERCENT TORQUE. NO EMER GENCY WAS DECLARED. AIRCRAFT RETURNED TO PARKING. MAINTENANCE FROM CLT REMOVED AND REPLACED THE P-3 GASKET. AIRCRAFT RU N AND OPS CHECKED GOOD. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1998050801153 19980508 01153 NM 1998 5 8 TWRA9817 1 19980326 A 5242 65B135943 UPPER GATE BOEING 747 7472F6B 1384807 NM NR 3 L ME DOOR CRACKED A TWRA K NONE O OTHER IN INSP/MAINT 1 EA 15 623FF 083 22382 NR 3L ME DOOR, UPPER GATE IS CRACKED AT CENTER. REMOVED AND REPLACED NR 3 ME DOOR UPPER GATE PER MM 52-11-01. LEAK CHE CK OK. (X) 2 L 7 4 4F A20WE 1998050801154 19980508 01154 CE 1998 5 8 COEA9801709 1 19980331 A 3030 PITOT HEAT CESSNA 208 208B 2073701 CE RT WING FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 709FX 1148 208B0430 DURING CLIMB-OUT IN IMC CONDITIONS, THE PAR WARNING ILLUMINATED INDICATING EXCESS AIRSPEED. COPILOT AIRSPEED INDICATOR WAS ABOVE REDLINE. PILOT DECLARED AN EMERGENCY AND RETURNED TO BASE WITHOUT EVENT. MAINTENANCE FOUND NR 2 PITOT HEAT I NOPERATIVE AND HAD ICED OVER IN-FLIGHT CAUSING COPILOT AIRSPEED TO INDICATE ABOVE ACTUAL. NR 2 PITOT TUBE WAS REPLACED. STATIC SYSTEM LEAK CHECKED SATISFACTORY. PITOT HEAT SYSTEM FUNCTION CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE . (X) 1 H 7 1 3T A37CE 1998050801155 19980508 01155 EU 1998 5 8 VTZA98123 1 19980308 A 6120 89741011 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 497UE 904 EWR/IAD - FLT 6555 - DURING TAKEOFF AT 1245 HOURS ON 3-8-98, AIRCRAFT ABORTED TAKEOFF DUE TO RT ENGINE RPM ONLY REACHED 98.5 PERCENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED X-SCREW ON PROP G OVERNOR. GROUND RAN AIRCRAFT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998050801156 19980508 01156 GL 1998 5 8 98ZZZX1701 2 19980312 A 7261 23058110A TUBE BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL SCAVENGE OIL CHAFED D A K NONE O OTHER IN INSP/MAINT 1 NM 01 108W 2100 52034 CAE895731 WHILE REMOVING RENTAL ENGINE AND TRANSFERRING HARD LINE P/N 23058110-A FROM RENTAL ENGINE TO ORIGINAL ENGINE, SEVERE CHA FING NOTED UNDER ADEL CLAMP. THIS IS SCAVENGE OIL LINE FROM BOTTOM OF COMPRESSOR TO THE N1 SIDE OF GEARBOX. ABRASIVE D UST AND AIRBORNE DIRT CREEPS IN BETWEEN HARD RUBBER ADEL CLAMP AND OIL LINE AND CHAFES OR WEARS OIL LINE TO THE POINT OF FAILURE. THE NEED EXISTS FOR CLAMPING DEVICES THAT WOULD ELIMINATE THIS CHAFING CONDITION. IN THE MEANTIME, INSPECTIO N UNDER CLAMPED AREAS IS PRUDENT TO AVOID AN UNSUSPECTED FAILURE. 1 G 7 1 3U 3 U NC H2SW E1GL 1998050801157 19980508 01157 WP 1998 5 8 98ZZZX1702 1 19980416 A 6520 369D25400 GEARBOX HUGHES 369 369D 4470706 WP T/R MAKING METAL B LS1R K NONE O OTHER IN INSP/MAINT 1 EA 13 369AW 1195 470117D DURING ROUTINE INSPECTION, MECHANIC FOUND METAL AND EXCESSIVELY DARK OIL IN GEARBOX. REMOVED FOR REPAIR AND REPLACED WI TH SERVICEABLE UNIT. CONTROL NR 98-4-8. 1 G 7 1 3U H3WE 1998050801158 19980508 01158 EU 1998 5 8 98ZZZX1703 1 19980424 A 2612 17343624101 DETECTOR BOLKMS 117 BK117B1 5626012 EU LOWER AFT FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 460H 7142 FOUND LOWER AFT FIRE DETECTOR STARTING TO SHORT INTERNALLY. REMOVED DEFECTIVE PART, INSTALLED SERVICEABLE PART. 1 G 7 2 3U H13EU 1998050801159 19980508 01159 EU 1998 5 8 98ZZZX1704 1 19980421 A 6410 117317411 BLADE BOLKMS 117 BK117B1 5626012 EU T/R CRACKED A BAQA K NONE O OTHER IN INSP/MAINT 1 EA 03 911TG 1087 134 7506 DURING A PRE-FLIGHT INSPECTION, THE MECHANIC FOUND A 3 INCH CRACK AT THE ROOT END OF TAIL ROTOR BLADE. THIS IS THE THIR D EVENT. 11-18-94, 198.4 HRS, S/N 116/118. 5-3-96, 1,050.1 HRS, S/N 103/104. 858.5 HOURS ON THE BLADES, SAME P/N. 1 G 7 2 3U H13EU 1998050801161 19980508 01161 NE 1998 5 8 98ZZZX1706 1 19980427 A 6320 7635109032047 SPUR GEAR SKRSKY S76 S76A 8143006 NE M/R GEARBOX FRACTURED B S A HEER K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G B12800040 760076 INVESTIGATION INTO A SERIES OF CHIP DETECTOR LIGHTS ON THE MAIN GEARBOX REVEALED THE SPUR GEAR HAD FRACTURED IN THREE PL ACES. THE WEB OF THE GEAR HAD TWO SEPARATE FRACTURES AND THE SHAFT OF THE GEAR HAD ONE FRACTURE. TWO OF THE PINS (P/N HL12VLJ-8-5/6) THAT SECURE THE SPUR GEAR ASSEMBLY TOGETHER HAD ALSO SHEARED. MANY OTHER PINS SHOWED SIGNS OF WORKING. T HE MAIN GEARBOX WAS OVERHAULED 227 OPERATING HOURS PRIOR TO THIS OCCURRENCE. THE SPUR GEAR IS NOT A LIFE LIMIT PART; TH EREFORE, HISTORICAL RECORDS ARE NOT REQUIRED AND THE TOTAL TIME IN SERVICE OF THE GEAR IS NOT KNOWN AT THIS TIME. 1 G 7 2 3U H1NE 1998050801162 19980508 01162 WP 1998 5 8 HALA9800078 1 19980401 A 2131 10256852 CONTROLLER DOUG DC9 DC951 3022051 WP COCKPIT FAILED A HALA K NONE O OTHER TO TAKEOFF 1 WP 13 420EA 1051502 47689 OGG - FLT 533 - LOG PAGE A142518. DURING LIFT-OFF AND EXTENSION OF NOSE GEAR, THE CABIN PRESSURE DESCENDS MORE THAN 1,5 00 FPM. REPLACED CABIN PRESSURE CONTROLLER. (X) 2 L 7 2 4F RT A6WE 1998050801261 19980508 01261 EU 1998 5 8 PNSA980401 1 19980417 A 3020 NH24668161 DUCT SAAB SF340 340B 7860101 EU RT INLET FAILED A PNSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 685PA 212 RT INTAKE HEAT FAILED DURING CRUISE IN ICE. LEFT ICING AREA, RETURNED TO BASE. REPLACED LOWER INLET DUCT, OPS CHECKED OK. 2 L 7 2 4T RT A52EU 1998050801262 19980508 01262 SW 1998 5 8 PNSA980402 1 19980403 A 5230 SEAL SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR OUT OF POSITION A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 640PA AC759B AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BASE. ADJUSTED CARGO DOOR SEAL INFLATION VALVE, OPS CHECK OK. 2 L 7 2 4T RT A8SW 1998050801263 19980508 01263 1998 5 8 PNSA980403 4 19980404 A 2350 M1035 AUDIO PANEL SWRNGN SA227 SA227AC 8780603 SW COCKPIT INOPERATIVE A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 2708D 54617 AC713B BEFORE ENGINE START, INTERCOM INOP. REPLACED AUDIO PANEL, OPS CHECK OK. 2 L 7 2 4T RT A8SW 1998050801264 19980508 01264 SO 1998 5 8 RAAA98E8011 1 19980504 A 3350 240998C RELAY LKHEED 188 188C 5262604 SO BS 530 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 ON SERVICE CHECK EXTERNAL OVERWING EMERGENCY LIGHTS WILL NOT TURN OFF. CHANGED ARM-DISARM K106M RELAY DUE FAILED. 2 L 7 4 4T 4A22 1998050801265 19980508 01265 SO 1998 5 8 RAAA98E8012 1 19980504 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT LT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT DUE FAILED. 2 L 7 4 4T 4A22 1998050801266 19980508 01266 NM 1998 5 8 CALA9800751 1 19980504 A 5414 301A31091 SKIN BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 23588 A .5 INCH CRACK COMING FROM UPPER FWD CORNER OF NR 1 PYLON PANEL 5724. REPAIRED PYLON PER EC/RA 5430-01204. 2 L 7 2 4F RT A16WE 1998050801267 19980508 01267 WP 1998 5 8 CALA9800756 1 19980501 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1117 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 TEMP REPAIR ON AIRPHONE ANTENNA AT STA 1117. REPLACED PER SRM 53-04 AND EC/RA 5330-02657. 2 L 7 2 4F A6WE 1998050801268 19980508 01268 WP 1998 5 8 CALA9800757 1 19980501 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1098 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 TEMP REPAIR ON AIRPHONE ANTENNA AT STA 1098. REPAIRED PER SRM 53-04 AND EC/RA 5330-02657. 2 L 7 2 4F A6WE 1998050801269 19980508 01269 WP 1998 5 8 CALA9800758 1 19980504 A 5210 49559481N HOUSING DOUG DC9 DC982 3022082 WP L1 DOOR WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 MAIN CABIN DOOR HOLD OPEN HOOK WELL WORN INTO BY HOOK AND SKIN AROUND LOWER EDGE OF HOOK WELL OPENING DAMAGED FORWARD FU SELAGE. BURNISHED MAIN CABIN DOOR SKIN AND REPLACED HOLD OPEN HOOK HOUSING PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998050801270 19980508 01270 WP 1998 5 8 CALA9800759 1 19980503 A 2612 59585701 SUPPORT DOUG DC9 DC982 3022082 WP NR 2 ENGINE BROKEN A CALA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 71828 49488 NUMBER 2 ENGINE FIRE LIGHT ILLUMINATED AFTER TAKEOFF. ACCOMPLISHED ABNORMAL CHECKLIST. LIGHT REMAINED ON. FOUND FIRE DETECTOR SUPPORT BROKEN AND LOOP CONNECTORS CORRODED AND DAMAGED. REPLACED A AND B LOOP CONNECTORS AND TESTED SYSTEM. R EPLACED NR 1 AND 2 FIRE BOTTLES AND SQUIBS PER MM 26-20-01, 26-20-02, AND 26-20-03. 2 L 7 2 4F A6WE 1998050801271 19980508 01271 WP 1998 5 8 CALA9800760 1 19980430 A 5210 9955758 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 MAIN CABIN DOOR NR 7 BEAM FWD END CRACKED (1). INSTALLED REPAIR ANGLE PER SRM 52-05 FIG 31. 2 L 7 2 4F A6WE 1998050801272 19980508 01272 WP 1998 5 8 CALA9800761 1 19980429 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FWD ENTRY DOOR NR 6 BEAM CRACKED AT FWD END ABOVE INTERLOCK MECHANISM (1.5). REPAIRED PER SRM 52-05 FIG 31. 2 L 7 2 4F A6WE 1998050801273 19980508 01273 WP 1998 5 8 CALA9800762 1 19980429 A 5311 9911859121 FRAME DOUG DC9 DC982 3022082 WP BS 1446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CANTED FRAME HAS IMPROPER STOP DRILL HOLES AT END OF CRACKS WITH CRACK GOING BEYOND DRILLED HOLES AT STA 1446 IN 8 PLACE S (10 TOTAL FOR ALL CRACKS). REPLACD BELTFRAME AT STATION 1446 FROM LONG 10 LT TO 10 RT PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998050801274 19980508 01274 WP 1998 5 8 CALA9800763 1 19980429 A 5210 4917851505 FITTING DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 T-FITTING CRACKED (2) AT LEFT SIDE ON FORWARD SIDE IN LINE WITH LATCHING MECHANISM, AFT ENTRY DOOR. REMOVED AND REPLACE D FITTING PER SRM 51-30-0. 2 L 7 2 4F A6WE 1998050801275 19980508 01275 WP 1998 5 8 CALA9800764 1 19980429 A 5210 591412161N PAN DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 FORWARD ENTRY DOOR PAN CRACKED (1.5) AT FWD LOWER STOP PAD. REPLACED FWD LOWER PAN ON FWD ENTRY DOOR PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998050801276 19980508 01276 WP 1998 5 8 CALA9800765 1 19980429 A 5347 SR095301157003 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 208 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CORROSION RIGHT OUTBOARD SEAT TRACK STA 208. FABRICATED NEW SEAT TRACK SPLICE AND INSTALLED PER SRM 53-05 FIG 4F. 2 L 7 2 4F A6WE 1998050801277 19980508 01277 WP 1998 5 8 CALA9800766 1 19980429 A 5320 SUB FLOOR DOUG DC9 DC982 3022082 WP BS 200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 SURFACE CORROSION AT UNDER SIDE OF CABIN SUB FLOOR, E AND E COMPT AREA, STA 200 RBL 10, FWD SIDE OF FRAME. REMOVED DAMA GED AREA. FABRICATED AND INSTALLED DOUBLED PER SRM 53-01. 2 L 7 2 4F A6WE 1998050801278 19980508 01278 WP 1998 5 8 CALA9800767 1 19980430 A 5320 DRAIN PAN DOUG DC9 DC982 3022082 WP BS 148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 E AND E COMPARTMENT UPPER FLOOR STA 148 RBL 45, DRAIN LINE FITTING AREA SUB FLOOR CORROSION. REMOVED DAMAGED AREA. FAB RICATED AND INSTALLED DOUBLER PER EC/RA 5320-01210. 2 L 7 2 4F A6WE 1998050801279 19980508 01279 WP 1998 5 8 CALA9800768 1 19980430 A 5311 SR09530057 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 AFT CARGO COMPT STA 1309 LONG 29R TO 29L HEAVY SURFACE CORROSION, BELTFRAME AND SKIN ATTACH CLIP. TRIMMED OUT CORRODED SECTION PER SRM 53-05 FIG 2A, FABRICATED AND SPLICED IN NEW BELTFRAME SECTION PER SRM 53-03 FIG 2A. 2 L 7 2 4F A6WE 1998050801280 19980508 01280 NM 1998 5 8 9807796612 1 19980127 A 5330 SKIN BOEING 747 747251B 1384892 NM BS 1473 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND SKIN DELAMINATED AND CORRODED AT LEFT BODY LANDING GEAR WHEEL WELL FS 1473, LBL 120, WL 175. REPA IRED PER EA 66-156323. 2 L 7 4 4F A20WE 1998050801281 19980508 01281 NM 1998 5 8 9807806612 1 19980116 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON STRINGER END FITTING FS 2360. REPLACED FITTING (P/N 65B0437-8) PER DWG 65B04161. 2 L 7 4 4F A20WE 1998050801282 19980508 01282 NM 1998 5 8 9807816612 1 19980222 A 5320 DOUBLER BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON REINFORCING DOUBLER ON INTERFACE AREA FS 2360 AT 6 O'CLOCK POSITION. REPAIRED PER EA 66-153214. 2 L 7 4 4F A20WE 1998050801283 19980508 01283 NM 1998 5 8 9807826612 1 19980210 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 1000 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON THE STRINGER END FITTING 46R AT FS 1000. INSTALLED NEW STRINGER END FITTING PER SRM 51-30-02, 05. 2 L 7 4 4F A20WE 1998050801284 19980508 01284 NM 1998 5 8 9807836612 1 19980218 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 460 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND FLOORBEAM WEB CRACKED AT FS 460 ADJACENT TO STR 13R. REPAIRED PER EA 66-156307. 2 L 7 4 4F A20WE 1998050801285 19980508 01285 NM 1998 5 8 9807846612 1 19980309 A 5320 CHORD BOEING 747 747251B 1384892 NM FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK ON UPPER CHORD TOP SURFACE FASTENER HOLE AT WL 199, RBL 66. REPAIRED PER EA 66-156316. 2 L 7 4 4F A20WE 1998050801286 19980508 01286 NM 1998 5 8 9807856612 1 19980122 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 1350 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON FLOORBEAM WEB AT FS 1350, LBL 33. REPAIRED PER EA 66-153207. 2 L 7 4 4F A20WE 1998050801287 19980508 01287 NM 1998 5 8 9807866612 1 19980222 A 5313 STRINGER BOEING 747 747251B 1384892 NM BS 2360 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON STRINGER WEB AT FS 2360 ADJACENT TO DRAIN HOLE. REPAIRED PER EA 66-153214. 2 L 7 4 4F A20WE 1998050801288 19980508 01288 NM 1998 5 8 9808266612 1 19980116 A 5320 CHORD BOEING 747 747251B 1384892 NM BS 495-520 CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON DIAGONAL FLOOR INTERCOSTAL UPPER CHORD CLIP NUT HOLES AT FS 495 TO 520, LBL 9 TO 40. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998050801289 19980508 01289 NM 1998 5 8 9807876612 1 19980208 A 5320 DOUBLER BOEING 747 747251B 1384892 NM BS 730 CORROSION A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON BONDED DOUBLER OUT OF LIMIT AT FS 730, STR 12R. REPAIRED PER EA 66-155576. 2 L 7 4 4F A20WE 1998050801290 19980508 01290 NM 1998 5 8 9807886612 1 19980209 A 5312 BULKHD FASTENER BOEING 747 747251B 1384892 NM BS 140 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK ON FASTENER HOLE AT FS 140 BULKHEAD, STR 14R, INNER RING DOUBLER AREA. REPAIRED PER EA 66-1 56319. 2 L 7 4 4F A20WE 1998050801291 19980508 01291 NM 1998 5 8 9807896612 1 19980128 A 5320 PRESSURE DECK BOEING 747 747251B 1384892 NM BS 1394 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON LEFT BODY LANDING GEAR WHEEL WELL PRESSURE DECK AT FS 1394, LBL 119, WL 180. REPAIRE D PER EA 66-155575. 2 L 7 4 4F A20WE 1998050801292 19980508 01292 NM 1998 5 8 9807906612 1 19980118 A 5313 LONGERON BOEING 747 747251B 1384892 NM BS 1040-1060 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK ON STR 7L AT FS 1040 AND 1060. REPAIRED PER EA 66-156558. 2 L 7 4 4F A20WE 1998050801293 19980508 01293 WP 1998 5 8 9807919990 1 19980501 A 5610 WINDOW SEAL DOUG DC9 DC931 3022065 WP LT COCKPIT BLOWN A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8950E 47186 DURING CLIMB AT 13,000 FEET AND 5 PSI, THE CAPTAIN'S SLIDING WINDOW SEAL BLEW OUT AND CAUSED A LOUD NOISE AND SOME LOSS OF CABIN PRESSURE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE RESEALED WINDOW. 2 L 7 2 4F A6WE 1998050801294 19980508 01294 WP 1998 5 8 9807929983 1 19980430 A 2450 CIRCUIT BREAKER DOUG DC9 DC932 3022066 WP LT AC BUS DAMAGED A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 983US 47282 ALL PHASES OF LEFT AC BUS CIRCUIT BREAKERS POPPED IN FLIGHT. FLIGHT WAS DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. M AINTENANCE FOUND LEFT AC C PHASE CIRCUIT BREAKER DAMAGED. REPLACED CIRCUIT BREAKER AND RESET ALL TRIPPED CIRCUIT BREAKE RS ON AFT PANEL, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801295 19980508 01295 WP 1998 5 8 9807939615 1 19980501 A 2450 POWER RELAY DOUG DC9 DC932 3022066 WP RIGHT FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 615NW 47129 CREW DETECTED ELECTRICAL BURNING SMELL IN COCKPIT DURING FINAL APPROACH. AIRCRAFT LANDED WITHOUT INCIDENT AND POWER WAS SWITCHED TO EMERGENCY POWER ONLY. SMELL DISSIPATED. MAINTENANCE FOUND LOOSE HARDWARE AT TERMINAL STRIPS ON EITHER SID E OF CROSSTIE RELAY AND RIGHT AC POWER RELAY STUD BROKEN. REPLACED AND RESECURED HARDWARE AND REPLACED RIGHT AC POWER R ELAY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801296 19980508 01296 WP 1998 5 8 9807949955 1 19980501 A 3250 59142965505 VALVE DOUG DC9 DC931 3022065 WP NLG STEERING FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 922RW 37289 31703 47182 CREW ABORTED TAKEOFF AT 80 KNOTS DUE TO AIRCRAFT PULLING TO THE LEFT. MAINTENANCE FOUND NOSE STEERING RETURNING LEFT OF CENTER. REPLACED NOSE STEERING CONTROL VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801297 19980508 01297 WP 1998 5 8 9807959301 1 19980501 A 3220 LANDING GEAR DOUG DC9 DC982 3022082 WP NLG LACK OF LUBE A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 301RC 48054 NOISE AND VIBRATION COMING FROM NOSE GEAR AREA AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. M AINTENANCE LUBED ENTIRE NOSE GEAR ASSEMBLY, SHOOK WIRING, AND CYCLED GEAR SEVERAL TIMES. DISCREPANCY COULD NOT BE DUPLI CATED. 2 L 7 2 4F A6WE 1998050801298 19980508 01298 1998 5 8 9807969969 4 19980502 A 2565 113317 SLIDE DOUG DC9 DC931 3022065 WP PAX DOOR LOW PRESSURE A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9333 52233 3616 47246 DURING PERIODIC CHEDK, FOUND MAIN CABIN DOOR EVACUATION SLIDE BOTTLE PRESSURE LOW. REPLACED SLIDE. 2 L 7 2 4F A6WE 1998050801299 19980508 01299 WP 1998 5 8 9807979905 1 19980430 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN NOT SECURE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 955N 47160 DURING LINE MAINTENANCE INSPECTION, FOUND AISLE EMERGENCY LIGHT AT ROW 15 INOPERATIVE. RESEATED CONNECTOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801300 19980508 01300 WP 1998 5 8 9807989617 1 19980430 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 617NW 47235 FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 5 THRU 7 INOPERATIVE. REPAIRED BROKEN WIRES AT RIGHT FORWARD OVERWING EME RGENCY LIGHTS POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801301 19980508 01301 WP 1998 5 8 9807999758 1 19980502 A 3350 BULBS DOUG DC9 DC941 302207N WP CABIN NOT SECURE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 20 THRU 23 INOPERATIVE. SECURED BULBS IN SOCKETS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801302 19980508 01302 WP 1998 5 8 9808009758 1 19980502 A 3350 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 758NW 47286 DURING LINE MAINTENANCE INSPECTION, FOUND AFT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT AND BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801303 19980508 01303 WP 1998 5 8 9808019619 1 19980502 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 619NW 47518 DURING PERIODIC CHECK, FOUND FORWARD FLIGHT ATTENDANT UPPER EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERIES, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801304 19980508 01304 WP 1998 5 8 9808029614 1 19980502 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 614NW 47128 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801305 19980508 01305 WP 1998 5 8 9808039611 1 19980501 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611NA 47435 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801306 19980508 01306 WP 1998 5 8 9808049931 1 19980429 A 2782 ROD END DOUG DC9 DC931 3022065 WP SLAT DRIVE ACT BROKEN A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 90S 47244 DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH AIRCRAFT ROLL OF APPROXIMATELY 20 DEGREES ON SLAT EXTENSION. M AINTENANCE FOUND LEFT LOWER SLAT DRIVE CYLINDER ROD END BROKEN. REPLACED ROD END, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801307 19980508 01307 WP 1998 5 8 9808059611 1 19980501 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611NA 47435 DURING LINE MAINTENANCE INSPECTION, FOUND MAIN CABIN DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATION AL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801308 19980508 01308 WP 1998 5 8 9808069980 1 19980502 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9344 47440 DURING LINE MAINTENANCE INSPECTION, FOUND BOTH LEFT AND RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE DURING TEST. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801309 19980508 01309 WP 1998 5 8 9808079978 1 19980503 A 3350 BC50447907 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9342 47391 DURING LINE MAINTENANCE INSPECTION, FOUND AFT RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801310 19980508 01310 WP 1998 5 8 9808089971 1 19980503 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGTHS ABOVE TAIL CONE EXIT HATCH INOPERATIVE. REPLACED BATTERY PAC K, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801311 19980508 01311 WP 1998 5 8 9808099971 1 19980503 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP RT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9335 47337 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT ENGINE NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801312 19980508 01312 WP 1998 5 8 9808109953 1 19980501 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 918RW 47158 FLIGHT ATTENDANT REPORTED EMERGENCY LIGHTS BETWEEN ROWS 8 THRU 10 WOULD NOT EXTINGUISH WITH SWITCH IN OFF POSITION. REP LACED POWER SUPPLY AND BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801313 19980508 01313 WP 1998 5 8 9808119953 1 19980501 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 918RW 47158 DURING PERIODIC CHECK, FOUND EMERGENCY LIGHTS BETWEEN ROWS 9 THRU 11 AND AT LEFT FORWARD OVERWING EMERGENCY EXIT INOPERA TIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801314 19980508 01314 WP 1998 5 8 9808129940 1 19980501 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3322L 47031 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NO RMAL. 2 L 7 2 4F A6WE 1998050801315 19980508 01315 WP 1998 5 8 9808139925 1 19980501 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP RT NACELLE INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 925US 47472 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERIE S, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801316 19980508 01316 WP 1998 5 8 9808149909 1 19980501 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 959N 47255 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AND POW ER SUPPLIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801317 19980508 01317 WP 1998 5 8 9808159906 1 19980502 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST UK UNKNOWN 1 GL 01 956N 47252 FLIGHT ATTENDANT REPORTED MAIN CABIN DOOR UPPER FLASHLIGHT NOT BLINKING. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMA L. 2 L 7 2 4F A6WE 1998050801318 19980508 01318 WP 1998 5 8 9808169878 1 19980502 A 3350 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 787NC 48149 DURING LINE MAINTENANCE INSPECTION, FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS IN MAIN CABIN INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050801319 19980508 01319 WP 1998 5 8 9808179868 1 19980501 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD LIGHTS BETWEEN ROWS 11 THRU 14 INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050801320 19980508 01320 WP 1998 5 8 9808189853 1 19980503 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 762NC 47710 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS BETWEEN ROWS 19 THRU 22 INOPERATIVE. REPLACE D BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050801321 19980508 01321 WP 1998 5 8 9808199308 1 19980501 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 311RC 48089 DURING LINE MAINTENANCE INSPECTION, FOUND FLOOR PROXIMITY EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. REPAIRED BROKE N WIRING, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801322 19980508 01322 WP 1998 5 8 9808209308 1 19980502 A 3350 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 311RC 48089 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT CENTER OVERHEAD BETWEEN ROWS 29 THRU 32 AND AT AFT CABIN D OOR INOPERATIVE. REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801323 19980508 01323 NE 1998 5 8 9808211160 2 19980502 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 160US 46769 686168 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT REACHED 800C BEFORE THE ENG INE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER TAFI 71-00-00 WITH NO DEFECTS NOTED. THE THRUST REVERSER WAS P LACED ON MEL 78-1A UNTIL A RABS CHECK IS ACCOMPLISHED. THE AIRCRAFT RETURNED TO SERVICE. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998050801324 19980508 01324 WP 1998 5 8 9808229877 1 19980504 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 9 THRU 13. MAINTENANCE REPLACED THE POWER SUPPL Y AND BATTERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050801325 19980508 01325 NM 1998 5 8 9808236302 1 19980504 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 662US 23720 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT ROWS 43ABC AND 51ABC AND FROM ROWS 36HJK TO 43HJK. R ECONNECTED WIRES, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998050801326 19980508 01326 WP 1998 5 8 9808249920 1 19980503 A 2131 10256861 CONTROLLER DOUG DC9 DC932 3022066 WP CABIN FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 942N 32062 2916 47459 AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CABIN ALTITUDE INDICATED 11,000 FEET WITH AIRCRAFT ALTITUDE AT 16,000 FEET . CABIN DID NOT DESCEND UNTIL ACTUAL AIRCRAFT DESCENT. FLIGHT WAS RETURNED TO YYC AND LANDED WITHOUT INCIDENT. MAINTE NANCE REPLACED THE CABIN PRESSURE CONTROLLER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801327 19980508 01327 WP 1998 5 8 9808259960 1 19980504 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 920RW 47163 DURING PERIODIC CHECK, FOUND LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801328 19980508 01328 SO 1998 5 8 COMA9810113 1 19980504 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 243CA 17218 868 120212 CABIN EMERGENCY LIGHTS FAIL AFTER 15 SECONDS OF USE. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4T RT A31SO 1998050801329 19980508 01329 NE 1998 5 8 COMA9860095 2 19980504 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT BIRD STRIKE A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 916CA 7014 807305 BIRD STRIKE AFTER TAKEOFF. LEFT ENGINE VIB INDICATED 2.8. COMPLIED WITH BIRD STRIKE INSPECTION. REPLACED THE LEFT ENG INE DUE TO BIRD INJESTION. 2 L 7 2 4F 4 F RT A21EA E15NE 1998050801330 19980508 01330 NM 1998 5 8 UPS98226548 1 19980505 A 3350 BATTERY PACK BOEING 727 72727C 138400J NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 907UP 19118 INSPECTION TYPE-N/A, EMERG EXIT LIGHTS AT COCKPIT DOOR AND FWD ENTRY DEAD. REPLACED BATTERIES IN BOTH PACKS, OPS CHECKE D NORMAL MANUAL AND IN ARMED. 2 L 7 3 4F A3WE 1998050801331 19980508 01331 NM 1998 5 8 UPS98426555 1 19980505 A 3350 BULB BOEING 747 747123 1384873 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 671UP 20323 INSPECTION TYPE-N/A, FWD L1 DOOR EMER LIGHT IS INOP. INSTALLED LT BULB, OP CHK OK. 2 L 7 4 4F A20WE 1998050801332 19980508 01332 NM 1998 5 8 UPS98526544 1 19980505 A 2421 727792K IDG BOEING 757 75724APF 1384969 NM LT ENGINE FAILED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 456UP 25477 INSPECTION TYPE-N/A, LEFT GEN FAILED. EICAS MSG L GEN DRIVE DISPLAYED. GEN DRIVE LIGHT ILLUM. GEN DRIVE DISCONECTED, RIGHT GEN WAS DEFERRED. FOUND FILTER BYPASS POPPED AND METAL CHIPS IN FILTER. REPLACED LT IDG (P/N 727792K), (S/N A112 0) OFF, (S/N A1004) ON. SEE ITEM 3 FOR POSSIBLE OIL COOLER CONTAMINATION. WORK PER MM 24-11-01, OPS CHECKS GOOD PER MM 24-11-00. 2 L 7 2 4F RT A2NM 1998050801333 19980508 01333 NM 1998 5 8 UPS98526556 1 19980505 A 3350 SWITCH BOEING 757 75724APF 1384969 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 466UP 25482 INSPECTION TYPE-N/A, EMER LIGHT OVER MAIN ENTRY DOOR ON WHEN SW IS OFF. FOUND BAD SWITSH ASSY. REMOVED AND REPLACED EM ER LIGHT SWITCH ASSY IAW MM 33-50, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 1998050801334 19980508 01334 WP 1998 5 8 UPS98826543 1 19980424 A 5320 3755841501 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, SHEAR TIE FITTING CRACKED AT FS 1200 BTWN LONG 33R AND 34R. REMOVED AND REPLACED FITTING IAW SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1998050801335 19980508 01335 WP 1998 5 8 UPS98826545 1 19980423 A 5320 37558472N SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FS 1160 AT STR 33R SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050801336 19980508 01336 WP 1998 5 8 UPS98826546 1 19980422 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FRAME CRACKED FS 1600 L-21L FWD OF FITTING. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998050801337 19980508 01337 WP 1998 5 8 UPS98826549 1 19980422 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 304-310 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING L/E SKIN ON TOP AT FRONT SPAR, BTWN STA XFS 304.00 TO 310.25 HAS 3 CRACKS AROUND FASTENERS. R EPAIRED IAW SRM 57-2-1 AND 57-3-1. 2 L 7 4 4F RT 4A25 1998050801338 19980508 01338 WP 1998 5 8 UPS98826550 1 19980423 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, LT WING L/E RIB CRACKED JUST ABOVE PNEUMATIC DUCT AT STA XOLDI 6.225. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998050801339 19980508 01339 WP 1998 5 8 UPS98826551 1 19980420 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING UPPER SURFACE AT STA XRS 74.5 AND STR 12 THE EXTERIOR SKIN IS CRACKED. REPAIRED IAW SRM 57-2 -1. 2 L 7 4 4F RT 4A25 1998050801340 19980508 01340 WP 1998 5 8 UPS98826552 1 19980422 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, LT WING UPPER SKIN CRACKED JUST I/B OF STA XRS 74 STR 11. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998050801341 19980508 01341 WP 1998 5 8 UPS98826553 1 19980423 A 5320 3750257503N SPLICE DOUG DC8 DC871F 302199D WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FS 1040 TO 1060 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998050801342 19980508 01342 WP 1998 5 8 UPS98826554 1 19980423 A 5320 37799191 SPLICE DOUG DC8 DC871F 302199D WP BS 1340-1360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FS 1340 TO 1360 STR 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998050801343 19980508 01343 NM 1998 5 8 98FDEA00326 1 19980505 A 3260 2314143 SWITCH BOEING 727 72725C 138400H NM LT MLG DOOR INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 116FE 19298 AFTER TAKEOFF FOLLOWING GEAR RETRACTION, LEFT MAIN GEAR DOOR LIGHT AND RED DOORS LIGHT REMAINED ILLUMINATED. RECYCLED G EAR SAME RESULTS. *S/D* REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR WARNING SWITCH. OPERATIONAL CHECK OF LEFT MA IN LANDING GEAR DOOR WARNING SYSTEM IS GOOD. REFERENCE MAINTENANCE MANUAL 32-62-11. 2 L 7 3 4F A3WE 1998050801344 19980508 01344 NM 1998 5 8 98FDEA00327 1 19980505 A 2781 INDICATION BOEING 727 72727C 138400J NM NR 7 LE FLAP MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 145FE 19109 AFTER TAKEOFF WITH FLAPS SELECTED UP THE YELLOW LEADING EDGE FLAP INDICATOR STAYED ON WITH CORRESPONDING NR 7 SLAT INTRA NSIT LIGHT ON THE SECOND OFFICERS'S AUXILIARY PANEL. CYCLED THE FLAP PER CHECKLIST, LIGHTS STAYED ON AS STATED ABOVE. R ETURNED TO DEPARTURE FIELD WITH OUT INCIDENT. *S/D* FOUND PROBLEM WITH NR 7 SLAT TO BE AN INDICATION PROBLEM. REMOVED AND REPLACED NR 7 SLAT ACTUATOR AS PER MAINTENANCE MANUAL 37-81-32. OPERATIONAL CHECK NORMAL, LEAK CHECK NORMAL. 2 L 7 3 4F A3WE 1998050801346 19980508 01346 NM 1998 5 8 98UAL900159 1 19980425 A 2750 285N001140 FSEU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 FAILED A UALA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 WP 29 545UA 25323 FLAPS WOULD NOT MOVE PAST 20 DEGREES. DIVERTED TO LAX. *S/D* FOUND FAULTY NR 1 FSEU. REPLACED FSEU, OPERATIONALLY CH ECKED AND FOUND SYSTEM NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998050801347 19980508 01347 NM 1998 5 8 98UAL900160 1 19980420 A 2710 POWER CONT UNIT BENDIX 31701207 BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE LT AILERON FAILED A A UALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 29 153UA 7070251 20102 DURING OPERATIONAL CHECK OF AILERON CONTROL SYSTEM, LT INBOARD AILERON POWER CONTROL PACKAGE STARTED GUSHING HYDRAULIC F LUID. UPON EXAMINATION OF PCP AFTER REMOVAL, FOUND INNER ACTUATOR ROD SHEARED AT FORWARD END. AIRCRAFT WAS IN UAL-OMB MAINTENANCE FACILITY FOR C-CHECK WHEN THIS DISCREPANCY OCCURRED. LT INBOARD AILERON PCP REPLACED WITH SERVICEABLE UNIT, OPERATIONAL CHECK OK. 2 L 7 4 4F 4 F A20WE E20EA 1998050801348 19980508 01348 NE 1998 5 8 98UAL900161 2 19980423 A 7200 ENGINE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 MALFUNCTIONED A UALA E ENGINE SHUTDOWN E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 381UA 24656 SHUT DOWN THE NUMBER ONE ENGINE WHILE TURNING BASE LEG INTO SMF DUE TO ENGINE VIBRATION AND OIL QUANTITY DIMINISHING. 2 L 7 2 4F 4 F RT A16WE E2GL 1998050801349 19980508 01349 NM 1998 5 8 98UAL900162 1 19980425 A 2131 CONTROLLER HAMILTON STA 7638101 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 928UA 89104571 26651 CABIN PRESSURE WAS UNCONTROLLABLE DURING CLIMB OUT IN BOTH AUTO AND STANDBY. *S/D* AFTER RECYCLING THE PACKS, PRESSURI ZATION OPERATES PROPERLY. ALL DOOR SEALS WERE CHECKED AND FOUND TO BE OK. REPLACED THE CABIN PRESSURE CONTROLLER. 2 L 7 2 4F 4 F RT A16WE E2GL 1998050801350 19980508 01350 NM 1998 5 8 98UAL900163 1 19980426 A 2121 215201 FAN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7258U 21405 RETURNED TO DEN DUE TO ELECTICAL FUMES IN COCKPIT. *S/D* REPLACED GASPER FAN. 2 L 7 3 4F 4 F A3WE E2EA 1998050801352 19980508 01352 WP 1998 5 8 98UAL900165 1 19980427 A 3397 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1836U 47968 EEL LIGHTS AT 19-20H INOP. POWER FEED TO EEL 20H. REPLACED, CHECKS OK. 2 L 7 3 4F 4 F A22WE E23EA 1998050801353 19980508 01353 NE 1998 5 8 98UAL900166 2 19980427 A 7230 COMPRESSOR PRATT & WHIT 782276 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION TO TAKEOFF 1 WP 29 7277U DT8877 21424 JUST AFTER ROTATION FLIGHT ENCOUNTERED LOUD BANG AND VIBRATION FROM THE REAR OF AIRCRAFT. SHUT DOWN NR 3 ENGINE. DUMPE D FUEL AND RETURNED TO MIA. *S/D* ENGINE DISASSEMBLY REVEALED FIVE SECOND STAGE NOZZLE GUIDE VANES BURNED THROUGH AND SUBSEQUENT DOWNSTREAM DAMAGE. THE FAILURE WAS CONTAINED. THE T2 NGV BURN THROUGH WAS CAUSED BY A LEAKING NR 8 FUEL NOZ ZLE WHICH WAS SEVERELY DETERIORATED. THE NOZZLE PASSED A SUBSEQUENT FLOW CHECK. THE NOZZLE IS UNDER INVESTIGATION TO D ETERMINE THE ROOT CAUSE OF THE LEAK. 2 L 7 3 4F 4 F A3WE E2EA 1998050801354 19980508 01354 NM 1998 5 8 98UAL900167 1 19980428 A 4920 APU BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE APU COMPT SMOKING A UALA C D ABORTED TAKEOFF RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 WP 29 983UA 21641 ABORTED TAKEOFF DUE TO SMOKE COMING OUT OF THE APU. LOW OIL PRESSURE LIGHT WAS ON. 2 L 7 2 4F 4 F A16WE E2EA 1998050801355 19980508 01355 NM 1998 5 8 98UAL900168 1 19980430 A 3350 900535A BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7457U 21911 CARGO DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY CARTRIDGE. 2 L 7 3 4F 4 F A3WE E2EA 1998050801356 19980508 01356 NM 1998 5 8 98UAL900169 1 19980430 A 2613 OVERHEAT LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING/BODY ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 302UA 23643 LEFT WING BODY OVERHEAT LIGHT WAS ILLUMINATED AND REMAINED ON AFTER THE DUCT WAS DEPRESSURIZED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998050801357 19980508 01357 NM 1998 5 8 98UAL900170 1 19980429 A 3320 5521081 BULB BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAILED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 774UA 26936 READING LIGHTS AT 28AB WOULD NOT TURN OFF, SMOKE EMITTED FROM PASSENGER SERVICE UNIT PANEL. POWER TURNED OFF FROM CACP. *S/D* BOTH LAMPS WERE REMOVED AND REPLACED. AREA WAS INSPECTED FOR SIGNS OF OVERHEAT OR BURNING, NONE FOUND. ALL OP ERATIONS RETURNED TO NORMAL AFTER LAMP REPLACEMENT. THERE HAVE BEEN NO REOCCURRENCES OF THIS ANOMALY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998050801358 19980508 01358 WP 1998 5 8 MWEA98566 1 19980504 A 5720 99116033N TEE DOUG DC9 DC915 3022036 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FOUND CRACK ON LEFT WING LOWER TEE OUTBOARD LOWER LEG AT STATION 58. MTC REMOVED AND REPLACED TEE. 2 L 7 2 4F A6WE 1998050801359 19980508 01359 WP 1998 5 8 MWEA98567 1 19980504 A 5720 S261321212000 ANGLE DOUG DC9 DC915 3022036 WP LT WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FOUND A 2 INCH CRACK AND CORROSION ON LEFT HAND WING BETWEEN XRS 69 AND 91 AT STRINGER 11. MTC FABRICATED AND INSTALLED REPAIR SPLICE ANGLES. 2 L 7 2 4F A6WE 1998050801360 19980508 01360 WP 1998 5 8 MWEA98568 1 19980504 A 5720 4912009AN CLIP DOUG DC9 DC915 3022036 WP WS 69 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 REMOVED CLIP FROM LEFT HAND WING AT STATION 69 STRINGER 11 TO FACILITATE OTHER MAINTENANCE. MTC FABRICATED AND INSTALLE D STRINGER CLIP. 2 L 7 2 4F A6WE 1998050801361 19980508 01361 WP 1998 5 8 MWEA98569 1 19980504 A 5320 DOUBLER DOUG DC9 DC915 3022036 WP BS 256 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 REMOVED TCAS ANTENNA AND DOUBLER STATION 256 FRAME SHEAR CLIP FASTENERS IN SKIN LAP AT STATION 229, L27 LEFTHAND TO L28 RIGHT HAND TO FACILITATE OTHER MAINTENANCE. MTC REINSTALLED ANTENNA DOUBLER AND SHEAR CLIP. 2 L 7 2 4F A6WE 1998050801362 19980508 01362 WP 1998 5 8 MWEA98570 1 19980504 A 5720 4912005501N CLIP DOUG DC9 DC915 3022036 WP WS 111 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 FOUND CRACKED LEFT WING RIB 111 MOST AFT LOWER SHEAR CLIP. MTC FABRICATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 1998050801363 19980508 01363 WP 1998 5 8 MWEA98571 1 19980502 A 5312 995789923 BULKHEAD TEE DOUG DC9 DC914 3022034 WP BS 69 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND CRACK ON FORWARD ACCESSORY COMPARTMENT T-ANGLE AT FS 69 BULKHEAD LEFT SIDE STATION X=10. MTC FABRICATED AND INSTA LLED NEW T-ANGLE. 2 L 7 2 4F A6WE 1998050801364 19980508 01364 WP 1998 5 8 MWEA98572 1 19980503 A 5532 591216612 SKIN DOUG DC9 DC914 3022034 WP TAIL SECTION CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND HEAVY CHAFING ON VERTICAL STABILIZER CANOE FAIRING AFT RIGHT HAND SKIN. MTC REMOVED AND REPLACED FAIRING SKIN. 2 L 7 2 4F A6WE 1998050801365 19980508 01365 WP 1998 5 8 MWEA98573 1 19980503 A 5532 591216611 SKIN DOUG DC9 DC914 3022034 WP TAIL SECTION CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND HEAVY CHAFING ON VERTICAL STABILIZER CANOE FAIRING AFT LEFT HAND SKIN. MTC REMOVED AND REPLACED FAIRING SKIN. 2 L 7 2 4F A6WE 1998050801366 19980508 01366 WP 1998 5 8 MWEA98574 1 19980503 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP FWD GALLEY SLIDE FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 209ME 47730 THE GALLEY DOOR SLIDE COVER FELL OFF. MTC REINSTALLED COVER. 2 L 7 2 4F A6WE 1998050801367 19980508 01367 WP 1998 5 8 MWEA98575 1 19980428 A 5532 591216612N SKIN DOUG DC9 DC932 3022066 WP TAIL SECTION GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FOUND A DEEP GOUGE IN RIGHT SIDE VERTICAL STABILIZER UPPER AFT CANOE SKIN. MTC FABRICATED AND INSTALLED SKIN. 2 L 7 2 4F A6WE 1998050801368 19980508 01368 WP 1998 5 8 MWEA98576 1 19980428 A 5510 591801539 TIP DOUG DC9 DC932 3022066 WP LT HORIZ STAB ERODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FOUND A HOLE ERODED IN THE LEFT HORIZONTAL STABILIZER LEADING EDGE TIP. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998050801369 19980508 01369 NM 1998 5 8 VNAA9804026 1 19980429 A 3251 2304000001 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 458PS 55568 7958 3068 DURING THE TAXI FOR TAKEOFF, A NOSE WHEEL STEERING FAIL WARNING MESSAGE OCCURRED. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND REPLACED THE HYDRAULIC STEERING CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32- 51-01. OPERATION AND LEAK CHECKS WERE COMPLIED WITH, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998050801412 19980508 01412 NM 1998 5 8 CA980128005 1 19980108 A 3150 10613302 LIGHT ASSEMBLY BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE RT CAUTION DEFECTIVE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 674383 (CAN) AFTER TAKEOFF,RIGHT HAND MASTER CAUTION LIGHT WOULD NOT CANCEL. AIR TURNBACK. OVERWEIGHT LANDING. MASTER CAUTION LIGHT REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998050801413 19980508 01413 EU 1998 5 8 CA980407009 2 19980202 A 7250 BLADE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU ENG TURBINE SHIFT W K NONE O OTHER IN INSP/MAINT 1 CA 17666 3155 18129 (CAN) FIRST START OF THE DAY WAS ABORTED DUE TO ABNORMAL VIBRATION NOTED ON START. INSPECTION OF THE ENGINE (FROM AFT) INDICATED TURBINE SHIFT/FAILURE. ONE HP TURBINE BLADE WAS DISPLACED. ENGINE REMOVED ON SITE AND FORWARDED FOR REPAIR. P ART TC: 18,011. 2 L 7 2 3T 4 T A24EU A196 1998050801415 19980508 01415 NE 1998 5 8 CA980415010 2 19980409 A 7200 ENGINE BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NR 2 FAILED W A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CA 709479B (CAN) ON CLIMB, NR 2 ENGINE FAILED. AIRCRAFT RETURNED TO RAMP. ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. ENGI NEERING REPORT TO FOLLOW. 2 L 7 2 4F 4 F A16WE E2EA 1998050801417 19980508 01417 SW 1998 5 8 CA980421009 1 19980417 A 5711 SPAR WEB SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP WING CENTER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 26289 P54143 (CAN) FAIRCHILD RECENTLY REVISED ITS AIRFRAME INSPECTION MANUAL TO INCLUDE A DETAILED INSPECTION OF THE WING CENTER SPAR INNER WEB. INSPECTION FOUND CRACKING ON THREE DIFFERENT AIRCRAFT. PART TC: 39,582. ACFT TT: 25,974 HOURS. 2 L 7 2 4T 4 T RT A8SW E4WE 1998050801418 19980508 01418 WP 1998 5 8 CALA9800769 1 19980505 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 CRACK (2) ON LOWER ANGLE OF LONGERON AT AFT LEFT GEAR WHEEL WELL. REMOVED ANGLE, FABRICATED NEW ANGLE, TREATED, PAINTED , AND INSTALLED PER SRM 53-53-1 FIG 4, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998050801419 19980508 01419 WP 1998 5 8 CALA9800770 1 19980505 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 CRACK (2) ON SUPPORT ANGLE OF AFT SIDE FITTING (AFT LONGERON) AT RIGHT MAIN LANDING GEAR WHEEL WELL. REMOVED CRACKED AN GLE, FABRICATED, TREATED, PRIMED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998050801420 19980508 01420 WP 1998 5 8 CALA9800771 1 19980505 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 CRACK (2) IN VERTICAL ANGLE LEFT MLG WHEEL WELL AFT BULKHEAD. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PAINTED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00 AND 51-31-01. 2 L 7 3 4F A22WE 1998050801421 19980508 01421 WP 1998 5 8 CALA9800772 1 19980505 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP RT MAIN WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 CRACK ON VERTICAL ANGLE OF RIGHT MAIN L/G WHEEL WELL AFT BULKHEAD. REMOVED CRACKED ANGLE, FABRICATED, TREATED, PAINTED, AND INSTALLED NEW ANGLE PER SRM 53-53-01, 51-20-00 AND 51-31-01. 2 L 7 3 4F A22WE 1998050801422 19980508 01422 WP 1998 5 8 CALA9800773 1 19980505 A 5320 S2922883 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1921 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 FLOOR SUPPORT CRACKED (2) UNDER AFT GALLEY STA 1921 LBL 20 RBL 20. REMOVED CRACKED SUPPORT SECTION. FITTED NEW SECTION PER SRM 51-20-00 AND 51-35-01. 2 L 7 3 4F A22WE 1998050801423 19980508 01423 WP 1998 5 8 CALA9800774 1 19980505 A 5754 RIB DOUG DC10 DC1010 3022110 WP NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 FOUND CRACK (2) IN SLAT NUMBER 1 RT. CRACKED RIB REMOVED, INSTALLED NEW RIB ARB1566-502 AS ORIGINAL PER SRM 51-31-01. 2 L 7 3 4F A22WE 1998050801424 19980508 01424 WP 1998 5 8 CALA9800775 1 19980505 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1884-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 SUPPORT UNDER AFT GALLEY CORRODED STA 1884 TO 2007 RBL 24. REMOVED CORRODED PARTS, FABRICATED NEW PART, TREATED AND INS TALLED PER SRM 53-16-01, 53-60-01, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998050801425 19980508 01425 WP 1998 5 8 CALA9800776 1 19980505 A 5720 FASTENER DOUG DC10 DC1030 3023501 WP WS 402 FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 RIVET HEAD POPPED ON LEFT WING LOWER SKIN FWD OF REAR SPAR WING STA XORS402, JUST OUTBOARD OF SAILBOAT PANEL. REMOVED A ND REPLACED FASTENER PER SRM 51-33-01. 2 L 7 3 4F A22WE 1998050801426 19980508 01426 WP 1998 5 8 CALA9800777 1 19980505 A 2121 605457 RECIRC FAN DOUG DC10 DC1030 3023501 WP CABIN FAILED A CALA A B J UNSCHED LANDING EMER. DESCENT DUMP FUEL B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 17085 47957 A/C DIVERTED TO MAD FROM FCO DUE TO ELECTRIC SMELL IN CABIN. FOUND NR 4 CABIN AIR RECIRCULATION FAN FAILED. FAN TO BE REPLACED. 2 L 7 3 4F A22WE 1998050801427 19980508 01427 NM 1998 5 8 CALA9800778 1 19980505 A 5512 ACCESS PANEL BOEING 727 727224 1384076 NM LT HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LT LOWER HORIZ STAB BAL BAY ACCESS PANEL CORRODED. CUT OUT CORRODED AND DELAMINATED AREA, FABRICATED DOUBLER AND BONDED TO CUT OUT AREA PER SRM 55-20-3 AND 51-40-5. 2 L 7 3 4F A3WE 1998050801428 19980508 01428 NM 1998 5 8 CALA9800779 1 19980505 A 5350 FAIRING BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LOWER SKIN FAIRING AT STA 950 IS CORRODED BEYOND LIMITS. FABRICATED, TREATED, PRIMED, AND INSTALLED NEW LOWER SKIN FAIR ING PER SRM 51-40-2, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050801429 19980508 01429 NM 1998 5 8 CALA9800780 1 19980505 A 5330 PANEL BOEING 727 727224 1384076 NM BS 950-970 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 TRANSITION PANEL AFT PIT STA 950 TO 970 LT SIDE CORRODED ON UNDER SIDE OF PANEL. REMOVED CORRODED AREAS, FABRICATED AND INSTALLED REPAIR DOUBLERS PER SRM 51-10-6, 53-10-1, 51-4-0-2, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050801430 19980508 01430 NM 1998 5 8 CALA9800781 1 19980505 A 5260 STEP BOEING 727 727224 1384076 NM AFT AIRSTAIRS CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT AIRSTAIRS NR 8 STEP PANEL CORRODED. REMOVED CORRODED AREA, FABRICATED, TREATED AND INSTALLED REPAIR SECTION PER SRM 51-40-2, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050801431 19980508 01431 NM 1998 5 8 CALA9800782 1 19980505 A 5330 PANEL BOEING 727 727224 1384076 NM BS 580-620 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 FORWARD PIT LT TRANSITION PANEL STA 620 TO 580 HAS CORROSION. FABRICATED, TREATED, PRIMED AND INSTALLED REPAIR PER SRM 51-40-2, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998050801432 19980508 01432 NM 1998 5 8 CALA9800783 1 19980505 A 5343 TRUNNION BOEING 727 727224 1384076 NM LT MLG GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LEFT MAIN LANDING GEAR FORWARD TRUNNION FITTING O/B SIDE OF FITTING BOTH UPPER AND LOWER BUSHING ARE GOUGED. REAMED HOL E AND FABRICATED 2 BUSHINGS PER BOHM 32-10-13 FIGURE 3. 2 L 7 3 4F A3WE 1998050801433 19980508 01433 NM 1998 5 8 CALA9800784 1 19980505 A 5343 TRUNNION BOEING 727 727224 1384076 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LEFT MLG FORWARD TRUNNION FITTING HAS CORROSION AROUND BOTH LOWER BUSHINGS INNER SIDES AND I/B SIDE OF FITTING UPPER BUS SING INNER SIDE. REAMED HOLES AND FABRICATED TWO BUSHINGS PER BOHM 32-10-13. 2 L 7 3 4F A3WE 1998050801434 19980508 01434 NM 1998 5 8 CALA9800785 1 19980505 A 5343 TRUNNION BOEING 727 727224 1384076 NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 RIGHT MLG FORWARD TRUNNION ATTACH FITTING AIRCRAFT SIDE HAS CORROSION ON INNER FACE OF BOTH I/B AND O/B ATTACH FITTINGS AROUND BUSHINGS BOTH UPPER AND LOWER HOLES. REMOVED CORROSION, REAMED HOLES, FABRICATED AND INSTALLED BUSHINGS PER BOHM 32-10-13 AND BSOP 20-10-3. 2 L 7 3 4F A3WE 1998050801435 19980508 01435 WP 1998 5 8 CALA9800786 1 19980505 A 3397 WIRE DOUG DC10 DC1010 3022110 WP CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68047 47801 EMERGENCY FLOOR ILLUMINATION LIGHTS INOP ROWS 29 TO 35 LEFT AND RIGHT AISLES. FOUND WIRES UNDER SEAT 30B SHORTED. REPA IRED WIRING AND REPLACED BATTERY FUSE. 2 L 7 3 4F A22WE 1998050801436 19980508 01436 WP 1998 5 8 CALA9800787 1 19980506 A 2620 8762962 CARTRIDGE DOUG DC10 DC1030 3023501 WP NR 1 ENGINE OPEN CIRCUIT A CALA O OTHER L NO TEST IN INSP/MAINT 1 SW 09 13067 47866 NUMBER 1 ENGINE FIRE BOTTLE AGENT ONE FILAMENT A NOT LIGHTING ON TEST BOX DURING TEST. CARTRIDGE FOUND U/S. INSTALLED NEW CARTRIDGE. 2 L 7 3 4F A22WE 1998050801437 19980508 01437 WP 1998 5 8 CALA9800788 1 19980506 A 2621 FIRE BOTTLE DOUG DC10 DC1030 3023501 WP NR 2 ENGINE DAMAGED A CALA O OTHER L NO TEST IN INSP/MAINT 1 SW 09 13067 47866 NUMBER 2 ENGINE AND APU FIRE BOTTLE LOW PRESSURE CONNECTOR P1-1264 SOCKET B FOUND PUSHED BACK. ELECTRICAL CONNECTOR REP LACED PER MM 20-00-00. 2 L 7 3 4F A22WE 1998050801438 19980508 01438 WP 1998 5 8 CALA9800789 1 19980506 A 2621 WIRE DOUG DC10 DC1030 3023501 WP NR 2 FIRE BOTTLE BROKEN A CALA O OTHER L NO TEST IN INSP/MAINT 1 SW 09 13067 47866 CARGO FIRE BOTTLE NR 2 LOW PRESSURE SWITCH ELECTRICAL CONNECTOR WIRE FOUND BROKEN. WIRE W277B24 FOUND BROKEN AT PIN B O F CONECTOR P1-2189. NEW PIN FITTED AND TESTED. 2 L 7 3 4F A22WE 1998050801439 19980508 01439 NM 1998 5 8 CALA9800790 1 19980506 A 5330 SKIN BOEING 737 737291 138448W NM BS 787 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 LOWER RIGHT SIDE AFT FUSELAGE AT BS 787 STR R26 DENTED FORWARD OF AFT CARGO DOOR CUTOUT. REMOVED DAMAGED AREA. INSTALL ED REPAIR PER SRM 53-30-1, 51-00-00, 53-30-1, 51-10-2, 53-30-3 AND MM 25-52-1. 2 L 7 2 4F A16WE 1998050801440 19980508 01440 NM 1998 5 8 CALA9800791 1 19980505 A 5330 6551624 SKIN BOEING 737 7373T0 1384582 NM BS 867 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 23588 DENT 64 OF AFT CARGO DOOR. CUT OUT DAMAGED SKIN, PERFORMED HFEC PER SRM 53-00-01. INSTALLED REPAIR PER SRM 53-00-01. 2 L 7 2 4F RT A16WE 1998050801441 19980508 01441 WP 1998 5 8 CALA9800792 1 19980505 A 5350 3913359545 CABLE DOUG DC9 DC982 3022082 WP TAIL CONE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 FORCE REQUIRED TO RELEASE TAIL CONE TO HIGH. REPLACED CABLE, RIGGED TAIL CONE PER MM 53-53-00 AND FUNCTIONAL CHECKED. 2 L 7 2 4F A6WE 1998050801442 19980508 01442 WP 1998 5 8 CALA9800793 1 19980505 A 5350 RIGGING DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF RIG A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 FORCE REQUIRED TO PULL INTERIOR TAIL CONE RELEASE HANDLE IS TO LOW. RIGGED HANDLE PER MM 53-53-00. 2 L 7 2 4F A6WE 1998050801443 19980508 01443 WP 1998 5 8 CALA9800794 1 19980506 A 5210 9915565159 ANGLE DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 AFT ENTRY DOOR NR 3 BEAM 1.5 INCH CRACK IN RADIUS OF ATTACH ANGLE NEAR HINGE SIDE OF DOOR. FABRICATED NEW ANGLE AND INS TALLED PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998050801444 19980508 01444 WP 1998 5 8 CALA9800795 1 19980506 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 146.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CORROSION ON LOWER SUPPORT ANGLE ON LOWER RIGHT COCKPIT SIDEWALL AFT AT STA 146.5 RT. FABRICATED NEW ANGLE AND INSTALLE D PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998050801445 19980508 01445 WP 1998 5 8 CALA9800796 1 19980506 A 5753 CASTING DOUG DC9 DC982 3022082 WP NR 3 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 LEFT WING NR 3 FLAP HINGE TOP I/B BOLT HOLE CORRODED. OPENED HOLE TO .596 TO CLEAN UP CORROSION PER OHM. 2 L 7 2 4F A6WE 1998050801446 19980508 01446 WP 1998 5 8 CALA9800797 1 19980506 A 5320 CHANNEL DOUG DC9 DC982 3022082 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 CORRODED J-CHANNEL FORWARD ENTRY FLOOR STA 180 LBL 55. REPLACED CHANNEL PER SRM 51-30-0. 2 L 7 2 4F A6WE 1998050801447 19980508 01447 WP 1998 5 8 9808279881 1 19980504 A 5610 WINDSHIELD DOUG DC9 DC951 3022051 WP LT COCKPIT CRACKED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 676MC 47652 DURING CLIMB THROUGH FL250, 280 KIAS, CAPTAIN'S WINDSHIELD OUTER PANE CRACKED. FLIGHT RETURNED TO DTW AND LANDED WITHOU T FURTHER INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD. 2 L 7 2 4F RT A6WE 1998050801448 19980508 01448 WP 1998 5 8 9808289872 1 19980501 A 5210 MECHANISM DOUG DC9 DC951 3022051 WP PAX DOOR OUT OF ADJUST A NWAA K NONE O OTHER UK UNKNOWN 1 GL 01 781NC 48121 UPON ARRIVAL AT GATE, THE GATE AGENT WAS UNABLE TO OPEN THE MAIN CABIN DOOR. RIGGED MAIN CABIN DOOR, FUNCTIONAL CHECK O K. 2 L 7 2 4F RT A6WE 1998050801449 19980508 01449 WP 1998 5 8 9808299933 1 19980501 A 5350 RELEASE MECH DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING TAIL CONE FUNCTION CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO DEPLOY TAIL CONE USING THE INTERIOR HANDLE. RIGGED TAIL CONE DEPLOYMENT SYSTEM, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998050801450 19980508 01450 WP 1998 5 8 9808309874 1 19980505 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 783NC 48108 DURING LINE CHECK, FOUND EMERGENCY LIGHTING IN TAIL COMPARTMENT VERY DIM. MAINTENANCE REPLACED BATTERIES, OPERATIONAL C HECK NORMAL. 2 L 7 2 4F RT A6WE 1998050801451 19980508 01451 WP 1998 5 8 9808319859 1 19980505 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 768NC 47729 DURING LINE CHECK, FOUND EMERGENCY EXIT LIGHTING INOPERATIVE IN TAIL CONE CATWALK SECTION. MAINTENANCE REPLACED THE BAT TERY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998050801452 19980508 01452 WP 1998 5 8 9808329302 1 19980505 A 3350 POWER PACK DOUG DC9 DC982 3022082 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 302RC 48055 DURING LINE CHECK, FOUND AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE TIGHTENED LOOSE LUG ON POWER PACK, OPERA TIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998050801453 19980508 01453 WP 1998 5 8 9808339106 1 19980505 A 3350 BATTERY DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 96S 47206 DURING LINE CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F A6WE 1998050801454 19980508 01454 WP 1998 5 8 UPS98826557 1 19980422 A 5720 5642970161 GUSSET DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT FLAP AT SPLIT UNDER SURFBOARD LWR RIB SUPPORT GUSSET IS CRACKED. REMOVED, FABRICATED AND INSTALLE D REPLACEMENT GUSSET IAW SRM 51-1-21 AND DWG 5642970. 2 L 7 4 4F RT 4A25 1998050801455 19980508 01455 WP 1998 5 8 UPS98826558 1 19980423 A 5320 975377623F FITTING DOUG DC8 DC871F 302199D WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FS 1180 AT STR 27L DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLAC EMENT FITTING IAW SRM 51-1-20D AND DWG 9753776. 2 L 7 4 4F RT 4A25 1998050801456 19980508 01456 WP 1998 5 8 UPS98826559 1 19980423 A 5320 37558541 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FS 1200 AT STR 27L DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLAC EMENT FITTING IAW SRM 51-1-20D AND DWG 3753776. 2 L 7 4 4F RT 4A25 1998050801457 19980508 01457 WP 1998 5 8 UPS98826560 1 19980422 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING L/E SKIN ON TOP AT STA XOLDI 6.225 HAS 2 CRACKS AROUND RIVETS 8 FWD OF FRONT SPAR. REPAIRED IAW SRM ADDN DC8-5720-4087. 2 L 7 4 4F RT 4A25 1998050801458 19980508 01458 WP 1998 5 8 UPS98826563 1 19980428 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT L/E BETWEEN ENG NR 3 AND NR 4 HAS CRACKED RIB AFT OF O/B SLOT ACTUATOR BOTTOM SIDE. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998050801459 19980508 01459 WP 1998 5 8 UPS98826564 1 19980423 A 5712 RIB DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, LT WING T/E RIB CRACKED AT NR 5 SPOILER NR 2 HINGE, (INBD RIB). REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998050801460 19980508 01460 WP 1998 5 8 UPS98826565 1 19980422 A 5712 RIB DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING T/E AT FLAP STA 3.00 THE I/B RIB IS CRACKED AT MID SPAN. REPAIRED IAW SRM ADDN DC8-5720-6998 . 2 L 7 4 4F RT 4A25 1998050801461 19980508 01461 WP 1998 5 8 UPS98826567 1 19980422 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 747.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING L/E AT STA XFS 747.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998050801462 19980508 01462 WP 1998 5 8 UPS98826568 1 19980423 A 5347 5759223537 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 1320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FS 1320 ABOVE STR 33L CARGO TRACK HAS HEAVY CORROSION AND IS CRACKED AT FS 1260. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0 AND DWG 5759223. 2 L 7 4 4F RT 4A25 1998050801463 19980508 01463 WP 1998 5 8 UPS98826569 1 19980423 A 5320 3755847502 FITTING DOUG DC8 DC871F 302199D WP BS 1225 S CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, FS 1225 BTWN STR 30R TO 33R SHEAR TIE FITTING IS CRACKED IN 2 PLCS. REMOVED, FABRICATED AND INSTALLE D REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3755847. 2 L 7 4 4F RT 4A25 1998050801464 19980508 01464 WP 1998 5 8 UPS98826571 1 19980420 A 5330 SKIN DOUG DC8 DC871F 302199D WP WS 193-250 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 730UP 46030 INSPECTION TYPE-C, RT WING L/E STUB WING OVER NR 3 PYLON ON TOP HAS MANY CRACKS DUE TO CORROSION FROM STA XFS 193.00 TO 250.089. REPAIRED IAW SRM ADDN DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 1998050801465 19980508 01465 NM 1998 5 8 98FDEA00328 1 19980430 A 5711 SPAR CHORD BOEING 727 727225 1384077 NM WS 207 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 CORROSION ON RT WING REAR SPAR LOWER CHORD, WS 207. CORROSION WAS REMOVED AREA APPROX 7 WIDE, HEIGHT .625, .25 DEPTH. R EPAIRED PER SRM 57-10-6, FIG 2, SHEET 4 AREA WAS NOT CHECKED AND NO CRACKS FOUND. 2 L 7 3 4F A3WE 1998050801466 19980508 01466 NM 1998 5 8 98FDEA00329 1 19980501 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 520 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 CRACK IN STRINGER 24L STATION 520. REPAIRED STRINGER PER SRM 53-10-3 AT STR 24L BS 520. 2 L 7 3 4F A3WE 1998050801467 19980508 01467 NM 1998 5 8 98FDEA00330 1 19980501 A 5311 BELLFRAME BOEING 727 727225 1384077 NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 LWR FWD CARGO, DENT IN BELLFRAME BS 520, STR 23L TO 24L WEB DEFORMED. REPAIRED BELLFRAME AT BS 520, STR 23L TO 24L PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998050801468 19980508 01468 WP 1998 5 8 ABXA9800444 1 19980428 A 5610 5613217507 WINDOW DOUG DC9 DC933F 302207A WP LT COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 932AX 47465 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED CAPTAIN'S CLEARVIEW WINDOW IAW DC9 MM 56-10-3. 2 L 7 2 4F A6WE 1998050801469 19980508 01469 NM 1998 5 8 DL72K980950 1 19980422 A 5532 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 THREE EACH .125 IN CRACKS IN VERTICAL STABILIZER OUTER SKIN RT SIDE FWD OF PANEL 9501 (MARKED). INSTALLED REPAIR PER M M 54-30-0. 2 L 7 3 4F A3WE 1998050801470 19980508 01470 NM 1998 5 8 DL72K980951 1 19980503 A 5320 DOUBLER BOEING 727 727232 1384082 NM R-1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 DURING ACCOMPLISHMENT OF EO 4-72762-12, A 2.5 IN CRACK WAS FOUND IN THE R-1 DOOR UPPER HINGE CUTOUT INTERNAL DOUBLER. R EPAIR WAS ACCOMPLISHED PER ERA 364679-14. 2 L 7 3 4F A3WE 1998050801471 19980508 01471 NM 1998 5 8 DL72L980953 1 19980504 A 5320 WEB BOEING 727 727232 1384082 NM BS 1235 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 FOUND ON A2 LETTER CK, 1.25 IN CRACK LT LOWER TORQUE BOX WEB AT THE UPPER ROW OF RIVETS STA 1235. REPAIRED PER MM 53-11 -0. 2 L 7 3 4F A3WE 1998050801472 19980508 01472 NM 1998 5 8 DL72S980954 1 19980504 A 2612 FIRE WARNING BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE ACTIVATED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 27 400DA 62771 21144 687678 ON CLIMBOUT 12,000 FT, GOT FIRE WARNING AND FIRE BELL NR 1 ENGINE. DISCHARGED ONE FIRE BOTTLE AND SHUT DOWN ENGINE. RE TURNED TO SLC. ENGINE WINDMILLED 10 MINUTES WITH POSITIVE OIL PRESSURE. T/S IN PROGRESS. 2 L 7 3 4F 4 F A3WE E2EA 1998050801473 19980508 01473 NM 1998 5 8 DL73E980955 1 19980430 A 5330 SKIN BOEING 737 7372S3 NM BS 460 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 369DL 21776 A 1.5 X 1.5 PUNCTURE WAS FOUND IN THE FUSELAGE SKIN JUST AFT OF STA 460 BELOW THE STRINGER 25R SKIN LAP SPLICE. THE PUN CTURE WAS TRIMMED TO A SMOOTH CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND AN ADDITIONAL DOUBLER TO OVERLAP THE SKIN LAP SPLICE. THE REPAIR WAS ACCOMPLISHED PER ER/A 364666-14, REV A. 2 L 7 2 4F RT A16WE 1998050801474 19980508 01474 NM 1998 5 8 DL72K980956 1 19980501 A 5320 STRAP BOEING 727 727232 1384082 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 THE UPPER HINGE CUTOUT OF THE R1 DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE DOOR SURROUND BEAR STRAP. THE CRACK WAS TERMINATED AND REPAIRED WITH AN ALUMINUM EXTERNAL DOUBLER PER BAC S/B 727-53-0136, REV 3, FIGURE 6 AS DOCUME NTED IN ER/A 364679-14. 2 L 7 3 4F A3WE 1998050801475 19980508 01475 NM 1998 5 8 SCNA98500 1 19980423 A 5320 SUPPORT BOEING 727 727225 1384077 NM BS 1118 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 282SC 22558 DURING HEAVY MAINTENANCE, THE MAIN CABIN FLOOR SUPPORT AT STA 1118 LBL 30 CLAMP SUPPORT STIFFENER WAS FOUND CRACKED AT T HE EDGES, 2 EA CRACKS. REMOVED, FABRICATED AND INSTALLED NEW SUPPORT IAW SRM 511002, 512001, 513005 AND 513006. 2 L 7 3 4F A3WE 1998051500001 19980515 00001 WP 1998 5 15 TWAA9806515 1 19980416 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED RIB PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500002 19980515 00002 WP 1998 5 15 TWAA9806514 1 19980416 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 937-965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STA 937 TO STA 965, CABIN FLOORBEAM CAP WITH METAL REMOVED BEYOND LIMITS FOR CORROSION REMOVAL. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, ITEM 6A, AND ARA 10993. ACFT TT: 75 ,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500003 19980515 00003 WP 1998 5 15 TWAA9806513 1 19980421 A 5753 ANGLE DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE FLAP INTERIOR AT IDLER HINGE, INBD ANGLE CRACKED AT TWO PLACES. R EPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500004 19980515 00004 WP 1998 5 15 TWAA9806511 1 19980422 A 5511 SPAR CAP DOUG DC9 DC932 3022066 WP LT HORIZ STAB RUSTY A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT IN FRONT SPAR FOR STABILIZER A TTACHMENT TO CENTER SECTION WAS VERY RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. INSTALLED NEW LT HORIZONTAL STABILIZE R UPPER SPAR CAP. INSTALLED NEW BOLT/BARREL NUT AND RETAINER AND TORQUED PER MM 55-10-02, AND TWA STANDARD PRACT MM 20- 14-00 AD 20-16-00. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500005 19980515 00005 WP 1998 5 15 TWAA9806512 1 19980422 A 5511 SPAR DOUG DC9 DC932 3022066 WP LT HORIZ STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT HOLE IN FRONT SPAR CRACKED BEY OND LIMITS. REPLACED FRONT SPAR PER SRM 51-01 AND ARA 15277. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500006 19980515 00006 WP 1998 5 15 TWAA9806510 1 19980422 A 5712 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT FASTENER IN WING LE RIB ABOVE LE LOWER PANEL 11 13. REMOVED AND REPLACED WITH NEW RIB AND INSTALLED DOUBLER PER SRM 57-01, PG 8, AND SRM 51-01 PG 1 ITEM C. ACFT TT: 7 5,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500007 19980515 00007 WP 1998 5 15 TWAA9806509 1 19980422 A 5712 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LOWER PANEL NR 1112. INSTALLED NEW RIB PER SRM 51-01. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500008 19980515 00008 WP 1998 5 15 TWAA9806508 1 19980422 A 5712 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LE LOWER PA NEL NR 1111. INSTALLED NEW RIB PER SRM 51-01, PG 1. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500009 19980515 00009 WP 1998 5 15 TWAA9806507 1 19980423 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 955U 49427 MCI - DURING OVERNIGHT MAINTENANCE FOUND CRACK MIGRATING OUT OF FASTENER HOLE RT SIDE VERTICAL STABILIZER ATTACH ANGLE, FS 1388. REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE PER SRM 51-10-0 AND TWA STD PRACTICES. CHECK-C 2-9-98 STL. ACF T TT: 33,526 HOURS. ACFT TC: 16,902. (X) 2 L 7 2 4F A6WE 1998051500010 19980515 00010 WP 1998 5 15 TWAA9806506 1 19980423 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 955U 49427 MCI - DURING OVERNIGHT MAINTENANCE, FOUND LOWER ATTACH ANGLE FOR WRAP AROUND FAIRING AT VERTICAL STABILIZER CRACKED THRO UGH FASTENER HOLE, 7 IN FORWARD OF PRODUCTION BREAK, LT SIDE FS 1421. REMOVED ATTACH ANGLE AND INSTALLED NEW ATTACH ANG LE PER SRM 51-10-0 AND TWA STD PRACTICES. CHECK-C 2-9-98 STL. ACFT TT: 33,526 HOURS. ACFT TC: 16,902. (X) 2 L 7 2 4F A6WE 1998051500011 19980515 00011 WP 1998 5 15 TWAA9806505 1 19980423 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERTICAL STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 955U 49427 MCI - DURING OVERNIGHT MAINTENANCE, FOUND LOWER ATTACH ANGLE FOR WRAP AROUND FAIRING AT VERTICAL STABILIZER CRACKED THRO UGH FASTENER HOLE, 7 IN FORWARD OF PRODUCTION BREAK, RT SIDE FS 1421. REMOVED CRACKED ANGLE, INSTALLED NEW ANGLE PER SR M 51-10-0, AND TWA STD PRACTICES. CHECK-C 2-9-98 STL. ACFT TT: 33,526 HOURS. ACFT TC: 16,902. (X) 2 L 7 2 4F A6WE 1998051500012 19980515 00012 WP 1998 5 15 TWAA9806504 1 19980410 A 5320 DOUBLER DOUG DC9 DC933F 302207A WP BS 937 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT FACE OF FORMER DOUBLER AT FS 937 CORRODED ABOVE L28L TO 29L. REMOVED CO RROSION PER SRM 51-10-3. INSTALLED NEW DOUBLER PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500013 19980515 00013 WP 1998 5 15 TWAA9806503 1 19980407 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON AFT FACE OF FORMER FS 965 BETWEEN LONGERONS 29L AND 29R. REMOV ED CORROSION AND REPAIRED PER SRM 53-03, PG 4. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500014 19980515 00014 WP 1998 5 15 TWAA9806502 1 19980325 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 570-617 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK FOUND CORROSION BEYOND LIMITS IN CHAIR TRACK AT STA 570 TO STA 617, LBL 45 IN. REM OVED AND REPLACED SEAT TRACK AT STA 570 TO STA 617, LBL 45 IN, PER SRM 53-05, PG 10G. ACFT TT: 75,041 HOURS. ACFT TC : 81,086. (X) 2 L 7 2 4F A6WE 1998051500015 19980515 00015 WP 1998 5 15 TWAA9806501 1 19980318 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 237-256 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 924TW 49100 MCI - DURING CHECK-C, MAINTENANCE FOUND NR 1 CHAIR TRACK CORRODED BEYOND LIMITS AT FS 237 TO FS 256. REPLACED CHAIR TRA CK SECTION PER SRM 51-01, PAGE 1. ACFT TT: 38,048 HOURS. ACFT TC: 32,705. (X) 2 L 7 2 4F A6WE 1998051500016 19980515 00016 WP 1998 5 15 TWAA9806416 1 19980421 A 5712 RIB DOUG DC9 DC933F 302207A WP WS 490 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING XRS 490 LE RIB CRACKED. REPLACED RIB PER SRM 51-01, PG 1 ITEM C. A CFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500017 19980515 00017 WP 1998 5 15 TWAA9806415 1 19980421 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 1074 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK FOUND FS 1074 LONGERON 2R FORMER RING FROM L17L TO 17R WITH FIELD REPAIR INSTALLED. INSTALLED NEW FORMER RING FROM LONGERON 17L TO 17R PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66, 322. (X) 2 L 7 2 4F A6WE 1998051500018 19980515 00018 WP 1998 5 15 TWAA9806414 1 19980421 A 5744 CASTING DOUG DC9 DC933F 302207A WP RT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE REAR SPAR NR 2 FLAP HINGE CASTING, UPPER INBD AND OTBD MOUNT HOLE S WITH CORROSION ABOVE HOLES. REMOVED CORROSION. STOP DRILLED CRACK WITH .25 INCH. INSTALLED FILLER IN BLENDED OUT AR EA. INSTALLED DOUBLERS PER ATA 10992 AND DWG J060272. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500019 19980515 00019 WP 1998 5 15 TWAA9806413 1 19980416 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED PART PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. 2 L 7 2 4F A6WE 1998051500020 19980515 00020 WP 1998 5 15 TWAA9806412 1 19980416 A 5510 BARREL NUT DOUG DC9 DC932 3022066 WP HORIZ STABILIZER RUSTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT RT BARREL NUT IN FRONT SPAR FOR STABILIZER A TTACH TO CENTER SECTION WAS RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. REMOVED BOLT AND BARREL NUT AND CLEANED. REAM ED AND BUSHED HOLE PER ARA 15271A. INSTALLED NEW BOLT AND NUT AND RETAINER PER MM 55-10-00 AND TWA STD PRACTICES. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500021 19980515 00021 WP 1998 5 15 TWAA9806411 1 19980421 A 5753 ANGLE DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP INTERIOR AT IDLER HINGE, INBD ANGLE CRACKED AT 2 PLACES. REPLA CED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500022 19980515 00022 WP 1998 5 15 TWAA9806410 1 19980416 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 937/965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND METAL REMOVED BEYOND LIMIT FOR CORROSION REMOVAL AT CABIN STA 937 TO STA 965 , CENTER FLOOR CAP. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, 6A, AND ARA 10993. ACFT TT: 75,041 HOU RS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500023 19980515 00023 WP 1998 5 15 TWAA9806409 1 19980416 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE HAD CRACK AT LOWER AFT FASTENER IN LE RIB ABOVE LE PANEL NR 1211A . INSTALLED NEW RIB PER SRM 51-01, PAGE 1. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X) 2 L 7 2 4F A6WE 1998051500024 19980515 00024 WP 1998 5 15 TWAA9806408 1 19980416 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 484 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 484 FORMER CRACKED AT TOP AREA OF WINDOW BELT, RT SIDE. REPLACED FORMER PER SRM 53-03, FIG 32. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500025 19980515 00025 WP 1998 5 15 TWAA9806407 1 19980416 A 5753 SKIN DOUG DC9 DC933F 302207A WP TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT TE FLAP, THIRD TE FLAP SECTION, DELAMINATED ON LOWER FORWARD END. REPAIR ED IN SHOP PER SRM 51-01, AND STANDARD PROCESSES. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500026 19980515 00026 WP 1998 5 15 TWAA9806406 1 19980416 A 5347 FLOOR TRACK DOUG DC9 DC933F 302207A WP BS 198 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 198 FLOOR TRACK WITH CORROSION RBL 21 TO RBL 26. REMOVED CORROSION PER 5 1-10-3. REINSTALLED TRACK PER MM 53-40-1 PG 201. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500027 19980515 00027 WP 1998 5 15 TWAA9806405 1 19980416 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 522 BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 522 FORMER BENT BETWEEN LONGERON 18R AND LONGERON 17R. REPAIRED PER SRM 53-03, PAGE 5. Z-FRAME FLANGE REPAIR INSTALLED. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500028 19980515 00028 WP 1998 5 15 TWAA9806404 1 19980421 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 225 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND UPPER FUSELAGE DENT IN SKIN 1.50 INCH BY 1.50 INCH BY .080 INCH DEEP AT FS 2 25 ON STR 11L. REPAIRED DENT PER SRM 53-04 FIG 38. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500029 19980515 00029 WP 1998 5 15 TWAA9806403 1 19980421 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 433 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 STUBBY FRAME CRACKED 3 INCHES ABOVE FLOOR. REPLACED FRAME PER SRM 51 -01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500030 19980515 00030 WP 1998 5 15 TWAA9806402 1 19980421 A 5347 FLOOR TRACK DOUG DC9 DC933F 302207A WP BS 269 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, RBL 8 IN SGTA 269 FOUND FLOOR TRACK WITH EXCESS METAL REMOVED BEYOND LIMITS TO CLE AN UP CORROSION. REPLACED SECTION OF TRACK PER SRM 53-05 PG 10G, VIEW A. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. ( X) 2 L 7 2 4F A6WE 1998051500031 19980515 00031 NE 1998 5 15 TWAA9806401 2 19980425 A 7230 789777 VANE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE RT ENGINE SEPARATED A TWAA C E F D ABORTED TAKEOFF ENGINE SHUTDOWN ACTIVATE FIRE EXT. RETURN TO BLOCK D J A INFLIGHT SEPARATION WARNING INDICATION FLAME/FIRE TO TAKEOFF 1 CE 05 981Z 47345 DTW - FLT 349 - RT ENGINE STALLED ON TAKEOFF ROLL. ABORTED TAKEOFF. SHUT ENGINE DOWN. TOWER REPORTED FIRE OUT TAIL PI PE. FIRE FIRE EXTINGUISHING BOTTLES. PASSENGERS EXITED FROM FWD EVACUATION SLIDES. REPLACED ENGINE. CHECK-C 5-22-97 STL. ONE EACH SEVENTH STAGE STATOR VANE LIBERATED AND RESULTED IN HIGH PRESSURE COMPRESSOR FAILURE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1998051500032 19980515 00032 WP 1998 5 15 TWAA9806301 1 19980422 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 412EA 47733 STL - FLT 579 - ESCAPE PATH LIGHTING STRIP BY FIRST CLASS DIVIDER HAD A 2 FOOT SECTION UNLIT. PLACARDED PER MEL. ON LA YOVER, MAINTENANCE RESEATED EGRESS LT SEGMENT AND OPS OK. CHECK-C 8-16-97 STL. (X) 2 L 7 2 4F RT A6WE 1998051500033 19980515 00033 WP 1998 5 15 TWAA9806302 1 19980421 A 5320 JAMB DOUG DC9 DC933F 302207A WP CARGO DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT CARGO BIN LOWER DOOR JAMB CORROSION BETWEEN SKIN AND FRAME AND 3 EACH CR ACKS APPROXIMATELY .25 INCH LONG FROM STA 900 TO STA 917, 17 INCHES RBL. REMOVED CORROSION PER 51-10-3. REPLACED CORRO DED PARTS PER 51-01 PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500034 19980515 00034 WP 1998 5 15 TWAA9806303 1 19980421 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 1074 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME CRACKED AT LONGERON 14R, STA 1074. INSTALLED NEW FORMER RING F ROM LONGERONS 17L TO 17R PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500035 19980515 00035 WP 1998 5 15 TWAA9806304 1 19980421 A 5712 RIB DOUG DC9 DC933F 302207A WP WS 485 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND XRS 485 LT WING LE RIB CORRODED AND CRACKED. REPLACED RIB PER SRM 51-10 PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500036 19980515 00036 WP 1998 5 15 TWAA9806305 1 19980421 A 5753 ANGLE DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP INTERIOR AT IDLER HINGE, OTBD SIDE ANGLE CRACKED. REPLACED CRA CKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500037 19980515 00037 WP 1998 5 15 TWAA9806306 1 19980421 A 5320 DOUBLER DOUG DC9 DC933F 302207A WP BS 433 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 DOUBLER ON AFT FACE OF STUBBY FORMER CRACKED 4 INCHES ABOVE FLOOR LEV EL. REPLACED DOUBLER PER SRM 51-01 PG 1. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500038 19980515 00038 WP 1998 5 15 TWAA9806307 1 19980421 A 5347 FLOOR TRACK DOUG DC9 DC933F 302207A WP BS 180-240 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK FROM STA 180 TO STA 240, 21 INCHES LBL. REMOVED CO RRODED TRACK FROM STA 180 TO STA 248. FABRICATED AND INSTALLED NEW TRACK PER SRM 53-01, PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500039 19980515 00039 WP 1998 5 15 TWAA9806308 1 19980421 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 917 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 917 ABOVE LONGERON 27L, FORMER HAS .50 INCH EYEBROW CRACK ON FORWARD SIDE . WELDED FLOOR SUPPORT AND STRESS RELIEVED. REINSTALLED REPAIRED PER SSRM 53-00-106. ACFT TT: 70,506 HOURS. ACFT TC : 66,322. (X) 2 L 7 2 4F A6WE 1998051500040 19980515 00040 WP 1998 5 15 TWAA9806309 1 19980421 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 1074 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 1074 LONGERON 3L FORMER FRAME WITH FIELD REPAIR INSTALLED. INSTALLED NEW FORMER RING FROM LONGERON 17L TO LONGERON 17R PER SRM 51-01 PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. ( X) 2 L 7 2 4F A6WE 1998051500041 19980515 00041 WP 1998 5 15 TWAA9806310 1 19980421 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 1074 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 1074 LONGERON 3R FORMER FRAME WITH A FIELD REPAIR INSTALLED. INSTALLED N EW FORMER RING FROM LONGERON 17L TO LONGERON 17R PER SRM 51-01 PG 1 ITEM C. ACFT TT: 70,506 HOURS. ACFT TC: 66,322. (X) 2 L 7 2 4F A6WE 1998051500042 19980515 00042 NE 1998 5 15 TWAA9803402 2 19980309 A 7240 726560 CHAMBER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE RT ENGINE CRACKED A TWAA A UNSCHED LANDING M C OVER TEMP F.O.D. TO TAKEOFF 1 CE 05 983Z 730 47411 2140 RDU - FLT 503 - RT ENGINE INJESTED BIRD ON ROTATION FOR TAKEOFF. EGT ROSE TO 620 DEGREES. N1 AND N2 STEADY. NO VIBRAT ION. REDUCED POWER AND RETURNED TO RDU. REPLACED ENGINE. S/D: EXAMINATION OF THE ENGINE SHOWED SEA GULL WAS INGESTED CAUSING STALLS. THE HIGH, TRANSITORY PRESSURE CHANGE CAUSED AN EXISTING CRACK IN THE COMBUSTION CHAMBER INNER CASE TO RUPTURE CREATING PRESSURE INSTABILITY IN THE HIGH PRESSURE TURBINE, AND AN INCREASE OF EGT. THE ENGINE WAS DISASSEMBLED AND REPAIRED. 2 L 7 2 4F 4 F A6WE E2EA 1998051500043 19980515 00043 NE 1998 5 15 USAABB98034 1 19980415 A 3610 16J081 DUCT BOEING 757 757225 1384959 NM RROYCE RB211 RB211535E4 54555 NE LT ENGINE RUPTURED A USAA A B UNSCHED LANDING EMER. DESCENT J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 603AU 22198 30543 CLT - FL 41 - AFTER TAKEOFF FROM CLT, CREW RECEIVED THE EICAS MESSAGES 'L ENG OVHT' AND 'CABIN ALTITUDE' AND THE 'OVERHE AT' LIGHT ILLUMINATED. THE CREW REDUCED POWER ON THE LEFT ENGINE AT WHICH TIME THE OVERHEAT LIGHT EXTINGUISHED. CABIN PRESSURIZATION COULD NOT BE MAINTAINED, AND THE CREW ACCOMPLISHED AN EMERGENCY DESCENT. FLIGHT RETURNED TO CLT AND LAND ED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT ENGINE HAD DUCT BLOWN. THE DUCT WAS REPLACED. (X) 2 L 7 2 4F 4 F RT A2NM E12EU 1998051500044 19980515 00044 NM 1998 5 15 USAABB98038 1 19980407 A 3350 20121 BATTERY CHARGER BOEING 767 767201 1385125 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 648US 23900 PIT - FOUND THE LAST TWO SECTIONS, LEFT SIDE, OF FLOOR LIGHTING INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND REP LACED A BATTERY CHARGER. (X) 2 L 7 2 4F RT A1NM 1998051500045 19980515 00045 NM 1998 5 15 USAABB98039 1 19980409 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 LAX - FOUND R4 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A2NM 1998051500046 19980515 00046 NM 1998 5 15 USAABB98040 1 19980409 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 LAX - FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE AT ROWS 18, 23, AND 26. MAINTENANCE REPLACED THE BATTERIES. (X) 2 L 7 2 4F RT A2NM 1998051500047 19980515 00047 NM 1998 5 15 USAABB98041 1 19980415 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 627AU 27805 LAX - FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE AT ROWS 1 AND 33. MAINTENANCE REPLACED THE BATTERIES. (X) 2 L 7 2 4F RT A2NM 1998051500048 19980515 00048 NM 1998 5 15 USAABB98037 1 19980404 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AU 22198 LAX - FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE AT ROWS 13 AND 18. MAINTENANCE REPLACED THE BATTERIES. (X) 2 L 7 2 4F RT A2NM 1998051500049 19980515 00049 NM 1998 5 15 USAASB98100 1 19980418 A 3350 20124 CHARGER BOEING 737 737301 1384611 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 592US 23937 CLE - MAINTENANCE FOUND THE EMERGENCY AISLE LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE M1132 EMERGENCY LIG HT CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998051500050 19980515 00050 WP 1998 5 15 USAAD98068 1 19980414 A 3222 MS288892 VALVE DOUG DC9 DC931 3022065 WP NLG STRUT LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 927VJ 48154 LGA - FL 475 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RAISE AND THERE WAS AN UNSAFE NOSE GEAR INDICATION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT AND REPLACED THE SC HRADER VALVE. (X) 2 L 7 2 4F A6WE 1998051500051 19980515 00051 1998 5 15 USAAD98069 4 19980415 A 3431 LOCALIZER DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A USAA L ABORTED APPROACH O OTHER AP APPROACH 1 EA 19 978VJ 47371 LGA - FL 1703 - WHILE ON APPROACH TO RUNWAY 4 AFTER PASSING 1,000 FEET, BOTH CAPTAIN'S AND FIRST OFFICER'S LOCALIZER HAD A FULL RIGHT DEFLECTION AFTER BEING ON CENTERLINE. A MISSED APPROACH WAS EXECUTED. THE NEXT APPROACH WAS NORMAL WITH NO PROBLEM WITH THE RECEIVERS. MAINTENANCE PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THE ILS SYSTEM PER THE R5 CARD. (X) 2 L 7 2 4F A6WE 1998051500052 19980515 00052 NM 1998 5 15 USAASB98097 1 19980416 A 3350 67104789 BATTERY PACK BOEING 737 737201 1384454 NM CARGO COMPT DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 246US 22753 PIT - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHT AND THE WING-TO-BODY FAIRING EMERGENCY LIGHT INOPERABLE. MAI NTENANCE REMOVED AND REPLACED THE M193 EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998051500053 19980515 00053 NM 1998 5 15 USAA980166 1 19980420 A 5330 SKIN BOEING 737 737296 1384486 NM BS 569 LIGHTNING STRIKE A USAA K NONE C F.O.D. IN INSP/MAINT 1 EA 19 238US 45471 22398 ROA - DURING B-CHECK, VISUAL INSPECTION FOUND .50 INCH DAMAGED AREA (LIGHTNING STRIKE) BS 569, STR 7, RT FUSELAGE SKIN. REMOVED DAMAGED AREA, AND INSTALLED DOUBLER. REPAIRED PER SRM 53-30-3. (X) 2 L 7 2 4F RT A16WE 1998051500054 19980515 00054 NM 1998 5 15 USAA980167 1 19980420 A 5330 SKIN BOEING 737 737296 1384486 NM BS 737 LIGHTNING STRIKE A USAA K NONE C F.O.D. IN INSP/MAINT 1 EA 19 238US 45471 22398 ROA - DURING B-CHECK VISUAL INSPECTION, FOUND .75 INCH DAMAGED AREA (LIGHTNING STRIKE) AT BS 737-B STR 10, RT FUSELAGE S KIN. REMOVED DAMAGED AREA AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3. (X) 2 L 7 2 4F RT A16WE 1998051500055 19980515 00055 NM 1998 5 15 USAA980168 1 19980420 A 5330 SKIN BOEING 737 737201 1384454 NM BS 947 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 47844 22018 ROA - DUIRNG A-CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND 1.75 INCH CRACK BS 947, STR 24L, FUSELAGE SKIN. INSTALLE D REPAIR WITH BLIND FASTENERS/SOLID FASTENERS TO BE INSTALLED NEXT Q-CHECK. REPAIRED PER SRM 53-30-3, PAGE 2C. (X) 2 L 7 2 4F A16WE 1998051500056 19980515 00056 NM 1998 5 15 USAA980165 1 19980403 A 5330 SKIN BOEING 737 737201 1384454 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 244US 42527 22752 ROA - DURING CX-3 CHECK VISUAL/EDDY CURRENT INSPECTION, FOUND A 2 INCH CRACK FUSELAGE SKIN BS 807 STR 19L. INSTALLED DO UBLER, REPAIRED PER SRM 53-30-3, FIG 6. (X) 2 L 7 2 4F A16WE 1998051500057 19980515 00057 EU 1998 5 15 98ZZZX1707 1 19980315 A 3260 848401 PROX SWITCH ELDEC AIRBUS 320 A320231 3930325 EU LT MLG FAILED A P9RA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 09 EITLJ A9967 257 LGCIU 1 INDICATES LT MAIN GEAR UNLOCKED. LGCIU NR 2 INDICATES GEAR OK. GEAR DOOR POSSIBLY NOT CLOSING UPON EXTENSION. THROUGH CFD'S FOUND LGCIU FAULTING PROXIMITY SENSOR 17GA. REMOVED AND REPLACED PROXIMITY SWITCH IAW AMM 32-31-73 BITE TEST PER TASK NR 32-69-00-740-001, CHECK NORMAL. (X) 2 L 7 2 4F RT A28NM 1998051500058 19980515 00058 NM 1998 5 15 MBXA9800003 1 19980423 A 5610 001A561A0000200 WINDSHIELD DORNER DO32 DO328100 2996000 NM LT COCKPIT CRACKED A M8XA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 331MX 3407 1069 3074 DEN - FLT 7405 - EN ROUTE FROM DEN TO RAP, CREW REPORTED THE CAPTAIN'S WINDSCREEN HAD CRACKED AND THE AIRCRAFT WAS RETUR NING TO DEN. AIRCRAFT LANDED IN DENVER WITH NO FURTHER INCIDENTS. AIRCRAFT LATER MOVED FROM DEN TO COS WHERE MAINTENAN CE REPLACED THE DAMAGED WINDSCREEN. AIRCRAFT WAS THEN RETURNED TO SERVICE. PART TOTAL CYCLES: 3,853. X) 2 H 7 2 4T RT A45NM 1998051500059 19980515 00059 WP 1998 5 15 HALA9800100 1 19980423 A 3350 600304031 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 47654 HNL - FLT 112 - LOG PAGE A138890 - OVERHEAD EMERGENCY LIGHTS ROWS 5-10 INOPERABLE. REPLACED BATTERY, OPS CHECK GOOD. ( X) 2 L 7 2 4F RT A6WE 1998051500060 19980515 00060 WP 1998 5 15 HALA9800099 1 19980422 A 2750 CONTROL VALVE DOUG DC10 DC1010 3022110 WP TE FLAPS MALFUNCTIONED A HALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 119AA 46519 LAS - FLT 03 - LOG PAGE 4091834 - WHILE TURNING ONTO RUNWAY FOR DEPARTURE, SELECTED FLAPS AT 10 DEGREES. SHORTLY AFTER FLAPS AND INDICATOR REACHED 10 DEGREES, THE FLAP INDICATORS INDICATED THAT FLAPS WERE STILL CREEPING DOWN. RAN FLAP FUL L DOWN THEN UP AND THEN TO 10 DEGREES AGAIN. CONDITION SAME, RETURNED TO GATE. REPLACED FLAP CONTROL VALVE, OPS CHECK GOOD. (X) 2 L 7 3 4F A22WE 1998051500061 19980515 00061 WP 1998 5 15 98ZZZX1708 1 19980402 A 5414 SKIN DOUG DC8 DC8F55 3021928 WP NR 3 PYLON WRINKLED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 72192 45678 GYE - ON POST-FLIGHT INSPECTION, THE NR 3 ENGINE PYLON SKIN WAS FOUND WRINKLED AT STA YIP 217. INTERNAL PYLON INSPECTIO N REVEALED A BROKEN SPAR CAP AT STA YIP 217 REF SRM 54-3-0 PG 4A FIG 4, ITEM E. DACO NOTIFIED AND AIRCRAFT BEING PREPAR ED FOR 3 ENGINE FERRY TO MIA FOR REPAIRS TO NR 3 PYLON. PART TOTAL CYCLES: 21,631. 2 L 7 4 4F 4A25 1998051500062 19980515 00062 NM 1998 5 15 AALA980690 1 19980403 A 5311 FRAME BOEING 727 727227 1384078 NM BS 540 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - STA 540 ABOVE STR 21L IS CRACKED IN THE BELL FRAME. STOP DRILLED CRACK AFTER DYE CHECK TO VERIFY END OF CRACK AND INSTALLED DOUBLER PER SRM 53-10-4. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500063 19980515 00063 NM 1998 5 15 AALA980689 1 19980403 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - LEFT LOWER KEEL BEAM STRINGER CRACKED AT FORWARD END IN THE ANGLE RADIUS. REMOVED DAMAGED AREA AND INSTALLED DOUB LER PER SB 727-53-0208. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500064 19980515 00064 NM 1998 5 15 AALA980688 1 19980403 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - SHEAR TIE CORRODED AND CRACKED AT STA 720C BETWEEN STR 28R AND STR 28L. INSTALLED SHEAR TIE REPAIR PER 53-20-04. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500065 19980515 00065 NM 1998 5 15 AALA980687 1 19980403 A 5330 SKIN BOEING 727 727227 1384078 NM BS 686 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - CORROSION ON SKIN. INSTALLED SKIN AND SPLICE DOUBLER PER SRM 53-30-3, FIG 5. TST: 68,146 HOURS. CYCLES: 45,80 8. (X) 2 L 7 3 4F A3WE 1998051500066 19980515 00066 NM 1998 5 15 AALA980686 1 19980403 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - CRACK IN SKIN BETWEEN TWO RIVETS. STA 920C PLUS 8 INCHES, INBOARD OF STR 28L 3 INCHES. CRACK CONFIRMED TO END IN RIVET HOLES BY NDT AND INSTALLED DOUBLER PER 53-30-3 PAGE 8. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500067 19980515 00067 NM 1998 5 15 AALA980685 1 19980403 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - LOWER FUSELAGE SKIN AT BS 720C AROUND STR 28R HAS HEAVY WORN AREA. BLENDED DAMAGED AREA, FOUND OUT OF LIMITS PER SRM 53-30-1 PAGE 2 FIG 1. INSTALLED DOUBLER PER SRM 53-30-3 PAGE 8. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500166 19980515 00166 WP 1998 5 15 CALA9800798 1 19980506 A 3350 BR964412 BULBS DOUG DC10 DC1010 3022110 WP CABIN FAILED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68041 46900 EMERGENCY LIGHTS INOP NEAR FLT ATTEND SEAT 2L, IVS CLOSET, B-ZONE SEATS 29K TO 36K, ABOVE 26K RT OF B-ZONE AND SEATS IN A ZONE. REPLACED BURNT BULBS PER MM 33-50-00. 2 L 7 3 4F A22WE 1998051500167 19980515 00167 NM 1998 5 15 CALA9800799 1 19980506 A 5230 SKIN BOEING 737 737291 138448W NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 FORWARD CARGO DOOR INNER SKIN CRACKED (1/2). FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR PER SRM 51-40-2, 51-10-2 , 51-30-2 AND MM 51-20-0. 2 L 7 2 4F A16WE 1998051500168 19980515 00168 NM 1998 5 15 CALA9800801 1 19980506 A 5320 ANGLE BOEING 737 737291 138448W NM BS 520 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 CABIN FLOORBEAM ATTACH ANGLE CRACKED STA 520 BL 0.0. REMOVED CRACKED ATTACH ANGLE. FABRICATED, TREATED, PRIMED AND INS TALLED NEW ANGLE PER SRM 51-40-3, 51-10-2 AND MM 51-20-0. 2 L 7 2 4F A16WE 1998051500169 19980515 00169 NM 1998 5 15 CALA9800802 1 19980506 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 FS 950 RT ELEPHANT EAR FAIRING ATTACH ANGLE HAS CORROSION ON UPPER AND LOWER FLANGES. CUT OUT SECTION OF ATTACH ANGLE F ABRICTED FILLER AND ANGLE. TREATED, PRIMED AND INSTALLED ANGLES PER SRM 51-10-6, 53-10-6, 53-10-1, 51-40-4 51-30-2, AND 57-40-4. 2 L 7 3 4F A3WE 1998051500170 19980515 00170 NE 1998 5 15 CALA9800803 2 19980506 A 7260 GEARBOX BOEING 727 727224 1384076 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 NUMBER 2 ENGINE GEARBOX DATA PLATE MOUNT BOLT HOLE (UPPER AFT) BROKEN OUT. REPAIRED GEARBOX DATD PLATE MOUNT BOLT HOLE PER EC/RA 7261-01251. 2 L 7 3 4F 4 F A3WE E2EA 1998051500171 19980515 00171 NM 1998 5 15 CALA9800804 1 19980506 A 7110 APRON BOEING 727 727224 1384076 NM NR 1 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 NUMBER 1 ENGINE FORWARD APRON CRACKED (2) ON UPPER SIDE. REMOVED DAMAGED, INSTALLED DOUBLER AND FILLER PER SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998051500172 19980515 00172 NM 1998 5 15 CALA9800805 1 19980506 A 7110 APRON BOEING 727 727224 1384076 NM NR 1 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 NUMBER ONE ENGINE AFT APRON HAS DAMAGED SKIN CAUSED BY CHAFING ON FORWARD STIFFENER. FABRICATED, TREATED, PRIMED, AND I NSTALLED REPAIR PER SRM 51-10-2, 54-10-3, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998051500173 19980515 00173 NM 1998 5 15 CALA9800806 1 19980506 A 5411 RIB BOEING 727 727224 1384076 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 FIRST RIB AFT OF AFT ENG MOUNT IS CHAFED TWO SPOTS NUMBER ONE ENGINE PYLON. REMOVED DAMAGED AREA NR 1 ENGINE PYLON MOUN T RIB. FABRICATED NEW REPAIR, INSTALLED PER SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998051500174 19980515 00174 NM 1998 5 15 CALA9800807 1 19980506 A 2910 10605634 HOSE BOEING 727 727232 1384082 NM NR 2 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 15790 20644 ON CLIMBOUT, A-SYSTEM WENT TO 0 QUANTITY. FOUND .125 INCH HOLE IN ENGINE DRIVEN PUMP OUTLET HOSE. REPLACED HOSE AND IN SPECTED LINE FILTERS AND MAIN SCAVANGE, LEAK CHECK OK. 2 L 7 3 4F A3WE 1998051500175 19980515 00175 WP 1998 5 15 CALA9800808 1 19980506 A 5311 991224343 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 AFT CARGO BIN BELTFRAME CORRODED STA 1309 LONG 28 LT TO 28 RT. REMOVED AND REPLACED CORRODED SECTION OF BELTFRAME PER S RM 53-03 FIG 2A. 2 L 7 2 4F A6WE 1998051500176 19980515 00176 NM 1998 5 15 CALA980800 1 19980506 A 7110 DOUBLER BOEING 737 737291 138448W NM NR 1 ENGINE COWL CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 NUMBER ONE ENGINE O/B COWLING NUMBER SIX RIB CHAFED AT DOUBLER REPAIR. REMOVED DOUBLER AND FILLER MATERIAL. FABRICATED , TREATED, PRIMED, AND INSTALLED NEW DOUBLER PER SRM 51-40-3, 51-10-2, AND MM 51-20-11. 2 L 7 2 4F A16WE 1998051500177 19980515 00177 NM 1998 5 15 9808346612 1 19980121 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 1314 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON DOOR 3L MEDIUM CUTOUT AFT LOWER CORNER SILL FITTING TOP SURFACE AT FS 1314, LBL 125, WL 199. INSTALLED NEW REVEAL (P/N 65B11752-9) PER DWG SA 5340-01062-7. 2 L 7 4 4F A20WE 1998051500178 19980515 00178 NM 1998 5 15 9808356612 1 19980121 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 1272 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK AT DOOR 3L MEDIUM FORWARD LOWER CORNER SILL FITTING FS 1272, LBL 125, WL 200. INSTALLED NEW REVEAL (P/N 65B11751-601) PER DWG SA 5340-1062-7. 2 L 7 4 4F A20WE 1998051500179 19980515 00179 NM 1998 5 15 9808366612 1 19980121 A 5711 SPAR BOEING 747 747251B 1384892 NM WS 971 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON FRONT SPAR ABOVE LOWER CHORD AT FS 971 OPPOSITE LEADING EDGE FLAP NR 7. REPAIRED PER EA 66-155580. 2 L 7 4 4F A20WE 1998051500180 19980515 00180 NM 1998 5 15 9808376612 1 19980118 A 5730 SKIN BOEING 747 747251B 1384892 NM WS 1392 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON LOWER CHORD LOWER SKIN AT FRONT SPAR AREA FS 1392. REPAIRED PER EA 66-156321. 2 L 7 4 4F A20WE 1998051500181 19980515 00181 NM 1998 5 15 9808386612 1 19980124 A 5320 WEB BOEING 747 747251B 1384892 NM NR 4 FRAME CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK ON WEB AT RIGHT NR 4 MEDIUM FORWARD FRAME. REPAIRED PER EA 66-155570. 2 L 7 4 4F A20WE 1998051500182 19980515 00182 NM 1998 5 15 9808396612 1 19980218 A 5312 BULKHEAD BOEING 747 747251B 1384892 NM BS 400 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK ON TOP OUTBOARD (RHS) CORNER AT BULKHEAD 400, ZONE 110. REPAIRED PER EO 6-53-41184. 2 L 7 4 4F A20WE 1998051500183 19980515 00183 NM 1998 5 15 9808406612 1 19980121 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 1256 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK AT DOOR 3R MEDIUM FORWARD FRAME, LOWER FORWARD CORNER FITTING AT FS 1256, RBL 124, WL 198. I NSTALLED NEW FITTING PER DWG SA 5340-01062-7. 2 L 7 4 4F A20WE 1998051500184 19980515 00184 NM 1998 5 15 9808416612 1 19980127 A 5320 FITTING BOEING 747 747251B 1384892 NM BS 1690 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON DOOR 4R MEDIUM CUTOUT FORWARD FRAME ON INSIDE SURFACE BELOW LEVELING COMPOUND, 6TH FI TTING UP FROM BOTTOM CUTOUT AT FS 1690. REPLACED DOOR STOP FITTING (P/N 65B08936-6) PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998051500185 19980515 00185 NM 1998 5 15 9808426612 1 19980119 A 5311 FRAME BOEING 747 747251B 1384892 NM BS 260 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK ON MAIN DECK A-ZONE FS 260 FRAME WEB ADJACENT TO STR 25R. FABRICATED AND INSTALLED NEW WEB PER EA 66-153227. 2 L 7 4 4F A20WE 1998051500186 19980515 00186 NM 1998 5 15 9808436612 1 19980119 A 5311 FRAME BOEING 747 747251B 1384892 NM BS 360 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CRACK ON MAIN DECK A-ZONE FS 360 FRAME WEB ADJACENT TO STR 25L. FABRICATED AND INSTALLED NEW WEB PER EA 66-153228. 2 L 7 4 4F A20WE 1998051500187 19980515 00187 NM 1998 5 15 9808446612 1 19980121 A 5320 FITTING BOEING 747 747251B 1384892 NM 3R DOORWAY CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 612US 20357 DURING M-CHECK, FOUND CORROSION ON DOOR 3R MEDIUM CUTOUT AFT LOWER CORNER SILL FITTING TOP SURFACE. REPLACED FITTING (P /N 65B11752-10) PER DWG SA 5340-01062-7. 2 L 7 4 4F A20WE 1998051500188 19980515 00188 WP 1998 5 15 9808459929 1 19980505 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8923E 45838 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT INADEQUATE FORCE WAS REQUIRED TO REMOVE BOTH THE INTERIOR AND EXTERIOR TAI L CONE RELEASE HANDLES FROM THE RETAINING CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998051500189 19980515 00189 WP 1998 5 15 9808469101 1 19980506 A 3230 LATCH DOUG DC9 DC915 3022036 WP RT MLG OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 91S 47063 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT I NCIDENT. MAINTENANCE ADJUSTED RIGHT MAIN GEAR DOOR LATCH MECHANISM, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500190 19980515 00190 WP 1998 5 15 9808479996 1 19980506 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG LACK OF LUBE A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8932E 47141 NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW UTILIZED EMERGENCY GEAR EXTENSION PROCEDURE S AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY ON GROUND. LUBRICATED NOSE GEAR AS SEMBLY. 2 L 7 2 4F A6WE 1998051500191 19980515 00191 WP 1998 5 15 9808489917 1 19980505 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP RT NACELLE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500192 19980515 00192 WP 1998 5 15 9808499150 1 19980506 A 3350 POWER SUPPLY DOUG DC9 DC914 3022034 WP RT NACELLE FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8908E 45749 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500193 19980515 00193 WP 1998 5 15 9808509178 1 19980506 A 3350 BATTERIES DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN FORWARD CABIN DIM. REPLACED BATTERIES IN BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500194 19980515 00194 WP 1998 5 15 9808519178 1 19980506 A 3350 POWER SUPPLY DOUG DC9 DC914 3022034 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 3310L 45705 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS IN TAIL COMPARTMENT AND IN AFT CABIN INOPERATIVE. R EPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500195 19980515 00195 WP 1998 5 15 9808529869 1 19980506 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 778NC 48100 DURING LINE MAINTENANCE INSPECTION, FOUND OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 9, 10, AND 11 INOPERATIVE. REPLACED BA TTERIES IN FIRST BATTERY PACK AFT OF OVERWING EMERGENCY EXIT DOORS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998051500196 19980515 00196 WP 1998 5 15 9808539873 1 19980506 A 3350 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 782NC 48107 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. REPLACED BATTERIES, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998051500197 19980515 00197 EA 1998 5 15 COMA9860096 1 19980504 A 5610 601R330331 WINDSHIELD CNDAIR CL600 CL6002B19 EA LT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 941CA 7050 PILOTS WINDSHIELD OUTER PANE SHATTERED AT 26,000 FT. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1998051500198 19980515 00198 NM 1998 5 15 SWAA980706 1 19980428 A 3350 900547 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722SW 22698 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHT IN CENTER CABIN FLICKERS. REMOVED AND REPLACED EMERGENCY EXIT LIGHT CARTRIDGE AND BATTERY PACK. 2 L 7 2 4F A16WE 1998051500199 19980515 00199 NM 1998 5 15 SWAA980707 1 19980428 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 924 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 924, STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998051500200 19980515 00200 NM 1998 5 15 SWAA980708 1 19980428 A 5330 SKIN BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING WALKAROUND CHECK, FOUND APPROX 4 SKIN CRACKED AT RT SIDE ABOVE PASSENGER WINDOW NR 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500201 19980515 00201 NM 1998 5 15 SWAA980709 1 19980428 A 3350 6104789 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 302SW 22942 DURING TERMINAL CHECK, FOUND EGRESS TRACK LIGHTING INOP FWD CABIN TO MID CABIN. REMOVED AND REPLACED FWD CABIN EGRESS L IGHTING BATTERY PACK AS PER BOEING MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998051500202 19980515 00202 NM 1998 5 15 SWAA980710 1 19980428 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 890/1009 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 1010, 2 ABOVE STR 14L BS 1009, 4 BELOW STR 11 AND BS 890, 2 BELO W STR 14L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998051500203 19980515 00203 NM 1998 5 15 SWAA980711 1 19980428 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344/986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED FLOORBEAM TOP FLANGE AT BS 344, LBL 8 TO 35, WL 208 AND BS 986.5, RBL 4 TO 12, WL 207 TO 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998051500204 19980515 00204 NM 1998 5 15 SWAA980712 1 19980428 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND EXFOLIATED CORROSION FLOORBEAM SUPPORT AT BS 986.5 FAR RIGHT SIDE. REPAIRED PER SWA RA NR 1-353-1808. 2 L 7 2 4F RT A16WE 1998051500205 19980515 00205 NM 1998 5 15 SWAA980713 1 19980428 A 5330 SKIN BOEING 737 7373G7 1384595 NM NR 1/2 LE SLATS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED C4 CHECK, FOUND CRACKED SKIN NR 1 SLAT LWR T/E O/B OF AND NR 2 SLAT LWR T/E OF ACTUATOR. REPAIRED PER BOEING RA T1-A57-018. 2 L 7 2 4F RT A16WE 1998051500206 19980515 00206 NM 1998 5 15 SWAA980714 1 19980428 A 5330 SKIN BOEING 737 7372K6 NM BS 880 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 880, S20 R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500207 19980515 00207 NM 1998 5 15 SWAA980715 1 19980429 A 5320 WEB BOEING 737 7372H4 138448C NM BS 530 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED WEB ABOVE LT RAM AIR INTAKE DUCT AT BS 530. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998051500208 19980515 00208 NM 1998 5 15 SWAA980716 1 19980429 A 5320 WEB BOEING 737 7372K6 NM BS 335 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED WEB ANGLE AT BS 335 STR 5R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500209 19980515 00209 NM 1998 5 15 SWAA980717 1 19980429 A 5312 BULKHD SUPPORT BOEING 737 7372K6 NM BS 380 WRINKLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND WRINKLED SIDE BULKHEAD SUPPORT AT BS 380, STR 25L TO 19L, LBL 29 TO 55, WL 194 TO 160. REMO VED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500210 19980515 00210 NM 1998 5 15 SWAA980718 1 19980429 A 5315 FLOORBEAM BOEING 737 7372K6 NM BS 813 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUT PLATE LOCATIONS AT BS 813 AND 825, LBL 2.5 WL 159. REMO VED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500211 19980515 00211 NM 1998 5 15 SWAA980719 1 19980429 A 5320 PRESS PANEL BOEING 737 7372K6 NM BS 663 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CORRODED AT BS 663, RBL 47, WL 197 ON WHEEL WELL BULKHEAD. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500212 19980515 00212 NM 1998 5 15 SWAA980720 1 19980429 A 5320 SUPPORT ANGLE BOEING 737 7372K6 NM BS 352-360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND INTERCOSTAL SUPPORT ANGLE HAS ELONGATED FASTENER HOLES AT BS 352 TO 360, RBL 1, WL 149. REM OVED AND REPLACED DAMAGE INTERCOSTAL SUPPORT ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500213 19980515 00213 NM 1998 5 15 SWAA980721 1 19980429 A 5315 FLOORBEAM BOEING 737 7372K6 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND DENTED FLOORBEAM AT BS 500B, WL 150. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500214 19980515 00214 NM 1998 5 15 SWAA980722 1 19980429 A 5313 STRINGER BOEING 737 7372K6 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CRACKED STRINGER CLIP AT FWD CARGO BAY BS 500C, STR 23L, LBL 45, WL 164. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500215 19980515 00215 NM 1998 5 15 SWAA980723 1 19980429 A 5532 SKIN BOEING 737 7373A4 1384585 NM VERT STAB BIRD STRIKE A SWAA K NONE O OTHER AP APPROACH 1 SW 07 673SW 23251 ON APPROACH, FOUND BIRD STRIKE DAMAGE TO VERTICAL STAB, RT INBD WING L/E, AND PAX CABIN WINDOW AT BS 747. AIRCRAFT MADE AN UNEVENTFUL LANDING. ACCOMPLISHED BIRD STRIKE INSP PER MM A/C FERRY TO TRAMCO. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500216 19980515 00216 NM 1998 5 15 SWAA980724 1 19980430 A 5230 SEAL BOEING 737 7373Q8 1384670 NM CARGO DOOR FAILED A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 689SW 23387 FLT LEVEL 350, CABIN ALT WARNING HORN SOUNDED WOULD NOT HOLD PRESSURE IN AUTO/STBY OR MANUAL WITH OUTFLOW VALVE SULL CLO SE, DESCENDED TO FLT LEVEL 240 AND STILL WOULD NOT HOLD CABIN PRESSURE. WENT TO HIGH ON PACKS, REGAINED PRESSURIZATION, PRESSURE WOULD HOLD WITH EITHER OR BOTH PACKS IN HIGH. MADE AN UNEVENTFUL LANDING. REPAIRED AFT CARGO DOOR SEAL PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998051500217 19980515 00217 NM 1998 5 15 SWAA980725 1 19980430 A 5320 FRAME BOEING 737 7372K6 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED AFT ENTRY DOOR/FUSELAGE FRAME AT FWD SIDE BELOW LWR CAM PLATE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500218 19980515 00218 NM 1998 5 15 SWAA980726 1 19980430 A 5320 FRAME BOEING 737 7372K6 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED OUTER SKIN AT FWD LOWER CORNER OF DOOR FRAME APPROX 1.3 LONG. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500219 19980515 00219 NM 1998 5 15 SWAA980727 1 19980430 A 5512 SKIN BOEING 737 7372K6 NM LT HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND LT HORIZONTAL STAB LEADING EDGE FIX COWL HAS A BULGE AND IS DENTED. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998051500220 19980515 00220 NM 1998 5 15 SWAA980728 1 19980430 A 5330 SKIN BOEING 737 7372K6 NM NR 2 ENGINE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED EXTERNAL SKIN ON NR 2 ENG NOSE COWL 8 O'CLOCK POSITION. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500221 19980515 00221 NM 1998 5 15 SWAA980729 1 19980430 A 5330 SKIN BOEING 737 7373H4 1384600 NM L2 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND CRACKED L2 LOWER HINGE CUTOUT ON FUSELAGE SIDE (.875 LONG). REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500222 19980515 00222 NM 1998 5 15 SWAA980730 1 19980430 A 5330 SKIN BOEING 737 7373H4 1384600 NM R2 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED C1 CHECK, FOUND CRACKED R2 LOWER HINGE CUTOUT ON FUSELAGE SIDE (.850 LONG). REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500223 19980515 00223 NM 1998 5 15 SWAA980731 1 19980430 A 2612 FIRE LOOP BOEING 737 7373H4 1384600 NM NR 2 ENGINE FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 686SW 23175 DURING WALKAROUND CHECK, FOUND NR 2 ENG FIRE LOOP WILL NOT TEST. REMOVED AND REPLACED NR 2 ENG FIRE LOOP UNIT PER BOEIN G MM. 2 L 7 2 4F RT A16WE 1998051500224 19980515 00224 NM 1998 5 15 SWAA980732 1 19980430 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 403 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN AT BS 403, WL 226, RBL 74.0 BELOW STR 14R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500225 19980515 00225 NM 1998 5 15 SWAA980733 1 19980430 A 5230 SKIN BOEING 737 7375H4 138449D NM CARGO DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 509SW 24186 DURING WALKAROUND CHECK, FOUND AFT CARGO DOOR HAS DEEP DENT WITH GOUGE SKIN AREA. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500226 19980515 00226 NM 1998 5 15 SWAA980748 1 19980501 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 328-344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED INTERCOSTAL AT BS 328 TO 344, LBL 47, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500227 19980515 00227 NM 1998 5 15 SWAA980749 1 19980501 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED ANGLE AT BS 328, LBL 47, WL 200 TO 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500228 19980515 00228 NM 1998 5 15 SWAA980750 1 19980501 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 312 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND ANGLE AT BS 312, RBL 17, WL 207 HAS MECHANICAL DAMAGE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500229 19980515 00229 NM 1998 5 15 SWAA980751 1 19980501 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 885-990 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND DENTED SKIN AT BS 990, WL 217, LBL 72.1 ABOVE STR 14L TO INCLUDE BS 885 AND BS 889, LBL 72 B ELOW STR 14L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500230 19980515 00230 NM 1998 5 15 SWAA980752 1 19980501 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED INTERCOSTAL AT BS 380 TO 400, LBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500231 19980515 00231 NM 1998 5 15 SWAA980753 1 19980501 A 5320 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 907-927 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CREASE BEAM WEB AT BS 907 TO 927, RBL 60, WL 208 HAS SEVERAL ELONGATED FASTENER HOLES. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500232 19980515 00232 NM 1998 5 15 SWAA980754 1 19980501 A 5711 SPAR CHORD BOEING 737 7373H4 1384600 NM WS 224 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATION ON TOP MOST INBOARD FASTENER HOLE COMMON TO MAIN LANDING GEAR BEAM FITT ING (RIGHT SIDE) RSS 224 (CRACK ON SPAR CHORD UPPER). REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500233 19980515 00233 NM 1998 5 15 SWAA980755 1 19980501 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 867, RBL 21, WL 166. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500234 19980515 00234 NM 1998 5 15 SWAA980756 1 19980501 A 5730 SKIN BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 24374 DURING SCHEDULED D-CHECK, FOUND SMALL CRACK AT FIXED L/E SKIN LOWER PANEL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500235 19980515 00235 NM 1998 5 15 SWAA980757 1 19980501 A 5330 SKIN BOEING 737 7372K6 NM BS 540 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BULGING OUTWARD AND SEVERAL FASTENERS PULLING THROUGH ALONG KEEL BEAM 6 FORWARD OF AIR CONDITIONING SERVICE PANEL AT BS 540. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500236 19980515 00236 NM 1998 5 15 SWAA980758 1 19980501 A 5330 PANEL BOEING 737 7372K6 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4D CHECK, FOUND AFT KEEL BEAM ACCESS PANEL BETWEEN A/C BAY DOORS HAS 2 FWD FASTENERS PULLING THROUGH SKIN. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500237 19980515 00237 NM 1998 5 15 SWAA980759 1 19980501 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 941/946 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 941 AND 946 STR 23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998051500238 19980515 00238 NM 1998 5 15 SWAA980760 1 19980501 A 5730 ANGLE BOEING 737 7372K6 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4D CHECK, FOUND UPPER I/B L/E FLAPWELL PANEL CRACKED AT FASTENER HOLE. REMOVED AND REPLACED CRACKED ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500239 19980515 00239 NM 1998 5 15 SWAA980761 1 19980503 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 LONG BELOW STR 23R AT BS 727D. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998051500240 19980515 00240 NM 1998 5 15 SWAA980762 1 19980503 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 LONG ABOVE STR 23R FWD AT BS 727E. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998051500241 19980515 00241 NM 1998 5 15 SWAA980763 1 19980504 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 502SW 24179 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT ROW TRACK LIGHTING LOOSE. SECURED FLOOR TRACK LIGHTING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998051500242 19980515 00242 NM 1998 5 15 SWAA980764 1 19980504 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1011 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 95SW 23054 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT RIVET HOLES DUE TO CORROSION BULGING SKIN AT BS 1011 AND O/T B /D AND INBD SIDE OF STR 26L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998051500243 19980515 00243 NM 1998 5 15 SWAA980765 1 19980504 A 7110 COWL BOEING 737 7373H4 1384600 NM NR 1 ENGINE PUNCTURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND 1 X .5 PUNCTURE ON INNER SKIN OF NR 1 O/B ENG COWL 8.5 FROM L/E AND 29 FROM LOWER EDGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500244 19980515 00244 NM 1998 5 15 SWAA980766 1 19980504 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 866 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND DENTED WEB AT BS 866, RBL 29, WL 170. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500245 19980515 00245 NM 1998 5 15 SWAA980767 1 19980504 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 791 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 791, RBL 60, WL 190 HAS DOUBLE DRILLED HOLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500246 19980515 00246 NM 1998 5 15 SWAA980768 1 19980504 A 2752 BUSHING BOEING 737 7373H4 1384600 NM NR 2 LE FLAP ACT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND CORRODED NR 2 K-FLAP ACTUATOR ROD END FITTING BUSHINGS. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500247 19980515 00247 NM 1998 5 15 SWAA980769 1 19980504 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 334SW 23938 DURING SCHEDULED D-CHECK, FOUND RIGHT REAR EMERGENCY EXIT LIGHT AT RIGHT REAR SERVICE DOOR INOP. REMOVED AND REPLACED B ULB, CLEANED CONTACTS, AND OP CK GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998051500248 19980515 00248 NM 1998 5 15 SWAA980770 1 19980504 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294.5-310 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CORRODED INTERCOSTAL WEB AT BS 294.5 TO 310, LBL 41 TO 46, WL 161. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500249 19980515 00249 NM 1998 5 15 SWAA980771 1 19980504 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 438 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CRACKED EZ-4 RACK SUPPORT ANGLE AT BS 438, LBL 6 TO 28, WL 158. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998051500250 19980515 00250 NM 1998 5 15 SWAA980772 1 19980504 A 5511 RIB BOEING 737 7373H4 1384600 NM RT HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND RT HORIZONTAL STAB L/E HAS A CREASED DENT ON A RIB AT STA 148. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998051500251 19980515 00251 EU 1998 5 15 SWAA980773 2 19980506 A 7230 BEARING BOEING 737 7373H4 1384600 NM CFMINT CFM56 CFM563C1 13802 EU NR 1 ENGINE FAILED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 652SW 27722 INFLIGHT SHUTDOWN OF NR 1 ENGINE ON CLIMBOUT AT 19K AFTER COMPRESSOR STALL WITH ASSOCIATED OIL QTY AND PRESSURE LOSS. S USPECT NR 3 BEARING FAILURE. AIRCRAFT RETURN TO PVD AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED ENGINE AND P ERFORMED POWER ASSURANCE RUN PER BOEING MM. 2 L 7 2 4F 4 F RT A16WE E21EU 1998051500252 19980515 00252 NM 1998 5 15 98FDEA00289 1 19980424 A 5315 65163169 FLOORBEAM BOEING 727 727233 138408A NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION (C53-224-03-1/2) ON FLOORBEAM AROUND NUT PLATE HOLE BS 344, RBL 12, WL 208. *S/D* REPAIRED FLOORBEAM UPPER C HORD AT BS 344, RBL 68 TO LBL 68 PER FED-EX SRM 51-30-2, FEDEX DRAWING SR 27-53-007. 2 L 7 3 4F RT A3WE 1998051500253 19980515 00253 NM 1998 5 15 98FDEA00290 1 19980424 A 5311 65163455 FRAME BOEING 727 727233 138408A NM BS 1090 GOUGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 GOUGE IN FRAME AT BS 1090, LBL 60, WL 182. *S/D* REPAIRED FRAME AT BS 1090, LBL 60, WL 182 PER FED-EX SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998051500254 19980515 00254 NM 1998 5 15 98FDEA00294 1 19980425 A 5320 6914817112 SHEAR TIE BOEING 727 727233 138408A NM BS 700 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 WHILE WORKING NR 0450 FOUND SHEAR TIE BS 700 STRINGER 28R TO 28L CORRODED. *S/D* REPLACED SHEAR TIE BS 700, STR 28R TO 28L IN ACCORDANCE WITH FED-EX SRM 51-20-1, 51-30-2, BAC DRAWING 65-15938. 2 L 7 3 4F RT A3WE 1998051500255 19980515 00255 NM 1998 5 15 98FDEA00295 1 19980425 A 5314 65184072 KEEL BEAM BOEING 727 72722C 138400F NM BS 1063-1068 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 105FE 19194 CORROSION ON KEEL BEAM BS 1063 TO 1068, RBL 7, WL 150. *S/D* ACCOMPLISHED KEEL BEAM REPAIR PER FED-EX EA NR 7-5310-386 60, BS 1063 TO 1068, RBL 7, WL 150. 2 L 7 3 4F A3WE 1998051500256 19980515 00256 NM 1998 5 15 98FDEA00331 1 19980506 A 3010 SHUTOFF VALVE BOEING 727 7272S2F 1384O81 NM NR 3 RT ANTI-ICE MALFUNCTION A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 212FE 22934 AFTER TAKEOFF, DUCT OVERHEAT LIGHT ILLUM FOLLOW BY ZONE 4 MAIN CARGO SMOKE WARN LIGHT AND BELL. SMELL SMOKE IN COCKPIT LIGHTS AND BELL EXTINGUISH THEN CAME ON ANOTHER. THE NR 3 ENG DUCT TEMP WAS 220 DEG NR 1 ENG WAS APPROX 180. OPER CKD W ING ANTI-ICE SYS, ALL SYS ALL INDICATION NORMAL. REMOVED AND REPLACED NR 3 RIGHT HAND WING ANTI ICE SHUTOFF VALVE PER M /M 30-11-31 (PRECAUTIONARY). LEAK CHECK GOOD. REMOVED AND REPLACED WING ANTI-ICE HIGH PRESS SHUTOFF VALVE PER M/M 30-1 1-11 OPER CK GOOD. RAN ENG 1 AND 3 TO PERFORM A FUNCTIONAL TEST OF WING THERMAL ANTI-ICE SYS PER M/M 30-13-0, ALL CHECK S GOOD. 2 L 7 3 4F A3WE 1998051500257 19980515 00257 NM 1998 5 15 98FDEA00332 1 19980505 A 2150 CONDENSER BOEING 727 72722 1384002 NM LT PACK MALFUNCTIONED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 167FE 18864 DURING FLIGHT, LEFT PACK EMITS STRONG ODOR. SMELLS LIKE PAINT, HOT ODOR. REMOVED AND REPLACED LEFT PACK CONDENSER, WAT ER SEPARATOR. OPERATIONAL LEFT PACK NO ODOR NOTICED AFTER 20 MINUTES. LEFT PACK OK FOR SERVICE. 2 L 7 3 4F A3WE 1998051500258 19980515 00258 NM 1998 5 15 98FDEA00333 1 19980507 A 2150 CONDENSER BOEING 727 72722 1384002 NM LT PACK MALFUNCTIONED A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 167FE 18864 AT TAKEOFF POWER COCKPIT FILLS WITH STRONG BURNING ODOR. SUSPECT LEFT PACK OR ENGINE NR 1 BLEED SYSTEM IS CONTRIBUTING TO PROBLEM. WHEN LEFT PACK IS TURNED OFF IN FLIGHT ODOR IS REDUCED. DO NOT APPEAR TO GET ODOR EXCEPT IN HIGH ENGINE PO WER SITUATION. RAN LEFT PACK FOR OVER 30 MINUTES NO BURNING SMELL NOTED. SUSPECT LEFTOVER RESIDUE FROM BAD CONDENSER R EFERENCE PREVIOUS WRITE-UP. 2 L 7 3 4F A3WE 1998051500259 19980515 00259 NM 1998 5 15 98FDEA00334 1 19980506 A 2613 OVERHEAT LOOP BOEING 727 727233 138408A NM AFT BODY OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 SO 25 274FE 22039 LOWER AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT WITH WING ANTI-ICE ON. TURNED OFF WING ANTI-ICE, LIGHT WENT OUT. TURNE D ENGINE NR 1 WING ANTI-ICE ON LIGHT CAME BACK ON. SECURED SYSTEM THEN RECHECKED WITH ENGINE NR 3 WING ANTI-ICE ON, LIG HT CAME BACK ON AGAIN. REMOVED KEEL BEAM PANEL AND PANELS IN AFT CARGO COMPARTMENT. LEAKED CHECKED ANTI-ICE LINE FROM AIRSTAIR AREA TO KEEL BEAM AREA NO LEAKS FOUND. DID FIND LOOP TOUCHING ANTI-ICE LINE IN KEEL BEAM REPOSITIONED LOOP AWA Y FROM LINE. OPERATIONAL CHECKS GOOD ON GROUND RUN NEEDS PANELS REINSTALLED. REINSTALLED KEEL BEAM PANEL AND AFT CARGO COMPARTMENT PANELS. 2 L 7 3 4F RT A3WE 1998051500260 19980515 00260 NM 1998 5 15 SCNA98038 1 19980430 A 2530 CONNECTORS BOEING 727 727225 1384077 NM AFT GALLEY SHORTED A SCNA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NR NOT REPORTED 1 GL 15 283SC 22559 SPARKING APPEARED IN THE AFT GALLEY AREA. BOTH OVENS WERE TURNED OFF AND CIRCUIT BREAKERS PULLED. REMOVED THE OVENS AN D CLEANED AND DRIED CANNON PLUGS AND CONNECTIONS. NO FAULTS FOUND. 2 L 7 3 4F A3WE 1998051500265 19980515 00265 CE 1998 5 15 98ZZZX1713 1 19980424 A 5743 51227201 SUPPORT CESSNA 402 402C 207590R CE LT MLG TRUNNION CRACKED A A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 26150 12286 402C0111 DURING INSPECTION, FOUND LEFT MAIN GEAR TRUNNION SUPPORT CRACKED ALONG WEBBING. REPLACED UNIT. 1 L 7 2 3O A7CE 1998051500266 19980515 00266 CE 1998 5 15 98ZZZX1714 1 19980424 A 5320 501101110 GUSSET CESSNA 402 402C 207590R CE PILOT SEAT CRACKED A OEZA K NONE O OTHER IN INSP/MAINT 1 WP 19 26150 12286 402C0111 DURING INSPECTION, FOUND GUSSET UNDER PILOT SEAT CRACKED. REPLACED WITH NEW PART. 1 L 7 2 3O A7CE 1998051500394 19980515 00394 EU 1998 5 15 MALA976118 1 19980502 A 2613 OVERHEAT LOOP SAAB SF340 SF340A 7850100 EU LT WING MALFUNCTIONED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 112XJ 340A112 DURING FLIGHT, THE LEFT BLEED LEAK CAUTION LIGHT CAME ON. CREW COMPLETED QRH TO NO RESOLVE, LIGHT REMAINS ON. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED SENSING LOOP BEHIND LEFT WING SPAR IAW SAAB MM PERFORMED CHECK, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998051500395 19980515 00395 EU 1998 5 15 MALA976119 1 19980505 A 2910 HYD PRESSURE BAC 146 AVRO146RJ85A 1500097 EU YELLOW HYD SYST FAILED A MALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 511XJ E2326 ON ARRIVAL AT GATE, YELLOW SYSTEM PRESSURE WENT TO ZERO, PARKING BRAKE SET PRESSURE BLED TO ZERO IN TWO SECONDS, GREEN S IDE OK. MAINTENANCE COULD NOT DUPLICATE PROBLEM, INSPECTED BRAKE AND HYDRAULIC SYSTEM NO LEAKAGE NOTED. PERFORMED CHEC K IAW AMM ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998051500396 19980515 00396 1998 5 15 MALA976120 4 19980504 A 3414 AIRSPEED IND SAAB SF340 340B 7860101 EU RT COCKPIT SPLIT A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 410XJ 410 DURING FLIGHT, THE FLIGHT DIRECTOR WOULD NOT SYNC USING VERTICAL SYNC, AVIONICS HEADING FLAG ILLUMINATED IN FLIGHT, APPE AREDTO BE FO'S SIDE. 10 KNOTS AIRSPEED INDICATION SPLIT. MAINTENANCE COULD NOT DUPLICATE AIRSPEED SPLIT NOR HEADING FL AG. FLIGHT DIRECTOR FUNCTIONING NORMALLY DUE TO AP BREAKERS BEING PULLED. ALL SYSTEMS OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998051500397 19980515 00397 EU 1998 5 15 MALA976121 1 19980427 A 5230 SKIN SAAB SF340 SF340A 7850100 EU CARGO DOOR DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ 340A112 DURING HEAVY CHECK, THE CARGO DOOR HAS A SINGLE 2' WIDE BY 2' LONG BY .032' DEEP DENT IN THE OUTER SKIN. DENT IS LOCATE D AT THE LOWER EDGE OF THE DOOR APPROX 8 OF THE FORWARD LOWER CORNER. DENT IS, 40' FROM THE LOWER SKIN EDGE. DENT IS A LLOWED AND CAN BE ACCEPTED AS LONG AS NO CRACKS OF DELAMINATIONS ARE NOTED. 2 L 7 2 4T RT A52EU 1998051500398 19980515 00398 EU 1998 5 15 MALA976123 1 19980427 A 5720 ANGLE SAAB SF340 SF340A 7850100 EU WS 42 CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ 340A112 DURING HEAVY CHECK, THE LEFT AND RIGHT WS 42 AFT SPAR ANGLE CRACKS. MAINTENANCE REFERENCE STEP 2.3.2. CRACKS HAVE ALREA DY BEEN APPROVED ON SAAB STATEMENT 72SAS1558. NO FURTHER ACTION IS REQUIRED. 2 L 7 2 4T RT A52EU 1998051500399 19980515 00399 NM 1998 5 15 RAAA98B2026 1 19980506 A 3350 873100112 LIGHT BOEING 727 72722C 138400F NM CABIN BROKEN A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK DUE BROKEN LAMP ASSY. CHANGED PROXIMITY LIGHT ASSY. 2 L 7 3 4F A3WE 1998051500400 19980515 00400 WP 1998 5 15 CALA9800809 1 19980507 A 5720 ANGLE DOUG DC10 DC1010 3022110 WP LT WING CRACKED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 68041 46900 LT WING FUEL STA CRACK (2) AT RT FWD SIDE BETWEEN HI-LOCKS. CRACKED AREA TRIMMED AND BLENDED OUT. INSTALLED DOUBLER PE R SRM 57-10-00 AND 51-33-01. 2 L 7 3 4F A22WE 1998051500401 19980515 00401 WP 1998 5 15 CALA9800810 1 19980507 A 2620 WIRE DOUG DC10 DC1030 3023501 WP NR 3 ENGINE BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13067 47866 NUMBER 3 ENGINE NUMBER 1 AGENT FIRE BOTTLE LOW PRESSURE SWITCH FAILED. WIRE FOUND BROKEN AT EARTH POINT 6015D. WIRE RE TERMINATED WITH A NEW TAG PER MM20-00-00. 2 L 7 3 4F A22WE 1998051500402 19980515 00402 NE 1998 5 15 CALA9800811 2 19980507 A 7320 8901274 SENSOR BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE INOPERATIVE A CALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 33637 27540 NUMBER TWO ENGINE FAILED TO RESPOND TO THROTTLE MOVEMENTS DURING CLIMB. REPLACE NUMBER TWO ENGINE COMPRESSOR INLET TEMP SENSOR PER MM 73-21-02. 2 L 7 2 4F 4 F RT A16WE E2GL 1998051500403 19980515 00403 NM 1998 5 15 CALA9800812 1 19980507 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 10791 20645 MAIN CABIN O/H EMERGENCY LIGHT FLICKERING. RECHARGED BATTERY PACK PER MM 33-50-0. 2 L 7 3 4F A3WE 1998051500404 19980515 00404 WP 1998 5 15 CALA9800813 1 19980506 A 5347 5936663521 TIE DOWN RAIL DOUG DC9 DC982 3022082 WP BS 1007-1220 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 AFT CRGO BIN LEFT TIE DOWN RAIL STA 1007 TO 1220 CORRODED AT FASTENERS. REPLACED LEFT TIE DOWN RAIL PER SRM 51-30-5. 2 L 7 2 4F A6WE 1998051500405 19980515 00405 WP 1998 5 15 CALA9800814 1 19980507 A 5347 5936663501 TIE DOWN RAIL DOUG DC9 DC982 3022082 WP BS 1007-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 AFT CARGO BIN RIGHT SIDE TIE DOWN RAIL STA 1007 TO 1155 CORRODED AT FASTENERS. INSTALLED NEW TIE DOWN RAIL PER SRM 51-3 0. 2 L 7 2 4F A6WE 1998051500406 19980515 00406 WP 1998 5 15 CALA9800815 1 19980506 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 MAIN CABIN DOOR NR 8 BEAM FWD END CRACKED (1). INSTALLED DOUBLER PER SRM 52-05 PG 177. 2 L 7 2 4F A6WE 1998051500407 19980515 00407 WP 1998 5 15 CALA9800816 1 19980507 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 AFT SERVICE DOOR FWD ESCAPE SLIDE SUPPORT HAS CORROSION. REMOVED CORROSION. REINSTALLED SUPPORT. INSTALLED DOUBLER UN DER MOUNT PER SRM 51-30-3, 51-30-2, AND 53-01 FIG 4. 2 L 7 2 4F A6WE 1998051500408 19980515 00408 NM 1998 5 15 CALA9800817 1 19980507 A 5330 SKIN BOEING 737 737291 138448W NM BS 905 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 FUSELAGE SKIN HAS A DENT AT STA 905 STR 22R. REMOVED DAMAGED AREA, FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED PE R SRM 53-30-1, 53-30-3, 51-20-2, AND MM 51-21-11. 2 L 7 2 4F A16WE 1998051500409 19980515 00409 NM 1998 5 15 CALA9800818 1 19980507 A 5320 BRACKET BOEING 727 727224 1384076 NM LT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LT MLG WALKING BEAM PANEL HAS BROKEN ATTACH BRACKET (1/2 CRACK) I/B END OF PANEL. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1998051500410 19980515 00410 NM 1998 5 15 CALA9800819 1 19980507 A 5320 PAN BOEING 727 727224 1384076 NM AFT LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT LAV SERVICE PAN HAS CORROSION THROUGH OUT. REMOVED SERVICE PAN WEB FRAME. FABRICATED REPAIR ANGLE. INSTALLED NEW WEB FRAME. NEW SUPPORT HINGES PER SRM 51-30-2, 51-20-1, AND 51-10-2. 2 L 7 3 4F A3WE 1998051500411 19980515 00411 WP 1998 5 15 CALA9800820 1 19980507 A 5320 59360381 JAMB DOUG DC9 DC982 3022082 WP BS 670-690 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 MID CARGO BIN DOOR JAMB BEAM (Z ANGLE) HAS SURFACE CORROSION FROM STA 670 TO 690. BURNISHED CORROSION AND INSTALLED REP AIR DOUBLER UNDER FWD LOWER DOOR STOP PER EC/RA 5310-03723. 2 L 7 2 4F A6WE 1998051500412 19980515 00412 1998 5 15 9808549903 4 19980506 A 3454 ANTENNA DOUG DC9 DC931 3022065 WP RIGHT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 953N 47083 BOTH VOR SYSTEMS FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED RIGHT VOR ANTE NNA AND TRANSFORMER ASSEMBLY. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998051500413 19980515 00413 NM 1998 5 15 9808556717 1 19980506 A 3241 CONTROL UNIT BOEING 747 747251F 1384898 NM ANTI-SKID SYST FAILED A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 617US 21121 DURING APPROACH, THREE ANTI-SKID LIGHTS ILLUMINATED. INITIATED A GO-AROUND AND RECYCLED THE LANDING GEAR AND THE LIGHTS EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE ANTI-SKID CONTROL UNIT. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998051500414 19980515 00414 NM 1998 5 15 9808566309 1 19980506 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 24H - 31H. REPAIRED WIRE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998051500415 19980515 00415 NM 1998 5 15 9808576310 1 19980507 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 670US 24225 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM DOOR 4R - 54. RECONNECTED LIGHTS. OPERATIONAL CH ECK GOOD. 2 L 7 4 4F RT A20WE 1998051500416 19980515 00416 WP 1998 5 15 9808589307 1 19980507 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 309RC 48088 DURING LINE CHECK, FOUND FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY. OPERATIONAL CHECK O K. 2 L 7 2 4F A6WE 1998051500417 19980515 00417 WP 1998 5 15 9808599106 1 19980507 A 3260 ROLLER DOUG DC9 DC915 3022036 WP RT MLG OUT OF ADJUST A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 96S 47206 DURING LANDING GEAR UPLATCH CHECK, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. FLIGHT CREW RECYCLED THE LANDI NG GEAR HANDLE PER COM PROCEDURES AND LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE RIGHT MAIN LANDI NG GEAR DOOR ROLLERS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500419 19980515 00419 EU 1998 5 15 QXEA9800634 1 19980505 A 3350 XB864041 COVER GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN MISSING A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 BOI - SEAT 12B EMERGENCY EXIT COVER MISSING. MAINTENANCE REPLACED COVER, OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT A20EU 1998051500420 19980515 00420 EU 1998 5 15 QXEA9800635 1 19980505 A 3350 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 BOI - 2 EVACUATION LIGHTS IN CABIN INOPERATIVE. MAINTENANCE RELAMPED AND CHECKED OPERATION OF LIGHTS, TEST NORMAL. 2 L 7 2 4F RT A20EU 1998051500421 19980515 00421 NM 1998 5 15 QXEA9800636 1 19980505 A 3231 RETRACT MECH DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR OUT OF ADJUST A QXEA K NONE J WARNING INDICATION CL CLIMB 1 NM 09 814PH 43 SEA - AFTER GEAR RETRACTION, THE LEFT GEAR DOOR REMAINED IN THE OPEN POSITION. CYCLED THE LANDING GEAR AND THE DOOR CLO SED NORMALLY. INSPECTED THE AIRCRAFT AND FOUND IT SAFE FOR A FERRY FLIGHT SEA-PDX. IN PDX ADJUSTED THE JAM NUT ON THE LEFT FORWARD DOOR ACTUATOR STOP PLATE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998051500422 19980515 00422 NM 1998 5 15 98FDEA00335 1 19980507 A 2170 COALESCER BAG BOEING 727 72722 1384002 NM NR 2 ENGINE DIRTY A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 25 167FE 18864 98-0118 - ON T/O WITH T/O PWR SET. COCKPIT FILL WITH BURN ODOR. NR 1 BLD WAS OPEN AND LEFT PACK ON. SWITCH BLD AIR SO URCE TO NR 2 ENG. STILL HAD FUMES SWITCH TO RIGHT PACK OPER AND WAS OK. AFTER T/O TURNED LEFT PACK ON WITH CLIMB POWER AND SMELL CAME BACK. SWITCH FROM NR 1 TO NR 2 BLEED SOURCE AND STILL HAD FUMES. REMOVED AND REPLACED LEFT CONDENSER/W ATER SEPARATOR SOCK. INSP RAM AIR DOOR AREA AND PRECOOLER EXHAUST FOR SIGN OF BIRD STRIKE/BIRD NEST. ACM MACH OIL LEV EL GOOD. RAN ENG AT T/O PWR AND GOT SMELL WHEN N2 ABOVE 85 PERCENT DECREASE WITH THROT RETARD. SMELL IS FROM NR 1 ENG ONLY. REMOVED AND REPLACED RIGHT H2O SEP BAG PER M/M 21 TAKEOFF POWER RUN OF ALL ENG AND ALL PACKS AND BLD AT MULTIPLE 2 L 7 3 4F A3WE 1998051500423 19980515 00423 NE 1998 5 15 98FDEA00336 2 19980508 A 7200 ENGINE BOEING 727 72725C 138400H NM PWA JT8 JT8D9A 52048 NE NR 3 FOD A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 SO 25 116FE 1291298 SUSPECTED BIRDSTRIKE ON CLIMB-OUT, NR 3 ENG CONTINUED TO RUN W/SEVERE VIBRATION. UNDER VOLTAGE SYS NR 3. NR 3 GEN FIEL D, AGR AND BUS TIE TRIP. NR 3 ENG OIL PRESS DROPPED TO 16 PSI AFTER SHUTDOWN FOR 10 MIN. ACCOMP ENG FAILURE SEVERE DAM AGE CHECKLIST. AFT CARGO DOOR LIGHT ILLUM'D AFTER BIRDSTRIKE. REMOVED AND REPLACED NR 3 ENG PER MM 71-00 AND WORKCARD KIT 70T0503. C/W ENG TYPE 'A' PER JT8-D MM 72-00 PG 553-554, ALL CK GOOD. AFT CARGO DOOR LIGHT FUNCTIONING NORMALLY. A /C OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998051500424 19980515 00424 WP 1998 5 15 MWEA98577 1 19980506 A 3350 60030431 TERMINAL DOUG DC9 DC932 3022066 WP CABIN LOOSE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 FOUND 5 CABIN CEILING EMERGENCY LIGHTS INOP FROM SEATS 13 TO AFT CABIN. MAINTENANCE FOUND TERMINAL END ON BATTERY PACK LOOSE AND SECURED. 2 L 7 2 4F A6WE 1998051500425 19980515 00425 WP 1998 5 15 MWEA98578 1 19980506 A 5330 SKIN DOUG DC9 DC932 3022066 WP NLG DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE RIGHT AFT NOSE GEAR HINGE CUTOUT SKIN REPAIR IS CRACKED. MAINTENANCE REMOVED OLD REPAIR FABRICATED AND INSTALLED DO UBLER. 2 L 7 2 4F A6WE 1998051500426 19980515 00426 WP 1998 5 15 MWEA98579 1 19980506 A 5330 SKIN DOUG DC9 DC932 3022066 WP NLG DOORWAY MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 205ME 47601 THE LEFT HAND AFT NOSE GEAR HINGE CUTOUT HAS A PREVIOUS IMPROPER REPAIR. MAINTENANCE REMOVED REPAIR AND FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998051500427 19980515 00427 WP 1998 5 15 MWEA98580 1 19980506 A 5347 SEAT TRACKS DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 THE CAPTAINS ON FIRST OFFICERS LOWER OUTBOARD SEAT TRACK IS WORN. MAINTENANCE FABRICATED AND INSTALLED SEAT TRACKS. 2 L 7 2 4F A6WE 1998051500428 19980515 00428 WP 1998 5 15 SCNA98039 1 19980506 A 2150 PACK DOUG DC10 DC1010 3022110 WP CABIN SMOKING A SCNA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 571SC 46645 THE NUMBER THREE PACK APPEARS TO CAUSE LIGHT SMOKE WHEN ON IN THE AFT PORTION OF THE AIRCRAFT. RAN NUMBER THREE PACK OF F AND ON SETTING. INSPECTED DUCT, FOUND NO DEFECTS AND NO RETURNED SMOKE. PACK SYSTEM FUNCTIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1998051500429 19980515 00429 NM 1998 5 15 DHL98726003 1 19980508 A 3260 3186301001036 LIGHT SOCKET BOEING 727 727228 NM RT MLG FAILED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 726DH 20409 ON APPROACH, GEAR DOWN RT MLG GREEN LIGHT NOT ON, SECONDARY INDICATION OK. REMOVED AND REPLACED LIGHT SOCKET. 2 L 7 3 4F A3WE 1998051500430 19980515 00430 SO 1998 5 15 SWIA971162 1 19980404 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CARGO DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 292SW 120319 CARGO DOOR WARNING LIGHT IS ON. RETURNED TO FIELD. MEL 52-70-1. ADJUSTED CARGO DOOR WARNING LIGHT MICRO SWITCH, OPS C HECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998051500431 19980515 00431 SO 1998 5 15 SWIA971163 1 19980405 A 5230 SEAL EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE CARGO DOOR OUT OF POSITION A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 234SW 120308 LOUD POP AFT OF GALLEY, FOLLOWED BY SLOW DEPRESSURIZATION. RETURNED TO PDX. REPOSITIONED CARGO DOOR LOWER LIP SEAL SEC TION. PERFORMED GROUND PRESSURE CHECKS IAW MM 52-30-01, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998051500432 19980515 00432 SO 1998 5 15 SWIA971165 1 19980409 A 3260 AIR/GROUND RELAY EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE NLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 216SW 120285 AFTER NORMAL TAKEOFF UPON FLAP RETRACTION, FLAP AURAL WARNING SOUNDED, AUTO FEATHER WARNING THEN SOUNDED. ALL WARNINGS BRIEFLY STOPPED WHEN POWER LEVERS WERE MOVED TO DIFFERENT PLACE. HOWEVER, AURAL WARNING NEVER COMPLETELY SILENCED. RET URNED TO PSP. COULD NOT DUPLICATE PROBLEM ON GROUND CHECKS. RERACKED AURAL WARNING UNIT. REQUESTED FLIGHT CHECK FOR F URTHER TROUBLESHOOTING. CHECKED BAD. SLAVED IN ALL THREE NEW SHOCK ABSORBER PROXIMITY SENSORS, NEW FLAP CONTROL BOX AN D FLAP HANDLE. TESTED LANDING GEAR RELAY BOX AND AURAL WARNING UNIT. WARNING STILL EXISTED. REMOVED AND REPLACED NOSE LANDING GEAR AIR/GROUND RELAY K0122, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998051500433 19980515 00433 SO 1998 5 15 SWIA971166 1 19980409 A 3230 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT MLG MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION AP APPROACH 1 NM 07 218SW 120287 LEFT LANDING GEAR WOULD NOT INITIALLY EXTEND. CYCLED GEAR HANDLE AND GEAR THEN EXTENDED. REPLACED LANDING GEAR CONTROL BOX SWING LANDING GEAR 25 TIMES. COULD NOT DUPLICATE PROBLEM. CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998051500434 19980515 00434 SO 1998 5 15 SWIA971167 1 19980410 A 5270 BULBS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE SERVICE DOOR FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 296SW 120325 SERVICE DOOR LIGHT REMAINS LIT AFTER TAKEOFF. RETURNED TO FIELD. MEL 52-70-1. INSTALLED NEW BULBS IN SERVICE DOOR LIG HT. LIGHT CHECKS GOOD AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1998051500436 19980515 00436 GL 1998 5 15 98ZZZX1741 2 19980329 A 7200 23005290 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 FAILED A HEEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 22342 12081 592 760096 CAE8904315E MARCH 29, 1998 IN CRUISE FLIGHT, THE NR 1 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. SHUT DOWN ENGINE AND DIVERTED TO BRAZ ORIA COUNTY FOR SINGLE ENGINE LANDING. MAINTENANCE FOUND NR 1 ENGINE OIL SCAVENGE INADEQUATE, OIL TANK EMPTY, AND ENGIN E GEARBOX FULL OF OIL. REPLACED ENGINE ASSEMBLY RTS. 1 G 7 2 3U 3 U H1NE E1GL 1998051500439 19980515 00439 NM 1998 5 15 AALA980684 1 19980326 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 870 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - RIGHT LOWER KEEL BEAM STRINGER CRACKED AT FORWARD END IN THE ANGLE RADIUS. REMOVED DAMAGED AREA AND INSTALLED DOU BLER PER SB 727-53-0208. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500440 19980515 00440 NM 1998 5 15 AALA980683 1 19980403 A 5320 BRACKET BOEING 727 727227 1384078 NM BS 320 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - RIGHT NOSE WHEEL WELL SUPPORT BRACKET HAS CORROSION AT SKATE ANGLE, STA 328. INSTALL NEW SUPPORT BRACKET PER SRM 51-30-2. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500441 19980515 00441 NM 1998 5 15 AALA980682 1 19980403 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 520-540 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - STA 520 TO STA 540, STR 27R HAS CORROSION AT 2 SPOTS ON OUTBOARD END OF STRINGER. REMOVED AND REPLACED CORRODED P ART OF STRINGER 27, STA 520 TO STA 540 IAW SRM 53-10-6. TST: 68,146 HOURS. CYCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500442 19980515 00442 NM 1998 5 15 AALA980681 1 19980403 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 721AA 20729 TUL - DENTED BELLFRAME AT 950B, STR 22R. INSTALLED BELLFRAME REPAIR AND REINSTALLED INTERCOSTAL. TST: 68,146 HOURS. C YCLES: 45,808. (X) 2 L 7 3 4F A3WE 1998051500443 19980515 00443 NM 1998 5 15 AALA980657 1 19980401 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - CORROSION AROUND RAM AIR DOOR ACTUATOR CUT-OUT. INSTALLED DOUBLER REPAIR PER ESO 11697 DATED 3-23-98. TST: 49,3 06 HOURS. CYCLES: 26,738. (X) 2 L 7 3 4F A3WE 1998051500444 19980515 00444 NM 1998 5 15 AALA980656 1 19980401 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1149-1156 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 890AA 22006 TUL - STR 30 SPLICE ANGLE CORRODED. RT FLANGE STA 1149 - STA 1156. REMOVED CORRODED STR 30 SPLICE ANGLE STA 1149 - STA 1156. INSTALLED NEW SPLICE ANGLE PER SRM 53-10-3. TST: 49,306 HOURS. CYCLES: 26,738. (X) 2 L 7 3 4F A3WE 1998051500445 19980515 00445 WP 1998 5 15 AALA980723 1 19980407 A 5744 POST DOUG DC10 DC1030 3023501 WP WS 118 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - RIGHT INBOARD FLAP TRACK NR 1 ATTACH POST BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 PAGES 1-5 . REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL II. TREATED, PRIMED/PAINTED, SRM 51-21-01, VOL II. TST: 91,033.07 HOURS. CYCLES: 18,134. (X) 2 L 7 3 4F A22WE 1998051500446 19980515 00446 WP 1998 5 15 AALA980722 1 19980407 A 5744 POST DOUG DC10 DC1030 3023501 WP WS 118 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - RIGHT INBOARD FLAP TRACK NR 2 ATTACH POST BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 PAGES 1-5 . REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL 22. TREATED, PRIMED, AND PAINTED SRM 51-21-01 VOL II. TST: 91,033. 07 HOURS. CYCLES: 18,134. (X) 2 L 7 3 4F A22WE 1998051500447 19980515 00447 WP 1998 5 15 AALA980721 1 19980407 A 5744 POST DOUG DC10 DC1030 3023501 WP WS 118 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - RIGHT INBOARD FLAP TRACK NR 4 ATTACH POST FORWARD BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 P AGES 105. REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL II. TREATED, PRIMED, AND PAINTED/SRM 51-21-01 VOL II. TST: 91,033.07 HOURS. CYCLES: 18,134. (X) 2 L 7 3 4F A22WE 1998051500448 19980515 00448 WP 1998 5 15 AALA980720 1 19980407 A 5744 POST DOUG DC10 DC1030 3023501 WP WS 118 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - RIGHT INBOARD FLAP TRACK NR 3 ATTACH POST BORES AND FACE CORRODED. RE-WORKED BORES PER AARD 57-20-00-10 PAGES 1-5 . REMOVED CORROSION FROM FACE PER SRM 51-21-01 VOL II. TREATED, PRIMED/PAINTED, SRM 51-21-01 VOL II. TST: 91,033.07 H OURS. CYCLES: 18,134. (X) 2 L 7 3 4F A22WE 1998051500449 19980515 00449 WP 1998 5 15 AALA980650 1 19980327 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70524 49916 TUL - SILL BEAM CORRODED FROM STA 1155 - STA 1212 (LIGHT). HEAVY CORROSION AT STA 1200. FABRICATED AND INSTALLED DOUBL ER PER AARD 53-10-00-3 AND ESO 80559, 3-27-98. TST: 23,359 HOURS. CYCLES: 12,378. (X) 2 L 7 2 4F A6WE 1998051500450 19980515 00450 EU 1998 5 15 VTZA98148 1 19980330 A 7722 8974696 HARNESS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 470UE 814 IAD/PIT - FLT 6588 - DURING CRUISE AT 2,005 HOURS ON 3-30-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE EGT GAUGE FLUCTUATION AND SRL/TTL OFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOV ED AND REPLACED SOFT HARNESS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998051500451 19980515 00451 EU 1998 5 15 VTZA98142 1 19980324 A 3350 DM21 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CABIN LOOSE A VTZA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 EA 27 310UE 41028 IAD/DAY - FLT 6303 - DURING TAXI AT 0705 HOURS ON 3-24-98, AIRCRAFT RETURNED TO GATE DUE TO EMERGENCY TRACK LIGHTS WERE INOPERABLE. MAINTENANCE INSPECTED AND REPAIRED LOOSE WIRE TO TRACK LIGHTING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND A PPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998051500452 19980515 00452 EU 1998 5 15 VTZA98150 1 19980402 A 7921 SYLC522454 ACTUATOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 306UE 41020 IAD/ILM - FLT 6623 - DURING CRUISE AT 2,000 HOURS ON 4-2-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO LT OIL C OOLER FLAP WOULD NOT CLOSE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL COOLER ACTUATOR. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998051500453 19980515 00453 EU 1998 5 15 VTZA98146 1 19980325 A 3350 8G500599705 LIGHTS JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 EA 27 314UE 41027 IAD/MHT - FLT 6388 - DURING TAXI AT 0650 HOURS ON 3-25-98, AIRCRAFT RETURNED TO GATE DUE TO LEFT SIDE EMERGENCY EXIT ROW LIGHTS BEING INOPERABLE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LIGHT BULBS, OPS CHECK OK. AIRCRAFT WAS RELEA SED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998051500454 19980515 00454 1998 5 15 VTZA98144 4 19980328 A 6122 89741016 PROP GOVERNOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 488UE 907 IAD/BDL - FLT 6521 - DURING CRUISE AT 1635 HOURS ON 3-38-29, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT ENGINE RPM H AS TO BE PULLED BACK ALMOST TO THE TAXI RANGE TO GET 97 PERCENT. AIRCRAFT LANDED AT IAD AND RETURNED TO GATE WITH NO FU RTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LT PROP GOVERNOR, OPS CHECK OK. AIRCRAFT WAS RELEASED A ND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998051500455 19980515 00455 EU 1998 5 15 VTZA98153 1 19980404 A 5210 H50002051235 LATCH JETAIR JETSTM JETSTM4101 1500501 EU PASSENGER DOOR LACK OF LUBE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 320UE 41043 IAD/CHS - FLT 6483 - DURING CLIMB AT 0740 HOURS ON 4-4-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED AND ALIGNMENT MARKS OFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANC E INSPECTED AND CLEANED AND LUBED DOOR LATCH MECHANISM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998051500456 19980515 00456 EU 1998 5 15 VTZA98154 1 19980405 A 2121 12502101 BLOWER MOTOR BAG JETSTM JETSTM3201 1500217 EU CARGO COMPART FAILED A VTZA A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 482UE 897 JFK/IAD - FLT 6473 - DURING CRUISE AT 1414 HOURS ON 4-5-98, MADE AN UNSCHEUDLED LANDING AND AN EMERGENCY DESCENT DUE TO SMOKE IN CABIN. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EVA PORATOR BLOWER MOTOR AND RESISTOR INSIDE CAPACITOR MODULE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE . REF: OPERATOR CONTROL NR 98ZZZX1744. (X) 2 L 7 2 4T RT A56EU 1998051500457 19980515 00457 EU 1998 5 15 98ZZZX1744 1 19980405 A 2121 12502127 RESISTOR BAG JETSTM JETSTM3201 1500217 EU CARGO COMPART FAILED A VTZA A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 482UE 897 JFK/IAD - FLT 6473 - DURING CRUISE AT 1414 HOURS ON 4-5-98, MADE AN UNSCHEUDLED LANDING AND AN EMERGENCY DESCENT DUE TO SMOKE IN CABIN. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EVA PORATOR BLOWER MOTOR AND RESISTOR INSIDE CAPACITOR MODULE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE . REF: OPERATOR CONTROL NR VTZA98154. 2 L 7 2 4T RT A56EU 1998051500458 19980515 00458 1998 5 15 VTZA98152 4 19980403 A 3417 7000700966 DADC JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPARTMENT FAILED A VTZA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 27 310UE 41028 IAD/BDL - FLT 6212 - DURING CRUISE AT 0830 HOURS ON 4-3-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 ADC AND NR 1 AHRS FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 ADC. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: OPERATOR CONTROL NR 98ZZZX1745. (X) 2 L 7 2 4T RT A41NM 1998051500459 19980515 00459 1998 5 15 98ZZZX1745 4 19980403 A 3425 AHRS JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPARTMENT FAILED A VTZA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 EA 27 310UE 41028 IAD/BDL - FLT 6212 - DURING CRUISE AT 0830 HOURS ON 4-3-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING DUE TO NR 1 ADC AND NR 1 AHRS FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 ADC. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: OPERATOR CONTROL NR VTZA98152. 2 L 7 2 4T RT A41NM 1998051500460 19980515 00460 NM 1998 5 15 USAASB98095 1 19980415 A 2751 2061141 INDICATOR BOEING 737 737301 1384611 NM COCKPIT FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 355US 30228 23558 RDU - FL 1494 - ON APPROACH TO RDU, CREW EXTENDED FLAPS FROM 25 TO 30 DEGREES AND RECEIVED A FLAP ASSYMETRY. CREW PLACE D FLAPS BACK TO 25 DEGREES, ADVISED THE TOWER THEY HAD A PROBLEM AND DECLARED AN EMERGENCY. CREW ACCOMPLISHED A GO-AROU ND AND PERFORMED EMERGENCY CHECK LIST IN REFERENCE TO TRAILING EDGE FLAP PROBLEM. CREW EXECUTED A LONG FINAL AND BROUGH T THE AIRCRAFT IN ON A SHALLOW APPROACH. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN PO WER. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR. RAN FLAPS SEVERAL TIMES. OPERATIONAL CHECK GOOD PER MM. (X) 2 L 7 2 4F RT A16WE 1998051500461 19980515 00461 WP 1998 5 15 TWAA9805907 1 19980214 A 5711 SPAR DOUG DC9 DC931 3022065 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 991Z 47096 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING AFT FLAP INBD HINGE CASTING, LOWER INBD HOLE ON REAR SPAR, HAD A CRA CK INDICATION ON FACE. INSTALLED REPAIR DOUBLER PER PRINT JO60271 PER WORK SHEET MC8-AD-36. ACFT TT: 70,732 HOURS. A CFT TC: 76,937. (X) 2 L 7 2 4F A6WE 1998051500462 19980515 00462 EU 1998 5 15 VTZA98137 1 19980319 A 3310 13730390K10 PANEL BAG JETSTM JETSTM3201 1500217 EU COCKPIT SHORTED A VTZA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 370MT 800 IAD/PHI - FLT 6455 - DURING TAXI AT 0635 HOURS ON 3-19-98, AIRCRAFT REURNED TO GATE DUE TO SMOKE SMELL IN CABIN. MAINTE NANCE INSPECTED AND OPENED DMI 57772, MEL 33-1 ON SKIRT LIGHTING PANEL. MAINTENANCE CLOSED DMI 57772 ON 3-28-98 BY REMO VING AND REPLACING FASCIA PANEL, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998051500463 19980515 00463 1998 5 15 VTZA98157 4 19980409 A 3425 7003110901 EHSI DISPLAY JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 322UE 41058 IAD/LGA - FLT 6500 - DURING CRUISE AT 0645 HOURS ON 4-9-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING AT IAD DUE TO LT FHSI S CREEN WENT BLANK. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED E HSI SCREEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998051500464 19980515 00464 EU 1998 5 15 VTZA98149 1 19980401 A 3060 660715288 BRUSH BLOCK BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 474UE 849 IAD/ORF - FLT 6616 - DURING CLIMB AT 0700 HOURS ON 4-1-97, MADE AN UNSCHEDULED LANDING AT IAD DUE TO LT PROP HEAT SHOWED ZERO AMPS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT BRUS H BLOCK, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998051500465 19980515 00465 EU 1998 5 15 VTZA98156 1 19980408 A 3230 1849F UPLOCK BAG JETSTM JETSTM3201 1500217 EU LT MLG MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 491UE 911 IAD/RDU - FLT 6435 - DURING CLIMB AT 2130 HOURS ON 4-8-98, MADE AN UNSCHEUDLED LANDING AT IAD DUE TO LEFT MLG WOULD NOT RETRACT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED UPLOCK HOO K ASSY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998051500466 19980515 00466 EU 1998 5 15 VTZA98161 1 19980413 A 5270 JE5 SWITCH BAG JETSTM JETSTM3201 1500217 EU PASSENGER DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 491UE 911 IAD/SYR - FLT 6387 - DURING CRUISE AT 2230 HOURS ON 4-13-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO PASSENGE R DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANE D AND LUBED MICROSWITCH ACTUATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998051500467 19980515 00467 1998 5 15 VTZA98160 4 19980413 A 3425 7003360948 AHRU JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPARTMENT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 324UE 41017 BOS/JFK - FLT 6439 - DURING CRUISE AT 1800 HRS ON 4-13-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT BOS DUE TO NR 2 AHRU FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. AIRCRAFT FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND RE MOVED AND REPLACED AHRS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998051500468 19980515 00468 NE 1998 5 15 VTZA98159 2 19980412 A 7230 COMPRESSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE DAMAGED A VTZA A UNSCHED LANDING B C SMOKE/FUMES/ODORS/SPARKS F.O.D. CL CLIMB 1 EA 27 307UE 41021 IAD/EWR - FLT 6342 - DURING TAKEOFF ON 4-12-98 AT 1700 HOURS, EXPERIENCED SMOKE IN THE CABIN. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO IAD WHERE THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOT IFIED AND THE AIRCRAFT WAS REPOSITIONED TO THE MAINTENANCE HANGAR AFTER IT WAS NOTED THE BY LINE STATION MECHANICS THE R T ENGINE HAD INGESTED A BIRD AND THAT THERE WERE SEVERAL IMPELLER BLADES BENT. THE RT HAND ENGINE WAS REMOVED AND REPLA CED. ALL MAINTENANCE PROCEDURES WERE ACCOMPLISHED ALONG WITH APPROPRIATE POST-MAINTENANCE CHECKS. AIRCRAFT WAS THEN RE LEASED FOR SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1998051500469 19980515 00469 WP 1998 5 15 VTZA98158 2 19980411 A 7230 31011607 COMPRESSOR SEALS BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT/RT ENGINES WORN A VTZA A UNSCHED LANDING B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CL CLIMB 1 EA 27 495UE 818 IAD/BDL - FLT 6521 - DURING TAKEOFF ON 4-11-98 AT 1607 HOURS, EXPERIENCED A SMELL AND NOTICED SMOKE IN THE CABIN. THE F LIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO IAD. CREW AND PASSENGERS DEPLANED THE AIRCRAFT, MAINTENANCE CONTROL WA S NOTIFIED. AIRCRAFT WAS REPOSITIONED TO THE MAINTENANCE HANGAR WHERE IT WAS NOTICED THAT OIL WAS LEAKING FROM THE COMP RESSOR SEALS ON BOTH ENGINES. MAINTENANCE REMOVED AND REPLACED BOTH COMPRESSOR SEALS, PERFORMED GROUND RUNS, CHECKED FO R LEAKAGE. AIRCRAFT COMPLETED THE REQUIRED MAINTENANCE ACCEPTANCE FLIGHT WITH NO FURTHER PROBLEMS. AIRCRAFT WAS THEN R ELEASED FOR SERVICE. (X) 2 L 7 2 4T 3 T RT A56EU E3WE 1998051500470 19980515 00470 EA 1998 5 15 VTZA98162 1 19980414 A 2740 601R92301 HSTCU COMPUTER CNDAIR CL600 CL6002B19 EA H STAB TRIM FAILED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 623BR 7192 IAD/TPA - FLT 6707 - DURING CLIMB ON 4-14-98, AIRCRAFT MADE UNSCHEUDLED LANDING AT IAD DUE TO BOTH STABILIZER TRIMS WILL NOT ENGAGE AND MACH TRIM FALLS OFF-LINE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AN D REMOVED AND REPLACED HSTCU COMPUTER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998051500471 19980515 00471 EU 1998 5 15 VTZA98145 1 19980325 A 3310 8G500537605 BULB JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 313UE 41026 FLT 6479 - ORF-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO RT CONSOLE LIGHTS SMOKING. MAINTENANCE INSPECTED AND OPENED DMI 57694, MEL 33-1 ON LIGHTS. MAINTENANCE CLOSED DMI 57694, BY REMOVING AND REPLACING CONSOLE LIGHT BULB. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998051500472 19980515 00472 WP 1998 5 15 EISA98085 1 19980413 A 3350 110049 BATTERY CHARGER DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A EISA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 943VJ 47058 FOUND SECTIONS 2 AND 3 FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. GENERATED BY PILOT REPORT. FOUND 3 CHAFED WIRES UNDER SEAT 14D. SPLICED TOGETHER WIRES AND RE-SEATED WIRE BUNDLE. ALSO, FOUND FORWARD AND AFT BATTERY CHARGERS INOPERATIVE F OR SECTIONS 2 AND 3 FLOOR PATH EMERGENCY LIGHTS. REMOVED AND REPLACED BOTH BATTERY CHARGERS. ALL SYSTEM OPS CHECK GOOD PER MM 33-5. (X) 2 L 7 2 4F A6WE 1998051500473 19980515 00473 EA 1998 5 15 VTZA98151 1 19980403 A 3230 RETRACT MECH CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A VTZA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 27 624BR 7211 IAD/IND - FLT 6724 - DURING APPROACH AT 1415 HRS ON 4-3-98, AIRCRAFT MADE ABORTED APPROACH INTO IND DUE TO LANDING GEAR FAILED TO EXTEND NORMALLY AND CREW USED EMERGENCY EXTENSION. AIRCRAFT LANDED AT IND AND WENT TO GATE WITH NO FURTHER PR OBLEMS. MAINTENANCE INSPECTED AND PERFORMED GEAR SWINGS AND COULD NOT DUPLICATE PROBLEM AND RECEIVED NO FAULT CODES. O PS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998051500474 19980515 00474 NE 1998 5 15 VTZA98155 2 19980414 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE ACTIVATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 320UE 41043 IAD/ILM - FLT 6623 - DURING CLIMB AT 1900 HRS ON 4-14-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING AT IAD DUE TO RT ENGINE O IL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED SMALL FUZZ OFF CHIP DETECTOR AND TOOK OIL SAMPLE AND GROUND RAN AIRCRAFT, OPS CHECK OK. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1998051500475 19980515 00475 1998 5 15 VTZA98163 4 19980415 A 3417 7858062 ADS CONTROLLER CNDAIR CL600 CL6002B19 EA E/E COMPARTMENT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 624BR 7211 IAD/BNA - FLT 6700 - DURING CRUISE AT 0745 HOURS ON 4-15-98, AIRCRAFT MADE UNSCHEDULED LANDING DUE TO TAT AND RT PITOT H EAT FAILURE. AIRCRAFT LANDED AT IND AND WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED A ND REPLACED AIR DATA SENSOR CONTROLLER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998051500476 19980515 00476 EU 1998 5 15 VTZA98143 1 19980329 A 2731 TRIM CONTROL JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT LACK OF LUBE A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 27 302UE 41013 EWR/BOS - FLT 6240 - DURING CRUISE AT 1740 HOURS ON 3-29-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT EWR DUE TO ELEVATOR TRIM STUCK. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND LUBED FRICTION LOCK CONTROLS AND LUBED ELEVATOR TRIM CONTROL, 0PS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998051500477 19980515 00477 WP 1998 5 15 AALA980633 1 19980326 A 3610 4102900S COUPLING DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 208AA 49159 BNA - FLT 0691 - DURING CLIMB-OUT AT 18,000 FEET, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. CREW FOLLOWED CH ECK LIST AND TAIL COMPARTMENT HIGH TEMPERATURE LIGHT EXTINGUISHED. AIRCRAFT AIR INTERRRUPTED AND RETURNED TO BNA WITHOU T FURTHER INCIDENT. REPLACED BROKEN COALESCER ASSEMBLY COUPLING AND AS A PRECAUTIONARY, REPLACED WATER SEPARATOR BAG. R AN ENGINES AND PACKS WITH NO LEAKS DETECTED AND TAIL COMPARTMENT HIGH TEMPERATURE LIGHT DID NOT ILLUMINATE. SYSTEM GROU ND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500478 19980515 00478 WP 1998 5 15 AALA980696 1 19980403 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 493AA 49731 DFW - FLT 0455 - DURING CLIMB-OUT, GEAR SELECTED UP, THE RED NOSE GEAR LIGHT REMAINED ILLUMINATED FOR APPROXIMATELY 4 MI NUTES AFTER TAKEOFF. AIRCRAFT AIR INTERRUPTED AND RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR UP SENS OR AND PERFORMED NOSE GEAR SWING AND POSITION CHECK WITH NORMAL RESULTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500479 19980515 00479 NE 1998 5 15 AALA980245 2 19980201 A 7250 808904 TURBINE BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE FAILED A A AALA E ENGINE SHUTDOWN E Y VIBRATION/BUFFET ENGINE STOPPAGE AP APPROACH 1 SW 07 274AA 49271 SAN - FLT 1147 - ON APPROACH TO SAN AT 2,000 FEET, CREW HEARD LOUD BANG, NR 2 ENG SHUT DOWN. LANDED WITHOUT INCIDENT. REPLACED NR 2 ENG. SYS GRND CHKED, NORMAL. CONFIRMED 4TH STAGE TURB BLADE FAILED ABOVE ROOT PLATFORM FROM HCF. FRACT URE ORIGIN LOCATED ON CONVEX OF AIRFOIL AT MID-CORD. FATIGUED AREA EXTENDS 2MM ACROSS BLADE (50 PERCENT OF THICKNESS) A ND 5.5MM TO EACH SIDE OF ORIGIN. BLADE PREVIOUSLY O/H AND CONVERTED TO WIDE NOTCH CONFIG PER SB 6090. BLADE HAS 5,480 HRS TSO AND AN ISOTOPE INSP ACCOMPLISHED 500 HRS PRIOR TO FAILURE WITH MINOR WEAR REPORTED. 2ND VANES HAD EVIDENCE OF A HOT SPOT AT 3:30 POSTION. NR 3 FUEL NOZZLE BURNT ALONG SUPPORT HEAT SHIELD. ENG PROCESSED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F 4 F A6WE E9NE 1998051500480 19980515 00480 NM 1998 5 15 AALA980605 1 19980326 A 3230 BACC2C3A03295FG CONTROL CABLE BOEING 767 767223 1385123 NM LANDING GEAR BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 308AA 22314 LAX - FLT 0280 - AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT WITH GEAR HANDLE IN THE UP POSITION. GEAR DISAGREE AND G EAR CONFIGURATION MESSAGES ILLUMINATED WITH GEAR INDICATING DOWN AND LOCKED WITH THREE GREEN LIGHTS. AIRCRAFT AIR INTER RUPTED AND RETURNED TO LAX AND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED BROKEN LANDING GEAR CONTROL CABLE AND ACCOM PLISHED OVERWEIGHT LANDING INSPECTION WITH NO DISCREPANCIES NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F RT A1NM 1998051500481 19980515 00481 NM 1998 5 15 AALA980716 1 19980405 A 3240 015T143312 ROD BOEING 767 767323 1385205 NM RT MLG BRAKE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 362AA CPT4863NTW 24043 GRU FLT 0998 - AFTER TAKEOFF, GEAR DISAGREE AND GEAR DOOR MESSAGE APPEARED ON EICAS ALONG WITH UNSAFE GEAR AND GEAR DOO R LIGHTS ILLUMINATED. AIRCRAFT AIR INTERRUPTED AND RETURNED GRU AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. OVERWE IGHT LANDING INSPECTION ACCOMPLISHED WITH NO DAMAGE NOTED. HIGH ENERGY STOP INSPECTION ACCOMPLISHED WHICH REVEALED DAMA GE TO NR 8 MLG HYDRAULIC LINE, BRAKE AND WHEEL ASSEMBLIES DUE TO A FAILED BRAKE ROD RETAINING BOLT AND PIN. REPLACED ML G WHEEL/BRAKE ASSEMBLIES, BRAKE ROD/PIN, AND BRAKE HYDRAULIC LINE. SYSTEM GROUND AND LEAKED CHECKED NORMAL OPERATION. ( X) 2 L 7 2 4F RT A1NM 1998051500482 19980515 00482 WP 1998 5 15 AALA980715 1 19980407 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 432AA 49350 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS ALONG FIRST CLASS GALLEY FOUND INOPERATIVE. REPLAC ED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AND JUMPERS ALONG FIRST CLASS GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500483 19980515 00483 WP 1998 5 15 AALA980712 1 19980407 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 432AA 49350 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD GALLEY FOUND INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500484 19980515 00484 WP 1998 5 15 AALA980702 1 19980406 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 227AA 49177 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM PASSENGER SEAT ROW 22 AFT FOUND INOPERATIVE. RECONNECTED DISCONNECTED CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP SEAT ROW 22. SYSTEM GROUND CHECKED, NORMA L OPERATION. (X) 2 L 7 2 4F A6WE 1998051500485 19980515 00485 WP 1998 5 15 AALA980704 1 19980406 A 3350 A3060720102 CONDUCTOR DOUG DC9 DC982 3022082 WP CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 285AA 49297 SFO - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY FLOOR PATH LIGHTING FROM SEAT ROW 25 DEF THROUGH FIRST CLASS FOUND I NOPERATIVE. REPLACED CORRODED SECTION OF EMERGENCY EXIT PATH LIGHT STRIP CONDUCTOR ASSEMBLY AT SEAT ROW 3 EF. SYSTEM G ROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500486 19980515 00486 WP 1998 5 15 AALA980745 1 19980410 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 573AA 53092 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD OVERWING EXIT FOUND INOPERATIVE. REPL ACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD OVERWING EXIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500487 19980515 00487 WP 1998 5 15 AALA980736 1 19980410 A 3610 5953625521 DUCT DOUG DC9 DC983 3022083 WP AFT ACCESSORY RUPTURED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 562AA 49344 DFW - FLT 1396 - AFTER TAKEOFF DFW DURING CLIMB-OUT THROUGH FL 230, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURES AND AIRCRAFT RETURNED TO DFW LANDING WITHOUT INCIDENT. REPLACED RUPTURED DUCT ASSY. SYSTEM LEAK CHECKED AND OPERATED NORMALLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998051500488 19980515 00488 WP 1998 5 15 AALA980738 1 19980410 A 3350 4TL1110B SWITCH DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3515 49892 BOS - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY LIGHT SWITCH WOULD NOT ILLUMINATE EMERGENCY LIGHTS. 2 L 7 2 4F A6WE 1998051500489 19980515 00489 WP 1998 5 15 AALA980748 1 19980410 A 3610 CLAMP DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 422AA 49334 MCO - FLT 0626 - EN ROUTE FLL/LGA, TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED AND ACFT DIVERTED AND LANDED OVER WEIGHT MCO WITHOUT FURTHER INCIDENT. OVERWEIGHT INSPECTION ACCOMPLISHED WITH NO DAMAGE NOTED. TAIL COMPARTMENT DUCTING INSPECTED AND RIGHT AUGMENTATION INBD AND OTBD VALVE CLAMPS RE-TORQUED. SYSTEM PLACARDED AND ACFT FERRIED TO TULSA FOR FURTHER EVALUATION PER SPOTTING MESSAGE 04-049. TULSA MAINTENANCE INSPECTED AND FOUND A CLAMP ON THE CROSSOVER DUCT BE LOW ANTI-ICE HIGH TEMPERATURE SWITCH LOOSE. TIGHTENED CLAMP ON CROSSOVER DUCT AND SYSTEM LEAK CHECKED GOOD. FUNCTIONAL CHECK FLIGHT REVEALED NO FURTHER LEAKS OR TAIL COMPARTMENT INDICATIONS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500490 19980515 00490 WP 1998 5 15 AALA980749 1 19980412 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7532A 49924 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS FOUND INOPERATIVE. REPLACED EMERGEN CY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500491 19980515 00491 WP 1998 5 15 AALA980697 1 19980404 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 471AA 49601 PHX - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHTING NEAR PASSENGER SEAT 16D FOUND INOPERATIVE. REPAIRED E MERGENCY FLOOR PATH LIGHT STRIP AT PASSENGER SEAT 16D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500492 19980515 00492 WP 1998 5 15 AALA980700 1 19980405 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7547A 53029 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT FIRST CLASS GALLEY FOUND INOPERATIVE. R EPLACED EMERGENCY EXIT FLOOR PATH LIGTH STRIP AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998051500493 19980515 00493 NM 1998 5 15 AALA980691 1 19980402 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING BETWEEN PASSENGER SEAT ROWS 25H THROUGH 31H FOUND INOPE RATIVE. REPAIRED SHORTED EMERGENCY EXIT PATH LIGHT WIRE AT PASSENGER SEAT ROW 27H. SYSTEM GROUND CHECKED, NORMAL OPERA TION. (X) 2 L 7 2 4F RT A1NM 1998051500494 19980515 00494 NM 1998 5 15 AALA980658 1 19980401 A 3350 1721651 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352AA 24033 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 24 AB FOUND INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 24 AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998051500495 19980515 00495 NE 1998 5 15 98ZZZX1746 2 19980429 A 7250 430203802 BEARING 400100025 BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE FAILED B BAQR K NONE O OTHER IN INSP/MAINT 1 EA 03 213AE 122 7219 LE45584 BEARING, WHICH IS PART OF THE POWER TURBINE THRUST SYSTEM AND INSTALLED IN THE ENGINE 121.6 HOURS EARLIER BY THE INCORPO RATION OF SB LT 101-72-50-0174, FAILED 2.8 HOURS AFTER BEING RE-INSTALLED AFTER MAJOR MAINTENANCE. THE SUSPECT BEARING WAS INSPECTED PRIOR TO INSTALLATION. NO ANOMALIES NOTED AT THAT TIME. THE ENGINE EXPERIENCED SEVERAL CHIP EVENTS ON TH E (FORWARD) FULL FLOW CHIP DETECTOR, THE ENGINE WAS REMOVED. 1 G 7 2 3U 3 U H13EU E5NE10 1998051500497 19980515 00497 GL 1998 5 15 HEEA0014112 2 19980504 A 7250 6886407 WHEEL 6898735 BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL 1ST STAGE SULFIDATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81982 1056 CAT40070 S818 CAE800670F ENGINE REMOVED DUE TO COMPRESSOR IMPELLER CYCLES. TURBINE DISASSEMBLED DUE TO LOW POWER ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED: MINOR SULPHIDATION ON ALL BLADES OF NR1 WHEEL. SCRAPPED #1 WHEEL. 1 G 7 2 3U 3 U H3EU E4CE 1998051500498 19980515 00498 SW 1998 5 15 HEEA0014113 1 19980504 A 6322 206061432109 BLOWER IMPELLER 206040370103 BELL 206 206L1 1182107 SW COOLING FAN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B BT561 45598 BLOWER IMPELLER HAS EXCESSIVE CORROSION. SCRAPPED AND REPLACED WITH NEW ASSY. 1 G 7 1 3U H2SW 1998051500499 19980515 00499 SW 1998 5 15 HEEA0014114 1 19980504 A 6322 206061432109 BLOWER IMPELLER 206040370103 BELL 206 206L1 1182107 SW COOLER FAN CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 HCBXL PHI140 45219 BLOWER IMPELLER HAS EXCESSIVE CORROSION. SCRAPPED AND REPLACED WITH NEW ASSY. 1 G 7 1 3U H2SW 1998051500500 19980515 00500 NE 1998 5 15 HEEA0014115 1 19980504 A 2430 7655009006106 CONTROL UNIT SKRSKY S76 S76A 8143006 NE DC SYS DAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 5128 760181 CONTROL UNIT WILL NOT TURN ON GENERATOR. 1 G 7 2 3U H1NE 1998051500501 19980515 00501 SW 1998 5 15 HEEA0014116 1 19980504 A 6240 KDW021 RPM WARNING BOX BELL 206 206L3 1182108 SW M/R FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 42EA 51542 RPM WARNING FLAG DOES NOT DROP WHEN POWER APPLIED. 1 G 7 1 3U H2SW 1998051500502 19980515 00502 EU 1998 5 15 HEEA0014117 1 19980504 A 2422 412075101101 INVERTER BOLKMS 105 BO105S 5626006 EU AC SYS MALFUNCTION E HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 3071K S859 450VA INVERTER INTERMITTENT WARNING IN FLIGHT. 1 G 7 2 3U H3EU 1998051500503 19980515 00503 1998 5 15 HEEA0014118 4 19980504 A 3421 206075607103 ATTITUDE GYRO BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 293CA 33005 ATTITUDE GYRO INOPERATIVE. 1 G 7 2 4U H4SW 1998051500504 19980515 00504 SW 1998 5 15 HEEA0014119 1 19980504 A 2430 51509002R CONTROL UNIT BELL 412 412 1182202 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 CONTROL UNIT WOULD NOT ALLOW NR1 GENERATOR TO COME ON LINE. 1 G 7 2 4U H4SW 1998051500505 19980515 00505 SW 1998 5 15 HEEA0014120 1 19980504 A 7722 3030083 TRIM COMPENSATOR BELL 412 412 1182202 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 TRIM COMPENSATOR WILL NOT ADJUST. 1 G 7 2 4U H4SW 1998051500506 19980515 00506 SW 1998 5 15 HEEA0014121 1 19980504 A 2822 9A1746 CARTRIDGE BELL 214 214ST 1182106 SW BOOST PUMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 A/C STUD BROKEN OFF. 2 G 7 2 4U H10SW 1998051500507 19980515 00507 SW 1998 5 15 HEEA0014122 1 19980505 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 STARTER INOPERATIVE. 2 G 7 2 4U H10SW 1998051500508 19980515 00508 SW 1998 5 15 HEEA0014123 1 19980505 A 2435 2CM272B1 STARTER BELL 214 214ST 1182106 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 28139 STARTER GEN WILL NOT SPIN. 2 G 7 2 4U H10SW 1998051500509 19980515 00509 EU 1998 5 15 HEEA0014125 1 19980506 A 2821 402A124 ELEMENT SNIAS 350 AS350B2 8680813 EU FUEL FILTER CLOGGED E HEEA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 03 40466 3004 FUEL FILTER LIGHT FLICKERED TWICE IN FLIGHT. 1 G 7 1 3U H9EU 1998051500510 19980515 00510 EU 1998 5 15 HEEA0014126 1 19980507 A 7712 3005731365 INDICATOR SNIAS 350 AS350B2 8680813 EU ENG TORQUE ERRATIC E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 2873 TORQUE INDICATOR READING VERY ERRATIC. 1 G 7 1 3U H9EU 1998051500511 19980515 00511 EU 1998 5 15 HEEA0014127 1 19980507 A 5210 350A25125004 HANDLE SNIAS 350 AS350B2 8680813 EU DOOR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 NO CORES AVAILABLE. 1 G 7 1 3U H9EU 1998051500512 19980515 00512 EU 1998 5 15 HEEA0014128 1 19980507 A 5210 350A2513500901 CYLINDER LOCK SNIAS 350 AS350B2 8680813 EU DOOR DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 NO CORES AVAILABLE. 1 G 7 1 3U H9EU 1998051500513 19980515 00513 EU 1998 5 15 HEEA0014129 1 19980507 A 6310 350A35105901 COUPLING SNIAS 350 AS350B2 8680813 EU ENG/XMSN CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4000L 2873 COUPLING BUSHES DISC CRACKED. 1 G 7 1 3U H9EU 1998051500514 19980515 00514 GL 1998 5 15 HEEA0014130 2 19980507 A 7320 VSB628CP FADEC HORN BELL 407 407 SW ALLSN 250C 250C47B GL COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 457PH 53147 FADEC FAIL HORN SOUNDS WEAK. 1 G 7 1 3U 3 U O H2SW E1GL 1998051500515 19980515 00515 SW 1998 5 15 HEEA0014131 1 19980507 A 6340 222375077115 TRANSDUCER BELL 407 407 SW ROTOR INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 TRANSDUCER INTERMITTENT ZERO OUTPUT. 1 G 7 1 3U O H2SW 1998051500516 19980515 00516 SW 1998 5 15 HEEA0014132 1 19980507 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998051500517 19980515 00517 SW 1998 5 15 HEEA0014133 1 19980507 A 6300 407040104101 ADAPTER BELL 407 407 SW M/R LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 437PH 53072 ADAPTER SEAL LEAKS. 1 G 7 1 3U O H2SW 1998051500518 19980515 00518 SW 1998 5 15 HEEA0014134 1 19980507 A 6300 400040055109 HOUSING BELL 407 407 SW M/R LEAKS E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 HOUSING SEAL LEAKS. 1 G 7 1 3U O H2SW 1998051500519 19980515 00519 SW 1998 5 15 HEEA0014135 1 19980507 A 6320 206040156001 SEAL ASSY BELL 407 407 SW TRANSMISSION LEAKS E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 437PH 53072 SEAL LEAKS. 1 G 7 1 3U O H2SW 1998051500619 19980515 00619 NM 1998 5 15 98FDEA00337 1 19980508 A 2120 AIR DISTRIBUTION BOEING 727 727227 1384078 NM COCKPIT ODOR A FDEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 495FE 21669 AFTER TAKEOFF HAD STRONG BURNING SMELL IN COCKPIT FOR ABOUT 10 MINUTES DURATION. RAN BOTH PACKS FOR 20 MINUTES WITH NO SMELL COMING OUT OF AIR VENTS. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998051500620 19980515 00620 EU 1998 5 15 98FDEA00338 1 19980510 A 2170 COALESCER BAGS AIRBUS 300 A300F4605R 3930327 EU NR 2 PACK CONTAMINATED A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 650FE 726 ON CLIMBOUT, MULTIPLE SMOKE INDICATIONS AND A STRONG ODOR, SMOKE INDICATION ILLUMINATED. SHUT OFF NR 2 PACK, ODOR REMAI NED. DIVERTED TO KORD. INSP A/C PER M/M 05-51-25-0 FOUND SMALL PARTICLES OF RUBBER/ASPHALT ON FWD BELLY OF A/C. CLEAN ED OFF, REPLACED BOTH WATER SEPARATOR BAGS, RAN PACKS WITH APU AND ENGINES. RUBBER SMELL DISSIPATED. 2 L 7 2 4F RT A35EU 1998051500621 19980515 00621 NM 1998 5 15 DL72S980959 1 19980421 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 ACTUATOR ATTACH BRACKET CRACKED FWD LOWER INBD CORNER OF NR 5 KRUEGER FLAP. REPAIRED PER M/M 57-20-21 FIG 807. 2 L 7 3 4F A3WE 1998051500622 19980515 00622 NM 1998 5 15 DL72S980960 1 19980506 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 525DA 21585 DURING L/O, CHK TEST EMERG LT AFT TRACK AND OVHD LT FAILED. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998051500623 19980515 00623 NM 1998 5 15 DL72S980961 1 19980421 A 5311 FRAME BOEING 727 727232 1384082 NM BS 950 BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 FOUND AT HMV, FRAME BENT STA 950E BETWEEN STR 26L-27L. STARTED REPAIR PER SRM 53-10-4, COMPLETED REPAIR PER SRM 53-10- 4. 2 L 7 3 4F A3WE 1998051500624 19980515 00624 NM 1998 5 15 DL72S980965 1 19980506 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND AT A2 LETTER CHECK, VERTICAL STAB STRINGER 6L CRACKED AT BOLT HOLE FIN STA 157.2. REPAIRED PER M/M 55-30-0. 2 L 7 3 4F A3WE 1998051500625 19980515 00625 NM 1998 5 15 DL72S980966 1 19980421 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 6 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 AT HMV, FOUND RW ACTUATOR BRACKET CRACKED NR 6 KRUEGER FLAP ACTUATOR BRACKET LOWER O/B FWD CORNER. REMOVED ACT AND BEAM PER MM 57-20-21, STOP DRILLED CRACK, INSTALLED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998051500626 19980515 00626 NM 1998 5 15 DL72S980967 1 19980421 A 5720 ANGLE BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 ANGLE CRACKED IN WING LEADING EDGE, INBD END NR 3 KRUEGER FLAP. DYE CKD TO CONFIRM CRACK. STOP DRILLED, FABD DOUBLER P ER SRM 51-40-3, C/W MM 57-20-21 FIG 807. 2 L 7 3 4F A3WE 1998051500627 19980515 00627 NM 1998 5 15 DL72S980968 1 19980507 A 5754 SKIN BOEING 727 727232 1384082 NM NR 3 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 A 1.5 INCH CRACK AT NR 3 L/E FLAP I/B LIP HINGE CUTOUT. REPAIRED PER M/M 57-53-0 AND ERA 364735-14. 2 L 7 3 4F A3WE 1998051500628 19980515 00628 NM 1998 5 15 DL72S980969 1 19980507 A 2761 FITTING BOEING 727 727232 1384082 NM NR 3 SPOILER ACT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 NR 3 SPOILER O/B ACTUATOR ATTACH CASTING BROKEN. REPLACED FITTING PER M/M 57-42-0. 2 L 7 3 4F A3WE 1998051500629 19980515 00629 NM 1998 5 15 DL72W980970 1 19980415 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 FLOORBEAM CORRODED STA 344 BL 0. REMOVED CORROSION PER SRM 51-10-3. OUT OF LIMITS PER SRM 53-10-1 FIG 4. REMOVED ANGL E SUPPORTS, STARTED MANUFACTURING NEW SUPPORT. BEGAN REMOVAL OF T-CAP. COMPLETED REMOVAL OF T-CAP. DRILLED UP NEW T- CAP, EXCEPT TOP OF SPLICE. 2 L 7 3 4F A3WE 1998051500630 19980515 00630 NM 1998 5 15 DL72W980971 1 19980415 A 5512 PANEL BOEING 727 727247 138408F NM HORIZ STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 HORIZONTAL STABILIZER T/E LT SIDE HAS HOLE PUNCHED IN THE UPPER PANEL APPROX 10 INCHES INBD OF ELEVATOR POWERPACK CUTOUT . REMOVED DAMAGE WITH .375 DIA HOLE. DYE CHECKED, NO CRACKS FOUND. MANUFACTURED REPAIR PER SRM 55-10-3 FIG 3. INSTAL LED REPAIR PER SRM 55-10-3 FIG 3. REMOVED PANEL 9114 FOR ACCESS REPAIR. OK TO CLOSE. INSTALLED PANEL 9114. 2 L 7 3 4F A3WE 1998051500631 19980515 00631 NM 1998 5 15 DL72W980972 1 19980422 A 5350 FAIRING BOEING 727 727247 138408F NM BS 957 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 ANGLE OUT AT STA 957 LT SIDE OF FUSELAGE OVER STA 18A. FAIRING ATTACH WEB CRACKED REF EO 4-60175-3. STARTED FABRICATIN G REPAIR AS PER M/M 53-12-0 FIG 1. FABRICATED REPAIR PER M/M 53-12-0. HEAT TREATED REPAIR PORTS PER PS 900-4-1 NR 1. O K TO INST SPLICE ANGLES. INSTALLED SPLICE REPAIR IAW M/M, FABRICATED WEB PER SRM 51-00. INSTALLED WEB PER SRM 51-00. 2 L 7 3 4F A3WE 1998051500632 19980515 00632 NM 1998 5 15 DL72W980973 1 19980414 A 2782 BRACKET BOEING 727 727247 138408F NM NR 2 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 BRACKET CRACKED NR 1 KRUEGER ACTUATOR SUPPORT BRACKET AT I/B LOWER CORNER. REMOVED FASTENERS TO FACILITATE DOUBLER AND STOP DRILLED CRACK PER M/M 57-20-21 PG 811. FABRICATED DOUBLER PER M/M 57-20-21 PG 811. INSTALLED DOUBLER PER MM 57-2 0-21 FIG 807. 2 L 7 3 4F A3WE 1998051500633 19980515 00633 NM 1998 5 15 DL72S980974 1 19980507 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 21145 AFT GALLEY OVERHEAD EXIT SIGN INOP. REPLACED POWER PACK. 2 L 7 3 4F A3WE 1998051500634 19980515 00634 NM 1998 5 15 DLM88980975 1 19980508 A 2170 COALESCER BAG DOUG MD88 MD88 3023688 NM CABIN ICED UP A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 947DL 49878 ON CLIMBOUT, BOTH SMOKE DETECTORS IN AFT LAVS WENT OFF AND SMELL OF HOT AIR ODOR IN CABIN. CABIN SUPPLY TEMP 65 DEGS, B OTH ENG HAD A/I ON. HP OFF, NO HELP. A/I OFF AND TEMP RTN TO NORMAL. REPLACED COALESCER BAGS DUE ICING. 2 L 7 2 4F RT A6WE 1998051500635 19980515 00635 NM 1998 5 15 DL72L980976 1 19980508 A 2782 1U11032 ACTUATOR BOEING 727 727232 1384082 NM NR 4 LE SLAT FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 512DA 21314 LOST ALL A-SYSTEM HYDRAULIC FLUID. REPLACED NR 4 SLAT ACTUATOR. 2 L 7 3 4F A3WE 1998051500636 19980515 00636 NM 1998 5 15 DL72E980979 1 19980508 A 5522 SKIN BOEING 727 727247 138408F NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 FOUND ON C1 LETTER CK, TWO .75 INCH CRACKS IN THE RT ELEVATOR LOWER SKIN LOWER FWD EDGE OF ELEVATOR. REPAIRED PER SRM 5 5-20-3. 2 L 7 3 4F A3WE 1998051500637 19980515 00637 NM 1998 5 15 DL72E980980 1 19980508 A 2782 BRACKET BOEING 727 727247 138408F NM NR 1 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 NR 1 SLAT ACTUATOR MOUNT BRACKET CRACKED 1.5 INCH VISIBLE O/B END. REPAIRED PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998051500638 19980515 00638 WP 1998 5 15 DLL19980988 1 19980510 A 2761 GASKET LKHEED 1011 10113853 5265020 WP NR 5 SPOILER ACT TORN A DALA O OTHER K FLUID LOSS CR CRUISE 1 SO 27 756DR 193Y1185 LOSS OF C-SYS HYD FLUID DUE TO RT NR 5 SPOILER HYD LK. LANDING GEAR WAS MANUALLY EXTENDED. REPLACED SEAL ON NUMBER 5 S POILER ACTUATOR. 2 L 7 3 4F A23WE 1998051500639 19980515 00639 NM 1998 5 15 DL72K980989 1 19980510 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 472DA 14495 20749 RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998051500640 19980515 00640 WP 1998 5 15 DLL14980990 1 19980510 A 3350 672320101 POWER SUPPLY LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 193C1244 L1 AND L3 EMER SLIDE LGTS INOP. REPLACED PWR SUPPLY, CKS GOOD. 2 L 7 3 4F A23WE 1998051500641 19980515 00641 NM 1998 5 15 DHL9870701C 1 19980420 A 5712 RIB BOEING 727 72722 1384002 NM WS 338 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, LEADING EDGE COVE RIB IS CRACKED AT FRONT SPAR STATION 338 ON OUTBD SIDE. REMOVED AND REPLACED ATTACH ANGL E PER SRM 51-40-3, 20 X 1.5 X 1.5. N/R 1027 2 L 7 3 4F A3WE 1998051500642 19980515 00642 NM 1998 5 15 DHL9870702C 1 19980420 A 5730 SKIN BOEING 727 72722 1384002 NM WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, NR 3 SLAT INBD TRACK CUTOUT IN WING LEADING EDGE IS CRACKED. STOP DRILL, HFEC, INSTALLED DOUBLER REPAIR PE R SRM 51-10-1, 6 X 10. N/R 1016 2 L 7 3 4F A3WE 1998051500643 19980515 00643 NM 1998 5 15 DHL9870703C 1 19980422 A 5712 RIB BOEING 727 72722 1384002 NM WS 656 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, RT WING PREV REPAIR DOUBLER CRACKED ON RIB WS 656 LOWER FLANGE AT SECOND FROM AFT STRINGER. REPLACED PREVIO US DOUBLER PER SRM 57-10-5, 8 X 3.25 X 1 X 1. N/R 2844 2 L 7 3 4F A3WE 1998051500644 19980515 00644 NM 1998 5 15 DHL9870704C 1 19980422 A 5712 RIB BOEING 727 72722 1384002 NM WS 546 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, RT WING RIB WS 546 CRACKED AT TOP FLANGE AT THIRD FROM AFT STRINGER. STOP DRILLED CRACK, HFEC, INSTALLED D OUBLER REPAIR PER SRM 57-10-5, 2 X 1 X 1. N/R 2843 2 L 7 3 4F A3WE 1998051500645 19980515 00645 NM 1998 5 15 DHL9870705C 1 19980422 A 5730 PANEL BOEING 727 72722 1384002 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, RT WING L/E AT NR 7 SLAT, ACCESS PANEL 8 INBD OF SLAT ACTUATOR HAS SEVERAL CRACKS. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2, 9 X 7. N/R 2842 2 L 7 3 4F A3WE 1998051500646 19980515 00646 NM 1998 5 15 DHL9870706C 1 19980422 A 5754 ANGLE BOEING 727 72722 1384002 NM NR 5 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, NR 5 SLAT THE INBD SLAT TO TRACK ATTACH ANGLES ARE CRACKED. REPLACED ATTACH ANGLES PER SRM 51-40-4, 4.25. N /R 2808 2 L 7 3 4F A3WE 1998051500647 19980515 00647 NM 1998 5 15 DHL9870707C 1 19980421 A 5720 652165833 CHANNEL BOEING 727 72722 1384002 NM WS 491 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, R/W OUTBD T/E FLAP WELL T/E LOWER PANEL SUPPORT INBD CHANNEL AT WS 491 CRACKED. REPLACED CRACK PER SRM 51- 30-2. N/R 2797 2 L 7 3 4F A3WE 1998051500648 19980515 00648 NM 1998 5 15 DHL9870708C 1 19980421 A 5720 ANGLE BOEING 727 72722 1384002 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, RT WING L/E LOWER COVE PANEL SIDE ATTACH ANGLE L/E 130 IS CRACKED AT ATTACH FASTENERS. INSTALLED NEW ANGLE PER SRM 51-40-3, 24 X 12. N/R 2783 2 L 7 3 4F A3WE 1998051500649 19980515 00649 NM 1998 5 15 DHL9870709C 1 19980421 A 5755 FITTING BOEING 727 72722 1384002 NM NR 10 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CRACK INDICATION AT R/W INBD T/E FLAP CAVITY NR 10 SPOILER OUTBD HINGE SUPPORT FITTING. REMOVED AND REPLAC ED FITTING PER SRM 51-30-2. N/R 2778 2 L 7 3 4F A3WE 1998051500650 19980515 00650 NM 1998 5 15 DHL9870710C 1 19980421 A 5720 ANGLE BOEING 727 72722 1384002 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CRACKED UPPER SKIN SUPPORT ANGLE AT R/W INBD TRAILING EDGE CAVITY, JUST FWD OF INBD AILERON. REPLACED ANGLE PER SRM 51-40-3, 4 X 2.5. N/R 2776 2 L 7 3 4F A3WE 1998051500651 19980515 00651 NM 1998 5 15 DHL9870711C 1 19980421 A 5532 PANEL BOEING 727 72722 1384002 NM VERT STAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, TAIL ACCESS PANEL 9705 SHOWS SIGNS OF DELAMINATION. INSTALLED REPAIR PER SRM 51-40-8, 24 X 15. N/R 4805 2 L 7 3 4F A3WE 1998051500652 19980515 00652 NM 1998 5 15 DHL9870713C 1 19980420 A 5230 HINGE BOEING 727 72722 1384002 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 MAIN CARGO DOOR UPPER HINGE CRACKED LUG AT AFT END. REMOVED AND REPLACED HINGE PER SRM 51-30-2. N/R 3529 2 L 7 3 4F A3WE 1998051500653 19980515 00653 NM 1998 5 15 DHL9870714C 1 19980421 A 5320 BRACKET BOEING 727 72722 1384002 NM BS 945 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, SUPPORT BRACKET CRACKED AT STRINGER 18A LT FS 945 AS VIEWED FROM TOP OF WING. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-20-2. N/R 3645 2 L 7 3 4F A3WE 1998051500654 19980515 00654 NM 1998 5 15 DHL9870715C 1 19980421 A 5210 SKIN BOEING 727 72722 1384002 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, FWD ENTRY DOOR LOWER BOTTOM FWD EDGE OF DOOR INNER SKIN BENT INWARD AND CRACKED. STOP DRILLED, HFEC AND INS TALLED DOUBLER REPAIR PER SRM 51-40-3, 4 X 5. N/R 3666 2 L 7 3 4F A3WE 1998051500655 19980515 00655 NM 1998 5 15 DHL9870716C 1 19980428 A 5312 BULKHEAD BOEING 727 72722 1384002 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT APPROX RBL 12 WL 185. STOP DRILLED END OF CRACK, HFEC, INSTALLED DOUBLE R REPAIR PER SRM 53-10-9, 12 X 5. N/R 3711 2 L 7 3 4F A3WE 1998051500656 19980515 00656 NM 1998 5 15 DHL9870717C 1 19980428 A 5312 BULKHEAD BOEING 727 72722 1384002 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT APPROX RBL 22 WL 185. STOP DRILLED ENDS OF CRACK, HFEC, INSTALLED DOUBL ER REPAIR 12 X 5. N/R 3713 2 L 7 3 4F A3WE 1998051500657 19980515 00657 NM 1998 5 15 DHL9870718C 1 19980420 A 5330 SKIN BOEING 727 72722 1384002 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CRACKS IN RADUIS AND CORROSION IS PRESENT AT CIRCUMFERENTIAL AT BS 480, OUTBD OF STR 27L AFT IN E AND E COM PT. STOP DRILL CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-3. 7 X 5'. INSTALLED ANGLE PER SRM 51-40-3, 3 X 2. N/R 3513 2 L 7 3 4F A3WE 1998051500658 19980515 00658 NM 1998 5 15 DHL9870719C 1 19980421 A 5220 69335421 FITTING BOEING 727 72722 1384002 NM RT EMER EXIT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT D-CHECK, RT AFT EMERGENCY CUTOUT EXIT HAS LOWER CENTER LOCK FITTING CRACKED. REPLACED FITTING PER SRM 51-30-2. N/R 3581 2 L 7 3 4F A3WE 1998051500659 19980515 00659 NM 1998 5 15 DHL9870720C 1 19980420 A 3231 LINKS BOEING 727 72722 1384002 NM NLG DOOR CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, NLG WHEEL WELL DOORS ACTUATING MECHANISM ACTUATION ROD, QUADRANT, LINKS ARE CHAFED SEVERELY AT FWD BULKHEAD . REMOVED AND REPLACED MECHANISM AND LINK PER MM 32-21-21. N/R 3577 2 L 7 3 4F A3WE 1998051500660 19980515 00660 NM 1998 5 15 DHL9870721C 1 19980420 A 5230 HINGE BOEING 727 72722 1384002 NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, MCD UPPER HINGE CRACKED LUG AT 2ND FROM FWD END. REMOVED AND REPLACED HINGE PER SRM 51-30-2. N/R 3528 2 L 7 3 4F A3WE 1998051500661 19980515 00661 NM 1998 5 15 DHL9870722C 1 19980423 A 5330 SKIN BOEING 727 72722 1384002 NM BS 1275 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, 3 DENTS IN EMPENNAGE SKIN JUST ABOVE STR 8R, ONE AT BS 1275 AND TWO AT BS 1285. CUT OUT DAMAGED AREAS AND I NSTALLED DOUBLER REPAIR PER SRM 53-30-3, 27 X 17. N/R 4845 2 L 7 3 4F A3WE 1998051500662 19980515 00662 NM 1998 5 15 DHL9870723C 1 19980423 A 5543 TAB BOEING 727 72722 1384002 NM RUDDER DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, LOWER RUDDER TAB SEPARATING AT LOWER RT AFT EDGE. INSTALLED REPAIR PER SRM 51-40-8, 15 X 15. N/R 4840 2 L 7 3 4F A3WE 1998051500663 19980515 00663 NM 1998 5 15 DHL9870724C 1 19980422 A 5320 FRAME BOEING 727 72722 1384002 NM GALLEY DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CABIN HORIZIONTAL SIDEWALL PANEL SUPPORT FRAME IS CRACKED AT GALLEY DOOR FORWARD CUT OUT FRAME ATTACHMENT JU ST ABOVE UPPER DOOR HINGE. INSTALLED DOUBLER PER SRM 51-40-2, 6 X 3. N/R 5592 2 L 7 3 4F A3WE 1998051500664 19980515 00664 NM 1998 5 15 DHL9870725C 1 19980422 A 5347 SEAT TRACK BOEING 727 72722 1384002 NM BS 540 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CABIN SEAT TRACK CORRODED AT STA 540 LBL 24. CUT OUT DAMAGED SECTION, INSTALLED NEW TRACK PER SRM 53-10-5. N/R 5586 2 L 7 3 4F A3WE 1998051500665 19980515 00665 NE 1998 5 15 VNAA9805004 3 19980505 A 6110 PROPELLER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DAMAGED A VNAA K NONE O OTHER NR NOT REPORTED 1 GL 07 440JS 37945 2914 3058 DURING THE POST FLIGHT INSPECTION, THE CREW FOUND EVIDENCE OF A LIGHTNING STRIKE ON THE LEFT HAND PROPELLER. MAINTENANC E INSPECTED AND REPLACED THE LEFT HAND PROPELLER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00. THE AIRCRAFT W AS THEN INSPECTED AND APPROVED FOR A FERRY FLIGHT TO DAY, FOR FURTHER MAINTENANCE. THE FERRY FLIGHT TOOK PLACE WITHOUT I NCIDENT. DAY MAINTENANCE COMPLETED A LIGHTNING STRIKE INSPECTION IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-51-02, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998051500666 19980515 00666 NM 1998 5 15 TWAA9804902 1 19980401 A 3350 582243 BATTERY PACK BOEING 767 7673Q8 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 JFK - DURING OVERNIGHT MAINTENANCE, FOUND THE L3 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK. ( X) 2 L 7 2 4F RT A1NM 1998051500692 19980515 00692 EU 1998 5 15 98ZZZX1772 1 19980401 A 7714 1179405603 INDICATOR BOLKMS 117 BK117A1 5626010 EU ENG NG FAILED B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 117M 145 S7023 NG INDICATOR INTERMITTENT OPERATION. AT TIMES, WILL NOT MOVE OFF ZERO. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 1998051500694 19980515 00694 EU 1998 5 15 98ZZZX1774 1 19980314 A 2612 542112538 FIRE LOOP AIRBUS 320 A320231 3930325 EU NR 1 ENGINE CHAFED A P9RA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 09 EITLI 8790 405 NR 1 ENGINE FIRE WARNING OVERHEAD PANEL ONLY. INSPECTED ENGINE PER AMM 2C-O0-00, FOUND ENGINE FAN FIRE LOOPS A/B CHAFED APPROXIMATELY ONE-HALF DIAMETER. REMOVED AND REPLACED NR 1 ENGINE FAN FIRE LOOP ASSY PER AMM 26-12-15. FOUND ALL GROU ND TESTS SATISFACTORY WITH NO FAULTS. 2 L 7 2 4F RT A28NM 1998051500695 19980515 00695 WP 1998 5 15 TWAA9806102 1 19980219 A 5320 SOCKET DOUG DC9 DC982 3022082 WP EMERGENCY EXIT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929TW 48014 MCI - DURING MODIFICATION VISIT, FOUND LT FORWARD OVERWING EXIT FORWARD LOCK PIN SOCKET CRACKED ON THE LOWER OVERWING EX IT FRAME. REPAIRED PER SRM 53-05, FIG 32A. ACFT TT: 37,475 HOURS. ACFT TC: 34,855. (X) 2 L 7 2 4F A6WE 1998051500696 19980515 00696 WP 1998 5 15 ORJA9857 1 19980301 A 3350 EM1267 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 805RA 48087 NUMEROUS OVERHEAD EMERGENCY LIGHTS INOPERATIVE INCLUDING OVERWING AND TAIL CONE LIGHTS. REMOVED AND REPLACED BATTERIES FOR OVERWING AND CEILING EMERGENCY LIGHTS. OPS CHECK GOOD. (X) 2 L 7 2 4F A6WE 1998051500697 19980515 00697 NM 1998 5 15 ORJA9869 1 19980409 A 2560 SLIDE DOUG MD90 MD9030 3023690 NM GALLEY DOOR LOOSE A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 904RA 53570 RETURN TO GATE DUE TO GALLEY DOOR SLIDE DISCONNECTED AFTER PUSH BACK. STOWED EMERGENCY SLIDE AT AFT GALLEY SERVICE DOOR . (X) 2 L 7 2 4F RT A6WE 1998051500698 19980515 00698 WP 1998 5 15 98ZZZX1775 1 19980213 A 3350 873100112 LIGHT DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A L2KA K NONE O OTHER IN INSP/MAINT 1 SO 17 831LA 6151 46936 DURING A-CHECK, MAINTENANCE FOUND 19C AND 19DE PATH LIGHT ASSY INOPERABLE. THE LIGHT ASSY REPLACED AND TESTED IAW THE M M. OPS CHECK GOOD. AIRCRAFT RETURNED BACK TO SERVICE. (X) 2 L 7 3 4F A22WE 1998051500699 19980515 00699 EA 1998 5 15 MASA98073 1 19980407 A 3350 GE1317 BULB BRUCE BM10006002 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27173 7173 WHILE PERFORMING ROUTINE MAINTENANCE, FOUND LT MID-OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOV ED AND REPLACED BULB. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A21EA 1998051500700 19980515 00700 1998 5 15 COEA9801976 4 19980401 A 3442 071137800 RT UNIT CESSNA 208 208B 2073701 CE RT WING INOPERATIVE A COEA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 13 976FE 169 3101 208B0103 ON CLIMB-OUT, PILOT FOUND WEATHER RADAR NOT DISPLAYING RETURNS OF VISIBLE MOISTURE AHEAD, AND OTHER PILOTS WERE REPORTIN G HEAVY WEATHER RETURNS ON SAME DEPARTURE AND DIRECTION AT SAME TIME. PILOT ELECTED TO RETURN TO BASE AND NOT PROCEED W ITHOUT THE ASSISTANCE OF WEATHER RADAR. MAINTENANCE FOUND RADAR RT INOPERATIVE. RADAR RT WAS REPLACED AND ALIGNED, SYS TEM TESTED SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (X) 1 H 7 1 3T A37CE 1998051500701 19980515 00701 CE 1998 5 15 C2XA98CL034 1 19980403 A 7712 1143800653 TORQUE GAUGE BEECH 1900 1900D 1154162 CE RT ENGINE INTERMITTENT A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 47542 3462 284M UE198 CLE - FLT 3263 - CREW REPORTED THE RIGHT HAND ENGINE TORQUE GAUGE FLUCTUATES FROM 5,000 TO ZERO IN FLIGHT. AIRCRAFT RET URNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND ENGINE TORQUE GAUGE IAW B1900D MM 77-10-00, OPERATION CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1998051500702 19980515 00702 EU 1998 5 15 SIMA980911 1 19980401 A 3350 3013000 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 459 533 CMI - SEVERAL FLOOR LIGHTS OUT FORWARD OF GALLEY. REPAIRED POWER SUPPLY AT 805 VT. PERFORMED OPERATIONAL CHECK SATISFA CTORILY AND RETURNED AIRCRAFT TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998051500703 19980515 00703 NM 1998 5 15 98ZZZX1776 1 19980323 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A RYNA K NONE L NO TEST CR CRUISE 1 CE 07 CGMKF 21119 BOX/PHL - FLT 431 - MID-CABIN CEILING EMERGENCY EXIT LIGHT INOPERATIVE. RE-SECURED LOOSE CANNON PLUG ON EXIT FIXTURE. 2 L 7 3 4F A3WE 1998051500802 19980515 00802 GL 1998 5 15 LR7A9806 2 19980423 A 7260 6825694 GEARBOX LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 2 ENGINE FAILED A LR7A E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 AL 03 289F 11972 1110 500774 NR 2 ENGINE SHUTDOWN AT 1545Z DUE TO LOW ENGINE AND REDUCTION GEARBOX OIL PRESSURE. FOUND TACH DRIVE GEARS AND OIL PUMP DRIVE GEARS WOULD NOT TURN WHEN PROP WAS TURNED. 2 L 7 4 4T 4 T 4A22 E282 1998051500803 19980515 00803 SO 1998 5 15 LR7A9807 1 19980127 A 5320 3717927 WEB LKHEED 382 382G 526414U SO BS 597-617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, A CRACK AT WEB CTR FUS, FS 597.0 TO 617.0, BL 61.625 UPPER, EXTENDING FROM ONE WIRE BUNDLE CUTOUT HOLE TO ANOTHER, APPROXIMATELY 1 INCH LENGTH AND AN ADDITIONAL CRACK WHICH HAS EXTENDED JUST PAST A CREW HOLE ABOVE THE 1 INCH CRACK. THE WEB WAS REPLACED WITH A CHANNEL STIFFENER INSTALLED IN THE CENTER OF THE WEB. 2 H 7 4 4T A1SO 1998051500804 19980515 00804 SO 1998 5 15 LR7A9808 1 19980127 A 5313 3625381L LONGERON LKHEED 382 382G 526414U SO BS 410-485 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND CRACKS ON A LONGERON, NR 2 AND NR 3 ENGINE, FS 410 TO FS 485, PPBL 10.00L, AND WEAR ALONG THE LONGERON WHICH IS .030 TO .035 INCHES DEEP. EXISTING REPAIR REMOVED, CRACKED PORTION OF LONGERON TRIMM ED OUT, FILLER INSTALLED, REPAIR DOUBLER INSTALLED. 2 H 7 4 4T A1SO 1998051500805 19980515 00805 SO 1998 5 15 LR7A9809 1 19980127 A 5400 3410454 TEE LKHEED 382 382G 526414U SO BS 410 WORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, TEE EXTRUSION IS WORN, NR 3 ENGINE, FS 410, PPBL 0.0 AND PPWL 11.0, AT THE TOP OF TH E BULKHEAD. THE WORN AREA WAS BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED. 2 H 7 4 4T A1SO 1998051500806 19980515 00806 SO 1998 5 15 LR7A9810 1 19980127 A 5412 36253710 FIREWALL CAP LKHEED 382 382G 526414U SO NR 3 ENGINE WORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND NR 3 ENGINE FIREWALL CAP WORN AT WL 225. BLENDED GROOVE, APPLIED FILLER, INST ALLED DOUBLER. 2 H 7 4 4T A1SO 1998051500807 19980515 00807 SO 1998 5 15 LR7A9811 1 19980127 A 5313 34298613 LONGERON LKHEED 382 382G 526414U SO FUSELAGE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, LT SLOPING LONGERON FOUND CRACKED AT RS1 RETAINER HOOK. LONGERON REPLACED. 2 H 7 4 4T A1SO 1998051500808 19980515 00808 SO 1998 5 15 LR7A9812 1 19980127 A 5400 3410454 EXTRUSION LKHEED 382 382G 526414U SO BS 410 WORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND TEE EXTRUSION WORN 0.025 THICKNESS AND GOUGED TO DEPTH OF 0.045 AT NR 4 ENGINE , LHS, FS 410, 11.0. WORN AREA BLENDED SMOOTH, EPOXY FILLER APPLIED, STAINLESS STEEL WEAR STRIP INSTALLED. 2 H 7 4 4T A1SO 1998051500809 19980515 00809 SO 1998 5 15 LR7A9813 1 19980127 A 5400 3410454 BULKHEAD LKHEED 382 382G 526414U SO NR 4 ENGINE WORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, NR 4 ENGINE QEC FRONT BULKHEAD ASSEMBLY WORN ON BOTH SIDES OF FILLER, TOP CENTER. R EPLACED EXISTING FILLER, INSTALLED WEAR STRIP. 2 H 7 4 4T A1SO 1998051500810 19980515 00810 SO 1998 5 15 LR7A9814 1 19980127 A 5330 3729861R SKIN LKHEED 382 382G 526414U SO BS 480 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, SPIDER CRACKS FOUND ON THE MLG WHEEL WELL RT PANEL SKIN, FS 480 AND WL 198. CRACKS IN SKIN PANEL TRIMMED OUT, REPAIR DOUBLER INSTALLED. 2 H 7 4 4T A1SO 1998051500811 19980515 00811 SO 1998 5 15 LR7A9815 1 19980127 A 5350 3705701L FAIRING LKHEED 382 382G 526414U SO WS 174 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, CENTER WING LEADING EDGE TO INBOARD ENGINE NACELLE FAIRING ASSY WEB HAS 2 CRACKS AT CW STA 174. TRIMMED OUT CRACKS, INSTALLED FILLER AND DOUBLER. 2 H 7 4 4T A1SO 1998051500812 19980515 00812 SO 1998 5 15 LR7A9816 1 19980127 A 5320 3716105 WEB LKHEED 382 382G 526414U SO BS 590 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, CRACKS LOCATED IN THE WEB AT WL 200, FS 590 ON BOTH LT AND RT SIDES. REPLACED WEB. 2 H 7 4 4T A1SO 1998051500813 19980515 00813 SO 1998 5 15 LR7A9817 1 19980127 A 5320 370499 CHINE CAP LKHEED 382 382G 526414U SO BS 425-817 DAMAGED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND SEVERAL CHINE CAPS, FS 245E TO 817E LT AND RT, WITH ELONGATED HOLES AT 10K TIE DOWNS, CORROSION, CRACKS, ANCHOR NUT RIVET HOLES. REPLACED ALL CHINE CAPS, EXCEPT ONE REPAIRED. 2 H 7 4 4T A1SO 1998051500814 19980515 00814 SO 1998 5 15 LR7A9818 1 19980127 A 5720 3705433 BEAM LKHEED 382 382G 526414U SO BS 597 CRACKED A LR7A O OTHER O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND CENTER WING REAR BEAM CRACKED AT CWS 72R, FS 597, APPROX WL 268. INSTALLED NE W INBD SECTION OF WEB, DOUBLER, AUXILIARY DOUBLER, SPACER STRAP, RADIUS BLOCK, REPAIR FINISHED. 2 H 7 4 4T A1SO 1998051500815 19980515 00815 SO 1998 5 15 LR7A9819 1 19980127 A 5730 3988513 SKIN LKHEED 382 382G 526414U SO LT WING WORN A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, LT AUX TANK CAVITY LOWER WING SKIN UPPER AND LOWER SURFACE HAS WEAR MARKS. WEAR MAR KS BLENDED SMOOTH, EDDY CURRENT INSPECTED, AND ROTO-PEENED. 2 H 7 4 4T A1SO 1998051500816 19980515 00816 SO 1998 5 15 LR7A9820 1 19980127 A 5400 36112228R ANGLE LKHEED 382 382G 526414U SO NR 1/2/3/4 NAC CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND ANGLE AT LOWER AFT NACELLE ASSY CRACKED NEAR FORWARD MOST SPOT WELD NR 1, 2, 3 , 4 ENGINES FS 517, PPBL 5.0. 2 H 7 4 4T A1SO 1998051500817 19980515 00817 SO 1998 5 15 LR7A9821 1 19980127 A 5412 3701161 BULKHEAD LKHEED 382 382G 526414U SO NR 1/2/3 NACELLE CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND 2 CRACK RADIATING ACROSS THE NR 1, 2, 3 AFT NACELLE BULKHEAD ASSY LOWER OUTBOA RD SIDE, FS 485.9, PPWL 3.5. STOP DRILLED AND INSTALLED REPAIR DOUBLER. 2 H 7 4 4T A1SO 1998051500818 19980515 00818 SO 1998 5 15 LR7A9822 1 19980127 A 5510 3734401L CAP LKHEED 382 382G 526414U SO HORIZ STAB CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 903SJ 4590 DURING C-CHECK/BRIDGING INSPECTION, FOUND CRACKED TANG AT HSS 180.0. DAMAGE AREA CLEANED UP AND TANG REPLACED WITH LS30 661 EXTRUSION. 2 H 7 4 4T A1SO 1998051500819 19980515 00819 1998 5 15 M8XA9800004 4 19980407 A 3442 7008470922 RADAR UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE DEFECTIVE A M8XA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 328MX 3071 CREW REPORTED THAT THE RADAR APPEARED TO BE INOPERATIVE, NO GROUND PAINT. CREW ELECTED TO RETURN TO DENVER. AIRCRAFT L ANDED IN DEN WITH NO FURTHER INCIDENTS. MX REPLACED WEATHER RADAR UNIT IAW AMM 34-41-01, OPERATIONAL CHECK IAW AMM 34-4 1-00 WAS CONDUCTED WITH SATISFACTORY RESULTS. AIRCRAFT WAS THEN RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998051500820 19980515 00820 NM 1998 5 15 M8XA9800005 1 19980508 A 5240 001A524D00071202 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE FAILED A M8XA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 330PH 3008 DURING CLIMBOUT, THE CREW REPORTED A PROBLEM WITH AIR LEAKING AROUND THE DOCUMENT DOOR. CREW THEN ELECTED TO RETURN TO DEN. AIRCRAFT LANDED IN DEN WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE DOCUMENT DOOR AND FOUND NO DISCREPANCI ES. ALSO, CONDUCTED A GROUND OPERATIONAL CHECK OF THE PRESSURIZATION SYSTEM IAW AMM 21-31-00 COULD NOT DUPLICATE THE PR OBLEM. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. IT SHOULD BE NOTED, THE DOCUMENT DOOR WAS REPLACED THE FOLLOWING DAY , BECAUSE OF A SEAL FAILURE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998051500821 19980515 00821 WP 1998 5 15 CALA9800821 1 19980511 A 3520 LATCH DOUG DC10 DC1010 3022110 WP OXYGEN COMPT FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 OXYGEN COMPARTMENT DOORS DID NOT OPEN ABOVE THE FOLLOWING SEATS, 1A 1D 1E 2D 16A 16E AND 34G. REPLACED DOORS PER MM 35- 20-00. 2 L 7 3 4F A22WE 1998051500822 19980515 00822 WP 1998 5 15 CALA9800822 1 19980509 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1280-1305 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 OVERWING SECTION SWELLING ON UPPER SURFACE LBL 90 BETWEEN STA 1280 TO 1305. SWELLING SKIN TRIMMED OUT, REWORKED AREA, T REATED, PRIMED AND INSTALLED UPPER AND LOWER DOUBLER PER SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998051500823 19980515 00823 WP 1998 5 15 CALA9800823 1 19980509 A 5312 BULKHEAD ANGLE DOUG DC10 DC1010 3022110 WP AFT PRESS BLKHD CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 AFT UPPER FUSELAGE AFT BULKHEAD LOWER LEFT ANGLE CRACKED. INSTALLED NEW ANGLE PER SRM 53-40-00 FIG 6 VOL 1. 2 L 7 3 4F A22WE 1998051500824 19980515 00824 1998 5 15 CALA9800824 4 19980509 A 2565 D30655123 SLIDE BOEING 757 757224 1384958 NM R2 DOOR JAMMED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14102 6192 6192 27292 R2 DOOR JAMMED IN DOORWAY DURING SAMPLE SLIDE DEPLOYMENT, SLIDE COVER HIT DOOR JAMB. REPLACED SLIDE AND ASSIST BOTTLE P ER CAL WORKCARDS. 2 L 7 2 4F RT A2NM 1998051500825 19980515 00825 NM 1998 5 15 CALA9800825 1 19980509 A 2910 65445101472 HYD LINE BOEING 737 737219 1384469 NM LT MLG WW LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 10248 20344 AFTER 1 HOUR OF FLIGHT, A-SYSTEM HYDRAULIC LOW PRESSURE LIGHT FLICKERED. FOUND HYD LINE LEAKING IN LEFT GEAR AREA. INS TALLED FLEX LINE REPAIR PER GMM 10-799-78. 2 L 7 2 4F A16WE 1998051500826 19980515 00826 NM 1998 5 15 CALA9800826 1 19980511 A 5330 SKIN BOEING 737 737291 138448W NM BS 259 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 FUSELAGE SKIN DENTED STA 259 BETWEEN STR 23R AND 24R. FABRICATED, PRIMED, SEALED, AND INSTALLED DOUBLER PER SRM 53-30-3 , 51-10-2 AND 51-20-4. 2 L 7 2 4F A16WE 1998051500827 19980515 00827 NM 1998 5 15 CALA9800827 1 19980510 A 5321 FLOOR PANEL BOEING 737 737291 138448W NM BS 380-420 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 FLOOR PANEL FWD PIT FS 380 TO 420 HAS TEARS. FABRICATED FWD PIT PANEL PER ECRA 2550-01046. 2 L 7 2 4F A16WE 1998051500828 19980515 00828 NM 1998 5 15 CALA9800828 1 19980509 A 2910 HYD LINE BOEING 737 7373T0 1384582 NM B-HYD SYST LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14307 23358 B-SYSTEM HYDRAULIC FAILURE. ENGINE NR 2 LOW PRESSURE WARNING. FOUND LINE BETWEEN B-SYSTEM HYDRAULIC SYSTEM PUM TO ACOU STIC FILTER LEAKING. REPLACED LINE. 2 L 7 2 4F RT A16WE 1998051500829 19980515 00829 NM 1998 5 15 CALA9800829 1 19980508 A 5314 KEEL BEAM BOEING 737 7373T0 1384582 NM BS 720 - 727 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18350 23588 RT W/W KEEL BEAM CORROSION FROM BS 720 TO 727. FABRICATED AND INSTALLED STRAP PER EC/RA 5310-03727. 2 L 7 2 4F RT A16WE 1998051500830 19980515 00830 NM 1998 5 15 CALA9800830 1 19980508 A 2910 5718604 HYD LINE BOEING 727 727224 1384076 NM B-HYD SYST LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 69735 20664 DURING CLIMB, B-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. FOUND LEAKING HYDRAULIC LINE. REPLACED LINE. 2 L 7 3 4F A3WE 1998051500831 19980515 00831 NM 1998 5 15 CALA9800831 1 19980509 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT FUSELAGE AT FS 950 RT ELEPHANT EAR FAIRING ATTACH ANGLE CRACKED (3). CUT OUT CRACKED PORTION OF FAIRING ATTACH ANGL E. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-4. 2 L 7 3 4F A3WE 1998051500832 19980515 00832 NM 1998 5 15 CALA9800832 1 19980509 A 5330 SKIN BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT CARGO PIT STR 29R STA950 CORRODED. REMOVED AND REPLACED NR 4 BELLY SKIN PER DWGS 65C20489 AND 65C13913. 2 L 7 3 4F A3WE 1998051500833 19980515 00833 NM 1998 5 15 CALA9800833 1 19980509 A 5313 65564418 STRINGER BOEING 727 727224 1384076 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT CARGO PIT STR 29R STA 950 CORRODED. REMOVED AND REPLACED STRINGER PER DWGS 65C20489 AND 65C13913. 2 L 7 3 4F A3WE 1998051500834 19980515 00834 NM 1998 5 15 CALA9800834 1 19980509 A 3230 0OWNLOCK BOEING 727 727224 1384076 NM LT MLG WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LEFT MLG DOWNLOCK CRANK HOLES ARE OVERSIZED. FABRICATED AND INSTALLED TWO BUSH INGS PER OHM 32-01-02. 2 L 7 3 4F A3WE 1998051500835 19980515 00835 NM 1998 5 15 CALA9800835 1 19980509 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 COMPLY WITH FWD DRAIN HOLE EA 5330-01463. REMOVED BELLY SKIN AND VERIFIED DOUBLERS INSTALLED. CLEANED AND REINSTALLED EXISTING DOUBLERS PER EA 5330-01463. 2 L 7 3 4F A3WE 1998051500836 19980515 00836 NM 1998 5 15 CALA9800836 1 19980509 A 3211 SWING LINK BOEING 727 727224 1384076 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LEFT MLG SWING LINK ATTACH LUGS ARE CORRODED ON FACES AND BORE HOLES. COMPLIED WITH REWORK PER EO 98-0847 AND EC/RA 574 0-01842. 2 L 7 3 4F A3WE 1998051500837 19980515 00837 NM 1998 5 15 CALA9800837 1 19980511 A 3211 BEAM BOEING 727 727224 1384076 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LEFT MLG SUPPORT BEAM LOWER ATTACH BORE FOR SWING LINK FORWARD AND AFT FACES CORRODED. REMOVED CORROSION, PEENED AREA, ALODINED AND PRIMED AREA, FABRICATED AND INSTALLED BUSHINGS PER EC/RA 5740-01841. 2 L 7 3 4F A3WE 1998051500838 19980515 00838 NM 1998 5 15 CALA9800838 1 19980509 A 5743 FITTING BOEING 727 727224 1384076 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LEFT MLG FWD TRUNNION ATTACH ANGLE FITTING ON LEG CORRODED. REPAIRED PER EO 98-871 AND EC/RA 5740-01840. 2 L 7 3 4F A3WE 1998051500839 19980515 00839 NM 1998 5 15 CALA9800839 1 19980509 A 2550 PANEL BOEING 727 727224 1384076 NM BS 950-1183 STAINED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 AFT CARGO COMPARTMENT FS 950 TO 1183, LBL 60 TO RBL 60 STAINED WITH BLUE WATER. FABRICATED AND INSTALLED NEW CEILING AN D SIDE WALL PANELS PER EC/RA 2550-01040 AND EC/RA 2011-01000. 2 L 7 3 4F A3WE 1998051500840 19980515 00840 NM 1998 5 15 CALA9800840 1 19980509 A 5743 TRUNNION BOEING 727 727224 1384076 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LEFT MLG FWD TRUNNION I/B SIDE OF FITTING INNER SIDE CORRODED. REPAIRED PER EO 97-871 AND EC/RA 5740-01840. 2 L 7 3 4F A3WE 1998051500841 19980515 00841 NM 1998 5 15 CALA9800841 1 19980508 A 5730 PANEL BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 LT UPPER INBOARD T/E PANEL HAS SURFACE CORROSION AND CRACK. REMOVED SURFACE CORROSION. STOP DRILLED CRACK AND INSTALLE D DOUBLER PER SRM 51-10-1, 51-10-6, AND 51-40-2. 2 L 7 3 4F A3WE 1998051500842 19980515 00842 NM 1998 5 15 CALA9800842 1 19980509 A 2910 NUT BOEING 727 727232 1384082 NM A-HYD SYST LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 45793 20647 ON TAKEOFF DURING GEAR RETRACTION, A-SYSTEM HYDRAULICS FAILED. FOUND LEAK AT A-SYSTEM RETURN LINE T-FITTING AT FWD KEEL BEAM RT WHEEL WELL. TIGHTENED B-NUT AND SERVICED SYSTEM. 2 L 7 3 4F A3WE 1998051500843 19980515 00843 WP 1998 5 15 CALA9800843 1 19980510 A 5512 SKIN DOUG DC9 DC982 3022082 WP LT HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 819NY 49479 LEFT HORIZ STAB LOWER AFT SKIN PANEL NR 3 FOUND CORROSION BETWEEN STA XHS86 AND XHS104. INSTALLED REPAIR DOUBLERS PER E C/RA 5510-01409. 2 L 7 2 4F A6WE 1998051500844 19980515 00844 1998 5 15 CALA9800844 4 19980512 A 2565 D29984103 SLIDE DOUG DC9 DC982 3022082 WP TAIL CONE FAILED A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 18835 29472 2805 49439 TAIL CONE DEPARTED AIRCRAFT AND SLIDE FAILED TO COMPLETELY DEPLOY. REPLACED SLIDE AND TAIL CONE ASSEMBLY PER MM 25-63-0 1 AND 53-53-00. 2 L 7 2 4F A6WE 1998051500845 19980515 00845 WP 1998 5 15 CALA9800845 1 19980511 A 3350 1001191 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16895 49394 PORTABLE FLASHLIGHT AT MAIN CABIN DOOR HAS DEAD BATTERY. REPLACED FLASHLIGHT. 2 L 7 2 4F A6WE 1998051500846 19980515 00846 WP 1998 5 15 CALA9800846 1 19980512 A 5711 SPAR CAP DOUG DC9 DC982 3022082 WP WS 164 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 A 1 INCH CRACK AROUND I/B HOLE ON RIGHT WING LOWER SPAR CAP. REPAIRED PER TASK CARD 08-5710-1-0020 OP 7. 2 L 7 2 4F A6WE 1998051500847 19980515 00847 WP 1998 5 15 CALA9800847 1 19980512 A 5711 SPAR CAP DOUG DC9 DC982 3022082 WP WS 161.7 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 LEFT WING LOWER SPAR CAP CRACKED 2.35 AT STA XRS 161.7. PERFORMED REPAIR PER TASK CARD 08-5700-1-0025 OP 12. 2 L 7 2 4F A6WE 1998051500848 19980515 00848 WP 1998 5 15 CALA9800848 1 19980512 A 5530 SKIN DOUG DC9 DC982 3022082 WP DORSAL FIN WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 DORSAL FIN ATTACHMENT ANGLES FUSELAGE SKIN HAS SEVERAL OVERSIZED HOLES. REPAIRED PER EC/RA 5330-02660. 2 L 7 2 4F A6WE 1998051500849 19980515 00849 EU 1998 5 15 9808613214 1 19980506 A 3350 321454 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOPERATIVE A NWAA K NONE L NO TEST NR NOT REPORTED 1 GL 01 314US 160 CREW OBSERVED CABIN LIGHTING CIRCUIT BREAKER POPPED. FURTHER INVESTIGATION REVEALED EMERGENCY EXIT LIGHTS AFT OF ROW 9 INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY 13WL AND 11WL. 2 L 7 2 4F RT A28NM 1998051500850 19980515 00850 NE 1998 5 15 9808621162 2 19980506 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 162US 46771 686171 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 880C BEFORE THE ENG INE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER TAFI STALL PROCEDURE WITH NO TROUBLE FOUND. RABS CHECK WAS NOT ACCOMPLISHED AND THE REVERSER WAS LOCKED OUT AND PLACED ON MEL 78-1A. THE AIRCRAFT RETURNED TO SERVICE. EXACT PART CA USING PROBLEM TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998051500851 19980515 00851 NM 1998 5 15 9808636303 1 19980508 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35 TO 40. REPAIRED WIRE, OPERATIONAL CHECK G OOD. 2 L 7 4 4F RT A20WE 1998051500852 19980515 00852 NM 1998 5 15 9808646638 1 19980507 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 638US 23549 DURING LINE CHECK, FOUND D-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998051500853 19980515 00853 NM 1998 5 15 9808656307 1 19980507 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 667US 24222 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 40 TO 43. REPAIRED WIRING, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998051500854 19980515 00854 NM 1998 5 15 9808666306 1 19980508 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 666US 23821 DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35 TO 39 AND AT DOOR 3L. REPAIRED WIRES, OPE RATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1998051500855 19980515 00855 WP 1998 5 15 9808679880 1 19980510 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 675MC 47651 FLIGHT ATTENDANT REPORTED EMERGENCY FLASHLIGHT NOT BLINKING AT ENTRY DOOR 1L. MAINTENANCE REPLACED BATTERIES. OPERATION AL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998051500856 19980515 00856 WP 1998 5 15 9808689875 1 19980508 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 784NC 48109 FLIGHT ATTENDANT REPORTED LOWER EMERGENCY FLASHLIGHT NOT BLINKING AT ENTRY DOOR 1L. MAINTENANCE REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998051500857 19980515 00857 WP 1998 5 15 9808699855 1 19980509 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 764NC 47717 FLIGHT ATTENDANT REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT BLINKS UNRELIABLY. MAINTENANCE REPLACED BATTERIES, OPERAT IONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998051500858 19980515 00858 WP 1998 5 15 9808709877 1 19980509 A 3350 LIGHTS DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 786NC 48148 DURING LINE CHECK, FOUND TAIL COMPARTMENT EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATT ERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998051500859 19980515 00859 WP 1998 5 15 9808719101 1 19980508 A 3350 BATTERIES DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 91S 47063 DURING LINE CHECK, FOUND SEVERAL FLOOR TRACK EMERGENCY EXIT LIGHTS INOPERATIVE, EXIT LIGHTING WEAK OVER LEFT WING EXIT, AND EMERGENCY LIGHTING OUT OF SEQUENCE IN FIRST CLASS SECTION. MAINTENANCE REPLACED BATTERIES AND REARRANGED LIGHT ASSE MBLIES IN FIRST CLASS SECTION, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500860 19980515 00860 WP 1998 5 15 9808729101 1 19980508 A 3230 59164605509 VALVE DOUG DC9 DC915 3022036 WP MLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 91S 40054 40054 47063 DURING CLIMBOUT, THE RIGHT MAIN LANDING GEAR UNSAFE AND DOOR OPEN LIGHTS ILLUMINATED. THE FLIGHT CREW FOLLOWED COM PROC EDURES, RECYCLED LANDING GEAR HANDLE, RETURNED TO MEM, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAIN LANDI NG GEAR CONTROL VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500861 19980515 00861 WP 1998 5 15 9808739966 1 19980508 A 3260 SOCKET DOUG DC9 DC931 3022065 WP NLG SHORTED A NWAA O OTHER N FALSE WARNING DE DESCENT 1 GL 01 9330 47138 NOSE LANDING GEAR GREEN LIGHT ILLUMINATED WHEN THROTTLES WERE BROUGHT TO IDLE POWER DURING DESCENT. CREW REQUESTED EMER GENCY EQUIPMENT ON STANDBY AS A PRECAUTION AND FLIGHT WAS CONTINUED TO DESTINATION. NORMAL INDICATIONS WERE ACHIEVED WH EN GEAR WAS LOWERED FOR LANDING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR GREEN LIGHT SOCKET ASSE MBLY SHORTED INTERNALLY. REPLACED SOCKET, OPERATIONAL CHECK NORMAL ON GEAR CYCLE. 2 L 7 2 4F A6WE 1998051500862 19980515 00862 WP 1998 5 15 9808749992 1 19980429 A 5320 JAMB DOUG DC9 DC931 3022065 WP NLG DOORWAY CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8960E 45869 DURING M-CHECK, FOUND CRACKS IN NOSE LANDING GEAR DOOR JAMB BEAMS AT THE UPPER BOLT HOLE FOR SPRAY DEFLECTOR GUIDES LEFT AND RIGHT SIDES. REPAIRED PER EA 99-156911. 2 L 7 2 4F A6WE 1998051500863 19980515 00863 WP 1998 5 15 9808759996 1 19980422 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 937 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8932E 47141 DURING M-CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT FLOORBEAM FS 937, RBL 16. REPAIRED PER EA 99-157312. 2 L 7 2 4F A6WE 1998051500864 19980515 00864 WP 1998 5 15 9808769933 1 19980416 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 513 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING M-CHECK, FOUND CORROSION ON LONGERON 29L AT FS 513. REPAIRED PER EA 99-154884. 2 L 7 2 4F A6WE 1998051500865 19980515 00865 WP 1998 5 15 9808779933 1 19980325 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1334U 47280 DURING M-CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL HORIZONTAL PRESSURE PANEL FS 110 AT THE LEFT OUTBOARD VERTIC AL BEAM. REPAIRED PER EA 99-154798. 2 L 7 2 4F A6WE 1998051500866 19980515 00866 WP 1998 5 15 9808789928 1 19980418 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING H-CHECK, FOUND CRACK IN RIGHT OUTBOARD KEEL TO BULKHEAD FITTING FS 756. REPLACED FITTING (P/N 3915135-506N) PER SRM 51-01. 2 L 7 2 4F A6WE 1998051500867 19980515 00867 WP 1998 5 15 9808799928 1 19980419 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING H-CHECK, FOUND CRACK IN LEFT OUTBOARD KEEL TO BULKHEAD FITTING AT FS 756. REPLACED FITTING (P/N 3915135-505N) PE R SRM 51-01. 2 L 7 2 4F A6WE 1998051500868 19980515 00868 WP 1998 5 15 9808809928 1 19980420 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP BS 748 -754 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING H-CHECK, FOUND CORROSION ON KEEL TO BULKHEAD FITTING AT FS 748 TO 754, BL 0 THRU LBL 3. REPLACED FITTING (P/N 39 15134-517N) PER SRM 51-10-8. 2 L 7 2 4F A6WE 1998051500869 19980515 00869 WP 1998 5 15 9808819928 1 19980420 A 5312 BULKHEAD FITTING DOUG DC9 DC931 3022065 WP BS 748- 754 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING H-CHECK, FOUND CORROSION ON KEEL TO BULKHEAD FITTING AT FS 748 TO 754, BL 0 THRU RBL 3. REPLACED FITTING (P/N 39 15134-517N) PER SRM 51-10-8. 2 L 7 2 4F A6WE 1998051500870 19980515 00870 WP 1998 5 15 9808829928 1 19980505 A 5320 PRESSURE WEB DOUG DC9 DC931 3022065 WP BS 756 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8921E 45836 DURING H-CHECK, FOUND CORROSION ON FS 756 PRESSURE WEB AT RBL 7. REPAIRED PER EA 99-157315. 2 L 7 2 4F A6WE 1998051500871 19980515 00871 NM 1998 5 15 9808835515 1 19980505 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM BS 310 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 515US 23203 DURING TRANSITION CHECK, FOUND CORROSION ON FLOORBEAM AT FS 310, RBL 2 TO 3. REPAIRED PER EA 55-156867. 2 L 7 2 4F RT A2NM 1998051500872 19980515 00872 NM 1998 5 15 9808842284 1 19980327 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING M-CHECK, FOUND CORROSION ON FLOORBEAM AT FS 1130, LBL 24, WL 208. REPAIRED PER EA 22-156532. 2 L 7 3 4F A3WE 1998051500873 19980515 00873 NM 1998 5 15 9808852284 1 19980327 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 1130 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 284US 21323 DURING M-CHECK, FOUND CORROSION ON FLOORBEAM AT FS 1130, LBL 30, WL 208. REPAIRED PER EA 22-156532. 2 L 7 3 4F A3WE 1998051500874 19980515 00874 WP 1998 5 15 9808869944 1 19980510 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE HANDLE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 1309T 47316 DURING TAIL CONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE THE EXTERIOR DEPLOYMENT HANDLE FROM THE CLIPS. ADJUSTED CLIPS, FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998051500875 19980515 00875 NM 1998 5 15 9808876638 1 19980509 A 3350 BATTERY PACK BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 638US 23549 DURING LINE CHECK, FOUND D-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND POWER SUPPLY, OPERAT IONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998051500876 19980515 00876 WP 1998 5 15 9808889871 1 19980508 A 7711 EPR LINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE LT ENGINE BROKEN A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 780NC 48102 688777 AS TAKEOFF POWER WAS APPLIED THE LEFT ENGINE WOULD NOT REACH TARGET EPR INDICATION. CREW ABORTED TAKEOFF AND RETURNED T O GATE. MAINTENANCE REPLACED EPR LINE. ENGINE OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F RT A6WE E2EA 1998051500877 19980515 00877 EU 1998 5 15 9808893211 1 19980509 A 2761 31077050 ACTUATOR AIRBUS 320 A320211 3930320 EU NR 1 SPOILER ACT FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 311US 18641 18501 125 DURING CRUISE, LOST GREEN HYDRAULIC SYSTEM FLUID. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPL ACED LEAKING SPOILER ACTUATOR, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998051500878 19980515 00878 EU 1998 5 15 9808903201 1 19980506 A 2131 9022157028 CONTROLLER AIRBUS 320 A320211 3930320 EU E/E COMPARTMENT FAILED A NWAA A B UNSCHED LANDING EMER. DESCENT G J MULTIPLE FAILURE WARNING INDICATION CR CRUISE 1 GL 01 301US 16439 16439 31 DURING CRUISE, ECAM MESSAGE CAB PR SYS 1+2 FAULT ILLUMINATED AND ESCESSIVE CABIN ALTITUDE WAS NOTICED. CREW INITIATED E MERGENCY DESCENT WHILE USING MANUAL PRESSURIZATION CONTROL AVERTING PASSENGER OXYGEN MASK DEPLOYMENT. FLIGHT DIVERTED T O MSP AND LANDED WITHOUT INCIDEN. MAINTENANCE REPLACED NR 1 AND NR 2 CABIN PRESSURE CONTROLLERS AND OUTFLOW VALVE, OPER ATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998051500879 19980515 00879 WP 1998 5 15 9808911150 1 19980510 A 7830 TR RIGGING DOUG DC10 DC1040 3023508 WP NR 3 ENGINE OUT OF ADJUST A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 01 150US 46759 UPON APPLICATION OF TAKEOFF POWER, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE A IRCRAFT RETURNED TO THE GATE. MAINTENANCE ADJUSTED THE REVERSER VENT VALVE RIGGING AND FOUND ALL INDICATIONS NORMAL. A IRCRAFT DEPARTED WITHOUT FURTHER PROBLEMS. 2 L 7 3 4F A22WE 1998051500880 19980515 00880 NE 1998 5 15 9808921141 2 19980507 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN O OTHER LD LANDING 1 GL 01 141US 46750 686150 DURING THE LANDING ROLLOUT, THE NR 3 ENGINE COMPRESSOR STALLED WHILE IN REVERSE THRUST. THE EGT REACHED 970C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE PERFORMED A BORESCOPE INSPECTION AND FOUND DAMAGE TO THE HIGH PRESSURE COMPRESSOR. T HE AIRCRAFT WAS REMOVED FROM SERVICE FOR AN ENGINE CHANGE. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998051500881 19980515 00881 WP 1998 5 15 9808939866 1 19980511 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 775NC 47785 DURING LINE CHECK, FOUND LEFT WING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK, OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998051500882 19980515 00882 WP 1998 5 15 9808949969 1 19980511 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9333 47246 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS AT MAIN CABIN DOOR EXIT SIGN AND AT GALLEY ESCAPE PATH INOPER ATIVE. REPLACED BATTERIES AT MAIN CABIN DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500883 19980515 00883 WP 1998 5 15 9808959924 1 19980510 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926RC 47473 DURING LINE MAINTENANCE INSPECTION, FOUND RIGHT EXTERIOR OVERWING EMERGENCY EVACUATION LIGHT INOPERATIVE. REPLACED BATT ERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500884 19980515 00884 WP 1998 5 15 9808969950 1 19980510 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT FORWARD OVERWING EMERGENCY EXIT INOPERATIVE. REPLACED POWER SUPPLY, OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500885 19980515 00885 WP 1998 5 15 9808979950 1 19980510 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE MAINTENANCE INSPECTION, FOUND AFT RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED POWER SUPPLY, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500886 19980515 00886 WP 1998 5 15 9808989950 1 19980510 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9346 47376 DURING LINE MAINTENANCE INSPECTION, FOUND FORWARD EMERGENCY LIGHTS NEAR GALLEY INOPERATIVE. FOUND WIRE LOOSE AT POWER S UPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500887 19980515 00887 WP 1998 5 15 9808999609 1 19980510 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND AFT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED DEAD CELLS IN BATTERY , OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500888 19980515 00888 WP 1998 5 15 9809009614 1 19980509 A 3260 HARNESS DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 614NW 47128 DURING APPROACH INTO CLT, LANDING GEAR WARNING HORN SOUNDED FOR APPROXIMATELY TWO SECONDS WITH NOSE GEAR GREEN LIGHT OFF AND RED UNSAFE LIGHT ON. CREW RECYCLED GEAR AND RECEIVED NORMAL INDICATIONS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINT ENANCE REPORTED PSEU FAULT OF NLG LOCKED PROX SENS OPEN. REPLACED NOSE GEAR WIRING HARNESS. OPERATIONAL CHECK NORMAL O N GEAR SWING. 2 L 7 2 4F A6WE 1998051500889 19980515 00889 WP 1998 5 15 9809019602 1 19980511 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 602NW 47046 DURING LINE MAINTENANCE INSPECTION, FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500890 19980515 00890 WP 1998 5 15 9809029992 1 19980511 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8960E 45869 DURING PERIODIC CHECK, FOUND RIGHT TAIL EVACUATION SLIDE AND RIGHT NACELLE EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTE RY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998051500891 19980515 00891 WP 1998 5 15 9809039926 1 19980508 A 2163 TEMP SENSOR DOUG DC9 DC932 3022066 WP RIGHT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 926NW 47425 RIGHT AIR CONDITIONING SUPPLY TEMPERATURE HIGH LIGHT ILLUMINATED DURING TAKEOFF ROLL. TAKEOFF WAS ABORTED AT APPROXIMAT ELY 15 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED TEMPERATURE SENSOR, OPERATIONAL CEHCK NORMAL. 2 L 7 2 4F A6WE 1998051500892 19980515 00892 SO 1998 5 15 COMA9810114 1 19980508 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 01 168CA 12649 420 120168 EMERGENCY FLOOR PATH LIGHTING VERY DIM. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998051500893 19980515 00893 SO 1998 5 15 COMA9810115 1 19980510 A 3350 1011105 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 120152 EXIT SIGN AT ROW 5A IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998051500894 19980515 00894 EA 1998 5 15 COMA9860097 1 19980506 A 3150 WARNING CNDAIR CL600 CL6002B19 EA COCKPIT ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 981CA 7163 COPILOT ROLL COMMAND MESSAGE DURING TAKEOFF. OPERATIONAL CHECK OF ROLL DISCONNECT STATISFACTORY. COULD NOT DUPLICATE D ISCREPANCY. 2 L 7 2 4F RT A21EA 1998051500895 19980515 00895 EA 1998 5 15 COMA9860098 1 19980510 A 3411 PITOT CNDAIR CL600 CL6002B19 EA FWD FUSELAGE CONTAMINATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 940CA 7048 TAKEOFF ABORTED, DUE TO AIRSPEED COMPARATOR WARNING MESSAGE. DRAINED WATER FROM PITOT STATIC SYSTEM. 2 L 7 2 4F RT A21EA 1998051500896 19980515 00896 EA 1998 5 15 COMA9860099 1 19980510 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAPS MALFUNCTION A COMA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 SO 01 708CA 7235 FLAPS FAILED TO ZERO. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1998051500897 19980515 00897 SO 1998 5 15 COMA9810116 1 19980511 A 3260 12038594001 BOX CONTROL EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A COMA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 269CA 13764 120263 WHEN LANDING GEAR EXTENDED BOTH GREEN AND RED INDICATOR LIGHTS ILLUMINATED, AND ANTI-SKID FAIL INDICATION. COULD NOT DU PLICATE DISCREPANCY. REPLACED LANDING GEAR CONTROL ASSEMBLY FOR TROUBLESHOOTING. 2 L 7 2 4T RT A31SO 1998051500898 19980515 00898 NM 1998 5 15 UPS98226588 1 19980506 A 5754 651622369 SKIN BOEING 727 727247 138408F NM NR 2 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 211UP 21700 INSPECTION TYPE-SI, NR 2 SLAT LOWER SKIN FASTENERS SHEARED AND CRACK EMITTING FROM FASTENER HOLE JUST BELOW UPSTOP (I/B) . REMOVED AND REPLACED NR 2 SLAT IAW MM 27-81-11. 2 L 7 3 4F A3WE 1998051500899 19980515 00899 NM 1998 5 15 UPS98226589 1 19980508 A 3350 9621024 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, 1 OVERHEAD EMERGENCY LIGHT ON RIGHT SIDE 11 FED INOP. REPLACED BATTERY, OPS CHECK GOOD PER TASK CA RD 3000 (P/N 96-2-1024). 2 L 7 3 4F A3WE 1998051500900 19980515 00900 NM 1998 5 15 UPS98226590 1 19980509 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, 2 OVERHEAD EMERGENCY LIGHTS OVER RIGHT GALLEY INOP. BATTERY PACK AND LIGHT ON ORDER REQ A428361. R EPLACED BATTERY PACKS, OPS CHECK GOOD PER T/C MC-3000. 2 L 7 3 4F A3WE 1998051500901 19980515 00901 WP 1998 5 15 UPS98826591 1 19980511 A 5330 SKIN DOUG DC8 DC873F 302199F WP FWD FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 852UP 46052 INSPECTION TYPE-N/A, SKIN AND RIVETS ERODED JUST AFT OF RADOME AT 12 O'CLOCK POSITION. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-2-1 AND ALODINED PER SRM. 2 L 7 4 4F RT 4A25 1998051500902 19980515 00902 EU 1998 5 15 QXEA9800637 1 19980508 A 3350 COVER GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN MISSING A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 EXIT SIGN COVER MISSING, SEAT 8A-B. MAINTENANCE REPLACED EMERGENCY EXIT LIGHT COVER, LAMP TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998051500903 19980515 00903 EU 1998 5 15 QXEA9800638 1 19980510 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 SEAT 9E EVACUATION LIGHT INOPERATIVE. MAINTENANCE RELAMPED, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998051500904 19980515 00904 EU 1998 5 15 QXEA9800639 1 19980510 A 3350 XB864041 COVER GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN MISSING A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 EVACUATION LIGHT AT ROW 8 MISSING COVER. MAINTENANCE INSTALLED NEW LIGHT ASSEMBLY, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998051500905 19980515 00905 EU 1998 5 15 QXEA9800640 1 19980509 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 LEFT FORWARD WINDOW EXIT EVACUATION LIGHT INOPERATIVE. MAINTENANCE RELAMPED, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998051500906 19980515 00906 EU 1998 5 15 QXEA9800641 1 19980509 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 EXIT LIGHT INOPERATIVE OVER EXIT HATCH 8A. MAINTENANCE RELAMPED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998051500907 19980515 00907 EU 1998 5 15 QXEA9800642 1 19980510 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 FORWARD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998051500908 19980515 00908 EU 1998 5 15 QXEA9800643 1 19980510 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 SEVERAL OVERHEAD EMERGENCY LIGHTS OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTED GOOD. 2 L 7 2 4F RT A20EU 1998051500909 19980515 00909 EU 1998 5 15 QXEA9800644 1 19980509 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 ALL EMERGENCY EXIT SIGNS HAVE BULBS OUT. MAINTENANCE RELAMPED, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998051500910 19980515 00910 EU 1998 5 15 QXEA9800645 1 19980509 A 3350 1315 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998051500911 19980515 00911 EU 1998 5 15 QXEA9800646 1 19980508 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 EXIT SIGN AT FORWARD CABIN IS INOPERATIVE. MAINTENANCE RELAMPED, TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998051500912 19980515 00912 NE 1998 5 15 98FDEA00339 2 19980512 A 7200 ENGINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 3 FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 258FE 20940 ON T/O, NR 3 ENG FAILED, SLIGHT SHUDDER ACCOMMP BY LOSS OF EPR AND N1, HIGH EGT AND LOSS OF OIL QTY, SHUTDOWN PER 727 A/ C FLT MANUAL. REMOVED AND REPLACED NR 3 ENG PER W/C 70T0001. 2 L 7 3 4F 4 F RT A3WE E2EA 1998051500913 19980515 00913 NM 1998 5 15 98FDEA00340 1 19980511 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 AFT LOWER CARGO COMP CEILING, FLOORBEAM AT FS 1130 IS HEAVILY CORRODED IN AND AROUND CENTER CEILING SUPPORT STRAP BL 0. FABRICATED AND INSTALLED DOUBLER PER EA 7-5310-29488 DATED APRIL 23, 1988. 2 L 7 3 4F A3WE 1998051500914 19980515 00914 WP 1998 5 15 98UAL900171 1 19980505 A 3350 BATTERY DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 1839U 46633 1L DOOR EMERGENCY SLIDE LIGHT IS INOP. REPLACED BATTERY. 2 L 7 3 4F 4 F A22WE E23EA 1998051500915 19980515 00915 NM 1998 5 15 98UAL900172 1 19980501 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7443U 21897 EMERGENCEY EXIT LIGHT IN CABIN ABOVE FORWARD OVERWING DOOR IS DIM. REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1998051500916 19980515 00916 NM 1998 5 15 98UAL900173 1 19980504 A 3020 567620 ANTI-ICE TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7267U 21414 RETURNED TO DEN DUE TO NR 3 ENGINE OIL PRESSURE LOW AND LOST OIL QUANTITY. PULLED THROTTLE BACK TO IDLE BUT DID NOT SHU T DOWN ENGINE. *S/D* THE SHOP FOUND NO PROBLEM WITH THE BASIC ENGINE. THE ANTI-ICE TUBE HAD FAILED AND WAS BLOWING HO T AIR ON THE HARNESS RESULTING IN WHAT APPEARED TO BE AN INDICATION PROBLEM. HARNESS CHECKED GOOD. REPLACED THE ANTI-I CE TUBE ASSEMBLY. OTHER UNRELATED WORK WAS PERFORMED WHILE THE ENGINE WAS IN THE SHOP. 2 L 7 3 4F 4 F A3WE E2EA 1998051500917 19980515 00917 NM 1998 5 15 98UAL900174 1 19980505 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7458U 21912 EXTERIOR RIGHT WING EMERGENCY EXIT AFT LIGHT INOPERATIVE. REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1998051500918 19980515 00918 1998 5 15 98UAL900175 4 19980504 A 2565 D3O657322 TUBE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE SLIDE RAFT FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 588UA 35 26717 DURING SHOP OVERHAUL OF SLIDE/RAFT, IT FAILED THE AIR RETENTION TEST. FAILURE DUE TO POROSITY IN THE UPPER TUBE INFLATA BLE MATERIAL. SLIDE/RAFT SENT TO VENDOR FOR REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1998051500919 19980515 00919 1998 5 15 98UAL900176 4 19980504 A 2565 7A14376 TUBE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE SLIDE RAFT FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 155UA 36 20104 DURING SHOP OVERHAUL OF SLIDE/RAFT IT FAILED THE AIR RETENTION TEST. FAILURE DUE TO A SEAM LEAK IN THE UPPER TUBE ON TH E LOWER END CROSS OVERTUBE LOWER SEAM UNDER CHAFING PANEL. SLIDE/RAFT SENT TO VENDOR FOR REPAIR. 2 L 7 4 4F 4 F A20WE E20EA 1998051500921 19980515 00921 NE 1998 5 15 98UAL900178 2 19980506 A 7230 50B927 BEARING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT ENGINE STALLED A UALA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 WP 29 767UA 8537 26918 777021 EICAS (ENGINE INDICATION AND CREW ALERT SYSTEM) MESSAGE ENG OIL FILTER R DISPLAYED IN FLIGHT AT 1700Z. AT 1920Z OIL PRE SSURE STARTED DOWNWARD STEADILY UNTIL LOW PRESSURE LIGHT ILLUMINATED, SHUT DOWN ENGINE. FOUND METAL ON ALL MAGNETIC CHI P DETECTORS AND OIL FILTER OF RIGHT ENGINE. REMOVED ENGINE. NR 1 BEARING FAILED. MOST PROBABLE ORIGIN IS OUTER RACE. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998051500922 19980515 00922 WP 1998 5 15 MWEA98581 1 19980507 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 THE FORWARD CABIN DOOR SLIDE COVER CAME OFF WHEN DOOR WAS CLOSED. MTC REINSTALLED FORWARD ENTRANCE DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998051500923 19980515 00923 WP 1998 5 15 MWEA98582 1 19980508 A 3350 60030431 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 900ME 45841 THE EMERGENCY LIGHTS AT LAST ROW OF SEATS CEILING REMAINED ON WHEN POWER TURNED OFF. MTC REMOVED AND REPLACED POWER SUP PLY. 2 L 7 2 4F A6WE 1998051500924 19980515 00924 WP 1998 5 15 MWEA98583 1 19980507 A 3150 ANNUNCIATOR DOUG DC9 DC932 3022066 WP RT COCKPIT MALFUNCTIONED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE FIRST OFFICERS MASTER CAUTION ANNUNCIATOR STICKS INTERMITTANTLY IN RESET. MTC REMOVED CLEANED AND REINSTALLED FIRST OFFICERS MASTER CAUTION ANNUNCIATOR. 2 L 7 2 4F A6WE 1998051500925 19980515 00925 WP 1998 5 15 MWEA98584 1 19980506 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 BOTH FORWARD OVERWING EMERGENCY EXIT SIGNS DID NOT ILLUMINATE WHEN TESTED. MTC CHARGED THE EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1998051500926 19980515 00926 WP 1998 5 15 MWEA98585 1 19980505 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 210 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND SMALL DENT ON SKIN AT LONGERON 18L STATION 210. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998051500927 19980515 00927 WP 1998 5 15 MWEA98586 1 19980509 A 5320 5910071001 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 39 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND CRACK ON FORWARD ACCESSORY COMPARTMENT INTERCOSTAL AT STATION 39. MTC FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 1998051500928 19980515 00928 WP 1998 5 15 MWEA98587 1 19980509 A 5320 59132624 ANGLE DOUG DC9 DC914 3022034 WP BS 786 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND CRACK ON RIGHT HAND PYLON UPPER FUSELAGE TO PYLON ATTACH ANGLE AT STATION 786. MTC REMOVED AND REPLACED ATTACH AN GLE. 2 L 7 2 4F A6WE 1998051500929 19980515 00929 NM 1998 5 15 SCNA98040 1 19980510 A 3230 656021119 LGAU BOEING 727 7272J4 1384006 NM E/E COMPT INOPERATIVE A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 284SC 21438 AFTER TAKEOFF, COULD NOT RETRACT LANDING GEAR NORMALLY. RETRACTED GEAR WITH THE OVERRIDE SWITCH BUT GEAR UNSAFE LIGHT I LLUMINATED. RETURNED TO BOS AND GEAR EXTENDED NORMALLY. REMOVED AND REPLACED K5, K6 AND K8 GROUND RELAYS AND K9, K10, K11 AIR RELAYS AND LANDING GEAR ACCESSORY UNIT. PERFORMED LANDING GEAR RETRACTION CHECK IN ACCORDANCE WITH MAINTENANCE MANUAL CHAPTER 32-11-00 AND OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1998051500930 19980515 00930 WP 1998 5 15 SCNA98041 1 19980505 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP CABIN SHORTED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 572SC 46977 DURING A-LINE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING IN THE AFT MID CABIN AND FORWARD PART OF AFT CABIN WAS FOUND INO PERATIVE. REPAIRED SHORTED WIRING IN TRACK BASE, ALL FLOOR TRACK LIGHTING CHECKS GOOD. 2 L 7 3 4F A22WE 1998051500931 19980515 00931 NM 1998 5 15 SCNA98042 1 19980504 A 2613 OVERHEAT LIGHT BOEING 727 7272J4 1384006 NM AFT BODY ILLUMINATED A SCNA O OTHER N FALSE WARNING CR CRUISE 1 GL 15 285SC 21676 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AT FL370. SHUT OFF NUMBER ONE BLEED VALVE AND LEFT PACK. COULD NOT HOLD PRES SURIZATION SO THE NUMBER ONE BLEED VALVE AND PACK TURNED BACK ON AND A DESCENT INITIATED DOWN TO FL250. DURING THE DESC ENT THE LOWER AFT OVERHEAT LIGHT EXTINGUISHED. PERFORMED MEG CHECK OF ENGINE FIRE LOOPS WITH NO TROUBLE FOUND. KEEL BE AM AND AFT PIT PANELS CHECKED FOR LEAKS AT TAKEOFF AND PART POWER WITH NO DISCREPANCIES NOTED. LEFT AND RIGHT PACK OPER ATED NORMALLY WITH NO DISCREPANCIES NOTED. FUNCTIONALLY TESTED GOOD. 2 L 7 3 4F RT A3WE 1998051500945 19980515 00945 EU 1998 5 15 98ZZZX1790 1 19980116 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 39 12473 S789 PRESSURE TRANSMITTER UNIT CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1998051500946 19980515 00946 EU 1998 5 15 98ZZZX1791 1 19980125 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 15 12690 S789 PRESSURE TRANSMITTER UNIT CAUSES PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1998051500947 19980515 00947 EU 1998 5 15 98ZZZX1792 1 19980102 A 6420 ABWT82008 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 118 7230 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500948 19980515 00948 EU 1998 5 15 98ZZZX1793 1 19980211 A 6321 AH090635 PAD BOLKMS 117 BK117B1 5626012 EU ROTOR BRAKE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 250 7230 ROTOR BRAKE PAD WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500949 19980515 00949 EU 1998 5 15 98ZZZX1794 1 19980405 A 6410 11731743 BLADE BOLKMS 117 BK117B1 5626012 EU T/R DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 395 369 7229 T/R BLADE PAINT PEELING CAUSING HIGH FREQUECY VIBRATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500951 19980515 00951 EU 1998 5 15 98ZZZX1796 1 19980126 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A3 5626015 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 70 7063 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500952 19980515 00952 EU 1998 5 15 98ZZZX1797 1 19980310 A 6510 551253 BEARING BOLKMS 117 BK117A3 5626015 EU T/R DRIVE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 424MB 254 7082 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500954 19980515 00954 EU 1998 5 15 98ZZZX1799 1 19980202 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 75 12447 S754 PRESSURE TRANSMITTER UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1998051500955 19980515 00955 EU 1998 5 15 98ZZZX1800 1 19980214 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 26 12640 S754 PRESSURE TRANSMITTER UNIT CAUSES PRESSURE GAUGE FLUCTUATION ON HIGH SIDE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1998051500956 19980515 00956 EU 1998 5 15 98ZZZX1801 1 19980225 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 31 12796 S754 PRESSURE TRANSMITTER UNIT CAUSES PRESSURE GAUGE FLUCTUATION ON HIGH SIDE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1998051500957 19980515 00957 EU 1998 5 15 98ZZZX1802 1 19980302 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 15 12837 S754 PRESSURE TRANSMITTER UNIT CAUSES PRESSURE GAUGE FLUCTUATION ON HIGH SIDE. TRANSMITTER REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1998051500959 19980515 00959 EU 1998 5 15 98ZZZX1804 1 19980126 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 44 7129 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500961 19980515 00961 EU 1998 5 15 98ZZZX1806 1 19980114 A 6420 ABWT82008 BEARING BOLKMS 117 BK117B1 5626012 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911VU 342 7141 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500964 19980515 00964 EU 1998 5 15 98ZZZX1809 1 19980127 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 155 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998051500965 19980515 00965 NM 1998 5 15 98ZZZX1810 1 19980405 A 6720 900C2010240103 BRACKET DOUG MD900 MD900 3027375 NM PITCH CABLE ATT CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 2018 90000012 PILOT'S REPORT - WHILE ADJUSTING SNOW COVER ON THRUSTER CAN, PILOT HEAR A LOUD CRACK AS IF SOMETHING INSIDE THE TAILBOOM BROKE. MECHANIC DISASSEMBLED THRUSTER AND FOUND A BRACKET CRACKED AROUND THE 'PITCH CHANGE CABLE MOUNT POINT'. REPL ACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998051500966 19980515 00966 NM 1998 5 15 98ZZZX1811 1 19980322 A 7720 311671204 THERMOCOUPLE DOUG MD900 MD900 3027375 NM ENGINE T6 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 265 10A244 90000012 THERMOCOUPLE HAS FAULTY INDICATION AND EXCESSIVE RESISTANCE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998051500967 19980515 00967 NM 1998 5 15 98ZZZX1812 1 19980322 A 7720 311671204 THERMOCUPLE DOUG MD900 MD900 3027375 NM ENGINE T6 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 265 10A226 90000012 THERMOCOUPLE HAS FAULTY INDICATION AND EXCESSIVE RESISTANCE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998051500968 19980515 00968 NM 1998 5 15 98ZZZX1813 1 19980322 A 7712 3038226 TRIM BOX DOUG MD900 MD900 3027375 NM TORQUE DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 82 EMB56569007 90000012 TORQUE TRIM BOX TRIGGERING FAULT CODES: NCFALL - 13 AND AIRCRAFT FLT - 11. RESISTANCES FLUCTUATE WHEN CANNON PLUG IS W IGGLED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998051500978 19980515 00978 WP 1998 5 15 ASAA9880051 1 19980312 A 5210 NUT DOUG DC9 DC983 3022083 WP L1 DOOR MISSING A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 962AS 53076 SEA - AFTER ARRIVAL OF FLT 113, CREW REPORTED THE L1 DOOR WOULD NOT LATCH OPEN. REPLACED MISSING NUT ON DOOR HOLD OPEN LATCH AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998051500979 19980515 00979 WP 1998 5 15 ASAA9880050 1 19980312 A 5610 MECHANISM DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 935AS 49236 SEA - AFTER ARRIVAL OF FLT 92, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WAS DIFFICULT TO OPEN. ADJUSTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW MECHANISM, REPOSITIONED SIDEWALL PANEL AND WINDOW TRIM AND OPERATED NORMALLY . (M) 2 L 7 2 4F A6WE 1998051500980 19980515 00980 WP 1998 5 15 ASAA9880063 1 19980329 A 5210 LATCH DOUG DC9 DC982 3022082 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 957AS 49126 PDX - AFTER ARRIVAL OF FLT 281, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO RELEASE FROM THE LOCKED OPEN POSITION. LUBRI CATED THE DOOR HOLD OPEN LATCH AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998051500981 19980515 00981 NM 1998 5 15 ASAA9840048 1 19980306 A 5520 65C25746154 FITTING BOEING 737 7374Q8 NM ELEV HINGE FRETTING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 SEA - DURING C-CHECK, THE LEFT AND RT HORIZONTAL STAB OUTBOARD HINGE FITTINGS WERE FOUND TO BE FRETTING. REPAIRED PER E A 5520-01055. (M) 2 L 7 2 4F RT A16WE 1998051500982 19980515 00982 NM 1998 5 15 ASAA9840049 1 19980306 A 5753 6546486130 SKIN BOEING 737 7374Q8 NM RT TE MIDFLAP DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 SEA - DURING C-CHECK, RIGHT INBOARD MID FLAP WEDGE LOWER SURFACE WAS FOUND TO BE DENTED. REPAIRED PER EA 5750-01272 AND BOEING TELEX ASA-SEA-98-0062RR. (M) 2 L 7 2 4F RT A16WE 1998051500983 19980515 00983 NM 1998 5 15 ASAA9840050 1 19980306 A 5751 65259112 SPAR BOEING 737 7374Q8 NM RT AILERON DELAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 SEA - DURING C-CHECK, FOUND DELAMINATION IN THE LOWER INBOARD EDGE OF THE RT AILERON FRONT SPAR. REPAIRED PER EA 5760-0 1008 AND BOEING TELEX ASA-SEA-98-0063RR. (M) 2 L 7 2 4F RT A16WE 1998051500984 19980515 00984 NM 1998 5 15 ASAA9840052 1 19980310 A 5210 MECHANISM BOEING 737 7374Q8 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 782AS 25113 SEA - PRIOR TO F340, THE L1 DOOR WAS FOUND TO BE VERY STIFF DURING OPENING AND CLOSING. LUBRICATED DOOR HINGE AND CYCLE D DOOR SEVERAL TIMES, DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998051500985 19980515 00985 NM 1998 5 15 ASAA9840051 1 19980306 A 7830 6997542 DOOR BOEING 737 7374Q8 NM NR 2 ENG TR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 SEA - DURING C-CHECK, THE NR 2 ENGINE INBOARD T/R MID ACTUATOR ACCESS DOOR CUTOUT WAS FOUND TO BE DAMAGED. REPAIRED PER EA 7110-01064 AND BOEING TELEX ASA-SEA-98-0061RR. (M) 2 L 7 2 4F RT A16WE 1998051500986 19980515 00986 NE 1998 5 15 WRLA98077 2 19980329 A 7260 3508806 SEAL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE LEAKING A WRLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 9MMAW 46959 DURING INITIAL CLIMB-OUT, FLIGHT CREW NOTE NR 2 ENGINE OIL QUANTITY DROPPING. FLIGHT CREW ELECTED TO RETURN TO POINT OF DEPARTURE FOR MAINTENANCE. AIRCRAFT RETURNED TO POINT OF DEPARTURE, LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE PER SONNEL FOUND 'GARLOCK' SEAL ON ACCESSORY GEARBOX (AT RT HYD PUMP LOCATION) LEAKING. REPLACED SEAL, GROUND RAN ENGINE WI TH NO FAULTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F A22WE E23EA 1998051500988 19980515 00988 WP 1998 5 15 RAIA980311 2 19980317 A 7314 8974007 FUEL PUMP BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 03 423AM 858 FLT 7344 - STL - RIGHT FUEL LOW PRESSURE CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT FUEL PUMP/CONT ROL. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998051500989 19980515 00989 EU 1998 5 15 AALA980300 1 19980210 A 2840 CGCC AIRBUS 300 A300B4605R 3930308 EU E/E COMPT MALFUNCTIONED A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 8067A 510 JFK - FLT 611 - INITALLY RECEIVED AFT FUEL TRANSFER UNAVAILABLE, SEVERAL MINUTES LATER WE RECEIVED EXCESSIVE AFT CG ECAM WARNING. CG AT THE TIME WAS APPROX 29.3 PERCENT. WENT TO ALTERNATE FUEL BURN PROCEED. AND CG WENT TO 28.3 PERCENT. T HEN RECEIVED CONTINUOUS EXCESSIVE AFT CG WARNING ABOUT EVERY 10 MINUTES. PLACARDED/DEFRD THE CGCC INOP IAW MEL REF 28-2 7B AUTH 2-145DC-C. ENTERED IN MIC SHEET. REPLACED CGCC. PERFORMED INSTALLATION TEST AND RESET. NO FAULTS INDICATED. NO DEFECTS NOTED. REMOVED MEL 2-145DC-C. CLEARED MIC. (M) 2 L 7 2 4F RT A35EU 1998051500990 19980515 00990 1998 5 15 AALA980258 4 19980205 A 3460 FMC AIRBUS 300 A300B4605R 3930308 EU E/E COMPT FAILED A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 33069 512 JFK - FLT 132 - FMC WENT INDEPENDENT OPERATION AFTER TAKEOFF. COULD NOT GET THEM BACK TO NORMAL OPS 1R. REPLACED FMC N R 1 AND NR 2 FMC. ACCOMPLISHED DATA BASE LOAD UPDATE. BOTH SYSTEMS 1 AND 2. ACCOMPLISHED BITE CHECK. NORMAL OPERATIO N RESTORED. OK FOR SERVICE. (M) 2 L 7 2 4F RT A35EU 1998051500991 19980515 00991 NE 1998 5 15 ORJA9865 2 19980317 A 7200 ENGINE DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE NR 1 LEFT OVERTEMP A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 902RA 53490 ON TAKEOFF ROLL, BELOW 20 KTS, ENGINES JUST SPOOLED, LEFT ENGINE EGT REACHED 663 DEGREES PEAK, AFTER FUEL LEVER SHUT OFF AND TAKEOFF REJECTED. OPENED UPPER AND LOWER NR 1 ENGINE C-DUCTS, INSPECTED ENGINE EXTERIOR FOR OVERTEMP DAMAGE, TAIL EXHAUST SECTION FOR OVERTEMP. BOROSCOPED HPC SECTION, NO DISCREPANCIES NOTED, RAN ENGINE PER MM 71-01-02. ALL TEMPS WI THIN NORMAL PARAMETERS, CLOSED C-DUCTS ASSY PER MM CH 71-13-00. (M) 2 L 7 2 4F 4 F RT A6WE A40NE 1998051500992 19980515 00992 NE 1998 5 15 ORJA9840 2 19980223 A 7230 COMPRESSOR DOUG DC9 DC987 3022087 WP PWA JT8 JT8D217C 52053 NE NR 1 ENGINE STALLED A ORJA O OTHER K FLUID LOSS TO TAKEOFF 1 WP 11 754RA 49641 LEFT ENGINE COMPRESSOR STALLED DURING TAKEOFF RUN SUSPECT ICE INGESTION DUE TO SEVERE WINTER CONDITIONS. INSPECTED NR 1 ENGINE INLET FAN AND EXHAUST AREAS, NO DAMAGED NOTED RAN NR 1 ENGINE TO TAKEOFF POWER AND PERFORMED ACCELERATION AND PO WER ASSURANCE RUN NR 1 ENGINE PARAMETERS ARE NORMAL PER MM 71-00-00. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1998051500993 19980515 00993 WP 1998 5 15 RAIA980318 2 19980327 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 424AM 865 FLT 7468 - BRL - AIRCRAFT DIVERTED TO BRL, RIGHT ENGINE TORQUE FLUCTUATED IN FLIGHT. MAINTENANCE REPLACED RIGHT ENGINE FUEL BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998051500994 19980515 00994 NE 1998 5 15 AALA980556 2 19980321 A 7510 ANTI-ICE VALVE AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 1 ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 8067A 510 YQX - FLT 141 - NR 1 ENGINE ANTI-ICE NACELLE VALVE FAILED TO OPEN. ICING CONDITIONS ANTICIPATED AT JFK. DIVERTED TO GA NDER. NR 1 ENGINE NACELLE ANTI-ICE VALVE LOCKED OPEN AND DEFERRED PER MEL 30-1B AUTH NO 3-55DC-C. REMOVED AND REPLACED NR 1 ANTI-ICE VALVE. OPS CHECKS OK IAW MM 30-21-11-4. REMOVED MEL PLACARD 30-1B AUTH 3-55DC-C. CLEARED MIC SHEET. ( M) 2 L 7 2 4F 4 F RT A35EU E13NE 1998051500995 19980515 00995 NE 1998 5 15 HALA9800070 2 19980322 A 7321 7036025 FUEL CONTROL DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 ENGINE MALFUNCTIONED A HALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 13 420EA 47689 HNL - FLT 508 - DURING CLIMB-OUT AT TAKEOFF POWER 2.05 THE RIGHT ENGINE HAD A FLUCTUATION OF 2.01 TO 2.08 ON THE EPR. A LL OTHER ENGINE GAUGES SHOWED SAME FLUCTUATION ON THE RT ENGINE. REMOVED AND REPLACED NR 2 ENGINE FCU PER HAL 97.6. GR OUND RUN CHECK OK. (M) 2 L 7 2 4F 4 F RT A6WE E2EA 1998051500996 19980515 00996 NE 1998 5 15 WTAA980043 2 19980305 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT/RT OVERTEMP A WTAA O OTHER J WARNING INDICATION CR CRUISE 1 WP 17 284YV 120284 SFO - POSSIBLE ENGINE OVERTEMP AND OVER TORQUE REPORTED ON BOTH ENGINES DURING STALL WARNING ACTIVATION WHILE AIRCRAFT W AS IN HOLDING PATTERN. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT REMAINS IN SFO MAINTENANCE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998051500997 19980515 00997 NE 1998 5 15 REXA98068 2 19980315 A 7597 WIRE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A REXA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 922MA 340A077 AIR VALVE LIGHT ON LEFT ENGINE 92 PERCENT NG AND 60 PERCENT TORQUE. REPAIRED WIRING BETWEEN ANTI-ICE SH/BLEED VALVE AND GARRET VALVE IAW 75-10-00. OPS CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998051500998 19980515 00998 NE 1998 5 15 EISA98067 2 19980324 A 7314 371900 FUEL PUMP BOEING 727 7272A7 138407K NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 310NE 20241 AFTER TAKEOFF FROM BDL, NR 2 ENGINE COMPRESSOR STALLED AND FAILED. ACCOMPLISHED APPROPRIATE TWO ENGINE OPERATING CHECKL IST. FLIGHT CONTINUED TO DESTINATION BOS. REMOVED AND REPLACED ENGINE FUEL PUMP IAW PRATT AND WHITNEY MM 73-11-1. OPS LEAK CHECK GOOD IAW MM 71-00. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998051500999 19980515 00999 NE 1998 5 15 USAASB98081 2 19980329 A 7261 05630606 FILTER BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE DIRTY A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 270AU 22882 MCO - FLT 254 - THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED OVER MCO AT 25,000 FEET. CREW REDUCED POER AND LIGH T WENT OUT, BUT THEN REILLUMINATED AND REMAINED ON EVEN AT IDLE. CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED TO MCO WHE RE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 5 MINUTES. MAI NTENANCE REMOVED AND REPLACED THE NR 1 ENGINE OIL FILTER. NO DEFECTS OR DEBRIS NOTED. ALSO, REPLACED OIL FILTER DIFFER ENTIAL PRESSURE SWITCH. RAN ENGINE. LEAK CHECK AND OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998051501000 19980515 01000 WP 1998 5 15 USAAD98048 1 19980322 A 2840 FUEL INDICATION DOUG DC9 DC981 3022081 WP CTR WING MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 819US 48099 BWI - FLT 545 - THE A/C WAS OPERATING UNDER MEL 28.2, CENTER TANK FORWARD BOOST PUMP INOPERATIVE. IT WAS DETERMINED THE LINE OF FLIGHT COULD OPERATE WITH THE MAIN FUEL TANK FUEL ONLY, BASED ON THE THEN CURRENT CONDITIONS. AFTER DEPARTURE, THE CREW NOTICED THAT DUE TO ATC VECTORS AND NOT CLIMBING TO OPTIMUM ALTITUDE, 1,000 LBS OF ADDITIONAL FUEL WAS USED. T HE CREW ALSO NOTICED THAT THE ORIGINAL 350 LBS OF FUEL TRAPPED IN THE CENTER TANK WAS NOW INDICATING 600 LBS. CONCERNED ABOUT A POSSIBLE FUEL MIGRATION AND THE OVERBURN, THE AIRCRAFT DIVERTED TO BWI FOR ADDITIONAL FUEL AND MAINTENANCE INSP ECTION. MAINTENANCE BACKFLUSHED THE CENTER TANK CHECK VALVES, TRANSFERED FUEL FROM THE LEFT AND RIGHT TANKS TO THE CEN 2 L 7 2 4F A6WE 1998051501001 19980515 01001 WP 1998 5 15 USAAD98049 1 19980320 A 2160 32185831 VALVE DOUG DC9 DC981 3022081 WP AFT FUSELAGE FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 813US 48093 MHT - FLT 353 - AFTER TAKEOFF THE LEFT AIR CONDITIONING PACK OVERHEATED PRODUCING SMOKE IN THE COCKPIT AND PASSENGER CAB IN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE MEL'D THE LEFT AIR CONDITIONING PACK. LATER THE LEFT CABIN TEMPERATURE CONTROL VALVE WAS REPLACED. (M) 2 L 7 2 4F A6WE 1998051501002 19980515 01002 NM 1998 5 15 USAABB98027 1 19980406 A 2750 251N42045 TRANSMISSION BOEING 757 7572B7 1384964 NM RT TE FLAP REQ'D SERVICE A USAA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 EA 19 611AU 27123 DCA - FLT 10 - ON APPROACH TO DCA, WHEN PILOT MOVED THE FLAPS FROM THE '20' POSITION, RECEIVED THE TRAILING EDGE LIGHT A ND THE EICAS MESSAGE 'TE FLAP DISAGREE'. PILOT PERFORMED GO-AROUND, SELECTED ALTERNATE FLAPS, AND LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE FOUND BOTH OUTBOARD FLAP TRANSMISSION INDICATORS EXTENDED. THE RIGHT TRANSMISSION (NR 8) WAS F OUND WITH LOW TRANSMISSION FLUID. TRANSMISSION WAS SERVICED AND THE ASSEMBLY LUBED AND OPERATIONALLY CHECKED. (M) 2 L 7 2 4F RT A2NM 1998051501003 19980515 01003 WP 1998 5 15 HALA9800091 1 19980408 A 3610 CONTROLLER DOUG DC10 DC1010 3022110 WP NR 1 PNEU SYSTEM FAILED A HALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 WP 13 148AA 46703 FLT 25 - LOS - NR 1 MANIFOLD FAIL LIGHT ILLUMINATED DURING CLIMB. PERFORMED ABNORMAL PROCEDURE. SUPPLY SELECTOR AND PA CK OFF. LIGHT DIDN'T GO OUT WITH SYSTEM UNPRESSURIZED AND PNEU TEMPERATURE BELOW 120 DEGREES. LEFT SYSTEM UNPRESSURIZE D AND DEACTIVATED FAULTY WARNING SYSTEM. PULLED MANIFOLD FAILURE DET LT LOOP 1 C/B. (M) 2 L 7 3 4F A22WE 1998051501004 19980515 01004 WP 1998 5 15 HALA9800093 1 19980409 A 2120 72743510 CIRCUIT BREAKER DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 152AA 46707 LAX - FLT 1 - OBNOXIOUS FUMES NOTICED IN COCKPIT, SOURCE UNKNOWN. FOUND AUX COMPT FAN RUNNING ON A AND C PHASES ONLY. R EPLACED FAILED C/B B1-277 AND N1-221. OPS CHECK AND SNIFF CHECK OK. (M) 2 L 7 3 4F A22WE 1998051501005 19980515 01005 NM 1998 5 15 BJNA9800301 1 19980331 A 2560 SLIDE BOEING 737 7372H4 138448C NM R1 DOOR FELL OFF A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 456TM 20336 R-I EMERGENCY ESCAPE SLIDE FELL OFF DOOR. MECHANIC REATTACHED TO DOOR, REINSPECTED SLIDE PACK ASSY PER BMM 25-61-311. ( M) 2 L 7 2 4F A16WE 1998051501006 19980515 01006 NM 1998 5 15 BJNA9800302 1 19980402 A 2613 CONNECTOR BOEING 737 737214 138446R NM NR 1 ENGINE DIRTY A BJNA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 SLT - NR 1 ENGINE OVERHEAT LIGHT IS ON INTERMITTENT IN FLIGHT, ON 100 PERCENT ON GROUND. AIRCRAFT RELEASED PER MEL 26-2 , DMI 0402, PER PLACARD INSTALLED. CLEANED OIL FROM CONNECTORS ON NR 1 ENGINE PER BMM 26-11-0. TESTS NORMAL PER BMM 26 -11-0. (M) 2 L 7 2 4F A16WE 1998051501007 19980515 01007 NM 1998 5 15 BJNA9800303 1 19980407 A 2611 CONNECTORS BOEING 737 737214 138446R NM NR 1 ENGINE DIRTY A BJNA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 NR 1 ENGINE OVERHEAT LIGHT ON. CLEANED OVERHEAT LOOP CONNECTORS, REPLACED COPPER GASKETS. OPS CHECKED OK, IAW BMM 26-1 0-00. (M) 2 L 7 2 4F A16WE 1998051501008 19980515 01008 WP 1998 5 15 ARWA980405 1 19980409 A 2750 472085119 COMPARATOR LKHEED 1011 1011385115 5265015 WP TE FLAPS FAILED A ARWA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 19 306GB 301 193U1138 ATL - FLT 20 - FLAPS LOCKED OUT ON TAKEOFF AT 10. NO EMERGENCY DECLARED, AIR TURN BACK NO FUEL DUMPED. REMOVED AND REP LACED SLAT COMPARATOR. OPS CHECKED NORMAL AT THIS TIME IAW MM 27-00-00. (M) 2 L 7 3 4F A23WE 1998051501009 19980515 01009 NM 1998 5 15 PCAA9800743 1 19980302 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 829EX 146 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM FORWARD OF SEAT 1DF. REMOVED AND REPLACED BULB. OPE RATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501010 19980515 01010 NM 1998 5 15 PCAA9800740 1 19980302 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 813AW 247 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGH T ASEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501011 19980515 01011 NM 1998 5 15 PCAA9800746 1 19980301 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 832EX 280 AFT EMERGENCY FLOOR PROXIMITY LIGHT INOPERATIVE. REMOVED AND REPLACED AFT FLOOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501012 19980515 01012 NM 1998 5 15 PCAA9800742 1 19980303 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 820EX 019 LEFT FLOOR EMERGENCY PROXIMITY LIGHTING HAS SEVERAL LIGHTS INOPERATIVE. SECURED LOOSE PLUG AT AFT CABIN WIRING CIRCUIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501013 19980515 01013 NM 1998 5 15 PCAA9800741 1 19980304 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 818EX 235 COCKPIT PORTABLE EMERGENCY LIGHT CAME ON TWICE AND REMAINED ON. CABIN EMERGENCY LIGHTS ARE OFF. REMOVED AND REPLACED C OCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT A13NM 1998051501014 19980515 01014 NM 1998 5 15 PCAA9800747 1 19980305 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 811AW 201 EMERGENCY LIGHT INOPERATIVE AT AFT CABIN CEILING. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501015 19980515 01015 NM 1998 5 15 PCAA9800748 1 19980312 A 5610 17180003 WINDOW DHAV DHC8 DHC8102 2809003 NM LT COCKPIT CRACKED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 815EX 321 DURING CRUISE FLIGHT FROM BOS TO SYR, THE CAPTAINS SIDE WINDOW CRACKED. A/C LANDED WITHOUT INCIDENT IN SYR. MAINTENANC E REMOVED AND REPLACED THE CAPTAINS SIDE WINDOW IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501016 19980515 01016 NM 1998 5 15 PCAA9800754 1 19980312 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 821EX 173 SEVERAL SMALL BULBS INOPERATIVE IN FORWARD OVERHEAD EMERGENCY EXIT SIGN. REMOVED AND REPLACED BULBS. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501017 19980515 01017 NM 1998 5 15 PCAA9800751 1 19980313 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 809EX 302 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT REMAINS ILLUMINATED WHEN POWER IS SHUT OFF. REMOVED AND REPLACED COCKPIT OVER HEAD PORTABLE EMERGENCY LIGHT ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501018 19980515 01018 NM 1998 5 15 PCAA9800750 1 19980313 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 804EX 227 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT STAYS ON IN FLIGHT. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT AND BASE ASSEMBLY WITH SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501019 19980515 01019 NM 1998 5 15 PCAA9800749 1 19980314 A 3234 SELECTOR VALVE DHAV DHC8 DHC8102 2809003 NM LANDING GEAR FAILED A PCAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 13 834EX 285 UPON APPROACH INTO MDT, WHEN GEAR WAS SELECTED DOWN THE NR 2 HYDRAULIC SYSTEM PRESSURE WENT TO ZERO. CREW PERFORMED AN ALTERNATE EXTENSION AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, FOUND THE LANDING GEAR SE LECTOR VALVE AT FAULT. REMOVED AND REPLACED THE SELECTOR VALVE IAW DHC PROCEDURES. PERFORMED THE LOSS OF FLUID INSPECT ION REQUIREMENTS. OPERATION OF GEAR AND LEAK CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501020 19980515 01020 NM 1998 5 15 PCAA9800752 1 19980315 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 809EX 302 FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH INTERNAL LAMP INOPERATIVE. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501021 19980515 01021 NM 1998 5 15 PCAA9800753 1 19980315 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 818EX 235 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501022 19980515 01022 NM 1998 5 15 PCAA9800755 1 19980315 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 EICHP 258 CABIN CENTER AND FORWARD OVERHEAD EMERGENCY SIGNS HAVE SEVERAL INOPERATIVE BULBS. REMOVED AND REPLACED BULBS. OPERATIO NAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501023 19980515 01023 NM 1998 5 15 PCAA9800762 1 19980316 A 3350 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 828EX 392 ONE LIGHT INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REMOVED AND REPLACED BULB. OPERATIONAL TEST NORMAL . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501024 19980515 01024 NM 1998 5 15 PCAA9800756 1 19980316 A 5610 17180003 WINDOW DHAV DHC8 DHC8102 2809003 NM LT COCKPIT CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 839EX 226 EN ROUTE TO BWI, THE CAPTAINS SIDE WINDOW CRACKED. A/C LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE C APTAINS SIDE WINDOW IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501025 19980515 01025 NM 1998 5 15 PCAA9800757 1 19980317 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 804EX 227 LEFT AFT EXTERIOR AND TWO OVERHEAD CABIN EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWR SUPPLY AT POSITION NR 300. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501026 19980515 01026 NM 1998 5 15 PCAA9800759 1 19980317 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 804EX 227 LEFT FORWARD FUSELAGE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT POSITION NR 200. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501027 19980515 01027 NM 1998 5 15 PCAA9800760 1 19980317 A 3350 6104781 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 804EX 227 EMERGENCY EXIT LIGHTED SIGN ABOVE AIRSTAIR DOOR WILL NOT LIGHT. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT PO SITION NR 100. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501028 19980515 01028 NM 1998 5 15 PCAA9800761 1 19980319 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 807EX 292 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGH T ASSEMBLY WILL SERVICEABLE UNIT. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501029 19980515 01029 NM 1998 5 15 PCAA9800764 1 19980320 A 3350 SIGN DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 819EX 016 EMERGENCY EXIT ICON AT RIGHT FORWARD CABIN HAS BROKEN BULBS. REMOVED AND REPLACED EXIT ICON. OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501030 19980515 01030 NM 1998 5 15 PCAA9800763 1 19980320 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A PCAA K NONE L NO TEST IN INSP/MAINT 1 EA 13 832EX 280 COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT A SSEMBLY WITH SERVICEABLE UNIT, OPERATIONAL TEST NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501031 19980515 01031 NM 1998 5 15 PCAA9800765 1 19980323 A 5610 17180003 WINDOW DHAV DHC8 DHC8102 2809003 NM LT COCKPIT CRACKED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 835EX 289 DURING CRUISE FLIGHT OUT OF SYR, THE CAPTAINS SIDE WINDOW CRACKED. AIRCRAFT RETURNED TO SYR AND LANDED WITHOUT INCIDENT . MAINTENANCE REMOVED AND REPLACED THE SIDE WINDOW IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501032 19980515 01032 NM 1998 5 15 PCAA9800767 1 19980330 A 2611 3023143 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGG COMPT FAILED A PCAA K NONE O OTHER TO TAKEOFF 1 EA 13 810EX 000017 308 UPON TAKEOFF FROM BDL, THE BAGGAGE SMOKE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. THE BAGGAGE COMPARTMENT WAS INSPECTED FOR EVIDENCE FO FIRE, NO EVIDENCE FOUND. MAINTENANCE ISOLATED THE SMOKE DETECTO RS AND THE AIRCRAFT WAS DISPATCHED UNDER MEL RELIEF. SUBSEQUENTLY, THE NR 1 AND NR 2 DETECTORS WERE REPLACED AND OPERAT IONALLY CHECKED IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501033 19980515 01033 NM 1998 5 15 PCAA9800745 1 19980302 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM TE FLAP DELAMINATED A PCAA K NONE O OTHER IN INSP/MAINT 1 EA 13 822EX 187 LEFT OUTBOARD FLAP COMPOSITE TRAILING EDGE UPPER SURFACE DELAMINATED OVER APPROXIMATELY 60 PERCENT OF SURFACE. REMOVED AND REPLACED LEFT OUTBOARD FLAP ASSEMBLY WITH SERVICEABLE UNIT. INVESTIGATION TO DETERMINE CAUSE OF TRAILING EDGE DEBON D CONTINUES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501034 19980515 01034 SO 1998 5 15 C2XA98CL033 1 19980403 A 3250 2050000001 POTENTIOMETER EMB 120 EMB120RT SO NLG OUT OF ADJUST A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 27716 133 120128 CLE - FLT 3214 - CREW REPORTED THAT DURING TAXI THE NOSE WHEEL STEERING INOP. DISCONNECT LIGHT ILLUMINATED AND THE NOSE ALIGNS TO THE RIGHT WITH THE HANDLE IN THE NEUTRAL POSITION. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. M AINTENANCE REMOVED AND REPLACED THE 9 DEGREE FEED BACK POT, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-120 MM 27-50-00 . AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998051501035 19980515 01035 SO 1998 5 15 C2XA98CL032 1 19980329 A 2150 PE2703462518 CLAMP EMB 120 EMB120RT SO RT PACK BROKEN A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 27716 120128 HPN - FLT 3066 - CREW REPORTED THAT DURING AIRCRAFT REPOSITIONED AFTER AN ABORTED TAKEOFF. SMOKE FILLED BOTH THE COCKPI T AND CABIN. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN CLAMP ON THE RIGHT PACK DISTRIBUTION DUCT. THE CLAM P WAS REMOVED AND REPLACED, THE OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-120 MM 21-50-00. AIRCRAFT RELEASED FOR SER VICE. (M) 2 L 7 2 4T RT A31SO 1998051501036 19980515 01036 SO 1998 5 15 C2XA98CL031 1 19980329 A 3250 12037995001 TILLER EMB 120 EMB120RT SO NLG STEERING FAILED A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 09 27716 120128 HPN - FLT 3066 - CREW REPORTED THAT UPON TAKEOFF THE AIRCRAFT PULLED HARD LEFT ASSOCIATED WITH THE PEDAL STEERING INOP L IGHT ILLUMINATING AND TEMPORARY STEERING LOSS. THE CREW ACCOMPLISHED QRH ITEMS AND ABORTED THE TAKEOFF. MAINTENANCE IN SPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE STEERING TILLER IAW EMB-120 MM 32-50-01. OPERATIONAL CHECKS WERE SAT ISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998051501037 19980515 01037 SO 1998 5 15 C2XA98IA083 1 19980329 A 5320 12009846001 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, FRAME 16 LEFT T-PROFILE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROFILE IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998051501038 19980515 01038 SO 1998 5 15 C2XA98IA084 1 19980329 A 5320 12004149001 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, FRAME 33 LEFT T-PROFILE WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED PROFILE IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998051501039 19980515 01039 SO 1998 5 15 C2XA98IA085 1 19980329 A 5320 12006442002 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 42 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED PROFILE IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998051501040 19980515 01040 SO 1998 5 15 C2XA98IA086 1 19980329 A 3350 30043221 LIGHT EMB 120 EMB120RT SO CABIN SHORTED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE LEFT OVERWING AFT EMERGENCY EXIT LIGHT HOUSING WAS FOUND SHORTED. MAINTENANCE REMO VED AND REPLACED THE AFFECTED HOUSING AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998051501041 19980515 01041 SO 1998 5 15 C2XA98IA087 1 19980329 A 5753 12034222010 SUPPORT EMB 120 EMB120RT SO RT TE FLAP CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 40717 120133 IAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FLAP CENTER SKIN SUPPORT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SUPPORT IAW THE EMB SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998051501042 19980515 01042 EU 1998 5 15 C2XA98023 1 19980403 A 7312 STUD AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE FUEL BOWL BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 BTV - DURING A LINE CHECK IN BTV, THE FUEL HEATER FILTER HAD A TIME CHANGE. DURING REINSTALLATION OF THE FILTER AND FI LTER BOWEL WHILE APPLYING PROPER TORQUE THE FILTER BOWEL ATTACHING STUD BROKE OFF. REMOVED AND REPLACED FUEL HEATER UNI T AND LEAK CHECKED OPS CHECK GOOD. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998051501043 19980515 01043 GL 1998 5 15 WRLA98080 2 19980412 A 7532 07P954 RELAY DOUG MD11 MD11 3023602 NM GE CF6 CF680C GL NR 3 ENGINE CORRODED A WRLA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 277WA 48743 DURING INITIAL TAKEOFF ROLL, NR 3 ENGINE EXPERIENCED HIGH EGT (661 DEGREES CELSIUS). FLIGHT CREW ELECTED TO ABORT TAKEO FF (80 KNOTS). AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND 2.95 BLEED VALVE STUCK IN THE OPEN POSITION. FURTHER INVESTIGATION FOUND THE BLEED VALVE RELAY CORRODED AND FROZEN. REPLACED RELAY AS A PRECA UTION, REPLACED BLEED VALVE SOLENOID. ENGINE HOT SECTION WAS BOROSCOPED PER MM REQUIREMENTS WITH NO FAULTS NOTED. PERF ORMED HIGH POWER GROUND RUNS WITH NOT FAULTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A22WE E23EA 1998051501044 19980515 01044 NE 1998 5 15 WTAA980062 2 19980405 A 7310 3035681 FUEL FILTER EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE RESTRICTED A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 455UE 120163 SFO - RIGHT FUEL FILTER LIGHT ILLUMINATED ON TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE REPLACED RIGHT ENGINE HIGH AND LOW PRESSURE FUEL FILTERS. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998051501045 19980515 01045 WP 1998 5 15 ORJA9878 1 19980412 A 3350 59306431 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 878RA 53184 ROW 18D AISLE EMERGENCY IGHT OUT. ALSO, THREE OVERHEAD EMERGENCY LIGHTS OUT. RESEALED CONNECTOR RECESSED PIN AND REPLA CED BATTERIES FOR OVERHEAD LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998051501046 19980515 01046 NE 1998 5 15 WTAA980063 2 19980410 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT BIRD STRIKE A WTAA K NONE C F.O.D. UK UNKNOWN 1 WP 17 221YV 120221 FAT - BIRD STRIKE TO LEFT ENGINE INLET REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998051501047 19980515 01047 EU 1998 5 15 WTAA980064 1 19980413 A 5330 SKIN BAG JETSTM JETSTM3101 1500215 EU FUSELAGE BIRD STRIKE A WTAA K NONE C F.O.D. UK UNKNOWN 1 WP 17 431UE 813 SMF - BIRD STRIKE ON LEFT SIDE OF AIRCRAFT REPORTED. MAINTENANCE INSPECTED AIRCRAFT FOR DAMAGE. NO DAMAGE NOTED. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998051501048 19980515 01048 WP 1998 5 15 WTAA980067 2 19980416 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RIGHT BIRD STRIKE A WTAA K NONE C F.O.D. AP APPROACH 1 WP 17 419UE 779 OXR - BIRD STRIKE TO RIGHT ENGINE ON APPROACH. MAINTENANCE INSPECTED ENGINE FOR DAMAGE. FOUND RIGHT ENGINE INGESTED BI RD. REPLACED RIGHT ENGINE. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998051501049 19980515 01049 EU 1998 5 15 WTAA980066 1 19980416 A 5400 NACELLE BAG JETSTM JETSTM3101 1500215 EU RIGHT BIRD STRIKE A WTAA K NONE C F.O.D. LD LANDING 1 WP 17 107XV 723 SMF - BIRD STRIKE TO RIGHT NACELLE ON LANDING. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998051501050 19980515 01050 EU 1998 5 15 WTAA980065 1 19980413 A 7931 CONNECTOR BAG JETSTM JETSTM3101 1500215 EU LT ENGINE DIRTY A WTAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 17 418UE 780 FAT - LEFT ENGINE OIL PRESSURE REPORTED IN THE YELLOW WITH NEEDLE ERRATIC. AIRCRAFT RETURNED TO STATION WITHOUT INCIDEN T. MAINTENANCE CLEANED CANNON PLUG TO OIL PRESSURE TRANSMITTER. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998051501051 19980515 01051 1998 5 15 WTAA980068 4 19980417 A 3417 02702M0D1 AIR DATA SENSOR EMB 120 EMB120RT SO FUSELAGE FAILED A WTAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 17 250YV 120250 FAT - AURAL WARNING, GROUND PROXIMITY WARNING AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION. MAINTENANCE DEFERRED GPWS. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPLACING AIR DATA SENSOR NR 3. GPWS TEST NORMAL. LEAK CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1998051501052 19980515 01052 NM 1998 5 15 GAIA9841 1 19980421 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 854AA 20995 THE FOLLOWING ITEM LEVEL 2 CORROSION FINDINGS DURING A HEAVY C-CHECK FOR AIRCRAFT CORROSION ON STRINGER, AT STATION 720, STRINGER 29L. REPAIRED BY AAR ON NON-ROUTINE 1000-0272. (M) 2 L 7 3 4F A3WE 1998051501053 19980515 01053 EU 1998 5 15 WTAA980069 1 19980418 A 3260 622800200 SWITCH BAG JETSTM JETSTM3101 1500215 EU RT MLG FAILED A WTAA K NONE O OTHER DE DESCENT 1 WP 17 424UE 796 LAX - RIGHT MAIN LANDING GEAR INTRANSIT LIGHT REMAINED ILLUMINATED FOR ONE MINUTE. AFTER GEAR SELECTED DOWN. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK MICROSWITCH. OPERATIONAL CHECK SATIS FACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998051501054 19980515 01054 WP 1998 5 15 WRLA98081 1 19980416 A 2932 VT0107F PRESS XMITTER DOUG DC10 DC1030 3023501 WP NR 2 HYD SYSTEM FAILED A WRLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 9MMAW 46959 DURING INITIAL TAXI, FLIGHT CREW NOTED NR 2 HYDRAULIC SYSTEM PRESSURE INDICATION INOPERATIVE. FLIGHT CREW ELECTED TO RE TURN TO DEPARTURE GATE FOR MAINTENANCE. AIRCRAFT RETURNED TO DEPARTURE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERS ONNEL FOUND NR 2 HYDRAULIC SYSTEM PRESSURE TRANSMITTER HAD FAILED. REPLACEMENT PART WAS NOT AVAILABLE AT CURRENT LOCATI ON. SYSTEM DEFERRED PER MEL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A22WE 1998051501055 19980515 01055 WP 1998 5 15 WRLA98082 1 19980416 A 2781 DISAGREE LIGHT DOUG DC10 DC1030 3023501 WP LE SLATS ILLUMINATED A WRLA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 9MMAZ 46933 DURING TAKEOFF, FLIGHT CREW NOTED SLAT DISAGREE LIGHT. FLIGHT CREW ELECTED TO DISCONTINUE TAKEOFF (MAX SPEED ATTAINED 1 40 KNOTS) AND RETURN TO DEPARTURE GATE FOR MAINTENANCE. AIRCRAFT RETURNED TO DEPARTURE GATE WITHOUT FURTHER INCIDENT. M AINTENANCE PERSONNEL PERFORMED SLAT RETRACTION AND EXTENSION CHECKS WITH NO FAULTS NOTED. PERFORMED CHECK ON ALL PROXIM ITY TARGETS WITH NO FAULTS NOTED. MAINTENANCE PERSONNEL WERE UNABLE TO DUPLICATE FAULT. AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 3 4F A22WE 1998051501056 19980515 01056 EU 1998 5 15 SIMA981083 1 19980418 A 5347 S53375001206 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 425MJ 425 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT FORWARD OUTBOARD, LEF T CENTER OUTBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT CENTER OUTBOARD AND THE RIGHT FLIGHT ATTENDANT. MAINTENAN CE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998051501057 19980515 01057 EU 1998 5 15 SIMA981111 1 19980421 A 5315 S5367240620801 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 342AT 345 SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36 WAS CORRODED. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SR M 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998051501058 19980515 01058 EU 1998 5 15 SIMA981112 1 19980421 A 5320 S53678008200 SUPPORT AEROSP ATR72 ATR72212 EU FRAME 39/40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 342AT 345 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT SIDE FLOOR SUPPORT BETWEEN FRAME 39 AND 40 CORRODED. M AINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998051501059 19980515 01059 NM 1998 5 15 MASA98082 1 19980413 A 3350 6038443 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 FLT 7565 - SHR-GCC - CREW TESTED EMERGENCY LIGHTS AND THEY WOULD NOT ILLUMINATE. MAINTENANCE CHARGED BATTERIES, OPS CHE CK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998051501060 19980515 01060 NM 1998 5 15 MASA98083 1 19980414 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 DURING ROUTINE MAINTENANCE, EMERGENCY LIGHTS THROUGHOUT CABIN FAILED TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLIES , 6 TOTAL. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998051501061 19980515 01061 NM 1998 5 15 GAIA9840 1 19980422 A 5313 STRINGER BOEING 727 727251 138408H NM BS 740 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 264US 19983 DURNG A ZERO LIGHT 'C' INSPECTION, FOUND STRINGER 27L AT THE TIE END HAD CORROSION AT STATION 740. REMOVED TIE END, CLE ANED CORROSION AND FOUND TO BE WITHIN LIMITS. REMOVED AND REPLACED 30 INCHES OF STRINGER IAW SRM 53-10-3 AT 27L, STATIO N 740. (M) 2 L 7 3 4F A3WE 1998051501062 19980515 01062 NM 1998 5 15 P2EA98041 1 19980324 A 3350 LIGHT BOEING 737 737244 138448U NM CABIN INOPERATIVE A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 620PC 19708 ATL - DISCREPANCY FOUND DURING SCHEDULED MAINTENANCE CHECK, EMERGENCY TRACK LIGHTING INOP, SEAT ROW 11 AND AFT. REPAIRE D WIRING AT ROW 18 AND AFT BULKHEAD. REPLACED FUSES IN FWD AND AFT BATTERY PACKS. (M) 2 L 7 2 4F A16WE 1998051501063 19980515 01063 NM 1998 5 15 P2EA98042 1 19980325 A 3340 LIGHT BOEING 737 737222 1384473 NM NLG MISSING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 FLT 435 - PIT - FOUND DURING PREFLIGHT WALK AROUND, TAXI LIGHT MISSING, BRACKET CRACKED. DEFERRED PER CDL 33-40-2. CI NR C603807 ASSIGNED. INSTALLED NOSE TAXI LIGHT ASSY AND WIRE HARNESS REF MM 33-42-51. OPS CHECK OK. PERFORMED NOSE GE AR SWING ALL CLEARANCES CHECK OK. (M) 2 L 7 2 4F A16WE 1998051501064 19980515 01064 EU 1998 5 15 RAIA980403 1 19980403 A 7714 AG34 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 338TE 932 FLT 7532 - STL - RIGHT ENGINE RPM DROPPED TO ZERO. MAINTENANCE REPLACED RIGHT ENGINE TACH GENERATOR. (M) 2 L 7 2 4T RT A56EU 1998051501065 19980515 01065 1998 5 15 RAIA980404 4 19980409 A 3452 6226590001 TRANSPONDER BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 338TE 932 FLT 7438 - STL - BOTH TRANSPONDERS WOULD NOT TRANSMIT OR ENCODE INFORMATION TO ATC. MAINTENANCE REPLACED CAD 62 ADAPTER . (M) 2 L 7 2 4T RT A56EU 1998051501066 19980515 01066 EU 1998 5 15 RAIA980405 1 19980412 A 7921 L86023281 COOLER JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA B E EMER. DESCENT ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 03 571HK 4244 41090 FLT 7756 - JFK - RIGHT ENGINE OIL PRESSURE DROPPED, CREW PERFORMED ENGINE SHUTDOWN. MAINTENANCE REPLACED RIGHT ENGINE O IL COOLER ASSEMBLY. (M) 2 L 7 2 4T RT A41NM 1998051501067 19980515 01067 EU 1998 5 15 SIMA980972 1 19980407 A 5320 S536780026901 SUPPORT AEROSP ATR72 ATR72212 EU SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 399AT 399 SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SUPPORT BEAM UNDER SILL PLATE CORRODED. MAINTENAN CE REMOVED AND INSTALLED A NEW SERVICE DOOR SUPPORT BEAM IAW SRM 51-21-58 AND SRM 51-24-01. A/C WAS RETURNED TO SERVICE . (M) 2 H 7 2 4T RT A53EU 1998051501068 19980515 01068 EU 1998 5 15 SIMA980971 1 19980407 A 5320 S5367121729801 DRAIN TRACK AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 399AT 399 SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR SILL PLATE DRAIN TRACK AND THE PAX DOOR INTERCOSTAL WA S CORRODED. MAINTENANCE REPLACED THE DRAIN TRACK IAW SRM 51-25-03 AND THE PAX DOOR INTERCOSTAL IAW SRM 51-21-58 AND SRM 51-24-01. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998051501069 19980515 01069 NM 1998 5 15 TWRA9819 1 19980409 A 3350 58801 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 EGRESS LIGHTING IN AFT GALLEY INOP. REPLACED GALLEY LEFT FLOOR STRIP. OPS CHECKED OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1998051501077 19980515 01077 EU 1998 5 15 PLGA980317A 1 19980317 A 3020 SM15CSD1 RELAY SAAB SF340 340B 7860101 EU LT INTAKE HEAT OPEN A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 361BE 340B290 BOS - FLT 4243 - AFTER TAKEOFF, THE LEFT INTAKE HEAT FAILED. AIRCRAFT RETURNED TO BOS DUE TO WEATHER CONDITIONS. MAINT ENANCE REPLACED UPPER DUCT POWER RELAY (37HE). SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998051501078 19980515 01078 EU 1998 5 15 PLGA980315A 1 19980315 A 3150 044WS00 WEU SAAB SF340 SF340A 7850100 EU COCKPIT MALFUNCTIONED A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NE 05 745BA 1168 340A111 BOS - FLT 4388 - TAKEOFF WAS ABORTED DUE TO CONFIGURATION WARNING. MAINTENANCE REPLACED WARNING ELECTRICAL UNIT. SYSTE M TESTED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998051501079 19980515 01079 EU 1998 5 15 PLGA980313A 1 19980313 A 2611 SMOKE DET SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A PLGA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NE 05 363BE 340B293 YOW - FLT 4519 - TAKEOFF WAS ABORTED DUE TO CARGO SMOKE WARNING. MAINTENANCE INSPECTED CARGO AREA AND FOUND NO EVIDENCE OF SMOKE OF FIRE. SMOKE DETECTOR WAS CLEANED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998051501080 19980515 01080 EU 1998 5 15 PLGA980310A 1 19980310 A 3246 5006227 WHEEL SAAB SF340 SF340A 7850100 EU LT NLG OUT OF ROUND A PLGA O OTHER O OTHER TO TAKEOFF 1 NE 05 742BA OCT951877 340A092 LGA - FLT 4792 - TAKEOFF WAS ABORTED DUE TO NOSE WHEEL SHIMMY. MAINTENANCE REPLACED BOTH NOSE GEAR WHEELS AND TIRES. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998051501081 19980515 01081 NM 1998 5 15 TWAA9806201 1 19980420 A 5330 SKIN BOEING 727 727231 1384079 NM BS 700-720 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54333 20460 JFK - DURING C-CHECK, FOUND FUSELAGE LAP SEAM BULGED AT STATION 700-720, STRINGER 25L. REMOVED CORROSION AND TREATED AR EA PER SRM 51-10-6. ALSO, REMOVED AND REPLACED CORRODED SECTION OF STRINGER PER SRM STRIGNER REPAIR 53-10-3, DETAIL 1. (M) 2 L 7 3 4F A3WE 1998051501082 19980515 01082 NM 1998 5 15 TWAA9806202 1 19980420 A 5311 FRAME BOEING 727 727231 1384079 NM BS 783.95 MISREPAIRED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 54333 20460 JFK - DURING C-CHECK, FOUND FUSELAGE FRAME REPAIR AT FLOORBEAM AREA LEFT SIDE OF CABIN AT STATION 783.95 WAS NOT PER MO 71T68 PHASE C. ACCOMPLISHED REPAIR PER MO 71T68 PHASE C, AND S/B 727-53-0197. (M) 2 L 7 3 4F A3WE 1998051501083 19980515 01083 NM 1998 5 15 TWAA9806203 1 19980420 A 5330 SKIN BOEING 727 727231 1384079 NM BS 700-720 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54333 20460 DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED AT STATION 700-720, STRINGER 27L. REMOVED CORRODED SECTION OF SKIN AND INS TALLED AN EXTERNAL DOUBLER REPAIR PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998051501084 19980515 01084 NM 1998 5 15 TWAA9806204 1 19980420 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 700/720 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54333 20460 JFK - DURING C-CHECK, FOUND FUSELAGE STRINGER 27L WITH CORROSION BETWEEN STATION 700 AND STATION 720. REMOVED SECTION O F STRINGER AND INSTALLED SPLICE SECTION PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998051501085 19980515 01085 NM 1998 5 15 TWAA9806205 1 19980326 A 5320 INTERCOSTAL BOEING 727 727231 1384079 NM BS 420 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54342 21629 JFK - DURING C-CHECK, MAINTENANCE FOUND CABIN FLOOR PANEL INTERCOSTAL SUPPORT BEAM CORRODED BETWEEN SEAT TRACKS AT FS 42 0. REMOVED AND REPLACED BEAM PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998051501086 19980515 01086 NM 1998 5 15 TWAA9806206 1 19980327 A 5313 LONGERON BOEING 727 727231 1384079 NM BS 450-480 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64347 21634 STL - DURING MAINTENANCE CHECK, FOUND CORROSION ON SPLICE AT STATION 480, 28R AND 28L. REMOVED AND REPLACED LONGERON 28 R AND 28L, STATION 450 TO 480, PR SRM 53-10-3, AND 51-30-2, AND STANDARD PRACTICES. (M) 2 L 7 3 4F A3WE 1998051501087 19980515 01087 NM 1998 5 15 TWAA9806207 1 19980327 A 5320 DOOR FRAME BOEING 727 727231 1384079 NM BS 450 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64347 21634 STL - DURING ROUTINE MAINTENANCE, FOUND CORROSION ON DOOR FRAME AT STATION 450, L28R AND 28L. REMOVED AND REPLACED AFT E/E DOOR FRAME AT STATION 450, PER SRM 51-30-2, SRM 51-10-1, AND STD PRACTICES. (M) 2 L 7 3 4F A3WE 1998051501088 19980515 01088 NM 1998 5 15 TWAA9806208 1 19980326 A 5320 GUSSET BOEING 727 727231 1384079 NM BS 825.95 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54342 21629 JFK - DURING C-CHECK, FOUND WHILE ACCOMPLISHING MAINTENANCE FORM M27-AD-EL FOUND A 1.5 INCH CRACK IN LOWER RADIUS OF FRA ME GUSSET, RT SIDE OF FUSELAGE, BS 825.95. REMOVED AND REPLACED FRAME GUSSET PER MO 71T68 AND S/B 727-53-0197. (M) 2 L 7 3 4F A3WE 1998051501089 19980515 01089 WP 1998 5 15 ORJA9872 1 19980410 A 3610 F17D87 CLAMP DOUG DC9 DC983 3022083 WP TAIL COMPARTMENT BROKEN A ORJA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 WP 11 876RA 53183 RETURN TO GATE DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FOUND BROKEN CLAMP ON RT CROSSFEED VA LVE. LEAK CHECK OK. REMOVED AND REPLACED CLAMP. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998051501090 19980515 01090 WP 1998 5 15 ORJA9870 1 19980408 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 EMERGENCY LIGHT AT ROW 14 INOP. REPINNED BROKEN WIRE AT CONNECTOR. OPS NOW OK. (M) 2 L 7 2 4F RT A6WE 1998051501091 19980515 01091 WP 1998 5 15 ORJA9880 1 19980415 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 EMERGENCY LIGHT OUT AT SEAT 23D. REPAIRED BROKEN WIRE AT SEAT 23D. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998051501092 19980515 01092 NM 1998 5 15 ORJA9876 1 19980411 A 3397 WIRE DOUG MD90 MD9030 3023690 NM CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 901RA 53489 EMERGENCY FLOOR TRACK LIGHTING ONE LAMP INOP AT ROW 8. FOUND BROKEN WIRE. RECONNECTED, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998051501093 19980515 01093 WP 1998 5 15 ORJA9873 1 19980414 A 3411 851AH PITOT TUBE DOUG DC9 DC983 3022083 WP VERT STAB MALFUNCTIONED A ORJA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 WP 11 871RA 49788 RETURN TO GATE DUE TO PITOT/STALL HEAT OFF. NO POWER TO RUDDER LIMIT IN FLT OR GROUND POSITION THROUGH GROUND CONTROL R ELY C/B'S. REMOVED AND REPLACED PITOT STATIC TUBE PER MM 34-11-02. LEAK AND HEAT CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998051501094 19980515 01094 WP 1998 5 15 ORJA9875 1 19980412 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY EXIT SEAT LIGHTS INOP BETWEEN ROW 6 AND ROW 8. REPAIRED WIRING AT PIG TAIL AT ROW 6. REMOVED AND REPLACED FU SE AT FORWARD GALLEY SERVICE EXIT SIGN. (M) 2 L 7 2 4F RT A6WE 1998051501095 19980515 01095 EU 1998 5 15 VTZA98147 1 19980329 A 5610 1379628C402 WINDSHIELD BAG JETSTM JETSTM3201 1500217 EU COCKPIT CRACKED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 493UE 805 FLT 6233 - IAD-BWI - DURING CRUISE, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO FO'S WINDSCREEN CRACKED. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FO'S WINDSCREEN. OPS CHECK OK. AI RCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998051501096 19980515 01096 NM 1998 5 15 USAABB98028 1 19980406 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 LAX - EMERGENCY FLOOR LIGHTING INOPERATIVE AT ROWS 1 AND 23. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998051501097 19980515 01097 NM 1998 5 15 USAABB98032 1 19980425 A 3350 9221009 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 SFO - L1 AND R1 DOOR EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998051501098 19980515 01098 NM 1998 5 15 USAABB98031 1 19980405 A 3397 WIRE BOEING 757 757225 1384959 NM NLG NOT GROUNDED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 SFO - EMERGENCY LIGHTS WILL NOT TEST FROM SWITCH AT NOSE GEAR. MAINTENANCE REPAIRED A GROUND WIRE BETWEEN CONNECTOR D40 488J AND SWITCH S10035. (M) 2 L 7 2 4F RT A2NM 1998051501099 19980515 01099 NM 1998 5 15 USAABB98029 1 19980413 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 PHL - EMERGENCY FLOOR LIGHTING INOPERATIVE AT ROWS 1, 4, AND 29. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998051501100 19980515 01100 NM 1998 5 15 USAABB98033 1 19980405 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 SFO - FOUND EMERGENCY FLOOR LIGHTS AT ROWS 1, 6, AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998051501101 19980515 01101 NM 1998 5 15 USAAB98030 1 19980402 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 618AU 22210 LAX - FOUND FIRST THREE FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998051501102 19980515 01102 NM 1998 5 15 USAASB98096 1 19980416 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 526AU 23861 ROC - DURING TRANSIT CHECK WHILE ACCOMPLISHING OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM, MAINTENANCE FOUND THE FOR WARD ENTRYWAY EMERGENCY EXIT LIGHTS DIM AND AFTER 30 SECONDS OF OPERATION, LIGHTS WENT OUT. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK IN THE M1133 POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998051501103 19980515 01103 NM 1998 5 15 USAABB98035 1 19980413 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 LAX - FOUND EMERGENCY FLOOR LIGHTING AT ROWS 1, 4, 6 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998051501104 19980515 01104 WP 1998 5 15 TWAA9806104 1 19980322 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945-950 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 23L CORRODED, STATION 945 TO 950. REMOVED CORROSION PER SRM 51-10- 03. INSTALLED NEW PART PER SRM 51-01, PG 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998051501115 19980515 01115 NM 1998 5 15 TWAA9806004 1 19980419 A 5522 SKIN BOEING 767 767231 1385131 NM LT ELEVATOR GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 LAX - DURING C-CHECK, FOUND THE LEFT OUTBOARD HORIZONTAL STABILIZER ELEVATOR WITH A 6 INCH GOUGE AT TOP TRAILING EDGE, A PPROX 4.5 FT FROM INBOARD TE APPROX .0625 IN DEEP. FILLED GOUGE WITH FILLER 934NA AND HOT BONDED AND PAINTED PER SRM 55 -20-01. (M) 2 L 7 2 4F RT A1NM 1998051501119 19980515 01119 NM 1998 5 15 TWAA9805908 1 19980417 A 5753 SKIN BOEING 767 767231 1385131 NM NR 4 TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 LAX - DURING C-CHECK, MAINTENANCE FOUND ON RT WING THE NR 4 OUTBOARD TE FLAP, THE UNDERSIDE HAD A 1 INCH BY 4 INCH DELAM INATION TWO FEET FROM OUTBOARD END. MADE HOT BOND REPAIR PER SRM 51-70-05. (M) 2 L 7 2 4F RT A1NM 1998051501133 19980515 01133 NM 1998 5 15 K3HA980070 1 19980511 A 3350 08163000111 TRACK BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY PATH LIGHT TRACK TAPED OVER FORWARD OF SEAT 2ABC. REMOVED TAPE INSTALLED NEW PORTION OF TRACK PER MM 33-50-0. 2 L 7 3 4F A3WE 1998051501135 19980515 01135 NM 1998 5 15 M8XA9800007 1 19980512 A 3030 08516W PITOT HEAT ROSEMONT 08516W DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE FAILED A M8XA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 331MX 1536 148855 3074 EN ROUTE FROM DEN TO CYS, AIRCRAFT ENCOUNTERED ICING CONDITIONS. SINCE THE PITOT HEAT SYSTEM WAS MEL'D, AIRCRAFT WAS FO RCED TO RETURN TO DEN. AIRCRAFT LANDED IN DEN WITHOUT FURTHER INCIDENT. DEN MAINTENANCE PERSONNEL REPLACED THE NR 2 PI TOT TUBE IAW AMM 34-11-04. CONDUCTED A STATIC LEAK CHECK IAW AMM 34-11-00. NO DEFECTS NOTED. AIRCRAFT WAS THEN RETURN ED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998051501136 19980515 01136 WP 1998 5 15 CALA9800849 1 19980513 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 46900 INTERIOR LOWER LOBE AFT CARGO BILGE CORROSION ON FLOORBEAM STA 1841 UPPER SIDE ABOVE AND UNDER BETWEEN RBL 50 AND LBL 50 . TRIMMED OUT CORRODED AREA. FABRICATED AND INSTALLED DOUBLER AND ANGLE PER SRM 57-60-01, 53-16-01, 51-20-00, 53-00-01 . 2 L 7 3 4F A22WE 1998051501137 19980515 01137 WP 1998 5 15 CALA9800850 1 19980512 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 TAIL COMPARTMENT STA 1418 LONG 2L AND LONG 2R BELTFRAME CRACKED (3). REPAIRED BELTFRAME PER SRM 53-03 FIG 32 AND EC/RA 5310-03720. 2 L 7 2 4F A6WE 1998051501138 19980515 01138 WP 1998 5 15 CALA9800851 1 19980512 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83870 48056 TAIL COMPARTMENT STA 1418 LONG 2L AND 2R CRACKED (1). REPAIRED CRACKED LONGERON PER SRM 53-02 FIG 18. 2 L 7 2 4F A6WE 1998051501139 19980515 01139 WP 1998 5 15 ABXA9800445 1 19980511 A 3260 700010101 SWITCH DOUG DC8 DC863 302198A WP LT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 GEAR UPLATCH CHECK FAILED. LEFT GEAR LIGHT ON. RECYCLED GEAR, LIGHTS WENT OUT. REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH, OPS CHECK AND INDICATION WAS GOOD IAW DC8 MM 32-21-3. 2 L 7 4 4F 4A25 1998051501140 19980515 01140 WP 1998 5 15 ABXA9800446 1 19980511 A 7830 5958782503 DRIVE LINK DOUG DC9 DC941 302207N WP NR 2 ENGINE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 DURING COMPLIANCE WITH AD 96-10-11 AND AD 75-14-06, FOUND NR 2 ENGINE THRUST REVERSER, UPPER, LEFT, DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 MM 78-31-5. 2 L 7 2 4F A6WE 1998051501141 19980515 01141 NM 1998 5 15 DL72S980991 1 19980511 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8882Z 14371 21579 EMERGENCY EXIT LIGHT M1088 FAIL TEST. REPLACED BATTERY PACK, CHECKS OK. 2 L 7 3 4F A3WE 1998051501142 19980515 01142 NM 1998 5 15 DL72K980992 1 19980508 A 5313 65583757 STRINGER BOEING 727 727232 1384082 NM BS 848.95 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 THE OUTER CHORD OF THE STRINGER 17L CREASE BEAM WAS FOUND WITH A .5 CRACK AT STA 848.95. THE CRACK WAS IN THE HORIZONTA L FLANGE OF THE TEE WHERE THE FLANGE WAS MILLED AWAY TO PASS UNDER THE FRAME. THE CRACK WAS ROUTED OUT OF THE HORIZON TAL FLANGE AND STOP DRILLED IN THE BASE FLANGE. TWO REPAIR ANGLES AND A STRAP WERE INSTALLED PER ER/A 364638-14, REV A. 2 L 7 3 4F A3WE 1998051501143 19980515 01143 WP 1998 5 15 DLL10980993 1 19980508 A 5730 1527139108 SKIN LKHEED 1011 10113851 5265010 WP WS 570 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1734D 193C1225 TWO FASTENER HOLES WERE FOUND CRACKED IN THE LOWER WING SKIN AT THE END OF THE SKIN SPLICE STRAP AT STRINGER 10, IWS 570 . THE CRACKS ARE THE SUBJECT OF SID AD 95-20-04, R1 (ITEM 57-3-4). THE CRACKS WERE REMOVED BY OVERSIZING THE HOLES WI TH AN INSURANCE CUT. THE HOLES WERE BUSHED AND ORIGINAL TYPE FASTENERS INSTALLED PER ER/A 364728-14AD, REV A. 2 L 7 3 4F A23WE 1998051501144 19980515 01144 NM 1998 5 15 DL72S980994 1 19980421 A 5414 SKIN BOEING 727 727232 1384082 NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 C/W ERA 300554-14 CODE 4-54-31 PERM REPAIR, NACELLES/THINNER SKIN, NR 2 ENG FS 1151.68. TIME LIMITED. REMOVED DAMAGED SKIN, FABD REPAIR PER SRM 54-10-3 FIG 13. DYE CKD AND FOUND TO BE REMOVED PER PS 900-6-3 NR 1 REF N/R 398. 2 L 7 3 4F A3WE 1998051501145 19980515 01145 NM 1998 5 15 DL72W980996 1 19980511 A 5240 FRAME BOEING 727 7272Q8 138407W NM SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831L 21826 A .5 INCH CRACK IN DOUBLER RT FWD SVC DOOR AFT FRAME UPPER CORNER. REPAIR PER M/M 52-12-0 FIG 805. 2 L 7 3 4F A3WE 1998051501146 19980515 01146 NM 1998 5 15 DL72E980997 1 19980511 A 3350 BATTERY PACK 900542 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 283WA 5394 21485 ON L/O CK, FOUND O/W EXIT SIGNS OVER LT EXITS INOP W/EMERG LIGHT TEST. REPLACED RACK AND BATTERY PACK M 1090 PER M/M, O PN CKS OK. 2 L 7 3 4F A3WE 1998051501147 19980515 01147 NM 1998 5 15 DL72E980998 1 19980511 A 3350 BATTERY PACK 10617842 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 283WA 9663 21485 ON L/O CK, FOUND EXIT SIGNS AT CEILING BULLNOSE L1023A AND L1022A INOP W/EMER LIGHT TEST. REPLACED RACK AND BATTERY PAC K PER M/M, OPN CKS OK. 2 L 7 3 4F A3WE 1998051501148 19980515 01148 NM 1998 5 15 DL73E980999 1 19980506 A 5330 SKIN BOEING 737 737247 138448D NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 244WA 23518 THE UPPER OUTBD CORNER OF THE COCKPIT L1 WINDOW SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK. WHILE STOP DRILLING THE C RACK PER SRM, THE DRILL HOLE WAS MISTAKENLY DRILLED THROUGH THE WINDOW POST. THE DRILL HOLE WAS ROUTED OUT OF THE POST AND POST STRAP. AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE SKIN AND WINDOW POST. THE REPAIR WAS ACCOMPLISHED PER ER/A 364718-14. 2 L 7 2 4F A16WE 1998051501149 19980515 01149 NM 1998 5 15 DL73K981000 1 19980506 A 5330 SKIN BOEING 737 737232 1384475 NM BS 920 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 THE FUSELAGE SKIN WAS PUNCTURED DUE TO GROUND EQUIPMENT IMPACT AT FS 920 AND STRINGERS 21L-22L. ALSO, STRINGER 22L WAS DAMAGED. THE SKIN WAS REPAIRED WITH AN EXTERNAL ALUM DOUBLER PER SRM 53-30-3 WITH MINOR FASTENER CHANGES AND THE STRING ER WAS REPAIRED PER SRM 53-10-3 WITH MINOR FASTENER CHANGES. THE REPAIRS WERE DOCUMENTED PER ER/A 364707-14. 2 L 7 2 4F RT A16WE 1998051501150 19980515 01150 NM 1998 5 15 DL72L981001 1 19980506 A 5330 65545703 SKIN BOEING 727 727232 1384082 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 A .5 INCH LONG CRACK WAS FOUND IN THE UPPER FWD CORNER OF THE R1 DOOR SKIN CUTOUT. THE CRACK WAS ROUTED OUT AND AN EXTE RNAL ALUMINUM DOULBER INSTALLED PER ER/A 364704-14, REV A. 2 L 7 3 4F A3WE 1998051501151 19980515 01151 NM 1998 5 15 DL733981004 1 19980512 A 5330 6545772188 SKIN BOEING 737 737347 1384647 NM FUSELAGE WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 FUSELAGE SKIN AT THE BLADE SEAL FUSELAGE INTERFACE WAS FOUND TO HAVE AN EXISTING REPAIR (REF 5-72770-3). WEAR WAS FOUND FWD OF THE REPAIR. REPAIRED PER ERA 331664-14. 2 L 7 2 4F RT A16WE 1998051501152 19980515 01152 NM 1998 5 15 DL733981005 1 19980512 A 5312 6546568187 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 1016 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 AFT PRESSURE BLKHD AT FS 1016 WAS FOUND CORRODED AND CRACKED AT BL 0. REPAIRED PER ERA 331673-14. 2 L 7 2 4F RT A16WE 1998051501153 19980515 01153 NM 1998 5 15 DL733981006 1 19980512 A 5312 65163007 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302WA 23182 FOUR CRACKS FOUND IN THE BLKHD WEB AT FS 178. THE CRACKS ARE LOCATED AT WL 200 AND WL 188, BETWEEN LBL 5.7 AND RBL 5.7. REPAIRED PER ERA 331672-14. 2 L 7 2 4F RT A16WE 1998051501154 19980515 01154 NM 1998 5 15 DL72S981007 1 19980506 A 5312 BULKHEAD BOEING 727 727232 1384082 NM BS 277 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 THE RT SIDE WALL OF THE NOSE LANDING GEAR WHEEL WELL WAS FOUND WITH A .75 VERTICAL CRACK AT FS 277. THE CRACK IS TYPICA L OF BAC S/B 727-53-0145. THE CRACK WAS CUTOUT AND A DOUBLER INSTALLED PER SRM 51-40-2. A PORTION OF THE S/B MODIFICA TION WAS ALSO INSTALLED AT THE DAMAGE LOCATION. THE REPAIR WAS DOCUMENTED PER ER/A 364683-14AD. 2 L 7 3 4F A3WE 1998051501155 19980515 01155 NM 1998 5 15 DLM88981008 1 19980512 A 5330 5953050 SKIN DOUG MD88 MD88 3023688 NM BS 235 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 991DL 53343 FUSELAGE SKIN AFT OF THE L1 DOOR WAS FOUND WITH SEVERAL DENTS FROM STA 230 TO 240 AND BETWEEN L18-20 L. REPAIRED PER ER A 331699-14. 2 L 7 2 4F RT A6WE 1998051501156 19980515 01156 NM 1998 5 15 DLM88981009 1 19980512 A 5330 5924802 SKIN DOUG MD88 MD88 3023688 NM BS 240 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 991DL 53343 SEVERAL DENTS WERE FOUND IN THE FUSE SKIN FROM FS 232 TO 251, NEAR L18L. REPAIRED PER ERA 331712-14. 2 L 7 2 4F RT A6WE 1998051501157 19980515 01157 NM 1998 5 15 DLM88981010 1 19980512 A 5330 5911401 SKIN DOUG MD88 MD88 3023688 NM BS 226 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 991DL 53343 SEVERAL DENTS FOUND IN FUSE SKIN AT APPROX FS 224 TO 227 NEAR L18L. REPAIRED PER ERA 331715-14. 2 L 7 2 4F RT A6WE 1998051501158 19980515 01158 NM 1998 5 15 DL72W981011 1 19980512 A 5311 FRAME BOEING 727 727247 138408F NM BS 784 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 FS 784 LT OVERWING EXIT FRAME WAS FOUND CRACKED IN THE OUTBD CHORD AT THE LWR EDGE. REPAIRED PER ERA 331643-14AD. 2 L 7 3 4F A3WE 1998051501159 19980515 01159 NM 1998 5 15 DL72W981012 1 19980512 A 5320 65585211 BRACE BOEING 727 727247 138408F NM BS 351 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 DRAG BRACE SUPPORT ANGLE WAS FOUND DAMAGED AT APPROX BL 0. REPAIRED PER ERA 331714-14. 2 L 7 3 4F A3WE 1998051501160 19980515 01160 NM 1998 5 15 DL76S981014 1 19980511 A 5330 SKIN BOEING 767 767332 1382001 NM BS 436 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 133DN 24982 THE FUSELAGE SKIN AT FS 436, STRG 33R TO 34R, WAS DENTED BY GROUND EQUIPMENT. THE AFT EDGE OF THE UNDERLYING SKIN SPLIC E STRAP WAS CRACKED AT A FASTENER LOCATION. THE DENTED SKIN AND CRACKED AREA OF THE STRAP WERE TRIMMED OUT AND AN EXTER NAL ALUMINUM REPAIR DOUBLER WAS INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 364759-14, REV A. 2 L 7 2 4F RT A1NM 1998051501161 19980515 01161 NM 1998 5 15 DL72W981015 1 19980415 A 5400 S-DUCT BOEING 727 727247 138408F NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 NR 2 ENG INLET DUCT INTERNAL TWO CRACKS AT 3 O'CLOCK AND 11 O'CLOCK AT STA 1151 DOGHOUSE SIDE. REMOVED DAMAGE PER SRM 5 4-10-3 FIG 13. FABRICATED DOUBLER AND FILLER PER SRM 54-10-3 FIG 13. DYE CHECKED AREA PER PS 900-6-3 NR 1. NO CRACKS FOUND. OK TO INSTALL REPAIR 3 O'CLOCK ONLY. INSTALLED REPAIR AT 3 O'CLOCK POSITION PER SRM 54-10-3, 3 O'CLOCK REPAIR O K. CUT OUT DAMGE AT 11 AND 1 O'CLOCK. 2 L 7 3 4F A3WE 1998051501162 19980515 01162 NM 1998 5 15 DL72W981016 1 19980415 A 5400 S-DUCT BOEING 727 727247 138408F NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 NR 2 ENG INLET DUCT INTERNAL UPPER S-DUCT CRACKED AT 9 O'CLOCK AT STA 1151. BLENDED AREA AND DYE CHECKED AND TREATED AN D PAINTED AREA, NO MORE CRACKS WERE FOUND. ALL WORK PERFORMED PER ERA 331669-14 OK PER PRI 331669-14.C/W ERA 33169-14. 2 L 7 3 4F A3WE 1998052200013 19980522 00013 EU 1998 5 22 98ZZZX1835 1 19980207 A 7714 430106202 PICKUP BOLKMS 117 BK117B1 5626012 EU NR 2 ENG N1 MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 80 96A0122 7230 SPEED PICKUP UNIT CAUSES N1 GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998052200014 19980522 00014 EU 1998 5 22 98ZZZX1836 1 19980207 A 7714 430106202 PICKUP BOLKMS 117 BK117B1 5626012 EU NR 2 ENG N1 MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 80 960A0122 7230 SPEED PICKUP UNIT CAUSES N1 GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998052200015 19980522 00015 EU 1998 5 22 98ZZZX1837 1 19980102 A 7712 105957411 INDICATOR BOLKMS 105 BO105LSA3 5626020 EU DUAL TORQUE STICKS A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 13 154 2014 DUAL TORQUE INDICATOR NEEDLES STICK. REPLACES WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998052200019 19980522 00019 EU 1998 5 22 98ZZZX1841 1 19980115 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R LAMINATED WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 354 2728 LAMINATED T/R BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036- 01, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998052200022 19980522 00022 EU 1998 5 22 98ZZZX1844 1 19980313 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R LAMINATED WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 473 2818 LAMINATED T/R BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS FROM KIT 355A09-1036- 01, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998052200023 19980522 00023 EU 1998 5 22 98ZZZX1845 1 19980319 A 6410 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R GREEN WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 318 2818 GREEN LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 350A33-2153- 00, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998052200024 19980522 00024 EU 1998 5 22 98ZZZX1846 1 19980427 A 6520 350A33215300 HINGE SNIAS 350 AS350B 8680801 EU T/R LAMINATED DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 LAMINATED HINGE DEFECTIVE, RECALLED PER SL 1337-65-97, BATCH 95L. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998052200025 19980522 00025 EU 1998 5 22 98ZZZX1847 1 19980427 A 6520 4639311002 BEVEL GEAR BOLKMS 117 BK117A1 5626010 EU T/R GEARBOX DEFECTIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 787 CANNOT GET GEAR PATTERN TO MOVE OFF TOE. TRIED IN TWO DIFFERENT GEARBOXES WITHOUT SUCCESS. REPLACED WITH NEW UNIT, COR RECTED PROBLEM. 1 G 7 2 3U H13EU 1998052200035 19980522 00035 CE 1998 5 22 98ZZZX1857 1 19980504 A 8110 8797 GEAR BEECH 18 G18S 1151010 CE PWA R985 R985AN14B 52008 NE CHARGER DRIVE FAILED A KVJA K NONE O OTHER IN INSP/MAINT 1 SW 05 621KE 96 2051 BA556 14832 SUPERCHARER DRIVE GEAR FAILED. CAUSE UNKNOWN. 1 L 7 2 3R 3 R A765 5E1 1998052200049 19980522 00049 EA 1998 5 22 98ZZZX1871 2 19980426 A 7310 3040637 FUEL LINE BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA LT ENGINE CHAFED A A YADA K NONE K FLUID LOSS NR NOT REPORTED 1 AL 01 45GL UC45 ON NR 1 ENGINE - STARTER/GENERATOR COOLING DUCT HOSE CAME IN CONTACT WITH AN ENGINE FUEL LINE AND CHAFED A HOLE THROUGH THE TUBING WALL THICKNESS CAUSING FUEL TO LEAK INTO THE ACCESSORY SECTION OF THE ENGINE COMPARTMENT. P&WC SB 13250 ADDR ESSES THIS PROBLEM AND HAD NOT BEEN C/W. BEECH HAS NO S/B THAT ADDRESSES THIS PROBLEM ON THE B1900C MODEL. BEECH COMMU NIQUE NR 34 STATES THE P&WC SB CORRECTS THIS PROBLEM. 2 L 7 2 4T 4 T RT A24CE E4EA 1998052200052 19980522 00052 NE 1998 5 22 98ZZZX1874 2 19980427 A 7200 ENGINE LEAR 25 25B 5170511 CE GE CJ610 CJ6106 30006 NE LT ENGINE FAILED A KKFA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 GL 23 83CK 5895 3860 183 249069A LEFT ENGINE EGT INCREASED. ENGINE SHOOK, ENGINE SHUT DOWN FOR PRECAUTIONARY MEASURE. UNEVENTFUL RETURN TO AIRPORT ACCO MPLISHED. LEFT ENGINE REMOVED FOR TURBINE FOD. INSTALLED SERVICEABLE ENGINE SN 251-290A. GROUND PERFORMANCE RUN, LEAK CHECKED, AND RETURNED TO SERVICE. 2 L 7 2 4J 4 J A10CE 1E16 1998052200055 19980522 00055 NM 1998 5 22 K3HA980071 1 19980512 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 EMERGENCY FLOOR TRACK LIGHTING BROKEN AT ROW NR 2 (LEFT). REMOVED AND REPLACED BROKEN SECTION OF TRACK PER MM 33-50-00. OPS CHECK OK. 2 L 7 3 4F A3WE 1998052200056 19980522 00056 WP 1998 5 22 IXXA9800048 1 19980311 A 5312 BULKHEAD CAP DOUG DC8 DC862 3021970 WP BS 1606 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 31CX 68112 2977 45911 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE AFT PRESSURE BULKHEAD UPPER CAP AT FUSELAGE STATION 1606. REPAIR WAS ACCOMPLISHED BY STOP DRILLING OF CRACK, FABRICATION AND INSTALLATION OF A REPAIR ANGLE DOUBLER AND TRIPLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING E22-R04 AND ENGINEERING ORDER 53-DC8-836. 2 L 7 4 4F 4A25 1998052200057 19980522 00057 WP 1998 5 22 IXXA9800049 1 19980228 A 5320 56410072 FITTING DOUG DC8 DC862 3021970 WP BS 781.5 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 31CX 68112 2977 45911 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON FUSELAGE FRAME FITTING AT FUSELAGE STATION 781.5 RIGHT INBOAR D AREA. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A MILLED ANGLE PLATE IN ACCORDA NCE WITH DOUGLAS FAX MESSAGE ACTION NR 365160/365206, FILE NR98-04-03-012, ROD SKETCH NR 98-03-18-016 AND ENGINEERING OR DER 53-DC8-837. 2 L 7 4 4F 4A25 1998052200058 19980522 00058 WP 1998 5 22 IXXA9800050 1 19980225 A 5330 PLATING DOUG DC8 DC862 3021970 WP BS 1268 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 31CX 68112 45911 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING AT STATION 1268 BETWEEN LONGERON S 35 AND 36 LEFT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN INTERNAL REPAIR FI LLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING E22-R02 AND ENGINEERING ODER 53-DC8-833. 2 L 7 4 4F 4A25 1998052200059 19980522 00059 WP 1998 5 22 IXXA9800051 1 19980224 A 5730 PLATING DOUG DC8 DC862 3021970 WP WS 736-761 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 31CX 68112 2977 45911 DURING ROUTINE C CHECK INSPECTION, TWO CRACKS WERE DETECTED ON RIGHT WING LOWER LEADING EDGE EXTERNAL PLATING BETWEEN ST ATION 736.5 AND 761.695. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREAS, FABRICATION AND INSTALLATION REPAIR FILLE RS AND EXTERNAL REPAIR DOUBLER IN ACCORDANCE WHIT FAA DER APPROVED DRAWING E33-R03 AND ENGINEERING ORDER 57-DC8-834. 2 L 7 4 4F 4A25 1998052200060 19980522 00060 WP 1998 5 22 IXXA9800052 1 19980225 A 5730 PLATING DOUG DC8 DC862 3021970 WP WS 120 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 31CX 68112 2977 45911 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON LEFT WING UPPER EXTERNAL PLATING ADJACENT TO THE REAR SPAR AT STATION XW120. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGE AREA, FABRICATION AND INSTALLATION A REPAIR FILLER AND AN EXTE RNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING E22-R01 AND ENGINEERING ORDER 57-DC8-827. 2 L 7 4 4F 4A25 1998052200061 19980522 00061 WP 1998 5 22 IXXA9800053 1 19980224 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 960 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 31CX 68112 2977 45911 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON FLOOR CUSP VERTICAL SUPPORT FITTING AT FUSELAGE STATION 960 LONGERON 21 LEFT. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF AN REPAIR FITTING AND A REPAIR DOUBLER IN ACCORDANCE WITH DOUGLAS STRUCTURAL REPAIR MANUAL 53-20-0, 51-1-8 AND ENGINEERING ORDER 53-DC8-98. 2 L 7 4 4F 4A25 1998052200062 19980522 00062 WP 1998 5 22 IXXA9800056 1 19980501 A 3297 WIRE DOUG DC8 DC871F 302199D WP LT MLG CHAFED A IXXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 826BX 78826 2350 45998 EN ROUTE TOL TO DFW, DURING GEAR EXTENTION FOR LANDING THE LEFT MAIN LANDING GEAR INDICATOR LIGHT DID NOT ILLUMINATE IN THE DOWN POSITION. THE CREW CYCLED THE GEAR THREE TIMES PRIOR TO RECEIVING A DOWN AND LOCKED INDICATION. MAINTENANCE I NSPECTED THE LEFT GEAR INDICATION SYSTEM AND FOUND A CHAFED WIRE AT THE DOWNLOCK SWITCH. THE WIRING WAS REPAIRED, SYSTE M CHECKED GOOD IN ACCORDANCE WITH MAINTENANCE MANUAL 32-60-06, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F RT 4A25 1998052200063 19980522 00063 NM 1998 5 22 CALA9800852 1 19980513 A 3350 1356B37 BATTERY PACK BOEING 747 747238B 1384828 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14024 20534 OVERHEAD CEILING LIGHT FOR EMERGENCY LIGHTING AT SEAT ROW 23 ABC CAUSING INTERMITTENT ILLUMINATION IN ZONE C. REMOVED A ND REPLACED BATTERY PACK UNIT AT ROW 23 ABC PER MM 33-51-01 AND 33-51-07. 2 L 7 4 4F A20WE 1998052200064 19980522 00064 1998 5 22 CALA9800853 4 19980513 A 2565 D30656126 SLIDE BOEING 757 757224 1384958 NM R 4 DOOR LOW PRESSURE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17122 3199 27564 DOOR R 4 SLIDE PACK PRESSURE LOW OUT OF GREEN BAND. REMOVED AND REPLACED SLIDE PACK PER MM 25-66-01. 2 L 7 2 4F RT A2NM 1998052200065 19980522 00065 NM 1998 5 22 CALA9800854 1 19980513 A 3397 07912 WIRE BOEING 737 737217 1384464 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12230 19884 ESCAPE PATH LIGHT INOP AT ROW 24. BROKEN WIRE AND MISSING LENS. REPAIRED LIGHT SOCKET WIRE AND REPLACED LENS SET PER M M 33-51-5. 2 L 7 2 4F A16WE 1998052200066 19980522 00066 NM 1998 5 22 CALA9800855 1 19980514 A 5320 6547951503 THRESHOLD BOEING 737 737291 138448W NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 AFT PIT THRESHOLD AFT CORNER CRACKED (3.5). REMOVED AFT PIT THRESHOLD CORNER AND INSTALLED A NEW CORNER PER SRM 51-30-2 . 2 L 7 2 4F A16WE 1998052200067 19980522 00067 NM 1998 5 22 CALA9800856 1 19980514 A 3350 MISC062 BATTERY BOEING 727 727243 138408D NM CABIN DISCHARGED A CALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 17410 21663 EMERGENCY EXIT LIGHT OVER COCKPIT DOOR INOP. REPLACED BATTERY PACK. 2 L 7 3 4F RT A3WE 1998052200068 19980522 00068 WP 1998 5 22 CALA9800857 1 19980513 A 5320 INTECOSTAL DOUG DC9 DC932 3022066 WP BS 160-170 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 47798 FWD SERVICE DOOR JAMB INTERIOR STRUCTURE BETWEEN STA 160 - 170 AND BETWEEN LONGERONS 12 R AND 13 R IS CRACKED (2). ROUT ED OUT CRACKED AREA. FABRICATED, PRIMED AND INSTALLED NEW ANGLE PER SRM 51-10-3 AND 51-30-5. 2 L 7 2 4F A6WE 1998052200069 19980522 00069 WP 1998 5 22 CALA9800858 1 19980513 A 5320 2777976 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 47798 RIGHT FLOOR CUSP ANGLE CORRODED. REMOVED DAMAGED ANGLE OF CUSP. FABRICATED, PRIMED, AND INSTALLED REPLACEMENT ANGLE PE R SRM 53-05, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998052200070 19980522 00070 WP 1998 5 22 CALA9800859 1 19980513 A 3350 08163000624 LIGHT DOUG DC9 DC932 3022066 WP CABIN LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17557 47424 ESCAPE PATH LIGHTING AT REAR OF CABIN BETWEEN LAVS IS COMING UP AND WILL NOT SNAP BACK IN PLACE. REINSTALLED AISLE PATH LIGHTING NEAR LAVATORY. 2 L 7 2 4F A6WE 1998052200071 19980522 00071 WP 1998 5 22 CALA9800860 1 19980513 A 5320 991158221R BEAM DOUG DC9 DC982 3022082 WP NR 4 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 F/S/D NR 4 BEAM IS CRACKED (1) AT FWD END. REMOVED AND REPLACED BEAM PER 51-30-2. 2 L 7 2 4F A6WE 1998052200072 19980522 00072 WP 1998 5 22 CALA9800861 1 19980514 A 5330 7268418 SKIN DOUG DC9 DC982 3022082 WP BS 237 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 TEMP AIRPHONE REPAIR AT STA 237 BETWEEN L30 AND L29. INSTALLED DOUBLER PER SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1998052200073 19980522 00073 WP 1998 5 22 CALA9800862 1 19980514 A 5330 6165438 SKIN DOUG DC9 DC982 3022082 WP BS 383 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 TEMP AIRPHONE REPAIR AT STA 383 BETWEEN L 30 AND L 29. INSTALLED DOUBLER PER SRM 53-04 FIG 38. 2 L 7 2 4F A6WE 1998052200074 19980522 00074 WP 1998 5 22 9809049305 2 19980508 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LEFT FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 307RC 48086 708449 DURING CLIMB AT 19,000 FEET, THE LEFT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED WITH ASSOCIATED VIBRATION. CREW SHUT D OWN THE LEFT ENGINE, RETURNED TO ONT, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE. OPERA TIONAL CHECK OK. RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E9NE 1998052200075 19980522 00075 EU 1998 5 22 9809053219 1 19980511 A 2913 4205602 PUMP AIRBUS 320 A320211 3930320 EU LT HYD SYST LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 319US 3951 2100 208 DURING CRUISE, RECEIVED HYD B RSVR LOW LEVEL MESSAGE. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING BLUE ELECTRIC HYDRAULIC PUMP. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998052200076 19980522 00076 NM 1998 5 22 9809066635 1 19980507 A 7603 36633061 CONTROL CABLE BOEING 747 747227B 1384888 NM PWA JT9 JT9D7Q 52054 NE NR 3 ENGINE FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 01 635US 15564 13083 21682 702179 UPON APPLICATION OF TAKEOFF POWER, THE CREW NOTICED NO RESPONSE FROM THE NR 3 ENGINE WITH POWER LEVER MOVEMENT. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE STRUT AREA PUSH/PULL CABLE AND CONTROL BOX . ENGINE RUN WAS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1998052200078 19980522 00078 1998 5 22 9809089610 4 19980512 A 3418 9650041029 COMPUTER DOUG DC9 DC932 3022066 WP E/E COMPARTMENT INOPERATIVE A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 610NW 19361 8875 47432 EN ROUTE TO IAD, ALL STALL WARNING INDICATIONS SOUNDED OFF. FLIGHT CREW FOLLOWED COM PROCEDURES, CONTACTED DISPATCH CON TROL, DIVERTED FLIGHT TO DTW, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE STALL WARNING COMPUTER. OPRATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052200079 19980522 00079 WP 1998 5 22 9809099611 1 19980512 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 611NA 47435 DURING LINE CHECK, FOUND CATWALK EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED TAIL COMPARTMENT EMER GENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052200080 19980522 00080 WP 1998 5 22 9809109914 1 19980512 A 3350 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 964N 47416 DURING LINE CHECK, FOUND COCKPIT, MAIN ENTRY, AND GALLEY DOOR OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLAC ED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052200081 19980522 00081 WP 1998 5 22 9809119856 1 19980512 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 765NC 47718 DURING LINE CHECK, FOUND CABIN CEILING EMERGENCY EXIT LIGHTS INOPERATIVE AT SEAT ROWS 16 THROUGH 20. MAINTENANCE REPLAC ED BATTERIES IN POWER SUPPLY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998052200082 19980522 00082 NM 1998 5 22 SWAA980774 1 19980504 A 5320 ANGLE BOEING 737 7372K6 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D CHECK, FOUND CORRODED Z ANGLE ST DOOR WAY AT BS 294 TO 328. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052200083 19980522 00083 NM 1998 5 22 SWAA980775 1 19980504 A 5330 SKIN BOEING 737 7372K6 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED 1/4 D CHECK, FOUND FWD SERVICE DOOR CUTOUT CRACKED AT LOWER FWD CORNER. REPAIRED PER BOEING DRAWING 6 5C27287. 2 L 7 2 4F RT A16WE 1998052200084 19980522 00084 NM 1998 5 22 SWAA980776 1 19980504 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING WALKAROUND CHECK, FOUND APPROX 4 SKIN CRACK RT SIDE OF FUSELAGE ABOVE NR 9 CABIN WINDOW. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998052200085 19980522 00085 NM 1998 5 22 SWAA980777 1 19980505 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 500A-500D, RBL 24. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200086 19980522 00086 NM 1998 5 22 SWAA980778 1 19980505 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED SKATE ANGLE AT BS 540, STR 22. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200087 19980522 00087 NM 1998 5 22 SWAA980779 1 19980505 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 784/417/376 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 784, 5 BELOW STR 23R; BS 417, BETWEEN STR 20R AND 21R; AND BS 376 , 3 ABOVE STR 21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200088 19980522 00088 NM 1998 5 22 SWAA980780 1 19980505 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 380-520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED INTERCOSTAL AT NUT PLATE HOLE BS 380-400; AND BS 500-520. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998052200089 19980522 00089 NM 1998 5 22 SWAA980781 1 19980505 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED FLOORBEAM BELOW TIE DOWN FITTING AT BS 787, RBL 14. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998052200090 19980522 00090 NM 1998 5 22 SWAA980782 1 19980505 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 277-360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED Z ANGLE AT BS 277 TO 360. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200091 19980522 00091 NM 1998 5 22 SWAA980783 1 19980505 A 5320 ANGLE BOEING 737 7373H4 1384600 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED L ANGLE SUPPORT THAT ATTACHES TO Z ANGLE FOR THRESHOLD. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998052200092 19980522 00092 NM 1998 5 22 SWAA980784 1 19980505 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED LT TRANSITION ANGLE FROM BS 727 TO 787, LBL 20. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998052200093 19980522 00093 NM 1998 5 22 SWAA980785 1 19980506 A 5532 65C25824 SKIN BOEING 737 7373A4 1384585 NM VERT STAB BIRD STRIKE A SWAA K NONE C F.O.D. IN INSP/MAINT 1 SW 07 673SW 23251 BIRDSTRIKE INBOUND TO SMF. BIRDSTRIKE INSPECTION PERFORMED, FOUND DAMAGE TO VERTICAL STABILIZER L/E AT BS 1006, STA 57, RT WING LEADING EDGE AND PAX WINDOWS BADLY SCRATCHED. INSTALLED INTERIM REPAIRS FOR AERODYNAMIC SMOTHNESS. A/C FERRY TO TRAMCO FOR PERMANENT REPAIRS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052200094 19980522 00094 NM 1998 5 22 SWAA980786 1 19980505 A 2120 AIR DISTRIBUTION BOEING 737 7375H4 138449D NM COCKPIT ODOR A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 503SW 24180 EN ROUTE, COCKPIT CREW DETECTED SMELL OF ELECTRICAL SMOKE ODOR, LASTED SEVERAL MINUTES, THEN DISSIPATED. RESET APU CONT ROL CB APU OPS CK GOOD PER BOEING MM. RAN APU AT FULL LOAD AND INSPECTED APU CONTROL CIRCUIT WIRING IN COCKPIT NO ELECT RICAL SMOKE ODOR PRESENT. 2 L 7 2 4F RT A16WE 1998052200095 19980522 00095 NM 1998 5 22 SWAA980787 1 19980505 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 398SW 27689 DURING SERVICE CHECK, FOUND FWD LT FLASHLIGHT LED NOT BLINKING. REMOVED AND REPLACED FLASHLIGHT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052200096 19980522 00096 NM 1998 5 22 SWAA980788 1 19980505 A 5241 SKIN BOEING 737 7373H4 1384600 NM GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23338 DURING SERVICE CHECK, FOUND FWD GALLEY DOOR HINGE CUTOUT LWR CRACKED IN LWR RADIUS. REPAIRED PER ACO 3189-52. 2 L 7 2 4F RT A16WE 1998052200097 19980522 00097 NM 1998 5 22 SWAA980789 1 19980505 A 5330 SKIN BOEING 737 7372H4 138448C NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 81SW 22730 DURING SCHEDULED 1/4 D CHECK, FOUND AFT GALLEY DOOR SKIN CRACK AT LOWER HINGE CUTOUT LOWER CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998052200098 19980522 00098 NM 1998 5 22 SWAA980790 1 19980505 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND SCREW HOLE ON FLOORBEAM AT BS 986 CORRODED. REPAIRED PER SWA T1-A53-014. 2 L 7 2 4F RT A16WE 1998052200099 19980522 00099 NM 1998 5 22 SWAA980791 1 19980505 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 502SW 24179 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT ROW TRACK LIGHTING LOOSE. SECURED FLOOR TRACK LIGHTING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052200100 19980522 00100 NM 1998 5 22 SWAA980792 1 19980505 A 7930 BYPASS LIGHT BOEING 737 7372H4 138448C NM NR 2 ENGINE ILLUMINATED A SWAA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 050SW 21447 DURING DESCENT TO STL, FOUND NR 2 OIL FILTER BYPASS LT ILLUMINATED, NR 2 ENG SHUTDOWN IN ACCORDANCE WITH QRH, ALL OTHER ENGINE INDICATIONS HAD BEEN NORMAL. MADE AN UNEVENTFUL LANDING. PULLED AND CHECKED MAIN OIL SCREEN, FOUND CLEAN. RESE ATED BYPASS SWITCH, RELAMPED INDICATOR. RAN ENGINE, NO LEAKS NOTED. ALL INDICATIONS NORMAL PER BOEING MM. BYPASS LIGH T NORMAL. 2 L 7 2 4F A16WE 1998052200101 19980522 00101 NM 1998 5 22 SWAA980793 1 19980506 A 5312 BULKHEAD WEB BOEING 737 7372H4 138448C NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND ULTRA SONIC INSP REVEALS 100 PERCENT CRACK INDICATION RBL 5.4, WL 199 UNDER STRAP. R EPAIRED CRACKED WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1998052200102 19980522 00102 NM 1998 5 22 SWAA980794 1 19980506 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY LIGHT AT BETWEEN AISLE'S 2-3 FLASHING WHEN TURN ON. REMOVED AND REPLACED BAT TERY PACK PER BOEING MM, AND OPS CHECK GOOD. 2 L 7 2 4F A16WE 1998052200103 19980522 00103 NM 1998 5 22 SWAA980795 1 19980506 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C1 CHECK, FOUND CRACKED LT FUSELAGE SKIN 1/5 L AT BS 520 STR 16L. NEAR UPPER EDGE OF WING TO BODY FAIR ING. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998052200104 19980522 00104 NM 1998 5 22 SWAA980796 1 19980506 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 767-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 767 - 787, RBL 20. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200105 19980522 00105 NM 1998 5 22 SWAA980797 1 19980506 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 793-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED THRESHOLD WEB AT BS 793 - 847, RBL 25. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998052200106 19980522 00106 NM 1998 5 22 SWAA980798 1 19980506 A 5320 WEB BOEING 737 7373H4 1384600 NM CARGO BIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND DAMAGED WEB AT AFT SIDE OF AFT CARGO DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200107 19980522 00107 NM 1998 5 22 SWAA980799 1 19980506 A 2750 FLAP BOEING 737 7373H4 1384600 NM LT WING DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND OUTBD T/E FLAP DENTED 1.5 BY 1 WIDE WITH UPPER SURFACE BULGED; INBD OF NR 1 CANOE. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200108 19980522 00108 NM 1998 5 22 SWAA980800 1 19980506 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOOR ANGLE AT BS 500 D, RBL 24, LBL 24. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998052200109 19980522 00109 NM 1998 5 22 SWAA980801 1 19980507 A 5320 WEB BOEING 737 7373H4 1384600 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND DAMAGED WEB AT FWD SIDE OF AFT CARGO DOOR CUT OUT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200110 19980522 00110 NM 1998 5 22 SWAA980802 1 19980507 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED SUPPORT ANGLE FOR FWD BULKHEAD PANEL AT 727 + 2, RBL 4. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200111 19980522 00111 NM 1998 5 22 SWAA980803 1 19980507 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 492-500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 492-500A, RBL 24. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998052200112 19980522 00112 NM 1998 5 22 SWAA980804 1 19980507 A 5320 WEB BOEING 737 7373Q8 1384670 NM BS 950 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED C3 CHECK, FOUND WEB DAMAGE JUST FWD OF AFT SERVICE DOOR FRAME AT BS 950. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052200113 19980522 00113 NM 1998 5 22 SWAA980805 1 19980511 A 3260 SENSOR BOEING 737 7373Q8 1384670 NM LT MLG MALFUNCTIONED A SWAA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 695SW 23506 FLIGHT ROUTED FROM TPA TO ABQ DIVERTED TO DAL WITH THE LEFT GEAR RED LIGHT ILLUM IN FLIGHT, BUT WENT OUT WHEN THE GEAR WAS LOWERED FOR LANDING. MADE AN UNEVENFUL LANDING. REMOVED AND REPLACED THE GEAR POSITION SENSOR AND C/W RETRACT CHEC K WITH NO DISCREPANCY NOTED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052200114 19980522 00114 NE 1998 5 22 SWAA980806 2 19980511 A 7260 332A1000 GEAR BOX BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING T ENGINE CASE PENETRATION CL CLIMB 1 SW 07 322SW 23343 NR 2 ENGINE FAILED CLIIMBING THROUGH 31,000, AIRCRAFT RETURN TO DAL MADE AN UNEVENTFUL LANDING. INSPECTED AND FOUND ACC Y GEARBOX FAILURE WITH DAMAGE TO RT T/B COWLING AND R/T INBD LANDING LIGHT LENS COVER. REMOVED AND REPLACED NR 2 ENGINE AND R/T I/B LANDING LIGHT LENS PER BOEING MM. 2 L 7 2 4F 4 F RT A16WE E2GL 1998052200115 19980522 00115 NM 1998 5 22 SWAA980807 1 19980509 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357SW 26594 DURING WALKAROUND CHECK, FOUND EMERGENCY LIGHTS BETWEEN ROW 12-16 INOP. REPAIRED WIRING ON EGRESS LIGHTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052200117 19980522 00117 WP 1998 5 22 UPS98826593 1 19980413 A 5220 ANGLE DOUG DC8 DC871F 302199D WP EMER EXIT DOOR CRAKCED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK RIGHT HAND FWD EMERGENCY EXIT DOOR INNER SUPPORT ANGLE CRACKED. FABRICATED NEW ANGLE IAW DC8 SRM 5 2 7 1 HEAT TREATED 0807075-0 TO 0 80 7075 T6 IAW DC8 TPS 1003 REV A. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 INSTALLED IAW DC8 SRM 51 3 0. 2 L 7 4 4F RT 4A25 1998052200118 19980522 00118 WP 1998 5 22 UPS98826594 1 19980414 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 46 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK FLOOR SUPPORT ANGLE AT FS 46 IS CRACKED IN AREA BETWEEN LBL 50 TO LBL 62. FABRICATED FLOOR SUPPORT ANGLE AND ANGLE REPAIR IAW DC8 SRM 53 7 1. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 2 0D. 2 L 7 4 4F RT 4A25 1998052200119 19980522 00119 WP 1998 5 22 UPS98826595 1 19980414 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 157.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK CRACKED SKIN AT RIGHT WING LEADING EDGE AUX FUEL TANK LOWER SURF XFS 157.5. FABRICATED NEW DOUBLE R AND FILLER IAW DC8 SRM 57 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED NEW DOUBLER AND FILLER IAW DC8 S RM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200120 19980522 00120 WP 1998 5 22 UPS98826596 1 19980415 A 5522 SKIN DOUG DC8 DC871F 302199D WP RT ELEV CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK RIGHT ELEVATOR LOWER SKIN IS CRACKED OUT AT TRAILING EDGE STA XH 282. FABRICATED NEW DOUBLER IAW D C8 SRM 55 21. ALODINED AND PRIMED AND INSTALLED DOUBLER IAW DC8 SRM 51 1 8 AND 51 1 21A. 2 L 7 4 4F RT 4A25 1998052200121 19980522 00121 WP 1998 5 22 UPS98826597 1 19980416 A 5320 STIFFINER DOUG DC8 DC871F 302199D WP BS 1723 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK INTERIOR AFT 6 FUSELAGE FLOOR STIFFENER HAS CORROSION ON UNDERSIDE AT STATION 1723 LONGERON 34 RIG HT. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53 2 0. FABRICATED WEB IAW DOUGLAS DRAWING 5755032 ALODINED AN D PRIMED IAW DC8 SRM 5 1 1 8. INSTALLED WEB IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200122 19980522 00122 WP 1998 5 22 UPS98826598 1 19980416 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP BS 980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK CORROSION ON UPPER PRESSURE PANEL U CHANNEL AT FS 980 LT W/W THE MOST O/B. FABBED NEW HAT CHANNEL S AND SPLICES IAW REPAIR ENGINEERING ORDER REO 04626. ALODINED AND PRIMED HAT CHANNELS AND SPLICES IAW DC8 SRM 51 1 8. INSTALLED HAT CHANNELS AND SPLICES IAW REO 04626 AND DC8 SRM 51 121. 2 L 7 4 4F RT 4A25 1998052200123 19980522 00123 WP 1998 5 22 UPS98826599 1 19980416 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP BS 980 CORRODED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK CORROSION ON UPPER PRESSURE PANEL U CHANNEL AT FUSELAGE 980 LT WW 2ND FROM MOST O/B CHANNEL. REPAI RED REO 04626 REF UPS CARD 542514. 2 L 7 4 4F RT 4A25 1998052200124 19980522 00124 WP 1998 5 22 UPS98826600 1 19980419 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 680 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK MAIN CABIN STA 680 AND RBL 50 FLOORBEAM GOUGED, CHAFFED AND CORRODED UNDERSIDE. FABRICATED REPAIR STRAP IAW REO 04670. ALODINED, PRIMED AND INSTALLED REPAIR STRAP IAW DC8 SRM 51 18 AND REO 04670. 2 L 7 4 4F RT 4A25 1998052200125 19980522 00125 WP 1998 5 22 UPS98826601 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK STA 680 LONGERON 2L AND BATHTUB FITTING CRACKED. REMOVED CRACKED FITTING STA 680 L-2 LOCATED AND D RILLED NEW FITTING IAW DC8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D AND 51 3 0 AND 51 1 23. 2 L 7 4 4F RT 4A25 1998052200126 19980522 00126 WP 1998 5 22 UPS98826602 1 19980417 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 55-72 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK STA 55 TO 72 SEAT TRACK 11 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 53 7 3 AND DC8 SR M 51 1 8. 2 L 7 4 4F RT 4A25 1998052200127 19980522 00127 NE 1998 5 22 UPS98826603 2 19980512 A 7314 6411194 FUEL PUMP DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 4 ENGINE MALFUNCTIONED A IPXA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SO 01 772UP 46072 DURING CRUISE AT 35.0 NR 4 ENGINE FLAMED OUT. PERFORMED ENGINE FLAMEOUT PROCEDURE AND ENGINE START CHECKLIST WITH A SUC CESSFUL ENGINE START. ALL FURTHER INDICATIONS AND PARAMETERS WERE NORMAL. PERFORMED 71-00 FAULT 51 PG 101-104 CFM56. R EPLACED ENGINE DRIVEN BOOST PUMP PER MM 73-10-01 PG 201-206. SYSTEM OPS CHECK AND LEAK CHECKS OK P/N OFF/ON 64-1119-4 S /N OFF FB74919 S/N ON FB69547. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998052200128 19980522 00128 EU 1998 5 22 QXEA9800647 1 19980511 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 GEG - 28 VOLT LIGHTS INOPERATIVE AT BOTH FORWARD EMERGENCY EXIT SIGNS. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052200129 19980522 00129 EU 1998 5 22 QXEA9800648 1 19980511 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 GEG - AFT OVERHEAD 28V LIGHT INOPERATIVE. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052200130 19980522 00130 EU 1998 5 22 QXEA9800649 1 19980511 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 GEG - 28V EMERGENCY LIGHT ABOVE MAIN CABIN DOOR INOPERATIVE. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052200131 19980522 00131 EU 1998 5 22 QXEA9800650 1 19980511 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 BOI - EMERGENCY OVERHEAD LIGHT OUT AT ROW 13 AND ROW 9. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052200132 19980522 00132 EU 1998 5 22 QXEA9800651 1 19980511 A 3350 5515900004 CIRCUIT PANNEL GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 GEG - FORWARD FACING EXIT SIGN HAS BULBS BURNT OUT. MAINTENANCE REPLACED THE LAMP CIRCUIT PANEL, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052200133 19980522 00133 EU 1998 5 22 QXEA9800652 1 19980511 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX - EMERGENCY LIGHT AT SEAT 9A INOPERATIVE. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052200134 19980522 00134 WP 1998 5 22 98FDEA00344 1 19980513 A 3230 61912 HYD FUSE DOUG DC10 DC1030F 3023504 WP RT MLG WW BLOWN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 317FE 46835 GEAR HANDLE W/N COME UP AFTER T/O, STEERING HANDLE CENTERED, GROUND TENSION CHECKED OK ON TAT. PRESSED HANDLE RELEASE A ND HANDLE STILL W/N COME UP. REMOVED AND REPLACED TRIM CYLINDER INTERLOCK FUSE, SYS OPS CK NORMAL PER MM 32-31-06-02. 2 L 7 3 4F RT A22WE 1998052200135 19980522 00135 NM 1998 5 22 98FDEA00345 1 19980513 A 5320 STRAP BOEING 727 727225 1384077 NM BS 1176 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR1277 - MAIN CARGO COMPT HAS 3 EA ELONGATED FASTENERS HOLES IN PREVIOUS STRAP REPAIR STA 1176 LBL 30 WL 212. INSTALLED FREEZE PLUGS AND NEW STRAP PER EA 7-5310-29491. 2 L 7 3 4F A3WE 1998052200136 19980522 00136 NM 1998 5 22 98FDEA00346 1 19980513 A 5320 STRAP BOEING 727 727225 1384077 NM BS 1176 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 NR1276 MAIN CARGO 2 EA LARGE HOLES IN FLOOR STRAP LBL 4 STA 1176. INSTALLED FREEZE PLUGS AND NEW STRAP PER EA 7-5310-2 9491. 2 L 7 3 4F A3WE 1998052200137 19980522 00137 WP 1998 5 22 ABXA9800447 1 19980512 A 3350 387 BULB DOUG DC9 DC932F 3022067 WP COCKPIT FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 904AX 47040 COCKPIT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. RELAMPED COCKPIT EMERGENCY LIGHTS. OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998052200138 19980522 00138 WP 1998 5 22 ABXA9800448 1 19980512 A 3350 A5395X3 LIGHT DOUG DC8 DC862 3021970 WP COCKPIT LOOSE A ABXA K NONE L NO TEST CR CRUISE 1 GL 23 802AX 46134 DURING CRUISE EMERGENCY LIGHT ON CAPTAIN'S SIDE WAS ARCING BETWEEN LIGHT ASSEMBLY BRACKET AND BULB. LIGHT ASSEMBLY WAS LOOSE IN MOUNT. TIGHTENED MOUNT NUT. OPS CHECKED GOOD IAW DC8 MM 33-00. 2 L 7 4 4F 4A25 1998052200139 19980522 00139 WP 1998 5 22 MWEA98591 1 19980513 A 3260 0080004003 PROX CONTRL UNIT DOUG DC9 DC932 3022066 WP LANDING GEAR DEFECTIVE A MWEA D RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 GL 31 204ME 47680 AFTER TAKEOFF, THE RED GEAR UNSAFE LIGHT REMAINED ON EVEN AFTER RECYCLING GEAR. MAINTENANCE REMOVED AND REPLACED PROX S WITCH CONNECTOR AND PROX CONTROL UNIT. 2 L 7 2 4F A6WE 1998052200140 19980522 00140 WP 1998 5 22 MWEA98592 1 19980507 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP RT WING CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND CORROSION ON RIGHT WING FRONT SPAR TEE CAP SPLICE PLATE INBOARD OF NUMBER 1 SLAT DRIVE TRACK. MAINTENANCE FABRICA TED AND INSTALLED NEW STRAP. 2 L 7 2 4F A6WE 1998052200141 19980522 00141 WP 1998 5 22 MWEA98593 1 19980510 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 990 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND CRACK ON RIGHT HAND SKIN AT FS 990 BELOW LONGERON 14R. MAINTENANCE REMOVED DAMAGED SKIN AND FABRICATED AND INSTAL LED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998052200142 19980522 00142 WP 1998 5 22 MWEA98594 1 19980512 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 206ME 47791 THE LEFT ENTRANCE WAY PORTABLE LIGHT BATTERY CONTACTS FOUND BAD. MAINTENANCE REPLACED BATTERIES. 2 L 7 2 4F A6WE 1998052200143 19980522 00143 WP 1998 5 22 MWEA98595 1 19980513 A 5511 998114634 RIB DOUG DC9 DC982 3022082 WP HORIZ STAB MISDRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND DOUBLE DRILLED HOLE ON HORIZONTAL STABILIZER AT STATION XH6 RIB ASSEMBLY AT AFT SPAR AREA. MAINTENANCE FABRICATED AND INSTALLED BUSHING FOR REPAIR. 2 L 7 2 4F A6WE 1998052200144 19980522 00144 WP 1998 5 22 SCNA98501 1 19980513 A 5320 ANGLE DOUG DC10 DC1015 3022118 WP BS 2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE RIGHT TUNNEL LEG IN THE WASTE TANK COMPARTMENT, APPROXIMATELY STATION 2007, FLOOR LEVEL. REMOVED CORRODED SECTION AND SPLICED IN A REPAIR IN ACCORDANCE WITH SRM 53-40-00, FIGURE 16 . 2 L 7 3 4F A22WE 1998052200145 19980522 00145 WP 1998 5 22 SCNA98502 1 19980513 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY MAINTENANCE VISIT, CORROSION WAS FOUND ON THE RIGHT TUNNEL 186 END AT FLOOR SUPPORT BEAM END IN THE WASTE T ANK COMPARTMENT, APPROXIMATELY STATION 2007, FLOOR LEVEL. REMOVED CORRODED SECTION AND SPLICED IN A REPAIR IN ACCORDANC E WITH SRM 53-70-00, FIGURE 13 AND SRM 51-31-01. 2 L 7 3 4F A22WE 1998052200146 19980522 00146 WP 1998 5 22 SCNA98503 1 19980513 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP CABIN CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY CHECK, THE REMOVAL OF A FLOOR PANEL TO FACILITATE MAINTENANCE REVEALED A CRACKED FLOOR SUPPORT UNDER THE PA TIO FLOOR PANEL. FABRICATION OF ONE DOUBLER, 2024 T3 .040 AND ONE FILLER 2029 T3 .032 PER SRM 53-00-01 AND TREATED PER SRM 51-21-01 AND INSTALLED PER SRM 51-31-01. THE REPAIR PER SRM 53-00-01. 2 L 7 3 4F A22WE 1998052200147 19980522 00147 WP 1998 5 22 SCNA98504 1 19980513 A 5720 BRACKET DOUG DC10 DC1015 3022118 WP RT WING CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY CHECK, RIGHT HAND LATERAL CONTROL SPOILER MIXER BRACKET HAS A .25 CRACK NOTED ON AFT SPOILER BRACKET ON AFT SIDE AT TRANSITION RADII BETWEEN THE LEGS AND BODY OF THE BRACKET INBOARD LEG. REPLACED WITH A NEW AND IMPROVED MIXER BRACKET P/N APH7275-517 PER MM 27-61-01. STOP MEASUREMENTS VERIFIED ON ENGINEERING ORDER. OPERATIONAL CHECK IS COMPLIE D WITH ON ENGINEERING ORDER. 2 L 7 3 4F A22WE 1998052200148 19980522 00148 WP 1998 5 22 SCNA98505 1 19980513 A 5712 RIB DOUG DC10 DC1015 3022118 WP WS 491 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY CHECK, THE RIGHT HAND LEADING EDGE INTERNAL HAS A THREE INCH CRACK ON THE LOWER RIB APPROX AT STATION 491. FABRICATED TWO EACH DOUBLERS 7975 .063 AND 7075 .025 AND FILLER 7075 T6 .040 HEAT TREATED AND PRIMED IAW SRM 51-21-01 A ND INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998052200149 19980522 00149 1998 5 22 SCNA98043 2 19980512 A 7260 717000 GEARBOX BOEING 727 7272A1 138407F NM NR 2 ENGINE CRACKED A SCNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 15 287SC 21345 DURING CRUISE FLIGHT, NUMBER TWO ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE DROPPED TO 25 PSI WITH THE Q UANTITY DOWN TO .8 GALLONS. SHUT DOWN NUMBER TWO ENGINE AND DIVERTED TO DEN. REMOVED AND REPLACED NUMBER TWO ENGINE MA IN ACCESSORY GEARBOX. LEAKS, OPERATIONAL CHECK AND POWER RUN ACCOMPLISHED. FUNCTIONALLY CHECKED GOOD IN ACCORDANCE WIT H JT8D MAINTENANCE MANUAL SECTION 7260. 2 L 7 3 4F A3WE 1998052200150 19980522 00150 NM 1998 5 22 DHL9870726C 1 19980423 A 5320 ANGLE BOEING 727 72722 1384002 NM BS 1263 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CRACK AT BS 1263 RT SIDE BELOW UPPER SKIN TORQUE BOX FWD SIDE OF FS 1263 UNDER FILLER. REMOVED AND INSTALL ED ANGLE PER SRM 51-30-2. 30 BY 1.5 BY 1.5. INSTALLED WEB REPAIR ON TORQUE BOX PER SRM 51-40-2, 31. BY 15. N/R 4850. 2 L 7 3 4F A3WE 1998052200151 19980522 00151 NM 1998 5 22 DHL9870727C 1 19980427 A 5210 78333199 FITTING BOEING 727 72722 1384002 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, LEFT SIDE 1183 DOOR FRAME STOP FITTING CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-30-2. DOOR ADJUSTE D ON N/R 5546 N/R 5600. 2 L 7 3 4F A3WE 1998052200152 19980522 00152 NM 1998 5 22 DHL9870728C 1 19980427 A 5210 FITTING BOEING 727 72722 1384002 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, RIGHT SIDE STA 1183 DOOR FRAME 7 DOOR STOP FITTING CRACKED. REMOVED NR 7 STOP FITTING AND REPLACED PER SRM 51-10-1, N/R 5599. 2 L 7 3 4F A3WE 1998052200153 19980522 00153 NM 1998 5 22 DHL9870729C 1 19980422 A 5320 6518636251 STIFFENER BOEING 727 72722 1384002 NM BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, RIGHT MLG W/W INBD WALL VERTICAL STIFFENER LOWER AT BS 940 IS CRACKED. REPLACED STIFFENER PER SRM 53-10-1. REPLACED LOWER ATTACH ANGLE PER SRM 53-10-1. N/R 7912. 2 L 7 3 4F A3WE 1998052200154 19980522 00154 NM 1998 5 22 DHL9870730C 1 19980421 A 5755 SKIN BOEING 727 72722 1384002 NM LT SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, 32 SPOILER PANEL IS DELAMINATED ON TOP SIDE. INSTALLED FIBERGLASS OVERLAY REPAIR UPPER AND LOWER PER SRM 51 -40-8. N/R 1041. 2 L 7 3 4F A3WE 1998052200155 19980522 00155 NM 1998 5 22 DHL9870731C 1 19980421 A 5755 65192228 FITTING BOEING 727 72722 1384002 NM NR 7 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, NR 7 SPOILER ACTUATOR MOUNT CASTING CRACKED AT UPPER FLANGE AFT END BOTH SIDES. INSTALLED NEW FITTING PER S RM 51-10-1. N/R 1053. 2 L 7 3 4F A3WE 1998052200156 19980522 00156 NM 1998 5 22 DHL9870732C 1 19980421 A 5311 FRAME BOEING 727 72722 1384002 NM BS 930 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, LT WHEEL WELL BS 930 FRAME CRACKED AT UPPER 2 ATTACH FASTENERS, JUST BELOW PRESSURE DECK. HFEC FOR VERIFICA TION, STOP DRILLED DECK, HFEC. INSTALLED ASSURANCE CUT, INSTALLED REPAIR PER S/B 53-130 PART 3, N/R 3616. 2 L 7 3 4F A3WE 1998052200157 19980522 00157 NM 1998 5 22 DHL9870733C 1 19980422 A 5320 655348315 FITTING BOEING 727 72722 1384002 NM CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, FWD CARGO COMPT DOOR CUT OUT FWD FRAME LOWER STOP FITTING CRACKED. REMOVED AND REPLACED STOP FITTING PER SR M 51-10-4. N/R 3635. 2 L 7 3 4F A3WE 1998052200158 19980522 00158 NM 1998 5 22 DHL9870734C 1 19980421 A 5330 SKIN BOEING 727 72722 1384002 NM BS 384 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C CHECK, LOWER SKIN CRACKED AT LAP JOINT BS 384 LOWER FASTENER ROW. REMOVED FASTENERS, OVERSIZED HOLE, ACCOMPLISHED HFEC. INSTALLED FASTENER. N/R 3646. 2 L 7 3 4F A3WE 1998052200159 19980522 00159 NM 1998 5 22 DHL9870735C 1 19980424 A 5315 FLOOR BEAM BOEING 727 72722 1384002 NM BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, LEFT MLG BEAM SUPPORT AT BS 940 CRACKED AT FWD LOWER FLOORBEAM FLANGE. HFEC OF CRACK, STOP DRILLED, HFEC. I NSTALLED REPAIR KIT PER S/B 53-190. N/R 3683. 2 L 7 3 4F A3WE 1998052200160 19980522 00160 NM 1998 5 22 DHL9870736C 1 19980423 A 5400 6524509502 FITTING BOEING 727 72722 1384002 NM NR 2 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CENTER ENGINE INLET DUCT HOUSING ATTACH FITTING CRACKED AT STA 1130 RT SIDE I/B SIDE. REMOVED AND REPLACED ATTACH FITTING PER S/B 54-011, N/R 4829. 2 L 7 3 4F A3WE 1998052200161 19980522 00161 NM 1998 5 22 DHL9870737C 1 19980423 A 5400 INLET BOEING 727 72722 1384002 NM NR 2 NACELLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CENTER INLET OUTER HOUSING DELAMINATED AND CRACKED FROM BS 1116 TO BS 1151 12 O'CLOCK TO 3 O'CLOCK POSITION . INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51-40-8, 75 BY 38, 20 BY 38. N/R 4891. 2 L 7 3 4F A3WE 1998052200162 19980522 00162 NM 1998 5 22 DHL9870738C 1 19980430 A 5712 BULKHEAD BOEING 727 72722 1384002 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, AFT BAGGAGE 950 BULKHEAD CRACKED AT LBL 12 WL 185. STOP DRILLED END OF CRACK, HFEC. INSTALLED DOUBLER REPA IR 5 BY 12 PER SRM 53-10-9. N/R 3724. 2 L 7 3 4F A3WE 1998052200163 19980522 00163 NM 1998 5 22 DHL9870739C 1 19980428 A 5712 BULKHEAD BOEING 727 72722 1384002 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, AFT 950 BULKHEAD CRACKED AT APPROX RBL 41 WL 185. STOP DRILLED ENDS OF CRACK, HFEC. INSTALLED DOUBLER REPA IR PER SRM 53-10-9, 11.5 BY 5. N/R 3712. 2 L 7 3 4F A3WE 1998052200164 19980522 00164 NM 1998 5 22 DHL9870740C 1 19980422 A 5712 BULKHEAD BOEING 727 72722 1384002 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, AFT BAGGAGE 950 BULKHEAD HAS 7 INCH CRACK AT LBL 58 WL 190 . CUT OUT CRACKED SKIN 10 BY 1.25, HFEC. INSTAL LED DOUBLER REPAIR PER SRM 53-10-9. N/R 3697. 2 L 7 3 4F A3WE 1998052200165 19980522 00165 NM 1998 5 22 DHL9870741C 1 19980422 A 5312 BULKHEAD BOEING 727 72722 1384002 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C CHECK, AFT BAGGAGE 950 BULKHEAD HAS 8 INCH CRACK AT LBL 22 WL 185. STOP DRILLED CRACK, HFEC. INSTALLED DOUBLER R EPAIR PER SRM 53-10-9, 5 BY 12, N/R 3696. 2 L 7 3 4F A3WE 1998052200166 19980522 00166 NM 1998 5 22 DHL9870742C 1 19980422 A 5312 BULKHEAD BOEING 727 72722 1384002 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, AFT BAGGAGE 950 BULKHEAD HAS 3 INCH CRACK AT RBL 57 WL 191. STOP DRILLED CRACK, HFEC. INSTALLED DOUBLER RE PAIR PER SRM 53-10-9, 5.75 BY 2.75, N/R 3695. 2 L 7 3 4F A3WE 1998052200167 19980522 00167 NM 1998 5 22 DHL9870743C 1 19980421 A 5330 SKIN BOEING 727 72722 1384002 NM BS 259 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, BUTT JOINT BS 259 AFT PANEL INDICATES 10 PERCENT MATERIAL LOSS JUST BELOW STR 14R TO 16R. CUT OUT DAMAGED A REA, INSTALLED SKIN SPLICE PER S/B 53-084 AREA 2 FT BY 2 FT, N/R 3647. 2 L 7 3 4F A3WE 1998052200168 19980522 00168 NM 1998 5 22 DHL9870744C 1 19980420 A 5330 SKIN BOEING 727 72722 1384002 NM BS 390 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, SKIN BULGE AT BS 390, STR 4 LT. ACCOMPLISHED HFEC, FROM BS 360 TO 440. 10 PERCENT MATERIAL LOSS. CUT OUT DAMAGED AREA 6 BY 3 PER SRM 53-30-3. FABRICATED AND INSTALLED REPAIR PARTS BS 390, STR 14 LEFT PER SRM 53-30-3. N/R 35 27. 2 L 7 3 4F A3WE 1998052200169 19980522 00169 NM 1998 5 22 DHL9870745C 1 19980422 A 5754 ANGLE BOEING 727 72722 1384002 NM NR 6 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, 36 SLAT ACTUATOR ACCESS PANEL ATTACH ANGLES ARE CRACKED. REPLACED ANGLES PER SRM 51-40-4, N/R 2814. 2 L 7 3 4F A3WE 1998052200170 19980522 00170 NM 1998 5 22 DHL98742002 1 19980514 A 2120 AIR DISTRIBUTION BOEING 727 727225 1384077 NM COCKPIT ODOR A DHLA H G DEACTIVATE SYST/CIRCUITS O2 MASK DEPLOYED N FALSE WARNING DE DESCENT 1 SO 01 742DH 21290 AT FL 240, CARGO SMOKE LIGHT ILLUMINATED. ALL CREW MEMBERS SMELLED SMOKE. PERFORMED SMOKE SOURCE IDENT CHECKLIST. INS PECTED FOR SOURCE, INSPECTED CARGO, CARGO COMPT, E/E COMPT, LOWER CARGO COMPTS AND AFT AIRSTAIRS AREA. RAN ENGINES, RAN A/C PACKS AND GASPER SYSTEMS. USED DIFFERENT BLEED COMBINATIONS, OPS CHECK SMOKE SYSTEM. UNABLE TO DUPLICATE OR FIND S OURCE OF SMOKE. 2 L 7 3 4F A3WE 1998052200171 19980522 00171 WP 1998 5 22 ARWA980503 1 19980511 A 2731 179894 TRIM ACTUATOR DOUG DC8 DC862 3021970 WP ELEVATOR ERRATIC A ARWA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 19 791AL 46150 AFTER ROTATION STAB SETTING WENT ALL THE WAY FWD. SAME AT ALL SPEEDS UP TO 320 KTS. RETURNED TO MIAMI WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED PTC ACTUATOR IAW MM 27-30-6. OPS CHECK NORMAL IAW MM 27-30-0 PILOT REPORTS ELEVETOR/STA B TRIM OPERATES NORMAL ON TEST FLIGHT. 2 L 7 4 4F 4A25 1998052200172 19980522 00172 NM 1998 5 22 VJ9800149 1 19980508 A 3350 07192 LIGHT BOEING 737 7372P6 NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 EICJW 21355 LIGHT RECEPTACLE INOP ON AFT TRACK FOR THE E-PATH LIGHTING. REPLACED 1 LIGHT RECEPTACLE ON AFT TRACK IAW BAC MM 33-21-2 7. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998052200173 19980522 00173 NM 1998 5 22 VJ9800150 1 19980508 A 3350 LIGHT BOEING 737 7372E1 138448F NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 461AT 20976 FWD EMERGENCY PATH LIGHTING INOP. FERRIED AC TO MCO, THEN ONTO DHN FOR C CHECK WHERE IT WILL BE FIXED. 2 L 7 2 4F A16WE 1998052200174 19980522 00174 WP 1998 5 22 VJ9800151 1 19980512 A 3397 081691 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 907VJ 47444 EMERGENCY EXIT LIGHT AT SEAT ROW 10D INOP. WIRE BROKEN. REMOVED AND REPLACED EMERGENCY LIGHT SOCKET IAW 33-50. 2 L 7 2 4F A6WE 1998052200175 19980522 00175 EU 1998 5 22 MALA976124 1 19980511 A 7931 IPTE1191000200 TRANSDUCER SAAB SF340 340B 7860101 EU LT GEAR BOX FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 426XJ 426 AFTER CLIMB THE LEFT OIL PRESSURE GRADUAL FELL FROM 100 PSI TO 25 PSI, STAYED THERE AND THEN WENT BACK TO 100 PSI. AIRC RAFT RETURNED TO MSP. ON TAXI IN THE PRESSURE WENT DOWN TO ABOUT 5 PSI. PROP OPERATED NORMALLY AT ALL TIMES. MAINTENA NCE REPLACED PROP GEAR BOX OIL TRANSDUCER. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998052200176 19980522 00176 NM 1998 5 22 K3HA980072 1 19980512 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN LOOSE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 FLOOR EXIT LIGHT LOOSE AT SEATS 2ABC. SECURED TRACK. 2 L 7 3 4F A3WE 1998052200177 19980522 00177 NE 1998 5 22 CALA9800863 2 19980514 A 7314 378201 FUEL PUMP BOEING 727 727243 138408D NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A CALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 09 17410 11310 4281 21663 NUMBER 2 ENGINE FAILED AT ROTATION. FOUND FUEL PUMP SHAFT SHEARED. REPLACED NUMBER 2 ENGINE FUEL PUMP AND FUEL CONTROL PER MM 71-00-67. 2 L 7 3 4F 4 F RT A3WE E2EA 1998052200178 19980522 00178 WP 1998 5 22 CALA9800864 1 19980514 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 47798 FLOORBEAM IS CORRODED AT FS 980 LBL 15 TO LBL 50. REMOVED DAMAGED AREA. FABRICATED, PRIMED, AND INSTALLED REPAIR PER S RM 51-10-3, 53-01, 53-05, AND 51-30-5. 2 L 7 2 4F A6WE 1998052200179 19980522 00179 WP 1998 5 22 CALA9800865 1 19980514 A 5313 2777922 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 47798 CRACK (1.3) AT FRAME STA 756 L3L. REMOVED DAMAGED SECTION OF LONGERON. FABRICATED AND INSTALLED REPAIR SPLICES PER SRM 53-02 AND 51-10-3. 2 L 7 2 4F A6WE 1998052200180 19980522 00180 WP 1998 5 22 CALA9800866 1 19980514 A 5330 6165438 SKIN DOUG DC9 DC982 3022082 WP BS 256 DENTED A CALA O OTHER O OTHER IN INSP/MAINT 1 SW 09 18833 49493 FUSELAGE DENTED STA 256 L 18. INSTALLED DOUBLER REPAIR PER EC/RA 5330-02664. 2 L 7 2 4F A6WE 1998052200181 19980522 00181 SO 1998 5 22 COMA9810117 1 19980512 A 2730 ATG120TR SENSORS EMB 120 EMB120RT SO ELEVATOR MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 257CA 120248 'TAKE OFF TRIM' WARNING SOUNDED. REPLACED ELEVATOR TRIM PROXIMITY SENSORS. 2 L 7 2 4T RT A31SO 1998052200182 19980522 00182 SO 1998 5 22 COMA9810118 1 19980512 A 3260 922AA2YA6PZ722 SENSOR EMB 120 EMB120RT SO NLG MALFUNCTIONED A COMA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 244CA 120217 WHEN LANDING GEAR RETRACTED, THE NLG DOWN LIGHTS AND INTRANSIT LIGHTS REMAINED ON. REPLACED THE NLG DOWN LOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1998052200183 19980522 00183 SO 1998 5 22 COMA9810119 1 19980513 A 3350 101107 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 120233 EMERGENCY EXIT SIGN AT ROW 8 BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998052200184 19980522 00184 SO 1998 5 22 COMA9810120 1 19980513 A 3350 1011107 SIGN EMB 120 EMB120RT SO CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 205CA 120250 EXIT SIGN LOOSE AT ROW 5A. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998052200185 19980522 00185 EA 1998 5 22 COMA9860100 1 19980513 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 959CA 7116 CABIN DOOR OUTER HANDLE CAUTION MESSAGE AFTER TAKEOFF. ADJUSTED DOOR HANDLE MECHANISM. 2 L 7 2 4F RT A21EA 1998052200186 19980522 00186 EA 1998 5 22 COMA9860101 1 19980512 A 7931 1153P0012 SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 917CA 7017 807061 OIL PRESSURE WARNING DURING TAKEOFF. REPLACED OIL PRESSURE SWITCH. 2 L 7 2 4F 4 F RT A21EA E15NE 1998052200187 19980522 00187 NE 1998 5 22 COMA9860102 2 19980512 A 7320 505OT37G01 VG ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE LEAKING A COMA K NONE K FLUID LOSS UK UNKNOWN 1 SO 01 977CA 3272 1722 7157 807435 FUEL DRIPPING FROM LEFT HAND ENGINE DRAIN. REPLACED THE INBOARD VG ACTUATOR. 2 L 7 2 4F 4 F RT A21EA E15NE 1998052200188 19980522 00188 EA 1998 5 22 COMA9860103 1 19980513 A 2841 INDICATOR CNDAIR CL600 CL6002B19 EA LT FUEL SYST FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 912CA 7011 LEFT HAND FUEL QUANTITY FAILED. FUEL QUANTITY SYSTEM PLACED ON DEFERRED MAINTENANCE LIST. 2 L 7 2 4F RT A21EA 1998052200189 19980522 00189 EA 1998 5 22 COMA9860104 1 19980513 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA LT EXTERIOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 984CA 7171 LEFT HAND EXTERIOR EMERGENCY LIGHT INOPERABLE. REPLACED LAMP. 2 L 7 2 4F RT A21EA 1998052200190 19980522 00190 EA 1998 5 22 COMA9860105 1 19980513 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA COCKPIT BIRDSTRIKE A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 954CA 7100 BIRDSTRIKE DURING DEPARTURE. C/W BIRDSTRIKE INSPECTION. NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 1998052200192 19980522 00192 WP 1998 5 22 UPS98826605 1 19980417 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK CABIN FLOORBEAM, STA 8 RBL 26, HAS CORROSION ON FWD FLANGE. FABRICATED REPAIR STRAP AND INSTALLED IT IAW REO 04644 (ATTACHED TO UPS NR 542659) AND DC8 SRM 51 1 8, 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200193 19980522 00193 WP 1998 5 22 UPS98826606 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK STA 680, LONGERON 7R FWD BATHTUB FITTING CRACKED. REMVOED FITTING, DRILLED AMD INSTALLED NEW ONE I AW DC8 SRM 51 3 0 A ND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200194 19980522 00194 WP 1998 5 22 UPS98826607 1 19980416 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK FWD PIT STA 160 180 FLOOR POST SEAT TRACK AND SPLICES CORRODED. REMOVED CORROSION FROM POST AND SP LICES ALODINED AND PRIMED IAW DC8 SRM 51 1 8. REMOVED DAMAGED SEAT TRACK DRILLED AND INSTALLED NEW SECTION IAW DC8 SRM 51 1 8 AND 51 3 0 AND 51 1 24. 2 L 7 4 4F RT 4A25 1998052200195 19980522 00195 WP 1998 5 22 UPS98826608 1 19980414 A 5320 FORMER DOUG DC8 DC871F 302199D WP BS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK AFT PIT STA 1060 AND LONGERON 36 FORMER CORRODED. REMOVED FORMER FABRICATED NEW ONE IAW DWG DC8 5 3 0229 AND DC8 SRM 51 1 8. INSTALLED IAW DAC DWG 53 0229. 2 L 7 4 4F RT 4A25 1998052200196 19980522 00196 WP 1998 5 22 UPS98826609 1 19980411 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK ZEE FITTING AT FS 1160, LONGERON 34 RIGHT TO LONGERON 33 RIGHT CRACKED. REMOVED FITTING DRILLED NE W ONE IAW DC8 SRM, 53 2 0 FIG 2G WITH SPLICES. INSTALLED IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200197 19980522 00197 WP 1998 5 22 UPS98826610 1 19980513 A 2612 FIRE LOOPS DOUG DC8 DC873F 302199F WP NR 4 ENGINE MALFUNCTIONED A IPXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 808UP 46008 AT FL 330 OBSERVED THE MASTER WARNING LIGHT ON. NO OTHER INDICATIONS ABNORMAL. CHECKED SHORT CIRCUT NR 4 DID NOT TEST IN EITHER POSITION THE WARNING LIGHT CAME ON AGAIN, CHOOSE TO SHUT DOWN NR 4. UNABLE TO DETERMINE IF FIRE EXISTS. AFTE R SHUT DOWN NR 4 MAN AIR OVER TEMP LIGHT ILLUM, THEN EXTING ABOUT 20 SEC LATER RT MAN TEMP (SEE HARD COPY). VISUALLY IN SP NR 4 ENG PNUE DUCTING FOR COND AND SEC NO DEFECTS. REMOVED AND REPLACED ALL CORE SECTION FIRE DETECTION LOOPS. ALSO REMOVED AND REPLACED WIRE HARNESS FROM PYLON TO ENG, RAN ENGINE AT HIGH POWER AND SYSTEM OPS CK'D GOOD. 2 L 7 4 4F RT 4A25 1998052200198 19980522 00198 WP 1998 5 22 UPS98826613 1 19980511 A 5320 37502571N SPLICE DOUG DC8 DC873F 302199F WP BS 600-620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C SPLICE FITTING FROM F/S 600-620 LONG 31L CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998052200199 19980522 00199 WP 1998 5 22 UPS98826614 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK STA 680 LONGERON 8L FWD BATHTUB FITTING CRACKED. REMOVED FITTING DRILLED AND INSTALLED NEW ONE IA W DC8 SRM 51 1 20D AND 51 3 0 AND 51 1 23. 2 L 7 4 4F RT 4A25 1998052200200 19980522 00200 WP 1998 5 22 UPS98826615 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK STA 680 LONGERON 4 L FWD BATHTUB FITTING CRACKED. REMOVED FITTING FABBED AND INSTALLED NEW ONE IAW DC8 SRM 51 1 20D AND 51 3 0 AND 51 1 23. 2 L 7 4 4F RT 4A25 1998052200201 19980522 00201 WP 1998 5 22 UPS98826616 1 19980406 A 5755 BRACKET DOUG DC8 DC871F 302199D WP LT SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK PERMANENT REPAIR TO LEFT HAND WING INBBOARD SPOILER BRACKET PER REO DC8 5720 6998. FABRICATED REPA IR ANGLES ALODINED AND PRIMED AND INSTALLED REPAIR IAW REO DC8 5720 6998, DC8 SRM 57 2 0 FIG 2 AND DC8 SRM 51 1 8. 2 L 7 4 4F RT 4A25 1998052200202 19980522 00202 WP 1998 5 22 UPS98826617 1 19980414 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 900-920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK MAIN CABIN STA 900 TO 920 LONGERON 7L END FITTING CRACKED. REMOVED OLD FITTING FROM AC LOCATED AN D DRILLED NEW FITTING IAW DC 8 SRM 51 3 2. INSTALLED NEW FITTING IAW DC8 SRM, 51 3 0. 2 L 7 4 4F RT 4A25 1998052200203 19980522 00203 WP 1998 5 22 UPS98826618 1 19980417 A 5320 STIFFINER DOUG DC8 DC871F 302199D WP BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK RT W/W VERTICAL STIFFENER AT FS 940 FOR OB WW CLOSE OUT WALL HAS CRACK, JUST FWD OF FLAP BUS CABLE DRUM. FABRICATED DOUBLER IAW DC8 SRM 53 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED DOUBLER IAW SRM 53 2 0 AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200204 19980522 00204 WP 1998 5 22 UPS98826619 1 19980417 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK FRAME CRACKED AT STA 1680 LONGERON 22 RIGHT. REMOVED DAMAGED FRAME SECTION IAW DC8 SRM 51 1 21. F ABRICATED NEW FRAME SECTION IAW DC8 SRM 51 1 4 HEAT TREATED NEW FRAME SECTION FROM 7075 0 TO 7075 T6, .071 IAW TPS 1003 REV A ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200205 19980522 00205 WP 1998 5 22 UPS98826620 1 19980422 A 5320 SUPPORT DOUG DC8 DC871F 302199D WP COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK CRACK, CORROSION ON FLOOR SUPPORT AT STA 8 TO STA 25. FABRICATED DOUBLER IAW DC8 SRM 53 2 0. ALOD INED AND PRIMED IAW DC8 SRM 51 1 8. REMOVED CORROSION IAW DC8 SRM 51 1 8. INSTALLED DOUBLER IAW DC 8 SRM 51 1 21. 2 L 7 4 4F RT 4A25 1998052200206 19980522 00206 WP 1998 5 22 UPS98826621 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK LONGERON 24 RIGHT OF FLOOR FITTING HAS CORROSION ON AFT FACE AND CRACKED ON AFT UPPER LEG AT FS 94 0. REMOVED FLOOR FITTING FABRICATED SPLICE ASSY IAW DC8 SRM 53 2 0. ALODINED AND PRIMED SURFACE IAW DC8 SRM 51 1 8 AND INSTALLED SPLCIE ASSY IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200207 19980522 00207 WP 1998 5 22 UPS98826622 1 19980415 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK SEAT TRACK B HAS CORROSION BETWEEN FS 980 1000. REMVOED SEAT TRACK B FS 980 1000. DRILLED NEW SEA T AND INSTALLED IAW DC8 SRM 51 1 24 AND 51 3 0. 2 L 7 4 4F RT 4A25 1998052200208 19980522 00208 WP 1998 5 22 UPS98826623 1 19980414 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 480-500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK CORROSION IN SEAT TRACK D BETWEEN FS 480 AND 500. REMOVED 4 HOLE PLUG AND ROUTED OUT FOR NEW 5 HO LE PLUG IAW DC8 SRM 53 2 3. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 PUT 5 HOLE PLUG IAW DC8 SRM 53 2 3. INSTALLED FASTE NERS IAW DC8 SRM 51 3 0. 2 L 7 4 4F RT 4A25 1998052200209 19980522 00209 WP 1998 5 22 UPS98826624 1 19980512 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE:DALY EMER EXIT LIGHT INOP. REMOVED AND REPLACED EMER LIGHT BATTERY PACK PER DC8 MM 33-50-01. LIGHTS OP S CHECK GOOD. 2 L 7 4 4F RT 4A25 1998052200210 19980522 00210 EU 1998 5 22 QXEA9800654 1 19980512 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 PDX - EVACUATION LIGHT AT ROW 8 IS INOPERATIVE IN ARM POSITION, WORKED IN ON POSITION. MAINTENANCE RELAMPED, OPERATIONA L TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998052200211 19980522 00211 NM 1998 5 22 98FDEA00347 1 19980514 A 5320 6517688107 SILL BOEING 727 727227 1384078 NM BS 340-343 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 484FE 21466 CORROSION (C53-224-06) ON FWD ENTRY DOOR MOPSILL BS 340-343 LBL 60 WL 208. 2 L 7 3 4F A3WE 1998052200212 19980522 00212 NM 1998 5 22 98FDEA00348 1 19980514 A 5320 691541610 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 484FE 21466 NR-0408, WHILE WORKING NR0384, FOUND SHEAR TIE BS720 STR 28L - 28R, WL 148 TO BE CORRODED. REMOVED CORROSION ON SHEAR T IE BS 720 STR 28L - 28R, WL 138. FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX 727 SRM 53-10-1. FABRICATED, LOCATED BA CKDRILLED AND INSTALLED NEW SHEAR TIE PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1998052200213 19980522 00213 NM 1998 5 22 98FDEA00349 1 19980514 A 5330 6554577 SKIN BOEING 727 727227 1384078 NM BS 720-724 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 484FE 21466 CORROSION ON SKIN BS 720 - 724 BETWEEN STR 28L - 28R WL 148. REMOVED CORROSION ON SKIN BS 720-724 STR 28L - 28R WL 148 . FOUND CORROSION TO BE OUT OF LIMITS PER FEDEX 727 SRM 5-10-1. REMOVED DAMAGED, FABRICATED REPAIR AND INSTALLED PER F EDEX 727 SRM 53-30-3. 2 L 7 3 4F A3WE 1998052200214 19980522 00214 NM 1998 5 22 98FDEA00350 1 19980515 A 3230 RETRACT MECH BOEING 727 72722 1384002 NM NLG LACK OF LUBE A FDEA K NONE J WARNING INDICATION AP APPROACH 1 SO 25 184FE 18870 ON FINAL, NOSE GEAR DID NOT INDICATE DOWN (NO GREEN LIGHT) WHEN GEAR DOWN WAS INITIALLY SELECTED. GEAR HANDLE RECYCLED AND ALL GEAR INDICATED NORMAL DOWN AND LOCKED. LUBED NOSE GEAR, CYCLED GEAR SEVERAL TIMES, OPS CK NORMAL, INDICATED THR EE GREEN LIGHTS, PER MM 32-00. 2 L 7 3 4F A3WE 1998052200215 19980522 00215 WP 1998 5 22 98FDEA00341 1 19980512 A 5400 BOLT DOUG DC10 DC1030F 3023504 WP PYLON LOOSE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 SNRM N 00874, A/C 304, FOUND 9 EA BOLTS LOOSE AT BOTTOM OF PYLON FWD MOUNT. REMOVE, INSPECTED AND INSTALLED 9 EA BOLTS PER M/M 20-50-0212. 2 L 7 3 4F RT A22WE 1998052200216 19980522 00216 WP 1998 5 22 98FDEA00342 1 19980512 A 5511 SR105500043 SPAR CAP DOUG DC10 DC1030F 3023504 WP RT HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 304FE 46992 FOUND .5 INCH CRACK IN UPPER REAR SPAR CAP OUTER SECTION SKIN PANEL (RIGHT HAND SIDE). REF: EO 8-5510-7-3310 PART 4. R EPAIRED PER EA 8-5510-38504- HORIZONTAL STAB RT UPPER AFT SKIN PANEL REPAIR. 2 L 7 3 4F RT A22WE 1998052200217 19980522 00217 NM 1998 5 22 98FDEA00343 1 19980513 A 5270 SWITCH BOEING 727 727247 138408F NM AFT AIRSTAIRS DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 235FE 21329 AFT AIRSTAIR LIGHT ILLUMINATED AT ROTATION AND STAYED LIGHTED. OPENED AFT AIRSTAIR, CLEANED SW, CYCLED STAIRS. OPS CK NORMAL. 2 L 7 3 4F A3WE 1998052200218 19980522 00218 NM 1998 5 22 98FDEA00292 1 19980424 A 5240 65569925 SKIN BOEING 727 727233 138408A NM BS 1040 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 NR 0141 013, LEFT HAND SERVICE DOOR OUTER SKIN IS CRACKED APPROX .75 AT LWR FWD CORNER, CRACK IS GOING THROUGH FASTENER. REPAIRED L/SERVICE DOOR OUTER SKIN, LWR FWD CORNER IAW FEDEX SRM 52-40-2 PG 1, 5. 2 L 7 3 4F RT A3WE 1998052200219 19980522 00219 NM 1998 5 22 98FDEA00293 1 19980424 A 5315 BAC150611087075T FLOORBEAM BOEING 727 727233 138408A NM BS 760-800 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 NR 0454 014, CORROSION (C53-224-01(2)) ON LONGITUDINAL BEAM AT RBL 45, BS 760-800, WL 208, I/B FLANGE. REMOVED CORROSIO N ON LONGITUDINAL BEAM RBL 45, BS 760-800. FOUND TO BE OUT LIMITS, PER FEDEX SRM 53-10-1. REMOVED AND REPLACED LONGIT UDINAL FLOORBEAM PER FEDEX SRM 51-30-2, 51-20-1 AND MM 51-20-151. 2 L 7 3 4F RT A3WE 1998052200220 19980522 00220 NM 1998 5 22 98FDEA00291 1 19980424 A 5230 6556927108 FRAME BOEING 727 727233 138408A NM BS 1092-1122 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 NR 0240 012, NR 3 LWR CARGO DOOR FWD FRAME IS CRACKED IN O/B RADIUS, AT LWR STOP FITTING. REMOVED AND REPLACED LWR FWD NR 3 CARGO DOOR FRAME IAW FEDEX SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F RT A3WE 1998052200221 19980522 00221 WP 1998 5 22 ABXA9800449 1 19980512 A 3231 57156105501 VALVE DOUG DC8 DC862 3021970 WP RT MLG DOOR DEFECTIVE A ABXA K NONE J WARNING INDICATION CL CLIMB 1 GL 23 804AX 45987 ON CLIMB-OUT, GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AND THE RIGHT MAIN LANDING GEAR DOOR NOT LATC HED LIGHT WAS ILLUMINATED. RECYCLED GEAR WITH THE SAME RESULTS. REPLACED RIGHT MAIN LANDING GEAR DOOR CONTROL VALVE AN D UPLATCH ASSY. INSPECTED ALL PULLEYS, BRACKETS AND CABLES IN BOTH WHEEL WELLS. NO DEFECTS NOTED. PERFORMED OPS CHECK IAW DC8 MM 32-60-0. 2 L 7 4 4F 4A25 1998052200222 19980522 00222 WP 1998 5 22 ABXA9800450 1 19980513 A 3230 57146745503 VALVE ASSY DOUG DC8 DC862 3021970 WP MLG BYPASSING A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 826AX 46060 AFTER TAKEOFF AND GEAR RETRACTED, GEAR UNSAFE LIGHT WAS ILLUMINATED. RECYCLED GEAR WITH SAME RESULTS. PERFORMED GEAR U PLATCH CHECK AND LEFT AND RIGHT MAIN GEAR AND DOORS, 'NOT LATCHED' LIGHT WAS ILLUMINATED. REPLACED SYSTEM SELECTOR VALV E FOR BYPASSING. OPS CHECKED NORMAL IAW DC8 MM 32-36-00. 2 L 7 4 4F 4A25 1998052200223 19980522 00223 NM 1998 5 22 SCNA98700 1 19980502 A 5320 WEB BOEING 727 727227 1384078 NM BS 1303 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 275AF 22092 DURING A HEAVY MAINT CHECK, AT FUSE STA 1303 SECTION 48 CROWN WEB RT SIDE HAS 2 CRACK. CUT-OUT DAMAGE AREA IN ACCORANCE WITH B727 SRM 51-40-2. MATERIAL IS PER B727 SRM 53-10-2 FIG 6 AS 7075-T6 .025C. FABRICATED DOUBLER FROM 7075-T6 .032C IAW/B727 SRM 51-40-2. TREATED AND PRIMED PARTS AND AREA IAW/B727 SRM 51-10-6. INSTALLED REPAIR IAW/B727 SRM 51-40-2 A ND 51-30-2. 2 L 7 3 4F A3WE 1998052200224 19980522 00224 NE 1998 5 22 RRXA98086 2 19980510 A 7200 ENGINE DOUG DC8 DC871F 302199D WP GE CFM56 CFM562C1 13802 NE NR 1 FLAMED OUT A RRXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 WP 15 500MH 45812 DURING DESCENT GOING THROUGH 12000 FT, NR 1 ENGINE FLAME OUT. NO RESPOND WITH IGNITION OVERRIDE, OIL PRESSURE LIGHT ILL UMINATED WITH OIL PRESS DECREASING. OIL PRESS REMAINED AT 0 PSI THROUGHOUT FLIGHT. SUMPED NR 1 AND NR 1 ALT TANKS REMO VED APPROX 1 CUP WATER FROM NR 1 MAIN TANK SUMPED UNTIL NO ADDITIONAL WATER FOUND. PERFORMED VISUAL INSPECTION NR 1 ENG INLET AND EXHAUST. NO DEFECTS. INSPECTED CHIP DETECTORS AND FUEL FILTER, SPECIFIC GRAVITY ADJ, NO DEFECTS FOUND. ON ENG RUN GRD IDLE CHECKS GOOD, FLIGHT IDLE GOOD AND ACCELS NORMAL TO 90 PERCENT N2, FUEL PRESS ALSO GOOD W/PUMP OFF. AC OKAY TO CONTINUE. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998052200225 19980522 00225 NM 1998 5 22 VNAA9805006 1 19980506 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 436JS 57984 22805 3052 DURING THE PREFLIGHT INSPECTION, ROW SEVEN AND NINE EMERGENCY LIGHTS, FAILED TO ILLUMINATE DURING TEST. OUTSTATION MAIN TENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO DCA . THE FERRY FLIGHT TOOK PLACE WITHOUT INCIDENT. M AINTENANCE IN DCA INSPECTED AND REPLACED 7LK EMERGENCY BATTERY, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998052200226 19980522 00226 WP 1998 5 22 TC8A98021 1 19980505 A 2432 CA51N BATTERY DOUG DC8 DC862F 3021972 WP BATTERY COMPT DISCHARGED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 817EV 73 46022 TRIP NR 1742A, AFTER ENGINE START BATTERY VOLTAGE READ ZERO. REMOVED AND REPLACED SHIPS BATTERY, OPS CHECKS NORMAL IAW MM 24-30-1. 2 L 7 4 4F 4A25 1998052200227 19980522 00227 WP 1998 5 22 TC8A98022 1 19980507 A 2130 NASI SYST DOUG DC8 DC8F55 3021928 WP CABIN MALFUNCTIONED A TC8A O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 GL 23 182SK 45817 TRIP NR 1764, UNABLE TO PRESSURIZE, PERFORMED TCA PROCEDURES FOR UNPRESSURIZED FLIGHT. OIL SMELL WAS NOTED. ON GROUND (KILN) PRESSURIZATION TEST DONE, FOUND RIGHT NASI VERY WEAK. CHECK OUTFLOW VALVE FOR OPS, CHECK OK. CHECKED FLOW CONTR OL VALVE ON NASI SYSTEM CHECK OK. PRESSURIZED A/C AND CHECK FOR FUSELAGE LEAKS, NONE WERE FOUND. AIRCRAFT WAS PRESSURI ZED UP TO 6 PSI, OPERATIONAL CHECK OF THE SYSTEM WAS DONE IAW MM 21-1-0, OPS CHECKS OK. 2 L 7 4 4F 4A25 1998052200228 19980522 00228 WP 1998 5 22 TC8A98023 1 19980510 A 5543 5644220501 TAB DOUG DC8 DC862 3021970 WP RUDDER DAMAGED A TC8A A UNSCHED LANDING E VIBRATION/BUFFET UK UNKNOWN 1 GL 23 181SK 45910 TRIP NR 01787, AIRCRAFT VIBRATING AFTER 290 KTS (SUSPECT RUDDER) WITH AUTO-PILOT ON OR OFF, YAW DAMPER ON OR OFF. VIBRA TION INCREASED WITH RUDDER HYDRAULIC POWER IN OFF POSITION. REMOVED AND REPLACED TAB ASSY, RUDDER OPS CHECK ON GROUND G OOD IAW DC8 MM 27-21-2. 2 L 7 4 4F 4A25 1998052200230 19980522 00230 WP 1998 5 22 TC8A98025 1 19980514 A 3010 ANTI-ICE DUCT DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 2 BROKEN A TC8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 183SK 45904 671250 FIRE WARNING NR 2 ON CLIMBOUT. REMOVED AND REPLACED BROKEN ANTI-ICE DUCT IAW MM 75-10-3 AND REPAIRED CRACK ON DIFFUSER IAW MM 72-00. 2 L 7 4 4F 4 F 4A25 1E8 1998052200449 19980522 00449 WP 1998 5 22 VJ9800152 1 19980514 A 2170 COALESCER DOUG DC9 DC932 3022066 WP CABIN DIRTY A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 907VJ 47444 AFTER TAKEOFF, FLIGHT ATTENDANT EXPERIENCED AN UNUSUAL SMELL IN FWD CABIN. AS A PRECAUTIONARY MEASURE, FLIGHT CREW ELEC TED TO RETURN TO MAIN MAINTENANCE BASE. INSPECTED AIRCRAFT, OPERATED BOTH ENGINES, INSPECTED APU, AIR CONDITIONING DUCT ING IN GALLEYS. NO DEFECTS NOTED. AS PRECAUTIONARY MEASURE, REPLACED THE LT AND RT COALESCER BAGS PER MM21-00. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998052200450 19980522 00450 NM 1998 5 22 K3HA980073 1 19980514 A 3397 WIRE BOEING 727 727225 1384077 NM GALLEY BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 AFT GALLEY CENTER AISLE DOUBLE EMERGENCY LIGHT DID NOT WORK. FOUND PIN 3 TO EMERGENCY LIGHT ASSEMBLY BROKEN IN RECEPTAC LE REPAIRED WIRING PER 33-51-02, OPS CHECK OK, EMERGENCY LIGHTS MM 33-50-81. 2 L 7 3 4F A3WE 1998052200451 19980522 00451 NM 1998 5 22 RAAA98B2027 1 19980513 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998052200452 19980522 00452 NM 1998 5 22 RAAA98B2028 1 19980513 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998052200453 19980522 00453 SO 1998 5 22 RAAA98E9016 1 19980514 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998052200454 19980522 00454 SO 1998 5 22 RAAA98ER012 1 19980514 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 AFT LT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998052200455 19980522 00455 1998 5 22 9809126717 4 19980513 A 2210 YAW DAMPER BOEING 747 747251F 1384898 NM E/E COMPT FAILED A A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 617US 21121 DURING CLIMB, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED YAW MOTION. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPLACED THE UPPER AND LOWER YAW DAMPER COMPUTER. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998052200456 19980522 00456 NE 1998 5 22 9809131149 2 19980511 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 01 149US 46758 686157 WHILE IN CRUISE FLIGHT AT FL340, THE AIRCRAFT ENCOUNTERED MODERATE TURBULENCE, POSSIBLY WAKE TURBULENCE, AND THE NR 1 EN GINE FLAMED OUT. THE ENGINE WAS SECURED PER ENGINE FAILURE CHECKLIST AND A DESCENT FROM FL340 WAS STARTED. AT FL300, A RESTART WAS ACCOMPLISHED PER COM PROCEDURE. ALL ENGINE INDICATIONS WERE NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINT ENANCE INSPECTED THE ENGINE AND PERFORMED A FULL POWER ENGINE RUN, ALL WITH NO PROBLEMS FOUND. THE AIRCRAFT RETURNED TO SERVICE. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998052200457 19980522 00457 NE 1998 5 22 9809146638 2 19980511 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 2 ENGINE STALLED A NWAA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 GL 01 638US 23549 715178 AT TOP OF DESCENT WITH POWER REDUCTION, THE NR 2 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN AND A SUCCESSFUL RE START WAS ACCOMPLISHED AT FL290. ENGINE OPERATION FOR THE REMAINDER OF THE FLIGHT WAS NORMAL. MAINTENANCE INSPECTED THE ENGINE FOR A STALL PER MM 71-00-00 WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E3NE 1998052200458 19980522 00458 WP 1998 5 22 9809169945 1 19980513 A 2613 OVERHEAT SENSOR DOUG DC9 DC931 3022065 WP TAIL COMP FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 8925E 45840 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE TAIL COMPARTMENT OVERHEAT SENSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998052200459 19980522 00459 1998 5 22 9809179619 4 19980513 A 3442 20671570153 TRANSCEIVER DOUG DC9 DC932 3022066 WP RADAR FAILED A NWAA A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 01 619NW 12924 1695 47518 WEATHER RADAR SYSTEM PAINTED WIDE BAND OF RED ACROSS TOP AND RIGHT OF SCREEN AT ALL ALTITUDES AND RANGES. FLIGHT WAS RE TURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RADAR TRANSCEIVER. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998052200460 19980522 00460 WP 1998 5 22 9809189139 1 19980513 A 3350 BATTERY DOUG DC9 DC914 3022034 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 948L 47049 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS AT FS 762, 864, AND 996 INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN POWER SUPPLY B5-28. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052200461 19980522 00461 WP 1998 5 22 9809199752 1 19980513 A 3620 SENSOR DOUG DC9 DC941 302207N WP TAIL COMPT INOPERATIVE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 752NW 47116 DURING CLIMB-OUT, THE TAIL COMPARTMENT HIGH TEMPERATURE LIGHT ILLUMINATED. FLIGHT CREW FOLLOWED COM PROCEDURES, RETURNE D TO BNA, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT HIGH TEMPERATURE SENSOR. OPERATIONAL CHECK NORMA L. 2 L 7 2 4F A6WE 1998052200462 19980522 00462 WP 1998 5 22 9809209859 1 19980512 A 3246 WHEEL DOUG DC9 DC951 3022051 WP NLG OUT OF BALANCE A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 GL 01 768NC 47729 DURING TAKEOFF, THE AIRCRAFT EXPERIENCED NOSE WHEEL SHAKING AT 60 KTS AIRSPEED. FLIGHT CREW ABORTED TAKEOFF AND RETURNE D TO THE GATE WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AND RIGHT NOSE TIRE AND WHEEL ASSEMBLIES. OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F RT A6WE 1998052200463 19980522 00463 WP 1998 5 22 9809219863 1 19980514 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 772NC 47774 DURING LINE CHECK, FOUND TAILCONE EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998052200464 19980522 00464 WP 1998 5 22 9809229759 1 19980514 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN CORRODED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 759NW 47287 DURING LINE CHECK, FOUND EMERGENCY LIGHT IN FIRST CLASS SECTION INOPERATIVE. MAINTENANCE CLEANED CORRODED WIRE SPLICE A T SEATS 1C AND D. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052200465 19980522 00465 WP 1998 5 22 UPS98826625 1 19980426 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 80 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK INTERCOSTAL CRACKED, FS 80 AT L30R. REMOVED INTERCOSTAL FABBED AND INSTALLED NEW ONE IAW DC8 SRM 5 1 1 20D, 51 1 8 AND DOUGLAS DWG 5613064. 2 L 7 4 4F RT 4A25 1998052200466 19980522 00466 WP 1998 5 22 UPS98826626 1 19980419 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK MAIN CABIN FLOORBEAM FITTING AT STA 781 AND BTL 50R CRACKED. REMOVED FITTING, DRILLED AND INSTALLE D NEW ONE IAW DC8 SRM 5130, 51 1 20D, AND 51 3 2. 2 L 7 4 4F RT 4A25 1998052200467 19980522 00467 WP 1998 5 22 UPS98826627 1 19980413 A 5414 SKIN DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, OUTBOARD SIDE OF PYLON NR 1 CRACKED. REPAIRED PER EO 04609 AND DC8 SB 54 95 BY INSTALLING REPAIR DOUBLERS. 2 L 7 4 4F RT 4A25 1998052200468 19980522 00468 WP 1998 5 22 UPS98826628 1 19980413 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 219.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, RIGHT WING LEADING EDGE SKIN CRACKED AT XFS 219.5. CUT OUT DAMAGED AREA IN SKIN AND FABRICATED RE PAIR FILLER AND DOUBLER IAW DC8 SRM 57 2 1. ALODINED AND PRIMED REPAIR PART A/C STRUCTURE IAW DC8 SRM 51 1 8. INSTALLE D REPAIR IAW DC8 SRM 51 1 21 AND 51 1 20 D, SEALED IAW DC8 SRM 51 1 15 AND 51 1 17. 2 L 7 4 4F RT 4A25 1998052200469 19980522 00469 WP 1998 5 22 UPS98826629 1 19980414 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1150 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, Z FITTING CRACKED STA 1150 LONGERON 33 RIGHT TO 34 RIGHT. REMOVED Z FITTING CUT NEW FITTING AND FABBED SPLICES IAW DC8 SRM 53 2 0 FIG 2G. INSTALLED IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200470 19980522 00470 WP 1998 5 22 UPS98826630 1 19980415 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, STA 1690 END FITTING CRACKED, LONGERON 29 LEFT. REMOVED FITTING INSTALLED NEW FITTING. FABBED O N OPS 50013 IAW DC8 SRM 51 1 24, AND 51 1 21. 2 L 7 4 4F RT 4A25 1998052200471 19980522 00471 WP 1998 5 22 UPS98826631 1 19980415 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, STA 1690, LONGERON 31 RIGHT END FITTING CRACKED. REMOVED FITTING DRILLED AND INSTALLED NEW ONE IA W DC8 SRM 51 1 21 AND 51 1 20D. FABBED FITTING IAW DAC DWG 4641324. 2 L 7 4 4F RT 4A25 1998052200472 19980522 00472 WP 1998 5 22 UPS98826632 1 19980416 A 5312 BULKHEAD FITTING DOUG DC8 DC871F 302199D WP FWD PRESS BLKHD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, FWD PIT AFT 6 BULKHEAD FITTING CRACKED, LONGERON 33 RIGHT. REMOVED FITTING DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200473 19980522 00473 WP 1998 5 22 UPS98826633 1 19980416 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK MAIN CABIN STA 660 680 LONGERON 11 LEFT CRACKED. REMOVED FITTING DRILLED AND INSTALLED NEW PART IAW DC8 SRM, 51 1 20 D AND 51 3 0 NAD 51 1 8. 2 L 7 4 4F RT 4A25 1998052200474 19980522 00474 WP 1998 5 22 UPS98826634 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, STA 680 LONGERON 6 RIGHT FWD BATHTUB FITTING CRACKED. REMOVED FITTING INSTALLED NEW ONE IAW DC8 SRM 51 1 20D NAD 51 3 0 AND 51 1 23. 2 L 7 4 4F RT 4A25 1998052200475 19980522 00475 WP 1998 5 22 UPS98826635 1 19980417 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, FLOORBEAM STA 55 AT RBL 5 UPPER T CAP AFT FLANGE CRACKED. REMOVED DAMAGED AREA, FABRICATED AND IN STALLED T CAP REPAIR IAW REO 04620, DC8 SRM 53 3 3 AND 51 1 21 AND 51 1 8 AND 51 1 11. 2 L 7 4 4F RT 4A25 1998052200476 19980522 00476 WP 1998 5 22 UPS98826636 1 19980418 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 834 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, MAIN CABIN FRAME FITTING CRACKED AT STA 834 AND LONGERON 22 RIGHT. REMOVED DAMAGED FITTING, DRILL ED AND REAMED HOLES INTO NEW FITTING IAW DC8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM, 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200477 19980522 00477 WP 1998 5 22 UPS98826637 1 19980418 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 855 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, MAIN CABIN FRAME FITTING AT STA 855 AND LONGERON 22 RIGHT CRACKED. REMOVED FITTING FABBED NEW ONE IAW DAC DWG 577994 ALODINED AND PRIMED AND INSTALLED IT IAW DC8 SRM 51 1 8 AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200478 19980522 00478 WP 1998 5 22 UPS98826638 1 19980419 A 5320 CLIP DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, MAIN CABIN STA 680 AND BTL 25 RIGHT FLOORBEAM CLIP CRACKED. REMOVED ANGLE FABBED AND INSTALLED N EW ONE IAW DC8 DWG 5773275. INSTALLED IAW DC8 SRM 51 1 20D AND 51 1 8. 2 L 7 4 4F RT 4A25 1998052200479 19980522 00479 WP 1998 5 22 UPS98826639 1 19980419 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1634-1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, CORROSION, SEAT TRACK E AT STA 1634 TO 1680. REMOVED DAMAGED SECTION, STA 1600 TO 1680. FABBED A ND INSTALLED NEW SECTION IAW DC8 SRM 51 3 0 AND UPS EO DC8 5320 5167. 2 L 7 4 4F RT 4A25 1998052200480 19980522 00480 NM 1998 5 22 QXEA9800653 1 19980511 A 2611 473054 SMOKE DETECTOR DHAV 82523211001 DHAV DHC8 DHC8202 2809007 NM CARGO COMP MALFUNCTION A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 358PH 542 506 SEA - SMOKE WARNING LIGHT FLASHED ON IN FLIGHT. UPON ARRIVAL IN SEA, MAINTENANCE INSPECTED BAGGAGE COMPARTMENT, NO SMOK E, FIRE, OR SMELL NOTED. REPLACED NR 1 AND NR 2 SMOKE DETECTORS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVIC E. NR 2 S/N 0542 542 HOURS, 772 CYCLES. 2 H 7 2 4T RT A13NM 1998052200481 19980522 00481 NM 1998 5 22 98FDEA00351 1 19980515 A 3230 PIN DOUG MD11 MD11F 3023600 NM CTR MLG INSTALLED A FDEA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 25 583FE 48421 CENTER GEAR W/N RETRACT AFTER T/O. RED TABS C/W RETURNED TO MEM. REMOVED L/GEAR PIN FROM CENTER GEAR. 2 L 7 3 4F RT A22WE 1998052200482 19980522 00482 NE 1998 5 22 SCNA98044 2 19980514 A 7230 COMPRESSOR BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17 52049 NE ENGINE STALLED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 15 288SC 20765 COMPRESSOR STALL ON ENGINE RUNUP, TAKEOFF ABORTED. INSPECTED ALL THREE ENGINES IN ACCORDANCE WITH 720000 FOR DAMAGE. N O DAMAGE FOUND. PERFORMED BLEED SHIFT CHECK AND OPERATIONALLY CHECKS GOOD IN ACCORDANCE WITH 710000. OK FOR SERVICE AT THIS TIME. 2 L 7 3 4F 4 F RT A3WE E2EA 1998052200483 19980522 00483 WP 1998 5 22 CKSA98269 1 19980511 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 729 TEMPORARY A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 TEMPORARY REPAIR INSTALLED ON FUSELAGE STA 729 AT LONGERON 34. REMOVED PREVIOUS REPAIR. INSTALLED PERMANENT REPAIR IAW L1011 SRM 53-31-00 FIG 815. CORROSION TASK CARD NUMBER C53-120-04-01. NON-ROUTINE TASK CARD NUMBER 18490. 2 L 7 3 4F A23WE 1998052200484 19980522 00484 WP 1998 5 22 CKSA98270 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 639 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP STA 639 BETWEEN LONGERON 35 AND 36 DISBONDED. R EPAIRED DISBONDED TEARSTRAP IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD NUMBER C53-120-04-01, CARD NUMBER 53-CR -1001. NON ROUTINE TASK CARD NUMBER 18492. 2 L 7 3 4F A23WE 1998052200485 19980522 00485 WP 1998 5 22 CKSA98271 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 659 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION ,FOUND LEVEL 2 CORROSION: FAILSAFE STRAP STA 659 BETWEEN LONGERON 31 AND 32 DISBONDED AND SKIN HAS CORROSION. REMOVED CORROSION IAW L1011 SRM 51-10-01. CORROSION REMOVAL WITHIN LIMITS IAW L1011 SRM 53-31-00. REPAIRED FAILSAFE STRAP IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD NUMBER C53-120-04-01, CARD NUMBER 53-CR-1 001. NON ROUTINE TASK CARD NUMBER 18493. 2 L 7 3 4F A23WE 1998052200486 19980522 00486 WP 1998 5 22 CKSA98272 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1393 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1393 BETWEEN LONGERON 30 AND 31. REPAIRED DISBONDED TEARSTRAP AT STA 1393 LONGERON 30-31 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD NUMBER C53 -120-04-02, CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18514. 2 L 7 3 4F A23WE 1998052200487 19980522 00487 WP 1998 5 22 CKSA98273 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1413 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1413 BETWEEN LONGERON 30 AND 31. R EPAIRED DISBONDED TEARSTRAP AT STA 1413 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD NUMBER C53-120-04-02, CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18515. 2 L 7 3 4F A23WE 1998052200488 19980522 00488 WP 1998 5 22 CKSA98274 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1433 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1433 BETWEEN LONGERON 35 AND 36. REPAIRED DISBONDED TEARSTRAP AT STA 1433 BETWEEN LONGERON 35 AND 36 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CAR D NUMBER C53-120-04-02, CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18516. 2 L 7 3 4F A23WE 1998052200489 19980522 00489 WP 1998 5 22 CKSA98275 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1433 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1433 BETWEEN LONGERON 29 AND 31. REPAIRED DISBONDED TEARSTRAP AT STA 1433 BETWEEN LONGERON 29 AND 31 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CAR D NUMBER C53-120-04-02 CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18517. 2 L 7 3 4F A23WE 1998052200490 19980522 00490 WP 1998 5 22 CKSA98276 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1490 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1490 BETWEEN LONGERON 31 AND 32. REPAIRED DISBONDED TEARSTRAP AT STA 1490 BETWEEN LONGERON 31 AND 32 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CAR D NUMBER C53-120-04-02, CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18518. 2 L 7 3 4F A23WE 1998052200491 19980522 00491 WP 1998 5 22 CKSA98277 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1512 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1512 BETWEEN LONGERON 31 AND 32. REPAIRED DISBONDED TEARSTRAP AT STA 1512 BETWEEN LONGERON 31 AND 32 IAW L1011 SRM 53-31-00 FIG 816, CORROSION TASK CARD NUMBER C53-120-04-02, CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18519. 2 L 7 3 4F A23WE 1998052200492 19980522 00492 WP 1998 5 22 CKSA98278 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1535 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1535 BETWEEN LONGERON 27 AND 32. REPAIRED DISBONDED TEARSTRAP AT STA 1535 BETWEEN LONGERON 27 AND 32 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CAR D NUMBER C53-120-04-02, CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18520. 2 L 7 3 4F A23WE 1998052200493 19980522 00493 WP 1998 5 22 CKSA98279 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1555 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 1555 BETWEEN LONGERON 29 AND 31. REPAIRED DISBONDED TEARSTRAP AT STA 1555 BETWEEN LONGERON 29 AND 31 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CAR D NUMBER C53-120-04-02, CARD NUMBER 53-CR-1002. NON ROUTINE TASK CARD NUMBER 18521. 2 L 7 3 4F A23WE 1998052200494 19980522 00494 WP 1998 5 22 CKSA98280 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1575 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED AND CORROSION ON INNER SKIN STA 1575 BETWEEN LONGERON 29 AND 30. REMOVED CORROSION IAW L1011 SRM 51-10-03. CORROSION REMOVAL BEYOND LIMITS IAW L1011 SRM 53 -31-00. REPAIRED AREA IAW L1011 SRM 53-31-00 FIG 815. REPAIRED FAILSAFE STRAP IAW L1011 SRM 53-31-00 FIG 816. CORROSI ON TASK CARD NUMBER C53-120-04-02. NON ROUTINE TASK CARD NUMBER 18522. 2 L 7 3 4F A23WE 1998052200495 19980522 00495 WP 1998 5 22 CKSA98281 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 839 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 839 BETWEEN LONGERON 31 AND 32. R EPAIRED DISBONDED TEARSTRAP AT STA 839 BETWEEN LONGERON 31 AND 32 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD N UMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18495. 2 L 7 3 4F A23WE 1998052200496 19980522 00496 WP 1998 5 22 CKSA98282 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 839 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 839 BETWEEN LONGERON 27 AND 28. R EPAIRED DISBONDED TEARSTRAP AT STA 839 BETWEEN LONGERON 27 AND 28 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD N UMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18496. 2 L 7 3 4F A23WE 1998052200497 19980522 00497 WP 1998 5 22 CKSA98283 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 856 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 856 BETWEEN LONGERON 30 AND 32. R EPAIRED FAILSAFE STRAP AT STA 856 BETWEEN LONGERON 30 AND 32 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18499. 2 L 7 3 4F A23WE 1998052200498 19980522 00498 WP 1998 5 22 CKSA98284 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 856 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 856 BETWEEN LONGERON 26 AND 27. R EPAIRED DISBONDED TEARSTRAP AT STA 856 BETWEEN LONGERON 26 AND 27 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD N UMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18500. 2 L 7 3 4F A23WE 1998052200499 19980522 00499 WP 1998 5 22 CKSA98285 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 875 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 875 BETWEEN LONGERON 31 AND 32. R EPAIRED FAILSAFE STRAP AT STA 875 BETWEEN LONGERON 31 AND 32 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18502. 2 L 7 3 4F A23WE 1998052200500 19980522 00500 WP 1998 5 22 CKSA98286 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 893 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 INSPECTION: FAILSAFE STRAP DISBONDED STA 893 BETWEEN LONGERON 30 AND 32. REPAIRED FAILSAFE STRAP AT STA 893 BETWEEN LONGERON 30 AND 32 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK CARD NUMB ER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18503. 2 L 7 3 4F A23WE 1998052200501 19980522 00501 WP 1998 5 22 CKSA98287 1 19980511 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 913 DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: FAILSAFE STRAP DISBONDED STA 913 BETWEEN LONGERON 27 AND 29. R EPAIRED DISBONDED FAILSAFE STRAP AT STA 913 BETWEEN LONGERON 27 AND 29 IAW L1011 SRM 53-31-00 FIG 816. CORROSION TASK C ARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18505. 2 L 7 3 4F A23WE 1998052200502 19980522 00502 WP 1998 5 22 CKSA98288 1 19980511 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 923 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: CORROSION ON SHEAR TIE STA 923 BETWEEN LONGERON 28 AND 29. RE MOVED CORROSION IAW L1011 SRM 51-10-03. CORROSION REMOVAL OUT OF LIMITS IAW L1011 SRM 53-12-00. REPAIRED SHEAR TIE IAW L1011 SRM 53-72-00 FIG 805. CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18506. 2 L 7 3 4F A23WE 1998052200503 19980522 00503 WP 1998 5 22 CKSA98289 1 19980511 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 943 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION: CORROSION ON SHEAR TIE STA 943 BETWEEN LONGERON 27 AND 28. RE MOVED CORROSION IAW L1011 SRM 51-10-03. CORROSION REMOVAL OUT OF LIMITS IAW L1011 SRM 53-12-00. REPAIRED SHEAR TIE IAW L1011 SRM 53-12-00 FIG 805. CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18507. 2 L 7 3 4F A23WE 1998052200504 19980522 00504 WP 1998 5 22 CKSA98290 1 19980511 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 923 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 INSPECTION: CORROSION ON SHEAR TIE STA 923 BETWEEN LONGERON 27 AND 28. R EMOVED CORROSION IAW L1011 SRM 51-10-03. CORROSION REMOVAL BEYOND LIMITS IAW L1011 SRM 53-12-00. REPLACED SHEAR TIE IA W L1011 SRM 51-10-05 AND 51-40-01. CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18508. 2 L 7 3 4F A23WE 1998052200505 19980522 00505 WP 1998 5 22 CKSA98291 1 19980511 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 923 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 INSPECTION: CORROSION ON SHEAR TIE STA 923 BETWEEN LONGERON 31 AND 32. R EMOVED CORROSION IAW L1011 SRM 51-10-03. CORROSION REMOVAL OUT OF LIMITS IAW L1011 SRM 53-12-00. REPAIRED SHEAR TIE IA W L1011 SRM 53-12-00 FIG 805. CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18510. 2 L 7 3 4F A23WE 1998052200506 19980522 00506 WP 1998 5 22 CKSA98292 1 19980511 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 923 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 INSPECTION: CORROSION ON SHEAR TIE STA 923 BETWEEN LONGERON 35 AND 36. R EMOVED CORROSION IAW L1011 SRM 51-10-03. CORROSION REMOVAL OUT OF LIMITS IAW L1011 SRM 53-12-00. REPAIRED SHEAR TIE IA W L1011 SRM 53-12-00 FIG 805. CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CARD NUMBER 18511. 2 L 7 3 4F A23WE 1998052200507 19980522 00507 WP 1998 5 22 CKSA98293 1 19980511 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 923-943 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 INSPECTION: INNER SKIN CORRODED STA 923-943 BETWEEN STR 27 AND 28. REMOV ED CORROSION IAW L1011 SRM 51-10-03. CORROSION REMOVAL BEYOND LIMITS IAW L1011 SRM 53-31-00. REPAIRED INNER SKIN IAW A IA EA L1-53-012 REV A AND AIA SKETCH NO AIA/E/2699 REV A, CORROSION TASK CARD NUMBER C53-130-05-00. NON ROUTINE TASK CA RD NUMBER 18491. 2 L 7 3 4F A23WE 1998052200508 19980522 00508 WP 1998 5 22 CKSA98294 1 19980511 A 5313 LONGERON LKHEED 1011 1011385115 5265015 WP BS 933 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 INSPECTION: LONGERON 34 CORRODED AND CRACKED STA 933. REPAIRED LONGERON 34 AND STA 933 IAW L1011 SRM 53-13-00 FIG 804 BY SPLICING IN NEW STRINGER SECTION. CORROSION TASK CARD NUMBER C53-130-0 6-00, CARD NUMBER 53-CR-1005. NON ROUTINE TASK CARD NUMBER 18509. 2 L 7 3 4F A23WE 1998052200509 19980522 00509 EU 1998 5 22 HEEA0014136 1 19980511 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R DELAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 4034Q 2918 ONE BEARING DELAMINATED. 1 G 7 1 3U H9EU 1998052200510 19980522 00510 EU 1998 5 22 HEEA0014137 1 19980511 A 3340 356H2801 LIGHT SNIAS 350 AS350B2 8680813 EU ANTI COLL FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 2820 ANTI COLL LIGHT INOPERATIVE. 1 G 7 1 3U H9EU 1998052200511 19980522 00511 EU 1998 5 22 HEEA0014139 1 19980511 A 6730 SC5084 SERVO SNIAS 350 AS350B2 8680813 EU M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 6100R 683 2862 LEAKING OUT OF PISTON. 1 G 7 1 3U H9EU 1998052200512 19980522 00512 1998 5 22 HEEA0014140 4 19980511 A 3120 M803B205VBATT CLOCK BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 406PH 53198 CLOCK DOESN'T RESET FOR TIMES. 1 G 7 1 3U O H2SW 1998052200513 19980522 00513 1998 5 22 HEEA0014142 4 19980511 A 3424 206070274101 INDICATOR BELL 407 407 SW TURN & SLIP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 1638 53070 TURN & SLIP INDICATOR FLAG WON'T PULL. 1 G 7 1 3U O H2SW 1998052200514 19980522 00514 SW 1998 5 22 HEEA0014143 1 19980511 A 6320 50501008380401 SEAL 407340100101 BELL 407 407 SW M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 427PH BH771 53059 OIL SEAL LEAK. 1 G 7 1 3U O H2SW 1998052200515 19980522 00515 SW 1998 5 22 HEEA0014144 1 19980511 A 7714 206075682107 GAGE BELL 206 206L3 1182108 SW GAS PRODUCER FLUCTUATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141BH 51303 GAS PRODUCER NEEDLE FLUCTUATES EXCESSIVELY. 1 G 7 1 3U H2SW 1998052200516 19980522 00516 1998 5 22 HEEA0014145 4 19980511 A 3416 212070238003 ALTIMETER BELL 412 412 1182202 SW COCKPIT ERROR E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 YV928 INDICATOR EXCESSIVE FRICTION ERROR. 1 G 7 2 4U H4SW 1998052200517 19980522 00517 SW 1998 5 22 HEEA0014146 1 19980511 A 6240 412075010111 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 ROTOR NEEDLE IS INOPERATIVE AND NR2 NEEDLE NOISY. TIME SINCE REPAIR 225:00. 1 G 7 2 4U H4SW 1998052200518 19980522 00518 1998 5 22 HEEA0014147 4 19980511 A 2200 4030182901 ALTITUDE SENSOR BELL 412 412 1182202 SW AUTO FLIGHT MALFUNCTION E HEEA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 SW 03 107X 33113 WHEN VHF TRANSMITTER IS KEYED, CYCLIC STICK MOTORS FORWARD AND A/C NOSES DOWN. 1 G 7 2 4U H4SW 1998052200519 19980522 00519 SW 1998 5 22 HEEA0014148 1 19980511 A 7714 206062627003 TACH GEN BELL 206 206L1 1182107 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ON GROUND RUN INDICATOR INDICATES BACKWARDS. 1 G 7 1 3U H2SW 1998052200520 19980522 00520 1998 5 22 HEEA0014149 4 19980511 A 2562 ELT910 ELT NARCO BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 8594X 51531 ELT ACTIVATES UPON LANDING. 1 G 7 1 3U H2SW 1998052200521 19980522 00521 1998 5 22 HEEA0014150 4 19980511 A 3421 1113034 INDICATOR BELL 412 412 1182202 SW ATTITUDE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 7128R 36007 GS AND FD FLAGS SLOW TO PULL AND RT FLAG STICKS. 1 G 7 2 4U H4SW 1998052200522 19980522 00522 SW 1998 5 22 HEEA0014151 1 19980511 A 7931 209070262101 INDICATOR BELL 412 412 1182202 SW OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22608 33075 ENG OIL TEMP/PRESS PSI NEEDLE FLUCTUATES WHEN VIBRATED. 1 G 7 2 4U H4SW 1998052200523 19980522 00523 1998 5 22 HEEA0014152 4 19980511 A 3421 4020936903 INDICATOR BELL 412 412 1182202 SW COCKPIT PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 142PH 33150 3 AXIS GYRO INDICATOR PRECESSES IN PITCH. 1 G 7 2 4U H4SW 1998052200525 19980522 00525 SW 1998 5 22 HEEA0014154 1 19980511 A 2435 23046020 GENERATOR BELL 412 412 1182202 SW START/GEN FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 23023 4162 33080 WILL NOT COME ON LINE AFTER SHUTDOWN. FOUND NOT TO MOTOR WITH START SWITCH ENGAGED. 1 G 7 2 4U H4SW 1998052200526 19980522 00526 1998 5 22 HEEA0014155 4 19980511 A 2312 7001840913 TRANSCEIVER BELL 214 214ST 1182106 SW COCKPIT FAILED E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 5748M 28102 TRANSCEIVER WILL NOT TEST. 2 G 7 2 4U H10SW 1998052200527 19980522 00527 1998 5 22 HEEA0014156 4 19980511 A 2562 ELT910 ELT NARCO SKRSKY S76 S76A 8143006 NE COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546G 760076 ELT SWITCH IS INTERMITTENT. 1 G 7 2 3U H1NE 1998052200528 19980522 00528 SW 1998 5 22 HEEA0014157 1 19980511 A 2621 A352T EXTINGUISHER BELL 206 206L1 1182107 SW FIRE EXT SYS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2761X 45283 FIRE EXT PRESSURE IS LOW. 1 G 7 1 3U H2SW 1998052200529 19980522 00529 1998 5 22 HEEA0014158 4 19980511 A 2350 AMS44 AUDIO BELL 206 206B3 1181506 SW DUAL CHANNEL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 103PH 3000 CAUSES INTERMITTENT LOSS ON VHF AND ICS. 1 G 7 1 3U H2SW 1998052200530 19980522 00530 EU 1998 5 22 HEEA0014159 1 19980511 A 2436 51565000R REGULATOR BOLKMS 105 BO105S 5626006 EU DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911HM S683 VOLTAGE GOES TO 30 VOLTS AND WILL NOT ADJUST. 1 G 7 2 3U H3EU 1998052200531 19980522 00531 1998 5 22 HEEA0014160 4 19980511 A 3416 10220011850 ALTIMETER BELL 212 212 1181420 SW COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3208H 31304 ALTIMETER KOLLSMAN IS HARD TO TURN. NEEDS CERTIFICATION. 1 G 7 1 4U H4SW 1998052200532 19980522 00532 1998 5 22 HEEA0014161 4 19980511 A 3425 1113025 INDICATOR BELL 412 412 1182202 SW COCKPIT HSI FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 INDICATOR REQUIRES EXCESSIVE VOLTAGE TO MOVE DEVIATION NEEDLE. 1 G 7 2 4U H4SW 1998052200533 19980522 00533 1998 5 22 HEEA0014162 4 19980511 A 3425 066304604 INDICATOR KI525A BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 91070 S145 HSI INDICATOR HAS LOOSE PARTS INSIDE. 1 G 7 2 3U H3EU 1998052200534 19980522 00534 SW 1998 5 22 HEEA0014163 1 19980511 A 2840 384178103 SWITCH BELL 412 412 1182202 SW FUEL SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893S 33022 CAPACITANCE READS HIGH ON RIGHT POSITION. 1 G 7 2 4U H4SW 1998052200535 19980522 00535 SW 1998 5 22 HEEA0014164 1 19980511 A 2422 412075101101 INVERTER BELL 412 412 1182202 SW AC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 33008 36004 INVERTER-450VA INOPERATIVE. 1 G 7 2 4U H4SW 1998052200537 19980522 00537 1998 5 22 HEEA0014166 4 19980511 A 2210 7000298901 COMPUTER BELL 412 412 1182202 SW AFCS DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3893L 33006 AFCS COMPUTER SLOW OUTPUT TO ACTUATOR. 1 G 7 2 4U H4SW 1998052200538 19980522 00538 1998 5 22 HEEA0014167 4 19980511 A 2350 AA95758 AUDIO CONTROL BOLKMS 105 BO105S 5626006 EU COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 133AE S800 AUDIO CONTROL HAS LOUD STATIC WHEN TALKING ON FM. 1 G 7 2 3U H3EU 1998052200539 19980522 00539 1998 5 22 HEEA0014168 4 19980511 A 2350 AMS44 AUDIO SELECTOR BELL 206 206L3 1182108 SW DUAL CHANNEL INTERMITTENT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 81SP 51029 DUAL CHANNEL AUDIO PILOT SELECTOR INTERMITTENT. 1 G 7 1 3U H2SW 1998052200540 19980522 00540 1998 5 22 HEEA0014169 4 19980512 A 3452 066106200 TRANSPONDER KT76 BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31821 51076 INSTALLED TRANSPONDER IN AIRCRAFT AND POWERED UP FOR TEST. REPLY LIGHT STAYED ON BUT NO OUTPUT COULD BE MEASURED. PERFO RMED PRELIMINARY INSPECTION, COULD NOT DUPLICATE PROBLEM. ADJUSTED FREQUENCY AND PULSE WIDTH. BENCH CHECK GOOD. 1 G 7 1 3U H2SW 1998052200541 19980522 00541 1998 5 22 HEEA0014170 4 19980512 A 3452 066106200 TRANSPONDER KT76 BELL 407 407 SW COCKPIT FAILED E HEEA K NONE O OTHER CR CRUISE 1 SW 03 427PH 53059 TRANSPONDER QUIT DURING CRUISE FLIGHT. PERFOMED PRELIMINARY INSPECTION. FOUND UNIT TO FIRE UP OK AT FIRST, BUT AFTER AW HILE, UNIT HAD ONLY 50% REPLY. ADJUSTED PRESELECTOR. NO HELP. REPLACED MIXER DIODE CR202. REPAIRED PROBLEM. UNIT QU IT RECEIVING AFTER WARM UP. FOUND PROBLEM TO BEON PRESELECTOR SIDE OF UNIT. REPLACED PRESELECTOR. FOUND UNIT NOT FIRI NG UP. MOVED COILS IN LOCAL OSCILLATOR. NO HELP. 1 G 7 1 3U O H2SW 1998052200542 19980522 00542 1998 5 22 HEEA0014171 4 19980512 A 3452 066106200 TRANSPONDER BELL 206 206L3 1182108 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31821 51076 TRANSPONDER DEAD, WILL NOT POWER UP. PERFORMED PRELIMINARY INSPECTION. FOUND PULSE WIDTH OUT OF SPECS. ADJUSTED V101 F OR GOOD POWER OUT AND ADJUSTED FREQUENCY. NO HELP. ALSO FOUND NO TRANSMIT. REPLACED V101 TUBE. REPAIRED TRANSMIT PRO BLEM BUT PULSE WIDTH AND FREQUENCY STILL OUT OFSPECS AND RECEIVER VERY WEAK. 1 G 7 1 3U H2SW 1998052200543 19980522 00543 1998 5 22 HEEA0014172 4 19980512 A 2312 069102100 TRANSCEIVER KY195B BELL 206 206L1 1182107 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 27702 45300 TRANSCEIVER UNREADABLE WHEN TRANSMITTING. FOUND NO MODULATION AND UNIT DRAWING 4-5 AMPS OF CURRENT WHEN VOLUME WAS TURNE D UP. REPLACED TRANSMIT BRACKET AND T702 TRANSFORMER. REPAIRED BOTH PROBLEMS. ADJUSTED C/N SQUELCH, SIDETONE AND MODU LATION. FOUND GUIDE PIN ON REAR CONNECTOR BROKEN. 1 G 7 1 3U H2SW 1998052200544 19980522 00544 1998 5 22 HEEA0014173 4 19980512 A 3457 0845000000 GPS SKYNAV5000 SNIAS 350 AS350B2 8680813 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6095S 2777 GPS DUMPS MEMORY AND LIGHTS FADE. FOUND AFTER UNIT IS TURNED OFF AWHILE, UNIT LOSES MEMORY AND LIGHTING FADES. 1 G 7 1 3U H9EU 1998052200545 19980522 00545 1998 5 22 HEEA0014174 4 19980512 A 3457 0845000000 GPS SKYNAV5000 BOLKMS 117 BK117B1 5626012 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911TL 7198 SATELLITE SIGNALS WEAK. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT TO TAKE TOO LONG TO LOCK ON AND IS DROPPING SATELL ITES. 1 G 7 2 3U H13EU 1998052200546 19980522 00546 1998 5 22 HEEA0014175 4 19980512 A 3457 0110010600 GPS GPS165 BELL 412 412 1182202 SW COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 TIME CHANGE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT GIVING COURSE INPUT FAIL MESSAGE. 1 G 7 2 4U H4SW 1998052200547 19980522 00547 1998 5 22 HEEA0014176 4 19980512 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911PF S718 PERFORMED PRELIMINARY INSPECTION. FOUND BATTERY NOT CHARGING. 1 G 7 2 3U H3EU 1998052200548 19980522 00548 1998 5 22 HEEA0014177 4 19980512 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 624MB S751 GPS INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND UNIT HAS BURNT PANEL LIGHTS. TIME SINCE REPAIR 100:30. 1 G 7 2 3U H3EU 1998052200549 19980522 00549 1998 5 22 HEEA0014178 4 19980512 A 3457 0110005400 GPS GPS150 BOLKMS 105 BO105S 5626006 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 137AE S851 GPS LOSES WAYPOINTS. FOUND UNIT LOSES WAYPOINTS WHEN UNIT IS TURNED OFF AWHILE. PLACED UNIT IN FREEZER AND LOST DATA ME SSAGE CAME UP. 1 G 7 2 3U H3EU 1998052200550 19980522 00550 SW 1998 5 22 HEEA0014179 1 19980512 A 5320 206031314083S CHANNEL BELL 206 206L1 1182107 SW FUSELAGE DISTORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 45598 FUSELAGE CHANNEL HAS EXCESSIVE BOW AT CENTER. 1 G 7 1 3U H2SW 1998052200551 19980522 00551 NE 1998 5 22 HEEA0014180 1 19980512 A 6230 7635109030044 MAST 763510950004 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 5962 A08100260 760181 MAST WORN WHERE BEARING RIDES. REPLACED WITH A SERVICEABLE PART. 1 G 7 2 3U H1NE 1998052200552 19980522 00552 NE 1998 5 22 HEEA0014181 1 19980512 A 6320 7635109026107 ADAPTER SHAFT 763510950004 SKRSKY S76 S76A 8143006 NE M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 4537 A08100260 760181 ADAPTER SHAFT WORN SEAT. REPLACED WITH A SERVICEABLE PART. 1 G 7 2 3U H1NE 1998052200553 19980522 00553 NE 1998 5 22 HEEA0014182 1 19980512 A 6320 SB3615102 BEARING 763510950004 SKRSKY S76 S76A 8143006 NE M/R SPALLED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 A08100260 760181 BEARING SPALLING. REPLACED WITH A SERVICEABLE PART. 1 G 7 2 3U H1NE 1998052200554 19980522 00554 NE 1998 5 22 HEEA0014183 1 19980512 A 6320 7635109042101 FLINGERS 763510950004 SKRSKY S76 S76A 8143006 NE M/R GR BOX GROOVED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5128 A08100260 760181 HYD PUMP SEAL FLINGER IS GROOVED. REPLACED WITH A SERVICEABLE PART. 1 G 7 2 3U H1NE 1998052200555 19980522 00555 SW 1998 5 22 HEEA0014184 1 19980512 A 6410 206310105101 BEARING 206016201131 BELL 206 206L1 1182107 SW T/R BLADE WORN E HEEA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SW 03 2761N 2104 CS918CS961 45277 STIFF OPERATION OF TAIL ROTOR PEDAL CONTROLS. REPLACED GALLED BEARINGS. (SCRAPPED BEARINGS) 1 G 7 1 3U H2SW 1998052200557 19980522 00557 SW 1998 5 22 HEEA0014186 1 19980512 A 6500 327211 DISC BELL 206 206L1 1182107 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 45598 T/R DRIVE HAS PITTING (CORROSION) AROUND BOLT HOLES. REPLACED WITH NEW DISCS. 1 G 7 1 3U H2SW 1998052200558 19980522 00558 SW 1998 5 22 HEEA0014188 1 19980512 A 6322 206061432109 IMPELLER 206040370103 BELL 206 206L3 1182108 SW BLOWER CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6161A PHI216 51611 BLOWER IMPELLER SCRAPPED DUE TO EXCESSIVE CORROSION. REPLACED WITH NEW PART. 1 G 7 1 3U H2SW 1998052200559 19980522 00559 EU 1998 5 22 HEEA0014189 1 19980512 A 6220 1051418101 SPINDLE BOLKMS 105 BO105S 5626006 EU M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6607K S841 NUMEROUS DISCREPANICES WITH BUSHING BORES. SERIAL NUMBERS REMOVED ARE B4679, B3979, B2637, AND B4006. REPLACED WITH SER VICEABLE PARTS. 1 G 7 2 3U H3EU 1998052200560 19980522 00560 SW 1998 5 22 HEEA0014190 1 19980512 A 6210 412015300109 BLADE BELL 412 412 1182202 SW M/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 22347 11234 36005 M/R BLADE OUTBOARD LEADING EDGE STRIP HAS NUMEROUS PIN HOLES. 1 G 7 2 4U H4SW 1998052200561 19980522 00561 NE 1998 5 22 HEEA0014191 1 19980512 A 6410 7610105101041 BLADE SKRSKY S76 S76A 8143006 NE T/R SPLIT E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1547D 11350 760077 T/R BLADE TRAILING EDGE ON PADDLE "B" IS SPLIT OPEN. 1 G 7 2 3U H1NE 1998052200562 19980522 00562 NE 1998 5 22 HEEA0014192 1 19980512 A 6210 7615009100041A BLADE SKRSKY S76 S76A 8143006 NE M/R DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3122G 9465 760232 CANNOT BALANCE M/R BLADE ON AIRCRAFT (SUSPECT WATER IN THE CORE) 1 G 7 2 3U H1NE 1998052200563 19980522 00563 NE 1998 5 22 HEEA0014193 1 19980512 A 3242 50034261 BRAKE SKRSKY S76 S76A 8143006 NE LT WHEEL CRACKED E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 31217 760229 L/H WHEEL BRAKE ASSY LEAKED FLUID FROM LOWER PUCK AREA. INSPECTED WHEEL BRAKE. FOUND HOUSING CRACKED. REPLACED WITH SE RVICEABLE HOUSING. 1 G 7 2 3U H1NE 1998052200564 19980522 00564 NE 1998 5 22 HEEA0014194 1 19980512 A 3242 50034261 BRAKE SKRSKY S76 S76A 8143006 NE HOUSING CRACKED E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 31217 760229 CALIPER LEAKING OUT OF THE PISTONS. INSPECTED WHEEL BRAKE. FOUND HOUSING CRACKED. REPLACED WITH SERVICEABLE HOUSING. 1 G 7 2 3U H1NE 1998052200565 19980522 00565 SW 1998 5 22 HEEA0014195 1 19980512 A 3213 206324007 SKID TUBE BELL 206 206L1 1182107 SW UNDERCARRIAGE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2770Y 45291 INSP FOUND CRACKS ON SKID TUBE IN SEVERAL PLACES. 1 G 7 1 3U H2SW 1998052200566 19980522 00566 EU 1998 5 22 HEEA0014196 1 19980512 A 5510 11730610 END PLATE BOLKMS 117 BK117A3 5626015 EU H STAB V FIN CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 401PH 7050 HORIZ STAB V FIN VERT END PLATE HAS THREE INCH CRACK AFT OF MOUNTING FLANGE. 1 G 7 2 3U H13EU 1998052200567 19980522 00567 SW 1998 5 22 HEEA0014197 1 19980512 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 SHAFT ASSY HAS EXCESSIVE CORROSION. SCRAPPED AND REPLACED WITH NEW PART. 2 G 7 2 4U H10SW 1998052200568 19980522 00568 SW 1998 5 22 HEEA0014198 1 19980512 A 6510 214040622005 SHAFT ASSY BELL 214 214ST 1182106 SW T/R CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5748M 28102 SHAFT ASSY HAS EXCESSIVE CORROSION. SCRAPPED AND REPLACED WITH NEW PART. 2 G 7 2 4U H10SW 1998052200569 19980522 00569 1998 5 22 HEEA0014199 4 19980513 A 3421 5040017901 INDICATOR BELL 412 412 1182202 SW COCKPIT PRECESSES E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5759N 33002 ATTITUDE INDICATOR PRECESSES. REPLACED BEARINGS AND REBALANCE UNIT. RETURNED TO SERVICE. 1 G 7 2 4U H4SW 1998052200570 19980522 00570 SW 1998 5 22 HEEA0014200 1 19980513 A 5412 206064902127 FIREWALL BELL 407 407 SW AFT LT SIDE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 AFT FIREWALL L/H SIDE: SPOT WELDS ARE CRACKING AT L/H OIL LINE FITTING SUPPORT. STOP DRILLED CRACK. MFG REPAIR USING 0 25 TITANIUM. LOCATED AND INSTALLED TO FIREWALL USING MS20615M-3 RIVETS. 1 G 7 1 3U O H2SW 1998052200571 19980522 00571 GL 1998 5 22 HEEA0014203 2 19980513 A 7250 23034775 SUPPORT 23035128 BELL 206 206L1 1182107 SW ALLSN 250C 250C30P 03013 GL ENG NOZZLE MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 5007N CAT90682 45184 CAE895589 RECEIVING INSPECTION REVEALED: MISALIGNMENT OF G.P. SUPPORT NOZZLE SLOTS. TRIED SEVERAL NR2 NOZZLES UNABLE TO INSTALL INTO G.P. SUPPORT SLOTS. 1 G 7 1 3U 3 U H2SW E1GL 1998052200572 19980522 00572 SW 1998 5 22 HEEA0014204 1 19980514 A 6220 407010150103 FRAHM ASSY BELL 407 407 SW M/R UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 CGOFL 53130 RUBBER BUMPER UNBONDED FROM PAD ASSY P/N 407-010-171-101. UNABLE TO BALANCE M/R HUB AND BLADE ASSY. TO WITHIN LIMITS (4 PER VIBRATION) 1 G 7 1 3U O H2SW 1998052200573 19980522 00573 SW 1998 5 22 HEEA0014205 1 19980514 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 STARTER DISENGAGES AFTER 3 SECONDS. 2 G 7 2 4U H10SW 1998052200574 19980522 00574 SW 1998 5 22 HEEA0014206 1 19980514 A 2510 412070843105 RESTRAIN SYS BELL 214 214ST 1182106 SW COCKPIT MALFUNCTION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 59805 28141 RESTRAIN SYS WILL NOT LOCK PROPERLY. 2 G 7 2 4U H10SW 1998052200575 19980522 00575 SW 1998 5 22 HEEA0014207 1 19980514 A 2435 2CM272B1 STARTER GENERTOR BELL 214 214ST 1182106 SW ENGINE DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6957Y 233 28139 START/GEN CLUTCH HAS EXCESSIVE END PLAY .018. LIMITS ARE .004 TO .010. 2 G 7 2 4U H10SW 1998052200576 19980522 00576 SW 1998 5 22 HEEA0014208 1 19980514 A 3212 212073905001 PRESSURE GAUGE BELL 407 407 SW FLOAT CONTAMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 WATER INSIDE PRESSURE GAUGE. 1 G 7 1 3U O H2SW 1998052200577 19980522 00577 SW 1998 5 22 HEEA0014209 1 19980514 A 6320 222331617101 ISOLATION MT BELL 230 230 1182149 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 23009 ISOLATION MOUNT HAS WORN BEARING. 1 G 7 2 3U NC H9SW 1998052200578 19980522 00578 EU 1998 5 22 HEEA0014212 1 19980514 A 6720 350A33214501 ROD BEARING SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 126 3004 PITCH CONTROL ROD BEARING WORN. 1 G 7 1 3U H9EU 1998052200579 19980522 00579 EU 1998 5 22 HEEA0014213 1 19980514 A 6720 350A33212101 LINK SNIAS 350 AS350B2 8680813 EU T/R PITCH CONT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 140 3004 T/R PITCH CONTROL LINK BEARING WORN. 1 G 7 1 3U H9EU 1998052200580 19980522 00580 EU 1998 5 22 HEEA0014214 1 19980515 A 6520 350A33020005 GEAR BOX SNIAS 350 AS350B2 8680813 EU T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 60951 2470 2771 T/R GR BOX OUTPUT SHAFT CHROME PLATING WEAR. 1 G 7 1 3U H9EU 1998052200581 19980522 00581 GL 1998 5 22 HEEA0014215 2 19980515 A 7260 23039794 PUMP ASSY 23035178 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENG OIL DEFECTIVE E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 8592X CAG95727 51508 CAE895719 RECEIVING INSPECTION REVEALED: DEEP CASTING FLAWS BEYOND SERVICEABLE LIMITS ON PUMP ASSY. SCAVENGE PORT. INSTALLED A SE RVICEABLE PUMP ASSY. 1 G 7 1 3U 3 U H2SW E1GL 1998052200596 19980522 00596 EU 1998 5 22 98ZZZX1890 1 19980420 A 7931 53408 TRANSMITTER AEROSP SA365 AS365N2 8680815 EU ENGINE OIL PRESS FAILED A EGRA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 17 291LL 6402 AIRCRAFT DEPARTED MIFFLIN CO AIRPORT AND NR 1 ENGINE OIL PRESSURE DROPPED TO ZERO. NR 1 ENGINE WAS SHUT DOWN AND AIRCRA FT RETURNED TO MIFFLIN CO AIRPORT. TRANSMITTER REPLACED. 1 G 7 2 3U RT H10EU 1998052200619 19980522 00619 SO 1998 5 22 98ZZZX1913 1 19980430 A 5280 5452810 DOOR PIPER PA31T PA31T 7103124 SO LT MLG CRACKED A FRKA K NONE O OTHER IN INSP/MAINT 1 NE 01 10MC 6100 31T7920028 DURING PRE-FLIGHT INSPECTION, THE PILOT NOTED THAT THE LEFT MAIN OUTBOARD LANDING GEAR DOOR HAD A 6 INCH CRACK IN IT WIT H SLIGHT BENDING. THE CRACK WAS 2 INCHES BELOW THE ATTTACHMENT RODS. 1 L 7 2 3T A8EA 1998052200638 19980522 00638 WP 1998 5 22 9809259966 1 19980514 A 2751 WARNING LIGHT DOUG DC9 DC931 3022065 WP TE FLAP SYST ILLUMINATED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 9330 47138 SPOILER/FLAP EXTENDED LIGHT ILLUMINATED WITH FLAPS SELECTED TO 15 DEGREES. CAPTAIN DECLARED A YELLOW EMERGENCY AND LAND ED WITH FLAPS AT 5 DEGREES. MAINTENANCE INSPECTED AND TESTED SYSTEM. DISCREPANCY COULD NOT BE DUPLICATED. AIRCRAFT RE TURNED TO SERVICE. 2 L 7 2 4F A6WE 1998052200639 19980522 00639 WP 1998 5 22 9809269613 1 19980515 A 2130 94840213 AMPLIFIER DOUG DC9 DC932 3022066 WP CABIN PRESS SYST FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 613NW 21193 3623 47438 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF, FLIGHT WAS RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE RE PLACED CABIN PRESSURE AMPLIFIER. OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998052200640 19980522 00640 WP 1998 5 22 9809279613 1 19980515 A 2130 93468946 RELAY DOUG DC9 DC932 3022066 WP GROUND CONTROL FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 613NW 47438 AUTO PRESSURIZATION SYSTEM FAILED AFTER TAKEOFF. FLIGHT RETURNED TO STL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED R2-4 GROUND CONTROL RELAY. OPERATIONAL CHECK NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998052200641 19980522 00641 SO 1998 5 22 COMA9810121 1 19980514 A 7603 0881824 SOLENOID EMB 120 EMB120RT SO LT NACELLE SHORTED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 241CA 120211 FLIGHT IDLE STOP SOLENOID CIRCUIT BREAKER TRIPPED. REPLACED SOLENOID. 2 L 7 2 4T RT A31SO 1998052200642 19980522 00642 SO 1998 5 22 COMA9810122 1 19980514 A 7921 1593731 HOSE EMB 120 EMB120RT SO RT OIL COOLER LEAKING A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 255CA 120238 LOW OIL PRESSURE WARNING ON RIGHT HAND ENGINE INFLIGHT SHUTDOWN. REPLACED OIL COOLER HOSE ASSEMBLY THAT WAS LEAKING DUE TO CHAFING DAMAGE. 2 L 7 2 4T RT A31SO 1998052200643 19980522 00643 EU 1998 5 22 WWMA9800084 1 19980503 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 245AE 340B245 DURING PREFLIGHT, THE FLIGHT ATTENDENTS EMERGENCY ARM LIGHT FAILED TO ILLUMINATE, REPLACED BULB. 2 L 7 2 4T RT A52EU 1998052200644 19980522 00644 EU 1998 5 22 WWMA9800083 1 19980505 A 6120 PROP CONTL UNIT SAAB SF340 340B 7860101 EU RT ENGINE FAILED A A WWMA E D ENGINE SHUTDOWN RETURN TO BLOCK O OTHER CR CRUISE 1 WP 15 313AE 340B313 RIGHT ENGINE PROPELLER RPM WAS UNCONTROLLABE AND STUCK AT 1100 RPM, SHUT DOWN THE ENGINE. MAINTENANCE CHECKED ENGINE RI GGING AND REINDEXED THE PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A52EU 1998052200645 19980522 00645 EU 1998 5 22 WWMA9800082 1 19980503 A 3350 GE307 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST NR NOT REPORTED 1 WP 15 256AE 340B256 EMERGENCY FLOOR LIGHT AT SEAT 8A FAILS TO ILLUMINATE, REPLACED BULB. 2 L 7 2 4T RT A52EU 1998052200646 19980522 00646 EU 1998 5 22 WWMA9800081 1 19980430 A 2611 WIRE SAAB SF340 340B 7860101 EU CARGO COMPT BROKEN A WWMA K NONE L NO TEST IN INSP/MAINT 1 WP 15 306AE 340B306 DURING MAINTENANCE CHECK, THE CARGO SMOKE DETECTOR FAILED TO TEST. FOUND BROKEN WIRES ON THE FWD CARGO SMOKE DETECTOR 9 WK. REPLACED CONNECTOR 9WKP1. 2 L 7 2 4T RT A52EU 1998052200647 19980522 00647 EU 1998 5 22 WWMA9800088 1 19980514 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 283AE 340B283 FLIGHT ATTENDANT EMERGENCY ARM LIGHT DOES NOT ILLUMINATE. REPLACED BULB. 2 L 7 2 4T RT A52EU 1998052200648 19980522 00648 EU 1998 5 22 WWMA9800086 1 19980516 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 313AE 340B313 DURING PREFLIGHT, THE FLIGHT ATTENDANTS EMERGENCY ARM FAILED TO ILLUMINATE, REPLACED BULB. 2 L 7 2 4T RT A52EU 1998052200649 19980522 00649 EU 1998 5 22 WWMA9800087 1 19980514 A 2121 EVCTA465A FAN SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 283AE 340B283 CREW SMELLED STRONG ELECTRICAL SMELL IN THE REAR OF THE AIRCRAFT. MAINTENANCE FOUND THE RIGHT RECIRCULATION FAN FROZEN AND CAUSING THE SMELL. REPLACED THE FAN. 2 L 7 2 4T RT A52EU 1998052200650 19980522 00650 NM 1998 5 22 98FDEA00352 1 19980516 A 2613 CONNECTOR BOEING 727 7272S2F 1384O81 NM AFT BODY DIRTY A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CL CLIMB 1 SO 25 203FE 22925 LWR AFT BODY OVERHEAT ILLUM'D DURING CLIMB W/LEFT PACK SUPPLIED BY NR 2 ENG, SWP PACK TO NR 1 ENG AND LIGHT STAYED ON, C LOSED NR 1 BAV AND LWR AFT BODY LIGHT WENT OUT. INSPECTED LEFT AND RIGHT OVHT DETECTOR LOOPS, NO DEFECT, CLEANED PLUG S ENSORS AND L/LOOP RAN NR 1 AND NR 2 ENG PER JRH W/BLEEDS ON, INSP'D AFT STAIRWELL NO LEAKS FOUND. PERF'D HI PWR ENG RUN PER JRH TO VERIFY OPS OF L/AFT BODY OVHT SENSORS AFTER CLEANING OF CONNECTORS. RAN ENG W/BLEEDS NR 1 AND 2 OPEN AND NR 1 AND 2 PACKS OPD, NO DEFECT, OK FOR SERVICE. 2 L 7 3 4F A3WE 1998052200652 19980522 00652 NM 1998 5 22 DL73K981020 1 19980512 A 3350 LIGHT 1864 BOEING 737 737232 1384475 NM R-1 SLIDE FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 325DL 23097 R-1 SLIDE LIGHT INOP ON TEST, REPLACE LIGHT. 2 L 7 2 4F RT A16WE 1998052200653 19980522 00653 NM 1998 5 22 DL76S981021 1 19980512 A 2530 COFFEEMAKER 811150417 BOEING 767 767332 1382001 NM FWD GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 134DL 148 25123 ELEC TYPE SMOKE WAS SEEN COMING FROM THE LIGHTING OVERHEAD IN THE FORWARD GALLEY, THE LIGHTS WERE TURNED OFF WITH SWITCH ES AND CIRCUIT BREAKER THE SMOKE DISSIPATED QUICKLY 2-3 MINS THIS OCCURRED 10 MINS PRIOR TO LDG. ALL OTHER IND WERE NML . DURING POST FLT INSP, THE COMPARTMENT ABOVE THE TWO FIRST CLASS COFFEE MAKERS WAS FOUND TO BE VERY HOT TO THE TOUCH. FOUND NR 1 COFFEEMAKER FAILED. REPLACED NR 1 COFFEEMAKER AND NR 2 AS PRECAUTION ALL CKS NML 2 L 7 2 4F RT A1NM 1998052200654 19980522 00654 NM 1998 5 22 DL72W981024 1 19980513 A 5320 WEB BOEING 727 727247 138408F NM BS 1214 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 FOUND AT C1 LETTER CK, RT TORQUE BOX WEB CRACKED AT UPPER END STA 1214, REPAIRED PER M/M 53-11-0 PG 832 RT TORQUE BOX WE B CRACKED .25 INCH AT UPPER LIGHTENING HOLE STA 1225. REPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1998052200655 19980522 00655 NM 1998 5 22 DL72S981025 1 19980512 A 5320 FITTING BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 FOUND AT A2 LETTER CH, 1.5 INCH CRACK LT INBD TENSION TIE BOLT CASTING. REPLACED FIITING PER DRAWING 65-17509 REV M AND COLD WORK AND SPOT FACE PER DRAWING 65-16350. 2 L 7 3 4F A3WE 1998052200656 19980522 00656 NM 1998 5 22 DL72W981026 1 19980513 A 5754 RIB BOEING 727 727247 138408F NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 FOUND ON C1 LETTER CK, L/E NOSE RIB CRACKED 1.25 INCH PAST, STOP DRILL, NR 5 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PE R MM 57-54-0. 2 L 7 3 4F A3WE 1998052200657 19980522 00657 NM 1998 5 22 DLM11981027 1 19980513 A 3510 ZH83416 OXYGEN LINE DOUG MD11 MD11 3023602 NM COCKPIT LEAKING A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 806DE 48477 IN CRUISE, FOUND CREW 02 BOTTLE EMPTY. FOUND FLEX LINE TO OBSERVER 02 REGULATOR LEAKING BADLY. REPLACED LINE AND REPLA CED 02 BOTTLE. LEAK CK GOOD. 2 L 7 3 4F RT A22WE 1998052200658 19980522 00658 NM 1998 5 22 DL72K981029 1 19980420 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 8 SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 NR 8 SLAT ACT ATTACH BRACKET CRACKED AT WEB. REPAIRED PER MM 57-20-21 P 812. 2 L 7 3 4F A3WE 1998052200659 19980522 00659 NM 1998 5 22 DL72K981030 1 19980504 A 5521 REAR SPAR BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 AN .375 INCH CRACK RT ELEVATOR REAR SPAR AT 2ND FROM O/B TAB, HINGE. REPLACED REAR SPAR UNDER EO 4-70183-3AD ME 02 AND ME 03. 2 L 7 3 4F A3WE 1998052200660 19980522 00660 NM 1998 5 22 DL72K981031 1 19980512 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 410DA 21222 DURING BUYBACK OF N/R 218, FOUND NUT PLATE EMBEDDED AT RT ELEVATOR LOWER SKIN. SKIN HAS .3125 INCH IN HOLE REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1998052200661 19980522 00661 NM 1998 5 22 DL72S981034 1 19980514 A 5400 S-DUCT BOEING 727 727232 1384082 NM NR 2 ENG INLET CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 489DA 21019 3 INCH SECTION OF S DUCT INNER SKIN DAMAGED/BENT BACK 3 FT. AFT OF INLET AT 1 OCLOCK POSITION, ERA 364794-14 DOUBLER. 2 L 7 3 4F A3WE 1998052200662 19980522 00662 NM 1998 5 22 DL73K981035 1 19980514 A 3350 BULB 81 BOEING 737 737232 1384475 NM RT OVERWING FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 324DL 23096 RT OVERWING EVACUATION HATCH OUTSIDE EMERG LIGHT INOP, REPLACE LAMP. 2 L 7 2 4F RT A16WE 1998052200663 19980522 00663 WP 1998 5 22 DLL17981037 1 19980515 A 3350 BATTERY PACK 20131A LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 766DA 44177 193H1207 SECTION OF EMERGENCY LIGHTS FAILED TO TEST. REPLACE BATT PACK. 2 L 7 3 4F A23WE 1998052200664 19980522 00664 NM 1998 5 22 DLM11981038 1 19980515 A 3244 TIRE DOUG MD11 MD11 3023602 NM NR 3 PUNCTURED A DALA K NONE C F.O.D. TO TAKEOFF 1 SO 27 801DE 216 48472 APPROXIMATELY 1 MINUTE AFTER TAKEOFF, TIRE PRESSURE LOW MESSAGE CAME ON. CONFIG PAGE SHOWED NR 3 MAIN DECREASING THROUG H 140 PSI. EVENTUALLY WENT TO 30 PSI WITH TIRE FAIL MESSAGE. REPLACED WHEEL ASSY. 2 L 7 3 4F RT A22WE 1998052200665 19980522 00665 NM 1998 5 22 DL72L981039 1 19980515 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND AT E1 LETTER CHECK, WEB CRACKED RT SIDE FWD UPPER LIGHTENING HOLE REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998052200666 19980522 00666 NM 1998 5 22 DL72L981041 1 19980515 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND ON E1 LETTER CK, 1.25 INCH CRACK INBD ATTACH CASTING FOR NR 4 L/E EDGE SLAT ACTUATOR. REPLACED ANGLE. 2 L 7 3 4F A3WE 1998052200667 19980522 00667 NM 1998 5 22 DL72L981042 1 19980515 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND ON E1 LETTER CK, 1 INCH CRACK INBD ATTACH CASTING NR 5 L/E SLAT ACTUATOR. REPLACED ANGLE. 2 L 7 3 4F A3WE 1998052200668 19980522 00668 NM 1998 5 22 DL72L981043 1 19980515 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FOUND AT E-1 LETTER CHECK, WEB CRACKED LT SIDE ABOVE LIGHTENING HOLE AFT STAIR AREA STA 1223. REPAIRED PER M/M53-11-0. 2 L 7 3 4F A3WE 1998052200669 19980522 00669 NM 1998 5 22 DL72L981044 1 19980516 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 21306 LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK CHECKS GOOD. 2 L 7 3 4F A3WE 1998052200670 19980522 00670 NE 1998 5 22 DLL17981046 2 19980516 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB21122* 54555 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SO 27 765DA 41818 14870 193H1206 14870 ON T/O, THE NR 1 ENG GAVE LOUD BANG. VIBES PEGGED OUT AT 5 PLUS AND EGT LT CAME ON. SHUT NR 1 ENG DOWN AND LANDED ATL. REPLACE NUMBER ONE ENGINE. 2 L 7 3 4F 4 F A23WE A12EU 1998052200671 19980522 00671 NM 1998 5 22 DL73K981048 1 19980515 A 3320 BV031120333 BULB HOLDER BOEING 737 737232 1384475 NM CABIN FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 324DL 23096 14870 SMELLS LIKE ELECTRICAL SMOKE COMING FROM OVERHEAD VENT NEAR ROW 17. FOUND FLOUR BULB CONTACTS BURNED AT ROW 18 RIGHT SI DE. REPLACED BALLAST AT ROW 17 FOR LAMPS 17-18 RIGHT SIDE. REPLACED FWD LAMP HOLDER DUE TO SAME BEING BURNED. NEW BUL B AND SHIELD INSTALLED. OPS CKS GOOD, (BELIEVE HOLDER WAS SOURCE OF SMOKE, BALLAST CHANGED AS PRECAUTION.) 2 L 7 2 4F RT A16WE 1998052200672 19980522 00672 NM 1998 5 22 DL72S981049 1 19980517 A 3340 81 BULB BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 499DA 21143 EMERGENCY LIGHT OUT AT RIGHT WING ROOT FAIRING. RELAMPED. 2 L 7 3 4F A3WE 1998052200673 19980522 00673 NM 1998 5 22 DL76L981050 1 19980517 A 3350 BATTERY CHARGER BPS73 BOEING 767 767332 1382001 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 173DN 12953 24800 DURING L/O, FOUND EMERGENCY AISLE EXIT SIGN INOP RT OVERWING AND AISLE ILLUMINATION LIGHT INOP. REMOVED AND BATTERY CHA RGER ASSY, M732. EMERGENCY LIGHTS OP CK GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS. 2 L 7 2 4F RT A1NM 1998052200674 19980522 00674 NM 1998 5 22 K3HA980074 1 19980514 A 3350 079123 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHT TRACK MISSING LENS COVER AND BULB BURNED OUT. REPLACED BULB (P/N 3071BPEGPL) (S/N NSN) AND RED LEN S COVER ON EMERGENCY PATH LIGHT STRIP PER MM 33-50-01. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998052200675 19980522 00675 NM 1998 5 22 K3HA980075 1 19980515 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 FOUND WIRE BROKEN AT BASE OF SOCKET ASSEMBLY AND INSTALLED NEW SOCKET (ACROSS FROM AFT GALLEY). OPS CHECKS GOOD. INSTA LLED NEW SOCKET ASSEMBLY TEST REF MM 33-50-01. OPS CHECK OK. 2 L 7 3 4F A3WE 1998052200676 19980522 00676 NM 1998 5 22 K3HA980076 1 19980517 A 3350 079123 LENS BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 FORWARD EMERGENCY PATH LIGHT, THIRD FROM FRONT MISSING LENS. REPLACED MISSING LENS REF MM 33-50-0, OPS CHECK OK. 2 L 7 3 4F A3WE 1998052200677 19980522 00677 SO 1998 5 22 COMA9810123 1 19980517 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 247CA 13838 1180 120225 SOME OF THE CABIN EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998052200678 19980522 00678 WP 1998 5 22 UPS98826640 1 19980511 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 622.500, REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998052200679 19980522 00679 WP 1998 5 22 UPS98826641 1 19980509 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, F/S 640 BETWEEN STR 26L-27L - SHEAR TIE HAS 3 CRACK. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-2-0 F IG 2B. 2 L 7 4 4F RT 4A25 1998052200680 19980522 00680 WP 1998 5 22 UPS98826642 1 19980509 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, F/S 640 BETWEEN STR 26R-27R - SHEAR TIE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT S HEAR TIE IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998052200681 19980522 00681 WP 1998 5 22 UPS98826643 1 19980511 A 5720 5769857 CLIP DOUG DC8 DC873F 302199F WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, LT WING L/E UPPER RIB ATTACH CLIP CRACKED AT STA XOLDI 6.225. REMOVED, FABRICATED, AND INSTALLED REP LACEMENT CLIP IAW SRM 51-1-20D AND DWG 5769857. 2 L 7 4 4F RT 4A25 1998052200682 19980522 00682 WP 1998 5 22 UPS98826644 1 19980511 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 585 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, LT WING L/E RIB CRACKED ON UPPER ARM BY AFT FASTENER STA XFS 585.000, REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998052200683 19980522 00683 WP 1998 5 22 UPS98826645 1 19980426 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1660-1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, INTERCOSTAL CRACKED, FS 1660 1680, L32R. REMOVED, FABRICATED NEW INTERCOSTAL IAW DOUGLAS DWG 5613064 . ALODINED AND PRIMED AND INSTALLED IT IAW DC8 SEM 51 1 8 AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200684 19980522 00684 WP 1998 5 22 UPS98826646 1 19980414 A 5320 FORMER DOUG DC8 DC871F 302199D WP BS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, AFT PIT FORMER CORRODED STA 1080, L36 TO 35L. REMOVED CORROSION, FABBED STRAP REPAIR AND SAM IAW REO 04666 AND DC. 2 L 7 4 4F RT 4A25 1998052200685 19980522 00685 WP 1998 5 22 UPS98826647 1 19980414 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1230 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, STA 1230 LONGERON 35 RIGHT TO LONGERON 36 Z FITTING CORRODED. REMOVED FITTING CUT AND INSTALLED NEW FITTING WITH SPLICES IAW DC8 SRM 53 2 0 AND 51 1 8 AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200686 19980522 00686 WP 1998 5 22 UPS98826648 1 19980415 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, STA 1690 LONGERON 29 RIGHT END FITTING CRACKED AND CORRODED. REMOVED FITTING DRILLED AND INSTALL ED NEW ONE IAW DC8 SRM 51 3 0, 5 1 1 20D, AND 51 1 24. 2 L 7 4 4F RT 4A25 1998052200687 19980522 00687 WP 1998 5 22 UPS98826649 1 19980416 A 5311 FRAME DOUG DC8 DC871F 302199D WP CARGO COMPT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, FUSELAGE STATION LONGERON 35 RIGHT FRAME HAS CORROSION AT NUT PLATE HOLES. FABRICATED FRAME SPLCI E IAW DC8 SRM 53 2 0, ALDOINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200688 19980522 00688 WP 1998 5 22 UPS98826651 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, MAIN CABIN STATION 980 AND LONG 22R FUSELAGE BRACE FITTING IS CRACKED IN TWO PLACES. REMOVED DAMAGED FITTING, LOCATED, DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200689 19980522 00689 WP 1998 5 22 UPS98826652 1 19980417 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, MAIN CABIN STATION 940 AND LONG 22L FUSELAGE FRAME FITTING CORRODED. REMOVED FITTING FOR FABRICATION OF NEW FITTING SEE OPS 50018 FOR FABRICATION ALODINED AND PRIMED FITTING IAW DC8 SRM 51 MAT ID FOR WEB DOUBLER IAW DC8 SRM 53 4 1 .032 2024 T 3. FABRICATED REPAIR IAW DC8 EO DC8 5350 7876. ALODINED AND PRIMED DOUBLER IAW DC8 SRM 51 1 8. INSTALLED FITTING AND DOUBLER IAW DC8 SRM 51 1 20D AND 51 1 21. 2 L 7 4 4F RT 4A25 1998052200690 19980522 00690 WP 1998 5 22 UPS98826653 1 19980414 A 5720 ANGLE DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, RIGHT HAND WING REAR SPAR I/B AILERON I/B CENTER HINGE FITTING ATTACH ANGLE BENT AND CRACKED. REMOVE D CRACKED ANGLE FABBED NEW ONE ON TPA 1003 REV A INSTALLED IAW DC8 SRM 51 3 0. 2 L 7 4 4F RT 4A25 1998052200691 19980522 00691 WP 1998 5 22 UPS98826654 1 19980413 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, LT ELEVATOR LOWER SKIN CORRODED AROUND FASTENER AT CLOSING CHANNEL STA XE 310. MRR FILED OPEN NO COR ECTIVE ACTION. 2 L 7 4 4F RT 4A25 1998052200692 19980522 00692 WP 1998 5 22 UPS98826655 1 19980412 A 5311 RIB DOUG DC8 DC871F 302199D WP BS 960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, INNER RIB BETWEEN MLG DOORS FS 960 HAS CRACKS. REMOVED RIB FABBED NEW ONE ON DAC DWG 5616306, INSTAL LED IAW DC8 SRM 51 1 4 AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200693 19980522 00693 WP 1998 5 22 UPS98826656 1 19980414 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 70-280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, STA 45 TRACK A CORROSION REMOVED FLOOR PANEL 1 AFS 70 TO FS 280. REMOVED CORRODED SEAT TRACK A F S 570 TO FS 280. PUT NEW SEAT TRACK, DRILLED HOLES IAW DC8 SRM 5 1 1 24. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INST ALLED NEW SEAT TRACK FS 70 TO FS 280 IAW DC8 SRM 51 3 0. INSTALLED FLOOR PANEL IAW D C8 SRM 51 3 0. 2 L 7 4 4F RT 4A25 1998052200694 19980522 00694 WP 1998 5 22 UPS98826657 1 19980419 A 5347 PLUG DOUG DC8 DC871F 302199D WP BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, SEAT TRACK PLUG CORRODED STA 680 BL25R. REMOVED AND REPLACED PLUG IAW DC8 SRM 53 3 2, 51 3 0, 51 1 8 . 2 L 7 4 4F RT 4A25 1998052200695 19980522 00695 WP 1998 5 22 UPS98826658 1 19980419 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 758 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, FITTING CRACKED STA 758 BL50R IN MAIN CARGO. REMOVED FITTING INSTALLED NEW ONE IAW DC8 SRM, 51 3 0 A ND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200696 19980522 00696 WP 1998 5 22 UPS98826659 1 19980418 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 834 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, MAIN CABIN FRAME FITTING CRACKED AT STA 834 AND LONG 22R UNDER FLOOR. REMOVED DAMAGED FITTING DRILLE D AND REAMED HOLES INTO NEW FITTING IAW DC8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200697 19980522 00697 WP 1998 5 22 UPS98826662 1 19980414 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, MAIN CABIN FITTING AT STA 781 LONG 13L CRACKED. DRILLED UP NEW FITTING IAE DC8 SRM 51 1 24. INSTALL ED FITTING IAW DC8 SRM 51 1 20D. REF TO OP 50026 FOR FITTING FAB. 2 L 7 4 4F RT 4A25 1998052200698 19980522 00698 WP 1998 5 22 UPS98826663 1 19980414 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, AFT PIT STA 1150 AND LONG 33R AND 34R Z FITTING IS CRACKED. REMOVED Z FITTING FABBED REPAIR ANGLE AN D FILLERS IAW DC8 SRM 53 2 0 FIG 2. ALODINED AND PRIMED REPAIR ANGLES AND FILLER IAW DC8 SRM 51 1 8. CUT NEW Z FITTING AT LOMATION AS SPECFIFIED IN DC8 SRM 53 2 0 FIG 2A. INSTALLED Z FITTING REPAIR ANGLES AND FILLER IAW DC8 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200699 19980522 00699 WP 1998 5 22 UPS98826665 1 19980423 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, FRAME CORRODED AT CAP STALL 1060 L35 36R. FABBED REPAIR STRAP AND INSTALLED IAW REO 04646. INSTALLE D STRAP IAW 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200700 19980522 00700 WP 1998 5 22 UPS98826667 1 19980419 A 5320 MEMBRANE DOUG DC8 DC871F 302199D WP BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, CORROSION/CRACKED REAR CABIN FLOOR MAIN FRAME SUPPORT CLIP AFT ACCESS RY COMP. RT CRSP STA 1580 REAR SIDE OF FLOORBEAM REMOVED CLIP AND FABBED NEW SUPPORT CLIP ALODINED AND PRIMED IAW DC8 SRM 51. INSTALLED CLIP IAW DC8 SRM 51. 2 L 7 4 4F RT 4A25 1998052200701 19980522 00701 WP 1998 5 22 UPS98826671 1 19980420 A 5720 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, ANGLE REPAIR CRACKED FOR STIFFENER RUNNING BETWEEN NR 1 AND NR 2 RIBS AT LEFT HAND LEADING EDGE F UEL TANK. FABRICATED NEW REPAIR ANGLE 7075 T6 IAW DC8 SRM 57 2 0. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED R EPAIR IAW DC8 SRM 57 2 0. 2 L 7 4 4F RT 4A25 1998052200702 19980522 00702 WP 1998 5 22 UPS98826672 1 19980415 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, FITTING AT LONGERON 20 RIGHT FRAME STATION 1230 CRACKED. LOCATED AND DRILLED NEW FITTING 750419 502 IAW DC8 SRM 51 1 24. INSTALLED FITTING IAW DC8 SRM 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200703 19980522 00703 WP 1998 5 22 UPS98826673 1 19980416 A 5751 SKIN DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, RIGHT OUTBOARD AILERON TOP LEADING EDGE AREA AND SKIN CRACKED ON OUTBOARD END. REPAIRED SKIN IAW REO 04658 REO ATTACHED TO UPS NR 542301. 2 L 7 4 4F RT 4A25 1998052200704 19980522 00704 WP 1998 5 22 UPS98826675 1 19980414 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, LONGERON 11 RIGHT TIE FITTING FOR LONGERON CRACKED STA 680. DRILLED AND REAMED NEW FITTING IAW DC 8 SRM 51 1 24. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20D AND DC8 SRM 51 3 0. 2 L 7 4 4F RT 4A25 1998052200705 19980522 00705 WP 1998 5 22 UPS98826677 1 19980413 A 5522 SKIN DOUG DC8 DC871F 302199D WP LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, LEFT ELEVATOR UPPER SKIN HAS 1 CRACK 2 INCHES AFT OF SPAR AT STA XE77 STOP DRILLED CRACK. FAB REPAIR IAW DC8 SRM 55 2 1 FIG 7. ALODINED AND PRIMED IAW DC8 SRM 51 1 8 AND INSTALLED IAW DC8 SRM 51 1 21A. 2 L 7 4 4F RT 4A25 1998052200706 19980522 00706 WP 1998 5 22 UPS98826678 1 19980413 A 5320 FITTING DOUG DC8 DC871F 302199D WP AFT FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, LONGERON END FITTING CRACKED, 27 LEFT AT AFT PRODUCTION SPLICE. INSTALLED NEW FITTING IAW DC8 SRM 51 1 24 AND 51 1 20D AND 51 1 21 A ND 51 3 0. 2 L 7 4 4F RT 4A25 1998052200707 19980522 00707 WP 1998 5 22 UPS98826679 1 19980417 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, CABIN FLOORBEAM STATION 8 RBL 26 HAS CORROSION AND UPPER FWD FLANGE LOWER SURFACE AT ATTACH LUG BO LT BROKEN OFF IN LUG. FABRICATED REPAIR STRAP IAW REO 04644. INSTALLED REPAIR STRAP IAW DC 8 SRM 51 1 20D BAD REO 046 44. REF TO UPS NR 542659 FOR COPY OF REO. 2 L 7 4 4F RT 4A25 1998052200708 19980522 00708 WP 1998 5 22 UPS98826681 1 19980416 A 5751 SKIN DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, RIGHT AILERON UPPER SKIN OUTBOARD END CRACKED. ROUTED OUT CRACK, FABBED PRIMED AND INSTALLED DOUB LER IAW REO 04658. 2 L 7 4 4F RT 4A25 1998052200709 19980522 00709 WP 1998 5 22 UPS98826683 1 19980416 A 5320 CHANNEL DOUG DC8 DC871F 302199D WP LT MLG WW CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, CORRODED U CHANNEL AT UPPER PRESSURE PANEL. REPAIRED PER REO 04626 ON UPS NR 542514. 2 L 7 4 4F RT 4A25 1998052200710 19980522 00710 WP 1998 5 22 UPS98826684 1 19980419 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 717 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, MAIN CARGO FITTING CRACKED AT STA 717, LONGERON 22 RIGHT. REMOVED FITTING FABBED NEW ONE IAW DAC DWG 3616947. INSTALLED IT IAW DC8 SRM 51 1 15 AND 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200711 19980522 00711 WP 1998 5 22 UPS98826685 1 19980416 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, RIGHT INBOARD AILERON UPPER SKIN CRACKED AT OUTBOARD END. FABBED REPAIR STRAP TREATED AND INSTALL ED IAW REO 04638 REV A. 2 L 7 4 4F RT 4A25 1998052200712 19980522 00712 WP 1998 5 22 UPS98826688 1 19980414 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, FRAME TO FLOOR FITTING AT FUSELAGE STATION 35 RIGHT SIDE IS CORRODED ON AFT FACE. REMOVED 459764 3 1 ATTACHED FITTING AT FS 35 RECEIVED NEW 4597643-1. ATTACHED FITTING FROM STORES DRILLED 4597643-1 ATTACHED FITTING I AW DC8 SRM 51 1 24. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED 4597643-1, FITTING IAW DC8 SRM 51 3 0 AND DC8 SR M 51 1 20D. 2 L 7 4 4F RT 4A25 1998052200713 19980522 00713 NM 1998 5 22 98UAL900179 1 19980505 A 3230 RETRACT MECH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LANDING GEAR MALFUNCTIONED A UALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 29 658UA 27113 INITIAL LANDING GEAR EXTENSION RENDERED AMBER TAIL SKID AND GEAR LIGHTS AND EICAS GEAR DISAGREE MESSAGE. DID GO-AROUND, RECYCLED GEAR. SUBSEQUENT GEAR EXTENSION NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1998052200714 19980522 00714 NM 1998 5 22 98UAL900180 1 19980507 A 3150 EICAS BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT ACTIVATED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 777UA 26916 FLIGHT RETURN TO IAD, DO TO SPOILER EICAS (ENGINE INDICATION AND ALERT SYSTEM) MESSAGES. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998052200716 19980522 00716 NM 1998 5 22 98UAL900182 1 19980510 A 3350 BATTERY AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 801UA 686 CABIN EMERGENCY LIGHTS FAILED TEST. ESPU BITE SHOWS BATTERY FAULT. REPLACED BATTERY. 2 L 7 2 4F 4 F RT A28NM E40NE 1998052200717 19980522 00717 NM 1998 5 22 98UAL900183 1 19980512 A 2741 STAB TRIM IND BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT ACTIVATED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 605UA 21866 ABORTED TAKEOFF AT 100 KNOTS DUE TO STABILIZER TRIM INDICATION. 2 L 7 2 4F 4 F RT A1NM E3NE 1998052200718 19980522 00718 NM 1998 5 22 98UAL900185 1 19980512 A 2810 FUEL TANK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CENTER TANK LEAKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7287U 21565 EXTERIOR OF CENTER FUEL TANK HAS STRONG ODOR OF FUEL. FOUND EVIDENCE OF FUEL AT REAR SPAR WEB. *S/D* FOUND FUEL SEEP AT LOWER EDGE OF CENTER SECTION REAR SPAR AT APPROXIMATELY LBL 7.50. PERFORMED INTERIM REPAIR AND LEAKED CHECKED OK. T HE AREA WILL BE CHECKED AT 50 HOUR INTERVALS FOR THREE TIMES. PERMANENT REPAIR WILL BE MADE AT THE NEXT HEAVY MAINTENAN CE VISIT. 2 L 7 3 4F 4 F A3WE E2EA 1998052200719 19980522 00719 NM 1998 5 22 98UAL900186 1 19980505 A 5330 SKIN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE R 1 DOORWAY CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7288U 21566 APPROXIMATELY THREE INCH CRACK IN FUSELAGE SKIN AT LOWER AFT RADIUS OF DOOR 1R FRAME. 2 L 7 3 4F 4 F A3WE E2EA 1998052200720 19980522 00720 NE 1998 5 22 98UAL900187 2 19980512 A 7261 LP 5/6 LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE COKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 7271U 21418 NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AT CRUISE POWER. LIGHT OUT AT IDLE. RETURNED TO ORD. *S/D* CORRECTED SYSTEM FROM FUEL TO OIL. THE OIL FILTER BYPASS LIGHT ILLUMINATION WAS CAUSED BY COKING. BLOWING OUT THE LP 5 AND LP 6 LINES AND CLEANING THE OIL SCREEN SOLVED THE PROBLEM. 2 L 7 3 4F 4 F A3WE E2EA 1998052200721 19980522 00721 NM 1998 5 22 98UAL900188 1 19980512 A 3350 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7461U 21915 CENTER EMERGENCY EXIT SIGN LIGHTS INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1998052200722 19980522 00722 NM 1998 5 22 98UAL900189 1 19980512 A 3350 SIGN BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7283U 21561 FORWARD FACE OF AFT DROP CEILING EMERGENCY EXIT SIGN INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1998052200723 19980522 00723 NM 1998 5 22 98UAL900190 1 19980514 A 2560 LIGHT GULTON INDUS 81020401 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 2R DOOR SLIDE ILLUMINATED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 517UA 24861 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT AT DOOR 2R INOP. RELAMPING DID NOT HELP. *S/D* PROBLEM DUPLICATED BY TAPPING O N RH GIRT BAR SENSOR S10221 WHICH MADE SLIDE LIGHT COME ON. REPLACED S10221 PER MM AND OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998052200724 19980522 00724 NE 1998 5 22 98UAL900191 2 19980511 A 7230 ENGINE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 STALLED A UALA O OTHER Y ENGINE STOPPAGE IN INSP/MAINT 1 WP 29 179UA 25158 724420 AFTER FIRST 3 ENGINES WERE STARTED NR 1 ENGINE DID AN AUTO SHUTDOWN. *S/D* FLIGHT DATA RECORDER INFORMATION INDICATES THE NUMBER 1 ENGINE EXPERIENCED AN OFF-IDLE STALL WHICH PREVENTED THE ENGINE FROM REACHING STABILIZED IDLE. THE ENGINE SLOWLY DECELERATED TO A SUB IDLE CONDITION WHICH RESULTED IN ENGINE FLAME-OUT AND TAILPIPE FIRE. INSTALLED A ELECTRONIC ENGINE CONTROL WITH UP-GRADED SOFTWARE DESIGNED TO ALLEVIATE OFF-IDLE STALLS. 2 L 7 4 4F 4 F RT A20WE E24NE 1998052200725 19980522 00725 NM 1998 5 22 98UAL900192 1 19980512 A 3350 3F17664501 LIGHT BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 151UA 23736 E-ZONE EEL LIGHTS FLICKER. *S/D* EMI PICKED UP ON THE OFF CONTROL LINE. INSERT EMI FILTER PER SERVICE TIP IN MM 33-51 -12 PAGE 200/A. 2 L 7 4 4F 4 F RT A20WE E3NE 1998052200726 19980522 00726 NM 1998 5 22 98UAL900193 1 19980514 A 3244 TIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LANDING GEAR BLOWN A UALA O OTHER O OTHER LD LANDING 1 WP 29 580UA 26698 LANDED UNDER AMBER ALERT DUE TO A SUSPECTED BLOWN TIRE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998052200727 19980522 00727 NM 1998 5 22 98UAL900194 1 19980514 A 5620 WINDOW PILKINGTON PA65457914AS BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DAMAGED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 555UA 11242 26647 RETURNED TO FIELD SHORTLY AFTER TAKEOFF DUE TO LOOSE PASSENGER WINDOW FRAME. *S/D* BOTH PASSENGER WINDOWS AT ROW SIX O N THE RIGHT HAND SIDE OF FUSELAGE EXHIBITED DAMAGE DUE TO MISPLACEMENT OF GROUND POWER UNIT ON RAMP PRIOR TO DEPARTURE. ACCOMPLISHED VISUAL INSPECTION OF SURROUNDING STRUCTURE AND PERFORMED CONDUCTIVITY CHECK OF FUSELAGE SKIN WITH NO DEFEC TS NOTED. BOTH DISCREPANT WINDOWS REPLACED WITH NEW WINDOW ASSEMBLIES PER THE MM. 2 L 7 2 4F 4 F RT A2NM E17NE 1998052200728 19980522 00728 EU 1998 5 22 98UAL900195 1 19980514 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 433UA 589 EMERGENCY LIGHT SYSTEM TEST FAILED. REPLACED FORWARD LEFT EPS UNIT. 2 L 7 2 4F 4 F RT A28NM E40NE 1998052200729 19980522 00729 WP 1998 5 22 ABXA9800451 1 19980513 A 7920 779606 RELIEF VALVE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 851AX 45940 643743 AFTER TAKEOFF NR 2 ENGINE OIL QUANTITY DROPPED FROM 9.1 GAL TO 4 GAL AND WAS DECREASING. SHUT NR 2 ENGINE DOWN. ENGINE WINDMILLED FOR ONE HOUR. OIL PRESSURE STAYED AT 35 PSI UNTIL THE LAST 15-20 MINUTES THEN DROPPED TO 11-15. REPLACED O IL PRESSURE RELIEF VALVE. 2 L 7 4 4F 4 F 4A25 1E8 1998052200730 19980522 00730 WP 1998 5 22 ABXA9800452 1 19980513 A 7931 41800141 TRANSMITTER DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 824AX 1041 46141 671269 IN CLIMB WITH MCT SET, NR 1 ENGINE OIL PRESSURE DROPPED TO APPROXIMATELY 37 PSI WITH FLUCTUATION OF PLUS AND MINUS, MINU S 7 PSI. WHEN THROTTLE MOVED TO IDLE, OIL PRESSURE DROPPED TO 33 PSI. ENGINE SHUT DOWN. ENGINE WINDMILLED FOR APPROX 3.4 HRS WITH OIL PRESSURE ABOVE 14 PSI AND FOR 5 MIN AT 4 PSI DURING APPROACH. INSPECTED MAIN OIL FILTER. CHECKED GOOD . REPLACED FILTER. REPLACED OIL PRESSURE TRANSMITTER. ENGINE OPS AND LEAKED CHECKED GOOD ON GROUND RUN. 2 L 7 4 4F 4 F 4A25 1E8 1998052200731 19980522 00731 WP 1998 5 22 ABXA9800453 1 19980514 A 3350 60030451 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 904AX 1187 47040 CABIN EMERGENCY LIGHTS WOULD NOT TEST DURING PREFLIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1998052200732 19980522 00732 NM 1998 5 22 DL76S981053 1 19980518 A 5754 114T410135 SKIN BOEING 767 767332 1382001 NM NR 1 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 137DL 25306 NR 1 L/E SLAT T/E WEDGE WAS FOUND TO HAVE THE UPPERR SKIN DAMAGED AT A LOCATIONS WHICH IS APPROX 24 INCHES FROM THE OUTB D EDGE AND RUNS APPROX 2 INCHES FWD FROM THE AFT EDGE. REPAIRED PER ERA 364811-14AD. 2 L 7 2 4F RT A1NM 1998052200733 19980522 00733 WP 1998 5 22 DLL14981054 1 19980518 A 5320 LS13112 PRESSURE DECK LKHEED 1011 1011385115 5265015 WP BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 FUSELAGE HORIZ PRESSURE DECK PANEL WAS FOUND TWO CRACKS, ONE APPROX 1 LONG AT RBL 102 JUST AFT OF FS378. THE SECOND IS APPROX 0.5 LONG AT THE SAME FRAME CUTOUT. REPAIRED PER ERA 331636-14. 2 L 7 3 4F A23WE 1998052200734 19980522 00734 WP 1998 5 22 DLL14981055 1 19980518 A 5330 1505394175 SKIN LKHEED 1011 1011385115 5265015 WP BS 157 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 FUSELAGE SKIN HAS MULTIPLE LIGHTNING STRIKES AND EXISTING DENTS. THE SKIN PANEL WILL BE REPLACED. REPAIRED PER 273391- 14 REV B. 2 L 7 3 4F A23WE 1998052200735 19980522 00735 WP 1998 5 22 DLL14981056 1 19980518 A 5712 1527031358 RIB LKHEED 1011 1011385115 5265015 WP WS 503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 RT WING IWS 503 UPPER CAP WAS FOUND CRACKED AND WAS REPLACED. REPAIRED/REPLACED PER ERA 331644-14. 2 L 7 3 4F A23WE 1998052200736 19980522 00736 WP 1998 5 22 DLL14981057 1 19980518 A 5730 1527139 SKIN LKHEED 1011 1011385115 5265015 WP WS 570 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 WHILE ACCOMPLSHING INSPECTION PER 7-70958-12AD A CRACK WAS FOUND ON THE RT WING LWR SURFACE AT IWS 570, STRG 10. REPAIR ED PER ERA 331660-14AD. 2 L 7 3 4F A23WE 1998052200737 19980522 00737 WP 1998 5 22 DLL14981058 1 19980518 A 5320 1641606102 DOUBLER LKHEED 1011 1011385115 5265015 WP BS 1363 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 LWR END OF THE SKIN DOUBLER JUST AFT OF FS 1363 WAS DAMAGED DUE TO TOOLING. REPAIRED PER ERA 331666-14AD. 2 L 7 3 4F A23WE 1998052200738 19980522 00738 WP 1998 5 22 DLL14981059 1 19980518 A 5312 1502220111 BULKHEAD CAP LKHEED 1011 1011385115 5265015 WP BS 1363 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 FOUR HOLES AT LBL 25.5 AND THREE HOLES AT 42.5 WERE MISDRILLED DURING FABRICATION OF THE REPLACEMENT LWR CAP OF THE FS 1 363 BLKHD. REPAIRED PER ERA 331683-14AD. 2 L 7 3 4F A23WE 1998052200739 19980522 00739 WP 1998 5 22 DLL14981060 1 19980518 A 5312 1502220105 BULKHEAD WEB LKHEED 1011 1011385115 5265015 WP BS 1363 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1739D 193C1237 GOUGE FOUND ON THE FS 1363 BLKHD WEB AT LBL 56.5 AND WL 168. REPAIRED PER ERA 331685-14AD. 2 L 7 3 4F A23WE 1998052200740 19980522 00740 NM 1998 5 22 DL72S981061 1 19980518 A 5311 FRAME BOEING 727 727232 1384082 NM BS 784 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 CRACKS FOUND IN THE INBD FLANGES OF BOTH LT AND RT OVER WING EXIT FRAMES AT FS 783.95. REPAIRED PER ERA 331706-14AD. 2 L 7 3 4F A3WE 1998052200741 19980522 00741 NM 1998 5 22 DL72S981062 1 19980518 A 5320 FITTING BOEING 727 727232 1384082 NM BS 1183 WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 SIX FASTENER HOLES WERE FOUND WORN OUT OF ROUND. THE HOLES ARE AT FS 1183 TORQUE BOX AREA AND ARE COMMON TO THE AFT INB D AND OUTBD TENSION TIE FITTINGS. REPAIRED PER ERA 331729-14. 2 L 7 3 4F A3WE 1998052200742 19980522 00742 NM 1998 5 22 DL72S981063 1 19980518 A 5330 65562312 SKIN BOEING 727 727232 1384082 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 A 1.5 INCH CRACK WAS FOUND IN THE UPPER HINGE CUTOUT DOUBLER OF THE R1 DOOR. REPAIRED PER ERA 331703-14. 2 L 7 3 4F A3WE 1998052200743 19980522 00743 NM 1998 5 22 DL72S981064 1 19980518 A 5330 65545831 SKIN BOEING 727 727232 1384082 NM BS 1158 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 DURING ACCOMPLISHMENT OF 4-69078-3AD AN EXISTING REPAIR WAS FOUND TO BE CORRODED. REPAIRED PER ERA 331732-14. 2 L 7 3 4F A3WE 1998052200744 19980522 00744 NM 1998 5 22 DL72W981065 1 19980518 A 5312 BULKHEAD WEB BOEING 727 727247 138408F NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 CRACKS WERE DISCOVERED IN THE FS 178 BLKHD WEB AT WL 200 ANDLBL 5.8. REPAIRED PER ERA 331668-14. 2 L 7 3 4F A3WE 1998052200745 19980522 00745 NM 1998 5 22 DL72W981066 1 19980518 A 5330 651842012 SKIN BOEING 727 727247 138408F NM BS 300 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 THE SKIN AROUND THE FWD LAV PAN WAS FOUND CORRODED AROUND THE AFT LWR CORNER OF THE CUTOUT. REPAIRED PER ERA 331722-14. 2 L 7 3 4F A3WE 1998052200746 19980522 00746 NM 1998 5 22 DL72S981068 1 19980518 A 5754 SKIN BOEING 727 727232 1384082 NM NR 5 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 NR 5 L/E FLAP CRACKED AT I/B GATE HINGE CUTOUT O/B SIDE. REPAIRED PER M/M 57-53-0. 2 L 7 3 4F A3WE 1998052200747 19980522 00747 NM 1998 5 22 DLM88981069 1 19980518 A 3244 TIRE MD88M DOUG MD88 MD88 3023688 NM NR 1 MLG BLOWN A DALA K NONE O OTHER TO TAKEOFF 1 SO 27 909DL 49540 JUST PRIOR TO ROTATION WE HEARD A LOUD BANG INST NORMAL. CONTINUED T/O. ON CLIMB-OUT NOTIFIED ANOTHER AIRCRAFT MAIN TI RE SHREADED ON T/O ROLL NEAR ROTATION. FOUND NUMBER 1 MAIN TIRE AT 0 PSI AND NR 2 AT 200PSI. R/E BOTH 1 AND 2 MAIN ASS EMBLIES. INSTALLED SPACERS. 2 L 7 2 4F RT A6WE 1998052200748 19980522 00748 NM 1998 5 22 DL72S981070 1 19980518 A 5210 SKIN BOEING 727 727232 1384082 NM R-1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 542DA 22391 FOUND ON C-2 CHECK, TPA 1 CRACK IN R-1 DOOR SKIN AT FWD EDGE JUST ABOVE LOWER HINGE CUTOUT. INSTALLED DOUBLER PER ERA 3 64822-14 AND M/M 52-11-01. 2 L 7 3 4F A3WE 1998052200749 19980522 00749 NM 1998 5 22 SCNA98045 1 19980517 A 3350 900853A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING LINE CHECK, FOUND LEFT EMERGENCY LIGHT ON AFT PORTION OF WING ROOT FAIRING INOPERATIVE. REMOVED AND REPLACED BAT TERY PACK FOR LEFT AFT EMERGENCY EGRESS LIGHT. OPERATIONAL CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998052200750 19980522 00750 NM 1998 5 22 SCNA98046 1 19980513 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 222558 DURING AN OVERNIGHT LINE CHECK, A FORWARD THREE FOOT SECTION OF FLOOR TRACK LIGHTING AT THE FORWARD GALLEY WAS FOUND TO BE INOPERATIVE. REPAIRED A BROKEN WIRE AND THE EMERGENCY FLOOR TRACK LIGHTING OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1998052200751 19980522 00751 NM 1998 5 22 SCNA98047 1 19980510 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 222558 DURING AN OVERNIGHT LINE CHECK, THE AFT EMERGENCY EXIT BULLNOSE LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK FOR THE AFT EMERGENCY EXIT BULLNOSE LIGHT. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998052200752 19980522 00752 NM 1998 5 22 P5CA9800774 1 19980515 A 7711 60BJBB1A6 TRANSMITTER BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE EPR INOPERATIVE A P5CA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 23 857FT 20246 662258 NR 2 ENGINE WOULD NOT MAKE TAKEOFF THRUST. TEMP 912 DEGREES 1:08 EPR. ABORTED TAKEOFF. REMOVED AND REPLACED EPR TRANSM ITTER REF MM 77-11-00. REMOVED AND REPLACED T7 LINE AS PRECAUTION REF MM 77-12-00. REQ OPS CHECK. OPS CHECK SATISFACT ORY PER MM 77-00-00. 2 L 7 4 4F 4 F A20WE E20EA 1998052200753 19980522 00753 NE 1998 5 22 P5CA9800775 2 19980515 A 7230 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 MALFUNCTIONED A P5CA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION LD LANDING 1 WP 23 852FT 19757 662811 ON LANDING, NR 2 ENGINE OIL PRESSURE LIGHT CAME ON, EGT ROSE IMMEDIATELY. SHUT DOWN ENGINE. EGT WAS 938 DEGREES PER M/ M 71-00-00 PAGE 216 AREA B OVER TEMPERATURE. ACCOMPLISHED VISUAL INSPECTION PER M/M 72-00-00, M/M 72-00-43 PAGE 115, 71 -00-42, 71-00-46 AND 78-34-08. NO DISCREPANCIES NOTED. SUSPECT STALL IN REVERSE PLACARDED THRUST REVERSER PRECAUTIONAR Y. AIRCRAFT SCHEDULED FOR BORESCOPE WITHIN 80 HOURS. 2 L 7 4 4F 4 F A20WE E20EA 1998052200754 19980522 00754 NM 1998 5 22 VNAA9805008 1 19980512 A 7603 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT LACK OF LUBE A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 433JS 3047 DURING TAXI PRIOR TO TAKEOFF, THE LEFT HAND POWER LEVER WOULD NOT ADVANCE ABOVE THE FLIGHT IDLE POSITION, WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBRICATED THE POWER LEVER CONTROL LOCK GATE IN ACCORDAN CE WITH DORNIER MAINTENANCE MANUAL 76-11-06. OPERATION CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVI CE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998052200755 19980522 00755 NM 1998 5 22 BJNA9803004 1 19980403 A 2612 655280945 FIRE DETECTOR BOEING 737 737214 138446R NM LT ENGINE DEFECTIVE A BJNA K NONE J WARNING INDICATION UK UNKNOWN 1 WP 11 457TM 20156 LEFT ENGINE OVERHEAT LIGHT ILLUMINATES INTERMITTENTLY. REMOVED AND REPLACED FIRE DETECTION ACCESSORY UNIT PER bMM20-10- 111, GROUND TEST NORMAL PER BMM 26-11-0. (EKO) (X). 2 L 7 2 4F A16WE 1998052200756 19980522 00756 NM 1998 5 22 BJNA9803005 1 19980406 A 2612 6937307112 CONTROL MODULE BOEING 737 737214 138446R NM NR 1 ENGINE DEFECTIVE A BJNA K NONE N FALSE WARNING CR CRUISE 1 WP 11 457TM 20156 NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN-FLIGHT INTERMITTENTLY. REMOVED AND REPLACED ENGINE AND APU FIRE CONTROL MODUL E, RAN ENGINE, NO LEAKS FOUND. CHECKED WIRING, ALL OK. REF MM 26-21-41, AND 26-21-0. (X) 2 L 7 2 4F A16WE 1998052200757 19980522 00757 NM 1998 5 22 BJNA9803006 1 19980407 A 2613 878581 FIRE LOOP BOEING 737 737214 138446R NM LT ENGINE CHAFED A BJNA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 LEFT ENGINE OVERHEAT LIGHT COMES ON INTERMITTENTLY. DISCOVERED CHAFED WIRES ON FIRE LOOP CONNECTORS, LT ENGINE, AFT. R EMOVED AND REPLACED CONNECTORS PER BSWPM 20-62-16, OPS CHECKS NORMAL. (X) 2 L 7 2 4F A16WE 1998052200758 19980522 00758 NM 1998 5 22 ASAA9810028 1 19980413 A 3234 BEARING BOEING 737 737290C 138448V NM SELECTOR VALVE DRY A ASAA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 01 742AS 23136 ANC - FLT 52 - AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE TO OFF OR DOWN POSITION. AIRCRAFT RETURNED TO ANC AND LANDED W ITHOUT INCIDENT. INSPECTED AND FOUND GEAR SELECTOR VALVE CONTROL QUADRANT UPPER BEARING DRY, LUBRICATED SAME. INSPECTE D CABLE RUN AND PULLEYS FROM GEAR HANDLE TO SELECTOR VALVE, NO DEFECTS NOTED. LUBRICATED PULLEYS. COMPLETED EXTENSION AND RETRACTION TEST AND GEAR OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1998052200759 19980522 00759 NM 1998 5 22 ASAA9840056 1 19980327 A 3350 S417N5048 LIGHT BOEING 737 7374Q8 NM AFT CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 782AS 25113 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE FROM ROW 27 AFT. REPLACED LIGHT SOCKET ASSEMBLY AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1998052200760 19980522 00760 EU 1998 5 22 AALA980603 1 19980325 A 2822 229945 PUMP FOKKER F28 F28MK0100 4990807 EU LEFT WING DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1442E 487 11437 ORD - FLT 0454 - DURING CLIMB-OUT, L1 AND L2 FUEL BOOST PUMPS FAULTED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCI DENT. REPLACED 1L AND L2 FUEL BOOST PUMPS. SYSTEM OPERATED NORMALLY WITH NO FAULTS OR LEAKS. SYSTEM GROUND AND LEAK C HECKED NORMAL OPERATION. REF: OPERATOR CONTROL NR 98ZZZX1932. (X) 2 L 7 2 4F RT 1998052200761 19980522 00761 EU 1998 5 22 98ZZZX1932 1 19980325 A 2822 229945 PUMP FOKKER F28 F28MK0100 4990807 EU LEFT WING DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1442E 494 11437 ORD - FLT 0454 - DURING CLIMB-OUT, L1 AND L2 FUEL BOOST PUMPS FAULTED. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCI DENT. REPLACED 1L AND L2 FUEL BOOST PUMPS. SYSTEM OPERATED NORMALLY WITH NO FAULTS OR LEAKS. SYSTEM GROUND AND LEAK C HECKED NORMAL OPERATION. REF: OPERATOR CONTROL NR AALA980603. 2 L 7 2 4F RT 1998052200762 19980522 00762 WP 1998 5 22 AALA980809 1 19980420 A 2131 21171803 CONTROLLER GARRTT DOUG DC9 DC982 3022082 WP AFT FUSELAGE DEFECTIVE A AALA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 07 205AA 103595 49155 DFW - FLT 1617 - DURING CRUISE LGA/DFW FL 280, FLOW LIGHT ILLUMINATED WITH ANTI-ICE ON. CREW ACCOMPISHED RAPID DECOMPRE SSION/EMERGENCY DESCENT PROCEDURES AND DEPLOYED PASSENGER OXYGEN MASKS. CABIN DECOMPRESSED ALONG WITH A TEMPERATURE CHA NGE IN CABIN. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED BOTH CABIN PRESSURE CONTROLLERS. REPLACED ALL PA SSENGER OXYGEN CANISTERS AND REPACKED MASKS. RAN ENGINES AND PACKS ON THE GROUND WITH NO ABNORMAL INDICATION NOTED. AI RCRAFT WAS FLOWN ON FUNCTIONAL CHECK FLIGHT AND PRESSURIZATION CHECKS NORMAL IN ALL PHASES OF FLIGHT WITH ANTI-ICE ON OR OFF. AIRCRAFT WAS RELEASED INTO SERVICE. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. REF OPER CNTRL NR 98ZZZX 2 L 7 2 4F A6WE 1998052200763 19980522 00763 WP 1998 5 22 98ZZZX1933 1 19980420 A 2131 21171803 CONTROLLER GARRTT DOUG DC9 DC982 3022082 WP AFT FUSELAGE DEFECTIVE A AALA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 07 205AA 761035 49155 DFW - FLT 1617 - DURING CRUISE LGA/DFW FL 280, FLOW LIGHT ILLUMINATED WITH ANTI-ICE ON. CREW ACCOMPISHED RAPID DECOMPRE SSION/EMERGENCY DESCENT PROCEDURES AND DEPLOYED PASSENGER OXYGEN MASKS. CABIN DECOMPRESSED ALONG WITH A TEMPERATURE CHA NGE IN CABIN. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED BOTH CABIN PRESSURE CONTROLLERS. REPLACED ALL PA SSENGER OXYGEN CANISTERS AND REPACKED MASKS. RAN ENGINES AND PACKS ON THE GROUND WITH NO ABNORMAL INDICATION NOTED. AI RCRAFT WAS FLOWN ON FUNCTIONAL CHECK FLIGHT AND PRESSURIZATION CHECKS NORMAL IN ALL PHASES OF FLIGHT WITH ANTI-ICE ON OR OFF. AIRCRAFT WAS RELEASED INTO SERVICE. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. REF: OPER CNTRL NR AALA9 2 L 7 2 4F A6WE 1998052200764 19980522 00764 WP 1998 5 22 AALA980735 1 19980410 A 4990 1945189004 OIL CAP WISCOPROD DOUG DC9 DC983 3022083 WP APU DEFECTIVE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 593AA 53256 BOS - FLT 1055 - AFTER TAKEOFF, A BURNING SMELL OF OIL AND SMOKE WERE NOTED IN THE CABIN. AIRCRAFT AIR INTERRUPTED AND RETURNED TO BOS WITHOUT FURTHER INCIDENT. REPLACED APU OIL FILLER CAP AND AS A PRECAUTIONARY, REPLACED BOTH COALESCER B AGS. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998052200765 19980522 00765 WP 1998 5 22 AALA980847 1 19980428 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP AFT ACCESSORY LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 476AA P80204 49651 MIA - FLT 1327 - DURING TAKEOFF, FLIGHT CREW NOTICED SMOKE IN THE CABIN. FLIGHT AIR INTERRUPTED AND RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. UPON LANDING, SMOKE DISSIPATED FOR THE CABIN. MAINTENANCE FOUND THE APU LEAKING OIL INTO THE AIR CONDITIONING SYSTEM. REPLACED APU AND RAN WITH PACKS ON WITH NO LEAKS OR SMELL NOTED. SYSTEM GROUND CHECK ED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998052200766 19980522 00766 WP 1998 5 22 AALA980772 1 19980408 A 5330 FUSELAGE DOUG DC9 DC982 3022082 WP RT LOWER FWD DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 434AA 49452 TUL - DENT IN FUSELAGE, FS 570 - FS 589 ABOVE L21R. REPAIRED IAW SRM 53-04 FIG 12B SHT 5. TST: 33,764 HOURS. CYCLES: 17,035. (X) 2 L 7 2 4F A6WE 1998052200767 19980522 00767 WP 1998 5 22 AALA980790 1 19980414 A 2150 20495061 TURBINE GARRTT DOUG DC9 DC982 3022082 WP NOSE SECTION DEFECTIVE A AALA H O DEACTIVATE SYST/CIRCUITS OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 454AA 1142556 49559 DTW - FLT 1932 - DURING TAKEOFF DFW, FLIGHT CREW NOTED ACRID SMELL AND HAZE IN CABIN. CREW TURNED OFF RECIRCULATING FAN AND INCREASED TEMPERATURE, HAZE, AND SMELL DISSIPATED. AIRCRAFT CONTINUED TO DTW WITH NO FURTHER SMELL NOTED UNTIL DES CENT WHEN SMELL RETURNED. AIRCRAFT LANDED DTW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAKEN OUT OF SERVICE AND MAINTENA NCE REPLACED BOTH AIR CYCLE MACHINES AND ACCOMPLISHED BURN-OUT PER MM PROCEDURES. SYSTEM GROUND AND LEAK CHECKED, NORMA L OPERATION. REF: OPER CONTROL NR 98ZZZX1934. (X) 2 L 7 2 4F A6WE 1998052200768 19980522 00768 WP 1998 5 22 98ZZZX1934 1 19980414 A 2150 20495061 TURBINE GARRTT DOUG DC9 DC982 3022082 WP NOSE SECTION DEFECTIVE A AALA K O NONE OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 454AA 8759073 49559 DTW - FLT 1932 - DURING TAKEOFF DFW, FLIGHT CREW NOTED ACRID SMELL AND HAZE IN CABIN. CREW TURNED OFF RECIRCULATING FAN AND INCREASED TEMPERTURE, HAZE, AND SMELL DISSIPATED. AIRCRAFT COTNINUED TO DTW WITH NO FURTHER SMELL NOTED UNTIL DESC ENT WHEN SMELL RETURNED. AIRCRAFT LANDED DTW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAKEN OUT OF SERVICE AND MAINTENAN CE REPLACED BOTH AIR CYCLE MACHINES AND ACCOMPLISHED BURN-OUT PER MM PROCEDURES. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. REF: OPER CONTROL NR AALA980790. 2 L 7 2 4F A6WE 1998052200769 19980522 00769 WP 1998 5 22 AALA980806 1 19980419 A 2150 20495061 TURBINE GARRTT DOUG DC9 DC982 3022082 WP NOSE SECTION OVERSERVICED A AALA H O DEACTIVATE SYST/CIRCUITS OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 454AA 1242585 49559 ORD - FLT 0571 - DURING CLIMB FL 150, CABIN FILLED WITH SMOKE AND SMELL OF HOT DUCTING. CREW SELECTED RIGHT HI PRESSURE BLEED-OFF, RIGHT PNEUMATIC X-FEED CLOSED, AND AIRFOIL ANTI-ICE VALVES OFF. SMOKE AND HOT DUCTING SMELL DISSIPATED. AI RCRAFT CONTINUED TO ORD WITH RIGHT ACM ISOLATED AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAKEN OUT OF SERVICE. TROUBLESHOOTING FOUND RIGHT ACM'S HAD BEEN OVER SERVICED. DRAINED EXCESS OIL AND ACCOMPLISHED RIGHT PACK BURN-OUT PER MM PROCEDURES. REPLACED RIGHT HAND WATER SEPARATOR BAG. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998052200770 19980522 00770 WP 1998 5 22 AALA980792 1 19980418 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 493AA 49731 DFW - FLT 1222 - AFTER TAKEOFF, NOSE LANDING GEAR UNSAFE RED LIGHT REMAINED ILLUMINATED UNTIL 15,000 FEET AND EXTINGUISH ED. AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING GEAR PROXIMITY SENSOR. PSEU BITE CHECK AND GEAR SWING TESTED NORMAL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998052200771 19980522 00771 WP 1998 5 22 AALA980744 1 19980411 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 70401 49312 DFW - FLT 1741 - DURING CRUISE, NOSE GEAR UNSAFE RED LIGHT ILLUMINATED WITH HYDRAULIC PUMPS ON. CREW ACCOMPLISHED CHECK LIST AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED NLG PROXIMITY SENSOR. ACCOMPLISHED PSEU BITE CHECK AND SWUNG G EAR WITH NORMAL INDICATIONS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998052200772 19980522 00772 NM 1998 5 22 AALA980853 1 19980430 A 3350 PR01051127 MODULE DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 1766A AA24 48597 LHR - FLT 0086 - DURING GROUND TAXI TO THE GATE, RIGHT SIDE EMERGENCY EXIT PATH LIGHTING ILLUMINATED. REPLACED EMERGENC Y EXIT PATH LIGHTING CONTROL MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200773 19980522 00773 WP 1998 5 22 AALA980857 1 19980503 A 3350 0200333001 LIGHT ASSY DOUG DC9 DC983 3022083 WP VENTRAL STAIRS BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 599AA 53289 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT VENTRAL STAIR FLOOD LIGHT WAS FOUND BROKEN. REPLACED EMERGENCY EXIT VENTRAL STAIR FLOOD LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998052200774 19980522 00774 WP 1998 5 22 AALA980851 1 19980429 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456AA 49561 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EX IT FLOOR PATH LIGHT STRIP JUMPER WIRE IN FORWARD CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998052200775 19980522 00775 EU 1998 5 22 AALA980701 1 19980326 A 3350 LIGHT STRIP AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 34078 615 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH ARROWS AT R4 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH ARROW LIGHT STRIP AT R4 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998052200776 19980522 00776 NM 1998 5 22 AALA980713 1 19980408 A 3350 L205301 LIGHT DOUG MD11 MD11 3023602 NM L4 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1762B 48552 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN L4 FORWARD DOOR FRAME INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN L4 FORWARD DOOR FRAME. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200777 19980522 00777 NM 1998 5 22 AALA980730 1 19980408 A 3350 A3060709102 LIGHT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1765B 48596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 20G INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 20G. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200778 19980522 00778 NM 1998 5 22 AALA980729 1 19980409 A 3350 A3060841 LIGHT STRIP DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1756 48491 DFW - DURING OVERNIGHT MAINTENANCE CHECK, RIGHT HAND FORWARD CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPL ACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN RIGHT HAND FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200779 19980522 00779 EU 1998 5 22 AALA980679 1 19980402 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 25071 514 LHR - FLT 0106 - DURING CRUISE, NR 1 FIRST CLASS OVEN WAS EMITTING SMOKE WHILE HEATING FOOD. REMOVED BURNED FOOD AND TH OROUGHLY CLEANED ENTIRE INTERIOR OF NR 1 FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998052200780 19980522 00780 EU 1998 5 22 AALA980695 1 19980405 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 14056 463 JFK - DURING OVERNIGHT MAINTENANCE, AFT GALLEY RIGHT AND LEFT SIDE EMERGENCY EXIT FLOOR TRACT LIGHTING INOPERATIVE. REP LACED AFT GALLEY RIGHT AND LEFT SIDE EMERGENCY EXIT FLOOR TRACT LIGHT STRIPS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998052200781 19980522 00781 NM 1998 5 22 AALA980742 1 19980410 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1760A 48550 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FRONT OF LAVATORY '2' HAS ONE BULB INOPERATIVE . REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FRONT OF LAVATORY '2'. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 3 4F RT A22WE 1998052200782 19980522 00782 NM 1998 5 22 AALA980747 1 19980411 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN LOOSE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 1766A 48597 SJC - FLT 0128 - DURING CRUISE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST AND BUSINESS CLASS INTERMITTENTLY FLICKERED. CHECKED EMERGENCY EXIT FLOOR PATH LIGHT STRIP CONNECTIONS AND RESEATED AS NECESSARY. ACCOMPLISHED EMERGENCY EXIT LIGH T TEST WITH NO FAULTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200783 19980522 00783 NM 1998 5 22 AALA980770 1 19980413 A 2611 72130001012 DETECTOR FENWAL DOUG MD11 MD11 3023602 NM LAV 'W' DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT MAINTENANCE, SMOKE DETECTOR IN LAVATORY 'W' FAILED SMOKE DETECTION TEST. REPLACED SMOKE DETECTOR IN LAVATORY 'W'. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200784 19980522 00784 NM 1998 5 22 AALA980769 1 19980413 A 2612 72130001012 DETECTOR FENWAL DOUG MD11 MD11 3023602 NM LAV 'M' DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 9401 48551 DFW - DURING OVERNIGHT MAINTENANCE, SMOKE DETECTOR IN LAVATORY 'M' FAILED SMOKE DETECTION TEST. REPLACED SMOKE DETECTOR IN LAVATORY 'M'. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200785 19980522 00785 NM 1998 5 22 AALA980768 1 19980413 A 2612 72130001012 DETECTOR FENWAL DOUG MD11 MD11 3023602 NM LAVATORY 'J' DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 9430 48551 DFW - DURING OVERNIGHT MAINTENANCE, SMOKE DETECTOR IN LAVATORY 'J' FAILED SMOKE DETECTION TEST. REPLACED SMOKE DETECTOR IN LAVATORY 'J'. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200786 19980522 00786 NM 1998 5 22 AALA980830 1 19980424 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1764B 48554 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT AT AFT GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT CEI LING LIGHT POWER SUPPLY CONNECTOR AT AFT GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200788 19980522 00788 EU 1998 5 22 AALA980751 1 19980412 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7062A 474 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS REMAINED ON IN DIM POSITION. SECURED LOOSE CONNECTOR AT EMERG ENCY EXIT LIGHT ARM/DISARM SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998052200789 19980522 00789 1998 5 22 AALA980799 4 19980420 A 3460 COM5089 FMS AIRBUS 300 A300B4605R 3930308 EU E/E COMPT MALFUNCTIONED A AALA O OTHER O OTHER CR CRUISE 1 SW 07 33069 512 LHR - FLT 0116 - AFTER 3 HOURS OF FLIGHT WHEN SELECTING POSITION, FREEZE ON PROGRESS PAGE. THE FMS JUMPED SEVERAL HUNDR ED MILES OFF COURSE TO THE NORTH AND WOULD NOT UNFREEZE. FMS WAS TOTALLY OFF AND DUMPED THE NAV DISPLAY ON THE ND. THE ACTUAL IRS.S SEEMED TO BE OK. ACTIVATED THE SECONDARY FLIGHT PLAN. UPDATED THE PRESENT POSITION ON THE PROGRESS PAGE USING IRS COORDINATES. DELETED POINTS BEHIND, THEN WENT DIRECT TO NEXT NAV POINT WHICH RECOVERED THE FMS NAV TO A REASO NABLE POSITION AND WAS THEN OK TO NAVIGATE. (X) 2 L 7 2 4F RT A35EU 1998052200790 19980522 00790 EU 1998 5 22 AALA980807 1 19980421 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU R3 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 80057 465 JFK - DURING OVERNIGHT MAINTENANCE, R3 DOOR OVERHEAD AND CEILING EMERGENCY LIGHTS WERE INOPERATIVE. RESEATED CONNECTOR AT R3 EMERGENCY EXIT DOOR LIGHT PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998052200791 19980522 00791 EU 1998 5 22 AALA980644 1 19980325 A 3040 WIN1222 SENSOR AIRBUS 300 A300B4605R 3930308 EU WINDOW HEAT FAILED A AALA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 07 33069 512 LHR - FLT 0093 - RT WINDOW HEAT FAULTED ON TAXI OUT. FOUND WINDOW HEAT SENSOR FAULT. SWAPPED TO ALTERNATE SENSOR. OPS NOW OK. WINDOW HEAT TEST OK. ALL OPS AND INDICATIONS NOW NML. NOTE: EXTENDED RANGE EVENT REPORT (ER) NR TUL15. (X ) 2 L 7 2 4F RT A35EU 1998052200792 19980522 00792 WP 1998 5 22 AALA980774 1 19980407 A 5320 CUSP WEB DOUG DC9 DC982 3022082 WP INBD OF AFT SVS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 434AA 49452 TUL - CORROSION ON CUSP WEB UNDER SEAT TRACK NR 1 AT STA 1174. INSTALLED DOUBLER 4 INCHES BY 5 INCHES AFTER CUT-OUT OF DAMAGE PER SRM 53-01. (X) 2 L 7 2 4F A6WE 1998052200793 19980522 00793 NM 1998 5 22 AALA980728 1 19980408 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT HAND AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. RESEATED LOOSE CONNECTOR ON EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998052200794 19980522 00794 NM 1998 5 22 AALA980841 1 19980414 A 2420 GCU BOEING 767 767323 1385205 NM RT SYSTEM MALFUNCTIONED A AALA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 362AA 24043 RTY - FLT 2101 - AT 330, 1 HR IN-FLIGHT, RT GEN CONTACTOR R-BUS. R-BUS TIE ISO AND UTILITY BUS LIGHTS ILLUMINATED. CYC LED RT GEN AND RESTORED BUS, BUT ISO LIGHT AND UTILITY BUS LIGHTS REMAINED ON. HELP FROM TECH SUPPORT, ISOLATED THE PRO B TO THE GALLEY. PULLED GALLEY FWD/MID CB AND RESET UTILITY BUSES. WORKED FINE FOR 30 MINUTES. NEXT, THE RT UTILITY B US WAS LEFT OFF AND THE RT GEN CONT AND BUS TIE SWITCHES. WORKED 5 MINTUES. BITE OF BPCU/SHOWED DP TRIP AND RT MAIN BU S OVERLAP ZONE. ACCOMPLISHED T/S CHECKS PER MM REF 24-20-00-1. ALL CKS NORMAL. INSP IDG HARNESS FROM IDG TO ENG FIRE WALL. NO DEFECTS FOUND. REPLACED RT GCU, RT IDG, RT BUS TIE BREAKER (C904) AND THE BPCU. ALL CKS NORMAL. (X) 2 L 7 2 4F RT A1NM 1998052200795 19980522 00795 NM 1998 5 22 AALA980842 1 19980424 A 2421 5103 IDG BOEING 767 767323 1385205 NM RT GEN FAILED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CE 05 352AA 24033 MAD - FLT 0069 - RT IDG PLAC INOP AS MEL 24-01 AUTH 4-32-9DC-B NO TIME AT MAD NO PARTS ENTERED MICS MEL PROCEDURES C/W E NG APU. COWLINGS CLOSED BOTH IDG AND APU SERVICED TO PROPER LEVEL. R/R RT IDG PER MM LEAK CK NO LEAKS NOTED. OPS CHEC K THRU ALL OPERATIONS CKS NORMAL. NOTE: EXTENDED RANGE EVENT REPORT (ER) NR AFW777. (X) 2 L 7 2 4F RT A1NM 1998052200796 19980522 00796 NM 1998 5 22 AALA980845 1 19980428 A 3350 SOCKET BOEING 767 767323 1385205 NM PASSENGER SEAT BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7375A 25202 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT PATH LIGHT AT PASSENGER SEAT 35 AB INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT SOCKET AT PASSENGER SEAT 35 AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052200797 19980522 00797 NM 1998 5 22 AALA980808 1 19980421 A 3350 LIGHT ASSY BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 648AA 24606 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT LIGHT AT FORWARD COACH CABIN INOPERATIVE. REPLACED EMERGENCY L IGHT ASSEMBLY IN FORWARD COACH CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998052200798 19980522 00798 NM 1998 5 22 AALA980791 1 19980417 A 5270 853504 CARD ELDEC BOEING 767 767223 1385123 NM E/E COMPARTMENT DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 308AA 882 22314 ORD - FLT 0021 - DURING CRUISE, RIGHT OVER WING SLIDE DOOR EICAS MESSAGE APPEARED ALONG WITH AN EMERGENCY DOOR UNSAFE LI GHT. AIRCRAFT DIVERTED AND LANDED ORD WITHOUT FURTHER INCIDENT. SYSTEM WAS PLACARDED AND FLIGHT RE-DEPARTED TO LAX. L AX MAINTENANCE PERFORMED BITE CHECK OF OVER WING SLIDE DOOR SENSORS WHICH CHECKED NORMAL. REPLACED FAULTED CARD IN PSEU SLOT 014 AND SYSTEM BITE CHECKED GOOD. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052200799 19980522 00799 WP 1998 5 22 AALA980793 1 19980418 A 3620 6274543 CONTROL GARRTT DOUG DC10 DC1030 3023501 WP ENGINE DEFECTIVE A AALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 SW 07 164AA 018C272 46950 HNL - FLT 0072 - DURING CRUISE, NR 2 PNEU HIGH TEMPERATURE LIGHT ILLUMINATED. CREW FOLLOWED EMERGENCY CHECKLIST, AIR IN TERRUPTED, AND RETURNED TO HNL LANDING WITHOUT FURTHER INCIDENT. REPLACED NR 2 PNEU CONTROLLER AND AS A PRECAUTIONARY, REPLACED FAN AIR PRECOOLER PYLON AND PNEUMATIC VALVE. SYSTEM GROUND AND LEAK CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1998052200800 19980522 00800 NM 1998 5 22 AALA980750 1 19980411 A 3610 M9131 VALVE BOEING 767 767323 1385205 NM LT ENGINE DEFECTIVE A AALA O A OTHER UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 366AA 25193 SFO - FLT 0037 - LT BLEED DUCT LEAK LIGHT ON TAKEOFF. LIGHT EXTINGUISHED AFTER ENGINE BLEED VALVE CLOSED. INSPECTED AN D FOUND AFT GROUND AIR SUPPLY CHECK VALVE OPEN. REMOVED AND REPLACED GROUND AIR SUPPLY CHECK VALVE. LEAK CHECK GOOD. A CCOMPLISHED HIGH POWER RUN. NO PROBLEMS NOTED. (X) 2 L 7 2 4F RT A1NM 1998052200801 19980522 00801 NM 1998 5 22 AALA980546 1 19980318 A 2421 IDG BOEING 767 767323 1385205 NM LT GEN FAILED A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 370AA 25197 SCL - FLT 2101 - AFTER TAKEOFF DURING CLIMB-OUT PASSING 12,000 FEET, LEFT GENERATOR LIGHT ILLUMINATED. TRIED RESET, BUT LT GEN CAME BACK ON. AFTER CONSULTATION WITH COMPANY AND TULSA TECH, CONTINUED ON WITH APU RUNNING FOR ENTIRE FLIGHT. REMOVED AND REPLACED LT ENG IDG PER MM 24-11-01-4-2. RUN LT ENG IDG WORKS OK. NOTE: EXTENDED RANGE EVENET REPORT (ER ) NR AFW770. (X) 2 L 7 2 4F RT A1NM 1998052200802 19980522 00802 1998 5 22 AALA980705 4 19980326 A 2310 TRANSCEIVER BOEING 767 767323 1385205 NM LT HF FAILED A AALA K NONE O OTHER CR CRUISE 1 SW 07 39356 24037 JFK - FLT 0068 - BOTH HF RADIOS INOP IN-FLIGHT SUSPECT ANTENNA COUPLER. TROUBLESHOT SYSTEM. REPLACED DEFECTIVE LT HF T RANSCEIVER AND RT HF COUPLER. BOTH SYSTEMS CHKS NORMAL. (X) 2 L 7 2 4F RT A1NM 1998052200803 19980522 00803 NM 1998 5 22 AALA980773 1 19980415 A 3350 LIGHTS BOEING 757 757223 1384957 NM CABIN INTERMITENT A AALA K NONE O OTHER DE DESCENT 1 SW 07 613AA 24489 AUA - FLT 1047 - DURING DESCENT AUA, EMERGENCY EXIT LIGHTS ILLUMINATED AND EXTINGUISHED. MAINTENANCE TROUBLESHOT AND TE STED THE SYSTEM. UNABLE TO DUPLICATE PROBLEM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998052200804 19980522 00804 WP 1998 5 22 VJ9800153 1 19980518 A 2130 PRESSURIZATION DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A ZZDA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SO 15 931VV 47674 AIRCRAFT LOST CABIN PRESSURIZATION AT FL 32.6 CABIN ALTITUDE INCREASED TO 12500 FEET, O2 MASK DROPPED, SYSTEM WAS FUNCTI ONING PROPERLY UNTIL THIS POINT. CREW AND PAX O2 USED. 2 L 7 2 4F A6WE 1998052200805 19980522 00805 WP 1998 5 22 VJ9800154 1 19980519 A 3350 20131A BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 910VJ 47277 FWD CABIN EMERGENCY TRACK LIGHT INOP. REPLACED THE FWD CABIN EPL BATTERY PACK PER MM 33-50. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998052200806 19980522 00806 NM 1998 5 22 AWXA9800125 1 19980510 A 3350 FUSE BOEING 757 7572S7 1384962 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 901AW 23321 DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT AFT SIDE SEAT EMERGENCY LIGHTS INOP FROM MID-LAVS TO AFT GALLEY. 4L AND 4R LOWER EMERGENCY LIGHTS INOP ALSO. REMOVED AND REPLACED BAD FUSE IN POWER SUPPLY SYSTEM. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998052200807 19980522 00807 EA 1998 5 22 PNSA980501 2 19980516 A 8500 ENGINE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LT/RT POWER LOSS A PNSA A E UNSCHED LANDING ENGINE SHUTDOWN G Y MULTIPLE FAILURE ENGINE STOPPAGE CR CRUISE 1 AL 03 15PR 318052011 WHILE IN CRUISE, THE PILOT NOTED A RAPID DROP IN FUEL QUANTITY INDICATION. SHORTLY THERE AFTER THE LEFT ENGINE LOST POW ER. FOLLOWED BY A RT ENGINE POWER LOSS TWO MINUTES LATER. A SUCCESSFUL LANDING WAS ACCOMPLISHED WITH NO DAMAGE TO THE AIRCRAFT. CURRENTLY THIS INCIDENT IS UNDER INVESTIGATION. 1 L 7 2 3O 3 O A20SO E14EA 1998052200808 19980522 00808 NM 1998 5 22 RAAA98B2029 1 19980517 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 FWD RT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998052200809 19980522 00809 WP 1998 5 22 CALA9800867 1 19980515 A 3231 39567851 LINK DOUG DC9 DC982 3022082 WP RT NLG DOOR FAILED A CALA O OTHER E J VIBRATION/BUFFET WARNING INDICATION TO TAKEOFF 1 SW 09 14810 49264 A VIBRATION WAS FELT AFTER GEAR RETRACTION LEAVING DCA. ALL GEAR INDICATIONS WERE NORMAL. RECYCLING THE GEAR MADE NO CH ANGE. THE AIRCRAFT WAS RETURNED TO DCA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT NLG FORWARD DOOR LIN K FAILED WITH THE DOOR HANGING DOWN. THE RT NLG FORWARD DOOR LINK WAS REMOVED AND REPLACED IAW MM 32-22-01. A RETRACTI ON CHECK WAS PERFORMED AND THE DOOR OPERATED NORMALLY. 2 L 7 2 4F A6WE 1998052200810 19980522 00810 WP 1998 5 22 CALA9800868 1 19980515 A 5320 ANGLE DOUG DC9 DC982 3022082 WP CARGO DOOR JAMB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND CORROSION ON FORWARD FACE OF MAIN BAGGAGE BIN LOWER DOOR JAMB Z-ANGLE. A REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998052200811 19980522 00811 WP 1998 5 22 CALA9800869 1 19980515 A 5320 JAMB DOUG DC9 DC982 3022082 WP BAGGAGE DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND FORWARD BAGGAGE BIN DOOR JAMB PAN CORRODED. THE CORRODED AREA OF DOOR PAN WAS CUT OUT. A REPAIR PAN WA S INSTALLED IAW SRM 53-05, FIGURE 44, SHEET 1. 2 L 7 2 4F A6WE 1998052200812 19980522 00812 WP 1998 5 22 CALA9800870 1 19980515 A 5347 TIEDOWN RAIL DOUG DC9 DC982 3022082 WP BS 1007-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND CORROSION ON LT TIE DOWN RAILS AT STA 1007-1174 AND STA 1212-1231. NEW TIE DOWN RAILS WERE INSTALLED I AW SRM 51-30-01. 2 L 7 2 4F A6WE 1998052200813 19980522 00813 WP 1998 5 22 CALA9800871 1 19980516 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND A 1 CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-10-3. 2 L 7 2 4F A6WE 1998052200814 19980522 00814 WP 1998 5 22 CALA9800872 1 19980516 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND A .5 INCH CRACK AT FORWARD END OF FORWARD SERVICE DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND REPLACED IA W SRM 51-30-2. 2 L 7 2 4F A6WE 1998052200815 19980522 00815 NM 1998 5 22 CALA9800873 1 19980516 A 5720 SPLICE BOEING 737 737291 138448W NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND A 1 CRACK IN LT WING LANDING GEAR BEAM AFT SPLICE PLATE AT FS 727. THE SPLICE PLATE WAS REPAIRED IAW D RAWING NR 65C292288. 2 L 7 2 4F A16WE 1998052200816 19980522 00816 NM 1998 5 22 CALA9800874 1 19980516 A 5320 WEB BOEING 737 737291 138448W NM BS 492.4 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR CUTOUT AFT FRAME AFT FACE OF WEB AT BS 492.4, STRING ER 25R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 2 4F A16WE 1998052200817 19980522 00817 NM 1998 5 22 CALA9800875 1 19980516 A 5320 TEAR STRAP BOEING 737 737291 138448W NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND FRAME TO SKIN TEAR STRAP CORRODED AT BS 360, STRINGER 29R. REPAIRED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1998052200818 19980522 00818 NM 1998 5 22 CALA9800876 1 19980517 A 5330 SKIN BOEING 737 737291 138448W NM BS 294.5 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND FUSELAGE SKIN DENTED AT FS 294.5, STRINGER 14. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1998052200819 19980522 00819 NM 1998 5 22 CALA9800877 1 19980519 A 3230 CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM LANDING GEAR TRIPPED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 69333 23571 THE GEAR LEVER WOULD NOT MOVE FROM THE OFF TO THE UP POSITION UPON GEAR RETRACTION AFTER TAKEOFF FROM IAH. CHECKLIST PR OCEDURES WERE ACCOMPLISHED AND THE LOCK OVERRIDE TRIGGER WAS USED TO RETRACT THE GEAR. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEVER LATCH CIRCUIT BREAKER ON P6 PANEL POPPED. THE CIRCUIT B REAKER WAS RESET AND MM 32-31-21 PROCEDURES WERE COMPLIED WITH. GROUND AND AIR MODES WERE SIMULATED AND OPERATION OF TH E LANDING GEAR HANDLE WAS GOOD. 2 L 7 2 4F RT A16WE 1998052200820 19980522 00820 WP 1998 5 22 CALA9800878 1 19980519 A 2150 97968011 VALVE DOUG DC9 DC981 3022081 WP RT PACK LEAKING A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 16884 48074 SMOKE APPEARED IN COCKPIT AND CABIN ON DEPARTURE FROM DCA. THE RT PACK WAS SHUT OFF AND THE SMOKE CLEARED. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RT OIL FILLED WATER SEPARATOR VALVE LEAKING OI L. THE VALVE WAS REMOVED AND REPLACED. IN ADDITION, THE WATER SEPARATOR BAG WAS REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998052200821 19980522 00821 NM 1998 5 22 CALA9800879 1 19980518 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AROUND NUT PLATES AT STA 986.5 FROM BL 0 TO LBL 50. THE UPPER CHORD OF F LOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03450 AND SRM 53-00-51. 2 L 7 2 4F RT A16WE 1998052200822 19980522 00822 WP 1998 5 22 CALA9800880 1 19980517 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP WS 118 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND A 1 CRACK IN ANGLE AT LT WHEEL WELL REAR SPAR, WS 118. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRI CATED AND INSTALLED IAW SRM 51-20-00, 51-33-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998052200823 19980522 00823 WP 1998 5 22 CALA9800881 1 19980518 A 2560 BATTERIES DOUG DC10 DC1030 3023501 WP MEGAPHONE DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND AFT MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 25- 60-00. 2 L 7 3 4F A22WE 1998052200824 19980522 00824 WP 1998 5 22 CALA9800882 1 19980518 A 3350 BR9279103 LIGHT DOUG DC10 DC1030 3023501 WP LAVATORY INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 83071 48293 INSPECTION FOUND THE EMERGENCY FLOODLIGHT AT LAV B INOPERATIVE. THE FLOODLIGHT WAS REPLACED IAW MM 33-50-00. 2 L 7 3 4F A22WE 1998052200825 19980522 00825 WP 1998 5 22 CALA9800883 1 19980518 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 EXCESSIVE FORCE WAS REQUIRED TO RELEASE TAILCONE USING AFT CABIN DOOR AND THE INTERIOR RELEASE HANDLE. THE CABLES AND L ATCHES WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998052200826 19980522 00826 WP 1998 5 22 CALA9800884 1 19980518 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND A .5 INCH CRACK WITH DENT AT LOWER AFT CORNER OF FORWARD MAIN CABIN DOOR SKIN. A REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 37. 2 L 7 2 4F A6WE 1998052200827 19980522 00827 WP 1998 5 22 CALA9800885 1 19980518 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND LONGERON 29R CORRODED AT STA 580. A SPLICE WAS INSTALLED IAW SRM 51-10-5. 2 L 7 2 4F A6WE 1998052200828 19980522 00828 WP 1998 5 22 CALA9800886 1 19980519 A 5347 TIEDOWN RAIL DOUG DC9 DC982 3022082 WP BS 1007-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND RIGHT TIE DOWN RAIL CORRODED IN AFT CARGO BIN AT STA 1007 TO 1155. THE TIE DOWN RAIL WAS REMOVED AND T HE CORROSION WAS REMOVED IAW SRM 51-30-3. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5320-01519. 2 L 7 2 4F A6WE 1998052200829 19980522 00829 NM 1998 5 22 CALA9800887 1 19980516 A 5311 FRAME BOEING 737 737291 138448W NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND A 1.5 CRACK IN RADIUS OF FRAME AT STA 675, RBL 24, WBL 208 AND A 1.5 CRACK IN FRAME AT STA 675, LBL 24, WBL 208. REPAIRS WERE PERFORMED IAW SA001-5710-01638. 2 L 7 2 4F A16WE 1998052200830 19980522 00830 NM 1998 5 22 CALA9800888 1 19980516 A 5320 BEAM BOEING 737 737291 138448W NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND TRANSVERSE BEAM CRACKED IN RADIUS FORWARD AND AFT IN THREE EACH PLACES AT STA 675, RBL 24, WBL 208. TH E CRACKS WERE APPROXIMATELY 1 INCH LONG. THE CRACKS WERE STOP DRILLED. A REPAIR WAS INSTALLED IAW SA001-5710-01638. 2 L 7 2 4F A16WE 1998052200831 19980522 00831 NM 1998 5 22 CALA9800889 1 19980518 A 5330 SKIN BOEING 747 747243B 1384830 NM BS 580-600 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND A PUNCTURE IN FUSELAGE SKIN ABOUT 2 INCHES BELOW BOTTOM OF FORWARD CARGO DOOR AT BS 580-600. REPAIRED IAW SRM 53-30-03. 2 L 7 4 4F A20WE 1998052200832 19980522 00832 WP 1998 5 22 9809289994 1 19980515 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8979E 47328 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHT AT ROW12D INOPERATIVE. SECURED CONNECTOR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052200833 19980522 00833 WP 1998 5 22 9809299301 1 19980516 A 3230 59370365501 CYLINDER DOUG DC9 DC982 3022082 WP LT MLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 301RC 44624 17486 48054 LEFT MAIN LANDING GEAR UNSAFE AND GEAR DOOR OPEN LIGHTS ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDE D WITHOUT INCIDENT. MAINTENANCE REPLACED MAIN LANDING GEAR RETRACT CYLINDER. OPERATIONAL CHECK NORMAL. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F A6WE 1998052200834 19980522 00834 WP 1998 5 22 9809309612 1 19980515 A 3260 HARNESS DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 612NW 47436 DURING APPROACH INTO FAR, NOSE LANDING GEAR GREEN DOWNLOCK LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. CREW DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR PROXIMITY HARNESS. OPERATIONAL CHEC K NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998052200835 19980522 00835 WP 1998 5 22 9809319760 1 19980514 A 5350 CLIPS DOUG DC9 DC941 302207N WP TAIL CONE OUT OF ADJUST A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 760NW 47288 DURING TAILCONE FUNCTIONAL CHECK, FOUND THAT EXCESSIVE FORCE WAS REQUIRED TO REMOVE BOTH THE INTERIOR AND EXTERIOR RELEA SE HANDLES FROM THE RETENTION CLIPS. ADJUSTED CLIPS. FUNCTIONAL CHECK OK. 2 L 7 2 4F A6WE 1998052200836 19980522 00836 WP 1998 5 22 9809329946 1 19980517 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8926E 45863 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS ON CATWALK ILLUMINATED WITH SWITCH IN OFF POSITION. REPAIRED BROKEN WIRING TO SPLICE NEAR TAILCONE BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052200837 19980522 00837 WP 1998 5 22 9809339905 1 19980518 A 3260 SENSOR DOUG DC9 DC931 3022065 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 955N 47160 DURING APPROACH INTO EWR, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. NOSE GEAR UNSAFE L IGHT WAS ILLUMINATED. FLIGHT CREW RECYCLED GEAR AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENA NCE REPLACED THE NOSE GEAR PROXIMITY SENSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998052200838 19980522 00838 NE 1998 5 22 9809346601 2 19980515 A 7200 ENGINE BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 2 FLAMED OUT A NWAA E ENGINE SHUTDOWN R X PARTIAL RPM/PWR LOSS ENGINE FLAMEOUT CR CRUISE 1 GL 01 601US 19778 662678 WHILE AT CRUISE FL330 AND IN LIGHT TO MODERATE TURBULENCE, THE NR 2 ENGINE APPEARED TO ROLL BACK TO IDLE AND WOULD NOT R ESPOND TO THRUST LEVER MOVEMENT. ENGINE FLAMEOUT PROCEDURES WERE FOLLOWED AND THE ENGINE WAS RESTARTED. AFTER RESTART THE ENGINE OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT. NO OPERATING PARAMETERS WERE EXCEEDED. MAINTENANCE PERFO RMED FIM 71-01-00 PROCEDURE AND REPLACED THE FUEL FILTER AND TT2 SENSOR. AN ENGINE RUN WAS COMPLETED WITH NO PROBLEMS N OTED AND THE AIRCRAFT RETURNED TO SERVICE. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998052200839 19980522 00839 NM 1998 5 22 UPS98226690 1 19980517 A 5412 MILT9046 FIREWALL BOEING 727 727172C 1384058 NM NR 2 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 NUMBER 2 ENG FIREWALL CRACKED AND WRINKLED REPAIRED PER EO B727-5410-10083-B. 2 L 7 3 4F A3WE 1998052200840 19980522 00840 NM 1998 5 22 UPS98226691 1 19980506 A 5313 1498142 STRINGER BOEING 727 72751C 1384015 NM BS 450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D STRINGER 24 RIGHT HAS SURFACE CORROSION AT STA 445 AND 460. STRINGER SECTION REPAIRED IAW SRM 53-10-3 . 2 L 7 3 4F A3WE 1998052200841 19980522 00841 NM 1998 5 22 UPS98226692 1 19980504 A 5310 ANGLE BOEING 727 72751C 1384015 NM BS 560-580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D SUSPECT CRACK IN UPPER CHORD OF INTERCOSTAL BETWEEN BS 560-580 (JUST AFT OF 560) RBL 25. REPLACED CHO RD ANGLE IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998052200842 19980522 00842 NM 1998 5 22 UPS98226693 1 19980430 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 600 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D LOWER O/B CHORD OF FRAME 600 BROKEN OFF BETWEEN STRINGERS 25-25 LEFT, REPAIR IAW SRM 53-10-4 FIG 12. 2 L 7 3 4F A3WE 1998052200843 19980522 00843 NM 1998 5 22 UPS98226694 1 19980430 A 5741 69139017 BOTTLE PIN BOEING 727 72751C 1384015 NM BS 870 PITTING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D PITTING ON FWD EDGE OF RT AFT REAR SPAR TO BODY BOTTLE PIN. BOTTLE PIN REPLACED IAW MM 57-41-01. 2 L 7 3 4F A3WE 1998052200844 19980522 00844 NM 1998 5 22 UPS98226695 1 19980430 A 5755 ANGLE BOEING 727 72751C 1384015 NM NR 1 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D NR 1 SPOILER ACTUATOR SUPPORT FITTING INB SUPPORT ANGLE HAS CRACKS AROUND LWR HOLE. REPLACED SUPPORT ANGLE IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998052200845 19980522 00845 NM 1998 5 22 UPS98226696 1 19980428 A 5730 66171751 ACCESS PANEL BOEING 727 72751C 1384015 NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D EXTENSIVE CORROSION ON NR 1 FRONT SPAR FUEL TANK ACCESS PANEL RT WING. REPLACED IAW MM 28-11-21. 2 L 7 3 4F A3WE 1998052200846 19980522 00846 NM 1998 5 22 UPS98226697 1 19980429 A 5320 INTERCOSTAL BOEING 727 72751C 1384015 NM BS 211-219 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D INTERCOSTAL BETWEEN STR 219 AND 211 RT SIDE BL 25 APPROX CORRODED. REPLACED PER SRM 51-10-1 AND SRM 5 3-10-2. 2 L 7 3 4F A3WE 1998052200847 19980522 00847 NM 1998 5 22 UPS98226698 1 19980429 A 5320 STIFFENER BOEING 727 72751C 1384015 NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D STIFFENER CRACKED BS 178, STR 17 R. CARRIED OUT REPAIR IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998052200848 19980522 00848 NM 1998 5 22 UPS98226699 1 19980425 A 5720 RING CLAMPS BOEING 727 72751C 1384015 NM WS 716-491 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D SEVERAL FUEL TANK ACCESS DOORS, RING CLAMPS HAVE FRETTING CORROSION LT WING. RING CLAMPS REPLACED IAW 28-11-21 MM 6 OFF PANEL NR'S 3, 5, 6, 7, 8, 9, 10 CORROSION REMOVED AND FOUND TO BE IN LIMITS OF SRM 57-30-03, REPROTEC TED IAW SRM 57-30-03. 2 L 7 3 4F A3WE 1998052200849 19980522 00849 NM 1998 5 22 UPS98226700 1 19980430 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D CRACK IN UPPER CHORD OF FRAME 640 BETWEEN STRINGERS 21 AND 22 LT. FRAME AT BS 640 BETWEEN STR 21 AND 22L REPAIRED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1998052200850 19980522 00850 NM 1998 5 22 UPS98226701 1 19980424 A 5313 SKIN BOEING 727 72751C 1384015 NM BS 1173-1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D CORROSION BETEEN STR 1173-1185 RT BETWEEN STRS 22 AND 25 IN BETWEEN THE BONDED INTERNAL DOUBLER. DISB ONDED INTERNAL DOUBLER AND SKIN REMOVED SKIN REPAIR CARRIED OUT IAW SRS EO 98-12-004. 2 L 7 3 4F A3WE 1998052200851 19980522 00851 NM 1998 5 22 UPS98226702 1 19980423 A 5320 69163803 TUNING FORK BOEING 727 72751C 1384015 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, TUNING FORK AT BS 870 STR 2 R CRACKED. TUNING FORK REPLACED IAW SRM51-30-2. 2 L 7 3 4F A3WE 1998052200852 19980522 00852 NM 1998 5 22 UPS98226703 1 19980422 A 5712 RIB BOEING 727 72751C 1384015 NM WS 519 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D CRACK ON RIB AT LWR SUPPORT ANGLE NR 6 SLAT BELOW O/B HOOK. REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998052200853 19980522 00853 NM 1998 5 22 UPS98226704 1 19980422 A 5712 RIB BOEING 727 72751C 1384015 NM WS 410 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, NR 5 SLAT I/B RIB AT ACTUATOR ROD END CRACKED. CRACK REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998052200854 19980522 00854 NM 1998 5 22 UPS98226705 1 19980428 A 5330 SKIN BOEING 727 72751C 1384015 NM BS 328 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D CRACKS FOUND IN BOTH UPPER AND LWR FWD ENTRY DOOR HINGE CUTOUTS. REPAIRED BOTH UPPER AND LWR FWD ENTR Y DOOR HINGE CUTOUTS IAW EO B727- 5330-128. 2 L 7 3 4F A3WE 1998052200855 19980522 00855 NM 1998 5 22 UPS98226706 1 19980429 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 540 CRACK A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D SUSPECT CRACK IN CLEAT JOINING FRAME TO FUSELAGE STRUCTURE AT FLOORBEAM 540 LT SIDE. REPAIR CARRIED O UT IAW SRM 51-40-2 FIG 1. 2 L 7 3 4F A3WE 1998052200856 19980522 00856 NM 1998 5 22 UPS98226707 1 19980506 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, SUSPECT CRACK IN OUTER CHORD OF FRAME 580 STR 17 L. REPAIRED FRAME IAW SRM 53-10-2. 2 L 7 3 4F A3WE 1998052200857 19980522 00857 NM 1998 5 22 UPS98226708 1 19980425 A 5730 66171751 PANEL BOEING 727 72751C 1384015 NM WS 198 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D LT WING FRONT SPAR FUEL TANK ACCESS PANEL CORRODED. ACCESS REPLACED IAW MM 28-11-2. 2 L 7 3 4F A3WE 1998052200858 19980522 00858 NM 1998 5 22 UPS98226709 1 19980430 A 5320 CLEAT BOEING 727 72751C 1384015 NM BS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, SUSPECT CRACK IN CLEAT JOINING FRAME TO FUSELAGE STRUCTURE AT FLOORBEAM 560 LT SIDE. CLEAT REPLACED IAW SRM 51-10-1 AND 53-10-2 FIG 3 HEAT TREATMENT REF. 2 L 7 3 4F A3WE 1998052200859 19980522 00859 NM 1998 5 22 UPS98226710 1 19980430 A 5320 CLEAT BOEING 727 72751C 1384015 NM BS 600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, SUSPECT CRACK IN CLEAT JOINING FRAME TO FUSELAGE STRUCTURE AT FLOORBEAM 600 LT SIDE. CLEAT REPLACED IAW SRM 51-10-1 AND 53-10-2. 2 L 7 3 4F A3WE 1998052200860 19980522 00860 NM 1998 5 22 UPS98426689 1 19980518 A 2612 69B475193 FIRE CARD BOEING 747 747123F NM E/E COMPT MALFUNCTIONED A IPXA D C RETURN TO BLOCK ABORTED TAKEOFF N FALSE WARNING CR CRUISE 1 SO 01 675UP 20390 FIRE WARNING INDICATION AND BELL, INTERMITTENT, SUSPECTED FROM LWR CARGO BUT CANNOT ISOLATE DUE TO RAPID ONSET AIR DIVER T TO MSP. REMOVED AND REPLACED FIRE WARNING CIRCUIT CARD A8 ON M825 PER MM 26-10-01 AND TESTED PER MM 26-16-00. GRD CH ECKS NORMAL. PN ON OFF - 69B47519-3, NSN ON/OFF. PLEASE NOTE L/P 011538 ITEM 2 AND 3. 2 L 7 4 4F A20WE 1998052200861 19980522 00861 WP 1998 5 22 UPS98826660 1 19980415 A 5230 SKIN DOUG DC8 DC871F 302199D WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C, C4 DOOR LOWER FWD CORNER ABOVE SCUFF PLATE GLS CRACK FROM EDGE TO RIVET. REMOVED DAMAGE IAW DC8 SRM 53 2 0, FABBED REPAIR DOUBLER FILLER IAW D C8 SRM 53 2 0 AND 51 1 20D. ALODINED AND PRIMED REPAIR DOUBLER AND FILLER IA W DC8 SRM 51 1 8. FABBED TRIPLER IAW DC8 SRM 51 1 20D AND 53 20. INSTALLED INTERCOSTAL IAW DC8 SRM 51 1 20D, WELD REPA IRED SCUFF PLATE IAW DPS 10225 LOCATED DRILLED HOLES INSTALLED SCUFF PLATE. 2 L 7 4 4F RT 4A25 1998052200862 19980522 00862 WP 1998 5 22 UPS98826674 1 19980415 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, FITTING AT LONGERON 17 RIGHT TO FRAME STA 1200 CRACKED. INSTALLED NEW FITTING IAW DC8 SRM 51 1 20 D. 2 L 7 4 4F RT 4A25 1998052200863 19980522 00863 WP 1998 5 22 UPS98826712 1 19980512 A 5320 37502571N FITTING DOUG DC8 DC873F 302199F WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, LONGERON SPLICE FITTING BETWEEN STA 1040-1060 LONG 31R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052200864 19980522 00864 WP 1998 5 22 UPS98826713 1 19980513 A 5320 37502571N FITTING DOUG DC8 DC873F 302199F WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, STA 440-460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052200865 19980522 00865 WP 1998 5 22 UPS98826714 1 19980513 A 5320 37502571N FITTING DOUG DC8 DC873F 302199F WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, STA 440-460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052200866 19980522 00866 WP 1998 5 22 UPS98826715 1 19980514 A 5320 97540241 FITTING DOUG DC8 DC873F 302199F WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, MAIN DECK FLOORBEAM SUPPORT FITTING AT STA 1200 AND STR 27R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998052200867 19980522 00867 WP 1998 5 22 UPS98826717 1 19980511 A 5712 5769857614 RIB DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, THE RIGHT OUTBOARD SLOT OUTBOARD UPPER CLOSURE RIB IS CRACKED. REMOVED AND REPLACED CLOSURE RIB IAW DWG 5769857 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998052200868 19980522 00868 WP 1998 5 22 UPS98826718 1 19980513 A 5720 5769857375 BRACKET DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, RT LEADING EDGE BETWEEN NR 3 AND NR 4 ENG OUTBOARD SLOT ATTACH BRACKET TO STUB WING RIB IS CRACKED. R EMOVED, FABRICATED AND REPLACED IAW DWG 5769857 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998052200869 19980522 00869 WP 1998 5 22 UPS98826719 1 19980509 A 5311 3646688506 FRAME DOUG DC8 DC873F 302199F WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, STA 660 AT STR 22R, THE FRAME HAS A 3 INCH CRACK. REMOVED, FABRICATED AND REPLACED FRAME CAP IAW DWG 3646688 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998052200870 19980522 00870 NM 1998 5 22 UPS98226733 1 19980513 A 5711 SPAR CHORD BOEING 727 72725C 138400H NM WS 462-464 CRACKED A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C, CRACK INDICATION NOTED ON RT WING UPPER REAR CHORD FROM WS 462 TO WS 464 (APPROX). CRACK INDICATION WAS CORROSION WS 457-470. REPAIRED PER SRM 57-10-6 FIG 3 AND DWG 65C19647 CAT II REPAIR. 2 L 7 3 4F A3WE 1998052200871 19980522 00871 NM 1998 5 22 UPS98226734 1 19980515 A 5751 652176618 AILERON BOEING 727 72725C 138400H NM RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C, R/W O/B AILERON I/B FITTING ON AILERON CORRODED AT ACTUATOR MOUNT ATTACHMENT. REMOVED AND REPLACED A ILERON IAW MM 27-10-31. 2 L 7 3 4F A3WE 1998052200872 19980522 00872 NM 1998 5 22 UPS98226735 1 19980514 A 5754 651622684 FLAP BOEING 727 72725C 138400H NM NR 5 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C, NR 5 K-FLAP NOSE FLAP TO K-FLAP BONDING JUMPER BOLTS HOLES ARE CORRODED. REMOVED AND REPLACED K-FLAP ASSEMBLY DUE TO NO FLAP NOSE ASSEMBLY AVAILABLE PER MM 27-81-01. 2 L 7 3 4F A3WE 1998052200873 19980522 00873 NM 1998 5 22 UPS98226736 1 19980514 A 5751 651926012 FITTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C, CORROSION ON RIGHT WING OUTBD AILERON CENTER INBD FIXED TRAILING EDGE HINGE FITTING. REMOVED AND REP LACED HINGE FITTING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998052200874 19980522 00874 NM 1998 5 22 UPS98226737 1 19980514 A 5751 65129596 HINGE FITTING BOEING 727 72725C 138400H NM RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C, CORROSION ON RIGHT WING OUTBD AILERON CENTER OUTBD FIXED TRAILING EDGE HINGE FITTING. REMOVED AND RE PLACED HINGE FITTING IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998052200875 19980522 00875 NM 1998 5 22 UPS98226738 1 19980507 A 5312 BULKHEAD FRAME BOEING 727 72751C 1384015 NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, FRAME ON FWD SIDE OF B/H 351 LT SIDE IS CORRODED BETWEEN STR 22 AND 23. FRAME REPAIRED IAW SRM 53-10 -4 FIG 13. 2 L 7 3 4F A3WE 1998052200876 19980522 00876 WP 1998 5 22 UPS98826720 1 19980509 A 5311 52641520 FRAME DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, FRAME AT LWR FLANGE AT STA 1580 HAS HEAVY CORROSION BETWEEN LONG 35L - 35R. REPAIRED AREA BY REPLAC EMENT AND SPLICING IAW SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998052200877 19980522 00877 WP 1998 5 22 UPS98826721 1 19980513 A 5320 37584972 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, LONGERON TO INTERCOSTAL TIE FITTING AT STA 1180 AND LONG 35R IS CRACKED. REMOVED AND REPLACED FITTIN G IAW DWG 3758497 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998052200878 19980522 00878 WP 1998 5 22 UPS98826722 1 19980511 A 5347 5759223513 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 980-1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, STA 980-1070 AT STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759229 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052200879 19980522 00879 WP 1998 5 22 UPS98826723 1 19980515 A 5320 3754473501N FITTING DOUG DC8 DC873F 302199F WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, STA 1260-1280, STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND S RM 51-1-20. 2 L 7 4 4F RT 4A25 1998052200880 19980522 00880 WP 1998 5 22 UPS98826724 1 19980515 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, RT WING L/E AT STA XFS 616.250, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998052200881 19980522 00881 WP 1998 5 22 UPS98826725 1 19980515 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 621 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, RT WING L/E AT STA XFS.621.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998052200882 19980522 00882 WP 1998 5 22 UPS98826726 1 19980416 A 5320 JAMB DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, LEFT AFT ENTRY DOOR JAMB WEB CRACKED AT ATTACH HOLE, TOP AFT CORNER REMOVED DAMAGED WEB, FABRI CATED NEW WEB, REPAIR ANGLES, SPLICES AND BUSHINGS IAW REO 04632. ALODINED AND PRIMED ALL PARTS AND WORK AREA IAW DC8 S RM 51-1-8. INSTALLED NEW WEB, REPAIR ANGLES, SPLICES AND BUSHING IAW REO 04632. 2 L 7 4 4F RT 4A25 1998052200883 19980522 00883 WP 1998 5 22 UPS98826727 1 19980417 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK, FLOORBEAM AT STA 1580 RIGHT HAND TUNNEL AREA CORRODED. REMOVED CORROSION, OUT OF LIMITS IAW DC8 S RM 51-1-8. FABRICATED TWO ANGLES AND FILLERS IAW REO 04682. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. INSTALLED ANGLES AND FILLERS IAW REO 04682. 2 L 7 4 4F RT 4A25 1998052200884 19980522 00884 WP 1998 5 22 UPS98826728 1 19980515 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 666.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, RT WING L/E AT STA XFS.666.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998052200885 19980522 00885 WP 1998 5 22 UPS98826729 1 19980504 A 5320 JAMB DOUG DC8 DC871F 302199D WP L2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 700UP 45900 INSPECTION TYPE:C/CK L2 DOOR JAMB, AFT PAN CRACKED AT UPPER DOOR STOP. CUT OUT DAMAGED SEGMENT OF 9 DOOR PAN IAW REO 04 645. FABRICATED AND DRILLED NEW- 9 PAN SEGMENT AND PAN SPLICE DOUBLERS IAW REO 04645. ALODINED AND PRIMED IAW DC8 SRM 51 1 8. INSTALLED -9 PAN SEGMENT AND PAN SPLICE DOUBLERS IAW DC8 SRM 51 1 20D AND REO 04645. 2 L 7 4 4F RT 4A25 1998052200886 19980522 00886 WP 1998 5 22 UPS98826730 1 19980515 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, RT WING L/E AT STA XFS635.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998052200887 19980522 00887 WP 1998 5 22 UPS98826731 1 19980514 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 397.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, LT WING L/E AT STA XFS397.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998052200888 19980522 00888 WP 1998 5 22 UPS98826732 1 19980514 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 280-340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, LONGERON 29L AND 30L BETWEEN STA 280-340 EACH HAVE HEAVY CORROSION. REPAIRED AREAS IAW SRM 53-2-2 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998052200889 19980522 00889 WP 1998 5 22 UPS98826739 1 19980510 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 710 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, LT WING L/E LWR SURFACE HAS HEAVY CORROSION 3 INCHES AFT OF L/E AT STA XFS710.000. REPAIRED AREA IAW SRM ADDENDUM DC8-5720-4087-A. 2 L 7 4 4F RT 4A25 1998052200890 19980522 00890 WP 1998 5 22 ABXA00454 1 19980519 A 3230 RETRACT MECH DOUG DC8 DC861 3021952 WP NLG DOOR LACK OF LUBE A ABXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 845AX 46157 AFTER TAKEOFF WHEN LANDING GEAR RETRACTED, HEARD LOUD RUMBLING NOISE FROM NOSE GEAR AREA. ALL RETRACTION INDICATIONS WE RE NORMAL. RECYCLED GEAR THREE TIMES WITH SAME RESULT. GEAR FAILED UPLATCH CHECK. AIR TURNED BACK TO ONT. NOSE LANDI NG GEAR DOOR WAS OPEN ON TAXI-IN. INSPECTED AND LUBRICATED NOSE LANDING GEAR CABLES AND LINKAGE. NO DEFECTS NOTED. PE RFORMED NOSE GEAR OPERATIONAL CHECK. GEAR AND DOORS OPERATED PROPERLY. UPLATCH CHECK WAS GOOD IAW DC8 MM 32-31-6. 2 L 7 4 4F 4A25 1998052200891 19980522 00891 WP 1998 5 22 MWEA98596 1 19980508 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP CABIN DOOR FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 BDL - FLT 149 - THE GALLEY SLIDE COVER FELL OFF. MAINTENANCE REPACKED GALLEY SERVICE DOOR ESCAPE SLIDE. (M) 2 L 7 2 4F A6WE 1998052200892 19980522 00892 WP 1998 5 22 MWEA98597 1 19980514 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP FWD GALLEY FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 502ME 48132 MKE - FLT 207 - THE GALLEY DOOR EMERGENCY SLIDE COVER DISLODGED. MAINTENANCE INSTALLED GALLEY DOOR SLIDE COVER. (M) 2 L 7 2 4F A6WE 1998052200893 19980522 00893 WP 1998 5 22 MWEA98598 1 19980516 A 5720 5910041504 VANE DOUG DC9 DC914 3022034 WP RT WING DELAMINATION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 MKE - FOUND DELAMINATION ON RIGHT FLAP INBOARD FIXED VANE ON UPPER SKIN AT STATION XRS 134. MAINTENANCE REMOVED DELAMIN ATION FABRICATED AND INSTALLED DOUBLER. (M) 2 L 7 2 4F A6WE 1998052200894 19980522 00894 WP 1998 5 22 MWEA98599 1 19980515 A 5720 5910041504 VANE DOUG DC9 DC914 3022034 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 MKE - FOUND A DEEP CHAFE IN RIGHT INBOARD FIXED VANE UPPER SKIN AT STATION XRS 164. MAINTENANCE FABRICATED AND INSTALLE D REPAIR DOUBLER. (M) 2 L 7 2 4F A6WE 1998052200895 19980522 00895 NM 1998 5 22 DHL98727003 1 19980125 A 5720 65179113 FITTING BOEING 727 727228 NM WS 543 BROKEN A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 727DH 20204 AIRFRAME VIBRATION AND BUFFETING DURING LEFT TURNS. REPLACED BROKEN CHANNEL FITTING COVE PANEL WING STA 521 I/B SIDE. R EPLACED AND ADJUSTED BROKEN ROD END IN LT COVE PANEL ASSY STA 543. INSTALLED MISSING NUT, WASHER, IN RT I/B FLAP CARRIA GE TRACK ROLLER BEARING PER MM 57-20-0 AND 57-52-0. 2 L 7 3 4F A3WE 1998052200896 19980522 00896 WP 1998 5 22 RRXA9809 1 19980514 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 192 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A JOINT FAA INSPECTION AND EMERY MAINTENANCE PERSONNEL, FOUND .5 INCH CRACK ON RIGHT WING LEADING EDGE AT XFS 192 . STOP DRILLED ENDS OF CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E6 3-B01 REV 1B. 2 L 7 4 4F RT 4A25 1998052200897 19980522 00897 WP 1998 5 22 ARWA980504 1 19980512 A 2770 3653163527 WIRE ROPE DOUG DC8 DC863F 302198F WP GUST LOCK BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 SJU - FLT 510 - ON PRE-DEPARTURE CHECK, FOUND MANUAL REVERSION LIGHT ON WITH GUST LOCK LOCKED. FABRICATED GUST LOCK CAB LE RUN IAW MM 91-10-22. INSTALLED IAW MM 27-70-0, OPS CHECKED NORMAL. (M) 2 L 7 4 4F 4A25 1998052200898 19980522 00898 WP 1998 5 22 ARWA980505 1 19980514 A 2822 11250803 BOOST PUMP LKHEED 1011 1011385115 5265015 WP LEFT SHORTED A ARWA K NONE J WARNING INDICATION IN INSP/MAINT 1 SO 19 307GB 1214288 193U131 MIA - FLT 501 - TANK NR 1 LEFT FUEL BOOST PUMP LOW PRESS LIGHT ILLUM PUMP INOP. THIS WAS PLACED ON DMI. AFTER REFUELIN G AIRCRAFT, A FUEL LEAK WAS NOTED AT THE 1 LEFT FUEL BOOST PUMP. FURTHER INVESTIGATION REVEALED BURNED ELECTRICAL CONNE CTORS HOLES IN THE PUMP HOUSING, ARC BURNED AND INDICATIONS OF SEVERELY HEATED WIRING. PUMP HOUSING ASSY, PUMP ELECTRIC AL HARNESS, WIRING HARNESS AND PUMP ASSY AND OPS CHECK OK IAW MM 28-24-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A23WE 1998052200899 19980522 00899 WP 1998 5 22 CKSA98295 1 19980513 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 618 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 108CK 193N1204 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION FS 618 STR 32 HAS CORROSION. REMOVED CORROSION IAW L1011 SRM 51 -21-01 FOUND TO BE OUT OF LIMITS IAW L1011 SRM 53-13-00. REPAIRED STRINGER IAW L1011 SRM 53-13-00 FIG 803. CORROSION T ASK CARD NUMBER C53-120-04-01. NON ROUTINE TASK CARD NUMBER 22658. 2 L 7 3 4F A23WE 1998052200900 19980522 00900 WP 1998 5 22 CKSA98296 1 19980513 A 5347 SEAT TRACK LKHEED 1011 1011385115 5265015 WP BS 1625 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 108CK 193N1204 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, C2 THRESHOLD CARGO HOLD DOWN TRACK JUST FWD OF BS 1625, TRACK I S CRACKED AND TWO SCREWS SHEARED. REPLACED FASTENERS IAW L1011 SRM 51-40-01. REPAIRED CRACKED HOLD DOWN IAW L1011 SRM 51-50-04. TREATED AND PRIMED IAW L1011 SRM 51-21-02 AND MM 20-51-09. INSTALLED REPAIR IAW L1011 SRM 51-50-04. CORROSI ON TASK CARD NUMBER C53-150-02-03. NON ROUTINE TASK CARD NUMBER 22683. 2 L 7 3 4F A23WE 1998052200901 19980522 00901 WP 1998 5 22 CKSA98297 1 19980503 A 3350 516574 POWER PACK LKHEED 1011 1011385115 5265015 WP R2 DOOR INOPERATIVE A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 109CK 193N1205 DURING TERMINATING SERVICE INSPECTION, FOUND DOOR 2R EMERGENCY EXIT LIGHTS AND IDENTIFIERS NO TEST. REMOVED AND REPLACE D EMERGENCY POWER PACK, OPS CHECK GOOD IAW MM 33-51-00. NON ROUTINE ITEM NR 16. 2 L 7 3 4F A23WE 1998052200902 19980522 00902 WP 1998 5 22 CKSA98298 1 19980503 A 3350 873100211 SIGN LKHEED 1011 1011385115 5265015 WP L1 DOOR MALFUNCTION A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 109CK 193N1205 DURING TERMINATING SERVICE INSPECTION, FOUND L1 EMERGENCY EXIT IDENTIFIER DOES NOT TEST. BATTERY NO HELP. REMOVED AND REPLACED L1 EMERGENCY EXIT IDENTIFIER ASSEMBLY, SYSTEM OPS CHECK GOOD IAW MM 33-51-04. NON ROUTINE ITEM NR 18. 2 L 7 3 4F A23WE 1998052200903 19980522 00903 WP 1998 5 22 CKSA98299 1 19980427 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 490 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING ROUTINE B CHECK INSPECTION, FOUND SEAT TRACK STA 490 RBL25 CORRODED. REMOVED AND REPLACED SEAT TRACK PER DC-8 SR M 53-02-3. NON ROUTINE TASK CARD NUMBER 23625. 2 L 7 4 4F 4A25 1998052200904 19980522 00904 WP 1998 5 22 CKSA98300 1 19980427 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 100 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING ROUTINE B CHECK INSPECTION, FOUND FS 100 AT STR 33L SKIN HAS CRACK. REPAIRED SKIN IAW DC-8 SRM 53-2-1 FIG 7. CLA SS II REPAIR INSTALLED. REPAIR MUST BE RE-INSPECTED EVERY 4000 LANDINGS AND REPLACED WITHIN 24,000 LANDINGS IAW DC8 SRM 53-2-1 PARAGRAPH 16. (INITIAL INSPECTION DUE 12,000 LANDINGS). NON-ROUTINE TASK CARD NUMBER 23570. 2 L 7 4 4F 4A25 1998052200905 19980522 00905 WP 1998 5 22 CKSA98301 1 19980427 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 70 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 DURING ROUTINE B CHECK INSPECTION, FOUND RIVET PULLED FS 70 STRINGER 23R. REPAIRED SKIN IAW DC-8 SRM 53-2-1 FIG 7. CLA SS II REPAIR INSTALLED. REPAIR MUST BE RE-INSPECTED EVERY 4000 LANDINGS (INITIAL INSPECTION OF 12,000 LANDINGS) AND REP LACED WITH CLASS I REPAIR WITHIN 24,000 LANDINGS IAW DC8 SRM 53-2-1 PARAGRAPH 16. NON ROUTINE TASK CARD NUMBER 23457. 2 L 7 4 4F 4A25 1998052200906 19980522 00906 WP 1998 5 22 CKSA98302 1 19980506 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 332 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 868BX 46034 DURING ROUTINE B CHECK INSPECTION, FOUND NR 2 SEAT TRACK STA 332 WORN. REMOVED DAMAGED SECTION OF SEAT TRACK, SPLICED I N NEW SECTION OF SEAT TRACK IAW DC-8 SRM 53-2-3. NON-ROUTINE TASK CARD NUMBER 23935. 2 L 7 4 4F 4A25 1998052200907 19980522 00907 WP 1998 5 22 CKSA98303 1 19980506 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP CABIN BROKEN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 868BX 46034 DURING ROUTINE B CHECK INSPECTION, FOUND P-1-1 SEAT TRACK BROKEN. REMOVED DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION IAW DC-8 SRM CHAPTER 53-2-3. NON-ROUTINE TASK CARD NUMBER 23703. 2 L 7 4 4F 4A25 1998052700004 19980527 00004 NE 1998 5 27 SWIA971090 2 19980224 A 7320 HMU EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENGINE MALFUNCTIONED A A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 291SW 120318 ON TAKEOFF AT 5000 MSL, EXPERIENCED AN UNCOMMANDED TORQUE INCREASE WITH AN EEC FAILURE LIGHT ON THE LEFT ENGINE. TORQUE VALUE WENT TO 130 PERCENT FOR APPROXIMATELY 5 SECONDS BEFORE WE COULD GET AIRCRAFT POWER LEVER RETRACTED AND THE EEC SW ITCH OFF. RETURNED TO SLC. REPLACED LEFT HMU AND EEC. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052700005 19980527 00005 NM 1998 5 27 P5CA9800269 1 19980218 A 5753 FAIRING BOEING 747 747128 1384894 NM NR 2 CANOE SPONGY A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 3203Y 19751 LEFT WING NR 2 CANOE FAIRING MIDDLE LOWER AREA FOUND SPONGY. FIBERGLASS REPAIRED PER SRM 51-40-14. 2 L 7 4 4F A20WE 1998052700006 19980527 00006 1998 5 27 P5CA9800352 4 19980223 A 3441 7886580011 INU BOEING 747 747249F 1384849 NM NR 1/2 FAILED A P5CA A J UNSCHED LANDING DUMP FUEL G MULTIPLE FAILURE CL CLIMB 1 WP 23 920FT 22237 NR 1 INS FAILED AT LIFTOFF. NR 2 INS RED WING LIGHT ILLUMINATED AT 2000 FT AGL AFTER TAKEOFF. JETTISONED FUEL TO LAND UNDER MAX LNDG WEIGHT. REMOVED AND REPLACED NR 1 INU IAW BACOMM34-41-03. REMOVED AND REPLACED NR 2 INU IAW BACOMM 34-4 1-03. OPS CK OK. 2 L 7 4 4F A20WE 1998052700007 19980527 00007 WP 1998 5 27 MWEA98241 1 19980427 A 5320 4912772 FITTING DOUG DC9 DC932 3022066 WP BS 218-237 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 THE CUSP SPLICE FITTING AT FS 218 TO FS 237 WERE FOUND CORRODED. REMOVED AND REPLACED DAMAGED FITTING. 2 L 7 2 4F A6WE 1998052700008 19980527 00008 WP 1998 5 27 CALA9800714 1 19980428 A 5350 CABLES DOUG DC9 DC983 3022083 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14879 49526 THE TAILCONE HUNG UP ON AFT UPPER LATCH WHEN DEPLOYED AND THE TAILCONE RELEASE EXTERIOR HANDLE HUNG UP ON LOWER EDGE OF OPENING. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-53-00. IN ADDITION, THE SIDE CLIP ON FORWARD SIDE WAS STRAIGHTENE D. 2 L 7 2 4F RT A6WE 1998052700009 19980527 00009 NM 1998 5 27 DHL98726118 1 19980228 A 5400 S-DUCT BOEING 727 727228 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 20409 AT D CHECK, NR 2 ENGINE INLET DUCT FWD EDGE CRACKED AND SEVERAL GOUGES BETWEEN 4-6 O'CLOCK. CUT OUT DAMAGED AREA, INSTA LLED DOUBLER REPAIR PER SRM 54-10-3, 14 BY 5. CUT OUT DAMAGED AREA FROM 4-6 O'CLOCK AND INSTALLED DOUBLER REPAIR PER SR M 54-10-3, 19 BY 3. N/R 6279. 2 L 7 3 4F A3WE 1998052700010 19980527 00010 NM 1998 5 27 DHL98726123 1 19980228 A 5400 S-DUCT BOEING 727 727228 NM NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 726DH 9 20409 AT D CHECK, NR 2 ENGINE INLET S DUCT FWD EDGE CRACKED AT 9 O'CLOCK. REMOVED FASTENERS AND TRIMMED OUT DAMAGED AREA. IN STALLED DOUBLER REPAIR PER SRM 54-10-3, 11 BY 2.5. N/R 6280. 2 L 7 3 4F A3WE 1998052700011 19980527 00011 WP 1998 5 27 RRXA98079 1 19980421 A 3411 4714037521 STATIC HOSE DOUG DC8 DC8F54 3021926 WP LEFT COLLAPSED A RRXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 991CF 45801 CAPT'S ALTIMETER IS STUCK AT 500 FEET. FOUND STATIC HOSE ASSY FROM CAPTS STATIC SOURCE SELECTOR TO MANIFOLD MOUNTED ON BACK OF INSTRUMENT PANEL TO BE PARTIALLY COLLAPSED. REMOVED AND REPLACED LINE SYSTEM CK NORMAL. PITOT STATIC LEAK CHEC K PERFORMED. 2 L 7 4 4F 4A25 1998052700013 19980527 00013 EU 1998 5 27 HEEA0014039 1 19980429 A 6710 1054537110 BEARING 10545371 BOLKMS 105 BO105S 5626006 EU MIXING LEVER UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 911HM S683 TEFLON UNBONDING FROM BEARING. REPLACED WITH NEW BEARING. 1 G 7 2 3U H3EU 1998052700016 19980527 00016 NM 1998 5 27 CALA9800752 1 19980505 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 535 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 FLOOR SUPPORT AT STA 535 LBL 8 OUT OF LIMITS. FORMED ANGLE FROM 7075-0 PER SRM 51-40-3. HEAT TREAT PER BCA 5602. TRAT ED, PRIMED AND INSTALLED PER SRM 51-10-2, 51-40-3, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998052700017 19980527 00017 NM 1998 5 27 CALA9800753 1 19980505 A 5510 652240331 ACCESS PANEL BOEING 727 727224 1384076 NM LT HORIZ STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 HORIZ STAB ELEVATOR PCU ACCESS PANEL DELAMINATED 3 X 10. CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER AND BONDED TO PANEL PER SRM 55-20-3 AND 51-40-5. 2 L 7 3 4F A3WE 1998052700018 19980527 00018 NM 1998 5 27 CALA9800754 1 19980505 A 7120 APRON BOEING 727 727224 1384076 NM NR 1 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69741 22250 NUMBER ONE ENGINE FORWARD APRON CRACKED AT RIVET HEAD IN LOWER AFT CORNER (.5). REMOVED CRACKED DOUBLER. FABRICATED, T REATED, PRIMED, AND INSTALLED DOUBLER AFTER REMOVING CRACKED AREA PER SRM 51-40-2, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998052700019 19980527 00019 NM 1998 5 27 CALA9800755 1 19980505 A 3350 1001141 LIGHT BOEING 727 727224 1384076 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69741 22250 AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT AIRSTAIR EMERGENCY EXIT LIGHT PER MM33-50-61. 2 L 7 3 4F A3WE 1998052700023 19980527 00023 EU 1998 5 27 MALA976122 1 19980429 A 5330 SKIN SAAB SF340 SF340A 7850100 EU BS 634 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 112XJ 340A112 DURING HEAVY CHECK, LOCATED DENT IN FUSELAGE STA 634. MAINTENANCE COMPLETE STEP 3.2.1 FOR THE DYE PENETRANT/EDDY CURREN T INSPECTION OF THE SURROUNDING PANEL AND ADJACENT AND WEB AREAS OF FRAME AT STA 632.112, REF NTM 51-08-00 AND 51-06-00. REFERENCE STEP 3.3.2 IF NO FURTHER DAMAGE IS NOTED THE SENT IS SMOOTH, IT CAN BE ACCEPTED AS IS. NO FURTHER ACTION IS REQUIRED. 2 L 7 2 4T RT A52EU 1998052700025 19980527 00025 WP 1998 5 27 VJ9800148 1 19980507 A 5101 STRUCTURE DOUG DC9 DC932 3022066 WP AIRFRAME DAMAGED A ZZDA A UNSCHED LANDING C F.O.D. CR CRUISE 1 SO 15 948VV 47559 MAJOR HAIL DAMAGE ENCOUNTERED INFLIGHT TO MIDWAY AND DECLARED AN EMERGENCY LANDING, DIVERTED INTO CHA, TN. LANDED IN CH A SAFELY AND DEBORDED PAX AT GATE. PRELIMINARY REPORT BY CAPT- RADOME, ANTENNA FUSELAGE, FLIGHT CONTROLS AND AT LEAST N R 2 ENGINE FOD. WINDSHIELDS SHATTERED 3 EA. NO DEPRESSURIZATION. 2 L 7 2 4F A6WE 1998052700026 19980527 00026 NM 1998 5 27 DL72S980963 1 19980505 A 2612 FIRE LOOP BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SO 27 400DA 62779 21144 687678 NR 1 ENGINE FIRE INDICATION IN FLIGHT. FOUND 13TH STAGE FLANGE GASKET LEAK. REPLACED GASKET. FOUND 8TH STATE DUCT LEA K. SECURED DUCT, REPLACED NR 1 FIRE LOOP CONNECTORS AND CHECKED RESISTANCE REPLACED NR 1 LWR FIRE LOOP. REPLACED NR 1 FIRE DETECTOR CONTROL UNIT. REPLACED NR 1 FIRE HANDLE. REPLACED NR 1 FIREWALL DETECTOR AND CONNECTORS. RAN ENGINE, A LL CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998052700027 19980527 00027 NM 1998 5 27 DHL9870712C 1 19980430 A 5755 FITTING BOEING 727 72722 1384002 NM NR 10 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 707DH 18321 AT C-CHECK, CRACK INDICATION AT R/W INBD T/E FLAP CAVITY NR 10 SPOILER INBD HINGE SUPPORT FITTING. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-30-2. N/R 2777 2 L 7 3 4F A3WE 1998052700030 19980527 00030 NM 1998 5 27 ASAA9840047 1 19980306 A 5330 SKIN BOEING 737 7374Q8 NM BS 1138 DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 784AS 28199 SEA - DURING C-CHECK, FOUND DAMAGE ON THE FUSELAGE CUTOUTS FOR THE APU ACCESS DOOR HINGE. REPAIRED PER EA 5380-01006 AN D BOEING TELEX ASA-SEA-98-0069RR. (M) 2 L 7 2 4F RT A16WE 1998052700031 19980527 00031 NM 1998 5 27 DL73E981013 1 19980512 A 5315 654510223 FLOORBEAM BOEING 737 737247 138448D NM BS 665 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 378DL 23605 THE UPPER CAP OF THE BL 0.07 CENTER WING BOX FLOORBEAM WAS FOUND SEVERED AT STA 665. THE WEB AND WEB DOULBER WERE ALSO FOUND CRACKED AT THIS LOCATION. THE BEAM WAS REPAIRED PER BAC S/B 737-57-1210 AND DOCUMENTED PER ER/A 364760-14, REV A. 2 L 7 2 4F A16WE 1998052800001 19980528 00001 EU 1998 5 28 WWMA9800085 1 19980514 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A WWMA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 15 341SB 340B341 DURING PREFLIGHT, CREW FOUND THE EXIT SIGN OVER THE MAIN CABIN DOOR HAD FALLEN OFF. MAINTENANCE ADJUSTED CLIPS ON THE E MERGENCY EXIT SIGN AND REINSTALLED. 2 L 7 2 4T RT A52EU 1998052900001 19980529 00001 EU 1998 5 29 AALA980789 1 19980416 A 5320 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU FR 72 TO FR 76 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 FLOOR SUPPORT CRACKED. REPLACED LONGITUDINAL BEAM P/N A53279222200 PER SRM 51-72-10. TST: 27,077.37 HOURS. CYCLES: 1 0,835. (X) 2 L 7 2 4F RT A35EU 1998052900002 19980529 00002 EU 1998 5 29 AALA980778 1 19980415 A 5320 SUPPORT BEAM AIRBUS 300 A300B4605R 3930308 EU BS 4744 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 CORROSION ON U-LAV ANCHOR POINTS LAV SUPPORT NR 5A AND NR 6 JUST AFT OF FR 74. REMOVED AND REPLACED U-LAV SUPPORT BEAM BETWEEN NR 5A AND NR 6 TRACKS/LAV SUPPORTS AND REMOVED AND REPLACED ANCHOR MOUNT FITTINGS ON BEAM PER SRM 51-72-10-0. TS T: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900003 19980529 00003 EU 1998 5 29 AALA980779 1 19980415 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU AFT CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON NR 5 TRACK JUST FORWARD OF FR 72. REMOVED AND REPLACED NR 5 TRACK FROM FR 71 TO FR 74 PER SRM 51-72- 10-0. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900004 19980529 00004 EU 1998 5 29 AALA980780 1 19980415 A 5320 SUPPORT BEAM AIRBUS 300 A300B4605R 3930308 EU BS 4600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON FORWARD LAV 'U' MOUNT SUPPORT BEAM AT STA 4600 BETWEEN NR 5A AND NR 6 SEAT TRACKS/LAV SUPPORTS. REMO VED AND REPLACED SUPPORT BEAM PER SRM 51-72-10-0. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900005 19980529 00005 EU 1998 5 29 AALA980777 1 19980415 A 5320 SUPPORT BEAM AIRBUS 300 A300B4605R 3930308 EU BS 4600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON FORWARD LAV U-MOUNT SUPPORT BEAM BETWEEN FLOOR TRACKS NR 6 AND NR 6A IN AREA BETWEEN FR 71 AND FR 72. REMOVED AND REPLACED LAV SUPPORT BEAM PER SRM 51-72-10-0, ALODINZED, PRIMED, AND PAINTED SUPPORT BEAM PER SRM 51-21-00 -0. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900006 19980529 00006 EU 1998 5 29 AALA980785 1 19980415 A 5320 SUPPORT BEAM AIRBUS 300 A300B4605R 3930308 EU BS 4600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON LAV V-MOUNT SUPPORT BEAM BETWEEN TRACKS/FLOOR SUPPORTS NR 4 AND NR 5 IN AREA BETWEEN FR 71 AND FR 72. REPLACED SUPPORT BEAM PER SRM 51-72-10 AND SRM 51-21-00 AND AARD 51-10-00-3. (X) 2 L 7 2 4F RT A35EU 1998052900007 19980529 00007 NM 1998 5 29 AALA980831 1 19980426 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325AA 22326 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT GALLEY MID-FLOOR INOPERATIVE. REPAIRED EMERGENCY EXIT L IGHT BROKEN WIRE AT MID-GALLEY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900008 19980529 00008 NM 1998 5 29 AALA980829 1 19980424 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324AA 22325 SFO - DURING OVERNIGHT MAINTENANCE, RIGHT HAND EMERGENCY EXIT PATH LIGHTS FROM SEAT ROW 31H AFT INOPERATIVE. REPAIRED W IRE AT AFT RIGHT EMERGENCY EXIT DOOR SIGN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900009 19980529 00009 NM 1998 5 29 AALA980794 1 19980418 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7375A 25202 ORY - FLT 0062 - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH MARKING LIGHTS INOPERATIVE AT PASSENGER SEAT 3 6H. PERFORMED EMERGENCY EXIT TEST, UNABLE TO DUPLICATE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900010 19980529 00010 NM 1998 5 29 AALA980795 1 19980419 A 3350 0201820001 LIGHT BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306AA 22312 JFK - DURING OVERNIGHT MAINTENANCE, MID-GALLEY WALL MOUNTED EMERGENCY LIGHT ASSEMBLY BROKEN. REPLACED MID-GALLEY WALL M OUNTED EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900011 19980529 00011 NM 1998 5 29 AALA980781 1 19980415 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374AA 25201 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 27H INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT CONNECTOR AT PASSENGER SEAT 27H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900012 19980529 00012 EU 1998 5 29 AALA980739 1 19980410 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 33069 512 LHR - FLT 0106 - DURING CRUISE, FIRST CLASS OVEN WAS EMITTING SMOKE WHILE HEATING FOOD. REMOVED AND CLEANED OVEN FAN GU ARD ON FIRST CLASS OVEN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998052900013 19980529 00013 NM 1998 5 29 AALA980798 1 19980419 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 378AN 25447 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH MARKING LIGHTS INOPERATIVE AT PASSENGER SEAT 37HJ. REPLA CED EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 37HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900014 19980529 00014 NM 1998 5 29 AALA980797 1 19980419 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 378AN 25447 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 29HJ. REPLACED EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 29HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900015 19980529 00015 NM 1998 5 29 AALA980796 1 19980419 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 378AN 25447 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH MARKING LIGHTS INOPERATIVE AT PASSENGER SEAT 24HJ. REPLA CED EMERGENCY EXIT ESCAPE PATH LIGHT CONNECTOR PASSENGER SEAT 24HJ. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998052900016 19980529 00016 EU 1998 5 29 AALA980758 1 19980413 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU R4 ENTRY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION AROUND 3 EACH SCREW HOLES ON FLOORBOARD SUPPORT BETWEEN FR 73 AND FR 74 IN NR 8 POSITION. INSTALLED NEW SUPPORT AT POSITION NR 8 FROM FR 73 TO FR 74 PER SRM 51-72-10-0. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900017 19980529 00017 EU 1998 5 29 AALA980757 1 19980413 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU R4 ENTRY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON NR 7 SEAT TRACK BETWEEN FR 73 AND FR 74. REMOVED AND REPLACED TRACK NR 7 FROM FR 71 TO FR 74 PER SRM 51-72-10-0. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900018 19980529 00018 EU 1998 5 29 AALA980754 1 19980409 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU 'U' LAV CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON 'U' LAV SUPPORT NR 6A FROM FR 71 TO FR 73 AND AT 'U' LAV MOUNT HOLE FORWARD OF FR 74 ON SAME SUPPORT. REMOVED AND REPLACED SUPPORT FROM FR 71 TO FR 74 IAW SRM 51-72-10-0. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900019 19980529 00019 EU 1998 5 29 AALA980755 1 19980409 A 5347 TIE DOWN AIRBUS 300 A300B4605R 3930308 EU LAV FR 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION AROUND FOWARD LAV TIE-DOWN BOLT HOLE AND ON THE TRACK OUTBOARD EAR AT FRAME 31, TRACK 8 A. REMOVED AND REPLACED BEAM PER SRM 51-72-10, ALODINED, PRIMED AND PAINTED PER SRM 51-21-00-0. TST: 27,077.37 HOURS. CYCLES: 10,83 5. (X) 2 L 7 2 4F RT A35EU 1998052900020 19980529 00020 EU 1998 5 29 AALA980756 1 19980413 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU R4 ENTRY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL CORROSION ON SUPPORT 8A JUST AFT OF FR 73. REPLACED SUPPORT FROM FR 73 TO FR 74 AT POSITION 8A PER SRM 51-72-10-0. (X) 2 L 7 2 4F RT A35EU 1998052900021 19980529 00021 EU 1998 5 29 AALA980645 1 19980330 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BULK CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - CORROSION ON STRINGER SPLICE 54L AT FRAME 65 IN BULK CARGO. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-72-10 . TST: 27,050.02 HOURS. CYCLES: 10,790. (X) 2 L 7 2 4F RT A35EU 1998052900022 19980529 00022 EU 1998 5 29 AALA980646 1 19980330 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BULK CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - CORROSION BETWEEN FRAMES 64 AND 65 AT STR 51L. REMOVED CORROSION ON STR 51L PER SRM 51-74-10. REPLACED STRINGER SPLICE PER SRM 51-72-10. TST: 27,050.02 HOURS. CYCLES: 10,790. (X) 2 L 7 2 4F RT A35EU 1998052900023 19980529 00023 EU 1998 5 29 AALA980542 1 19980330 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BULK CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - CORROSION ON STR 57 FROM FRAMES 65 TO 70. REMOVED AND REPLACED STR 57 FROM FRAMES 65 TO FRAME 70 PER SRM 51-72-10 . TST: 27,050.02 HOURS. CYCLES: 10,790. (X) 2 L 7 2 4F RT A35EU 1998052900024 19980529 00024 EU 1998 5 29 AALA980649 1 19980331 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FORWARD CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - NR 3 ROLLER TRAY CORRODED AT FRAME 38.2. INSTALLED TRACK PER SRM 51-72-10. TST: 27,050.02 HOURS. CYCLES: 10,7 90. (X) 2 L 7 2 4F RT A35EU 1998052900025 19980529 00025 EU 1998 5 29 AALA980648 1 19980330 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FORWARD CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - NR 1 ROLLER TRAY CORRODED SEVERAL PLACES BETWEEN FRAMES 32 AND 37. INSTALLED NEW SECTION OF TRACK PER SRM 51-72-1 0-2. TST: 27,050.02 HOURS. CYCLES: 10,790. (X) 2 L 7 2 4F RT A35EU 1998052900026 19980529 00026 EU 1998 5 29 AALA980651 1 19980330 A 5414 PANEL AIRBUS 300 A300B4605R 3930308 EU NR 2 PYLON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - MILD CORROSION ON PANEL LANDING. REPLACED PANEL PER SRM 51-72-10-0. TST: 27,050.02 HOURS. CYCLES: 10,790. (X ) 2 L 7 2 4F RT A35EU 1998052900027 19980529 00027 EU 1998 5 29 AALA980652 1 19980330 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FORWARD CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - NR 6 ROLLER TRAY CORRODED. REMOVED AND REPLACED ROLLER TRAY PER SRM 53-10-15. TST: 27,050.02 HOURS. CYCLES: 1 0,790. (X) 2 L 7 2 4F RT A35EU 1998052900028 19980529 00028 EU 1998 5 29 AALA980653 1 19980330 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU FORWARD CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - TWO EACH PALLET GUIDE FITTINGS CORRODED. REMOVED AND REPLACED 2 EACH PALLET GUIDE FITTINGS PER SRM 53-10-15. TST : 27,050.02 HOURS. CYCLES: 10,790. (X) 2 L 7 2 4F RT A35EU 1998052900029 19980529 00029 EU 1998 5 29 AALA980654 1 19980330 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FORWARD CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - CORROSION ON SLANT PANEL SUPPORT. REMOVED AND REPLACED SLANT PANEL SUPPORT PER SRM 53-10-15. TST: 27,050.02 HOU RS. CYCLES: 10,790. (X) 2 L 7 2 4F RT A35EU 1998052900030 19980529 00030 EU 1998 5 29 AALA980680 1 19980402 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 0200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 11060 470 TUL - CORRODED FITTING. REMOVED AND REPLACED CORRODED PART. TST: 27,050.02 HOURS. CYCLES: 10,790. (X) 2 L 7 2 4F RT A35EU 1998052900031 19980529 00031 EU 1998 5 29 AALA980765 1 19980331 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 4308 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON STR 55L. REPLACED STRINGER SECTION PER SRM 53-10-14. TST: 25,942 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900032 19980529 00032 EU 1998 5 29 AALA980766 1 19980409 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 4044 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON STR 53L. REPLACED STRINGER SECTION PER SRM 53-10-14-2. TST: 25,942 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900033 19980529 00033 EU 1998 5 29 AALA980767 1 19980409 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 4468 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON STR 48L SPLICE. REPLACED STRINGER SPLICE PER SRM 51-72-10-0. TST: 25,942 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900034 19980529 00034 NM 1998 5 29 AALA980761 1 19980413 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 490-495 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 702AA 22460 TUL - STR 490 - STR 495 AT STR 28R CORROSION ON SIDE OF STRINGER COMPLETE THROUGH STRINGER. FABRICATED STRINGER REPAIR SPLICE AND FILLER AND INSTALLED IAW SRM 53-10-3, FIG 1. TST: 47,528 HOURS. CYCLES: 24,511. (X) 2 L 7 3 4F A3WE 1998052900035 19980529 00035 WP 1998 5 29 AALA980762 1 19980413 A 5753 FLAP TRACK DOUG DC10 DC1030 3023501 WP WS XW118 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - LEFT WING INBOARD FLAP, INBOARD TRACK, ALL BORES (4 EACH) IN ALL POSTS 1, 2, 3, AND 4, ARE CORRODED (16 EACH TOTAL ). (X) 2 L 7 3 4F A22WE 1998052900036 19980529 00036 WP 1998 5 29 AALA980763 1 19980413 A 5753 FLAP TRACK DOUG DC10 DC1030 3023501 WP LT WING INBD CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - LEFT WING INBOARD FLAP, INBOARD TRACK, NR'S 1, 2, AND 4 ATTACH POST FACES CORRODED. BLENDED CORRODED AREAS. CHEC KED FOR CRACKS AND THEN ETCHED FACES WITH NAVEL JELLY, CLEANED, ALODINED AND PRIMED PER AARD 57-20-00-10, PAGE 2. TST: 91,033 HOURS. CYCLES: 18,134. (X) 2 L 7 3 4F A22WE 1998052900037 19980529 00037 WP 1998 5 29 AALA980764 1 19980409 A 5753 FLAP DOUG DC10 DC1030 3023501 WP LT WING OTBD DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - DENT IN LOWER SURFACE OF OUTBORD FLAP APPROX 2 FEET OUTBOARD OF FLAP VANE SPRING CARTRIDGE PANEL. FABRICATED AND INSTALLED DOUBLER PER SRM 57-20-00. TST: 91,033.07 HOURS. CYCLES: 18,134. (X) 2 L 7 3 4F A22WE 1998052900038 19980529 00038 WP 1998 5 29 AALA980782 1 19980415 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 840-859 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - RIGHT GALLEY FLOOR CORRODED. REPLACED FULL LENGTH GALLEY SUPPORT PER AARD 51-10-00. TST: 91,033.07 HOURS. CYCL ES: 18,134. (X) 2 L 7 3 4F A22WE 1998052900039 19980529 00039 WP 1998 5 29 AALA980783 1 19980415 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 475-502 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - LAV 'B' FLOOR SUPPORT CORRODED. REPLACED FLOOR SUPPORT FOR LAV 'B' PER SRM 51-01-00-05. TST: 91,033.07 HOURS. C YCLES: 18,134. (X) 2 L 7 3 4F A22WE 1998052900040 19980529 00040 WP 1998 5 29 AALA980775 1 19980414 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 502 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - LAV 'A' INBOARD AFT HOLD-DOWN HOLE HAS CORROSION. REPLACED FLOOR SUPPORT BEAM PER SRM 51-01-00-05 PAGE 1. ALODIN ED, PRIMED, AND PAINTED. (X) 2 L 7 3 4F A22WE 1998052900041 19980529 00041 EU 1998 5 29 AALA980760 1 19980409 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU 'U' LAV CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON NR 8 TRACK BETWEEN FR 72 AND FR 73. REMOVED AND REPLACED SECTION OF SUPPORT/TRACK PER SRM 51-72-10-0 . TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900042 19980529 00042 EU 1998 5 29 AALA980759 1 19980413 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU LAV 'Z' CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON AFT ANCHOR SUPPORT HOLE FOR LAV 'Z' BETWEEN SEAT TRACKS NR 9 AND NR 10, AND BETWEEN FRAMES 73 AND 74. INSTALLED STRAP ON SUPPORT IN AREA OF ANCHOR HOLE PER AARD 53-20-00-2 AFTER CORROSION WAS REMOVED AND FOUND BEYOND LIM ITS. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900043 19980529 00043 EU 1998 5 29 AALA980786 1 19980415 A 5720 ANGLE AIRBUS 300 A300B4605R 3930308 EU FR 40 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - FRAME 40 LOWER WING ROOT PICKUP ANGLE WAS FOUND TO HAVE 0.8 INCH LONG CRACK. REPLACED PICKUP ANGLE PER ESO 30595 DATED 4-8-98. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900044 19980529 00044 EU 1998 5 29 AALA980787 1 19980405 A 5320 SUPPORT BEAM AIRBUS 300 A300B4605R 3930308 EU CABIN FLOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON LAV SUPPORT BEAM NR 4A FROM FORWARD OF FR 72 - FR 74. INSTALLED FLOOR SUPPORT (NEW) PER SRM 51-72-10 -0 AND SRM 51-21-00-0. (X) 2 L 7 2 4F RT A35EU 1998052900045 19980529 00045 EU 1998 5 29 AALA980788 1 19980415 A 5320 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU FR 71 CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON FLOOR SUPPORT NR 6 BETWEEN FRAMES 71 AND 72. INSTALLED FLOOR SUPPORT (NEW) NR 6 BETWEEN FRAMES 71 AN D 72 PER SRM 51-72-10-0. TST: 27,077 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900046 19980529 00046 EU 1998 5 29 AALA980822 1 19980421 A 5347 ROLLER TRACK AIRBUS 300 A300B4605R 3930308 EU AFT CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION DAMAGE FOUND ON ROLLER TRACK. REPLACED CARGO FLOOR ROLLER TRACK AT POSITION NR 1 BETWEEN FRAMES 54 AND 58. 53-10-15, PAGES 211 AND 212. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900047 19980529 00047 EU 1998 5 29 AALA980801 1 19980416 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 4600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION ON NR 6 SEAT TRACK RT FLOORBOARD FLANGE BETWEEN FRAMES 71 AND 72. CORROSION REMOVED AND BARE METAL WAS ALODINED, PRIMED AND RETURNED TO ORIGINAL FINISH. NO OTHER REPAIRS REQUIRED PER ESO 30595 DATED 4-15-98, REF: SRM 51-2 1-00. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900048 19980529 00048 EU 1998 5 29 AALA980776 1 19980402 A 5320 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU BS 3838 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON SHEAR TIE BETWEEN STR 54L AND STR 55L. REPLACED SHEAR TIE PER SRM 51-72-10. TST: 25,942 HOURS. CY CLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900049 19980529 00049 EU 1998 5 29 AALA980731 1 19980408 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU NOSE GEAR BAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CONNECTING FITTING LEFT SIDE BETWEEN FR 13A AND FR 14A CRACKED AT UPPER OUTBOARD EDGE OF REGION B. BLENDED CRACK AT UPPER OUTBOARD EDGE OF REGION 'B' OF LT CONNECTING FITTING BETWEEN FR 13A AND FR 14A. CORROSION PROTECTED PER SRM 51 -75-10. COMPLETED REPAIR PER ESO 30595 DATED 4-3-98. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900050 19980529 00050 EU 1998 5 29 AALA980732 1 19980408 A 5313 STRINGER SPLICE AIRBUS 300 A300B4605R 3930308 EU FR 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - STRINGER SPLICE AT FRAME 65 TO LEFT IS CORRODED. REMOVED AND REPLACED PER SRM 51-72-10-0. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900051 19980529 00051 EU 1998 5 29 AALA980733 1 19980408 A 5313 STRINGER SPLICE AIRBUS 300 A300B4605R 3930308 EU FR 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - STRINGER SPLICE AT FRAME 65 STRINGER 49L CORRODED. REMOVED AND REPLACED PER SRM 51-72-10-0. TST: 25,942.58 HOUR S. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900052 19980529 00052 EU 1998 5 29 AALA980734 1 19980408 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FR 60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - FLOORBOARD SUPPORT FRAME HAS CORROSION FORWARD SIDE BETWEEN NR 4 AND NR 6 ROLLER TRAYS. SPLICED IN NEW SECTION OF CROSSBEAM 12 INCHES RIGHT OF CENTERLINE TO DOOR FITTING. REF: SRM 53-10-15-2, FIG 207. TST: 25,942 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900053 19980529 00053 EU 1998 5 29 AALA980724 1 19980406 A 5320 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU FR 11 TO 12A CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON FLOOR SUPPORT INBOARD OF COCKPIT DOOR AT FRAME 12. INSTALLED NEW EXTRUSION, ALODINED, PRIMED AND PAI NTED PER SRM 53-12-15-0. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900054 19980529 00054 EU 1998 5 29 AALA980725 1 19980407 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 4308 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON STRINGER 51L. REPLACED STRINGER SECTION PER SRM 53-10-14-2. TST: 25,942 HOURS. CYCLE: 10,261. ( X) 2 L 7 2 4F RT A35EU 1998052900055 19980529 00055 EU 1998 5 29 AALA980726 1 19980407 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 4415 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON STRINGER 49L. INSTALLED NEW STRINGER SECTION PER SRM 53-10-14-2. TST: 25,942 HOURS. CYCLES: 10,2 61. (X) 2 L 7 2 4F RT A35EU 1998052900056 19980529 00056 EU 1998 5 29 AALA980727 1 19980407 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FR 57.2 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CORROSION ON RT SIDE OF LONGERON 56 RT BETWEEN FRAMES 57.2 AND 57.3. BLENDED OUT CORROSION PER SRM 51-74-14-2 AND INSTALLED DOUBLER PER SRM 53-10-14-2. TST: 25,942.58 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900057 19980529 00057 EU 1998 5 29 AALA980708 1 19980406 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU FRAME 61 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - CROSSBEAM END FITTING CORRODED ON FORWARD FLANGE AT TRAY NR 6. INSTALLED DOUBLER REF SRM 53-10-15-2. TST: 25,94 2 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900058 19980529 00058 EU 1998 5 29 AALA980709 1 19980406 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 TUL - STRINGER SPLICE CORRODED AT 48L FRAME 65. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-72-10-0. TST: 25,942 HOURS. CYCLES: 10,261. (X) 2 L 7 2 4F RT A35EU 1998052900067 19980529 00067 EU 1998 5 29 AALA980784 1 19980416 A 5320 INTERCOSTAL AIRBUS 300 A300B4605R 3930308 EU FR 68-69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 18066 509 CORROSION ON INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-72-10. TST: 25,900 HOURS. CYCLES: 10,200. (X ) 2 L 7 2 4F RT A35EU 1998052900068 19980529 00068 EU 1998 5 29 AALA980821 1 19980421 A 5320 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU AFT CARGO CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80058 466 TUL - CORROSION DAMAGE TO FLOOR SUPPORT UNDER ROLLER TRAY. FABRICATE NEW FLOOR SUPPORT PER AARD 51-10-00 AND SRM 53-10- 15, AND INSTALL IN CARGO FLOOR. TST: 27,077.37 HOURS. CYCLES: 10,835. (X) 2 L 7 2 4F RT A35EU 1998052900069 19980529 00069 EU 1998 5 29 MALA976125 1 19980516 A 3350 AML9ILA85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 416XJ 416 DURING INSPECTION, EMERGENCY ARMED LIGHT IN THE CABIN WAS REPORTED BY THE FLIGHT ATTENDANT AS NOT ILLUMINATING WITH THE EMERGENCY LIGHTS ARMED. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998052900070 19980529 00070 SO 1998 5 29 LR7A9823 1 19980520 A 6100 CAP LKHEED 382 382G 526414U SO NR 2 PROP LOOSE A LR7A E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 AL 03 401LC 4606 NR 2 ENGINE SHUTDOWN IN CLIMB AT 1750 Z DUE TO PROP OIL LOW LIGHT ON. RESECURED PRESSURIZED CAP ON NR 2 PROP. RESERVIC ED IAW HAM STD MM PARA 7-10, 7-11 PF 706 AND 707, OPS CHECK NORMAL. 2 H 7 4 4T A1SO 1998052900071 19980529 00071 NM 1998 5 29 CALA9800890 1 19980518 A 5753 69396451 BOLT 6521631323A BOEING 727 727232 1384082 NM LT TE FOREFLAP FAILED A A CALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 14788 23842 20642 WHEN GEAR WAS EXTENDED WITH FLAPS AT 25 DEGREES ON FINAL APPROACH TO JAX, THE AIRCRAFT ROLLED LEFT. THE PILOT MAINTAINE D LEVEL FLIGHT USING FULL RT AILERON AND ALMOST FULL RT RUDDER. THE AIRCRAFT LANDED AT JAX WITHOUT INCIDENT. MAINTENAN CE FOUND AN EIGHT FOOT SECTION OF THE LT OUTBOARD TRAILING EDGE FOREFLAP MISSING. ENGINEERING FOUND AN ATTACHMENT BOLT FOR THE FOREFLAP HAD FAILED. THE REMAINING BOLTS WERE INSPECTED AND FOUND IN GOOD CONDITION. THE LOST SECTION OF FOREF LAP HAS NOT BEEN RECOVERED. THE AIRCRAFT WAS TAKEN OUT OF SERVICE FOR REPAIR. 2 L 7 3 4F A3WE 1998052900072 19980529 00072 NM 1998 5 29 CALA9800891 1 19980519 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1145 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 1145, STRINGER 24L. A REPAIR WAS FABRICATED AND DOUBLERS WERE INSTALLED IAW SRM 51-30-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998052900073 19980529 00073 NM 1998 5 29 CALA9800892 1 19980519 A 2782 BRACKET BOEING 727 727224 1384076 NM LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND A 1 INCH CRACK IN NR 5 LEADING EDGE FLAP AFT INBOARD ACTUATOR MOUNT BRACKET BELOW ACTUATOR TRUNNION. T HE MOUNT BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998052900074 19980529 00074 NM 1998 5 29 CALA9800893 1 19980519 A 5711 SPAR BOEING 727 727224 1384076 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND A 1.5 INCH CRACK ON OUTBOARD SIDE AND A 1.5 INCH CRACK ON INBOARD DOUBLER OF NR 8 SLAT INBOARD ACTUATOR MOUNT AREA OF FRONT SPAR. THE INBOARD DOUBLER WAS REMOVED AND REPLACED AND THE OUTBOARD CRACK WAS STOP DRILLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998052900075 19980529 00075 NM 1998 5 29 CALA9800894 1 19980519 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79749 22451 INSPECTION FOUND A .25 INCH CRACK COMING FROM SCREW HOLE TO ACCESS CUTOUT IN RT ELEVATOR SKIN. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-20-03. 2 L 7 3 4F A3WE 1998052900076 19980529 00076 WP 1998 5 29 CALA9800895 1 19980519 A 5530 ANGLE DOUG DC9 DC982 3022082 WP LT VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND SEVERAL .75 INCH CRACKS IN LT VERTICAL STABILIZER ATTACH ANGLE ABOVE CANTED STA 1463. THE CRACKED AREA S WERE CUT OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 23. 2 L 7 2 4F A6WE 1998052900077 19980529 00077 WP 1998 5 29 CALA9800896 1 19980520 A 2450 FEEDER CABLE DOUG DC9 DC982 3022082 WP BS 218 SHORTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18833 49493 INSPECTION FOUND APU POWER FEEDER CABLE NR 2 SHORTED ON STANDOFF ANGLE CLIP LOCATED IN TAIL COMPARTMENT AT SUPPORT CLAMP BETWEEN AFT PRESSURE BULKHEAD AND TERMINAL BLOCK. THE APU POWER FEEDER CABLE WAS REPLACED FROM T-STRIP STA 218 TO APU T-STRIP IN TAIL COMPARTMENT. 2 L 7 2 4F A6WE 1998052900078 19980529 00078 NM 1998 5 29 CALA9800897 1 19980520 A 5414 SKIN BOEING 737 7373T0 1384582 NM NR 1 ENG PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69351 23589 INSPECTION FOUND A .5 INCH CRACK COMING FROM CUTOUT FOR PANEL 5724 ON INBOARD SKIN OF NR 1 ENGINE PYLON. REPAIRED IAW E CRA 5430-01204. 2 L 7 2 4F RT A16WE 1998052900079 19980529 00079 SO 1998 5 29 COMA9810124 1 19980519 A 2750 3472001001 FCU EMB 120 EMB120RT SO E/E COMPT MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 255CA 17896 3100 120238 FLAP AND ADVANCED SWS INDICATIONS ON MAP. REPLACED THE FLAP CONTROL UNIT. 2 L 7 2 4T RT A31SO 1998052900080 19980529 00080 EA 1998 5 29 COMA9860106 1 19980511 A 3610 NM1024200200 CLAMP CNDAIR CL600 CL6002B19 EA BLEED AIR SYSTEM CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 933CA 7040 A 24, 48 MONTH INSPECTION, BLEED AIR DUCT CLAMP CORRODED. REPLACED CLAMP. 2 L 7 2 4F RT A21EA 1998052900081 19980529 00081 EA 1998 5 29 COMA9860107 1 19980511 A 3350 487190 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 933CA 7040 A 24, 28 MONTH INSPECTION, EMERGENCY FLOOR STRIP LIGHT HAS BROKEN CONNECTORS. REPLACED CONNECTORS. 2 L 7 2 4F RT A21EA 1998052900082 19980529 00082 EA 1998 5 29 COMA9860108 1 19980520 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 917CA 7017 OVERHEAD EMERGENCY LIGHT INOPERABLE AT ROW 10. REPLACED BULB. 2 L 7 2 4F RT A21EA 1998052900083 19980529 00083 EA 1998 5 29 COMA9860109 1 19980519 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 976CA 5801 7151 FLAPS FAIL MESSAGE DURING APPROACH. REPLACED THE LEFT HAND FLAP BPSU. 2 L 7 2 4F RT A21EA 1998052900084 19980529 00084 NM 1998 5 29 98FDEA00354 1 19980519 A 2782 269002911 ACTUATOR BOEING 727 727233 138408A NM NR 3 LE SLAT FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 280FE 22347 AFTER T/O, DURING FLAP RETRACTION FROM 2 DEG TO UP, AMBER LEADING FLAPS LIGHT REMAINED ON, NR 3 SLAT AMBER LIGHT IND INT ERMEDIATE POS, A-SYS HYD QTY OBSERVED AT ZERO. RED TAB CKLT ACCOMPLISHED. SAFETY WIRE BROKEN ON A FLUID S/O VALVES AND GPWS FLAP. UNEVENTFUL LANDING AT STL, GEAR PINNED AND TOWED TO PARKING. SAFETY WIRE BROKEN ON ALT FLAP SW. ZERO QTY AND PRESS. *S/D* REMOVED AND REPLACED NR 1 AND 2 'A' SYS HYD PUMP, REMOVED AND REPLACED NR 1 AND 2 HYD PUMP CASE DRAIN FILTERS, REMOVED AND REPLACED NR 3 L/E SLAT ACT, REMOVED AND REPLACED 'A' HYD RETURN FILTER ASSY. OPS AND FUNCTIONAL C HECKS NORMAL, REMOVED GEAR PINS. 2 L 7 3 4F RT A3WE 1998052900085 19980529 00085 NM 1998 5 29 98FDEA00358 1 19980519 A 2613 OVERHEAT LIGHT BOEING 727 7272S2F 1384O81 NM AFT BODY ILLUMINATED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 203FE 22925 LWR AFT BODY OVHT LIGHT CAME ON DURING CLIMB OUT, LIGHT WAS ON STEADY FOR 30 TO 40 SECONDS, THEN FLICKERED FOR 1 MINUTE, THEN WENT OUT, NR 1 AND 3 ENG BLEEDS WERE OPEN, BOTH PACKS WERE ON. CHECKED ALL CONN ON AFT OVHT LOOP AND RAN ENG AND CK'D FOR HOT AIR LEAKS AS IN FLT MODE, ALL CK GOOD. REMOVE AND REPLACED FIRE DETECTION CONTROL BOX FOR TROUBLESHOOTING PURPOSE, OPS CK GOOD ON GROUND, ALL WORK DONE PER MM 26-14-1. 2 L 7 3 4F A3WE 1998052900086 19980529 00086 NM 1998 5 29 98FDEA00359 1 19980514 A 3211 TRUNNION BOEING 727 727225 1384077 NM LT MLG CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 L/MLG FWD TRUNNION CASTING CORRODED AROUND LWR I/B BUSHING. REMOVED CORROSION, REAMED HOLES, RESURFACED BUSHINGS, FLAP PEENED AND ALODINED, PRIMED, PER FEDEX EA 7-5140-29514. 2 L 7 3 4F A3WE 1998052900087 19980529 00087 NM 1998 5 29 98FDEA00360 1 19980514 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 485 WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 464FE 21288 LWR FWD CARGO GROOVE WORN INTO INSIDE OF STR 26L STA 485. BLENDED DAMAGE, INSIDE STR, INSTALLED STR SPLICE PER SRM 53-1 0-3. 2 L 7 3 4F A3WE 1998052900088 19980529 00088 WP 1998 5 29 MWEA98609 1 19980519 A 2560 591769037 COVER DOUG DC9 DC914 3022034 WP GALLEY SLIDE BROKE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 700ME 45696 THE METAL TIP BROKE OFF GALLEY SLIDE COVER. REMOVED AND REPLACED BRACKET ON DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998052900089 19980529 00089 WP 1998 5 29 MWEA98610 1 19980519 A 5512 SKIN DOUG DC9 DC982 3022082 WP HORIZ STAB MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 809ME 48071 FOUND PREVIOUS REPAIR ON LEFT HAND HORIZONTAL STABILIZER LEADING EDGE INBOARD PANEL. FABRICATED AND INSTALLED REPAIR DO UBLER. 2 L 7 2 4F A6WE 1998052900090 19980529 00090 WP 1998 5 29 RRXA98130 1 19980514 A 5312 576953053 RIB DOUG DC8 DC873F 302199F WP WS 360.25 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND WING, CENTER L/E RIB AT XRS=360.250 HAS 0.5 INCH CRACK. 2 L 7 4 4F RT 4A25 1998052900091 19980529 00091 WP 1998 5 29 RRXA98131 1 19980515 A 7830 305519803 SPACER DOUG DC8 DC873F 302199F WP NR 1 TR UNIT CORRDED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING MAINTENANCE VISIT, FOUND NR 1 PYLON, T/R SPACER (P/N 305-519-803), WORN AND CORRODED AROUND SHAFT AT ATTACH PONIT S. FABRICATED AND INSTALLED NEW T/R SPACER, IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04727. 2 L 7 4 4F RT 4A25 1998052900092 19980529 00092 WP 1998 5 29 RRXA98132 1 19980518 A 5311 97510503 FRAME DOUG DC8 DC873F 302199F WP BS 1610 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME WEB AT STA 1610 AND LONGERON 20 LEFT. REMOVED DAMAGED SECTI ON, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SK ETCH REO-04735. 2 L 7 4 4F RT 4A25 1998052900093 19980529 00093 WP 1998 5 29 RRXA98133 1 19980518 A 5315 2759472 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM 2 EACH LOCATIONS, STA 1700 AT BL 0 AND LBL 34. REMOVED DAMAGED SECTIONS, TREATED AREAS IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED 2 EACH DOUBLER REPAIRS AT BL 0, AND LBL 3 4, IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04736. 2 L 7 4 4F RT 4A25 1998052900094 19980529 00094 WP 1998 5 29 RRXA98134 1 19980518 A 5315 1706317 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1730 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1730 AND LBL 32. REMOVED DAMAGED SECTION, TREATE D AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0 4737. 2 L 7 4 4F RT 4A25 1998052900095 19980529 00095 WP 1998 5 29 RRXA98135 1 19980518 A 5311 5750886501 FRAME DOUG DC8 DC873F 302199F WP BS 600 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO FRAME, INNER FLANGE AT STA 600 AND LONGERON 9 LEFT. FABRICATED AND INS TALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04739. 2 L 7 4 4F RT 4A25 1998052900096 19980529 00096 WP 1998 5 29 RRXA98136 1 19980519 A 5315 5644657501 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 920 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 920 AND RBL 64. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04 740. 2 L 7 4 4F RT 4A25 1998052900097 19980529 00097 1998 5 29 VNAA9805010 4 19980519 A 3418 STICK PUSHER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E COMPT WARNING A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 429JS 3043 DURING THE TAXI FOR TAKEOFF, A STICK PUSHER FAIL WARNING MESSAGE OCCURED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENAN CE INSPECTED AND CYCLED THE AIRCRAFT POWER. AN OPERATIONAL CHECK WAS CARRIED OUT, IN ACCORDANCE WITH DORNIER MAINTENANC E MANUAL 27-33-00. THE OPERATIONAL CHECK WAS SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998052900098 19980529 00098 WP 1998 5 29 TC8A98026 1 19980522 A 7933 CONNECTOR DOUG DC8 DC862F 3021972 WP NR 1 CSD TEMP LOOSE A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 183SK 45904 NR 1 AND NR 2 CSD TEMP REACHED 140 DEGREES ON TAXI. NR 1 ENGINE SECURED LOOSE CANNON PLUG, OPS CHECK OK ON RUN-UP IAW M M 75-20-4. NR 2 ENGINE CSD TEMP, TRANSFERRED TO DMI 8422 MEL 75-1 CAT C. 2 L 7 4 4F 4A25 1998052900099 19980529 00099 SW 1998 5 29 HEEA0014217 1 19980518 A 6240 412075010109 INDICATOR BELL 412 412 1182202 SW TRIPLE TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2298Z 33077 ROTOR NEEDLE INOPERATIVE. 1 G 7 2 4U H4SW 1998052900100 19980529 00100 GL 1998 5 29 HEEA0014218 2 19980518 A 7230 23051122 REAR DIFFUSER 23051643 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE SEPARATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 706AE CAC91772 760275 CAE890469S ENGINE REMOVED DUE TO COMPRESSOR WAS SEIZED ON FIRST START. COMPRESSOR DISASSEMBLY INSPECTION REVEALED: SEPARATION OF REAR DIFFUSER MAJOR SEAL. 1 G 7 2 3U 3 U H1NE E1GL 1998052900101 19980529 00101 SW 1998 5 29 HEEA0014219 1 19980519 A 6720 406312103101 LINK BELL 407 407 SW T/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 LINK HAS WORN BEARINGS. 1 G 7 1 3U O H2SW 1998052900102 19980529 00102 SW 1998 5 29 HEEA0014221 1 19980519 A 6520 406040453101 SEAL BELL 407 407 SW T/R GRBOX MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 SEAL MISMANUFACTURED. 2 PART "B" SENT IN PACK. 1 G 7 1 3U O H2SW 1998052900103 19980529 00103 SW 1998 5 29 HEEA0014222 1 19980519 A 7712 407375003107 INDICATOR BELL 407 407 SW TORQUE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 141MA 53016 TORQUE GAUGE INOPERATIVE IN FLIGHT. PEGGED TO HIGH SIDE ONCE AND WENT TO ZERO IN FLIGHT 1 G 7 1 3U O H2SW 1998052900104 19980529 00104 SW 1998 5 29 HEEA0014224 1 19980519 A 6300 406040500119 SUPPORT SEAL BELL 407 407 SW M/R LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407MM 53060 SUPPORT SEAL LEAKING. 1 G 7 1 3U O H2SW 1998052900105 19980529 00105 SW 1998 5 29 HEEA0014225 1 19980519 A 2844 407375007101 INDICATOR BELL 407 407 SW FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM 811 53060 FUEL PRESSURE WILL NOT INDICATE PRESSURE. BUT WILL TEST GOOD. 1 G 7 1 3U O H2SW 1998052900106 19980529 00106 SW 1998 5 29 HEEA0014226 1 19980519 A 7931 407375005101 INDICATOR BELL 407 407 SW OIL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM 53060 OIL PRESSURE INDICATOR FLICKERS FULL SCALE AND OFF CONTINUOUSLY AFTER 3RD START. 1 G 7 1 3U O H2SW 1998052900107 19980529 00107 SW 1998 5 29 HEEA0014227 1 19980519 A 7714 407375002103 INDICATOR BELL 407 407 SW ENG NG FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM 53060 NG INDICATOR INTERMITTENT. GOES BLANK. LOSES POWER. 1 G 7 1 3U O H2SW 1998052900108 19980529 00108 SW 1998 5 29 HEEA0014228 1 19980519 A 7700 407375016103 SIGNAL COND UNIT BELL 407 407 SW ENGINE WRONG PART E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 WRONG PART NUMBER FOR A/C SERIAL NUMBER. 1 G 7 1 3U O H2SW 1998052900109 19980529 00109 SW 1998 5 29 HEEA0014229 1 19980519 A 7933 407375004101 INDICATOR BELL 407 407 SW ENG OIL TEMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 ENG OIL TEMP DISPLAY VERY DIM. 1 G 7 1 3U O H2SW 1998052900110 19980529 00110 SW 1998 5 29 HEEA0014230 1 19980519 A 2822 407362013101 SWITCH BELL 407 407 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 402PH 53159 SWITCK INTERMITTENTLY STAYS CLOSED WITH PRESSURE OFF. 1 G 7 1 3U O H2SW 1998052900111 19980529 00111 SW 1998 5 29 HEEA0014231 1 19980519 A 3212 407350301101 FLOAT BAG BELL 407 407 SW LT FLOAT LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 403PH 53177 LT FLOAT BAG LEAKING. 1 G 7 1 3U O H2SW 1998052900112 19980529 00112 SW 1998 5 29 HEEA0014232 1 19980519 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 403PH 53177 DISK COUPLING HAS A CRACKED DISC. 1 G 7 1 3U O H2SW 1998052900113 19980529 00113 SW 1998 5 29 HEEA0014233 1 19980519 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 53207 DISK COUPLING HAS A CRACKED DISC. 1 G 7 1 3U O H2SW 1998052900114 19980529 00114 SW 1998 5 29 HEEA0014234 1 19980519 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DISK COUPLING HAS A CRACKED DISC. 1 G 7 1 3U O H2SW 1998052900115 19980529 00115 SW 1998 5 29 HEEA0014235 1 19980519 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 NR 1 DISC CRACKED. 1 G 7 1 3U O H2SW 1998052900116 19980529 00116 SW 1998 5 29 HEEA0014236 1 19980519 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DISK COUPLING IS CORRODED. 1 G 7 1 3U O H2SW 1998052900117 19980529 00117 SW 1998 5 29 HEEA0014237 1 19980519 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 53038 DISK COUPLING IS CRACKED. 1 G 7 1 3U O H2SW 1998052900118 19980529 00118 SW 1998 5 29 HEEA0014238 1 19980519 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 DISK COUPLING CRACKED AND CORRODED. 1 G 7 1 3U O H2SW 1998052900119 19980529 00119 SW 1998 5 29 HEEA0014239 1 19980519 A 6230 406010129101 ROD ASSY BELL 407 407 SW M/R DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 ONE BEARING ON CONTROL ROD DAMAGED, OUT RACE. THE OTHER BEARING IS BADLY WORN. 1 G 7 1 3U O H2SW 1998052900120 19980529 00120 SW 1998 5 29 HEEA0014240 1 19980519 A 6321 206076047101 CYLINDER ASSY BELL 407 407 SW M/R BRAKE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 53207 CYLINDER ASSY HAS NO OUTPUT PRESSURE. CYCLES FLUID IN RESERVOIR. 1 G 7 1 3U O H2SW 1998052900121 19980529 00121 SW 1998 5 29 HEEA0014241 1 19980519 A 6520 206011721113 HOUSING BELL 407 407 SW T/R MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 437PH 1429 53072 T/R CONTROL HOUSING MISMANUFACTURED. THE BORE OF THE MS27641-4 BEARING IS NOT MACHINED ENOUGH ON ONE SIDE. 1 G 7 1 3U O H2SW 1998052900122 19980529 00122 SW 1998 5 29 HEEA0014244 1 19980519 A 6300 406010417101 BEARING BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 BEARING WORN. SERIAL NUMBERS REMOVED ARE A1279 AND A1226. 1 G 7 1 3U O H2SW 1998052900123 19980529 00123 SW 1998 5 29 HEEA0014245 1 19980519 A 6300 406010425107 LEVER ASSEMBLY BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 1111 53059 LEVER ASSY HAS WORN LININGS. SERIAL NUMBERS REMOVED ARE A1738 AND A1741. 1 G 7 1 3U O H2SW 1998052900124 19980529 00124 SW 1998 5 29 HEEA0014246 1 19980519 A 6340 222375077115 TRANSDUCER BELL 407 407 SW ROTOR DRIVE FAILED E HEEA K NONE O OTHER NR NOT REPORTED 1 SW 03 427PH 53059 TRANSDUCER FAILED. GOES ON ZERO IN FLIGHT. 1 G 7 1 3U O H2SW 1998052900125 19980529 00125 EU 1998 5 29 HEEA0014247 1 19980519 A 7931 648180101 INDICATOR SNIAS 350 AS350B2 8680813 EU ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 2862 OIL PRESSURE INDICATOR STUCK ON ZERO; HAS TO BE TAPPED. 1 G 7 1 3U H9EU 1998052900126 19980529 00126 SW 1998 5 29 HEEA0014248 1 19980520 A 5320 206033412003 SUPPORT BELL 206 206L1 1182107 SW FUSELAGE DAMAGED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 2249Z 45753 DEEP SANDING MARKS ON BOTTOM AT RADIUS OF BRACKET. POOR QUALITY CONTROL. 1 G 7 1 3U H2SW 1998052900127 19980529 00127 SW 1998 5 29 HEEA0014249 1 19980520 A 2435 214060056103 STARTER BELL 214 214ST 1182106 SW ENGINE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3897N 28106 STARTER ENERGIZES; BUT DOES NOT ENGAGE, KICKS OUT AFTER 4 SECONDS. 2 G 7 2 4U H10SW 1998052900128 19980529 00128 SW 1998 5 29 HEEA0014250 1 19980522 A 2432 31908001 BATTERY BELL 407 407 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 WEAK WHILE DOING VOLTAGE CHECK. FOUND ONE CELL WITH THERMAL RUNNERWAY. 1 G 7 1 3U O H2SW 1998052900129 19980529 00129 SW 1998 5 29 HEEA0014251 1 19980522 A 6320 406340100101 PUMP BEARING BELL 407 407 SW TRANSMISSION WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 TRANSMISSION OIL PUMP BEARING WORN. 1 G 7 1 3U O H2SW 1998052900130 19980529 00130 SW 1998 5 29 HEEA0014252 1 19980522 A 6320 407064702101 TUBE ASSEMBLY BELL 407 407 SW M/R GR BOX DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 427PH 53059 TUBE ASSY LOWER ROD END BEARING ROUGH. 1 G 7 1 3U O H2SW 1998052900131 19980529 00131 SW 1998 5 29 HEEA0014253 1 19980522 A 2820 407076010101 TUBE ASSEMBLY BELL 407 407 SW FUEL SYS CHAFED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 TUBE ASSY CHAFFED. 1 G 7 1 3U O H2SW 1998052900132 19980529 00132 SW 1998 5 29 HEEA0014254 1 19980522 A 6300 406310405101 UNIVERSAL BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 1071 53114 UNIVERSAL HAS WEAR IN BEARING. 1 G 7 1 3U O H2SW 1998052900133 19980529 00133 SW 1998 5 29 HEEA0014255 1 19980522 A 6320 222375077113 TRANSMITTER BELL 407 407 SW M/R GEARBOX FLUCTUATION E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 53114 OIL PRESSURE FLUCTUATION. 1 G 7 1 3U O H2SW 1998052900134 19980529 00134 SW 1998 5 29 HEEA0014256 1 19980522 A 2822 407362013101 SWITCH BELL 407 407 SW FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 447PH 53114 R/H BOOST PUMP LIGHT WOULD NOT COME ON WHEN TURNED OFF. 1 G 7 1 3U O H2SW 1998052900135 19980529 00135 SW 1998 5 29 HEEA0014259 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 DISK COUPLING CRACKEDCRACKED. 1 G 7 1 3U O H2SW 1998052900136 19980529 00136 SW 1998 5 29 HEEA0014260 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998052900137 19980529 00137 SW 1998 5 29 HEEA0014261 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 CRACKED DISC AND CORROSION. 1 G 7 1 3U O H2SW 1998052900138 19980529 00138 SW 1998 5 29 HEEA0014262 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 CORROSION BETWEEN DISC. 1 G 7 1 3U O H2SW 1998052900139 19980529 00139 SW 1998 5 29 HEEA0014263 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DISK COUPLING FRETTING AND CORRODED. 1 G 7 1 3U O H2SW 1998052900140 19980529 00140 SW 1998 5 29 HEEA0014264 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW TR DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998052900141 19980529 00141 SW 1998 5 29 HEEA0014265 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407PH 53003 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998052900142 19980529 00142 SW 1998 5 29 HEEA0014266 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 53038 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998052900143 19980529 00143 SW 1998 5 29 HEEA0014267 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 417PH 53038 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998052900144 19980529 00144 SW 1998 5 29 HEEA0014268 1 19980522 A 6510 406040340101 DISK COUPLING BELL 407 407 SW T/R DRIVE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 DISK COUPLING CRACKED. 1 G 7 1 3U O H2SW 1998052900145 19980529 00145 SW 1998 5 29 HEEA0014269 1 19980522 A 7933 407375004101 INDICATOR BELL 407 407 SW ENG OIL TEMP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 ENG OIL TEMP WILL NOT ALREADY TEST ON LCD INST. CHECK. 1 G 7 1 3U O H2SW 1998052900146 19980529 00146 SW 1998 5 29 HEEA0014270 1 19980522 A 6500 406040339105 BEARING 406040303101 BELL 407 407 SW T/R ROUGH E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 343 A883 53142 ROUGH BEARINGS. SERIAL NUMBERS REMOVED ARE H96-0267 AND H96-0325. 1 G 7 1 3U O H2SW 1998052900147 19980529 00147 SW 1998 5 29 HEEA0014271 1 19980522 A 7120 407060111101 BIPOD MOUNT BELL 407 407 SW ENGINE WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 612PH 177 53199 BIPOD MOUNT WORN. 1 G 7 1 3U O H2SW 1998052900148 19980529 00148 SW 1998 5 29 HEEA0014272 1 19980522 A 3212 206050247132 COVER BELL 407 407 SW FLOAT DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FLOAT COVER DETERIORATED. 1 G 7 1 3U O H2SW 1998052900149 19980529 00149 SW 1998 5 29 HEEA0014273 1 19980522 A 3212 206050247135 COVER BELL 407 407 SW FLOAT DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FLOAT COVER DETERIORATED. 1 G 7 1 3U O H2SW 1998052900150 19980529 00150 SW 1998 5 29 HEEA0014274 1 19980522 A 3212 206050247138 COVER BELL 407 407 SW FLOAT DETERIORATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 DETERIORATED. 1 G 7 1 3U O H2SW 1998052900151 19980529 00151 SW 1998 5 29 HEEA0014275 1 19980522 A 2841 407375006101 INDICATOR BELL 407 407 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 INDICATOR DOES NOT INDICATE OR TEST AS REQUIRED. 1 G 7 1 3U O H2SW 1998052900152 19980529 00152 SW 1998 5 29 HEEA0014276 1 19980522 A 2841 407375006101 INDICATOR BELL 407 407 SW FUEL QTY FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FUEL QTY INDICATOR WILL NOT SHOW ANY INDICATION. 1 G 7 1 3U O H2SW 1998052900153 19980529 00153 SW 1998 5 29 HEEA0014277 1 19980522 A 3150 407375015101 CAUTION PANEL BELL 407 407 SW CHIP WARN ILLUMINATED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 1349 53070 CHIP SEGMENT COMES ON INTERMITTENTLY. 1 G 7 1 3U O H2SW 1998052900154 19980529 00154 SW 1998 5 29 HEEA0014278 1 19980522 A 3212 206050247135 COVER BELL 407 407 SW FLOAT TORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 53070 FLOAT COVER END CAP TORN. 1 G 7 1 3U O H2SW 1998052900155 19980529 00155 SW 1998 5 29 HEEA0014280 1 19980522 A 6340 222375077119 TRANSMITTER BELL 407 407 SW TORQUE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 TORQUE INDICATOR INOPERATIVE. 1 G 7 1 3U O H2SW 1998052900156 19980529 00156 SW 1998 5 29 HEEA0014281 1 19980522 A 3212 407350302101 FLOAT BAG BELL 407 407 SW FWD END LEAKING E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 FLOAT BAG LEAKING AT FORWARD END. 1 G 7 1 3U O H2SW 1998052900157 19980529 00157 SW 1998 5 29 HEEA0014282 1 19980522 A 2844 407375007103 TRANSMITTER BELL 407 407 SW FUEL PRESS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 460 53207 FUEL PRESSURE FALLS TO ZERO INTERMITTENTLY. 1 G 7 1 3U O H2SW 1998052900158 19980529 00158 SW 1998 5 29 HEEA0014283 1 19980522 A 6321 206340301103 ROTOR BRAKE BELL 407 407 SW LT ROTOR UNBONDED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 57416 1557 53070 L/H ROTOR BRAKE CALIPER PAD ASSY UNBONDED. 1 G 7 1 3U O H2SW 1998052900159 19980529 00159 SW 1998 5 29 HEEA0014284 1 19980522 A 7714 407375008101 INDICATOR BELL 407 407 SW DUAL TACH FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 141MA 53016 T-NEEDLE GOES UP A LITTLE, THEN GOES BACK TO ZERO ON TEST AND STAYS AT ZERO ON RUN UP. 1 G 7 1 3U O H2SW 1998052900160 19980529 00160 SW 1998 5 29 HEEA0014285 1 19980522 A 6220 407010207101 STOP BELL 407 407 SW M/R WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 467PH 53142 STOP ELASTOMER WORN. 1 G 7 1 3U O H2SW 1998052900161 19980529 00161 SW 1998 5 29 HEEA0014286 1 19980522 A 7120 407060111101 BIPOD MOUNT BELL 407 407 SW LT MOUNT WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 437PH 53072 BIPOD MOUNT LEFT HAND BEARING WORN. 1 G 7 1 3U O H2SW 1998052900162 19980529 00162 SW 1998 5 29 HEEA0014287 1 19980522 A 6321 206076047101 CYLINDER ASSY BELL 407 407 SW ROTOR BRAKE WEAK E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 405PH 390 53207 SINCE NEW, ROTOR BRAKE HAS ALWAYS BEEN WEAK AND IS DETERIORATING. 1 G 7 1 3U O H2SW 1998052900163 19980529 00163 SW 1998 5 29 HEEA0014288 1 19980522 A 6320 214040806003 PRESSURE SWITCH BELL 407 407 SW M/R GEARBOX FAILED E HEEA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 SW 03 407PH 53003 TRANSMISSION PRESSURE LIGHT DOES NOT COME ON WHEN THERE IS NO PRESSURE. 1 G 7 1 3U O H2SW 1998052900164 19980529 00164 SW 1998 5 29 HEEA0014289 1 19980522 A 6710 PM212302 SWITCH BELL 407 407 SW CYCLIC STICK FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 407MM 53060 CYCLIC STICK SWITCH FAILED. 1 G 7 1 3U O H2SW 1998052900165 19980529 00165 1998 5 29 HEEA0014290 4 19980522 A 3120 B1894522282A CLOCK SNIAS 350 AS350B2 8680813 EU COCKPIT FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 1479 2820 CLOCK INOPERATIVE. 1 G 7 1 3U H9EU 1998052900166 19980529 00166 EU 1998 5 29 HEEA0014291 1 19980522 A 7160 350A54108004 AIR INTAKE SNIAS 350 AS350B2 8680813 EU ENGINE CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 40466 820 3004 ENG AIR INTAKE CRACKED. 1 G 7 1 3U H9EU 1998052900167 19980529 00167 EU 1998 5 29 HEEA0014292 1 19980522 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 99 2862 PITCH CONTROL ROD REMOVED FOR REPAIR. 1 G 7 1 3U H9EU 1998052900168 19980529 00168 EU 1998 5 29 HEEA0014293 1 19980522 A 6420 350A33200405 SPIDER SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 1147 2862 T/R SPIDER WORN BEARINGS. 1 G 7 1 3U H9EU 1998052900169 19980529 00169 EU 1998 5 29 HEEA0014294 1 19980522 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU PITCH CONTROL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 285 2862 PITCH CONTROL ROD HAS WORN BEARINGS. 1 G 7 1 3U H9EU 1998052900170 19980529 00170 EU 1998 5 29 HEEA0014295 1 19980522 A 6420 350A33211905 BODY SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6100R 2862 TAIL ROTOR BODY HAS WORN BEARINGS. 1 G 7 1 3U H9EU 1998052900171 19980529 00171 EU 1998 5 29 HEEA0014296 1 19980522 A 2930 806966 ELEMENT SNIAS 350 AS350B2 8680813 EU HYD SYS DEFECTIVE E HEEA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 03 6097Z 2820 ELEMENT CAUSES BYPASS BUTTON TO POP. SCRAPPED PART AT PHI. 1 G 7 1 3U H9EU 1998052900172 19980529 00172 SW 1998 5 29 HEEA0014299 1 19980522 A 6520 222312753103 BEARING BELL 230 230 1182149 SW T/R GEARBOX CRACKED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 230UN 193 23009 T/R GEARBOX BEARINGS CRACKED. 1 G 7 2 3U NC H9SW 1998052900173 19980529 00173 SW 1998 5 29 HEEA0014300 1 19980522 A 6320 406340100101 PUMP BELL 407 407 SW TRANSMISSION OIL LEAKING E HEEA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PH 53003 TRANSMISSION OIL PUMP LEAKING OIL. 1 G 7 1 3U O H2SW 1998052900183 19980529 00183 CE 1998 5 29 GLBA98048 1 19980403 A 7120 11490455 TRUSS BEECH 1900 1900C 1154161 CE RT ENGINE CRACKED A A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 174GL 4051 UC174 RIGHT ENGINE TRUSS CRACKED IN AREA 'A' INBOARD. REPLACED RIGHT HAND ENGINE TRUSS. (X) 2 L 7 2 4T RT A24CE 1998052900184 19980529 00184 CE 1998 5 29 GLBA98061 1 19980416 A 5210 MECHANISM BEECH 1900 1900C 1154161 CE PASSENGER DOOR LACK OF LUBE A GLBA K NONE O OTHER TX TAXI/GRND HDL 1 CE 01 125GL UC125 PASSENGER DOOR WILL NOT LOCK ALL THE TIME. NOTE: THIS WAS FOUND WHILE TAKING AIRCRAFT FROM HANGAR TO THE GATE. NO PAS SENGERS ONBOARD. LUBED PLUNGER ON LOCK MECHANISM. OPS CHECK OK. (X) 2 L 7 2 4T RT A24CE 1998052900185 19980529 00185 SO 1998 5 29 GLBA98069 1 19980429 A 3310 9923068118149 LAMP SOCKET EMB 120 EMB120RT SO YAW DAMPENER FAILED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 01 452UE 120096 YAW DAMPENER LIGHT BULB FELL OUT OF SOCKET. SHORTED OUT TO GROUND. SMOKE CAME INTO COCKPIT. RETURNED TO GATE. YAW DA MPENER LIGHT BULB REMOVED FROM DEFECTIVE SOCKET AND MEL'D. (X) 2 L 7 2 4T RT A31SO 1998052900186 19980529 00186 WP 1998 5 29 G60A022 1 19980422 A 5754 SKIN DOUG DC10 DC1030 3023501 WP NR 1 LE SLAT DENTED A G6OA K NONE O OTHER IN INSP/MAINT 1 EA 27 606GC 47929 DURING WALK-AROUND, GROUND MAINTENANCE FOUND A DENT IN THE RIGHT HAND NR 1 LEADING EDGE SLAT. THE DENT WAS 6 INCHES LON G BY 4 INCHES WIDE AND .125 INCHES DEEP. GROUND MAINTENANCE REWORKED THE AREA TO ALMOST SMOOTH SURFACE AND APPLIED FILL ER MATERIAL IAW SRM 57-10-00. OK FOR SERVICE. (X) 2 L 7 3 4F A22WE 1998052900187 19980529 00187 NM 1998 5 29 98ZZZX1953 1 19980417 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN CHAFED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 772AT 22003 DURING PRE-FLIGHT, THE RIGHT EMERGENCY EXIT CONTROL CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. FUEL VALVE 'CLOSED', L AMPS WENT DIM THEN BRIGHT WHEN CIRCUIT BREAKER TRIPPED AGAIN. FOUND WIRE SPLICE IN AFT AIRSTAIRS COMPARTMENT CHAFED ARO UND AN ADEL CLAMP. WIRE REPAIRED. 2 L 7 3 4F A3WE 1998052900188 19980529 00188 WP 1998 5 29 98ZZZX1954 1 19980424 A 3350 BATTERY PACK LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 186AT 193C1074 DURING PRE-FLIGHT, FOUND AFT ZONE EGRESS LIGHT INOPERABLE. REMOVED AND REPLACED EMERGENCY POWER PACK AT 3R. 2 L 7 3 4F A23WE 1998052900189 19980529 00189 NM 1998 5 29 98ZZZX1955 1 19980427 A 3350 CHARGER BOEING 727 727214 138407R NM CABIN FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 786AT 21692 EGRESS CEILING EXIT LIGHT INOPERABLE AT ROW 5A-F. REMOVED AND REPLACED BATTERY CHARGER. 2 L 7 3 4F A3WE 1998052900190 19980529 00190 NM 1998 5 29 98ZZZX1956 1 19980430 A 3350 CHARGER BOEING 727 727208 138407W NM CABIN FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 780AT 22295 EGRESS LIGHTS INOPERABLE AT AFT CARGO DOOR. REMOVED AND REPLACED BATTERY CHARGER. 2 L 7 3 4F RT A3WE 1998052900191 19980529 00191 NM 1998 5 29 98ZZZX1957 1 19980430 A 3350 CHARGER BOEING 727 727208 138407W NM CABIN FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 780AT 22295 DURING PRE-FLIGHT, FOUND RIGHT FORWARD EGRESS LIGHT FLICKERS DURING TEST. REMOVED AND REPLACED BATTERY CHARGER. 2 L 7 3 4F RT A3WE 1998052900192 19980529 00192 NM 1998 5 29 98ZZZX1958 1 19980430 A 3350 BATTERY BOEING 727 727208 138407W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 780AT 22295 EGRESS LIGHTS INOPERABLE AT AFT AIRSTAIRS. REMOVED AND REPLACED BATTERY. 2 L 7 3 4F RT A3WE 1998052900196 19980529 00196 NM 1998 5 29 98ZZZX1962 1 19980320 A 2910 LINE BOEING 727 7272B7 138407L NM A-HYD SYSTEM FAILED A AMTA H O DEACTIVATE SYST/CIRCUITS OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 11 760AT 21954 DURING DESCENT, A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO THEN PRESSURE WENT TO ZERO. COMPLETED LOSS OF A-FLUID CHECK LIS T. REMOVED AND REPLACED HYDRAULIC PRESSURE LINE AT STA 1342, SECTION 48. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE HYD RAULIC DRIVEN PUMPS AND ASSOCIATED FILTERS PER MM 29-11-33. LEAK CHECKED AND GOOD. 2 L 7 3 4F A3WE 1998052900197 19980529 00197 1998 5 29 98ZZZX1963 4 19980314 A 3497 WIRE BOEING 727 727227 1384078 NM RT COCKPIT SHORTED A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 766AT 21999 FORWARD PANEL WARNING LIGHTS ILLUMINATED AS IF STICKING OR STUCK IN TEST MODE. CIRCUIT BREAKER RECYCLING INEFFECTIVE IN CLEARING LIGHTS. FOUND TERMINAL SHORTED TO GROUND ON FIRST OFFICER'S COMPASS TRANSFER LIGHT. REPAIRED AND SECURED PER SWPM 20-10-13. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998052900198 19980529 00198 EU 1998 5 29 SIMA981201 1 19980430 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1964, 98ZZZX1965, AND 98ZZZX1966. (X) 2 H 7 2 4T RT A53EU 1998052900199 19980529 00199 EU 1998 5 29 98ZZZX1964 1 19980430 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981201, 98ZZZX1965, AND 98ZZZX1966. 2 H 7 2 4T RT A53EU 1998052900200 19980529 00200 EU 1998 5 29 98ZZZX1965 1 19980430 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981201, 98ZZZX1964, AND 98ZZZX1966. 2 H 7 2 4T RT A53EU 1998052900201 19980529 00201 EU 1998 5 29 98ZZZX1966 1 19980430 A 5347 S5367800210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT AFT INBOARD, LEFT AFT OUTBOARD, AND BOTH FLIGHT ATTENDANTS. MAINTENANCE REMOVED AND REPLACED ALL SEAT TRACKS IAW SRM 53-63-00. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981201, 98ZZZX1964, AND 98ZZZX1965. 2 H 7 2 4T RT A53EU 1998052900202 19980529 00202 EU 1998 5 29 SIMA981196 1 19980429 A 5330 S5317220120805 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPAIRED DENT ON RIGHT SIDE OF FUSELAGE ABOVE NLG WELL AT FRAME 3 WL 2327.5. MAINTENANCE REPAIRED DENT IAW SRM 53-00-00 FIGURE 403. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998052900203 19980529 00203 EU 1998 5 29 SIMA981194 1 19980429 A 5320 S5367800820002 ZEE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT ZEE MEMBER LOCATED BETWEEN FRAMES 39 AND 41 CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT AFT ZEE MEMBER IAW SRM 51-21-28. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998052900204 19980529 00204 EU 1998 5 29 SIMA981193 1 19980429 A 5315 S5367240620801 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND R EPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1967. (X) 2 H 7 2 4T RT A53EU 1998052900205 19980529 00205 EU 1998 5 29 98ZZZX1967 1 19980429 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 377AT 377 SAW - DURING HMBV-1 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND R EPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL SIMA981193 2 H 7 2 4T RT A53EU 1998052900206 19980529 00206 EU 1998 5 29 SIMA981192 1 19980429 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND R EPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1968. (X) 2 H 7 2 4T RT A53EU 1998052900207 19980529 00207 EU 1998 5 29 98ZZZX1968 1 19980429 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAMS 36 AND 38 WERE CORRODED. MAINTENANCE REMOVED AND R EPLACED BOTH FLOORBEAMS IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981192. 2 H 7 2 4T RT A53EU 1998052900208 19980529 00208 EU 1998 5 29 SIMA981191 1 19980429 A 5320 S52678008200 WEB AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. T HE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IA W SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX1969, 98ZZZX1970, AND 98ZZZX1971. (X) 2 H 7 2 4T RT A53EU 1998052900209 19980529 00209 EU 1998 5 29 98ZZZX1969 1 19980429 A 5320 S5367121720402 SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. T HE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IA W SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981191, 98ZZZX1970, AND 98ZZZX1971. 2 H 7 2 4T RT A53EU 1998052900210 19980529 00210 EU 1998 5 29 98ZZZX1970 1 19980429 A 5320 S5367800822251 SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. T HE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IA W SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981191, 98ZZZX1969, AND 98ZZZX1971. 2 H 7 2 4T RT A53EU 1998052900211 19980529 00211 EU 1998 5 29 98ZZZX1971 1 19980429 A 5320 S5367800020402 SUPPORT AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 322AC 320 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING ITEMS CORRODED BETWEEN FRAMES 39 AND 41 LEFT SIDE. T HE LEFT Z-MEMBER, WEB, FLOOR CHANNEL SUPPORT, AND GUSSET. MAINTENANCE REMOVED AND REPLACED THE ABOVE MENTIONED ITEMS IA W SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA981191, 98ZZZX1969, AND 98ZZZX1970. 2 H 7 2 4T RT A53EU 1998052900212 19980529 00212 EU 1998 5 29 SIMA981113 1 19980421 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 342AT 345 SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT MIDDLE OUTBOARD SEAT TRACK WAS DAMAGED AT SEAT MOUNTING SU RFACE. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998052900213 19980529 00213 EU 1998 5 29 SIMA981141 1 19980424 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 11660 223 SAW - DURING PS-2 INSPECTION, MAINTENANCE REPORTED THE FORWARD EMERGENCY FLOOR LIGHTS, NR'S 1, 3, 5, AND THE FORWARD LEF T EXTERIOR EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCAT ION 3WL. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998052900214 19980529 00214 EU 1998 5 29 SIMA981073 1 19980417 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 045 ORD - FLT 4074 - FLOOR PROXIMITY LIGHT INOPERATIVE AT ROW 7. MEL'D PER 33-23 AND RETURNED AIRCRAFT TO SERVICE. 4-19-98 : RE-SOLDERED WIRE TO PIN OF FLOOR PROXIMITY LIGHT BULB SOCKETS. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURN ED AIRCRAFT TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998052900215 19980529 00215 EU 1998 5 29 SIMA981121 1 19980422 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 260AE 675 263 DFW - FLT 3825 - EMERGENCY LIGHTS AT FORWARD EMERGENCY EXITS INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD IAW AT R 72 JUC 24-30-00. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998052900216 19980529 00216 CE 1998 5 29 MASA980886 1 19980417 A 2930 INDICATING SYST BEECH 1900 1900D 1154162 CE HYD SYSTEM MALFUNCTIONED A MASA B EMER. DESCENT N FALSE WARNING CR CRUISE 1 SW 07 17YV UE17 MBX/PIT - FLT 5940 - IN-FLIGHT, THE HYDRAULIC FLUID LOW CAUTION ANNUNCIATOR ILLUMINATED. PIT EMERGENCY EQUIPMENT WAS DI SPATCHED AS A PRECAUTIONARY MEASURE. PILOT RECEIVED THREE GREEN DOWN LIGHTS WITH GEAR EXTENSION ON FIRST ATTEMPT. NO G EAR UNSAFE LIGHTS ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED CLEAR OF THE RUNWAY. PASSENGERS WERE BUSSED TO THE TERMINAL AND THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND THE FLUID LEVEL TO BE SATISFACTORY. THE HYD RAULIC FLUID LOW ANNUNCIATOR SYSTEM WAS DEFERRED PER MEL 32-5. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998052900217 19980529 00217 CE 1998 5 29 MASA98084 1 19980416 A 7921 330997F120290 HOSE BEECH 1900 1900D 1154162 CE RT OIL COOLER LEAKING A MASA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 5YV 1143890005 UE5 FLT 4441 - AFTER TAKEOFF OF TRAINING FLIGHT, CREW NOTICED THE MASTER WARNING FLASHING THEN NOTICED THE OIL PRESSURE LOW ANNUNCIATOR ILLUMINATED. THE ENGINE WAS SECURED AND THE CREW DECLARED AN EMERGENCY. AIRCRAFT RETURNED TO THE FIELD WIT HOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE OIL COOLER RIGHT INLET LINE. AIRCRAFT WAS RETURNED TO SERVICE. ( X) 2 L 7 2 4T RT A24CE 1998052900218 19980529 00218 NM 1998 5 29 MASA98097 1 19980501 A 3350 AML91LA85 BULB GRIMES 40005130003 DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 436YV 436 DURING ROUTINE MAINTENANCE, FOUND 'NORMAL SWITCH EMERGENCY LIGHT AT FLIGHT ATTENDANT'S PANEL WOULD NOT ILLUMINATE. MAIN TENANCE REMOVED AND REPLACED THE LIGHT BULB, OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998052900219 19980529 00219 WP 1998 5 29 NOCA1198 1 19980424 A 3350 0105606003 HARNESS DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 TWO EMERGENCY PATH LIGHTS INOPERABLE AT ROW 22. REPLACED TWO EACH LIGHT HARNESS ASSEMBLIES. OPS CHECKS OK. (X) 2 L 7 2 4F RT A6WE 1998052900220 19980529 00220 WP 1998 5 29 NOCA1298 1 19980428 A 3350 0105606303 HARNESS DOUG DC9 DC983 3022083 WP CABIN FAILED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 ONE WHITE EMERGENCY PATH LIGHT INOPERABLE AT ROW 12. REPLACED LIGHT ASSEMBLY HARNESS AT ROW 12. OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998052900221 19980529 00221 EU 1998 5 29 SABA980027 1 19980420 A 6120 8659566 SWITCH BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A SABA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 33 164PC 5961 682 HTS - FLT 5169 - ON FLIGHT FROM HTS TO CLT, LEFT BETA LIGHT CAME ON DURING TAKEOFF ROLL. PILOT ABORTED TAKEOFF. EMERGE NCY WAS DECLARED. AIRCRAFT RETURNED TO PARKING WITH NO OTHER PROBLEMS. MAINTENANCE FROM CLT FOUND THE LEFT BETA SWITCH BAD. REMOVED AND REPLACED LEFT BETA SWITCH, SYSTEM RUN AND OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A21EU 1998052900222 19980529 00222 WP 1998 5 29 HALA9800116 1 19980503 A 3350 BATTERY CHARGER DOUG DC10 DC1010 3022110 WP CABIN FAILED A HALA K NONE L NO TEST TX TAXI/GRND HDL 1 WP 13 153AA 46708 HNL - FLT 26 - LOG PAGE 4096350 - ON PRE-FLIGHT IN HNL FOUND EMERGENCY LIGHT TEST INOPERATIVE. BITE TEST SHOWED OVERWIN G BATTERY PACK INOPERATIVE. REPLACED BATTERY CHARGER AT L-3 DOOR. OPS CHECK OK. (X) 2 L 7 3 4F A22WE 1998052900223 19980529 00223 WP 1998 5 29 HALA9800112 1 19980507 A 5711 SPAR CAP DOUG DC10 DC1010 3022110 WP RT WING CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 116AA 46516 LAX - FLT 09 - RIGHT WING CRACKED N THE REAR SPAR CAP WEB NEAR XORS 433/402. INSTALLED FUEL TANK REPAIR DOUBLER PER ES0 7349, DATED 5-7-98. (X) 2 L 7 3 4F A22WE 1998052900224 19980529 00224 WP 1998 5 29 HALA9800110 1 19980407 A 5320 3920324501 ANGLE DOUG DC9 DC951 3022051 WP BS 700-705 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 RIGHT AND LEFT LOWER KEEL BEAM ANGLES TO FRAME ATTACH BRACKET FS 700 - FS 705 HAVE 3 INCH CRACKS RUNNING HORIZONTALLY. R EMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM ANGLES PER SRM 51-30-5. TOTAL TIME: 45,975 HOURS. TOTAL CYCLES: 71,775. REF: OPERATOR CONTROL NR 98ZZZX1972. (X) 2 L 7 2 4F RT A6WE 1998052900225 19980529 00225 WP 1998 5 29 98ZZZX1972 1 19980407 A 5320 3920324502 ANGLE DOUG DC9 DC951 3022051 WP BS 700-705 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 RIGHT AND LEFT LOWER KEEL BEAM ANGLES TO FRAME ATTACH BRACKET FS 700 - FS 705 HAVE 3 INCH CRACKS RUNNING HORIZONTALLY. R EMOVED AND REPLACED LEFT AND RIGHT KEEL BEAM ANGLES PER SRM 51-30-5. TOTAL TIME: 45,975 HOURS. TOTAL CYCLES: 71,775. REF: OPERATOR CONTROL NR HALA9800110. 2 L 7 2 4F RT A6WE 1998052900226 19980529 00226 EU 1998 5 29 UF6A980419 1 19980424 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 SBM - MX - OVERWING EXITS LEFT AND RIGHT SIDES ARE OUT. MAINTENANCE REMOVED AND REPLACED BOTH LEFT AND RIGHT BULBS. (X ) 2 L 7 2 4T RT A27NM 1998052900227 19980529 00227 EU 1998 5 29 UF6A980418 1 19980424 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 SBN - MX - EMERGENCY LIGHT OUT AT AFT BAGGAGE DOOR. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 1998052900228 19980529 00228 EU 1998 5 29 UF6A980424 1 19980427 A 5330 3D11519 SKIN BAG ATP ATP EU BAGG DOORWAY DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 13884 2021 SBN - MX - AFT BAGGAGE DOOR SURROUND HAS DENT ON AFT SECTION OF SURROUND. MAINTENANCE STRAIGHTENED DENT BACK TO ORIGINA L CONTOUR IAW ENGINEERING REPORT NR 98-057. (X) 2 L 7 2 4T RT A27NM 1998052900229 19980529 00229 EU 1998 5 29 UF6A980423 1 19980427 A 5510 1G3056 SPAR BAG ATP ATP EU LT HORIZ STAB CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 13884 2021 SBN - MX - CRACK FOUND ON FRONT SPAR OF LEFT HAND HORIZONTAL STABILIZER AT STA 42.00 TOP EDGE. MAINTENANCE STOP DRILLED CRACK AND INSTALLED SINGLE FLANGE REPAIR. (X) 2 L 7 2 4T RT A27NM 1998052900230 19980529 00230 EU 1998 5 29 UF6A980422 1 19980427 A 5315 10D11498 FLOORBEAM BAG ATP ATP EU BS 378 CORROSION A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 13884 2021 FLOORBEAM AT FORMER FS 378 HAS CORROSION. MAINTENANCE REMOVED CORROSION AND FABRICATED REPAIR ANGLE FROM 2024-T3 .063 I NCH IAW ENGINEERING REPORT NR 98-057. (X) 2 L 7 2 4T RT A27NM 1998052900231 19980529 00231 EU 1998 5 29 UF6A980421 1 19980425 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 SBN - MX - LEFT HAND AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 1998052900232 19980529 00232 EU 1998 5 29 98ZZZX1973 1 19980320 A 6420 704A33633171 HINGE SNIAS 350 AS350B2 8680813 EU T/R PINK WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 391 2917 LAMINATED HINGE ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS FROM KIT 3 50A33-2153-00, C ORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998052900234 19980529 00234 EU 1998 5 29 98ZZZX1975 1 19980314 A 2844 642792002 TRANSMITTER SNIAS 350 AS350B2 8680813 EU FUEL PRESSURE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 388 1316 2917 FUEL PRESSURE TRANSMITTER UNIT INOPERATIVE. INDICATES LOW FUEL PRESSURE AT ALL TIMES. REPLACED WITH NEW UNIT, CORRECTE D PROBLEM. 1 G 7 1 3U H9EU 1998052900235 19980529 00235 CE 1998 5 29 98ZZZX1976 1 19980319 A 5610 1013840257 WINDSHIELD PPG BEECH 200 B200 1152922 CE LT COCKPIT SHATTERED A R7MA O OTHER O OTHER CR CRUISE 1 NM 11 220TB 92220H5435 BB1057 WHILE AT 22,000 FEET AND IN CRUISE FLIGHT, THE PILOT TURNED ON WINDSHIELD HEAT AND IMMEDIATELY THE WINDSHIELD SHATTERED. BOTH PPG AND RAYTHEON ADMIT THIS IS A COMMON OCCURRENCE. THE EXACT DATE WHEN THE DISCREPANT WINDSHIELD WAS INSTALLED I S NOT CLEAR. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. CORE ROUTED TO SCRAP. DATE: 4-23-98. 1 L 7 2 4T A24CE 1998052900240 19980529 00240 WP 1998 5 29 VJ9800155 1 19980521 A 3233 39132445501 ACTUATOR DOUG DC9 DC932 3022066 WP NLG FAILED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 915VV 47443 AIRCRAFT AIR RETURNED, NOSE GEAR UNSAFE LIGHT ON AFTER RETRACTION. CYCLED THE GEAR WITH THE SAME INDICATION. REPLACED NOSE GEAR RETRACT CYLINDER AND OPS CHECKED GOOD PER MM32-32-06. PAGES 201-205 AIRCRAFT OK FOR SERVICE. 2 L 7 2 4F A6WE 1998052900241 19980529 00241 NE 1998 5 29 MALA976126 2 19980514 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RIGHT MALFUNCTIONED A MALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 15 68XJ 068 ON CLIMB-OUT, THE RIGHT ENGINE STARTED SURGING, ITT CLIMBED TO 906 DEGREES, PULLED POWER BACK TO 50 PERCENT TORQUE AND I TT WAS 819. COMPLETED QRH AND RETURNED TO SDF. LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT ENGINE. ALL CHECK S GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998052900242 19980529 00242 EU 1998 5 29 MALA976127 1 19980519 A 3230 643500300 SWITCH BAC 146 AVRO146RJ85A 1500097 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION CL CLIMB 1 GL 15 502XJ E2307 ON CLIMB-OUT, THE GEAR CAN NOT BE RETRACTED WITHOUT USING THE OVERRIDE SWITCH. AIRCRAFT LANDING IN DTW WITHOUT INCIDENT . MAINTENANCE REPLACED RELAY 6A-30 AND UNDERCARRIAGE SWITCH. ALL MAINTENANCE AND TESTS PERFORMED IAW AIR32-30-14. ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998052900243 19980529 00243 1998 5 29 MALA976128 4 19980515 A 3442 071131900 RADAR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 849MA 347 IN FLIGHT, THE WEATHER RADAR IS INTERMITTENT, DIVERTED TO CWA. MAINTENANCE REPLACED WEATHER RADAR SENSOR TRANSMITTER. A LL WORK DONE IAW DASH 8 CCV 34-41-04. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998052900244 19980529 00244 EU 1998 5 29 MALA976129 1 19980518 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 GL 15 422XJ 422 ON LANDING INTO ATW, THE LANDING GEAR WILL NOT COME DOWN WHEN SELECTED. AIRCRAFT DIVERTED TO DTW. HYDRAULIC PUMP OPERA TED NORMALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE PROBLEM, REPLACED LANDING CONTROL CIRCUIT BRE AKER F7 FOR PRECAUTION. PERFORMED SEVERAL GEAR SWINGS, ALL CHECKS GOOD IAW SAAB AMM 32-30-00. 2 L 7 2 4T RT A52EU 1998052900245 19980529 00245 EU 1998 5 29 MALA976130 1 19980520 A 3234 HTE94904 SELECTOR VALVE BAC 146 AVRO146RJ85A 1500097 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 501XJ E2208 ON DESCENT UPON GEAR EXTENSION AT DSM, THE GEAR HANDLE MOVED TO THE DOWN POSITION, RED INTRANSIT LIGHTS ILLUMINATED BUT NO GEAR EXTENSION. PERFORMED QRH PROCEDURES EXTENDED GEAR USING EMERGENCY GEAR EXTENSION-OBTAINED 3 GREEN LIGHTS WITH N O INTRANSIT LIGHTS, LANDED NORMALLY. MAINTENANCE RESET EMERGENCY GEAR SELECTOR, PRESSURIZED HYDRAULICS AND CHECKED GEAR SELECTOR POSITION BY NIPS INDICATOR. MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998052900246 19980529 00246 1998 5 29 MALA976131 4 19980520 A 3425 6226190113 AHRS SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 68XJ 068 DURING FLIGHT, THE RED HEADING FLAG AND RMI FLAG WITH HEADINGS AGREEING, BUT ABOUT 30 DEGREES OFF CLOCKWISE. NO CIRCUIT BREAKERS POPPED, ALSO FLIGHT DIRECTOR RED FLAG. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 1 AHRS COMPUTER . OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998052900247 19980529 00247 NM 1998 5 29 M8XA9800008 1 19980518 A 2751 INDICATION DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE TE FLAPS MALFUNCTIONED A M8XA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 03 328PH 3006 EN ROUTE FROM DEN TO DRO, THE FLIGHT CREW NOTICED ON THE FLAP POSITION INDICATION PORTION OF THE EICAS. SCREEN THAT THE RIGHT FLAP INDICATED A ONE DEGREE DEFLECTION AND THE LEFT FLAP WAS AT ZERO DEGREE DEFLECTION. THIS WAS NOT ASSOCIATED WITH A FAULT OR ASSEMTERY WARNING. THE FLIGHT CREW ELECTED TO RETURN TO DEN. AIRCRAFT LANDED IN DENVER WITHOUT FURTHER INCIDENT. MX INSPECTED THE AIRCRAFT IAW JIC 27-50-00. NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 1998052900248 19980529 00248 NM 1998 5 29 SWAA980808 1 19980508 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CORRODED FRAME AT BS 312, LBL 50, WL 182 ABOVE STR 20L. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998052900249 19980529 00249 NM 1998 5 29 SWAA980809 1 19980508 A 5230 FRAME BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CRACKED UPPER FWD INNER SKIN FRAME BETWEEN STOP FITTINGS NR 2 AND NR 3 ON FWD CARGO DOOR. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900250 19980529 00250 NM 1998 5 29 SWAA980810 1 19980508 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 500, RBL 41, WL 164. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900251 19980529 00251 NM 1998 5 29 SWAA980811 1 19980508 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED FRAME AT BS 794, RBL 26, WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900252 19980529 00252 NM 1998 5 29 SWAA980812 1 19980509 A 5320 ANGLE BOEING 737 7372H4 138448C NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FWD SERVICE DOOR ANGLE BELOW FWD LOWER ATTACH FOR TORQUE BOX. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998052900253 19980529 00253 NM 1998 5 29 SWAA980813 1 19980509 A 5320 WEB BOEING 737 7372H4 138448C NM BS 380 HOLE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB ABOVE BELT FRAME AT BS 380, STR 26L HAS HOLE .5 INCH CENTER. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998052900254 19980529 00254 NM 1998 5 29 SWAA980814 1 19980509 A 5720 ANGLE BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED SUPPORT ANGLE JUST OUT/BD OF PYLON AND IN/BD OF PANEL 8715R. REMOVED AND RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900255 19980529 00255 NM 1998 5 29 SWAA980815 1 19980509 A 5754 SEAL BOEING 737 7373H4 1384600 NM NR 1 LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D-CHECK, FOUND NR 1 KRUGER FLAP SEAL CRACKED OUT/BD TOP. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900256 19980529 00256 NM 1998 5 29 SWAA980816 1 19980510 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND BULGING CORROSION ON FUSELAGE SKIN AT BS 727, STR 27R, 6 AFT; AND STR 27L. REPAIRED PER BOEING SRM 2 L 7 2 4F A16WE 1998052900257 19980529 00257 NM 1998 5 29 SWAA980817 1 19980510 A 5320 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND E3-4 FWD RACK ANGLE BENT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998052900258 19980529 00258 NM 1998 5 29 SWAA980818 1 19980510 A 3350 900835A BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SERVICE CHECK, FOUND FWD AISLE OVERHEAD EMERGENCY EXIT SIGN LIGHT INOP. REMOVED AND REPLACED BATTERY PACK CARTRI GE PER BOEING MM. 2 L 7 2 4F A16WE 1998052900259 19980529 00259 NM 1998 5 29 SWAA980819 1 19980510 A 3350 6127421 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 096SW 23055 DURING SERVICE CHECK, FOUND AFT SERVICE AND AFT ENTRY EMERGENCY EXIT SIGN LIGHTS INOP. REMOVED AND REPLACED BATTERY PAC K HOUSING PER BOEING MM. 2 L 7 2 4F A16WE 1998052900260 19980529 00260 NM 1998 5 29 SWAA980820 1 19980510 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 569 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED RT SKATE ANGLE AT BS 569, RBL 48 WL 173. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900261 19980529 00261 NM 1998 5 29 SWAA980821 1 19980510 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 569 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING CHEDULED D CHECK, FOUND CRACKED LT SKATE ANGLE AT BS 569, LBL 48 WL 173. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900262 19980529 00262 NM 1998 5 29 SWAA980822 1 19980510 A 5320 CLIP BOEING 737 7373G7 1384595 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 663, STR 10 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900263 19980529 00263 NM 1998 5 29 SWAA980823 1 19980510 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 947 BELOW STR 14 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900264 19980529 00264 NM 1998 5 29 SWAA980824 1 19980510 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 387 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR WEB UPPER ATTACH L-ANGLE AT BS 387 BL 0 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900265 19980529 00265 NM 1998 5 29 SWAA980825 1 19980510 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL AT BS 639, RBL 68.5 WL 221. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900266 19980529 00266 NM 1998 5 29 SWAA980826 1 19980510 A 7110 SKIN BOEING 737 7373H4 1384600 NM LT ENGINE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 390SW 26593 DURING SCHEDULED C3 CHECK, FOUND INLET ACOUSTIC SKIN DENTED AT 5:00 DENT MEASURES .75 WIDE, 2 LONG AND 0:060 DEEP. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900267 19980529 00267 NM 1998 5 29 SWAA980827 1 19980511 A 3350 LIGHT BOEING 737 7372K6 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C1 CHECK, FOUND ONE RED EGRESS LIGHT INOP, AFT END OF FLOOR EMERGENCY LIGHT TRACK AND END CAP MISSING. RELAMPED EGRESS TRACK LIGHT AND REPLACED END CAP COVER PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052900268 19980529 00268 NM 1998 5 29 SWAA980828 1 19980511 A 5280 WEB BOEING 737 7373A4 1384585 NM RT MLG DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679SW 23291 DURING SCHEDULED BC4 CHECK, FOUND RT MLG INNER DOOR AFT WEB CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900269 19980529 00269 NM 1998 5 29 SWAA980829 1 19980511 A 5754 SKIN BOEING 737 7373A4 1384585 NM NR 4 LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679SW 23291 DURING SCHEDULED BC4 CHECK, FOUND NR 4 L/E SLAT LOWER SKIN CRACKED AT OUTBOARD MAIN TRACK. REPAIRED PER BOEING DRM NR 6 5C30133. 2 L 7 2 4F RT A16WE 1998052900270 19980529 00270 NM 1998 5 29 SWAA980830 1 19980511 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT TE FLAP DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED C4 CHECK, FOUND INBD AFT FLAP DENTED ON LWR SURFACE NEAR T/E APPROX 1 FOOT FROM INBD END. REPAIRED PER BOEING DRM NR 65C30133. 2 L 7 2 4F RT A16WE 1998052900271 19980529 00271 NM 1998 5 29 SWAA980831 1 19980511 A 5753 SKIN BOEING 737 7373A4 1384585 NM LT TE FOREFLAP GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679SW 23291 DURING SCHEDULED C4 CHECK, FOUND INBD FORE FLAP GOUGED AT INBD END, TOP SURFACE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900272 19980529 00272 NM 1998 5 29 SWAA980832 1 19980512 A 5312 BULKHEAD WEB BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, WL 199-200 AND WL 201.5-202.25, LBL 47; WL 198.50-199.25 , RBL 6.7 AND WL 212-213, RBL 47. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900273 19980529 00273 NM 1998 5 29 SWAA980833 1 19980512 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 727 E LBL 44, WL 166; AND\NBS 807, LBL 49, WL 173. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998052900274 19980529 00274 NM 1998 5 29 SWAA980834 1 19980512 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 663, STR 10RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900275 19980529 00275 NM 1998 5 29 SWAA980835 1 19980512 A 5220 COVER BOEING 737 7373H4 1384600 NM LT EMER EXIT GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2 D CHECK, FOUND EMERGENCY EXIT COVER GOUGED AROUND THE EDGES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900276 19980529 00276 NM 1998 5 29 SWAA980836 1 19980512 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CORRODED INTERCOSTAL AROUND NUTPLATE LOC AT BS 500C-500D, LBL 25, WL 156; BS 500B PLUS 1 8, LBL 25, WL 156; AND BS 500A PLUS 2 LBL 25 WL 156. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900277 19980529 00277 NM 1998 5 29 SWAA980837 1 19980513 A 2121 FAN BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 375SW 26583 DURING WALKAROUND CHECK, FOUND BURNING SMELL IN CABIN AND E/E FAN C/B TRIPPED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900278 19980529 00278 NM 1998 5 29 SWAA980838 1 19980512 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 460 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 460, LBL 35, WL 161. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900279 19980529 00279 NM 1998 5 29 SWAA980839 1 19980512 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 469 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED SKIN AROUND NR 1 DME ANTENNA AT BS 469, BL0, WL 148. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900280 19980529 00280 NM 1998 5 29 SWAA980840 1 19980512 A 5312 BULKHEAD ANGLE BOEING 737 7373G7 1384595 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 23, LBL 23, WL 156. REMOVED AN D REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900281 19980529 00281 NM 1998 5 29 SWAA980841 1 19980512 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 500D, STR 19 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900282 19980529 00282 NM 1998 5 29 SWAA980842 1 19980512 A 5312 BULKHEAD ANGLE BOEING 737 7373G7 1384595 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED SIDEWALL TO BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 25, WL 158. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900283 19980529 00283 NM 1998 5 29 SWAA980843 1 19980512 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL TO FRAME SUPPORT ANGLE AT BS 380, LBL 25, WL 254. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900284 19980529 00284 NM 1998 5 29 SWAA980844 1 19980512 A 5230 STIFFENER BOEING 737 7373H4 1384600 NM CARGO DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND STIFFENER BETWEEN NR 2 AND NR 2 RIB ON FWD CARGO DOOR DAMAGED AREA. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900285 19980529 00285 NM 1998 5 29 SWAA980845 1 19980512 A 5312 BULKHEAD WEB BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SERVICE CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, WL 198.25 TO 199.25, WL 200.25 - 201.25, RBL 4.7; BS 178, WL 208.5- 209, LBL 6.7 AND WL 211.375 -211.75, LBL 6.7; AND BS 178, WL 201.5-202, LBL 6.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900286 19980529 00286 NM 1998 5 29 SWAA980846 1 19980512 A 2612 LIGHT ILLUM BOEING 737 7372T4 1384492 NM NR 2 ENG OVHT A SWAA D RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 SW 07 701SW 22054 AFTER TAKEOFF NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. A FIRE DETECT ALREADY ON MEL. AIRCRAFT RETURNED TO MCI AND MADE AN UNEVENTFUL LANDING. FOUND BROKEN TERMINAL END AND REMOVED AND REPLACED OVERHEAT MODULE PER BOEING MM. 2 L 7 2 4F A16WE 1998052900287 19980529 00287 NM 1998 5 29 SWAA980847 1 19980512 A 5320 TIE STRAP BOEING 737 7373G7 1384595 NM BS 859 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR PANEL TIE STRAP AT BS 859, RBL 18.5, LBL 21, WL 168. REMOVED AND REPLACE D PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052900288 19980529 00288 NM 1998 5 29 SWAA980848 1 19980513 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636SW 27709 DURING WALKAROUND CHECK, FOUND ONE RED FLOOR TRACK LIGHT INOP AT OVERWING EXIT. RELAMPED FLOOR TRACK LIGHT PER BOEING M M, OPS CH'D OK. 2 L 7 2 4F RT A16WE 1998052900289 19980529 00289 NM 1998 5 29 SWAA980849 1 19980514 A 5240 GUSSET BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FWD SERVICE DOOR AT GUSSET IN LWR AFT CORNER. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998052900290 19980529 00290 NM 1998 5 29 SWAA980850 1 19980514 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 885 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C3 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 885, STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998052900291 19980529 00291 NM 1998 5 29 SWAA980851 1 19980514 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 388SW 26591 DURING WALKAROUND CHECK, FOUND LOWER AFT EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998052900292 19980529 00292 NM 1998 5 29 SWAA980852 1 19980514 A 5512 SKIN BOEING 737 7373G7 1384595 NM HORIZ STAB GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND GOUGE AT RT HORIZ STAB LEADING EDGE PANEL LE BS 149.75. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900293 19980529 00293 NM 1998 5 29 SWAA980853 1 19980514 A 5512 PANEL BOEING 737 7373G7 1384595 NM HORIZ STAB GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND GOUGE AT RT HORIZ STAB LEADING EDGE PANEL LE BS 100.56. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900294 19980529 00294 NM 1998 5 29 SWAA980854 1 19980514 A 3350 LIGHTS BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 524SW 26566 DURING SERVICE CHECK, FOUND EGRESS LIGHTING INOP AT ROW 13ABC. REPAIRED LOOSE WIRE CONNECTION AT ROW 13ABC PER BOEING M M. OPS CH'K GOOD. 2 L 7 2 4F RT A16WE 1998052900295 19980529 00295 NM 1998 5 29 SWAA980855 1 19980514 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 902 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND DENTED FUSELAGE SKIN AT BS 902, 3 BELOW STR 14L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900296 19980529 00296 NM 1998 5 29 SWAA980856 1 19980514 A 5241 SKIN BOEING 737 7373H4 1384600 NM GALLEY DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED FWD GALLEY DOOR OUTER SKIN LOWER HINGE CUTOUT UPPER CORNER. REPAIRED PER SWA ACO 31 8952. 2 L 7 2 4F RT A16WE 1998052900297 19980529 00297 NM 1998 5 29 SWAA980858 1 19980514 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 947-967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 947-967, RBL 45, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900298 19980529 00298 NM 1998 5 29 SWAA980859 1 19980515 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED FLOORBEAM AT BS 1016, LBL 6-36, WL 207-208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900299 19980529 00299 NM 1998 5 29 SWAA980860 1 19980515 A 5320 ANGLE BOEING 737 7373H4 1384600 NM TAIL CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED RT VERT TO FUSELAGE L ANGLE IS KNIFE EDGED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900300 19980529 00300 NM 1998 5 29 SWAA980857 1 19980515 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 1010/1028 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND VERTICAL STABILIZER LT SKATE ANGLE GOUGED AT APPROX BS 1010 AND BS 1028. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900301 19980529 00301 NM 1998 5 29 SWAA980861 1 19980515 A 5320 ANGLE BOEING 737 7373H4 1384600 NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FRAME FWD SIDE OF W/W OPENING LBL60. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900302 19980529 00302 NM 1998 5 29 SWAA980862 1 19980516 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1093 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND GOUGES ON WEB AT BS 1093, 3 BELOW BOTTOM STIFFENER COMMON TO RAM AIR INLET CUTOUT, APU TORQU E BOX. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900303 19980529 00303 NM 1998 5 29 SWAA980863 1 19980516 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 442 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND SKIN DAMAGED AT BS 422, WL 236, RBL 73.8 BELOW STR 13R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900304 19980529 00304 NM 1998 5 29 SWAA980864 1 19980516 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED SKATE ANGLE AT BS 540, LBL 70, WL 169. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900305 19980529 00305 NM 1998 5 29 SWAA980865 1 19980516 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED STRINGER CLIP AT BS 727C, LBL 31, WL 162. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900306 19980529 00306 NM 1998 5 29 SWAA980866 1 19980516 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED STRINGER 21R AT BS 727A +10, RBL 56, WL 176. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900307 19980529 00307 NM 1998 5 29 SWAA980867 1 19980516 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 986.5 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND UPPER ROW OF FASTENERS HAS SHORT E.D. ON FRAME AND FAIL SAFE ANGLE AT BS 986.5, WL 208, LBL 68. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900308 19980529 00308 NM 1998 5 29 SWAA980868 1 19980517 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C1 CHECK, FOUND CRACKED LT FUSELAGE SKIN AT BS 520 AND S-16L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998052900309 19980529 00309 NM 1998 5 29 SWAA980869 1 19980517 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 893 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 893, STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998052900310 19980529 00310 NM 1998 5 29 SWAA980870 1 19980517 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED STRINGER CLIP AT BS 727C, STR 21L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900311 19980529 00311 NM 1998 5 29 SWAA980871 1 19980517 A 3350 6104791 POWER SUPPLY BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LT OVERWING EXIT POWER SUPPLY PER BOEING MM. OPS CK GOOD. 2 L 7 2 4F A16WE 1998052900312 19980529 00312 NM 1998 5 29 SWAA980872 1 19980517 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED AT BS 847 STRINGER 24R-25R BELTFRAME WEB AFT OF CARGO DOOR. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900313 19980529 00313 NM 1998 5 29 SWAA980873 1 19980517 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 797 BULGING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND SKIN BULGING AND WRINKLED LAP SPLICE FUSELAGE AT BS 797, LT SIDE OF FUSELAGE. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998052900314 19980529 00314 NM 1998 5 29 SWAA980874 1 19980517 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359SW 26596 DURING SERVICE CHECK, FOUND AFT SECTION OF EMERGENCY LIGHTING INOP. REMOVED AND REPLACED AFT LT BATTERY PACK EMERGENCY LIGHTING PER BOEING MM. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1998052900315 19980529 00315 NM 1998 5 29 UPS98226740 1 19980428 A 5320 WEB BOEING 727 72751C 1384015 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, RT MAIN WHEEL WELL CORROSION ON WEB AT BL 20 STA 870 BULKHEAD JUST BELOW FLOOR LEVEL. REPAIR CARRIE D OUT IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1998052900316 19980529 00316 NM 1998 5 29 UPS98226741 1 19980424 A 5753 651920216 CARRIAGE BOEING 727 72751C 1384015 NM NR 8 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D NR 8 FLAP CARRIAGE HAS CORROSION IN BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM. 2 L 7 3 4F A3WE 1998052900317 19980529 00317 NM 1998 5 29 UPS98226742 1 19980424 A 5753 CARRIAGE BOEING 727 72751C 1384015 NM NR 3 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, NR 3 FLAP CARRIAGE SPINDLE LINK CORRODED. LINK ASSY REPLACED IAW OHM 57-52-01. 2 L 7 3 4F A3WE 1998052900318 19980529 00318 NM 1998 5 29 UPS98226743 1 19980424 A 5753 CARRIAGE BOEING 727 72751C 1384015 NM NR 3 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, NR 3 FLAP CARRIAGE SPINDLE LINK SUPPORT CORRODED. LINK SUPPORT REPLACED IAW OHM 57-52-01. 2 L 7 3 4F A3WE 1998052900319 19980529 00319 NM 1998 5 29 UPS98226744 1 19980511 A 5311 651985126 FRAME BOEING 727 72751C 1384015 NM BS 880.45 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, WINDOW FRAME BS 880.45 RT FOUND CRACKED FWD TOP CORNER. REPLACED IAW BOEING DRG NR 65C-18383 AND EO B727-5310-3057. 2 L 7 3 4F A3WE 1998052900320 19980529 00320 NM 1998 5 29 UPS98226745 1 19980424 A 5400 WEB BOEING 727 72751C 1384015 NM BS 1387 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, SUSPECT CRACK ON RT WEB AT BS 1387 IN SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL ENGINE NR 2. HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4 . CRACK CONFIRMED WEB REPLACED WITH WEB FABRICATED AND INSTALLED IAW DRG 6517 555. 2 L 7 3 4F A3WE 1998052900321 19980529 00321 NM 1998 5 29 UPS98226746 1 19980424 A 5400 WEB BOEING 727 72751C 1384015 NM BS 1387 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, SUSPECT CRACK ON LT WEB AT BS 1387 IN SUPPORT STRUCTURE ABOVE HORIZONTAL FIREWALL ENGINE NR 2. HFEC CARRIED OUT IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4. CRACK CONFIRMED WEB REPLACED WITH WEB FABRICATED AND INSTALLED IAW DRG 657 555. 2 L 7 3 4F A3WE 1998052900322 19980529 00322 NM 1998 5 29 UPS98226747 1 19980422 A 2780 65162261 TORQUE TUBE BOEING 727 72751C 1384015 NM NR 2 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, CRACK CONFIRMED IN NR 2 KRUEGER FLAP TORQUE TUBE STRUCTURE. REPLACED NR 2 KREUGER FLAP ASSY IAW MM 2 7-81-01. 2 L 7 3 4F A3WE 1998052900323 19980529 00323 NM 1998 5 29 UPS98226748 1 19980503 A 5320 ANGLE BOEING 727 72751C 1384015 NM BS 351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, CORRODED ANGLE RT WALKWAY AFT SUPPORT AT ST 351. REPLACED ANGLE IAW SRM 53-10-2. 2 L 7 3 4F A3WE 1998052900324 19980529 00324 NM 1998 5 29 UPS98226749 1 19980504 A 5230 SKIN BOEING 727 72751C 1384015 NM CARGO DOOR DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE:D, A NUMBER OF DEEP DENTS IN SKIN (FWD CARGO DOOR) SKIN HAS ALOT REPAIRS. SKIN REPLACED IAW DRW NO 65-8 620. 2 L 7 3 4F A3WE 1998052900325 19980529 00325 WP 1998 5 29 UPS98826750 1 19980514 A 5320 3750257503 FITTING DOUG DC8 DC873F 302199F WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, STA 1040-1060, STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DWG.375025 7 QND SRM 51-3 -0. 2 L 7 4 4F RT 4A25 1998052900326 19980529 00326 WP 1998 5 29 UPS98826751 1 19980514 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 426 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, STA 426 AT LONGERON 34L, THE FINGER DOUBLER IS CRACKED. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK 874-569. 2 L 7 4 4F RT 4A25 1998052900327 19980529 00327 WP 1998 5 29 UPS98826752 1 19980514 A 5320 37502571N FITTING DOUG DC8 DC873F 302199F WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, STA 440-460, STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998052900328 19980529 00328 WP 1998 5 29 UPS98826753 1 19980515 A 5720 565544114 STRAP DOUG DC8 DC873F 302199F WP WS 621 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, RT WING L/E AT STA XFS621.000, THE L/E RIB TIE STRAP IS CRACKED. REMOVED, FABRICATED AND REPLACED ST RAP IAW DWG 5655441 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998052900329 19980529 00329 WP 1998 5 29 UPS98826754 1 19980515 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 397.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, RT WING L/E AT STA XFS397.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998052900330 19980529 00330 WP 1998 5 29 UPS98826755 1 19980514 A 5330 SKIN DOUG DC8 DC873F 302199F WP WS 598 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE:C, LT WING L/E LWR SKIN AT STA XFS598.000 IS CRACKED AT THE DRAIN HOLE AND 1 SCREW. STOP DRILLED CRACKS AND REPAIRED IAW SRM ADD DC8-5320-4087. 2 L 7 4 4F RT 4A25 1998052900331 19980529 00331 WP 1998 5 29 UPS98826756 1 19980521 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 EMER LTS INOP. REMOVED AND REPLACED EMER BATTERY PACK, GROUND CHECKS NORMAL. ON P/N 5708458-503 S/N FTL 145 OFF P/N 57 08458-503 S/N 925. 2 L 7 4 4F RT 4A25 1998052900332 19980529 00332 1998 5 29 SWIA971173 4 19980509 A 3425 AHARS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT/RT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 221SW 120290 BOTH AHRS FAILED IN FLIGHT. RETURNED TO FIELD AS HEADINGS GAVE ERRONEOUS READINGS. REINITIALIZED BOTH AHRS COMPUTORS. O PS CHECKS GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052900333 19980529 00333 SO 1998 5 29 SWIA971174 1 19980509 A 2750 CONTROL UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 205SW 120260 IN THE APPROACH AREA BOUGHT FLAP LEVER TO 15 DEGREES CONTROL FAULT AND STALL WARNING LIGHTS FLASHING. FOLLOWED QRH TRIE D TO RESET BUT WOULDN'T. CALLED MX CONTROL, VIA ALTERNATE RADIO AND TOLD US BRING FLAP LEVER UP AND THEN FLAPS WOULD NO T COME UP. OUTBOARD FLAP PAIR FLASHING THROUGHOUT. DIVERTED FROM CLD TO LAX. REPLACED FCU. CYCLED FLAPS TEN TIMES. O PS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052900334 19980529 00334 SO 1998 5 29 SWIA971175 1 19980509 A 2751 ANN UNIT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 NM 07 205SW 120260 ON APPROACH, CONTROL FAULT ON OUTBOARD FLAP. FLAPS WERE STUCK AT 6 DEGREES AND WE COULD NOT EXTEND OR RETRACT. UNABLE TO LAND IN OXNARD. RETURNED TO LAX. REPLACED FLAP ANNUNICATOR UNIT. CLEARED FAULT HISTORY AND CYCLED FLAPS SEVERAL TI MES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052900335 19980529 00335 SO 1998 5 29 SWIA971176 1 19980502 A 2750 FILTERS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 214SW 120280 AFTER TAKEOFF, WE HAD A FLAP DISAGREEMENT LIGHT. PERFORMED ABNORMAL CHECKLIST AND RETURNED TO LAX. INSPECTED AND CLEAN ED OUTBOARD FLAP ACTUATOR LINE FILTERS (BOTH LEFT AND RIGHT). PERFORMED OPS CHECKS OF FLAP SYSTEM. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052900336 19980529 00336 SO 1998 5 29 SWIA971177 1 19980502 A 2751 CONNECTORS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS DIRTY A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 214SW 120280 AFTER TAKEOFF, ATTEMPTED FLAPS UP. DISAGREEMENT FLAP LIGHT ILLUMINATED (OUTBOARD WAS AGREEING BUT NOT THE NACELLE AND I NBOARD). REFERED TO QRH HOWEVER UNSUCCESSFUL. RETURNED TO LAX. CLEANED CANNON PLUGS ON OUTBOARD FLAPS AND RECHECKED F LAP CONTROL UNIT. OPERATED FLAPS NUMEROUS TIMES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052900337 19980529 00337 SO 1998 5 29 SWIA971178 1 19980506 A 2750 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT TE FLAP ACT FAILED A SWIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CR CRUISE 1 NM 07 235SW 120310 IN CRUISE FLIGHT, FLAP AND ADVANCED STALL WARNING LIGHTS ILLUMINATED ON MAP ALSO CONTROL FAULT LEFT AND RIGHT. NUMERIC DISPLAY ILLUMINATED ON FLAP ANNUNICATOR PANEL WITH OUTBOARD FLAP PAIRS FLASHING. RESET IAW QRH AND PROBLEM REOCCURRED. REPAIRED BROKEN WIRE AT LEFT OUTBOARD FLAP ACTUATOR CANNON PLUG. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052900338 19980529 00338 EU 1998 5 29 QXEA9800668 1 19980520 A 3310 LG18 BALLAST GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 09 483US 11233 GTF - ELECTRICAL/ACRID SMELL COMING FROM CAPTAINS INSTRUMENT PANEL. WHITE FLOOD LIGHTS WORK, RED FLOOD LIGHTS DO NOT. L OCAL MAINTENANCE INSPECTED BALLAST AND PLACED RED FLOOD LIGHTS ON MEL. SEA MAINTENANCE LATER CLEARED MEL BY REPLACING T HE BALLAST TRANSFORMER LG18. OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998052900339 19980529 00339 EU 1998 5 29 QXEA9800669 1 19980521 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 GEG - BOTH OVERHEAD EMERGENCY EXIT SIGNS AT ROW 8 OUT. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052900340 19980529 00340 WP 1998 5 29 ABXA9800455 1 19980518 A 3260 840534 SENSOR DOUG DC9 DC941 302207N WP LT MLG OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 958AX 47760 IN CRUISE FLIGHT, GEAR DOOR OPEN LIGHT ILLUMINATED WITH RIGHT HYDRAULIC PUMP IN HIGH MODE. LIGHT WENT OUT FOR 10 MINUTE S THEN ILLUMINATED WITH PUMPS IN HIGH. RECYCLED GEAR AND PERFORMED UPLATCH CHECK SATISFACTORILY. ADJUSTED LEFT MAIN LA NDING GEAR DOOR POSITION SENSOR IAW DC9 SMM 32-60-03. 2 L 7 2 4F A6WE 1998052900341 19980529 00341 WP 1998 5 29 ABXA9800456 1 19980511 A 5400 591326241 ANGLE DOUG DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE LEFT UPPER PYLON ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW DC9 SRM 54-04. 2 L 7 2 4F A6WE 1998052900342 19980529 00342 WP 1998 5 29 ABXA9800457 1 19980506 A 5753 5912149511 HINGE DOUG DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, THE LEFT FLAP CENTER HINGE WAS FOUND CRACKED. REPLACED IAW DC9 MM 27-50-1. 2 L 7 2 4F A6WE 1998052900343 19980529 00343 WP 1998 5 29 ABXA9800458 1 19980512 A 5313 3915129501 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 604 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, LEVEL II CORROSION WAS FOUND ON LONGERON 28 RIGHT END CAP STATION 604. REPLACED IAW DC9 SRM 51-10-03. 2 L 7 2 4F A6WE 1998052900344 19980529 00344 WP 1998 5 29 ABXA9800459 1 19980511 A 5320 3915129507 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 604 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, LEVEL II CORROSION WAS FOUND ON LONGERON 27 RIGHT AND END CAP AT STATION 604. REPLACED FITTING IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998052900345 19980529 00345 WP 1998 5 29 ABXA9800460 1 19980512 A 5312 3917853503 BLKHD FITTING DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, AFT PRESSURE BULKHEAD DOOR RIGHT VERTICAL SUPPORT FITTING WAS FOUND CRACKED. REPLACED FITTING IAW DC9 S RM 51-10-04. 2 L 7 2 4F A6WE 1998052900346 19980529 00346 WP 1998 5 29 ABXA9800461 1 19980511 A 5313 95301281 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 756 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, LONGERON 5 RIGHT WAS FOUND CRACKED AT STATION 756. REPAIRED IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998052900347 19980529 00347 WP 1998 5 29 ABXA9800462 1 19980511 A 5320 3914677501 SPLICE DOUG DOUG DC9 DC932 3022066 WP BS 794-813 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, LONGERON SPLICE AT STATION 794-813, LONGERON 30 WAS FOUND CRACKED. REPLACED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998052900348 19980529 00348 WP 1998 5 29 ABXA9800463 1 19980512 A 5315 99115451 FLOORBEAM DOUG DOUG DC9 DC932 3022066 WP BS 351 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, FLOORBEAM AT STATION 351 BL6 LEFT WAS FOUND CRACKED. REPAIRED IAW ABX REA D953-23658-MR. 2 L 7 2 4F A6WE 1998052900349 19980529 00349 WP 1998 5 29 ABXA9800464 1 19980520 A 3260 7000010101 SWITCH DOUG DC9 DC941 302207N WP NLG OUT OF ADJ A ABXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 958AX 47760 DURING APPROACH, NOSE GEAR UNSAFE LIGHT ILLUMINATED. LIGHT CAME ON WHEN THROTTLES RETARDED AND REMAINED ON FOR APPROX 3 0 SECONDS. RECYCLED GEAR AND LIGHT WENT OUT. GEAR OPERATED NORMALLY. ADJUSTED DOWNLOCK PROXIMITY SWITCH. OPS CHECKED GOOD IAW DC9 MM 32-60-00. 2 L 7 2 4F A6WE 1998052900350 19980529 00350 WP 1998 5 29 MWEA98619 1 19980521 A 2910 LINE DOUG DC9 DC914 3022034 WP LT MLG WW LEAKING A MWEA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 31 400ME 45727 AFTER TAXING IN TO GATE RAMP EMPLOYEES NOTICED BAD FUMES UPON OPENING FOWARD PIT DOOR PAX DEPLANED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC BRAKE PRESSURE TRANSMITER SUPPLY LINE. 2 L 7 2 4F A6WE 1998052900351 19980529 00351 NE 1998 5 29 DL767981067 2 19980518 A 7200 ENGINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 108DL 33979 5414 22220 580317 IN DESCENT, NR 2 ENG SHOWED NO OIL QTY AND 10 PSI PRESS. SHUT DOWN ENGINE PER POM. MAINTENANCE IN PROGRESS. FOUND MET AL ON CHIP DETECTOR, REPLACED ENGINE. 2 L 7 2 4F 4 F RT A1NM E13NE 1998052900352 19980529 00352 WP 1998 5 29 DLL19981071 1 19980518 A 3530 PBE MR10046NY LKHEED 1011 10113853 5265020 WP CABIN DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 PBE IN AFT LEFT CABIN FOUND DAMAGED. REPLACED PBE UNIT. 2 L 7 3 4F A23WE 1998052900353 19980529 00353 NM 1998 5 29 DL72L981072 1 19980519 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 514DA 611 21430 AT DEPARTURE CHECK, FOUND THAT THE LT OVERWING EXIT EMER LIGHT FAILED THE STDBY PWR CHECK. REMOVED AND REPLACED BATTERY PACK AND PWR SUPPLY RACK. 2 L 7 3 4F A3WE 1998052900354 19980529 00354 WP 1998 5 29 DLL19981074 1 19980519 A 2800 LS1439415A CIRCUIT BREAKER LKHEED 1011 10113853 5265020 WP E/E COMPT MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 763DL 193Y1197 AT ALTITUDE COULD NOT GET FUEL OUT OF TANK NR 1, IMBALANCE AT 5000 LBS BETWEEN TANKS 1 AND 3. WITH TANK PUMPS FOR ENGIN E NR 3 UNLATCHED FUEL QUANTITY CONTINUED TO DECREASE, INDICATORS TESTED 4.0. BOTH RCCBS FOR TANK 3 BOOST PUMPS WOULD NO T SHUT OFF EITHER WITH SWITCHLIGHT ACTUATION OR BY PULLING COCKPIT CIRCUIT BREAKERS. REPLACED TANK 3 INBD AND OTBD BO OST PUMP RCCBS. RAN ENGINES VERIFIED NR 1 TANK WAS ABLE TO FEED ALL ENGINES BOTH BOOST PUMPS OPERATED NORMAL. 2 L 7 3 4F A23WE 1998052900355 19980529 00355 WP 1998 5 29 DLL13981076 1 19980519 A 5711 1528390107 SPAR CAP LKHEED 1011 10113851 5265010 WP WS 258 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 786DL 193A1123 OVERSIZED FASTENER HOLES WERE FOUND IN THE VERTICAL FLANGE OF THE LT WING LWR REAR SPAR CAP AT APPROX IWS 258. THE FAST ENER FINAL DIAMETER WAS 0.3428. REPAIRED PER ERA 331709-14AD. 2 L 7 3 4F A23WE 1998052900356 19980529 00356 NM 1998 5 29 DL72S981081 1 19980519 A 5330 SKIN BOEING 727 727232 1384082 NM L-1 DOORWAY CRCAKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FOUND AT A-1 LETTER CHECK, 1.125 INCH CRACK AT FUSELAGE SKIN AT MAIN ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED PER 53-30- 3. 2 L 7 3 4F A3WE 1998052900357 19980529 00357 NM 1998 5 29 DL72S981082 1 19980519 A 5720 BRACKET BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 NR 1 SLAT ACT O/B ATTACH BRACKET CRACKED AT I/B WEB. REPAIRED PER MM 57-20-21 P 812. 2 L 7 3 4F A3WE 1998052900358 19980529 00358 NM 1998 5 29 DL72S981083 1 19980519 A 5720 STIFFENER BOEING 727 727232 1384082 NM NR 3 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 NR 3 SLAT O/B TRACK I/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21 P 813. 2 L 7 3 4F A3WE 1998052900359 19980529 00359 NM 1998 5 29 DL72S981084 1 19980519 A 5320 65872607 FITTING BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 TAIL SECTION TIE BOLT FITTING CRACKED LT I/B FITTING, CRACKED JUST O/B OF BOLT HEAD. REPLACED FITTING PER BOEING DWG 65 -17509 REV M. 2 L 7 3 4F A3WE 1998052900360 19980529 00360 NM 1998 5 29 DL72S981085 1 19980519 A 5754 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 FOUND ON A-1 LETTER CHECK, NR 6 SLAT NOSE RIB CRACKED I/B SIDE OF ACTUATOR .75 INCH. REPAIRED PER M/M 57-54-0. 2 L 7 3 4F A3WE 1998052900361 19980529 00361 NM 1998 5 29 DLM11981086 1 19980519 A 3350 6044113 BATTERY PACK DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 814DE 48769 ON TRIP CHECK, FOUND EMERGENCY TRACK LIGHTING INOP BETWEEN ROWS 30-49 ON BOTH SIDES OF A/C. REPLACED NR 5 BATTERY PACK. EMERGENCY LIGHTS OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 1998052900362 19980529 00362 NM 1998 5 29 DL72W981089 1 19980520 A 3350 P2070003001 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 22108 EMERGENCY FLASHLIGHT AT 1 LEFT DOOR, FAILED LED CK. REPLACED FLASHLIGHT. 2 L 7 3 4F A3WE 1998052900363 19980529 00363 NM 1998 5 29 DL72S981091 1 19980512 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 477DA 20754 MAIN ENTRANCE EMERG EXIT LIGHTS INOP DURING EMERG LIGHT TEST. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1998052900364 19980529 00364 NM 1998 5 29 DHL98726004 1 19980521 A 7930 1163P005202 SWITCH BOEING 727 727228 NM NR 3 ENGINE FAILED A DHLA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 726DH 20409 ON TAKEOFF, NR 3 ENGINE OIL FILTER BY PASS LIGHT CAME ON. AFTER RETRACTION OF GEAR, THE LIGHT WENT OUT. OIL TEMPERATUR E AND PRESSURE WERE NORMAL. PERFORMED ALTERNATE PROCEDURES. REMOVED AND INSPECTED NR 3 OIL FILTER. DEFERRED OIL FILTER BY PASS SWITCH PER MEL 79-2. 2 L 7 3 4F A3WE 1998052900365 19980529 00365 NM 1998 5 29 P5CA9800776 1 19980521 A 7110 COWL BOEING 747 747132 1384882 NM NR 2 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NUMBER 2 ENGINE NOSE COWL SKIN DENTED AT 0630 POSITION. REPAIRED NOSE COWL PANEL AT 0630 POSITION PER SRM 51-40-07. 2 L 7 4 4F A20WE 1998052900366 19980529 00366 WP 1998 5 29 RRXA98137 1 19980413 A 5330 5773863 SKIN DOUG DC8 DC873F 302199F WP BS 254 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND DENT 8 INCHES FROM STATIC PORT CENTER, AT STA 257 BETWEEN LONGERONS 27 LEFT AND 28 LEF T. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED DOUBLER REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0458 4. 2 L 7 4 4F RT 4A25 1998052900367 19980529 00367 WP 1998 5 29 RRXA98138 1 19980519 A 5311 5772964513 FRAME DOUG DC8 DC873F 302199F WP BS 260 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 260 BETWEEN LONGERONS 25 LEFT AND 26 LEFT. REMOVED D AMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO EN GINEERING SKETCH REO-04718. 2 L 7 4 4F RT 4A25 1998052900368 19980529 00368 WP 1998 5 29 RRXA98139 1 19980521 A 5311 561306481 FRAME DOUG DC8 DC873F 302199F WP BS 70 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 70 AT LONGERON 27 RIGHT. REMOVED DAMAGED SECTION, TR EATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH R EO-04747. 2 L 7 4 4F RT 4A25 1998052900369 19980529 00369 WP 1998 5 29 RRXA98140 1 19980520 A 5313 5613858229 LONGERON DOUG DC8 DC873F 302199F WP BS 23 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 3 RIGHT AT STA 12, ALSO CORROSION DAMAGE TO LONGERON 10 R IGHT AT STA 23. REMOVED DAMAGED SECTIONS FROM LONGERONS 3 RIGHT AND 10 RIGHT, TREATED AREAS IAW DC-8 SRM 51-1-8. FABRI CATED AND INSTALLED REPAIR DOUBLERS TO LONGERON 3 RIGHT AND 10 RIGHT IAW FAA APPROVED ENGINEERING SKETCH REO-04748. 2 L 7 4 4F RT 4A25 1998052900370 19980529 00370 WP 1998 5 29 RRXA98141 1 19980521 A 5755 565516712 CHANNEL DOUG DC8 DC873F 302199F WP NR 3 SPOILER CHAFING A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CHAFFING ON UPPER FLANGE CHANNEL ON NR 3 SPOILER RIGHT WING, MATERIAL LOSS WAS THROUGH THE ENTIRE FLANGE THICKNESS. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMC O ENGINEERING SKETCH REO-04752. 2 L 7 4 4F RT 4A25 1998052900371 19980529 00371 WP 1998 5 29 RRXA98142 1 19980522 A 5311 5772787 FRAME DOUG DC8 DC873F 302199F WP BS 120 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CRACK ON FRAME AT STA 120 AT LONGERON 6 LEFT. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04759. 2 L 7 4 4F RT 4A25 1998052900372 19980529 00372 WP 1998 5 29 RRXA98143 1 19980522 A 5311 56402433 FRAME DOUG DC8 DC873F 302199F WP BS 1680 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND MULTIPLE CORROSION AREAS ON FRAME AT STA 1680 BETWEEN LONGERONS 9 LEFT TO 9 RIGHT. RE MOVED DAMAGED SECTIONS, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER T IMCO ENGINEERING SKETCH REO-09610. 2 L 7 4 4F RT 4A25 1998052900373 19980529 00373 WP 1998 5 29 RRXA98144 1 19980519 A 2720 75130 TRANSFER VALVE DOUG DC8 DC862F 3021972 WP RUDDER CONTROL MALFUNCTIONED A RRXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 15 998CF 46139 UPON LEAVING 10,000 FT ASKING FOR CLIMB CK, AIRCRAFT EXPERIENCED A UNCONTROLLED RIGHT TURN, AS IF FLYING IN ANOTHER A/C WAKE. CK WITH ATC TO VERIFY POSSIBLE TRAFFIC. SHORTLY AFTER INITIAL TURN UNCONTROLLED AND UNCOMMANDED FLIGHT CONDITION S (YAW AND ROLL) INCREASED IN FREQUENCY, UNABLE TO CONTROL A/C HDG/ALT. DECLARED EMERGENCY AND RETURN TO BSM WITH PROBL EM PERSISTING ALL WAY TO GROUND. DEFERRED AUTO FLIGHT/YAW DAMPER SYSTEM IAW MEL 22-2 CAT C CONTROL NR 805312. REMOVED AND REPLACED RUDDER TRANSFER VALVE, OPS CHECKS LEAK CHECKS GOOD CLEARS DMI 805312 PLACARD REMOVED. 2 L 7 4 4F 4A25 1998052900374 19980529 00374 WP 1998 5 29 RRXA98145 1 19980519 A 3260 STRIKER DOUG DC8 DC873F 302199F WP RT MLG OUT OF ADJUST A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 605AL 46106 RIGHT MAIN GEAR DOOR WARNING LIGHT ALTERNATE AND RED DOORS NOT LATCHED LIGHT ON WITH GEAR UP CYCLED GEAR NO HELP. ADJ ALTERNATE LIGHT STRIKER PLATE RIGHT SIDE. ADJ ADJUSTABLE LINK TO MAINTAIN MIN OF 0.010 W/GEAR DOWN AND DOORS OPEN BETWE EN LINK OPS CK OK. 2 L 7 4 4F RT 4A25 1998052900375 19980529 00375 1998 5 29 VNAA9805011 4 19980520 A 3418 CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AOA SYST TRIPPED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 328JS 3030 THE AIRCRAFT RETURNED TO THE GATE AFTER RECEIVING AN ANGLE OF ATTACK, AND SHAKER FAIL WARNING MESSAGES. MAINTENANCE INS PECTED AND FOUND THE RIGHT HAND ANGLE OF ATTACK, AND THE RIGHT HAND STALL WARNING CIRCUT BREAKER OPEN. THEY CLOSED THE CIRCUT BREAKERS, AND PERFORMED OPERATION CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-33-00. THE CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998052900376 19980529 00376 NM 1998 5 29 98FDEA00365 1 19980523 A 2710 ARH7057517 ACTUATOR DOUG MD11 MD11 3023602 NM RT AILERON FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 584FE 48436 STA-LAX: ALL DEFLECT DISAG ALERT ON SLAT RETRACTION. RETURNED TO LAX. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL 27-2. REMOVED ACTUATOR AND INSTALLED FIXED PUSHROD PER MEL MX PROCEDURE 27-2. REMOVED AND REPLACED RT OUTBOARD AILERON DEFL ECTION ACTUATOR PER M/M 22-16-02-4. 2 L 7 3 4F RT A22WE 1998052900377 19980529 00377 WP 1998 5 29 98FDEA00364 1 19980523 A 2612 FIRE LOOP DOUG DC10 DC1030F 3023504 WP NR 1 ENGINE MALFUNCTIONED A FDEA A F E UNSCHED LANDING ACTIVATE FIRE EXT. ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 320FE 47835 NR 1 ENG FIRE DETECT SYS LOOP-B LT ON IN FLT, RED TABS ACCOMPLISHED, CHECKED OK. APPROX 2 HRS LATER NR 1 ENG FIRE LIGHT S ON. ACCOMPLISHED RED TABS, EMERGENCY LANDING ABQ. LANDED OVERWEIGHT. 2 L 7 3 4F RT A22WE 1998052900378 19980529 00378 NM 1998 5 29 98FDEA00361 1 19980521 A 2613 OVERHEAT LIGHT BOEING 727 7272S2F 1384O81 NM LWR AFT FUSELAGE ILLUMINATED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 203FE 22925 LOWER AFT BODY OVERHEAT LIGHT CAME ON JUST AFTER FIRST LEVEL OFF. NR 2 AND NR 3 BLEEDS OPEN BOTH PACKS ON, LIGHT WENT O UT AFTER ONE MINUTE BUT CAME BACK ON DURING CLIMB. STARTED RED TAB PROCEDURE, LIGHT WENT OUT WHEN NR 1 BLEED AND LEFT P ACK TURNED OFF REMAINDER OF FLIGHT WITH NR 3 BLEED AND RIGHT PACK, LIGHT DID NOT COME BACK ON. THE M366 OVERHEAT DETECT OR WAS REPLACED, SHORT ONE IN KEEL BEAM. ALSO, REPLACED M365 OVERHEAT DETECTOR, RIGHT AFT AIRSTAIR DETECTOR. OPERATION AL CHECKS NORMAL ON ENGINE AND APU RUNS. 2 L 7 3 4F A3WE 1998052900379 19980529 00379 WP 1998 5 29 SCNA98048 1 19980520 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1015 3022118 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 5924 48289 DURING A LINE CHECK, THE EMERGENCY LIGHT SELF TEST FAILED IN THE AFT SECTION OF THE CABIN. REMOVED AND REPLACED THE BAT TERY POWER SUPPLY AND BATTERY PACK, FUNCTIONALLY TESTED GOOD. 2 L 7 3 4F A22WE 1998052900380 19980529 00380 WP 1998 5 29 DHL98803001 1 19980522 A 2897 WIRE DOUG DC8 DC873F 302199F WP NR 4 FUEL SYST BROKEN A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 803DH 46123 NR 4 ALT QUAN LOW LIGHT ILLUMINATED. USED ABNORMAL PROCEDURE AND LIGHT WOULD NOT EXTINGUISH. NR 4 ALT SHUT OFF VALVE C LOSED AND LIGHT WOULD NOT EXTINGUISH WHILE USING ABNORMAL PROCEDURE. FOUND BROKEN WIRE AT CANNON PLUG P1-113 TO ALT NR 4 REFILL SOLENOID. REPAIRED WIRE. OPS CHECKED GOOD PER MM 28-21-2 . NR 4 LOW LEVEL LIGHT SYSTEM OPS CHECK GOOD PER MM 28-42-0. 2 L 7 4 4F RT 4A25 1998052900381 19980529 00381 NM 1998 5 29 P5CA9800777 1 19980522 A 2612 65B4750944 FIRE DET PANEL BOEING 747 747124 1384874 NM COCKPIT SPARKING A P5CA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 23 855FT 19733 AFTER ENGINE START WHEN POWER WAS TRANSFERRED TO AIRCRAFT POWER AN ACRID SMELL WAS NOTICED IN COCKPIT. SPARKS WERE SEEN COMING FORM FIRE DETECTION PANEL BEHIND P6 PANEL. REPLACED CARD INDEX PANEL PER M/M 26-11-05 AND OPERATIONAL CHECKED P ER M/M 26-11-00. 2 L 7 4 4F A20WE 1998052900382 19980529 00382 WP 1998 5 29 TC8A98027 1 19980522 A 3240 1542522 BRAKE DOUG DC8 DC8F54 3021926 WP MLG LOCKED UP A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 802CK 6852 45679 ON TAXI OUT, AIRPLANE SHUDDERED AND CAME TO A STOP, WOULD NOT MOVE. REMOVED AND REPLACED NR 6 BRAKE ASSY, LEAK CHECK O PS CHECKED OK PER M/M 32-42-1. 2 L 7 4 4F 4A25 1998052900389 19980529 00389 SO 1998 5 29 98ZZZX1984 1 19980430 A 5610 6971200 WINDOW PIPER PA34 PA34200T 7103406 SO PILOT LT FWD DEPARTED A DZDA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 NM 07 1597X 5650 347570305 PILOT SIDE WINDOW CRACKED AND BLEW OUT DURING FLIGHT. 1 L 7 2 3O A7SO 1998052900393 19980529 00393 SW 1998 5 29 98ZZZX1988 1 19980429 A 2612 8777871 FLEX CABLE BELL 214 214ST 1182106 SW ENG COMPT CHAFED A HEEA O OTHER N FALSE WARNING AP APPROACH 1 SW 03 6957Y 28139 APPROXIMATELY ONE MILE FROM BASE, NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED. AIRCRAFT LANDED AT MORGAN CITY BASE. FLE X CABLE CHAFED AT BEND. REPAIRED AND RETURNED TO SERVICE. 2 G 7 2 4U H10SW 1998052900394 19980529 00394 NM 1998 5 29 98ZZZX1989 1 19980413 A 2140 900P3250210103 VALVE DOUG MD900 MD900 3027375 NM FLOW CONTROL FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 253 0047 90000012 FLOW CONTROL VALVE WILL NOT OPEN AND CLOSE PROPERLY. ALSO, THE VALVE WILL NOT REMAIN SEATED WHICH CAUSES BLEED AIR TO P ASS BY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998052900395 19980529 00395 NM 1998 5 29 98ZZZX1990 1 19980414 A 5320 900FF337012102 SUPPORT DOUG MD900 MD900 3027375 NM RT INLET CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 147 90000012 RT INLET SUPPORT ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998052900396 19980529 00396 NM 1998 5 29 98ZZZX1991 1 19980414 A 5320 900FF337012101 SUPPORT DOUG MD900 MD900 3027375 NM LT INLET CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 147 90000012 LT INLET SUPPORT ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998052900399 19980529 00399 SO 1998 5 29 98ZZZX1994 2 19980420 A 8520 643202 CRANKCASE STUD CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO NR 1 CYL BASE BROKEN A A HBCA K NONE O OTHER IN INSP/MAINT 1 SW 11 402BF 1269 402B1076 183537R DURING THE COURSE OF A 100-HOUR INSPECTION, THE MECHANIC NOTICED THE LEFT ENGINE, NR 1 CYLINDER, MOST FORWARD UPPER STUD HAD BROKEN OFF FLUSH WITH THE CYLINDER BASE/SKIRT. THE CYLINDER WAS REMOVED AND THE CASE WAS INSPECTED FOR CRACKS AND ANY SIGNS OF CHAFING. NONE WAS FOUND. IT IS SUSPECTED THAT TIME IN SERVICE IS THE MAIN CAUSE FOR BREAKAGE OF THE STUD. NO WAY TO DETERMINE THE TOTAL TIME OF THIS STUD OR THE CRANKCASE DUE TO THE REMOVAL OF THE DATA PLATE DURING THE OVERH AUL/CRANKCASE RECERTIFICATION PROCESS. 1 L 7 2 3O 3 O A7CE E8CE 1998052900401 19980529 00401 SO 1998 5 29 98ZZZX1996 2 19980415 A 8520 643202 CRANKCASE BOLT CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO BACKBONE CRACKED A A HBCA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 11 5040Q 1367 402B0347 183973R DURING THE COURSE OF A 100-HOUR INSPECTION, THE MECHANIC NOTICED A SIZEABLE AMOUNT OF OIL ON THE TOP LEFT PORTION OF THE ENGINE CASE. A CLOSER INSPECTION REVEALED A CRACK APPROXIMATELY 1.6250 INCH LONG EMITTING FROM THE 9TH BACKBONE BOLT ( COUNTING FROM FRONT TO BACK). THE CRACK/CASE WAS INSPECTED IAW TCM SBM90-17 AND WAS DETERMINED TO BE UNAIRWORTHY DUE TO THE AMOUNT OF OIL LEAKING FROM SAID CRACK/CASE. THE CASE IN QUESTION HAS NOT BEEN REPAIRED/WELDED IN THE AREA AROUND T HE CRACK. (THE CASE IS THE 'HEAVY' - 7TH STUD VERSION). 1 L 7 2 3O 3 O A7CE E8CE 1998052900402 19980529 00402 EA 1998 5 29 98ZZZX1997 2 19980505 A 8520 75158 SHAFT CESSNA 172 172P 2072436 CE LYC O320 O320D2J 41508 EA CRANK IDLER BROKEN A DUIA K NONE O OTHER IN INSP/MAINT 1 GL 27 51700 17274338 L106423A REMOVED SUCTION SCREEN FOUND CHUNK OF METAL. REMOVED MAGS, LEFT IDLER GEAR 'LOOSE'. REMOVED ACCESSORY CASE, SHAFT-CRAN KSHAFT IDLER BASE BROKEN. 1 H 7 1 3O 3 O NT 3A12 E274 1998052900409 19980529 00409 NE 1998 5 29 98ZZZX2004 2 19980305 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1-2 MALFUNCTIONED A AJLF C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 23 191AJ 53191 FLT JM090 - DURING TAKEOFF ROLL, THE THROTTLES REACHED THE MECHANICAL STOPS WHEN THE TAKEOFF POWER OF 1.97 EPR WAS ACHIE VED. WITH THE ASSISTANCE OF THE FLIGHT CREW, A GROUND RUN WAS PERFORMED BY MAINTENANCE, BUT NO DISCREPANCY WAS DETECTED . THE AIRCRAFT WAS THEN DISPATCHED. 2 L 7 2 4F 4 F RT A6WE E9NE 1998052900414 19980529 00414 WP 1998 5 29 TWAA9806908 1 19980317 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 13R CRACKED AT STATION 1076. REPLACED LONGERON PER SRM 51-03, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998052900415 19980529 00415 WP 1998 5 29 TWAA9806907 1 19980317 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 541 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 27R CRACKED AT STATION 541. REMOVED AND REPLACED WITH NEW PART PER SRM 5 1-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998052900416 19980529 00416 WP 1998 5 29 TWAA9806906 1 19980327 A 5210 SKIN DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FWD ENTRY DOOR INNER SKIN CRACKED AT LOWER FWD CORNER OF DOOR. REPAIRED PER SRM 53-01, PAGE 8, AND STD PRACTICE. (M) 2 L 7 2 4F A6WE 1998052900417 19980529 00417 WP 1998 5 29 TWAA9806905 1 19980327 A 5320 CASTING DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND TAIL SKID CASTING CRACKED AT STATION 1038, LBL 4 INCH, BOTTOM OF FORMER RING . REPLACED CASTING PER SRM 51-01, ITEM 1 PAGE C, AND STANDARD MAINTENANCE PRACTICE. (M) 2 L 7 2 4F A6WE 1998052900418 19980529 00418 WP 1998 5 29 TWAA9806904 1 19980331 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 680 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN CHAIR AND FLOORBEAM SUPPORT CRACKED AT STATION 680, LBL 22 IN. REPLAC ED PART PER SRM 51-01-01 AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998052900419 19980529 00419 WP 1998 5 29 TWAA9806903 1 19980330 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 1043 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FS 1043 LBL 10.5 INCH INTERCOSTAL CRACKED ON LWR FLANGE, LEFT SIDE OF TAIL S KID CASTING. REPAIRED AND REINSTALLED PER SRM 53-01, FIG 2 PAGE 10. (M) 2 L 7 2 4F A6WE 1998052900420 19980529 00420 NM 1998 5 29 TWAA9806902 1 19980502 A 3350 20121 BATTERY PACK BOEING 767 7673Y0 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 STL - FLT 2 - DURING GROUND CHECK, FOUND LEFT SIDE, ROW 32 THROUGH LAV A1, EGRESS LIGHTS INOP. REPLACED BATTERY PACK. C HECK C 5-2-98 MCI. (M) 2 L 7 2 4F RT A1NM 1998052900421 19980529 00421 WP 1998 5 29 TWAA9806901 1 19980501 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9414W 53189 STL - FLT 411 - DURING PRE-FLIGHT CHECK, FOUND EGRESS LIGHTING INOPERATIVE AT CABIN SEAT ROW 22. FOUND BROKEN WIRE. CU T OFF BROKEN CONNECTOR AND DAMAGED WIRE AND SPLICED ON NEW CONNECTOR AND WIRE. CHECK-C 10-26-97 MCI. (M) 2 L 7 2 4F RT A6WE 1998052900422 19980529 00422 NM 1998 5 29 TSAA9833219 1 19980416 A 3350 9221009 POWER PACK BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED AFT SERVICE DOOR EMERGENCY IDENTIFICATION LIGHT POWER PACK DUE TO LIGHT BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900423 19980529 00423 NM 1998 5 29 TSAA9833220 1 19980417 A 3350 1000679 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY DUE TO YELLOW LED STAYING ON ALL THE TIME IN POSITION. OPS CHECKED OK AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900424 19980529 00424 NM 1998 5 29 TSAA9833221 1 19980419 A 3350 8731002511 SIGN BOEING 737 7372M6C 1384708 NM CABIN INOP A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED RIGHT FORWARD SERVICE DOOR EMERGENCY LIGHT IDENTIFIER DUE TO 'ALL'S WELL' LIGHT NOT ILLUMINATING. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998052900425 19980529 00425 NM 1998 5 29 TSAA9833222 1 19980420 A 3350 86210066 BATTERY ASSY BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT. REPLACED BATTERY PACK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998052900426 19980529 00426 NM 1998 5 29 TSAA9833223 1 19980421 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 2 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1998052900427 19980529 00427 NM 1998 5 29 TSAA9833224 1 19980421 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 5 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1998052900428 19980529 00428 NM 1998 5 29 TSAA9833217 1 19980415 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FLOOR PROXIMITY LIGHT BATTERY PACK AT NR 5 POSITION DUE TO UNIT BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998052900429 19980529 00429 NM 1998 5 29 TSAA9833215 1 19980419 A 3350 6013211 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 OUTSIDE LEFT SIDE OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900430 19980529 00430 NM 1998 5 29 TSAA9833229 1 19980422 A 3350 963100211 LIGHT BOEING 737 737297 1384480 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 1 EMERGENCY EXIT FLOOR LIGHT ASSY DUE TO BEING INOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900431 19980529 00431 NM 1998 5 29 TSAA9833228 1 19980422 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 1 EMERGENCY EXIT FLOOR LIGHT BATTERY PACK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900432 19980529 00432 NM 1998 5 29 TSAA9827199 1 19980403 A 5754 GUIDES BOEING 737 73725A 1384481 NM NR 3 LE SLAT WORN A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 FLT 272 - HNL-OGG - DURING APPROACH PHASE WITH FLAPS 5 SET, THE NR 3 SLAT TRANSIT LIGHT REMAINED ILLUMINATED AND PILOTS VISUALLY CONFIRMED THE SLAT PARTIALLY EXTENDED. DECLARED EMERGENCY AND LANDED WITHOUT NO INCIDENT. REPLACED NR 3 SLAT OUTBOARD TRACK GUIDES PER MM 27-81-0 AND ADJUSTED NR 3 SLAT OUTBOARD AND INBOARD AUXILIARY TRACK DETENTS PER MM 29-81-21 . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998052900433 19980529 00433 NM 1998 5 29 TSAA9853210 1 19980413 A 5330 SKIN BOEING 737 7372S5C 1384499 NM BS 360 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 GROUND AIR STARTER HOSE CAME LOOSE AND DENTED FUSELAGE AT BS 360 AND STRINGER 21R. CONFIRMED SKIN CRACK WITH HFEC. REP AIRED AIRCRAFT SKIN IAW BOEING SRM 53-30-3 FIGURE 28. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998052900434 19980529 00434 NM 1998 5 29 TSAA9853211 1 19980413 A 5330 SKIN BOEING 737 7372S5C 1384499 NM BS 328 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 GROUND AIR STARTER HOSE CAME LOOSE AND DENTED FUSELAGE AT BS 328 AND STRINGER 23R. CONFIRMED SKIN CRACK WITH HFEC. REP AIRED AIRCRAFT SKIN IAW BOEING SRM 53-30-3 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998052900435 19980529 00435 NM 1998 5 29 TSAA9853218 1 19980415 A 5330 SKIN BOEING 737 7372X6C 1384552 NM BS 318/322/328 DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 THREE HOLES IN LEFT SIDE OF AIRCRAFT BELOW FORWARD ENTRY DOOR CAUSED BY RUNAWAY BAGGAGE CART. LOCATIONS ARE BS 328 BETW EEN STRINGER 19L/20L, BS 322 BETWEEN STRINGER 21L/22L, AND BS 318 AT STRINGER 23L. REPAIRED DAMAGE PER ECO 2897. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998052900436 19980529 00436 NM 1998 5 29 TSAA9853212 1 19980410 A 5320 FITTING BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 FOUND CORRODED END FITTING AT BS 1016 AFT PRESSURE BULKHEAD AND STRINGER 20L. REPLACED FITTING PER ECO 2894. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900437 19980529 00437 NM 1998 5 29 TSAA9857213 1 19980409 A 5730 SKIN BOEING 737 7372T4 1384492 NM WS 495 CORROSION A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 CORROSION FOUND ON LEFT SIDE OUTBOARD WING LOWER SKIN AT WING STATION 495. REWORKED AREA PER ECO 1684R8 AND DEVIATION ' F' FOR ECO 1684R8. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900438 19980529 00438 NM 1998 5 29 TSAA9855214 1 19980415 A 5510 BUSHING BOEING 737 7372T4 1384492 NM RT HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 HORIZONTAL STABILIZER RT SIDE UPPER AFT BUSHING CORRODED. REPAIRED BUSHING PER ECO 2895. BLEND OUT DIMENSION 1.2560 IN CH BY 1.2640 INCH. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900439 19980529 00439 NM 1998 5 29 TSAA9853216 1 19980414 A 5320 FRAME BOEING 737 7372T4 1384492 NM CARGO DOORWAY CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 APPLIED PREVENTATIVE MODIFICATION TO AFT LOWER CARGO DOORWAY FORWARD AND AFT BODY FRAMES PER ECO 1474R9. DEVIATION 'F' APPLIED TO ECO 1474R9 INSTRUCTIONS DUE TO CORROSION ON FORWARD FRAME WEB. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998052900440 19980529 00440 SO 1998 5 29 ASOA98030 1 19980418 A 2450 RELAY PANEL EMB 120 EMB120RT SO COCKPIT LOOSE A ASOA O OTHER J WARNING INDICATION AP APPROACH 1 SO 11 227AS 120023 ON FINAL APPROACH DHN-ATL, EXPERIENCED EMERGENCY BUS 1 FAILURE. CREW EXECUTED A GO-AROUND AND PROCEEDED WITH CHECKLIST. WHILE CIRCLING TO LAND, RIGHT ENGINE NP FELL TO 50 PERCENT WITH ENGINE PRODUCING POWER. CREW ELECTED TO LEAVE ENGINE RUNNING, DECLARE AN EMERGENCY AND MAKE A VISUAL APPROACH AND LANDING. LANDING WAS MADE WITHOUT FURTHER INCIDENT. ATL M AINTENANCE FOUND RELAY PANEL ON LEFT SIDE OF COCKPIT TO BE UNSECURED. PANEL WAS RESECURED, EMERGENCY BUS 1 C/B RESET, A ND NP CANNON PLUG RESEATED. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998052900441 19980529 00441 SO 1998 5 29 ASOA98029 1 19980414 A 2120 AIR DISTRIBUTION EMB 120 EMB120RT SO COCKPIT ODOR A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 11 285AS 120265 DURING TAKEOFF ATL-BQK, CREW SMELLED AN ACRID SMOKE ODOR IN THE COCKPIT AND SHORTLY THEREAFTER, THE F/A REPORTED A STRON G SMELL IN THE CABIN AND THE LAV SMOKE DETECTOR GOING OFF. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL, WHERE LANDIN G WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. ATL MAINTENANCE INSPECTED THE WIRING IN THE LAV, FORWARD AND AFT CLOSET S, THE GALLEY AND THE COCKPIT (LEFT AND RIGHT SIDES AND OVERHEAD). NO DEFECTS WERE NOTED. PERFORMED GROUND RUN WITH PA CKS ON ENGIEN BLEED AND APU BLEED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998052900442 19980529 00442 1998 5 29 ASOA98028 4 19980414 A 2210 992226E118096 SWITCH EMB 120 EMB120RT SO COCKPIT SHORTED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 229AS 120042 ON DEPARTURE ATL-TLH, CREW OBSERVED ELECTRICAL SMOKE COMING FROM THE GLARESHIELD PANEL IN THE VICINITY OF THE AUTOPILOT TRANSFER BUTTON. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCID ENT. ATL MAINTENANCE REMOVED AND REPLACED THE AUTOPILOT TRANSFER SWITCH. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998052900443 19980529 00443 SO 1998 5 29 ASOA98027 1 19980414 A 5320 12018804003 FITTING EMB 120 EMB120RT SO PAX DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 269AS 120210 DURING C-CHECK INSPECTION, FOUND A CRACK IN THE MACHINED HINGE FITTING FOR AFT PASSENGER DOOR HINGE MOUNT. REMOVED AND REPLACED FITTING (SRM 53-10-02 FIG 1 SHEET 4 PAGE 5 ITEM 44) USING SRM 51-00-00 AS A GUIDE. (M) 2 L 7 2 4T RT A31SO 1998052900445 19980529 00445 SO 1998 5 29 ASOA98036 1 19980427 A 5210 12026749001 BOLT EMB 120 EMB120RT SO AIRSTAIR DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 238AS 120053 DURING C-CHECK INSPECTION, FOUND CORROSION AT THE AFT HINGE OF THE A/S/D. THE DOOR WAS REMOVED AND THE ATTACHMENT BOLT FOUND TO HAVE SEVERE PITTING. REMOVED AND REPLACED HINGE ATTACHMENT BOLT. (M) 2 L 7 2 4T RT A31SO 1998052900446 19980529 00446 SO 1998 5 29 ASOA98035 1 19980427 A 5210 73192 ACTUATOR EMB 120 EMB120RT SO AIRSTAIR DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 238AS 120053 DURING C-CHECK INSPECTION, FOUND AIRSTAIR DOOR ACTUATOR ROD SHEARED. INVESTIGATION REVEALED A CRACK ABOUT HALFWAY THROU GH THE THREADED AREA. REMOVED AND REPLACED ACTUATOR. (M) 2 L 7 2 4T RT A31SO 1998052900447 19980529 00447 EU 1998 5 29 ASOA98034 1 19980425 A 3350 NEC3012000 POWER PACK AEROSP ATR72 ATR72212 EU CABIN DEFECTIVE A ASOA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 11 630AS 336 CREW REPORTED THAT SOME EMERGENCY LIGHTS STAYED ON WHEN SYSTEM WAS SELECTED OFF. LOCAL MECHANIC INSPECTED AIRCRAFT AND FOUND SAFE FOR A FERRY FLIGHT TO ATL. ATL MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHTING POWER SUPPLY. OP ERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 H 7 2 4T RT A53EU 1998052900448 19980529 00448 SO 1998 5 29 ASOA98033 1 19980421 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR BLOWN A ASOA B EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SO 11 504AS 120278 ON CLIMB-OUT FYV-DFW, CABIN BEGAN CLIMBING IN EXCESS OF 1000 FPM AT 16,000 FT. AS CABIN CONTINUED TO CLIMB, CREW INITIA TED THE AUTOMATIC PRESSURIZATION INOP CHECKLIST. THE PROCEDURE DID NOT WORK AS THE CABIN WAS STILL CLIMBING AT 22,000 F EET. OXYGEN MASKS WERE DEPLOYED AND AIRCRAFT DESCENDED TO 10,000 FT WHERE FLIGHT WAS CONTINUED IN A NORMAL MANNER. DFW MAINTENANCE FOUND THE CARGO DOOR SEAL BLOWN. THE SEAL AND RETAINER WERE REPAIRED AND MASKS WERE RESECURED. NO OTHER D EFECTS WERE FOUND AND AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998052900449 19980529 00449 EA 1998 5 29 ASOA98032 1 19980421 A 5243 12007993612 DOOR DHAV DHC6 DHC6300 EA RT NACELLE MISSING A ASOA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 SO 11 126AS 756 ON POSTFLIGHT INSPECTION, FOUND THE RIGHT SIDE NACELLE HYDRAULIC ACCESS DOOR TO BE MISSING, AND CORRESPONDING INBOARD FL AP HAD A HOLE IN IT. PANEL APPEARED TO HAVE BLOWN OFF IN FLIGHT. TXK MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOAR D FLAP ASSEMBLY, REPAIRED THE RIGHT FLAP FOLLOWUP PANEL AND INSTALLED ON AIRCRAFT AND REPLACED THE RIGHT HYDRAULIC BAY L OWER PANEL IAW/MM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 1 H 7 2 3T A9EA 1998052900450 19980529 00450 SO 1998 5 29 ASOA98031 1 19980419 A 2150 22045402 ACM EMB 120 EMB120RT SO AFT FUSELAGE INOPERATIVE A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 11 501AS 120273 AFTER TAKEOFF ATL-ILM, THE CREW NOTICED A BURNING OIL TYPE SMELL COMING FROM THE AIR CONDITIONING SYSTEM, FOLLOWED BY TH E LAVATORY SMOKE DETECTOR GOING OFF. THE CREW SHUT OFF THE AIR CONDITIONING SYSTEM, DECLARED AN EMERGENCY AND RETURNED TO ATL WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. ATL MAINTENANCE FOUND THE LEFT ACM SEIZED UP. REMOV ED AND REPLACED THE ACM. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998052900455 19980529 00455 EU 1998 5 29 UF6A980420 1 19980426 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 SBN - AFT BAGGAGE DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900456 19980529 00456 EU 1998 5 29 UF6A980416 1 19980417 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 13315 2028 SBN - LEFT AFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900457 19980529 00457 EU 1998 5 29 UF6A980412 1 19980414 A 3350 P4010021 BATTERY BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 12373 2036 GRB - FLT 5734 - AFT FLIGHT ATTENDANT FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY. (M) 2 L 7 2 4T RT A27NM 1998052900459 19980529 00459 EU 1998 5 29 UF6A980410 1 19980415 A 3350 362634 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 13305 2028 SBN - FOUND EMERGENCY LIGHT STRIP INOP AT ROW 16 CD. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT STRIP. (M) 2 L 7 2 4T RT A27NM 1998052900460 19980529 00460 EU 1998 5 29 UF6A980406 1 19980410 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 9939 2028 GRB - FLT 5745 - OVERSEAT EMERGENCY EXIT LIGHTS AND LEFT SIDE WALL EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900461 19980529 00461 EU 1998 5 29 UF6A980403 1 19980408 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 13957 2020 SBN - EMERGENCY LIGHT LEFT AFT OVERWING INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900462 19980529 00462 1998 5 29 UF6A980407 4 19980411 A 3425 AHRS BAG ATP ATP EU NR 2 FAILED A UF6A O OTHER O OTHER CL CLIMB 1 GL 31 859AW 2036 ORD - FLT 5760 - NR 2 AHRS FAILED IN FLIGHT. OPS CHECKED SYSTEM. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900463 19980529 00463 EU 1998 5 29 UF6A980408 1 19980411 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 14025 2022 SBN - AFT BAGGAGE DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900464 19980529 00464 EU 1998 5 29 UF6A980409 1 19980411 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 14025 2022 SBN - LEFT AFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900465 19980529 00465 EU 1998 5 29 UF6A980426 1 19980427 A 5230 JD539J0199001 ANGLE BAG ATP ATP EU BAGG DOORWAY CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 12884 2029 SBN - FOUND CRACK ON FORWARD LANDING ANGLE VERTICLE FORWARD BAGGAGE DOOR SURROUND. MAINTENANCE REMOVED AND REPLACED FOR WARD LANDING ANGLE ON FORWARD BAGGAGE DOOR SURROUND. (M) 2 L 7 2 4T RT A27NM 1998052900466 19980529 00466 EU 1998 5 29 UF6A980425 1 19980428 A 5753 BOOMS BAG ATP ATP EU TE FLAPS CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 13884 2021 SBN - DURING X-RAY INSPECTION OF THE BOOMS ON THE FRONT AND REAR SPARS OF THE FLAPS ONE CRACK WAS NOTED ON THE LEFT SIDE OF THE UPPER AFT STRINGER ON THE FORWAD SPAR STATION 76.16. MAINTENANCE REPAIRED CRACK. (M) 2 L 7 2 4T RT A27NM 1998052900467 19980529 00467 EU 1998 5 29 UF6A980415 1 19980421 A 3350 GE1317 BULB BAG ATP ATP EU COCKPIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 12497 2034 SBN - OVERHEAD COCKPIT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900468 19980529 00468 EU 1998 5 29 UF6A980417 1 19980422 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 9824 2036 ORD - FLT 5750 - COCKPIT AND FORWARD VESTIBULE EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED NR 1 POWER SUPPL Y. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900470 19980529 00470 EU 1998 5 29 UF6A980414 1 19980421 A 3350 OL3071BPEGPL BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 12497 2034 SBN - AFT PASSENGER DOOR EMERGENCY EXIT LIGHT FILAMENT INOP. MAINTENANCE REMOVED AND REPLACED FILAMENT. (M) 2 L 7 2 4T RT A27NM 1998052900471 19980529 00471 EU 1998 5 29 UF6A980413 1 19980419 A 3350 58785 WIRE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 14071 2022 ORD - UPON DAILY INSPECTION, FOUND EMERGENCY FLOOR PROXIMITY STRIP INOP. MAINTENANCE REMOVED AND REPLACED STRIP. (M) 2 L 7 2 4T RT A27NM 1998052900472 19980529 00472 EU 1998 5 29 UF6A980214 1 19980226 A 3350 GE1317 BULB BAG ATP ATP EU FLIGHT DECK FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 12094 2036 SBN - FLIGHT COMPARTMENT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900473 19980529 00473 1998 5 29 UF6A980213 4 19980225 A 2565 2077001 SLIDE BAG ATP ATP EU PAX DOOR LOOSE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 12261 2034 ORD - FLT 5730 - FORWARDED PASSENGER DOOR EVACUATION SLIDE IS DISCONNECTED FROM GIRT BAR. MAINTENANCE REMOVED AND REPLA CED EVACUATION SLIDE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900474 19980529 00474 EU 1998 5 29 UF6A980331 1 19980328 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 855AW 12723 2029 SBN - AFT PASSENGER DOOR OUTER EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900475 19980529 00475 1998 5 29 UF6A980329 4 19980327 A 2565 20770001 SLIDE BAG ATP ATP EU PAX DOOR LOOSE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 8604 190 2029 SBN - FLT 5761 - FORWARD PAX DOOR EMERGENCY SLIDE PULLED LOOSE FROM DOOR. MAINTENANCE REMOVED AND REPLACED SLIDE. SYST EM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900476 19980529 00476 EU 1998 5 29 UF6A980330 1 19980328 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 855AW 12723 2029 SBN - AFT BAGGAGE DOOR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900477 19980529 00477 EU 1998 5 29 UF6A980332 1 19980329 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 13928 2022 SBN - AFT CARGO DOOR EXTERNAL EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900478 19980529 00478 EU 1998 5 29 UF6A980326 1 19980318 A 5720 JD573J0040001 TIP BAG ATP ATP EU RT WING TIP DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 13209 2028 CWA - FOUND DAMAGE TO RIGHT HAND FORWARD WING TIP HALF. MAINTENANCE REMOVED RIGHT HAND FORWARD WING TIP. INSPECTED STR UCTURE BEHIND WING TIP. NO DEFECTS NOTED. INSTALLED NEW WING TIP. ACFT T: 13,209 HOURS. (X) 2 L 7 2 4T RT A27NM 1998052900479 19980529 00479 EU 1998 5 29 UF6A980327 1 19980327 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 12353 2034 SBN - LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900480 19980529 00480 EU 1998 5 29 UF6A980328 1 19980327 A 3350 P4010021 BATTERY BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 12353 2034 SBN - AFT FLIGHT ATTENDANT FLASHLIGHT BATTERY LOW. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECKED G OOD. (M) 2 L 7 2 4T RT A27NM 1998052900481 19980529 00481 EU 1998 5 29 UF6A980401 1 19980404 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 12609 2032 SBN - RIGHT AFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900482 19980529 00482 EU 1998 5 29 UF6A980402 1 19980404 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 12609 2032 SBN - LEFT AFT OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900483 19980529 00483 EU 1998 5 29 UF6A980321 1 19980321 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 13227 2028 SBN - RIGHT AFT BAGGAGE DOOR EXTERNAL EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900484 19980529 00484 EU 1998 5 29 UF6A980322 1 19980322 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 13880 2022 SBN - AFT BAGGAGE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900485 19980529 00485 EU 1998 5 29 UF6A980323 1 19980322 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 13880 2022 SBN - RIGHT AFT OVERWING EMERGENCY LIGHT OUT. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900486 19980529 00486 EU 1998 5 29 UF6A980324 1 19980318 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 11875 2035 SBN - OUTSIDE OVERWING EMERGENCY LIGHT ON NR 2 SIDE INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900487 19980529 00487 EU 1998 5 29 UF6A980203 1 19980210 A 7712 JF760J0020004 TORQUE SHAFT BAG ATP ATP EU NR 1 ENGINE WORN A UF6A C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 852AW 9801 2021 ORD - FLT 5701 - NR 1 NH EXCEEDED TAKEOFF LIMIT (APPROX 103 PERCENT). MAINTENANCE REMOVED AND REPLACED THE NR 1 TORQUE SHAFT ASSEMBLY. RERIGGED ENGINE AND PERFORMED OPS CHECK. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900488 19980529 00488 EU 1998 5 29 UF6A980204 1 19980210 A 3350 58786 LIGHT BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 11674 2035 ORD - EMERGENCY FLOOR PROXIMITY LIGHT INOP AT ROW 3CD. MAINTENANCE REMOVED AND REPLACED PROXIMITY LIGHT. SYSTEM OPS CH ECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900489 19980529 00489 EU 1998 5 29 UF6A980325 1 19980318 A 2730 JD273J0170000 SWITCH BAG ATP ATP EU ELEVATOR OUT OF ADJUST A UF6A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 855AW 12659 2029 ORD - FLT 5731 - TAKEOFF CONFIGURATION CWP ILLUMINATED ON TAKEOFF ROLL WITH EVERYTHING IN PROPER POSITION. MAINTENANCE ADJUSTED ELEVATOR TRIM MICROSWITCH. SYSTEM OPS CHECKED GOOD. ACFT TT: 12,656 HOURS. (X) 2 L 7 2 4T RT A27NM 1998052900490 19980529 00490 1998 5 29 UF6A980303 4 19980301 A 2565 2077001 SLIDE BAG ATP ATP EU PAX DOOR DISCONNECTED A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 854AW 8374 2028 AZO - FLT 5707 - GIRT BAR DISCONNECTED FROM SLIDE ON FORWARD PAX DOOR. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAP E SLIDE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900491 19980529 00491 1998 5 29 UF6A980215 4 19980226 A 3451 066110700 DME BAG ATP ATP EU NR 2 FAILED A UF6A A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 857AW 6731 3895 2034 ORD - FLT 5732 - BOTH DME'S FAILED IN FLIGHT. MAINTENANCE REMOVED AND REPLACED NR 2 DME, NR 1 DME OPS CHECKED GOOD. SY STEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900492 19980529 00492 EU 1998 5 29 UF6A980301 1 19980301 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 13745 2022 SBN - AFT RIGHT OVERWING EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900493 19980529 00493 EU 1998 5 29 UF6A980302 1 19980301 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 13745 2022 SBN - AFT LEFT WING EXTERIOR OVERWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900494 19980529 00494 EU 1998 5 29 UF6A980304 1 19980303 A 3350 P4010021 BATTERY BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 11798 2035 ORD - FLT 5752 - AFT F/A FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900495 19980529 00495 EU 1998 5 29 UF6A980320 1 19980319 A 3350 1 BATTERY BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 12215 2036 PIA - FLT 5743 - RED LED ON AFT FLIGHT ATTENDANT FLASHLIGHT IS NOT FLASHING. MAINTENANCE REMOVED AND REPLACED BATTERY P ACK. SYSTEM OPS CHECKED GOOD. ACFT TT: 12,215 HOURS. (X) 2 L 7 2 4T RT A27NM 1998052900496 19980529 00496 1998 5 29 UF6A980103 4 19980103 A 2565 2077001 SLIDE BAG ATP ATP EU PAX DOOR FAILED TEST A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 9374 181 2034 SBN - AFT PASSENGER DOOR EVACUATION SLIDE BATTERY FAILED FUNCTIONAL TEST. MAINTENANCE REMOVED AND REPLACED EVACUATION S LIDE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900497 19980529 00497 EU 1998 5 29 UF6A980102 1 19980103 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 2034 SBN - EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED ALL POWER SUPPLIES. SYSETM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900498 19980529 00498 EU 1998 5 29 UF6A980101 1 19980102 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 12083 2032 SBN - LEFT AFT OVERWING EMERGENCY LIGHT HAS FORWARD BULB INOP. MAINTENANCE REMOVED AND REPLACED FWD BULB. SYSTEM OPS C HECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900499 19980529 00499 EU 1998 5 29 UF6A980118 1 19980114 A 2720 WARNING LIGHT BAG ATP ATP EU RUDDER CONTROL ILLUMINATED A UF6A K NONE N FALSE WARNING UK UNKNOWN 1 GL 31 854AW 2028 PIA - FLT 5760 - STANDBY CONTROL CWP ILLUMINATED WITH RUDDER ENGAGED PBSI ILLUMINATED. MAINTENANCE PERFORMED OPS CHECK OF RUDDERS SCS SYSTEM, NO DEFECTS NOTED. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900500 19980529 00500 EU 1998 5 29 UF6A980119 1 19980115 A 3350 58786 LIGHT BAG ATP ATP EU CABIN LOOSE A UF6A K NONE L NO TEST UK UNKNOWN 1 GL 31 858AW 2035 ORD - FLT 5757 - EMERGENCY FLOOR LIGHTS AT ROWS 1 TO 3 ARE LOOSE. MAINTENANCE RESECURED EMERGENCY FLOOR TRACK LIGHTING. (M) 2 L 7 2 4T RT A27NM 1998052900501 19980529 00501 EU 1998 5 29 UF6A980317 1 19980310 A 3260 1SE13 SWITCH BAG ATP ATP EU NLG DIRTY A UF6A O OTHER O OTHER TO TAKEOFF 1 GL 31 852AW 13767 2021 CWA - FLT 5718 - UPON RETRACTION OF GEAR AFTER TAKEOFF GOT AURAL WARNING, TAKEOFF CONFIGURATION CWP, AND NOSE GEAR INDIC ATING DOWN. RECYCLED GEAR TWICE AND STILL INDICATING GEAR DOWN. MAINTENANCE CLEANED AND EXERCISED MICROSWITCH. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998052900502 19980529 00502 EU 1998 5 29 UF6A980319 1 19980312 A 3350 GE1317 BULB BAG ATP ATP EU FLIGHT DECK FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 SBN - FLT DECK OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998052900503 19980529 00503 NM 1998 5 29 F3LA98038 1 19980427 A 5320 TIE BOEING 737 7372L9 1384497 NM BS 437 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK, INSPECTION REPORTED STRINGER TIE CORRODED ON STRIGNER 25R AT BS 437. MAINTENANCE FABRICATED STRIN GER TIE AND INSTALLED PER SRM 51-20-1, 51-30-2 AND 51-20-4. (M) 2 L 7 2 4F RT A16WE 1998052900504 19980529 00504 NM 1998 5 29 F3LA98040 1 19980430 A 5313 STRINGER BOEING 737 7372L9 1384497 NM BS 766 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER AROUND FASTENER HOLE IN STRINGER 23L, BS 766. MAINTENAN CE FABRICATED REPLACEMENT SHIM AND REPAIRED PER SRM 51-30-2 AND 53-10-1. (M) 2 L 7 2 4F RT A16WE 1998052900505 19980529 00505 NM 1998 5 29 F3LA98018 1 19980409 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 500 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK INSPECTION REPORTED, CRACK IN STRINGER 16L AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION L IGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0277. (M) 2 L 7 2 4F A16WE 1998052900506 19980529 00506 NM 1998 5 29 F3LA98019 1 19980409 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 500 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK INSPECTION REPORTED CRACK IN STRINGER 16R AT BS 500B PLUS 16 INCHES, AFT OF WING ILLUMINATION LIGHT . MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0275. (M) 2 L 7 2 4F A16WE 1998052900507 19980529 00507 NM 1998 5 29 F3LA98020 1 19980406 A 5330 SKIN BOEING 737 737201 1384454 NM BS 500 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON STRINGER 4L SKIN LAP AT BS 500A PLUS 10 INCHES. MAINTENANCE REMO VED A 1.2 INCH BY 2 INCH CORRODED AREA, FABIRCATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998052900508 19980529 00508 NM 1998 5 29 F3LA98037 1 19980430 A 3397 WIRE BOEING 737 737201 1384454 NM CABIN FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 20214 ELP - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT WAS 1 INOPERATIVE. MAINTENANCE REPAIRED WI RING AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998052900509 19980529 00509 NM 1998 5 29 F3LA98036 1 19980424 A 5753 SKIN BOEING 737 737317 138447P NM LT TE FLAP DISBONDED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 PAE - DURING C-CHECK INSPECTION REPORTED, LT WING OUTBOARD TRAILING EDGE FLAP SKIN DISBONDED ON UPPER INBOARD AFT CORNER . MAINTENANCE REMOVED DAMAGED AREA (6 INCH BY 9 INCH) OF UPPER SURFACE SKIN AND DAMAGED AREA (3.5 INCH BY 4.5 INCH) OF LOWER SURFACE SKIN, FABRICATED REPAIR PARTS AND REPAIRED PER SRM 51-70-10. (M) 2 L 7 2 4F RT A16WE 1998052900510 19980529 00510 NM 1998 5 29 F3LA98035 1 19980423 A 5320 WEB BOEING 737 737317 138447P NM BS 847 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 PAE - DURING C-CHECK INSPECTION REPORTED, 1 INCH CRACK IN WEB AT BS 847, RBL 29. MAINTENANCE REMOVED WEB. FABRICATED R EPLACEMENT PARTS AND REPAIRED PER SRM 51-30-1, 51-40-2 AND 51-40-08. (M) 2 L 7 2 4F RT A16WE 1998052900511 19980529 00511 NM 1998 5 29 F3LA98034 1 19980423 A 5753 SKIN BOEING 737 737317 138447P NM RT TE FLAP CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 PAE - DURING C-CHECK INSPECTION REPORTED, RT WING OUTBOARD TRAILING EDGE FLAP SKIN BULGED ON UPPER SURFACE AND DISBONDED ON LOWER SURFACE 13 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED DAMAGED AREA (2.5 INCH BY 3 INCH). FABRICATED REPLA CEMENT PARTS AND REPAIRED PER SRM 51-70-10, PAGE 13, PARAGRAPH 15. (M) 2 L 7 2 4F RT A16WE 1998052900512 19980529 00512 NM 1998 5 29 F3LA98022 1 19980409 A 5311 FRAME BOEING 737 737201 1384454 NM BS 360 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK INSPECTION REPORTED, FRAME CRACKED AT BS 360 BETWEEN STRINGER 20R AND 21R. MAINTENANCE REMOVED A 1 . INCH BY 3.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1 AND 51-40-3. (M) 2 L 7 2 4F A16WE 1998052900513 19980529 00513 NM 1998 5 29 F3LA98021 1 19980409 A 5330 SKIN BOEING 737 737201 1384454 NM BS 950 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK INSPECTION REPORTED, CRACK AT BS 950 BELOW STRINGER 14R AT EDGE OF SKIN LAP. MAINTENANCE REMOVED A 1 INCH BY 3 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998052900514 19980529 00514 NM 1998 5 29 F3LA98041 1 19980430 A 5313 STRINGER BOEING 737 7372L9 1384497 NM BS 380-540 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION REPORTED, CORROSION IN STRINGER 25L, BSL 380-540. MAINTENANCE REMOVED CORRODED AREAS, F ABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, AND 53-10-3. (M) 2 L 7 2 4F RT A16WE 1998052900515 19980529 00515 NM 1998 5 29 F3LA98042 1 19980430 A 5311 FRAME BOEING 737 7372L9 1384497 NM BS 490 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON FRAME WEB AFT OF FORWARD CARGO DOOR CUTOUT AT BS 490, STRINGER 24 R TO 25R. MAINTENANCE REMOVED CORROSION. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-03, 51-30-2, 53-10-1 AND OHM 20-50-14. (M) 2 L 7 2 4F RT A16WE 1998052900516 19980529 00516 NM 1998 5 29 F3LA98039 1 19980428 A 5312 BULKHEAD SUPPORT BOEING 737 7372L9 1384497 NM BS 947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON AFT BULKHEAD TO FLOOR SUPPORT AT BS 947 FROM RBL 22 - LBL 22. MA INTENANCE FABRICATED BULKHEAD TO FLOOR SUPPORT AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 51-30-8. (M) 2 L 7 2 4F RT A16WE 1998052900517 19980529 00517 NM 1998 5 29 MASA98085 1 19980417 A 3397 82425110001 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN SHORTED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 FLT 7594 - DEN-GJT - CREW REPORTED THAT THE FIRST TWO EMERGENCY ESCAPE PATH LIGHTS INOP. AIRCRAFT WAS FERRIED TO GJT WH ERE MAINTENANCE REMOVED AND REPLACED THE TRACK LIGHT SECTION. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998052900518 19980529 00518 NM 1998 5 29 MASA98096 1 19980423 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 DURING A ROUTINE SERVICE CHECK, MAINTENANCE NOTED SIX BURNED BULBS IN THE OVERHEAD CABIN CEILING EXIT LIGHT AT THE AIRS TAIR DOOR. THE BULBS WERE REPLACED. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998052900519 19980529 00519 NM 1998 5 29 MASA98095 1 19980424 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING A LINE CHECK INSPECTION, MAINTENANCE NOTED EIGHT BULBS WITHIN THE CABIN CENTER OVERHEAD EMERGENCY EXIT LIGHT ASSY WERE NOT ILLUMINATING. THE BULBS WERE REPLACED, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998052900520 19980529 00520 WP 1998 5 29 GTIA9800050 1 19980418 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 DTW - RIGHT FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BULBS OPERATIONAL CHECKED GOOD IAW DC-9 MM 33-50. (M) 2 L 7 2 4F A6WE 1998052900521 19980529 00521 WP 1998 5 29 GTIA9800048 1 19980414 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 DTW - EMERGENCY LIGHTING. TWO RED LIGHTS FIRST STRIP OUT. EXIT LIGHTS OVER AFT EMERGENCY EXIT OUT. REMOVED AND REPLAC ED LIGHTS BULBS, OPERATIONAL CHECK GOOD. REMOVED AND REPLACED BATTERY PACK BATTERIES, OPERATIONAL CHECK GOOD. NO DEFEC TS NOTED IAW DC-9 MM 33-53. (M) 2 L 7 2 4F A6WE 1998052900522 19980529 00522 EU 1998 5 29 SIMA981102 1 19980420 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 15385 223 SAW - DURING PS-2 INSPECTION, MAINTENANCE REPORTED THE FORWARD CEILING, LEFT FORWARD EXTERIOR AND EVERY OTHER FORWARD EM ERGENCY FLOOR LIGHT INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 3WL. PERFORMED OPE RATIONAL CHECK SATISFACTORILY. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998052900523 19980529 00523 EU 1998 5 29 SIMA981101 1 19980420 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 314AE 7131097 340B314 DFW - FLT 3754 - CARGO SMOKE LIGHT CAME ON IN FLIGHT. CREW DISCHARGED NR 1 CARGO EXIT SWITCH AND THE CARGO SMOKE LIGHT WENT OFF AFTER APROX 8 MINUTES. DFW, MAINTENANCE RAI BOTH CARGO SMOKE DETECTORS AND THE RT CARGO C02 BOTTLE. NO EVIDEN CE OF SMOKE OR FIRE REPORTED FROM MTX. A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998052900524 19980529 00524 EU 1998 5 29 SIMA981082 1 19980418 A 3350 3013017 BATTERY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AE 0571 494 ORD - FLT 9750 - EMERGENCY LIGHTS INOP. R/I'D BATTERY PACK AT 62WL. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RET URNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998052900525 19980529 00525 EU 1998 5 29 SIMA981081 1 19980418 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 37AE 5001 037 ORD - FLT 4361 - BOTH FORWARD UPPER EMERGENCY EXIT SIGNS INOP. REMOVED AND INSTALLED SERVICEABLE EMERGENCY BATTERY POWE R SUPPLY IAW JIC 33-51-21. OPERATIONAL CHECKS GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998052900526 19980529 00526 EU 1998 5 29 SIMA981071 1 19980417 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 423MQ 10909 030 ORD - FLT 4092 - EVERY OTHER LIGHT OUT IN CABIN EMERGENCY PATH INOP. RAI BATTERY PACK AT 3WL AND 10WL LOCATION. OPS CH ECK GOOD. RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998052900527 19980529 00527 NM 1998 5 29 USAA980162 1 19980423 A 5330 SKIN BOEING 767 767201 1385125 NM BS 1582 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 650US 40925 23902 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A 47 INCH BY 20 INCH CRACK ON THE EXTERNAL SKIN STATION 1582 STRINGER 32 LT. INSTALLED EXTERNAL SKIN DOUBLER 47 INCH BY 20 INCH PER REPAIR DOCUMENT EA37577. (M) 2 L 7 2 4F RT A1NM 1998052900528 19980529 00528 NM 1998 5 29 USAABB98043 1 19980420 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND EMERGENCY FLOOR LIGHTS INOPERATIVE AT ALL SEAT POSITIONS. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998052900529 19980529 00529 NM 1998 5 29 USAABB98044 1 19980424 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 PHL - FOUND EMERGENCY LIGHT BATTERIES WEAK AT SEATS 1, 4, 6, 9 13, 29 AND 33. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998052900530 19980529 00530 WP 1998 5 29 USAAD98074 1 19980425 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918VJ 48138 IND - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 4 AND 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATT ERIES. (M) 2 L 7 2 4F A6WE 1998052900531 19980529 00531 WP 1998 5 29 USAAD98075 1 19980427 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 956VJ 47588 PIT - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT BATTERY . (M) 2 L 7 2 4F A6WE 1998052900532 19980529 00532 WP 1998 5 29 USAAD98076 1 19980426 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 932VJ 47189 IND - THE CARRY AROUND EMERGENCY LIGHT AT THE ENTRANCE DOOR WAS DIM. MAINTENANCE REPLACE THE CARRY AROUND EMERGENCY LIG HT BATTERY. (M) 2 L 7 2 4F A6WE 1998052900533 19980529 00533 WP 1998 5 29 USAAD98071 1 19980423 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 942VJ 47057 IND - THE OVERHEAD EMERGENCY LIGHTS IN THE FIRST CLASS SECTION WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIG HT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998052900534 19980529 00534 WP 1998 5 29 VJ9800156 1 19980523 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 914VV 47486 EMERGENCY LIGHTS OUT, AFT OVERWING EXITS. REMOVED AND REINSTALLED SAME BATTERIES AND THE SYSTEM OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998052900535 19980529 00535 NM 1998 5 29 K3HA980077 1 19980521 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHTING FORWARD HAS ABOUT 2 FOOT SECTION OF TRACK COMING OUT WON'T LOCK IN POSITION, ALSO HAS TAPE AROUN D IT. REMOVED TAPE REPAIRED WIRING AND REMOVED DEBRIS FROM TRACK OPS CHECK OK PER MM 33-59-00 AND 33-50-01. 2 L 7 3 4F A3WE 1998052900536 19980529 00536 NM 1998 5 29 K3HA980078 1 19980521 A 3510 11442025 OXYGEN MASK BOEING 727 727225 1384077 NM COCKPIT MISINSTALLED A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 8881Z 21578 FLIGHT ENGINEER'S OXYGEN MASK INCORRECT FOR COMPATABILITY WITH SMOKE GOGGLES. REMOVED AND REPLACED FLIGHT ENGINEER'S OX YGEN MASK PER MM 35-11-0, TO MAKE COMPATIBLE WITH GOGGLES. 2 L 7 3 4F A3WE 1998052900537 19980529 00537 NM 1998 5 29 K3HA980079 1 19980522 A 2620 WIRE BOEING 727 727225 1384077 NM APU FIRE BOTTLE BROKEN A K3HA F ACTIVATE FIRE EXT. A FLAME/FIRE IN INSP/MAINT 1 EA 25 8881Z 21578 APU HAD STACK TORCHING. TRIED TO DISCHARGE FIRE BOTTLE FROM WHEEL WELL. BOTTLE DID NOT DISCHARGE. TROUBLESHOT AND FOU ND BROKEN WIRE AT CANNON PLUG TO FIRE BOTTLE REPAIRED WIRE CHECKED SYSTEM IAW 49-41-01. 2 L 7 3 4F A3WE 1998052900538 19980529 00538 NM 1998 5 29 K3HA980080 1 19980524 A 3350 328 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 THREE BULBS AT THE R2 EMERGENCY EXIT POSITION DID NOT ILLUMINATE DURING OPERATION. REBULBED EMERGENCY EXIT LIGHTS OPS C HECK OK REF MM 33-50-101. 2 L 7 3 4F A3WE 1998052900539 19980529 00539 SO 1998 5 29 RAAA98E8014 1 19980526 A 5313 STRINGER LKHEED 188 188C 5262604 SO BS 328 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 1 CHECK, FOUND STR 42 AND SKIN DENTED AT FS 328. REPAIRED STR PER SRM 53-2-2. REMOVED MINOR SKIN D ENT M-54 NR 37. 2 L 7 4 4T 4A22 1998052900540 19980529 00540 SO 1998 5 29 RAAA98E9017 1 19980520 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY DUE FAILED. 2 L 7 4 4T 4A22 1998052900541 19980529 00541 SO 1998 5 29 RAAA98E9018 1 19980524 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT RT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998052900542 19980529 00542 WP 1998 5 29 CALA9800898 1 19980525 A 2761 AYG70915505 ACTUATOR VALVE DOUG DC10 DC1030 3023501 WP RT SPOILER LEAKING A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 13088 84930 46850 THE AIRCRAFT LOST HYDRAULIC QUANTITY ON SYSTEM NR 1 WHILE EN ROUTE. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF LOW PRE SSURE LIGHTS. THE AIRCRAFT WAS APPROXIMATELY 20 MINUTES FROM MAN WHEN THE FLUID LOSS OCCURRED. FUEL WAS DUMPED AND THE AIRCRAFT WAS DIVERTED TO MAN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT SPOILER DRIVE SERVO ACTUATOR/V ALVE LEAKING. THE SPOILER DRIVE SERVO ACTUATOR/VALVE WAS REMOVED AND REPLACED IAW MM 27-61-05, PAGE 201. THE NR 1 HYDR AULIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998052900543 19980529 00543 WP 1998 5 29 CALA9800899 1 19980525 A 3260 92743643 RELAY DOUG DC9 DC932 3022066 WP LG LEVER INOPERATIVE A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 12532 45791 WHEN GEAR WAS EXTENDED ON APPROACH, ONLY UPPER HALF OF GREEN DOWN AND LOCKED LIGHTS ILLUMINATED. THE GEAR WAS RECYCLED AND CIRCUIT BREAKERS WERE CHECKED. A GO-AROUND WAS PERFORMED AND THE GEAR WAS CONFIRMED DOWN AND LOCKED THROUGH VIEW PO RT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LEVER R2-28 RELAY AT FAULT. THE R2-28 RE LAY WAS REPLACED AND SYSTEM CHECK ON GROUND WAS GOOD. 2 L 7 2 4F A6WE 1998052900544 19980529 00544 1998 5 29 CALA9800900 4 19980524 A 2230 2593342976 COMPUTER DOUG DC10 DC1030 3023501 WP NR 1 INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 13067 18679 47866 THE CAPTAIN'S STICK SHAKER ACTIVATED, THE SLAT DISAGREE LIGHT ILLUMINATED, AND SLAT RESET ILLUMINATED DURING TAKEOFF FRO M IAH. CONFIRMED SLAT RETRACTION PER CHECKLIST AND THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. M AINTENANCE FOUND THE NR 1 STALL WARNING SYSTEM NOT TESTING FROM COCKPIT. THE NR 1 AUTOTHROTTLE COMPUTER WAS REMOVED AND REPLACED. IN ADDITION, THE NR 1 STALL WARNING ANGLE OF ATTACK TRANSDUCER WAS REMOVED AND REPLACED AS A PRECAUTIONARY M EASURE. THE FLAP/SLAT SYSTEM WAS OPERATED AND GROUND CHECKS WERE NORMAL. AN AUTOSLAT TEST WAS ALSO PERFORMED WITH NO F AULTS NOTED. 2 L 7 3 4F A22WE 1998052900545 19980529 00545 NE 1998 5 29 COMA9810125 2 19980520 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT DAMAGED A COMA K NONE M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 259CA 7325 120252 115474 RT ENGINE HOT START, TEMP REACHED 978 DEGREES. REMOVED ENGINE FOR INSPECTION. 2 L 7 2 4T 4 T RT A31SO E20NE 1998052900546 19980529 00546 SO 1998 5 29 COMA9810126 1 19980521 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 15775 1000 120152 FORWARD CABIN EMERGENCY LIGHTING IS INOP. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998052900547 19980529 00547 SO 1998 5 29 COMA9810127 1 19980521 A 6120 4122009006 PUMP EMB 120 EMB120RT SO LT ENGINE INOPERATIVE A COMA K NONE O OTHER TX TAXI/GRND HDL 1 SO 01 256CA 14784 120245 LEFT ENGINE ELECTRIC FEATHER PUMP IS INOP. REPLACED AUXILIARY FEATHER PUMP. 2 L 7 2 4T RT A31SO 1998052900548 19980529 00548 1998 5 29 COMA9860110 4 19980525 A 3442 6229302003 RADAR CNDAIR CL600 CL6002B19 EA FWD FUSELAGE FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 964CA 8956 501 7129 WEATHER RADAR FAILED. REPLACED THE RADAR ANTENNA. 2 L 7 2 4F RT A21EA 1998052900549 19980529 00549 EA 1998 5 29 COMA9860111 1 19980524 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 954CA 7100 CABIN DOOR OUTER HANDLE WARNING AFTER TAKEOFF. ADJUSTED CABIN DOOR LATCHING AND OPERATING MECHANISMS. 2 L 7 2 4F RT A21EA 1998052900550 19980529 00550 EA 1998 5 29 COMA9860112 1 19980513 A 7931 601509197 TRANSDUCER CNDAIR CL600 CL6002B19 EA LT ENGINE MALFUNCTION A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 917CA 1641 7017 LEFT ENGINE OIL PRESSURE BELOW NORMAL LIMITS IFSD. REPLACED PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 1998052900551 19980529 00551 EA 1998 5 29 COMA9860113 1 19980524 A 2613 356024310 OVERHEAT LOOP CNDAIR CL600 CL6002B19 EA RIGHT MALFUNCTIONED A COMA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 915CA 7013 RT 14TH STAGE BLEED AIR DUCT LEAK WARNING IFSD. REPLACED THE PYLON BLEED AIR LEAK DETECTION LOOP. 2 L 7 2 4F RT A21EA 1998052900552 19980529 00552 EA 1998 5 29 COMA9860114 1 19980521 A 3350 100865 BATTERY CNDAIR CL600 CL6002B19 EA CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 938CA 7046 EMERGENCY LIGHTING INOP. REPLACED EMERGENCY BATTERIES. 2 L 7 2 4F RT A21EA 1998052900553 19980529 00553 EA 1998 5 29 COMA9860115 1 19980522 A 5240 DOOR CNDAIR CL600 CL6002B19 EA SERVICE DOOR NOT LATCHED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 948CA 7079 LOUD WHINING NOISE AFTER TAKEOFF. FOUND 02 SERVICE DOOR OPEN. SECURED DOOR. 2 L 7 2 4F RT A21EA 1998052900554 19980529 00554 EU 1998 5 29 QXEA9800670 1 19980523 A 3350 1315 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 RIGHT REAR EXTERIOR WING EMERGENCY LIGHT OUT. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052900555 19980529 00555 EU 1998 5 29 QXEA9800671 1 19980522 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 EMERGENCY EXIT LIGHT IN CENTER AISLE HAS SEVERAL BURNT OUT BULBS. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052900556 19980529 00556 EU 1998 5 29 QXEA9800672 1 19980526 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 LIGHT IN FORWARD RIGHT EMERGENCY EXIT IS OUT. MAINTENANCE RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A20EU 1998052900557 19980529 00557 EU 1998 5 29 QXEA9800673 1 19980523 A 3350 COVER FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 EMERGENCY EXIT LIGHT COVER AT ROW 9 NEEDS TO BE SAFETY WIRED. MAINTENANCE APPLIED BRAKE AWAY WIRE TO COVER OVER EXIT HA NDLE AT ROW 9. 2 L 7 2 4F RT A20EU 1998052900558 19980529 00558 EU 1998 5 29 QXEA9800674 1 19980525 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 EXIT SIGN LIGHTS DIM ABOVE GALLEY/CABIN CEILING. MAINTENANCE REMOVED AND REPLACED INOPERATIVE 28V BULBS, OPERATIONAL CH ECK NORMAL. 2 L 7 2 4F RT A20EU 1998052900559 19980529 00559 EU 1998 5 29 QXEA9800675 1 19980525 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 TWO OVERHEAD EMERGENCY EXIT LIGHTS INOPERATIVE AT ROWS 1 AND 3. MAINTENANCE RELAMPED BOTH 28V LAMPS, OPERATIONAL CHECK IS NORMAL. 2 L 7 2 4F RT A20EU 1998052900560 19980529 00560 WP 1998 5 29 MWEA98620 1 19980522 A 2560 3952273501 LATCH DOUG DC9 DC932 3022066 WP GIRT BAR LACK OF LUBE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 THE GIRT BAR LATCH FOR MAIN CABIN DOOR SLIDE NEEDS TO BE LUBRICATED. MTC LUBRICATED GIRT BAR LATCHES. 2 L 7 2 4F A6WE 1998052900561 19980529 00561 WP 1998 5 29 MWEA98621 1 19980523 A 3350 100865 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 THE AFT COMPARTMENT AND CABIN FLOOR EMERGENCY LIGHT FOUND INOP. MTC REMOVED AND REPLACED BATTERY PACK IN RIGHT LAVATORY . 2 L 7 2 4F A6WE 1998052900562 19980529 00562 1998 5 29 MWEA98622 4 19980525 A 3425 5223877001 ADI DOUG DC9 DC932 3022066 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 207ME 47794 ON CLIMBOUT, FIRST OFFICER ADI DID NOT INDICATE MORE THAN 3 DEGREE NOSE UP WHEN IN 15 DEGREE CLIMB. MTC REMOVED AND REP LACED FIRST OFFICERS ADI. 2 L 7 2 4F A6WE 1998052900563 19980529 00563 WP 1998 5 29 MWEA98623 1 19980525 A 5210 995576311 INTERCOSTAL DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND CRACK ON PASSENGER DOOR INTERCOSTAL AFT OF INTERIOR HANDLE MECHANISM. MTC REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 1998052900564 19980529 00564 WP 1998 5 29 MWEA98624 1 19980525 A 5712 SS095700316 RIB DOUG DC9 DC932 3022066 WP RT WING CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND CORROSION ON RIGHT WING LEADING EDGE RIB AT NUMBER 3 SLAT DRIVE TRACK. MTC FABRICATED AND INSTALLED NEW FITTING. 2 L 7 2 4F A6WE 1998052900565 19980529 00565 WP 1998 5 29 MWEA98625 1 19980525 A 5210 9915565133 PAN DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND CRACK ON AFT ENTRANCE DOOR PAN AT UPPER RIGHT STOP FITTING. MTC FABRICATED AND INSTALLED NEW UPPER DOOR PAN. 2 L 7 2 4F A6WE 1998052900566 19980529 00566 NM 1998 5 29 DL72S981094 1 19980521 A 5320 WEB BOEING 727 727232 1384082 NM BS 1285 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 524DA 21584 FOUND AT A-1 LETTER CHECK, VERT TORQUE BOX WEB CRACKED .625 AT UPPER LIGHTENING HOLE STA 1285 RT. REPAIRED PER M/M 53-1 1-0. 2 L 7 3 4F A3WE 1998052900567 19980529 00567 WP 1998 5 29 DLL14981095 1 19980521 A 3350 POWER SUPPLY 5165741 LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1739D 60773 193C1237 R3 EMERGENCY EXIT SIGN LIGHT INOP. REPLACED PWR SUPPLY. 2 L 7 3 4F A23WE 1998052900568 19980529 00568 NM 1998 5 29 DL76S981096 1 19980522 A 5330 143T32522 SKIN BOEING 767 767332 1382001 NM BS 687 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 132DN 24981 FUSELAGE SKIN AT STA 687 WAS FOUND WITH CORROSION DAMAGE AT THE LT AIRFONE ANTENNA ATTACH POINT BETWEEN STR 35L AND 36L. REPAIRED PER ERA 331718-14. 2 L 7 2 4F RT A1NM 1998052900569 19980529 00569 NM 1998 5 29 DL767981097 1 19980519 A 5754 114T410117A WEDGE BOEING 767 767232 1385132 NM NR 5 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 NR 5 LEADING EDGE SLAT T/E WEDGE WAS FOUND WITH DELAMINATION ON THE UPPER SURFACE MEASURING 3 X 5. REPAIR PER ERA 36483 1-14AD. 2 L 7 2 4F RT A1NM 1998052900570 19980529 00570 NM 1998 5 29 DL76S981099 1 19980521 A 5330 146T32621 SKIN BOEING 767 767332 1382001 NM BS 1197-1296 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 132DN 24981 FUSELAGE SKIN AT STA 1197 + 99 FOUND WITH CORROSION DAMAGE AT VHF ANTENNA ATTACH POINT BETWEEN STR 39L AND 39R. REPAIRE D PER ERA 331730-14. 2 L 7 2 4F RT A1NM 1998052900571 19980529 00571 WP 1998 5 29 DLL13981100 1 19980519 A 5743 1527275 FITTING LKHEED 1011 10113851 5265010 WP WS 346 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 786DL 193A1123 RT MLG ATTACH RIB FITTING FOUND WITH CORROSION ON FACES AND IN BORES OF MLG ATTACH LUGS. REPAIRED PER ERA 331716-14. 2 L 7 3 4F A23WE 1998052900572 19980529 00572 NM 1998 5 29 DL72S981102 1 19980522 A 2133 7110035 OUTFLOW VALVE BOEING 727 727225 1384077 NM CABIN STUCK A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 8882Z 21579 AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. ALL MODES TRIED, PULLED AND RESET C/B, NO HELP. REPLACED OUTFLOW VALVE A ND PRESSURE CONTROLLER AND CONTROL PANEL. 2 L 7 3 4F A3WE 1998052900573 19980529 00573 NM 1998 5 29 DL72E981103 1 19980522 A 3350 BATTERY PACK 900542 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 7823 21481 LT WING CTR EMER EXIT LIGHT INOP. REPLACED RACK AND BATTERY M956. 2 L 7 3 4F A3WE 1998052900574 19980529 00574 1998 5 29 DLL10981104 2 19980523 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP NR 3 FAILED A DALA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 27 1732D 40755 193C1213 10113 NR 3 ENG AT CRUISE 37,000 FT, HIGH VIBS INDICATED 2.6-2.8 UNITS. VERIFIED WITH BOTH A AND B PICKUPS. ALSO, FELT SLIGHT AIRFRAME VIB, SWITCHED TO LOW MED HIGH SETTINGS. MED HIGH WERE NORM BUT LOW FREQ PICK UP IND HIGH VIB READINGS. ENG S HUT DOWN ACCOMPLISHED. REPLACED ENGINE. 2 L 7 3 4F A23WE 1998052900575 19980529 00575 NM 1998 5 29 DL757981105 1 19980523 A 2133 OUTFLOW VALVE 60683221 BOEING 757 757232 1384965 NM CABIN FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 645DL 1021694 24216 BOTH 1 AND 2 AUTO PRESS SYSTEMS INOP. REPLACED OUTFLOW VLV. 2 L 7 2 4F RT A2NM 1998052900576 19980529 00576 WP 1998 5 29 DLL17981111 1 19980524 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 766DA 62850 193H1207 10113 EMERGENCY LIGHTS INOP AT L2. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998052900577 19980529 00577 NM 1998 5 29 DL72S981112 1 19980522 A 5744 FITTING BOEING 727 727232 1384082 NM NR 4 TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 NR 4 FLAP TRACK FWD ATTACH FITTING LARGE HOLE HAS CORROSION IN HOLE. REPAIRED PER M/M 57-42-0. 2 L 7 3 4F A3WE 1998052900578 19980529 00578 WP 1998 5 29 DLL10981118 1 19980526 A 5240 1313T10013 COUNTERBALANCE LKHEED 1011 10113851 5265010 WP L-4 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 DURING LETTER CHECK, FOUND L-4 DOOR COUNTERBALANCE CASE SEVERELY CRACKED. 2 L 7 3 4F A23WE 1998052900579 19980529 00579 NM 1998 5 29 DLM88981120 1 19980526 A 7430 SWITCH 792055 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 918DL 49583 JUST AFTER IGN OVER-RIDE WAS SELECTED ARCING OCCURRED IN AREA OF IGN SWITCH. COCKPIT HAD SMOKE. DIVERTED TO LIT. CONT RACT MTC REPORTS IGN C/BERS ARE TRIPPED AND IGN SW TERMINALS ARE BURNT ALONG WITH 2 FUEL HETA SWITCHES AND THE DC STREAT PUMP SW ALL DAMAGED WHEN WIRING TOUCHED SWITCHES. REPLACED AFFECTED SWITCHES AND REPAIRED WIRING AS NECESSARY. 2 L 7 2 4F 4 F RT A6WE E9NE 1998052900580 19980529 00580 NM 1998 5 29 DL72W981121 1 19980526 A 5522 SKIN BOEING 727 727247 138408F NM LT/RT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 T/E OF LT AND RT ELEV DELAMINATED FROM I/B EDGE TO 15 INCHES O/B OF ELEV TAB. REPAIRED PER MM 55-20-0 P 801. 2 L 7 3 4F A3WE 1998052900581 19980529 00581 NM 1998 5 29 DL72W981122 1 19980526 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 A .5 INCH CRACK ON A/C SKIN FROM RT SIDE OF AIRSTAIR CUTOUT FWD SIDE. REPAIRED PER MM 53-30-0 P 803. 2 L 7 3 4F A3WE 1998052900582 19980529 00582 NM 1998 5 29 DL72W981123 1 19980526 A 5320 WEB BOEING 727 727247 138408F NM BS 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 A .5 INCH CRACK LIGHTENING HOLE STA 1248 ON AIRSTAIR CUTOUT VERTICAL WEB LT SIDE. A .25 INCH CRACK LIGHTENING HOLE STA 1228 ON AIRSTAIR CUTOUT VERTICAL WEB RT SIDE. REPAIRED PER MM 53-11-0 P 828. 2 L 7 3 4F A3WE 1998052900583 19980529 00583 NM 1998 5 29 DL72S981126 1 19980521 A 5730 SKIN BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 SKIN CRACKED INNER L/E SKIN IS CRACKED AT FASTENERS 36 O/B OF FUSELAGE. AREA REPAIRED PER M/M 57-54-0 PG 804A. 2 L 7 3 4F A3WE 1998052900584 19980529 00584 WP 1998 5 29 RRXA98147 1 19980225 A 5730 5769589505 SKIN DOUG DC8 DC863F 302198F WP WS 326 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LEFT WING, LEADING EDGE, LOWER SKIN CRACKED AT XFS=326. FABRICATED AND INSTALLED REPA IR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04378. 2 L 7 4 4F 4A25 1998052900585 19980529 00585 WP 1998 5 29 RRXA98148 1 19980316 A 5730 576985986 SKIN DOUG DC8 DC863F 302198F WP WS 820 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LEFT WING, LEADING EDGE WITH CORROSION DAMAGE AT XFS=820. REMOVED DAMAGED SECTION, TR EATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH REO-043 93. 2 L 7 4 4F 4A25 1998052900586 19980529 00586 WP 1998 5 29 RRXA98149 1 19980330 A 5730 57517841 SKIN DOUG DC8 DC863F 302198F WP WS 207 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LEFT WING, LEADING EDGE, SLANT CRACKED AT XFS=207.5. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04400. 2 L 7 4 4F 4A25 1998052900587 19980529 00587 WP 1998 5 29 RRXA98150 1 19980306 A 5330 5779934 SKIN DOUG DC8 DC863F 302198F WP BS 450 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FUSELAGE, INTERNAL SKIN WITH CORROSION DAMAGE AT STA 450 BETWEEN LONGERONS 34 LEFT AND 35 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA A PPROVED DER TIMCO ENGINEERING SKETCH REO-04405. 2 L 7 4 4F 4A25 1998052900588 19980529 00588 WP 1998 5 29 RRXA98151 1 19980306 A 5753 5642970 SKIN DOUG DC8 DC863F 302198F WP RT TE FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, FLAP SKIN GOUGED AT XRS=230.5. FABRICATED AND INSTALLED REPAIR DOUBLER IA W FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04407. 2 L 7 4 4F 4A25 1998052900589 19980529 00589 WP 1998 5 29 RRXA98152 1 19980402 A 5311 97585201 FRAME DOUG DC8 DC863F 302198F WP BS 272 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO FRAME FLANGE RADIUS, AT STA 272 BETWEEN LONGERONS 32 RIGHT AND 33 RIGHT . FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER ENGINEERING SKETCH REO-04411. 2 L 7 4 4F 4A25 1998052900590 19980529 00590 WP 1998 5 29 RRXA98153 1 19980414 A 7110 575716503 COWL DOUG DC8 DC863F 302198F WP NR 1 ENGINE WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND NR 1 ENGINE FAN COWLING, ZEE CLOSE-OUT WORN. FABRICATED AND INSTALLED NEW ZEE CLOSE-O UT, (P/N 575716-503), IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04413. 2 L 7 4 4F 4A25 1998052900591 19980529 00591 WP 1998 5 29 RRXA98154 1 19980402 A 5321 57582665 PLANK DOUG DC8 DC863F 302198F WP BS 1580-1689 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FLOOR PLANK EDGE CORRODED BEYOND LIMITATIONS IAW DC-8 SRM, AT STA 1580 TO 1689. REMOV ED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMC O ENGINEERING SKETCH REO-04415. 2 L 7 4 4F 4A25 1998052900592 19980529 00592 WP 1998 5 29 RRXA98155 1 19980306 A 5311 5779772 FRAME DOUG DC8 DC863F 302198F WP BS 1020 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE AT STA 1020 BETWEEN LONGERONS 34 LEFT TO 34 RIGHT. REMOVE D DAMAGE SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO E NGINEERING SKETCH REO-04416. 2 L 7 4 4F 4A25 1998052900593 19980529 00593 WP 1998 5 29 RRXA98156 1 19980306 A 5311 5779772 FRAME DOUG DC8 DC863F 302198F WP BS 1060 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE AT 1060 BETWEEN LONGERONS 34 RIGHT AND 36. REMOVED DAMAGE D SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEER ING SKETCH REO-04417. 2 L 7 4 4F 4A25 1998052900594 19980529 00594 WP 1998 5 29 RRXA98157 1 19980305 A 5753 5653070162 FAIRING DOUG DC8 DC863F 302198F WP RT TE FLAP CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, FLAP TRAILING EDGE FAIRING CHAFED AT OUTBOARD SECTION. FABRICATED AND INS TALLED SPLICE REPAIR IAW FAA APPROVED DER ENGINEERING SKETCH REO-04420. 2 L 7 4 4F 4A25 1998052900595 19980529 00595 WP 1998 5 29 RRXA98158 1 19980305 A 7810 575051518 CHANNEL DOUG DC8 DC863F 302198F WP EXHAUST NOZZLE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND EXHAUST NOZZEL AT 12 O'CLOCK POSITION HAD PREVIOUS REPAIR, AND INTERNAL CHANNEL CRACKE D. 2 L 7 4 4F 4A25 1998052900596 19980529 00596 WP 1998 5 29 RRXA98159 1 19980402 A 5311 5754671502 FRAME DOUG DC8 DC863F 302198F WP BS 1140 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO FRAME FLANGE AT STA 1140 AND LONGERON 36. FABRICATED AND INSTALLED REP AIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04425. 2 L 7 4 4F 4A25 1998052900597 19980529 00597 WP 1998 5 29 RRXA98160 1 19980306 A 5330 5756067 SKIN DOUG DC8 DC863F 302198F WP BS 400/418 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, REMOVED DRAIN MAST, NO LONGER REQUIRED AT STA 400 AND STA 418 BETWEEN LONGERONS 35 RIGHT AND 36. FABRICATE AND INSTALLED BLANK-OFF PLATES TO COVER REMAINING HOLES IAW FAA APPROVED DER ENGINEERING SKETCH REO-0442 8. 2 L 7 4 4F 4A25 1998052900598 19980529 00598 WP 1998 5 29 RRXA98161 1 19980309 A 2510 5641031519AB SEAT DOUG DC8 DC863F 302198F WP COCKPIT CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FIRST OBSERVER SEAT BACK CLOSE-OUT WEB CRACKED. CRACK ORIGINATED AT LIGHTNING HOLE AN D ENDED AT EDGE. SRM DOES NOT GIVE A SPECIFIC REPAIR. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIM CO ENGINEERING SKETCH REO-04433. 2 L 7 4 4F 4A25 1998052900599 19980529 00599 WP 1998 5 29 RRXA98162 1 19980309 A 5320 37549301 FITTING DOUG DC8 DC863F 302198F WP BS 1170 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND BATHTUB, DOOR JAMB FITTING DAMAGED AT STA 1170. FABRICATED NEW FITTING IAW DAC DWG 37 54930. ORIGINAL MATERIAL NOT AVAILABLE FOR PURCHASE, REO-04434 PROVIDED SUBSTITUTION 7075-T651 FOR 7075-T6. 2 L 7 4 4F 4A25 1998052900600 19980529 00600 WP 1998 5 29 RRXA98163 1 19980309 A 5751 576313317 SKIN DOUG DC8 DC863F 302198F WP LT AILERON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LEFT WING AILERON CRACKED AT XA=621.625. FABRICATED AND INSTALLED SPLICE REPAIR IAW F AA APPROVED DER TIMCO ENGINEERING SKETCH REO-04435. 2 L 7 4 4F 4A25 1998052900601 19980529 00601 WP 1998 5 29 RRXA98164 1 19980312 A 5730 5643243503 ACCESS PANEL DOUG DC8 DC863F 302198F WP LT WING MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO LEFT WING ACCESS PNL: 506B. FABRICATED AND INSTALLED REPAIR DOUBLER IA W FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04436. 2 L 7 4 4F 4A25 1998052900602 19980529 00602 WP 1998 5 29 RRXA98165 1 19980316 A 5313 9758506 LONGERON DOUG DC8 DC863F 302198F WP BS 1160 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LONGERON 34 RIGHT WITH CORROSION DAMAGE AT STA 1160. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-044 37. 2 L 7 4 4F 4A25 1998052900603 19980529 00603 WP 1998 5 29 RRXA98166 1 19980414 A 7110 5757519502 COWLING DOUG DC8 DC863F 302198F WP NR 4 ENGINE CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 4 ENGINE, RIGHT SIDE AFT FAN COWLING, ZEE CLOSE-OUT. REMOVED D AMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO EN GINEERING SKETCH REO-04439. 2 L 7 4 4F 4A25 1998052900604 19980529 00604 WP 1998 5 29 RRXA98167 1 19980316 A 5753 5642970 SKIN DOUG DC8 DC863F 302198F WP LT TE FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND RIGHT WING OUTBOARD FLAP, LOWER SKIN GOUGED AT XRS=240. FABRICATED AND INSTALLED REPA IR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04441. 2 L 7 4 4F 4A25 1998052900605 19980529 00605 WP 1998 5 29 RRXA98168 1 19980316 A 5753 565239631 PANEL DOUG DC8 DC863F 302198F WP LT TE FLAP DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, NEWLY FABRICATED LEFT SIDE INBOARD FLAP FILLET PANEL NEEDS REPLACEMENT OF BEADED SECTION WIT H FLAT SHEET. BEADED SECTION OF LEFT SIDE INBOARD FLAP FILLET PANEL, WAS PLACED WITH FLAT SHEET IAW FAA APPROVED DER TI MCO ENGINEERING SKETCH REO-04449. 2 L 7 4 4F 4A25 1998052900606 19980529 00606 WP 1998 5 29 RRXA98169 1 19980312 A 5720 56143725 FITTING DOUG DC8 DC863F 302198F WP WS 98 CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LEFT WING CANOE FITTING CHAFED AT STA 97.9. FABRICATED AND INSTALLED REPAIR IAW FAA A PPROVED DER TIMCO ENGINEERING SKETCH REO-04453. 2 L 7 4 4F 4A25 1998052900607 19980529 00607 WP 1998 5 29 RRXA98170 1 19980316 A 5711 5597831 SPAR CAP DOUG DC8 DC863F 302198F WP WS 304 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO LEFT WING, FRONT SPAR CAP AT XFS=304. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04456. 2 L 7 4 4F 4A25 1998052900608 19980529 00608 WP 1998 5 29 RRXA98171 1 19980313 A 5730 5769857 SKIN DOUG DC8 DC863F 302198F WP LT WING MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND TOOL DAMAGE TO LEFT WING, LEADING EDGE LOWER SKIN AT XFS=285 AND XFS=526. FABRICATED AND INSTALLED REPAIR DOUBLER TO XFS=285 AND 526, IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04457. 2 L 7 4 4F 4A25 1998052900609 19980529 00609 WP 1998 5 29 RRXA98172 1 19980402 A 5350 57103692 FILLET DOUG DC8 DC863F 302198F WP RT WING CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FILLET PANEL CORRODED RIGHT WING. FILLET PANEL DAMAGED BEYOND SRM REPAIR, FABRICATED AND INSTALLED NEW FILLET PANEL IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04463. 2 L 7 4 4F 4A25 1998052900610 19980529 00610 WP 1998 5 29 RRXA98173 1 19980330 A 5711 5597838502 SPAR CAP DOUG DC8 DC863F 302198F WP WS 519 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT FOUND RIGHT WING, FORWARD SPAR CAP LOWER CRACKED AT XFS=519. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04464. 2 L 7 4 4F 4A25 1998052900611 19980529 00611 WP 1998 5 29 RRXA98174 1 19980317 A 5315 561620233 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 857 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH TOOL DAMAGE AT STA 857.188 BL 25 RIGHT. FABRICATED AND INSTALLED REPAI R DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04472. 2 L 7 4 4F 4A25 1998052900612 19980529 00612 WP 1998 5 29 RRXA98175 1 19980318 A 5712 9753297 RIB DOUG DC8 DC863F 302198F WP WS 57.75 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LEFT WING LEADING EDGE, RIB UPPER CAP CRACKED AT XFS=57.750. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04474. 2 L 7 4 4F 4A25 1998052900613 19980529 00613 WP 1998 5 29 RRXA98176 1 19980316 A 5320 3755841 FITTING DOUG DC8 DC863F 302198F WP BS 123 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LOWER CARGO DOOR JAMB, ZEE FITTING CORRODED BEYOND LIMITATIONS IAW DC-8 SRM AT STA 123 AND LONGERON 33 LEFT. FABRICATED AND INSTALLED NEW FITTING IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04484. 2 L 7 4 4F 4A25 1998052900614 19980529 00614 WP 1998 5 29 RRXA98177 1 19980414 A 7110 5757516504 COWLING DOUG DC8 DC863F 302198F WP NR 1 ENGINE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO NR 1 ENGINE RIGHT SIDE FAN COWLING, ZEE CLOSE-OUT. REMOVED DAMAGE D SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEE RING SKETCH REO-04480. 2 L 7 4 4F 4A25 1998052900615 19980529 00615 WP 1998 5 29 RRXA98178 1 19980320 A 5330 5644981 SKIN DOUG DC8 DC863F 302198F WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND FUSLAGE SKIN CORRODED AT STA 70 BETWEEN LONGERONS 28 RIGHT AND 34 RIGHT. REMOVED DAMA GED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGIN EERING SKETCH REO-04486. 2 L 7 4 4F 4A25 1998052900616 19980529 00616 WP 1998 5 29 RRXA98179 1 19980413 A 5330 5758874 SKIN DOUG DC8 DC863F 302198F WP BS 110 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND DENT TO FUSELAGE SKIN AT STA 114 AND LONGERON 23 LEFT. FABRICATED AND INSTALLED REPAI R DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04496. 2 L 7 4 4F 4A25 1998052900617 19980529 00617 WP 1998 5 29 RRXA98180 1 19980323 A 2121 5614739 BRACKET DOUG DC8 DC863F 302198F WP E/E COMPT CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT FOUND FAN ATTACHMENT MOUNT BRACKET CORRODED IN VARIOUS AREAS, REPLACEMENT PART NOT AVAILABLE. REMOVED BRACKET, TREATED AREA IAW DC-8 SRM 51-1-8. CLEANED BRACKET BY GLASS BEADED AREAS TO REMOVE CORROSION. USED F AA TIMCO DER ENGINEERING SKETCH REO-04501 FOR MATERIAL SPECIFICATIONS. 2 L 7 4 4F 4A25 1998052900618 19980529 00618 WP 1998 5 29 RRXA98181 1 19980316 A 5330 5758874 SKIN DOUG DC8 DC863F 302198F WP BS 80 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND CORROSION ON FUSELAGE SKIN AT STA 80 TO STA 90 BETWEEN LONGERONS 27 RIGHT AND 28 RIGHT . REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04506. 2 L 7 4 4F 4A25 1998052900619 19980529 00619 WP 1998 5 29 RRXA98182 1 19980316 A 5330 5756067 SKIN DOUG DC8 DC863F 302198F WP BS 1726 HOLE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT REMOVED DRAIN MAST, NO LONGER REQUIRED AT STA 1726.656 BETWEEN LONGERONS 28 LEFT AND 30 LEFT. FABRICATED AND INSTALLED BLANKED PLATES TO COVER HOLES IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0442. 2 L 7 4 4F 4A25 1998052900620 19980529 00620 WP 1998 5 29 RRXA98183 1 19980325 A 5730 5611015502 PANEL DOUG DC8 DC863F 302198F WP LT WING MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND LEFT WING TRAILING EDGE, PANEL MISDRILLED HOLE, (P/N 5611015-502). FABRICATED AND INS TALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04513. 2 L 7 4 4F 4A25 1998052900621 19980529 00621 WP 1998 5 29 RRXA98184 1 19980401 A 5315 575503271 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 1726 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1726.656 AND BL 20 RIGHT. REMOVED DAMAGED SECTIO N, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAW FAA APPROVED DER TIMCO ENGINEERING SKET CH REO-04549. 2 L 7 4 4F 4A25 1998052900622 19980529 00622 WP 1998 5 29 RRXA98185 1 19980401 A 5350 56544402 FILLET DOUG DC8 DC863F 302198F WP LT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 865F 46088 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT WING FILLET PANEL, NR 162. REMOVED FILLET PANEL FOR REPLACEM ENT, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FILLET PANEL IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-04608. 2 L 7 4 4F 4A25 1998052900623 19980529 00623 WP 1998 5 29 TC8A98029 1 19980513 A 2913 AS63665LE PUMP DOUG DC8 DC862F 3021972 WP NR 3 HYD SYST DAMAGED A TC8A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 183SK 802 45904 LOSS OF HYDRAULIC FLUID TO STAND PIPE ON APPROACH. INSPECTED AND FOUND HYDRAULIC NR 3 ENGINE PUMP DAMAGED. REMOVED AND REPLACED NR 3 ENGINE HYDRAULIC PUMP DUE TO LEAK IAW MM 29-10-12, OPERATIONAL AND LEAK CHECKED IAW MM 29-10-12. 2 L 7 4 4F 4A25 1998052900624 19980529 00624 WP 1998 5 29 TC8A98030 1 19980521 A 2910 LINE DOUG DC8 DC861F 3021953 WP NR 3 HYD SYST FAILED A TC8A O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 GL 23 184SK 45981 DURING APPROACH, EXPERIENCED LOSS OF HYDRAULIC FLUID AND PRESSURE. COMPLIED WITH EMERGENCY CHECKLIST. FOUND AND REPLAC ED 2 PRESSURE HARD LINES FROM ENGINE HYDRAULIC PUMP THAT WERE SPLIT W/FLEX LINES. HYDRAULIC CASE DRAIN FILTERS FOUND OK . CHECKED ON RUN IAW 29-10-0. 2 L 7 4 4F 4A25 1998052900625 19980529 00625 EU 1998 5 29 AWXA9800127 1 19980424 A 5330 SKIN AIRBUS 320 A320231 3930325 EU L2 DOORWAY CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 624AW 55 FEW SPOTS CORROSION AFT OF L2 DOOR AREA NR 5066917 CORROSION REMOVAL BEYOND LIMITS. FABRICATED ANGLE DOUBLER AS PER ER 32-53-17-05. 2 L 7 2 4F RT A28NM 1998052900626 19980529 00626 EU 1998 5 29 AWXA9800132 1 19980518 A 3350 321251 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 644AW 317 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT AT 17 C INOP. REPAIRED BROKEN WIRE AT WALL DISCONNECT. REMOVED CAP REPLACED POWER SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1998052900627 19980529 00627 WP 1998 5 29 CALA9800901 1 19980523 A 3350 110049 BATT CHARGER RADIANT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 98876 49444 INSPECTION FOUND AFT SECTION OF SEAT TRACK EMERGENCY LIGHTS INOPERATIVE. THE AFT SEAT TRACK EMERGENCY LIGHT BATTERY CHA RGER WAS REMOVED AND REPLACED AND OPERATION OF EMERGENCY LIGHTS WAS RESTORED. 2 L 7 2 4F A6WE 1998052900628 19980529 00628 NM 1998 5 29 CALA9800902 1 19980524 A 5320 WEB BOEING 737 7372C0 1384488 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14241 20070 INSPECTION FOUND A 2 INCH CRACK IN LT WHEEL WELL SHEAR WEB AT STA 727. A REPAIR WAS INSTALLED IAW DRAWING 65C29228. 2 L 7 2 4F A16WE 1998052900629 19980529 00629 NM 1998 5 29 CALA9800903 1 19980527 A 5320 WEB BOEING 737 7372C0 1384488 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 2 INCH CRACK IN SHEAR BEAM WEB IN LT WHEEL WELL AT STA 727. REPAIRED IAW DRAWING 65C29228. 2 L 7 2 4F A16WE 1998052900630 19980529 00630 WP 1998 5 29 CALA9800904 1 19980527 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 1309 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 THE AFT LT LAV SERVICE PAN STA 1309, WAS DAMAGED BY LAV TRUCK. THE RESULTANT DAMAGE WAS A 1 INCH CRACK. THE LAV SERVIC E PANEL WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998052900631 19980529 00631 WP 1998 5 29 9809359752 1 19980518 A 3610 AIR DUCTS DOUG DC9 DC941 302207N WP TAIL COMPT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 752NW 47116 DURING CLIMBOUT, THE TAIL COMPARTMENT OVERHEAT LIGHT ILLUMINATED. FLIGHT CREW FOLLOWED COM PROCEDURES, RETURNED TO BNA, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FOLLOWING LEFT SIDE COMPONENTS: THE 8TH AND 13TH STAGE AIR DUCT S, CROSSFEED VALVE, AUGMENTATION VALVE, PRESSURE REGULATING AND SHUTOFF VALVE, AND FLOW CONTROL VALVE AND DUCT. OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052900632 19980529 00632 WP 1998 5 29 9809369915 1 19980525 A 2742 95901 ACTUATOR DOUG DC9 DC931 3022065 WP PRIMARY TRIM FAILED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 965N 33426 1702 47417 PRIMARY TRIM WOULD NOT OPERATE WITH SWITCHES OR SUITCASE HANDLES AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED W ITHOUT INCIDENT. MAINTENANCE REPLACED PRIMARY TRIM ACTUATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998052900633 19980529 00633 WP 1998 5 29 UPS98826796 1 19980515 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, FS 1040 TO 1060 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052900634 19980529 00634 WP 1998 5 29 UPS98826797 1 19980527 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 813UP 46059 INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK OK. (P/N 60-1223-5) (S/N 262) OFF, (P/N 5708458-503) (S/N PTL 1005) ON. 2 L 7 4 4F RT 4A25 1998052900635 19980529 00635 WP 1998 5 29 UPS98826798 1 19980514 A 5347 57572231 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 70-260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C,STA 70 TO 260 ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TR ACK IAW DWG 5759223 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052900636 19980529 00636 WP 1998 5 29 UPS98826799 1 19980514 A 5347 57572231 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 70-260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, STA 70 TO 260 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED T RACK IAW DWG 5759223 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052900637 19980529 00637 WP 1998 5 29 UPS98826800 1 19980515 A 5347 57592231 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, STA 1140, ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223. 2 L 7 4 4F RT 4A25 1998052900638 19980529 00638 WP 1998 5 29 UPS98826801 1 19980515 A 5347 57592231 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, STA 1140 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052900639 19980529 00639 WP 1998 5 29 UPS98826802 1 19980515 A 5347 57592231 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 1240-1260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, STA 1240 TO 1260 ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACE D TRACK IAW DWG 5759223 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052900640 19980529 00640 WP 1998 5 29 UPS98826803 1 19980520 A 5320 3755822501N FITTING DOUG DC8 DC873F 302199F WP BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, STA 320 BETWEEN STR 35L TO 36, THE BACK-UP FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1998052900641 19980529 00641 WP 1998 5 29 UPS98826804 1 19980520 A 5347 529559781 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 360-440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, STA 360 TO 440 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 52955978 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052900642 19980529 00642 WP 1998 5 29 UPS98826805 1 19980514 A 5347 57592231 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 470-640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, STA 470 TO 640 ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998052900643 19980529 00643 WP 1998 5 29 UPS98826806 1 19980515 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1160-1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, LONGERON 31L AND FINGER DOUBLER HAVE CORROSION BTWN STA 1160 TO 1220. REMOVED CORROSION FROM DOUBLER AND REPAIRED LONGERON 31L IAW 8110- 3 APPROVED DHC SK 874-770. 2 L 7 4 4F RT 4A25 1998052900644 19980529 00644 WP 1998 5 29 SCNA98506 1 19980526 A 5313 STRINGER DOUG DC10 DC1015 3022118 WP BS 899-919 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY CHECK, FORWARD CARGO SUMP AREA BETWEEN STA 899 AND 919 STR 52 WAS FOUND TO HAVE LEVEL 2 CORROSION. MATERIA L LOSS IS OUT OF LIMITS. MATEIRIAL VERIFIED AS 7075.160. FABBED TWO EACH STRINGERS TWO EACH SPLICE AND TWO EACH FILLER S PER SRM 53-10-00 FIGURE 1 PRIMED AND TOP COATED TWO EACH SPLICES AND TWO EACH FILLERS PER SRM 51-20-01 PRIMED AND TOP COATED TWO EACH FILLERS PER SRM 51-21-01 PARTS INSTALLED PER SRM 53-10-00 FIGURE 2. 2 L 7 3 4F A22WE 1998052900645 19980529 00645 WP 1998 5 29 SCNA98507 1 19980526 A 5521 SPAR CAP DOUG DC10 DC1015 3022118 WP RT HORIZ STAB CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY CHECK, THE RIGHT HAND HORIZONTAL STABILIZER XFS77 XE57 WAS FOUND TO HAVE A 2 INCH CRACK AS VIEWED FROM INTE RSPAR BOX ON TOP OF FORWARD SPAR AT JUNCTION OF FUSELAGE SKIN ON FORWARD SPAR. MATERIAL VERIFIED 7075 T6 .125 FOR REPA IR DOUBLER -11 AND 13 (4.75 X 31) PER SRM 55-20-00 PAGE 43 MATEIRIAL VERIFICATION FOR TWO EACH FILLERS -17 AND -19 7075 T6 .160. FABBED -17 AND -19 FILLERS PER SRM 55-20-00 FIG 8 PRIMED FILLERS MATERIAL VERIFICATION FOR TAPERED SHIM ON FWD SPAR CAP SPLICE 7075 T6 .125. CUTOUT DAMAGED AREA PER SRM 55-20-00 FIGURE 8 PER SRM 51-21-01. DRILLED AND LOCATED NEW SPAR CAP -3, -7 ANGLES -19 FILERS TREATED PRIMED AREA AND INSTALLED NEW PARTS. 2 L 7 3 4F A22WE 1998052900646 19980529 00646 WP 1998 5 29 SCNA98508 1 19980526 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1959-2007 CORRDED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY CHECK IN THE WASTE TANK COMPARTMENT RIGHT TUNNEL 186 STATION 2007 AT THE FLOOR LEVEL OUTER FLOORBEAM WAS CO RRODED ON THE END. MATERIAL VERIFICATION TO BE 7075 T6511, FOR EACH SEAT TRACK AND MATERIAL VERIFIED FOR EACH U CHANNEL SPLICE TO BE 7075 T6511. DURING THIS THE RIGHT AFT DOOR OPEN UP THRESHOLD STATION 1853.950 TO 1887. SUN COUNTRY REQU ESTED OPPORTUNITY INSPECTION AND SEAT TRACK WAS REMOVED AND REPLACED AND LOCATED LAV ATTACH POINTS PER SRM 53-70-00 FI GURE 1. 2 L 7 3 4F A22WE 1998052900647 19980529 00647 WP 1998 5 29 SCNA98509 1 19980526 A 3520 LATCH SOLENOID DOUG DC10 DC1015 3022118 WP OXYGEN BOX INOPERATIVE A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING HEAVY CHECK, THE FLIGHT ATTENDANT L-4 OXYGEN BOX WOULD NOT OPEN DURING OXYGEN DROP CHECK. REMOVED AND REPLACED L ATCH SOLENOID AT L-4 FLIGHT ATTENDANT STATION OXYGEN BOX PER MM 35-20-00, OPERATIONAL CHECKS GOOD PER MM 35-20-00. 2 L 7 3 4F A22WE 1998052900648 19980529 00648 NM 1998 5 29 SCNA98701 1 19980516 A 5320 SUPPORT BOEING 727 727225 1384077 NM BS 848.95 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK, A FLOOR SUPPORT STRUCTURE AT STATION 848.95 CENTER HAS CRACKS AROUND FASTENERS. REMOVED DAM AGED SECTION IAW B727 SRM 51403 FIG 1. MATERIAL VERIFICATION PER B727 SRM 53102 FIG 7 SHEET 14 AS 7075-T6 .040. FABRCI ATED REPAIR ANGLES FROM 7075-T6 .040C IAW B727 SRM 51403 FIG 1. TREATED AND PRIMED IAW B727 SRM 51106. INSTALLED REPAI R IAW B727 SRM 51302 AND 51403 FIG 1. 2 L 7 3 4F A3WE 1998052900649 19980529 00649 NM 1998 5 29 SCNA98702 1 19980518 A 5311 FRAME BOEING 727 727225 1384077 NM BS 760.95 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK, FLOOR FRAME AT STATION 760.95 WAS FOUND CRACKED IN CORNER. REMOVED DAMAGE FROM FLOOR SUPPOR T. MATERIAL VERIFICATION PER B727 SRM 53102 FIG 7A 7075 T6 .040C. FABRICATED REPAIR ANGLES FROM 7075 T6 .040C IAW B727 SRM 51403 FIG 1. TREATED AND PRIMED IAW B727 SRM 51106. INSTALLED IAW SRM B727 53102. 2 L 7 3 4F A3WE 1998052900650 19980529 00650 NM 1998 5 29 SCNA98704 1 19980515 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 1090-1120 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND AT THE LEFT CENTER SEAT TRACK AT STATION 1090 TO 1120 ON THE INSIDE OF T HE TRACK. REMOVED SEAT TRACK IAW B727 SRM 51302. TRACK OUT OF LIMITS IAW B727 SRM 513002. MATERIAL ID 7075 T6 PER SRM 511001. FABRICATED NEW SEAT TRACK MATERIAL ID 7075 T6. ALODINED AND PRIMED PER SRM B727 511002 AND 514005. INSTALLED SEAT TRACK IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998052900651 19980529 00651 NM 1998 5 29 SCNA98705 1 19980513 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM CABIN DAMAGED A SCNA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK, THE RIGHT SIDE UNDER FLOORBOARD NUMBER 9 UNDER INBOARD SEAT TRACK HAS HOLE AND DRILL BIT TRA CK MARKS. REMOVED DAMAGED INTERCOASTAL. MATERIAL ID 7075 T6 .03. FABRICATED REPAIR PER ORIGINAL PART. ALODINED AND P RIMED SRM 51-10-02. INSTALLED REPAIR PART AT NUMER 9 INTERCOASTAL PER SRM 513002 2 L 7 3 4F A3WE 1998052900652 19980529 00652 NM 1998 5 29 SCNA98703 1 19980515 A 5347 SEAT TRACK BOEING 727 727225 1384077 NM BS 1070 MISDRILLED A SCNA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK, THE LEFT CENTER SEAT TRACK AT STATION 1070 HAD A NUT PLATE HOLE THAT WAS MISDRILLED AND EXTR EMELY WALLOWED OUT. REMOVED SEAT TRACK IAW B727 SRM 513002. TRACK OUT OF LIMITS IAW B727 SRM 513002. MATERIAL ID 7075 T6 B727 SRM 511001. FABRICATED NEW SEAT TRACK MATERIAL ID 7075 T6. TREATED AND PRIMED B727 SRM 514005. INSTALLED SEA T TRACK IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998052900653 19980529 00653 WP 1998 5 29 RRXA98186 1 19980217 A 7810 NOZZLE DOUG DC8 DC863 302198A WP NR 1 ENGINE CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND NR 1 ENGINE EXHAUST NOZZLE OUTBOARD SKIN CRACKED AT 9:30 POSITION. REMOVED NR 1 ENGIN E EXHAUST NOZZLE OUTBOARD SKIN AND STRUCTURE IAW DC-8 SRM 51-1-21. FABRICATED AND INSTALLED SPLICE DOUBLER IAW FAA APPR OVED DER COTNEY ENGINEERING SKETCH E04-R04. 2 L 7 4 4F 4A25 1998052900654 19980529 00654 WP 1998 5 29 RRXA98187 1 19980217 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 340 TORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND FUSELAGE SKIN TORN, AFT EDGE OF A PIT DOOR, AT STA 340 BETWEEN LONGERONS 30 RIGHT AND 31 RIGHT. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKET CH E04-R03. 2 L 7 4 4F 4A25 1998052900655 19980529 00655 WP 1998 5 29 RRXA98188 1 19980218 A 5320 5750198502 FITTING DOUG DC8 DC863 302198A WP BS 900 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND CORROSION ON TOP OF LONGERON 24 RIGHT AT AFT EDGE OF BATH TUB FITTING AT STA 900. REM OVED CORROSION IAW DC-8 SRM 51-1-8. ORIGINAL THICKNESS (0.250 INCH) IAW DC-8 SRM 53-2-2, FIGURES (SHEET 7/8). REMOVED 0.006 INCH WITHIN LIMITS IAW DC-8 SRM 53-2-0 FIGURE 1F. TRIMMED EDGE OF FUSELAGE AT STA 902 FITTING APPROX 0.030 INCH S URFACE CORROSION. STOPPED AND DID NOT PROCEED UNDER FITTING, CLEANED AND PRIMED IAW DC-8 SRM 51-1-8. TRIM ON FITTING W AS COMPLETED IAW DAC FAX FILE NR 98-03-04-003. 2 L 7 4 4F 4A25 1998052900656 19980529 00656 WP 1998 5 29 RRXA98189 1 19980221 A 5315 4640968 FLOORBEAM DOUG DC8 DC863 302198A WP BS 920 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND RIVET HEAD SHEARED AND CORROSION ON STIFFENER ON LEFT SIDE OF UPPER WHEEL WELL AT STA 902 BL 27 TO 31 LEFT. HI-LOK SHEARED AND STIFFENER BULGING WITH CORROSION EVIDENT ON PRESSURE WEB AT STA 902 BL 50 LEFT TO 57 LEFT. PRESSURE WEB WAS CUT FOR ACCESS AND FOUND FLOORBEAM CORRODED BEYOND LIMITS. REMOVED CORROSION, TREATED AR EA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLERS AND DOUBLER REPAIR TO FLOORBEAM IAW DC-8 SRM 53-2-2 AND IAW FA A APPROVED DER ENGINEERING SKETCH E04-R08. FABRICATED AND INSTALLED DOUBLER REPAIR IAW COTNEY ENGINEERING SKETCHES E04- R06 AND E04-R07. 2 L 7 4 4F 4A25 1998052900657 19980529 00657 WP 1998 5 29 RRXA98190 1 19980302 A 5751 1645646 SPAR DOUG DC8 DC863 302198A WP WS 741-755 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RIGHT WING AILERON SPAR AT XA=741 TO XA=755. REMOVED DAMAGED SECT ION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE REPAIR IAR FAA APPROVED DER ENGINEERING SKETCH E 04-R09. 2 L 7 4 4F 4A25 1998052900658 19980529 00658 WP 1998 5 29 RRXA98191 1 19980303 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 69.5 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND LEFT WING, UPPER SKIN CRACKED AT XCW=69.5, 3.5 INCHES FORWARD OF TRAILING EDGE. FABRI CATED AND INSTALLED REPAIR DOUBLER IAW BCAG ROD SKETCH 98-03-05-001 AND FAX MISC-3063/GDA ATA 08-57-01-02, DTD 9 MARCH 9 8 AND REFTS 98-141. UNDER ACMI WO EO47 NR Y1313. 2 L 7 4 4F 4A25 1998052900659 19980529 00659 WP 1998 5 29 RRXA98192 1 19980303 A 5315 2772345 FLOORBEAM DOUG DC8 DC863 302198A WP BS 1702 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON FLOORBEAM AT STA 1702 AND BL 27 RIGHT. REMOVED DAMAGED SECTION, T REATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E04-R12 AND RFTS 98-142. UNDER ACMI WO EO47 N/R X0089. 2 L 7 4 4F 4A25 1998052900660 19980529 00660 WP 1998 5 29 RRXA98193 1 19980305 A 5711 SPAR DOUG DC8 DC863 302198A WP WS 337-380 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, AIRCRAFT ARRIVED WITH LOG ITEM PAGE 6736-01, LEFT WING, AFT SPAR WEB CRACKED XRS=337 TO XRS= 380. FABRICATED AND INSTALLED REPAIR IAW DOUGLAS SERVICE SKETCH 1635, 1628 AND SKETCH NR 97147. 2 L 7 4 4F 4A25 1998052900661 19980529 00661 WP 1998 5 29 RRXA98194 1 19980309 A 5320 DOUBLER DOUG DC8 DC863 302198A WP BS 1620 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND CORROSION IN AFT ACCESSORY COMPARTMENT TO SKIN DOUBLER UNDER LONGERON 33 RIGHT AT STA 1620 TO STA 1640. REMOVED CORRODED DOUBLER, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E04-R5. 2 L 7 4 4F 4A25 1998052900662 19980529 00662 WP 1998 5 29 RRXA98195 1 19980309 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 408.34 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND LEFT WING, LEADING EDGE, SCREW LOOSE AND WORN THROUGH SKIN AT XW=408.34. REMOVED SECT ION WORN THROUGH SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E04-R02. 2 L 7 4 4F 4A25 1998052900663 19980529 00663 WP 1998 5 29 RRXA98196 1 19980312 A 5320 DOUBLER DOUG DC8 DC863 302198A WP BS 900 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND FINGER DOUBLERS (2 EACH), CORRODED AT SUB FLOOR AT STA 900 AND BL 0 AND WL-9. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E04-R10. 2 L 7 4 4F 4A25 1998052900664 19980529 00664 WP 1998 5 29 RRXA98197 1 19980317 A 5321 FLOOR DOUG DC8 DC863 302198A WP BS 45 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 45. REMOVED OLD FLOOR, TREATED AREA IAW DC-8 S RM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR PANEL IAW ENGINEERING DIRECTIVE EDE 04-1 AND STC 1802SO. 2 L 7 4 4F 4A25 1998052900665 19980529 00665 WP 1998 5 29 RRXA98198 1 19980318 A 5711 SPAR DOUG DC8 DC863 302198A WP WS 373 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796AL 46054 DURING A MAINTENANCE VISIT, FOUND LEFT WING, UPPER AFT SPAR GOUGED AT XRS=373, DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E04-R11. UNDER ACMI WO EO47 NR N0004. 2 L 7 4 4F 4A25 1998053000001 19980530 00001 NE 1998 5 30 UPS98526604 2 19980513 A 7200 ENGINE BOEING 757 75724APF 1384969 NM RROYCE RB211 RB211535E437 54555 NE NR 2 VIBRATION A IPXA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 SO 01 457UP 25478 NR 2 ENG VIB INDICATOR WENT TO 5.0 YELLOW RANGE ON CLIMB-OUT LEVELED OFF POWER TO IDLE, VIB WENT TO 2.8 - 4.3 FLUCTUATIN G. ENG SHUT DOWN. RETURN TO PIE. AWAITING PARTS, USED A/C 707 TO PICK UP LOAD. VISUAL CK OF INLET AND EXHAUST AND CH IP DETECTORS OK. MONITOR FAILED SELF CK. 2 L 7 2 4F 4 F RT A2NM E12EU 1998053000002 19980530 00002 NM 1998 5 30 VNAA9805005 1 19980510 A 6120 OVERSPEED TEST DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROPELLER FAILED A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 440JS 3058 ON THE TAXI OUT, PRIOR TO TAKEOFF, THE LEFT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998053000006 19980530 00006 SW 1998 5 30 HEEA0014187 1 19980512 A 6220 206010360005 LINK ASSY BELL 206 206L1 1182107 SW M/R HEAD CORRODED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3905B 45598 LINK ASSY HAS CORROSION AROUND END FITTING. SCRAPPED AND REPLACED WITH SERVICEABLE PART. 1 G 7 1 3U H2SW 1998053000008 19980530 00008 NM 1998 5 30 DL73E981052 1 19980513 A 5315 6545410515 FLOORBEAM BOEING 737 737247 138448D NM BS 665 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 378DL 23605 WING/CENTER WING BOX/FLOORBEAM, STA 665, BL 0.07, REPAIR FOR UPPER CAP AND WEB CRACKS. CRACKS WERE FOUND IN THE WING CE NTER SECTION BL 0.07 FLOORBEAM AT STA 665. THE UPPER CAP OF THE BEAM WAS COMPLETELY SEVERED AND THE WEB AND WEB DOUBLER WERE FOUND WITH A 4 INCH CRACK AT THE SAME LOCATION. THE DAMAGE WAS REPAIRED PER BAC S/B 737-57-1210 AS DOCUMENTED IN ER/A 364760-14, REV B. 2 L 7 2 4F A16WE 1998060400001 19980604 00001 WP 1998 6 4 VTZA98208 2 19980213 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP NR 1 MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 470UE 814 FLT 6455 - IAD-PHL - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO NR 1 ENGINE TORQUE EGT AND RPM FLU CTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 57154 MEL 76-2 ON T TL. DMI 57154 CLOSED ON 3-3-98 BUT COULD NOT DUPLICATE PROBLEM AND NO DEFECTS NOTED, OPS CHECK OK. AIRCRAFT WAS RELEAS ED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998060400002 19980604 00002 EU 1998 6 4 UF6A980343 1 19980322 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 13880 2022 SBN - LEFT AFT OVERWING EMERGENCY LIGHT OUT. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998060400003 19980604 00003 EU 1998 6 4 UF6A980340 1 19980325 A 3350 P4010021 BATTERY BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 ORD - AFT FLIGHT ATTENDANT FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECKED GOOD. 2 L 7 2 4T RT A27NM 1998060400004 19980604 00004 EU 1998 6 4 UF6A980341 1 19980317 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 13209 2028 SBN - OVERWING AFT EMERGENCY LIGHT ON NR 1 SIDE INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998060400005 19980604 00005 EU 1998 6 4 UF6A980342 1 19980318 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 11875 2035 SBN - OUTSIDE OVERWING EMERGENCY LIGHT ON NR 1 SIDE INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998060400006 19980604 00006 SO 1998 6 4 RAAA98E8013 1 19980526 A 5230 SKIN LKHEED 188 188C 5262604 SO CARGO DOOR CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 1 CHECK, FOUND FWD LOWER CARGO DOOR OUTER SKIN CRACKED APPROX 1 INCH AT HANDLE RECESS. REPAIRED PER SRM 53-2-1, FIG 2 (SHEET 3) AND FIG 2 (SHEET 5), M-54 NR 14. 2 L 7 4 4T 4A22 1998060400007 19980604 00007 NM 1998 6 4 RAAA98B1025 1 19980526 A 3350 900835A BATTERY PACK GRIMES 1000679LB BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT FWD AND RT AFT EXTERNAL OVERWING EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE LOW CHARGE. 2 L 7 3 4F A3WE 1998060400008 19980604 00008 NM 1998 6 4 DLM90980828 1 19980416 A 2421 28B5282 GENERATOR 28B5282 DOUG MD90 MD9030 3023690 NM APU FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 910DN 120 53390 ON CLIMBOUT PASSING 10,000 FT, APU AC PWR FAULT MSG ILLUMINATED. APU ABNORMAL COMPLIED WITH, APU GEN OFF AND APU MASTE R SWITCH OFF. RETURNED TO DFW. REPLACED APU GEN. NO LEAKS, FAULTS, OR MSGS. OPN TEST GOOD. NOTE: LT ENG GEN ALREADY ON MCO. 2 L 7 2 4F RT A6WE 1998060400009 19980604 00009 NM 1998 6 4 UPS98426584 1 19980504 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE N/A, CRACK FOUND ON PYLON NR 1 RT SIDE WHICH EXTENDS THE TRIMMING AREA REQUIRED BY SB 54-2034 IN FRONT O F STATION 180. REMOVED PREVIOUS REPAIR, TRIMMED EFFECTED CRACK, INSTALLED REPAIR PER SB 54-2034. 2 L 7 4 4F A20WE 1998060400010 19980604 00010 NM 1998 6 4 UPS98426585 1 19980404 A 5400 DOUBLER BOEING 747 747212B 1384886 NM NR 3 PYLON MISREPAIRED A IPXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE-N/A, PREVIOUS DOUBLER REPAIR ON PYLON NR 3 LT SIDE FOUND INSTALLED ON THE AREA WHERE IT WILL INTERFERE W ITH THE INSTALLATION OF NEW DOULBLER PER SB-54-2034. REMOVED PREVIOUS REPAIR, INSTALLED NEW REPAIR PER SB 54-2034. 2 L 7 4 4F A20WE 1998060400011 19980604 00011 NM 1998 6 4 UPS98426586 1 19980404 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 2 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE-N/A, RT SIDE OF PYLON NR 2 IS CRACKED ON EXTERIOR SKIN IN FRONT OF STA 180 WHICH EXTENDS THE TRIMMING AR EA, REPAIRED PER SB-54-2034. REMOVED PREVIOUS REPAIR, TREATED AND INSTALLED NEW REPAIR UP TO TRIMMING AREA PER SB-54-20 34. 2 L 7 4 4F A20WE 1998060400012 19980604 00012 NE 1998 6 4 DLL14981023 2 19980512 A 7261 RB211524B4I OIL TUBE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B402 54555 NE NR 3 ENGINE CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 740DA 56613 193C1244 014629 EN ROUTE TO HNL CONT DROP NR-3 OIL QTY DIVERTED TO SFO. QTY, DROPPED TO 3.1 QTS SHORTLY AFTER DROPPED TO ZERO NML TEMP/ PRESS AT 2055Z OIL PRESS FLUCT 10 PSI FROM 35 TO 55 PSI, ENG SHUT DN AT THAT TIME AND FOLLOW UP PROC ACCOMP. FOUND OIL TUBE CRACKED AT OIL RETURN COMBUSTION LP TURBINE BRG TO 3 WAY CONN ASSY. 2 L 7 3 4F 4 F A23WE E12EU 1998060400014 19980604 00014 NM 1998 6 4 DL72S981115 1 19980520 A 5280 DOOR BOEING 727 727225 1384077 NM LT/RT MLG CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 A .300 LONG CRACK AT THE RT AND LT MLG DOOR CLOSE OUTS. TIME LIMITED REPAIR MADE PER ERA 364849-14. 2 L 7 3 4F A3WE 1998060500005 19980605 00005 NE 1998 6 5 98ZZZX2013 1 19980514 A 2612 473205 DETECTOR SKRSKY S76 S76A 8143006 NE NR 2 ENGINE FAILED A HEEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 03 1546K 1188 760082 SHORTLY AFTER TAKEOFF, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED INTERMITTENTLY (APPROXIMATELY 5 SECONDS/MINUTES). AFT ER DETERMINING NO FIRE, RETURNED TO BASE. MAINTENANCE REPLACED DEFECTIVE FLAME DETECTOR. REF: S-76 IPC, CHAPTER 26-11 -00, FIGURE 1, ITEM 21. 1 G 7 2 3U H1NE 1998060500007 19980605 00007 EU 1998 6 5 98ZZZX2015 1 19980520 A 5512 D55180000000 STABILIZER AIRBUS 320 A320214 EU RT HORZ STAB DAMAGED A S AJLF K NONE O OTHER IN INSP/MAINT 1 SO 23 630AJ 2339 CG1529 630 RIGHT-HAND HORIZONTAL STABILIZER AND ELEVATOR FOUND DAMAGED ON TRANSIT CHECK IN MONTEGO BAY BY MAINTENANCE. THERE WAS N O REPORT FROM THE FLIGHT CREW. INVESTIGATION REVEALED DEBRIS (ASPHALT) EMBEDDED IN THE RIGHT-HAND ELEVATOR. THE DETAIL S OF THE TOTAL DAMAGE ARE ATTACHED. IN KINGSTON, RUNWAY 12 WAS VISITED AT ABOUT 1130 HOURS (LOCAL) ON MAY 20, 1998, WIT H A VIEW THAT THE DAMAGE TO THE RIGHT-HAND STABILIZER AND ELEVATOR WAS A RESULT OF AN IMPACT DURING AIRCRAFT TAKEOFF. R EF: 20-10-98. ACFT TC: 1,581. 2 L 7 2 4F RT A28NM 1998060500013 19980605 00013 NM 1998 6 5 98ZZZX2021 1 19980413 A 3350 BAC1522452 TRACK COVER BOEING 757 75723A 1384967 NM CABIN DISLODGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 757NA 24567 THREE INCH SECTION OF E-PATH TRACK COVER DISLODGED FROM AFT END OF TRACK. SECURED E-PATH TRACK COVER. OPERATIONAL CHEC K OK. 2 L 7 2 4F RT A2NM 1998060500044 19980605 00044 SO 1998 6 5 98ZZZX2052 1 19980513 A 3260 CONNECTOR PIPER PA31 PA31310 7103103 SO RT MLG DOWNLOCK DIRTY A ATJA K NONE P NO WARNING INDICATION IN INSP/MAINT 1 NE 05 9287Y 31380 DURING PREFLIGHT INSPECTION, RIGHT DOWN/LOCKED (LANDING GEAR) LIGHT WAS NOT ILLUMINATED. FOUND INTERMITTENT CONNECTION IN CANNON PLUG AT RIGHT WING ROOT (LEADING EDGE). REMOVED CONNECTORS FROM PLUG, CLEANED AND REINSTALLED. SYSTEM OPERAT ES NORMALLY. AIRCRAFT TOTAL TIME, 8,972.9 HOURS. 1 L 7 1 3O RT A20SO 1998060500045 19980605 00045 SO 1998 6 5 98ZZZX2053 1 19980430 A 2434 ALU8421 ALTERNATOR PIPER PA31 PA31 7103102 SO RT ENGINE SHORTED A ATJA O OTHER H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 NE 05 9287Y 701 5052763 31380 PILOT REPORTED BOTH ALTERNATORS FAILED. PILOT TRIED AUXILIARY REGULATOR, ALTERNATOR CAME ON-LINE FOR SHORT TIME, THEN F AILED. INVESTIGATION REVEALED THE FIELD OF THE RT GENERATOR WAS INTERMITTENTLY SHORTING TO GROUND. SUBMITTER SUSPECTED INSULATION BREAKDOWN DUE TO HEAT. SINCE ONE VOLTAGE REGULATOR CONTROLS BOTH ALTERNATORS, THIS FAILURE CAUSED THE LT AL TERNATOR TO FAIL. 1 L 7 2 3O A20SO 1998060500049 19980605 00049 1998 6 5 CALA9800905 4 19980521 A 2210 19361005 SENSOR DOUG DC10 DC1010 3022110 WP RT COCKPIT INOPERATIVE A A CALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 09 68043 29488 46902 THE AIRCRAFT PITCHED UP RAPIDLY WITH NR 1 AUTOPILOT ENGAGED WHILE IN CLIMB AT APPROXIMATELY 31,000 FEET AFTER DEPARTURE. THE CAPTAIN COUNTERED THE AFT YOKE MOTION AND DISENGAGED AUTOPILOT. THE AIRCRAFT WAS IN TRIM WITH AUTOTHROTTLES STABL E IN N1 AND CLIMB POWER. THE AIRCRAFT WAS RETURNED TO LAX. TROUBLESHOOTING BY ENGINEERING FOUND THE FIRST OFFICER'S CO NTROL WHEEL SENSOR AT FAULT. BOTH THE FIRST OFFICER'S AND CAPTAIN'S CONTROL WHEEL SENSORS WERE REMOVED AND REPLACED. T HE SENSORS WERE CHECKED IAW MM 22-12-03 AND OPERATION CHECKED GOOD. AN EVALUATION FLIGHT WAS PERFORMED AND BOTH AUTOPIL OT SYSTEMS NR 1 AND NR 2 CHECKED NORMAL. 2 L 7 3 4F A22WE 1998060500050 19980605 00050 SO 1998 6 5 COMA9810128 1 19980525 A 5753 DRP138112VT ROLLER EMB 120 EMB120RT SO LT TE FLAP WORN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 244CA 120217 FLAPS WOULD NOT RETRACT AFTER TAKEOFF. REPLACED FLAP ROLLERS AT LEFT HAND OUTBOARD FLAP. 2 L 7 2 4T RT A31SO 1998060500051 19980605 00051 EA 1998 6 5 COMA9860116 1 19980526 A 3350 BF10044004 SIGN CNDAIR CL600 CL6002B19 EA CABIN MISSING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 963CA 7127 EMERGENCY EXIT LIGHT OVER SERVICE DOOR MISSING. REPLACED SIGN ASSEMBLY. 2 L 7 2 4F RT A21EA 1998060500052 19980605 00052 NM 1998 6 5 UPS98226809 1 19980525 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1372 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-C, CORROSION AND PILLOWING SKIN ABOVE NR 2 ENGINE FAIRING BS 1372 RBL 30 WL 250. REMOVED AND REPLACED S KIN PANEL AND REPAIRED DAMAGED FWD SKIN IAW SRM 53-30-03. 2 L 7 3 4F A3WE 1998060500053 19980605 00053 NM 1998 6 5 UPS98226812 1 19980505 A 5330 SKIN BOEING 727 72751C 1384015 NM BS 1080-1183 DISBONDED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 902UP 18898 INSPECTION TYPE-D, DISBONDED SKIN REMOVED LEFT HAND 1183 TO BS 1080 FROM STRINGER 18 TO 26. REPAIR CARRIED OUT PER SRM ENGINEERING ORDER 98-12-007, REF UPS ENGINEERING FILE NUMBER 5330-2032 AND DRAWING 65-18386. 2 L 7 3 4F A3WE 1998060500054 19980605 00054 WP 1998 6 5 UPS98826785 1 19980509 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1600 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, FRAME LWR FLANGE AT STA 1600, HAS CORROSION AT LONGERON 34L TO 34R. REPAIRED AREA IAW DWG 2641520 AN D SRM 53-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998060500055 19980605 00055 WP 1998 6 5 UPS98826807 1 19980515 A 5313 STRINGER DOUG DC8 DC873F 302199F WP BS 280-300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, FS 280 TO 300 STR 28L CORRODED BEYOND LIMITS. REPAIRED IAW SRM 53-2-2 AND 53-4-1. 2 L 7 4 4F RT 4A25 1998060500056 19980605 00056 WP 1998 6 5 UPS98826808 1 19980517 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 280-300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, FS 280 TO 300 LONGERON 29L CORRODED. REPAIRED IAW SRM 53-2-2 AND 53-4-1. 2 L 7 4 4F RT 4A25 1998060500057 19980605 00057 WP 1998 6 5 UPS98826810 1 19980514 A 5320 57503229 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, INTERCOSTAL LWR ATTACH ANGLE JUST FWD OF FS 1160 ABOVE LONG 35R CRACKED. REMOVED AND REPLACED FITTIN G IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998060500058 19980605 00058 WP 1998 6 5 UPS98826811 1 19980513 A 5320 37558272 FITTING DOUG DC8 DC873F 302199F WP BS 300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, FS 300 AT STR 33R FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998060500059 19980605 00059 WP 1998 6 5 UPS98826814 1 19980512 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, FRAME HAS HEAVY CORROSION UNDER NUT PLATE AT FS 1060 LONG 36. REPAIRED IAW DHC SK-802-676. 2 L 7 4 4F RT 4A25 1998060500060 19980605 00060 WP 1998 6 5 UPS98826815 1 19980513 A 5320 475851411 CLIP DOUG DC8 DC873F 302199F WP BS 1300-1320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, FS 1300 TO 1320 LONG 32R FWD INTERCOSTAL ATTACH CLIP HAS EXTREME CORROSION AND AFT ATTACH CLIP IS CRA CKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIPS IAW SRM 51-1-21 AND DWG 4758514-11 AND -12. 2 L 7 4 4F RT 4A25 1998060500061 19980605 00061 WP 1998 6 5 UPS98826816 1 19980512 A 5320 5751516121 SUPPORT DOUG DC8 DC873F 302199F WP BS 980-1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, C PIT FLOOR TRACK SUPPORT HAS CORROSION UNDER NUT PLATES FROM FS 980 TO 1200 LONG 33L. REMOVED, FABR ICATED, AND INSTALLED REPLACEMENT TRACK SUPPORT IAW SRM 51-1-21 AND DWG 5751516. 2 L 7 4 4F RT 4A25 1998060500062 19980605 00062 WP 1998 6 5 UPS98826817 1 19980511 A 5320 36410042 FITTING DOUG DC8 DC873F 302199F WP BS 880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, RMLG W/W O/B FWD CORNER AT FS 880, FWD LWR SIDE OF FITTING HAS HEAVY CORROSION LONGERON 24. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998060500063 19980605 00063 NM 1998 6 5 QXEA9800676 1 19980522 A 3350 MS25231316 BULB GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 816PH 54 PSC- EMERGENCY OVERHEAD LIGHT AT ROW NR 6 HAS A LIGHT BULB THAT IS INOP. REPLACED LAMP, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998060500064 19980605 00064 NM 1998 6 5 QXEA9800677 1 19980518 A 5210 WIRE ROPE DHAV DHC8 DHC8102 2809003 NM CABIN DOOR MISRIGGED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 840PH 74 SEA- MAIN CABIN DOOR WOULD NOT OPEN. INSPECTED AND FOUND THE MAIN CABIN DOOR CABLE TO BE WINDING UP WRONG AS THE DOOR C LOSED. REWOUND CABLE AND RIGGED DOOR PER DHC-8 MAINTENANCE MANUAL, OPERATIONAL CHECKS GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998060500065 19980605 00065 NM 1998 6 5 98FDEA00366 1 19980527 A 5313 6518382225 STRINGER BOEING 727 72721C 138400M NM BS 950-1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 NR 0684 044, CORROSION (C53-224-01(3)) ON STRINGER 2 LT, BS 950-1050. REPAIRED NR 2 LT STRINGER, BS 950-1050 IAW FED-EX SRM 53-10-3. 2 L 7 3 4F A3WE 1998060500067 19980605 00067 NM 1998 6 5 98FDEA00367 1 19980527 A 5315 FLOORBEAM BOEING 727 727225 1384077 NM BS 950 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 MAIN CARGO, PREVIOUS DAMAGE DOUBLER DRILLED HOLE IN FLOORBEAM BS 950F, RBL 3. REMOVED DAMAGE AND REPAIRED FLOORBEAM PER SRM 53-10-8 FIG 8. 2 L 7 3 4F A3WE 1998060500068 19980605 00068 NM 1998 6 5 98FDEA00368 1 19980526 A 5311 FRAME BOEING 727 727225 1384077 NM BS 500 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 LOWER FWD CARGO FRAME DENTED BS 500, BETWEEN STR 24L AND 25L. REPAIRED BELL FRAME BS 500 PER SRM 51-40-3 AND EA 7-5310- 29526. 2 L 7 3 4F A3WE 1998060500069 19980605 00069 NM 1998 6 5 98FDEA00369 1 19980526 A 5311 FRAME BOEING 727 727225 1384077 NM BS 520 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 LOWER FWD CARGO COMP LT FS 520 BELL FRAME IS DENTED IN SEVERAL AREAS BETWEEN STR 23L AND 26L. REPAIRED BELL FRAME PER S RM 51-40-3 AND WA 7-5310-29526. 2 L 7 3 4F A3WE 1998060500070 19980605 00070 NM 1998 6 5 98FDEA00370 1 19980526 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1010 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 2129236 DENT IN FRAME BS 1010 ABOVE STR 26R IN AFT CARGO. REMOVED DAMAGE FROM FRAME PER SRM 53-10-4, INSTALLED REPAIR DOUBLER P ER SRM 53-10-4 FIG 1 PG 3 AND 4. 2 L 7 3 4F A3WE 1998060500071 19980605 00071 WP 1998 6 5 ABXA9800465 1 19980525 A 5320 995823911 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP BS 1019 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 980AX 47176 DURING C-CHECK, FOUND FRAME SHEAR TIE AT STATION 1019 CRACKED BETWEEN LONGERON 14L AND 15L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998060500072 19980605 00072 WP 1998 6 5 ABXA9800466 1 19980525 A 5311 5911448503 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 446 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND FRAME AT STATION 446 AND LONGERON 28L TO 29R CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998060500073 19980605 00073 WP 1998 6 5 ABXA9800467 1 19980525 A 5312 9915558137N BULKHEAD ANGLE DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD, FORWARD RIGHT SIDE 3RD STIFFENER ATTACH ANGLE CRACKED. REPAIRED ANGLE IAW DC9 SB 53-166 AND CACO DWG 941558. 2 L 7 2 4F A6WE 1998060500074 19980605 00074 WP 1998 6 5 ABXA9800468 1 19980525 A 5320 991050127 WEB DOUG DOUG DC9 DC931 3022065 WP BS 260 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND CUSP WEB STATION 260 RIGHT SIDE CRACKED. REPAIRED CUSP WEB IAW ABX REA D953-23794-MR AND REA 953- 23777MR. 2 L 7 2 4F A6WE 1998060500075 19980605 00075 WP 1998 6 5 ABXA9800469 1 19980525 A 5320 991551827 ANGLE DOUG DOUG DC9 DC931 3022065 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, FOUND THE LEFT MAIN LANDING GEAR WHEEL WELL DOOR JAMB ANGLE CRACKED INBOARD OF HAND PUMP. REPLACED ANGL E IAW DACO DWG 9915518 AND DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998060500076 19980605 00076 WP 1998 6 5 MWEA98626 1 19980525 A 5313 3913291501 LONGERON DOUG DC9 DC982 3022082 WP BS 1375-1400 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CORROSION IN AFT ACCESSORY COMPARTMENT LONGERON 24L BETWEEN FS 1375 TO 1400. MTC FABRICATED AND INSTALLED NEW SEC TION OF LONGERON. 2 L 7 2 4F A6WE 1998060500077 19980605 00077 NM 1998 6 5 P5CA9800778 1 19980523 A 3010 69B476006 CONTROL CARD BOEING 747 747122 1384872 NM COCKPIT OVERHEATED A P5CA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 23 852FT 19757 APPROXIMATELY 6 HOURS INTO FLIGHT HAD STRONG ODOR OF ELECTRICAL COMPONENTS OVER HEATING/BURNING. ALSO, HAD VISIBLE SMOK E HAZE. RAN SMOKE SOURCE AND ELECTRICAL FIRE CHECKLIST. CREW USED OXYGEN ODOR DISSIPATED AFTER 20 TO 30 MINUTES. FOUN D WING ANTI-ICE CONTROL CARD AND RELAY WITH EVIDENCE OF OVERHEAT/BURNING. REPLACED RELAY AND CONTROL CARD OPERATIONAL C HECK NORMAL PER M/M 36-11-00 AND 24-00-00. ALSO, REPLACED A1, A8, A10, A13, AND A17 MASTER DIMMER CONTROL CARDS DUE TO SIGNS OF OVERHEATING PER M/M 33-12-00. 2 L 7 4 4F A20WE 1998060500078 19980605 00078 NM 1998 6 5 P5CA9800779 1 19980520 A 5330 SKIN BOEING 747 747122 1384872 NM BS 820-840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 2 CORROSION AT UNDERSIDE OF ANTENNA 10 AFT OF CENTER ELECTRONICS BAY DOOR CUTOUT BS 820 TO 840 S47L TO S47R. REMO VED CORROSION REPLACED DOUBLER PER BOEING SRM 53-30-03. 2 L 7 4 4F A20WE 1998060500079 19980605 00079 NM 1998 6 5 P5CA9800780 1 19980520 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1780-1800 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT IN THE LOWER FUSELAGE AT BS 1780 TO 1800 S35R TO S36R. REPAIRED PER BOEING SRM 53-30-03 FIG 1. 2 L 7 4 4F A20WE 1998060500080 19980605 00080 NM 1998 6 5 P5CA9800781 1 19980520 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2598 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT AFT FUSELAGE SKIN AT PREVIOUS REPAIR FORWARD AND AFT OF BS 2598 JACK POINT. REPAIRED PER BOEING SRM 53-30-03 FIG 1 A. 2 L 7 4 4F A20WE 1998060500081 19980605 00081 NM 1998 6 5 P5CA9800782 1 19980520 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 2 CORROSION RIVET SHEARED AND SKIN BULGED AT BS 1000 AT S-42L. CORROSION REMOVED AND STRINGER REPAIRED PER BOEING SRM 53-10-03 FIG 1. 2 L 7 4 4F A20WE 1998060500082 19980605 00082 NM 1998 6 5 P5CA9800783 1 19980520 A 5240 SKIN BOEING 747 747122 1384872 NM SERVICE DOOR DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT ON UPPER DECK CREW SERVICE DOOR AFT EDGE MID PORTION. REPAIRED PER BOEING SRM 52-00-03 FIG 3. 2 L 7 4 4F A20WE 1998060500083 19980605 00083 NM 1998 6 5 P5CA9800784 1 19980520 A 5311 FRAME BOEING 747 747122 1384872 NM BS 380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED FRAME WEB AND DOUBLER AT BS 380 S-24L. REPAIRED PER BOEING TELEX PAO-HKG-98-106TE/0116RE AND HAECO REPAIR SCHEM E R-53-12-33742. 2 L 7 4 4F A20WE 1998060500084 19980605 00084 NM 1998 6 5 P5CA9800785 1 19980520 A 5311 FRAME BOEING 747 747122 1384872 NM BS 360 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED FRAME WEB BS 360 S-23L. REPAIRED PER BOEING TELEX PAO=HKG-98-0109RE/0099TE AND HAECO REPAIR SCHEME R-53-12-3372 4. 2 L 7 4 4F A20WE 1998060500085 19980605 00085 NM 1998 6 5 P5CA9800786 1 19980520 A 5320 STIFFENER BOEING 747 747122 1384872 NM BS 460 DEFORMED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DEFORMED UPPER DECK FLOORBEAM ATTACH VERTICAL STIFFENERS AT BS 460 RBL 55 AND RBL 74. REPLACED STIFFENERS PER BOEING SR M 51-10-01. 2 L 7 4 4F A20WE 1998060500086 19980605 00086 NM 1998 6 5 P5CA9800787 1 19980520 A 5320 WEB BOEING 747 747122 1384872 NM BS 360-380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 MAIN DECK BS 360 TO 380 RT WEB FOUND CRACKED AT S-32R. WEB REPAIRED PER BOEING SRM 51-40-01. 2 L 7 4 4F A20WE 1998060500087 19980605 00087 NM 1998 6 5 P5CA9800788 1 19980520 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 380-400 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED STRINGER S-24L AT BS 380 TO 400. REPLACED STRINGER PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1998060500088 19980605 00088 NM 1998 6 5 P5CA9800789 1 19980520 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1375 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED FRAME WEB AT LEFT WING LANDING GEAR WHEEL WELL BS 1375 S-32L. REPAIRED PER BOEING TELEX PAO-HKG-98-0091TE/0108R E AND HAECO REPAIR SCHEME R-53-42-33743. 2 L 7 4 4F A20WE 1998060500089 19980605 00089 NM 1998 6 5 P5CA9800790 1 19980520 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION LEFT WING LOWER SKIN AT NR 1 MAIN FUEL TANK INBOARD BOOST PUMP. REMOVED CORROSION AND SHOT PEENED INS TALLED A SEALANT RAMP PER BOEING TELEX PAO-HKG-98-0093TE AND HAECO REPAIR SCHEME R-57-26-33741. 2 L 7 4 4F A20WE 1998060500090 19980605 00090 NM 1998 6 5 P5CA9800791 1 19980520 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 2 CORROSION LEFT WING LEADING EDGE SKIN PANEL AT FSSO 1486. REPAIRED PER BOEING SRM 57-30-03 FIG 4. 2 L 7 4 4F A20WE 1998060500091 19980605 00091 NM 1998 6 5 P5CA9800792 1 19980520 A 5411 FRAME BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 PYLON RIGHT FRAME AT NAC STN 168 CRACKED AND LEFT FRAME AT NAC STN 193 FOUND CHAFED. REPLACED FRAMES PER BOEING SR M 51-10-01. 2 L 7 4 4F A20WE 1998060500092 19980605 00092 NM 1998 6 5 P5CA9800793 1 19980520 A 5414 SKIN BOEING 747 747122 1384872 NM NR 1 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 PYLON LEFT OUTER SKIN AT NAC STN 220 AND RT SKIN AT STN 233 FOUND DAMAGED. REPAIRED PER BOEING SRM 54-30-03. 2 L 7 4 4F A20WE 1998060500093 19980605 00093 NM 1998 6 5 P5CA9800794 1 19980520 A 7120 MOUNT BOEING 747 747122 1384872 NM NR 1 ENGINE WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 ENGINE FORWARD UPPER ENGINE MOUNT INBOARD HANGER FITTING INNERMOST LUG WAS PREVIOUSLY REWORKED AND BUSHIN MIGRATED OUT. SPOT FACED THE LUG, SHOT PEENED THE REWORKED SURFACE, REWORKED THE BUSHING AND INSTALLED WITH NEW WASHER PER BOEIN G TELEX PAO-HKG-98-0121RE/0105TE AND HAECO REPAIR SCHEME R-53-13-33725. 2 L 7 4 4F A20WE 1998060500094 19980605 00094 NM 1998 6 5 P5CA9800795 1 19980520 A 7810 CASE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 1 ENG EXH CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 662276 NR 1 ENGINE TURBINE EXHAUST CASE CRACKED, FLANGE AT 10 O'CLOCK POSITION. REPLACED CASE PER P AND W OVERHAUL MANUAL 72-0 0-00. 2 L 7 4 4F 4 F A20WE E20EA 1998060500096 19980605 00096 EA 1998 6 5 CA980210013 1 19980130 A 7603 87620130101 SHAFT 87620128001 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENG BROKEN W A E ENGINE SHUTDOWN O OTHER IN INSP/MAINT 1 CA 123028 (CAN) DURING A POWER RUN UP WITH CONDITION LEVERS AT MAXIMUM AND POWER LEVERS ADVANCED TO APPROXIMATELY 80 PERCENT TORQU E, THE NR 2 CONDITION LEVER SUDDENLY MOVED BY ITSELF TO MINIMUM SETTING. ATTEMPT TO FEATHER PROP USING CONDITION LEVER WAS UNSATISFACTORY. ENGINE SHUTDOWN USING THE PULL FUEL OFF HANDLE. INVESTIGATION REVEALED THE BROKEN SHAFT ON THE SPR ING STRUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1998060500097 19980605 00097 SW 1998 6 5 CA980302007 1 19980222 A 2697 WIRE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP DETECTOR DAMAGED W A E L UNSCHED LANDING ENGINE SHUTDOWN ABORTED APPROACH J N WARNING INDICATION FALSE WARNING AP APPROACH 1 CA 33574 P54082 (CAN) ON APPROACH, THE RIGHT HAND ENGINE FIRE LIGHT ILLUMINATED BRIEFLY FOR 1 TO 2 SECONDS - THREE DIFFERENT TIMES. THEN IT CAME ON STEADY. RH ENGINE SHUTDOWN. APPROACH ABORTED. POWER WIRE FOUND DAMAGED AT THE FIRE DETECTOR BY THE OIL COOLE R. PART TOTAL CYCLES, 53,047. 2 L 7 2 4T 4 T RT A8SW E4WE 1998060500099 19980605 00099 SW 1998 6 5 CA980430011 1 19980422 A 5311 2722019007 FRAME SWRNGN SA226 SA226TC 8780404 SW STA 272.271 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 26289 (CAN) DURING FRAME REMOVAL FOR WEB CRACK REPAIR, THE LEFT FRAME AT NR 11 STRINGER POSITION WAS FOUND CRACKED. CRACK RUN NING FROM STRINGER CUT TO EDGE OF FRAME. THIS AREA NOT ADDRESSED IN AIRFRAME INSPECTION MANUAL. PART TC: 39,582. 2 L 7 2 4T RT A8SW 1998060500105 19980605 00105 NM 1998 6 5 CA980504025 1 19980426 A 2730 ELEVATOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CONTROLS JAMMED W A A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 18457 120387 (CAN) ON CLIMB, CREW NOTICED THE ELEVATOR CONTROLS WERE JAMMED. ELEVATOR DISCONNECT DID NOT WORK. ELEVATOR JAMMED ON B OTH SIDES. FULL NOSE DOWN TRIM NECESSARY TO MAINTAIN LEVEL FLIGHT AT 160 KNOTS. AT 14,000 FEET, CREW ABLE TO MAINTAIN LEVEL FLIGHT. AIRCRAFT RETURNED USING TRIM. ABOUT ONE MINUTE AFTER LANDING, THE ELEVATOR CONTROLS WERE BACK TO NORMAL. WEATHER WAS PLUS 1 CELSIUS WITH MELTING SNOW AND RAIN. NO DEICING HAD BEEN APPLIED. FOLLOW-UP SDR INDICATED COMPLETE ELEVATOR SYST CHECKED AND ELEV SYSTEM CONSIDERED FULLY OPERATIONAL. SOME ROUGH PAINT ON ELEV LEADING EDGE. PAINT SAN DED TO SMOOTH SURFACE AND ALL COMPANY AIRCRAFT CHECKED FOR SAME THING. CONCLUSION IS THAT ICE FORMED ON ELEV. PART TC: 2 H 7 2 4T 4 T RT A13NM E20NE 1998060500107 19980605 00107 WP 1998 6 5 VJ9800157 1 19980528 A 2560 5928730503 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE FELL OFF A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 915VV 47443 DOOR SLIDE (GALLEY) ACCIDENTALLY CAME OUT OF THE COVER. SLIDE DID NOT DEPLOY. INSTALLED SLIDE COVER IAW 25-61 / SP 810 0. 2 L 7 2 4F A6WE 1998060500108 19980605 00108 NM 1998 6 5 9809376626 1 19980526 A 3231 SENSORS BOEING 747 747251B 1384892 NM NLG DOOR DIRTY A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 626US 21708 DURING CLIMB, THE NOSE LANDING GEAR DOOR DID NOT CLOSE AFTER LANDING GEAR RETRACTION. RECYCLED THE LANDING GEAR AND THE DOOR CLOSED. AIRCRAFT CONTINUED TO LAX AND LANDED WITHOUT INCIDENT. CLEANED THE NOSE LANDING GEAR DOOR SENSORS, OPERA TIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998060500109 19980605 00109 WP 1998 6 5 9809381233 1 19980526 A 5241 DOOR DOUG DC10 DC1030 3023501 WP GALLEY AIR LEAK A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 233NW 46640 DURING CLIMB, DOOR 2R WAS LEAKING WITH A GAP VISIBLE AT TOP OF DOOR. FLIGHT RETURNED TO MSP WITHOUT FURTHER INCIDENT. M AINTENANCE FOUND DOOR PARTIALLY OPEN. CYCLED DOOR CLOSED AND RETURNED AIRCRAFT TO SERVICE. 2 L 7 3 4F A22WE 1998060500110 19980605 00110 WP 1998 6 5 9809399918 1 19980526 A 2150 ACM DOUG DC9 DC932 3022066 WP RIGHT FAILED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 GL 01 940N 47572 BOTH AFT LAVATORY SMOKE ALARMS ACTIVATED AFTER TAKEOFF. FLIGHT ATTENDANT REPORTED AN ELECTRICAL TYPE SMELL IN AFT CABIN . FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH HEAT EXCHANGERS AND RIGHT AIR CYCL E MACHINE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998060500111 19980605 00111 1998 6 5 9809405639 4 19980521 A 2330 1142400130 SEAT BOX BOEING 757 757251 1384970 NM CABIN FAILED A NWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 GL 01 539US 26486 DURING APPROACH, SMOKE ACCUMULATED FROM SEAT BOX UNDER SEAT 32B. FLIGHT CREW DECLARED EMERGENCY AND RAISED CABIN ALTITU DE TO AID IN SMOKE REMOVAL. AIRCRAFT LANDED, TAXIED TO GATE, AND DEPARTED PASSENGERS WITHOUT INCIDENT. MAINTENANCE REP LACED SEAT BOX, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1998060500112 19980605 00112 EU 1998 6 5 QXEA9800678 1 19980526 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 CEILING EMERGENCY LIGHT OUT AT ROW 13. MAINTENANCE RELAMPED AND TESTED, OPERATION IS NORMAL. 2 L 7 2 4F RT A20EU 1998060500113 19980605 00113 EU 1998 6 5 QXEA9800679 1 19980527 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 SEVERAL 28V AISLE EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, OPERATION IS NORMAL. 2 L 7 2 4F RT A20EU 1998060500114 19980605 00114 EU 1998 6 5 QXEA9800680 1 19980527 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 483US 11233 THE 28V ENTRANCE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, OPERATION IS NORMAL. 2 L 7 2 4F RT A20EU 1998060500115 19980605 00115 EU 1998 6 5 QXEA9800681 1 19980526 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 AISLE EVACUATION LIGHT AT SEAT 6 IS INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, OPERATION IS NORMAL. 2 L 7 2 4F RT A20EU 1998060500116 19980605 00116 EU 1998 6 5 QXEA9800682 1 19980526 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 FORWARD AND AFT CABIN CEILING EMERGENCY EXIT SIGNS HAVE BULBS OUT. MAINTENANCE RELAMPED AND TESTED, OPERATION IS NORMAL . 2 L 7 2 4F RT A20EU 1998060500117 19980605 00117 NM 1998 6 5 QXEA9800683 1 19980527 A 3350 1013079 BULBS GRIMES 82520977001 DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 829PH 304 NUMEROUS BULBS OUT IN THE FLOOR PROX LIGHT STRIPS, AND THE AFT EMERGENCY EXIT SIGN IS INOP. RELAMPED FLOOR PROX STRIPS, AND RECONNECTED RIGHT AFT EMERGENCY EXIT SIGN, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998060500118 19980605 00118 WP 1998 6 5 RRXA98218 1 19980504 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 487-490 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FUSELAGE SKIN AT STA 487 TO STA 490 AND LONGERON 29 RIGHT. REMOVE D DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNE Y ENGINEERING SKETCH E54-R01. 2 L 7 4 4F 4A25 1998060500119 19980605 00119 WP 1998 6 5 RRXA98219 1 19980504 A 5320 4611067 FITTING DOUG DC8 DC862 3021970 WP BS 270 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME FITTING AT STA 270 AND LONGERON 33 RIGHT. REMOVED DAMAGED F ITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E54-R02. 2 L 7 4 4F 4A25 1998060500120 19980605 00120 WP 1998 6 5 UPS98826818 1 19980515 A 5320 9755536501 FITTING DOUG DC8 DC873F 302199F WP BS 1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, FRAME FITTING JUST UNDER LT CUSP CRACKED AT FS 1280. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998060500121 19980605 00121 WP 1998 6 5 UPS98826819 1 19980513 A 5744 5751189506 FITTING DOUG DC8 DC873F 302199F WP WS 409 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, THE RT WING FLAP HINGE SUPPORT FITTING AT STA XF 409.6673, INBOARD SIDE HAS A CRACK. REMOVED AND REP LACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998060500122 19980605 00122 WP 1998 6 5 UPS98826820 1 19980514 A 5744 745493711 FITTING DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 874UP 46074 INSPECTION TYPE-C, LT WING NR 4 FLAP HINGE ACTUATOR MOUNT FITTING IS CRACKED. REMOVED AND REPLACED CANOE FITTING IAW MM 27-51-00. 2 L 7 4 4F RT 4A25 1998060500123 19980605 00123 WP 1998 6 5 UPS98826821 1 19980512 A 5320 47518202 FITTING DOUG DC8 DC873F 302199F WP BS 702 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE-C, RT UPPER CABIN WING BOX AREA AT FS 702.8 RBL 25 FLOORBEAM SPLICE FITTING IS CRACKED. REMOVED AND REP LACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998060500124 19980605 00124 NE 1998 6 5 ABXA9800470 2 19980527 A 7200 ENGINE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 FAILED A ABXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 849AX 45891 669379 LOST OIL PRESSURE AND QUANTITY DURING FLIGHT. ENGINE WAS SHUT DOWN. OIL PRESSURE WAS 3 PSI DURING WINDMILLING. REMOVE D AND REPLACED NR 2 ENGINE. 2 L 7 4 4F 4 F 4A25 1E8 1998060500125 19980605 00125 1998 6 5 P5CA9800796 4 19980528 A 3417 19039253 CADC BOEING 747 747249F 1384849 NM COCKPIT MALFUNCTIONED A P5CA K NONE O OTHER CR CRUISE 1 WP 23 920FT 22237 A 400 FT SPLIT IN ALTIMETERS AT 39,000 FT. REPLACED NR 1 CENTRAL AIR DATA COMPUTER PER M/M 34-11-00. 2 L 7 4 4F A20WE 1998060500126 19980605 00126 NE 1998 6 5 P5CA9800797 2 19980528 A 7260 24101K SEAL BOEING 747 747122 1384872 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE LEAKING A P5CA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 854FT 19754 663042 NR 4 ENGINE LOST OIL QTY AND PRESSURE. OIL PRESSURE LIGHT CAME ON AND TEMP BEGAN TO RISE. ENGINE SHUT DOWN. FOUND OIL LEAK TO BE FROM CSD PAD. REPLACED CSD SEAL PER BOEING M/M 24-11-01, LEAK CHECK OK. 2 L 7 4 4F 4 F A20WE E20EA 1998060500127 19980605 00127 WP 1998 6 5 VJ9800158 1 19980106 A 5730 PANEL DOUG DC9 DC932 3022066 WP WS 50 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 915VV 47443 DURING C-CHECK, FOUND LT WING STA 50 ABOVE HYD GROUND SERVICE ACCESS PANEL, LOWER SKIN PANEL CHAFED THROUGH AND MISSING FASTENER. REMOVED PANEL AND REPAIRED PANEL IAW EO 98-759 AERO NR 2024 TREATED AND PRIMED IAW DC-9 SRM 51-10-3. REINSTA LLED PANEL IAW DC-9 51-30-1. 2 L 7 2 4F A6WE 1998060500128 19980605 00128 WP 1998 6 5 VJ9800159 1 19980427 A 5315 1A3336333364 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 DURING C-CHECK, FOUND CORROSION ON STA 996 FLOORBEAM RT BL 44 UNDER NUT PLATE. REMOVED CORRODED SECTION OF THE BEAM, FA BBED NEW SECTION FROM 60-15273 EXTRUSION 1 BY 40 BY 1 DRILLED DEBURRES, TREATED AND PRIMED IAW DC-9 SRM 51-10-4, 51-10- 3 AND EO 98=863, INSTALLED NEW BEAM SECTION IAW DC-9 SRM 51-10-01 AND 51-10-2. 2 L 7 2 4F A6WE 1998060500129 19980605 00129 WP 1998 6 5 VJ9800160 1 19980507 A 5320 26524791A33140 SUPPORT DOUG DC9 DC932 3022066 WP BS 167-198 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 CABIN STA Y-167-198, -X=44, FLOOR SUPPORT UPPER SURFACE HAS CORROSION. REMOVED CORROSION FROM STA 167-198 FLOOR SUPPORT GROUND BEYOND LIMITS. REMOVED FLOOR SUPPORT, FABBED NEW FLOOR SUPPORT P/N 2652479 2 BY 38, DRILLED TRIM TO FIT. TREAT ED AND PRIMED IAW DC-9 SRM 51-10-3, 53-01 FIG SRM 51-30-4, (DIAL CALIPER 3268-1) SRM 53-11-1 FIG 13. 2 L 7 2 4F A6WE 1998060500130 19980605 00130 WP 1998 6 5 VJ9800161 1 19980427 A 5330 1A33157 SKIN DOUG DC9 DC932 3022066 WP BS 639 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 DURING ACCOMPLISHMENT OF AD 88-24-08 INSPECTION PER EO-12-5330-29-B1058I/R, HFEC INDICATES EXTERNAL FUSELAGE SKIN CRACK .100 AT COUNTERSINK FASTENER HOLE CONDTO FS 639 RT LONGERON 5 LOWER SHEAR TIE. REMOVED 1 FASTENER, NDT VERIFIED CRACK I N SKIN AT COUNTERSINK. CUT OUT 21/8 SKIN WERE CRACK WAS FOUND. FABBED FINGER DOUBLER REPAIR OUT OF MIL T 90641H .032 P /N 1A-33157-1. FABBED, TREATED AND PRIMED FILLER ON THE AC FS 639 RT 5 IAW DC-9 SRM 51-10-3, 51-30-2, 53-04 FIG 38, 51- 10-4, EO 12-5330-29-BI058 I/R. 2 L 7 2 4F A6WE 1998060500131 19980605 00131 WP 1998 6 5 VJ9800162 1 19980428 A 5330 1A32453331661 SKIN DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 DURING THE ACCOMPLISHMENT OF AD 88-24-08 INSP PER EO 12-5330-29-B1058 I/R, HFEC INDICATES EXTERNAL FUSELAGE SKIN CRACKED AT FS 617 RT LONG 1 SHEAR TIE. REMOVED 1 FASTENER IAW DC-9 SRM 51-30-2 HFEC VERIFIED CRACK IN SKIN AT COUNTERSINK IAW DC-9 STD PRACTICE PTC. REMOVED FASTENER CUT OUT 2.5 HOLE AT CRACK AREA IAW DC-9 SRM 53-04 FIG 38. FABBED REPAIR FINGER DOUBLER EXTERIOR DOUBLER AND SKIN FILLER IAW DC-9 SRM 51-10-3 6.98 BY 761 FINGER DOUBLER SKIN FILLER 2.65, EXTERIOR DOU BLER 8.58 BY 6.14. 2 L 7 2 4F A6WE 1998060500132 19980605 00132 WP 1998 6 5 VJ9800163 1 19980423 A 5320 1A331471 SUPPORT DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 CABIN STA 218 FLOOR SUPPORT HAS CORROSION AT FASTENER HOLE. REMOVED CORROSION IAW DC-9 SRM 51-10-3, MATERIAL LOSS 50 PER CENT OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1 GAUGE NR 4782-01. FABBED REPAIR FLOOR SUPPORT OUT OF 7075 T6 511 ANGLE 18 X 2 IAW DC-9 SRM 51-10-2, TREATED AND PRIMED IAW DC-9 51-10-3. INSTALLED REPAIR IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998060500133 19980605 00133 WP 1998 6 5 VJ9800165 1 19980422 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1059 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 INSTALLED PERMANENT REPAIR TO RT FUSELAGE FRAME STA PER DACO LETTER 97-01-012. FABRICATED FRAME FROM 7075 O .050 19 BY 1 AND 24 BY 1. FABRICATED SPLICE REPAIR FROM 7075 0 .063 12 BY 1 (2 EACH) AND 11 BY 2. INSTALLED REPAIR PARTS IAW DC-9 SRM 53-03 FIG 32, 51-30-1, 51-30-2, 51-30-4, AND DACO LETTER 97-01-16-012 AMD NDC LETTER 96-09-19-011. 2 L 7 2 4F A6WE 1998060500134 19980605 00134 NM 1998 6 5 MALA976132 1 19980520 A 7810 SEAL DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE FAILED A MALA O OTHER A FLAME/FIRE LD LANDING 1 GL 15 826MA 330 AFTER LANDING WHEN TAXIING CLEAR OF RUNWAY HAD FIRE ON NR 2 ENGINE, SHUT DOWN BOTH ENGINES, DID NOT BLOW BOTTLES. FIRE WENT OUT ON ITS OWN. MAINTENCE FOUND EVIDENCE OF EXHAUST LEAKAGE ON SHROUD IN RIGHT NACELLE, REPLACED SEAL ON SHROUD AN D REINSTALLED SHROUD. GROUND RAN AIRCRAFT AT HIGH POWER SETTINGS, NO DEFECTS NOTED. 2 H 7 2 4T RT A13NM 1998060500135 19980605 00135 EU 1998 6 5 MALA976133 1 19980524 A 3234 D49412001 HANDLE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 418XJ 418 ON APPROACH, UPON SELECTING THE LANDING GEAR HANDLE DOWN, THE HYDRAULIC PUMP RAN AS NORMAL BUT THE GEAR DID NOT CHANGE P OSITION. THE HYDRAULIC CONTROL BREAKER F-7 WAS TRIPPED, WHEN RESET AND PROCEDURE REPEATED IT TRIPPED AGAIN. WITH BREAK ER STILL TRIPPED, GEAR HANDLE WAS SELECTED DOWN THEN BREAKER F-7 WAS CLOSED AND GEAR CAME DOWN NORMALLY AND BREAKER DID NOT TRIP. MAINTENANCE REPLACED LANDING GEAR CONTROL HANDLE. SECURITY AND OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998060500136 19980605 00136 EU 1998 6 5 MALA976134 1 19980520 A 2560 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR MALFUNCTIONED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 502XJ E2307 WHEN OPENING THE PASSENGER DOOR THE EMERGENCY SLIDE FELL OUT OF THE CASE, IT DID NOT DEPLOY, GIRT BAR WAS DISENGAGED PRI OR TO OPENING. MAINTENANCE REPLACED SLIDE ASSEMBLY. SECURITY CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998060500137 19980605 00137 EU 1998 6 5 MALA976135 1 19980525 A 3233 AIR86A101 ACTUATOR SAAB SF340 SF340A 7850100 EU RT MLG FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 110XJ 340A110 ON LANDING WHEN LANDING GEAR WAS EXTENDED FOR LANDING THE HYDRAULIC LIGHT WENT ON AND 2 GREEN LIGHTS CAME ON. QRH PROCE DURES USED TO EXTEND GEAR. LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. A LL IAW SAAB AMM CH 32. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998060500138 19980605 00138 1998 6 5 MALA976136 2 19980524 A 7261 CHIP LIGHT SAAB SF340 SF340A 7850100 EU LT ENGINE ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 79XJ 079 AFTER TAKEOFF, THE LEFT CHIP DETECTOR LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE INSPECTED DEBRIS IN ACC ORDANCE WITH GE 72-00-00, PAGE 198.17, TROUBLE 10 AND FOUND ACCEPTABLE FOR CONTINUED SERVICE. SENT CHIPS IN FOR ANALYSI S. 2 L 7 2 4T RT A52EU 1998060500139 19980605 00139 1998 6 5 MALA976137 4 19980528 A 3425 6226190113 AHRS COMPUTER SAAB SF340 SF340A 7850100 EU RT COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 79XJ 079 DURING FLIGHT CREW RESET HEADING SEVERAL TIMES, YELLOW HAEDING LIGHT REMAINED ON WITH 8 DEGREES DIFFERENCE IN HEADINGS. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE NR 2 AHRS COMPUTER. SYSTEM OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998060500140 19980605 00140 NM 1998 6 5 M8XA9800009 1 19980526 A 2120 AIR DISTR DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE CABIN ODOR A M8XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 NM 03 336PH 3014 CREW REPORTED RECEIVING AN EICAS. LEFT PACK FAIL MESSAGE DURING TAXI. PILOT CYCLED THE LT PACK SWITCH,THE FAIL MESSAGE THEN CLEARED ITSELF. FAIL MESSAGE ILLUMINATED AGAIN AFTER T/O. THIS WAS ACCOMPANIED WITH AN AMBER LAV SMOKE EICAS. CR EW REPORTED, NO EVIDENCE OF SMOKE OR FIRE COMING FROM THE LAV. JUST A SMELL OF FUMES. A/C RETURNED TO DENVER WITH NO F URTHER INCIDENTS. MX GROUND RAN THE A/C AND PERFORMED AN OP'S CHECK OF THE AIR CONDITIONING SYSTEM IAW AMM 21-21-00, NO DEFECTS NOTED. THE A/C WAS THEN RELEASED FOR SERV. THE CREW LATER REPORTED THAT THEY HAD AN EXTENDED TAXI PERIOD WITH THE ENGS IN GROUND IDLE AND A 12 KNOT TAIL WIND. SUBMITTER STATES, WE CAN ONLY SURMIZE THAT THE HEAVY TAIL WIND AND LO 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998060500141 19980605 00141 NM 1998 6 5 SWAA980875 1 19980518 A 2781 LIGHT BOEING 737 7372H4 138448C NM LE FLAP ILLUMINATED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 057SW 21722 IN FLIGHT, NR 4 L/E FLAP LIGHT ILLUMINATED. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. REPLACED DOWN PRO X SENSOR PER BOEING MM. 2 L 7 2 4F A16WE 1998060500142 19980605 00142 NM 1998 6 5 SWAA980876 1 19980518 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 747/757-870 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FLOORBEAM UNDER CARGO NET TIEDOWN LUG AT BS 747, RBL 14; AND BS 757 TO 870, R BL 14. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500143 19980605 00143 NM 1998 6 5 SWAA980877 1 19980518 A 5400 DOUBLER BOEING 737 7373H4 1384600 NM NR 2 PYLON DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND DAMAGED DOUBLER ON THE NR 2 0/B PYLON SKIN AT THE WING LEADING EDGE INTERFACE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500144 19980605 00144 NM 1998 6 5 SWAA980878 1 19980518 A 5400 DOUBLER BOEING 737 7373H4 1384600 NM NR 2 PYLON DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND DAMAGED DOUBLER ON THE NR 2 0/B PYLON SKIN AT THE WING LEADING EDGE INTERFACE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500145 19980605 00145 NM 1998 6 5 SWAA980879 1 19980518 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 276 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED TOP FRAME AT BS 276, WL 167, LBL 28 TO 31. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500146 19980605 00146 NM 1998 6 5 SWAA980880 1 19980518 A 5755 BRACKET BOEING 737 7373H4 1384600 NM NR 4 SPOILER CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND UPON PANEL REMOVAL FOUND BROKEN L BRACKET ON T/E FIXED PANEL O/B OF NR 4 SPOILER. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500147 19980605 00147 NM 1998 6 5 SWAA980881 1 19980518 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED AFT CARGO DOOR HOLD OPEN LATCH INTERCOSTAL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500148 19980605 00148 NM 1998 6 5 SWAA980882 1 19980518 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986.5 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND DAMAGED INTERCOSTAL AT BS 986.5, STR 20L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500149 19980605 00149 NM 1998 6 5 SWAA980883 1 19980518 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 729 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CORRODED VERTICAL STIFFENER AT BS 729, RBL 14, WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500150 19980605 00150 NM 1998 6 5 SWAA980884 1 19980518 A 5414 PANEL BOEING 737 7373H4 1384600 NM LT PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND CRACKED LT PYLON INBOARD SIDE, AT PANEL 5742, DOUBLER AT AFT EDGE OF PANEL CUTOUT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500151 19980605 00151 NM 1998 6 5 SWAA980885 1 19980518 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND NUMEROUS SKIN DENTS AT BS 500+10- 500A BETWEEN STR 21 AND 22 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500152 19980605 00152 NM 1998 6 5 SWAA980886 1 19980518 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND CRACKED BS 178 PRESSURE BULKHEAD WEB AT LBL 4.7, WL 201.25 - 200.25 AND WL 198.7 - 197.5. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500153 19980605 00153 NM 1998 6 5 SWAA980887 1 19980518 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 669 DRILLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND HORIZONTAL PRESSURE WEB HAS DRILL START ON LOWER SURFACE AT BS 669, LBL 23 AT MLG WHEEL WELL . REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500154 19980605 00154 NM 1998 6 5 SWAA980888 1 19980518 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND CORRODED FLOORBEAM AT BS 328, RBL 12-40, WL 207-208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500155 19980605 00155 NM 1998 6 5 SWAA980889 1 19980518 A 5753 WEDGE BOEING 737 7373H4 1384600 NM RT TE MIDFLAP GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND GOUGED R/W I/B MIDFLAP T/E WEDGE LOWER SURFACE AT I/B T/E CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500156 19980605 00156 NM 1998 6 5 SWAA980890 1 19980519 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 485 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED SERVICE CHECK, FOUND DAMAGED CLOSURE WEB EDGE AT BS 485 ABOVE STR 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500157 19980605 00157 NM 1998 6 5 SWAA980891 1 19980519 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY LIGHTS CAME ON WHEN A/C POWER IS LEFT IN OFF. REPLACED LT O VERWING ESCAPE SLIDE LIGHTS BATTERY PACK BASE PER BOEING MM. OPS CHK GOOD. 2 L 7 2 4F A16WE 1998060500158 19980605 00158 NM 1998 6 5 SWAA980892 1 19980519 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BAGGAGE COMPT LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND UPLATCH HOLDER FOR REAR B/BIN DOOR LOOSE WITH INTERCOSTAL MOVING. REMOVED AND REPLAC ED INTERCOSTAL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500159 19980605 00159 NM 1998 6 5 SWAA980893 1 19980519 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND EGRESS EMERGENCY LIGHT IN BULLNOSE AT 5 DEF COMING LOOSE AND IMPROPERLY INSTALLED. R EINSTALLED LIGHT AND LENS AS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998060500160 19980605 00160 NM 1998 6 5 SWAA980894 1 19980519 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 947-993 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT Z ANGLE AT BS 947 - 993, RBL 50. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500161 19980605 00161 NM 1998 6 5 SWAA980895 1 19980519 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 727- 767. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500162 19980605 00162 NM 1998 6 5 SWAA980896 1 19980520 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTS INOP IN LEFT HAND EMERGENCY EXIT LOCATION. RECONNECTED BROKEN WIRE PER BOEING MM. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1998060500163 19980605 00163 NM 1998 6 5 SWAA980897 1 19980519 A 5512 SKIN BOEING 737 7372H4 138448C NM HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22643 DURING SERVICE CHECK, FOUND 2.5 BY 2.0 BY .218 DENTED HORIZONTAL STABILIZER L/E 24 O/B OF FUSELAGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998060500164 19980605 00164 NM 1998 6 5 SWAA980898 1 19980519 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1017 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND CRACKED WEB AT BS 1017, LBL 9, WL 208 DRAIN HOLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500165 19980605 00165 NM 1998 6 5 SWAA980899 1 19980519 A 5320 DOOR POST BOEING 737 7373H4 1384600 NM BS 286 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND FWD DOOR POST CRACKED AT FLOOR LEVEL BS 286. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500166 19980605 00166 NM 1998 6 5 SWAA980900 1 19980520 A 5210 WEB BOEING 737 7373H4 1384600 NM PAX DOOR CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR UPPER TORQUE TUBE BOLT IS CHAFFING WEB. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998060500167 19980605 00167 NM 1998 6 5 SWAA980901 1 19980520 A 5330 PANEL BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED PANEL UPPER WING SURFACE AT END OF ENG PYLON PANELS. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500168 19980605 00168 NM 1998 6 5 SWAA980902 1 19980520 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL FWD SIDE AND AFT SIDE AT BS 540, RBL 1; AND AFT SIDE AT 540, LBL 1. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500169 19980605 00169 NM 1998 6 5 SWAA980903 1 19980520 A 5241 ANGLE BOEING 737 7373H4 1384600 NM GALLEY DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FWD SERVICE DOOR ENTRY Z ANGLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500170 19980605 00170 NM 1998 6 5 SWAA980904 1 19980520 A 5400 ANGLE BOEING 737 7373H4 1384600 NM NR 2 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND NR 2 PYLON I/B AND O/B ACCESS CUTOUT PANEL SUPPORT ANGLE CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500171 19980605 00171 NM 1998 6 5 SWAA980905 1 19980520 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT TE FOREFLAP GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND RIGHT WING INBOARD FOREFLAP HAS A GOUGE AT LOWER SURFACE NEXT TO BULL NOSE 49 FROM I/B END 1 2 FROM T/E. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500172 19980605 00172 NM 1998 6 5 SWAA980906 1 19980520 A 5753 SKIN BOEING 737 7373H4 1384600 NM LT TE FOREFLAP DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND LEFT O/B FOREFLAP 24.5 FROM I/B END DENTED AND PUNTURE ON LWR T/E SURFACE. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998060500173 19980605 00173 NM 1998 6 5 SWAA980907 1 19980520 A 5220 SEAL BOEING 737 7373G7 1384595 NM EMER EXIT DOOR COLLAPSED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND EMERGENCY EXIT DOOR HANDLE PRESSURE SEAL COLLAPSED LT. REMOVED AND INSTALLED NEW EMERGE NCY EXIT DOOR HANDLE PRESSURE SEAL PER BOEING MM. 2 L 7 2 4F RT A16WE 1998060500174 19980605 00174 NM 1998 6 5 SWAA980908 1 19980520 A 5320 CHANNEL BOEING 737 7373G7 1384595 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CORRODED CHANNEL AT BS 500-500A, LBL 25, WL 156; BS 500B-500C, RBL 25, WL 156; AND BS 50 0C-500D, RBL 25, WL156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500175 19980605 00175 NM 1998 6 5 SWAA980909 1 19980520 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 178, BL 0, WL 188-189. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500176 19980605 00176 NM 1998 6 5 SWAA980910 1 19980520 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9LT AND 8LT, AT BS 847; BS 8 27, STRINGERS 9LT AND 8LT; AND BS 767, STRINGERS 9LT AND 8LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500177 19980605 00177 NM 1998 6 5 SWAA980911 1 19980520 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 827/907/887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9RT AND 8RT, AT BS 827; BS 9 07, STRINGERS 9LT AND 8LT; AND BS 887, STRINGERS 9LT AND 8LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500178 19980605 00178 NM 1998 6 5 SWAA980912 1 19980520 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 867/787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9LT AND 8LT, AT BS 867; BS 7 87, STRINGERS 9RT AND 8RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500179 19980605 00179 NM 1998 6 5 SWAA980913 1 19980520 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER SPLICE AT BS 907, STR 4LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500180 19980605 00180 NM 1998 6 5 SWAA980914 1 19980520 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR WEB UPPER ATTACH L ANGLE AT BS 500D-11, WL 208, BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500181 19980605 00181 NM 1998 6 5 SWAA980915 1 19980520 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 294, RBL 39, 45 TO 52, WL 208 AND WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500182 19980605 00182 NM 1998 6 5 SWAA980916 1 19980520 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED FLOORBEAM STIFFENER AT BS 328, RBL 32, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500183 19980605 00183 NM 1998 6 5 SWAA980917 1 19980520 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 1006 DRILLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND HOLE DRILLED IN RADIUS OF FLOORBEAM AT BS 1006, WL 208, RBL 30. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998060500184 19980605 00184 NM 1998 6 5 SWAA980918 1 19980520 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AROUND NUTPLATE HOLES AT BS 947, WL 208, RBL 5 TO LBL 43. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500185 19980605 00185 NM 1998 6 5 SWAA980919 1 19980521 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL AT BS 380-400 C/L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500186 19980605 00186 NM 1998 6 5 SWAA980920 1 19980521 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM UNDER CARGO NET TIE DOWN LUG AT BS 747, RBL 14. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998060500187 19980605 00187 NM 1998 6 5 SWAA980921 1 19980521 A 5320 COVER BOEING 737 7373G7 1384595 NM BS 792-794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CORRODED DOOR FRAME COVER PLATE AT BS 792-794, RBL 41-48, WL 164-170. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998060500188 19980605 00188 NM 1998 6 5 SWAA980922 1 19980521 A 2781 CONNECTORS BOEING 737 7373G7 1384595 NM TE FLAPS LOOSE A SWAA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 683SW 24008 DURING APPROACH TO ABQ, L/E ANDT/E FLAPS FAILED TO EXTEND, ALT SYSTEM ACTIVATED, FLAPS POSITIONED TO 15 FOR LANDING. A/ C MADE AN UNEVENTFUL LANDING. CLEANED AND RESEATED CONNECTORS ON BOTH FLAP TRANSMITTERS, RUN FLAPS SEVERAL TIMES OPS NO RMALLY. REMOVED AND REPLACED OPC STYLUS PEN BATTERY, OPS CKS NORMAL. 2 L 7 2 4F RT A16WE 1998060500189 19980605 00189 NM 1998 6 5 SWAA980923 1 19980521 A 2910 HYD MODULE BOEING 737 7373Q8 1384670 NM RIGHT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 687SW 23388 WHEN RT PACK TURNED ON CABIN AND COCKPIT FILLED WITH SMOKE. SMOKE CONTINUED WITH APU BLEED ON OR OFF. APU INOP DUE TO OIL SMELL IN CABIN WITH PACKS ON. REMOVED AND REPLACED HYD PRESSURIZATION MODULE PER BOEING MM. REMOVED AND REPLACED W ATER SEPARATOR BAGS PER BOEING MM. LK AND CK GOOD . 2 L 7 2 4F RT A16WE 1998060500190 19980605 00190 NM 1998 6 5 SWAA980924 1 19980521 A 2560 1061323459 GIRT BAR BOEING 737 7375H4 138449D NM SERVICE DOOR WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING SCHEDULED BC4 CHECK, FOUND FWD SERVICE DOOR EMERGENCY SLIDE GIRT BAR MATERIAL WORN/FRAYED. REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY SLIDE AS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998060500191 19980605 00191 NM 1998 6 5 SWAA980925 1 19980524 A 2781 SENSOR BOEING 737 7373H4 1384600 NM NR 4 LE FLAP MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 333SW 23697 AFTER TAKEOFF WITH FLAP LEVER UP, HAD LE FLAPS TRANSIT LIGHT AND AN OVERHEAD INDICATIONS OF NR 4 KRUEGER FLAP EXTENDED. AIRCARAFT RETURN TO BHM AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED PROX SENSOR FOR NR 4 KRUEGER DOWN INDICAT ION PER BOEING MM. SYSTEM CHECKED OK, OPS NORMAL. 2 L 7 2 4F RT A16WE 1998060500192 19980605 00192 1998 6 5 SWAA980926 4 19980523 A 2210 65C370539 YAW DAMPER BOEING 737 7372H4 138448C NM E/E COMPT FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 CLIMBING OUT OF FL250, AIRCRAFT FISHTAILED LEFT AND RIGHT FOR 3 COMPLETE CYCLES. OSCILLATIONS CEASED WHEN YAW DAMPER TU RNED OFF. NO FURTHER PROBLEMS. REMOVED AND REPLACED YAW DAMPER COUPLER AND RUDDER PCU PER BOEING MM. OPS AND LEAKS CK NORMAL. 2 L 7 2 4F A16WE 1998060500193 19980605 00193 NM 1998 6 5 SWAA980927 1 19980523 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING WALKAROUND CHECK, FOUND APPROX 4 SKIN CRACK RT SIDE ABOVE PASSENGER WINDOW NR 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500194 19980605 00194 NM 1998 6 5 SWAA980928 1 19980523 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED RON CHECK, FOUND RT OVER EMERGENCY EXIT DOOR INNER AND LT EXIT OVER WING EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998060500195 19980605 00195 NM 1998 6 5 SWAA980929 1 19980523 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 367 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED 2 1/4 FUSELAGE SKIN FWD OF EQUIPMENT COOLING DUCT AT BS 367. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500196 19980605 00196 NM 1998 6 5 SWAA980930 1 19980523 A 5314 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4 D CHECK, FOUND CRACKED KEELBEAM SKIN AT BS 663. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500197 19980605 00197 NM 1998 6 5 SWAA980931 1 19980523 A 5330 SKIN BOEING 737 7373H4 1384600 NM CARGO DOORWAY PUNCTURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 618SW 28034 DURING SCHEDULED C3 CHECK, FOUND AFT CARGO COMPARTMENT DOOR FRAME FWD WEB SKIN HAS 1.0 PUNCTURE. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998060500198 19980605 00198 NM 1998 6 5 SWAA980932 1 19980523 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 890 -945 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CHAFFED AT BS 890 TO BS 945, RBL 4.5-9.5, WL 306.5. REPAIRED PER TRAMCO E O NR 98-0409. 2 L 7 2 4F RT A16WE 1998060500199 19980605 00199 NM 1998 6 5 SWAA980933 1 19980523 A 5320 CHORD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED CHECK, FOUND CRACKED SIDE CHORD AT BS 178, RBL 29 WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500200 19980605 00200 NM 1998 6 5 SWAA980934 1 19980523 A 5320 DORSAL FIN BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND DAMAGED DORSAL FIN OK TO CORE SPLICE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500201 19980605 00201 NM 1998 6 5 SWAA980935 1 19980523 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721SW 22697 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY LIGHT ON FLOOR INOP AT 14D. REPLACED LAMP AT 14D, OPS CK LAMPS PER BOEING MM . 2 L 7 2 4F A16WE 1998060500202 19980605 00202 NM 1998 6 5 SWAA980936 1 19980523 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CRACKED INDICATIONS NOTED AT BS 178 BULKHEAD WEB AT WL 209.3 TO 212.7 LBL 6.7; AND BS 17 8 WL 212 TO 212.9 RBL 6.7. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500203 19980605 00203 NM 1998 6 5 SWAA980937 1 19980523 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CRACKED INDICATIONS NOTED AT BS 178 BULKHEAD WEB AT WL 209.7 TO 212.6 LBL 4.7; AND WL 20 9.5 TO 212.7 RBL 4.7. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500204 19980605 00204 NM 1998 6 5 SWAA980938 1 19980523 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 180 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 180 WL 208, RBL 24; BS 180, WL 208, LBL 24. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500205 19980605 00205 NM 1998 6 5 SWAA980939 1 19980523 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 986 RBL 26-BL 0 WL 208 AROUND FASTENER HOLES UPPER AND LOWER SI DE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500206 19980605 00206 NM 1998 6 5 SWAA980940 1 19980523 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AROUND NUTPLATE AT BS 986 RBL 43, WL 208. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998060500207 19980605 00207 NM 1998 6 5 SWAA980941 1 19980524 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 967 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 967 APROX 27 BELOW AFT ENTRY DOOR CUT OUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500208 19980605 00208 NM 1998 6 5 SWAA980942 1 19980524 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT TE FOREFLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED I/B FOREFLAP SKIN O/B OF TRACK. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500209 19980605 00209 NM 1998 6 5 SWAA980943 1 19980524 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTS ON FLOOR LOOSE AT ROW 9. SECURED EMERGENCY EXIT LIGHTS AT ROW 9 PE R BOEING MM. 2 L 7 2 4F RT A16WE 1998060500210 19980605 00210 NM 1998 6 5 SWAA980944 1 19980524 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SCHEDULED C2 CHECK, FOUND CRACKED FLOOR INTERCOSTAL AT BS 540 LEFT AND RIGHT OF CENTER. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500211 19980605 00211 NM 1998 6 5 SWAA980945 1 19980524 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 947, STR 24 RT WL 160. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500212 19980605 00212 NM 1998 6 5 SWAA980946 1 19980524 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 727 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND WORN T-ANGLE AT BS 727 TO 727B, STR 20 LT AND BS 727, STR 20 RT. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500213 19980605 00213 NM 1998 6 5 SWAA980947 1 19980524 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND DAMAGED SKIN AT BS 500 + 19, RBL 1, WL 148. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500214 19980605 00214 NM 1998 6 5 SWAA980948 1 19980524 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL AT BS 500A-500B, RBL 25 WL 156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500215 19980605 00215 NM 1998 6 5 SWAA980949 1 19980525 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 310SW 22949 DURING SERVICE CHECK, FOUND 2 CRACK IN SKIN AT STRINGER 17, 4 AFT AT BS 727C. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500216 19980605 00216 NM 1998 6 5 SWAA980950 1 19980525 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND DENTED FUSELAGE SKIN, AT BS 500A +1 BETWEEN STRINGERS 21R AND 22R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500217 19980605 00217 NM 1998 6 5 SWAA980951 1 19980526 A 5320 FRAME BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 073SW 22673 DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO FWD DOORWAY FRAME OUTBD END OF EXT DOUBLER FASTENER. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1998060500218 19980605 00218 NM 1998 6 5 SWAA980952 1 19980526 A 5753 SKIN BOEING 737 7373H4 1384600 NM RT TE FOREFLAP GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND GOUGED AREA, RIGHT HAND I/B FOREFLAP UPPER SURFACE 13 FROM I/B END. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998060500219 19980605 00219 NM 1998 6 5 SWAA980953 1 19980526 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SERVICE CHECK, FOUND CRACKED INDICATIONS AT BS 178 PRESSURE BULKHEAD WEB AT RBL 4.7, WL 201.5 TO 200.0 AND WL 198 .4 TO 197.8. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500220 19980605 00220 NM 1998 6 5 SWAA980954 1 19980526 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 947, LBL 21, RBL 21 AND WL 180. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500221 19980605 00221 NM 1998 6 5 SWAA980955 1 19980528 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED C1 CHECK, FOUND CRACKED UPLOCK INTERCOSTAL. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998060500222 19980605 00222 NM 1998 6 5 SWAA980956 1 19980528 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING WALKAROUND CHECK, FOUND CRACKED 3 FUSELAGE SKIN AT RT SIDE APPROX 18 FT AFT OF WING ILLUMINATION LIGHT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500223 19980605 00223 NM 1998 6 5 SWAA980957 1 19980528 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT ANGLE UPPER SURFACE IN SEVERAL AREAS, AT BS 947, LBL 21 TO RBL 21, WL 179. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500224 19980605 00224 NM 1998 6 5 SWAA980958 1 19980528 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND DENTED FUSELAGE SKIN AT BS 500A+12 STR 23L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500225 19980605 00225 NM 1998 6 5 SWAA980959 1 19980528 A 5220 STOP PADS BOEING 737 7373H4 1384600 NM EMERG EXIT WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND LEFT AND RIGHT EMERGENCY EXIT HATCH STOP PADS WORN 6 EACH. REMOVED AND REPLACED PER BOE ING MM. 2 L 7 2 4F RT A16WE 1998060500226 19980605 00226 NM 1998 6 5 SWAA980960 1 19980528 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 986, LBL 4-43, WL 208 AROUND FASTENER HOLES UPPER AND LOWER SID ES. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998060500227 19980605 00227 NM 1998 6 5 SWAA980961 1 19980528 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 983 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 983, LBL 18, WL 208. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998060500228 19980605 00228 NM 1998 6 5 SWAA980962 1 19980528 A 5510 TIP BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND RT HORIZONTAL STAB TIP HAS 2 CRACK INTERNAL AND EXTERNAL SURFACES 4 FROM L/E AT LOWER ED GE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500229 19980605 00229 NM 1998 6 5 SWAA980963 1 19980528 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CRACKED ANGLE AT BS 328, WL 200-207, LBL 45, FORWARD SIDE OF FLOORBEAM AND AT BS 328, WL 200-207, LBL 45 AFT SIDE OF FLOORBEAM. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500230 19980605 00230 NM 1998 6 5 SWAA980964 1 19980528 A 5755 SKIN BOEING 737 7373H4 1384600 NM NR 7 SPOILER DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND NR 7 SPOILER UPPER SURFACE HAS 2 DENT 14 FROM I/B END 5 FROM T/E. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998060500231 19980605 00231 NM 1998 6 5 SWAA980965 1 19980528 A 5510 ANGLE BOEING 737 7373H4 1384600 NM HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB WEB AT HSS 175.5 HAS CRACKED L ANGLE STIFFENER APPROX 30 AFT OF FRONT SPAR . REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998060500232 19980605 00232 NM 1998 6 5 SWAA980966 1 19980528 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 4 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CRACKED NR 4 SLAT ON LOWER SKIN, O/B OF PUSHROD SITTING. REPAIRED PER TRAMCO EO NR 98-0 440. 2 L 7 2 4F RT A16WE 1998060500233 19980605 00233 NM 1998 6 5 SWAA980967 1 19980528 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND CRACKED L ANGLE BETWEEN BS 380 AND 400, BL 0, WL 208. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998060500234 19980605 00234 NM 1998 6 5 SWAA980968 1 19980528 A 5512 SKIN BOEING 737 7373H4 1384600 NM LT HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 635SW 27708 DURING SERVICE CHECK, FOUND LT HORIZONTAL STABILIZER LEADING EDGE DENTED 3 FT OUTBD OF INBD SIDE. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998060500235 19980605 00235 EU 1998 6 5 QXEA9800684 1 19980528 A 3350 CIRCUIT BREAKER FOKKER F28 F28MK4000 4990810 EU CARGO COMPT TRIPPED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 PDX - EVACUATION LIGHTS DO NOT OPERATE FROM EITHER FA'S POSITION. MAINTENANCE RESET EVACUATION LIGHT CIRCUIT BREAKER IN FORWARD CARGO PIT. OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998060500236 19980605 00236 WP 1998 6 5 MWEA98627 1 19980529 A 5531 99118902 RIB DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CRACK ON VERTICAL STABILIZER RIB AT STATION ZFS 4.750. MAINTENANCE FABRICATED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 1998060500237 19980605 00237 WP 1998 6 5 MWEA98628 1 19980529 A 5320 99100733 PRESSURE PANEL DOUG DC9 DC914 3022034 WP NLW WW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK ON NOSE LANDING GEAR PRESSURE PANEL LEFT HAND OUTBOARD AT FUSELAGE SKIN AND FS 83.5515. MAINTENANCE FABRICA TED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998060500238 19980605 00238 WP 1998 6 5 MWEA98629 1 19980529 A 5320 991152017 SUPPORT DOUG DC9 DC914 3022034 WP BS 218 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK ON VERTICAL SUPPORT AT STATION 218 AND LONGERON 30. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998060500239 19980605 00239 WP 1998 6 5 DLL10981125 1 19980526 A 3350 337001090 BATTERY LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 727DA 193C1167 NR 2 LT EMERGENCY LIGHTING BATT WILL NOT HOLD CHARGE. REPLACED NR 2 LT BATT, OPS CK GOOD. 2 L 7 3 4F A23WE 1998060500240 19980605 00240 WP 1998 6 5 DLL10981127 1 19980526 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 714DA 65562 193C1090 ON L/O FOUND LOWER GALLEY EMERGENCY LIGHT PWR SUPPLY INOP. REPLACED EMER LIGHT PWR SUPPLY, OPS NML. 2 L 7 3 4F A23WE 1998060500241 19980605 00241 NM 1998 6 5 DL72S981130 1 19980519 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 545DA 22494 CORROSION ON FLOORBEAM STA 344 HAS CORROSION FROM ENTRY DOOR TO FWD LAV WALL. REPAIRED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998060500242 19980605 00242 WP 1998 6 5 DLL14981131 1 19980524 A 5711 1503231105 SPAR CAP LKHEED 1011 1011385115 5265015 WP BS 1163 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 CENTER WING, INTERMEDIATE SPAR, FS 1163, UPPER SPAR CAP: CAP SPLICE REPAIR. THE RT END OF THE UPPER SPAR CAP ON THE FS 1163 INTERMEDIATE SPAR WAS FOUND CRACKED BEYOND LIMITS. THE RT END OF THE CAP WAS CUT OFF AND A NEW SECTION WAS SPLICED IN PER ER/A 364821-14, REV A. 2 L 7 3 4F A23WE 1998060500243 19980605 00243 NM 1998 6 5 DL767981132 1 19980522 A 5414 SKIN BOEING 767 767232 1385132 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 107DL 22219 NACELLES, NR 2 PYLON, TORQUE BOX, INBD STRUT SKIN, ACCESS CUTOUT: REPAIR FOR CRACK. THE NR 2 PYLON TORQUE BOX SKIN WAS FOUND WITH A CRACK IN THE UPPER AFT CORNER OF THE ACCESS CUTOUT AT NAC STA 231. THE CRACK WAS STOP DRILLED ON A TIME-L IMITED BASIS WITH A REPAIR DOUBLER INSTALLED WITHIN 10 DAYS. FURTHER TORQUE BOX MODIFICATIONS/REINFORCEMENTS ARE TO BE ACCOMPLISHED AT NEXT HMV VISIT. THE REPAIR WAS ACCOMPLISHED PER ER/A 364868-14. 2 L 7 2 4F RT A1NM 1998060500244 19980605 00244 WP 1998 6 5 DLL14981133 1 19980522 A 5312 154789109 BULKHEAD WEB LKHEED 1011 1011385115 5265015 WP BS 328 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 736DY 193C1227 FUSELAGE, BULKHEAD FS 328 LBL 6 WL 126, REPAIR FOR WEB CORROSION. THE FS 328 BULKHEAD WEB WAS FOUND CORRODED AT LBL 6 A ND WL 126A 6 BY 3 CUTOUT WAS MADE IN THE WEB TO REMOVE THE CORROSION THE WEB WAS REPAIR WITH AND ALUMINUM DOUBLER AND TR IPLER PER ER/A 364835-14AD, REV A. 2 L 7 3 4F A23WE 1998060500245 19980605 00245 NM 1998 6 5 DL757981134 1 19980528 A 3350 BATTERY 61020 BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 651DL 24391 FWD EMERG FLASHLIGHT STRAP BROKEN AND BATTERY DEAD. REPLACED BATTERY. 2 L 7 2 4F RT A2NM 1998060500246 19980605 00246 WP 1998 6 5 DLL14981135 1 19980527 A 3350 BATTERY M835369024 LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST DE DESCENT 1 SO 27 1739D 193C1237 IN DESCENT, FLT ATTENDANTS REPORTED EMERG TRACK LTS ON IN C AND D ZONES. REPLACED 3399K3 RELAY. PERFORMED OPS CK PER O PN 78100. 2 L 7 3 4F A23WE 1998060500247 19980605 00247 NM 1998 6 5 DL72S981141 1 19980528 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 LT ELEV T/E SEPARATING I/B SIDE, REPAIRED PER MM 55-20-0 P801. 2 L 7 3 4F A3WE 1998060500248 19980605 00248 NM 1998 6 5 DL72S981142 1 19980528 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 FOUND AT A2 LETTER CK, FUSELAGE SKIN HAS A .25 INCH CRACKED AT LWR I/B FASTENER HOLE FOR R-4 WINDOW CUTOUT. REPAIRED PE R SRM 53-30-3. 2 L 7 3 4F A3WE 1998060500249 19980605 00249 NM 1998 6 5 DL72K981144 1 19980528 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 471DA 20748 ON L/O, FOUND EMERGENCY LIGHT ON AFT CARGO DOOR INOP. REPLACED BATT PACK AS PER M/M. OPS CHK NML. 2 L 7 3 4F A3WE 1998060500250 19980605 00250 NM 1998 6 5 DL72S981145 1 19980529 A 3260 SWITCH BOEING 727 727232 1384082 NM TAIL SKID DIRTY A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 467DA 20744 TAILSKID LIGHT ON TAKEOFF ROLL AT 70 KNOTS, CLEANED PROX SWITCH. 2 L 7 3 4F A3WE 1998060500251 19980605 00251 NM 1998 6 5 DLM88981146 1 19980529 A 2421 GENERATOR 696233B DOUG MD88 MD88 3023688 NM NR 2 FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 27 955DL 4244 49886 AFTER T/O, 400 FT AGL HAD BOTH BUSSES FAIL IN SUCCESSION AND HAD STBY PWR IN USE. REPLACED RIGHT GENERATOR AND CSD. 2 L 7 2 4F RT A6WE 1998060500252 19980605 00252 NM 1998 6 5 DL72L981147 1 19980529 A 5320 WEB BOEING 727 727232 1384082 NM BS 1300 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 510DA 21312 RT VERT TORQUE BOX WEB CRACKED .875 INCH AT UPPER LIGHTENING HOLE STA 1300 RT. REPAIRED PER MM 53+11+0 P 828. 2 L 7 3 4F A3WE 1998060500253 19980605 00253 NM 1998 6 5 DL76S981149 1 19980530 A 3260 BULB BOEING 767 767332 1382001 NM RT MLG FAILED A DALA O OTHER N FALSE WARNING AP APPROACH 1 SO 27 129DL 24079 ON FINAL APPROACH, LANDING GEAR SELECTED DOWN, RIGHT MAIN GEAR SHOWED UNSAFE. ACCOMPLISHED ALTERNATE GEAR EXTENSION PRO CEDURE AND LANDING WITH UNSAFE INDICATION. LANDING AND ROLLOUT WITHOUT INCIDENT. RELAMPED RIGHT MAIN GEAR LIGHT IN C OCKPIT. ALL INDICATION NORMAL. 2 L 7 2 4F RT A1NM 1998060500254 19980605 00254 NM 1998 6 5 DL73K981151 1 19980530 A 3350 LIGHT BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 301DL REFLECTER 23073 10261 FOUND ON SVC CK, 2 FWD LT SIDE EXTERIOR EMERGENCY LIGHT INOP. REPLACED REFLECTOR AND SOCKET. 2 L 7 2 4F RT A16WE 1998060500255 19980605 00255 NM 1998 6 5 DLM88981152 1 19980531 A 3350 BATTERY RPS1 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 939DL 1171 49812 A/C ARRIVED WITH EMER TRACK LIGHTING INOP IN FWD HALF OF CABIN. REPLACED FWD BATTERY AND PWR SUPPLY. CKS GOOD. 2 L 7 2 4F RT A6WE 1998060500256 19980605 00256 NM 1998 6 5 DL73S981153 1 19980531 A 2910 LINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE RUPTURED A DALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 331DL 23103 717135 SYS 'A' LOSS INDICATIONS LOW HYD QTY AND NR 2 SYS 'A' LOW PRESS LIGHT. FOUND PRESSURE LINE ON RT ENG HYD PUMP RUPTURED. REPLACED LINE. SERVICED SYS BLEED SYS. ALL CK GOOD PER M/M. 2 L 7 2 4F 4 F RT A16WE E2EA 1998060500257 19980605 00257 NM 1998 6 5 DL72S981155 1 19980531 A 2820 CONNECTOR BOEING 727 727225 1384077 NM NR 2/3 FUEL TANK DIRTY A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 8875Z 21293 ON DEPARTURE, COULD NOT CROSSFEED NR 1 ENG OFF OF FUEL TANKS NR 2 OR NR 3. REMOVED LOCKWIRE FROM VALVE. CLEANED CANNON PLUG AND MOTOR PLUG. OPN OF VALVE NML. REMOVED MCO AND PLACARD. 2 L 7 3 4F A3WE 1998060500258 19980605 00258 WP 1998 6 5 DLL13981157 1 19980531 A 3397 WIRE LKHEED 1011 10113851 5265010 WP CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 790DL 193A1143 EMERGENCY TRACK LIGHTS ARE VERY DIM FROM ROW 10 THROUGH 16 AND ROW 20 THROUGH 26 ON LT SIDE AND ROW 20 THROUGH 26 ON THE RT SIDE. FOUND A SHORTED WIRE AT NR 2 CROSS-AISLE EMERG PATH TRACK LIGHTS. REPAIRED SAME WDM. ALL EMERGENCY TRACK LI GHTS FUNCTION GOOD. ALL SECURED. 2 L 7 3 4F A23WE 1998060500259 19980605 00259 WP 1998 6 5 DLL10981158 1 19980531 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP L2 DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718DA 193C1097 ON LAYOVER, FOUND FLASHLIGHT AT L-2 FLT ATTN SEAT INOP. RED IND NOT FLASHING. RELAMPED INDICATOR LIGHT. CKS OK. 2 L 7 3 4F A23WE 1998060500260 19980605 00260 NE 1998 6 5 VNAA9805014 2 19980523 A 7321 311888802 ECU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 07 431JS 65711 3028 DURING TAKEOFF, A LEFT HAND ECU FAIL WARNING MESSAGE OCCURED. THE AIRCRAFT ABORTED TAKEOFF, AND RETURNED TO THE GATE. M AINTENANCE INSPECTED AND REPLACED THE LEFT HAND ENGINE ELECTRONIC CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 73-21-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998060500261 19980605 00261 NM 1998 6 5 CKSA98304 1 19980520 A 3350 BATTERY PACK BOEING 747 747146 NM CABIN DISCHARGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 704CK 20528 DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS, SEVERAL LIGHTS INOP. ALL EMERGENCY LIGHTS PACKS WERE REMOVED, RECHARGED I AW MM 33-51-00. REINSTALLED AND TESTED GOOD IAW MM 33-51-03. NON-ROUTINE TASK CARD NUMBER B0083-02-N-00014. 2 L 7 4 4F A20WE 1998060500262 19980605 00262 NM 1998 6 5 CKSA98305 1 19980520 A 5320 BEAM BOEING 747 747146 NM BS 740 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 LT FWD CARGO COMPARTMENT STA 740 SUPPORT BEAM IS CRACKED. REMOVED DAMAGED AREA IAW B747 SRM 51-40-04. ID MATERIAL BAC1 490-2785, BAC150-100117. INSTALLED REPAIR IAW B747 SRM 51-30-02. NON-ROUTINE TASK CARD NUMBER B0083-02-N-00093. 2 L 7 4 4F A20WE 1998060500263 19980605 00263 NM 1998 6 5 CKSA98306 1 19980520 A 5330 SKIN BOEING 747 747146 NM MAIN DECK CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 ON MAIN DECK, GALLEY NR 7 LT CAVITY SERVICE CAR UPPER INTERIOR SKIN AND FASTENERS CORRODED. REMOVED CORROSION IAW SRM 5 1-10-01. FOUND OUT OF LIMITS IAW SRM 51-10-01. REMOVED DAMAGED AREAS IAW SRM 51-10-01. MATERIAL ID 2024-T3 .040. INS TALLED REPAIR IAW SRM 51-30-02. NON-ROUTINE TASK CARD NUMBER B0083-02-N-00126. 2 L 7 4 4F A20WE 1998060500264 19980605 00264 NM 1998 6 5 CKSA98307 1 19980520 A 5400 BRACE BOEING 747 747146 NM NR 1 PYLON WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ACCOMPLISHMENT OF AD 95-10-16, FOUND NR 1 PYLON DIAGONAL BRACE DAMAGED BEYOND LIMITS, .240 WIDE .405 LONG .085 D EEP, .090 AWAY .190 WIDE .400 LONG .040 DEEP. REPLACED DIAGONAL BRACE IAW MM 54-10-03 AND SECURED HOLD OPEN STRUT. NON -ROUTINE TASK CARD NUMBER B0083-09-N-00019. 2 L 7 4 4F A20WE 1998060500265 19980605 00265 NM 1998 6 5 CKSA98308 1 19980520 A 5730 SKIN BOEING 747 747146 NM BS 340 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ACCOMPLISHMENT OF AD 96-26-04, FOUND NOSE WHEEL WELL LOWER CORNER LT STA 340 VERTICAL STIFFENER WITH CRACK. EXTE RNAL SKIN REPAIR CRACK IN SKIN IAW SRM 51-10-01 AND 57-10-01. REMOVED AND REPLACED PREVIOUS REPAIR AND REPAIRED SKIN CR ACK IAW SRM 51-30-02 AND 51-10-02. NON-ROUTINE TASK CARD NUMBER B0083-09-N-00033. 2 L 7 4 4F A20WE 1998060500266 19980605 00266 NM 1998 6 5 CKSA98309 1 19980520 A 5313 STRINGER BOEING 747 747146 NM BS 2360 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ACCOMPLISHMENT OF AD 86-16-05, FOUND CORROSION ON STRINGER S35L STA 2360 AFT OF PRESSURE BULKHEAD. REMOVED CORRO SION. FOUND OUT OF LIMITS IAW B747 SRM 53-30-02. REMOVED DAMAGED STRINGER AND END STRINGER IAW B747 SRM 53-10-03. MAT ERIAL ID PN BAC1498-146.7075-T62 STRINGER REPAIR ID PN BAC1498-1317075-T62. INSTALLED REPAIR IAW B747 SRM 53-10-03. NO N-ROUTINE TASK CARD NUMBER B0083-09-N-00035. 2 L 7 4 4F A20WE 1998060500267 19980605 00267 NM 1998 6 5 CKSA98310 1 19980520 A 5312 BACB30USK34 BULKHEAD BOLT BOEING 747 747146 NM BS 2360 SHEARED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ACCOMPLISHMENT OF AD 87-23-01, FOUND AFT PRESSURE BULKHEAD BS 2360 BETWEEN S32 AND S33, 6 HR POSITION ONE BOLT IS MISSING. REMOVED SHEARED BOLT IAW MM 20-51-01. INSTALLED BOLT IAW SRM 51-30-04. NON-ROUTINE TASK CARD NUMBER B0083-0 9-N-00042. 2 L 7 4 4F A20WE 1998060500268 19980605 00268 NM 1998 6 5 CKSA98311 1 19980520 A 5312 B30US6K34 BULKHEAD BOLT BOEING 747 747146 NM BS 2360 SHEARED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ACCOMPLISHMENT OF AD 87-23-01, FOUND AFT BULKHEAD (PRESSURE) BS 2360 BETWEEN S5 TO S6, 1 HR POSITION ONE BOLT MIS SING (SHEARED). REPLACED BOLT IAW SRM 51-30-04. NON-ROUTINE TASK CARD NUMBER B0083-09-N-00043. 2 L 7 4 4F A20WE 1998060500269 19980605 00269 NM 1998 6 5 CKSA98312 1 19980520 A 5312 BULKHEAD SKIN BOEING 747 747146 NM BS 2360 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ACCOMPLISHMENT OF AD 87-23-01, FOUND AFT PRESSURE BULKHEAD BS 2360 AT STRINGER 50, SKIN IS CORRODED (SKIN) UNPRES SURIZED AREA. REMOVED CORROSION IAW B747 SRM 51-10-01. SKIN FOUND OUT OF LIMITS IAW B747 SRM 53-30-01. MATERIAL ID 20 24-T3 IAW B747 SRM 53-30-02. INSTALLED DOUBLER IAW B747 SRM 53-30-03. NON-ROUTINE TASK CARD NUMBER B0083-09-N-00046. 2 L 7 4 4F A20WE 1998060500270 19980605 00270 NM 1998 6 5 CKSA98313 1 19980520 A 5330 SKIN BOEING 747 747146 NM BS 2412 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ACCOMPLISHMENT OF AD 95-16-02, FOUND STRUCTURE OF BS 2412 CRACKED AND CORRODED BETWEEN STRINGER 50R TO STRINGER 4 7R ACCESS DOOR NR 312. REMOVED DAMAGED PARTS IAW SRM 51-30-02. MATERIAL ID 7075-0. REPAIRED DAMAGE PARTS AND REINFORC ED SKIN IAW SRM 51-30-02 AND 51-10-01. NON-ROUTINE TASK CARD NUMBER B0083-09-N-00075. 2 L 7 4 4F A20WE 1998060500271 19980605 00271 NM 1998 6 5 CKSA98314 1 19980520 A 5720 WEB BOEING 747 747146 NM BS 1241 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, RT WING LANDING GEAR BAY STA 1241 BULKHEAD WEB UPPER SURFACE. S TIFFENER HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-01. FOUND OUT OF LIMITS IAW SRM 51-10-01. REPAIRED IAW SRM 51 -40-04. ID MATERIAL TO MAKE WEB REPAIR 7075-T6 .156. CORROSION TASK CARD NUMBER C53-100-01-8. NON-ROUTINE TASK CARD N UMBER B0083-16-N-00304. 2 L 7 4 4F A20WE 1998060500272 19980605 00272 NM 1998 6 5 CKSA98315 1 19980520 A 5720 STIFFENER BOEING 747 747146 NM WS 160 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND RT WING FRONT SPAR, WS160, WBL140 HAS CRACKED STIFFENER. REMOVED CRACKED STIFFENE R IAW SRM 51-30-02. MATERIAL ID 7075-T6 0.080 IAW SRM 57-10-02. REPLACED STIFFENER IAW SRM 51-10-01 AND 51-30-02. COR ROSION TASK CARD NUMBER C57-510-01-2. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00324. 2 L 7 4 4F A20WE 1998060500273 19980605 00273 NM 1998 6 5 CKSA98316 1 19980520 A 5347 SEAT TRACK BOEING 747 747146 NM BS 580-600 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 580 TO BS 600, BWL 310 (UPPER DECK) LBL65. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. ID MATERIAL PN BAC1520-156 6. REPAIRED SEAT TRACK IAW SRM 53-10-21. CORROSION TASK CARD NUMBER C53-210-03-4. NON-ROUTINE TASK CARD NUMBER B0083- 16-N-00393. 2 L 7 4 4F A20WE 1998060500274 19980605 00274 NM 1998 6 5 CKSA98317 1 19980520 A 5347 SEAT TRACK BOEING 747 747146 NM BS 580-600 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, SEAT TRACK CORRODED BETWEEN BS 580-BS 600, BWL 310 (UPPER DECK), LBL 45. REMOVED CORROSION IAW SRM 51-10-01. CORROSION OUT OF LIMITS IAW 53-10-01. ID MATERIAL PN BAC1520-1567P .0729 5. REPAIRED SEAT TRACK IAW B747 SRM 53-10-21. CORROSION TASK CARD NUMBER C53-210-03-4. NON-ROUTINE TASK CARD NUMBER B 0083-16-N-00394. 2 L 7 4 4F A20WE 1998060500275 19980605 00275 NM 1998 6 5 CKSA98318 1 19980520 A 5347 SEAT TRACK BOEING 747 747146 NM BS 510-660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 510 TO BS 660, BWL 199.8, LBL33 (SEV ERAL PLACES). REMOVED CORROSION IAW SRM 51-10-01. DAMAGE OUT OF LIMITS AT LBL 33 ON BS 510 TO BS 516 AND CRACK FOUND A T BS 552 LBL 33 IAW SRM 51-10-01. ID MATERIAL PN BAC1520-1854 IAW SRM 53-10-21. REPAIRED IAW SRM 53-10-21. CORROSION TASK CARD NUMBER C53-210-03-4. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00395. 2 L 7 4 4F A20WE 1998060500276 19980605 00276 NM 1998 6 5 CKSA98319 1 19980520 A 5347 SEAT TRACK BOEING 747 747146 NM BS 450-510 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, SEAT TRACK CORRODED BETWEEN BS 510 AND BS 520, BWL 199.8, RBL 12 . FOUND SEAT TRACK OUT OF LIMITS, STA 450 TO 510 IAW SRM 51-10-01. ID MATERIAL PN BAC1520-1566. REMOVED OUT OF LIMIT SEAT TRACK STA 450 TO 5510 IAW SRM 51-10-01. REPAIRED IAW B747 SRM 53-10-03. CORROSION TASK CARD NUMBER C53-210-03-4. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00396. 2 L 7 4 4F A20WE 1998060500277 19980605 00277 NM 1998 6 5 CKSA98320 1 19980520 A 5347 SEAT TRACK BOEING 747 747146 NM BS 510-660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, SEAT TRACK CORRODED FROM BS 510 TO BS 660, BWL 199.8, RBL 33 (SE VERAL PLACES). FOUND SEAT TRACK OUT OF LIMITS. ID MATERIAL PN BAC1520-1854. REPAIRED IAW SRM 51-30-02. CORROSION TAS K CARD NUMBER C53-210-03-4. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00397. 2 L 7 4 4F A20WE 1998060500278 19980605 00278 NM 1998 6 5 CKSA98321 1 19980520 A 5347 SEAT TRACK BOEING 747 747146 NM BS 820-860 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, IN MAIN CABIN ON FLOOR SUPPORT BETWEEN BS 820 THROUGH BS 860, RB L 10 IS CORRODED. REMOVED CORROSION, FOUND OUT OF LIMITS IAW B747 SRM 51-10-06. ID MATERIAL PN BAC1520-1566 IAW B747 S RM 53-10-21. REPAIRED SEAT TRACK IAW B747 SRM 53-10-21. CORROSION TASK CARD NUMBER C53-210-03-4. NON-ROUTINE TASK CAR D NUMBER B0083-16-N-00445. 2 L 7 4 4F A20WE 1998060500279 19980605 00279 NM 1998 6 5 CKSA98322 1 19980520 A 5312 BACB30US6K34 BULKHEAD BOLT BOEING 747 747146 NM BS 2360 SHEARED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND BOLT SHEARED AT BS 2360 AND BL0, PRESSURE BULKHEAD ATTACH AREA BELOW AFT LAVATORY FRAME SUPPORT. REMOVED AND REPLACED SHEARED BOLT IAW MM 20-51-01 AND 51-30-04. CORROSION TASK CARD NUMBER C53-210-03-3 . NON-ROUTINE TASK CARD NUMBER B0083-16-N-00477. 2 L 7 4 4F A20WE 1998060500280 19980605 00280 NM 1998 6 5 CKSA98323 1 19980520 A 5330 SKIN BOEING 747 747146 NM BS 960 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, FWD CARGO COMPARTMENT STA 960, BETWEEN S47R AND S47L SKIN HAS CO RROSION. REMOVED CORROSION IAW B747 SRM 51-10-01 MATERIAL LOSS 30 PERCENT OUT OF LIMITS IAW B747 SRM 53-30-01. DAMAGED SKIN WAS REMOVED IAW B747 SRM 53-30-03 FIG 1 AND ANGLE T BETWEEN FRAME AND SKIN. ID MATERIAL REPAIR SHEET ALUMINIUM 20 24T3 .071. CORROSION TASK CARD NUMBER C53-125-01-1. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00604. 2 L 7 4 4F A20WE 1998060500281 19980605 00281 NM 1998 6 5 CKSA98324 1 19980520 A 5320 ANGLE BOEING 747 747146 NM BS 640 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT STA 640 LBL 43 FLOOR SUPPORT IS CRACKED. CUT OUT DAMAGED AR EA IAW B747 SRM 51-10-01. ID MATERIAL 2024T3 .050. INSTALLED ANGLE AND FILLER IAW B747 SRM 51-30-02. CORROSION TASK C ARD NUMBER C53-125-01-1. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00643. 2 L 7 4 4F A20WE 1998060500282 19980605 00282 NM 1998 6 5 CKSA98325 1 19980520 A 5311 FRAME BOEING 747 747146 NM BS 680 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT STA 680, RBL 70, WL118 RIB IS CRACKED. REMOVED DAMAGED RIB IAW SRM 51-30-2. MATERIAL CHECK 2024-T3 .040. INSTALLED NEW RIB IAW SRM 51-30-02. CORROSION TASK CARD NUMBER C53-125- 01-1. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00644. 2 L 7 4 4F A20WE 1998060500283 19980605 00283 NM 1998 6 5 CKSA98326 1 19980520 A 5320 SUPPORT BOEING 747 747146 NM BS 570 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT STA 570 LBL 24 FLOOR SUPPORT IS CRACKED. REMOVED DAMAGED MA TERIAL IAW B747 SRM 51-30-00. ID MATERIAL 2024T3 0.63 IAW B747 SRM 51-10-01. INSTALLED SUPPORT IAW B747 SRM 51-21-01. CORROSION TASK CARD NUMBER C53-125-01-1. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00655. 2 L 7 4 4F A20WE 1998060500284 19980605 00284 NM 1998 6 5 CKSA98327 1 19980520 A 5347 SEAT TRACK BOEING 747 747146 NM BS 520-540 BROKEN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND IN UPPER DECK CABIN IN FLOOR SUPPORT BETWEEN BS 520 TO BS 540, LBL 40, WL 310 ARE BROKEN. REMOVED DAMAGED SEAT TRACK SECTION IAW B747 SRM 51-30-02. SEAT TRACK WAS FOUND OUT OF LIMITS IAW B747 SRM 51-3 0-02. MATERIAL ID BAC1520-1567 AND 6511. INSTALLED NEW SEAT TRACK IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C 53-210-03-4. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00700. 2 L 7 4 4F A20WE 1998060500285 19980605 00285 NM 1998 6 5 CKSA98328 1 19980520 A 5330 SKIN BOEING 747 747146 NM BS 1720 TORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND WEB SKIN TORN IN AFT CARGO COMPARTMENT FLOOR STRUCTURE AT BS 1720 AND RBL 54 ABOVE S44R. REMOVED DAMAGED MATERIAL IAW SRM 51-10-07. MATERIAL ID 2024-T3 .040 IAW SRM 51-40-02. INSTALLED DOUBLER IAW SR M 51-40-02 FIG 1. CORROSION TASK CARD NUMBER C53-125-01-2. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00753. 2 L 7 4 4F A20WE 1998060500286 19980605 00286 NM 1998 6 5 CKSA98329 1 19980520 A 5330 SKIN BOEING 747 747146 NM BS 1580 DENTED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND 2.5 INCH DENT IN BS 1580 FRAME WEB SKIN DIRECTLY ABOVE S47R IN AFT CARGO COMPARTME NT FLOOR STRUCTURE FORWARD SECTION. REMOVED DAMAGED MATERIAL AND DENT IAW B747 SRM 51-10-01. MATERIAL ID FILLER 7075-T 6 .025 AND DOUBLER 7075-T6 .040. INSTALLED REPAIR IAW SRM B747 SRM 53-10-21. CORROSION TASK CARD NUMBER C53-125-01-2. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00754. 2 L 7 4 4F A20WE 1998060500287 19980605 00287 NM 1998 6 5 CKSA98330 1 19980520 A 5311 FRAME BOEING 747 747146 NM BS 1500 BUCKLED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND FRAME WEB BUCKLED AT BS 1500 BETWEEN STRINGER 43-47 BOTH LEFT AND RIGHT SIDE IN AF T CARGO COMPARTMENT FLOOR STRUCTURE FWD SECTION. REMOVED DAMAGE IAW B747 SRM 51-40-03 LEFT SIDE. ID MATERIAL IAW B747 SRM 53-10-23 7075-T6 .020. REMOVED DAMAGE IAW B747 SRM 51-40-03 RIGHT SIDE. ID MATERIAL IAW B747 SRM 53-10-23 7075-T6 .040. INSTALLED DOUBLER BOTH LEFT AND RIGHT SIDE IAW B747 SRM 53-10-04. CORROSION TASK CARD NUMBER C53-125-01-2. NON- ROUTINE TASK CARD NUMBER B0083-16-N-00755. 2 L 7 4 4F A20WE 1998060500288 19980605 00288 NM 1998 6 5 CKSA98331 1 19980520 A 5330 SKIN BOEING 747 747146 NM BS 2220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION ON THE SKIN AFT OF STA 2220 IN AFT CARGO COMPARTMENT B ETWEEN S46L AND S45L. REMOVED CORROSION IAW B747 SRM 51-10-01 SKIN IS OUT OF LIMITS IAW B747 SRM 53-10-01. MATERIAL LO OSE BETWEEN S46L AND 45L 0.028 PERCENT IAW B747 SRM 53-30-01 AND 53-30-02 ID MATERIAL 2024T3 .100. REPAIRED, CORROSION TASK CARD NUMBER C53-125-01-2. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00807. 2 L 7 4 4F A20WE 1998060500289 19980605 00289 NM 1998 6 5 CKSA98332 1 19980520 A 5330 SKIN BOEING 747 747146 NM BS 2220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION ON THE SKIN AFT OF STA 2220 BETWEEN STRINGER 46R-47R A ND STRINGER 45R-46R IN AFT CARGO COMPARTMENT. REMOVED CORROSION IAW B747 SRM 51-10-01. SKIN IS OUT OF LIMITS IAW B747 SRM 53-10-01. MATERIAL LOSS BETWEEN S46R AND S47R, .068 INCH IAW B747 SRM 53-30-01 AND 53-30-02. MATERIAL LOSS BETWEEN S45R AND S46R .057 INCH IAW B747 SRM 53-30-01 AND 53-30-02 ID MATERIAL 2024T3 .100 IAW SRM 53-30-03. REPAIRED, CORROSI ON TASK CARD NUMBER C53-125-01-2. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00808. 2 L 7 4 4F A20WE 1998060500290 19980605 00290 NM 1998 6 5 CKSA98333 1 19980520 A 5311 FRAME BOEING 747 747146 NM BS 1820 CRUNCHED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND CRUNCHED ON THE WEB FRAME OF STA 1820 IN AFT CARGO COMPARTMENT ABOVE STRINGER 51L. REMOVED DAMAGED MATERIAL DENT IAW B747 SRM 51-10-01. MATERIAL ID 7076T6 .025. DOUBLER 7075T6 .040. INSTALLED REPAIR IAW B747 SRM 53-10-04. CORROSION TASK CARD NUMBER C53-125-01-2. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00809. 2 L 7 4 4F A20WE 1998060500291 19980605 00291 NM 1998 6 5 CKSA98334 1 19980520 A 5311 FRAME BOEING 747 747146 NM BS 1820 TORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 DURING ROUTINE CPCP INSPECTION, FOUND FRAME WEB TORN AT BS 1820 AND RBL 27 IN AFT CARGO COMPARTMENT FLOOR STRUCTURE. RE MOVED DAMAGED AREA IAW SRM 51-10-01. MATERIAL ID 7075-T6 .025 AND 7075-T6 .040. INSTALLED REPAIR IAW SRM 53-10-04 AND 51-30-02. CORROSION TASK CARD NUMBER C53-125-01-2. NON-ROUTINE TASK CARD NUMBER B0083-16-N-00812. 2 L 7 4 4F A20WE 1998060500292 19980605 00292 NM 1998 6 5 CKSA98335 1 19980520 A 5330 SKIN BOEING 747 747146 NM BS 470 DENTED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 704CK 20528 BS 470, SWL 118 LT (LOWER BELLY AREA) HAS A DENT L-2, W-2, D-.350, OUT OF LIMITS. CUT OUT AND REMOVED THE DAMAGED PORTI ON OF THE SKIN IAW B747 SRM 53-30-03. CHECK MATERIAL FOR FABRICATE SHIM AND DOUBLER 7075T6 .071, 2024T3 .063 IAW SRM 53 -30-03. REPAIRED IAW B747 SRM 53-30-03. NON-ROUTINE TASK CARD NUMBER B0083-81-N-0003. 2 L 7 4 4F A20WE 1998060500293 19980605 00293 NE 1998 6 5 CKSA98337 2 19980525 A 7200 ENGINE BOEING 747 747269B NM PWA JT9 JT9D7J 52054 NE NR 1 FAILED A A CKSA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 GL 23 707CK 21541 689567 AFTER TAKEOFF, NR 1 ENGINE HAD A FIRE WARNING SHUTDOWN ENGINE AS PER AOM DISCHARGED ONE FIRE BOTTLE, LIGHT WENT OUT. ON POST FLIGHT, FOUND HEAT DAMAGE TO BOTH COWLS, AFT FIRE LOOP, AND AFT WIRING HARNESS. DETERMINED ACFT WILL DO 3 ENGINE FERRY. NR 1 ENGINE PREPARED FOR FERRY FLIGHT IAW BOEING B747 MM 71-00-61 N1 FAN STRAPPED, N2 LOCK-OUT INSTALLED, REVERS ER BOLTED IN STOWED POSITION. COMPLIED WITH FORM M-29A PREP FOR FERRY FLIGHT. AIRCRAFT INSPECTED AND FOUND TO BE SAFE FOR INTENDED FERRY FLIGHT. REMOVED AND REPLACED NR 1 ENGINE IAW 71-00-00 AND AIA 7EC7100 OPS AND LEAK CHECK GOOD. PREL IMINARY TEARDOWN FINDINGS: NR 3 BEARING AREA OIL COKING AND FOUND TURBINE DAMAGE. 2 L 7 4 4F 4 F RT A20WE E20EA 1998060500294 19980605 00294 NM 1998 6 5 USAA980171 1 19980415 A 5315 6545818510 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 504AU 35827 23379 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .50 INCH CORROSION AREA AT FLOORBOARD HOLES TOP OF FLOOR BEAM T-CAP ST A 344 LBL ZERO TO LBL 48. CORROSION TASK CARD NR C53-107-01. INSTALLED NEW T-CAP REPAIR ANGLE AND SPLICES PER REPAIR D OCUMENT TRM 53-10-03. (X) 2 L 7 2 4F RT A16WE 1998060500295 19980605 00295 NM 1998 6 5 USAASB98108 1 19980502 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 374US 22953 IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ON THE FORWARD ENTRY DOOR INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATION CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998060500296 19980605 00296 EU 1998 6 5 USAAF98038 1 19980421 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 860US 11295 RIC - MAINTENANCE FOUND THE FORWARD EMERGENCY FLOOR LIGHTING INOPERATIVE. THEY REPLACED THE POWER SUPPLY AND BATTERY PA CK. REF: OPERATOR CONTROL NR 98ZZZX2057. (X) 2 L 7 2 4F RT 1998060500297 19980605 00297 EU 1998 6 5 98ZZZX2057 1 19980421 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 860US 11295 RIC - MAINTENANCE FOUND THE FORWARD EMERGENCY FLOOR LIGHTING INOPERATIVE. THEY REPLACED THE POWER SUPPLY AND BATTERY PA CK. (REF: OPERATOR CONTROL NR USAAF98038. 2 L 7 2 4F RT 1998060500298 19980605 00298 NM 1998 6 5 USAASB98104 1 19980503 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 22273 PIT - PILOT REPORTED THE AFT RIGHT-HAND EMERGENCY EXIT LIGHT ABOVE THE AFT SERVICE DOOR IS INOPERABLE. MAINTENANCE REMO VED AND REPLACED THE AFT RIGHT-HAND EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998060500299 19980605 00299 NM 1998 6 5 USAASB98101 1 19980418 A 3260 6552811109 ACCESSORY UNIT BOEING 737 737201 1384454 NM E/E COMPARTMENT FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 241US 42651 22443 BUF - FL475 - UPON LOWERING LANDING GEAR TO LAND AT BUF, CREW RECEIVED 3 GREEN LIGHTS AND 3 RED LIGHTS FOR THE GEAR. CR EW RECYCLED GEAR 3 TIMES WHEREAS THE THIRD ATTEMPT, A NORMAL GEAR INDICATION WAS RECEIVED. THE CREW THEN ACCOMPLISHED A FLYBY AND THE TOWER CONFIRMED THE GEAR WAS DOWN. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE ON ITS OWN. AN EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. LIGHT OPERATIONAL C HECK NORMAL. OPERATIONAL CHECK OF GEAR HANDLE LATCH SWITCH GOOD ALSO. (X) 2 L 7 2 4F A16WE 1998060500300 19980605 00300 NM 1998 6 5 USAASB98099 1 19980417 A 8012 1G309 SWITCH BOEING 737 7372B7 1384560 NM LEFT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 287AU 23134 BWI - FLT 8026 - AFTER TAKEOFF, THE NR 1 START VALVE 'OPEN' LIGHT ILLUMINATED. THE LIGHT EXTINGUISHED AFTER THE ENGINE POWER WAS REDUCED TO IDLE. THE FLIGHT RETURNED TO BWI AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE ST ART VALVE PRESSURE SWITCH. (X) 2 L 7 2 4F A16WE 1998060500301 19980605 00301 NM 1998 6 5 USAASB98102 1 19980421 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 CLE - MAINTENANCE FOUND THE AFT CENTER OVERHEAD EMERGENCY LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998060500302 19980605 00302 NM 1998 6 5 USAABB98045 1 19980422 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 600AU 22192 LAX - EMERGENCY FLOOR LIGHTING INOPERATIVE AT ROWS 9 AND 29. MAINTENANCE REPLACED THE BATTERIES. (X) 2 L 7 2 4F RT A2NM 1998060500303 19980605 00303 NM 1998 6 5 USAABB98046 1 19980422 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 613AU 27144 LAX - EMERGENCY FLOOR LIGHTING AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F RT A2NM 1998060500304 19980605 00304 WP 1998 6 5 USAAD98077 1 19980501 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 997VJ 47336 CMH - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 4 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POW ER SUPPLY. (X) 2 L 7 2 4F A6WE 1998060500305 19980605 00305 NM 1998 6 5 USAASB98103 1 19980425 A 3230 BACV10CD12 CHECK VALVE BOEING 737 737301 1384611 NM NLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 589US 23934 PIT - FL8051 - AFTER TAKEOFF AND LANDING GEAR 'UP' SELECTED, THE NOSE GEAR FAILED TO RETRACT. SELECTED GEAR 'DOWN' AND PERFORMED CHECKLIST. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. M AINTENANCE FOUND THE NOSE LANDING GEAR STEERING CHECK VALVE HAD FAILED. REPLACED CHECK VALVE. CYCLED GEAR NUMEROUS TIM ES. ALL TESTED GOOD. LEAK CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998060500306 19980605 00306 EU 1998 6 5 USAAF98037 1 19980425 A 3297 2011251244 WIRE HARNESS FOKKER F28 F28MK0100 4990807 EU RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 888AU 11357 CLT - FLT 1693 - EN ROUTE TO TYS, 'GND/FLT CTL' MESSAGE APPEARED ON MULTI FUNCTION DISPLAY. THIS MESSAGE APPEARED THEN RESET FIVE DIFFERENT TIMES. FLIGHT RETURNED TO CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDI NG GEAR UPPER HARNESS AND CONNECTOR J1120B. (M) 2 L 7 2 4F RT 1998060500307 19980605 00307 EU 1998 6 5 98ZZZX2058 1 19980425 A 3260 PVWOR1832SNL CONNECTOR FOKKER F28 F28MK0100 4990807 EU RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 888AU 11357 CLT - FLT 1693 - ENROUTE TO TYS, 'GND/FLT CTL' MESSAGE APPEARED ON MULTI-FUNCTION DISPLAY. THIS MESSAGE APPEARED THEN R ESET FIVE DIFFERENT TIMES. FLIGHT RETURNED TO CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDIN G GEAR UPPER HARNESS AND CONNECTOR J1120B. REF: OPER CONTROL NR USAAF98037. 2 L 7 2 4F RT 1998060500308 19980605 00308 EU 1998 6 5 USAAF98039 1 19980502 A 3230 715381 SELECTOR VALVE FOKKER F28 F28MK0100 4990807 EU ZONE 126 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 884US 16789 11338 PNS - FLT 243 - ON APPROACH TO PNS WHEN LANDING GEAR WAS SELECTED DOWN, NOSE GEAR DID NOT INDICATE DOWN AND LOCKED (NO G REEN 'SAFE'). CREW RECYCLED GEAR AND ALL THREE GEAR INDICATED DOWN AND LOCKED. FLIGHT LANDED PNS WITHOUT FURTHER INCID ENT. AIRCRAFT FERRIED TO CLT MAINTENANCE STATION WITH THE GEAR DOWN. CLT MAINTENANCE REPLACED THE NOSE LANDING GEAR SE LECTOR VALVE. GEAR SWING WAS NORMAL. (X) 2 L 7 2 4F RT 1998060500309 19980605 00309 WP 1998 6 5 USAAD98078 1 19980502 A 2130 94840213 AMPLIFIER DOUG DC9 DC931 3022065 WP E/E/ COMPARTMENT FAILED A USAA B EMER. DESCENT O OTHER CR CRUISE 1 EA 19 974VJ 47130 MCO - FLT 8564 - ENROUTE AT 31,000 FEET, THE PRESSURIZATION OUTFLOW VALVE MOVED RAPIDLY TO THE OPEN POSITION. THE CREW MANUALLY MOVED THE VALVE CLOSED AND DECLARED AN EMERGENCY. AFTER DESCENDING TO 20,000 FEET, THE CABIN PRESSURE STABILIZ ED. THE FLIGHT THEN CONTINUED TO THE DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PRESSURIZATION AMPLIFIER. (X) 2 L 7 2 4F A6WE 1998060500310 19980605 00310 EU 1998 6 5 RAIA980415 1 19980430 A 3310 GE328 BULB BAG JETSTM JETSTM3201 1500217 EU INST PANEL FAILED A RAIA B EMER. DESCENT N FALSE WARNING LD LANDING 1 CE 03 422AM 500 856 STL - FLT 7467 - CREW COULD NOT GET NOSE GEAR DOWN AND LOCKED INDICATION, FOLLOWED CHECKLIST. MAINTENANCE INSPECTED AND REPLACED NOSE GEAR INDICATOR BULBS. (X) 2 L 7 2 4T RT A56EU 1998060500311 19980605 00311 EU 1998 6 5 RAIA980414 1 19980430 A 7931 41SG107150G14 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 338TE 3407 932 STL - FLT 7424 - LEFT ENGINE OIL PRESSURE ABOVE RED LINE, ALL OTHER INDICATIONS NORMAL. MAINTENANCE REPLACED LEFT ENGIN E OIL PRESSURE TRANSDUCER. (X) 2 L 7 2 4T RT A56EU 1998060500312 19980605 00312 NE 1998 6 5 RAIA980413 2 19980430 A 7321 8058131005 EEC AEROSP ATR72 ATR72202 8680940 EU PWA PW120 PW124B NE LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CE 03 722TE 3528 220 PIA - FLT 7127 - LEFT ENGINE WOULD ONLY MAKE 30 PERCENT TORQUE ON TAKOEFF ROLL. MAINTENANCE REPLACED LEFT ENGINE ELECTR ONIC CONTROL UNIT. (X) 2 H 7 2 4T 4 T RT A53EU E2ONE 1998060500313 19980605 00313 EU 1998 6 5 RAIA980412 1 19980427 A 7931 31058872 PRESS REGULATOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 03 569HK 4441 41088 JFK - FLT 7779 - RIGHT ENGINE LOW OIL PRESSURE CAPTION ILLUMINATED, CREW PERFORMED ENGINE SHUTDOWN. MAINTENANCE REPLACE D RIGHT ENGINE OIL PRESSURE REGULATING VALVE, PERFORMED MAINTENANCE CHECK FLIGHT: RESULT SATISFACTORY. (X) 2 L 7 2 4T RT A41NM 1998060500314 19980605 00314 EU 1998 6 5 RAIA980411 1 19980427 A 3060 FUSE JETAIR JETSTM JETSTM4101 1500501 EU RT PROPELLER FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 558HK 6108 41071 STL - FLT 7478 - RIGHT PROPELLER DEICE FAILED ON TAKEOFF ROLL. MAINTENANCE REPLACED FUSE IN RIGHT POWER DISTRIBUTION UN IT. (X) 2 L 7 2 4T RT A41NM 1998060500315 19980605 00315 EU 1998 6 5 RAIA980410 1 19980428 A 2150 CA06R10SL3SF80 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LEFT AIR SHORTED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 342TE 11603 954 STL - FLT 7348 - LEFT AIR OFF CAPTION ILLUMINATED ON TAKEOFF ROLL. MIANTENANCE REPLACED LEFT AIR OFF PRESSURE SWITCH CO NNECTOR. (X) 2 L 7 2 4T RT A56EU 1998060500316 19980605 00316 EU 1998 6 5 RAIA980409 1 19980424 A 2611 721112111000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 557HK 2883 2431 41074 JFK - FLT 7782 - POD SMOKE CAPTION ILLUMINATED DURING CLIMB. MAINTENANCE INSPECTED AND REPLACED POD SMOKE DETECTOR. (X ) 2 L 7 2 4T RT A41NM 1998060500317 19980605 00317 EU 1998 6 5 RAIA980408 1 19980424 A 5630 137169C417 WINDOW BAG JETSTM JETSTM3201 1500217 EU RT EMER EXIT CRACKED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 432AM 14586 883 STL - FLT 7476 - CLIMBING THROUGH 7,000 FEET, THE RIGHT WING EMERGENCY EXIT OUTER PANE WINDOW CRACKED. MAINTENANCE REPL ACED RIGHT EMERGENCY EXIT WINDOW OUTER PANE. (X) 2 L 7 2 4T RT A56EU 1998060500318 19980605 00318 GL 1998 6 5 RAIA980407 3 19980422 A 6112 PROPELLER BAG JETSTM JETSTM3201 1500217 EU ROTOL R333 R333482F12 GL RIGHT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 339TE 13823 2085 935 DRG856289 STL - FLT 7468 - RIGHT PROPELLER DEICE SHOWS 30 AMPS ON FIRST CYCLE, ICE BUILDING ON PROPELLER. MAINTENANCE INSPECTED, FOUND BAD HEATER MAT ON NR 2 BLADE, MAINTENANCE REPLACED RIGHT PROPELLER. (X) 2 L 7 2 4T RT A56EU 6 C P61GL 1998060500319 19980605 00319 EU 1998 6 5 RAIA980406 1 19980423 A 7931 41SG107100G14 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA B EMER. DESCENT K N FLUID LOSS FALSE WARNING CR CRUISE 1 CE 03 559HK 4497 41075 JFK - FLT 7667 - RIGHT ENGINE OIL PRESSURE DROPPED TO ZERO, OIL CAPTION ILLUMINATED, CREW PERFORMED ENGINE SHUT DOWN. M AINTENANCE INSPECTED, FOUND RIGHT ENGINE OIL PRESSURE TRANSDUCER LEAKING. MAINTENANCE REPLACED RIGHT ENGINE OIL PRESSUR E TRANSDUCER. (X) 2 L 7 2 4T RT A41NM 1998060500320 19980605 00320 EU 1998 6 5 RAIA980502 1 19980506 A 2435 8260121A STARTER AEROSP ATR72 ATR72202 8680940 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 721TE 16197 1100 217 STL - FLT 7400 - RIGHT DC GENERATOR FAULTED AND WOULD NOT RESET. MAINTENANCE REPLACED RIGHT ENGINE STARTER GENERATOR. (X) 2 H 7 2 4T RT A53EU 1998060500321 19980605 00321 NE 1998 6 5 RAIA980501 2 19980504 A 7320 31055017 P2 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114GR 01514 NE LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 553HK 5086 104 41066 BOS - FLT 7707 - LEFT RED BETA LIGHT ILLUMINATED WHEN BOTH POWER LEVERS WERE ADVANCED ABOVE FLIGHT IDLE. MIANTENANCE IN SPECTED AND REPLACED LEFT ENGINE P2 INLET SENSOR. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1998060500322 19980605 00322 WP 1998 6 5 TWAA9807105 1 19980330 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 965 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND TEMPORARY REPAIR ON OUTER FUSELAGE SKIN AT STA 965, LONGERONS 13 AND 14L. R EPAIRED PER SRM 53-04, FIG 32, AND TWA STD PRACTICES. (X) 2 L 7 2 4F A6WE 1998060500323 19980605 00323 WP 1998 6 5 TWAA9807104 1 19980317 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 637 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON TO CANTED KEEL FORMER TIE CRACKED AT STA 637, APPROX 15 LBL. REPLAC ED TIE PER SRM 51-01, PAGE 1 ITEM C. SEALED REPAIR PER SRM 51-20-0. (X) 2 L 7 2 4F A6WE 1998060500324 19980605 00324 WP 1998 6 5 TWAA9807103 1 19980317 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 965 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND TEMPORARY REPAIR ON OUTER FUSELAGE SKIN AT STA 965, BETWEEN LONGERON 13 AND 14 RT SIDE. REPAIRED PER SRM 53-04, FIG 32, AND TWA STD PRACTICES. (X) 2 L 7 2 4F A6WE 1998060500325 19980605 00325 WP 1998 6 5 TWAA9807102 1 19980218 A 5412 FIREWALL ANGLE DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK FOUND ON NR 2 PYLON AFT FIREWALL A ONE INCH CRACK IN UPPER FLANGE, AT OTBD END APPR OX 40 INCHES AFT OF AFT ENGINE MOUNT. REPAIRED CRACKED ANGLE UPPER FLANGE ON AFT FIREWALL PER SRM 53-01. (X) 2 L 7 2 4F A6WE 1998060500326 19980605 00326 NM 1998 6 5 TWAA9807101 1 19980504 A 2781 834503 SENSOR BOEING 767 767231 1385131 NM NR 4 LE SLAT WORN A TWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 604TW 22567 SDQ - FLT 149 - AFTER FLAPS RETRACTED, GOT EICAS MESSAGE, LE SLAT ASYM WAS DISPLAYED WITH LEADING EDGE LIGHT ILLUMINATED . REPLACED NR 4 LE SLAT PROXIMITY SENSOR S285. CHECK-C 3-20-98 LAX. (X) 2 L 7 2 4F RT A1NM 1998060500327 19980605 00327 WP 1998 6 5 TWAA9807014 1 19980424 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 1250 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LIGHT CORROSION AROUND SCREW HOLES IN FLOOR MEMBRANE AT FS 1250, LBL 47 TO L BL 53. REMOVED CORROSION PER SRM 51-10-3. REPAIRED PER SRM 53-10 FIG 2. (X) 2 L 7 2 4F A6WE 1998060500328 19980605 00328 WP 1998 6 5 TWAA9807013 1 19980428 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 575 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON LOWER FUSELAGE, SKIN CORRODED ON TOP SIDE AT FS 575 TO FS 598. REMOVED AN D REPLACED DAMAGED DOUBLER AND TRIPLER PER SRM 51-01 ITEM 1, AND SRM 53-04, FIG 43. (X) 2 L 7 2 4F A6WE 1998060500329 19980605 00329 WP 1998 6 5 TWAA9807012 1 19980428 A 5330 SKIN DOUG DC9 DC933F 302207A WP RIGHT CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON LOWER FUSELAGE, RT KIDNEY PLATE, LOWER INBD CORNER, SKI SEPARATED WITH COR ROSION. REMOVED AND REPLACED DAMAGED DOUBLER AND TRIPLER PER SRM 51-01, ITEM 1, AND PER SRM 53-04, FIG 43 (SKIN). (X) 2 L 7 2 4F A6WE 1998060500330 19980605 00330 WP 1998 6 5 TWAA9807011 1 19980428 A 5320 CASTING DOUG DC9 DC933F 302207A WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK FOUND IN RT WHEEL WELL, RT 718 CASTING CRACKED BEYOND REPAIR ON FORWARD SIDE. REPL ACED RT 718 CASTING PER SB 53-131, AND SRM 51-01 PAGE 1, ITEM C. (X) 2 L 7 2 4F A6WE 1998060500331 19980605 00331 WP 1998 6 5 TWAA9807010 1 19980428 A 5347 TRACK DOUG DC9 DC933F 302207A WP BS 180-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK FOUND CORROSION ON RT OTBD GALLEY TRACK FROM STA 180 TO STA 237, 44 IN RBL. REPLAC ED SECTION OF TRACK PER SRM 51-01, PAGE 1 ITEM C, AND 51-30-0. (X) 2 L 7 2 4F A6WE 1998060500332 19980605 00332 WP 1998 6 5 TWAA9807009 1 19980408 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 985 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 989Z 47135 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND TEMPORARY REPAIR 3 INCHES BY 6 INCHES AT APPROX FS 985 BETWEEN L22R AND L23R . INSTALLED REPAIR PER ARA 11690 AND SRM 53-04, FIG 12B. (X) 2 L 7 2 4F A6WE 1998060500333 19980605 00333 WP 1998 6 5 TWAA9807008 1 19980417 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM FS 200, RBL 58 IN. REMOVED FLOOR SUPPORT BEAM AND IN STALLED NEW BEAM PER SRM 51-01 AND TWA STANDARD PRACTICES. (X) 2 L 7 2 4F A6WE 1998060500334 19980605 00334 WP 1998 6 5 TWAA9807007 1 19980422 A 5754 ANGLE DOUG DC9 DC982 3022082 WP NR 2 LE SLAT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND ANGLE BRACE CRACKED AND DOUBLER BELOW ALSO CRACKED, JUST INBD OF NR 2 LE SLA T INBD TRACK. MANUFACTURED ANGLE BRACE AND DOUBLER AND INSTALLED PER SRM 51-01, PAGE 1 ITEM C, AND STANDARD PRACTICES. (X) 2 L 7 2 4F A6WE 1998060500335 19980605 00335 NE 1998 6 5 TWAA9807002 2 19980503 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE LEFT FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CE 05 EIBWD 49575 3259 PDX - FLT 350 - LEFT ENGINE OIL FILTER STRAINER CLOGGING LIGHT CAME ON IN-FLIGHT. LIGHT STAYED ON WHEN THROTTLE WAS RET ARDED TO IDLE. SHUT DOWN ENGINE AND RETURNED TO PDX. REPLACED ENGINE. (X) 2 L 7 2 4F 4 F RT A6WE E9NE 1998060500337 19980605 00337 WP 1998 6 5 TWAA9807004 1 19980424 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP LT MLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI- DURING OP 15 MAINTENANCE CHECK, FOUND FORWARD INBOARD CORNER OF LT WHEEL WELL FAIRING SUPPORT STRUCTURE CRACKED, FW D AND AFT SIDES, LBL 6. INSTALLED REPAIR PER SRM 53-01. (X) 2 L 7 2 4F A6WE 1998060500338 19980605 00338 WP 1998 6 5 TWAA9807005 1 19980424 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 940 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK FOUND IN LT GEAR WHEEL WELL, FS 940 LBL 4, FRAME WEB CRACKED AND U-CHANNEL AFT SIDE OF WEB CRACKED IN 2 PLACES. INSTALLED REPAIR PER SRM 53-01 PAGE 9. (X) 2 L 7 2 4F A6WE 1998060500339 19980605 00339 WP 1998 6 5 TWAA9807006 1 19980414 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM CAP, FS 200, LBL 12 IN. REPLACED CAP PER SRM 51-01. (X) 2 L 7 2 4F A6WE 1998060500340 19980605 00340 NM 1998 6 5 EISA98102 1 19980424 A 3240 26011826 BRAKE BENDIX BOEING 727 727223 1384074 NM NR 3 BRAKE FAILED A EISA K NONE O OTHER LD LANDING 1 SW 07 315NE 3461 20190 ON LANDING AT PORTLAND (PDX), THE BRAKES WERE GRABBING AND PULSING THE BRAKE PEDALS. ON POST-FLIGHT FOUND NR 3 BRAKE P AD BROKEN INTO PIECES AND JAMMED IN WHEEL ASSEMBLY. GENERATED BY PILOT REPORT. REMOVED AND REPLACED NR 3 BRAKE ASSEMBL Y. OPS CHECK GOOD IAW 32-41-32. (X) 2 L 7 3 4F A3WE 1998060500341 19980605 00341 NM 1998 6 5 EISA98101 1 19980422 A 2611 SMOKE DETECTOR BOEING 727 72731 1384010 NM CABIN MALFUNCTIONED A EISA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 240NE 18906 IN-FLIGHT, MAIN CARGO SMOKE DETECTION ILLUMINATED. DEPARTED (CVG), UNSCHEDULED LANDING AT HARRISBURG, PENNSYLVANIA (MDT ), CONTINUED TO PHILADELPHIA (PHL). GENERATED BY PILOT REPORT. COMPLETED OPERATIONAL CHECK. OPERATION CHECK GOOD. IN SPECTION OF AFT CABIN FOUND MOISTURE TO CAUSE FALSE INDIICATION. OPERATION CHECK GOOD IAW MM 26-00. (X) 2 L 7 3 4F A3WE 1998060500342 19980605 00342 WP 1998 6 5 EISA98100 1 19980418 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 965 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND AFT CARGO PIT CORROSION AROUND NUTPLATE ON FLOORBEAM FS 965 RIGHT-HAND SID E. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-05, FIGURE 20 AND 51-30-2. TT: 66,670:41 HOURS. TC: 61,562. ( X) 2 L 7 2 4F A6WE 1998060500343 19980605 00343 WP 1998 6 5 EISA98099 1 19980418 A 5320 EXTRUSION DOUG DC9 DC931 3022065 WP BS 1098 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND RIGHT-HAND AFT LAV SUPPORT STRUCTURE CORRODED AT STA 1098. REMOVED AND RE PLACED EXTRUSION PER SRM 53-05. TT: 66,670:41 HOURS. TC: 61,562. (X) 2 L 7 2 4F A6WE 1998060500344 19980605 00344 WP 1998 6 5 EISA98098 1 19980418 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 579-680 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND FLOOR PANEL AT STA 579 TO STA 680, RIGHT-HAND OF CENTER, WITH C RACKED OUT FASTENER HOLES. FABRICATED AND INSTALLED REPAIR PER 53-03, 51-70-0, AND 51-30-2. TT: 66,670:41 HOURS. TC: 61,562. (X) 2 L 7 2 4F A6WE 1998060500345 19980605 00345 WP 1998 6 5 EISA98097 1 19980418 A 5321 FLOOR DOUG DC9 DC931 3022065 WP BS 579-680 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND LEFT-HAND CENTER FLOORBOARD, STA 579 TO STA 680, WITH 6 EACH FA STENER HOLES CRACKED OUT. FABRICATED AND INSTALLED REPAIR PER 53-05, 51-70-0, AND 51-30-2. TT: 66,670:41 HOURS. TC: 61,562. (X) 2 L 7 2 4F A6WE 1998060500346 19980605 00346 WP 1998 6 5 EISA98096 1 19980418 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP STA 737 TO 908 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND SEAT TRACK CORRODED AT STA 737, 757, 775, 850, 870, 887, AND 908, RIGHT-HA ND OUTBOARD TRACK. REPLACED RIGHT-HAND OUTBOARD TRACK FROM STA 737 TO STA 965 PER SRM 53-05. TT: 66,670:41 HOURS. TC : 61,562. (X) 2 L 7 2 4F A6WE 1998060500347 19980605 00347 WP 1998 6 5 EISA98095 1 19980418 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHEMNT OF CPCP WORKCARD, FOUND CORROSION ON RIGHT-HAND INBD SEAT TRACK AT STA 690, 718, 737, 756, 813, 83 2, 870, AND 889. CORROSION REMOVED FROM STA 690 - STA 737 AND MATERIAL LOSS WITHIN SRM LIMITS 53-05, FIG 4. REPLACED S EAT TRACK FROM STA 748 TO STA 965 PER SRM 53-05 AND SRM 51-30. TT: 66,670:41 HOURS. TC: 61,562. (X) 2 L 7 2 4F A6WE 1998060500348 19980605 00348 WP 1998 6 5 EISA98094 1 19980418 A 5320 STIFFENERS DOUG DC9 DC931 3022065 WP BS 160-200 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND RIGHT-HAND FLOOR PANEL AT STA 160 TO STA 200 WITH 2 CRACKED STIFFENERS. F ABRICATED AND INSTALLED NEW STIFFENERS PER SRM 53-21-0 AND SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1998060500349 19980605 00349 WP 1998 6 5 EISA98093 1 19980418 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1039 DENTED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, FOUND DENT 1.5 INCHES BY 1.75 INCHES AT FS 1039 BELOW CUSPLINE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-04 AND SRM 51-30-2. (X) 2 L 7 2 4F A6WE 1998060500350 19980605 00350 WP 1998 6 5 EISA98092 1 19980418 A 5730 SKIN DOUG DC9 DC931 3022065 WP WS 447.3 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF CPCP WORKCARD, CORROSION WAS FOUND ON LEFT-HAND WING TRAILING EDGE AT APPROXIMATELY STA XRS 447 .3 AS SEEN FROM BELOW. FABRICATED AND INSTALLED NEW SKIN AND DOUBLERS PER SRM 51-70-2. (X) 2 L 7 2 4F A6WE 1998060500351 19980605 00351 WP 1998 6 5 EISA98091 1 19980418 A 5220 BRACKET DOUG DC9 DC931 3022065 WP EMERGENCY DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF AD 80-02-06, NOTED ONE EACH BRACKET CRACKED ON AFT EMERGENCY DOOR. FABRICATED NEW BRACKET PER SRM 51-40-3 AND INSTALLED PER SRM 51-10-3. TT: 66,670:41 HOURS. TC: 61,562. (X) 2 L 7 2 4F A6WE 1998060500352 19980605 00352 NM 1998 6 5 RAAA98B1005 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM RT WING CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 56712 19093 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-112, FOUND HFEC CRACK INDICATION FWD 2 EA VERTICAL FASTENER HOLES OF RT WING BL 70.5 UPPER RIB CHORD. REPAIRED PER S/B 727-57-0112, REV 4 M-54 NR 008. 2 L 7 3 4F A3WE 1998060500353 19980605 00353 NM 1998 6 5 RAAA98B1006 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM LT WING CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 56712 19093 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-112, FOUND HFEC CRACK INDICATION FWD 2 EA VERTICAL FASTENER HOLES OF LT WING BL 70.5 UPPER RIB CHORD. REPAIRED PER S/B 727-57-0112, REV 5 M-54 NR 009. 2 L 7 3 4F A3WE 1998060500354 19980605 00354 NM 1998 6 5 RAAA98B1007 1 19980514 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 660 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 56712 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-52103, FOUND BS 660 FRAME SHEAR TIE CORRODED AT STR 27 -28L. REPAIR ED PER SRM 53-10-4 M-54 NR 011. 2 L 7 3 4F A3WE 1998060500355 19980605 00355 NM 1998 6 5 RAAA98B1008 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 623 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-52103, FOUND BS 623 FUSELAGE SKIN AND STR 28L SPLICE CORRODED. REPA IRED PER DWG NR 65C153782 AND SRM 53-10-3 M-54 NR 015. 2 L 7 3 4F A3WE 1998060500356 19980605 00356 NM 1998 6 5 RAAA98B1009 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 580 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-5210, FOUND BS 580 FRAME SHEAR TIE CORRODED AT STR 27L -28L. REPAIR ED PER SRM 53-10-4 M-54 NR 018. 2 L 7 3 4F A3WE 1998060500357 19980605 00357 NM 1998 6 5 RAAA98B1010 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 614-640 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-52103, FOUND STR 26L CORRODED AT BS 618 TO 640. REPLACED STR SECTIO N FROM BS 618 TO 680 PER SRM 53-10-3 M-54 NR 017. 2 L 7 3 4F A3WE 1998060500358 19980605 00358 NM 1998 6 5 RAAA98B1011 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 540-550 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-52103, FOUND STR 27L CORRODED AT BS 540 TO 550. REPAIRED PER SRM 53 -10-3 M-54 NR 020. 2 L 7 3 4F A3WE 1998060500359 19980605 00359 NM 1998 6 5 RAAA98B1012 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 540 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-52103, FOUND BS 540 FRAME SHEAR TIE CORRODED AT STR 27L -28L. REPAI RED PER SRM 53-10-4 M-54 NR 021. 2 L 7 3 4F A3WE 1998060500360 19980605 00360 NM 1998 6 5 RAAA98B1013 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 520 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-52103, FOUND BS 520 FRAME SHEAR TIE CORRODED AT STR 27L -28L. REPAI RED PER SRM 53-10-4 M-54 NR 024. 2 L 7 3 4F A3WE 1998060500361 19980605 00361 NM 1998 6 5 RAAA98B1014 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM WS 629 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-127, FOUND LT WS 629 RIB CRACKED AT S-6 AND S-10 ATTACHMENTS. RE PAIRED PER SRM 57-10-5 M-54 NR 063. 2 L 7 3 4F A3WE 1998060500362 19980605 00362 NM 1998 6 5 RAAA98B1015 1 19980514 A 5320 SILL BOEING 727 72722C 138400F NM BS 520-562 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-52103, FOUND FWD CARGO COMPT DOOR SILL WEB CORRODED AT BS 520 TO 562. REPLAC ED WEB PER SRM 51-10-1 M-54 NR 066. 2 L 7 3 4F A3WE 1998060500363 19980605 00363 NM 1998 6 5 RAAA98B1016 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 717 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED C1 CHECK PER CARD C 52003, FOUND BS 717 FUSELAGE SKIN INTERIOR CORRODED AT STR 27L TO 28L. REPAIRED PE R DWG NR 65C15378 M-54 NR 081. 2 L 7 3 4F A3WE 1998060500364 19980605 00364 NM 1998 6 5 RAAA98B1017 1 19980514 A 5320 CHORD BOEING 727 72722C 138400F NM BS 1342 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED C1 CHECK, FOUND UPPER RT TORQUE BOX INBD CHORD CORRODED WITH 2.75 IN. CRACK AT FS 1342. REPAIRED PER S /B 727-55-0076 M-54 NR 086. 2 L 7 3 4F A3WE 1998060500365 19980605 00365 NM 1998 6 5 RAAA98B1018 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 450-475 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND STR 28L CORRODED AT BS 450 TO 475. REPLACED STRINGER SECTION PE R SRM 51-10-1 M-54 NR 090. 2 L 7 3 4F A3WE 1998060500366 19980605 00366 NM 1998 6 5 RAAA98B1019 1 19980514 A 5320 SPLICE BOEING 727 72722C 138400F NM BS 740 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S3 INSPECTION PER CARD S3-53102, FOUND STR 24L END SPLICE CORRODED AT BS 740. REPLACED STRINGER END SP LICE PER SRM 51-10-1 AND 53-10-3 M-54 NR 094. 2 L 7 3 4F A3WE 1998060500367 19980605 00367 NM 1998 6 5 RAAA98B1020 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 688 GOUGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED C1 CHECK PER CARD C-96002, FOUND BS 688 FUSELAGE EXTERIOR SKIN GOUGED AT STR 25R. REPAIRED PER SRM 53- 30-3, FIG 1 M-54 NR 097. 2 L 7 3 4F A3WE 1998060500368 19980605 00368 NM 1998 6 5 RAAA98B1021 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 540-567 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED C1 CHECK PER CARD C-52003, FOUND STR 26R UPPER CHORD CORRODED AT BS 540 TO 567. REPLACED UPPER CHORD P ER SRM 51-10-1 M-54 NR 098. 2 L 7 3 4F A3WE 1998060500369 19980605 00369 NM 1998 6 5 RAAA98B1022 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 545 DAMAGED A RAAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-52103, FOUND PREVIOUS FUSELAGE SKIN REPAIR NOT PER SRM AT BS 545, STR 27L. R EPAIRED PER SRM 53-30-3, PG 8, FIG 1 M-54 NR 102. 2 L 7 3 4F A3WE 1998060500370 19980605 00370 NM 1998 6 5 RAAA98B1023 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 460-464 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND STR 21R CORRODED AT BS 460 AND 464. REPAIRED PER SRM 53-10-3 M- 54 NR 110. 2 L 7 3 4F A3WE 1998060500371 19980605 00371 NM 1998 6 5 RAAA98B1024 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 461-466 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND STR 22R CORRODED AT BS 461 AND 466. REPAIRED PER SRM 53-10-3 M- 54 NR 111. 2 L 7 3 4F A3WE 1998060500372 19980605 00372 WP 1998 6 5 CALA9800906 1 19980528 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP RT WING/BODY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 3.75 CRACK COMING FROM SCREW HOLE IN RT WING UPPER WING TO BODY FAIRING BONDED DOUBLER. A DOUBLER WA S FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3. 2 L 7 2 4F A6WE 1998060500373 19980605 00373 WP 1998 6 5 CALA9800907 1 19980528 A 5720 DOUBLER DOUG DC9 DC932 3022066 WP WS 444.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1.5 CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT WS 444.5. THE DOUBLER WAS REMOVED. A REPAI R WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2. 2 L 7 2 4F A6WE 1998060500374 19980605 00374 WP 1998 6 5 CALA9800908 1 19980528 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERTICAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND INTERIOR CRACKS ON VERTICAL FIN LEADING EDGE FORWARD OF PITOT TUBE AROUND COUNTER SINK. DOUBLER AND FIL LER WERE FABRICATED AND INSTALLED IAW SRM 55-01, FIGURE 2. 2 L 7 2 4F A6WE 1998060500375 19980605 00375 WP 1998 6 5 CALA9800909 1 19980528 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND SEVERAL CRACKS IN RT NR 61 FLOORBOARD. A FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51- 30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998060500376 19980605 00376 WP 1998 6 5 CALA9800910 1 19980528 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 466 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CRACKS IN FORWARD PIT FRAME AT FS 466, STRINGER 29L. THE CRACKS WERE STOP DRILLED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998060500377 19980605 00377 WP 1998 6 5 CALA9800911 1 19980528 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A 1 CRACK IN NR 4 HORIZONTAL BEAM AT FORWARD END INSIDE FORWARD SERVICE DOOR. THE BEAM WAS REMOVED AND A NEW BEAM WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998060500378 19980605 00378 WP 1998 6 5 CALA9800912 1 19980528 A 5230 SKIN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND THREE .25 CRACKS IN EDGE OF FORWARD CARGO DOOR SKIN AT HANDLE. THE CRACKS WERE TRIMMED OFF AND A SCUFF PLATE WAS INSTALLED IAW SRM 52-05, FIGURE 30. 2 L 7 2 4F A6WE 1998060500379 19980605 00379 NM 1998 6 5 CALA9800913 1 19980529 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND LT INBOARD SEAT TRACK IN AFT GALLEY AT STA 947.5 CORRODED. A SEAT TRACK REPAIR WAS INSTALLED IAW SRM 5 3-00-52. 2 L 7 2 4F RT A16WE 1998060500380 19980605 00380 NM 1998 6 5 CALA9800914 1 19980529 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 947-967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND ANGLE CORRODED AT AFT GALLEY NEAR L-2 DOOR THRESHOLD AREA, STA 947 TO 967. A NEW ANGLE WAS INSTALLED I AW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1998060500381 19980605 00381 NM 1998 6 5 CALA9800915 1 19980531 A 5754 SKIN BOEING 737 7373T0 1384582 NM NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND THREE .25 CRACKS COMING FROM RIVETS IN NR 1 SLAT LOWER SKIN BETWEEN OUTBOARD MAIN TRACK AND OUTBOARD AU X TRACK. A REPAIR WAS INSTALLED IAW BOEING DRAWING NR 65C30133. 2 L 7 2 4F RT A16WE 1998060500382 19980605 00382 WP 1998 6 5 CALA9800916 1 19980529 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 CRACK IN FLOOR PANEL ATTACH ANGLE AT FS 680, LBL 4. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REP AIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1998060500383 19980605 00383 WP 1998 6 5 CALA9800917 1 19980530 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 955 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A CRACK OUT OF UPPER FASTENER HOLE BEHIND ANGLE BRACKET IN LONGERON 17L AT FS 955. THE ANGLE BRACKET W AS ALSO CRACKED. THE LONGERON AND ANGLE BRACKET WERE REMOVED. A NEW LONGERON AND BRACKET WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-1, 51-10-4, 51-10-3, 51-30-2, AND 51-30-1. 2 L 7 2 4F A6WE 1998060500384 19980605 00384 NE 1998 6 5 9809416632 2 19980528 A 7261 OIL SYST BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 1 ENGINE HIGH CONSUMPTION A NWAA A J UNSCHED LANDING DUMP FUEL O OTHER CR CRUISE 1 GL 01 632US 23112 715209 DURING CRUISE, THE CREW NOTICED WHAT APPEARED TO BE HIGH OIL CONSUMPTION ON THE NR 1 ENGINE. THE FLIGHT DIVERTED TO ANC AND LANDED WITHOUT DIFFICULTY. MAINTENANCE SERVICED THE ENGINE OIL AND INSPECTED THE ENGINE FOR OIL LEAKS INCLUDING AN ENGINE RUN WITH NO LEAKS NOTED. THE ENGINE WAS PLACED ON OIL MONITOR AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1998060500385 19980605 00385 1998 6 5 COMA9810129 4 19980528 A 3425 6226190204 AHRS EMB 120 EMB120RT SO E/E COMPT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 269CA 18799 6437 120263 PILOTS AHRS FAILED. REPLACED NR 1 AHRS. 2 L 7 2 4T RT A31SO 1998060500386 19980605 00386 EA 1998 6 5 COMA9860117 1 19980520 A 5330 601R3110519 SKIN CNDAIR CL600 CL6002B19 EA PAX DOORWAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 958CA 7111 DAMAGE WAS DISCOVERED TO PAX DOOR CUTOUT LOWER FORWARD CORNER. AIRCRAFT WAS FERRIED TO WVAC WHERE REPAIRS WERE COMPLETE D IN ACCORDANCE WITH REO 601R-53-21-165. 2 L 7 2 4F RT A21EA 1998060500387 19980605 00387 EA 1998 6 5 COMA9860118 1 19980523 A 5753 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 3893 7145 C CHECK INSPECTION, LEFT HAND INBOARD FLAP VANE HAS CHAFE DAMAGE. REPLACED FLAP VANE LEADING EDGE SKIN. 2 L 7 2 4F RT A21EA 1998060500388 19980605 00388 EA 1998 6 5 COMA9860119 1 19980523 A 5753 601R1430342 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 971CA 7145 C CHECK TASK 002-27-680-100, RIGHT HAND FLAP VANCE INBOARD HAS EXCESSIVE CHAFE DAMAGE. REPLACED FLAP VANE LEADING EDGE SKIN. 2 L 7 2 4F RT A21EA 1998060500389 19980605 00389 EA 1998 6 5 COMA9860120 1 19980523 A 5320 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 071CA 3893 7145 C CHECK INSPECTION, CARGO FLOOR SUPPORT ANGLE AT FS 621 IS CRACKED. REPAIRED FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 A. 2 L 7 2 4F RT A21EA 1998060500390 19980605 00390 EA 1998 6 5 COMA9860121 1 19980523 A 2750 601R93106105 FLEX SHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 071CA 7145 C CHECK TASK 002-12-680-100, RIGHT HAND FLAP NR 1 FLEX DRIVE SHAFT HAS STRAND SEPARATION. REPLACED FLEX CABLE. 2 L 7 2 4F RT A21EA 1998060500391 19980605 00391 EA 1998 6 5 COMA9860122 1 19980528 A 2750 7804011 FLAP LEVER CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 938CA 9279 7046 FLAPS FAILED AT 20 DEGREES. REPLACED FLAP CONTROL LEVER. 2 L 7 2 4F RT A21EA 1998060500392 19980605 00392 EA 1998 6 5 COMA9860123 1 19980529 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA CABIN DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 954CA 7100 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. ADJUST CABIN DOOR LATCH MECHANISM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1998060500393 19980605 00393 NE 1998 6 5 COMA9860124 2 19980531 A 7321 CONTROL UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 933CA 7040 LEFT ENGINE DOES NOT RESPOND TO POWER LEVER MOVEMENT, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED THE ELECTRONIC SPEED CONTROL SYSTEM. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998060500394 19980605 00394 EA 1998 6 5 COMA9860125 1 19980522 A 4980 1079900004 CLAMP CNDAIR CL600 CL6002B19 EA APU EXHAUST BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 DURING C CHECK, FOUND APU EXHAUST CLAMP BROKEN. REPLACED CLAMP. 2 L 7 2 4F RT A21EA 1998060500395 19980605 00395 EA 1998 6 5 COMA9860126 1 19980522 A 4980 601R9720413 SHIELD CNDAIR CL600 CL6002B19 EA APU EXHAUST CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 DURING 'C CHECK, FOUND APU EXHAUST SHIELD CRACKED. REPLACED SHIELD. 2 L 7 2 4F RT A21EA 1998060500396 19980605 00396 EA 1998 6 5 COMA9860127 1 19980523 A 3610 401059101 BRACKET CNDAIR CL600 CL6002B19 EA RT PYLON CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 DURING 'C' CHECK, FOUND RIGHT ENGINE 14TH STAGE BLEED AIR DUCT INSULATION DAMAGED. REPLACED HEAT BRACKET. 2 L 7 2 4F RT A21EA 1998060500397 19980605 00397 EA 1998 6 5 COMA9860128 1 19980522 A 5320 601R3520553 BRACKET CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 DURING 'C' CHECK, FOUND CARGO DOOR STEP PLATE BRACKET P/N 601R 35205-53 BROKEN. REPLACED BRACKET. 2 L 7 2 4F RT A21EA 1998060500398 19980605 00398 EA 1998 6 5 COMA9860129 1 19980522 A 5230 601R3520521 BRACKET CNDAIR CL600 CL6002B19 EA CARGO COMPT BENT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 DURING 'C' CHECK, FOUND CARGO DOOR STEP PLATE BRACKET, P/N 601R35205-21, BENT BEYOND REPAIR. REPLACED BRACKET. 2 L 7 2 4F RT A21EA 1998060500399 19980605 00399 EA 1998 6 5 COMA9860130 1 19980531 A 5297 WIRE HARNESS CNDAIR CL600 CL6002B19 EA PAX DOOR WARNING DEFECTIVE A COMA I B A CABIN DEPRESSURIZATION EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 946CA 7072 CABIN DOOR WARNING DURING CRUISE AT 26,000 FEET, PERFORMED EMERGENCY DEPRESSURIZATION AS PER QRH LANDED SAFELY AT BMI. R EPLACED DEFECTIVE SECTIONS OF DOOR WARNING WIRING HARNESS, WIRE NR MB20C22 AND WIRE NR MB67B22 AT CONNECTOR P1MB. 2 L 7 2 4F RT A21EA 1998060500400 19980605 00400 NM 1998 6 5 UPS98226822 1 19980528 A 2170 COALESCER BAG BOEING 727 727247 138408F NM CABIN DIRTY A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 211UP 21700 CREW REPORTED STRONG FUMES IN COCKPIT SHUT DOWN PAX INFLIGHT, PREVIOUS WRITE-UP SDF, MX DEFERED APU M 152622. SUBMITTER STATES, SUSPECT FUEL FUMES, VAPORS IN COALESTER BAGS AOG NEW BAGS AND O-RINGS FOR T-FITTING FOR SOLENOID VALVE. REPLAC ED BAGS AND O-RINGS TO FUEL SOLENOID VALVE RAN ENGINE FOR SEVERAL HRS NO VAPORS NOTED. 2 L 7 3 4F A3WE 1998060500401 19980605 00401 NM 1998 6 5 UPS98226830 1 19980516 A 5754 69284809 RIB BOEING 727 72725C 138400H NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, CRACK GROWING PAST STOP DRILL HOLD IN NR 4 SLAT I/B END RIB. REMOVED CRACKED RIB AND REPLACED WITH N EW ITEM PER SRM 51-30-2 AND SRM 20-50-01. 2 L 7 3 4F A3WE 1998060500402 19980605 00402 NM 1998 6 5 UPS98226831 1 19980519 A 5754 SKIN BOEING 727 72725C 138400H NM NR 4 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, CRACK GROWING PAST STOP DRILL HOLE IN NR 4 SLAT, I/B TRACK, O/B SIDE OF SKIN SUPPORT ANGLE. STOP DRI LLED END OF CRACK, NDT VERIFIED CONTAINMENT, RE-INSTALLED EXISTING REPAIR IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1998060500403 19980605 00403 NM 1998 6 5 UPS98226832 1 19980529 A 5330 SKIN BOEING 727 72725C 138400H NM BS 1179 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, CORROSION (C53-100-01.00-05) ON SKIN BS 1179, LBL 60, WL 250. REMOVED DAMAGED AREA AND INSTALLED FIL LER AND REPAIR DOUBLER PER UPS SRM 53-30-3, FIG 3A, AND 51-30-2. 2 L 7 3 4F A3WE 1998060500404 19980605 00404 NM 1998 6 5 UPS98226833 1 19980516 A 5414 SKIN BOEING 727 72725C 138400H NM BS 1130-1145 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C, CORROSION (C53-100-01.01-05) AND POPPED RIVET HEAD ON SKIN LAP LEFT SIDE OF NR 2 ENGINE INLET BS 1130 -1145, LBL 20-30, WL 290. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-30-1 IN AND AREA OF 8 BY 8. DAMAGED SKIN REMO VED AND A STANDARD SKIN LAP REPAIR ACCOMPLISHED PER SRM 53-30-3, SRM 51-10-2, MM 51-20-13 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998060500405 19980605 00405 NE 1998 6 5 UPS98426823 2 19980529 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7A 52054 NE NR 2 DAMAGED A IPXA C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 SO 01 682UP 20349 662255 NR 2 ENGINE WOULD NOT MAKE TAKEOFF POWER. ABORTED TAKEOFF. FOUND LPT DAMAGED. REPLACED NR 2 ENGINE. 2 L 7 4 4F 4 F A20WE E20EA 1998060500406 19980605 00406 WP 1998 6 5 UPS98826824 1 19980521 A 5320 47585141 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, FITTING AT STA 1180, LONG 35L IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-3- 0. 2 L 7 4 4F RT 4A25 1998060500407 19980605 00407 WP 1998 6 5 UPS98826825 1 19980521 A 5320 37584962N FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, FITTING AT STA 1180, LONG 35R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758496 AND SRM 51-3- 0. 2 L 7 4 4F RT 4A25 1998060500408 19980605 00408 WP 1998 6 5 UPS98826826 1 19980521 A 5320 4758514501 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, FITTING AT STA 1180, LONG 33R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-3- 0. 2 L 7 4 4F RT 4A25 1998060500409 19980605 00409 WP 1998 6 5 UPS98826827 1 19980521 A 5320 37584971N FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, FITTING AT STA 1180, LONG 35L IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758497 AND SRM 51-3- 0. 2 L 7 4 4F RT 4A25 1998060500410 19980605 00410 WP 1998 6 5 UPS98826828 1 19980522 A 5320 975494962 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1160-1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, INTERCOSTAL AT LONG 33R BTWN STA 1160-1180 IS CRACKED AND HAS LIGHT CORROSION. REMOVED, FABRICATED A ND REPLACED INTERCOSTAL IAW DWG 9754949 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998060500411 19980605 00411 WP 1998 6 5 UPS98826829 1 19980513 A 5347 58876231 CARGO TRACK DOUG DC8 DC873F 302199F WP BS 435 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 802UP 46100 INSPECTION TYPE:C, STA 435 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW D WG 5887623 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998060500412 19980605 00412 NM 1998 6 5 QXEA9800685 1 19980529 A 3397 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN DAMAGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 358PH 506 PDX - FORWARD FLOOR EMERGENCY PROX LIGHT BULBS BURNED OUT. REPAIRED SPLICE E35. OPERATIONAL CHECK GOOD. NO PARTS REPL ACED. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998060500413 19980605 00413 NM 1998 6 5 QXEA9800686 1 19980530 A 3350 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 348PH 484 SEA - MISCELLANEOUS CABIN EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY AT 3350 PSI WITH BATTERY. OPS CHECKS GOOD. AIR CRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998060500414 19980605 00414 1998 6 5 98FDEA00371 4 19980529 A 3417 HG480B13 CADC BOEING 727 72725C 138400H NM E/E COMPT FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 127FE 19719 98-0140, AT ROTATION OFF FLAG APPEARED IN THE CAPTAIN'S ALTIMETER AND NEEDLES FROZE AT 50 FT INDICATED ALTITUDE. OFF FL AG WENT OUT OF VIEW WHEN DESCENDING BELOW 50 FT ON LANDING. REMOVED AND REPLACED NR 1 CADC AND CAPTAIN'S ALTIMETER INDI CATOR PER MAINTENANCE MANUAL 34-12-23 AND 34-12-11 LOW LEVEL LEAK CHECKS GOOD PER 34-12-25 AND 21. 2 L 7 3 4F A3WE 1998060500415 19980605 00415 1998 6 5 98FDEA00372 4 19980529 A 3444 GPWS BOEING 727 72725C 138400H NM E/E COMPT MALFUNCTION A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 136FE 19855 98-0141 - GPWS WARNING FOR GEAR AT 500 FT ABOVE GROUND LEVEL (FULL LANDING CONFIGURATION). DURING TROUBLE SHOOTING PROC ESS, FOUND TAILSKID CANNON PLUG. INSTALLED GEAR PINS AND CYCLED GEAR AND FLAPS SEVERAL TIMES. ALL INDICATIONS WERE NOR MAL. GPWS CHECKED NORMAL PER M/M 34-52-3, PAGE 102. SYSTEM OK FOR NORMAL SERVICE. 2 L 7 3 4F A3WE 1998060500416 19980605 00416 1998 6 5 98FDEA00373 2 19980519 A 7260 WASHER AIRBUS 310 A310203 EU GEARBOX OUT OF POSITION A FDEA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 25 410FE 356 98-0133, NR 1 OIL QTY WAS 16 QTS ON GRND AT LEVEL OFF FL 310 12 QTY. STARTED TIMING THE DROP AT 7 QTS, LOST 1 QT PER 7 MIN. PRECAUTIONARY LANDING IN DEN. WHEN WE LANDED ANALOG AND ECAM SHOWED 4 QTS. REMOVED WASHER LODGED BETWEEN SEAL AN D AFT CASE OF TOWER SHAFT GEAR BOX. LEAK CHECKS OK. SERVICED WITH 11 QTS OIL. 2 L 7 2 4F RT A35EU 1998060500417 19980605 00417 NM 1998 6 5 98FDEA00374 1 19980529 A 2910 6556235159 PANEL BOEING 727 7272S2F 1384O81 NM HYD SERVICE MISSING A FDEA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 210FE 22932 98-0142, PANEL MISSING FOR HYDRAULIC SYSTEM B. INSTALLED MISSING HYDRAULIC ACCESS PANEL AND HARDWARE, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1998060500418 19980605 00418 EU 1998 6 5 98FDEA00375 1 19980529 A 2130 CONTROL AIRBUS 310 A310222 3930315 EU CABIN FAILURE A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 419FE 345 98-0143, STA-TPE, LOSS OF CABIN PRESS CLIMBING TO FL310. CABIN PRESS CONTINUED TO CLIMB PAST 10000 FT. AUTO PRESS WAS INEFFECTIVE A DESCENT WAS BEGUN AND MANUAL PRESS BROUGHT PRESS BELOW 10000 FT. UPON DESCENDING BELOW 18000 FT FLIGHT RE MAINED IN MANUAL PRESS MODE. A/C RELEASED FOR SERVICE PER MEL/CDL 21-44. PERFORMED THE CPC 1 AND 2 TEST FOUND CPC NR 1 TEST FAILURE. TRIED TO REPLACE WITH NEW CONTROLLER, NO HELP. ITEM DEFERRED PER MEL 21-44. C/B PULLED. NR 1 CPC BITE TEST SHOWED TORQUE MOTOR CONTROL FAILED, THE ORIGINAL CPC WAS REINSTALLED. 2 L 7 2 4F RT A35EU 1998060500419 19980605 00419 EU 1998 6 5 98FDEA00376 1 19980529 A 7932 8TJ146AAA1 TRANSMITTER AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE DEFECTIVE A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 670FE 777 98-0144, NR 2 ENG OIL QTY AT TOP OF CLIMB STARTED A RATE OF 1 QT PER 10 TO 15 MIN DECREASE. DURING DESCENT AND APPROACH IT WENT BACK TO NORMAL. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL 79-1A. NR 2 ENG OIL QTY CHECKED 20 QTS. MONITOR OI L TEMP ON ECAM. NR 2 OIL QTY TRANSMITTER WAS REPLACED AT THE NEXT STATION ANCHORAGE. 2 L 7 2 4F RT A35EU 1998060500420 19980605 00420 NM 1998 6 5 98FDEA00377 1 19980527 A 3610 CLAMP BOEING 727 727233 138408A NM NR 3 ENGINE LOOSE A FDEA O OTHER J WARNING INDICATION CR CRUISE 1 SO 25 265FE 21671 98-0145, NUMBER 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT WITH WING ANTI-ICE OFF, LIGHT WENT OUT WHEN THROTTLE WAS RETARDED. RAN ENGINE FOUND CLAMP ON DUCT COMING FROM THE PRECOOLER LEAKING. TIGHTENED CLAMP, RAN ENGINE AGAIN LEA K CHECKED GOOD. OPERATIONAL CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1998060500421 19980605 00421 NM 1998 6 5 98FDEA00378 1 19980528 A 5243 6556235159 DOOR BOEING 727 727225 1384077 NM HYD SERVICE MISSING A FDEA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 469FE 21581 98-0146, HYDRAULIC SERVICE DOOR MISSING. INSTALLED MISSING DOOR WITH NEW UNIT PER MAINTENANCE MANUAL 52-00-5 PAGE 2, OP ERATION GOOD. 2 L 7 3 4F A3WE 1998060500422 19980605 00422 NM 1998 6 5 98FDEA00379 1 19980512 A 5311 FRAME BOEING 727 727225 1384077 NM BS 500 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 NR 0328, FWD LOWER CARGO. DAMAGED BELLFRAME, BS 500, STR 23 TO 24R. REPAIRED BELLFRAME BS 500 PER SRM 53-10-04. 2 L 7 3 4F A3WE 1998060500423 19980605 00423 NM 1998 6 5 98FDEA00380 1 19980520 A 5314 KEEL BEAM BOEING 727 727225 1384077 NM BS 872 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 NR 0507 71C503-00, KEEL BEAM BS 872, ABOVE FWD 870 KEEL BEAM FITTING CHORD CRACKED IN RADIUS THROUGH 2ND FASTENER LEFT S IDE. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER EA 7-5310-29533 AND SERVICE BULLETIN 727-53-208. 2 L 7 3 4F A3WE 1998060500424 19980605 00424 NM 1998 6 5 98FDEA00381 1 19980521 A 5311 FRAME BOEING 727 727225 1384077 NM BS 580 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 NR 0322 71C207-00, LOWER FWD, CARGO BELLFRAME DAMAGED ABOVE STR 25L TO STR 24L BS 580. REMOVED DAMAGED AREA, INSTALLED REPAIR DOUBLER PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998060500425 19980605 00425 NM 1998 6 5 98FDEA00382 1 19980521 A 5311 FRAME BOEING 727 727225 1384077 NM BS 1090 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 NR 1321 71C709-02, AFT LWR CARGO 2 EA DENTS IN BELLFRAME BS 1090, STR 26L - 27L. REMOVED DAMAGED AREA OF FRAME PER SRM 53-10-4. INSTALLED REPAIR DOUBLER PER SRM 53-10-4 FIG 1 PG 3 AND 4. 2 L 7 3 4F A3WE 1998060500426 19980605 00426 NM 1998 6 5 98FDEA00383 1 19980527 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 152FE 18285 NR 0866, UPPER LOBE, BS 620, LBL 63 - RBL 8, FLOORBEAM CORRODED. REMOVED CORROSION PERFORMED FLOORBEAM REPAIR FROM RBL 9- LBL 39, BS 620, PER SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 1998060500427 19980605 00427 NM 1998 6 5 98FDEA00384 1 19980527 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 152FE 18285 NR 0914, UPPER LOBE BS 680, CORROSION ON FLOORBEAM RBL 2 - RBL 13. REMOVED CORROSION REPAIRED PER 53-10-07 IN SRM. 2 L 7 3 4F A3WE 1998060500428 19980605 00428 WP 1998 6 5 MWEA98630 1 19980530 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 639 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACK ON LONGERON 5R AT STATION 639. MAINTENANCE FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998060500429 19980605 00429 WP 1998 6 5 MWEA98631 1 19980531 A 3350 1001191 LIGHT DOUG DC9 DC915 3022036 WP CABIN DIM A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 900ME 45841 THE PORTABLE EMERGENCY LIGHT FOUND DIM. MAINTENANCE INSTALLED SERVICEABLE PORTABLE EMERGENCY LIGHT. 2 L 7 2 4F A6WE 1998060500430 19980605 00430 WP 1998 6 5 MWEA98632 1 19980531 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 602ME 48133 FOUND THE EMERGENCY LIGHT FROM SEAT ROW 18 AFT INOP. MAINTENANCE REPLACED BATTERIES IN EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1998060500431 19980605 00431 WP 1998 6 5 MWEA98633 1 19980531 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 207ME 47794 THE FORWARD ENTRANCE DOOR SLIDE COVER ASSEMBLY FELL OFF. MAINTENANCE REINSTALLED SLIDE COVER ASSEMBLY. 2 L 7 2 4F A6WE 1998060500432 19980605 00432 WP 1998 6 5 MWEA98634 1 19980529 A 5320 99124515 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 305 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FOUND CORROSION ON SHEAR TIE AT STATION 305 BETWEEN LONGERON 29L AND 29R. MAINTENANCE FABRICATED AND INSTALLED SHEAR TI E. 2 L 7 2 4F A6WE 1998060500433 19980605 00433 NM 1998 6 5 MWEA98635 1 19980530 A 3350 60030431 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 601ME 49762 THE FORWARD SECTION EMERGENCY FLOOR TRACK WON'T EXTINGUISH. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 1998060500434 19980605 00434 WP 1998 6 5 MWEA98636 1 19980529 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE FELL OFF A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 401ME 47133 THE FORWARD PASSENGER DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1998060500435 19980605 00435 NM 1998 6 5 SCNA98706 1 19980515 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 580-560 CORRODED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND IN FORWARD CARGO AREA STRINGER 28L STATION 580 TO 560. REMOVED DAMAGED AREA, FOUND TO BE OUT OF LIMITS IAW 511006. FABRICATED REPAIR PARTS MATERIAL ID 7075 T6 IAW B727 SRM 531003. TREATED A ND PRIMED IAW B727 SRM 5101006. INSTALLED IAW SRM 531003. 2 L 7 3 4F A3WE 1998060500436 19980605 00436 NM 1998 6 5 SCNA98707 1 19980515 A 5320 INTERCOSTAL BOEING 727 727225 1384077 NM BS 318 MISDRILLED A SCNA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK, A .5 INCH HOLE DRILLED AND WALLOWED OUT AT FOREWARD ENTRY DOOR FLOOR AND THRESHOLD SUPPORT INTERCOASTAL STATION 318. ROUTED OUT DAMAGE, FOUND TO BE OUT OF LIMITS IAW B727 SRM 514004. FABRICATED REPAIR PARTS FR OM MATERIAL 2024 T3 .080 IAW SRM 531004. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED REPAIR PARTS IAW B727 SRM 5 14004. 2 L 7 3 4F A3WE 1998060500437 19980605 00437 NM 1998 6 5 SCNA98049 1 19980523 A 3350 1155981 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A LINE CHECK, FOUND THE EMERGENCY TRACK LIGHTING INOPERATIVE AT SEATS'S 5ABC, 28DEF AND 29DEF. REMOVED AND REPLA CED THE EMERGENCY TRACK LIGHTING PIGTAILS AT SEATS 5ABC, 28DEF AND 29DEF. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998060500438 19980605 00438 NM 1998 6 5 SCNA98050 1 19980523 A 3350 1155591 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A LINE CHECK, FOUND AN EMERGENCY LIGHT OUT AT THE R1 DOOR EXIT. REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT LIGH T ASSEMBLY AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998060500439 19980605 00439 1998 6 5 SCNA98051 4 19980530 A 2397 WIRE DOUG DC10 DC1010 3022110 WP CABIN FAILED A SCNA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 571SC 46645 A SMOKE SMELL AT ROW 22ABC. FOUND WIRES BURNT UNDER SEAT 22E TRACK. TAPED AND INSULATED INDIVIDUAL WIRES AND UNPLUGGED UNDERSEAT BURNT DECODER HARNESSES. PLACED SEATS ON MEL. REMOVED AND REPLACED MUX CABLE AT SEAT 22C. SEATS OPERATIONA LLY CHECK GOOD REMOVED MEL. 2 L 7 3 4F A22WE 1998060500440 19980605 00440 NM 1998 6 5 RRXA98220 1 19980528 A 2612 65249203 DETECTOR BOEING 727 727222 1384073 NM AFT LOWER BODY FAILED A RRXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 7638U 19911 LOWER AFT BODY OVER-HEAT LIGHT ILLUMINATED IN CRUISE, AFTER COMPLETING ENTIRE EMERGENCY CHECK-LIST LIGHT REMAINED ILLUMI NATED. PRECAUTIONARY LANDING MADE. REMOVED AND REPLACED FIRE DETECTION DETECTOR UNIT, GND RUN-UP NORMAL. 2 L 7 3 4F A3WE 1998060500441 19980605 00441 WP 1998 6 5 RRXA98221 1 19980529 A 3397 WIRE DOUG DC8 DC863F 302198F WP COCKPIT BROKEN A RRXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 957R 46137 STRONG ELEC ODOR DEVELOPING IN COCKPIT. TURNED OFF MAX WHITE LIGHTS. ODOR DISSIPATED. DEFERRED PER MEL 33-1 CAT 'C' D UE 6-9-98 CONT NR 805491. PLACARD INSTALLED, CONNECTOR DISCONNECTED. FOUND 2 WIRES BROKEN AT CONNECTOR. 2 L 7 4 4F 4A25 1998060500442 19980605 00442 WP 1998 6 5 RRXA98222 1 19980530 A 2612 DETECTOR DOUG DC8 DC862 3021970 WP NR 1 ENGINE MALFUNCTIONED A RRXA O OTHER N FALSE WARNING CR CRUISE 1 WP 15 993CF 46028 AT FL 330, CREW EXPERIENCE BRIEF FIRE WARNING OF 2 RINGS AND LIGHT IN HANDLE ON NR 1 FIRE HANDLE. WARNING WAS OUT BEFOR E RESET WAS PUSHED ON FIRE WARNING LIGHT. FIRE WARNING TEST WAS DONE TO ALL 4 ENGINES TO CONFIRM NO FIRE PRESENT. AT T HE TIME NR 1 OIL TEMP WAS 131 DEG C. NR 1 THROTTLE WAS REDUCED TO FLIGHT IDLE AND OIL TEMP CAME DOWN TO 120 DEG . RETU RNED THROTTLE LEVER TO NORMAL CRUISE, OIL TEMP STABILIZED AT 110 DEG ALL ENG INDICATION NORMAL. REMOVED AND REPLACED NR 1 FIRE DETECTION SYSTEM AMP. NR 1 ENG FIRE WARNING OPS CHECKS GOOD. 2 L 7 4 4F 4A25 1998060500443 19980605 00443 WP 1998 6 5 RRXA98223 1 19980601 A 5311 56119433 FRAME DOUG DC8 DC873F 302199F WP BS 70 CUT A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME CAP CUT AT STA 70 BETWEEN LONGERONS 25 LEFT AND 26 LEFT. FABRICATED AND INSTALL ED REPAIR SPLICE IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH RE0-04801. 2 L 7 4 4F RT 4A25 1998060500444 19980605 00444 CE 1998 6 5 NSVA980001 1 19980128 A 3230 11438800013 POWER PACK BEECH 1900C BEECH 1900 1900C 1154161 CE LANDING GEAR FAILED A NSVA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 119CJ UC19 UC19 UPON GEAR RETRACTION AFTER TAKEOFF, THE PILOTS NOTICED THE RED GEAR TRANSIT LIGHT WOULD NOT EXTINGUISH. THE PILOTS DIVE RTED TO BHB. MAINTENANCE CLEANED THE GEAR SWITCHES AND SWUNG THE GEAR BUT COULD NOT DUPLICATE THE PROBLEM. THE AIRCRAF T WAS RELEASED FOR A TEST FLIGHT. UPON TAKEOFF THE GEAR WOULD NOT RETRACT. THE GEAR WERE PUMPED DOWN BY HAND AND THE A IRCRAFT LANDED SAFELY. MAINTENANCE DETERMINED THAT THE GEAR HYDUALIC POWER PACK FAILED. 2 L 7 2 4T RT A24CE 1998060500445 19980605 00445 EA 1998 6 5 NSVA0526 2 19980524 A 7321 8061328A FUEL CONTROL BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA HARTZL HCB4M HCB4M GL LT ENGINE FAILED A NSVA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 27 129CJ 10027 10027 UC129 DURING CLIMBOUT, LEFT ENGINE TORQUE DROPPED TO 2200 AND FUEL FLOW DROPPED ACCORDINGLY TO 200 LBS BELOW RT SIDE. 2 L 7 2 4T 4 T RT A24CE E4EA 6 C P56GL 1998060500446 19980605 00446 NM 1998 6 5 SPAA9800002 1 19980519 A 3350 BULB BOEING 737 7372T4 1384492 NM CABIN FAILED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE EXTERNAL EMERGENCY EXIT LIGHT AFT OF THE R2 DOOR WAS FOUND INOPERATIVE. THE LAMP WAS REPLAC ED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY PER BMM 33-51-11. 2 L 7 2 4F A16WE 1998060500447 19980605 00447 NM 1998 6 5 RAAA98B1026 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 461-480 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND STR 23R CORRODED AT BS 461 TO 480. REPAIRED PER SRM 53-10-3. M -54 NR 113. 2 L 7 3 4F A3WE 1998060500448 19980605 00448 NM 1998 6 5 RAAA98B1027 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 420 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND STR 25L CORRODED AND CRACKED AT BS 420. REPAIRED PER SRM 53-10- 3, FIG 2. M-54 NR 118. 2 L 7 3 4F A3WE 1998060500449 19980605 00449 NM 1998 6 5 RAAA98B1028 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM WS 629 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-127, FOUND LT WS 629 RIB CRACKED AT LOWER S-6 ATTACHMENT. REPAIR ED PER SRM 57-10-5. M-54 NR 120. 2 L 7 3 4F A3WE 1998060500450 19980605 00450 NM 1998 6 5 RAAA98B1029 1 19980514 A 5744 FITTING BOEING 727 72722C 138400F NM WS 343 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED C1 CHECK PER CARD C-22004, FOUND RT WS 343 NR 10 SPOILER CENTER HINGE BEARING FITTING CRACKED APPROX .7 5 INCH AT UPPER OUTBD MOUNT BOLT HOLE. REPLACED FITTING PER SRM 51-10-1, PG 4 AND 51-30-2, PG 8 AND 14. M-54 NR 130. 2 L 7 3 4F A3WE 1998060500451 19980605 00451 NM 1998 6 5 RAAA98B1030 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM WS 629 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-127, FOUND RT WS 629 RIB CRACKED AT LOWER S-9 ATTACHMENT. REPAIR ED PER SRM 57-10-5. M-54 NR 182. 2 L 7 3 4F A3WE 1998060500452 19980605 00452 NM 1998 6 5 RAAA98B1031 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM WS 686.5 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-127, FOUND RT WS 686.5 RIB CRACKED AT LOWER S-10 ATTACHMENT. REP AIRED PER SRM 57-10-5. M-54 NR 183A. 2 L 7 3 4F A3WE 1998060500453 19980605 00453 NM 1998 6 5 RAAA98B1032 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM WS 546.5 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED AD 94-07-08 INSPECTION PER S/B 727-57-127, FOUND RT WS 546.5 RIB CRACKED AT LOWER S-8 ATTACHMENT. REPA IRED PER SRM 57-10-5. M-54 NR 183B. 2 L 7 3 4F A3WE 1998060500454 19980605 00454 NM 1998 6 5 RAAA98B1033 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 460-480 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND STR 19L CORRODED AT BS 460 TO 480. REPAIRED PER SRM 53-10-3, FI G 2. M-54 NR 189. 2 L 7 3 4F A3WE 1998060500455 19980605 00455 NM 1998 6 5 RAAA98B1034 1 19980514 A 5744 FITTING BOEING 727 72722C 138400F NM WS 440 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED C1 CHECK PER CARD C-22004, FOUND RT WS 440 NR 11 SPOILER INBD DOWN STOP FITTING CRACKED AT STOP PAD. R EPLACED FITTING PER SRM 51-10-1. M-54 NR 132. 2 L 7 3 4F A3WE 1998060500456 19980605 00456 NM 1998 6 5 RAAA98B1035 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 380 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-51103, FOUND BS 380 FRAME CORRODED AT STR 26R TO 28R. REPAIRED PER SRM 53-10-4, FIG 12. M-54 NR 206. 2 L 7 3 4F A3WE 1998060500457 19980605 00457 NM 1998 6 5 RAAA98B1036 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 360-380 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND STR 25R CORRODED AT BS 360 TO 380. REPLACED STRINGER SECTION PE R SRM 51-10-1. M-54 NR 211. 2 L 7 3 4F A3WE 1998060500458 19980605 00458 NM 1998 6 5 RAAA98B1037 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 480 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-52103, FOUND BS 480 FRAME DAMAGED ABOVE STR 26R. REPAIRED PER SRM 5 1-40-3, FIG 1 PG 5. M-54 NR 249. 2 L 7 3 4F A3WE 1998060500459 19980605 00459 NM 1998 6 5 RAAA98B1038 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1090-1168 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND FUSELAGE SKIN INTERNAL DOUBLER DEBONDED AT BS 1148 TO 1166. DUR ING CONCURRENTLY SCHEDULED AD 91-06-06 EXTERNAL INSPECTION FOUND FUSELAGE SKIN BULGED DUE CORROSION AT BS 1090 TO 1111, BS 1129 TO 1168 ALONG STR 17L AND BS 1149 TO 1163 ALONG STR 18L. REPLACED SKIN PANEL FROM BS 1080.45 TO 1183 AND STR 14 L TO 20L PER BAC MSG RVV-SEA-98-0002RR, SRM 51-10-1 AND 51-30-2. M-54 NR 251, 416 AND 417. 2 L 7 3 4F A3WE 1998060500460 19980605 00460 NM 1998 6 5 RAAA98B1039 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1148-1168 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND FUSELAGE SKIN STR 20L LAP JOINT CORRODED AT BS 1148 TO 1168. RE PAIRED PER SRM 53-30-3. M-54 NR 252. 2 L 7 3 4F A3WE 1998060500461 19980605 00461 NM 1998 6 5 RAAA98B1040 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1166 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-54104, FOUND BS 1166 FRAME AFT SHEAR TIE CORRODED AT STR 28L TO 28R. REPLACED AFT SHEAR TIES PER SRM 51-10-1. M-54 NR 253. 2 L 7 3 4F A3WE 1998060500462 19980605 00462 NM 1998 6 5 RAAA98B1041 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 1160-1166 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-54104, FOUND STR 30 CORRODED AT BS 1160 TO 1166. REPAIRED PER SRM 5 3-10-3, FIG 1. M-54 NR 254. 2 L 7 3 4F A3WE 1998060500463 19980605 00463 NM 1998 6 5 RAAA98B1042 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1080-1183 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND STR 20R FUSELAGE SKIN LAP JOINT CORRODED AT BS 1148 TO 1180 AND INTERNAL SKIN DOUBLER DEBONDED AT BS 1148 TO 1166 BETWEEN STR 19R AND 20R. DURING CONCURRENTLY SCHEDULED AD 91-06-06 EX TERNAL INSPECTION FOUND FUSELAGE SKIN BULGED DUE CORROSION AT BS 1080 TO 1111 BETWEEN STR 17R AND 19R, AND BS 1183 AT ST R 20R. REPLACED SKIN PANEL FROM BS 1080.45 TO 1183 AND STR 14R TO 20R PER BAC MSG RVV-SEA-98-0002RR, SRM 51-10-1 AND 51 -30-2. M-54 NR 260, 261, 432 AND 433. 2 L 7 3 4F A3WE 1998060500464 19980605 00464 NM 1998 6 5 CALA9800918 1 19980529 A 3213 65461169 AXLE BOEING 737 737291 138448W NM RT MLG FAILED A CALA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 17252 57034 20362 THE NR 4 MAIN WHEEL SEPARATED FROM AIRCRAFT DURING TAXI IN. MAINTENANCE FOUND THE AXLE SHEARED OFF, NO OTHER AIRCRAFT D AMAGE WAS FOUND. THE RT MLG INNER CYLINDER WAS REMOVED AND REPLACED IAW MM 32-11-21 AND 12-15-31. *S/D* INVESTIGATION BY ENGINEERING CONCLUDED THAT THE CAUSE OF MAIN WHEEL SEPARATION WAS DUE TO A CRACK WHICH STARTED AT BRAKE FLANGE BOLT HOLE. STRESS CORROSION CRACKING IS SUSPECT. 2 L 7 2 4F A16WE 1998060500465 19980605 00465 NM 1998 6 5 CALA9800919 1 19980529 A 2612 693730752 FIRE DETECTOR BOEING 737 737291 138448W NM APU INOPERATIVE A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 10251 13182 20361 THE APU FIRE WARNING LIGHT AND BELL ACTIVATED, WITH APU OFF, WHILE EN ROUTE. THE APU FIRE BOTTLE WAS DISCHARGED, BUT TH E LIGHT AND BELL CONTINUED TO ACTIVATE INTERMITTENTLY. THE AIRCRAFT WAS DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDEN T. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE ENGINE/APU FIRE DETECTION MODULE WAS REMOVED AND REPLACED. THE APU WAS RUN WITH NO FIRE WARNING AND OPERATION CHECKING GOOD. IN ADDITION, THE APU FIRE BOTTLE WAS REMOVED AND REPLACED. 2 L 7 2 4F A16WE 1998060500466 19980605 00466 WP 1998 6 5 CALA9800920 1 19980530 A 5320 BEAM DOUG DC9 DC982 3022082 WP BAGG COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND AFT BAGGAGE BIN THRESHOLD DOOR BEAM CORRODED. A REPAIR WAS INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 1998060500467 19980605 00467 WP 1998 6 5 CALA9800921 1 19980531 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 474 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT VHF ANTENNA, STA 474, LONGERONS 29L-30. REPAIRED IAW ECRA 5330-0256 3 AND INITIATED A DIP FOR PERMANENT REPAIR WITHIN 3600 FLIGHT CYCLES OR ONE YEAR, WHICHEVER COMES FIRST. 2 L 7 2 4F A6WE 1998060500468 19980605 00468 WP 1998 6 5 CALA9800922 1 19980529 A 3350 110049 BATT CHARGER RADIANT DOUG DC10 DC1010 3022110 WP BS 825 INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND EMERGENCY PATH LIGHTING AT SEATS 28 TO 35AB (STA 825) INOPERATIVE. THE EMERGENCY AISLE LIGHT BATTERY C HARGER WAS REMOVED AND REPLACED IAW MM 33-55-00, PAGE 1. 2 L 7 3 4F A22WE 1998060500469 19980605 00469 WP 1998 6 5 CALA9800923 1 19980530 A 5512 PLATES DOUG DC9 DC982 3022082 WP LT/RT HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND LT HORIZONTAL STABILIZER PIVOT OUTBOARD PLATES AND RT HORIZONTAL STABILIZER PIVOT OUTBOARD PLATES CORRO DED. THE PLATES WERE REPLACED IAW SRM 51-30-00. 2 L 7 2 4F A6WE 1998060500470 19980605 00470 WP 1998 6 5 CALA9800924 1 19980601 A 5320 JAMB DOUG DC9 DC982 3022082 WP BAGG COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR JAMB PAN CORRODED AT STA 370 TO 427. THE DOOR JAMB PAN WAS REPLACED IAW SRM 53-05-44. 2 L 7 2 4F A6WE 1998060500471 19980605 00471 NM 1998 6 5 CALA9800925 1 19980601 A 7110 COWLING BOEING 727 727224 1384076 NM NR 2 ENGINE CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND NR 2 ENGINE INLET COWLING RING CORRODED. THE CORRODED AREA WAS CUT OUT. FILLER AND DOUBLERS WERE FABR ICATED AND INSTALLED IAW SRM 54-30-3, 51-10-2, 51-40-5 AND 51-30-2. 2 L 7 3 4F A3WE 1998060500472 19980605 00472 NM 1998 6 5 CALA9800926 1 19980601 A 2782 BRACKET BOEING 727 727224 1384076 NM NR 1 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND A 1 INCH CRACK AT LOWER INBOARD AND OUTBOARD CORNERS OF LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-6. 2 L 7 3 4F A3WE 1998060500473 19980605 00473 NM 1998 6 5 CALA9800927 1 19980601 A 2782 BRACKET BOEING 727 727224 1384076 NM NR 2 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND A 1 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET AT LOWER INBOARD CORNER INSIDE LEADING EDGE AREA. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, AN D 51-10-2. 2 L 7 3 4F A3WE 1998060500474 19980605 00474 NM 1998 6 5 CALA9800928 1 19980601 A 3397 WIRE BOEING 727 727224 1384076 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 22 AND AFT. BROKEN WIRING WAS REPAIRED AND A FUSE WAS REPLACED IAW MM 33-50-00 AND OPERATION OF THE LIGHTS CHECKED GOOD. 2 L 7 3 4F A3WE 1998060500475 19980605 00475 NM 1998 6 5 CALA9800929 1 19980601 A 5330 SKIN BOEING 727 727224 1384076 NM BS 480-500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 480 TO 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998060500476 19980605 00476 NM 1998 6 5 CALA9800930 1 19980601 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND INTERCOSTAL CORRODED IN FORWARD BAGGAGE BIN AT STA 500, RBL 9. THE INTERCOSTAL WAS REMOVED AND CORRODE D STRINGER WAS CUT OUT IAW SRM 53-10-3. NEW STRINGER AND SPLICES WERE FABRICATED IAW SRM 53-10-5 AND 51-10-2. THE STRI NGER, SPLICES AND INTERCOSTAL WERE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998060500477 19980605 00477 WP 1998 6 5 CALA9800931 1 19980601 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 470-456 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT INBOARD CABIN SEAT TRACK CORRODED AT STA 470 TO 456. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SR M 53-05, FIGURE 4F, AND 53-20-1, PAGE 205. 2 L 7 2 4F A6WE 1998060500478 19980605 00478 WP 1998 6 5 CALA9800932 1 19980601 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 598 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CABIN INTERIOR WEB CRACKED AT BS 598, RBL 55. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIG URE 2. 2 L 7 2 4F A6WE 1998060500479 19980605 00479 WP 1998 6 5 CALA9800933 1 19980601 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 598 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 4 INCH CRACK IN CABIN INTERIOR DOUBLER AT BS 598, RBL 55. THE DOUBLER WAS REMOVED, REPAIRED, AND REI NSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30. 2 L 7 2 4F A6WE 1998060500480 19980605 00480 EA 1998 6 5 COMA9860131 1 19980521 A 3620 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 EA LT BLEED AIR MALFUNCTIONED A COMA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SO 01 957CA 11636 5009 7109 LEFT HAND STAGE DUCT LEAK WARNING DURING APPROACH. ENGINE WAS SHUT DOWN AND LANDED SAFELY. REPLACED THE BLEED AIR LEAK CONTROL UNIT. 2 L 7 2 4F RT A21EA 1998060500481 19980605 00481 EU 1998 6 5 QXEA9800687 1 19980601 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 EMERGENCY LIGHTS AT ROWS 4, 7, AND 9 OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998060500482 19980605 00482 EU 1998 6 5 QXEA9800688 1 19980601 A 3350 BATTERY PACK GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 FORWARD LEFT WING EVACUATION LIGHT OUT. MAINTENANCE PLACED ON MEL. LATER THAT SAME DAY IN PDX MAINTENANCE REMOVED AND REPLACED BATTERY PACK, CLEANED CORROSION FROM LEFT FOWARD EVACUATION LIGHT RECEPTACLE, AND REMOVED AND REPLACED BLOWN FU SE IN NEW BATTERY PACK. MAINTENANCE PERFORMED OPERATIONAL TEST, TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998060500483 19980605 00483 EU 1998 6 5 QXEA9800689 1 19980530 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 CENTER FORWARD EMERGENCY EXIT HAS INOPERATIVE LIGHTS. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998060500484 19980605 00484 EU 1998 6 5 QXEA9800690 1 19980531 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 EMERGENCY LIGHT AT ROW 10 IS OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998060500485 19980605 00485 EU 1998 6 5 QXEA9800691 1 19980601 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 EMERGENCY LIGHTS OUT AT ROWS 9 AND 13. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998060500486 19980605 00486 NM 1998 6 5 98FDEA00385 1 19980530 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 683-710 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 DRILL MARKS ON BOTH SIDES OF STR 26R, BS 683 TO 710 IN FWD CARGO. REMOVED DAMAGED AREA OF STRINGER PER SRM 51-10-6. I NSTALLED REPAIR PER SRM 53-10-3. 2 L 7 3 4F A3WE 1998060500487 19980605 00487 NM 1998 6 5 98FDEA00386 1 19980530 A 5313 STRINGER BOEING 727 727225 1384077 NM BS 680-715 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 LWD FWD CARGO CORROSION ON STR 27R BETWEEN BS 680 TO 715. REMOVED STR 27R CORRODED SECTION BETWEEN BS 680 TO 715. REIN STALLED NEW STR SECTION BS 680 TO 715 PER SRM 53-10-3. 2 L 7 3 4F A3WE 1998060500488 19980605 00488 NM 1998 6 5 98FDEA00387 1 19980531 A 5330 SKIN BOEING 727 727225 1384077 NM BS 684-689 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 CORROSION ON SKIN BS 684 TO 689 AT STR 27R. REMOVED CORRODED SKIN AND REPAIRED WITH DOUBLER PER SRM 53-30-3. 2 L 7 3 4F A3WE 1998060500489 19980605 00489 WP 1998 6 5 ABXA9800471 1 19980528 A 3230 5777513501 RETRACT PIN DOUG DOUG DC8 DC861 3021952 WP LT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 LEFT MAIN LANDING GEAR RETRACT PIN BOSS HOLE HAD CORROSION. REPAIRED IAW ABX REA D832-23373 MR. 2 L 7 4 4F 4A25 1998060500490 19980605 00490 WP 1998 6 5 ABXA9800472 1 19980528 A 3210 5777513501 RETRACT PIN DOUG DOUG DC8 DC861 3021952 WP RT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 RIGHT MAIN LANDING GEAR RETRACT PIN BOSS HOLE HAD CORROSION. REPAIRED IAW ABX REA D832-23374 MR. 2 L 7 4 4F 4A25 1998060500491 19980605 00491 WP 1998 6 5 ABXA9800473 1 19980531 A 5230 99576643 BEAM DOUG DOUG DC9 DC931 3022065 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, FOUND FORWARD LOWER CARGO COMPARTMENT DOOR VERTICAL BEAM CRACKED AT BOTTOM FORWARD PRESSURE STOP. REPLA CED VERTICAL BEAM IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998060500492 19980605 00492 WP 1998 6 5 ABXA9800474 1 19980531 A 5320 9910078873 SUB FLOOR DOUG DOUG DC9 DC931 3022065 WP BS 205 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND SUB FLOOR CRACKED AT STATION 205 AND LBL 22 AND STATION 200 AT BL 0. REPAIRED SUB FLOOR IAW DC9 S RM 53-01. 2 L 7 2 4F A6WE 1998060500493 19980605 00493 WP 1998 6 5 ABXA9800475 1 19980531 A 5313 76378133 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 237 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, FOUND LONGERON 16L CRACKED AT STATION 237. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998060500494 19980605 00494 WP 1998 6 5 ABXA9800476 1 19980601 A 5320 49203601 ANGLE DOUG DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND FORWARD LOWER INBOARD CORNER ATTACH ANGLE CRACKED AT EDGE OF RIGHT WHEEL WELL STRUCTURE. REPLACED ANGLE IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998060500495 19980605 00495 WP 1998 6 5 ABXA9800477 1 19980529 A 3230 59164605509 VALVE DOUG DC9 DC932 3022066 WP LANDING GEAR FAILED A ABXA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 23 980AX 47176 AFTER TAKEOFF, GEAR HANDLE SELECTED UP, THE NOSE LANDING GEAR AND MAIN LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. GEAR WAS RECYCLED THREE TIMES WITH THE SAME RESULT. REPLACED LANDING GEAR CONTROL VALVE IAW DC9 MM 32-32-0. 2 L 7 2 4F A6WE 1998060500496 19980605 00496 NM 1998 6 5 MZZA98133 1 19980405 A 2752 240863 ACTUATOR BOEING 727 7272F9 138407D NM LT TE FLAP LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 83428 21426 GUM - FLT 921 - AFTER DEPARTURE DEPARTURE SPN CREW DECLARED AN EMERGENCY INTO GUM BASE DUE TO LOSS OF 'A' SYSTEM HYDRAUL ICS. MAINTENANCE FOUND INBOARD FLAP HYDRAULIC ACTUATOR MOTOR LEAKING (LT W/W) ON REMOVAL FOUND 3 SCREWS ON MOTOR ACCESS PANEL MISSING AND O-RING BLOWN OUT. REMOVED AND REPLACED HYDRAULIC MOTOR PER MM 27-51-52. RESERVICE A, B AND STANDBY SYSTEM TO FULL. RAN FLAPS, NO PRESSURE OR FLUID LOSS NOTED. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 3 4F RT A3WE 1998060500497 19980605 00497 WP 1998 6 5 HALA9800101 1 19980425 A 2720 37723745503 SHUTOFF VALVE DOUG DC9 DC951 3022051 WP RUDDER LEAKING A HALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 679HA 47662 FLT HNL - 108 - RUDDER STICKS IN MANUAL (RESTRICTED RUDDER) AFTER MANUAL RUDDER CHECK, SWITCHED BACK TO PWR. MUST PRESS ON RUDDER PEDAL APPROX 10 TIMES BEFORE IT WILL COME OUT OF RESTRICTED POSITION. REPLACED RUDDER POWER SHUTOFF VALVE, L EAK CHECK AND OPS CHECK OK, PER MM 27-200-09. (M) 2 L 7 2 4F RT A6WE 1998060500498 19980605 00498 NM 1998 6 5 USAABB98036 1 19980415 A 3240 CONTROL CABLE BOEING 757 7572B7 1384964 NM COCKPIT MISRIGGED A USAA O OTHER W INADEQUATE Q C IN INSP/MAINT 1 EA 19 630AU 27808 PIT - FLT 108 - THE AIRPLANE WAS TAXIED TO A PARKING AREA OF AN ATC HOLD BEFORE TAKEOFF. WHILE ON HOLD, THE CONFIGURATI ON OF THE AIRCRAFT WAS AS FOLLOWS, BOTH ENGINES SHUT DOWN, APU RUNNING. ELECTRIC HYDRAULIC PUMPS OFF. PARKING BRAKE SE T. AFTER APPROXIMATELY 30 MINUTES, THE AIRCRAFT BEGAN TO DRIFT BACKWARDS. THE AIRCRAFT STOPPED WITH THE RIGHT MAIN LAN DING GEAR OFF THE PAVEMENT AND BURIED IN MUD. MAINTENANCE FOUND THAT THE CABLING FROM THE BRAKE PEDALS TO THE BRAKE MET ERING VALVE WAS MISRIGGED, PREVENTING THE VALVE FROM SHUTTING COMPLETELY. THE CABLING WAS RIGGED AND THE BLEED DOWN CHE CKED. A CAMPAIGN DIRECTIVE IS BEING PREPARED TO CHECK THE REST OF THE FLEET FOR EXCESSIVE BLEED DOWN. A PROCEDURE FOR 2 L 7 2 4F RT A2NM 1998060500499 19980605 00499 NM 1998 6 5 MZZA98134 1 19980413 A 2910 BACH30AU12R0290 HOSE BOEING 727 727212 138407G NM HYD SERV COMPT RUPTURED A MZZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 13 86425 21459 KIX - EN ROUTE TO CTS DIVIRTED TO KIX DUR LOSS OF 'B' SYSTEM HYD FLUID DOWN TO 'ZERO'. 'B' HYD SYSTEM FAILED 'B' HYD QU ANTITY AND PRESSURE INDICATE ZERO. PRIMARY LOSS OF FLUID TRACED TO FAILURE OF HYD 'B' PUMP TO RESERVOIR SUPPLY HOSE ASS Y REFER IPC 29-14-06 ITEM 45. REPLACED HOSE ASSY. ALSO HAD SMALL LEAK AT NR 3 HYD SPOILER ACTUATOR FILTER BOWL SEAL. B UT DID NOT CONTRIBUTE TO PROBLEM REPLACED SEAL AND A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998060500500 19980605 00500 NM 1998 6 5 TAOA049802 1 19980417 A 5220 65587708 STEP BOEING 727 727225 1384077 NM RT EMERG EXIT MISSING A TAOA K NONE D INFLIGHT SEPARATION IN INSP/MAINT 1 EA 15 918TS 20445 RIGHT AFT OVERWING EMERGENCY EXIT DOOR LOCKED CLOSE, EMERGENCY EXIT STEP WAS NOT SECURED AND DISLODGED IN FLIGHT. REPLA CED RIGHT AFT OVERWING EMERGENCY EXIT STEP ASSEMBLY AND CABLES OPERATIONAL CHECK NORMAL IAW MM CHAPTER 53-21-0 PAGE 506. (M) 2 L 7 3 4F A3WE 1998060500501 19980605 00501 WP 1998 6 5 HALA9800103 1 19980415 A 5320 BEAM DOUG DC9 DC951 3022051 WP BS 49 CRACKED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 NOSE LANDING GEAR W/W, LEFT STATION 49 LOWER BEAM IS STRUCTURE ATTACHING UPPER FASTENER AREA IS CRACKED APPROX 5/8 INCH LONG. CRACKED STOP DRILLED IAW DOUBLER AND ANGLE 'L' TREATED SRM 57-05-FIG 110, 51-10-02 AND INSTALLED REPAIR DOUBLER A ND 'L' ANGLE SRM 57-30-5. (M) 2 L 7 2 4F RT A6WE 1998060500502 19980605 00502 WP 1998 6 5 HALA9800104 1 19980415 A 5330 SPLICE DOUG DC9 DC951 3022051 WP FS 1258 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 EVIDENCE OF CORROSION EMINATING FROM SKIN JOINT, FS 1258 PRODUCTION SPLICE RT 6 INCH BELOW PYLON TRAILING EDGE FAIRING S UPPORT. REMOVED CORROSION AND TREATED PER SRM 51-10-3. REMOVED AND REPLACED FASTENERS AS REQUIRED PER SRM 51-30-2. RE MOVED AND REPLACED INNER SPLICE STRAP SECTION PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F RT A6WE 1998060500503 19980605 00503 WP 1998 6 5 HALA9800106 1 19980415 A 5530 TIP FAIRING DOUG DC9 DC951 3022051 WP VERT STABILIZER CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 VERT STABILIZER AFT TIP FAIRING AREA LOWER WEB, DIRECTLY ABOVE TOP OF RUDDER) HAS CORROSION AT SEVERAL SIGHTS, FORWARD M OST AREA 10 INCH BY 8 INCH, LOCATION 2V113 FROM 8 INCH AFT OF AFT SPAR TO 48 INCHES AFT OF SPAR. REMOVED, FABRICATED, R EPLACED WEB SECTIO NPER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 1998060500504 19980605 00504 WP 1998 6 5 HALA9800107 1 19980415 A 5230 PAN DOUG DC9 DC951 3022051 WP FWD CARGO DOOR CRACK A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 FORWARD CARGO DOOR OUTER PAN RADIUS HAS 1 INCH CRACK BOTTOM END OF DOOR. LOCATED AND FABRICATED 7 DOUBLER STOP DRILLED CRACK AND PRIMED PER SRM 51-10-3, 52-03 FIG 8 SHT 2, AND INSTALLED PER 51-30-2. (M) 2 L 7 2 4F RT A6WE 1998060500505 19980605 00505 WP 1998 6 5 HALA9800108 1 19980415 A 5312 HAT CHANNEL DOUG DC9 DC951 3022051 WP FS 1292 CORROSION A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 672MC 47661 STATION 1292 RT AFT FACE CANTED BLKHD 3RD STIFFENER (HAT CHANNEL) UP IN VENT BOX AREA LEVEL 2 CORROSION. REMOVED HAT CH ANNEL FABRICATED REPLACEMENT HAT CHANNEL PER SRM 51-10-2, INSTALLED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A6WE 1998060500506 19980605 00506 WP 1998 6 5 GTIA9800051 1 19980423 A 3260 PROX SWITCH DOUG DC9 DC932 3022066 WP LANDING GEAR DIRTY A GTIA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 947ML 47514 LRD - FLT 902 - LANDING GEAR EXTENSION WAS NORMAL. ABOUT 700 FEET ABOVE THE RUNWAY, RT MAIN GEAR RED UNSAFE LIGHT CAME ON FOR 1-2 SECONDS, EVER 5-10 SECONDS. WENT AROUND BUT THE LEFT GEAR DOWN. UNSAFE INDICATIONS STOPPED. USED QRH PROCE DURES, RECYCLED GEAR. AFTER LOOKING IN GEAR IN PERISCOPE, WE WERE NOT CERTAIN STRIPES WERE LINED UP. WARNING DID NOT O CCUR AGAIN AFTER GEAR WAS EXTENDED SECOND TIME. RE-RACKED PROXIMITY WARNING SYSTEM CONTROL BOX AND CLEANED RT MAIN GEAR PROXIMITY SWITCH SYSTEM. SELF TEST GOOD IAW DC-9 MM 32-60-1. (M) 2 L 7 2 4F A6WE 1998060500507 19980605 00507 WP 1998 6 5 TWAA9806620 1 19980421 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 900-917 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT CARGO COMPT LOWER DOOR JAM WITH CORROSION BETWEEN SKIN AND FRAME. ALSO, 3 CRACKS APPROX .25 INCH LONG FROM STATION 900 TO 917, RBL 17 INCH. REMOVED CORROSION PER SRM 51-10-3. REPLACED CORRO DED PARTS PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500508 19980605 00508 WP 1998 6 5 TWAA9806619 1 19980421 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 1074 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME CRACKED AT LONGERON 14R, STATION 1074. INSTALLED NEW FORMER RI NG FROM L17L TO 17R PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500509 19980605 00509 WP 1998 6 5 TWAA9806618 1 19980421 A 5712 RIB DOUG DC9 DC933F 302207A WP WS 485 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND XRS 485 LEFT WING LE RIB CORRODED AND CRACKED. REPLACED RIB PER SRM 51-10, PG 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500510 19980605 00510 WP 1998 6 5 TWAA9806617 1 19980421 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 1074 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FIELD REPAIR AT STATION 1074, LONGERON 2R. INSTALLED NEW FORMER RING FROM L 17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500511 19980605 00511 WP 1998 6 5 TWAA9806616 1 19980416 A 5542 PANEL DOUG DC9 DC932 3022066 WP RUDDER TORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND TOP TE PANEL ON RUDDER SEPARATED AND TORN AT JOINT SEAMS. REPAIRED PER SRM 51-90-0. (M) 2 L 7 2 4F A6WE 1998060500512 19980605 00512 WP 1998 6 5 TWAA9806615 1 19980421 A 5753 ANGLE DOUG DC9 DC933F 302207A WP RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP INTERIOR AT IDLER HINGE, OUTBOARD SIDE ANGLE CRACKED. REPLACED CRACKED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500513 19980605 00513 WP 1998 6 5 TWAA9806614 1 19980421 A 5320 DOUBLER DOUG DC9 DC933F 302207A WP BS 433 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 DOUBLER ON AFT FACE OF STUBBY FORMER, CRACKED 4 IN ABOVE FLOOR LEVEL. REPLACED DOUBLER PER SRM 51-01 PAGE 1. (M) 2 L 7 2 4F A6WE 1998060500514 19980605 00514 WP 1998 6 5 TWAA9806613 1 19980421 A 5347 FLOOR TRACK DOUG DC9 DC933F 302207A WP BS 180-240 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK FROM STATION 180 TO 240, LBL 21 INCH. REMOVED CORR ODED TRACK FROM STATION 180 TO 248. FABRICATED AND INSTALLED NEW TRACK PER SRM 53-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500515 19980605 00515 WP 1998 6 5 TWAA9806612 1 19980421 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 917 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND IN AFT CARGO AT FS 917, ABOVE L27L, FORMER HAD .5 INCH EYEBROW CRACK ON FWD SIDE. WELDED FLOOR SUPPORT AND STRESS RELIEVED. REINSTALLED REPAIRED PART PER SSRM 53-00-106. (M) 2 L 7 2 4F A6WE 1998060500516 19980605 00516 WP 1998 6 5 TWAA9806611 1 19980421 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 1074 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME FIELD REPAIR INSTALLED AT FS 1074, LONGERON 3L. INSTALLED NEW FORMER RING FROM L17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500517 19980605 00517 WP 1998 6 5 TWAA9806610 1 19980421 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 1074 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER FRAME WITH FIELD REPAIR INSTALLED AT FS 1074, LONGERON 3R. INSTALLED NEW FORMER RING FROM LONGERON 17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500518 19980605 00518 WP 1998 6 5 TWAA9806609 1 19980421 A 5712 RIB DOUG DC9 DC933F 302207A WP WS 490 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING XRS 490, LE RIB CRACKED. REPLACED RIB PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500519 19980605 00519 WP 1998 6 5 TWAA9806608 1 19980421 A 5347 FLOOR TRACK DOUG DC9 DC933F 302207A WP BS 269 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK AT RBL 8 INCH BS 269 HAS FLOOR TRACK WITH EXCESS METAL REMOVED BEYOND LIMITS TO CLE AN UP CORROSION. REPLACED SECTION OF TRACK PER SRM 53-05, PG 10G VIEW A. (M) 2 L 7 2 4F A6WE 1998060500520 19980605 00520 WP 1998 6 5 TWAA9806607 1 19980421 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 433 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 433 STUBBY FRAME CRACKED 3 INCHES ABOVE FLOOR. REPLACED FRAME PER SRM 51 -01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500521 19980605 00521 WP 1998 6 5 TWAA9806606 1 19980421 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 225 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN UPPER FUSELAGE SKIN, 1.5 INCH BY 1.5 INCH BY .080 DEEP AT FS 225, ON STRINGER 11L. REPAIRED DENT PER SRM 53-04 FIG 38. (M) 2 L 7 2 4F A6WE 1998060500522 19980605 00522 WP 1998 6 5 TWAA9806605 1 19980416 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 522 BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER BENT AT FS 522, BETWEEN LONGERON 18R AND 17R. REPAIRED PER SRM 53-03 , PAGE 5. 'Z' FRAME FLANGE REPAIR INSTALLED. (M) 2 L 7 2 4F A6WE 1998060500523 19980605 00523 WP 1998 6 5 TWAA9806604 1 19980416 A 5347 FLOOR TRACK DOUG DC9 DC933F 302207A WP BS 198-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR TRACK CORROSION AT FS 198 TO 237, RBL 21 TO 26. REMOVED CORROSION PER 51-10 -3. REINSTALLED TRACK PER MM 53-40-1 PAGE 201. (M) 2 L 7 2 4F A6WE 1998060500524 19980605 00524 WP 1998 6 5 TWAA9806603 1 19980416 A 5753 SKIN DOUG DC9 DC933F 302207A WP LT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LEFT TE FLAP, THIRD TE FLAP SECTION DELAMINATED ON LOWER FWD END. REPAIR ED PER SRM 51-01 AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500525 19980605 00525 WP 1998 6 5 TWAA9806602 1 19980416 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 484 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 484, A FORMER CRACKED AT TOP AREA OF WINDOW BELT, RT SIDE. REPLACED F ORMER PER SRM 53-03, FIG 32. (M) 2 L 7 2 4F A6WE 1998060500526 19980605 00526 WP 1998 6 5 TWAA9806601 1 19980416 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WITH CRACK AT LOWER AFT FASTENER IN LE ABOVE LE PANEL NR 1211A. I NSTALLED NEW RIB PER SRM 51-01 PAGE 1. (M) 2 L 7 2 4F A6WE 1998060500527 19980605 00527 WP 1998 6 5 TWAA9806710 1 19980403 A 5320 ANGLE DOUG DC9 DC933F 302207A WP BS 917 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 917, ATTACH ANGLE ON FWD FACE OF FORMER TO FLOOR SUPPORT, BETWEEN LONG ERON 27L AND 28L, WAS CRACKED AND CORRODED. REPLACED ANGLE PER SRM 51-01, PAGE 1, ITEM C AND TWA STD PRACTICE. (M) 2 L 7 2 4F A6WE 1998060500528 19980605 00528 WP 1998 6 5 TWAA9806709 1 19980403 A 5753 ANGLE DOUG DC9 DC933F 302207A WP LT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING CRACK INSIDE REAR FLAP ON SUPPORT ANGLE FOR OUTBOARD HINGE, CRACKED ON B OTH INBOARD AND OUTBOARD SIDES. REMOVED AND REPLACED INBOARD AND OUTBOARD SUPPORT ANGLES FOR OUTBOARD HINGE, PER SRM 51 -01, ITEM C, AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500529 19980605 00529 WP 1998 6 5 TWAA9806708 1 19980413 A 5312 BULKHEAD CLIP DOUG DC9 DC933F 302207A WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AFT PRESSURE BULKHEAD AT RADIAL 16L, OUTBOARD END CLIP WITH .5 INCH CRACK RU NING FROM EDGE OF CLIP TO FIRST FASTENER HOLE. REPLACED CLIP AT RADIAL 16L, AFT PRESSURE BULKHEAD, PER SRM 51-01, PAGE 1 ITEM C, AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500530 19980605 00530 WP 1998 6 5 TWAA9806707 1 19980413 A 5320 ANGLE DOUG DC9 DC933F 302207A WP BS 937 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ATTACH ANGLE ON FWD FACE OF FORMER TO FORMER FOOT CORRODED AT FS 937, LONGER ON 27L TO 28L. INSTALLED NEW ANGLE PER SRM 51-01 PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500531 19980605 00531 WP 1998 6 5 TWAA9806706 1 19980407 A 5320 ANGLE DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP16 MAINTENANCE CHECK, FOUND LEFT FWD OVERWING EXIT ANGLE CRACKED AS SEEN THROUGH UPPER AFT 1 INCH BY 5 IN CH INSPECTION SLOT. MADE AND INSTALLED NEW CLIP WITH HI-LOCK PER SRM 51-30-0. (M) 2 L 7 2 4F A6WE 1998060500532 19980605 00532 WP 1998 6 5 TWAA9806705 1 19980403 A 5330 SKIN DOUG DC9 DC951 3022051 WP BS 1209 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 406EA 47686 STL - DURING OP 9 MAINTENANCE CHECK, FOUND SKIN CRACKS FROM 4 RIVETS AT STATION 1209, AT LONGERON 14L. CRACKS MEASURE . 3750 INCH IN LONG TO .09375 INCH LONG. REPAIRED PER SRM 53-04, FIG 18. (M) 2 L 7 2 4F RT A6WE 1998060500533 19980605 00533 WP 1998 6 5 TWAA9806704 1 19980313 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 370-427 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 907TW 49165 STL - DURING C-CHECK, FOUND SKIN BELOW FWD CARGO DOOR SILL SCRATCHED AT STATION 370 TO 427, L29R TO 28R. MINOR SKIN DAM AGE. ROUNDED OUT AND TAPERED SCRATCHES AND TREATED PER SRM 53-04, FIG 38. (M) 2 L 7 2 4F A6WE 1998060500534 19980605 00534 WP 1998 6 5 TWAA9806703 1 19980414 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 503 BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 503 FORMER BENT AT UPPER AREA OF WINDOW BELT. REPAIRED PER SRM 53-03, PA GE 5, FIG 4. (M) 2 L 7 2 4F A6WE 1998060500535 19980605 00535 WP 1998 6 5 TWAA9806702 1 19980413 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 370 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 DURING OP 16 MAINTENANCE CHECK, FOUND FS 370 FORMER CRACKED ABOVE LONGERON 9R, APPROX .75 INCH LONG. REPLACED FORMER SE CTION PER SRM 51-01, PAGE 1 ITEM C, AND TWA STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500536 19980605 00536 WP 1998 6 5 TWAA9806701 1 19980413 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 180 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FS 180 LONGERON 4L WITH CRACK .75 INCH LONG. SPLICED IN SECTION OF LONGERON PER SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 1998060500537 19980605 00537 WP 1998 6 5 TWAA9806816 1 19980422 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 1074 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 1074, LONGERON 2R, FORMER FRAME UPPER CHORD CRACKED. INSTALLED NEW FO RMER RING FROM LONGERON 17L TO 17R, PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500538 19980605 00538 WP 1998 6 5 TWAA9806815 1 19980312 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND L ANGLE ON AFT PRESSURE BULKHEAD CRACKED AT S996, BELOW CUSP ANGLE LBL 58.5. REPLACED L ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500539 19980605 00539 WP 1998 6 5 TWAA9806814 1 19980312 A 5320 FORMER DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FORMER RING AT STATION 1076, LONGERON 15R, CRACKED. REPLACED PER SRM 53-03, FIG 4, AND STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500540 19980605 00540 WP 1998 6 5 TWAA9806813 1 19980312 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 639 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 6L CRACKED AT STATION 639. INSTALLED LONGERON SECTION AND SPLICED PER SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 1998060500541 19980605 00541 WP 1998 6 5 TWAA9806812 1 19980312 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 980 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENT AT FS 980, S5R, .75 INCH BY .068. REPAIRED DENT PER SRM 53-04, PAGE 218K, FIG 38. SEALED REPAIR PER SRM 51-20. (M) 2 L 7 2 4F A6WE 1998060500542 19980605 00542 WP 1998 6 5 TWAA9806811 1 19980327 A 5320 RIVETS DOUG DC9 DC932 3022066 WP BS 354 FAILED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 26L WITH A RIVET POPPED AT FS 354. REMOVED AND REPLACED RIVETS AS REQUIRED PER SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1998060500543 19980605 00543 WP 1998 6 5 TWAA9806810 1 19980311 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 945 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 DURING OP15 MAINTENANCE CHECK, FOUND AFT CABIN FUSELAGE SKIN TO FORMER RING CRACKED AT STATION 945, BETWEEN L14 AND 15R. REPLACED PART PER SRM 51-01 PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500544 19980605 00544 WP 1998 6 5 TWAA9806809 1 19980323 A 5620 WINDOW FRAME DOUG DC9 DC932 3022066 WP CABIN CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP15 MAINTENANCE CHECK, FOUND CABIN WINDOW 23L HAD WINDOW TO FRAME TIE CRACKED. REPLACED WITH NEW FRAME PE R SRM 51-10-1, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500545 19980605 00545 WP 1998 6 5 TWAA9806808 1 19980330 A 5330 SKIN DOUG DC9 DC933F 302207A WP CARGO DOORWAY DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP16 MAINTENANCE CHECK, FOUND AFT END OF AFT CARGO DOOR CUTOUT SKIN DAMAGED BELOW LONGERON 24R. REPAIRED P ER SRM 53-05, FIG 80. (M) 2 L 7 2 4F A6WE 1998060500546 19980605 00546 WP 1998 6 5 TWAA9806807 1 19980403 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 220 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP16 MAINTENANCE CHECK, FOUND .5 INCH CRACK IN FUSELAGE SKIN RUNNING FROM AFT LOWER CORNER OF A CUTOUT FOR 1.375 INCH IN BY 3 INCH REPAIR, STATION 220 ONE INCH ABOVE S17L. CRACK DOES NOT RUN INTO RIVET HOLE. CUTOUT DAMAGE AND ADDED DOUBLER AND FINGER DOUBLERS PER SRM 53-04, FIG 12B. (M) 2 L 7 2 4F A6WE 1998060500547 19980605 00547 WP 1998 6 5 TWAA9806806 1 19980407 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS273 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND UPPER FUSELAGE DENT IN FUSELAGE SKIN 3.5 INCH IN BY 2 INCH IN BY .100 DEEP, AT FS 273, JUST ABOVE STRINGER 17L. VERIFIED NO CRACK WITH NDT TEST. REPAIRED PER SRM 53-04, FIG 38. (M) 2 L 7 2 4F A6WE 1998060500548 19980605 00548 WP 1998 6 5 TWAA9806805 1 19980331 A 5730 SKIN DOUG DC9 DC933F 302207A WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING SKIN CRACKED 12 INCH INBOARD OF INBOARD SIDE OF INBOARD SPOILER AT R EAR SPAR UPPER TE. SKIN WAS CRACKED ONE IN LONG. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-01, FIG 3 SHEET 2 . (M) 2 L 7 2 4F A6WE 1998060500549 19980605 00549 WP 1998 6 5 TWAA9806801 1 19980430 A 2720 25878261 COMPUTER DOUG DC9 DC934 302207E WP RUDDER WORN A TWAA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 CE 05 928L 270390 48124 FLT 732 - CREW REPORTED VERY LITTLE RUDDER CONTROL AFTER TAKEOFF. THE NOSE WOULD HUNT BOTH SIDES. TURNED STAB AUG OFF W ITH NO HELP. RETURNED TO STL. REPLACED THE STAB AUGMENTATION COMPUTER. (M) 2 L 7 2 4F RT A6WE 1998060500550 19980605 00550 WP 1998 6 5 TWAA9806804 1 19980403 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 313 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HOLE AT STATION 313 FORMER L9R. MADE METAL REPAIR ON FORMER PER SRM 53-03, PAGE 5 FIG 4, FORMER STATION 313. (M) 2 L 7 2 4F A6WE 1998060500551 19980605 00551 WP 1998 6 5 TWAA9806803 1 19980407 A 5320 FORMER DOUG DC9 DC933F 302207A WP BS 965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON AFT FACE OF FORMER FS 965, BETWEEN L29L AND 29R. REMOVED CORRO SION AND REPAIRED PER SRM 53-04, PAGE 4. (M) 2 L 7 2 4F A6WE 1998060500552 19980605 00552 WP 1998 6 5 TWAA9806802 1 19980410 A 5320 DOUBLER DOUG DC9 DC933F 302207A WP BS 937 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AT FS 937, AFT FACE OF FORMER DOUBLER, ABOVE L28L TO 29L. REMOVED CORROSION PER SRM 51-10-3. INSTALLED NEW DOUBLER PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998060500553 19980605 00553 WP 1998 6 5 TWAA9806922 1 19980319 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP15 MAINTENANCE CHECK, FOUND LONGERON 14R AT STATION 1076 WITH CRACKED FORMER. REPAIRED FRAME PER SRM 53- 03, FIG 4, AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500554 19980605 00554 WP 1998 6 5 TWAA9806921 1 19980312 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT CUSP ANGLE CRACKED AT STATION 996, 58.5 LBL, APPROX 4 INCH LONG. MANUF ACTURED NEW TIE PLATE AND INSTALLED PER SRM 51-01, PAGE 1, AND TWA STANDARD PRACTICE. (M) 2 L 7 2 4F A6WE 1998060500555 19980605 00555 WP 1998 6 5 TWAA9806920 1 19980414 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 180 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP15 MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM AT FS 180, RBL 20 INCH TO 43 INCH. REMOVED AND INSTAL LED NEW FLOORBEAM PER SRM 51-01. (M) 2 L 7 2 4F A6WE 1998060500556 19980605 00556 WP 1998 6 5 TWAA9806919 1 19980416 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 197 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP15 MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM AT FS 197, LBL 6 INCH. REPLACED BEAM PER SRM 51-01, A ND STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500557 19980605 00557 WP 1998 6 5 TWAA9806918 1 19980417 A 5347 FLOOR TRACK DOUG DC9 DC982 3022082 WP BS 1212-1322 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON RT FLOOR TRACK FROM FS 1212 TO 1322. REMOVED AND REPLACED TRAC K PER SRM 51-01, PAGE 2 ITEM C, AND TWA STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500558 19980605 00558 WP 1998 6 5 TWAA9806917 1 19980422 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 940 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT MLG WHEEL WELL FS 940, RBL 4, FRAME WEB CRACKED AND U-CHANNEL CRACKED AFT SIDE OF WEB. REPLACED U-CHANNEL AND FASTENER IN WEB PER SRM 51-01. (M) 2 L 7 2 4F A6WE 1998060500559 19980605 00559 WP 1998 6 5 TWAA9806916 1 19980422 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 172 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND HOLD CORRODED THROUGH CABIN FLOOR MEMBRANE AT STATION 172, RBL 52. REPAIRED PER SRM 53-01, FIG 4 AND TWA STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998060500560 19980605 00560 WP 1998 6 5 TWAA9806915 1 19980327 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 164 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT WING STATION XRS 164 INSIDE TANK, FWD FACE OF LOWER SPAR CAP, VERTICAL LEG HAD CRACK EXTENDING INTO LOWER RADIUS BELOW INBOARD FLAP BARREL NUT ATTACH POINT. INSTALLED NEW SPAR CAP AND SPLICE PER DWG JO60165 AND STD PROCEDURE PER SRM 51-01, PAGE 1. (M) 2 L 7 2 4F A6WE 1998060500561 19980605 00561 WP 1998 6 5 TWAA9806914 1 19980403 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP PRESS BULKHEAD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE TO BULKHEAD ATTACH ANGLE CRACKED BETWEEN LONG 15L AND 16L. REPLACED ANGL E PER SRM 51-01, PAGE 1 ITEM C, AND TWA STD PRACTICE. (M) 2 L 7 2 4F A6WE 1998060500562 19980605 00562 WP 1998 6 5 TWAA9806913 1 19980403 A 5753 RIB DOUG DC9 DC932 3022066 WP RT TE FLAP WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND HOLE WORN THROUGH FLAP RIBS AT RT WING INBOARD AND OUTBOARD FLEX JOINT BOTTO M SIDE. REPLACED END RIBS PER SRM 51-01 AND TWA STD PRACTICE. (M) 2 L 7 2 4F A6WE 1998060500563 19980605 00563 WP 1998 6 5 TWAA9806912 1 19980317 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 902 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CORROSION ON LONGERON 26L AT STATION 902 'FINGER DOUBLER'. REPLACED FINGER DOUBLER PER SRM 51-01, PAGE 1 ITEM C. REMOVED CORROSION PER SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1998060500564 19980605 00564 WP 1998 6 5 TWAA9806911 1 19980218 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 617 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FLOORBEAM CRACKED AT STATION 617, APPROX 58.6 RBL. INSTALLED NEW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C AND SRM 51-30-0. (M) 2 L 7 2 4F A6WE 1998060500565 19980605 00565 WP 1998 6 5 TWAA9806910 1 19980317 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 560-579 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED BETWEEN STATION 560 AND 579, APPROX 58 INCH RBL , UNDER AFT END OF FLOOR PANEL 37. REPAIRED PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F A6WE 1998060500567 19980605 00567 NM 1998 6 5 TWRA9821 1 19980418 A 2612 21561 AMPLIFIER BOEING 747 747212B 1384886 NM E/E COMPT MALFUNCTIONED A TWRA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 620FF 1396 21162 FLT 24 - SFO-JFK - DIVERTED TO COS DUE FWD CARGO COMPT FIRE DETECTION LIGHT ILLUMINATED IN FLIGHT. BOTH FIRE BOTTLES DI SCHARGED PER LOWER FWD COMPT FIRE CHECK LIST. POST FLIGHT INSPECTION FOUND NO INDICATION OF FIRE. SYSTEM GIVES FALSE F IRE WARNINGS INTERMITTENTLY. REPLACED BOTH FWD CARGO COMPT FIRE BOTTLES PER MM 26-23-01. REPLACED NR 1 AND NR 2 FIRE D ETECTORS AND FWD AMPLIFIER PER MM 26-13-00. OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1998060500568 19980605 00568 NM 1998 6 5 TWRA9820 1 19980416 A 7603 65B962689 LINKAGE BOEING 747 747282B 1384860 NM NR 3 ENGINE BINDING A TWRA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 EA 15 610FF QB13858 20501 INBOUND FLT 711, JFK-LAS, NR 3 ENGINE WAS SHUT DOWN IN FLIGHT DUE TO THROTTLE BEING STUCK AT 1.5 POSITION. PERFORMED IN SPECTION AS PER 76-11-03, FOUND THROTTLE STIFF, CLEANED AND LUBED, OPS CHECK OK. ON NEXT FLIGHT FOUND THRUST LEVER WOUL D NOT RETURN TO IDLE DETENT AFTER LANDING. REPLACED NR 3 ENGINE MIXING BOX AS PER 76-11-09. (M) 2 L 7 4 4F A20WE 1998060500569 19980605 00569 NM 1998 6 5 TSAA9833186 1 19980315 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK OPS CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1998060500570 19980605 00570 NM 1998 6 5 TSAA9833187 1 19980328 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND POSITION NR 1 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998060500571 19980605 00571 NM 1998 6 5 TSAA9833188 1 19980328 A 3350 1000679 LIGHT BOEING 737 7372S2C 138448G NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND RIGHT AFT EMERGENCY EXIT LIGH TINOP. REPLACED LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1998060500572 19980605 00572 NM 1998 6 5 TSAA9826189 1 19980328 A 2612 CONNECTOR BOEING 737 7372Q9 138448M NM NR 1 ENGINE LOOSE A TSAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 WP 13 804AL 21719 FLT 95 - NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO OVHT LIGHT. REPAIRED CONNECTOR ON NR 1 ENGINE LOWER FIRE LOOP. GROUND O PS CHECK OK. GROUND ENGINE RUN OPS CHECK GOOD. REMOVED AND REPLACED NR 1 FIRE BOTTLE. OPS CHECK COMPLETED PER MM 26-2 1-11 AND SQUIB TEST COMPLETED. REMOVED AND REPLCED NR 2 FIRE BOTTLE. OPS CHECK COMPLETED PER MM 26-21-11. (M) 2 L 7 2 4F A16WE 1998060500573 19980605 00573 NE 1998 6 5 TSAA9872190 2 19980329 A 7250 TURBINE BOEING 737 737230C 1384472 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILURE A A TSAA A E UNSCHED LANDING ENGINE SHUTDOWN E R M VIBRATION/BUFFET PARTIAL RPM/PWR LOSS OVER TEMP TO TAKEOFF 1 WP 13 820AL 22138 FLT 81 - KOA-HNL - SERVICE VIBRATION ON NR 1 ENGINE AFTER TAKEOFF AND SUDDEN LOSS OF THRUST, EPR DECREASED FROM 1.98-1.5 EGT AT 550 ONE MINUTE THEN CLIMBED TO RED LINE. NR 1 THRUST REVERSER FOD DAMAGE. NR 1 TAILPIPE EXTENSION FOD DAMAGE. RETURNED AIRCRAFT TO KOA. REPLACED NR 1 ENGINE ASSY IAW FORMS 17211, 17212, 17213, 17214, M-215. RUN-UP CHECK OK. RE PLACED NR 1 THRUST REVERSER ASSY IAW FORM M-211. OPS AND LEAK CHECK OK. REPLACED NR 1 TAILPIPE EXTENSION IAW FORM M-21 1. RII COMPLETED FOR INSTALLATION OF NR 1 ENGINE PER FORM M-211, M-212, M-213, M-214, AND M-215. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998060500574 19980605 00574 NM 1998 6 5 TSAA9833206 1 19980409 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND NR 2 EMERGENCY FLOOR LIGHT INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998060500575 19980605 00575 NM 1998 6 5 TSAA9833205 1 19980409 A 3350 9631002211 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FLOOR PROXIMITY LIGHT ASSY AT NR 2 POSITION DUE TO UNIT BEING INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1998060500576 19980605 00576 NM 1998 6 5 TSAA9833204 1 19980409 A 3350 1000679 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFICATION LIGHT ASSY DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998060500577 19980605 00577 NM 1998 6 5 TSAA9833201 1 19980407 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST TO TAKEOFF 1 WP 13 808AL 23445 ON SERVICE CHECK, FOUND NR 2 POSITION EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998060500578 19980605 00578 NM 1998 6 5 TSAA9833200 1 19980410 A 3350 96210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998060500580 19980605 00580 NM 1998 6 5 TSAA9833202 1 19980408 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK OPS CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998060500581 19980605 00581 NM 1998 6 5 TSAA9833309 1 19980410 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 ON SERVICE CHECK, FOUND POSITION NR 5 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998060500582 19980605 00582 EU 1998 6 5 SIMA981051 1 19980415 A 5330 S5337122820205 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 425MJ 425 DURING MBV-1 INSPECTION, MAINTENANCE REPORTED A RIVET AT FRAME 23 RIGHT STRINGER 18 WITH A BURN HOLE IN THE COUNTER SINK . MAINTENANCE INSTALLED A PATCH TO THE RIGHT LOWER SIDE OF FUSELAGE IAW SRM 53-00-00 PAGE 526. AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1998060500583 19980605 00583 EU 1998 6 5 SIMA981042 1 19980414 A 5315 S5367240620801 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 425MJ 425 SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36 WAS CORRODED. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SR M 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998060500584 19980605 00584 EU 1998 6 5 SIMA981031 1 19980413 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 431AT 810 431 DFW - DURING P5-2 CHECK, MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE FORWARD PART OF THE CABIN NOT WORKING PROPERL Y. BATTERY PACK FOR POWER SUPPLY 43WL WAS REMOVED AND REPLACED. OPERATIONAL CHECK SAS SATISFACTORY. AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998060500585 19980605 00585 EU 1998 6 5 SIMA981021 1 19980412 A 3350 167006 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 211 ORD - FLT 4087 - ONE FLOOR PROX LIGHT INOP DUE TO BROKE WIRE. MEL'D PER 33-22 AND RETURNED A/C TO SERVICE. R/I'D BULB AND REPAIRED WIRE CONNECTION. PERFORMED OPERATIONAL CHECK SATIFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998060500586 19980605 00586 EU 1998 6 5 SIMA980982 1 19980408 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 0610 536 GRR - FORWARD FLOOR ESCAPE PATH LIGHT INOPERATIVE. RAI BATTERY PACK. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND A/ C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998060500587 19980605 00587 NM 1998 6 5 SABA980026 1 19980409 A 2910 HYD LINE DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE LOOSE A SABA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 33 859MA 361 CLT - FLT 5234 - ON FLIGHT FROM CLT TO AGS, DURING CLIMB-OUT FROM CLT. THE NR 2 HYD SYSTEM FAILED. AIRCRAFT RETURNED T O CLT. INFLIGHT EMERGENCY WAS DECLARED. EMERGENCY PROCEDURES WERE USED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINT ENANCE FOUND A LOOSE 'B' NUT ON THE NR 2 HYD RETURN LINE AT NR 2 ENGINE FIRE WALL LOOSE. RETORQUED 'B' NUT, RUN, LEAK A ND OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998060500588 19980605 00588 NM 1998 6 5 MASA98032 1 19980218 A 2121 BC2206F120 FAN DHAV DHC8 DHC8202 2809007 NM E/E COMPT FAILED A MASA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 07 449YV 449 FLT 7565 - GCC-DEN - EN ROUTE TO DEN, PILOT RECEIVED AN AVIONICS FAN FAILED ANNUNC, WITH AN ELECTRICAL ODOR. DEN MAINTE NANCE DEFERRED THE AVIONICS COOLING FAN PER MEL 21-11. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, TH E AVIONICS COOLING FAN WAS REMOVED AND REPLACED. (M) 2 H 7 2 4T RT A13NM 1998060500589 19980605 00589 NM 1998 6 5 F3LA98026 1 19980410 A 5313 STRINGER BOEING 737 737201 1384454 NM BS440-500 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 14-R, BS 440-500, AND CRACK IN STRINGER 14-R, BS 440-448 . MAINTENANCE REPAIRED CORRODED AREAS, PER SRM 51-30-2, 53-30-1,53-30-3 AND 51-40-2. FABRICATED REPLACEMENT PARTS AND REPAIRED CRACK PER SRM 53-30-3, FIGURE 16, SRM 53-30-30 AND SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998060500590 19980605 00590 NM 1998 6 5 F3LA98025 1 19980409 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 500 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, INSPECTION REPORTED STRINGER 16-R CRACKED AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION L IGHT. MAINTENANCE REMOVED A 1 INCH BY 1.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, AND ER 98-0277. (M) 2 L 7 2 4F A16WE 1998060500591 19980605 00591 NM 1998 6 5 F3LA98023 1 19980406 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 450-459 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-L, BS 450-459. MAINTENANCE REMOVED A 3 INCH BY 2.5 I NCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, PAGES 3 AND 4, SRM 53-30-3, FIGURE 16, SRM 53-30-3, PAGES 51-53, AND SRM 51-30-00. (M) 2 L 7 2 4F A16WE 1998060500592 19980605 00592 NM 1998 6 5 F3LA98028 1 19980415 A 5330 SKIN BOEING 737 737201 1384454 NM BS 1018 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, INSPECTION REPORTED BULGE IN SKIN AT BS 1018 BETWEEN STRINGER 27-R AND 28-R. MAINTENANCE REMOVED DAMAGED AREA (7.1 INCH BY 2 INCH). FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3, PAGE 97, SRM 53-30-3, FIGURE 128, SRM 51-30-2, AND SRM 51-20-4, PARAGRAPH B. (M) 2 L 7 2 4F A16WE 1998060500593 19980605 00593 NM 1998 6 5 F3LA98029 1 19980417 A 5330 SKIN BOEING 737 737201 1384454 NM BS 415-430 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, INSPECTION REPORTED SKIN PILLOWING AT BS 415-430, STRINGER 18R TO 19R. MAINTENANCE REMOVED A 13 I NCH BY 20 INCH CORRODED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, AND 53-30-3. (M) 2 L 7 2 4F A16WE 1998060500594 19980605 00594 NM 1998 6 5 F3LA98033 1 19980421 A 5754 SKIN BOEING 737 737317 138447P NM NR 1 LE FLAP CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 EICHH 23177 PAE - DURING C-CHECK, INSPECTION REPORTED NR 1 SLAT SKIN CRACKED AROUND FASTENER HEADS. MAINTENANCE REMOVED DAMAGED ARE A (18 INCH BY 4.5 INCH). FABRICATED REPLACEMENT PARTS PER BOEING DRAWING 65C 30133, SHEET 3, AND REPAIRED PER SRM 51-40 -02. (M) 2 L 7 2 4F RT A16WE 1998060500595 19980605 00595 NM 1998 6 5 F3LA98032 1 19980418 A 5330 SKIN BOEING 737 737201 1384454 NM BS 294 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, INSPECTION REPORTED BULGING SKIN AT AFT CORNER OF CUTOUT AT BS 294.5 WL 148, RBL 24. MAINTENANCE REMOVED CORRODED AREAS. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-1, 51-30-2 AND ER 96-0315. (M) 2 L 7 2 4F A16WE 1998060500596 19980605 00596 NM 1998 6 5 F3LA98030 1 19980417 A 5230 SKIN BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LOWER CORNER OF AFT CARGO DOOR. MAINTENANCE FABRICATED REPLACE MENT PARTS AND REPAIRED PER SRM 53-30-1, FIGURE 2, SRM 51-10-6, SRM 51-30-2 AND ER 98-0291. (M) 2 L 7 2 4F A16WE 1998060500597 19980605 00597 NM 1998 6 5 F3LA98031 1 19980416 A 3350 LIGHTS BOEING 737 737201 1384454 NM CABIN INOPERATIVE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 207AU 19423 DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 15 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998060500598 19980605 00598 NM 1998 6 5 F3LA98027 1 19980414 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 360-540 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-R, BS 360-540. MAINTENANCE REMOVED CORRODED AREAS, F ABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3, FIGURE 16, AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998060500599 19980605 00599 NM 1998 6 5 F3LA98024 1 19980409 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 500 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 19423 PAE - DURING C-CHECK INSPECTION, FOUND STRINGER 16L CRACKED AT BS 500B PLUS 19 INCHES, AFT OF WING ILLUMINATION LIGHT. M AINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, SRM 51-10-1 AND ER 98-0277. (M) 2 L 7 2 4F A16WE 1998060500600 19980605 00600 NM 1998 6 5 EISA98084 1 19980405 A 3350 BULB BOEING 727 7272M7 138407S NM CABIN FAILED A EISA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 721RW 21200 L1 DOOR EMERGENCY LIGHT BULB INOPERATIVE. GENERATED BY PILOT REPORT. RELAMPED AS REQUIRED PER MM 30-00, CHECK GOOD. ( M) 2 L 7 3 4F A3WE 1998060500601 19980605 00601 WP 1998 6 5 EISA98083 1 19980409 A 5542 SKIN DOUG DC9 DC931 3022065 WP RUDDER CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 DURING REMOVAL OF PAINT, A CRACK WAS FOUND ON RIGHT SIDE RUDDER AT STATION ZR 25. FABRICATED AND INSTALLED REPAIR DOUBL ERS PER SRM 55-03 FIGURE 8. (M) 2 L 7 2 4F A6WE 1998060500602 19980605 00602 WP 1998 6 5 EISA98082 1 19980409 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 260 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 DURING HIGH FREQUENCY EDDY CURRENT INSPECTION FOR CRACKS AT DENT LOCATION, FOUND CRACK JUST BELOW DENT AT LIGHTNING STRI KE AT FS 260 AND LONGERON 19L. CUT OUT, FABRICATED DOUBLERS AND INSTALLED PER SRM 53-04 FIGURE 38. (M) 2 L 7 2 4F A6WE 1998060500603 19980605 00603 WP 1998 6 5 EISA98081 1 19980409 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 275 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 WHILE ACCOMPLISHING AD 97-03-05, CORROSION WAS NOTED ON UPPER FUSELAGE SKIN, UNDER NR 1 AND NR 2 ADF ANTENNAS AT APPROXI MATELY FS 275. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLERS PER SRM 53-04 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1998060500604 19980605 00604 WP 1998 6 5 EISA98080 1 19980409 A 5730 SKIN DOUG DC9 DC931 3022065 WP LT WING LE PUNCTURED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 WHILE ACCOMPLISHING 'B' CHECK ROUTINE WORK CARD, NOTED A PUNCTURE IN WING LEADING EDGE JUST OUTBOARD OF FUSELAGE, LEFT S IDE. FABRICATED AND INSTALLED DOUBLER PER SRM 57-06A, 57-01 AND 51-10-05. (M) 2 L 7 2 4F A6WE 1998060500605 19980605 00605 WP 1998 6 5 EISA98079 1 19980409 A 5280 SKIN DOUG DC9 DC931 3022065 WP LT NLG DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 WHILE ACCOMPLISHING 'B' CHECK ROUTINE WORK CARD, NOTED A 3 INCH CRACK IN SKIN OF LEFT FWD NOSE GEAR TRAILING EDGE. REMO VED AND REPLACED LEFT NOSE GEAR DOOR PER MM 32-22-01. (M) 2 L 7 2 4F A6WE 1998060500606 19980605 00606 WP 1998 6 5 EISA98078 1 19980409 A 5280 DOOR DOUG DC9 DC931 3022065 WP NLG CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 WHILE ACCOMPLISHING 'B' CHECK WORK CARD, TWO 2 INCH CRACKS WERE NOTED ON LEFT FWD NOSE GEAR DOOR TRAILING EDGE. REMOVED AND REPLACED LEFT NOSE GEAR DOOR PER MM 32-22-01. (M) 2 L 7 2 4F A6WE 1998060500607 19980605 00607 WP 1998 6 5 EISA98077 1 19980409 A 5754 SKIN DOUG DC9 DC931 3022065 WP NR 1 LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 WHILE ACCOMPLISHING 'B' CHECK WORK CARD, A .20 INCH LONG CRACK WAS NOTED AT OUTBOARD END OF NR 1 SLAT. STOP DRILLED CRA CK, FABRICATED AND INSTALLED DOUBLER PER SRM 57-02. (M) 2 L 7 2 4F A6WE 1998060500608 19980605 00608 WP 1998 6 5 EISA98076 1 19980409 A 5280 SKIN DOUG DC9 DC931 3022065 WP NLG DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 WHILE ACCOMPLISHING 'B' CHECK WORK CARD, A CRACK WAS NOTED ON LEFT NOSE GEAR DOOR TRAILING EDGE, RUNNING THROUGH A RIVET . REMOVED AND REPLACED NOSE GEAR DOOR PER MM 32-22-1. (M) 2 L 7 2 4F A6WE 1998060500609 19980605 00609 WP 1998 6 5 EISA98075 1 19980409 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 945VJ 47066 DURING ACCOMPLISHMENT OF 'B' ROUTINE WORK CARD, NOTED LOWER SURFACE OF TAILCONE AREA AFT OF STATION 1087, THERE IS A .5 INCH CRACK IN THE EXTERIOR SKIN AT LONGERON 29L. DRILLED OUT CRACK PER SRM 53-04 FIGURE 38. INSTALLED RIVET PER SRM 53 -04 FIGURE 38 AND SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1998060500612 19980605 00612 WP 1998 6 5 AALA980699 1 19980405 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7549A 53031 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT FORWARD GALLEY INOPERATIVE. RESEATED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998060500613 19980605 00613 WP 1998 6 5 AALA980694 1 19980403 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 476AA 49651 DFW - DURING OVERNIGHT MAINTENANCE, STAIRWAY EMERGENCY LIGHTS WERE INOPERATIVE. REPAIRED CHAFED STAIRWAY EMERGENCY EXIT LIGHTING WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998060500614 19980605 00614 NM 1998 6 5 AALA980740 1 19980411 A 2611 PU90461AR3 DETECTOR BOEING 767 767223 1385123 NM CABIN DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 332AA 22331 LHR - FLT 46 - DURING CRUISE, FORWARD MID CABIN LAVATORY SMOKE DETECTOR CHIMED CONTINUOUSLY. REPLACED FORWARD MID CABIN LAVATORY SMOKE DETECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500615 19980605 00615 NM 1998 6 5 AALA980640 1 19980330 A 2611 PU90461AR3 SMOKE DETECTOR BOEING 767 767323 1385205 NM FWD LAVATORY DIRTY A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 380AN 25449 LHR - DURING CRUISE JFK-LHR, FORWARD LAVATORY FIRE DETECTION LIGHTS ILLUMINATED INTERMITTENTLY. CLEANED FORWARD LAVATOR Y SMOKE DETECTOR AND LAVATORY COMPARTMENT INSPECTION REVEALED NO FURTHER ABNORMALITIES. SYSTEM GROUND CHECKED NROMAL OP ERATION. (M) 2 L 7 2 4F RT A1NM 1998060500616 19980605 00616 NM 1998 6 5 AALA980753 1 19980413 A 3350 0201820001 LIGHT BOEING 767 767323 1385205 NM R1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 382AN 25451 SFO - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOD LIGHT IN R1 DOOR INOPERATIVE. REPLACED R1 DOOR EMERGENCY FLOOD LIGHT BASE ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500617 19980605 00617 NM 1998 6 5 AALA980752 1 19980413 A 3350 CONNECTOR BOEING 767 767223 1385123 NM FUSELAGE DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 301AA 22307 SFO - DURING OVERNIGHT MAINTENANCE, EXTERIOR EMERGENCY EXIT LIGHT FORWARD OF AFT CARGO DOOR INOPERATIVE. CLEANED AND RE SEATED CONNECTORS ON EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500618 19980605 00618 NM 1998 6 5 AALA980718 1 19980407 A 3350 PIN BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 308AA 22314 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTS FROM SEAT ROWS 9AB THROUGH 19AB INOPERATIVE. RESEATED PU SHED OUT PIN ON ELECTRICAL CONNECTOR AT SEAT 19A. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500619 19980605 00619 NM 1998 6 5 AALA980717 1 19980408 A 3350 LIGHTS BOEING 767 767323 1385205 NM CABIN INTERMITTENT A AALA K NONE L NO TEST CR CRUISE 1 SW 07 361AA 24042 LHR - FLT 136 - DURING CRUISE, EMERGENCY EXIT LIGHTS ILLUMINATED FOR SEVERAL MINUTES AND EXTINGUISHED. MAINTENANCE CHEC KED AND TESTED EMERGENCY EXIT LIGHT SYSTEM UNABLE TO DUPLICATE INTERMITTENT FAULT. SYSTEM GROUND CHECKED NORMAL OPERATI ON. (M) 2 L 7 2 4F RT A1NM 1998060500620 19980605 00620 NM 1998 6 5 AALA980703 1 19980406 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 390AA 27450 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT A SEAT ROW 17AB INOPERATIVE. CLEANED EMERGENCY EXIT PATH LIGHT ASSEMBLY CONTACTS AT SEAT ROW 17AB AFTER REPLACING LAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500621 19980605 00621 NM 1998 6 5 AALA980678 1 19980402 A 3350 1722331 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386AA 27060 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 41H INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT SIDE WALL CONNECTOR AT PASSENGER SEAT ROW 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500622 19980605 00622 NM 1998 6 5 AALA980638 1 19980327 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 617AM 24525 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED EMERGENCY EX IT FLOOR PATH LIGHTING WIRES IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998060500623 19980605 00623 NM 1998 6 5 AALA980698 1 19980404 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325AA 22326 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT PASSENGER SEAT 29H INOPERATIVE. RESECURED EMERGENCY EXIT PATH LIGHT CONNECTOR AT PASSENGER SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500624 19980605 00624 NM 1998 6 5 AALA980693 1 19980404 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHTING AT PASSENGER SEAT 40HJ INOPERATIVE. REPLACED EMERGENC Y EXIT PATH LIGHT CONNECTOR AT PASSENGER SEAT 40HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500625 19980605 00625 NM 1998 6 5 AALA980692 1 19980403 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 JFK - DURING OVERNIGHT MAINTENANCE, AFT LEFT DOOR EMERGENCY EXIT MARKER SIGN INOPERATIVE. REPAIRED SHORTED EMERGENCY EX IT PATH LIGHT WIRE AT PASSENGER SEAT 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998060500626 19980605 00626 EU 1998 6 5 C2XA98IA137 1 19980421 A 5320 S53970916362 SUPPORT AEROSP ATR42 ATR42500 EU FRAME 29 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING C-CHECK INSPECTION, FOUND WING TO FUSELAGE FAIRING FRAME NR 29 RIGHT CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR 42 500 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 1998060500627 19980605 00627 SO 1998 6 5 C2XA98IA136 1 19980415 A 5320 12006150001 BUTT STRAP EMB 120 EMB120RT SO FRAME CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 39 TO 46. MAINTENANCE REMOVED AND REPLACED THE BUTT STRAP IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500628 19980605 00628 SO 1998 6 5 C2XA98IA135 1 19980415 A 5320 12006152002 BUTT STRAP EMB 120 EMB120RT SO FRAME 39-46 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP BETWEEN FRAMES 39 AND 46 WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE BUTT STRAP IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500629 19980605 00629 SO 1998 6 5 C2XA98IA134 1 19980415 A 5713 12004389001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURNG C-CHECK INSPECTION, THE PREVIOUS REPAIR AT STRINGER 10 OF THE LEFT WING WAS FOUND TO BE CRACKED BETWEEN RIBS 7 AND 8. MAINTENANCE REMOVED AND REPLACED THE REPAIR DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORI ZATION EC5710-01010 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500630 19980605 00630 SO 1998 6 5 C2XA98IA133 1 19980415 A 5320 12031597602 DRAG ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE RIGHT DRAG ANGLE ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE R EPAIRED THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5530-01013 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500631 19980605 00631 SO 1998 6 5 C2XA98IA132 1 19980415 A 5320 12004149001 T-PROFILE EMB 120 EMB120RT SO FRAME 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 36 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED T-PROFILE IAW EMB 120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500632 19980605 00632 SO 1998 6 5 C2XA98IA131 1 19980415 A 5320 12027928001 BUTT STRAP EMB 120 EMB120RT SO FRAME 30-34 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER BUTT STRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 30 AND 34. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB-120 SRM 51-20-04 AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500633 19980605 00633 SO 1998 6 5 C2XA98IA130 1 19980415 A 5313 12004973005 STRINGER EMB 120 EMB120RT SO FRAME 41-42 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, STRINGER 21 LEFT WAS FOUND TO BE CORRODED BETWEEN FRAMES 41 AND 42. MAINTENANCE REMOVE D THE DAMAGED SECTION OF STRINGER AND PERFORMED A SPLICE REPAIR IAW EMB120 SRM 53-00-03 AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500634 19980605 00634 SO 1998 6 5 C2XA98IA129 1 19980415 A 5320 12046158002 BUTT STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE CENTER BUTT STRAP AT FRAMES 25-30 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED BUTT STRAP IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998060500635 19980605 00635 WP 1998 6 5 CALA9800934 1 19980601 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 INCH CRACK IN FORWARD PIT FRAME AT STA 446, STRINGER 29R. THE CRACK WAS STOP DRILLED. A REPAIR WA S FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998060500636 19980605 00636 WP 1998 6 5 CALA9800935 1 19980601 A 5210 INTERCOSTAL DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A .25 INCH CRACK IN MAIN CABIN DOOR INTERCOSTAL FORWARD OF LOCK MECHANISM. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998060500637 19980605 00637 WP 1998 6 5 CALA9800936 1 19980601 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 253 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND A 2 DIAMETER HOLE IN FUSELAGE SKIN SIXTEEN INCHES ABOVE AND TWO INCHES AFT OF FORWARD LEFT LAV SERVICE PANEL (STA 253, LONGERON 18-19L). A DOUBLER WAS INSTALLED IAW SRM 53-04, CLASS II, PAGE 33, FIGURE 12B, SHEET 1 AND A D IP WAS INITIATED FOR REPETITIVE INSPECTION. 2 L 7 2 4F A6WE 1998060500638 19980605 00638 WP 1998 6 5 CALA9800937 1 19980601 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 239 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND LONGERON 30 CORRODED AT STA 239 IN FORWARD BAGGAGE BIN. THE CORRODED AREA WAS REMOVED AND A LONGERON R EPAIR WAS INSTALLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1998060500639 19980605 00639 WP 1998 6 5 CALA9800938 1 19980602 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJMT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 THE TAIL CONE RELEASE PULLED HIGH FROM EXTERIOR HANDLE. THE LATCH LEVERS, LEVER CABLES, AND EXTERNAL RELEASE CABLE SYST EM WERE ADJUSTED IAW MM 53-53-00, PARAGRAPH A. 2 L 7 2 4F A6WE 1998060500640 19980605 00640 WP 1998 6 5 CALA9800939 1 19980602 A 5320 TIE DOWN DOUG DC9 DC982 3022082 WP BS 1007-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND AFT CARGO RT SIDE FLOOR TIE DOWN STRIP CORRODED WITH SHEARED SCREWS AND CRACKED FLANGE FROM STA 1007 TO 1155. THE CORRODED AREA WAS CUT OUT, REPAIR SPLICES WERE INSTALLED IAW ECRA 5320-01521. 2 L 7 2 4F A6WE 1998060500641 19980605 00641 WP 1998 6 5 CALA9800940 1 19980602 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 160 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN LONGERON 2L AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED, A REPAIR WAS FA BRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, SHEET 1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998060500642 19980605 00642 WP 1998 6 5 CALA9800941 1 19980602 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 237 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD PIT RT INTERCOSTAL FRAME L-ANGLE AT FS 237, RBL 17. A NEW ANGLE WAS FABRIC ATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998060500643 19980605 00643 WP 1998 6 5 CALA9800942 1 19980602 A 5720 BRACKET DOUG DC9 DC932 3022066 WP RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN BRACKET OF RT WING LEADING EDGE PANEL FRAME. THE BRACKET WAS REMOVED, A NEW ANGLE B RACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 1998060500644 19980605 00644 WP 1998 6 5 CALA9800943 1 19980602 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 256 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2.75 INCH CRACK IN LT FORWARD PIT FLOOR SUPPORT AT FS 256, LBL 35. THE CRACK WAS STOP DRILLED AND AN L-ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263, SRM 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998060500645 19980605 00645 WP 1998 6 5 CALA9800944 1 19980602 A 5320 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .25 INCH CRACK IN SHEAR TIE AT FS 965 BETWEEN STRINGER 13R AND 12R, FORWARD OF AFT LAV. THE CRACK WA S STOP DRILLED, REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 28. 2 L 7 2 4F A6WE 1998060500646 19980605 00646 WP 1998 6 5 CALA9800945 1 19980602 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 955.091 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 11.25 INCH CRACK IN LONGERON 14R AT STA 955.091. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02, FIGURE 2. LONGERON AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-02, FIGURE 18, 51-10-3, 51-30- 2, FIGURE 8, AND 51-30-5. 2 L 7 2 4F A6WE 1998060500647 19980605 00647 NM 1998 6 5 98FDEA00388 1 19980601 A 5311 BELLFRAME BOEING 727 727225 1384077 NM BS 680 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 466FE 21292 STA-TUL: LOWER FWD CARGO HAS DAMAGED BELLFRAME BS 680 BETWEEN STR 25R AND 23R. DAMAGED AREA OF BELLFRAME REMOVED. REP AIR OF FRAME PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998060500648 19980605 00648 NM 1998 6 5 98FDEA00389 1 19980601 A 5330 6516203 SKIN BOEING 727 72721C 138400M NM BS 870-867 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 STA-PAE: CORROSION (C57-174-01) LOWER CENTER TANK SKIN BS 870-867, WL 138, LBL 65- RBL 65, FOUND WHILE WORKING NR 0734. 2 L 7 3 4F A3WE 1998060500649 19980605 00649 NM 1998 6 5 98FDEA00390 1 19980603 A 3231 RETRACT MECH BOEING 727 7272S2F 1384O81 NM NLG DOOR MALFUNCTION A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 213FE 22935 ON TAKEOFF WHEN LANDING GEAR WAS RETRACTED NOSE GEAR DOOR A REMAINED ON. NOISE IN NOSE GEAR AREA CONFIRMED DOORS WERE N OT CLOSED. GEAR WAS RECYCLED AND ALL FURTHER OPERATIONS WERE NORMAL. ADJUSTED BOTH NOSE GEAR DOOR SWITCHES AS PER MAIN TENANCE MANUAL 32-62-11 PAR 3-B PAGE 402 AND 403, OPERATIONAL CHECK GOOD. 2 L 7 3 4F A3WE 1998060500650 19980605 00650 WP 1998 6 5 ABXA9800478 1 19980528 A 3260 H1419951 SWITCH DOUG DC9 DC933F 302207A WP NLG FAILED A ABXA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 931AX 47384 NOSE GEAR GREEN DOWN LIGHT FAILED TO ILLUMINATE. GEAR UNSAFE LIGHT OPERATED NORMAL. RECYCLED GEAR, SAME RESULTS. NORM AL LANDING WAS ACCOMPLISHED. REPLACED NOSE LANDING GEAR DOWNLOCK SWITCH IAW DC9 SMM 32-60-00. 2 L 7 2 4F A6WE 1998060500651 19980605 00651 NE 1998 6 5 ABXA9800479 2 19980602 A 7200 ENGINE DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 2 FAILED A ABXA E ENGINE SHUTDOWN E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 845AX 41683 46157 669579 DURING CRUISE FLIGHT AT FL 280, MACH.82, A SUDDEN VIBRATION WAS FELT. NR 2 ENGINE INDICATED; EGT 540, N2 80 PERCENT, OI L TEMP 125 DEG. OIL QUANTITY WAS ZERO AND EPR WAS 1.0. NR 2 ENGINE WAS SHUTDOWN AND EMERG CHECKLIST WAS ACCOMPLISHED. ENGINE WINDMILLED AT APPROX 35 PERCENT N2, OIL PRESSURE INDICATED 15-20 PSI. ENGINE WINDMILLED FOR 2 HRS AND 20 MIN. AIRCRAFT 3 ENGINE FERRIED TO ILN. NR 2 ENGINE WAS REPLACED. 2 L 7 4 4F 4 F 4A25 1E8 1998060500652 19980605 00652 WP 1998 6 5 DLL10981160 1 19980529 A 5711 1602821103 SPAR WEB LKHEED 1011 10113851 5265010 WP BS 1103 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 THE FS 1103 INTERMEDIATE SPAR WEB WAS FOUND WITH 4 INCH LONG CRACK EMANATING FROM THE LOWER OUTBOARD CORNER OF THE LBL 6 0 PASS THROUGH HOLE. THE CRACK WAS ROUTED OUT AND A DOUBLER AND TRIPLER INSTALLED TO REPAIR THE AREA PER ER/A 364887-1 4 REV A. 2 L 7 3 4F A23WE 1998060500653 19980605 00653 WP 1998 6 5 DLL19981161 1 19980529 A 5711 REAR SPAR LKHEED 1011 10113853 5265020 WP WS 322 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 762DA 193Y1210 THE RT WING REAR SPAR WAS FOUND WITH TWO CRACKED FASTENER HOLES DURING ROUTINE INSPECTIONS. ONE HOLE WAS COMMON TO THE UPPER WING SKIN AND SPAR CAP AND THE OTHER TO THE SPAR WEB AND UPPER CAP. BOTH HOLES WERE APPROX AT IWS 322. BOTH HO LES WERE OVERSIZED TO REMOVE THE CRACKS, COLD WORKED AND BUSHED. AN EXTERNAL SKIN DOUBLER WAS ALSO INSTALLED. THE REPA IR WAS PER ER/A 364903-14AD, REV A. 2 L 7 3 4F A23WE 1998060500654 19980605 00654 WP 1998 6 5 DLL19981162 1 19980529 A 5711 REAR SPAR LKHEED 1011 10113853 5265020 WP WS 322 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 762DA 193Y1210 THE LT WING REAR SPAR WAS FOUND WITH TWO CRACKED FASTENER HOLES COMMON TO THE UPPER WING SKIN AND SPAR CAP AT APPROX IW S 322. THE CRACKS WERE FOUND DURING ROUTINE INSPECTIONS AND WERE REMOVED BY OVERSIZING THE HOLES. THE OVERSIZE HOLES WERE COLD WORKED, BUSHED, AND NEW FASTENERS INSTALLED PER ER/A 364902-14AD, REV A. 2 L 7 3 4F A23WE 1998060500655 19980605 00655 NM 1998 6 5 DL72K981163 1 19980529 A 5711 65192922 SPAR WEB BOEING 727 727232 1384082 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 466DA 20743 THE CENTER WING REAR SPAR WEB WAS FOUND WITH 3.5 INCH LONG CRACK AT RBL 3. THE CRACK IS NEAR THE UPPER CAP AT A CHEM-MI LL RADIUS IN THE WEB AND IS TYPICAL OF AD 97-25-15. THE CRACK WAS ROUTED OUT AND A LOCAL DOUBLER REPAIR WAS INSTALLED P ER ER/A 364880-14, REV B. MANDATED INSPECTIONS ARE CONTINUED UNTIL COMPLETE SPAR MODIFICATION AT NEXT HMV. 2 L 7 3 4F A3WE 1998060500656 19980605 00656 NM 1998 6 5 DL72S981164 1 19980522 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 RIGHT ELEVATOR TRAILING EDGE DELAMINATED 2 PLACES. REPAIRED PER M/M 55-20-0 PG 801. 2 L 7 3 4F A3WE 1998060500657 19980605 00657 NM 1998 6 5 DL72W981166 1 19980601 A 5753 SHIM BOEING 727 727247 138408F NM TE FLAP TRACK MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 DURING ROUTINE INSPECTIONS PER SI 4-58662-12AD, LAMINATED SHIMS WERE FOUND MIGRATED GREATER THAN THE .25 LIMIT ALLOWED P ER BAC S/B 727-57-0178 AND AD 90-07-05. THE SHIMS WERE REPLACED PER THE REQUIREMENTS OF THE S/B AND THE AD. THE INSPEC TIONS PER SI 4-58662-12AD WILL CONTINUE. THE REPAIR WAS DOCUMENTED PER ER/A 364927-14AD, REV A. 2 L 7 3 4F A3WE 1998060500658 19980605 00658 NM 1998 6 5 DL73E981167 1 19980601 A 3350 BATTERY PACK BPS73 BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 244WA 23518 L2 DOOR EXTERIOR EMER LIGHT INOP AND 3 AFT LEFT CABIN LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F A16WE 1998060500659 19980605 00659 NM 1998 6 5 DL72W981168 1 19980602 A 3350 BATTERY PACK 900542 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA UA4797 22108 CENTER AISLE BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATTERY RACK, CHECKS OK. 2 L 7 3 4F A3WE 1998060500660 19980605 00660 NM 1998 6 5 DL72W981169 1 19980602 A 3350 BATTERY PACK 900542 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 290WA 10883 22108 FIRST CLASS EMERGENCY LIGHT INOP. REPLACED BATTERY RACK, CHECKS OK. 2 L 7 3 4F A3WE 1998060500661 19980605 00661 NM 1998 6 5 DL72S981170 1 19980522 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 STA 1303 WEB CRACKED LT AND RT SIDE AT BOTTOM INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1998060500662 19980605 00662 NM 1998 6 5 DL72L981172 1 19980601 A 3350 BATTERY S106 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 21306 ON L/O CK, AISLE EMERG LIGHT OVERHEAD ROW 13 DID NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998060500663 19980605 00663 NM 1998 6 5 DL72L981173 1 19980601 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 21306 ON L/O CK, LIGHTED EXIT SIGNS OVER LT O/W EXIT DID NOT ILLUMINATE. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998060500664 19980605 00664 NM 1998 6 5 DL72S981175 1 19980602 A 5754 SKIN BOEING 727 727232 1384082 NM NR 4 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 FOUND AT B2 LETTER CHECK, 2 CRACKS .75 INCH AND 2 INCH AT NR 4 L/E FLAP O/B HINGE CUTOUT. REPAIRED PER ERA 364950-14 AN D M/M 57-53-0. 2 L 7 3 4F A3WE 1998060500665 19980605 00665 NM 1998 6 5 DL73S981176 1 19980601 A 2930 TRANSMITTER 4006454 BOEING 737 737232 1384475 NM A-HYD SYST FAILED A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 328DL DL1083 23100 HYD QTY GAUGE F/O INST PANEL A-SYS QTY GAUGE INDICATES DECREASING FLUID LEVEL BEGAN AT 3.5 NOW AT 1.75. PERFORMED WALKA ROUND OF A/C CKED ALL FLT. CONTROLS AND LANDING GEAR NO LEAKS NOTED. FOUND COCKPIT QUTY IND STICKING, REPLACED TRANSMI TTER, OPS CK GOOD, LKS CK GOOD. USAIR LOANER PART INSTALLED. 2 L 7 2 4F RT A16WE 1998060500666 19980605 00666 NE 1998 6 5 DL757981177 2 19980602 A 7261 1A821101 OIL LINE 1A821101 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE CRACKED A DALA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 SO 27 674DL 25979 716478 THE MAIN OIL BEARING MANIFOLD SCAVENGE LINE CRACKED AT AN ELBOW WHERE IT GOES INTO THE TOWER SHAFT, MFG NR 1A821101. RE PLACED LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998060500667 19980605 00667 NM 1998 6 5 SCNA98708 1 19980515 A 5320 STIFFENER BOEING 727 727225 1384077 NM BS 360 GOUGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 283SC 22559 DURING A HEAVY MAINT CHECK VERTICAL STIFFENER WAS FOUND GOUGED AT STATION 360 STRINGER 19 LEFT. REMOVED EXTRUDED ANGLE BRACKET AT STATION 390 STRINGER 19 LEFT, FOUND TO BE OUT LIMITS PER B727 514004. FABRICATED REPAIR PARTS IAW SRM B727 5 1404. ALODINED AND PRIMED PER B727 SRM 514005. INSTALLED PER B727 SRM 513002. 2 L 7 3 4F A3WE 1998060500668 19980605 00668 NM 1998 6 5 DHL98726005 1 19980531 A 3260 512776 ACCESSORY UNIT 656021132 BOEING 727 727228 NM RT MLG MALFUNCTIONED A DHLA A UNSCHED LANDING A FLAME/FIRE CR CRUISE 1 SO 01 726DH 1742 20409 AT FL 270 280 KTS, ENCOUNTER MODERATE TURBULENCE, GEAR WARNING HORN SOUNDED. RT MAIN LANDING GEAR GREEN DOWN AND LOCKED LIGHT CAME ON. MAIN GEAR DOOR LIGHT ON S/O PANEL CAME ON. A SMALL ELECTRICAL FIRE WAS NOTED BEHIND LOUVERED PAN EL AB OVE S/O STATION. NUMEROUS C/B' S TRIPPED AND FIRE WENT OUT. GEAR WARNING COULD NOT BE SILENCED EXCEPT BY PULLING GEAR WARNING HORN C/B. REMOVED AND REPLACED CONNECTOR 4774J, REMOVED AND REPLACED AURAL WARNING DEVICE AND LANDING GEAR ACCY UNIT. REPLACED DAMAGED WIRES. REPLACED RIGHT GEAR AND NOSE GEAR GREEN AND RED MODULES. REMOVED AND REPLACED R2 WINDO W HEAT CONTROLLER. AFFECTED SYSTEMS AND COMPONENTS OPS CHECK GOOD PER M/M 32-61-00 AND 31-26-0 AND 32-62-11. 2 L 7 3 4F A3WE 1998060500669 19980605 00669 NM 1998 6 5 DHL98727002 1 19980603 A 5610 ROLLER BOEING 727 727228 NM R2 WINDOW LOOSE A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 727DH 20204 R2 WINDOW EXCESSIVE AIR LEAK AT 2.8 PSI. INSPECTED R2 WINDOW, FOUND BOTTOM FWD ROLLER OFF AND WINDOW LOOSE IN FRAME. R EINSTALLED ROLLER AND REPRESSURIZED TO 7 PSI. NO LEAKS OR SQUEALS NOTED, OPS CHECK GOOD PER MM 56-12-11. 2 L 7 3 4F A3WE 1998060500670 19980605 00670 1998 6 5 DHL98804001 4 19980603 A 3442 20171570153 RT UNIT DOUG DC8 DC873F 302199F WP FWD FUSELAGE MALFUNCTIONED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 804DH 46124 RADAR ANTENNA TILT WENT TO FULL NOSE UP ON DEPARTURE. REPLACED RADAR R/T AND CONTROL PANEL. 2 L 7 4 4F RT 4A25 1998060500671 19980605 00671 WP 1998 6 5 RRXA98224 1 19980531 A 3260 CONNECTOR DOUG DC8 DC873F 302199F WP NLG LOOSE A RRXA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 WP 15 792FT 46046 ON 2 MILE FINAL NOSE GEAR LIGHT WENT OUT, RECYCLED GEAR, NO LIGHT BELOW 1,000 FT. GPWS SOUNDED, WENT AROUND, RECYCLED G EAR. GOT THREE GREEN, VERIFIED BY LOOKING THRU NOSE GEAR HOLE. SECURED LOOSE CONNECTOR AT DOWN LATCH SWITCH. ELECTRIC AL AND VISUAL CHK GOOD. 2 L 7 4 4F RT 4A25 1998060500672 19980605 00672 WP 1998 6 5 ARWA980508 1 19980603 A 2711 5598273502 SWIVEL DOUG DC8 DC862 3021970 WP AILERON TAB LEAKING A ARWA O OTHER K FLUID LOSS LD LANDING 1 SO 19 802BN 45909 ON LANDING ROLL, NOTICED HYD QUANTITY DECREASING DOWN TO STAND PIPE. REMOVED AND REPLACED AILERON TAB LOCK OUT CYLINDER SWIVEL GLAND IAW MM 27-11-7, OPERATION LEAK CHECK NORMAL. 2 L 7 4 4F 4A25 1998060500673 19980605 00673 NE 1998 6 5 VNAA9806001 2 19980602 A 7260 3022375 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 431JS 3028 DURING CRUISE, THE RIGHT HAND ENGINE OIL PRESSURE DROPPED INTO THE WARNING (AMBER) RANGE. THE CREW EXECUTED LOW OIL PR ESSURE PROCEDURES, CALLED OUT FOR IN THE CHECKLIST. THE RIGHT HAND PROPELLER WAS FEATHERED, AND THE POWER WAS SET TO FL IGHT IDLE. THE CREW DECLARED AN EMERGENCY, AND THE AIRCRAFT DIVERTED INTO CAK FOR LANDING. THE LANDING TOOK PLACE WITH OUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND ENGINE STARTER SEAL, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-60-02. OPERATION AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998060500674 19980605 00674 WP 1998 6 5 CKSA98338 1 19980601 A 2760 MECHANISM DOUG DC8 DC861 3021952 WP LT SPOILERS OUT OF ADJUST A A CKSA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 817CK 45887 FLIGHT CONTROLS ACT LIKE THEY ARE IN MANUAL REVERSION AT AIRSPEED GREATER THAN 230 KCAS. UNCOMMANDED ROLL TO THE LEFT O CCURS. DURING DESCENT AIRSPEED BELOW 230 KCAS SYSTEM OPERATES NORMALLY. ADJUSTED L-3 AND L-4 SPOILER PANELS IAW DACO M M 27-61-1, OPS CHECKS GOOD. 2 L 7 4 4F 4A25 1998060500675 19980605 00675 WP 1998 6 5 TC8A98031 1 19980528 A 7722 RESISTOR DOUG DC8 DC862F 3021972 WP NR 2 EGT FAILED A TC8A A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 23 187SK 46022 NR 2 ENGINE NEEDED TO REDUCE POWER TO 1.70 EPR TO MAINTAIN EGT LIMIT DURING TAKEOFF. ALSO, NOTED DURING IDLE EGT 375 DE GREES. REPLACED NR 2 ENGINE EGT BALANCING RESISTOR AND CALIBRATED IAW MM 77-20-2. NR 2 ENGINE RUN CARRIED OUT IAW TCA MIP CHPT 2, ALL READING WITHIN LIMITS, T/O AND IDLE. 2 L 7 4 4F 4A25 1998060500676 19980605 00676 1998 6 5 TC8A98032 4 19980531 A 3442 ANTENNA DOUG DC8 DC862F 3021972 WP RADAR MALFUNCTIONED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 187SK 46022 ON TAXI OUT, RADAR WOULD NOT TEST. RESET R/T ANTENNA WAVE GUIDE, OPS CHECK OK IAW 34-41-0. 2 L 7 4 4F 4A25 1998061200001 19980612 00001 WP 1998 6 12 VJ9800176 1 19980430 A 3350 41B004AD07G3 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 933VV 47489 EMERGENCY LIGHT OVER JUMPSEAT, L1 DOOR AND R1 DOOR INOP. REPLACED BATTERIES AND PACK, SYSTEM OPS CHECKS GOOD IAW MM 33- 50-02. 2 L 7 2 4F A6WE 1998061200002 19980612 00002 WP 1998 6 12 VJ9800177 1 19980510 A 3350 110049 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 909VJ 47322 EPL TRACK LIGHTING FROM ROW 24 TO AFT CABIN DOOR INOP. RECONNECTED CANNON PLUG TO BATTERY PACK, OPS CHECKS GOOD IAW MM 33-50. 2 L 7 2 4F A6WE 1998061200003 19980612 00003 WP 1998 6 12 VJ9800178 1 19980510 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 933VV 47489 FORWARD OVERHEAD EMERGENCY LIGHTS INOP IN GALLEY AND COCKPIT. REPLACED POWER SUPPLY, OPS CHECKS GOOD. 2 L 7 2 4F A6WE 1998061200004 19980612 00004 WP 1998 6 12 VJ9800179 1 19980604 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 914VV 47486 AFT CABIN OVERWING EXIT LIGHTS DO NOT ILLUMINATE WHEN EMERGENCY SWITCH ON. REPLACED POWER SUPPLY IAW MM 33-00, OPS CHEC KS GOOD. 2 L 7 2 4F A6WE 1998061200005 19980612 00005 NM 1998 6 12 RAAA98B1043 1 19980514 A 5312 BLKHD STIFFENER BOEING 727 72722C 138400F NM BS 1183 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1183 BULKHEAD VERTICAL STIFFENER CRACKED APPROX .2 INCH AT RB L 46.93, WL 189. REPAIRED PER S/B 727-53-0181. M-54 NR 262. 2 L 7 3 4F A3WE 1998061200006 19980612 00006 NM 1998 6 12 RAAA98B1044 1 19980514 A 5320 SILL BOEING 727 72722C 138400F NM BS 1060-1108 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND AFT CARGO COMPT DOOR SILL WEB AND CHORD CORRODED AT BS 1060 TO 1 108. REPLACED WEB AND CHORD PER SRM 51-10-6. M-54 NR 265. 2 L 7 3 4F A3WE 1998061200007 19980612 00007 NM 1998 6 12 RAAA98B1045 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1130 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1130 FRAME SHEAR TIE CORRODED AT STR 29L. REPLACED SHEAR TIE PER SRM 53-10-4. M-54 NR 278. 2 L 7 3 4F A3WE 1998061200008 19980612 00008 NM 1998 6 12 RAAA98B1046 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 1131 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-54104, FOUND STR 30 CORRODED AT BS 1131. REPAIRED PER SRM 53-10-3. M-54 NR 279. 2 L 7 3 4F A3WE 1998061200009 19980612 00009 NM 1998 6 12 RAAA98B1047 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1148 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1148 FRAME SHEAR TIE CORRODED AT STR 28R TO 30. REPAIRED PER SRM 53-10-4. M-54 NR 284. 2 L 7 3 4F A3WE 1998061200010 19980612 00010 NM 1998 6 12 RAAA98B1048 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 380-400 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-51103, FOUND STR 25R CORRODED AT BS 380 TO 400. REPAIRED PER SRM 53 -10-3. M-54 NR 293. 2 L 7 3 4F A3WE 1998061200011 19980612 00011 NM 1998 6 12 RAAA98B1049 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1110-1130 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED AD 91-06-06 EXTERNAL INSPECTION, FOUND STR 26R FUSELAGE SKIN LAP JOINT CORRODED AT BS 110 TO 1130. REP LACED SKIN PANEL FROM BS 1080.45 TO 1183 AND STR 20R TO 26RL. PER BAC MSG RVV-SEA-98-0002RR, SRM 51-10-1 AND 51-30-2. M -54 NR 309. 2 L 7 3 4F A3WE 1998061200012 19980612 00012 NM 1998 6 12 RAAA98B1050 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 698 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD PER CARD S6-25104, FOUND BS 698 FUSELAGE SKIN EXTERIOR AND ANTENNA LEAD CUTOUT D OUBLER CORRODED AT STR 27L TO 28L. REPAIRED PER BAC DWG NR 65C15379. M-54 NR 81. 2 L 7 3 4F A3WE 1998061200013 19980612 00013 SO 1998 6 12 RAAA98E8015 1 19980603 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 PAX ROW 12 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998061200014 19980612 00014 SO 1998 6 12 RAAA98E9019 1 19980603 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998061200015 19980612 00015 NM 1998 6 12 RAAA98B1051 1 19980514 A 5320 CHORD BOEING 727 72722C 138400F NM BS 940 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-25104, FOUND LT WHEEL WELL PRESSURE DECK CHORD CRACKED APPROX .5 INCH IN RADI US AT BS 940, WL 201, LBL 64. REPAIRED PER SRM 51-40-3. M-54 NR 368. 2 L 7 3 4F A3WE 1998061200016 19980612 00016 NM 1998 6 12 RAAA98B1052 1 19980514 A 5520 STRINGER BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED C1 CHECK PER CARD C-31003, FOUND LOWER RT ELEVATOR STRINGER CRACKED AT ELEV STA 35. REPAIRED PER SRM 5 1-10-1. M-54 NR 379. 2 L 7 3 4F A3WE 1998061200017 19980612 00017 NM 1998 6 12 RAAA98B1053 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1070 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1070 FRAME UPPER FLANGE CRACKED APPROX .5 INCH ABOVE STR 29R AT U-CHANNEL ATTACHMENT. REPAIRED PER SRM 51-40-3. M-54 NR 380. 2 L 7 3 4F A3WE 1998061200018 19980612 00018 NM 1998 6 12 RAAA98B1054 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1070 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1070 FRAME UPPER FLANGE CRACKED APPROX .3 INCH ABOVE STR 28R AT U-CHANNEL ATTACHMENT. REPAIRED PER SRM 51-40-3. M-54 NR 381. 2 L 7 3 4F A3WE 1998061200019 19980612 00019 NM 1998 6 12 RAAA98B1055 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1090 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1090 FRAME UPPER FLANGE CRACKED APPROX .5 INCH ABOVE STR 28R AT U-CHANNEL ATTACHMENT. REPAIRED PER SRM 51-40-3. M-54 NR 382. 2 L 7 3 4F A3WE 1998061200020 19980612 00020 NM 1998 6 12 RAAA98B1056 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1030 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1030 FRAME UPPER FLANGE DENTED ABOVE STR 29R AT U-CHANNEL ATT ACHMENT. REPAIRED PER SRM 51-40-3 AND 51-20-04. M-54 NR 383. 2 L 7 3 4F A3WE 1998061200021 19980612 00021 NM 1998 6 12 RAAA98B1057 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1030 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1030 FRAME UPPER FLANGE DENTED ABOVE STR 29L AT U-CHANNEL ATT ACHMENT. REPAIRED PER SRM 51-40-3 AND 51-20-04. M-54 NR 384. 2 L 7 3 4F A3WE 1998061200022 19980612 00022 NM 1998 6 12 RAAA98B1058 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1050 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1050 FRAME UPPER FLANGE CRACKED APPROX .4 INCH IN TWO LOCATIO NS ABOVE STR 30 AT U-CHANNEL ATTACHMENT. REPAIRED PER SRM 51-40-3. M-54 NR 385. 2 L 7 3 4F A3WE 1998061200023 19980612 00023 NM 1998 6 12 RAAA98B1059 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 1055 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND STR 28R SPLICE JOINT CORRODED AT BS 1055. REPAIRED PER SRM 53-1 0-3, FIG 1. M-54 NR 387. 2 L 7 3 4F A3WE 1998061200024 19980612 00024 NM 1998 6 12 RAAA98B1060 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 1065 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND STR 28R CORRODED AT BS 1065. REPAIRED PER SRM 53-10-3, FIG 1. M -54 NR 389. 2 L 7 3 4F A3WE 1998061200025 19980612 00025 NM 1998 6 12 RAAA98B1061 1 19980514 A 5347 TRACK BOEING 727 72722C 138400F NM BS 950-1110 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND AFT CARGO COMPT RBL 13 FLOOR TRACK CORRODED AT BS 950 TO 1110. R EPLACED TRACK PER SRM 51-10-1 AND 51-30-2. M-54 NR 392. 2 L 7 3 4F A3WE 1998061200026 19980612 00026 NM 1998 6 12 RAAA98B1062 1 19980514 A 5347 TRACK BOEING 727 72722C 138400F NM BS 636-680 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-52103, FOUND FWD CARGO COMPT LBL 18 FLOOR TRACK CORRODED AT BS 636, 646 AND 6 60 TO 680. REPLACED TRACK PER SRM 51-10-1. M-54 NR 401. 2 L 7 3 4F A3WE 1998061200027 19980612 00027 NM 1998 6 12 RAAA98B1063 1 19980514 A 5347 TRACK BOEING 727 72722C 138400F NM BS 589 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-52103, FOUND FWD CARGO COMPT LBL 18 FLOOR TRACK CORRODED AT BS 589. REPLACED TRACK PER SRM 51-10-1. M-54 NR 402. 2 L 7 3 4F A3WE 1998061200028 19980612 00028 NM 1998 6 12 RAAA98B1064 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 1076 IMPROPER A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND STR 27R PREVIOUS REPAIR AT BS 1076 NOT PER SRM. REPAIRED PER SR M 53-10-3. M-54 NR 446. 2 L 7 3 4F A3WE 1998061200029 19980612 00029 NM 1998 6 12 RAAA98B1065 1 19980514 A 5347 TRACK BOEING 727 72722C 138400F NM BS 950-1110 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND AFT CARGO COMPT LBL 19 FLOOR TRACK CORRODED AT BS 950 TO 1110. R EPLACED TRACK PER SRM 51-10-1 AND 51-30-2. M-54 NR 447. 2 L 7 3 4F A3WE 1998061200030 19980612 00030 NM 1998 6 12 RAAA98B1066 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 990-1010 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND STR 28R CORRODED AT BS 990 TO 1010. REPAIRED PER SRM 53-10-3, F IG 1. M-54 NR 449. 2 L 7 3 4F A3WE 1998061200031 19980612 00031 NM 1998 6 12 RAAA98B1067 1 19980514 A 5314 KEEL BEAM BOEING 727 72722C 138400F NM BS 960-990 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND STR 29R KEEL BEAM EXTENSION CORRODED AT BS 960 TO 990. REPAIRED PER S/B 727-53-179 AND BAC DWG NR 65C33750. M-54 NR 495 AND 499. 2 L 7 3 4F A3WE 1998061200032 19980612 00032 NM 1998 6 12 RAAA98B1068 1 19980514 A 5313 STRINGER BOEING 727 72722C 138400F NM BS 960-970 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND STR 28R CORRODED AT BS 960 TO 970. REPAIRED PER SRM 53-10-3, FI G 1. M-54 NR 498. 2 L 7 3 4F A3WE 1998061200033 19980612 00033 NM 1998 6 12 RAAA98B1069 1 19980514 A 5312 BULKHEAD CHORD BOEING 727 72722C 138400F NM BS 950 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 950 BULKHEAD LOWER CHORD CORRODED AT STR 29R. ALSO, CHORD CR ACKED APPROX 1.5 INCH AT SAME LOCATION BY TOOL DAMAGE FROM ADJACENT REPAIR IN PROGRESS. REPAIRED PER SRM 51-40-3. M-54 NR 500. 2 L 7 3 4F A3WE 1998061200034 19980612 00034 NM 1998 6 12 RAAA98B1070 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 990 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 990 FRAME UPPER FLANGE DENTED ABOVE STR 25R. REPAIRED PER SR M 53-10-4, FIG 1, SHEET 3. M-54 NR 502. 2 L 7 3 4F A3WE 1998061200035 19980612 00035 NM 1998 6 12 RAAA98B1071 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1010 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1010 FRAME UPPER FLANGE DENTED ABOVE STR 26R. REPAIRED PER S RM 53-40-4, FIG 1, SHEET 3. M-54 NR 503. 2 L 7 3 4F A3WE 1998061200036 19980612 00036 NM 1998 6 12 RAAA98B1072 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1030 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1030 FRAME UPPER FLANGE DENTED ABOVE STR 26R. REPAIRED PER S RM 53-10-4, FIG 1, SHEET 3. M-54 NR 504. 2 L 7 3 4F A3WE 1998061200037 19980612 00037 NM 1998 6 12 RAAA98B1073 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1148 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1148 FRAME UPPER FLANGE DENTED ABOVE STR 25R. REPAIRED PER S RM 51-40-3. M-54 NR 505. 2 L 7 3 4F A3WE 1998061200038 19980612 00038 NM 1998 6 12 RAAA98B1074 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1148 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1148 FRAME UPPER FLANGE DENTED ABOVE STR 23R. REPAIRED PER S RM 51-40-3. M-54 NR 506. 2 L 7 3 4F A3WE 1998061200039 19980612 00039 NM 1998 6 12 RAAA98B1075 1 19980514 A 5311 FRAME BOEING 727 72722C 138400F NM BS 990 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 990 FRAME UPPER FLANGE DENTED ABOVE STR 25L. REPAIRED PER SR M 53-10-4. M-54 NR 507. 2 L 7 3 4F A3WE 1998061200040 19980612 00040 NM 1998 6 12 RAAA98B1076 1 19980514 A 5230 DOUBLER BOEING 727 72722C 138400F NM BS 1070 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54106, FOUND AFT CARGO COMPARTMENT DOOR PREVIOUS REPAIR INTERNAL DOUBLER CRAC KED AT FWD HINGE INTERCOSTAL. REPAIRED PER SRM 51-40-3, FIG 1. M-54 NR 516. 2 L 7 3 4F A3WE 1998061200041 19980612 00041 NM 1998 6 12 RAAA98B1077 1 19980514 A 5312 BLKHD STIFFENER BOEING 727 72722C 138400F NM BS 1183 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-54104, FOUND BS 1183 BULKHEAD VERTICAL STIFFENER CRACKED APPROX .15 INCH AT L BL 46.93, WL 189. REPAIRED PER S/B 727-53-0181. M-54 NR 519. 2 L 7 3 4F A3WE 1998061200042 19980612 00042 NM 1998 6 12 RAAA98B1078 1 19980514 A 5320 DOUBLER BOEING 727 72722C 138400F NM BS 376-396 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED S6 INSPECTION PER CARD S6-51103, FOUND BS 376 TO 396 FUSELAGE SKIN INTERNAL DOUBLER CORRODED AT STR 20R TO 21R. REPLACED DOUBLER PER SRM 51-30-2. M-54 NR 520. 2 L 7 3 4F A3WE 1998061200043 19980612 00043 NM 1998 6 12 RAAA98B1079 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1115-1125 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING FUSELAGE SKIN PANEL REPLACEMENT FUSELAGE SKIN DAMAGED AT BS 1115 TO 1125 AND STR 19L TO 20L. REPAIRED PER BAC MS G NR RVV-SEA-98-0005RR AND BAC DWG NR 69-61590. M-54 NR 536. 2 L 7 3 4F A3WE 1998061200044 19980612 00044 NM 1998 6 12 RAAA98B1080 1 19980514 A 5320 CHORD BOEING 727 72722C 138400F NM BS 950 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING REPAIR OF M-54 NR 368 FOUND LT WHEEL WELL PRESSURE DECK CHORD CRACKED APPROX .7 INCH IN RADIUS AT BS 950, WL 201, LBL 64. REPAIRED PER SRM 51-40-3. M-54 NR 557. 2 L 7 3 4F A3WE 1998061200045 19980612 00045 NM 1998 6 12 RAAA98B1081 1 19980514 A 5314 KEEL BEAM BOEING 727 72722C 138400F NM BS 978 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING REPAIR OF M-54 NR 499, STR 29R KEEL BEAM EXTENSION INBD CHORD LEG TOOL DAMAGED AT BS 978. REPAIRED PER BAC MSG N R RVV-SEA-98-0006RR. M-54 NR 578. 2 L 7 3 4F A3WE 1998061200046 19980612 00046 WP 1998 6 12 CALA9800946 1 19980602 A 5320 ANGLE DOUG DC9 DC982 3022082 WP MAIN BAG BIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND Z-ANGLE REPAIR SPACER CORRODED AT MAIN BAGGAGE BIN. THE Z-ANGLE WAS REPLACED IAW SRM 53-05, FIGURE 63 AND ECRA 5300-01186. 2 L 7 2 4F A6WE 1998061200047 19980612 00047 WP 1998 6 12 CALA9800947 1 19980603 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 72825 49485 INSPECTION FOUND A 1 INCH CRACK AT EACH END OF MAIN CABIN DOOR NR 1 BEAM. THE BEAM WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998061200048 19980612 00048 NM 1998 6 12 CALA9800948 1 19980602 A 5320 SHEAR TIE BOEING 727 727224 1384076 NM BS 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND SHEAR TIE CORRODED AT STA 500, STRINGER 27R-28R. THE CORRODED AREA WAS CUT OUT, A NEW SHEAR TIE WAS FA BRICATED AND INSTALLED IAW SRM 51-30-4, FIGURE 15, REPAIR 3. 2 L 7 3 4F A3WE 1998061200049 19980612 00049 NM 1998 6 12 CALA9800949 1 19980602 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 915-937 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND CORROSION ON RT INBOARD SEAT TRACK BETWEEN STA 915 AND 937. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00- 52. 2 L 7 2 4F RT A16WE 1998061200050 19980612 00050 WP 1998 6 12 CALA9800950 1 19980603 A 3350 P4010021 BATTERY DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND FLASHLIGHT AT L-2 DOOR INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED IAW MM 25-60-00. 2 L 7 3 4F A22WE 1998061200052 19980612 00052 WP 1998 6 12 CALA9800952 1 19980515 A 5230 DOOR DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27509 47798 INSPECTION FOUND A 7 INCH CRACK IN FORWARD CARGO DOOR AFT EDGE ADJACENT TO LATCHING MECHANISM, 15 INCHES ABOVE LOWER EDG E. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998061200053 19980612 00053 WP 1998 6 12 CALA9800953 1 19980603 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBEAM CORRODED AT BS 980, RBL 18. THE L-ANGLE, FILLER, AND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4A. 2 L 7 2 4F A6WE 1998061200054 19980612 00054 WP 1998 6 12 CALA9800954 1 19980603 A 5753 BRACKET DOUG DC9 DC932 3022066 WP FLAP FAIRING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 3 INCH CRACK AT OUTBOARD FORWARD RADIUS OF RT WING NR 2 FORWARD FLAP HINGE FAIRING RETAINING BRACKET. THE BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-10-4, 51-10-2 , AND 51-30-2. 2 L 7 2 4F A6WE 1998061200055 19980612 00055 WP 1998 6 12 CALA9800955 1 19980603 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 140 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 3 INCH CRACK IN LONGERON 3L AT STA 140. A LONGERON AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 17. 2 L 7 2 4F A6WE 1998061200056 19980612 00056 WP 1998 6 12 CALA9800956 1 19980603 A 5350 BRACKET DOUG DC9 DC932 3022066 WP BS 579 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN FORWARD WING TO FUSELAGE FAIRING ATTACH BRACKET AT STA 579. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1998061200057 19980612 00057 WP 1998 6 12 CALA9800957 1 19980603 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 228 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT OF LT FORWARD CARGO COMPARTMENT, STA 228. THE FLOOR SUPPORT WAS REMO VED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061200058 19980612 00058 WP 1998 6 12 9809429853 1 19980601 A 2751 SWITCH DOUG DC9 DC951 3022051 WP TE FLAP INOPERATIVE A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 762NC 47710 DURING CLIMBOUT, THE LANDING GEAR WARNING HORN SOUNDED AND THE LANDING GEAR UNSAFE INDICATION ILLUMINATED. THE FLIGHT C REW FOLLOWED COM PROCEDURES, RETURNED TO MEM, AND LANDED WITHOUT INDICDENT. MAINTENANCE REPLACED THE S1-85 FLAP SWITCH, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998061200059 19980612 00059 WP 1998 6 12 9809439970 1 19980531 A 3260 SENSOR DOUG DC9 DC931 3022065 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 9334 47247 DURING APPROACH, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. EMERGENCY GEAR EXTENSION PR OCEDURES WERE UTILIZED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR PROXIMITY SENSOR BROKEN. R EPLACED SENSOR. ALSO, REPLACED LEFT NOSE GEAR DOOR DUE TO DAMAGE INCURRING ON LANDING. 2 L 7 2 4F A6WE 1998061200060 19980612 00060 SO 1998 6 12 COMA9810130 1 19980603 A 3350 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 22259 323 120233 EMERGENCY LIGHTS BY CABIN DOOR ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998061200061 19980612 00061 EA 1998 6 12 COMA9860132 1 19980603 A 5753 601R14303041 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 7141 C-CHECK TASK 002-27-580-100, LEFT HAND INBOARD FLAP VANE LEADING EDGE HAS CHAFE DAMAGE AT WS 56.3. REPLACED FLAP VANE L EADING EDGE. 2 L 7 2 4F RT A21EA 1998061200062 19980612 00062 EA 1998 6 12 COMA9860133 1 19980603 A 2751 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT/RT TE FLAPS MALFUNCTION A COMA O OTHER J WARNING INDICATION TO TAKEOFF 1 SO 01 912CA 7875 2502 7011 FLAPS FAILED AFTER TAKEOFF. REPLACED THE LT AND RT FLAP BPSU. 2 L 7 2 4F RT A21EA 1998061200063 19980612 00063 EA 1998 6 12 COMA9860134 1 19980603 A 3350 BR9279106 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951CA 7091 SERVICE DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A21EA 1998061200064 19980612 00064 EA 1998 6 12 COMA9860135 1 19980603 A 3230 4622 VALVE CNDAIR CL600 CL6002B19 EA NLG MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 989CA 910 7215 LANDING GEAR DISAGREE MESSAGE, CYCLED GEAR ONCE FOR NORMAL GEAR DOWN INDICATION. REPLACED THE NLG PRIORITY VALVE. 2 L 7 2 4F RT A21EA 1998061200065 19980612 00065 EA 1998 6 12 COMA9860136 1 19980602 A 5753 601R14303042 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 969CA 7141 C-CHECK TASK 002-27-680-100, RT INBD FLAP VANE LEADING EDGE HAS CHAFE DAMAGE AT WS 56.3. REPLACED FLAP VANE LEADING EDG E SKIN. 2 L 7 2 4F RT A21EA 1998061200066 19980612 00066 EA 1998 6 12 COMA9860137 1 19980603 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 EA LT MLG BROKEN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 964CA 7129 LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. LT MLG INDICATED UNSAFE. REPLACED BROKEN UPLOCK PROXIMITY SENSOR TARGET A T LT MLG UPLOCK. 2 L 7 2 4F RT A21EA 1998061200067 19980612 00067 EU 1998 6 12 QXEA9800693 1 19980509 A 5400 STRUT FOKKER F28 F28MK4000 4990810 EU NR 1 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 NR 1 THRUST STRUT IS DAMAGED IN TWO LOCATIONS APPROXIMATLEY 7 AFT IN FORWARD END AND 10 FORWARD ON AFT END. REPAIRED IA W FOKKER SRM 54-40-03, PAGE 201 TO 203 AND HORIZON AIR EA 4-71-81. 2 L 7 2 4F RT A20EU 1998061200068 19980612 00068 EU 1998 6 12 QXEA9800694 1 19980509 A 5400 STRUT FOKKER F28 F28MK4000 4990810 EU NR 2 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 NR 2 THRUST STRUT IS DAMAGED APPROXIMATELY 10 AFT OF NACELLE TO STUB WING FEED THROUGH. REPAIRED IAW FOKKER MM 54-40-03 , PAGE 201 TO 203, AND HORIZON AIR EA 4-71-81. 2 L 7 2 4F RT A20EU 1998061200069 19980612 00069 EU 1998 6 12 QXEA9800695 1 19980501 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU RT COCKPIT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CO-PILOTS OUTBOARD SEAT TRACK OUTBOARD SIDE RAIL HAS AREAS OF SMALL NICKS. REPLACED SEAT RAIL. 2 L 7 2 4F RT A20EU 1998061200070 19980612 00070 EU 1998 6 12 QXEA9800696 1 19980429 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU LT COCKPIT WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 INBOARD PILOT SEAT TRACK IS WORN TO LIMITS. REPLACED SEAT TRACK IAW FOKKER SRM 53-40-01, PAGE 201. 2 L 7 2 4F RT A20EU 1998061200071 19980612 00071 EU 1998 6 12 QXEA9800697 1 19980429 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU LT COCKPIT WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 OUTBOARD PILOT SEAT TRACK WORN TO LIMITS. REPLACED OUTBOARD SEAT TRACK IAW FOKKER SRM 53-40-01, PAGE 201B, CODE 2. 2 L 7 2 4F RT A20EU 1998061200072 19980612 00072 EU 1998 6 12 QXEA9800698 1 19980514 A 5321 FLOOR FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CORROSION ON COCKPIT FLOOR UNDER CO-PILOTS INBOARD AND OUTBOARD SEAT RAILS. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4, PAGE 9. 2 L 7 2 4F RT A20EU 1998061200073 19980612 00073 EU 1998 6 12 QXEA9800699 1 19980524 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU FRAME 1890 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CRACK THROUGH RIVET APPROXIMATELY .5 INCH LONG AT FRAME 1890 WL+ 16.141 APPROXIMATELY. REPAIRED IAW FOKKER SRM 53-02-02 , FIGURE 1. 2 L 7 2 4F RT A20EU 1998061200074 19980612 00074 EU 1998 6 12 QXEA9800700 1 19980507 A 5310 STRUCTURE FOKKER F28 F28MK4000 4990810 EU ACM BAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 RIGHTHAND ACM BAY STRESS CRACK ABOUT 3.5 LONG ABOVE RIVET LINE. REPAIRED IAW FOKKER SRM 53-11-60, PAGE 3 FIGURE 2. 2 L 7 2 4F RT A20EU 1998061200075 19980612 00075 EU 1998 6 12 QXEA9800701 1 19980519 A 3222 STRUT FOKKER F28 F28MK4000 4990810 EU NLG REQD SERVICE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CHECK VALVE FOR NOSE LANDING GEAR STRUT SERVICING IS LEAKING. INSTALLED CHECK VALVE IAW HORIZON AIR EA 4-32-47. 2 L 7 2 4F RT A20EU 1998061200076 19980612 00076 EU 1998 6 12 QXEA9800702 1 19980511 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU BS 3820 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 FLOOR SUPPORT UNDER GALLEY IS CORRODED AND BENT AT STATION 3820 AFT END. REPAIRED IAW FOKKER SRM 53-02-14, FIGURE 1. 2 L 7 2 4F RT A20EU 1998061200077 19980612 00077 EU 1998 6 12 QXEA9800703 1 19980510 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU GALLEY BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 FLOOR SUPPORT UNDER NR 1 GALLEY IS BENT AND CORRODED AT AFT END. REPAIRED IAW FOKKER SRM 53-02-14, FIGURE 1. 2 L 7 2 4F RT A20EU 1998061200078 19980612 00078 EU 1998 6 12 QXEA9800704 1 19980430 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU BS 4900-3820 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BEAM FROM 4900 TO 3820 AT BL6004T. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 1 3. 2 L 7 2 4F RT A20EU 1998061200079 19980612 00079 EU 1998 6 12 QXEA9800705 1 19980429 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 3820 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CORROSION ON FLOOR SUPPORT BEAM FROM FORWARD OF INBOARD RIGHT SEAT TRACK TO FRAME 3820 ON UPPER SURFACE. REPAIRED IAW F OKKER SRM 51-31-01, PAGE 13. 2 L 7 2 4F RT A20EU 1998061200080 19980612 00080 EU 1998 6 12 QXEA9800706 1 19980430 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 3820-4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CORROSION ON FLOOR SUPPORT BEAM UPPER SURFACE FROM FRAME 4900 TO 3820 CENTERLINE BEAM. REPAIRED IAW FOKKER SRM 51-10-05 AND 51-21-01. 2 L 7 2 4F RT A20EU 1998061200081 19980612 00081 EU 1998 6 12 QXEA9800707 1 19980511 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU BS 4150 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 FLOOR SUPPORT BEAM IS DENTED JUST FORWARD OF FY.4150 AT BL600RT. REPAIRED IAW FOKKER SRM 53-02-14, FIGURE 1. 2 L 7 2 4F RT A20EU 1998061200082 19980612 00082 EU 1998 6 12 QXEA9800708 1 19980512 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU FRAME16060/16660 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CEILING WEB ATTACHMENT TO FRAMES 16060 AND 16660 IS BENT ABOVE CARGO DOOR OPENING. REPAIRED IAW HORIZON AIR EA 4-53-425 . 2 L 7 2 4F RT A20EU 1998061200083 19980612 00083 EU 1998 6 12 QXEA9800709 1 19980512 A 5230 DOUBLER FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 DOUBLER FOR INNER SKIN ON AFT CARGO DOOR IS CORRODED. REPAIRED IAW FOKKER SRM 52-30-00, FIGURE 4, ITEM 290. 2 L 7 2 4F RT A20EU 1998061200084 19980612 00084 EU 1998 6 12 QXEA9800710 1 19980507 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 SHARP DENT IN OUTER SKIN APPROXIMATELY 9 BELOW HANDLE ACCESS DOOR OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-01-01, FIGURE 7, PARAGRAPH 5 AND 2. 2 L 7 2 4F RT A20EU 1998061200085 19980612 00085 EU 1998 6 12 QXEA9800711 1 19980512 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 NUMEROUS SPOTS OF CORROSION ON INSIDE OF INNER DOOR SKIN OF AFT CARGO DOOR. REPAIRED IAW FOKKER SRM 52-30-00, FIGURE 4. 2 L 7 2 4F RT A20EU 1998061200086 19980612 00086 EU 1998 6 12 QXEA9800712 1 19980505 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CLIP CRACKED FRAME 4610 STRINGER 7. REPAIRED IAW FOKKER SRM 51-31-01, 53-02-13, PAGE 4, 51-10-05 AND 51-10-04. 2 L 7 2 4F RT A20EU 1998061200087 19980612 00087 WP 1998 6 12 ABXA9800480 1 19980602 A 5320 99115497 INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP E/E COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 942AX 47552 DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT STATION 180 TO 200 LONGERON 30. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 A ND 51-30-5. 2 L 7 2 4F A6WE 1998061200088 19980612 00088 WP 1998 6 12 ABXA9800481 1 19980602 A 5313 591140959 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 256/275 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 256 AND 275. REPAIRED LONGERON IAW DC9 SRM 53-00. 2 L 7 2 4F A6WE 1998061200089 19980612 00089 WP 1998 6 12 ABXA9800482 1 19980602 A 5320 99115234 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 256 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT STATION 256 AND LONGERON 17R. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51- 30-1. 2 L 7 2 4F A6WE 1998061200090 19980612 00090 WP 1998 6 12 ABXA9800483 1 19980602 A 5320 99581715 ANGLE DOUG DOUG DC9 DC941 302207N WP BS 218 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, FOUND INTERCOSTAL FORWARD SUPPORT ANGLE CRACKED AT STATION 218 AND BL 0.0. REPLACED ANGLE IAW DC9 SRM 5 1-10-2A AND DRAWING 9958171. 2 L 7 2 4F A6WE 1998061200091 19980612 00091 WP 1998 6 12 ABXA9800484 1 19980602 A 5320 99105035 WEB DOUG DOUG DC9 DC931 3022065 WP BS 945-965 CANNED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, FOUND CUSP WEB OIL CANNING AT STATION 945 TO 965, LEFT SIDE. REPAIRED CUSP WEB IAW ABX REA D953-23817-M R. 2 L 7 2 4F A6WE 1998061200092 19980612 00092 WP 1998 6 12 ABXA9800485 1 19980602 A 5400 99155559 ANGLE DOUG DOUG DC9 DC931 3022065 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, FOUND NR 1 ENGINE PYLON TRAILING EDGE INTERIOR ANGLE CRACKED AT AFT OUTBOARD CORNER. REPLACED ANGLE IAW DC9 SRM 51-30-2, 51-30-5 AND DACO DWG 9915555. 2 L 7 2 4F A6WE 1998061200093 19980612 00093 WP 1998 6 12 ABXA9800486 1 19980602 A 5313 59114279 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 DURING C-CHECK, FOUND LONGERON 17L CRACKED AT STATION 980 FRAME ATTACH POINT. REPLACED LONGERON IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998061200094 19980612 00094 WP 1998 6 12 ABXA9800487 1 19980601 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 905AX 47147 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1998061200095 19980612 00095 NM 1998 6 12 SCNA98052 1 19980601 A 3610 DUCT BOEING 727 727225 1384077 NM NR 3 STRUT LEAKING A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 282SC 22558 DURING CLIMBOUT, HAD A NUMBER THREE STRUT OVERHEAT LIGHT COME ON AND LEFT PACK WAS UNABLE TO KEEP PRESSURE. DIVERTED AI RCRAFT TO IAH. TIGHTENED LOOSE DUCT CLAMPS IN THE NUMBER THREE STRUT. RAN UP NUMBER THREE ENGINE TO POWER WITH NO MORE LEAKS DETECTED. GROUND CHECKED LEFT PACK OK. 2 L 7 3 4F A3WE 1998061200096 19980612 00096 SO 1998 6 12 SWIA971186 1 19980409 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 BUTT STRAP CENTER FORWARD OF LAVATORY HAS CORROSION. REMOVED AND REPLACED BUTT STRAP CENTER FORWARD OF LAVATORY IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200097 19980612 00097 SO 1998 6 12 SWIA971187 1 19980409 A 5315 BEAM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 CAPS FOR CROSSBEAMS FORWARD AND AFT OF LAVATORY HAVE CORROSION. REMOVED AND REPLACED T-SECTIONS ON FORWARD AND AFT OF L AVATORY CROSSBEAMS IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200098 19980612 00098 SO 1998 6 12 SWIA971188 1 19980409 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CARGO COMPT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 RIGHT BUTT STRAP IN AFT CARGO BAY AREA HAS CORROSION. REMOVED AND REPLACED AFT RIGHT BUTT STRAP IN CARGO AREA, IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200099 19980612 00099 SO 1998 6 12 SWIA971189 1 19980409 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CARGO COMPT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 AFT CENTER BUTT STRAP IN CARGO AREA HAS CORROSION. REMOVED AND REPLACED AFT CENTER BUTT STRAP IN CARGO AREA, IAW SRM 51 -40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200100 19980612 00100 SO 1998 6 12 SWIA971190 1 19980409 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 BUTT STRAP RIGHT SIDE FORWARD OF LAVATORY HAS CORROSION. REMOVED AND REPLACED RIGHT BUTT STRAP FORWARD OF LAVATORY IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200101 19980612 00101 SO 1998 6 12 SWIA971191 1 19980409 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 BUTT STRAP CENTER FORWARD OF LAVATORY HAS CORROSION. REMOVED AND REPLACED BUTT STRAP CENTER FORWARD OF LAVATORY IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200102 19980612 00102 SO 1998 6 12 SWIA971192 1 19980409 A 5320 BEAM EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 CAPS FOR CROSSBEAMS FORWARD AND AFT OF LAVATORY HAVE CORROSION. REMOVED AND REPLACED T-SECTIONS ON FORWARD AND AFT OF L AVATORY CROSSBEAMS IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200103 19980612 00103 SO 1998 6 12 SWIA971193 1 19980409 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CARGO COMPT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 RIGHT BUTT STRAP IN AFT CARGO BAY AREA HAS CORROSION. REMOVED AND REPLACED AFT RIGHT BUTT STRAP IN CARGO AREA, IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200104 19980612 00104 SO 1998 6 12 SWIA971194 1 19980409 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CARGO COMPT CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 293SW 120320 AFT CENTER BUTT STRAP IN CARGO AREA HAS CORROSION. REMOVED AND REPLACED AFT CENTER BUTT STRAP IN CARGO AREA, IAW SRM 51 -40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200105 19980612 00105 SO 1998 6 12 SWIA971195 1 19980509 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 294SW 120321 CORROSION ON BUTT STRAP JUST FORWARD OF CENTER MOST AFT STRAP. REMOVED AND REPLACED THE BUTT STRAP JUST FORWARD OF CENT ER MOST AFT STRAP, IAW MM 51-00-0. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200106 19980612 00106 SO 1998 6 12 SWIA971196 1 19980509 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FRAME 38-41 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 294SW 120321 CORROSION ON RIGHT BUTT STRAP BETWEEN FRAMES 38-41. REMOVED AND REPLACED THE RIGHT BUTT STRAP BETWEEN FRAMES 38 AND 41 IAW SRM 51-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200107 19980612 00107 SO 1998 6 12 SWIA971197 1 19980509 A 5311 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE FRAME 38 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 294SW 120321 CORROSION ON CROSS FRAME AT FRAME 38. REMOVED AND REPLACED CROSS FRAME AT FRAME 38, IAW SRM 51-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200108 19980612 00108 SO 1998 6 12 SWIA971198 1 19980509 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 294SW 120321 CORROSION IN LEFT AFT FLOOR LEVEL SEAT TRACK. REMOVED AND REPLACED THE LEFT AFT FLOOR LEVEL SEAT TRACK WITH NEW IAW MM 51-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200109 19980612 00109 SO 1998 6 12 SWIA971199 1 19980509 A 5320 SILL EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 220SW 120288 RIGHT SIDE FORWARD HAS CORROSION. INSTALLED RIGHT SIDE FORWARD WITH NEW SILL IAW SRM 51-40-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200110 19980612 00110 SO 1998 6 12 SWIA971200 1 19980509 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 220SW 120288 CORROSION ON SEAT TRACK NEAR LAV AREA. REPLACED SEAT TRACK AS REQUIRED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200111 19980612 00111 SO 1998 6 12 SWIA971201 1 19980509 A 5347 SEAT TRACK EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 220SW 120288 CORROSION ON SEAT TRACK NEAR GALLEY AREA. REMOVED CORRODED PORTION OF SEAT TRACK AND FABRICATED NEW LEFT SEAT TRACK NEA R GALLEY AREA. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200112 19980612 00112 SO 1998 6 12 SWIA971202 1 19980505 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 NUMEROUS AREAS OF CORROSION ON RIGHT AFT FLOOR BUTT STRAP, REPLACED STRAP. REPLACED RIGHT AFT BUTT STRAP SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200113 19980612 00113 SO 1998 6 12 SWIA971203 1 19980505 A 5311 FRAME EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 CORROSION PITTING ON CROSS FRAME JUST AFT OF RIGHT AFT SEAT TRACK. REPLACED CROSS FRAME UPPER MEMBER SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200114 19980612 00114 SO 1998 6 12 SWIA971204 1 19980505 A 5320 STRAP EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE CABIN CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 296SW 120325 NUMEROUS AREAS OF CORROSION IN AFT CENTER FLOOR BUTT STRAP. REPLACED AFT CENTER FLOOR BUTT STRAP IAW SRM 51-40-02. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200115 19980612 00115 EU 1998 6 12 MALA976138 1 19980529 A 3350 6104789 BATTERY SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 115XJ 340A115 DURING INSPECTION FOUR EMERGENCY LIGHTS INOP AT FORWARD EXIT. MAINTENANCE REPLACED FORWARD BATTERY PACK AT LOCATION 21L N. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998061200116 19980612 00116 EU 1998 6 12 MALA976139 1 19980529 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 415XJ 340B415 DURING INSPECTION ONE FORWARD EMERGENCY EXIT LIGHT INOP. MAINTENANCE RESECURED CANNON PLUG 463UP-P2. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998061200117 19980612 00117 1998 6 12 MALA976140 2 19980531 A 7260 CHIP LIGHT SAAB SF340 SF340A 7850100 EU LT ENGINE ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 79XJ 079 IN FLIGHT THE LEFT ENGINE OIL CHIP DETECT LIGHT ILLUMINATED. ALL ENGINE PARAMETERS NORMAL. AIRCRAFT RETURNED TO MSP. M AINTENANCE INSPECTED LEFT ENGINE CHIP DETECTOR IAW GE MM 72-00-00 AND FOUND ACCEPTABLE MATERIAL DETERMINED TO BE OPERATI NG DEBRIS. AIRCRAFT GOOD FOR CONTINUED SERVICE. 2 L 7 2 4T RT A52EU 1998061200118 19980612 00118 SO 1998 6 12 LR7A9824 1 19980603 A 3260 H1413 SWITCH LKHEED 188 188C 5262604 SO NLG MALFUNCTIONED A LR7A O OTHER N FALSE WARNING AP APPROACH 1 AL 03 289F 1110 LANDING PAKN UNSAFE GEAR INDICATION ON NOSE GEAR, RECYCLED GEAR HAD THREE GREEN LIGHTS, SAFE INDICATION. INSPECTED NOSE GEAR, NO DEFECTS NOTED, INSTALLED GEAR PIN, FERRIED A/C TO PANC, REPLACED NOSE GEAR DOWNLOCK SWITCH IAW L-188 WDM G-2. OPS CHECKS NORMAL. 2 L 7 4 4T 4A22 1998061200119 19980612 00119 NM 1998 6 12 AWXA9800133 1 19980521 A 5330 SKIN BOEING 737 737277 1384570 NM L2 DOORWAY CRACKED A AWXA K NONE O OTHER UK UNKNOWN 1 WP 28 183AW 22650 D-POSSIBLE CRACK REPORTED L2 LWR FWD CORNER OF LOWER HINGE CUTOUT OF SKIN, CONFIRMED BY EDDY CURRENT INSPECTION. C-REMO VED DAMAGE PORTION OF SKIN AND BONDED DOUBLER INSTALLED DOUBLER PER 53-30-03 FIG 34. 2 L 7 2 4F RT A16WE 1998061200120 19980612 00120 NM 1998 6 12 AWXA9800134 1 19980521 A 2913 106047013 PUMP BOEING 737 737277 1384570 NM NR 2 ENGINE FAILED A AWXA O OTHER J WARNING INDICATION CL CLIMB 1 WP 28 187AW 22654 NR 2 HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON AFTER GEAR RETRACTION ALSO LOST A SYSTEM HYDRAULIC FLUID CAUSING NR 1 A L OW PRESSURE LIGHT TO COME ON. REMOVED AND REPLACED E2 HYDRAULIC PUMP IAW R5M29001 AND REMOVED AND REPLACED NR 1 AND NR 2 PRESSURE FILTER, CASE DRAIN FILTER AND RETURN FILTERS NO METAL OBSERVED. REMOVED AND REPLACED E1 HYD EDP AS PRECAUTIO N. 2 L 7 2 4F RT A16WE 1998061200121 19980612 00121 1998 6 12 AWXA9800135 2 19980527 A 7200 ENGINE BOEING 737 7372A6 138448B NM NR 1 BIRD STRIKE A AWXA O OTHER C F.O.D. TO TAKEOFF 1 WP 28 145AW 20194 ON T/O AT APPROXIMATELY 120 KNOTS, HEARD A LOUD BANG ON LEFT OF A/C FOLLOWED BY SLIGHT YAW. AIRSPEED PAUSE AND BAD SMEL L. FOUND EVIDENCE OF BIRD INGESTION OF NR 1 ENG. C/W BIRD STRIKE INSPECTION PER AWM 382. A/C DETERMINED TO BE OK FOR SERVICE. 2 L 7 2 4F A16WE 1998061200122 19980612 00122 NM 1998 6 12 AWXA9800136 1 19980527 A 3350 321430 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 189AW 22656 EMERGENCY LIGHT ABOVE L-2 FELL OUT AND E-LIGHTS CAME ON. ALL LIGHTS WERE ON FOR APPROXIMATELY 1 HOUR. MAINTENANCE INST ALLED LIGHT ASSY AND A/C MX FERRIED TO PHX FOR BATTERIES. 2 L 7 2 4F RT A16WE 1998061200123 19980612 00123 NM 1998 6 12 AWXA9800137 1 19980528 A 2751 1061141 INDICATOR BOEING 737 73733A 1384673 NM TE FLAPS MALFUNCTIONED A AWXA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 28 169AW 23630 FLAPS DID NOT DEPLOY WITH PRIMARY CONTROL, ALTERNATE OK. REMOVED AND REPLACED FLAP POSITION INDICATOR PER 27-58-41, OPS GOOD ON GROUND AT THIS TIME. 2 L 7 2 4F RT A16WE 1998061200124 19980612 00124 WP 1998 6 12 CALA9800958 1 19980603 A 3240 BRACKET DOUG DC10 DC1030 3023501 WP LT MLG WW FAILED A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 87070 48292 THE LT MLG RED LIGHT REMAINED ILLUMINATED ON BOTH PANELS WITH GEAR UP AFTER TAKEOFF FROM EWR. A VISUAL CHECK THROUGH VI EWPORT INDICATED DOOR PARTIALLY OPEN. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE F OUND THE TORQUE LINK BRAKE HOSE SUPPORT BRACKET IN LT MLG WHEEL WELL FAILED. THE SUPPORT BRACKET WAS REPLACED. IN ADDI TION, THE NR 6 BRAKE HOSE AND LT MLG UPPER TORQUE LINK HOSE GUIDE ASSEMBLY WERE REPLACED DUE TO RESULTANT DAMAGE. A GEA R SWING WAS PERFORMED IAW MM 07-11-00, PAGE 201 AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1998061200125 19980612 00125 WP 1998 6 12 CALA9800959 1 19980603 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 218 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 CRACK IN Z-ANGLE AT LT FORWARD PIT BULKHEAD STA 218, LBL 17. THE CRACK WAS STOP DRILLED. REPAIR A NGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 10. 2 L 7 2 4F A6WE 1998061200126 19980612 00126 WP 1998 6 12 CALA9800960 1 19980603 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 695 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND TWO .0625 INCH CRACKS AT RIVETS IN LT FUSELAGE FORWARD NOSE SECTION EXTERIOR SKIN, STA 695. A REPAIR W AS FABRICATED AND INSTALLED IAW EA 5330-02413 AND DOUGLAS DRAWING SR09530239. 2 L 7 2 4F A6WE 1998061200127 19980612 00127 WP 1998 6 12 CALA9800961 1 19980603 A 5330 PANEL DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 3 CRACK IN FORWARD ADF SENSE ANTENNA PANEL. THE CRACKED AREA WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061200128 19980612 00128 WP 1998 6 12 CALA9800962 1 19980604 A 5720 ANGLE DOUG DC9 DC932 3022066 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 CRACK IN ANGLE OF LT WING FORWARD SIDE AT WING ROOT, WHERE FORWARD SPAR GOES INTO FUSELAGE. THE SE AL BRACKET AND ANGLE AT WING ROOT WERE REMOVED IAW SRM 51-30-3. AN ANGLE WAS FABRICATED IAW SRM 51-10-4. THE ANGLE AND SEAL BRACKET WERE INSTALLED IAW SRM 51-30-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998061200129 19980612 00129 WP 1998 6 12 CALA9800963 1 19980604 A 5320 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 CRACK IN AFT CARGO DOOR OVERHEAD PAN AT STA 929. THE CRACK WAS STOP DRILLED IAW SRM 53-01. A REPA IR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 53-01. 2 L 7 2 4F A6WE 1998061200130 19980612 00130 WP 1998 6 12 CALA9800964 1 19980604 A 5280 CHANNEL DOUG DC9 DC932 3022066 WP RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 CRACK IN Z-CHANNEL OF RT MLG DOOR FORWARD INNER CORNER. THE CRACKED AREA OF CHANNEL WAS CUT OUT IA W SRM 52-05, FIGURE 14. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 52-05, FIGURE 14. 2 L 7 2 4F A6WE 1998061200131 19980612 00131 WP 1998 6 12 CALA9800965 1 19980604 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 389 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD NR 36 HAD CORROSION AT FOUR SCREW HOLES ON END OF PANEL, STA 389. THE FLOORBOARD WAS REPAIR ED IAW SRM 53-01, FIGURE 1, SHEET 2, SRM 53-21-0, AND 51-30-2. 2 L 7 2 4F A6WE 1998061200132 19980612 00132 WP 1998 6 12 CALA9800966 1 19980604 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 756-832 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD NR 72 FORWARD LEADING EDGE AND AFT SCREW HOLES CRACKED AND WORN BETWEEN STA 756 AND 832. TW O EACH REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-21, FIGURE 4, 53-01, FIGURE 2, SHEET 3, 51-10-3, AND 51- 30-2. 2 L 7 2 4F A6WE 1998061200133 19980612 00133 NM 1998 6 12 CALA9800967 1 19980604 A 5230 DOOR BOEING 737 7373T0 1384582 NM BAGGAGE COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND A 1 CRACK AT FORWARD LOWER CORNER (JUST BELOW HOLD OPEN HOOK) OF FORWARD BAGGAGE BIN DOOR. THE DOOR WA S REPAIRED IAW ECRA 5234-01004. 2 L 7 2 4F RT A16WE 1998061200134 19980612 00134 WP 1998 6 12 CALA9800968 1 19980604 A 2560 A125A MEGAPHONE DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND TWO CABIN MEGAPHONES INOPERATIVE. BOTH MEGAPHONES WERE REPLACED AND CHECKED IAW MM 25-60-00. 2 L 7 3 4F A22WE 1998061200135 19980612 00135 NM 1998 6 12 CALA9800969 1 19980605 A 3350 20131A BATTERY PACK RADIANT BOEING 737 7373T0 1384582 NM BS 960/326 DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17316 23367 THE EMERGENCY LIGHTS AT OVERHEAD OF L-1, R-1, AND R-2 DOORS; THE SLIDE LIGHTS AT R-1, R-2, AND R-3 DOORS; AND LIGHTS AT PSU'S 3ABC, 5F, AND 25F ALL ILLUMINATED WHEN TESTED, BUT WENT OUT WITHIN APPROXIMATELY 10 SECONDS. CHARGING WAS NO HELP . THE BATTERY PACKS AT EACH OF THREE LOCATIONS (STA 960L, 960R, AND 326L) WERE REPLACED. NORMAL OPERATION OF THE LIGHT S WAS RESTORED. 2 L 7 2 4F RT A16WE 1998061200136 19980612 00136 NM 1998 6 12 9809446627 1 19980603 A 2751 INDICATOR BOEING 747 747251B 1384892 NM TE FLAPS MALFUNCTIONED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 627US 21709 DURING CLIMB, THE LEFT OUTBOARD TRAILING EDGE FLAPS DID NOT RETRACT BEYOND ONE DEGREE. AIRCRAFT RETURNED TO LAX AND LAN DED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE FAULT BUT REPLACED THE FLAP POSITION INDICATOR AS A PRECAUTIO N. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998061200137 19980612 00137 NE 1998 6 12 9809456603 2 19980603 A 7230 BOSS BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE BROKEN A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 603US 19780 662452 AFTER TAKEOFF, THE OIL QUANTITY INDICATION FOR THE NR 1 ENGINE WENT TO ZERO AND OIL PRESSURE DROPPED. THE ENGINE WAS SH UT DOWN PER COM AND THE AIRCRAFT RETURNED TO NRT. MAINTENANCE INSPECTED THE ENGINE AND FOUND A BROKEN DIFFUSER CASE BOS S. REPLACED THE NR 1 ENGINE. 2 L 7 4 4F 4 F A20WE E20EA 1998061200138 19980612 00138 WP 1998 6 12 9809469876 1 19980531 A 3230 59164605509 VALVE DOUG DC9 DC951 3022051 WP NLG INOPERATIVE A NWAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 01 785NC 49670 49670 48110 THE NOSE LANDING GEAR DID NOT EXTEND. THE FLIGHT CREW FOLLOWED COM PROCEDURES, MANUALLY EXTENDED THE NOSE LANDING GEAR, AND LANDED AT MEM WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL VALVE AND THE NOSE LANDING GEAR CYLI NDER. (CYLINDER NO HELP) OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998061200139 19980612 00139 NM 1998 6 12 UPS98226841 1 19980602 A 5330 65184201021 SKIN BOEING 727 72725C 138400H NM BS 305 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C CORROSION ON EXTERNAL SKIN BETWEEN STR 24L AND 26L BS 305. REMOVED AND REPLACED FUSELAGE SKIN PANEL BS 227 TO 360 IAW SRM 51-30-02, 51-20-1, 51-50-1, 51-50-4 BFGOODRICH ENGINEERING REPAIR 98-2513. 2 L 7 3 4F A3WE 1998061200140 19980612 00140 NM 1998 6 12 UPS98226842 1 19980521 A 5712 RIB BOEING 727 72725C 138400H NM WS 686 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C FLOURSCENT PEN INSPECTION EXHIBITS CRACKS IN WS 686 RIB LOWER FLANGE RADUIS AT STR 6 LOWER ATTACH HOLE (LEFT WING). REMOVED AND REPLACED CRACKED RIB AT LEFT WS 686 PER SRM 51-30-2 AND EO B727-5710-1325H. 2 L 7 3 4F A3WE 1998061200141 19980612 00141 NM 1998 6 12 UPS98226843 1 19980518 A 5343 ALN1BR2 FITTING BOEING 727 72725C 138400H NM NLG CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C CORROSION IN BEARING BORE OF LT NLG TRUNNION SUPPORT FITTING. BORE LT NLG TRUNNION FITTING BORE IAW S RM 53-40-1. 2 L 7 3 4F A3WE 1998061200142 19980612 00142 NM 1998 6 12 UPS98226844 1 19980601 A 5755 65C8067822 FITTING BOEING 727 72725C 138400H NM NR 6 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE:C NR 6 SPOILER SUPPORT HINGE FITTING CRACKED AT UPPER HORIZONTAL LUG AFT SIDE O/B SIDE. REMOVED NR 6 SU PPORT HINGE FITTING (SPOILER) IAW SRM 51-30-5, MM 57-42-75. 2 L 7 3 4F A3WE 1998061200143 19980612 00143 NM 1998 6 12 UPS98226846 1 19980601 A 5754 HINGE BOEING 727 7271A7C 13840X2 NM NR 4 LE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C, NR 4 K-FLAP OUTBRD HINGE LUG CORRODED AROUND UPPER AND LOWER FASTENER HOLES. REPLACED COMPLETE K-FLA P ASSY PER MM 27-81-01. 2 L 7 3 4F A3WE 1998061200144 19980612 00144 NM 1998 6 12 UPS98226847 1 19980519 A 5711 SPAR CHORD BOEING 727 7271A7C 13840X2 NM RT WING CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C R/W UPPER F/SPAR CHORD SHOW SIGNS OF CORROSION AT FSS 398.0, 497.0, 513.5, 521.5, 730.02, 737.0. REMO VE CORROSION FOUND OUT OF LIMITS AND REPLACE SPAR CHORD IAW 98-2421. 2 L 7 3 4F A3WE 1998061200145 19980612 00145 NM 1998 6 12 UPS98226848 1 19980521 A 5711 BAC15141926 SPAR BOEING 727 7271A7C 13840X2 NM WS 438/446 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C R/W FRONT SPAR LOWER CHORD IS CORRODED AT FSS 438 AND FS 446. REMOVED CORROSION OUT OF LIMITS AND REP AIRED IAW ER NR 98-2449. 2 L 7 3 4F A3WE 1998061200146 19980612 00146 NM 1998 6 12 UPS98226849 1 19980527 A 2761 FITTING BOEING 727 7271A7C 13840X2 NM NR 4 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C CORROSION (C57-581-03.00-01) ON NR 4 SPOILER ACTUATOR SUPPORT FITTING. REPLACED SUPPORT FITTING AND R EINSTALLED SPOILER AND ACTUATOR AND ASSOCIATED PARTS PER MM 27-61-01 AND 27-61-81. 2 L 7 3 4F A3WE 1998061200147 19980612 00147 NM 1998 6 12 UPS98226850 1 19980528 A 2761 FITTING BOEING 727 7271A7C 13840X2 NM NR 1 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C CORROSION (C57-581-03.00-01) ON NR 1 SPOILER ACTUATOR SUPPORT FITTING. REPLACED SUPPORT FITTING AND R EINSTALLED ASSOCIATED PARTS PER MM 27-61-01 AND 27-61-81. 2 L 7 3 4F A3WE 1998061200148 19980612 00148 NM 1998 6 12 UPS98226851 1 19980518 A 5320 65C8067870 CHANNEL BOEING 727 7271A7C 13840X2 NM BS 322-334 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE:C CORROSION (C53-224-06.00-01) AROUND NUT PLATES ON U-CHANNEL JUST OUTBOARD OF MOP SILL BETWEEN BS 322-3 34, WL 209, LBL 63. REMOVED AND REPLACED U-CHANNEL PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998061200149 19980612 00149 NM 1998 6 12 UPS98526839 1 19980604 A 2150 MS280341 TEMP BULB BOEING 757 75724APF 1384969 NM LT PACK MALFUNCTIONED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 SO 01 449UP 27738 BURNING SMELL IN COCKPIT WITH LEFT PACK OPERATING. SMELL GOES AWAY WITH RT PACK ONLY OPERATING. REMOVED AND REPLACED L EFT PRE-COOLER OUT TEMP BULB. OPERATED PACK WITH LEFT ENGINE NO SMELL NOTED. 2 L 7 2 4F RT A2NM 1998061200150 19980612 00150 WP 1998 6 12 UPS98826838 1 19980604 A 2150 3964202 CONTROL VALVE DOUG DC8 DC873F 302199F WP LT PACK FAILED A IPXA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 819UP 46019 CREW EVACUATED AIRCRAFT DUE TO SMOKE IN COCKPIT. CREW FOLLOWED EVACUATION CHECKLIST, FIRED ALL BOTTLES, SHUTDOWN ALL EN GINES AFTER AIRCRAFT WAS REPOSITIONED TO UPS RAMP, THEN MOVED A/C TO MERCURY CARGO RAMP. DETERMINED LEFT PACK WILL NOT SHUT OFF, SUSPECT FLOW CONTROL VALVE. REPLACED FLOW CONTROL VALVE AND WATER SEPARATOR BAG FOR LEFT PACK. OPS CK, LEFT PACK OPS CKS NORMAL. NO SMOKE OR FUMES NOTED IN COCKPIT. 2 L 7 4 4F RT 4A25 1998061200151 19980612 00151 EU 1998 6 12 QXEA9800777 1 19980602 A 3350 1312 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 BOI- EMERGENCY EVACUATION LIGHT ON RIGHT WING IS OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998061200152 19980612 00152 EU 1998 6 12 QXEA9800778 1 19980602 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 SEA - LIGHTS OUT IN EXIT SIGN. MAINTENANCE REPLACED EXIT SIGN CIRCUIT BOARD, OPERATIONAL TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998061200153 19980612 00153 EU 1998 6 12 QXEA9800779 1 19980603 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 PDX - FORWARD CABIN CEILING EXIT SIGN LIGHT DIM. MAINTENANCE REPLACED EXIT SIGN CIRCUIT BOARD, OPERATIONAL TESTS ARE NO RMAL. 2 L 7 2 4F RT A20EU 1998061200154 19980612 00154 NM 1998 6 12 98FDEA00391 1 19980601 A 5330 6516203 SKIN BOEING 727 72721C 138400M NM BS 870-867 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 STA-PAE: CORROSION (C57-174-01) LOWER CENTER TANK SKIN BS 870-867, WL 138, LBL 65 - RBL 65 FOUND WHILE WORKING NR 0734. *S/D* REMOVED CORROSION ON LOWER CENTER TANK SKIN BS 870-867, WL 138, LBL 65 - RBL 65 PER FED-EX EA 7-5730-35051. 2 L 7 3 4F A3WE 1998061200155 19980612 00155 NM 1998 6 12 98FDEA00392 1 19980604 A 5711 65162071 SPAR BOEING 727 72721C 138400M NM WS 277 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 STA-PAE - CRACK IN R/W T/E UPPER CHORD AT MAIN LANDING GEAR BEAM. BLENDED OUT CRACKED AREA AND INSTALLED REPAIR DOUBLER S IAW FED-EX EA 7-5710-35024. 2 L 7 3 4F A3WE 1998061200156 19980612 00156 NM 1998 6 12 98FDEA00393 1 19980604 A 5730 652163811 SKIN BOEING 727 72721C 138400M NM CENTER FUEL TANK CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 STA-PAE CORROSION (C57-174-01) ON UPPER CENTER TANK SKIN BS 870-867, WL 178, LBL 65 - RBL 65 FOUND WHILE WORKING NR 073 4. *S/D* REMOVED CORROSION ON UPPER CENTER TANK SKIN BS 870-867, WL 178, LBL 65 - RBL 65 PER FED-EX EA 7-5730-35051. 2 L 7 3 4F A3WE 1998061200157 19980612 00157 WP 1998 6 12 ABXA9800488 1 19980604 A 3260 DC26A1415S CONNECTOR DOUG DC8 DC863 302198A WP LT MLG WW BROKEN A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 AFTER TAKEOFF AND GEAR RETRACTION, GEAR UNSAFE LIGHT ILLUMINATED. AFTER GEAR RECYCLE AND 2 SUBSEQUENT UPLATCH CHECKS L IGHT WENT OUT. REPLACED CANNON PLUG P1-1387 IAW WIRING DIAGRAM 32-61-01. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998061200158 19980612 00158 NM 1998 6 12 DL76G981165 1 19980531 A 5220 STOP B767 BOEING 767 7673P6 1385105 NM LT EMER EXIT MISRIGGED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 154DL 25241 ON CLIMB-OUT THROUGH 15,000 FT, THE LEFT OVERWING EXIT LATCH OPENED SLIGHTLY. THE PRESSURE DIFF WAS 6 TO 8 PSID. FOUND DOOR STOPS OUT OF RIG. TWO (2) STOPS WERE NOT SAFTIED. RIGGED DOOR PER M/M AND INSTALLED SAFTIES, PRESSURIZED AIRCRAF T TO 8.5 PSID, NO LEAKS AND NO DOOR HANDLE MOVEMENT. 2 L 7 2 4F RT A1NM 1998061200159 19980612 00159 NM 1998 6 12 DL757981171 1 19980602 A 5350 FILLET D31393109 BOEING 757 757232 1384965 NM LT WING/FUS DAMAGED A DALA O OTHER D INFLIGHT SEPARATION CL CLIMB 1 SO 27 629DL 22919 INBOUND DAMAGE TO FUESLAGE FILLET PANELS AND LT WING INBOARD FLAP DUE TO OVERWING SLIDE DOOR OPENED AND SLIDE FELL OUT I NTO AIR STREAM. REPAIRED DAMAGE AND REPLACED SLIDE. 2 L 7 2 4F RT A2NM 1998061200160 19980612 00160 1998 6 12 DLL19981178 4 19980603 A 2211 7876027011 COMPUTER LKHEED 1011 10113853 5265020 WP E/E COMPT MALFUNCTIONED A DALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 27 759DA 193Y1176 AUTO SPOILERS DEPLOYED AT FL280. REPLACED FCES COMPUTER. 2 L 7 3 4F A23WE 1998061200161 19980612 00161 NM 1998 6 12 DLM88981179 1 19980530 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN EXPOSED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 907DE 53416 EMERG TRACK LIGHTING HAS EXPOSED WIRES AT LAST ROW OF FIRST CLASS. REPLACED EMERGENCY TRACK LIGHT BULB AND LENS ASSY. 2 L 7 2 4F RT A6WE 1998061200162 19980612 00162 NM 1998 6 12 DL72K981180 1 19980603 A 3350 10617844 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 479DA 20756 LEFT OVERWING EMERGENCY EXIT LIGHTS FAIL TO ILLUMINATE ON STANDBY POWER. REPLACED BATERRY PACK SLED AND RELAMPED EMERGE NCY EXIT SIGNS OVERWING EMERG EXIT, CKS NML PER MM. 2 L 7 3 4F A3WE 1998061200163 19980612 00163 WP 1998 6 12 DLL19981181 1 19980530 A 5330 1608987103 SKIN LKHEED 1011 10113853 5265020 WP FS 639 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 761DA 193Y1208 FUSELAGE SKIN, FS 639, STRG 32, REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN AT FS 639 AND STRG 32R WAS FOUND CORRODE D. THE CORROSION WAS REMOVED BY MAKING A 8.2 BY 5.8 CUTOUT IN THE SKIN. A SECTION OF STRINGER 32 WAS ALSO CUTOUT DUE T O CORROSION. THE SKIN CUTOUT WAS REPAIRED WITH AN INTERNAL TITANIUM DOUBLER. THE STRINGER WAS REPAIRED PER THE L1011 S RM. THE REPAIR WAS DOCUMENTED PER ER/A 364916-14, REV A. 2 L 7 3 4F A23WE 1998061200164 19980612 00164 NM 1998 6 12 DL76L981182 1 19980602 A 5754 114T410115A WEDGE BOEING 767 767332 1382001 NM NR 1 LE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 180DN 25985 WING, LEADING EDGE SLAT NR 1 TE WEDGE. REPAIR FOR DISBONDING SKIN. THE TRAILING EDGE WEDGE ON THE NR 1 SLAT WAS FOUND WITH A 6 AREA OF DELAMINATION ON THE UPPER AND LOWER SKINS. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B767 SRM 57-43-02, FIGURE 201. THE REPAIR WAS DOCUMENTED PER ER/A 364939-14AD. 2 L 7 2 4F RT A1NM 1998061200165 19980612 00165 NM 1998 6 12 DL72S981183 1 19980603 A 2782 54093031 ACTUACTOR BOEING 727 727232 1384082 NM NR 3 LE FLAP LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 403DA 5983DEFG 21147 IN CRUISE FLIGHT LEVEL 310 A SYSTEM QTY RAPIDLY DECREASED TO ZERO FOLLOWED BY A SYSTEM PRESSURE DECREASING TO ZERO. WHI LE RUNNING POM OUTBOARD FLAPS FAILED TO ALT EXTEND. REPLACED NR 3 LED FLAP ACUTATOR. REPLACED NR 1 AND NR 2 HYD CASE D RAIN FILTERS. LEAK CHECK OK. RAN ENGINE OPERATION OF PUMPS AND FLAPS NORMAL. CLEANED CANNON PLUG ON OUTBOARD ALT FLAP BYPASS VALVE. OPERATION OF ALT FLAPS OPERATION NORMAL. 2 L 7 3 4F A3WE 1998061200166 19980612 00166 NM 1998 6 12 DL72L981184 1 19980603 A 2761 CASTING BOEING 727 727232 1384082 NM NR 4 SPOILER CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 0/B ACTUATOR ATTACH CASTING BROKEN AT LOWER MOUNT BOLT NR 4 SPOILER. REPLACED CASTING PER M/M 57-42-0. 2 L 7 3 4F A3WE 1998061200167 19980612 00167 NM 1998 6 12 DL72L981185 1 19980603 A 5320 WEB BOEING 727 727232 1384082 NM BS 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 .1875 IN CRACK ON VERTICAL WEB LIGHTNING HOLE STA 1228 LT SIDE. ROUTE CRACK PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998061200168 19980612 00168 NM 1998 6 12 DL72L981186 1 19980603 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 5 IN LENGTH DELAMINATION ON RT ELEVATOR TRAILING EDGE I/B END. REPAIR PER M/M 55-20-0. 2 L 7 3 4F A3WE 1998061200169 19980612 00169 NM 1998 6 12 DL72L981187 1 19980603 A 2782 MOUNT BOEING 727 727232 1384082 NM NR 1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 NR 1 LE FLAP ACTUATOR MOUNT CRACKED UPPER O/B CORNER. REPAIR PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998061200170 19980612 00170 NM 1998 6 12 DL72S981188 1 19980601 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1110 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 CORROSION FOUND ON STA 1110 FLOORBEAM O/B OF RT SEAT TRACK. REPAIRED PER SRM 53-20-11 PG 811B. 2 L 7 3 4F A3WE 1998061200171 19980612 00171 NM 1998 6 12 DL76S981189 1 19980604 A 3350 BATTERY 61020 BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 116DL 23275 JUST PRIOR TO DEPARTURE F/A ADVISE MTC, THE MID RT EMERGENCY FLASH LIGHT HAD LOW BATTERIES. MAINTENANCE REPLACED THE BA TTERY AND BULB ASSY AND INSTALLED PLACARD, P/N257204896 BULB P/N 012211663. 2 L 7 2 4F RT A1NM 1998061200172 19980612 00172 NM 1998 6 12 DL72W981190 1 19980604 A 5522 SKIN BOEING 727 727247 138408F NM RT ELEVATOR SEPARATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 T/E RT ELEVATOR SEPARATING SEVERAL SMALL AREAS. REPAIR PER M/M 55-20-0. 2 L 7 3 4F A3WE 1998061200173 19980612 00173 NM 1998 6 12 DL72W981191 1 19980604 A 5320 WEB BOEING 727 727247 138408F NM BS 1239 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 WEB CRACKED AT FASTENER STA 1239 RT SIDE AFT AIRSTAIR AREA REPAIR PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998061200174 19980612 00174 NM 1998 6 12 DL73E981192 1 19980604 A 3350 BATTERY 61020 BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 374DL 23521 DURING SVC CK, NR 3 FOUND F/C EMER FLASH LIGHT RED LED DOES NOT FLASH. REPLACED BATT PER M/M LIGHT NOW OPS TEST OK PER M/M. 2 L 7 2 4F A16WE 1998061200175 19980612 00175 1998 6 12 SCNA98053 4 19980604 A 2565 5WD260100211 SLIDE DOUG DC10 DC1010 3022110 WP R4 DOOR FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 571SC 768 46645 DURING DEPLOYMENT OF THE R4 DOOR SLIDE FOR TRAINING PURPOSES THE SLIDE FAILED TO INFLATE FULLY. 2 L 7 3 4F A22WE 1998061200176 19980612 00176 1998 6 12 SCNA98054 4 19980604 A 2565 5WD260100111 SLIDE DOUG DC10 DC1010 3022110 WP R4 DOOR FAILED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 572SC 609 46977 DURING DEPLOYMENT OF THE R4 DOOR SLIDE FOR TRAINING PURPOSES THE SLIDE FAILED TO INFLATE FULLY. 2 L 7 3 4F A22WE 1998061200177 19980612 00177 NM 1998 6 12 K3HA980081 1 19980605 A 3350 30718P1GPL LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 ONE RED EMERGENCY PATH LIGHT OUT AT SEAT AREA 18/19. RELAMPED PER MM 33-59-00, OPS CHECK OK. 2 L 7 3 4F A3WE 1998061200178 19980612 00178 GL 1998 6 12 LR7A9825 2 19980605 A 7261 6821270 OIL PUMP LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 4 ENGINE FAILED A LR7A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 401LC 1001 4606 750581 NR 4 ENGINE LOW AND DECREASING OIL QUANTITY. PRECAUTIONARY SHUTDOWN. REPLACED TURBINE REAR SCAVANGE OIL PUMP PER 72-2- 3 201-204. SERVICED OIL TANK, RUNUP AND LEAK CHECK NORMAL PER 72-2-3 204-205. 2 H 7 4 4T 4 T A1SO E282 1998061200179 19980612 00179 NM 1998 6 12 M8XA9800010 1 19980603 A 2750 1050A000003 FLAP CONTROL DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE E/E COMPT MALFUNCTIONED A M8XA A UNSCHED LANDING A FLAME/FIRE TO TAKEOFF 1 NM 03 331MX 3074 SHORTLY AFTER TAKE-OFF, THE FLIGHT CREW REPORTED A FLAP CONTROL FAULT AND ASYMMETRY WARNING MESSAGE. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. ON-CALL MAINTENANCE CONTRACTOR RESET THE FLAP CONTROL UNIT IAW AMM JI C 27-50-00-810-001-AAO, CONDUCTED AN OPERATIONAL CHECK IAW AMM 27-50-00 WITH SATISACTORY RESULTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998061200180 19980612 00180 EU 1998 6 12 AWXA9800139 1 19980601 A 5347 SEAT TRACK AIRBUS 320 A320231 3930325 EU FRAME 20-23 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 632AW 81 RT I/B SEAT TRACK CORRODED NUMEROUS SPOTS FROM FR 20 TO 64. CORROSION REMOVED AS PER SRM 53-00-15, TREATED, PRIMED SEAT TRACK FROM FR 20 TO 23. NEW SECTION SPLICED AS PER SRM 53-00-15 FIG 201. 2 L 7 2 4F RT A28NM 1998061200181 19980612 00181 NM 1998 6 12 AWXA9800144 1 19980606 A 5313 STRINGER BOEING 737 7372U9 1384498 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 149AW 22575 AIRCRAFT FUSELAGE CRACK, RT SIDE AT STRINGER 18 STA 727 JUST AFT OF WEB FAIRING. INSTALLED BLIND FASTENERS IAW SRM 53-3 0-03 FIG 1, PLACE ON MONITOR. 2 L 7 2 4F RT A16WE 1998061200182 19980612 00182 1998 6 12 COMA9810131 2 19980604 A 7532 97962641 BLEED VALVE EMB 120 EMB120RT SO RIGHT MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 261CA 20609 4371 120254 RIGHT HAND BLEED AIR OVERHEAT WARNING DURING FLIGHT. REPLACED THE HIGH PRESSURE BLEED VALVE. 2 L 7 2 4T RT A31SO 1998061200183 19980612 00183 SO 1998 6 12 COMA9810132 1 19980604 A 7540 1173T0303 SWITCH EMB 120 EMB120RT SO RIGHT MALFUNCTION A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 261CA 120254 RIGHT HAND BLEED AIR OVERHEAT WARNING DURING FLIGHT. REPLACED THE BLEED AIR OVERHEAT SWITCH. 2 L 7 2 4T RT A31SO 1998061200184 19980612 00184 SO 1998 6 12 COMA9810133 1 19980604 A 3520 11820404 SOLENOID EMB 120 EMB120RT SO CABIN INOPERATIVE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 261CA 120254 DURING 1C INSPECTION TASK 35-09, THE ROW 4 OXYGEN DOOR LATCH MECHANISM FAILED TO OPEN THE DOOR AND RELEASE THE OXYGEN MA SKS. REPLACED THE SOLENOID FOR ROW 4 OXYGEN DOOR. 2 L 7 2 4T RT A31SO 1998061200185 19980612 00185 NM 1998 6 12 SWAA980969 1 19980528 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS AT BS 178 BULKHEAD WEB WL 197.3 TO 201.9, LBL 4.7. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200186 19980612 00186 NM 1998 6 12 SWAA980970 1 19980528 A 5320 WEB BOEING 737 7372H4 138448C NM BS 250.3 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 053SW 21534 DURING SERVICE CHECK, FOUND 3.5 VERTICAL CRACK IN LT NOSE WHEEL WELL AT BS 258.3, 12 BELOW CEILING. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1998061200187 19980612 00187 1998 6 12 SWAA980971 4 19980528 A 2565 SLIDE BOEING 737 7375H4 138449D NM SERV DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 501SW 24178 DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR ESCAPE SLIDE ACCIDENTALLY DEPLOYED AFTER ENGINES/SHUT DOWN. REPAIRED P ER BOEING MM. 2 L 7 2 4F RT A16WE 1998061200188 19980612 00188 NM 1998 6 12 SWAA980972 1 19980528 A 5320 INTERCOSTAL BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INSIDE INTERCOSTAL AT BS 178 LBL 26, WL 195 FWD END. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F A16WE 1998061200189 19980612 00189 NM 1998 6 12 SWAA980973 1 19980528 A 5320 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND LT FUSELAGE TO VERTICAL STAB SKATE ANGLE IS WORN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200190 19980612 00190 NM 1998 6 12 SWAA980974 1 19980528 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED A1 CHECK, FOUND FWD SECTION EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY PACK AS REQUIRED PER BOEING MM, TEST NORMAL. 2 L 7 2 4F RT A16WE 1998061200191 19980612 00191 NM 1998 6 12 SWAA980975 1 19980528 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 954 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CRACKED FWD SIDE OF FWD DOOR FRAME AFT SERVICE DOOR CUTOUT AT BS 954, RBL 55, WL 265. REMOV ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200192 19980612 00192 NM 1998 6 12 SWAA980976 1 19980528 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 827.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CRACKED INTERCOSTAL UPPER FWD CORNER AT BS 827.5 RBL 5.5 WL 158. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998061200193 19980612 00193 NM 1998 6 12 SWAA980977 1 19980528 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 879 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 879, LBL 2.5, WL 166. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200194 19980612 00194 NM 1998 6 12 SWAA980978 1 19980528 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUT PLATE AT BS 794, LBL 2.5 WL 158. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998061200195 19980612 00195 NM 1998 6 12 SWAA980979 1 19980528 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 352 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CRACKED WEB AT BS 352, RBL 1, WL 135. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200196 19980612 00196 NM 1998 6 12 SWAA980980 1 19980528 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 325 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND CORRODED UPPER CHORD AT BS 325, LBL 9 TO 14, WL 155. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200197 19980612 00197 NM 1998 6 12 SWAA980981 1 19980528 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 432 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND DENTED SKIN AT BS 432, RBL 45, WL 164. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200198 19980612 00198 NM 1998 6 12 SWAA980982 1 19980528 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 877 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND DENTED SKIN AT BS 877 TO 907, STR 14 LEFT WL 230. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200199 19980612 00199 NM 1998 6 12 SWAA980983 1 19980528 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 359 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING SERVICE CHECK, FOUND INTERCOSTAL SUPPORT ANGLE HAS ELONGATED FASTENER HOLES AT BS 359, BL 0, WL 149 TO 154. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200200 19980612 00200 NM 1998 6 12 SWAA980984 1 19980528 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 658SW 23332 DURING SERVICE CHECK, FOUND FLOORBEAM AT BS 947, LBL 4, WL 208 HAS FLOORBOARD FASTENER HOLE DRILLED INTO SPLICE REPAIR F ASTENER. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200201 19980612 00201 NM 1998 6 12 SWAA980985 1 19980528 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 1146 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 1146, RBL 18. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200202 19980612 00202 NM 1998 6 12 SWAA980986 1 19980528 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 178, WL 207, RBL 25 TO 29 AND LBL 25 TO 29. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200203 19980612 00203 NM 1998 6 12 SWAA980987 1 19980528 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 294, WL 252, LBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200204 19980612 00204 NM 1998 6 12 SWAA980988 1 19980528 A 5512 SKIN BOEING 737 7373T5 NM LT HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 692SW 23062 DURING SCHEDULED BC 3 CHECK, FOUND LT HORIZ STAB HAS A DENT 4 FT FROM FUSELAGE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200205 19980612 00205 NE 1998 6 12 SWAA980989 2 19980531 A 7230 COMPRESSOR BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE STALLED A A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 73SW 22673 AIR RETURN AT 2200 MSL ON CLIMB, A CHILDS BALLOON WENT THROUGH NR 2 ENGINE. A MODERATE COMPRESSOR STALL, SMELL IN CABIN , LOSS OF .2 EPR. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MDW, ENGINE IND NORMAL ON FINAL. VISUALLY INSPECTED INLET AN D EXHAUST AREAS, REMOVED DEBRIS FROM INLET AREA AND CSD OIL COOLER. RAN ENGINE PER BOEING MM, OPS CHECK NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1998061200206 19980612 00206 NM 1998 6 12 SWAA980990 1 19980529 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 291.5 BELOW STRINGER 12R. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200207 19980612 00207 NM 1998 6 12 SWAA980991 1 19980529 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL ATTACH ANGLE AT BS 291.5 ABOVE STRINGER 12 RT. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200208 19980612 00208 NM 1998 6 12 SWAA980992 1 19980529 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND DAMAGED WEB AT BS 500 TO 500A, RBL 6.5, WL 147. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200209 19980612 00209 NM 1998 6 12 SWAA980993 1 19980529 A 5320 WEB BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND INNER FWD WEB CRACKED NEAR CENTER STOP FITTING. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200210 19980612 00210 NM 1998 6 12 SWAA980994 1 19980529 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 1015-1030 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED STRAP AT BS 1015 TO 1030, LBL 3 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200211 19980612 00211 NM 1998 6 12 SWAA980995 1 19980529 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED VERTICAL STIFFENER AT BS 328 FLOORBEAM (FWD SIDE), RBL 35, WL 20. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200212 19980612 00212 NM 1998 6 12 SWAA980996 1 19980529 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, LBL 10 TO 12, RBL 10 TO 12, LBL 21. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998061200213 19980612 00213 NM 1998 6 12 SWAA980997 1 19980529 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 315 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 315, RBL 60, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200214 19980612 00214 NM 1998 6 12 SWAA980998 1 19980529 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 189 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED TRAN CHECK, FOUND DENTED FUSELAGE SKIN AT BS 189, BL 0, LOWER LOBE. REPAIR PER TRAMCO EO NR 98-0356. 2 L 7 2 4F RT A16WE 1998061200215 19980612 00215 NM 1998 6 12 SWAA980999 1 19980529 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 380 STR 1, AND STR 2 RT. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998061200216 19980612 00216 NM 1998 6 12 SWAA981000 1 19980529 A 5320 DOUBLER BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND DAMAGED SKIN DOUBLER OF FUSELAGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200217 19980612 00217 NM 1998 6 12 SWAA981001 1 19980529 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT DOOR STOP FITTING NR 9 AT BS 348, LBL 65, WL 223. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998061200218 19980612 00218 NM 1998 6 12 SWAA981002 1 19980529 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 295, WL 215, LBL 58 AND BS 295, WL 244, LBL 55. REMOVED A ND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200219 19980612 00219 NM 1998 6 12 SWAA981003 1 19980529 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 301.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 301.9 WL 257.5, LT 54. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200220 19980612 00220 NM 1998 6 12 SWAA981004 1 19980529 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 987-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 987 TO 1016, RBL 39 TO 46, WL 208. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998061200221 19980612 00221 NM 1998 6 12 SWAA981005 1 19980529 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 1028 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND GOUGED WEB AT BS 1028, RBL 2, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200222 19980612 00222 NM 1998 6 12 SWAA981006 1 19980529 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 1007 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 1007, STR 16 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200223 19980612 00223 NM 1998 6 12 SWAA981007 1 19980529 A 5720 ANGLE BOEING 737 7372H4 138448C NM WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE ON TOP WING PANEL I/B OF NR 5 GROUND. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F A16WE 1998061200224 19980612 00224 NM 1998 6 12 SWAA981008 1 19980530 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 480 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND HOLE BURNED IN SKIN FROM LIGHTNING STRIKE AT BS 480, BELOW STR 4L. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1998061200225 19980612 00225 NM 1998 6 12 SWAA981009 1 19980530 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 310 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED TRAN CHECK, FOUND DENTED FUSELAGE EXTERIOR SKIN AT BS 310, STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200226 19980612 00226 NM 1998 6 12 SWAA981019 1 19980530 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 806 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED TRAN CHECK, FOUND DENT BELOW AFT CARGO DOOR AT BS 806, STR 26 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200227 19980612 00227 NM 1998 6 12 SWAA981010 1 19980530 A 5312 BULKHEAD BOEING 737 7373G7 1384595 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND DENTED BULKHEAD PANEL SUPPORT ANGLE AT BS 727+3 RBL 53 WL 191. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200228 19980612 00228 NM 1998 6 12 SWAA981011 1 19980530 A 5320 BEAM BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED CREASE BEAM AT BS 178, RBL 29, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200229 19980612 00229 NM 1998 6 12 SWAA981012 1 19980530 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 787-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB TIE STRAP AT BS 787 TO 847, RBL 19, WL 157 TO 162. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200230 19980612 00230 NM 1998 6 12 SWAA981013 1 19980530 A 5320 STRAP BOEING 737 7373G7 1384595 NM BS 840-852 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED LOWER VERTICAL TIE STRAP AT BS 840 TO 852, RBL 19, WL 161. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200231 19980612 00231 NM 1998 6 12 SWAA981014 1 19980530 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, RBL 3, WL 159. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998061200232 19980612 00232 NM 1998 6 12 SWAA981015 1 19980530 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, RBL 8, WL 159. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998061200233 19980612 00233 NM 1998 6 12 SWAA981016 1 19980530 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 12.5, WL 159 LBL 8, WL 159 AND LBL 3 WL 1 59. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200234 19980612 00234 NM 1998 6 12 SWAA981017 1 19980530 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 794-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT BS 794 TO 847, RBL 19, WL 164. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200235 19980612 00235 NM 1998 6 12 SWAA981018 1 19980530 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 787-794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 787 TO 794, RBL 23, WL 158. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200236 19980612 00236 NM 1998 6 12 SWAA981020 1 19980530 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 767 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 767, RBL 29, WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200237 19980612 00237 NM 1998 6 12 SWAA981021 1 19980530 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 767-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB AT 767 TO 787, RBL 19, WL 156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200238 19980612 00238 NM 1998 6 12 SWAA981022 1 19980530 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 400-420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 400 TO 420, LBL 25 WL 156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200239 19980612 00239 NM 1998 6 12 SWAA981023 1 19980530 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGER 9RT AND 8RT AT BS 887. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200240 19980612 00240 NM 1998 6 12 SWAA981024 1 19980530 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED LOWER STUB FRAME AT BS 295, WL 209, RBL 55. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200241 19980612 00241 NM 1998 6 12 SWAA981025 1 19980530 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 277, WL 231, RBL 54. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200242 19980612 00242 NM 1998 6 12 SWAA981026 1 19980530 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 328, RBL 66, WL 210. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200243 19980612 00243 NM 1998 6 12 SWAA981027 1 19980530 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 339 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED THRESHOLD Z-ANGLE SUPPORT AT BS 339 TO 317, LBL 63.5 TO LBL 60, WL 209. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200244 19980612 00244 NM 1998 6 12 SWAA981028 1 19980530 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 268 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 268, LBL 10, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200245 19980612 00245 NM 1998 6 12 SWAA981029 1 19980530 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED Z-ANGLE CHORD AT BS 270, LBL 9, 6, 3, 5, BL 0, RBL 10, 6, 3, 5, WL 207. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200246 19980612 00246 NM 1998 6 12 SWAA981030 1 19980530 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 270 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE STIFFENER AT BS 270 LBL 47, WL 208. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998061200247 19980612 00247 NM 1998 6 12 SWAA981031 1 19980530 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 274 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 274, RBL 53, WL 247. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200248 19980612 00248 NM 1998 6 12 SWAA981032 1 19980530 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 1010 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 1010 2 BELOW STRINGER 5 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200249 19980612 00249 NM 1998 6 12 SWAA981033 1 19980530 A 5320 COVER BOEING 737 7373G7 1384595 NM BS 492-496 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND DOOR FRAME COVER PLATE DENTED AND GOUGED AT BS 492 TO 496, RBL 25 TO 30, WL 156 TO 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200250 19980612 00250 NM 1998 6 12 SWAA981034 1 19980530 A 5330 SKIN BOEING 737 7373H4 1384600 NM NR 1 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED C2 CHECK, FOUND CRACKED BOTTOM SKIN OF NR 1 SLAT IN ACTUATOR AREA. REPAIRED PER BOEING NR T1-A57-015. 2 L 7 2 4F RT A16WE 1998061200251 19980612 00251 NM 1998 6 12 SWAA981035 1 19980530 A 2910 LINE BOEING 737 7373H4 1384600 NM B-HYD SYST LEAKING A SWAA K NONE O OTHER DE DESCENT 1 SW 07 332SW 23696 DURING FLIGHT LOST ALL B-SYSTEM HYDRAULIC FLUID. A/C MADE AN UNEVENTFUL LANDING. FOUND PRESS LINE LEAKING AT B-ELECT P UMP REPLACED LINE, LEAK CK'D PER BOEING MM. REPLACED B-CASE DRAIN AND B-SYSTEM RETURN FILTERS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998061200252 19980612 00252 NM 1998 6 12 SWAA981036 1 19980601 A 3350 LIGHT BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING WALKAROUND CHECK, FLOOR EGRESS LIGHTS HAVE ONE RED LENS MISSING AT CEILING EXIT AND TWO WHITE LIGHTS INOP AT NO A DJACENT LOCATIONS. INSTALLED LENS AND REPAIRED LIGHT PER BOEING MM, OPS CHK NORMAL. 2 L 7 2 4F RT A16WE 1998061200253 19980612 00253 NM 1998 6 12 SWAA981037 1 19980602 A 3020 ANTI-ICE VALVE BOEING 737 7372H4 138448C NM NR 2 ENGINE LOOSE A SWAA C E ABORTED TAKEOFF ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 07 054SW 21535 AIR TURNBACK, A/C ON DEPARTURE PASSING 7000 FT NR 2 ENG. SHUTDOWN IN FLIGHT DUE TO FIRE WARNING CAME ON. ACCOMPLISHED ORH ITEMS AND WARNING LIGHT EXTINGUISHED WHEN NR 2 FIRE SWITCH WAS PULLED. EXTINGUISHER BOTTLE WAS NOT DISCHARGED. A/ C MADE AN UNEVENTFUL LANDING IN SJC. NR 2 ENGINE COWL ANTI-ICE LINE LEAKING. VALVE IN CLOSED POSITION PER SP NR 30. O K TO CONTINUE PER MEL. REMOVED AND REPLACED NR 2 ENG COWL ANTI-ICE DUCT PER BOEING MM. 2 L 7 2 4F A16WE 1998061200254 19980612 00254 NM 1998 6 12 SWAA981038 1 19980601 A 5320 FRAME BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FWD UPPER DOOR FRAME AT AFT SERV DOOR ABOVE UPPER HINGE. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1998061200255 19980612 00255 NM 1998 6 12 SWAA981039 1 19980601 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 270 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED C4 CHECK, FOUND CRACKED LOWER HINGE CUTOUT ON FUSELAGE SKIN AT BS 270 ABOVE STR 14R. REPAIRED PER BOE ING SRM AND TYPICAL REPAIR T1-253-013. 2 L 7 2 4F A16WE 1998061200256 19980612 00256 NM 1998 6 12 SWAA981042 1 19980601 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C 2 CHECK, FOUND CRACKED AFT CARGO DOOR UPLATCH INTERCOSTAL. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200257 19980612 00257 NM 1998 6 12 SWAA981043 1 19980601 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 375 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN HAS IMPROPER REPAIR AT BS 375 BELOW STR 15 LT. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1998061200258 19980612 00258 NM 1998 6 12 SWAA981044 1 19980601 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 910 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED SKIN AT BS 910, BELOW STR 21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200259 19980612 00259 NM 1998 6 12 SWAA981045 1 19980601 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 947 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND GOUGED SKIN AT BS 947 BELOW STR 21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200260 19980612 00260 NM 1998 6 12 SWAA981046 1 19980601 A 5320 THRESHOLD BOEING 737 7372T4 1384492 NM FWD CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FWD CARGO DOOR THRESHOLD AT FWD END. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200261 19980612 00261 NM 1998 6 12 SWAA981047 1 19980601 A 5350 WEB BOEING 737 7372T4 1384492 NM NR 3 LE SLAT WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB FOR SLIPPER FAIRING I/B OF NR 3 SLAT WORN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200262 19980612 00262 NM 1998 6 12 SWAA981048 1 19980601 A 5720 ANGLE BOEING 737 7372T4 1384492 NM WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND T-ANGLE WORN I/B UPPER FLAP WELL PANEL. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200263 19980612 00263 NM 1998 6 12 SWAA981049 1 19980601 A 5330 SKIN BOEING 737 7372T4 1384492 NM NR 5 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED SKIN AT NR 5 SLAT TRACK O/B AUX. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200264 19980612 00264 NM 1998 6 12 SWAA981050 1 19980601 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED C1 CHECK, FOUND CRACKED INTERCOSTAL FOR DOOR UPLATCH HOOK. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200265 19980612 00265 NM 1998 6 12 SWAA981051 1 19980601 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED A2 CHECK, FOUND CRACKED 2 AT BS 767 STR 22. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200266 19980612 00266 NM 1998 6 12 SWAA981052 1 19980602 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 950 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED C2 CHECK, FOUND CRACKED FUSELAGE SKIN AT FASTENER AT BS 950 ABOVE STR 21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200267 19980612 00267 NM 1998 6 12 SWAA981053 1 19980602 A 5330 SKIN BOEING 737 7372H4 138448C NM L1 DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED BC CHECK, FOUND SHEET METAL REPAIR TO AFT ENTRY DOOR AREA L1 DOOR RIG. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200268 19980612 00268 NM 1998 6 12 SWAA981054 1 19980602 A 2560 SLIDE BOEING 737 7375H4 138449D NM EMER EXIT DOOR OUT OF CASE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING WALKAROUND CHECK, FOUND LEFT FWD EMERGENCY SLIDE CAME OUT OF CONTAINER WHEN DOOR WAS SHUT FOR PUSH BACK. REINSTA LLED SLIDE IN HARD CASE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998061200269 19980612 00269 NM 1998 6 12 SWAA981055 1 19980602 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FWD GALLEY DOOR ENTRY Z-ANGLE STRAP AT BS 294, RBL 55. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200270 19980612 00270 NM 1998 6 12 SWAA981056 1 19980602 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 530 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED RT RAM AIR DUCT SUPPORT WEB ANGLE AT BS 530. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998061200271 19980612 00271 NM 1998 6 12 SWAA981057 1 19980602 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 530 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED RT RAM AIR DUCT SUPPORT LOWER Z-ANGLE AND HAS A HOLE AT BS 530. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061200272 19980612 00272 NM 1998 6 12 SWAA981058 1 19980602 A 3397 WIRE BOEING 737 7373A4 1384585 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680SW 23505 DURING SCHEDULED BC1 CHECK, FOUND CABIN EMERGENCY TRACK LIGHT PULLED OUT AND MISSING CLEAR LENS AT SEAT ROW 3 DEF, AND A LSO WIRING PULLED OUT OF TRACK AT SEAT ROW 11 DEF. REINSTALLED TRACK LIGHT AND REPLACED CLEAR LENS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998061200273 19980612 00273 NM 1998 6 12 SWAA981059 1 19980603 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 944 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 051SW 21448 DURING SCHEDULED C3 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 944 STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061200274 19980612 00274 NM 1998 6 12 SWAA981060 1 19980602 A 3350 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680SW 22505 DURING SCHEDULED BC1 CHECK, FOUND CABIN EMERGENCY TRACK LIGHT RED LIGHT OUT AT EMERGENCY OVERWING EXIT. REPAIRED PER B OEING MM. 2 L 7 2 4F RT A16WE 1998061200275 19980612 00275 NM 1998 6 12 SWAA981061 1 19980603 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 784 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 784 STR 24L. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998061200276 19980612 00276 NM 1998 6 12 UPS98426857 1 19980606 A 3350 BULB BOEING 747 747121 1384871 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 683UP 20353 INSPECTION TYPE N/A, EEL IN CREW ENTRY DOOR AND MAIN CARGO DOOR INOP. RELAMPED SAME AS REQUIRED, OPS CHECK NORMAL. 2 L 7 4 4F A20WE 1998061200277 19980612 00277 WP 1998 6 12 UPS98826854 1 19980605 A 3350 CIRCUIT BREAKER DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 836UP 45936 INSPECTION TYPE N/A, EMERGENCY EXIT LIGHTS ARE ON CONTINUOUSLY IN THE ARM POSITION AND WILL NOT DISARM CHECK. REMOVED A ND REPLACED EEL CIRCUT BREAKER REF 20-50-00, OPS CHECK GOOD W/REF TO MM 33-50-01. 2 L 7 4 4F RT 4A25 1998061200278 19980612 00278 WP 1998 6 12 UPS98826855 1 19980606 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE N/A, EMERG EXIT LIGHTS INOP. REMOVED AND REPLACED EMERG LIGHT BATT PACK (P/N 5708458-503) ON, (P/N 60-1 223-5) OFF, (S/N 588) ON, (S/N 219) OFF. 2 L 7 4 4F RT 4A25 1998061200279 19980612 00279 WP 1998 6 12 UPS98826856 1 19980605 A 3350 5708458503 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE N/A, EEL WILL NOT STAY ON. REMOVED AND REPLACED EMERG BATT PACK, OPS CHECK GOOD (P/N 5708458-503) ON, ( S/N 2054) ON. 2 L 7 4 4F RT 4A25 1998061200280 19980612 00280 NM 1998 6 12 DL75A981194 1 19980604 A 3350 BULB 767 BOEING 757 757212 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 752AT 23128 EXTERIOR EMERGENCY LIGHT FOR L2 DOOR INOP. RELAMPED SAME, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998061200281 19980612 00281 WP 1998 6 12 DLL19981196 1 19980604 A 5730 SKIN 1529104189 LKHEED 1011 10113853 5265020 WP LT WING CRACKED A A DALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 SO 27 753DA H0198 193W1189 ON DESCENT SPEEDBRAKES WERE USED. WHEN SPEEDBRAKES WERE STOWED THE LT SPOILERS DID NOT RETRACT. AIRCRAFT DID SEVERE RO LL TO LT, TOOK ALMOST FULL CONTROL WHEEL TO RT TO HOLD WINGS LEVEL. WHEN FLAPS WERE EXTENDED THE SPOILERS STOWED. DID NOT USE AUTO SPOILERS FOR LANDING BUT WHEN EXTENDED MANUALLY THE SPOILERS EXTENDED EVENLY. FOUND NR 4 SPOILER LT WI NG CRACKED AT O/B SIDE OF ACTUATOR FITTING. REPLACED PANEL AND ADJUSTED PER MM 27-61-17. 2 L 7 3 4F A23WE 1998061200282 19980612 00282 NM 1998 6 12 DLM88981199 1 19980605 A 3350 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DL 49540 ON LAYOVER, AFT EMERGENCY LIGHTS DID NOT TEST FROM COCKPIT OR TEST FROM TEST SWITCH ON AFT POWER SUPPLY. REPLACED AFT P OWER SUPPLY AND BATTERY PACK, SYSTEM OP NORMAL. 2 L 7 2 4F RT A6WE 1998061200283 19980612 00283 NM 1998 6 12 DL72S981200 1 19980605 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 A .5 INCH CRACK NR 2 L/E FLAP ACT ATTACH BRACKET, LOWER FWD END. FOUND ON D1 LTR CHECK. INSTALLED DOUBLER PER M/M 57-2 0-21. 2 L 7 3 4F A3WE 1998061200284 19980612 00284 NM 1998 6 12 DL72S981202 1 19980606 A 3350 900542 RACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 21145 OVERWING EXIT EMERG LIGHTS FAILED TO ILLUMINATE. REPLACED RACK. 2 L 7 3 4F A3WE 1998061200285 19980612 00285 NM 1998 6 12 DL757981203 1 19980607 A 3297 WIRE 4346741033 BOEING 757 757232 1384965 NM COCKPIT FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 602DL NONE 22809 STRONG SMELL/FUMES LIKE ELECTRIC INSULATION BURNING DETECTED DURING APPROACH IN COCKPIT AND BY FLT ATTENDANT IN FWD GALL EY. REPLACED NOSE GEAR GREEN LIGHT IN COCKPIT AND REPAIRED ASSOCIATED WIRING. 2 L 7 2 4F RT A2NM 1998061200286 19980612 00286 NM 1998 6 12 DL72S981204 1 19980607 A 3350 POWER SUPPLY 900542 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 534DA VA6227 22047 DURING LAYOVER INSP, FOUND LEFT FWD OVERWING EMERG LIGHTS INOP. REPLACED ASSOCIATED POWER SUPPLY BASE-DAL (P/N 33470174 4), (S/N VA-6227). 2 L 7 3 4F A3WE 1998061200287 19980612 00287 NM 1998 6 12 DL72W981205 1 19980607 A 3350 POWER SUPPLY 900835A BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 295 22110 FOUND ON LAYOVER INSP, AIRSTAIR DOOR EXIT LIGHT FLICKERING. REPLACED ASSOCIATED POWER SUPPLY. 2 L 7 3 4F A3WE 1998061200288 19980612 00288 NM 1998 6 12 DHL98740002 1 19980606 A 2611 SMOKE DETECTOR BOEING 727 7272Q9 138448M NM CABIN MALFUNCTIONED A DHLA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 740DH 21930 MAIN CABIN SMOKE WARNING ILLUMINATED IN DESCENT THROUGH FL 200. WARNING LIGHT EXTINGUISHED ON TAXI, NO SMOKE NOTED. RE LAMPED SMOKE DETECTOR BEACON LAMPS , 6 EACH, OPS CHECKED NORMAL ON GROUND. LAMPS REPLACED AS PRECAUTION. 2 L 7 3 4F RT A3WE 1998061200290 19980612 00290 1998 6 12 SWIA971206 4 19980501 A 3425 AHF EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE E/E COMPT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 294SW 120321 CAPTAINS AND FIRST OFFICERS HEADING INDICATORS DIFFER BY 15 DEGREES. RETURNED TO SLC. REPLACED AHF 85 PREVIOUSLY C/W. 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200291 19980612 00291 WP 1998 6 12 CKSA98339 1 19980512 A 5330 SKIN DOUG DC8 DC861 3021952 WP BS 1200 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING ROUTINE B-CHECK INSPECTION, FOUND RT SIDE FS 1200 SKIN ABOVE NLG STRUT DOOR CRACKED. REMOVED DOOR AND ACCESS PAN EL AS REQUIRED. REMOVED DAMAGED AREA IAW DC8 SRM 53-02-01. REPAIRED DAMAGED AREA IAW DC8 SRM 53-02-01. INSTALLED ACCE SS PANEL AND DOOR IAW DC8 MM 21-54-2. CLASS II REPAIR INSTALLED INITIAL REINSPECTION DUE IN 12000 CYCLES REINSPECT THER EAFTER DUE EVERY 4000 CYCLED. REPAIR MUST BE REPLACED WITHIN 24000 CYCLES IAW DC8 SRM 53-2-1 PARAGRAPH 16. NON-ROUTINE TASK CARD NUMBER 23645. 2 L 7 4 4F 4A25 1998061200292 19980612 00292 WP 1998 6 12 CKSA98340 1 19980512 A 5347 SEAT TRACK DOUG DC8 DC861 3021952 WP CABIN DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 812CK 45890 DURING ROUTINE B-CHECK INSPECTION, FOUND COMP NR 18 SIDE WALL RESTRAINT PULLED OUT OF SEAT TRACK, DAMAGED SEAT TRACK. R EMOVED FLOOR PANEL TO FOM. REMOVED DAMAGED SECTION OF SEAT TRACK. REPLACED DAMAGED SEAT TRACK IAW DC8 SRM 51-3-0. INS TALLED FLOOR PANEL IAW DC8 SRM 51-3-0. NON-ROUTINE TASK CARD NUMBER 22596. 2 L 7 4 4F 4A25 1998061200293 19980612 00293 WP 1998 6 12 CKSA98341 1 19980513 A 5347 SEAT TRACK DOUG DC8 DC863F 302198F WP BS 380 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 815CK 46151 FOUND TWO SECTIONS OF SEAT TRACK DAMAGED AT STA 380 ON NR 1 AND NR 2 TRACKS AFTER REMOVAL OF CARGO. REPAIRED DAMAGED AR EAS OF SEAT TRACK IAW DOUGLAS DC-8 SRM CH 53-2-3. NON-ROUTINE M-7 ITEM 1 LOG PAGE 815-0860. 2 L 7 4 4F 4A25 1998061200294 19980612 00294 1998 6 12 GLBA98059 4 19980415 A 6113 SPINNER EMB 120 EMB120ER 3260203 SO HAMSTD 14RF 14RF9 NE RT PROPELLER LOOSE A GLBA K NONE D INFLIGHT SEPARATION CR CRUISE 1 CE 01 299UX 120299 950402 UPON ARRIVAL IN FSD, CREW NOTICED SCREWS LOOSE AND MISSING FROM RT SPINNER. AFTER FURTHER INVESTIGATION, NOTICED THAT 3 PROP BLADES WERE ALSO DAMAGED. REMOVED AND REPLACED PROPELLER BLADES NR 1 AND NR 3, AND REBALANCED PROP. OPS CHECK AN D LEAK CHECK GOOD. 2 L 7 2 4T RT A31SO 6 C P11NE 1998061200295 19980612 00295 SO 1998 6 12 98ZZZX2059 1 19980121 A 2497 WIRE PIPER PA31 PA31350 7103110 SO RT ALT FIELD BROKEN A A E2XA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 07 6657Y 317405176 REPORT PER 135H15 (A)(16) PILOT REPORTS RT ALTERNATOR FAILED EN ROUTE PHX. ELECTRICAL SYSTEM APPEARED TO BE OPERATING O FF BATTERY ONLY. PILOT CONFIRMED TO ATC HE WAS DECLARING AN EMERGENCY AS COMMUNCIATONS BECAME WEAK. PRELIMINARY INSPEC TION REVEALS NO OBVIOUS DEFECTS. DETAILED INSP IN PROGRESS TO DETERMINE CAUSE OF SYSTEM FAILURE. FINDINGS WILL BE PROV IDED IAW 135.415 (H) AS SOON AS AVAILABLE. SD: RT ALTERNATOR FIELD WIRE BROKE AT THE ALTERNOR 2 TERMINAL CONNECTION. THIS IS NOT UNCOMMON BECAUSE THE ALTERNATOR IS FWD MOUNTED WITH ALL OF ITS WIRING IN EXTREME AIRFLOW. LT ALTERNATOR CO ULD NOT PICK UP THE LOAD DUE TO THE CONSTANT OPEN IN THE C/P SWITCH. ACFT OPERATED ON BATTERY UNTIL RETURNING TO PHX. 1 L 7 2 3O A20SO 1998061200297 19980612 00297 NM 1998 6 12 TWAA9807001 1 19980502 A 3350 1N68 INVERTER BOEING 767 7673Q8 NM GALLEY FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 JFK - DURING OVERNIGHT MAINTENANCE CHECK FOUND FORWARD GALLEY EGRESS LIGHTS INOPERATIVE. REPLACED FORWARD GALLEY EGRESS LIGHT INVERTER. (X) 2 L 7 2 4F RT A1NM 1998061200298 19980612 00298 EU 1998 6 12 98ZZZX2061 1 19980212 A 5720 S5241053900000 NUT PLATE FLANGE AEROSP ATR72 ATR72212 EU RT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT WING PANEL 622CT NUT PLATE FLANGE CORRODED. REPLACED PANEL 622 CT NUT PLATE COLLAR IAW ATR72 JIC 57-00-00 OAC 100000-001. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200299 19980612 00299 EU 1998 6 12 98ZZZX2062 1 19980212 A 5320 S5367800826900 FLOOR CHANNEL AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR SILL PLATE FLOOR CHANNEL CORRODED. INSTALLED NEW FLO OR CHANNEL IAW ATR72 SRM 53-61-01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200300 19980612 00300 EU 1998 6 12 98ZZZX2063 1 19980212 A 5320 S5367800121002 DRAIN TRACK AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR SILL DRAIN TRACK CORRODED. INSTALLED NEW DRAIN TRACK IAW ATR72 SRM 53-61-00. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998061200302 19980612 00302 EU 1998 6 12 98ZZZX2065 1 19980212 A 2810 S5241055200200 PANEL AEROSP ATR72 ATR72212 EU LT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LT WING FUEL PANEL 522CT CORRODED BYEOND LIMITS. INSTALLED NEW PA NEL IAW JIC 57-00-00 OAC 100000-001. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200303 19980612 00303 EU 1998 6 12 98ZZZX2066 1 19980212 A 5720 S5241053900000 NUT PLATE FLANGE AEROSP ATR72 ATR72212 EU LT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LT WING FUEL ACCESS PANEL 522CT NUT PLATE FLANGE CORRODED BEYOND L IMITS. INSTALLED NEW FLANGE IAW ATR72 JIC 57-00-00 OAC 100000-001. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200304 19980612 00304 EU 1998 6 12 98ZZZX2067 1 19980210 A 5230 S5237651922251 HINGE AEROSP ATR72 ATR72212 EU CARGO DOOR CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FORWARD CARGO DOOR 'PIANO' HINGE CRACKED AND DENTED ON 2 LUGS. MA INTENANCE REPLACED THE 'PIANO' HINGE IAW ATR72 SRM 51-25-03. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200305 19980612 00305 EU 1998 6 12 98ZZZX2068 1 19980211 A 5320 S5367125720402 INTERCOSTAL AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT INTERCOSTAL AT STR 17 CORRODED BYEOND LIMITS. INSTALLED NEW IN TERCOSTAL AT STR 17 IAW ATR72 SRM 53-61-01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200306 19980612 00306 EU 1998 6 12 98ZZZX2069 1 19980211 A 5210 S5367122100001 BRACKET AEROSP ATR72 ATR72212 EU PASSENGER DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED PASSENGER DOOR HANDRAIL SUPPORT CORRODED. INSTALLED NEW SUPPORT I AW ATR72 SRM 53-67-20 FIG 5. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200307 19980612 00307 EU 1998 6 12 98ZZZX2070 1 19980212 A 5210 S5367120921402 PLATE AEROSP ATR72 ATR72212 EU PASSENGER DOOR CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED PASSENGER DOOR FOLDING STEP STRIKER PLATE CORRODED. REPLACED STRI KER PLATE AS REQUIRED IAW JIC STANDARD PRACTICE CHAPTER 20. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200308 19980612 00308 EU 1998 6 12 98ZZZX2071 1 19980212 A 5730 S5241055200200 PANEL AEROSP ATR72 ATR72212 EU RT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RT WING PANEL 622CT CORRODED BEYOND LIMITS. INSTALLED NEW PANEL 6 22CT IAW ATR72 JIC 57-00-00 OAC 10000-001. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998061200309 19980612 00309 NM 1998 6 12 F3LA98010 1 19980407 A 5311 FRAME BOEING 737 737201 1384454 NM BS 7472 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 207AU 3307 19423 DURING C-CHECK, MAINTENANCE REPORTED FRAME CRACKED AT STA 7472, STR 9L. MAINTENANCE FABRICATED AND INSTALLED REPAIR PAR TS PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1998061200311 19980612 00311 NM 1998 6 12 98ZZZX2073 1 19980223 A 5720 ANGLE DHAV DHC8 DHC8103 1386005 NM WING SPAR CRACKED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 803WP 141 DURING SCHEDULED INSPECTION, (DISBONDING) CRACKS WERE DETECTED AT THE LEFT AFT CLOSING ANGLE VERTICAL FLANGE 2ND AND 3R D FASTENERS FROM OTBD EDGE. THE CRACKS THAT WERE AROUND THE FASTENERS WERE DETECTED DURING A THOROUGH EDDY CURRENT AND FLUORESCENT LIQUID PENETRANT INSPECTION. AN APPROVED REPAIR DRAWING WAS OBTAINED FROM THE AIRCRAFT MANUFACTURER (RD 8-5 3-2878/8-53-3381) PROCEDURES TO ALLOW THE AIRCRAFT TO RETURN TO SERVICE WITH A REPEAT INSPECTION TO BE ACCOMPLISHED AT E VERY C-CHECK INSPECTION (400 HRS), WITH A PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 40,000 FLIGHTS. 2 H 7 2 4T RT A13NM 1998061200312 19980612 00312 NM 1998 6 12 ORJA9874 1 19980414 A 2430 CIRCUIT BREAKER DOUG MD90 MD9030 3023690 NM LT DC PWR UNIT TRIPPED A ORJA D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 WP 11 905RA 53573 RETURN TO GATE FOR LEFT GENERATOR OFF AND LIGHT A/C POWER FAULT ANNUNCIATED. PULLED AND RESET CIRCUIT BREAKERS ON DC PO WER ISOLATION UNIT. ENGINE RUN AND LEFT GENERATOR CAME ON-LINE AND OPS CHECK. (X) 2 L 7 2 4F RT A6WE 1998061200313 19980612 00313 1998 6 12 98ZZZX2074 4 19980207 A 2565 D31516109 SLIDE AIRBUS 320 A320214 EU R1 DOOR DEPLOYED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 GBXKD 735 ON PRE-FLIGHT FLIGHT 1322 IN CUN, R-1 DOOR SLIDE INADVERTENTLY DEPLOYED ON THE GROUND. REMOVED AND REPLACED R-1 DOOR SL IDE ASSEMBLY. 2 L 7 2 4F RT A28NM 1998061200314 19980612 00314 EU 1998 6 12 SIMA981041 1 19980414 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 0553 533 ORD - FLT 4076 - EMERGENCY LIGHT ABOVE REAR JUMP SEAT IS INOPERATIVE AND FLOOR STRIP LIGHTING IN REAR OF AIRCRAFT HAS 2 BULBS INOPERATIVE. REPLACED EMERGENCY LIGHT SYSTEM POWER SUPPLIES 61WL, 62WL, 73WL, AND 93WL. PERFORMED OPERATIONAL TE ST OF THE SYSTEM AND ALL LIGHTS OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX2075, 98Z ZZX2076, AND 98ZZZX2077. (X) 2 H 7 2 4T RT A53EU 1998061200315 19980612 00315 EU 1998 6 12 98ZZZX2075 1 19980414 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 0555 533 ORD - FLT 4076 - EMERGENCY LIGHT ABOVE REAR JUMP SEAT IS INOPERATIVE AND FLOOR STRIP LIGHTING IN REAR OF AIRCRAFT HAS 2 BULBS INOPERATIVE. REPLACED EMERGENCY LIGHT SYSTEM POWER SUPPLIES 61WL, 62WL, 73WL, AND 93WL. PERFORMED OPERATIONAL TE ST OF THE SYSTEM AND ALL LIGHTS OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL SIMA98104-1, 98ZZZ X2076, AND 98ZZZX2077. (X) 2 H 7 2 4T RT A53EU 1998061200316 19980612 00316 EU 1998 6 12 98ZZZX2076 1 19980414 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 0564 533 ORD - FLT 4076 - EMERGENCY LIGHT ABOVE REAR JUMP SEAT IS INOPERATIVE AND FLOOR STRIP LIGHTING IN REAR OF AIRCRAFT HAS 2 BULBS INOPERATIVE. REPLACED EMERGENCY LIGHT SYSTEM POWER SUPPLIES 61WL, 62WL, 73WL, AND 93WL. PERFORMED OPERATIONAL TE ST OF THE SYSTEM AND ALL LIGHTS OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL SIMA98104-1, 98ZZZ X2075, AND 98ZZZX2077. (X) 2 H 7 2 4T RT A53EU 1998061200317 19980612 00317 EU 1998 6 12 98ZZZX2077 1 19980414 A 3350 3013017 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 0647 533 ORD - FLT 4076 - EMERGENCY LIGHT ABOVE REAR JUMP SEAT IS INOPERATIVE AND FLOOR STRIP LIGHTING IN REAR OF AIRCRAFT HAS 2 BULBS INOPERATIVE. REPLACED EMERGENCY LIGHT SYSTEM POWER SUPPLIES 61WL, 62WL, 73WL, AND 93WL. PERFORMED OPERATIONAL TE ST OF THE SYSTEM AND ALL LIGHTS OPERATED NORMALLY. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL SIMA98104-1, 98ZZZ X2075, AND 98ZZZX2076. (X) 2 H 7 2 4T RT A53EU 1998061200318 19980612 00318 EU 1998 6 12 SABA980025 1 19980409 A 7603 SCREW BAG JETSTM JETSTM3201 1500217 EU POWER LEVER BACKED OUT A SABA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 33 965AE 965 CLT/OAJ - FLT 5151 - WHILE AT CRUISE ALTITUDE, THE LEFT EGT AND TORQUE STARTED TO FLUCTUATE. THIS WAS WITH SRL ON OR OF F. AIRCREW MADE A PRECAUTIONARY ENGINE SHUTDOWN. NO IN-FLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED AT OAJ WITH NO OTHER PROBLEMS. MAINTENANCE FROM CLT DEPLOYED TO OAJ. MAINTENANCE PERFORMED TTL, SRL, AND DELTA P/P ENGINE POWER RUNS. MAINTENANCE FOUND THE POWER LEVER, LOWER FLIGHT IDLE COVER ATTACHMENT SCREW HAD BACKED OUT AND WAS INTERFERRING WITH T HE RIGHT POWER LEVER. RE-TORQUED SCREW, PERFORMED ENGINE RUN SHEET. ENGINE CHECKED GOOD. NO REPEATS AS OF TODAY. (X) 2 L 7 2 4T RT A56EU 1998061200319 19980612 00319 NM 1998 6 12 98ZZZX2078 1 19980418 A 2520 771921 BRACKET BOEING 747 7472F6B 1384807 NM CABIN BROKEN A TWRA K NONE E VIBRATION/BUFFET CR CRUISE 1 EA 15 623FF 22382 ORY/JFK - FLT 37 - FLIGHT EXPERIENCED TURBULENCE. ON ACOMPLISHMENT OF CONDITIONAL INSPECTION, FOUND SEAT BELTS ATTACH P OINT BROKEN AT 55 D & E. REPLACED SAFETY BELTS BRACKET ASSY. OK FOR SERVICE. (X) 2 L 7 4 4F A20WE 1998061200320 19980612 00320 NM 1998 6 12 TSAA9833227 1 19980422 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 2 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACKS DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAF T RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061200321 19980612 00321 NM 1998 6 12 TSAA9833207 1 19980409 A 3350 1000679 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED EXIT IDENTIFICATION LIGHT ASSY FOR AFT SERVICE DOOR DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURN ED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061200322 19980612 00322 NM 1998 6 12 TSAA9833226 1 19980422 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 4 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACKS DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAF T RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061200323 19980612 00323 NM 1998 6 12 TSAA9833225 1 19980422 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 5 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACKS DUE TO BEING INOPERABLE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061200324 19980612 00324 SW 1998 6 12 98ZZZX2079 1 19980510 A 6510 406040340101 DISC PACK 407040325101 BELL 407 407 SW AFT SHORT SHAFT CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 547AL RNFS8042 53240 DURING DAILY INSPECTION, NR 3 DISC PACK P/N 406-040-340-101 FOUND CRACKED - LOCATED FORWARD END OF AFT SHORT SHAFT P/N 4 07-040-325-101. NUMBER OF DISCS IN PACK, 10 EACH. NR 10 DISC WAS CRACKED. CRACK WAS LOCATED IN CENTER OF 2 BOLT HOLES . 1 G 7 1 3U O H2SW 1998061200325 19980612 00325 EU 1998 6 12 98ZZZX2080 1 19980515 A 7714 430106202 PICKUP BOLKMS 117 BK117B1 5626012 EU ENGINE NG FAILED A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 170MC 7217 NG PICKUP INOPERATIVE. REPLACED NG PICKUP. 1 G 7 2 3U H13EU 1998061200328 19980612 00328 NM 1998 6 12 98ZZZX2083 1 19980511 A 6710 600N85203 POTENTIOMETER DOUG 600N 600N 3027377 NM COLLECTIVE WRONG PART A QKLA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 19 605AS 163 A212756 RN003 P/N 600N8520-3 WAS INSTALLED ON THE COLLECTIVE. IT IS INCORRECTLY LISTED IN THE IPC. P/N 600N8540-1 IS THE CORRECT POT ENTIOMETER FOR THE COLLECTIVE. THIS PART IS LISTED AS THE T/R POT IN THE IPC. P/N 600N8520-3 WAS REMOVED AND REPLACED BY P/N 600N8540-1. REMOVED POT. DESTROYED LOCALLY PER MDHS INSTRUCTIONS. 1 G 7 1 3U NC H3WE 1998061200329 19980612 00329 NM 1998 6 12 98ZZZX2084 1 19980508 A 2435 6854424 SHAFT SEAL DOUG 600N 600N 3027377 NM START/GENERATOR LEAK A QKLA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 605AS RN003 SEAL STARTED LEAKING. REPLACED WITH NEW SEAL. 1 G 7 1 3U NC H3WE 1998061200335 19980612 00335 GL 1998 6 12 98ZZZX2090 2 19980430 A 7322 2543398 BELLOWS BENDIX 23059933 SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 1 ENG FCU FAILED A ALGA O OTHER Y ENGINE STOPPAGE CR CRUISE 1 SW 03 5427S 1289 760168 CAE890417S DURING CRUISE FLIGHT, NR 1 ENGINE FAILED. RUN-ON LANDING CONDUCTED AT ABBEVILLE AIRPORT, NO DAMAGE OR INJURIES. 1 G 7 2 3U 3 U H1NE E1GL 1998061200336 19980612 00336 GL 1998 6 12 98ZZZX2091 2 19980420 A 7320 23064695 FADEC CHNDLREVANS DOUG 600N 600N 3027377 NM ALLSN 250C 250C47B GL ENGINE MALFUNCTIONED A QKLA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 19 605AS 106 JG7ALW0034 RN003 EIGHT PERCENT DROOP OCCURRED WHEN GOING FROM RIGHT PEDAL TO LEFT PEDAL IN-FLIGHT. REPLACED WITH ZERO TIME FADEC ASSY. ( ECU) SUPPLIED BY CHANDLER EVANS. DEFECTIVE UNIT RETURNED TO MANUFACTURER. 1 G 7 1 3U 3 U NC H3WE E1GL 1998061200355 19980612 00355 1998 6 12 98ZZZX2110 4 19980423 A 2312 064105430 TRANSCEIVER BOLKMS 105 BO105S 5626006 EU NR 2 VHF FAILED A HEEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 911HM 23600 S683 ON 4-23-98 (HOUMA) WHILE IN CRUISE FLIGHT, PILOT HEARD SEVERAL LOUD 'POPS' FROM NR 2 VHF RADIO AND BEGAN TO PRODUCE THIC K BLACK SMOKE. HE PULLED THE VHF 2 CIRCUIT BREAKER AND VENTILATED THE CABIN. CONTINUED WITH FLIGHT. MAINTENANCE REPLA CED VHF RADIO. 1 G 7 2 3U H3EU 1998061200382 19980612 00382 WP 1998 6 12 VJ9800180 1 19980529 A 5330 591140311 SKIN DOUG DC9 DC932 3022066 WP FWD FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 REMOVED AND REPLACED LT UPPER CROWN SKIN NOSE SECTION IAW DC9 SRM 5103902. ORDERED, FIT, TRIMMED, LOCATED AND DRILLED N EW SKIN IAW DC9 SRM 51-10-4. INSTALLED NEW SKIN LT UPPER NOSE IAW DC9 SRM 51-30-2, 51-30-5 AND EO 9-53-003. 2 L 7 2 4F A6WE 1998061200383 19980612 00383 WP 1998 6 12 VJ9800181 1 19980530 A 5330 1A3339801 SKIN DOUG DC9 DC932 3022066 WP FWD FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 REMOVE AND REPLACE RT UPPER NOSE CROWN SKIN NOSE SECTION. FABRICATED, DRILLED, COUNTERSUNK AND INSTALLED NEW NOSE SKIN IAW EO 9-53-003. 2 L 7 2 4F A6WE 1998061200384 19980612 00384 WP 1998 6 12 VJ9800182 1 19980530 A 5330 59114009004 SKIN DOUG DC9 DC932 3022066 WP FWD FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 REPLACED LOWER RT NOSE CROWN SKIN. CUT OUT DENTED SECTION, ORDERED NEW SECTION, FABRICATED INTERNAL DOUBLER AND FINGER DOUBLER IAW EO 9-53-003. DRILLED, COUNTERSUNK AND INSTALLED SKIN IAW EO 9-53-003. 2 L 7 2 4F A6WE 1998061200385 19980612 00385 WP 1998 6 12 VJ9800183 1 19980530 A 5330 IA345341 SKIN DOUG DC9 DC932 3022066 WP FWD FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 CUT OUT DENTED SECTION OF LT CENTER NOSE SKIN. FABRICATED NEW SKIN SECTION, INTERNAL DOUBLER AND FINGER DOUBLER AND INS TALLED IAW EO 9-53-003. 2 L 7 2 4F A6WE 1998061200386 19980612 00386 WP 1998 6 12 VJ9800184 1 19980604 A 5312 BULHEAD DOUG DC9 DC932 3022066 WP BS 371 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 REMOVED STA 37 LOWER BULKHEAD ASSY, FABRICATED ANTENNA DISH IAW EO 9-53-003. ORDERED, DRILLED AND INSTALLED STA 37 LOWE R BULKHEAD SERRATED ASSY, SUPPORT STRUCTURE AND REMAINING BULKHEAD ASSEMBLY. INSTALLED RADOME, PERFORMED FIT CHECK IAW DC9 MM 53-50-1 PG 202. CHECKED GOOD. 2 L 7 2 4F A6WE 1998061200387 19980612 00387 WP 1998 6 12 VJ9800185 1 19980605 A 5532 IA34830 SKIN DOUG DC9 DC932 3022066 WP VERT STAB DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 REMOVED VERTICAL STABILIZER, FABRICATED DOUBLER AND FILLER FROM 7075 T6.063. CUT OUT DENTED AREA, TRIMMED, DRILLED AND INSTALLED REPAIR IAW EO 9-53-004, REINSTALLED VERTICAL STABILIZER LEADING EDGE. 2 L 7 2 4F A6WE 1998061200388 19980612 00388 NM 1998 6 12 VJ9800186 1 19980606 A 3397 WIRE BOEING 737 7372P6 1C84609 NM CABIN CHAFED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 1PC 21613 SECTION 3 OF EMERGENCY FLOOR PATH LIGHTING PULLED UP. REPAIRED CHAFED WIRE BETWEEN SIDEWALL AND LIGHT TRACK AT PASSENGE R SEAT ROW 18DEF, OPS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 1998061200389 19980612 00389 WP 1998 6 12 VJ9800187 1 19980607 A 3260 H201 SWITCH DOUG DC9 DC932 3022066 WP LANDING GEAR FAILED A ZZDA K NONE N FALSE WARNING IN INSP/MAINT 1 SO 15 938VV 47442 GEAR HORN SOUNDED AND 3 UNSAFE LIGHTS ILLUMINATED. FLIGHT CREW ELECTED TO RETURN TO BASE AND CREW OBTAINED 3 SAFE LANDI NG GEAR DOWN LIGHTS. AIRCRAFT FERRIED TO ATL. MAINTENANCE BASE FOR JACKING OF AIRCRAFT AND GEAR SWING AND REAIRS AS NE CESSARY. REPLACED FLAP SWITCH AND PERFORMED GEAR SWING IAW MM 32-00 AND 27-00, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998061200390 19980612 00390 GL 1998 6 12 LR7A9826 2 19980604 A 7230 6894133 DIFFUSER LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 4 ENGINE CRACKED A LR7A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 401LC 5052 1994 4606 550224 NR 4 ENGINE LOW AND DECREASING OIL QUANTITY, PRECAUTIONARY SHUTDOWN. INSPECTED NR 4 ENGINE, AIRCRAFT IN SAFE CONDITION FOR INTENDED FERRY FLIGHT TO ANC, 3 ENGINE FERRY. REMOVED QEC, BORESCOPE INSPECTED ENGINE AND SUPSPECT CRACKED DIFFUSER . 2 H 7 4 4T 4 T A1SO E282 1998061200391 19980612 00391 WP 1998 6 12 CALA9800970 1 19980605 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD NR 71 WITH THREE EACH BLOWN OUT HOLES AND ONE CRACKED. THE CRACK WAS STOP DRILLED. A REPAI R DOUBLER WAS FABRICATED AND INSTALLED ON FLOORBOARD OVER BLOWN OUT HOLES AND CRACK IAW SRM 53-01, FIGURE 2, 51-10-3, PA GE 15 AND 16, 51-10-4, AND 51-30-2, PAGES 1-36. 2 L 7 2 4F A6WE 1998061200392 19980612 00392 WP 1998 6 12 CALA9800971 1 19980605 A 5350 FILLET DOUG DC9 DC932 3022066 WP BS 756-832 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT FUSELAGE FILLET PANEL MATING SURFACE CORRODED AT STA 756 TO 832. A DOUBLER WAS FABRICATED AND INSTA LLED IAW SRM 53-01, FIGURE 4, 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061200393 19980612 00393 WP 1998 6 12 CALA9800972 1 19980605 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 617 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CABIN INTERIOR WEB CRACKED AT FS 617, RBL 50 TO 55. THE CUSP WEB WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 53-01, FIGURE 9. 2 L 7 2 4F A6WE 1998061200394 19980612 00394 WP 1998 6 12 CALA9800973 1 19980605 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 160 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CORROSION ON ATTACH ANGLE BELOW GENERATOR AT STA 160. THE CORRODED SECTIONS OF ANGLE WERE REMOVED IAW SRM 51-30-2. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 53-01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061200395 19980612 00395 WP 1998 6 12 CALA9800974 1 19980605 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 15 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND COCKPIT FLOORBOARD CORRODED ON PILOT'S SIDE IN CORNER FORWARD OF E AND E COMPARTMENT ACCESS DOOR AT STA 15L. THE FLOOR PANELS WERE REMOVED IAW SRM 51-30-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3 AND 51-30-2 . 2 L 7 2 4F A6WE 1998061200396 19980612 00396 WP 1998 6 12 CALA9800975 1 19980605 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 897 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN FITTING AT STA 897 BETWEEN LONGERONS 27L AND 28L. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-5, 51-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998061200397 19980612 00397 WP 1998 6 12 CALA9800976 1 19980605 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1121 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT STA 1121, FIFTEEN INCHES BELOW RT NEGATIVE PRESSURE LOUVERS. THE CR ACK WAS STOP DRILLED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-30-2. 2 L 7 2 4F A6WE 1998061200398 19980612 00398 WP 1998 6 12 CALA9800977 1 19980605 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1104 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND THREE 1 INCH CRACKS AT FASTENER HOLES IN FUSELAGE SKIN AT STA Y= 1104, X= 30. THE CRACKS WERE STOP DRI LLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 3. 2 L 7 2 4F A6WE 1998061200399 19980612 00399 WP 1998 6 12 CALA9800978 1 19980605 A 5530 FAIRING DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND TWO 1 INCH CRACKS IN RADIUS OF ATTACH FLANGE ON LT VERTICAL STABILIZER LOWER FAIRING. THE CRACKS WERE STOP DRILLED IAW SRM 51-01. A FORMED ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998061200400 19980612 00400 WP 1998 6 12 CALA9800979 1 19980605 A 5330 SKIN DOUG DC9 DC932 3022066 WP APU COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A CRACK IN SKIN OF APU COMPARTMENT AT LT SIDE FORWARD BELOW INSPECTION PANEL ACCESS. THE CRACK WAS STO P DRILLED IAW SRM 51-10-44. TWO REPAIR DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-01. 2 L 7 2 4F A6WE 1998061200401 19980612 00401 WP 1998 6 12 CALA9800980 1 19980605 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND SURFACE SKIN OF CABIN FLOORBOARD PANEL NR 77 PUNCTURED. A DOUBLER, HAT SECTION, AND REPAIR PANELS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 1, 51-70-2, 51-10-3, AND 51-20. 2 L 7 2 4F A6WE 1998061200402 19980612 00402 WP 1998 6 12 CALA9800981 1 19980607 A 5312 BULKHEAD BEAM DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN HORIZONTAL BEAM OF RT AFT LAV AFT PRESSURE BULKHEAD. THE CRACK WAS LOCATED JUST AFT OF STA 996, 62 INCHES UP FROM THE FLOOR AT THE OUTBOARD CORNER. THE CRACK WAS STOP DRILLED IAW SRM 53-01. REPAIR ANGL ES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 6, 53-10-3, 51-30-4, AND 51-20-0. 2 L 7 2 4F A6WE 1998061200403 19980612 00403 WP 1998 6 12 CALA9800982 1 19980607 A 5320 ANGLE DOUG DC9 DC932 3022066 WP L1 DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND L-1 DOOR SILL ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATE D AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998061200404 19980612 00404 WP 1998 6 12 CALA9800983 1 19980607 A 5320 FITTING DOUG DC9 DC932 3022066 WP MLG DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN SUPPORT FITTING ON LT AFT END MLG DOOR CUTOUT. THE CRACK WAS TRIMMED OUT IAW SRM 53- 05, FIGURE 71. A REPAIR WAS FABRICATED AND INSTALLED SRM 53-05, FIGURE 71 AND 51-10-3. 2 L 7 2 4F A6WE 1998061200405 19980612 00405 WP 1998 6 12 CALA9800984 1 19980607 A 5520 FAIRING DOUG DC9 DC932 3022066 WP RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 INCH CRACK IN INBOARD AFT CORNER OF RT ELEVATOR GEAR TAB CONTROL ROD FAIRING. A DOUBLER WAS FABRIC ATED AND INSTALLED IAW SRM 55-01, FIGURE 2, 51-10-2, 51-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998061200406 19980612 00406 WP 1998 6 12 CALA9800985 1 19980607 A 5414 PANEL DOUG DC9 DC932 3022066 WP NR 1 ENG PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND THREE .5 INCH CRACKS AT CORNER OF INNER DOUBLER ON NR 1 ENGINE PYLON PANEL NR 8103. THE CRACKED AREA W AS CUT OUT. A DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4. 2 L 7 2 4F A6WE 1998061200407 19980612 00407 WP 1998 6 12 CALA9800986 1 19980608 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CO-PILOT'S FLOORBOARD CORRODED AT STA 130, RBL 34 TO RBL 50. THE FLOORBOARD AND SKIN WERE REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, FIGURE 2F, 51-30-2, 51-10-2, 51-10-4, 51-10-3 AND MM 53-20-1. 2 L 7 2 4F A6WE 1998061200408 19980612 00408 WP 1998 6 12 CALA9800987 1 19980608 A 5313 END CAP DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 INCH CRACK IN END CAP OF LONGERON 19L AT AFT PRESSURE BULKHEAD STA 996. THE END CAP WAS REMOVED AN D REPLACED IAW SRM 51-10-4. 2 L 7 2 4F A6WE 1998061200409 19980612 00409 WP 1998 6 12 CALA9800988 1 19980608 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND L-ANGLE CORRODED AT STA 996, RBL 28. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10, 51-10-2, 51-30-1, AND 51-10-3. 2 L 7 2 4F A6WE 1998061200410 19980612 00410 WP 1998 6 12 CALA9800989 1 19980608 A 5753 RIB DOUG DC9 DC932 3022066 WP WS 270 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN LT WING FLAP RIB AT WS XRS 270 WITH CORROSION AT INBOARD END OF RIB. THE RIB WAS REM OVED IAW SRM 51-30-2. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1998061200411 19980612 00411 NE 1998 6 12 CALA9800990 2 19980607 A 7230 500563501 AIR SEAL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENG COMP WORN A CALA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 09 478AC 48063 717368 THE NR 1 ENGINE FAILED ACCOMPANIED BY A LOUD BANG DURING CLIMB-OUT OF EWR AT 10,000 FEET. THE CREW SHUT THE ENGINE DOWN AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE ENGINE WAS RUN AND ALL PARAMETERS CHECKED GOOD. ENGINEERING CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO A WORN SECOND STAGE INNER AIR SEAL. 2 L 7 2 4F 4 F A6WE E9NE 1998061200412 19980612 00412 WP 1998 6 12 CALA9800991 1 19980608 A 3260 PROX SENSOR DOUG DC9 DC982 3022082 WP NLG INOPERATIVE A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 938AS 49365 THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE FLIGHT WAS CONTINUED TO ORD WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND THE NLG UPLOCK PROXIMITY SENSOR AT FAULT. THE SENSOR WAS REPLACED AND RESHIMMED. THE NOSE GEAR WAS SWUNG WITH OPERATION AND INDICATIONS CHECKIN G GOOD. 2 L 7 2 4F A6WE 1998061200413 19980612 00413 WP 1998 6 12 CALA9800992 1 19980608 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 351 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .75 INCH CRACK IN FORWARD PIT RT FLOOR SUPPORT FRAME ABOVE LONGERON 9R AT STA 351. THE CRACKED SECTI ON OF STANDOFF FLOOR SUPPORT WAS REMOVED. A STANDOFF FLOOR SUPPORT ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-012 63. 2 L 7 2 4F A6WE 1998061200414 19980612 00414 WP 1998 6 12 CALA9800993 1 19980605 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 275-294 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FUSELAGE SKIN DENTED IN FORWARD LAV SERVICE AREA BETWEEN STA 275 AND 294 ABOVE LONGERON 21L. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1998061200415 19980612 00415 WP 1998 6 12 CALA9800994 1 19980605 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND A 1.375 INCH CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REP LACED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998061200416 19980612 00416 NM 1998 6 12 CALA9800995 1 19980605 A 5753 652163092 SKIN BOEING 727 727224 1384076 NM RT TE FOREFLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 23309 22452 INSPECTION FOUND A 4 X 2 AREA OF RT WING TRAILING EDGE INBOARD FOREFLAP LOWER SURFACE DELAMINATED. THE FOREFLAP WAS REM OVED AND REPLACED IAW MM 27-51-12. 2 L 7 3 4F A3WE 1998061200417 19980612 00417 WP 1998 6 12 CALA9800996 1 19980608 A 3350 20131A BATTERIES RADIANT DOUG DC10 DC1010 3022110 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 68046 47800 EMERGENCY LIGHTS AT FORWARD, MID, AND AFT ZONES FAILED FUNCTIONAL CHECK. THE EMERGENCY LIGHT SYSTEM BATTERIES WERE REMO VED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-50-00. 2 L 7 3 4F A22WE 1998061200418 19980612 00418 WP 1998 6 12 CALA9800997 1 19980608 A 5720 DOUBLER DOUG DC9 DC932 3022066 WP BS 438 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT STA 438. THE ANGLE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998061200419 19980612 00419 WP 1998 6 12 CALA9800998 1 19980609 A 5320 ANGLE DOUG DC9 DC981 3022081 WP BAGGAGE DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13881 48045 INSPECTION FOUND AFT BAGGAGE BIN DOOR JAMB Z-ANGLE CORRODED. REPAIRED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998061200420 19980612 00420 NM 1998 6 12 CALA9800999 1 19980609 A 5230 FRAME BOEING 737 737291 138448W NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND A 3 INCH CRACK AT FORWARD LOWER CORNER OF DOOR FRAME JUST BELOW OPEN LATCH ASSEMBLY OF FORWARD CARGO DO OR. THE AREA WAS REPAIRED IAW SRM 51-10-2. 2 L 7 2 4F A16WE 1998061200421 19980612 00421 NE 1998 6 12 9809479997 2 19980607 A 7314 378200 FUEL PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7 52053 NE LT ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 GL 01 8933E 32723 4284 47142 653840 DURING CRUISE AT 33,000 FEET, THE LEFT ENGINE FLAMED OUT. AIRCRAFT DIVERTED TO OMA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL PUMP AND FUEL CONTROL. ENGINE OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998061200422 19980612 00422 WP 1998 6 12 9809489914 1 19980606 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP LT MLG DOOR DIRTY A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 964N 47416 DURING APPROACH, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. FLIGHT CREW PERFORMED EMERGENCY GEAR EX TENSION PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT GEAR DOOR SEQUENCE CABLE AND TELESCOPE SWIVEL BINDING. CLEANED GUMMY SUBSTANCE FROM FITTING AND RERIGGED CABLE. OPERATIONAL CHECK NORMAL ON GEAR SWING. 2 L 7 2 4F A6WE 1998061200423 19980612 00423 1998 6 12 COMA9810134 4 19980604 A 3497 WIRE EMB 120 EMB120RT SO LT STICK SHAKER BROKEN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 259CA 120252 STALL AURAL WARNING WILL NOT SILENCE. REPAIRED BROKEN WIRE AT CONNECTOR PO194 COPILOTS STICK SHAKER. 2 L 7 2 4T RT A31SO 1998061200424 19980612 00424 SO 1998 6 12 COMA9810135 1 19980608 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 462CA 14185 783 120267 EMERGENCY LIGHTS AFT OF ROW 6 ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY. 2 L 7 2 4T RT A31SO 1998061200425 19980612 00425 EA 1998 6 12 COMA9860138 1 19980530 A 5753 601R1430341 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 C-CHECK TASK 002-27-580-100, LEFT HAND INBOARD FLAP VANE HAS CHAFE DAMAGE AT WS 53.60. REPLACED FLAP VANE LEADING EDGE SHIN. 2 L 7 2 4F RT A21EA 1998061200426 19980612 00426 EA 1998 6 12 COMA9860139 1 19980530 A 5753 601R1430342 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 C-CHECK TASK 002-27-680-100, RIGHT HAND FLAP VANE LEADING EDGE HAS CHAFE DAMAGE. REPLACED FLAP VANE LEADING EDGE SHIN P ANEL. 2 L 7 2 4F RT A21EA 1998061200427 19980612 00427 EU 1998 6 12 QXEA9800780 1 19980606 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 ENTRY EMERGENCY EXIT LIGHT OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998061200428 19980612 00428 EU 1998 6 12 QXEA9800781 1 19980606 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 OVERHEAD EMERGENCY EXIT LIGHT AT ROW 9 OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998061200429 19980612 00429 NM 1998 6 12 98FDEA00395 1 19980608 A 5730 65185522 SKIN BOEING 727 72721C 138400M NM BS 869 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 FOUND CRACK EMITTING FROM HOLE IN AFT ROW OF FASTENERS FOR UPPER SKIN BS 869 AT RBL 35. 2 L 7 3 4F A3WE 1998061200430 19980612 00430 WP 1998 6 12 98FDEA00394 1 19980605 A 5530 AMC72971 ANGLE DOUG DC10 DC1030F 3023504 WP VERTICAL STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 311FE 46871 UPPER VERTICAL FIN BASE ANGLE HAS CRACK INDICATION BETWEEN THE NR 4, 5 FASTENER HOLES FROM THE RT SIDE REF WC 8-55307430 3B1 - P1 EA 8-5530-3855 DATED 6/8/98 WRITTEN BASE ANGLE WILL BE REPETITIVE INSPECTED AT INTERVALS NOT TO EXCEED 1800 HRS . BASE ANGLE TO BE REPLACED AT NEXT C-CHECK OR APPROXIMATELY 3,600 FLIGHT HOURS. 2 L 7 3 4F RT A22WE 1998061200431 19980612 00431 NM 1998 6 12 98UAL900038 1 19980128 A 3231 RETRACT MECH BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE GEAR DOORS OUT OF SEQUENCE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 175UA 24382 ON TAKEOFF, GEAR DOOR MESSAGE APPEARED ON EICAS. AFTER BECOMING AIRBORNE, LANDING GEAR HANDLE WAS RAISED AND GEAR CAME UP BUT MESSAGE REMAINED ON. LOWERED GEAR, BURNED DOWN FUEL, AND LANDED UNEVENTFULLY. *S/D* GEAR DOORS FAILED TO CLOSE DUE TO AN OUT OF SEQUENCE CONDITION OF THE ALTERNATE EXTEND MOTOR. RECYCLED LANDING GEAR ALTERNATE EXTEND SYSTEM. GEA R CYCLED AND CHECKED OK. AIRCRAFT RETURNED TO SERVICE. NO FURTHER ACTION TAKEN. NO PARTS REPLACEMENT REQUIRED. RECYC LING OF ALTERNATE EXTEND SYSTEM ACCOMPLISHED PER IRREGULAR PROCEDURES 7-52. 2 L 7 4 4F 4 F RT A20WE E24NE 1998061200432 19980612 00432 NM 1998 6 12 98UAL900198 1 19980515 A 2450 2TC610MOD CIRCUIT BREAKER BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE P7 PANEL FAILED A UALA F A ACTIVATE FIRE EXT. UNSCHED LANDING A FLAME/FIRE NR NOT REPORTED 1 WP 29 157UA 20106 FIRE FROM NR 2 C/B INS. *S/D* C/B C787 FAILED INTERNALLY. REPLACED BREAKER. 2 L 7 4 4F 4 F A20WE E20EA 1998061200433 19980612 00433 NM 1998 6 12 98UAL900201 1 19980517 A 3244 0207910 TIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG BLOWN A UALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 29 7291U 21569 RETURNED TO DEN DUE TO BLOWN RIGHT INBOARD MAIN TIRE. *S/D* FOUND EXTENSIVE DAMAGE TO RIGHT MAIN GEAR, WING AND FLAP A REA. REPLACED NR 3 AND NR 4 MLG WHEEL TIRE ASSEMBLIES. REPAIRED RIGHT WING TRAILING EDGE UPPER AND LOWER WING PANELS, PANEL SUPPORT RIBS AND FUSELAGE FAIRINGS. REPLACED RIGHT MLG INBOARD DOOR, SPOILER PANELS NR 8 AND NR 9, MIDFLAP AND IN BOARD AFT FLAP PANELS. PERFORMED MANUAL EXTENSION CHECK OF ALL THREE GEARS. 2 L 7 3 4F 4 F A3WE E2EA 1998061200434 19980612 00434 NM 1998 6 12 98UAL900210 1 19980521 A 2130 COOLING VALVE SUNDSTRAND 56697 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E COMPT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 7253U 21400 LOST CABIN PRESSURIZATION CONTROL. DESCENDED TO 10,000 FEET AND DIVERTED TO ORD. *S/D* REPLACED E AND E COMPARTMENT C OOLING VALVE DUE TO STUCK OPEN. 2 L 7 3 4F 4 F A3WE E2EA 1998061200435 19980612 00435 NM 1998 6 12 98UAL900211 1 19980521 A 2150 PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LEFT MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 29 7275U 21422 SMOKE IN CABIN WHILE LEFT AIR CONDITIONING PACK OPERATING. PACK SHUT DOWN AND SMOKE CLEARED. CREW REPORTED PACK DISCHA RGE, TEMP WENT HIGH AFTER TAKEOFF FROM DEN. *S/D* MAINTENANCE PERFORMED AN OPERATIONS CHECK AND FOUND ALL INDICATIONS NORMAL. THE PROBLEM HAS NOT REPEATED. 2 L 7 3 4F 4 F A3WE E2EA 1998061200436 19980612 00436 NM 1998 6 12 98UAL900214 1 19980524 A 5210 SEAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE 1 L DOOR OUT OF ADJUST A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 910UA 25254 A LOUD SQUEAL WAS HEARD AT DOOR 1L. *S/D* ADJUSTED THE LOWER HINGE INSIDE THE FLAP SEAL. PRESSURIZED THE AIRCRAFT, NO LEAKS OR SQUEAL DETECTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998061200437 19980612 00437 NE 1998 6 12 98UAL900224 2 19980531 A 7261 ENGINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 519UA 24872 726693 LANDED DEN UNDER AMBER ALERT WITH NR 1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998061200438 19980612 00438 NM 1998 6 12 98UAL900225 1 19980530 A 3610 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 550UA 25398 DIVERTED TO SFO DUE TO A BLEED VALVE PROBLEM. *S/D* LEFT ENGINE BLEED SYSTEM WAS CLOSING OFF DUE TO TEMPERATURE. LEFT ENGINE FAN AIR MODULATING VALVE TEMPERATURE SENSOR AND LEFT ENGINE AIR BLEED OVERTEMP SENSOR REPLACED. NO PNEUMATIC WR ITE-UPS SINCE DIVERSION. 2 L 7 2 4F 4 F RT A2NM E17NE 1998061200439 19980612 00439 NE 1998 6 12 98UAL900226 2 19980530 A 7200 ENGINE BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE NR 2 LOW POWER A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 982UA 21640 THE NUMBER TWO ENGINE WOULD NOT MAKE TAKEOFF EPR. 2 L 7 2 4F 4 F A16WE E2EA 1998061200441 19980612 00441 NM 1998 6 12 98UAL900228 1 19980601 A 2130 PRESSURIZATION BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 595UA 28748 CABIN ALTITUDE AUTO 1 AND 2 STATUS MESSAGES, AND AUTO INOP LIGHT ON OVERHEAD ILLUMINATED. UNSCHEDULED LANDING WAS MADE INTO DEN. 2 L 7 2 4F 4 F RT A2NM E17NE 1998061200442 19980612 00442 GL 1998 6 12 98UAL900229 2 19980601 A 7314 FUEL PUMP DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 1 ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 1837U 47969 451274 SHORTLY AFTER TAKEOFF, NR 1 ENGINE THRUST WENT TO 85 PERCENT N1, THEN UNABLE TO INCREASE OR DECREASE THRUST. OPENED FUE L CROSS FEED VALVE AND THEN ABLE TO CONTROL ENGINE POWER. RETURNED TO SFO. REPLACED THE MAIN FUEL PUMP AND THE MEC. R AN ENGINE AT HIGH POWER WITH ALL PARAMETERS NORMAL. NO PROBLEMS. 2 L 7 3 4F 4 F A22WE E23EA 1998061200443 19980612 00443 EU 1998 6 12 98UAL900230 1 19980601 A 2720 CONTROLS AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RUDDER STIFF A UALA A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 WP 29 430UA 568 VIBRATION IN FLIGHT MOST PRONOUNCED AT 260KTS. COULD FEEL IN THE RUDDER PEDALS AND AFT CABIN. FA STATES THEY COULD HEA R A THUMPING SOUND AFT AND TO THE RIGHT. CREW SAID RUDDER MOVEMENT WAS STIFF ON THE GROUND AND IN FLIGHT. DIVERTED TO LAX. 2 L 7 2 4F 4 F RT A28NM E40NE 1998061200444 19980612 00444 NM 1998 6 12 98UAL900231 1 19980602 A 2530 285W00122 POWER SUPPLY BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE GALLEY OVERHEATED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 773UA 26929 CREW REPORTS ELECTRICAL BURNING SMELL IN AFT GALLEY ON DESCENT. *S/D* THE SMELL RESULTED FROM OVERHEATING OF POWER SUP PLY COMPONENTS IN THE CABIN AREA CONTROL PANEL. UNDER CONDITIONS WHERE BOTH BACK LIGHTS FAIL, THE POWER SUPPLY MAY OVER HEAT. BOEING SERVICE BULLETIN 777-23-0033 ADDRESSES THIS ISSUE BY HAVING THE UNITS REMOVED AND THE POWER SUPPLY UPGRADE D. UNITED IS CURRENTLY CAMPAIGNING THE FLEET TO REMOVE ALL 285W0012-2 UNITS AND REPLACE THEM WITH 285W0012-3 UNITS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998061200445 19980612 00445 NM 1998 6 12 98UAL900232 1 19980601 A 3350 164073 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7265U 21412 FORWARD FACING AFT DROP CEILING EMERGENCY LIGHT INOPERATIVE. BATTERY DISCHARGED. BATTERY WAS REPLACED AND SYSTEM CHECK ED FOR PROPER OPERATION. 2 L 7 3 4F 4 F A3WE E2EA 1998061200446 19980612 00446 NM 1998 6 12 98UAL900233 1 19980530 A 2730 651785073 HYD LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT ELEVATOR FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7280U 21558 LOST ALL A-SYSTEM HYDRAULIC FLUID AND PRESSURE WHEN FLAPS RETRACTED FROM 15 TO 5 DEGREES. RETURNED TO MSY. *S/D* REPL ACED LEFT ELEVATOR HYDRAULIC ACTUATOR SUPPLY LINE. LEAK CHECKED SYSTEM, NO LEAKS FOUND. 2 L 7 3 4F 4 F A3WE E2EA 1998061200447 19980612 00447 NM 1998 6 12 98UAL900234 1 19980601 A 2761 PACKING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 SPOILER LEAKING A UALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 29 7290U 21568 HYDRAULIC SYSTEM-A LOSING FLUID. *S/D* FOUND NR 2 SPOILER ACTUATOR LEAKING FROM PACKING UNDER CAM RETAINER. REPLACED PACKING AND LEAK CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1998061200448 19980612 00448 NM 1998 6 12 98UAL900235 1 19980530 A 2750 RETRACT MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT TE AFT FLAP OUT OF ADJUST A UALA O OTHER E VIBRATION/BUFFET CL CLIMB 1 WP 29 7290U 21568 MEDIUM FREQUENCY VIBRATION FELT IN ENTIRE AIRCRAFT DURING HIGH SPEED CLIMB, CRUISE AND DESCENT. *S/D* FOUND RIGHT HAND OUTBOARD AFT FLAP TRAILING EDGE PLAY EXCESSIVE. ADJUSTED FLAP ECCENTRICS. 2 L 7 3 4F 4 F A3WE E2EA 1998061200449 19980612 00449 NM 1998 6 12 98UAL900236 1 19980602 A 2752 65222346 HYD MOTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7264U 21411 ON CLIMBOUT WHEN FLAPS RETRACTED TO ZERO, INBOARD FLAPS REMAINED AT 2 UNITS. A SYSTEM QUANTITY AND PRESSURE WAS ZERO. R ETRACTED FLAPS AND CONTINUED TO ORD. *S/D* REPLACED INBOARD FLAP HYDRAULIC MOTOR, SYSTEM OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998061200450 19980612 00450 NM 1998 6 12 98UAL900237 1 19980602 A 2150 PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 TRIPPED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7298U 21893 NR 2 PACK TRIPPED AT GATE. CABIN FILLED WITH SMOKE. 2 L 7 3 4F 4 F A3WE E2EA 1998061200451 19980612 00451 NM 1998 6 12 98UAL900238 1 19980529 A 2613 OVERHEAT LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LOWER AFT BODY ILLUMINATED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7448U 21902 LOWER AFT BODY OVER HEAT LIGHT ON. AFTER TURNING APU OFF LIGHT FLICKERS. 2 L 7 3 4F 4 F A3WE E2EA 1998061200452 19980612 00452 NM 1998 6 12 98UAL900239 1 19980603 A 7603 69203343 BEARING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 THROTTLE WORN A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 7285U 21563 NR 2 ENGINE THROTTLE ADVANCES ON ITS OWN AND SPRINGS BACK TO CLIMB EPR SETTING AFTER INITIAL POWER. RETURNED TO ORD. * S/D* REPLACED COMPENSATOR ROD DUE TO WORN BEARING. RIGGED AND CHECKED FRICTION OF THROTTLE. 2 L 7 3 4F 4 F A3WE E2EA 1998061200453 19980612 00453 NM 1998 6 12 MWEA98641 1 19980606 A 3350 60030431 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 701ME 49760 THE CABIN FLOOR TRACK LIGHTS AT ROW 28 AFT ILLUMINATE WHEN POWER IS SHUT OFF. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F RT A6WE 1998061200454 19980612 00454 WP 1998 6 12 MWEA98642 1 19980606 A 5530 591216611N SKIN DOUG DC9 DC915 3022036 WP VERT STAB CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FOUND RIGHT AND LEFT LOWER AFT SKINS ON CANOE FAIRING CHAFED BEYOND LIMITS. MTC REMOVED AND REPLACED SKIN. 2 L 7 2 4F A6WE 1998061200455 19980612 00455 WP 1998 6 12 MWEA98643 1 19980606 A 5312 1109618 BLKHD STIFFENER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FOUND CRACK IN AFT PRESSURE BULKHEAD RIGHT RADIAL 14 IN STIFFENER. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998061200456 19980612 00456 SO 1998 6 12 C2XA98IA128 1 19980415 A 5320 12007089003 SUPPORT EMB 120 EMB120RT SO FRAME 13 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOOR SUPPORT WAS FOUND TO BE CRACKED AT FRAME 13. MAINTENANCE PERFORMED A SPLICE REPAIR IAW EMB120 SRM 51-21-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200457 19980612 00457 SO 1998 6 12 C2XA98IA127 1 19980415 A 5320 12004149002 SUPPORT EMB 120 EMB120RT SO FRAME 16 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 16 LEFT WAS FOUND TO BE CORRODED. MAINTENANCE PERFORME D DOUBLER REPAIR IAW EMB120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200458 19980612 00458 SO 1998 6 12 C2XA98IA126 1 19980415 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED SEAT TRACK IAW EMB-120 SRM 53-01-05 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200459 19980612 00459 SO 1998 6 12 C2XA98IA125 1 19980415 A 5347 12015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD SEAT TRACK WAS FOUND TO BE CORRODED FROM FRAME 17 THROUGH FRAME 25. M AINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW EMB120 SRM 53-01-05 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200460 19980612 00460 SO 1998 6 12 C2XA98IA124 1 19980415 A 5320 1200494001 SUPPORT EMB 120 EMB120RT SO FRAME 13 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE VERTICLE SUPPORT AT FRAME 13 RIGHT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200461 19980612 00461 SO 1998 6 12 C2XA98IA123 1 19980415 A 5320 12004940003 SUPPORT EMB 120 EMB120RT SO FRAME 13 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE VERTICLE FLOOR SUPPORT AT FRAME 13 LEFT WAS FOUND TO BE CRACKED. MAINTENANCE PERFO RMED A DOUBLER REPAIR IAW EMB-120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200462 19980612 00462 SO 1998 6 12 C2XA98IA122 1 19980415 A 5320 12006436003 SUPPORT EMB 120 EMB120RT SO FRAME 43 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM AT FRAME 43 UNDER THE LEFT CENTER BUTT STRAP WAS FOUND TO BE COR RODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A31SO 1998061200463 19980612 00463 SO 1998 6 12 C2XA98IA121 1 19980415 A 5320 12018804003 FITTING EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR ROTATING ARM TO FUSELAGE ATTACH FITTING AT FRAME 15A WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200464 19980612 00464 SO 1998 6 12 C2XA98IA120 1 19980415 A 5320 12018804003 FITTING EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR ROTATING ARM TO FUSELAGE ATTACH FITTINGS WERE FOUND TO BE CORRODED A T FRAME 13A. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ATTACH FITTING IAW EMB-120 SRM 51-40-02, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200465 19980612 00465 SO 1998 6 12 C2XA98IA119 1 19980415 A 5741 12062387601 FITTING EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING AUXILLARY SPAR TO FUSELAGE ATTACH FITTING WAS FOUND TO BE CRACKED. MAIN TENANCE REPAIRED THE FITTING IAW DER APPROVED EMBRAER FAX NR SST-0618/98, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4T RT A31SO 1998061200466 19980612 00466 SO 1998 6 12 C2XA98IA118 1 19980415 A 5320 120057790001 T-PROFILE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE T-PROFILE CORRODED AT FRAME NR 40. MAINTENANCE REMOVED AND REPLACED T HE T-PROFILE IAW EMB 120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200467 19980612 00467 SO 1998 6 12 C2XA98IA117 1 19980415 A 5320 120061590501 CREASE BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CREASE BEAM CORRODED FROM FRAMES NR 38 TO NR 44. MAINTENANCE REMOVED AND REPLACED THE DAMAGED CREASE BEAM IAW EMB-120 SRM 51-40-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200468 19980612 00468 SO 1998 6 12 C2XA98IA116 1 19980415 A 5347 12026865609 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE S EAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200469 19980612 00469 SO 1998 6 12 C2XA98IA115 1 19980415 A 5315 1200449001 FLOORBEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM T-PROFILE CORRODED AT FRAME NR 38. MAINTENANCE REMOVED AND REPLACED TH E T-PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200470 19980612 00470 SO 1998 6 12 C2XA98IA114 1 19980415 A 5411 12018758001 RIB EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE RIB CRACKED ON LEFT SIDE AT FRAME NR 13. MAINTENANCE STOP DRILLED T HE CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200471 19980612 00471 SO 1998 6 12 C2XA98IA113 1 19980415 A 5530 14531597601 DRAG ANGLE EMB 120 EMB120RT SO VERT STABILIZER CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT SIDE DRAG ANGLE CRACKED IN TWO PLACES AT FORWARD END. M AINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED REPAIR ANGLES IAW CONTINTENTAL EXPRESS EC5530-01013. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200472 19980612 00472 SO 1998 6 12 C2XA98IA112 1 19980415 A 5347 12015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WALL SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TR ACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200473 19980612 00473 SO 1998 6 12 C2XA98IA111 1 19980415 A 5347 12016000603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FORWARD FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED T HE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200474 19980612 00474 EU 1998 6 12 C2XA98BT025 1 19980419 A 3310 8ES00451401 TRANSFORMER AEROSP ATR42 ATR42320 8680930 EU COCKPIT OVERHEATED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 19812 99 EWR - AFTER TAKEOFF FROM NEWARK FLIGHT 3340, REPORTED ELECTRICAL SMOKE FILLING CABIN FROM RIGHT FRONT OVERHEAD. CREW AI R RETURNED TO EWR AND EMERGENCY DECLARED. AIRCRAFT LANDED UNEVENTFULLY. MAINTENANCE TROUBLESHOT AIRCRAFT, FOUND READIN G LIGHT TRANSFORMER OVERHEATED AND BECAME INOPERATIVE. AIRCRAFT RELEASED UNDER MEL, P/N 8ES004514 PLACED ON ORDER. (M) 2 H 7 2 4T RT A53EU 1998061200475 19980612 00475 NE 1998 6 12 C2XA98CL036 2 19980411 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 27716 120128 115383 CVG - FLIGHT - 3274 - CREW REPORTED THAT DURING CLIMB THE LEFT ENGINE TORQUE SURGED, 80-105 PERCENT THE NH SURGED TO 131 PERCENT THE NL SURGED TO 120 PERCENT, ALSO THE OIL PRESSURE FLUCTUATED AND THE OIL TEMPERATURE ROSE TOWARD THE RED LINE . THE CREW ACCOMPLISHED A ENGINE SHUTDOWN AND DIVERTED INTO CVG WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE EN GINE AND AFTER EXTENSIVE TROUBLESHOOTING REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINENTAL EXPRESS TASK CARD NR 1S125 671007 AND NR 1S125671008, OPERATIONAL AND LEAK CHECKS WERE GOOD. AIRCRAFT RELEASED. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998061200476 19980612 00476 SO 1998 6 12 C2XA98CL037 1 19980413 A 3240 21582 BRAKE EMB 145 EMB145 SO LT MLG LOCKED UP A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 12934 1656 0136 145019 EWR - FLIGHT 4111 - CREW REPORTED THAT DURING TAXI, SMOKE WAS SEEN COMING FROM THE LEFT MAIN LANDING GEAR AREA, AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE LEFT MAIN LANDING GEAR, THEN REMOVED AND REPLACED THE NR 2 BRAKE ASSEMBLY IAW EMB-145 MM 32-49-03. OPERATIONAL AND LEAK CHECK WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998061200477 19980612 00477 EU 1998 6 12 C2XA98IA110 1 19980411 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING LINE CHECK INSPECTION, FUOND EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE REMOVED AND REPLACED T HE AISLE PATH LIGHTING BATTERY PACK IAW ATR 42-500 MM 33-51-21. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200478 19980612 00478 EU 1998 6 12 C2XA98IA138 1 19980421 A 3350 7012210 LIGHT AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE LIGHT BULB. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200479 19980612 00479 EU 1998 6 12 C2XA98IA139 1 19980421 A 5311 S53971402294 FRAME AEROSP ATR42 ATR42500 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING C-CHECK INSPECTION, FOUND BELLY FAIRING FRAME NR 27A CRACKED AT VERTICAL SUPPORT ON RIGHT SIDE. MAINTENANC E STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW ATR-42 500 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200480 19980612 00480 EU 1998 6 12 PLGA980415A 1 19980415 A 2120 SENSOR SAAB SF340 340B 7860101 EU LT/RT DUCTS MISWIRED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 365BE 340B299 DURING A SPECIAL INSPECTION, MAINTENANCE FOUND THE LEFT AND RIGHT DUCT OVERTEMP SENSOR CONNECTORS (29HD AND 30HD) REVERS ED. CONNECTORS WERE CORRECTLY INSTALLED. (M) 2 L 7 2 4T RT A52EU 1998061200481 19980612 00481 EU 1998 6 12 PLGA980403A 1 19980403 A 5210 SEAL SAAB SF340 340B 7860101 EU PAX DOOR LOOSE A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 347BE 340B187 BOS - FLT 4397 - AFTER TAKEOFF, THE CREW HEARD A LOUD SQUEAL. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MA INTENANCE FOUND FUSELAGE RAIN GUARD SEAL HAD PULLED LOOSE. SEAL WAS REINSTALLED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998061200482 19980612 00482 EU 1998 6 12 PLGA980401A 1 19980401 A 3697 WIRE SAAB SF340 SF340A 7850100 EU LT BLEED BROKEN A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 745BA 340A111 MHT - FLT 4532 - AFTER TAKEOFF, THE LEFT ENGINE ICE LIGHT ILLUMINATED WITH ENGINE ABOVE 98 PERCENT N1. AIRCRAFT RETURNE D TO MHT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKE WIRE ON LEFT LP BLEED VALVE CONNECTOR. SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998061200483 19980612 00483 EU 1998 6 12 PLGA980330A 1 19980330 A 3610 7769022 CONTROL VALVE SAAB SF340 SF340A 7850100 EU LEFT FAILED A A PLGA A UNSCHED LANDING M N OVER TEMP FALSE WARNING CR CRUISE 1 NE 05 358CA 840496 340A047 BOS - FLT 4414 - CREW RECEIVED THE RIGHT DUCT OVERTEMP WARNING WHILE IN FLIGHT. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT BLEED AIR. WARNING LIGHT REMAINED ILLUMINATED. CREW STARTED RIGHT ENGINE SHUT DOWN PROCEDURES WHEN THE WARNI NG LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENACNE FOUND THE LEFT AND RIGHT DUCT OVERTEMP SENSORS CONNECTORS 929HD AND 30HD) WERE REVERSED. ALSO, FOUND LEFT DUCT TEMP CONTROL VALVE HAD FAILED WHICH W AS THE CAUSE OF THE PROBLEM. THE LEFT DUCT TEMP CONTROL VALVE WAS REPLACED AND THE DUCT OVERTEMP SENSOR CONNECTORS WERE CORRECTLY INSTALED. SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998061200484 19980612 00484 EU 1998 6 12 PLGA980325A 1 19980325 A 5210 DOOR SAAB SF340 SF340A 7850100 EU PAX COMPT NOT LATCHED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 749BA 340A152 BTV - FLT 4208 - AFTER TAKEOFF, THE MAIN PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BTV AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED DOOR AND FOUND THAT HANDLE WAS NOT PROPERLY CLOSED. AIRCRAFT WAS RETURNED TO S ERVICE. (M) 2 L 7 2 4T RT A52EU 1998061200485 19980612 00485 EU 1998 6 12 PLGA980309A 1 19980309 A 5270 G6669 SWITCH SAAB SF340 SF340A 7850100 EU MAIN DOOR FAILED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 340BE 340A062 BOS - FLT 4324 - AFTER TAKEOFF, THE MAIN PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DOOR HANDLE SWITCH AND FAILED. SWITCH WAS REPLACED AND AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4T RT A52EU 1998061200486 19980612 00486 EU 1998 6 12 PLGA980305A 1 19980305 A 2910 AIR124470 SWIVEL SAAB SF340 SF340A 7850100 EU NR 2 BRAKE FAILED A PLGA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NE 05 743BA 340A093 BOS - FLT 4781 - WHILE TAXIING TO THE GATE, THE HYDRAULIC PRESSURE INDICATOR WHEN TO 0 PSI. AIRCRAFT CAME TO A STOP AND PASSENGERS DEPLANED. MAINTENANCE FOUND NR 2 BRAKE HYDRAULIC LINE SWIVEL HAD FAILED. LINE WAS REPLACED AND AIRCRAFT WA S RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998061200487 19980612 00487 EU 1998 6 12 PLGA980303A 1 19980303 A 5610 7256100501 WINDSHIELD SAAB SF340 SF340A 7850100 EU LEFT HEAT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 745BA SW4921 340A111 LGA - FLT 4781 - AFTER TAKEOFF, THE LEFT WINDSHIELD HEAT FAILED. AIRCRAFT RETURNED TO LGA DUE TO WEATHER CONDITIONS. M AINTENANCE REPLACED THE LEFT WINDSHIELD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998061200488 19980612 00488 NM 1998 6 12 AALA980899 1 19980506 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 SFO - DURING OVERNIGHT CHECK, SEAT 36H EMERGENCY EXIT LIGHT INOPERATIVE. RESET PUSH BACK PIN AT SEAT 36H CONNECTOR. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200489 19980612 00489 NM 1998 6 12 AALA980898 1 19980506 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 SFO - DURING OVERNIGHT CHECK, SEAT 32H EMERGENCY EXIT PATH LIGHT INOPERATIVE. REPAIRED CONNECTOR PIN AT SEAT 32H. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200490 19980612 00490 NM 1998 6 12 AALA980872 1 19980501 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7667A 25301 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MOST FORWARD CABIN CENTER POSITION INOPERATIVE. CLEANED EME RGENCY EXIT LIGHT ASSEMBLY CONNECTORS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998061200491 19980612 00491 NM 1998 6 12 AALA980859 1 19980503 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 624AA 24582 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BETWEEN PASSENGER SEAT ROWS 9 THROUGH 17 INOPERAT IVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE AT PASSENGER SEAT ROW 9. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F RT A2NM 1998061200492 19980612 00492 NM 1998 6 12 AALA980858 1 19980502 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372AA 25199 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 32H INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200493 19980612 00493 NM 1998 6 12 AALA980854 1 19980403 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 328AA 22328 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROW 32H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WI RE AT SEAT ROW 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200494 19980612 00494 NM 1998 6 12 AALA980855 1 19980430 A 3350 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 328AA 22328 SFO - DURING OVERNIGHT MAINTENANCE, LEFT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED AFT LEFT ENTRY DOOR E MERGENCY EXIT LIGHT CONTACTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200495 19980612 00495 NM 1998 6 12 AALA980856 1 19980501 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN DISCONNECTED A AALA K NONE L NO TEST CR CRUISE 1 SW 07 320AA 22321 ORD - FLT 42 - DURING FLIGHT, EMERGENCY EXIT LIGHT AT PAX SEAT 26B INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200496 19980612 00496 NM 1998 6 12 AALA980848 1 19980430 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635AA 24593 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE PATH LIGHTING WAS INOPERATIVE. REPLACED EMERGENCY EXIT AISLE P ATH LIGHTING CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998061200497 19980612 00497 EU 1998 6 12 AALA980917 1 19980505 A 5270 SC1535B5F48X05N HORN AIRBUS 300 A300B4605R 3930308 EU EMER EXIT DOOR DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14061 471 JFK - DURING OVERNIGHT MAINTENANCE R3 DOOR EMERGENCY EXIT HORN INOPERATIVE. REPLACED EMERGENCY EXIT HORN AT R3 DOOR. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998061200498 19980612 00498 NM 1998 6 12 AALA980823 1 19980422 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 25B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CON NECTOR AT PAX SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200499 19980612 00499 NM 1998 6 12 AALA980824 1 19980422 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CON NECTOR AT PAX SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200500 19980612 00500 NM 1998 6 12 AALA980937 1 19980509 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN CHAFED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 387AM 27184 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS FROM SEAT ROW 32B TO 42B INOPERATIVE. REPAIRED WIRE AT LAMP SO CKET AT SEAT ROW 39B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200501 19980612 00501 NM 1998 6 12 AALA980943 1 19980510 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 663AM 25297 MIA - DURING OVERNIGHT MAINTENANCE, L1 AND R1 AND RIGHT FORWARD SECTION EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRING AT L-25. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998061200502 19980612 00502 WP 1998 6 12 AALA980963 1 19980513 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN MISINSTALLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 285AA 49297 ORD - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT IS INTERMITTENT. RECONNECTED FORWA RD LIGHT STRIP CORRECTLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200503 19980612 00503 NM 1998 6 12 AALA980926 1 19980508 A 3350 P4010051112 MODULE BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 620AA 24578 SFO - DURING OVERNIGHT MAINTENANCE, R2 DOOR EMERGENCY EXIT LIGHT JUST AFT OF DOOR INOPERATIVE, REPLACED EMERGENCY EXIT A ISLE PATH LIGHTING CONTROL MODULE AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998061200504 19980612 00504 NM 1998 6 12 AALA980860 1 19980501 A 5610 141T480149 WINDOW BOEING 767 767223 1385123 NM COCKPIT DEFECTIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 321AA TX2655R 22322 JFK - FLT 142 - DURING CRUISE, FLIGHT CREW NOTICED AN ELECTRICAL SMELL IN THE COCKPIT. FLIGHT AIR INTERRUPTED AND RETUR NED JFK AND LANDED WITHOUT FURTHER INCIDENT. REPLACED CAPTAINS NR 1 WINDOW DUE TO TERMINAL BLOCK ARCHING. WINDOW HEAT CHECKED NORMAL WITH NO ELECTRICAL SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200505 19980612 00505 WP 1998 6 12 AALA980901 1 19980506 A 3397 WIRE DOUG DC9 DC982 3022082 WP AFT STAIR WELL DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7538A 49992 DFW - DURING OVERNIGHT CHECK AFT STAIR SIDE WALL EMERGENCY EXIT LIGHT INOPERATIVE. REATTACHED WIRE TO AFT STAIR SIDE WA LL EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200506 19980612 00506 EU 1998 6 12 AALA980771 1 19980414 A 3350 P4010049 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A AALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 1465K 11491 DFW - FLT 1474 - DURING TAXIING OUT, EMERGENCY EXIT FLOOR PATH LIGHTING ILLUMINATED FROM SEAT ROW 12 AFT AND THEN EXTING UISHED WITH SYSTEM ARMED. REPLACED EMERGENCY EXIT FLOOR LIGHTING BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F RT 1998061200507 19980612 00507 EU 1998 6 12 AALA980834 1 19980424 A 3350 LIGHTS FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1461C 11481 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMEREGNCY FLOOR PATH LIGHTING HAS SEVERAL BULBS INOPERATIVE. REPLACED T WO EMERGENCY EXIT FLOOR PATH LIGHT STRIPS IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998061200509 19980612 00509 EU 1998 6 12 SIMA981195 1 19980429 A 3350 OL3071BPEGPL BULB AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 342AT 345 ORD - FLT 4169 - FLOOR PROXIMITY LIGHT AT ROW 6 INOP. ISSUED MEL 33-22 AND RETURNED A/C TO SERVICE. RAI FLOOR PROX LIG HT BULB. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200510 19980612 00510 EU 1998 6 12 SIMA981114 1 19980421 A 3320 E033601 SOCKET AEROSP ATR42 ATR42300 8680920 EU CABIN BURNED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 21 223AT 223 ORD - FLT 4078 - ELECTRICAL SMELL IN FORWARD CARGO COMP. RAI'D UPPER FLOURSCENT TUBE NR 1 SOCKET ON LEFT SIDE AND RETUR NED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200511 19980612 00511 EU 1998 6 12 SIMA981122 1 19980422 A 2530 16707 ELECT PLUG AEROSP ATR42 ATR42300 8680920 EU GALLEY BURNED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 269AT 269 FWA - FLT 4005 - EN ROUTE FROM ORD TO CMH, A SMOKE SMELL WAS DETECTED FROM THE GALLEY BY THE FLIGHT ATTENDANT. CREW DID NOT DECLARE AN EMERGENCY, BUT ELECTED TO DIVERT INTO FWA. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE SOURCE OF THE ODOR WAS THE PLUG TO THE COFFEE WARMER IN THE GALLEY. THE ITEM WAS DEFERRED PER MEL ITEM 25-10. A/C RETURNED T O SERVICE. REPLACED ELECTRICAL RECEPTICAL AND COFFEE JUG AS PRECAUTIONARY. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200512 19980612 00512 EU 1998 6 12 SIMA981211 1 19980501 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 045 ORD - FLT 4379 - EMERGENCY FLOOR LIGHT INOP AT ROW 7. REPAIRED FAULTY CONNECTION AT ROW 7 BULB. SOLDER REPAIR. A/C WA S RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200513 19980612 00513 EU 1998 6 12 SIMA981241 1 19980504 A 3397 WIRE AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 211 DFW - FLT 4008 - EMERGENCY FLOOR LIGHT INOP. REPAIRED BROKEN WIRE AT EMERGENCY FLOOR RECEPTICLE SOCKET. OPS CHECK GOOD . A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200514 19980612 00514 EU 1998 6 12 SIMA981281 1 19980508 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN LOW VOLTAGE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 275BC 148668 275 SAW - DURNIG PS-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT AND THE NR 1, THREE, FIVE A ND SEVEN EMERGENCY FLOOR LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 3 WL. EMERGENCY LIGHT SYSTEM OPS CHECKED GOOD. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200515 19980612 00515 EU 1998 6 12 SIMA981282 1 19980508 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 11406 017 GRR - CABIN EMERGENCY FLOOR LIGHTING HAS LIGHTS INOP AND FWD CENTER ESCAPE SIGN INOP. RAI BATTERY PACK FOR POWER SUPPLY 10WL IAW ATR JIC, OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200516 19980612 00516 CE 1998 6 12 S2YA98012 1 19980504 A 2612 24409015 FIRE LOOP BEECH 1900 1900D 1154162 CE RT ENGINE BROKEN A S2YA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 118SK UE108 FLT 1029 - MKE-GRB, DURING TAKEOFF, THE RT ENGINE HAD A FIRE INDICATION. AT 400 FT AGL THE FLIGHT CREW SHUT THE ENGINE DOWN AND ACTUATED THE FIRE EXTINGUISHER. DECLARED AN EMERGENCY AND RETURNED TO MKE. AFTER MAKING A SAFE LANDING, MAINT ENANCE INSPECTED THE A/C AND FOUND THE RT ENGINE AFT FIRE LOOP BROKEN WHERE IT TRAVELS THROUGH THE AFT FIER SEA. THE FI RE LOOP AND EXTINGUISHING BOTTLE WERE REPLACED, THE SYSTEM CHECKED GOOD, AND THE A/C WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998061200517 19980612 00517 CE 1998 6 12 S2YA98011 1 19980415 A 3244 TIRE BEECH 1900 1900D 1154162 CE NLG OUT OF ROUND A S2YA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 13 92SK 341 UE92 FLT 1124 - GRR-YYZ, AFTER TAKEOFF, THE FLIGHT CREW FELT A STRONG VIBRATION FROM THE FRONT OF THE A/C. NOTIFIED ATC AND RETURNED TO GRR. AFTER MAKING A SAFE LANDING IN GRR, MAINTENANCE INSPECTED THE A/C AND FOUND THE NOSE TIRE OUT OF ROUND . THE A/C WAS FERRIED TO MKE WHERE THE NOSE WHEEL ASSEMBLY WAS REPLACED. AFTER TEARDOWN OF THE NOSE WHEEL, IT WAS FOUN D THAT A BALANCE WEIGHT HAD BECOME DEBONDED FROM THE INSIDE OF THE TIRE. (M) 2 L 7 2 4T RT A24CE 1998061200518 19980612 00518 CE 1998 6 12 S2YA98008 1 19980312 A 5270 WARNING LIGHT BEECH 1900 1900D 1154162 CE PAX DOOR ILLUMINATED A S2YA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 13 841SK UE84 FLT 1163 - DAY-SBN - IMMEDIATELY AFTER TAKEOFF, THE CABIN DOOR ANNUNCIATOR ILLUMINATED. THE FLT CREW DECIDED TO RETURN TO DAY TO PLACE THE ANNUNCIATOR ON MEL. AFTER AN UNEVENTFUL LANDING, THE CABIN DOOR ANNUNCIATOR WAS PLACED ON MEL. MAI NTENANCE INSPECTED THE DOOR SWITCHES AND ASSOCIATED WIRING. NO DEFECTS WRE FOUND, THE CABIN DOOR ANUNCIATOR OPERATIONAL LY CHECKED GOOD, THE MEL WAS CLEARED. DOOR WAS CONFIRMED CLOSED BY VISUAL INSPECTION IAW MEL. (M) 2 L 7 2 4T RT A24CE 1998061200519 19980612 00519 CE 1998 6 12 S2YA98007 1 19980311 A 6120 5038912121 PRESSURE SWITCH BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A S2YA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 13 118SK UE108 FLT 1162 - MKE-SBN - DURING CLIMB-OUT, THE LT AUTO-FEATHER ANNUNCIATOR EXTINGUISHED. THE CREW DECIDED TO DECLARE AN EME RGENCY AND RETURN TO MKE. AFTER MAKING AN UNEVENTFUL LANDING MAINTENANCE INSPECTED THE A/C AND DETERMINED THAT THE RT H IGH PRESSURE AUTO-FEATHER PRESSURE SWITCH WAS INTERMITTENT. THE SWITCH WAS REPLACED AND THE A/C WAS RETURNED TO SERVICE . (M) 2 L 7 2 4T RT A24CE 1998061200520 19980612 00520 1998 6 12 P2EA98080 4 19980419 A 3414 CONNECTOR BOEING 737 737247 138448D NM RT AIRSPEED IND LOOSE A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 05 204AU 19603 FLT 712 - MCI - REJECTED TAKEOFF AT 85 KTS, ZERO AIRSPEED INDICATION ON F/O'S SIDE. FOUND PITOT CONNECTION ON F/O AIRSP EED INDICATOR LOOSE, RESECURED AND LEAK CHECKED PER MM 34-12-0. (M) 2 L 7 2 4F A16WE 1998061200521 19980612 00521 NM 1998 6 12 P2EA98079 1 19980418 A 3350 1000679 LIGHT BOEING 737 737222 1384473 NM COCKPIT INOPERATIVE A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 208AU 19547 FLT 119 - ATL - FLT DECK EMERGENCY LIGHT INOP. DEFERRED PER MEL 33-15A, CI M208000 ASSIGNED. REF CI M208000, FLT DECK EMERGENCY LIGHT INOP. REPLACED FLT DECK EMERGENCY LIGHT ASSY, OPS OK CI M208000 CLEARED. (M) 2 L 7 2 4F A16WE 1998061200522 19980612 00522 NM 1998 6 12 P2EA98081 1 19980420 A 5210 DOOR BOEING 737 737247 138448D NM CABIN DAMAGED A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 204AU 19603 FLT 106 - MSP - FORWARD ENTRANCE DOOR WAS DAMAGED BY THE JETWAY AT GATE 36 AT MSP. EVALUATED DAMAGE, DETERMINED TO BE D AMAGE TO DOOR LINER ONLY, TRANSFERRED TO C1 NR P204009 DOOR OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1998061200523 19980612 00523 NM 1998 6 12 P2EA98078 1 19980417 A 3411 106145815 PITOT TUBE BOEING 737 737222 1384473 NM RIGHT FAILED A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 05 208AU 143950 19547 FLT 264 - MCI - ON TAKEOFF POWER APPLICATION, CAPTAINS ALTIMETER DROPPED 20 FT TO 980. AN OFF FLAG CME ON. A CROSS CHE CK OF THE F/O'S ALTIMETER SHOWED THE SAME. REPLACED UPPER RT PITOT PROBE PER MM 34-11-11, LEAK CHECKS OF CAPTAINS AND F /O'S SYSTEMS NORMAL MM 34-11-0A. (M) 2 L 7 2 4F A16WE 1998061200524 19980612 00524 NM 1998 6 12 WRLA98084 1 19980508 A 2450 763222 RELAY DOUG MD11 MD11 3023602 NM E/E COMPT FAILED A WRLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 271WA 48518 DURING TAXI OUT, FLIGHT CREW WAS UNABLE TO PARALLEL THE NR 2 AC BUS. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE GATE FO R MAINTENANCE. A/C RETURNED TO GATE WITHOTU FURTHER INCIDENT. MAINTENANCE PERSONNEL REPLACED NR 2 AC BUS TIE RELAY. R ETURN TO SERVICE TEST PERFORMED WITH NO FAULTS NOTED. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998061200525 19980612 00525 NM 1998 6 12 MASA98087 1 19980418 A 3350 GE1619 BULB DHAV DHC8 DHC8202 2809007 NM CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 FLT 7707 - DEN-RAP - PILOT REPORTED LEFT FORWARD EMERGENCY EXTERIOR LIGHT INOP. MAINTENANCE ACTION WAS DEFERRED PER MEL 33-10. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS RESECURED. (M) 2 H 7 2 4T RT A13NM 1998061200526 19980612 00526 NM 1998 6 12 GAIA9846 1 19980512 A 2750 69680081 SPRING BOEING 727 727223 1384074 NM FLAP CONTL VALVE MALFUNCTIONED A GAIA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 854AA 20995 ON DEPARTURE FROM STL, WHEN FLAPS WERE RETRACTED FROM 5 DEGREES TO UP, OUTBOARD AND INBOARD FLAPS STOPPED AT THE 2.5 TO 3 DEGREE RANGE. LE FLAPS REMAINED FULLY EXTENDED. AIRCRAFT RETURNED TO STL AND MADE AN UNEVENTFUL LANDING. REMOVED AN D REPLACED FLAP CONTROL VALVE RETURN SPRING, IW B727 MM 27-51-51. FLAPS FUNCTIONALLY TESTED NORMAL ON GROUND. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998061200527 19980612 00527 NM 1998 6 12 F3LA98043 1 19980506 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 767-787 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURNIG C-CHECK INSPECTION, REPORTED CORROSION ON ANTENNA MOUNT, BS 767-787, LBL 2, AND ON SKIN UNDER ANTENNA MOUNT . MAINTENANCE REMOVED DAMAGED AREA (11 INCH BY 4 INCH), FABRICATED REPAIR DOUBLER AND INSTALLED NEW ANTENNA MOUNT PER S RM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1998061200528 19980612 00528 NM 1998 6 12 F3LA98044 1 19980511 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 773 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLES ON FLOORBEAM AT BS 773, WL 155, (RBL 3, RBL 6, LBL 3, LBL 8 AND LBL 12). MAINTENANCE REMOVED CORRODED AREAS, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30- 2, 51-30-5, 53-10-1 AND 53-10-5. (M) 2 L 7 2 4F RT A16WE 1998061200529 19980612 00529 EU 1998 6 12 WTAA980070 1 19980420 A 5400 NACELLE BAG JETSTM JETSTM3101 1500215 EU RIGHT BIRD STRIKE A WTAA K NONE C F.O.D. UK UNKNOWN 1 WP 17 418UE 780 SMF - BIRD STRKE TO RIGHT WING OUTBOARD NACELLE. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998061200530 19980612 00530 EU 1998 6 12 WTAA980071 1 19980420 A 2150 PACK BAG JETSTM JETSTM3101 1500215 EU CABIN MALFUNCTIONED A WTAA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 17 423UE 799 CIC - FREON PACK CAUSES ELECTRIC ODOR IN CABIN. MAINTENANCE DEFERRED PACK PER MEL 21-13. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998061200531 19980612 00531 WP 1998 6 12 WTAA980072 2 19980420 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RIGHT FAILED A WTAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 17 424UE 796 P63186 SMF - EN ROUTE SMF TO ACV RIGHT ENGINE REPORTED TO RUN ROUGH FOLLOWED BY ABNORMAL ENGINE NOISE, TORQUE LOSS AND DROP IN OIL PRESSURE. IN FLT SHUT DOWN OF RIGHT ENGINE ACCOMPLISHED. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENAN CE REPLACED RIGHT ENGINE. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVCE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998061200532 19980612 00532 SO 1998 6 12 WTAA980073 1 19980425 A 3233 19895 PIN EMB 120 EMB120RT SO RT MLG ACT FAILED A WTAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 17 221YV 120221 ACV - RIGHT MAIN GEAR FAILED TO INDICATE UP WITH ASSOCIATED VIBRATION AND SLIGHT YAW TO THE RIGHT. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. FOUND RIGHT LANDING GEAR ACTUATOR PIN ASSEMBLY AT LANDING GEAR BROKEN. MAINTENANCE REPLACED RIGHT GEAR ACTUATOR PIN ASSEMBLY AND BUSHING. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061200533 19980612 00533 SO 1998 6 12 WTAA9880075 1 19980504 A 5350 RADOME EMB 120 EMB120RT SO FWD FUSELAGE BIRD STRIKE A WTAA K NONE C F.O.D. UK UNKNOWN 1 WP 17 251YV 120251 FAT - BIRD STRIKE TO NOSE CONE AREA. AIRCRAFT REMAINS IN MAINTENANCE FOR REPAIRS. (M) 2 L 7 2 4T RT A31SO 1998061200534 19980612 00534 NM 1998 6 12 USAA980173 1 19980423 A 5330 SKIN BOEING 737 737201 1384454 NM BS 759-761 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 51395 21666 CLT - DURING PILOTS REPORT A 2.75 INCH CRACK WAS FOUND IN THE SKIN BS 759-761.75 STRINGER 24L. INSTALLED FILLER AND DOU BLER PER REPAIR DOCUMENT SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1998061200535 19980612 00535 NM 1998 6 12 USAA980176 1 19980501 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 282AU 39966 23115 ROA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND 1.333 INCH BY 2.5 INCH CORROSION BS 967 STRINGER 25 LEFT. REMOVED CORR OSION AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3 FIG 9. (M) 2 L 7 2 4F A16WE 1998061200536 19980612 00536 WP 1998 6 12 USAA980172 1 19980421 A 5311 FRAME DOUG DC9 DC931 3022065 WP COCKPIT CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 63295 47351 PIT - DURING UNSCHEDULED MAINTENANCE, PILOT REPORT FOUND CORROSION LEVEL 1 AT LOWER F/O EYEBROW WINDOW FRAME 3.25 INCH B Y 9.5 INCH. INSTALLED TEMPORARY WINDOW PANEL AND INTERNAL AND EXTERNAL DOUBLERS PER EA 49467. (M) 2 L 7 2 4F A6WE 1998061200537 19980612 00537 NM 1998 6 12 USAASB98093 1 19980411 A 3350 342658 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 777AU 24979 PVD - DURING OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM, MAINTENANCE FOUND THE LOWER LEFT, FORWARD OVERWING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998061200538 19980612 00538 NM 1998 6 12 USAA980159 1 19980412 A 5330 SKIN BOEING 737 737201 1384454 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 226US 49824 21815 ROA - DURING C-5 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT LOWER HINGE CUTOUT OF AFT SERVICE DOOR. REMOVED CRACK AN D INSTALLED DOUBLER PER EA 61580. (M) 2 L 7 2 4F A16WE 1998061200539 19980612 00539 WP 1998 6 12 EIAA980147 1 19980419 A 3246 95608593 WHEEL DOUG DC9 DC933F 302207A WP MLG CRACKED A EIAA O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 NM 09 933F 547 47191 NR 2 MAIN TIRE, WHEEL RIM CRACKED AND TIRE DEFLATED, DEBRIS SEVERED BOTH HYDRAULIC LINES. REMOVED AND REPLACED NR 2 TIR E AND BRAKE ASSY IAW MM 32-40-1 AND 32-42-1. REPLACED BOTH BRAKE HYD LINES. CHECKED GEAR, FLAP AND ENGINE FOR FOD DAMA GE, NONE NOTED. (M) 2 L 7 2 4F A6WE 1998061200540 19980612 00540 NM 1998 6 12 EIAA980139 1 19980204 A 5400 FITTING BOEING 747 747273C 1384896 NM NR 1 PYLON MISALIGNED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 471EV 20651 DURING 'C5/D' CHECK INSPECTION, NR 1, 2, 3 AND 4 PYLON DSB AND BACKUP FITTING HOLES DO NOT ALIGN. ALTERNATE HOLE LOCATI ONS IAW SB AND HAECO RS R57-04-33642, R57-04-33631, R57-04-33632, AND R57-04-33633. (M) 2 L 7 4 4F A20WE 1998061200541 19980612 00541 WP 1998 6 12 TWAA9805605 1 19980404 A 5720 WEB DOUG DC9 DC951 3022051 WP WING GROOVED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 406EA 47686 STL - DURING OP 9 MAINTENANCE CHECK, FOUND WING LEADING EDGE AREA CUTOUT FOR NR 2 LEADING EDGE SLAT DRIVE TRACK WITH A D EEP WORN GROOVE AT OUTBOARD RIB .3.75 INCH LONG. BLENDED AREA PER ARA 15082 AND SRM 51-10-3. (M) 2 L 7 2 4F RT A6WE 1998061200542 19980612 00542 EU 1998 6 12 UF6A980404 1 19980408 A 7601 JD760J0020020 POWER CABLE BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A O OTHER O OTHER CR CRUISE 1 GL 31 858AW 12090 2035 FWA - FLT 5722 - POWER LEVER CONTROL INOP ON RIGHT SIDE. STANDBY CONTROLS OPERATE NORMALLY. MAINTENANCE REMOVED AND RE PLACED NR 1 POWER CABLE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998061200543 19980612 00543 EU 1998 6 12 AALA980997 1 19980515 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 58-63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - LIGHT CORROSION AND PAINT PEELING OR BLISTERING WITH LIGHT CORROSION UNDER BLISTERS AT RIVET HEADS. TREATED PRIME D PAINTED PER SRM 51-21-00. REINSTALLED FASTENERS PER ESO 30595D, 05-14-98. (M) 2 L 7 2 4F RT A35EU 1998061200544 19980612 00544 WP 1998 6 12 AALA980874 1 19980501 A 5312 BULKHEAD DOUG DC10 DC1030 3023501 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND CORROSION ON FORWARD FACE OF BULKHEAD STATION 1841, STRINGER 43R. REMOVED SECTION OF FRAME AND SPLICED IN A NEW SECTION OF FRAME AND WEB PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998061200545 19980612 00545 WP 1998 6 12 AALA980827 1 19980423 A 5320 BEAM DOUG DC10 DC1030 3023501 WP BS 1902-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - NR 1 GALLEY SUPPORT BEAM AFT OF CABIN 'C' ZONE STATION 1902 TO 2007 HAS CORROSION SEVERAL BELOW AND ABOVE FLOOR LI NE PLACES. FABRICATED AND INSTALLED NEW FLOOR BOARD NR 1 GALLEY SUPPORT BEAM PER AARD 51-10-001 AND SRM 51-10-00-01. ( M) 2 L 7 3 4F A22WE 1998061200546 19980612 00546 WP 1998 6 12 AALA980828 1 19980422 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1964-1975 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - DR FRAME CORRODED AT STATION 1964 BETWEEN STRINGER 48L AND 46L. TREATED, PRIMED AND PAINTED AREA PER SRM 51-21-01 VOL 11 PER ESO 7349, DATED 4-14-98. (M) 2 L 7 3 4F A22WE 1998061200547 19980612 00547 WP 1998 6 12 AALA980886 1 19980505 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 1033-1038 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - SKIN BULGED AND FASTENER HEAD SHEARED 4 FT OUTBOARD OF OUTBOARD AILERON, BOTTOM SURFACE OF WING AND ONE FOOT AFT O F REAR SPAR. REMOVED CORROSION PER SRM 51-21-01 AND REPAIRED AREA PER ESO 7349, DATED 5-1-98. (M) 2 L 7 3 4F A22WE 1998061200548 19980612 00548 WP 1998 6 12 AALA980810 1 19980421 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1139 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND CORROSION UNDER SKIN BULGE AT STATION 1139 STRINGER 44R. REMOVED CORROSION PER SRM 51-21-01 AND INSTALLED R EPAIR PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998061200549 19980612 00549 WP 1998 6 12 AALA980838 1 19980426 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1997 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND CORROSION FOUND ON AFT SUPPORT ANGLE OF BELLFRAME AT BS 1997. INSTALLED NEW SECTION OF CHANNEL PER SRM 53-3 0-00. (M) 2 L 7 3 4F A22WE 1998061200550 19980612 00550 WP 1998 6 12 AALA980839 1 19980426 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1010-1040 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND CORROSION ON SKIN AT BS 1010-1040. INSTALLED REPAIR DOUBLERS PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998061200551 19980612 00551 WP 1998 6 12 AALA980840 1 19980427 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1139 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND CORROSION UNDER TEAR STRIPE BETWEEN STRINGER 41L AND 46L. REMOVED CORROSION SKIN PER SRM 51-21-01 VOL II AN D INSTALLED DOUBLER PER SRM 53-20-00, VOL I PAGE 75. (M) 2 L 7 3 4F A22WE 1998061200552 19980612 00552 WP 1998 6 12 AALA980805 1 19980420 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND CORROSION FOUND ON GALLEY SUPPORT. REMOVED AND REPLACED AND GALLEY SUPPORT PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998061200553 19980612 00553 WP 1998 6 12 AALA980804 1 19980420 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1975 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND VERTICAL SUPPORT AT STATION 1975 AND STRINGER 48L HAS SURFACE CORROSION. INSTALLED NEW INTERCOSTAL PER AARD 51-01-00-5. (M) 2 L 7 3 4F A22WE 1998061200554 19980612 00554 WP 1998 6 12 AALA980803 1 19980420 A 5320 BRACKET DOUG DC10 DC1030 3023501 WP BS 1964 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND BRACKET CORRODED AT STATION 1964 BETWEEN STRINGER 48L AND DR FRAME. INSTALLED NEW BRACKET PER AARD 51-01-00 -5. (M) 2 L 7 3 4F A22WE 1998061200555 19980612 00555 WP 1998 6 12 AALA980802 1 19980420 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1921 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FOUND CORROSION ON AFT CX LOWER AFT CUTOUT JAM, AS SEEN THROUGH AFT SPOOL SUPPORT LIGHTNING HOLE. INSTALLED NEW S HEAR TIE PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998061200556 19980612 00556 WP 1998 6 12 AALA980836 1 19980424 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1955 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - SHEAR TIE CORRODED AT STATION 1955 BETWEEN LONGERON 40L AND 48L. REMOVED CORROSION PER 51-21-01 AND INSTALLED NEW SHEAR TIE PER AARD 51-10-00-01. (M) 2 L 7 3 4F A22WE 1998061200557 19980612 00557 WP 1998 6 12 AALA980837 1 19980423 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1119 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - SKIN BULDGING AND RIVET HEADS ARE DISHED AT STRINGER 44L AND 45L, STATION 1119. REMOVED CORRODED SECTIONS OF SKIN PER SRM 51-21-01 VOL II AND INSTALLED DOUBLER PER SRM 53-20-00 VOL II PAGE 73. (M) 2 L 7 3 4F A22WE 1998061200558 19980612 00558 WP 1998 6 12 AALA980835 1 19980424 A 5320 FITTING DOUG DC10 DC1030 3023501 WP BS 1721 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 163AA 46914 TUL - FORWARD OMNI ROLLER SUPPORT FITTING HAS CORROSION BEHIND AND IN ONE OF THE HOLES THROUGH DOOR JAMB. REMOVED CORRO SION PER SRM 51-21-01 AND REPAIRED CENTER DOOR JAMB PER ESO 7349, DATED 17 APR 98. (M) 2 L 7 3 4F A22WE 1998061200559 19980612 00559 WP 1998 6 12 AALA980914 1 19980505 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 227AA 49177 TUL - FOUND CORROSION ON AFT SIDE OF FRAME FS 1231 LONGER 30. CUTOUT DAMAGE AND INSTALLED FRAME CUTOUT REPAIR PER SRM 5 3-03 FIG 32. (M) 2 L 7 2 4F A6WE 1998061200560 19980612 00560 NM 1998 6 12 AALA984076 1 19980416 A 5311 FRAME BOEING 767 767223 1385123 NM BS 1346 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - BLENDED OUT AN AREA OF CORROSION ON THE AFT SIDE OF THE VERTICAL FLANGE OF THE 146T1044-2 INNER CHORD JUST OUTBOAR D OF STRINGER 36R. REFINISHED THE BLENDED AREA PER SRM SECTION 53-00-7 FIG 101. (M) 2 L 7 2 4F RT A1NM 1998061200561 19980612 00561 NM 1998 6 12 AALA984075 1 19980416 A 5730 SKIN BOEING 767 767223 1385123 NM BS 955 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - WING BOX UPPER SKIN AT STATION N955 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION PER SRM 51-10-0 0. EDDY CURRENT REWORKED AREA FOR CRACKS. FLAP PEEN BLENDED AREAS PER SRM 51-20-06 AND APPLIED PRIMER, PAINT AND TOP C OAT VAPOR BARRIER. (M) 2 L 7 2 4F RT A1NM 1998061200562 19980612 00562 NM 1998 6 12 AALA984074 1 19980316 A 5320 BEAM BOEING 767 767223 1385123 NM BS 1307 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - MAINTENANCE FOUND AND BLENDED OUT AN AREA OF CORROSION ON THE UPPER SURFACE OF THE INBOARD FLANGE OF THE OUTER CHO RD AT STATION 1307. EN SURE THE BLENDOUT IS FLAT IN THE AREA OF THE FASTENERS TO ALIGN FOR PROPER SEATING OF THE FASTEN ERS WHEN REINSTALLED. (M) 2 L 7 2 4F RT A1NM 1998061200563 19980612 00563 NM 1998 6 12 AALA984073 1 19980417 A 5313 STRINGER BOEING 767 767223 1385123 NM BS 1307 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - FOUND CORROSION WAS FOUND ON STRINGER 539R UNDER THE STATION 130. FABRICATE A REPLACEMENT STRINGER SPLICE FROM TH E SAME MATERIAL AND THICKNESS AS ORIGINAL STRINGER SPLICE THAT EXTEND BEYOND DAMAGE AS PER SKETCH. (M) 2 L 7 2 4F RT A1NM 1998061200564 19980612 00564 NM 1998 6 12 AALA984072 1 19980416 A 5330 SKIN BOEING 767 767223 1385123 NM BS 1356-1362 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - FUSELAGE HAS CUTOUT DUE TO CORROSION ON THE INTERIOR SURFACE OF SKIN AT STATION 1356.5 TO 1362. ACCOMPLISHED REPA IR TO THE SKIN AT STATION 1356.5-1362 USING THE INSTRUCTION IN SRM 53-60-01 AND 202 AS A GUIDE. (M) 2 L 7 2 4F RT A1NM 1998061200565 19980612 00565 NM 1998 6 12 AALA984086 1 19980430 A 5320 CHORD BOEING 767 767323 1385205 NM CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 370AA 25197 AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE INNER CHORD OF THE AFT CARGO DOOR LOWER MAIN SILL. TH E BLEND OUT EXCEEDS SRM MAX LIMITS. ALODINED, PRIMED AND PAINTED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDI TION BY ENGINEERING PER MRB767-1612. (M) 2 L 7 2 4F RT A1NM 1998061200566 19980612 00566 NM 1998 6 12 AALA984092 1 19980430 A 3211 TRUNNION BOEING 767 767323 1385205 NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 370AA 25197 AFW - RIGHT MAIN AFT TRUNNION OUTER BUSHING HOLE HAD LIGHT SCORING AND CORROSION BLENDED. REMOVED CORROSION AND LIGHTLY BLENDED SCORING. APPLIED ALODINE TO INSIDE SURFACE OF BORE AND APPLIED SEALANT FOR BUSHING INSTALLATION. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1611. (M) 2 L 7 2 4F RT A1NM 1998061200567 19980612 00567 NM 1998 6 12 AALA984091 1 19980430 A 5311 FRAME BOEING 767 767323 1385205 NM BS 1285 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 370AA 25197 AFW - FOUND AND BLENDED OUT CORROSION ON THE LOWER SURFACE OF THE FRAME INNER CHORD FORWARD FLANGE IN THE AFT CARGO. TH E BLENDOUT EXCEEDED SRM MAX LIMITS. ALODINED, PRIMED AND PAINTED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOT ED CONDITION BY ENGINEERING PER MRB 767-1617. (M) 2 L 7 2 4F RT A1NM 1998061200568 19980612 00568 NM 1998 6 12 AALA984090 1 19980430 A 5320 SUPPORT BOEING 767 767323 1385205 NM R2 DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 370AA 25197 AFW - FOUND AND BLENDED OUT CORROSION ON THE FLOOR SUPPORT TEE 146T0051-40 AT THE R2 DOOR LOWER SILL. REFINISHED THE BL ENDOUT PER SRM 53-00-15. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1616. (M) 2 L 7 2 4F RT A1NM 1998061200569 19980612 00569 NM 1998 6 12 AALA984089 1 19980430 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 786-830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 370AA 25197 AFW - FOUND AND BLENDOUT CORROSION IN CABIN FLOORBEAM. THE BLENDOUT EXCEEDS SRM MAX ALLOWABLE LIMITS. SPLICED IN NEW S ECTION FLOORBEAM FROM STATION 782 TO STATION 831 PER MRB 767-1615. (M) 2 L 7 2 4F RT A1NM 1998061200570 19980612 00570 NM 1998 6 12 AALA984088 1 19980430 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 782-830 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 370AA 25197 AFW - FOUND AND BLENDED CORROSION IN CABIN FLOORBEAMS. THE BLENDOUTS EXCEED SRM MAX ALLOWABLE LIMITS. SPLICED IN NEW S ECTION OF FLOORBEAM ON BOTH FLOORBEAM PER MRB767-1614. (M) 2 L 7 2 4F RT A1NM 1998061200571 19980612 00571 NM 1998 6 12 AALA984087 1 19980430 A 5311 FRAME BOEING 767 767323 1385205 NM BS 1219 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 370AA 25197 AFW - FOUND AND BLENDED OUT CORROSION ON THE LOWER SURFACE OF THE FRAME INNER CHORD AFT FLANGE IN THE AFT CARGO COMPARTM ENT. THE BLENDOUT EXCEEDED SRM MAX LIMITS. ALODINED PRIMED AND PAINTED BLENDED AREA, APPROVED FOR CONTINUED SERVICE WI TH NOTED CONDITION BY ENGINEERING PER MRB 767-1613. (M) 2 L 7 2 4F RT A1NM 1998061200572 19980612 00572 NM 1998 6 12 AALA984077 1 19980416 A 5320 STRAP BOEING 767 767223 1385123 NM BS 1270 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 304AA 22310 AFW - BLENDED OUT TWO AREAS OF CORROSION ON THE UPPER SURFACE OF THE 146T1043-3 FAIL/SAFE CHORD OF THE FRAME AT STATION 1270. REFINISHED THE BLENDED AREAS PER SRM 53-00-15 FIG 101 AND INSTALLED NECESSARY SHIMS UNDER THE LINING ATTACHMENT F ITTING 453T15464. (M) 2 L 7 2 4F RT A1NM 1998061200573 19980612 00573 NM 1998 6 12 AALA980957 1 19980512 A 3350 1013272 LIGHT BOEING 757 757223 1384957 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645AA 24603 ORD - DURING OVERNIGHT CHECK, LEFT FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT FORWARD EMERGENCY EXIT LIGHT . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998061200574 19980612 00574 NM 1998 6 12 AALA980985 1 19980516 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7375A 25202 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT PATH LIGHT AT PASSENGER SEAT 36B INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T CONNECTOR AT PASSENGER SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200575 19980612 00575 NM 1998 6 12 AALA980984 1 19980517 A 3350 P2010031303 LIGHT BOEING 757 757223 1384957 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 625AA 24583 LAX - DURING OVERNIGHT MAINTENANCE, L3 DOOR EMERGENCY EXIT AFT SIDE SIGN WAS FOUND BROKEN. REPLACED L3 DOOR AFT SIDE EM ERGENCY EXIT SIGN LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998061200576 19980612 00576 NM 1998 6 12 AALA980987 1 19980516 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT PATH LIGHT AT PASSENGER SEAT 26B INOPERATIVE. REPLACED EMERGENCY EXIT LIGH T CONNECTORS AT PASSENGER SEAT 26B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200577 19980612 00577 NM 1998 6 12 AALA980992 1 19980515 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 355AA 24036 EZE - FLT 955 - DURING GROUND OPERATIONS, EMERENCY EXIT PATH LIGHT AT PASSENGER SEATS 27B AND 34B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTORS AT PASSENGER SEAT ROWS 27B AND 34B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200578 19980612 00578 NM 1998 6 12 AALA980999 1 19980518 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE SEAT 25H EMERGENCY EXIT SEAT LIGHT WIRING BROKEN AT THE WALL. REPAIRED EMERGENCY EXI T SEAT LIGHT WIRE AT SEAT 25H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200579 19980612 00579 NM 1998 6 12 AALA981002 1 19980519 A 3350 1721651 CONNECTOR BOEING 767 767323 1385205 NM CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357AA 24038 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS AT SEATS 26H AND 31H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGH T CONNECTORS AT SEATS 26H AND 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200580 19980612 00580 WP 1998 6 12 AALA980955 1 19980512 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 400AA 49311 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED FLAT CONNECTOR ON FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200581 19980612 00581 WP 1998 6 12 AALA980990 1 19980515 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59523 49915 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK LIGHTING IN FORWARD CABIN INOPERATIVE. REPAIRED EMERGENC Y EXIT FLOOR TRACK LIGHTING WIRE IN FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200582 19980612 00582 WP 1998 6 12 AALA980991 1 19980515 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 556AA 53086 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK LIGHTING IN MID CABIN INOPERATIVE. RESEATED LOOSE EMERGE NCY EXIT FLOOR TRACK LIGHTING CONNECTOR AT SEAT ROW 18. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200583 19980612 00583 WP 1998 6 12 AALA981001 1 19980519 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG OUT OF ADJUST A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 440AA 49549 DFW - FLT 555 - AFTER TAKEOFF COS EN ROUTE DFW, RED NOSE LANDING GEAR LIGHT ILLUMINATED WITH GEAR HANDLE IN UP POSITION. CYCLED GEAR AND LIGHT EXTINGUISHED. ALL INDICATIONS NORMAL REMAINDER OF FLT. LANDED DFW WITHOUT INCIDENT. INSPECTED AND INCREASED UPLOCK SENSOR TARGET AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200584 19980612 00584 NM 1998 6 12 AALA980819 1 19980421 A 3350 1000677 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 3622 21387 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT ABOVE LEFT ENTRY DOOR IN AFT GALLEY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY ABOVE LEFT ENTRY DOOR IN AFT GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998061200585 19980612 00585 NM 1998 6 12 AALA980902 1 19980506 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 707AA 22464 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. RESECURED EMERGENCY EXIT FLOOR PATH LIGHT CO NNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998061200586 19980612 00586 NM 1998 6 12 AALA980944 1 19980511 A 3260 209125 BULB BOEING 767 767223 1385123 NM COCKPIT FAILED A AALA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 07 336AA 22334 BOS - FLT 155 - DURING APPROACH LEFT MAIN LANDING GEAR DOWN AND LOCK LIGHTS INOPERATIVE AND ONE LIGHT ON RIGHT SIDE INOP ERATIVE. CREW REQUESTED EMERGENCY EQUIPMENT TO STANDBY. AIRCRAFT LANDED BOS WITHOUT INCIDENT. PERFORMED BITE OF PROXI MITY UNIT, NO FAULTS OR EICAS MESSAGES NOTED. RELAMPED BOTH LEFT AND ONE RIGHT GEAR DOWN AND LOCK LIGHT BULBS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998061200587 19980612 00587 WP 1998 6 12 AALA980897 1 19980506 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 16545 53027 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 21 AND 29 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROWS 21 AND 29. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200588 19980612 00588 WP 1998 6 12 AALA980826 1 19980422 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 585AA 53248 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN IN AFT COACH INOPERATIVE. REPLACED EMERGENCY EXIT SIGN LIGHT AS SEMBLY IN AFT COACH. SYSTEM GROUND CHECKS NORMAL. (M) 2 L 7 2 4F A6WE 1998061200589 19980612 00589 WP 1998 6 12 AALA980900 1 19980506 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DISCONNECTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7538A 49992 DFW - DURING OVERNIGHT CHECK, AFT OVERHEAD COMPARTMENT EMERGENCY EXIT LIGHT ABOVE CATWALK INOPERATIVE. REATTACHED WIRE TO AFT OVERHEAD COMPARTMENT EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200590 19980612 00590 WP 1998 6 12 AALA980876 1 19980504 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 249AA 2693 49269 PHX - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY EXIT SPOT LIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED EMERGENCY EX IT SPOT LIGHT AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200591 19980612 00591 WP 1998 6 12 AALA980930 1 19980508 A 3350 LIGHTS DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 457AA 49562 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LGIHT STRIP AT SEAT 26D INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200592 19980612 00592 WP 1998 6 12 AALA980929 1 19980509 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 489AA 49682 SFO - DURING OVERNIGHT MAINTENANCE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROWS 36 THROUGH 43AB INOPERATIVE. REPAIRED WIRE AT SEAT ROW 36AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200593 19980612 00593 WP 1998 6 12 AALA980878 1 19980504 A 7830 LINE DOUG DC9 DC982 3022082 WP NR 2 ENGINE LOOSE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 70524 49916 DEN - FLT 1320 - IMMEDIATELY AFTER TAKEOFF DEN SMOKE AND FUMES ENTERED THE CABIN, AIR INTERRUPTED BACK TO DEN AND LANDED WITHOUT INCIDENT. TIGHTENED NR 2 ENGINE THRUST REVERSER BYPASS VALVE B-NUT. CLEANED OUT RESIDUAL HYDRAULIC FLUID IN A PU. CHANGED COALESCER BAGS. ACCOMPLISHED PACK BURNOUT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998061200594 19980612 00594 WP 1998 6 12 EISA98090 1 19980418 A 5310 STRUCTURE DOUG DC9 DC931 3022065 WP RT LAVATORY CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF CPCP WORKCARD, FOUND CORROSION IN RIGHT AFT LAVATORY FLOOR PAN ATTACH STRUCTURE. FABRICATED AN D INSTALLED REPAIR PARTS PER SRM 51-16, FIGURE 1 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1998061200595 19980612 00595 WP 1998 6 12 EISA98089 1 19980418 A 5220 ANGLE DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A 2 INCH CRACK IN RIGHT AFT EMERGENCY DOOR STRUCTURE LOWER AN GLE. REPLACED ANGLE IN DOOR STRUCTURE PER SRM 52-21-1. (M) 2 L 7 2 4F A6WE 1998061200596 19980612 00596 WP 1998 6 12 EISA98088 1 19980418 A 5220 ANGLE DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A .25 INCH LONG CRACK IN LEFT AFT EMERGENCY EXIT LOWER ANGLE. REPLACED ANGLE IN DOOR STRUCTURE PER SRM 52-21-00. (M) 2 L 7 2 4F A6WE 1998061200597 19980612 00597 WP 1998 6 12 EISA98087 1 19980418 A 5220 ANGLE DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A 1.5 INCH CRACK IN LEFT AFT EMERGENCY EXIT LOWER STRUCTURE A NGLE. REPLACED ANGLE IN DOR STRUCTURE PER SRM 52-21-00. (M) 2 L 7 2 4F A6WE 1998061200598 19980612 00598 WP 1998 6 12 EISA98086 1 19980417 A 5220 ANGLE DOUG DC9 DC931 3022065 WP EMERGENCY EXIT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 977ML 47329 DURING ACCOMPLISHMENT OF ROUTINE 'C' CHECK WORKCARD, NOTED A 1 INCH CRACK IN RIGHT FORWARD EMERGENCY EXIT DOOR STRUCTURE LOWER ANGLE AFT END. REPLACED ANGLE IN DOOR STRUCTURE PER SRM 52-21-1. (M) 2 L 7 2 4F A6WE 1998061200599 19980612 00599 NM 1998 6 12 EISA98103 1 19980428 A 2611 302842 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO COMPT FAILED A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 CARGO SMOKE LIGHT ILLUMINATED DURING CRUISE FROM TMP TO BRU, VISUALLY CHECKED CARGO COMPT FOUND NORMAL. RESET SWITCH. C ONDITION REAPPEARED, LIGHT WENT OUT ON DESCENT UNEVENTFUL LANDING AT BRU. GENERATED FROM PILOT REPORT. REMOVED AND REP LACED NR 1 SMOKE DETECTOR ON MAIN DECK OF CARGO COMPARTMENT. OPS CHECK GOOD IAW BMM CHAPTER 26-00-00. AERONAUTICAL 727- 100 CARGO DOOR CONVERSION MM. (M) 2 L 7 3 4F A3WE 1998061200600 19980612 00600 NM 1998 6 12 TWRA9824 1 19980418 A 2612 335D5 FIRE CARD BOEING 747 747212B 1384886 NM APU INTERMITTENT A TWRA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 619FF 5834 21316 IN FLT APU INTERMITTENT FIRE INDICATION, DISCHARGED FIRE BOTTLE, 'A' LOOP STILL INTERMITTENT. INSPECTION APU COMPT, NO EVIDENCE OF FIRE. INSPECTION ACCOMPLISHED, REPLACED APU FIRE BOTTLE AND SQUIB PER MM 26-22-00. REPLACED FIRE DET CARD AS PER MM 26-10-00. APU OPS CHECK NORMAL. FIRE DETECTION SYSTEM OPS CHECK NORMAL PER MM 26-22-00. (M) 2 L 7 4 4F A20WE 1998061200601 19980612 00601 NM 1998 6 12 TWRA9827 1 19980429 A 3350 S1356B37 LIGHT BOEING 747 747282B 1384860 NM CABIN SHORTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 ON DAILY CHECK, FOUND EMERGENCY LIGHTS IN 'A' ZONE AND UPPER DECK WILL NOT TURN ON WHEN TESTED. REPLACED NR 3 EMERGENCY EXIT LIGHT PACK IN OVERHEAD CENTER OF UPPER DECK AND OVERHEAD ASSY AFT OF P-6 PANEL IN COCKPIT. OPS CHECK NORMAL PER M M 33-51-00. (M) 2 L 7 4 4F A20WE 1998061200603 19980612 00603 NM 1998 6 12 TWRA9826 1 19980428 A 3397 WIRE BOEING 747 747282B 1384860 NM CABIN SHORTED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 610FF 20501 PRIOR TO DEPARTURE WITH COCKPIT EMERGENCY EXIT SWITCH IN OFF POSITION CABIN EXIT LIGHTS CAME ON ALSO IN ARMED POSITION. REPAIRED SHORTED WIRE AT R3 DOOR, OPS CHECK OK AS PER 33-51-00. (M) 2 L 7 4 4F A20WE 1998061200604 19980612 00604 NM 1998 6 12 EIAA980152 1 19980320 A 5754 SKIN BOEING 747 747132 1384882 NM NR 18 LE FLAP DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 HKG - DURING 'B' CHECK INSPECTION, NR 18 L/E FLAP BULLNOSE INBOARD END SKIN DAMAGED. REPAIRED IAW SRM 57-50-03 FIG 8. ( M) 2 L 7 4 4F A20WE 1998061200605 19980612 00605 NM 1998 6 12 EIAA980153 1 19980312 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 500 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, FLOORBEAM CRACKED UPPER CHORD AT STATION 500. REPAIRED FLOORBEAM UPPER CHORD FROM R BL 37 TO RBL 55 AT BS 500 IAW SRM 53-10-07 FIG 8. (M) 2 L 7 4 4F A20WE 1998061200606 19980612 00606 NM 1998 6 12 EIAA980154 1 19980312 A 5230 65B382492 FITTING BOEING 747 747132 1384882 NM CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, FORWARD CARGO DOOR, AFT FITTING P/N 65B38249-2 CRACKED. REPLACED FITTING IAW MM 52- 34-02. (M) 2 L 7 4 4F A20WE 1998061200607 19980612 00607 NM 1998 6 12 EIAA980155 1 19980313 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1490 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, STATION 1490 STRINGER 33R CORROSION BEYOND LIMITS. REPLACED 18 INCH SECTION OF STRI NGER IAW SRM 53-10-03. (M) 2 L 7 4 4F A20WE 1998061200608 19980612 00608 NM 1998 6 12 EIAA980156 1 19980312 A 5711 SPAR BOEING 747 747132 1384882 NM WS 1375 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, LT WING L/E OUTBOARD OF NR 1 PYLON WS 1375 FRONT SPAR LOWER CHORD VERTICAL LEG HAS A REA OF EXFOLIATION CORROSION. REPAIRED SPAR IAW EVERGREEN INTERNATIONAL AIRLINES ECRA NR 481-57-122-2. (M) 2 L 7 4 4F A20WE 1998061200609 19980612 00609 NM 1998 6 12 EIAA980157 1 19980325 A 5414 SKIN BOEING 747 747132 1384882 NM NR 4 PYLON DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, LARGE DENT IN SKIN PANEL LEFT SIDE NAC STATION 185 ABOVE DOOR CUTOUT NR 4 PYLON. RE PAIRED SKIN IAW EVERGREEN INTERNATIONAL AIRLINES ECRA NR 481-54-123-2. (M) 2 L 7 4 4F A20WE 1998061200610 19980612 00610 NM 1998 6 12 EIAA980158 1 19980325 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 1750 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 DURING 'C4' CHECK INSPECTION, STATION 1750 STRINGER 51L CRACKED. FABRICATED SPLICE CHANNEL AND ANGLES AND INSTALLED IAW SRM 51-30-02 FIG 2 AND 9. (M) 2 L 7 4 4F A20WE 1998061200611 19980612 00611 NM 1998 6 12 EIAA980159 1 19980320 A 5414 SKIN BOEING 747 747132 1384882 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, 2.5 INCH CRACK IN PYLON SKIN EXTENDING UP FROM DOUBLER ON RT SIDE OF NR 2 PYLON AT S TATION 180. INSTALLED LARGER DOUBLER IAW S/B 747-54-2034. (M) 2 L 7 4 4F A20WE 1998061200612 19980612 00612 NM 1998 6 12 EIAA980160 1 19980323 A 5411 FRAME BOEING 747 747132 1384882 NM NR 4 PYLON HOLE A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, NR 4 PYLON HAS A HOLE IN FRAME THAT IS BEHIND THE LEFT DOUBLER AT STATION 180. FABR ICATED AND INSTALLED THREE ANGLES IAW SRM 54-10-03 AND SRM 51-30-02. (M) 2 L 7 4 4F A20WE 1998061200613 19980612 00613 NM 1998 6 12 EIAA980161 1 19980320 A 5400 DOUBLER BOEING 747 747132 1384882 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, NR 2 PYLON OUTBOARD DOUBLER HAS A CRACK FROM CORNER RADIUS GOING INTO FASTENER HOLE STATION 180. INSTALLED NEW DOUBLER IAW SRM 51-10-02, 51-30-02, 51-30-05, AND S/B 747-54-2034. (M) 2 L 7 4 4F A20WE 1998061200614 19980612 00614 NM 1998 6 12 EIAA980162 1 19980323 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 480 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, FLOORBEAM UPPER CHORD IS CORRODED AND CRACKED AT STATION 480 RBL 55-65. REPAIRED T- CHORD IAW SRM 51-40-04. (M) 2 L 7 4 4F A20WE 1998061200615 19980612 00615 NM 1998 6 12 EIAA980163 1 19980313 A 5320 SPLICE BOEING 747 747132 1384882 NM BS 1480 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, U-CHANNEL SPLICE PLATE BETWEEN STRINGER 32R AND 33R HAS CORROSION AT FWD 2 BOLTS AT BS 1480, AFT SIDE OF BULKHEAD. REPAIRED SPLICE PLATE PER SB 747-53A2390. (M) 2 L 7 4 4F A20WE 1998061200616 19980612 00616 NM 1998 6 12 EIAA980164 1 19980410 A 5711 SPAR BOEING 747 747132 1384882 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, LEFT WING OLES 1481, FRONT SPAR LOWER RABBET STRUCTURE HAS EXFOLIATION PROGRESS UNDE R FRONT SPAR STIFFENER FITTING. REMOVED CORROSION AND REPAIRED FRONT SPAR LOWER CHORD PER ECRA 481-54-121-2. (M) 2 L 7 4 4F A20WE 1998061200617 19980612 00617 NM 1998 6 12 EIAA980165 1 19980409 A 5720 T-CHORD BOEING 747 747132 1384882 NM RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, RT WING WBL 235.2, CRACKED AND BROKEN UPPER 'T' CHORD. REPAIRED 'T' CHORD PER ECRA 481-57-119-2. (M) 2 L 7 4 4F A20WE 1998061200618 19980612 00618 NM 1998 6 12 EIAA980166 1 19980328 A 5330 SKIN BOEING 747 747132 1384882 NM BS 400-420 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, EXTERIOR FUSELAGE BS 400-420 RT SIDE, INSIDE EXTERNAL POWER RECEPTICAL HOUSING, STRU CTURE HAS CORROSION. REPAIRED FUSELAGE SKIN AT EXTERNAL POWER RECEPTICAL PER ECRA 481-53-127-2. (M) 2 L 7 4 4F A20WE 1998061200619 19980612 00619 NM 1998 6 12 EIAA980168 1 19980416 A 5312 BULKHEAD FITTING BOEING 747 747132 1384882 NM BS 1480 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, U-CHANNEL SPLICE PLATE BETWEEN STRINGER 32L AND 33L HAS CORROSION AT FWD TWO BOLT HO LES AT BS 1480 ON AFT SIDE OF BULKHEAD. REPAIRED OF THE LT BS 1480 BULKHEAD SIDE FITTING AND LT FUSELAGE SKIN (REMOVED FOR ACCESS) PER ECRA 481-53-128-2. (M) 2 L 7 4 4F A20WE 1998061200620 19980612 00620 NM 1998 6 12 EIAA980169 1 19980409 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1920 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, LOWER AFT CARGO COMP, BS 1920 FRAME CRACKED AT STRINGER 40 BELOW DOOR LOCK FITTING. REPAIRED FRAME WEB FROM STRINGER 42R TO 36R PER ECRA 481-52-124-2. (M) 2 L 7 4 4F A20WE 1998061200621 19980612 00621 NM 1998 6 12 EIAA980170 1 19980416 A 5230 LATCH BOEING 747 747132 1384882 NM CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, MAIN CARGO DOOR LATCH FITTING NR 10 HAS CORROSION AT THE FWD INBOARD HOLE. REMOVED CORROSION AT NR 10 FITTING PER ECRA 481-52-125-2 AND REINSTALLED FITTING PER EO 52-747-1002-90 REV D. (M) 2 L 7 4 4F A20WE 1998061200622 19980612 00622 NM 1998 6 12 EIAA980171 1 19980416 A 5230 LATCH BOEING 747 747132 1384882 NM CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, MAIN CARGO DOOR LATCH FITTING NR 9 HAS CORROSION AT THE AFT OUTBOARD HOLE. REMOVED CORROSION AT NR 9 FITTING PER ECRA 481-52-126-2 AND REINSTALLED FITTING PER EO 52-747-1002-90 REV D. (M) 2 L 7 4 4F A20WE 1998061200623 19980612 00623 NM 1998 6 12 EIAA980172 1 19980416 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 1920 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 481EV 19896 MZJ - DURING 'C4' CHECK INSPECTION, AFT PIT CEILING TO FLOOR 'I' BEAM SUPPORT IS CRACKED AT BASE, BS 1920 AT RBL 50. RE PLACED 'I' BEAM POST PER SRM 51-10-01 AND 51-30-02. (M) 2 L 7 4 4F A20WE 1998061200624 19980612 00624 NM 1998 6 12 EIAA980173 1 19980423 A 7931 3440330A221 TRANSMITTER BOEING 747 747SR46 NM NR 4 ENGINE INOPERATIVE A EIAA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 477EV 20784 ORD - DURING CRUISE NR 4 OIL PRESSURE INDICATION DROPPED TO 27 PSI, OIL PRESSURE ANNUNCIATOR LAMP REMAINED EXTINGUISHED, OIL QTY AND TEMP NORMAL. INFLIGHT ENGINE SHUTDOWN ACCOMPLISHED. REPLACED OIL PRESSURE TRANSMITTER PER MM 79-32-03, OP S CHECKED NORMAL. REPLACED OIL PRESS INDICATOR PRECAUTIONARY. ACCOMPLISHED WIND MILL INSPECTION PER MM 72-00-00, 72-61 -00, 72-61-05. NO DISCREPANCIES NOTED. (M) 2 L 7 4 4F A20WE 1998061200625 19980612 00625 EU 1998 6 12 C2XA98BT028 1 19980429 A 3240 5012609 BRAKE AEROSP ATR42 ATR42320 8680930 EU NR 3 INOPERATIVE A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 14833 188 EWR - AFTER LANDING IN NEWARK FLIGHT 3320 CREW REPORTED, 'BRAKES DO NOT WORK EFFECTIVELY, CLATTERING ON RIGHT SIDE AND W HEN FULLY DEPRESSED SLOW BRAKING OCCURS. MAINTENANCE FOUND AN INOPERATIVE BRAKE IN THE NR 3 POSITION, REMOVED AND REPLA CED WITH SERVICEABLE UNIT, OPS AND LEAK CHECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1998061200626 19980612 00626 EU 1998 6 12 C2XA98BT029 1 19980427 A 3260 UNLOCK LIGHTS AEROSP ATR42 ATR42320 8680930 EU LANDING GEAR ILLUMINATED A C2XA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 14813 100 EWR - FLIGHT 3383 - INBOUND TO NEWARK REPORTED HAD A SYSTEM TWO MAIN LANDING GEAR UNLOCK LIGHT ILLUIMINATE IN FLIGHT. A IRCRAFT LANDED WITHOUT PROBLEMS. MAINTENANCE PERFORMED PSEU BITE CHECK FOUND NO DEFECTS, AIRCRAFT TEST FLOWN NO DEFECTS NOTED, AND AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200627 19980612 00627 NM 1998 6 12 ORJA9864 1 19980327 A 7830 TR FAULT LIGHT DOUG MD90 MD9030 3023690 NM NR 1 ENGINE ACTIVATED A ORJA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 WP 11 902RA 53490 RETURN TO GATE LEFT ENGINE SYSTEM FAIL AND LEFT REVERSER FAULT. INSPECTION OF NR 1 ENGINE INLET AND EXHAUST, NO DISCREP ANCIES NOTED TEMP MOMENTARY RISE ACCEPTABLE PER TRANSIENT GRAPH MM CH 71-01-02 REV FAULT GONE. (M) 2 L 7 2 4F RT A6WE 1998061200628 19980612 00628 EU 1998 6 12 C2XA98IA142 1 19980430 A 3350 GE1864 BULB AEROSP ATR42 ATR42500 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14451 512 EFD - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EXTERIOR EMERGENCY FLOOD LIGHT ON THE LEFT SIDE WAS INOPER ATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AND OPERATIONALLY CHECK IAW ATR42-500 JIC 33-50-00 OPT 10000-001 AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061200629 19980612 00629 EU 1998 6 12 C2XA98BT027 1 19980422 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 09 17831 185 EWR - UPON SHUTTING AIRCRAFT DOWN FOLLOWING A FLIGHT, FOUND EMERGENCY EXIT LIGHTS ON. COULD NOT EXTINGUISH. PRIOR TO R E-CHARGING BATTERY, AIRCRAFT WAS POWERED UP, AND SWITCH CYCLED TO OFF. THEN BATTERIES WERE RE-CHARGED. 2 H 7 2 4T RT A53EU 1998061200630 19980612 00630 EU 1998 6 12 C2XA98BT026 1 19980423 A 5330 SKIN AEROSP ATR42 ATR42320 8680930 EU FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 25811 094 BTV - DURING A SCHEDULED INSPECTION, RT SIDE FUSELAGE, 3 INCHES FROM FWD LOWER CORNER OF 7TH WINDOW BACK, A DEEP GOUGE W AS FOUND, .290 LONG, .060 WIDE, .0455 DEEP. REPAIRED DAMAGED AREA IAW SRM 53-31-22 PAGE 420, FIGURE 405. LEAK CHECKED IAW ATR42 JIC 05-53-00. NO LEAKS. (M) 2 H 7 2 4T RT A53EU 1998061200631 19980612 00631 CE 1998 6 12 C2XA98IA141 1 19980503 A 6120 1293640919 P/C BOARD BEECH 1900 1900D 1154162 CE NR 2 PROP INOPERATIVE A C2XA K NONE O OTHER AP APPROACH 1 SW 09 69548 UE193 IAH - DURING FLT 3838 - THE NR 2 PROPELLER FEATHERED ON APPROACH TO IAH. THE A/C LANDED WITHOUT INCIDENT AT IAH WHERE M AINTENANCE REMOVED AND REPLACED AUTOFEATHER PRINTED CIRCUIT BOARD. OPERATION CHECKS WERE DONE IAW B1900-D MM 61-21-00 A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998061200632 19980612 00632 EU 1998 6 12 C2XA98BT030 1 19980430 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 97841 280 BTV - DURING A 2A INSPECTION, FOUND EMERGENCY LIGHTS BATTERY PACK INOP AT POSITIONS 29WL AND 18WL. REMOVED AND REPLACED BATTERY PACKS AND OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998061200633 19980612 00633 NM 1998 6 12 BJNA9803007 1 19980428 A 2613 87858201 CONNECTOR BOEING 737 737214 138446R NM ENGINE FAILED A BJNA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 ENGINE OVERHEAT LIGHT FLICKERED ON AND OFF. REMOVED AND REPLACED CONNECTOR PER BSWM 20-67-14, OPS CHECK NORMAL PER BMM 26-11-0. (M) 2 L 7 2 4F A16WE 1998061200634 19980612 00634 WP 1998 6 12 AALA980875 1 19980504 A 2530 700976 COFFEE MAKER DOUG DC9 DC982 3022082 WP GALLEY DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 205AA 49155 DFW-SJC - FLT 1967 - DURING CRUISE, FLT ATTENDANTS REPORTED A STRONG ELECTRICAL BURNING SMELL IN THE AFT GALLEY. THE SM ELL WENT AWAY WHEN GALLEY POWER WAS TURNED OFF. LANDED SJC WITHOUT INCIDENT. REPLACED NR 4 COFFEE MAKER, ACCOMPLISHED SNIFF CHECK. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F A6WE 1998061200635 19980612 00635 NM 1998 6 12 AALA980915 1 19980504 A 2421 IDG BOEING 767 767323 1385205 NM NR 2 ENGINE MALFUNCTIONED A AALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SW 07 374AA 25201 R GEN DRIVE EICAS MESSAGE WITH ASSOCIATED DRIVE LIGHT ON, GEN DRIE DISCONNECTED AS PER ABNORMAL CHECKLIST. PLACARDED RT IDG INOP PER MEL 24-1 AUTH NR 5-49DC-B ENT IN MIC. BOTH IDGS SERVICED AND APU OIL QTY READS FULL. NO SERVICE REQUIRED . REMOVED AND REPLACED NR 2 ENGINE IDG OPS AND LK CHECK GOOD 374240236/1854. (M) 2 L 7 2 4F RT A1NM 1998061200636 19980612 00636 NM 1998 6 12 AALA980916 1 19980504 A 2421 IDG BOEING 767 767323 1385205 NM LT ENGINE FAILED A AALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 352AA 24033 GRU - FLT 920 - ON LEFT ENGINE START GEN DRIVE LIGHT FAILED TO EXTINGUISH. DEFERRED LT ENGINE IDG AS PER MEL REF MIC SH EET AND PLACARDED. PERFORMED AND SERVICED OIL LEVEL RT/LT AND APU GENERATOR AS REQUIRED PER MPM 24-01. REPLACED LT ENG IDG REQUIRES OPS CHECK LEAK CHECK DFRL.4. REPLACED NR 1 IDG AND SERVICED WITH OIL. LEAK CHECK AND OPS CHECK OK. REMO VED PLACARD AND CLEARED MIC SHEET. (M) 2 L 7 2 4F RT A1NM 1998061200637 19980612 00637 NM 1998 6 12 AALA980894 1 19980430 A 7722 EGT PROBE BOEING 767 767323 1385205 NM LT ENGINE FAILED A AALA K NONE O OTHER AP APPROACH 1 SW 07 372AA 25199 LAX - FLT 38 - EGT LEFT ENGINE WENT TO 30 MOMENTARILY ON APPROACH. ITEM PREV ACCOMP AT ORD NR 133275. REF L/P 4254905. REMOVED AND REPLACED 3 EGT PROBES ON LOWER HARNESS. SYTEM GROUND CHECK NORMAL ON GROUND. (M) 2 L 7 2 4F RT A1NM 1998061200638 19980612 00638 NM 1998 6 12 AALA980892 1 19980430 A 2612 FIRE LOOP BOEING 767 767323 1385205 NM LT ENGINE MALFUNCTIONED A AALA K NONE O OTHER CR CRUISE 1 SW 07 378AN 25447 GIG - FLT 904 - LT ENGINE FIRE LOOP 1 STATUS MSG WILL NOT ERASE FIRE LOOP DEF INOP AS PER MEL REF MIC SHEET ENTERED. RE PLACED LOWER FWD LOOP AND UPPER AFT LOOP FOR LEFT ENGINE PER MM. OPS CHECK NORMAL. REMOVED PLACARD AND CLRD MIC SHEET. (M) 2 L 7 2 4F RT A1NM 1998061200639 19980612 00639 NM 1998 6 12 AALA980849 1 19980428 A 2612 FIRE LOOP BOEING 767 767323 1385205 NM LT ENGINE MALFUNCTIONED A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 373AA 25200 MIA - FLT 2101 - LT ENGINE FIRE LP2, VERIFIED FIRE DETECTION WITH MANUAL MEL AND TUL TECH. NO ABNORMAL ENGINE INDICATIO NS. CHECK NR 1 ENGINE FIRE PROTECTION, ERASED STATUS MESSAGE. AIRCRAFT OK FOR SERVICE PER RMM 26-2. (M) 2 L 7 2 4F RT A1NM 1998061200640 19980612 00640 NM 1998 6 12 AALA980895 1 19980430 A 7722 HARNESS BOEING 767 767323 1385205 NM RT EGT FAILED A AALA K NONE O OTHER CR CRUISE 1 SW 07 376AN 25445 JFK - FLT 956 - RIGHT EGT WENT TO ZERO ONE HOUR INTO FLIGHT CAME BACK ON ABOUT 6 HOURS INTO FLIGHT OPERATION INTERMITTEN T FOR REMAINDER OF FLT. CHECKED WIRING FROM RT ENGINE 'J' BOX TO FIRE WALL CONNECTOR AND WIRING CHECKED GOOD. REPLACED RT ENGINE LOWER EGT HARNESS PER MM RAN RT ENGINE AND EGT WAS NORMAL OK FOR SERVICE. (M) 2 L 7 2 4F RT A1NM 1998061200641 19980612 00641 NM 1998 6 12 AALA980850 1 19980427 A 3610 DUCT BOEING 767 767323 1385205 NM LT ENGINE LOOSE A AALA O OTHER J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 381AN 25450 MIA - FLT 2101 -DURING CLIMB AT ABOUT 20,000 FT LEFT ENGINE OVERHEAT WARNING APPEARED. RAN PROCEDURE AND WHEN RETARDING LEFT THROTTLE BELOW 70 PERCENT THE ENGINE OVERHEAT LIGHT EXTINGUISHED. CHECKED ALL PNEUMATIC DUCTS FOR CONDITION, ALL OK. CHECKED CLAMPS, FOUND ONE CLAMP LOOSE ON DUCT. TIGHTENED CLAMP. RAN ENG AT 97 PERCENT N1. OPS CHECK NORMAL. LT ENGINE OVERHEAT LOOP DET 5407 REPLACED. PERFORMED GROUND OPS CHECK OF DET SYSTEM CHECKS NORMAL. (M) 2 L 7 2 4F RT A1NM 1998061200642 19980612 00642 WP 1998 6 12 TWAA9807313 1 19980312 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND BELOW RT AFT LAVATORY FLOOR, ANGLE AT STATION 996 BELOW LONGERON 18R, AT CUS T LINE, CRACKED. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998061200643 19980612 00643 WP 1998 6 12 TWAA9807312 1 19980413 A 5744 BLOCK DOUG DC9 DC932 3022066 WP RT TE FLAPS CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE FLAP INSIDE FLAP OUTBOARD FLAP HINGE TO FORWARD MOUNT BOLT, RT AN D LT SIDE MOUNT WEBS CRACKED OUT FROM BOLT HOLES. REPLACED MOUNT BLOCK PER STANDARD PRACTICES AND SRM 51-01. (M) 2 L 7 2 4F A6WE 1998061200644 19980612 00644 WP 1998 6 12 TWAA9807311 1 19980327 A 5753 PIVOT ARM DOUG DC9 DC932 3022066 WP LT TE FLAP WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP16 MAINTENANCE CHECK, FOUND LT TE FLAP CENTER HINGE PIVOT BEARING OUTBOARD LUG WORN AND CORRODED INBEARIN G BORE. INBOARD BEARING BORE WORN OVERSIZE. INSTALLED NEW HINGE CASTING PER MM 27-50-1. (M) 2 L 7 2 4F A6WE 1998061200645 19980612 00645 WP 1998 6 12 TWAA9807310 1 19980327 A 5753 PIVOT ARM DOUG DC9 DC932 3022066 WP RT TE FLAP WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP CENTER HINGE PIVOT BEARING INBOARD AND OUTBOARD LUGS WITH WORN GROOVES AND PITTING CONDITION IN BEARING BORES. INSTALLED NEW CENTER HINGE PIVOT ARM PER MM 27-50-01. (M) 2 L 7 2 4F A6WE 1998061200646 19980612 00646 WP 1998 6 12 TWAA9807309 1 19980323 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION ON FLOORBEAM CAP AT FS 160 FROM OL-288. REPLACED FLOORBEA M CAP PER SRM 51-01, PAGE 1 ITEM 1C. SEALED PER SRM 91-20-0. (M) 2 L 7 2 4F A6WE 1998061200647 19980612 00647 WP 1998 6 12 TWAA9807308 1 19980307 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 965 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND UNFILLED HOLES IN FUSELAGE SKIN AT STATION 965, BELOW LONGERON 14R. REPAIRE D PER ARA 15017A. (M) 2 L 7 2 4F A6WE 1998061200648 19980612 00648 WP 1998 6 12 TWAA9807307 1 19980307 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 155 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 44 INDICATING CRACK IN RT WING LOWER REAR SPAR STATION XSR 155. REWORKE D PER SERVICE REWORK DRAWING JO60173 AND TWS STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061200649 19980612 00649 WP 1998 6 12 TWAA9807306 1 19980407 A 5510 HORIZ STAB DOUG DC9 DC932 3022066 WP LEFT GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP16 MAINTENANCE CHECK, FOUND ON LT HORIZ STAB TOP AFT 2 BARREL NUT HOLES GOUGED. REAMED HOLES AND INSTALL ED BUSHING AND REDRILLED .562 IN PER ARA 15267. (M) 2 L 7 2 4F A6WE 1998061200650 19980612 00650 WP 1998 6 12 98ZZZX2137 1 19980520 A 3397 B13350081653718 WIRE LKHEED 1011 10113851 5265010 WP CABIN BROKEN A WRNA K NONE L NO TEST IN INSP/MAINT 1 SO 05 826CR 193A1141 ON PERFORMING LAYOVER SERVICE, FOUND BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHTING SYSTEM AT SEAT ROWS 45 HJ. BROKEN WI RE REPAIRED. 2 L 7 3 4F A23WE 1998061200652 19980612 00652 SO 1998 6 12 98ZZZX2139 1 19980325 A 3250 AN3H5A BOLT PIPER PA31 PA31350 7103110 SO NLG STEERING FAILED A L A VLGA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 633D 317852098 WHILE IN-FLIGHT AND AFTER MAIN GEAR WAS DOWN AND LOCKED, PILOT TRIED TO RERACT THE GEAR. THE GEAR WOULD NOT FULLY RETRA CT. GEAR WAS PLACED DOWN. PILOT OBSERVED 3 GREENS. ON LANDING AT ANE, THE PILOT NOTICED THE AIRCRAFT HAD A LEFT TURNI NG TENDENCY. AFTER TWO ATTEMPTS TO LAND, THE PILOT LANDED WITHOUT OCCURRENCE. FOUND THE NOSE GEAR WOULD SHAKE IN A LT TURN. IT WAS ALSO FOUND THAT THE SHIMMY DAMPENER ROD WAS BENT AND THIS IS WHAT CAUSED NOSE LANDING GEAR TO STICK IN A L T TURN. ALSO, BELIEVED TO BE THE REASON FOR THE LANDING GEAR NOT FULLY RETRACTING. THE INSPECTION ALSO FOUND THE 3 AN 3H-5A BOLTS THAT ATTACH THE NOSE GEAR STEERING PLATE ASSEMBLY. 1 L 7 2 3O A20SO 1998061200667 19980612 00667 SO 1998 6 12 98ZZZX2154 1 19980406 A 3233 AN83740 FITTING PIPER PA31 PA31350 7103110 SO MLG ACTUATOR FAILED A GAJA O OTHER J WARNING INDICATION AP APPROACH 1 NM 11 3528Y 317952149 'AN' FITTING CRACKED WITH NO SIGNS OF LEAK OR WEAR CAUSING HYD SYSTEM TO BE DRAINED ON GEAR RETRACT. BECAUSE SYSTEM HAS STANDPIPE FOR EMERGENCY USE WAS ABLE TO PUMP GEAR DOWN AND GET 3 GEAR GREEN, BUT ALSO RED LIGHT SAYS SYSTEM NOT COMPLET ELY CYCLED. LANDED GEAR DOWN AND LOCKED, BUT FOLLOW-UP GEAR DOOR DOWN. NO INCIDENT. 1 L 7 2 3O A20SO 1998061200670 19980612 00670 WP 1998 6 12 IXXA9800054 1 19980514 A 3260 H2024B SWITCH DOUG DC8 DC871F 302199D WP RT MLG DOOR DEFECTIVE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 830BX 45973 DURING CLIMBOUT, THE GEAR DOOR WARNING LIGHT WAS INTERMITTENTLY FLASHING. THE CREW CYCLED THE LANDING GEAR AND PERFORME D A GEAR UPLATCH CHECK, ALL INDICATIONS WERE NORMAL. MAINTENANCE INSPECTED THE GEAR DOOR WARNING SYSTEM AND TRACED THE DISCREPANCY TO THE RIGHT MAIN GEAR DOOR SWITCH. THE SWITCH WAS REPLACED AND A SUCCESSFUL OPERATIONAL CHECK WHICH RETURN ED THE AIRCRAFT TO SERVICE. 2 L 7 4 4F RT 4A25 1998061200671 19980612 00671 WP 1998 6 12 IXXA9800055 1 19980609 A 3231 RETRACT MECH DOUG DC8 DC862 3021970 WP NLG DOORS LACK OF LUBE A IXXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 61CX 46142 AFTER TAKEOFF WHEN THE GEAR WAS RETRACTED, THE FORWARD NOSE GEAR DOORS REMAINED OPEN. THE CREW CYCLED THE GEAR WITH NO HELP. THE FLIGHT CONTINUED TO TOL, MAKING AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE NOSE GEAR DOOR LATCH MECHAN ISMS, WITH NO DISCREPANCIES NOTED. MAINTENANCE CLEANED AND LUBRICATED THE DOOR LATCH MECHANISMS AND RETURNED THE AIRCRA FT TO SERVICE FOLLOWING A SUCCESSFUL GEAR SWING IN ACCORDANCE WITH THE DOUGLAS DC-8 MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 1998061200672 19980612 00672 SO 1998 6 12 PNSA980501A 1 19980516 A 2842 SENDING UNIT PIPER PA31 PA31350 7103110 SO FUEL SYST FAILED A A PNSA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 AL 03 15PR 318052011 WHILE IN CRUISE, THE PILOT NOTED A RAPID DROP IN FUEL QTY INDICATION. SHORTLY THEREAFTER THE LT ENG LOST POWER. FOLLOW ED BY A RT ENG POWER LOSS 2 MIN LATER. A SUCCESSFUL LANDING WAS ACCOMPLISHED WITH NO DAMAGE TO THE ACFT. UPON FURTHER INVESTIGATION, IT WAS FOUND THAT 5 OF THE FUEL QTY SENDING UNITS IN THE ACFT DID NOT MEET THE CORRECT OHM VALUE. THE FA ULTY SENDERS WERE REPLACED AND THE ACFT WAS RETURNED TO SERVCE. SUBSEQUENTLY A FLEET WIDE SURVEY (6 ACFT) WAS CONDUCTED . APPROX 40 PERCENT OF THE SENDERS IN SERVICE WERE FOUND OUT OF TOLERENCE. IN REPLACING THESE SENDERS IT WAS NOTED THA T 50 PERCENT OF THE NEW SENDERS ACQUIRED FROM PIPER WERE ALSO OUT OF TOLERENCE AND THEREFORE REJECTED. 1 L 7 2 3O A20SO 1998061200673 19980612 00673 SW 1998 6 12 PNSA980502 1 19980523 A 7603 LEVER SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP COCKPIT OUT OF POSITION A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK W INADEQUATE Q C TO TAKEOFF 1 AL 03 640PA AC759B RPM ROLLED BACK ON BOTH MOTORS DURING TAKEOFF ROLL. TAKEOFF ABORTED. PILOT NOTED SPEED LEVERS WERE NO LONGER IN THE TA KEOFF POSITION. SPEED LEVERS RESET AND FRICTION LOCKS SET, NEXT TAKEOFF UNEVENTFUL. NO FAULTS FOUND. 2 L 7 2 4T 4 T RT A8SW E4WE 1998061200674 19980612 00674 SO 1998 6 12 PNSA980503 1 19980505 A 8120 4091709001 TURBO CHARGER PIPER PA31 PA31350 7103110 SO LT ENGINE MALFUNCTIONED A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 15PR 1470 318052011 LT ENGINE WOULD NOT DEVELOPE FULL POWER, ABORTED TAKEOFF. REPLACED TURBO CHARGER, OPERATIONAL CHECK OK. 1 L 7 2 3O A20SO 1998061200675 19980612 00675 SO 1998 6 12 PNSA980504 1 19980502 A 5210 MECHANISM PIPER PA31 PA31350 7103110 SO CREW COMPT DOOR NOT LATCHED A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 AL 03 27663 317852094 CREW DOOR OPENED ON TAKEOFF. ABORTED TAKEOFF. SECURED DOOR. NO FAULT FOUND. 1 L 7 2 3O A20SO 1998061200676 19980612 00676 NM 1998 6 12 RAAA98B1082 1 19980608 A 3530 4566M37B042NM PBE BOEING 727 72722C 138400F NM COCKPIT VACUUM LOST A RAAA K NONE O OTHER CR CRUISE 1 AL 03 831RV 19093 FLIGHT CREW REPORTED COCKPIT PBE INDICATOR PROTRUDES IN FLIGHT. CHANGED PBE DUE POUCH VACUUM LOST. 2 L 7 3 4F A3WE 1998061200677 19980612 00677 SO 1998 6 12 RAAA98E4013 1 19980603 A 5320 BEAM LKHEED 188 188C 5262604 SO BS 191 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED S/B 609A INSPECTION, FOUND FLIGHT STATION PRESSURE DECK LOWER BEAM CAP CRACKED APPROX 4.0 INCHES AT FS 191, RBL 40. REPAIRED PER LAC DWG NR 841292. M-54 NR 55. 2 L 7 4 4T 4A22 1998061200678 19980612 00678 SO 1998 6 12 RAAA98E4014 1 19980603 A 5320 BEAM LKHEED 188 188C 5262604 SO BS 130 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED S/B 609A INSPECTION, FOUND FLIGHT STATION PRESSURE DECK LOWER BEAM CAP CRACKED APPROX 2.0 INCHES AT FS 130, LBL 40. REPAIRED PER LAC DWG NR 841292. M-54 NR 56. 2 L 7 4 4T 4A22 1998061200679 19980612 00679 SO 1998 6 12 RAAA98E4015 1 19980603 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 152 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 2 CHECK, FOUND PILOT'S SEAT, AFT TRACK CRACKED APPROX 1.2 INCH AT UPPER LEG, FS 152, LBL 31. REPLAC ED TRACK PER SRM 51-2-12. M-54 NR 90. 2 L 7 4 4T 4A22 1998061200680 19980612 00680 SO 1998 6 12 RAAA98E4016 1 19980603 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 863 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 9744C 188C1140 DURING SCHEDULED NR 2 CHECK, FOUND FS 863 FRAME CORRODED AT STR 42 TO 46. REPAIRED PER SRM 53-2-3. M-54 NR 151. 2 L 7 4 4T 4A22 1998061200681 19980612 00681 SO 1998 6 12 RAAA98E8016 1 19980604 A 3350 240998C RELAY LKHEED 188 188C 5262604 SO BS 530 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EXTERNAL EMERGENCY LIGHTS WOULD NOT EXTINGUISH ON SERVICE CHECK. CHANGED K106M RELAY DUE FAILED AND EXTERNAL EMERGENCY LIGHT BATTERY DUE DISCHARGED. 2 L 7 4 4T 4A22 1998061200682 19980612 00682 SO 1998 6 12 RAAA98E8017 1 19980604 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FWD LT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT DUE FAILED. 2 L 7 4 4T 4A22 1998061200683 19980612 00683 NM 1998 6 12 UPS98226858 1 19980610 A 2120 CONTROL VALVE BOEING 727 72725C 138400H NM LT PACK FAILED A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 01 933UP 19857 INSPECTION TYPE N/A, LEFT PACK TRIPPED OFF LIGHT ON LANDING ROLLOUT. LEFT PACK SWITCH DID NOT TURN OFF, WHITE SMOKE ENT ERED COCKPIT. LOST CONTROL OF PACK EVEN WITH SWITCH OFF. LEFT PACK VLV STUCK OPEN, CYCLED VLV TO CLOSED POSITION AND I TEM DEFERRED PER MEL 21-2-2 ACCOMPLISHED DMP PROCEDURES 21-2-1. 2 L 7 3 4F A3WE 1998061200684 19980612 00684 NM 1998 6 12 UPS98226859 1 19980529 A 5230 6518625152 SKIN BOEING 727 72725C 138400H NM CARGO DOOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, NUMEROUS SCRATCHES AND GOUGES OUTSIDE LIMITS IN AFT CARGO DOOR ALSO PATCHES ON INSIDE SKIN. DOOR REP LACED IAW MM 52-30-00 REF N/R 704898 FOR RIG AND OPERATION OF DOOR. 2 L 7 3 4F A3WE 1998061200685 19980612 00685 NM 1998 6 12 UPS98226860 1 19980527 A 5320 WEB BOEING 727 72725C 138400H NM CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, CRACK IN WEB AFT OF AFT CARGO DOOR CUTOUT EXTENDING BEYOND EXISTING REPAIR. REMOVED EXISTING PATCH AND REPAIRED WEB. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998061200686 19980612 00686 NM 1998 6 12 UPS98226861 1 19980525 A 5330 SKIN BOEING 727 72725C 138400H NM BS 188 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, SUSPECT SKIN CRACKS BS 188 WL 207 RT SIDE. AREA REPAIRED PER SRM 53-30-3 FIG 3 AT BS 188 WL 207 RT. 2 L 7 3 4F A3WE 1998061200687 19980612 00687 NM 1998 6 12 UPS98226862 1 19980527 A 5280 SKIN BOEING 727 72725C 138400H NM LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, LT WING MLG WING DOOR HAS CRACK ON EXISTING REPAIR ON OUTER SKIN. HIFEC INSPECTION CARRIED OUT IAW B 727 NDT MANUAL D6-48875 PART 6 51-00-00 FIG 4 AND 16 CRACKS CONFIRMED AND STOPPED DRILL. 2 L 7 3 4F A3WE 1998061200688 19980612 00688 NM 1998 6 12 UPS98226863 1 19980529 A 5311 FRAME BOEING 727 72725C 138400H NM FRAME 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, OUTER CHORD OF FRAME 400 CRACKED AT STR 20 TO 21. FRAME REPAIR CARRIED OUT IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1998061200689 19980612 00689 NM 1998 6 12 UPS98226864 1 19980526 A 5330 SKIN BOEING 727 72725C 138400H NM BS 243 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, CRACKS IN FUSELAGE SKIN BS 243.7 BETWEEN 212 AND 215 RT. AREA REPAIRED PER SRM 53-30-3 FIG 3 AT BS 2 43.7 BETWEEN 212 AND 215 RT. 2 L 7 3 4F A3WE 1998061200690 19980612 00690 NM 1998 6 12 UPS98226865 1 19980528 A 7120 MOUNT BOEING 727 72725C 138400H NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, NR 3 ENG PITTING CORROSION ON BORE OF HOLES ON FWD ENG MOUNT FITTING = 2 O/B HOLES. REPAIR CARRIED O UT PER SRS EO 98-14-002 AND 98-14-005 REF CPT 049-8 AND 052-98 FOR BUSHING MANUFACTURE. 2 L 7 3 4F A3WE 1998061200691 19980612 00691 NM 1998 6 12 UPS98226866 1 19980528 A 7120 MOUNT BOEING 727 72725C 138400H NM NR 1 ENGINE CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, NR 1 ENG PITTING CORROSION ON BORE OF HOLES FWD ENG MOUNT FITTING TWO O/B HOLES AND I/B AFT HOLE. RE PAIR CARRIED OUT PER SRS EO 98-14-003 AND 98-14-004 REF CPT 006/98 056/98 AND 055/98 FOR BUSHING MANUFACTURE. 2 L 7 3 4F A3WE 1998061200692 19980612 00692 NM 1998 6 12 UPS98226867 1 19980529 A 5320 SILL BOEING 727 72725C 138400H NM BS 620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, CREASE BEAM SILL CHORD WEB CRACKED AT BS 620 LT. WEB REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998061200693 19980612 00693 WP 1998 6 12 UPS98826868 1 19980610 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 805UP 46117 INSPECTION TYPE-N/A, EEL BATTERY VOLTAGE IS 19 VOLTS. REMOVED AND REPLACED EEL BATT PACK IAW MM 33-50-33 (P/N F5708458- 503) (S/N ED2) ON, (S/N FTL004) OFF. 2 L 7 4 4F RT 4A25 1998061200694 19980612 00694 EU 1998 6 12 98FDEA00396 1 19980609 A 3260 GEAR LIGHT AIRBUS 300 A300F4605R 3930327 EU NLG MALFUNCTION A FDEA O OTHER P NO WARNING INDICATION LD LANDING 1 SO 25 662FE 761 ON LANDING NOSE GEAR LIGHT ON FRONT PANEL DIDN'T ILLUMINATE WHEN GEAR WAS LOWERED. OVERHEAD LIGHTS WERE NORMAL. SWITCH ED TO STEM 2 WITH NO HELP. LIGHT TEST INDICATED TEST WAS GOOD. REMOVED AND REPLACED 40GB (P/N 141FL01D3) AND NOSE GEAR LIGHT ON FRONT PANEL INDICATES GREEN GEAR DOWN AND LOCKED. OK FOR SERVICE REF M/M 32-61-00-05. 2 L 7 2 4F RT A35EU 1998061200695 19980612 00695 WP 1998 6 12 MWEA98644 1 19980609 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 THE EMERGENCY CEILING LIGHTS WOULD NOT COME ON DURING TEST. MTC REMOVED AND REPLACED EMERGENCY CEILING BATTERY PACK. 2 L 7 2 4F A6WE 1998061200696 19980612 00696 WP 1998 6 12 MWEA98645 1 19980609 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 THE EMERGENCY OVERWING EXIT LIGHTS WENT OUT AFTER A 14 HOUR CHARGE. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998061200697 19980612 00697 NM 1998 6 12 SCNA98055 1 19980606 A 3010 GASKET BOEING 727 727225 1384077 NM NR 3 STRUT LEAKING A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 282SC 22558 ENGINE NUMBER THREE STRUT OVERHEAT LIGHT ILLUMINATED ON CLIMBOUT. RAN COM CHECKLIST. LIGHT EXTINGUISHED WHEN THE NUMBE R THREE ENGINE THRUST LEVER WAS RETARDED. RETURNED TO IAH. FOUND A GASKET ON THE WING ANTI-ICE HIGH PRESSURE SHUTOFF V ALVE LEAKING. REMOVED AND REPLACED VALVE GASKET IN ACCORDANCE WITH MAINTENANCE MANUAL 301111. RAN ENGINE AND FUNCTIONA LLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998061200698 19980612 00698 WP 1998 6 12 RRXA98225 1 19980604 A 5753 NUT DOUG DC8 DC8F54 3021926 WP TE FLAP TRACK MISSING A RRXA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 15 992CF 45884 FLAP SPLIT ON APPROACH. A/C ROLLS TO LEFT AT 10 DEG PERFORMED A ZERO FLAP LNDG. REPLACED MISSING NUTS ON FLAP TRACK ON LEFT FLAP, OPS CHECKS NORMAL, NO SPLIT NOTED ON GROUND OPS CHECK. 2 L 7 4 4F 4A25 1998061200699 19980612 00699 NE 1998 6 12 ARWA980602 2 19980606 A 7321 FUEL CONTL UNIT DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE FAILED A A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 1804 45896 AIR TURNBACK, AFTER DEPARTURE NR 3 ENGINE UNSPOOLED AND WHEN POWER LEVER WAS ADVANCED ENGINE WOULD NOT ACCELERATE. RETU RNED TO TUS WITHOUT INCIDENT. INSPECTED ENGINE INLET, TAILPIPE, OIL AND FUEL FILTERS. NO DEFECTS NOTED. REMOVED AND R EPLACED FCU, MAIN OIL PUMP AND P AND D VALVE. ENGINE DOES NOT ACCELERATE ABOVE IDLE. THREE ENGINE FERRIED TO MIA FOR E NGINE CHANGE CAUSE OF FAILURE UNDER INVESTIGATION. 2 L 7 4 4F 4 F 4A25 1E8 1998061200700 19980612 00700 NM 1998 6 12 VNAA9806004 1 19980606 A 7603 GATE LOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT POWER LEVER LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 433JS 3047 THE LEFT HAND POWER LEVER WOULD NOT MOVE PAST THE FLIGHT IDLE POSITION WHEN SELECTED, DURING THE TAKEOFF. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBRICATED THE POWER GATE LOCK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-04. OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998061600003 19980616 00003 WP 1998 6 16 VJ9800164 1 19980424 A 5330 1A331481 SKIN DOUG DC9 DC932 3022066 WP BS 944 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 IN AFT CARGO COMPARTMENT, FOUND CORROSION OF SKIN ADJACENT TO STR 28 L I/B SIDE AT STA 944. MECH REMOVED CORROSION, FOU ND AREA TO BE OUT OF LIMITS MORE THAN 50 PERCENT MATERIAL LOSS IAW DC-9 53-01 FIG. FABBED DOUBLER, DRILLED AND COUNTERS UNK, DEBURRED HOLES, TREATED, PRIMED AND INSTALLED DOUBLER IAW DC-9 SRM 53-04 FIG 38 (MAT 2024 T3 .032 5 BY 5.5). 2 L 7 2 4F A6WE 1998061600004 19980616 00004 WP 1998 6 16 VJ9800167 1 19980423 A 5330 1A20920130921 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 MATERIAL THICKNESS OF FUSELAGE SKIN AT ADF ANTENNA IS BEYOND LIMITS SRM 51-01 LIMITS AFTER CORROSION REMOVAL. REMOVED O VERHEAD CEILING PANELS, A/C DUCTS FOR ACCESS TO THE ANTENNA AREA. REPAIRED CORRODED SKIN AREA UNDER AFT ADF LOOP ANTENN A IAW DC-9 53-04 FIG 29, REINSTALLED AC DUCT AND CEILING PANELS IAW DC-9 MM 25-22-0, 25-28-0, 20-11-0. (DOUBLER 28.5 BY 16) FINGER DOUBLERS 28.5 BY 3. 2 L 7 2 4F A6WE 1998061600005 19980616 00005 WP 1998 6 16 VJ9800168 1 19980423 A 5313 S27779225 STRINGER DOUG DC9 DC932 3022066 WP BS 370-389 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 FWD CARGO PIT AT STA 380 28L IS CORRODED BETWEEN STA 370-389. REMOVED CORROSION IAW DC-9 51-10-3, FOUND TO BE BEYOND LI MITS MATERIAL LOSS 75 PERCENT. REMOVED LONGERON 28L FROM STA 345-398. DRILLED AND DEBURRED NEW LONGERON 28L. TREATED, PRIMED AND INSTALLED IAW DC-9 SRM 51-30-2, AND 51-10-4. UPON ARRIVAL OF THE LONGERON, FOUND SHEAR TIE CRACKED AT STA 3 51, FABRICATED REPAIR, DRILLED DEBURRED SHEAR TIE REPAIR, TREATED, PRIMED AND INSTALLED IAW DC-9 SRM 51-10-4, 51-10-3 AN D 51-30-2. (DIMENSIONS 3 BY 14.5 BY 1.75 BY .875, 3.875 BY .875. 2 L 7 2 4F A6WE 1998061600006 19980616 00006 WP 1998 6 16 VJ9800169 1 19980423 A 5720 59124371 DOUBLER DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 LEFT WING LOWER MLG DOUBLER HAS SEVERAL BLEND OUTS BEYOND LIMITS. REMOVED LEFT 1WR MLG DOUBLER IAW DC-9 SRM 51-30-5. R ECEIVED NEW DOUBLER, DRILLED, COUNTERSUNK, AND DEBURRED NEW MLG DOUBLER IAW DC-9 SRM 51-10-3, INSTALLED AND SEALED NEW MLS DOUBLER IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998061600007 19980616 00007 WP 1998 6 16 VJ9800170 1 19980313 A 2571 1A306501 BATTERY TRAY DOUG DC9 DC932 3022066 WP BATTERY COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 E/E COMP BATTERY TRAY LT SIDE HAS CORROSION. REMOVED CORROSION IAW DC-9 SRM 51-10-3 MATERIAL LOSS WAS FOUND TO BE 100 P ERCENT, OUT OF LIMITS IAW IAW DC-9 SRM 53-01 FIG 1. FABRICATED DOUBLER REPAIR FROM 2004 T3 .875 BY 1.875 X 3.875 IAW DC -9 SRM 53-01 FIG 2. TREATED AND PRIMED IAW 51-10-3, INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F A6WE 1998061600008 19980616 00008 WP 1998 6 16 VJ9800171 1 19980321 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 STATION 996 LOWER WEBS HAVE EXTENSIVE CORROSION THROUGH OUT. LOWER CAP HAS CORROSION. FABRICATED LOWER WEBS FROM 7075 T6 .040 BY 9.5 BY 61 BY 12 BY 22 2 EACH. INSTALLED IAW DC-9 SRM 51-10-4, 51-30-5, AND 51-10-3. 2 L 7 2 4F A6WE 1998061600009 19980616 00009 WP 1998 6 16 VJ9800172 1 19980411 A 5330 1A268001 SKIN DOUG DC9 DC932 3022066 WP BS 522 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 DENT FUSELAGE AT LONG FS 522 2.50 BY 6 BY .0110. REPAIRED IAW EO 98-845, CUT OUT SKIN AT STA 522 L 29R 8.8 BY 5, FABRIC ATED DOUBLER REPAIR FROM 7075 T6 .063, DIMENSIONS 16.5 BY 10 AND FINGER DOUBLERS FROM 7075 T6 .025 DIMENSIONS 17.875 BY 8 BY 5 IAW EO 98-845. TREATED AND PRIMED DOUBLER REPAIR IAW SRM 51-10-3. INSTALLED IAW DC-9 SRM 51-30-2, 51-30-5, AND EO 98-845. 2 L 7 2 4F A6WE 1998061600010 19980616 00010 NE 1998 6 16 DL76L981143 2 19980527 A 7200 ENGINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A DALA A E UNSCHED LANDING ENGINE SHUTDOWN C F.O.D. TO TAKEOFF 1 SO 27 191DN 5873 28448 727655 BIRD STRIKE ON TAKEOFF JFK, APPEARED TO BE RIGHT ENGINE. RETURNED TO JFK. SHUT DOWN ENGINE AFTER LANDING. RT EEC INOP WITH EICAS MSG. BOTH ENGS OPERATED WITHIN NORMAL LIMITS. RADOME AND RT OUTBD FLAP ALSO DAMAGED. ENGINE AND RADOME CH ANGED. A/C TO BE FERRIED TO ATL FOR FLAP REPLACEMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1998061600011 19980616 00011 WP 1998 6 16 CKSA98336 1 19980521 A 2910 HYDRAULIC LINE DOUG DC8 DC8F54 3021926 WP NR 2 ENGINE LEAKING A CKSA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 8052U 46009 DURING CRUISE, LOSS OF HYDRAULIC FLUID ON QUANTITY INDICATOR (5.8 GALLONS). ACCOMPLISHED AIA EMERGENCY PROCEDURES. ON POSTFLIGHT, DISCOVERED NR 2 ENGINE LEAKING HYDRAULIC FLUID. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC LINE. OPS CHECK OK ON ENGINE RUN UP IAW DC8 MM 29-1-7. 2 L 7 4 4F 4A25 1998061600012 19980616 00012 NM 1998 6 16 SPAA9800001 1 19980206 A 3350 8731002511 LIGHT BOEING 737 737297 1384480 NM CABIN INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 725S 22051 DURING SCHEDULED CHECK, THE L1 DOOR INTERNAL EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED. SUBSEQUENT SYSTEM TEST WAS SATISFACTORY PER BMM 335101. 2 L 7 2 4F A16WE 1998061600013 19980616 00013 WP 1998 6 16 VJ9800173 1 19980514 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 294 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 966VV 47168 CORROSION AT FS 294, LONGERON 30. REMOVED CORRODED SECTION OF LONGERON AND REPAIRED PER RES-1-05422. 2 L 7 2 4F A6WE 1998061600014 19980616 00014 WP 1998 6 16 VJ9800174 1 19980522 A 5712 1A3317933178 RIB DOUG DC9 DC932 3022066 WP WS 58.768 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 966VV 47168 LT WING NR 1 SLAT, STA 58.768. VERTICAL ATTACH WEB CRACKED APPROXIMATELY 1 INCH. REMOVED EXISTING REPAIR AND REPAIRED SLAT WEB IAW EO 9-27-003. 2 L 7 2 4F A6WE 1998061600015 19980616 00015 1998 6 16 JBXA980040 4 19980602 A 2210 8220044001 FCP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE E/E COMPT INOPERATIVE A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 573ML 7227 AUTOPILOT FAILED TO ENGAGE IN FLIGHT, HAD FCC INDICATIONS, APC FLASHES, NO FLIGHT DIRECTOR INDICATIONS ON CAPT SIDE AND 1/2 BANK CAME ON. LIGHT ON NAV LT SIDE, RT SIDE ON HEADING MODE, LT SIDE ON SPEED. REMOVED AND REPLACED FCP IAW CRJ MM CHP 22-11-07 OPERATIONAL CK GOOD, NO FAULTS NOTED AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 1998061600016 19980616 00016 WP 1998 6 16 TWAA9806909 1 19980317 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 579-598 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP15 MAINTENANCE CHECK, FOUND CABIN FLOOR MEMBRANE CRACKED BETWEEN STATION 579 AND 598, APPROX 58 INCH RBL, UNDER FWD END OF FLOOR PANEL 43. REPAIRED PER SRM 53-01, FIG 4. (M) 2 L 7 2 4F A6WE 1998061600017 19980616 00017 NM 1998 6 16 VJ9800175 1 19980602 A 2130 PRESSURIZATION BOEING 737 7372L9 1384497 NM CABIN MALFUNCTIONED A ZZDA B EMER. DESCENT O OTHER CR CRUISE 1 SO 15 464AT 21278 AT CRUISE FL 290 HEARD SMALL POP AND NOTICED CABIN ALTITUDE STARTED TO CLIMB. WENT TO STANDBY AND MANUAL, NO HELP. CAB IN STARTED TO CLIMB 4,000 FEET PER MINUTE. EMERGENCY DESCENT ACCOMPLISHED BEFORE CABIN ALTITUDE GOT TO 10,000 FT. PRES SURIZED AIRCRAFT TO 4.5 PSI WITH APU ONLY. COULD NOT DUPLICATE. REF MM 21-31-0. 2 L 7 2 4F RT A16WE 1998061900002 19980619 00002 CE 1998 6 19 98ZZZX2158 1 19980422 A 3213 05411989 GEAR CESSNA 172 172P 2072436 CE RT MLG MISDRILLED A EBVA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 09 5361K 794586 1727480 WHILE COMPLETING SERVICE KIT SK172-37 ON THE AIRCRAFT'S RT MAIN GEAR LEG, IT WAS DECIDED TO CHANGE THE LEG WITH A NEW ON E. INSTALLING THE NEW LEG REVEALED THAT THE BOLT HOLE, FOR MOUNTING THE LEG TO THE AIRFRAME, WAS MISDRILLED AND WOULD N OT ALLOW THE BOLT TO GO COMPLETELY THROUGH THE LEG. ALL ATTEMPTS TO FACILITATE BOLT INSTALL FAILED. NEW LEG WAS RETURN ED TO MANUFACTURER. SUSPECT NEW LEG WAS NOT PROPERLY SET-UP IN JIG WHEN DRILLED AT FACTORY. 1 H 7 1 3O NT 3A12 1998061900012 19980619 00012 CE 1998 6 19 98ZZZX2168 1 19980518 A 2432 4076 BATTERY SAFT BEECH 18 C45H 1151018 CE DC SYSTEM OVERHEAT A KKFA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 231SK KFS119 AF856 WHILE EN ROUTE, A HOT BATTERY LIGHT ILLUMINATED. AIRCRAFT LANDED AT AN ALTERNATE AIRPORT. INVESTIGATION REVEALED ONE B ATTERY WAS OVERHEATED. BATTERY WAS REPLACED. CHARGING SYSTEM AND BATTERY PERFORMANCE WAS CHECKED. 1 L 7 2 3R A765 1998061900014 19980619 00014 EA 1998 6 19 98ZZZX2170 2 19980528 A 8520 CONNECT ROD PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA NR 5 CYLINDER FAILED A WVBA A UNSCHED LANDING E R K VIBRATION/BUFFET PARTIAL RPM/PWR LOSS FLUID LOSS CL CLIMB 1 AL 01 300ED 3821 2024 317852008 RL267268A ON CLIMB-OUT FROM FAI, RIGHT ENGINE FAILED. NR 5 CYLINDER SEPARATED FROM ENGINE, NR 5 CONNECTING ROD BROKEN AT PISTON P IN. CASE RECEIVED MASSIVE DAMAGE. 1 L 7 2 3O 3 O A20SO E14EA 1998061900016 19980619 00016 EA 1998 6 19 98ZZZX2172 2 19980527 A 8520 LW16586 TAPPET CESSNA 172 172N 2072434 CE LYC O320 O320H2AD 41508 EA CAMSHAFT SPALLED A ZWSA K NONE O OTHER IN INSP/MAINT 1 GL 13 733MU 787 17268404 L213376 INSPECTION FOUND SPALLED TAPPET PROBLEM. THE CAMSHAFT WAS IN GOOD SHAPE, BUT DID NEED A REGRIND. 1 H 7 1 3O 3 O NT 3A12 E274 1998061900019 19980619 00019 NM 1998 6 19 VJ9800188 1 19980607 A 2710 65447618 PCU BOEING 737 7372L9 1384497 NM RT AILERON MALFUNCTIONED A ZZDA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 15 737Q 21279 GOING TO RIGHT, AILERON APPEARS TO BE BINDING. FOUND B-SYSTEM HYDRAULICS MALFUNCTION IN AILERON PCU. REMOVED AND REPLA CED PCU. 2 L 7 2 4F RT A16WE 1998061900020 19980619 00020 WP 1998 6 19 VJ9800189 1 19980610 A 2436 939D2171 VOLTAGE REG DOUG DC9 DC932 3022066 WP E/E COMPT FAILED A ZZDA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 15 967VV 47170 NR 1 GENERATOR LIGHT OFF, UNABLE TO START APU INFLIGHT. REPLACED VOLTAGE REGULATOR. 2 L 7 2 4F A6WE 1998061900021 19980619 00021 1998 6 19 MALA976141 2 19980606 A 7261 CHIP DETECTOR SAAB SF340 340B 7860101 EU RIGHT ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 434XJ 434 INFLIGHT THE RIGHT CHIP DETECTOR CAUTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REMOVED RIGHT ENGINE CHIP DETECTOR, INSPECTED DEBRIS AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW GE CT7 MM CHAPTER 72-00-00. RAN ENGINE FOR 15 MINUTES, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998061900022 19980619 00022 SO 1998 6 19 RAAA98E9020 1 19980609 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT LT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998061900023 19980619 00023 NM 1998 6 19 CALA9801000 1 19980610 A 2752 MS9391130ZE SEAL BOEING 727 727224 1384076 NM FLAP ACTUATOR FAILED A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 69736 20665 THE AIRCRAFT LOST A-SYSTEM HYDRAULICS AFTER TAKEOFF. THE HYDRAULIC SWITCHES WERE TURNED OFF BEFORE ALL PRESSURE WAS LOS T. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE OUTBOA RD FLAP HYD DRIVE MOTOR FRONT SEAL BLOWN. THE FLAP HYD DRIVE MOTOR WAS REPLACED. IN ADDITION, BOTH THE NR 1 AND NR 2 E NGINE DRIVEN HYDRAULIC PUMPS WERE REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE HYDRAULIC SYSTEM WAS SERVICED. L EAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1998061900024 19980619 00024 WP 1998 6 19 CALA9801001 1 19980609 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT FLOORBEAM AT BS 996, LBL 18 CORRODED. AN UPPER CAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-0 AND 51-10-1. 2 L 7 2 4F A6WE 1998061900025 19980619 00025 WP 1998 6 19 CALA9801002 1 19980609 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND .5 INCH CRACKS AT SCREW HOLES OF FLOORBOARD NR 51. REPAIRED IAW SRM 53-01, FIGURE 2, PAGE 3. 2 L 7 2 4F A6WE 1998061900026 19980619 00026 WP 1998 6 19 CALA9801003 1 19980609 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A HOLE IN FLOORBOARD PANEL NR 71. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-3, PAGES 15-16, AND 51-30-2, PAGES 1-30. 2 L 7 2 4F A6WE 1998061900027 19980619 00027 WP 1998 6 19 CALA9801004 1 19980609 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 200-244 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD AT STA 200 TO 244 DELAMINATING. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05 , PAGE 122B. 2 L 7 2 4F A6WE 1998061900028 19980619 00028 WP 1998 6 19 CALA9801005 1 19980609 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CRACKS IN LT FLOORBOARD NR 58. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-70-1 , AND 51-70-3, PAGE 1 AND 2. 2 L 7 2 4F A6WE 1998061900029 19980619 00029 WP 1998 6 19 CALA9801006 1 19980609 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 917 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND AFT PIT UPPER FLOORBEAM GOUGED AT STA 917. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED I AW SRM 53-05, FIGURE 86, 51-30-1, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900030 19980619 00030 WP 1998 6 19 CALA9801007 1 19980609 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 589 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN WEB AT STA 589 ON LT SIDE OF FUSELAGE. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 51-30-2, AND 53-10-2. 2 L 7 2 4F A6WE 1998061900031 19980619 00031 WP 1998 6 19 CALA9801008 1 19980609 A 5720 SUPPORT DOUG DC9 DC932 3022066 WP WS 280 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT WING STA 280 FLAP LEADING EDGE SUPPORT CAP CRACKED AND CORRODED. THE SUPPORT CAP WAS REMOVED, A NEW SUPPORT CAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900032 19980619 00032 WP 1998 6 19 CALA9801009 1 19980609 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 207 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LONGERON 5L GOUGED AT STA 207. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1998061900033 19980619 00033 WP 1998 6 19 CALA9801010 1 19980609 A 5712 RIB DOUG DC9 DC932 3022066 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 3 INCH CRACK IN RT WING LEADING EDGE RIB. THE RIB WAS REMOVED AND A NEW RIB WAS FABRICATED AND INSTA LLED IAW SRM 51-30-2 AND 51-00-00. 2 L 7 2 4F A6WE 1998061900034 19980619 00034 WP 1998 6 19 CALA9801011 1 19980609 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 851-870 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND STRAP CORRODED BETWEEN LONGERONS 27L AND 28L AT STA 851 TO 870. THE STRAP WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-2A, 51-10-04, 51-10-3, 51-30-2, AND 53-01. 2 L 7 2 4F A6WE 1998061900035 19980619 00035 WP 1998 6 19 CALA9801012 1 19980609 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 260 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT OUTBOARD SEAT TRACK CORRODED AT STA 260. THE CORRODED SECTION OF SEAT TRACK WAS CUT OUT, A NEW REPA IR SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1998061900036 19980619 00036 WP 1998 6 19 CALA9801013 1 19980609 A 5280 HINGE DOUG DC9 DC932 3022066 WP RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .375 INCH CRACK IN AFT LOBE OF RT MLG DOOR UPPER HINGE. A NEW HINGE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-4. 2 L 7 2 4F A6WE 1998061900037 19980619 00037 WP 1998 6 19 CALA9801014 1 19980609 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP RT NLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 INCH CRACK IN AFT CHANNEL OF RT NLG WHEEL WELL FORWARD FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIGURE 2. TWO ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, 51-30-2, AND 51-10-6. 2 L 7 2 4F A6WE 1998061900038 19980619 00038 WP 1998 6 19 CALA9801015 1 19980610 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 351 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOOR SUPPORT CRACKED IN FORWARD PIT AT STA 351 ABOVE LONGERON 26R. THE FLOOR SUPPORT WAS REMOVED, A R EPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263 AND SRM 51-10-3. 2 L 7 2 4F A6WE 1998061900039 19980619 00039 WP 1998 6 19 CALA9801016 1 19980610 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 240 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 240. THE SEAT TRACK WAS REMOVED AND A NEW SECTION OF SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-10-3, AND 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1998061900040 19980619 00040 WP 1998 6 19 CALA9801017 1 19980610 A 5210 ANGLE DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN L-ANGLE ON AFT ENTRY DOOR. THE ANGLE WAS REMOVED, A NEW ANGLE WAS FABRICATED AND INS TALLED IAW SRM 53-01, FIGURE 2, 51-10-3, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900041 19980619 00041 WP 1998 6 19 CALA9801018 1 19980610 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1104 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .25 INCH CRACK AT FASTENER IN FRAME AT STA 1104, LONGERON 3R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1998061900042 19980619 00042 WP 1998 6 19 CALA9801019 1 19980611 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 908 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RIGHT OUTBOARD SEAT TRACK CORRODED AT STA 908. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1998061900043 19980619 00043 WP 1998 6 19 CALA9801020 1 19980611 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 980-996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT AFT LAV FLOOR WEB CORRODED AT BS 980 TO 996, LBL 18. THE FLOOR WEB WAS REMOVED, A REPAIR WAS FABRIC ATED AND INSTALLED IAW SRM 51-10-4, 51-30-2, 51-10-3, AND 51-30-1. 2 L 7 2 4F A6WE 1998061900044 19980619 00044 WP 1998 6 19 CALA9801021 1 19980611 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 332 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND THREE .5 INCH CRACKS IN FORWARD PIT RT FLOOR SUPPORT AT STA 332 ABOVE LONGERON 29R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998061900045 19980619 00045 WP 1998 6 19 CALA9801022 1 19980611 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CORROSION AROUND RIVETS IN WEB AT STA 218, STRINGER 18R. THE WEB WAS REMOVED, A REPAIR WEB WAS FABRICA TED AND INSTALLED IAW SRM 51-10-3, 51-10-2, 51-10-4, 51-30-2, AND 51-30. 2 L 7 2 4F A6WE 1998061900046 19980619 00046 EU 1998 6 19 QXEA9800782 1 19980610 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 ROW 8 LEFT SIDE EMERGENCY EXIT LIGHT OUT. MAINTENANCE RELAMPED AND OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998061900047 19980619 00047 EU 1998 6 19 QXEA9800783 1 19980610 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 EMERGENCY EXIT COVER SAFETY WIRE BROKEN. MAINTENANCE REPLACED BREAK-AWAY WIRE AS REQUIRED. 2 L 7 2 4F RT A20EU 1998061900048 19980619 00048 EU 1998 6 19 QXEA9800784 1 19980608 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 EMERGENCY EXIT LIGHT AT ROW 8 OUT. MAINTENANCE RELAMPED AND OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998061900049 19980619 00049 EU 1998 6 19 QXEA9800785 1 19980609 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 ROW 1 AISLE EMERGENCY EXIT LIGHT OUT. MAINTENANCE RELAMPED AND OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998061900050 19980619 00050 EU 1998 6 19 QXEA9800746 1 19980524 A 3350 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 UNDER SEAT BATTERY PACKS FOR EMERGENCY LIGHT MISSING. REPLACED PACKS AND OPS CHECKED GOOD. 2 L 7 2 4F RT A20EU 1998061900051 19980619 00051 EU 1998 6 19 QXEA9800747 1 19980526 A 2560 LATCH FOKKER F28 F28MK4000 4990810 EU COCKPIT OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 ESCAPE SLIDE DOES NOT LATCH PROPERLY TO FLOOR. REPOSITIONED LATCH RECEPTICLE, OPS CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998061900052 19980619 00052 EU 1998 6 19 QXEA9800748 1 19980508 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT FIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 LEFTHAND FUSE TO VERTICAL FIN CONNECTION ANGLE IS CRACKED AT THE 50 PERCENT SPAR LOCATION. REPAIRED IAW FOKKER SRM 55-3 1-01, PAGE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998061900053 19980619 00053 EU 1998 6 19 QXEA9800749 1 19980509 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOORWAY DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 THERE IS A 1 X .100 DENT 4.5 FORWARD OF THE RIGHTHAND CORNER OF THE 41A DOOR OPENING. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1. 2 L 7 2 4F RT A20EU 1998061900054 19980619 00054 EU 1998 6 19 QXEA9800750 1 19980512 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CRACKED FRAME CASTELLATION AT FRAME 17565 ABOVE STRINGER 21A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1998061900055 19980619 00055 EU 1998 6 19 QXEA9800751 1 19980514 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 22293 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 FRAME 22293 CRACKED AT AFT END OF STRINGER 53A. REPAIRED IAW HORIZON AIR EA 4-53-415 AND INSTALLED IAW FOKKER SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1998061900056 19980619 00056 EU 1998 6 19 QXEA9800752 1 19980524 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 FRAME CASTELLATION CRACKED ON FRAME 20075 BETWEEN STRINGERS 39 AND 40 ADJACENT TO PREVIOUSLY STOP DRILLED CRACK. REPAIR ED IAW HORIZON AIR EA 4-53-447 STEP 7 AND FOKKER SRM 51-31-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 1998061900057 19980619 00057 EU 1998 6 19 QXEA9800753 1 19980524 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 FRAME CASTELLATION CRACKED PAST STOP DRILL ON FRAME 20075 BETWEEN STRINGER 35 AND 36. REPAIRED IAW HORIZON AIR EA 4-53- 447, STEP 2. 2 L 7 2 4F RT A20EU 1998061900058 19980619 00058 EU 1998 6 19 QXEA9800754 1 19980506 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 THERE ARE 2 DEEP CHAFE MARKS AT RIGHTHAND SPEEDBRAKE INNER SKIN APPROXIMATELY 28 DOWN FROM TOP AFT CORNER. REPAIRED IAW HORIZON AIR EA 4-53-421. 2 L 7 2 4F RT A20EU 1998061900059 19980619 00059 EU 1998 6 19 QXEA9800755 1 19980506 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 THERE IS A DEEP CHAFE MARK AT TOP AFT CORNER OF THE RIGHTHAND SPEEDBRAKE INNER SKIN. REPAIRED IAW HORIZON AIR EA 4-53-4 21. 2 L 7 2 4F RT A20EU 1998061900060 19980619 00060 EU 1998 6 19 QXEA9800756 1 19980506 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 THE RIGHTHAND SPEED BRAKE INNER SKIN IS COMING LOOSE AT THE T/E OF THE SPEED BRAKE. REPAIRED IAW HORIZON AIR EA 4-53-42 1. 2 L 7 2 4F RT A20EU 1998061900061 19980619 00061 EU 1998 6 19 QXEA9800757 1 19980513 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 THE RIGHTHAND SPEED BRAKE HAS A DENT ON THE BOTTOM 15 BACK FROM THE LEADING EDGE, DENT MEASURES 3 X 1.5 X .125. REPAIRE D IAW FOKKER SRM 53-01-01 PAGE 8, PARAGRAPH 5. 2 L 7 2 4F RT A20EU 1998061900062 19980619 00062 EU 1998 6 19 QXEA9800758 1 19980524 A 5530 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 67-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 FRAME 67-2 CRACKED AT RIGHTHAND SIDE OF VERTICAL FIN BASE RIB WHERE ATTACHES TO COMPOSITE TAIL CONE. STOP DRILLED BUT D AMAGE EXCEEDS 1.02 MAXIMUM CRACK LIMIT. REPAIRED IAW HORIZON AIR EA 4-53-430. 2 L 7 2 4F RT A20EU 1998061900063 19980619 00063 EU 1998 6 19 QXEA9800759 1 19980506 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 HOLE IN FUSELAGE SKIN AFT OF OBLIQUE FRAME 50-2 BETWEEN STRINGER 66 AND 70. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, F IGURE 1. 2 L 7 2 4F RT A20EU 1998061900064 19980619 00064 EU 1998 6 19 QXEA9800760 1 19980521 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 THE RIGHTHAND SPEED BRAKE HAS A DENT ON THE BOTTOM 18 BACK FROM THE LEADING EDGE, DENT MEASURES 3 X 1.5 X .125. REPAIRE D IAW HORIZON AIR EA 4-53-31A. 2 L 7 2 4F RT A20EU 1998061900065 19980619 00065 EU 1998 6 19 QXEA9800761 1 19980515 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CLIP AT OBLIQUE FRAME 16-2 AFT SIDE BETWEEN STRINGER 40 AND 41 IS CRACKED IN RADIUS. REPAIRED IAW FOKKER SRM 53-11-05, PAGE 63, FIGURE 602 AND 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998061900066 19980619 00066 EU 1998 6 19 QXEA9800762 1 19980506 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 LEFT VERTICAL STAB CONNECTION ANGLE AT INTERMEDIATE SPAR 1 (32 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, P AGE 2, FIGURE 1. 2 L 7 2 4F RT A20EU 1998061900067 19980619 00067 EU 1998 6 19 QXEA9800763 1 19980515 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 RIGHT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR (16 PERCENT) IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, F IGURE 1. 2 L 7 2 4F RT A20EU 1998061900068 19980619 00068 EU 1998 6 19 QXEA9800764 1 19980511 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 AFT VERTICAL STAB CONNECTION ANGLE AT FRONT SPAR IS CRACKED AND MISSING RIVET HEAD. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1. 2 L 7 2 4F RT A20EU 1998061900069 19980619 00069 EU 1998 6 19 QXEA9800765 1 19980508 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 LEFT VERTICAL STAB CONNECTION ANGLE AT REAR SPAR IS CRACKED. REPAIRED IAW FOKKER SRM 55-31-00, PAGE 2, FIGURE 1. 2 L 7 2 4F RT A20EU 1998061900070 19980619 00070 EU 1998 6 19 QXEA9800766 1 19980511 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 THERE IS A BROKEN/CRACKED OUT RIB (NR 5) AT THE LEADING EDGE OF THE RUDDER. REPAIRED IAW FOKKER SRM. 2 L 7 2 4F RT A20EU 1998061900071 19980619 00071 EU 1998 6 19 QXEA9800768 1 19980507 A 2730 BUSHING FOKKER F28 F28MK4000 4990810 EU ELEVATOR OUT OF POSITION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 BUSHING HITS HOUSING WHERE ACTUATING LEVER IS ATTACHED. REPAIRED IAW HORIZON AIR EA 4-27-37. 2 L 7 2 4F RT A20EU 1998061900072 19980619 00072 EU 1998 6 19 QXEA9800769 1 19980518 A 2770 BOLT FOKKER F28 F28MK4000 4990810 EU GUSTLOCK DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 GUSTLOCK HOUSING LEVER FORWARD MOUNT BOLT HAS HEAD SHAVED OFF AT LEAST 25 PERCENT. REPAIRED IAW HORIZON AIR EA 4-55-67. 2 L 7 2 4F RT A20EU 1998061900073 19980619 00073 EU 1998 6 19 QXEA9800770 1 19980511 A 5730 BRACKET FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 BRACKET CRACKED AT 11:00 POSITION FROM UPPER LARGE BOLT HOLE INSIDE PANEL 82X. REPAIRED IAW FOKKER SRM 51-31-05. 2 L 7 2 4F RT A20EU 1998061900074 19980619 00074 EU 1998 6 19 QXEA9800771 1 19980513 A 5720 BRACKET FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 CRACK FROM UPPER BOLT HOLE ON BRACKET INSIDE PANEL 81X. REPAIRED IAW FOKKER SRM 51-31-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 1998061900075 19980619 00075 EU 1998 6 19 QXEA9800772 1 19980526 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP VANE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 RIGHTHAND WING OUTBOARD FLAP VANE HAS A DEEP GOUGE 2 INCHES LONG, ON LOWER SURFACE AT APPROXIMATELY STATION 7306. REPAI RED IAW HORIZON AIR EA 4-57-120. 2 L 7 2 4F RT A20EU 1998061900076 19980619 00076 EU 1998 6 19 QXEA9800773 1 19980513 A 5720 LUG FOKKER F28 F28MK4000 4990810 EU LT MLG CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 AFT GEAR LUG ON WING FOR LEFTHAND MLG STRUT IS CHAFED AND CORRODED. REPAIRED IAW HORIZON AIR EA 4-57-113. 2 L 7 2 4F RT A20EU 1998061900077 19980619 00077 EU 1998 6 19 QXEA9800774 1 19980522 A 5751 SKIN FOKKER F28 F28MK4000 4990810 EU LT AILERON DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 LEFTHAND AILERON LOWER SKIN DAMAGED AT INBOARD HINGE ARM OPENING. REPAIRED IAW HORIZON AIR EA 4-27-45. 2 L 7 2 4F RT A20EU 1998061900078 19980619 00078 EU 1998 6 19 QXEA9800775 1 19980430 A 5280 SKIN FOKKER F28 F28MK4000 4990810 EU RT MLG DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 RIGHTHAND INBOARD GEAR DOOR IS CRACKED THROUGH THREE RIVETS ALONG THE FORWARD RIVET LINE OUTER SKIN SURFACE. REPAIRED I AW HORIZON AIR EA 4-53-23B. 2 L 7 2 4F RT A20EU 1998061900079 19980619 00079 EU 1998 6 19 QXEA9800776 1 19980521 A 5743 STRAP FOKKER F28 F28MK4000 4990810 EU BS 3310 MISALIGNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 478US 11227 LEFTHAND STATION 3310 BUTTSTRAP FOURTH HOLE ABOVE TURBULATOR STRIP INBOARD SIDE IS MISALIGNED BY APPROXIMATELY HALF OF S CREW HOLE. REPAIRED IAW FOKKER SRM 57-20-01, PAGE 402 TO 410, PARAGRAPH 3C-3E AND HORIZON AIR EA 4-57-117. 2 L 7 2 4F RT A20EU 1998061900080 19980619 00080 WP 1998 6 19 ABXA9800499 1 19980610 A 5250 5956574275 DOOR DOUG DOUG DC9 DC931 3022065 WP COCKPIT UNSERVICEABLE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 908AX 47008 COCKPIT ENTRY DOOR WAS DIFFICULT TO OPEN AND CLOSE. REPLACED COCKPIT ENTRY DOOR, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998061900081 19980619 00081 WP 1998 6 19 ABXA9800489 1 19980605 A 5730 576985915 SKIN DOUG DOUG DC8 DC863F 302198F WP WS 251 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE UPPER SKIN INTERNAL DOUBLER AT STATION XS 251 CRACKED. REPAIRED IAW DACO DWG 5769759 AND DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1998061900082 19980619 00082 WP 1998 6 19 ABXA9800490 1 19980429 A 5712 5769496 RIB DOUG DOUG DC8 DC863F 302198F WP WS 347.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 347.75 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DRAWING KO5056. 2 L 7 4 4F 4A25 1998061900083 19980619 00083 WP 1998 6 19 ABXA9800491 1 19980504 A 5320 37502571 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LONGERON 31L SPLICE BETWEEN STATION 440 TO 460 IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998061900084 19980619 00084 WP 1998 6 19 ABXA9800492 1 19980429 A 5712 5769496 RIB DOUG DOUG DC8 DC863F 302198F WP WS 448.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XS 448.50 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056. 2 L 7 4 4F 4A25 1998061900085 19980619 00085 WP 1998 6 19 ABXA9800493 1 19980428 A 5312 46143971 BULKHEAD FITTING DOUG DOUG DC8 DC863F 302198F WP BS 70 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STATION 70 BULKHEAD FORWARD SIDE LONGERON 31R INBOARD FITTING HAS HEAVY CORROSION ON LOWER FLANGE BELOW BOLT HEAD. REPL ACED FITTING IAW SRM 51-1-21 AND DWG 4614397. 2 L 7 4 4F 4A25 1998061900086 19980619 00086 WP 1998 6 19 ABXA9800494 1 19980428 A 5720 5769948 ANGLE DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 THE LEFT OUTBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM END. REPAIRED IAW DC8 SRM 51-1-21 AND 57-3-3. 2 L 7 4 4F 4A25 1998061900087 19980619 00087 WP 1998 6 19 ABXA9800495 1 19980428 A 5712 5769496 RIB DOUG DOUG DC8 DC863F 302198F WP WS 446.651 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT AFT UPPER END. REPAIRED IAW DWG K05056. 2 L 7 4 4F 4A25 1998061900088 19980619 00088 WP 1998 6 19 ABXA9800496 1 19980606 A 5730 5769859 SKIN DOUG DOUG DC8 DC863F 302198F WP WS 197 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE SKIN UPPER SURFACE AT STATION XFS 197 IS CRACKED AT A FASTENER HOLE. REPAIRED LEADING EDGE SKIN IAW DWG 5769859 AND DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998061900089 19980619 00089 WP 1998 6 19 ABXA9800497 1 19980606 A 5730 5643000 SKIN DOUG DOUG DC8 DC863F 302198F WP WS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING UPPER TRAILING EDGE SKIN STATION XRS 160 AT THE REAR SPAR IS CRACKED IN 2 PLACES. REPAIRED SKIN IAW DC8 SRM 5 7-2-0. 2 L 7 4 4F 4A25 1998061900090 19980619 00090 WP 1998 6 19 ABXA9800498 1 19980606 A 5720 5769859 ANGLE DOUG DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING INBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998061900091 19980619 00091 NM 1998 6 19 DL72K981207 1 19980607 A 5320 DOUBLER BOEING 727 727232 1384082 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 471DA DL471 20748 DURING ACCOMPLISHMENT OF SI 4-72762-12 ME-03, A CRACK WAS FOUND IN EXISTING DOUBLER. A REPAIR IS TO BE ACCOMPLISHED PER ERA 364990-14 FILE CODE 53-31-20. 2 L 7 3 4F A3WE 1998061900092 19980619 00092 NM 1998 6 19 DL733981208 1 19980529 A 5312 65163007 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303WA 23183 DURING INSPECTION, FOUR CRACKS WERE FOUND IN THE BLKHD WEB AT BS 178. CRACKS WERE LOCATED BETWEEN WL 180 AND WL 210 AND BETWEEN RBL 5 AND LBL 5. REPAIRED PER ERA 331749-14. 2 L 7 2 4F RT A16WE 1998061900093 19980619 00093 NM 1998 6 19 DL757981209 1 19980605 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681.8 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 FLOORBEAM BS 1681.8 WAS FOUND WITH CORROSION DAMAGE ALONG ENTIRE LENGTH OF UPPER CAP. REPAIRED PER ERA 364763-14. 2 L 7 2 4F RT A2NM 1998061900094 19980619 00094 NM 1998 6 19 DL757981210 1 19980605 A 5330 146N37805 SKIN BOEING 757 757232 1384965 NM BS 1690 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 618DL 22908 A DENT WAS FOUND IN THE FUSELAGE SKIN AT APPROX BS 1690 JUST BELOW THE LAP JOINT AT STGR 20R. REPAIRED PER ERA 364767-1 4. 2 L 7 2 4F RT A2NM 1998061900095 19980619 00095 NM 1998 6 19 DL767981211 1 19980608 A 5330 143T13522 SKIN BOEING 767 767232 1385132 NM BS 632 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 109DL 22221 FUSELAGE SKIN WAS FOUND WITH A GOUGE LOCATED AT BS 632 BETWEEN STRINGERS 30R AND 31R. REPAIRED PER ERA 331774-14 REV B. 2 L 7 2 4F RT A1NM 1998061900096 19980619 00096 NM 1998 6 19 DL767981212 1 19980605 A 5730 111T30001 SKIN BOEING 767 767232 1385132 NM CENTER WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 109DL 22221 CORROSION WAS FOUND AROUND SEVERAL FASTENER HOLES WHERE THE FWD AND AFT CTR WING UPR SKIN ATTACHES TO STGR U-17 BETWEEN LBL 74 AND LBL 90. A SECTION AFT OF THE AFT UPPER WING SKIN WAS REMOVED. REPAIRED PER ERA 331767-14. 2 L 7 2 4F RT A1NM 1998061900097 19980619 00097 NM 1998 6 19 DL767981213 1 19980605 A 5412 331T15361 BULKHEAD BOEING 767 767232 1385132 NM NR 2 PYLON DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 109DL 22221 BULKHEAD AT NAC STA 163.5 ON THE RT OF PYLON HAD TOOLING DAMAGE THAT NECESSITATED PART REPLACEMENT. NO REPLACEMENT PART AVAILABLE, A NEW PART WAS FABRICATED. PART FABRICATED PER ERA 331773-14. 2 L 7 2 4F RT A1NM 1998061900098 19980619 00098 NM 1998 6 19 DL72W981214 1 19980608 A 5311 6516326 FRAME BOEING 727 727247 138408F NM BS 784 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FS 784 FRAME ON THE LT SIDE HAD TWO CRACKS AT THE SECOND HOLE UP FROM THE FLOOR LINE. REPAIRED PER ERA 331783-14AD. 2 L 7 3 4F A3WE 1998061900099 19980619 00099 NM 1998 6 19 DL757981215 1 19980608 A 5330 146N331010 SKIN BOEING 757 757232 1384965 NM BS 1433 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 629DL 22919 DENT WAS FOUND OUT OF LIMITS AT STA 1433 2 INCHES BELOW THE S-14L LAP SPLICE. DAMAGE REMOVAL RESULTED IN A 1 INCH SQUAR E CUTOUT. REPAIR DOUBLER AND FILLERS WERE INSTALLED PER ER/A 364966-14. 2 L 7 2 4F RT A2NM 1998061900100 19980619 00100 NM 1998 6 19 DLM90981216 1 19980602 A 5320 591214185 ANGLE DOUG MD90 MD9030 3023690 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 913DN 53393 LT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND CRACKED AT FS 940. THE CRACK MEASURED APPROXIMATELY 1 INCH LE NGTH AND EXTENDED FWD/AFT IN THE FLANGE COMMON TO THE FUSELAGE BODY. THE CRACK WAS REPAIRED BY THE INSTALLATION OF A RE PAIR DOUBLER PER ER/A 364942-14. 2 L 7 2 4F RT A6WE 1998061900101 19980619 00101 NM 1998 6 19 DL76G981217 1 19980604 A 5754 114T410131 SKIN BOEING 767 7673P6 1385105 NM NR 5 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 THE NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED ALONG THTE I/B EDGE 3 FWD OF TH E TRAILING EDGE OF THE PANEL. THE DAMAGED AREA MEASURES APPROX 5 (FWD/AFT) X 12. THE DAMAGE WAS REPAIRED WITH AN SRM C OMPOSITE REPAIR PER ER/A 364968-14AD. 2 L 7 2 4F RT A1NM 1998061900102 19980619 00102 NM 1998 6 19 DL76G981218 1 19980604 A 5754 114T410225A SKIN BOEING 767 7673P6 1385105 NM NR 2 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 THE NR 2 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED ALONG THE I/B EDGE 4 FWD OF THE TRAILING EDGE. THE DELAMINATED AREA MEASURES 4 X 4. THE DAMAGE WAS REPAIRED USING AN SRM COMPOSITE REPAIR AUTHORI ZED BY ER/A 364969-14AD. 2 L 7 2 4F RT A1NM 1998061900103 19980619 00103 NM 1998 6 19 DL76G981219 1 19980604 A 5754 114T410226A SKIN BOEING 767 7673P6 1385105 NM RT LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 THE NR 11 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED ALONG THE O/B EDGE. THE D AMAGE MEASURES 3 X 3. THE DAMAGE WAS REPAIRED USING AN SRM COMPOSITE REPAIR AUTHORIZED BY ER/A 364970-14AD. 2 L 7 2 4F RT A1NM 1998061900104 19980619 00104 NM 1998 6 19 DL76G981220 1 19980604 A 5754 114T410437A SKIN BOEING 767 7673P6 1385105 NM NR 4 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 THE NR 4 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED AT A LOCATION 6 INCHES FROM THE O/B END. THE DAMAGE MEASURES APPROX 4 X 4 AND WAS REPAIRED USING AN SRM COMPOSITE REPAIR PER ER/A 364971-14AD. 2 L 7 2 4F RT A1NM 1998061900105 19980619 00105 NM 1998 6 19 DL76G981221 1 19980604 A 5754 114T310023 SKIN BOEING 767 7673P6 1385105 NM NR 6 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 152DL 24984 THE NR 6 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED ALONG THE O/B EDGE 1 FWD OF THE TRAILING EDGE OF THE PANEL. THE DAMAGED AREA MEASURED 2 X 2 AND WAS REPAIRED USING SRM COMPOSITE REPAIR PER ER/A 36497 2-14AD. 2 L 7 2 4F RT A1NM 1998061900106 19980619 00106 WP 1998 6 19 DLL10981222 1 19980605 A 5311 1506092103 FRAME LKHEED 1011 10113851 5265010 WP BS 1163 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 733DS 193C1224 THE STA 1163 FUSELAGE FRAME WAS FOUND WITH THE FRAME TO SKIN ATTACH ANGLE CRACKED AT WL 201 JUST ABOVE PASSENGER FLOOR L EVEL ON THE LT SIDE OF THE FUSELAGE. THE CRACK IS APPROX 1 INCH LENGTH. THE DAMAGE WAS TRIMMED OUT AND A REPAIR DOUBLE R AND FILLER INSTALLED PER ER/A 364952-14. 2 L 7 3 4F A23WE 1998061900107 19980619 00107 WP 1998 6 19 DLL10981223 1 19980605 A 5711 1503229103 SPAR LKHEED 1011 10113851 5265010 WP CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 733DS 193C1224 TWO CENTER WING INTERMEDIATE SPAR UPPER CAPS WERE FOUND WITH CRACKS BEYOND TYPICAL SRM REPAIR. CRACKS WERE LOCATED IN T HE RT O/B END OF THE STA 1043 SPAR AND THE RT O/B END OF THE STA 1163 SPAR. THE CAPS WERE REPAIRED BY TRIMMING OFF TH E O/B ENDS AND SPLICING IN A NEW SECTION WITH REPAIR ANGLES AND STRAPS PER ER/A 364936-14. 2 L 7 3 4F A23WE 1998061900108 19980619 00108 NM 1998 6 19 DL72S981224 1 19980608 A 5400 S-DUCT BOEING 727 727232 1384082 NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 S-DUCT LEADING EDGE ROLLED OVER AND CRACKED JUST AFT OF NOSE COWL AT 12 O'CLOCK POSITION. REMOVED DAMAGED AREA AND FABR ICATED REPAIR PER SRM 54-10-3 FIG 13. OK TO INST REPAIR. INSTALLED REPAIR PER SRM 54-10-3 FIG 13. OK TO CLOSE. CLOSE D OUTER SKIN. 2 L 7 3 4F A3WE 1998061900109 19980619 00109 NM 1998 6 19 DL72W981225 1 19980601 A 2761 ACTUATOR BOEING 727 727247 138408F NM NR 13 SPOILER LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 NR 13 SPOILER ACTUATOR MOUNT LOWER INBD AND OUTBD BOLTS ARE LOOSE. REPAIRED MOUNT HOLES IAW MM 57-42-0. 2 L 7 3 4F A3WE 1998061900110 19980619 00110 NM 1998 6 19 DL72S981226 1 19980608 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 409DA 19964 21153 L2 DOOR EMERG LIGHT INOP. REPLACED CHARGER. 2 L 7 3 4F A3WE 1998061900111 19980619 00111 NM 1998 6 19 DL757981227 1 19980609 A 5610 WINDOW BOEING 757 757232 1384965 NM RT COCKPIT NOT LATCHED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 663DN 24992 COPILOTS WINDOW ON RIGHT SIDE OPENED SHORTLY AFTER TAKEOFF. INSP WINDOW PER MM, CYCLED WINDOW AND ALL CKS GOOD. 2 L 7 2 4F RT A2NM 1998061900112 19980619 00112 NM 1998 6 19 DL72K981230 1 19980606 A 3350 334701744 BATTERY PACK BOEING 727 727232 1384082 NM BS 950 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 471DA 20748 AFT RT SLIDE LIGHT ON AFT CARGO DOOR INOP. REPLACED ASSOCIATED BATTERY RACK, OP CK OK PER MM. 2 L 7 3 4F A3WE 1998061900113 19980619 00113 NM 1998 6 19 DL72W981231 1 19980609 A 2782 FITTING BOEING 727 727247 138408F NM NR 4 SPOILER ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 NR 4 SPOILER O/B ACT SUPPORT FITTING CRACKED. REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1998061900114 19980619 00114 NM 1998 6 19 DL72W981232 1 19980609 A 5754 BRACKET BOEING 727 727247 138408F NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 A 1.75 INCH CRACK O/B AFT MOUNT BRACKET NR 1 SLAT ACT. ALSO INBD BRACKET CRACKED 2 INCHES. REPAIRED PER MM 57-21-21. 2 L 7 3 4F A3WE 1998061900115 19980619 00115 NM 1998 6 19 DL72W981233 1 19980609 A 5720 STIFFENER BOEING 727 727247 138408F NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 OUTBOARD L/E SPAR STIFFENER CRACKED NR 6 SLAT I/B TRACK O/B SIDE. REPLACED SPAR STIFFENER PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998061900116 19980619 00116 NM 1998 6 19 DL72S981234 1 19980609 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 11843 21860 EMERGENCY LIGHT INOP RT SIDE EXTERIOR AFT OF THE AFT OVERWING EMERGENCY EXIT HATCH. RELAMPED AND REPLACED BATTERY PACK REF M/M, CHECKS OK. 2 L 7 3 4F A3WE 1998061900117 19980619 00117 NM 1998 6 19 DLM88981235 1 19980610 A 2150 PACK 20495061 DOUG MD88 MD88 3023688 NM RIGHT MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 945DL 49818 ON T/O, THE SMOKE DETECTORS IN THE AFT LAVS SOUNDED THEN QUIT AFTER POWER REDUCTION. AT CRUISE FLIGHT THE FLIGHT ATTN REPORTED AN ODOR FROM THE AIRCOND SYS AT THAT TIME THE ODOR BECAME NOTICEABLE IN THE COCKPIT AND A HAZE WAS NOTICE D IN THE CABIN. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO CHA. CONTRACT MTC VERIFIED THE OIL LEVEL IN THE A CMS AND FOUND THE RT PACK WAS PRODUCING THE SMOKE. DEACTIVATED THE PACK PER MEL 21-00-01A. 2 L 7 2 4F RT A6WE 1998061900118 19980619 00118 NM 1998 6 19 DL72S981237 1 19980609 A 5320 651751738 BEAM BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 THE RT VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A TYPICAL CRACK IN THE FS 1263 BEAM. THE CRACK IS TYPICAL OF BAC S/B 53-0129. THE CRACKED PART WAS REMOVED AND REPLACED WITH A NEW PART PER THE REQUIREMENTS OF THE S/B. THE REPAIR WAS DO CUMENTED PER ER/A 365003-14AD. 2 L 7 3 4F A3WE 1998061900119 19980619 00119 NM 1998 6 19 SCNA98056 1 19980603 A 3350 900835A BATTERY PACK BOEING 727 727282 138408T NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A MAINTENANCE CHECK, THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACE D BATTERY PACK AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998061900120 19980619 00120 NM 1998 6 19 SCNA98057 1 19980603 A 3350 BATTERIES BOEING 727 727282 138408T NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A MAINTENANCE CHECK, THE LEFT FUSELAGE EMERGENCY LIGHT FOR THE OVERWING EXIT WOULD NOT TEST. PLACED THE COCKPIT EMERGENCY EXIT LIGHT SWITCH IN THE ARM POSITION FOR SEVERAL MINUTES TO ALLOW AIRCRAFT TO CHARGE BATTERIES. TEST CHECKED GOOD FOLLOWING CHARGE CYCLE. 2 L 7 3 4F RT A3WE 1998061900121 19980619 00121 NM 1998 6 19 SCNA98058 1 19980603 A 3350 BULB BOEING 727 727282 138408T NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A MAINTENANCE CHECK, ONE BULB FOR THE EMERGENCY LIGHT IN THE AFT CARGO DOOR WAS FOUND TO BE INOPERATIVE. RELAMPE D LIGHT BULB AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998061900122 19980619 00122 NM 1998 6 19 SCNA98059 1 19980603 A 3350 6013211 POWER SUPPLY BOEING 727 727282 138408T NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 8048 21949 DURING A MAINTENANCE CHECK, THE R1 AND R2 DOOR SLIDE EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REMOVED AND RE PLACED THE BATTERY AND POWER SUPPLY ASSEMBLY AT M982. ALL EMERGENCY LIGHTS OPERATIONALLY CHECK GOOD. 2 L 7 3 4F RT A3WE 1998061900123 19980619 00123 NM 1998 6 19 DHL98720001 1 19980606 A 5230 MECHANISM BOEING 727 727228 NM CARGO DOOR OUT OF ADJUST A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 720DH 19544 MAIN CARGO DOOR UNLOCK LIGHT ILLUMINATED AT FL 200, AND WENT OUT AT FL 130 AT 3 PSI. RECYCLED SEVERAL TIMES, ADJUSTED DOOR CLOSED, PRESSURIZED TO 8 PSI OPS CHECK OK PER M/M 52-73-0. 2 L 7 3 4F A3WE 1998061900125 19980619 00125 WP 1998 6 19 VJ9800190 1 19980611 A 2120 700F69400112 DUCT DOUG DC9 DC932 3022066 WP CABIN FAILED A ZZDA B EMER. DESCENT O OTHER DE DESCENT 1 SO 15 946VV 47226 DESENDING THRU FL320, CABIN BEGAN CLIMBING UNCONTROLLABLY. ENACTED EMERGENCY PROCEDURES AND DESCENDED TO FL 100. FOUND RT WATER SEPARATOR INLET DUCT BLOWN. REPLACED DUCT AND CHECKED IAW MM 21-20; NO LEAKS DURING GROUND TEST. 2 L 7 2 4F A6WE 1998061900126 19980619 00126 WP 1998 6 19 CALA9801023 1 19980610 A 5754 SKIN DOUG DC10 DC1010 3022110 WP RT LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 2 CRACK IN RT WING LOWER SURFACE ON LEADING EDGE SLAT CUTOUT FOR SLAT TRACK. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-10-00, 51-31-01, AND 54-11-00, FIGURE 1C. 2 L 7 3 4F A22WE 1998061900127 19980619 00127 WP 1998 6 19 CALA9801024 1 19980610 A 5720 ANGLE DOUG DC10 DC1010 3022110 WP LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND SUPPORT ANGLES CORRODED IN CAVITY OF TRAILING EDGE FIXED FAIRING BETWEEN INBOARD AILERON AND OUTBOARD T RAILING EDGE FLAP, LT WING. THE ANGLES WERE REMOVED. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-20-00 AND 51-3 1-01. 2 L 7 3 4F A22WE 1998061900128 19980619 00128 WP 1998 6 19 CALA9801025 1 19980610 A 5730 SKIN DOUG DC10 DC1010 3022110 WP WS 402-372 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND CORROSION ON LOWER SKIN AT LT WING REAR SPAR BETWEEN STA XORS 402 AND XORS 372. THE AREA WAS REPAIRED IAW ECRA 5731-01004. 2 L 7 3 4F A22WE 1998061900129 19980619 00129 WP 1998 6 19 CALA9801026 1 19980610 A 5712 RIB DOUG DC10 DC1010 3022110 WP WS 855-917 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB IN BETWEEN XORS 855 AND XORS 917. THE CRACKED AREA WAS TR IMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-20-00, FIGURE 1, 51-01-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998061900130 19980619 00130 WP 1998 6 19 CALA9801027 1 19980611 A 5712 RIB DOUG DC10 DC1010 3022110 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB IN FRONT OF NR 5 LEADING EDGE SLAT. THE RIB WAS REPAIRED IAW SRM 57-20-00, FIGURE 1 AND 51-31-01. 2 L 7 3 4F A22WE 1998061900131 19980619 00131 WP 1998 6 19 CALA9801028 1 19980611 A 5712 RIB DOUG DC10 DC1010 3022110 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 1 CRACK IN LT WING LEADING EDGE CAVITY RIB ADJACENT TO OUTBOARD SLAT ACCESS PANEL, OUTBOARD SIDE. TH E CRACKED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-20-00, FIGURE 1, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998061900132 19980619 00132 WP 1998 6 19 CALA9801029 1 19980610 A 5720 ANGLE DOUG DC10 DC1010 3022110 WP WS 562 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 1 CRACK ON METAL STRIP AND A 1 CRACK ON SUPPORT ANGLE IN LT WING LEADING EDGE CAVITY AT XORS 562. RE PAIRS WERE INSTALLED IAW SRM 57-00-01, 51-31-01, 57-31-01, FIGURE 1, AND 51-21-01. 2 L 7 3 4F A22WE 1998061900133 19980619 00133 WP 1998 6 19 CALA9801030 1 19980611 A 5330 SKIN DOUG DC10 DC1010 3022110 WP FUSELAGE DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND FUSELAGE SKIN DELAMINATING AT AFT UPPER CORNER OF LT WINDOW NR 12. THE DELAMINATED AREA OF SKIN WAS TR IMMED OUT. TWO SPLICES AND A DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-20-00, FIGURE 8, PAGE 89, 51-21-01, AND 5 1-31-01. 2 L 7 3 4F A22WE 1998061900134 19980619 00134 WP 1998 6 19 CALA9801031 1 19980611 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 824 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A .25 CRACK IN FLOOR SUPPORT AT STA 824 BETWEEN LBL 50 AND 70. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-16-01, 51-20-00, AND 51-31-01. 2 L 7 3 4F A22WE 1998061900135 19980619 00135 WP 1998 6 19 CALA9801032 1 19980611 A 5754 RIB DOUG DC10 DC1030 3023501 WP NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND A 1 CRACK IN OUTBOARD RIB OF NR 1 SLAT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51-37- 01 AND 51-35-02. 2 L 7 3 4F A22WE 1998061900136 19980619 00136 WP 1998 6 19 CALA9801033 1 19980611 A 5754 RIB DOUG DC10 DC1030 3023501 WP NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND A 1 CRACK IN INBOARD END RIB OF NR 2 SLAT. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 51- 31-01. 2 L 7 3 4F A22WE 1998061900137 19980619 00137 WP 1998 6 19 CALA9801034 1 19980611 A 5400 FAIRING DOUG DC10 DC1030 3023501 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND A 2 CRACK IN NR 1 PYLON LT FAIRING. THE FAIRING WAS REMOVED. A NEW FAIRING WAS FABRICATED AND INSTALL ED IAW SRM 51-35-02. 2 L 7 3 4F A22WE 1998061900138 19980619 00138 WP 1998 6 19 CALA9801035 1 19980611 A 7110 ANGLE DOUG DC10 DC1030 3023501 WP NOSE COWL CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND A 2 CRACK IN NR 1 ENGINE NOSE COWL AFT BULKHEAD AND ANGLE SUPPORT. THE ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 54-11-01, FIGURE 1 AND 51-31-01. 2 L 7 3 4F A22WE 1998061900139 19980619 00139 WP 1998 6 19 CALA9801036 1 19980610 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND MAIN BAGGAGE BIN DOOR JAMB Z-ANGLE CORRODED. THE ANGLE WAS REPAIRED IAW SRM 53-05, FIGURE 63. 2 L 7 3 4F A22WE 1998061900140 19980619 00140 NM 1998 6 19 CALA9801037 1 19980610 A 7830 HINGE BOEING 737 7373T0 1384582 NM NR 1 THRUST REV GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND NR 1 ENGINE INBOARD AND OUTBOARD THRUST REVERSER FORWARD HINGE POINT FORWARD LUGS GOUGED. THE HINGES W ERE REPAIRED IAW ECRA 7832-01125. 2 L 7 2 4F RT A16WE 1998061900141 19980619 00141 WP 1998 6 19 CALA9801038 1 19980610 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND AFT BAGGAGE BIN BELTFRAME CORRODED AT STA 1309 FROM LONGERON 27L TO 27R. A NEW BELTFRAME WAS INSTALLED IAW SRM 53-03. 2 L 7 2 4F A6WE 1998061900142 19980619 00142 WP 1998 6 19 CALA9801039 1 19980610 A 5347 TIEDOWN RAIL DOUG DC9 DC982 3022082 WP BS 1212-1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND AFT BAGGAGE BIN LEFT TIE DOWN RAIL AT SPLICE BETWEEN STA 1212 AND 1231 CORRODED AROUND NUT PLATE HOLES. A REPAIR WAS INSTALLED IAW ECRA 5320-01523. 2 L 7 2 4F A6WE 1998061900143 19980619 00143 WP 1998 6 19 CALA9801040 1 19980611 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 824-840 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 824 AND 840, RBL 70. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED. A NEW SECTION OF SEAT TRACK AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-60-01, FIGURE 1, SHEET 1, 51-21-01, AND 5 1-31-01. 2 L 7 3 4F A22WE 1998061900144 19980619 00144 WP 1998 6 19 CALA9801041 1 19980611 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND TWO 1 CRACKS OVER OUTBOARD SKIN SURFACE OF LONGERON BOX AT RT L/E WHEEL WELL. TWO EACH ANGLES WERE REM OVED AND TWO NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-20-00 AND 51-31-01. 2 L 7 3 4F A22WE 1998061900145 19980619 00145 WP 1998 6 19 CALA9801042 1 19980611 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1780 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 1 CRACK IN CENTER CARGO COMPARTMENT ANGLE BRACKET ON AFT FRAME CUTOUT AT MID SIDE STA 1780. THE ANGL E WAS REMOVED AND A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-38-00, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998061900146 19980619 00146 WP 1998 6 19 CALA9801043 1 19980612 A 5320 BRACKETS DOUG DC10 DC1010 3022110 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND LOWER SILL CENTER CARGO COMPARTMENT BRACKETS CORRODED. THE CORRODED AREAS WERE REMOVED. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-15-01, FIGURE 15. 2 L 7 3 4F A22WE 1998061900147 19980619 00147 WP 1998 6 19 CALA9801044 1 19980611 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 980-996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CUSP CORRODED AT STA 980-996, RT SIDE. THE CORRODED SECTION OF CUSP WAS CUT OUT IAW SRM 53-05, FIGURE 25. A REPAIR CUSP WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 25 AND 51-30-2. 2 L 7 2 4F A6WE 1998061900148 19980619 00148 WP 1998 6 19 CALA9801045 1 19980611 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 968 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBEAM GOUGED AT STA 968. THE GOUGED SECTION OF FLOORBEAM WAS CUT OUT. AN L-ANGLE DOUBLER AND FILL ER WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 20A, 53-05, 51-10-3, 51-30-2, AND 51-20-0. 2 L 7 2 4F A6WE 1998061900149 19980619 00149 WP 1998 6 19 CALA9801046 1 19980611 A 5321 FLOOR DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD NR 82 HAT SECTIONS WORN THROUGH AND CRACKED. A FLOOR PANEL AND HAT SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-21-0, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900150 19980619 00150 WP 1998 6 19 CALA9801047 1 19980611 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR JAMB PAN CORRODED. THE CORRODED SECTION OF PAN WAS REMOVED. REPAIR SPL ICES WERE FABRICATED AND THE NEW SECTION OF PAN WAS INSTALLED IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 1998061900151 19980619 00151 WP 1998 6 19 CALA9801048 1 19980612 A 5320 STIFFENER DOUG DC10 DC1030 3023501 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35084 46991 INSPECTION FOUND A 2 CRACK ON VERTICAL STIFFENER IN AFT WEB OF LEFT MLG WHEEL WELL. THE STIFFENER WAS REMOVED. A NEW P ART WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998061900152 19980619 00152 WP 1998 6 19 9809499621 1 19980609 A 2170 COALESCER BAG DOUG DC9 DC932 3022066 WP CABIN DIRTY A NWAA B EMER. DESCENT O OTHER CR CRUISE 1 GL 01 621NW 47544 AT FL280, THE CABIN PRESSURE CLIMBED RAPIDLY. THE FLIGHT CREW INITIATED AN EMERGENCY DESCENT TO 10,000 FEET AND GAINED CONTROL OF CABIN PRESSURIZATION. NO FURTHER PROBLEMS WERE NOTED AND THE AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT . MAINTENANCE REPLACED THE LEFT WATER SEPARATOR AND RIGHT COALESCER BAG. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998061900153 19980619 00153 WP 1998 6 19 9809509972 1 19980609 A 2780 T-DUCT DOUG DC9 DC931 3022065 WP RT WING LACK OF LUBE A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 9336 47338 SLAT DISAGREEMENT LIGHT ILLUMINATED ACCOMPANIED BY AIRCRAFT ROLL ON SLAT EXTENSION DURING APPROACH INTO JAN. FLIGHT CRE W DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY USING FLAPS ONLY. MAINTENANCE FOUND THE RIGHT WING ANTI-ICE T DU CT BINDING. LUBRICATED DUCT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998061900154 19980619 00154 EA 1998 6 19 COMA9860140 1 19980609 A 3610 DUCT CNDAIR CL600 CL6002B19 EA LEFT FAILED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 926CA 7027 LEFT HAND 14TH STAGE BLEED AIR DUCT FAIL WARNING. COULD NOT DUPLICATE DISCREPANCY. FUNCTIONAL CHECK OF SYSTEM FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 1998061900155 19980619 00155 NM 1998 6 19 SWAA981062 1 19980604 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 1040 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND STRINGER 26 RT IS CHAFE UNDER APU BLEED DUCT JUST AFT OF BS 1040. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998061900156 19980619 00156 NM 1998 6 19 SWAA981063 1 19980604 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178, WL 207 LBL 55, 178 BULKHEAD SIDE CHORD, BS 178 WL 207, RBL 55, 178 BULKH EAD SIDE CHORD AND BS 178 BULKHEAD, LBL 1, WL 185 HAS 1 CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900157 19980619 00157 NM 1998 6 19 SWAA981064 1 19980604 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED AT BS 178 BULKHEAD WEB WL 197 TO 201.4, RBL 4.7. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998061900158 19980619 00158 NM 1998 6 19 SWAA981065 1 19980604 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 860, RBL 8, WL 164. REPAIRE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900159 19980619 00159 NM 1998 6 19 SWAA981066 1 19980604 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND STRINGER 28L, AT BS 500+7 EFFECTS INSTALLATION OF VHF SUPPORT STRUCTURE MODIFICATION. R EPAIRED SECTION OF STRINGER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900160 19980619 00160 NM 1998 6 19 SWAA981067 1 19980604 A 5321 FLOOR BOEING 737 7373H4 1384600 NM BS 1030 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1030, LBL 9, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900161 19980619 00161 NM 1998 6 19 SWAA981068 1 19980604 A 5320 ANGLES BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED FWD GALLEY DOORWAY LOWER SILL SUPPORT Z-ANGLES, NR 1, 3, 4. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998061900162 19980619 00162 NM 1998 6 19 SWAA981069 1 19980604 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 344-360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 344 TO 360, LBL 11, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900163 19980619 00163 NM 1998 6 19 SWAA981070 1 19980604 A 5320 ANGLE BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FWD GALLEY DOOR ENTRY Z-ANGLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900164 19980619 00164 NM 1998 6 19 SWAA981071 1 19980604 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FWD BULKHEAD ATTACH ANGLE AT BS 727, RBL 4. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900165 19980619 00165 NM 1998 6 19 SWAA981072 1 19980604 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 630SW 27705 DURING SERVICE CHECK, FOUND CABIN FLOOR EMERGENCY LIGHT AT ROWS 18, 19, 20, INOP. REPLACED LIGHT ASSY AT ROW 20 PER BO EING MM. CABIN FLOOR EMERGENCY LIGHT CHECK GOOD. 2 L 7 2 4F RT A16WE 1998061900166 19980619 00166 NM 1998 6 19 SWAA981073 1 19980604 A 2560 SLIDE DOOR BOEING 737 7373H4 1384600 NM PAX DOOR OPENED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 610SW 27696 DURING WALKAROUND CHECK, FOUND FWD ENTRY DOOR (1L) PARTIALLY OPENED W/EMERGENCY SLIDE ARMED. SLIDE DID NOT INFLATE. RE INSTALLED FWD ENTRY SLIDE INTO HARD CASE CHECK OK. 2 L 7 2 4F RT A16WE 1998061900167 19980619 00167 NM 1998 6 19 SWAA981074 1 19980604 A 2560 SLIDE DOOR BOEING 737 7373H4 1384600 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 657SW 23331 DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR EMERGENCY SLIDE LOOSE. REINSTALLED FWD SERVICE DOOR EMERGENCY SLIDE PE R BOEING MM. 2 L 7 2 4F RT A16WE 1998061900168 19980619 00168 NM 1998 6 19 SWAA981075 1 19980604 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 960 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND GOUGED SKIN AT BS 960 BELOW STR 19L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061900169 19980619 00169 NM 1998 6 19 SWAA981076 1 19980604 A 5312 BULKHEAD CHORD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED VERTICAL CHORD AT BS 178, LBL 5.5 WL 184 AFT SIDE. REPAIRED PER BOEING TYPI CAL REPAIR TI- 253-031. 2 L 7 2 4F A16WE 1998061900170 19980619 00170 NM 1998 6 19 SWAA981077 1 19980604 A 5530 ANGLE BOEING 737 7373H4 1384600 NM VERT STAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND RT FUSELAGE TO VERTICAL STAB SKATE ANGLE WORN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900171 19980619 00171 NM 1998 6 19 SWAA981078 1 19980604 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1037 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND DENTED AT BS 1037 BETWEEN STRS 12 AND 14 LT (SKIN). REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900172 19980619 00172 NM 1998 6 19 SWAA981079 1 19980604 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT LOWER END CORNER AT BS 344, LBL 37, WL 285. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900173 19980619 00173 NM 1998 6 19 SWAA981080 1 19980604 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM HOLES AT BS 312, BL 0 AND BS 344, RBL 1. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998061900174 19980619 00174 NM 1998 6 19 SWAA981081 1 19980607 A 2751 FLAP INDICATION BOEING 737 7373G7 1384595 NM TE FLAPS SPLIT A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 670SW 23784 AFTER TAKEOFF, RETRACTING THE FLAPS FROM POSITION 5 TO 1, FLAPS SPLIT. THE RIGHT FLAP STOPPED AT 2 AND THE LEFT FLAP ST OPPED AT 1. A/C TURNBACK, MADE AN UNEVENTFUL LANDING. PERFORMED ASSEMITY CHECK. UNLOCKED FLAP INDICATE. OPS CHECKS N ORMAL, FLAP CYCLED STANDBY AND NORMAL. SYSTEM OPERATED NORMAL PER BOEING MM. 2 L 7 2 4F RT A16WE 1998061900175 19980619 00175 NM 1998 6 19 SWAA981082 1 19980605 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500/764-767 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN JUST FWD AT BS 500B BETWEEN STR 20 AND 21 LT AND AT BS 764 TO 767, STR 21 TO 23. RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900176 19980619 00176 NM 1998 6 19 SWAA981083 1 19980605 A 5320 SEAL BOEING 737 7373H4 1384600 NM LT MLG TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND TORN LT MLG BEAM PANEL FWD BULB SEAL. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900177 19980619 00177 NM 1998 6 19 SWAA981084 1 19980605 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SHEAR TIE AT BS 344 BETWEEN STR 20 AND 21 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900178 19980619 00178 NM 1998 6 19 SWAA981085 1 19980605 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 371-374 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND DENTED SKIN DOUBLER AT BS 371 TO 374 BETWEEN STR 22 AND 23 RT. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900179 19980619 00179 NM 1998 6 19 SWAA981086 1 19980605 A 5312 BULKHEAD PANEL BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FWD CARGO BAY FWD BULKHEAD PANEL AT BS 380 RBL 12 WL 183. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998061900180 19980619 00180 NM 1998 6 19 SWAA981087 1 19980606 A 3350 6104781 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 094SW 23053 DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY SLIDE LIGHTS ARE OUT. REMOVED AND REPLACED BATTERY PACK AND CHARGER , OPS GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998061900181 19980619 00181 NM 1998 6 19 SWAA981088 1 19980605 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND BULGING CORROSION ON FUSELAGE SKIN FWD AT BS 727-A, STR 27R. REPAIRED PER SWA RA 1- 253-1829. 2 L 7 2 4F A16WE 1998061900182 19980619 00182 NM 1998 6 19 SWAA981089 1 19980605 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 987, RBL 35 AROUND FLOORBOARD SCREW HOLE, BS 987 FASTENER H OLE TOP FWD SIDE RBL 39 AND BS 987 FASTENER HOLE TOP FWD SIDE RBL 42.5. REPAIRED PER SWA RA 1-353-1830. 2 L 7 2 4F RT A16WE 1998061900183 19980619 00183 NM 1998 6 19 SWAA981090 1 19980607 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 460 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND LIGHTNING STRIKE DAMAGED AT BS 460 UPPER LEFT CROWN AREA. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998061900184 19980619 00184 NM 1998 6 19 SWAA981091 1 19980607 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 773, RBL 8, WL 156. REPAIRE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900185 19980619 00185 NM 1998 6 19 SWAA981092 1 19980606 A 3350 6104791 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY SLIDE LIGHTS WON'T ILLUMINATE. REMOVED AND REPLACED BATTERY AND B ATTERY CHARGER PER BOEING MM. 2 L 7 2 4F A16WE 1998061900186 19980619 00186 NM 1998 6 19 SWAA981093 1 19980606 A 5330 SKIN BOEING 737 7373G7 1384595 NM E/E DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED SKIN .2 LONG AT E AND E BAY DOOR FWD RIGHT CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900187 19980619 00187 NM 1998 6 19 SWAA981094 1 19980606 A 5320 WEB BOEING 737 7373G7 1384595 NM TAIL CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB ON I/B SIDE OF HOLES STAB APPROX 12 AFT OF REAR SPAR ATTACH FITTINGS. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900188 19980619 00188 NM 1998 6 19 SWAA981095 1 19980606 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 670SW 23784 DURING SCHEDULED D-CHECK, FOUND CORRODED FRAME AT BS 847, RBL 19, WL 165. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900189 19980619 00189 NM 1998 6 19 SWAA981096 1 19980607 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 727/773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 727D+5, RBL 8, WL 155, BS 72 7D+5, RBL 3, WL 155, AND BS 773, LBL 2, WL 175. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900190 19980619 00190 NM 1998 6 19 SWAA981097 1 19980607 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 727/773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AROUND FASTENER HOLE AT BS 727E+3, LBL 2, WL 155, BS 77 3, LBL 11, WL 156, AND BS 754, RBL 3, WL 155. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900191 19980619 00191 NM 1998 6 19 SWAA981098 1 19980607 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 792-801 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT AT BS 792 TO 801, RBL 8, WL 157. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900192 19980619 00192 NM 1998 6 19 SWAA981099 1 19980607 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT RT HAT RACK SUPPORT BS 440 BETWEEN STR 8 AND STR 9 RT. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900193 19980619 00193 NM 1998 6 19 SWAA981100 1 19980607 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 787, BETWEEN STR 9 AND 9L, BS 907 BETWEEN STR 8 AND 9L AN D BS 867 BETWEEN STR 8 AND 9L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900194 19980619 00194 NM 1998 6 19 SWAA981101 1 19980607 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 993 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 993, LBL 25 TO 28, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900195 19980619 00195 NM 1998 6 19 SWAA981102 1 19980607 A 5320 BEAM BOEING 737 7373H4 1384600 NM BS 400-420 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED PASSENGER COMPARTMENT, SHEAR WEB, CREASE BEAM, BETWEEN BS 400 TO 420, WL 208, L BL 64 TO 71, AND BS 460 TO 480, WL 208, LBL 69. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900196 19980619 00196 NM 1998 6 19 SWAA981103 1 19980607 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 480/500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 480, BETWEEN STR 8 AND 9 RT, BS 500A BETWEEN STR 8 AND 9 RT AND BS 500C BETWEEN STR 8 AND 9 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900197 19980619 00197 NM 1998 6 19 SWAA981104 1 19980607 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE FRAME AT BS 827, BETWEEN STR 8 AND 9 RT AND BS 827, BETWEEN STR 8 AND 9 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900198 19980619 00198 NM 1998 6 19 SWAA981105 1 19980607 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 344-360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 344 TO 360, LBL 0, WL 208 AND BS 312 TO 328, RBL 35, WL 208. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900199 19980619 00199 NM 1998 6 19 SWAA981106 1 19980607 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727/747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME PAX CABIN UPPER LOBE STRUCTURE LEFT HAND AT BS 727D BETWEEN STR 8 AND 9, BS 727D RIGHT HAND SIDE BETWEEN STR 8 AND 9 AND BS 747 RIGHT HAD SIDE BETWEEN STR 8 AND 9. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900200 19980619 00200 NM 1998 6 19 SWAA981107 1 19980607 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND DAMAGED FLOORBEAM WEB AT BS 328, RBL 35, WL 206. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900201 19980619 00201 NM 1998 6 19 SWAA981108 1 19980607 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME PAX CABIN UPPER LOBE STRUCTURE, RIGHT HAND SIDE AT BS 787 BETWEEN STR 8 AN D 9. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900202 19980619 00202 NM 1998 6 19 SWAA981109 1 19980607 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 992 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 992, LBL 34, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900203 19980619 00203 NM 1998 6 19 SWAA981110 1 19980608 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 382 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED B1B2 CHECK, FOUND DENTED FUSELAGE SKIN AT BS 382 JUST BELOW STRINGER 15L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900204 19980619 00204 NM 1998 6 19 SWAA981111 1 19980608 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 402 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND DENTED STRINGER FWD CARGO BAY AT BS 402, STR 24 RT. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998061900205 19980619 00205 NM 1998 6 19 SWAA981112 1 19980608 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 500D, LBL 24, RBL 24, WL 156. REMOVED AN D REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900206 19980619 00206 NM 1998 6 19 SWAA981113 1 19980608 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP, FWD CARGO BAY AT BS 500D, STR 19 RT AND BS 500D, STR 19 LT. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900207 19980619 00207 NM 1998 6 19 SWAA981114 1 19980608 A 5330 SKIN BOEING 737 737317 138447P NM BS 395-420 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 693SW 23174 DURING SCHEDULED D-CHECK, FOUND DAMAGED FWD CARGO DOORWAY HAS BIG HOLE IN FUSELAGE BETWEEN STR 25R AND 26R AT BS 395 TO 420. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900208 19980619 00208 NM 1998 6 19 SWAA981115 1 19980609 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 520 LT SIDE BETWEEN NR 11 AND 12 WINDOW BELOW STR 15. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900209 19980619 00209 NM 1998 6 19 SWAA981116 1 19980609 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 254-277 LIGHTNING STRIKE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND LIGHTNING STRIKE ON FUSELAGE BETWEEN BS 254 TO 277 JUST ABOVE STR 11R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061900210 19980619 00210 NM 1998 6 19 SWAA981120 1 19980611 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D CHECK, FOUND FLOORBEAM CORRODED AT BS 312, BL0. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900211 19980619 00211 NM 1998 6 19 SWAA981121 1 19980611 A 3350 65C27095 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 81SW 22730 DURING PREFLIGHT CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE FWD ENTRY DOOR INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F A16WE 1998061900212 19980619 00212 NM 1998 6 19 SWAA981122 1 19980610 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 970 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 60SW 21812 DURING SCHEDULED B CHECK, FOUND FUSELAGE SKIN DENTED BELOW AFT ENTRY DOOR AT BS 970, S21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998061900213 19980619 00213 NM 1998 6 19 SWAA981123 1 19980609 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 794 - 850 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D CHECK, FOUND TEAR STRAP CORRODED AT BS 794 TO 850, RBL 20.5. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998061900214 19980619 00214 WP 1998 6 19 UPS98826877 1 19980611 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 707UP 45907 EMERG EXIT LIGHT INOP ON BATT POWER. REMOVED AND REPLACED EMER BATT PACK , OPS CHECK GOOD, P/N ON/OFF 5708458-503, S/N OFF FTL157 S/N ON 976. 2 L 7 4 4F RT 4A25 1998061900215 19980619 00215 EU 1998 6 19 QXEA9800786 1 19980608 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 BOI - CEILING EMERGENCY LIGHT INOPERATIVE AT ROWS 1 AND 8. MAINTENANCE RELAMPED AND OPERATIONAL TESTED, CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998061900216 19980619 00216 NM 1998 6 19 98FDEA00398 1 19980612 A 2730 680005007 CONTROL BOEING 727 727227 1384078 NM RT ELEVATOR LEAKING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 479FE 21461 INFLIGHT LOSS OF A-SYSTEM HYDRAULIC. HYDRAULIC FLUID SHUTOFFS CLOSED FOR 52 MINUTES. *S/D* REPLACED RIGHT ELEVATOR PO WER CONTROL PACKAGE PER M/M 27-30-81. REPLACED A-SYSTEM PRESSURE AND CASE DRAIN FILTERS PER M/M 29-11-10, PAGE 102. NO METAL FOUND. OPERATIONAL CHECKS AND LEAK CHECKS GOOD. REMOVED GEAR PINS. DOWNGRADED CAT STATUS TO CHECK CAT II A/C S TATUS IS NOT CAT II. 2 L 7 3 4F A3WE 1998061900217 19980619 00217 WP 1998 6 19 ABXA9800500 1 19980429 A 5720 5769496 ANGLE DOUG DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XS 448.501 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998061900218 19980619 00218 WP 1998 6 19 ABXA9800501 1 19980429 A 5720 5769496 ANGLE DOUG DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XFS 772.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 5 1-1-8. 2 L 7 4 4F 4A25 1998061900219 19980619 00219 WP 1998 6 19 ABXA9800502 1 19980429 A 5720 5769496 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 585 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 585.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51 -1-8. 2 L 7 4 4F 4A25 1998061900220 19980619 00220 WP 1998 6 19 ABXA9800503 1 19980429 A 5720 5769496 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 822.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 822.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51 -1-8. 2 L 7 4 4F 4A25 1998061900221 19980619 00221 WP 1998 6 19 ABXA9800504 1 19980429 A 5720 5769496 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 803.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 803.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 5 1-1-8. 2 L 7 4 4F 4A25 1998061900222 19980619 00222 WP 1998 6 19 ABXA9800505 1 19980427 A 5720 5769496 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 791.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 791.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 5 1-1-8. 2 L 7 4 4F 4A25 1998061900223 19980619 00223 WP 1998 6 19 ABXA9800506 1 19980429 A 5720 5769496 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 741.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 5 1-1-8. 2 L 7 4 4F 4A25 1998061900224 19980619 00224 WP 1998 6 19 ABXA9800507 1 19980429 A 5720 57694668 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 585 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XFS 585.00 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998061900225 19980619 00225 WP 1998 6 19 ABXA9800508 1 19980429 A 5720 576946614 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 603.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XFS 603.75 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998061900226 19980619 00226 WP 1998 6 19 ABXA9800509 1 19980429 A 5712 5769496 RIB DOUG DOUG DC8 DC863F 302198F WP WS 442.185 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XS 442.185 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056. 2 L 7 4 4F 4A25 1998061900227 19980619 00227 WP 1998 6 19 ABXA9800510 1 19980429 A 5712 5769496 RIB DOUG DOUG DC8 DC863F 302198F WP WS 747.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 747.5 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW DRAWING K05056. 2 L 7 4 4F 4A25 1998061900228 19980619 00228 WP 1998 6 19 ABXA9800511 1 19980429 A 5720 5769545 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 778.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XFS 778.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG NR K05056 AND DC8 S RM 51-1-8. 2 L 7 4 4F 4A25 1998061900229 19980619 00229 WP 1998 6 19 ABXA9800512 1 19980429 A 5720 5769545 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 672.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XFS 672.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 5 1-1-8. 2 L 7 4 4F 4A25 1998061900230 19980619 00230 WP 1998 6 19 ABXA9800513 1 19980429 A 5720 5769545 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 785 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XFS 785.0 IS CRACKED AT THE AFT LWR END. REPAIRED IAW DWG K05056 AND DC8 SRM 51- 1-8. 2 L 7 4 4F 4A25 1998061900231 19980619 00231 WP 1998 6 19 ABXA9800514 1 19980602 A 5313 27779221 LONGERON DOUG DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, LONGERON 17 LEFT WAS FOUND CRACKED AT STATION 408, 389, 294, 275 AND 256. REPLACED LONGERON IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998061900232 19980619 00232 WP 1998 6 19 ABXA9800515 1 19980602 A 5230 995766633 DOUBLER DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE AFT LOWER CARGO DOOR INTERNAL DOUBLER WAS FOUND CRACKED. REPAIRED IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998061900233 19980619 00233 WP 1998 6 19 ABXA9800516 1 19980604 A 5210 59121419 PAN DOUG DOUG DC9 DC941 302207N WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE FORWARD ENTRY DOOR PAN WAS FOUND CRACKED IN SEVERAL PLACES. REPLACED IAW DC9 SRM 51-30-8 AND REA D9 52-23898. 2 L 7 2 4F A6WE 1998061900234 19980619 00234 WP 1998 6 19 ABXA9800517 1 19980608 A 5311 9925406502 FRAME DOUG DOUG DC9 DC941 302207N WP BS 677 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, FUSELAGE FRAME AT STATION 677 WAS FOUND CRACKED AT LONGERON 19R. REPLACED FRAME IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998061900235 19980619 00235 WP 1998 6 19 ABXA9800518 1 19980602 A 5320 99577397 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, A SHEAR-TIE WAS FOUND CRACKED AT STATION 1021 LONGERON 15 AND 16 R. REPLACED SHEAR-TIE IAW DC9 SRM 51-3 0-2. 2 L 7 2 4F A6WE 1998061900236 19980619 00236 WP 1998 6 19 ABXA9800519 1 19980601 A 5330 592032379 SKIN DOUG DOUG DC9 DC941 302207N WP BS 427 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 970AX 47494 DURING C-CHECK, THE FUSELAGE SKIN WAS FOUND CRACKED AT STATION 427 LONGERON 26 R. REPAIRED IAW REA D953-23873-MR. 2 L 7 2 4F A6WE 1998061900237 19980619 00237 WP 1998 6 19 MWEA98646 1 19980609 A 5312 R91013013 BULKHEAD DOUBLE DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE AFT PRESSURE BULKHEAD -13 DOUBLER WAS FOUND CRACKED. MAINTENANCE REMOVED OLD DOUBLER OBTAINED NEW DOUBLER AND INSTA LLED USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900238 19980619 00238 WP 1998 6 19 MWEA98647 1 19980609 A 5312 R591013011 BULKHEAD CHANNEL DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 AFT PRESSURE BULKHEAD CHANNELS HAVE CRACKS IN UPPER CORNERS. MAINTENANCE REMOVED CRACKS BY BLENDOUT IAW SABRETECH EA. 2 L 7 2 4F A6WE 1998061900239 19980619 00239 WP 1998 6 19 MWEA98648 1 19980609 A 5400 5913262 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE LEFT PYLON FWD SPAR AFT INBOARD SURFACE HAS A IMPROPER REPAIR. MAINTENANCE REMOVED DAMAGED AREA INSTALLED REPLACEME NT PARTS USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900240 19980619 00240 WP 1998 6 19 MWEA98649 1 19980609 A 5400 SR09540004 SPAR DOUG DC9 DC932 3022066 WP LT PYLON DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE LEFT PYLON UPPER SPAR CAPS WERE FOUND DAMAGED. REMOVED AND REPLACED SPAR CAPS USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900241 19980619 00241 WP 1998 6 19 MWEA98650 1 19980609 A 5330 59114273 SKIN DOUG DC9 DC932 3022066 WP BS 945-965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 PREVIOUS REPAIR AT STA 962 LONGERON 16R WAS REMOVED AND FOUND TO BE CRACKED. INSTALLED FILLER AND DOUBLER REPAIR OF FUS ELAGE SKIN PANEL STA 945-96. 2 L 7 2 4F A6WE 1998061900242 19980619 00242 WP 1998 6 19 MWEA98651 1 19980609 A 5311 9958214 FRAME DOUG DC9 DC932 3022066 WP BS 897 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE FRAME AT FUSELAGE STATION 897 HAS ELONGATED FASTENER HOLES BETWEEN LONGERON 27L AND 29R. REPAIRED FRAME USING APPRO VED DATA. 2 L 7 2 4F A6WE 1998061900243 19980619 00243 WP 1998 6 19 MWEA98652 1 19980609 A 5320 5912528 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE AFT CARGO DOOR JAMB PAN WAS FOUND CORRODED. MAINTENANCE REMOVED DAMAGED SECTION INSTALLED REPLACEMENT SECTION OF PA N USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900244 19980619 00244 WP 1998 6 19 MWEA98653 1 19980609 A 5311 995773945 FRAME DOUG DC9 DC932 3022066 WP BS 945 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FRAME AT STA 945 BETWEEN LONGERON 28R AND 29R IS DENTED BEYOND SRM LIMITS. INSTALLED STACKED ANGLE REPAIR. 2 L 7 2 4F A6WE 1998061900245 19980619 00245 WP 1998 6 19 MWEA98654 1 19980609 A 5720 DOUBLER DOUG DC9 DC932 3022066 WP WS 198 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING INTERNAL BEADED DOUBLER CRACKED AT STATION XO 198. MAINTENANCE ROUTED OUT CRACK AND INSTALLED REPAIR USING AP PROVED DATA. 2 L 7 2 4F A6WE 1998061900246 19980619 00246 WP 1998 6 19 MWEA98655 1 19980609 A 5730 5910465 SKIN DOUG DC9 DC932 3022066 WP RT WING CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 RIGHT WING LOWER SURFACE FORWARD OF FUEL PANEL NUMBER 1460 HAS NUMEROUS AREAS OF CORROSION AROUND FASTENERS. REMOVED CO RROSION FABRICATED AND INSTALLED REPAIR DOUBLER USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900247 19980619 00247 WP 1998 6 19 MWEA98656 1 19980609 A 5730 5910465 SKIN DOUG DC9 DC932 3022066 WP RT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 RIGHT WING LOWER SKIN PANEL CORROSION AROUND FUEL PANEL NUMBER 1456. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR DOUBLER USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900248 19980619 00248 NM 1998 6 19 DHL98726006 1 19980611 A 5610 WINDOW BOEING 727 727228 NM LT COCKPIT FAILED A DHLA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 01 726DH 20409 ON TAKEOFF OUT OF SAT, SEALANT ON L1 WINDOW BLEW OUT. T/S SYSTEM FOUND ONLY SCOTCH CAL TAPE LOOSE. NO SEALANT MISSING AROUND WINDOW PERIMETER. PERFORMED PRESSURE CHECK, FOUND ONLY SMALL AIR SEEPS AT RIVETS ON L1 WINDOW POST AND TWO SCREW S ON METAL TRIM POST. APPLIED PRC SEALANT TO WINDOW TRIM SCREWS PER MM 20-60-4. PERFORMED PRESSURE CHECK TO CABIN 5.5 PSI DIFF, NO LEAKS NOTED. 2 L 7 3 4F A3WE 1998061900249 19980619 00249 NM 1998 6 19 P5CA9800815 1 19980425 A 5310 STRUCTURE BOEING 747 747122 1384872 NM BS 2460-2484 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 EMP CMPT STA 2460-2484 WL 366 CTR AREA SLIGHT CORROSION. CORROSION REMOVED AND REPROTECTED PER SRM 51- 10-01 AND 51-10-0 2. 2 L 7 4 4F A20WE 1998061900250 19980619 00250 NM 1998 6 19 P5CA9800816 1 19980425 A 5310 STRUCTURE BOEING 747 747122 1384872 NM BS 2436-2460 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION EMP COMPT BS 2436-2460 RT WL 334-350 AREA STR AND SUPPORT ROD. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900251 19980619 00251 NM 1998 6 19 P5CA9800817 1 19980425 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1168-1548 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION UPPER SKIN SURFACE SEVERAL LOCATIONS BS 1168 TO 1548. REMOVED CORROSION IAW SRM 51-10-01 AND PROTECTI VE FINISH APPLIED IAW SRM 51-14-11. 2 L 7 4 4F A20WE 1998061900252 19980619 00252 NM 1998 6 19 P5CA9800818 1 19980425 A 3620 69B400794 BRACKET BOEING 747 747122 1384872 NM RT PNEU DUCT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 PNEUMATIC DUCT RT PRESS TRANSMITTER SUPPORT BRACKET CRACKED. SUPPORT BRACKET REPLACED PER SRM 51-10-0. 2 L 7 4 4F A20WE 1998061900253 19980619 00253 NM 1998 6 19 P5CA9800819 1 19980425 A 3610 CF15200 CLAMP BOEING 747 747122 1384872 NM NR 3 AIR DUCT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 3 TRIM AIR DUCT CLAMP AROUND COUPLING INBD OF PAC VALVE CORRODED. CLAMP REPLACED IAW MM 36-11-01. 2 L 7 4 4F A20WE 1998061900254 19980619 00254 NM 1998 6 19 P5CA9800820 1 19980425 A 3610 DUCT BOEING 747 747122 1384872 NM NR 2 PACK CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 PACK DUCT CRACKED AT DISCHARGE TEMP SENSOR BOSS. DUCT REMOVED FOR WELDING PER OHM 36-10-04 REV 66. DETAILS REF FO RM 8130-3. 2 L 7 4 4F A20WE 1998061900255 19980619 00255 NM 1998 6 19 P5CA9800821 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1780-1800 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT LOWER FUSELAGE SKIN AT BS 1780 TO 1800 S33R - S32R. REPAIRED PER BOEING SRM 51-10-02. 2 L 7 4 4F A20WE 1998061900256 19980619 00256 NM 1998 6 19 P5CA9800822 1 19980425 A 5713 LONGERON BOEING 747 747122 1384872 NM BS 1330-1338 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON RT WING WW O/B LONGERON LOWER CHORD UPPER SURFACE BS 1330-1338. CORROSION REMOVED PER SRM 51-10-01 , 51-10-02. 2 L 7 4 4F A20WE 1998061900257 19980619 00257 NM 1998 6 19 P5CA9800823 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 800 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT FUSELAGE SKIN BS 800 BETWEEN S43L AND S44L. REPAIRED PER BOEING SRM 51-40-01. 2 L 7 4 4F A20WE 1998061900258 19980619 00258 NM 1998 6 19 P5CA9800824 1 19980425 A 5210 SKIN BOEING 747 747122 1384872 NM PAX DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIVETS CORRODED FWD UPPER CORNER FWD OF NR 1 LT ENTRY DOOR. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02 AND PAINTED PER 570-26-11. 2 L 7 4 4F A20WE 1998061900259 19980619 00259 NM 1998 6 19 P5CA9800825 1 19980425 A 5330 SKIN BOEING 747 747122 1384872 NM BS 760 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON RIVETS AND LIGHT SURFACE CORROSION AROUND RIVETS AT STA 760 STR 7A, 10 AND 11. REMOVED CORROSION A ND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900260 19980619 00260 NM 1998 6 19 P5CA9800826 1 19980422 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 854 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 SUPPORT BRACKETS FOR PANEL 191S AT BS 854 LBBL 5 TO RBBL 5 CORRODED. REPLACED BRACKETS PER BOEING SRM 51-10-08. 2 L 7 4 4F A20WE 1998061900261 19980619 00261 NM 1998 6 19 P5CA9800827 1 19980425 A 5230 HINGE BOEING 747 747122 1384872 NM CARGO DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LOWER FUSELAGE AFT CARGO DOOR HINGE SURFACE CORROSION AT FWD SIDE AND AFT SIDE. REMOVED CORROSION FROM DOOR HINGE AREA AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900262 19980619 00262 NM 1998 6 19 P5CA9800828 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 800 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AT BS 800 BBL 0 FORWARD OF CENTER ELECTRONICS ACCESS DOOR. REMOVED CORROSION PER BOEING SRM 51-10-01 REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1998061900263 19980619 00263 NM 1998 6 19 P5CA9800829 1 19980425 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING PANEL 671BT FOUND CRACK AT FASTENER HOLE. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900264 19980619 00264 NM 1998 6 19 P5CA9800830 1 19980422 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 910 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AT BS 910 RBBL 2 AFT SECTON OF SUPPORT BRACKET CORRODED. REPAIRED PER BOEING SRM 51-40-03, 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900265 19980619 00265 NM 1998 6 19 P5CA9800831 1 19980425 A 5532 PANEL BOEING 747 747122 1384872 NM VERT STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 VERTICAL STABILIZER PANEL 321D DENT FOUND. REPAIRED PANEL PER SRM 51-40-01. 2 L 7 4 4F A20WE 1998061900266 19980619 00266 NM 1998 6 19 P5CA9800832 1 19980425 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING PANEL 672DB HAS 2 HOLES. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900267 19980619 00267 NM 1998 6 19 P5CA9800833 1 19980422 A 7110 65B9151435 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DAMAGED AND LOOSE NR 2 ENGINE FAN COWL SUPPORT STRUCTURE AND UPPER SKIN. REPLACED SKIN AND DOUBLER PER BOEING SRM 51-10 -01. 2 L 7 4 4F A20WE 1998061900268 19980619 00268 NM 1998 6 19 P5CA9800834 1 19980425 A 3250 COLLAR BOEING 747 747122 1384872 NM NLG STEERING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON NOSE LANDING GEAR COLLAR ASSY IN FRONT OF LT STEERING. AREA CLEANED AND CORROSION REMOVED PER SRM 51-10-01 AND 51-26-11. 2 L 7 4 4F A20WE 1998061900269 19980619 00269 NM 1998 6 19 P5CA9800835 1 19980422 A 3213 STRUT BOEING 747 747122 1384872 NM MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON BODY LANDING GEAR STRUT AFT SIDE BELOW UPPER TORQUE LINK. CORROSION BLENDED OUT PER OHM 20-10-01 W ITHIN LIMITS PER 32-13-38. 2 L 7 4 4F A20WE 1998061900270 19980619 00270 NM 1998 6 19 P5CA9800836 1 19980425 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON RT WING LOWER SURFACE AT WBL 1140. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02 . 2 L 7 4 4F A20WE 1998061900271 19980619 00271 NM 1998 6 19 P5CA9800837 1 19980425 A 5414 COWL BOEING 747 747122 1384872 NM NR 1 ENGINE DISBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 1 ENG LT FAN COWL INNER SKIN IS DISBONDED AT THE BOTTOM EDGE. HOT BOND REPAIR C/OUT IAW SRM 51-40-06 FIG 17A. 2 L 7 4 4F A20WE 1998061900272 19980619 00272 NM 1998 6 19 P5CA9800838 1 19980425 A 5400 FAIRING BOEING 747 747122 1384872 NM NR 2 PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 PYLON V FAIRING IS DELAMINATED. REPAIRED IAW SRM 51-40-06 FIG 17. 2 L 7 4 4F A20WE 1998061900273 19980619 00273 NM 1998 6 19 P5CA9800839 1 19980425 A 5330 SKIN BOEING 747 747122 1384872 NM BS 520-740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSIN MD BS 520-740 S19L LAP JOINT INNER SURFACE. REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900274 19980619 00274 NM 1998 6 19 P5CA9800840 1 19980425 A 5280 DOOR BOEING 747 747122 1384872 NM RT MLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT BODY GEAR DOOR 762, FOUND CRACK ON AFT FACE. DOOR REPAIRED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998061900275 19980619 00275 NM 1998 6 19 P5CA9800841 1 19980425 A 7110 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE DISTORTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 ENG RT SIDE LOWER CHORD IS DISTORTED AT THE GUIDE PIN ARE JUST FWD OF NR 4 U BOLT. REPAIRED IAW SRM 51-10-02, 51-1 0-02 AND MM 71-11-06. 2 L 7 4 4F A20WE 1998061900276 19980619 00276 NM 1998 6 19 P5CA9800842 1 19980425 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION RT WING UPPER SKIN AT SEVERAL LOCATIONS FROM FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 51-10 -01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998061900277 19980619 00277 NM 1998 6 19 P5CA9800843 1 19980425 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION RT WING UPPER SKIN FROM FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 51-10-01, 51-10-20 AND MM 51-14-11. 2 L 7 4 4F A20WE 1998061900278 19980619 00278 NM 1998 6 19 P5CA9800844 1 19980425 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION UPPER RT WING SKIN WS 614 TO 862 FRONT SPAR TO MID SPAR. REMOVED CORROSION PER SRM 51-10-01, 51-10-02 AND MM 51-14-11. 2 L 7 4 4F A20WE 1998061900279 19980619 00279 NM 1998 6 19 P5CA9800845 1 19980422 A 3213 STRUT BOEING 747 747122 1384872 NM LT MLG CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION LEFT BODY LANDING GEAR SURFACE AT SIDE STRUT. CORROSION BLENDED PER BOEING OHM 20-10-01, 02 FOUND WIT HIN LIMITS PER 32-13-38. 2 L 7 4 4F A20WE 1998061900280 19980619 00280 NM 1998 6 19 P5CA9800846 1 19980425 A 5730 SKIN BOEING 747 747122 1384872 NM WS 862 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION RT WING UPPER SKIN SURFACE WS 862 TO 1168 FRONT SPAR TO REAR SPAR. REMOVED CORROSION PER SRM 51-10-01 , 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998061900281 19980619 00281 NM 1998 6 19 P5CA9800847 1 19980424 A 5414 65B907533 SKIN BOEING 747 747122 1384872 NM NR 1 PYLON DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 PYLON ACCESS PANEL 453CL IS DEBONDED, CRACKED AND RUBBER PADS ARE MISSING FROM PANEL LATCHES. REMOVED AND REPLACED DOOR PER MM 54-32-00. 2 L 7 4 4F A20WE 1998061900282 19980619 00282 NM 1998 6 19 P5CA9800848 1 19980424 A 5414 65B9031564 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON DISTORTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 PYLON ACCESS PANEL 463EL IS DISTORTED AT FWD END. REMOVED AND REPLACED PANEL PER MM 54-32-00. 2 L 7 4 4F A20WE 1998061900283 19980619 00283 NM 1998 6 19 P5CA9800849 1 19980424 A 7110 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE SPLIT A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 ENG RT SIDE COWL INNER SKIN HEAT SHIELD IS SPLIT BETWEEN 4 AND 5 FRAME. REPAIRED PER SRM 54-30-03 FIG 14. 2 L 7 4 4F A20WE 1998061900284 19980619 00284 NM 1998 6 19 P5CA9800850 1 19980424 A 5411 FRAME BOEING 747 747122 1384872 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 ENG LT SIDE COWL FOURTH FRAME FROM FRONT IS CRACKED ABOVE THE LATCH. REPAIRED PER SRM 51-10-01 P 18. 2 L 7 4 4F A20WE 1998061900285 19980619 00285 NM 1998 6 19 P5CA9800851 1 19980424 A 5280 FITTING BOEING 747 747122 1384872 NM NLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NLG W/W RT FWD DOOR FWD HINGE FITTING FWD ANGLE FOUND CRACK. 'T' ANGLE REPAIRED FROM BS 220-280 AT RT SIDE WALL LOWER PR HX R.S. R 53-18-33745. 2 L 7 4 4F A20WE 1998061900286 19980619 00286 NM 1998 6 19 P5CA9800852 1 19980422 A 3250 LINK BOEING 747 747122 1384872 NM NLG STEERING RUSTY A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION NOSE LANDING GEAR STEERING LINK ARM. TREATED PER BOEING OH MANUAL 20-10-01, 20-10-02. 2 L 7 4 4F A20WE 1998061900287 19980619 00287 NM 1998 6 19 P5CA9800853 1 19980424 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1580-1620 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AFT LOWER FUSELAGE AT STA 1580-1620 BOTTOM SIDE LBL 1 TO RBL 1. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900288 19980619 00288 NM 1998 6 19 P5CA9800854 1 19980422 A 3810 PANEL BOEING 747 747122 1384872 NM WATER SERVICE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DELAMINATED POTABLE WATER SERVICE PANEL. REPAIRED PER BOEING SRM 51-40-12 FIG 9. 2 L 7 4 4F A20WE 1998061900289 19980619 00289 NM 1998 6 19 P5CA9800855 1 19980424 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1660 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AFT LOWER FUSELAGE CORROSION AT LT LOWER BRACKET OF PANEL 193F AT STA 1660. REMOVED CORROSION FROM BRACKET AND REPROTEC TED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900290 19980619 00290 NM 1998 6 19 P5CA9800856 1 19980425 A 7830 SUPPORT BOEING 747 747122 1384872 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED CASCADE SUPPORT RING UPPER END. BLENDED OUT CRACK PER BOEING SRM 51-10-01 AND REPROTECTED PER 51-10-02. 2 L 7 4 4F A20WE 1998061900291 19980619 00291 NM 1998 6 19 P5CA9800857 1 19980424 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION RT WING UPPER SURFACE BETWEEN PANEL 671CT AND 671DT. CORROSION REMOVED AND REPLACED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900292 19980619 00292 NM 1998 6 19 P5CA9800858 1 19980424 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED NR 4 ENGINE SIDE COWL UPPER 3.5 BLEED EXHAUST. WELD REPAIRED PER BAC 5975. 2 L 7 4 4F A20WE 1998061900293 19980619 00293 NM 1998 6 19 P5CA9800859 1 19980424 A 5532 SKIN BOEING 747 747122 1384872 NM VERT STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 VERT STAB SKIN LEFT SIDE HAS DENT NEAR L/E STA 200-220 AT 2 LOCATIONS. DENT REPAIRED PER SRM 51-40-06 AND MM 51-26-11. 2 L 7 4 4F A20WE 1998061900294 19980619 00294 NM 1998 6 19 P5CA9800860 1 19980424 A 5730 PANEL BOEING 747 747122 1384872 NM WS 528-568 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING 3 EACH T/E UPPER PANEL FOUND DELAMINATED AT WS 528-568. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900295 19980619 00295 NM 1998 6 19 P5CA9800861 1 19980424 A 5720 STRAP BOEING 747 747122 1384872 NM WS 970 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING REAR SPAR UPPER SURFACE ATT STRAP FOUND CRACK AT WS 970. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900296 19980619 00296 NM 1998 6 19 P5CA9800862 1 19980424 A 5247 DOOR BOEING 747 747122 1384872 NM APU COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 APU LT COMPARTMENT ACCESS DOOR FWD LOWER FLANGE BENT AND CRACKED AND 1 RIVET MISSING. DOOR REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998061900297 19980619 00297 NM 1998 6 19 P5CA9800863 1 19980424 A 5247 DOOR BOEING 747 747122 1384872 NM APU COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 APU LT COMPARTMENT ACCESS DOOR LOWER FLANGE SLIGHTLY CRACKED AND LIFTED UP BETWEEN NR AND NR 4 VERTICAL FRAME. REPAIRED DOOR FLANGE PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900298 19980619 00298 NM 1998 6 19 P5CA9800864 1 19980422 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BENT/CRACKED NR 4 ENGINE RT SIDE COWL BRACKET FORWARD HOOK UPPER EDGE. 2 L 7 4 4F A20WE 1998061900299 19980619 00299 NM 1998 6 19 P5CA9800865 1 19980424 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING UPPER T/E PANEL FOUND DELAMINATED AT WBL 1160. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900300 19980619 00300 NM 1998 6 19 P5CA9800866 1 19980424 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING UPPER T/E PANEL FOUND DELAMINATED AT WBL 927. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900301 19980619 00301 NM 1998 6 19 P5CA9800867 1 19980424 A 5330 SKIN BOEING 747 747122 1384872 NM BS 480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON SKIN AT STA 480 BWL 122 RT SIDE ABOVE LAP JOINT. CORROSION REMOVED PER SRM 51-10-01 AND SRM 51-10- 02. 2 L 7 4 4F A20WE 1998061900302 19980619 00302 NM 1998 6 19 P5CA9800868 1 19980424 A 5753 SKIN BOEING 747 747122 1384872 NM TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 I/B AFT FLAP LWR SURFACE DELAMINATED IN 2 AREAS. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900303 19980619 00303 NM 1998 6 19 P5CA9800869 1 19980424 A 5532 SKIN BOEING 747 747122 1384872 NM VERT STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 VERT STAB T/E UPPER AREA HAS A DENT NEAR TOP OF UPPER RUDDER. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900304 19980619 00304 NM 1998 6 19 P5CA9800870 1 19980424 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2718 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BS 2718-2728 LT UPPER FUSELAGE AREA BWL 310 SLIGHT DENT. AREA SMOOTHED PER SRM 51-10-01 AND REPROTECTED PER SRM 51-10-0 2. 2 L 7 4 4F A20WE 1998061900305 19980619 00305 NM 1998 6 19 P5CA9800871 1 19980424 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1000 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 PANEL SUPPORT BRACKET RIB CORRODED AT STA 1000 BBL 18L AIR COND BAY. REPAIRED SUPPORT PER SRM 51-40-04. 2 L 7 4 4F A20WE 1998061900306 19980619 00306 NM 1998 6 19 P5CA9800872 1 19980422 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGIINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT NR 4 ENGINE RIGHT SIDE COWL OUTTER SKIN FORWARD UPPER EDGE. REPAIRED PER BOEING SRM 54-40-01 FIG 1. 2 L 7 4 4F A20WE 1998061900307 19980619 00307 NM 1998 6 19 P5CA9800873 1 19980424 A 5720 LONGERON BOEING 747 747122 1384872 NM WS 1284-1301 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON RT WING LANDING GEAR WW LONGERON BETWEEN ST 1284 AND 1301. CORROSION REMOVED AND TREATED PER SRM 5 1-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900308 19980619 00308 NM 1998 6 19 P5CA9800874 1 19980424 A 5320 PRESS WEB BOEING 747 747122 1384872 NM BS 1460-1480 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON LT BODY LANDING GEAR WW BETWEEN BS 1460-1480 ON OUTBD WALL BWL 200. CORROSION REMOVED AND TREATED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900309 19980619 00309 NM 1998 6 19 P5CA9800875 1 19980504 A 5320 WEB BOEING 747 747122 1384872 NM BS 320-340 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 M/D B/S 320-340 LT SIDE FLOOR SUPPORT WEB FOUND CRACKED AT S26L AREA. FLOOR SUPPORT WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900310 19980619 00310 NM 1998 6 19 P5CA9800876 1 19980424 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT INBOARD ELEVATOR T/E O/B AREA UPPER SURFACE COATING PEELING OFF. FIBERGLASS REPAIRED PER SRM 51-40-15 AND 51-26-11. 2 L 7 4 4F A20WE 1998061900311 19980619 00311 NM 1998 6 19 P5CA9800877 1 19980424 A 5522 SKIN BOEING 747 747122 1384872 NM RT ELEVATOR DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT I/B ELEVATOR E/B UPPER SURFACE 2 DENTS. FIBERGLASS REPAIRED PER SRM 51-40-15 AND MM 51-25-11. 2 L 7 4 4F A20WE 1998061900312 19980619 00312 NM 1998 6 19 P5CA9800878 1 19980424 A 5512 SKIN BOEING 747 747122 1384872 NM LT HORIZ STAB DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT STABILIZER ROOT UPPER SURFACE T/E FIXED PANEL HAS DENTS. FIBERGLASS REPAIRED PER SRM 51-40-15 AND MM 51-26-11. 2 L 7 4 4F A20WE 1998061900313 19980619 00313 NM 1998 6 19 P5CA9800879 1 19980501 A 5753 FLAP TRACK BOEING 747 747122 1384872 NM LT TE MIDFLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AFTER REMOVAL OF BEARING FROM L/W I/B MIDFLAP O/B SLIDING TRACK FWD ATTACH CORROSION FOUND IN BORE. TRACK REPAIRED IAW OHM 57-52-35. 2 L 7 4 4F A20WE 1998061900314 19980619 00314 NM 1998 6 19 P5CA9800880 1 19980424 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT INBOARD ELEVATOR OUTBD AREA T/E DAMAGED. FIBERGLASS REPAIR PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900315 19980619 00315 NM 1998 6 19 P5CA9800881 1 19980429 A 5753 FITTING BOEING 747 747122 1384872 NM LT TE FOREFLAP CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FOUND LEVEL 1 SURFACE CORROSION ON LEFT WING I/B FOREFLAP LOWER SURFACE CENTER AND O/B NR 3 SEQUENCE CARRIAGE FITTING A REA AFTER FOREFLAP REMOVAL. CORROSION REMOVED AND AREA REPROTECTED IAW SROM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900316 19980619 00316 NM 1998 6 19 P5CA9800882 1 19980424 A 5751 SKIN BOEING 747 747122 1384872 NM LT AILERON CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON LT WING OUTBD AILERON OUTBD LOWER T/E AREA. CORROSION REMOVED PER SRM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1998061900317 19980619 00317 NM 1998 6 19 P5CA9800883 1 19980422 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED NR 4 ENGINE RIGHT SIDE COWL BREATHER EXHAUST DUCT. WELD REPAIRED PER BAC 5975. 2 L 7 4 4F A20WE 1998061900318 19980619 00318 NM 1998 6 19 P5CA9800884 1 19980429 A 5753 FAIRING BOEING 747 747122 1384872 NM RT WING PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT WING NR 5 CANOE FAIRING TAIL CONE PUNCTURED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900319 19980619 00319 NM 1998 6 19 P5CA9800885 1 19980424 A 5247 DOOR BOEING 747 747122 1384872 NM APU COMPT CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON APU INLET DOOR EXTERIOR SURFACE. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900320 19980619 00320 NM 1998 6 19 P5CA9800886 1 19980424 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CRACKED NR 4 ENGINE SIDE COWL FWD FRAME FWD OF BREATHER DUCT. REPLACED ANGLE PER BOEING SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900321 19980619 00321 NM 1998 6 19 P5CA9800887 1 19980424 A 2910 BRACKET BOEING 747 747122 1384872 NM NR 1 HYD RESV CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 HYD RESERVOIR LT AFT ATTACH ANCHOR NUT SUPPORT BRACKET CRACKED. REPAIRED PER SRM 51-10-01 P 18. 2 L 7 4 4F A20WE 1998061900322 19980619 00322 NM 1998 6 19 P5CA9800888 1 19980429 A 5753 WEB BOEING 747 747122 1384872 NM LT TE FOREFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING I/B FOREFLAP I/B WEB FOUND CRACKED. REPAIRED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900323 19980619 00323 NM 1998 6 19 P5CA9800889 1 19980424 A 2910 BRACKET BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 PYLON HYD LINE SUPPORT BRACKET AT NAC ST 190 IS CRACKED. SUPPORT BRACKET REPLACED IAW SRM 51-10-01 P 18. 2 L 7 4 4F A20WE 1998061900324 19980619 00324 NM 1998 6 19 P5CA9800890 1 19980424 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT IN LOWER AFT FUSELAGE PANEL 293E. REPAIRED PER BOEING SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900325 19980619 00325 NM 1998 6 19 P5CA9800891 1 19980428 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING INBOARD FOREFLAP L/E, OUTBOARD OF NR 3 FLAP TRACK DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900326 19980619 00326 NM 1998 6 19 P5CA9800892 1 19980424 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT IN NR 4 ENGINE RIGHT FAN COWL OUTER SKIN. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1998061900327 19980619 00327 NM 1998 6 19 P5CA9800893 1 19980424 A 5280 ANGLE BOEING 747 747122 1384872 NM LT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING LANDING GEAR DOOR 733 AFT LOWER ANGLE CRACKED. AFT LOWER DOOR ATTACH ANGLE REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900328 19980619 00328 NM 1998 6 19 P5CA9800894 1 19980428 A 5753 SUPPORT BOEING 747 747122 1384872 NM LT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING INBOARD FOREFLAP UPPER T/E SUPPORT DELAMINATED (INBOARD OF NR 4 FLAP TRACK). REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900329 19980619 00329 NM 1998 6 19 P5CA9800895 1 19980424 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DELIMATED LOWER EDGE FWD AND AFT CORNERS NR 3 ENGINE RT FAN COWL. REPAIRED PER BOEING SRM 51-40-06 FIG 17. 2 L 7 4 4F A20WE 1998061900330 19980619 00330 NM 1998 6 19 P5CA9800896 1 19980428 A 5753 ANGLE BOEING 747 747122 1384872 NM LT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING INBOARD MIDFLAP INNERMOST RIB AFT ATTACHMENT ANGLE FOR AFT ACCORDIAN SEAL FITTING CRACKED AT LOWER BOLT HOLE. ANGLE REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900331 19980619 00331 NM 1998 6 19 P5CA9800897 1 19980424 A 5320 STRUCTURE BOEING 747 747122 1384872 NM BS 340-360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON MLG CAVITY AT RT SIDE BETWEEN STA 340-360 BWL 119 TO BWL 180. REMOVED CORROSION PER SRM 51-1 0-01 AND SRM 51-10-02. PAINTED PER MM 51-26-11. 2 L 7 4 4F A20WE 1998061900332 19980619 00332 NM 1998 6 19 P5CA9800898 1 19980428 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 520-740 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 MAIN DECK STRINGER R19 HAS CRACKED STRINGER HOLES, BS 520-560, 600-620, 640-660 AND 720-740. STRINGER 19R REPLACED FROM BS 520-BS 741 AS PER SRM 51-10-01 AND 53-10-03. 2 L 7 4 4F A20WE 1998061900333 19980619 00333 NM 1998 6 19 P5CA9800899 1 19980421 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LARGE DENT NR 3 ENGINE LEFT FAN COWL OUTER SURFACE. REPAIRED PER BOEING SRM 51-40-06 FIG 14. 2 L 7 4 4F A20WE 1998061900334 19980619 00334 NM 1998 6 19 P5CA9800900 1 19980421 A 7110 COWL BOEING 747 747122 1384872 NM NR 4 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LARGE DENT NR 4 ENGINE LEFT FAN COWL OUTER SKIN. REPAIRED PER BOEING SRM 51-40-06 FIG 14. 2 L 7 4 4F A20WE 1998061900335 19980619 00335 NM 1998 6 19 P5CA9800901 1 19980428 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 380-400 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 MAIN DECK LEFT OUTBOARD INTERCOSTAL FOUND CRACKED BS 380-400 S26L. FLOOR INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900336 19980619 00336 NM 1998 6 19 P5CA9800902 1 19980424 A 5280 SKIN BOEING 747 747122 1384872 NM NLG DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON NLG RT FWD DOOR 712 ON AFT TOP INSIDE SKIN. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900337 19980619 00337 NM 1998 6 19 P5CA9800903 1 19980428 A 5753 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON LEFT WING UPPER T/E WING SKIN EXTENSION AT WBL 515, OUTBOARD OF INBOARD AILERON. CORROSION R EMOVED AND AREA REPROTECTED IAW SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998061900338 19980619 00338 NM 1998 6 19 P5CA9800904 1 19980424 A 5280 SKIN BOEING 747 747122 1384872 NM RT MLG DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON RT WING GEAR WW DOOR 742 OUTSIDE SKIN. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. PAINTED P ER MM 51-26-11. 2 L 7 4 4F A20WE 1998061900339 19980619 00339 NM 1998 6 19 P5CA9800905 1 19980428 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 360-380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 MAIN DECK LEFT OUTBOARD FLOOR INTERCOSTAL FOUND CRACKED BS 360-380 S26L. INTERCOSTAL WEB REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900340 19980619 00340 NM 1998 6 19 P5CA9800906 1 19980421 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DAMAGED UPPER AFT CORNER NR 3 ENGINE RT FAN COWL. REPAIRED PER BOEING SRM 51-40-06 FIG 17. 2 L 7 4 4F A20WE 1998061900341 19980619 00341 NM 1998 6 19 P5CA9800907 1 19980424 A 5280 SKIN BOEING 747 747122 1384872 NM RT MLG DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON RT BODY GEAR DOOR 761 AFT FACE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02 AND PAINTED PER MM 51-26-11. 2 L 7 4 4F A20WE 1998061900342 19980619 00342 NM 1998 6 19 P5CA9800908 1 19980428 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 360-380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 MAIN DECK RIGHT OUTBOARD FLOOR INTERCOSTAL CRACKED BS 360-380 S26R. INTERCOSTAL REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900343 19980619 00343 NM 1998 6 19 P5CA9800909 1 19980424 A 5330 SKIN BOEING 747 747122 1384872 NM E/E DOORWAY CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AROUND CTR ELECTORNICS DOOR CUTOUT. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900344 19980619 00344 NM 1998 6 19 P5CA9800910 1 19980428 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON UPPER WING SKIN EXTENSION AT ILES 374. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10- 01, 51-10-02. 2 L 7 4 4F A20WE 1998061900345 19980619 00345 NM 1998 6 19 P5CA9800911 1 19980424 A 2150 69B430101 INLET FLAP BOEING 747 747122 1384872 NM NR 3 PACK CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 3 A/C PACK RAM AIR INLET FLAP SHAFT BEARINGS INBD AND OUTBD CORRODED. REPLACED NR 3 PACK RAM INLET FLAP SHAFT BEARIN GS IAW FAA FORM 8130-3 REF NO 001038. 2 L 7 4 4F A20WE 1998061900346 19980619 00346 NM 1998 6 19 P5CA9800912 1 19980428 A 5753 FAIRING BOEING 747 747122 1384872 NM RT TE FLAP PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT WING NR 5 FLAP FIXED FAIRING FOUND 2 PUNCH HOLES. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900347 19980619 00347 NM 1998 6 19 P5CA9800913 1 19980424 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT IN LOWER FORWARD FUSELAGE AT RT JACK PAD ACCESS PANEL. REPAIRED PER BOEING SRM 51-40-15 FIG 7. 2 L 7 4 4F A20WE 1998061900348 19980619 00348 NM 1998 6 19 P5CA9800914 1 19980428 A 7110 COWL BOEING 747 747122 1384872 NM NR 2 ENGINE PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 2 ENGINE RT SIDE COWL SKIN PUNCTURED AT 3 O'CLOCK POSITION. SKIN REPAIRED AS PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998061900349 19980619 00349 NM 1998 6 19 P5CA9800915 1 19980421 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT LOWER FUSELAGE PANEL 194D. REPAIRED PER BOEING SRM 51-40-15 FIG 7. 2 L 7 4 4F A20WE 1998061900350 19980619 00350 NM 1998 6 19 P5CA9800916 1 19980426 A 5522 SKIN BOEING 747 747122 1384872 NM LT ELEVATOR PEELING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 EMP - LT INBD ELEVATOR T/E O/B AREA UPPER SURFACE COATING PEELING. REPAIRED PER SRM 51-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998061900351 19980619 00351 NM 1998 6 19 P5CA9800917 1 19980428 A 7110 COWL BOEING 747 747122 1384872 NM NR 1 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 1 ENGINE LEFT SIDE COWL FORWARD UPPER EDGE DAMAGED. REPAIRED PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998061900352 19980619 00352 NM 1998 6 19 P5CA9800918 1 19980428 A 5400 FAIRING BOEING 747 747122 1384872 NM NR 2 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 2 PYLON LEFT SIDE SKIRT FAIRING AT NAC STA 153 CRACKED. REPAIRED AS PER SRM 51-40-02. 2 L 7 4 4F A20WE 1998061900353 19980619 00353 NM 1998 6 19 P5CA9800919 1 19980428 A 5230 FITTING BOEING 747 747122 1384872 NM CARGO DOOR RUSTY A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AFT CARGO DOOR NR 9 LATCH FITTING FOUND RUSTY ON BORE PIN AREA. SURFACE RUST CLEANED AND LATCH FITTING REPLACED REF SB 747-52-2186. 2 L 7 4 4F A20WE 1998061900354 19980619 00354 NM 1998 6 19 P5CA9800920 1 19980427 A 5321 FLOOR BOEING 747 747122 1384872 NM BS 460 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND UNDER FLOOR RIGHT HAND SIDE STA 460 WBL R199.8. CORROSION REMOVED AND AREA REPROTECTED AS PER S RM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900355 19980619 00355 NM 1998 6 19 P5CA9800921 1 19980427 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON PANEL 191S. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900356 19980619 00356 NM 1998 6 19 P5CA9800922 1 19980425 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING OUTBOARD FOREFLAP INBOARD LEADING EDGE DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900357 19980619 00357 NM 1998 6 19 P5CA9800923 1 19980427 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 PANEL 191P LEFT FOUND DELAMINATED. FIBERGLASS REPAIRED AS PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900358 19980619 00358 NM 1998 6 19 P5CA9800924 1 19980427 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING INBOARD FOREFLAP INBOARD EDGE LOWER SURFACE DELAMINATED. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998061900359 19980619 00359 NM 1998 6 19 P5CA9800925 1 19980427 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND ON PANEL 191S. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900360 19980619 00360 NM 1998 6 19 P5CA9800926 1 19980427 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND ON PANEL 193KK. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900361 19980619 00361 NE 1998 6 19 P5CA9800927 2 19980421 A 7250 65B90130178 BRACKET BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 1 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BROKEN BRACKET NR 1 ENGINE TOP SUPPORT TO PRECOOLER ASSY. REPLACED PER M/M 72-50-00. 2 L 7 4 4F 4 F A20WE E20EA 1998061900362 19980619 00362 NM 1998 6 19 P5CA9800928 1 19980421 A 7830 65B9740325 HOUSING BOEING 747 747122 1384872 NM NR 1 TR UNIT BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BROKEN NR 1 ENGINE DIAPHRAGM SEGMENT AT 9 O'CLOCK POSITION. REPLACED HOUSING ASSY PER M/M 78-31-15. 2 L 7 4 4F A20WE 1998061900363 19980619 00363 NM 1998 6 19 P5CA9800929 1 19980421 A 5246 65B9066527 HINGE BOEING 747 747122 1384872 NM NR 4 ENG OIL DR WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 4 ENGINE LEFT SIDE COWL OIL TANK ACCESS DOOR DENTED AND LOWER HINGE WORN. DOOR AND HINGES REPLACED PER MM 71-11-13 A ND SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900364 19980619 00364 NM 1998 6 19 P5CA9800930 1 19980427 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 770 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FWD CARGO COMPT SUPPORT ANGLE AT STA 770 LBL 20-30, FOUND DEFORMED AND CRACKED. SUPPORT ANGLE REFORMED PER SRM 51-40-01 . 2 L 7 4 4F A20WE 1998061900365 19980619 00365 NM 1998 6 19 P5CA9800931 1 19980427 A 5711 SPAR WEB BOEING 747 747122 1384872 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON AFT SPAR LWR WEB AT ATTACHMENT OF BONDING LEAD OF NR 2 AFT BOOST PUMP. REPAIRED CORROSION PE R SRM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1998061900366 19980619 00366 NM 1998 6 19 P5CA9800932 1 19980427 A 5311 FRAME BOEING 747 747122 1384872 NM BS 400 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FWD E/E COMPT RT CORRODED RIVETS AND FRAME AT STA 400 BLKHD FWD FACE BWL 150-118 LHR OF RH TUNNEL. CORROSION REMOVED AND REPLACED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900367 19980619 00367 NM 1998 6 19 P5CA9800933 1 19980426 A 7110 COWL BOEING 747 747122 1384872 NM NR 1 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 ENG RT SIDE COWL 7TH FRAME FROM FRONT HAS SEGMENT OF REINFORCING PLATE MISSING AT THE UPPER MOST ENT. PLATE REPLAC ED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900368 19980619 00368 NM 1998 6 19 P5CA9800934 1 19980422 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 7 CANOE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT WING NR 7 CANOE FAIRING EXTERNAL SURFACE FOUND SPONGY IN TWO LOCATIONS. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900369 19980619 00369 NM 1998 6 19 P5CA9800935 1 19980422 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 8 CANOE SPONGY A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT WING NR 8 CANOE FAIRING EXTERNAL SURFACE FOUND SPONGY. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900370 19980619 00370 NM 1998 6 19 P5CA9800936 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2400-2420 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND AT AFT FUSELAGE PREVIOUS REPAIR AREA, STATION 2400-2420 RBL 0 TO RBL 4. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900371 19980619 00371 NM 1998 6 19 P5CA9800937 1 19980427 A 5754 SKIN BOEING 747 747122 1384872 NM RT LE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING NR 16 KRUEGER FLAP CAVITY FWD CUTOUT FOUND CRACK AT ILES 542. REPAIRED IAW SRM 51-40-03 FIG 1. 2 L 7 4 4F A20WE 1998061900372 19980619 00372 NM 1998 6 19 P5CA9800938 1 19980422 A 5720 FITTING BOEING 747 747122 1384872 NM NR 5 CANOE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT WING NR 5 CANOE FAIRING FORWARD OUTBOARD HINGE MOUNT FITTING BROKEN. FAIRING SUPPORT REPLACED IAW MM 27-51-44. 2 L 7 4 4F A20WE 1998061900373 19980619 00373 NM 1998 6 19 P5CA9800939 1 19980427 A 5400 ANGLE BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 ENG HYDRAULIC RESERVOIR INBD AND OUTBD SUPPORT ANGLE CRACKED AT MID AREA. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998061900374 19980619 00374 NM 1998 6 19 P5CA9800940 1 19980422 A 5414 SKIN BOEING 747 747122 1384872 NM NR 1 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 1 PYLON RIGHT SAILPLANE DOOR PRESSURE RELIEF PANEL INNER SKIN IS CHAFED THROUGH. REPAIRED IAW SRM 51-40-06 AND 5 1-30-02. 2 L 7 4 4F A20WE 1998061900375 19980619 00375 NM 1998 6 19 P5CA9800941 1 19980422 A 5414 SKIN BOEING 747 747122 1384872 NM NR 1 PYLON DEBONDED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER ONE LEFT SAILPLANE DOOR OUTER SKIN IS DEBONDED. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998061900376 19980619 00376 NM 1998 6 19 P5CA9800942 1 19980422 A 5320 STRAP BOEING 747 747122 1384872 NM BS 940 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 STATION 940 LT FUSELAGE NR 2 INLET PACK PHELEM LOWER LEFT SUPPORT STRAP FOUND CORRODED. REPLACED SUPPORT STRAP AS PER S RM 51-10-01. 2 L 7 4 4F A20WE 1998061900377 19980619 00377 NM 1998 6 19 P5CA9800943 1 19980422 A 7110 BRACKET BOEING 747 747122 1384872 NM NR 3 COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 3 ENGINE RIGHT SIDE COWL LOWER EDGE AFT CORNER BRACKET CRACKED. REPAIRED IAW SRM 51-40-03 AND SRM 51-30-02. 2 L 7 4 4F A20WE 1998061900378 19980619 00378 NM 1998 6 19 P5CA9800944 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 680 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND AT STATION 680 BWL 91. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900379 19980619 00379 NM 1998 6 19 P5CA9800945 1 19980422 A 5320 RIVETS BOEING 747 747122 1384872 NM BS 145-160 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 CORROSION FOUND ON 26 RIVETS AT STA 145-160 285 LT AND RT SIDE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900380 19980619 00380 NM 1998 6 19 P5CA9800946 1 19980422 A 2510 STOWAGE BIN BOEING 747 747122 1384872 NM LT COCKPIT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 COCKPIT LEFT STA 370-400 EQUIP STOWAGE FOUND CRACKED IN TWO PLACES. REPAIRED AS PER MM 25-59-00. 2 L 7 4 4F A20WE 1998061900381 19980619 00381 NM 1998 6 19 P5CA9800947 1 19980427 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1580-1600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AT AFT CARGO COMPARTMENT STR S46R STA 1580-1600. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 A ND 51-10-02. 2 L 7 4 4F A20WE 1998061900382 19980619 00382 NM 1998 6 19 P5CA9800948 1 19980422 A 5400 BRACKET BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 1 PYLON CRACKED BRACKET AT MIDSPAR WEB STIFFENER AT NACELLE STA 211. BRACKET REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900383 19980619 00383 NM 1998 6 19 P5CA9800949 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 145-160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 SURFACE CORROSION FOUND ON 44 RIVETS AT STA 145-160 BWL 189 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED AS PER SR M 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900384 19980619 00384 NM 1998 6 19 P5CA9800950 1 19980422 A 2910 BRACKET BOEING 747 747122 1384872 NM NR 2 PYLON BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 2 PYLON HYDRAULIC PRESSURE LINE SUPPORT BRACKET BROKEN AT NACELLE STA 186. BRACKET REPLACED IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900385 19980619 00385 NM 1998 6 19 P5CA9800951 1 19980427 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1540-1560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT AT STR S46R STA 1540-1560. CORROSION REMOVED AND REPROTECTED AREA PERS RM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900386 19980619 00386 NM 1998 6 19 P5CA9800952 1 19980422 A 5320 RIVETS BOEING 747 747122 1384872 NM BS 145-160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 SURFACE CORROSION FOUND ON 32 RIVETS AT 145-160 BWL 205 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900387 19980619 00387 NM 1998 6 19 P5CA9800953 1 19980427 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1520-1540 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT STRINGER S46R STA 1520-1540. CORROSION REMOVED AND REPROTECTED AREA PE R SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900388 19980619 00388 NM 1998 6 19 P5CA9800954 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 145-160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 SURFACE CORROSION FOUND ON 52 RIVETS AT 145-160 BWL 270 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900389 19980619 00389 NM 1998 6 19 P5CA9800955 1 19980427 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1500-1520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND AT AFT CARGO COMPARTMENT STR S46R STA 1500-1520. CORROSION REMOVED AND REPROTECTED PER SRM 51-1 0-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900390 19980619 00390 NM 1998 6 19 P5CA9800956 1 19980427 A 5730 SKIN BOEING 747 747122 1384872 NM LT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND ON LT WING L/E UPPER INSPAR WING SKIN. CORROSION REMOVED AND AREA REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900391 19980619 00391 NM 1998 6 19 P5CA9800957 1 19980422 A 5320 RIVET BOEING 747 747122 1384872 NM BS 145-160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 SURFACE CORROSION FOUND ON 44 RIVETS AT 145-160 BWL 195 LT AND RT. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900392 19980619 00392 NM 1998 6 19 P5CA9800958 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND ON FUSELAGE SKIN FWD OF TOILET SERVICE PNL SECTION 42. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900393 19980619 00393 NM 1998 6 19 P5CA9800959 1 19980427 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1480-1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND IN AFT CARGO COMPT AT STRINGER S40L STA 1480-1500. CORROSION REMOVED AND REPROTECTED PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900394 19980619 00394 NM 1998 6 19 P5CA9800960 1 19980422 A 5412 BULKHEAD BOEING 747 747122 1384872 NM NR 1 PYLON WORN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 1 PYLON AFT 'V' FAIRING DEBONDING, DRAIN TUBE BROKEN, FWD BULKHEAD WORN AND SEALS SPLIT. REPAIRED AS PER SRM 51- 40-06. 2 L 7 4 4F A20WE 1998061900395 19980619 00395 NM 1998 6 19 P5CA9800961 1 19980422 A 7110 BRACKET BOEING 747 747122 1384872 NM NR 4 COWLING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 4 ENGINE LEFT SIDE COWL UPPER EDGE FWD CORNER BRACKET CRACKED. BRACKET REPAIRED AS PER SRM 54-10-03. 2 L 7 4 4F A20WE 1998061900396 19980619 00396 NM 1998 6 19 P5CA9800962 1 19980427 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1480-1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT STRINGER S46L STA 1480-1500. CORROSION REMOVED AND REPLACED PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900397 19980619 00397 NM 1998 6 19 P5CA9800963 1 19980425 A 5320 SPLICE BOEING 747 747122 1384872 NM BS 1241 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BS 1241 LEFT SIDE B/H SPLICE STRAP CRACKED AT FWD HOLE RUNNING AFT THROUGH THICKNESS. MODIFIED PER SB 747-53-2283. 2 L 7 4 4F A20WE 1998061900398 19980619 00398 NM 1998 6 19 P5CA9800964 1 19980427 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1480-1500 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND IN AFT CARGO COMPARTMENT STRINGER S46L STA 1480-1500. CORROSION REMOVED AND REPLACED PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900399 19980619 00399 NM 1998 6 19 P5CA9800965 1 19980427 A 5350 FAIRING BOEING 747 747122 1384872 NM RT VERT STAB BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT STABILIZER ROOT UPPER FAIRING FWD EDGE BROKEN. FIBERGLASS REPAIRED PER SRM 51-40-15 AND 51-24-11. 2 L 7 4 4F A20WE 1998061900400 19980619 00400 NM 1998 6 19 P5CA9800966 1 19980426 A 5320 SPLICE BOEING 747 747122 1384872 NM BS 1241 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT SIDE BS 1241 BH SPLICE STRAP CRACKED AT FWD HOLE THROUGH THICKNESS RUNNING AFT. MODIFIED PER SB 747-53-2283. 2 L 7 4 4F A20WE 1998061900401 19980619 00401 NM 1998 6 19 P5CA9800967 1 19980427 A 5312 BULKHEAD BOEING 747 747122 1384872 NM NLG WW CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT AND RIGHT NLG WHEEL WELL FORWARD CORNERS CANTED BULKHEAD AND SIDEWALL LOWER CHORD FOUND CRACKED. REPAIRED AS PER S B 747-53-2112. 2 L 7 4 4F A20WE 1998061900402 19980619 00402 NM 1998 6 19 P5CA9800968 1 19980427 A 5330 PANEL BOEING 747 747122 1384872 NM L1 DOORWAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 MAIN DECK 1L DOOR AFT CUTOUT PANEL FOUND SLIGHT CORROSION ADJACENT TO CENTER GUIDE TRACK FITTING MOUNTED AREA. CORROSIO N REMOVED AND REPROTECTED AREA PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900403 19980619 00403 NM 1998 6 19 P5CA9800969 1 19980422 A 5280 SKIN BOEING 747 747122 1384872 NM RT MLG DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT WING LANDING GEAR LOWER SLAVE DOOR 743 FOUND DELAMINATED ON INSIDE. REPAIRED AS PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998061900404 19980619 00404 NM 1998 6 19 P5CA9800970 1 19980425 A 5711 SPAR CHORD BOEING 747 747122 1384872 NM WS 822-840 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON RT WING LOWER CHORD SURFACE AT FSS 822-840. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900405 19980619 00405 NM 1998 6 19 P5CA9800971 1 19980505 A 7110 DUCT BOEING 747 747122 1384872 NM NR 2 COWLING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 2 ENGINE RT SIDE COWL BREATHER EXHAUST DUCT CRACKED AT FLANGE RADIUS. WELD REPAIRED PER BAC 5975 REV L. 2 L 7 4 4F A20WE 1998061900406 19980619 00406 NM 1998 6 19 P5CA9800972 1 19980425 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1335 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING GEAR WW BRACKET CRACKET BELOW GEAR OPP SEQUENCE VALVE AT DOOR CUTOUT STA 1335. BRACKET REPLACED PER SRM 51-10-0 1. 2 L 7 4 4F A20WE 1998061900407 19980619 00407 NM 1998 6 19 P5CA9800973 1 19980425 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING INBOARD FORE FLAP L/E DELAMINATED IN 3 AREAS BETWEEN NR 3 AND NR 4 FLAP TRACKS. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900408 19980619 00408 NM 1998 6 19 P5CA9800974 1 19980422 A 7110 DUCT BOEING 747 747122 1384872 NM NR 3 COWLING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 3 ENGINE RT SIDE COWL BREATHER EXHAUST DUCT CRACKED. WELD REPAIRED IAW BAC 5975 REV L. 2 L 7 4 4F A20WE 1998061900409 19980619 00409 NM 1998 6 19 P5CA9800975 1 19980425 A 5753 FAIRING BOEING 747 747122 1384872 NM LT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING OUTBOARD FORE FLAP L/E OB OF NR 2 CANOE FAIRING DELAMINATED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900410 19980619 00410 NM 1998 6 19 P5CA9800976 1 19980425 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE AFT FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING INBOARD AFT FLAP OUTBOARD LOWER EDGE DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900411 19980619 00411 1998 6 19 P5CA9800977 4 19980425 A 2360 BASE BOEING 747 747122 1384872 NM RUDDER CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND UPPER RUDDER NR 1 STATIC DISCHARGER BASE. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AN D 51-10-02. 2 L 7 4 4F A20WE 1998061900412 19980619 00412 NM 1998 6 19 P5CA9800978 1 19980425 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 7 TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RIGHT WING NR 7 T/E FLAP FWD FIXED FAIRING PUNCH MARK FOUND. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900413 19980619 00413 NM 1998 6 19 P5CA9800979 1 19980425 A 5350 FAIRING BOEING 747 747122 1384872 NM LT HORIZ STAB BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 EMPENNAGE LEFT STABILIZER ROOT UPPER FAIRING FORWARD EDGE BROKEN. REPAIRED AS PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900414 19980619 00414 NM 1998 6 19 P5CA9800980 1 19980425 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 2 CANOE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING NR 2 CANOE FAIRING O/B SIDE DELAMINATED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900415 19980619 00415 NM 1998 6 19 P5CA9800981 1 19980423 A 5755 SKIN BOEING 747 747122 1384872 NM NR 3 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING NR 3 SPOILER UPPER SURFACE FOUND DELAMINATED. SPOILER REPLACED IAW SRM 27-61-02. 2 L 7 4 4F A20WE 1998061900416 19980619 00416 NM 1998 6 19 P5CA9800982 1 19980425 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 1 CANOE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING NR 1 CANOE FAIRING O/B SIDE DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900417 19980619 00417 NM 1998 6 19 P5CA9800983 1 19980425 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE MID FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING INBOARD MID FLAP L/E DELAMINATED BETWEEN 3 AND 4 FLAP TRACKS. FIBERGLASS REPAIR PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900418 19980619 00418 NM 1998 6 19 P5CA9800984 1 19980425 A 5753 FAIRING BOEING 747 747122 1384872 NM NR 3 CANOE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING NR 3 CANOE FAIRING AREA OF DELAMINATION ON I/B SIDE. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900419 19980619 00419 1998 6 19 P5CA9800985 4 19980423 A 2360 BASE BOEING 747 747122 1384872 NM RT ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND ON RT OUTBOARD ELEVATOR NR 1, NR 2 AND NR 3 STATIC DISCHARGER BASES. CORROSION REMOVED AND AR EA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900420 19980619 00420 NM 1998 6 19 P5CA9800986 1 19980425 A 5753 SKIN BOEING 747 747122 1384872 NM LT TE MIDFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT WING INBD MID FLAP OUTBD L/E AND LWR SURFACE DELAMINATED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900421 19980619 00421 1998 6 19 P5CA9800987 4 19980423 A 2360 BASE BOEING 747 747122 1384872 NM LT ELEVATOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND ON LEFT OUTBOARD ELEVATOR NR 1, NR 2, NR 3 AND NR 4 STATIC DISCHARGER BASES. ONE BASE REPLACE D, CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900422 19980619 00422 NM 1998 6 19 P5CA9800988 1 19980425 A 5753 SKIN BOEING 747 747122 1384872 NM TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 IB FORE FLAP O/B LWR SURFACE DELAMINATED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900423 19980619 00423 NM 1998 6 19 P5CA9800989 1 19980423 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1940-1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND AT AFT LOWER FUSELAGE STA 1940-1960 STR S39R TO S40R. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900424 19980619 00424 NM 1998 6 19 P5CA9800990 1 19980423 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND AT AFT LOWER FUSELAGE STA 1960 STR S38R TO S39R. CORROSION REMOVED AND AREA REPROTECTED AS PE R SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900425 19980619 00425 NM 1998 6 19 P5CA9800991 1 19980424 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1920-1940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND AFT LOWER FUSELAGE AT STA 1920-1940 STR S38R. CORROSION REMOVED AND AREA REPROTECTED AS PER S RM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900426 19980619 00426 NM 1998 6 19 P5CA9800992 1 19980424 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1940-1980 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND AFT LOWER FUSELAGE AT STA 1940-1980 STR S51L AND S50L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900427 19980619 00427 NM 1998 6 19 P5CA9800993 1 19980423 A 5242 DOOR BOEING 747 747122 1384872 NM E/E COMPARTMENT DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 DENT MARK FOUND AT FORWARD EDGE OF CENTER E/E ACCESS DOOR. REPAIRED AS PER SRM 51-40-01. NO CRACKS FOUND. 2 L 7 4 4F A20WE 1998061900428 19980619 00428 NM 1998 6 19 P5CA9800994 1 19980423 A 7110 COWLING BOEING 747 747122 1384872 NM NR 2 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 2 ENGINE NOSE COWL FOUND DENTED AT 5 O'CLOCK POSITION. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998061900429 19980619 00429 NM 1998 6 19 P5CA9800995 1 19980423 A 5414 PANEL BOEING 747 747122 1384872 NM NR 1 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NUMBER 1 PYLON VALVE ACCESS PANEL CUTOUT DAMAGED AT AFT EDGE. ACCESS PANEL CUTOUT TRIMMED OFF AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998061900430 19980619 00430 NM 1998 6 19 P5CA9800996 1 19980423 A 5320 WALL BOEING 747 747122 1384872 NM BS 1394-1416 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL ONE CORROSION FOUND AT LEFT BODY LANDING GEAR WHEEL WELL OUTBOARD WALL BETWEEN BS 1394 AND 1416 BWL 200. CORROSIO N REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900431 19980619 00431 NM 1998 6 19 P5CA9800997 1 19980424 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1840-1860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON AFT LOWER FUSELAGE SKIN AT STA 1840-1860 STR S44L. CORROSION REMOVED AND REPROTECTED PER SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900432 19980619 00432 NM 1998 6 19 P5CA9800998 1 19980423 A 5240 SKIN BOEING 747 747122 1384872 NM NR 2 PYLON DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 2 ENG RT SAILPLANE DOOR INNER SKIN PUNCTURED. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998061900433 19980619 00433 NM 1998 6 19 P5CA9800999 1 19980423 A 3830 PANEL BOEING 747 747122 1384872 NM TOILET SVC CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON FWD TOILET SERVICE PANEL SURFACE INSIDE. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51 -10-02. 2 L 7 4 4F A20WE 1998061900434 19980619 00434 NM 1998 6 19 P5CA9801000 1 19980423 A 5400 BRACKET BOEING 747 747122 1384872 NM NR 1 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 1 PYLON GAP PANEL AREA CLOSURE SPAR RT SIDE FAIRING AFT BRACKET CRACKED. REPAIRED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900435 19980619 00435 NM 1998 6 19 P5CA9801001 1 19980423 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2320 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AFT FUSELAGE DENT MARK AT STA 2320 STR S48L-S49L. REPAIRED PER SRM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1998061900436 19980619 00436 NM 1998 6 19 P5CA9801002 1 19980423 A 7110 COWL BOEING 747 747122 1384872 NM NR 3 ENGINE DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 NR 3 ENG LT SIDE COWL FWD EDGE UPPER SECTION DENTED. REPAIRED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1998061900437 19980619 00437 NM 1998 6 19 P5CA9801003 1 19980423 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 RT WING SURFACE T/E FIXED PANEL AT I/B OF I/B AILERON SCREW MOUNTED AREA DAMAGED. REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998061900438 19980619 00438 NM 1998 6 19 P5CA9801004 1 19980423 A 5330 SKIN BOEING 747 747122 1384872 NM CARGO DOORWAY DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AFT LOWER FUSELAGE DENT AT BULK CARGO DOOR CUTOUT UPER AFT-END. REPAIRED IAW SRM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1998061900439 19980619 00439 NM 1998 6 19 P5CA9801005 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1820-1840 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND AFT LOWER FUSELAGE AT STA 1820-1840 STR S45L AND S46L. REMOVED CORROSION AND REPROTECTED PER SM R 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900440 19980619 00440 NM 1998 6 19 P5CA9801006 1 19980422 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1920-1940 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AFT LOWER FUSELAGE AT STA 1920-1940 STR S25L-S24L AFT OF MAIN CARGO DOOR LOWER CORNER. CORROSION REMO VED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900441 19980619 00441 NM 1998 6 19 P5CA9801007 1 19980422 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 PANEL SUPPORT STIFFENER AT STA 1000 BBL 55 CORNER HAS CORROSION. REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900442 19980619 00442 NM 1998 6 19 P5CA9801008 1 19980423 A 3231 BACB10AD5 ROD BOEING 747 747122 1384872 NM LT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LT BODY GEAR WW DOOR 745 ACT MANUAL SELECTOR ROD LOWER EYE END FOUND CORRODED. REPLACED ROD PER MM 32-35-08. 2 L 7 4 4F A20WE 1998061900443 19980619 00443 NM 1998 6 19 P5CA9801009 1 19980422 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1800-1820 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AFT LOWER FUSELAGE STA 1820-1800 STR S47L. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51- 10-02. 2 L 7 4 4F A20WE 1998061900444 19980619 00444 NM 1998 6 19 P5CA9801010 1 19980422 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AIR CONDITIONING PANEL 192AR SURFACE CORROSION ON EXTERIOR AROUND LATCHES. REMOVED CORROSION AND REPROTECTED PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900445 19980619 00445 NM 1998 6 19 P5CA9801011 1 19980422 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON PANEL 192H ON OUTER SKIN. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900446 19980619 00446 NM 1998 6 19 P5CA9801012 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2360 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON AFT FUSELAGE AT STA 2360 RBL 2O TO RBL 30. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998061900447 19980619 00447 NM 1998 6 19 P5CA9801013 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION AFT FUSELAGE AT STA 2360 LBL 40 T LBL 20. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-1 0-02. 2 L 7 4 4F A20WE 1998061900448 19980619 00448 NM 1998 6 19 P5CA9801014 1 19980422 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2340-2360 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION FOUND AFT FUSELAGE AT STA 2360-2340 RBL 60. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51 -10-02. 2 L 7 4 4F A20WE 1998061900449 19980619 00449 NM 1998 6 19 P5CA9801015 1 19980422 A 5320 BRACKET BOEING 747 747122 1384872 NM BS 1060 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 PANEL SUPPORT BRACKET RIB CORRODED AT STA 1060 BBL 15R AIR CONDITIONING BAY. PANEL REPAIRED PER SRM 51-40-04 FIG 1. 2 L 7 4 4F A20WE 1998061900450 19980619 00450 NM 1998 6 19 TSAA9833244 1 19980504 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 DURING SERVICE CHECK, FOUND NR 3 POSITION EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECKED OK. AI RCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900451 19980619 00451 NM 1998 6 19 TSAA0933251 1 19980508 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND NR 4 POSITION EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998061900452 19980619 00452 NM 1998 6 19 TSAA9833250 1 19980510 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY, INOPERABLE. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURN ED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998061900453 19980619 00453 NM 1998 6 19 TSAA9833253 1 19980509 A 3350 1000679 LIGHT BOEING 737 7372M6C 1384708 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 FORWARD PASSENGER EXIT DOOR LIGHT COVER BROKEN. REPLACED FORWARD EXIT IDENTIFIER EMERGENCY LIGHT. OPS CHECKED OK. AIR CRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900454 19980619 00454 NM 1998 6 19 TSAA9833252 1 19980508 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND NR 1 POSITION EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998061900455 19980619 00455 NM 1998 6 19 TSAA9833254 1 19980511 A 3350 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED RT AFT EMERGENCY EXIT LIGHT BATTERY DUE TO BEING LOW. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900456 19980619 00456 NM 1998 6 19 TSAA9833245 1 19980507 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY, INOPERABLE. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURN ED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998061900457 19980619 00457 NM 1998 6 19 TSAA9833246 1 19980507 A 3350 10000679 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY, INOPERABLE AND CRACKED. REPLACED LIGHT ASSY. OPS CHECKED OK . AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900458 19980619 00458 NM 1998 6 19 TSAA9833247 1 19980507 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOPERABLE. REPLACED BATTERY PACK, OPS CHECK GOOD. AIRCRAF T RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900459 19980619 00459 NM 1998 6 19 TSAA9851255 1 19980510 A 5320 FITTING BOEING 737 737230 NM BS 695 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 RIGHT SIDE MAIN LANDING GEAR SUPPORT FITTING CRACKED AT BS 695 AND INBOARD OF STR 18R. CRACKED CONFIRMED TO BE 2.25 INC HES LONG. REMOVED AND REPLACED SUPPORT FITTING PER SRM 51-10-1. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900460 19980619 00460 NM 1998 6 19 TSAA9857248 1 19980427 A 5730 SKIN BOEING 737 7372S5C 1384499 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 RIGHT WING UPPER SURFACE ABOVE NR 5 L/E SLAT ANTI-ICING DUCT FRONT SPAR CAP SHOWS BULGING AND POPPED RIVET. REPAIRED PE R ECO 2159R5 BETWEEN SLAT STA SS163.4 AND SS 189.4. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900461 19980619 00461 NM 1998 6 19 TSAA9857249 1 19980427 A 5730 SKIN BOEING 737 7372S5C 1384499 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 RIGHT WING UPPER SURFACE ABOVE NR 5 L/E SLAT ANTI-ICING DUCT FRONT SPAR CAP SHOWS BULGING AND POPPED RIVET. REPAIRED PE R ECO 2159R5 BETWEEN SLAT STA SS 189.4 AND STA SS 215.4. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900462 19980619 00462 NM 1998 6 19 TSAA9833257 1 19980514 A 3350 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 6 EMERGENCY LIGHT 'ALL IS WELL LIGHT' NOT COMING ON. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO S ERVICE. (X) 2 L 7 2 4F RT A16WE 1998061900463 19980619 00463 1998 6 19 TSAA9808002 4 19980520 A 3442 20671570153 RT UNIT DOUG DC9 DC931 3022065 WP RADAR SYSTEM FAILED A TWAA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 05 976Z 8109 47248 STL - FLR 647 - AFTER TAKEOFF, WEATHER RADAR SHOWS NO TARGETS ON DISPLAY. REPLACED RADAR RADIO TRANSMITTER MFG P/N 2067 157-0153. OP-15 5-20-97 STL CLOSED. (X) 2 L 7 2 4F A6WE 1998061900464 19980619 00464 WP 1998 6 19 TSAA9808001 1 19980519 A 3350 58222 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 416EA 47751 STL - FLT 625 - DURING PRE-FLIGHT INSPECTION, FOUND AFT EGRESS AND AFT OVERWING EMERGENCY LIGHTS INOPERABLE. REPLACED B ATTERY PACK MFG P/N 5822-2, FLEX CABLES MFG P/N 5853-1 AND P/N 5854-3. OP-15 12-17-97 STL CLOSED. (X) 2 L 7 2 4F RT A6WE 1998061900465 19980619 00465 NM 1998 6 19 TSAA9807911 1 19980511 A 5754 SKIN BOEING 767 767231 1385131 NM NR 7 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING CHECK-C., MAINTENANCE FOUND NR 7 LE SLAT WITH 4 INCH BY 3 INCH BULGE ON AFT SIDE OF SLAT WITH .3125 INCH IN HEIGHT, APPROX 5.50 FEET FROM INBD END AND 2 INCHES ABOVE SEAL. REMOVED DELAMINATED AREA, FOUND NO EVIDENCE OF WATER. INSTALLED CORE AND DOUBLER HOT BOND REPAIR PER SRM 51-70-10 AND APPLIED SEALANT. (X) 2 L 7 2 4F RT A1NM 1998061900476 19980619 00476 NM 1998 6 19 TWAA9807801 1 19980503 A 3350 S417N5095 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 JFK - DURING OVERNIGHT MAINTENANCE, FOUND EGRESS LIGHTS INOP ROWS 32-37 ON RT SIDE OF CABIN. REPLACED EGRESS LIGHT STRI P. (M) 2 L 7 2 4F RT A1NM 1998061900477 19980619 00477 WP 1998 6 19 TWAA9807705 1 19980508 A 5511 SPAR DOUG DC9 DC933F 302207A WP HORIZ STAB CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FUOND ON HORIZ STABILIZER LEFT UPPER SPAR CAP AFT BARREL NUT HOLE PITTED AT AFT LO WER POSITION, WHERE BOLT HOLE INTERSECTS WITH BARREL NUT HOLE. REPLACED LT UPPER LE SPAR CAP DUE TO CRACK PER SRM 51-01 , PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998061900478 19980619 00478 WP 1998 6 19 TWAA9807704 1 19980501 A 5320 ANGLE DOUG DC9 DC933F 302207A WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FLOORBOARD ATTACH CUSP ANGLE, LEFT SIDE, JUST FORWARD OF FS 965 BUL KHEAD. REPAIRED CUSP ANGLE PER SRM 53-05, PAGE 60E-60F, AND TWA STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900479 19980619 00479 WP 1998 6 19 TWAA9807703 1 19980501 A 5312 BULKHEAD ANGLE DOUG DC9 DC933F 302207A WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT FS 996 LBBL 57, SIDE WALL BELOW FLOOR, WEB SUPPORT ANGLE FOR BULKHEAD WIT H CRACK APPROX 3 INCHES LONG. REPAIRED PER SRM 53-05 FIG 93. (M) 2 L 7 2 4F A6WE 1998061900480 19980619 00480 WP 1998 6 19 TWAA9807702 1 19980424 A 5744 HINGE FITTING DOUG DC9 DC933F 302207A WP LT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING EYEBROW CRACK INDICATION AT LOWER OUTBOARD MOUNT HOLE FOR FLAP IDL ER HINGE. INSTALLED REPAIR PER ROD SKETCH 95-12-06-18, AND ARA 10991. (M) 2 L 7 2 4F A6WE 1998061900481 19980619 00481 NM 1998 6 19 TWAA9807701 1 19980503 A 3350 767 LIGHT BOEING 767 7673Y0 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 JFK - DURING OVERNIGHT MAINTENANCE, FOUND L2 CABIN DOOR EMERGENCY LIGHT INOPERATIVE ON TEST. RELAMPED THE LIGHT. (M) 2 L 7 2 4F RT A1NM 1998061900482 19980619 00482 NM 1998 6 19 TWAA9807601 1 19980512 A 3350 LIGHT BOEING 767 7673Y0 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 JFK - DURING ROUTINE MAINTENANCE CHECK, FOUND EGRESS LIGHTS INOP AT SEAT ROW 32 ON LEFT SIDE OF AIRCRAFT. REPAIRED BROK EN WIRE. (M) 2 L 7 2 4F RT A1NM 1998061900483 19980619 00483 WP 1998 6 19 TWAA9807602 1 19980512 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 110HM 49787 PBI - FLT 396 - EGRESS LIGHT REPORTED NOT ILLUMINATED AT ROW 23. REPAIRED WIRING AND REPLACED ONE LAMP. (M) 2 L 7 2 4F RT A6WE 1998061900484 19980619 00484 NM 1998 6 19 TWAA9807603 1 19980510 A 3244 6572761 TIRE BOEING 727 727231 1384079 NM LT MLG FAILED A TWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL C F G F.O.D. FLT CONT AFFECTED MULTIPLE FAILURE TO TAKEOFF 1 CE 05 54348 21967 SLC - FLT 342 - DURING TAKEOFF FROM SLT, THE LEFT INBOARD TIRE CAME APART AND WAS DIGESTED INTO THE NR 1 ENGINE. SHUT D OWN NR 1 ENGINE. FLT PROCEEDED TO HOLDING AREA TO DUMP FUEL, THEN RETURNED TO SLC. REPLACED WHEEL, REPAIRED DAMAGE TO TE FLAP, AND REPLACED ENGINE. (M) 2 L 7 3 4F A3WE 1998061900485 19980619 00485 WP 1998 6 19 TWAA9807604 1 19980508 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 69 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 955U 49427 MCI - DURING OVERNIGHT MAINTENANCE CHECK, FOUND SKIN AND FORMER DENTED AT STATION 69.5 ON RT SIDE BELOW PRESS DUCT, .5 I NCH WIDE BY 7 INCH LONG BY 5/8 INCH DEEP. NDT INSPECTION OF SKIN SHOWED NO CRACK OR CORROSION. REPLACED FORMER PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998061900486 19980619 00486 NM 1998 6 19 MZZA98156 1 19980428 A 5755 SKIN BOEING 727 727264 138408M NM NR 8 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING NR 8 SPOILER T/E UPPER SKIN. THE DAMAGED SKIN 9 INCHES BY 11.5 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X) 2 L 7 3 4F A3WE 1998061900487 19980619 00487 NM 1998 6 19 MZZA98158 1 19980430 A 5523 SKIN BOEING 727 727264 138408M NM RT ELEVATOR TAB PUNCTURED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PUNCTURE WAS FOUND ON RT ELEVATOR TAB UPPER SKIN AT ELEV STA 110. TH E DAMAGED SKIN 0.5 INCH DIAMETER WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X) 2 L 7 3 4F A3WE 1998061900488 19980619 00488 NM 1998 6 19 K3HA980082 1 19980613 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 VARIOUS EMEGENCY FLOOR LIGHTS MISSING BY FORWARD GALLEY, ALSO THE RETAINING STRIP IS LOOSE. REMOVED UPPER AND LOWER TRA CKS, INSTALLED NEW TRACK UPPER AND LOWER, CUT TO FIT OPS CHECK EMERGENCY LIGHT SYSTEM (LENS P/N 07912-3) (SOCKET P/N .81 69-01) (LAMP P/N 3071BPEGPL) REF MM 33-50-01. 2 L 7 3 4F A3WE 1998061900489 19980619 00489 1998 6 19 K3HA980083 2 19980612 A 7261 803689 SEAL BOEING 727 727225 1384077 NM NR 3 ENGINE FAILED A K3HA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 25 354PA 20624 AIRCRAFT DIVERTED TO ATLANTA DUE TO LOSS OF OIL NR 3 ENGINE. FOUND NR 3 ENGINE CSD GARLOCK SEAL LEAKING. REMOVED AND R EPLACED GARLOCK SEAL, RESET CSD. GROUND RUN UP, CHECKED NORMAL. NO LEAKS PER MM 72-61-0. 2 L 7 3 4F A3WE 1998061900490 19980619 00490 NM 1998 6 19 CALA9801049 1 19980613 A 3260 SWITCH BOEING 737 737130 1384435 NM NLG INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14206 19023 THE UNSAFE NOSE GEAR INDICATION ILLUMINATED ON APPROACH. TO EWR. THE GEAR WAS CYCLED, APPROPRIATE CHECKLISTS WERE COMPL IED WITH, AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG DOWNLOCK SWITCH AT FAULT. THE NLG DOWNLO CK SWITCH WAS REMOVED AND REPLACED IAW MM 32-61-51 AND ALL TESTS WERE GOOD. 2 L 7 2 4F A16WE 1998061900491 19980619 00491 NM 1998 6 19 CALA9801050 1 19980611 A 5343 FITTING BOEING 727 727224 1384076 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND LT MLG TRUNNION FITTING CORRODED. THE TRUNNION FITTING WAS REPAIRED IAW ECRA 5340-01320. 2 L 7 3 4F A3WE 1998061900492 19980619 00492 NM 1998 6 19 CALA9801051 1 19980611 A 5210 FITTING BOEING 727 727224 1384076 NM L-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79750 22452 INSPECTION FOUND A 2 INCH CRACK ON L-1 DOOR UPPER HINGE FITTING. THE CRACKED AREA WAS CUT OUT, AN ANGLE REPAIR WAS FABR ICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-40-5. 2 L 7 3 4F A3WE 1998061900493 19980619 00493 NM 1998 6 19 CALA9801052 1 19980612 A 3350 30043231 SOCKET GRIMES BOEING 737 737130 1384435 NM CABIN CORRODED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77204 19021 INSPECTION FOUND AFT EXTERIOR EXIT SLIDES INOPERATIVE BOTH SIDES. THE RIGHT EXTERIOR SLIDE LIGHT SOCKET WAS CORRODED. T HE SOCKET WAS REPLACED. IN ADDITION, BATTERY PACK M572 WAS REPLACED, OPERATION OF BOTH LIGHTS CHECKED GOOD. 2 L 7 2 4F A16WE 1998061900494 19980619 00494 WP 1998 6 19 CALA9801053 1 19980612 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 740-755 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 740 TO 755, LONGERON 29L TO 29R. THE CORRODED AREA WAS CUT OUT, A REPAIR SPLICE DOUBLER AND EXTERNAL REPAIR SPLICE WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-04, FIGURE 42, AND 51-30-1. 2 L 7 2 4F A6WE 1998061900495 19980619 00495 WP 1998 6 19 CALA9801054 1 19980612 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 627-657 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT FLOOR MEMBRANE DISTORTED AND CRACKED AT STA 627 TO 657. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR WEB WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900496 19980619 00496 WP 1998 6 19 CALA9801055 1 19980612 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBEAM CORRODED AT BS 980, LBL 12. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 53-05, FI GURE 20A, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900497 19980619 00497 WP 1998 6 19 CALA9801056 1 19980613 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 639 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 3 INCH CRACK IN CABIN FRAME AT STA 639, LBL 60. THE CRACK WAS STOP DRILLED IAW SRM 53-03, PAGE 40. A N ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-03. 2 L 7 2 4F A6WE 1998061900498 19980619 00498 WP 1998 6 19 CALA9801057 1 19980613 A 5320 JAMB DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2.25 INCH CRACK IN FORWARD PASSENGER ENTRANCE DOOR JAMB UPPER FORWARD CORNER INSIDE SKIN. A REPAIR W AS INSTALLED IAW ECRA 5330-02619 AND SRM 53-05, FIGURE 25A. A DIP WAS ISSUED FOR PERMANENT REPAIR PRIOR TO 1,000 LANDIN GS OR NEXT SCHEDULED S-CHECK OR HIGHER, WHICHEVER COMES FIRST. 2 L 7 2 4F A6WE 1998061900499 19980619 00499 WP 1998 6 19 CALA9801058 1 19980613 A 5280 SKIN DOUG DC9 DC932 3022066 WP NLG DOOR DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT NLG REAR DOOR DAMAGED BY LIGHTNING STRIKE. THE DAMAGED SKIN WAS REMOVED AND REPAIR SKIN WAS INSTALL ED IAW SRM 52-81-0 AND 51-30-2. 2 L 7 2 4F A6WE 1998061900500 19980619 00500 WP 1998 6 19 CALA9801059 1 19980613 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND THREE DENTS WITH A CRACK IN FLOORBOARD PANEL NR 83. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW GMM 10-900-01, PAGE 1, SRM 51-70-1, 51-10-3, AND 53-05. 2 L 7 2 4F A6WE 1998061900501 19980619 00501 WP 1998 6 19 CALA9801060 1 19980614 A 5720 BRACKET DOUG DC9 DC932 3022066 WP WS 332-232 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND TWO CRACKS IN RT WING FLAP LEADING EDGE SUPPORT BRACKET AT XRS 332 TO 232. THE SUPPORT BRACKET WAS REM OVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-20-0, 51-10-2, 51-10-1, AND 51-10-3. 2 L 7 2 4F A6WE 1998061900502 19980619 00502 WP 1998 6 19 CALA9801061 1 19980614 A 5320 CLIP DOUG DC9 DC932 3022066 WP BS 980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK OUT OF UPPER FASTENER HOLE IN SHEAR CLIP AT FS 980 BELOW LONGERON 14L. THE SHEAR CLIP W AS REMOVED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-22, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998061900503 19980619 00503 1998 6 19 9809519151 4 19980611 A 3442 RADAR DOUG DC9 DC914 3022034 WP COCKPIT FAILED A NWAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 01 8909E 45770 WEATHER RADAR SYSTEM FAILED AFTER TAKEOFF. FLIGHT WAS RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE D RADAR TRANSCEIVER AND ANTENNA, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998061900504 19980619 00504 WP 1998 6 19 9809521149 1 19980611 A 2910 LINE DOUG DC10 DC1040 3023508 WP NR 1 HYD SYST FAILED A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 149US 46758 DURING CRUISE, NR 1 HYDRAULIC SYSTEM INDICATED TOTAL LOSS OF FLUID. FLIGHT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENGINE HYDRAULIC KIT AND REPLACED LINE IN CENTER WHEEL WELL. LEAK AND OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998061900505 19980619 00505 NE 1998 6 19 9809536614 2 19980610 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7J 52054 NE NR 4 FLAMEDOUT A NWAA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 GL 01 614US 20359 686103 WHILE AT CRUISE, THE NR 4 ENGINE EXPERIENCED A FLAME-OUT. THE RESTART WAS SUCCESSFUL AND THE FLIGHT CONTINUED TO NRT WI THOUT FURTHER DIFFICULTY. THE ENGINE OPERATION WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE E NGINE WITH NO DEFECTS NOTED. THE MAIN FUEL FILTER AND TT2 SENSOR WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E20EA 1998061900506 19980619 00506 NM 1998 6 19 9809546641 1 19980612 A 2612 FIRE WARNING BOEING 747 747212B 1384886 NM NR 1 ENGINE ACTIVATED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 01 641NW 21941 DURING TAKEOFF, THE NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AND THE FIRE BELL SOUNDED. AIRCRAFT ABORTED TAKEOFF RESU LTING IN 10 BLOWN TIRES. AIRCRAFT STOPPED ON TAXI-WAY WHERE THE PASSENGERS WERE SAFELY DEPLANED AND TRANSPORTED BACK TO THE TERMINAL. REPLACED THE NR 1 ENGINE PRESSURE REGULATING VALVE AND CLAMP, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998061900507 19980619 00507 NM 1998 6 19 UPS98226878 1 19980525 A 5312 BULKHEAD BOEING 727 72725C 138400H NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-C, CRACK ON FWD PRESSURE BULKHEAD, BS 178 AT WL 207.5, RBL 5. BULKHEAD REPAIRED IAW UPS EO B727-5310-42 90. 2 L 7 3 4F A3WE 1998061900508 19980619 00508 WP 1998 6 19 UPS98826879 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 741.250 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E RIB UPPER ARM IS CRACKED AT THE AFT END AT STA XFS741, 250. STOP DRILLED CRACK AND REPAI RED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900509 19980619 00509 WP 1998 6 19 UPS98826880 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 735 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING LWR L/E RIB IS CRACKED AT THE AFT END AT STA XFS.735.000. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900510 19980619 00510 WP 1998 6 19 UPS98826881 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 672.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E UPPER RIB IS CRACKED AT THE AFT END AT STA XFS672.500. STOP DRILLED CRACK AND REPAIRED I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900511 19980619 00511 WP 1998 6 19 UPS98826882 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS.660.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900512 19980619 00512 WP 1998 6 19 UPS98826883 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS.653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900513 19980619 00513 WP 1998 6 19 UPS98826884 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS 653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900514 19980619 00514 WP 1998 6 19 UPS98826885 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS635.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900515 19980619 00515 WP 1998 6 19 UPS98826886 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS.622.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900516 19980619 00516 WP 1998 6 19 UPS98826887 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS.610.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900517 19980619 00517 WP 1998 6 19 UPS98826888 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 822 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS.822.800, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900518 19980619 00518 WP 1998 6 19 UPS98826889 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS810.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900519 19980619 00519 WP 1998 6 19 UPS98826890 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 776 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E STA XFS776.00, THE LWR L/E RIB IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2- 0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900520 19980619 00520 WP 1998 6 19 UPS98826891 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 822.8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS822.800, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900521 19980619 00521 WP 1998 6 19 UPS98826892 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 797.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS797.500, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900522 19980619 00522 WP 1998 6 19 UPS98826893 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 828.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS828.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900523 19980619 00523 WP 1998 6 19 UPS98826894 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 828.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS828.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900524 19980619 00524 WP 1998 6 19 UPS98826895 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 791.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS791.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900525 19980619 00525 WP 1998 6 19 UPS98826896 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 766.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS766.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900526 19980619 00526 WP 1998 6 19 UPS98826897 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 747.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS747.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900527 19980619 00527 WP 1998 6 19 UPS98826898 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 876. CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS876.00, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPA IRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900528 19980619 00528 WP 1998 6 19 UPS98826899 1 19980609 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS.760.00, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900529 19980619 00529 WP 1998 6 19 UPS98826900 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 603.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS603.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900530 19980619 00530 WP 1998 6 19 UPS98826901 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS597.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900531 19980619 00531 WP 1998 6 19 UPS98826903 1 19980603 A 5330 57799133N1 SKIN DOUG DC8 DC873F 302199F WP BS 450-610 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, FUSELAGE SKIN AT STA 450 TO 610 STR 33R-33L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW DWG 5779913 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900532 19980619 00532 WP 1998 6 19 UPS98826904 1 19980603 A 5320 3755841501 FITTING DOUG DC8 DC873F 302199F WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, STA 1200 AT LONG 34R, THE BACK-UP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755841. 2 L 7 4 4F RT 4A25 1998061900533 19980619 00533 WP 1998 6 19 UPS98826905 1 19980615 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 867UP 45967 INSPECTION TYPE-PRE, PREFLIGHT FOUND EMERGENCY LIGHT BATT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY, OPS CHECK OK. (P/N 5708458-503) (S/N UPS 3310) ON, (S/N FTL132) OFF. 2 L 7 4 4F RT 4A25 1998061900534 19980619 00534 EU 1998 6 19 98FDEA00399 1 19980612 A 2131 82010B040901 CONTROLLER AIRBUS 310 A310203 EU CABIN FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 424FE 241 ON DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE, THE NR 2 FWD OUTFLOW VALVE INDICATED OPEN AND RED ON ECAM. REMOVED AND RE PLACED NR 2 PRESSURIZATION CONTROLLER. 2 L 7 2 4F RT A35EU 1998061900535 19980619 00535 EU 1998 6 19 98FDEA00400 1 19980614 A 3150 20662155 ECAM AIRBUS 300 A300F4605R 3930327 EU COCKPIT SMOKING A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 670FE 777 LEFT ECAM SCREEN WENT BLANK, ABOUT TWO MINS LATER, SMOKE STARTED TO COME OUT OF FORWARD PANEL BEHIND ECAM SCREEN. REMOV ED AND REPLACED LEFT HAND ECAM DISPLAY UNIT, GROUND TESTS NORMAL. 2 L 7 2 4F RT A35EU 1998061900536 19980619 00536 WP 1998 6 19 MWEA98657 1 19980614 A 5712 9919306403 RIB DOUG DC9 DC932 3022066 WP WS 214 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FOUND 1 INCH CRACK ON LEFT WING NUMBER 2 SLAT DRIVE OUTBOARD RIB AT XRS 214. MTC FABRICATED AND INSTALLED NEW NOSE RIBS . 2 L 7 2 4F A6WE 1998061900537 19980619 00537 WP 1998 6 19 MWEA98658 1 19980614 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 940 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 215ME 47744 FOUND A DOUBLE DRILLED HOLE THROUGH A FLANGE OF LONGERON AT STATION 940 AT LONGERON 8R. MTC FABRICATED AND INSTALLED NE W SECTION OF LONGERON. 2 L 7 2 4F A6WE 1998061900538 19980619 00538 WP 1998 6 19 MWEA98659 1 19980611 A 2560 591769037 COVER DOUG DC9 DC914 3022034 WP GALLEY SLIDE FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 800ME 45842 THE GALLEY SLIDE FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998061900539 19980619 00539 WP 1998 6 19 MWEA98660 1 19980610 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP BS 294 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FOUND SLIGHT DENT ON SKIN AT FS 294 BELOW LONGERON 25L. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998061900540 19980619 00540 WP 1998 6 19 MWEA98661 1 19980610 A 5330 5911412191 SKIN DOUG DC9 DC932 3022066 WP BS 351 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FUSELAGE SKIN IS DENTED AT FS 351 BELOW LONGERON 26L. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998061900541 19980619 00541 WP 1998 6 19 MWEA98662 1 19980610 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP BS 370 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE FUSELAGE SKIN IS DENTED AT FS 370 ABOVE LONGERON 20L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998061900542 19980619 00542 WP 1998 6 19 MWEA98663 1 19980610 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP BS 442 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE FUSELAGE SKIN IS DENTED AT FS 442 AT LONGERON 22L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998061900543 19980619 00543 WP 1998 6 19 MWEA98664 1 19980610 A 5320 99579165 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 294 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE SHEAR TIE IS DENTED INWARD AT STATION 294 BETWEEN L20L AND L19L. MTC SPLICED IN NEW SECTION. 2 L 7 2 4F A6WE 1998061900544 19980619 00544 WP 1998 6 19 MWEA98665 1 19980610 A 5320 99579165 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 351 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE SHEAR TIE CRACKED AT STATION 351 BETWEEN LONGERON 26L AND 27L. MTC SPLICED IN NEW SECTION. 2 L 7 2 4F A6WE 1998061900545 19980619 00545 WP 1998 6 19 MWEA98666 1 19980610 A 5313 29127274 LONGERON DOUG DC9 DC932 3022066 WP BS 427-446 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 22L IS DENTED BETWEEN STATION 427 AND 446. MTC SPLICED IN LONGERON SECTION. 2 L 7 2 4F A6WE 1998061900546 19980619 00546 WP 1998 6 19 MWEA98667 1 19980610 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 300 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 23L IS DENTED AT FS 300. MTC SPLICED IN NEW LONGERON SECTION. 2 L 7 2 4F A6WE 1998061900547 19980619 00547 WP 1998 6 19 MWEA98668 1 19980610 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 450 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 24L IS CRACKED AT FS 450. MTC SPLICED IN LONGERON SECTION. 2 L 7 2 4F A6WE 1998061900548 19980619 00548 WP 1998 6 19 MWEA98669 1 19980610 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP BS 451 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FUSELAGE SKIN IS DENTED AT FS 451 BELOW LONGERON 24L. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998061900549 19980619 00549 WP 1998 6 19 MWEA98670 1 19980610 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP BS 351 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FUSELAGE SKIN IS DENTED AT FS 351 AT LONGERON 22L. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998061900550 19980619 00550 WP 1998 6 19 MWEA98671 1 19980610 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP BS 300 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE FUSELAGE SKIN IS DENTED AT FS 300 ABOVE AND BELOW LONGERON 23L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998061900551 19980619 00551 WP 1998 6 19 MWEA98672 1 19980610 A 5330 5911410175 SKIN DOUG DC9 DC932 3022066 WP BS 296 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 THE FUSELAGE SKIN IS DENTED AT FS 296 BETWEEN LONGERON 19 AND 20L. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998061900552 19980619 00552 WP 1998 6 19 MWEA98673 1 19980610 A 5330 59114013 SKIN DOUG DC9 DC932 3022066 WP BS 214 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 FUSELAGE SKIN IS DENTED AT FS 214 ABOVE LONGERON 21L AND AT STATION 218 BETWEEN LONGERON 24 AND 25L. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998061900553 19980619 00553 WP 1998 6 19 MWEA98674 1 19980610 A 5313 27779225 LONGERON DOUG DC9 DC932 3022066 WP BS 452 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 206ME 47791 LONGERON 25L IS DENTED INWARD APPROXIMATELY .125 INCH AT STATION 452. MTC SPLICED IN NEW SECTION OF LONGERON. 2 L 7 2 4F A6WE 1998061900554 19980619 00554 NM 1998 6 19 DL72L981240 1 19980610 A 5512 PANEL BOEING 727 727232 1384082 NM LT HORIZ STAB HOLE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 503DA 21305 FOUND ON F1 LETTER CHECK, HOLE .25 IN LOWER LT HORIZONTAL STAB ACCESS PANEL INBD OF ELEV PWR PACK. INSTALLED DOUBLER PE R SRM 55-20-3. 2 L 7 3 4F A3WE 1998061900555 19980619 00555 NM 1998 6 19 DL72S981243 1 19980611 A 5522 SKIN BOEING 727 727232 1384082 NM LT/ RT ELEV DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 FOUND AT LETTER CHECK C1, 30 OF LEFT AND 24 OF RIGHT ELEVATOR DELAMINATED AT TRAILING EDGE. REPAIR PER M/M 55-20-0. 2 L 7 3 4F A3WE 1998061900556 19980619 00556 NM 1998 6 19 DL72W981244 1 19980529 A 5343 6517692 TRUNNION BOEING 727 727247 138408F NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 RT MLG TRUNNION BEAM SUPPORT FITTING AT FS 940 FOUND WITH 1.5 INCH FATIGUE CRACK ON INBRD SURFACE, WL 190. REPAIRED WIT H FABRICATED DOUBLER PER ER/A 373040-14. CRACK FOUND DURING MID VISIT INSPECTION. 2 L 7 3 4F A3WE 1998061900557 19980619 00557 NM 1998 6 19 DL757981246 1 19980609 A 5330 143N33203 SKIN BOEING 757 757232 1384965 NM BS 625 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 666DN 25034 THE FUSELAGE SKIN AT FS 625 WAS FOUND WITH AN OIL CANNED DENT BETWEEN STRINGERS 16L AND 17L. THE DAMAGED AREA OF SKIN W AS CUTOUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 365010-14. 2 L 7 2 4F RT A2NM 1998061900558 19980619 00558 NM 1998 6 19 DL72K981247 1 19980609 A 5320 65562312 STRAP BOEING 727 727232 1384082 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 471DA 20748 THE R1 DOOR SURROUND DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE SKIN WAS CUT T O ACCESS THE BEAR STRAP UNDERNEATH. THE CRACK WAS CUT OUT OF THE BEAR STRAP AND AN EXTERNAL REPAIR DOUBLER AND TRIPLER WERE INSTALLED PER BAC S/B 727-53-0136. THE REPAIR WAS DOCUMENTED PER ER/A 364990-14. 2 L 7 3 4F A3WE 1998061900559 19980619 00559 NM 1998 6 19 DL72L981248 1 19980612 A 5320 WEB BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 511DA 21313 FOUND AT D-1 LETTER CHECK, WEB CRACKED RT FWD LOWER AFT AIRSTAIR AREA. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998061900560 19980619 00560 NM 1998 6 19 DL72S981249 1 19980612 A 2910 LINE BOEING 727 727232 1384082 NM B-HYD SYST LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 470DA 20747 DURING DESCENT, SYSTEM-B HYDRAULIC PRESSURE WAS LOST. ACCOMPLISHED APPLICABLE ABNORMAL PROCEDURES, HAD TO USE PNEUMATIC BRAKES, B-FLUID QTY REMAINED ABOVE 1.5 GALLONS. FOUND CASE DRAIN LINE FOR NR 2 B-HYD PUMP LOOSE AND LEAKING AT PUM P P RESSURE LINE DISCONNECT BRACKET. SECURED LINE, PRESSURIZED SYSTEM, NO LEAKS FOUND. 2 L 7 3 4F A3WE 1998061900561 19980619 00561 NM 1998 6 19 DL72S981250 1 19980612 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 520DA 21471 EMERGENCY LIGHT INOP ROW 12 TO 19. 2 L 7 3 4F A3WE 1998061900562 19980619 00562 WP 1998 6 19 DLL19981251 1 19980612 A 2910 LINE 1802921 LKHEED 1011 10113853 5265020 WP CENTER HYD SECT BROKEN A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 754DL 193Y1181 C-SYSTEM HYD RESERVOIR QTY SLOWLY DROPPED TO ZERO, ONE AND ONE HALF HOURS. SWITCHING OFF PUMPS DID NOT STOP GAUGE DROP. LOW QTY LIGHT ILLUMINATED. FOUND BROKEN LINE IN HYD BAY. REPLACED LINE. 2 L 7 3 4F A23WE 1998061900563 19980619 00563 NM 1998 6 19 DL73S981252 1 19980613 A 3244 TIRE B737NN BOEING 737 737232 1384475 NM NLG FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 328DL DL166 23100 AT 120 KT ON TAKEOFF, SEVERE NOSEWHEEL SHIMMY AND LOUD THUMP UNDER COCKPIT. AIRSPEED STAGNATED THROTTLES FIREWALLED; EG T RED LINED AT 635 BOTH ENGINES FOR ABOUT 5 SECONDS. RIGHT NOSE TIRE THREW IT'S CAP. REPLACED BOTH NOSE WHEEL ASSY. I NSPECTED A/C FOR DAMAGE FROM CAP. MTC PERFORMING INSPECTION TO BOTH ENGINES PER M/M. REPLACED BOTH ENGINES. 2 L 7 2 4F RT A16WE 1998061900564 19980619 00564 NM 1998 6 19 DL72W981254 1 19980612 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 2810W 20648 RT OVERWING EMERG EXIT LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998061900565 19980619 00565 NM 1998 6 19 DL72S981256 1 19980613 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA 424 20746 TRACK LIGHTING OUT BETWEEN ROW 12DEF AND 19DEF. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 1998061900566 19980619 00566 NM 1998 6 19 DL72S981257 1 19980614 A 3350 60540 RACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA 20746 EMER EXIT FLOOR TRACK WILL NOT SHUT OFF. REPLACED EMER LIGHT RACK IN FIRST CLASS OVERHEAD CEILING. 2 L 7 3 4F A3WE 1998061900567 19980619 00567 NM 1998 6 19 DLM11981258 1 19980614 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 814DE 48769 FLASHLIGHT AT 4L NOT BLINKING. REPLACED FLASHLIGHT. 2 L 7 3 4F RT A22WE 1998061900568 19980619 00568 1998 6 19 DLM11981259 4 19980613 A 2565 DL250006275 PINS DOUG MD11 MD11 3023602 NM L 2 DOORSLIDE PULLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 813DE 48600 FOUND L2 DOOR SLIDE PINS PULLED OUT OF SLIDE PACK. REPLACED PACK. 2 L 7 3 4F RT A22WE 1998061900569 19980619 00569 1998 6 19 DL72W981260 4 19980613 A 2565 146110018 SLIDE BOEING 727 727247 138408F NM 2R DOOR INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2811W 20649 2R PASSENGER DOOR SLIDE PRESSURE LOW. REPLACED SLIDE ASSY. 2 L 7 3 4F A3WE 1998061900570 19980619 00570 NM 1998 6 19 F3LA98046 1 19980511 A 5320 SHEAR TIE BOEING 737 7372L9 1384497 NM BS 767 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON SHEAR TIE AT BS 767, LBL 7 TO RBL 15. MAINTENANCE REMOVED DAMAGE D AREA (1 INCH BY 3 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-1, FIG 1. (M) 2 L 7 2 4F RT A16WE 1998061900571 19980619 00571 NM 1998 6 19 F3LA98049 1 19980511 A 5743 FITTING BOEING 737 7372L9 1384497 NM RT MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 DURING C-CHECK INSPECTION, REPORTED CORROSION ON AFT STABILIZER BEAM INBOARD LUG FACE AND LUG BORES ON RIGHT MAIN LANDIN G GEAR BEAM. MAINTENANCE REPLACED AFT STABILIZER BEAM FITTING PER OHM 57-40-01. (M) 2 L 7 2 4F RT A16WE 1998061900572 19980619 00572 NM 1998 6 19 F3LA98051 1 19980511 A 5743 FITTING BOEING 737 7372L9 1384497 NM LT MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION IN LUG BOLT HOLES FOR AFT STABILIZER FITTING ON LEFT MIAN LANDING GE AR SUPPORT BEAM. MAINTENANCE REMOVED CORROSION PER ER 98-0370, FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0370 AND SRM 51-10-0. (M) 2 L 7 2 4F RT A16WE 1998061900573 19980619 00573 NM 1998 6 19 F3LA98050 1 19980511 A 5320 FITTING BOEING 737 7372L9 1384497 NM RT MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION IN RT MAIN LANDING GEAR SUPPORT BEAM LUG BORES WHERE AFT STABILIZER BEAM ATTACHES. MAINTENANCE REMOVED CORROSION AND REPAIRED PER ER 98-0370. (M) 2 L 7 2 4F RT A16WE 1998061900574 19980619 00574 NM 1998 6 19 F3LA98052 1 19980526 A 5330 SKIN BOEING 737 737201 1384454 NM BS 353-356 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INTERNAL SKIN AT BS 353-356, RBL 3. MAINTENANCE REPAIRED SKIN PE R SRM 53-30-3, FIG 28. (M) 2 L 7 2 4F A16WE 1998061900575 19980619 00575 NM 1998 6 19 F3LA98053 1 19980511 A 5313 STRINGER BOEING 737 7372L9 1384497 NM BS 757 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION UNDER NUTPLATE ON STRINGER 19R, BS 757. MAINTENANCE REMOVED CORRODE D AREA (1.6 INCH BY 1 INCH BY .035 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-1 AND 53-10-3. (M) 2 L 7 2 4F RT A16WE 1998061900576 19980619 00576 NM 1998 6 19 F3LA98055 1 19980517 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 440 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON SHEAR TIE AT BS 440, BL0, WL 148. MAINTENANCE REMOVED DAMAGED AR EA (4.6 INCH BY 1.1 INCH). FABRICATED REPAIR DOUBLER AND REPAIRED PER SRM 51-30-2 AND 53-10-4. (M) 2 L 7 2 4F A16WE 1998061900577 19980619 00577 NM 1998 6 19 F3LA98047 1 19980511 A 5311 FRAME BOEING 737 7372L9 1384497 NM BS 435-440 DAMAGED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION, REPORTED DAMAGE TO FRAME WEB AT BS 435-440, STRINGER 25R TO 26R, FORWARD OF FORWARD CAR GO DOOR CUTOUT. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-3, 51-30-2 AN D 51-40-2. (M) 2 L 7 2 4F RT A16WE 1998061900578 19980619 00578 NM 1998 6 19 F3LA98045 1 19980511 A 5313 STRINGER BOEING 737 7372L9 1384497 NM BS 767-807 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON STRINGER 26R, BS 767-807. MAINTENANCE FABRICATED REPLACEMENT STR INGER AND DOUBLERS AND REPAIRED PER SRM 51-30-2, 51-40-2 AND 53-10-3. (M) 2 L 7 2 4F RT A16WE 1998061900579 19980619 00579 WP 1998 6 19 ZIAA98004 1 19980326 A 2612 24407332 FIRE LOOP DOUG DC8 DC8F55 3021928 WP NR 4 ENGINE SHORTED A ZIAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 811TC 45883 YIP - NR 4 ENGINE FIRE WARNING IN FLIGHT. SHUT DOWN ENGINE AND RETURNED TO YIP. INSPECTED NR 4 ENGINE AND FOUND NO EVI DENCE OF FIRE. FOUND SHORTED FIRE LOOP. REPLACED UPPER AFT FIRE LOOP NR 4 ENGINE IAW DC-8 MM 26-11-02. (M) 2 L 7 4 4F 4A25 1998061900580 19980619 00580 SO 1998 6 19 MASA98100 1 19980508 A 3350 3071BPE BULB EMB 120 EMB120RT SO CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 180YV 120180 FLT 5275 - TPA-GNV - AFTER ARRIVAL IN GNV, THE CREW REPORTED AN OVERHEAD EMERGENCY EXIT LIGHT AT ROW 6A WAS INOP. MAINT ENANCE REMOVED AND REPLACED THE BULB, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998061900581 19980619 00581 WP 1998 6 19 ASAA9880077 1 19980425 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRE D WIRING TO LGIHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998061900582 19980619 00582 WP 1998 6 19 ASAA9880074 1 19980419 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 940AS 49825 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998061900583 19980619 00583 WP 1998 6 19 ASAA9880073 1 19980417 A 3350 0105606003 BULB DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FWD CABIN WERE FOUND INOPERATIVE. REPLACED DEFE CTIVE LAMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998061900584 19980619 00584 WP 1998 6 19 ASAA9880072 1 19980415 A 3350 S103 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 953AS 49386 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 14 TO 18 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998061900585 19980619 00585 WP 1998 6 19 ASAA9880070 1 19980410 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FWD CABIN WERE FOUND INOPERATIVE. RECONNECTED W IRE IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998061900586 19980619 00586 WP 1998 6 19 ASAA9880069 1 19980409 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 0063 49657 PDX - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998061900587 19980619 00587 NM 1998 6 19 ASAA9840064 1 19980425 A 5210 MECHANISM BOEING 737 7374Q8 NM R1 DOOR LACK OF LUBE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 782AS 25113 SEA - PRIOR TO FLT 549, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. REPLACED THE R1 DOOR HANDLE CENTERING CAM BEARING AND LUBRICATED DOOR. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998061900588 19980619 00588 NM 1998 6 19 ASAA9840066 1 19980501 A 3230 654482515 ACTUATOR BOEING 737 7374Q8 NM RT MLG INOPERATIVE A ASAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 01 765AS 25102 SAN - FLT 501 - ON DEPARTURE FROM SAN, RAISED LANDING GEAR NORMALLY BUT WHEN SELECTED GEAR HANDLE TO OFF, THE RIGHT GEAR EXTENDED UNCOMMANDED. PLACED GEAR HANDLE BACK TO UP, THEN RETURNED GEAR HANDLE TO OFF POSITION AND THE RIGHT GEAR REMA INED UP. CONTINUED TO SEA WHERE EXTENDED NORMALLY AND ACFT LANDED WITHOUT INCIDENT. SEA MAINTENANCE REPLACED THE RIGH T MLG LOCK ACTUATOR. COMPLETED GEAR SWING AND EMERGENCY EXTENSION CHECK, AND THE GEAR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998061900589 19980619 00589 NM 1998 6 19 ASAA9840065 1 19980430 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 772AS 25105 ANC - FLT 62 - PRIOR TO DEPARTURE, CREW REPORTED THE EMERGENCY EXIT FLOOR TRACK LIGHTING WAS INOPERATIVE AT ROW 21. SEC URED WIRE TO LAMP SOCKET AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998061900590 19980619 00590 NM 1998 6 19 ASAA9840063 1 19980423 A 3350 900835A BATTERY PACK BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 SEA - DURING MAINTENANCE CHECK, ROW 25 AND THE AFT CABIN EMERGENCY EXIT TRACK LIGHTS AND THE LT DOOR EXIT IDENTIFIER WER E FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND THE LIGHTS WERE FOUND TO BE INOPERATIVE. (M) 2 L 7 2 4F RT A16WE 1998061900591 19980619 00591 NM 1998 6 19 ASAA9840062 1 19980421 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 PDX - DURING MAINTENANCE CHECK, THE AFT 4 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED W IRING AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998061900592 19980619 00592 NM 1998 6 19 ASAA9810032 1 19980424 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING RECON/MAINTENANCE CHECK, THE NR 1 AND NR 2 SEAT PALLET EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE I NOPERATIVE. REPLACED THE BATTERY PACKS AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998061900593 19980619 00593 NM 1998 6 19 ASAA9810027 1 19980412 A 3350 8821004 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 8 WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998061900594 19980619 00594 CE 1998 6 19 RU3A98001 1 19980506 A 5330 SKIN LEAR 60 60LEAR 5170707 CE FUSELAGE LIGHTNING STRIKE A RU3A K NONE O OTHER AP APPROACH 1 SW 21 54 009 GJT - ON ILS WAS HIT BY LIGHTING. POST FLIGHT REVEALED .125 TO .166 INCH HOLES IN FUSELAGE AFT OF RADOME BELOW FLOOR DE CL LEVEL. NO EVIDENCE OF HOLES IN PRESSURE VESSLE. RIGHT ENGINE SUSTAINED EVIDENCE OF ARCING ON ENGINE MOUNT, AND FAN BLADES. (M) 2 L 7 2 4F RT A10CE 1998061900595 19980619 00595 EU 1998 6 19 VTZA9164 1 19980419 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT FAILED A VTZA O OTHER N FALSE WARNING LD LANDING 1 EA 27 323UE 41059 FLT 6178 - TYS-IAD - DURING LANDING, EXPERIENCED A DISCREPANCY WITH THE POD SMOKE WARNING LIGHT ILLUMINATING. AIRCRAFT LANDED AT IAD WITH NO PROBLEM AND SMOKE LIGHT EXTINGUISHED UPON TOUCHDOWN. MAINTENANCE WAS NOTIFIED AND DISPATCHED TO T HE AIRCRAFT WHERE THEY FOUND THE SMOKE DETECTOR TO BE AT FAULT. MAINTENANCE REMOVED AND REPLACED SMOKE DETECTOR AND ACC OMPLISHED ALL APPROPRIATE CHECKS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998061900596 19980619 00596 WP 1998 6 19 VTZA98168 2 19980420 A 7230 31037503 SEAL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE WORN A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 485UE 901 P66097 FLT 6427 - IAD-ROA - DURING CRUISE, EXPERIENCED A DISCREPANCY WITH THE LT ENGINE OIL PRESSURE FLUCTUATING AND CAPTION LI GHT FLICKERING. AIRCRAFT RETURNED TO IAD AND MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCHED TO THE AIRCR AFT AND THE AIRCRAFT WAS MOVED TO THE HANGAR. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THAT THE LEFT ENGINE COMPRES SOR SEAL HAD FAILED. MAINTENANCE REMOVED AND REPLACED THE LT ENGINE COMPRESSOR SEAL AND ACCOMPLISHED ALL APPROPRIATE CH ECKS. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998061900597 19980619 00597 EU 1998 6 19 VTZA98166 1 19980418 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT DIRTY A VTZA B EMER. DESCENT N FALSE WARNING CL CLIMB 1 EA 27 331UE 41099 FLT 6628 - ORH-IAD - DURING CLIMB, EXPERIENCED A DISCREPANCY WITH THE POD SMOKE LIGHT ILLUMINATING. AIRCRAFT LANDED AT ORH AFTER DECLARING AN EMERGENCY. MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCHED AND FOUND THAT THE POD SMOKE DETECTOR WAS FAULTY. MAINTENANCE REMOVED AND REPLACED THE SMOKE DETECTOR AND ACCOMPLISHED ALL REQUIRED MAINTENANC E ACTIONS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998061900598 19980619 00598 EU 1998 6 19 VTZA98167 1 19980418 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU BAGG COMPT DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 325UE 41063 FLT 6302 - IAD-BOS - DURING CRUISE, EXPERIENCED A DISCREPANCY WITH THE POD SMOKE LIGHT ILLUMINATING. AIRCRAFT LANDED AT BOS AFTER DECLARING AN EMERGENCY. MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCHED AND FOUND THAT THE POD SMOKE DETECTOR WAS DIRTY. MAINTENANCE CLEANED THE SMOKE DETECTOR AND ACCOMPLISHED ALL. REQUIRED MAINTENANCE ACTIONS. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998061900599 19980619 00599 EU 1998 6 19 VTZA98169 1 19980420 A 5270 JE5 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 497UE 904 FLT 6461 - EWR-IAD - DURING CRUISE, EXPERIENCED A DISCREPANCY WITH THE PAX DOOR CAPTION LIGHT ILLUMINATING. AIRCRAFT DE CLARED AN EMERGENCY AND DIVERTED TO ABE. MAINTENANCE CONTROL WAS NOTIFIED. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND DEFERRED THE PAX DOOR WARNING SYSTEM UNDER MEL 52-2. AIRCRAFT WAS RELEASED FOR SERVICE. AIRCRAFT CONTINUED TO IAD AND UPON ARRIVAL MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE LOWER DOOR WARNING MICROSWITCH OUT OF ADJUSTMENT. ADJ USTMENTS WERE MADE AND ALL REQUIRED CHECKS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998061900600 19980619 00600 EU 1998 6 19 VTZA98172 1 19980424 A 3060 C40631 BRUSH BLOCK JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 309UE 41022 FLT 6516 - IAD-IGA - DURING CRUISE, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO LEFT PROP HEAT FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTION AND REMOVED AND REPLACED LEFT PROP BRUSH BLOCK, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998061900601 19980619 00601 EU 1998 6 19 VTZA98171 1 19980424 A 7714 AG44AF GENERATOR BAG JETSTM JETSTM3201 1500217 EU LEFT TACH FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 471UE 821 FLT 6379 - IAD-SYR - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT IAD DUE TO LEFT RPM GAUGE FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TACH GENERTOR. OPS CHECK OK. AIRCRAF T WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998061900602 19980619 00602 1998 6 19 VTZA98170 4 19980423 A 3417 7000700966 ADC JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILURE A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 310UE 41028 FLT 6399 - IAD-BOS - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CAPTS ASI OFF BY 15 TO 40 KNOTS. AIRCRA FT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTION AND REMOVED AND REPLACED LEFT ADC, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998061900603 19980619 00603 EU 1998 6 19 VTZA98173 1 19980424 A 6120 8210263 GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RIGHT OUT OF ADJUST A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 476UE 884 FLT 6248 - IAD-BGM - DURING CLIMB, MADE AN UNSCHEDULED LANDING AT IAD DUE TO RT ENGINE WOULD NOT MAKE TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED X-SCREW ON PROP GOV. OPS CHECK OK. AIRC RAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998061900604 19980619 00604 EU 1998 6 19 VTZA98174 1 19980429 A 3244 AHA1837 TIRES JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA O OTHER O OTHER LD LANDING 1 EA 27 309UE 41022 FLT 6457 - EWR-IAD - DURING LANDING, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS AIRCRAFT BLEW BOT H RT MAIN TIRES ON LANDING. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BOTH RT TIRES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998061900605 19980619 00605 1998 6 19 VTZA98176 4 19980429 A 3417 7000700961 ADC JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 330UE 41098 FLT 6235 - IAD-CHO - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO CAPTAINS ALIMETER STICKING. AIRCR AFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 ADC. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998061900606 19980619 00606 EU 1998 6 19 VTZA98178 1 19980430 A 2120 L3797311407 DUCT BAG JETSTM JETSTM3201 1500217 EU LEFT DAMAGED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 478UE 892 FLT 6193 - IAD-JFK - DURING CLIMB, MADE A UNSCHEDULED LANDING AT IAD DUE TO AIRCRAFT WILL NOT PRESSURIZE. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT ACM DUCT. OPS CHECK OK. AI RCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998061900607 19980619 00607 1998 6 19 VTZA98180 4 19980501 A 3413 066500012704 VSI BAG JETSTM JETSTM3201 1500217 EU LEFT FALED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 486UE 905 FLT 6552 - IAD-CLE - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO LEFT VSI INOP. AIRCRAFT RETURNED TO THE GATE WIT H NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED VSI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RET URNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998061900608 19980619 00608 EU 1998 6 19 VTZA98181 1 19980501 A 3230 106A703056A RETRACT MECH BAG JETSTM JETSTM3201 1500217 EU NLG REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 485UE 901 FLT 6598 - IAD-RDU - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO LANDING GEAR WOULD NOT RETRACT. AIRCRFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND NOSE GEAR NEEDING SERVICED. MAINTENANCE SERVICED NOSE GEAR AND PERFORMED GEAR SWING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998061900609 19980619 00609 EU 1998 6 19 VTZA98177 1 19980430 A 3222 106A703056A STRUT BAG JETSTM JETSTM3201 1500217 EU NLG REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 485UE 901 FLT 6598 - IAD-RDU - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING AND AT IAD DUE TO LANDING GEAR WOULD NOT RETRACT. AIRC RAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND NOSE STRUT STUCK. MAINTENANCE DESERVIC ED STRUT AND RESERVICED STRUT AND PERFORMED GEAR SWING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A56EU 1998061900610 19980619 00610 WP 1998 6 19 TWAA9807207 1 19980327 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 964 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK AT APPROX STATION 964, LONGERON 22L, CORROSION ON DOUBLER INBOARD SIDE AND PELLED R IVETS AREA ON OUTER SKIN. REPLACED DOUBLER PER SRM 51-01, PG 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998061900611 19980619 00611 WP 1998 6 19 TWAA9807206 1 19980317 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 DURING OP 15 MAINTENANCE CHECK, FOUND AT RT STATION 980, FORMER RING TO FUSELAGE ATTACH ANGLE CRACKED AT 2 PLACES JUST B ELOW LONGERON 15R. FORMER FOOT FORMED AND HEAT TREATED TO 7075 PER SRM 51-102A. INSTALLED NEW FORMER FOOT SECTION PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998061900612 19980619 00612 WP 1998 6 19 TWAA9807205 1 19980311 A 5320 FORMER DOUG DC9 DC932 3022066 WP BS 637 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON TO CANTED KEEL FORMER TIE CRACKED AT STATION 637, APPROX 15 IN RBL. REPLACED TIE PER SRM 51-01, PAGE 1 ITEM C. SEALED REPAIR PER SRM 51-20-0. (M) 2 L 7 2 4F A6WE 1998061900613 19980619 00613 WP 1998 6 19 TWAA9807204 1 19980323 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HO LES. STOP DRILLED CRACK. REPAIRED PER DAC DWG J060271 AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900614 19980619 00614 WP 1998 6 19 TWAA9807203 1 19980317 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 503 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN BEYOND LIMITS AT FS 503 BETWEEN L27 AND L38R, 5.5 INCH BY 2.5 INCH BY .175. (M) 2 L 7 2 4F A6WE 1998061900615 19980619 00615 WP 1998 6 19 TWAA9807202 1 19980414 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 916-945 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN BENEATH DOOR THRESHOLD HAD CORROSION AT STATION 916 TO 945, L2 9R TO L27R. REPAIRED AS PER ARA 15272 AND STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900616 19980619 00616 WP 1998 6 19 TWAA9807201 1 19980218 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 503 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN DENTED BEYOND LIMITS AT FS 503, BETWEEN L26R AND L26R, 3 INCH BY 2 INCH BY .145 DEEP. REPAIRED PER SRM 53.04, FIG 38 SHEET 22. (M) 2 L 7 2 4F A6WE 1998061900617 19980619 00617 WP 1998 6 19 TWAA9807404 1 19980510 A 2530 4110001143 COFFEEMAKER DOUG DC9 DC982 3022082 WP GALLEY SHORTED A TWAA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NR NOT REPORTED 1 CE 05 904TW 3488 49156 STL - FLT 315 - NR 3 COFFEEMAKER CIRCUIT BREAKER POPPED. CREW RESET CB AND SPARKS WERE PRESENT AT THE COFFEEMAKER AND C B POPPED AGAIN. CREW LEFT CB POPPED. REPLACED COFFEEMAKER. CHECK-C 4-1-98 STL. (M) 2 L 7 2 4F A6WE 1998061900618 19980619 00618 NM 1998 6 19 TWAA9807403 1 19980510 A 2530 4000704 OVEN BOEING 767 767231 1385131 NM GALLEY WORN A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 610TW 22573 JFK - FLT 842 - CREW REPORTED AN ELECTRICAL SMELL AND SMOKE FROM THE A3 GALLEY OVEN. CREW TURNED OFF THE OVEN. REPLACE D OVEN. CHECK-C 3-18-98 LAX. (M) 2 L 7 2 4F RT A1NM 1998061900619 19980619 00619 WP 1998 6 19 TWAA9807402 1 19980510 A 3040 6172 CONTROLLER DOUG DC9 DC982 3022082 WP RT WINDSHIELD WORN A TWAA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 957U 229 49702 SFO - FLT 422 - AFTER DEPARTURE FROM SJC, SMOKE APPEARED AT FWD EDGE OF GLARESHIELD BY CENTER WINDSHIELD. TURNED OFF WI NDSHIELD HEAT AND SMOKE STOPPED. MAKE UNSCHEDULED LANDING AT SFO. CHECKED WINDSHIELD SENSORS AND TERMINALS, AND REPLAC ED WINDSHIELD HEAT CONTROLLER. CHECK-C 12-22-97 MCI. (M) 2 L 7 2 4F A6WE 1998061900620 19980619 00620 WP 1998 6 19 TWAA9807401 1 19980510 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 987Z 47137 HOU - FLT 309 - AFTER PASSENGERS AND CREW DEPLANED AN FAA INSPECTOR TURNED ON THE EMERGENCY LIGHTS AND REPORTED THAT A S ECTION OF EGRESS LIGHTS IN THE FIRST CLASS CABIN WAS INOPERATIVE. MAINTENANCE CHECKED THE LIGHTS AND FOUND THEM ALL OPE RATIVE. (M) 2 L 7 2 4F A6WE 1998061900621 19980619 00621 WP 1998 6 19 TWAA9807320 1 19980414 A 5551 FITTING DOUG DC9 DC932 3022066 WP HORIZ STAB FLAT SPOT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZ STABILIZER LEFT PIVOT BEARING LUG, IN LT SIDE OF STAB CENTER SECTION R IB, WITH FLAT SPOT IN BEARING BORE AT APPROX 3 O'CLOCK POSITION, .017 IN DEEP AND LUG IS .010 IN THICKER AT TOP 12 O'CLO CK POSITION AT SPOT FACE THAN AT 6 O'CLOCK POSITION AT SPOT FACE. ALSO, 3 SMALL CORROSION PITS AT 4 O'CLOCK AND 11 O'CL OCK POSITION. REMOVED AND REPLACED LEFT RIB PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998061900622 19980619 00622 WP 1998 6 19 TWAA9807319 1 19980413 A 5312 BULKHEAD CASTING DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FOOT CASTING AFT INBOARD SIDE OF 965 BULKHEAD, CRACKED. REMOVED AND REPLACED CASTING PER SRM 51-01 AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900623 19980619 00623 WP 1998 6 19 TWAA9807318 1 19980323 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CEHCK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HO LES. STOP DRILLED CRACK, REPAIRED PER DAC DWG J060271 AND STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900624 19980619 00624 WP 1998 6 19 TWAA9807317 1 19980323 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L BROKEN JUST FORWARD OF FORMER 160. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M) 2 L 7 2 4F A6WE 1998061900625 19980619 00625 WP 1998 6 19 TWAA9807316 1 19980323 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT STATION 200. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M) 2 L 7 2 4F A6WE 1998061900626 19980619 00626 WP 1998 6 19 TWAA9807315 1 19980327 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 196-218 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BEYOND LIMIT ON FLOORBEAM CAP FROM STATION 196 TO 218 OBL. FABRIC ATED AND INSTALLED NEW BEAM CAP PER SRM 51-01 PAGE 1. (M) 2 L 7 2 4F A6WE 1998061900627 19980619 00627 WP 1998 6 19 TWAA9807314 1 19980312 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 237 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FLOORBEAM WITH WEAR AREA AT STATION 237, LBL 4 INCHES. REPAIRED FLOOR BEAM PER SRM 53-05 FIG 30. (M) 2 L 7 2 4F A6WE 1998061900628 19980619 00628 EU 1998 6 19 USAASB98088 2 19980404 A 7200 ENGINE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU LEFT FAILED A USAA E L A ENGINE SHUTDOWN ABORTED APPROACH UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 EA 19 448US 24892 721181 BDA - FLT 2295 - DURING CRUISE, THE NR 1 ENGINE INDICATED LOW OIL PRESSURE AND HIGH OIL TEMPERATURE. CREW SHUT DOWN THE NR 1 ENGINE AND A DECISION WAS MADE TO DIVERT TO BDA, THE CLOSEST MOST SUITABLE AIRPORT. FLIGHT PROCEEDED TO BDA AND M ADE TWO MISSED APPROACHES ON RUNWAY 12 DUE TO HIGH CROSSWINDS AND RAIN. FLIGHT LANDED ON THIRD APPROACH, THIS TIME ON R UNWAY 30. WINDS ON LANDING WERE 20 TO 28 KNOTS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. T OTAL SINGLE ENGINE WAS 50 MINUTES. MAINTENANCE PULLED THE NR 1 ENGINE GEARBOX CHIP DETECTOR AND FOUND IT FULL OF METAL. REMOVED AND REPLACED THE NR 1 ENGINE ASSY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1998061900629 19980619 00629 NE 1998 6 19 TSAA9871191 2 19980401 A 7200 ENGINE BOEING 737 73725A 1384481 NM PWA JT8 JT8D9A 52048 NE NR 2 MALFUNCTIONED A TSAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 819AL 23791 FLT 297 - NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED ON CLIMB-OUT FOLLOWED BY 'O' OIL QTY INDICATION AND OIL PRESSURE SL OWLY DECREASED TO FLUCTUATE BETWEEN 10-15 LBL PSI. SHUTDOWN PERFORMED. REPLACED NR 2 ENGINE IAW M-211, M-212, M-213, M -214 AND M-215. OK FOR SERVICE REQUIRED INSPECTION C/W FOR NR 2 ENGINE. REMOVE AND INSTALL IAW M-211, M212, M-213, M-2 14, AND M-215. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1998061900630 19980619 00630 NE 1998 6 19 USAASB98094 2 19980414 A 7320 7139M91G01 PMC BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE FAILED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 519AU 20434 23705 CLT - FLT835 - ON CLIMB-OUT FROM CLT, THE NR 1 ENGINE N1 AND ALL ENGINE PARAMETERS BEGAN FLUCTUATING. CREW COULD HEAR T HAT THE ENGINE WAS SURGING. FLIGHT RETURNED TO FIELD AT CLT. ON APPROACH, ENGINE STABILIZED. FLIGHT LANDED WITHOUT FU RTHER INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE POWER MANAGEMENT CONT ROL. ADJUSTED AND RAN ENGINE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 1998061900631 19980619 00631 NE 1998 6 19 EIAA980151 2 19980329 A 7261 OIL SYSTEM BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE LACK OF LUBE A EIAA E ENGINE SHUTDOWN W INADEQUATE Q C CR CRUISE 1 NM 09 471EV 20651 JFK - SHUTDOWN NR 3 ENGINE AFTER 30 MINUTES INTO FLIGHT DUE TO LOSS OF OIL PRESSURE. OIL VISCOSITY WAS VERY THICK AND E NGINE REQUIRED 26 QUARTS TO FILL. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998061900632 19980619 00632 NE 1998 6 19 S2YA98010 2 19980330 A 7200 ENGINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RIGHT MALFUNCTIONED A S2YA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 13 91SK UE91 AFTER TAKEOFF OF FLT 1235 - MKE TO MQT, THE FLT CREW NOTICED THAT THERE WERE SPARKS COMING OUT OF THE RT ENGINE EXHAUST STACK. THE FLIGHT CREW DECIDED TO RETURN TO MKE SO MAINTENANCE COULD INSPECT THE ENGINE. AFTER AN UNEVENTFUL LANDING M AINTENANCE INSPECTED THE RT ENGINE COMPRESSOR INLET, HOT SECTION, AND THE 2ND STAGE POWER TURBINE/EXHAUST AREA. NO DISC REPANCIES WERE NOTED. AFTER A SATISFACTORY GROUND PERFORMANCE RUN THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1998061900633 19980619 00633 NE 1998 6 19 C2XA98IA140 2 19980424 A 7397 311591102 WIRE HARNESS EMB 120 EMB120RT SO PWA 118 PW118 NE RT NACELLE CHAFED A C2XA F ACTIVATE FIRE EXT. O OTHER CR CRUISE 1 SW 09 58733 120197 IAH - DURING FLIGHT 3950 FROM VCT TO IAH, THE NUMBER 2 ENGINE EXPERIENCED A TORQUE SURGE FOLLOWED BY A LOSS OF POWER. T HE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REPAIRED THE NR 2 ENGINE EEC WIRE HARNESS, AND THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998061900634 19980619 00634 NE 1998 6 19 WTAA980074 2 19980503 A 7320 7863904 HMU EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A WTAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 17 193YV 120193 SBA - AT 14,000 FT, LEFT ENGINE TORQUE DROPPED TO ZERO AND T6 DROPPED TO 200-300 DEGREES. CREW SHUT DOWN ENGINE AND RET URNED TO THE STATION WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT ENGINE HMU. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998061900635 19980619 00635 NE 1998 6 19 ASOA98011S 2 19980127 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LEFT FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 265AS 120170 115174 DURING CLIMB-OUT DFW-LAW, RECEIVED LOW OIL PRESSURE WARNING ON MAP, PRESSURE GAUGE CONFIRMED THAT THE OIL PRESSURE WAS B ELOW 40 PSID. CREW FOLLOWED THE POH AND SHUT DOWN THE LEFT ENGINE, THEN DECLARED AN EMERGENCY AND RETURNED TO DFW WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. DFW MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW/MM. AL L GROUND RUNS AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. INVESTIGATION REVEALED FAILU RE OF THE NR 5 BEARING, LEADING TO THE LOSS OF OIL PRESSURE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998061900636 19980619 00636 NE 1998 6 19 UF6A980405 2 19980409 A 7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 10185 2029 ORD - NR 1 PROP ASSEMBLY WAS STRUCK BY AIRCRAFT TUG DURING PUSH BACK. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE AND PROP ASSEMBLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998061900637 19980619 00637 WP 1998 6 19 SABA980022 2 19980326 A 7320 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE OUT OF ADJUST A SABA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 33 962AE 962 FLT 5163 - ON TAKEOFF FROM CLT TO LEX, AT MAX POWER FOR TAKEOFF. THE RIGHT ENGINE WAS AT 100 PERCENT TORQUE. THE LEFT ENGINE WAS BARELY MAKING 75 PERCENT. PILOT ABORTED TAKEOFF. NO EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO PARKING. MAINTENANCE ADJUSTED THE 'X' SCREW. AIRCRAFT RUN AND OPS CHECKED GOOD. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998061900639 19980619 00639 NM 1998 6 19 WRLA98083 1 19980502 A 3610 50N49501 DUCT DOUG MD11 MD11 3023602 NM NR 2 ENGINE LOOSE A WRLA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 EA 27 272WA 48437 DURING T/O ROLL, NR 2 ENG EXPERIENCED HIGH EGT. FLT CREW ELECTED TO ABORT T/O. A/C RETURNED TO GATE W/O INCIDENT. HOW EVER, WHILE A/C WAS STANDING ON GATE 4 MAIN WHEEL ASSY'S LOST AIR PRESS DUE TO THERMAL PLUG RELEASE. MX PERSONNEL COOLE D A/C BRAKES, AND REPLACED MAIN WHEELS THAT HAD LOST PRESS. A/C WAS TOWED TO ENG RUN UP PAD WHERE NR 2 WAS GROUND RUN T O MAX PERMISSIBLE POWER. INDICATIONS 2.5 BLEED VALVE WAS ALLOWING HPC AIR TO BYPASS CORE, CAUSING INCREASE IN N1 SPEED AND RISE IN EGT FOR HIGH POWER EPR SETTINGS. ENG DID NOT EXCEED EGT LIMITS. A/C TO BE 'TWO-ENGINE' FERRIED TO LOCATION WHERE ENGINE TO BE REMOVED AND FORWARDED TO ENGINE REPAIR FACILITY FOR CORRECTIVE ACTION. (M) 2 L 7 3 4F RT A22WE 1998061900640 19980619 00640 NE 1998 6 19 USAAD98067 2 19980413 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D17 52049 NE RIGHT FAILED A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 820US 49119 MCO - FLT 1554 - DURING CLIMB A VIBRATION WAS FELT COMING FROM NUMBER 2 ENGINE, FOLLOWED BY AN OIL CLOG LIGHT ILLUMINATI NG. THE ENGINE THRUST WAS REDUCED IDLE AND THE AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLA CED THE NR 2 ENGINE. (M) 2 L 7 2 4F 4 F A6WE E2EA 1998061900641 19980619 00641 WP 1998 6 19 TWAA9807305 1 19980327 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 268 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 104 INDICATING CRACK RT WING LOWER SPAR STATION XRS 268. REPAIRED PER S ERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900642 19980619 00642 WP 1998 6 19 TWAA9807304 1 19980327 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP WS 164 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP15 MAINTENANCE CHECK, FOUND STATION XRS 164 INSIDE TANK FWD FACE OF LOWER SPAR CAP, VERTICAL LEG WITH CRA CK EXTENDING INTO LOWER RADIUS, BELOW INBOARD FLAP BARREL NUT ATTACH POINT. INSTALLED NEW SPAR CAP AND SPLICE PER DWG J 060165 AND STD PROCEDURE, AND SRM 51-01 PAGE 1. (M) 2 L 7 2 4F A6WE 1998061900643 19980619 00643 WP 1998 6 19 TWAA9807303 1 19980319 A 5753 SPAR DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TE INBOARD FLAP REAR SPAR INBOARD FLAP CASTING MOUNT HOLE, LOWER INB OARD HOLE, WITH CRACK EXTENDING INTO RADIUS FORWARD SIDE OF FUEL TANK. SPLICED SECTION OF LOWER SPAR FROM STATION XRS 1 11.510 TO XRS 195.210 PER DOUGLAS DWG J060165, AND STANDARD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900644 19980619 00644 WP 1998 6 19 TWAA9807302 1 19980327 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND FUSELAGE TO BULKHEAD ATTACH ANGLE CRACKED BETWEEN RT STRINGER 13 AND 14, ON FUSELAGE SIDE OF BULKHEAD STATION 965. REPLACED ANGLE PER SRM 51-01, PATE 1 ITEMC AND TWA STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998061900645 19980619 00645 WP 1998 6 19 TWAA9807301 1 19980327 A 5751 SKIN DOUG DC9 DC932 3022066 WP RT AILERON CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND UPPER TE PANEL FORWARD OF RT WING AILERON UPPER SURFACE, OUTBOARD AREA HAD S EVERAL FASTENER HEADS STRESSED AND ALL SKIN PILLOWING. REPLACED TE SKIN PANEL, NEW PANEL INSTALLED PER SRM 51-01. (M) 2 L 7 2 4F A6WE 1998061900646 19980619 00646 EU 1998 6 19 AALA980908 1 19980430 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT FRAME 74 4 INCHES LEFT OF AIRCRAFT C/L. REPLACED SUPPORT PER SRM 51-22-00-0. (M ) 2 L 7 2 4F RT A35EU 1998061900647 19980619 00647 EU 1998 6 19 AALA980907 1 19980430 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT, FRAME 74, 8 INCHES RIGHT OF AIRCRAFT C/L. REPLACED SUPPORT PER SRM 51-22-00-0. (M) 2 L 7 2 4F RT A35EU 1998061900648 19980619 00648 EU 1998 6 19 AALA980906 1 19980506 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 66 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON LONGERON. SPLICE IN NEW SECTION OF LONGERON PR SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998061900649 19980619 00649 EU 1998 6 19 AALA980879 1 19980505 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU BS 4206 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION DAMAGE TO LONGERON. SPLICE IN SECTION OF NEW LONGERON PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998061900650 19980619 00650 EU 1998 6 19 AALA980884 1 19980505 A 5347 RAIL AIRBUS 300 A300B4605R 3930308 EU BS 1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR BOARD RAIL NR 8 BY R-1 DOOR STATION 1212, FRAME 15. SURFACE TREATED PER SRM 51-21-00-02. FABRICATED AND INSTALLED STRAP PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998061900651 19980619 00651 EU 1998 6 19 AALA980889 1 19980504 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION DAMAGE ON LONGERON. SPLICE IN NEW SECTION OF LONGERON PER SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998061900652 19980619 00652 EU 1998 6 19 AALA980888 1 19980505 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 73-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR BOARD SUPPORT BETWEEN FRAMES 73 AND 74, 7 INCHES AFT OF FRAME 73 AND 73 INCHES FROM CENTE R OF A/C LEFT SIDE OF A/C. REPAIRED PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998061900653 19980619 00653 EU 1998 6 19 AALA980903 1 19980430 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT FROM FRAME 71 TO FRAME 74, 29 INCHES RIGHT OF A/C C/L. REPLACED SUPPORT PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998061900654 19980619 00654 NM 1998 6 19 AALA980904 1 19980616 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION IN STRINGER 23 RT, AT STATION 1148. REMOVED STRINGER 23R, STATION 1141-1155, SPLICED IN NEW SECTI ON PER SRM 53-10-3 FIG 1 SHEET 1 PAGE 3. (M) 2 L 7 3 4F A3WE 1998061900655 19980619 00655 EU 1998 6 19 AALA980905 1 19980506 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION DAMAGE TO FLOOR SUPPORT INBOARD OF NR 1 ROLLER TRAY. INSTALLED ANGLE REPAIR AND PER SRM 53-10-15 PAGE 839. (M) 2 L 7 2 4F RT A35EU 1998061900656 19980619 00656 EU 1998 6 19 AALA980935 1 19980508 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FRAME 20-23 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - NR 1 ROLLER TRAY OUTBOARD FLANGE AT ATTACH POINT AT FRAME 21 HAS CORROSION. REMOVED SECTION OF NR 1 ROLLER TRAY F ROM FRAME 20 TO FRAME 23 AND SPLICED NEW ROLLER TRAY IN PER SRM 53-10-15-2. (M) 2 L 7 2 4F RT A35EU 1998061900657 19980619 00657 EU 1998 6 19 AALA980934 1 19980430 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4627 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT, FRAME 7273, 34 INCHES LEFT OF AIRCRAFT C/L. REPAIRED SUPPORT WITH DOUBLER PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998061900658 19980619 00658 EU 1998 6 19 AALA980933 1 19980507 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU BS 3991 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOORBEAM 60 AT NR 5 TRAY. SPLICED IN NEW FLOORBEAM SECTION AS PER SRM 53-10-15-2, TREATED, PR IMED AND PAINTED EPR SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1998061900659 19980619 00659 EU 1998 6 19 AALA980932 1 19980507 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 67-68 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - STRINGER 50L CORRODED FROM FRAME 67 TO 68. CUT OUT STRINGER SECTION, SPLICED IN NEW SECTION IAW SRM 53-10-14-2. ( M) 2 L 7 2 4F RT A35EU 1998061900660 19980619 00660 EU 1998 6 19 AALA980920 1 19980507 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 74-75 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND LIGHT CORROSION ON FLOOR BOARD SUPPORT BETWEEN FRAMES 74 AND 75, 17 INCHES FROM CENTER OF A/C ON LEFT SIDE O F A/C. REPLACED FLOOR BOARD SUPPORT PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998061900661 19980619 00661 EU 1998 6 19 AALA980919 1 19980507 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 73-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR BOARD SUPPORT BETWEEN FRAMES 73 AND 74, 7 INCHES AFT OF FRAME 73 AND 73 INCHES FROM CENTE R OF OF AIRCRAFT ON RT SIDE. REPAIRED WITH REPLACEMENT OF NEW PART AS PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998061900662 19980619 00662 EU 1998 6 19 AALA980918 1 19980507 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 67 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION FLOOR BOARD SUPPORT AT FRAME 67 LOWER FORWARD CORNER OF CARGO DOOR CUTOUT. REPLACED FLOOR BOARD S UPPORT PER AARD 51-10-00-3. (M) 2 L 7 2 4F RT A35EU 1998061900663 19980619 00663 EU 1998 6 19 AALA980952 1 19980508 A 5315 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 59-62 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON LONGERON AND PAINT PEELING ON RIVETS. REMOVED OLD LONGERON DRILLED NEW LONGERON AND INSTALLED AS PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061900664 19980619 00664 EU 1998 6 19 AALA980951 1 19980508 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU FRAME 64-65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON LONGERON 55L BETWEEN FRAMES 64 AND 65. REMOVED OLD LONGERON, DRILLED UP NEW LONGERON AND INSTA LLED AS PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061900665 19980619 00665 EU 1998 6 19 AALA980950 1 19980512 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71/73 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 71 AND 73 AND 29 INCHES LEFT OF CENTER OF AC, 3 SPOTS MARKED. REP AIRED PER AARD 53-20-00-2 PAGE 1 SEE BACK FOR DETAILS AS PER ESO 30595, DATES 5-7-98. (M) 2 L 7 2 4F RT A35EU 1998061900666 19980619 00666 EU 1998 6 19 AALA980949 1 19980510 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 71 AND 72, 18 INCHES FROM CENTER OF AC ON LEFT SIDE 3 INCHES FORWA RD OF FRAME 72. REPAIRED PER AARD 53-20-00-2 PAGE 1, SEE BACK FOR DETAILS OF ESO 30595, DATED 5-7-98. (M) 2 L 7 2 4F RT A35EU 1998061900667 19980619 00667 EU 1998 6 19 AALA980948 1 19980512 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 71-72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND LIGHT CORROSION ON FLOOR SUPPORT BETWEEN FRAME 71 AND 72, ON LEFT SIDE OF A/C, 35 INCHES FROM CENTER OF A/C. REPAIRED PER ESO 5 '30595' DATED 5-7-98 AND PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998061900668 19980619 00668 EU 1998 6 19 AALA980947 1 19980511 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 3885 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON ROLLER TRAY FLOOR SUPPORT AT ROLLER TRAYS NR 1 AND NR 2 AND NR 3 AND NR 4. INSTALLED NEW FLOOR SUPPORT AT FRAME 58, TREATED, PAINTED PRIMED PER 51-21-10-0, 51-27-10, INSTALLED PER 72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061900669 19980619 00669 EU 1998 6 19 AALA980946 1 19980429 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 4740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT AT FRAME 74-75 17 INCHES RIGHT OF AIRCRAFT C/L. INSTALLED NEW FLOOR SUPPORT PER ESO 30595, DATED 5/6/98. (M) 2 L 7 2 4F RT A35EU 1998061900670 19980619 00670 EU 1998 6 19 AALA980945 1 19980511 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU BS 4044 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOORBEAM AT FRAME 61 AND NR 5 ROLLER TRAY. SPLICED FRAME SECTION PER SRM 53-10-15-2. (M) 2 L 7 2 4F RT A35EU 1998061900671 19980619 00671 EU 1998 6 19 AALA980887 1 19980505 A 5320 SPLICE AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ON HORIZONTAL SURFACE OF STRINGER SPLICE. REPLACED STRINGER SPLICE PER SRM 51-72-10. 2 L 7 2 4F RT A35EU 1998061900672 19980619 00672 EU 1998 6 19 AALA980885 1 19980505 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CARGO COMPT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ON FLOOR SUPPORT BETWEEN ROLLER TRACK 1 AND 2. INSTALLED DOUBLER AND FILLER PER SRM 53-10-15. (M ) 2 L 7 2 4F RT A35EU 1998061900673 19980619 00673 EU 1998 6 19 AALA980891 1 19980504 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FLOOR SUPPORT AT FRAME 63 BETWEEN ROLLER TRACK 1 AND 2 IS CORRODED. REPLACED CORRODED SECTION OF FLOORBEAM PER SR M 53-10-15. (M) 2 L 7 2 4F RT A35EU 1998061900674 19980619 00674 EU 1998 6 19 AALA980890 1 19980504 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 1024-1030 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FLOOR SUPPORT CORRODED AT STATION 1024 TO 1030, TRACK NR 6A. REMOVED AND REPLACED NR 6A FLOOR SUPPORT FROM FRAME NR 11 AND TO FRAME 13 PER SRM 51-72-10-0, ALODINED, PRIMED AND PAINTED PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998061900675 19980619 00675 EU 1998 6 19 AALA980883 1 19980506 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1231-1238 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - TOP OF NR 7 SEAT TRACK FLANGE CORRODED STATION 1231 TO 1238. REPLACED UPPER HALF OF TRACK NR 7 FROM STATION 1231 TO 1238 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061900676 19980619 00676 EU 1998 6 19 AALA980913 1 19980506 A 5320 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU FRAME 26 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ON SHEAR TIE AT LONGER 45R FRAME 26. INSTALLED NEW SHEAR TIE PER SRM 51-22-10. (M) 2 L 7 2 4F RT A35EU 1998061900677 19980619 00677 EU 1998 6 19 AALA980912 1 19980505 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 15-16 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION ON FLOOR SUPPORT AT R1 DOOR. REMOVED AND REPLACED UPPER T-ANGLE PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061900679 19980619 00679 EU 1998 6 19 AALA980910 1 19980506 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 59-60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ON STRINGER 56 LEFT BETWEEN FRAME 59 AND 60. REMOVED CORRODED STRINGER AND INSTALLED NEW STRINGER AND SPLICE AS EPR SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998061900680 19980619 00680 EU 1998 6 19 AALA980909 1 19980505 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU FRAME 26 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND STRINGER SPLICE FITTING CORRODED AT STRINGER 45R, FRAME 26. INSTALLED NEW SPLICE FITTING PER SRM 51-22-10. (M) 2 L 7 2 4F RT A35EU 1998061900681 19980619 00681 EU 1998 6 19 AALA980882 1 19980506 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ON FLOOR SUPPORT AT FRAME 60 BETWEEN ROLLER TRAY AND 1 AND 2 AND 4. INSTALLED NEW FLOORBEAM SUPPO RT PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1998061900682 19980619 00682 EU 1998 6 19 AALA980881 1 19980505 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 16 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FLOOR SUPPORT CORRODED FROM FRAME 12 TO FRAME 16, (NR 9 SUPPORT). REMOVED AND REPLACED FLOOR SUPPORT NR 9 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061900683 19980619 00683 EU 1998 6 19 AALA980953 1 19980511 A 5540 STRIP AIRBUS 300 A300B4605R 3930308 EU RUDDER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ALONG ENTIRE LENGTH OF RUDDER T/E RT AND LT SIDES. REPLACED APEX STRIP RT AND LT SIDES PER 55-41- 12-2 AND ESO 30595, DATED 4/13/98. (M) 2 L 7 2 4F RT A35EU 1998061900684 19980619 00684 EU 1998 6 19 AALA981009 1 19980515 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FRAME 55/56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON NUT PLATE DOUBLER ASSEMBLY ON A/C SKIN, BETWEEN FRAMES 55 AND 56 AND BETWEEN STRINGERS 55L AND 56L. REPAIRED AS PER ESO 30595, DATED 5-14-98. (M) 2 L 7 2 4F RT A35EU 1998061900685 19980619 00685 EU 1998 6 19 AALA981008 1 19980515 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FRAME 56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND FRAME 56 LEFT CASTING HAS CORROSION ON TOP LIP ABOVE STRINGER 44L. INSTALLED REPAIR ANGLE PER ESO 30595, DA TED 5-15-98. (M) 2 L 7 2 4F RT A35EU 1998061900686 19980619 00686 EU 1998 6 19 AALA981007 1 19980518 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FRAME 13 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CRACK BETWEEN TWO FASTER A JUNTION OF FRAME TO RT OUTBOARD WHEEL WELL WEB. INSTALL DOUBLERS PER AIRBUS DRAW ING R53610650 AND ESO 30595, DATED 5/12/98 AND 5/18/98, 5/14/98. (M) 2 L 7 2 4F RT A35EU 1998061900687 19980619 00687 EU 1998 6 19 AALA980961 1 19980512 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU FRAME 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON FLOOR SUPPORT UNDER ROLLER TRAY. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-72-10 AND AARD 51-10-00-2. (M) 2 L 7 2 4F RT A35EU 1998061900688 19980619 00688 EU 1998 6 19 AALA980960 1 19980512 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU FRAME 61 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON STRINGER 52L. SPLICE IN NEW SECTION OF STRINGER PER SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998061900689 19980619 00689 EU 1998 6 19 AALA980959 1 19980512 A 5320 SHEAR TIE AIRBUS 300 A300B4605R 3930308 EU FRAME 61/62 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON SHEAR TIE. REMOVED AND REPLACED SHEAR TIES PER SRM 51-22-10-0, 52/53L. (M) 2 L 7 2 4F RT A35EU 1998061900690 19980619 00690 EU 1998 6 19 AALA980995 1 19980514 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU FRAME 56-58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND CORROSION ON NR 6 ROLLER TRACY ON FORWARD END, AFT END. REMOVED AND REPLACED ROLLER TRAY, PER 51-72-10-0. ( M) 2 L 7 2 4F RT A35EU 1998061900691 19980619 00691 EU 1998 6 19 AALA980996 1 19980515 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 58-63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 FOUND CORROSION ON FORWARD AND AFT ENDS OF ROLLER TRAY NR 1 FROM STATION 58L-63L. REMOVED AND REPLACED ROLLER TRAY PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061900692 19980619 00692 NM 1998 6 19 USAA980208 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACKED .5 INCH LONG STATION 460, STRINGER 20L TO 22L FRAME. REPLACED F RAME SECTION, REPAIRED PER SRM 51-40-3, BOEING DRW 69C36696, EO 5387G271. (M) 2 L 7 2 4F A16WE 1998061900693 19980619 00693 NM 1998 6 19 USAA980209 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCH LONG STATION 360 AT STRINGER 20R FRAME. INSTALLED REPAIR D OUBLER AND REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1998061900694 19980619 00694 NM 1998 6 19 USAA980210 1 19980515 A 5312 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS BS 178 LBL 4.75 WL 201 AND WL 198 BULKHEAD WEB. INSTA LLED DOUBLER AND REPAIRED PER TR 53-10-11. (M) 2 L 7 2 4F A16WE 1998061900695 19980619 00695 NM 1998 6 19 USAA980211 1 19980515 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 706-714 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH LONG STATION 706 TO 714 BL '0' LONGITUDINAL FLOORBEAM. INS TALLED DOUBLER REPAIRED PER SB 737-57-1210 AND EA 43855. (M) 2 L 7 2 4F A16WE 1998061900696 19980619 00696 NM 1998 6 19 USAA980212 1 19980515 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 676.5 WL 206 LBL 25 FLOORBEAM UPPER TEE DOUBLER AND TRIPLER OF LONGITUDINAL FLOOR SUPPORT. INSTALLED DOUBLER AND CHANNEL, REPAIRED PER EO 5791G632, 65C3453726. (M) 2 L 7 2 4F A16WE 1998061900697 19980619 00697 NM 1998 6 19 USAA980213 1 19980515 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 676.5 CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK STATION 676.5, WL 206 PLUS WL 204, RBL 25 FLOORBEAM DOUBLER AND TRIPLER ON LONG FLOORBEAM UPPER AND LOWER CHORD. INSTALLED NEW DOUBLER AND CHANNEL, REPAIRED PER EO 5791G632 AND 6 5C34537-26. (M) 2 L 7 2 4F A16WE 1998061900698 19980619 00698 NM 1998 6 19 USAA980214 1 19980515 A 5330 SKIN BOEING 737 737201 1384454 NM ENTRY DOORWAY CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AFT ENTRY DOOR LOWER HINGE CUTOUT, LOWER FORWARD EDGE OF FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER, REPAIRED PER SRM 53-30-3 FIG 34. (M) 2 L 7 2 4F A16WE 1998061900699 19980619 00699 NM 1998 6 19 USAA980215 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 2 INCH LONG STATION 360 STRINGER 20 R FRAME. INSTALLED REPAIR ANG LE, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1998061900700 19980619 00700 NM 1998 6 19 USAA980216 1 19980515 A 5320 DOUBLER BOEING 737 737201 1384454 NM BS 952 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK STATION 952 STRINGER 12 LEFT DOUBLER. REPLACED DOUBLER A ND REPAIRED PER TR53-30-07. (M) 2 L 7 2 4F A16WE 1998061900701 19980619 00701 NM 1998 6 19 USAA980217 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 296 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .75 INCH CRACK FORWARD SERVICE DOOR CUTOUT FORWARD FRAME STATION 296, WL 208.5 LOW INBOARD RADIUS. INSTALLED REPAIR ANGLE, REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F A16WE 1998061900702 19980619 00702 NM 1998 6 19 USAA980218 1 19980515 A 5320 CHORD BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 727 BULKHEAD LBL 25 COMPRESSION CHORD. STOP DRILLED AND INSTALLED DOUBLER. REPAIRED PER TR 53-10-03A. (M) 2 L 7 2 4F A16WE 1998061900703 19980619 00703 NM 1998 6 19 USAA980219 1 19980515 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 706-714 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH LONG STATION 706 TO 714 LBL 25 LONGITUDIAL FLOORBEAM. INST ALLED DOUBLER, REPAIRED PER SRM 51-40-2 FIG 1. (M) 2 L 7 2 4F A16WE 1998061900704 19980619 00704 NM 1998 6 19 USAA980220 1 19980515 A 5320 CHORD BOEING 737 737201 1384454 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK 4 INCH LONG STATION 663 BL '0' UPPER CHORD AND WEB. INSTALLED REP AIR DOUBLERS AND REPAIRED PER EA 43856. (M) 2 L 7 2 4F A16WE 1998061900705 19980619 00705 NM 1998 6 19 USAA980221 1 19980515 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 10 INCH BY 2 INCH AREA OF CORROSION FUSELAGE SKIN AT STATION 727, LBL 5. 5 TO RBL 5.5. SKIN DOUBLER INSTALLED PER SRM 53-30-3 FIG 28. CORROSION TASK NR C53-101-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998061900706 19980619 00706 NM 1998 6 19 USAA980223 1 19980515 A 5320 CHORD BOEING 737 737201 1384454 NM BS 259 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING Q-5 CHECK VISUAL INSPECTIN, FOUND 25 INCHES CORRODED AREA BS 259 LBL 10 RBL 10 WL 207 CHORDS. INSTALLED RE PAIR FOR 65-45804-535 AND REPLACED 65-458-4-534, REPAIRED PER TR 53-10-16. CORROSION TASK NR C53-101-01, CORROSION LEVE L 2. (M) 2 L 7 2 4F A16WE 1998061900707 19980619 00707 NM 1998 6 19 USAA980192 1 19980512 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 687 SCRATCH A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AU 41932 22884 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND 3 INCH SCRATCH APPROX .025 INCH DEEP IN CROWN SKIN STATON 687, STRINGER 1L. BURNISHED AND INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998061900708 19980619 00708 NM 1998 6 19 USAA980193 1 19980512 A 5330 SKIN BOEING 737 7372B7 1384560 NM ENTRY DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 272AU 41932 22884 ROA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK IN SKIN FORWARD SIDE OF LOWER HINGE CUTOUT AT FORWARD E NTRY DOOR. INSTALLED DOUBLER, REPAIRED PER SRM 53-30-3 FIG 31. (M) 2 L 7 2 4F A16WE 1998061900709 19980619 00709 NM 1998 6 19 USAA980179 1 19980509 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 717-715 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 712-715 25 INCHES RBL WL 103 LONGITUDINAL FLOORBEAM WEB. INSTALLED WEB REPAIR PARTS, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998061900710 19980619 00710 NM 1998 6 19 USAA980180 1 19980509 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 717-715 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 712-715 WL 203 BL '0' LONGITUDINAL FLOORBEAM WEB. CUTOU T DAMAGED AREA, INSTALLED WEB REPAIR PARTS AND REPAIRED PER EO 5394G176 AND DRAWING 165C34537. (M) 2 L 7 2 4F A16WE 1998061900711 19980619 00711 NM 1998 6 19 USAA980181 1 19980509 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 695 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 695 LBL 45 WL 202.5 LONGITUDINAL FLOORBEAM. INSTALLED R EPAIR ANGLES, REPAIRED PER SRM 51-40-4 FIG 1. (M) 2 L 7 2 4F A16WE 1998061900712 19980619 00712 NM 1998 6 19 USAA980182 1 19980509 A 5210 SKIN BOEING 737 737201 1384454 NM ENTRY DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK FUSELAGE SKIN AT LOWER HINGE CUTOUT AFT ENTRY DOOR. INST ALLED SKIN REPAIR/MOD, REPAIRED PER SRM 53-30-3 FIG 34. (M) 2 L 7 2 4F A16WE 1998061900713 19980619 00713 NM 1998 6 19 USAA980183 1 19980509 A 5240 SKIN BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .0625 INCH CRACK IN FUSELAGE SKIN UPPER FORWARD END OF CUTOUT AFT SERVIC E DOOR FUSELAGE SKIN. INSTALLED EXT DOUBLER, REPAIRED PER SRM 53-30-3 FIG 21A. (M) 2 L 7 2 4F A16WE 1998061900714 19980619 00714 NM 1998 6 19 USAA980184 1 19980509 A 5320 DOUBLER BOEING 737 737201 1384454 NM BS 374 TORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH TEAR IN BONDED DOUBLER BS 374, RBL 2 AT EQUIPMENT COOLING DUCT OU TLET. INSTALLED EXT SKIN DOUBLER, REPAIRED PER TR 53-30-4. (M) 2 L 7 2 4F A16WE 1998061900715 19980619 00715 NM 1998 6 19 USAA980185 1 19980509 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 1016 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 2 INCH CHAFE MARK ON MAIN FRAME 'I' BEAM BS 1016, RBL 34, 67 I NCHES ABOVE FLOOR WL 275. FABRICATED AND INSTALLED DOUBLER, REPAIRED PER EA 43941. (M) 2 L 7 2 4F A16WE 1998061900716 19980619 00716 NM 1998 6 19 USAA980186 1 19980509 A 5320 CHORD BOEING 737 737201 1384454 NM BS 718 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 6 INCHES STATION 718 LEFT KEEL BEAM CHORD. INSTALLE D DOUBLER, REPAIRED PER EA 43946. CORROSION TASK NR C53-212-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998061900717 19980619 00717 NM 1998 6 19 USAA980187 1 19980509 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 986.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS OF 1 INCH BY 1 INCH EACH BS 986.5 LBL 42 INCHES T O RBL 40 FLOORBEAM. REMOVED UPPER CHORD, INSTALLED TEE CHORD WITH SPLICE ANGLES AND STRAPS. REPAIRED PER EA 43952. CO RROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998061900718 19980619 00718 NM 1998 6 19 USAA980188 1 19980509 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 947.5 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT CLIPNUT HOLES ON FLOORBEAM UPPER 'T' CAP BS 947.5, RBL 8 TO RBL 50 (RT END). INSTALLED 'T' CAP REPAIR, REPAIRED PER TR 53-10-05C. CORROSION TASK NR C53-107-02, CORROSION LEVEL 1 . (M) 2 L 7 2 4F A16WE 1998061900719 19980619 00719 NM 1998 6 19 USAA980189 1 19980509 A 5240 FRAME BOEING 737 737201 1384454 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK IN DOOR FRAME CUTOUT JUST BELOW DOOR CENTERING FITTING (O N DOOR) FORWARD SERVICE DOOR. INSTALLED DOOR FRAME REPAIR, REPAIRED PER SRM 52-20-1, 51-40-3. (M) 2 L 7 2 4F A16WE 1998061900720 19980619 00720 NM 1998 6 19 USAA980190 1 19980509 A 5320 WEB BOEING 737 737201 1384454 NM BS 180 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 257AU 40383 22799 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 180 LBL 26 INCHES WL 195 SHEAR WEB. INSTALLED DOUBLER A ND COVER PLATE ON 178 PRESSURE BULKHEAD, REPAIRED PER SRM 53-10-11 AND TR 53-10-18. (M) 2 L 7 2 4F A16WE 1998061900721 19980619 00721 NM 1998 6 19 USAASB98109 1 19980509 A 2170 V1211 COALESCER BAG BOEING 737 737201 1384454 NM CABIN DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 254AU 22796 GSO - FLT 1704, EN ROUTE ATL-BWI, BOTH THE FORWARD AND AFT CABIN SMOKE DETECTOR ALARMS WENT OFF DURING FLIGHT. CREW NOT ED A BURNING PLASTIC SMELL BUT COULD NOT LOCATE SOURCE. THERE WAS NO INDICATION OF SMOKE OF FIRE. FLIGHT DIVERTED TO G SO AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED. MAINTENANCE DETERMINED THE A/C TO HAVE OILY SMELL IN THE CA BIN. RAN BOTH ENGINES WITH PACKS ON HOT AND BURNED OIL OUT OF DUCTS, THEN RAN BOTH ENGINES AND PACKS AT CRUISE POWER FO R 15 MINUTES. NO FURTHER SMELL NOTED. REPLACED BOTH WATER SEPARATOR BAGS AS PRECAUTIONARY. (M) 2 L 7 2 4F A16WE 1998061900722 19980619 00722 NM 1998 6 19 USAA980194 1 19980512 A 5315 654581292 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 328 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 31093 24412 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 7.5 INCH CORROSION AREA ON FLOORBEAM 328 UPPER AND LOWER SURFACE OF UP PER T-CAP RBL 14.5 TO RBL 56.5. CORROSION NR C53-107-02. REPLACED T-CAP AND INSTALLED SPLICE ANGLES PER TYPICAL REPAIR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998061900723 19980619 00723 NM 1998 6 19 USAA980195 1 19980512 A 5315 6545815180 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344.17 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 31093 24412 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 4 INCH CRACK ON FLOORBEAM 344.17 UPPER 'T' CAP LBL 7 TO LBL 35. CORROSI ON NR C53-170-02. REPAIRED 'T' CAP TO FLOORBEAM PER TYPICAL REPAIR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998061900724 19980619 00724 NM 1998 6 19 USAA980196 1 19980512 A 5320 69353651 WEB BOEING 737 7373B7 1384580 NM BS 380/400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 31093 24412 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO 2 INCH CRACKS BETWEEN BS 380 AND BS 400 AT BL 0 SHEAR WEB INSTALLATI ON. FABRICATED NEW ANGLE AND INSTALLED ANGLE ON SHEAR WEB PER REPAIR DOCUMENT SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1998061900725 19980619 00725 NM 1998 6 19 USAA980197 1 19980512 A 5315 65468101 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 967 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 530AU 31093 24412 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION APPROX 1.5 INCH ON FLOORBEAM FWD FLANGE LBL 45 BS 967 PAX FLOO R. CORROSION NR C53-107-02. INSTALLED FILLER AND DOUBLER ANGLES ON FWD FLANGE PER SRM 53-50-51 FIG 202 AND EA 61664. ( M) 2 L 7 2 4F RT A16WE 1998061900726 19980619 00726 EU 1998 6 19 C2XA98IA178 1 19980517 A 5315 S53672408202 FRAME AEROSP ATR42 ATR42320 8680930 EU CABIN FLOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM AT FRAME 39 CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED REPAIR DOBLERS IAW CONTINENTAL EXPRESS ATR-42 ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-01037. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900727 19980619 00727 EU 1998 6 19 C2XA98IA177 1 19980517 A 5315 S53672409218 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM AT FRAME 40 CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED REPAIR DOUBLERS IAW CONTINENTAL EXPRESS ATR-42 ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-01037. THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900728 19980619 00728 EU 1998 6 19 C2XA98IA176 1 19980517 A 5312 S5387140921401 BLKHD STIFFENER AEROSP ATR42 ATR42320 8680930 EU AFT PRESS BLKHD CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND AFT PRESSURE BULKHEAD LOWER STIFFENER CORRODED. MAINTENANCE REMOVED AND REPLACED THE STIFFENER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900729 19980619 00729 EU 1998 6 19 C2XA98IA175 1 19980517 A 5315 S5367240820200 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM AT FRAME 36 CORRODED ON UPPER AND LOWER SURFACE. MAINTENANCE REMOVED A ND REPLACED THE FLOORBEAM IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900730 19980619 00730 EU 1998 6 19 C2XA98IA174 1 19980517 A 5320 S53671406202 DOUBLER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND VHF ANTENNA DOUBLER CORRODED AND CRACKED AFT OF FRAME 33 LOWER FUSELAGE. MAINTEN ANCE REMOVED AND REPLACED THE DOUBLER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900731 19980619 00731 EU 1998 6 19 C2XA98IA173 1 19980517 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT CENTER SEAT TRACK CORRODED FROM FRAMES 29 TO 36. MAINTENANCE REMOVED A ND REPLACED THE SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900732 19980619 00732 EU 1998 6 19 C2XA98IA172 1 19980517 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLIGHT ATTENDANTS SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900733 19980619 00733 EU 1998 6 19 C2XA98IA171 1 19980517 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, RIGHT AFT OUTBOARD SEAT TRACK CORRODED FROM FRAMES 31 TO 36. MAINTENANCE REMOVED AND R EPLACED THE SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900734 19980619 00734 EU 1998 6 19 C2XA98IA170 1 19980517 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM AT FRAME 38 CORRODED ON UPPER AND LOWER SURFACES. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900735 19980619 00735 EU 1998 6 19 C2XA98IA169 1 19980517 A 5210 S5217666500200 SHOOT BOLT AEROSP ATR42 ATR42320 8680930 EU PASSENGER DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER DOOR CENTER AFT SHOOT BOLT WORN. MAINTENANCE REMOVED AND REPLACED THE SHOOT BOLT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900736 19980619 00736 EU 1998 6 19 C2XA98IA168 1 19980517 A 5210 S5217666400200 SHOOT BOLT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER DOOR TOP FORWARD SHOOT BOLT WORN. MAINTENANCE REMOVED AND REPLACED THE SHOOT BOLT. THE AIRCRAFT WAS APPRVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900737 19980619 00737 EU 1998 6 19 C2XA98IA167 1 19980517 A 5210 S5217666400200 SHOOT BOLT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER DOOR CENTER FORWARD SHOOT BOLT WORN. MAINTENANCE REMOVED AND REPLACED THE SHOOT BOLT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900738 19980619 00738 EU 1998 6 19 C2XA98IA166 1 19980517 A 5240 S5247764300200 SHOOT BOLT AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND SERVICE DOOR AFT UPPER SHOOT BOLT WORN. MAINTENANCE REMOVED AND REPLACED THE SHO OT BOLT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900739 19980619 00739 EU 1998 6 19 C2XA98IA165 1 19980517 A 5320 S5397130920401 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND CENTER SUPPORT DIAPHRAGM FOR PANEL 194CR CRACKED. MAINTENANCE REMOVED AND REPLAC ED THE SUPPORT IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900740 19980619 00740 EU 1998 6 19 C2XA98IA164 1 19980517 A 5313 S53671400230 STRINGER AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND STRINGER 21 LEFT CORRODED AFT OF FRAME 41. MAINTENANCE REMOVED THE DAMAGED SECTI ON OF THE STRINGER AND INSTALLED A REPAIR SPLICE IN REFERENCE TO ATR-42 SRM 53-00-00 AND 51-21-28. THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900741 19980619 00741 EU 1998 6 19 C2XA98IA163 1 19980517 A 5320 S5367131120601 ANGLE AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FRAME 37 FAIL/SAFE ANGLE BELOW SERVICE DOOR THRESHOLD CORRODED. MAINT ENANCE REPLACED THE FAIL/SAFE ANGLE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT AFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900742 19980619 00742 EU 1998 6 19 C2XA98IA162 1 19980517 A 5320 S53671257208 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND INTERCOSTAL AT STRINGER 17 RIGHT CORRODED BETWEEN FRAMES 38 AND 39. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IN FERFERENCE TO ATR-42 SRM 51-25-01 (02, 04) AND 51-21-42. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900743 19980619 00743 EU 1998 6 19 C2XA98IA161 1 19980517 A 5320 S53671257206 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND INTERCOSTAL AT STRINGER 17 RIGHT CORRODED BETWEEN FRAMES 37 AND 38. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IN REF TO ATR-42 SRM 51-25-01 (02, 04) AND 51-21-42. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900744 19980619 00744 EU 1998 6 19 C2XA98IA160 1 19980517 A 5320 S53671257202 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND INTERCOSTAL AT STRINGER 17 RIGHT, CORRODED BETWEEN FRAMES 36 AND 37. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IN REFERENCE TO ATR-42 SRM 51-25-01 (02, 04) AND 51-21-52. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900745 19980619 00745 EU 1998 6 19 C2XA98IA159 1 19980517 A 5320 S53671257228 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND INTERCOSTAL AT STRINGER 17 RIGHT BETWEEN FRAMES 35 AND 36 CORRODED. MAINTENANCE REMOVED AND REPLACED THE INTERCOSTAL IN REFERENCE TO ATR-42 SRM 51-25-01 (02, 04) AND 51-21-42. THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900746 19980619 00746 EU 1998 6 19 C2XA98IA158 1 19980517 A 5280 S5287660600401 HINGE AEROSP ATR42 ATR42320 8680930 EU NLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT NOSE LANDING GEAR DOOR FORWARD HINGE CRACKED. MAINTENANCE REMOVED AND R EPLACED THE DOOR HINGE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900747 19980619 00747 EU 1998 6 19 C2XA98IA157 1 19980517 A 5744 NSA504208236 FITTING AEROSP ATR42 ATR42320 8680930 EU LT WING ELONGATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING RIB 5 LUG FITTING FOR FLAP HINGE, FASTENER HOLE ELONGATED. MAINTENANCE REPAIRED THE WING LUG IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5750-01112. THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900748 19980619 00748 EU 1998 6 19 C2XA98IA156 1 19980517 A 5311 S53871409201401 FRAME AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 44 CORRODED ON FORWARD AND AFT SIDES. MAINTENANCE REMOVED THE DAMAGED SECT ION OF FRAME AND INSTALLED A REPAIR SLICE IAW ATR-42 REPAIR DRAWING NR 18S538R-0031 AND CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-01089. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900749 19980619 00749 EU 1998 6 19 C2XA98IA155 1 19980517 A 5341 S5357280020800 FITTING AEROSP ATR42 ATR42320 8680930 EU WING/FUS CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOND LEFT SIDE WING TO FUSELAGE FITTING AT FRAME 27 TO HAVE A CRACK INDICATION AT BOLT HOLE NR 1 USING EDDY CURRENT INSPECTION METHOD IAW ATR-42 NDTM 53-56-03. MAINTENANCE REMOVED AND REPLACED THE RADIUS FI LLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5340-01034. THE AIRCRAFT WAS APPROVED FOR RETRN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900750 19980619 00750 EU 1998 6 19 C2XA98IA154 1 19980517 A 5341 S5357280020800 FITTING AEROSP ATR42 ATR42320 8680930 EU WING/FUS CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WING TO FUSELAGE FITTING AT FRAME 27 TO HAVE A CRACK INDICATION AT BOLT HOLE NR 2 USING EDDY CURRENT INSPECTION METHOD IAW ATR-42 NDTM 53-56-03. MAINTENANCE REPAIRED THE CRACK IAW CONTINENTA L EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5340-01034. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900751 19980619 00751 EU 1998 6 19 C2XA98IA153 1 19980517 A 5341 S5357280020800 FITTING AEROSP ATR42 ATR42320 8680930 EU WING/FUS CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WING TO FUSELAGE FITTING AT FRAME 27 TO HAVE A CRACK INDICATION AT BOLT HOLE NR 3 USING EDDY CURRENT INSPECTION METHOD IAW ATR-42 NDTM 53-56-03. MAINTENANCE REPAIRED THE CRACK IAW CONTINENTA L EXPERSS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5340-01034. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900752 19980619 00752 EU 1998 6 19 C2XA98IA152 1 19980517 A 5230 S5337121415064 LATCH AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND CENTER AND AFT CARGO DOOR LATCH FITTINGS DAMAGED. MAINTENANCE REMOVED AND REPLAC ED THE FITTINGS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900753 19980619 00753 EU 1998 6 19 C2XA98IA151 1 19980517 A 5320 S53571401208 STRAP AEROSP ATR42 ATR42320 8680930 EU RT MLG WW CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17831 185 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WELL FORWARD CORNER FUSELAGE STRAP CRACKED AT FRAME 25. M AINTENANCE INSTALLED AN EXTERNAL DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-0 1088. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900754 19980619 00754 EU 1998 6 19 C2XA98BT034 1 19980519 A 3260 D22924010 SWITCH AEROSP ATR42 ATR42320 8680930 EU RT MLG FAULTED A C2XA O OTHER N FALSE WARNING CR CRUISE 1 SW 09 34817 152 EWR - CREW REPORTED, 'LANDING GEAR POSITION INDICATOR SYSTEM 2 RIGHT MAIN UNLOCK NO GREEN LIGHT. WE GOT ASSOCIATED GPWS AND MASTER WARNING. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED RIGHT MAIN LANDING GEAR SYSTEM 2 SWITCH ASSEMBLY OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998061900755 19980619 00755 EU 1998 6 19 C2XA98BT033 1 19980516 A 3260 DHE1148 SWITCH AEROSP ATR72 ATR72212 EU LT MLG INOPERATIVE A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 12903 459 BDL - ON RON IN HARTFORD, LEFT MAIN GEAR UNLOCK LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED MAIN LANDING GEAR P ROXIMITY SWITCH AND OPERATIONALLY CHECKED THE SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998061900756 19980619 00756 EU 1998 6 19 C2XA98IA179 1 19980506 A 5230 S5337122301200 LATCH AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, FOUND CARGO DOOR FORWARD LATCH FITTING AFT LUG HAD CRACK INDICATION WHEN INSPECTED USIN G ULTRASONIC METHOD IAW ATR-42 NDTM 53-37-06. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR FITTING. THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900757 19980619 00757 EU 1998 6 19 C2XA98IA180 1 19980506 A 5311 S53671311200 FRAME AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FRAME NR 37 CORRODED ON FORWARD AND AFT SIDES AT SERVIEC DOOR THRESHOL D. MAINTENANCE REMOVED THE DAMAGED AREA OF THE FRAME AND INSTALLED REPAIR DOUBLER IAW ATR-42 SRM 57-67-70. THE AIRCRAF T WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900758 19980619 00758 EU 1998 6 19 C2XA98IA181 1 19980506 A 5315 S53172158204 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14828 179 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOORBEAM AT FRAME NR 7 CORRODED. MAINTENANCE REMOVED THE CORROSION, F ABRICATED AND INSTALLED ANGLE AND REINFORCEMENT STRAP IAW CONTINENTAL EXPRESS ATR-42 ENGINEERING CHANGE/REPAIR AUTHORIZA TION (EC)5310-01037. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900759 19980619 00759 SO 1998 6 19 C2XA98CL038 1 19980505 A 3233 23092800503 ACTUATOR EMB 145 EMB145 SO RT MLG UNLOCK FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 15932 044 145015 CLE - FLT 4032 - CREW REPORTED THAT UPON TAKEOFF THE RIGHT MAIN LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED T O FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT MAIN LANDING G EAR UNLOCK ACTUATOR IAW EMB145 MM 32-33-09, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVIC E. (M) 2 L 7 2 4F RT T00011AT 1998061900760 19980619 00760 EU 1998 6 19 C2XA98IA144 1 19980429 A 5320 S5367800821602 ZEE CHANNEL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING C-CHECK INSPECTION, THE RIGHT Z-CHANNEL AT FRAME 39 TO 41 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED SECTION OF Z-CHANNEL IAW ATR42-320 SRM 51-25-02 AND 51-25-03, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900761 19980619 00761 EU 1998 6 19 C2XA98IA150 1 19980429 A 5311 S53671311200 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING C-CHECK INSPECTION, FRAME 37 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CO NTINENTAL EXPRESS ENGINEERING AND CHANGE REPAIR AUTHORIZATION EC5310-01013, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900762 19980619 00762 EU 1998 6 19 C2XA98IA149 1 19980429 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING C-CHECK INSPECTION, THE LEFT FLIGHT ATTENDANTS SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE SEAT TRACK IAW ATR42-320 SRM 51-25-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900763 19980619 00763 EU 1998 6 19 C2XA98IA148 1 19980429 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS RIGHT SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE SEAT TRACK IAW ATR 42-300 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900764 19980619 00764 EU 1998 6 19 C2XA98IA147 1 19980429 A 3350 3011206 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERTIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY IAW ATR42-320 MM 33-51-24, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1998061900765 19980619 00765 EU 1998 6 19 C2XA98IA146 1 19980429 A 5311 S53970916234 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING C-CHECK INSPECTION, THE FRAME BETWEEN PANELS 295AL AND 295EL WAS FOUND TO BE CRACKED. MAINTENANCE PERFORME D A DOUBLER REPAIR IAW ATR 42-320 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900766 19980619 00766 EU 1998 6 19 C2XA09IA145 1 19980429 A 3350 3011160 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR CUTOUT EMERGENCY LIGHT WAS FOUND TO OPERATE INTERMITTENTLY. MAINTENAN CE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND OPERATIONALLY CHECKED IAW ATR42-320 MM 33-51-00, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998061900767 19980619 00767 EU 1998 6 19 C2XA98BT032 1 19980511 A 3350 013042PBE BULB AEROSP ATR42 ATR42320 8680930 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 EWR - ON LINE CHECK FOUND RIGHT EMERGENCY LIGHT BROKEN. MAINTENANCE RELAMPED BULB AS REQUIRED. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998061900768 19980619 00768 EU 1998 6 19 C2XA98BT031 1 19980508 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34820 159 BTV - DURING A 2A INSPECTION, FOUND 'EMERGENCY LIGHTS DO NOT WORK PROPERLY WITH 6WL C/B PULLED. REMOVED AND REPLACED BA TTERY IN POWER SUPPLY 30WL. OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998061900769 19980619 00769 NM 1998 6 19 ASAA9810031 1 19980424 A 5511 RIB BOEING 737 7372Q8C 138448S NM HORIZ STABILIZER WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING C-CHECK, WEAR WAS FOUND AT THE HORIZONTAL STABILIZER TRAILING EDGE RIBS AT STATION 66.54, 94.07, AND 121.9. REPAIRED PER EA 5510-01066 AND BOEING TELEX'S ASA-SEA-91-0202RR AND ASA-SEA-97-004RR. (M) 2 L 7 2 4F A16WE 1998061900770 19980619 00770 NM 1998 6 19 ASAA9810030 1 19980424 A 5315 FLOORBEAM BOEING 737 7372Q8C 138448S NM BS 500 CORRODED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING C-CHECK. FOUND CORROSION WAS FOUND IN THE LOWER FORWRD FLANGE OF THE FLOORBEAM AROUND A FASTENER HOLE AT ST ATION 500, LBL 9. REPAIRED PER EA 5310-01579. (M) 2 L 7 2 4F A16WE 1998061900771 19980619 00771 WP 1998 6 19 VJ9800191 1 19980613 A 2410 696233A CSD DOUG DC9 DC932 3022066 WP LT ENGINE FAILED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 932VV 47451 LT GENERATOR PADDED AND APU CARRYING LT BUSS, RT CSD TEMP INDICATION WENT FULL SCALE HIGH WITH MASTER CAUTION LIGHT ILLU MINATED AND RT CSD OIL PRESSURE LIGHT ON. FLIGHT CREW DISCONNECTED RT CSD AND REQUESTED EMERGENCY AUTHORIZATION TO RETU RN TO ATL MAINTENANCE BASE. REPLACED LT CSD AND GENERATOR ON NR 1 ENGINE, SYSTEM OPS CHECKED OK. REMOVED PLACARD. 2 L 7 2 4F A6WE 1998061900772 19980619 00772 WP 1998 6 19 VJ9800192 1 19980614 A 5610 4616968501 MECHANISM DOUG DC9 DC932 3022066 WP COCKPIT WINDOW OUT OF ADJUST A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 CAPTAIN'S WINDOW WOULDN'T OPEN. ADJUSTED UPPER RELEASE MECHANISM, OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998061900773 19980619 00773 WP 1998 6 19 VJ9800193 1 19980612 A 2130 94840211 AMPLIFIER DOUG DC9 DC932 3022066 WP E/E COMPT FAILED A ZZDA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 15 966VV 47168 EMERGENCY DESCENT PERFORMED BECAUSE AUTO PRESSURIZATION CONTROL INOP, MANUAL WAS OK. PASSENGER OXYGEN MASKS DEPLOYED. R EPLACED OUTFLOW ACTUATOR AND RIGGED SUGAR SCOOP AS PRECAUTIONARY MEASURE AND REPLACED PRESSURE AMPLIFIER. PERFORMED TES T FLIGHT AND AUTO PRESSIZATION SYSTEM CHECKED NORMAL. 2 L 7 2 4F A6WE 1998061900774 19980619 00774 NM 1998 6 19 AWXA9800145 1 19980615 A 3350 CONNECTOR BOEING 757 7572S7 1384962 NM CABIN FAILED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 902AW 23322 DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SECTION OF EMERGENCY EXIT LIGHTS INOP ON SEATS AND DOORS. REMOVED AND REPLA CED FUSE ON POWER SUPPLY AND REPAIRED CONNECTOR AT L-4 DOOR, OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 1998061900775 19980619 00775 SO 1998 6 19 RAAA98E4017 1 19980612 A 3213 800808 STRUT LKHEED 188 188C 5262604 SO RT MLG BROKEN A RAAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 9744C 206 188C1140 ON CLIMBOUT, FLIGHT CREW REPORTED RIGHT MAIN LANDING GEAR INTRANSIT LIGHT DID NOT EXTINGUISH WITH LANDING GEAR CONTROL H ANDLE IN UP POSITION. WHEN NEUTRAL SELECTED RIGHT MAIN LANDING GEAR FELL FROM WELL TO DOWN AND LOCKED POSITION. REROUT ED TO ANC AND ACCOMPLISHED UNSCHEDULED LANDING WITHOUT INCIDENT. FOUND RIGHT MAIN LANDING GEAR SHOCK STRUT CYLINDER LT AFT TRUNNION ARM ATTACH LUG BROKEN. CHANGED RIGHT MAIN LANDING GEAR ASSY PER AF 32-2-0. ADJUSTED LDG DOORS PER L188 MM 32-0. 2 L 7 4 4T 4A22 1998061900776 19980619 00776 SO 1998 6 19 RAAA98E8018 1 19980612 A 3350 873100112 LIGHT LKHEED 188 188C 5262604 SO CABIN INOPERATIVE A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 PAX ROW 7 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 4 4T 4A22 1998061900777 19980619 00777 NM 1998 6 19 CALA9801062 1 19980612 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 360 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND SMALL DENTS IN RT FUSELAGE SKIN JUST FORWARD OF STA 360 BETWEEN STRINGERS 18R AND 19R. REPAIRED IAW EC RA 5331-01024. 2 L 7 2 4F RT A16WE 1998061900778 19980619 00778 WP 1998 6 19 CALA9801063 1 19980613 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1065 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT STA 1065 BETWEEN LONGERON 2L AND 3L. THE SKIN WAS CUT OUT AND REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1998061900779 19980619 00779 WP 1998 6 19 CALA9801064 1 19980614 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND BELTFRAME CORRODED IN AFT BAGGAGE BIN AT STA 1271, LONGERON 30. A BELTFRAME AND SPLICES WERE INSTALLED IAW SRM 53-03, FIGURE 2A. 2 L 7 2 4F A6WE 1998061900780 19980619 00780 WP 1998 6 19 CALA9801065 1 19980614 A 5712 RIB DOUG DC9 DC982 3022082 WP WS 270-289 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 33817 49371 INSPECTION FOUND THREE .75 INCH CRACKS IN RT WING LEADING EDGE RIBS AT STA XRS 276.5, XRS 270, AND XRS 289. THE RIBS WE RE REMOVED AND NEW RIBS WERE INSTALLED IAW ECRA 5721-01008. 2 L 7 2 4F A6WE 1998061900781 19980619 00781 WP 1998 6 19 CALA9801066 1 19980614 A 5753 SKIN DOUG DC10 DC1010 3022110 WP LT TE FLAP CANNED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND OIL CANNING ON LEFT INBOARD TRAILING EGDE FLAP UPPER SKIN AT INBOARD SIDE. THE DAMAGED SKIN SECTION WA S REMOVED, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-30-02. 2 L 7 3 4F A22WE 1998061900782 19980619 00782 WP 1998 6 19 CALA9801067 1 19980614 A 5312 BULKHEAD TEE DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 2.5 INCH CRACK ON BULKHEAD TEE VERTICAL LEG AT LT BS 1156 BETWEEN LONGERON 39L AND 40L. A 2.5 INCH C RACK WAS FOUND ON BULKHEAD TEE HORIZONTAL LEG AT LT BS 1156 BETWEEN LONGERON 38L AND 39L. THE BULKHEAD TEE WAS REPAIRED IAW DOUGLAS DRAWING SR10530073. 2 L 7 3 4F A22WE 1998061900783 19980619 00783 WP 1998 6 19 CALA9801068 1 19980612 A 3320 6910 BALLAST DOUG DC10 DC1030 3023501 WP CABIN FAILED A CALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 76073 46940 SMOKE STARTED COMING FROM OVERHEAD ABOVE ROW 44L JUST PRIOR TO LANDING. HALON WAS APPLIED AND THE SMOKE CEASED. MAINTE NANCE FOUND SIDEWALL BALLAST AT ROW 44L BURNT. THE BALLAST WAS REMOVED AND THE SIDEWALL LIGHT WAS PLACARD INOPERATIVE. 2 L 7 3 4F A22WE 1998061900784 19980619 00784 WP 1998 6 19 CALA9801069 1 19980615 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CABIN FLOOR PANEL NR 29 CORRODED ON UPPER AND LOWER SURFACES AT STA 237, BL 0 TO RBL 22. A NEW PANEL W AS FABRICATED AND INSTALLED IAW SRM 53-05 AND 51-70-2. 2 L 7 2 4F A6WE 1998061900785 19980619 00785 WP 1998 6 19 CALA9801070 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CABIN FLOORBOARD NR 45B FORWARD LEADING EDGE LIP CRACKED AND TORN. THE TORN AREA WAS ROUTED OUT. A RE PAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, PAGE 122, FIGURE 4, 51-10-3 AND 51-10-4. 2 L 7 2 4F A6WE 1998061900786 19980619 00786 WP 1998 6 19 CALA9801071 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 756/680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT SIDE FLOORBOARD HAD FOUR CRACKS AT SCREW HOLES OF FS 756 AND THREE CRACKS AT SCREW HOLES OF FS 680. THE HAT SECTIONS WERE REMOVED, A NEW FLOOR PANEL WAS FABRICATED AND HAT SECTIONS WERE BONDED TO NEW PANEL IAW SRM 51-30 -2, 51-10-2, 51-10-3, 53-05, AND 51-20-0. 2 L 7 2 4F A6WE 1998061900787 19980619 00787 WP 1998 6 19 CALA9801072 1 19980615 A 5320 CLIP DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND TIE CLIP CRACKED AT STA 996, RBL 56. A NEW TIE CLIP WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 1 AND 51-10-3. 2 L 7 2 4F A6WE 1998061900788 19980619 00788 WP 1998 6 19 CALA9801073 1 19980615 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 851 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FITTING UNDER FRAME AT STA 851, LONGERON 27 TO 28R CORRODED. THE FITTING WAS REPAIRED IAW SRM 51-10-4, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1998061900789 19980619 00789 WP 1998 6 19 CALA9801074 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CRACKS AT THREE SCREW HOLES IN RT FLOORBOARD NR 41. A STRAP WAS FABRICATED AND INSTALLED ON FLOOR PANE L IAW SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A6WE 1998061900790 19980619 00790 WP 1998 6 19 CALA9801075 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CRACKS AT FORWARD AND AFT ENDS OF FLOORBOARD NR 45. THE FLOORBOARD WAS REPAIRED IAW SRM 53-01, PAGE 9. 2 L 7 2 4F A6WE 1998061900791 19980619 00791 WP 1998 6 19 CALA9801076 1 19980615 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND TWO .25 INCH CRACKS IN TITANIUM FINGER DOUBLER AT STA 996, LONGERON 20L. THE FINGER DOUBLER WAS REMOVE D AND A NEW FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ENGINEERING ORDER 98-888. 2 L 7 2 4F A6WE 1998061900792 19980619 00792 WP 1998 6 19 CALA9801077 1 19980615 A 5320 CLIP DOUG DC9 DC932 3022066 WP BS 996 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND AFT PRESSURE BULKHEAD FORWARD SIDE STA 996 THIRD HORIZONTAL STIFFENER FROM FLOORING HAD CLIP BROKEN OFF . THE FASTENERS WERE REMOVED IAW SRM 51-30-2. A REPAIR CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900793 19980619 00793 WP 1998 6 19 CALA9801078 1 19980615 A 5730 PANEL DOUG DC9 DC932 3022066 WP RT WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A GOUGE IN LOWER RT WING ACCESS PANEL. THE GOUGED AREA WAS CUT OUT, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-6, FIGURE 13. 2 L 7 2 4F A6WE 1998061900794 19980619 00794 WP 1998 6 19 CALA9801079 1 19980615 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN CABIN WEB AT STA 756, LBL 53. THE WEB WAS REMOVED IAW SRM 51-30-2. TWO REPAIR DOUBL ERS WERE FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-4, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900795 19980619 00795 WP 1998 6 19 CALA9801080 1 19980615 A 5320 ANGLE DOUG DC9 DC932 3022066 WP DORSAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN LT DORSAL FIN PANEL ATTACH ANGLE. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ATT ACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A6WE 1998061900796 19980619 00796 SO 1998 6 19 COMA9810136 1 19980605 A 3240 426871 CONTROL UNIT EMB 120 EMB120RT SO E/E COMPT FAILED A COMA K NONE O OTHER LD LANDING 1 SO 01 267CA 120259 AIRCRAFT HAS NO BRAKES DURING LANDING ROLL. REPLACED THE BRAKE CONTROL UNIT. 2 L 7 2 4T RT A31SO 1998061900797 19980619 00797 EA 1998 6 19 COMA9860141 1 19980614 A 3250 STEERING CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 917CA 7017 FULL LEFT RUDDER REQUIRED DURING TAKEOFF ROLL. INSPECTED AIRCRAFT AND FOUND NOTHING THAT COULD CAUSE DISCREPANCY. HIGH SPEED TAXI CHECKS SATISFACTORY. 2 L 7 2 4F RT A21EA 1998061900798 19980619 00798 EA 1998 6 19 COMA9860142 1 19980611 A 5330 601R310211 SKIN CNDAIR CL600 CL6002B19 EA FUSELAGE CRUSHED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 7168 MECHANIC NOTICED FORWARD AND AFT FUSELAGE SKIN IN THE AREA OF THE LOWER DOOR LATCH PINS WAS DAMAGED. SKIN WAS REPAIRED IN ACCORDANCE WITH REO NR 601R-53-21-176 AND 601R-53-21-160. 2 L 7 2 4F RT A21EA 1998061900799 19980619 00799 EA 1998 6 19 COMA980143 1 19980605 A 4980 601R972013 EXHAUST DUCT CNDAIR CL600 CL6002B19 EA APU COMPT CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 APU EXHAUST DUCT HAS A BROKEN TAB AND CHAFING. REPLACED APU EXHAUST DUCT. 2 L 7 2 4F RT A21EA 1998061900800 19980619 00800 EA 1998 6 19 COMA9860144 1 19980605 A 4980 601R9720419 SHIELD CNDAIR CL600 CL6002B19 EA APU EXHAUST CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 APU EXHAUST SHIELD CRACKED. REPLACED APU EXHAUST SHIELD. 2 L 7 2 4F RT A21EA 1998061900801 19980619 00801 EA 1998 6 19 COMA9860145 1 19980606 A 2750 601R93106107 FLEXDRIVE CNDAIR CL600 CL6002B19 EA LT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 LEFT FLAP NR 5 FLEXSHAFT, INBOARD IS UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED FLEXDRIVE. 2 L 7 2 4F RT A21EA 1998061900802 19980619 00802 EA 1998 6 19 COMA9860146 1 19980606 A 2750 601R93106105 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 RIGHT FLEXSHAFT NR 1 UNSERVICEABLE DUE TO SEPARATED STRANDS. REPLACED RIGHT NR 1 FLAP DRIVE FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998061900803 19980619 00803 EA 1998 6 19 COMA9860147 1 19980606 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PAX DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 947CA 7077 FORWARD PAX DOOR SEAL STRIKER HAS DAMAGE TO PREVIOUS REPAIR. REPAIRED IN ACCORDANCE WITH CANADAIR REO 601R-52-11-008. 2 L 7 2 4F RT A21EA 1998061900804 19980619 00804 NM 1998 6 19 UPS98426918 1 19980506 A 5720 BEAM BOEING 747 747123 1384873 NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-C, RT WING SPOILER SUPPORT BEAM UPPER CHORD CRACKED AT I/B END. MODED ANGLES AND SPLICED IN A NEW SECTI ON OF CHORD IAW SRM 51-40-03 AND SB 747-57-224. 2 L 7 4 4F A20WE 1998061900805 19980619 00805 NM 1998 6 19 UPS98426919 1 19980508 A 5313 LONGERON BOEING 747 747123 1384873 NM BS 1245 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-C, CORROSION REPAIR TO OVERWING LONGERON OUTER CHORD AT BS 1241 RT SIDE. THE 2.75 CRACK ON LONGERON FWD END AT BS 1245 CRACK HAS NOW EXTENDED TO 3.75. CRACK FOUND PROPAGATED TO 3.75 REPAIRED IAW BOEING DRAWING 144U3542 AND EO B747-5310-0523. 2 L 7 4 4F A20WE 1998061900806 19980619 00806 NM 1998 6 19 UPS98426920 1 19980506 A 5711 SPAR BOEING 747 747123 1384873 NM WS 1320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 672UP 20324 INSPECTION TYPE-C, CORROSION ON INNER SPAR SKIN EXTENSION RT WING STATION 1320 JUST O/B OF JACKING POINT. REMOVED CORRO SION. 2 L 7 4 4F A20WE 1998061900807 19980619 00807 EU 1998 6 19 QXEA9800791 1 19980611 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 EMERGENCY EXIT LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. LIGHT TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998061900808 19980619 00808 EU 1998 6 19 QXEA9800793 1 19980611 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 EMERGEMCY EXIT LIGHT AT ROW 8 HAS BURNT OUT BULBS. MAINTENANCE REPLACED EMERGENCY EXIT SIGN AND OPERATIONALLY TESTED. L IGHT TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998061900809 19980619 00809 EU 1998 6 19 QXEA9800794 1 19980611 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT INOPERATION A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 COCKPIT ENTRANCE EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED COCKPIT ENTRANCE SIGN AND OPERATIONALLY TESTED. TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998061900810 19980619 00810 EU 1998 6 19 QXEA9800790 1 19980614 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 EXIT LIGHT ABOVE COCKPIT DOOR IS DIM. MAINTENANCE REPLACED 5 28V BULBS IN EXIT SIGN AND OPERATIONALLY TESTED INSTALLATI ON. 2 L 7 2 4F RT A20EU 1998061900811 19980619 00811 EU 1998 6 19 QXEA9800795 1 19980612 A 3350 1012721 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 A 3 VOLT EXIT SIGN ON SEAT 9B IS BROKEN. MAINTENANCE INSTALLED A NEW SIGN ASSEMBLY ON SEAT 9B, OPERATIONAL TESTS ARE NO RMAL. 2 L 7 2 4F RT A20EU 1998061900812 19980619 00812 EU 1998 6 19 QXEA9800796 1 19980614 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 486US 11237 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE, OVER ROW 4. MAINTENANCE RELAMPED, OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998061900813 19980619 00813 EU 1998 6 19 QXEA9800797 1 19980614 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 488US 11240 EMERGENCY EVACUATION LIGHT BURNT OUT AT ROW 8. MAINTENANCE RESEATED THE CONNECTOR FOR THE EVACUATION LIGHT AT ROW 8, OP ERATIONALLY TESTED, FUNCTIONS NORMAL. 2 L 7 2 4F RT A20EU 1998061900814 19980619 00814 NM 1998 6 19 98FDEA00401 1 19980608 A 5330 SKIN BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 485FE 21488 CORROSION ON SKIN AND STRINGER 28L, BS 950E+12 TO 950F+6. CUT OUT CORRODED STR SECTION. INSTALLED STRINGER REPAIR PER SRM 53-10-3. CUT OUT CORRODED SKIN, INSTALLED EXTERNAL REPAIR PER SRM 53-30-3. 2 L 7 3 4F A3WE 1998061900815 19980619 00815 NM 1998 6 19 98FDEA00402 1 19980608 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1120-1126 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 485FE 21488 FUSELAGE BS 1120 TO 1126 SKIN CORROSION UNDER STR 29 LEFT. CUT OUT DAMAGED SKIN AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1998061900816 19980619 00816 NM 1998 6 19 98UAL900196 1 19980516 A 3350 5822 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 648UA 25285 EMERGENCY EXIT FLOOR LIGHTS FLICKER ON AND OFF ON RIGHT SIDE BETWEEN ROWS 15 TO 20. *S/D* REPLACED EMERGENCY LIGHTS PO WER SUPPLY, M1559. 2 L 7 2 4F 4 F RT A1NM E24NE 1998061900817 19980619 00817 NE 1998 6 19 98UAL900216 2 19980526 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RIGHT MALFUNCTIONED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 610UA 21871 709611 DURING CLIMB AND CRUISE, RIGHT ENGINE POWER LEVEL FLUCTUATES WITH THROTTLE LEVEL STATIONARY, RESULTING IN AIRSPEED FLUCT UATION OF +/- 10 KNOTS. *S/D* FUEL PUMP, FUEL CONTROL UNIT, ENGINE VANE AND BLEED CONTROLLER, AIRCRAFT P2/T2 SENSOR AN D FCU TT2 SENSOR WERE REPLACED. THE ENGINE WAS BORESCOPED. THE THROTTLES WERE RIGGED. NO HARD FAULTS COULD BE FOUND W ITH THE ENGINE. ENGINE WAS THEN REPLACED TO FIX PROBLEM. AIRCRAFT HAS FLOWN SIX FLIGHTS SINCE THE ENGINE CHANGE WITHOU T FURTHER INCIDENT. OFF ENGINE WILL BE RUN IN THE TEST CELL FOR TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A1NM E3NE 1998061900819 19980619 00819 NM 1998 6 19 98UAL900241 1 19980605 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 155UA 20104 NA THREE EMERGENCY EXIT SIGNS ARE INOP AT DOOR 4 RIGHT. FOUND BAD BATTERY PACK. REPLACED BATTERY PACK. 2 L 7 4 4F 4 F A20WE E20EA 1998061900820 19980619 00820 NM 1998 6 19 98UAL900242 1 19980605 A 3397 WIRE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 155UA 20104 EMERGENCY EEL LIGHTS IN D-ZONE FROM SEATS 34 A, B, C TO 42 A, B, C ARE INOP. FOUND BROKEN WIRE. SPLICED IN NEW SECTION OF POWER CABLE. 2 L 7 4 4F 4 F A20WE E20EA 1998061900821 19980619 00821 NM 1998 6 19 98UAL900243 1 19980608 A 7711 D4244J CONNECTOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT ENGINE FAILED A UALA K NONE O OTHER CR CRUISE 1 WP 29 613UA 21874 709613 RIGHT ENGINE EPR AND STANDBY EPR INTERMITTENT, CAUSES AUTOTHROTTLES TO DISCONNECT. *S/D* REPLACED ENGINE (S/N 707520) TO FIX THE PROBLEM, DID NOT HELP. FURTHER TROUBLESHOOTING AFTER THE ENGINE CHANGE UNCOVERED A BAD CONTACT (PIN 11) IN C ONNECTOR D4244J ON THE UPPER SIDE OF THE ENGINE-PYLON INTERFACE. THE CONTACT WAS REPLACED AND THERE HAS BEEN NO REOCCUR ANCE OF THE PROBLEM SINCE THAT REPAIR WAS ACCOMPLISHED ON 11JUN98. 2 L 7 2 4F 4 F RT A1NM E3NE 1998061900822 19980619 00822 EU 1998 6 19 98UAL900245 1 19980608 A 2131 CONTROLLER AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 FAILED A UALA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 443UA 820 NR 2 PRESSURE CONTROLLER FAILED. NR 1 PRESSURE CONTROLLER DID NOT PICK-UP SYSTEM. RELIEF VALVES OPENED, DIVERTED. 2 L 7 2 4F 4 F RT A28NM E40NE 1998061900823 19980619 00823 1998 6 19 98UAL900246 4 19980609 A 2312 6221181003 TRANSCEIVER BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 1 VHF MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 985UA 21747 THE NUMBER ONE COMM WENT INOP AND WAS FOLLOWED BY AN ELECTRICAL TYPE SMELL. THE TEMPERATURE IN THE COCKPIT WAS VERY WAR M WHILE THE CABIN WAS VERY COLD. *S/D* REPLACED NUMBER 1 VHF TRANSCEIVER AND NUMBER 1 AUDIO CONTROL PANEL. ELECTRICAL SMELL WAS UNRELATED TO COMMUNICATION PROBLEM AND WAS CAUSED BY RUPTURED LT PACK ACM OUTLET DUCT. 2 L 7 2 4F 4 F A16WE E2EA 1998061900824 19980619 00824 NM 1998 6 19 98UAL900247 1 19980606 A 3260 65B43673 ANGLE BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE LT MLG BENT A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 151UA 23736 AFTER GEAR RETRACTION THE LEFT WING GEAR TILT LIGHTS CAME ON BOTH PRIMARY AND ALTERNATE. ALSO, THE GEAR LEVER LATCH SO LENOID WAS IN VIEW. THE CAPTAIN DECIDED TO DIVERT TO SFO FOR MAINTENANCE. FOUND LEFT WING GEAR TILT SENSOR MOUNTING BR ACKET BENT. REPLACED BRACKET AND SENSOR INSTALLATION ADJUSTED TO PROPER GAP. AIRCRAFT GEAR EXTENSION RETRACTION TEST A CCOMPLISHED. ALL CHECKED NORMAL. 2 L 7 4 4F 4 F RT A20WE E3NE 1998061900825 19980619 00825 NM 1998 6 19 98UAL900248 1 19980609 A 2497 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E/E COMPT BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 531UA 25042 RETURNED TO FIELD DUE TO PARTIAL ELECTICAL FAILURE. WIRE W2018-0003-06 WAS FOUND BROKEN AT L GENERATOR CIRCUIT BREAKER C901 PHASE C. LOSS OF PHASE C AT L GEN CB CAUSED PARTIAL ELECTRICAL FAILURE. THE WIRE TERMINAL HAD BROKEN DUE TO A ONE -TIME OVERSTRESS APPLICATION. THE WIRE TERMINAL WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998061900826 19980619 00826 EU 1998 6 19 98UAL900249 1 19980610 A 2130 PRESSURIZATION AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA B A EMER. DESCENT UNSCHED LANDING J G WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 WP 29 443UA 820 CABIN OVER-PRESSURE IN SYSTEM 1 THEN RAPID DECOMPRESSION AT FL310. OXYGEN MASKS DEPLOYED. DESCENDED TO 6,000 FEET. LA NDED SFO, AMBER ALERT. 2 L 7 2 4F 4 F RT A28NM E40NE 1998061900827 19980619 00827 NE 1998 6 19 98UAL900250 2 19980610 A 7200 ENGINE AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE NR 2 STALLED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 WP 29 806UA 788 NR 2 ENGINE STALL AT FL330, OVER TEMP LIGHT ILLUMINATED. ENGINE SHUTDOWN, DIVERTED TO SMF. OVERWEIGHT LANDING. 2 L 7 2 4F 4 F RT A28NM E40NE 1998061900828 19980619 00828 NM 1998 6 19 98UAL900251 1 19980610 A 2740 TRIM BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE HORIZ STAB FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 352UA 24320 CREW DIVERTED TO BNA DUE TO INOPERATIVE HORIZONTAL STABILIZER TRIM. 2 L 7 2 4F 4 F RT A16WE E2GL 1998061900829 19980619 00829 NM 1998 6 19 98UAL900253 1 19980610 A 3350 BULB BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7252U 21399 EEL LIGHT FOR LEFT WING EXTERIOR WALKWAY INOPERATIVE. REPLACED LAMPS. 2 L 7 3 4F 4 F A3WE E2EA 1998061900830 19980619 00830 NM 1998 6 19 98UAL900254 1 19980609 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7276U 21423 FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1998061900831 19980619 00831 WP 1998 6 19 ABXA9800520 1 19980612 A 2110 523294411014 CTC DUCT DOUG DOUG DC8 DC862 3021970 WP NR 2 LOOSE A ABXA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 805AX 45906 ON TAKEOFF AND CLIMBOUT, GEAR RETRACTION HAD RUMBLING FROM NOSE GEAR AREA. RECYCLED GEAR, NOISE STOPPED ON DOWN CYCLE B UT RETURNED ON THE RETRACTION. AIR TURNBACK TO MHR. FOUND LOOSE NR 2 CTC DUCT. ADJUSTED AND SECURED DUCT. NO OTHER D EFECTS NOTED. 2 L 7 4 4F 4A25 1998061900832 19980619 00832 WP 1998 6 19 MWEA98716 1 19980615 A 5320 99105014 WEB DOUG DC9 DC932 3022066 WP BS 237-275 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 CUSP WEBS BETWEEN STA 237 TO 275 ON RIGHT SIDE ARE CORRODED. INSTALLED FABRICATED CUSP WEBS L18R. 2 L 7 2 4F A6WE 1998061900833 19980619 00833 WP 1998 6 19 MWEA98717 1 19980615 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 275 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 215ME 47744 PREVIOUS REPAIR AT STA 275 LONG 18R DOES NOT CONFORM TO SRM REQUIREMENT. DOUBLER REPAIR INSTALLED. 2 L 7 2 4F A6WE 1998061900834 19980619 00834 WP 1998 6 19 MWEA98718 1 19980615 A 5311 9912453 FRAME DOUG DC9 DC932 3022066 WP BS 370 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE FRAME AT STATION 370 LONGERON 30 WAS FOUND CORRODED. FRAME WAS REPAIRED USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900835 19980619 00835 WP 1998 6 19 MWEA98719 1 19980615 A 5311 9912453 FRAME DOUG DC9 DC932 3022066 WP BS 427 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FRAME AT STATION 427 LONGERON 30 WAS FOUND CORRODED. REPAIRED FRAME USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900836 19980619 00836 WP 1998 6 19 MWEA98720 1 19980615 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 436-475 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 SKIN BULGED AND IRREGULAR FASTENERS INSTALLED AT STA 436 TO 475 BETWEEN LONGERON 18L AND 26L SKIN SPLICE. REPAIR WAS IN STALLED AND ATTACHING STRUCTURE WAS REPLACED. 2 L 7 2 4F A6WE 1998061900837 19980619 00837 WP 1998 6 19 MWEA98721 1 19980615 A 5311 5911448521 FRAME DOUG DC9 DC932 3022066 WP BS 503 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 215ME 47744 FUSELAGE FRAME AT STA 503 BETWEEN LONG 28R AND 28L HAS PREVIOUS REPAIR THAT DOES NOT MEET SRM REQUIREMENTS. INSTALLED P ROPER SPLICE REPAIR IAW SRM. 2 L 7 2 4F A6WE 1998061900838 19980619 00838 WP 1998 6 19 MWEA98722 1 19980615 A 5320 SILL DOUG DC9 DC932 3022066 WP CARGOWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE FORWARD CARGO DOOR SILL PAN AN SUPPORT STRUCTURE WAS FOUND CORRODED. REMOVED DAMAGED PARTS FABRICATED AND INSTALLED REPAIR SECTIONS USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900839 19980619 00839 WP 1998 6 19 MWEA98723 1 19980615 A 5320 PAN DOUG DC9 DC932 3022066 WP CARGOWAY DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE FORWARD CARGO DOOR HANDLE RECESS PAN WAS FOUND DAMAGED. REMOVED AND REPLACED PAN USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900840 19980619 00840 NM 1998 6 19 SCNA98060 1 19980609 A 3350 BATTERIES BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE AFT ENTRY OVERHEAD PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED A ND REPLACED THE BATTERIES AND THE LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998061900841 19980619 00841 NM 1998 6 19 SCNA98061 1 19980609 A 3350 BATTERIES BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE AFT ENTRY OVERHEAD PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED A ND REPLACED THE BATTERIES AND THE LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998061900842 19980619 00842 NM 1998 6 19 DHL9870601C 1 19980514 A 7110 COWLING BOEING 727 72722C 138400F NM NR 1 ENGINE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 1 ENG LOWER COWL HAS AN AREA OF CORROSION ON SKIN. CUT OUT DAMAGED SECTION, INSTALLED REPAIR PER SRM 54 -10-3 FILLER 29 X 4.5 DOUBLER, 18.5 X 18.5. CUT OUT DAMAGED AREA OF SKIN AT INBD SIDE PER SRM 54-10-3 FILLER 29 X 5, D OUBLER 18 X 19. N/R 6897. 2 L 7 3 4F A3WE 1998061900843 19980619 00843 NM 1998 6 19 DHL9870602C 1 19980514 A 7110 COWLING BOEING 727 72722C 138400F NM NR 1 ENGINE TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 1 ENGINE COWL SKIN TORN BETWEEN NR 2 AND NR 3 LATCH. REMOVED DAMAGED AREA, INSTALLED DOUBLER REPAIR PER RM 54-10-3 6 X 3. N/R 6871. 2 L 7 3 4F A3WE 1998061900844 19980619 00844 NM 1998 6 19 DHL9870603C 1 19980518 A 7110 COWLING BOEING 727 72722C 138400F NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 1 ENGINE FWD FIXED COWL AFT FRAME IS CRACKED AT LOWER END BY MOUNT BRACKET. INSTALLED ANGLE REPAIR PER S RM 51-40-3, 4.5 X 2. N/R 6939. 2 L 7 3 4F A3WE 1998061900845 19980619 00845 NM 1998 6 19 DHL9870604C 1 19980515 A 5720 ANGLE BOEING 727 72722C 138400F NM NR 1 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 1 FLAP TRACK OUTBD COVE PANEL SUPPORT ANGLE CRACKED. REMOVED DAMAGED SUPPORT, FABRICATED AND INSTALLED A NGLE PER SRM 51-30-2. N/R 1652. 2 L 7 3 4F A3WE 1998061900846 19980619 00846 NM 1998 6 19 DHL9870605C 1 19980517 A 5712 RIB BOEING 727 72722C 138400F NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, LEFT WING WS 686.5 RIB CRACK AT LOWER STR 9. STOP DRILLED CRACK, HFEC, INSTALLED DOUBLER REPAIR PER SRM 57 -10-5, 9 X 4. N/R 1669. 2 L 7 3 4F A3WE 1998061900847 19980619 00847 NM 1998 6 19 DHL9870606C 1 19980517 A 5713 STRINGER BOEING 727 72722C 138400F NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, CRACKED VENT STRINGER 13 AT WS 629 LEFT WING. CUT OUT DAMAGED SECTION PER S/B 57-A159, INSTALLED ATTACH ANG LE PER S/B 57-A159, 12 LONG. N/R 1671. 2 L 7 3 4F A3WE 1998061900848 19980619 00848 NM 1998 6 19 DHL9870607C 1 19980513 A 5720 STIFFENER BOEING 727 72722C 138400F NM WS 120 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RIGHT WING LEADING EDGE VERTICAL STIFFENER HAS A 2 INCH CRACK AT LOWER END AS VIEWED THROUGH ACCESS OPENING NR 6401 FRONT SPAR STA 120. STOP DRILL, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 7 X 1.25 X 1. N/R 2017. 2 L 7 3 4F A3WE 1998061900849 19980619 00849 NM 1998 6 19 DHL9870608C 1 19980513 A 2782 ANGLE BOEING 727 72722C 138400F NM NR 6 LE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RIGHT WING NR 6 KRUEGER FLAP ACTUATOR CHECK PREV REPAIR, AT INBD VERTICAL SUPPORT ANGLE AT LOWER FWD END. R EMOVED AND REPLACED SUPPORT ANGLE PER SRM 57-10-1, 8 X 4. N/R 2023. 2 L 7 3 4F A3WE 1998061900850 19980619 00850 NM 1998 6 19 DHL9870609C 1 19980515 A 5330 SKIN BOEING 727 72722C 138400F NM PAX DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, AFT ENTRY DOOR RIGHT NR 7 DOOR STOP FITTING CUTOUT IS CRACKED. ACCOMPLISHED NDT, STOP DRILLED, INSTALLED REPAIR PER S/B 53-055 22 X 8.5 AND 13 X 7. N/R 3609. 2 L 7 3 4F A3WE 1998061900851 19980619 00851 NM 1998 6 19 DHL9870610C 1 19980516 A 5330 STRAP BOEING 727 72722C 138400F NM BS 380 DISBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, SKIN BONDED TEAR STRAP AT STA 380 STR 3L TO 1 HAS DISBONDED. CUT OUT TEAR STRAP AT STA 380 BETWEEN STR 1L T O STR 4. CLEANED INNER FUS SKIN , NO CORROSION NOTED. INSTALLED NEW TEAR STRAP PER S/B 53-0082, 30 X 3. N/R 3627. 2 L 7 3 4F A3WE 1998061900852 19980619 00852 NM 1998 6 19 DHL9870611C 1 19980519 A 2730 65C337355 BOB WEIGHT BOEING 727 72722C 138400F NM LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, LT ELEVATOR BOB WEIGHTS CRACKED AND DETORATED ON TAB. REMOVED AND REPLACED WEIGHTS PER SRM 51-30-2. N/R 45 68. 2 L 7 3 4F A3WE 1998061900853 19980619 00853 NM 1998 6 19 DHL9870613C 1 19980514 A 5330 PLATE BOEING 727 72722C 138400F NM WS 350 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT WING I/B PANEL SUPPORT CORRUGATED PLATE HAS CRACK AND LOOSE FASTENERS BETWEEN LOWER WING SPAR AND LOWER W ING SKIN WS 350. REMOVED AND REPLACED SUPPORT PANEL PER SRM 51-10-1. N/R 2064. 2 L 7 3 4F A3WE 1998061900854 19980619 00854 NM 1998 6 19 DHL9870614C 1 19980514 A 5755 BRACKET BOEING 727 72722C 138400F NM NR 11 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT WING I/B SPOILER NR 11 HAS PANEL VERTICAL BRACKET CRACKED, ATTACHED TO SUPPORT ROD LOWER END. REMOVED AN D REPLACED BRACKET PER SRM 51-10-1. N/R 2087. 2 L 7 3 4F A3WE 1998061900855 19980619 00855 NM 1998 6 19 DHL9870615C 1 19980514 A 5730 6521658374 PLATE BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT WING BELOW NR 13 SPOILER REMOVED AND REPLACED CORRUGATE PLATE AT RT WING PER SRM 57-20-1. N/R 2090. 2 L 7 3 4F A3WE 1998061900856 19980619 00856 NM 1998 6 19 DHL9870616C 1 19980510 A 5712 RIB BOEING 727 72722C 138400F NM WS 546 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, CRACKED IN RIGHT WING RIB WS 546 AT LOWER STR 5. STOP DRILLED CRACK, HFEC, INSTALLED DOUBLER REPAIR PER S/B 57-0127 AND SRM 51-30-2, 3 X 5. N/R 2116. 2 L 7 3 4F A3WE 1998061900857 19980619 00857 NM 1998 6 19 DHL9870617C 1 19980519 A 5730 SKIN BOEING 727 72722C 138400F NM WS 70.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RIGHT WING UPPER SURFACE, HFEC REVEALED 3 CRACK INDICATIONS AT 3 FASTENER HOLES AT WING RIB UPPER CHORD AT 70.5 O/B HORIZ FLANGE. OVERSIZED HOLES, HFEC, INSTALLED PREV MOD PER S/B 57-0112. N/R 2130. 2 L 7 3 4F A3WE 1998061900858 19980619 00858 NM 1998 6 19 DHL9870618C 1 19980520 A 5712 RIB BOEING 727 72722C 138400F NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT WING RIB AT STA 629 CRACKED AT STR 14 LOWER. STOP DRILLED CRACK, ACCOMPLISHED HFEC, INSTALLED DOUBLER PE R SRM 51-30-2, 3 X 6'. N/R 2132. 2 L 7 3 4F A3WE 1998061900859 19980619 00859 NM 1998 6 19 DHL9870619C 1 19980514 A 5230 SKIN BOEING 727 72722C 138400F NM BAGGAGE DOOR DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, L/E OF AFT BAGGAGE BIN DOOR IS DENTED IN SEVERAL PLACES. REPLACED SKIN AT AFT CARGO DOOR PER SRM 52-30-02, 48 X 52.5. N/R 3549. 2 L 7 3 4F A3WE 1998061900860 19980619 00860 NM 1998 6 19 DHL9870620C 1 19980515 A 5330 SKIN BOEING 727 72722C 138400F NM PAX DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, AFT ENTRY DOOR LEFT NR 7 DOORS TOP FITTING CUTOUT IS CRACKED. HFEC OF STOP DRILL, INSTALLED REPAIR PER S/B 53-055 AND DRAWING 65C15764. REPAIRS 22 X 8.5' AND 13' X 7. N/R 3608. 2 L 7 3 4F A3WE 1998061900861 19980619 00861 NM 1998 6 19 DHL9870621C 1 19980515 A 5210 66138732 STOP BOEING 727 72722C 138400F NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RIGHT HAND AFT ENTRY DOOR STOP NR 7 IS CRACKED. REMOVED AND REPLACED STOP PER SRM 51-30-2. N/R 5802. 2 L 7 3 4F A3WE 1998061900862 19980619 00862 NM 1998 6 19 DHL9870622C 1 19980513 A 5330 SKIN BOEING 727 72722C 138400F NM BS 203 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, EXTERIOR FUSELAGE HAS SKIN CRACK AROUND FASTENER AT BS 203 WL 217 RIGHT SIDE. CUT OUT DAMAGED SECTION, HFEC , AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3. DOUBLER 1 X 1. N/R 3535. 2 L 7 3 4F A3WE 1998061900863 19980619 00863 NM 1998 6 19 DHL9870623C 1 19980513 A 5712 RIB BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RIGHT WING LEADING EDGE, INBD SIDE AND AFT OF NR 5 SLAT, PREV REPAIR TO UPPER SECTION OF L/E RIB, CRACKED IN TWO PLACES. REPLACED CRACKED ANGLE PER SRM 51-40-3, 18 X 1 X 1. N/R 2026. 2 L 7 3 4F A3WE 1998061900864 19980619 00864 NM 1998 6 19 DHL9870624C 1 19980513 A 5755 66147352 BRACKET BOEING 727 72722C 138400F NM NR 8 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT WING NR 8 SPOILER ACTUATOR LOWER LEFT SUPPORT ATTACHED TO LOWER PANEL HAS CRACK 2.5 WL 237. REMOVED AND REPLACED SUPPORT BRACKET PER SRM 51-30-2. N/R 2045. 2 L 7 3 4F A3WE 1998061900865 19980619 00865 NM 1998 6 19 DHL9870625C 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM WS 70.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, LT UPPER RIB AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD UPPER HOLE AND 3 CRACKS AT FWD LOWER HOLE. STO P DRILLED CRACKS, HFEC, INSTALLED REPAIR AT LEFT WING PER S/B 57-0112 O/B OF 70.5. INSTALLED REPAIR AT I/B OF LT WING C ENTER SECTION PER S/B 57-0112. N/R 1587. 2 L 7 3 4F A3WE 1998061900866 19980619 00866 NM 1998 6 19 DHL9870626C 1 19980514 A 5754 ANGLE BOEING 727 72722C 138400F NM NR 2 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, LEFT WING L/E, NR 2 SLAT OUTBD TRACK, INBD SUPPORT RIB AFT VERTICAL DOUBLER HAS A VERTICAL CRACK AT BOTTOM. REMOVED AND REPLACED ANGLE SUPPORT PER SRM 57-10-1, 16 LONG. N/R 1615. 2 L 7 3 4F A3WE 1998061900867 19980619 00867 NM 1998 6 19 DHL9870627C 1 19980515 A 5711 SPAR BOEING 727 72722C 138400F NM WS 115 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, LEFT WING FRONT SPAR WS 115 LOWER END OF VERTICAL ANGLE CRACKED. STOP DRILLED END OF CRACK, HFEC, FABRICATE D ANGLE REPAIR, 6 X 2 PER SRM 51-40-3. N/R 1648. 2 L 7 3 4F A3WE 1998061900868 19980619 00868 NM 1998 6 19 DHL9870628C 1 19980515 A 5754 RIB BOEING 727 72722C 138400F NM NR 4 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 4 SLAT INBD TRACK OUTBD RIB IS CRACKED PAST STOP DRILL. STOP DRILLED END OF CRACK, HFEC, FABRICATED RIB REPAIR PER SRM 57-50-3, 4 X 5. N/R 1667. 2 L 7 3 4F A3WE 1998061900869 19980619 00869 NM 1998 6 19 DHL9870629C 1 19980515 A 5754 RIB BOEING 727 72722C 138400F NM NR 1 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 1 SLAT INBD TRACK OUTBD RIB IS CRACKED AT FWD END. STOP DRILLED, HFEC, INSTALLED DOUBLER PER SRM 57-50-3 , 1 X 4. N/R 1668. 2 L 7 3 4F A3WE 1998061900870 19980619 00870 NM 1998 6 19 DHL9870630C 1 19980517 A 5713 STRINGER BOEING 727 72722C 138400F NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, VENT STR S-14 CRACK LEFT WING RIB STA 686.5 UPPER. TRIMMED OUT DAMAGED AREA, INSTALLED REPAIR OF VENT PER S RM 57-10-5, L-ANGLE 14. N/R 1670. 2 L 7 3 4F A3WE 1998061900871 19980619 00871 NM 1998 6 19 DHL9870631C 1 19980519 A 5755 CASTING BOEING 727 72722C 138400F NM NR 7 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 7 SPOILER CENTER HINGE CASTING CRACKED AT I/B LOWER END. REMOVED AND REPLACED CENTER CASTING PER 727 SRM 57-10-1. N/R 1698. 2 L 7 3 4F A3WE 1998061900872 19980619 00872 NM 1998 6 19 DHL9870632C 1 19980521 A 5320 FORGING BOEING 727 72722C 138400F NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, FUSE FORGING BS 950 LT SIDE HAS 1 INCH CRACK AT SECOND ROW TOP NR 1 FASTENER. INSTALLED S/B REPAIR PER S/B 53-0126 PART VI. N/R 1701. 2 L 7 3 4F A3WE 1998061900873 19980619 00873 NM 1998 6 19 DHL9870633C 1 19980513 A 5754 ANGLE BOEING 727 72722C 138400F NM NR 5 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, TR WING NR 5 KRUEGER FLAP ACTUATOR INBD VERTICAL SUPPORT ANGLE CRACKED IN RADIUS FWD UPPER END. REMOVED AN D REPLACED VERTICAL SUPPORT ANGLE, 7 X 5. N/R 2020. 2 L 7 3 4F A3WE 1998061900874 19980619 00874 NM 1998 6 19 DHL9870634C 1 19980513 A 5720 STIFFENER BOEING 727 72722C 138400F NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT WING LEADING EDGE FRONT SPAR OUTBD VERTICAL STIFFENER CRACKED AT LOWER END, NR 6 SLAT OUTBD. REPLACED VE RTICALS STIFFENER PER SRM 51-10-1. N/R 2065. 2 L 7 3 4F A3WE 1998061900875 19980619 00875 NM 1998 6 19 DHL9870635C 1 19980520 A 5710 CENTER SECTION BOEING 727 72722C 138400F NM WS 70.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT UPPER AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD LOWER HOLE. INSTALLED REPAIR AT RT WING LOWER I/B AND CENTER SECT PER S/B 57-0112. N/R 213. 2 L 7 3 4F A3WE 1998061900876 19980619 00876 NM 1998 6 19 DHL9870636C 1 19980522 A 5754 RIB BOEING 727 72722C 138400F NM NR 5 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, NR 5 SLAT I/B CLOSURE RIB IS CRACKED. REPLACED RIB PER SRM 51-30-2. N/R 2137. 2 L 7 3 4F A3WE 1998061900877 19980619 00877 NM 1998 6 19 DHL9870637C 1 19980514 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 480 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, FWD CARGO RT SEAT TRACK STR 27R HAS CORROSION AT TOP AND BOTTOM BS 480 TO 510. N/R 3550. 2 L 7 3 4F A3WE 1998061900878 19980619 00878 NM 1998 6 19 DHL9870638C 1 19980514 A 5230 SKIN BOEING 727 72722C 138400F NM CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, LOWER FWD CARGO DOOR EXT SKIN HAS BULGE AT LWR FWD AREA. CUT OUT DAMAGED AREA, HFEC, INSTALLED EXTERNAL DOU BLER PER SRM 52-00-3, 7 X 6. N/R 3558. 2 L 7 3 4F A3WE 1998061900879 19980619 00879 NM 1998 6 19 DHL9870639C 1 19980514 A 5230 ANGLE BOEING 727 72722C 138400F NM CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, LOWER FWD CARGO DOOR INTERIOR CRACK INTO RADIUS OF ANGLE SUPPORT, INSIDE AFT CTR SIDE. REMOVED AND REPLACE D ANGLE AT LEFT LOWER END PER SRM 52-30-1, 6 X 4. N/R 3562. 2 L 7 3 4F A3WE 1998061900880 19980619 00880 NM 1998 6 19 DHL9870640C 1 19980514 A 5330 SKIN BOEING 727 72722C 138400F NM PAX DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, FWD ENTRY DOOR CUTOUT EXTERIOR SKIN JUST ABOVE UPPER FWD CORNER OF CUTOUT. STOP DRILLED CRACK, INSTALLED EX TERNAL DOUBLER PER S/B 53-186 21 X 50. N/R 3565. 2 L 7 3 4F A3WE 1998061900881 19980619 00881 NM 1998 6 19 DHL9870641C 1 19980514 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 480-600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, CORROSION AT NUT PLATE ON OUTBD FLANGE OF SEAT TRACK LBL 46 BETWEEN BS 480 AND 600. REMOVED SEAT TRACK, REM OVED CORROSION FROM CABIN FLOOR, WITHIN LIMITS AND INSTALLED NEW TRACK PER SRM FROM BS 480 TO 550 PER SRM 53-10-5. N/R 3576. 2 L 7 3 4F A3WE 1998061900882 19980619 00882 NM 1998 6 19 DHL9870642C 1 19980514 A 5312 47485953 BULKHEAD FITTING BOEING 727 72722C 138400F NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, CORROSION ON FITTING LOCATED ON AFT SIDE OF BULKHEAD AND KEEL BEAM FWD END LBL 15, WL 166. REMOVED AND REPL ACED FITTING PER SRM 51-10-1. N/R 3580. 2 L 7 3 4F A3WE 1998061900883 19980619 00883 NM 1998 6 19 DHL9870643C 1 19980515 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, CORROSION ON DOOR SILL FITTING BOTTOM SURFACE OF TOP FLANGE AT BS 560 LBL 60. CUT OUT DAMAGED SECTION OF C ABIN FLOORBEAM UPPER CHORD STA 560 LBL 28, INSTALLED FLOORBEAM UPPER CHORD, REPAIR BETWEEN LBL 28 TO 62 PER SRM 53-10-8. N/R 3601. 2 L 7 3 4F A3WE 1998061900884 19980619 00884 NM 1998 6 19 DHL9870644C 1 19980514 A 5712 RIB BOEING 727 72722C 138400F NM WS 70.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT UPPER RIB AT 70.5 WING CENTER SECTION HAS 2 CRACKS AT FWD LOWER HOLE. STOP DRILLED, HFEC, AND PERFORMED M ODIFICATION PER S/B 57-0112. N/R 2073. 2 L 7 3 4F A3WE 1998061900885 19980619 00885 NM 1998 6 19 DHL9870645C 1 19980514 A 5320 FRAME BOEING 727 72722C 138400F NM CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, FWD CARGO DOOR FUS FRAME, FWD SIDE INNER SKIN HAS CRACK RUNNING FROM RIVET HOLE TO EDGE OF FRAME, JUST UNDE R SECOND STOP FITTING. REMOVED DOUBLER, HFEC, CUT OUT DAMAGED SECTION, HFEC CUT OUT AND INSTALLED DOUBLER REPAIR AND TR IPLER 22 X 8 PER AVIATAS ENGINEERING DRAWING 98PMSI211D-1. N/R 3548. 2 L 7 3 4F A3WE 1998061900886 19980619 00886 NM 1998 6 19 DHL9870646C 1 19980603 A 5347 SEAT TRACK BOEING 727 72722C 138400F NM BS 580 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, CABIN SEAT TRACK CRACKED AT STA 580 LBL 24. CUT OUT DAMAGED SECTION OF SEAT TRACK FROM BS 560 TO 620, INSTA LLED NEW SEAT TRACK 5' LONG PER SRM 53-10-5. N/R 5816. 2 L 7 3 4F A3WE 1998061900887 19980619 00887 NM 1998 6 19 DHL9870647C 1 19980515 A 5530 65174522 ANGLE BOEING 727 72722C 138400F NM VERT STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, VERT STAB RT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. REMOVED STRIP AND FOUND VERT ATTACH SUPPORT ANGLE CORRODED. INSTALLED NEW SUPPORT PER SRM 55-30-1. N/R 4545. 2 L 7 3 4F A3WE 1998061900888 19980619 00888 NM 1998 6 19 DHL9870648C 1 19980515 A 5530 65174523 ANGLE BOEING 727 72722C 138400F NM VERT STAB CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, VERTICAL STAB LT STAINLESS STEEL RUB STRIP FOR THE HORIZ STAB RUB BLOCK IS BULGED. VERTICAL SUPPORT ANGLE C ORRODED. INSTALLED NEW ANGLE PER SRM 55-30-1. N/R 4544. 2 L 7 3 4F A3WE 1998061900889 19980619 00889 NM 1998 6 19 DHL9870649C 1 19980515 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, CORROSION ON FLOORBEAM AFT UPPER FLANGE LOWER SURFACE AT BS 560 LBL 48. CUT OUT DAMAGED SECTION AT STA 560 FROM LBL 24 TO O/B END. INSTALLED FLOORBEAM UPPER CHORD PER SRM 53-10-8, 44 LONG, STRAP 3 X 24 SUPPORT ANGLE 2 X 1 X 24. N/R 3600. 2 L 7 3 4F A3WE 1998061900890 19980619 00890 NM 1998 6 19 DHL9870650C 1 19980519 A 2730 BOB WEIGHTS BOEING 727 72722C 138400F NM RT ELEV CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RT ELEV TAB BOB WEIGHTS CRACKS AND DETERIORATED. REMOVED AND REPLACED WEIGHTS PER SRM 51-10-1 AND 51-30-2. N/R 4569. 2 L 7 3 4F A3WE 1998061900891 19980619 00891 WP 1998 6 19 RRXA98233 1 19980611 A 3310 BALLAST DOUG DC8 DC871F 302199D WP RT COCKPIT FAILED A RRXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 15 8087U 45977 SMOKE FROM UNKNOWN ORIGIN ON FO SIDE COCKPIT. FOUND BALLAST OVERHEATED. DEFERRED THIS ITEM IAW EWA MEL 33-1 CAT 'C' DM I NR 806173 PLACARD INSTALLED. REMOVED AND REPLACED FLOURESCENT LIGHT BALLAST ASSY, LIGHTS OPS CK GOOD, THIS CLEARS DMI 806173 PLACARD REMOVED. 2 L 7 4 4F RT 4A25 1998061900892 19980619 00892 WP 1998 6 19 RRXA98234 1 19980613 A 5230 DOOR DOUG DC8 DC862 3021970 WP CARGO COMPT NOT LATCHED A RRXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 15 995CF 46024 CARGO DOOR OPENED IN FLIGHT. DOOR SECURED PER DER INSTRUCTIONS. ACFT FERRIED TO MACON FOR REPAIRS. 2 L 7 4 4F 4A25 1998061900893 19980619 00893 WP 1998 6 19 RRXA98235 1 19980614 A 3610 C264064 CLAMP DOUG DC8 DC871F 302199D WP NR 3 ENGINE FAILED A RRXA A UNSCHED LANDING G MULTIPLE FAILURE CR CRUISE 1 WP 15 801GP 46039 DURING CRUISE, RT MAN IND 22PSI WITH LT MAN TEMP NORM, NEXT NR 3 ENG EGT WENT OFF SCALE LOW, NEXT CAPTS STICK SHAKER WEN T OFF, NEXT RT MAN TEMP WENT OFF SCALE HIGH WITH NO OVHT LITES COMING ON. ISOLATED S/O BLEED VALVES TEMP BEGAN TO DROP. NEXT NR 4 ALT LOW LVL LITE ILLUM, NEXT NR 3 AND NR 4 ENG LOW PRESS AGENT LITES INBD AND OTBD CAME ON. NEXT FLAP SLOT CAME ON WITH NO MOVEMENT OF THE FLAPS. NEXT MAN-AIR OTEMP LITE CAME ON WITH NO AIR ON RT WING AND LT WING NORMAL. R/R' D NR 3 ENG PYLON AFT 'Y' MAN PNEU DUCT CLAMP, REPLACED BURNT WIRES FROM WING STA 63.750 - 347.50. REPLACED BOTH FIRE BO TTLES, REPLACED NR 3 ENG EGT HARNESS WIRE FROM WING TO FUSELAGE PRESS FEED THRU OUT TO NR 3 ENG AFT PYLON. R/R'D STALL 2 L 7 4 4F RT 4A25 1998061900894 19980619 00894 NE 1998 6 19 VNAA9806008 2 19980614 A 7200 GEARBOX DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 426JS 59334 3038 116125 HL182 WHEN CONDITION LEVERS WERE SELECTED TO HIGH, A LT PROPELLER LOW OIL PRESSURE CAS MESSAGE OCCURRED, DURING THE APPROACH. THE AIRCRAFT CONTINUED APPROACH TO PWM AND LANDED SAFELY. MAINTENANCE INSPECTED AND FOUND THE LEFT HAND PROPELLER CONT ROL UNIT DRIVE GEAR TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND TURBO MACHINE, IN ACCORDANCE WITH DOR NIER MAINTENANCE MANUAL 71-02-02. OPERATION AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998061900895 19980619 00895 WP 1998 6 19 CKSA98342 1 19980615 A 5230 SKIN LKHEED 1586301101 LKHEED 1011 1011385115 5265015 WP CARGO DOOR DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK A022 193N1193 C1A CARGO DOOR AFT LOWER CORNER IS DEFORMED/DAMAGED. DAMAGED AREA IS APPROX 7 IN LENGTH ALONG RIM OF DOOR SKIN. (REF: G AMCO NON-ROUTINE CARD NUMBER 4114). CUT AND TRIMMED DAMAGED AREA WITH MINIMUM RADIUS OF .025 DEGREE. FABRICATED AND IN STALLED REPAIR IAW GAMCO REPAIR SCHEME L52-30-07 REV 00. 8110-3 APPROVED DATED, JUNE 10, 1998. DOOR SKIN (2024T3). 2 L 7 3 4F A23WE 1998061900896 19980619 00896 WP 1998 6 19 CKSA98343 1 19980601 A 3350 86210066 BATTERY LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 EMERGENCY LIGHT OUT AT 1D. REMOVED AND REPLACED BATTERY AT 1D IAW L1011 MM CH 33, OPS CHECK NORMAL. NON-ROUTINE ITEM 1 . 2 L 7 3 4F A23WE 1998061900897 19980619 00897 WP 1998 6 19 CKSA98344 1 19980601 A 3350 86210066 BATTERY LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 EMERGENCY LIGHT OUT AT 20D. REMOVED AND REPLACED BATTERY AT 20D IAW MM CH 33, OPS CHECK NORMAL. NON-ROUTINE ITEM 2. 2 L 7 3 4F A23WE 1998061900898 19980619 00898 WP 1998 6 19 CKSA98345 1 19980601 A 3350 86210066 BATTERY LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 EMERGENCY LIGHTE OUT AT 25D. REMOVED AND REPLACED BATTERY AT 25D IAW MM CH 33, OPS CHECK NORMAL. NON-ROUTINE ITEM 3. 2 L 7 3 4F A23WE 1998061900899 19980619 00899 WP 1998 6 19 CKSA98346 1 19980601 A 3350 86210066 BATTERY LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 EMERGENCY LIGHT OUT AT 15G. REMOVED AND REPLACED BATTERY AT 15G IAW MM CH 33, OPS CHECK NORMAL. NON-ROUTINE ITEM 4. 2 L 7 3 4F A23WE 1998061900900 19980619 00900 WP 1998 6 19 CKSA98347 1 19980601 A 3350 86210066 BATTERY LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 EMERGENCY LIGHT OUT AT 34H. REMOVED AND REPLACED BATTERY AT 34H IAW MM CH 33, OPS CHECK NORMAL. NON-ROUTINE ITEM 5. 2 L 7 3 4F A23WE 1998061900901 19980619 00901 WP 1998 6 19 CKSA98348 1 19980601 A 3350 873100111 LIGHT LKHEED 1011 1011385115 5265015 WP CABIN INOPERATIVE A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 108CK 193N1204 EMERGENCY LIGHT OUT/INOP AT 14D. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IAW MM CH 33, OPS CHECK NORMAL ON GROUND TEST. NON-ROUTINE ITEM 6. 2 L 7 3 4F A23WE 1998061900912 19980619 00912 SO 1998 6 19 98ZZZX2185 2 19980524 A 8530 CYLINDER BEECH 58 58 1152740 CE CONT O550 IO550C SO CYLINDER HEAD CRACKED A P HRMA K NONE O OTHER IN INSP/MAINT 1 NE 01 5565D 880 TH1552 2719667R SEVENTY HOURS AGO, THIS ENGINE HAD TWO CRACKED CYLINDER HEADS. THE CRACKS WERE IN THE AREA BETWEEN THE TOP SPARK PLUG H OLE AND THE FUEL INJECTOR BOSS. THIS INSPECTION SHOWED ANOTHER CRACK. THE OPPOSITE ENGINE HAD FOUR CRACKED HEADS AT TH IS TIME AND ONE CRACKED HEAD PREVIOUSLY. ALL CRACKS WERE NEARLY IDENTICAL. TCM'S ANALYTICAL INSPECTION REVEALED THE CR ACK STARTED IN THE AREA BEHIND (AS YOU FACE THE CRANKSHAFT WITH THE CYLINDER INSTALLED) THE FUEL INJECTOR BOSS. ALL CRA CKED HEADS WERE DATE STAMPED 3-95 ON A ROCKER ARM SHAFT SUPPORT AND HAD 'REV K' CAST INTO THE HEAD. THE PREVIOUS ENGINE S ON THIS AIRCRAFT RAN TO 1,675 HOURS WITHOUT PROBLEMS. THE AFFECTED ENGINES WERE FACTORY REBUILT. 1 L 7 2 3O 3 O 3A16 E3SO 1998061900913 19980619 00913 SO 1998 6 19 98ZZZX2186 2 19980524 A 8530 CYLINDER BEECH 58 58 1152740 CE CONT O550 IO550C SO CYLINDER HEAD CRACKED A P A HRMA K NONE O OTHER IN INSP/MAINT 1 NE 01 5565D 880 TH1552 271968R SEVENTY HOURS AGO, THIS ENGINE HAD TWO CRACKED CYLINDER HEADS. THE CRACKS WERE IN THE AREA BETWEEN THE TOP SPARK PLUG H OLE AND THE FUEL INJECTOR BOSS. THIS INSPECTION SHOWED ANOTHER CRACK. THE OPPOSITE ENGINE HAD FOUR CRACKED HEADS AT TH IS TIME AND ONE CRACKED HEAD PREVIOUSLY. ALL CRACKS WERE NEARLY IDENTICAL. TCM'S ANALYTICAL INSPECTION REVEALED THE CR ACK STARTED IN THE AREA BEHIND (AS YOU FACE THE CRANKSHAFT WITH THE CYLINDER INSTALLED) THE FUEL INJECTOR BOSS. ALL CRA CKED HEADS WERE DATE STAMPED 3-95 ON A ROCKER ARM SHAFT SUPPORT AND HAD 'REV K' CAST INTO THE HEAD. THE PREVIOUS ENGINE S ON THIS AIRCRAFT RAN TO 1,675 HOURS WITHOUT PROBLEMS. THE AFFECTED ENGINES WERE FACTORY REBUILT. 1 L 7 2 3O 3 O 3A16 E3SO 1998061900919 19980619 00919 CE 1998 6 19 98ZZZX2192 1 19980512 A 2910 CM35740460B000S HOSE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE LT HYDRAULIC LEAKING A FRKA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 01 245CC 5500212 PILOT REPORTED HYDRAULIC LOW LEVEL LIGHT CAME ON IN-FLIGHT. AIRPLANE MADE LANDING AT NEAREST AIRPORT. LANDING GEAR EX TENSION WAS NORMAL, SPEED BRAKES AND THRUST REVERSERS DEPLOYED NORMALLY. UPON REMOVING COWLING, THE LEFT HYDRAULIC PRES SURE HOSE WAS FOUND LEAKING. THE HOSE WAS REPLACED, HYDRAULIC SYSTEM SERVICED AND AN OPERATIONAL CHECK OF ALL HYDRAULIC SYSTEMS ACCOMPLISHED. HOSE MFG DATE: 8/91. 1 L 7 2 4F 4 F A22CE E1NE 1998061900920 19980619 00920 EU 1998 6 19 98ZZZX2193 1 19980526 A 6120 89548119 PPC BAG JETSTM JETSTM3101 1500215 EU PROP PITCH MALFUNCTIONED A L S4WA K NONE O OTHER NR NOT REPORTED 1 WP 07 608JX 608 PILOT REPORTS EXCESSIVE YAW TO THE RIGHT. REMOVED AND REPLACED RT ENGINE PPC UNIT. PILOT REPORTS NO DEFECT NOTED. OPS CHECK GOOD. SEE ATTACHED QUALITY ASSURANCE FINDINGS REPORT FROM ALLIED SIGNAL DATED MAY 18, 1998. 2 L 7 2 4T RT A21EU 1998061900927 19980619 00927 1998 6 19 SADF9802 4 19980523 A 3442 MI585306401 R/T UNIT COLLINS BAC 146 AVRO146RJ100 1500096 EU RADAR FAILED A SADF O OTHER J WARNING INDICATION CL CLIMB 1 SO 23 507MM 2605 94040738 E3245 BOB/BOB - FLT 184 - WEATHER RADAR IS INOPERATIVE DURING INITIAL CLIMB. THE WEATHER RADAR RECEIVER TRANSMITTER WAS CHANG ED ACCORDING AMM 34-41-00. (X) 2 H 7 4 4F RT A49EU 1998061900929 19980619 00929 NM 1998 6 19 CALA9801081 1 19980616 A 3412 1477950101 TAT INDICATOR BOEING 737 7372C0 1384488 NM RT COCKPIT SHORTED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 14245 16254 20074 THE TAT CIRCUIT BREAKER POPPED FOLLOWED BY SMOKE IN THE COCKPIT AFTER TAKEOFF. THE SMOKE APPEARED TO COME FROM THE TAT GUAGE. THE AIRCRAFT WAS RETURNED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TAT INDICATOR AT FAULT . THE INDICATOR WAS REMOVED AND REPLACED. THE TAT CIRCUIT BREAKER WAS REPLACED AS A PRECAUTIONARY MEASURE. TAT INDICA TION TESTED NORMAL. ALL WIRING FOR TAT INDICATOR AND BREAKER WAS INSPECTED AND NO DEFECTS WERE FOUND. 2 L 7 2 4F A16WE 1998061900930 19980619 00930 WP 1998 6 19 CALA9801082 1 19980615 A 5523 HOUSING DOUG DC9 DC932 3022066 WP LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND THE LT ELEVATOR OUTBOARD TRIM TAB INBOARD TRIM ROD HOUSING SHIELD CRACKED AT THE INBOARD UPPER COUNTERS UNK HOLE. THE CRACK WAS STOP DRILLED IAW SRM 55-01, FIGURE 2. A PATCH DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 55- 01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900931 19980619 00931 WP 1998 6 19 CALA9801083 1 19980615 A 5414 SKIN DOUG DC9 DC932 3022066 WP NR 1 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND NR 1 ENGINE PYLON TRAILING EDGE CRACKED AND CHAFED. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 4. 2 L 7 2 4F A6WE 1998061900932 19980619 00932 WP 1998 6 19 CALA9801084 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD NR 70 CRACKED. A NEW FLOORBOARD WAS FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 122B. 2 L 7 2 4F A6WE 1998061900933 19980619 00933 WP 1998 6 19 CALA9801085 1 19980615 A 5754 RIB DOUG DC9 DC932 3022066 WP LT LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLAP RIB LEADING EDGE OF LT WING AT XRS 270 CRACKED AND CORRODED. THE FLAP RIB WAS REMOVED IAW SRM 51- 30-2. A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1998061900934 19980619 00934 WP 1998 6 19 CALA9801086 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND HAT SECTION OF 49 FLOORBOARD CRACKED AT BOTH ENDS. THE HAT SECTION WAS REMOVED AND A NEW SECTION WAS F ABRICATED AND INSTALLED IAW SRM 53-21-0 AND 51-70-2. 2 L 7 2 4F A6WE 1998061900935 19980619 00935 WP 1998 6 19 CALA9801087 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD PANEL NR 79 CRACKED AT THE RT FORWARD EDGE. THE CRACK WAS STOP DRILLED, A REPAIR DOUBLER WA S FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, 53-01 PAGE 12-18. 2 L 7 2 4F A6WE 1998061900936 19980619 00936 WP 1998 6 19 CALA9801088 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOORBOARD PANEL NR 86 GOUGED AND CORRODED. A PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-3, 53-0 5 PAGE 1, 51-20-0 AND 51-30-2. 2 L 7 2 4F A6WE 1998061900937 19980619 00937 WP 1998 6 19 CALA9801089 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 680-756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT FLOORBOARD PANEL BETWEEN STA 680 AND 756 CRACKED AT THE LT FORWARD NR 5 ATTACH HOLE. A NEW FLOOR PA NEL WAS FABRICATED. TWO HAT SECTIONS WERE REMOVED, CLEANED, AND REBONDED TO NEW FLOOR PANEL IAW SRM 53-05, PAGE 1. 2 L 7 2 4F A6WE 1998061900938 19980619 00938 WP 1998 6 19 CALA9801090 1 19980615 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 465-579 SPLITTING A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND NR 48 FLOORBOARD SKIN SPLITTING AT FS 465 TO 579. SKIN AND FOUR HAT SECTIONS WERE FABRICATED AND INSTA LLED IAW SRM 53-21-0 AND 51-70-2. 2 L 7 2 4F A6WE 1998061900939 19980619 00939 WP 1998 6 19 CALA9801091 1 19980615 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1074 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FRAME STA 1074 CRACKED AT FASTENERS AT LONGERON 3R, 4R, 5R, AND 4L. THE CRACKED SECTION OF FRAME WAS RE MOVED AND A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW SRM 53-03, FIGURE 30. 2 L 7 2 4F A6WE 1998061900940 19980619 00940 WP 1998 6 19 CALA9801092 1 19980528 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 658 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN VERTICAL ATTACH ANGLE AT FS 658, BL 45R. A REPAIR ANGLE WAS FABRICATED AND INSTALLE D IAW SRM 51-10-1, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1998061900941 19980619 00941 WP 1998 6 19 CALA9801093 1 19980530 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 955/945 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LONGERON 17R AT FS 955.091 AND FS 945. THE CRACKED SECTIONS OF LONGERON WERE REMOVED IAW SRM 51-30-2. NEW SECTIONS OF LONGERON WERE FABRICATED AND INSTALLED IAW SRM 53-02, FIGURE 18, 51-10-3, 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998061900942 19980619 00942 WP 1998 6 19 CALA9801094 1 19980602 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 610-620 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 610 TO 620. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED, A N EW SECTION OF TRACK, SPLICE AND PLATE WERE FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-1, AND 51-30-2. 2 L 7 2 4F A6WE 1998061900943 19980619 00943 WP 1998 6 19 CALA9801095 1 19980602 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 180 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 4.5 INCH CRACK IN FRAME AT STA 180, LONGERON 5L AND 6L. REPAIR PARTS WERE FABRICATED AND INSTALLED I AW SRM 53-03, FIGURE 36. 2 L 7 2 4F A6WE 1998061900944 19980619 00944 WP 1998 6 19 CALA9801096 1 19980604 A 5230 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND TWO CRACKS AT AFT END OF BEAM NR 4 OF AFT CARGO COMPARTMENT DOOR OUTER PAN. ONE CRACK WAS .3 LONG IN R ADIUS AND THE OTHER WAS .7 LONG AT FASTENER. BOTH CRACKS WERE STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW E CRA 5261-C-01000. 2 L 7 2 4F A6WE 1998061900945 19980619 00945 WP 1998 6 19 CALA9801097 1 19980607 A 5320 STRAP DOUG DC9 DC932 3022066 WP BS 945-996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND AFT CARGO PIT RT SIDEWALL PANEL STRAP CORRODED AT STA 945 TO 996. A REPAIR WAS FABRICATED AND INSTALLE D IAW SRM 51-10-3 AND 51-10-2. 2 L 7 2 4F A6WE 1998061900946 19980619 00946 NM 1998 6 19 UPS98426921 1 19980615 A 3350 BULB BOEING 747 747123 1384873 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 676UP 20101 INSPECTION TYPE-N/A, MAIN CARGO DECK EMERGENCY LIGHT INOP FWD OF CREW STAIRS. RELAMPED PER 747 MM, OPS CHECK GOOD. 2 L 7 4 4F A20WE 1998061900947 19980619 00947 WP 1998 6 19 UPS98826922 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 603.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XFS603.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900948 19980619 00948 WP 1998 6 19 UPS98826923 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 484.895 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E AT STA XS484.895, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900949 19980619 00949 WP 1998 6 19 UPS98826924 1 19980607 A 5320 37558411 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, FUSELAGE STA 1220, AT LONG 34R, THE BACK-UP FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTIN G IAW DWG 3755841 AND SRM 53-2-0 FIG 2G. 2 L 7 4 4F RT 4A25 1998061900950 19980619 00950 WP 1998 6 19 UPS98826925 1 19980607 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 737 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, LT WING TIP JUST AFT OF FWD NAV LIGHT HAS SKIN CORROSION BEYOND LIMITS. REPAIRED AREA IAW SRM 57-2-1 FIG 2M. 2 L 7 4 4F RT 4A25 1998061900951 19980619 00951 WP 1998 6 19 UPS98826926 1 19980611 A 5720 57698595 DOUBLER DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, LT WING INBD SLOT, OTBD CLOSE OUT RIB DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER P ER DWG 5769859 AND SRM 57-3-1 FIG 6. 2 L 7 4 4F RT 4A25 1998061900952 19980619 00952 WP 1998 6 19 UPS98826927 1 19980606 A 5320 3750330529 FITTING DOUG DC8 DC873F 302199F WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, FS 450 AT LONG 36 THE LONG SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900953 19980619 00953 WP 1998 6 19 UPS98826928 1 19980605 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, LT WING L/E RIB AT STA XFS 616.250 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900954 19980619 00954 WP 1998 6 19 UPS98826929 1 19980604 A 5712 2771189501 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, LT WING I/B SLOT O/B Z-ANGLE CLOSE OUT RIB IS CRACKED. REMOVED AND REPLACED Z-ANGLE PER DWG 5769859 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998061900955 19980619 00955 WP 1998 6 19 UPS98826930 1 19980604 A 5320 36471171 FITTING DOUG DC8 DC873F 302199F WP BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, FS 960 ABOVE LONG 24R THE FITTING IS CORRODED. REMOVED AND REPLACED FITTING PER DWG 3647117 AND SRM 51-1-20D, 51-1-3, 53-2-0 FIG 8. 2 L 7 4 4F RT 4A25 1998061900956 19980619 00956 WP 1998 6 19 UPS98826931 1 19980609 A 5347 3657503501 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, 2ND O/B FWD SEAT TRACK HAS CORROSION AROUND THE MOUNT FASTENERS. REMOVED AND REPLACED THE 2ND O/B FW D SEAT TRACK PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998061900957 19980619 00957 WP 1998 6 19 UPS98826932 1 19980606 A 5320 3750330519 FITTING DOUG DC8 DC873F 302199F WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, LONG SPLICE FITTING AT STA 450 AT LONG 32R IS CRACKED. REMOVED AND REPLACED THE LONG SPLICE FITTING PER SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900958 19980619 00958 WP 1998 6 19 UPS98826933 1 19980602 A 5320 4611067N FITTING DOUG DC8 DC871F 302199D WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 70 THE LONG 28L END FITTING IS CRACKED. REMOVED AND REPLACED THE END FITTING PER SRM 51-1-21, 51- 1-20D AND DWG 4611067. 2 L 7 4 4F RT 4A25 1998061900959 19980619 00959 WP 1998 6 19 UPS98826934 1 19980602 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 585 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 585.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PE R SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900960 19980619 00960 WP 1998 6 19 UPS98826935 1 19980602 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 653.75 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAI RED PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998061900961 19980619 00961 WP 1998 6 19 UPS98826936 1 19980603 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 329/335.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E UPPER SKIN AT STA XFS 329.0 AND 335.25 IS CRACKED IN TWO PLACES. REPAIRED PER SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998061900962 19980619 00962 WP 1998 6 19 UPS98826937 1 19980603 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 591.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E UPPER SKIN AT STA XFS 591.25 IS CRACKED. REPAIRED PER EO DC8-5720-7767. 2 L 7 4 4F RT 4A25 1998061900963 19980619 00963 WP 1998 6 19 UPS98826938 1 19980603 A 5320 3754473501B FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1260 TO 1280 LONG 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3754473 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900964 19980619 00964 WP 1998 6 19 UPS98826939 1 19980603 A 5320 37592221N FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1260 TO 1280 LONG 34L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3759222 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900965 19980619 00965 WP 1998 6 19 UPS98826940 1 19980603 A 5320 37592221N FITTING DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1260 TO 1280 LONG 34R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3759222 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900966 19980619 00966 WP 1998 6 19 UPS98826941 1 19980603 A 5311 97540552 FRAME DOUG DC8 DC871F 302199D WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1220 ABOVE LONG 35R TO 36 THE FRAME HAS A 5 INCH CRACK. REMOVED AND REPLACED THE FRAME CAP PER DW G 9754055 AND SRM 51-1-20D AND 51-1-22 FIG 47. 2 L 7 4 4F RT 4A25 1998061900967 19980619 00967 WP 1998 6 19 UPS98826942 1 19980603 A 5320 37585701N FITTING DOUG DC8 DC871F 302199D WP BS 1231 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1231 ABOVE LONG 35R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FRAME TIE FITTING PER DWG 3758570 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900968 19980619 00968 WP 1998 6 19 UPS98826943 1 19980603 A 5730 97532978 ANGLE DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT OTBD WING SLOT OTBD AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE PER DWG 9753297 AND SRM 51-1-2, 51-1-20D. 2 L 7 4 4F RT 4A25 1998061900969 19980619 00969 EU 1998 6 19 98FDEA00403 1 19980616 A 2424 764067 GCU AIRBUS 300 A300F4605R 3930327 EU NR 2 GENERATOR INOPERATIVE A FDEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 25 658FE 752 NR 2 GENERATOR INOPERATIVE AFTER ENGINE START, ONE RESET. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT. APU GENERA TOR REQUIRED FOR T/O. LOST APU GENERATOR AFTER TAKEOFF. DEFERRED APU GENERATOR PER MEL 24-8. 2 L 7 2 4F RT A35EU 1998061900970 19980619 00970 WP 1998 6 19 MWEA98724 1 19980616 A 5320 9912455501 DOUBLER DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 FORWARD CARGO DOOR LOWER CUTOUT DOUBLER AREA HAS CORROSION BLEND OUTS BEYOND LIMITS. INSTALLED INTERIOR TITANIUM DOUBLE R REPAIR IAW SRM. 2 L 7 2 4F A6WE 1998061900971 19980619 00971 WP 1998 6 19 MWEA98725 1 19980616 A 5330 5911418 SKIN DOUG DC9 DC932 3022066 WP BS 588-667 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE FUSELAGE SKIN FROM FUSELAGE STATION 588 TO STATION 667 WAS FOUND CORRODED. REMOVED AND REPLACED SKIN USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900972 19980619 00972 WP 1998 6 19 MWEA98726 1 19980616 A 5320 5912995 PAN DOUG DC9 DC932 3022066 WP EMER EXIT GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 THE RIGHT HAND AFT OVERWING EMERGENCY EXIT LOWER PAN WAS FOUND GOUGED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED R EPAIR ANGLE USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900973 19980619 00973 WP 1998 6 19 MWEA98727 1 19980616 A 5713 5911280 STRINGER DOUG DC9 DC932 3022066 WP WS 58.5 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 RIGHT WING STRINGER NUMBER 23 HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR STRAPS USING APPROVED D ATA FROM XCW 58.5 TO XRS 69. 2 L 7 2 4F A6WE 1998061900974 19980619 00974 WP 1998 6 19 MWEA98728 1 19980616 A 5713 5911279 STRINGER DOUG DC9 DC932 3022066 WP WS 58-69 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING STRINGER 19 WAS FOUND CORRODED ON UPPER FWD AND AFT LEGS FROM XCW 58 TO XRS 69 0. REMOVED CORROSION AND INSTA LLED REPAIRS USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900975 19980619 00975 WP 1998 6 19 MWEA98729 1 19980616 A 5713 5911280 STRINGER DOUG DC9 DC932 3022066 WP WS 58-5-69 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING STRINGER 22 WAS FOUND CORRODED ON UPPER FORWARD AND AFT LEGS FROM XCW 58 TO XRS 69. REMOVED CORROSION AND FAB RICATED AND INSTALLED REPAIR USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900976 19980619 00976 WP 1998 6 19 MWEA98730 1 19980616 A 5713 59112791 STRINGER DOUG DC9 DC932 3022066 WP WS 58.5-69 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING STRINGER 18 HAS NUMEROUS AREAS CORROSION BETWEEN STA XCW 58.5 TO 69 SOME BLEND OUTS BEYOND LIMITS. INSTALLED ANGLE REPAIR ON LOWER FLANGE OF STRINGER 18 REPAIR IS TEMPORARY FOR 1 GEAR PENDING BOEING DTA. 2 L 7 2 4F A6WE 1998061900977 19980619 00977 WP 1998 6 19 MWEA98731 1 19980616 A 5712 9919349 RIB DOUG DC9 DC932 3022066 WP WS 69 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING RIB AT STATION XRS 69 HAS CORROSION ON LOWER RIB CAP. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR USIN G APPROVED DATA. 2 L 7 2 4F A6WE 1998061900978 19980619 00978 WP 1998 6 19 MWEA98732 1 19980616 A 5713 5911280 STRINGER DOUG DC9 DC932 3022066 WP WS 73 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING STRINGER 22 HAS A BLEND OUT AT STATION XRS 73. FABRICATED AND INSTALLED REPAIR STRAP USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900979 19980619 00979 WP 1998 6 19 MWEA98733 1 19980616 A 5713 5919236 STRINGER DOUG DC9 DC932 3022066 WP WS 79 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING STRINGER 11 HAS A BLEND OUT AT STATION XRS 79. FABRICATED AND INSTALLED A REPAIR USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900980 19980619 00980 WP 1998 6 19 MWEA98734 1 19980616 A 5713 5919238 STRINGER DOUG DC9 DC932 3022066 WP WS 111-137 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING STRINGER NUMBER 14 HAS BEEN FOUND CORRODED FROM XRS 111 TO XRS 137. REMOVED CORROSION FABRICATED AND INSTALLE D REPAIR USING APPROVED USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900981 19980619 00981 WP 1998 6 19 MWEA98735 1 19980616 A 5712 9919353 RIB DOUG DC9 DC932 3022066 WP WS 164 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 CORROSION WAS FOUND ON LT WING INTERNAL RIB AT STATION XRS 164 ON THE LOWER HORIZONTAL FLANGES. REMOVED CORROSION AND I NSTALLED REPAIR STRAP USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900982 19980619 00982 WP 1998 6 19 MWEA98736 1 19980616 A 5730 5910465 SKIN DOUG DC9 DC932 3022066 WP WS 164 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 DURING MTC HOLES WHERE MISDRILLED ON THE RIGHT HAND WING LOWER SKIN AT STATION XRS 164 BY STRINGER 11R AND 12R. REMOVED DAMAGE AND FABRICATED AND INSTALLED REPAIR BUSHINGS USING APPROVED DATA. 2 L 7 2 4F A6WE 1998061900983 19980619 00983 WP 1998 6 19 MWEA98737 1 19980616 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 215ME 47744 LEFT WING LEADING EDGE HAS A PIECE OF SKIN BROKEN OUT BY NUMBER 3 SLAT TRACK CUTOUT. REMOVED DAMAGED AREA, FABRICATED A ND INSTALLED A REPAIR USING APPROVED DATA. 2 L 7 2 4F A6WE 1998062300001 19980623 00001 NM 1998 6 23 UPS98626840 1 19980605 A 2761 NAS161210 PACKING BOEING 767 76734AF 1385212 NM NR10 SPOILER ACT WORN A IPXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 313UP 27764 C HYD QTY DECREASED TO .22 QTY STABLE WITH SYSTEM PUMPS OFF. FOUND HYD LEAK FROM NR 10 FLT SPOILER ACTUATOR SERVO VALVE FILTER PLUG. REPLACED PACKING LEAK CHECK CARRIED OUT SATIS. C HYD SYSTEM SERVICED 7 GALLONS. 2 L 7 2 4F RT A1NM 1998062300002 19980623 00002 NM 1998 6 23 SWAA981040 1 19980601 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 1 LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED BC 1 CHECK, FOUND CRACKED NR 1 L/E SLAT LOWER SKIN AT INBOARD AUX TRACK. REPAIRED PER BOEING SRM AND T YPICAL REPAIR T1-A57-015. 2 L 7 2 4F RT A16WE 1998062300003 19980623 00003 NM 1998 6 23 SWAA981041 1 19980601 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 2 LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 349SW 24408 DURING SCHEDULED BC 1 CHECK, FOUND CRACKED NR 2 L/E SLAT LOWER SKIN AT INBOARD AUX TRACK. REPAIRED PER BOEING TYPICAL R EPAIR T1-A57-015 AND BOEING DRAWING 65C30133 SHEET 3. 2 L 7 2 4F RT A16WE 1998062300004 19980623 00004 NM 1998 6 23 UPS98626852 1 19980605 A 2612 FIRE LIGHT BOEING 767 76734AF 1385212 NM CF680 COCKPIT ILLUMINATED A IPXA K NONE N FALSE WARNING TO TAKEOFF 1 SO 01 317UP 27745 INSPECTION TYPE, FIRE LIGHT ON FORWARD PANEL ILLUMINATED FOR 10 SECONDS AFTER LIFT OFF ON A MAX POWER TAKEOFF. NO OTHER INDICATIONS OF A FIRE, SYSTEM TESTS OK. CAME BACK ON WHEN THRUST REDUCED FOR DESCENT AND APPROACH. PERFORMED SYSTEM O PS CHECK ON GROUND PER B767 FIM 2600, OPS CHECKED GOOD. 2 L 7 2 4F RT A1NM 1998062300005 19980623 00005 NM 1998 6 23 UPS98626853 1 19980605 A 2120 AIR DISTRIBUTION BOEING 767 76734AF 1385212 NM CABIN ODOR A IPXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 308UP 27761 INSPECTION TYPE, ORGANIC BURNING SMELL FROM LEFT PACK AFTER TAKEOFF. POSSIBLE ANIMAL INGESTION. INSPECTED LEFT ENGINE FOR INGESTION, NONE NOTED. RAN LT PACK SEVERAL MINUTES, NO SMELL NOTED. 2 L 7 2 4F RT A1NM 1998062300006 19980623 00006 NM 1998 6 23 VNAA9806003 1 19980601 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 433JS 57955 4590 3047 DURING THE ENGINE START UP, THE EMERGENCY FLOOR LIGHTS WERE NOTED TO BE INOPERATIVE. OUTSTATION MAINTENANCE INSPECTED T HE AIRCRAFT, AND APPROVED IT FOR A FERRY FLIGHT TO OUR CAK MAINTENANCE BASE. THE FERRY WAS CARRIED OUT WITHOUT ANY PROB LEMS. CAK MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY PACK , IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T RT A45NM 6 C P34NE 1998062300007 19980623 00007 WP 1998 6 23 ARWA980601 1 19980609 A 2781 CONNECTOR LKHEED 1011 10113851 WP NR 7 LE FLAP LOOSE A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK F N FLT CONT AFFECTED FALSE WARNING TO TAKEOFF 1 SO 19 307GB 193U1131 DURING TAKEOFF, THE TAKEOFF AURAL WARNING SOUNDED, AT THE SAME TIME L/E EXT LIGHT WAS FLICKERING. ALSO RT WING NR 7 SLA T MONITORING LIGHT FLICKERING. RETURNED TO BLOCKS. FOUND LOOSE CANNON PLUG IN RT NR 7 SLAT ASYMMETRY BRAKE COMPARTMENT . CLEANED AND SECURED CANNON PLUG AS PER MM 27-82-0, OPERATIONAL AND INDICATION CHECK OK. 2 L 7 3 4F RC A23WE 1998062300008 19980623 00008 SO 1998 6 23 C2XA98IA212 1 19980415 A 5320 12004149001 TEE EMB 120 EMB120ER 3260203 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16718 120136 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE T-PROFILE IAW WITH EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998062400001 19980624 00001 NE 1998 6 24 DL72S981236 2 19980610 A 7311 FUEL OIL COOLER 749965 BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 538DA DL628 22076 695224 PRECAUTIONARY NR 3 ENG SHUTDOWN AT TOP OF CLIMB. NR 3 OIL TEMPSETTLED IN YELLOW BAND, ALL OTHER ENG IND NORM, 60 DEG HO TTER THAN 1 AND 2 ENG. COULD NOT GET TEMP OUT OF YELLOW AFTER 15 MINS. REPLACED FUEL/OIL COOLER. IN FLIGHT SHUT DOWN. 2 L 7 3 4F 4 F A3WE E2EA 1998062400002 19980624 00002 NM 1998 6 24 DLM88981242 1 19980610 A 4990 OIL SYST DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE APU LEAKING A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 945DL 49818 P80398 AT CRUISE, CABIN AND COCKPIT NOTED SMOKE. DIVERTED CHA. FOUND APU LEAKING OIL CONTAMINATING PACKS. REPLACED APU. 2 L 7 2 4F 4 F RT A6WE E9NE 1998062400003 19980624 00003 NM 1998 6 24 DHL9870612C 1 19980513 A 5754 SKIN BOEING 727 72722C 138400F NM NR 6 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 AT C-CHECK, RIGHT WING LEADING EDGE NR 6 SLAT INBD TRACK CUTOUT HAS 1 INCH CRACK AT TOP END. STOP DRILLED, HFEC OF STOP DRILL, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 3 X 3. N/R 2042. 2 L 7 3 4F A3WE 1998062600001 19980626 00001 NM 1998 6 26 MZZA98157 1 19980430 A 5753 SKIN BOEING 727 727264 138408M NM RT TE FOREFLAP GOUGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION, ON AIRCRAFT AT AIR ASIA, GOUGE WAS FOUND ON RT WING T/E INBOARD FOREFLAP UPPER SKIN EXI STING REPAIR DOUBLER AT WBL 88. THE DAMAGED EXITING REPAIR DOUBLER WAS REMOVED AND REPAIRED PER B727 SRM 51-40-6. (X) 2 L 7 3 4F A3WE 1998062600002 19980626 00002 NM 1998 6 26 MZZA98155 1 19980430 A 5753 SKIN BOEING 727 727264 138408M NM RT TE FOREFLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RT WING INBOARD T/E FOREFLAP T/E LOW ER SKIN AT WBL 88. THE DAMAGED SKIN 4 INCHES BY 5 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X ) 2 L 7 3 4F A3WE 1998062600003 19980626 00003 NM 1998 6 26 MZZA98154 1 19980430 A 5753 SKIN BOEING 727 727264 138408M NM RT TE FOREFLAP GOUGED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, GOUGE WAS FOUND ON RT WING T/E INBOARD FOREFLAP NOSE SKIN AT WB L 240. THE GOUGED SKIN WAS STOP DRILLED AND REPAIRED PER B727 SRM 57-50-4 FIGURE 1. (X) 2 L 7 3 4F A3WE 1998062600004 19980626 00004 NM 1998 6 26 MZZA98153 1 19980428 A 5320 WEB BOEING 727 727264 138408M NM BS 1233/1253 CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING FOUND ON AFT AIRSTAIR RT TORQUE BOX INBOARD WEB. R T SIDE BETWEEN BS 1233 AND BS 1253. RT SIDE BETWEEN BS 1282 AND BS 1313. THE AFT AIRSTAIR RT TORQUE BOX INBOARD WEB OI L CANNING AREAS AND REINFORCEMENT STIFFENER ANGLES WERE INSTALLED PER B727 SRM 51-40-2. REF: OPERATOR CONTROL NR 98ZZZ X____. (X) 2 L 7 3 4F A3WE 1998062600005 19980626 00005 NM 1998 6 26 98ZZZX2200 1 19980428 A 5320 WEB BOEING 727 727264 138408M NM BS 1283/1313 CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING FOUND ON AFT AIRSTAIR RT TORQUE BOX INBOARD WEB. R T SIDE BETWEEN BS 1233 AND BS 1253. RT SIDE BETWEEN BS 1282 AND BS 1313. THE AFT AIRSTAIR RT TORQUE BOX INBOARD WEB OI L CANNING AREAS AND REINFORCEMENT STIFFENER ANGLES WERE INSTALLED PER B727 SRM 51-40-2. REF: OPERATOR CONTROL NR MZZA9 8153. 2 L 7 3 4F A3WE 1998062600006 19980626 00006 NM 1998 6 26 MZZA98152 1 19980428 A 5320 WEB BOEING 727 727264 138408M NM BS 1293/1323 CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIS, OIL CANNING WAS FOUND ON AFT AIRSTAIR LT TORQUE BOX INBOARD WEB . LT SIDE BETWEEN BS 1293 AND BS 1323. LT SIDE BETWEEN BS 1243 AND BS 1283. REF: OPERATOR CONTROL NR 98ZZZX____. (X ) 2 L 7 3 4F A3WE 1998062600007 19980626 00007 NM 1998 6 26 98ZZZX2201 1 19980428 A 5320 WEB BOEING 727 727264 138408M NM BS 1243/1283 CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 625DH 20780 TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIS, OIL CANNING WAS FOUND ON AFT AIRSTAIR LT TORQUE BOX INBOARD WEB . LT SIDE BETWEEN BS 1293 AND BS 1323. LT SIDE BETWEEN BS 1243 AND BS 1283. REF: OPERATOR CONTROL MZZA98152. 2 L 7 3 4F A3WE 1998062600008 19980626 00008 NM 1998 6 26 HNAA9890804 1 19980116 A 3350 82410162007 CONTROL BOX DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 908HA 32933 015 PHL/PHF - FLT 3175 - DURING PRE-FLIGHT CHECKS, THE CABIN EMERGENCY LIGHTS CYCLE ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL BOX. (X) 2 H 7 2 4T RT A13NM 1998062600009 19980626 00009 NM 1998 6 26 HNAA9893803 1 19980114 A 3350 6038443 POWER SUPPLY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 938HA 24109 2199 152 PHF/PIT - FLT 3163 - DURING PRE-FLIGHT CHECKS, FOUND THE FIRST TWO RED ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REP LACED POWER SUPPLY 3352-PS2. (X) 2 H 7 2 4T RT A13NM 1998062600010 19980626 00010 NM 1998 6 26 HNAA9893701 1 19980104 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 937HA 9706 SBY30 148 PHL/DCA - FLT 3095 - DURING PRE-FLIGHT WALK-AROUNDS, FOUND TWO RED AND ONE WHITE EMERGENCY FLOOR LIGHTS INOPERABLE. REM OVED AND REPLACED EMERGENCY BATTERY 3352-PS2. (X) 2 H 7 2 4T RT A13NM 1998062600016 19980626 00016 NM 1998 6 26 HNAA9894110 1 19980220 A 3350 6104791X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISHCARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 941HA 21683 SBY32 161 SBY/PHL - FLT 3184 - NR 1 AND NR 2 RED FLOOR ESCAPE PATH LIGHTS INOPERABLE. REMOVED AND REPLACED BATTERY AND BASE ASSEM BLIES. (X) 2 H 7 2 4T RT A13NM 1998062600017 19980626 00017 NM 1998 6 26 HNAA9892805 1 19980123 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 928HA 9740 SBY30 120 ORF/PHF - FLT 3121 - ROW 8 OVERHEAD AISLE EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BATTERY 3351-PS3. (X) 2 H 7 2 4T RT A13NM 1998062600018 19980626 00018 NM 1998 6 26 HNAA9897507 1 19980118 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 975HA 25268 116 176 PIT/LYH - FLT 3403 - EMERGENCY EXIT LIGHT OVERHEAD CABIN AT ROW 4, OVERHEAD MIDDLE, AND EXTERIOR RIGHT SIDE LIGHTS INOPE RABLE. REMOVED AND REPLACED BATTERY 3351-PS4. (X) 2 H 7 2 4T RT A13NM 1998062600019 19980626 00019 NM 1998 6 26 HNAA9893808 1 19980119 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 938HA 13876 JAX034 152 ROA/DCA - FLT 3199 - FIRST TWO EMERGENCY PATH LIGHTS INOPERATIVE. FIRST FOUR WHITE EMERGENCY LIGHTS INOPERATIVE. REMOV ED AND REPLACED BATTERY PS4. (X) 2 H 7 2 4T RT A13NM 1998062600020 19980626 00020 WP 1998 6 26 HALA9800130 1 19980521 A 3246 RIM DOUG DC9 DC951 3022051 WP NR 4 MLG BROKEN A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 679HA 47662 HNL - FLT 517 - (LOG PAGE A140487). NR 4 MAIN TIRE RIM BROKEN, NO PRESSURE LOSS. REPLACED NR 4 TIRE AND BEARING ASSY. BRAKE CHECK GOOD, SPIN CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1998062600021 19980626 00021 WP 1998 6 26 HALA9800129 1 19980521 A 3260 SENSOR TARGET DOUG DC9 DC951 3022051 WP RT MLG DOOR WORN A HALA K NONE N FALSE WARNING TO TAKEOFF 1 WP 13 661HA 47796 HNL - FLT 61 - (LOG PAGE A140341). ON CLIMB-OUT WITH HYDRAULIC PUMP ON HIGH, RT GEAR UNSAFE LIGHT AND GEAR DOOR OPEN LI GHT CAME ON. IT STAYED ON APPROXIMATELY 30 SECONDS THEN WENT OUT. BEFORE ACTION COULD BE TAKEN, GEAR-UP LATCH CHECKED GOOD AFTER LIGHT WENT OUT. HYDRAULIC PUMP LOW-NORMAL FLIGHT. REPLACED WORN RT HAND LANDING GEAR DOOR POSITION SENSOR T ARGET. GROUND CHECK OK OF DOOR WARNING SYSTEM. (X) 2 L 7 2 4F RT A6WE 1998062600022 19980626 00022 WP 1998 6 26 HALA9800128 1 19980517 A 3260 CONDUIT DOUG DC9 DC951 3022051 WP NLG LOCK BROKEN A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 660HA 48122 HNL - FLT 204 - (LOG PAGE A140278). AFTER GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT REMAINED ON IN CRUISE. FOUND NOSE GE AR LOCK SENSOR CONDUIT BROKEN. REPLACED NOSE GEAR LOCK SENSOR CONDUIT, OK FOR SERVICE. (X) 2 L 7 2 4F RT A6WE 1998062600023 19980626 00023 WP 1998 6 26 HALA9800118 1 19980504 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A HALA K NONE L NO TEST CR CRUISE 1 WP 13 672MC 47661 SBA - TEST FLIGHT - EMERGENCY LIGHTS ABOVE JUMP SEAT ARE INOPERATIVE. RE-LAMPED AND OPS CHECK OK IAW MM 33-50-00. (X) 2 L 7 2 4F RT A6WE 1998062600024 19980626 00024 WP 1998 6 26 HALA9800117 1 19980504 A 3260 BRACKET DOUG DC9 DC951 3022051 WP NLG OUT OF ADJUST A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 672MC 47661 SBA - TEST FLIGHT - (LOG PAGE 18N00688). NLG UNSAFE LIGHT STAYS ON WITH GEAR RETRACTED. ADJUSTED NOSE LANDING GEAR POS ITION INDICATION BRACKETS AND TESTED GOOD IAW MM 32-60-0, PAGE 201 TO PAGE 203. (X) 2 L 7 2 4F RT A6WE 1998062600025 19980626 00025 WP 1998 6 26 HALA9800119 1 19980506 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 674MC 47735 HNL - FLT 113 - (LOG PAGE A138813). OVERHEAD MID-CABIN EMERGENCY LIGHTS INOPERATIVE AFT CABIN FLOOR LIGHTS EMERGENCY IN OPERATIVE. REPLACED BATTERY AND CLEANED CONNECTOR ON FLOOR LIGHTS, OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1998062600026 19980626 00026 WP 1998 6 26 HALA9800126 1 19980520 A 7603 THROTTLE DOUG DC10 DC1010 3022110 WP NR 3 ENGINE OUT OF ADJUST A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 171AA 46906 SFO - FLT 12 - NR 3 THROTTLE STIFF WHEN RETARDED. RE-TORQUED CLUTCH SHAFT RETAINING NUT AND ADJUSTED NR 3 THROTTLE CLUT CH TENSION PUSH/PULL FORCE CHECKS OK AT 4 POUNDS. THROTTLE FORCE WITHIN LIMITS PER MM 76-11-00. (X) 2 L 7 3 4F A22WE 1998062600027 19980626 00027 WP 1998 6 26 HALA9800123 1 19980422 A 7603 CONTROL CABLE DOUG DC9 DC951 3022051 WP LT ENGINE BINDING A HALA O OTHER O OTHER TX TAXI/GRND HDL 1 WP 13 661HA 47796 ITO - FLT 122 - (LOG PAGE A140193). LEFT ENGINE STUCK IN IDLE. NO RESPONSE FROM THROTTLES. FOUND POWER CABLE ON QUADR ANT, ENGINE SIDE BINDING. RE-SECURED POWER CABLE, OPS CHECK OK. RUN-UP CHECK OK. SECURITY CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998062600028 19980626 00028 WP 1998 6 26 HALA9800125 1 19980515 A 2430 RCCB DOUG DC10 DC1010 3022110 WP CB PANEL FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 148AA 46703 HNL - FLT 465 - (LOG PAGE NR 4205729). MULTIPLE INDICATIONS OF POSSIBLE RCCB FAILURE. MANIFOLD FAIL LIGHTS 1 AND 2 DO N OT TEST. CABIN STANDBY PRESSURE DOES NOT TEST. NO AMPERAGE DRAWN ON AUXILIARY PITOT HEAT. NO PRESSURE INDICATION ON N R 2 PNEN DUCT PRESSURE GAUGE. (X) 2 L 7 3 4F A22WE 1998062600029 19980626 00029 NM 1998 6 26 98ZZZX2203 1 19980325 A 2731 TRIM DORNER DO32 DO328100 2996000 NM ELEVATOR MALFUNCTIONED A EQGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 19 335LS 3035 DFW/DRT - FLT 365 - AFTER TAKEOFF, CAS MESSAGE 'ELEVATOR DISC LOAD HI' APPEARED AND NOSE DOWN ELEVATOR TRIM FAILED. CRE W SELECTED STANDBY ELEV TRIM AND CONTINUED TO CLIMB AWAY FROM DFW (TRAFFIC AREA). AT SAFE ALTITUDE, CREW CONTACTED FLIG HT CONTROL. MAINT WAS CONSULTED AND DECISION MADE TO RETURN DFW. CREW INFORMED ATC SITUATION WAS NOT AN EMERGENCY. DU RING RETURN, CREW RECEIVED CAS MESSAGE 'ELEV TRIM FAIL'. MESSAGE DISAPPEARED AFTER A FEW MINUTES. AIRCRAFT LANDED WITH OUT INCIDENT. MAINT INSPECTED ACFT AND PERFORMED NUMEROUS OPER CHECKS. NO DEFECTS NOTED. TEST FLIGHT SATISFACTORY. S UBMITTER SUSPECTS HIGH WINDS CAUSED ELEVATOR TRIM PROBLEMS. WINDS WERE 29-32 KNOTS AT THE TIME OF THE INCIDENT. 2 H 7 2 4T RT A45NM 1998062600030 19980626 00030 NE 1998 6 26 EISA98105 2 19980513 A 7260 FITTING BOSS BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 1 ENG GEARBOX STRIPPED A EISA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 6826 19704 IN-FLIGHT, NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED, NR 1 OIL PRESSURE GAUGE READ JUST ABOVE LOWER RED RADIAL. OIL QUANT ITY READ ZERO. PRECAUTIONARY SHUT DOWN OF NR 1 ENGINE. RETURNED TO BRUSSELS (BRU). GENERATED FROM PILOT REPORT. FOUN D LEAKING FITTING AT GEARBOX, STRIPPED BOSS AT FITTING ON OIL PSI SWITCH LINE. HELICOIL INSTALLED BY SABENA. ENGINE RU N AND LEAK CHECK PERFORMED. HELICOIL INSTALLED PER CHAPTER 20-00. (X) 2 L 7 3 4F 4 F A3WE E2EA 1998062600031 19980626 00031 NM 1998 6 26 EISA98108 1 19980516 A 2611 SMOKE DETECTOR BOEING 727 72731 1384010 NM CARGO BAY INOPERATIVE A EISA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 240NE 18906 ON PREFLIGHT, FOUND NR 1 SMOKE DETECTOR IN MAIN CARGO COMPARTMENT INOPERATIVE. GENERATED FROM PILOT REPORT. FOUND CONN ECTOR WITH CONDENSATION. CLEANED CONNECTOR GROUND. CHECK GOOD MM 26-00. (M) 2 L 7 3 4F A3WE 1998062600032 19980626 00032 NM 1998 6 26 EISA98104 1 19980502 A 2611 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 FROM TAMPERE (TMP) TO BRUSSELS (BRU) - CARGO SMOKE LIGHT ILLUMINATED IN NORMAL FLIGHT CONDITIONS IN CARGO HOLD. UNEVENT FUL LANDING. GENERATED FROM PILOT REPORT. PURGED SMOKE DETECTOR OF MOISTURE, ALL SMOKE DETECTORS CHECKED GOOD PER AERO NAUTICAL MANUAL. (X) 2 L 7 3 4F A3WE 1998062600033 19980626 00033 WP 1998 6 26 TWAA9807501 1 19980511 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9401W 53137 STL - DURING MAINTENANCE GROUND CHECK, FOUND AFT MOST EGRESS LIGHT SECTION INOP. REPLACED POWER SUPPLY BATTERIES. (M) 2 L 7 2 4F RT A6WE 1998062600034 19980626 00034 NM 1998 6 26 USAABB98050 1 19980513 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 LAX - FOUND EMERGENCY FLOOR LEVEL LIGHTING INOPERATIVE AT ROW 18. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F RT A2NM 1998062600035 19980626 00035 NM 1998 6 26 USAABB98048 1 19980509 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM R1 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 LAX - R1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (X) 2 L 7 2 4F RT A2NM 1998062600036 19980626 00036 NM 1998 6 26 USAASB98117 1 19980519 A 3350 S106 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 257AU 22799 CLE - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN ABOVE THE AFT RIGHT SERVICE DOOR INOPERABLE. MAINTENANCE REMOVED AND RE PLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998062600037 19980626 00037 NM 1998 6 26 USAASB98112 1 19980509 A 2612 6676 FIRE DETECTOR BOEING 737 7374B7 1384702 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 782AU 25021 SJU - FLT 2134 - AIRCRAFT DEPARTED FOR PHL WITH THE NR 2 ENGINE B-FIRE LOOP ON MEL FOR NOT TESTING. SHORTLY AFTER TAKEO FF, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED PROCEDURES, BUT THE LIGHT WOULD NOT EXTINGUISH. CAPT AIN ELECTED TO DIVERT TO SJU. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMO VED AND REPLACED NR 2 ENGINE FAN COWL LOWER LOOP FIRE/OVERHEAT DETECTOR AND CANNON PLUG D3094. RAN ENGINE AT VARIOUS PO WER SETTINGS. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. FIRE/OVERHEAT DETECTOR - P/N 6676. CANNON PLUG - P/N FRF6E14 S5SX08. REF: OPER CONTROL NR 98ZZZX____. (X) 2 L 7 2 4F RT A16WE 1998062600038 19980626 00038 NM 1998 6 26 98ZZZX2204 1 19980509 A 2612 FRF6E14S5SX08 CONNECTOR BOEING 737 7374B7 1384702 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 782AU 25021 SJU - FLT 2134 - AIRCRAFT DEPARTED FOR PHL WITH THE NR 2 ENGINE B-FIRE LOOP ON MEL FOR NOT TESTING. SHORTLY AFTER TAKEO FF, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED PROCEDURES, BUT THE LIGHT WOULD NOT EXTINGUISH. CAPT AIN ELECTED TO DIVERT TO SJU. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMO VED AND REPLACED NR 2 ENGINE FAN COWL LOWER LOOP FIRE/OVERHEAT DETECTOR AND CANNON PLUG D3094. RAN ENGINE AT VARIOUS PO WER SETTINGS. OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. FIRE/OVERHEAT DETECTOR - P/N 6676. CANNON PLUG - P/N FRF6E14 S5SX08. REF: OPER CONTROL NR USAASB98112. 2 L 7 2 4F RT A16WE 1998062600039 19980626 00039 NM 1998 6 26 USAASB98110 1 19980510 A 2424 948F4581 GCU BOEING 737 737301 1384611 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 335US 26064 2176 23232 ORF - FLT 326 - EN ROUTE TO PHL, THE NR 1 ENGINE GENERATOR CONTROL UNIT OVERHEATED, BUT FAILED TO TRIP CIRCUIT BREAKER. CREW PULLED CIRCUIT BREAKER, HOWEVER, SMOKE HAD ACCUMULATED IN COCKPIT AND DECISION WAS MADE TO DIVERT TO ORF. EMERGEN CY WAS DECLARED AND EQUIPMENT WAS CALLED OUT. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER . MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE GENERATOR CONTROL UNIT. RAN ENGINE AND ELECTRICAL SYSTEMS. OPERATI ONAL CHECK NORMAL. (X) 2 L 7 2 4F RT A16WE 1998062600040 19980626 00040 WP 1998 6 26 VJ9800194 1 19980616 A 3350 610304 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 914VV 47486 AFT OVERWING EMERGENCY LIGHTS INOP. REPLACED AFT OVERWING EMERGENCY LIGHT BATTERY PACK IAW MM 33-50. 2 L 7 2 4F A6WE 1998062600041 19980626 00041 WP 1998 6 26 VJ9800195 1 19980617 A 2560 702957A SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 916VV 47445 GALLEY DOOR SLIDE NEEDS REINSTALLING. RESECURED SLIDE IAW MM, PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998062600042 19980626 00042 WP 1998 6 26 CALA9801098 1 19980608 A 5320 STIFFENER DOUG DC9 DC932 3022066 WP BS 313 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CABIN FLOORBOARD STIFFENER CRACKED AND BENT AT FLOOR SUPPORT BS 313, RT CENTER OF CEILING. A NEW STIFF ENER WAS FABRICATED AND INSTALLED IAW SRM 53-05 AND NEW SKIN WAS INSTALLED IAW SRM 53-05, 51-30-2, AND 51-70-2. 2 L 7 2 4F A6WE 1998062600043 19980626 00043 WP 1998 6 26 CALA9801099 1 19980612 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 218-284 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CORROSION ON NR 1 FLOORBOARD IN FORWARD PIT WITH DELAMINATION ON EDGES AT STA 218 TO 284. TWO HAT SECT IONS AND SIX NUT PLATE STRIPS WERE REMOVED. A FLOORBOARD WAS FABRICATED. THE FLOORBOARD, HAT SECTION, AND NUT PLATE ST RIPS WERE INSTALLED IAW ECRA 2551-01010, SRM 51-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998062600044 19980626 00044 WP 1998 6 26 CALA9801100 1 19980612 A 5321 FLOORPANEL DOUG DC9 DC932 3022066 WP BS 365-430 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOOR PANEL AT BS 365 TO 430 IN FORWARD PIT DELAMINATED. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLE D IAW SRM 51-10-2 AND ECRA 2551-01010. 2 L 7 2 4F A6WE 1998062600045 19980626 00045 WP 1998 6 26 CALA9801101 1 19980612 A 5321 FLOORPANEL DOUG DC9 DC932 3022066 WP BS 579-680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND NR 42 LT CENTER FLOOR PANEL IN FORWARD PIT CRACKED AT FS 579 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, 53-05, PAGE 1, AND 51-70-1. 2 L 7 2 4F A6WE 1998062600046 19980626 00046 WP 1998 6 26 CALA9801102 1 19980613 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 389-465 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND NR 40 FLOORBOARD DELAMINATED AT CENTER AISLE STA 389 TO 465. A NEW FLOORBOARD WAS FABRICATED AND INSTA LLED IAW SRM 53-05, PAGE 122B. 2 L 7 2 4F A6WE 1998062600047 19980626 00047 WP 1998 6 26 CALA9801103 1 19980608 A 5321 FLOORPANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND COCKPIT FLOORBOARD PANEL NR 12 CORRODED. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21- 0 AND 53-05, PAGE 1. 2 L 7 2 4F A6WE 1998062600048 19980626 00048 WP 1998 6 26 CALA9801104 1 19980609 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 465-579 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CRACKS AT SCREW HOLES OF FLOORBOARD NR 51, STA 465 TO 579 AND FLOORBOARD NR 40, STA 578 WITH SCREWS PUL LING THROUGH. NEW FLOORBOARDS WERE FABRICATED AND INSTALLED IAW SRM 53-05, PAGE 1, 51-20-0, 51-30-2, 51-10-2, 51-10-3, AND 51-70-2. 2 L 7 2 4F A6WE 1998062600049 19980626 00049 WP 1998 6 26 CALA9801105 1 19980609 A 5712 RIB DOUG DC9 DC932 3022066 WP WS 280 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1.5 INCH CRACK WITH CORROSION ON LT WING STA XRS 280 FLAP RIB ON LEADING EDGE PANEL FLANGE. THE RIB WAS REMOVED FROM SUPPORT CAP, A NEW RIB WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1998062600050 19980626 00050 WP 1998 6 26 CALA9801106 1 19980609 A 5753 BRACKET DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A CRACK WITH CORROSION IN LT WING FLAP XRS 270 LEADING EDGE SUPPORT BRACKET CAP. THE SUPPORT BRACKET C AP WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1998062600051 19980626 00051 WP 1998 6 26 CALA9801107 1 19980602 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BAGGAGE COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35832 49492 INSPECTION FOUND AFT BAGGAGE BIN Z-ANGLE REPAIR DOUBLER CORRODED. THE Z-ANGLE DOUBLER WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998062600052 19980626 00052 WP 1998 6 26 CALA9801108 1 19980615 A 5320 STRAP DOUG DC9 DC932 3022066 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT AFT CEILING PANEL ATTACHING STRAPS CORRODED. NEW STRAPS WERE FABRICATED AND INSTALLED IAW SRM 51-10 -2 AND 51-10-3. 2 L 7 2 4F A6WE 1998062600053 19980626 00053 WP 1998 6 26 CALA9801109 1 19980615 A 5530 PANEL DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND VERTICAL STABILIZER PHENOLIC PANEL CRACKED AT STA 96. THE PANEL WAS REMOVED IAW SRM 51-30-2, A NEW PAN EL WAS FABRICATED AND INSTALLED IAW SRM 55-01, PAGE 1 AND 51-30-2. 2 L 7 2 4F A6WE 1998062600054 19980626 00054 WP 1998 6 26 CALA9801110 1 19980616 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 980-996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CUSP CORRODED AT LT SIDE OF STA 980 TO 996. THE CORRODED SECTION OF CUSP WAS REMOVED AND A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE25. 2 L 7 2 4F A6WE 1998062600055 19980626 00055 WP 1998 6 26 CALA9801111 1 19980616 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND L-ANGLE ON BULKHEAD FRAME CORRODED AT STA 996, STRINGER 19L. THE ANGLE WAS REMOVED IAW SRM 51-30-02, A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-02, 51-10-4, 51-10-3 AND 51-30-02. 2 L 7 2 4F A6WE 1998062600056 19980626 00056 WP 1998 6 26 CALA9801112 1 19980616 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 937 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND SKIN CORRODED AT STA 937, LONGERON 20L. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5330-02673. 2 L 7 2 4F A6WE 1998062600057 19980626 00057 WP 1998 6 26 CALA9801113 1 19980616 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP CABIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CORROSION AROUND SCREW HOLES OF CABIN FLOORBOARD PANEL NR 44. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-21-0, AND 51-70-2. 2 L 7 2 4F A6WE 1998062600058 19980626 00058 WP 1998 6 26 CALA9801114 1 19980616 A 5350 FAIRING DOUG DC9 DC932 3022066 WP LT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND AFT INBOARD SIDE OF LT WHEEL WELL FORWARD FAIRING CRACKED. THE CRACK WAS STOP DRILLED, REPAIR ANGLES W ERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1998062600059 19980626 00059 WP 1998 6 26 CALA9801115 1 19980616 A 5230 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .25 INCH CRACK AT FORWARD END OF THE BEAM NR 3 DOOR STOP CUTOUT OF AFT CARGO COMPARTMENT DOOR OUTER P AN. THE CRACK WAS STOP DRILLED, A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 3. 2 L 7 2 4F A6WE 1998062600060 19980626 00060 SO 1998 6 26 COMA9810137 1 19980617 A 3350 LIGHT EMB 120 EMB120RT SO CABIN LOOSE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 257CA 120248 FORWARD EMERGENCY EXIT FLOOR LIGHT IS LOOSE. SECURED LIGHT ASSY TO FLOOR. 2 L 7 2 4T RT A31SO 1998062600061 19980626 00061 SO 1998 6 26 COMA9810138 1 19980617 A 3350 1317 LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 120233 FORWARD EMERGENCY LIGHT WILL NOT ILLUMINATE. REPLACED LAMP. 2 L 7 2 4T RT A31SO 1998062600062 19980626 00062 SO 1998 6 26 COMA9810139 1 19980616 A 2750 MECHANISM EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 196CA 120196 FLAP ASYMMETRY, INBOARD FLAPS WOULD NOT DEPLOY. COULD NOT DUPLICATE DISCREPANCY, SYSTEM OPERATIONAL CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 1998062600063 19980626 00063 EA 1998 6 26 COMA9860148 1 19980615 A 2910 AE2460010HD264 LINE CNDAIR CL600 CL6002B19 EA NR 1 HYD SYST LEAKING A COMA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 987CA 7199 NR 1 HYDRAULIC SYSTEM FAILED DURING FLIGHT. REPLACED LEAKING HYDRAULIC PRESSURE LINE IN ENGINE PYLON. 2 L 7 2 4F RT A21EA 1998062600064 19980626 00064 EA 1998 6 26 COMA9860149 1 19980616 A 2611 473052 DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 931CA 10432 7037 CARGO SMOKE MESSAGE ON EICAS. REPLACED CARGO SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 1998062600065 19980626 00065 EU 1998 6 26 QXEA9800788 1 19980616 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 BOTH FORWARD EXIT SIGNS HAVE LIGHTS OUT. MAINTENANCE RELAMPED BOTH FORWARD OVERHEAD 28V EXIT SIGNS. BOTH OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998062600066 19980626 00066 EU 1998 6 26 QXEA9800792 1 19980615 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 FORWARD FACING EXIT SIGN IN CABIN HAS MOST OF THE BULBS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED CIRCUIT BOAR D, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998062600067 19980626 00067 NM 1998 6 26 QXEA9800801 1 19980616 A 3350 10126271 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 827PH 275 EXIT LIGHT AT MAIN CABIN DOOR ENTRANCE IS INOP. REPLACED EXIT LIGHT ASSEMBLY, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998062600068 19980626 00068 WP 1998 6 26 ABXA9800536 1 19980614 A 7932 INDICATION DOUG DC8 DC863 302198A WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE MALFUNCTION A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 817AX 45928 670961 NR 1 ENGINE WAS SHUTDOWN DURING FLIGHT DUE TO DECREASING OIL QUANTITY. INSPECTED OIL QUANTITY INDICATION WIRING, DRAINE D AND REFILLED OIL TANK WITH KNOWN QUANTITY OF OIL, BAGGED ENGINE DRAIN LINES AND RAN ENGINE AT 75 PERCENT FOR 5 MINUTES . NO LEAKS OR DEFECTS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1998062600069 19980626 00069 WP 1998 6 26 MWEA98738 1 19980615 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 401ME 47133 THE GALLEY DOOR EMERGENCY SLIDE FELL OFF. MTC RESECURED GALLEY EMERGENCY SLIDE. 2 L 7 2 4F A6WE 1998062600070 19980626 00070 WP 1998 6 26 MWEA98739 1 19980615 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 401ME 47133 THE GALLEY DOOR EMERGENCY SLIDE FELL OFF MOUNTING BRACKETS. MTC RESECURED GALLEY ESCAPE SLIDE. 2 L 7 2 4F A6WE 1998062600071 19980626 00071 WP 1998 6 26 MWEA98740 1 19980615 A 2560 591769037 SLIDE DOUG DC9 DC914 3022034 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 800ME 45842 THE PASSENGER ENTRANCE ESCAPE SLIDE FELL OFF. MTC REINSTALLED COVER. 2 L 7 2 4F A6WE 1998062600072 19980626 00072 WP 1998 6 26 MWEA98741 1 19980616 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE GALLEY SERVICE DOOR SLIDE FELL OUT OF DOOR. MTC REINSTALLED SLIDE. 2 L 7 2 4F A6WE 1998062600073 19980626 00073 WP 1998 6 26 MWEA98742 1 19980617 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP DOOR GALLEY FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 502ME 48132 THE EMERGENCY GALLEY SLIDE FELL OFF. MTC REPAIRED LOOSE RIVET AND REATTACHED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998062600074 19980626 00074 NM 1998 6 26 MWEA98743 1 19980617 A 3350 60030431 BATTERY PACK DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 601ME 49762 FOUND AFT CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. MTC FOUND A LOSE TERMINAL END ON BATTERY PACK IN AFT OVERHEAD BIN TI GHTENED TERMINAL SCREW. 2 L 7 2 4F RT A6WE 1998062600075 19980626 00075 WP 1998 6 26 MWEA98744 1 19980618 A 5260 991199215 TORQUE TUBE DOUG DC9 DC981 3022081 WP VERTICAL STAIR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CRACK ON VERTICAL STAIR TORQUE TUBE BEAM IN RADIUS AT CABIN ARM ATTACHMENT LEFT SIDE. MTC REPAIRED WITH DOUBLER. 2 L 7 2 4F A6WE 1998062600076 19980626 00076 WP 1998 6 26 MWEA98745 1 19980618 A 5330 591022819 SKIN DOUG DC9 DC981 3022081 WP BS 1468 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CORROSION ON AFT ACCESSORY COMPARTMENT FUSELAGE SKIN AFT FS 1463 CANTED FRAME. MTC REPAIRED DOUBLER. 2 L 7 2 4F A6WE 1998062600077 19980626 00077 WP 1998 6 26 MWEA98746 1 19980618 A 5311 491224672 FRAME DOUG DC9 DC981 3022081 WP BS 1380 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND GOUGE ON FWD FACE OF WEB ON FUSELAGE FRAME FS 1380 AT LONGERON 6L. MTC BLENDED OUT DAMAGE AND INSTALLED DOUBLER R EPAIR. 2 L 7 2 4F A6WE 1998062600078 19980626 00078 WP 1998 6 26 MWEA98747 1 19980618 A 5280 HINGE DOUG DC9 DC932 3022066 WP RT MLG DOOR WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FOUND CONSIDERABLE FWD AND AFT PLAY ON RIGHT HAND FLYING DOOR. MTC REPLACED WORN HINGE BUSHING ON BOTH HINGE HALVES. 2 L 7 2 4F A6WE 1998062600079 19980626 00079 WP 1998 6 26 MWEA98748 1 19980618 A 5320 DOUBLERS DOUG DC9 DC932 3022066 WP FUSELAGE MISMANUFACTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 501ME 47132 FOUND FWD AND AFT ADF LOOP ANTENNA DOUBLER NOT TO CURRENT SRM STANDARDS. MTC FABRICATED AND INSTALLED NEW DOUBLERS. 2 L 7 2 4F A6WE 1998062600080 19980626 00080 NM 1998 6 26 SCNA98062 1 19980614 A 3350 1000677 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE AFT ENTRY OVERHEAD PORTABLE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED A ND REPLACED THE LIGHT ASSEMBLY, OPERATIONALLY CHECKS GOOD IN ACCORDANCE WITH MAINTENANCE MANUAL 3350101. 2 L 7 3 4F RT A3WE 1998062600081 19980626 00081 NM 1998 6 26 SCNA98063 1 19980607 A 2133 39608831 CONTROL VALVE BOEING 727 7272J4 1384006 NM RIGHT INOPERATIVE A A SCNA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 15 288SC 2542 20765 ON CLIMBOUT THROUGH APPROXIMATELY 25,000 FEET, THE AIRCRAFT CABIN STARTED AN UNCONTROLLABLE CLIMB. INITIATED COM PROCED URES AND CABIN REACHED APPROXIMATELY 12,000 FEET AND HELD. DESCENDED TO 10,000 FEET AND RETURNED TO SAT. DUMPED 6000 P OUNDS OF FUEL BEFORE LANDING. REMOVED AND REPLACED RIGHT FLOW CONTROL VALVE IN ACCORDANCE WITH MAINTENANCE MANUAL 36120 . OPERATIONAL AND LEAK CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998062600082 19980626 00082 NM 1998 6 26 VNAA9806009 1 19980614 A 5310 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AIRFRAME LIGHTNING STRIKE A VNAA K NONE O OTHER CR CRUISE 1 GL 07 422JS 3018 WHILE EN ROUTE, THE CREW SUSPECTED THAT THE AIRCRAFT WAS STRUCK BY LIGHTNING. THEY DID NOT RECEIVE ANY ABNORMAL INDICAT IONS, AND CONTINUED THE FLIGHT INTO PIT. THE AIRCRAFT LANDED NORMALLY IN PIT. MAINTENANCE INSPECTED AND PERFORMED OPER ATION CHECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-51-02. NO DEFECTS WERE NOTED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998062600083 19980626 00083 NM 1998 6 26 VNAA9806010 1 19980615 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 442JS 40509 572 3060 DURING THE PREFLIGHT INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS SEVEN THROUGH NINE, FAILED TO OPERATE WHEN SELECTED. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT TO ACCOMPLISH REPAIR. THE FERRY FLIGHT WAS CARRIED OUT WITHOUT ANY PROBLEMS. MAINTENANCE IN PIT INSPECTED AND REPLACED THE 6LK EMERGENCY BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998062600124 19980626 00124 WP 1998 6 26 VJ9800196 1 19980619 A 3350 41B004AD073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 930VV 47723 OVERHEAD EMERGENCY LIGHTS INOP IN AFT CABIN. REPLACED BATTERIES IN POWER SUPPLY; OPS CHECKED GOOD IAW MM 33-42. 2 L 7 2 4F A6WE 1998062600125 19980626 00125 EU 1998 6 26 JBXA980041 1 19980618 A 2612 FIRE DETECTOR FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU APU MALFUNCTIONED A JBXA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SO 05 107ML 5293 11450 ON FINAL APPROACH TO RDU, STARTED APU AND WHILE IN START CYCLE APU FIRE WARNING CAME ON. DISCHARGED FIRE BOTTLE. INSPE CTION OF APU ENCLOSURE AND APU AREA REVEALING NO EVIDENCE OF FIRE. ASSIGNED DMI NR 05336 PER MEL 49-00-1 APU INOP. NO OPERATION ALLOWED. 2 L 7 2 4F 4 F RT 1998062600126 19980626 00126 SO 1998 6 26 RAAA98E8019 1 19980617 A 3350 1000553 EMERGENCY LIGHT LKHEED 188 188C 5262604 SO PAX CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT LT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT ASSY DUE FAILED. 2 L 7 4 4T 4A22 1998062600127 19980626 00127 NM 1998 6 26 CALA9801116 1 19980618 A 3260 LIGHT BOEING 737 737222 1384473 NM LT MLG LOOSE A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 12235 19758 WHEN GEAR WAS EXTENDED ON APPROACH TO EWR, NEITHER A RED OR GREEN INDICATION WAS RECEIVED FOR RT MLG. THE APPROACH WAS ABORTED, AND WHEN GEAR WAS CYCLED, THE GREEN DOWN AND LOCKED LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. M AINTENANCE FOUND THE RT MLG GREEN LIGHT ASSEMBLY LOOSE IN SOCKET. THE LIGHT AND SOCKET ASSEMBLY WAS REMOVED AND REPLACED . THE RIGHT MAIN GEAR TESTED GOOD IAW MM 32-61-21, PAGE 404, PARAGRAPH 6B AND MM 32-61-31, PAGE 404, PARAGRAPH K. 2 L 7 2 4F A16WE 1998062600128 19980626 00128 WP 1998 6 26 CALA9801117 1 19980617 A 5210 ANGLE DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND THREE CRACKED ANGLES ON RT SIDE OF AFT ENTRY DOOR. THE DOOR SKIN AND ANGLES WERE REMOVED. NEW ANGLES WERE AND DOOR SKIN WERE INSTALLED IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1998062600129 19980626 00129 WP 1998 6 26 CALA9801118 1 19980617 A 5321 FLOORBOARD DOUG DC9 DC932 3022066 WP BS 389-465 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND CABIN FLOORBOARD NR 41 DELAMINATED AT LT SIDE FS 389-465. A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-05, 53-21-0, 51-30-2, 51-10-3, 51-70-2, AND 51-20-0. 2 L 7 2 4F A6WE 1998062600130 19980626 00130 WP 1998 6 26 CALA9801119 1 19980617 A 5230 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 0.7 CRACK AT FORWARD END OF BEAM NR 2 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-03, FIGURE 8. 2 L 7 2 4F A6WE 1998062600131 19980626 00131 WP 1998 6 26 CALA9801120 1 19980617 A 5230 WEB DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FORWARD CARGO DOOR INNER WEB CORRODED. THE CORROSION WAS REMOVED AND REPAIR DOUBLERS WERE FABRICATED A ND INSTALLED IAW SRM 52-01, 51-10-3, AND 52-30-0. 2 L 7 2 4F A6WE 1998062600132 19980626 00132 WP 1998 6 26 CALA9801121 1 19980617 A 5230 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1/2 CRACK AT AFT END OF BEAM NR 3 FASTENER LOCATION OF AFT CARGO COMPARTMENT DOOR OUTER PAN. A REPAI R DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5261C-01000. 2 L 7 2 4F A6WE 1998062600133 19980626 00133 WP 1998 6 26 CALA9801122 1 19980617 A 5753 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT TRAILING EDGE INBOARD FLAP INTERIOR CORRODED AND FINGER DOUBLERS SEPARATED. THE T/E FLAP SKIN WAS R EMOVED. NEW SKIN AND BONDED DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 57-50-9, FIGURE 6, 51-70-2, AND 51-30-2. 2 L 7 2 4F A6WE 1998062600134 19980626 00134 WP 1998 6 26 CALA9801123 1 19980617 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND A 1/2 CRACK AT BOTH ENDS OF MAIN CABIN DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND A NEW BEAM WAS INSTALL ED IAW SRM 51-30, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1998062600135 19980626 00135 WP 1998 6 26 CALA9801124 1 19980616 A 5210 ANGLE DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1.25 CRACK IN L-ANGLE FOR AFT ENTRY DOOR. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A REPAIR PART WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-2A. 2 L 7 2 4F A6WE 1998062600136 19980626 00136 WP 1998 6 26 CALA9801125 1 19980618 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1/2 CRACK AT FASTENER HOLE OF FUSELAGE SKIN AT AFT CABIN LT SIDE STA 980 ABOVE LONGERON 15L. THE CRA CKED AREA OF SKIN WAS CUT OUT. A FINGER DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 32 AND 51-10-38. 2 L 7 2 4F A6WE 1998062600137 19980626 00137 WP 1998 6 26 CALA9801126 1 19980617 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND A 1.5 CRACK IN FORWARD END OF FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-1 , 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998062600138 19980626 00138 WP 1998 6 26 CALA9801127 1 19980618 A 5210 INTERCOSTAL DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND THE MAIN CABIN DOOR INTERCOSTAL JUST AFT OF LOCK MECHANISM HAD A 1/2 CRACK AT EXTERNAL HANDLE RECESS. T HE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F A6WE 1998062600139 19980626 00139 WP 1998 6 26 CALA9801128 1 19980619 A 5320 JAMB DOUG DC9 DC982 3022082 WP BS 1155-1211 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND AFT CARGO COMPARTMENT DOOR JAMB Z-ANGLE BEAM CORRODED AT STA 1155-1211, LONGERON 26R. REPAIR PARTS WER E FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998062600140 19980626 00140 WP 1998 6 26 CALA9801129 1 19980618 A 3350 RPS1B BATTERY CHARGER RADIANT DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59083 47926 INSPECTION FOUND THE EMERGENCY AISLE LIGHTING INOPERATIVE AT ROWS 9 AND 10 (LEFT AND RIGHT). THE BATTERY CHARGER AT DOO R 2R AND 2L GALLEY OVERHEAD PANEL WAS REPLACED AND THE EMERGENCY LIGHT BATTERY PACK WAS CHARGED. OPERATIONAL CHECKS WER E GOOD IAW MM 33-50-00. 2 L 7 3 4F A22WE 1998062600141 19980626 00141 WP 1998 6 26 CALA9801130 1 19980618 A 3350 EMSE299 BATTERY PACK ENGMAGNETICS DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND EMERGENCY LIGHTS IN LEFT AFT ZONE INOPERATIVE. THE BATTERY AND BATTERY CHARGER WERE REMOVED AND REPLAC ED. 2 L 7 3 4F A22WE 1998062600142 19980626 00142 NE 1998 6 26 9809551153 2 19980612 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 2 FAILED A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 153US 46762 686136 DURING CLIMB-OUT, THE NR 2 ENGINE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED AND THE INDICATED OIL TEMPERATURE WAS INCRE ASING. THE ENGINE WAS SHUT DOWN. 50,000 LBS OF FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO LAX WITHOUT FURTHER DIFFIC ULTY. THE AIRCRAFT WAS FERRIED ON TWO ENGINES TO MSP FOR AN ENGINE CHANGE. EXACT PART CAUSING PROBLEM TO BE DETERMINED . 2 L 7 3 4F 4 F A22WE E20EA 1998062600143 19980626 00143 1998 6 26 UPS98426975 2 19980618 A 7261 SEAL BOEING 747 747121 1384871 NM NR 3 ENGINE FAILED A IPXA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 682UP 20349 ON TAKEOFF CREW NOTICE SMOKE IN COCKPIT, TURN ON A/C PACKS SMOKE WENT AWAY RETURN TO KSDF. FOUND NR 3 ENGINE HAD BAD OI L SEAL REMOVED AND REPLACED ENGINE. 2 L 7 4 4F A20WE 1998062600144 19980626 00144 WP 1998 6 26 UPS98826944 1 19980609 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 442.185 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E AT STA XFS442.185, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600145 19980626 00145 WP 1998 6 26 UPS98826945 1 19980609 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 484.895 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E AT STA XFS 484.895, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600146 19980626 00146 WP 1998 6 26 UPS98826946 1 19980609 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 397 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E AT STA XFS 397.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600147 19980626 00147 WP 1998 6 26 UPS98826947 1 19980609 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 297 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E AT STA XFS297.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600148 19980626 00148 WP 1998 6 26 UPS98826948 1 19980609 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 291.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E AT STA XFS291.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600149 19980626 00149 WP 1998 6 26 UPS98826949 1 19980607 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 120/140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D LONGERON 32R IS CRACKED AT THE FRAME ATTACH BOLT AT STA 120 AT 140. REMOVED AND REPLACED SECTION OF L ONGERON IAW SRM 53-2-2. 2 L 7 4 4F RT 4A25 1998062600150 19980626 00150 WP 1998 6 26 UPS98826950 1 19980605 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 113.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING L/E AT STA XFS 113.750 THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600151 19980626 00151 WP 1998 6 26 UPS98826951 1 19980607 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 188.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E AT STA XFS188.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REP AIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600152 19980626 00152 WP 1998 6 26 UPS98826952 1 19980605 A 5720 576985938 INTERCOSTAL DOUG DC8 DC871F 302199D WP WS 201.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E I/B OF THE STA XFS201.25 RIB, THE INTERCOSTAL IS CRACK EDAT THE I/B END. REMOVED, FABRIC ATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5769859 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998062600153 19980626 00153 WP 1998 6 26 UPS98826953 1 19980603 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 722.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING L/E AT STA XFS722.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600154 19980626 00154 WP 1998 6 26 UPS98826955 1 19980603 A 5320 37799191 FITTING DOUG DC8 DC871F 302199D WP BS 1340-1360 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, STA 1340-1360 STR 36 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779919 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600155 19980626 00155 WP 1998 6 26 UPS98826956 1 19980603 A 5720 576989115 DOUBLER DOUG DC8 DC871F 302199D WP WS 7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E LWR INTERNAL DOUBLER AT STA XOLDI7.00 IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBL ER IAW DWG 5769891 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600156 19980626 00156 WP 1998 6 26 UPS98826957 1 19980603 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E RIB AT STA XFS304.000 IS CRACKED AT THE LWR AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600157 19980626 00157 WP 1998 6 26 UPS98826959 1 19980604 A 5720 9753293 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING I/B SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 69753293 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600158 19980626 00158 WP 1998 6 26 UPS98826960 1 19980604 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 329 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING L/E AT STA XFS329.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600159 19980626 00159 WP 1998 6 26 UPS98826961 1 19980604 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING L/E AT STA XFS304.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600160 19980626 00160 WP 1998 6 26 UPS98826962 1 19980606 A 5320 45976431 FITTING DOUG DC8 DC871F 302199D WP BS 40 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, MAIN CABIN AT STA 40 STR 21R, THE FRAME TO CUSP TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACE D FITTING IAW DWG 4597643 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600161 19980626 00161 WP 1998 6 26 UPS98826963 1 19980607 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, STA 440-460 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600162 19980626 00162 WP 1998 6 26 UPS98826964 1 19980604 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING UPPER SKIN AT STR 10 IS CRACKED AT STA XRS74 (STRESS CORR CRACK). REPAIRED AREA IAW SRM 57-3 -1 FIG 10. 2 L 7 4 4F RT 4A25 1998062600163 19980626 00163 WP 1998 6 26 UPS98826965 1 19980607 A 5320 46402691 FITTING DOUG DC8 DC871F 302199D WP WS 1286 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:C, STA 1286 AT STR 19L, THE DOOR FRAME SUPPORT FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTIN G IAW DWG 4640269 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600164 19980626 00164 WP 1998 6 26 UPS98826966 1 19980608 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 798 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, L ANGLE CRACKED AT STA 798 LBL54. STOP DRILLED CRACK AND REPAIRED IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1998062600165 19980626 00165 WP 1998 6 26 UPS98826969 1 19980602 A 5320 561650951AD SHEAR TIE DOUG DC8 DC871F 302199D WP BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, SHEAR TIE BLOWNOUT AT FS 640 BETWEEN LONG 35L AND 35R. REMOVED, FABRICATED AND REPLACED SHEAR TIE PE R DWG 5616509 AND SRM 51-1-4 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600166 19980626 00166 WP 1998 6 26 UPS98826970 1 19980602 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E RIB AT STA XFS 785.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PE R SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600167 19980626 00167 WP 1998 6 26 UPS98826971 1 19980603 A 5320 37533061 FITTING DOUG DC8 DC871F 302199D WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D LONG 23R END FITTING JUST AFT OF FS 980 IS CRACKED. REMOVED AND REPLACED FITTING PER DWG 3753306-1 AN D SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600168 19980626 00168 WP 1998 6 26 UPS98826972 1 19980604 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 7095 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING L/E RIB AT STA XILD .7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED P ER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600169 19980626 00169 WP 1998 6 26 UPS98826973 1 19980603 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 841.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING L/E RIB AT STA XFS 841.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED P ER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600170 19980626 00170 WP 1998 6 26 UPS98826974 1 19980605 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 113.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT WING L/E RIB AT STA XFS 113.75 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600171 19980626 00171 NM 1998 6 26 98FDEA00404 1 19980618 A 7711 EPR TRANSMITTER BOEING 727 727227 1384078 NM NR 3 ENGINE MALFUNCTION A FDEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 25 496FE 21670 98-0154 STA-IND, ON T/O AIRCRAFT ROLL WAS EXTREMELY LONG. AIRBORNE WITH STANDARD T/O EPR'S SET NR 1 AND NR 3 N1'S WERE APPROXIMATELY 82 PERCENT AND NR 2 N1 WAS APPROX 91 PERCENT. A/C BLEED SWITCHES WERE NR 1 OPEN NR 2 AND NR 3 WERE CLOSE D. CHECKED ANTI-ICE BLEEDS ALL WERE CLOSED. OTHER ENGINE INSTRUMENTS SEEMED TO MATCH N1 SETTINGS. REMOVED AND REPLACE D NR 3 PRESS RATIO TRANSMITTER EPR OPER CHECK NORMAL ON GROUND AT THIS TIME. SEE A/C MAINTENANCE LOG PAGE 972220 FOR NR 1 EPR DEFERRAL. FOUND INSECT NEST (MUD DAUBER) IN PT 2 PORT NR 1 AND NR 3 ENGINE. CLEANED OUT NEST AND BLEW OUT PT 2 PORT. RAN ENGINES PER JET RUN HANDBOOK CHAPTER 6. ALL PARAMETERS NORMAL. 2 L 7 3 4F A3WE 1998062600172 19980626 00172 NM 1998 6 26 98FDEA00405 1 19980617 A 5610 PPG5893543110 WINDSHIELD BOEING 727 72725C 138400H NM RT COCKPIT CRACKED A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 133FE 19851 98-0155 - STA-IAD - SAW FLAME AND ARCING ON COPILOTS FROM WIND SCREEN RIGHT NR 1 FROM WINDOW HEAT. WINDOW HEAT WAS SECU RED ON RIGHT SIDE, MINUTES LATER WIND SCREEN ON OUTER PANEL BEGAN CRACKING. REMOVED RIGHT NR 1 WINDOW AND INSTALLED SE RVICEABLE WINDOW AND TORQUED FASTENERS PER MAINTENANCE MANUAL 56-11-11. COMPLETED INSTALLATION OF RIGHT NR 1 WINDOW PER 56-11-11. 2 L 7 3 4F A3WE 1998062600173 19980626 00173 NM 1998 6 26 98FDEA00406 1 19980617 A 5320 651627910 BEAM BOEING 727 727232 1384082 NM BS 760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 498FE 20867 STA-PAE - WHILE WORKING NR 0490, FOUND LONGITUDINAL BEAM UPPER HORIZONTAL FLANGE TO BE CRACKED AT BS 760, RBL 26, WL 208 . REMOVED AND REPLACED LONGITUDINAL BEAM UPPER HORIZONTAL FLANGE AT BS 760 TO BS 850, RBL 26, WL 208 PER BOEING DRAWING 65-16279 AND FED-EX SRM 51-30-2. 2 L 7 3 4F A3WE 1998062600174 19980626 00174 WP 1998 6 26 ABXA9800521 1 19980617 A 5320 99220422 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 332 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND FUSELAGE FRAME FITTING CRACKED AT STATION 332 NEAR LONGERON 24 RT. REPLACED FRAME FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998062600175 19980626 00175 WP 1998 6 26 ABXA9800522 1 19980617 A 5240 99115797 ANGLE DOUG DOUG DC9 DC933F 302207A WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND ATTACH ANGLE CRACKED AT FWD END OF SERVICE DOOR UPPER MOST BEAM. REPLACED ANGLE IAW DC9 SRM 51-30 -52 AND 51-30-1. 2 L 7 2 4F A6WE 1998062600176 19980626 00176 WP 1998 6 26 ABXA9800523 1 19980617 A 5720 99582099 ANGLE DOUG DOUG DC9 DC933F 302207A WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND FRAME STATION 718 SUPPORT ANGLE CRACKED ON LONGERON 20. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND DA CO DWG 9958209. 2 L 7 2 4F A6WE 1998062600177 19980626 00177 WP 1998 6 26 ABXA9800524 1 19980617 A 5311 99552387 FRAME DOUG DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND FRAME CRACKED AT FS 1056 AND LONGERON 16L. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998062600178 19980626 00178 WP 1998 6 26 ABXA9800525 1 19980617 A 5530 991182012 BRACKET DOUG DOUG DC9 DC941 302207N WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND THE SUPPORT BRACKET FOR THE RIGHT VOR ANTENNA IN THE VERTICAL STABILIZER LEADING EDGE ASSY CRACKED . REPLACED SUPPORT BRACKET IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998062600179 19980626 00179 WP 1998 6 26 ABXA9800526 1 19980612 A 5753 591215057 BRACKET DOUG DOUG DC9 DC933F 302207A WP LT TE FLAP BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 931AX 47384 DURING FINAL APPROACH, LOUD THUD WAS HEARD AND FLAPS INDICATED LEFT 40 DEG AND RIGHT 17 DEG. LEFT FLAP AFT HINGE AT STA TION 164.00 WAS BROKEN AT BOLT BOSSES. BRACKET WAS REPLACED IAW DC-9 MM 27-50-1. 2 L 7 2 4F A6WE 1998062600180 19980626 00180 WP 1998 6 26 ABXA9800527 1 19980601 A 5311 99582387 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 WHILE COMPLYING WITH C-CHECK, FOUND FUSELAGE FRAME AT FS 980 CRACKED AT LONGERON 16R. REPLACED FUSELAGE FRAME SECTION F ROM LONGERON 15R TO LONGERON 18R IAW DC-9 SRM CHAPTER 53-03. 2 L 7 2 4F A6WE 1998062600181 19980626 00181 WP 1998 6 26 ABXA9800528 1 19980502 A 5712 5769496 RIB DOUG DOUG DC8 DC863F 302198F WP WS 466.651 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XS 466.651 IS CRACKED AT THE AFT LWR END. REPAIRED IAW ABX DWG K05056 AND DC8 SR M 51-1-20D. 2 L 7 4 4F 4A25 1998062600182 19980626 00182 WP 1998 6 26 ABXA9800529 1 19980503 A 5320 5616674 INTERCOSTAL DOUG DOUG DC8 DC863F 302198F WP BS 1440 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 INTERCOSTAL CRACKED AT STATION 1440 AND LONGERON 34R. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5616674. 2 L 7 4 4F 4A25 1998062600183 19980626 00183 WP 1998 6 26 ABXA9800530 1 19980504 A 5720 9753293 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 250 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 54927 LEFT INBOARD STUB WING AT STATION XS 250 CRACKED AT BOTTOM. INSTALLED REPAIR ANGLE STIFFENER IAW DWG 9753203 AND DC8 SR M 51-1-20. 2 L 7 4 4F 4A25 1998062600184 19980626 00184 WP 1998 6 26 ABXA9800531 1 19980504 A 5720 5655445 BRACKET DOUG DOUG DC8 DC863F 302198F WP WS 603.75-610 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING OUTBOARD LEADING EDGE FWD TAI SUPPORT BRACKET BETWEEN STATION XFS 603.75 AND 610 IS CRACKED IN TWO PLACES. RE PAIRED IAW DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998062600185 19980626 00185 WP 1998 6 26 ABXA9800532 1 19980504 A 5320 3750257503 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STATION 1040-1060 STRINGER 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998062600186 19980626 00186 WP 1998 6 26 ABXA9800533 1 19980604 A 5330 59114273 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT AFT FUSELAGE SKIN CRACKED AT FS 945 BETWEEN LONGERONS 15R AND 16R. R EPAIRED IAW ABX REA D953-23860MR. 2 L 7 2 4F A6WE 1998062600187 19980626 00187 WP 1998 6 26 ABXA9800534 1 19980604 A 5320 591326218 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 929AX 45874 WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT ENGINE PYLON TO FUSELAGE ATTACH ANGLE CRACKED AT FS 996. REPLACED AT TACH ANGLE IAW DC-9 SRM CHAPTER 51-30-2. 2 L 7 2 4F A6WE 1998062600188 19980626 00188 WP 1998 6 26 ABXA9800535 1 19980605 A 2701 5614271 CONTROL COLUMN DOUG DOUG DC9 DC941 302207N WP COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 WHILE ACCOMPLISHING AD 90-01-12, THE RIGHT CONTROL COLUMN WAS FOUND CRACKED. CONTROL COLUMN WAS REPLACED IAW DC-9 S/B 2 7-288 AND ABX REA D927-23891. 2 L 7 2 4F A6WE 1998062600189 19980626 00189 WP 1998 6 26 DLL10981261 1 19980615 A 2560 MECHANISM LKHEED 1011 10113851 5265010 WP L1/L2 DOOR FAILED TEST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 722DA 193C1147 L-1 AND L-2 DOORS FAILED EMERGENCY OPS, TEST PER OPN 68116, EXCEEDED TIME LIMIT. REPLACED COUNTER BALANCES. 2 L 7 3 4F A23WE 1998062600190 19980626 00190 NM 1998 6 26 DL72L981262 1 19980615 A 2782 ANGLE BOEING 727 727232 1384082 NM NR 2 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND ON F1 LETTER CK, NR 2 LE FLAP ACTUATOR SUPPORT BOX CRACKED O/B SIDE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998062600191 19980626 00191 NM 1998 6 26 DL72L981263 1 19980615 A 5320 WEB BOEING 727 727232 1384082 NM BS 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 WEB CRACKED AT STA 1228 RBL 20 WL208 AT LIGHTNING HOLE. REPAIR PER M/M 53-11-0 PG 832. 2 L 7 3 4F A3WE 1998062600192 19980626 00192 NM 1998 6 26 DL72L981264 1 19980615 A 2782 SUPPORT BOEING 727 727232 1384082 NM NR 6 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 NR 6 L/E FLAP ACTUATOR SUPPORT BRACKET CRACKED AT RADIUS I/B UPPER END AND O/B LOWER END. INSTALLED DOUBLERS PER M/M 5 7-20-21. 2 L 7 3 4F A3WE 1998062600193 19980626 00193 NM 1998 6 26 DL76S981265 1 19980615 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 124DE 6528 23438 ON L/O, FOUND ZONE EMERGENCY TRACK LIGHTS INOP BOTH AISLES. REPLACED PWR SUPPLY M9010. LIGHTS OPS NML. 2 L 7 2 4F RT A1NM 1998062600194 19980626 00194 1998 6 26 DLL10981266 4 19980615 A 2330 PROJECTOR 7001076001 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 721DA 0716 193C1139 STRONG ODOR LIKE ELECTRICAL BURNING BETWEEN FIRST CLASS AND COACH NO SMOKE NOTICED PER CREW REPORTS APPROX 10 MIN. AFTE R MOVIE STARTED B ZONE PROJECTOR INOP WITH ELECTRICAL ODOR NOTICED. ODOR WAS NOTICED IN B ZONE ONLY. OPENED AND INSP ECTED ALL CEILING AREAS. FOUND ODOR TO BE ISOLATED TO B ZONE PROJECTOR. REPLACED SAME. 2 L 7 3 4F A23WE 1998062600195 19980626 00195 NM 1998 6 26 DL72S981268 1 19980616 A 5400 SKIN BOEING 727 727232 1384082 NM S-DUCT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 467DA 20744 RIVETS LOOSE .25 INCH CRACK IN DORSAL FIN OUTER SKIN RT SIDE BELOW PANEL 9516. REPAIR PER M/M 54-30-0 FIG 801. 2 L 7 3 4F A3WE 1998062600196 19980626 00196 NM 1998 6 26 DL72S981269 1 19980615 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR SEPARATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 RT ELEVATOR I/B T/E SKIN, SEPARATED. DRILLED REPAIR FASTENER HOLES PER M/M 55-20-0 PG 801. INSTALLED REPAIR FASTENER P ER M/M 55-20-0 PG 801. 2 L 7 3 4F A3WE 1998062600197 19980626 00197 NM 1998 6 26 DL73E981270 1 19980616 A 3610 656620111 DUCT BOEING 737 737247 138448D NM APU AREA CRACKED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 236WA 23184 WITH APU BLEED OPEN POWERING RIGHT PACK LEFT WING BODY OVERHEAT LIGHT ILLUMINATED APU BLEED PLACED OFF AFTER DELAY LIGHT WENT OUT LATER F/A NOTICED BURNING SMELL IN MID CABIN AREA. FOUND APU BLEED LINE CRACKED JUST AFT OF APU BLEED VALVE. REPLACED BLEED DUCT. 2 L 7 2 4F A16WE 1998062600198 19980626 00198 NM 1998 6 26 DL76S981272 1 19980616 A 5754 SKIN BOEING 767 767332 1382001 NM LT SLATS DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 119DL 23278 UPPER SKINS ON THE TRAILING EDGE WEDGES OF THE NR 9, 10, AND 12 SLATS WERE FOUND WITH DELAMINATED AREAS. REPAIRED PER E RA 365048-14AD. 2 L 7 2 4F RT A1NM 1998062600199 19980626 00199 NM 1998 6 26 DL72S981273 1 19980617 A 3350 BATTERY PACK 20131A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 35905 21074 ON LAYOVER, FOUND L2 DOOR EMERGENCY LIGHT INOP. REPLACED M9027 CONTROLLER AND BATTERY PACK. 2 L 7 3 4F A3WE 1998062600200 19980626 00200 NM 1998 6 26 DL72K981274 1 19980615 A 5320 65562312 STRAP BOEING 727 727232 1384082 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 FUSELAGE R1 DOOR SURROUND UPPER HINGE CUTOUT. REINFORCEMENT DOUBLER : REPAIR FOR CRACKED BEAR STRAP. THE R1 DOOR OPENI NG REINFORCING DOUBLER (BEAR STRAP) WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLE D AND REPAIRED WITH AN EXTERNAL DOUBLER PER BAC S/B 727-53-0136. THE REPAIR WAS DOCUMENTED PER ER/A365040-14. 2 L 7 3 4F A3WE 1998062600201 19980626 00201 WP 1998 6 26 DLL10981275 1 19980614 A 5330 1503542107 SKIN LKHEED 1011 10113851 5265010 WP BS 1693 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 721DA 193C1139 FUSELAGE SKIN FS 1693 STRG 38 : REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 1693 AND STRG 38. THE DAMAGED SKIN WAS CUTOUT OVER A 3.1 BY 6.8 AREA TO REMOVE THE CORROSION. THE CUTOUT WAS REPAIRED WITH AN EXTERN AL ALUMINUM DOUBLER PER ER/A 365024-14, REV A. 2 L 7 3 4F A23WE 1998062600202 19980626 00202 NM 1998 6 26 DL72S981277 1 19980614 A 5711 65192922 SPAR WEB BOEING 727 727232 1384082 NM CENTER SECTION CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 WING CENTER SECTION REAR SPAR WEB, RBL 3 AND LBL 10 : REPAIR FOR WEB CRACK. THE WING CENTER SECTION REAR SPAR WEB WAS FOUND WITH TYPICAL CRACKS NEAR THE UPPER CAP AT RBL 3 AND LBL 10. THE DAMAGED AREAS OF WEB WERE CUTOUT AND REPAIRED WIT H ALUMINUM REPAIR DOUBLERS. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365002-14AD, REV B. THE REPAIRS ARE CONSIDERED TEMP ORARY UNTIL HMV WHEN THE FULL SPAR WEB MODIFICATION WILL BE ACCOMPLISHED PER AD 97-25-15. 2 L 7 3 4F A3WE 1998062600203 19980626 00203 NM 1998 6 26 DL72S981278 1 19980614 A 5711 65192923 SPAR WEB BOEING 727 727232 1384082 NM CENTER SECTION CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 WING CENTER SECTION REAR SPAR, WEB RBL 3 AND RBL 9 : REPAIR FOR WEB CRACKS. THE WING CENTER SECTION SPAR WEB WAS FOUND WITH TYPICAL CRACKS NEAR THE UPPER SPAR CAP. THE CRACKS WERE CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 365001-14AD, REV B. THE REPAIR IS TEMPORARY UNTIL HMV WHEN THE SPAR WEB WILL BE M ODIFIED PER AD 97-25-15. 2 L 7 3 4F A3WE 1998062600204 19980626 00204 NM 1998 6 26 DLM88981279 1 19980617 A 2131 ACTUATOR 20219742 DOUG MD88 MD88 3023688 NM OUTFLOW VALVE FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 945DL 111432 49818 AFTER T/O, BOTH AUTO PRESS CONTROLLERS FAILED COULD NOT PRESSURIZE A/C IN AUTO. A/C ATB-RETURNED TO STL. REPLACE OUTF LOW VALVE ACTUATOR PER M/M CKS NML. 2 L 7 2 4F RT A6WE 1998062600205 19980626 00205 WP 1998 6 26 DLL17981280 1 19980617 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP 2R DOOR INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 765DA 193H1206 ON LAYOVER, FOUND EMERGENCY BATTERY PACK NOT CHARGING. REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 3 4F A23WE 1998062600206 19980626 00206 NM 1998 6 26 DL767981281 1 19980609 A 5754 SKIN BOEING 767 767232 1385132 NM LE FLAPS DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 104DA 22216 DELAMINATION WAS FOUND ON SEVERAL T/E WEDGES OF THE L/E SLATS (NR 1, 2, 4 AND 5). REPAIRED PER ERA 365004-14AD. 2 L 7 2 4F RT A1NM 1998062600207 19980626 00207 NM 1998 6 26 DL72S981283 1 19980609 A 5313 65564414 STRINGER BOEING 727 727232 1384082 NM BS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 S29R WAS FOUND CRACKED NEAR FS 950F. REPAIRED PER ERA 331781-14. 2 L 7 3 4F A3WE 1998062600208 19980626 00208 NM 1998 6 26 DL72S981284 1 19980609 A 5311 65561314 FRAME BOEING 727 727232 1384082 NM BS 1090 CUT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 FUSELAGE FRAME AT FS 1090 AND S28R WAS FOUND TO HAVE A CUT ACROSS A ROW OF FASTENERS AT THE SHEAR CLIP. REPAIRED PER ER A 331789-14. 2 L 7 3 4F A3WE 1998062600209 19980626 00209 NM 1998 6 26 DL72K981285 1 19980617 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 466DA WA7035 20743 AFT LEFT EMERGENCY LIGHT INOP. REPLACED BATT PACK. LIGHT NOW WILL NOT TURN OFF. REPLACED BATTERY RACK. CKS GOOD PER MM. 2 L 7 3 4F A3WE 1998062600210 19980626 00210 NM 1998 6 26 DL72S981286 1 19980617 A 3350 BATTERIES BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 408DA 21152 ON L/O, FOUND 2L DOOR EMERGENCY LIGHT INOP. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1998062600211 19980626 00211 NM 1998 6 26 DL76P981288 1 19980618 A 5330 146T35514 SKIN BOEING 767 767332 1382001 NM BS 1197 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1402A 25989 FUSELAGE SKIN FS 1197+77, STRG 36R : REPAIR FOR SKIN CUTOUT AT LAP SPLICE. THE FUSELAGE SKIN WAS BADL Y DENTED BY GROUND EQUIPMENT AT THE STRINGER 36R LAP SPLICE AT FS 1197+77. THE DAMAGED SKIN WAS CUTOUT AND EXTERNAL ALU MINUM REPAIR DOUBLERS WERE INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 365068-14, REV A. 2 L 7 2 4F RT A1NM 1998062600212 19980626 00212 NM 1998 6 26 DL73S981289 1 19980618 A 5330 6573742 SKIN BOEING 737 737232 1384475 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 UPON HFEC AND LFEC INSPECTIONS OF THE UPPER AFT CORNER OF THE FWD GALLEY DOORWAY PER 3-58715-3AD, A CRACK WAS INDICATED. REPAIRED PER ERA 331849-14AD. 2 L 7 2 4F RT A16WE 1998062600213 19980626 00213 NM 1998 6 26 DLM88981290 1 19980618 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 MTC FOUND A CRACK AT L2L ON THE FS1418 FRAME WHICH IS A TYPICAL LOCATION. REPAIRED PER ERA 331832-14. 2 L 7 2 4F RT A6WE 1998062600214 19980626 00214 NM 1998 6 26 DLM88981291 1 19980618 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 A DENT WAS FOUND ON THE FUSELAGE SKIN JUST AFT OF THE L1 DOOR OPENING AT APPROX FS237, BETWEEN L18-20L. REPAIRED PER ER A 331828-14. 2 L 7 2 4F RT A6WE 1998062600215 19980626 00215 NM 1998 6 26 DLM88981292 1 19980618 A 5330 5911401 SKIN DOUG MD88 MD88 3023688 NM BS 225 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 A DENT WAS FOUND ON THE FUSELAGE SKIN JUST AFT OF THE L1 DOOR OPENING AT APPROX FS 225, BETWEEN LONGERONS 17L AND 18L. R EPAIRED PER ERA 331827-14. 2 L 7 2 4F RT A6WE 1998062600216 19980626 00216 NM 1998 6 26 DLM88981293 1 19980618 A 5311 9912243241 FRAME DOUG MD88 MD88 3023688 NM BS 1307 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 990DL 53342 FS1307 FRAME WAS CORRODED FROM JUST INBD OF L29R TO BETWEEN L28L AND L29L. REPAIRED PER ERA 331842-14. 2 L 7 2 4F RT A6WE 1998062600217 19980626 00217 NM 1998 6 26 DL73S981294 1 19980618 A 5330 6545767531 SKIN BOEING 737 737232 1384475 NM BS 400 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 FUSELAGE SKIN AND BONDED DOUBLER WERE FOUND DENTED BETWEEN S17L AND 18L AT FS 400. REPAIRED PER ERA 331844-14. 2 L 7 2 4F RT A16WE 1998062600218 19980626 00218 NM 1998 6 26 DL72W981296 1 19980618 A 3350 LIGHTS RPS1 BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2819W 1093 21057 FWD SECTION OF FLOOR TRACK LIGHTING IN FC INOP. REPLACED FWD AND AFT FLOOR TRACK LGT PWR SUPPLIES AND BATTS. REPAIRED CHAFFED WIRE UNDER SEAT 1 AB. 2 L 7 3 4F A3WE 1998062600219 19980626 00219 NM 1998 6 26 DLM88981297 1 19980617 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 582 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 928DL 49715 FUSELAGE SKIN FS 579-588, STRG 20L-21L : SKIN CUTOUT REPAIR FOR DENT. THE FUSELAGE SKIN BETWEEN FS 579 AND 588 AND BETW EEN STRINGERS20L AND 21L WAS BADLY DENTED BY IMPACT WITH GROUND EQUIPMENT. THE DAMAGED AREA OF SKIN WAS TRIMMED AWAY AN D AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 365054-1 4, REV B. 2 L 7 2 4F RT A6WE 1998062600220 19980626 00220 WP 1998 6 26 DLL19981299 1 19980618 A 7732 VIBRATION LIGHT LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB21122* 54555 NE NR 3 ENGINE ILLUMINATED A DALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 27 755DL 75747 193Y1184 14738 NR 3 VIBRATION LIGHT CAME ON. INDICATED APPROX 2.9 BOTH A AND B. ACCOMPANIED BY ENGINE VIBRATION. SHUT DOWN ENGINE VI APOM. CRUISE AT 350. NO THROTTLE MOVEMENT AT TIME OF FAILURE. LUBED FAN BLADE CLAPPERS. CHECKED CHIP DETECTORS. INS PECTED ENGINE FOR LOOSE HOLD OPEN RODS. NO TROUBLE FOUND. RAN VIBRATION SURVEY PER PFHB. ALL WITHIN LIMITS. 2 L 7 3 4F 4 F A23WE A12EU 1998062600221 19980626 00221 WP 1998 6 26 DLL10981301 1 19980618 A 3350 BULB 2232 LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 735D 193C1226 R3 OUTSIDE EMERGENCY LIGHT INOP. RELAMPED, OPN NML. 2 L 7 3 4F A23WE 1998062600222 19980626 00222 WP 1998 6 26 DLL19981302 1 19980618 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 193H1216 FOUND EMERGENCY AISLE EXIT LIGHTING POWER SUPPLY CHARGING CONTINUOSLY. REPLACED POWER SUPPLY PER MM. OPS CHKS GOOD. 2 L 7 3 4F A23WE 1998062600223 19980626 00223 NM 1998 6 26 RRXA98236 1 19980619 A 2612 FIRE LOOPS BOEING 727 727222 1384073 NM AFT FUSELAGE MALFUNCTIONED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 7638U 19911 AFTER TAKEOFF, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED AND REMAINED ILLUMINATED UNTIL LANDING. *S/D* REMOVED AND REP LACED FWD AND MIDDLE LOWER AFT BODY FIRE LOOPS, LOWER AFT BODY OVERHEAT WARNING SYSTEM. OPS CHECKS NORMAL ON GROUND, NO DEFECTS. 2 L 7 3 4F A3WE 1998062600224 19980626 00224 NM 1998 6 26 VNAA980611 1 19980617 A 3260 869701 SENSOR 2291500001 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG OUT OF ADJUST A VNAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 07 437JS 3055 SHORTLY AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT WHEN SELECTED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED. MAINTENANCE INSPECTED AND ADJUSTED, THE RIGHT HAND WEIGHT ON WHEELS SENSOR CLEARANCE, AND PERFORMED OPERATIONAL GEAR C HECKS IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-61-10 AND 32-31-00. THE CHECKS WERE SATISFACTORY, AND THE AIRCRA FT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998062600225 19980626 00225 NM 1998 6 26 B4MR98028 1 19980618 A 5313 STRINGER BOEING 727 727191 1384063 NM BS 600 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND BS 600 S19 RT BULGE IN LAP. REMOVED CORRODED STRINGER AND REPAIRED IAW BOEING 727 SRM 53-10-04 FIG 1. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 110055. AMERICAN INTERNATION AL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600226 19980626 00226 NM 1998 6 26 B4MR98029 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 480 DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND BS 480 S4 RT SKIN DAMAGED. REMOVED DAMAGE AND INSTALLED REPAIR IAW B727 SRM 53 -30-3 FIG 14. C-CHECK CARD NUMBER 1C-133. NON-ROUTINE TASK CARD NUMBER 112383. AMERICAN INTERNATIONAL AIRWAYS INC (B4 MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600227 19980626 00227 NM 1998 6 26 B4MR98030 1 19980618 A 5210 GATE BOEING 727 727191 1384063 NM L1 DOOR CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND L-1 DOOR UPPER AND LOWER GATES HAVE CORROSION. LOWER GATE CORROSION WITHIN LIMITS IAW B727 SRM CH 52-00-2 FIG 2. REMOVED AND REPLACED UPPER GATE IAW B727 MM CH 52-11-00 AND SRM CH 51-30-2. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 112393. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMP LISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600228 19980626 00228 NM 1998 6 26 B4MR98031 1 19980618 A 5744 FITTING BOEING 727 727191 1384063 NM WS 515 CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND NR 3 SPOILER ACTUATOR/FLAP TRANS ATTACH FITTING CRACKED APPROXIMATELY WS 515. REM OVED AND REPLACED BRACKET IAW AIA EDR NR B2-05594 AND IAW B727 SRM 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C57- 581-03. NON-ROUTINE TASK CARD NUMBER 113701. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600229 19980626 00229 NM 1998 6 26 B4MR98032 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 1000 DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND SKIN DAMAGED AT BS 1000 S4 RT. REPAIRED SKIN IAW B727 SRM 53-30-3 FIG 5. C-CH ECK CARD NUMBER 1C-133. NON-ROUTINE TASK CARD NUMBER 113705. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHI NG COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600230 19980626 00230 NM 1998 6 26 B4MR98033 1 19980618 A 5522 SKIN BOEING 727 727191 1384063 NM LT ELEVATOR CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND 2ND FROM O/B TIP OF LEFT HAND ELEVATOR STATIC WICK BASE CORRODED BETWEEN SKIN. REPAIRED IAW B727 SRM CH 55-20-3 FIG 2 SHT 1. C-CHECK CARD NUMBER 1C-52. NON-ROUTINE TASK CARD NUMBER 113726. AMERIC AN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600231 19980626 00231 NM 1998 6 26 B4MR98034 1 19980618 A 5741 BUSHING BOEING 727 727191 1384063 NM RT WING DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND RIGHT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHING HAS SECTION OF LINING MIS SING. REMOVED AND REPLACED RIGHT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHINGS IAW 727 MM 57-41-11. CORROSION TA SK CARD NUMBER C53-132-03. NON-ROUTINE TASK CARD NUMBER 113818. ALT (P/N 65-15940-110) BUSHING / 10-60516-1 BUSHING. A MERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600232 19980626 00232 NM 1998 6 26 B4MR98035 1 19980618 A 5741 BUSHING BOEING 727 727191 1384063 NM LT WING DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND LEFT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHING HAS SECTION OF LINING MISS ING. REMOVED AND REPLACED LEFT FRONT SPAR WING TO BODY FITTING BOTTLE PIN BUSHINGS IAW B727 MM 57-41-11. CORROSION TAS K CARD NUMBER C53-132-03. NON-ROUTINE TASK CARD NUMBER 113819. ALT (P/N 65-15940-110) BUSHING / 10-60516-1 BUSHING. A MERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600233 19980626 00233 NM 1998 6 26 B4MR98036 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 1080 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ACCOMPLISHMENT OF AD 90-21-10 / SB 727-53-0109, FOUND WHILE ACCOMPLISHING LFEC INSPECTION OF BS 1080 SB 727-53-01 09 NOTED MATERIAL LOSS OF GREATER THAN 10 PERCENT AT RT S10 APPROX 3 AREA. REPAIRED SKIN IAW B727 DRAWING NR 69-62161 F IG 12 (SB 727-53-0109). NON-ROUTINE TASK CARD NUMBER 113846. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHI NG COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600234 19980626 00234 NM 1998 6 26 B4MR98037 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 1080 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ACCOMPLISHMENT OF AD 90-21-10 / SB 727-53-0109, FOUND WHILE ACCOMPLISHING LFEC INSPECTION OF BS 1080 S/B 727-53-0 109 NOTED MATERIAL LOSS GREATER THAN 10 PERCENT AT LT S3 APPROX 1 TO .5 AREA. REPAIRED SKIN IAW B727 DRAWING NR 69-6216 1 FIG 13 (SB 727-53-0109). NON-ROUTINE TASK CARD NUMBER 113847. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLI SHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600235 19980626 00235 NM 1998 6 26 B4MR98038 1 19980618 A 5713 STRINGER BOEING 727 727191 1384063 NM WS 601 CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND MAIN BOX INTERIOR HAS CRACKED STRINGER AT RIB WS 601. REPAIRED IAW SB 727 57A159 FIG 4. CORROSION TASK CARD NUMBER C57-571-01. NON-ROUTINE TASK CARD NUMBER 113875. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600236 19980626 00236 NM 1998 6 26 B4MR98039 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 760-850 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND SEAT TRACK CORRODED STA 760 TO 785 RBL 42.5. REMOVED AND REPLACED SEAT TRACK BS 7 60 TO BS 850 IAW B727 SRM 51-10-1 AND 51-30-2 TREATED AREA FOR CORROSION CONTROL IAW B727 SRM 51-10-2. CORROSION TASK C ARD NUMBER C53-224-03. NON-ROUTINE TASK CARD NUMBER 113922. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHIN G COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600237 19980626 00237 NM 1998 6 26 B4MR98040 1 19980618 A 5744 FITTING BOEING 727 727191 1384063 NM WS 546 CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND NR 13 SPOILER ACTUATOR / FLAP TRANS ATTACH FITTING CRACKED APPROXIMATELY WS 546. R EMOVED AND REPLACED BRACKET IAW AIA EDR NR B205594 AND B727 SRM 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C57-581 -03. NON-ROUTINE TASK CARD NUMBER 115289. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LE ASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600238 19980626 00238 NM 1998 6 26 B4MR98041 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 1110 & 1130 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND SEAT TRACK CORRODED BETWEEN BS 1110 AND 1130 RBL 45. REMOVED AND REPLACED SEAT TR ACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 113940. AME RICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600239 19980626 00239 NM 1998 6 26 B4MR98042 1 19980618 A 5730 SKIN BOEING 727 727191 1384063 NM WS 760 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON CENTER WING UPPER SKIN APPROX STA 760 RBL 44 TO BE OUT OF LIMITS IAW B727 SRM 57-30-1 FIG 4 NOTE A. PERFORM HFEC INSPECTION ON EFFECT HOLES NO DEFECT NOTED. INSTALLED REPAIR PARTS IAW AIA ENGINEERING DRAWING NR 2730, EDR B2-05531 AND EDR B2-05617. CORROSION TASK CARD NUMBER C53-224-05. NON-ROUTINE TASK C ARD NUMBER 113949. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURC HASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600240 19980626 00240 NM 1998 6 26 B4MR98043 1 19980618 A 3270 65261133 FORGING BOEING 727 727191 1384063 NM TAIL SKID CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND TAIL SKID COMPT ACTUATOR ATTACH FORGING CRACKED. REMOVED AND REPLACED TAIL SKI D ACTUATOR ATTACH FORGING IAW B727 MM 32-71-41. OPS CHECKED TAIL SKID ACTUATOR, FOUND TO CHECK OUT GOOD IAW 727-100 MM REF 32-71-00. C-CHECK CARD NUMBER 1C-109. NON-ROUTINE TASK CARD NUMBER 113950 AND 114729. YOKE = 65-26113-4. AMERICA N INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600241 19980626 00241 NM 1998 6 26 B4MR98044 1 19980618 A 5311 FRAME BOEING 727 727191 1384063 NM FS 930 CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND 2 CRACKS IN RT FUSELAGE FRAME AT STA 930 S-14R. REPAIRED 2 CRACKS IN RT FUSELAGE FRAME STA 930 S14R IAW 727 SRM 53-10-4. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 113955. A MERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600242 19980626 00242 NM 1998 6 26 B4MR98045 1 19980618 A 5311 FRAME BOEING 727 727191 1384063 NM FS 930 CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND 2 CRACKS IN LT FUSELAGE FRAME AT STA930 S-14L. REPAIRED 2 CRACKS IN FUSELAGE FRAM E STA 930 S-14L IAW 727 SRM 53-10-4. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 113956. AMER ICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600243 19980626 00243 NM 1998 6 26 B4MR98046 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 760-784 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON SEAT TRACK RBL-25 STA 760 TO 784. REMOVED AND REPLACED SEAT TRACK IA W 727 SRM 51-10-1 AND 53-10-5. PORTION OF SEAT TRACK REPLACED BETWEEN BS 760 AND BS 784 RBL 25. SEAT TRACK SPLICE GAP IS MORE THAN 0.19, NO SEALANT IN CHANNEL AND HOLE NO REFINISHED IAW SRM 53-10-5 PAGE 4A. REPAIRED SEAT TRACK BS 760 TO FS 784 RBL 25 IAW B727 SRM 53-10-5 FIG 2 PAGE 4A-4B. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMB ERS 113960 AND 114345. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600244 19980626 00244 NM 1998 6 26 B4MR98047 1 19980618 A 5313 STRINGER BOEING 727 727191 1384063 NM BS 380 DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND BS 380 S-4 RT STRINGER DAMAGED. REPAIRED STRINGER 4 RT AS PER B727 SRM 53-10-3 FIG 2. CROWN STRINGER REPAIR PER SRM. C-CHECK CARD NUMBER 5C-12. NON-ROUTINE TASK CARD NUMBER 113980. AMERICAN INTE RNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600245 19980626 00245 NM 1998 6 26 B4MR98048 1 19980618 A 5320 69154243 FITTING BOEING 727 727191 1384063 NM BS 680 CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND BS 680 S-16 RT END FITTING CRACKED. REMOVED FITTING IAW SRM 51-30-2. INSTALLE D FITTING IAW B727 SRM 51-30-2. C-CHECK CARD NUMBER 5C-12. NON-ROUTINE TASK CARD NUMBER 113990. AMERICAN INTERNATIONA L AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600246 19980626 00246 NM 1998 6 26 B4MR98049 1 19980618 A 5315 FLOORBEAM BOEING 727 727191 1384063 NM BS 720 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND BS 720 RBL 35 FLOORBEAM CORRODED AROUND NUT PLATES. CUT OUT DAMAGED AREA THAT WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-10-06. REPAIRED IAW 727 SRM 53-10-8. CORROSION TASK CARD NUMBER C53-224-01. NON -ROUTINE TASK CARD NUMBER 113992. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WOR KSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600247 19980626 00247 NM 1998 6 26 B4MR98050 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 700-740 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND BS 700 RBL 45 SEAT TRACK CORRODED UPPER AND LOWER SURFACES AROUND NUT PLATES. REM OVED AND REPLACED SEAT TRACK BS 700 TO BS 740 IAW 727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-224-01. N ON-ROUTINE TASK CARD NUMBER 113995. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING W ORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600248 19980626 00248 NM 1998 6 26 B4MR98051 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 480-600 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND BS 520 TO 580 RBL 25 SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK FROM BS 480 TO BS 600 IAW 727 SRM 53-10-5. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 114004. AMERI CAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600249 19980626 00249 NM 1998 6 26 B4MR98052 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 460-480 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND BS 480 LBL 45 SEAT TRACK CORRODED. REPLACED SEAT TRACK FROM BS 460 TO BS 480 IAW BOEING 727 SRM 53-10-5. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 114007. AMERICAN INTERNAT IONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600250 19980626 00250 NM 1998 6 26 B4MR98053 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 400-344 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND BS 400 TO 344 SEAT TRACK CORRODED RBL 45. REMOVED AND REPLACED SEAT TRACK IAW 727 SRM 53-10-5. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 114009. AMERICAN INTERNATIONAL AIRW AYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600251 19980626 00251 NM 1998 6 26 B4MR98054 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM FUSELAGE CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ACCOMPLISHMENT OF AD 93-05-17 S/B 727-53-0086, FOUND X-RAY SHOWS A CRACK INDICATION IN ROW OF FASTENERS ADJACENT TO TOP AFT CORNER OF EYEBROW WINDOW CUTOUT RIGHT SIDE. REPAIRED TOP AFT CORNER OF EYEBROW WINDOW IAW 727 SRM 53-30-3. R EPAIR AT CO-PILOT EYEBROW WINDOW SHOWS FIVE HI-LOK HEADS NO FLUSH ON COUNTERSINK; THREE SMALL HI-LOKS WITH NUTS ONLY SRM REQUIRES COLLARS: 51-30-2 STEP NR 3 AND ONE HI-LOK NUT COMPLETELY LOOSE. REMOVED AND REPLACED FASTENERS IAW BOEING SRM 51-30-2. NON-ROUTINE TASK CARD NUMBERS 114037 AND 114346. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600252 19980626 00252 NM 1998 6 26 B4MR98055 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 1070-1110 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FS 1070 TO FS 1110 LBL 10 SEAT TRACK CORRODED. FOUND TO BE OUT OF LIMITS IAW BOEI NG SRM 727 53-10-1. REMOVED SEAT TRACK IAW SRM 53-10-5. INSTALLED NEW SEAT TRACK IAW BOEING 727 SRM 53-10-5 FIG 7. CO RROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 114040. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J ) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600253 19980626 00253 NM 1998 6 26 B4MR98056 1 19980618 A 5315 FLOORBEAM BOEING 727 727191 1384063 NM BS 1110 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FS 1110 TOP OF FLOORBEAM IN SEVERAL AREAS CORRODED. REPAIRED TOP OF FLOORBEAM AS PER BOEING 727 SRM 53-10-8 PAGE 44 FIG 8. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 114046. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETIO N. 2 L 7 3 4F A3WE 1998062600254 19980626 00254 NM 1998 6 26 B4MR98057 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 1110-1130 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FS 1110 TO 1130 LBL 24 SEAT TRACK CORRODED. FOUND TO BE OUT OF LIMITS IAW B727 SR M 53-10-1. REMOVED AND REPLACED NEW SEAT TRACK IAW B727 SRM 53-10-5, 51-10-2 AND 51-20-12. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 114048. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRC RAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600255 19980626 00255 NM 1998 6 26 B4MR98058 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 680 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT LWR BILGE AREA, AT BS 680, RT SEAT TRACK CORRODED ON TOP SUR FACE. REPAIRED IAW B727 SRM 53-10-5. CORROSION TASK CARD NUMBER C53-113-01. NON-ROUTINE TASK CARD NUMBER 114073. AME RICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600256 19980626 00256 NM 1998 6 26 B4MR98059 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 480-580 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FWD CARGO COMPARTMENT LWR BILGE AREA, FROM BS 480 TO BS 580, LFT SEAT TRACK WITH L IGHT CORROSION ON TOP SURFACE. REMOVED AND REPLACED SEAT TRACK FROM BS 480 TO BS 580 AT ORIGINAL SPLICE LOCATIONS PER B OEING 727 SRM 51-3-2 AND 51-10-1. CORROSION TASK CARD NUMBER C53-113-01. NON-ROUTINE TASK CARD NUMBER 114075. AMERICA N INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600257 19980626 00257 NM 1998 6 26 B4MR98060 1 19980618 A 5313 STRINGER BOEING 727 727191 1384063 NM BS 440 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FS 440 STR 21R, STRINGER SPLICE CORRODED. REMOVED CORROSION IAW SRM 51-10-6. FOU ND OUT OF LIMITS IAW SRM 53-10-1. TREATED AND PRIMED IAW SRM 51-20-12. INSTALLED NEW PART IAW SRM 53-10-3. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 114079. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMP LISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600258 19980626 00258 NM 1998 6 26 B4MR98061 1 19980618 A 5343 TRUNNION BOEING 727 727191 1384063 NM NLG CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF NLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND NOSE LANDING GEAR LT TRUNNION UPPER SUPPORT HAS CORROSION. REMOVED CORROSION IAW B727 SRM 53-40-1 PG 7 STEP 4. FABRICATED OVERSIZE BEARING IAW B727 SRM 53-40-1 PG 7 STEP 8. INSTALLED OVERSIZED BEARING IAW B727 SRM 53-40-1, R/O 504-098. NON-ROUTINE T ASK CARD NUMBER 114102. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600259 19980626 00259 NM 1998 6 26 B4MR98062 1 19980618 A 5343 TRUNNION CAP BOEING 727 727191 1384063 NM NLG CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF NLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND NOSE LANDING GEAR LT TRUNNION LOWER CAP HAS CORROSION. REMOVED CORROSION IAW B727 SRM 53-40-1 PG 7 STEP 4. FABRICATED OVERSIZE BEAR ING IAW B727 SRM 53-40-1 PG 7 STEP 8. INSTALLED LOWER CAP IAW B727 SRM 53-40-1, R/O 504-098. NON-ROUTINE TASK CARD NUM BER 114101. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UP ON COMPLETION. 2 L 7 3 4F A3WE 1998062600260 19980626 00260 NM 1998 6 26 B4MR98063 1 19980618 A 5343 651620510 TRUNNION BOEING 727 727191 1384063 NM MLG CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND RT MLG FWD TRUNNION SUPPORT FITTING CORRODED. REMOVED AND REPLACED RT MLG FWD TRUNNION SUPPORT FITTING IAW B727 OHM 37-10-13/MM 32-11-51. C-CHECK CARD NUMBER C1-63. NON-ROUTINE TASK CARD NUMBER 11 4355. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COM PLETION. 2 L 7 3 4F A3WE 1998062600261 19980626 00261 NM 1998 6 26 B4MR98064 1 19980618 A 5347 SEAT TRACK BOEING 727 727191 1384063 NM BS 580-680 BROKEN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND SCREW HOLE ON SEAT TRACK FLANGE AT STA 670 RBL 24 IS BROKEN OUT. REPLACED SEAT TR ACK AT BS 580 TO BS 680 IAW BOEING 727 SRM 53-10-5. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBE R 114106. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600262 19980626 00262 NM 1998 6 26 B4MR98065 1 19980618 A 5315 FLOORBEAM BOEING 727 727191 1384063 NM BS 312 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND BS 312, BETWEEN LBL 10 AND LBL 30, FLOORBEAM WITH SIGNS OF CORROSION AT LWR AFT FA CE. REMOVED DAMAGED PART AND FABRICATED NEW PARTS AND HEAT TREATED IAW B727 SRM 51-20-2 AND 51-10-3. TREATED AND PRIME D IAW SRM 51-10-2 MM 20-10-22. INSTALLED NEW PARTS IAW B727 SRM 53-10-8 AND SRM 51-30-2. CORROSION TASK CARD NUMBER C5 3-224-01. NON-ROUTINE TASK CARD NUMBER 114108. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRA FT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600263 19980626 00263 NM 1998 6 26 B4MR98066 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 520-540 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FUSELAGE EXTERIOR BETWEEN BS 520 AND BS 540, CORROSION AT LAP JOINT OVER S-4L AREA . REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REPAIRED SKIN IAW B727 SRM 53-30-3. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 114272. AMERICAN INTERNATIONAL AIRWAYS I NC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600264 19980626 00264 NM 1998 6 26 B4MR98067 1 19980618 A 5315 FLOORBEAM BOEING 727 727191 1384063 NM BS 760 CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FLOORBEAM STA 760 RBL 44 HAS 2 INCH CRACK ON LOWER LEG. REPAIRED FLOORBEAM IAW AI A DRAWING 2730 AND EDR B2-05617. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 114273. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600265 19980626 00265 NM 1998 6 26 B4MR98068 1 19980618 A 3211 106054580 TRUNNION BOEING 727 727191 1384063 NM RT MLG WORN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF RT MLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND RT MLG FWD TRUNNION BEARING WORN. REMOVED RT MLG FWD TRUNNION BEARING IAW B727 MM 32-11-51. REPLACED RT MLG FWD TRUNNION BEARING IAW B727 OHM 32-10-13, R/O 504-100. NON-ROUTINE TASK CARD NUMBER 114052. SPRING PIN (P/N NAS 561P5-30), FITTING ASSY 1-74902-2. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPO N COMPLETION. 2 L 7 3 4F A3WE 1998062600266 19980626 00266 NM 1998 6 26 B4MR98069 1 19980618 A 3211 10618497 BEARING BOEING 727 727191 1384063 NM LT MLG WORN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF LT MLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND LT MLG AFT TRUNNION BEARING WORN AND CORRODED. REMOVED AND REPLACED LT MLG AFT TRUNNION BEARING IAW BOEING 727 MM 32-11-0. R/O 5 04-099. NON-ROUTINE TASK CARD NUMBER 114051. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600267 19980626 00267 NM 1998 6 26 B4MR98070 1 19980618 A 3211 65821531 BUSHING BOEING 727 727191 1384063 NM LT MLG TRUNNION CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF LT MLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND LT MLG AFT TRUNNION BEARING BUSHING CORRODED. REMOVED AND REPLACED LT MLG AFT TRUNNION BEARING BUSHING IAW BOEING SOPM 20-50-03. R/O 504-099. NON-ROUTINE TASK CARD NUMBER 114053. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AI RCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600268 19980626 00268 NM 1998 6 26 B4MR98071 1 19980618 A 3211 1560545138 BEARING BOEING 727 727191 1384063 NM LT MLG WORN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF LT MLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND LT MLG SID E STRUT FWD BEARING WORN. REMOVED AND REPLACED LT MLG SIDE STRUT FWD BEARING IAW 727 MM 32-11-41. REF W/O 504099 KB99 FOR TORQUES AND OPS CHECK. R/O 504-099. NON-ROUTINE TASK CARD NUMBER 114067. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR 567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600269 19980626 00269 NM 1998 6 26 B4MR98072 1 19980618 A 3211 1060545138 BEARING BOEING 727 727191 1384063 NM RT MLG FROZEN A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF RT MLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND RT MLG SID E BRACE FWD BEARING FROZEN. REPLACED BEARING IAW 727 MM 32-11-41. OPERATIONAL CHECK GOOD ON GEAR SWING IAW BOEING MM 3 2-32-0. R/O 504-100. NON-ROUTINE TASK CARD NUMBER 114061 AND 114340. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) AC COMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600270 19980626 00270 NM 1998 6 26 B4MR98073 1 19980618 A 5320 FITTING BOEING 727 727191 1384063 NM BS 360 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND FORWARD PRODUCTION SPLICE FITTING AT BS 360, S26R IS CORRODED. REMOVED AND REP LACED SPLICE FITTING IAW B727 SRM 51-30-2 AND EDR NR B2-05633. C-CHECK CARD NUMBER 1C-134. NON-ROUTINE TASK CARD NUMBE R 114559. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600271 19980626 00271 NM 1998 6 26 B4MR98074 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 1080 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ACCOMPLISHMENT OF AD 90-21-10 S/B 727-53-0109, FOUND AFTER LFEC INSPECTION OF BS 1080 (SB 727-53-0109) APPROX 2.7 5 AREA OF SKIN IN BETWEEN S6L-S7L WAS NOTED A MATERIAL LOSS OF GREATER THAN 10 PERCENT. REPAIRED SKIN IAW B727 DRAWING NR 69-62161 FIG 11 (SB 727-53-0109). NON-ROUTINE TASK CARD NUMBER 114565. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J ) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600272 19980626 00272 NM 1998 6 26 B4MR98075 1 19980618 A 5313 STRINGER BOEING 727 727191 1384063 NM BS 1108 DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND STRINGER 6 LEFT AT BS 1108 IS DAMAGED. REPAIRED IAW B727 SRM 53-10-3. C-CHECK CARD NUMBER 5C-12. NON-ROUTINE TASK CARD NUMBER 114563. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING C OOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600273 19980626 00273 NM 1998 6 26 B4MR98076 1 19980618 A 5320 CLIP BOEING 727 727191 1384063 NM BS 480 DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND FRAME CLIP TO STRINGER 9L IS DAMAGED AT BS 480. REPLACED CLIP IAW B727 SRM 51- 30-2 AND 51-10-1. C-CHECK CARD NUMBER 5C-12. NON-ROUTINE TASK CARD NUMBER 114556. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600274 19980626 00274 NM 1998 6 26 B4MR98077 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 870 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND LOWER EXTERNAL FUSELAGE SKIN AT STA 870 RBL 44 TO RBL 54 CENTER FUEL TANK HAS A BU LGE AREA AND MISSING 2 RIVET HEAD AREAS. PERFORMED THICKNESS CHECK, VARIOUS THICKNESSES, AREA MAPPED C/W HFEC INSPECTIO N IN REPAIR AREA IAW BOEING REC. NO DEFECTS NOTED. REPAIRED AREA IAW AIA EA NR B2-57-018. CORROSION TASK CARD NUMBER C53-132-01. NON-ROUTINE TASK CARD NUMBER 114684. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRC RAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600275 19980626 00275 NM 1998 6 26 B4MR98078 1 19980618 A 5320 WINDOW FRAME BOEING 727 727191 1384063 NM BS 910-930 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND RT CABIN WINDOW NR 21 FRAME IN BETWEEN BS 910 TO BS 930 HAS CORROSION ON WINDOW FLANGE INTERNAL. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 56-20-1. REPAIRED WI NDOW FRAME IAW B727 SRM 56-20-3. C-CHECK CARD NUMBER 1C-133. NON-ROUTINE TASK CARD NUMBER 114693. AMERICAN INTERNATIO NAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600276 19980626 00276 NM 1998 6 26 B4MR98079 1 19980618 A 5320 WINDOWFRAME BOEING 727 727191 1384063 NM BS 930-950 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 RT CABIN WINDOW NR 22 FRAME IN BETWEEN BS 930 TO BS 950 HAS CORROSION ON WINDOW FLANGE INTERNAL. REMOVED CORROSION FOUN D TO BE OUT OF LIMITS IAW B727 SRM 56-20-1. REPLACED WINDOW FRAME IAW B727 51-30-2 AND 51-10-1 SEALED IAW B727 SRM 51-2 0-4. C-CHECK CARD NUMBER 1C-133. NON-ROUTINE TASK CARD NUMBER 114694. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) A CCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600277 19980626 00277 NM 1998 6 26 B4MR98080 1 19980618 A 5343 TRUNNION CAP BOEING 727 727191 1384063 NM NLG CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF NLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND NOSE LANDING GEAR RT TRUNNION LOWER CAP HAS CORROSION. REMOVED CORROSION IAW B727 SRM 53-40-1 PG 7 STEP 4. FABRICATED OVERSIZE BEAR ING IAW B727 SRM 53-40-1 PG 7 STEP 8. INSTALLED LOWER CAP IAW B727 SRM 53-40-1. R/O 504-098. NON-ROUTINE TASK CARD NU MBER 114726. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE U PON COMPLETION. 2 L 7 3 4F A3WE 1998062600278 19980626 00278 NM 1998 6 26 B4MR98081 1 19980618 A 5343 BEARING BOEING 727 727191 1384063 NM NLG TRUNNION CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING REMOVAL AND REPLACEMENT OF NLG PER CUSTOMER REQUEST, HARD TIME ITEM REFER TO CAL727 OPS SPEC, FOUND NOSE LANDING GEAR RT TRUNNION UPPER SUPPORT HAS CORROSION. REMOVED CORROSION IAW B727 SRM 53-40-1 PG 7 STEP 4. FABRICATED OVERSIZE BEARING IAW B727 SRM 53-40-1 PG 7 STEP 8. INSTALLED OVERSIZED BEARING IAW B727 SRM 53-40-1. R/O 504-098. NON-ROUTINE TASK CARD NUMBER 114727. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FO R PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600279 19980626 00279 NM 1998 6 26 B4MR98082 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS478 S4L CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ACCOMPLISHMENT OF AD 90-26-09 / SB727-53-0084, FOUND INTERNAL SKIN AT BS 478 ABOVE S4L HAS CORROSION. REMOVED CO RROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. ULTRASONIC THICKNESS CHECK MINIMUM NOMIN AL .034 TO .036. HFEC INSP C/W NO DEFECTS NOTED. REPAIRED PER PART III OF BOEING S/B 727-53-0084 REV 4 IAW BOEING DRAW ING 69-62161 SHEET 3. NON-ROUTINE TASK CARD NUMBERS 114557 AND 114796. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) A CCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600280 19980626 00280 NM 1998 6 26 B4MR98083 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS480 S3L CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ACCOMPLISHMENT OF AD 90-26-09 / SB 727-53-0084, FOUND INTERNAL SKIN CIRCUMFERENTIAL JOINT SPLICE AT BS 480 HAS CO RROSION UNDER SEALANT FOUR INCHES ABOVE S3L. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE WITHIN LIMITS IAW B72 7 SRM 53-10-1. ULTRASONIC THICKNESS CHECK MINIMUM NOMINAL THICKNESS .036. HFEC INSP C/W NO DEFECTS NOTED. PERFORMED P ART IV MODIFICATION (OVERSIZE UNIVERSAL FAST INSTALL) IAW BOEING S/B 727-53-0084 REV 4. NON-ROUTINE TASK CARD NUMBERS 1 14560 AND 114795. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCH ASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600281 19980626 00281 NM 1998 6 26 B4MR98084 1 19980618 A 5720 MOUNT BOEING 727 727191 1384063 NM RT WING DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND RT WING NR 5 KRUEGER FLAP CENTER HINGE MOUNT DAMAGED. REPAIRED CENTER HINGE MO UNT IAW AIA EDR NR B2-05608 REF: AIA SKETCH E/2726. C-CHECK CARD NUMBER 1C-57. NON-ROUTINE TASK CARD NUMBER 115171. A MERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600282 19980626 00282 NM 1998 6 26 B4MR98085 1 19980618 A 5320 WEB BOEING 727 727191 1384063 NM TAIL SKID AREA CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND TAIL SKID AREA TOP WEB IS CRACKED. REPAIRED WEB IAW B727 SRM 51-40-2 AND 51-30 -2. TREATED AND PRIMED IAW B727 MM 51-20-12. C-CHECK CARD NUMBER 1C-109. NON-ROUTINE TASK CARD NUMBER 114376. AMERIC AN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600283 19980626 00283 NM 1998 6 26 B4MR98086 1 19980618 A 5270 FITTING BOEING 727 727191 1384063 NM TAIL SKID CRACKED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND TAIL SKID MAIN MOUNT FITTINGS (2) ARE CRACKED. REMOVED AND REPLACED SKID MOUNT FITTINGS IAW 51-30-2 AND 51-10-1. R/S MAIN SKID FITTING=65-29943-5. L/S MAIN SKID FITTING 65-29943-6. C-CHECK CARD N UMBER 1C-109. NON-ROUTINE TASK CARD NUMBER 114373. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AI RCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600284 19980626 00284 NM 1998 6 26 B4MR98087 1 19980618 A 5230 SKIN BOEING 727 727191 1384063 NM CARGO DOOR DAMAGED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE C-CHECK INSPECTION, FOUND C-2 DOOR FWD AND AFT EDGE OF SKIN DAMAGED. REMOVED AND REPLACED C-2 DOOR IAW B OEING 727 MM 52-31-0. C-CHECK CARD NUMBER 1C-132. NON-ROUTINE TASK CARD NUMBERS 113702, 113703, AND 113934. AMERICAN INTERNATIONAL AIRWAYS INC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600285 19980626 00285 NM 1998 6 26 B4MR98088 1 19980618 A 5330 SKIN BOEING 727 727191 1384063 NM BS 440 CORRODED A B4MR K NONE O OTHER IN INSP/MAINT 1 GL 23 504MG 19395 DURING ROUTINE CPCP INSPECTION, FOUND FS 440 STR 26R, CORROSION AROUND RIVETS. REMOVED CORROSION IAW B727 SRM 51-10-6. FOUND TO BE OUT OF LIMITS IAW 727 SRM 53-10-1. REPAIRED STRINGER IAW B727 SRM 53-10-3. INSTALLED REPAIR IAW B727 SRM 53-30-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 114217. AMERICAN INTERNATIONAL AIRWAYS I NC (B4MR567J) ACCOMPLISHING COOK AIRCRAFT LEASING WORKSCOPE FOR PURCHASE UPON COMPLETION. 2 L 7 3 4F A3WE 1998062600286 19980626 00286 1998 6 26 TC8A98033 4 19980617 A 3420 2588533901 AMPLIFIER DOUG DC8 DC8F55 3021928 WP COCKPIT FAILED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 182SK 934 45817 TRIP NR 2003, RED HEADING FLAG ON CAPTAINS HSI AND RED BOW TIE PRIOR TO TAKEOFF. REMOVED AND REPLACED INSTRUMENT AMP LO ANER FROM ABX. TRANSFERRED TO C/O LIST NR 00377 IAW M/M 34-7-6. 2 L 7 4 4F 4A25 1998062600287 19980626 00287 1998 6 26 TC8A98034 4 19980617 A 3420 AMPLIFIER DOUG DC8 DC8F55 3021928 WP NR 1 TRIPPED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 182SK 45817 TRIP NR 2003, LEFT ATTITUDE FLAG CAME ON ON TAKEOFF. ABORTED TAKEOFF. RERACKED INSTRUMENT AMP NR 1, OPS CHECKS GOOD IA W MM 34-7-6. 2 L 7 4 4F 4A25 1998062600288 19980626 00288 1998 6 26 TC8A98035 4 19980617 A 3422 25883025 GYRO DOUG DC8 DC8F55 3021928 WP E/E COMPT REPLACED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 182SK 2569 45817 TRIP NR 2003, NR 1 COMPASS FLAG CAME ON DURING TAKEOFF. REMOVED NR 2 DIRECTIONAL GYRO, OPS CHECKS GOOD IAW MM 34-5-4. 2 L 7 4 4F 4A25 1998062600294 19980626 00294 EA 1998 6 26 98ZZZX2245 2 19980423 A 7261 310732401 PUMP HOUSING BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RT ENGINE SCAV ERODED A AOBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 11 5UN 6770 3725 PT186 BB697 PCE81665 OIL WAS FOUND ON COWL. INVESTIGATION FOUND THE AFT EXTERNAL SCAVENGE PUMP HOUSING WAS LEAKING OIL. PUMP WAS DISASSEMBL ED AND FOUND CAVITATION EROSION WHICH CAUSED A PIN HOLE THROUGH THE HOUSING. 1 L 7 2 4T 4 T A24CE E4EA 1998062600303 19980626 00303 NM 1998 6 26 MALA976142 1 19980616 A 7797 82455015005 WIRE HARNESS DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 832MA 341 DURING CLIMBOUT PASSING 11,000 FT, NR 1 PROP RPM WENT TO 0 THEN STARTED TO FLUCUATE. AIRCRAFT RETURNED TO MSP WITHOUT I NCIDENT. MAINTENANCE REPLACED HARNESS ON NR 1 ENGINE, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998062600304 19980626 00304 EU 1998 6 26 MALA976143 1 19980608 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN MISWIRED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 441XJ 441 DURING WALKAROUND, FOUND BACK HALF OF CABIN AND FLOOR TRACK EMERGENCY LIGHT INOP. MAINTENANCE FOUND PINS WIRED BACKWARD S AT PLUG 101VU P2, CORRECTED WIRING ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998062600305 19980626 00305 EU 1998 6 26 MALA976144 1 19980616 A 2611 2LA00510900 LIGHT SAAB SF340 SF340A 7850100 EU CARGO COMPT SHORTED A MALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 98XJ 098 ON TAKEOFF ROLL, CARGO SMOKE LIGHT ILLUMINATED. ABORTED TAKEOFF. MAINTENANCE REPLACED AFT CARGO LIGHT ASSEMBLY AND SMO KE DETECTOR (P/N 72-111211-00), OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998062600306 19980626 00306 EU 1998 6 26 MALA976145 1 19980617 A 3350 1011513 LIGHT BAC 146 AVRO146RJ85A 1500097 EU CABIN BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 505XJ E2313 DURING INSPECTION, EMERGENCY LIGHT SOCKET BROKE AT ROW 2 ON THE OVERHEAD PANEL. MAINTENANCE REPLACED EMERGENCY LIGHT AS SEMBLY AT ROW 2, ALL CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998062600307 19980626 00307 EU 1998 6 26 MALA976146 1 19980607 A 3350 43187 CONTROL PANEL SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 433XJ 433 DURING INSPECTION, FLIGHT ATTENDANT EMERGENCY ARM LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED FLIGHT ATTENDANT CON TROL PANEL, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998062600308 19980626 00308 EU 1998 6 26 MALA976147 1 19980612 A 3230 CONTROL UNIT SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA K NONE J WARNING INDICATION LD LANDING 1 GL 15 421XJ 421 ON LANDING, LANDING GEAR WOULD NOT EXTEND, CB F7 POPPED, RESET AND GEAR CAME DOWN. MAINTENANCE JACKED AIRCRAFT AND SWUN G GEAR, ALL CHECKS GOOD. AS A PRECAUTIONARY MEASURE MAINTENANCE REPLACED THE LANDING GEAR CONTROL UNIT PN D494-12-001. ALL WORK DONE IAW SF340 MM 32-31-05. 2 L 7 2 4T RT A52EU 1998062600309 19980626 00309 1998 6 26 MALA976148 4 19980605 A 3425 AHRS SAAB SF340 SF340A 7850100 EU LT COCKPIT MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 98XJ 098 AFTER TAKEOFF, THE CAPTAIN RECEIVED A YELLOW HEADING FLAG ON EFIS TUBE AND THEY WHERE SPLIT ABOUT 15 DEGREES. AIRCRAFT RETURN TO DTW. MAINTENANCE INSPECTED AND RESET THE AHRS SYSTEM, OPS CHECKED AND FOUND SYSTEM TO BE GOOD. 2 L 7 2 4T RT A52EU 1998062600310 19980626 00310 NE 1998 6 26 9809561141 2 19980616 A 7310 FUEL LINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 ENGINE CRACKED A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 141US 46750 86121 WHILE AT CRUISE FL330, THE NR 2 ENGINE COMPRESSOR STALLED. ALL NR 2 PARAMETERS ROLLED BACK TO FLIGHT IDLE. THE ENGINE DID NOT RESPOND TO POWER LEVER INPUTS AND WAS SHUT DOWN. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. THE CREW DID ATTEMPT ONE RESTART AT FL290 WHICH WAS UNSUCCESSFUL. MAINTENANCE FOUND A FUEL LINE FROM THE EVC TO THE STATOR VANE ACTUATOR CRACKED. 2 L 7 3 4F 4 F A22WE E20EA 1998062600311 19980626 00311 SO 1998 6 26 COMA9810140 1 19980621 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 243CA 120212 EMERGENCY EXIT SIGN AT 5A IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998062600312 19980626 00312 EA 1998 6 26 COMA9860150 1 19980614 A 2760 60010300639 BUSHING CNDAIR CL600 CL6002B19 EA RT SPOILER MISSING A COMA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 976CA 7151 C-CHECK INSPECTION, RIGHT HAND WING INBOARD FLIGHT SPOILER, PCU HINGE BUSHING IS MISSING. REPLACED MISSING BUSHING. 2 L 7 2 4F RT A21EA 1998062600313 19980626 00313 EA 1998 6 26 COMA9860151 1 19980613 A 5320 601R3520537 SUPPORT CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 DURING C-CHECK, FOUND CARGO DOOR STEP PLATE SUPPORT BROKEN. REPLACED CARGO DOOR STEP PLATE SUPPORT. 2 L 7 2 4F RT A21EA 1998062600314 19980626 00314 EA 1998 6 26 COMA9860152 1 19980615 A 5240 601R3892423 PLUNGER CNDAIR CL600 CL6002B19 EA SERVICE DOOR BENT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 DURING C-CHECK, FOUND SERVICE DOOR PLUNGER BENT. REPLACED PLUNGER. 2 L 7 2 4F RT A21EA 1998062600315 19980626 00315 EA 1998 6 26 COMA9860153 1 19980614 A 5210 600380903 BOLT CNDAIR CL600 CL6002B19 EA PAX DOOR BENT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 936CA 7043 DURING C-CHECK, FOUND PAX DOOR FORWARD STOP BOLT ASSY BENT. REPLACED STOP BOLT. 2 L 7 2 4F RT A21EA 1998062600316 19980626 00316 EA 1998 6 26 COMA9860154 1 19980613 A 4980 1079900004 CLAMP CNDAIR CL600 CL6002B19 EA APU DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 7151 C-CHECK TASK 002-49-310-102, APU EXHAUST FINGER CLAMP HAS HOLES CHAFED THROUGH. REPLACED CLAMP. 2 L 7 2 4F RT A21EA 1998062600317 19980626 00317 EA 1998 6 26 COMA9860155 1 19980613 A 4980 601R9720317 BLANKETS CNDAIR CL600 CL6002B19 EA APU EXHAUST CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 7151 C-CHECK TASK 002-49-310-102, APU EXHAUST BLANKETS ARE CRACKED. REPLACED EXHAUST BLANKETS. 2 L 7 2 4F RT A21EA 1998062600318 19980626 00318 EA 1998 6 26 COMA9860156 1 19980613 A 4980 601R9720913 SUPPORT CNDAIR CL600 CL6002B19 EA APU DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 7151 C-CHECK TASK 002-49-310-102, APU EXHAUST DUCT SUPPORT ASSY CHAFED. REPLACED SUPPORT. 2 L 7 2 4F RT A21EA 1998062600319 19980626 00319 EA 1998 6 26 COMA9860157 1 19980613 A 4980 601R972011 DUCT CNDAIR CL600 CL6002B19 EA APU EXHAUST BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 7151 C-CHECK TASK 002-49-310-102, APU EXHAUST DUCT HAS BROKEN RETAINING TABS. REPLACED EXHAUST DUCT. 2 L 7 2 4F RT A21EA 1998062600320 19980626 00320 NM 1998 6 26 UPS98227005 1 19980622 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, RIGHT SIDE FWD OVERWING EMER LIGHT DOES NOT TEST. REMOVED AND REPLACED EMER LIGHT BATTERY PACK, OP 'S CHECK GOOD. 2 L 7 3 4F A3WE 1998062600321 19980626 00321 WP 1998 6 26 UPS98826976 1 19980606 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E SKIN ON BOTTOM, ABOVE THE NR 3 PYLON HAS A CRACKED REPAIR DOUBLER. REMOVED EXISTING REPA IR DOUBLER, FABRICATED AND INSTALLED A NEW REPAIR DOUBLER PER SRM 51-1-20D AND 57-2-0. 2 L 7 4 4F RT 4A25 1998062600322 19980626 00322 WP 1998 6 26 UPS98826977 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 810.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PE R SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600323 19980626 00323 WP 1998 6 26 UPS98826978 1 19980606 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-C, RT WING L/E RIB AT STA XFS 616.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED P ER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600324 19980626 00324 WP 1998 6 26 UPS98826979 1 19980602 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 610.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600325 19980626 00325 WP 1998 6 26 UPS98826980 1 19980602 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 616.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED AND REPAIRED PER SRM 5 7-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600326 19980626 00326 WP 1998 6 26 UPS98826981 1 19980602 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 641.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 641.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600327 19980626 00327 WP 1998 6 26 UPS98826982 1 19980602 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 828.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 828.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600328 19980626 00328 WP 1998 6 26 UPS98826983 1 19980603 A 5320 4758514509 FITTING DOUG DC8 DC871F 302199D WP BS 1238 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1238 ABOVE LONG 33R, THE TIE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED AND INSTALLE D PER DWG 4758514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600329 19980626 00329 WP 1998 6 26 UPS98826984 1 19980603 A 5320 37584952 FITTING DOUG DC8 DC871F 302199D WP BS 1239 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1239 ABOVE LONG 35R, THE TIE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED AND INSTALLE D PER DWG 3758495 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600330 19980626 00330 WP 1998 6 26 UPS98826985 1 19980603 A 5320 37584982 FITTING DOUG DC8 DC871F 302199D WP BS 1241 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1241 ABOVE LONG 35R, THE TIE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED AND INSTALLE D PER DWG 3758498 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600331 19980626 00331 WP 1998 6 26 UPS98826986 1 19980603 A 5310 97585074 GUSSET DOUG DC8 DC871F 302199D WP BS 1100 CORRODED A A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FRAME TO INTERCOSTAL GUSSET AT STA 1100 AT LONG 35L HAS MODERATE CORROSION. REMOVED GUSSET, FABRICAT ED AND INSTALLED PER DWG 9758507 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600332 19980626 00332 WP 1998 6 26 UPS98826987 1 19980603 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E LWR SKIN AT STA XFS 304.0 IS CRACKED JUST FWD OF THE SPAR. STOP DRILLED CRACK AND REPAIR ED PER EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 1998062600333 19980626 00333 WP 1998 6 26 UPS98826988 1 19980603 A 5720 97532938 ANGLE DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT INBD SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED VERTICAL ANG LE PER DWG 9753293 AND SRM 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 1998062600334 19980626 00334 WP 1998 6 26 UPS98826989 1 19980603 A 5720 975329424 CLIP DOUG DC8 DC871F 302199D WP WS 262 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E ABOVE THE NR 3 PYLON, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED AND INSTAL LED CLIP PER DWG 9753294 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998062600335 19980626 00335 WP 1998 6 26 UPS98826990 1 19980604 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1520-1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1520 TO 1540, LONG 34L HAS HEAVY CORROSION. CUT OUT DAMAGED LONGERON AND REPAIRED PER SRM 53-2-2 FIG 11. 2 L 7 4 4F RT 4A25 1998062600336 19980626 00336 WP 1998 6 26 UPS98826991 1 19980603 A 5320 3755854502 FITTING DOUG DC8 DC871F 302199D WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1180 AT LONG 27L, THE DOOR OPEN STOP/FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING PER DWG 3755854 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600337 19980626 00337 WP 1998 6 26 UPS98826993 1 19980603 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 90 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING T/E UPPER SKIN AT THE AUX SPAR, 16 O/B OF THE MLG TRUNNION IS CRACKED. CUT OUT DAMAGE AND RE PAIRED PER EO DC8-5720-7767. 2 L 7 4 4F RT 4A25 1998062600338 19980626 00338 WP 1998 6 26 UPS98826994 1 19980604 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 338 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LT WING L/E UPPER SKIN AT STA XFS 338 IS CRACKED. CUT OUT DAMAGE AND REPAIRED PER SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998062600339 19980626 00339 WP 1998 6 26 UPS98826995 1 19980604 A 5720 576989113 DOUBLER DOUG DC8 DC871F 302199D WP WS 7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LT WING L/E LWR SKIN INTERNAL DOUBLER AT STA XOLDI 7 IS CRACKED. REMOVED DOUBLER, FABRICATED AND INS TALLED PER DWG 5769891 AND SRM 51-1-20D, 51-1-21. 2 L 7 4 4F RT 4A25 1998062600340 19980626 00340 WP 1998 6 26 UPS98826996 1 19980604 A 5320 46409291 DOUBLER DOUG DC8 DC871F 302199D WP BS 25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 25 AT LONG 31R, AFTER CORROSION REMOVAL THE FINGER DOUBLER IS OUT OF LIMITS. REMOVED DAMAGED FING ER DOUBLER, FABRICATED AND INSTALLED PER DWG 4640929 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998062600341 19980626 00341 WP 1998 6 26 UPS98826997 1 19980605 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 227.335 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D RT WING L/E RIB AT STA XS 227.335 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PE R SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600342 19980626 00342 WP 1998 6 26 UPS98826998 1 19980605 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 0 .7095 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XILD 0.7095 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PER SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600343 19980626 00343 WP 1998 6 26 UPS98826999 1 19980607 A 5320 37502571N SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 440 TO 460, AT LONG 31L, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 1998062600344 19980626 00344 WP 1998 6 26 UPS98827000 1 19980607 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 466.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, RT WING L/E RIB AT STA XFS 466.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED PE R SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998062600345 19980626 00345 WP 1998 6 26 UPS98827001 1 19980608 A 5320 46413241N SPLICE DOUG DC8 DC871F 302199D WP BS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1690, THE LONG 26R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED LONG SPLICE FITTING. 2 L 7 4 4F RT 4A25 1998062600346 19980626 00346 WP 1998 6 26 UPS98827002 1 19980622 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED EMER BATT PACK, OP'S NORMAL (S/N 1125) OFF, (S/N 321) ON, (P/N 60-122 3-5) ON, (P/N 5708458-503) OFF. 2 L 7 4 4F RT 4A25 1998062600347 19980626 00347 WP 1998 6 26 UPS98827003 1 19980622 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED BATT PACK, OP'S CHECK OK. (S/N 335) ON, (S/N 255) OFF. 2 L 7 4 4F RT 4A25 1998062600348 19980626 00348 WP 1998 6 26 UPS98827004 1 19980622 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 750UP 45950 INSPECTION TYPE-N/A, EEL COCKPIT ENTRY AND DOME DID NOT WORK. REPLACED EMERGENCY EXIT LIGHT BATT PACK PER MM 33-50-01, OP'S CHECK NORMAL. 2 L 7 4 4F RT 4A25 1998062600349 19980626 00349 NM 1998 6 26 QXEA9800802 1 19980522 A 5753 CARRIAGE DHAV DHC8 DHC8102 2809003 NM LT NR 5 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 CHAFE MARKS ON LEFTHAND NR 5 CARRIAGE CAUSED BY FAIL-SAFE STRAPS. REPAIRED IAW HORIZON AIR EA 9-57-364. 2 H 7 2 4T RT A13NM 1998062600350 19980626 00350 NM 1998 6 26 QXEA9800803 1 19980522 A 5753 CARRIAGE DHAV DHC8 DHC8102 2809003 NM RT NR 5 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 CHAFE MARKS ON RIGHTHAND NR 5 CARRIAGE CAUSED BY FAIL-SAFE STRAPS. REPAIRED IAW HORIZON AIR EA 9-57-364. 2 H 7 2 4T RT A13NM 1998062600351 19980626 00351 NM 1998 6 26 QXEA9800804 1 19980525 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 FORWARD RIGHTHAND CLOSING ANGLE FOUND CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1998062600352 19980626 00352 NM 1998 6 26 QXEA9800805 1 19980525 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 AFT LEFTHAND CLOSING ANGLE FOUND CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00, PAGE 6. 2 H 7 2 4T RT A13NM 1998062600353 19980626 00353 NM 1998 6 26 QXEA9800806 1 19980525 A 5320 ANGLE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 AFT RIGHTHAND CLOSING ANGLE FOUND CRACKED. REPAIRED IAW DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1998062600354 19980626 00354 NM 1998 6 26 QXEA9800807 1 19980527 A 5730 SKIN DHAV DHC8 DHC8102 2809003 NM WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 NR 1 AUX PUMP ACCESS CUTOUT HAS DAMAGE TO LOWER SURFACE OF WING. REPAIRED IAW HORIZON AIR EA 9-57-362. 2 H 7 2 4T RT A13NM 1998062600355 19980626 00355 NM 1998 6 26 QXEA9800808 1 19980527 A 5730 SKIN DHAV DHC8 DHC8102 2809003 NM WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 NR 2 AUX PUMP ACCESS CUTOUT HAS FRETTING CORROSION DAMAGE ON UNDERSIDE OF WING. REPAIRED IAW HORIZON AIR EO 9-57-362. 2 H 7 2 4T RT A13NM 1998062600356 19980626 00356 NM 1998 6 26 QXEA9800809 1 19980521 A 5751 SKIN DHAV DHC8 DHC8102 2809003 NM LT AILERON DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 DAMAGED SKIN, TRAILING EDGE OF LEFTHAND AILERON AT OUTBOARD HINGE OF SPRING TAB. REPAIRED IAW HORIZON AIR EA 9-27-84. 2 H 7 2 4T RT A13NM 1998062600357 19980626 00357 NM 1998 6 26 QXEA9800810 1 19980526 A 5720 FITTING DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 NR 2 ENGINE INBOARD FRONT SPAR SUPPORT FITTING HAS CHAFING DAMAGE. REPAIRED IAW CONAIR EO 1998 AND HORIZON AIR EA 9-57- 365. 2 H 7 2 4T RT A13NM 1998062600358 19980626 00358 NM 1998 6 26 QXEA9800811 1 19980601 A 5400 HEATSHIELD DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 NR 1 ENGINE NACELLE HEATSHIELD ASSEMBLY INBOARD SIDE HAS HOLE WORN THROUGH APPROXIMATELY STATION 228.0. REPAIRED IAW HO RIZON AIR EA 9-54-160 AND CONAIR EO 1995. 2 H 7 2 4T RT A13NM 1998062600359 19980626 00359 NM 1998 6 26 QXEA9800812 1 19980527 A 5531 SPAR DHAV DHC8 DHC8102 2809003 NM VERT STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 VERTICAL STABILIZER AFT SPAR UPPER RADIUS ROD FITTING LOWER LUG INSIDE FACE GOUGED. REPAIRED IAW DHC 51-20-00, 51-20-16 AND 51-20-26. 2 H 7 2 4T RT A13NM 1998062600360 19980626 00360 NM 1998 6 26 QXEA9800813 1 19980601 A 2722 85540100007 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER ACTUATOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 FORE RUDDER LOWER CENTER HINGE ASSEMBLY, BEARING BORE FOR RUDDER ACTUATOR FOUND BEYOND LIMITS. REPLACED FITTING ASSEMBL Y IAW DASH 8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1998062600361 19980626 00361 NM 1998 6 26 QXEA9800814 1 19980522 A 5542 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 TRAILING RUDDER RIGHTHAND SIDE 2ND RIB FROM TOP SKIN CRACKED IN THREE SPOTS AROUND RIVETS. REPAIRED IAW DASH 8 SRM SECT ION 55-40-28 PAGE 3, FIGURE 3. 2 H 7 2 4T RT A13NM 1998062600362 19980626 00362 NM 1998 6 26 QXEA9800815 1 19980522 A 5540 85545002011 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 TRAILING RUDDER UPPER RADIUS ROD HINGE FITTING ASSEMBLY GOUGED BEYOND LIMITS. REPLACED UPPER HINGE FITTING ASSEMBLY IAW DHC8 SRM 55-40-00. 2 H 7 2 4T RT A13NM 1998062600363 19980626 00363 NM 1998 6 26 QXEA9800816 1 19980525 A 5522 SKIN DHAV DHC8 DHC8102 2809003 NM RT ELEVATOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 RIGHTHAND ELEVATOR BALANCE HORN EXTENSION UPPER SKIN RIVETS LOOSE. REPLACED RIGHTHAND ELEVATOR HORN EXTENSION UPPER SKI N IAW DASH 8 SRM 55-20-48, PAGE 2 FIGURE 2. 2 H 7 2 4T RT A13NM 1998062600364 19980626 00364 NM 1998 6 26 QXEA9800817 1 19980521 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM CARGO DOORWAY GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 GOUGE AT FORWARD EDGE OF CARGO DOOR CUTOUT AT STRINGER 18. REPAIRED IAW HORIZON EA 9-53-388. 2 H 7 2 4T RT A13NM 1998062600365 19980626 00365 NM 1998 6 26 QXEA9800818 1 19980522 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 551 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 DENT AT STRINGER 27 RIGHTHAND AND FUSELAGE STATION 551.00. REPAIRED IAW DHC -8 RD 8-53-2181, PARAGRAPH 2, PAGE 3. 2 H 7 2 4T RT A13NM 1998062600366 19980626 00366 NM 1998 6 26 QXEA9800819 1 19980527 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 771.803 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 820PH 63 SMALL DENT IN SKIN FORWARD OF STATION X 771.803 ABOVE STRINGER 4P. REPAIRED IAW DASH-8 GENERIC STRUCTURAL REPAIR SCHEME S VOLUME 1 RD 8-53-2181. 2 H 7 2 4T RT A13NM 1998062600367 19980626 00367 NM 1998 6 26 QXEA9800820 1 19980618 A 3350 10005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 828PH 6314 535 287 COCKPIT OVERHEAD EMERGENCY LIGHT DEAD. REPLACED COCKPIT OVERHEAD PORTABLE EMERGENCY LIGHT, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998062600368 19980626 00368 WP 1998 6 26 98FDEA00407 1 19980429 A 5730 SKIN DOUG DC10 DC1010 3022110 WP CENTER WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 CENTER WING TAPERED FWD LWR SKIN (P/N APB 7002-1) HAS CORROSION AT STRINGERS 44 AND 45 BETWEEN XCW STATIONS 4.0 TO 14.5. MAJOR REPAIR PERFORMED IAW EA 8-5734-38427. REMOVED FASTENERS ADJACENT TO CORROSION AND INSPECTED HOLES PER SRM 57-20 -00. REMOVED CORROSION AND CHECKED VALUES PER SRM 57-20-00, FOUND OUT OF LIMITS. INSTALLED OVERSIZED FASTENERS PER SRM 51-31-00 AND COMPLETED REWORK PER SRM 57-20-00, FIGURE 8, SHEET 1. (13 JUNE 1998) 2 L 7 3 4F A22WE 1998062600369 19980626 00369 WP 1998 6 26 98FDEA00408 1 19980605 A 5320 CHANNEL DOUG DC10 DC1010 3022110 WP CARGO COMPT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 CENTER CARGO COMPT SUMP O/RAIN BILGE AREA. FOUND CORROSION ON WEB FROM STA 1741 TO STA 1788 STRG 49 RT. REMOVED FASTEN ERS AND CUTTED CHANNEL AT STA 1741. REMOVED CORRODED SECTION, REMOVED CORROSION, METAL PICK-UP WITHIN LIMITS ON WEB AND STRUCTURE AND TREATED PER SRM 51-21-01 AND SRM 53-00-01. INSTALLED 3 NEW CHANNEL SECTIONS WITH SPLICE PLATES AND FILLE RS PER SRM 51-31-01 AND SRM 51-00-01. INSTALLED WITH NEW FASTENERS OVERSIZED. (JUNE 9, 1998) 2 L 7 3 4F A22WE 1998062600374 19980626 00374 WP 1998 6 26 98FDEA00413 1 19980620 A 2621 FIRE BOTTLE DOUG DC10 DC1030F 3023504 WP NR 2 ENGINE DISCHARGED A FDEA F ACTIVATE FIRE EXT. N FALSE WARNING IN INSP/MAINT 1 SO 25 322FE 47908 ENGINE NR 2, NR 1 BOTTLE LOW PRESSURE LIGHT ILLUMINATING JUST PRIOR TO DEPARTURE. FOUND NR 1 BOTTLE OF APU FIRE EXTINGU ISHER SYSTEM HAD DISCHARGED THRU APU PORT (NR 2 ENG FIREX CONTAINER 1). REPLACED NR 2 ENG FIREX CONTAINER 1 PER M/M 26- 21-02 AND SQUIB FOR SAME (P/N 876296-2). ALSO, REPLACED DISCHARGE HEAD STRAINER (P/N 260968). 2 L 7 3 4F RT A22WE 1998062600375 19980626 00375 WP 1998 6 26 ABXA9800538 1 19980617 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 943AX 47528 EMERGENCY LIGHTS WOULD NOT SHUT OFF WITH POWER OFF OF THE AIRCRAFT. REPLACED THE POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1998062600376 19980626 00376 WP 1998 6 26 ABXA9800539 1 19980617 A 3350 CONNECTOR DOUG DC9 DC931 3022065 WP CABIN LOOSE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 944AX 47550 COCKPIT EMERGENCY LIGHTS WOULD NOT COME ON DURING TEST. SECURED A LOOSE WIRING CONNECTOR AT THE LIGHT FIXTURE. 2 L 7 2 4F A6WE 1998062600377 19980626 00377 WP 1998 6 26 ABXA9800540 1 19980618 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 958AX 47760 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1998062600378 19980626 00378 WP 1998 6 26 MWEA98749 1 19980619 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 203ME 47673 FOUND FORWARD ENTRANCE EMERGENCY LIGHT INOP. MTC REMOVED AND REPLACED FORWARD ENTRANCE EMERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 1998062600379 19980626 00379 WP 1998 6 26 MWEA98750 1 19980617 A 2560 113313 COVER DOUG DC9 DC932 3022066 WP FWD GALLEY SLIDE DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 THE GALLEY SLIDE AND COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE AND COVER. 2 L 7 2 4F A6WE 1998062600380 19980626 00380 WP 1998 6 26 MWEA98751 1 19980617 A 2410 696233B CSD DOUG DC9 DC914 3022034 WP COCKPIT INOPERATIVE A MWEA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 31 800ME 45842 EMERGENCY DC BUSS OFF LIGHT CAME ON FLIGHT INSTRUMENTS FLAGGED WITH NO DC CURRENT ON PITOT HEAT AND ALL RADIO INOP. MTC REMOVED AND REPLACED LEFT GENERATOR CSD AND REMOVED AND REPLACED RADIO RACK CODING FAN VENTURE ASSEMBLY AND R2-19 RELAY . 2 L 7 2 4F A6WE 1998062600381 19980626 00381 NM 1998 6 26 SCNA98064 1 19980620 A 2782 1U109592 ACTUATOR BOEING 727 727282 138408T NM NR 8 LE FLAP FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 281SC 205 21949 ON CLIMB, THE NUMBER EIGHT LEADING EDGE SLAT WOULD NOT RETRACT ON SCHEDULE. TWO ATTEMPTS WERE MADE TO RECYCLE FLAPS AS PER COM PROCEDURE BUT THE NUMBER EIGHT SLAT REMAINED FULLY EXTENDED AS CONFIRMED BY VISUAL INSPECTION. FOUND THE LEADIN G EDGE NUMBER EIGHT SLAT ACTUATOR STICKING. REMOVED AND REPLACED THE ACTUATOR IN ACCORDANCE WITH MAINTENANCE MANUAL CHA PTER 278132. OPERATIONAL AND LEAK CHECK GOOD. 2 L 7 3 4F RT A3WE 1998062600382 19980626 00382 NM 1998 6 26 SCNA98065 1 19980618 A 2611 SMOKE DETECTOR BOEING 727 7272J4 1384006 NM FWD LAVATORY INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE FORWARD LAVATORY SMOKE DETECTOR FAILED SELF TEST. REMOVED AND REPLACED SMOKE DETEC TOR, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998062600383 19980626 00383 1998 6 26 CKSA98349 4 19980618 A 2350 PLUG DOUG DC8 DC8F54 3021926 WP RT MICROPHONE MISLOCATED A CKSA O OTHER B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C CL CLIMB 1 GL 23 806CK 45932 ON CLIMBOUT, BURNING SMELL NOTED IN COCKPIT. FO'S AUDIO PANEL CB POPPED. AFTER 5 MIN COOL DOWN, CB RESET AN IMMEDIATEL Y POPPED AGAIN. BURNING SMELL DISIPATED. FOUND FO'S MIC JACK SHORTING OUT DUE TO LOCATION OF MOUNTING BRACKET. RELOCA TED AS REQUIRED. SYSTEM OPS CHECK NORMAL AT THIS TIME (C/B DID NOT POP AFTER APPROX 2 HRS). 2 L 7 4 4F 4A25 1998062600589 19980626 00589 1998 6 26 VJ9800198 2 19980619 A 7260 717000 GEARBOX BOEING 737 737214 138446R NM NR 2 ENGINE LEAKING A ZZDA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 15 460AT 20158 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE AND OIL QTY WENT TO ZERO. OIL PRESSURE LIGHT ILLUMINATED. FO UND THAT THE NR 2 ENGINE HAD A BANJO FITTING BROKEN FROM THE GEARBOX LOSING OIL. REMOVED THE GEARBOX. THE HELICOIL WAS PULLED OUT OF THE GEARBOX AND THE GEARBOX WAS REPLACED. 2 L 7 2 4F A16WE 1998062600590 19980626 00590 WP 1998 6 26 VJ9800199 1 19980620 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 901VJ 47275 EMERGENCY EXIT LIGHTS INOP AT OVERHEAD SEATS 18 TO 22. REPLACED THE FWD POWER SUPPLY AND BATTERIES ALONG WITH THREE LIG HT BULBS. 2 L 7 2 4F A6WE 1998062600591 19980626 00591 NM 1998 6 26 VJ9800201 1 19980619 A 2560 BATTERY BOEING 737 737222 1384473 NM MEGAPHONE DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 468AT 19074 FWD MEGAPHONE WAS INOP. REPLACED THE MEGAPHONE BATTERIES, OPS CHECKED GOOD. 2 L 7 2 4F A16WE 1998062600592 19980626 00592 NM 1998 6 26 VJ9800202 1 19980621 A 3397 WIRE BOEING 737 7372L9 1384497 NM CABIN BROKEN A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 737Q 21279 EMERGENCY E-PATH LIGHTING IN FWD HALF OF THE CABIN INOP. REPAIRED EPL WIRES AT ROW 10DEF AND OPERATIONALLY TESTED THE S YSTEM. OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998062600593 19980626 00593 NM 1998 6 26 VJ9800203 1 19980518 A 5320 ANGLE BOEING 737 7372E1 138448F NM BS 277 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 461AT 20976 DURING C-CHECK, FOUND MAIN CABIN FS 277 RBL 12 FLOOR SUPORT ANGLE HAS HEAVY SURFACE CORROSION. REMOVED CORROSION AND IN STALLED L-ANGLE REPAIR IAW 737 SRM 51-20-2. 2 L 7 2 4F A16WE 1998062600594 19980626 00594 NM 1998 6 26 VJ9800204 1 19980601 A 5320 SUPPORT BOEING 737 7372E1 138448F NM BS 294-306 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 461AT 20976 DURING C-CHECK, FOUND FLOORBOARD SUPPORT HAS I/G CORROSION AT FS 294 TO 306 LBL 12. 2 L 7 2 4F A16WE 1998062600595 19980626 00595 NM 1998 6 26 VJ9800205 1 19980601 A 5330 SKIN BOEING 737 7372E1 138448F NM BS 784 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 461AT 20976 DURING C-CHECK, FOUND DOOR FRAME WEB SKIN CRACKED AT AFT CARGO FWD LANDING AT FS 784 RS 23 ABOVE LOWER STOP PAD. 2 L 7 2 4F A16WE 1998062600596 19980626 00596 EU 1998 6 26 MALA976149 1 19980619 A 7931 OIL PRESS LIGHT SAAB SF340 SF340A 7850100 EU RT ENGINE ILLUMINATED A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 115XJ 340A115 WHILE IN FLIGHT, THE RIGHT ENGINE OIL PSI CWP LIGHT CAME ON FOR 1 TO 2 SECONDS THEN WENT OUT. THE RIGHT ENGINE OIL PRES SURE GAUGE WAS ALSO AROUND 40 PSI AND FLUCTUATING 10 TO 20 PSI, PROBLEM DID NOT OCCUR WHILE ENGINE WAS FEATHERED. AIRCR AFT RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE CHECKED OIL AND SERVICED OIL LEVELS. ENTERED AS WATCH ITEM. ALL CHE CKS HAVE BEEN GOOD. 2 L 7 2 4T RT A52EU 1998062600597 19980626 00597 NM 1998 6 26 MALA976150 1 19980622 A 2120 AIR DISTRIBUTION DHAV DHC8 DHC8102 2809003 NM CABIN CONDENSATION A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 848MA 346 ON TAXI, THE FLIGHT ATTENDANT SUSPECTED SMOKING IN THE CABIN. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RAN BOTH ENGI NES AND LEFT AND RIGHT BLEED SYSTEMS, DETERMINED SMOKE TO BE CONDENSATION DUE TO HIGH AMBIENT HUMIDITY. 2 H 7 2 4T RT A13NM 1998062600598 19980626 00598 NM 1998 6 26 MALA976151 1 19980621 A 7712 10167N01W00 TORQUE GAUGE DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 830MA 337 LEFT TORQUE GAUGE FAILED ON CLIMBOUT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED LEFT TORQUE GAUGE. OPS AND RUN C HECKS GOOD. 2 H 7 2 4T RT A13NM 1998062600599 19980626 00599 1998 6 26 MALA976152 2 19980620 A 7260 CHIP LIGHT SAAB SF340 SF340A 7850100 EU LT ENGINE ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 LEFT ENGINE CHIP DETECTION LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT RETURNED TO DTW. MAINTENANCE REMOVED CHIP DETECTO R AND FOUND CHIP TO BE ALLOWABLE PLATING MATERIAL. RAN AIRCRAFT, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998062600600 19980626 00600 EU 1998 6 26 MALA976153 1 19980504 A 2560 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR LOOSE A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 507XJ E2316 WHEN CLOSING CABIN DOOR, ESCAPE SLIDE FELL OUT OF PACKAGE. MAINTENANCE REPLACED SLIDE IAW AVRO MM ALL CHECKS GOOD AT TH IS TIME. 2 H 7 4 4F RT A49EU 1998062600601 19980626 00601 WP 1998 6 26 CALA9801131 1 19980617 A 3260 806124 SWITCH DOUG DC10 DC1030 3023501 WP LANDING GEAR INOPERATIVE A CALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 09 41068 87331 47867 WHEN GEAR WAS RETRACTED AFTER TAKEOFF, ALL GEAR RED LIGHTS REMAINED ILLUMINATED. THE AIRCRAFT WAS RETURNED TO GIG WHERE IT LANDED WITHOUT INCIDENT. THE LANDING GEAR WAS SWUNG SEVERAL TIMES AND THE FAILURE COULD NOT BE DUPLICATED. THE AIR CRAFT HAD A BRIEF HISTORY WITH THIS ANOMALY. THE PROXIMITY CONTROL SWITCH UNIT WAS REMOVED AND REPLACED AS A PRECAUTION ARY MEASURE. 2 L 7 3 4F A22WE 1998062600602 19980626 00602 WP 1998 6 26 CALA9801132 1 19980619 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 282 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND A DENT IN RT FUSELAGE SKIN AT STA 282. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1998062600603 19980626 00603 WP 1998 6 26 CALA9801133 1 19980619 A 5720 FRAME DOUG DC9 DC932 3022066 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN FRAME AT RT WING REFUELING STATION. THE CRACK WAS ROUTED OUT, A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW ECRA 5730-01564. 2 L 7 2 4F A6WE 1998062600604 19980626 00604 WP 1998 6 26 CALA9801134 1 19980619 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 980-996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LAV FLOOR WEB CORRODED BETWEEN STA 980 AND 996 AT RBL 59. THE WEB WAS REMOVED, A NEW WEB WAS FABRICATE D AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998062600605 19980626 00605 WP 1998 6 26 CALA9801135 1 19980617 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 279-378 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND FLOOR PANEL IN FORWARD PIT CORRODED AND DELAMINATED AT STA 378 TO 279. A NEW PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010. 2 L 7 2 4F A6WE 1998062600606 19980626 00606 WP 1998 6 26 CALA9801136 1 19980617 A 5754 PANEL DOUG DC9 DC932 3022066 WP LT LE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND LT FLAP LEADING EDGE PANEL NR 3 DELAMINATED AT XFL 267. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-70-2. 2 L 7 2 4F A6WE 1998062600607 19980626 00607 WP 1998 6 26 CALA9801137 1 19980617 A 5754 PANEL DOUG DC9 DC932 3022066 WP RT LE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT WING NR 3 FLAP LEADING EDGE PANEL CRACKED AND CORRODED AT XFLS 283. THE CORROSION WAS REMOVED AND T HE AREA WAS REPAIRED IAW SRM 51-30-2 AND 51-70-2. 2 L 7 2 4F A6WE 1998062600608 19980626 00608 WP 1998 6 26 CALA9801138 1 19980619 A 5753 FAIRING DOUG DC9 DC932 3022066 WP LT TE FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2.5 INCH CRACK IN LT FLAP INBOARD FLAP TRACK FAIRING TRAILING EDGE. THE FAIRING WEB AND ANGLE WERE R EMOVED. A NEW WEB AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998062600609 19980626 00609 WP 1998 6 26 CALA9801139 1 19980619 A 5540 WEDGE DOUG DC9 DC932 3022066 WP RUDDER TE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .5 INCH CRACK IN RUDDER TRAILING EDGE WEDGE. THE AREA WAS REPAIRED IAW SRM 55-03 AND 51-70-2. 2 L 7 2 4F A6WE 1998062600610 19980626 00610 WP 1998 6 26 CALA9801140 1 19980620 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT WING PANEL NR 1246 CORRODED AND DELAMINATED. THE OUTER SKIN WAS REMOVED AND HONEYCOMB WAS CLEANED. NEW SKIN AND HONEYCOMB WERE FABRICATED AND INSTALLED IAW SRM 51-31-1, FIGURE 1 AND 51-70-2. 2 L 7 2 4F A6WE 1998062600611 19980626 00611 WP 1998 6 26 CALA9801141 1 19980620 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 1 INCH CRACK IN OUTER PAN RADIUS OF FORWARD CARGO COMPARTMENT DOOR LOWER FORWARD STOP FITTING. A REP AIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 2-03, FIGURE 8. 2 L 7 2 4F A6WE 1998062600612 19980626 00612 WP 1998 6 26 CALA9801142 1 19980620 A 5230 BEAM DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A .25 INCH CRACK AT FORWARD END OF BEAM NR 1 FASTENER LOCATION AND A .5 INCH CRACK AT FORWARD END OF BE AM NR 5 FASTENER LOCATION OF FORWARD CARGO COMPARTMENT DOOR OUTER PAN. THE CRACKS WERE STOP DRILLED. REPAIRS WERE FABR ICATED AND INSTALLED IAW SRM 52-03. 2 L 7 2 4F A6WE 1998062600613 19980626 00613 WP 1998 6 26 CALA9801143 1 19980620 A 5240 BEAM DOUG DC9 DC932 3022066 WP FWD SERV DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2 INCH CRACK IN FORWARD END OF NR 6 BEAM OF FORWARD SERVICE DOOR. THE BEAM WAS REPAIRED IAW EA 5240- 01192. 2 L 7 2 4F A6WE 1998062600614 19980626 00614 NM 1998 6 26 UPS98227017 1 19980623 A 3350 BULB BOEING 727 72722C 138400F NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 930UP 19096 INSPECTION TYPE-N/A, COCKPIT EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY F/C OK (P/N 10-0067-9), (S/N 14867) ON, ( S/N 32U) OFF. 2 L 7 3 4F A3WE 1998062600615 19980626 00615 WP 1998 6 26 UPS98827006 1 19980608 A 5320 FRAME DOUG DC8 DC871F 302199D WP LT WINDSHIELD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, CAPT'S FWD WINDSHIELD FRAME CRACKED. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998062600616 19980626 00616 WP 1998 6 26 UPS98827007 1 19980608 A 5320 FRAME DOUG DC8 DC871F 302199D WP RT WINDSHIELD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, F/O'S FWD WINDSHIELD FRAME CRACKED. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998062600617 19980626 00617 WP 1998 6 26 UPS98827008 1 19980604 A 5320 37558452 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1229 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1229 BTWN STR 35R-36 SHEAR TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998062600618 19980626 00618 WP 1998 6 26 UPS98827009 1 19980608 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 660 BELOW STR 21R - FRAME HAS A 3 INCH CRACK. REPAIRED CRACK BY WELDING IAW DPS 10.225. 2 L 7 4 4F RT 4A25 1998062600619 19980626 00619 WP 1998 6 26 UPS98827010 1 19980603 A 5320 37532351 FITTING DOUG DC8 DC871F 302199D WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LONG 22R END FITTING JUST AFT OF FS 980 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTI NG IAW SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998062600620 19980626 00620 WP 1998 6 26 UPS98827011 1 19980609 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 467.323 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LT WING L/E RIB AT STA XS467.323 IS CRACKED. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998062600621 19980626 00621 WP 1998 6 26 UPS98827012 1 19980603 A 5320 4758514520N SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1237 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, FS 1237 BTWN STR 33R TO 34R SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1998062600622 19980626 00622 WP 1998 6 26 UPS98827013 1 19980606 A 5313 56138627 LONGERON DOUG DC8 DC871F 302199D WP BS 8-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LONGERON 31R AT FS 8 TO 70 EXFOLIATED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20 AND DWG 5613862. 2 L 7 4 4F RT 4A25 1998062600623 19980626 00623 WP 1998 6 26 UPS98827014 1 19980603 A 5320 37502571 SPLICE DOUG DC8 DC871F 302199D WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LONGERON 31R SPLICE FITTING CRACKED BTWN FS 1040 TO 1060. REMOVED AND REPLACED FITTING IAW SRM 51-1- 20. 2 L 7 4 4F RT 4A25 1998062600624 19980626 00624 WP 1998 6 26 UPS98827015 1 19980610 A 5320 4640162502N FITTING DOUG DC8 DC871F 302199D WP BS 1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, CORROSION BLEND OUTS ON FRAME TO CUSP FITTING AT FS 1520 RT SIDE BEYOND SRM LIMITS. REMOVED AND REPL ACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998062600625 19980626 00625 WP 1998 6 26 UPS98827016 1 19980604 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597.5 - 638.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LT WING L/E UPPER SKIN XFS 597.5 TO 638.75 IS CRACKED 4 PLACES. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998062600626 19980626 00626 WP 1998 6 26 UPS98827018 1 19980622 A 3350 BULB DOUG DC8 DC873F 302199F WP CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 819UP 46019 INSPECTION TYPE-N/A, EMER ENTRY DOOR (L-1) HAS A BAD LIGHT. RELAMPED EMER EXIT DOOR LIGHT AT PAX DOOR PER MM 33-50-02. 2 L 7 4 4F RT 4A25 1998062600627 19980626 00627 NM 1998 6 26 98FDEA00414 1 19980623 A 2612 FIRE WARNING BOEING 727 727233 138408A NM COCKPIT MALFUNCTION A FDEA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 25 280FE 22347 98-0157 STA-DAY - MASTER FIRE WARNING LIGHTS AND BELL ANNUNCIATED WITH NO OTHER INDICATIONS. WARNING SYSTEMS CHECKED O K ON ENGINE, SMOKE, AND APU, NO FAULTS. 10,000 FEET 300 KTS. COULD NOT DUPLICATE ENGINE, APU AND SMOKE DETECTION SYSTE M CHECKS GOOD ON GROUND. CLEANED AND CHECKED CONNECTION AT R421 RECTIFIER AS PRECAUTION PER WIRING DIAGRAM MANUAL 49-41 -01. NO HISTORY. 2 L 7 3 4F RT A3WE 1998062600628 19980626 00628 NM 1998 6 26 98UAL900208 1 19980525 A 2612 21562B SMOKE DETECTOR BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE CARGO MALFUNCTIONED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 29 4728U 19925 FORWARD LOWER CARGO FIRE INDICATED IN FLIGHT. EXTINGUISHING AGENT FIRED INTO COMPARTMENT. *S/D* FOUND NO EVIDENCE OF F IRE IN FWD CARGO COMPT. BOTH SMOKE DETECTORS REPLACED FOR PRECAUTIONARY REASONS. SUBSEQUENT SHOP FINDINGS INDICATE ONE OF THE TWO DETECTORS HAD A LAMP BURNED OUT CAUSING A FIRE CONDITION. ENGINEERING VIEWS THIS AS AN ISOLATED INCIDENT. F UTURE MAINTENANCE PROGRAM UNDER DISCUSSION TO REPLACE SMOKE DETECTOR BULBS ON A ROUTINE SCHEDULE TO PREVENT SUCH OCCURRE NCES. PRESENTLY, THE EXISTING MAINTENANCE MANUAL HAS INSTRUCTIONS TO REMOVE AND INSTALL THE BULBS IN EACH SMOKE DETECTO R. 2 L 7 4 4F 4 F A20WE E20EA 1998062600629 19980626 00629 NM 1998 6 26 98UAL900218 1 19980525 A 3350 BPS73 BATTERY PACK BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 518UA 24871 EMERGENCY FLOOR LIGHTS INOP ROW 9 TO ROW 16. BATTERY NOT SECURE IN POWER SUPPLY. *S/D* BATTERY WAS NOT SECURE IN POWE R SUPPLY. REPLACED BATTERY AND SECURED FASTENERS. 2 L 7 2 4F 4 F RT A2NM E17NE 1998062600630 19980626 00630 NM 1998 6 26 98UAL900255 1 19980616 A 5320 RIVETS BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUSELAGE CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7280U 21558 EVIDENCE OF CORROSION, ONE CRACKED RIVET HEAD AND TEN DISHED RIVETS AT ABOUT SIX INCHES BELOW FORWARD LAVATORY SERVICE P ANEL. *S/D* RIVETS REPLACED AND SKIN REPAIRED PER STRUCTURAL REPAIR MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 1998062600631 19980626 00631 NM 1998 6 26 98UAL900256 1 19980618 A 3260 CIRCUIT BREAKER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GEAR LIGHTS TRIPPED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 953UA 26700 WITH THE GEAR DOWN, THERE WERE NO GREEN GEAR EXTENSION LIGHTS DURING FINAL APPROACH. *S/D* CREW UTILIZED LANDING GEAR MANUAL EXTENSION SYSTEM TO LOWER LANDING GEAR. FURTHER INSPECTION REVEALED CIRCUIT BREAKER AIR GRND RELAY AND LIGHTS WE RE OUT. RESET CIRCUIT BREAKER. ACCOMPLISHED VISUAL CHECK OF CIRCUT BREAKER AND LANDING GEAR SENSOR WIRING IN WHEEL WEL LS. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998062600632 19980626 00632 1998 6 26 98UAL900257 4 19980613 A 3420 IRS HONEYWELL HG1050AD0504 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1/2 MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 354UA 43736740 24360 INERTIAL REFERENCE SYSTEM DRIFT OR FLIGHT MANAGEMENT COMPUTER NAV PROBLEM IN FLIGHT. *S/D* BOTH NR 1 AND NR 2 INERTIAL REFERENCE UNITS (NAV UNITS) WERE REPLACED PRECAUTIONARY. SYSTEM OPERATION HAS SINCE BEEN NORMAL. THE SHOP REPORTED TH EY WERE UNABLE TO FIND ANY FAULT IN THE REPLACED IRU'S, TESTED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1998062600633 19980626 00633 NM 1998 6 26 98UAL900258 1 19980610 A 2133 CONTROL VALVE SUNDSTRAND 56697 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E COMPT MALFUNCTIONED A UALA K NONE O OTHER CL CLIMB 1 WP 29 7281U 21559 CABIN DOES NOT PRESSURIZE DURING CLIMB IN AUTO, STANDBY OR MANUAL. *S/D* FOUND THAT THE ELECTRICAL EQUIPMENT FLOW CON TROL VALVE WOULD NOT CLOSE. REPLACED EQUIPMENT FLOW CONTROL VALVE. OPERATED ENGINES NR 1 AND NR 3 AT IDLE AND AT CLIMB POWER AND AIRCRAFT PRESSURIZED NORMALLY AT CLIMB POWER. DUCT PRESSURE 50 PSI AND RATE OF CLIMB 2000 FT PER MINUTE. AT IDLE CLIMB THE RATE IS 500 TO 1000 FPM. ACCOMPLISHED PRESSURIZATION CONTROL TEST. 2 L 7 3 4F 4 F A3WE E2EA 1998062600634 19980626 00634 NM 1998 6 26 98UAL900259 1 19980613 A 2530 OVEN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY DIRTY A UALA O OTHER A FLAME/FIRE NR NOT REPORTED 1 WP 29 543UA 25698 FOOD WRAPPER IN FORWARD OVEN CAUGHT FIRE. HALON EXTINGUISHER USED TO PUT FIRE OUT. *S/D* FOOD WRAPPER WAS NOT PROPERL Y INSTALLED. REMOVED WRAPPER, CLEANED OVEN, OPS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998062600635 19980626 00635 NM 1998 6 26 98UAL900260 1 19980613 A 3230 273N20043 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 524UA 24977 RETURNED TO DEN DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. NORMAL LANDING. *S/D* LEFT MLG TRUCK POSITION ACTUATOR BLEED PL UG CAME LOOSE, CAUSING FLUID LOSS. ACTUATOR REPLACED. AIRCRAFT TO BE TESTED FOR PROPER FUSE OPERATION. 2 L 7 2 4F 4 F RT A2NM E17NE 1998062600636 19980626 00636 WP 1998 6 26 98UAL900261 1 19980614 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1857U 46986 EEL LIGHTS OUT ON RIGHT SIDE OF AIRCRAFT ROWS 27 TO 36. *S/D* RECONNECTED AT PWR LEAD IN, CKS GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1998062600637 19980626 00637 WP 1998 6 26 98UAL900262 1 19980613 A 3260 LIGHTS DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LANDING GEAR MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 1837U 47969 RED WARNING LIGHTS ILLUMINATED WHEN GEAR HANDLE SELECTED TO GEAR DOWN POSITION. CYCLED GEAR ONCE RED LIGHTS STILL ON. J IGGLED GEAR HANDLE GREEN LIGHTS CAME ON. LANDING NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 1998062600638 19980626 00638 NM 1998 6 26 98UAL900263 1 19980615 A 2611 SMOKE DETECTOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E/E COMPT FAILED A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 574UA 26686 LANDED SFO UNDER AMBER ALERT DUE TO OVERHEAT LIGHT AND SMOKE INDICATION IN FORWARD EQUIPMENT BAY. *S/D* AIRCRAFT EXPER IENCED A SMOKE INDICATION. MAINTENANCE REPLACED BOTH EQUIPMENT COOLING SMOKE DETECTORS. REPLACED RELAY K10506 ALTERNAT E MODE RELAY. 2 L 7 2 4F 4 F RT A2NM E17NE 1998062600639 19980626 00639 NM 1998 6 26 98UAL900264 1 19980615 A 2420 LUG BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 GENERATOR MELTED A UALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 WP 29 945UA 26684 ELECTRICAL SMELL AND LOST THE LEFT GENERATOR. *S/D* B-PHASE LUG OVERHEATED ON THE NR 1 GENERATOR CONTROL BREAKER. THE LUG WAS REPLACED, AS WAS THE BREAKER. 2 L 7 2 4F 4 F RT A16WE E2GL 1998062600640 19980626 00640 EU 1998 6 26 98UAL900265 1 19980614 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 410UA 463 EEL EXIT LIGHTS AT DOOR 2L AND 2R INOPERATIVE. 2 L 7 2 4F 4 F RT A28NM E40NE 1998062600641 19980626 00641 WP 1998 6 26 98UAL900266 1 19980616 A 3397 WIRE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1856U 46975 EMERGENCY LIGHTING DISARM CAUTION LIGHT INOP. FOUND RT AISLE EEL LIGHT STRIP IN FIRST-CLASS INOP. *S/D* SECURED BUSSI NG CABLE AT DOOR 1R, OPS CKD SATISFACTORY. 2 L 7 3 4F 4 F A22WE E23EA 1998062600642 19980626 00642 NM 1998 6 26 98UAL900267 1 19980617 A 5220 S140T263110 SEAL BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE EMER EXIT MISINSTALLED A UALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 WP 29 618UA 21878 RIGHT OVERWING HATCH MAJOR AIR LEAK. UNABLE TO MAINTAIN CABIN PRESSURIZATION. RETURNED TO SFO. *S/D* FOUND DOOR SEAL AT RIGHT OVERWING EXIT DOOR TO BE INSTALLED INCORRECTLY. SEAL REINSTALLED PER MM, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E3NE 1998062600643 19980626 00643 NM 1998 6 26 98UAL900268 1 19980617 A 7931 TRANSMITTER A BIEDERMAN, FLA461004054 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE MALFUNCTIONED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 7294U 21572 700005 NR 3 ENGINE OIL PRESSURE LOW TO RED BAND ON TAKEOFF ROLL. ABORTED TAKEOFF. *S/D* CLEANED THE ELECTRICAL CONNECTOR TO THE OIL PRESSURE TRANSMITTER AND SWAPPED THE NR 1 AND NR 3 GAUGES TO ISOLATE THE PROBLEM. IT SHOWED THAT THE PROBLEM WA S WITH THE INDICATION AND NOT TRUE OIL PRESSURE. THE OIL PRESSURE TRANSMITTER WAS CHANGED AS A PRECAUTION. 2 L 7 3 4F 4 F A3WE E2EA 1998062600644 19980626 00644 NE 1998 6 26 98UAL900269 2 19980618 A 7230 COMPRESSOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE STALLED A UALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 607UA 47673 493 21868 707509 LEFT ENGINE COMPRESSOR STALL IN CRUISE. ENGINE RECOVERED AND CONTINUED OPERATING. *S/D* CHECKS WERE ACCOMPLISHED PER 767-200 MM 7. NO FAULTS COULD BE FOUND. ENGINE WAS REMOVED FOR REFURBISHMENT DUE TO LACK OF A POSITIVE FIX DURING TROU BLESHOOTING. THE ON ENGINE HAS NOT HAD ANY PROBLEMS WITH COMPRESSOR STALLS SINCE INSTALLATION. 2 L 7 2 4F 4 F RT A1NM E3NE 1998062600645 19980626 00645 NE 1998 6 26 98UAL900270 2 19980609 A 7320 CONTROL CABLE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2/3 PYLONS WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 185UA 25395 MULTICONDUCTOR CABLE AT AREA WHERE ROUTED THROUGH PYLON, HAS BRAIDED JACKET, INSULATION OVER WIRES, AND RUBBER PAD ON CA BLE CLAMP IS EATEN AWAY BY SURFACE VIBRATION OR FOREIGN OBJECT DAMAGE FROM SUBSTANCES IN AIR BLOWING OVER CABLE. NR 2 A ND 3 PYLONS ARE AFFECTED. THIS IS THE THIRD AIRCRAFT IN SEQUENCE WHERE THE PROBLEM HAS BEEN OBSERVED. CABLES ARE PART OF ENGINE FUEL AND CONTROL SYSTEM. LOCATION OF DAMAGED AREAS VARIES SLIGHTLY BETWEEN AIRCRAFT. REPAIRED CABLE AT HEAVY MAINTENANCE CHECK. 2 L 7 4 4F 4 F RT A20WE E24NE 1998062600646 19980626 00646 1998 6 26 98UAL900271 4 19980618 A 3460 FMC HONEYWELL BOEING 777 777222 1385219 NM E/E COMPT DEFECTIVE A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 796UA 26931 FIGHT DIVERTED TO IAD DUE TO BOTH FMC'S NOT OPERATING NORMALLY. LANDED OVERWEIGHT. *S/D* THE FLIGHT MANAGEMENT SYSTEM SOFTWARE PROGRAM COULD NOT COMPLETELY PROCESS THE NEW NAV DATA BASE SOFTWARE (P/N UA4-9807-002). NEW NAV DATA BASE SOF TWARE WAS CREATED AND INSTALLED ON THE FLEET. 2 L 7 2 4F RT T0001SE 1998062600647 19980626 00647 NM 1998 6 26 98UAL900283 1 19980615 A 5754 114W28048 ARM BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 8 LE SLAT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 26930 RIGHT INBOARD NR 8 LEADING EDGE SLAT CENTER PAIR OUTBOARD ARM (114W2804-8) CRACKED AT UPPER FLANGE NEAR AFT END ROLLERS. REPLACED ARM (114W2804-8). 2 L 7 2 4F 4 F RT T0001SE E46NE 1998062600648 19980626 00648 WP 1998 6 26 MWEA98752 1 19980619 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP GALLEY SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 209ME 47730 THE LANYARD ON THE GALLEY DOOR SLIDE COVER DETACHED FROM THE ANCHOR POINT. MTC REINSTALLED GALLEY SLIDE COVER AND LANYA RD. 2 L 7 2 4F A6WE 1998062600649 19980626 00649 WP 1998 6 26 MWEA98753 1 19980618 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP TAIL COMPARTMENT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 215ME 47744 BOTH TAIL COMPARTMENT EMERGENCY LIGHTS ARE INOP. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998062600650 19980626 00650 WP 1998 6 26 MWEA98754 1 19980619 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP CABIN BINDING A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 215ME 47744 THE MAIN CABIN DOOR GIRT BAR IS HARD TO ARM AND DISARM. MTC REMOVED PAINT BUILD-UP FROM THE NEW LATCHES. 2 L 7 2 4F A6WE 1998062600651 19980626 00651 NM 1998 6 26 DL72S981304 1 19980615 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 VERT WEB CRACKED INSIDE STABILIZER ABOVE S-DUCT STA 1303. REPAIRED PER SRM 53-10-4 FIG 17, LT AND RT SIDE. 2 L 7 3 4F A3WE 1998062600652 19980626 00652 NM 1998 6 26 DL72S981305 1 19980615 A 5512 SKIN BOEING 727 727232 1384082 NM HORIZ STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 OUTER SKIN DAMAGED AT FASTENER HOLE ON PANEL 9115. REPAIRED PER SRM 55-30-3 FIG 3. 2 L 7 3 4F A3WE 1998062600653 19980626 00653 NM 1998 6 26 DL72S981306 1 19980619 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 LT ELEVATOR CRACKED ADJACENT PREVIOUS REPAIR LOWER SIDE AFT OF NR 3 BALANCE BOARD PANEL SRM 55-20-3. 2 L 7 3 4F A3WE 1998062600654 19980626 00654 NM 1998 6 26 DL72W981308 1 19980620 A 3350 LIGHT 900542 BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 294WA 8376 22112 AFT LT O/W EMERG LIGHT INOP. REPLACED M955 RACK, OPS CKS GOOD. 2 L 7 3 4F A3WE 1998062600655 19980626 00655 1998 6 26 DLM88981309 4 19980620 A 2565 D29985103 SLIDE DOUG MD88 MD88 3023688 NM L2 DOOR DEFECYIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 919DE 53422 L2 DOOR SLIDE BOTTLE PRESS LOW. REPLACED DOOR SLIDE. 2 L 7 2 4F RT A6WE 1998062600656 19980626 00656 NM 1998 6 26 DL73E981310 1 19980621 A 3230 CIRCUIT BREAKER BOEING 737 737247 138448D NM COCKPIT TRIPPED A DALA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SO 27 245WA 23519 AFTER T/O, LND GEAR HANDLE WOULD NOT COME UP. C/W POM, PULLED RED LOCK OVERRIDE TRIGGER, RAISED GEAR, CONTINUED NML. A T GATE, MECH FOUND LVR LATCH C/B POPPED. TESTED LEV LATCH LOCK SOLENOID PER MM 32-31-31 PG 402 SEVERAL TIMES OPN TEST N ML. C/B CKS NML. LAND GEAR HANDLE OPN CKS NML PER TEST. A/C OK FOR SVC. AIR/GD TELEFLEX CONNECTED AND SAFETIED. 2 L 7 2 4F A16WE 1998062600657 19980626 00657 NM 1998 6 26 DL73S981313 1 19980621 A 7312 HEAT VALVE 320114 BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 332DL 15810 23104 717134 DURING FLIGHT, NR 1 ENGINE OIL TEMP WAS INDICATING IN AMBER RANGE. PERFORMED POM PROCEDURES, AFTER 15 MINUTES ELAPSED S HUT NR 1 ENGINE DOWN. REPLACED LT ENGINE FUEL HEAT VALVE. RAN ENGINE, CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2EA 1998062600658 19980626 00658 NM 1998 6 26 DL72W981314 1 19980622 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2814W 20870 OVERWING RT EMERG LIGHTS INOP ON TEST FOR L/O. REPLACED BATT RACK AND BATT PACK, CKS GOOD. 2 L 7 3 4F A3WE 1998062600659 19980626 00659 NE 1998 6 26 DLL10981315 2 19980622 A 7310 000002134 O-RING LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE LEAKING A DALA E ENGINE SHUTDOWN K FLUID LOSS DE DESCENT 1 SO 27 1734D 193C1225 010056 ENG NR 1 SHUTDOWN IN FLT DUE TO HIGH FUEL FLOW AND FUEL USED INDICATIONS WITH ENG AT IDLE F/F IND. 9,500 TO 10,000 LBS. POM COMPLIED WITH FOR HIGH FUEL USE AND ENG SHUTDOWN. FOUND O-RING SEAL LEAKING AT FUEL FILTER FUEL LINE. REPLACED SE AL PER MM AND ENG RUN LEAK CK OK. 2 L 7 3 4F 4 F A23WE E12EU 1998062600660 19980626 00660 NM 1998 6 26 DL76S981317 1 19980622 A 5754 SKIN BOEING 767 767332 1382001 NM NR 9/11/12 SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 127DL 24077 THE NR 9, 11 AND 12 SLATS WERE FOUND WITH AREAS OF DELAMINATION ON THE TRAILING EDGE WEDGES. THE DAMAGED AREAS WERE TRI MMED OUT AND REPAIRED PER THE B767 SRM, 57-43-02. THE REPAIRS WERE DOCUMENTED PER ER/A 365088-14AD. (S/N 000222). 2 L 7 2 4F RT A1NM 1998062600661 19980626 00661 NM 1998 6 26 DL72L981319 1 19980622 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 514DA 21430 FOUND ON C2 LETTER CK, .375 INCH CRACK ON LIGHTENING HOLE, LT LOWER TORQUE BOX WEB AT STA 1228. REPAIRED PER MM 53-11-0 . 2 L 7 3 4F A3WE 1998062600662 19980626 00662 NM 1998 6 26 DL72S981320 1 19980615 A 5530 STRINGER BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 STRINGER CRACKED INSIDE VERTICAL STAB 4TH BAY UP FROM ACCESS 9504 STR 8R. STOP DRILLED CRACK, DYE CHECKED PER PS900-6-3 , NR 1 FABRICATED REPAIR PER M/M 53-30-0 FIG 803. INSTALLED DOUBLER PER MM 53-30-0 FIG 803. 2 L 7 3 4F A3WE 1998062600663 19980626 00663 NM 1998 6 26 DL72S981321 1 19980618 A 5530 ANGLE BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 ANGLE CRACKED INSIDE OF VERT STAB 4TH BAY DOWN FROM OPENING STR 5 ON RT SIDE CRACK IS ON VERT LEG. REMOVED FASTENERS, D RILLED OP REPAIR PARTS PER MM 55-30-0 PG 802. INSTALLED DOUBLER PER MM 55-30-0 PG 802. 2 L 7 3 4F A3WE 1998062600664 19980626 00664 NM 1998 6 26 SCNA98709 1 19980620 A 5320 SUPPORT BOEING 727 7272J4 1384006 NM BS 303.9 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING A HEAVY MAINT CHECK, A CRACK 4 INCHES LONG WAS FOUND ON THE FLOOR SUPPORT WEB IN THE UPPER ANGLE RADIUS IN THE MA IN CABIN FLOOR STRUCTURE AT STATION 303.9 LBL 41. NDT VERIFIED CRACK IAW BOEING NDT MANUAL D6 48875 510000. MATERIAL VE RIFIED AS 7075 T6 .032. FABRICATED REPAIR ANGLE IAW SRM 514003. TREATED AND PRIMED ANGLE PER SRM 511002. INSTALLED PE R SRM 514002 AND MM 512000. 2 L 7 3 4F RT A3WE 1998062600665 19980626 00665 WP 1998 6 26 CKSA98350 1 19980616 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 889 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 TEMPORARY REPAIR INSTALLED ON FUSELAGE STA 889 AT LONGERON 34. REMOVED PREVIOUS REPAIR. INSPECTED AREA MORE CORROSION NOTED ON INNER SKIN. REMOVED CORROSION, CORROSION REMOVAL OUT OF LIMITS IAW L1011 SRM 53-31-00. REPAIRED SKIN IAW L101 1 SRM 53-31-00 FIG 826. CORROSION TASK CARD NUMBER C53-120-04-01. NON-ROUTINE TASK CARD NUMBER 18489. 2 L 7 3 4F A23WE 1998062600666 19980626 00666 NM 1998 6 26 ASAA9810029 1 19980424 A 5320 ANGLE BOEING 737 7372Q8C 138448S NM BS 540 CRACKED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING C-CHECK, CRACKS WERE FOUND IN THE LEFT UPPER WING TO BODY DRAG ANGLE AND FRAME SPLICE ANGLE. REPLACED ANGL E PER EA 5310-01572. (M) 2 L 7 2 4F A16WE 1998062600667 19980626 00667 1998 6 26 ASAA9880079 4 19980506 A 2565 D37013121 INFLATION DOUG DC9 DC983 3022083 WP L1 DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 942AS ALT2262261 53052 PDX - DURING MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1998062600668 19980626 00668 1998 6 26 ASAA9880080 4 19980506 A 2565 D37013111 INFLATION BOTTLE DOUG DC9 DC983 3022083 WP L2 DOOR LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 942AS ALT210A4773 53052 PDX - DURING MAINTENANCE CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1998062600669 19980626 00669 WP 1998 6 26 ASAA9880071 1 19980412 A 5210 LATCH DOUG DC9 DC982 3022082 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 957AS 49126 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND DIFFICULT TO RELEASE FROM THE LOCKED OPEN POSITION. LUBRICATED TH E DOOR HOLD OPEN LATCH MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998062600670 19980626 00670 WP 1998 6 26 ASAA9880075 1 19980420 A 5240 MECHANISM DOUG DC9 DC982 3022082 WP R1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 LAX - DURING MAINTENANCE CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN AND CLOSE. LUBED THE R1 DOOR MECHANISM AND OPER ATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998062600671 19980626 00671 WP 1998 6 26 ASAA9880078 1 19980426 A 5610 TRACK DOUG DC9 DC982 3022082 WP LT COCKPIT DIRTY A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 953AS 49386 FAI - AFTER ARRIVAL OF FLT 119, CRE REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. CLEANED DEBRIS FROM WINDOW ROLLER TRACK AND LUBED WINDOW MECHANISM AND OPERATED NORMALLY.(M) 2 L 7 2 4F A6WE 1998062600672 19980626 00672 WP 1998 6 26 ASAA9880076 1 19980424 A 2912 AC7031H8K2 FILTER DOUG DC9 DC982 3022082 WP AFT ACCY COMPT LEAKING A ASAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 01 954AS 49387 SEA - DURING CRUISE OF FLT 516, CREW NOTED RT HYDRAULIC SYSTEM QUANTITY DECREASING AND PRESSURE FLUCTUATING. ACCOMPLISH ED QRH PROCEDURE AND QUANTITY STABILIZED AT 4 QUARTS. EXTENDED LANDING GEAR BY ALTERNATE METHOD AND LANDED WITHOUT INCI DENT. FOUND THE RT HYDRAULIC SYSTEM FILTER HOUSING ASSEMBLY LEAKING. REPLACED THE RT HYDRAULIC SYSTEM FILTER HOUSING A SSEMBLY AND PRESSURIZED THE SYSTEM, NO LEAK NOTED. (M) 2 L 7 2 4F A6WE 1998062600673 19980626 00673 WP 1998 6 26 ORJA9894 1 19980508 A 2560 SLIDE DOUG DC9 DC983 3022083 WP PAX DOOR LOOSE A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 FORWARD ENTRY DOOR ESCAPE SLIDE PACK FASTENER CAME OUT. SLIDE IS OFF THE DOOR (DID NOT DEPLOY). REINSTALLED SLIDE ASSY . OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998062600674 19980626 00674 WP 1998 6 26 ORJA9895 1 19980512 A 3350 EM1267 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 823RA 49889 ROW 28 TO 31 OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998062600675 19980626 00675 WP 1998 6 26 ORJA9897 1 19980514 A 3350 59306431 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 SEVERAL EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN EMERGENCY LIGHT BATTERY CHARGERS. OPS CHECK IS GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600676 19980626 00676 EU 1998 6 26 SIMA981381 1 19980518 A 5320 S53671217298 DRAIN TRACK AEROSP ATR42 ATR42300 8680920 EU FRAME 36/40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURNG CPCP-4 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR DRAIN TRACK BETWEEN FRAME 36 AND 40 CORRODED. MAIN TENANCE REMOVED AND REPLACED THE SERVICE DOOR DRAIN TRACK IAW SRM 53-61-00. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600677 19980626 00677 EU 1998 6 26 SIMA981382 1 19980518 A 5320 S53678008216 ZEE MEMBER AEROSP ATR42 ATR42300 8680920 EU FRAME 39/40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE RIGHT AFT ZEE MEMBER, BETWEEN 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT ZEE MEMBER IAW SRM 51-25-03. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600678 19980626 00678 EU 1998 6 26 SIMA981332 1 19980513 A 5315 S5367240720201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAM 38 WAS CORRODED. MAINTENANCE REPAIRED FLOORBEAM 38 IAW SRM 53-00-00. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600679 19980626 00679 NM 1998 6 26 TAOA059808 1 19980514 A 2161 5483765 CONTROLLER BOEING 727 727225 1384077 NM E/E COMPARTMENT FAILED A TAOA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 15 923TS 20441 FLT 6150 - DCA-LGA - LEFT PACK OVERHEATED ON TAKEOFF ROLL, ABORTED TAKEOFF WHEN PACK TRIPPED AND SMOKE FILLED CABIN AND COCKPIT. REPLACED LEFT PACK CONTROLLER, OPERATIONAL CHECK NORMAL IAW MM 21-51-91. (M) 2 L 7 3 4F A3WE 1998062600680 19980626 00680 NM 1998 6 26 TAOA059809 1 19980518 A 2612 894120 FIRE SENSOR BOEING 727 727254 138408L NM NR 1 ENGINE MALFUNCTIONED A TAOA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 15 913TS 20250 FLT 6160 - LGA-BOS - ENGINE NR 1 FIRE WARNING IN FLIGHT. UNABLE TO PUT OUT LIGHT. SHUTDOWN ENGINE AND DISCHARGED FIRE BOTTLE, AFTER COMPLETING PROCEDURE LIGHT REMAINED ILLUMINATED. REPLACED NR 1 ENGINE LOWER FIRE WARNING SENSOR AND FIRE WARNING CONTROL UNIT. PERFORMED OPERATIONAL CHECK OF SYSTEM, CHECKS NORMAL PER MM 26-11-0. (M) 2 L 7 3 4F A3WE 1998062600681 19980626 00681 NM 1998 6 26 TWRA9823 1 19980420 A 3340 8906K1559 SWITCH BOEING 747 747124 1384874 NM COCKPIT FAILED A TWRA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 15 602FF 19734 DURING APPROACH TURNED ON LANDING LGIHTS AND STARTED SMOKING BEHIND SWITCHS. TURNED OFF LIGHTS, SMOKE WENT AWAY. FOUND LEFT OUTBOARD LANDING LIGHT AT FAULT, PULLED AND COLLARED CIRCUIT BREAKER ON P15 PANEL. PLACARDED INOP. REMOVED AND R EPLACED SWITCH. REACTIVATED SYSTEM. PERFORMED OPS CHECK OK, NO SMOKE IN COCKPIT PER MM 33-11-00. (M) 2 L 7 4 4F A20WE 1998062600682 19980626 00682 EU 1998 6 26 WTAA980079 1 19980518 A 5330 SKIN BAG JETSTM JETSTM3101 1500215 EU FUSELAGE BIRD STRIKE A WTAA K NONE C F.O.D. NR NOT REPORTED 1 WP 17 424UE 796 SFO - BIRD STRIKE REPORTED TO RIGHT SIDE OF FUSELAGE FORWARD OF THE POD. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAM AGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998062600683 19980626 00683 SO 1998 6 26 WTAA980076 1 19980505 A 3610 38E966 AIR REGULATOR EMB 120 EMB120RT SO RT WING LEAKING A WTAA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 17 455UE 120163 ACV - RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE REPLACED RIGHT AIR REGULATOR. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998062600684 19980626 00684 SO 1998 6 26 WTAA980078 1 19980512 A 5297 WIRE EMB 120 EMB120RT SO CARGO DOOR BROKEN A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 17 284UE 120145 SFO - CARGO DOOR WARNING ACTIVATED ON TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE DEFERRED DOOR WARNIN G SYSTEM PER MEL 52-70-1. AIRCRAFT RETURNED TO SERVICE. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REPAIRING BROKEN WIRE ON CARGO DOOR MICROSWITCH. OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A31SO 1998062600685 19980626 00685 SO 1998 6 26 WTAA980080 1 19980519 A 3230 RETRACT MECH EMB 120 EMB120 3260201 SO LANDING GEAR MALFUNCTIONED A WTAA O OTHER J WARNING INDICATION DE DESCENT 1 WP 17 203YV 120203 SMF - GEAR WOULD NOT EXTEND WHEN SELECTED. CREW ACCOMPLISHED GEAR EXTENSION USING ELECTRICAL OVERRIDE PROCEDURES. AIRC RAFT LANDED WITHOUT INCIDENT. AIRCRAFT FERRIED TO FAT FOR REPAIRS. MAINTENANCE SWAPPED SYSTEM 'A' AND SYSTEM 'B' CONNE CTORS AND DEFERRED EPR MEL 32-60-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998062600686 19980626 00686 NM 1998 6 26 WRLA98085 1 19980516 A 7797 51A118 WIRE HARNESS DOUG MD11 MD11F 3023600 NM NR 3 ENGINE FAULTY A WRLA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 274WA 48633 DURNG TAXI, FLT CREW RECEIVED NR 3 ENGINE VIBRATION MONITORING (EVM) COMPRESSOR HIGH ALERT. FLIGHT CREW ELECTED TO RETU RN TO GATE. A/C RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOOTING FOUND NR 3 ENGINE (EVM) HARNESS FAULTING. PART NOT IN STOCK, ASSIGNED DMI M77MA16-25 PER MEL 77-32-1. PART WILL BE REPLACED WHEN AVAILABLE. A/C RETU RNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998062600687 19980626 00687 WP 1998 6 26 GTIA9800058 1 19980511 A 3350 606043 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 942ML 13790 47478 ON DAILY, FOUND FORWARD GALLEY AND COCKPIT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD GALLEY A ND COCKPIT OVERHEAD EMERGENCY BATTERY POWER SUPPLY IAW DC0 MM 33-53-0. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998062600688 19980626 00688 WP 1998 6 26 GTIA9800056 1 19980509 A 3350 BULB DOUG DC9 DC932 3022066 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941ML 47131 DTW - ROW 8 EMERGENCY TRACK LIGHT INOPERATIVE. RELAMPED ROW 8 EMERGENCY LIGHT OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998062600689 19980626 00689 WP 1998 6 26 GTIA9800055 1 19980506 A 3350 110049 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12505 0106 45788 AFT STAIRWAY EMERGENCY TRACK LIGHTING INOP. FOUND BURNED OUT POWER SUPPLY. REMOVED AND REPLACED POWER SUPPLY IAW MM 33 -50-00, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998062600690 19980626 00690 WP 1998 6 26 GTIA9800054 1 19980506 A 3350 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 500TR 49144 DTW - FORWARD SECTION OF EMERGENCY TRACK LIGHTING INOPERATIVE, BATTERY PACK BAD. RESEATED CANNON PLUG, CHECK GOOD IAW M M 33-50. (M) 2 L 7 2 4F A6WE 1998062600691 19980626 00691 WP 1998 6 26 GTIA9800052 1 19980504 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 FORWARD SECTION OF EMERGENCY FLOOR LIGHTING (EXIT) INOPERATIVE. REMOVED AND REPLACED FORWARD SECTION OF FLOOR LIGHT IAW MM 33-50-00, PERFORMED OPERATIONAL CHECK ON SYSTEM, NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 1998062600692 19980626 00692 NM 1998 6 26 F3LA98057 1 19980517 A 5312 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, LBL 6.7, WL 212-213. MAINTENANCE STOP DRILLE D CRACK, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, PATE 2, DETAIL III AND PAGE 6, FIG 1. (M) 2 L 7 2 4F A16WE 1998062600693 19980626 00693 NM 1998 6 26 F3LA98056 1 19980517 A 5312 BULKHEAD WEB BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BULKHEAD WEB AT BS 178, RBL 4.7, WL 190-191.5. MAINTENANCE REMOVED D AMAGED AREA (1 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-11, FIG 1, DETAIL IV AND SRM 51 -30-2. (M) 2 L 7 2 4F A16WE 1998062600694 19980626 00694 EU 1998 6 26 FJT98059170 1 19980516 A 7810 31015828 EXHAUST DUCT BAG JETSTM JETSTM3201 1500217 EU ENGINE CRACKED A A FJTA K NONE T O S ENGINE CASE PENETRATION OTHER AFFECT SYSTEMS IN INSP/MAINT 1 SO 03 917AE 075902902730 917 BNA - ENGINE S/N P65319C WAS REMVOED FOR OTHER MAINTENANCE. AFTER THE REMOVAL, A CRACK APPROXIMATELY 2 INCHES LONG WAS NOTED AT THE 3:30 POSITION 'AS VIEWED FROM THE REAR' RUNNING HORIZONTALLY ACROSS THE TOP REAR TURBINE BEARING SCAVENGE O IL WELDED MOUNT BOSS, LOCATED ON THE DUCT EXHAUST SHIELD OF THE ENGINE. REFERENCE IPC 72-50-05 PAGE 0 FIG 1. ENGINE WI LL BE RETURNED TO GARRETT. INSTALLED QEC UNIT. (M) 2 L 7 2 4T RT A56EU 1998062600695 19980626 00695 NM 1998 6 26 GAIA9844 1 19980428 A 7933 162BL704C TEMP INDICATOR BOEING 727 727223 1384074 NM NR 1 ENGINE MALFUNCTIONED A GAIA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 855AA 20996 AFTER DEPARTING MCO, NR 1 ENGINE OIL TEMPERATURE WENT TO RED LINE CLIMB AND ENGINE SHUT DOWN WAS ACCOMPLISHED. AIRCRAFT MADE AN UNEVENTFUL RETURN TO MCO. INSPECTED NR 1 ENGINE OIL TEMP TABS, WITH NO EVIDENCE OF OVERTEMP. SWAPPED NR 1 AND NR 2 OIL TEMP INDICATORS FOR TROUBLESHOOTING. RAN ENGINES, PROBLEM FOLLOWED IND. RETURNED INDICATORS TO ORIGINAL POSI TION. REMOVED AND REPLACED NR 1 OIL TEMP INDICATOR. RAN ENGINES, FUNCTIONALLY TESTED GOOD PER B727 MM 79-33. (M) 2 L 7 3 4F A3WE 1998062600696 19980626 00696 NM 1998 6 26 GAIA9843 1 19980424 A 2910 6517840489 TUBE BOEING 727 727214 138407R NM RT WING SPLIT A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 751US 21513 OAK-TOL - EN ROUTE TO TOL, THE AIRCRAFT EXPERIENCED TOTAL LOSS OF THE 'B' SYSTEM HYDRAULIC FLUID. THE FLIGHT CREW DECLA RED AN EMERGENCY AND DIVERTED TO SLC AND MADE AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESHOT THE LEAK AND FOUND A BROKE N RETURN LINE IN THE SPOILER SYSTEM LOCATED ALONG THE RIGHT WING AUX SPAR, APPROX AT WBL 92.8 AND WS 196. A TEMPORARY L INE WAS INSTALLED IAW BOEING MM 20-10-5 AND 20-10-12. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998062600697 19980626 00697 GL 1998 6 26 ZIAA98003 2 19980316 A 7230 6844936 SUPPORT LKHEED 188 188A 5262602 WP ALLSN 501D 501D13 03004 GL NR 3 ENGINE CRACKED A ZIAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 GL 23 343HA 188A1053 501316 SHV - FIRE WARNING CAME ON FOR NR 3 ENGINE ABOUT TWO HOURS AND FIFTEEN MINUTES INTO FLIGHT. PULLED EMERGENCY SHUTDOWN H ANDLE AND THE FIRE WARNING WENT OUT. REMOVED AND REPLACED REAR TURBINE BEARING SUPPORT. ALSO, REPLACED NR 3 FIRE WARNI NG SENSING ELEMENT AND CHECKED IWA L-188 MM 26-1-0 PAGES 201-203. INSPECTED ENGINE AND FOUND NO EVIDENCE OF ACTUAL FIRE . GROUND RUN OK. (M) 2 L 7 4 4T 4 T RT 4A22 E282 1998062600698 19980626 00698 WP 1998 6 26 ZIAA98002A 1 19980304 A 2612 8063613 FIRE LOOP LKHEED 188 188A 5262602 WP NR 4 ENGINE BROKEN A ZIAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 GL 23 5512 188A1017 CAE - DURING DESCENT, NR 4 ENGINE FIRE WARING CAME ON AT 0403Z, SHUT DOWN ENGINE AND DISCHARGED HRD. REMOVED AND REPLAC ED BROKEN FIRE WARNING LOOP WIRE ON LEFT SIDE OF NR 4 ENGINE. INSPECTED ENGINE AND FOUND NO EVIDENCE OF ACTUAL FIRE. R EMOVED AND REPLACED HRD FIRE BOTTLE. (M) 2 L 7 4 4T RT 4A22 1998062600699 19980626 00699 WP 1998 6 26 ZIAA9801 1 19980218 A 2612 829792501 FIRE LOOP LKHEED 188 188A 5262602 WP NR 3 ENGINE MALFUNCTIONED A ZIAA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 343HA 188A1053 FIRE WARNING CAME ON FOR NR 3 ENGINE, SHUT DOWN ENGINE. REMOVED AND REPLACED SWIRL STRAIGHTENER, OPERATIONAL CHECK GOOD ON GROUND RUN IAW MX FORM ONE 120, ITEM 23. (M) 2 L 7 4 4T RT 4A22 1998062600700 19980626 00700 WP 1998 6 26 ZIAA98006 1 19980425 A 2612 FIRE LOOP LKHEED 188 188A 5262602 WP NR 3 ENGINE OUT OF POSITION A A ZIAA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 5512 188A1017 FIRE WARNING ON NR 3 ENGINE ZONE 1 LIGHT. SHUT DOWN NR 3 ENGINE. INSPECTED ZONE 1 AREA OF NR 3 ENGINE FIRE DETECTION S YSTEM. FOUND NR 3 SWIRL STRAIGHTENER COCKED AND CLAMP LOOSE. REMVOED AND RESEATED SWIRL STRAIGHTENER AND TORQUED IAW O NE-120 ITEM NR 23. PERFORMED EXTENSIVE GROUND RUN OF NR 3 ENGINE, OPERATIONAL CHECK OK, NO DEFECTS NOTED. (M) 2 L 7 4 4T RT 4A22 1998062600701 19980626 00701 WP 1998 6 26 ZIAA98009 1 19980620 A 2612 CONTROL UNIT LKHEED 188 188A 5262602 WP NR 3 ENGINE MALFUNCTIONED C TM9B E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE NR NOT REPORTED 1 GL 23 346HA 188A1043 YIP - NR 3 ENGINE FIRE WARNING INDICATION. PERFORMED EMERGENCY PROCEDURES PER AFM. INSPECTED ENGINE AND TAILPIPE AREA, NO INDICATION OF FIRE NOTED. REPLACED NR 3 FIRE DETECTION CONTROL UNIT. OPERATIONAL CHECK GOOD ON GROUND RUN. (X) 2 L 7 4 4T RT 4A22 1998062600702 19980626 00702 WP 1998 6 26 ZIAA98008 1 19980429 A 2612 CONNECTOR LKHEED 188 188A 5262602 WP NR 4 ENGINE SHORTED A ZIAA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 5512 188A1017 LRD - NR 4 ENGINE FIRE WARNING LIGHTS IN ZONES 2 AND 3 ON CONTINUOUSLY. CHECKED AND FOUND CONNECTOR SHORTED ON FIREWALL . REMOVED, CLEANED AND RESECURED CONNECTOR. FIRE WARNING SYSTEM CHECKED NORMAL. (M) 2 L 7 4 4T RT 4A22 1998062600703 19980626 00703 WP 1998 6 26 USAA980191 1 19980507 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 699 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 956VJ 61013 47588 PIT - DURING C-2 CHECK, FOUND .125 INCH CRACK IN SKIN AT STATION 699, LONGERON 2R. CUTOUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 38. (M) 2 L 7 2 4F A6WE 1998062600704 19980626 00704 NM 1998 6 26 USAABB98042 1 19980419 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM L4 DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 620AU 27199 LAX - FOUND L4 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998062600705 19980626 00705 NM 1998 6 26 TWRA9828 1 19980501 A 3397 WIRE BOEING 747 747130 1384880 NM CABIN BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 'B' ZONE EMERGENCY LIGHTS INOP RIGHT SIDE. FOUND AND REPAIRED BROKEN WIRE, OPS CHECK OK PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1998062600706 19980626 00706 GL 1998 6 26 ZIAA98005 2 19980423 A 7261 SEAL LKHEED 188 188A 5262602 WP ALLSN 501D 501D13 03004 GL NR 4 ENG GB LEAKING C TM9B E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 346HA 188A1043 500573 YIP - SHUT DOWN NR 4 ENGINE FOR REDUCTION GEAR BOX LOW OIL PRESSURE INDICATIONS. GROUND RUN NR 4 ENGINE AND FOUND START ER LEAKING. RESEALED STARTER GARLOCK AND SHAFT. CHECKED REDUCTION GEAR MAGNETIC PLUG FOR CONTAMINATION, INSUFFICIENT C ONTAMINATION FOUND. CHANGED RGB OIL SCREEN, OPS CHECK GOOD ON GROUND RUN. (M) 2 L 7 4 4T 4 T RT 4A22 E282 1998062600707 19980626 00707 NM 1998 6 26 TAOA059802 1 19980503 A 3350 1000677 LIGHT BOEING 727 727254 138408L NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 913TS 4475 20250 FLT 6463 - LGA-DCA - EMERGENCY EXIT LIGHT AFT AIRSTAIRS AREA AND LEFT FORWARD CABIN OVERWING EXIT LIGHT INTERMITTENT. R EPLACED AFT AIRSTAIRS AND FORWARD CABIN OVERWING EMERGENCY EXIT LIGHT ASSEMBLIES. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998062600708 19980626 00708 NM 1998 6 26 TAOA059801 1 19980502 A 3260 69482726 CARD BOEING 727 727225 1384077 NM NLG SHORTED A TAOA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 EA 15 919TS 20447 FLT 6140 - LGA-BOS - ON GEAR EXTENSION FOR LANDING, NO NOSE GEAR GREEN LIGHT AND NO PRESS TO TEST. AFTER GO AROUND RELA MPED AND HAD GREEN NOSE GEAR LIGHT WITH DIM SWITCH ON BRIGHT, NO GREEN WITH DIM SWITCH ON DIM. FOUND CARD ASSEMBLY DIOD E MASTER DIM M833 TO BE DEFECTIVE, REPLACED CARD ASSEMBLY OPERATIONAL CHECK NORMAL IAW MM 33-19-02. (M) 2 L 7 3 4F A3WE 1998062600709 19980626 00709 NM 1998 6 26 TAOA059803 1 19980504 A 2612 65602097 FIRE LOOP BOEING 727 727254 138408L NM NR 1 ENGINE MALFUNCTIONED A TAOA O OTHER N FALSE WARNING DE DESCENT 1 EA 15 913TS 20250 NR 1 ENGINE FIRE WARNING ILLUMINATED ON DESCENT AT IDLE POWER, DESCENDING THROUGH 15,000 FEET AT 300 KNOTS, WHILE ACCOMP LISHING AIRCRAFT OPERATIONS PROCEDURE, FIRE WARNING EXTINGUISHED. ENGINE AT IDLE POWER REMAINDER OF FLT NO FURTHER FIRE INDICATION. INSPECTED ENGINE DUCTS, FIRE LOOP HARNESS FOR SHORT, REPOSITIONED ENGINE FIRE LOOP. CLEANED ENGINE HARNES S CONNECTOR AND RESECURED. TIGHTENED CLAMPS ON 8TH AND 13TH STAGE DUCTS. REPLACED FIRE DETECTION UNIT RAN ENGINE AT ID LE, PART POWER AND TAKEOFF POWER. NO LEAKS FOUND OPERATIONAL CHECK NORMAL IAW MM CHAPTER 26-11-01 AND 71-00. (M) 2 L 7 3 4F A3WE 1998062600710 19980626 00710 NM 1998 6 26 TAOA059805 1 19980508 A 3242 M15851641 ANTENNA BOEING 727 727227 1384078 NM RADOME MALFUNCTIONED A TAOA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 15 927TS 20837 FLT 6411 - LGA-BOS - AT ALL ALTITUDES AND TILT SETTINGS RADAR UNRELIABLE. REPLACED RADAR ANTENNA OPERATIONAL CHECK NORM AL IAW MM CHAPTER 34-41-0 SWAPPED NR 1 VERTICAL GYRO WITH NR 2 VERTICAL GYRO PRECAUTIONARY. (M) 2 L 7 3 4F A3WE 1998062600711 19980626 00711 EU 1998 6 26 SABA980028 1 19980430 A 3234 DNID76ZMK4 SELECTOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT MALFUNCTIONED A SABA L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 SO 33 942AE 178597 942 CLT-AHN - FLT 5067 - ON APPROACH TO AHN, THE CREW EXTENDED THE LANDING GEAR AND DID NOT GET THREE GREEN LGIHT. RECYCLED GEAR SEVERAL TIMES, STILL NO SAFE GEAR INDICATION. THE CREW MADE A FLYBY OF THE TOWER. DUE TO WEATHER, TOWER COULD NO T SEE IF THE GEAR WAS DOWN. THEY FINALLY GOT THREE LIGHTS. INFLIGHT EMERGENCY WAS DECLARED AND EMERGENCY PROCEDURES WE RE USED. AIRCRAFT MADE A SAFE LANDING AT AHN. MAINTENANCE FROM CLT FOUND GEAR SELECTOR SWITCH. RETRACTION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 2 4T RT A56EU 1998062600712 19980626 00712 EU 1998 6 26 REXA98091 1 19980420 A 3244 5006491 TIRE SAAB SF340 SF340A 7850100 EU NLG OUT OF ROUND A REXA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 SO 25 112PX 340A025 NOSE WHEEL SHIMMY FROM 40-70 KNOTS EXTREMELY BAD. REMOVED AND REPLACED NOSE TIRES (LT AND RT). ALSO, SERVICED SHIMMY D AMPNER. (M) 2 L 7 2 4T RT A52EU 1998062600713 19980626 00713 1998 6 26 REXA98090 4 19980419 A 3442 6224022001 RT UNIT SAAB SF340 SF340A 7850100 EU FWD FUSELAGE FAILED A REXA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 327PX 2321 340A059 WEATHER RADAR INOP INFLGHT. REMOVED AND REPLACED WEATHER RADAR R/T. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998062600714 19980626 00714 EU 1998 6 26 REXA98088 1 19980416 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3101 1500215 EU LEFT MALFUNCTIONED A REXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 SO 25 335PX 712 ON CLIMB-OUT, THE LEFT ENGINE FIRE CWP LIGHT WENT OFF. CREW BLEW BOTH BOTTLES. LIGHT STILL DID NOT GO OUT. REMOVED AND REPLACED LEFT ENGINE FIRE LOOP ASSY. (M) 2 L 7 2 4T RT A21EU 1998062600715 19980626 00715 EU 1998 6 26 REXA98087 1 19980407 A 3610 7275031503 BLEED PIPE SAAB SF340 340B 7860101 EU RIGHT FAILED A REXA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 361PX 340B249 RIGHT ENGINE OVERTEMP AFTER TAKEOFF. REMOVED AND REPLACED HP BLEED PIPE AND CLAMP, AND PERFORMED BOROSCOPE INSPECTION O F HOT SECTION AND POWER TURBINE IAW WITH GE MM 72-00-00. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A52EU 1998062600716 19980626 00716 EU 1998 6 26 REXA98086 1 19980408 A 6120 8210153 PCU SAAB SF340 340B 7860101 EU LT ENGINE SURGED A REXA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 25 366PX 340B267 ABORTED TAKEOFF, APPEARED THAT LEFT ENGINE TORQUE SURGED AND CAUSED AIRCRAFT TO YAW TO RIGHT. REMOVED AND REPLACED LEFT PCU. PERFORMED GROUND RUNS. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998062600717 19980626 00717 EU 1998 6 26 REXA98085 1 19980411 A 3241 140041 TRANSDUCER SAAB SF340 SF340A 7850100 EU LT MLG INOP A REXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 25 402BH 223 340A058 ANTI-SKID INOP. REMOVED AND REPLACED LHOB WHEEL SPEED TRANSDUCER. (M) 2 L 7 2 4T RT A52EU 1998062600718 19980626 00718 EU 1998 6 26 REXA98084 1 19980404 A 2421 2308031 GENERATOR SAAB SF340 340B 7860101 EU RIGHT FAILED A REXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 367PX 6916 340B271 RIGHT GENERATOR IS INOP. REMOVED AND REPLACED RIGHT GENERATOR AND REPAIRED ALL WIRES ON TERMINAL BLOCK. OPS CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 1998062600719 19980626 00719 EU 1998 6 26 REXA98078 1 19980323 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3101 1500215 EU RIGHT MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 316PX 687 RIGHT DETECT LIGHT ON IN FLIGHT. REMOVED AND REPLACED RIGHT FIRE DETECTION LOOP. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A21EU 1998062600720 19980626 00720 1998 6 26 ORJA9890 4 19980506 A 2565 D29982121 SLIDE DOUG DC9 DC983 3022083 WP GALLEY LOW PRESSURE A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 878RA 53184 FORWARD GALLEY ESCAPE SLIDE PRESSURE IS BELOW OPERATING LIMITS. REMOVED AND REPLACED FORWARD GALLEY ESCAPE SLIDE. (M) 2 L 7 2 4F RT A6WE 1998062600721 19980626 00721 WP 1998 6 26 ORJA9891 1 19980501 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 LEFT EMERGENCY EXIT ROW LIGHTS STAY ON. REMOVED AND REPLACED BATTERY BACK AT LEFT EMERGENCY EXIT ROW. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600722 19980626 00722 WP 1998 6 26 ORJA9892 1 19980501 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 EMERGENCY EXIT LIGHT OUT AT ROW 11 SEAT D. REPAIRED BROKEN WIRES ON LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600723 19980626 00723 WP 1998 6 26 ORJA9893 1 19980506 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN BROKEN A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 EMERGENCY LIGHT INOP AT SEAT 26DEFT. SPLICED BROKEN WIRE FOR EMERGENCY LIGHT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600724 19980626 00724 WP 1998 6 26 ORJA9884 1 19980424 A 3350 CONNECTORS DOUG DC9 DC982 3022082 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 842RA 49604 FLOOR TRACK EMERGENCY LIGHTING INOP. FOUND LOOSE SIDEWALL CONNECTORS. REPLACED CONNECTOR. ALL CHECKS OK. (M) 2 L 7 2 4F A6WE 1998062600725 19980626 00725 WP 1998 6 26 ORJA9882 1 19980418 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 ROW 7 EMERGENCY EXIT LIGHT INOP. RESET PINS IN WALL CONNECTOR. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600726 19980626 00726 WP 1998 6 26 ORJA9883 1 19980417 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 EMERGENCY LIGHT OUT ON 7D. SECURED BAD CONNECTION. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600727 19980626 00727 WP 1998 6 26 ORJA9881 1 19980421 A 3350 59306431 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 882RA 49949 TWO EMERGENCY LIGHTS OUT, ILLUMINATE TAIL CONE. REMOVED AND REPLACED BATTERIES IN BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600728 19980626 00728 WP 1998 6 26 ORJA9888 1 19980501 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RT EMERGENCY PATH LIGHT FLASH ON/OFF INTERMITTENTLY ROWS 21-24. REPLACED AFT LEFT OVERWING EMERGENCY LIGHTS POWER PACK FOR ROWS 21-24. ALSO, FOUND BAD BUTT SPLICES. REMOVED AND REPLACED SPLICE AND SECURED WIRING. OPS CHECK NORMAL OF RT EMERGENCY PATH LIGHTS. (M) 2 L 7 2 4F RT A6WE 1998062600729 19980626 00729 WP 1998 6 26 ORJA9887 1 19980430 A 3350 59306431 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHT INOP AT SEAT ROW 3-7, 12-16, 21-24 AND LT MID EXIT. REMOVED AND REPLACED BATTERIES FOR ROWS 12-16, 21-2 4. REMOVED AND REPLACED FUSE FOR ROWS 3-7. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600730 19980626 00730 WP 1998 6 26 ORJA9886 1 19980430 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 878RA 53184 EMERGENCY EXIT LIGHT OUT AT SEAT 18DEF. REPLACED LIGHT RECEPTICLE AT SEAT 18DEF. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600731 19980626 00731 WP 1998 6 26 ORJA9885 1 19980426 A 3350 EM1267 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 880RA 53186 OVERWING AFT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY FOR EMERGENCY LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998062600732 19980626 00732 1998 6 26 NOCA1398 2 19980506 A 7320 8062550 GOVERNOR BOEING 757 75723A 1384967 NM LT ENGINE MALFUNCTIONED A NOCA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 15 757NA 24567 ON TAKEOFF, MAX EPR ATTAINABLE FROM LEFT ENGINE WAS 1.46. TAKEOFF REJECTED. REPLACED LEFT ENGINE FUEL FLOW GOVERNOR. O PS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 1998062600733 19980626 00733 WP 1998 6 26 NOCA1498 1 19980507 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 E-PATH WHITE LIGHT INOP AT ROW 23 DEF. REPLACED LIGHT ASSEMBLY HARNESS AT ROW 23 DEF. (M) 2 L 7 2 4F RT A6WE 1998062600734 19980626 00734 NM 1998 6 26 NOCA0998 1 19980409 A 3350 1317 BULB BOEING 757 75728A 1384976 NM CABIN FAILED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 751NA 28164 EMERGENCY OVERHEAD AISLE LIGHTS FOUND INOPERATIVE DURING TEST AT ROW 9 ABC AND 15 DEF. RELAMPED EMERGENCY OVERHEAD AISL E LIGHTS AT ROW 9 ABC AND ROW 15 DEF. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 1998062600735 19980626 00735 NM 1998 6 26 F3LA98048 1 19980511 A 5753 TRACK BOEING 737 7372L9 1384497 NM NR 6 TE FLAP CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 271FL 22734 PAE - DURING C-CHECK, INSPECTION REPORTED AFT ENGINE MOUNT ATTACH POINT ON NR 6 FLAP TRACK CORRODED. MAINTENANCE REMOVE D CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 96-0388. OHM 20-10-2, OHM 20-42-10, AND OHM 20-42-05. (M ) 2 L 7 2 4F RT A16WE 1998062600736 19980626 00736 NM 1998 6 26 F3LA98054 1 19980517 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 727 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON SHEAR TIE AT BS 727A, WL 149, RBL 13. MAINTENANCE FABR ICATED REPLACEMENT SHEARTIE AND REPAIRED PER SRM 53-10-1, 51-30-2 AND 53-10-4. (M) 2 L 7 2 4F A16WE 1998062600737 19980626 00737 NM 1998 6 26 P2EA98102 1 19980504 A 3297 WIRE BOEING 737 737205 1384456 NM LT MLG DAMAGED A P2EA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 412CE 20412 FLT 119 - ATL - NO EMERGENCY DECLARED, LANDING NORMAL. LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATES INTERMITTENTLY, IN UP AN D OFF POSITIONS. FOUND BLUE WIRE TO UPLOCK SENSOR PINCHED IN ADELL CLAMP IN LT W/W, WHEN GROUNDED ON BARE WIRE RED LIGH T FOR LEFT MAIN GEAR GOES ON. REPAIRED WIRE PER OHM 20-11-02. OPS CHECK OK PER MM 32-61-21. (M) 2 L 7 2 4F RT A16WE 1998062600738 19980626 00738 NM 1998 6 26 P2EA98101 1 19980501 A 2820 2172004 CHECK VALVE BOEING 737 737244 138448U NM RT CENTER TANK FAILED A P2EA K NONE O OTHER CL CLIMB 1 CE 05 620PC 19708 FLT 119 - MCI - NO EMERGENCY DECLARED LANDING NORMAL. WITH CENTER FUEL TANK BOOST PUMPS ON, RIGHT MAIN TANK CONTINUES T O FEED ON CLIMB-OUT DURING CRUISE, CENTER TANK TAKES ON FUEL WITH CENTER TANK BOOST PUMPS OFF. REPLACED RIGHT CENTER TA NK BOOST PUMP CHECK VALVE PER MM 28-22-71. OPS CHECK OK, INSPECTED CENTER TANK FOR FUEL MIGRATION, NO DISCREPANCY NOTED . (M) 2 L 7 2 4F A16WE 1998062600739 19980626 00739 NM 1998 6 26 P2EA98100 1 19980324 A 7110 COWL BOEING 737 737205 NM NR 2 ENGINE DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - ENGINE NR 2, NOSE COWL AFT SPLIT STRAP HAS MISSING MATERIAL, 6 O'CLOCK POSITION. REPAIRED NOSE COWL PER BOEING FA X COO-SJO-98-0246RR DATED 3-23-98 AND BOEING FAX COO-SJO-98-0161TR DATED 3-13-98. DOCUMENTED ON FAA FORM 8110-3. APPRO VED AND SUBMITTED BY FAA DER FE WING DSIGNATION NR NMR20 DATED 3-25-98. (M) 2 L 7 2 4F A16WE 1998062600740 19980626 00740 NM 1998 6 26 P2EA98098 1 19980319 A 5753 BOLTS BOEING 737 737205 NM RT TE FLAPS LOOSE A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, REF VANGUARD EO 963757A058, RIGHT WING INBOARD FLAP, OUTBOARD TRACK WITH LOOSE BOLTS. ACCOMPLISHED PREVE NTATIVE MODIFICATION PER VANGUARD EO 963757A58. (M) 2 L 7 2 4F A16WE 1998062600741 19980626 00741 NM 1998 6 26 P2EA98096 1 19980407 A 5330 SKIN BOEING 737 737205 NM BS 827-847 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - EXTERIOR FUSELAGE SKIN CRACKED AT BS 830, STRINGER 14RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 827 TO BS 847, BE TWEEN STRINGER 11RT AND STRINGER 14 RT, PER BOEING FAX COO-SJO-98-0296RR DATED 4-3-98. DOCUMENTED ON FAA FORM 8110-3. A PPROVED AND SUBMITTED BY FAA DER NR NM2605 DATED 4-15-98. (M) 2 L 7 2 4F A16WE 1998062600742 19980626 00742 NM 1998 6 26 P2EA98095 1 19980330 A 5315 FLOORBEAM BOEING 737 737205 NM BS 967.5-986.6 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 Q-CHECK ITEM, FLOORBEAM CORRODED BEYOND LIMITS BETWEEN BS 967.5 AND 986.6, RBL 20 WL 208.1. REPAIRED FLOORBEAM BETWEEN BS 967.5 AND BS 986.6 RBL 20 PER BOEING FAX COO-SJO-98-0178RR DATED ON 3-1398. DOCUMENTED ON FAA FOR 8110-3. APPROVED AND SUBMITTED BY FAA DER DESIGNATION NR NM2256 DATED 4-15-98. CORROSION REMOVED FROM BS 947 TO BS 967.5 RBL 20 PER SRM 51-10-6. FOUND WITHIN LIMITS PER 53-101 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600743 19980626 00743 NM 1998 6 26 P2EA98082 1 19980401 A 5330 SKIN BOEING 737 737205 NM BS 727-765 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, EXTERIOR FUSELAGE SKIN CRACKED AT BS 765 BETWEEN STRINGER 13 LT AND 14 LT. REPAIRED FUSELAGE SKIN SECTIO N FROM BS 727B PLUS 15 TO BS 767 BETWEEN STRINGER 10 LT AND STRINGER 14 LT PER COOPESA EO NR COO-3-53-199-98 DATED APR 2 , 1998, SKETCH SKCOORR 980402 DATED APRIL 2, 1998, BOEING FA COO-SJO-98-0288RR. DOCUMENTED ON FAA FORM 8110-3. APPROVE D AND SUBMITTED BY FAA DER DESIGNATION NR NM2605 DATED APRIL 10, 1998. (M) 2 L 7 2 4F A16WE 1998062600744 19980626 00744 NM 1998 6 26 P2EA98077 1 19980309 A 5230 SKIN BOEING 737 737205 NM CARGO DOOR DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, FORWARD CARGO DOOR SKIN HAS VARIOUS DENTS. RESKINNED FWD CARGO DOOR PER SRM 51-10-1 PAGE 5, 51-30-2, 51- 20-1, 51-10-1, 51-10-2. (M) 2 L 7 2 4F A16WE 1998062600745 19980626 00745 NM 1998 6 26 P2EA98076 1 19980403 A 5311 65457859 FRAME BOEING 737 737205 NM BS 747 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, WINDOW FRAME (24LT) WITH PROVISIONAL REPAIR AND CORRODED BEYOND LIMITS, BS 747. REPLACED WINDOW FRAME BE TWEEN BS 747 AND BS 767 PER SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1998062600746 19980626 00746 NM 1998 6 26 P2EA98075 1 19980401 A 5320 CHORD BOEING 737 737205 NM BS 227.8 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 Q-CHECK, NOSE LANDING GEAR WHEEL WELL TORQUE BOX RIGHT LOWER 'T' CHORD CORRODED BEYOND LIMITS AT BS 227.8. REPLACED T-C HORD BETWEEN BS 227.8 AND BS 294.5, WL 157, RBL 15 PER SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1998062600747 19980626 00747 NM 1998 6 26 P2EA98074 1 19980401 A 5320 CHORD BOEING 737 737205 NM BS 294.5 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, NOSE LANDING GEAR WHEEL WELL TORQUE BOX LOWER LEFT 'T' CHORD CORRODED BEYOND LIMITS AT BS 229.8. FABRICA TED 'T' CHORD PER SRM 51-20-1, 51-10-1, 51-10-3, 51-10-2. REPLACED CHORD FROM BS 227.8 TO BS 294.5, WL 157, LBL 15 INCH ES PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1998062600748 19980626 00748 NM 1998 6 26 P2EA98073 1 19980316 A 5315 FLOORBEAM BOEING 737 737205 NM BS 1006 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, FLOORBEAM CORRODED BEYONDED LIMITS AT BS 1006, BETWEEN LBL 12 INCHES AND RBL 4 INCHES. REPAIRED FLOORBEA M PER SRM 53-10-4 FIG 2. (M) 2 L 7 2 4F A16WE 1998062600749 19980626 00749 NM 1998 6 26 P2EA98071 1 19980325 A 5330 SKIN BOEING 737 737205 NM BS 1104 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, UPPER FUSELAGE SKIN CORRODED BEYOND LIMITS AT BS 1104, STRINGER 5 LT AND STRINGER 6LT. REPAIRED FUSELAGE SKIN SECTION FROM BS 1098 TO BS 1111, BETWEEN STRINGER 5 LT AND STRINGER 6 LT PER SRM 53-30-3, PAGE 26 FIG 1 SHEET 4. ( M) 2 L 7 2 4F A16WE 1998062600750 19980626 00750 NM 1998 6 26 P2EA98070 1 19980404 A 5753 CHORD BOEING 737 737205 NM RT TE MIDFLAP CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, RIGHT WING INBOARD TRAILING EDGE MID FLAP 'T' CHORD CRACKED AT WBL 87.73. REPAIRED MID FLAP TRAILING EDG E PER SRM 51-10-1 FIG PAGE 5. RIVETS REPLACED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998062600751 19980626 00751 NM 1998 6 26 P2EA98069 1 19980327 A 5241 FITTING BOEING 737 737205 NM GALLEY DOORWAY CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, FORWARD GALLEY DOOR (R1) FITTING CRACKED BS 290, STRINGER 8RH. REPLACED FITTING REPLACED PER SRM 51-10-1 FIG PAGE 6. RIVETS REPLACED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998062600752 19980626 00752 NM 1998 6 26 P2EA98068 1 19980314 A 5542 SKIN BOEING 737 737205 NM RUDDER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, RUDDER SKIN DELAMINATION LOWER RIGHT SIDE. REPAIRED SKIN PER BOEING FAX COO-SJO-173RR, DATED MARCH 11, 1 998. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER, DESIGNATION NR NM2013 DATED 3-16-98. (M) 2 L 7 2 4F A16WE 1998062600753 19980626 00753 NM 1998 6 26 P2EA980667 1 19980327 A 5320 FITTING BOEING 737 737205 NM BS 290 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, FORWARD GALLEY DOOR, LOWER HINGE SUPPORT FITTING CRACKED AT BS 290, STRINGER 14RT. REPLACED FITTING PER S RM 51-10-1, PAGE 6. RIVETS REPLACED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998062600754 19980626 00754 NM 1998 6 26 P2EA98066 1 19980327 A 5330 SKIN BOEING 737 737205 NM BS 500 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, EXTERIOR FUSELAGE SKIN CRACKED BETWEEN BS 500 PLUS 9 INCHES TO BS 500A PLUS 2 INCHEC, STRINGER 12 RT AND STRINGER 14 RT. REPAIRED FUSELAGE SKIN SECTION PER SRM 53-30-3 FIG 38. (M) 2 L 7 2 4F A16WE 1998062600755 19980626 00755 NM 1998 6 26 P2EA98065 1 19980327 A 5330 SKIN BOEING 737 737205 NM BS 458-491 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, EXTERIOR FUSELAGE SECTION CRACKED AT TWO POSITIONS BETWEEN BS 458 AND BS 491, STRINGER 10 RT TO STRINGER 14 RT. REPAIRED FUSELAGE SKIN SECTION PER SRM 53-30-3 FIG 38. (M) 2 L 7 2 4F A16WE 1998062600756 19980626 00756 NM 1998 6 26 P2EA98063 1 19980331 A 5320 FRAME BOEING 737 737205 NM CARGO DOORWAY CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, FORWARD CARGO DOOR FRAME CRACKED FROM BEAM NR 4 TO BEAM NR 5, INNER SKIN CRACKED BETWEEN BEAM NR 5 AND TH E LOWER FRAME. FABRICATED AND REPAIRED NR 5 BEAM PER SRM 51-10-1 PAGE 5, 51-20-1, 51-10-3, BAC 5602, 51-10-2. REPAIRED /REINFORCED PER SB 737-52-1100, PART III, PARAGRAPH C REVISION 2, FIGURE 6 DATED MARCH 31, 1994. (M) 2 L 7 2 4F A16WE 1998062600757 19980626 00757 NM 1998 6 26 P2EA98062 1 19980319 A 5315 FLOORBEAM BOEING 737 737205 NM BS 787 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, AFT CARGO CMPT FLOORBEAM CORRODED BEYOND LIMITS, BS 787, BETWEEN BL 0 AND RIGHT BL 68.5. REPAIRED FLOORB EAM PER BOEING FAX COO-SJO-98-0191RR, DATED MARCH 16, 1998, AND SRM 53-10-9 FIG 2. FAA FORM 8110-3 APPROVED AND SUBMITT ED BY FAA DER DESIGNATINO NR NM2256 DATED ON MARCH 17, 1998. (M) 2 L 7 2 4F A16WE 1998062600758 19980626 00758 NM 1998 6 26 P2EA98061 1 19980319 A 5330 SKIN BOEING 737 737205 NM BS 259.5-294 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, LOWER FUSELAGE CORRODED SKIN SECTION, BETWEEN BS 259.5-BS 294, STRINGER 22R AND STRINGER 24R. REPLACED F USEALGE SKIN PANEL BETWEEN BS 259.5-BS 360, STRINGER 19 RT AND STRINGER 24RT PER SRM 51-10-1 PAGE 5, SRM 51-30-2, 51-10- 1, SRM 51-10-2. (M) 2 L 7 2 4F A16WE 1998062600759 19980626 00759 NM 1998 6 26 P2EA98060 1 19980326 A 5320 FITTING BOEING 737 737205 NM BS 954 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, AFT GALLEY DOOR LOWER HINGE SUPPORT FITTING CRACKED, BS 954, STRINGER 14 RT. REPLACED HINGE SUPPORT FITT ING PER SRM 51-10-1 PAGE 5. RIVETS REPLACED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998062600760 19980626 00760 NM 1998 6 26 P2EA98059 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 578-579 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASS CABIN WINDOW FRAME (15 RT) CORRODED BEYOND LIMITS, BETWEEN BS 578-BS 597, STRINGER 11 THROUGH STRING ER 13. REPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600761 19980626 00761 NM 1998 6 26 P2EA98058 1 19980323 A 5330 SKIN BOEING 737 737205 NM BS 320 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, LOWER FUSELAGE SKIN BULGED AT BS 320, STRINGER 19 RT. REPAIRED FUSELAGE SKIN BETWEEN BS 316 TO BS 324, S TRINGER 18 TO STRINGER 19 RT PER SRM 53-30-3 FIG 16. (M) 2 L 7 2 4F A16WE 1998062600762 19980626 00762 NM 1998 6 26 P2EA98057 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 727/747 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (23 RT) CORRODED BEYOND LIMITS, BETWEEN BS 727B - BS 747, STRINGER 11 AND ST RINGER 13 RT. REPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600763 19980626 00763 NM 1998 6 26 P2EA98056 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 616 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (15 LT) CORRODED BEYOND LIMITS, BETWEEN BS 597 - BS 616, STRINGER 11 AND STR INGER 13 LT. REPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600764 19980626 00764 NM 1998 6 26 P2EA98055 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 787-807 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (26 LT) CORRODED BEYOND LIMITS, BETWEEN BS 787 THROUGH BS 807, STRINGER 11 A ND STRINGER 13 LT. REPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600765 19980626 00765 NM 1998 6 26 P2EA98054 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 639-663 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME CORRODED BEYOND LIMITS, BETWEEN BS 639 THROUGH BS 663, STRINGER 11 AND STRIN GER 13 LT. REPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600766 19980626 00766 NM 1998 6 26 P2EA98053 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 727 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (22 LT) CORRODED BEYOND LIMITS, BETWEEN BS 727A THROUGH BS 727B, STRINGER 11 AND STRINGER 13 LT. REPAIRED PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600767 19980626 00767 NM 1998 6 26 P2EA98052 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 480-500 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (7LT) CORRODED BEYOND LIMITS, BETWEEN BS 480 THROUGH BS 500, STRINGER 11 AND STRINGER 13 LT. REPAIRED PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600768 19980626 00768 NM 1998 6 26 P2EA98050 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 867-887 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (30 LT) CORRODED BEYOND LIMITS, BETWEEN BS 867 AND BS 887, STRINGER 11 AND S TRINGER 13 LT. REPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600769 19980626 00769 NM 1998 6 26 P2EA98049 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 887-907 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (31 LT) CORRODED BEYOND LIMITS, BETWEEN BS 887 AND BS 907, BETWEEN STRINGER 11 AND STRINGER 13 LT. REPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600770 19980626 00770 NM 1998 6 26 P2EA98048 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 907-927 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME (32 LT) CORRODED BEYOND LIMITS BETWEEN BS 907 AND BS 927, STRINGER 11-13. R EPAIRED WINDOW FRAME PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600771 19980626 00771 NM 1998 6 26 P2EA98045 1 19980318 A 3211 TRUNNION BOEING 737 737205 NM BS 706 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, LEFT MAIN LANDING GEAR TRUNNION SUPPORT FITTING CRACKED BS 706. REPAIRED PER (VAM-010) VANGUARD EO NR 96 3753A055. (M) 2 L 7 2 4F A16WE 1998062600772 19980626 00772 NM 1998 6 26 P2EA98044 1 19980319 A 5313 STRINGER BOEING 737 737205 NM BS 328 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, LOWER FUSELAGE, E/E COMPT, STRINGER 28R CORRODED, LOCATION BS 328. REPAIRED STRINGER 28R BETWEEN BS 298 AND BS 328 PER SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600773 19980626 00773 NM 1998 6 26 P2EA98106 1 19980511 A 2780 MECHANISM BOEING 737 737244 138448U NM NR 1 LE SLAT OUT OF ADJUST A P2EA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 05 620PC 19708 MCI - FLT 703 - NR 1 LEADING EDGE SLAT NOT EXTENDED WITH FLAPS AT 1 DEGREE. ADJUSTED NR 1 SLAT MID EXTEND DETENT ARMS P ER MM 27-81-21. LEADING EDGE SLATS CHECK NORMAL PER MM 27-81-0. (M) 2 L 7 2 4F A16WE 1998062600774 19980626 00774 NM 1998 6 26 P2EA98105 1 19980508 A 3260 UPLOCK SENSOR BOEING 737 737205 NM LT MLG OUT OF ADJUST A P2EA O OTHER N FALSE WARNING AP APPROACH 1 CE 05 412CE 20412 MCI - FLT 917 - LEFT GEAR RED LIGHT ILLUMINATED. GEAR HANDLE PLACED DOWN, RED LIGHT OUT, GREEN LIGHT ON. ADJUSTED UPLO CK SENSOR PER MM 32-61-21 AND PERFORMED GEAR SWING TO VERIFY OPERATION. (M) 2 L 7 2 4F A16WE 1998062600775 19980626 00775 NM 1998 6 26 P2EA98103 1 19980507 A 5210 LATCH BOEING 737 737222 1384473 NM L1 DOOR BROKEN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 ATL - FLT 264 - DURING REPOSITIONING OF JETWAY CAB ON THROUGH FLT, CONTACT WITH THE L-1 DOOR OCCURRED. FORWARD ENTRY DO OR LATCH BROKEN, GUIDE ARM, EYEBOLT, AND HINGE FAIRING BROKEN. REPLACED ROD END AND HINGE FAIRING, ADJUSTED PER MM 52-1 1-00. (M) 2 L 7 2 4F A16WE 1998062600776 19980626 00776 NM 1998 6 26 P2EA98047 1 19980314 A 5320 WINDOW FRAME BOEING 737 737205 NM BS 927-947 OUT OF LIMITS A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, PASSENGER CABIN WINDOW FRAME 33 LT OUT OF LIMITS. REPAIRED PAX WINDOW FRAME BETWEEN BS 947 AND BS 927, S TRINGER 11 LT AND STRINGER 13 LT PER SRM 56-20-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998062600777 19980626 00777 NM 1998 6 26 P2EA98064 1 19980316 A 5330 SKIN BOEING 737 737205 NM BS 727 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, UPPER FUSELAGE LAP JOINT SKIN SECTION CORRODED BEYOND LIMITS, BS 727 PLUS 4.5 TO BS 727 PLUS 16.5, STRIN GER 14 LT. REPAIRED SKIN SECTION PER SRM 53-30-3 FIG 16. (M) 2 L 7 2 4F A16WE 1998062600778 19980626 00778 NM 1998 6 26 P2EA98043 1 19980303 A 5315 FLOORBEAM BOEING 737 737205 NM BS 747 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 SJO - Q-CHECK, AFT CARGO COMPT BS 747, BETWEEN RBL 25 AND RBL 62 FLOORBEAM LOWER FLANGE HAS CORROSION AT UPPER SURFACE. REPAIRED PER SRM 53-10-09 FIG 7, CORROSION REMOVED PER SRM 51-10-06. (M) 2 L 7 2 4F A16WE 1998062600779 19980626 00779 NM 1998 6 26 EISA98113 1 19980518 A 2611 SMOKE DETECTORS BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 CARGO SMOKE DETECTOR LIGHT COMES ON IN CRUISE. NO SMOKE DETECTED. EXTINGUISHES ON GROUND AFTER LANDING. GENERATED FRO M PILOT REPORT. PURGED SMOKE DETECTORS TUBES PER MM 26-00. GROUND TEST NORMAL. (M) 2 L 7 3 4F A3WE 1998062600780 19980626 00780 NM 1998 6 26 EISA98114 1 19980519 A 3610 DUCT BOEING 727 727223 1384074 NM NR 1 ENG STRUT LOOSE A EISA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 CLIMBING OUT NR 1 ENGINE STRUT LIGHT ILLUMINATED. FOLLOWED PROCEDURES IAW ABNORMALS, LIGHT EXTINGUISHED WITH POWER REDU CTION. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED CLAMP ON 8TH STAGE DUCT. LEAK CHECK GOOD ON ENGINE RUN UP. (M) 2 L 7 3 4F A3WE 1998062600781 19980626 00781 NM 1998 6 26 EISA98110 1 19980515 A 2611 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 290NE 18972 CARGO SMOKE LIGHT CAME ON IN DESCENT TO BRU, RECYCLED SWITCH NO FURTHER PROBLEMS. GENERATED FROM PILOT REPORT. PERFORM ED OPERATIONAL CHECK OF MAIN CARGO SMOKE DETECTOR SYSTEM, PER AERONAUTICAL MANUAL, NO DEFECT NOTED. (M) 2 L 7 3 4F A3WE 1998062600782 19980626 00782 NM 1998 6 26 EISA98111 1 19980514 A 2611 DETECTOR BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 RED CARGO SMOKE LIGHT CAME ON IN FLIGHT. VISUAL INSPECTION NO SMOKE DETECTED. ON TAXI, IN RIGHT PACK SWITCH TURNED OFF AND LIGHT EXTINGUISHED. GENERATED FROM PILOT REPORT. OPS CHECKS GOOD ON GROUND IAW MM CHAPTER26-00. (M) 2 L 7 3 4F A3WE 1998062600783 19980626 00783 NM 1998 6 26 EISA98109 1 19980515 A 2611 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 290NE 18972 CARGO SMOKE RED LIGHT ILLUMINATED ON DESCENT INTO CPH, NO SMOKE SEEN AFTER LANDING LIGHT WENT OFF. GENERATED FROM PILOT REPORT. RAN APU TO HEAT UP AND CHECK OUT SMOKE DETECTORS. OPS CHECK GOOD, MM 26-00. NO DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 1998062600784 19980626 00784 NM 1998 6 26 EISA98112 1 19980517 A 7830 LINE BOEING 727 727223 1384074 NM NR TR UNIT LOOSE A EISA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 AFTER TAKEOFF, NR 1 STRUT OVERHEAT LIGHT CAME ON. DUCT PRESSURE DROPPED TO 4 PSI. AFTER BLEED CLOSED. GENERATED FROM PILOT REPORT. FOUND THRUST REVERSER SUPPLY LINE LOOSE, RESECURED LINE LEAK CHECKED NORMAL IAW MM 36-11-0. (M) 2 L 7 3 4F A3WE 1998062600785 19980626 00785 NM 1998 6 26 EISA98107 1 19980515 A 3610 DUCT BOEING 727 727223 1384074 NM NR 1 ENGINE LOOSE A EISA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 DURING CLIMB-OUT, ENGINE NR 1 STRUT, OVERHEAT LIGHT ILLUMINATED. ACCOMPLISHED ABNORMAL CHECK LIST, AFTER CLOSING NR 1 B LEED VALVE, LEFT PACK PRESSURE WAS STILL 26 PSI. LIGHT EXTINGUISHED. GENERATED FROM PILOT REPORT. FOUND DUCT LEAKING NR 1 STRUT. TIGHTENED DUCT. LEAK CHECKED GOOD IAW MM 36-10-0. (M) 2 L 7 3 4F A3WE 1998062600786 19980626 00786 NM 1998 6 26 TSAA9833243 1 19980502 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 4 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600787 19980626 00787 NM 1998 6 26 TSAA9833242 1 19980502 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600788 19980626 00788 NM 1998 6 26 TSAA9833241 1 19980501 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998062600789 19980626 00789 NM 1998 6 26 TSAA9833240 1 19980501 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600790 19980626 00790 NM 1998 6 26 TSAA9833239 1 19980501 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600791 19980626 00791 NM 1998 6 26 TSAA9833238 1 19980501 A 3350 86210066 BATTERY ASSY BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 ON SERVICE CHECK, FOUND POSITION NR 6 EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998062600792 19980626 00792 NM 1998 6 26 TSAA9827256 1 19980511 A 2781 655280737 SWITCH BOEING 737 73725A 1384481 NM NR 1 LE FLAP FAILED A TSAA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 13 819AL 23791 T/O WARNING CONFIG COMES ON WITH POWER ADVANCE. RE-GAP PROX SENSOR NR 1 LE FLAP UNIT AND REPLACE FLAP/SLAT POSITION SWI TCH UNIT. PERFORM OPS AND FUNCTIONS CHECK OF T/O CONFIG AND WARNING SYSTME OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600793 19980626 00793 NM 1998 6 26 TSAA9833237 1 19980430 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 DURNIG SERVICE CHECK, FOUND NR 6 POSITION EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600794 19980626 00794 NM 1998 6 26 F3LA98059 1 19980527 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1006-1014 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURNIG C-CHECK, INSPECTION REPORTED CORROSION AND CRACK ON STRINGER 26R, BS 1006-1014. MAINTENANCE FABRICATED REP LACEMENT STRINGER AND REPAIR PARTS AND REPAIRED PER SRM 51-20-1, 53-10-1 AND 53-10-2. (M) 2 L 7 2 4F A16WE 1998062600795 19980626 00795 NM 1998 6 26 F3LA98060 1 19980527 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 888-892 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26L, BS 888-892, LBL 13, WL 163. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2 AND 53-10-3. (M) 2 L 7 2 4F A16WE 1998062600796 19980626 00796 NM 1998 6 26 F3LA98061 1 19980527 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, RBL 4.7, WL 212-213. MAINTENANCE REMOVED CRACKED AR EA (2 INCH BY 3.5 INCH), FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998062600797 19980626 00797 NM 1998 6 26 F3LA98080 1 19980614 A 2424 915F2125 GCU BOEING 737 737201 1384454 NM NR 1 GEN FAILED A F3LA O OTHER J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 03 205AU 19421 PHX - FLT 429 - DURING DESCENT INTO PHX, FLIGHT CREW REPORTED NR 1 GENERATOR OFF BUS LIGHT ILLUMINATED FOLLOWED BY THE S MELL OF ELECTRICAL SMOKE WITH A SMALL AMOUNT OF VISIBLE SMOKE NOTICED. COMPLIED WITH SMOKE REMOVAL CHECKLIST AND SMOKE DISSIPATED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED GENERATOR CONTROL UNIT AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1998062600798 19980626 00798 NM 1998 6 26 TSAA9833260 1 19980523 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND NR 4 POSITION EMERGENCY FLOOR LIGHT INOP, REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998062600799 19980626 00799 NM 1998 6 26 TSAA9833261 1 19980523 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 ON SERVICE CHECK, FOUND POSITION NR 2 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600800 19980626 00800 NM 1998 6 26 TSAA9833262 1 19980523 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 ON SERVICE CHECK, FOUND POSITION NR 3 EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600801 19980626 00801 NM 1998 6 26 TSAA9833258 1 19980523 A 3350 1000679 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED AFT PASSENGER DOOR EMERGENCY EXIT LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998062600802 19980626 00802 NM 1998 6 26 TSAA9833259 1 19980523 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND NR 5 POSITION EMERGENCY FLOOR LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998062600803 19980626 00803 EU 1998 6 26 SIMA981292 1 19980509 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 47AE 14324 047 SAW - DURING PS-2 INSPECTION, MAINTENANCE REPORTED THE FORWARD EMERGENCY FLOOR LIGHTS INOP AT THE NR 2, 4 AND 6 POSITION . MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AT LOCATION 30WL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600804 19980626 00804 EU 1998 6 26 SIMA981333 1 19980513 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 11425 223 GRR - FLT 4051 - FORWARD AND AFT EMERGENCY LIGHTS INOP. RAI'D 3WL AND 15WL EMERGENCY BATTERY PACKS. OPS CHECK FOUND GO OD. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600805 19980626 00805 EU 1998 6 26 SIMA981371 1 19980517 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 14866 045 SAW - DURING PS-2 INSPECTION, MAINTENANCE REPORTED THE FORWARD NR 7, NR 9 AND NR 11 EMERGENCY FLOOR LIGHTS AND THE RIGHT FORWARD EXTERIOR LIGHT INOP. MAINTENANCE REMOVED AND REPLACED TIE EMERGENCY LIGHT BATTERY PACK AT LOCATION 10WL. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600806 19980626 00806 EU 1998 6 26 SIMA981334 1 19980513 A 3350 3071BPEG BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 344SB 340B344 DFW - FLT 3512 - EMERGENCY FLOOR LIGHT OUT BY ROW 4. RAI EMERGENCY FLOOR LIGHT ROW 4 IAW 33-50-00, OPS CHECK GOOD. A/R RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998062600807 19980626 00807 EU 1998 6 26 SIMA981291 1 19980509 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 538AT 0599 538 SBN - FLT 4275 - AT DEPARTURE, CREW NOTED EMERGENCY EXIT LIGHTS OVER CABIN AND SERVICE DOOR INOP AS WELL AS SEVERAL PAX FLOOR LTS. RAI EMERGENCY LT BATT PACK IN BALLAST 73WL FOR LTS OVER CABIN AND SERVICE DOOR AND RAI EMERGENCY LT BATT PAC K IN BALLAST 62WL FOR FLOOR PROX LTS. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600808 19980626 00808 1998 6 26 RAIA980511 4 19980520 A 3442 6227337001 RT UNIT BAG JETSTM JETSTM3201 1500217 EU RADOME FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 435AM 889 FLT 7438 - STL - WEATHER RADAR FAULTED IN FLIGHT. MAINTENANCE REPLACED WEATHER RADAR RECEIVER TRANSMITTER. (M) 2 L 7 2 4T RT A56EU 1998062600809 19980626 00809 EU 1998 6 26 RAIA980508 1 19980513 A 3230 100A703142 FORK BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 429AM 5401 879 FLT 7030 - COU - ALL THREE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. MAINTENANCE INSPECTED AND FERRIED AIRCRAFT FRO M COU TO STL. MAINTENANCE REPLACED NOSE OLEO SWITCH FORK. (M) 2 L 7 2 4T RT A56EU 1998062600810 19980626 00810 1998 6 26 RAIA980507 4 19980511 A 2210 7002260822 SERVO AEROSP ATR42 ATR42300 8680920 EU AILERON FAILED A RAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 03 426TE 228 FLT 7156 - STL - CREW REPORTED VIBRATION IN YOKE DURING CLIMB. MAINTENANCE INSPECTED AND REPLACED AILERON ROLL SERVO. ( M) 2 H 7 2 4T RT A53EU 1998062600811 19980626 00811 1998 6 26 RAIA980506 3 19980507 A 6140 8659566 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 427AM 876 FLT 7421 - EVV - LEFT ENGINE BETA CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED LEFT ENGINE BETA PRESSURE S WITCH. (M) 2 L 7 2 4T RT A56EU 1998062600812 19980626 00812 1998 6 26 RAIA980504 4 19980511 A 3425 7003365944 AHRS COMPUTER AEROSP ATR42 ATR42300 8680920 EU E/E COMPT FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 421TE 102 FLT 7134 - STL - EFIS HEADING COMPARATOR CAPTION ILLUMINATED DURING TAKEOFF. MAINTENANCE REPLACED LEFT AHRS COMPUTER. ( M) 2 H 7 2 4T RT A53EU 1998062600813 19980626 00813 EU 1998 6 26 RAIA980503 1 19980507 A 2435 23095002 STARTER/GEN JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 558HK 41071 FLT 7502 - STL - LEFT GENERATOR CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED LEFT STARTER GENERATO R. (M) 2 L 7 2 4T RT A41NM 1998062600814 19980626 00814 NM 1998 6 26 MASA98108 1 19980518 A 3350 MS25237327 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 444YV 444 FLT 5157 - ASE-GJT - UPON ARRIVAL IN GJT, CREW REPORTED THE SECOND FROM THE AFT OVERHEAD EMERGENCY LIGHT WAS INOP. MAIN TENANCE REMOVED AND REPLACED THE BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998062600815 19980626 00815 NM 1998 6 26 MASA98107 1 19980518 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 FLT 7565 - GCC-DEN - CREW REPORTED TWO RED AND THREE WHITE EMERGENCY FLOOR TRACK LIGHTS INOP. MAINTENANCE RESECURED THE LIGHT STRIP, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVIEC. (M) 2 H 7 2 4T RT A13NM 1998062600816 19980626 00816 SO 1998 6 26 MASA98104 1 19980515 A 3350 OL3071BPE LAMP EMB 120 EMB120RT SO CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 340JS 120172 FLT 7593 - GNV-JAX - AFTER ARRIVING IN JAX, CREW REPORTED ONE WHITE EMERGENCY FLOOR TRACK LIGHT INOP. MAINTENANCE REMOV ED AND REPLACED A BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998062600817 19980626 00817 NM 1998 6 26 MASA98093 1 19980421 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE INSPECTION, PERSONNEL FOUND THE FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH INOP. REPLACED BULB IN SWITCH. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998062600818 19980626 00818 SO 1998 6 26 MASA98092 1 19980421 A 3350 036604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 289UE 120191 DURING ROUTINE MAINTENANCE, FOUND AFT EMERGENCY LIGHT BATTERY WEAK. REMOVED AND REPLACED BATTERY. (M) 2 L 7 2 4T RT A31SO 1998062600819 19980626 00819 SO 1998 6 26 MASA98091 1 19980420 A 3350 10130115 LIGHT EMB 120 EMB120RT SO CABIN CRACKED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 289UE 120191 DURING ROUTINE MAINTENANCE, FOUND EMERGENCY EXIT SIGN HOUSING CRACKED (AT LEFT OVERWING EMERGENCY EXIT). REMOVED AND RE PLACED EMERGENCYEXIT SIGN ASSEMBLY. (M) 2 L 7 2 4T RT A31SO 1998062600820 19980626 00820 NM 1998 6 26 MASA98090 1 19980420 A 3350 BULBS DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE LINE CHECK INSPECTION, FOUND TWO FORWARD RED BULBS IN THE EMERGENCY EXIT PATH LIGHTING WOULD NOT ILLUMINA TE. THE FORWARD 6 INCH STRIP WAS REPLACED. NO OTHER DEFECTS NOTED. (M) 2 H 7 2 4T RT A13NM 1998062600821 19980626 00821 SO 1998 6 26 MASA98089 1 19980420 A 3350 12021299501 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 289UE 120191 DURING ROUTINE MAINTENANCE, FOUND LT LOWER EXTERIOR EMERGENCY LIGHT BULB WOULD NOT ILLUMINATE. REMOVED AND REPLACED EXT ERIOR EMERGENCY LIGHT ASSEMBLY. (M) 2 L 7 2 4T RT A31SO 1998062600822 19980626 00822 SO 1998 6 26 MASA98088 1 19980419 A 3350 301 BULB EMB 120 EMB120RT SO CABIN GOOD A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 289UE 120191 DURING ROUTINE MAINTENANCE, FOUND FORWARD EMERGENCY LIGHT BULB HAD COME LOOSE FROM THE SOCKET. CLEANED LIGHT SOCKET ASS EMBLY AND REINSTALLED BULB. (M) 2 L 7 2 4T RT A31SO 1998062600823 19980626 00823 NM 1998 6 26 USAASB98115 1 19980518 A 2910 R276800153 HYD LINE BOEING 737 737201 1384454 NM RT MLG FAILED A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 247US 22754 BWI - FLT 915 - EN ROUTE FROM BOS-DCA, CREW REPORTED VIA ACARS THAT THE HYDRAULIC QTY GAUGE WAS INDICATING A LITTLE MORE THAN A GALLON. HYD QTY SHOWED FULL BEFORE DEPARTURE. IT WAS DECIDED THAT WHEN THE CAPT LOWERED THE GEAR, IF THE GAUGE SHOWED THEY WERE LOSING MORE FLUID, THE FLIGHT WOULD DIVERT BWI. WHEN THE GEAR WAS LOWERED THE HYDRAULIC LEVEL REMAINE D THE SAME, BUT WHEN THE FLAPS WERE LOWERED THE HYD LEVEL WENT TO ZERO. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERT ED TO BWI WHERE IT LANDED WITHOUT FURTHER INCIDENT. MX FOUND THE RT MLG DOWNLOCK HYD LINE HAD FAILED AND WAS LEAKING. R EPLACED SAME. CLEANED WHEELWELL AND SERVICED RESERVOIR. LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998062600824 19980626 00824 NM 1998 6 26 USAASB98116 1 19980518 A 3610 1074845 REGULATOR BOEING 737 7374B7 1384702 NM RT ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 438US 29522 24560 PIT - FLT 158 - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE. RIGHT PACK SHOWED ZERO PSI. MANUAL AND AUTO SYSTEM DID N OT OPERATE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENAN CE FOUND THE RIGHT ENGINE BLEED VALVE CIRCUIT BREAKER POPPED AND THE RIGHT ENGINE HIGH STAGE PNEUMATIC SYSTEM REGULATOR AT FAULT. REMOVED AND REPLACED REGULATOR AND RESET CIRCUIT BREAKER. RUNUP, PRESSURIZATION AND BLEED CHECK NORMAL. RIG HT PACK 20 PSI AT IDLE AND LEFT PACK 20 PSI AT IDLE. (M) 2 L 7 2 4F RT A16WE 1998062600825 19980626 00825 NM 1998 6 26 USAASB98098 1 19980416 A 5210 BAC1521522 SEAL BOEING 737 7373B7 1384580 NM PAX DOOR FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 393US 23315 PHL - FLT 1934 - AFTER TAKEOFF AND DURING CLIMB-OUT FROM PHL, THE FLIGHT ATTENDANTS REPORTED TO THE CAPTAIN OF HEARING A LOUD NOISE AROUND THE MAIN ENTRY DOOR. CREW STOPPED CLIMB AT 10,000 FT AND ELECTED TO RETURN TO FIELD AT PHL DUE TO LO UDNESS OF NOISE. FLIGHT LANDED WITHOUT INCIDENT WITH NO EMERGENCY BEING DECLARED. MAINTENANCE FOUND THE MAIN ENTRY DOO R NOT SEALING PROPERLY. ACCOMPLISHED REPAIR TO DOOR SEAL AREA. OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998062600826 19980626 00826 NM 1998 6 26 USAA980169 1 19980420 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 947 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 30928 24478 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH CORROSION TOP OF FLOORBEAM BS 947, BL 8L. REMOVED DAMA GED SECTION, INSTALLED NEW T-CAP LBL 37 RBL 32 BS 947. REPAIRED PER 737-300 SRM 53-00-51 FIG 202. CORROSION TASK NR C5 3-107-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F RT A16WE 1998062600827 19980626 00827 NM 1998 6 26 USAA980170 1 19980420 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 531AU 30928 24478 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK IN STATION 500 FRAME RBL 1.75 INCH BELOW TOP OF FRAME. I NSTALLED DOUBLER, REPAIRED PER EA 43886. (M) 2 L 7 2 4F RT A16WE 1998062600828 19980626 00828 WP 1998 6 26 GAIA9855 1 19980516 A 5330 99155871 PANEL DOUG DC9 DC915F 3022037 WP BS 484-585 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 47014 DURING INSPECTION PSE 53.09.017 WHILE AIRCRAFT WAS IN C-CHECK A CRACK WAS FOUND AT THE WINDOW BELT PANEL BETWEEN STATION 484-585. A TEMPORARY REPAIR WAS PERFORMED ON THE PANEL IAW BOEING LETTER SEQUENCE 9815050 DATED 8 MAY 98. THE AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600829 19980626 00829 WP 1998 6 26 GAIA9854 1 19980516 A 5541 99579783 RIB DOUG DC9 DC915F 3022037 WP RUDDER CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 46907 47014 DURING INSPECTION FOR AD 87-08-02 A CRACK WAS FOUND ON RUDDER RIB AT RIB STATION Z=55.679. THE RIB WAS REPLACED IAW DOU GLAS DC-9 SERVICE BULLETIN 55-23R6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600830 19980626 00830 WP 1998 6 26 GAIA9853 1 19980516 A 5320 992348487 TEE DOUG DC9 DC915F 3022037 WP BS 200 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 47014 DURING INSPECTION OF CORROSION TASK 46-53303 WHILE AIRCRAFT WAS IN C-CHECK LEVEL 2 CORROSION WAS FOUND ON THE FLOORBEAM UPPER CHORD AT STATION Y=200 FROM X=0 TO X=56. THE UPPER CHORD TEE WAS REPAIRED IAW KITTY HAWK EA D9-53-063. THE AIRCR AFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600831 19980626 00831 WP 1998 6 26 GAIA9852 1 19980516 A 5320 991007813 CUSP DOUG DC9 DC915F 3022037 WP BS 200 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 46097 47014 DURING INSPECTION OF CORROSION TASK 46-53303 WHILE AIRCRAFT WAS IN C-CHECK LEVEL 2 CORROSION WAS FOUND ON THE RIGHT FLOO R CUSP MEMBRANE AT STATION 200. THE CUSP WAS REPAIRED IAW KITTY HAWK EA D9-53-062. THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 L 7 2 4F A6WE 1998062600832 19980626 00832 WP 1998 6 26 GAIA9851 1 19980516 A 5330 5911400 SKIN DOUG DC9 DC915F 3022037 WP BS 112 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 47014 DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR ON THE FUSELAGE SKIN BETWEEN LONGERON 25L AND 26L AT FUSELAGE STATIO N 112. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-061. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600833 19980626 00833 WP 1998 6 26 GAIA9850 1 19980516 A 5241 99115793 BEAM DOUG DC9 DC915F 3022037 WP GALLEY DOOR CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 46907 47014 DURING INSPECTION AD 81-10-10R1 A ONE INCH CRACK WAS FOUND ON THE NR 1 BEAM IN THE UPPER FORWARD CORNER OF THE FORWARD G ALLEY SERVICE DOOR. THE BEAM WAS REPAIRED IAW THE DOUGLAS SRM CHAPTER 52 FIG 25. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600834 19980626 00834 WP 1998 6 26 GAIA9849 1 19980516 A 5330 5911427 SKIN DOUG DC9 DC915F 3022037 WP BS 756-766 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 47014 DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR ON THE FUSELAGE SKIN BETWEEN LONGERON 24L AND 25L BETWEEN FUSELAGE S TATION 756 AND 766. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-059. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600835 19980626 00835 WP 1998 6 26 GAIA9848 1 19980516 A 5330 5911411 SKIN DOUG DC9 DC915F 3022037 WP BS 213-229 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 47014 DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR ON THE FUSELAGE SKIN BETWEEN LONGERON 18R AND 21R BETWEEN FUSELAGE S TATION 213 AND 229. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-058. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600836 19980626 00836 WP 1998 6 26 GAIA9847 1 19980516 A 5330 5911411 SKIN DOUG DC9 DC915F 3022037 WP BS 407 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 561PC 46907 47014 DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR ON THE FUSELAGE SKIN BETWEEN LONGERON 23R AND 24R AT FUSELAGE STATIO N 407. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-057. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998062600837 19980626 00837 NM 1998 6 26 GAIA9856A 1 19980526 A 3260 656021132 ACCESSORY UNIT BOEING 727 727214 138407R NM E/E COMPT UNSERVICEABLE A GAIA O OTHER N FALSE WARNING LD LANDING 1 SW 07 750US 21512 NCHEDULED ARRIVAL FROM PHX-MCI, ON LANDING, WHEN GEAR WAS SELECTED DOWN. THREE GREEN AND THREE RED LIGHTS WHERE BOTH BE ING DISPLAYED AT THE SAME TIME. THE SECONDARY MAIN GEAR POSITION LIGHTS INDICATED LEFT DOWN AND LOCKED RIGHT NOT DOWN A ND LOCKED. THE CREW THEN CYCLED THE GEAR AND NOTICED THREE GREEN LIGHTS ONLY. THE SECONDARY MAIN GEAR INDCIATED AGAIN LEFT DOWN AND LOCK. RIGHT NOT DOWN AND LOCKED. THE CREW THEN DECLARED AN EMERGENCY LANDING INTO MCI AND MADE A SAFE AN D UNEVENTFUL LANDING. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. GROUND CHECKED NORMAL. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998062600838 19980626 00838 WP 1998 6 26 ASAA9880083 1 19980515 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FWD CABIN WERE FOUND INOPERATIVE. RECONNECTED W IRE IN FLOOR TRACK AT ROW 10 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998062600839 19980626 00839 WP 1998 6 26 ASAA9880081 1 19980509 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 939AS S103 49657 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998062600840 19980626 00840 NM 1998 6 26 ASAA9840070 1 19980518 A 3350 20131A BATTERY BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 SEA - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS, AFT EMERGENCY EXIT SIGN, AND L2 DOOR EMERGENC Y EXIT IDENTIFIER WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY PACK AND BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998062600841 19980626 00841 NM 1998 6 26 ASAA9840069 1 19980517 A 3350 20131A BATTERY BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 PDX - DURING MAINTENANCE CHECK, THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS AND THE AFT GALLEY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998062600842 19980626 00842 NM 1998 6 26 ASAA9840068 1 19980511 A 3350 S283T0143 BATTERY PACK BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 26C AND 27C, L2 DOOR OVERHEAD EXIT, AND AI SLE OVERHEAD EXIT BETWEEN L2 AND R2 DOORS WOULD NOT ILLUMINATE. REPLACED BATTERY PACK IN AFT CABIN OVERHEAD AND ALL LIG HTS OPERATED NORMAL. (M) 2 L 7 2 4F RT A16WE 1998062600843 19980626 00843 NM 1998 6 26 ASAA9840067 1 19980507 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 782AS 25113 SEA - FLT 27 - PRIOR TO FLT, ONE WHITE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 27. REPLACED LAMP BASE ASSEMBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998062600844 19980626 00844 NM 1998 6 26 ASAA9810038 1 19980517 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURNG MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS AT NR 1 PALLET WOULD NOT EXTINGUISH. REPLACED NR 1 PALLE T RECEIVER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998062600845 19980626 00845 NM 1998 6 26 ASAA9810037 1 19980515 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 2 WERE FOUND TO BE INOPERATIVE. REPLACED B ATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998062600846 19980626 00846 NM 1998 6 26 ASAA9810036 1 19980514 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WOULD NOT PROPERLY. REPLACED BATTERY AND LIGHT O PERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998062600847 19980626 00847 NM 1998 6 26 ASAA9810035 1 19980512 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMEREGNCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AN D LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998062600848 19980626 00848 NM 1998 6 26 ASAA9810034 1 19980508 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - FL 43 - DURING PREFLIGHT, CREW REPORTED THAT THE EMERGENCY EXIT TRACK LIGHTS AT PALLET 6-2 WOULD NOT EXTINGUISH AF TER TEST. REPLACED BATTERY PACK AT PALLET 6-2 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998062600849 19980626 00849 NM 1998 6 26 ASAA9810033 1 19980502 A 3397 WIRE BOEING 737 737290C 138448V NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - DURING MAINTENANCE CHECK, ONE EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 18. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998062600850 19980626 00850 WP 1998 6 26 ASAA9880082 1 19980511 A 5610 WINDOW DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF TRACK A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 956AS 48079 PDX - AFTER ARRIVAL OF FLT 405 - CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. REPOSITIONED WINDOW MECHANISM UPPER GUIDE PIN BACK INTO TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998062600851 19980626 00851 EU 1998 6 26 USAAF98041 1 19980509 A 3230 200444004 UPSTOP DAMPER FOKKER F28 F28MK1000 4990808 EU LT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 868US 11313 PIT - FLT 536 - AFTER TAKEOFF FROM PIT, LEFT MAIN GEAR DID NOT FULLY RETRACT. CREW RECYCLED GEAR TWO TIMES WITH SAME RE SULT. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR UPST OP DAMPER. (M) 2 L 7 2 4F RT A20EU 1998062600852 19980626 00852 NM 1998 6 26 USAABB98051 1 19980504 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 616AU 27147 LAX - FOUND R1 DOOR EMERGENCY EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998062600853 19980626 00853 NM 1998 6 26 USAABB98052 1 19980504 A 3350 86210151 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND POWER PACK IN AFT MID STATION 1310 CONTROL MODULE INSPECTION. MAINTENANCE REPLACED THE POWER PACK. (M) 2 L 7 2 4F RT A2NM 1998062600854 19980626 00854 NM 1998 6 26 USAABB98053 1 19980504 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND FLOOR EMERGENCY LIGHT AT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998062600855 19980626 00855 NM 1998 6 26 USAABB98054 1 19980511 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 617AU 27148 LAX - FOUND THE EMERGENCY LOW LEVEL LIGHT AT ROW 18 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998062600856 19980626 00856 NM 1998 6 26 WRLA98086 1 19980516 A 2560 60289117 SLIDE DOUG MD11 MD11 3023602 NM L-1 DOOR OUT OF POSITION A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 275WA 48631 DURING MAINTENANCE PREFLIGHT, MAINTENANCE REPRESENATIVE NOTED L-1 DOOR SLIDE RAFT SHIFTED OUT OF ALIGNMENT IN ITS CARRIE R WHEN L-1 DOOR WAS OPEN. MAINTENANCE PERSONNEL REPOSITIONED SLIDE RAFT. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998062600857 19980626 00857 NM 1998 6 26 TAOA059813 1 19980522 A 3350 1000677 LIGHT BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 923TS 20441 FLT 6491 - LGA-BOS - COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998062600858 19980626 00858 NM 1998 6 26 TAOA059812 1 19980522 A 3350 90052 CHARGER BOEING 727 727227 1384078 NM CABIN FAILED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 926TS 20774 FLT 6131 - LGA-BOS - EXTERIOR EMERGENCY EXIT LIGHT ON LEFT SIDE OF AIRCRAFT BLINKS INTERMITTENTLY. REPLACED BATTERY PAC K CHARGER UNIT, OPERATIONAL CHECK NORMAL PER MM CHAPTER 33-50. (M) 2 L 7 3 4F A3WE 1998062600859 19980626 00859 EU 1998 6 26 SIMA981401 1 19980520 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT DIRTY A SIMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 278AE 340B278 RDU - FLT 4832 - CARGO SMOKE LIGHT CAME ON DURING TAXI. CLEANED SMOKE DETECTORS. NO DEFECTS NOTED. A/C RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A52EU 1998062600860 19980626 00860 1998 6 26 SIMA981421 4 19980522 A 3425 6226342022 EADI SAAB SF340 340B 7860101 EU LT COCKPIT FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 250AE 3363 340B250 JFK - FLT 4929 - AFTER TAKEOFF, CAPTAIN EFIS FAILED, NEXT CREW SMELLED SMOKE IN COCKPIT. RETURNED TO JFK. REMOVED AND REPLACED CAPTAINS EADI SCREEN IAW S7340 MM 34-24-10 GND. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998062600861 19980626 00861 EU 1998 6 26 SIMA981391 1 19980519 A 2150 22051201 ACM AEROSP ATR72 ATR72212 EU LEFT FAILED A SIMA H O DEACTIVATE SYST/CIRCUITS OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SW 21 434AT 434 DFW - FLT 3544 - INBOUND FROM HOU TO DFW, THE CREW REPORTED A LEFT BLEED FAULT AT 125 KTS IN LANDING CONFIGURATION. UPO N TOUCHDOWN, THE AIRCRAFT WAS TAXIING WHEN SMOKE STARTED TO FLOW INTO THE COCKPIT. THE CREW SHUT DOWN THE AIRCRAFT AND EVACUATED THE PAX ONBOARD. RAI'D THE ACM AND HEAT EXCHANGER ON THE NR 1 SIDE. A/R RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600862 19980626 00862 EU 1998 6 26 SIMA981383 1 19980518 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 11686 223 ORD - SEVERAL EMERGENCY FLOOR LIGHTS INOP. REPLACED APPLICABLE BATTERY PACK. PERFORMED OPERATIONAL CHECK SATISFACTORIL Y. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998062600863 19980626 00863 NM 1998 6 26 98ZZZX2254 1 19980212 A 3350 6013211X BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 912HA 18018 JAX095 40 PHL/SBY - FLT 3221 - AFT CEILING EMERGENCY DOWN LIGHT INOPERABLE. LEFT EMERGENCY EGRESS EXIT SIGN AND LOCATOR LIGHTS IN OPERABLE. REPLACED EMERGENCY LIGHT BATTERY PACK 3351-PS3. 2 H 7 2 4T RT A13NM 1998062600864 19980626 00864 1998 6 26 USAASB98114 4 19980518 A 3417 HG480B42 DADC BOEING 737 7373B7 1384580 NM E/E/ COMPT FAILED A USAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 19 397US 29979 23319 CLT - FLT 1435 - ON TAKEOFF ROLL AT 100 KNOTS, THE FIRST OFFICER'S AIRSPEED, ALTIMETER AND VERTICAL SPEED HAD FAILED. F LIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE N R 2 DIGITAL AIR DATA COMPUTER HAD FAILED. REPLACED SAME. FUNCTIONAL TEST GOOD. (X) 2 L 7 2 4F RT A16WE 1998062600865 19980626 00865 WP 1998 6 26 USAA980175 1 19980426 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 825US 38340 49237 PIT - DURING Q-3 CHECK, FOUND .50 INCH LONG CRACK IN SKIN AT STA 1380 ABOVE LONGERON 14R. INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 38 SHEET 21. (X) 2 L 7 2 4F A6WE 1998062600867 19980626 00867 WP 1998 6 26 USAAD98079 1 19980503 A 5610 5912290506 PANEL DOUG DC9 DC982 3022082 WP FLIGHT DECK CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 823US 49142 CLT - FLT 467 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD GLASS CRACKED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD ASSEMBLY AND THE WINDSHIELD HEAT CONTROLLER. REF: OPERATO R CONTROL NR 98ZZZX2256. (X) 2 L 7 2 4F A6WE 1998062600868 19980626 00868 WP 1998 6 26 98ZZZX2256 1 19980503 A 3040 6171 CONTROL DOUG DC9 DC982 3022082 WP E/E COMPARTMENT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 823US 49142 CLT - FLT 467 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD GLASS CRACKED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD ASSEMBLY AND THE WINDSHIELD HEAT CONTROLLER. REF: OPERATO R CONTROL NR USAAD98079. 2 L 7 2 4F A6WE 1998062600869 19980626 00869 WP 1998 6 26 USAAD98080 1 19980505 A 2410 CSD DOUG DC9 DC981 3022081 WP NR 2 ENGINE OVERSERVICED A USAA A UNSCHED LANDING H W ELECT. POWER LOSS-50 PC INADEQUATE Q C CR CRUISE 1 EA 19 814US 48094 PIT - FLT 336 - DURING CRUISE, THE NR 2 CSD LOW OIL PRESSURE LIGHT ILLUMINATED. THE APU WAS ON MEL AT THE TIME. THE AC FT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTNANCE FOUND THE NR 2 CSD OIL OVERSERVICED. THE OIL WAS DRAI NED TO THE CORRECT LEVEL AND THE MAG PLUS CHECKED. OPERATION WAS NORMAL DURING TEST. (X) 2 L 7 2 4F A6WE 1998062600870 19980626 00870 NM 1998 6 26 USAASB98111 1 19980511 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 274US 22886 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT THE CENTER AISLE CEILING BETWEEN THE EXIT HATCHES INOPERABLE. MAINTE NANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998062600871 19980626 00871 EU 1998 6 26 USAAF98040 1 19980509 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 894US 11379 GSO - CENTER SECTION OF FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PA CK. (X) 2 L 7 2 4F RT 1998062600872 19980626 00872 NM 1998 6 26 USAABB98047 1 19980508 A 3610 2703600 COUPLING BOEING 767 767201 1385125 NM LT ENGINE RUPTURED A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CR CRUISE 1 EA 19 648US 23900 PHL - FLT 894 - APPROXIMATELY 40 MINUTES OUT OF PHL EN ROUTE TO FRA, CREW RECEIVED THE EICAS MESSAGE 'L ENG BLEED OFF' A ND ASSOCIATED LIGHT. CREW ALSO RECEIVED THE EICAS MESSAGE 'L ENG OVHT' AND ASSOCIATED LIGHT. FLIGHT RETURNED TO PHL AN D LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A BLOWN COUPLING ON THE TOP OF THE PRECOOLER VALVE. (X) 2 L 7 2 4F RT A1NM 1998062600873 19980626 00873 NM 1998 6 26 USAA980178 1 19980505 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 31116 24479 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 2 INCH BY 18 INCH AREA OF SURFACE CORROSION STA 947, LBL 12 TO RBL 12 FLOORBEAM. CUT OUT CORRODED SECTION OF UPPER T-CAP ON FLOORBEAM AND SPLICED NEW SECTION. REPAIRED PER SR M 53-00-51. CORROSION TASK NR: C53-107-02. CORROSION LEVEL: 2. (X) 2 L 7 2 4F RT A16WE 1998062600874 19980626 00874 NM 1998 6 26 USAA980174 1 19980425 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 36162 23316 CLT - DURING RON VISUAL INSPECTION, FOUND A 2.675 INCH CRACK IN THE SKIN AT RIGHT BS 727D AT S23R. INSTALLED DOUBLER PE R REPAIR DOCUMENT EA 61668. (X) 2 L 7 2 4F RT A16WE 1998062600875 19980626 00875 NM 1998 6 26 USAASB98105 1 19980504 A 5241 65458492 MECHANISM BOEING 737 7373B7 1384580 NM GALLEY DOOR OUT OF ADJUST A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 387US 22959 BWI - FLT 2150 - UPON CLIMB-OUT FROM BWI, AIRCRAFT HAD A PRESSURIZATION PROBLEM AND A BANGING NOISE COULD BE HEARD FROM THE REAR OF THE AIRCRAFT. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAR ED. MAINTENANCE FOUND THE AFT RIGHT GALLEY SERVICE DOOR NOT SEATED PROPERLY AND OUT OF RIG. ADJUSTED DOOR FOR LOWER DO OR INTERFERENCE. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998062600876 19980626 00876 NE 1998 6 26 USAASB98106 2 19980504 A 7200 ENGINE BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE LEFT FAILED A A USAA A UNSCHED LANDING M R OVER TEMP PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 273AU 37845 6234 22885 709082 PHL - FLT 1717 - UPON CLIMB-OUT FROM PHL, THE NR 1 ENGINE EXPERIENCED LOW POWER AND ABNORMAL ENGINE PARAMETERS. EGT, N2 , AND FUEL FLOW WERE ABNORMALLY HIGH. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENC Y WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY. OPERATIONAL AND LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F A16WE E2EA 1998062600877 19980626 00877 NM 1998 6 26 USAASB98113 1 19980513 A 2913 5718610 PUMP BOEING 737 7374B7 1384702 NM B HYD SYSTEM FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 437US 18322 24559 CLT - FLT 1854 - DURING CRUISE, B-SYSTEM ELECTRIC HYDRAULIC PUMP LIGHT ILLUMINATED. CREW FOLLOWED ABNORMAL PROCEDURES A ND RESET CIRCUIT BREAKER FOR PUMP. LIGHT REMAINED ON. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE ELECTRIC MOTOR DRIVEN PUMP FOR THE B-HYDRAULIC SYSTEM. OP ERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998062600878 19980626 00878 WP 1998 6 26 USAAD98081 1 19980506 A 3350 14597101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 808US 48040 ROC - THE CEILING EMERGENCY EVACUATION LIGHTS FOR THE CENTER SECTION OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACE D THE EMERGENCY LIGHT BATTERIES. (X) 2 L 7 2 4F A6WE 1998062600879 19980626 00879 WP 1998 6 26 USAAD98082 1 19980506 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 927VJ 48154 CMH - THE CEILING EMERGENCY EVACUATION LIGHTS FOR THE CENTER SECTION OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACE D THE EMERENCY LIGHT POWER SUPPLY. (X) 2 L 7 2 4F A6WE 1998062600880 19980626 00880 WP 1998 6 26 USAAD98083 1 19980508 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 952VJ 47574 IND - THE FORWARD CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (X) 2 L 7 2 4F A6WE 1998062600881 19980626 00881 WP 1998 6 26 USAAD98070 1 19980421 A 3350 873100171 LIGHT DOUG DC9 DC982 3022082 WP CABIN MISSING A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 824US 49143 BWI - LOW LEVEL EMERGENCY LIGHT AT ROW 3 WAS MISSING. MAINTENANCE REPLACED THE MISSING LOW LEVEL EMERGENCY LIGHT. (X) 2 L 7 2 4F A6WE 1998062600882 19980626 00882 1998 6 26 USAAD98064 4 19980406 A 2210 DC36E1626SN CONNECTOR DOUG DC9 DC981 3022081 WP E/E COMPT CORRODED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 810US 48042 MCO - FLT 1826 - ON CLIMB-OUT, AIRCRAFT BEGAN TO YAW AT AROUND 3,000 FEET. CAPTAIN TURNED YAW DAMPER OFF AND RUDDER UNR ESTRICTED LIGHT CAME ON. CAPTAIN SWITCHED TO RUDDER POWER CONTROL TO MANUAL AND YAW STOPPED. TURNED AUTOPILOT ON AND Y AW BEGAN AGAIN. TURNED AUTOPILOT OFF AND AIRCRAFT CONTINUED TO YAW, NOW AT 25,000 FEET. CAPTAIN RETURNED TO FIELD AT M CO AND LANDED WITH NO FURTHER INCIDENT. MAINT FOUND CANNON PLUG ON RUDDER YAW DAMPER CORRODED. REPLACED CANNON PLUG ON YAW DAMPER AND REPLACED YAW DAMPER ACTUATOR AS PRECAUTIONARY. REPLACED BOTH PROX SENSORS AND PERFORMED SENSOR ADJUSTEM ENT. OPS CHECKS NORMAL. PERFORMED OVERWIEGHT LANDING INSP. REF: OPER CNTRL NR 98ZZZX2257 AND NR 98ZZZX2258. (X) 2 L 7 2 4F A6WE 1998062600883 19980626 00883 1998 6 26 98ZZZX2257 4 19980406 A 2210 2589445933 ACTUATOR DOUG DC9 DC981 3022081 WP E/E COMPT MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 810US 48042 MCO - FLT 1826 - ON CLIMB-OUT, AIRCRAFT BEGAN TO YAW AT AROUND 3,000 FEET. CAPTAIN TURNED YAW DAMPER OFF AND RUDDER UNR ESTRICTED LIGHT CAME ON. CAPTAIN SWITCHED TO RUDDER POWER CONTROL TO MANUAL AND YAW STOPPED. TURNED AUTOPILOT ON AND Y AW BEGAN AGAIN. TURNED AUTOPILOT OFF AND AIRCRAFT CONTINUED TO YAW, NOW AT 25,000 FEET. CAPTAIN RETURNED TO FIELD AT M CO AND LANDED WITH NO FURTHER INCIDENT. MAINT FOUND CANNON PLUG ON RUDDER YAW DAMPER CORRODED. REPLACED CANNON PLUG ON YAW DAMPER AND REPLACED YAW DAMPER ACTUATOR AS PRECAUTIONARY. REPLACED BOTH PROX SENSORS AND PERFORMED SENSOR ADJUSTEM ENT. OPS CHECKS NORMAL. PERFORMED OVERWIEGHT LANDING INSP. REF: OPER CNTRL NR USAAD98064 AND NR 98ZZZX2258. 2 L 7 2 4F A6WE 1998062600884 19980626 00884 1998 6 26 98ZZZX2258 4 19980406 A 2210 855601 SENSOR DOUG DC9 DC981 3022081 WP E/E COMPT INTERMITTENT A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 810US 48042 MCO - FLT 1826 - ON CLIMB-OUT, AIRCRAFT BEGAN TO YAW AT AROUND 3,000 FEET. CAPTAIN TURNED YAW DAMPER OFF AND RUDDER UNR ESTRICTED LIGHT CAME ON. CAPTAIN SWITCHED TO RUDDER POWER CONTROL TO MANUAL AND YAW STOPPED. TURNED AUTOPILOT ON AND Y AW BEGAN AGAIN. TURNED AUTOPILOT OFF AND AIRCRAFT CONTINUED TO YAW, NOW AT 25,000 FEET. CAPTAIN RETURNED TO FIELD AT M CO AND LANDED WITH NO FURTHER INCIDENT. MAINT FOUND CANNON PLUG ON RUDDER YAW DAMPER CORRODED. REPLACED CANNON PLUG ON YAW DAMPER AND REPLACED YAW DAMPER ACTUATOR AS PRECAUTIONARY. REPLACED BOTH PROX SENSORS AND PERFORMED SENSOR ADJUSTEM ENT. OPS CHECKS NORMAL. PERFORMED OVERWIEGHT LANDING INSP. REF: OPER CNTRL USAAD98064 AND NR 98ZZZX2257. 2 L 7 2 4F A6WE 1998062600885 19980626 00885 NM 1998 6 26 USAA980199 1 19980515 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947-1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND CORROSION ON STR 26L FROM STA 947+4 INCHES TO STA 1006. INSTALLED DOU BLER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1998062600886 19980626 00886 NM 1998 6 26 USAA980198 1 19980515 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947.6/967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 3 FEET TO 6 FEET CORRODED AREA STR 25R BETWEEN STA 947.6 AND STA 967. INSTALLED STRINGER SPLICE AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR: C53-202-01. CORROSION LEVEL; 2. (X) 2 L 7 2 4F A16WE 1998062600887 19980626 00887 NM 1998 6 26 USAA980222 1 19980515 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 954-970 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 16 INCH BY 1 INCH AREA OF CORROSION, STR 27L, STA 954 TO STA 970. CUT OUT 16 INCH SECTION OF STRINGER AND INSTALLED NEW STRINGER SECTION PER SRM 53-10-3, FIG 1. CORROSION TASK NR: C53-202 -01. CORROSION LEVEL: 2. (X) 2 L 7 2 4F A16WE 1998062600888 19980626 00888 NM 1998 6 26 USAA980200 1 19980515 A 3233 SUPPORT BOEING 737 737201 1384454 NM NLG ACTUATOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK NOSE GEAR ACTUATOR SUPPORT BEAM WEB AT RIVET HOLE, STA 22 7.8 + 4 INCHES. DOUBLER INSTALLED PER SRM 51-40-2, REPAIRED PER SRM 51-40-2. (X) 2 L 7 2 4F A16WE 1998062600889 19980626 00889 NM 1998 6 26 USAA980201 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACK BS 500 FRAME BETWEEN STR 28L AND STR 28R. INSTALLED DOUB LER AND FILLER, REPAIRED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1998062600890 19980626 00890 NM 1998 6 26 USAA980202 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK BS 500 FRAME BETWEEN STR 28L AND STR 28R. CUT OUT DAMAGE , INSTALLED TWO DOUBLERS, REPAIRED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1998062600891 19980626 00891 NM 1998 6 26 USAA980203 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STA 500 FRAME BETWEEN STR 28L AND STR 28R. DOUBLER INSTA LLED PER SRM 51-40-3, REPAIRED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1998062600892 19980626 00892 NM 1998 6 26 USAA980204 1 19980515 A 5311 FRAME BOEING 737 737201 1384454 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 3 INCH CRACKED FRAME AT LT BS 480 AT STR 22L. INSTALLED DOUBLER, REPA IRED PER SRM 51-40-3. (X) 2 L 7 2 4F A16WE 1998062600893 19980626 00893 NM 1998 6 26 USAA980205 1 19980515 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT ATTACH HOLE OF STR 16R (TIE CLIP) BS 747, STR 16R. F ABRICATED REPAIR PARTS AND INSTALLED STRINGER SPLICE. REPAIRED PER SRM 53-10-3. (X) 2 L 7 2 4F A16WE 1998062600894 19980626 00894 NM 1998 6 26 USAA980206 1 19980515 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 460 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND TOOL DAMAGE .25 INCH STA 460 STR 19L STRINGER. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. (X) 2 L 7 2 4F A16WE 1998062600895 19980626 00895 NM 1998 6 26 USAA980207 1 19980515 A 5320 SUPPORT BOEING 737 737201 1384454 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40455 22798 INT - DURING 'Q-5' CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 178 LBL 5.5 WL 184 SUPPORT. INSTALLED REPAIR ANGLE AN D REPAIRED PER TR 53-10-17. (X) 2 L 7 2 4F A16WE 1998062600896 19980626 00896 NM 1998 6 26 PCAA9800768 1 19980411 A 1100 DATA PLATE DHAV DHC8 DHC8102 2809003 NM APU OUT OF POSITION A A PCAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 13 836EX 297 DESCENDING WITH AUTOPILOT ON, GOT A NOSE DOWN MIS-TRIM MESSAGE ON 802 PANEL. TOUCHED TCS BUTTON AND HAD A STRONG NOSE U PTRIM, ELEVATOR MANUAL TRIM WOULD NOT WORK UP OR DOWN (FROZEN). SHUT AUTOPILOT OFF WITH STANDBY TRIM, ACFT COULD NOT BE TRIMMED DOWN. MAINTENANCE TROUBLESHOT SYSTEM, FOUND A DATA PLATE FROM THE APU SUSPECT. IT HAD FALLEN INTO THE ELEVATO R ACTUATING CHAIN TRAY, POSSIBLY CAUSING JAM. DATA PLATE WAS REMOVED, AND RETAINED FOR RE-INSTALL. ACFT RETURNED TO SE RVICE. ACFT TC: 17,966. (X) 2 H 7 2 4T RT A13NM 1998062600897 19980626 00897 NM 1998 6 26 PCAA9800769 1 19980413 A 2731 ACTUATOR DHAV DHC8 DHC8102 2809003 NM ELEVATOR TRIM LACK OF LUBE A PCAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 13 836EX 297 IN CRUISE FLIGHT WITH AUTOPILOT ON, GOT A NOSE DOWN MIS-TRIM MESSAGE ON 802 PANEL. ELEVATOR MANUAL TRIM WOULD NOT WORK PROPERLY (FROZEN). SELECED AUTOPILOT OFF AND MANUAL TRIM STILL FROZEN. CREW PERFORMED ABNORMAL CHECK LIST PROCEDURES A ND LANDED WITHOUT INCIDENT. INSPECTED ELEVATOR TRIM SERVO AND ASSOCIATED SYSTEM IN APU BAY. NO DEFECTS NOTED. INSPECT ED TRIM TABS AND JACK SCREWS ON TAIL, NO DEFECTS NOTED. LUBED ELEVATOR TRIM JACK SCREWS/ACTUATOR PER DHC MANUAL 12-20-0 0. ELEVATOR TRIM ACTUATED NORMAL. AIRCRAFT RETURNED TO SERVICE. ACFT TC: 17,980. (X) 2 H 7 2 4T RT A13NM 1998062600898 19980626 00898 NM 1998 6 26 PCAA9800770 1 19980423 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGG COMPT MALFUNCTIONED A PCAA O OTHER N FALSE WARNING NR NOT REPORTED 1 EA 13 814EX 318 EN ROUTE TO ISP FROM DCA, THE BAGGAGE SMOKE DETECTOR ILLUMINATED ON AND OFF SEVERAL TIMES. THE AIRCRAFT DIVERTED INTO A CY AND LANDED WITHOUT INCIDENT. THE BAGGAGE BAY WAS INSPECTED AND NO FIRE WAS EVIDENT. MAINTENANCE REMOVED AND REPLACE D THE NR 2 DETECTOR AND ISSUED MEL 26-8 FOR THE NR 1. THE NR 1 WAS SUBSEQUENTLY REPLACED. AIRCRAFT RETURNED TO SERVICE . PART S/N'S 167 AND 171. (X) 2 H 7 2 4T RT A13NM 1998062600899 19980626 00899 NM 1998 6 26 USAA980177 1 19980505 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 188 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 532AU 31116 24479 INT - DURING 'Q-3' CHECK VISUAL INSPECTION, FOUND APPROXIMATELY 4 INCH BY 6 INCH TEMPORARY REPAIR DOUBLER INSTALLED PER EA 59798 BS 188, WL 190 ON LEFT SIDE FUSELAGE SKIN. INSTALLED PERMANENT REPAIR DOUBLER PER SRM 53-00-01 FIG 202. (X) 2 L 7 2 4F RT A16WE 1998062600900 19980626 00900 WP 1998 6 26 IXXA9800057 1 19980618 A 3233 45973405505 ACTUATOR DOUG DC8 DC862 3021970 WP LT MLG MISRIGGED A IXXA K NONE J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 GL 23 728PL 74563 729 45918 EN ROUTE, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCH WARNING LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR WIT H THE INDICATION REMAINING THE SAME. THE FLIGHT CONTINUED TO SUU FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR AND INDICATION SYSTEMS WITH DISCREPANCIES NOTED. MAINTENANCE PLACED THE UPLATCH CHECK ON DEFERRAL IAW CO M EL PROCEDURES, ACFT VISITED HEAVY MAINTENANCE. HEAVY MAINTENANCE PERFORMED A GEAR SWING WHICH REVEALED THE LT UPLATCH M ECHANISM AND LT MAIN GEAR RETRACT CYLINDER MISRIGGED. HEAVY MAINTENANCE CORRECTED THE DISCREPANCIES IAW THE MM AND A SU CCESSFUL GEAR SWING. 2 L 7 4 4F 4A25 1998062600901 19980626 00901 WP 1998 6 26 CALA9801145 1 19980619 A 5530 PIVOT PLATES DOUG DC9 DC982 3022082 WP VERT FIN CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND VERTICAL FIN RIGHT SIDE INBOARD AND OUTBOARD SET OF PIVOT PLATES CORRODED IN SLEEVE BORE. THE INBOARD AND OUTBOARD SET OF PIVOT PLATES WERE REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998062600902 19980626 00902 NM 1998 6 26 CALA9801146 1 19980620 A 5347 FLOOR TRACK BOEING 737 7373T0 1384582 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND FORWARD GALLEY FLOOR TRACK CORRODED AT STA 294.5. THE FLOOR TRACK WAS REMOVED AND A NEW ONE WAS FABRIC ATED AND INSTALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 1998062600903 19980626 00903 NM 1998 6 26 CALA9801147 1 19980621 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND FLOORBEAM CAP IN FORWARD GALLEY AREA CORRODED AT FS 294.5, RBL 8. THE FLOORBEAM CAP WAS REPAIRED IAW S RM 53-10-51. 2 L 7 2 4F RT A16WE 1998062600904 19980626 00904 WP 1998 6 26 CALA9801148 1 19980621 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12080 47981 INSPECTION FOUND LOWER END OF FORWARD CARGO DOOR FRAME CORRODED AT STA 887. THE FRAME WAS REPAIRED IAW SRM 53-50-00, FI GURE 1. 2 L 7 3 4F A22WE 1998062600905 19980626 00905 WP 1998 6 26 CALA9801149 1 19980620 A 3350 FUSE DOUG DC10 DC1030 3023501 WP CABIN BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND EMERGENCY LIGHT IN ZONE-D ON RT SIDE, SEATS 37KL-45KL INOPERATIVE. A BLOWN FUSE FOR BATTERY PACK WAS F OUND. THE FUSE WAS REPLACED AND OPERATION OF THE EMERGENCY LIGHTS WAS RESTORED. 2 L 7 3 4F A22WE 1998062600906 20010830 00906 NE 2001 8 30 CALA9801144 2 19980619 A 7200 ENGINE BOEING 747 747230B 1384889 NM PWA JT9 JT9D7F 52054 NE NR 1 FAILED A CALA J A J DUMP FUEL UNSCHED LANDING DUMP FUEL Y ENGINE STOPPAGE CL CLIMB 1 SW 09 78019 20527 662347 THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS AND AUTOMATICALLY SHUTDOWN AFTER TAKEOFF FROM GUM. THE ENGINE FAILURE WAS ACCOMPANIED BY A LOUD BANG. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. IN SPECTION BY MAINTENANCE REVEALED THAT THE ENGINE FAILURE WAS CONTAINED WITH METAL FOUND IN THE ENGINE TAILPIPE. THE AIR CRAFT WILL BE FERRIED TO NRT FOR AN ENGINE CHANGE. 2 L 7 4 4F 4 F A20WE E20EA 1998062600907 19980626 00907 WP 1998 6 26 CALA9801150 1 19980623 A 2530 CIRCUIT BREAKER DOUG DC9 DC981 3022081 WP FWD GALLEY FAILED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 13881 48045 A BURNING ELECTRICAL SMELL WAS DETECTED AT THE FORWARD FLIGHT ATTENDANT PANEL WHILE ON FINAL APPROACH. THERE WAS NO VIS IBLE SMOKE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. THE CIRCUIT BREAKER PANELS IN COCKPIT BEHIND JUMPSEAT AND THE E AND E COMPARTMENT WERE INSPECTED. THE ENGINES WERE RUN AND VARIOUS POWER SOURCES WERE OPERATED. NO DEFECTS WERE FOU ND WITH ALL SYSTEMS CHECKING GOOD. MAINTENANCE FOUND THE COFFEEMAKER CIRCUIT BREAKER IN FORWARD GALLEY HAD SIGNS OF BUR NING. THE CIRCUIT BREAKER WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998062600908 19980626 00908 WP 1998 6 26 CALA9801151 1 19980622 A 5730 DOOR DOUG DC9 DC932 3022066 WP WS 240 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND RT WING LEADING EDGE SLAT DOOR GOUGED AT XOS 240. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5730- 01568. 2 L 7 2 4F A6WE 1998062600909 19980626 00909 WP 1998 6 26 CALA9801152 1 19980622 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A CRACK IN CABIN INTERIOR WEB AT STA 756, RBL 53. THE WEB WAS REMOVED, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 4. 2 L 7 2 4F A6WE 1998062600910 19980626 00910 WP 1998 6 26 CALA9801153 1 19980622 A 5320 JAMB DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND INNER AFT CARGO DOOR PAN CUTOUT CORRODED. THE DOOR PAN AND THRESHOLD TRIM WERE REMOVED IAW SRM 51-30-2 . THE THRESHOLD WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A THRESHOLD WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51- 30-2, AND 51-30-5. THE DOOR JAMB PAN WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998062600911 19980626 00911 WP 1998 6 26 CALA9801154 1 19980622 A 5320 RAIL DOUG DC9 DC982 3022082 WP BS 1003-1221 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 INSPECTION FOUND LT TIE DOWN RAIL HAD EXFOLIATED CORROSION AT ATTACH FASTENER AND BELTFRAME AT STA 1022 WITH LIGHT TO MO DERATE CORROSION AT STA 1003 TO 1221. THE TIE DOWN RAIL WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998062600912 19980626 00912 WP 1998 6 26 CALA9801155 1 19980622 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 THE TAIL CONE PULL FROM INTERIOR RELEASE HANDLE, EXTERIOR RELEASE HANDLE, AND AFT ENTRY DOOR WAS LOW. THE TAIL CONE CAB LES WERE RIGGED AND FUNCTIONALLY CHECKED GOOD IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998062600913 19980626 00913 WP 1998 6 26 CALA9801156 1 19980623 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18835 49439 THE TAIL CONE RELEASE HANDLE INSIDE TAIL COMPARTMENT PULLED HIGH FROM CLIPS AT 45 POUNDS. THE CLIPS WERE ADJUSTED AND F UNCTIONALLY CHECKED GOOD IAW MM 53-50-00. 2 L 7 2 4F A6WE 1998062600914 19980626 00914 WP 1998 6 26 9809579996 1 19980621 A 3230 59516395001 BUNGEE CYLINDER DOUG DC9 DC931 3022065 WP NLG FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8932E 23809 23809 47141 DURING APPROACH, NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. FLIGHT CREW UTILIZED EMERGENCY GEAR EXTENSION PROCEDURES AND CONFIRMED THROUGH PEEP HOLE THAT GEAR WAS DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS REQUES TED ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NOSE GEAR BUNGEE CYLINDER. OPE RATIONAL CHECK NORMAL ON GEAR CYCLE. 2 L 7 2 4F A6WE 1998062600915 19980626 00915 NM 1998 6 26 SWAA981117 1 19980610 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED C2 CHECK, FOUND CRACKED INTERCOSTAL AT BS 540 FLOOR RT 1.5 FROM CENTER, AND AT BS 540 FLOOR LT 1.5 FRO M CENTER. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600916 19980626 00916 1998 6 26 SWAA981118 4 19980610 A 2565 SLIDE BOEING 737 7373H4 1384600 NM GALLEY DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 658SW 23332 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY DOOR ESCAPE SLIDE MISSING. REINSTALLED AFT ENTRY DOOR AND FWD AFT GALL EY DOOR ESCAPE SLIDE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998062600917 19980626 00917 NE 1998 6 26 SWAA981119 2 19980609 A 7230 BLADE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE FAILED A A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 375SW 26583 DURING CLIMBOUT, NR 1 ENGINE FAILED AT FL 370, NR 1 ENGINE THREW A FAN BLADE. SHUTDOWN ENGINE AND A/C WAS DIVERTED. AI RCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 ENGINE ASSY PER SRM 385, OPS CHECK NORMAL. ENGINE AND EQU IPMENT SENT FROM PHX. WORK IN PROGRESS. 2 L 7 2 4F 4 F RT A16WE E2GL 1998062600918 19980626 00918 NM 1998 6 26 SWAA981132 1 19980615 A 5210 ANGLE BOEING 737 7373H4 1384600 NM PAX DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED DOOR LINER RETAINER SUPPORT ANGLE, LOWER AFT CORNER. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600919 19980626 00919 NM 1998 6 26 SWAA981133 1 19980615 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND THAT ULTRA SONIC INSP SHOWS 100 PERCENT CRACK INDICATION UNDER STRAP LBL 6.5, WL 213 AT BS 178 BULKHEAD LBL 5, WL 210.5 (UNDER BRKT AND OR STRAP) AT BS 178 BULKHEAD AND LBL 6.5, WL 213 BS 178 BULKHEAD. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600920 19980626 00920 NM 1998 6 26 SWAA981134 1 19980615 A 5312 BLKHD FASTENER BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND THAT EDDY CURRENT SHOWS CRACK AT FASTENER HEAD, FWD SIDE, WL 234, RBL 10 BS 178 BULK HEAD. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600921 19980626 00921 NM 1998 6 26 SWAA981135 1 19980615 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWNS AT BS 787, STR 26R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600922 19980626 00922 NM 1998 6 26 SWAA981136 1 19980615 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM BS 1006 AT FLOOR PANEL HOLE LBL 26. REPAIRED PER BOEING TYPICAL REPAIR TI NR A53-014. 2 L 7 2 4F RT A16WE 1998062600923 19980626 00923 NM 1998 6 26 SWAA981137 1 19980615 A 5320 ANGLE BOEING 737 7373H4 1384600 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED AFT ENTRY DOORWAY AT Z-ANGLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600924 19980626 00924 NM 1998 6 26 SWAA981138 1 19980615 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 429 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM NUT PLATE AT BS 429, RBL 8.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600925 19980626 00925 NM 1998 6 26 SWAA981139 1 19980615 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND HEAVY CORROSION AT BS 1006, STR 27L AND BS 1006, STR 26L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600926 19980626 00926 NM 1998 6 26 SWAA981140 1 19980615 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 987 - 1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED SPLICE PLATE BETWEEN BS 987 AND 1006 AT O/B GALLEY TRACK. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600927 19980626 00927 NM 1998 6 26 SWAA981141 1 19980615 A 5320 CROSS MEMBER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOOR CROSS MEMBER AT BS 1003.5 LBL 10.5, BS 1004 LBL 11.5, BS 1008.5 LBL 7 .5, BS 1010 LBL 8.5 AND BS 1011 LBL 6.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600928 19980626 00928 NM 1998 6 26 SWAA981142 1 19980615 A 5320 CROSS MEMBER BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOOR CROSS MEMBER AT BS 1011 LBL 7.5, BS 1013 LBL 6, BS 998 LBL 13.5, BS 9 99 LBL 11.5 AND 1001 LBL 12. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600929 19980626 00929 NM 1998 6 26 SWAA981143 1 19980616 A 3260 UPLOCK SWITCH BOEING 737 7373Y0 1384671 NM LT MLG MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 699SW 23826 AIR RETURN AFTER TAKEOFF AND GEAR RETRACTION. LEFT MAIN GEAR GREEN LIGHT REMAINED ILLUMINATED, LEFT RED GEAR LIGHT DID NOT EVER ILLUMINATE. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED LT MLG UP AND LOCK SWITCH, DOWN AND LOC K SWITCH AND LT GREEN LIGHT BASE. OPS CHECKED OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998062600930 19980626 00930 NM 1998 6 26 SWAA981144 1 19980616 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM HOLE AT BS 294, LBL 47. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600931 19980626 00931 NM 1998 6 26 SWAA981145 1 19980616 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 328-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED INTERCOSTAL AT CLIP NUT HOLES AT BS 328 TO 344, LBL 10. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600932 19980626 00932 NM 1998 6 26 SWAA981146 1 19980616 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 504/505 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CORROSION UNDER FLOORBEAM NUT PLATE AT BS 504 LBL 13.5, BS 505 LBL 8.5 AND BS 504 RB L 2.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600933 19980626 00933 NM 1998 6 26 SWAA981147 1 19980616 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1136 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED FUSELAGE SKIN AT 2 ADJACENT FASTENERS AT BS 1136, STR 10R. REPAIRED PER BOE ING SRM. 2 L 7 2 4F A16WE 1998062600934 19980626 00934 NM 1998 6 26 SWAA981148 1 19980616 A 5720 ANGLE BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED I/B FLAP WELL LWR SURFACE SUPPORT ANGLE AND WORN JUST ABOVE CANOE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600935 19980626 00935 NM 1998 6 26 SWAA981149 1 19980616 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 967-986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL UPPER AND LOWER SURFACES AT PANEL HOLES RBL 18 FROM BS 967 TO 9 86.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600936 19980626 00936 NM 1998 6 26 SWAA981150 1 19980616 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 827-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND INTERGRANULAR CORROSION AT FLOOR SUPPORT BEAM BS 827 TO 787 ABOVE STR 26R. REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600937 19980626 00937 NM 1998 6 26 SWAA981151 1 19980616 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 747 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWN AT FLOOR SUPPORT BEAM BS 747, STR 26L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600938 19980626 00938 NM 1998 6 26 SWAA981152 1 19980616 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 289 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE ABOVE STR 12, BS 289. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600939 19980626 00939 NM 1998 6 26 SWAA981153 1 19980616 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN 6.5 AFT OF FWD SERVICE DOOR GOUGED BELOW STR 8R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600940 19980626 00940 NM 1998 6 26 SWAA981154 1 19980616 A 5320 FRAME BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FRAME AT FWD LOWER CORNER OF FWD GALLEY DOOR CUTOUT. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998062600941 19980626 00941 NM 1998 6 26 SWAA981155 1 19980616 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND BROKEN INTERCOSTAL AT BS 540, LBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600942 19980626 00942 NM 1998 6 26 SWAA981156 1 19980616 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM HOLE AT BS 344, LBL 9 AND BS 344, RBL 1. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600943 19980626 00943 NM 1998 6 26 SWAA981157 1 19980617 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 540 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN ON TOP OF RT OUTBOARD SEAT TRACK FLOORBEAM DAMAGED/PEELING AT BS 540 JUST FWD O F CENTER. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600944 19980626 00944 NM 1998 6 26 SWAA981158 1 19980617 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 344-360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL FLOORBOARD HOLES AT BS 344 TO 360, RBL 11. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600945 19980626 00945 NM 1998 6 26 SWAA981160 1 19980617 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FASTENER HOLES IN RIGHT TRANSITION ANGLE BETWEEN BS 500 AND 500B. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600946 19980626 00946 NM 1998 6 26 SWAA981159 1 19980617 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED BETWEEN SHEAR TIE AND SKIN AT BS 927 STR 23L TO 24L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600947 19980626 00947 NM 1998 6 26 SWAA981161 1 19980617 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR SUPPORT BEAM AT BS 867, RBL 8.10. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998062600948 19980626 00948 NM 1998 6 26 SWAA981162 1 19980617 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED AND BROKEN CARGO TIE DOWN AT FLOOR SUPPORT BEAM AT BS 787, STR 26L, LBL 17. 20. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600949 19980626 00949 NM 1998 6 26 SWAA981163 1 19980617 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED CLIP AT BS 663R, STR 11 AND BS 663L, STR 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600950 19980626 00950 NM 1998 6 26 SWAA981164 1 19980617 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED INDICATION UNDER ANGLE STIFFENER WL 218, LBL 11 AT BS 178. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998062600951 19980626 00951 NM 1998 6 26 SWAA981165 1 19980617 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 767-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM UPPER AND LOWER SURFACE AT BS 770 LBL 17, FLOORBEAM AT BS 767 TO 787 RBL 13 UPPER SRFC, BS 770 RBL 3 AND BS 787 TO 847 LBL 12. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600952 19980626 00952 NM 1998 6 26 SWAA981166 1 19980617 A 5320 ANGLE BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED ANGLE LT WING TRAILING EDGE O/B OF NR 3 JACKSCREW FAIRING. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600953 19980626 00953 NM 1998 6 26 SWAA981167 1 19980617 A 5320 ANGLE BOEING 737 7373H4 1384600 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED LOWER DOOR LINER ATTACH WEB AT BRACKET FWD CORNER. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600954 19980626 00954 NM 1998 6 26 SWAA981168 1 19980617 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 747-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 727E TO 747, RBL 22 AND BS 747 TO 767, RBL 22. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600955 19980626 00955 NM 1998 6 26 SWAA981169 1 19980618 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 629SW 27704 DURING SERVICE CHECK, FOUND RT OVERWING EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR OVE RWING RT EXIT PER BOEING MM, OPS NORMAL. 2 L 7 2 4F RT A16WE 1998062600956 19980626 00956 1998 6 26 SWAA981171 4 19980618 A 3497 7771825001 WIRE BOEING 737 7373H4 1384600 NM LT HSI LOOSE A QS7R B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 375SW 26583 AIRCRAFT DIVERTED, CAPT HSI HEADING FLAG DISPLAY INTERMITTENTLY, HEADING IS BAD AND HEADING SLEW BUG IS ERRATIC, PLACING COMPASS SWITCH TO BOTH ON NR 2 DOES NOT FIX THE PROBLEM. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED C APT HSI PER BOEING MM AND TIGHTENED LOOSE WIRE ON TRANSFER SWITCH, OPS OK AT THIS TIME. 2 L 7 2 4F RT A16WE 1998062600957 19980626 00957 NM 1998 6 26 SWAA981172 1 19980618 A 5320 TRIPLER BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND TRIPLER CRACKED AT FWD LWR CORNER OF AFT ENTRY DOOR CUTOUT. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1998062600958 19980626 00958 NM 1998 6 26 SWAA981173 1 19980618 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED WEB AFT SIDE OF BLKHD LBL 27, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600959 19980626 00959 NM 1998 6 26 SWAA981174 1 19980618 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 736-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED AFT CARGO FLOOR SUPPORT ZEE ANGLE LBL 21, UPPER SURFACE BETWEEN BS 736 AND BS 9 47. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600960 19980626 00960 NM 1998 6 26 SWAA981175 1 19980618 A 5320 SHEAR WEB BOEING 737 7373H4 1384600 NM BS 472-480 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORROSION AT BS 472 TO 480, RBL 68, WL 208 ON SHEAR WEB. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998062600961 19980626 00961 NM 1998 6 26 SWAA981176 1 19980618 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 967-987 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND FUSELAGE CROWN SKIN HAS A WORN AREA AT BS 967 TO 987, RBL 12 COMMON TO DORSAL FIN, BS 96 7 TO 986 LBL 12, 7, BS 920 TO 967 RBL 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600962 19980626 00962 NM 1998 6 26 SWAA981177 1 19980618 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED D-CHECK, FOUND CORRODED Z-CHORD AT BS 270 RBL 11, LBL 11 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600963 19980626 00963 NM 1998 6 26 SWAA981178 1 19980618 A 5320 ANGLE BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED Z-ANGLE I/B OF FWD GALLEY DOOR THRESHOLD AROUND SCREW HOLES. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600964 19980626 00964 NM 1998 6 26 SWAA981179 1 19980618 A 5320 ANGLE BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR SUPPORT ANGLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600965 19980626 00965 NM 1998 6 26 SWAA981180 1 19980618 A 3350 20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE AND ENTRY DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PA CKS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998062600966 19980626 00966 NM 1998 6 26 SWAA981181 1 19980619 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED BL 0 CABIN FLOORBOARD INTERCOSTAL AT BS 540, LBL 2. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F A16WE 1998062600967 19980626 00967 NM 1998 6 26 SWAA981182 1 19980619 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORROSION UNDER STR SPLICE AT BS 907, STR 24L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600968 19980626 00968 NM 1998 6 26 SWAA981183 1 19980619 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 834 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED BELTFRAME AT BS 834, STR 27R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600969 19980626 00969 NM 1998 6 26 SWAA981184 1 19980619 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 987-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED AFT LAV DOOR SUPPORT INTERCOSTAL BETWEEN BS 987 TO 1006 AND BS 987. REPAIR ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600970 19980626 00970 NM 1998 6 26 SWAA981185 1 19980619 A 5320 ANGLE BOEING 737 7372H4 138448C NM LAV DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED L-ANGLE ON TOP OF AFT LAV DOOR SUPPORT INTERCOSTAL. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1998062600971 19980626 00971 NM 1998 6 26 SWAA981186 1 19980619 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 277-294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FWD END OF INTERCOSTAL AT BS 277 LBL 40, BS 280 LBL 26 AND TOP SIDE AND THE BOTTOM AT BS 277 TO 294 LBL 35. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600972 19980626 00972 NM 1998 6 26 SWAA981187 1 19980619 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 277-294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FWD AND AFT ENDS OF INTERCOSTAL AT BS 277 TO 294, LBL 48. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600973 19980626 00973 NM 1998 6 26 SWAA981188 1 19980619 A 5414 SKIN BOEING 737 7372H4 138448C NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED I/B ENGINE PYLON PANEL ABOVE STATIONARY COWLING. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998062600974 19980626 00974 NM 1998 6 26 SWAA981189 1 19980619 A 5320 ANGLE BOEING 737 7373H4 1384600 NM RT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND I/B ANGLE WORN JUST I/B FROM I/B FOREFLAP. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600975 19980626 00975 NM 1998 6 26 SWAA981190 1 19980619 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986.5-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006 AT PANEL HOLES, BL 0. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600976 19980626 00976 NM 1998 6 26 SWAA981191 1 19980619 A 5320 CHANNEL BOEING 737 7373H4 1384600 NM BS 994 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED HAT CHANNEL AT PANEL HOLES BS 994, LBL 14 TO LBL 44. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600977 19980626 00977 NM 1998 6 26 SWAA981192 1 19980619 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT AFT OF FWD ENTRY DOOR HAS LOOSE LENS. REMOVED AND REP LACED LENS RETAINER ASSY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998062600978 19980626 00978 NM 1998 6 26 SWAA981193 1 19980619 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE AT BS 360 STR 14 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600979 19980626 00979 NM 1998 6 26 SWAA981194 1 19980619 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED STRINGER 14L AT BS 360. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600980 19980626 00980 NM 1998 6 26 SWAA981195 1 19980619 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 847-867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SUPPORT WEB AT BS 847 TO 867, JUST AFT OF DOOR CUTOUT. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600981 19980626 00981 NM 1998 6 26 SWAA981196 1 19980619 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 767-797 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED AND CORRODED SIDEWALL SUPPORT WEB FWD OF DOOR CUTOUT AT BS 767 TO 797. REMO VED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600982 19980626 00982 NM 1998 6 26 SWAA981197 1 19980619 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 312, RBL 7 TO 25 LBL 10 TO 12, WL 207 TO 208. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600983 19980626 00983 NM 1998 6 26 SWAA981198 1 19980620 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294-312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SURFACE ON INTERCOSTAL BETWEEN BS 294 AND 312, RBL 11. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600984 19980626 00984 NM 1998 6 26 SWAA981199 1 19980621 A 5754 SEAL BOEING 737 7373H4 1384600 NM RT LE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C2 CHECK, FOUND K-FLAP BULB SEAL WORN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600985 19980626 00985 NM 1998 6 26 SWAA981200 1 19980621 A 5754 SEAL BOEING 737 7373H4 1384600 NM RT LE FLAP WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED C2 CHECK, FOUND O/B K-FLAP TEFLON RUBSTRIP AND SEAL WORN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600986 19980626 00986 NM 1998 6 26 SWAA981201 1 19980622 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED RON CHECK, FOUND CRACKED SKIN ON LT FUSELAGE AT 48 AFT OF FLAP AND 10 BELOW SKIN LAP JOINT. REPAIRED P ER BOEING SRM. 2 L 7 2 4F A16WE 1998062600987 19980626 00987 NM 1998 6 26 SWAA981202 1 19980622 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED ZEE ANGLE AT BS 270. REPAIRED PER SWA RA NR 1-353-1840. 2 L 7 2 4F RT A16WE 1998062600988 19980626 00988 NM 1998 6 26 SWAA981203 1 19980622 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED A2 CHECK, FOUND 2 INCH CRACK IN WEB AT BS 767, STR 22. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600989 19980626 00989 NM 1998 6 26 SWAA981204 1 19980622 A 5312 BULKHEAD BOEING 737 737301 1384611 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND CRACKED INDICATION NOTED DURING UT, BS 178 BULKHEAD, WL 198.3 TO 202.5, RBL 4.7 AND B S 178, WL 198.0 TO WL 202.5, LBL 4.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998062600990 19980626 00990 NM 1998 6 26 SWAA981205 1 19980619 A 3241 TRANSDUCER BOEING 737 7372H4 138448C NM ANTI-SKID MALFUNCTIONED A SWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 060SW 21812 AIRCRAFT DIVERTED, OUTBOARD ANTI-SKID LIGHT CAME ON AFTER T/O. LIGHT STAYED ON FOR 1 HR. RECYCLED GEAR, NO HELP. LIGH T WENT OUT IN PATTERN AT STL. OK CONT MEL. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED TRANSDUCER PER B OEING MM. 2 L 7 2 4F A16WE 1998062600991 19980626 00991 1998 6 26 SWAA981206 2 19980622 A 7200 65737691 ENGINE BOEING 737 7372H4 138448C NM NR 2 FAILED A A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 057SW 21722 AIR RETURN/INFLT SHUTDOWN WITH NR 2 ENGINE FAILURE. AIRCRAFT MADE AN UNEVENTFUL LANDING. NR 2 ENGINE TAILPIPE EXTENSIO N INNER LINER HAS NUMEROUS DAMAGES. REMOVED AND REPLACED NR 2 ENGINE PER BOEING MM. OPS CK AND LEAK CHECK GOOD PER MM. 2 L 7 2 4F A16WE 1998062600992 19980626 00992 NM 1998 6 26 SWAA981170 1 19980623 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED RON CHECK, FOUND CRACKED NLG WHEEL WELL CEILING PRESSURE BULKHEAD LOCATED AT FWD RT ACCESS PANEL AT AF T I/B CORNER. REPAIRED PER BOEING TI-A53-001. 2 L 7 2 4F A16WE 1998062600993 19980626 00993 EU 1998 6 26 QXEA9800798 1 19980621 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 9 AND 14. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998062600994 19980626 00994 EU 1998 6 26 QXEA9800799 1 19980621 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 CEILING EMERGENCY EXIT SIGN LIGHTS DIM NEXT TO COAT CLOSET. MAINTENANCE RELAMPED AND OPERATIONALY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998062600995 19980626 00995 EU 1998 6 26 QXEA9800800 1 19980622 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 ROW 8 FORWARD 28V EXIT SIGN INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TEST RESULTS NORMAL. 2 L 7 2 4F RT A20EU 1998062600996 19980626 00996 NM 1998 6 26 QXEA9800822 1 19980622 A 2150 78279016 ACM DHAV DHC8 DHC8202 2809007 NM ACM COMPT MALFUNCTION A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 359PH 514 SMOKE SMELL IN COCKPIT AND CABIN. REPLACED AIR CYCLE MACHINE, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998062600997 19980626 00997 NM 1998 6 26 QXEA9800823 1 19980622 A 3350 6101781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 357PH 259 504 RIGHT EGRESS LIGHT INOP. REPLACED EMERGENCY BATTERY PACK, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998062600998 19980626 00998 NM 1998 6 26 RRXA98237 1 19980624 A 2611 SMOKE DETECTOR BOEING 727 727222 1384073 NM CARGO COMPT MALFUNCTIONED A RRXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 15 7635U 19908 CARGO SMOKE LIGHT ILLUMINATED IN FLT. REMOVED CARGO AND PERFORMED MAIN CARGO COMPT, FWD AND AFT BELLY CARGO COMPT. INS PECTED CONTENTS OF ULD'S AND BELLY, NO DEFECTS NOTED. UNABLE TO DUPLICATE. TEST OK. 2 L 7 3 4F A3WE 1998070200001 19980702 00001 NM 1998 7 2 98UAL900199 1 19980515 A 3233 651783013 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7290U 21568 RETURNED TO DEN ACCOUNT UNABLE TO RAISE THE RIGHT MAIN GEAR. *S/D* REPLACED RIGHT GEAR DOOR ACTUATOR, DOOR SEQUENCE VA LVE AND RIGHT MAIN LANDING GEAR RETRACT ACTUATOR. 2 L 7 3 4F 4 F A3WE E2EA 1998070200002 19980702 00002 1998 7 2 98UAL900252 4 19980611 A 2310 HF RADIO BOEING 777 777222 1385219 NM COCKPIT FAILED A UALA A J UNSCHED LANDING DUMP FUEL G MULTIPLE FAILURE CL CLIMB 1 WP 29 788UA 26942 BOTH HIGH FREQUENCY RADIOS FAILED SHORTLY AFTER TAKEOFF. AIRCRAFT RETURNED TO JFK DUE TO INSUFFICIENT ALTERNATIVE ROUTE FUEL. 2 L 7 2 4F RT T0001SE 1998070200003 19980702 00003 NM 1998 7 2 UPS98526992 1 19980620 A 3230 SEQUENCE VALVE BOEING 757 75724APF 1384969 NM NLG FAILED A IPXA K NONE O OTHER TO TAKEOFF 1 SO 01 461UP 28265 INSPECTION TYPE-N/A, NOSE GEAR FAILED TO RETRACT. REMOVED AND REPLACED NOSE SEQUENCE VALVE IAW B757 MM32-34-05. CLEANE D AND LUBED NOSE GEAR RETRACT LINKAGE AND GEAR BUSHINGS PREFORMED NOSE GEAR RETRACTION TEST PER MM 32-34-00. A 21 SECON D RETRACT TIME, SYSTEM CHECKS OK. 2 L 7 2 4F RT A2NM 1998070200006 19980702 00006 NM 1998 7 2 VJ9800197 1 19980618 A 3350 1000679 LIGHT BOEING 737 737214 138446R NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 FOUND EMERGENCY EXIT LIGHT INOP AT L-2 DOOR DURING THE LAYOVER CHECK. REPLACED THE LIGHT ASSY. 2 L 7 2 4F A16WE 1998070200007 19980702 00007 1998 7 2 VJ9800200 4 19980620 A 2565 113317 CABLE DOUG DC9 DC932 3022066 WP ESCAPE SLIDE DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING PREFLIGHT, FOUND THE FWD LOADING DOOR CHUTE CABLE DETACHED. REINSTALLED L-1 DOOR SLIDE IAW MM 25-62-0. 2 L 7 2 4F A6WE 1998070200008 19980702 00008 1998 7 2 DL757981312 4 19980621 A 2565 D30654122 SLIDE BOEING 757 757232 1384965 NM L 1 DOOR MALFUNCTIONED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 618DL 22908 THE LEFT SLIDE INADVERTANTLY DEPLOYED BY FLIGHT CREW. SLIDE DID NOT FULLY INFLATE. REPLACED SLIDE. 2 L 7 2 4F RT A2NM 1998070200009 19980702 00009 WP 1998 7 2 ABXA9800537 1 19980616 A 5610 5613217507 WINDOW DOUG DC9 DC932 3022066 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER UK UNKNOWN 1 GL 23 988AX 47084 CAPTAIN'S SLIDING WINDOW JAMMED WHEN OPENING. CLEANED AND LUBRICATED WINDOW IAW DC9 MM. 2 L 7 2 4F A6WE 1998070200010 19980702 00010 EU 1998 7 2 QXEA9800821 1 19980618 A 3350 1820 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 A 28 VOLT LIGHT INOP IN AFT CEILING EXIT SIGN. RELAMPED SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998070300001 19980703 00001 WP 1998 7 3 EISA98106 1 19980511 A 7332 SWITCH DOUG DC9 DC931 3022065 WP LT ENGINE FAILED A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 943VJ 47058 AFTER TAKEOFF FROM ATLANTIC CITY (ACY), MASTER CAUTION AND LEFT INLET FUEL PRESSURE LOW LIGHT ILLUMINATED. RETURNED TO ACY. INSPECTED LOW INLET FUEL PRESURE SWITCH AND WIRING FOR DEFECTS, NO DEFECTS FOUND. PERFORMED ENGINE RUN. OPS CHEC K GOOD PER MM 73-30-4. (X) 2 L 7 2 4F A6WE 1998070300002 19980703 00002 1998 7 3 98FDEA00415 2 19980624 A 7311 548003 COOLER BOEING 727 72721C 138400M NM NR 1 ENGINE FAILED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 143FE 19136 AFTER TAKEOFF, NR 1 OIL TEMP ENTERED YELLOW BAND (APPROX 140C) OTHER 2 ENGINES REMAINED IN GREEN BAND ENTIRE FLIGHT TEMP REMAINED IN YELLOW UNTIL TOP OF CLIMB FL 290, THEN BEGAN CREEPING HIGHER. CHECKLIST CALLED FOR THROTTLE TO IDLE AND MO NITOR TEMP NEARED RED BAND, THEN LOWERED TO 125 TO 130C AND STABILIZED FOR OVER 15 MORE MIN. CHECKLIST FOLLOWED AND PRE CAUTIONARY SHUTDOWN ACCOMPLISHED. REMOVED AND REPLACED NR 1 ENG FUEL COOLANT OIL COOLER PER M/M 79-20-1. REMOVED AND R EPLACED NR 1 ENG OIL TEMP BULB PER M/M 70-34-21. ALSO, DRAINED OIL AND REPLACED NR 1 ENG OIL FILTER AND RESERVICED WITH OIL PER M/M 79-00. GROUND RAN, GOOD TEMP WERE NORMAL, NO LEAKS NOTED AT THIS TIME. 2 L 7 3 4F A3WE 1998070300003 19980703 00003 WP 1998 7 3 98FDEA00416 1 19980623 A 5297 WIRE DOUG DC10 DC1010F 3022111 WP AC DOOR BROKEN A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 052FE 47806 AIR COND DOORS LIGHT ILLUMINATED INFLIGHT, RED TABS COMPLETED AND DIVERTED INTO KSLC. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL: 52-4D. CHECKED AIR CONDITIONING DOORS. ALL DOORS POSITIVELY CLOSED AND LOCKED. REPLACED LEFT AFT DOOR SWITC H, NO HELP. FOUND BROKEN WIRE ON NR2 LEAD. REPAIRED BROKEN WIRE, OPS CHECK GOOD. 2 L 7 3 4F A22WE 1998070300004 19980703 00004 WP 1998 7 3 ABXA9800541 1 19980625 A 3260 7000010101 SWITCH DOUG DC9 DC933F 302207A WP NLG INTERMITTENT A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 934AX 47462 FIRST ATTEMPT ON FINAL, NO NOSE GEAR DOWN AND LOCKED GREEN LIGHT. RECYCLED GEAR OBTAINED ALL THREE GEAR GREEN LIGHTS. R EPLACED NOSE GEAR DOWNLOCK POSITION SWITCH. 2 L 7 2 4F A6WE 1998070300005 19980703 00005 WP 1998 7 3 MWEA98755 1 19980624 A 5400 99581913 CHANNEL DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACK ON RIGHT PYLON 2 CHANNEL FORWARD OF AFT ENGINE MOUNT. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998070300006 19980703 00006 WP 1998 7 3 MWEA98756 1 19980624 A 5320 991016461 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 718 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACKED INTERCOSTAL ON LEFT WHEEL WELL STATION 718 AFT SIDE. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1998070300007 19980703 00007 WP 1998 7 3 MWEA98757 1 19980624 A 5320 591013037 ANGLE DOUG DC9 DC932 3022066 WP VENTRAL DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACK ON VENTRAL DOOR JAMB CUTOUT THRESHOLD SUPPORT ANGLE. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998070300008 19980703 00008 WP 1998 7 3 MWEA98758 1 19980624 A 5347 995787111 SEAT TRACK DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CAPTAINS AFT OUTBOARD SEAT TRACK WORN BEYOND LIMITS. MTC FABRICATED AND INSTALLED SEAT TRACK. 2 L 7 2 4F A6WE 1998070300009 19980703 00009 WP 1998 7 3 MWEA98759 1 19980624 A 5512 SKIN DOUG DC9 DC982 3022082 WP HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CORROSION ON HORIZONTAL STABILIZER CENTER SECTION LOWER PLATING. MTC REMOVED CORROSION AND FABRICATED AND INSTALL ED REPAIR STRAP. 2 L 7 2 4F A6WE 1998070300010 19980703 00010 WP 1998 7 3 MWEA98760 1 19980624 A 5313 S27779223 LONGERON DOUG DC9 DC982 3022082 WP BS 275 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CRACK ON LONGERON AT STATION 275 IN THE LOWER FLANGE. MTC FABRICATED AND INSTALLED REPAIR SPLICES AND LONGERON. 2 L 7 2 4F A6WE 1998070300011 19980703 00011 NM 1998 7 3 DL72S981322 1 19980622 A 3230 65404676 ACTUATOR BOEING 727 727232 1384082 NM NLG BROKEN A DALA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 27 526DA 21586 NOSE GEAR WOULD NOT GO DOWN AND LOCKED WHEN GEAR EXTENDED. FOLLOWED LANDING GEAR EXTENSION MALFUNCTIONS PER POM. GEAR CAME DOWN AND LOCKED WITH MANUAL EXTENSION NOSE GEAR. FOUND UPLOCK CYLINDER ROD END PULLED OUT. REPLACED UPLOCK CYLIND ER AND PERFORMED NOSE GEAR RETRACT AND LEAK CK. ALL CKS OK. 2 L 7 3 4F A3WE 1998070300012 19980703 00012 NE 1998 7 3 DLM88981324 2 19980623 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 960DL 14847 49979 726907 JUST AFTER LIFTOFF, RT OIL STRAINER CLOGGED ON AND RT OIL TEMP ROSE TO 120 AND CONTINUED TO CLIMB. SHUT DOWN RT ENGINE. FOUND METAL IN MAIN OIL FILTER AND CHIP DETECTOR FOR NR 3 BEARING. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1998070300013 19980703 00013 WP 1998 7 3 DLL17981326 1 19980623 A 3350 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 769DL 193H1218 AFT LEFT HAND EMERGENCY TRACK LIGHTING WAS INOP. CHANGED THE ADDITIONAL POWER SUPPLY AND THE REGULAR POWER SUPPLY. 2 L 7 3 4F A23WE 1998070300014 19980703 00014 WP 1998 7 3 DLL13981327 1 19980621 A 3520 TIMER 25720481 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 786DL 193A1123 MASKS DID NOT DROP IN D-ZONE DURING OXY DROP CHECK. REPLACED SEQUENCING TIMER (P/N 25720481) OPS CHECK GOOD. 2 L 7 3 4F A23WE 1998070300015 19980703 00015 NM 1998 7 3 DL72S981328 1 19980623 A 5720 BEAM BOEING 727 727225 1384077 NM LT WING CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8873Z 21291 MLG STRUT DOOR CHAFING ON MLG BEAM 4 FEET I/B OF MLG STRUT. REPAIRED PER MM 57-43-0 PG 801. 2 L 7 3 4F A3WE 1998070300016 19980703 00016 WP 1998 7 3 DLL10981329 1 19980623 A 3397 WIRE LKHEED 1011 10113851 5265010 WP CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1731D 193C1200 EMERGENCY LIGHTS AT L2 R2 X-AISLE INOP. REPAIRED BROKEN WIRE AND OPS NORMAL. 2 L 7 3 4F A23WE 1998070300017 19980703 00017 NM 1998 7 3 DL757981330 1 19980624 A 2530 OVEN BOEING 757 757232 1384965 NM NR 2 GALLEY DIRTY A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 627DL 22917 FLIGHT ATTENDANT REPORTED SMELL OF SMOKE TAXIING OUT SLC. RETURNED TO GATE. CHECKED OVENS AND COFFEEMAKERS IN QUESTION , FOUND BURNED TAPE IN NR 2 OVEN CENTER GALLEY FOOD CARRIER. ALSO, CHECKED FWD BAG BIN, NO ODORS NOTED. 2 L 7 2 4F RT A2NM 1998070300018 19980703 00018 NE 1998 7 3 DLM88981331 2 19980624 A 7200 JT8D219 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 905DL 18025 49536 725817 DURING FLT, NR 1 ENG COMPRESSOR STALLED AND ROLLED BACK. THIS WAS PROCEEDED BY A SINGLE CHUG AT APPROX FL 140 AND 280 K TS IN THE CLIMB. ENG SHUTDOWN IN FLT AND RETURNED TO BASE. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1998070300019 19980703 00019 NM 1998 7 3 DL75A981332 1 19980624 A 2560 SLIDE BOEING 757 757212 NM 3R DOOR OUT OF POSITION A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 750AT 23126 AFTER T/O, R AFT ENTRY DOOR LIGHT CAME ON. F/A TRIED TO GET HANDLE TO LOCK DOWN, NO LUCK. RETURNED TO ATL. FOUND 3R D OOR SLIDE SHIFTED OFF FWD SUPPORT. REPOSITIONED SLIDE, DOOR CLOSES NORM. 2 L 7 2 4F RT A2NM 1998070300020 19980703 00020 NM 1998 7 3 SCNA98710 1 19980620 A 5311 FRAME BOEING 727 7272J4 1384006 NM BS 303.9 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 285SC 21676 DURING A HEAVY MAINT CHECK, A CRACK 3 INCHES LONG RUNNING FORE TO AFT WAS FOUND IN THE MAIN CABIN FLOORBOARD FRAME AT ST A 303.9 LBL 55. MATERIAL WAS VERIFIED AS 7075 T6 .040. FABED FLOORBOARD FRAME PER SRM 512002. TREATED PER SRM 511002, PRIMED PER MM 512000, INSTALLED. 2 L 7 3 4F RT A3WE 1998070300021 19980703 00021 NM 1998 7 3 P5CA9801022 1 19980623 A 5512 SKIN BOEING 747 747123 1384873 NM RT HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND ON RIGHT HAND HORIZONTAL STABILIZER LOWER SURFACE AT LEADING EDGE STA 260. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300022 19980703 00022 NM 1998 7 3 P5CA9801023 1 19980623 A 5330 PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE BODY FAIRING NR 191BB FOUND CORRODED IN DRAIN LINE AREA. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51- 10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300023 19980703 00023 NM 1998 7 3 P5CA9801024 1 19980623 A 5320 BRACKET BOEING 747 747123 1384873 NM BS 1000-1235 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE STATION 1000 TO 1235 KEEL BEAM AREA LOWER ACCESS PANEL SUPPORT BRACKET FOUND CORRODED. CORROSION AND AREA REPR OTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300024 19980703 00024 NM 1998 7 3 P5CA9801025 1 19980623 A 5320 STIFFENER BOEING 747 747123 1384873 NM BS 1014 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION ON KEEL BEAM VERTICAL STIFFENER. REMOVED AND RETREATED CORROSION IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300025 19980703 00025 NM 1998 7 3 P5CA9801026 1 19980623 A 5320 FITTING BOEING 747 747123 1384873 NM R1 DOORWAY CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 MAIN DECK R1 DOOR SILL FLOOR SUPPORT FITTING FOUND CORRODED. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300026 19980703 00026 NM 1998 7 3 P5CA9801027 1 19980623 A 5320 PLATE BOEING 747 747123 1384873 NM BS 1283 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 MAIN DECK BS 1283 BL 100L FLOOR SUPPORT PLATE FOUND CORRODED. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01 A ND 51-10-02. 2 L 7 4 4F A20WE 1998070300027 19980703 00027 NM 1998 7 3 P5CA9801028 1 19980623 A 5280 DOOR BOEING 747 747123 1384873 NM RT MLG CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT WING O/B STRUT DOOR LOWER SURFACT AREA CORROSION. TREATED AREA AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300028 19980703 00028 NM 1998 7 3 P5CA9801029 1 19980623 A 5320 ANGLE BOEING 747 747123 1384873 NM R3 DOORWAY CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 MAIN DECK R3 DOOR SILL FLOOR SUPPORT ANGLE FOUND CORRODED. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 A ND 51-10-02. 2 L 7 4 4F A20WE 1998070300029 19980703 00029 NM 1998 7 3 P5CA9801030 1 19980623 A 5512 SKIN BOEING 747 747123 1384873 NM HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LT HORIZONTAL STAB LOWER SURFACE CORROSION REVEAL AT AREA JUST BELOW AFT OF LOWER AIR GATE SEAL FAIRING STA 2600. CORRO SION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300030 19980703 00030 NM 1998 7 3 P5CA9801031 1 19980623 A 5350 SKIN BOEING 747 747123 1384873 NM TAIL CONE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 TAIL CONE AREA CORROSION REVEALED AT FORWARD AREA OF APU BATTERY ACCESS DOOR STA 2600. CORROSION AREA REMOVED AND REPRO TECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300031 19980703 00031 NM 1998 7 3 P5CA9801032 1 19980623 A 5320 RIVET BOEING 747 747123 1384873 NM BS 920 SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FWD CARGO COMPARTMENT STA 920 FLOORBEAM WEB VERTICAL SUPPORT FOUND 3 RIVETS SHEARED. REPLACED RIVETS AS PER SRM 51-30-0 3. 2 L 7 4 4F A20WE 1998070300032 19980703 00032 NM 1998 7 3 P5CA9801033 1 19980623 A 5330 SKIN BOEING 747 747123 1384873 NM BS 2460-2484 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT UPPER TAIL CONE AREA CORROSION REVEALED AT STA 2460 TO 2484. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300033 19980703 00033 NM 1998 7 3 P5CA9801034 1 19980623 A 5512 SKIN BOEING 747 747123 1384873 NM RT HORIZ STAB CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT HORIZONTAL STAB UPPER SURFACE CORROSION REVEALED. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300034 19980703 00034 NM 1998 7 3 P5CA9801035 1 19980623 A 5314 KEEL BEAM BOEING 747 747123 1384873 NM BS 1427 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION ON KEEL BEAM CHORD UPPER EDGE BS 1427 BL 10. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 5 1-10-02. 2 L 7 4 4F A20WE 1998070300035 19980703 00035 NM 1998 7 3 P5CA9801036 1 19980623 A 5320 RIVET BOEING 747 747123 1384873 NM BS 960 MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FOUR RIVETS FOUND NOT INSTALLED AT FWD CARGO COMPT STA 960 FLOORBEAM UPPER CHORD, BL 0 AND BL 6. INSTALLED RIVETS AS PE R SRM 51-30-02. 2 L 7 4 4F A20WE 1998070300036 19980703 00036 NM 1998 7 3 P5CA9801037 1 19980623 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 600 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION AT UPPER DECK SEAT TRACK BS 600 BL 46L. REMOVED AND REPROTECTED SEAT TRACK PER SRM 51-10-01 AND 51-10 -02. 2 L 7 4 4F A20WE 1998070300037 19980703 00037 NM 1998 7 3 P5CA9801038 1 19980623 A 5330 SKIN BOEING 747 747123 1384873 NM BS 1740 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE RIGHT HAND STATION 1740 AT S44 FOUND SKIN DAMAGED. SKIN REPAIRED AS PER SRM 53-30-03. 2 L 7 4 4F A20WE 1998070300038 19980703 00038 NM 1998 7 3 P5CA9801039 1 19980623 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 2280 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROISON ON MAIN DECK SEAT TRACK UPPER SURFACE AT BS 2280. REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10- 02. 2 L 7 4 4F A20WE 1998070300039 19980703 00039 NM 1998 7 3 P5CA9801040 1 19980623 A 5330 PANEL BOEING 747 747123 1384873 NM FUSELAGE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT FUSELAGE ACCESS PANEL 193P INNER FACE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 5 1-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300040 19980703 00040 NM 1998 7 3 P5CA9801041 1 19980623 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT STA 1720 TO 1740 AFT CARGO AREA LEFT HAND STRINGER 47. CORROSION REMOVED AND AREA REPROTEC TED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300041 19980703 00041 NM 1998 7 3 P5CA9801042 1 19980623 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT STA 1700 TO 1720 AFT CARGO AREA S51L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300042 19980703 00042 NM 1998 7 3 P5CA9801043 1 19980624 A 5280 DOOR BOEING 747 747123 1384873 NM RT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RIGHT WING GEAR OUTBOARD STRUT DOOR FOUND CORROSION AT FASTENERS ON LOWER SIDE OF UPPER DOOR. CORROSION REMOVED AND ARE A REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300043 19980703 00043 NM 1998 7 3 P5CA9801044 1 19980623 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1900 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT AFT CARGO AREA STA 1900 TO 1920 STRINGER 46L. CORROSION REMOVED AND AREA REPROTECTED AS PE R SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300044 19980703 00044 NM 1998 7 3 P5CA9801045 1 19980623 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1700 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT AFT CARGO AREA STA 1700 TO 1720 STRINGER 43L LOWER SURFACE. CORROSION REMOVED AND AREA REP ROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300045 19980703 00045 NM 1998 7 3 P5CA9801046 1 19980623 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT AFT CARGO AREA STA 1820 TO 1840 STRINGER S46L. CORROSION REMOVED AND AREA REPROTECTED AS P ER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300046 19980703 00046 NM 1998 7 3 P5CA9801047 1 19980623 A 5330 SKIN BOEING 747 747123 1384873 NM BS 940 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT SATELLITE COMMUNICATIONS ANTENNA SURROUNDING SKIN AT FS 940. CORROSION REMOVED AND AREA RE PROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300047 19980703 00047 NM 1998 7 3 P5CA9801048 1 19980623 A 5330 PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT PANEL 191J UPPER SURFACE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 5 1-10-02. 2 L 7 4 4F A20WE 1998070300048 19980703 00048 NM 1998 7 3 P5CA9801049 1 19980623 A 5330 PANEL BOEING 747 747123 1384873 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT PANEL 191G. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300049 19980703 00049 NM 1998 7 3 P5CA9801050 1 19980623 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT BS 1720 STRINGER 47L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10 -02. 2 L 7 4 4F A20WE 1998070300050 19980703 00050 NM 1998 7 3 P5CA9801051 1 19980622 A 5330 PANEL BOEING 747 747123 1384873 NM BS 1112 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT PANEL 191EL LOWER SURFACE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300051 19980703 00051 NM 1998 7 3 P5CA9801052 1 19980622 A 5320 BRACKET BOEING 747 747123 1384873 NM BS 2080 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 STATION 2080 AFT FRAME SUPPORT BRACKET FOUND CRACKED. BRACKET REPLACED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998070300052 19980703 00052 NM 1998 7 3 P5CA9801053 1 19980622 A 5320 FASTENER BOEING 747 747123 1384873 NM BS 140 RUSTY A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE STATION 140 STR 23L FOUND 6 FASTENERS RUSTY. FASTENERS REPLACED AS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998070300053 19980703 00053 NM 1998 7 3 P5CA9801054 1 19980622 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 480-630 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT UPPER DECK SEAT TRACK BS 480 TO 630 LBL 64. CORROSION REMOVED AND AREA REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300054 19980703 00054 NM 1998 7 3 P5CA9801055 1 19980623 A 5347 SEAT TRACK BOEING 747 747123 1384873 NM BS 2276 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT MAIN DECK SEAT TRACK STATION 2276. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10 -01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300055 19980703 00055 NM 1998 7 3 P5CA9801056 1 19980623 A 5320 SUPPORT BOEING 747 747123 1384873 NM BS 1860-1920 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL ONE CORROSION FOUND AT STA 1860 TO 1920 AFT CARGO AREA FLOOR PANEL SUPPORT STRUCTURE. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300056 19980703 00056 NM 1998 7 3 P5CA9801057 1 19980624 A 5320 SHEAR TIE BOEING 747 747123 1384873 NM BS 1720 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 STATION 1720 AFT CARGO AREA RT S48-49 SHEAR TIE FOUND CRACKED. REPAIRED AS PER SRM 53-10-04. 2 L 7 4 4F A20WE 1998070300057 19980703 00057 NM 1998 7 3 MALA976154 1 19980622 A 6120 SELECT SWITCH DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 848MA 346 AUTOFEATHER COULD NOT BE DISARMED AFTER TAKEOFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED AUTOFEATHER SELECT SWI TCH. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998070300058 19980703 00058 EU 1998 7 3 MALA976155 1 19980622 A 3230 M8353660222 RELAY SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 418XJ 418 ON DESCENT, HYDRAULIC LANDING CONTROL BREAKER POPPED REPEATEDLY, USED THE EMERGENCY GEAR EXTENSION QRH PROCEDURE TO EXTE ND GEAR, LANDING WITHOUT INCIDENT. MAINTENANCE REPLACED RELAY AND CONNECTOR 15GA AND 15GAJ1, REPLACED SEPARATION BOLTS. ALL CHECKS GOOD PER SF3 AMM 32-30-00. 2 L 7 2 4T RT A52EU 1998070300059 19980703 00059 EU 1998 7 3 MALA976156 1 19980623 A 3350 66902 LIGHT SAAB SF340 340B 7860101 EU CABIN BROKEN A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING WALKAROUND, FLOOR TRACK LIGHTING STRIP BROKEN. MAINTENANCE REPLACED EMERGENCY FLOOR TRACK LIGHTING STRIP. ALL C HECKS GOOD. 2 L 7 2 4T RT A52EU 1998070300060 19980703 00060 NM 1998 7 3 M8XA9800012 1 19980522 A 2131 22260A020201 CONTROLLER ABG SECMA 22260A020201 DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE COCKPIT DEFECTIVE A M8XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 331MX 16402 205 3074 SHORTLY AFTER T/O, THE FLIGHT CREW REPORTED A PROBLEM WITH THE AIRCRAFT PRESSURIZATION SYSTEM. AIRCRAFT WOULD NOT PRESS URIZE IN AUTO OR MANUAL MODE. AIRCRAFT RETURNED TO THE FIELD LANDED WITHOUT FURTHER INCIDENT. DENVER MX PERSONNEL REPL ACED THE CABIN PRESSURIZATION CONTROL UNIT IAW AMM 21-31-00 OPERATIONAL CHECK WAS CONDUCTED WITH SATISFACTORY RESULTS. A IRCRAFT WAS THEN RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998070300061 19980703 00061 SO 1998 7 3 RAAA98E8020 1 19980623 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FWD RT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998070300062 19980703 00062 NM 1998 7 3 CALA9801157 1 19980623 A 3350 6013211 POWER SUPPLY BOEING 737 737130 1384435 NM CARGO COMPT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14206 19023 INSPECTION FOUND FORWARD ENTRY AND SERVICE DOOR EMERGENCY EXIT LIGHTS INOPERATIVE. THE BATTERY PACK/POWER SUPPLY WAS RE MOVED AND REPLACED. 2 L 7 2 4F A16WE 1998070300063 19980703 00063 NM 1998 7 3 CALA9801158 1 19980623 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND SEAT TRACK CORRODED AT FS 328-344. THE CORRODED SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 53 -00-52. 2 L 7 2 4F RT A16WE 1998070300064 19980703 00064 NM 1998 7 3 CALA9801159 1 19980623 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 927 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND OUTBOARD SEAT TRACK CORRODED AT STA 927, RBL 48, WL 208.1. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-5 2, FIGURE 204, SHEET 1-4 AND SRM 51-30-00. 2 L 7 2 4F RT A16WE 1998070300065 19980703 00065 WP 1998 7 3 CALA9801160 1 19980624 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 484 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12538 47218 INSPECTION FOUND A 2.5 CRACK IN FORWARD PIT FRAME AT STA 484 BETWEEN STRINGER 26L AND 27L. THE CRACKED AREA OF FRAME WA S CUT OUT IAW ECRA 5320-01263. A NEW SECTION OF FRAME WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998070300066 19980703 00066 NM 1998 7 3 CALA9801161 1 19980624 A 5330 PANEL BOEING 737 7373T0 1384582 NM BS 847-867 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND RT TRANSITION PANEL CORRODED AT STA 847-867. THE TRANSITION PANEL WAS REMOVED AND REPLACED IAW SRM 51- 10-2. 2 L 7 2 4F RT A16WE 1998070300067 19980703 00067 NM 1998 7 3 CALA9801162 1 19980625 A 3260 CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM E/E COMPT TRIPPED A CALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 09 17326 23456 WHEN LANDING GEAR WAS EXTENDED ON FINAL APPROACH TO IAH NO GREEN DOWN AND LOCKED INDICATIONS WERE ILLUMINATED FOR ALL TH REE GEAR. THE CHECKLIST WAS RUN DURING AN ABORTED APPROACH AND THE AIR/GROUND RELAY CIRCUIT BREAKER WAS FOUND POPPED. T HE CIRCUIT BREAKER WAS RESET AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF LOGI C CIRCUITS IAW MM 32-09-20 AND ALL SYSTEMS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998070300068 19980703 00068 NM 1998 7 3 CALA9801163 1 19980624 A 5320 CHANNEL BOEING 737 7373T0 1384582 NM BS 294-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12349 23587 INSPECTION FOUND R-1 DOOR Z-CHANNEL CORRODED AT STA 294-328. THE Z-CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F RT A16WE 1998070300069 19980703 00069 NM 1998 7 3 CALA9801164 1 19980624 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 917 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED AT STA 917, LBL 24. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53- 00-52, FIGURE 204. 2 L 7 2 4F RT A16WE 1998070300070 19980703 00070 NM 1998 7 3 CALA9801165 1 19980625 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 907-937 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 907-937, RBL 24. A NEW SECTION OF SEAT TRACK WAS SPLICED IN IAW SRM 53-00-52, FIGURE 204. 2 L 7 2 4F RT A16WE 1998070300071 19980703 00071 NM 1998 7 3 CALA9801166 1 19980625 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND L-2 DOOR THRESHOLD SUPPORT Z-ANGLE CORRODED AT STA 967, LBL 46, WL 208. THE Z-ANGLE WAS REPLACED IAW S RM 51-10-2. 2 L 7 2 4F RT A16WE 1998070300072 19980703 00072 NM 1998 7 3 CALA9801167 1 19980625 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND FLOORBEAM CORRODED AT FORWARD ENTRY, STA 312, RBL 21. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998070300073 19980703 00073 NM 1998 7 3 CALA9801168 1 19980625 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 312-340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND Z-ANGLE CORRODED AT FORWARD ENTRY, LT SIDE, STA 312-340. A NEW Z-ANGLE WAS INSTALLED IAW SRM 53-10-2. 2 L 7 2 4F RT A16WE 1998070300074 19980703 00074 NM 1998 7 3 CALA9801169 1 19980626 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 967-996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND CORROSION AROUND FASTENER HOLES OF R-2 DOOR THRESHOLD Z-ANGLE FROM STA 967 TO 996, LBL 48, WL 208.1. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1998070300075 19980703 00075 NM 1998 7 3 CALA9801170 1 19980626 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND FLOORBEAM CAP CORRODED AT STA 986 FROM RBL 0 TO RBL 46. THE FLOORBEAM WAS REPAIRED IAW ECRA 5310-03450 . 2 L 7 2 4F RT A16WE 1998070300076 19980703 00076 WP 1998 7 3 9809589885 1 19980621 A 3231 RETRACT MECH DOUG DC9 DC951 3022051 WP MLG DOORS OUT OF ADJUST A NWAA K NONE J WARNING INDICATION CL CLIMB 1 GL 01 401EA 47682 AFTER TAKEOFF, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE FLIGHT CREW FOL LOWED COM PROCEDURES AND LANDED AT MEM WITH LANDING GEAR DOOR EXTENDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AND RIGHT MAIN LANDING GEAR DOORS AND RIGGED SYSTEM PER MM PROCEDURES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998070300077 19980703 00077 SO 1998 7 3 COMA9810141 1 19980624 A 5320 12005805003 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 17584 120238 DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP . THE BUTT-STRAP WAS REPLACED PER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998070300078 19980703 00078 SO 1998 7 3 COMA9810142 1 19980624 A 5320 12006962001 TEE SECTION EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 17584 120238 DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE LEFT HAND T-SECTI ON AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998070300079 19980703 00079 SO 1998 7 3 COMA9810143 1 19980624 A 5320 12008896001 TEE SECTION EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 17584 120238 DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE RIGHT HAND T-SECT ION AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998070300080 19980703 00080 SO 1998 7 3 COMA9810144 1 19980624 A 5320 12007089003 STRAP EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 17584 120238 DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP . THE BUTT STRAP WAS REPLACED PER AERODESIGN REPORT NR 1671-1, REV A, 1-28-97. 2 L 7 2 4T RT A31SO 1998070300081 19980703 00081 SO 1998 7 3 COMA9810145 1 19980624 A 5320 12005807007 BEAM EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 255CA 17584 120238 DURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER OMEGA BEAM . THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NR 1957-5, REV IR, 6-23-98. 2 L 7 2 4T RT A31SO 1998070300082 19980703 00082 SO 1998 7 3 COMA9810146 1 19980623 A 2752 3203001005 ACTUATORS EMB 120 EMB120RT SO TE FLAPS MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 196CA 4652 120196 INBOARD FLAPS ASYMMETRY WARNING DURING TAKEOFF. REPLACED THE INBOARD FLAPS ACTUATORS. 2 L 7 2 4T RT A31SO 1998070300083 19980703 00083 SO 1998 7 3 COMA9810147 1 19980624 A 5270 12042482001 ROCKERS EMB 120 EMB120RT SO CARGO DO0R OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 01 257CA 120248 AFTER TAKEOFF CARGO DOOR AURAL WARNING SOUNDED. ADJUSTED THE DOOR WARNING SWITCH ROCKERS. 2 L 7 2 4T RT A31SO 1998070300084 19980703 00084 EA 1998 7 3 COMA9860159 1 19980622 A 3010 601R593201 SWITCH CNDAIR CL600 CL6002B19 EA LT WING MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 710CA 7241 ANTI-ICE DUCT LEAK WARNING. COULD NOT DUPLICATE DISCREPANCY. TROUBLE SHOOTING FOUND NO DEFECTS. REPLACED MID WING LEA K SENSORS FOR TROUBLE SHOOTING. 2 L 7 2 4F RT A21EA 1998070300085 19980703 00085 EA 1998 7 3 COMA9860160 1 19980623 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTION A COMA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SO 01 965CA 4985 240 7131 DURING TAKEOFF, CONFIG WARNING, SPOILERONS CAUTION MESSAGE. REPLACED THE NR 1 SECU. 2 L 7 2 4F RT A21EA 1998070300086 19980703 00086 NM 1998 7 3 UPS98227020 1 19980616 A 5520 BRACKET BOEING 727 72722C 138400F NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C ANGLE BRACKET CRACKED ON RT ELEVATOR AFT OF REAR SPAR INBD OF NR 5 TAB HINGE. ANGLE BRACKET REPLACED IAW DRAWING NO 69-19144. 2 L 7 3 4F A3WE 1998070300087 19980703 00087 NM 1998 7 3 UPS98227021 1 19980615 A 2782 SLAT BOEING 727 72722C 138400F NM ACTUATOR DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, NR 5 SLAT O/B ACTUATOR RIB DAMAGED. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998070300088 19980703 00088 NM 1998 7 3 UPS98227022 1 19980615 A 5754 SLAT BOEING 727 72722C 138400F NM NR 5 LE SLAT DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C, NR 5 SLAT I/B ACTUATOR RIB DAMAGED. REPAIR CARRIED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998070300089 19980703 00089 NM 1998 7 3 UPS98227023 1 19980617 A 5400 WEB BOEING 727 72722C 138400F NM BS 1381 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE: C, CRACK ON WEB ABOVE NR 2 ENG HORIZONTAL FIREWALL RT SIDE AT STA 1381. WEB FABRICATED AND INSTALLED I AW DRAWING 65-17555. 2 L 7 3 4F A3WE 1998070300090 19980703 00090 NM 1998 7 3 UPS98227039 1 19980625 A 3350 9621015 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 L1 FWD LOWER EEL REMAINS ON AT ALL TIMES. REMOVED AND REPLACED EXIT LT BATT PACK. OPS CK OK P/N ON AND OFF 96-2-1015 S N ON TAG 315525 OFF TAG 937150. 2 L 7 3 4F A3WE 1998070300091 19980703 00091 NM 1998 7 3 UPS98227040 1 19980625 A 2613 65249203 OVERHEAT DET BOEING 727 72725C 138400H NM E/E COMPT MALFUNCTIONED A IPXA K NONE N FALSE WARNING DE DESCENT 1 SO 01 950UP 19718 PASSING 10,000 FT ON CLIMB-OUT, WHEEL WELL LIGHT FLASHED AND BELL RANG MOMENTARILY. PASSING 7,000 FT ON DESCENT, CAME O N AND STAYED ON UNTIL GEAR WAS EXTENDED. MEASURED BRAKE TEMPERATURE AT BLOCK-IN AND NO HOT BRAKE WAS NOTED. INSPECTED ALL WHEEL WELLS WITH NO DEFECTS NOTED. RAN ENGINES AND NO LEAKS WERE NOTED IN WHEEL WELL DUCTS. WILL REMOVED AND REPLA CED FIRE AND OVERHEAT DETECTOR ACCESSORY UNIT, PRECAUTIONARY. 2 L 7 3 4F A3WE 1998070300092 19980703 00092 WP 1998 7 3 UPS98827024 1 19980615 A 5320 36410042N FITTING DOUG DC8 DC871F 302199D WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 879 AT LONG 24R, THE CUSP TIE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3 641004 AND SRM 53-2-0 FIG 8. 2 L 7 4 4F RT 4A25 1998070300093 19980703 00093 WP 1998 7 3 UPS98827025 1 19980608 A 5320 5641007501 FITTING DOUG DC8 DC871F 302199D WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D LTH MAIN DECK FLOORBEAM END FITTING IS CRACKED AT STA 781 AND 21L. REMOVED AND REPLACED FITTING IAW D WG 5641007 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300094 19980703 00094 WP 1998 7 3 UPS98827026 1 19980603 A 5400 5803961503 ANGLE DOUG DC8 DC871F 302199D WP NR 1 PYLON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, THE NR 1 PYLON OUTBOARD ANGLE DOUBLER AT THE FRONT SPAR IS CRACKED. REMOVED FABRICATED AND REPLACED ANGLE IAW DWG 5803961 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998070300095 19980703 00095 WP 1998 7 3 UPS98827027 1 19980606 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 1580L, FRAME IS CRACKED IN 2 PLACES AT STR 21L. REPAIRED AREA IAW SRM 53-4-1 FIG 51. 2 L 7 4 4F RT 4A25 1998070300096 19980703 00096 WP 1998 7 3 UPS98827028 1 19980604 A 5347 5759223501 TRACK DOUG DC8 DC871F 302199D WP BS 1320-1400 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 1320-1400 ABOVE STR 33R, THE CARGO TRACK AND SPLICE BLOCK HAVE HEAVY CORROSION. REMOVED, FABRICAT ED AND REPLACED TRACK AND BLOCK IAW DWG 5759223. 2 L 7 4 4F RT 4A25 1998070300097 19980703 00097 WP 1998 7 3 UPS98827029 1 19980603 A 5311 5764343509 FRAME DOUG DC8 DC871F 302199D WP BS 1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 1100 AT LONG 36 THE FRAME UPPER CAP HAS HEAVY CORROSION. REMOVED AND REPLACED CAP IAW DWG 5764343 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300098 19980703 00098 WP 1998 7 3 UPS98827030 1 19980606 A 5320 37540432D FITTING DOUG DC8 DC871F 302199D WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 1180 AT STR 21R, THE FRAME TO CUSP TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3 754043 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300099 19980703 00099 WP 1998 7 3 UPS98827031 1 19980611 A 5730 DOUBLER DOUG DC8 DC871F 302199D WP WS 22.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, LT WING FUEL ACCESS PANEL DOUBLED (LANDING) IS CRACKED IN 3 PLCS REF STA. XRS 22.750 AND STR.6. REPA IRED AREA IAW SRM 57-2-1 FIG 36. 2 L 7 4 4F RT 4A25 1998070300100 19980703 00100 WP 1998 7 3 UPS98827032 1 19980616 A 5320 4758514505 FITTING DOUG DC8 DC871F 302199D WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 1240 BTWN STR 32R-33R, THE INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AN D REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300101 19980703 00101 WP 1998 7 3 UPS98827033 1 19980603 A 5320 37558451N FITTING DOUG DC8 DC871F 302199D WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D C-3 DOOR FWD TORQUE BOX FWD. SHEAR TIE HAS HEAVY CORROSION STA 1180 BTWN STR 35R-36. REMOVED AND RE PLACED FITTING IAW DWG 3755845 AND SRM 53-2-0 FIG. 2D. 2 L 7 4 4F RT 4A25 1998070300102 19980703 00102 WP 1998 7 3 UPS98827034 1 19980615 A 5320 5716454293 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1038 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D INTERCOSTAL AT STA 1038 AND STR 35R HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5716454 AND SRM 53-4-1. 2 L 7 4 4F RT 4A25 1998070300103 19980703 00103 WP 1998 7 3 UPS98827035 1 19980603 A 5320 37584961N FITTING DOUG DC8 DC871F 302199D WP BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 1140 AT STR 35L, THE INTERCOSTAL ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE (FITTING) IA W SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300104 19980703 00104 WP 1998 7 3 UPS98827036 1 19980607 A 5320 5613064106 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 70 AT RBL16-24, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5613064 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998070300105 19980703 00105 WP 1998 7 3 UPS98827037 1 19980604 A 5320 564531321 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 25-35 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D STA 25 TO 35 AT STR 32L, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5645313 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998070300106 19980703 00106 WP 1998 7 3 UPS98827038 1 19980606 A 5320 5711283516 FITTING DOUG DC8 DC871F 302199D WP BS 1222 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D HOLD DOWN FITTING AT STA 1222 AND STR 31R HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITTI NG IAW 8110-3 APPROVED DHC SK772-781 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300107 19980703 00107 WP 1998 7 3 UPS98827041 1 19980522 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 69.500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 RW UPPER INBD AFT SKIN PANEL AT APPROX STA XCW 69.500 IS CRACKED. CUT ATTACHMENT ANGLE TO FWD END OF CRACK, BLENDED AREA OF CRACK IAW DC8 SRM 57-20-0 FIG 7 FOUND TO BE WITHIN LIMITS, PERFORMED HFEC IAW MIL-STD-271F. F OUND NO CRACKS AFTER BLENDING. ALODINED AND PRIMED BLENDED AREA IAW DC8 SRM 51-1-8. FABRICATED ANGLE SPLICE IAW DC8 SR M 53- 20-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED SPLICE IAW. 2 L 7 4 4F RT 4A25 1998070300108 19980703 00108 WP 1998 7 3 UPS98827043 1 19980523 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 80 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 FRAME STA 80 HAS DAMAGE AT L21RT. CUT OUT DAMAGED SECTION OF FRAME. FABRICATED SPLICE REPAIR ANGL ES AND FRAME SEGMENT IAW DC8 SRM 53-2-0. ALODINED AND PRIMED SPLICE REPAIR ANGLE AND FRAME SEGMENT. INSTALLEDSPLICE RE PAIR ANGLES AND FRAME SEGMENT IAW DC8 SRM 53-2-0 IAW DC8 SRM 51-1-8 AND 51-1-21, 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300109 19980703 00109 WP 1998 7 3 UPS98827044 1 19980524 A 5280 DOOR DOUG DC8 DC873F 302199F WP LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 LT MLG DOOR CRACKED AT FWD AND AFT DRAIN HOLES OBS EDGE, 2 PLACES LT MLG INBD DOOR, MAT ID 7075-T6 .050 SUBSTITUTED TO 2024-0 .050 HEAT TREATED TO T4 FABRICATED, ALODINED AND INSTALLED ALL IAW DC8 SRM 52-6-1, TP91003 RE V A 51-1-8 AND 51-1-21. 2 L 7 4 4F RT 4A25 1998070300110 19980703 00110 WP 1998 7 3 UPS98827045 1 19980525 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 558 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 CORROSION ON RIGHT WING TRAILING EDGE PANEL SUPPORT ANGLE AT XRS 558 .00. ORDER NEW ANGLE RECEIVED NEW ANGLE DRILLED HOLES AND INSTALLED ANGLE IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998070300111 19980703 00111 WP 1998 7 3 UPS98827047 1 19980525 A 5511 SPAR DOUG DC8 DC873F 302199F WP RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 RT HORIZONTAL STABILIZER OB GEAR TAB LINKAGE BIX CRACKED AND GOUGED XRS 216. REMOVED RT OB HORIZO NTAL STAB GEAR TAB LINKAGE BOX IAW DC8 SRM 51-1- 21 WELDED BOX IAW DPS 10.225 ALODINED AND PRIMED IAW DC8 SRM 51-1-8. R EINSTALLED BOX IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998070300112 19980703 00112 WP 1998 7 3 UPS98827048 1 19980525 A 5511 SPAR DOUG DC8 DC873F 302199F WP LT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 LT HORIZONTL STAB I/B GEAR TAB LINKAGE BOX CRACKED AND GOUGED XRS 137. REMOVED AND REPLACED IB GEA R TAB LINKAGE BOX IAW DC8 SRM 51-1-21 WELDED EFFECTED AREAS IAW DPS 10.225. ALODINED AND PRIMED IAW DC8 SRM 51 -1-8. 2 L 7 4 4F RT 4A25 1998070300113 19980703 00113 WP 1998 7 3 UPS98827049 1 19980526 A 5313 STRINGER DOUG DC8 DC873F 302199F WP BS 450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 FS 450 LONG 31R CORRODED AND CHIPPED METAL ALONNG EDGES AND FASTENER HOLES AT THE FWD END OF FITTIN G. REMOVED FASTENERS IAW DC8 SRM 51-1-20D. REMOVED CORROSION IAW WITH DC 8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. BLENDED DAMAGE IAW DC8 SRM 53-2-0 DRILLED NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SR M 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300114 19980703 00114 WP 1998 7 3 UPS98827050 1 19980526 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP BS 683 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 CABIN STA 683, X=0 ABOVE C/W BOX VERT STIFFENER CRACKED. MAT ID IAW DOUGLAS DWG-5773275 -1002024-0 PO NR 185371, HEAT TREATED ANGLE FROM 2024-0 .100 TO 2024-T4 .100 IAW TPS -1003. REV AS FABBED ANGLE IAW DC8 SRM 51-1- 24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300115 19980703 00115 WP 1998 7 3 UPS98827051 1 19980526 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 702 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 CABIN-STA 702 X=69 (CUSP) AT FLOORBEAM ATTACH FITTING CRACKED. REMOVED OLD FITTING DRILLED UP NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300116 19980703 00116 WP 1998 7 3 UPS98827052 1 19980526 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 702 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 CABIN STA 702 X=23 AT CABIN FLOORBEAM UPPER CHORD UNDER SEAT TRACK CRACKED. REMOVED AND REPLACED F ITTING SUPPORT IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300117 19980703 00117 WP 1998 7 3 UPS98827053 1 19980526 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 CABIN STA 760 X=23 FLOORBEAM FITTING ON AFT SIDE CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300118 19980703 00118 WP 1998 7 3 UPS98827054 1 19980526 A 5530 FITTING DOUG DC8 DC873F 302199F WP VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 VERT STAB AFT SPAR STA ZR297 FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300119 19980703 00119 WP 1998 7 3 UPS98827055 1 19980526 A 5530 WEB DOUG DC8 DC873F 302199F WP VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 VERT STAB CLOSEOUT WEB AT ST ZR297 IS CRACKED. CLEANED AREA IAW DC8 SRM 51-1-8. PERFORMED HFEC IA W MIL-STD-271F ON VENT CLOSE OUT WEB ZR297 AFTER CLEANING AREA FOUND CORROSION AROUND RIVET. REMOVED RIVET IAW DC8 SRM 51-1-21. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-1. INSTALLED RIVET IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998070300120 19980703 00120 WP 1998 7 3 UPS98827056 1 19980526 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 CORROSION ON LONGERON 30R AT STA 1540. REMOVED CORROSION IAW DC8 SRM 51-1-8. MATERIAL FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. MAT ID 7075-T6 .050 PO NR 260338, 7075-T6 .080 PO NR 262218, 7075-T6 .160 PO NR 2541 27 IAW DC8 SRM 53-2-2 FIG 8. FABRICATED REPAIR STRAPS IAW DC8 SRM 53-2-2 FIG 8. ALODINED AND PRIMED IAW DC 8 SRM 51-1- 8. INSTALLED REPAIR STRAPS IAW DC8 SRM 53-2-2 FIG 8. 2 L 7 4 4F RT 4A25 1998070300121 19980703 00121 WP 1998 7 3 UPS98827057 1 19980527 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 FS 280 LONG 35R -36 ZEE FITTING IS CORRODED. INSTALLED NEW FITTING IAW DC8 SSRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300122 19980703 00122 WP 1998 7 3 UPS98827058 1 19980527 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 370 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 AFT BANANA FITTING CRACKED AT C-1 DOOR FS 370 AT LONGERON 32R. REMOVED CRACKED FITTING LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2, INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300123 19980703 00123 WP 1998 7 3 UPS98827059 1 19980528 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1725 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 FS 1725 LONGERON 16R FRAME IS CORRODED/EXFOLIATED NEXT TO LONGERON ATTACH BOLTS. FABBED ANGLE IAW REO-04829 AND INSTALLED IAW DC8 SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1998070300124 19980703 00124 WP 1998 7 3 UPS98827060 1 19980528 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 66 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 IN NR 3 MAIN TANK ON INBD SIDE AT APPROX STA XRS 66 TO APPROX XRS 61 LOWER STRINGER NR 51 IS CRACKE D ON THE AFT SIDE. REMOVED END FITTING IAW DAC DWG 3704841 PART NR 3704841-501. DRILLED NEW FITTING IAW DC8 SRM 51-3-2 . ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300125 19980703 00125 WP 1998 7 3 UPS98827061 1 19980528 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C+S2 IN NR 3 MAIN TANK JUST OUTBD OF XRS74 LOWER STRINGER NR 51 IS CRACKED IN TWO SEPARATE PLACES ON THE FWD SIDE AND BETWEEN 3 FASTENERS ON THE AFT SIDE. REMOVED CRACKED END FITTING. DRILLED NEW FITTINGS IAW 51-3-2. INST ALLED FITTINGS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998070300126 19980703 00126 EU 1998 7 3 QXEA9800824 1 19980623 A 3350 1312 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 BOI - 3.5 VOLT EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 8A. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS NORMAL . 2 L 7 2 4F RT A20EU 1998070300127 19980703 00127 EU 1998 7 3 QXEA9800825 1 19980624 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 BOI - FORWARD CABIN EMERGENCY LIGHT IS DIM. MAINTENANCE RELAMPED SEVERAL LIGHT BULBS AND OPERATIONALLY TESTED. TESTS N ORMAL. 2 L 7 2 4F RT A20EU 1998070300128 19980703 00128 EU 1998 7 3 QXEA9800826 1 19980623 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 GEG - FORWARD AND AFT ROW 8 OVERHEAD EXIT ANNUNCIATORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CIRCUIT BOARDS AND OPERATIONALLY TESTED. TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998070300129 19980703 00129 NM 1998 7 3 98FDEA00417 1 19980626 A 2780 40173 SWITCH BOEING 727 727233 138408A NM NR 4 LE FLAP FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 270FE 22035 98-0160 STA-IND: AFTER TAKEOFF AND INITIAL CLEAN UP, PASSING THROUGH 10,000 FEET FROM THE ACCELERATION TO CLIMB SPEED, THE FRONT AMBER LEADING EDGE WARNING CAME ON. PER POSITION INDICATION SHOWED THE NR 4 LEADING EDGE DEVICE AS CONSTANTLY YELLOW IN TRANSIT. AT FLAPS 15 EVERYTHING WORKED NORMAL, POSITION GREEN. RETURNED TO DEPARTURE BASE. REMOVED AND REP LACED NR 4 LEADING EDGE FLAP MICROSWITCH PER MAINTENANCE MANUAL 27-82-1 OPERATES NORMAL. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998070300130 19980703 00130 NM 1998 7 3 98FDEA00418 1 19980626 A 5270 DOOR LIGHT BOEING 727 727227 1384078 NM CARGO DOOR ILLUMINATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 484FE 21466 98-0161 - STA-PIT - CLIMBING THROUGH FLIGHT LEVEL 290, MAIN CARGO DOOR LIGHT ON CAUTION LIGHT PANEL ILLUMINATED AND REMA INED ILLUMINATED DURING DIVERSION TO PIT. ACCOMPLISHED RED TAB PROCEDURES. FOUND BUS SUPPLY AND BATTERY CHARGER CIRCUI T BREAKERS POPPED. OPENED AND CLOSED DOOR AFTER CLOSING CIRCUIT BREAKERS. ALL DOOR LIGHT EXTINGUISHED INDICATIONS SHOW DOOR CLOSED AND LOCKED. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998070300131 19980703 00131 WP 1998 7 3 ABXA9800543 1 19980623 A 5313 59114277 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND LONGERON 16L CRACKED AT HI-LOCK STATION 945. REPAIRED LONGERON IAW ABX DC9 SSRM DWG K05864. 2 L 7 2 4F A6WE 1998070300132 19980703 00132 WP 1998 7 3 ABXA9800544 1 19980623 A 5313 591140869 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 446 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND LONGERON 2R CRACKED AT STATION 446. REPAIRED LONGERON IAW DC9 SRM 53-02-00. 2 L 7 2 4F A6WE 1998070300133 19980703 00133 WP 1998 7 3 ABXA9800545 1 19980623 A 5311 59114481 FRAME DOUG DOUG DC9 DC933F 302207A WP BS 484 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND FUSELAGE FRAME CRACKED AT STATION 484, AND LONGERON 29L. REPLACED FRAME FROM LONGERONS 28L TO 28R IAW DC9 53-03-00. 2 L 7 2 4F A6WE 1998070300134 19980703 00134 WP 1998 7 3 ABXA9800546 1 19980623 A 5320 9922042505 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 775 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND FLOORBEAM VERTICAL SUPPORT LOWER FITING AT STATION 775 AND LONGERON 23L CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-05. 2 L 7 2 4F A6WE 1998070300135 19980703 00135 WP 1998 7 3 ABXA9800547 1 19980623 A 5320 99155544 INTERCOSTAL DOUG DOUG DC9 DC933F 302207A WP BS 218-237 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND INTERCOSTAL AT STATION 218-237 AND LONGERON 28R CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300136 19980703 00136 WP 1998 7 3 ABXA9800548 1 19980623 A 5320 99155543 INTERCOSTAL DOUG DOUG DC9 DC933F 302207A WP BS 218-237 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND INTERCOSTAL AT STATION 218-237 AND LONGERON 28L CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300137 19980703 00137 WP 1998 7 3 ABXA9800549 1 19980623 A 5320 991965814 INTERCOSTAL DOUG DOUG DC9 DC933F 302207A WP BS 870-889 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND INTERCOSTAL AT LONGERON 8R STATION 870-889 CORRODED BEYOND LIMITS. REMOVED AND REPLACED INTERCOST AL IAW DC9 SRM 51-30-2 AND 51-30-3. 2 L 7 2 4F A6WE 1998070300138 19980703 00138 WP 1998 7 3 ABXA9800550 1 19980622 A 5313 565192719 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1790 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 LONGERON 2R CRACKED AT STATION 1790 CANTED BULKHEAD. REPAIRED IAW ABX REA D853-23411MR. 2 L 7 4 4F 4A25 1998070300139 19980703 00139 WP 1998 7 3 ABXA9800551 1 19980622 A 3211 5777513502 TRUNNION DOUG DOUG DC8 DC861 3021952 WP RT MLG CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 RIGHT HAND MAIN LANDING GEAR TRUNNION CORRODED. FABRICATED BUSHINGS PER AD 71-25-09 AND ABX REA D832-23410MR. 2 L 7 4 4F 4A25 1998070300140 19980703 00140 WP 1998 7 3 ABXA9800552 1 19980622 A 5312 57763835 FLANGE DOUG DOUG DC8 DC861F 3021953 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 AFT PRESSURE BULKHEAD AFT SIDE HORIZONTAL BEAM HAS 3 CRACK ON LOWER FLANGE AT AIRCRAFT CENTERLINE. REPAIRED IAW ABX REA D853-23407MR. 2 L 7 4 4F 4A25 1998070300141 19980703 00141 WP 1998 7 3 ABXA9800553 1 19980622 A 5312 577265833 BEAM DOUG DOUG DC8 DC861 3021952 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 AFT PRESSURE BULKHEAD AFT SIDE, HORIZONTAL BEAM HAS 3.5 CRACK ON LOWER FLANGE AND 1 CRACK ON UPPER FLANGE AT AIRCRAFT CE NTERLINE, 24 ABOVE FRP. REPAIRED PER ABX REA D853-23406MR. 2 L 7 4 4F 4A25 1998070300142 19980703 00142 WP 1998 7 3 DLL19981334 1 19980624 A 5330 1608986101 SKIN LKHEED 1011 10113853 5265020 WP BS 840 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 754DL 193Y1181 FUSELAGE/SKIN, FS 829-846, STRG 33-34, REPAIR FOR CORROSION CUTOUT. THE FUSELAGE BELLY SKIN BETWEEN FS 829 AND 846 WAS FOUND CORRODED AT STRINGER 33. THE CORRODED ARE OF SKIN WAS REMOVED WITH A 10 BY 9.5 CUTOUT. THE DAMAGE WAS REPAI RED WITH AN EXTERNAL REPAIR DOUBLER PER ER/A 365086-14, REV A. 2 L 7 3 4F A23WE 1998070300143 19980703 00143 WP 1998 7 3 DLL10981335 1 19980621 A 5412 1527807101 BULKHEAD FITTING LKHEED 1011 10113851 5265010 WP WS 520-529 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 722DA 193C1147 REPAIR FOR CRACK, LT WING IWS 503-529, PYLON BACKUP FITTING BULKHEAD. THE LT WING PYLON BACKUP FITTING BULKHEAD BETWEEN IWS 503 AND 539 WAS FOUND WITH A 6 LONG CRACK THROUGH THE UPPER FLANGE RUNNING TOWARDS THE INTEGRAL CENTER RING FLANGE. THE CRACK AREA WAS CUT OUT. TWO REPAIR FITTINGS AND A REPAIR PLATE WERE FABRICATED AND INSTALLED TO REPAIR THE DAMA GE. THE REPAIR WAS ACCOMPLISHED PER ER/A 365050-14, REV C. 2 L 7 3 4F A23WE 1998070300144 19980703 00144 NM 1998 7 3 DL73S981336 1 19980625 A 7720 CONNECTOR BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE DIRTY A DALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 27 323DL 23095 717143 ON T/O, ROLL WITH INITIAL APPLICATION OF PWR, THE NR 2 ENGINE EGT FLUX BETWEEN 0 AND 500 DEGREES. CHECKED ENG WIRING FR OM TERMINAL BLOCK TO CONNECTOR D400. CLEANED PINS 25/26. RAN ENGINE TO T/O PWR SEVERAL TIMES, COULD NOT DUPLICATE. E GT INDICATED NORMAL. USING METER EGT WIRING ALL THE WAY TO PYLON ALL CHECKED GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 1998070300145 19980703 00145 NM 1998 7 3 DLM88981337 1 19980623 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 410 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 973DL 53241 FUSELAGE SKIN, FS 400-421, STRG 25L-26L, REPAIR FOR SKIN DAMAGE CUTOUT. THE FUSELAGE SKIN BETWEEN FS 400 AND 421 AND BE TWEEN STRINGERS 25L AND 26L WAS BADLY DAMAGED BY GROUND EQUIPMENT. THE SKIN DAMAGE WAS REMOVED WITH A 21 BY 6.5 CUTOUT. THE SKIN WAS REPAIRED WITH A CLASS 2 EXTERNAL REPAIR DOUBLER PER THE GUIDLINES OF MD-88 SRM 53-04, FIG. 12B. THE REPA IR WAS DOCUMENTED PER ER/A 365087-14, REV A. 2 L 7 2 4F RT A6WE 1998070300146 19980703 00146 NM 1998 7 3 DL72K981338 1 19980621 A 5711 65192922 SPAR WEB BOEING 727 727232 1384082 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 480DA 20860 WING, CENTER SECTION, REAR SPAR WEB, RBL 10.75 AND LBL 14.5. REPAIR FOR WEB CRACKS. THE CENTER WING REAR SPAR WEB WAS FOUND WITH THE TYPICAL CRACKS NEAR THE UPPER SPAR CAP AT RBL 10.75 AND LBL 14.5. THE CRACKS WERE ROUTED OUT AND REPAIRE D WITH LOCAL REPAIR DOUBLERS. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365047-14AD, REV A. 2 L 7 3 4F A3WE 1998070300147 19980703 00147 NM 1998 7 3 DL72S981339 1 19980625 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 468DA 20745 FOUND ON F2 LETTER CK, CRACK IN SKIN I/B AFT CORNER OF GROUND AIR CONNECTION PANEL. REPAIRED PER MM 53-30-0. 2 L 7 3 4F A3WE 1998070300148 19980703 00148 NM 1998 7 3 DL72S981340 1 19980625 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 535DA 22048 R-2 DOOR EMER EXIT SIGN INOP. REPLACED BATT OPS CK OK. 2 L 7 3 4F A3WE 1998070300149 19980703 00149 NM 1998 7 3 DL72S981341 1 19980625 A 3350 BULB 07912 BOEING 727 727232 1384082 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 483DA 20863 EMERGENCY TRACK LIGHT JUST FWD OF SEAT 30D MISSING LENS AND BULB. REPLACED BULB AND LENS. 2 L 7 3 4F A3WE 1998070300150 19980703 00150 WP 1998 7 3 RRXA98238 1 19980625 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 250 DAMAGE A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING CARGO LOADING, K LOADER STRUCK AIRCRAFT FUSELAGE SKIN AT STA 250 AND LONGERON 26 LEFT. DAMAGE IS 2 INCHES BY 3 I NCHES, AND 1.250 INCHES ABOVE STATIC PORT. *S/D* AIRCRAFT WAS FERRIED TO KGSO FOR INSPECTION. REMOVED DAMAGE, FABRICA TED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04984. 2 L 7 4 4F RT 4A25 1998070300151 19980703 00151 WP 1998 7 3 RRXA98239 1 19980617 A 5720 STRUCTURE DOUG DC8 DC863 302198A WP LT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 950R 45903 EXTENSIVE DAMAGE TO LEFT WING EXTENDED LEADING EDGE INTO NR 1 ALT FUEL TANK. AIRCRAFT STRUCK BY GROUND HANDLERS FORK LI FT. AIRCRAFT FERRIED FROM KMSP TO KGSO. 2 L 7 4 4F 4A25 1998070300152 19980703 00152 NM 1998 7 3 RRXA98240 1 19980624 A 2611 CONNECTOR BOEING 727 727222 1384073 NM CARGO COMPT DIRTY A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 7635U 19908 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT. REMOVED, CLEANED AND RESECURED CONNECTORS ON ALL SMOKE DETECTORS. REMOVED CLE ANED AND REINSTALLED COALESCER BAGS, OPS CHECK GOOD ON GROUND RUN AND ON FLT FROM KCLT TO KBDL. 2 L 7 3 4F A3WE 1998070300153 19980703 00153 NM 1998 7 3 RRXA98241 1 19980624 A 2611 SMOKE LIGHT BOEING 727 727222 1384073 NM CARGO COMPT ILLUMINATED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 7635U 19908 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT. REMOVED CARGO AND INSPECTED MAIN CARGO COMPARTMENT AND FWD AND AFT BELLY CARGO COMPARTMENTS, INSPECTED CONTENTS OF ULD'S AND BELLY. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1998070300154 19980703 00154 NM 1998 7 3 RRXA98242 1 19980626 A 2611 SMOKE LIGHT BOEING 727 727222 1384073 NM CARGO COMPT ILLUMINATED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 7635U 19908 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT. REMOVED ALL CARGO, INSP CONTAINERS FOR OVERHEAT AND FOUND ALL NORMAL. INSPECT ED SMOKE DETECTOR, CHECKS NORMAL PER BOEING MM 26-10-02. RELOADED CARGO AND LAUNCHED. 2 L 7 3 4F A3WE 1998070300155 19980703 00155 NM 1998 7 3 RRXA98243 1 19980626 A 3260 656021132 CONTROL BOX BOEING 727 727222 1384073 NM LT MLG FAILED A RRXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 15 7638U 19911 LEFT MAIN GEAR WARING LIGHT REMAINED ILLUMINATED AFTER GEAR WAS SELECTED UP. REMOVED AND REPLACED LANDING GEAR CONTROL BOX. LEFT MAIN GEAR WARNING LIGHT OPS CHECKS GOOD ON GROUND TEST. 2 L 7 3 4F A3WE 1998070300156 19980703 00156 NM 1998 7 3 VNAA9806012 1 19980623 A 3240 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE LEAKED A VNAA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 GL 07 430JS 58616 20565 3044 AFTER DEPARTURE FROM PIT, AN EMERGENCY PARKING BRAKE ACCUMULATOR LOW PRESSURE WARNING OCCURED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE, IN ACCORD ANCE WITH DORNIER MAINTENANCE MANUAL 32-43-02. OPERATION AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998070300157 19980703 00157 NM 1998 7 3 VNAA9806013 1 19980624 A 3610 4069B000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 441JS 66481 3059 A CROSSBLEED WARNING MESSAGE OCCURED DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPE CTED AND REPLACED THE CROSSBLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERATION CHECKS WERE C OMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998070300158 19980703 00158 WP 1998 7 3 CKSA98351 1 19980619 A 3310 BA170 BALLAST DOUG DC8 DC8F55 3021928 WP FLIGHT COMPT FAILED A CKSA K NONE O OTHER CR CRUISE 1 GL 23 6161M 45762 STRONG ELECTRICAL BURNING SMELL FROM FO FLUORESCENT BALLAST AREA. REMOVED AND REPLACED BALLAST TRANSFORMER PLUS RELAMPE D 5 LIGHT ASSEMBLY. SYSTEM OPS CHECK NORMAL PER DC8 MM 33-2-0. 2 L 7 4 4F 4A25 1998070300159 19980703 00159 WP 1998 7 3 TC8A98036 1 19980625 A 7910 OIL TANK DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE LOOSE A TC8A E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 802CK 45679 642684 ON CLIMB-OUT AT APPROX 10000 FEET, NR 3 ENGINE FIRE WARNING BELL AND LIGHTS. PERFORMED ENGINE SHUTDOWN. FOUND MIDDLE S TRAP ON ENGINE OIL TANK LOOSE AND IN CONTACT WITH LT FAN DOOR FIRE WARNING LOOP. SECURED CLAMP, PERFORMED ENGINE RUN-UP AND FIRE WARNING TEST IAW 26-10-0, ALL OPERATIONS NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1998070300331 19980703 00331 SW 1998 7 3 HEEA0014788 1 19980617 A 7714 212075037113 INDICATOR BELL 412 412 1182202 SW ENGINE N1 STICKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 22608 33075 GAUGE STICKS AND DROPS TO ZERO, UNIT FUNCTION CHECKED BAD, UNIT HAS NO NEEDLE MOVEMENT. 1 G 7 2 4U H4SW 1998070300366 19980703 00366 NM 1998 7 3 M8XA9800013 1 19980622 A 5610 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE COCKPIT DEFECTIVE A M8XA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 03 329MX 3049 AIRCRAFT RETURNED TO DEN BECAUSE OF A CRACKED RIGHT FRONT WINDSHIELD AS A RESULT OF ENCOUNTERING A HAIL STORM SHORTLY AF TER TAKEOFF. AIRCRAFT LANDED IN DEN WITHOUT FURTHER INCIDENT. DENVER MAINTENANCE INSPECTED THE AIRCRAFT FUSELAGE IAW S RM 53-00-11 AND WINDSHIELD IAW AMM 56-11-00. AIRCRAFT FOUND TO BE SAFE FOR FERRY FLIGHT TO COS. MAINTENANCE REPLACED T HE RIGHT FRONT WINDSHIELD, LEFT PROPELLER SPINNER, AND RIGHT PROPELLER SPINNER BULKHEAD. FUSELAGE DAMAGE WAS INSPECTED AND FOUND TO BE WITHIN ACCEPTABLE LIMITS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998070300367 19980703 00367 1998 7 3 M8XA9800014 4 19980623 A 3130 7013348913 DAU HONEYWELL 7013348913 DORNER DO32 DO328100 2996000 NM PWA 119 PW119C NE HARTZL HDE6C HDE6C3B NE E/E COMPT DEFECTIVE A M8XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 03 330PH 94120309 3008 SHORTLY AFTER TAKEOFF, THE FLIGHT CREW REPORTED A PROBLEM WITH THE NR 1 ALTERNATOR. THEY WERE ALERTED BY AC VOLT FAIL M ESSAGE ON THE EICAS SCREEN. AIRCRAFT RETURNED TO DEN, LANDED WITHOUT FURTHER INCIDENT. DENVER MAINTENANCE REPLACED THE NR 1 DAU IAW AMM 31-42-00, OPERATIONAL CHECK WAS CONDUCTED WITH SATISFACTORY RESULTS. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998070300368 19980703 00368 WP 1998 7 3 IXXA9800058 1 19980621 A 2913 AS63665 PUMPS DOUG DC8 DC862 3021970 WP NR 2/3 ENGINES DEFECTIVE A IXXA A UNSCHED LANDING G K MULTIPLE FAILURE FLUID LOSS CR CRUISE 1 GL 23 8974U 46110 EN ROUTE, THE MAIN HYDRAULIC SYSTEM FAILED AND HYDRAULIC PRESSURE DROPPED TO ZERO. THE FLIGHT CONTROL MANUAL REVERSION LIGHTS ILLUMINATED CONFIRMING THE FAILURE. THE FLIGHT WAS DIVERTED TO DNA FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPE CTED THE AIRCRAFT AND FOUND THE NUMBER TWO AND THREE ENGINE DRIVEN HYDRAULIC PUMPS DEFECTIVE. FURTHER INVESTIGATION REV EALED THE MAIN HYDRAULIC QUANTITY TRANSMITTER DEFECTIVE AND A RUPTURED HYDRAULIC LINE ON THE LEFT WING INBOARD SLOT ACTU ATOR. MAINTENANCE REPLACED ALL DEFECTIVE COMPONENTS IN ACCORDANCE WITH THE MAINTENANCE MANUAL. A SUCCESSFUL OPERATIONA L TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 1998070300369 19980703 00369 WP 1998 7 3 CALA9801173 1 19980627 A 2910 9696181190 HYD LINE DOUG DC10 DC1030 3023501 WP RT MLG RUPTURED A CALA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION TO TAKEOFF 1 SW 09 19072 46576 THE LANDING GEAR HANDLE WOULD NOT RAISE TO THE UP POSITION AFTER TAKEOFF. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO HNL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG TRIM CYLINDER HYDRAULIC LINE RUPTURED. THE HYDR AULIC LINE WAS REMOVED AND REPLACED AND OPERATION OF THE GEAR HANDLE CHECKED GOOD. 2 L 7 3 4F A22WE 1998070300370 19980703 00370 NM 1998 7 3 CALA9801174 1 19980628 A 2910 65445101472 LINE BOEING 737 737219 1384469 NM A-HYD SYST LEAKING A CALA O OTHER K FLUID LOSS CR CRUISE 1 SW 09 10248 20344 THE A-HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE. THE A-SYSTEM PUMPS WERE TURNED OFF AND THE AIRCRAFT LANDED AT EWR WITHO UT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC LINE AT A-HYDRAULIC SYSTEM MODULE LEAKING. THE HYDRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1998070300371 19980703 00371 NM 1998 7 3 CALA9801175 1 19980628 A 3260 LOGIC CARD BOEING 737 737524 1384721 NM E/E COMPT INOPERATIVE A CALA O OTHER O OTHER CL CLIMB 1 SW 09 14639 28900 THE AIRCRAFT HAD A BRIEF HISTORY OF THE LANDING GEAR HANDLE BINDING IN THE OFF POSITION DURING GEAR RETRACTION. CYCLING THE GEAR HANDLE REMEDIED THE PROBLEM. MAINTENANCE REMOVED AND REPLACED THE M991 LOGIC CARD AND RELAY R276. A GEAR SWI NG WAS PERFORMED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998070300372 19980703 00372 WP 1998 7 3 CALA9801176 1 19980626 A 5241 BEAM DOUG DC9 DC982 3022082 WP GALLEY DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF FORWARD GALLEY SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998070300373 19980703 00373 NM 1998 7 3 CALA9801177 1 19980626 A 3350 30043211 LIGHT BOEING 737 7373T0 1384582 NM L2 DOOR RUSTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17317 23368 THE EMERGENCY SLIDE LIGHT AT L-2 DOOR DID NOT COME ON WHEN TESTING EMERGENCY LIGHTS FROM EITHER SWITCH. THE LIGHT ASSEM BLY WAS REPLACED DUE TO INTERNAL RUSTING. THE LENS COVER SEAL WAS FOUND BAD ALLOWING MOISTURE TO ENTER. REPLACED LENS AND SEAL. 2 L 7 2 4F RT A16WE 1998070300374 19980703 00374 NM 1998 7 3 CALA9801178 1 19980626 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND CORROSION AROUND FASTENER HOLES OF FLOORBEAM AT STA 967, RBL 40 TO 50. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 202. 2 L 7 2 4F RT A16WE 1998070300375 19980703 00375 NM 1998 7 3 CALA9801179 1 19980626 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 328-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 328 TO 344. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS FABRIC ATED AND INSTALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 1998070300376 19980703 00376 NM 1998 7 3 CALA9801180 1 19980626 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND FLOORBEAM CORRODED AT STA 328, LBL 2. REPAIRED IAW SRM 53-10-51, FIGURE 205. 2 L 7 2 4F RT A16WE 1998070300377 19980703 00377 NM 1998 7 3 CALA9801181 1 19980628 A 5320 ANGLE BOEING 737 7373T0 1384582 NM BS 290-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14346 23584 INSPECTION FOUND ANGLE CORRODED AT R-1 DOOR, STA 290 TO 294 AND 344. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-0 0. 2 L 7 2 4F RT A16WE 1998070300378 19980703 00378 WP 1998 7 3 CALA9801182 1 19980626 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF MAIN CABIN DOOR NR 1 HORIZONTAL BEAM FORWARD END. A DOUBLER WAS INSTALLE D IAW SRM 52-05, FIGURE 31. 2 L 7 2 4F A6WE 1998070300379 19980703 00379 NE 1998 7 3 9809599605 2 19980523 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LEFT FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 01 605NW 47223 66669 DURING CLIMB AT 1500 FEET, THE LEFT ENGINE EXPERIENCED A CONTAINED FAILURE. AIRCRAFT RETURNED TO MKE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998070300380 19980703 00380 WP 1998 7 3 9809601162 1 19980619 A 3260 PROXIMITY BOX DOUG DC10 DC1040 3023508 WP NLG FAILED A NWAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 01 162US 46771 RECEIVED NOSE GEAR UNSAFE INDICATION WHEN GEAR EXTENDED FOR LANDING. RECYCLED GEAR AND FOLLOWED COCKPIT OPERATING MANUA L PROCEDURE. VISUALLY CONFIRMED GEAR DOWN. FLIGHT LANDED WITHOUT INCIDENT. REPLACED PROXIMITY SWITCH ELECTRONIC BOX. FOUND NOSE GEAR DOWN POSITION SENSOR OUT OF LIMITS. ADJUSTED NOSE GEAR POSITION SENSOR, OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998070300381 19980703 00381 WP 1998 7 3 9809619885 1 19980628 A 2131 CONTROLER DOUG DC9 DC951 3022051 WP COCKPIT FAILED A NWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 01 401EA 47682 AIRCRAFT LOST CABIN PRESSURIZATION AT FL350. FLIGHT CREW FOLLOWED COM PROCEDURES AND DESCENDED TO FL90. CABIN OXYGEN M ASK DEPLOY SYSTEM ACTIVATED. FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED OXYGEN GENERATOR CANISTERS AT 3CD, 3AB, 1AB, AND JUMPSEAT FORWARD CANISTER AND REPLACED THE CABIN PRESSURE CONTROLLER, OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998070300382 19980703 00382 SO 1998 7 3 COMA9810148 1 19980628 A 3350 013071BPE LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 196CA 120196 EMERGENCY FLOOR LIGHT AT ROW 9 IS INOPERABLE. REPLACED LAMP. 2 L 7 2 4T RT A31SO 1998070300383 19980703 00383 SO 1998 7 3 COMA9810149 1 19980628 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 266CA 120258 EMERGENCY EXIT SIGN AT ROW 5 BROKEN. REPLACED SIGN. 2 L 7 2 4T RT A31SO 1998070300384 19980703 00384 EA 1998 7 3 COMA9860161 1 19980621 A 7120 MOUNT CNDAIR CL600 CL6002B19 EA LT ENGINE DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 AT 48 MONTH INSPECTION TASK 002-54-410-500, LEFT ENGINE PYLON FRONT SPAR/ENGINE MOUNT IS DAMAGED ON INBOARD SIDE OF ACCE SS HOLE FOR 14TH STAGE BLEED AIR. REPAIRED DAMAGE IAW REO 601R-54-50-010. 2 L 7 2 4F RT A21EA 1998070300385 19980703 00385 EA 1998 7 3 COMA9860162 1 19980621 A 3610 601R800045 CLAMPS CNDAIR CL600 CL6002B19 EA BS 559 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 AT 24 MONTH INSPECTION TASK 002-53-170-321, UNDER FLOOR BLEED AIR DUCT LAMPS (2) ARE CRACKED. REMOVED AND REPLACED CLAM PS. 2 L 7 2 4F RT A21EA 1998070300386 19980703 00386 EA 1998 7 3 COMA9860163 1 19980621 A 5312 6013501251 BLKHD BRACKETS CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 934CA 7042 AT 48 MONTH INSPECTION TASK 002-53-310-501, ATTACH BRACKETS AT PRESSURE BULKHEAD 621 LEFT AND RIGHT ARE CRACKED. REPLAC ED BRACKETS. 2 L 7 2 4F RT A21EA 1998070300387 19980703 00387 EU 1998 7 3 98FDEA00419 1 19980628 A 2131 88005B0306 CONTROLLER AIRBUS 300 A300* EU CABIN MALFUNCTION A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 655FE 742 CABIN PRESSURE CONTROLLER NR 2 FAULTED AFTER T/O. UNABLE TO CONTROL IN MANUAL. REMOVED AND REPLACED FWD OUTFLOW VALVE. 2 L 7 2 4F RT A35EU 1998070300388 19980703 00388 WP 1998 7 3 98FDEA00420 1 19980515 A 5730 ARB0840 SKIN DOUG DC10 DC1010 3022110 WP WS 826 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 RT WING LOWER WING SKIN, STA X0RS 826.00 THERE IS DAMAGE TO THE LOWER SKIN (WIDTH: 0.250, DEPTH: 0.065, DISTANCE TO NEAR EST FASTENER: 0.5). CENTER TO CENTER. MAJOR REPAIR PERFORMED IAW EA 8-5732-38431, ENCLOSED. (22 JUNE 1998) 2 L 7 3 4F A22WE 1998070300389 19980703 00389 NM 1998 7 3 98FDEA00421 1 19980626 A 5330 SKIN BOEING 727 7272S2F 1384O81 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 215FE 22936 FUSE SKIN BULGED BS 990 AT STR 28L. CUT OUT CORRODED SKIN AND STRINGER SECTION. INSTALLED EXTERNAL SKIN REPAIR PER SRM 53-30-3 PG 12. INSTALLED STRINGER REPAIR PER SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1998070300390 19980703 00390 WP 1998 7 3 ABXA9800554 1 19980623 A 5250 AR25291GR41 LATCH DOUG DC9 DC941 302207N WP COCKPIT DOOR OUT OF POSITION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 959AX 47761 UNABLE TO OPEN COCKPIT DOOR. REPOSITIONED LATCH ON DOOR JAMB. 2 L 7 2 4F A6WE 1998070300391 19980703 00391 WP 1998 7 3 DLL10981343 1 19980625 A 5730 1527138133 SKIN LKHEED 1011 10113851 5265010 WP WS 450 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 733DS 193C1224 A 4 INCH LONG CRACK WAS FOUND EXTENDING FROM THE AFT EDGE OF LOWER SKIN PANEL AT IWS 450. THE CRACK RAN FWD, TERMINATIN G UNDER THE AFT EDGE OF THE LOWER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE WING SKIN PANEL. THE CUTOUT WAS REPAIRED W ITH THREE EXTERNAL ALUMINUM DOUBLERS AND TWO INTERNAL ALUMINUM STRAPS. THE REPAIR WAS ACCOMPLISHED PER ER/A 365053-14, REV A. 2 L 7 3 4F A23WE 1998070300392 19980703 00392 NM 1998 7 3 DL72W981344 1 19980616 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 292WA 22110 CORROSION AT FLOORBEAM STA 344 FROM LBL 13 TO RBL 17-MARKED. REPAIRED PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1998070300393 19980703 00393 NM 1998 7 3 DL72S981345 1 19980626 A 3350 BATTERY PACK 1001141 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 496DA 3234 21076 AFT AIRSTAIR EMER LIGHT INOP. REPLACED BATT PACK AND LIGHT RACK, OPS OK. 2 L 7 3 4F A3WE 1998070300394 19980703 00394 NM 1998 7 3 DLM11981346 1 19980626 A 2720 VALVE AV24E1162 DOUG MD11 MD11 3023602 NM RUDDER CONTL FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 803DE 774 48474 DURING FLIGHT, ACFT LOST NR 3 HYDRAULIC PRESSURE, RETURNED TO KATL. DURING INSPECTION FOUND RUDDER SHUTOFF VALVE LEAKIN G EXCESSIVELY. REMOVED AND REPLACED RUDDER SHUTOFF VALVE PER MM (P/N AV24E1162) DELTA NUMBER 290001011. SYSTEMS CHECK AND LEAK CHECKED GOOD. 2 L 7 3 4F RT A22WE 1998070300395 19980703 00395 NM 1998 7 3 DL72S981350 1 19980627 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 404DA 11728 21148 RT FWD OVERWING EMER EXIT LIGHT INOP. REPLACED BATT RACK, OPS OK. 2 L 7 3 4F A3WE 1998070300396 19980703 00396 WP 1998 7 3 DLL10981351 1 19980626 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 714DA 56576 193C1090 SEVERAL AISLE EMER LIGHTS OUT NEAR CENTER CABIN. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998070300397 19980703 00397 WP 1998 7 3 DLL10981352 1 19980626 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 714DA 193C1090 EMER LIGHT PWR SUPPLY INOP 3L. REPLACED PWR SUPPLY. 2 L 7 3 4F A23WE 1998070300398 19980703 00398 NM 1998 7 3 DL72W981353 1 19980627 A 3350 BATTERY PACK S106 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2820W 21058 OVERHEAD EMER LIGHT AT ROW 13 INOP. REPLACED BATT PACK, CK OK. 2 L 7 3 4F A3WE 1998070300399 19980703 00399 NM 1998 7 3 DL72W981354 1 19980514 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 REMOVED EXISTING T-CAP REPAIR, FWD AND AFT SPLICE ANGLES, 1 VERTICAL STIFFENER AND 1 FLOORBOARD SUPPORT. REMOVED EXISTI NG T-CAP FROM C/L TO RBL 52. BEGAN DRILLING NEW T-CAP. COMPLETED FABRICATION OF REPAIR PER SRM 53-10-8 PG 56-57. INST ALLED T-CAP BEAM SPLICE REPAIR PER SRM 53-10-8 PG 56-57. 2 L 7 3 4F A3WE 1998070300400 19980703 00400 NM 1998 7 3 DL72L981356 1 19980628 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 504DA 4482 21306 OVERWING EXIT EMERGENCY LIGHTS FAILED TO TEST DURING NR 3 SERVICE CHECK. REPLACED BATTERY PACK AND BASE, NOW CHECKS NML . 2 L 7 3 4F A3WE 1998070300401 19980703 00401 NM 1998 7 3 SCNA98067 1 19980620 A 2530 1430E1 OVEN BOEING 727 7272J4 1384006 NM GALLEY SPARKING A SCNA K NONE A FLAME/FIRE NR NOT REPORTED 1 GL 15 284SC 20 21438 THE LEFT FORWARD OVEN WAS REPORTED TO BE SPARKING. FOUND THE LEFT FORWARD OVEN CIRCUIT BREAKER POPPED. RESET CIRCUIT B REAKER. OPERATED OVEN WITH NO DISCREPANCIES FOUND. OVEN RACKS HAD ALREADY BEEN REMOVED. SUSPECT OVEN RACKS MAY HAVE B EEN HITTING FAN, OVEN OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998070300402 19980703 00402 SO 1998 7 3 SWIA971207 1 19980601 A 5270 MECHANISM EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 218SW 120287 CARGO DOOR LIGHT ILLUMINATED ON TAKEOFF, MEL 52-70-1. RETURNED TO FIELD. INSTALLED NEW HARDWARE AND ADJUSTED MICROSWIT CH ARM AS REQUIRED, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998070300403 19980703 00403 SO 1998 7 3 SWIA971208 1 19980609 A 3230 SOLENOID VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NM 07 562SW 120336 LANDING GEAR CYCLED UP AND DOWN UPON EXTENSION, GEAR LIGHTS ON PANEL. REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. CYCLED LANDING GEAR NUMEROUS TIMES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998070300404 19980703 00404 NM 1998 7 3 P5CA9801058 1 19980625 A 5320 SILL BOEING 747 747123 1384873 NM CARGO DOORWAY CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 FUSELAGE LT STA 1780 MAIN DECK SIDE CARGO DOOR LOWER FWD ATTACH DOOR SILL CHAFING MARK. CHAFE MARKS SMOOTHED OUT AND RE PROTECTED PER SRM 51-01-01 AND 51-10-02, WITHIN SRM LIMITS 53-30-01. 2 L 7 4 4F A20WE 1998070300405 19980703 00405 NM 1998 7 3 P5CA9801059 1 19980625 A 5330 SKIN BOEING 747 747123 1384873 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LOWER FUSELAGE SKIN SURFACE CORROSION AT BS 600 LEFT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300406 19980703 00406 NM 1998 7 3 P5CA9801060 1 19980625 A 5350 FAIRING BOEING 747 747123 1384873 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION FOUND ON BODY FAIRING PANEL 191 BBL ANTENNA CUTOUT AREA. CORROSION REMOVED AND REPROTECTED PER SRM 51 -10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300407 19980703 00407 NM 1998 7 3 P5CA9801061 1 19980625 A 5280 SKIN BOEING 747 747123 1384873 NM RT MLG DOOR CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT BODY GEAR INBD STRUT DOOR SURFACE CORROSION AT AFT EDGE AND MID AREA OF DOOR. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300408 19980703 00408 NM 1998 7 3 P5CA9801062 1 19980625 A 5532 SKIN BOEING 747 747123 1384873 NM LT HORIZ STAB CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LT HORIZONTAL STAB TOP SURFACE MINOR CORROSION ALONG STAB TORQUE BOX SKIN AREA FROM L/E TO T/E. CORROSION REMOVED AND R EPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300409 19980703 00409 NM 1998 7 3 P5CA9801063 1 19980625 A 5311 FRAME BOEING 747 747123 1384873 NM BS 1350 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION LT WING GEAR WHEEL WELL AT TOP OF FRAME AT STA 1350 LBL 10. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300410 19980703 00410 NM 1998 7 3 P5CA9801064 1 19980625 A 5320 RIVETS BOEING 747 747123 1384873 NM BS 2664 LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 APU COMPARTMENT LT SIDEWALL STA 2664 AND STA WL 305 VERTICAL FRAME SUPPORT ANGLE ATTACH RIVETS LOOSE. RIVETS REPLACED P ER 51-30-02. 2 L 7 4 4F A20WE 1998070300411 19980703 00411 NM 1998 7 3 P5CA9801065 1 19980625 A 5320 ANGLE BOEING 747 747123 1384873 NM BS 2718 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 APU RT COMPARTMENT SIDEWALL STA 2718 WL 305 VERTICAL FRAME SUPPORT ANGLE CRACKED. REPLACED VERTICAL FRAME SUPPORT ANGLE PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998070300412 19980703 00412 NM 1998 7 3 P5CA9801066 1 19980625 A 5320 RIVETS BOEING 747 747123 1384873 NM BS 2669 LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 APU COMPARTMENT RT SIDEWALL STA 2664 AND STA 2669 WL 305 VERTICAL FRAME SUPPORT ANGLE ATTACH RIVETS LOOSE. RIVETS REPLA CED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998070300413 19980703 00413 NM 1998 7 3 P5CA9801067 1 19980625 A 5280 DOOR BOEING 747 747123 1384873 NM RT MLG CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT BODY GEAR CORROSION ON FORWARD SIDE OF O/B STRUT DOOR. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10- 02. 2 L 7 4 4F A20WE 1998070300414 19980703 00414 NM 1998 7 3 P5CA9801068 1 19980625 A 5220 WEB BOEING 747 747123 1384873 NM EMER EXIT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 COCKPIT OVERHEAD EMERGENCY HATCH AFT HINGE WEB CRACKED. REPAIRED HINGE WEB PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998070300415 19980703 00415 NM 1998 7 3 P5CA9801069 1 19980626 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION ON STRINGER S48 BS 1720 TO 1740 AFT CARGO AREA RIGHT SIDE. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300416 19980703 00416 NM 1998 7 3 P5CA9801070 1 19980626 A 5321 FLOOR BOEING 747 747123 1384873 NM CARGO COMPT CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO FLOOR PANELS 1920 TO 2040 LT TO RT FOUND CORROSION ON LOWER EDGE AREA. CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998070300417 19980703 00417 NM 1998 7 3 P5CA9801071 1 19980626 A 5730 PANEL BOEING 747 747123 1384873 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT WING UPPER SURFACE ALONG FRONT SPAR CHORD SEVERAL AREAS OF FIBERGLASS LAYERS CRACKED. FIBERGLASS REPAIRED PER SRM 51 -40-18. 2 L 7 4 4F A20WE 1998070300418 19980703 00418 NM 1998 7 3 P5CA9801072 1 19980626 A 5311 RIBS BOEING 747 747123 1384873 NM BS 2160-2200 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMPART LEFT SIDE RIBS ATTACHED TO BULKHEAD BETWEEN BS 12160 TO 2200 FOUND CRACKED AND DEFORMED. REPAIRED PE R SRM 51-40-03 AND REPROTECTED PER SRM 51-24-11. 2 L 7 4 4F A20WE 1998070300419 19980703 00419 NM 1998 7 3 P5CA9801073 1 19980626 A 5320 SUPPORT BOEING 747 747123 1384873 NM CARGO COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO COMP BELOW FLOOR STRUCTURE TIE DOWN SUPPORT HAT SECTION CRACKED AND DEFORMED AT LT NR 2 I/B ONE FROM BS 1960 TO BS 1970. HAT SECTION REPAIRED PER SRM 51-40-03 FIG 1. REPROTECTED PER MM 51-24-11. 2 L 7 4 4F A20WE 1998070300420 19980703 00420 NM 1998 7 3 P5CA9801074 1 19980626 A 5320 WEB BOEING 747 747123 1384873 NM CARGO COMPT CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 BULK CARGO AREA STA 1940 S40 LT SUPPORT WEB FOUND CRACKED. SUPPORT WEB REPAIRED PER SRM 51-40-02 FIG 1. HFEC INSP PER NDT PART 6, 51-00-00 FIG 4. STOP DRILLED CRACK, NO CRACK BEYOND STOP DRILL. PROTECTED PER MM 51-24-11. 2 L 7 4 4F A20WE 1998070300421 19980703 00421 NM 1998 7 3 P5CA9801075 1 19980626 A 5753 SKIN BOEING 747 747123 1384873 NM RT TE FOREFLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT WING INBOARD FOREFLAP LOWER SURFACE FOUND DELAMINATED. REPAIRED AREA OF FIBERGLASS DELAMINATION PER SRM 51-40-12. 2 L 7 4 4F A20WE 1998070300422 19980703 00422 NM 1998 7 3 P5CA9801076 1 19980626 A 3213 STRUT BOEING 747 747123 1384873 NM RT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 RT BODY GEAR SHOCK STRUT SURFACE CORROSION AT FORWARD FACE OF SHOCK STRUT. CORROSION REMOVED PER SRM 51-10-01. SHOT PE ENING CARRIED OUT PER OHM 20-10-03. STYLUS CADMIUM PLATING APPLED PER OHM 32-10-21. 2 L 7 4 4F A20WE 1998070300423 19980703 00423 NM 1998 7 3 P5CA9801077 1 19980625 A 5730 SKIN BOEING 747 747123 1384873 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 LEVEL 1 CORROSION FOUND ON RT WING LOWER SKIN FWD OF FRONT SPAR. THE AREA HAS BEEN PREVIOUSLY BLENDED. CORROSION REMOV ED AND REPROTECTED PER HAECO REPAIR SCHEME NR R57-26-33785. 2 L 7 4 4F A20WE 1998070300425 19980703 00425 NM 1998 7 3 VNAA9806015 1 19980625 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 426JS 55372 6718 3038 DURING THE PREFLIGHT INSPECTION,THE GALLEY AREA EMERGENCY EXIT SIGN, FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE INSP ECTED AND REPLACED THE 7LK BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WER E COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998070300427 19980703 00427 WP 1998 7 3 VJ9800206 1 19980626 A 2560 702957A COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE LOOSE A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 CHECK SLIDE COVER ON GALLEY DOOR. REINSTALLED DOOR SLIDE COVER IAW MM 25-60-1 AND PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998070300428 19980703 00428 WP 1998 7 3 VJ9800207 1 19980620 A 3350 P2010014 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 967VV 47170 EMERGENCY EXIT LIGHT AT GALLEY DOOR INOP. REPLACED LIGHT, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998070300429 19980703 00429 WP 1998 7 3 VJ9800208 1 19980627 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 967VV 47170 EMERGENCY LIGHTS AT FORWARD GALLEY, COCKPIT AND OVERWING INOP. REPLACED BATTERIES, OPS CHECKED GOOD IAW MM 33-50. 2 L 7 2 4F A6WE 1998070300430 19980703 00430 NM 1998 7 3 K3HA980085 1 19980628 A 3350 3071BPEGPL LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHT OUT SECOND LIGHT FORWARD CABIN. RELAMPED EMERGENCY PATH LIGHT, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998070300431 19980703 00431 NE 1998 7 3 CALA9801183 2 19980627 A 7310 7958538503 FUEL TUBE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE NR 2 ENGINE RUPTURED A A CALA O OTHER X K ENGINE FLAMEOUT FLUID LOSS CR CRUISE 1 SW 09 16807 49261 717409 THE NR 2 ENGINE FLAMED OUT WHILE EN ROUTE FL330. THE NR 2 ENGINE WAS RESTARTED. THE NR 2 ENGINE FLAMED OUT A SECOND TI ME AND WAS RESTARTED AGAIN. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NR 2 ENGINE FUEL FLEX TUBE RUPTURED. THE FUEL FLEX TUBE WAS REMOVED AND REPLACED IAW MM 73-11-02, PAGE 216. THE F UEL FILTER WAS REPLACED AS A PRECAUTIONARY MEASURE. IN ADDITION, THE MOISTURE TRAP AND SENSE LINE WERE CHECKED WITH NO DEFECTS NOTED. A LEAK CHECK WAS PERFORMED WITH NO LEAKS FOUND. A POWER ASSURANCE RUN WAS PERFORMED ON THE NR 2 ENGINE AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F A6WE E9NE 1998070300432 19980703 00432 WP 1998 7 3 CALA9801184 1 19980629 A 5210 INTERCOSTAL DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND A .5 INCH CRACK AT EXTERNAL HANDLE RECESS CUP OF MAIN CABIN DOOR INTERCOSTAL. THE INTERCOSTAL WAS REMO VED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998070300433 19980703 00433 WP 1998 7 3 CALA9801185 1 19980629 A 5320 SPACER DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND CORROSION ON AFT BAGGAGE BIN Z-ANGLE REPAIR SPACER AT STA 1155 TO 1212. THE REPAIR SPACER WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998070300434 19980703 00434 WP 1998 7 3 CALA9801186 1 19980630 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND A .25 INCH CRACK IN MAIN CABIN DOOR SKIN WITH DEEP WEAR MARKS ON HOLD OPEN HOOK PAN ON DOOR. A REPAIR DOUBLER WAS INSTALLED AND THE PAN WAS REPLACED IAW SRM 52-05. 2 L 7 2 4F A6WE 1998070300435 19980703 00435 NM 1998 7 3 CALA9801187 1 19980627 A 3397 WIRE BOEING 737 7373T0 1384582 NM CABIN DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND THE EMERGENCY PATH LIGHTING INOPERATIVE FROM ROW 6ABC TO 12AB. TROUBLESHOOTING FOUND A CRUSHED WIRE UN DER SEAT AT ROW 9ABC. THE WIRE WAS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED. 2 L 7 2 4F RT A16WE 1998070300436 19980703 00436 WP 1998 7 3 CALA9801188 1 19980629 A 5280 DOOR DOUG DC10 DC1010 3022110 WP LT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68046 47800 INSPECTION FOUND A 1 INCH CRACK WITH CORROSION ON LT MLG DOOR ADJACENT TO LANDING GEAR BUMPER UPPER ATTACH POINT. THE C RACKED AND CORRODED AREA WAS TRIMMED AND BLENDED OUT. A REINFORCEMENT SPLICE PLATE AND ANGLE WERE INSTALLED IAW SRM 52- 10-00, FIGURE 5, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998070300437 19980703 00437 NE 1998 7 3 CALA9801171 2 19980625 A 7200 ENGINE BOEING 737 737130 1384435 NM PWA JT8 JT8D7 52053 NE NR 1 MALFUNCTIONED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 09 14209 19206 655865 THE NR 1 ENGINE LOST POWER DURING CLIMB-OUT OF EWR AT 1800 FEET. THE ENGINE WENT TO IDLE POWER. THE NR 1 ENGINE WAS SH UT DOWN PER FLIGHT MANUAL AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS RE MOVED AND REPLACED. THE ENGINE IS BEING PLACED IN LONG TERM STORAGE AND NO TEARDOWN IS PLANNED. 2 L 7 2 4F 4 F A16WE E2EA 1998070300438 19980703 00438 WP 1998 7 3 9809629996 1 19980623 A 3230 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 8932E 47141 NOSE LANDING GEAR WOULD NOT EXTEND ON LANDING INTO IAD. CREW RECYCLED GEAR AND NOSE GEAR EXTENDED NORMALLY WITH PROPER INDICATIONS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR OVERCENTER LINKAGE AND LEFT DOOR OUT OF RIG . ADJUSTED LINKAGE AND DOOR, OPERATIONAL CHECK NORMAL ON TEST FLIGHT. 2 L 7 2 4F A6WE 1998070300440 19980703 00440 WP 1998 7 3 9809649918 1 19980626 A 3260 SENSOR DOUG DC9 DC932 3022066 WP NLG BROKEN A NWAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 GL 01 940N 47572 DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. EMERGENCY GEAR EXTENSION PROCEDURES W ERE UTILIZED AND FLIGHT WAS DIVERTED TO ORD. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PR OXIMITY SENSOR BROKEN. REPLACED SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998070300441 19980703 00441 WP 1998 7 3 9809659985 1 19980627 A 2130 AUGMENTATION VLV DOUG DC9 DC932 3022066 WP CABIN PRESSURE FAILED A NWAA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 GL 01 985US 47479 LOSS OF CABIN PRESSURE OCCURRED DURING CRUISE FLIGHT AT 33,000 FEET EN ROUTE. CREW ACCOMPLISHED EMERGENCY DESCENT AND F LIGHT WAS DIVERTED TO MKE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AUGMENTATION VALVE AND BROKEN L EFT ENGINE ANTI-ICE DUCT, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998070300442 19980703 00442 WP 1998 7 3 9809669610 1 19980628 A 2130 CLAMPS DOUG DC9 DC932 3022066 WP LT AUG VALVE LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 610NW 47432 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDE NT. MAINTENANCE REPLACED CLAMPS AT LEFT AUGMENTATION VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998070300443 19980703 00443 WP 1998 7 3 9809679105 1 19980629 A 2131 10256861 CONTROLLER DOUG DC9 DC915 3022036 WP COCKPIT FAILED A NWAA B EMER. DESCENT J G WARNING INDICATION MULTIPLE FAILURE CR CRUISE 1 GL 01 95S 4159 3218 47205 AT FL290, THE CABIN PRESSURE BEGAN CLIMBING 1500 FEET PER MINUTE. THE FLIGHT CREW CLOSED THE OUTFLOW VALVE, CHECKED FOR CLOSED CROSSFEED VALVES, FOLLOWED EMERGENCY CHECK LIST, AND INITIATED AN EMERGENCY DESCENT TO FL100. THE OXYGEN MASK A UTO DEPLOY SYSTEM OPERATED AT FL100. THE FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPL ACED THE CABIN PRESSURE CONTROLLER, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998070300444 19980703 00444 EU 1998 7 3 QXEA9800827 1 19980628 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 EMERGENCY EXIT LIGHT IN SIGN AT ROW 9-CDE IS OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998070300445 19980703 00445 EU 1998 7 3 QXEA9800828 1 19980628 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 EMERGENCY EXIT LIGHT IN CEILING AT ROW 9 IS OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998070300446 19980703 00446 EU 1998 7 3 QXEA9800829 1 19980626 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 CABIN EMERGENCY EXIT SIGN ABOVE COCKPIT DOOR IS DIM. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998070300447 19980703 00447 NM 1998 7 3 QXEA9800830 1 19980628 A 3350 10126267 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN MISSING A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 355PH 500 EXIT SIGN AT THE LEFT UNDERWING EXIT MISSING. REPLACED SIGN, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998070300448 19980703 00448 NM 1998 7 3 QXEA9800831 1 19980626 A 3350 10126267 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 821PH 104 THRESHOLD EXIT SIGN BROKEN AT THE RIGHT UNDERWING EXIT DOOR. INSTALLED NEW SIGN AT THE RIGHT UNDERWING EXIT, OPERATIONA L CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998070300449 19980703 00449 NM 1998 7 3 98FDEA00422 1 19980630 A 3610 PACK VALVE BOEING 727 72722 1384002 NM NR 1 BLEED LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 181FE 18868 CLIMBING THRU 17,000 LOWER AFT BODY HEAT LIGHT CAME ON. COMPLIED WITH PROCEDURES. LIGHT WENT OUT AFTER SECURING NR 1 B LEED. LEAK BETWEEN PACK AND BLEED VALVE ON NUMBER 1 ACCORDING TO PROCEDURE. RAN ENGINE DUPLICATING BLEED CONFIGURATION . CHECKED DUCTING CLAMPS FOR SECURITY WITH NO LEAKS OR DEFECTS NOTED. AFT BODY OVERHEAT LIGHT REMAINED EXTINGUISHED. O PERATIONAL CHECKS OK PER 26-14-00. 2 L 7 3 4F A3WE 1998070300450 19980703 00450 NM 1998 7 3 98UAL900197 1 19980516 A 3230 LOGIC CARD 806002 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E/E COMPT FAILED A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 930UA 26655 THE LANDING GEAR WOULD NOT RETRACT ON TAKEOFF UNTIL THE PILOT USED THE OVERRIDE TRIGGER. *S/D* REPLACED THE AIR SENSIN G LOGIC CARD (M991). 2 L 7 2 4F 4 F RT A16WE E2GL 1998070300451 19980703 00451 WP 1998 7 3 98UAL900219 1 19980527 A 3610 9057M84G03 MANIFOLD GE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE FAILED A UALA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CL CLIMB 1 WP 29 1853U 47812 517273 OVERTEMP LIGHT WENT ON NR 1 ENG, EGT 945 DEG. REDUCED POWER DURING CLIMB TO APPROX 108 PERCENT N1 AND LIGHT WENT OUT. A PPROX 500 FEET DURING CLIMB, BOTH ENG FIRE LOOP LIGHTS ILLUM AND WARNING HORN ALARM SOUNDED. CHECKLIST FOR ENG FIRE ACC P AND FIRE LIGHT WENT OUT AFTER NR 1 THRUST WAS REDUCED TO IDLE. SHUTDOWN ENG. *S/D* THE ENG 14TH STAGE CDP LT MANIFO LD FAILED, ACTIVATING THE FIRE WARNING SYSTEM. ANALYSIS OF THE MANIFOLD THAT FAILED INDICATED FATIGUE FAILURE AT THE JU NCTION OF THE LT UPPER BLEED TUBE TO THE MAIN DUCT. SINCE THIS PART NUMBER MANIFOLD HAS HAD A VERY LOW HISTORICAL FAILU RE RATE, IT IS FELT THAT AN EXTERNAL PERLOAD CAUSED THE ABNORMAL STRESS AND FAILURE. 2 L 7 3 4F 4 F A22WE E23EA 1998070300452 19980703 00452 WP 1998 7 3 98UAL900272 1 19980620 A 3610 DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN FAILED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 1858U 46987 A BANG AND RUSHING SOUND OF AIR REPORTED COMING FROM AREA OF DOOR 4 CROSS AISLE. RETURNED TO GATE. 2 L 7 3 4F 4 F A22WE E23EA 1998070300453 19980703 00453 NE 1998 7 3 98UAL900273 2 19980620 A 7310 A60302B SWITCH BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FUEL FILTER FAILED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 614UA 21875 709612 FUEL FILTER LIGHT WOULD NOT EXTINGUISH. RETURNED TO ORD. *S/D* REPLACED THE FUEL FILTER AND THE FUEL FILTER DIFFERENT IAL PRESSURE SWITCH. THERE HAS BEEN NO FURTHER PROBLEMS WITH THIS SYSTEM. 2 L 7 2 4F 4 F RT A1NM E3NE 1998070300454 19980703 00454 NM 1998 7 3 98UAL900274 1 19980619 A 2130 PRESSURIZATION BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 9032U 19070 AIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY. 2 L 7 2 4F 4 F A16WE E2EA 1998070300455 19980703 00455 NM 1998 7 3 98UAL900275 1 19980621 A 2613 WIRE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 2 FUEL CONTL LOOSE A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 987UA 21749 NUMBER TWO ENGINE OVER TEMPERATURE INDICATION. *S/D* HEAT DAMAGE NEAR FRONT OF FUEL CONTROL CAUSED WIRE TO BE PULLED L OOSE. REPLACED CONNECTOR. 2 L 7 2 4F 4 F A16WE E2EA 1998070300456 19980703 00456 1998 7 3 98UAL900276 4 19980621 A 2350 3F17567501 SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT COCKPIT STICKING A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 316UA 23948 INTERMITTENT RADIO FAILURE. *S/D* REPLACED FIRST OFFICER'S PENDANT (PUSH-TO-TALK) SWITCH BECAUSE OF STICKING. 2 L 7 2 4F 4 F RT A16WE E2GL 1998070300457 19980703 00457 NM 1998 7 3 98UAL900277 1 19980619 A 5610 141W74002 WINDOW PPG BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE COCKPIT CRACKED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 771UA 1572 26932 APPROXIMATELY ONE HOUR AFTER DEPARTURE, FLIGHT EXPERIENCED PROBLEM WITH RIGHT FORWARD WINDOW ARCING AND CRACKED. FLIGHT RETURNED TO ORD LANDING OVERWEIGHT. PRELIMINARY FINDINGS INDICATES DELAMINATION OF THE ANTI FOG LAYER CAUSING ARCING F ROM THE BUS BAR, AND RESULTING IN CRACKING. WINDOW P/N 141W7400-2 WAS REPLACED AND THE AIRPLANE WAS RETURNED TO SERVICE . SUSPECT FAILURE WAS CAUSED FROM WORKMANSHIP. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998070300458 19980703 00458 NM 1998 7 3 98UAL900278 1 19980618 A 2780 H1010261 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 LE FLAP FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7277U 21424 RIGHT WING NR 4 LEADING EDGE FLAP DID NOT EXTEND. *S/D* REPLACED NR 4 LEADING EDGE FLAP POSITION SWITCH. SYSTEM OPS C HECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998070300459 19980703 00459 NM 1998 7 3 98UAL900280 1 19980618 A 7997 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE LOOSE A UALA D RETURN TO BLOCK O OTHER NR NOT REPORTED 1 WP 29 7273U 21420 NR 3 ENGINE OIL TEMPERATURE ERRATIC. RETURNED TO BLOCKS. *S/D* CORRECTED WEAK GROUND FOR THE OIL TEMPERATURE INDICATI NG SYSTEM. NO RECCURRENCE. 2 L 7 3 4F 4 F A3WE E2EA 1998070300460 19980703 00460 NM 1998 7 3 98UAL900281 1 19980619 A 3260 1EN161RB1 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG DOOR FAILED A UALA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 29 7290U 21568 RIGHT MAIN LANDING GEAR WOULD NOT RETRACT WITH GEAR LEVER UP. FLIGHT CONTINUED TO DEN FROM COS. *S/D* REPLACED RT GE AR DOOR WARNING SWITCH, ADJUSTED AND CKD PER MAINTENANCE MANUAL. ACCOMPLISHED GEAR SWING, OPS CK GOOD. MANUAL GEAR DRO P GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1998070300461 19980703 00461 WP 1998 7 3 98UAL900282 1 19980620 A 5312 BULKHEAD DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL BS 1156 CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 1817U 46616 BS 1156 PRESSURE BULKHEAD FORWARD LEFT HAND SIDE AT L40 LONGERON HAS A CRACK. MANUFACTURED AND INSTALLED NEW REPAIR ANG LE. 2 L 7 3 4F 4 F A22WE E23EA 1998070300462 19980703 00462 NM 1998 7 3 98UAL900284 1 19980621 A 3397 WIRE BOEING 747 747422 1384935 NM CABIN FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 197UA 26901 EEL LIGHT INOP AT DOOR 4R CROSS AISLE. REPAIRED FEEDER PER GN 2-0-15-5, OPS CK OK. 2 L 7 4 4F RT A20WE 1998070300463 19980703 00463 NM 1998 7 3 98UAL900285 1 19980623 A 2560 GIRT BAR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 3R OUT OF ADJUST A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 560UA 26660 DOOR 3R WOULD NOT ARM. *S/D* SLIDE ARMED LIGHT DID NOT COME ON WHEN SLIDE ARMED. FOUND GIRT BAR OUT OF SEQUENCE. REA DJUSTED GIRT BAR. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998070300464 19980703 00464 GL 1998 7 3 98UAL900286 2 19980623 A 7261 OIL PRESSURE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 2 ENGINE LOST A UALA E ENGINE SHUTDOWN J WARNING INDICATION UK UNKNOWN 1 WP 29 1831U 46630 451566 LANDED ORD UNDER AMBER ALERT WITH NR 2 ENGINE SHUT DOWN DUE TO LOSS OF OIL PRESSURE. 2 L 7 3 4F 4 F A22WE E23EA 1998070300465 19980703 00465 NM 1998 7 3 98UAL900287 1 19980623 A 2130 VALVE HAMILTON STA 7110035 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE PRESSURE SYST MALFUNCTIONED A UALA B EMER. DESCENT O OTHER CL CLIMB 1 WP 29 7291U 21569 CLIMB POWER SET CLIMBING THROUGH 27,000 FEET CABIN ALTITUDE RISING THROUGH 9,500 FEET AT 700 FEET PER MINUTE. TRIED STA NDBY MANUAL AC AND DC, ALL TO NO AVAIL. BOTH PACKS OPERATING. DURING EMERGENCY DESCENT CABIN STARTED PRESSURIZATION IN STANDBY ONCE AIRCRAFT WAS STABILIZED AT 10,000 FEET. *S/D* REPLACED TASK VALVE DUE TO NOT CLOSING ON SCHEDULE. RAN E NGS AND CHECKED PNEUMATICS, FOUND GOOD. AC PRESSURIZED NORMALLY AND TASK VALVE CLOSED. 2 L 7 3 4F 4 F A3WE E2EA 1998070300466 19980703 00466 WP 1998 7 3 98UAL900288 1 19980624 A 3350 102100208 ANNUNCIATOR PNL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 1852U 2531 47811 EMERGENCY DISARMED LIGHT IS INOP. *S/D* REPLACED ANNUNCIATOR PANEL. 2 L 7 3 4F 4 F A22WE E23EA 1998070300467 19980703 00467 NM 1998 7 3 98UAL900289 1 19980623 A 3350 1102833LB LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7451U 21905 FORWARD ENTRY DOOR INTERIOR EEL LIGHT INOPERATIVE. *S/D* REPLACED LIGHT ASSY. 2 L 7 3 4F 4 F A3WE E2EA 1998070300468 19980703 00468 NE 1998 7 3 98UAL900290 2 19980625 A 7200 BEARING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 551UA 137 137 25399 727195 DIVERTED TO LAS DUE TO AN OIL INDICATION LIGHT ON THE RIGHT ENGINE. *S/D* METAL WAS FOUND IN THE MAIN OIL FILTER AND O N ALL CHIP DETECTORS. THIS WAS CAUSED BY A FAILED BUMPER BEARING. ENGINEERING HAS CREATED TASKS TO REPLACE THE BUMPER B EARINGS. 2 L 7 2 4F 4 F RT A2NM E17NE 1998070300469 19980703 00469 WP 1998 7 3 ABXA9800555 1 19980519 A 5320 37502571 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STATION 600 TO 620 LONGERON 31L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998070300470 19980703 00470 WP 1998 7 3 ABXA9800556 1 19980519 A 5320 37502571N FITTING DOUG DOUG DC8 DC863F 302198F WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STATION 440 TO 460 LONGERON 31R SPLICE FITTING IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21D AND 51-1-20D. 2 L 7 4 4F 4A25 1998070300471 19980703 00471 WP 1998 7 3 ABXA9800557 1 19980506 A 5712 5770124 RIB DOUG DOUG DC8 DC863F 302198F WP WS 227.335 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB STATION XS 227.335 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056 AND SRM 51-1 -20D. 2 L 7 4 4F 4A25 1998070300472 19980703 00472 WP 1998 7 3 ABXA9800558 1 19980505 A 5712 975329413 RIB DOUG DOUG DC8 DC863F 302198F WP WS 250.089 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT INBOARD STUB WING STATION XS 250.089 UPPER LEADING EDGE RIB CRACKED. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND DWG K05056. 2 L 7 4 4F 4A25 1998070300473 19980703 00473 WP 1998 7 3 ABXA9800559 1 19980505 A 5720 975329327 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 250.089 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT INBOARD STUB WING HAS 2 CRACKS AT STATION XS 250.089. REPAIRED IAW DC8 SRM 57-2-0, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 1998070300474 19980703 00474 WP 1998 7 3 ABXA9800560 1 19980504 A 5320 975329423 STIFFENER DOUG DOUG DC8 DC863F 302198F WP WS 250.089 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT INBOARD STUB WING AT STATION XS 250.089, THE VERTICAL STIFFENER ANGLE (RIB ATTACH ANGLE) IS CRACKED AT THE BOTTOM E ND. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-8. 2 L 7 4 4F 4A25 1998070300475 19980703 00475 WP 1998 7 3 ABXA9800561 1 19980504 A 5712 5769857613 RIB DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 THE LEFT OUTBOARD SLOT OUTBOARD UPPER CLOSURE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F 4A25 1998070300476 19980703 00476 WP 1998 7 3 ABXA9800562 1 19980504 A 5712 5769857614 RIB DOUG DOUG DC8 DC863F 302198F WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING OUTBOARD SLOT, OUTBOARD UPPER CLOSURE RIB IS CRACKED. REPAIRED IAW DC8 SRM 51-3-0 AND 51-1-21. 2 L 7 4 4F 4A25 1998070300477 19980703 00477 WP 1998 7 3 ABXA9800563 1 19980511 A 5320 561570011 WEB DOUG DOUG DC8 DC863F 302198F WP BS 150-160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LOWER TORQUE BOX WEB CRACKED AND CORRODED BEYOND LIMITS, FWD GALLEY DOOR FS 150 TO FS 160, LONGERON 17R TO LONGERON 21R . REPAIRED IAW DC8 SRM 51-1-21, 51-1-20, 51-1-8 AND 51-1-11. 2 L 7 4 4F 4A25 1998070300478 19980703 00478 WP 1998 7 3 ABXA9800564 1 19980511 A 5320 56157009 ANGLE DOUG DOUG DC8 DC863F 302198F WP BS 190-200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 TORQUE BOX WEB LOWER SUPPORT ANGLE CRACKED FROM FS 190 TO FS 200, LONGERON 21R. REPAIRED IAW DWG 575700 AND DC8 SRM 51- 1-21, 51-1-21D AND 51-1-8. 2 L 7 4 4F 4A25 1998070300479 19980703 00479 WP 1998 7 3 ABXA9800565 1 19980619 A 5313 59114277 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 16 LEFT CRACKED AT PYLON UPPER ATTACH BOLT AT FS 1041. REPAIRED LONGE RON IAW DC9 SRM CHAPTER 53-02. 2 L 7 2 4F A6WE 1998070300480 19980703 00480 WP 1998 7 3 ABXA9800566 1 19980619 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1052 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 RIGHT CRACKED AT UPPER FASTENER HOLE ATTACHING IT TO BULKHEAD AT FS 1052. REPLACED LONGERON SECTION IAW DC9 SRM CHAPTER 53-02. 2 L 7 2 4F A6WE 1998070300481 19980703 00481 WP 1998 7 3 ABXA9800567 1 19980619 A 5313 59114279 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT PYLON ATTACH BOLT AT FS 1041. REPAIRED LONGERON IA W DC9 SRM CHAPTER 53-02. 2 L 7 2 4F A6WE 1998070300482 19980703 00482 WP 1998 7 3 ABXA9800568 1 19980620 A 5315 9915527506 FLOORBEAM DOUG DOUG DC9 DC941 302207N WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH C-INSPECTION, FOUND A FLOORBEAM AT FS 718 CRACKED AT RBL 48. REPLACED FLOORBEAM IAW DC9 SRM CHAPTE RS 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300483 19980703 00483 WP 1998 7 3 ABXA9800570 1 19980618 A 5711 5911300501 SPAR CAP DOUG DOUG DC9 DC941 302207N WP WS 160 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH C-INSPECTION, FOUND LEVEL 2 CORROSION ON THE LEFT WING REAR SPAR UPPER T-CAP AT STATION XRS 160. R EPAIRED LEFT WING REAR SPAR UPPER CAP IAW ABX REA D957-23974 MR. 2 L 7 2 4F A6WE 1998070300484 19980703 00484 WP 1998 7 3 ABXA9800571 1 19980606 A 5311 259415 FRAME DOUG DOUG DC8 DC861 3021952 WP BS 80 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 FORWARD LOWER CARGO CIRCUMFERENTIAL FRAME CORRODED AT STATION 80, LONGERON 29R. REPAIRED IAW DC8 SRM 55-2-2 AND 51-1-9A . 2 L 7 4 4F 4A25 1998070300485 19980703 00485 WP 1998 7 3 ABXA9800572 1 19980626 A 5315 995821225 FLOORBEAM DOUG DOUG DC9 DC933F 302207A WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND THE LOWER TEE CAP OF THE FLOORBEAM THAT ATTACHES TO THE TOP OF THE AFT BULKHEAD OF THE LEFT WHEEL WELL EXFOLIATED. REPAIRED IAW ABX REA D953-23942-MR. 2 L 7 2 4F A6WE 1998070300486 19980703 00486 WP 1998 7 3 ABXA9800573 1 19980626 A 5320 99581763 INTERCOSTAL DOUG DOUG DC9 DC933F 302207A WP BS 992-945 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND INTERCOSTAL AT STATION 929 TO 945 AND LONGERON 11L CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL I AW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300487 19980703 00487 WP 1998 7 3 ABXA9800574 1 19980626 A 5320 995815019 INTERCOSTAL DOUG DOUG DC9 DC933F 302207A WP BS 465-484 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND INTERCOSTAL AT STATION 465 TO 484 AND LONGERON 6 L CORRODED BEYOND LIMITS. REPLACED INTERCOSTAL I AW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300488 19980703 00488 WP 1998 7 3 ABXA9800587 1 19980625 A 3350 60030431 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 958AX 47760 COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1998070300489 19980703 00489 WP 1998 7 3 ABXA9800588 1 19980629 A 5250 AR25291GR41 LATCH DOUG DC9 DC941 302207N WP COCKPIT DOOR INOPERATIVE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 967AX 47509 COCKPIT DOOR INSIDE LATCH INOPERATIVE. CREW WAS UNABLE TO OPEN DOOR FROM COCKPIT. REPAIRED AS REQUIRED. 2 L 7 2 4F A6WE 1998070300490 19980703 00490 WP 1998 7 3 ABXA9800589 1 19980630 A 5250 AR25291GR41 LATCH DOUG DC9 DC941 302207N WP COCKPIT DOOR LOOSE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 967AX 47509 COCKPIT DOOR LATCH LOOSE ON THE INSIDE, SOMETIMES WOULD BIND. REPLACED LATCH ASSY. 2 L 7 2 4F A6WE 1998070300491 19980703 00491 NM 1998 7 3 RRXA98244 1 19980626 A 2611 SMOKE LIGHT BOEING 727 727222 1384073 NM CARGO COMPT ILLUMINATED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 7635U 19908 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT. SMOKE DETECTOR SYSTEM OPS CHECKS NORMAL. 2 L 7 3 4F A3WE 1998070300492 19980703 00492 1998 7 3 VNAA9806017 4 19980626 A 3418 861EF1 AOA SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 424JS 3033 A STICK PUSHER FAIL WARNING OCCURED DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAI NTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO DCA, TO ACCOMPLISH REPAIR. THE FERRY FLIGHT TOOK PLA CE WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED WITH PARTS TO DCA FROM PIT, TO MEET THE AIRCRAFT. MECHANIC INSPECTED A ND REPLACED THE LEFT HAND ANGLE OF ATTACK SENSOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-33-01. OPERATIONAL C HECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998070300527 19980703 00527 EU 1998 7 3 SIMA981384 1 19980518 A 3350 AD3127 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AT 11779 0249 ORD - TWO EMERGENCY FLOOR LIGHT BULBS BURNED OUT. ISSUED MEL. REPLACED EMERGENCY POWER SUPPLY BATTERIES. PERFORMED OP ERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300528 19980703 00528 EU 1998 7 3 98ZZZM453 1 19980518 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AT 5239 0249 ORD - TWO EMERGENCY FLOOR LIGHT BULBS BURNED OUT. ISSUED MEL. REPLACED EMERGENCY POWER SUPPLY BATTERIES. PERFORMED OP ERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300529 19980703 00529 WP 1998 7 3 ORJA98100 1 19980516 A 3350 BR9661116 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 EMERGENCY ESCAPE LIGHTS INOP AT AFT WING AND AFT GALLEY. TROUBLESHOT EMERGENCY LIGHTING, FOUND BAD BATTERY UNITS PER MM 33-53-01, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998070300530 19980703 00530 WP 1998 7 3 98ZZZM454 1 19980516 A 3350 59306431 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 EMERGENCY ESCAPE LIGHTS INOP AT AFT WING AND AFT GALLEY. TROUBLESHOT EMERGENCY LIGHTING, FOUND BAD BATTERY UNITS PER MM 33-53-01. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998070300531 19980703 00531 WP 1998 7 3 ORJA9898 1 19980513 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 TAILCONE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED VENTRAL STAIR BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998070300532 19980703 00532 CE 1998 7 3 98ZZZM455 1 19980327 A 5511 1016200171 RIB BEECH 1900 1900D 1154162 CE HORIZ STAB CRACKED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 860CA 6847 UE134 DURING REMOVAL OF LEFT HORIZONTAL STABILIZER DE-ICE BOOT, RIVET HEADS FROM LEADING EDGE RIBS WERE STUCK TO OLD DE-ICE BO OT. UPON FURTHER INVESTIGATION AND INSPECTION OF COMPLETE HORIZONTAL STABILIZER, A TOTAL OF 6 LEADING EDGE RIBS AND 4 C ENTER RIBS WERE FOUND TO BE CRACKED AT VARIOUS LOCATIONS. ALL WERE REPLACED WITH NEW PARTS FROM FACTORY. 2 L 7 2 4T RT A24CE 1998070300533 19980703 00533 EU 1998 7 3 JBXA980039 1 19980521 A 7722 INDICATOR FOKKER F28 F28MK0100 4990807 EU NR 1 TGT MALFUNCTIONED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 103ML 11444 ON TAKEOFF ROLL LEVEL 3 HI TGT ALERT ENGINE NR 1. PERFORMED OVERTEMP INSPECTION PER MM 71-00-00 TASK 71-00-00-200-065-0 00. NO DEFECTS NOTED. RAN ENGINE PER MM 71-00-00. ENGINE RUN OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT 1998070300534 19980703 00534 WP 1998 7 3 GTIA9800059 1 19980514 A 3397 WIRE DOUG DC9 DC931 3022065 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 DTW - ONE LIGHT IN FLOOR TRACK EMERGENCY LIGHTING INOPERATIVE AT 17D, LENS COVER IS MISSING. REATTACHED LOOSE WIRE AND REPLACED BULB AND LENS COVER AS REQUIRED. (M) 2 L 7 2 4F A6WE 1998070300535 19980703 00535 SO 1998 7 3 GLBA98068 1 19980424 A 5312 360175450 FIRE LOOP EMB 120 EMB120RT SO LT ENGINE CHAFED A GLBA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 01 281UE 120092 LT WHEEL WELL FIRE DETECTION ILLUMINATED. AIRCRAFT RETURNED TO GATE. REPLACED FIRE LOOP. (M) 2 L 7 2 4T RT A31SO 1998070300536 19980703 00536 NM 1998 7 3 F3LA98069 1 19980527 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 907 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 26R, BS 907 PLUS 15, RBL 13, WL 169. MAINTENANCE REMOVE D DAMAGED AREA (1.5 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, 53-10-1 AND 53 -10-3. (M) 2 L 7 2 4F A16WE 1998070300537 19980703 00537 NM 1998 7 3 F3LA98067 1 19980527 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL RIGHT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA 12 INCHES. FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998070300538 19980703 00538 NM 1998 7 3 F3LA98062 1 19980529 A 5330 SKIN BOEING 737 737201 1384454 NM BS 949 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN AFT SERVICE DOOR SKIN ABOVE LOWER HINGE CUTOUT AT BS 949, STRINGER 14 R, WL 220. MAINTENANCE REMOVED DAMAGED AREA, 1.5 INCH BY 2.5 INCH. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 5 2-00-3. (M) 2 L 7 2 4F A16WE 1998070300539 19980703 00539 NM 1998 7 3 F3LA98065 1 19980527 A 5320 SHEAR TIE BOEING 737 737201 1384454 NM BS 1006 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT BS 1006, LBL 4 THROUGH RBL 4, WL 178. MAINTENANCE R EMOVED CORRODED AREA, 1.5 INCH BY 2.5 INCH. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1998070300540 19980703 00540 NM 1998 7 3 F3LA98063 1 19980527 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, RBL 25, WL 195. MAINTENANCE FABRICATED REPLACE MENT PARTS AND REPAIRED PER ER 98-0476 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998070300541 19980703 00541 NM 1998 7 3 F3LA98064 1 19980527 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178, LBL 25, WL 195. MAINTENANCE FABRICATED REPLACE MENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998070300542 19980703 00542 NM 1998 7 3 F3LA98068 1 19980527 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD, LBL 4.7, WL 192.5 TO 193.5. MAINTENANCE REMOVED DAM AGED AREA, FABRICATED REPLACMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-11. (M) 2 L 7 2 4F A16WE 1998070300543 19980703 00543 SO 1998 7 3 98ZZZM456 1 19980430 A 5400 1159P41920145 FAIRING GULSTM G1159 GIV 3980115 SO LT PYLON CRACKED A COZA K NONE O OTHER IN INSP/MAINT 1 WP 27 232K 1232 DURING AIRCRAFT CLEANING, THE LEFT PYLON AFT METAL FAIRING WAS FOUND TORN. THIS ITEM IS NOT IDENTIFIED IN THE GIV IPC O R THE GIV SRM. GAC IS AWARE OF THIS PROBLEM AND DOES HAVE A HAND DRAWING OF THE FAIRING. GULFSTREAM NEEDS TO ADDRESS T HE PROBLEM WHEN THIS MUCH DAMAGE IS NOTED ON AN AIRCRAFT WITH ONLY 1688.4 HOURS, 726 CYCLES AND PROVIDE A REPAIR OR UPGR ADED PART, LIST THE ITEMS IN THE IPC/SRM, AND ADVISE GULFSTREAM OPERATORS OF THIS DEFECT. THE PART WAS REPLACED PRIOR T O THE NEX FLIGHT. 2 L 7 2 4F RT A12EA 1998070300544 19980703 00544 NM 1998 7 3 98ZZZM457 1 19980502 A 3350 BATTERY BOEING 727 7272Q8 138407W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 776AT 21608 RT CENTER OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1998070300545 19980703 00545 NM 1998 7 3 98ZZZM458 1 19980503 A 3350 BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 772AT 22003 L-2 AND R-2 AFT EXIT OVERHEAD LIGHT DOES NT WORK. REMOVED AND REPLACED BATTERY PACK, CHARGER ASSY. (M) 2 L 7 3 4F A3WE 1998070300546 19980703 00546 NM 1998 7 3 98ZZZM459 1 19980503 A 3350 CHARGER BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 772AT 22003 EGRESS LIGHT ABOVE AFT FLIGHT ATTENDANT JUMPSEAT INOP. REMOVED AND REPLACED BATTERY PACK CHARGER ASSY. (M) 2 L 7 3 4F A3WE 1998070300547 19980703 00547 NM 1998 7 3 98ZZZM460 1 19980512 A 3350 BATTERY BOEING 727 727290 138408W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 774AT 21510 AFT AIR STAIR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY. (M) 2 L 7 3 4F A3WE 1998070300548 19980703 00548 NM 1998 7 3 98ZZZM461 1 19980512 A 3350 PLUG BOEING 727 727290 138408W NM CABIN LOOSE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 774AT 21510 RT AFT OVERWING EGRESS LIGHT INOP. FOUND CANNON PLUG DISCONNECTED AT C-2 CARGO DOOR. RECONNECTED PLUG, OPS CHECKED NOR MAL. (M) 2 L 7 3 4F A3WE 1998070300549 19980703 00549 NM 1998 7 3 98ZZZM462 1 19980520 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 769AT 21998 R-1 SERVICE DOOR EXIT LGIHT INOP. REMOVED AND REPLACED EXIT LIGHT ASSY. (M) 2 L 7 3 4F A3WE 1998070300550 19980703 00550 NM 1998 7 3 98ZZZM463 1 19980517 A 3350 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 769AT 21998 AFT AIR STAIR OVERHEAD EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY. (M) 2 L 7 3 4F A3WE 1998070300551 19980703 00551 WP 1998 7 3 98ZZZM464 1 19980516 A 3350 LIGHT LKHEED 1011 10113851 5265010 WP CABIN MALFUNCTIONED A AMTA O OTHER O OTHER CR CRUISE 1 GL 11 188AT 193C1078 DURING CRUISE, THE EMERGENCY EVACUATION LIGHTS CAME ON, HAD TO TURNOFF AT OVERHEAD PANEL. THE EMERGENCY SENSE C/B 'J6' POPPED, WOULD NOT RESET. CONTINUED FLT. T/S EMERGENCY LIGHT SYSTEM PER FIM 33-59-10 UNABLE TO DUPLICATE PROBLEM. SYST EM OPERATIONAL. (M) 2 L 7 3 4F A23WE 1998070300552 19980703 00552 NM 1998 7 3 98ZZZM465 1 19980522 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 767AT 22001 AFT AIR STAIR OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT ASSY. (M) 2 L 7 3 4F A3WE 1998070300553 19980703 00553 NM 1998 7 3 98ZZZM466 1 19980510 A 3350 BATTERY BOEING 727 727208 138407W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 780AT 22295 OVERHEAD EGRESS LIGHT AT ROW 19 IS INOP. REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 3 4F RT A3WE 1998070300554 19980703 00554 NM 1998 7 3 98ZZZM467 1 19980520 A 3350 BATTERY BOEING 727 727214 138407R NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 786AT 21692 CEILING EGRESS LIGHT AT ROW 24 IS INOP. REMOVED AND REPLACED BATTERY, OPS CHECKED NORMAL. (M) 2 L 7 3 4F A3WE 1998070300555 19980703 00555 NM 1998 7 3 TAOA059811 1 19980521 A 2612 BACS30ES44 SWITCH BOEING 727 727254 138408L NM COCKPIT FAILED A TAOA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 15 913TS 20250 NR 1 ENGINE FIRE WARNING AT 3000 FT FIRE WARNING LIGHT AND BELL REPEATEDLY CYCLED ON AND OFF AFTER ENGINE SHUTDOWN. FIR E BOTTLE EXPENDED BOTH SIDES. FOUND WIRE NR W150-028-28 CHAFED AND SHORTING TO GROUND IN NR 1 ENGINE PYLON, REPAIRED WI RE PER CHAPTER 20 STANDARD OVERHAUL PRACTICES. SECURED AND PROTECTED WIRING INSIDE PYLON HOUSING. REPLACED NR 1 PYLON FIREWALL DETECTOR ELEMENT AND FIRE DETECTOR TEST SWITCH S467 IN COCKPIT. FIRE WARNING TESTS OK PER MM 26-11-0. (M) 2 L 7 3 4F A3WE 1998070300556 19980703 00556 NM 1998 7 3 GAIA9842 1 19980427 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1070 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6808 19483 THE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. FLOORBEAM STABILIZER CORRODED AT BS 1070 LBL 25. REMOVED CORRODED SECTION, FABRICATED REPAIR IAW B727 SRM 53-10-8. INSTALLED IAW B727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998070300557 19980703 00557 NM 1998 7 3 98ZZZM468 1 19980427 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6808 19483 THE FOLLOWING ITEM WS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. CORROSION ON LOWER SIDE OF UPPER FLANGE, FRAME 560 STRINGER 28R. REMOVED CORROSION IAW B727 SRM 51-10-6. FABRICATED NEW PART IAW 51-20-1. TREATED AND PRIMED I AW 51-10-2. INSTALLED IAW 51-30-2. (M) 2 L 7 3 4F A3WE 1998070300558 19980703 00558 NM 1998 7 3 98ZZZM469 1 19980427 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6808 19483 THE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. AFT PIT FUSELAGE FRAME CORRODED AT SKIN ATTACH FASTENER, BS 1110, STRINGER 27R. REPLACED STRAP AND FASTENERS IAW B727 SRM 51-20-1 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1998070300559 19980703 00559 NM 1998 7 3 98ZZZM470 1 19980427 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1070 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6808 19483 THE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. CORROSION ON FLOORBEAM UPPER CAP AT BS 1 070, LBL 12. FABRICATED PARTS IAW B727 SRM 53-10-8. REPAIRED AND INSTALLED IAW B727 SRM 53-10-1, 53-10-8. (M) 2 L 7 3 4F A3WE 1998070300560 19980703 00560 EA 1998 7 3 98ZZZM471 2 19980306 A 7230 COMPRESSOR BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA ENGINE INTERNAL FOD DAMAGE A YADA A UNSCHED LANDING C R F.O.D. PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 01 1563C UC20 PCE97527 DURING DESCENT FROM FL250 TO FL230 PILOT NOTICED NR 2 ENG ITT AT 760 DEGREES CELSIUS. PILOT REDUCED POWER TO 720 DEGREE S ITT. ONCE LEVEL AT FL 230, NR 2 ENGINE STARTED TO SURGE WITH SIGNS OF COMPRESSOR STALL. PILOT REDUCED POWER ON NR 2 TO LESS THAN 800 LBS OF TORQUE. DURING THE FIRST ATTEMPTING TO INCREASE TORQUE, AT 800 LBS ENGINE STARTED TO STALL AGA IN. PILOT TURNED AROUND AND RETURNED TO BET. THE SECOND ATTEMPTS TO INCREASE POWER, PILOT BROUGHT POWER UP TO 1500 LBS WITH SOME PROBLEMS. PILOT SHUTDOWN AND SECURED NR 2 ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FOD DAMAGE TO FIRST STAGE COMPRESSOR. (M) 2 L 7 2 4T 4 T RT A24CE E4EA 1998070300561 19980703 00561 WP 1998 7 3 AALA981103 1 19980601 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 405A 49316 DTW - DURING MAINTENANCE CHECK, FIRST CLASS CABIN EMERGENCY EXIT FLOOR LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR LIGHT STRIP JUMPER WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300562 19980703 00562 WP 1998 7 3 AALA981091 1 19980531 A 3320 L2042023 LIGHT DOUG DC9 DC982 3022082 WP CABIN SHORTED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 443AA 49469 ORD - FLT 1197 - AFTER TAKEOFF DURING CLIMB, FLIGHT ATTENDANT NOTICED AN ELECTRICAL SMELL IN AFT CABIN. AIRCRAFT AIR IN TERRUPTED AND RETURNED ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND OVERHEAD CONDITIONED AIR SUPPLY DUCTS LEAKING IN AFT CABIN BETWEEN AFT LAVATORIES. REPOSITIONED AND TIGHTENED THREE SUPPLY DUCT CLAMPS. LEAK CHECKED DUCTS UNDER PA CK PRESSURE WITH NO LEAKS DETECTED. REPLACED TWO READING LIGHTS THAT WERE WET AND SHORTING. SYSTEMS GROUND CHECKED NOR MAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300563 19980703 00563 WP 1998 7 3 AALA981031 1 19980526 A 2840 5D00035 BREAKER DOUG DC9 DC982 3022082 WP COCKPIT DEFECTIVE A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 7531A 49923 PHX - FLT 821 - DURING CRUISE, THE FORWARD CENTER TANK BOOST PUMP CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. FLIGHT A IR INTERRUPTED AND LANDED PHX WITHOUT FURTHER INCIDENT. REPLACED FORWARD CENTER TANK BOOST PUMP CIRCUIT BREAKER. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300564 19980703 00564 WP 1998 7 3 AALA980956 1 19980512 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 440AA 49549 ORD - FLT 1576 - AFTER TAKEOFF LAX EN ROUTE TO ORD, NOSE GEAR RED LIGHT ILLUMINATED FOR THREE MINUTES WITH GEAR HANDLE R AISED. GEAR DOOR LIGHT WAS EXTINGUISHED. LANDED ORD WITHOUT INCIDENT. CLEANED 'UP AND LOCKED' PROXIMITY SENSOR AND RE PLACED PROXIMITY SWITCHING UNIT. PERFORMED NOSE GEAR SWING WITH NO FAULTS NOTED. CYCLED GEAR SEVERAL TIMES. SYSTEM GR OUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300565 19980703 00565 WP 1998 7 3 AALA980989 1 19980516 A 4920 5940405503 APU DOUG DC9 DC982 3022082 WP FUSELAGE DEFECTIVE A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 450AA 49476 DFW - FLT 311 - DURING CLIMB-OUT AUS, FLIGHT CREW NOTICED ACRID SMELL IN CABIN WITH SOME SMOKE AND HAZE. FLIGHT CONTINU ED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED AUXILIARY POWER UNIT AND AS A PRECAUTIONARY, REPLACED BOTH COALESCER GA GS. OPERATIONS CHECK NORMAL WITH NO LEAKS NOTED. PACK BURN OUT ACCOMPLISHED WITH NO ODOR NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300566 19980703 00566 WP 1998 7 3 AALA980998 1 19980517 A 3260 INDICATOR DOUG DC9 DC982 3022082 WP COCKPIT MALFUNCTIONED A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 218AA 49168 ORD - FLT 756 - DURING CRUISE, EN ROUTE TUL-ORD RED GEAR UNSAFE LIGHTS ILLUMINATED WITH NO ADVERSE YAW OR EXCESS NOISE. NO ASSOCIATED ORAL WARNING WITH GEAR UNSAFE LIGHTS. LANDED ORD WITHOUT INCIDENT. CYCLED GEAR WITH NO DEFECTS INDICATE D. COULD NOT DUPLICATE. PRECAUTIONARY REPLACED PROXIMITY CONTROL BOX AND TESTED ACCORDING TO MM. NO DEFECTS INDICATED . CYCLED GEAR AGAIN NUMEROUS TIMES COULD NOT DUPLICATE. AIRCRAFT HAS NO HISTORY OR RED GEAR UNSAFE LIGHTS ILLUMINATING . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300567 19980703 00567 WP 1998 7 3 AALA981000 1 19980518 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 485AA 49678 DFW - FLT 1640 - DURING CRUISE, EN ROUTE BUR-DFW, RED NOSE GEAR LIGHT ILLUMINATED. REPLACED NOSE GEAR UP LOCK SENSOR AN D ADJUSTED NOSE GEAR PIN AS REQUIRED. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300568 19980703 00568 WP 1998 7 3 AALA981003 1 19980518 A 3610 FITTING DOUG DC9 DC982 3022082 WP TAIL LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 7544A 53026 DFW - FLT 568 - AFTER TAKEOFF DFW PASSING 9,000 FT TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. RAN ABNORMAL PR OCEDURE CHECKLIST, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT FLICKERED A FEW MINUTES AND THAN EXTINGUISHED. A FEW MINUTES LATER, WHEN POWER INCREASED, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT FLICKERED ON/OFF. RETURNED DFW AND LANDED WITHOUT INCIDENT. TIGHTENED EXTERNAL START AIR FITTING AND RAN ENGINES AND ACCOMPLISHED LEAK CHECK. (M) 2 L 7 2 4F A6WE 1998070300569 19980703 00569 NM 1998 7 3 AALA981013 1 19980521 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 619AA 24577 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY E XIT FLOOR PATH LIGHT WIRE IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998070300570 19980703 00570 NM 1998 7 3 AALA981005 1 19980529 A 3350 CONNECTOR BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 619AA 24577 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LGIHTS IN FIRST CLASS INOPERATIVE. REPAIRED EMERGENCY EXI T FLOOR PATH LIGHT STRIP CONNECTOR AT ROW 10 ON LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998070300571 19980703 00571 NM 1998 7 3 AALA981089 1 19980531 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 378AN 25447 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 41H INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CON NECTOR AT PAX SEAT 41H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998070300572 19980703 00572 WP 1998 7 3 HALA9800138 1 19980531 A 2131 CONTROLLER DOUG DC10 DC1010 3022110 WP CABIN FAILED A HALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 13 116AA 46516 SEA - FLT 21 - AFTER TAKEOFF FROM SEA TO HNL, AIRCRAFT WAS UNABLE TO PRESSURIZE IN ANY MODE. AIRCRAFT RETURNED TO SEA W HERE AN UNEVENTFUL LANDING WAS MADE. REPLACED AUTOPRESSURE CONTROLLER. OPS CHECK AND LEAK CHECK OK. (X) 2 L 7 3 4F A22WE 1998070300573 19980703 00573 WP 1998 7 3 HALA9800136 1 19980527 A 3097 WIRE DOUG DC10 DC1010 3022110 WP NR 1 ENGINE BROKEN A HALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 13 125AA 46525 HNL - FLT 482 - ENGINE NR 1 ANTI-ICE DISAGREE LIGHT ILLUMINATED WITH NR 1 ENGINE ANTI-ICE SWITCH OFF. ACCOMPLISHED ABNO RMAL PROCEDURES SECTION 6-6. REPAIRED BROKEN WIRE ON PIN E OF PLUG. OPS CHECK ON E58 AND OPS CHECK NORMAL ON ENGINE RU N. (M) 2 L 7 3 4F A22WE 1998070300574 19980703 00574 WP 1998 7 3 HALA9800137 1 19980526 A 3610 CONTROLLER DOUG DC10 DC1010 3022110 WP NR 3 FAILED A HALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 WP 13 171AA 46906 FLT 10 - LAX - DURING CRUISE NR 3 MANIFOLD FAIL LIGHT CAME ON TEMP ABOUT 190 DEGRESS PSI AT 10 AFTER SHUT OFF. REPLACED MANIFOLD FAIL DET CONTROLLER, THE PNEU MANIFOLD FAULT INDICATOR, NO FAULT NOTED, OPS CHECKED OK. ON ENG RUN. (M) 2 L 7 3 4F A22WE 1998070300575 19980703 00575 WP 1998 7 3 HALA9800131 1 19980526 A 3610 SEAL DOUG DC9 DC951 3022051 WP AFT FUSELAGE LEAKED A HALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP TO TAKEOFF 1 WP 13 709HA 47764 FLT 114 - HNL - ON FLIGHT FROM HNL TO OGG, THE TAIL COMPARTMENT WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO HNL, WH ERE AN UNEVENTFUL LANDING WAS MADE. REPLACED LT PERI SEAL DUCTS. FOUND BOTH ARM PERI SEALS LEAKING. REPLACED RT AND L T PERI SEALS. GROUND OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998070300576 19980703 00576 WP 1998 7 3 HALA9800139 1 19980531 A 3230 39208025001 ACTUATOR DOUG DC9 DC951 3022051 WP LT MLG BROKEN A HALA K NONE O OTHER DE DESCENT 1 WP 13 673MC DCA969 47726 FLT 552 - HNL - WHEN LANDING GEAR WAS LOWERED THE A/C SHUTTERED AND THE LEFT LANDING GEAR INSTANTLY INDICATED DOWN, WITH A GREEN LIGHT. CHECKED CONDITION AND SECURITY OF LANDING GEAR. FOUND LEFT MAIN GEAR RET CYL BROKEN AND LEFT MAIN BUNG EE CYL BROKEN, REPLACED LEFT MAIN RET AND BUNGEE CYL PER MM 32-32-2 AND 32-32-3. GEAR SWING CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998070300577 19980703 00577 WP 1998 7 3 98ZZZM472 1 19980531 A 3233 39140165505 ACTUATOR DOUG DC9 DC951 3022051 WP LT MLG BROKEN A HALA K NONE O OTHER DE DESCENT 1 WP 13 673MC CAN012 47726 FLT 552 - HNL - WHEN LANDING GEAR WAS LOWERED THE A/C SHUTTERED AND THE LEFT LANDING GEAR INSTANTLY INDICATED DOWN, WITH A GREEN LIGHT. CHECKED CONDITION AND SECURITY OF LANDING GEAR. FOUND LEFT MAIN GEAR RET CYL BROKEN AND LEFT MAIN BUNG EE CYL BROKEN, REPLACED LEFT MAIN RET AND BUNGEE CYL PER MM 32-32-2 AND 32-32-3. GEAR SWING CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998070300578 19980703 00578 NE 1998 7 3 GLBA98085 2 19980525 A 7250 TURBINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A A GLBA D E RETURN TO BLOCK ENGINE SHUTDOWN Y ENGINE STOPPAGE TX TAXI/GRND HDL 1 CE 01 179YV UE179 CREW WAS TAXIING OUT TO THE RUNWAY, HEARD A LOUD BANG AND SHUT DOWN THE ENGINE (LT). FIRST AND SECOND STAGE POWER TURBI NE BLADES APPEAR TO HAVE FAILED. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1998070300579 19980703 00579 CE 1998 7 3 GLBA98074 1 19980503 A 2612 SWITCH BEECH 1900 1900D 1154162 CE RT 'T' HANDLE DIRTY A GLBA E ENGINE SHUTDOWN N FALSE WARNING LD LANDING 1 CE 01 170GL UE170 RIGHT 'T' HANDLE ILLUMINATE RETURNED TO GATE. CLEANED MICROSWITCHES ON 'T' HANDLE AND REPAIRED GROUND WIRE AT LOOP. (M ) 2 L 7 2 4T RT A24CE 1998070300580 19980703 00580 CE 1998 7 3 GLBA98072 1 19980430 A 5270 WARNING LIGHT BEECH 1900 1900C 1154161 CE PAX DOOR ILLUMINATED A GLBA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 01 168GL UC168 PASSENGER DOOR WARNIGN LIGHT CAME ON IN FLIGHT. ON FLIGHT FROM ORD TO APN, EMERGENCY STOP IN MKG. MAINTENANCE ADJUSTED LIMIT SWITCH SCREW ON FORWARD PASSENGER DOOR. PRESSURE CHECKED OK ON GROUND. (M) 2 L 7 2 4T RT A24CE 1998070300581 19980703 00581 SO 1998 7 3 GLBA98076 1 19980508 A 6120 78249035 PCU EMB 120 EMB120ER 3260203 SO RT ENGINE MALFUNCTIONED A GLBA O OTHER E VIBRATION/BUFFET CL CLIMB 1 CE 01 293UX 120293 RIGHT PROPELLER STARTED TO OSCILLATE, 98.3 - 101.2 PERCENT TORQUE FOR APPROXIMATELY 15-20 SEC, THEN SETTLED DOWN. REMOV ED AND REPLACED PROPELLER CONTROL UNIT. (M) 2 L 7 2 4T RT A31SO 1998070300582 19980703 00582 NM 1998 7 3 EISA98118 1 19980524 A 3610 CLAMP BOEING 727 7272A7 138407K NM NR 1 ENGINE LOOSE A EISA K NONE J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 310NE 20241 DURING CLIMB-OUT, ENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST EXTINGUISHED LIGHT. GENERATED FROM PIL OT REPORT. TROUBLESHOT FOUND 8TH STAGE DUCT CLAMP LOOSE, DUCT MISALIGNED, TIGHTENED AND ALIGNED CAMP, RAN ENGINE. NO L EAKS NOTED. (M) 2 L 7 3 4F A3WE 1998070300583 19980703 00583 NM 1998 7 3 EISA98117 1 19980524 A 3610 CLAMP BOEING 727 7272A7 138407K NM NR 1 ENGINE LOOSE A EISA K NONE J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 310NE 20241 DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED. REDUCING THRUST PER ABNORMAL CHECK LIST EXTINGUISHED LIGHT. G ENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED CLAMP ON PNEUMATIC DUCT NR 1 ENGINE. RAN ENGINE, LEAK CHECK GOO D. (M) 2 L 7 3 4F A3WE 1998070300584 19980703 00584 NM 1998 7 3 EISA98116 1 19980524 A 2611 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO COMPT MALFUNCTIONED A EISA K NONE N FALSE WARNING CL CLIMB 1 SW 07 290NE 18972 CARGO SMOKE LIGHT ON IN FLIGHT ILLUMINATED DURNIG CLIMB. WILL NOT TEST IN FLIGHT, EXTINGUISHED DURING DESCENT BELOW 10, 000. GENERATED FROM PILOT REPORT. COULD NOT DUPLICATE MALFUNCTION. CARGO SMOKE DETECTORS. OPS CHECK OK ON GROUND PER AERONAUTICAL MANUAL. (M) 2 L 7 3 4F A3WE 1998070300585 19980703 00585 NM 1998 7 3 98ZZZM473 1 19980519 A 5414 SKIN BOEING 747 747257B 1384853 NM NR 4 PYLON CHAFED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 303TW 20116 DURING C-CHECK INSPECTION DISCOVERED CHAFING DAMAGE ON THE UPPER EDGE OF THE NR 4 PYLON OUTBOARD SKIN. REPAIRED BY TRIM MING OUT THE DAMAGE, FABRICATING AND INSTALLING REPAIR STRAP AND EXTERNAL DOUBLER. REPAIRED IAW EVERGREEN AIR CENTER, E NGINEERING CHANGE/REPAIR AUTHORIZATION NR N303TW-54-003EAC. (M) 2 L 7 4 4F A20WE 1998070300586 19980703 00586 NM 1998 7 3 98ZZZM474 1 19980519 A 5312 BULKHEAD BOEING 747 747257B 1384853 NM BS 1241 CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 303TW 20116 DURING C-CHECK INSPECTION DISCOVERED CORROSION ON THE CANTER BULKHEAD AROUND THE APU FUEL FEED CUTOUT AT BS 1241 BETWEEN BL 0.00 AND 11.33. REPAIRED BY TRIMMING OUT THE SLOPING CANTER PRESSURE DECK WEB BETWEEN BL 0.0 AND RBL 15, FABRICATIN G AND INSTALLING A REPAIR WEB SECTION SPLICED IN PLACE WITH DOUBLERS AND FILLERS. REPAIRED IAW EVERGREEN AIR CENTER, EN GINEERING CHANGE/REPAIR AUTHORIZATION NR N303TW-53-009-EAC. (M) 2 L 7 4 4F A20WE 1998070300587 19980703 00587 NM 1998 7 3 98ZZZM475 1 19980519 A 5414 SKIN BOEING 747 747257B 1384853 NM NR 1 PYLON CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 303TW 20116 DURING C-CHECK INSPECTION DISCOVERED A SKIN DENT AND CRACK IN THE NR 1 PYLON OUTBOARD SKIN AT NACELLE STATION 188, WL 14 8.5. REPAIRED BY BLENDING OUT THE DAMAGED OUTER SKIN, REMOVING THE EXISTING EXTERNAL CUTOUT CORNER DOUBLER, FABRICATING AND INSTALLING A REPAIR FILLER. REPAIRED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N303TW-5 4-004-EAC. (M) 2 L 7 4 4F A20WE 1998070300588 19980703 00588 NM 1998 7 3 98ZZZM476 1 19980519 A 5312 BULKHEAD BOEING 747 747257B 1384853 NM BS 1241 CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 303TW 20116 DURING C-CHECK INSPECTION DISCOVERED CORROSION ON THE CANTER BULKHEAD AROUND THE APU FUEL FEED CUTOUT AT BS 1241 BETWEEN BL 0.0 AND 11.33. REPAIRED BY TRIMMING OUT THE SLOPING CANTER PRESSURE DECK WEB BETWEEN BL 0.0 AND RBL 15, FABRICATING AND INSTALLING A REPAIR WEB SECTION SPLICED IN PLACE WITH DOUBLERS AND FILLERS. REPAIRED IAW EVERGREEN AIR CENTER, ENG INEERING CHANGE/REPAIR AUTHORIZATION NR N303TW-53-009-EAC. (M) 2 L 7 4 4F A20WE 1998070300589 19980703 00589 NM 1998 7 3 98ZZZM477 1 19980519 A 5313 STRINGER BOEING 747 747257B 1384853 NM BS 1335-1350 CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 303TW 20116 DURING C-CHECK INSPECTION, DISCOVERED A CRACK IN STRINGER 5R BETWEEN BS 1335 AND 1350.31, RBL 40. REPAIRED BY TRIMMING OUT THE DAMAGED SECTION OF STRINGER, FABRICATING AND INSTALLING A REPLACEMENT SECTION OF STRINGER WITH THREE REPAIR SPLI CE STRAPS. REPAIRED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N303TW-53-013-EAC. 2 L 7 4 4F A20WE 1998070300590 19980703 00590 NM 1998 7 3 98ZZZM478 1 19980519 A 5414 SKIN BOEING 747 747257B 1384853 NM NR 1 PYLON CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 303TW 20116 DURING C-CHECK INSPECTION DISCOVERED CRACKS ON THE INBOARD SIDE OF THE NR 1 PYLON SKIN AT THE SLOT SEAL POSITION, NACELL E STATION 180, WL 152. REPAIRED BY TRIMMING OUT THE CRACK IN THE SKIN, HFEC INSPECTING, FABRICATING AND INSTALLING REPA IR FILLER AND DOUBLER. REPAIRED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N303TW-54-015-EAC. 2 L 7 4 4F A20WE 1998070300591 19980703 00591 NM 1998 7 3 98ZZZM479 1 19980519 A 5711 SPAR WEB BOEING 747 747257B 1384853 NM WS 1241 CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 303TW 20116 DURING C-CHECK INSPECTION DISCOVERED CORROSION ON THE CENTER TANK REAR SPAR WEB AT STATION 1241, BL 0.0. REPAIRED BY CU TTING OUT A SECTION OF PRESSURE WEB ANGLE BETWEEN LBL 5 AND RBL 15, BLENDING OUT CORROSION COMMON TO THE REAR SPAR WEB, HFEC INSPECTING AREA AND HOLES, FINISHING AND FLAP PEENING REAR SPAR WEB, FABRICATING AND INSTALLING REPAIR PRESSURE WEB ANGLE. REPAIRED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N303TW-53-016-EAC. 2 L 7 4 4F A20WE 1998070300592 19980703 00592 SO 1998 7 3 C2XA98IA182 1 19980513 A 3350 30043221 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16710 120106 IAH - DURING PREFLIGHT INSPECTION, THE LEFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE EMERGENCY LIGHT ASSEMBLY IAW EMB-120 MM 33-50-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1998070300593 19980703 00593 CE 1998 7 3 C2XA98IA183 1 19980519 A 6120 MS250851 SWITCH BEECH 1900 1900D 1154162 CE NR 2 ENGINE INOPERATIVE A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 69548 UE193 LCH - FLT 3818 - THE PILOT REPORTED THE NR 2 ENGINE CYCLED IN AND OUT OF FEATHER SEVERAL TIMES ON APPROACH UNTIL THE AUT OFEATHER SYSTEM WAS TURNED OFF. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT POWER L EVEL SWITCH (NR 1) AND ADJUSTED ALL REMAINING SWITCHES IAW BEECH MM 61-21-00. THE AIRCRAFT WAS TEST FLOWN SATISFACTORIL Y, AND WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998070300594 19980703 00594 EU 1998 7 3 C2XA98BT036 1 19980526 A 3350 LIGHTS AEROSP ATR42 ATR42320 8680930 EU CABIN MALFUNCTIONED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15823 165 EWR - CREW REPORTED, 'EMERGENCY LIGHTS NOT WORKING'. MAINTENANCE CYCLED THE CIRCUIT BREAKER FOR THE EMERGENCY LIGHTS AN D OPERATIONALLY CHECKED LIGHTS GOOD. (M) 2 H 7 2 4T RT A53EU 1998070300595 19980703 00595 EU 1998 7 3 C2XA98BT035 1 19980525 A 3350 301180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 DURING 1A INSPECTION IN BTV MAINTENANCE, FOUND EMERGENCY LIGHT EXIT SIGNS FAILED TO LIGHT. REMOVED AND REPLACED POWER S UPPLY AND OPERATIONLLY CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998070300596 19980703 00596 CE 1998 7 3 C2XA98CL039 1 19980526 A 3246 114800121 BEARING BEECH 1900 1900D 1154162 CE NLG FAILED A A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 09 87557 UE246 MBS - FLT 3242 - CREW REPORTED, ABORTED TAKEOFF DUE TO THE NLG WHEEL ASSEMBLY DEPARTING THE AIRCRAFT DURING THE TAKEOFF RUN. MAINTENANCE INSPECTED THE NLG AND WHEEL ASSEMBLY AND FOUND THE WHEEL BEARINGS TO BE FRICTION WELDED TO AXLE CAUSIN G THE DAMAGE. THE NOSE GEAR WHEEL ASSEMBLY WAS REMOVED AND REPLACED IAW B1900 MM 32-40-00. THE LOWER NLG STRUT ASSEMBL Y WAS ALSO REMOVED AND REPALCED IAW B1900D MM 32-20-00, OPERATIONAL AND LEAKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998070300597 19980703 00597 EU 1998 7 3 C2XA98BT037 1 19980530 A 3320 EO33601 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 25811 094 EWR - BURNED WIRE SMELL, REMOVED AND REPLACED LATERAL LIGHT SOCKET ASSY IAW ATR JIC 33-30-00. IN CABIN, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998070300598 19980703 00598 EU 1998 7 3 C2XA98BT038 1 19980531 A 6130 FE1595007 PROP BRAKE AEROSP ATR42 ATR42320 8680930 EU NR 2 ENGINE BURNED A C2XA F ACTIVATE FIRE EXT. A J FLAME/FIRE WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 14821 160 EWR - NR 2 ENGINE PROP BRAKE FIRE DISCHARGED BOTH AGENTS INTO NR 2 ENGINE. PERFORMED DVI OF NR 2 ENGINE IAW ATR MM 05-5 0-00 SECTION X. NO DISCREPANCIES. NO FURTHER DAMAGE. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FIRE BOTTLES. AIRCRAF T RELEASED UNDER MEL DUE TO PROP BRAKE INOP. (M) 2 H 7 2 4T RT A53EU 1998070300599 19980703 00599 EU 1998 7 3 C2XA98BT039 1 19980531 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 BTV - DURING IA INSPECTION, FOUND EMERGENCY AISLE PATH LIGHTS IN CENTER SECTION OF CABIN TO BE INOP. REMOVED AND REPLAC ED EMERGENCY LIGHT BATTERY PACK , IAW ATR42 JIC 33-50-00. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998070300600 19980703 00600 EU 1998 7 3 C2XA98IA190 1 19980527 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT OUTBOARD AFT SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEA T TRACK, IAW ATR SRM 51-70-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300601 19980703 00601 EU 1998 7 3 C2XA98IA189 1 19980527 A 5320 S53671406200 DOUBLER AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 IAH - DURING C-CHECK INSPECTION, FOUND VHF ANTENNA DOUBLER CORRODED. MAINTENANCE REMOVED AND REPLACED THE DOUBLER IAW A TR SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300602 19980703 00602 EU 1998 7 3 C2XA98IA188 1 19980527 A 5315 S53672408202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM 39 CORRODED. MAINTENANCE REMOVED ALL CORROSION AND INSTALLED 4 DOUBLER S, IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-01037. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300603 19980703 00603 EU 1998 7 3 C2XA98IA187 1 19980527 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD AFT SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW ATR SRM 51-70-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300604 19980703 00604 EU 1998 7 3 C2XA98IA186 1 19980527 A 5320 S5367121729402 CREASE BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE CREASE BEAM PLATE CORRODED BETWEEN FRAME SUPPORT AND FRAME 39. MAINTEN ANCE REMOVED AND REPLACED THE CREASE BEAM PLTE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 H 7 2 4T RT A53EU 1998070300605 19980703 00605 EU 1998 7 3 C2XA98IA185 1 19980527 A 5320 S53173206200 ATTACH PLATE AEROSP ATR42 ATR42320 8680930 EU COCKPIT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14834 193 IAH - DURING C-CHECK INSPECTION, FOUND CAPTAINS SIDE SEAT, FLOOR ATTACH PLATE CORRODED. MAINTENANCE REMOVED AND REPLACE D THE ATTACH PLATE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300606 19980703 00606 CE 1998 7 3 C2XA98CL042 1 19980531 A 2913 11438800013 POWER PACK BEECH 1900 1900D 1154162 CE LT MLG FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 47542 5092 MX559733 UE198 CLE - FLT 3280 - CREW REPORTED THAT AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD WITHOT U FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE HYDRAULIC POWER PACK IAW B1900D MM 32-30-02. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998070300607 19980703 00607 EU 1998 7 3 C2XA98IA195 1 19980602 A 5230 S52376108202 BRACKET AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING C-CHECK INSPECTION, FOUND A CRACK IN THE CARGO DOOR FORWARD HINGE BRACKET. MAINTENANCE REMOVED AND REPLACE D THE BRACKET IAW ATR SRM 51-25-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIEC. (M) 2 H 7 2 4T RT A53EU 1998070300608 19980703 00608 EU 1998 7 3 C2XA98IA194 1 19980602 A 5240 S5247765600400 PIN AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CHIPPED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING C-CHECK INSPECTION, FOUND SERVICE DOOR LOWER FORWARD SHOOT BOLT PLATING CHIPPED. MAINTENANCE REMOVED AND R EPLACED PIN ASSY. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300609 19980703 00609 EU 1998 7 3 C2XA98IA193 1 19980602 A 5240 S536713902801 SEAL RETAINER AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING C-CHECK INSPECTION, FOUND SERVICE DOOR CUTOUT LOWER FORWARD SEAL RETAINER CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER FORWARD SEAL RETAINER IAW ATR SRM 51-25-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300610 19980703 00610 EU 1998 7 3 C2XA98IA192 1 19980602 A 5311 S53372411210 FRAME AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 13 RIGHT SIDE IS CORRODED AT WALL SUPPORT ANGLE. MAINTENANCE REMOVED ALL C ORROSION AND INSTALLED REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-01037. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300611 19980703 00611 EU 1998 7 3 C2XA98IA191 1 19980602 A 5230 S523765192202 HINGE AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING C-CHECK INSPECTION, FOUND FORWARD LUG CRACKED ON CARGO DOOR HINGE. MAINTENANCE REMOVED AND REPLACED FORWAR D HINGE ON CARGO DOOR IAW ATR SRM 51-25-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998070300612 19980703 00612 WP 1998 7 3 ARWA980507 1 19980520 A 7830 TR COWL LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE DENTED A ARWA O OTHER C F.O.D. IN INSP/MAINT 1 SO 19 306GB 193U1138 MIA - NR 2 ENGINE T/R COWL DENTED LOWER SIDE 6 O'CLOCK POSITION. FABRICATED WEB DOUBLER INSTALLED NEW SKID AND SPLICED IAW SRM 51-21-02, 51-50-02, 51-50-01 AND E0980306-0062. (M) 2 L 7 3 4F A23WE 1998070300613 19980703 00613 WP 1998 7 3 ARWA980506 1 19980519 A 3231 MECHANISM DOUG DC8 DC862 3021970 WP NLG DOOR OUT OF ADJUST A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 1804 45896 IN FLT RETURN DUE TO LOUD RATTLING NOISE FROM NOSE WHEEL WELL AREA. UNABLE TO PRESSURIZE AIRCRAFT AUTO OR MANUALLY. AD JUSTED NOSE GEAR DOOR PER MM 32-10-0. RUN UP ENGINES PRESSURIZED OK IN MANUAL, AUTO INOP OPEN DMI ON AUTO PRESS. (M) 2 L 7 4 4F 4A25 1998070300614 19980703 00614 NM 1998 7 3 AALA984117 1 19980519 A 5347 SEAT TRACK BOEING 767 767323 1385205 NM BS 343 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 372AA 25199 AFW - CORROSION REMOVED FROM UPPER SURFACE OF SEAT TRACK. BLENDED OUT EXCEEDED SRM MAX ALLOWABLE LIMITS. BLENDED OUT C ORROSION AND REMOVED TABS ADJACENT TO THE DAMAGED AREA ALODINED AND PRIMED. APPROCHED BY ENGINEER WITH NOTED CONDITION PER MRB 767-1632. (M) 2 L 7 2 4F RT A1NM 1998070300615 19980703 00615 NM 1998 7 3 AALA984123 1 19980521 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 372AA 25199 AFW - FLOORBEAM HAS CORROSION BEYOND SRM LIMITS. BLENDED AREA FLAT SO THE FASTENER WILL SEAT PROPERLY WHEN REINSTALLED AND REFINISHED AREA PER THE REF/D1 SRM SECTION. (M) 2 L 7 2 4F RT A1NM 1998070300616 19980703 00616 EU 1998 7 3 AALA980873 1 19980501 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - FOUND FLOOR/FRAME UNDER ROLLER TRAY NR 3 HAS CORROSION. REMOVED CORRODED SECTION AND INSTALLED NEW SECTIN WITH SP LICES PER SRM 53-10-15-2. (M) 2 L 7 2 4F RT A35EU 1998070300617 19980703 00617 EU 1998 7 3 AALA980965 1 19980512 A 5230 LATCH AIRBUS 300 A300B4605R 3930308 EU CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 41063 506 TUL - NR 7 DOOR LATCH FITTING HAS CORROSION AROUND BOTH FITTINGS. REPLACED DOOR FRAME FITTING PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998070300618 19980703 00618 NM 1998 7 3 AALA984108 1 19980508 A 5313 STRINGER BOEING 767 767223 1385123 NM BS 1314-1299 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - STRINGER SPLICE AND STRINGER HAD CORROSION. FABRICATE A REPLACEMENT STRINGER SPLICE FROM .071 THICK 7075-T6. (M) 2 L 7 2 4F RT A1NM 1998070300619 19980703 00619 NM 1998 7 3 AALA984109 1 19980508 A 5311 FRAME BOEING 767 767223 1385123 NM BS 1346 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - FAIL/SAFE CHORD HAS CORROSION. FABRICATE A REPAIR ANGLE FROM 7075T6 USING BAC1503400141 THE CORNER OF THE ANGLE S HOULD BE CHAMFERED TO ALOOW PROPER NESTING IN THE EXISTING CHORD. (M) 2 L 7 2 4F RT A1NM 1998070300620 19980703 00620 NM 1998 7 3 AALA984110 1 19980508 A 5311 FRAME BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - WHILE IN FOR MBV, MAINTENANCE FOUND AN AREA OF CORROSION ON THE FWD FACE OF THE VERTICAL FLANGE OF THE INNER CHORD ABOVE STRINGER 33R. ENSURE BLENDOUT IS FLAT IN AREA OF THE FASTENER. REFINISH THE BLENDED AREA PER REF SRM. (M) 2 L 7 2 4F RT A1NM 1998070300621 19980703 00621 NM 1998 7 3 AALA984111 1 19980511 A 5314 KEEL BEAM BOEING 767 767223 1385123 NM BS 800 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - LEFT KEEL BEAM OUTER FLANGE HAD SEVERE CORROSION. CUT OUT CORRODED AREA. FABRICATED A FILLER PIECE FROM 7075-T6 AND A STIFFENING ANGLE FROM 7075-T6 AND INSTALLED PER SRM. (M) 2 L 7 2 4F RT A1NM 1998070300622 19980703 00622 NM 1998 7 3 AALA984112 1 19980511 A 5311 FRAME BOEING 767 767223 1385123 NM BS 1175 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - FUSELAGE FRAME AT CAP UPPER SURFACE HAS CORROSION. BLENDED AND REFINISHED PER SRM 53-00-07 FIGURE 101. (M) 2 L 7 2 4F RT A1NM 1998070300623 19980703 00623 NM 1998 7 3 AALA984113 1 19980508 A 5330 SKIN BOEING 767 767223 1385123 NM BS 587.5 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - AREA OF CORROSION IN FORWARD CARGO AT ALTIMETER ANTENNA AT STATION 587.5, JUST LEFT OF BL 0. ENSURE THE BLENDOUT IS FLAT IN AREA OF NUTPLATE FOR PROPER RESEATING WHEN REINSTALLED, REFINISH THE BLENDED OUT AREA PER REF SRM. (M) 2 L 7 2 4F RT A1NM 1998070300624 19980703 00624 NM 1998 7 3 AALA984114 1 19980508 A 5400 FIRE SEAL BOEING 767 767223 1385123 NM LT PYLON WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - FOUND WEAR ON INBOARD AND OUTBOARD OF LEFT PYLON FIRE SEAL AND 2 GAUGES ON PYLON AFT OF PNL 416BR. BLENDED DAMAGE D AREA PER SRM, VERIFIED NO CRACKS AND REFINISH PER SRM. (M) 2 L 7 2 4F RT A1NM 1998070300625 19980703 00625 NM 1998 7 3 AALA980871 1 19980430 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND STRINGER 15 LEFT CRACKED AT END FORWARD OF LEFT ICE LIGHT ASSY STATION 720B PLUS 3 INCHES. REPAIRED PER SRM 53-10-3 PAGE 12. (M) 2 L 7 3 4F A3WE 1998070300626 19980703 00626 NM 1998 7 3 AALA980870 1 19980430 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELL FRAME DENTED AT FS 950B BETWEEN STRINGER 23L AND 24L. INSTALLED DOUBLER REPAIR ON BELL FRAME AT FS 950B BETW EEN STRINGER 23L AND 24L PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998070300627 19980703 00627 NM 1998 7 3 AALA980869 1 19980430 A 5720 STIFFENER BOEING 727 727227 1384078 NM BS 686 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND UPPER SPAR STIFFENER NR 10 CRACKED AT WS 686.5. REPAIRED CRACK IAW SERVICE BULLETIN 727-57-A159 FIG 12 AND 18. (M) 2 L 7 3 4F A3WE 1998070300628 19980703 00628 NM 1998 7 3 AALA980868 1 19980430 A 5320 CLIP BOEING 727 727227 1384078 NM BS 567 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND STRINGER CLIP CORRODED AT STUB FRAME STATION 567 AT STRINGER 27R. INSTALLED NEW STRIGNER CLIP PER SRM 51-10 -1. (M) 2 L 7 3 4F A3WE 1998070300629 19980703 00629 NM 1998 7 3 AALA981049 1 19980526 A 5730 SKIN BOEING 727 727227 1384078 NM BS 805-810 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORROSION ON WING CENTER SECTION LOWER SKIN ABOVE LEFT PRIMARY HEAT EXCHANGER. INSTALLED STRAP REPAIR PER E SO 11697 AFTER CORROSION REMOVAL, TREAT AND PRIME. (M) 2 L 7 3 4F A3WE 1998070300630 19980703 00630 NM 1998 7 3 AALA981048 1 19980526 A 5532 SKIN BOEING 727 727227 1384078 NM VERT STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - AN .25 INCH CRACK FROM SCREW HOLE IN VERT STAB SKIN AT BODY STATION 1213 LEFT SIDE. INSTALLED DOUBLER PER B 727 A ARD/DC PAGE 55-30-03-1. (M) 2 L 7 3 4F A3WE 1998070300631 19980703 00631 NM 1998 7 3 AALA981047 1 19980526 A 5320 FITTING BOEING 727 727227 1384078 NM BS 720/770 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORROSION ON STRINGER 28R END FITTING AT STATION 720 PLUS 720 PLUS 10. INSTALLED REPAIR ANGLES AND REMOVED CORROSION, TREATED AND PRIMED IAW ESO 11697, DATED 5-4-98. (M) 2 L 7 3 4F A3WE 1998070300632 19980703 00632 NM 1998 7 3 AALA981046 1 19980526 A 5330 SKIN BOEING 727 727227 1384078 NM BS 520-532 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORROSION ON SKIN BETWEEN STRINGER 27L FROM STATION 520-532. CUT OUT CORROSION AREA INSTALLED DOUBLER PER S RM 53-30-3 FIG 14. (M) 2 L 7 3 4F A3WE 1998070300633 19980703 00633 NM 1998 7 3 AALA981045 1 19980526 A 5313 STRINGERS BOEING 727 727227 1384078 NM BS 680-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND STRINGER 28R CORRODED FROM STATION 680-720. REMOVED AND REPLACED STRINGER 28R PER SRM 51-10-3 PAGE 4B FIG 1 . (M) 2 L 7 3 4F A3WE 1998070300634 19980703 00634 NM 1998 7 3 AALA981044 1 19980526 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 680-720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORRSION ON STRINGER 27R STATION 680 TO 720 TO 10 CORROSION ON STRINGER 28L STATION 680 TO 720. REMOVED STR INGER SECTIONS AND INSTALLED NEW STRINGER. CORROSION PER SRM 51-10-6 PAGE 27-29, STRINGER PER SRM 53-10-3 PAGE 4B FIG 1 . (M) 2 L 7 3 4F A3WE 1998070300635 19980703 00635 NM 1998 7 3 AALA981043 1 19980526 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 342 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND SMALL CRACKS IN STRINGER 5R FROM FASTENER HOLES STRINGER 342, TWO CRACKS INBOARD AND OUTBOARD SIDES OF STRIN GER 1. INSTALLED DOUBLERS AT STATION 342 PER SRM 53-10-3 PAGE 40. (M) 2 L 7 3 4F A3WE 1998070300636 19980703 00636 NM 1998 7 3 AALA981042 1 19980526 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 520 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORROSION IN STRINGER 27L FWD OF STATION 520. REMOVED AND INSTALLED NEW SECTION OF STRINGER PER SRM 53-10-3 PAGE 4B FIG 1. (M) 2 L 7 3 4F A3WE 1998070300637 19980703 00637 NM 1998 7 3 AALA981041 1 19980526 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 1263 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - VERTICAL WEB SHEAR TIE IS CRACKED AT STATION 1263 BETWEEN STRINGER 11 AND 12R AT OUTBOARD WALL. REMOVED ANGLE AND INSTALLED NEW ANGLE PER SRM 53-10-4 PAGE 50. (M) 2 L 7 3 4F A3WE 1998070300638 19980703 00638 NM 1998 7 3 AALA981040 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELLFRAME TOP FLANGE BENT STATION 500, STRINGER 23L-25L. INSTALLED REPAIR TO BELLFRAME PER SRM 51-40-3 FIG 1. (M ) 2 L 7 3 4F A3WE 1998070300639 19980703 00639 NM 1998 7 3 AALA981039 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 540 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELLFRAME TOP FLANGE BENT AT STATION 540, STRINGER 23L FACE OF WEB DEFORMED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300640 19980703 00640 NM 1998 7 3 AALA981038 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 580 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELLFRAME TOP FLANGE BENT STATION 580, STRINGER 24L. REPAIRED ACCORDING TO SRM 53-10-4 FIG 1 WITH DOUBLER. (M) 2 L 7 3 4F A3WE 1998070300641 19980703 00641 NM 1998 7 3 AALA981037 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 520 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELLFRAME TOP FLANGE BENT STATION 520, STRINGER 24R THROUGH 25R. INSTALLED FRAME REPAIR AT STATION 520, STRINGER 24R-25R SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300642 19980703 00642 NM 1998 7 3 AALA981036 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELLFRAME TOP FLANGE BENT STATION 500, STRINGER 24R-25R. CUT OUT DAMAGED TOP BELLFRAME FLANGE AT STATION 500 FROM STRINGER 24R-25R. INSTALLED REPAIR PER SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300643 19980703 00643 NM 1998 7 3 AALA981035 1 19980526 A 5320 SPLICE BOEING 727 727227 1384078 NM BS 1007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORROSION ON STRINGER SPLICE, 30 LEFT AT STATION 1007. REMOVED CORRODED SPLICE AND CLEANED AREA, INSTALLED NEW SPLICES PER 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1998070300644 19980703 00644 NM 1998 7 3 AALA981034 1 19980526 A 5320 CLIP BOEING 727 727227 1384078 NM BS 567 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORROSION ON STRINGER CLIP STATION 567, STRINGER 27R. REMOVED AND REPLACED STATION 27R CLIP AT STATION 567 SRM 51-10-2 PAGE 6 FIG 6A-B. (M) 2 L 7 3 4F A3WE 1998070300645 19980703 00645 NM 1998 7 3 AALA981033 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 375 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - FOUND CORROSION ON FRAME AT STATION 375 JUST ABOVE FLOOR LINE, STRINGER 17R. BLENDED OUT CORROSION PER SRM 51-10- 6 AND INSTALLED A DOUBLER IAW SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998070300646 19980703 00646 NM 1998 7 3 AALA981032 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 560 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELLFRAME DENTED TOP FLANGE STATION 560 STRINGER 24L. INSTALLED BELLFRAME REPAIR IAW SRM 51-40-3 PAGE 2. (M) 2 L 7 3 4F A3WE 1998070300647 19980703 00647 NM 1998 7 3 AALA981077 1 19980526 A 5311 FRAME BOEING 727 727227 1384078 NM BS 520 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 TUL - BELLFRAME TOP FLANGE BENT STATION 520 AT STRINGER 23L. INSTALLED REPAIR TO BELLFRAME PER SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300648 19980703 00648 NM 1998 7 3 AALA980867 1 19980430 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FLOORBEAM UPPER CAP CORRODED STATION 380, RBL 12 TO RBL 62. FLOORBEAM REPAIR INSTALLED STATION 380 RBL 12 TO RBL 62 AS PER SRM 53-10-8, REF NR 0129529. (M) 2 L 7 3 4F A3WE 1998070300649 19980703 00649 NM 1998 7 3 AALA980866 1 19980430 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FUSELAGE BELLFRAME BENT AT FS 500 BETWEEN STRINGER 24R AND 25R. INSTALLED DOUBLER REPAIR PER SRM 53-10-4 PAGE 6 D ETAIL 3. (M) 2 L 7 3 4F A3WE 1998070300650 19980703 00650 NM 1998 7 3 AALA980865 1 19980430 A 5311 FRAME BOEING 727 727227 1384078 NM BS 720 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - BELLFRAME BENT AT STRINGER 24 LEFT STATION 720A. INSTALLED DOUBLER PER SRM 53-10-4 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300651 19980703 00651 NM 1998 7 3 AALA980816 1 19980421 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 300 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION ON RT SIDE OF DOGHOUSE BET WALKING PANEL AND MIDDLE CHORD ANGLE STATION 300 AT RBL 15. REMOVED CO RROSION, INSTALLED REPAIR STRAP PER ESO 11697, DATED 16 APR 98. (M) 2 L 7 3 4F A3WE 1998070300652 19980703 00652 NM 1998 7 3 AALA980815 1 19980422 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 344 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - UPPER AFT FLANGE OF FLOORBEAM CRACKED STATION 344 LBL 28. STOP DRILLED CRACK INSTALLED REPAIR PER SRM 53-10-8 FIG 9 AT STATION 344 LBL 28 FLOORBEAM. (M) 2 L 7 3 4F A3WE 1998070300653 19980703 00653 NM 1998 7 3 AALA980983 1 19980514 A 5320 WINDOW FRAME BOEING 727 727227 1384078 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION AT WINDOW CUTOUT STRUCTURE RT STATION 950A TO 950B. INSTALLED DOUBLER ALL FASTENERS, AND SEALED P ER SRM 56-20-3, APPLIED SM5-5-28 TYPE 3 TO AREA OF CORROSION PER SRM 56-20-3. (M) 2 L 7 3 4F A3WE 1998070300654 19980703 00654 NM 1998 7 3 AALA980982 1 19980514 A 5320 WINDOW FRAME BOEING 727 727227 1384078 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION AT WINDOW CUTOUT STRUCTURE RT STATION 950C TO 950D. FABRICATED DOUBLER, INSTALLED, SEALED DOUBLER . INSTALLED FASTENERS, AERODYNAMICALLY SEALED AROUND DOUBLER, APPLIED BMS 5-28 TYPE 3 TO AREA OF CORROSION REMOVAL PER SRM 56-20-3. (M) 2 L 7 3 4F A3WE 1998070300655 19980703 00655 NM 1998 7 3 AALA980981 1 19980514 A 5320 WINDOW FRAME BOEING 727 727227 1384078 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 FOUND CORROSION AT WINDOW CUTOUT STRUCTURE RT STATION 950E TO 950F. INSTALLED DOUBLER ALL FASTENERS AND SEALED PER SRM 56-20-3. APPLIED BMS 5-28 TYPE 3 TO AREA OF CORROSION PER SRM 58-20-3. (M) 2 L 7 3 4F A3WE 1998070300656 19980703 00656 NM 1998 7 3 AALA980980 1 19980514 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FLOORBEAM UPPER CAP CORRODED STATION 380 RBL 12 TO RBL 62. CORROSION BLENDED OUT AND FLOORBEAM REPAIR INSTALLED P ER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998070300657 19980703 00657 NM 1998 7 3 AALA980979 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1010 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - STATION 1010 LEFT BELTFRAME DENTED ABOVE STRINGER 24. REPAIRED BELTFRAME DAMAGE WITH DOUBLER AS OUTLINED IN SRM 5 3-10-4 PAGE 3A-6. (M) 2 L 7 3 4F A3WE 1998070300658 19980703 00658 NM 1998 7 3 AALA980978 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - DENT IN FUSELAGE BELLFRAME AT FS 950F AND STRINGER 256. INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998070300659 19980703 00659 NM 1998 7 3 AALA980977 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FRAME DENT IN 14 INCH AREA STRINGER 24L TO 23L AT STATION 500 EXTENDING INTO WEB. REMOVED DAMAGE AND INSTALLED DO UBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998070300660 19980703 00660 NM 1998 7 3 AALA980976 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - BELLFRAME DENTED STATION 700 BETWEEN STRINGER 24R AND 23R. CUTOUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER E SO 11697 DATED 5-1-98. (M) 2 L 7 3 4F A3WE 1998070300661 19980703 00661 NM 1998 7 3 AALA980975 1 19980514 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 296 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND CORROSION ON LEFT SIDE OF DOGHOUSE BET WALKWAY PANEL AND MIDDLE CHORD ANGLE STATION 296 LBL 15. REMOVED COR ROSION CUT OUT DAMAGED AREA FABRICATED A FILLER AND STEEL STRAP. INSTALLED FILLER, STRAP AND FLOOR WORK ACCOMPLISHED IA W ESO 11697, DATED 4/16/98. (M) 2 L 7 3 4F A3WE 1998070300662 19980703 00662 NM 1998 7 3 AALA980974 1 19980514 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND STRINGER 15R CRACKED AFT SIDE AT RT ICE LIGHT STATION 720B. REPAIRED STRINGER 15R, AFT SIDE OF RT ICE LIGHT , STATION 720B IAW SRM 53-10-3 PAGE 3-48. (M) 2 L 7 3 4F A3WE 1998070300663 19980703 00663 NM 1998 7 3 AALA980973 1 19980514 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FOUND STRINGER 15R CRACKED FORWARD SIDE OF RT ICE LIGHT STATION 720B. CUT OUT DAMAGE STRINGER FABRICATED NEW STRI NGER DRILLED, ALODINED, PRIMED AND INSTALLED NEW STRINGER PER SRM 53-10-3 DETAIL 3. (M) 2 L 7 3 4F A3WE 1998070300664 19980703 00664 NM 1998 7 3 AALA980972 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - BELLFRAME DENTED AT STATION 700 STRINGER 23L EXTENDS INTO WEB AREA. REPAIRED BELLFRAME PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998070300665 19980703 00665 NM 1998 7 3 AALA980971 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - BELLFRAME DENTED AT STATION 680 STRINGER 25L EXTENDS INTO WEB. REPAIRED BELLFRAME PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998070300666 19980703 00666 NM 1998 7 3 AALA980970 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - BELLFRAME STATION 930 BETWEEN STRINGER 13L AND STRINGER 14L IS CRACKED. REMOVED FASTENERS, CUT OUT DAMAGED BELLFR AME DRILLED NEW PARTS, TREATED, PRIMED INSTALLED FASTENERS PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998070300667 19980703 00667 NM 1998 7 3 AALA980969 1 19980514 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 440 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - STATION RBL 24, AFT FLANGE LOWER SIDE DEEPLY GOUGED NDT NO CRACK RBL 6. AFT FLANGE IMPROPER REPAIR RBL 12. AFT F LANGE LOWER SIDE UPPER CAP CORRODED AROUND FASTENER HOLE. EACH ITEM WAS INCORPORATED INTO ONE REPAIR. FLOORBEAM UPPER CAP REPAIR PER SRM 53-10-08 FIGURE 9A AND 9B. (M) 2 L 7 3 4F A3WE 1998070300668 19980703 00668 NM 1998 7 3 AALA980968 1 19980514 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - FUSELAGE SKIN CORRODED AT PRODUCTION BREAK STATION 1007 BELOW STRINGER 14L. CUTOUT CORRODED AREA AND FABRICATED F ILLER, DOUBLER AND TRIPLER DRILLED HOLES AND COUNTER SUNK. APPLIED ALODINED, PRIMED, SEALED INSTALLED FASTENERS SEALED EDGES PER SRM 53-30-3 FIG 3A AND FIG 5. (M) 2 L 7 3 4F A3WE 1998070300669 19980703 00669 NM 1998 7 3 AALA980967 1 19980514 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1040 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - SKIN BULGING AND SPLITTING JUST BELOW STRINGER 10L SKIN LAP. INSTALLED NEW TAPERED SIGN STATION 1040 AT UPPER HIN GE IN ACCORDANCE WITH SRM 51-10-1 PAGE 103-104 AND RE-INSTALLED SEAL LANDING. (M) 2 L 7 3 4F A3WE 1998070300670 19980703 00670 NM 1998 7 3 AALA980966 1 19980514 A 5320 WEB BOEING 727 727227 1384078 NM BS 1148-1170 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 723AA 20731 TUL - TOP OF FLOOR WEB CORRODED INBOARD OF LAV HAT CHANNEL LBL 20, STATION 1148 AND STATION 1170. FABRICATED DOUBLER AN D FILLER FOR STATION 170 BL 20 PER SRM 51-40-2 ALODINE AND PRIMED AND INSTALLED. (M) 2 L 7 3 4F A3WE 1998070300671 19980703 00671 EU 1998 7 3 AALA980940 1 19980510 A 5297 WIRE FOKKER F28 F28MK0100 4990807 EU EMERG EXIT DOOR BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1436A 11426 ORD - DURING OVERNIGHT CHECK, LEFT EMERGENCY EXIT DOOR COVER MISSING BREAK AWAY SAFETY WIRE. INSTALLED SAFETY WIRE. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998070300672 19980703 00672 EU 1998 7 3 AALA980942 1 19980509 A 2913 UP60324 O-RING FOKKER F28 F28MK0100 4990807 EU HYDRAULIC PUMP LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 1448A 11457 ATL - FLT 1825 - DURING APPROACH WHEN SPEED BRAKE EXTENDED NR 1 HYDRAULIC QTY LOW ILLUMINATED. AIRCRAFT EXPERIENCED SYS TEM 1 HYDRAULIC FAILURE. CREW DECLARED EMERGENCY AND LANDED ATL WITHOUT INCIDENT. REPLACED O-RING ON FITTING AT NR 1 H YDRAULIC SYSTEM PUMP ON NR 2 ENGINE. ACCOMPLISHED ENGINE LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998070300673 19980703 00673 1998 7 3 AALA981010 4 19980518 A 2565 D31873101 SLIDE FOKKER F28 F28MK0100 4990807 EU SVC DOOR DEPLOYED A AALA O OTHER O OTHER IN INSP/MAINT 1 SW 07 1431B 11416 IAH - WHILE AT THE GATE, THE FORWARD SERVICE DOOR EMERGENCY SLIDE WAS INADVERTENTLY ACTIVATED AND FAILED TO FULLY DEPLOY . REPLACED FORWARD SERVICE DOOR EMERGENCY SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998070300674 19980703 00674 WP 1998 7 3 AALA981004 1 19980520 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 560AA 53090 DFW - DURING OVERNIGHT CHECK, MID CABIN FORWARD EMERGENCY EXIT FLOOR PATH LIGHTS AT EXIT STICKERS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT MID CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300675 19980703 00675 WP 1998 7 3 AALA981092 1 19980531 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 236AA 49251 DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED EMERGENCY FLOOD LIGH T ASSEMBLY IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300676 19980703 00676 WP 1998 7 3 AALA981086 1 19980530 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 593AA 53256 LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACK LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR TRACK LIGHT CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998070300677 19980703 00677 WP 1998 7 3 AALA981084 1 19980529 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, AFT CABIN EMERGENCY LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR AT AFT GALLEY DOOR FL OOR EXIT SIGN. REPAIRED CONNECTOR AT AFT GALLEY DOOR FLOOR EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300678 19980703 00678 WP 1998 7 3 AALA981083 1 19980529 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 DFW - DURING OVERNIGHT MAINTENANCE, BOTH STAIRWAY EMERGENCY SIDE WALL LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT FEED ER WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300679 19980703 00679 WP 1998 7 3 AALA981104 1 19980531 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 422AA 49334 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS CABIN EMERGENCY EXIT FLOOR LIGHTING INOPERATIVE ALONG FORWARD GALLEY. R EPLACED EMERGENCY EXIT FLOOR LGHT STRIP JUMPER WIRE AT FWD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998070300680 19980703 00680 NM 1998 7 3 AALA981050 1 19980526 A 5311 FRAME BOEING 727 727223 1384074 NM BS 351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - STATION 351 BETWEEN STRINGER 28 LT AND 28 RT CORROSION ON BELTFRAME. INSTALLED NEW BELTFRAME STATION 351 PER SRM 51-10-1 AT STRINGER 26L TO 26R. (M) 2 L 7 3 4F A3WE 1998070300681 19980703 00681 NM 1998 7 3 AALA981051 1 19980526 A 5320 FLOOR PAN BOEING 727 727223 1384074 NM BS 1159-1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON LAV FLOOR STATION 1159 TO STATION 1174 RBL 25 THROUGH RBL 45 9 PLACES. REMOVED CORROSION, REPA IRED PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998070300682 19980703 00682 NM 1998 7 3 AALA981052 1 19980527 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 640 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON AFT SIDE OF SHEAR TIE STATION 640 OUTBOARD STRINGER 27RT. REMOVED AND REPLACED SHEAR TIE. (M) 2 L 7 3 4F A3WE 1998070300683 19980703 00683 NM 1998 7 3 AALA981053 1 19980526 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON FORWARD SIDE OF BELLFRAME STATION 720D BETWEEN STRINGER 28 LT AND 28 RT. FRAME REPAIRED PER SR M 53-10-4 FIG 12. (M) 2 L 7 3 4F A3WE 1998070300684 19980703 00684 NM 1998 7 3 AALA981054 1 19980526 A 5330 SKIN BOEING 727 727223 1384074 NM BS 505-515 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FORWARD CARGO BELLY SKIN CORRODED STATION 505-515, INBOARD SIDE STRINGER 26L. REMOVED CORROSION AND INSTALLED SKI N REPAIR PER SRM 53-30-3 FIG 24. (M) 2 L 7 3 4F A3WE 1998070300685 19980703 00685 NM 1998 7 3 AALA981055 1 19980526 A 3221 FITTING BOEING 727 727223 1384074 NM NLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - RT CORROSION EMITTING FROM NLG RT TRUNNION BEARING BORE. LEFT CORROSION IN BORE LT TRUNNION BEARING BORE. REPLAC ED RT TRUNNION FITTING. REPLACED LEFT TRUNNION FITTING. (M) 2 L 7 3 4F A3WE 1998070300686 19980703 00686 NM 1998 7 3 AALA981075 1 19980526 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 310 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - LEFT FORWARD AND AFT VERTICAL STIFFENERS CRACKED AT LT NLG TRUNNION. REPLCED LT FORWARD VERTICAL STIFFENER. (M) 2 L 7 3 4F A3WE 1998070300687 19980703 00687 NM 1998 7 3 AALA981074 1 19980527 A 5330 SKIN BOEING 727 727223 1384074 NM BS 350 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - SKIN BULGED AND RIVETS BROKEN, CORRODED. DOUBLER INSTALLED PER SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300688 19980703 00688 NM 1998 7 3 AALA981073 1 19980526 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1033 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND SKIN CORROSION STATION 1033 STRINGER 28R. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998070300689 19980703 00689 NM 1998 7 3 AALA981072 1 19980526 A 5330 SKIN BOEING 727 727223 1384074 NM BS 703 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON SKIN STATION 703 OUTBOARD STRINGER 27 RT BY DOME NUT. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1998070300690 19980703 00690 NM 1998 7 3 AALA981071 1 19980526 A 5330 SKIN BOEING 727 727223 1384074 NM BS 502-518 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - LEVELING COMPOUND BULGING STATION 502-518 INBOARD STRINGER 26 RT. CUT OUT DAMAGED AREA, INSTALLED REPAIR PARTS AS PER SRM 53-30-3 FIG 24 DETAIL 1. (M) 2 L 7 3 4F A3WE 1998070300691 19980703 00691 NM 1998 7 3 AALA981070 1 19980527 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND HEAVY CORROSION INSIDE STRINGER 23R AT JUNCTION TO BELLFRAME STATION 1148. INSTALLED STRINGER SPLICE PER SR M 53-10-3. (M) 2 L 7 3 4F A3WE 1998070300692 19980703 00692 NM 1998 7 3 AALA981069 1 19980527 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - HEAVY CORROSION INSIDE STRINGER AT JUNCTION TO BELLFRAME STRINGER 22R STATION 1148. INSTALLED STRINGER SPLICE PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998070300693 19980703 00693 NM 1998 7 3 AALA981068 1 19980526 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - CORROSION ON FLOORBEAM UPPER CAP STATION 1110 LBL 10 TO LBL 12. INSTALLED DOUBLER PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998070300694 19980703 00694 NM 1998 7 3 AALA981067 1 19980526 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON UPPER AND LOWER SURFACE OF TOP FLANGE OF FLOORBEAM STATION 380 RBL 24 TO RBL 64. FABRICATED AN D INSTALLED REPAIR PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998070300695 19980703 00695 NM 1998 7 3 AALA981066 1 19980526 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1040 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - STRINGER HEAVILY CORRODED INBOARD/OUTBOARD SECTION STATION 1040 STRINGER 26R. REPAIRED STRINGER PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998070300696 19980703 00696 NM 1998 7 3 AALA981065 1 19980526 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1100 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - OUTBOARD SIDE OF STRINGER 28R CORRODED STATION 1100. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998070300697 19980703 00697 NM 1998 7 3 AALA981064 1 19980526 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1033 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND STRINGER CORRODED OUTBOARD SECTION. FASTENED STRINGER CLIP TO FRAME AND STRINGER. COMPLETED CRACKED STRING ER TYPICAL REPAIR PER SRM 53-10-3 PAGE 4C. (M) 2 L 7 3 4F A3WE 1998070300698 19980703 00698 NM 1998 7 3 AALA981063 1 19980526 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 620-628 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION IN STRINGER 27 RT STATION 620-628. REMOVED CORROSION AND INSTALLED CHANNEL REPAIR PER ESO 11697, DATED 5-8-98. (M) 2 L 7 3 4F A3WE 1998070300699 19980703 00699 NM 1998 7 3 AALA981062 1 19980515 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON BOTH SIDES OF TOP FLANGE OF FLOORBEAM STATION 344 LBL 38 TO 39. CUT OUT CORRODED FLANGE AND IN STALLED NEW FLANGE AND DOUBLERS PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998070300700 19980703 00700 NM 1998 7 3 AALA981061 1 19980526 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - STRINGER 15R CRACKED AT FORWARD AND AFT END OF ICE LIGHT CUTOUT. REPAIRED PER SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 1998070300701 19980703 00701 NM 1998 7 3 AALA981060 1 19980526 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND STRINGER 15L CRACKED AT FORWARD AND AFT END OF ICE LIGHT CUTOUT. REPAIRED PER SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 1998070300702 19980703 00702 NM 1998 7 3 AALA981059 1 19980526 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 345 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON BOTH SIDES OF UPPER FLANGE OF FLOORBEAM STATION 345 RBL 44-64. BLENDED OUT CORROSION REPAIRED AND INSTALLED DOUBLER PER SRM 53-10-8 PAGE 9D. (M) 2 L 7 3 4F A3WE 1998070300703 19980703 00703 NM 1998 7 3 AALA981058 1 19980526 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION TOP OF FLOORBEAM. INSTALLED DOUBLER AT FLOORBEAM STATION 400 RBL 12 PER SRM 53-10-8 9C-9E. ALSO, INSTALLED FLOOR SUPPORT AND BRACKET STATION 380-400 RBL 12. (M) 2 L 7 3 4F A3WE 1998070300704 19980703 00704 NM 1998 7 3 AALA981057 1 19980526 A 5711 SPAR BOEING 727 727223 1384074 NM WS 373 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - WING FRONT SPAR LOWR CAP CORRODED AT NR 5 SLAT INBOARD TRACK TOP SIDE WS 373. INSTALLED REPAIR PER ESO 11697 DATE D 5/11/98. (M) 2 L 7 3 4F A3WE 1998070300705 19980703 00705 NM 1998 7 3 AALA981056 1 19980526 A 5510 BEAM BOEING 727 727223 1384074 NM RT HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - FOUND CORROSION ON UPPER SURFACE OF RT HORIZ STAB TE BEAM FORWARD OF 4TH FROM OUTBOARD ELEV HINGE. COMPLETED REPA IR BY INSTALLING DOUBLER AS PER ESO 11697 AND SRM 55-10-6. TREATED, PRIMED AND SEALED AREA. (M) 2 L 7 3 4F A3WE 1998070300706 19980703 00706 NM 1998 7 3 AALA980958 1 19980511 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 868AA 21373 TUL - FOUND CORROSION ON CABIN FLOORBEAM LOWER FLANGE, WHERE CEILING PANEL OF CARGO COMP IS SECURED. REMOVED CORROSION, ALODINED AND PAINTED, INSTALLED SUPPORT ANGLES AND STRAP PER SRM 53-10-8 ON LOWER FLOORBEAM AT STATION 1070, BL 0 TO LB L 48. (M) 2 L 7 3 4F A3WE 1998070300707 19980703 00707 NM 1998 7 3 AALA980800 1 19980415 A 5522 SKIN BOEING 727 727223 1384074 NM RT ELEV CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 862AA 21089 TUL - FOUND SKIN CRACKED LOWER SURFACE OF RT ELEV INBOARD OF ELEV PCU. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 55-20-3. (M) 2 L 7 3 4F A3WE 1998070300708 19980703 00708 NM 1998 7 3 AALA980864 1 19980430 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1143 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 705AA 22462 TUL - RT AFT LAV FLOOR OUTBOARD OF FORWARD OUTBOARD TANK CABLE ATTACH LUG IS CORRODED, FORWARD OF INBOARD TANK CABLE ATT ACH IS CORRODED. REMOVED CORRODED HAT CHANNEL AND INSTALLED SERVICEABLE HAT CHANNEL. (M) 2 L 7 3 4F A3WE 1998070300709 19980703 00709 NM 1998 7 3 AALA980818 1 19980422 A 5330 SKIN BOEING 727 727223 1384074 NM BS 585-592 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 TUL - FUSE SKIN HAS CORROSION BELOW STRINGER 28L AT STATION 585 - STATION 592. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998070300710 19980703 00710 NM 1998 7 3 AALA980817 1 19980422 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 585-592 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 TUL - STRINGER CORRODED AT 28L, STATION 585-592. FABRICATED/INSTALLED STRINGER REPAIR FILLER AND 2 SPLICES AT STATION 5 70-592 SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300711 19980703 00711 NM 1998 7 3 AALA980811 1 19980416 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1070-1090 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 715AA 22470 TUL - FOUND CORROSION BELOW STRINGER 29L BETWEEN STATION 1070 TO STATION 1090. INSTALLED SKIN DOUBLER AT STATION 1077 T O STATION 1087 AS PER SRM 53-30-3 FIG 3 AND INSTALLED STRINGER REPAIR DOUBLER STATION 1070 TO STATION 1090 AS PER SRM 53 -10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998070300712 19980703 00712 NM 1998 7 3 AALA980862 1 19980430 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 513-517 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 713AA 22469 TUL - STRINGER 28R HAS HEAVY CORROSION FROM STATION 513 TO 517, INBOARD SIDE OF STRINGER AND FASTENER IS POPPED IN STRIN GER. INSTALLED DOUBLER (U-CHANNEL AND J-CHANNEL) PER SRM 53-10-3 FIG 1 SHEETS 1-4. INSTALLED NEW STRINGER TO FRAME CLI P. (M) 2 L 7 3 4F A3WE 1998070300713 19980703 00713 NM 1998 7 3 AALA980861 1 19980430 A 5311 FRAME BOEING 727 727223 1384074 NM BS 783 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 713AA 22469 TUL - FRAME STATION 783.95 LEFT CRACKED APPROX 1 INCH BELOW FLOOR LINE. CRACK EXTENDS FROM INBOARD FLANGE FORWARD AND O UTBOARD TO 1ST FASTENER HOLE IN FLOORBEAM, END OF CRACKED MARKED. HFEC STOP DRILLED CRACK AND INSTALLED DOUBLER AND TRI PLER IAW SB 53-0197. (M) 2 L 7 3 4F A3WE 1998070300714 19980703 00714 EU 1998 7 3 AALA980863 1 19980430 A 5320 FLOOR SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 1024-1030 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - THE FLOOR SUPPORT IS CORRODED FROM STATION 1024-1038 TRACK 4A. REMOVED CORRODED SUPPORT AND INSTALLED NEW SUPPORT PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998070300715 19980703 00715 NM 1998 7 3 AALA984106 1 19980511 A 5320 SPLICE BOEING 767 767223 1385123 NM BS 1298 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - STRINGER AND STRINGER SPLICE AT 537L HAD CORROSION. FABRICATED AND REPLACEMENT STRINGER SPLICE FROM .071 INCH THI CK 7075-T6 ALCLAD. INSTALLED PER SRM 51-40-02 AND 51-40-03. APPLIED ALODINE AND TWO COATS PRIMER. (M) 2 L 7 2 4F RT A1NM 1998070300716 19980703 00716 NM 1998 7 3 AALA984105 1 19980513 A 5313 STRINGER BOEING 767 767223 1385123 NM BS 1307 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 302AA 22308 AFW - FUSELAGE STRINGER AT STATION 1307 HAS CORROSION. FABRICATED NEW STRINGER SPLICE AND INSTALLED PER SRM. (M) 2 L 7 2 4F RT A1NM 1998070300717 19980703 00717 NM 1998 7 3 AALA984133 1 19980522 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 790-809 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 372AA 25199 AFW - FOUND AND BLENDED FIVE SMALL AREAS OF CORROSION ON THE UPPERS SURFACE OF THE LONGITUDINAL FLOORBEAM. THE BLENDOUT S EXCEED SRM MAX ALLOWABLE LIMITS. ROTOPEENED, TREATED, PRIMED AND FILLED BLEND AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1634. (M) 2 L 7 2 4F RT A1NM 1998070300718 19980703 00718 WP 1998 7 3 AALA981006 1 19980516 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 617-619 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 426AA 49338 TUL - FOUND CORROSION ON BOTTOM OF CUSP MEMBRANE STATION 617 TO STATION 619, LONGERON 18L. REMOVED OLD CUSP. MANUFACTU RED AND INSTALLED DOUBLER PER SRM 53-01 FIG 4-3. (M) 2 L 7 2 4F A6WE 1998070300719 19980703 00719 WP 1998 7 3 AALA981015 1 19980522 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 232AA 49179 TUL - CUSP ANGLE MEMBRANE CORRODED BENEATH FORWARD SERVICE DOOR PANEL. INSTALLED NEW SECTION OF CUSP ANGLE PER SRM 53-0 5, FIG 55. (M) 2 L 7 2 4F A6WE 1998070300720 19980703 00720 WP 1998 7 3 AALA981014 1 19980522 A 5320 FLOOR SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 232AA 49179 TUL - FLOOR SUPPORT CORRODED, BS 200. DRAWING ON SRM 51-10-3. CUT OUT CORRODED SECTION, BLENDED AIND INSTALLED DOUBLER PER AARD 53-00-00-2. (M) 2 L 7 2 4F A6WE 1998070300721 19980703 00721 WP 1998 7 3 AALA981106 1 19980601 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1741 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION ON FRAME 1741 FROM LONG 51L TO 51R. MANUFACTURED A REPAIR DOUBLER FOR FRAME J-CHANNEL PER AARD 51 -01-00-05 AND INSTALLED ON FRAME 1741 LONG 51L TO 51R. (M) 2 L 7 3 4F A22WE 1998070300722 19980703 00722 WP 1998 7 3 AALA981107 1 19980526 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1853-1996 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - GALLEY SUPPORT NR 3 HAS CORROSION AT 3 GALLEY MOUNTS. INSTALLED REPLACEMENT PART PER AARD 51-10-00-1, TREATED, PR IMED AND PAINTED. (M) 2 L 7 3 4F A22WE 1998070300723 19980703 00723 WP 1998 7 3 AALA981108 1 19980526 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 808 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - C-5 GALLEY RT FORWARD AND AFT SUPPORTS AND BEAM HAS HEAVY CORROSION. FABRICATED AND INSTALLED A SECTION OF A FLOO RBOARD GALLEY SUPPORT PER AARD 51-01-00-05 PAGE 1. (M) 2 L 7 3 4F A22WE 1998070300724 19980703 00724 WP 1998 7 3 AALA981109 1 19980602 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 840-860 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - G5 GALLEY CENTER SUPPORT AND BEAM HAS SURFACE CORROSION. REMOVED CORROSION PER SRM 51-21-01, TREATED AND PRIMED P ER SRM 51-21-01. (M) 2 L 7 3 4F A22WE 1998070300725 19980703 00725 WP 1998 7 3 AALA981110 1 19980602 A 5320 INTERCOSTAL DOUG DC10 DC1030 3023501 WP BS 1967 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - INTERCOSTAL CORRODED BETWEEN LONGERON 47R TO LONGERON 48R AND BET STATION 1967 TO STATION 1977. REMOVED AND REPLA CED INTERCOSTAL PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998070300726 19980703 00726 WP 1998 7 3 AALA981114 1 19980602 A 5320 SILL DOUG DC10 DC1030 3023501 WP BS 939 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION UNDER OMNI ROLLER SUPPORT CASTING AROUND BOLT HOLES ON DOOR SILL. PERFORMED REPAIR PER ESO DATED 6-1-98. SPOT FACED HOLES TO REMOVE CORROSION AND PLUGGED WITH SHIMS. (M) 2 L 7 3 4F A22WE 1998070300727 19980703 00727 WP 1998 7 3 AALA981097 1 19980530 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 2003-2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION ON T-ANGLE AT AFT END NR 4 GALLEY SUPPORT. REPAIRED T-ANGLE AT STATION 2007-2003 AND AFT NR 4 GAL LEY SUPPORT PER ESO 7349 DATED 05-28-98. (M) 2 L 7 3 4F A22WE 1998070300728 19980703 00728 WP 1998 7 3 AALA981100 1 19980530 A 5320 FLOOR SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT JUST AFT OF LAV F STATION 1887. INSTALLED FABRICATED REPAIR PER SRM 53-60-0 1 TO FLOORBOARD SUPPORT. (M) 2 L 7 3 4F A22WE 1998070300964 19980703 00964 EU 1998 7 3 MALA976157 1 19980629 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 142XJ 142 DURING INSPECTION, EMERGENCY LIGHT 1D INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998070300965 19980703 00965 EU 1998 7 3 MALA976158 1 19980630 A 3150 MASTER WARNING BAC 146 AVRO146RJ85A 1500097 EU COCKPIT MALFUNCTIONED A MALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 503XJ E2310 FIRST OFFICERS RED MASTER WARNING FLASHED ON TAKEOFF, NO OTHER INDICATIONS. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED T O THE GATE. MAINTENANCE CLEANED AND RERACKED PRINTED CIRCUIT BOARD NR 2. RAN THROTTLES SEVERAL TIMES AND PERFORMED OPS CHECK OF CONFIG WARNING, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998070300966 19980703 00966 SO 1998 7 3 LR7A9828 1 19980612 A 3260 1EN616 SWITCH LKHEED 382 382G 526414U SO LT MLG INTERMITTENT A LR7A O OTHER N FALSE WARNING LD LANDING 1 AL 03 401LC 4606 LT MLG IND STAYED UP WHEN GEAR SELECTED DOWN, OK ON SECOND TRY. REMOVED AND REPLACED LEFT DOWN LIMIT SWITCH PER MM 32-3 3-202, OPS CHECKED OK. 2 H 7 4 4T A1SO 1998070300967 19980703 00967 SO 1998 7 3 LR7A9829 1 19980622 A 5320 355671 FITTING LKHEED 382 382G 526414U SO BS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 4698 DURING B-CHECK, THE RT FS 617 25000 LB TIE DOWN FITTING WAS DISCOVERED CRACKED DURING EDDY CURRENT INSPECTION PER CARD S P-262. THE CRACK WAS .75 INCHES LONG, LOCATED IN THE AFT RADIUS. THE FITTING WAS REPAIRED IAW LOCKHEED SRM SMP 583 CHA P 53-40-40, PAGES 111 THRU 116. 2 H 7 4 4T A1SO 1998070300968 19980703 00968 SO 1998 7 3 LR7A9830 1 19980626 A 2612 700120 FIRE LOOP LKHEED 382 382G 526414U SO NR 1 ENGINE SHORTED A LR7A F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 AL 03 403LC 327 4590 NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER T/O, FIRE EMERGENCY HANDLE PULLED AT 2200Z, RETURNED TO BRW. REMOVED A ND REPLACED NORMAL AFT FIRE BOTTLE AND SQUIBB, INSPECTED NR 1 ENGINE NO EVIDENCE OF FIRE. THREE ENGINE FERRY AUTHORIZED IAW LYNDEN AIR CARGO GMM FORM 029. REPLACED NR 1 NACELLE FWD FIRE LOOP DUE SHORTED ENG FIRE WARNING, OPS NOMRAL PER 26 -10 MM. 2 H 7 4 4T A1SO 1998070300969 19980703 00969 SO 1998 7 3 PNSA980601 1 19980613 A 8120 4091709001 TURBO CHARGER PIPER PA31 PA31350 7103110 SO RT ENGINE FAILED A PNSA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 3588Z 1195 318052130 PARTIAL POWER LOSS ON RT ENGINE DURING AFTER TAKEOFF. RETURNED TO AIRPORT LANDING WAS UNEVENTFUL. REPLACED TURBO CHARG ER. 1 L 7 2 3O A20SO 1998070300970 19980703 00970 SO 1998 7 3 PNSA980602 1 19980605 A 8120 4091709001 TURBO CHARGER PIPER PA31 PA31350 7103110 SO LT ENGINE FAILED A PNSA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 AL 03 28KE 19433 318152049 POWER FLUCTUATION ON LT ENGINE DURING CRUISE. RETURNED TO AIRPORT. REPLACED TURBO CHARGER. 1 L 7 2 3O A20SO 1998070300971 19980703 00971 NM 1998 7 3 UPS98227080 1 19980617 A 5510 BEAM BOEING 727 72722C 138400F NM HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE-C, CORROSION ON HORIZONTAL STAB TRAILING EDGE UPPER SURFACE AT STAB STATION 188.65 LT. REPAIR CARRIED O UT IAW SRS ENGINEERING ORDER 98-19-008, UPS ENGINEERING FILE NUMBER 727-55-0372. 2 L 7 3 4F A3WE 1998070300972 19980703 00972 NM 1998 7 3 UPS98227081 1 19980616 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1080-1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER, BS 1120 BETWEEN S20R AND S19R. ON FURTHER INVESTIGATION, EXTESNIVE CORROSION DISCOVERED, SKIN PANEL. REMOVED BETWEEN BS 1183 AND BS 1080, STR 14 TO 209 RT. NEW PANEL AND DOU BLERS FABRICATED AND INSTALLED IAW SRS EINGEERING ORDER 98-19-00 5, REF UPS ENGINEERING FILE NR 5330-2041. 2 L 7 3 4F A3WE 1998070300973 19980703 00973 NM 1998 7 3 UPS98227082 1 19980615 A 5330 SKIN BOEING 727 72722C 138400F NM BS 1048 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE-C, CORROSION BETWEEN SKIN AND INTERNAL DOUBLER AT BS 1048, STR 18 RT. REPAIR TO SKIN CARRIED OUT IAW SR S ENGINEERING ORDRE 98-19-006, REF UPS ENGINEERING FILE NR 727-53-2042. 2 L 7 3 4F A3WE 1998070300974 19980703 00974 NM 1998 7 3 UPS98227083 1 19980616 A 7120 MOUNT BOEING 727 72722C 138400F NM NR 1 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE-C, PITTING CORROSION ON BORE OF HOLES ON NR 1 ENGINE INBD FWD MOUNT FITTING (FOUR HOLES). REPAIR CARRIE D PER SRS ENGINEERING ORDER 98-19-001, REF UPS ENGINEERING FILE NR 727-71-0069 AND SRS ENGINEERING ORDER 98-19-003, REF UPS ENGINEERING FILE NR 727-71-0067. 2 L 7 3 4F A3WE 1998070300975 19980703 00975 NM 1998 7 3 UPS98227084 1 19980616 A 7120 MOUNT BOEING 727 72722C 138400F NM NR 3 ENGINE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE-C, PITTING CORROSION ON BORE OF HOLES ON NR 3 ENGINE INBD FWD MOUNT FITTING (FOUR HOLES). REPAIR CARRIE D OUT IAW SRS ENGINEERING ORDER 98-19-002, REF UPS ENGINEERING FILE NUMBER 727-71-0070, AND SRS ENGINEERING ORDER 98-19- 00 4, REF UPS ENGINEERING FILE NR 727-71-0068. 2 L 7 3 4F A3WE 1998070300976 19980703 00976 NM 1998 7 3 UPS98227085 1 19980617 A 5320 65931158 FITTING BOEING 727 72722C 138400F NM BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE-C, DURING INSPECTION OF OF BS 520, A CRACK WAS DISCOVERED IN LATCH SUPPORT FITTING. LATCH SUPPORT FITTI NG REPLACED IAW EO B727-5310-4501, APPENDIX C. 2 L 7 3 4F A3WE 1998070300977 19980703 00977 NM 1998 7 3 UPS98527086 1 19980701 A 3230 2670296M1 SEQUENCE VALVE BOEING 757 75724APF 1384969 NM LANDING GEAR MALFUNCTIONED A IPXA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 465UP 28269 INSPECTION TYPE-N/A, GEAR DISAGREE DISPLAYED WITH GEAR HANDLE UP. ALSO, EICAS GEAR DOOR DISPLAYED. DOORS AND GEAR AMBE R LIGHTS ILLUM, ALL GREEN DN LGTS EXTIN. THERE WAS A VIBRATION, RECYCLED THE GEAR, THE GEAR CYCLED SLOWLY AT 250 KNOTS. REMOVED AND REPLACED GEAR OPERATED SEQUENCE VALVE PER M/M 32-34-06. OP'S CHECK NORMAL. (P/N 2670296M1) (S/N 0261) ON , (S/N 1652) OFF. 2 L 7 2 4F RT A2NM 1998070300978 19980703 00978 WP 1998 7 3 ABXA9800575 1 19980510 A 5730 57696001 SKIN DOUG DOUG DC8 DC863F 302198F WP WS 610 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE UPPER SKIN AT STATION XFS 610 HAS HEAVY CORROSION AND IS CRACKED. REPAIRED IAW DC8 SRM 52-2-1 A ND 51-1-21. 2 L 7 4 4F 4A25 1998070300979 19980703 00979 WP 1998 7 3 ABXA9800576 1 19980510 A 5320 47516401 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 742 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LONGERON END FITTING AT STATION 742 LONGERON 19L CRACKED. REPLACED FITTING PER DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998070300980 19980703 00980 WP 1998 7 3 ABXA9800577 1 19980510 A 5320 5644973502 FITTING DOUG DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STRINGER NR 59 END FITTING CRACKED AT NR 4 ALTERNATE FUEL TANK. INSTALLED REPLACEMENT FITTING PER DWG 5644973, DC8 SRM 51-1-20D AND 51-1-23. 2 L 7 4 4F 4A25 1998070300981 19980703 00981 WP 1998 7 3 ABXA980578 1 19980509 A 5712 5769603 RIB DOUG DOUG DC8 DC863F 302198F WP WS 442.185 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE RIB AT STATION XS 442.185 IS CRACKED AT AFT UPPER END. INSTALLED ANGLE REPAIR DOUBLERS IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F 4A25 1998070300982 19980703 00982 WP 1998 7 3 ABXA9800579 1 19980509 A 5720 5769859125 INTERCOSTAL DOUG DOUG DC8 DC863F 302198F WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE JUST OUTBOARD OF THE LEADING EDGE AUX TANK, THE INTERCOSTAL IS CRACKED AT THE INBOARD END. REPAI RED IAW DC8 SRM 51-01-20 AND DOUG DWG NR 5769859. 2 L 7 4 4F 4A25 1998070300983 19980703 00983 WP 1998 7 3 ABXA9800580 1 19980626 A 5320 992341711 FITTING DOUG DOUG DC9 DC941 302207N WP BS 696 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND FITTING AT LBL 44.5 STATION 696 CRACKED. REPLACED SEAT TRACK SUPPORT FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300984 19980703 00984 WP 1998 7 3 ABXA9800581 1 19980626 A 5522 99184804 SKIN DOUG DOUG DC9 DC941 302207N WP RT ELEVATOR CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND CORROSION ON RIGHT ELEVATOR SKIN AT STATION XE 49. REPLACED SKIN IAW DACO DWG 5910412. 2 L 7 2 4F A6WE 1998070300985 19980703 00985 WP 1998 7 3 ABXA9800582 1 19980626 A 5313 277792211200 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPLACED LONGERON 4 LEFT IAW DC9 SRM 51-30-2, 51-30-1 AND 51- 30-5. 2 L 7 2 4F A6WE 1998070300986 19980703 00986 WP 1998 7 3 ABXA9800583 1 19980626 A 5330 59114013 SKIN DOUG DOUG DC9 DC941 302207N WP BS 185-173 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED STATION 185 TO 173 LONGERON 27 LEFT. REPLACED LONGERON IAW DC9 SRM 53-04-0 0 AND SRM 51-10-3. 2 L 7 2 4F A6WE 1998070300987 19980703 00987 WP 1998 7 3 ABXA9800584 1 19980626 A 5320 39258171 FITTING DOUG DOUG DC9 DC941 302207N WP BS 677 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND FITTING (P/N 3925817-1) CRACKED LBL 22 STATION 677. REPLACED SEAT TRACK SUPPORT FITTING IAW DC9 S RM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300988 19980703 00988 WP 1998 7 3 ABXA9800585 1 19980626 A 5320 39258171 FITTING DOUG DOUG DC9 DC941 302207N WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 971AX 47497 DURING C-CHECK, FOUND FITTING (P/N 3925817-1) CRACKED LBL 44.5 STATION 718. REPLACED SEAT TRACK SUPPORT FITTING IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998070300989 19980703 00989 WP 1998 7 3 ABXA9800586 1 19980509 A 5712 5769603 RIB DOUG DOUG DC8 DC863F 302198F WP WS 354 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE RIB AT STATION XFS 354.0 IS CRACKED AT THE AFT UPPER END. INSTALLED REPAIR ANGLES IAW DC8 SRM 51 -1-20D AND 51-1-8. 2 L 7 4 4F 4A25 1998070300990 19980703 00990 WP 1998 7 3 ABXA9800590 1 19980630 A 7931 41800044 TRANSMITTER DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE CLOGGED A ABXA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 GL 23 813AX 1551 46136 671097 DURING CRUISE, NR 3 ENGINE OIL PRESSURE WENT TO 100 PSI. SECURED NR 3 ENGINE. REPLACED NR 3 ENGINE OIL PRESSURE TRANSM ITTER AND OIL FILTER IAW DC8 MM 79-30-00. 2 L 7 4 4F 4 F 4A25 1E8 1998070300991 19980703 00991 NM 1998 7 3 DL73K981358 1 19980627 A 5330 654577882 SKIN BOEING 737 737232 1384475 NM BS 960 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 THE SKIN ASSY AT THE LOWER FWD CORNER OF THE AFT ENTRY DOOR WAS FOUND WITH A TYPICAL CRACK THROUGH THE SKIN, DOUBLER, AN D BEAR STRAP. THE CRACK WAS REPAIRED PER B737 SRM 53-30-3 FIG 24 EXCEPT BLIND FASTENERS WERE AUTHORIZED ON A TEMPORARY BASIS. THE REPAIR WAS ACCOMPLISHED PER ER/A 365132-14, REV A. 2 L 7 2 4F RT A16WE 1998070300992 19980703 00992 WP 1998 7 3 DLL13981359 1 19980626 A 5711 1503229103 SPAR CAP LKHEED 1011 10113851 5265010 WP BS 1043 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 786DL 193A1123 THE UPPER CAP OF THE CENTER WING INTERMEDIATE SPAR AT FS 1043 WAS FOUND CRACKED BEYOND LIMITS AT THE LT OUTBD END. THE CAP WAS CUT NEAR LBL 80 AND A NEW OUTBD END WAS SPLICED IN WITH 4 STEEL SPLICE ANGLES AND 2 SPLICE STRAPS. THE REPAIR W AS ACCOMPLISHED PER ER/A 365093-14, REV A. 2 L 7 3 4F A23WE 1998070300994 19980703 00994 NM 1998 7 3 DL76L981361 1 19980629 A 2421 IDG 755359A BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 1200K L0180 28457 727775 RIGHT GEN DRIVE LIGHT CAME ON DURING CLIMBOUT. REPLACED RIGHT IDG, OPS CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1998070300995 19980703 00995 NM 1998 7 3 DL757981362 1 19980630 A 5210 MECHANISM BOEING 757 757232 1384965 NM PAX DOOR OUT OF ADJUST A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 612DL 22819 RT AFT ENTRY DOOR LIGHT ON OVERHEAD PANEL. ADJ DOOR PER M/M 52-11. PRESSURIZED A/C TO 8 PSI. DOOR WAS FAIRED AND EVEN , OK FOR SERVICE. 2 L 7 2 4F RT A2NM 1998070300996 19980703 00996 NM 1998 7 3 DL72S981365 1 19980630 A 5320 WEB BOEING 727 727225 1384077 NM BS 1230 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8889Z 21858 A .25 INCH CRACK LIGHTENING HOLE STA 1230 LT ON AFT AIRSTAIR CUTOUT VERT WEB. REPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1998070300997 19980703 00997 NM 1998 7 3 DLM90981367 1 19980630 A 2421 GENERATOR 1B1893 DOUG MD90 MD9030 3023690 NM RIGHT FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 906DA 115C0146 53386 AT ALT C/P LIGHTS FLICKERED SEVERAL TIMES THEN GOT RT GEN OFF MSG ON OAP. ALSO, RT AC BUS OFF MSG. REPLACED RT GENERAT OR CONVERTER CKS OK. 2 L 7 2 4F RT A6WE 1998070300998 19980703 00998 NM 1998 7 3 DL72K981368 1 19980630 A 3350 900835A BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 415DA 21257 LFT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS OK. 2 L 7 3 4F A3WE 1998070300999 19980703 00999 NM 1998 7 3 DL73E981369 1 19980630 A 3350 3548994 BULB BOEING 737 737247 138448D NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 375DL 23602 LT WING EMERGENCY LIGHT INOP. REPLAMPED. 2 L 7 2 4F A16WE 1998070301000 19980703 01000 WP 1998 7 3 RRXA98245 1 19980628 A 3310 LIGHT DOUG DC8 DC863 302198A WP COCKPIT ODOR A RRXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 951R 46092 ELECTRICAL ODOR DEVELOPED IN COCKPIT. TURNED OFF OVERRIDE WHITE LIGHT, ODOR DISSIPATED. TIGHTENED ALL CONNECTIONS ON O VERRIDE LIGHT CONTROL, OPS CHECKS OK. 2 L 7 4 4F 4A25 1998070301001 19980703 01001 WP 1998 7 3 CKSA98352 1 19980625 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 1615 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 105CK 193N1178 DURING ROUTINE A-5 CHECK INSPECTION, FOUND FS 1615 S-34 SKIN CRACKED. VERIFIED END OF CRACK BY MEANS OF HFEC MARKED. R EPAIRED CRACK IAW L1011 SRM 53-31-00 FIG 813. R/O NR 105-199. NON-ROUTINE TASK CARD NUMBER 24314. 2 L 7 3 4F A23WE 1998070301002 19980703 01002 WP 1998 7 3 CKSA98353 1 19980627 A 3610 CLAMP LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 3 ENGINE LOOSE A CKSA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 102CK 193N1198 14573 AFTER TAKEOFF, NR 3 ENGINE FIRE DET LOOP B ILLUMINATED, SWITCHED TO A LOOP AND FULL FIRE WARNING EXPERIENCED. WHEN PULL ING THROTTLE BACK ALL INDICATIONS EXTINGUISHED. FHB EMERGENCY PROCEDURES C/W, ENGINE SHUTDOWN. FOUND NR 3 ENGINE HIGH PRESSURE VALVE CLAMP LOOSE. RESECURED OPS AND LEAK CHECK GOOD IAW L1011 MM 36-11-02. OPS CHECK OF FIRE DET LOOP A AND B, NO DEFECTS NOTED IAW L1011 MM 26-11-00. 2 L 7 3 4F 4 F A23WE E12EU 1998070301003 19980703 01003 WP 1998 7 3 TC8A98037 1 19980630 A 2760 CONTROL CABLE DOUG DC8 DC8F55 3021928 WP LT SPOILER BROKEN A TC8A O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 GL 23 182SK 45817 DURING FLIGHT CONTROL CHECK, NO SPOILER PRESSURE DROP ON AILERON CHECK WHEN CHECKING THE LEFT SIDE. FOUND LT OUTBD SPOI LER RETRACT CABLE BROKEN. REPLACED CABLE AND TEST/ADJ AS PER MM 2736-0. 2 L 7 4 4F 4A25 1998071400001 19980714 00001 WP 1998 7 14 VJ9800209 1 19980624 A 5330 1A3401534007 SKIN DOUG DC9 DC932 3022066 WP BS 220 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 931VV 47674 REMOVED AND REPLACED TEMPORARY REPAIR WITH A PERMANENT REPAIR ON LT FUSELAGE AT FS 220. REMOVED EXISTING REPAIR, DUCTIN G, AND INSULATION. FABRICATED NEW REPAIR DOUBLER FROM .063 2024T3, 11 INCH BY 11.25 INCHES, AND 2 EACH FINGER DOUBLERS FROM .025 2024T3, 3 INCHES BY 11 INCHES AND 4 INCHES BY 8 INCHES. INSTALLED DOUBLERS, FILLET SEALED, INSTALLED DUCTING AND INSULATION IAW DC9 SRM 53-04, FIG 12B AND RES 1 NR 04596. 2 L 7 2 4F A6WE 1998071400002 19980714 00002 WP 1998 7 14 VJ9800210 1 19980628 A 5320 1A3402834027 FRAME DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 931VV 47674 AFT PITDOOR FRAME, FS889, L25R-26R, SKIN CORRODED ON BACKSIDE AROUND NUTPLATES. REMOVED CORROSION FOUND BEYOND LIMITS I AW DC9 SRM 51-10-3. FABRICATED WEB DOUBLER OUT OF 7075T6, .040, AND FABRICATED REPAIR DOUBLER FROM 7075T6, .050. TRIMM ED, FITTED, DRILLED, DEBURED, TREATED AND PRIMED IAW EO 98-895. INSTALLED DOUBLERS IAW DC9 SRM 98-895 AND DC9 SRM 51-30 -1. 2 L 7 2 4F A6WE 1998071400003 19980714 00003 WP 1998 7 14 IXXA9800059 1 19980624 A 3297 WIRE DOUG DC8 DC863F 302198F WP NLG CHAFED A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 906R 71009 2078 46087 EN ROUTE MGUM TO KFLL, THE GEAR UPLATCH CHECK FAILED WITH THE GEAR NOT LATCHED WARNING LIGHT ILLUMINATED. THE CREW CYC LED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO KFLL FOR AN UNEVENTFUL LANDING. MAI NTENANCE INSPECTED THE AIRCRAFT AND LOCATED CHAFFED WIRES AT THE NOSE GEAR UPLATCH SWITCH. MAINTENANCE REPAIRED THE WIR ES, CLEANED AND LUBRICATED THE RIGHT MAIN GEAR UPLATCH MECHANISM. MAINTENANCE PERFORMED A SUCCESSFUL GEAR SWING IN ACCO RDANCE WITH THE DOUGLAS MAINTENANCE MANUAL RETURNING THE AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 1998071400004 19980714 00004 NE 1998 7 14 CALA9800211 2 19980211 A 7313 FUEL NOZZLE BOEING 727 727227 1384078 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE STREAKING A A CALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 09 17773 21045 653917 THE NR 1 ENGINE POPPED AND EGT WENT TO 600 DEGREES WHILE CLIMBING THROUGH 18000 FEET AFTER TAKEOFF FROM IAH. THE ENGINE VIBRATED AND WAS SHUTDOWN. THE N2 DROPPED TO 70 PERCENT BEFORE THROTTLE WAS PULLED TO IDLE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THE PRIMARY CAUSE OF FAILURE WAS D UE TO TWO STREAKING FUEL NOZZLES WHICH CAUSED FIRST STAGE NGV'S TO HAVE COMPLETE BURN THROUGH, RESULTING IN FAILURE OF O NE HPT BLADE AND SUBSEQUENT DOWNSTREAM DAMAGE TO LPT. 2 L 7 3 4F 4 F A3WE E2EA 1998071400005 19980714 00005 NM 1998 7 14 CALA9801189 1 19980701 A 3230 1030875 SOLENOID BOEING 737 737524 1384721 NM LANDING GEAR INOPERATIVE A CALA O OTHER O OTHER CL CLIMB 1 SW 09 14639 28900 THE AIRCRAFT HAD A BRIEF HISTORY OF THE LANDING GEAR LEVER BINDING DURING GEAR RETRACTION. MAINTENANCE REMOVED AND REPL ACED THE LANDING GEAR LEVER LATCH SOLENOID IAW MM 32-31-31 AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1998071400006 19980714 00006 NM 1998 7 14 CALA9801190 1 19980630 A 5330 PANEL BOEING 727 727227 1384078 NM BS 290 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A .5 CRACK AT FASTENER HOLE OF NLG WHEEL WELL TOP CENTER PANEL, STA 290, LBL 2. THE CRACKED AREA WAS C UT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998071400007 19980714 00007 NM 1998 7 14 CALA9801191 1 19980630 A 5320 FITTING BOEING 727 727227 1384078 NM BS 940 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 2.5 INCH CRACK IN FITTING AT STA 940, STRINGER 18A. A NEW FITTING WAS FABRICATED AND INSTALLED IAW S RM 51-30-2. 2 L 7 3 4F A3WE 1998071400008 19980714 00008 NM 1998 7 14 CALA9801192 1 19980630 A 5320 BRACES BOEING 727 727227 1384078 NM BS 720-990 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND FLOORBEAM SUPPORT BRACES CRACKED BETWEEN STA 950A-950B, BL 0, STA 970-990, BL 0, AND STA 720-720A, BL 0 . THE CRACKS WERE 1-2.5 LONG. NEW SUPPORT BRACES WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-40-4, AND 51-30-2. 2 L 7 3 4F A3WE 1998071400009 19980714 00009 NM 1998 7 14 CALA9801193 1 19980701 A 5542 SKIN BOEING 727 727224 1384076 NM RUDDER TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1 TEAR IN UPPER RUDDER RT SIDE TRAILING EDGE SKIN. THE TORN AREA WAS CUT OUT. A DOUBLER WAS FABRICA TED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998071400010 19980714 00010 NM 1998 7 14 CALA9801194 1 19980701 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FLOORBEAM CORRODED AT STA 380, RBL 18. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10-8. A REPAIR WAS FA BRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, AND 51-40-4. 2 L 7 3 4F A3WE 1998071400011 19980714 00011 NM 1998 7 14 CALA9801195 1 19980701 A 5754 BRACKET BOEING 727 727224 1384076 NM NR 5 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .75 INCH CRACK IN NR 5 LEADING EDGE FLAP INBOARD MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BR ACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-40-3, AND 51-10-2. 2 L 7 3 4F A3WE 1998071400012 19980714 00012 NM 1998 7 14 CALA9801196 1 19980701 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND SEAT TRACK CORRODED AT STA 360, RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IA W SRM 51-10-1 AND 53-10-5. 2 L 7 3 4F A3WE 1998071400013 19980714 00013 NM 1998 7 14 CALA9801197 1 19980701 A 5753 ANGLE BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A CRACK IN AFT END OF LOWER ANGLE AT RT OUTBOARD MID-FLAP INBOARD END RIB. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998071400014 19980714 00014 NM 1998 7 14 CALA9801198 1 19980701 A 5712 RIB BOEING 727 727224 1384076 NM WS 171.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .375 INCH CRACK IN UPPER OUTBOARD FLANGE OF RT WING RIB AT WS 171.5, STRINGER 16. AN ANGLE REPAIR WA S FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-6. 2 L 7 3 4F A3WE 1998071400016 19980714 00016 WP 1998 7 14 CALA9801200 1 19980701 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 236 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 236, STRINGER 27R. THE CRACK WAS S TOP DRILLED IAW ECRA 5320-01263. AN ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998071400017 19980714 00017 WP 1998 7 14 CALA9801201 1 19980701 A 5720 BRACKETS DOUG DC9 DC932 3022066 WP LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT WING LEADING EDGE FRAMES HAD CRACKED BRACKETS BETWEEN STA 383 AND 370, BETWEEN STA 414 AND 426, STA 506, AND STA 551. THE CRACKS WERE .25 TO .5 INCH LONG. THE CRACKED BRACKETS WERE REMOVED AND NEW BRACKETS WERE FABRICA TED AND INSTALLED IAW SRM 51-30-2, 51-30-3, 51-30-5, 51-10-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998071400018 19980714 00018 WP 1998 7 14 CALA9801202 1 19980701 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 448 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1.5 INCHCRACK IN INTERCOSTAL IN FORWARD CARGO PIT AT STA 448, LONGERON 29R. THE INTERCOSTAL WAS REMO VED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998071400019 19980714 00019 WP 1998 7 14 CALA9801203 1 19980701 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 294 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND TWO .5 INCH CRACKS IN FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 294, STRINGER 27L. THE CRACKS WERE STOP DRILLED IAW ECRA 5320-01263. A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998071400020 19980714 00020 NE 1998 7 14 9809686614 2 19980626 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7J 52054 NE NR 2 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 01 614US 20359 689474 WHILE CLIMBING THROUGH FL340, THE NR 3 ENGINE FLAMED OUT. THE ENGINES WERE RESTARTED APPROXIMATELY ONE MINUTE LATER WIT H NORMAL INDICATIONS. THE FLIGHT CONTINUED TO SEL WITHOUT DIFFICULTY. MAINTENANCE INSPECTED THE ENGINES AND PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998071400021 19980714 00021 NE 1998 7 14 9809696614 2 19980626 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7F 52054 NE NR 2 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 GL 01 614US 20359 689456 WHILE CLIMBING THROUGH FL340, THE NR 2 ENGINE FLAMED OUT. THE ENGINES WERE RESTARTED APPROXIMATELY ONE MINUTE LATER WIT H NORMAL INDICATIONS. THE FLIGHT CONTINUED TO SEL WITHOUT DIFFICULTY. MAINTENANCE INSPECTED THE ENGINES AND PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E20EA 1998071400022 19980714 00022 NE 1998 7 14 9809706642 2 19980626 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7Q 52054 NE NR 4 FAILED A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 642NW 21942 702134 WHILE CLIMBING PAST FL320 (AMS), THE NR 4 ENGINE EPR AND FUEL FLOW INDICATIONS BEGAN TO FLUCTUATE WITH EGT RISING INTO T HE CAUTION RANGE. THE ENGINE WAS SHUT DOWN, FUEL WAS DUMPED, AND THE AIRCRAFT RETURNED TO AMS AND LANDED WITHOUT INCIDE NT. THE AIRCRAFT WAS THEN CONFIGURED FOR A THREE ENGINE FERRY FLIGHT TO MSP. EXACT PART CAUSING PROBLEM TO BE DETERMIN ED. 2 L 7 4 4F 4 F A20WE E3NE 1998071400023 19980714 00023 SO 1998 7 14 COMA9810150 1 19980701 A 6123 MS25253 SWITCH EMB 120 EMB120RT SO AUTO FEATHER SYS DIRTY A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 205CA 120205 AUTOFEATHER SYSTEM INOPERABLE DURING TAKEOFF. CLEANED THE AUTOFEATHER ARMING SWITCHES IN POWER LEVER QUADRANT. 2 L 7 2 4T RT A31SO 1998071400024 19980714 00024 SO 1998 7 14 COMA9810151 1 19980630 A 6120 78249046 PCU EMB 120 EMB120RT SO RT PROP MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 263CA 17566 2346 120255 RIGHT HAND RPM DROPPED 30 PERCENT DURING TAKEOFF ROLL. REPLACED THE RIGHT HAND PCU. 2 L 7 2 4T RT A31SO 1998071400025 19980714 00025 EA 1998 7 14 COMA9860164 1 19980628 A 2910 AE2460010H0264 LINE CNDAIR CL600 CL6002B19 EA NR 2 HYD SYST LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 712CA 29 7244 NR 2 HYDRUALIC SYSTEM LOW PRESSURE WARNING. REPLACED LEAKING PRESSURE HYD LINE ASSY RIGHT HAND PYLON. 2 L 7 2 4F RT A21EA 1998071400026 19980714 00026 EA 1998 7 14 COMA9860165 1 19980701 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 977CA 7157 FORWARD EMERGENCY FLOOR LIGHT IS INOPERABLE. REPLACED BROKEN LIGHT STRIP. 2 L 7 2 4F RT A21EA 1998071400027 19980714 00027 WP 1998 7 14 UPS98827088 1 19980527 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C/CK STATION 1220 RBL 25 SEAT TRACK SPLIT WITH CORROSION. FABRICATED SEAT TRACK IAW DC8 SRM 53-2-3, A LODINED AND PRIMED IAW DC 8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998071400028 19980714 00028 WP 1998 7 14 UPS98827089 1 19980527 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C/CK CORROSION SEAT TRACK D ON UPPER/LOWER SURFACE OF TOP FLANGE AT FUSELAGE STATION 1700. CUT OUT DAMG ED SECTION OF TRACK IAW DC8 SRM 51-1-24. DRILLED NEW SPLCIE SECTION IAW DC8 SRM 51-1-24. INSTALLED NEW SPLICE SECTION AND NEW SEAT TRACK SECTION IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998071400029 19980714 00029 WP 1998 7 14 UPS98827090 1 19980526 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C/CK FLOORBEAM AT STATION 1580 HAS CORROSION ON FWD LIP IN THE AREA OF LONGERON 22 AND 23 LEFT. REMOVED CORROSION FROM FLOORBEAM MAT REMOVED 50 PERCENT IAW DC8 SRM 53-2-0. FABRICATED FILLER AND 2 ANGLE DOUBLER REPAIR IAW R EO 04839 ALODINED AND PRIMED FILLER AND 2 ANGLES IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO 04839 AND DC8 SRM 51-1-2 1. 2 L 7 4 4F RT 4A25 1998071400030 19980714 00030 WP 1998 7 14 UPS98827091 1 19980530 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C/CK FLOORBEAM FUSELAGE STATION 1700, SEVERLY CORRODED BLO TO LBL 3. REMOVED DAMGED AREA FROM BEAM. FA BRICATED INTERNAL DOUBLER, ANGLE, AND FILLER AND SHIMS IAW REO-04822. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALL ED REPAIR IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998071400031 19980714 00031 WP 1998 7 14 UPS98827092 1 19980604 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C/CK CORROSION AND CRACK LONGERON 33 LEFT STATION 1540. REMOVED DAMAGED SECTION AND FABRICATED STRAPS A ND LONGERON. ALODINED AND PRIMED AND INSTALLED IAW DC8 SRM 53-2-2, 51-1-8, 51-1-20D. 2 L 7 4 4F RT 4A25 1998071400032 19980714 00032 WP 1998 7 14 UPS98827093 1 19980606 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1480-1680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C/CK AFTER REMOVAL OF SKIN STA 14801 TO 1680 FOUND INTERNAL DOUBLERS AT LONGERON 32 LEFT AND 32 RIGHT TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED DOUBLERS, FABBED DOUBLERS AND FILLER AND ALODINED AND PRIMED AND INSTALLED IAW REO 04866 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998071400033 19980714 00033 NM 1998 7 14 QXEA9800832 1 19980630 A 3350 6104781 PWR SUPPLY DHAV 82410191011 DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTION A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 823PH 17099 81 110 PDX- FORWARD EMERGENCY TRACK LIGHTING OUT. REPLACED EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998071400034 19980714 00034 EU 1998 7 14 QXEA9800833 1 19980630 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 SEA - THE EMERGENCY EXIT LIGHT IN THE GALLEY WAS OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071400035 19980714 00035 EU 1998 7 14 QXEA9800834 1 19980629 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 PDX - GALLEY AND ROW 8 EMERGENCY EXIT LIGHTS WERE OUT. MAINTENANCE RELAMPED BOTH BULBS, EACH WAS OPERATIONALLY TESTED A ND OPERATED NORMAL. 2 L 7 2 4F RT A20EU 1998071400036 19980714 00036 WP 1998 7 14 98FDEA00423 1 19980521 A 5312 SPAR WEB DOUG DC10 DC1010 3022110 WP WS 240 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 STA-VCE - SEVERAL CRACKS WERE FOUND COMMON TO LT REAR SPAR AFT WEB AT XRS = 240. MAJOR REPAIR PERFORMED IAW EA 8-5711-3 8429 A. FABRICATED PARTS IAW DETAIL PART TRAVELER F008593/N2593. (26 JUNE 1998). 2 L 7 3 4F A22WE 1998071400037 19980714 00037 WP 1998 7 14 98FDEA00424 1 19980514 A 5312 BULKHEAD FITTING DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 STA-VCE: DURING REMOVAL AND REPLACEMENT OF P/N AYB 7000-2 (Y=1156 BLKHD CORNER FITTING) A GAP WAS FOUND BETWEEN AYB 7000 -2 WEB AND P/N NYB6054-25, NOT COVERED BY SRM STANDARDS. REF NRC NR N1341. MAJOR REPAIR PERFORMED IAW EA 8-5314-34489B . (29 JUNE 1998). 2 L 7 3 4F A22WE 1998071400039 19980714 00039 WP 1998 7 14 ABXA9800591 1 19980520 A 5330 5644981 SKIN DOUG DOUG DC8 DC863F 302198F WP PAX DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 TWO .25 INCH CRACK ON FWD PASSENGER ENTRY DOOR LOWER AFT CORNER SKIN PANEL. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998071400040 19980714 00040 WP 1998 7 14 ABXA9800592 1 19980519 A 5712 576946626 RIB DOUG DOUG DC8 DC863F 302198F WP WS 641.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE AT STATION XFS 641.25 IS CRACKED AT UPPER END. REPAIRED IAW DRAWING ABX K05056. 2 L 7 4 4F 4A25 1998071400041 19980714 00041 WP 1998 7 14 ABXA9800593 1 19980518 A 5320 9755584507 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 1120 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STATION 1120 FRAME TO CUSP FITTING, RIGHT SIDE IS CRACKED. REPAIRED IAW DC8 SRM 51-1-18 AND DWG 9755584. 2 L 7 4 4F 4A25 1998071400042 19980714 00042 WP 1998 7 14 ABXA9800594 1 19980516 A 5312 975329915 RIB DOUG DOUG DC8 DC863F 302198F WP WS 550 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE STUB UPPER RIB CRACKED AT APPROXIMATELY XFS.550. REPAIRED IAW DC8 SRM 51-1-8, 51-1-20D AND ABX D WG K05056. 2 L 7 4 4F 4A25 1998071400043 19980714 00043 WP 1998 7 14 ABXA9800595 1 19980515 A 5720 5641253501 DOUBLER DOUG DOUG DC8 DC863F 302198F WP WS 372.75-379 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 RIGHT WING LEADING EDGE LOWER SKIN DOUBLER FORWARD EDGE BETWEEN STATION XFS 372.75 AND XF 379.0 HAS HEAVY EXFOLIATION CO RROSION. REPAIRED IAW DC8 SRM 51-3-0 AND DWG 5641253. 2 L 7 4 4F 4A25 1998071400044 19980714 00044 WP 1998 7 14 ABXA9800596 1 19980513 A 5320 4751643 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 717 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 AFT END FITTING ON LONGERON INTERCOSTAL AT STATION 717, LONGERON 14L IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998071400045 19980714 00045 WP 1998 7 14 ABXA9800597 1 19980630 A 5313 262218 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1230 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 AFT LOWER CARGO COMPARTMENT STATION 1230, LONGERON 29L INSIDE TORQUE BOX, WEB CORRODED. REPAIRED IAW ABX REA D853-23409 MR REV-A, 2 L 7 4 4F 4A25 1998071400046 19980714 00046 WP 1998 7 14 ABXA9800598 1 19980630 A 5320 3779659501 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 900 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 MAIN CABIN, LONGERON END FITTING AT STATION 900 LONGERON 8R CRACKED. REPAIRED IAW DC8 SRM 51-3-2 AND 51-1-20D. 2 L 7 4 4F 4A25 1998071400047 19980714 00047 WP 1998 7 14 ABXA9800599 1 19980630 A 5341 37048411 FITTING DOUG DOUG DC8 DC861 3021952 WP WS 74 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 STRINGER END FITTING CRACKED AFT SIDE OF STRINGER NR 51 OUTBOARD IN NR 2 MAIN TANK AT STATION 74.000. REPAIRED IAW DC8 SRM 51-1-24 AND 51-1-20D. 2 L 7 4 4F 4A25 1998071400048 19980714 00048 WP 1998 7 14 ABXA9800600 1 19980630 A 5720 3704841502 FITTING DOUG DOUG DC8 DC861 3021952 WP WS 74 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 CRACK IN LOWER NR 2 MAIN TANK JUST INBOARD OF XRS 74 STRINGER NR 51 ON FWD AND AFT SIDE OF SPLICE. REPAIRED TWO CRACKED FITTINGS IAW DC8 SRM'S 51-1-24, 51-1-8, AND 51-1-20D. 2 L 7 4 4F 4A25 1998071400049 19980714 00049 NM 1998 7 14 SCNA98068 1 19980624 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE MIDDLE OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998071400050 19980714 00050 NM 1998 7 14 VNAA9806018 1 19980629 A 7921 30VR1107 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT NACELLE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 430JS 77414 3044 A HIGH OIL TEMPERATURE WARNING MESSAGE OCCURED FOR THE RIGHT HAND ENGINE, DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RET URNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND OIL COOLER DOOR THERMAL VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 79-32-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998071400051 19980714 00051 1998 7 14 VNAA9806019 4 19980630 A 3418 AOA DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E COMPT TRIPPED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 442JS 3060 DURING TAKEOFF, A STICK PUSHER, SHAKER AND AOA FAIL WARNING MESSAGE OCCURED. THE AIRCRAFT ABORTED THE TAKEOFF AND RETUR NED TO THE GATE. MAINTENANCE INSPECTED AND RESET THE STALL WARNING SYSTEM, AND PERFORMED OPERATION CHECKS, IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 23-33-00. THE CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998071400052 19980714 00052 1998 7 14 CA980325011 4 19980324 A 3460 350E5151022 CONCENTRATOR AIRBUS 320 A320211 3930320 EU SDAC FAILED W A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 CA 19987 (CAN) AIRCRAFT RETURNED TO DEPARTURE TERMINAL DUE TO LOSS OF 6 PRIMARY FLIGHT DISPLAYS (CDU'S). SYSTEM DATA ACQUISITON CONCENTRATOR (SDCU) REPLACED. LOSS OF CDU'S WAS DUE TO MEL APPLIED THAT ALLOWED ALL CDU'S TO BE POWERED FROM NR 1 BUS. MEL WAS APPLIED BECAUSE OF DMC NR 2 PROBLEM. AIRBUS NOTIFIED OF MEL DISCREPANCY. CAIL SUGGESTED PROCEDURAL CHANGE TO SELECT ACCESS FEED PB TO ALTERNATE IS UNDER REVIEW BY AIRBUS. ALSO SUGGESTED OPERATIONAL PROCEDURAL CHANGE TO MMEL IN T HE EVENT OF AC BUS NR 1 FAILURE WHEN OPERATING WITH DMC 2. PART TC: 7,514. 2 L 7 2 4F RT A28NM 1998071400056 19980714 00056 NM 1998 7 14 CA980331010 1 19980324 A 3260 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT MLG FAILED W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA 120458 (CAN) ON SHORT FINAL, RIGHT MAIN GEAR UNSAFE LIGHT, GEAR HANDLE LIGHT AND GEAR WARNING SOUNDED. LIGHT CYCLED BACK AND F ORTH FROM GREEN TO RED. ALTERNATE EXTENSION CARRIED OUT. LANDING OK. RIGHT HAND DOWNLOCK SENSOR REPLACED ALONG WITH WIRING HARNESS. 2 H 7 2 4T 4 T RT A13NM E20NE 1998071400057 19980714 00057 NM 1998 7 14 CA980331011 1 19980324 A 5230 85230448001 LINK ASSEMBLY 85230400001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CARGO DOOR SPLIT W K NONE O OTHER IN INSP/MAINT 1 CA 20951 0010201 120370 (CAN) CARGO DOOR WOULD NOT CLOSE. INSPECTION FOUND LINK ASSY SPLIT IN HALF AROUND THE LOWER BEARING. PART TC: 17,765. 2 H 7 2 4T 4 T RT A13NM E20NE 1998071400058 19980714 00058 EA 1998 7 14 CA980331013 1 19980327 A 2460 ANL500 CURRENT LIMITER CNDAIR CL600 CL6002A12 1900304 EA GE CF34 CF341A NE BUS BAR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 350146 (CAN) FOLLOWING INCIDENT ON ANOTHER AIRCRAFT VISUAL INSPECTION OF CURRENT LIMITER TO BUS BAR FOUND THAT THE ALUMINUM WAS HERS UNDER THE HEAD OF THE BOLT WERE STARTING TO BURN AWAY. CANADAIR INFORMED. IPC WILL BE UPDATED AND OPERATORS WILL BE INFORMED OF DIFFICULTIES. 2 L 7 2 4F 4 F RT A21EA E15NE 1998071400059 19980714 00059 EU 1998 7 14 CA980331018 1 19980323 A 5720 S5711124120001 BRACKET AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE LT WING SPAR BURNT W K NONE O OTHER IN INSP/MAINT 1 CA 19955 120504 890205 (CAN) ON ATTEMPT TO START NR 1 ENGINE, THERE WAS NO ROTATION. THE SUPPORT BRACKET WHICH WAS USED FOR THE STARTER/GENERA TOR GROUND LEAD WAS FOUND BURNED THROUGH. IT WAS BURNED AT THE HI-LOCKS AND WAS LOOSE. INCIDENT REPORTED TO ATR SUPPOR T FOR FURTHER INVESTIGATION. PART TC: 26,773. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1998071400060 19980714 00060 NM 1998 7 14 CA980331022 1 19980317 A 2770 82700559001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PULLEY FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 30780 120383 (CAN) FLIGHT CREW ADVISED OF HAVING DIFFICULTIES ENGAGING FLIGHT CONTROL LOCK. CONTROL LOCK CABLE FOUND FRAYED AT THE RE AR QUADRANT PULLEY. PULLEY P/N MS20219-4. PART TC: 35,461. 2 H 7 2 4T 4 T RT A13NM E20NE 1998071400064 19980714 00064 EU 1998 7 14 CA980415024 1 19980408 A 3210 201107608 PIN DOWTY BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG CRACK W K NONE O OTHER IN INSP/MAINT 1 CA 1465 RXN78197 LFO5653A (CAN) MLG SHOCK ABSORBER PIN INSPECTED AS A RESULT OF PREVIOUS FIND. IMPERFECTION FOUND IN PIN USING ULTRASONIC. SEE S DR19980402024 ALSO. PART TC: 17,996. 2 H 7 4 4F 4 F RT A49EU E6NE 1998071400065 19980714 00065 NM 1998 7 14 CA980521013 1 19980511 A 3213 101251 TORQUE LINK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT/LT MLG MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 120387 (CAN) ON WALKAROUND, BOTH TORQUE LINKS WERE FOUND DAMAGED. THE UPPER TORQUE LINK WAS BENT AND DENTED. THE LOWER WAS ALS O DENTED. SUBMITTER SAYS THAT THE LOWER TORQUE LINK WAS INSTALLED UPSIDE DOWN. GEOMETRY OF TORQUE LINK UPSIDE DOWN CA USED DAMAGE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998071400066 19980714 00066 NM 1998 7 14 CA980521014 1 19980511 A 3213 101251 TORQUE LINK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT/LT MLG MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 120387 (CAN) ON WALKAROUND, BOTH TORQUE LINKS WERE FOUND DAMAGED. THE UPPER TORQUE LINK WAS BENT AND DENTED. THE LOWER WAS ALS O DENTED. SUBMITTER SAYS THAT THE LOWER TORQUE LINK WAS INSTALLED UPSIDE DOWN. GEOMETRY OF TORQUE LINK UPSIDE DOWN CA USED DAMAGE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998071400068 19980714 00068 WP 1998 7 14 VJ9800211 1 19980630 A 5330 3913209IN SKIN DOUG DC9 DC932 3022066 WP BS 560 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 931VV 47674 INTERNAL SKIN UNDER AUX PUMP AT STA 560, LONGERON 29L TO 29R, CORRODED. REMOVED LONGERON END CAPS FROM 25L TO 25R. REM OVED EXISTING REPAIR, INTERNAL DOUBLERS, TRIMMED OUT CORRODED AREA AND FABRICATED REPAIR DOUBLER FROM 2024T3 .80 MATERIA L, DRILLED, DEBURRED. ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER AND 5 EACH END CAPS IAW AERO EO NR 98-900 AND AIRTRA N RES NR 98985 AND DC9 SRM 51-10-4, 51-10-3, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998071400069 19980714 00069 WP 1998 7 14 VJ9800212 1 19980704 A 3350 60030431 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 933VV 47489 FWD AFT CABIN OVERHEAD EMERGENCY LIGHTS INOP. REPLACED BATTERIES; OPS CHECKED GOOD IAW MM 33-00. 2 L 7 2 4F A6WE 1998071400070 19980714 00070 WP 1998 7 14 VJ9800213 1 19980704 A 5610 5613217519 WINDOW DOUG DC9 DC932 3022066 WP LT COCKPIT OUT OF ADJUST A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 CAPTAIN'S SLIDING WINDOW JAMMED; WON'T OPEN. REINSTALLED UPPER HINGE IAW MM 56-10. OPS CHECKS GOOD. 2 L 7 2 4F A6WE 1998071400071 19980714 00071 NM 1998 7 14 AWXA9800146 1 19980618 A 5330 SKIN BOEING 737 737297 1384480 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 147AW 22630 D-FUSELAGE CRACK AT STA 727 NEAR STRINGER 17 RT SIDE C-CONFIRMED BY HFEC AND REPAIRED PER SRM 53-30-03 FIG 1. 2 L 7 2 4F A16WE 1998071400072 19980714 00072 NM 1998 7 14 AWXA9800147 1 19980621 A 3350 BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 D-ROW 1-6 EMERGENCY LIGHTS INOP. RESEATED BATTERY PACK IN RECHARER UNIT. OPS OK. 2 L 7 2 4F RT A16WE 1998071400073 19980714 00073 NM 1998 7 14 RAAA98B1083 1 19980630 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 MID CABIN DOOR EMERGENCY EXIT LIGHT WILL NOT TEST. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998071400074 19980714 00074 SO 1998 7 14 RAAA98E8021 1 19980702 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT EMERGENCY EXIT IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998071400075 19980714 00075 WP 1998 7 14 CALA9801204 1 19980703 A 2910 FITTING DOUG DC9 DC982 3022082 WP BRAKE METER VLV LOOSE A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 34838 49634 THE RT HYDRAULIC PUMP PRESSURE DROPPED TO ZERO FOLLOWED BY THE RT HYDRAULIC SYSTEM QUANTITY DROPPING TO ZERO WHILE EN RO UTE FROM EWR TO MCO. EMERGENCY GEAR EXTENSION WAS USED ON APPROAH TO MCO AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAI NTENANCE FOUND HYDRAULIC LINE AND FITTING LOOSE AT BRAKE METERING VALVE. THE FITTING WAS TIGHTENED AND LEAK CHECKS WERE GOOD. IN ADDITION, THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F A6WE 1998071400076 19980714 00076 WP 1998 7 14 CALA9801205 1 19980706 A 4900 38102621 APU GARRETT DOUG DC10 DC1010 3022110 WP AFT FUSELAGE MALFUNCTIONED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 68041 30903 46900 THE AIRCRAFT HAD A BRIEF HISTORY OF SMOKE APPEARING IN THE COCKPIT AND CABIN MOMENTARILY WHILE IN FLIGHT. THE SMOKE DIS SIPATED QUICKLY ONCE THE EFFECTED PACK WAS TURNED OFF. THE APU WAS REMOVED AND REPLACED IAW MM 49-00-00, PAGES 401-415. OPERATIONAL CHECKS WERE GOOD WITH NO SMOKE DETECTED. 2 L 7 3 4F A22WE 1998071400077 19980714 00077 WP 1998 7 14 CALA9801206 1 19980702 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 960-965 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND CABIN FLOOR PANEL CORRODED AND PUNCTURED AT STA 960-965, BL 0 TO RBL 21.5. A NEW FLOOR PANEL WAS FABRI CATED AND INSTALLED IAW SRM 51-70-1 AND 53-05, PAGE 122B. 2 L 7 2 4F A6WE 1998071400078 19980714 00078 WP 1998 7 14 CALA9801207 1 19980702 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 560 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1.25 CRACK IN FUSELAGE SKIN AT STA 560, STRINGER 18L. THE CRACKED SKIN WAS REMOVED AND A DOUBLER REP AIR WAS INSTALLED IAW ECRA 5330-02481. 2 L 7 2 4F A6WE 1998071400079 19980714 00079 WP 1998 7 14 CALA9801209 1 19980703 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 313 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 2 INCH CRACK EXTENDING FROM RADIUS TO FASTENER HOLE IN CABIN FLOOR SUPPORT AT STA 3113, BL 0. THE CR ACK WAS STOP DRILLED. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4, 51-10-3, AND 51-30 -2. 2 L 7 2 4F A6WE 1998071400080 19980714 00080 WP 1998 7 14 CALA9801210 1 19980705 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 935 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1 CRACK IN FUSELAGE SKIN AT STA 935, LONGERON 25R, AFT OF CARGO DOOR OPENING. THE CRACKED AREA WAS R EMOVED IAW SRM 53-05, FIGURE 80. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 53-05, FIGURE 80, 51-10-3, 51- 30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998071400081 19980714 00081 NM 1998 7 14 9809716719 1 19980628 A 3232 1U11985 ACTUATOR BOEING 747 747251F 1384898 NM NLG DOOR LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 619US 59024 50205 21321 DURING CLIMB, THE NR 1 HYDRAULIC SYSTEM FAILED AND THE NOSE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED. AIRCRAFT RETURNED TO ANC AND LANDED WITHOUT INCIDENT. REPLACED THE NOSE LANDING GEAR DOOR ACTUATOR. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998071400082 19980714 00082 NE 1998 7 14 9809726624 2 19980627 A 7230 COMPRESSOR BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 4 ENGINE STALLED A NWAA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL Y ENGINE STOPPAGE CL CLIMB 1 GL 01 624US 21706 702176 WHILE CLIMBING THROUGH 1400 FEET AGL, THE NR 4 ENGINE AUDIBLY COMPRESSOR STALLED AND FLAMED OUT. THE CREW SECURED THE E NGINE, DUMPED FUEL, RETURNED TO MSP, AND LANDED WITHOUT INCIDENT. THE NR 4 ENGINE WAS CHANGED. EXACT PART CAUSING PROB LEM TO BE DETERMINED. 2 L 7 4 4F 4 F A20WE E3NE 1998071400083 19980714 00083 SO 1998 7 14 COMA9810152 1 19980705 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 248CA 20359 1322 120228 EMERGENCY EXIT LIGHTS INOP AT ROW 4 AND 5. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998071400084 19980714 00084 EA 1998 7 14 COMA9860166 1 19980702 A 3080 DETECTOR CNDAIR CL600 CL6002B19 EA NR 2 MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 975CA 7150 NR 2 ICE DETECTOR FAIL WARNING. COULD NOT DUPLICATE DISCREPANCY. NO FAULTS FOUND WITH ICE DETECTOR SYSTEM. 2 L 7 2 4F RT A21EA 1998071400085 19980714 00085 SO 1998 7 14 SWIA971209 1 19980608 A 3260 PROX SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 562SW 120336 AFTER TAKEOFF, UPON GEAR RETRACTION, NOSE GEAR INDICATED 1 GREEN LIGHT B AND ONE RED LIGHT A. RETURNED TO PSP. REPLACE D NOSE B GEAR DOWN LOWER PROXIMITY SENSOR AND HARNESS. SET GAP, SAFTIED AND PERFORMED NUMEROUS GEAR SWINGS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998071400086 19980714 00086 EA 1998 7 14 SWIA971210 1 19980608 A 5270 SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE SERVICE DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 406SW 7030 SERVICE DOOR CAUTION MESSAGE IN FLIGHT. RETURNED TO FIELD. FOUND DOOR CLOSED, MICROSWITCH SLIGHTLY OUT OF ADJUSTMENT A ND DOOR SEAL FLANGE BENT. CONFIRM DOOR CLOSED, MEL 52-70-5. 2 L 7 2 4F 4 F RT A21EA E15NE 1998071400087 19980714 00087 EA 1998 7 14 SWIA971211 1 19980608 A 3230 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG FAILED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 408SW 7055 NOSE GEAR DISAGREE AND WOULD NOT EXTEND. USED EMERGENCY GEAR EXTENSION. UPON LANDING, NO NOSE WHEEL STEERING. SYSTEM NR 3 HYDRAULIC PRESSURE 2400 PSI MAXIMUM. REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW MM 32-31-00. CYCLED GEAR AND T AXIED AIRCRAFT. OPS CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1998071400088 19980714 00088 SO 1998 7 14 SWIA971212 1 19980608 A 5230 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 233SW 120307 CARGO DOOR SEAL BLEW OUT IN FLIGHT. RETURNED TO SFO. REPAIRED CARGO DOOR SEAL AT BOTTOM AFT. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998071400089 19980714 00089 NM 1998 7 14 UPS98227095 1 19980630 A 5311 FRAME BOEING 727 72730C 1384009 NM BS 294 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-221-01.00-01) ON FRAME AT STA 294 LBL 57 WL 236-239. REMOVED CORROSION FOUND OUT OF L IMITS, FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998071400090 19980714 00090 NM 1998 7 14 UPS98227096 1 19980618 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT FASTENER HOLE BS 312, LBL 3, WL 208. COR ROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8, 51-30-5, 51-30-2 AND MM 51-20-151. 2 L 7 3 4F A3WE 1998071400091 19980714 00091 NM 1998 7 14 UPS98227097 1 19980617 A 5320 69144925 SPLICE BOEING 727 72730C 1384009 NM BS 443 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 25R SPLICE AT BS 443. CORROSION FOUND TO BE OUT OF LIMITS PER SR M 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-5, 51-30-2 AND MM 51-30-00. 2 L 7 3 4F A3WE 1998071400092 19980714 00092 NM 1998 7 14 UPS98227098 1 19980617 A 5320 69144925 SPLICE BOEING 727 72730C 1384009 NM BS 436 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 25L SPLICE AT BS 442, BS 436. CORROSION FOUND TO BE OUT OF LIMIT S PER SRM 53-10-1, INSTALLED NEW SPLICE PER SRM 51-30-2, 51-30-5 AND SRM 51-30-6. 2 L 7 3 4F A3WE 1998071400093 19980714 00093 NM 1998 7 14 UPS98227099 1 19980618 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 328 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT BS 328 LBL 45. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. REMOVED DAMAGE FROM BEAM AND INSTALLED STANDARD REPAIR PER SRM 53-10-8, 53-10-2 AND 51-30-2 . 2 L 7 3 4F A3WE 1998071400094 19980714 00094 NM 1998 7 14 UPS98227100 1 19980626 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 474 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 24F BS 474. REPLACED STRINGER FROM BS 470 TO BS 490. INSTALLED STRINGER SECTION AND SPLICE PLATES PER 727 SRM 53-10-1, 53-10-3. 2 L 7 3 4F A3WE 1998071400095 19980714 00095 NM 1998 7 14 UPS98227101 1 19980618 A 2730 652791713 BALANCE PANEL BOEING 727 72722C 138400F NM LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE:C SURFACE CORROSION ON NR 5 BALANCE PANLE LT STAB. BALANCE PANEL REMOVED AND REPLACED IAW MM 27-30-21. 2 L 7 3 4F A3WE 1998071400096 19980714 00096 NM 1998 7 14 UPS98227102 1 19980630 A 2910 LINE BOEING 727 72751C 1384015 NM HYD BAY FAILED A IPXA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 903UP 18945 LOST HYD B SYSTEM FLUID WHILE SITTING ON TAXIWAY B HOLDING POSITION SHORT OF RUNWAY 20 AT SGF NR 1 B PUMP LOW PRESURE LI GHT FLICKERED; CAME ON STEADY, FOLLOWED QUICKLY BY NR 2 B PUMP LOW PRESSURE LIGHT ILLUMINATED STEADY. DETERMINED B SYST EM PRESSURE LINE IN HYDRAULIC BAY RUPTURED AT B-NUT. REPLACED LINE IAW MM PRESSURIZED SYSTEM. OPS CKS NORMAL. 2 L 7 3 4F A3WE 1998071400097 19980714 00097 WP 1998 7 14 UPS98827103 1 19980701 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 802UP 46100 EMERG LIGHTING BATTERY PACK DIMS LIGHTS WHEN ACTIVATED. REMOVED AND REPLACED BATT PACK FOR EEL PER M-M 33-50-01. OP'S CHECK GOOD. 2 L 7 4 4F RT 4A25 1998071400098 19980714 00098 NM 1998 7 14 QXEA9800835 1 19980701 A 2611 473054 SMOKE DETECTOR DHAV 82522710001 DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTION A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 361PH 222 516 RDM- SMOKE WARNING MASTER WARNING ILLUMINATED IN FLIGHT. NO EVIDENCE OF FIRE NOTED. ACCOMPLISHED UNEVENTFUL LANDING. P LACED ON MEL. MEL CLEARED IN SEA BY REPLACING THE NR 2 SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998071400099 19980714 00099 NM 1998 7 14 98FDEA00426 1 19980702 A 2150 VALVE BOEING 727 72722 1384002 NM LT PACK OVERHEAT A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 181FE 18868 98-0164 - STA-AFW - IN CRUISE FLIGHT LEVEL 250 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. AFTER OPENING NR 1 BLEED VALV E AND CLOSING THE LEFT NR 2 BLEED VALVE LIGHT EXTINGUISHED AFTER ABOUT 1 MINUTE. NO ANTI-ICE WAS USED. REMOVED AND RE PLACED LEFT PACK VALVE REFERENCE PER MAINTENANCE MANUAL 21-51-61. OPERATIONAL AND LEAK CHECK NORMAL. 2 L 7 3 4F A3WE 1998071400100 19980714 00100 NM 1998 7 14 98FDEA00427 1 19980702 A 3610 BLEED LINE BOEING 727 72722 1384002 NM NR 2 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 181FE 18868 98-0165 STA-FLL: LWR AFT BODY OVERHEAT LIGHT ILLUM PASSING FLT LEVEL 20. THE LIGHT EXTINGUISHED 3 MIN AFTER CLOSING NR 1 ENG BLEED AND THE LEFT PACK AS DIRECTED IN CHECKLIST. THE INITIAL CONFIGURATION WHEN THE LIGHT ILLUM WAS BOTH PACKS ON NR 1 AND RIGHT NR 2 BLEED VALVES CLOSED. LEFT NR 2 AND NR 3 BLDS OPEN. FOUND MINOR LEAK ON CLAMP ON LEFT DUCT NR 2 BLD ALSO FOUND TAP OFF BLD LINE FROM NR 2 BLD NOT SECURED AND TOUCHING OVERHEAT ELEMENT. RESECURED LINE AND REPOSITION ELEMENT. CLAMPS LOOSE ON LEFT NR 2 BLD VALVE, TIGHTENED. RAN ENG. CHECKED FOR LEAKS. NONE FOUND. OKAY FOR SERVICE. 2 L 7 3 4F A3WE 1998071400101 19980714 00101 NM 1998 7 14 98FDEA00428 1 19980702 A 2120 AIR DISTRIBUTION BOEING 727 727227 1384078 NM COCKPIT ODOR A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 25 484FE 21466 98-0166 STA-IND: SMOKE FUMES IN COCKPIT AT GEAR CONFIGURATION. SMOKE EMANATED INTO COCKPIT. SMOKE AND FUMES CHECKLIST RUN SMOKE NOTED IN COCKPIT AROMA LIKE WOOD BURNING. GASPER FAN SECURED. SMOKE MAY HAVE DECREASED. AIRCRAFT STOPPED A ND EMERGENCY EQUIP RESPONDED. AIRCRAFT INSP BY FIRE DEPT, FAA OFFICIALS AND LINE AIRCRAFT MAINTENANCE NO SOURCE FOUND. SUSPECT AIRCRAFT FLEW THROUGH A HEAVY SMOKE AREA DUE TO HEAVY BURNING IN AREA BECAUSE OF THUNDER STORM THE DAY BEFORE 6 /30/98. ALL AIRCRAFT SYSTEMS WORKING NORMALLY. 2 L 7 3 4F A3WE 1998071400102 19980714 00102 WP 1998 7 14 98FDEA00429 1 19980628 A 2910 HYDRAULIC SYS DOUG DC10 DC1030F 3023504 WP NR 2 HIGH TEMP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 315FE 48313 98-0167 STA-DXB: DURING TAXI OUT HYD SYS NR 2 READ 50-50 DEG AFTER APPROX 8 MIN OF FLT TEMP NR 2 HAD INCREASE TO 60 DEG TMP SHORTLY INCREASE TO 70 DEG RED TABS REFER TO ND TEMP INCREASE WITHIN 5 MIN TO 90 CONT RED TAB PROC WITH NR 2 SYS SH UT DOWN. WHEN TMP APPROX 98 DEG RT TEMP HI LITE FLICKER CONT 728 REMAIN OUT. ALL LITE TEST OK. TEMP PASS 100 DEG ND C ONT TO 105 WITHIN 30 MIN DURING DESCENT TEMP DIMINISH TO BELOW 100. ON FINAL APPROACH WITH ALL SYS SWITCH ON/ARMED TEMP DIMINISH TO 80 DEG THAN FURTHER TO 57 DEG DURING TAXI. OPEN ND CLOSE NR 2 FAN COWL AND WORK PLATE FORM LOCKS CK OK. H YD RESERVOIR SYS 2 REMOVED AND NEW RESERVOIR INSTALL. ENG NR 2 TEST RUN FOR TO CK HYD TEMP FND WITHIN LIMIT, CK FOR LE 2 L 7 3 4F RT A22WE 1998071400103 19980714 00103 EU 1998 7 14 98FDEA00430 1 19980701 A 2150 PACK AIRBUS 310 A310203 EU NR 2 OVERHEAT A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 430FE 394 STA-BOI - NR 2 PACK OVERHEAT WITHIN MAIN DECK CARGO SMOKE AND FIRE BELL WARNING. C/W BITE TEST ON PNEUMATIC CONTROLLER, PACK CONTROLLERS, ZONE CONTROLLERS, CARGO SMOKE DET CONTROLLERS. NO FAULTS FOUND. CLEANED AND INSPECTED WATER SEPARAT OR SOCK. FOUND OK FOR REUSE PER AMM 21-51-16. SYSTEMS ALL CHECK GOOD. SUSPECT RELATED TO HIGH AMBIENT TEMP ON GROUND. OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1998071400104 19980714 00104 NM 1998 7 14 98FDEA00431 1 19980703 A 2910 LINE DOUG MD11 MD11F 3023600 NM NR 1 HYD SYST LEAKING A FDEA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 587FE 48489 98-0169 - STA-HKG - APPROX 1.5 HR INTO FLT HYD 1 OFF LEVEL 2 ALERT ILLUMINATED WITH HYD 1 RESERVOIR INDICATING 2.8 GAL RESERVOIR QTY CONT TO DROP UNTIL HYD 1 FAIL LEVEL 2 ALERT ILLUM WITH QUAN INDICATING 1 GAL RESERVOIR CONT DECREASE UNTIL REACH ZERO. ON ARRIVAL FND HYD LEAK AT NR 1 ENG RT HYD PUMP CASE DRAIN LINE FAB LINE PER M/M SUP 20-10-01. REPLACED S AME LEAKS CKD OK SERV NR 1 HYD SYS QTY. NR 1 ENG HYD PUMPS OPS AND INDS CKD OK CKD NR 1 HYD MANIFOLD FILTERS, NO CONTAM INATION CKD POP OUT INDICATORS AND ALL STAYED IN. 2 L 7 3 4F RT A22WE 1998071400105 19980714 00105 WP 1998 7 14 98FDEA00432 1 19980703 A 2730 210005007 ACTUATOR DOUG DC10 DC1010F 3022111 WP RT ELEVATOR DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 SNRM N00048 STS-LAX: Rt I/B ELEVATOR ACTUATOR. X-RAY FILM EXHIBITS IRREGULAR GEOMETRIC PATTERNS OF DIFFERENT DENSITIES THROUGHOUT PISTON WALL (PRIMARY PATH). REMOVED AND REPLACED RT INBD ELEVATOR ACTUATOR. CLOSED 7/16/98. 2 L 7 3 4F A22WE 1998071400106 19980714 00106 WP 1998 7 14 98FDEA00433 1 19980703 A 7110 COWL DOUG DC10 DC1010F 3022111 WP NR 2 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 STA-LAX NR 2 ENGINE NOSE COWL INLET L/E HAD A 25 INCH CRACK AT 2:30 O'CLOCK POSITION. *S/D* REMOVED AND REPLACED NOSE COWL PER M/M 54-22-01-2. 2 L 7 3 4F A22WE 1998071400107 19980714 00107 WP 1998 7 14 98FDEA00434 1 19980702 A 5230 SEAL DOUG DC10 DC1010F 3022111 WP CARGO DOOR OUT OF POSITION A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 051FE 47805 98-170 - STA:EWR - DEPART EWR A/C DID NOT PRESSURIZE. RAN RED TABS NO HELP. RETURNED EWR. INDICATIONS OUT VALVE CLOSE D ALL PACKS OPS NORMAL. UPON WALK AROUND FOUND 18 INCH OF DOOR SEAL OUT OF FWD CARGO DOOR (LWR FWD CORNER). REINSTALLE D SAME. INSPECTED ALL DOORS ETC FOR SECURITY. PRESSURIZED A/C CABIN TO 3 PSID. ALL INDS WERE NORMAL. 2 L 7 3 4F A22WE 1998071400108 19980714 00108 NM 1998 7 14 VNAA9806020 1 19980629 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE DIRTY A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 436JS 3052 DURING THE TAXI FOR TAKEOFF, THE RIGHT HAND PROPELLER OVERSPEED TEST, FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RET URNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND CLEANED THE RIGHT HAND PROPELLER OVERSPEED GOVERNOR CANNON PLUG , IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-04. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998071400109 19980714 00109 NM 1998 7 14 VNAA9807002 1 19980701 A 2611 SD9422A0A0 SMOKE DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AFT LAV DAMAGED A VNAA O OTHER N FALSE WARNING CR CRUISE 1 GL 07 439JS 67911 3665 3057 EN ROUTE TO PIT, A SMOKE DETECT FAIL WARNING MESSAGE ILLUMINATED. A PASSENGER WAS EXITING THE RESTROOM, AND THE FLIGHT ATTENDANT NOTICED THAT THE SMOKE DETECTOR HAD BEEN TAMPERED WITH. THE AIRCRAFT CONTINUED ON TO PIT AND LANDED. THE PAS SENGER WAS DETAINED BY AIRPORT SECURITY. MAINTENANCE CONFIRMED THE TAMPERED CONDITION OF THE SMOKE DETECTOR, AND REPLAC ED IT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-15-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998071400110 19980714 00110 NM 1998 7 14 CKSA98354 1 19980630 A 5330 SKIN BOEING 747 747132 1384882 NM BS 1920 GOUGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE C CHECK INSPECTION FOUND: SEVERAL GOUGES IN FUSELAGE SKIN AT AFT LOWER CORNER OF C-2 DOOR CUT-OUT BS1920 . REMOVED FASTENERS AND BLENDED AREA IAW B747 SRM 51-30-2. C/W OPEN HOLE HFEC OF 3 FASTENER HOLE AND SURFACE PERIFERY OF BLEND-OUT AREA IAW 51-00-00 NDT MANUAL PART 6 AS OUTLINED IN BOEING PROPOSAL REPAIR NO CRACK INDICATIONS. TREATED AN D PRIMED IAW B747 MM 51-21-00. INSTALLED REPAIR IAW AIA EDR NBR B-453-047. C CHECK WORK CARD NUMBER 7EK7472. NON-ROUT INE TASK CARD NUMBER 24843. 2 L 7 4 4F A20WE 1998071400111 19980714 00111 NM 1998 7 14 CKSA98355 1 19980630 A 5230 SKIN BOEING 747 747132 1384882 NM CARGO DOOR CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION FOUND: C-2 DOOR OUTER SKIN IS DENTED AND HAS 2 EA 1 CRACKS AT BOTTOM EDGE BETWEEN BS 184 0 AND BS 1860. DAMAGED FOUND TO BE OUT OF LIMITS IAW B747 SRM 52-00-2. REPAIR DOOR SKIN IAW B747 SRM 52-00-03 FIG 3. I NSTALLED REPAIR IAW B747 SRM 52-00-03 FIG 3. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 24844 . 2 L 7 4 4F A20WE 1998071400112 19980714 00112 NM 1998 7 14 CKSA98356 1 19980630 A 5730 SKIN BOEING 747 747132 1384882 NM BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: FS1200 RBL95 CNTR WING SKIN HAS CORROSION. REMOVED CORROSION I AW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 57-10-01. INSTALLED REPAIR IAW AIA EA B4-57-051. C/W OPE N HOLE HFEC AND SURFACE HFEC IAW B747 NDT MANUAL PART 6 51-00-00 NO CRACKS. CORROSION TASK CARD NUMBER C53-210-05. NON -ROUTINE TASK CARD NUMBER 24935. 2 L 7 4 4F A20WE 1998071400113 19980714 00113 NM 1998 7 14 CKSA98357 1 19980630 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1060 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND AT BS1060, FROM BOTTOM CENTERLINE TO LBL50, PANEL SUPPORT FRAME WITH CORROSION ARO UND ANCHOR NUTS AND FASTENERS. REMOVED DAMAGED T-CHORD, FAB NEW PER SRM 51-10-01. FAB REPAIR ANGLES PER SRM 51-40-02. INSTALLED REPAIR ANGLES AND T-CHORD IAW SRM 51-40-04 FIGURE 1. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TAS K CARD NUMBER 25139. 2 L 7 4 4F A20WE 1998071400114 19980714 00114 NM 1998 7 14 CKSA98358 1 19980630 A 5311 FRAME BOEING 747 747132 1384882 NM BS 920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND BS920, FROM BOTTOM CENTERLINE TO BOTH RT AND LEFT BL50, PANEL SUPPORT FRAME CORROD ED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REPAIR FRAME IAW B747 S RM 53-50-04 AND AIA EDR NR B-4-05860. INSTALLED REPAIR IAW B747 SRM 53-50-04 AND AIA EDR NBR B-4-05860. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 25142. 2 L 7 4 4F A20WE 1998071400115 19980714 00115 NM 1998 7 14 CKSA98359 1 19980630 A 5311 FRAME BOEING 747 747132 1384882 NM BS 980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION BS980, RBL50, PANEL SUPPORT FRAME CORRODED. REMOVED CORROSION I AW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REPAIR FRAME FLANGE IAW B747 SRM 53-50-04. INS TALLED REPAIR IAW B747 SRM 53-50-04. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 25167. 2 L 7 4 4F A20WE 1998071400116 19980714 00116 NM 1998 7 14 CKSA98360 1 19980630 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1080 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND FS1080 LBL90 OUTBD SIDE WEB ATTACH ANGLE CRACKED. FAB NEW ATTACH ANGLE 7075-T6. I NSTALLED ATTACH ANGLE IAW B747 SRM 51-30-02. CORROSION TASK CARD NUMBER C53-210-05. NON-ROUTINE TASK CARD NUMBER 25171 . 2 L 7 4 4F A20WE 1998071400117 19980714 00117 NM 1998 7 14 CKSA98361 1 19980630 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1000 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND FS1000 LBL 30 FRONT SPAR FLOOR SUPPORT ATTACH ANGLE CRACKED. REMOVED FLOOR SUPPOR T. REWORKED FITTINGS IAW EDR B4-05869 DTD 6-2-98. INSTALLED FITTINGS IAW B747 SRM 51-30-02 AND EDR B4-05885 DTD 6-9-98 . CORROSION TASK CARD NUMBER C53-210-05. NON-ROUTINE TASK CARD NUMBER 25173. 2 L 7 4 4F A20WE 1998071400118 19980714 00118 NM 1998 7 14 CKSA98362 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 480 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION 2 AREA OF CORROSION ON BS480 FLOOR BEAM FWD, UPPER, SIDE AT RBL- 76. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBL ERS IAW B747 SRM 51-40-04 FIG 1. INSTALLED REPAIR DOUBLERS IAW B747 SRM 51-40-04 FIG 1. CORROSION TASK CARD NUMBER C53 -210-07. NON-ROUTINE TASK CARD NUMBER 25182. 2 L 7 4 4F A20WE 1998071400119 19980714 00119 NM 1998 7 14 CKSA98363 1 19980630 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 520 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND 1 AREA OF CORROSION ON BOTTOM OF RBL11.33 SEAT TRACK FWD OF BS 520. REMOVED CORRO SION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED SEAT TRACK IAW B747 SRM 51-30-02. INSTALLED NEW SEAT TRACK SECTION IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUT INE TASK CARD NUMBER 25187. 2 L 7 4 4F A20WE 1998071400120 19980714 00120 NM 1998 7 14 CKSA98364 1 19980630 A 5321 FLOOR BOEING 747 747132 1384882 NM BS 860-880 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND FLOOR HAS CORROSION BETWEEN STA 860 AND STA 880 RBL 98 BOTTOM SIDE. REMOVED FLOOR PANEL CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-20-00 FIG 2. MADE NEW FLOOR PANEL IAW B747 SRM 53-20-01. IN STALLED FLOOR PANEL IAW B747 SRM 51-30-2. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 25194. 2 L 7 4 4F A20WE 1998071400121 19980714 00121 NM 1998 7 14 CKSA98365 1 19980630 A 5320 FITTING BOEING 747 747132 1384882 NM BS 760 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA 760 AFT, LBL 79 FLOORBEAM ANGLE HAS CORROSION. REMOVED FITT ING IAW B747 SRM 51-30-2. REPLACED FITTING IAW 51-30-2 AND 51-10-1. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTIN E TASK CARD NUMBER 25204. 2 L 7 4 4F A20WE 1998071400122 19980714 00122 NM 1998 7 14 CKSA98366 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 760 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION STA760 FWD LBL72 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTOUT CORRODED SECTION OF UPPER CHORD AND FABRICATED REPAIR IAW SRM 51-40-4 FIG 1 . ALSO AIA EDR NR B4-05876. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 25206. 2 L 7 4 4F A20WE 1998071400123 19980714 00123 NM 1998 7 14 CKSA98367 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 760 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION STA760 FWD LBL44 FLOORBEAM HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. CUTOUT CORROSION AND FABRICATED REPAIR IAW B747 SRM 51-40-4 FIG 1. INSTALLED REPAI R IAW B747 SRM 51-40-1 FIG 1. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 25207. 2 L 7 4 4F A20WE 1998071400124 19980714 00124 NM 1998 7 14 CKSA98368 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION, CORROSION AROUND CLIP NUT ON UPPER CHORD OF BS680 FLOORBEAM LBL3 . CUTOUT DAMAGE AREA IAW SRM 51-40-04 FIG 1. MADE REPAIR ANGLES AND DRILLED IAW SRM 51-40-04 FIG 1. INSTALLED REPAIR IAW B747 SRM 51-40-4 FIG 1. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 25226. 2 L 7 4 4F A20WE 1998071400125 19980714 00125 NM 1998 7 14 CKSA98369 1 19980630 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION. CORROSION AROUND 2 CLIP NUTS ON RBL 49 SEAT TRACK FWD OF BS 24 0. REMOVED CORROSION IAW 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. REMOVED SEAT TRACK SECTION IAW B7 47 SRM 51-30-02. REPLACED SEAT TRACK IAW B747 SRM 51-10-01 AND 51-30-02. FABRICATED SEAT TRACK SPLICE REPAIR DOUBLERS IAW B747 SRM 53-10-05 FIG 1A. INSTALLED SEAT TRACK SPLICE REPAIR IAW B747 SRM 53-10-05 FIG 1A. CORROSION TASK CARD NUM BER C53-210-07. NON-ROUTINE TASK CARD NUMBER 25228. 2 L 7 4 4F A20WE 1998071400126 19980714 00126 NM 1998 7 14 CKSA98370 1 19980630 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 340 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA 340 FWD SIDE LBL33 SEAT TRACK FLANGE HAS CORROSION. REMOVE D CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-05 FIG 1A. INSTALLED SEAT TRACK REPAIR IAW B747 SRM 53-10-05 FIG 1A. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 25235. 2 L 7 4 4F A20WE 1998071400127 19980714 00127 NM 1998 7 14 CKSA98371 1 19980630 A 5347 SEAT TRACK BOEING 747 747132 1384882 NM BS 1100 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS1100 LBL70 SEAT TRACK UNDERSIDE HAS CORROSION. REMOVED CORRO SION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR IAW B747 SRM 53-10-5 FIG 34. INSTALLED SEAT TRACK SPLICE REPAIR IAW B747 SRM 53-10-05 FIG 34. CORROSION TASK CARD NUMBER C53-210-05. NON-ROUTINE T ASK CARD NUMBER 25305. 2 L 7 4 4F A20WE 1998071400128 19980714 00128 NM 1998 7 14 CKSA98372 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 1940-1960 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, STA1940-1960 LBL11.33 LONGITUDINAL FLOORBEAM UPPER CHORD CORROD ED. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IA W B747 SRM 53-10-05 FIG 1A. INSTALLED REPAIR DOUBLERS IAW B747 SRM 53-10-05 FIG 1A. CORROSION TASK CARD NUMBER C53-210 -07. NON-ROUTINE TASK CARD NUMBER 25526. 2 L 7 4 4F A20WE 1998071400129 19980714 00129 NM 1998 7 14 CKSA98373 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 440 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM HAS CORROSION ON FWD SIDE. RE MOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. MANF REPAIR PARTS IAW EDR B4-0 5871. INSTALLED REPAIR DOUBLERS IAW EDR B4-05871 AND IAW DWG AIA/E/2844. CORROSION TASK CARD NUMBER C53-210-03. NON-R OUTINE TASK CARD NUMBER 25572. 2 L 7 4 4F A20WE 1998071400130 19980714 00130 NM 1998 7 14 CKSA98374 1 19980630 A 5711 SPAR BOEING 747 747132 1384882 NM WS 1356 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE C CHECK INSPECTION, FOUND LOWER FWD SPAR LWS1356 EXFOLIATED. REMOVED NR 2 PANEL RT SIDE. HFEC INSPECTED FASTENERS HOLES IN THE HORIZ FLANGE OF THE SPAR CHORD PER NDT MANUAL 51-00-00 PART 6. NO DEFECTS NOTED. PENETRANT INS PECTED CHORD PER STANDARD OVERHAUL PRACTICES MANUAL 20-20-02 NO DEFECTS NOTED. REMOVED DAMAGED AREA IAW B747 SRM CH 57- 30-03. ROTO PEENED EDGE OF CUTOUT IAW B747 STANDARD OVERHAUL MANUAL CH 20-10-03. FABRICATED REPAIR PARTS IAW B747 SRM 57-30-03 AND SKETCH NBR AIA/E/2846. ALODINED PRIMED AND INSTALLED REPAIR PARTS IAW B747 SRM 51-10-02, SRM 57-30-03, MM 51-20 AND SRM 51-30-02 AND EDR AIA/E/2846. C CHECK WORK CARD NUMBER 7CI6010. NON-ROUTINE TASK CARD NUMBER 25734 AND 30 2 L 7 4 4F A20WE 1998071400131 19980714 00131 NM 1998 7 14 CKSA98375 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 2240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND FS2240 RBL75 FLOORBEAM T CHORD HAS CORROSION. REMOVED CORROSION IAW B747 SRM 51-1 0-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-01. FABRICATED REPAIR DOUBLERS IAW B747 SRM 51-40-4 FIG 12 AND AIA EDR B4-05887. INSTALLED REPAIR IAW B747 SRM 51-40-4 FIG 1 AND AIA EDR B4-05887. CORROSION TASK CARD NUMBER C53-210-07. NON-ROUTINE TASK CARD NUMBER 25751. 2 L 7 4 4F A20WE 1998071400132 19980714 00132 NM 1998 7 14 CKSA98376 1 19980630 A 5314 KEEL BEAM BOEING 747 747132 1384882 NM BS 1265 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION UPPER WEB OF KEEL BEAM BOX CORRODED AND CRACKED APPROX STA 1265 AT PREVIOUS REPAIR. REMOVED FASTENERS IAW B747 SRM 51-30-2. REMOVED CORROSION IAW B747 SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW B747 SRM 53-10-1. COMPLIED WITH HFEC INSPECTION OF OPEN HOLES AND BLENDED AREA NO CRACK INDICATIONS IAW B 747 NDT MANUAL PART 6 51-00-00. REPAIRED IAW AIA EA B4-53-046. U/T THICKNESS CK HI .270 LOW .198. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 25912. 2 L 7 4 4F A20WE 1998071400133 19980714 00133 NM 1998 7 14 CKSA98377 1 19980630 A 5313 LONGERON BOEING 747 747132 1384882 NM BS 1320 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON UPPER SURFACE OF LEFT OVERWING LONGERON APPROX STA 1320. REMOVED COR ROSION FROM ACCESSABLE AREA IAW SRM 51-10-01. CORROSION RUNNING UNDER LONGERON SPLICE RAISED EDR AS PER AIA ENGINEERING . REPAIRED LT OVERWING LONGERON IAW EA NBR B4-53-053. C/W THICKNESS CHECK .487 MIN THICKNESS, C/W HFEC SURFACE SCAR OF 8L X 2-1/4W AREA, UPPER HORIZ SURFACE OF LT OVERWING LONGERON 747 NDT MANUAL PART 6 51-00-00. NO CRACKS. CORROSION TA SK CARD NUMBER C53-190-01. NON-ROUTINE TASK CARD NUMBER 25913. 2 L 7 4 4F A20WE 1998071400134 19980714 00134 NM 1998 7 14 CKSA98378 1 19980630 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE C CHECK INSPECTION, FOUND BS 1980 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRE D UPPER CHORD IAW AIA EDR NBR B4-05878. INSTALLED REPAIR IAW AIA EDR B4-05878. NON-ROUTINE TASK CARD NUMBER 26148. 2 L 7 4 4F A20WE 1998071400135 19980714 00135 NM 1998 7 14 CKSA98379 1 19980630 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2000 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE C CHECK INSPECTION, FOUND BS 2000 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED UNDER FLOOR SUPPORT. REPAIRE D UPPER CHORD IAW AIA EDR NBR B4-05879. INSTALLED REPAIR IAW AIA EDR NBR B4-05879. NON-ROUTINE TASK CARD NUMBER 26149. 2 L 7 4 4F A20WE 1998071400136 19980714 00136 NM 1998 7 14 CKSA98380 1 19980630 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2020 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE C CHECK INSPECTION, FOUND BS 2020 RBL 22 UPPER CHORD OF MAIN FRAME CORRODED AND A FLOOR SUPPORT. PERFORM ED HFEC PER NDT MANUAL 51-00-00 PART 6. NO CRACKS NOTED. REPAIRED UPPER CHORD IAW AIA EDR NBR B4-05880. INSTALLED REP AIR IAW AIA EDR B4-05880. NON-ROUTINE TASK CARD NUMBER 26150. 2 L 7 4 4F A20WE 1998071400137 19980714 00137 NM 1998 7 14 CKSA98381 1 19980630 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 440 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND LEVEL 2 CORROSION, FS440 RBL50 UPPER DECK FLOORBEAM ATTACH ANGLE CRACKED ON AFT IN BD SIDE. REMOVED AND REPLACED ATTACH ANGLE IAW B747 SRM 51-10-01 AND 51-30-02. CORROSION TASK CARD NUMBER C53-210-03. NON-ROUTINE TASK CARD NUMBER 26169. 2 L 7 4 4F A20WE 1998071400138 19980714 00138 NM 1998 7 14 CKSA98382 1 19980630 A 5320 INTERCOSTAL BOEING 747 747132 1384882 NM BS 440-460 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND FS 440 TO FS 460 RBL 50 INTERCOSTAL WEB CRACKED. REMOVED CRACKED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW B747 SRM 53-10-07 FIG 11. INSTALLED REPAIR IAW B747 SRM 53-10-07 FIG 11. CO RROSION TASK CARD NUMBER C53-210-03. NON-ROUTINE TASK CARD NUMBER 26170. 2 L 7 4 4F A20WE 1998071400139 19980714 00139 NM 1998 7 14 CKSA98383 1 19980630 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 440 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION, FOUND FS 440 RBL 50 UPPER DECK FLOORBEAM WEB CRACKED. REMOVED DAMAGED WEB IAW B747 SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW SRM 53-10-07 FIG 11. INSTALLED REPAIR IAW SRM 53-10-07 FIG 11. CORROSION TAS K CARD NUMBER C53-210-03. NON-ROUTINE TASK CARD NUMBER 26171. 2 L 7 4 4F A20WE 1998071400140 19980714 00140 NM 1998 7 14 CKSA98384 1 19980630 A 5320 WEB BOEING 747 747132 1384882 NM BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 625PL 20247 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION FUSELAGE LWR AREA, BS 1200, RBL 58, WEB CORRODED AT O/B FACE LWR AREA. REMOVED CORROSION IAW B747 SRM 51-10-01. FABRICATED REPAIR IAW B747 SRM 51-40-02. INSTALLED REPAIR IAW BOEING 7 47 SRM 51-40-02. CORROSION TASK CARD NUMBER C53-100-01. NON-ROUTINE TASK CARD NUMBER 26227. 2 L 7 4 4F A20WE 1998071400141 19980714 00141 NE 1998 7 14 TC8A98038 2 19980702 A 7200 ENGINE DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 2 MALFUNCTIONED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 23 184SK 45981 642493 ABORTED T/O AT IAH DUE TO HIGH EGT ON ENGINE NR 2, 1.85 EPR, EGT GOES 555 REDLINE AND CONTINUE TO CLIMB, SHUT DOWN ENGIN E, TAXI BACK. ENGINE NR 2 EXCEEDS MAX EGT LIMITS. TO CLARIFY, NO LIMITS WERE EXCEEDED BUT APPEARED IT WOULD HAVE IF TH ROTTLE WAS NOT RETARDED. 2 L 7 4 4F 4 F 4A25 1E8 1998071400142 19980714 00142 1998 7 14 98ZZZX2337 4 19980523 A 2312 KY195B TRANSCEIVER HUGHES 369 369D 4470706 WP COCKPIT FAILED B LS1R K NONE O OTHER IN INSP/MAINT 1 EA 13 369AW 9543 470117D TRANSMITS WEAK AND SQUELCH DOES NOT WORK. SENT FOR REPAIR. CONTROL NR 98-5-11. 1 G 7 1 3U H3WE 1998071400168 19980714 00168 WP 1998 7 14 TWAA9808904 1 19980318 A 5320 SUPPORT DOUG DC9 DC951 3022051 WP NLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 418EA 47676 STL - DURING OP 9 MAINTENANCE CHECK, FOUND .0312 INCH IN CRACK IN UPPER ANGLE ON RT SIDE OF LOWER RADAR SUPPORT BRACKET, INSIDE NOSE WHEEL WELL. CLEANED UP CRACK AND BLENDED TO SRM LIMITS PER SRM 53-01, PAGE 4, FIG 1. (X) 2 L 7 2 4F RT A6WE 1998071400169 19980714 00169 WP 1998 7 14 TWAA9808905 1 19980320 A 5320 SUPPORT DOUG DC9 DC951 3022051 WP NLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 418EA 47676 STL - DURING OP 9 MAINTENANCE CHECK, FOUND CRACK IN LOWER ANGLE ON RT SIDE OF LOWER RADAR SUPPORT BRACKET INSIDE NOSE WH EEL WELL. FABRICATED NEW ANGLE PER SRM 51-10-02. INSTALLED ANGLE PER SRM 51-30-02. (X) 2 L 7 2 4F RT A6WE 1998071400170 19980714 00170 NM 1998 7 14 TWAA9809001 1 19980606 A 3350 COVER BOEING 727 727231 1384079 NM CABIN LOOSE A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 54342 21629 JFK - FLT 904 - REPORT TO MAINTENANCE THAT THE EGRESS LIGHTS AT ROW 13 WERE BUCKLED UP. COVER WAS RESECURED. CC-04 4-3 -98 JFK. (X) 2 L 7 3 4F A3WE 1998071400171 19980714 00171 WP 1998 7 14 TWAA9809002 1 19980606 A 3350 58541 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 405EA 47688 STL - FLT 604 - DURING PRE-FLIGHT INSPECTION, FOUND EGRESS LIGHTS INOPERATIVE ROW 3 TO ROW 7. REPLACED FEEDER CABLE MFG PN 5854-1. CC-00 12-23-97 STL. (X) 2 L 7 2 4F RT A6WE 1998071400172 19980714 00172 WP 1998 7 14 TWAA9809003 1 19980607 A 3350 4TL1110B SWITCH DOUG DC9 DC933F 302207A WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 937F 47409 STL - FLT 734 - DURING PRE-FLIGHT CHECK, EMERGENCY EGRESS LIGHTS STAYED ON WITH SWITCH IN ARMED POSITION. REPLACED EGRE SS LIGHT SWITCH MFG PN 4TL11-10B. OP-15 3-23-98 MCI. (X) 2 L 7 2 4F A6WE 1998071400173 19980714 00173 WP 1998 7 14 TWAA9809006 1 19980607 A 2133 20219741 ACTUATOR DOUG DC9 DC982 3022082 WP OUTFLOW VALVE FAILED A TWAA K NONE J WARNING INDICATION DE DESCENT 1 CE 05 915TW 027113 49186 STL - FLT 10 - DURING DESCENT EXPERIENCED AIRCRAFT DECOMPRESSION AT FL 140. NEITHER MANUAL OR AUTOPRESSURIZATION HAD AN Y EFFECT. REPLACED OUTFLOW VALVE ACTUATOR MFG PN 2021974-1. CC02D 5-17-98 STL. (X) 2 L 7 2 4F A6WE 1998071400174 19980714 00174 NM 1998 7 14 TWAA9809007 1 19980607 A 3350 6104781 POWER SUPPLY BOEING 727 727231 1384079 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64315 000306 20048 STL - FLT 8601 - DURING PRE-FLIGHT INSPECTION, FOUND L1 AND R1 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWE R SUPPLY MFG PN 61-0478-1. CC-01 10-31-97 JFK. (X) 2 L 7 3 4F A3WE 1998071400175 19980714 00175 NM 1998 7 14 TWAA9809008 1 19980607 A 3350 3005441 BATTERY BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64315 20048 STL - FLT 8601 - DURING PRE-FLIGHT INSPECTION, FOUND AFT AIRSTAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES MFG PN 30-0544-1. CC-01 10-31-97 JFK. (X) 2 L 7 3 4F A3WE 1998071400176 19980714 00176 WP 1998 7 14 TWAA9809009 1 19980607 A 2910 HYD FLUID DOUG DC9 DC982 3022082 WP RT HYD SYSTEM LOST A TWAA A D UNSCHED LANDING RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CE 05 951U 49245 STL - FLT 203 - DURING TAKEOFF, LOST RT SYSTEM HYDRAULIC FLUID. REPLACED RT NOSE TIRE MFG PN 3910097-535 DUE TO TREAD C AP MISSING. CC-010 7-20-97 LAX. (X) 2 L 7 2 4F A6WE 1998071400177 19980714 00177 NM 1998 7 14 SABA290029 1 19980526 A 7930 AS3209210 O-RING DHAV DHC8 DHC8102 2809003 NM RT ENGINE WORN A SABA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 33 859MA 361 CLT\CVG - FLT 5033 - ON CLIMB-OUT FROM CLT, THE NR 2 ENGINE HAD OIL PRESSURE FLUCTUATION. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED THE O-RING TO THE RIGHT AC GENERATOR. SHAFT SERVICED ENGINE WITH OIL, RUN AND OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A13NM 1998071400178 19980714 00178 NM 1998 7 14 SABA290030 1 19980523 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM BAGG COMPT MALFUNCTIONED A SABA C ABORTED TAKEOFF J WARNING INDICATION TX TAXI/GRND HDL 1 SO 33 859MA 0205 361 CLT/OAJ - FLT 5173 - DURING TAXI-OUT AT CLT, THE BAGGAGE BAY SMOKE DETECTOR WENT OFF. NO SMOKE WAS NOTED. PASSENGERS WERE DE-PLANED. EMERGENCY PROCEDURES WERE DECLARED (PRECAUTIONARY). MAINTENANCE REMOVED AND REPLACED THE BAGGAGE BAY S MOKE DETECTOR. SYSTEM OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A13NM 1998071400179 19980714 00179 WP 1998 7 14 EIAA980197 1 19980416 A 5320 5915055504N FITTING DOUG DC9 DC933F 302207A WP BS 579 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, RIGHT HAND BODY TO CENTER TANK ATTACH FITTING CRACKED AT BS 579. REPLACED FITTING PER SRM 51-1 0-03. (X) 2 L 7 2 4F A6WE 1998071400180 19980714 00180 WP 1998 7 14 EIAA980195 1 19980319 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 832 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME CRACKED AT BS 832 FROM STR 26L - STR 27L. REPAIRED FLOOR SUPPORT PER DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400181 19980714 00181 WP 1998 7 14 EIAA980196 1 19980416 A 5311 99118593 FRAME DOUG DC9 DC933F 302207A WP BS 1104 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, AFT ACCY COMPARTMENT, CANTED FRAME CRACKED AT BS 1104, STR 20L. REPLACED CANTED FRAME FROM STR 11L- STR 22L PER SRM'S 51-10-3 AND 51-30-05. (X) 2 L 7 2 4F A6WE 1998071400182 19980714 00182 NM 1998 7 14 SPAA9800003 1 19980703 A 2613 SENSOR BOEING 737 7372T4 1384492 NM NR 1 ENGINE OUT OF POSITION A SPAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 703S 22529 EN ROUTE BETWEEN DLH AND JAX, THE NR 1 ENGINE WAS SHUT DOWN DUE TO AN OVERHEAT WARNING. BOTH ENGINE FIRE EXTINGUISHER C YLINDERS WERE DISCHARGED. AIRCRAFT DIVERTED TO SAV AND LANDED WITHOUT INCIDENT. UPON INSPECTION, THE NR 1 ENGINE LOWER OVERHEAT SENSING ELEMENT WAS FOUND TO BE IN CONTACT WITH THE LOOP PROTECTIVE ENCLOSURE CAUSING A SHORT CIRCUIT IN THE S YSTEM. THE CONDITION WAS RECTIFIED, BOTH ENGINE EXTINGUISHERS WERE REPLACED. ALL SYSTEM TESTS PER BMM 26-11-0 AND 26-1 1-11 WERE ACCOMPLISHED SATISFACTORILY. THE AIRPLANE RETURNED TO SERVICE. 2 L 7 2 4F A16WE 1998071400183 19980714 00183 NM 1998 7 14 VJ9800214 1 19980702 A 3350 900835A BATTERY PACK BOEING 737 7372P6 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 EICJW 21355 CENTER CABIN CEILING EMERGENCY LIGHT FLASHED WHEN TESTED. REPLACED EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F RT A16WE 1998071400184 19980714 00184 WP 1998 7 14 9809739986 1 19980703 A 2150 BOOT DOUG DC9 DC932 3022066 WP LT ACM LOOSE A NWAA B EMER. DESCENT J WARNING INDICATION UK UNKNOWN 1 GL 01 986US 47480 LOSS OF CABIN PRESSURIZATION OCCURRED AT 31,000 FEET EN ROUTE. CREW ACCOMPLISHED EMERGENCY DESCENT TO 10,000 FEET. FLI GHT WAS CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE RUBBER BOOT BETWEEN LEFT AIR CYCL E MACHINE AND HEAT EXCHANGER. SECURED BOOT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998071400185 19980714 00185 WP 1998 7 14 9809749942 1 19980703 A 2910 LINE DOUG DC9 DC932 3022066 WP RT HYD SYSTEM LEAKING A NWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 01 3991C 47175 RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE WENT TO ZERO AFTER TAKEOFF. FLIGHT WAS RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HYDRAULIC LINE LEAKING. REPLACED LINE. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SE RVICE. 2 L 7 2 4F A6WE 1998071400186 19980714 00186 WP 1998 7 14 9809759993 1 19980704 A 2150 DUCT DOUG DC9 DC931 3022065 WP LT ACM BLOWN A NWAA B EMER. DESCENT J WARNING INDICATION UK UNKNOWN 1 GL 01 8986E 47402 LOSS OF CABIN PRESSURIZATION OCCURRED AT 33,000 FEET EN ROUTE. CABIN PRESSURE WARNING LIGHT ILLUMINATED AND CABIN ALTIT UDE REACHED APPROXIMATELY 11,000 FEET. CREW ACCOMPLISHED EMERGENCY DESCENT AND FLIGHT WAS CONTINUED TO DESTINATION. AI RCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT AIR CYCLE MACHINE DUCT BLOWN OFF. REPLACED DUCT AND TIGHTENED A LL CLAMPS. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998071400187 19980714 00187 WP 1998 7 14 9809769937 1 19980704 A 3232 59567435501 ACTUATOR DOUG DC9 DC931 3022065 WP LDG GEAR DOOR FAILED A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 908H 13139 534 47517 DURING APPROACH INTO MSP, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. FLIGHT CREW RECYCLED GEAR THRE E TIMES. MAINTENANCE REPLACED LANDING GEAR DOOR ACTUATOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998071400188 19980714 00188 WP 1998 7 14 9809779860 1 19980706 A 2780 TELESCOPING DUCT DOUG DC9 DC951 3022051 WP LT WING LACK OF LUBE A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 769NC 47757 DURING APPROACH INTO RDU, SLAT DISAGREEMENT LIGHT ILLUMINATED WITH NO BLUE SLAT EXTEND LIGHT. AIRCRAFT ROLLED TO THE RI GHT AND FLIGHT ATTENDANT OBSERVED NO SLAT EXTENSION ON LEFT WING. CAPTAIN DECLARED A YELLOW EMERGENCY AND REQUESTED EQU IPMENT ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE LUBED LEFT WING ANTI-ICE TELESCOPE DU CT. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A6WE 1998071400189 19980714 00189 SO 1998 7 14 COMA9810153 1 19980706 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 257CA 120248 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN ASSY. 2 L 7 2 4T RT A31SO 1998071400190 19980714 00190 EU 1998 7 14 QXEA9800926 1 19980704 A 3350 5515900004 PRINTED CIRCUIT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 SEA - EXIT SIGN LIGHTS IN FORWARD CABIN CEILING DIM. MAINTENANCE REMOVED AND REPLACED EXIT SIGN CIRCUIT BOARD, OPERATIO NALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071400191 19980714 00191 EU 1998 7 14 QXEA9800927 1 19980701 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 PDX - FORWARD EXIT LIGHT HAS BURNT OUT BULBS. MAINTENANCE REMOVED AND REPLACED BULBS, OPERATIONALLY TESTED, TESTS NORMA L. 2 L 7 2 4F RT A20EU 1998071400192 19980714 00192 EU 1998 7 14 QXEA9800928 1 19980701 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 PDX - FORWARD GALLEY EXIT LIGHT HAS A BURNT OUT BULB. MAINTENANCE REMOVED AND REPLACED BULB, OPERATIONALLY TESTED, TEST S NORMAL. 2 L 7 2 4F RT A20EU 1998071400193 19980714 00193 EU 1998 7 14 QXEA9800929 1 19980703 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 PDX - LIGHTS OUT IN EXIT SIGN ABOVE COCKPIT DOOR. MAINTENANCE REMOVED AND REPLACED LAMPS IN EXIT SIGN, OPERATIONALLY TE STED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071400194 19980714 00194 EU 1998 7 14 QXEA9800930 1 19980706 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 PDX - EXIT LIGHT OVER COCKPIT DOOR DOES NOT FULLY ILLUMINATE. MAINTENANCE REMOVED AND REPLACED EXIT LIGHT, OPERATIONALL Y TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071400195 19980714 00195 EU 1998 7 14 QXEA9800931 1 19980703 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 BOI - THE AISLE EMERGENCY EXIT LIGHTS ARE INOPERATIVE AT ROWS 1 AND 13. MAINTENANCE REMOVED AND REPLACED BULBS, OPERATI ONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071400196 19980714 00196 NM 1998 7 14 98FDEA00435 1 19980706 A 5311 6515927 FRAME BOEING 727 72722 1384002 NM BS 480 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 NR 866 001 - STA-PAE, CRACK IN RADIUS OF BS 480 FRAME B4 STR 27 RT. REPAIRED CRACK IN RADIUS OF BS 480 BY STR 27 RT PER FED-EX EA NR 7-5310-39851. 2 L 7 3 4F A3WE 1998071400197 19980714 00197 WP 1998 7 14 98FDEA00436 1 19980703 A 5320 ANGLE DOUG DC10 DC1010F 3022111 WP BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 FWD LOWER BELLY BS 1110 MOUNTING STRUCTURE FOR LINEAR ACCELEROMETERS ARE BADLY CORRODED, LOWER FACE. *S/D* REMOVED AND REPLACED FWD AND AFT SUPPORT STRUCTURE FOR LINEAR ACCELEROMETERS AS PER SRM 51-0-00 AND DAC DRAWING NR AAN7081. REF N/ R'S 00641 AND N00642. LINEAR ACCELEROMETERS REINSTALLED AND REALINED BY BOEING A/C. REF SNRM NR 00533. 2 L 7 3 4F A22WE 1998071400198 19980714 00198 WP 1998 7 14 98FDEA00437 1 19980703 A 5753 CASTING DOUG DC10 DC1010F 3022111 WP RT TE FLAP CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 058FE 46705 N/R N00434 STA-LAX: RT WING INBD FLAP, INBD FLAP DRIVE MOUNT HOLE (INBD) HAS DEEP CORROSION AROUND SECTION OF BUSHING. REMOVED CORROSION REF SRM 51-21-01. C/W HFEC REQUIRED BY ENGINEERING NO CRACK INDICATION FOUND. REF: EA 8-5750-38590 . 2 L 7 3 4F A22WE 1998071400199 19980714 00199 WP 1998 7 14 ABXA9800601 1 19980703 A 3260 H141003 SWITCH DOUG DC8 DC862 3021970 WP RT MLG INOPERATIVE A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 802AX 46134 ON GEAR EXTENSION RT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE. RECYCLED GEAR, LIGHT ILLUMINATED. REPLACED RIGHT MAIN LANDING GEAR INDICATION SWITCH IAW DC8 MM 32-60-00. 2 L 7 4 4F 4A25 1998071400200 19980714 00200 WP 1998 7 14 MWEA98761 1 19980629 A 3620 6712152180 SENSOR DOUG DC9 DC932 3022066 WP TAIL SECTION INOPERATIVE A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 215ME 47744 THE MASTER WARNING LIGHTS AND TAIL COMPARTMENT TEMP HIGH LIGHTS ILLUMINATED APPROACHING 138 KNOTS. MAINTENANCE PERFORME D REJECTED TAKEOFF INSPECTION INSPECTED TAIL COMPARTMENT. REMOVED AND REPLACED RT TEMP HIGH SENSOR. 2 L 7 2 4F A6WE 1998071400201 19980714 00201 WP 1998 7 14 MWEA98762 1 19980703 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP CABIN DOOR NOT INSTALLED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE MAIN CABIN DOOR SLIDE PACK IS REMOVED. MAINTENANCE REINSTALL DOOR SLIDE. 2 L 7 2 4F A6WE 1998071400202 19980714 00202 1998 7 14 MWEA98763 4 19980705 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR INOPERABLE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 THE GALLEY SERVICE DOOR ESCAPE SLIDE PRESSURE GAUGE IS IN RED AREA. MAINTENANCE REPLACED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1998071400203 19980714 00203 NM 1998 7 14 DL76L981370 1 19980630 A 5754 WEDGE BOEING 767 767332 1382001 NM NR 3 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 THE UPPER SKIN ON THE TRAILING EDGE WEDGE OF THE NR 3 SLAT WAS FOUND WITH A DELAMINATED AREA. DAMAGE WAS APPROX 1.5 BY 1.5. REPAIRED PER ERA 365144-14AD. 2 L 7 2 4F RT A1NM 1998071400204 19980714 00204 NM 1998 7 14 DL72W981371 1 19980701 A 5315 FLOOR BEAM BOEING 727 727247 138408F NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 SEVERAL SMALL AREAS OF CORROSION AND BARE METAL AT FLOORBEAM STA 344 AND RBL12 TO LBL 60. REPAIRED PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1998071400205 19980714 00205 NM 1998 7 14 DLM88981372 1 19980701 A 2560 61020 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 995DL 53362 FLT ATTENDANT ADVISED MAINTENANCE THAT F/C EMER FLASHLIGHT DID NOT BLINK. REPLACED BATTERY AND BULB. 2 L 7 2 4F RT A6WE 1998071400206 19980714 00206 NM 1998 7 14 DL72S981373 1 19980630 A 3350 900542 RACK BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 21145 RT SIDE EMER LIGHT OVERWING EXIT LIGHTS INOP. REPLACED LIGHT RACK. 2 L 7 3 4F A3WE 1998071400207 19980714 00207 NE 1998 7 14 DL767981374 2 19980701 A 7200 ENGINE BOEING 767 767232 1385132 NM GE CF680 CF680A2 NE NR 1 FAILED A DALA L ABORTED APPROACH R PARTIAL RPM/PWR LOSS AP APPROACH 1 SO 27 103DA 31154 22215 580373 AS POWER CAME UP FROM IDLE A BANG WAS HEARD AND LT ENG REMAINED AT IDLE PWR. NO CONTROL OF LEFT ENG FROM COCKPIT. NO E NG EXCEEDANCE NOTED AND NO INDICATIONS IN COCKPIT OF ENG FAILURE. ENG WAS NOT SHUTDOWN FOR EMERG LANDING AT JFK. FOU ND METAL IN TAILPIPE. ENG REPLACED. 2 L 7 2 4F 4 F RT A1NM E13NE 1998071400208 19980714 00208 NM 1998 7 14 DL73E981375 1 19980630 A 2910 LINE BOEING 737 737247 138448D NM NR 2 ENGINE CHAFFED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 236WA 23184 000000 A/C RETURN ATL, DUE TO RT HYD PUMP LOW PRESS LIGHT AND HYD QTY ZERO ON CLIMB-OUT. FOUND HYD RTN LINE CHAFFED. REPLACED LINE AND FILTER AND EDP PER M/M. LEAK CK GOOD AND SYS OPS NML PER M/M. 2 L 7 2 4F A16WE 1998071400209 19980714 00209 NM 1998 7 14 DL72S981376 1 19980630 A 5522 657278420 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 T/E OF RT ELEVATOR WAS DELAMINATING. INSTALLED ADDITIONAL TACK RIVETS BETWEEN FACTORY RIVETS AS PER M/M 55-20-0. 2 L 7 3 4F A3WE 1998071400210 19980714 00210 NM 1998 7 14 DL72W981377 1 19980701 A 5320 WEB BOEING 727 727247 138408F NM BS 1240 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 CRACK IN RT AIR STAIR WEB AT STA 1240 VERTICAL WEB. REPAIRED PER MM 53-11-0 P 832. 2 L 7 3 4F A3WE 1998071400211 19980714 00211 NM 1998 7 14 DL72W981378 1 19980701 A 5320 WEB BOEING 727 727247 138408F NM BS 1280-1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 VERT WEB CRACKED AT LIGHTENING HOLES STA 1280 AND 1303 LT. REPAIRED PER MM 53-11-0 P 828. 2 L 7 3 4F A3WE 1998071400212 19980714 00212 NM 1998 7 14 DL72W981379 1 19980701 A 5720 BEAM BOEING 727 727247 138408F NM LT WING CHAFED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2821W 21059 MLG CHAFFING FWD SIDE OF MLG BEAM BELOW STR 18A. REPAIR PER M/M 57-43-0. 2 L 7 3 4F A3WE 1998071400213 19980714 00213 NM 1998 7 14 DL76S981380 1 19980701 A 5330 SKIN BOEING 767 767332 1382001 NM BS 1461 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 137DL 25306 FUSELAGE/SKIN, BULK CARGO DOOR SURROUND FS 146. REPAIR FOR EDGED GOUGES. THE FUSELAGE SKIN AND UNDERLYING BEAR STRAP A T THE FWD EDGE OF THE BULK CARGO DOOR OPENING WAS DAMAGED BY GROUND EQUIP. THE DAMAGED AREAS WERE TRIMMED OUT FROM THE EDGE AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 365124-14, REV C . 2 L 7 2 4F RT A1NM 1998071400214 19980714 00214 NM 1998 7 14 DL72W981381 1 19980629 A 5313 65564411 STRINGER BOEING 727 727247 138408F NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 STRINGER 29L WAS FOUND CORRODED. THE STRINGER WAS TRIMMED AT STA 950D+10 AND THE AFT PORTION REMOVED. REPAIRED PER ERA 331787-14. 2 L 7 3 4F A3WE 1998071400215 19980714 00215 NM 1998 7 14 DL72W981382 1 19980629 A 5711 65162317 SPAR CHORD BOEING 727 727247 138408F NM WS 340 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FRONT SPAR UPPER CHORD WAS FOUND WITH A CRACK IN THE FORWARD FLANGE AT A FASTENER HOLE AT APPROX WL340. REPAIRED PER ER A 331817-14. 2 L 7 3 4F A3WE 1998071400216 19980714 00216 NM 1998 7 14 DL72W981383 1 19980629 A 5313 6556441 STRINGER BOEING 727 727247 138408F NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FUSELAGE STRINGER 29R WAS FOUND WITH CORROSION AT FS 950E PLUS 10. A NEW SECTION OF STRINGER IS SPLICED IN. REPAIRED P ER ERA 331848-14. 2 L 7 3 4F A3WE 1998071400217 19980714 00217 NM 1998 7 14 DL72W981384 1 19980629 A 5330 SKIN BOEING 727 727247 138408F NM L1 DOORWAY GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FUSELAGE SKIN WAS GOUGED FWD OF THE L1 DOOR AT S10L LAP SPLICE. REPAIRED PER ERA 331851-14. 2 L 7 3 4F A3WE 1998071400218 19980714 00218 NM 1998 7 14 DL72S981385 1 19980702 A 5311 6516325111 FRAME BOEING 727 727232 1384082 NM BS 761 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 WHILE PERFORMING THE REPAIR/MOD PER EO 4-61904-3AD. MAINTENANCE FOUND THE 2ND FASTENER BELOW THE FLOOR LINE TO BE AT A DIAMETER OF 0.375. REPAIRED PER ERA 331852-14AD. 2 L 7 3 4F A3WE 1998071400219 19980714 00219 NM 1998 7 14 DL72S981386 1 19980702 A 5330 65545905 SKIN BOEING 727 727232 1384082 NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 CORROSION DAMAGE FOUND IN THE LWR SKIN AT APPROX FS720C+10 AT S26R. REPAIRED PER ERA 331866-14. 2 L 7 3 4F A3WE 1998071400220 19980714 00220 NM 1998 7 14 DL72S981387 1 19980702 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 SEVERAL FASTENER HOLES AT S18A AT FS 940 ON THE LT SIDE WERE FOUND CRACKED. CRACKS WERE IN THE STRINGER ONLY AND DID NO T EXTEND TO THE UNDERLYING STRUCTURE. REPAIRED PER ERA 331854-14. 2 L 7 3 4F A3WE 1998071400221 19980714 00221 NM 1998 7 14 DL73S981388 1 19980630 A 5311 654654845 FRAME BOEING 737 737232 1384475 NM BS 747/827 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 331DL 23103 THE STA 747 FRAME WAS FOUND DENTED ON THE INBOARD FLANGE BETWEEN STR 24L AND 25L. THE STA 827 FRAME WAS FOUND DENTED ON THE INBOARD FLANGE AT STR 24L. THE DAMAGE WAS CAUSED IN SERVICE. REPAIRED PER ERA 331894-14. 2 L 7 2 4F RT A16WE 1998071400222 19980714 00222 NM 1998 7 14 DLM88981389 1 19980702 A 5311 591359577 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 993DL 53345 STA 1418 FRAME WAS FOUND WITH A 1.25 LONG CRACK IN THE RADIUS AT L2R. THE CRACK IS TYP PER SB 53-184; BUT SB EFFECTIVIT Y DOES NOT COVER THIS AC. REPAIRED PER ERA 331877-14. 2 L 7 2 4F RT A6WE 1998071400223 19980714 00223 NM 1998 7 14 DL73S981390 1 19980702 A 5311 654653949 FRAME BOEING 737 737232 1384475 NM BS 616 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 331DL 23103 LT AND RT INBD CHORD OF THE FS 616 FRAME BOTH HAVE A CRACK IN THE LOWEST FASTENER HOLE BELOW THE FLOOR LINE. REPAIRED P ER ERA 331885-14. 2 L 7 2 4F RT A16WE 1998071400224 19980714 00224 NM 1998 7 14 DL73S981391 1 19980702 A 5311 65479592 FRAME BOEING 737 737232 1384475 NM BS 800 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 331DL 23103 C2 DOOR CUTOUT FWD FRAME LWR CORNER AT FS 800 WAS FOUND CORRODED IN THE UPPER RADIUS NEAR S25R. REPAIRED PER ERA 331884 -14AD. 2 L 7 2 4F RT A16WE 1998071400225 19980714 00225 NM 1998 7 14 DL73S981392 1 19980702 A 5330 654577519 SKIN BOEING 737 737232 1384475 NM BS 847 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 331DL 23103 LWR AFT CORNER OF THE C2 DOOR CUTOUT WAS ROUTED OUT TO REMOVE DAMAGE. REPAIRED PER ERA 331876-14. 2 L 7 2 4F RT A16WE 1998071400226 19980714 00226 NM 1998 7 14 DL72W981393 1 19980629 A 5330 6554590 SKIN BOEING 727 727247 138408F NM BS 700 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 FUSELAGE BELLY SKIN WAS FOUND WITH CRACKS AND CORROSION AT STA 700 AND STR 28L - 28R. BELLY SKIN WILL BE REPLACED DUE T O NUMEROUS EXISTING REPAIRS. REPAIRED PER ERA 303637-14. 2 L 7 3 4F A3WE 1998071400227 19980714 00227 NM 1998 7 14 DL72S981394 1 19980623 A 7120 MOUNT BOEING 727 727232 1384082 NM NR 3 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 418DA 21271 DURING MODIFICAITON OF THE FASTENER HOLES IN THE NR 3 ENGINE MOUNT PER S/B 727-54A0010R4, FASTENER HOLE C WAS FOUND CRAC KED. THE HOLE WAS SUBSEQUENTLY OVERSIZED LARGER THAN IS ALLOWED BY THE S/B. REPAIRED PER ERA 331809-14. 2 L 7 3 4F A3WE 1998071400228 19980714 00228 NM 1998 7 14 DL72S981395 1 19980701 A 5330 65C139132 SKIN BOEING 727 727232 1384082 NM BS 1009 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 CORROSION WAS FOUND AT STA 1009 AND STR 28L ON THE INTERNAL SKIN BUTT SPLICE STRAP IN AN AREA PREVIOUSLY REPAIRED. THE PREVIOUS REPAIRS WERE REMOVED, AND RE-REPAIRED. REPAIRED PER ERA 237701-14. 2 L 7 3 4F A3WE 1998071400229 19980714 00229 NM 1998 7 14 DL73S981396 1 19980702 A 5312 65163007 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 331DL 23103 8 CRACKS FOUND IN THE BS 178 BULKHEAD WEB. REPAIRED PER ERA 331867-14. 2 L 7 2 4F RT A16WE 1998071400230 19980714 00230 WP 1998 7 14 DLL14981399 1 19980702 A 2150 COVER LKHEED 1011 1011385115 5265015 WP NR 2 PACK SEPARATED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 1738D 193C1234 AT 28000 FT HEARD A POP AND THEN THE AIRCRAFT WOULD NOT MAINTAIN CABIN ALTITUDE. CABIN ALTITUDE STARTED TO CLIMB AT 500 FT/MIN. FOUND NR 2 PACK WATER SEPARATOR COVER BLOWN LOOSE. REPLACED SEAL AND CLAMP ON THE NR 2 PACK SEPARATOR. OPS CH ECKED SATISFACTORY. PRESSURIZED ACFT. CHECKED CARGO DOORS AND PAX DOORS AND ALL AREA'S. CHECKED SATISFACTORY. 2 L 7 3 4F A23WE 1998071400231 19980714 00231 NM 1998 7 14 DL72W981401 1 19980702 A 3350 BATTERY RACK 1001141 BOEING 727 727247 138408F NM ROW 18 ABCDEF DISCHARGED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 2809W 9890 20581 SEAT ROW 18 ABCDEF OVERHEAD EMER LIGHT INOP. REPLACED BATTERY RACK OPS NOW NML. 2 L 7 3 4F A3WE 1998071400232 19980714 00232 NM 1998 7 14 DL72L981403 1 19980703 A 3350 LIGHT S106 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 502DA 21304 AFT AIRSTAIR EMER LIGHT INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998071400233 19980714 00233 NM 1998 7 14 DL72S981404 1 19980704 A 5240 ROLLER BOEING 727 727232 1384082 NM RT SERVICE DOOR OUT OF POSITION A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 515DA 21431 RIGHT AFT SERVICE DOOR SEAL NOT MAKING CONTACT. A/C WOULD NOT HOLD PRESSURIZATION. FOUND LOWER AFT CONER ROLLER NOT IN CAM. OPENED DOOR INSP ROLLER AND STOPS. ALL CK,D GOOD. CLOSED DOOR. OP NORMAL. 2 L 7 3 4F A3WE 1998071400234 19980714 00234 NM 1998 7 14 DLM88981405 1 19980630 A 3397 WIRE DOUG MD88 MD88 3023688 NM CABIN SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 911DE 49967 EMERGENCY FLOOR TRACK LIGHTING INOP. FOUND BARE WIRES ON FLOOR. MADE APPROVED REPAIRS. ALSO, FOUND SHORTED SOCKET. R EPLACED SAME. 2 L 7 2 4F RT A6WE 1998071400235 19980714 00235 NM 1998 7 14 DL72S981406 1 19980705 A 5240 DOOR BOEING 727 727232 1384082 NM SERVICE DOOR NOT CLOSED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 517DA 21433 AIRCRAFT WOULD NOT PRESSURIZE IN CLIMB. AIRCRAFT AIR TURN BACK TO ATL. FOUND R-1 DOOR NOT FULLY STOWED IN FUSELAGE. I NSPECTED DOOR AND CHECKED FOR PROPER OPERATION, CLOSED DOOR. CHKS OK. 2 L 7 3 4F A3WE 1998071400236 19980714 00236 NE 1998 7 14 DL73E981407 2 19980704 A 7200 ENGINE BOEING 737 7372J8 1384489 NM PWA JT8 JT8D15A 52051 NE NR 2 OVER TEMP A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SO 27 235WA 33604 709210 22859 709210 ENGINE IN FLIGHT, SHUT DOWN DUE TO OIL TEMP EXCEEDED RED LINE. ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1998071400237 19980714 00237 NM 1998 7 14 DL72S981409 1 19980705 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 21020 FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT BATTERY, BULB, AND PLAC. OPS CKS GOOD. 2 L 7 3 4F A3WE 1998071400238 19980714 00238 NM 1998 7 14 DLM88981410 1 19980705 A 3350 61020 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 945DL 49818 AFT JUMPSEAT CENTER FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED AFT JUMPSEAT AFT FLASHLIGHT, CKS OK. 2 L 7 2 4F RT A6WE 1998071400239 19980714 00239 NM 1998 7 14 DL72W981411 1 19980705 A 2782 ACTUATOR 269002917 BOEING 727 727247 138408F NM NR 2 SLAT LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 2820W DL344X 21058 NR 2 SLAT ACTUATOR LEAKING, LOST HYDAULICS ON FINAL. REPLACED ACTUATOR. 2 L 7 3 4F A3WE 1998071400240 19980714 00240 NM 1998 7 14 DL72S981412 1 19980706 A 5753 65192703 FLAP TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 INB'D FLAP, INB'D TRACK, TYP CORROSION AT FWD AND AFT, PAD-UP ATTACH HOLES AND FWD LUG: AD 90-07-05. FWD AND AFT PAD-U P ATTACH HOLES SUBJECT OF AD 90-07-05; REC'D BAC/FAA APPROVAL TO STEP-UP HOLES AND BUSH. FWD ATTACH LUG NOT SUBJECT OF AD; REC'D BAC APPROVAL TO BUSH AND SHIM LUG FACE. 2 L 7 3 4F A3WE 1998071400241 19980714 00241 NM 1998 7 14 DL76L981413 1 19980706 A 3350 61020 BATTERY BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST CR CRUISE 1 SO 27 175DN 24803 JUMP SEAT AFT CENTER FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 1998071400242 19980714 00242 NM 1998 7 14 DL72S981415 1 19980706 A 5210 SKIN BOEING 727 727232 1384082 NM L1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 FOUND ON E1 LETTER CK, .25 INCH CRACK IN L1 DOOR SKIN AT LOWER HINGE CUTOUT. REPAIRED PER MM 52-11-0. 2 L 7 3 4F A3WE 1998071400243 19980714 00243 NM 1998 7 14 DL757981417 1 19980706 A 3350 BATTERY 61020 BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 608DA 22815 EMERGENCY FLASHLIGHT BATTERY LOW. REPLACED BATTERY. 2 L 7 2 4F RT A2NM 1998071400244 19980714 00244 WP 1998 7 14 SCNA98510 1 19980706 A 5320 FRAME DOUG DC10 DC1015 3022118 WP R3 DOORWAY CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, CRACKS IN THE R3 DOOR FRAME BOX CUTOUT WERE DISCOVERED AT THE FLOOR LEVEL AT STATION 1256, INBOARD OF THE ARM SHAFT AT OPPOSITE CORNERS, (2 CRACKS). MATERIAL VERIFIED IAW SRM 535000 FIGURE 19 SHEET 1. DOUBLER FABRICA TED PER SRM 53-50-00 FIG 19 SHEET 1, TREATED, ALODINED AND PRIMED PER SRM 512101 AND INSTALLED PER SRM 53500 FIG 19 SHE ET 1. 2 L 7 3 4F A22WE 1998071400245 19980714 00245 WP 1998 7 14 SCNA98511 1 19980706 A 5521 SPAR DOUG DC10 DC1015 3022118 WP RT HORIZ STAB CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, CRACKS WERE DISCOVERED IN THE RIGHT HAND HORIZONTAL SPAR HAS A .5 INCH CRACK AT STATION XSFS 86/XE 28.42. LOCATED AND DRILLED ANGLES, DOUBLER, SHIM AND 'T' CHORD PER SRM 552000, ALODINED AND TREATED PER SRM 512101. IN STALLED ANGLES, DOUBLERS, SHIM AND 'T' CHORD PER 552000. INSTALLED RIB WEB AT STA HXS48, DOUBLERS, AND GANG CHANNEL P ER SRM 513101. SB 5524 FIGURE 6 COMPLIED WITH. 2 L 7 3 4F A22WE 1998071400246 19980714 00246 WP 1998 7 14 SCNA98512 1 19980706 A 5320 SUPPORTS DOUG DC10 DC1015 3022118 WP BS 1187 CORROSION A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, LEVEL TWO CORROSION WAS DISCOVERED AT STA 1887 LBL27 TO RBL80 ON CABIN FLOOR SUPPORTS. REMOVED FIVE EACH FLOOR SUPPORTS, FABRICATED FIVE EACH FLOOR SUPPORTS PER SRM 530001 AT STATION 1887 FROM LBL27 TO RBL80. TREATED A ND PRIMED PER SRM 512101. INSTALLED PER SRM 533101. 2 L 7 3 4F A22WE 1998071400247 19980714 00247 WP 1998 7 14 SCNA98513 1 19980706 A 5320 CHANNEL DOUG DC10 DC1015 3022118 WP BS 1912-1973 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, LEVEL TWO CORROSION WAS DISCOVERED ON THE HAT CHANNEL AT STATION 1912 TO 1973 IN THREE SPOTS. REMOV ED AND REPLACED DAMAGED HAT CHANNEL IAW SRM 530001, ALODINED AND PRIMED PER SRM 512101, TOP COATED PER SRM 512102. 2 L 7 3 4F A22WE 1998071400248 19980714 00248 WP 1998 7 14 SCNA98515 1 19980706 A 5320 SUPPORTS DOUG DC10 DC1015 3022118 WP BS 1908 CORROSION A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE FLOORBOARD SUPPORT AT STATION 1908 RBL56 ON THE CABIN FLOOR SUPPORT HAS LEVEL TWO CORROSION. CU T-OUT CORRODED AREA AND FABRICATED FLOOR SUPPORT AND SPLICE ANGLES PER SRM 537000 FIGURE 13 AND 530001. TREATED PARTS P ER SRM 512101 AND INSTALLED COMPLETED PER SRM 513101. 2 L 7 3 4F A22WE 1998071400249 19980714 00249 WP 1998 7 14 SCNA98514 1 19980706 A 5320 SUPPORTS DOUG DC10 DC1015 3022118 WP BS 1908 CORROSION A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE FLOORBOARD SUPPORT AT STATION 1908 LEADING EDGE OF THE RIGHT HAND AFT LAV HAS LIGHT CORROSION TH ROUGH OUT RIGHT SUPPORT. MATERIAL VERIFIED FOR FLOORBOARD SUPPORT STRUSION. FABRICATED ONE EACH FLOORBOARD PER SRM 530 001 FIG 1, TREATED PER SRM 512101, CORRODED FLOORBOARD SUPPORT. REMOVED AND PRIMED PER SRM 512102. INSTALLED ONE EACH FLOORBOARD PER SRM 530001 FIG 1 AND 513101. 2 L 7 3 4F A22WE 1998071400250 19980714 00250 NM 1998 7 14 DHL9870901C 1 19980611 A 5520 ANGLE BOEING 727 72782C 1384026 NM LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, LEFT ELEVATOR AFT EDGE SUPPORT ANGLE CRACKED AT LOWER INTERIOR SURFACE 8.5 OUTBD FROM ELEVATOR TAB INBD HIN GE. REMOVED AND REPLACED ANGLE PER SRM 55-20-1. N/R 4545. 2 L 7 3 4F A3WE 1998071400251 19980714 00251 NM 1998 7 14 DHL9870902C 1 19980611 A 5520 ANGLE BOEING 727 72782C 1384026 NM RT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, RIGHT ELEVATOR AFT EDGE SUPPORT CRACKED AT LOWER INTERIOR SURFACE 6 IN OUTBD FROM OUTBD ELEVATOR TAB HINGE . REMOVED AND REPLACED SUPPORT ANGLE PER SRM 55-20-1, N/R 4544. 2 L 7 3 4F A3WE 1998071400252 19980714 00252 NM 1998 7 14 DHL9870903C 1 19980611 A 5320 INTERCOSTAL BOEING 727 72782C 1384026 NM BS 1110 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, AFT BAGGAGE BIN INTERCOSTAL CRACKED AT UNDER SIDE RADIUS. ALSO, MISSING FASTENERS AT BS 1110 RBL 21. STO P DRILLED CRACK, HFEC, AND INSTALLED ANGLE REPAIR PER SRM 51-40-3, 10 BY 1.5 BY 1.5, N/R 3332. 2 L 7 3 4F A3WE 1998071400253 19980714 00253 NM 1998 7 14 DHL9870904C 1 19980610 A 5730 SKIN BOEING 727 72782C 1384026 NM WS 760 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, LEADING EDGE OF WING DAMAGED AT WING STATION 760.5 CUT OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER PER SRM 57-30-4, 4.5 BY 3.5, N/R 2253. 2 L 7 3 4F A3WE 1998071400254 19980714 00254 NM 1998 7 14 DHL9870905C 1 19980612 A 5730 SKIN BOEING 727 72782C 1384026 NM WS 716.5 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, LEADING EDGE OF WING DAMAGED AT WS 716.5. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-30-4, 8 BY 10. N/R 2252. 2 L 7 3 4F A3WE 1998071400255 19980714 00255 NM 1998 7 14 DHL9870906C 1 19980609 A 5751 SKIN BOEING 727 72782C 1384026 NM RT AILERON DISBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, RIGHT OUTBD AILERON UPPER SURFACE HAS PREVIOUS REPAIR, DISBONDING ATOUTBD END. INSTALLED BONDED REPAIR UPPE R AND LOWER PER SRM 51-40-6. NO BALANCE REQ'D PER SRM 51-80-4, N/R 2177. 2 L 7 3 4F A3WE 1998071400256 19980714 00256 NM 1998 7 14 DHL9870907C 1 19980615 A 5713 STRINGER BOEING 727 72782C 1384026 NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, WING UPPER STRINGER NR 9 CRACKED AT RIB ATTACH HOLE WS 656.5. STOP DRILLED CRACK, HFEC, INSTALLED HOLE REP AIR PER S/B 57A159. N/R 1887. 2 L 7 3 4F A3WE 1998071400257 19980714 00257 NM 1998 7 14 DHL9870908C 1 19980611 A 5730 SKIN BOEING 727 72782C 1384026 NM LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, LT WING LWR SKIN PANEL JUST FWD OF MLG DOOR GROUND RELEASEE HANDLE, INNER SURFACE DELAMINATED. INSTALLED BO NDED REPAIR PER SRM 51-40-6, N/R 1872. 2 L 7 3 4F A3WE 1998071400258 19980714 00258 NM 1998 7 14 DHL9870909C 1 19980609 A 5712 RIB BOEING 727 72782C 1384026 NM WS 656.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, FOUND CRACK AT STR 2 ATTACH POINT, STOP DRILLED CRACK, HFEC. INSTALLED REPAIR PER SRM 57-10-5, 12 BY 4, N/R 1810. 2 L 7 3 4F A3WE 1998071400259 19980714 00259 NM 1998 7 14 DHL9870910C 1 19980612 A 5753 FAIRING BOEING 727 72782C 1384026 NM NR 5 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, NR 5 FLAP TRACK FIXED FAIRING HAS CRACKED RIB AT AFT END. REMOVED AND REPLACED CRACKED RIB PER SRM 51-30-2, N/R 2241. 2 L 7 3 4F A3WE 1998071400260 19980714 00260 NM 1998 7 14 DHL9870911C 1 19980609 A 5755 SUPPORT BOEING 727 72782C 1384026 NM NR 8 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, RIGHT WING LOWER SUPPORT FRAME FOR NR 8 SPOILER ACTUATOR HAS CRACK. REMOVED AND REPLACED RIGHT WING LOWER S UPPORT FRAME PER SRM 51-30-2, N/R 2221. 2 L 7 3 4F A3WE 1998071400261 19980714 00261 NM 1998 7 14 DHL9870912C 1 19980609 A 5755 ANGLE BOEING 727 72782C 1384026 NM NR 12 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, RIGHT WING TRAILING EDGE LOWER SKIN SUPPORT ANGLE CRACKED AFT OF ROD SUPPORT. REMOVED AND REPLACED ANGLE P ER SRM 51-30-2, N/R 2182. 2 L 7 3 4F A3WE 1998071400262 19980714 00262 NM 1998 7 14 DHL9870913C 1 19980610 A 5320 FRAME BOEING 727 72782C 1384026 NM NLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, LEFT FWD NLG DOOR FRAME INBD SIDE BULGED UNDER SEAL RETAINER 17 IN FWD FROM AFT EDGE. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-10-3, 12 BY 4, N/R 7783. 2 L 7 3 4F A3WE 1998071400263 19980714 00263 NM 1998 7 14 DHL9870914C 1 19980609 A 5320 WEB BOEING 727 72782C 1384026 NM BS 283-294 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, HORIZ WEB LIGHTENING HOLE HAS 3 CRACKS IN NLG WHEEL WELL JUST INBD FROM RT SIDE WALL 34 IN DOWN FROM PRESSUR E DECK. REMOVED AND REPLACED WEB FROM STA 283- 294, 7 BY 4, N/R 7777. 2 L 7 3 4F A3WE 1998071400264 19980714 00264 NM 1998 7 14 DHL9870915C 1 19980601 A 5347 SEAT TRACK BOEING 727 72782C 1384026 NM BS 520 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, CENTER SEAT TRACK LOCK TABS DAMAGED AT STA 520. INSTALLED NEW SEAT TRACK FROM 500 TO 550 PER SRM 53-10-5, N /R 5379. 2 L 7 3 4F A3WE 1998071400265 19980714 00265 NM 1998 7 14 DHL9870916C 1 19980611 A 5320 ANGLE BOEING 727 72782C 1384026 NM BS 1070 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, AFT BAGGAGE BIN SIDE WALL ANGLE CRACKED AT BS 1070 APROX LBL 20. STOP DRILLED THE CRACK, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 9 BY 5, N/R 3331. 2 L 7 3 4F A3WE 1998071400266 19980714 00266 NM 1998 7 14 DHL9870917C 1 19980611 A 5347 SEAT TRACK BOEING 727 72782C 1384026 NM BS 1030 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, AFT BAGGAGE BIN FLOOR TRACK CRACKED AT UNDERSIDE RADIUS BS 1030 AND LBL 17. REMOVED AND REPLACED FLOOR TRAC K PER SRM 53-10-5 FROM BS 950 TO 1060, N/R 3330. 2 L 7 3 4F A3WE 1998071400267 19980714 00267 NM 1998 7 14 DHL9870918C 1 19980611 A 5347 SEAT TRACK BOEING 727 72782C 1384026 NM BS 1010 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, AFT BAGGAGE FLOOR TRACK CRACKED AT LBL 17 AND APPROX FROM BS 990 TO 1010. REMOVED AND REPLACED SEAT TRACK F ROM 950 TO 1060, N/R 3329. 2 L 7 3 4F A3WE 1998071400268 19980714 00268 NM 1998 7 14 DHL9870919C 1 19980609 A 5320 ANGLE BOEING 727 72782C 1384026 NM BS 1336 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, AFT AIRSTAIRS RT SIDE, FS 1336 RBL 20.5 ANGLE CRACKED AT RT LOWER TORQUE BOX UPPER FLOOR LEVEL. REMOVED AND INSTALLED NEW ANGLE PER SRM 51-10-1, 5 BY 4, N/R 3286. 2 L 7 3 4F A3WE 1998071400269 19980714 00269 NM 1998 7 14 DHL9870920C 1 19980609 A 5754 BRACKET BOEING 727 72782C 1384026 NM NR 6 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, NR 6 LEADING EDGE FLAP ACTUATOR MOUNT IS CRACKED BOTH SIDES OF ACTUATOR. REMOVED AND REPLACED BRACKET PER SRM 57-20-1, 10 BY 10, N/R 2161. 2 L 7 3 4F A3WE 1998071400270 19980714 00270 NM 1998 7 14 DHL9870921C 1 19980609 A 5712 RIB BOEING 727 72782C 1384026 NM WS 330 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, LEADING EDGE RIB IS CRACKED AT REPAIR AT WING STA 330.0. REMOVED AND REPLACED RIB PER SRM 51-40-3, 1 BY 2 F T BY 15.5, N/R 2159. 2 L 7 3 4F A3WE 1998071400271 19980714 00271 NM 1998 7 14 DHL9870922C 1 19980612 A 5730 SKIN BOEING 727 72782C 1384026 NM WS 716.5 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, LEADING EDGE OF WING IS DAMAGED AT WS 716.5. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 57-3 0-4, 5 FT BY 6.5, N/R 1883. 2 L 7 3 4F A3WE 1998071400272 19980714 00272 NM 1998 7 14 DHL9870923C 1 19980609 A 5712 RIB BOEING 727 72782C 1384026 NM WS 686.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, FOUND CRACK AT RIB STA 686.5. STOP DRILLED, HFEC. INSTALLED RIB REPAIR PER SRM 51-10-2, 12 BY 4, N/R 1812. 2 L 7 3 4F A3WE 1998071400273 19980714 00273 NM 1998 7 14 DHL9870924C 1 19980609 A 5712 RIB BOEING 727 72782C 1384026 NM WS 738 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, CRACK FOUND ON RIB STA 738.5. STOP DRILLED CRACK, HFEC. INSTALLED REPAIR PER SRM 57-10-5, 12 BY 4, N/R 18 11. 2 L 7 3 4F A3WE 1998071400274 19980714 00274 NM 1998 7 14 DHL9870925C 1 19980609 A 5712 RIB BOEING 727 72782C 1384026 NM WS 629 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, 2 CRACKS FOUND AT RIB LOWER FLANGE ATTACH POINT, HFEC. STOP DRILLED AND REPAIR PER SRM 57-10-5, 12 BY 4, N/ R 1809. 2 L 7 3 4F A3WE 1998071400275 19980714 00275 NM 1998 7 14 DHL9870926C 1 19980609 A 5712 RIB BOEING 727 72782C 1384026 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, FOUND CRACKS ON RIB AT 601.5, L/W. STOP DRILL, HFEC, INSTALL RIB REPAIR PER SRM 57-10-5, 12 BY 4, N/R 1808. 2 L 7 3 4F A3WE 1998071400276 19980714 00276 NM 1998 7 14 DHL9870927C 1 19980617 A 7110 ANGLE BOEING 727 72782C 1384026 NM NR 1 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, NR 1 ENGINE UPPER COWL HAS T ANGLE CRACKED AT AFT OUTBD CORNER OF COWL INTERIOR, JUST AFT OF NR 7 COWL LATCH . REPLACED ANGLE PER SRM 54-10-2, 8 BY 10 FT, N/R 6711. 2 L 7 3 4F A3WE 1998071400277 19980714 00277 NM 1998 7 14 DHL9870928C 1 19980612 A 5753 6521795U283 FAIRING BOEING 727 72782C 1384026 NM NR 4 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, NR 4 FLAP TRACK FIXED FAIRING HAS CRACKED RIB AT AFT END. REMOVED AND REPLACED FAIRING RIB PER SRM 51-30-2 , N/R 1877. 2 L 7 3 4F A3WE 1998071400278 19980714 00278 NM 1998 7 14 DHL9870929C 1 19980618 A 5320 ANGLE BOEING 727 72782C 1384026 NM BS 848 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, FLOOR SUPPORT CRACKED BS 848 RBL 27. INSTALLED FORMED ANGLE REPAIR PER SRM 51-40-3, 6 BY 3, N/R 5437. 2 L 7 3 4F A3WE 1998071400279 19980714 00279 NM 1998 7 14 DHL9870930C 1 19980609 A 5320 ANGLE BOEING 727 72782C 1384026 NM BS 1272 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, AFT AIRSTAIR RT SIDE FS 1272, RBL 22 SUPPORT ANGLE CRACKED, FWD OF INBD FASTENER, UNDER AFT AIRSTAIRS ACTUAT ING MECHANISM, AFT SIDE OF WEB RT LOWER TORQUE BOX. REMOVED AND REPLACED SUPPORT ANGLE PER S/B 53-0129, N/R 3289. 2 L 7 3 4F A3WE 1998071400280 19980714 00280 NM 1998 7 14 DHL9870931C 1 19980610 A 5753 FLAP TRACK BOEING 727 72782C 1384026 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, RIGHT WING FLAP TRACK HAS CRACK ABOVE RT MAIN LANDING GEAR AT DOUBLER REPAIR. REMOVED AND FABRICATED NEW DO UBLER PER SRM 57-30-1, 1 FT BY 2 FT, N/R 2231. 2 L 7 3 4F A3WE 1998071400281 19980714 00281 NM 1998 7 14 DHL9870932C 1 19980610 A 5754 69179002 BRACKET BOEING 727 72782C 1384026 NM NR 8 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, NR 8 INBD FLAP TRACK FAIRING ATTACH BRACKET CRACKED. REMOVED AND REPLACED PER SRM 51-30-2, N/R 2229. 2 L 7 3 4F A3WE 1998071400282 19980714 00282 NM 1998 7 14 DHL9870933C 1 19980609 A 5320 ANGLE BOEING 727 72782C 1384026 NM BS 1270 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, AFT AIRSTAIRS RIGHT SIDE FS 1270 RBL 21 ANGLE CRACK IN ACTUATING SUPPORT MECHANISM. REMOVED AND REPLACED B EAM, GUSSETT, STIFFENER ANGLE PER S/B 53-0129, N/R 3288. 2 L 7 3 4F A3WE 1998071400283 19980714 00283 NM 1998 7 14 DHL9870934C 1 19980620 A 5320 RIB BOEING 727 72782C 1384026 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, CLOSURE RIB IS CRACKED AND BENT AT MCD OPENING FWD SIDE OF FRAME FS 480 STR 5 LT. REMOVED AND REPLACED NEW CLOSURE RIB PER SRM 53-10-2, 36 BY 12, N/R 5439. 2 L 7 3 4F A3WE 1998071400284 19980714 00284 NM 1998 7 14 DHL9870935C 1 19980620 A 5320 RIB BOEING 727 72782C 1384026 NM BS 620 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, CLOSURE RIB IS BENT AND CRACKED AT MCD. OPENING AFT SIDE ON FRAME FS 620, STR 5 LT. REMOVED AND REPLACED C LOSURE RIB PER SRM 53-10-3, 36 BY 12, N/R 5440. 2 L 7 3 4F A3WE 1998071400285 19980714 00285 NM 1998 7 14 DHL9870936C 1 19980613 A 5230 DOUBLER BOEING 727 72782C 1384026 NM CARGO DOOR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, FWD LOWER CARGO INTERIOR DOUBLER AT EXTERIOR DOOR HANDLE CUTOUT CORRODED. REMOVED INTERIOR DOUBLER, FABRIC ATED AND INSTALLED PER SRM 52-30-1, 12 FT BY 27, N/R 3416. 2 L 7 3 4F A3WE 1998071400286 19980714 00286 NM 1998 7 14 DHL9870937C 1 19980611 A 5350 TAIL CONE BOEING 727 72782C 1384026 NM EMPENNAGE DISBONDED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 709DH 19968 AT C CHECK, VERTICAL STAB TAIL CONE HAS METAL DOUBLER DISBONDING AT UPPER SURFACE. INSTALLED BONDED REPAIR PER SRM 51-2 0-3, N/R 4557. 2 L 7 3 4F A3WE 1998071400287 19980714 00287 WP 1998 7 14 RRXA98246 1 19980325 A 5330 5758874 SKIN DOUG DC8 DC873F 302199F WP BS 80-90 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERIOR SKIN BETWEEN STA 80 TO STA 90 AND LONGERON 27 LEFT. REMO VED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO D ER ENGINEERING SKETCH REO-04506. 2 L 7 4 4F RT 4A25 1998071400288 19980714 00288 WP 1998 7 14 EIAA980194 1 19980317 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 963 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, LONGERON 16L CRACKED AT BS 963. REPAIRED LONGERON PER SRM 53-02 FIG 18. (X) 2 L 7 2 4F A6WE 1998071400289 19980714 00289 WP 1998 7 14 EIAA980193 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 832 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48378 47194 MZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED AT BS 832 FROM STR 27R TO STR 28R. REPAIRED FLOOR SUP PORT PER DPS 10-255. (X) 2 L 7 2 4F A6WE 1998071400290 19980714 00290 WP 1998 7 14 EIAA980192 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 794 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED AT BS 794 FROM STR 29L TO STR 28L. REPAIRED FLOOR SUP PORT PER DPS 10-255. (X) 2 L 7 2 4F A6WE 1998071400291 19980714 00291 WP 1998 7 14 EIAA980191 1 19980318 A 5320 99220422 FITTING DOUG DC9 DC933F 302207A WP BS 256 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, FRAME ATTACH FITTING CRACKED AT BS 256 AT STR 24R. REPLACED FRAME ATTACH FITTING PER SRM'S 51- 30-02 AND 51-10-03. (X) 2 L 7 2 4F A6WE 1998071400292 19980714 00292 WP 1998 7 14 EIAA980190 1 19980318 A 5320 STIFFENER DOUG DC9 DC933F 302207A WP BS 796 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MJZ - DURING 'C5' CHECK, BS 796 BULKHEAD LOWER STIFFENER IS BENT AT BL ZERO. REPLACED STIFENER PER SRM'S 51-10-03 AND 5 1-30-05. (X) 2 L 7 2 4F A6WE 1998071400293 19980714 00293 WP 1998 7 14 EIAA980189 1 19980318 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 275 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MJZ - DURING 'C5' CHECK, FUSELAGE FRAME LOWER CHORD CRACKED AT BS 275 FROM STR 29L - STR 29R. REPAIRED FRAME PER SRM 53 -03, FIG 5. (X) 2 L 7 2 4F A6WE 1998071400294 19980714 00294 WP 1998 7 14 EIAA980188 1 19980319 A 5320 59161751 FITTING DOUG DC9 DC933F 302207A WP BS 604 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, ATTACH FITTING IN LOWER WING TO FUSELAGE FILLET AREA AT BS 604 AT LBL 39, HAS 2 INCH CRACK. RE PLACED FITTING PER SRM 51-30-5. (X) 2 L 7 2 4F A6WE 1998071400295 19980714 00295 WP 1998 7 14 EIAA980187 1 19980318 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 965 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME AT BS 965 LONGERON 30 CRACKED AND CORRODED. REPAIRED FRAME PER SR M 53-03 PAGES 4A-4J. (X) 2 L 7 2 4F A6WE 1998071400296 19980714 00296 WP 1998 7 14 EIAA980186 1 19980318 A 5320 INTERCOSTAL DOUG DC9 DC933F 302207A WP BS 937 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, AFT PIT, LONGERON INTERCOSTAL CRACKED AND CORRODED AT BS 937 AT LONGERON 29R. REPLACED INTERCO STAL ON LONGERON 29R PER SRM 51-30-02. (X) 2 L 7 2 4F A6WE 1998071400297 19980714 00297 WP 1998 7 14 EIAA980185 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 256 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 256 AT STR 29R. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400298 19980714 00298 WP 1998 7 14 EIAA980183 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 351 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 351 FROM STR 25R - STR 26R , AND STR 28R - STR 29R. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400299 19980714 00299 WP 1998 7 14 EIAA980182 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 313 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 313 AT STR 25L AND STR 26L . REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400300 19980714 00300 WP 1998 7 14 EIAA980181 1 19980319 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 427 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 427 AT STR 26. REPAIRED F LOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400301 19980714 00301 WP 1998 7 14 EIAA980180 1 19980319 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 390 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, FORWARD PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 390 AT STR 26. REPAIRED F LOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400302 19980714 00302 WP 1998 7 14 EIAA980179 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 851 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME CRACKED IN UPPER CHORD RADIUS AT BS 851 AT STR 24L TO STR 25LR. R EPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400303 19980714 00303 WP 1998 7 14 EIAA980178 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 794 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, AFT PIT, FLOOR SUPPORT FRAME ATTACH FITTING CRACKED IN UPPER CHORD RADIUS AT BS 794 AT STR 28R. REPAIRED FLOOR SUPPORT FRAME WITH WELDING REPAIR DPS 10-225. (X) 2 L 7 2 4F A6WE 1998071400304 19980714 00304 WP 1998 7 14 EIAA980177 1 19980318 A 5320 SUPPORT DOUG DC9 DC933F 302207A WP BS 965 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 MZJ - DURING 'C5' CHECK, AFT PIT FLOOR SUPPORT FRAME CRACKED AT BS 965 AT STR 30. REPAIRED FLOOR SUPPORT FRAME PER SRM 53-03 FIG 2A. (X) 2 L 7 2 4F A6WE 1998071400305 19980714 00305 EA 1998 7 14 98ZZZX2339 1 19980531 A 2150 SZ430031A MOTOR SZ430021 DHAV DHC6 DHC6300 EA A/C COMPRESSOR FAILED A ASWA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 07 146SA 514 CREW REPORTED SMELLING SMOKE AND SMELL WENT AWAY AFTER LT DC BUSS WAS SHUT DOWN. MAINTENANCE PERSONNEL REPLACED AIR CON DITIONING COMPRESSOR MOTOR. AIR CONDITIONING SYSTEM IS INSTALLED ON THIS AIRCRAFT UNDER SUPPLEMENTAL TYPE CERTIFICATE N R SA4622SW. 1 H 7 2 3T A9EA 1998071400306 19980714 00306 SO 1998 7 14 GLBA98088 1 19980527 A 5313 12006173003 STRINGER EMB 120 EMB120RT SO FUSELAGE CRACKED A GLBA K NONE O OTHER IN INSP/MAINT 1 CE 01 452UE 21658 120096 FUSELAGE SKIN FLEXING UNDER AFT PASSENGER DOOR. ACTUATOR SUPPORT BRACKET HAS LOOSE RIVETS. FURTHER INSPECTION REVEALS CORROSION ON NR 10 STRINGER AND BRACKET. REPAIRED NR 10 STRINGER IAW EMB-120 SRM 53-00-03. (X) 2 L 7 2 4T RT A31SO 1998071400307 19980714 00307 WP 1998 7 14 GTIA9800066 1 19980610 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 SECTION OF EMERGENCY FLOOR TRACK LIGHTING IS INOPERATIVE (TOWARDS REAR OF CABIN). REPAIRED FAULTY WIRE (PULLED FROM BUTT SPLICE) OPERATION GOOD. REFERENCE: MM 33-50-0. (X) 2 L 7 2 4F A6WE 1998071400308 19980714 00308 NM 1998 7 14 EISA98128 1 19980605 A 2611 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO COMPT DAMAGED A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 CARGO SMOKE ILLUMINATED 4 TIMES, VERIFIED NO SMOKE. GENERATED FROM PILOT REPORT. REMOVED ALL SMOKE DETECTORS, BLEW OUT ALL LINES WITH NITROGEN. REPLACED 3 EACH DAMAGED FLEX LINES, REINSTALLED ALL DETECTORS. NO DEECTS NOTED. UNABLE TO D UPLICATE. IAW 26-10-00. (X) 2 L 7 3 4F A3WE 1998071400309 19980714 00309 NM 1998 7 14 EISA98127 1 19980531 A 3610 CLAMP BOEING 727 7272A7 138407K NM NR 1 ENGINE LOOSE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 310NE 20241 CLIMGING THROUGH 16,000 FEET AT 91 PERCENT N1, GOT A NR 1 STRUT OVERHEAT LIGHT OUT WITH THROTTLE RETARDED. SWAPPED NR 1 AND NR 3 BLEEDS PER AOM WITH NO RECURRENCE IN-FLIGHT. GENERATED FROM PILOT REPORT. TROUBLESHOT SYSTEM TO LOOSE CLAMP. TIGHTENED CLAMP. SYSTEM OPS CHECK NORMAL ON GROUND. (X) 2 L 7 3 4F A3WE 1998071400310 19980714 00310 NM 1998 7 14 EISA98126 1 19980605 A 2131 1310083 CONTROLLER BOEING 727 727223 1384074 NM CABIN MALFUNCTIONED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 311NE 56885 19703 WHILE CLIMBING THROUGH FL 240, CABIN BEGAN A CLIMB OF GREATER THAN 2,000 FPM. PERFORMED CHECKLIST, CABIN CONTINUED TO C LIMB UNCONTROLLABLY. RETURNED TO SAN JUAN (SJU). GENERATED FROM PILOT REPORT. REMOVED AND REPLACED AIR DISTRIBUTION D UCT PER MM, CHAPTER 21-20-00. REMOVED AND REPLACED MANUAL PRESSURE CONTROLLER PER MM CHAPTER 21-30-00. (X) 2 L 7 3 4F A3WE 1998071400311 19980714 00311 WP 1998 7 14 EISA98125 1 19980527 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN LOOSE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 950VJ 47564 AFT MOST EMERGENCY PATH BULB OUT OF TRACK. GENERATED FROM PILOT REPORT. REINSTALLED AFT MOST EMERGENCY PATH BULB COVER . LIGHTS CHECK GOOD PER MM CHAPTER 33-53-1. (X) 2 L 7 2 4F A6WE 1998071400312 19980714 00312 WP 1998 7 14 EISA98124 1 19980605 A 3320 P401002D BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 943VJ 47058 SLIDE ACTIVATED LIGHT FOR GALLEY SIDE DOOR INOPERATIVE. GENERATED FROM MAINTENANCE REPORT. REPLACED BATTERY PACK PER M M 33-50-1. OPS CHECK NORMAL. (X) 2 L 7 2 4F A6WE 1998071400313 19980714 00313 NM 1998 7 14 EISA98123 1 19980609 A 7830 BACH700161DL HOSE BOEING 727 7272A7 138407K NM NR 1 ENGINE CHAFED A EISA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 310NE 20241 AFTER TAKEOFF, INDIANAPOLIS (IND) WHILE CLIMBING THROUGH APPROXIMATELY 3,000 FEET, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLU MINATED. AOM ABNORMAL. C/W ENGINE NR 1, THRUST REDUCED, LIGHT EXTINGUISHED AFTER ABOUT 1 MINUTE COOLING. RETURNED TO (IND). GENERATED FROM PILOT REPORT. FOUND NR 1 ENGINE THRUST REVERSER HIGH PRESSURE HIGH TEMP HOSE CHAFFED THROUGH. R EPLACED. LEAK CHECK AND FUNCTION TESTED SYSTEM. OK FOR SERVICE IAW 78-30. (X) 2 L 7 3 4F A3WE 1998071400314 19980714 00314 NM 1998 7 14 EISA98122 1 19980525 A 7722 LINE BOEING 727 72731 1384010 NM NR 3 ENGINE CONTAMINATED A EISA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 240NE 18906 TAKEOFF ABORTED (BDL) BRADLEY DUE TO NR 3 ENGINE ABNORMAL EPR READING (HIGH). EGT, N1 NORMAL. THROTTLE 3 INCHES AFT OF NORMAL POSITION. FOUND MOISTURE IN PT 2 LINE. CLEARED LINE. OPS CHECK SATISFACTORY. (X) 2 L 7 3 4F A3WE 1998071400315 19980714 00315 NM 1998 7 14 EISA98121 1 19980525 A 2611 30284 DETECTOR BOEING 727 72725 1384006 NM CARGO COMPT MALFUNCTIONED A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 290NE 3747 18972 CARGO SMOKE LIGHT ILLUMINATED IN-FLIGHT. SYSTEM WILL NOT TEST IN-FLIGHT. TEST OK ON GROUND. GENERATED FROM PILOT REPO RT. REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW AERONAUTICAL MM. CHECKS GOOD. (X) 2 L 7 3 4F A3WE 1998071400316 19980714 00316 NM 1998 7 14 EISA98120 1 19980529 A 2611 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO COMPT CONTAMINATED A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 ON LAST LEG, CARGO SMOKE LIGHT ILLUMINATED HALF WAY THROUGH FLIGHT. NO SMOKE FOUND IN CARGO COMPARTMENT. GENERATED FRO M PILOT REPORT. PURGED ALL SMOKE DETECTOR HOSES WITH NITROGEN. SMOKE DETECTOR SYSTEM CHECKS NORMAL ON GROUND IAW AERON AUTICAL MANUAL. (X) 2 L 7 3 4F A3WE 1998071400317 19980714 00317 SO 1998 7 14 MASA98124 1 19980608 A 3350 10130115 LIGHT 12060342003 EMB 120 EMB120RT SO CABIN CRACKED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 180YV 120180 DURING ROUTINE MAINTENANCE, FOUND LEFT FORWARD EMERGENCY EXIT LIGHT ASSEMBLY CRACKED. REMOVED AND REPLACED LIGHT ASSEMB LY. (X) 2 L 7 2 4T RT A31SO 1998071400318 19980714 00318 NM 1998 7 14 98ZZZX2340 1 19980524 A 5521 SPAR BOEING 727 727251 138408H NM LT ELEVATOR CRACKED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282US 21161 DURING A SCHEDULED INSPECTION, FOUND THE LT ELEVATOR REAR SPAR CRACKED , 1 INCH LONG. CRACK EMANATES FROM LOWER INBOARD CORNER OF HINGE BRACKET SHEAR PLATE AT BS 66.50 AND PROTRUDES TO UPPER OUTBOARD STIFFENER MOUNT HOLE. N/R NR J0012/128 872. 2 L 7 3 4F A3WE 1998071400319 19980714 00319 NM 1998 7 14 SQ7A98282 1 19980520 A 5315 FLOORBEAM BOEING 727 727251 138408H NM BS 400 CORRODED A SQ7A K NONE O OTHER IN INSP/MAINT 1 SO 01 282US 21161 DURING A SCHEDULED INSPECTION AT LAKE CITY (AERO CORP) FLOOR BEAM AT STA 400 BL ZERO. UPPER CAP WAS FOUND CORRODED BEYO ND LIMITS. N/R NR 128746. W/O 060H1-0134. (X) 2 L 7 3 4F A3WE 1998071400320 19980714 00320 WP 1998 7 14 TWAA9809301 1 19980414 A 5412 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT PYLON UPPER AFT BULKHEAD ANGLE CRACKED AT INBOARD AND OUTBOARD ENDS. MAD E AND INSTALLED NEW ANGLE PER SRM 51-01, PAGE 1, ITEM C. (X) 2 L 7 2 4F A6WE 1998071400321 19980714 00321 WP 1998 7 14 TWAA9809302 1 19980330 A 5330 SKIN DOUG DC9 DC932 3022066 WP CARGO DOORWAY DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN RT SIDE AFT OF AFT CARGO DOOR. FOUND INTERIM REPAIR I NSTALLED. INSTALLED CLASS 1 REPAIR PER SRM 53-04, FIG 12B. (X) 2 L 7 2 4F A6WE 1998071400322 19980714 00322 WP 1998 7 14 TWAA9809303 1 19980430 A 5400 FITTING DOUG DC9 DC932 3022066 WP RT PYLON CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT PYLON WITH CORROSION ON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CO RROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 54-04, FIG 13, AND PLATED PER SR M 54-04, PAGE 53, ITEM 4. (X) 2 L 7 2 4F A6WE 1998071400323 19980714 00323 WP 1998 7 14 TWAA9809304 1 19980414 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 1104 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND 1104 CANTED BULKHEAD AT NR 3 LONGERON RT AND LT SIDE, WITH 2 EACH FASTENERS MISSING. HFEC AREA FOUND 2 INCH CRACK. REPAIRED PER SRM 53-05, PAGE 49. (X) 2 L 7 2 4F A6WE 1998071400324 19980714 00324 WP 1998 7 14 TWAA9809305 1 19980403 A 5400 FITTING DOUG DC9 DC932 3022066 WP NR 1 PYLON CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON NR 1 PYLON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORRO SION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 5-04, FIG 13 AND PLATED PER SRM 54- 04, PAGE 53, ITEM 4. (X) 2 L 7 2 4F A6WE 1998071400325 19980714 00325 WP 1998 7 14 TWAA9809306 1 19980327 A 5411 FRAME DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND NR 1 PYLON LOWER END CHORD ANGLE CRACKED, 60 INCHES AFT OF LEADING EDGE, 4 I NCHES INBOARD AT OUTBOARD END. INSTALLED DOUBLER PER SRM 54-01, FIG 2, PAGE 7. (X) 2 L 7 2 4F A6WE 1998071400326 19980714 00326 WP 1998 7 14 TWAA9809307 1 19980331 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CLASS III REPAIR INSTALLED ABOVE AND JUST FORWARD OF EXTERNAL POWER RECEPTAC LE. INSTALLED CLASS I REPAIR PER SRM 53-04, FIGURE 12 B. (X) 2 L 7 2 4F A6WE 1998071400327 19980714 00327 WP 1998 7 14 TWAA9809308 1 19980327 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 71 INDICATING CRACKED, LOWER REAR SPAR RT XRS 200. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X) 2 L 7 2 4F A6WE 1998071400328 19980714 00328 WP 1998 7 14 TWAA9809309 1 19980327 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 154 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 43 INDICATING CRACK WITH HFEC, RT WING LOWER REAR SPAR STA XR S 154. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X) 2 L 7 2 4F A6WE 1998071400329 19980714 00329 WP 1998 7 14 TWAA9809310 1 19980323 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 89 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE FRAME STA 89 WITH CRACK IN OUTBOARD RADIUS BETWEEN LONGERONS 18 AND 19. STOP DRILLED CRACK PER SRM 51-10 AND REPAIRED PER SRM 53-01, PAGE 10, FIGURE 2. (X) 2 L 7 2 4F A6WE 1998071400337 19980714 00337 NM 1998 7 14 USAA980226 1 19980522 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 41429 22885 ROA - DURING J28 (BX) FOUND 1.50 INCH CRACK AT BS 767 S19L ON FUSELAGE SKIN. REMOVED CRACK AND INSTALLED DOUBLER PER SR M 53-30-3 FIG 6. (X) 2 L 7 2 4F A16WE 1998071400338 19980714 00338 NM 1998 7 14 USAASB98129 1 19980530 A 7930 1163P181 SWITCH BOEING 737 7372B7 1384560 NM NR 2 ENGINE FAILED A USAA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 EA 19 275AU 1765 22887 PIT - FLT 8565 - ON DESCENT INTO PIT, THE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. CRE W DECLARED AN EMERGENCY AND SHUT DOWN THE NR 2 ENGINE PER APPROPRIATE CHECKLIST. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL FILTER BYPASS SWITCH AND CLEANED THE CANNON PLUG. OPERATED ENGINE AT ALL PARAMETERS. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998071400339 19980714 00339 NM 1998 7 14 USAASB98128 1 19980530 A 3610 BACC10CT2100 CLAMP BOEING 737 737201 1384454 NM LT A/C BAY LOOSE A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 259AU 22806 CLT - FLT 338 - FLIGHT DEPARTED CLT AND RIGHT PACK ON MEL. SHORTLY AFTER LIFTOFF, THE LEFT WING BODY OVERHEAT LIGHT ILL UMINATED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND BLOWING HOT AIR COMING FROM CLAMPS THAT WERE LOOSE ON THE LEFT PRIMARY HEAT EXCHANGER AND TURBOFAN. TIGHTENED LO OSE CLAMPS. OPERATIONAL CHECK NORMAL. NO LEAKS NOTED. (X) 2 L 7 2 4F A16WE 1998071400340 19980714 00340 EU 1998 7 14 USAAF98047 1 19980602 A 3230 DAMPER FOKKER F28 F28MK0100 4990807 EU RT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 854US 11282 PIT - FLT 1696 - AFTER DEPARTURE FROM PIT, 'RT MLG' MESSAGE APPEARED ON MULTIFUNCTION DISPLAY AND BLUE INTRANSIT LIGHTS REMAINED ON IN GEAR HANDLE. CREW RECYCLED GEAR WITH SAME RESULT. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INC IDENT. MAINTENANCE SERVICED THE RIGHT MAIN GEAR UPSTOP DAMPER. GEAR SWING WAS GOOD. (X) 2 L 7 2 4F RT 1998071400341 19980714 00341 NM 1998 7 14 USAASB98132 1 19980601 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 234US 22274 ALB - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE FLIGHT DECK EMERGENCY EVACUATION EXIT LIGHT IN THE CEILING TO BE INO PERABLE WHEN SWITCHED ON FROM THE OVERHEAD PANEL. LIGHT OPERATES NORMALLY WHEN SWITCHED ON AT EXIT LIGHT BATTERY PACK. MAINTENANCE REMOVED AND REPLACED THE FLIGHT DECK LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4F A16WE 1998071400342 19980714 00342 1998 7 14 USAAF98045 4 19980524 A 3444 959960714901 RT UNIT FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 881US 15677 11333 PIT - FLT 0669 - AFTER TAKEOFF FROM PIT, RA FLAG ON PFD ILLUMINATED ALONG WITH THE FOLLOWING FAULT MESSAGES: GPWS, ALAN D, STAB TRIM 1. THE NR 1 AUTOPILOT DISENGAGED. FLIGHT RETURNED TO PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED T HE NR 1 RADIO ALTIMETER RECEIVER/TRANSMITTER. (X) 2 L 7 2 4F RT 1998071400343 19980714 00343 EU 1998 7 14 USAAF98046 1 19980525 A 2740 231563 SENSOR FOKKER F28 F28MK0100 4990807 EU NR 2 STAB FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 866US 11310 CLT - FLT 8076 - EN ROUTE TO MSP, THE FOLLOWING MESSAGES APPEARED ON THE PFD: HYD STAB 2, HYD STAB 1&2, STAB TRIM 1&2. FLIGHT DIVERTED TO PIT FOR MAINTENANCE. FLIGHT LANDED PIT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 STA BILIZER PROXIMITY SENSOR SWITCH. (X) 2 L 7 2 4F RT 1998071400344 19980714 00344 NM 1998 7 14 USAASB98125 1 19980527 A 3350 1012623 LIGHT BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 266AU 22878 BWI - PILOT REPORTED THREE SEAT MOUNTED SINGLE BULB FIXTURES WERE FOUND INOPERATIVE AT THE EMERGENCY EXIT ROW. MAINTENA NCE REMOVED AND REPLACED THE EMERGENCY EXIT SIGN LIGHT ASEMBLY AND WIRE SAME. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998071400345 19980714 00345 NM 1998 7 14 USAASB98119 1 19980523 A 2410 A3164A DRAIN PLUG BOEING 737 737201 1384454 NM NR 2 ENGINE CSD LEAKING A USAA A UNSCHED LANDING K J H FLUID LOSS WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 251AU 22757 ATL - FLT 1901 - THE NR 2 ENGINE CSD LOW OIL PRESSURE LIGHT ILLUMINATED INTERMITTENTLY DURING CRUISE ALTITUDE. SINCE TH E APU WAS ALREADY ON MEL, DECISION WAS MADE TO TURN TOWARDS AN ALTERNATE AIRPORT. WHILE EN ROUTE TOWARDS ATL, THE CSD O IL PRESSURE WENT TO ZERO. CREW DISCONNECTED THE NR 2 ENGINE CSD PER HANDBOOK AND DIVERTED TO ATL. FLIGHT LANDED WITHOU T FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE MAGNETIC DRAIN PLUG ASSEMBLY CRACKED ON THE NR 2 ENGINE CSD. REPLACED PLUG ASSEMBLY. SERVICED AND RECONNECTED CSD. REPLACED BREAKAWAY WIRE ON NR 2 CSD SWITCH. OPS AN D LEAK CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998071400346 19980714 00346 NM 1998 7 14 USAASB98124 1 19980527 A 2410 CSD BOEING 737 737201 1384454 NM NR 2 ENGINE OVERSERVICED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 251AU 22757 MCO - FLT 806 - DURING CLIMB-OUT FROM FLL WITH THE APU ON MEL, THE NR 2 ENGINE CSD HIGH OIL TEMPERATURE LIGHT ILLUMINATE D AND THE TEMPERATURE INDICATOR SHOWED EXCESSIVE 'IN' TEMPERATURE. CREW DISCONNECTED THE NR 2 ENGINE CSD PER ABNORMAL P ROCEDURES AND DIVERTED TO MCO WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND T HE NR 2 ENGINE CSD OVERSERVICED. DRAINED CSD TO PROPER LEVEL, RECONNECTED CSD, AND RAN ENGINE. OPERATIONAL CHECK GOOD. REPLACED BREAKAWAY WIRE ON NR 2 CSD SWITCH. (X) 2 L 7 2 4F A16WE 1998071400347 19980714 00347 NM 1998 7 14 USAASB98120 1 19980524 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 227AU 21816 CLE - MAINTENANCE FOUND THE CENTER AISLE OVERWING EMERGENCY EXIT SIGN INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998071400348 19980714 00348 NM 1998 7 14 USAASB98122 1 19980525 A 3350 900835A BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 264AU 22961 ROC - MAINTENANCE FOUND THE FORWARD GALLEY INTERIOR AND EXTERIOR ENTRANCE AND SERVICE DOOR EMERGENCY LIGHTS WOULD NOT IL LUMINATE. ALSO, FOUND THE FORWARD SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN INOPERABLE. MAINTENANCE REMOVED AND REPLAC ED THE BATTERIES. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998071400349 19980714 00349 NM 1998 7 14 USAASB98133 1 19980601 A 3350 LIGHT BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 395US 23317 ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 5, 6, 7, 9, AND 11. MAINTENANCE REPAIRED EMERGENC Y LIGHT WIRING AT SEAT ROWS 7 AND 8, LEFT HAND SIDE. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998071400350 19980714 00350 NM 1998 7 14 USAAB98060 1 19980527 A 3350 20131ALP BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 603AU 22198 LAX - FOUND L-2 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTEANCE REPLACED THE BATTERY PACK. (X) 2 L 7 2 4F RT A2NM 1998071400351 19980714 00351 NM 1998 7 14 USAABB98057 1 19980512 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 615AU 27146 LAX - FOUND ALL LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL THE BATTERIES. (X) 2 L 7 2 4F RT A2NM 1998071400352 19980714 00352 NM 1998 7 14 USAA980232 1 19980512 A 5330 SKIN BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 404US 27730 23886 CLT - DURING A RON VISUAL INSPECTION, FOUND A .75 INCH CRACK AT RIGHT FUSELAGE STA 727E AT STR 23R ON THE SKIN. INSTALL ED DOUBLER PER EA 61760. 2 L 7 2 4F RT A16WE 1998071400353 19980714 00353 NM 1998 7 14 USAA980233 1 19980527 A 5330 65C257273 SKIN BOEING 737 7374B7 1384702 NM BS 124 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 779AU 21023 24996 CLT - DURING C-CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .1250 INCH CRACK AT STAB 124, LT HORIZONTAL STABILZIER LOWER SKIN. INSTALLED DOUBLER PER TYPICAL REPAIR 55-10-07. (X) 2 L 7 2 4F RT A16WE 1998071400354 19980714 00354 NM 1998 7 14 USAASB98127 1 19980529 A 2150 8012403 TURBOFAN BOEING 737 737401 1384701 NM RT PACK MALFUNCTIONED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 413US 23882 CLT - FLT 2250 - DURING APPROACH, PILOT REPORTED A FOUL OIL SMELL CAME FROM THE AIR CONDITIONING PACKS INTO THE CABIN AS THE FLAPS WERE LOWERED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK TURBO FAN AND TURBOFAN CONTROL VALVE. SYSTEM LEAK CHECK AND OPS CHECK GOOD. NO FURTHER OIL SMELL NOTED THROUGHOUT CABIN. RE F: OPERATOR CONTROL NR 98ZZZX2341. (X) 2 L 7 2 4F RT A16WE 1998071400355 19980714 00355 NM 1998 7 14 98ZZZX2341 1 19980529 A 2150 39237831 CONTROL VALVE BOEING 737 737401 1384701 NM RT PACK MALFUNCTIONED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 413US 23882 CLT - FLT 2250 - DURING APPROACH, PILOT REPORTED A FOUL OIL SMELL CAME FROM THE AIR CONDITIONING PACKS INTO THE CABIN AS THE FLAPS WERE LOWERED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK TURBO FAN AND TURBOFAN CONTROL VALVE. SYSTEM LEAK CHECK AND OPS CHECK GOOD. NO FURTHER OIL SMELL NOTED THROUGHOUT CABIN. RE F: OPERATOR CONTROL NR USAASB98127. 2 L 7 2 4F RT A16WE 1998071400356 19980714 00356 NE 1998 7 14 USAASB98130 2 19980530 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE LEFT FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J Y OVER TEMP WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 19 247US 30976 3212 22754 709554 JAX - FLT 8097 - SHORTLY AFTER DEPARTURE FROM TPA, CREW SHUT DOWN THE NR 1 ENGINE DUE TO HIGH OIL TEMPERATURE. FLIGHT D IVERTED TO JAX AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 9 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSEMBLY PER JOB CARD, OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F 4 F A16WE E2EA 1998071400357 19980714 00357 WP 1998 7 14 EIAA980201 1 19980416 A 5510 5912481517N FITTING DOUG DC9 DC933F 302207A WP HORIZ STABILIZER MISDRILLED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 944F 47194 DURING 'C5' CHECK, HORIZONTAL STABILIZER CENTER SECTION UPPER AFT FITTING HAS CORROSION. DURING REPLACEMENT, FITTING WA S MISDRILLED. REPLACED FITTING AND REPAIRED AREA IAW ECRA 944-55-033-02. (X) 2 L 7 2 4F A6WE 1998071400358 19980714 00358 NM 1998 7 14 EIAA980200 1 19980510 A 3232 65B105856 FITTING BOEING 747 747SR46 NM BS 1265 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 55110 20784 DURING B-CHECK, KEEL BEAM BOX, RT LANDING GEAR DOOR ACTUATOR BACK-UP FITTING HAS A CRACK AT RBL 10 BS 1265. REPLACED FI TTING PER SRM 51-30-02. (X) 2 L 7 4 4F A20WE 1998071400359 19980714 00359 NM 1998 7 14 TWRA9831 1 19980605 A 2530 50000011 COFFEE MAKER BOEING 747 747212B 1384886 NM CABIN FAILED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 6186 21439 IN FLIGHT, SMOKE SEEPING FROM AFT SLOT OF CEILING PANEL IN AFT GALLEY JUST FORWARD OF COFFEE MAKERS, TURNED OFF GALLEY P OWER AND PULLED OVEN CONTROL C/B'S, SMOKE STOPPED. INSPECTED AREA, FOUND COFFEE MAKER AT POSITION 516 WITH BURNED WIRES TO HOT JUG. REMOVED AND REPLACED COFFEE MAKER. OPS CHECK GOOD. NO OGHER DEFECTS NOTED. REACTIVATED GALLEY. (M) 2 L 7 4 4F A20WE 1998071400360 19980714 00360 NM 1998 7 14 TWRA9829 1 19980508 A 2530 OVEN BOEING 747 747131 1384881 NM GALLEY SHORTED A TWRA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 608FF 19672 SMOKE COMING FROM L-2 MID-GALLEY. FOUND CIRCUIT BREAKER NR 3 OVEN OPEN. SHUT DOWN AND SECURED NR 3 OVEN. MADE INSPECT ION OF OVEN AREA AND FOUND ALL OK. TRANSFER TO ODI PER MEL. NR 3 CIRCUIT BREAKER FOR OVEN COLLARED. REMOVED OVEN. (X ) 2 L 7 4 4F A20WE 1998071400361 19980714 00361 NE 1998 7 14 USAAD98097 2 19980530 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE NR 1 FAILED A USAA A UNSCHED LANDING E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 827US 36789 48049 708585 MCO - FLT 2292 - DURING CLIMB-OUT, THERE WAS A LOUD BANG FROM THE LEFT ENGINE AND THE N1 INDICATION DECREASED. THE VIBR ATION INDICATION WENT OFF SCALE ON THE HIGH SIDE. THE ENGINE THROTTLE WAS RETURNED TO IDLE, THE AIRCRAFT RETURNED TO TH E FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGINE. (X) 2 L 7 2 4F 4 F A6WE E9NE 1998071400362 19980714 00362 EU 1998 7 14 USAAF98044 1 19980522 A 2421 740514C GENERATOR FOKKER F28 F28MK0100 4990807 EU RIGHT FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 EA 19 883US 11337 PIT FLT 0540 - EN ROUTE TO MKE, RIGHT GENERATOR FAULTED. APU WAS STARTED AND APU GENERATOR WAS PUT ON LINE. TEN MINUT ES LATER, THE APU SHUT DOWN. FLIGHT RETURNED TO PIT DUE TO ONE GENERATOR OPERATION. FLIGHT LANDED WITHOUT FURTHER INCI DENT. MAINTENANCE REPLACED THE GENERATOR CONTROL UNIT AND THE NR 1 GENERATOR. REF: OPERATOR CONTROL NR 98ZZZX____. ( X) 2 L 7 2 4F RT 1998071400363 19980714 00363 EU 1998 7 14 98ZZZX2342 1 19980522 A 2424 74508 GCU FOKKER F28 F28MK0100 4990807 EU RIGHT FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC NR NOT REPORTED 1 EA 19 883US 11337 PIT FLT 0540 - EN ROUTE TO MKE, RIGHT GENERATOR FAULTED. APU WAS STARTED AND APU GENERATOR WAS PUT ON LINE. TEN MINUT ES LATER, THE APU SHUT DOWN. FLIGHT RETURNED TO PIT DUE TO ONE GENERATOR OPERATION. FLIGHT LANDED WITHOUT FURTHER INCI DENT. MAINTENANCE REPLACED THE GENERATOR CONTROL UNIT AND THE NR 1 GENERATOR. REF: OPERATOR CONTROL NR USAAF98044. 2 L 7 2 4F RT 1998071400364 19980714 00364 EU 1998 7 14 SIMA981541 1 19980603 A 3350 5211309111 LIGHT AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 425MJ 425 DFW - EMERGENCY LIGHT STRIP INOPERABLE AT GALLEY AREA. REPLACED REAR EMERGENCY LIGHT STRIP AND PERFORMED OPERATIONAL CH ECK IAW ATR JIC 33-51-21. OPERATION WAS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998071400365 19980714 00365 EU 1998 7 14 SIMA981543 1 19980603 A 2611 7211121000 SMOKE DETECTOR KIDDE SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A SIMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 348SB A4404 340B348 LAX - FLT 3246 - LAVATORY SMOKE LIGHT ILLUMINATED WHILE DEPLANEING PASSENGERS. REMOVED AND REPLACED LAVATORY SMOKE DETE CTOR. OPERATIONAL CHECK GOOD. AIRCRAFT REURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998071400366 19980714 00366 WP 1998 7 14 EIAA980176 1 19980318 A 5320 99220422 FITTING DOUG DC9 DC933F 302207A WP BS 256 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 DURING 'C5' CHECK, FRAME ATTACH FITTING CRACKED AT BS 256 AT STR 24R. REPLACED FRAME ATTACH FITTING PER SRM 51-10-03. ( X) 2 L 7 2 4F A6WE 1998071400367 19980714 00367 NM 1998 7 14 98ZZZX2343 1 19980603 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8103 1386005 NM CABIN FAILED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 802WP 22 D822 010 EMERGENCY LIGHT ON LEFT FORWARD SIDE OF CABIN INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AT LOCATION PS1 (WARDROBE CLOSET). SYSTEM OPS CHECKED GOOD IAW PSM 1-8-2 SECTION 33-51-00, PAGES 201-203. 2 H 7 2 4T RT A13NM 1998071400368 19980714 00368 WP 1998 7 14 IXXA9800060 1 19980707 A 3310 BA170MODB BALLAST DOUG DC8 DC862 3021970 WP COCKPIT FAILED A IXXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 728PL 45918 EN ROUTE FROM KWA TO HIK, SMOKE EMANATED FROM THE FIRST OFFICERS RIGHT PEDESTAL CONSOLE. THE CREW EXTINGUISHED THE MAIN INSTRUMENT GLARESHIELD WHITE LIGHTING, THE SMOKE STOPPED. THE FLIGHT CONTINUED TO HIK FOR AN UNEVENTFUL LANDING. MAIN TENANCE FOUND THAT THE GLARESHIELD WHITE LIGHTING BALLAST HAD FAILED AND PRODUCED THE SMOKE. MAINTENANCE DEFERRED THE G LARESHIELD LIGHTING IN ACCORDANCE WITH COMPANY MEL PROCEDURES. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1998071400369 19980714 00369 NM 1998 7 14 AWXA9800148 1 19980615 A 5313 STRINGER BOEING 737 737112 1384412 NM BS 787-867 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 708AW 19771 FOUND DURING SCHEDULED INSPECTION, STR 26R CORRODED BEYOUND LIMITS STA 787 TO 867, AND FRAME STA 285.5 RBL17. REMOVED A ND REPLACED STRINGER WITH SERVICEABLE PARTS PER SRM 51-30-02, AND REPAIRED FRAME PER SRM 51-40-03. 2 L 7 2 4F A16WE 1998071400370 19980714 00370 NM 1998 7 14 AWXA9800149 1 19980425 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 FLOORBEAMS CORRODED IN APPROXIMATELY 4 AREAS IN THE R1 DOOR GALLEY AREA. REPAIR PER SRM 53-10-09 PAGE 22-28. 2 L 7 2 4F RT A16WE 1998071400371 19980714 00371 WP 1998 7 14 CALA9801211 1 19980702 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 INSPECTION FOUND WEB CORRODED AT STA 1212 AFT OF DOOR INBOARD OF LONGERON 27R. A REPAIR WAS INSTALLED IAW ECRA 5310-037 42. 2 L 7 2 4F A6WE 1998071400372 19980714 00372 WP 1998 7 14 CALA9801212 1 19980706 A 5350 PINS DOUG DC9 DC982 3022082 WP TAILCONE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16887 49116 THE FORCE REQUIRED TO RELEASE TAILCONE USING EXTERIOR HANDLE WAS BELOW LIMITS. WORN ALIGNMENT PINS AND RECEPTACLES WERE REPLACED AND LATCHES WERE ADJUSTED IAW MM 53-50-00. 2 L 7 2 4F A6WE 1998071400373 19980714 00373 NM 1998 7 14 CALA9801213 1 19980706 A 3350 20131A BATTERY PACK RADIANT BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 70352 23590 INSPECTION FOUND AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. A BATTERY PACK IN THE AFT SECTION WAS REMOVED AND REPLACE D. 2 L 7 2 4F RT A16WE 1998071400374 19980714 00374 WP 1998 7 14 CALA9801214 1 19980706 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1708 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12080 47981 INSPECTION FOUND CORROSION AT LOWER END OF CENTER CARGO FORWARD DOOR FRAME, STA 1708. REPAIRED IAW SRM 53-50-00, FIGURE 21. 2 L 7 3 4F A22WE 1998071400375 19980714 00375 WP 1998 7 14 CALA9801215 1 19980707 A 5320 SILL DOUG DC10 DC1030 3023501 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12080 47981 INSPECTION FOUND CENTER CARGO BAY LOWER DOOR SILL CORRODED AT FORWARD END, STA 1701. REPAIRED IAW ECRA 5310-03473. 2 L 7 3 4F A22WE 1998071400376 19980714 00376 NM 1998 7 14 CALA9801216 1 19980701 A 3350 10617844 POWER SUPPLY GRIMES BOEING 727 727232 1384082 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND BOTH INTERIOR LT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE LT OVERWING EMERGENCY EXIT LIGHT POWE R SUPPLY WAS REMOVED AND REPLACED. 2 L 7 3 4F A3WE 1998071400377 19980714 00377 WP 1998 7 14 UPS98827104 1 19980627 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, LT WING L/E AT STA XFS760.00, THE L/E RIB IS CRACKED AT THE AFT END, STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998071400378 19980714 00378 WP 1998 7 14 UPS98827105 1 19980627 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 797.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, LT WING L/E AT STA XFS797.500, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998071400379 19980714 00379 WP 1998 7 14 UPS98827106 1 19980627 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, LT WING L/E AT STA XFS810.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998071400380 19980714 00380 WP 1998 7 14 UPS98827107 1 19980627 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 803.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, LT WING L/E AT STA XFS803.750, THE LOWER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998071400381 19980714 00381 WP 1998 7 14 UPS98827108 1 19980627 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 703.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, LT WING L/E AT STA XFS703.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998071400382 19980714 00382 WP 1998 7 14 UPS98827109 1 19980625 A 5347 5750726511 TRACK DOUG DC8 DC871F 302199D WP BS 1400-1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, CARGO TRACK AT STA 1400-1540 ABOVE STR 33R HAS CORROSION AND CRACK. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5750726 AND SRM 51-3-1. 2 L 7 4 4F RT 4A25 1998071400383 19980714 00383 WP 1998 7 14 UPS98827110 1 19980626 A 5720 576989123 TRIPLER DOUG DC8 DC871F 302199D WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, RT WING L/E LWR SKIN, THE INTERNAL TRIPLER AT THE I/B END OF THE O/ B SLOT IS CRACKED AT STA XOLDI 6. 225. REMOVED, FABRICATED AND REPLACED TRIPLER IAW DWG 5769891 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998071400384 19980714 00384 WP 1998 7 14 UPS98827111 1 19980630 A 5320 4647657 FITTING DOUG DC8 DC871F 302199D WP BS 100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, STA 100, LONG 36 END FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 4647657 AND S RM 51-1-20D. 2 L 7 4 4F RT 4A25 1998071400385 19980714 00385 WP 1998 7 14 UPS98827112 1 19980626 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, RT WING L/E UPPER RIB AT STA XFS304.00 IS CRACKED AT THE FWD END. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998071400386 19980714 00386 WP 1998 7 14 UPS98827113 1 19980626 A 5753 RIB DOUG DC8 DC871F 302199D WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C LT WING T/E AT FLAP STA 3.00, THE T/E RIB IS CRACKED BEHIND NR 1 SPOILER I/B HINGE. STOP DRILLED CRAC K AND REPAIRED IAW SRM57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998071400387 19980714 00387 WP 1998 7 14 UPS98827114 1 19980701 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 336 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE:C, RT WING L/E LWR SKIN AT STA XFS336.0 IS CRACKED AT THE DRAIN HOLE. REPAIRED AREA IAW DC8-5720-4087-B AND SRM 57-3-3 FIG 5. 2 L 7 4 4F RT 4A25 1998071400388 19980714 00388 WP 1998 7 14 UPS98827116 1 19980609 A 5751 5705321509 AILERON DOUG DC8 DC871F 302199D WP LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, THE LT INBD AILERON HAS AREAS OF LIGHT SURFACE CORROSION THROUGHOUT ENTIRE INNER SURFACE OF FORWARD S PAR AREA. REMOVED AND REPACED THE LT INBD AILERON PER MM 27-11-01. 2 L 7 4 4F RT 4A25 1998071400389 19980714 00389 WP 1998 7 14 UPS98827117 1 19980703 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803UP 46073 EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMER BATTERY PACK IAW DC8 MM 33-50-01. OPS CHECKS GOOD P/N ON 5 7-084 58-503 P/N OFF 60-1223-5 S/N ON FLT 135 S/N OFF 322. 2 L 7 4 4F RT 4A25 1998071400390 19980714 00390 1998 7 14 UPS98827118 4 19980706 A 2210 AUTO PILOT PANEL DOUG DC8 DC873F 302199F WP COCKPIT FAILED A IPXA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 01 803UP 46073 AUTOPILOT ROLL FUNCTION WOULD NOT ENGAGE, AIR ABORT, DUMPED 45,000 POUNDS OF FUEL, FUEL DUMP WIRE HAS BEEN CUT. FOUND N O VOLTAGE AT SERVO CLUTCH CONN. REMOVED AND REPLACED AUTO PILOT PANEL PER MM 22-10-02 OPS CK'D SYS PER 2200 SYS. CHK'S GOOD, P/N ON 622-6208-503 S/N ON 1140 OFF 622-6208-503 OFF 974. 2 L 7 4 4F RT 4A25 1998071400391 19980714 00391 WP 1998 7 14 UPS98827120 1 19980707 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 558-582 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 REPAIR TO FUSELAGE SKIN FS 558-582, LONGERON 35L-35R. COMPLIED WITH EO 5330-10147A INTERM REPAIR. REMOVED SURFACE CORR OISION TRANSFERED TO DEFERAL LIST. 2 L 7 4 4F RT 4A25 1998071400392 19980714 00392 WP 1998 7 14 UPS98827115 1 19980626 A 5751 DOUBLER DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 RT I/B AILERON INTERNAL DOUBLER IS CRACKED AT ACCESS PNL NR 541. REPAIRED IAW DHC SK 708-207. 2 L 7 4 4F RT 4A25 1998071400393 19980714 00393 1998 7 14 UPS98827121 2 19980707 A 7200 ENGINE DOUG DC8 DC871F 302199D WP CFM 56 NR 3 FAILED A IPXA E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE AP APPROACH 1 SO 01 700UP 45900 NR 3 ENG SEIZED ON SHORT FINAL. N2 BECAME 0 PERCENT RAN THE ENG FIRE AND SECURE ENGINE CHECK LIST. REMOVED AND REPLACED ENGINE IN WORK FOUND METAL IN OIL SYSTEM (CHIP DETECTOR) SUSPECT BEARING FAILURE. 2 L 7 4 4F RT 4A25 1998071400394 19980714 00394 WP 1998 7 14 UPS98827122 1 19980603 A 5510 37014272 FITTING DOUG DC8 DC871F 302199D WP RT HORZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, RT HORIZ STAB L/E ON THE INBD END THE UPPER AND LOWER TEE FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW SRM 53-1-0. 2 L 7 4 4F RT 4A25 1998071400395 19980714 00395 WP 1998 7 14 UPS98827123 1 19980608 A 5320 57550583 CHANNEL DOUG DC8 DC871F 302199D WP BS 790 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, U-CHANNEL CRACKED BOTTOM OF FUSELAGE AT STA 790, LBL 16. REMOVED AND REPLACED U-CHANNEL PER SRM 51-3 -0. 2 L 7 4 4F RT 4A25 1998071400396 19980714 00396 WP 1998 7 14 UPS98827124 1 19980608 A 5320 57550583 CHANNEL DOUG DC8 DC871F 302199D WP BS 790 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE:D, U-CHANNEL CRACKED BOTTOM OF FUSELAGE AT STA 790 RIB L16. REMOVED AND RPLACED U-CHANNEL PER SRM 51-3- 0. 2 L 7 4 4F RT 4A25 1998071400397 19980714 00397 WP 1998 7 14 UPS98827125 1 19980526 A 5320 STIFFINER DOUG DC8 DC873F 302199F WP BS 683 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE:C/CK COMPLIED WITH FWD BULKHEAD VIEWS FROM CABIN FLOOR STATION 683 X= -2 3 TOP OF VERTICAL STIFFENER BRA CKET CRACKED. MATERIAL ID 2024-0 IAW DWG 5773275, HEAT TREATED 2024-0 TO 2024 T4, .100 IAW TPS- 1003 FABRICATED IAW DC 8 SRM 51-1-4 AND 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998071400398 19980714 00398 NM 1998 7 14 98UAL900291 1 19980626 A 2910 AC11504K0232 HYDRAULIC LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG RUPTURED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 521UA 24891 RETURNED TO ORD DUE TO LEFT SYSTEM HYDRAULIC FAILURE. *S/D* LINE TO THE LEFT SIDE STRUT DOWNLOCK ACTUATOR WAS LEAKING. REPLACED LINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998071400399 19980714 00399 NM 1998 7 14 98UAL900293 1 19980627 A 3260 INDICATION BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NLG DOORS MALFUNCTIONED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 908UA 25008 UNSAFE NOSE GEAR INDICATION. NOSE GEAR DOORS APPEARED CLOSED THROUGH THE NOSE GEAR VIEWPORT. MANUALLY DEPLOYED THE NOS E GEAR. 2 L 7 2 4F 4 F RT A16WE E2GL 1998071400400 19980714 00400 NM 1998 7 14 98UAL900294 1 19980628 A 5350 654861539 FAIRNG BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 580 NOT SEALED A UALA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 319UA 31454 23951 VIBRATION AND HUM ADJACENT TO ROW 9. THE REPORTED VIBRATION THAT WAS HEARD FROM ROW 9 (LEFT) WAS A RESULT OF DETERIORAT ED SEALANT ON THE UPPER WING TO BODY FAIRING AT THAT SAME LOCATION. THE FAIRING WAS RESEALED AT THE IMC AND THE AIRCRAF T RELEASED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998071400401 19980714 00401 EU 1998 7 14 98UAL900295 1 19980630 A 5101 STRUCTURE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AIRFRAME VIBRATION A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 422UA 503 AIRCRAFT EXPERIENCED EXCESSIVE LOW FREQUENCY VIBRATION DURING CLIMB. DIVERTED TO LAS. AMBER ALERT, OVERWEIGHT LANDING. 2 L 7 2 4F 4 F RT A28NM E40NE 1998071400402 19980714 00402 NM 1998 7 14 98UAL900296 1 19980614 A 5510 65B026683 TUBE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE HORIZ STAB CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 165UA 76889 21658 A 1.2 INCH CRACK WAS FOUND IN 65B02668-3 DIAGONAL SUPPORT TUBE AT STA 2598 HORIZONTAL STABILIZER HINGE SUPPORT BULKHEAD. CRACK WAS AT UPPER END OF TUBE, BEGINNING AT TUBE EDGE AND RUNNING DOWN THROUGH FIRST ROD END ATTACH FASTENER HOLE. T UBE ASSEMBLY REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1998071400403 19980714 00403 NM 1998 7 14 98UAL900297 1 19980625 A 3350 3001817 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7277U 21424 EMERGENCY EXIT SIGN ABOVE DOOR 2R FLICKERS ON AND OFF WITH COCKPIT SWITCH IN ARMED POSITION. *S/D* REPLACED EMERGENCY LIGHTS AT DOOR 2R AND 1R. 2 L 7 3 4F 4 F A3WE E2EA 1998071400404 19980714 00404 NM 1998 7 14 98UAL900298 1 19980626 A 2910 BACH6P0310CTN HOSE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RUDDER LEAKING A UALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 7461U 21915 RETURNED TO GATE DUE TO LOSS OF HYDRAULIC QUANTITY. FOUND HYDRAULIC PRESSURE LINE TO RUDDER PCU LEAKING. REMOVED AND R EPLACED LINE. ALSO, LEAK CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1998071400406 19980714 00406 NM 1998 7 14 98UAL900300 1 19980627 A 2130 PRESSURIZATION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 29 7279U 21557 AIRCRAFT ALTITUDE 10K AND CABIN ALTITUDE 8.4K. CARGO HEAT AND OUTFLOW VALVES CLOSED. COULD NOT MAINTAIN PRESSURE. DIV ERTED BACK TO DEN. 2 L 7 3 4F 4 F A3WE E2EA 1998071400407 19980714 00407 NM 1998 7 14 98UAL900301 1 19980626 A 2130 PRESSURIZATION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7288U 21566 CABIN PRESSURE CANNOT BE MAINTAINED. 2 L 7 3 4F 4 F A3WE E2EA 1998071400408 19980714 00408 NM 1998 7 14 98UAL900302 1 19980630 A 5347 1A087 SEAT TRACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT COCKPIT LACK OF LUBE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 29 366UA 24535 CAPTAIN'S SEAT UNLOCKED DURING TAKEOFF. INSPECTED TRACK AND LOCK MECHANISM. FOUND SOME DEBRIS ON THE TRACK. CLEANEDTR ACK AND LUBED LOCK MECHANISM. OPERATED SEAT ON THE SEAT TRACK SEVERAL TIMES. OP CHECK GOOD. MM TO BE REVISED TO ADD S PECIFIC TRACK AND LOCK MECHANISM CLEAN AND LUBE TASKS (ATB-CHECK) TO HELP PRECLUDE THIS TYPE OF OCCURRENCE. TRACK CONDI TION CHECKS ALREADY IN PLACE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998071400409 19980714 00409 NM 1998 7 14 98UAL900303 1 19980629 A 2742 12970003 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE STAB TRIM FAILED A UALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 WP 29 7441U 21895 MAIN STABILIZER ELECTRIC TRIM COASTS MORE THAN TWO TURNS AFTER SWITCH IS RELEASED. ON APPROACH, HAND FLYING, THE MAIN E LECTRICAL TRIM RAN AWAY NOSE UP WHILE TRIMMING FORWARD. STOPPED BY PUSHING AGAINST NOSE UP. *S/D* REPLACED STAB TRIM ACTUATOR AND OPS CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1998071400410 19980714 00410 NM 1998 7 14 98UAL900304 1 19980630 A 2133 VALVE SUNDSTRAND 56697 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 7255U 21402 UNABLE TO CONTROL CABIN PRESSURE DURING DESCENT. CLOSING HEAT OUTFLOW VALVE AND ADDING POWER HELPED. *S/D* REPLACED C ABIN PRESSURE REGULATOR SHUTOFF VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998071400411 19980714 00411 NM 1998 7 14 98UAL900306 1 19980701 A 3840 AIR COMPRESSOR METAL BELLOW 288231 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE GALLEY FAILED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 552UA 2674D 26641 RETURNED TO LAX DUE TO VIBRATION UNDER AFT GALLEY. *S/D* POTABLE WATER SYSTEM ELECTRIC AIR COMPRESSOR FAILED. COMPRES SOR WAS REPLACED AND AN OPERATIONAL CHECK WAS PERFORMED. COMPRESSOR CHECKED OUT OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1998071400412 19980714 00412 EU 1998 7 14 98UAL900307 1 19980627 A 3610 BLEED AIR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 434UA 492 ON CLIMB-OUT, BLEED AIR PROBLEMS DEVELOPED. RETURNED TO IAD. 2 L 7 2 4F 4 F RT A28NM E40NE 1998071400413 19980714 00413 WP 1998 7 14 ABXA9800602 1 19980703 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 984AX 4388 47258 EMERGENCY LIGHTING WOULD NOT TEST. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY. 2 L 7 2 4F A6WE 1998071400414 19980714 00414 NM 1998 7 14 SCNA98069 1 19980705 A 2410 CONNECTOR BOEING 727 7272A1 138407F NM NR 1 ENGINE LOOSE A SCNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 287SC 21345 DURING CLIMB, THE NUMBER TWO ENGINE CSD TEMPERATURE INDICATION WAS LOST. THE NUMBER ONE CSD TEMP CLIMBED INTO THE YELLO W ARC AND THE NUMBER THREE ENGINE CSD TEMPERATURE INDICATION WAS ON MEL. AIR RETURNED INTO IAH. FOUND CANNON PLUG LOOS E ON OUT TEMPERATURE BULB FOR THE NUMBER ONE CSD. NUMBER TWO ENGINE CSD WAS FOUND TO BE AN INDICATION PROBLEM AND WAS M EL'D. RAN ENGINES WITH A LOAD AND POWER AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998071400415 19980714 00415 WP 1998 7 14 SCNA98516 1 19980629 A 3350 EMBS1392 BATTERY PACK DOUG DC10 DC1015 3022118 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 5967 48289 DURING A HEAVY MAINTENANCE CHECK, THE MID CABIN EMERGENCY EXIT LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE MID CABIN BATTERY PACK AT THE L2 LOCATION. OPERATIONALLY CHECKS GOOD PER MAINTENANCE MANUAL 335101. 2 L 7 3 4F A22WE 1998071400416 19980714 00416 WP 1998 7 14 SCNA98517 1 19980629 A 3350 EMBS1392 BATTERY PACK DOUG DC10 DC1015 3022118 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 1523 48289 DURING A HEAVY MAINTENANCE CHECK, THE OVERWING EMERGENCY EXIT LIGHT BATTERY PACK WAS FOUND TO BE INOPERATIVE. REMOVED A ND REPLACED THE OVERWING BATTERY PACK AT THE L3 LOCATION. OPERATIONALLY CHECKS GOOD PER MAINTENANCE MANUAL 335101. 2 L 7 3 4F A22WE 1998071400417 19980714 00417 NM 1998 7 14 DHL98702001 1 19980708 A 7931 LINE BOEING 727 72730C 1384009 NM NR 1 ENGINE HOLE A DHLA A UNSCHED LANDING E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 702DH 19793 AT FL 330, NR 1 ENGINE OIL PRESSURE LIGHT CAME ON. OIL QUAN DROPPED TO 1.5, ENGINE HAD VIBRATION. REMOVED AND REPLACED OIL LINE FROM OIL PRESSURE TRANSMITTER. 2 L 7 3 4F A3WE 1998071400418 19980714 00418 NM 1998 7 14 DHL98702002 1 19980708 A 2913 371380 HYD PUMP BOEING 727 72730C 1384009 NM NR 1 ENGINE FAILED A DHLA A UNSCHED LANDING E K J VIBRATION/BUFFET FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 702DH 19793 AT FL 330, NR 1 ENGINE OIL PRESSURE LIGHT CAME ON AND OIL QUAN DROPPED TO 1.5 . NR 1 ENGINE HAD VIBRATION. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP. 2 L 7 3 4F A3WE 1998071400419 19980714 00419 1998 7 14 DHL98807004 4 19980707 A 3442 RT UNIT DOUG DC8 DC873F 302199F WP E/E COMPT TRIPPED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 807DH 45990 RADAR DOES NOT PAINT WEATHER. CAPT CDI MIRRORS FIRST OFFICIER CDI, REGARDLESS OF CAPTS POSITION. RERACKED RADAR R/T, O PS CHECK GOOD. PUT CAPTS OVERHEAD NAV SWITCH TO CAPTS, RERACKED VOR/ILS RECEIVER. OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1998071500001 19980715 00001 NE 1998 7 15 UPS98627042 2 19980619 A 7200 ENGINE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B6 NE LEFT MALFUNCTIONED A IPXA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 01 319UP 27758 INSPECTION TYPE:ETOP LEFT ENGINE POWER FLUCTATES AT A CONSTANT SETTING (THRUST). CONDITION WAS INTERMITTENT ON CLIMB-O UT IN BOTH CLB 2 AND CLB PWR. N1,EGT,N2, AND FUEL FLOW ALL FLUXED WITH NO POWER SETTING CHANGE. PERFORMED BITE CHECK P ER FIM 73-21-00 COMBINED WITH ENGINE RUNS. NO STATUS MSG OR CURRENT FAULTS. 2 L 7 2 4F 4 F RT A1NM E13NE 1998071500003 19980715 00003 NE 1998 7 15 CALA9801172 2 19980625 A 7230 COMPRESSOR BOEING 757 757224 1384958 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE FAILED A CALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 09 13113 27555 31268 THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALL ACCOMPANIED BY HIGH EGT JUST AFTER TAKEOFF FROM LAS. THE AIRCRAFT WAS RETU RNED TO LAS WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE HIGH PRESSURE COMPRESS OR DAMAGE REPORTED DURING THE BORESCOPE IN LAS WAS CONFIRMED ON MODULE STRIP. A 90 DEGREE ARC OF STAGE 2 ROTOR PATH LIN ING HAD EVACUATED AND MOST PROBABLY CAUSED THE DAMAGE FROM STAGE 2 DOWNSTREAM. THIS CONDITION CAUSED A REDUCTION IN COM PRESSOR EFFICIENCY THAT RESULTED IN A SIGNIFICANT REDUCTION IN SURGE MARGIN THUS INCREASING THE POTENTIAL EXPOSURE TO A SURGE CONDITION. 2 L 7 2 4F 4 F RT A2NM E12EU 1998071500004 19980715 00004 NM 1998 7 15 98UAL900279 1 19980616 A 5412 65B903671 BULKHEAD FITTING BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE NR 3 PYLON CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 165UA 21658 DURING ROUTINE MAINTENANCE, THE NR 3 PYLON REAR ENGINE MOUNT BULKHEAD FITTING, 65B90367-1 WAS FOUND WITH THREE CRACKS EM ANATING FROM THE FASTENER HOLES. THERE IS NO RECORD OF THE MOD DESCRIBED IN BOEING S/B 747-54-2113 HAVING BEEN ACCOMPLI SHED IN THIS AREA. FITTING REMOVED AND REPLACED BEFORE FURTHER FLIGHT. 2 L 7 4 4F 4 F A20WE E20EA 1998071500005 19980715 00005 WP 1998 7 15 ABXA9800569 1 19980619 A 5400 9912243227 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 964AX 47781 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ENGINE PYLON SHEAR-TIE CRACKED AT LONGERON 14 LEFT AND FS 1041. REPLA CED SHEAR-TIE IAW DOUGLAS DC9 SRM CHAPTERS 53-12-3, 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998071500007 19980715 00007 NM 1998 7 15 F3LA98066 1 19980527 A 5312 BULKHEAD BOEING 737 737201 1384454 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN BS 178 BULKHEAD INTERCOSTAL LEFT CHORD, WL 196. MAINTENANCE REMOVED DAMAGED AREA, 12 INCHES. FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER 98-0426 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998071500008 19980715 00008 WP 1998 7 15 ARWA980611 1 19980628 A 2450 FUSE DOUG DC8 DC862 3021970 WP NR 1/2 BUS BLOWN A ARWA O OTHER H ELECT. POWER LOSS-50 PC IN INSP/MAINT 1 SO 19 791AL 46150 LIGHTING BOLT STRUCK NEAR AIRCRAFT ON GROUND. GROUND POWER WENT OFF AIRCRAFT. AFTER ONE HOUR (STORM) POWERED AIRCRAFT. SMOKE CAME UP BETWEEN CABIN PRESS CONTROL PANEL. LEFT DC INOPERATIVE. SEVERAL AIRCRAFT SYSTEMS INOPERATIVE. ALL FOU R FIRE DETECTION INOPERATIVE. ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW MM 5-8-3, NO ABNORMALITIES NOTED. FOUND 100 AMPS FUSE TO NUMBER ONE AND TWO BUS OPEN. REPLACED FUSE IAW M/M 24-2-1, OPERATIONAL NORMAL. ALL SYSTEMS FUNCTIONING P ROPERLY. 2 L 7 4 4F 4A25 1998071500009 19980715 00009 1998 7 15 ARWA980610 4 19980630 A 3414 CONNECTOR LKHEED 1011 10113851 WP AIR DATA COMP DIRTY A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK G MULTIPLE FAILURE TO TAKEOFF 1 SO 19 308GB 1133 ON TAKEOFF, CAPTAINS AIRSPEED INOPERATIVE WITH NUMBER ONE (1) MACH FEEL, NUMBER ONE (1) ATS, NUMBER ONE MAIN TRIM FAIL, THEN CAPTAINS AIRSPEED FAIL WITH NUMEROUS FLAGS, TAKEOFF REJECTED. CLEANED PINS NUMBER, ADC RACK AND ADC CONNECTORS, RE RACKED, CHECKED FOR OPERATION PER M/M 34-14-01, ALL CHECKED NORMAL, NO FLAGS. 2 L 7 3 4F RC A23WE 1998071500010 19980715 00010 WP 1998 7 15 ABXA9800542 1 19980622 A 5610 5613217508 WINDOW DOUG DC9 DC941 302207N WP RT COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 UNABLE TO OPEN FIRST OFFICER'S CLEARVIEW WINDOW. REPOSITIONED WINDOW AS REQUIRED. 2 L 7 2 4F A6WE 1998071600001 19980716 00001 1998 7 16 ARWA980701 4 19980702 A 3417 2593200951 ADC LKHEED 1011 1011385115 5265015 WP E/E BAY MALFUNCTIONED A ARWA C ABORTED TAKEOFF G MULTIPLE FAILURE TO TAKEOFF 1 SO 19 308GB 2110098 193U1133 BDL - FLT 505 - ON TAKEOFF, CAPTAIN'S AEROSPEED FAILED WITH NR 1 MACH FEEL, NR 1 ATS, NR 1 MACH TRIM FAIL WITH NUMEROUS FLAGS. REMOVED AND REPLACED NR 1 AIR DATA COMPUTER GROUND CHECKED AND OPERATIONAL CHECKED NORMAL IAW MM 34-14-00. AIRC RAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A23WE 1998071600003 19980716 00003 EU 1998 7 16 CA980331023 1 19980320 A 3246 AHA1489 FUSE PLUG HOLE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502* 41580 EA WHEEL CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10746 (CAN) CRACKS FOUND AT FUSE PLUG HOLE. PART TC: 10,759. 2 H 7 4 4F 4 F RT A49EU E6NE 1998071600004 19980716 00004 NM 1998 7 16 DL757981416 1 19980706 A 4930 211734219 ECU 211734219 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE APU COMPT FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 641DL 18803 23995 P1198 APU FLAMED OUT IN FLT FOLLOWED PROCEDURES AND GOT APU FAULT LIGHT, NO START ALLOWED. ONE ENG GEN PREV DEFERRED, ROBBED APU CONTROL ECU FROM A/C 628. INSTALLED BITE CK OK. OPERATED APU W/AIR AND ELECTRIC OPS NML. 2 L 7 2 4F 4 F RT A2NM E17NE 1998071700001 19980717 00001 WP 1998 7 17 VJ9800215 1 19980702 A 3520 17453004A OXYGEN MASK DOUG DC9 DC932 3022066 WP CABIN DEPLOYED A ZZDA O OTHER O OTHER DE DESCENT 1 SO 15 913VV 47318 WITH PRESSURIZATION IN MANUAL MODE, OXYGEN MASKS DEPLOYED IN BUSINESS CLASS SECTION, FLT ATTENDANT STATIONS AND 8 POSITI ONS IN COACH CLASS ON DESCENT FOR LANDING. REPACKED OXYGEN MASKS AND FLEW AIRCRAFT BELOW FL100 FROM MEM TO ATL. INSPEC TED AIRCRAFT AND NO DEFECTS NOTED; PERFORMED OXYGEN MASK DROP AND ALL MASKS DEPLOYED SUCESSFULLY. 2 L 7 2 4F A6WE 1998071700002 19980717 00002 WP 1998 7 17 VJ9800216 1 19980706 A 2560 5917689531 COVER DOUG DC9 DC932 3022066 WP L1 DOOR SLIDE DISLODGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 946VV 47226 EMERGENCY SLIDE COVER ON MAIN PASSENGER DOOR BECAME DISLODGED. REINSTALLED SLIDE PACK. 2 L 7 2 4F A6WE 1998071700003 19980717 00003 WP 1998 7 17 VJ9800217 1 19980706 A 2420 CONTROL PANEL DOUG DC9 DC932 3022066 WP NR 2 GENERATOR REPAIRABLE A ZZDA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 15 967VV 47170 NR 2 GENERATOR WENT OFF LINE EN ROUTE TO PHL FROM ATL. VOLTS AND FREQUENCY CHECKED NORMAL; GENERATOR WOULD NOT RESET. T AIL COMPARTMENT HI LIGHT ILLUMINATED AFTER APU STARTED AS BACK UP FOR ELECTRICAL POWER. AS PRECAUTIONARY MEASURE, FLIGH T CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE. REPLACED NR 2 GENERATOR, AC CONTROL PANEL AND REPOSITIONED TEMP SENSO R. 2 L 7 2 4F A6WE 1998071700004 19980717 00004 WP 1998 7 17 VJ9800218 1 19980707 A 2560 5928729511 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE DISLODGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 907VJ 47444 EMERGENCY EVACUATION SLIDE COVER ON GALLEY DOOR BECAME DISLODGED. REINSTALLED IAW MM 25-00 AND PERFORMED REQUIRED INSPE CTION. 2 L 7 2 4F A6WE 1998071700005 19980717 00005 WP 1998 7 17 VJ9800219 1 19980707 A 3230 4956769503 BUMPER DOUG DC9 DC932 3022066 WP LT MLG WORN A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 932VV 47451 UNSATISFACTORY GEAR UPLATCH CHECK OF LT MLG; DOOR OPEN AND GEAR UNSAFE INDICATION. FLIGHT CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE AS A PRECAUTIONARY MEASURE. REPLACED LT MAIN TORQUE LINK BUMPER; GEAR SWING PERFORMED AND CHECKED GOO D. 2 L 7 2 4F A6WE 1998071700006 19980717 00006 WP 1998 7 17 VJ9800220 1 19980708 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP L1 DOOR SLIDE DISLODGED A ZZDA K NONE O OTHER LD LANDING 1 SO 15 909VJ 47322 ON ARRIVAL AT GATE, EMERGENCY SLIDE PACK COVER DISLODGED. REINSTALLED IAW MM 25-60. PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998071700007 19980717 00007 EU 1998 7 17 MALA976159 1 19980702 A 7603 RELAY SAAB SF340 340B 7860101 EU E/E COMPT FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 414XJ 340B414 AFTER GEAR RETRACTION THE ORANGE FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED RELAYS 82KA AND 20GA IAW SAAB MM 76-10-60. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998071700008 19980717 00008 NM 1998 7 17 MALA976160 1 19980704 A 3260 CONNECTOR DHAV DHC8 DHC8102 2809003 NM NLG DIRTY A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 848MA 346 UPON ROTATION WHEN THE NOSE WHEEL LIFTED OFF THE WEIGHT ON WHEELS LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTEN ANCE INSPECTED WIRING AT NOSE LANDING GEAR: REMOVED, CLEANED AND REINSTALLED CANON PLUG CONNECTORS FOR NOSE GEAR AND CLE ANED WOW SWITCHES. PERFORMED GEAR SWINGS, NO DEFECTS NOTED. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998071700009 19980717 00009 NM 1998 7 17 K3HA980086 1 19980705 A 2150 56697 COOLING VALVE BOEING 727 727225 1384077 NM E/E COMPT FAILED A K3HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 356PA 20626 ON CLIMBOUT, CABIN CONTINUED TO CLIMB PAST ALTITUDE CALLED FOR (5500 FEET) AT 2400 FEET, CLOSED CARGO HEAT VALVE WENT TO MANUAL CONTROLLER FULL CABIN CONTINUED TO CLIMB AND RETURN TO NEWARK. *S/D* REMOVED AND REPLACED EQUIPMENT COOLING VA LVE AS PER MM 21-58-21. 2 L 7 3 4F A3WE 1998071700010 19980717 00010 WP 1998 7 17 IXXA9800061 1 19980709 A 3231 RETRACT MECH DOUG DC8 DC862 3021970 WP NLG DOOR MALFUNCTIONED A IXXA K NONE O OTHER CL CLIMB 1 GL 23 61CX 46142 AFTER TAKEOFF FROM MSP, EN ROUTE TO TOL, WHEN THE GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A LOUD NOISE AND SLIGHT VI BRATION COMING FROM THE NOSE WHEEL WELL AREA. THE CREW PERFORMED A GEAR UPLATCH CHECK WHICH PASSED, THEN CYCLED THE GEA R. THE VIBRATION CONDITION WAS STILL PRESENT AND THE AIRCRAFT CONTINUED AT A REDUCED AIRSPEED IN ACCORDANCE WITH THE CO MPANY OPERATIONS MANUAL TO TOL. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE FORWARD NOSE GEAR DOORS WERE OPE N. MAINTENANCE SECURED THE NOSE GEAR DOORS AND PERFORMED A GEAR SWING IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL WITH NO DISCREPANCIES NOTED, THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1998071700011 19980717 00011 NE 1998 7 17 9809786637 2 19980701 A 7261 613771 PUMP BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 1 ENGINE FAILED A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 637US 23548 715189 WHILE IN CRUISE FLIGHT, THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE. THE ENGINE WAS SHUT DOWN WHEN THE INDICATED OIL QUANTITY WAS ONE-HALF GALLON. THE FLIGHT CONTINUED TO SIN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ENGIN E OIL SCAVENGE PUMP AND RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1998071700012 19980717 00012 NE 1998 7 17 9809796637 2 19980703 A 7260 SEAL BOEING 747 747251B 1384892 NM PWA JT9 JT9D7R4G2 52054 NE NR 1 ENG GEARBOX FAILED A NWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 637US 23548 715189 WHILE IN CRUISE FLIGHT, THE NR 1 ENGINE OIL QUANTITY AND PRESSURE DROPPED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT CONT INUED TO NRT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ACCESSORY GEARBOX CARBON SEALS FOR THE HYDRAULIC PUMP A ND STARTER. SUBSEQUENT ENGINE RUN-UP FOUND NO LEAKS AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1998071700013 19980717 00013 NE 1998 7 17 COMA9860167 2 19980707 A 7321 6078T55P12 FCU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE FAILED A COMA K NONE O OTHER AP APPROACH 1 SO 01 989CA 1130 7215 807524 THE NR 2 ENGINE HAD ROLL BACK DURING LANDING APPROACH. REPLACED THE FUEL CONTROL UNIT. 2 L 7 2 4F 4 F RT A21EA E15NE 1998071700014 19980717 00014 EA 1998 7 17 COMA9860168 1 19980707 A 2421 IDG CNDAIR CL600 CL6002B19 EA NR 1 GENERATOR REQD SERVICE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 941CA 7050 NR 1 GENERATOR FAILED DURING TAKEOFF. FOUND IDG OIL LEVEL LOW. SERVICED OIL AND IDG RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1998071700015 19980717 00015 EA 1998 7 17 COMA9860169 1 19980705 A 2913 848847 PUMP CNDAIR CL600 CL6002B19 EA NR 3 HYD SYST LOW PRESSURE A COMA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 989CA 1131 7215 LANDING GEAR DISAGREEMENT WARNING DURING GEAR EXTENSION. REPLACED SYSTEM 3A HYRAULIC PUMP. 2 L 7 2 4F RT A21EA 1998071700016 19980717 00016 EA 1998 7 17 COMA9860170 1 19980630 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA E/E COMPT FAILED A COMA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 01 965CA 78 7131 FLIGHT SPOILERS CAUTION MESSAGE. REPLACED THE NR 2 SECU. 2 L 7 2 4F RT A21EA 1998071700017 19980717 00017 EA 1998 7 17 COMA9860171 1 19980627 A 5753 601R140021 VANE CNDAIR CL600 CL6002B19 EA LT TE FLAP DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 948CA 12139 7079 C-CHECK TASK 002-27-580-100 LEFT WING INBORAD FLAP VANE AT WS 86.30 HAS CHAFE DAMAGE. REPLACED FLAP. 2 L 7 2 4F RT A21EA 1998071700018 19980717 00018 EA 1998 7 17 COMA9860172 1 19980628 A 5320 601R350125251 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 948CA 7104 7079 C-CHECK TASK 002-53-170-320 TWO ANGLES CRACKED AT FS 621. REPLACED ANGLES. 2 L 7 2 4F RT A21EA 1998071700019 19980717 00019 EA 1998 7 17 COMA9860173 1 19980708 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA F ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 947CA 7137 7077 CARGO SMOKE WARNING DURING TAXI. FIRE BOTTLES DISCHARGED. CARGO SMOKE WAS FALSE WARNING. REPLACED SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 1998071700020 19980717 00020 EA 1998 7 17 COMA9860174 1 19980702 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 EA LT MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 751CA 7091 LEFT HAND MLG DISAGREE WARNING AFTER TAKEOFF. TIGHTENED LOOSE UPLOCK PROXIMITY SENSOR TARGET. 2 L 7 2 4F RT A21EA 1998071700021 19980717 00021 NM 1998 7 17 UPS98227126 1 19980708 A 2612 356802255 CONNECTOR BOEING 727 72725C 138400H NM NLG WW CORRODED A IPXA K NONE N FALSE WARNING AP APPROACH 1 SO 01 950UP 19718 AT APPROXIMETLY 3500 FT MSL WHEEL WEEL FIRE LIGHT ILLUMINATED WITH HORN (BELL) HOT BRAKES SHOULD NOT BE A FACTOR BRAKE C OOLING CHECKS WERE REFERENCED IN ROANOKE VA ALL APPROPRIATE CHECKLISTS ACCOMPLISHED. INSPECTED ALL LOOPS FOUND CONNECTO RS AT NOSE FIRE LOOP CORRODED, CLE ANED SAME, OPS CHECKS GOOD 2 L 7 3 4F A3WE 1998071700022 19980717 00022 NM 1998 7 17 UPS98227127 1 19980708 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION ON UPPER CHORD OF FLOORBEAM AT BS 344 FROM LBL 25 TO RBL 15. REMOVED AND REPLACED UPPER CH ORD AT FLOOR BEAM IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998071700023 19980717 00023 NM 1998 7 17 UPS98227128 1 19980706 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760-848, WL 208 R BL 45. REPLACED LONGITUDINAL FLOORBEAM AND SEAT TRACK (NRC 832504) BS 700 TO 848 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998071700024 19980717 00024 NM 1998 7 17 UPS98227129 1 19980706 A 5320 DOUBLER BOEING 727 72730C 1384009 NM BS 305 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI BONDED DOUBLER ON TOP SURFACE OF NLG (DOGHOUSE) IS CRACKED AT BS 305 LBL 2 WI L181. REPLACED DOUBLER 16.5 BY 24.5 LBL 14 TO RBL 14 PER 727 SRM 51-40-2, 51-30-2, 51-40-2. BONDED PER BAC5514-551 AND 5514-5101 AND DRAWING 65-18417 AND REPLACED STIFFENER BS 306 LBL 15 TO RBL 15 DUE TO OUT OF LIMITS CORROSION. 2 L 7 3 4F A3WE 1998071700025 19980717 00025 NM 1998 7 17 UPS98227130 1 19980706 A 5330 SKIN BOEING 727 72730C 1384009 NM BS 679 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-111-01.01-02) ON INTERNAL SKIN SURFACE OF LWR LAP JOINT AT BS 679 ABOVE STR 19L. REMO VED DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLERS PER 727 SRM 53-30-3. 2 L 7 3 4F A3WE 1998071700026 19980717 00026 NM 1998 7 17 UPS98227131 1 19980703 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 480-500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-111-01.00-02) ON STR 22R BS 480-500. REPLACED 22R STR CHANNEL BS 480 TO 500 PER 727 S RM 53-10-3. 2 L 7 3 4F A3WE 1998071700027 19980717 00027 NM 1998 7 17 UPS98227132 1 19980703 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 599-607 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI SEAT TRACK HAS CORROSION BS 599 TO 607 LBL 25 WL 208. REPLACED SEAT TRACK BS 540 TO 615 LBL 25 PER 7 27 SRM 53-10-5, 51-30-2, 53-10-1. 2 L 7 3 4F A3WE 1998071700028 19980717 00028 NM 1998 7 17 UPS98227133 1 19980703 A 5347 FLOOR TRACK BOEING 727 72730C 1384009 NM BS 568-582 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI SEAT TRACK HAS CORROSION UNDER NUT CLIPS BS 568-582 LBL 25 WL 208. REPLACED SEAT TRACK EXTRUSION FRO M 540 TO 615 PER SRM 53-10-5, 53-10-2, 51-20-151, 51-30-2. 2 L 7 3 4F A3WE 1998071700029 19980717 00029 NM 1998 7 17 UPS98227134 1 19980703 A 5320 FITTING BOEING 727 72730C 1384009 NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CRACK IN LT INBOARD 3A BOLT FITTING BS 1183 STRINGER 3A LT INBRD FITTING FWD FITTING. REPLACED FITTI NG 65-25591-9 PER SRM 51-10-1 AND MM 51-20-31. 2 L 7 3 4F A3WE 1998071700030 19980717 00030 NM 1998 7 17 UPS98227135 1 19980703 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760-848 LBL 25 WL 208. REPLACED LONG FLOORBEAM BS 760 TO 840 LBL 25 WL 208 AND EXPANSION LINK FROM 850 TO BS 870 PER 727 SRM 53-10-1 AND 51-30-2 EXPANSION LINK BS 850 TO 870 WILL BE REPLACED ON NRC 832520. 2 L 7 3 4F A3WE 1998071700031 19980717 00031 NM 1998 7 17 UPS98227136 1 19980703 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-111-01.00-01) ON STR 21R BS 312. REPLACED STRINGER CHANNEL FROM BS 292 TO 315 IAW SRM 51-10-7, 53-10-1 AND 53-10-3. 2 L 7 3 4F A3WE 1998071700032 19980717 00032 NM 1998 7 17 UPS98227137 1 19980621 A 5741 FITTING BOEING 727 72730C 1384009 NM WING/FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI RIGHT WING REAR SPARS BOTTLE PIN AND BODY SIDE ARE DAMAGED (CORROSION C53-100-05-4B). REMOVED BUSHIN G FOUND CORROSION OUT OF LIMITS IAW SRM 53-40-1 AND HAD BOEING REPAIR IAW DRAWING 65C36301 AND BOEING AGREEMENT NR 6-117 1-TA954. 2 L 7 3 4F A3WE 1998071700033 19980717 00033 EU 1998 7 17 98FDEA00438 1 19980709 A 5210 DOOR AIRBUS 310 A310203 EU CABIN NOT CLOSED A FDEA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 25 403FE 203 98-0171 - STA-MEM: ECAM DOOR NOT CLOSED IN FLT UPON VISUAL CK. NOTED AIR NOISE WARNING HORN, RED BAR. INSPECTED RT ENT RY DOOR. NO VISUAL DISP NOTED ON LOCKING MECHANISMS AND ASSOCIATED INDICATORS REMOVED DOOR LINING AND LUBED SPRINGS, RO LLER AND RODS. PERFORMED PULL TEST IAW M/M 52-10-11. ALL OK. REINSTALLED LINING. 2 L 7 2 4F RT A35EU 1998071700034 19980717 00034 EU 1998 7 17 98FDEA00439 1 19980709 A 2131 CONTROLLER AIRBUS 300 A300F4605R 3930327 EU NR 2 FAILED A FDEA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SO 25 670FE 777 STA-IAH: AT FL 310 DUAL PACK FAILURE SIMULTANEOUSLY. FOLLOWED ECAM PROC, COULD NOT RESTORE PACKS. CABIN CLIMBED ABOVE 10,000 FT AT WHICH TIME GOT CABIN EXCESS ECAM WARN DIRECTING A DESCENT TO 10,000 MSL. DECLARED EMERGENCY WITH ATC. DE SCENDED TO 10,000 FT WITH O2 MASKS ON. DIVERTED TO IAH FOR REPAIRS. ALL OTHER PRESSURIZATION INDICATIONS WERE NORMAL P RIOR TO FAILURE. FOUND NR 2 CONTROLLER NOT (BITE TEST) IN FLT POS, IT WAS IN COMP POS. RETURNED TO FLT POS. ALL BITE CKS NORMAL ON BOTH CONTROLLERS, OK FOR RETURN TO SERVICE. 2 L 7 2 4F RT A35EU 1998071700035 19980717 00035 NM 1998 7 17 SCNA98070 1 19980704 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE FROM SEAT ROW 6 AFT. FO UND A BROKEN GROUND WIRE AND REPAIRED AS REQUIRED. OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1998071700036 19980717 00036 NM 1998 7 17 P5CA9801125 1 19980630 A 7110 COWL BOEING 747 747124 1384874 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 2 INBOARD POWER COWL PREVIOUS REPAIR CRACKED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998071700037 19980717 00037 NM 1998 7 17 P5CA9801126 1 19980701 A 5414 SKIN BOEING 747 747124 1384874 NM NR 2 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 2 ENGINE PYLON, EXTERNAL SKIN, LOOSE AND WORKING FASTENERS. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700038 19980717 00038 NM 1998 7 17 P5CA9801127 1 19980701 A 5730 PANEL BOEING 747 747124 1384874 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LEFT WING FLYING PANEL HAS PROTECTIVE SEALANT PEELING. RESEALED PER SRM 51-21-03. 2 L 7 4 4F A20WE 1998071700039 19980717 00039 NM 1998 7 17 P5CA9801128 1 19980701 A 7110 COWL BOEING 747 747124 1384874 NM NR 3 ENGINE BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 3 ENGINE OUTBOARD POWER COWL RIB ANGLE BROKEN. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700040 19980717 00040 NM 1998 7 17 P5CA9801129 1 19980701 A 7110 CHAFE STRIP BOEING 747 747124 1384874 NM NR 2 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 2 ENG CORE COWL CHAFE STRIP DAMAGED/CRACKED. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700041 19980717 00041 NM 1998 7 17 P5CA9801130 1 19980701 A 3250 RIVETS BOEING 747 747124 1384874 NM RT MLG HINGE PIN SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 RIGHT BODY GEAR STEERING HINGE PIN BRACKET HAS SHEARED RIVETS. REMOVED AND REPLACED RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700042 19980717 00042 NM 1998 7 17 P5CA9801131 1 19980701 A 5230 FRAME BOEING 747 747124 1384874 NM CARGO DOOR DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 MAIN DECK CARGO DOOR FRAME LOWER FWD END IS DAMAGED. REPAIRED PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998071700043 19980717 00043 NM 1998 7 17 P5CA9801132 1 19980701 A 5400 BRACE BOEING 747 747124 1384874 NM NR 2 ENG PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 2 ENGINE PYLON DIAGONAL BRACE FORWARD LOWER END HAS CHAFE MARKS. BLENDED PER SRM 54-40-01 FIG 3. TREATED/PAINT PER SRM 51-10-02. 2 L 7 4 4F A20WE 1998071700044 19980717 00044 NM 1998 7 17 P5CA9801133 1 19980701 A 7110 COWL BOEING 747 747124 1384874 NM NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 3 ENGINE INBOARD CORE COWL HINGE BRACKET HAS CRACKED MOUNT. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700045 19980717 00045 NM 1998 7 17 P5CA9801134 1 19980701 A 5321 FLOOR BOEING 747 747124 1384874 NM COCKPIT DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 COCKPIT AREA, FLOOR PANEL UNDER F/E TABLE IS DELAMINATED. REPAIRED PER SRM 51-10-01 AND SRM 51-10-02. 2 L 7 4 4F A20WE 1998071700046 19980717 00046 NM 1998 7 17 P5CA9801135 1 19980701 A 7810 RIVETS BOEING 747 747124 1384874 NM NR 3 EXHAUST SHEARED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 3 ENGINE EXHAUST PLUG MOUNT BRACKET SHEARED RIVETS. REPLACED SHEARED RIVETS PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700047 19980717 00047 NM 1998 7 17 P5CA9801136 1 19980701 A 5230 ANGLE BOEING 747 747124 1384874 NM CARGO DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 LOWER FORWARD CORNER OF MAIN DECK CARGO DOOR HAS CRACKED T ANGLE. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998071700048 19980717 00048 NM 1998 7 17 P5CA9801137 1 19980701 A 5414 SKIN BOEING 747 747124 1384874 NM NR 1 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 1 PYLON INBOARD AFT LOWER SKIN HAS LOOSE FASTENERS. FASTENERS REMOVED AND REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700049 19980717 00049 NM 1998 7 17 P5CA9801138 1 19980701 A 5414 SKIN BOEING 747 747124 1384874 NM NR 1 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 1 PYLON OUTBOARD AFT LOWER SKIN HAS LOOSE FASTENERS. REMOVED AND REPLACED FASTENERS PER 51-30-20. 2 L 7 4 4F A20WE 1998071700050 19980717 00050 NM 1998 7 17 P5CA9801139 1 19980701 A 5414 SKIN BOEING 747 747124 1384874 NM NR 2 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 2 PYLON INBOARD SIDE HAS MANY LOOSE FASTENERS. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998071700051 19980717 00051 1998 7 17 P5CA9801140 2 19980701 A 7230 SLEEVE BOEING 747 747124 1384874 NM NR 1 FAN GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 855FT 19733 NR 1 FAN REVERSER SLEEVE ASSY. AFT INBOARD SIDE HAS GOUGE. REPAIRED PER SRM 51-24-11. 2 L 7 4 4F A20WE 1998071700052 19980717 00052 WP 1998 7 17 RRXA980246 1 19980702 A 2120 SEAL DOUG DC8 DC873 302199C WP CABIN FAILED A RRXA G O2 MASK DEPLOYED E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 15 105WP 46095 LOST LT PACK AT 35,000, CABIN DEPRESSURIZED, DEPLOYED MASKS. SUSPECT TURBINE IN TRIP. REF 6671-03 AND 6671-08, SAME CO NDITION. PACK TEMP WAS ABOVE 85 DEG C. ALSO, NOTABLE FLOOR VIBRATION INDICATED. DESCENDED TO 31,000 RE-INSTATED L-PAC K AND OPENED COOLING DOOR 20 PERCENT. DEFERRED PER MEL 21-38 CAT 'C', DMI NR 807031, PLACARD INSTALLED. CLOSED 7/3/98 REPLACED SEAL BETWEEN PRIMARY HEAT EXCHANGER AND FUSELAGE, NO LEAKS NOTED. CHECKS NORMAL PER MM 21-54-0. THIS CLEARS MEL NR 807031, PLACARD REMOVED. 2 L 7 4 4F RT 4A25 1998071700053 19980717 00053 1998 7 17 RRXA980247 4 19980707 A 3442 20671570153 RT UNIT DOUG DC8 DC862 3021970 WP E/E COMPT FAILED A RRXA A UNSCHED LANDING L NO TEST CL CLIMB 1 WP 15 993CF 46028 IR TURN-BACK, WX RADAR INOP, NO RETURNS (GND OR WX). REMOVED AND REPLACED RADAR RT, OPS CHECK GOOD ON GROUND. 2 L 7 4 4F 4A25 1998071700054 19980717 00054 WP 1998 7 17 ARWA980703 1 19980706 A 5270 SWITCH DOUG DC8 DC863 302198A WP FUSELAGE OUT OF ADJUST A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 345JW 46042 LCK - FLT 507 - BELLY DOOR ILLUMINATED, ABORTED TAKEOFF AND RETURNED TO BLOCKS. AFTER BELLY DOOR WAS CYCLED AND LIGHT E XTINGUISHED. SECOND TAKEOFF WAS UNEVENTFUL. BRAKE TEMPS OK, ABORTED LESS THAN 60 KNOTS. TROUBLESHOT AND FOUND 'C' BEL LY DOOR LIMIT SWITCH AT FAULT. SWITCH REPOSITIONED, DOOR TESTED SEVERAL TIMES SATISFACTORY IAW DC-8 MM 52-00-00. ALSO, BRAKE TEMPS CHECKED NORMAL AFTER TAKEOFF ABORT IAW AOM VOL NR 1 P 4300 PN REVISION 1. (M) 2 L 7 4 4F 4A25 1998071700055 19980717 00055 1998 7 17 TC8A98039 4 19980707 A 3442 20671570153 RT UNIT DOUG DC8 DC862F 3021972 WP E/E COMPT FAILED A TC8A A UNSCHED LANDING O OTHER UK UNKNOWN 1 GL 23 187SK 3933 46022 WEATHER RADAR SPOKING, NO TARGETS. REMOVED AND REPLACED RADAR R/T IAW DC8 MM 34-41-0, ALL OPS OK. 2 L 7 4 4F 4A25 1998071700062 19980717 00062 NE 1998 7 17 CHIA3099 2 19980613 A 7314 216079004 PUMP 200102021 BOEING 234 234 1385049 EA LYC AL5512 AL5512 41581 NE NR 2 ENGINE WORN A CHIA K NONE O OTHER IN INSP/MAINT 1 NM 09 241CH 5639 MJ016 LE60022 DURING TAKEOFF CHECK, PILOT NOTICED NR 2 FUEL PRESS 12 PSI LOWER THAN NR 1. THIS IS LOWER THAN IT NORMALLY OPERATES WIT H ENG AT FLY AND BOTH FUEL TANK BOOST PUMPS ON. PILOT VERIFIED FUEL TANK BOOST PUMPS OPERATIONAL. VERIFIED FUEL PRESS IND READING PROPERLY. WHEN BOTH NR 2 FUEL TANK BOOST PUMPS WERE TURNED OFF, NR 2 FUEL PRESS WENT INTO YELLOW. REMOVED NR 2 ENG DRIVEN FUEL PUMP AND FND INPUT SHAFT COULD BE TURNED WITH NO MOVEMENT OF PUMP IMPELLER. REMOVED AND REPLACED FUEL PUMP. SHAFT SPLINES WORN ALLOWING IT TO DISENGAGE. MALE SPLINES OF THE SHAFT HAD SMALL AREA OF WEAR. LENGTH OF FE MALE SPLINES OF THE PUMP ARE SMALLER THAN LENGTH OF MALE SPLINES CAUSING WEAR TO BE CONCENTRATED ON A SMALL AREA. (X) 2 G 7 2 4U 4 U H9EA E4NE 1998071700063 19980717 00063 WP 1998 7 17 CHIA3096 1 19980618 A 7933 369A45333 SENDER HUGHES 369 369D 4470706 WP OIL TEMP FAILED A CHIA K NONE O OTHER IN INSP/MAINT 1 NM 09 502CH 14 180252D AFTER 14.2 HOURS, THE OIL TEMPERATURE STARTED READING HIGH. AFTER TROUBLESHOOTING, THE SENDER WAS CHANGED AND THE PROBL EM WAS CORRECTED. 1 G 7 1 3U H3WE 1998071700173 19980717 00173 WP 1998 7 17 VJ980022 1 19980711 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 967VV 47170 EMERGENCY LIGHTS IN FWD GALLEY INOP. REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY IAW MM 33-50. 2 L 7 2 4F A6WE 1998071700174 19980717 00174 NM 1998 7 17 RAAA98B2037 1 19980710 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 10 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998071700175 19980717 00175 EU 1998 7 17 QXEA9800932 1 19980707 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 BOI - 28 VOLT LIGHTS INOPERATIVE ON AFT SIDE OF AISLE EMERGENCY LIGHTS. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071700176 19980717 00176 EU 1998 7 17 QXEA9800933 1 19980707 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 GEG - BOTTOM EMERGENCY EXIT LIGHT OUT BY DOOR SLIDE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071700177 19980717 00177 EU 1998 7 17 QXEA9800934 1 19980707 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 BOI - EMERGENCY EXIT LIGHT AT 9A INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071700178 19980717 00178 EU 1998 7 17 QXEA9800935 1 19980707 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 PDX - EXIT LIGHTS BURNT OUT IN EXIT SIGN ON CEILING BETWEEN ROWS 8 AND 9. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED , TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071700179 19980717 00179 NM 1998 7 17 QXEA9800936 1 19980707 A 3350 6104781 BATTERY DHAV 82410162007 DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 811PH 16705 213 23 PDX- LEFT HAND FORWARD EXTERIOR EMERGENCY LIGHT IS INOP. INSPECTED AND FOUND BATTERY PACK 3351-PS1 MALFUNCTION. REPLAC ED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998071700180 19980717 00180 NM 1998 7 17 QXEA9800937 1 19980708 A 5280 85420012091 DOOR DHAV 85420012031 DHAV DHC8 DHC8202 2809007 NM LT MLG DAMAGED A QXEA K NONE O OTHER CR CRUISE 1 NM 09 354PH 498 PDX - LEFT GEAR DOOR HANGING DOWN ABOUT 2 INCHES IN FLIGHT. ADJUSTED THE CENTER GEAR DOOR AND REPLACED THE NR 1 AFT OUT BOARD GEAR DOOR (DAMAGED). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998071700181 19980717 00181 EU 1998 7 17 QXEA9800938 1 19980709 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 PDX - EXIT ROW 8 EMERGENCY EXIT LIGHT BULB OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071700182 19980717 00182 EU 1998 7 17 QXEA9800939 1 19980709 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 SEA - LOWER EVACUATION LIGHT OUT BY ESCAPE SLIDE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998071700183 19980717 00183 NM 1998 7 17 QXEA9800940 1 19980709 A 3350 6014781 BATTERY DHAV 82410167007 DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 825PH 213 PDX - RIGHT FORE FUSELAGE EMERGENCY LIGHT INOP, RIGHT EXIT SIGN WITH THRESHOLD LIGHTS INOP, AND FRONT CABIN EXIT LOCATOR LIGHTS INOP. REPLACED PS2 BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998071700184 19980717 00184 NM 1998 7 17 QXEA9800941 1 19980709 A 3350 10126267 SIGN DHAV DHC8 DHC8102 2809003 NM CABIN MISSING A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 829PH 304 SEA - ROW 4AB EMERGENCY EXIT SIGN MISSING. REPLACED EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED T O SERVICE. 2 H 7 2 4T RT A13NM 1998071700185 19980717 00185 WP 1998 7 17 98FDEA00440 1 19980505 A 5320 AJC70135 WEB DOUG DC10 DC1010 3022110 WP BS 2007 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 STA-VCE LOWER AFTER FUSELAGE COMPARTMENT STA 2007 FOUND CRACK ON WEB CORNER. MAJOR REPAIR PERFORMED IAW EA 8-5317-3844 3 9-JULY 1998. 2 L 7 3 4F A22WE 1998071700186 19980717 00186 WP 1998 7 17 98FDEA00441 1 19980113 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 2092 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 CRACK ON LONGERON NR 4 LT SIDE. (REF SRM VOL III, 53-17-0 1, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LON GERON WITH SPLICES PER SRM 53-00-01 AND 53-10-00. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR CLIPS AND BRACKETS PER SRM 51-30-00. (15 JUNE 1998). 2 L 7 3 4F A22WE 1998071700187 19980717 00187 WP 1998 7 17 98FDEA00442 1 19980113 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 2092 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 N1087 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 EA CRACK ON LONGERON NR 5 LT SIDE. (REF SRM VOL II I, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PER SRM 53-00-01 AND 53-10-0. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR C LIPS AND BRACKETS PER SRM 51-30-00. (15 JUNE 1998). 2 L 7 3 4F A22WE 1998071700188 19980717 00188 WP 1998 7 17 98FDEA00443 1 19980113 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 2092 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 N1088 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 EA CRACK ON LONGERON NR 8, LT SIDE. (REF SRM VOL II I, 53-17-01, PAGE 20, FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONGERON WITH SPLICES PER SRM 53-00-01 AND 53-10-00. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR CLIPS AND BRACKETS PER SRM 51-30-00. (15 JUNE 1998). 2 L 7 3 4F A22WE 1998071700189 19980717 00189 WP 1998 7 17 98FDEA00444 1 19980113 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 2092 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 STA-VCE: AFT FUSELAGE UPPER TAIL BODY AT STA Y 2092, FOUND 1 CRACK ON LONGERON NR 9 LT SIDE. (REF SRM VOL III, 53-17-0 1, PAGE 20 FIG 5 AND PAGE 1, FIG 1). REMOVED SHEAR CLIPS AND BRACKETS, CUT OUT SECTION OF CRACK. INSTALLED REPAIR LONG ERON WITH SPLICES PER SRM 53-00-01 AND 53-10-00. REINSTALLED FASTENERS PER SRM 51-33-01. REINSTALLED SHEAR CLIPS AND B RACKETS PER SRM 51-30-00. (15 JUNE 1998). 2 L 7 3 4F A22WE 1998071700190 19980717 00190 WP 1998 7 17 98FDEA00445 1 19980130 A 5321 FLOOR DOUG DC10 DC1010 3022110 WP BS 1149 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 N1326 STA-VCE: UPPER FUSELAGE INTERNAL RT SIDE, AT STA 1149 FOUND 2 EA CRACKS 2 LONG ON FLOOR WEB L27. REMOVED CRACK ED FLOOR WEB AND REPLACED WITH A NEW ONE IAW SRM 51-41-01 AND 51-35-01. (11 JUNE 1998). 2 L 7 3 4F A22WE 1998071700191 19980717 00191 WP 1998 7 17 98FDEA00446 1 19980121 A 5230 SKIN DOUG DC10 DC1010 3022110 WP CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 365FE 46601 STA-VCE AFTER SCUFF PLATE REMOVAL ON LOWER CENTER CARGO DOOR IAW NRC N0933/F009933, FOUND LARGE AREA WITH SPREAD SEVERE CORROSION FROM STA 1701 TO STA 1781. MAJOR REPAIR PERFORMED REPAIR BY REPLACEMENT OF DAMAGED SKIN AND SPLICED IAW SRM 53-20-00, FIG 6. REMOVED CORROSION AND TREATED SKIN WITHIN ALLOWABLE LIMITS IAW SRM 51-21-01 AND 53-00-01 FIG 4. INSTA LLED SCUFF PLATE. 2 L 7 3 4F A22WE 1998071700193 19980717 00193 NM 1998 7 17 98FDEA00448 1 19980709 A 3260 H1010153 SWITCH BOEING 727 72722 1384002 NM NLG INOP A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 184FE 18870 STA-MEM: NOSE GEAR UNSAFE. RECYCLED 4 TIMES, FOURTH TIME AFTER 3 MINUTES DELAY GOT GREEN LIGHT. NOSE ALIGNMENT STRIPE SAFE. REPEAT. INSTALLED (3) GEAR LOCK PINS. REMOVED AND REPLACED NOSE GEAR POSITION SWITCH PER 32-61-20. OPERATIONA L CHECK PER MAINTENANCE MANUAL 32-61-21 PAGE 502, OPERATION NORMAL. REMOVED AND STOWED 3 GEAR LOCK PINS. 2 L 7 3 4F A3WE 1998071700194 19980717 00194 NE 1998 7 17 98FDEA00449 2 19980710 A 7261 LINE BOEING 727 727233 138408A NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTION A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 267FE 21673 STA-IND - NR 1 ENGINE LOST OIL QUANTITY APPROXIMATELY 5 MINUTES LATER OIL PRESSURE STARTED TO DROP. ENGINE SHUT DOWN PE R RED TABS. OIL PRESSURE NEVER AT 0 PSI. WINDMILLED WITH OIL PRESS AT 20 PSI FOR 20 MINUTES. REMOVED AND REPLACED OIL LINE TO #6 BEARING, RAN ENGINE, AND PERFORMED LEAK CHECK, ALSO COMPLIED WITH MAIN OIL STRAINER INSP ITEM 2. NO METAL N OTED AIRCRAFT. OK FOR SERVICE. 2 L 7 3 4F 4 F RT A3WE E2EA 1998071700195 19980717 00195 NE 1998 7 17 98FDEA00450 2 19980709 A 7261 DRAIN LINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE OPEN A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 307FE 48291 STA-BKK - IN CRUISE AT FL 330, 2.5 HOURS INTO FLIGHT NUMBER 2 ENGINE OIL PRESS COW LIGHT CAME ON AND OIL QUANTITY WENT T O 0 DID RED TABS PROCEDURE AND SHUT DOWN ENGINE. LANDED BKK WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE OIL MA STER CHIP DETECTOR, NO METAL FOUND. CAPPED OFF LEFT HYDRO PUMP SEAL DRAIN LINE. 2 L 7 3 4F 4 F A22WE E23EA 1998071700196 19980717 00196 NM 1998 7 17 98FDEA00451 1 19980711 A 3260 H1010154 SWITCH BOEING 727 72722 1384002 NM NLG MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 184FE 18870 98-0176 STA-MEM: AFTER TAKEOFF WHEN GEAR WAS RAISED, THE GREEN NLG LIGHT AND RED GEAR DOOR LIGHT FOR NOSE GEAR REMAINE D ON. AFM PROCEDURES WERE FOLLOWED BUT NO LUCK. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX AND NLG LOCK SWITCH P ER M/M 32-61-21. REMOVED AND REPLACED NOSE DOWN LOCK LINKAGE. OPS CHECK PER M/M 32-61-21. OPS CHECK GOOD ON GEAR SWIN G PER M/M 32-34-0. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998071700197 19980717 00197 WP 1998 7 17 98FDEA00452 1 19980221 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1236 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 N2203 STA-VCE: AFTER REMOVAL OF CORROSION ON LOWER SKIN BETWEEN STA 1236 AND STA 1521, LONGERON NR 48 RT TO LONGERON N R 48 LT, MATERIAL REMOVED IS OUT OF LIMITS. MAJOR REPAIR PERFORMED IAW EA 8-5334-38436. (08 JULY 1998). 2 L 7 3 4F A22WE 1998071700198 19980717 00198 WP 1998 7 17 98FDEA00453 1 19980109 A 5313 LONGERON DOUG DC10 DC1010 3022110 WP BS 1521-1541 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 377FE 47965 STA-VCE LONGERON NR 45, BETWEEN STA 1521 AND 1541 PRESENTS A PUNCHING DAMAGE NEAR THE 4TH HOLE IN THE MIDDLE ROW. MAJ OR REPAIR PERFORMED IAW EA 8-5315-38441. 2 L 7 3 4F A22WE 1998071700199 19980717 00199 NM 1998 7 17 98FDEA00454 1 19980702 A 5720 651594065 CHORD BOEING 727 72722 1384002 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 STA-PAE - LOWER CHORD AT BS 740 IS CORRODED AT RBL 13 TO RBL 20. COMPLIED WITH EA 7-5710-39850 ACCESS BLENDED AND TREAT ED CORROSION ON LOWER CHORD 740, RBL 13 - RBL 20. RESTORED AREA IAW ER 98-2645. 2 L 7 3 4F A3WE 1998071700200 19980717 00200 WP 1998 7 17 ABXA9800614 1 19980708 A 3260 7000010101ABX1 SWITCH DOUG DC8 DC863F 302198F WP LT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 ON DEPARTURE, DURING GEAR UPLATCH CHECK, GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ALTERNATE UPLATCH CHECK AND CONFIRMED TO BE LEFT MAIN GEAR UPLATCH. RECYCLED GEAR, SAME RESULTS. REPLACED LEFT MAIN LANDING GEAR UPLATCH SWITCH IAW DC8 MM 32-60-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998071700201 19980717 00201 WP 1998 7 17 ABXA9800615 1 19980708 A 2750 57511531 LINK DOUG DC8 DC863 302198A WP RT TE FLAP BROKEN A ABXA O OTHER J WARNING INDICATION AP APPROACH 1 GL 23 821AX 46116 WITH FLAPS SET AT 35 DEGREES THE INDICATOR SHOWED 5 DEGREES OF SPLIT, REQUIRING 2 DEGREES OF LEFT AILERON TRIM. REPLACE D BROKEN RIGHT FLAP DRIVER LINK IAW DC8 MM 27-51-04. RIGGED FLAP SYSTEM IAW DC8 MM 27-50-00. 2 L 7 4 4F 4A25 1998071700202 19980717 00202 WP 1998 7 17 ABXA9800604 1 19980701 A 5312 295015 BULKHEAD WEB DOUG DOUG DC8 DC861 3021952 WP FWD FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 RADOME BULKHEAD, RIGHT WEB HAS TWO 15 INCH CRACKS, 6 ABOVE AND BELOW FRP. REPAIRED IAW ABX REA D853-23417 MR. 2 L 7 4 4F 4A25 1998071700203 19980717 00203 WP 1998 7 17 ABXA9800605 1 19980701 A 5320 215591 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 860 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 MAIN CABIN LONGERON END FITTING AT STATION 860, LONGERON 10R CRACKED. REPAIRED IAW DC8 SRM'S 51-1-24 AND 51-1-20D. 2 L 7 4 4F 4A25 1998071700204 19980717 00204 WP 1998 7 17 ABXA9800606 1 19980701 A 5312 255263 BULKHEAD TEE CAP DOUG DOUG DC8 DC861 3021952 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 853AX 46037 AFT PRESS BULKHEAD TEE CAP CRACKED AT LONGERON 10R. REPAIRED IAW DC8 SRM 53-2-5, 51-1-20D AND 51-3-0. 2 L 7 4 4F 4A25 1998071700205 19980717 00205 WP 1998 7 17 ABXA9800607 1 19980703 A 5400 995815958 ANGLE DOUG DOUG DC9 DC933F 302207A WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND RIGHT PYLON STRUCTURE CRACKED AT STATION 1033 OUTBOARD OF PANEL 8206 BOTTOM OF PYLON. REPLACED AN GLE IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998071700206 19980717 00206 WP 1998 7 17 ABXA9800608 1 19980703 A 5510 5918000518 TEE CAP DOUG DOUG DC9 DC933F 302207A WP LT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND LEFT HORIZONTAL STABILIZER AFT UPPER TEE CAP EXFOLIATED AT HINGE POINT, AT STATION 204. REPAIRED TEE CAP IAW ABX REA D955-23948 MR. 2 L 7 2 4F A6WE 1998071700207 19980717 00207 WP 1998 7 17 ABXA9800609 1 19980703 A 5315 9922397501 FLOORBEAM DOUG DOUG DC9 DC933F 302207A WP BS 937 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 933AX 47291 DURING C-CHECK, FOUND UPPER CARGO COMPARTMENT FLOORBEAM AT STATION 937 LOWER TEE CAP CORRODED BEYOND LIMITS BETWEEN BL 0 AND LBL 40 TO 54. REPAIRED FLOORBEAM IAW ABX REA D953-24050 MR. 2 L 7 2 4F A6WE 1998071700208 19980717 00208 WP 1998 7 17 ABXA9800610 1 19980707 A 5310 9910078301 STRUCTURE DOUG DOUG DC9 DC915 3022036 WP BS 170 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK FOUND FORWARD SUB FLOOR CRACKED AT STATION 170 LBL 40. REPAIRED CRACKED SUB FLOOR IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998071700209 19980717 00209 WP 1998 7 17 ABXA9800611 1 19980707 A 5313 59114279 LONGERON DOUG DOUG DC9 DC915 3022036 WP BS 786 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK, FOUND LONGERON 17 RIGHT CRACKED AT FUSELAGE STATION 786. REPLACED LONGERON 17 RIGHT SECTI ON AT STATION 786 IAW DC9 SRM. 2 L 7 2 4F A6WE 1998071700210 19980717 00210 WP 1998 7 17 ABXA9800612 1 19980707 A 5711 59113021 SPAR CAP DOUG DOUG DC9 DC915 3022036 WP WS 459 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK, FOUND CORROSION ON LEFT WING FRONT SPAR UPPER CAP AT STATION XRS 459. REPAIRED UPPER CAP IAW REA D957-24092. 2 L 7 2 4F A6WE 1998071700211 19980717 00211 WP 1998 7 17 ABXA9800613 1 19980708 A 5210 3957087503 HOUSING DOUG DOUG DC9 DC915 3022036 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK, FOUND MAIN ENTRY DOOR EXTERIOR HANDLE HOUSING CRACKED. REPLACED HOUSING IAW DC9 SRM 51-30 -2. 2 L 7 2 4F A6WE 1998071700212 19980717 00212 WP 1998 7 17 MWEA98768 1 19980709 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR SHIFTED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 502ME 48132 CAN'T READ GALLEY DOOR SLIDE PRESSURE GAUGE DUE TO SHIFT OF SLIDE. MAINTENANCE ADJUSTED GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1998071700213 19980717 00213 WP 1998 7 17 MWEA98769 1 19980709 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP GALLEY SLIDE DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 THE GALLEY DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998071700214 19980717 00214 1998 7 17 MWEA98770 4 19980710 A 2565 D29982107 SLIDE DOUG MD88 MD88 3023688 NM SERVICE DOOR INOPERATIVE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 THE FORWARD SERVICE DOOR SLIDE FAILED AMP TEST. MAINTENANCE REMOVED AND REPLACED FORWARD SERVICE DOOR EMERGENCY SLIDE. 2 L 7 2 4F RT A6WE 1998071700215 19980717 00215 WP 1998 7 17 MWEA98771 1 19980708 A 3260 0080004003 CONTROL BOX DOUG DC9 DC932 3022066 WP COCKPIT MALFUNCTIONED A MWEA O OTHER N FALSE WARNING AP APPROACH 1 GL 31 215ME 47744 THREE RED UNSAFE LIGHTS STAYED ON UPON GEAR RETRACTION CYCLED GEAR DOWN AND RED LIGHTS STAYED ON WITHOUT ANY GREEN LIGHT S ON. REMOVED AND REPLACED PROX SWITCH CONTROL CIRCUIT BREAKER AND PROX SWITCH CONTROL BOX. 2 L 7 2 4F A6WE 1998071700216 19980717 00216 NM 1998 7 17 MWEA98772 1 19980710 A 5330 99115311 SKIN DOUG MD88 MD88 3023688 NM BS 284 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND DENT ON FUSELAGE SKIN IN WINDOW BELT AT FS 284. MAINTENANCE REMOVED AND REPLACED WINDOW PANEL. 2 L 7 2 4F RT A6WE 1998071700217 19980717 00217 NM 1998 7 17 MWEA98773 1 19980710 A 5230 59101575 PAN DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND GOUGE AND CRACK ON FORWARD CARGO DOOR INNER PAN AT EDGE OF PAN. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 1998071700218 19980717 00218 NM 1998 7 17 MWEA98774 1 19980710 A 5313 27779226 LONGERON DOUG MD88 MD88 3023688 NM BS 809 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND LONGERON 9L DENTED AT STATION 809. MAINTENANCE REPLACED LONGERON SECTION. 2 L 7 2 4F RT A6WE 1998071700220 19980717 00220 NM 1998 7 17 MWEA98776 1 19980710 A 5313 27779226 LONGERON DOUG MD88 MD88 3023688 NM BS 807 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND DENT ON LONGERON 10L AT STATION 807. MAINTENANCE REPLACED LONGERON SECTION. 2 L 7 2 4F RT A6WE 1998071700221 19980717 00221 NM 1998 7 17 MWEA98777 1 19980710 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 803 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND DENT ON SKIN AT STATION 803 BETWEEN LONGERON 16L AND 17L. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 1998071700222 19980717 00222 NM 1998 7 17 MWEA98778 1 19980710 A 5330 593271749 SKIN DOUG MD88 MD88 3023688 NM BS 807 823 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 SKIN PUNCTURED AT STATION 807 823 LONGERON 9-10L. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F RT A6WE 1998071700223 19980717 00223 NM 1998 7 17 MWEA98779 1 19980710 A 5230 59101575 PAN DOUG MD88 MD88 3023688 NM CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 MID CARGO DOOR IS GOUGED AND CRACKED AT EDGE OF DOOR AT THE FORWARD AND AFT HOLD OPEN HOOK CUT OUT. MAINTENANCE FABRICA TED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F RT A6WE 1998071700224 19980717 00224 NM 1998 7 17 MWEA98780 1 19980710 A 5330 5911408623 SKIN DOUG MD88 MD88 3023688 NM BS 315-330 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND DENT ON SKIN AT FS 315-330 LONGERON 10-11L. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 1998071700225 19980717 00225 NM 1998 7 17 MWEA98781 1 19980710 A 5330 59360013 SKIN DOUG MD88 MD88 3023688 NM BS 788-807 PUNCTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND PUNCTURE IN SKIN AT LONG 18-17L STATION 788 807. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F RT A6WE 1998071700226 19980717 00226 WP 1998 7 17 SCNA98518 1 19980710 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1912 CORROSION A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, STA 1912 RBL90 AT LAV MOUNT AREA CORROSION FOUND ON TRACK LEVEL 2. FABRICATED SEAT TRACK IAW SRM 51 2101 AND INSTALLED IAW SEAT TRACK IAW SRM 513000 FIG1. 2 L 7 3 4F A22WE 1998071700227 19980717 00227 WP 1998 7 17 SCNA98519 1 19980710 A 5347 SEAT TRACK DOUG DC10 DC1015 3022118 WP BS 1965 CORROSION A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, STA 1965 RBL77 AT LAV MOUNT AREA CORROSION FOUND ON TRACK LEVEL 2. FABRICATED SEAT TRACK IAW SRM 51 2101 AND INSTALLED IAW SEAT TRACK IAW SRM 513000 FIG 1. 2 L 7 3 4F A22WE 1998071700228 19980717 00228 WP 1998 7 17 SCNA98520 1 19980710 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1967-2007 CORROSION A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, STA 1947 TO 2007 AT RBL 55 AND RBL 60 COROSION FOUND ON FLANGE STRUCTURE. CUT OUT CORRODED AREA AND FABRICATED FLOOR SUPPORT AND SPLICE ANGLES PER SRM 537000 FIGURE 13 AND 530001, TREATED PARTS PER SRM 512101 AND INSTAL LED COMPLETE PER SRM 513101 2 L 7 3 4F A22WE 1998071700229 19980717 00229 WP 1998 7 17 SCNA98521 1 19980710 A 5322 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1947-2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, STA 1947 TO 2007 AT RBL 26 COROSION FOUND ON FLANGE STRUCTURE. GALLEY FLOOR SUPPORT CORRODED BEYOND LIMITS, FABRICATED REPAIR SUPPORT AND SPLICE IAW SRM 537000 FIG13. TREATED IAW SRM 512101 AND INSTALLED PER SRM 513101 . 2 L 7 3 4F A22WE 1998071700230 19980717 00230 WP 1998 7 17 SCNA98522 1 19980710 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1908 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, LEVEL 2 CORROSION STATION 1908 RBL56 ON CABIN FLOOR SUPPORT WAS DISCOVERED. CUT OUT CORRODED AREA AND FABRICATED FLOOR SUPPORT AND SPLICE ANGLES PER SRM 537000 FIG13, AND 530001 TREATED PARTS PER SRM 512101 AND INSTALL ED COMPLETE PER SRM 513101. 2 L 7 3 4F A22WE 1998071700231 19980717 00231 WP 1998 7 17 SCNA98523 1 19980710 A 5320 CHANNEL DOUG DC10 DC1015 3022118 WP GALLEY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE FORWARD INBOARD ATTACH POINT FOR THE G7 GALLEY WAS FOUND TO HAVE CORROSION ON THE FLOOR CHANNEL. THE GALLEY FLOOR SUPPORT WAS CORRODED BEYOND LIMITS REPAIR SUPPORT AND SPLICE WERE FABRICATED IAW SRM 537000 FIGURE13 AND TREATED IAW SRM 512101 AND INSTALLED IAW SRM 513101. 2 L 7 3 4F A22WE 1998071700232 19980717 00232 WP 1998 7 17 SCNA98524 1 19980710 A 5520 CHORD DOUG DC10 DC1015 3022118 WP RT ELEVATOR CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE RIGHT HAND INBOARD ACTUATOR SUPPORT STRUCTURES UPPER 'T' CHORD WAS FOUND TO BE CRACKED AT STATIO N XE103. REMOVED DAMAGED AREA AND REPAIRED IAW DWG SBX SBA 98 0124TR, SBX SBA 98 0140TR AND ROD SKETCH 980611010 AND AP PROVED BY 8110 3 DATED 980612, REFERENCE SCA ENGINEERING ORDER 55 5593 1. 2 L 7 3 4F A22WE 1998071700233 19980717 00233 WP 1998 7 17 SCNA98525 1 19980710 A 5400 WEB DOUG DC10 DC1015 3022118 WP NR 1 PYLON WORN A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE NUMBER 1 PYLON LEFT HAND SIDE INTERNAL STATION YN187 PYLON WEB LOWER CAP WAS FOUND WORN TO A KN IFE EDGE, FROM CHAFING AGAINST THE CABLE HOUSING VISIBLE THROUGH PANEL 437AL. ADJUSTED BRACKET AND REINSTALLED PER SRM 513101, REPAIRED IAW SBX SBA 98 0131TR AND APPROVED BY 8110 3, DATED 980611, REFER TO SCA EO 54 5594 1. 2 L 7 3 4F A22WE 1998071700234 19980717 00234 WP 1998 7 17 ARWA980704 1 19980609 A 5311 FRAME DOUG DC8 DC863 302198A WP BS 320 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 MAIN CARGO COMPARTMENT, FRAME AND ATTACHED PART DAMAGED, FS 320 AND L12R. CUT DAMAGED AREA. CLEANED SURROUNDING AREA I AW DC8 SRM 51-1-8. FABRICATED REPAIR PARTS IAW DC8 SRM 53-2-0, 53-4-1, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PA RTS IAW DC-8 SRM 51-1-8, 51-1-20D. ARROW AIR CONTROL NR 5254, FCT NRC 01123, WORK ORDER NR 020663, ENTERED ON LOG PAGE NR 75163, ITEM 203M. 2 L 7 4 4F 4A25 1998071700235 19980717 00235 WP 1998 7 17 ARWA980705 1 19980609 A 5751 SKIN DOUG DC8 DC863 302198A WP LT AILERON CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LEVEL I CORROSION, ON LT AILERON LOWER SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 57-2-0. REMO VED DAMAGED AREA CLEANED SURROUNDING AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW PLATING IAW EO NR CF-N345JW - 12/98 IRDTD 04/24/98. TREATED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21D. ARROW AIR CONTROL NR 1059. FCT NRC 0 961. WORK ORDER NR 020663. ENTERED ON LOG PAGE NR 75166, ITEM 214M. 2 L 7 4 4F 4A25 1998071700236 19980717 00236 WP 1998 7 17 ARWA980707 1 19980609 A 3150 SWITCHING UNIT DOUG DC8 DC863 302198A WP COCKPIT MALFUNCTIONED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 REMOVE INSTRUMENT SWITCHING UNIT-ROUTE TO STORES FOR COMPLIANCE OF EO 229-002, INSTALL INSTRUMENT SWITCHING UNIT-NOTING COMPLIANCE WITH EO 229-002/REMOVED INSTRUMENT SWITCHING UNIT-ROUTED TO STORES. INSTALLED SWITCHING UNIT EO 229-002. CO MPLIED BY AEROSERVICE AVIONICS FUNCTIONAL CHECK CARRIED OUT IAW 34-23-0. CHECK NORMAL. ARROW AIR CONTROL NR RB 8602 FC T NRC 01089. WORK ORDER NR 020663. ENTERED LOG PAGE 79015 106M. 2 L 7 4 4F 4A25 1998071700237 19980717 00237 WP 1998 7 17 ARWA980708 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1590 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 AFT FUSE SKIN BULGING 1 PLACE JUST AFT AND TOP OF RT RELIEF VALVE, FS 1590 L26R AND L27R. CUT DAMAGED AREA. CLEANED SU RROUNDING AREA IAW DC8 SRM 51-1-8. FABRICATED PARTS REPAIR IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4, TREATED, PRIMED AND INS TALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D. ARROW AIR CONTROL NR 5339. FCT NRC WORK ORDER NR 020663. 2 L 7 4 4F 4A25 1998071700238 19980717 00238 WP 1998 7 17 ARWA980709 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1570 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 AFT FUS SKIN BULGING 1 PLACE JUST AFT AND TOP OF RT RELIEF VALVE, FS 1570, L24R AND L25R. CUT DAMAGED AREA, CLEANED SUR ROUNDING AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4. TREATED, PRIMED AND IN STALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D. ARROW AIR CONTROL NR 5346 FCT. WORK ORDER 020663 . 2 L 7 4 4F 4A25 1998071700239 19980717 00239 WP 1998 7 17 ARWA980710 1 19980609 A 5712 RIB DOUG DC8 DC863 302198A WP WS 291.5 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LT WING SPLICE PAN OF INBOARD SLOT CRACKED XW 257.5 INBOARD SLOT INNER SKIN CRACKED. 6 INCH CRACK IN LE UPPER RIB XFS 2 91.5. REMOVED SPLICE PAN AND INNER DOUBLER AT LT WING STATION XILD 42. CLEANED SURROUNDING AREA IAW DC-8 SRM 51-1-8. F ABRICATED REPAIR PARTS IAW DC-8 DPS 4.710. TREATED AND PRIMED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11. DRILLED STOP HOLE AT END OF RIB CRACK 0.25 DIAMETER. REPAIRED CRACKED RIB IAW DC-8 SRM 57-2-0 FIG 2 SH 2. INSTALLED SPLICE PAN P/N ARW 5769859050598 AND SLOT SKIN IAW DC-8 SRM 57-3-3, FIG 3 SH 3, ITEM J, 51-1-20D AND 51-1-21. ARROW AIR CONTROL NR 103 6. FCT NRC 0886. WORK ORDER NR 020663. 2 L 7 4 4F 4A25 1998071700240 19980717 00240 WP 1998 7 17 ARWA980711 1 19980609 A 5320 SPLICE DOUG DC8 DC863 302198A WP BS 8 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 COCKPIT LEVEL II CORROSION IN SPLICE AND L24R, FS 8.00O. REMOVED DAMAGED SECTION, CLEANED SURROUNDING AREA IAW DC-8 SRM 51-1-8, FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-2, 53-3-3, 51-1-4. TREATED AND PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-20D. ARROW AIR CONTROL NR 4127, FCT NRC 01094. WORK ORDER NR 020663. ENTERED ON LOG NR 75165, ITEM 209M. 2 L 7 4 4F 4A25 1998071700241 19980717 00241 WP 1998 7 17 ARWA980712 1 19980609 A 5310 STRUCTURE DOUG DC8 DC863 302198A WP BS 67 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 FLIGHT COMPARTMENT SUB FLOOR, INSIDE LEVEL II CORROSION IN CORNER, FS - 67.000 AND L22R. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC-8 SRM 53-2-0. CUT DAMAGED AREA. CLEANED SURROUNDING AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR PARTS IAW EO NR CF-N345JW 11/98. REV 1 DTD 04/17/98. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 5 1-1-21, 51-1-20D, ARROW AIR CONTROL NR 4113. FCT NRC 1065, WORK ORDER 020663. ENTERED ON LOG PAGE NR 75165, ITEM 211M . 2 L 7 4 4F 4A25 1998071700242 19980717 00242 WP 1998 7 17 ARWA980713 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1120 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXCESSIVE EXTERNAL REPAIRS AROUND C3 AFT LOWER CARGO COMPARTMENT SURROUNDING SKIN. REMOVE SURROUNDING SKIN TO REPLACE I NNER DOUBLER FS 1120 TO FS 1260 L27R - L33L. PROCEED TO REPLACE SKIN. REMOVE C3 DOOR SURROUNDING SKIN. INSTALLED NEW SKIN PER EO N345JW -041. DRAWING 5753983, 5750322, 9754924 SPLICED SKIN AT L25R IAW ARROW DRAWING 020663-1108 DTD 05/7/ 98. ARROW AIR CONTROL NR 5247, FCT WORK ORDER NR 020663. NRC 01108. ENTER IN LOG PAGE 79011- 98M. 2 L 7 4 4F 4A25 1998071700243 19980717 00243 WP 1998 7 17 ARWA980714 1 19980609 A 5350 TAIL CONE DOUG DC8 DC863 302198A WP BS 1985 MISREPAIRED A ARWA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 19 345JW 46042 TAIL CONE IMPROPER REPAIR AT FS 1985. REMOVED IMPROPER REPAIR. CUT DAMAGED AREA. FABRICATED REPAIR PARTS IAW DC -8 SR M 53-2-0, 53-5-3, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11 AND 51-1-21. REF CF WORK ORDER 020663 NR CONTROL NR 6033. 2 L 7 4 4F 4A25 1998071700244 19980717 00244 WP 1998 7 17 ARWA980715 1 19980609 A 5350 TAIL CONE DOUG DC8 DC863 302198A WP BS 1995 MISREPAIRED A ARWA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 19 345JW 46042 TAIL CONE, IMPROPER REPAIR AT FS 1995. REMOVED IMPROPER REPAIR. CUT DAMAGED AREA. FABRICATED REPAIR PARTS IAW DC-8 SR M 53-2-0, 53-5-3, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21. REF CF WOR K ORDER 020663 NR CONTROL NR 6034. 2 L 7 4 4F 4A25 1998071700245 19980717 00245 WP 1998 7 17 ARWA980716 1 19980609 A 5313 2555970 LONGERON DOUG DC8 DC863 302198A WP BS 1220 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 AFT LWR CARGO COMPARTMENT 4 CRACK IN L 32L, FS 1220. REMOVED AND REPLACED L-32L IAW DC-8 SRM 51-1-20D, 53-40-0. REF WO RK ORDER 020663 NR CONTROL NR 5252. 2 L 7 4 4F 4A25 1998071700246 19980717 00246 WP 1998 7 17 ARWA980717 1 19980609 A 5311 FRAME DOUG DC8 DC863 302198A WP BS 220 PERFORATED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 MAIN CARGO COMPARTMENT, FRAME PERFORATED, FS 220, L12L. CUT DAMAGED AREA IAW DC-8 SRM 53-2-0. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0, 53-4-1, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-20D. REF CF WORK ORDER 020663 NR CONTROL NR 5253. 2 L 7 4 4F 4A25 1998071700247 19980717 00247 WP 1998 7 17 ARWA980718 1 19980609 A 5730 SKIN DOUG DC8 DC863 302198A WP WS 736.5-761 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LT WING LEVEL II CORROSION IN T/E BETWEEN XW 736.5 AND 761. REMOVED CORROSION, FOUND TO BE BEYOND LIMITS IAW DC-8 SRM 5 7-2-0. CUT DAMAGED AREA IAW DC-8 SRM 57-2-0. FABRICATED REPAIR PART IAW DC-8 SRM 57-3-3, 51-1-4. TREATED, PRIMED AND INSTALLED PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21A REF CF WORK ORDER 020663 NR CONTROL NR 1084. 2 L 7 4 4F 4A25 1998071700248 19980717 00248 WP 1998 7 17 ARWA980719 1 19980609 A 5311 FRAME DOUG DC8 DC863 302198A WP BS 1580 DENTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 MAIN CARGO COMPARTMENT DENTED FRAME AT FS 1580, L-21R. CUT DAMAGED AREA IAW DC-8 SRM 53-2-0. FABRICATED REPAIR PARTS I AW DC-8 SRM 53-2-0, 53-4-1, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-20D. REF CF WORK ORDER 020663 NR CONTROL NR 5259. 2 L 7 4 4F 4A25 1998071700249 19980717 00249 WP 1998 7 17 ARWA980720 1 19980609 A 5240 SKIN DOUG DC8 DC863 302198A WP SERVICE DOOR DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 TEMPORARY REPAIR IN AFT SERVICE DOOR FWD LOWER CORNER. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0, 53-4-1, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D. RE F SEE CF WORK ORDER 020663 NR CONTROL NR 5007. 2 L 7 4 4F 4A25 1998071700250 19980717 00250 WP 1998 7 17 ARWA980721 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1746 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1746 BETWEEN L-28R AND L-30R. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1 53-5-3, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 5 1-1-20D. REF SEE CF WORK ORDER 020663 NR CONTROL NR 6003. 2 L 7 4 4F 4A25 1998071700251 19980717 00251 WP 1998 7 17 ARWA980722 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1723 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1723, BETWEEN L-23L AND L-24L. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PA RTS IAW DC-8 SRM 53-2-1, 53-5-3, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-2 0D. RE. SEE CF WORK ORDER 020663. NR CONTROL NR 6001. 2 L 7 4 4F 4A25 1998071700252 19980717 00252 WP 1998 7 17 ARWA980723 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1746 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1746 BETWEEN L-29L AND L-30L. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-5-3, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-20D. REF SEE CF WORK ORDER 020663 NR CONTROL NR 6002. 2 L 7 4 4F 4A25 1998071700253 19980717 00253 WP 1998 7 17 ARWA980724 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1723 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1723, BETWEEN L-30R AND L-32R. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PA RTS IAW DC-8 SRM 53-2-1, 53-5-3, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1- 21, 51-1-20D. REF SEE CF WORK ORDER 020663 NR CONTROL NR 6004. 2 L 7 4 4F 4A25 1998071700254 19980717 00254 WP 1998 7 17 ARWA980725 1 19980609 A 5240 SKIN DOUG DC8 DC863 302198A WP LT SERVICE DOOR DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 TEMPORARY REPAIR IN LT AFT DOOR FWD LWR CORNER. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW EO NR CF-N345JW 4/ 98 REV 2 ACTION NR 365790 FILE 98-04-10-008, 98-04-01-0071, DRAWING 01780. TREATED PRIMED AND INSTALLED REPAIR PARTS IA W DC-8 CF WORK ORDER 020663 CONTROL NR 5014. 2 L 7 4 4F 4A25 1998071700255 19980717 00255 WP 1998 7 17 ARWA980726 1 19980609 A 5320 FRAME DOUG DC8 DC863 302198A WP SERVICE DOORWAY DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 IMPROPER REPAIR IN LT AFT DOOR FRAME AFT LWR PART. REMOVED IMPROPER REPAIR. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2- 0, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 51-1-20D. REF SEE CF WORK ORDER 020663 NR CONTROL NR 5015. 2 L 7 4 4F 4A25 1998071700256 19980717 00256 WP 1998 7 17 ARWA980727 1 19980609 A 5240 SKIN DOUG DC8 DC863 302198A WP RT SERVICE DOOR DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 TEMPORARY REPAIR IN RT SERVICE DOOR AFT LOWER CORNER. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PARTS IAW EO NR CF N 345JW 3/98 REV 1 ACTION NR 355211 FILE 98-04-02-004 DRAWING 01763. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 S RM 51-1-8, 51-1-11, 51-1-20D, 51-1-21 REF CF WORK ORDER NUMBER 020603 NR CONTROL NR 5016. 2 L 7 4 4F 4A25 1998071700257 19980717 00257 WP 1998 7 17 ARWA980728 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 55 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 55.000 BETWEEN L- 33L AND L-34L. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PA RTS IAW DC-8 SRM 53-2-1, 53-3-3, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-2 , 51-1-20D REF WORK ORDER 020663 NR CONTROL NR 4004. 2 L 7 4 4F 4A25 1998071700258 19980717 00258 WP 1998 7 17 ARWA980729 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1160 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1160 BETWEEN L27L AND L 28L. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21, 5 1-1-20D REF SEE CF WORK ORDER 020663 NR CONTROL NR 5023. 2 L 7 4 4F 4A25 1998071700259 19980717 00259 WP 1998 7 17 ARWA980730 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1200 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1200 BETWEEN L-27L, SNF L-28L. REMOVED TEMPORARY REPAIR FABRICATED REPAIR PART S IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11,51-1-21, 51-1-20D REF SEE CF WORK ORDER 020663 NR, CONTROL NR 5024. 2 L 7 4 4F 4A25 1998071700260 19980717 00260 WP 1998 7 17 ARWA980731 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1220 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE TEMPORARY REPAIR AT FS 1220 BETWEEN L-27L AND L-28L. REMOVED TEMPORARY REPAIR. FABRICATED REPAIR PAR TS IAW DC-8 SRM 53-2-1, 53-4-1, 51-1-4. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21 , 51-1-20D REF SEE CF WORK ORDER 020663 NR CONTROL, NR 5025. 2 L 7 4 4F 4A25 1998071700261 19980717 00261 WP 1998 7 17 ARWA980732 1 19980609 A 5320 DOUBLER DOUG DC8 DC863 302198A WP BS 1660-1680 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 EXTERIOR FUSELAGE LEVEL II CORROSION IN DOUBLER FUS STA 1660-1680 AND L-33R. REMOVED IMPROPER REPAIR FABRICATED REPAIR PARTS IAW EO CF N345JW. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-20D, 51-1-21, 8110 -3 FORM ISSUED DATED 4/3/98 REF SEE WORK ORDER 020663 NR CONTROL NR 5073. 2 L 7 4 4F 4A25 1998071700262 19980717 00262 WP 1998 7 17 ARWA980733 1 19980609 A 5330 SHIM DOUG DC8 DC863 302198A WP BS 857 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LT MLG W/W LEVEL 1 CORROSION IN FWD LT UPPER ANGLE SHIM FUS STA 857.000. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IA W DC-8 SRM 53-2-0. REMOVED CORRODED SHIM CLEANED SURROUNDING AREA WITHIN LIMITS IAW DC-8 SRM 53-2-0. FABRICATED NEW SH IM IAW DC-8 SRM 51-1-4. TREATED PRIMED AND INSTALLED NEW SHIM IAW DC-8 SRM 51-1-8, 51-1-20D. REF SEE CF WORK ORDER 020 663 NR CONTROL NR 5210. 2 L 7 4 4F 4A25 1998071700263 19980717 00263 WP 1998 7 17 ARWA980735 1 19980609 A 5542 SKIN DOUG DC8 DC863 302198A WP RUDDER CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 VERTICAL STABILIZER LEVEL II CORROSION IN RUDDER SKIN RIGHT SIDE ZR 110.750. SMOOTHED AND BLENDED OUT CORROSION AREA FA BRICATED REPAIR PARTS IAW EO NR CF-345JW 14/98. TREATED PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-20D, 51-1-21 8110-3 FORM ISSUED DATED 4/29/98. WORK ORDER CONTROL NR 6021 SEE CF WORK ORDER 020663. 2 L 7 4 4F 4A25 1998071700264 19980717 00264 WP 1998 7 17 ARWA980736 1 19980609 A 5330 SKIN DOUG DC8 DC863 302198A WP BS 1890-1995 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 TAILCONE, SEVERAL SPOTS OF LEVEL 1 CORROSION ON SKIN, RT SIDE, FS 1890 TO 1995. REMOVED CORROSION FOUND TO BE BEYOND LI MITS IAW DC-8 SRM 53-2-20. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS IAW DC-8 SRM 53-2-0, 51-1-4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-8, 51-1-11, 51-1-21. REF CF WORK ORDER 020663 NRC 0660. 2 L 7 4 4F 4A25 1998071700265 19980717 00265 WP 1998 7 17 ARWA980796 1 19980710 A 2420 51508000 GCU DOUG DC8 DC863 302198A WP NR 3 GEN FAILED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 345JW 696ABC 46042 SJU - FLT 508 - PREFERENTIAL SYSTEM INOP ON PUSH BACK. REMOVED AND REPLACED NR 3 GENERATOR GCU. OPS CHECKED NORMAL IAW MM 24-20-0. (M) 2 L 7 4 4F 4A25 1998071700266 19980717 00266 NE 1998 7 17 ARWA980797 2 19980710 A 7321 C8E702 AMPLIFIER LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122* 54555 NE NR 3 ENGINE FAILED A ARWA J A DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 307GB BY30095 193U131 MIA - FLT 239 - AFTER TAKEOFF, NR 3 ENGINE N1 INDICATOR FAILED. INDICATED 20.7 PERCENT AT ALL THRUST SETTINGS AND N2, H IGH READINGS DUMPED 5 LBS OF FUEL. CORRECTED BOTH N1 AND N2. REMOVED AND REPLACED NR 3 ENGINE SPEED CONTROL AMPLIFIER, OPS CHECKED ENGINE AND AMPLIFIER PER MM 73-21-00 AND 71-00-00 NORMAL. (M) 2 L 7 3 4F 4 F A23WE A12EU 1998071700268 19980717 00268 NE 1998 7 17 TC8A98040 2 19980710 A 7230 COMPRESSOR DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 802CK 45679 INITIATED ABORT PASSING 80 KNOTS BECAUSE OF SUSPECTED COMPRESSOR STALL OR BLOWN TIRE. RETURNED TO THE BLOCKS, LET BRAK ES COOL, INSPECTED BRAKES AND TIRES IAW M/M 32-40-1. ALSO RAN UP ALL FOUR ENGINES IAW 71-00, COULD NOT DUPLICATE COMPRE SSOR STALL, ENGINE RUN-UP NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1998071700269 19980717 00269 NM 1998 7 17 SPAA9800004 1 19980701 A 3350 110049 BATTERY CHARGER BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE FORWARD SECTIONS OF THE FLOOR TRACK EMERGENCY EXIT LIGHT SYSTEM ILLUMINATED WHEN THE CONTROL SWITCH WAS PLACED IN THE ARMED POSITION. THE ASSOCIATED SYSTEM BATTERY CHARGER WAS REPLACED. SUBSEQUENT SYSTEM TESTS WERE SATISFACTORY PER BMM 33-51-11. 2 L 7 2 4F A16WE 1998071700270 19980717 00270 NM 1998 7 17 VJ9800221 1 19980703 A 3350 81 BULB BOEING 737 7372T4 1384492 NM CABIN FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 467AT 22055 LT WING OVERWING EMERGENCY LIGHT INOP. RELAMPED; OPS CHECKS NORMAL IAW MM 33-50-00. 2 L 7 2 4F A16WE 1998071700271 19980717 00271 NM 1998 7 17 K3HA980087 1 19980707 A 3350 0816901 LIGHT BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHT SECOND LIGHT BACK L-1 DOOR MISSING. RECOVERED LENSE RELAMPED OPS CHECK GOOD PER 33-59-00. 2 L 7 3 4F A3WE 1998071700272 19980717 00272 NM 1998 7 17 K3HA980088 1 19980707 A 3350 0816901 LAMP BOEING 727 727225 1384077 NM CABIN LOOSE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHT CENTER AREA AT ROW 16 EMERGENCY PATH LIGHT DISLODGED. INSTALLLED LIGHT ASSEMBLY OPS CHECK GOOD PER MM 33-59-00. 2 L 7 3 4F A3WE 1998071700273 19980717 00273 NM 1998 7 17 K3HA980089 1 19980709 A 3350 1000677 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 EXIT SIGN AT L-1 DOOR BULB INOP. REMOVED AND RELPACED L-1 DOOR BARRIER STRAPS REF MM 25-60-0. 2 L 7 3 4F A3WE 1998071700274 19980717 00274 NM 1998 7 17 RAAA98B1084 1 19980704 A 3530 4566M37B042NM PBE BOEING 727 72722C 138400F NM CABIN INOPERATIVE A RAAA K NONE J WARNING INDICATION IN INSP/MAINT 1 AL 03 831RV 19093 FOUND RT FWD CABIN PBE INDICATOR PROTRUDING ON SERVICE CHECK. CHANGED PBE DUE POUCH VACUUM LOST. 2 L 7 3 4F A3WE 1998071700275 19980717 00275 NM 1998 7 17 RAAA98B2030 1 19980707 A 5312 BULKHEAD CHORD BOEING 727 72722C 138400F NM BS 950 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED B3 CHECK PER CARD B146001, FOUND BS 950 BULKHEAD UPPER CHORD TOOL DAMAGED AT RBL 42. REPAIRED PER SRM 51-40-3, M-54 NR 208. 2 L 7 3 4F A3WE 1998071700276 19980717 00276 NM 1998 7 17 RAAA98B2031 1 19980707 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 1166 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED S5 INSPECTION PER CARD S6 54104, FOUND BS 1166 FRAME SHEAR TIE CORRODED AT STR 28R TO 30. REPLACED SHE AR TIE PER SRM 51-30-2, 51-10-6, 51-20-04 AND 51-10-1, M-54 NR 260. 2 L 7 3 4F A3WE 1998071700277 19980717 00277 NM 1998 7 17 RAAA98B2032 1 19980707 A 5315 FLOORBEAM BOEING 727 72722C 138400F NM BS 1166 MISDRILLED A RAAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED S5 INSPECTION PER CARD S6 54104, FOUND BS 1166 FLOORBEAM WITH 2 DRILL HOLES IN UPPER CHORD. REPAIRED P ER BAC MSG RVV-SEA-98-0010RR AND SRM 53-10-8, FIG 3 M-54 NR 261. 2 L 7 3 4F A3WE 1998071700278 19980717 00278 NM 1998 7 17 RAAA98B2033 1 19980707 A 5320 ANGLE BOEING 727 72722C 138400F NM BS 1408 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED S5 INSPECTION PER CARD S5 33103, FOUND ACCESS PANEL NR 5222 ATTACH ANGLE CRACKED AT BS 1408. REPAIRED PER SRM 51-30-2 AND 51-40-3, M-54 NR 277. 2 L 7 3 4F A3WE 1998071700279 19980717 00279 NM 1998 7 17 RAAA98B2034 1 19980707 A 5311 FRAME BOEING 727 72722C 138400F NM BS 1130 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED S5 INSPECTION PER CARD S6 54104, FOUND BS 1130 FRAME FWD FACE AND SHEAR TIE CORRODED AT STR 29L TO 29R. REPAIRED PER SRM 53-10-4, FIG 15, SHEET 3, 51-10-6 AND 51-30-2, M-54 NR 305. 2 L 7 3 4F A3WE 1998071700280 19980717 00280 NM 1998 7 17 RAAA98B2035 1 19980707 A 5320 SHEAR TIE BOEING 727 72722C 138400F NM BS 1130 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED S5 INSPECTION PER CARD S6 54104, FOUND BS 1130 FRAME SHEAR TIE CORRODED AT STR 28R TO 29R. REPLACED SH EAR TIE PER SRM 51-10-1 AND 51-30-2, M-54 NR 307. 2 L 7 3 4F A3WE 1998071700281 19980717 00281 NM 1998 7 17 RAAA98B2036 1 19980707 A 5320 WEB BOEING 727 72722C 138400F NM BS 1223 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED S5 INSPECTION PER CARD S5 34103, FOUND RT LOWER TORQUE BOX VERTICAL WEB CRACKED AT LIGHTING HOLE, BS 12 23, RBL 21. REPAIRED PER SRM 53-10-2 AND 51-40-2, M-54 NR 354. 2 L 7 3 4F A3WE 1998071700282 19980717 00282 WP 1998 7 17 CALA9801217 1 19980708 A 2761 1040T1005 ACTUATOR DOUG DC9 DC931 3022065 WP SPOILER FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 18563 47487 SMOKE BEGAN COMING FROM TOP OF FIRST OFFICER'S GLARESHIELD/WINDOW AREA DURING CLIMB-OUT OF IAH BOUND FOR ORD. THE AIRCR AFT WAS DIVERTED TO SHV WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO GROUND SPOILER ACTUATOR LOCKED UP. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-62-5 AND OPERATIONAL CHECKS WERE GOOD. IN ADDITION, ALL SYSTEM AND EL ECTRICAL COMPONENTS IN COCKPIT AREA WERE INSPECTED WITH NO DEFECTS NOTED. 2 L 7 2 4F A6WE 1998071700283 19980717 00283 NM 1998 7 17 CALA9801218 1 19980708 A 3260 6552811118 ACCESSORY UNIT BOEING 737 737130 1384435 NM E/E COMPT INOPERATIVE A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 16201 17609 19018 THE GEAR HANDLE STOPPED IN THE OFF POSITION WHEN RAISING THE GEAR AFTER TAKEOFF. THE GEAR TRIGGER WAS PULLED AND THE GE AR CAME UP. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. TESTS WERE CONDUCTED IAW MM 32-09-200 AN D ALL CHECKED GOOD. 2 L 7 2 4F A16WE 1998071700284 19980717 00284 NM 1998 7 17 CALA9801219 1 19980708 A 3230 1U1085 SEQUENCE VLV BOEING 727 727227 1384078 NM LT MLG LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 76753 30088 21249 THE A SYSTEM HYDRAULIC FLUID WAS LOST WHEN LANDING GEAR WAS RETRACTED AFTER TAKEOFF FROM CRP. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG LOCK SEQUENCE VALVE LEAKING. THE SEQUENCE VALVE WAS REMOVED AND REPLACED IAW MM 32-32-31. THE HYDRAULIC SYSTEM WAS SERVICED. A GEAR RETRACTION WAS PERFORMED AND OPERA TIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1998071700285 19980717 00285 WP 1998 7 17 CALA9801220 1 19980708 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 294 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .25 INCH CRACK IN FLOOR SUPPORT AT STA 294, S28R, FORWARD CARGO COMPARTMENT. THE CRACK WAS STOP DRIL LED. AN L-ANGLE WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998071700286 19980717 00286 WP 1998 7 17 CALA9801221 1 19980708 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 332 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT STRIP AT STA 332, S27L. THE CRACK WAS STOP DRILLED. AN L-ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263. 2 L 7 2 4F A6WE 1998071700287 19980717 00287 WP 1998 7 17 CALA9801222 1 19980708 A 5400 ANGLE DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND NR 2 ENGINE PYLON INBOARD VERTICAL ATTACH ANGLE FORWARD OF WIRE BUNDLE CRACKED AT LOWER END. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30-5, 54-04, FIGURE 10, AND MM 51 -20-11. 2 L 7 2 4F A6WE 1998071700288 19980717 00288 WP 1998 7 17 CALA9801223 1 19980708 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 351 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND DOUBLER CORRODED WITH FASTENERS PULLING THROUGH AT STA 351, LONGERON 30. A FINGER DOUBLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A6WE 1998071700289 19980717 00289 WP 1998 7 17 CALA9801224 1 19980708 A 5712 RIB DOUG DC9 DC932 3022066 WP WS 516 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 3.5 INCH CRACK IN LT WING LEADING EDGE RIB AT HI-LOK IN UNDERSIDE OF LEADING EDGE AT XOS 516. THE RI B WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED ON RIB IAW SRM 57-02, FIGURE 6 AND 51-10-3. THE RIB WAS REINSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998071700290 19980717 00290 WP 1998 7 17 CALA9801225 1 19980708 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 256 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .5 INCH CRACK IN RADIUS OF FORWARD CARGO COMPARTMENT FLOOR FRAME AT STA 256, S27L. THE CRACK WAS STO P DRILLED. AN L-ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5320-01263 AND SRM 51-10-3. 2 L 7 2 4F A6WE 1998071700291 19980717 00291 WP 1998 7 17 CALA9801226 1 19980707 A 5320 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 945 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .5 INCH CRACK IN SHEAR TIE ON MAIN FRAME AT FS 945 BETWEEN LONGERON 14R AND 15R. THE SHEAR TIE WAS R EMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 53-11-3, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1998071700292 19980717 00292 WP 1998 7 17 CALA9801227 1 19980709 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965-996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOORBEAM CORROSION AT STA 980, LBL 34, STA 996, LBL 27, AND STA 965, LBL 16. L-ANGLES AND FILLERS WER E FABRICATED AND INSTALLED AT EACH LOCATION IAW SRM 53-05, FIGURE 20A AND 51-10-3. 2 L 7 2 4F A6WE 1998071700293 19980717 00293 WP 1998 7 17 CALA9801228 1 19980709 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 945 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND SKIN CORRODED AT AFT CARGO COMPARTMENT FRAME STA 945 BETWEEN LONGERON 25R AND 26R. THE CORRODED AREA W AS CUT OUT. A REPAIR DOUBLER, FINGER DOUBLER, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53 -04, FIGURE 12, SHEET 6. 2 L 7 2 4F A6WE 1998071700294 19980717 00294 NM 1998 7 17 CALA9801229 1 19980708 A 5320 ANGLE BOEING 737 737217 1384464 NM BS 648-767 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12230 19884 INSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT ANGLE AT STA 648-767, RBL 45. THE CRACKED AREA WAS CUT OUT. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND MM 51-20-11. 2 L 7 2 4F A16WE 1998071700295 19980717 00295 WP 1998 7 17 CALA9801230 1 19980709 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND A .75 INCH CRACK IN FORWARD SERVICE DOOR BOTTOM HORIZONTAL BEAM (NR 4) AT FORWARD END IN RADIUS NEXT TO SKIN. THE BEAM WAS REMOVED AND A NEW BEAM WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998071700296 19980717 00296 WP 1998 7 17 CALA9801231 1 19980710 A 5320 ANGLE DOUG DC9 DC982 3022082 WP DORSAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND A .25 INCH CRACK IN RT SIDE DORSAL FIN ATTACH ANGLE AND A .25 INCH CRACK IN LT SIDE DORSAL FIN ATTACH A NGLE. THE ANGLES WERE REPLACED IAW WORK CARD 08-5340-1-0007 AND 08-5340-1-0008. 2 L 7 2 4F A6WE 1998071700297 19980717 00297 NM 1998 7 17 CALA9801232 1 19980709 A 3350 3004185 LIGHT GRIMES BOEING 747 747243B 1384830 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33021 20520 INSPECTION FOUND L-1 DOOR MOUNTED SLIDE LIGHT INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-51-06. 2 L 7 4 4F A20WE 1998071700298 19980717 00298 WP 1998 7 17 CALA9801233 1 19980710 A 3350 P2070003001 LIGHT DME DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 39081 47861 INSPECTION FOUND EMERGENCY FLASHLIGHT IN CABIN INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED. 2 L 7 3 4F A22WE 1998071700299 19980717 00299 NM 1998 7 17 UPS98227140 1 19980710 A 2612 FIRE LOOP BOEING 727 72725C 138400H NM WHEEL WELL MALFUNCTIONED A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 950UP 19718 FALSE WHEEL WELL FIRE WARNING WENT OUT ON GEAR EXTENTION. INSPECTED LOOPS AND DEFERRED FOR LOOP PER 26-8. 2 L 7 3 4F A3WE 1998071700300 19980717 00300 NE 1998 7 17 UPS98427139 2 19980710 A 7230 GUIDE VANE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7 52054 NE NR 1 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 521UP ENG FAN EXIT GUIDE VANE HAS TWO CRACKS 1 APPX .125 INCH LONG 1 APPX .25 INCH LONG. BOTH HAVE DEFLECTION. NR 1 ENG FAN EXIT GUIDE VANE DAMAGE BEYOND LIMITS AND REMOVED FROM ENGINE AS PER MM 72-34-05. 2 L 7 4 4F 4 F A20WE E20EA 1998071700301 19980717 00301 WP 1998 7 17 UPS98827138 1 19980709 A 2611 30303A4 SMOKE DETECTOR DOUG DC8 DC871F 302199D WP CARGO COMPT FAILED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 702UP 45902 AT FL 350 MAIN CARGO SMOKE DETECTOR LIGHT ILLUMINATED IN ALL POSITIONS, LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACE D SMOKE DETECTOR AMPLIFIER; SYSTEM OPS CHECKED NORMAL IAW DC8 MM 26-00-00. 2 L 7 4 4F RT 4A25 1998071700302 19980717 00302 EU 1998 7 17 QXEA9800836 1 19980604 A 5400 DRAIN LINE FOKKER F28 F28MK4000 4990810 EU NR 2 NACELLE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - LEFT STUBWING NR 2 DRAIN LINE IS LOOSE AND CRACKED AT NACELLE FIREWALL BELOW AND OUTBOARD OF NR 1 SILENCER. REPAI RED IAW HORIZON AIR EA 4-54-38 AND 54-54-38A. 2 L 7 2 4F RT A20EU 1998071700303 19980717 00303 EU 1998 7 17 QXEA9800837 1 19980602 A 5414 SKIN FOKKER F28 F28MK4000 4990810 EU LT PYLON CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - LEFT STUBWING FORWARD OUTBOARD LEADING EDGE CRACKED AT ENGINE COWL. REPAIRED IAW HORIZON AIR EA 4-54-41. 2 L 7 2 4F RT A20EU 1998071700304 19980717 00304 EU 1998 7 17 QXEA9800838 1 19980507 A 7120 THRUST STRUT FOKKER F28 F28MK4000 4990810 EU RT ENGINE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - RIGHT ENGINE THRUST STRUT HAS CORROSION IN SPOTS AROUND CIRCUMFERENCE TUBE IN STUBWING BY SLEEVE. REPAIRED IAW HO RIZON AIR EA 4-71-82. 2 L 7 2 4F RT A20EU 1998071700305 19980717 00305 EU 1998 7 17 QXEA9800839 1 19980509 A 5610 WINDOW FRAME FOKKER F28 F28MK4000 4990810 EU LT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - CRACK AT PILOT SLIDING WINDOW LOWER AFT CORNER OF FRAME. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998071700306 19980717 00306 EU 1998 7 17 QXEA9800840 1 19980519 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - STRINGER 1B IS CRACKED AT AFT EDGE ON LOWER FLANGE THROUGH FIRST RIVET. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 8, FIGURE 6. 2 L 7 2 4F RT A20EU 1998071700307 19980717 00307 EU 1998 7 17 QXEA9800841 1 19980528 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 1890 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - FRAME CLIP CRACKED AT STRINGER 19 FRAME 1890. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998071700308 19980717 00308 WP 1998 7 17 ABXA9800603 1 19980630 A 5250 AR25291 LOCK DOUG DC8 DC863 302198A WP COCKPIT JAMMED A ABXA K NONE O OTHER CR CRUISE 1 GL 23 825AX 46115 COCKPIT ENTRY DOOR JAMMED IN LOCKED POSITION AND COULD NOT BE RELEASED. REPLACED LATCH ASSEMBLY IAW DC8 SRM 51-03-00. O PS CHECKED GOOD. 2 L 7 4 4F 4A25 1998071700417 19980717 00417 EU 1998 7 17 SIMA981664 1 19980606 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 14874 0209 GRR - CABIN CENTER SECTION FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. MEL'D PER MEL 33-22. RAI BATTERY PACK 16WL. OPER ATIONAL CHECK GOOD. MEL CLEARED. (M) 2 H 7 2 4T RT A53EU 1998071700418 19980717 00418 EU 1998 7 17 SIMA981542 1 19980603 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 142DD AE8042 040 GRR - FORWARD EMERGENCY FLOOR ESCAPE PATH LIGHTING INOP. INSTALLED SERVICEABLE BATTERY PACK IN POWER SUPPLY 3WL AND OPS CHECK FOUND GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700419 19980717 00419 EU 1998 7 17 SIMA981662 1 19980527 A 5347 7053799381 SEAT TRACK SAAB SF340 340B 7860101 EU BS 298-307 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 ABI - SEAT TRACK AT FS 298 TO FS 307 BL 18.3 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK SECTION AT FS 298 TO FS 307 IAW SRM 51-20-50. (M) 2 L 7 2 4T RT A52EU 1998071700420 19980717 00420 EU 1998 7 17 SIMA981661 1 19980527 A 5347 7053799381 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-307 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 394AE 340B394 ABI - SEAT TRACK AT FS 297 TO FS 307 BL 0 CORRODED BEYOND LIMITS. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED R EPAIRED SECTION IAW SRM 51-20-50. (M) 2 L 7 2 4T RT A52EU 1998071700421 19980717 00421 EU 1998 7 17 SIMA981591 1 19980608 A 3230 HP848430621 VALVE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 21 247AE 1319 340B247 JAN - FLT 5016 - AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. AIRCRAFT RETURNED TO JAN AFTER SEVERAL ATTEMPTS TO RETR ACT GEAR. CONTRACT MTX OPENED UP MEL ON LANDING SYSTEM AND FLT CREW REPO AIRCRAFT TO DFW FOR FURTHER MTX. RAI LANDING GEAR CONTROL VALVE. LANDING GEAR OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998071700422 19980717 00422 EU 1998 7 17 SIMA981561 1 19980605 A 3222 AIR127300 PIN SAAB SF340 340B 7860101 EU NLG BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 180AE 340B180 MIA - DURING PHASE 4 INSPECTION, FOUND PIN ASSY BROKEN AT THREADS AT END OF HOLD DOWN NUT. RAI PIN. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998071700423 19980717 00423 EU 1998 7 17 SIMA981531 1 19980602 A 7110 COWLING SAAB SF340 340B 7860101 EU RT ENGINE SEPARATED A SIMA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 21 268AE 340B268 FLT 5757 - MIA - AFTER TAKEOFF, A PIECE ON RT ENGINE COWLING CAME OFF, PANEL NR 463CL AND 463DR, ARE BOTH DAMAGED. RAI COWLINGS 463CL AND 463DR. (M) 2 L 7 2 4T RT A52EU 1998071700424 19980717 00424 EU 1998 7 17 SIMA981592 1 19980608 A 5311 S5367240725000 FRAME AEROSP ATR72 ATR72212 EU BS 38 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE LEFT FAIL/SAFE BETWEEN STRINGER 20 AND 21 AT FRAME 38 WAS CORRO DED. MAINTENANCE REMOVED AND REPLACED THE FAIL/SAFE ANGLE IAW SRM 51-25-01. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700425 19980717 00425 EU 1998 7 17 SIMA981593 1 19980608 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FLOORBEAM 36 AND 38 WAS CORRODED. MAINTENANCE REMOVED AND REPL ACED FLOORBEAM 36 AND 38 IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700426 19980717 00426 EU 1998 7 17 98ZZZM480 1 19980608 A 5315 S53672407208 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FLOORBEAM 36 AND 38 WAS CORRODED. MAINTENANCE REMOVED AND REPL ACED FLOORBEAM 36 AND 38 IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700427 19980717 00427 EU 1998 7 17 SIMA981594 1 19980608 A 5315 S53372411200 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAM 33 AND 39 WS CORRODED. MAINTENANCE REPAIRED FLOORBE AM 33 AND 39 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700428 19980717 00428 EU 1998 7 17 98ZZZM481 1 19980608 A 5315 S53372408254 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THAT FLOORBEAM 33 AND 39 WS CORRODED. MAINTENANCE REPAIRED FLOORBE AM 33 AND 39 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700429 19980717 00429 EU 1998 7 17 SIMA981663 1 19980515 A 5330 SKIN AEROSP ATR72 ATR72212 EU BS 133 PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 399AT 399 ABI - LEFT LOWER FUSELAGE SKIN AT FS 133B, RIB 28B PUNCTURED. FABRICATED REPAIR DOUBLER, POSITIONED AND INSTALLED IAW S RM 53-00-00 PAGE 407-410 FIG 403. (M) 2 H 7 2 4T RT A53EU 1998071700430 19980717 00430 NM 1998 7 17 TWAA9809201 1 19980609 A 3397 WIRE BOEING 727 727231 1384079 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54327 20234 DSM - FLT 290 - DURING GROUND CHECK OF EGRESS LIGHTS FOUND ONE ESCAPE PATH LIGHT STRIP INOP IN MID CABIN. PLACARDED LIG HT PER MEL. ON LAYOVER PLUGGED IN THE LIGHT STRIP IN WORKED NORMAL. CHECK-C 8-30-97 MCI. (M) 2 L 7 3 4F A3WE 1998071700431 19980717 00431 WP 1998 7 17 TWAA9809202 1 19980603 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 937 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 920L 47734 DURING OP-15 MAINTENANCE CHECK, FOUND FUSELAGE SKIN WITH .125 INCH CRACK ON CARGO DOOR CUTOUT EDGE, FS 937 AND L26R. TR IMMED DAMAGED AREA AND CRACK. INSTALLED REPAIR DOUBLER PER SRM 53-05, FIG 8C AND TWA STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998071700432 19980717 00432 WP 1998 7 17 TWAA9809203 1 19980604 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 200-220 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP16 MAINTENANCE CHECK, FOUND SKIN PILLOWED AND RIVET HEADS PULLED FROM FS 200 TO 220, LONG 18R TO 19R. RE MOVED REPAIR AND FOUND NO CORROSION. INSTALLED NEW REPAIR PER SRM 53-04, FIG 26 SHEET 2, AND SHIMMED AS REQUIRED. (M) 2 L 7 2 4F A6WE 1998071700433 19980717 00433 WP 1998 7 17 TWAA9809204 1 19980604 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 207-229 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SKIN PILLOWING AROUND RIVETS ON REPAIR AT FS 207 TO 229, LONG 20R TO 21R. R EMOVED REPAIR. NO CORROSION FOUND. INSTALLED NEW REPAIR PER SRM 53-04, FIG 26 SHEET 2, AND SHIMMED AS REQUIRED. (M) 2 L 7 2 4F A6WE 1998071700434 19980717 00434 WP 1998 7 17 TWAA9809205 1 19980605 A 5320 PAN DOUG DC9 DC982 3022082 WP BS 1212-1250 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT FLOOR PAN AT L18L BETWEEN FS 1212 AND 1250, CORRODED. REMOVED CORROSIO N PER SRM 51-10-03. REPAIRED FLOOR PAN REF SRM 53-05, FIG 96 PG 347. (M) 2 L 7 2 4F A6WE 1998071700435 19980717 00435 WP 1998 7 17 TWAA9809206 1 19980603 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP16 MAINTENANCE CHECK, FOUND FLOOR SUPPORT BEAM LBL 7.5 CORRODED AT FS 160 TO 200. REPLACED FLOOR SUPPORT PER SRM 51-10, PAGE 1 AND SRM 53-14-1 FIG 11. (M) 2 L 7 2 4F A6WE 1998071700436 19980717 00436 WP 1998 7 17 TWAA9809207 1 19980603 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 165-200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR SUPPORT BEAM CORRODED AT RBL 7.5, FS 165 TO FS 200. REPLACED FLOOR SU PPORT PER SRM 51-01, PAGE 1 AND SRM 53-14-1 FIG 11. (M) 2 L 7 2 4F A6WE 1998071700437 19980717 00437 WP 1998 7 17 TWAA9809208 1 19980527 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 256 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM CAP AT STATION 256, LBL 20 TO RBL 20. FABRICATED NEW BEAM AND INSTALLED PER SRM 51-01, PAGE 1. (M) 2 L 7 2 4F A6WE 1998071700438 19980717 00438 WP 1998 7 17 TWAA9809209 1 19980601 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR SUPPORT BEAM FS 200 CORRODED, LBL 15 IN TO RBL 46 IN. REPLACED FLOOR SUPPORT BEAM PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998071700439 19980717 00439 WP 1998 7 17 TWAA9809210 1 19980601 A 5330 SKIN DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 DURING OP 16 MAINTENANCE CHECK, FOUND A .25 INCH CRACK IN OUTER FUSELAGE SURFACE ADJACENT TO NOSE GEAR DOOR, RT SIDE. R EPAIRED CRACK PER SRM 53-05, FIG 62 SHEET 1 AND 2. SEALED REPAIR PER SRM 51-20-0. (M) 2 L 7 2 4F A6WE 1998071700440 19980717 00440 WP 1998 7 17 TWAA9809211 1 19980515 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 79 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND NOSE GEAR WHEEL WELL CHORD ANGLE CRACKED THROUGH A RIVET IN LT TUNNEL, .5 IN CH BELOW PRESSURE DECK AT STATION 79 LBL 17. STOP DRILLED AND INSTALLED DOUBLER PER SRM 53-01, PAGE 10. (M) 2 L 7 2 4F A6WE 1998071700441 19980717 00441 WP 1998 7 17 TWAA9809212 1 19980603 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 920L 47734 MCI - DURING OP 15 MAINTENANCE CEHCK, THE AFT CARGO DOOR CUTOUT FUSELAGE SKIN WAS DAMAGED AT AFT LOWER EDGE. REPAIRED D AMAGED SKIN PER SRM 54-05 FIG 80, AND TWA STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998071700442 19980717 00442 NM 1998 7 17 TWAA9809213 1 19980526 A 5753 SKIN BOEING 767 767231 1385131 NM LT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 609TW 22572 LAX - DURING C-CHECK MAINTENANCE ON LT WING THE OUTBD FLAP INBOARD LOWER END HAD A REPAIR PATCH THAT DELAMINATED 6 INCH BY 12 INCH. REPAIRED DELAMINATION PER SRM 51-70-05, PAGE 5 PARA 3. (M) 2 L 7 2 4F RT A1NM 1998071700443 19980717 00443 NM 1998 7 17 TWAA9809214 1 19980526 A 5753 SKIN BOEING 767 767231 1385131 NM RT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 609TW 22572 LAX - DURING C-CHECK MAINTENANCE ON RT WING INBOARD AFT FLAP, THE UPPER SURFACE HAD REPAIR PATHC 5 FT FROM INBD END THAT DELAMINATED 7 INCH BY 3 INCH. REPLACED 7 INCH DIAMETER REPAIR PER SRM 57-53-01 AND 51-70-10. (M) 2 L 7 2 4F RT A1NM 1998071700444 19980717 00444 WP 1998 7 17 TWAA9809101 1 19980320 A 5730 SKIN DOUG DC9 DC951 3022051 WP RT WING DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 418EA 47676 STL - DURING OP 9 MAINTENANCE CHECK, FOUND DELAMINATION IN RT WING UPPER PANEL JUST FWD OF AILERON. REMOVED AND REPLACE D UPPER WING PANEL JUST FWD OF AILERON. REF SRM 51-30-2 AND 20-30-0. (M) 2 L 7 2 4F RT A6WE 1998071700445 19980717 00445 WP 1998 7 17 TWAA9809102 1 19980218 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 2L CRACKED AT STATION 200. REPAIRED PER SRM 53-02, PAGE 48. (M) 2 L 7 2 4F A6WE 1998071700446 19980717 00446 WP 1998 7 17 TWAA9809103 1 19980317 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN LEFT SIDE BELOW FORWARD CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1.25 INCH BY .055. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M) 2 L 7 2 4F A6WE 1998071700447 19980717 00447 WP 1998 7 17 TWAA9809104 1 19980317 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK,F OUND DENT ON LEFT SIDE BELOW AFT CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1 INCH BY .045 INCH DEEP. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M) 2 L 7 2 4F A6WE 1998071700448 19980717 00448 WP 1998 7 17 TWAA9809105 1 19980218 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 69 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FORWARD FUSELAGE INTERCOSTAL TO FS 69.550 FORMER ATTACH 'T' ANGLE A T RBL 12 INCH. REPLACED 'T' ANGLE PER SRM 51-01, PAGE 2. (M) 2 L 7 2 4F A6WE 1998071700449 19980717 00449 WP 1998 7 17 TWAA9809106 1 19980317 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 69 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FORWARD FUSELAGE INTERCOSTAL TO FS 69.55 FORMER ATTACH 'T' ANGLE AT LBL 13 INCH. REPLACED 'T' ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998071700450 19980717 00450 WP 1998 7 17 TWAA9809107 1 19980218 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON NR 17R CRACKED AT LOWER FLANGE AT LONGERON TO FS 945 FORMER FRAME A TTACH FASTENER. REPLACED LONGERON PER SRM 51-01, AND SRM 53-02, FIG 18 AND 53-03. (M) 2 L 7 2 4F A6WE 1998071700451 19980717 00451 WP 1998 7 17 TWAA9809108 1 19980317 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 160-196 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOORBEAM CAP AT FS 160 TO 196, RBL 44, CORRODED BEYOND LIMITS. INSTALLED N EW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998071700452 19980717 00452 WP 1998 7 17 TWAA9809109 1 19980218 A 5313 LONGERON DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 929L 47174 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 17L CRACKED AT LOWER FLANGE AT LONGERON TO FORMER FRAME ATTACH FAST ENER. REMOVED AND REPLACED LONGERONS PER SRM 51-01, STANDARD PRACTICES, AND PER SRM 53-02-00, FIG 18 AND 53-03. (M) 2 L 7 2 4F A6WE 1998071700453 19980717 00453 NM 1998 7 17 TWAA9809110 1 19980602 A 5753 SKIN BOEING 767 7673Y0 NM LT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 LAX - DURING C-CHECK, MAINTENANCE FOUND LEFT WING, INBOARD TE FLAP FORWARD SECTION, TE HAD DELAMINATION TOP AND BOTTOM O F SANDWICH, 6 INCH BY 2.5 INCHES. INSTALLED TWO FILLERS WITH HOT BOND, PER SRM 51-70-17. (M) 2 L 7 2 4F RT A1NM 1998071700454 19980717 00454 NM 1998 7 17 TWAA9809111 1 19980603 A 5414 SKIN BOEING 767 7673Y0 NM LT PYLON DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 LAX - DURING C-CHECK, MAINTENANCE FOUND ON LEFT PYLON, AFT END LOWER INBOARD SIDE, DELAMINATION APPROX 7 IN BY 1.5 INCH. REPAIRED DELAMINATION PER SRM 51-70-10. (M) 2 L 7 2 4F RT A1NM 1998071700455 19980717 00455 NM 1998 7 17 TWAA9809112 1 19980602 A 5414 SKIN BOEING 767 7673Y0 NM RT PYLON DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 LAX - DURING C-CHECK, MAINTENANCE FOUND ON RT PYLON, FORWARD AND BELOW LEFT SDIE DRAIN HOLE, A 3 INCH BY 1.5 INCH DELAMI NATION. INSTALLED FABRICATED DOUBLERS USING HOT BOND PROCEDURES PER SRM 51-70-10. (M) 2 L 7 2 4F RT A1NM 1998071700456 19980717 00456 NM 1998 7 17 TWAA9809113 1 19980602 A 5414 SKIN BOEING 767 7673Y0 NM RT PYLON DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 LAX - DURING C-CHECK, MAINTENANCE FOUND APPROX 7 INCH BY 1.5 INCH DELAMINATION ON RT PYLON, INBOARD AFT SIDE. INSTALLED DOUBLER USING HOT BOND PROCEDURES PER SRM 51-70-10. (M) 2 L 7 2 4F RT A1NM 1998071700457 19980717 00457 WP 1998 7 17 TWAA9809114 1 19980605 A 5347 TIE DOWN DOUG DC9 DC982 3022082 WP BS 1128-1174 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON GALLEY TIE-DOWN AT STATION 1128 TO STATION 1174, BL 0. REMOVED CORROSION PER SRM 51-10-3, PARA 31-42, AND REPLACED TRACK PER SRM 51-01, 53-14-3, PGE 47. (M) 2 L 7 2 4F A6WE 1998071700458 19980717 00458 WP 1998 7 17 TWAA9809115 1 19980606 A 5320 VENT RAIL DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16, MAINTENANCE FOUND 2 VENT LOUVER RAILS CRACKED ON UPPER RT SIDE OF AFT FUSELAGE. STOP DRILLED CRACKS , INSTALLED DOUBLERS, SPLICED AND INSTALLED 4 LOUVERS PER SRM 53-05, FIG 66, SHEETS 1 TO 3. (M) 2 L 7 2 4F A6WE 1998071700459 19980717 00459 WP 1998 7 17 TWAA9809116 1 19980605 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK AT STATION 200, LONGERON 2L HAD 2 CRACKS. CUT OUT APPROX 17 INCHES OF LONGERON. A DDED NEW MATERIAL PLUS TWO REPAIR SPLICES PER SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 1998071700460 19980717 00460 WP 1998 7 17 TWAA9809117 1 19980529 A 5753 RIB DOUG DC9 DC932 3022066 WP TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 920L 47734 MCI - DURING OP 15 MAINTENANCE CHECK, THE LEFT WING OUTBOARD FLAP HINGE CASTING ATTACH RIBS WERE CRACKED ON INBOARD AND OUTBOARD SIDES INSIDE FLAP STRUCTURE. RIBS REMOVED AND NEW RIBS INSTALLED PER SRM 51-01, AND FASTENERS INSTALLED PER ST ANDARD PRACTICES AND 51-30-00. (M) 2 L 7 2 4F A6WE 1998071700461 19980717 00461 NM 1998 7 17 TSAA9857292 1 19980421 A 5315 FLOORBEAM BOEING 737 7372S5C 1384499 NM BS 790-827 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 SURFACE CORROSION FOUND AROUND NUT PLATE HOLES RT CARGO FLOORBEAM BS 790-827 AFT PIT. REPLACED FLOORBEAM ON RT AFT PIT IAW 53-10-5. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700462 19980717 00462 NM 1998 7 17 TSAA9857291 1 19980421 A 5730 SKIN BOEING 737 7372S5C 1384499 NM WS 163-189 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FRONT SPAR CAP SHOWS BULGING AND POPPED RIVET AT RT SIDE WING UPPER SURFACE ABOVE NR 5 LE SLAT ANTI-ICING DUCT. REPAIRE D AND TREATED AREAS BETWEEN SS 163.4 AND 189.4 CORROSION IAW ECO 2159R4. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700463 19980717 00463 NM 1998 7 17 TSAA9857290 1 19980421 A 5730 SKIN BOEING 737 7372S5C 1384499 NM WS 311 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 EXFOLIATION CORROSION ON RIGHT WING SURFACE AT DEFUELING PANEL AT FSS 311.0. REPAIRED AREA PER ECO 2135. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700464 19980717 00464 NM 1998 7 17 TSAA9853289 1 19980601 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 767 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 TWO INCH CRACK FOUND AT BS 767, STRINGER 18R. REPAIRED PER SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998071700465 19980717 00465 NM 1998 7 17 TSAA9853288 1 19980601 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 FOUND 1 INCH CRACK AT BS 727 PLUS 1.75 AND STRINGER 17R. REPAIRED PER SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1998071700466 19980717 00466 NM 1998 7 17 TSAA9827285 1 19980601 A 2751 655280737 SWITCH BOEING 737 737282 13844AT NM FLAP SYSTEM FAILED A TSAA O OTHER N FALSE WARNING TO TAKEOFF 1 WP 13 824AL 23045 TAKEOFF CONFIGURATION WARNING HORN SOUNDS WHEN THRUST LEVERS ADVANCED TO TAKEOFF POWER. CHECKED CONDITION AND RESISTANC E CHECK NR 1 AND NR 4 EXT. PROXIMITY SWITCH OK. REPLACED FLAP/SLAT POSITION SWITCH UNIT MODULE. OPERATIONAL CHECK OK PER TAKEOFF WARNING. AIRRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700467 19980717 00467 NM 1998 7 17 TSAA9853283 1 19980531 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 500 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 FOUND CORROSION ON STRINGER 21L BETWEEN BS 500 AND 500A IN FORWARD PIT. INSTALLED REPAIR PER SRM 53-10-3, FIGURE 1. AI RCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998071700468 19980717 00468 NM 1998 7 17 TSAA9853284 1 19980531 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 500 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 FOUND CORROSION UNDER NUT PLATE ON STRINGER 22L BETWEEN BS 500 AND 500A IN FORWARD PIT. INSTALLED REPAIR PER SRM 53-10- 3, FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998071700469 19980717 00469 1998 7 17 TSAA9824236 4 19980428 A 3197 WIRE HARNESS BOEING 737 737282 13844AT NM INST PANEL DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 824AL 23045 FLT 205 - OVERHEAD MASTER CAUTION LIGHT WILL NOT EXTINGUISH. FOUND WIRE BUNDLE W038 PLUS W047 ABOVE P-5 PANEL CHAFED AN D BURNED. REPLACED ALL WIRES, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700470 19980717 00470 NM 1998 7 17 TSAA9833287 1 19980601 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 5 POSITION EMERGENCY EXIT LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700471 19980717 00471 NM 1998 7 17 TSAA9833286 1 19980601 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 3 EMERGENCY EXIT LIGHT DOES NOT PASS TEST. REPLACED NR 3 EMERGENCY EXIT LIGHT ASSY BATTERY PACK. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700472 19980717 00472 NM 1998 7 17 TSAA9833282 1 19980530 A 3350 1000679 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 1998071700473 19980717 00473 NM 1998 7 17 TSAA9833281 1 19980530 A 3350 8621006 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED BATTERY PACK ON NR 5 FLOOR EMERGENCY LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998071700474 19980717 00474 NM 1998 7 17 TSAA9833280 1 19980530 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED BATTERY PACK ON NR 1 FLOOR EMERGENCY LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998071700475 19980717 00475 NM 1998 7 17 TSAA9833279 1 19980530 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 6 POSITION EMERGENCY EXIT BATTERY PACK DUE TO HAVING LOW VOLTAGE. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 1998071700476 19980717 00476 NM 1998 7 17 TSAA9827275 1 19980531 A 2751 189929 SENSOR BOEING 737 737282 13844AT NM NR 1 TE FLAP FAILED A TSAA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 13 824AL 23045 TAKEOFF CONFIGURATION WARNING HORN CAME ON ON TAKEOFF ROLL. REPLACED NR 1 FLAP PROXIMITY SENSOR NR 1 POSITION. OPS CHE CK OK PER MM 27-50-0. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700477 19980717 00477 EU 1998 7 17 SIMA981335 1 19980513 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 3815 223 GRR - FLT 4051 - FORWARD AND AFT EMERGENCY FLOOR LIGHTS INOP. RAI'D 3WL AND 15WL EMERGENCY BATTERY PACKS. OPS CHECK FO UND GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700478 19980717 00478 EU 1998 7 17 98ZZZM482 1 19980513 A 3350 AD3107 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 223AT 11425 223 GRR - FLT 4051 - FORWARD AND AFT EMERGENCY FLOOR LIGHTS INOP. RAI'D 3WL AND 15WL EMERGENCY BATTERY PACKS. OPS CHECK FO UND GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700479 19980717 00479 EU 1998 7 17 SIMA981462 1 19980526 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 11398 0209 SAW - DURING PS-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT AND LEFT AFT EXTERIOR EMERGENCY LIGHTS INOP. MAINTENANCE R EMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, LOCATION 15WL. SYSTEM OPS CHECKED GOOD. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700480 19980717 00480 EU 1998 7 17 SIMA981482 1 19980528 A 2611 FR3222 DETECTOR AEROSP ATR72 ATR72212 EU CARGO BAY MALFUNCTIONED A SIMA K NONE N FALSE WARNING CR CRUISE 1 SW 21 274AT 676 274 DFW - FLT 3828 - INBOUND FLT TO DFW FROM TUL, AFT AUX COMPARTMENT SMOKE WARNING ILLUMINATED 'SQUIB' LGIHT FLASHED ON AND THEN EXTINGUISHED BEFORE QRH PROCEDURES COULD BE COMPLETED. FLT ATTENDANT REPORTED THE AFT SMOKE LIGHT ILLUMINATED ON THE FA PANEL ALSO. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR DUE TO FALSE WARNING INDICATIONS. WORK ACCOMPLISHED I AW JIC 26-15-21. SYSTEM TEST GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700481 19980717 00481 EU 1998 7 17 SIMA981481 1 19980528 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 498AT 0578 498 GRR - FLT 4051 - AFT SECTION OF EMERGENCY FLOOR LIGHTING INOP. RAI'D POWER SUPPLY BATTERY PACK. OPS CHECK GOOD. A/C R ETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998071700482 19980717 00482 1998 7 17 S2YA98014 4 19980527 A 3416 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 831SK UE83 FLT 1124 - MKE-GRR - JUST AFTER TAKEOFF, THE FLIGHT CREW NOTICED THE PILOTS ALTIMETER WAS FLAGGED, ALTITUDE PRESELECT WA S ONLY SHOWING DASHES, AND THE TCAS WAS SHOWING A FAIL MESSAGE. THE CREW DECIDED TO RETURN TO MKE, ALTHOUGH DURING DESC ENT EVERYTHING STARTED WORKING AGAIN. AFTER MAKING AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT. LOSS OF POWER OR FAILURE OF THE NR 1 ALTIMETER WOULD CAUSE THE SAME FAILURE EXPERIENCED BY THE CREW. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM, THEY CHANGED THE NR 1 ALTIMETER AND CIRCUIT BREAKER FOR TROUBLESHOOTING, AND INSPECTED THE ASSOC IATED WIRING. (M) 2 L 7 2 4T RT A24CE 1998071700483 19980717 00483 CE 1998 7 17 S2YA98013 1 19980517 A 3610 PRECOOLER BEECH 1900 1900D 1154162 CE RT ENGINE CONTAMINATED A S2YA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 13 118SK UE108 FLT 1157 - MKE-MSN - SHORTLY AFTER TAKEOFF, THE FLIGHT CREW NOTICED A SLIGHT SMOKE HAZE IN THE COCKPIT. DECLARED AN EME RGENCY AND RETURNED TO MKE. AFTER MAKING AN UNEVENTFUL LANDING MAINTENANCE INSPECTED THE A/C. AFTER TESTING ALL SYSTEM S FOR PROPER OPERATION. FOUND OIL IN THE RT ENGINE PRECOOLER. THE OIL WAS BELIEVED TO HAVE LEAKED INTO THE PRECOOLER W HILE REMOVED FROM THE A/C THE PREVIOUS NIGHT DURING A SCHEDULED INSPECTION. THE PRECOOLER AND THE PRECOOLER BYPASS VALV E WERE CHANGED DUE TO OIL CONTAMINATION. AFTER THE A/C WAS EXTENSIVELY RAN, IT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998071700484 19980717 00484 WP 1998 7 17 TWAA9808001 1 19980519 A 3350 58222 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 416EA 47751 STL - FLT 625 - DURING PREFLIGHT INSPECTION, FOND AFT EGRESS AND AFT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY P ACK MFG P/N 5822-2, FLEX CABLES MFG P/NS 5853-1 AND 5854-3. (M) 2 L 7 2 4F RT A6WE 1998071700485 19980717 00485 1998 7 17 TWAA9808002 4 19980520 A 3442 20671570153 TRANSCEIVER DOUG DC9 DC931 3022065 WP WEATHER RADAR FAILED A TWAA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 05 976Z 8109 47248 STL - FLT 647 - AFTER TAKEOFF WEATHER RADAR SHOWS NO TARGETS ON DISPLAY. REPLACED RADAR RADIO TRANSMITTER MFG P/N 20671 57-0153. (M) 2 L 7 2 4F A6WE 1998071700486 19980717 00486 NM 1998 7 17 TWAA9807911 1 19980511 A 5754 SKIN BOEING 767 767231 1385131 NM NR 7 LE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING C-CHECK, MAINTENANCE FOUND NR 7 LE SLAT WITH 4 INCH BY 3 INCH BULGE ON AFT SIDE OF SLAT, WITH 5/16 IN HEIGH T, APPROX 5.5 FEET FROM INBOARD END AND 2 INCHES ABOVE SEAL. REMOVED DELAMINATED AREA, FOUND NO EVIDENCE OF WATER. INS TALLED CORE AND DOUBLER HOT BOND REPAIR PER SRM 51-70-10 AND APPLIED SEALANT. (M) 2 L 7 2 4F RT A1NM 1998071700487 19980717 00487 NM 1998 7 17 TAOA059814 1 19980527 A 2424 902F2U25 GCU BOEING 727 727227 1384078 NM COCKPIT FAILED A TAOA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 EA 15 926TS 20774 FLT 6041 - BOS-LGA - NR 3 GENERATOR DIFFERENTIAL FAULT AND FAILURE ON TAKEOFF. REPLACED NR 3 GENERATOR CONTROL PANEL, T ESTED SYSTEM PER MM 24-20-0. ADJUSTMENT AND TEST PAGES 501-504. ALL INDICATIONS NORMAL. (M) 2 L 7 3 4F A3WE 1998071700489 19980717 00489 WP 1998 7 17 CALA9801235 1 19980710 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP BS 389 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .5 INCH CRACK AROUND FASTENER HOLE IN CHANNEL AT FORWARD CARGO DOOR FRAME STA 389, S18R, RBL 52. THE CHANNEL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5. A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998071700490 19980717 00490 WP 1998 7 17 CALA9801236 1 19980710 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 1019 BULGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND DOUBLER BULGED WITH FASTENERS PULLING THROUGH AT STA 1019, LONGERON 19L. THE DOUBLER WAS REMOVED IAW SR M 51-10-2. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 53-04, FIGURE 12B. 2 L 7 2 4F A6WE 1998071700491 19980717 00491 WP 1998 7 17 CALA9801237 1 19980710 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 229-294 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOOR PANEL CORRODED AT STA 229 TO 294, BL 0. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS FABRICAT ED AND INSTALLED IAW SRM 53-21-0, 53-10-4, 51-20-2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998071700492 19980717 00492 WP 1998 7 17 CALA9801238 1 19980711 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 7 INCH CRACK IN KEEL BEAM FITTING AT BS 756, LONGERON 30. THE FITTING WAS REMOVED AND A NEW FITTING WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-30-5 AND 51-30-1, PAGE 6. 2 L 7 2 4F A6WE 1998071700493 19980717 00493 WP 1998 7 17 CALA9801239 1 19980712 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 945-965 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND CABIN FLOOR PANEL CORRODED FORWARD OF RT AFT LAV AT STA 945 TO 965, RBL 44. THE FLOOR PANEL WAS REMOVE D AND THE CORRODED SECTIONS WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 1, 51-10-3, AND 5 1-30-2. THE FLOOR PANEL WAS REINSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1998071700494 19980717 00494 WP 1998 7 17 CALA9801240 1 19980711 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945-980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND THREE CRACKS IN LONGERON 17R AT FRAME ATTACH HOLES FROM STA 945 TO 980. THE CRACKS WERE .5 TO 1 INCH L ONG. THE CRACKED AREAS OF LONGERON WERE REMOVED IAW SRM 53-02, FIGURE 18. LONGERON REPAIRS WERE FABRICATED AND INSTALL ED IAW SRM 53-02, FIGURE 18, 51-10-3, 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998071700495 19980717 00495 WP 1998 7 17 CALA9801241 1 19980711 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LONGERON 16R CRACKED AT UPPER FLANGE AND LONGERON 16L CRACKED OUT OF UPPER AND LOWER ATTACH CLIP FASTEN ERS, STA 965. THE CRACKED AREAS OF LONGERONS WERE REMOVED IAW SRM 51-30-2. LONGERONS AND SPLICES WERE FABRICATED AND I NSTALLED IAW SRM 53-02, FIGURE 18, 51-30-5, AND 51-10-3. 2 L 7 2 4F A6WE 1998071700496 19980717 00496 WP 1998 7 17 CALA9801242 1 19980712 A 5350 LATCH LEVERS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 THE PULL FROM INTERIOR, EXTERIOR, AND AFT CABIN DOOR TAIL CONE RELEASE HANDLES WAS LOW. THE TAIL CONE LATCH LEVERS WERE ADJUSTED IAW MM 53-53-02. 2 L 7 2 4F A6WE 1998071700497 19980717 00497 NM 1998 7 17 9809806641 1 19980709 A 3610 PNEUMATIC SYST BOEING 747 747212B 1384886 NM NR 2 ENGINE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 641NW 21941 DURING CLIMB, THE NR 2 ENGINE FIRE WARNING SOUNDED. SHUT DOWN THE ENGINE AND DISCHARGED THE FIRE BOTTLE. AIRCRAFT RETU RNED TO MSP AND LANDED WITHOUT INCIDENT. REPLACED THE NR 2 ENGINE STARTER, CONSTANT SPEED DRIVE, STARTER SHUTOFF VALVE, HIGH STAGE VALVE, AND HIGH STAGE CONTROL. OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998071700498 19980717 00498 NM 1998 7 17 9809816603 1 19980713 A 2822 BOOST PUMP BOEING 747 747151 1384891 NM NR 4 FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 603US 19780 DURING CLIMB, THE NR 4 FORWARD AND AFT BOOST PUMPS FAILED. AIRCRAFT RETURNED TO NRT AND LANDED WITHOUT INCIDENT. REPL ACED THE NR 4 FORWARD AND AFT BOOST PUMPS, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998071700499 19980717 00499 SO 1998 7 17 COMA9810154 1 19980712 A 3350 1317 LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 462CA 120264 THREE EMERGENCY LIGHTS ARE INOP ROW 6 AND 7. REPLACED INOP LAMPS. 2 L 7 2 4T RT A31SO 1998071700500 19980717 00500 SO 1998 7 17 COMA9810155 1 19980711 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 264CA 15034 120256 EMERGENCY LIGHTS ARE INOP. REPLACED EMERGENCY LIGHTING BATTERIES. 2 L 7 2 4T RT A31SO 1998071700501 19980717 00501 SO 1998 7 17 COMA9810156 1 19980709 A 3397 WIRE EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 254CA 120233 FLOOR EMERGENCY LIGHT AT ENTRANCE DOES NOT WORK. REPAIRED BROKEN WIRE AT FLOOR LIGHT. 2 L 7 2 4T RT A31SO 1998071700502 19980717 00502 EA 1998 7 17 COMA9860175 1 19980712 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 969CA 7141 EMERGENCY LIGHT AT CABIN ENTRANCE IS INOP. REPLACED LAMPS. 2 L 7 2 4F RT A21EA 1998071700503 19980717 00503 SO 1998 7 17 COMA9810157 1 19980713 A 3010 25C1175A CURRENT SENSOR 1204140400 EMB 120 EMB120RT SO RIGHT FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 120228 120228 CREW REPORTED F/O 'S AOA HEAT INOP. AVIONICS REPLACED THE RIGHT CURRENT SENSOR ASSEMBLY. UPON INSPECTION/TEARDOWN IN T HE AVIONICS SHOP, THE CURRENT SENSOR FOR THE RIGHT AOA VANE HEAT WAS FOUND TO BE DAMGED BY SEVERE OVERHEATING. THE CURR ENT SENSOR WAS REPLACED AND THE ASSEMBLY RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1998071700504 19980717 00504 NM 1998 7 17 UPS98227144 1 19980709 A 3350 BATTERY BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 INSPECTION TYPE-N/A, EMER LIGHTS WOULD NOT TEST PROPERLY (COCKPIT ENTRY UNIT). CHANGED EXIT LIGHT BATTERY ON DOOR, OPS CHECKED GOOD. 2 L 7 3 4F A3WE 1998071700505 19980717 00505 NM 1998 7 17 UPS98227145 1 19980617 A 5311 FRAME BOEING 727 72722C 138400F NM BS 940 CRACKED A IPXA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 945UP 19094 INSPECTION TYPE-N/A, CRACK FOUND AT BS 940 FRAME FITTING LT. REPLACED PER UPS EO B727-5310-4501. 2 L 7 3 4F A3WE 1998071700506 19980717 00506 WP 1998 7 17 UPS98827142 1 19980630 A 5320 4640162502N FITTING DOUG DC8 DC871F 302199D WP BS 1560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, RT UPPER CUSP TO FRAME FITTING HAS MODERATE CORROSION ON FWD SURFACE AT FS 1560. REMOVED AND REPLACE D FITTING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998071700507 19980717 00507 WP 1998 7 17 UPS98827143 1 19980710 A 3350 BATTERIES DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 702UP 45902 INSPECTION TYPE-N/A, EMER LIGHTS ARE DEAD. EMER LIGHT BATTERIES CHARGED ON GROUND POWER FOR 6 HRS, OPS CHECKED OK. 2 L 7 4 4F RT 4A25 1998071700508 19980717 00508 NM 1998 7 17 UPS98227149 1 19980714 A 3250 1000679 LIGHT BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE O OTHER CR CRUISE 1 SO 01 212UP 21392 INSPECTION TYPE-N/A, EMERGENCY LIGHT AT COCKPIT DOOR FAILURE. REMOVED AND REPLACED LIGHT ASSY, OPS CHECKED OK PER MM 33 -50-01. 2 L 7 3 4F A3WE 1998071700509 19980717 00509 NM 1998 7 17 UPS98227151 1 19980714 A 3260 H1010153 SWITCH BOEING 727 727180C 138406G NM NOSE GEAR MALFUNCTIONED A IPXA O OTHER N FALSE WARNING AP APPROACH 1 SO 01 920UP 19873 INSPECTION TYPE-N/A, ON FINAL APPROACH NOSE GEAR GREEN LIGHT WENT OUT, RED LIGHT AND HORN CAME ON. CREW CYCLED GEAR, SA ME PROBLEM. CYCLED GEAR AGAIN, EVERYTHING OK. CREW VERIFIED NOSE GEAR DOWN AND LOCKED VISUALLY. FOUND THAT WITH ONLY SLIGHT MOVEMENT OF NOSE LOCK SWITCH MECHANISM, ABOVE EVENTS WOULD OCCUR. REPLACED NOSE GEAR LOCK SWITCH PER MM 32-6 1-7 1, CK OK. 2 L 7 3 4F A3WE 1998071700510 19980717 00510 NM 1998 7 17 UPS98627150 1 19980706 A 5330 SKIN BOEING 767 76734AF 1385212 NM BS 1295 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 305UP 27243 INSPECTION TYPE-SP, DENT ON FUSELAGE CROWN AT STA 1295 AND STR 7R IS OUT OF LIMITS. REPAIRED AREA IAW SRM 53-00-01 FIG 201. 2 L 7 2 4F RT A1NM 1998071700511 19980717 00511 WP 1998 7 17 UPS98827141 1 19980709 A 2611 302314 SMOKE DETECTOR DOUG DC8 DC871F 302199D WP CARGO COMPT MALFUNCTIONED A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 702UP 45902 INSPECTION TYPE-N/A, FL 350 CARGO SMOKE LIGHT ILLUMINATED ALL POSITIONS INCLUDING NORMAL AND OFF / COMPLIED WITH AOM EXC EPT FOR FIRE BOTTLES. REMOVED AND REPLACED NR 3, 4, 6 SMOKE DETECTORS AND AMPLIFIER. FERRIED TO SDF FOR FWD ENTRY DOOR REPAIR. SMOKE DETECTOR SYSTEM TO BE RETESTED AT SDF. 2 L 7 4 4F RT 4A25 1998071700512 19980717 00512 WP 1998 7 17 UPS98827147 1 19980630 A 5320 3755842503N SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, SHEAR TIE FITTING BETWEEN L 32L TO 33L FS 1200 CRACKED. REMOVED AND REPLACED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998071700513 19980717 00513 WP 1998 7 17 UPS98827148 1 19980626 A 5712 576989125 RIB DOUG DC8 DC871F 302199D WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, RT WING L/E LWR RIB AT WS XOLDI 6.225 IS CRACKED AT THE FWD END. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT RIB IAW SRM 51-1-21 AND DWG 5769891. 2 L 7 4 4F RT 4A25 1998071700514 19980717 00514 WP 1998 7 17 UPS98827152 1 19980628 A 5320 9755584503 FITTING DOUG DC8 DC871F 302199D WP BS 1324 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, FS 1324, RT SIDE, THE FRAME TO CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998071700515 19980717 00515 WP 1998 7 17 UPS98827153 1 19980629 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1265 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, BELLY SKIN FS 1265 L 35L TO 35R HAS HEAVY CORROSION. REPAIRED IAW DHC SK-708-563. 2 L 7 4 4F RT 4A25 1998071700516 19980717 00516 WP 1998 7 17 UPS98827154 1 19980627 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C ,LT WING LE RIB UPPER ARM CRACKED BY AFT FASTENER AT WS XFS 572.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998071700517 19980717 00517 WP 1998 7 17 UPS98827155 1 19980630 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, LONGERON 35L AT FS 220 IS CRACKED. REPAIRED IAW SRM 53-2-2. 2 L 7 4 4F RT 4A25 1998071700518 19980717 00518 WP 1998 7 17 ABXA9800616 1 19980713 A 5610 5613217508 WINDOW DOUG DC8 DC863 302198A WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 FIRST OFFICER'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN. CLEANED LATCH AND LUBRICATED AS REQUIRED, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998071700519 19980717 00519 WP 1998 7 17 MWEA98783 1 19980713 A 5751 SKIN DOUG DC9 DC982 3022082 WP RT AILERON CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND RIGHT AILERON LOWER SKIN INBOARD EDGE CHAFED. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998071700520 19980717 00520 WP 1998 7 17 MWEA98784 1 19980713 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1474 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CRACK AT AFT COMPARTMENT CANTED FRAME AT FS 1474. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998071700521 19980717 00521 WP 1998 7 17 DLL10981420 1 19980703 A 5711 1503229103 SPAR CAP LKHEED 1011 10113851 5265010 WP BS 1043/1163 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 735D 193C1226 THE RT ENDS OF THE FS 1043 AND FS 1163 INTERMEDIATE SPAR UPPER SPAR CAPS WERE FOUND CRACKED BEYOND SRM OR LAC S/B LIMITS . THE CRACKED ENDS OF THE CAPS WERE CUT AND REMOVED AND NEW SECTIONS SPLICED IN WITH STEEL REPAIR ANGLES AND STRAPS. T HE REPAIRS WERE ACCOMPLISHED PER ER/A 365153-14, REV A. 2 L 7 3 4F A23WE 1998071700522 19980717 00522 NM 1998 7 17 DL733981421 1 19980706 A 5330 65184201059 SKIN BOEING 737 737347 1384647 NM LT COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 307WA 23440 A .375 INCH CRACK WAS FOUND IN THE FUSELAGE SKIN AND UNDERLYING GUSSET AT THE UPPER OUTBD CORNER OF THE L1 COCKPIT WINDO W (UPPER END OF THE C-D POST). THE CRACK WAS ROUTED OUT AND A STEEL REPAIR DOUBLER AND ALUMINUM REPAIR TRIPLER WERE INS TALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 365155-14, REV B. 2 L 7 2 4F RT A16WE 1998071700523 19980717 00523 NM 1998 7 17 DL767981422 1 19980707 A 2410 CHECK VALVE OMP250610 BOEING 767 767232 1385132 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 115DA 22227 000000 RIGHT GEN DRIVE LIGHT ILLUMINATED AFTER TAKEOFF. REPLACED PRESSURE SERVICE CHECK VALVE, LEAK CHECK GOOD. 2 L 7 2 4F RT A1NM 1998071700524 19980717 00524 NM 1998 7 17 DLM88981424 1 19980708 A 5244 DOOR DOUG MD88 MD88 3023688 NM ACCESS COMPT OPEN A DALA O OTHER J WARNING INDICATION CL CLIMB 1 SO 27 962DL 49981 AFTER TAKEOFF, ACCESS COMPARTMENT DOOR CAME OPEN AND AIRCRAFT WOULD NOT PRESSURIZE. DOOR LT EXTINGUISHED AFTER LANDING. UPON ARRIVAL, NO DOORS WERE FOUND TO BE OPEN. AIRCRAFT WAS PRESSURIZED AND NO LEAKS WERE DETECTED. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. NO PRESSURIZATION PROBLEMS WERE NOTED. 2 L 7 2 4F RT A6WE 1998071700525 19980717 00525 NM 1998 7 17 DL76L981427 1 19980708 A 2910 272T3100122 LINE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 191DN 28448 724166 RT HYD QTY ZERO EICAS MSG RT HYD DISPLAYED. SYS PRESS LIGHT ILLUM, RESVR QTY LIGHT ILLUM, EICAS MSG RT SYS PRESS DISPLA YED INFO PRIOR TO FLUID LOSS NOTED RT HYD SYS PRESSURE FLUCTUATIONS BETWWEN 1800 AND 3000 PSI. FOUND HYDRAULIC LINE ON FILTER BLOCK RIGHT ENGINE CRACKED. MADE TEMP. REPAIR. FLUSHED SYSTEM, REPLACED ENGINE PUMP AND FILTERS. LEAK CHECK AN D OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1998071700526 19980717 00526 WP 1998 7 17 DLL17981428 1 19980707 A 3350 POWER SUPPLY RPS1 LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 769DL 654 193H1218 EELS AFT OF SEAT 35 LEFT HAND SIDE INOP. REPLACED AFT POWER SUPPLY AND BATTERY PACK CKS GOOD. 2 L 7 3 4F A23WE 1998071700527 19980717 00527 NM 1998 7 17 DLM88981429 1 19980708 A 3350 POWER SUPPLY RPS1 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 918DE 0322 49959 FIRST CLASS EMERGENCY FLOOR TRACK LIGHTS WILL NOT ILLUMINATE. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 1998071700528 19980717 00528 NE 1998 7 17 DLL10981430 2 19980709 A 7260 RB21122B02 CHIP DETECTOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE NOT INSTALLED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 718DA 49855 193C1097 010553 NR 1 ENG OIL LOSS IN EXCESS OF 4 QTS HR. DIVERTED SLC. ENG WAS NOT SHUTDOWN AND NO LOSS OF OIL PRESS. FOUND NR 1 ENG FINE SCAVAGE CHIP DET NOT IN HOUSING AND LAYING ON TOP OF OIL TANK. DET VISUALLY CKD OK BUT ONE O-RING FELL OFF WHEN HA NDLED. REPLACED BOTH O-RINGS AND REINSTALLED CHIP DET. SERVICED OIL 28 PTS AND ENG LEAK CKD GOOD ON IDLE RUN. 2 L 7 3 4F 4 F A23WE E12EU 1998071700529 19980717 00529 WP 1998 7 17 DLL14981435 1 19980708 A 2560 GIRT BAR LKHEED 1011 1011385115 5265015 WP L4 DOOR OUT OF ADJUST A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 193C1244 GIRT BAR WOULD NOT LATCH IN PLACE ON L4 DOOR DURING OPN TEST DURING HMV. NR 29 NO CLEARANCE BETWEEN GIRT BAR AND LATCH COVER AT L4 DOOR. ADJUSTED PER M/M 25-61-00. 2 L 7 3 4F A23WE 1998071700530 19980717 00530 NM 1998 7 17 DL72S981437 1 19980623 A 5753 651927010 FLAP TRACK BOEING 727 727232 1384082 NM TE FLAPS CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 400DA 21144 INB'D FLAP/INB'D TRACK TYP CORROSION AT FWD AND AFT PAD-UP ATTACH HOLES AND FWD LUG - AD 90-07-05 AND 90-06-09. OVERSIZ E HOLES AND SHIM FWD LUG FACE. 2 L 7 3 4F A3WE 1998071700531 19980717 00531 NM 1998 7 17 DL72L981440 1 19980710 A 3350 1001141 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 502DA 21304 AFT EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES. 2 L 7 3 4F A3WE 1998071700532 19980717 00532 WP 1998 7 17 DLL10981441 1 19980710 A 3350 2232 BULB LKHEED 1011 10113851 5265010 WP CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 714DA 193C1090 EXTERIOR EMERGENCY LIGHT AT L3 DOOR INOP. RELAMPED SAME, CHECKS GOOD. 2 L 7 3 4F A23WE 1998071700533 19980717 00533 NM 1998 7 17 DL72W981442 1 19980708 A 2120 AIR DISTRIBUTION BOEING 727 727247 138408F NM CABIN SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 2810W 20648 SMOKE IN CBN/COCKPIT DURING DESCENT 22K TO 11K FT AT IDLE PWR. TOOK A/C FOR PWR RUN. UNABLE TO DUPLICATE. PACK OPN/BL EEDS CK NORMAL. 2 L 7 3 4F A3WE 1998071700534 19980717 00534 NM 1998 7 17 DLM88981443 1 19980711 A 3830 FLUSH MOTOR 834002403 DOUG MD88 MD88 3023688 NM FWD LAVATORY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 932DL 49719 ACRID ODOR ASSOCIATED WITH ELECTRICAL OVERHEAT DETECTED IN THE FWD PSG CABIN. SOURCE DETERMINED TO BE THE FWD LAV. PUL LED THE 3 C/BS FOR THE FLUSH MOTOR. THE ODOR WENT AWAY. COLLAR, OK. BLOCKED OFF THE F/C LAV FWD THE FLUSH MOTOR TO MC O AND PLAC. 2 L 7 2 4F RT A6WE 1998071700535 19980717 00535 NM 1998 7 17 DL73E981447 1 19980708 A 5320 CLIPS BOEING 737 7372S3 NM BS 559-887 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 WHILE ACCOMPLISHING REPLACEMENT OF CRACKED FRAME-TO-STRINGER CLIPS PER BAC S/B 737-53-1085 (AD 93-08-04), MTC. WAS UNABL ETO INSTALL THE REQUIRED RIVETS. THE RIVETS WERE SUBSTITUTED WITH STEEL HI-LOKS PER ER/A 365196-14AD, REV A. 2 L 7 2 4F RT A16WE 1998071700536 19980717 00536 NM 1998 7 17 DL72S981448 1 19980326 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 LOWER AFT CHORD ANGLE IS CRACKED AT 19, 22, 32, 37, 54 AND 59 FORM I/B END OF FLAP. REPAIR PER M/M 57/52/0 FIG 802. 2 L 7 3 4F A3WE 1998071700537 19980717 00537 NM 1998 7 17 DL73E981449 1 19980709 A 5320 693535214 CLIP BOEING 737 7372S3 NM BS 597 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 A SKIN AND STRINGER REPAIR WERE ACCOMPLISHED AT FS 597 STR 2L. THE FRAME-TO-STRINGER CLIP INSPECTION REQUIRED PER BAC S /B 737-53-1085 (AD 93-08-04) WAS ACCOMPLISHED AT THIS LOCATION AND RESULTED IN FINDING A CRACKED CLIP. A NEW CLIP HAD T O BE MODIFIED TO ALLOW FOR INSTALLATION IN THE REPAIRED STRINGER. THE CLIP ALTERATION WAS ACCOMPLISHED PER ER/A 365218- 14AD. 2 L 7 2 4F RT A16WE 1998071700538 19980717 00538 NM 1998 7 17 DL72L981450 1 19980713 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 507DA 671 21309 AFT FLOOR EMERGENCY LIGHTS DID NOT GO ON WHEN TESTED. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 1998071700539 19980717 00539 1998 7 17 VNAA9807004 4 19980711 A 3418 861EF1 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT AOA FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 437JS 72248 3055 THE AIRCRAFT RETURNED TO THE GATE, DUE TO AN ANGLE OF ATTACK WARNING MESSAGE. OUTSTATION MAINTENANCE INSPECTED AND APPR OVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT, TO ACCOMPLISH REPAIRS. THE FERRY FLIGHT WAS CARRIED OUT WITHOUT ANY PROBLE MS. PIT MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND ANGLE OF ATTACK SENSOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-33-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998071700541 19980717 00541 WP 1998 7 17 TWAA9809401 1 19980610 A 3350 0105606005 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9402W 53138 STL - FLT 765 - DURING GROUND CHECK, FOUND ONE EGRESS LAMP INOPERATIVE AT ROW 14, AND EGRESS LIGHTING ROW 30 TO ROW 33 I NOPERATIVE. REPLACED LAMP AT ROW 14, MFG P/N 7732. FOUND EXPOSED WIRES NEAR SEAT ROW 24, AND REPLACED LIGHT STRIP. CH ECK-C 10-29-97 LAX. (X) 2 L 7 2 4F RT A6WE 1998071700542 19980717 00542 WP 1998 7 17 TWAA9809402 1 19980422 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP BS 927 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND VERTICAL STIFFENER BELOW FLOOR AT STA 927, LBL 44, CRACKED. REPAIRED PER SR M 51-01. INSTALLED NEW CASTING. (X) 2 L 7 2 4F A6WE 1998071700543 19980717 00543 WP 1998 7 17 TWAA9809403 1 19980218 A 5320 JAMB DOUG DC9 DC932 3022066 WP SERVICE DOORWAY DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT FORWARD SERVICE DOOR JAMB PAN DAMAGED AT BAYONET PICK-UP BRACKET ON CENTE R AFT EDGE OF DOOR. INSTALLED REPAIR DOUBLER PER SRM 53-05, FIG 42. (X) 2 L 7 2 4F A6WE 1998071700544 19980717 00544 WP 1998 7 17 TWAA9809404 1 19980318 A 5320 SUPPORT DOUG DC9 DC951 3022051 WP CABIN CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 418EA 47676 MCI - DURING OP 9 MAINTENANCE CHECK, FOUND ONE INCH CRACK IN CENTER OF CENTER SUPPORT IN BIRD CAGE. REPAIRED CRACK IN C ENTER SUPPORT IN BIRD CAGE PER SRM 53-01 PAGE 10. (X) 2 L 7 2 4F RT A6WE 1998071700545 19980717 00545 WP 1998 7 17 TWAA9809405 1 19980312 A 5320 CASTING DOUG DC9 DC932 3022066 WP BS 718 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND 718 CASTING CRACKED BEYOND PREVIOUS REPAIR ON AFT SIDE OF CASTING, RT SIDE O F ACFT. REMOVED AND REPLACED CASTING PER SRM 51-01, PAGE 1 ITEM C, AND STANDARD MAINT PRACTICES. (X) 2 L 7 2 4F A6WE 1998071700546 19980717 00546 WP 1998 7 17 TWAA9809406 1 19980319 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 111-195 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 997Z 47029 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND RT WING TRAILING EDGE INBD FLAP REAR SPAR, INBD FLAP CASTING MOUNT HOLE LOWE R INBD HOLE, WITH CRACK EXTENDING INTO RADIUS ON FWD SIDE OF FUEL TANK. SPLICED SECTION OF LOWER SPAR FROM STA XRS 111. 510 TO XRS 195.210, PER DOUGLAS DWG J061065, AND STD PRACTICES. (X) 2 L 7 2 4F A6WE 1998071700547 19980717 00547 WP 1998 7 17 TWAA9809407 1 19980316 A 5320 SUPPORT DOUG DC9 DC983 3022083 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9306T 49567 MCI - DURING CHECK-C, MAINTENANCE FOUND AFT END OF LT MLG DOOR HINGE AND ABOVE DOORWAY FRAME SUPPORT BRACE WITH ID CRACK ED. REPLACED SUPPORT BRADE PER SRM 51-01, PG 1 ITEM C, AND TWA STD PRACT. (X) 2 L 7 2 4F RT A6WE 1998071700556 19980717 00556 WP 1998 7 17 TWAA9809416 1 19980609 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1016-1045 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND BODY FAIRING T-ANGLE AT BL ZERO CORRODED FROM APROXIMATELY FS 1016 TO FS 104 5. REPLACED T-ANGLE PER SRM 51-01, PAGE 1 ITEM C. (X) 2 L 7 2 4F A6WE 1998071700557 19980717 00557 WP 1998 7 17 TWAA9809417 1 19980609 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 980-996 CHAFED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 920L 47734 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND INTERCOSTAL FS 980 TO FS 996 BETWEEN S27R AND S28R WITH APPROXIMATELY .25 IN CH HOLE WORN INTO LIP. REPLACED AND INSTALLED NEW INTERCOSTAL PER SRM 51-01, PAGE 1 ITEM C. (X) 2 L 7 2 4F A6WE 1998071700558 19980717 00558 WP 1998 7 17 TWAA9809418 1 19980609 A 5311 FRAME DOUG DC9 DC932 3022066 WP FUSELAGE MISDRILLED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 920L 47734 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND .3125 INCH HOLE IN TOP OF FORMER 36Z AT STR 29R, RBL 6. HOLE DRILLED FOR RI VNUT NO LONGER NEEDED. DID NDT CHECK FOR CRACKS. PLUGGED AND REPAIRED PER ARA 15285. (X) 2 L 7 2 4F A6WE 1998071700559 19980717 00559 WP 1998 7 17 TWAA9809419 1 19980611 A 5753 RIB DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RIBS CRACKED, INBD AND OTBD SIDES OF OTBD HINGE CASTING ON RT WING TE FLAP. REPLACED RIBS, INBD AND OTBD OF HINGE CASTING PER SRM 51-01, PAGE 1 ITEM C. (X) 2 L 7 2 4F A6WE 1998071700560 19980717 00560 NM 1998 7 17 TSAA9833297 1 19980604 A 3350 8731002511 LIGHT BOEING 737 737230 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED AFT SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO ALL IS WELL LIGHT BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700561 19980717 00561 NM 1998 7 17 TSAA9833296 1 19980604 A 3350 8731002511 LIGHT BOEING 737 737230 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO ALL IS WELL LIGHT BEING INOP. OPS CHECKED OK. AIRC RAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700562 19980717 00562 NM 1998 7 17 TSAA9833298 1 19980605 A 3350 8731002511 LIGHT BOEING 737 737282 13844AT NM LT OVERWING INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 RIGHT SIDE OVERWING EXIT IDENTIFIER (EMERGENCY LIGHT) STAYS ON. REPLACED LIGHT ASSY. SYSTEM OPS CHECKED GOOD. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998071700563 19980717 00563 NM 1998 7 17 TSAA9833300 1 19980606 A 3350 8731002511 LIGHT BOEING 737 737230 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 FORWARD SERVICE DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998071700564 19980717 00564 NM 1998 7 17 TSAA9833306 1 19980614 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY IN NR 3 POSITION FLOOR PROXIMITY LIGHT DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998071700565 19980717 00565 NM 1998 7 17 TSAA9833305 1 19980614 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY IN NR 4 POSITION FLOOR PROXIMITY LIGHT DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998071700566 19980717 00566 1998 7 17 TSAA9834277 4 19980522 A 3417 HG480B13 DADC BOEING 737 7372Y5 1384554 NM NR 2 FAILED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 810AL 24031 FIRST OFFICER AIRSPEED, ALTIMETER, AND VERTICAL SPEED INDICATOR ERRATIC. REPLACED NR 2 DADC IAW MM 34-12-11. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4U RT A16WE 1998071700567 19980717 00567 NM 1998 7 17 TSAA9833274 1 19980528 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED BATTERY PACK ON NR 1 FLOOR EMERGENCY LIGHT DUE TO BEING INOPERATIVE. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE. (X) 2 L 7 2 4F RT A16WE 1998071700568 19980717 00568 NM 1998 7 17 TSAA9833273 1 19980528 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED BATTERY PACK ON NR 3 POSITION FLOOR EMERGENCY LIGHT DUE TO BEING INOPERATIVE. OPS CHECKED GOOD. AIRCRAFT RETU RNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998071700569 19980717 00569 NM 1998 7 17 TSAA9833272 1 19980526 A 3350 1000679 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 FORWARD SERVICE DOOR EMERGENCY LIGHT DOES NOT TEST. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVI CE. (X) 2 L 7 2 4F RT A16WE 1998071700570 19980717 00570 NM 1998 7 17 TSAA9833271 1 19980526 A 3350 1000679 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 FORWARD ENTRY DOOR EMERGENCY LIGHT DOES NOT TEST. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE . (X) 2 L 7 2 4F RT A16WE 1998071700571 19980717 00571 NM 1998 7 17 TSAA9833270 1 19980526 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND NR 3 POSITION EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998071700572 19980717 00572 NM 1998 7 17 TSAA9833269 1 19980526 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 ON SERVICE CHECK, FOUND NR 6 POSITION EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998071700573 19980717 00573 NM 1998 7 17 TSAA9821267 1 19980524 A 2131 CIRCUIT BREAKER BOEING 737 7372S5C 1384499 NM PRESSURE CONTROL TRIPPED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 AIRCRAFT DOES NOT PRESSURIZE AFTER TAKEOFF. FOUND PRESSURE CONTROL CIRCUIT BREAKERS TRIPPED. RESET CIRCUIT BREAKERS. P ERFORMED BITE CHECK. NO OTHER DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998071700574 19980717 00574 NM 1998 7 17 TWRA9833 1 19980614 A 3310 LIGHT BOEING 747 747212B 1384886 NM COCKPIT SHORTED A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 6186 21439 DURING CRUISE, HAD SMOKE IN COCKPIT. REPAIRED NR 4 FWD BOOST PUMP AMBER LIGHT MODULE. OPS CHECK OK. (X) 2 L 7 4 4F A20WE 1998071700575 19980717 00575 NM 1998 7 17 TWRA9834 1 19980615 A 3230 RETRACT MECH BOEING 747 747282B 1384860 NM NLG LACK OF LUBE A TWRA K NONE J WARNING INDICATION AP APPROACH 1 EA 15 610FF 20501 ON GEAR EXTENSION, NOSE GEAR REMAINED IN RETRACTED POSITION WITH DOOR CLOSED WITH ALL MAIN BODY GEAR DOWN AND LOCKED. W HEN GEAR HANDLE WAS RECYCLED TO UP POSITION AND THEN REPOSITIONED TO DOWN, ALL GEAR EXTENDED AND LOCKED DOWN NORMALLY. A IRCRAFT TOWED FROM GATE TO HANGAR. NOSE GEAR LUBED PER MM 32-00-50. NOSE GEAR RETRACTION PERFORMED PER MM 32-21-01, PA GE 601, ALL OPS NORMAL. (X) 2 L 7 4 4F A20WE 1998071700576 19980717 00576 NM 1998 7 17 TWRA9832 1 19980613 A 3350 CONNECTOR BOEING 747 747238B 1384828 NM CABIN LOOSE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 ON PRE-FLIGHT, FOUND UPPER DECK EVACUATION EMERGENCY TRACK LIGHTS INOPERATIVE. FOUND BROKEN CONNECTION AT 73HK. RESECUR ED CONNECTION. OPS CHECK UPPER DECK EVAC TRACK LIGHTS. OPS NORMAL AS PER MM 33-51-00. (X) 2 L 7 4 4F A20WE 1998071700577 19980717 00577 EU 1998 7 17 SIMA981675 1 19980612 A 5347 S53678001200 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THAT THE LEFT FWD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS WERE CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 22,385.5 HOURS. ACFT TC: 24,959. REF: OPERATOR CONTROL NRS 98ZZZX2360 THROUGH 98ZZZX2 363. (X) 2 H 7 2 4T RT A53EU 1998071700578 19980717 00578 EU 1998 7 17 98ZZZX2360 1 19980612 A 5347 S53678001201 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THAT THE LEFT FWD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS WERE CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 22,385.5 HOURS. ACFT TC: 24,959. REF: OPERATOR CONTROL NRS SIMA981675, AND 98ZZZX236 1 THROUGH 98ZZZX2363. 2 H 7 2 4T RT A53EU 1998071700579 19980717 00579 EU 1998 7 17 98ZZZX2361 1 19980612 A 5347 S53375001202 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THAT THE LEFT FWD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS WERE CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 22,385.5 HOURS. ACFT TC: 24,959. REF: OPERATOR CONTROL NRS SIMA981675, AND 98ZZZX236 0 THROUGH 98ZZZX2363. 2 H 7 2 4T RT A53EU 1998071700580 19980717 00580 EU 1998 7 17 98ZZZX2362 1 19980612 A 5347 S53678001202 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THAT THE LEFT FWD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS WERE CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT WAS RETURNED TO SERVICE. REPLACED 2 EACH. REF: OPERATOR CONTROL NRS ACFT TT: 22,385.5 HOURS. ACFT TC: 24,959. SIMA981 675, AND 98ZZZX2360 THROUGH 98ZZZX2363. 2 H 7 2 4T RT A53EU 1998071700581 19980717 00581 EU 1998 7 17 98ZZZX2363 1 19980612 A 5347 S53375001204 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THAT THE LEFT FWD INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS WERE CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 22,385.5 HOURS. ACFT TC: 24,959. REF: OPERATOR CONTROL NRS SIMA981675, AND 98ZZZX236 0 THROUGH 98ZZZX2362. 2 H 7 2 4T RT A53EU 1998071700582 19980717 00582 EU 1998 7 17 SIMA981667 1 19980524 A 5711 7257120014 SPAR SAAB SF340 340B 7860101 EU WS 398/391 DAMAGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 317AE 340B317 BNA - FLT 9850 - RIGHT WING OUTBOARD TRAILING EDGE DAMAGED BY SERVICE VEHICLE. REAR SPAR WEB, LOWER SPAR CAP, AND LOWER SKIN NEED REPAIR. INSPECTED DAMAGE. PERFORMED PRECAUTIONARY HARD LANDING INSPECTION OF AIRCRAFT. CUT OUT DAMAGE TO S PAR WEB CAP. REPLACED SECTION OF LOWER SPAR CAP EXTRUSION, REAR SPAR WEB, AND AFFECTED RIBS. FABRICATED AND INSTALLED REPAIR DOUBLER FOR LOWER SKIN. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 12,568.7 HOURS. ACFT TC: 12,796. REF: OPERATOR CONTROL NRS 98ZZZX2364 THROUGH 98ZZZX2366. (X) 2 L 7 2 4T RT A52EU 1998071700583 19980717 00583 EU 1998 7 17 98ZZZX2364 1 19980524 A 5712 7257286082 RIB SAAB SF340 340B 7860101 EU WS 415 DAMAGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 317AE 340B317 BNA - FLT 9850 - RIGHT WING OUTBOARD TRAILING EDGE DAMAGED BY SERVICE VEHICLE. REAR SPAR WEB, LOWER SPAR CAP, AND LOWER SKIN NEED REPAIR. INSPECTED DAMAGE. PERFORMED PRECAUTIONARY HARD LANDING INSPECTION OF AIRCRAFT. CUT OUT DAMAGE TO S PAR WEB CAP. REPLACED SECTION OF LOWER SPAR CAP EXTRUSION, REAR SPAR WEB, AND AFFECTED RIBS. FABRICATED AND INSTALLED REPAIR DOUBLER FOR LOWER SKIN. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 12,568.7 HOURS. ACFT TC: 12,796. REF: OPERATOR CONTROL NRS SIMA981667, AND, 98ZZZX2365 THROUGH 98ZZZX2366. 2 L 7 2 4T RT A52EU 1998071700584 19980717 00584 EU 1998 7 17 98ZZZX2365 1 19980524 A 5712 7257286024 SKIN SAAB SF340 340B 7860101 EU WS 396 DAMAGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 317AE 340B317 BNA - FLT 9850 - RIGHT WING OUTBOARD TRAILING EDGE DAMAGED BY SERVICE VEHICLE. REAR SPAR WEB, LOWER SPAR CAP, AND LOWER SKIN NEED REPAIR. INSPECTED DAMAGE. PERFORMED PRECAUTIONARY HARD LANDING INSPECTION OF AIRCRAFT. CUT OUT DAMAGE TO S PAR WEB CAP. REPLACED SECTION OF LOWER SPAR CAP EXTRUSION, REAR SPAR WEB, AND AFFECTED RIBS. FABRICATED AND INSTALLED REPAIR DOUBLER FOR LOWER SKIN. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 12,568.7 HOURS. ACFT TC: 12,796. REF: OPERATOR CONTROL NRS SIMA981667, AND, 98ZZZX2364 THROUGH 98ZZZX2366. 2 L 7 2 4T RT A52EU 1998071700585 19980717 00585 EU 1998 7 17 98ZZZX2366 1 19980524 A 5730 SKIN SAAB SF340 340B 7860101 EU WS 392/415 DAMAGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 317AE 340B317 BNA - FLT 9850 - RIGHT WING OUTBOARD TRAILING EDGE DAMAGED BY SERVICE VEHICLE. REAR SPAR WEB, LOWER SPAR CAP, AND LOWER SKIN NEED REPAIR. INSPECTED DAMAGE. PERFORMED PRECAUTIONARY HARD LANDING INSPECTION OF AIRCRAFT. CUT OUT DAMAGE TO S PAR WEB CAP. REPLACED SECTION OF LOWER SPAR CAP EXTRUSION, REAR SPAR WEB, AND AFFECTED RIBS. FABRICATED AND INSTALLED REPAIR DOUBLER FOR LOWER SKIN. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 12,568.7 HOURS. ACFT TC: 12,796. REF: OPERATOR CONTROL NRS SIMA981667, AND, 98ZZZX2364 THROUGH 98ZZZX2365. 2 L 7 2 4T RT A52EU 1998071700586 19980717 00586 EU 1998 7 17 SIMA981695 1 19980618 A 5347 4650000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DURING HMBV INSPECTION, SEAT TRACK BL ZERO AT STA 297 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 55 INCH SECTION O F CORRODED SEAT TRACK. FABRICATED AND INSTALLED 55 INCH EXTRUSION AND 15 INCH U-BEAM. ACFT TT: 15,388.4 HOURS. ACFT TC: 14,564. (X) 2 L 7 2 4T RT A52EU 1998071700587 19980717 00587 EU 1998 7 17 SIMA981694 1 19980618 A 5347 4640000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DURING HMBV INSPECTION, SEAT TRACK BL 18.3L AT STA 297 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 11 INCH SECTION OF CORRODED SEAT TRACK. FABRICATED AND INSTALLED 11 INCH EXTRUSION AND 15 INCH U-BEAM. ACFT TT: 15,388.4 HOURS. ACFT TC: 14,564. (X) 2 L 7 2 4T RT A52EU 1998071700588 19980717 00588 EU 1998 7 17 SIMA981651 1 19980614 A 5311 S5372408200 ZEE FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND ZEET OF FRAME 39 CORRODED BE TWEEN STR 14 AND STR 15. MAINTENANCE REP AIRED FRAME. ACFT TT: 22,385.5 HOURS. ACFT TC: 24,959. (X) 2 H 7 2 4T RT A53EU 1998071700589 19980717 00589 EU 1998 7 17 SIMA981652 1 19980614 A 5320 S5367800821602 ZEE MEMBER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 144DD 074 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE RIGHT AFT ZEE MEMBER CORRODED BETWEEN FRAMES 39 AND 41. MAINTENAN CE REMOVED AND REPLACED ZEE MEMBER. ACFT TT: 22,385.5 HOURS. ACFT TC: 24,959. (X) 2 H 7 2 4T RT A53EU 1998071700590 19980717 00590 WP 1998 7 17 EIAA980214 1 19980626 A 5347 TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN THE FOLLOWING AREAS: LBL 37, FS 328. LBL 37, FS 419. LBL 37 , FS 510. LBL 37, FS 601. LBL 37, FS 792. LBL 37, FS 983. LBL 37, FS 1074. LBL 37, FS 1165. LBL 16.25, FS 419. LB L 16.25, FS 510. LBL 16.25, FS 601. LBL 16,25, FS 792. LBL 16.25, FS 983. LBL 16.25, FS 1074. LBL 16.25, FS 1165. R BL 8.5, FS 510. RBL 8.5, FS 601. RBL 8.5, FS 792. RBL 8.5, FS 983. RBL 8.5, FS 1165. RBL 33.25, FS 237. RBL 33.25, FS 328. RBL 33.25, FS 510. RBL 33.25, FS 792. RBL 33.25, FS 1165. (X) 2 L 7 2 4F A6WE 1998071700591 19980717 00591 WP 1998 7 17 98ZZZX2367 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 419 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2368 THROUG H 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700592 19980717 00592 WP 1998 7 17 98ZZZX2368 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 510 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUG H 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700593 19980717 00593 WP 1998 7 17 98ZZZX2369 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 601 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUG H 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700594 19980717 00594 WP 1998 7 17 98ZZZX2370 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 792 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUG H 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700595 19980717 00595 WP 1998 7 17 98ZZZX2371 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 983 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUG H 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700596 19980717 00596 WP 1998 7 17 98ZZZX2372 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 1074 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUG H 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700597 19980717 00597 WP 1998 7 17 98ZZZX2374 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 37. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROUG H 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700598 19980717 00598 WP 1998 7 17 98ZZZX2375 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 419 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700599 19980717 00599 WP 1998 7 17 98ZZZX2376 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 510 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700600 19980717 00600 WP 1998 7 17 98ZZZX2377 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 601 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700601 19980717 00601 WP 1998 7 17 98ZZZX2378 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 792 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700602 19980717 00602 WP 1998 7 17 98ZZZX2379 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 983 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700603 19980717 00603 WP 1998 7 17 98ZZZX2380 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 1074 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700604 19980717 00604 WP 1998 7 17 98ZZZX2381 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT LBL 16.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700605 19980717 00605 WP 1998 7 17 98ZZZX2382 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 510 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 8.5. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROU GH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700606 19980717 00606 WP 1998 7 17 98ZZZX2383 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 601 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 8.5. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROU GH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700607 19980717 00607 WP 1998 7 17 98ZZZX2384 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 792 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 8.5. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROU GH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700608 19980717 00608 WP 1998 7 17 98ZZZX2385 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 983 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 8.5. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROU GH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700609 19980717 00609 WP 1998 7 17 98ZZZX2386 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 8.5. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THROU GH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700610 19980717 00610 WP 1998 7 17 98ZZZX2387 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 237 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 33.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700611 19980717 00611 WP 1998 7 17 98ZZZX2388 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 33.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700612 19980717 00612 WP 1998 7 17 98ZZZX2389 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 510 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 33.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700613 19980717 00613 WP 1998 7 17 98ZZZX2390 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 792 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 33.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998071700615 19980717 00615 WP 1998 7 17 VJ9800223 1 19980712 A 3610 591461325 CLAMP DOUG DC9 DC932 3022066 WP NR 1 ENGINE LOOSE A ZZDA O OTHER J WARNING INDICATION CR CRUISE 1 SO 15 967VV 47170 NR 1 ENGINE A-LOOP INDICATION INTERMITTENT DURING FLIGHT. REPLACED 13TH STAGE PNEUMATIC CLAMP AND REPOSITIONED. SUBSEQ UENTLY, CHECKED SYSTEM, RECONNECTED CONNECTORS P1-824 AND P1-825 TO R5-27 AND R5-29 RESPECTIVELY. SYSTEM CHECKED GOOD I AW MM 26-10. 2 L 7 2 4F A6WE 1998071700616 19980717 00616 WP 1998 7 17 VJ9800224 1 19980702 A 5320 1A340304912458 JAMB DOUG DC9 DC932 3022066 WP CARGO COMPT DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 931VV 47674 FWD AND AFT LOWER DOOR JAMB IN FWD CARGO COMPARTMENT REQUIRES REPAIR AT FWD AND AFT CORNER. FABRICATED REPAIR DOUBLER, DRILLED, TREATED, PRIMED AND INSTALLED IAW RES 1-06013 AND DC9 SRM 53005, FIG 44. 2 L 7 2 4F A6WE 1998071700617 19980717 00617 EU 1998 7 17 MALA976161 1 19980709 A 3610 7221100643 BLEED PIPE SAAB SF340 SF340A 7850100 EU LT WING CRACKED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 89XJ 089 LEFT BLEED AIR LEAK DETECT ANNUNICATOR CAME ON, RESET VALVES PER QRH, NO CHANGE. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED CRACKED BLEED PIPE AT POSITION 18 ON LEFT SIDE. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998071700618 19980717 00618 EU 1998 7 17 MALA976162 1 19980708 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A MALA A F UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CR CRUISE 1 GL 15 443XJ 443 INFLIGHT, CARGO SMOKE LIGHT ILLUMINATED, CREW DISCHARGED NR 1 AND NR 2 CARGO EXTINGUISHERS. CREW DECLARED EMERGENCY AND RETURNED TO PLN WHERE CFR FOUND NO SIGNS OF SMOKE OR FLAMES. MAINTENANCE INSPECTED CARGO, NO SIGNS OF SMOKE OR FLAMES. INSPECTED AND CLEANED CARGO SMOKE DETECTOR PER MM 26-13-00. MAINTENANCE REPLACED CARGO RT AND LT FIRE BOTTLES IAW SF3 40 MM ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 1998071700619 19980717 00619 NM 1998 7 17 K3HA980090 1 19980714 A 3010 ANTI-ICE VALVE BOEING 727 727225 1384077 NM NR 3 ENGINE LOOSE A K3HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 354PA 20624 NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER TAKEOFF LIGHT WOULD EXTINGUISH AT 1.4 EPR. SECURED LOOSE BOLTS ON WING A NTI-ICE VALVE MM 30-13-0. 2 L 7 3 4F A3WE 1998071700620 19980717 00620 NM 1998 7 17 AWXA9800150 1 19980628 A 5314 65458681 KEELBEAM BOEING 737 737112 1384412 NM BS 592.5 MISREPAIRED A AWXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 28 708AW 19771 FOUND DURING SCHEDULED INSPECTION EXISTING REPAIRS ON KEEL BEAM LOWER CHORD FROM BS 556.2 LML 6.7 TO SB 592.5 TO 638.5 R BL 6.7 FOUND TO BE STRUCTURALLY UNACCEPTABLE. REPAIRED PER ER 2-53-15-79 -15-79 8110-3 DATED 6/25/98. 2 L 7 2 4F A16WE 1998071700621 19980717 00621 NM 1998 7 17 AWXA9800151 1 19980623 A 4920 TURBINE BOEING 737 7373G7 1384595 NM APU FAILED A A AWXA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 28 306AW 19784 12993 24633 ON TAKEOFF, APU LOW OIL PRESSURE LIGHT ILLUMINATED. SHUT DOWN APU, NO OTHER PROBLEMS. UPON INSP FOUND TURBINE WHEEL M ISSING, NO DAMAGE NOTED BEYOND MUFFLER AND APU. APU PLACARDED INOP PER MEL. REMOVED AND REPLACED APU ON 4 JUL 98. 2 L 7 2 4F RT A16WE 1998071700622 19980717 00622 NM 1998 7 17 AWXA9800152 1 19980712 A 3350 900835A BATTERY PACK BOEING 737 737277 1384570 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 185AW 22652 FWD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK. 2 L 7 2 4F RT A16WE 1998071700623 19980717 00623 EU 1998 7 17 AWXA9800153 1 19980709 A 3231 BOLT AIRBUS 320 A320231 3930325 EU NLG DOOR ACT MISSING A AWXA O OTHER J WARNING INDICATION CL CLIMB 1 WP 28 634AW 091 AFTER GEAR RETRACTION, LEFT NOSE GEAR DOOR WOULD NOT CLOSE. REPLACED NLG DOOR ACTUATOR CYLINDER BOLT IAW 32-31-16, OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1998071700624 19980717 00624 WP 1998 7 17 CALA9801243 1 19980713 A 3222 STRUT DOUG DC9 DC931 3022065 WP NLG REQUIRED SERVICE A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 18563 47487 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING PIT. THE AIRCRAFT WAS RETURNED TO PI T WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE STRUT FLAT. THE NOSE STRUT WAS SERVICED IAW MM 32-21-02 . THE NOSE GEAR WAS SWUNG SEVERAL TIMES WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F A6WE 1998071700625 19980717 00625 WP 1998 7 17 CALA9801244 1 19980714 A 3260 LAMPS DOUG DC9 DC982 3022082 WP NLG FAILED A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 98876 49444 THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROAC. ALL OTHER INDICATIONS APPEARED NORMAL A ND GEAR WAS MECHANICALLY CONFIRMED DOWN AND LOCKED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPL ACED ALL FOUR NOSE GEAR INDICATION LAMPS. A GEAR RETRACTION WAS PERFORMED IAW MM 32-60-00, PAGE 201 WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F A6WE 1998071700626 19980717 00626 NM 1998 7 17 SWAA981207 1 19980623 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 1013 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED LOWER SURFACE OF UPPER FLANGE OF INTERCOSTAL AT BL 0, BS 1013. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700627 19980717 00627 NM 1998 7 17 SWAA981208 1 19980623 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED DIAGONAL INTERCOSTAL AT BS 1006 TO 1016, LBL 7. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998071700628 19980717 00628 NM 1998 7 17 SWAA981209 1 19980623 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 1016, FLOOR PANEL HOLE LBL 6, BS 1016 FLOOR PANEL HOLE LBL 10, BS 1016 FLOOR PANEL HOLE LBL 15 AND BS 1016 FLOOR PANEL HOLE LBL 16. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700629 19980717 00629 NM 1998 7 17 SWAA981210 1 19980623 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED BS 947.5 FLOORBEAM UPPER CHORD FROM SCREW HOLE AT LBL 54. REPAIRED PER SWA RA NR 1-353-1834. 2 L 7 2 4F RT A16WE 1998071700630 19980717 00630 NM 1998 7 17 SWAA981211 1 19980623 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 OUT OF LIMITS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND 4 FASTENER HOLES ALONG THE FLOORBEAM AT BS 1016 OUT OF LIMITS. REPAIRED PER BOEING TI-A53-014. 2 L 7 2 4F RT A16WE 1998071700631 19980717 00631 NM 1998 7 17 SWAA981212 1 19980623 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED CI-CHECK, FOUND CRACKED AFT CARGO DOOR UPLOCK INTERCOSTAL. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700632 19980717 00632 NM 1998 7 17 SWAA981213 1 19980623 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 373SW 26581 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED WEB ATTACH ANGLE JUST FWD OF GALLEY DOOR CUTOUT AT BS 291.5 ABOVE STR 9R. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700633 19980717 00633 NM 1998 7 17 SWAA981214 1 19980624 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1012-1020 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1012 TO BS 1020, LBL 2. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700634 19980717 00634 NM 1998 7 17 SWAA981215 1 19980624 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1016 LBL 13. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700635 19980717 00635 NM 1998 7 17 SWAA981216 1 19980624 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN ABOVE BS 767, STR 19R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700636 19980717 00636 NM 1998 7 17 SWAA981217 1 19980624 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 1028 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CLOSET WALL ATTACH ANGLE WEB AT BS 1028 BL 0. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998071700637 19980717 00637 NM 1998 7 17 SWAA981218 1 19980624 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED C2 CHECK, FOUND CRACKED AFT CARGO DOOR UPLATCH MECHANISM INTERCOSTAL. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700638 19980717 00638 NM 1998 7 17 SWAA981219 1 19980624 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 770 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 770 STR 23L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700639 19980717 00639 NM 1998 7 17 SWAA981220 1 19980624 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 020SW 21337 DURING SCHEDULED C2 CHECK, FOUND CRACKED AFT CARGO DOOR UPLATCH MECHANISM ABOVE DOOR INTERCOSTAL. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700640 19980717 00640 NE 1998 7 17 SWAA981265 2 19980707 A 7200 ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 701SW 22053 NR 2 ENGINE SHUTDOWN DUE TO HIGH EGT. AIRCRAFT MADE AN UNEVENTFUL LANDING. ENGINE CHANGE IN PROGRESS PER BOEING MM. 2 L 7 2 4F 4 F A16WE E2EA 1998071700641 19980717 00641 NM 1998 7 17 SWAA981266 1 19980706 A 2560 SLIDE BOEING 737 7375H4 138449D NM EMERGENCY EXIT DISLODGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 25318 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT SLIDE FELL OUT OF CONTAINER WHEN OPENING FORWARD EXIT DOOR. INSTALLED SLI DE, OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998071700642 19980717 00642 NM 1998 7 17 SWAA981267 1 19980706 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 292 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22730 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED ANGLE AT BS 292 BELOW 511R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700643 19980717 00643 NM 1998 7 17 SWAA981268 1 19980706 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22730 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL BRACKET AT BS 178, RBL 26 WL 195. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998071700644 19980717 00644 NM 1998 7 17 SWAA981269 1 19980706 A 5320 WEB BOEING 737 7372H4 138448C NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22730 DURING SCHEDULED 1/4 D-CHECK, FOUND LOWER WEB AT FWD SIDE OF CARGO DOOR CUTOUT DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700645 19980717 00645 NM 1998 7 17 SWAA981270 1 19980706 A 3350 LIGHTS BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721SW 22697 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT EGRESS FLOOR LIGHTING LOOSE AT ROW 14. SECURED AND STOWED FLOOR EGRESS LI GHTING, OPS CK GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998071700646 19980717 00646 NM 1998 7 17 SWAA981271 1 19980706 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE AT BS 639, BETWEEN STR 7 TO 8L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700647 19980717 00647 NM 1998 7 17 SWAA981272 1 19980706 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER 4R AT BS 907 STRINGER SERVICE AND 4L AT BS 907 STRINGER SPLICE. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700648 19980717 00648 NM 1998 7 17 SWAA981273 1 19980706 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 290, RBL 54 WL 254. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700649 19980717 00649 NM 1998 7 17 SWAA981274 1 19980706 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 277 WL 231 RBL 56. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700650 19980717 00650 NM 1998 7 17 SWAA981275 1 19980706 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 348 LBL 65 WL 223. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700651 19980717 00651 NM 1998 7 17 SWAA981276 1 19980706 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 301.9 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND WEB INTERCOSTAL GOUGED AT BS 301.9 LBL 59, WL 234. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700652 19980717 00652 NM 1998 7 17 SWAA981277 1 19980706 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 988-1005 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND SEVERAL GOUGES IN SKIN AT BS 988 TO 1005, STR 15L, WL 236. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998071700653 19980717 00653 NM 1998 7 17 SWAA981278 1 19980706 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 269 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 269, RBL 12, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700654 19980717 00654 NM 1998 7 17 SWAA981279 1 19980706 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 480/500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500C BETWEEN STR 8 TO 9L, BS 500A, BETWEEN STR 8 TO 9L AND BS 480 BE TWEEN STR 8 TO 9L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700655 19980717 00655 NM 1998 7 17 SWAA981280 1 19980706 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440/500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500C BETWEEN STR 8 TO 9R, BS 500A BETWEEN STR 8 TO 9R AND BS 440 BET WEEN STR 8 TO 9R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700656 19980717 00656 NM 1998 7 17 SWAA981281 1 19980706 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400/380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 400 BETWEEN STR 8 TO 9R AND BS 380 BETWEEN STR 8 TO 9R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700657 19980717 00657 NM 1998 7 17 SWAA981282 1 19980706 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER T-CHORD AT BS 294.5 WL 208 BBL 0 AROUND NUT PLATE HOLE. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700658 19980717 00658 NM 1998 7 17 SWAA981283 1 19980706 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 328-334 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AROUND NUT PLATE HOLES AT BS 328 TO 334 LBL 10 WL 208. REMOVED A ND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700659 19980717 00659 NM 1998 7 17 SWAA981284 1 19980706 A 5743 BEAM BOEING 737 7373H4 1384600 NM RT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED RIGHT HAND MAIN LANDING GEAR BEAM LOWER SURFACE AROUND FASTENER HOLES AT SEVEN LOCATIONS. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700660 19980717 00660 NM 1998 7 17 SWAA981285 1 19980706 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 3 WL 159. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998071700661 19980717 00661 NM 1998 7 17 SWAA981286 1 19980706 A 5510 ANGLE BOEING 737 737301 1384611 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND CRACKED AND GOUGED L-ANGLE BEHIND PANEL 9224 ON RT HORIZ STAB. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700662 19980717 00662 NM 1998 7 17 SWAA981287 1 19980706 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM PAX DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED INTERCOSTAL ON BOTTOM END OF FWD ENTRY DOOR ON FWD SIDE OF FWD ENTRY DOOR. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700663 19980717 00663 NM 1998 7 17 SWAA981288 1 19980706 A 5320 ANGLE BOEING 737 737317 138447P NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED TRANSITION ANGLE AT BS 787 RBL 23. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700664 19980717 00664 NM 1998 7 17 SWAA981289 1 19980707 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 766 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED C4 CHECK, FOUND CRACKED RT FUSELAGE SKIN AT BS 766 ABOVE S-19R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700665 19980717 00665 NM 1998 7 17 SWAA981290 1 19980707 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 297 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 297 WL 256 LBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700666 19980717 00666 NM 1998 7 17 SWAA981291 1 19980707 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 273.5 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 273.5, LBL 37, WL 168. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700667 19980717 00667 NM 1998 7 17 SWAA981292 1 19980707 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 500A+6 BELOW STR 20R, WL 182. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700668 19980717 00668 NM 1998 7 17 SWAA981293 1 19980707 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 945/963/962 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 851 TO 861, RBL 7.5-15, WL 157. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700669 19980717 00669 NM 1998 7 17 SWAA981294 1 19980707 A 5330 SKIN BOEING 737 737301 1384611 NM BS 457 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND GOUGED SKIN AT BS 457, 2 ABOVE STR 27 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700670 19980717 00670 NM 1998 7 17 SWAA981295 1 19980707 A 5320 ANGLE BOEING 737 737301 1384611 NM E/E COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND CRACKED E1-1 RACK, LEFT HAND SUPPORT ANGLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700671 19980717 00671 NM 1998 7 17 SWAA981296 1 19980707 A 5320 WEB BOEING 737 737301 1384611 NM BS 1006-1016 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND BS 1006 TO 1016, LBL 28, WL 208 AND BS 1006 TO 1016, LBL 18, WL 208 WITH ELONGATED H OLES ON SHEAR WEB. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700672 19980717 00672 NM 1998 7 17 SWAA981297 1 19980707 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 1006 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND FLOORBEAM AT BS 1006, LBL 16 AND 29 WITH ELONGATED HOLES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700673 19980717 00673 NM 1998 7 17 SWAA981298 1 19980707 A 5315 FLOORBEAM BOEING 737 737317 138447P NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 344 PANEL HOLE, LBL 28. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700674 19980717 00674 NM 1998 7 17 SWAA981299 1 19980707 A 5320 INTERCOSTAL BOEING 737 737317 138447P NM BS 927-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND C/L INTERCOSTAL HAS CRACKS AT SCREW HOLES BS 927 TO 947. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998071700675 19980717 00675 NM 1998 7 17 SWAA981300 1 19980707 A 5320 SPLICE BOEING 737 737317 138447P NM BS 490 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SPLICE AT BS 490, STR 27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700676 19980717 00676 NM 1998 7 17 SWAA981301 1 19980707 A 5320 SPLICE BOEING 737 737317 138447P NM BS 490 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SPLICE AT BS 470 TO 480, STR 27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700677 19980717 00677 NM 1998 7 17 SWAA981302 1 19980708 A 5320 INTERCOSTAL BOEING 737 737317 138447P NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED C/L INTERCOSTAL AT SCREW HOLES BS 380 TO 400. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998071700678 19980717 00678 NM 1998 7 17 SWAA981303 1 19980708 A 5330 SKIN BOEING 737 737317 138447P NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED SKIN AT BS 178, WL 198, RBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700679 19980717 00679 NM 1998 7 17 SWAA981304 1 19980708 A 5320 ANGLE BOEING 737 737317 138447P NM BS 294.5 MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND ANGLE MISSING AT FWD SERV DOOR POST FWD LOWER CORNER ATTACHED TO Z-ANGLE AT BS 294.5 , RBL 56. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700680 19980717 00680 NM 1998 7 17 SWAA981305 1 19980708 A 5312 BULKHEAD BOEING 737 737317 138447P NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED FWD SIDE OF BULKHD, RBL 5 WL 201 AND WL 201 LBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700681 19980717 00681 NM 1998 7 17 SWAA981306 1 19980708 A 5315 FLOORBEAM BOEING 737 737317 138447P NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 986 LBL 10.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700682 19980717 00682 NM 1998 7 17 SWAA981307 1 19980709 A 5330 SKIN BOEING 737 737317 138447P NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED SKIN AT BS 178 WL 188 LBL .5, WL 188 RBL .5 AND WL 198 RBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700683 19980717 00683 NM 1998 7 17 SWAA981308 1 19980709 A 2421 976J4981 GENERATOR BOEING 737 7372H4 138448C NM NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 052SW 21533 AIR TURNBACK DURING CLIMBOUT, MULTIPLE CIRCUIT BREAKERS POP (NO BAD GENERATOR INDICATIONS EXCEPT NO VOLTS/AMPS) TR1, BAT T CGR 1, LT AND RT FWD BOOST PUMPS POPPED RESET ONCE ALL REOCURRED RETURNED TO MCI AFTER 1 CB RESET. AIRCRAFT MADE AN U NEVENTFUL LANDING. REMOVED AND REPLACED NR 1 ENG GENERATOR PER BOEING MM, OPS CK GOOD. 2 L 7 2 4F A16WE 1998071700684 19980717 00684 NM 1998 7 17 SWAA981309 1 19980708 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 569 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED RT SKATE ANGLE AT BS 569, RBL 48 WL 173 AND LT SKATE ANGLE AT BS 569, LBL 48, WL 173. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700685 19980717 00685 NM 1998 7 17 SWAA981310 1 19980708 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 530 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CHAFED WEB AT BS 530 RBL 60 WL 164. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700686 19980717 00686 NM 1998 7 17 SWAA981311 1 19980708 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRAKCED AT BS 178 BULKHEAD, LBL 5.7, WL 198 TO 202, RBL 5.7, WL 198 TO 202 AND LBL 5.7, WL 212 TO 213. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700687 19980717 00687 NM 1998 7 17 SWAA981312 1 19980708 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD, LBL 10 TO 11, WL 215 AND RBL 8.75 TO 9.5 WL 215. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700688 19980717 00688 NM 1998 7 17 SWAA981313 1 19980708 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 12.5, WL 159. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998071700689 19980717 00689 NM 1998 7 17 SWAA981314 1 19980708 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED CARGO FLOORBEAM AT BS 727 TO 947, LBL 8 WL 159, RBL 3, WL 159 AND RBL 8, WL 159 . REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700690 19980717 00690 NM 1998 7 17 SWAA981315 1 19980708 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 787 TO 794, RBL 23, WL 158, BS 847 TO 867, RBL 23, WL 164, BS 500A TO 500B, RBL 25 WL 156, BS 500B TO 500C, RBL 25 WL 156 AND 500C-500D, RBL 25 WL 156. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998071700691 19980717 00691 NM 1998 7 17 SWAA981316 1 19980708 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND DENTED FLOOR PANEL SUPPORT ANGLE AT BS 727+8 LBL 5 WL 156. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998071700692 19980717 00692 NM 1998 7 17 SWAA981317 1 19980708 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21, RBL 21 WL 180. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700693 19980717 00693 NM 1998 7 17 SWAA981318 1 19980708 A 5320 TIE STRAP BOEING 737 7373H4 1384600 NM BS 774-857 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED VERTICAL SUPPORT WEB TIE STRAP AT BS 774 TO 857, RBL 19, WL 164. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700694 19980717 00694 NM 1998 7 17 SWAA981319 1 19980708 A 5320 DOORFRAME BOEING 737 7373H4 1384600 NM BS 849 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND GOUGED DOOR FRAME COVERPLATE AT BS 849, RBL 45, WL 174. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700695 19980717 00695 NM 1998 7 17 SWAA981320 1 19980708 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 807/827 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 807, LBL 42, WL 168 AND BS 827, LBL 20 WL 159. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998071700696 19980717 00696 NM 1998 7 17 SWAA981321 1 19980708 A 5321 FLOOR BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR WEB AT BS 178, LBL 25 TO 29 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700697 19980717 00697 NM 1998 7 17 SWAA981322 1 19980708 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 788 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED COVER PLATE SUPPORT WEB AT BS 788, RBL 37, WL 164. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700698 19980717 00698 NM 1998 7 17 SWAA981323 1 19980708 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 328, LBL 54, WL 182. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700699 19980717 00699 NM 1998 7 17 SWAA981324 1 19980708 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 1140-1143 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED LOWER CHORD BS 1140 TO 1143 STR 5 LT AND BS 1140 TO 1143, STR 5, RT. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700700 19980717 00700 NM 1998 7 17 SWAA981325 1 19980708 A 5320 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED AFT SERVICE DOOR HINGE CUTOUT, LWR CUTOUT FWD CRACK EXTENDED UNDER SKIN. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700701 19980717 00701 NM 1998 7 17 SWAA981326 1 19980708 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 380, STR 21L, WL 174. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700702 19980717 00702 NM 1998 7 17 SWAA981327 1 19980708 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD LBL 5.7, WL 200 TO 201. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700703 19980717 00703 NM 1998 7 17 SWAA981328 1 19980708 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 378SW 26585 DURING SCHEDULED C2 CHECK, FOUND CRACKED LT FLOORBEAM ROW 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700704 19980717 00704 NM 1998 7 17 SWAA981329 1 19980709 A 2560 GIRT BAR BOEING 737 7375H4 138449D NM DOOR SLIDE LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING WALKAROUND CHECK, FOUND RIGHT FWD EMERGENCY ESCAPE SLIDE RETENTION BAR PULLED LOOSE FROM VELCRO RETAINER. REINST ALLED SLIDE GIRT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998071700705 19980717 00705 NM 1998 7 17 SWAA981330 1 19980709 A 3350 20131A BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 376SW 26584 DURING SERVICE CHECK, FOUND MID LEFT EMERGENCY LIGHTING BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998071700706 19980717 00706 NM 1998 7 17 SWAA981331 1 19980713 A 2782 ACTUATOR BOEING 737 7372T4 1384492 NM NR 5 LE SLAT FAILED A SWAA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SW 07 721SW 22697 AFTER DEPARTURE CREW GOT INDICATIONS OF NR 5 SLAT ACTUATOR REMAINS EXTENDED, VISUALLY CONFIRMED. AIR TURNBACK TO NASHVI LLE. AIRCRAFT MADE AN UNEVENTFUL LANDING. REPLACED SLAT ACTUATOR PER BOEING MM. 2 L 7 2 4F A16WE 1998071700707 19980717 00707 NM 1998 7 17 SWAA981332 1 19980709 A 5320 STRAP BOEING 737 7372H4 138448C NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING 1/4 D-CHECK, FOUND STRAP ALONG WEBS AT AFT LOWER SIDE OF CARGO DOOR CUTOUT DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700708 19980717 00708 NM 1998 7 17 SWAA981333 1 19980709 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING WALKAROUND CHECK, FOUND CRACKED SKIN APPROX 3 RT SIDE FWD OF REAR BAG BELOW OTHER PATCH. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998071700709 19980717 00709 1998 7 17 SWAA981334 4 19980709 A 2565 D31591478 SLIDE BOEING 737 7373H4 1384600 NM PAX DOOR DEPLOYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING WALKAROUND CHECK, FOUND FORWARD ENTRY DOOR SLIDE DEPLOYED. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE ASSY PER B OEING MM. 2 L 7 2 4F RT A16WE 1998071700710 19980717 00710 NM 1998 7 17 SWAA981335 1 19980709 A 2420 CIRCUIT BREAKER BOEING 737 7373T5 NM NR 1 GCU FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 694SW 23061 DURING ENGINE START SMOKE STARTED COMING OUT OF THE CIRCUIT BREAKER PANEL IN THE VICINITY OF THE G1 GENERATOR CONTROL UN IT. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998071700711 19980717 00711 NM 1998 7 17 SWAA981336 1 19980709 A 5320 CHANNEL BOEING 737 737301 1384611 NM BS 986.5 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND HAT CHANNEL AT BS 986.5, WL 208 WITH ELONGATED HOLES LBL 22 TO 36. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998071700712 19980717 00712 NM 1998 7 17 SWAA981337 1 19980711 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED SKIN AT BS 178, LBL 5.5 WL 194. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998071700713 19980717 00713 NM 1998 7 17 SWAA981338 1 19980711 A 5512 SKIN BOEING 737 7373H4 1384600 NM RT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED RT HORIZONTAL STABILIZER, L/E SKIN AT FASTENER, STAB BS 66 TO 93 AND BS 84.93. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700714 19980717 00714 NM 1998 7 17 SWAA981339 1 19980711 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED TWO ANGLES AT BS 348 LBL 65 WL 216. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700715 19980717 00715 NM 1998 7 17 SWAA981340 1 19980711 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED FUSELAGE SKIN FWD SERVICE DOORWAY LOWER AFT CORNER AT BS 328 WL 211 RBL 67. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700716 19980717 00716 NM 1998 7 17 SWAA981341 1 19980711 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1031 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 1031, RBL 8 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700717 19980717 00717 NM 1998 7 17 SWAA981342 1 19980711 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB INTERCOSTAL AT BS 295, WL 216 LBL 56.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700718 19980717 00718 NM 1998 7 17 SWAA981343 1 19980711 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 294, WL 252, LBL 53. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700719 19980717 00719 NM 1998 7 17 SWAA981344 1 19980711 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 300 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE AT BS 300, WL 256, LBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700720 19980717 00720 NM 1998 7 17 SWAA981345 1 19980711 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 767 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 767 RBL 30 WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700721 19980717 00721 NM 1998 7 17 SWAA981346 1 19980711 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 787 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND GOUGED FRAME AT BS 787 RBL 25 WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700722 19980717 00722 NM 1998 7 17 SWAA981347 1 19980711 A 5311 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 787 BETWEEN STR 8 TO 9L, BS 827 BETWEEN STR 8 TO 9L, BS 867 BETWEEN STR 8 TO 9L AND BS 747 BETWEEN STR 8 TO 9L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700723 19980717 00723 NM 1998 7 17 SWAA981348 1 19980711 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 727/706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 727E, STR 16L AND BS 706, STR 11R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700724 19980717 00724 NM 1998 7 17 SWAA981349 1 19980711 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, RBL 8, BL 0, LBL 14, 21, 26, 33, 39, 46, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700725 19980717 00725 NM 1998 7 17 SWAA981350 1 19980711 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CORRODED Z-CHORD AT BS 270, BL 0, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700726 19980717 00726 NM 1998 7 17 SWAA981351 1 19980711 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 907/827/867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 907, BETWEEN STR 8 TO 9L, BS 827 BETWEEN STR 8 TO 9R AND BS 867, BET WEEN STR 8 TO 9R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700727 19980717 00727 NM 1998 7 17 SWAA981352 1 19980711 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 706, STR 11L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700728 19980717 00728 NM 1998 7 17 SWAA981353 1 19980711 A 5743 FITTING BOEING 737 7373H4 1384600 NM LT MLG CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D-CHECK, FOUND CRACKED UPPER I/B FASTENER HOLE COMMON TO THE MLG (LT) FITTING 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700729 19980717 00729 NM 1998 7 17 SWAA981354 1 19980710 A 5320 WEB BOEING 737 737317 138447P NM BS 360-380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND O/B WEB AT BS 360 TO 380, STR 17L IS BENT AND CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998071700730 19980717 00730 NM 1998 7 17 UPS98227164 1 19980714 A 3350 BATTERIES BOEING 727 72730C 1384009 NM FLIGHT DECK DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REPLACED WITH NEW BATTERIES, LIGHT OPS CHECKED OK. 2 L 7 3 4F A3WE 1998071700731 19980717 00731 NM 1998 7 17 UPS98227165 1 19980714 A 5712 6597104103 RIB BOEING 727 72730C 1384009 NM WS 6565 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CRACK INDICATION NOTED ON LT WING RIB AT WS 6565 STR 6 LOWER. REMOVED CRACKED RIB REPLACED WITH NEW RIB IAW EO B727-5710-1325D. 2 L 7 3 4F A3WE 1998071700732 19980717 00732 NM 1998 7 17 UPS98227166 1 19980714 A 5712 6597104104 RIB BOEING 727 72730C 1384009 NM WS 656.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CRACK INDICATION NOTED ON RT WING RIB AT WS 656.5 STR 6 LOWER. REPLACED CRACKED RIB WITH NEW RIB PE R EO B727-5710-1325. 2 L 7 3 4F A3WE 1998071700733 19980717 00733 NM 1998 7 17 UPS98227167 1 19980713 A 5313 STRINGER BOEING 727 72730C 1384009 NM BS 291 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-221-01.00-01) ON STR 1 AT STA 291. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW S RM 53-10-1. REMOVED DAMAGED AREA OF STRINGER AND FABRICATED REPAIR PARTS IAW SRM 53-10-3 SRM 53-10-4. 2 L 7 3 4F A3WE 1998071700734 19980717 00734 NM 1998 7 17 UPS98227168 1 19980710 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 760-850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 850 LBL 65 BL 208. REPLACED SEAT TRACK EXTRUSION BS 760 TO 850 LBL 65 WL 208 PER 727 SRM 51-30-2. ALSO, REFERENCE NRC 832521 REPLACED L-ANGLES PER SRM 51-20-1 AT BS 804. 2 L 7 3 4F A3WE 1998071700735 19980717 00735 NM 1998 7 17 UPS98227169 1 19980710 A 5320 ANGLE BOEING 727 72730C 1384009 NM BS 804 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, POSSIBLE CRACK IN FLOORBEAM SUPPORT ANGLE BS 804, LBL 46, WL 206. FLOORBEAM SUPPORT CRACKED, VERIF IED BY NDI. REPLACED SUPPORT ANGLE PER 727 SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1998071700736 19980717 00736 WP 1998 7 17 UPS98827156 1 19980628 A 5320 26499432 FITTING DOUG DC8 DC871F 302199D WP BS 154 L CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, FS 154 RT SIDE THE FRAME TO CUSP FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1- 20D AND DWG 2649943. 2 L 7 4 4F RT 4A25 1998071700737 19980717 00737 WP 1998 7 17 UPS98827157 1 19980630 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, LONGERON 35R AT FS 1270 IS CRACKED. REPAIRED IAW DHC SK 708-689. 2 L 7 4 4F RT 4A25 1998071700738 19980717 00738 WP 1998 7 17 UPS98827158 1 19980630 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, LONGERON 36 AT FS 1270 HAS 8 INCH CRACK. REPAIRED IAW DHC SK 708-690. 2 L 7 4 4F RT 4A25 1998071700739 19980717 00739 WP 1998 7 17 UPS98827159 1 19980701 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 25-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, SKIN DOUBLER HAS HEAVY CORROSION BEYOND LIMITS AT FS 25 TO 55 L-30R. REPAIRED IAW DHC SK 708-708. 2 L 7 4 4F RT 4A25 1998071700740 19980717 00740 WP 1998 7 17 UPS98827160 1 19980626 A 5720 5641253502 DOUBLER DOUG DC8 DC871F 302199D WP WS 347-385 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, RT WING L/E LWR SKIN INTERNAL DOUBLER WS XFS347.75 TO 354.0 AND 379.0 TO 385.25 HAS HEAVY EXFOLIATION CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW DWG NR 5641253 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998071700741 19980717 00741 WP 1998 7 17 UPS98827161 1 19980628 A 5313 3648667 LONGERON DOUG DC8 DC871F 302199D WP BS 35-55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, LONG 30R CORRODED FS 35 TO 55. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1- 21 AND DWG 3648667. 2 L 7 4 4F RT 4A25 1998071700742 19980717 00742 WP 1998 7 17 UPS98827162 1 19980626 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, LT WING UPPER SURFACE WS XRS 74 STR 15 SKIN IS CRACKED. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998071700743 19980717 00743 WP 1998 7 17 UPS98827163 1 19980627 A 5530 STRAP DOUG DC8 DC871F 302199D WP VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, MODERATE CORROSION ON THE LT SIDE OF THE VERTICAL STAB TO EMP BASE STRIP. REPAIRED IAW SRM 53-2-5. 2 L 7 4 4F RT 4A25 1998071700744 19980717 00744 EU 1998 7 17 QXEA9800842 1 19980604 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU LT WINDOW POST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 LEFTHAND WINDOW POST NR 2 LOWER CLIP CRACKED. REPAIRED IAW HORIZON AIR EO 4-53-06B. 2 L 7 2 4F RT A20EU 1998071700745 19980717 00745 EU 1998 7 17 QXEA9800843 1 19980609 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 3450 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 3450 STRINGER 42 FRAME CAP IS DENTED AND GOUGED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998071700746 19980717 00746 EU 1998 7 17 QXEA9800844 1 19980515 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 REPAIR ON BEAM VI FOR FORWARD PRESSURE BULKHEAD LOWER FLANGE IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-18. 2 L 7 2 4F RT A20EU 1998071700747 19980717 00747 EU 1998 7 17 QXEA9800845 1 19980528 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 3050 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CLIP IS CRACKED FRAME 3050 STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, FIG 2. 2 L 7 2 4F RT A20EU 1998071700748 19980717 00748 EU 1998 7 17 QXEA9800846 1 19980621 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 DENT IN FUSELAGE SKIN SIX INCHES FORWARD OF RIGHTHAND TAXI LIGHT, 1.25 WIDE AND .080 DEEP. REPAIRED IAW HORIZON AIR EA 4-53-478. 2 L 7 2 4F RT A20EU 1998071700749 19980717 00749 EU 1998 7 17 QXEA9800847 1 19980630 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 3200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 THREE DENTS VERTICALLY IN LEFTHAND FUSELAGE SKIN BETWEEN STRINGERS AT STATION 3200 MM FROM WL -100 TO -400 MM, TWO MEASU RE 5.0 WIDE X .060 DEEP AND THE THIRD 3.0 WIDE AND .040 DEEP. REPAIRED IAW HORIZON AIR EA 4-53-480. 2 L 7 2 4F RT A20EU 1998071700750 19980717 00750 EU 1998 7 17 QXEA9800848 1 19980629 A 5620 WINDOW FOKKER F28 F28MK4000 4990810 EU RIGHT NOT SEALED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 NR 2 RIGHTHAND WINDOW POST REQUIRES INSIDE REBATE AND OUTSIDE SEALANT. REMOVED AS REQUIRED SEALANT AND REBATE. APPLIED FLUSH EPOXY TO NR 2 RIGHTHAND WINDOW. 2 L 7 2 4F RT A20EU 1998071700751 19980717 00751 EU 1998 7 17 QXEA9800849 1 19980602 A 5720 ANGLE FOKKER F28 F28MK4000 4990810 EU LT MLG CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 UPPER ATTACH ANGLE FOR LEFTHAND MAIN LANDING GEAR BACK-UP STRUCTURE CRACKED AT LOWER BOLT HOLE. REPAIRED IAW FOKKER SRM 57-02-09, PAGE 2, PARAGRAPH 3, FIGURE 5. 2 L 7 2 4F RT A20EU 1998071700752 19980717 00752 EU 1998 7 17 QXEA9800850 1 19980520 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 REAR PRESSURE BULKHEAD BEAM I HAS STOP DRILLED CRACK BL 80L BOTTOM SIDE. REPAIRED IAW FOKKER SRM 53-02-18. 2 L 7 2 4F RT A20EU 1998071700753 19980717 00753 EU 1998 7 17 QXEA9800851 1 19980516 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 REAR PRESSURE BULKHEAD BEAM II RADIUS IS CRACKED BL 125R AND BL 225R. REPAIRED IAW FOKKER SRM 53-02-18, PAGES 30 TO 35. 2 L 7 2 4F RT A20EU 1998071700754 19980717 00754 EU 1998 7 17 QXEA9800942 1 19980710 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 EMERGENCY EXIT SIGN IN MID CABIN HAS SEVERAL 28V BULBS OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998071700755 19980717 00755 NM 1998 7 17 QXEA9800943 1 19980713 A 3350 6104789 BATTERY DHAV 82410191011 DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 815PH 50 FORWARD RIGHT EMERGENCY EXIT LAMP INOP. REPLACED EMERGENCY BATTERY, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998071700756 19980717 00756 NM 1998 7 17 QXEA9800944 1 19980710 A 3350 10126267 SIGN DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 827PH 275 EMERGENCY EXIT SIGN AT ROW 4AB BROKEN. REPLACED EMERGENCY EXIT SIGN, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998071700757 19980717 00757 NM 1998 7 17 QXEA9800945 1 19980712 A 3350 10126267 SIGN DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 830PH 314 EMERGENCY EXIT SIGN NEXT TO SEAT 4E BROKEN. REPLACED SIGN, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998071700758 19980717 00758 EU 1998 7 17 QXEA9800946 1 19980710 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 EXIT SIGN AT ROW 8 OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998071700759 19980717 00759 EU 1998 7 17 QXEA9800947 1 19980406 A 3310 LENS FOKKER F28 F28MK4000 4990810 EU GLARESHIELD OUT OF POSITION A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 487US 11238 AFTER TAKEOFF, A STRONG SMELL OF BURNING INSULATION AND WHITE SMOKE FLOWING FROM GLARESHIELD AREA. ACCOMPLISHED EMERGEN CY CHECK LIST AND ISOLATED AC BUS NR 2 AND SMOKE DID NOT REOCCUR. RETURNED TO FIELD. MAINTENANCE INSPECTED AND FOUND T HE LEFT RDS PANEL LIGHTING PLASTIC LENS MELTED. DEACTIVATED LIGHT AND PLACED ON MEL, REFERENCE MEL 33-1. THE MEL WAS C LEARED BY REPLACING THE DATA SELECTOR PANEL DUE TO INOPERATIVE BACK LIGHTING. COMPLIED WITH CAT 2 FUNCTIONAL TEST. NO DEFECTS NOTED. 2 L 7 2 4F RT A20EU 1998071700760 19980717 00760 EU 1998 7 17 QXEA9800948 1 19980713 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 AFT EMERGENCY OVERHEAD LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND OPERATIONALLY TEST ED GOOD. 2 L 7 2 4F RT A20EU 1998071700761 19980717 00761 WP 1998 7 17 98FDEA00455 1 19980712 A 2120 FLEX DUCT DOUG DC10 DC1030F 3023504 WP NR 1 PACK TORN A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 311FE 46871 STA-ORD - UNABLE TO CONTROL CABIN PRESS IN ANY MODE. CABIN ALT CLIMB AT RATE EXCEED AUTO-SCHEDULE AND AT LEVEL OFF CONT INUE TO CLIMB AT 300 TO 400 FPM. UNABLE TO GAIN CONTROL USING STBY PRESS OR MANUAL PRESS PER RED TABS. CABIN ALT EXCEE D 10000 AND EMERGENCY PROC ACCOMPLISHED AND DESCENT AND DIVERT TO ORD. FOUND NR 1 PACK OUTPUT DUCT APART AT FLEX DUCT. ALSO, FOUND FLEX DUCT TORN. REPLACED FLEX DUCT, LEAK CHECKED GOOD. PRESSURIZED A/C. HELD PRESS UP TO 2.0 PSID. IPC REF 21-54-01-01 SHEET 4 ITEM 563 P/N DUO1006-28-20. 2 L 7 3 4F RT A22WE 1998071700762 19980717 00762 WP 1998 7 17 ABXA9800617 1 19980714 A 5315 991556175 FLOORBEAM DOUG DOUG DC9 DC915 3022036 WP BS 817 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK FOUND STATION 817 FLOORBEAM WEB CORRODED. REPLACED WEB IAW DC9 SRM 51-10-2 AND 51-10-5. 2 L 7 2 4F A6WE 1998071700763 19980717 00763 WP 1998 7 17 ABXA9800618 1 19980714 A 5320 991556123 DOUBLER DOUG DOUG DC9 DC915 3022036 WP BS 817 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK, FOUND STATION 817 FLOORBEAM WEB DOUBLER CORRODED. INSTALLED WEB DOUBLER IAW DACO DWG NR 9 915561. 2 L 7 2 4F A6WE 1998071700764 19980717 00764 WP 1998 7 17 ABXA9800619 1 19980714 A 5720 5910003411 SHIELD DOUG DOUG DC9 DC915 3022036 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK FOUND A CRACKED HEAT SHIELD IN THE RIGHT WING NR 1 LEADING EDGE SECTION. REPAIRED IAW ABX REA NR D957-24148. 2 L 7 2 4F A6WE 1998071700765 19980717 00765 WP 1998 7 17 ABXA9800620 1 19980714 A 5330 59560651 PANEL DOUG DOUG DC9 DC915 3022036 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C-CHECK, FOUND LEFT SLANT PANEL CORRODED. REPAIRED IAW DACO DWG 5956065, ABX DWG NR 4255 AND DC9 S RM 51-30-2. 2 L 7 2 4F A6WE 1998071700766 19980717 00766 WP 1998 7 17 ABXA9800621 1 19980713 A 5320 S1245835 CAP DOUG DOUG DC9 DC941 302207N WP BS 80 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND CRACK IN LOWER LEG OF THE LEFT CAP IN THE NOSE WHEEL WELL AT STATION 80, BL 12. REPAIRED IAW ABX REA D953-24098 MR. 2 L 7 2 4F A6WE 1998071700767 19980717 00767 WP 1998 7 17 ABXA9800622 1 19980713 A 5320 995823870N SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND CRACK FUSELAGE STATION 1056 BELOW LONGERON 14 IN SHEAR TIE. REPLACED SHEAR TIE IAW DC9 SRM 51-30- 5. 2 L 7 2 4F A6WE 1998071700768 19980717 00768 WP 1998 7 17 ABXA9800623 1 19980713 A 5320 575468828 DOUBLER DOUG DOUG DC9 DC941 302207N WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND CRACK IN DOUBLER (P/N 5754688-28) AT UPPER AFT CORNER OF SLIDING WINDOW. REPLACED DOUBLER (P/N 57 54688-28) IAW SRM 51-10-3, 51-30-1, 51-20-0 AND 51-30-5. 2 L 7 2 4F A6WE 1998071700769 19980717 00769 WP 1998 7 17 ABXA9800624 1 19980713 A 5312 9915558153 BULKHEAD FORMER DOUG DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND CRACK AFT PRESSURE DOME END FORMER AT LONGERON 12 LT. REPAIRED IAW DC9 SERVICE DRAWING J060110 AN D 51-30-5. 2 L 7 2 4F A6WE 1998071700770 19980717 00770 WP 1998 7 17 ABXA9800625 1 19980713 A 5320 CUSP DOUG DOUG DC9 DC941 302207N WP BS 636 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND CUSP WEB CRACKED AT FS STATION 636 RIGHT RBL 54, LONGERON 18. REPLACED CUSP WEB IAW DC9 SRM 51-30 -1 AND 51-30-2. 2 L 7 2 4F A6WE 1998071700771 19980717 00771 WP 1998 7 17 ABXA9800626 1 19980714 A 5320 CUSP DOUG DOUG DC9 DC941 302207N WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND CUSP WEB CRACKED AT RBL 56 FS 945. REPAIRED CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998071700772 19980717 00772 WP 1998 7 17 ABXA9800627 1 19980713 A 5311 99115205 FRAME DOUG DOUG DC9 DC941 302207N WP CARGO COMPT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND FRAME 218 AT LONGERON 5 RT CRACKED. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998071700773 19980717 00773 WP 1998 7 17 ABXA9800628 1 19980714 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 817AX 45928 EMERGENCY LIGHTS WOULD NOT ILLUMINATE AFTER POWER LOSS. REPLACED EMERGENCY POWER PACK IAW DC8 MM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998071700774 19980717 00774 WP 1998 7 17 MWEA98785 1 19980713 A 2560 59129037 COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 212ME 47701 THE GALLEY DOOR SLIDE FELL OFF. MTC REINSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998071700775 19980717 00775 WP 1998 7 17 MWEA98786 1 19980714 A 5230 59101419 PAN DOUG DC9 DC914 3022034 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 THE FORWARD CARGO DOOR INNER DOOR PAN AT THE AFT TORGUE TUBE AREA HAS A CRACK IN RADIUS. MTC FABRICATED AND INSTALLED D OUBLER REPAIR. 2 L 7 2 4F A6WE 1998071700776 19980717 00776 WP 1998 7 17 MWEA98787 1 19980714 A 5230 591015775 SKIN DOUG DC9 DC914 3022034 WP CARGO DOOR OUT OF LIMITS A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FOUND A RUB MARK OUT OF LIMITS ON AFT CARGO DOOR OUTER SKIN. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998071700777 19980717 00777 WP 1998 7 17 DHL98805001 1 19980704 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1680 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 SKIN CORROSION LEFT AND RIGHT SIDE OF FUSELAGE AT STA 1680 AT LONGERON NR 30. ACCOMPLISHED DOUBLER REPAIR AT LEFT SIDE . CLEANED RIGHT SIDE, WITHIN LIMITS, PER SRM 51-8-1 AND 53-2-1. 2 L 7 4 4F RT 4A25 1998071700778 19980717 00778 NM 1998 7 17 VNAA9807005 1 19980714 A 3010 001B574A000001 DEICE BOOT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WING WORN A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 460PS 3061 THE RIGHT HAND WING SURFACE DE-ICE SYSTEM FAILED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DEFERRED THE SURFACE DE-ICE SYSTEM PER THE MINUMUM EQUIPMENT LIST, AND THE AIRCRAFT WAS RETURNED TO SERVICE . ON 15 JULY 98, MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND LEADING EDGE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 57-40-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE DEFERRAL WAS REMOVED FROM THE AIRCRAFT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998072200001 19980722 00001 NM 1998 7 22 P5CA9801141 1 19980625 A 5320 STRUCTURE BOEING 747 747283B 1384867 NM CARGO DOORWAY DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 A/C EXPERIENCED GROUND DAMAGE AT FWD EDGE AFT CARGO DOOR CUTOUT. DAMAGE EXTENDED INTO SKIN, INTERNAL BEAR STRAP, STA 18 00 AND STA 1810 FRAME AND STRINGER 31R AND 32R. REPAIRED IAW POLAR AIR CARGO MA 5310-26:02. 2 L 7 4 4F A20WE 1998072200002 19980722 00002 1998 7 22 ARWA980702 4 19980706 A 3417 2593200951 ADC LKHEED 1011 1011385115 5265015 WP E/E BAY MALFUNCTIONED A ARWA K NONE O OTHER TO TAKEOFF 1 SO 19 308GB 210098 193U1133 BDL - FLT 505 - ON TAKEOFF ROLL, CAPTAIN'S AIRSPEED FAILED WITH NR 1 MACH FEEL, NR 1 ATS, NR 1 MASK TRIM FAIL WITH NUMER OUS FLAGS. REMOVED AND REPLACED A.D.C., GROUND CHECKED, AND OPERATIONAL NORMAL IAW MM 34-14-00. (X) 2 L 7 3 4F A23WE 1998072200006 19980722 00006 NM 1998 7 22 UPS98427146 1 19980712 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 21944 INSPECTION TYPE-N/A, UPPER DECK AFT TWO EMERGENCY LIGHTS INOP. REMOVED AND REPLACED UPPER DECK AFT EMERGENCY LIGHT BATT ERY PACK PER B747 M/M 33-51-04 AT STA 650 M335 POWER SUPPLY. 2 L 7 4 4F A20WE 1998072200007 19980722 00007 1998 7 22 DHL98707002 2 19980714 A 7261 OIL SYST BOEING 727 72722 1384002 NM NR 2 ENGINE REQD SERVICE A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 707DH 18321 LOST OIL QUANTITY ON CLIMBOUT FROM NR 2 ENGINE FROM 3.8 GAL TO 2.2 GAL. OIL TEMP WAS 119 DEGREES AND DROPPED TO 105 DE GREES. SERVICED NR 2 ENGINE WITH 7 QTS OF OIL PER MM 12-13-1, RESECURED CAP. 2 L 7 3 4F A3WE 1998072200008 19980722 00008 EA 1998 7 22 COMA9860176 1 19980713 A 3350 OL3071BPEGPL LAMP CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 983CA 7169 LOW PRESSURE WARNING, HYDRAULIC SYSTEM NR 1. REPLACED LEAKING LINE ASSY IN AFT EQUIPMENT BAY. 2 L 7 2 4F RT A21EA 1998072400001 19980724 00001 NM 1998 7 24 ORJA98107 1 19980529 A 3350 1001191 LIGHT DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 901RA 53489 EMERGENCY FLOOR TRACK LIGHT AT ROW 2 IS INOPERABLE. REMOVED AND REPLACED 2 EMERGENCY PATH LIGHT ASSEMBLIES. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1998072400002 19980724 00002 NM 1998 7 24 ORJA9899 1 19980523 A 7711 EPR DOUG MD90 MD9030 3023690 NM NR 1 ENGINE MALFUNCTIONED A ORJA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 WP 11 903RA 53551 GATE RETURN DUE TO NR 1 EPR ROLLBACK TO 1.3 EPR. ABORT AT 80 KNOTS. MAXIMUM BRAKE TEMPERATURE, 320 DEGREES. INTERROGA TED MCDU, NOTED NO FAULTS. PERFORMED 2 FULL POWER RUN-UPS. OPS NORMAL. VISUALLY INSPECTED AIR INLET AND FAN AREA. CHE CKS OK. (X) 2 L 7 2 4F RT A6WE 1998072400003 19980724 00003 NM 1998 7 24 98ZZZX2392 1 19980525 A 3222 TORSION LINK BOEING 737 737222 1384473 NM NLG BROKEN A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CE 05 208AU 19547 TAKEOFF ABORTED. NO EMERGENCY DECLARED. ON INITIAL TAKEOFF ROLL, ENCOUNTERED NOSE WHEEL SHIMMY, ABORTED TAKEOFF. AIRC RAFT STOPPED AND WAS UNABLE TO TAXI BACK TO GATE DUE TO STEERING PROBLEM. AIRCRAFT TOWED BACK TO GATE. FOUND LOWER TOR SION LINK BROKEN. 2 L 7 2 4F A16WE 1998072400004 19980724 00004 EU 1998 7 24 SIMA981461 1 19980526 A 6120 7901996 ACTUATOR HAMSTD SAAB SF340 340B 7860101 EU LT PROPELLER WORN A SIMA K NONE O OTHER CL CLIMB 1 SW 21 235AE 5644 4333 951116 340B235 JFK - FLT 9852 - LEFT PROPELLER RPM SURGES. INSPECTED PROPELLER ACTUATOR. FOUND ABNORMAL WEAR. REPLACED LEFT PROP ACT UATOR. PERFORMED OPERATION CHECK SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES: 5,309. (X) 2 L 7 2 4T RT A52EU 1998072400005 19980724 00005 WP 1998 7 24 EIAA980175 1 19980318 A 5313 STRINGER DOUG DC9 DC933F 302207A WP BS 963 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 DURING 'C5' CHECK, LONGERON 16L CRACKED AT BS 963. REPAIRED LONGERON AT BS 963 PER SRM 53-02 FIG 18. (X) 2 L 7 2 4F A6WE 1998072400006 19980724 00006 WP 1998 7 24 EIAA980174 1 19980424 A 5320 SHEAR TIE DOUG DC9 DC933F 302207A WP BS 237 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 DURING 'C5' CHECK, FRAME SHEAR TIE CRACKED AT BS 237 BETWEEN STR 27R AND STR 28R. REPLACED SHEAR TIE PER SRM 51-10-03. (X) 2 L 7 2 4F A6WE 1998072400007 19980724 00007 WP 1998 7 24 EIAA980202 1 19980509 A 5320 PRESS PANEL DOUG DC9 DC933F 302207A WP BS 83 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 944F 48358 47194 DURING 'C5' CHECK, NOSE WHEEL WELL, LT TUNNEL AT BS 83, SIX INCHES INBD OF LT SIDEWALL (LBL 37.00). WHEEL WELL PRESSURE DECK CRACKED AT FRAME FOOT. REPAIRED PRESSURE DECK PER ECRA 944-53-037-2. (X) 2 L 7 2 4F A6WE 1998072400008 19980724 00008 NM 1998 7 24 USAASB98137 1 19980603 A 2150 22051701 ACM BOEING 737 7374B7 1384702 NM LT A/C BAY FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 430US 25404 24552 MIA - FLT 1431 - UPON CLIMB-OUT FROM MIA, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT. AFTER SEVERAL ATTEMPTS TO PRESSURIZE AIRCRAFT FAILED, CREW DECIDED TO RETURN TO FIELD AT MIA. FLIGHT LANDED WITHOUT FURTHER INCIDENT, AND NO EMERGENCY BEING DECLARED. MAINTENANCE FOUND THE LEFT AIR CYCLE MACHINE FROZEN (NO AIRFLOW). REMOVED AND REPLACED THE LEFT AIR CYCLE M ACHINE PER MM. OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4F RT A16WE 1998072400009 19980724 00009 NM 1998 7 24 USAASB98138 1 19980603 A 2150 32194211 SHUTOFF VALVE BOEING 737 7372B7 1384560 NM RT A/C BAY FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 277AU 48234 30872 22889 DAY - FLT 317 - CAPTAIN REPORTED A LOUD BANG/NOISE AT 3,000 FEET ON CLIMB-OUT OF DAY. FLIGHT ATTENDANTS FELT A VIBRATIO N IN THE FLOOR ALSO. CAPTAIN DID NOT NOTICE ANY CHANGE IN FLIGHT CONTROLS OR PRESSURIZATION. FLIGHT RETURNED TO FIELD AT DAY AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT PACK WATER SEPARATO R ICING UP. DISCONNECTED 35 DEGREE SENSOR AND FOUND VALVE WOULD NOT MOVE. RECONNECTED 35 DEGREE SENSOR AFTER THAWING O UT SYSTEM AND EVERYTHING OPS CHECKED GOOD. (X) 2 L 7 2 4F A16WE 1998072400010 19980724 00010 NM 1998 7 24 USAASB98143 1 19980607 A 3260 6552811109 ACCESSORY UNIT BOEING 737 737201 1384454 NM E/E COMPARTMENT FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 234US 41233 22274 BUF - FLT 461 - AFTER TAKEOFF FROM BUF, LANDING GEAR FAILED TO RETRACT. FLIGHT RETURNED TO FIELD AT BUF AND LANDED WITH OUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT. OPERATIONA L CHECK GOOD. PERFORMED REQUIRED CHECKS PER MM 32-09. OPS CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998072400011 19980724 00011 WP 1998 7 24 USAAD98098 1 19980530 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 974VJ 47130 IND - THE MAIN ENTRY DOOR EMERGENCY LIGHT AND THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE E MERGENCY LIGHT BATTERIES. REF: OPERATOR CONTROL NR 98ZZZX2393. (X) 2 L 7 2 4F A6WE 1998072400012 19980724 00012 WP 1998 7 24 98ZZZX2393 1 19980530 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 974VJ 47130 IND - THE MAIN ENTRY DOOR EMERGENCY LIGHT AND THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE E MERGENCY LIGHT BATTERIES. REF: OPERATOR CONTROL NR USAAD98098. 2 L 7 2 4F A6WE 1998072400013 19980724 00013 WP 1998 7 24 USAAD98099 1 19980530 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 963VJ 47508 IND - THE FORWARD CEILING EEMRGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (X) 2 L 7 2 4F A6WE 1998072400014 19980724 00014 WP 1998 7 24 USAAD98102 1 19980606 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 819US 48099 PIT - FOUND SEAT MOUNTED AISLE EMERGENCY LIGHT INOPERATIVE AT SEAT 16D. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F A6WE 1998072400015 19980724 00015 WP 1998 7 24 USAAD98101 1 19980603 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925VJ 48145 DTW - THE GALLEY AREA OVERHEAD EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE GALLEY AREA OVERHEAD EMERGENCY LIGHT BATTERIES. (X) 2 L 7 2 4F A6WE 1998072400016 19980724 00016 NM 1998 7 24 USAABB98049 1 19980407 A 2560 416T22311 SPRING BOEING 767 767201 1385125 NM GIRT BAR LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 CLT - DURING HEAVY MAINTENANCE C-CHECK, THE FORWARD SERVICE DOOR SLIDE WAS ACTUATED FOR AN ANNUAL CHECK. THE DOOR DID N OT OPEN FULLY THEREBY CAUSING THE SLIDE NOT TO AUTO-DEPLOY. THE SLIDE DID FUNCTION NORMALLY WHEN ACTIVATED MANUALLY. M AINTENANCE FOUND THE SEPARATION LINK INTERNAL SPRING WAS NOT SECURE. THE SPRING WAS REINSTALLED. (X) 2 L 7 2 4F RT A1NM 1998072400018 19980724 00018 NM 1998 7 24 USAA980227 1 19980522 A 5320 146N52421 SUPPORT BOEING 757 757225 1384959 NM BS 1640-1661 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 41850 22203 CLT - DURING A C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOOR SUPPORT CHANNEL 1 INCH BY 21 INCH BL ZERO BETWEEN S TA 1640 TO STA 1661. CORROSION TASK CARD NR C53-251-03. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (X) 2 L 7 2 4F RT A2NM 1998072400019 19980724 00019 NM 1998 7 24 USAASB98144 1 19980608 A 3350 20121 CHARGER BOEING 737 7374B7 1384702 NM CABIN DEFECTIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 779AU 24996 ORD - MAINTEANCE FOUND A SECTION OF LOW LEVEL EMERGENCY LIGHTS INOPERABLE AND THE AFT RIGHT OVERWING EXIT LIGHT INOPERAB LE. MAINTENANCE FOUND THE M1479 CHARGER ASSY AT STA 598R DEFECTIVE AND THE FUSE BLOWN. REPLACED CHARGER ASSY. OPERATI ONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998072400020 19980724 00020 NM 1998 7 24 USAA980229 1 19980522 A 5320 146N52421 SUPPORT BOEING 757 757225 1384959 NM BS 1661-1681 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 41850 22203 CLT - DURING A C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT CHANNEL 1 INCH BY 20 INCHES AT BL ZERO BETWEEN STA 1661 AND STA 1681. CORROSION TASK NR C53-251-03. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (X) 2 L 7 2 4F RT A2NM 1998072400021 19980724 00021 NM 1998 7 24 USAA980231 1 19980522 A 5315 146N509012 FLOORBEAM BOEING 757 757225 1384959 NM BS 1661 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 41850 22203 CLT - DURING A C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM AT CLIP NUT HOLES STA 1661 FROM BL ZERO TO LBBL 55.0. CORROSION TASK CARD NR C53-251-03. PARTIAL T-CAP REPLACEMENT FROM LBL 25 TO LBL 64. INSTALLED REPLACEMENT CHOR D/REPAIR ANGLES PER SRM 53-00-51. (X) 2 L 7 2 4F RT A2NM 1998072400022 19980724 00022 NM 1998 7 24 USAA980228 1 19980522 A 5315 146N508911 FLOORBEAM BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 41850 22203 CLT - DURING A C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON THE UPPER FLANGE OF FLOORBEAM STA 1640 FROM BL ZERO TO RB L 57-0. CORROSION TASK NR C53-251-03. INSTALLED REPAIR T-CAP AND SPLICE PER REPAIR DOCUMENT T/R 53-15-01. (X) 2 L 7 2 4F RT A2NM 1998072400023 19980724 00023 WP 1998 7 24 USAA980240 1 19980530 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 750-769 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 816US 39374 48096 PIT - DURING UNSCHEDULED MAINTENANCE FOUND 2 CRACKS, ONE CRACK .25 INCH LONG, AND ONE CRACK .1250 INCH LONG ON FUSELAGE SKIN BETWEEN STA 750 TO STA 769 LONGERON 30 TO LONGERON 29R. INSTALLED EXTERNAL DOUBLERS PER EA 49811 AND SRM 53-05 FIG 44. (X) 2 L 7 2 4F A6WE 1998072400024 19980724 00024 NM 1998 7 24 USAABB98058 1 19980601 A 5610 141T480119 WINDOW BOEING 757 7572B7 1384964 NM COCKPIT SHORTED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 619AU 27198 LIT/MEM- FLIGHTS 55/8081 - EN ROUTE CLT/SFO (FLT 55), AT FL 350, CREW EXPERIENCED AN ODOR LIKE THAT OF BURNING RUBBER. T HE ODOR WAS PREVALENT IN BOTH THE COCKPIT AND CABIN. CREW ISOLATED EACH PACK, BUT COULD NOT DETERMINE THE SOURCE OF THE ODOR. NO ABNORMAL COCKPIT INDICATIONS WERE EVIDENT. FLIGHT DIVERTED TO LIT AND LANDED WITH NO FURTHER INCIDENT. MAI NTENANCE IN LIT PLACED THE RECIRCULATION FAN ON MEL. ON THE SUBSEQUENT FERRY FLIGHT TO PHL, THE CREW EXPERIENCED THE SA ME ODOR. THE FLIGHT DIVERTED TO MEM AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE CAUSE OF THE SMOKE AND FUMES WERE DUE TO THE L1 WINDOW ARCING AND BURNING. THE WINDOW AND HEAT CONTROLLER WERE REPLACED. (X) 2 L 7 2 4F RT A2NM 1998072400025 19980724 00025 NM 1998 7 24 USAABB98059 1 19980602 A 3610 16J081 DUCT BOEING 757 7572B7 1384964 NM LT ENGINE RUPTURED A USAA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 624AU 27245 PIT - FLT 8876 - CLIMBING OUT OF PIT, CREW RECEIVED THE EICAS MESSAGE 'L ENG OVHT'. CREW REDUCED POWER AND THE MESSAGE EXTINGUISHED. THE MESSAGE REAPPEARED WITH POWER APPLICATION. THE BLEED SYSTEM HAD NO EFFECT ON THE MESSAGE. CREW REDU CED LEFT ENGINE POWER TO IDLE. FLIGHT RETURNED TO PIT, AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A BLO WN HIGH PRESSURE DUCT (HP6). (X) 2 L 7 2 4F RT A2NM 1998072400026 19980724 00026 NM 1998 7 24 USAABB98056 1 19980510 A 2530 2510000704 OVEN BOEING 757 7572B7 1384964 NM CABIN OVERHEATED A USAA O OTHER A FLAME/FIRE CR CRUISE 1 EA 19 631AU 27809 PIT - FLT 119 - CREW REPORTED THE FOIL LINED LID ON ONE OF THE MEALS IN THE INBOARD FIRST CLASS GALLEY OVEN IGNITED. CR EW PUT OUT THE FIRE (DID NOT USE EXTINGUISHER). MAINTENANCE REPLACED THE OVEN FOR OVERHEATING. (X) 2 L 7 2 4F RT A2NM 1998072400027 19980724 00027 WP 1998 7 24 USAAD98073 1 19980427 A 2150 DUCT DOUG DC9 DC981 3022081 WP LT A/C BAY LOOSE A USAA A B UNSCHED LANDING EMER. DESCENT O OTHER CR CRUISE 1 EA 19 812US 48092 RDU - FLT 888 - EN ROUTE PBI/PHL, AT FL 330 OVER FL0, CREW REPORTED THEY LOST PRESSURIZATION. OXYGEN MASKS DEPLOYED. F LIGHT DESCENDED IN ALTITUDE, DIVERTED TO RDU AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE RUBBER DUCTS AT THE LEFT AIR CYCLE MACHINE DISCONNECTED. REPLACED THE RUBBER DUCTS AND CLAMPS. ALSO, THE SAME DUCT FOR THE RIGHT AIR CYCLE MACHINE WAS REPLACED. (X) 2 L 7 2 4F A6WE 1998072400028 19980724 00028 NE 1998 7 24 USAAD98072 2 19980426 A 7261 2124502 FILTER DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE RT ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 806US 48038 MCO - FLT 1445 - EN ROUTE CLT/ MIA, CREW RECEIVED THE RIGHT ENGINE OIL CLOG LIGHT. CREW REDUCED POWER TO IDLE AND THE L IGHT REMAINED ILLUMINATED. FLIGHT DIVERTED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE OIL FILTE R PAPERS WERE SEPARATING AND REPLACED THE FILTER. (X) 2 L 7 2 4F 4 F A6WE E9NE 1998072400029 19980724 00029 WP 1998 7 24 ORJA98108 1 19980530 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 823RA 49889 EMERGENCY PATH LIGHT INOPERABLE AT ROWS 11, 19, 20. FOUND LOOSE CONNECTORS, SECURED CONNECTORS. OPS CHECKS GOOD. (X) 2 L 7 2 4F A6WE 1998072400030 19980724 00030 NM 1998 7 24 MASA98115 1 19980527 A 5542 85540021 COVER PLATE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 437YV 437 DUE TO THE OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE. A/C'S RUDDER WAS IN SPECTED WHILE THE A/C WAS INSPECTED DURING THE NORMAL FLIGHT SCHEDULE IN DEN BY A MECHANIC DISPATCHED OUT OF THE PRIMARY MAINTENANCE FACILITY. THE FWD RUDDER LOWER RIB END CAP ACCESS PANEL COVER PLATE WAS NOTED TO HAVE SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCESS PANEL COVER PLATE AND THE RIB END CAP HAD SEVERAL CRACKS. THE AIRCRAFT WAS FERRIED TO GR AND JUNCTION WHERE THE FORE AND AFT RUDDERS WERE REMOVED. A NEW ACCESS PANEL COVER PLATE WAS FABRICATED AND INSTALLED A ND THE RIB END CAP WAS REPLACED IAW RO NR DHC82-55-0001-GJT. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETURNED 2 H 7 2 4T RT A13NM 1998072400031 19980724 00031 NM 1998 7 24 MASA98113 1 19980527 A 5542 85540021 COVER PLATE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 454YV 454 DEN LINE MX PERSONNEL WERE REPLACING A TAIL NAV BULB WHEN THEY NOTICED A PIECE OF THE FORE RUDDER HANGING DOWN ON THE TA ILCONE OF THE AIRCRAFT. FURTHER INSPECTION, FOUND THE FORE RUDDER LOWER RIB END CAP HAD SEVERAL CRACKS AND THE ACCESS P ANEL COVER PLATE HAS ALMOST ALL OF THE ATTACHING RIVETS PULLED THROUGH. ALLOWING THE COVER PLATE TO HANG DOWN ON THE TA ILCONE OF THE AIRCRAFT. THE AIRCRAFT WAS FERRIED TO GJT, WHERE THE FORE AND AFT RUDDERS WERE REMOVED. A NEW ACCESS PAN EL COVER PLATE FABRICATED AND INSTALLED AND THE RIB END CAP WAS REPLACED IAW RO NR DHC82-55-0001 GJT. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998072400032 19980724 00032 NM 1998 7 24 MASA98114 1 19980527 A 5542 85540021 COVER PLATE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 456YV 3164 456 DUE TO OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LWR RIB END CAP AND/OR COVER PLATE DAMAGE. THE A/C RUDDER WAS INSPEC TED WHILE THE A/C WAS SITTING AS A SPARE AT THE MX FACILITY. THE FWD RUDDER LWR RIB END CAP ACCESS PNL COVER PLATE P/N 85540021 WAS NOTED TO HAVE SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCESS PANEL COVER PLATE. FABRICATED AND INSTALL ED AND THE RIB END CAP WAS REPLACED IAW RO NR DHC82-55-0001-GJT. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998072400033 19980724 00033 NM 1998 7 24 MASA98116 1 19980527 A 5542 85540021 COVER PLATE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 444YV 444 DUE TO OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE. A/C'S RUDDER WAS INSPEC TED DURING ROUTINE MAINTENANCE. THE FORWARD RUDDER LOWER RIB END CAP ACCESS PANEL COVER PLATE P/N 85540021 WAS NOTED TO HAVE SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCESS PANEL COVER PLATE. THE FORE AND AFT RUDDERS WERE REMOVED. A N EW ACCESS PANEL COVER PLATE WAS FABRICATED AND INSTALLED. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998072400034 19980724 00034 NM 1998 7 24 MASA98117 1 19980527 A 5542 85540021 COVER PLATE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 446YV 446 DUE TO OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE, A/C'S RUDDER WAS INSPECT ED WHILE THE AIRCRAFT WAS INSPECTED DURING ROUTINE MAINTENANCE. THE FORWARD RUDDER LOWER RIB END CAP ACCESS PANEL COVER PLATE WAS NOTED TO HAVE SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCESS PANEL COVER PLATE AND THE RIB END CAP HAD SE VERAL CRACKS. THE FORE AND AFT RUDDERS WERE REMOVED, A NEW ACCESS PANEL COVER PLAT FABRICATED AND INSTALLED AND THE RIB END CAP WAS REPLACED IAW RO NR DHC82-55-0001-GJT. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A13NM 1998072400035 19980724 00035 NM 1998 7 24 MASA98118 1 19980527 A 5542 85540021 COVER PLATE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 448YV 3965 448 DUE TO OTHER A/C BEING NOTED WITH FORE RUDDER LWR RIB END CAP AND/OR COVER PLATE DAMAGE. THIS AIRCRAFTS RUDDER WAS INSP ECTED WHILE THE AIRCRAFT WAS SITTING AS A SPARE. THE FORWARD RUDDER LOWER RIB END CAP ACCESS PANEL COVER PLATE WAS NOTE D TO HAVE SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCESS PANEL COVER PLATE. THE FORE AND AFT RUDDERS WERE REMOVED, AND A NEW ACCESS PANEL COVER PLATE WAS FABRICATED AND INSTALLED. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998072400036 19980724 00036 EU 1998 7 24 USAA980239 1 19980605 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU BS 3870 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 889US 15872 11358 PIT - DURING Q-CHECK, FOUND .3750 INCH BY .50 INCH CORRODED AREA AT BEAM AT STA 3870, BL 1127R. BLENDED OUT CORROSION O N FLOOR BEAM TO SMOOTH CONTOUR, ALODINE NR 1200S PRIME AND TOP COAT REWORKED AREAS, SEALED TOP SURFACE BEAM WITH PR 1436 G PER EA 49760. (X) 2 L 7 2 4F RT 1998072400037 19980724 00037 EU 1998 7 24 USAA980237 1 19980605 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU BS 3870 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 889US 15872 11358 PIT - DURING Q-CHECK, FOUND 1 INCH BY .50 INCH CORRODED AREA AT BEAM AT STA 3870 FORWARD BEAM BL 1127L. BLENDED OUT COR ROSION ON FLOORBEAM, INSTALLED L-ANGLE DOUBLER WET WITH PR 1436G USMS MS20426AD5 AND MS047AD5 FASTENERS PER EA 49771. (X ) 2 L 7 2 4F RT 1998072400038 19980724 00038 EU 1998 7 24 USAA980238 1 19980605 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU BS 3870/4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 889US 15872 11358 PIT - DURING Q-CHECK, FOUND SEVERAL .25 INCH BY .25 INCH CORRODED AREAS AT STA 3870 AND STA 4610 BL 1127L BEAM. BLENDED CORROSION TO SMOOTH CONTOUR. ALODINED AND PRIMED. SEALED TOP SURFACE WITH 1436G PER EA 49760. (X) 2 L 7 2 4F RT 1998072400039 19980724 00039 EU 1998 7 24 USAA980236 1 19980605 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 866US 18818 11310 PIT - DURING C-4 CHECK, FOUND .1875 INCH CRACK AND .25 INCH CRACK IN SKIN AT LT AND RT AFT CORNERS OF NOSE GEAR BAY. RE MOVED DAMAGED AREAS AND REINSTALLED FASTENERS PER EA 49826. (X) 2 L 7 2 4F RT 1998072400040 19980724 00040 EU 1998 7 24 USAAF98048 1 19980610 A 2923 42047 GASKET FOKKER F28 F28MK0100 4990807 EU NR 2 HYD PUMP FAILED A USAA A UNSCHED LANDING D J INFLIGHT SEPARATION WARNING INDICATION CL CLIMB 1 EA 19 864US 15496 6783 11306 CLT - FLT 1694 - AFTER TAKEOFF FROM CLT, SYSTEM NR 2 HYDRAULIC QUANTITY DROPPED TO 14 PERCENT. FLIGHT RETURNED TO CLT A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 2 ENGINE NR 2 HYDRAULIC PUMP DUE TO BLOWN GASKETS. (X) 2 L 7 2 4F RT 1998072400041 19980724 00041 NM 1998 7 24 USAASB98148 1 19980610 A 2822 568126713004 BOOST PUMP BOEING 737 7374B7 1384702 NM RT WING FAILED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 781AU 16119 25020 PHL - FLT 565 - UPON CLIMB-OUT FROM LGA, CREW NOTICED THERE WAS NO CENTER TANK FUEL BEING BURNED. FLIGHT DIVERTED TO PH L AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE RT AND LT CENTE R TANK FUEL BOOST PUMPS INOPERABLE. REPLACED BOOST PUMPS PER MM 28-22-41. OPERATIONAL CHECK GOOD. REF: OPERATOR CONT ROL NR 98ZZZX2394. (X) 2 L 7 2 4F RT A16WE 1998072400042 19980724 00042 NM 1998 7 24 98ZZZX2394 1 19980610 A 2822 568126713005 BOOST PUMP BOEING 737 7374B7 1384702 NM LT WING FAILED A USAA A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 EA 19 781AU 21243 25020 PHL - FLT 565 - UPON CLIMB-OUT FROM LGA, CREW NOTICED THERE WAS NO CENTER TANK FUEL BEING BURNED. FLIGHT DIVERTED TO PH L AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE RT AND LT CENTE R TANK FUEL BOOST PUMPS INOPERABLE. REPLACED BOOST PUMPS PER MM 28-22-41. OPERATIONAL CHECK GOOD. REF: OPERATOR CONT ROL NR USAASB98148. 2 L 7 2 4F RT A16WE 1998072400043 19980724 00043 NM 1998 7 24 USAASB98146 1 19980606 A 2810 2565616250 AIR FILTER BOEING 737 737401 1384701 NM AUX FUEL TANK DIRTY A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 408US 23878 MCI - FLT 165 - EN ROUTE TO PHX, CREW COULD NOT TRANSFER FUEL OUT OF THE AUXILIARY FUEL TANK. CREW PULLED ALL AUXILIARY FUEL TANK CIRCUIT BREAKERS AND RESET THEM PER MAINTENANCE CONTROL. COULD NOT RESET AFT TRANSFER CIRCUIT BREAKER ON FIR ST ATTEMPT, BUT BREAKER DID FINALLY RESET. FLIGHT DIVERTED TO MCI AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLAR ED. MAINTENANCE REMOVED AND REPLACED THE CABIN AIR FILTER SCREEN ON THE AUXILIARY FUEL TANK. FUEL TRANSFER AND OPERATI ONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998072400044 19980724 00044 NM 1998 7 24 USAASB98134 1 19980601 A 2150 654531453 A/C MODULE BOEING 737 737301 1384611 NM E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 585US 14415 23930 RDU - FLT 1012 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER DEPARTING PHL. CREW DECIDED TO DIVERT TO CLT, BUT ON THE WAY, A PASSENGER HAD A MEDICAL PROBLEM AND THE FLIGHT DIVERTED TO RDU INSTEAD. FLIGHT LANDED WITHOUT FURTHER INCIDENT W ITH NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACED THE DELTA-P AIR CONDITIONING MODULE. OPERATIONAL CHE CK GOOD PER MM 21-31-00. (X) 2 L 7 2 4F RT A16WE 1998072400045 19980724 00045 NM 1998 7 24 USAASB98147 1 19980608 A 2530 41600011G COFFEE MAKER BOEING 737 737201 1384454 NM GALLEY LEAKING A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 253AU 11532 22795 PIT - FLT 1250 - AFTER TAKEOFF, THE AFT GALLEY COFFEE MAKERS STARTED CREATING SMOKE AND PRODUCED A RUBBER SMELL. COFFEE MAKERS WERE NOT TURNED ON AT THE TIME. FLIGHT ATTENDANT PULLED CIRCUIT BREAKERS AND SMOKE AND SMELL DISSIPATED. FLIGH T CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AFT GALLEY COFFEE MAKERS FOR BURNED WIRING A ND COMPONENTS. NONE FOUND. FOUND THE NR 1 AFT GALLEY COFFEE MAKER LEAKING. REMOVED AND REPLACED SAME. OPERATIONAL CH ECK GOOD. (X) 2 L 7 2 4F A16WE 1998072400046 19980724 00046 NM 1998 7 24 USAABB98066 1 19980615 A 2751 TRANSMITTER BOEING 757 7572B7 1384964 NM TE FLAP OUT OF ADJUST A USAA L ABORTED APPROACH B F SMOKE/FUMES/ODORS/SPARKS FLT CONT AFFECTED AP APPROACH 1 EA 19 621AU 27200 CLT - FLT 62 - INBOUND TO CLT, CREW SELECTED 30 DEGREES FLAPS. FLAPS FAILED TO MOVE PAST 20 DEGREES. WHILE POSITIONING THE AIRCRAFT TO LAND ON A LONGER RUNWAY, THE CREW BECAME AWARE OF AN ODOR IN THE COCKPIT THAT SMELLED LIKE SOMETHING WA S GETTING HOT. FLIGHT LANDED AT CLT WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE COCKPIT AND COULD NOT FIND ANY PROBLEMS THAT WOULD CAUSE AN ODOR. THE LEFT FLAP POSITION TRANSMITTER WAS FOUND OUT OF LIMITS AND WAS ADJUSTED. (X) 2 L 7 2 4F RT A2NM 1998072400047 19980724 00047 NM 1998 7 24 USAABB98065 1 19980611 A 5243 14976104 SERVICE PANEL BOEING 757 7572B7 1384964 NM FUSELAGE SEPARATED A USAA A UNSCHED LANDING E D VIBRATION/BUFFET INFLIGHT SEPARATION CR CRUISE 1 EA 19 625VJ 27246 DEN - FLT 78 - EN ROUTE LAX/PHL, CREW REPORTED THEY HAD AN AIRFRAME VIBRATION AND HEARD A LOUD BANGING ON THE FUSELAGE. FLIGHT DIVERTED TO DEN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT HYDRAULIC SERVICE PANEL MISSING AND DAMAGE TO THE AIRCRAFT STRUCTURE AT STA 1240. SERVICE PANEL WAS REPLACED AND THE DAMAGE REPAIRED OR INSPECTED AND PROGRAMMED FOR REPAIR. (X) 2 L 7 2 4F RT A2NM 1998072400048 19980724 00048 WP 1998 7 24 TWAA9809501 1 19980614 A 3350 0105601003PA57 COVER DOUG DC9 DC983 3022083 WP CABIN CRACKED A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 9409F 53121 STL - FLT 74 - THE EMERGENCY FLOOR LIGHTING STRIP AT ROW 1 WAS FOUND BROKEN. REPLACED EMERGENCY FLOOR LIGHTING STRIP AT ROW 1. CHECK-C 5-6-98 STL. ACFTR TT: 15,970 HOURS. ACFT TC: 8,193. (X) 2 L 7 2 4F RT A6WE 1998072400049 19980724 00049 WP 1998 7 24 TWAA9809502 1 19980614 A 3350 BULBS DOUG DC9 DC941 302207N WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 934L 47618 STL - DURING OVERNIGHT MAINTENANCE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS INOPERABLE ON RT SIDE OF CABIN AT ROWS 24, 21, 12, AND 7. REPLACED BULBS AT ROWS 24, 21, AND 12, MFG P/N 315. REPLACED BATT AT ROW 7 RT SIDE, MFG P/N 14597-101. CH ECK-C 2-11-98 MCI. ACFT TT: 49,773 HOURS. ACFT TC: 46,067. (X) 2 L 7 2 4F A6WE 1998072400050 19980724 00050 WP 1998 7 24 TWAA9809503 1 19980614 A 2150 FAN DOUG DC9 DC941 302207N WP RT PACK MALFUNCTIONED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 935L 47603 STL - FLT 598 - AFATER TAKEOFF, THE RT PACK FILLED CABIN WITH SMOKE. THE PACK FAN WAS WORKING. RAN BOTH ENGINES AND RT PACK AND PACK FAN. NO SMOKE NOTED. GROUND CHECKS NORMAL. CHECK-C 3-23-98 MCI. (X) 2 L 7 2 4F A6WE 1998072400062 19980724 00062 EU 1998 7 24 SIMA981631 1 19980612 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL PLATE CORRODED. REMOVED AND REPLACED SILL PLA TE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X) 2 H 7 2 4T RT A53EU 1998072400063 19980724 00063 EU 1998 7 24 SIMA981668 1 19980615 A 5330 SKIN AEROSP ATR72 ATR72212 EU BS 2086 GOUGED A SIMA O OTHER O OTHER NR NOT REPORTED 1 SW 21 499AT 499 ORD - FLT 4070 - JET BRIDGE STRUCK FUSELAGE. CAUSED SKIN DAMAGE AT FS 2086. CUT OUT DAMAGE, INSTALLED 15 INCH BY 16 IN CH REPAIR DOUBLER. ACFT TT: 1,680.3 HOURS. ACFT TC: 2,339. (X) 2 H 7 2 4T RT A53EU 1998072400064 19980724 00064 EU 1998 7 24 SIMA981686 1 19980612 A 5320 S5367131830401 SILL AEROSP ATR72 ATR72212 EU SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE SERVICE DOOR SILL PLATE WEB CORRODED. REMOVED AND REPLACED THE WE B. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X) 2 H 7 2 4T RT A53EU 1998072400065 19980724 00065 EU 1998 7 24 SIMA981685 1 19980612 A 5320 S5367121729801 SILL AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR SILL PLATE GULLEY CORRODED. REMOVED AND REPLACED T HE GULLEY. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X) 2 H 7 2 4T RT A53EU 1998072400066 19980724 00066 EU 1998 7 24 SIMA981684 1 19980612 A 5320 S5367121729602 SILL AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE PASSENGER DOOR THROAT AND SILL PLATE CORRODED. REMOVED AND REPLAC ED THE THROAT PLATE. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. (X) 2 H 7 2 4T RT A53EU 1998072400067 19980724 00067 EU 1998 7 24 SIMA981683 1 19980612 A 5320 S5367121729602 SILL AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE JOINT PLATE FOR THE LEFT AFT OUTBOARD SEAT TRACK TO PASSENGER DOOR SILL PLATE AT FRAME 36 CORRODED. REMOVED AND REPLACED THE JOINT PLATE. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,55 6.0 HOURS. ACFT TC: 15,190. (X) 2 H 7 2 4T RT A53EU 1998072400068 19980724 00068 EU 1998 7 24 SIMA981682 1 19980612 A 5320 S5367121725802 STIFFENER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT AND RIGHT STIFFENER BETWEEN FRAMES 36 AND 39 CORRODED. REMOV ED AND REPLACED BOTH STIFFENERS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. REF: OPERATOR CONTROL NR 98ZZZX2395. (X) 2 H 7 2 4T RT A53EU 1998072400069 19980724 00069 EU 1998 7 24 98ZZZX2395 1 19980612 A 5320 S5367121731402 STIFFENER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT AND RIGHT STIFFENER BETWEEN FRAMES 36 AND 39 CORRODED. REMOV ED AND REPLACED BOTH STIFFENERS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. ACFT TT: 13,556.0 HOURS. ACFT TC: 15,190. REF: OPERATOR CONTROL NR SIMA981682. 2 H 7 2 4T RT A53EU 1998072400070 19980724 00070 EU 1998 7 24 SIMA981677 1 19980612 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDL E OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRA CKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13 ,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR 98ZZZX2396 THROUGH 98ZZZX2399. (X) 2 H 7 2 4T RT A53EU 1998072400071 19980724 00071 EU 1998 7 24 98ZZZX2396 1 19980612 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDL E OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRA CKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13 ,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2397 THROUGH 98ZZZX2399. 2 H 7 2 4T RT A53EU 1998072400072 19980724 00072 EU 1998 7 24 98ZZZX2397 1 19980612 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDL E OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRA CKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13 ,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2396 THROUGH 98ZZZX2399. 2 H 7 2 4T RT A53EU 1998072400073 19980724 00073 EU 1998 7 24 98ZZZX2398 1 19980612 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDL E OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRA CKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13 ,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2396 THROUGH 98ZZZX2399. 2 H 7 2 4T RT A53EU 1998072400074 19980724 00074 EU 1998 7 24 98ZZZX2399 1 19980612 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LT AFT INBD AND OTBD, LT AND RT AFT FLIGHT ATTENDANT, AND RT MIDDL E OTBD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE LT AFT INBD AND OTBD, AND LT AND RT AFT FLIGHT ATTENDANT SEAT TRA CKS. SPLICED IN A NEW SECTION OF SEAT TRACK FOR RT MIDDLE OTBD SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13 ,556.0 HRS. ACFT TC: 15,190. REF: OPERATOR CNTRL NR SIMZ981677, AND, 98ZZZX2396 THROUGH 98ZZZX2399. 2 H 7 2 4T RT A53EU 1998072400075 19980724 00075 EU 1998 7 24 SIMA981681 1 19980612 A 5320 S5367800920102 SUPPORT AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNE L SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR 98ZZZX2400 T HROUGH 98ZZZX2402. (X) 2 H 7 2 4T RT A53EU 1998072400076 19980724 00076 EU 1998 7 24 98ZZZX2400 1 19980612 A 5320 S5367800826801 SUPPORT AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNE L SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR SIMA98168-1, AND, 98ZZZX2401 THROUGH 98ZZZX2402. 2 H 7 2 4T RT A53EU 1998072400077 19980724 00077 EU 1998 7 24 98ZZZX2401 1 19980612 A 5320 S5367800021451 SUPPORT AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNE L SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR SIMA98168-1, AND, 98ZZZX2400 THROUGH 98ZZZX2402. 2 H 7 2 4T RT A53EU 1998072400078 19980724 00078 EU 1998 7 24 98ZZZX2402 1 19980612 A 5320 S5367800826901 SUPPORT AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THREE FLOOR CHANNEL SUPPORTS ON THE LT SIDE BETWEEN FRAMES 36 AND 38, AND ONE FLOOR CHANNEL SUPPORT ON THE RT SIDE BETWEEN FRAMES 38 AND 39 CORRODED. REMOVED AND REPLACED ALL 4 FLOOR CHANNE L SUPPORTS. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,190. REF: OPER CNTRL NR SIMA98168-1, AND, 98ZZZX2400 THROUGH 98ZZZX2401. 2 H 7 2 4T RT A53EU 1998072400079 19980724 00079 EU 1998 7 24 SIMA981676 1 19980612 A 5230 S53371293202 SUPPORT AEROSP ATR72 ATR72212 EU CARGO DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 260AE 263 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE CARGO DOOR DRAIN CHANNEL SUPPORT PLATE BETWEEN FRAMES 13 AND 17 CO RRODED. REMOVED AND REPLACED THE SUPPORT PLATE. AIRCRAFT RETURNED TO SERVICE. ACFT TT: 13,556.0 HRS. ACFT TC: 15,1 90. (X) 2 H 7 2 4T RT A53EU 1998072400080 19980724 00080 EU 1998 7 24 SIMA981693 1 19980618 A 5347 4650000043 SEAT TRACK SAAB SF340 340B 7860101 EU BS 658 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DURING HMBV INSPECTION, SEAT TRACK BL 18.3L AT STA 658 WAS FOUND CORRODED BEYOND LIMITS. CUT OUT 46 INCH SECTION OF CORRODED SEAT TRACK. INSTALLED NEW 46 INCH EXTRUSION AND 15 INCH U-BEAM. ACFT TT: 15,388.4 HRS. ACFT TC: 14,564. (X) 2 L 7 2 4T RT A52EU 1998072400081 19980724 00081 EU 1998 7 24 SIMA981692 1 19980618 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 733 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DURING HMBV INSPECTION, MAINTENANCE FOUND A DENT ON LT HAND SIDE OF FUSELAGE AT FS 733. CUT OUT DAMAGED AREA. PE RFORMED EDDY CURRENT INSPECTION AND INSTALLED A REPAIR 8.25 INCHES BY 8.0 INCHES WIDE. ACFT TT: 15,388.4 HRS. ACFT TC : 14,564. (X) 2 L 7 2 4T RT A52EU 1998072400082 19980724 00082 EU 1998 7 24 SIMA981691 1 19980618 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 340 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DURING HMBV INSPECTION, MAINTENANCE FOUND A DENT ON RT HAND SIDE OF FUSELAGE AFT OF ICE SHIELD AT FS 340. CUT OUT DAMAGED AREA. PERFORMED EDDY CURRENT INSPECTION AND INSTALLED A REPAIR 12.5 INCHES BY 7.0 INCHES WIDE. ACFT TT: 15,38 8.4 HRS. ACFT TC: 14,564. (X) 2 L 7 2 4T RT A52EU 1998072400083 19980724 00083 EU 1998 7 24 SIMA981678 1 19980616 A 2910 9302631002 LINE SAAB SF340 340B 7860101 EU NLG WW FAILED A SIMA E ENGINE SHUTDOWN K J Y FLUID LOSS WARNING INDICATION ENGINE STOPPAGE TX TAXI/GRND HDL 1 SW 21 243AE 340B243 DFW - FLT 5141 - AS AIRCRAFT TAXIED OUT FOR DEPARTURE, LOST MAIN HYDRAULIC SYSTEM PRESSURE INCLUDING STEERING AND BRAKES . AIRCRAFT ROLLED OFF TAXIWAY AND INTO THE GRASS. FOUND HOLE IN HYDRAULIC PUMP TO MANIFOLD PRESSURE LINE. REMOVED AND REPLACED HYDRAULIC LINE. LINE LEAK CHECK AND HYDRAULIC SYSTEM OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998072400084 19980724 00084 NM 1998 7 24 98ZZZX2403 1 19980614 A 5730 PANEL BOEING 727 727251 138408H NM RT WING MISINSTALLED A S84A A UNSCHED LANDING K W FLUID LOSS INADEQUATE Q C NR NOT REPORTED 1 EA 21 259US 19978 F/A REPORTED FUEL LEAKAGE FROM RT WING. AIRCRAFT RETURNED TO CUN. FOUND LOWER ACCESS PANEL ON RT WING LEAKING. RESECU RED AND TORQUED HARDWARE IAW MM 28-11-21. 2 L 7 3 4F A3WE 1998072400085 19980724 00085 NM 1998 7 24 98ZZZX2404 1 19980610 A 3350 38931002 BATTERY BOEING 727 727251 138408H NM CABIN DISCHARGED A S84A K NONE L NO TEST IN INSP/MAINT 1 EA 21 259US 19978 DURING B-CHECK INSPECTION, FOUND 2 EACH OVERHEAD EMERGENCY LIGHTS NOT WORKING. REPLACED BATTERIES. OPS CHECKED OK. 2 L 7 3 4F A3WE 1998072400086 19980724 00086 CE 1998 7 24 S2YA98016 1 19980610 A 3246 11480013 WHEEL BEECH 1900 1900D 1154162 CE NLG OUT OF BALANCE A S2YA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 GL 13 841SK 42 UE84 MKE/IND - FLT 1056 - AFTER TAKEOFF ROTATION, FLIGHT CREW FELT THE NOSE WHEEL SHUDDER. AFTER MAKING A SAFE LANDING IN MK E, MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE NOSE WHEEL TIRE OUT OF BALANCE. THE NOSE WHEEL ASSY WAS REPLACED AND TH E AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998072400087 19980724 00087 NM 1998 7 24 RAAA98B1085 1 19980715 A 3530 4566M37B042NM PBE BOEING 727 72722C 138400F NM CABIN MALFUNCTIONED A RAAA K NONE J WARNING INDICATION IN INSP/MAINT 1 AL 03 831RV 19093 FOUND PAX ROW 2ABC PBE INDICATOR PROTRUDING ON SERVICE CHECK. CHANGED PBE DUE POUCH VACUUM LOST. 2 L 7 3 4F A3WE 1998072400088 19980724 00088 WP 1998 7 24 CALA9801245 1 19980714 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 427-522 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FORWARD CARGO PIT FLOOR PANEL CRACKED AT ST 427 TO 522. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010. 2 L 7 2 4F A6WE 1998072400089 19980724 00089 WP 1998 7 24 CALA9801246 1 19980714 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 218-313 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FORWARD PIT FLOOR PANEL DELAMINATED AT STA 218 TO 313. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW ECRA 2551-01010. 2 L 7 2 4F A6WE 1998072400090 19980724 00090 WP 1998 7 24 CALA9801247 1 19980714 A 5320 END CAPS DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LONGERON 20R AND 21R END CAPS CORRODED IN AFT CARGO COMPARTMENT AT STA 996. THE END CAPS WERE REMOVED IAW SRM 51-30-2. NEW END CAPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1998072400091 19980724 00091 WP 1998 7 24 CALA9801248 1 19980714 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 237 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND WEB CORRODED AT CUSP LINE FORWARD AND AFT OF FRAME FITTING AT STA 237 ON LT SIDE. THE CORRODED AREA OF WEB WAS CUT OUT, A REPAIR WEB AND L-ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-3, AND 53-01, PAGE 9. 2 L 7 2 4F A6WE 1998072400092 19980724 00092 WP 1998 7 24 CALA9801249 1 19980715 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1212-1219 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15841 49581 INSPECTION FOUND WEB CORRODED IN AFT BAGGAGE BIN AT AFT SIDE OF DOOR CUTOUT NUT PLATE STRIP UNDER TIEDOWN, STA 1212 TO 1219.5, LONGERON 26L. THE AREA WAS REPAIRED IAW ECRA 5332-01003. 2 L 7 2 4F A6WE 1998072400093 19980724 00093 WP 1998 7 24 CALA9801250 1 19980715 A 5320 FRAME DOUG DC9 DC932 3022066 WP WINDOW DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON WINDOW FRAMES 28 TO 30R. REPAIRED IAW ECRA 5330-02683. 2 L 7 2 4F A6WE 1998072400094 19980724 00094 WP 1998 7 24 CALA9801251 1 19980715 A 5720 CLIP DOUG DC9 DC932 3022066 WP WS 429 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND RT WING LEADING EDGE RIB CLIP CRACKED JUST INBOARD OF WS XOS 429. THE CRACK WAS STOP DRILLED AND A REP AIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5. 2 L 7 2 4F A6WE 1998072400095 19980724 00095 WP 1998 7 24 CALA9801252 1 19980715 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 313-357 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FORWARD PIT FLOOR PANEL CORRODED AND DELAMINATED AT STA 313 TO 357. A NEW FLOOR PANEL WAS FABRICATED A ND INSTALLED IAW ECRA 2551-01010. 2 L 7 2 4F A6WE 1998072400096 19980724 00096 WP 1998 7 24 CALA9801253 1 19980715 A 5720 BRACKET DOUG DC9 DC932 3022066 WP WS 332 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .25 INCH CRACK AT BOLT HOLE OF LT WING SUPPORT BRACKET, XRS 332. THE BRACKET WAS REMOVED AND A NEW B RACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-1, 51-10-2, 51-10-2A, AND 51-10-3. 2 L 7 2 4F A6WE 1998072400097 19980724 00097 WP 1998 7 24 CALA9801254 1 19980715 A 5320 CUSP DOUG DC9 DC932 3022066 WP BS 986 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND CUSP CORRODED AT FS 986, RBL 62. THE CORRODED AREA OF CUSP WAS CUT OUT. A REPAIR CUSP AND L-ANGLE WER E FABRICATED AND INSTALLED IAW SRM 53-05, 51-20-2, AND 51-10-30. 2 L 7 2 4F A6WE 1998072400098 19980724 00098 WP 1998 7 24 CALA9801255 1 19980715 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 351 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 4 INCH CRACK IN RADIUS OF FORWARD CARGO FLOORBEAM AT STA 351, BL 0. AN L-ANGLE WAS FABRICATED AND IN STALLED IAW SRM 53-05, FIGURE 78. 2 L 7 2 4F A6WE 1998072400099 19980724 00099 WP 1998 7 24 CALA9801256 1 19980715 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 522-579 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOOR PANEL BROKEN AT STA 522 TO 579. THE FLOOR PANEL WAS REMOVED IAW MM 53-20-0. A NEW FLOOR PANEL W AS FABRICATED AND INSTALLED IAW SRM 53-20-0 AND 53-21-0. 2 L 7 2 4F A6WE 1998072400100 19980724 00100 WP 1998 7 24 CALA9801257 1 19980715 A 5320 ANGLE DOUG DC9 DC932 3022066 WP DORSAL FIN CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 2 INCH CRACK IN ATTACH ANGLE AT RT DORSAL FIN LOWER FORWARD ACCESS PANEL. THE ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1998072400101 19980724 00101 NE 1998 7 24 CALA9801258 2 19980714 A 7230 500200401 C-4 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE BROKEN A CALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 09 10801 49127 709855 THE NR 1 ENGINE GAVE OFF A LOUD BANG WITH VIBRATION AND YAW FELT WHILE EN ROUTE. THE NR 1 ENGINE GAUGES BECAME ERRATIC. THE N1 AND N2 EVENTUALLY STABILIZED. THE AIRCRAFT WAS DIVERTED TO MSY WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENG INE WAS REMOVED AND REPLACED. *S/D* INVESTIGATION CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO A BRO KEN C-4 BLADE. 2 L 7 2 4F 4 F A6WE E9NE 1998072400102 19980724 00102 SO 1998 7 24 COMA9810158 1 19980714 A 5610 NP1513111 WINDSHIELD EMB 120 EMB120RT SO LT COCKPIT SHATTERED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 463CA 3930 120267 PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4T RT A31SO 1998072400103 19980724 00103 SO 1998 7 24 COMA9810159 1 19980715 A 2150 HOSE EMB 120 EMB120RT SO RT PACK LOOSE A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 246CA 120223 RIGHT HAND AIR CONDITIONING PACK FAILED AFTER TAKEOFF. TIGHTENED SEVERAL LOOSE HOSE CLAMPS AT RIGHT HAND AIRCRAFT PACK. 2 L 7 2 4T RT A31SO 1998072400104 19980724 00104 NE 1998 7 24 COMA9860177 2 19980714 A 7230 COMPRESSOR BLADE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE MISSING A COMA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 924CA 350 7026 807050 RIGHT HAND N2 VIBRATION WARNING. PERFORMED BORESCOPE INSPECTION AND FOUND STAGE 8 COMPRESSOR MISSING ONE BLADE. REPLAC ED ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998072400105 19980724 00105 EA 1998 7 24 COMA9860178 1 19980715 A 3350 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA CABIN TRIPPED A COMA K NONE L NO TEST CR CRUISE 1 SO 01 920CA 7022 EMERGENCY LIGHTING ACTIVATED DURING FLIGHT. FOUND EMERGENCY LIGHTING CIRCUIT BREAKER TRIPPED. RESET BREAKER, SYSTEM OP ERATION NORMAL. 2 L 7 2 4F RT A21EA 1998072400106 19980724 00106 NM 1998 7 24 UPS98227171 1 19980715 A 3350 LIGHT BOEING 727 72730C 1384009 NM FLT DECK DOOR INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 918UP 19008 INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR WILL NOT STAY IN IT'S ELECTRICAL SOCKET CAUSING IT TO STAY ON IN FLIGHT. REINSTALLED EMER EXIT LIGHT PROPERLY UNTILL LATCHES ENGAGED, EMER EXIT LIGHT, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998072400107 19980724 00107 NE 1998 7 24 UPS98427170 2 19980716 A 7200 ENGINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7 52054 NE NR 2 FAILED A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 691UP 19641 P686089PN INSPECTION TYPE-N/A, NR 2 ENG FLAMED OUT. FOUND METAL IN LOWER RT BLEED SCREEN. REPLACED ENGINE. 2 L 7 4 4F 4 F A20WE E20EA 1998072400108 19980724 00108 WP 1998 7 24 UPS98826954 1 19980603 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 772UP 46072 INSPECTION TYPE-D, LT WING L/E AT STA XFS616.25, THE LWR L/E RIB IS CRACKED AT THE AFT BEND. STOP DRILLED CRACK AND RE PAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998072400109 19980724 00109 WP 1998 7 24 UPS98827094 1 19980701 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 807UP 46007 INSPECTION TYPE-N/A, CORROSION FOUND DURING INSPECTION. BULGE IN SKIN AFT OF NR 2 PIT DOOR CREATING HOLE IN FUSELAGE. C LEANED CORROSION PER SRM 53-2-0, TREATED AND PAINTED. COMPLIED WITH E/O 5330-10147A. 2 L 7 4 4F RT 4A25 1998072400110 19980724 00110 EU 1998 7 24 QXEA9800852 1 19980612 A 5320 SIDEWALL FOKKER F28 F28MK4000 4990810 EU ACM COMPT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 RIGHTHAND ACM COMPARTMENT SIDEWALL CRACKED BETWEEN 4TH AND 5TH VERTICAL CHANNELS ABOVE LOWER BEEM CONNECTION. REPAIRED IAW HORIZON AIR EA 4-53-462A. 2 L 7 2 4F RT A20EU 1998072400111 19980724 00111 EU 1998 7 24 QXEA9800853 1 19980528 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CENTER CARGO DOOR SUPPORT ROD ATTACH BRACKET ON THE DOOR APERATURE HAS SMALL CRACK. REPAIRED IAW FOKKER SRM 53-02-16, P AGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1998072400112 19980724 00112 EU 1998 7 24 QXEA9800854 1 19980613 A 5320 PRESSURE PANEL FOKKER F28 F28MK4000 4990810 EU NLG WW MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 494US 11167 RIGHTHAND SIDE OVERHEAD NOSE GEAR WELL THERE ARE 8 IMPROPERLY SHOT RIVETS THROUGH A PREVIOUS REPAIR. THE REPAIR IS PULL ED AWAY .25 INCH FROM THE GRAVEL GUARD. REPAIRED IAW FOKKER SRM 32-40-00 AND 51-31-05. 2 L 7 2 4F RT A20EU 1998072400113 19980724 00113 EU 1998 7 24 QXEA9800855 1 19980520 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 16060 CLIP HAS CORROSION OUTBOARD OF STRINGER 74. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998072400114 19980724 00114 EU 1998 7 24 QXEA9800856 1 19980601 A 5320 DOUBLER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CORROSION AFT OF COMM 3 ANTENNA ON ANTENNA DOUBLER AND FUSELAGE SKIN INTERIOR AT FOUR PLACES. REPAIRED IAW FOKKER SRM 5 3-02-04, PAGE 2 FIGURE 1. 2 L 7 2 4F RT A20EU 1998072400115 19980724 00115 EU 1998 7 24 QXEA9800857 1 19980601 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 15205 CLIP BETWEEN STRINGER 1 AND 74 IS CRACKED, CORRODED AND DISTORTED. REPAIRED IAW FOKKER SRM 53-02-17, PAGE 6 FIGURE 3. 2 L 7 2 4F RT A20EU 1998072400116 19980724 00116 EU 1998 7 24 QXEA9800858 1 19980528 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 13815B HAS CRACKED REPAIR DOUBLER CLIP AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-11, PAGES 2 AND 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1998072400117 19980724 00117 EU 1998 7 24 QXEA9800859 1 19980528 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 13815B HAS CRACKED REPAIR DOUBLER CLIP AT STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-11, FIGURE 1, PAGES 2 AND 3. 2 L 7 2 4F RT A20EU 1998072400118 19980724 00118 EU 1998 7 24 QXEA9800860 1 19980528 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 13815A HAS CRACKED REPAIR DOUBLER CLIP AT STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998072400119 19980724 00119 EU 1998 7 24 QXEA9800861 1 19980622 A 5320 STRIP FOKKER F28 F28MK4000 4990810 EU BS 3820 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 TYPE 2 CRACK FOUND AT STATION 3820 LEFTHAND AND RIGHTHAND IN NOSE LANDING GEAR BAY INNER STRIP. REPAIRED IAW HORIZON AI R EO 4-53-33B. 2 L 7 2 4F RT A20EU 1998072400120 19980724 00120 EU 1998 7 24 QXEA9800862 1 19980622 A 5230 DOOR FOKKER F28 F28MK4000 4990810 EU CARGO COMPT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 AFT CARGO DOOR FORWARD LOWER CORNER PROFILE HAS .080 DEEP DENT. REPAIRED IAW FOKKER SRM 52-00-2, PAGE 202, PARA 3C. 2 L 7 2 4F RT A20EU 1998072400121 19980724 00121 EU 1998 7 24 QXEA9800863 1 19980520 A 5312 BULKHEAD WEB FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 REAR PRESSURE BULKHEAD WEB CRACKED BETWEEN BEAM 1 AND 2 AT BL 750R. REPAIRED IAW FOKKER SRM 53-02-18. 2 L 7 2 4F RT A20EU 1998072400122 19980724 00122 EU 1998 7 24 QXEA9800864 1 19980528 A 5312 BULKHEAD FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 BOTTOM RADIUS OF THE FORWARD PRESSURE BULKHEAD AFT SIDE HAS A CRACK INDICATION 4 RIGHT OF THE AIRCRAFT CENTER LINE APPRO XIMATELY 3.75 LONG. REPAIRED IAW FOKKER SRM 53-02-18, FIGURE 11. 2 L 7 2 4F RT A20EU 1998072400123 19980724 00123 EU 1998 7 24 QXEA9800865 1 19980604 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 5805 AND STRINGER 5 THERE IS CORROSION ON THE CASTELLATION. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998072400124 19980724 00124 EU 1998 7 24 QXEA9800866 1 19980621 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 AT FRAME 9305 AND STRINGER 74 THERE IS CORROSION ON THE FRAME UNDER THE NUT PLATES. REPAIRED IAW HORIZON AIR EA 4-53-44 4. 2 L 7 2 4F RT A20EU 1998072400125 19980724 00125 NM 1998 7 24 98UAL900308 1 19980704 A 2781 PROX SENSOR ELDEC CORPOR 106122615 BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE LE FLAPS FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 987UA 21749 ON FLAP RETRACTION, THE LEADING EDGE FLAP TRANSIT LIGHT REMAINED ILLUMINATED. *S/D* THE LEADING EDGE FLAP RETRACT PROX IMITY SENSOR WAS REPLACED. THE FLAP POSITION INDICATION SYSTEM HAS OPERATED NORMALLY SINCE THE REPLACEMENT. 2 L 7 2 4F 4 F A16WE E2EA 1998072400126 19980724 00126 NE 1998 7 24 98UAL900309 2 19980704 A 7532 51D271 PIN PWA 51D048 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 BLEED VALVE FAILED A UALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 WP 29 774UA 9920 9920 26936 777009 CREW REPORTS THAT NR 1 ENGINE EXHAUST GAS TEMPERATURE (EGT) IS 35 DEGREES HIGHER THAN NR 2 ENGINE EGT AND CLIMBING. FUE L FLOW ON NR 1 IS 800 PPH GREATER THAT NR 2. RETURNED TO MIA. ENGINE REPLACED AT MIA. FOUND 2.5 BLEED VALVE BELLCRANK PIVOT PIN FAILED. PART WAS PRE-SB PW4G-112-72-60. PROJECT IS UNDERWAY TO UPGRADE BLEED DESIGN TO SUBSEQUENT SB PW4G-1 12-72-106. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998072400127 19980724 00127 1998 7 24 98UAL900310 4 19980705 A 2565 D31038201 SLIDE AIR CRUISERS D31038201 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1R DEPLOYED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 524UA 24977 NUMBER 1 RIGHT DOOR SLIDE DEPLOYED. *S/D* INADVERTENT DEPLOYMENT DUE TO HUMAN ERROR. DEPLOYMENT WAS NORMAL. SLIDE WA S REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998072400128 19980724 00128 NM 1998 7 24 98UAL900311 1 19980607 A 5240 DOOR BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RT FUSELAGE OPENED A UALA O OTHER J WARNING INDICATION AP APPROACH 1 WP 29 601UA 21862 ON APPROACH 1800 FT, EICAS ANNUNCIATED RIGHT AFT DOOR OPEN. AIRCRAFT DEPRESSURIZED. FLIGHT ATTENDANT REPORTED SOUND OF RAPID AIR MOVEMENT. EMERGENCY LIGHTING ON RIGHT HAND SIDE OF AIRCRAFT ILLUMINATED AT APPROX 500 FEET. 2 L 7 2 4F 4 F RT A1NM E3NE 1998072400129 19980724 00129 NM 1998 7 24 98UAL900312 1 19980707 A 3260 LIGHTS BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT MLG MALFUNCTIONED A UALA O OTHER P NO WARNING INDICATION AP APPROACH 1 WP 29 601UA 21862 ON APPROACH, LEFT MAIN LANDING GEAR GREEN LIGHT FAILED TO OPERATE. NO EICAS INDICATION. AMBER LIGHT DID NOT ILLUMINA TE. AMBER ALERT DECLARED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998072400130 19980724 00130 NM 1998 7 24 98UAL900313 1 19980612 A 2841 INDICATOR BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 1-NR 4 FUEL DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 156UA 20105 NR 1 AND 4 RESERVE FUEL QUANTITY INDICATORS DAMAGED, BURNT INDICATORS. 2 L 7 4 4F 4 F A20WE E20EA 1998072400131 19980724 00131 NM 1998 7 24 DL76S981455 1 19980713 A 5330 148T32511 SKIN BOEING 767 767332 1382001 NM BS 1600 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 134DL 25123 EXISTING TIME-LIMITED SKIN REPAIR WAS REMOVED FROM STA 1600, STR 37R TO 38R, FOR INSTALLATION OF PERMANENT REPAIR. ORIG INAL REPAIR WAS INSTALLED DUE TO A PUNCTURE CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 267563-14, REV B. 2 L 7 2 4F RT A1NM 1998072400132 19980724 00132 NM 1998 7 24 DL76S981456 1 19980713 A 5330 146T35525 SKIN BOEING 767 767332 1382001 NM BS 1197 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 134DL 25123 THE FUSELAGE SKIN WAS FOUND DENTED AT STA 1197+88 AT STRINGER 27R AND AT STA 1197+100 AT STRINGER 28R. THE DENT DAMAGE WAS CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 331896-14. 2 L 7 2 4F RT A1NM 1998072400133 19980724 00133 NM 1998 7 24 DL76S981457 1 19980713 A 5330 146T32112 SKIN BOEING 767 767332 1382001 NM BS 1241 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 134DL 25123 THE FUSELAGE SKIN WAS FOUND DENTED AT STA 1241 BETWEEN STR 33L AND 34L. THE UNDERLYING FRAME SHEAR TIE WAS ALSO DENTED. THE DISCREPANT CONDITION WAS CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 331906-14. 2 L 7 2 4F RT A1NM 1998072400134 19980724 00134 NM 1998 7 24 DL72S981459 1 19980713 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA B9978957 20746 ON PREFLIGHT, EMER STRIP LIGHTING DID NOT ILLUM IN MIDDLE OF CABIN. FERRIED A/C TO DFW. REPLACED M9026 RACK AND BATTER Y PACK, SYSTEM CK NORMAL. 2 L 7 3 4F A3WE 1998072400135 19980724 00135 NM 1998 7 24 DLM88981461 1 19980714 A 3320 BALLAST D77311001 DOUG MD88 MD88 3023688 NM CABIN FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 946DL 17551 49819 STRONG ODOR ASSOCIATED W/ PACKS TURNED ON. REPLACED LIGHT BALLAST AT SEAT 14DE. 2 L 7 2 4F RT A6WE 1998072400136 19980724 00136 NM 1998 7 24 DL72S981462 1 19980714 A 5320 WEB BOEING 727 727232 1384082 NM BS 1313 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 470DA 20747 FOUND AT E-2 LETTER CK, CRACK AT LIGHTNING HOLE VERTICAL WEB RT SIDE STA 1313. REPAIR PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998072400137 19980724 00137 NM 1998 7 24 DL73K981466 1 19980715 A 5330 SKIN BOEING 737 737232 1384475 NM R2 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 322DL 23094 THE LOWER FORWARD CORNER OF THE R-2 DOOR CUTOUT WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND DOUBLER. THE BEAR STRAP WAS NOT CRACKED. THE DAMAGE WAS REPAIRED PER B737 SRM53-30-3, FIG 24 EXCEPT BLIND BOLTS WERE SUBSTITUTED ON A TIME-LIMI TED BASIS. THE REPAIR WAS ACCOMPLISHED PER ER/A 365253-14, REV A. 2 L 7 2 4F RT A16WE 1998072400138 19980724 00138 NM 1998 7 24 DL73K981467 1 19980712 A 5330 655298862 SKIN BOEING 737 737232 1384475 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 321DL 23093 THE UPPER AFT CORNER OF THE L2 DOOR CUTOUT WAS FOUND WITH A 3.25 INCH LONG CRACK IN THE SKIN, BONDED DOUBLER, AND UNDERL YING BEAR STRAP. THE CRACK WAS ROUTED OUT AND AN ALUMINUM REPAIR DOUBLER AND TRIPLER WERE INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 365222-14, REV A. THE DAMAGED AREA IS WITHIN THE SSI F-17 REGION. 2 L 7 2 4F RT A16WE 1998072400139 19980724 00139 NM 1998 7 24 DL72S981468 1 19980714 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 402DA 6601 21146 FIRST CLASS EMER ESCAPE PATH LIGHTING INOP. FOUND BLOWN POWER SUPPLY FUSE AND MELTED WIRING AT C/P. REPLACED POWER SUP PLY AND BATTERY, REPAIRED DAMAGED WIRING. OPN TEST OK. 2 L 7 3 4F A3WE 1998072400140 19980724 00140 NM 1998 7 24 DL767981469 1 19980714 A 5754 WEDGE BOEING 767 767232 1385132 NM NR 1 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 110DL 22222 DELAMINATION WAS FOUND ON THE NR 1 SLAT T/E WEDGE. DELAM AREA IS APPROX 4 IN DIAMETER. REPAIRED PER ERA 365245-14AD. 2 L 7 2 4F RT A1NM 1998072400141 19980724 00141 NM 1998 7 24 DL733981470 1 19980712 A 5330 65737412 SKIN BOEING 737 737347 1384647 NM LT COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2310 23596 A .75 INCH CRACK WAS FOUND IN THE SKIN AND UNDERLYING CORNER GUSSET AT UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW (C-D WINDOW POST LOCATION). THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL REPAIR DOUBLER AND AN ALUMINUM REP AIR TRIPLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 365209-14, REV B. 2 L 7 2 4F RT A16WE 1998072400142 19980724 00142 NE 1998 7 24 DL757981471 2 19980714 A 7530 STATOR 45100 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 27 641DL 1100 23995 1100 NR 1 ENG STALLED AT V1 AND AUTO SHUT DOWN HARD CARD AND POM EMERGENCY PROCEDURES FOLLOWED RETURNED TO RUNWAY 9L. BORESC OPED OK OF 6TH STAGE LPT - 16TH STAGE HPC CKS OK, CKD WIRING BETWEEN EEC AND SVA ALL OK. REPLACED EEC AND SVA AS PRECAU TION DUE TO EICAS MSG. FOUND PMA ROTOR AND STATOR BAD. REPLACED SAME, OP CKS OK. RAN ENG PER PFHB, CKS OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1998072400143 19980724 00143 WP 1998 7 24 DLL10981472 1 19980714 A 3230 1646059101 SWIVEL LKHEED 1011 10113851 5265010 WP RT MLG CRACKED A DALA K NONE O OTHER DE DESCENT 1 SO 27 735D 193C1226 1100 RIGHT MLG GREEN LIGHT DID NOT ILLUMINATE ON APPROACH, GEAR INDICATOR ON RIGHT WING VERIFIED POPPED UP. FOUND UPPER DRAG BRACE SWIVEL CRACKED. PART AOG'G FROM ATL (327002516). 2 L 7 3 4F A23WE 1998072400144 19980724 00144 WP 1998 7 24 SCNA98527 1 19980715 A 3350 EMBS139 POWER SUPPLY DOUG DC10 DC1015 3022118 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 330 48289 DURING HEAVY CHECK, THE B-ZONE OVERHEAD EMERGENCY LIGHTS WERE FOUND TO BE INOP. A NEW POWER SUPPLY WAS INSTALLED ABOVE THE L1 DOOR AND OPERTAION CHECK IS GOOD. 2 L 7 3 4F A22WE 1998072400145 19980724 00145 WP 1998 7 24 SCNA98528 1 19980715 A 3520 DOORS DOUG DC10 DC1015 3022118 WP CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE PASSENGER OXYGEN SYSTEM WAS FUNCTIONALLY TESTED AND SEVERAL COMPARTMENT DOORS DID NOT OPEN. RE PAIRS TO WIRING AND RESET CBU SEB PERFORMED, OXYGEN DROP PER MM 352000, OPS CHECKS GOOD. 2 L 7 3 4F A22WE 1998072400146 19980724 00146 NM 1998 7 24 P5CA9801172 1 19980713 A 3350 90085 BATTERY PACK BOEING 747 747132 1384882 NM CABIN DISCHARGED A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 856FT 19897 UPPER DECK EMERGENCY LIGHTS WILL NOT GO OUT WITH POWER OFF POSTION. REMOVED AND REPLACED UPPER DECK EMERGENCY LIGHTING BATTERY PACK PER MM 33-51-00. 2 L 7 4 4F A20WE 1998072400147 19980724 00147 NM 1998 7 24 P5CA9801173 1 19980713 A 2932 50234 PRESS XMTR BOEING 747 747132 1384882 NM NR 4 HYD SYST INOPERATIVE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 4 HYD PRESS PEGGED AT 4,000 PSI, FOLLOWED BY A LOW QTY ANNUNCIATOR AND DECREASING HYD QTY. HYD TEMP REMAINED NORMAL PRIOR TO AND FOLLOWING ABNORMAL PROCEDURES IN AOM. REPLACED NR 4 HYD PRESS TRANSMITTER IAW MM 29-31-01. OPS AND LEAK C HECK NORMAL. SYSTEM PRESS FOUND NORMAL PER MM 29-11-00. 2 L 7 4 4F A20WE 1998072400148 19980724 00148 WP 1998 7 24 RRXA98251 1 19980327 A 5320 5892906 COVER DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND CARGO X-SLIDE DOOR COVER (PN: 589206) CORRODED BEYOND REPAIR, AT STA 340. REMOVED DAM GED COVER, TREATED AREA IAW DC-8 51-1-8. DUE TO UNAVAILABILITY OF REPLACEMENT PART A NEW COVER WAS MADE IAW FAA APPROVE D TIMCO DER ENGINEERING SKETCH REO-4507 AND DWG DC08-25-0234. EWA RELIABILITY SECTION WILL CONTINUE TO MONITOR CORROSIO N LEVELS. 2 L 7 4 4F RT 4A25 1998072400149 19980724 00149 WP 1998 7 24 ARWA980799 1 19980716 A 2710 CONTROLS DOUG DC8 DC863 302198A WP LT AILERON WORN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 345JW 46042 LEFT AILERON VERY STIFF IN RIGHT TURN WHILE TROUBLESHOOTING AILERONS PROBLEMS. FOUND LT CABLE ROD END BEARING WORN, CRA NK CRACKED AND SPOILER MIXER ROD END BEARING WORN. REMOVED AND REPLACED LATERAL SPOILER LT CONTROL CABLE IAW MM 20-17-0 . REPLACED ACTUATOR CRANK AND ROD END AT SPOILER POWER CYLINDER AND CONTROL VALVE, ACCOMPLISHED ADJUSTMENT, OPS CHECK N ORMAL IAW MM 27-60-00. 2 L 7 4 4F 4A25 1998072400150 19980724 00150 NM 1998 7 24 VNAA9807006 1 19980710 A 3350 321430 BATTERY PACK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 433JS 53227 1047 3047 DURING ENGINE START PRIOR TO TAKEOFF, SEVERAL EMERGENCY FLOOR LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE WAS CALL ED OUT TO TROUBLESHOOT THE PROBLEM. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY POWER PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998072400151 19980724 00151 NE 1998 7 24 TC8A98041 2 19980715 A 7230 COMPRESSOR DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 802CK 45679 LOUD, PRONOUNCED, SUSPECTED ENGINE COMPRESSOR STALL ON RT SIDE DURING TAKEOFF PASSING 70 KIAS, ABORT INITIATED. INSPECT ED NR 3 AND NR 4 ENGINES FOR DAMAGE, NONE NOTED. LUBED SURGE BLEED VALVE ON NR 3 AND NR 4 ENGINES. RAN ENGINES IAW 71- 00, NO COMPRESSOR STALLS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1998072400152 19980724 00152 EU 1998 7 24 QXEA9800867 1 19980531 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CANNED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - LEFT FRONT AIR SCOOP TOP SKIN OIL CANNING. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998072400153 19980724 00153 EU 1998 7 24 QXEA9800868 1 19980611 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - FUSELAGE SKIN IS CHAFFED IN TWO PLACES BETWEEN FRAMES 16660 AND 17065 AND BETWEEN STRINGERS 6 AND 7. REPAIRED IAW FOKKER SRM 51-30-01 AND 51-30-02. 2 L 7 2 4F RT A20EU 1998072400154 19980724 00154 EU 1998 7 24 QXEA9800869 1 19980510 A 5230 DOOR FOKKER F28 F28MK4000 4990810 EU CARGO COMPT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - BOTH LOWER FORWARD AND AFT CORNERS ON AFT CARGO DOOR ARE DENTED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-0 2. 2 L 7 2 4F RT A20EU 1998072400155 19980724 00155 EU 1998 7 24 QXEA9800870 1 19980526 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - FRAME 16060 IS CRACKED APPROXIMATELY 5/8 INCH JUST OUTBOARD OF STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-13, FIG URE 2, PAGE 4. 2 L 7 2 4F RT A20EU 1998072400156 19980724 00156 EU 1998 7 24 QXEA9800871 1 19980621 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - FORWARD CUTOUT FOR BLANKING PLATE AREA ON BOTTOM FUSELAGE SKIN HAS CORROSION. REPAIRED IAW HORIZON AIR EA 4-53-46 3 AND 4-53-446. 2 L 7 2 4F RT A20EU 1998072400157 19980724 00157 EU 1998 7 24 QXEA9800872 1 19980621 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - CORROSION ON SKIN AND IN BETWEEN ANTENNA DOUBLER INSIDE FORWARD CARGO PIT AT AFT CUTOUT AREA FOR BLANKING PLATE ON BOTTOM FUSELAGE SKIN. REPAIRED IAW HORIZON AIR EA 4-53-463 AND EA 4-53-446. 2 L 7 2 4F RT A20EU 1998072400158 19980724 00158 EU 1998 7 24 QXEA9800873 1 19980621 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - PITTING CORROSION ON THE INSIDE SURFACE OF THE FORWARD BLANKING PLATE. REPAIRED IAW HORIZON AIR EA 4-53-463, EA 4 -53-446 AND FOKKER SRM 51-11-4. 2 L 7 2 4F RT A20EU 1998072400159 19980724 00159 EU 1998 7 24 QXEA9800874 1 19980521 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - AFT CARGO DOOR FORWARD FRAME HAS CRACK AT NUT PLATE FOR DOOR STAY FITTING. REPAIRED IAW FOKKER SRM 52-30-00, PAGE 8 AND SRM 51-31-01, PAGES 1-17. 2 L 7 2 4F RT A20EU 1998072400160 19980724 00160 EU 1998 7 24 QXEA9800875 1 19980512 A 5230 DOOR FOKKER F28 F28MK4000 4990810 EU CARGO COMPT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - BOTH LOWER FORWARD AND AFT CORNERS ON AFT CARGO DOOR DENTED. REPAIRED IAW FOKKER SRM 53-30-00, PAGE 9. 2 L 7 2 4F RT A20EU 1998072400161 19980724 00161 EU 1998 7 24 QXEA9800876 1 19980525 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - DEEP CORROSION ON FRAME CAP AT NUT PLATE HOLE ON FRAME 6805 BETWEEN STRINGERS 73 AND 74. REPAIRED IAW HORIZON AIR EA 4-53-445. 2 L 7 2 4F RT A20EU 1998072400162 19980724 00162 EU 1998 7 24 QXEA9800877 1 19980521 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - AFT CARGO DOOR FORWARD FRAME REQUIRES REPLACEMENT. REPLACED IAW FOKKER SRM 52-30-00, PAGE 8 AND SRM 51-31-01, PAG ES 1-17. 2 L 7 2 4F RT A20EU 1998072400163 19980724 00163 EU 1998 7 24 QXEA9800878 1 19980605 A 5230 DOOR FOKKER F28 F28MK4000 4990810 EU CARGO COMPT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - AFT CARGO DOOR HAS TOOLING DAMAGE IN RADIUS. REPAIRED IAW FOKKER SRM 51-10-05 AND SRM 53-02-12. 2 L 7 2 4F RT A20EU 1998072400164 19980724 00164 EU 1998 7 24 QXEA9800879 1 19980621 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 4150 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PDX - DENT IN RIGHTHAND FUSELAGE SKIN AT STATION 4150MM AND WL-700MM 1.0 WIDE AND .035 DEEP. REPAIRED IAW FOKKER SRM 53 -01-01, PARAGRAPH 5A (2), PAGE 8. 2 L 7 2 4F RT A20EU 1998072400165 19980724 00165 EU 1998 7 24 QXEA9800963 1 19980713 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 SEA - LIGHT INOPERATIVE IN AISLE OVERHEAD EMERGENCY EXIT SIGN. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NOR MAL. 2 L 7 2 4F RT A20EU 1998072400166 19980724 00166 EU 1998 7 24 QXEA9800964 1 19980714 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 PDX - SOME LIGHTS OUT ON CENTER AISLE EXIT SIGN. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998072400167 19980724 00167 EU 1998 7 24 98FDEA00456 1 19980716 A 3230 CONTROLLER AIRBUS 310 A310222 3930315 EU LANDING GEAR MALFUNCTION A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 422FE 346 98-0178 STA-CEB: LANDING GEAR WOULD NOT RETRACT AFTER T/O. GEAR HANDLE STUCK IN MID DETENT. LANDED ASAP. PERFORMED B ITE CHECK ON PROX DETECTION UNIT. NO FAULT FOUND. RESET CONTROLLER. CHECKED PROX SWS VISUALLY, GOOD CONDITION. NO EV IDENCE OF LEAKS AND ALL LANDING GEAR C/B,S IN ACFT OK TO CONTINUE PER TSM 32-30- FIG 108. 2 L 7 2 4F RT A35EU 1998072400168 19980724 00168 NM 1998 7 24 98FDEA00458 1 19980717 A 3610 6558809194303 DUCT BOEING 727 727225 1384077 NM NR 1 PYLON BROKEN A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 466FE 21292 98-0180 STA-MEM: SHORTLY AFTER T/O THE ENG 1 STRUT OVERHEAT LIGHT CAME ON. COMPLETE THE RED TAB PROCEDURES PAGES 2-7-1 0 AND 2-7-11 AND THE LIGHT EXTINGUISHED AFTER RETARD THE NR 1 THRUST LEVER NR 1 THRUST WAS SLOWLY RESTORED AND THE LIGHT REMAIN EXTINGUISH WITH A GOOD OVERHEAT SYS TEST. RED TABS SAY BLEED AIR LEAK IS ON THE FUSELAGE SIDE OF THE BLEED AIR VALVE. FOUND BROKEN THRUST REVERSER PNEUMATIC SUPPLY LINE FROM 8TH AND 13TH STAGE DUCT. FITTING ON DUCT ELBOW ALSO HAS DAMAGE THREADS. REINSTALLED BLEED DUCT. NEED LEAK CHECK ON DUCT AND SHIMMING OF FIREWALL SWIVEL AND LEAK CHECK. ADJU STED THEN TIGHTENED SWIVEL COUPLING AND V CLAMPS. ALSO, REMOVED AND REPLACED NR 1 ENG BLEED DUCTING ALL FITTINGS AND CL 2 L 7 3 4F A3WE 1998072400169 19980724 00169 WP 1998 7 24 ABXA9800629 1 19980714 A 3260 DS077S059 CONNECTOR DOUG DC9 DC931 3022065 WP RT MLG WW LOOSE A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 946AX 47003 GEAR DOOR OPEN LIGHT STAYED ON DURING INITIAL RETRACTION. RECYCLED GEAR, LIGHT WENT OUT. SECURED THE RIGHT MAIN LANDIN G GEAR SWITCH CANNON PLUG BACKSHELL. 2 L 7 2 4F A6WE 1998072400170 19980724 00170 WP 1998 7 24 ABXA9800630 1 19980716 A 3350 41B004AD07G BATTERIES DOUG DC9 DC932F 3022067 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 909AX 47148 EMERGENCY LIGHTS WERE DIM. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1998072400171 19980724 00171 WP 1998 7 24 ABXA9800631 1 19980714 A 3260 7000010101 SWITCH DOUG DC9 DC931 3022065 WP LT MLG DOOR DEFECTIVE A ABXA K NONE N FALSE WARNING CR CRUISE 1 GL 23 946AX 47003 ON GEAR UPLATCH CHECK, 'GEAR DOOR OPEN' LIGHT CAME ON AND STAYED ON THROUGH SUBSEQUENT GEAR RECYCLING AND SECOND UPLATCH CHECK. LIGHT WENT OUT WHEN GEAR HANDLE WAS RETURNED TO UP POSITION. REPLACED LEFT MAIN GEAR DOOR SWITCH. 2 L 7 2 4F A6WE 1998072400172 19980724 00172 WP 1998 7 24 ABXA9800632 1 19980716 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941AX 47419 EMERGENCY EXIT LIGHTS WERE FLICKERING AND VERY DIM. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1998072400173 19980724 00173 WP 1998 7 24 ARWA9807124 1 19980717 A 5312 BULKHEAD BRACKET DOUG DC8 DC862 3021970 WP AFT PRESS BLKHD CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 BOTH ATTACH BRACKETS HOLDING PRESS. SEALS TRUMPETS ARE CRACKED AT AFT PRESSURE BULKHEAD AREA. FABRICATED REPAIR AND IN STALLED IN ACCORDANCE WITH JOSSAIR, CO EO NR18R539001. WORK ACCOMPLISHED UNDER ARROW AR FORM JW3B, WORK ORDER 980802, C ONTROL NR 5009. 2 L 7 4 4F 4A25 1998072400174 19980724 00174 WP 1998 7 24 ARWA9807125 1 19980717 A 5320 SUPPORT DOUG DC8 DC862 3021970 WP BS 1540 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 FLOOR SUPPORT CROSS BEAM AT STATION 1540 HAS CORROSION. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED IN ACCORDANCE WITH JOSSAIR, CO EO NR 18R537001. WORK ACCOMPLISHED UNDER ARROW AIR, INC FORM JW3B, WORK ORDER NR 980802, C ONTROL NR 5006. 2 L 7 4 4F 4A25 1998072400175 19980724 00175 WP 1998 7 24 ARWA9807126 1 19980717 A 3411 B-NUT DOUG DC8 DC862 3021970 WP PITOT-STATIC SYS LOOSE A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 802BN 45909 30 KNOT SPLIT ON AIRSPEED AND 1000 SPLIT ON ALTIMETERS CLIMBING THROUGH FL 310, SPLITS ON BOTH WERE INCREASING, BOTH HIG H ON F/O SIDE. SECURED LOOSE B NUT IN CEILING OF AIRCRAFT BELLY. ACCOMPLISHED PITOT-STATIC CHECK. OPS AND LEAK CHECK ED NORMAL IAW MM 34-12-0. 2 L 7 4 4F 4A25 1998072400176 19980724 00176 WP 1998 7 24 ARWA9807127 1 19980717 A 2120 COOLING VALVE DOUG DC8 DC862 3021970 WP RADIO RACK MISWIRED A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 802BN 45909 AIRCRAFT CABIN ALT AT 9000 AND CLIMBING WITH 3 T/C'S OPERATING AT 31,000 FOUND RADIO RACK COOLING VALVE OPEN WHEN AIRBOR NE. CORRECTED WIRING AT RELAY R2-64, OPS NORMAL IAW MM 21-50-0. PRESSURIZATION NORMAL ON RUN-UP IAW MM 21-30-0. 2 L 7 4 4F 4A25 1998072400177 19980724 00177 WP 1998 7 24 ARWA9807128 1 19980717 A 2450 50130003 BUSS PANEL DOUG DC8 DC863F 302198F WP COCKPIT FAILED A ARWA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 19 441J 45988 WHILE PERFORMING PRE-FLIGHT, COCKPIT FILLED WITH SMOKE. POWER SHUT DOWN, PROBLEM FOUND TO BE, SHORTED BUSS PROTECTION P ANEL AND ASSOCIATED WIRING. REMOVED AND REPLACED BUSS PROTECTION PANEL AND BURNT WIRING SYSTEM; TESTED IAW MM 24-20-7. FOUND NOTE: SWISPORT GPU NR 350 IN USE AT THE TIME OF PROBLEM FOUND OK, TO HAVE FLUCTUATING VOLTS AND FREQUENCY. 2 L 7 4 4F 4A25 1998072400178 19980724 00178 WP 1998 7 24 VJ9800225 1 19980715 A 2612 591461325 CONNECTOR DOUG DC9 DC932 3022066 WP NR 1 ENGINE DIRTY A ZZDA O OTHER N FALSE WARNING CR CRUISE 1 SO 15 967VV 47170 FIRE LOOP B LIGHT ILLUMINATED ON NR 1 ENGINE WITHOUT ANY OTHER WARNING BEING EVIDENCED. FOLLOWED PROCEDURES AND TESTED OPPOSITE LOOP WHICH TESTED GOOD. AIRCRAFT LANDED WITHOUT INCIDENT AND UPON INSPECTION OF BLEED AIR DUCTS NO LEAKS WERE DETECTED. ALSO, INSPECTED B LOOP AND NO DEFECTS WERE NOTED; AS PRECAUTIONARY MEASURE CLEANED AND SECURED APRON CONNECTO RS; B SYSTEM OPS CHECKED GOOD IAW MM 26-10. 2 L 7 2 4F A6WE 1998072400179 19980724 00179 WP 1998 7 24 VJ9800226 1 19980715 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 919VV 47260 FWD OVERWING EMERGENCY LIGHTS OUT. REPLACED FWD OVERWING EMERGENCY LIGHT BATTERY POWER SUPPLY IAW 33-50; OPS CHECKED GO OD. 2 L 7 2 4F A6WE 1998072400180 19980724 00180 NM 1998 7 24 VJ9800227 1 19980716 A 3350 900835 BATTERY PACK BOEING 737 737214 138446R NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 EMERGENCY LIGHTING BATTERY PACK INOP. REPLACED BATTERY PACK. 2 L 7 2 4F A16WE 1998072400181 19980724 00181 NM 1998 7 24 CALA9801259 1 19980716 A 3233 65446104 ACTUATOR BOEING 737 737524 1384721 NM NLG INOPERATIVE A CALA O OTHER O OTHER AP APPROACH 1 SW 09 14645 2615 28906 WHEN LANDING GEAR WAS EXTENDED ON APPROACH TO IAH, THE NOSE GEAR GAVE A HARD LOUD THUD THAT COULD BE FELT ON AIRCRAFT FL OOR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG RETRACT ACTUATOR AT FAULT. THE ACTUATOR WAS REMO VED AND REPLACED IAW MM 32-33-11. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1998072400182 19980724 00182 NM 1998 7 24 CALA9801260 1 19980716 A 3230 1U1085 SEQUENCE VALVE BOEING 727 727224 1384076 NM RT MLG LEAKING A CALA A J UNSCHED LANDING DUMP FUEL K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 32725 33020 20655 THE A HYDRAULIC SYSTEM PRESSURE AND FLUID WAS LOST AFTER GEAR WAS RETRACTED DEPARTING IAH. FUEL WAS DUMPED AND THE AIRC RAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG LOCK SEQUENCE VALVE LEAKING. T HE VALVE WAS REMOVED AND REPLACED IAW MM 32-32-31. LEAK AND OPERATIONAL CHECKS WERE GOOD IAW MM 32-32-0. 2 L 7 3 4F A3WE 1998072400183 19980724 00183 WP 1998 7 24 CALA9801261 1 19980716 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOOR GILL LINING ATTACH ANGLE CORRODED IN AFT CARGO COMPARTMENT AT STA 996, BL 0 TO LBL 6. THE CORROD ED SECTION OF ANGLE WAS CUT OUT. TWO L-ANGLES AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-4 , 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998072400184 19980724 00184 NE 1998 7 24 CALA9801262 2 19980716 A 7230 9527M99P09 FAN BLADE BOEING 737 737524 1384721 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE FRACTURED A CALA A UNSCHED LANDING C F.O.D. AP APPROACH 1 SW 09 14601 27314 856770 WHILE EN ROUTE, AN EMERGENCY LANDING WAS REQUIRED FOR FUEL STOP (DUE TO A COMBINATION OF LONG TAXI TIME IN EWR AND WEATH ER EN ROUTE). THE AIRCRAFT WAS DIVERTED TO JAX AND WHILE ON FINAL APPROACH THE NR 1 ENGINE FAILED. THE AIRCRAFT LANDED AT JAX WITHOUT INCIDENT. MAINTENANCE FOUND INTERNAL DAMAGE TO THE NR 1 ENGINE NOSE COWL, BELIEVED TO BE CAUSED BY SEPA RATION OF A FAN BLADE. THE NR 1 ENGINE WILL BE REMOVED AND REPLACED. *S/D* INVESTIGATION CONCLUDED THAT THE PRIMARY C AUSE OF ENGINE FAILURE WAS DUE TO SEPARATION OF A FAN BLADE CAUSED BY FOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998072400185 19980724 00185 WP 1998 7 24 UPS98827172 1 19980715 A 3231 DOOR DOUG DC8 DC871F 302199D WP LT MLG OUT OF ADJUST A IPXA K NONE J WARNING INDICATION CR CRUISE 1 SO 01 798UP 45898 RED DOOR NOT LATCHED, LIGHT ILLUMINATED IN FLT. LEFT ALT MAIN GEAR DOOR LIGHT ALSO ILLUMINATED IN FLT SEVERAL, ATTEMPTS WERE MADE TO RECYCLE GEAR TO NO AVAL. DIVERTED TO CAE PER DISPATCH REQUEST. CHECKED MLG DOOR LT FOLLOW UP PER 323105, CHECKED OK, CHECKED LT MLG DOOR UPLATCH PER 323104. REMOVED SHIMS FROM DOOR ROLLERS CHECKS OK, ALL DIMENSIONS WITHIN L IMITS PER 323104. 2 L 7 4 4F RT 4A25 1998072400186 19980724 00186 NM 1998 7 24 QXEA9800949 1 19980715 A 5210 85210200103 STOP DHAV DHC8 DHC8102 2809003 NM CABIN DOOR MISSING A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 814PH 43 ALW - MAIN CABIN DOOR MISSING BLACK RUBBER STOPPER FOR THE EXTERNAL HANDLE. AIRCRAFT FERRIED FROM ALW TO SEA FOR REPAIR S. IN SEA, REPLACED THE BLACK RUBBER STOPPER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998072400187 19980724 00187 NM 1998 7 24 QXEA9800962 1 19980715 A 3350 10005511 LIGHT DHAV 82510202001 DHAV DHC8 DHC8102 2809003 NM COCKPIT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 816PH 15165 6630 54 PDX - OVERHEAD EMERGENCY LIGHT IN COCKPIT ABOVE OBSERVER SEAT WILL NOT HOLD A CHARGE. REPLACED LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998072400188 19980724 00188 NM 1998 7 24 QXEA9800965 1 19980714 A 3350 6104789 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 829PH 304 SEA - DURING THE TIME CHANGE OF THE EMERGENCY LIGHT BATTERY PACKS, THE BATTERY PACK FOR PS4 WAS FOUND TO BE BAD FROM STO CK. REPLACED BATTERY PACK. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998072400189 19980724 00189 EU 1998 7 24 98FDEA00457 1 19980716 A 3610 9354M89G01 DUCT AIRBUS 310 A310203 EU NR 2 ENGINE RUPTURED A FDEA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 25 405FE 237 STA-OAK: ON CLIMB 250 KTS/10000. ADVANCED THROTTLE FOR CLIMB AND NR 2 ENG FIRE WARNING ILLUMINATED B-LOOP WAS CHECKED AND TURNED OFF. LEVELED OFF THEN STARTED TO CLIMB AGAIN. FIRE WARNING ILLUMINATED AGAIN THEN GOT HOT AIR SUPPLY OVERHE AT. RETURNED TO OAK. FOUND RUPTURED HIGH PRESS DUCT. REMOVED AND REPLACED DUCT PERFORM ENG RUN PER JRH. NO LEAKS NOT ED. 2 L 7 2 4F RT A35EU 1998072400190 19980724 00190 NM 1998 7 24 98FDEA00459 1 19980717 A 5320 69144925 SPLICE BOEING 727 72722 1384002 NM BS 440 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 193FE 19142 CRACKED STRINGER SPLICE AT BS 440, STR 20 RT. *S/D* REPLACED STRINGER SPLICE, BS 440, STR 20 RT IAW FED-EX SRM 53-10-3 . 2 L 7 3 4F A3WE 1998072400191 19980724 00191 NM 1998 7 24 98FDEA00460 1 19980717 A 7830 DUCT BOEING 727 727225 1384077 NM NR 1 ENGINE CRACKED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 466FE 21292 98-0181- STA-MEM, NR 1 ENG HAD STRUT OVERHEAT ON TAKEOFF PULLED THRUST LEVER BACK AND PERFORMED RED TAB PROCEDURES. REM OVED PANELS FROM LWR STRUT. FOUND LINE PN S145061408-0090 IS A BRAID LINE CRACK IN MIDDLE HALFWAY. CHECK VALVE FOR PRO PER INSTALL. VALVE INSTALLED CORRECT PER MM 78-30-10 PG 3. REMOVED THRUST REVERSER DUCT FROM NR 1 ENGINE HYDRAULIC LIN E ABOVE. REMOVED DUCT AND VALVES IAW 36-10-00. REINSTALLED DUCT, BLEED VALVE 13TH STAGE VALVE. NEED LEAK CK AT PWR FO R 8 MIN PERFORM HIGH PWR RUN. NO LEAK, NO STRUT OVERHEAT. 2 L 7 3 4F A3WE 1998072400192 19980724 00192 NM 1998 7 24 98FDEA00461 1 19980717 A 5313 6523535 STRINGER BOEING 727 72721C 138400M NM BS 560-580 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 CORROSION (C53-224-02) ON STRINGER 1 BL 0 BS 560 TO 580, BS 520 TO 540. *S/D* REMOVED CORROSION FROM STR 1, FOUND IT T O BE OUT OF LIMITS. REPAIRED STR 1, BS 520 TO 540 IAW FED-EX SRM 53-10-3. 2 L 7 3 4F A3WE 1998072400193 19980724 00193 NM 1998 7 24 98FDEA00462 1 19980717 A 5313 654237026 STRINGER BOEING 727 72721C 138400M NM BS 380-460 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 CORROSION (C53-224-02) ON STRINGER 9 LT, BS 380 TO 460. *S/D* REPAIRED STR 9 LT, BS 380 TO 480 PER FED-EX SRM 53-10-3. 2 L 7 3 4F A3WE 1998072400194 19980724 00194 NM 1998 7 24 DL72S981478 1 19980715 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 7997 21145 00000 LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY AND CHANGED BATTERY PACK PER M/M. OP CHECK GOOD BATTERY PAC K REMOVED 7997. BATTERY PACK INSTALLED, C6495 P/N 334102486. 2 L 7 3 4F A3WE 1998072400195 19980724 00195 WP 1998 7 24 DLL14981479 1 19980716 A 2560 GIRT BAR LKHEED 1011 1011385115 5265015 WP R4 DOOR OUT OF ADJUST A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 740DA 193C1244 GIRT BAR INOP, WILL NOT ENGAGE LATCH WHEN R4 DOOR IS CLOSED. ADJUSTED GIRT BAR, OPS CHECK NORMAL. 2 L 7 3 4F A23WE 1998072400196 19980724 00196 WP 1998 7 24 DLL14981481 1 19980716 A 3246 L1011250500ER WHEEL LKHEED 1011 1011385115 5265015 WP MLG OUT OF BALANCE A DALA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 SO 27 1738D 193C1234 AT ROTATION FELT VIBRATION AND HEARD LOUD NOISE. NOTICED TRUCK LIGHT, HYDRAULIC SYS AND FUEL SYS LIGHTS. A AND C SYS S HOW .25 AND .50 QTY. TANK 1 INBD BOOST PUMP LOW LIGHT ON REPLACED WHEEL ASSY. 2 L 7 3 4F A23WE 1998072400197 19980724 00197 NM 1998 7 24 DL757981482 1 19980716 A 3350 CHARGER BPS73 BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 654DL 10592 24394 SEAT 39 THROUGH 45 SEAT MOUNTED EMERGENCY LITES WILL NOT TEST. REPLACED CHARGER ASSY M-9002. OPS NML. 2 L 7 2 4F RT A2NM 1998072400198 19980724 00198 NM 1998 7 24 DL72W981485 1 19980716 A 3350 90085A BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2816W 20872 000000 WORKING L/O, NR 2 FOUND AIRSTAIR UPPER EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER M/M OP CK GOOD. 2 L 7 3 4F A3WE 1998072400199 19980724 00199 NM 1998 7 24 DLM88981488 1 19980716 A 3244 TIRES 5701195501 DOUG MD88 MD88 3023688 NM RT MLG FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 914DE 49957 ON TAKEOFF ROLL AT 15O KTS, TAIL COMPT TEMP HI MSG. ABORTED TAKEOFF. WHEELS NR 1 NR 2 AND NR 4 FUSE PLUGS MELTED AND T IRES DEFLATED. FOUND HOT AIR LEAK AROUND RT PACK HEAT EXCHANGER, DEFERRED RT PACK. 2 L 7 2 4F RT A6WE 1998072400200 19980724 00200 NM 1998 7 24 DLM88981489 1 19980715 A 2910 B-NUT DOUG MD88 MD88 3023688 NM LT TR CTL VALVE LOOSE A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 946DL 49819 LEFT HYD PRESS LOW LIGHT ANNUC 10 MINUTES FROM LANDING. LT ENGINE HYD PUMP OFF. AUX AND XFER PUMP ON PER POM. PRESS N ORMAL BUT QTY STILL DECREASING. FOUND LEAK AT B-NUT AT LT T/R CONT VLV TIGHTENED. 2 L 7 2 4F RT A6WE 1998072400201 19980724 00201 NM 1998 7 24 DL72S981490 1 19980717 A 5320 WEB BOEING 727 727232 1384082 NM BS 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 539DA 22385 FOUND AT D-1 LETTER CK, .375 IN CRACK ON LIGHTNING HOLE ON AIRSTAIRS CUTOUT VERTICAL WEB AT STA 1228. FOUND .375 INCH C RACK ON LIGHTNING HOLE ON AIRSTAIRS CUTOUT VERTICAL WEB AT STA 1248. FOUND .25 INCH CRACK ON LIGHTNING HOLE ON AIRSTAIR S CUTOUT VERTICAL WEB AT STA 1248. REPAIR PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998072400202 19980724 00202 NM 1998 7 24 DL76L981498 1 19980718 A 2121 732591F FAN BOEING 767 767332 1382001 NM CARGO COMPT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 187DN 27582 DURING CRUISE, AT FL 330, EXPERIENCED SMOKE (ELEC) FROM F/O PANEL AND A SOUND OF A MOTOR WINDING DOWN PLUS SEVERAL EICAS MSGS. FWD CARGO HEAT/FWD EZ EXH FAN/AFT CARGO HEAT/BULK CARGO HEAT. SMOKE QUIT AND FOUND C/B FOR FWD EXH EQUIP COOL F AN POPPED. FOUND FWD EQUIP EXH FAN INOP. POWER GOOD BUT FAN WILL NOT WORK. FWD TO MCO PER MEL 21-58-04B. FAN NEEDS T O BE REPLACED THIS STATION. 2 L 7 2 4F RT A1NM 1998072400203 19980724 00203 NM 1998 7 24 DL72S981499 1 19980719 A 3350 LIGHT 1619 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 470DA 20747 AFT OF L1 DOOR EMERGENCY EXIT LIGHT OUT. RELAMPING NO HELP HAD TO CHANGE THE LIGHT ASSY. 2 L 7 3 4F A3WE 1998072400204 19980724 00204 NM 1998 7 24 DLM88981502 1 19980719 A 3350 RPS1 POWER SUPPLY DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 964DL 49983 REAR EMERGENCY PATH LIGHTS INOP. REPLACED PWR SUPPLY. OPS NML. 2 L 7 2 4F RT A6WE 1998072400205 19980724 00205 NE 1998 7 24 DL73E981503 2 19980719 A 7230 COMPRESSOR BOEING 737 737247 138448D NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE BIRD STRIKE A DALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 27 245WA 26879 23519 717162 AFTER TAKEOFF, BIRDSTRIKES FOLLOWED BY COMPRESSOR STALLS ON THE NUMBER 1 ENGINE. CHANGED FAN. 2 L 7 2 4F 4 F A16WE E2EA 1998072400206 19980724 00206 WP 1998 7 24 SCNA98529 1 19980718 A 5415 FITTING DOUG DC10 DC1015 3022118 WP LT PYLON WORN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE LEFT WING PYLON SUPORT FITTING (FOOTSTOOL) WAS FOUND TO HAVE TWO EACH WEAR MARKS APPROXIMATELY 1 .5 AND AFT OF THE LEADING EDGE AND IS 5 LONG AND APPROXIMATELY .002 DEEP. THE SECOND MARK IS AT THE AFT END OF THE HOL E RUNNING 360 DEG AROUND THE HOLE AND APPROXIMATELY .0024 DEEP. THE FITTING WAS MACHINED PER BCAG FAX DATED 6/16/98 ACT ION NR 371101 SND DWG SBX SBA 98 0136TR AND APPROVED BY 8110 3. THE REPAIR COMPLIED WITH SUN COUNTRY ENGINEERING ORDER 57 5605 1. DATED 7/13/98 2 L 7 3 4F A22WE 1998072400207 19980724 00207 WP 1998 7 24 SCNA98530 1 19980718 A 5720 TIP DOUG DC10 DC1015 3022118 WP LT WING DENTED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE LEFT WING TIP WAS FOUND TO HAVE SEVEN DENTS, ALL LOCATED AT THE RIBS, ALL AT A VERTICLE LENGTH OF 1 AND A DEPTH OF .075 TO .020 ALL ARE SMOOTH WITHOUT CRACKS. REMOVED AND REPAIRED LEFT AND WINGTIP IAW SRM 571000 FIG 39, REINSTALLED SAME LT WINGTIP IAW DC1015 MM 572301 3(B) AND SRM 513101. BOEING TELEX 98 07 13 AND SCA EO 57 5601 1. 2 L 7 3 4F A22WE 1998072400208 19980724 00208 NM 1998 7 24 P5CA9801175 1 19980713 A 5414 SKIN BOEING 747 747122 1384872 NM NR 3 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 #3 ENGINE PYLON EXTERNAL SKIN OUTBOARD LOWER HALF SKIRT PANEL HAS NUMEROUS LOOSE AND WORKING FASTENERS. REMOVED AND REPL ACED FASTENERS PER 51-10-01. 2 L 7 4 4F A20WE 1998072400209 19980724 00209 NM 1998 7 24 P5CA9801176 1 19980713 A 5320 SILL BOEING 747 747122 1384872 NM CARGO DOORWAY DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 INNER MAIN CARGO DOOR SILL PROTECTOR DAMAGED. REMOVED AND REPLACED SILL PROTECTOR PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998072400210 19980724 00210 NM 1998 7 24 P5CA9801177 1 19980713 A 5753 SKIN BOEING 747 747122 1384872 NM RT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 RIGHT OUTBOARD FLAP, MID FLAP LOWER SKIN JUST OUTBOARD OF JACK SCREW HAS A HOLE IN THE SKIN. REMOVED, SANDED DAMAGED AR EA, PREPARED FOR BONDING, POTTED DAMAGED .5 INCH DIA APPLIED 3 PLY FIBERGLASS LAY-UP IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998072400211 19980724 00211 NM 1998 7 24 P5CA9801178 1 19980712 A 2170 7503993 WATER SEPARATOR BOEING 747 747122 1384872 NM NR 2 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NR 2 WATER SEPARATOR DELAMINATED AND CRACKED. REMOVED AND REPLACED NR 2 WATER SEPARATOR PER MM 21-51-05. 2 L 7 4 4F A20WE 1998072400212 19980724 00212 WP 1998 7 24 RRXA98252 1 19980711 A 2612 899096 FIRE LOOP DOUG DC8 DC873F 302199F WP NR 3 ENGINE MALFUNCTIONED A RRXA K NONE N FALSE WARNING CR CRUISE 1 WP 15 2674U 46062 INTERMITTENT FIRE WARNING IN FLIGHT AND ON TAXI IN, FIRE TEST AND SHORT CIRCUIT CHECKED NORMAL. INSPECTED FIRE LOOPS AN D RELATED WIRING, NO DEFECTS NOTED, OPS CK NORMAL. REMOVED AND REPLACED RT AFT, LT FWD, RT FWD, AND AFT CENTER TOP FIRE LOOPS AS PRECAUTIONARY ACTION, NR 3 ENG FIRE WARNING CKS NORMAL AFTER COMPONENT CHANGES. 2 L 7 4 4F RT 4A25 1998072400213 19980724 00213 WP 1998 7 24 RRXA98253 1 19980715 A 2612 D5020 FIRE AMPLIFIER DOUG DC8 DC862 3021970 WP NR 4 ENGINE MALFUNCTIONED A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 993CF 46028 ON CLIMBOUT, NR 4 ENG INDICATED FIRE. PERFORMED THE ENG FIRE CK LIST ACCORDING TO QRH, FIRED NR 4 BOTTLE, FIRE INDICATE D OUT. ON LDG ROLL, NR 4 ENG INDICATE FIRE AGAIN, PERFORM THE EMERG EVAC CK LIST WITH ENG COWLING OPEN, NO VISIBLE SIGN THAT ENG ON FIRE. *S/D* REMOVED AND REPLACED LOWER ENGINE FIRE LOOP CONN, FIRE CONTROL AMP, CKD ALL BLEED AIR LINES A ND OTHER CIRCUITS, GND RAN ENG, NO FIRE WARNING, SYSTEM TEST NORMAL IAW DC8 MM 26-20. 2 L 7 4 4F 4A25 1998072400214 19980724 00214 EU 1998 7 24 98ZZZX2405 1 19980513 A 3230 1005383400 VALVE MAGNAGHI AEROSP ATR42 ATR42300 8680920 EU MLG FAILED A A TRBA O OTHER J WARNING INDICATION AP APPROACH 1 SO 21 972NA 21338 36 023 NORMAL LANDING GEAR EXTENSION FAILED. EMERGENCY LANDING GEAR EXTENSION HAD TO BE USED. (STX) C/W MEL BOOK PROCEDURES A ND DEFERRED LANDING GEAR RETRACT SYSTEM PER MEL 32-03-C. (SJU) REPLACED LANDING GEAR SELECTOR VALVE AND PERFORMED OPERA TIONAL CHECK. FOUND SYSTEM OWRKING PROPERLY. MEL CLEARED. 2 H 7 2 4T RT A53EU 1998072400216 19980724 00216 NM 1998 7 24 TSAA9852338 1 19980619 A 5210 66109058 PIN BOEING 737 7372Y5 1384554 NM PAX DOOR BROKEN A TSAA K NONE O OTHER NR NOT REPORTED 1 WP 13 810AL 24031 LOUD HIGH PITCHED SQUEAL COMING FROM FORWARD ENTRY DOOR. STARTED ABOVE 2 PSI. FOUND BROKEN HINGE PIN ASSY. REPLACED A SSY AND PRESSURIZED AIRCRAFT TO 7.6 PSI. NO NOISE NOTED UPON CHECK. ALSO CLEANED DOOR SEALS AND HINGE SEAT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4U RT A16WE 1998072400217 19980724 00217 NM 1998 7 24 TSAA9853311 1 19980611 A 5330 SKIN BOEING 737 7372X6C 1384552 NM BS 947 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 LAP JOINT CORRODING AT STR 24L AND BS 947, ALSO SHOWS SIGNS OF BULGING. FORWARD OF POTABLE WATER ACCESS PANEL CUT-OUT. REPAIRED PER ECO 2907. AIRCRAFT RETURNED TO SERVICE. TAT: 31,369.6 HRS. TAC: 37,949. (X) 2 L 7 2 4F RT A16WE 1998072400218 19980724 00218 NM 1998 7 24 TSAA9852312 1 19980611 A 5330 SKIN BOEING 737 7372X6C 1384552 NM BS 377 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 MAIN CARGO DOOR LOWER FRAME AT NR 2 LATCH CUT-OUT HAS A CRACK AT FORWARD OUTBOARD CORNER CUT-OUT BS 377. HFEC CONFIRMED . REPAIRED PER ECO 2912. AIRCRAFT RETURNED TO SERVICE. TAT: 31,369.6 HRS. TAC: 37,949. (X) 2 L 7 2 4F RT A16WE 1998072400219 19980724 00219 NM 1998 7 24 TSAA9851314 1 19980602 A 5311 FRAME BOEING 737 7372X6C 1384552 NM BS 325 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 816AL 23122 BODY FRAME CRACKED AT BS 325 ABOVE STR 27L (ACCESS FOR E/E COMPARTMENT UNDER PITCH CONTROL CHANNEL BOX). REPAIRED PER S RM 51-40-3. AIRCRAFT RETURNED TO SERVICE. TAT: 31,369.6 HRS. TAC: 37,949. (X) 2 L 7 2 4F RT A16WE 1998072400220 19980724 00220 NM 1998 7 24 TSAA9853318 1 19980615 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 787 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 807AL 23443 FUSELAGE SKIN CRACK APPROXIMATELY 2.5 INCHES LONG AT BS 787 AND STR 18L. VERIFIED CRACK USING HIGH FREQUENCY EDDY CURRE NT. REPAIRED PER SRM 53-30-3 FIG 1. AIRCRAFT RETURNED TO SERIVCE. TAT: 29,087.1 HRS. TAC: 34,722. (X) 2 L 7 2 4F A16WE 1998072400221 19980724 00221 NM 1998 7 24 TAOA069809 1 19980626 A 2910 65178232 MODULE BOEING 727 727225 1384077 NM FUSELAGE LEAKING A TAOA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 923TS 5153 20441 DCA/LGA - FLT 6431 - HYDRAULIC SYSTEM 'A' FAILURE WHILE ON TAXIWAY PRIOR TO DEPARTURE. REPLACED LEAKING SYSTEM 'A' ELEV ATOR FLIGHT CONTROL MODULE PER MM 27-30-91, EXAMINED SYSTEM 'A' CASE DRAIN FILTERS. REPLACED CASE DRAIN FILTERS PER MM 29-11-41. RAN ENGINES AND OPERATED ALL HYDRAULIC SYSTEMS, OPERATION CHECK NORMAL. (X) 2 L 7 3 4F A3WE 1998072400222 19980724 00222 EU 1998 7 24 SIMA981753 1 19980624 A 3350 3011151 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 3934 223 ORD - FORWARD EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1998072400223 19980724 00223 EU 1998 7 24 SIMA981721 1 19980621 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 529AM 0601 529 ORD - FLT 4151 - NINE EMERGENCY FLOOR PROXIMITY LIGHTS IN AFT OF AIRCRAFT AND ONE EXIT SIGN ON AFT WALL DO NOT ILLUMINAT E. REMOVED AND REPLACED BATTERY PACK 73WL. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1998072400224 19980724 00224 EU 1998 7 24 SIMA981712 1 19980620 A 2432 121CC01A CONTACT AEROSP ATR42 ATR42300 8680920 EU MAIN FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 275BC 5875 275 MIA - FLT 5711 - DURING FLIGHT FROM JFK TO BOS, CREW REPROTED RT ESI (ELECTRICAL SYSTEM INDICATION) LIGHT. RELATED INDI CATIONS WERE MAIN BATTERY AT 22.7 VOLTS AND NR 1 GENERATOR AMPS FLUCTUATING FROM 25 TO 50 AMPS CONTINUOUSLY. CREW DIVER TED TO PVD. SMELLED ELECTRICAL BURNING DURING DESCENT. DECLARED EMERGENCY. LANDED SAFELY. REMOVED AND REPLACED MAIN BATTERY CONTACTOR AND BPU (BATTERY PROTECTIONS UNIT). OPERATIONAL CHECK NORMAL. REF: OPER CNTRL NR 98ZZZX2407. (X) 2 H 7 2 4T RT A53EU 1998072400225 19980724 00225 EU 1998 7 24 98ZZZX2407 1 19980620 A 2432 683GC01Y01 BPU AEROSP ATR42 ATR42300 8680920 EU BATTERY FAILED A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 275BC 205 275 MIA - FLT 5711 - DURING FLIGHT FROM JFK TO BOS, CREW REPROTED RT ESI (ELECTRICAL SYSTEM INDICATION) LIGHT. RELATED INDI CATIONS WERE MAIN BATTERY AT 22.7 VOLTS AND NR 1 GENERATOR AMPS FLUCTUATING FROM 25 TO 50 AMPS CONTINUOUSLY. CREW DIVER TED TO PVD. SMELLED ELECTRICAL BURNING DURING DESCENT. DECLARED EMERGENCY. LANDED SAFELY. REMOVED AND REPLACED MAIN BATTERY CONTACTOR AND BPU (BATTERY PROTECTIONS UNIT). OPERATIONAL CHECK NORMAL. REF: OPER CNTRL NR SIMA981712. 2 H 7 2 4T RT A53EU 1998072400226 19980724 00226 EU 1998 7 24 SIMA981711 1 19980620 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST NR NOT REPORTED 1 SW 21 249AT 1323 0249 CMI - FLT 9753 - PASSENGER DOOR STEP EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SU PPLY. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1998072400227 19980724 00227 EU 1998 7 24 SIMA981698 1 19980618 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AT 11827 327 GRR - FRONT EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK AT LOCATION 29WL. OPERATIONAL C HECK GOOD. (X) 2 H 7 2 4T RT A53EU 1998072400228 19980724 00228 NM 1998 7 24 F3LA98118 1 19980701 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 365 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3584 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON STR 25R, BS 365 AT STRINGER SPLICE. MAINTENANCE REMOVED CORROSIO N (.025 INCH) AND STRINGER FROM BS 360 - BS 420, FABRICATED REPLACEMENT PARTS, AND REPAIRED PER SRM 51-40-2 AND SRM 53- 00-3. CYCLES: 1,608.0. (X) 2 L 7 2 4F RT A16WE 1998072400229 19980724 00229 NM 1998 7 24 F3LA98119 1 19980701 A 5743 BEAM BOEING 737 737301 1384611 NM MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3584 23257 PAI - DURING C-CHECK INSPECTION, REPORTED CORROSION ON LT MLG BEAM LOWER SURFACE, OUTBOARD THREE FORWARD PANEL MOUNT HOL ES. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR WASHERS, AND INSTALLED PER SRM 51-40-2, ER NR 98-0596, AND OHM 20- 10-6. CYCLES: 1,608.0. (X) 2 L 7 2 4F RT A16WE 1998072400230 19980724 00230 NM 1998 7 24 F3LA98120 1 19980701 A 5743 BEAM BOEING 737 737301 1384611 NM MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3584 23257 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION LT MLG BEAM LOWER SURFACE. INBOARD AFT PANEL MOUNT HOLE. MAINTENAN CE BLENDED CORROSION (5.50 INCHES BY 2.0 INCHES BY .010 INCH, 2.20 INCHES BY 1.80 INCH BY .010 INCH, AND 1.91 INCH BY 1. 91 INCH BY .010 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER ER NR 98-0596A AND OHM 21-10-03. CYCLES: 1,608.0. (X) 2 L 7 2 4F RT A16WE 1998072400231 19980724 00231 NM 1998 7 24 F3LA98121 1 19980701 A 5320 WEB BOEING 737 737301 1384611 NM BS 705 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3584 23257 DURING C-CHECK, INSPECTION REPORTED CORROSION ON PRESSURE WEB FLOOR, BS 705, WL 203, LBL 67. MAINTENANCE REMOVED CORROS ION (1.5 INCH BY 1.5 INCH BY .010 INCH). FABRICATED REPLACEMENT PARTS AND INSTALLED PER SRM 51-40-5, 51-40-2, AND 53-30 -51. 1,608.0 CYCLES. (X) 2 L 7 2 4F RT A16WE 1998072400232 19980724 00232 NM 1998 7 24 F3LA98122 1 19980701 A 5320 WEB BOEING 737 737301 1384611 NM BS 795-867 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3584 23257 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION AROUND NUTPLATE HOLES ON AFT CARGO DOOR THRESHOLD SUPPORT WEB, BS 79 5 TO BS 867. MAINTENANCE REMOVED CORROSION (1 INCH BY 1 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40 -2. CYCLES: 1,608.0. (X) 2 L 7 2 4F RT A16WE 1998072400233 19980724 00233 CE 1998 7 24 98ZZZX2408 1 19980622 A 3260 LIGHT BEECH 1900 1900C 1154161 CE NLG FAILED A GUUA K NONE N FALSE WARNING LD LANDING 1 SO 19 154GA UB25 FLL/TPA - FLT 9164 - NOSE GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE UNTIL 2 MINUTES AFTER MAIN GEAR. FERRIED AIRC RAFT TO MIAMI. PERFORMED GEAR SWING SEVERAL TIMES WITH AIRCRAFT ON JACKS. COULD NOT DUPLICATE DISCREPANCY. (X) 2 L 7 2 4T RT A24CE 1998072400234 19980724 00234 CE 1998 7 24 98ZZZX2409 1 19980624 A 3260 H111541 SWITCH BEECH 1900 1900C 1154161 CE MLG INTERMITTENT A GUUA K NONE O OTHER CR CRUISE 1 SO 19 86UE UC86 TPA/MIA - FLT 5000 - LANDING GEAR MOTOR ENGAGED IN-FLIGHT (TWO TIMES). REMOVED AND REPLACED BOTH LEFT AND RIGHT UPLOCK SWITCHES. (X) 2 L 7 2 4T RT A24CE 1998072400235 19980724 00235 CE 1998 7 24 98ZZZX2410 1 19980603 A 2910 1013881075 LINE BEECH 1900 1900 1154160 CE HYDRAULIC SYSTEM CRACKED A GUUA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SO 19 192GA UB17 EYW/MIA - FLT 5300 - LANDING GEAR DOES NOT RETRACT. REMOVED AND REPLACED RIGHT HAND 'UP' HYDRAULIC LINE. (X) 2 L 7 2 4T RT A24CE 1998072400236 19980724 00236 WP 1998 7 24 HALA9800173 1 19980624 A 3350 1001191 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 217 47764 HNL - (LOG PAGE NR A143522). FORWARD EMERGENCY LIGHT BY THE FORWARD F/A SEAT IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY BATTERY PACK. OPS CHECK WAS OK. (X) 2 L 7 2 4F RT A6WE 1998072400237 19980724 00237 WP 1998 7 24 HALA9800177 1 19980626 A 3350 41B004A007G3 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 601AP 47658 HNL - (LOG PAGE NR A165001) - BOTH LEFT AND RIGHT VENTRAL STAIR EMERGENCY LIGHTS ARE INTERMITTENT. REPLACED THE EMERGEN CY LIGHT BATTERIES AND THE OPERATIONAL CHECK WAS OK. (X) 2 L 7 2 4F RT A6WE 1998072400238 19980724 00238 WP 1998 7 24 HALA9800178 1 19980625 A 3350 66030451 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN FAILED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 660HA 9507 48122 HNL - FLT 103 - (LOG PAGE NR A144870) - BOTH FORWARD OVER-WING EXIT EMERGENCY LIGHTS DO NOT COME ON. REPLACED THE OVER- WING POWER SUPPLY AND THE OPERATIONAL CHECK WAS OK. (X) 2 L 7 2 4F RT A6WE 1998072400239 19980724 00239 WP 1998 7 24 HALA9800179 1 19980626 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 601AP 47658 HNL - (LOG PAGE NR A165002) - CEILING EMERGENCY LIGHT ABOVE ROW 25/26 IS INOPERATIVE. REPLACED THE EMERGENCY LIGHT FIXT URE AND THE OPERATIONAL CHECK WAS OK. (X) 2 L 7 2 4F RT A6WE 1998072400240 19980724 00240 NE 1998 7 24 HALA9800174 2 19980627 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE NR 2 BIRD STRIKE A HALA K NONE O OTHER TO TAKEOFF 1 WP 13 662HA 47742 MKK - FLT 095 - (LOG PAGE NR A144626) - BIRD STRIKE RIGHT WING. CLEANED AREA NO DAMAGE NOTED. VISUAL CHECKED RIGHT WIN G AND NR 2 ENGINE ASSY. STABILIZER CHECKED OK. OK FOR SERVICE. (X) 2 L 7 2 4F 4 F RT A6WE E2EA 1998072400241 19980724 00241 WP 1998 7 24 HALA9800172 1 19980623 A 2720 SPRING DOUG DC9 DC951 3022051 WP RUDDER FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 679HA 47662 HNL - FLT 516 - (FROM LOG PAGE NR A-145680) - RUDDER IS EXTREMELY STIFF ON INITIAL CHECK. AFTER EXERCISING A FEW TIMES, THEY SEEM TO LOOSEN UP. FEELS LIKE THERE IS NO HYDRAULIC ASSISTANCE. (PILOT'S REMARKS 'QUESTION SAFETY FOR SINGLE ENG INE OPERATION'). REPLACED RUDDER TRIM AND LOAD FEEL SPRING. GROUND OPERATIONAL CHECK GOOD PER MM 27-20-7. (X) 2 L 7 2 4F RT A6WE 1998072400242 19980724 00242 WP 1998 7 24 HALA9800183 1 19980630 A 3260 008004003 CONTROL PANEL DOUG DC9 DC951 3022051 WP COCKPIT MALFUNCTIONED A HALA K NONE N FALSE WARNING CR CRUISE 1 WP 13 673MC 513 47726 ITO - FLT 101 - (LOG PAGE NR A144385) - NOSE GEAR UNSAFE LIGHT COMES ON IN-FLIGHT. REPLACED L/G POSITION WARNING CONTRO L PANEL AND NOSE GEAR ELECTRICAL HARNESS. (X) 2 L 7 2 4F RT A6WE 1998072400243 19980724 00243 WP 1998 7 24 HALA9800180 1 19980619 A 5753 FLAP TRACK DOUG DC10 DC1010 3022110 WP WS 118 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 171AA 19574 46906 TULE - (NR 116312) - INBOARD FLAP TRACK POST HAS CORROSION IN VARIOUS HOLES ON INBOARD FLAP ON RIGHT-HAND WING. STA 118 XORS. REAMED HOLES TO REMOVE CORROSION AND INSTALLED BUSHINGS PER AARD 57-20-00-10. (X) 2 L 7 3 4F A22WE 1998072400244 19980724 00244 EU 1998 7 24 SIMA981781 1 19980627 A 2120 DUCT SAAB SF340 340B 7860101 EU A/C BAY CONTAMINATED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 391AE 340B391 DFW - FLT 3657 - FUMES IN AIRCRAFT BURNS THROAT, EYES, AND LUNGS. GROUND RAN AIRCRAFT FOR 15 MINUTES. NO FUMES NOTED. AIRCRAFT RETURNED TO SERVICE. NOTE: AIRCRAFT HAD PREVIOUSLY BEEN WRITTEN UP ON THIS DAY FOR HOT CABIN/WEAK AIRFLOW. M AINTENANCE REPLACED THE ACM RUBBER ELBOW/DUCTS ON BOTH LEFT AND RIGHT SIDES. THIS MAY HAVE BEEN SOME TYPE OF RESIDUAL O R BURN-OFF. (X) 2 L 7 2 4T RT A52EU 1998072400245 19980724 00245 NM 1998 7 24 98ZZZX2411 1 19980624 A 3250 89900113 STEERING MESSIER 89681 DHAV DHC8 DHC8103 1386005 NM NLG MALFUNCTIONED A KPVA K NONE O OTHER NR NOT REPORTED 1 WP 13 803WP 1220 141 NOSE WHEEL STEERING WILL NOT TURN RIGHT. MAINTENANCE RETURNED TO MKK AND MADE REPAIRS TO AIRCRAFT AND REPOSITIONED BACK TO HNL, SEVERAL PIECES, PARTS WERE REPLACED, TO INCLUDE THE FOLLOWING: LINK SUB ASSY, PN 8988-1 AND 8968-1. PLUG, PN 8 995-1, BEARING PN 8993-3 AND 8994-3, AND 8967-1, AND 8962-1. RING, PN S11109014. NUT, PN 8996-1, PIN PN Q8105. RETAIN ER PN 8996-3. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998072400246 19980724 00246 EU 1998 7 24 SIMA981791 1 19980628 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 194AE 340B194 DFW - FLT 5020 - OVERHEAD EMERGENCY LIGHT AT ROW 4A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB AT SEAT 4A EMERGENCY LIGHT. (X) 2 L 7 2 4T RT A52EU 1998072400247 19980724 00247 EU 1998 7 24 SIMA981752 1 19980624 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 853 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DURING HMBV, FOUND TWO DENTS ON RIGHT SIDE OF TAILCONE UPPER SKIN JUST FORWARD OF FS 853. DYE PENETRANT INSPECTION REVEALED NO DEFECTS. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PLATE AND TWO FILLER PLATES. AIRCRAFT RETURNED TO SERV ICE. TOTAL TIME: 15,388.4 HOURS. RORAL CYCLES: 14,564. (X) 2 L 7 2 4T RT A52EU 1998072400248 19980724 00248 EU 1998 7 24 SIMA981751 1 19980624 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 608 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 264AE 340B264 ABI - DURING HMBV INSPECTION, DENT WAS FOUND AT RIGHT AFT FS 608. EDDY CURRENT REVEALED A CRACK INDICATION. CUT OUT DA MAGE AND INSTALLED REPAIR PLATE 25.5 INCHES BY 21 INCHES. AIRCRAFT RETURNED TO SERVICE. TOTAL TIME: 15,388.4 HOURS. T OTAL CYCLES: 14,564. (X) 2 L 7 2 4T RT A52EU 1998072400249 19980724 00249 NM 1998 7 24 F3LA98117 1 19980701 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 789 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 3584 23257 PAE - DURING C-CHECK INSPECTION REPORTED CORROSION ON FLOOR SUPPORT, BS 789, RBL 23, WL 155. MAINTENANCE REMOVED CORROS ION (5 INCHES BY 3 INCHES BY .015 INCH) AND DAMAGED FLOOR SUPPORT. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-40-2 AND 53-60-53. TOTAL CYCLES: 1,608. (X) 2 L 7 2 4F RT A16WE 1998072400250 19980724 00250 WP 1998 7 24 TWAA9810109 1 19980504 A 5330 SKIN DOUG DC9 DC941 302207N WP BS 617 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 933L 47617 STL - DURING OVERNIGHT, MAINTENANCE FOUND CORROSION AT A REPAIR IN THE FORWARD CARGO COMPARTMENT, STA 617, LONGERON 30. REPLACED REPAIR PER ARA 15069. CHECK-C 2-16-98 STL. TT: 51,189 HOURS. TOTAL CYCLES: 47,293. (X) 2 L 7 2 4F A6WE 1998072400256 19980724 00256 NM 1998 7 24 TWAA9810102 1 19980619 A 5754 SKIN BOEING 767 767231 1385131 NM NR 6 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 604TW 22567 LAX - DURING CHECK-C, MAINTENANCE FOUND APPROXIMATELY A 5 INCH BY 5 INCH DELAMINATION ON UPPER LEADING EDGE AFT OF NR 6 LE SLAT, APPROXIMATELY 5 FEET OTBD OF INBD END OF SLAT, LT WING. ROUTED OUT DELAMINATION. REMOVED 1 INCH SKIN AROUND A REA AND INSTALLED HEAT AND SUCTION PER SRM 51-70, 2B. INSTALLED WET LAY-UP PER SRM 51-70-17, PARA 3. TOTAL TIME: 51,17 7 HOURS. TOTAL CYCLES: 14,329. (X) 2 L 7 2 4F RT A1NM 1998072400257 19980724 00257 WP 1998 7 24 TWAA9810101 1 19980622 A 4990 379580XXX OIL PUMP DOUG DC9 DC982 3022082 WP APU LEAKING A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 902TW 49153 IN FULL COLD POSN LT AIR COND PACK REPORTED TO CAUSE OILY BURNING SMELL AND MADE CABIN APPEAR FOGGY. CREW WENT TO MANUA L AND SMELL AND FOG WENT AWAY. THE LT AND RT WATER SEPARATORS WERE REPLACED AND CHECKED OK. LATER FLT REPORTED SLIGHT FUMES FROM LT PACK, WHICH WAS PLACARDED PER MEL. ON OVERNIGHT TROUBLESHOOTING FOUND LT PACK OK, BUT OIL LEAK FROM APU. REACTIVATED LT PACK AND PLACARDED APU INOP PER MEL. CHECK-C 2-1-98 STL. *S/D* FOUND PACKINGS ON APU OIL PUMP ASSEMBL Y BANJO FITTING WERE LEAKING, ALLOWING OIL TO LEAK ONTO PLATFORM AND ON INTO APU AIR INLET. REPLACED PACKINGS ON OIL PU MP BANJO FITTING. 2 L 7 2 4F A6WE 1998072400258 19980724 00258 NM 1998 7 24 TWAA9810207 1 19980623 A 5754 SKIN BOEING 767 767231 1385131 NM NR 5 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING CHECK-C, MAINTENANCE FOUND ON LT WING THE NR 5 LE SLAT INBD SIDE WITH DELAMINATION ON AFT SIDE. INSTALLED 2 INCH BY 3 INCH HOT BONDED FLUSH DOUBLER PER SRM'S 57-43-02 AND 51-70-10. TOTAL TIME: 63,613 HOURS. TOTAL CYCLES: 1 4,886. (X) 2 L 7 2 4F RT A1NM 1998072400259 19980724 00259 NM 1998 7 24 TWAA9810206 1 19980625 A 5753 FLAP BOEING 767 767231 1385131 NM NR 4 TE CONTAMINED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING CHECK-C, MAINTENANCE FOUND ON RT WING THE NR 4 TE FLAP INBD AFT SIDE WITH INDICATION OF WATER. AFTER WATER REMOVED, INSTALLED 12 BY 30 PANEL AND ADHESIVE HOT BOND PER SRM 51-70-07, AND LIMITS PER 57-53. TOTAL TIME: 63,613 HO URS. TOTAL CYCLES: 14,886. (X) 2 L 7 2 4F RT A1NM 1998072400260 19980724 00260 NM 1998 7 24 TWAA9810205 1 19980625 A 5751 AILERON BOEING 767 767231 1385131 NM RT WING CONTAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING CHECK-C, MAINTENANCE FOUND ON TOP OF RT WING, THE OTBD AILERON HAD INDICATION OF WATER ON WHOLE SURFACE. A FTER WATER REMOVED, INSTALLED WET LAYUP PER SRM 51-70-17, PAGE 67, AND PAINTED AREAS. TOTAL TIME: 63,613 HOURS. TOTAL CYCLES: 14,886. (X) 2 L 7 2 4F RT A1NM 1998072400261 19980724 00261 WP 1998 7 24 TWAA9810204 1 19980517 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 945 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 STL - FOUND AFT OF AFT CARGO DOOR DAMAGED AT STA 945. REPAIRED FRAME PER ARA 15094 AND SRM 53-05, FIG 80. CHECK-C 10-1 2-97 MCI. TOTAL TIME: 67,905. TOTAL CYCLES: 78,196. (X) 2 L 7 2 4F A6WE 1998072400262 19980724 00262 WP 1998 7 24 TWAA9810203 1 19980517 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 945 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 STL - FOUND INTERNAL DOUBLER AFT OF AFT CARGO DOOR AT STA 945 DAMAGED. REMOVED AND REPLACED INTERNAL DOUBLER PER ARA 15 094, AND SRM 53-05, FIG 80. CHECK-C 10-12-97 MCI. TOTAL TIME: 67,905 HOURS. TOTAL CYCLES: 78,196. (X) 2 L 7 2 4F A6WE 1998072400263 19980724 00263 WP 1998 7 24 TWAA9810202 1 19980625 A 3230 39140165503 BOLT DOUG DC9 DC951 3022051 WP RT MLG BROKEN A TWAA O OTHER J WARNING INDICATION CL CLIMB 1 CE 05 411EA 47732 STL - FLT 617 - AFTER TAKEOFF FROM SGF, THE RT MAIN LANDING GEAR WOULD NOT RETRACT. OPERATED SGF TO STL WITH RT GEAR EX TENDED AT REDUCED AIR SPEED. FOUND RT MLG BUNGEE ACTUATOR PISTON END EYE BOLT BROKEN OFF. REPLACED BUNGEE. CHECK-C 7- 19-97 STL. (X) 2 L 7 2 4F RT A6WE 1998072400264 19980724 00264 WP 1998 7 24 TWAA9810201 1 19980624 A 2923 CONNECTOR DOUG DC9 DC932 3022066 WP HYDRAULIC PUMP FAILED A TWAA O OTHER J WARNING INDICATION IN INSP/MAINT 1 CE 05 925L 47357 STL - AFTER REPLACEMENT OF THE AUXILIARY HYDRAULIC PUMP, DURING CHECK-OUT, A FIRE IGNITED AT THE PUMP. FIRE WAS QUICKLY EXTINGUISHED WITH GROUND FIRE BOTTLE. PASSENGERS WERE DEPLANED THROUGH JETWAY. FOUND SHORT IN AUXILIARY PUMP HARNESS CONNECTOR. REPLACED AUXILIARY HYDRAULIC PUMP, PUMP HARNESS, CONNECTOR, AND CIRCUIT BREAKER. CHECK-C 10-23-97 STL. (X) 2 L 7 2 4F A6WE 1998072400265 19980724 00265 NM 1998 7 24 MZZA98179 1 19980610 A 5330 SKIN BOEING 727 7272F9 138407D NM BS 481/500 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 83428 21426 TNN - HNRC: 817298 (SEQ NR 01041) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FORWARD C ARGO COMPARTMENT FUSELAGE SKIN INNER SURFACE AT S28R BETWEEN BS 481 AND BS 500. THE CORRODED SKIN 3 INCHES BY 18 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3 FIG 3A. (X) 2 L 7 3 4F RT A3WE 1998072400266 19980724 00266 NM 1998 7 24 MZZA98180 1 19980610 A 5313 STRINGER BOEING 727 7272F9 138407D NM BS 490 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 83428 21426 TNN - HNRC: 817313 (SEQ NR 01036) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT STR 28R AT BS 490. THE CORRODED STR S28R FROM BS 480 TO BS 510 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. (X) 2 L 7 3 4F RT A3WE 1998072400267 19980724 00267 NM 1998 7 24 MZZA98178 1 19980611 A 5320 WEB BOEING 727 7272F9 138407D NM BS 1323 & 1333 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 83428 21426 TNN - HNRC: 837853 (SEQ NR 01063) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIR STAIR LT TORQUE BOX HORIZONTAL WEB BETWEEN BS 1323 AND BS 1333. A REINFORCEMENT STIFFENER ANGLE WAS INSTALLED TO THE DA MAGED WEB PER B727 SRM 51-40-2. (X) 2 L 7 3 4F RT A3WE 1998072400268 19980724 00268 NM 1998 7 24 MZZA98181 1 19980611 A 5320 WEB BOEING 727 7272F9 138407D NM TORQUE BOX CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 83428 21426 TNN - HNRC: 837851, 837852 (SEQ NR 01061, 01062) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS F OUND ON AFT AIRSTAIR LT TORQUE BOX VERTICAL WEB AT THE FOLLOWING AREAS: BETWEEN BS 1313 AND BS 1323 AND BETWEEN BS 1223 AND BS 1233. A REINFORCEMENT STIFFENER ANGLE WAS INSTALLED ON THE AIRSTAIR LT TORQUE BOX WEB OIL CANNING AREAS PER B72 7 SRM 51-40-2. (X) 2 L 7 3 4F RT A3WE 1998072400269 19980724 00269 NM 1998 7 24 MZZA98182 1 19980611 A 5320 WEB BOEING 727 7272F9 138407D NM TORQUE BOX CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 83428 21426 TNN - HNRC: 837848, 837849, 837850 (SEQ NR 01058, 01059, 01060) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR RT TORQUE BOX VERTICAL WEB AT THE FOLLOWING AREAS: BETWEEN BS 1243 AND BS 1253. BET WEEN BS 1283 AND BS 1303. BETWEEN BS 1313 AND BS 1323. A REINFORCEMENT STIFFENER ANGLE WAS INSTALLED AT THE AFT AIRSTA IR RT TORQUE BOX WEB OIL CANNING AREAS PER B727 SRM 51-40-2. (X) 2 L 7 3 4F RT A3WE 1998072400270 19980724 00270 EU 1998 7 24 PIVA11648 1 19980616 A 2910 SD3731019XA PIPE STBROS SD3 SD360 8100606 EU HYDRAULIC SYSTEM RUPTURED A PIVA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 13 711MP 20122 SH3698 HYDRAULIC PRESSURE FAILED IN-FLIGHT. HYDRAULIC FLUID LOSS DUE TO .50 INCH RUPTURE OF PIPE. P/N SD3-73-1019XA REQUIRING SHUT DOWN OF HYDRAULIC PUMPS AND RETURN TO FIELD. (X) 2 H 7 2 4T A41EU 1998072400271 19980724 00271 NM 1998 7 24 MZZA98183 1 19980610 A 5330 SKIN BOEING 727 7272F9 138407D NM BS 675 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 83428 21426 TNN - HNRC: 817317 (SEQ NR 01040) - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING AND DENT WERE FOUND ON FUSELAGE SKIN AT BS 675, BETWEEN S21R AND S22R. THE DAMAGED SKIN 2.5 INCH BY 5 INCH IN SIZE WAS TRIMMED OUT AND REPA IRED PER B727 SRM 53-30-3, FIGURE 3A. (X) 2 L 7 3 4F RT A3WE 1998072400272 19980724 00272 EU 1998 7 24 SIMA981741 1 19980623 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO MALFUNCTIONED A SIMA D F RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 227AE A5153 340B227 MIA - FLT 5711 - CARGO SMOKE WARNING LIGHT ILLUMINATED, DISCHARGED NR 1 CARGO FIRE EXTINGUISHER. REMOVED AND REPLACED F IRE EXTINGUISHER AND BOTH CARGO SMOKE DETECTORS. NO FURTHER DEFECTS NOTED. REF: OPERATOR CNTRL NR 98ZZZX2412. (X) 2 L 7 2 4T RT A52EU 1998072400273 19980724 00273 EU 1998 7 24 98ZZZX2412 1 19980623 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO MALFUNCTIONED A SIMA D F RETURN TO BLOCK ACTIVATE FIRE EXT. N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 227AE A2949 340B227 MIA - FLT 5711 - CARGO SMOKE WARNING LIGHT ILLUMINATED, DISCHARGED NR 1 CARGO FIRE EXTINGUISHER. REMOVED AND REPLACED F IRE EXTINGUISHER AND BOTH CARGO SMOKE DETECTORS. NO FURTHER DEFECTS NOTED. REF: OPERATOR CNTRL NR SIMA981741. 2 L 7 2 4T RT A52EU 1998072400274 19980724 00274 WP 1998 7 24 VJ9800228 1 19980717 A 3020 7988591501 DUCT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE RT NOSE COWL FAILED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 907VJ 47444 NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF, THROTTLE RETARDED AND LIGHT EXTINGUISHED. CREW ELECTED TO RET URN TO ATL MAINTENANCE BASE. INSPECTED AIRCRAFT AND FOUND BLOWN DUCT. REPLACED NR 2 ENGINE NOSE COWL ANTI-ICE DUCT, RA N ENGINE AND NO LEAKS NOTED. 2 L 7 2 4F 4 F A6WE E2EA 1998072400275 19980724 00275 WP 1998 7 24 VJ9800229 1 19980718 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 922VV 47274 RT EMERGENCY OVERWING LIGHT INOP. REPLACED EMERGENCY POWER SUPPLY. 2 L 7 2 4F A6WE 1998072400276 19980724 00276 WP 1998 7 24 VJ9800230 1 19980719 A 2560 598287291 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE DETACHED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 933VV 47489 GALLEY DOOR SLIDE COVER DISLODGED. RETURNED TO GATE AND REINSTALLED SLIDE PACK COVER AND PERFORMED REQUIRED INSPECTIONS . 2 L 7 2 4F A6WE 1998072400277 19980724 00277 EU 1998 7 24 MALA976163 1 19980717 A 3350 6104789 BATTERY PACK SAAB SF340 SF340A 7850100 EU CABIN DISCHARGED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 103XJ 340A103 DURING INSPECTION NOTED TWO OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE REPLACED BATTERY PACK UNDER FLOOR BETWEEN SEATS 7 AND 8, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998072400278 19980724 00278 EU 1998 7 24 MALA976164 1 19980715 A 3350 85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 436XJ 436 EMERGENCY LIGHTS ARMED LIGHT ON FLIGHT ATTENDANT PANEL INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998072400279 19980724 00279 EU 1998 7 24 MALA976165 1 19980715 A 3230 HP848430721 CONTROL VALVE SAAB SF340 340B 7860101 EU LANDING GEAR MALFUNCTIONED A MALA O OTHER O OTHER AP APPROACH 1 GL 15 441XJ 441 ON APPROACH, LANDING GEAR SELECTED DOWN, PUMP STARTED RUNNING AND AMBER INTRANSIT LIGHT CAME ON. GEAR WOULD NOT LOCK DO WN, PUMP RAN FOR SEVERAL SECONDS THEN LANDING CONTROL CIRCUIT BREAKER POPPED, PUMP CONTINUED TO RUN. AFTER RESETTING CI RCUIT BREAKER AND RECYCLING GEAR HANDLE SEVERAL TIMES LANDING GEAR CAME DOWN. AIRCRAFT LANDING WITHOUT INCIDENT. MAINT ENANCE REPLACED LANDING GEAR CONTROL VALVE. OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998072400280 19980724 00280 WP 1998 7 24 CALA9801263 1 19980717 A 5313 STRINGER DOUG DC9 DC932 3022066 WP BS 598 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND STRINGER/FRAME CORRODED AROUND FASTENERS AT KEEL BOX INTERIOR, STA 598, STRINGER 29R. THE KEEL BOX WEB WAS REMOVED. TWO REPAIR ANGLES WERE FABRICATED IAW SRM 53-01, FIGURE 2 AND 51-10-2A. THE ANGLES AND KEEL BOX PANEL WER E INSTALLED IAW SRM 51-10-4, 51-30-5, 53-01, FIGURE 2, AND 51-30-1. 2 L 7 2 4F A6WE 1998072400281 19980724 00281 WP 1998 7 24 CALA9801264 1 19980717 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOORBEAM CORRODED AT STA 980, RBL 21 AND RBL 34. THE CORRODED AREAS WERE CUT OUT, AN ANGLE, FILLER, A ND SHIM WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 20A. 2 L 7 2 4F A6WE 1998072400282 19980724 00282 WP 1998 7 24 CALA9801265 1 19980717 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 579-680 SEPARATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOOR PANEL SKIN SEPARATING AT STA 579 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-21-0, PAGE 11 AND 53-05, PAGE 122B. 2 L 7 2 4F A6WE 1998072400283 19980724 00283 WP 1998 7 24 CALA9801266 1 19980718 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 522 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO SKIN BELOW FLOOR LINE AT WING SCAN LIGHT AT STA 522. A DOUBLER AND FINGER D OUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1998072400284 19980724 00284 WP 1998 7 24 CALA9801267 1 19980718 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 996-1019 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND TWO CRACKS IN INTERCOSTAL AT STA 996 TO 1019, RBL 20. THE CRACKS WERE STOP DRILLED, AN ANGLE STRAP WAS FABRICATED AND INSTALLED IAW SRM 53-01, 51-30-2, AND 51-30-0. 2 L 7 2 4F A6WE 1998072400285 19980724 00285 WP 1998 7 24 CALA9801268 1 19980718 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 294 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A .25 INCH CRACK IN FORWARD CARGO COMPARTMENT FLOOR SUPPORT AT STA 294, STRINGER 27R. THE FLOOR SUPPOR T WAS REMOVED IAW SRM 51-30-2 AND THE CRACK WAS STOP DRILLED IAW ECRA 5320-01263. AN ANGLE REPAIR WAS FABRICATED AND IN STALLED IAW ECRA 5320-01263, SRM 51-10-3, 51-30-2, 51-30-5, AND 51-30-8. 2 L 7 2 4F A6WE 1998072400286 19980724 00286 WP 1998 7 24 CALA9801269 1 19980718 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND A .75 INCH CRACK IN NR 4 HORIZONTAL BEAM OF FORWARD SERVICE DOOR. A NEW BEAM WAS INSTALLED IAW SRM 51- 60-0. 2 L 7 2 4F A6WE 1998072400287 19980724 00287 WP 1998 7 24 CALA9801270 1 19980717 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A 5 INCH CRACK IN BELTFRAME AT STA 446, LONGERON 5L. THE BELTFRAME WAS REPAIRED IAW SRM 53-03, FIGURE 4. 2 L 7 2 4F A6WE 1998072400288 19980724 00288 WP 1998 7 24 CALA9801271 1 19980717 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 895 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND BELTFRAME CORRODED AT STA 895, LONGERON 18L. THE CORRODED SECTION OF FRAME WAS REMOVED AND REPLACED IA W SRM 51-30-2. 2 L 7 2 4F A6WE 1998072400289 19980724 00289 WP 1998 7 24 9809829104 1 19980718 A 3230 RETRACT MECH DOUG DC9 DC915 3022036 WP LANDING GEAR OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 94S 47204 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RETRACTED THE LANDING GEAR BY PUSHING THE LANDING HANDLE RELEASE BUTTON. FLIGHT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED THE ANTI-RETRACTION CABLE AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKED NORMAL. 2 L 7 2 4F A6WE 1998072400290 19980724 00290 SO 1998 7 24 COMA9810160 1 19980717 A 5246 DOOR EMB 120 EMB120RT SO FUEL SYSTEM NOT CLOSED A COMA C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 SO 01 258CA 120247 SERVICE DOOR WARNING DURING TAKEOFF. SECURED SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998072400291 19980724 00291 EA 1998 7 24 COMA9860179 1 19980717 A 4930 21188002 ECU CNDAIR CL600 CL6002B19 EA APU FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 963CA 1580 337 7127 APU FAILED AFTER TAKEOFF. REPLACED THE APU ECU. 2 L 7 2 4F RT A21EA 1998072400292 19980724 00292 EA 1998 7 24 COMA9860180 1 19980710 A 5312 6013501252 BULKHEAD ANGLE CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 DURING C-CHECK, FOUND PRESSURE BULKHEAD ANGLE BRACKET CRACKED. REPLACED ANGLE BRACKET. 2 L 7 2 4F RT A21EA 1998072400293 19980724 00293 EA 1998 7 24 COMA9860181 1 19980710 A 3240 16789101 COMPENSATOR CNDAIR CL600 CL6002B19 EA FUSELAGE LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 3715 7157 DURING C-CHECK, FOUND BRAKE COMPENSATOR TO BE LEAKING. REPLACED COMPENSATOR. 2 L 7 2 4F RT A21EA 1998072400294 19980724 00294 EA 1998 7 24 COMA9860182 1 19980710 A 5320 601R3502521 BRACKET CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 977CA 7157 DURING C-CHECK, FOUND CARGO DOOR STEP BRACKETS BROKEN. INSTALLED NEW BRACKETS. 2 L 7 2 4F RT A21EA 1998072400295 19980724 00295 EU 1998 7 24 QXEA9800890 1 19980526 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 SERVICE/EMERGENCY DOOR SKIN CRACKED AT FORWARD UPPER CORNER AT TWO RIVETS IN THE APERATURE RECESS. REPAIRED IAW FOKKER SRM 52-02-03, FIGURE 3 AND HORIZON AIR EA 4-52-136. 2 L 7 2 4F RT A20EU 1998072400296 19980724 00296 EU 1998 7 24 QXEA9800891 1 19980604 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 MAIN CABIN DOOR SKIN INSIDE SURFACE IS CORRODED AT LOWER FORWARD CORNER AREA. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRA PH 4 AND SRM 53-01-01. 2 L 7 2 4F RT A20EU 1998072400297 19980724 00297 EU 1998 7 24 QXEA9800892 1 19980605 A 5347 SPLICE FOKKER F28 F28MK4000 4990810 EU RT SEAT TRACK CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 RIGHTHAND INBOARD SEAT TRACK SPLICE HAS RIVETS CRACKED. REPLACED RIVETS IAW FOKKER SRM 53-31-01. 2 L 7 2 4F RT A20EU 1998072400298 19980724 00298 EU 1998 7 24 QXEA9800893 1 19980613 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU BS 3845 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CRACK IN FLOORBEAM UNDER FORWARD GALLEY AT STATION 3845 APPROXIMATELY 18 INCHES INBOARD FROM PASSENGER SERVICE EMERGENCY DOOR. REPAIRED IAW FOKKER SRM 53-11-05, PAGE 10, FIGURE 3, SRM 53-02-01 PAGE 7 FIGURE 5. 2 L 7 2 4F RT A20EU 1998072400299 19980724 00299 EU 1998 7 24 QXEA9800894 1 19980611 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU BS 16060/16660 BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 RHS FLOORBEAM AT BL 600R BETWEEN FRAME 16060 AND 16660 HAS BENT LOWER FLANGE. REPAIRED IAW HORIZON AIR EA 4-53-450. 2 L 7 2 4F RT A20EU 1998072400300 19980724 00300 EU 1998 7 24 QXEA9800895 1 19980621 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU BS 4150 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CRACK IN TOP EDGE OF FLOORBEAM SUPPORT ANGLE AT STATION 4150 16 INCHES FORWARD OF RIGHTHAND OUTBOARD SEAT TRACK. REPAIR ED IAW FOKKER SRM 51-30-02, PAGE 10, PARAGRAPH C AND SRM 51-31-01, PAGE 13, PARAGRAPH B. 2 L 7 2 4F RT A20EU 1998072400301 19980724 00301 EU 1998 7 24 QXEA9800896 1 19980622 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 LARGE DENT APPROXIMATELY 5.0 WIDE AND .135 DEEP AT RIGHTHAND SIDE OF FUSELAGE JUST ABOVE THE LAVATORY DUMP/SERVICE PANEL BETWEEN FRAMES 16660 AND 17065 AND WL 200. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 4 AND SRM 53-01-01, PARAGRAPH 6C. 2 L 7 2 4F RT A20EU 1998072400302 19980724 00302 EU 1998 7 24 QXEA9800897 1 19980622 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 5200 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 DENT IN LEFTHAND FUSELAGE SKIN AT STATION 5200MM AND WL 500MM 1.0 WIDE AND .090 DEEP. REPAIRED IAW FOKKER SRM 53-02-04, FIGURE 1. 2 L 7 2 4F RT A20EU 1998072400303 19980724 00303 EU 1998 7 24 QXEA9800898 1 19980624 A 3350 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 FORWARD GALLEY OVERHEAD EXIT SIGN DOES NOT ILLUMINATE WITH EMERGENCY LIGHT SWITCH IN ARM OR ON POSITION. REMOVED AND RE PLACED CIRCUIT BOARD/LIGHT ASSEMBLY, OPS CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998072400304 19980724 00304 EU 1998 7 24 QXEA9800899 1 19980624 A 3350 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 FORWARD PASSENGER COMPARTMENT OVERHEAD EXIT SIGN DOES NOT ILLUMINATE WITH EMERGENCY LIGHT SWITCH IN ARM OR ON POSITION. REMOVED AND REPLACED CIRCUIT BOARD LIGHT ASSEMBLY, OPS CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998072400305 19980724 00305 EU 1998 7 24 QXEA9800901 1 19980526 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME16 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME 16-2 FRAME CLIP CRACKED PAST STOP DRILL HOLE INBOARD OF STRINGER 41 AFT SIDE OF FRAME. CRACK PAST 1 LIMIT. REPAI RED IAW FOKKER SRM 53-02-13, PAGE 5 FIGURE 3. 2 L 7 2 4F RT A20EU 1998072400306 19980724 00306 EU 1998 7 24 QXEA9800902 1 19980526 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CRACK EXTENDING FROM STOP DRILL HOLE ON CLIP AT FRAME 32-2 STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 3. 2 L 7 2 4F RT A20EU 1998072400307 19980724 00307 EU 1998 7 24 QXEA9800903 1 19980526 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 TWO CRACKS ON FRAME CLIP AT FRAME 32-2 STRINGER 47 AFT SIDE OF FRAME. REPAIRED IAW FOKKER SRM 53-10-5, PAGE 601 AND SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998072400308 19980724 00308 EU 1998 7 24 QXEA9800904 1 19980526 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 41 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CRACK ON CLIP EXTENDING FROM RIVET BUCKTAIL AFT SIDE OF FRAME 41-2 STRINGER 45. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 , 4B AND SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1998072400309 19980724 00309 EU 1998 7 24 QXEA9800905 1 19980601 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FRAME CLIP CRACKED AT FRAME 50-2 STRINGER 48 ON BACKSIDE OF FRAME. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3, SRM 51-3 0-02, SRM 51-31-01 AND SRM 51-10-04. 2 L 7 2 4F RT A20EU 1998072400310 19980724 00310 NM 1998 7 24 98FDEA00463 1 19980718 A 5242 DOOR BOEING 727 72725C 138400H NM E/E COMPT NOT CLOSED A FDEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 25 119FE 19301 A/C WOULD NOT PRESSURIZE IN FLIGHT. FOUND E AND E COMPARTMENT DOOR CRACKED OPEN. EQUIPMENT ACCESS WARNING LIGHT INOPER ATIVE. REPLACED SWITCH S114 AND GROUNDING WIRE W346-112-20. REPAIRED WIRE W346-011-20. EQUIPMENT ACCESS LIGHT NOW OPE RATES NORMAL. CHECKED DOOR ADJUSTMENT. NO ABNORMALITIES NOTED. A/C PRESS PER JRH CHART 7 OK FOR SERVICE. 2 L 7 3 4F A3WE 1998072400311 19980724 00311 WP 1998 7 24 MWEA98788 1 19980714 A 3350 100865 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 WHEN APU BUSS TO GROUND BUSS WAS TURNED OFF THE BACK HALF OF FLOOR TRACK LIGHT CAME ON. MTC REMOVED AND REPLACED AFT FL OOR TRACK BATTERY PACK. 2 L 7 2 4F A6WE 1998072400312 19980724 00312 WP 1998 7 24 MWEA98789 1 19980714 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 602ME 48133 THE ENTRY DOOR SLIDE COVER CAME OFF. MTC REINSTALLED ENTRY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998072400313 19980724 00313 WP 1998 7 24 MWEA98790 1 19980714 A 2560 11320 GIRT BAR DOUG DC9 DC932 3022066 WP GALLEY DR SLIDE LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE FLIGHT ATTENDANT REPORTED DIFFICULTY ARMING THE GALLEY SLIDE GIRT BAR. MTC CLEANED AND LUBED GALLEY SLIDE GIRT BAR AND HOLDER. 2 L 7 2 4F A6WE 1998072400314 19980724 00314 WP 1998 7 24 MWEA98791 1 19980714 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP GALLEY DR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 401ME 47133 THE GALLEY SLIDE COVER POPPED OUT. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998072400315 19980724 00315 NM 1998 7 24 TSAA9857265 1 19980513 A 5511 SPAR BOEING 737 7372T4 1384492 NM HORIZONTAL STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 FOUND CORROSION ON RT SIDE HORIZONTAL STABILIZER REAR SPAR UPPER CHORD AT STAB STATION 68.14 AND STRIGNER S-1. REPAIRED PER ECO 1889R3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998072400316 19980724 00316 NM 1998 7 24 TSAA9857263 1 19980513 A 5711 SPAR BOEING 737 7372T4 1384492 NM RT WING CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 FOUND CORROSION AT WBL 318 ON RT WING FRONT SPAR LOWER CHORD HORIZONTAL FLANGE LOWER SURFACE. REPAIRED CORROSION PER EC O 1803 R4. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998072400317 19980724 00317 NM 1998 7 24 TSAA9857264 1 19980513 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 663 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 FOUND CRACK AT BBL .07 FLOORBEAM REPAIR AT BS 663. REPAIRED PER ECO 2223R2 FIGURE 4. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A16WE 1998072400318 19980724 00318 NM 1998 7 24 TSAA9853268 1 19980526 A 5330 SKIN BOEING 737 7372X6C 1384552 NM BS 767 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 SKIN CRACK, APPROXIMATELY .75 INCH LONG, NOTED AT BS 767 AND STRINGER 18L. CONFIRMED WITH HFEC. REPAIRED SKIN IAW BOEI NG SRM 53-30-3 FIGURE 1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998072400319 19980724 00319 EU 1998 7 24 SIMA981386 1 19980518 A 3350 4241601 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 12MQ 4193 012 ORD - EXTERNAL EMERGENCY PROX/EXIT LIGHT SOCKET BURNED OUT. REMOVED AND REPLACED EXTERIOR EMERGENCY PROX/EXIT LIGHT ASS Y. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998072400320 19980724 00320 EU 1998 7 24 SIMA981402 1 19980520 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMP DIRTY A SIMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 278AE 4193 340B278 CARGO SMOKE LIGHT CAME ON DURING TAXI. CLEANED BOTH CARGO SMOKE DETECTORS. OPERATIONAL CHECK GOOD. A/C RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A52EU 1998072400321 19980724 00321 EU 1998 7 24 SIMA981501 1 19980530 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS RACK MALFUNCTIONED A SIMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 305AE A3109 340B305 BDL - FLT 4973 - AVIONICS SMOKE DETECTION LIGHT ON DURING FLIGHT, ON TAXI INTO GATE, LIGHT WENT OFF. NO EVIDENCE OF SMO KE OR SMELL OF SMOKE IN AIRCRAFT. CONTACTED CONTRACT MAINTENANCE AND PERFORMED A VISUAL INSPECTION, FOUND NO DAMAGE AND OPENED UP MEL 26-03 AVIONICS RACK SMOKE DETECTION SYSTEM. JFK MAINTENANCE ON 5/31/98. RAI AVIONICS RACK SMOKE DETECTO R AND CLOSED MEL. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998072400322 19980724 00322 NM 1998 7 24 TWRA9830 1 19980527 A 2820 VALVE BOEING 747 747121 1384871 NM SUMP DRAIN LEAKING A TWRA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 15 617FF 19650 ON TAKEOFF FROM VCP, FLT 967, UPON FIRST ROTATION PRIOR TO FIRST PACK ON, STRONG FUEL ODOR IN COCKPIT. TRANSFERRED FUEL INTO CENTER TANK, NO LEAK NOTED, RESET CENTER TANK SUMP DRAIN VALVE THAT WAS WET. NO LEAK AFTER RESET. (M) 2 L 7 4 4F A20WE 1998072400323 19980724 00323 CE 1998 7 24 98ZZZM483 1 19980508 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG FAILED A JJBA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 01 836CA 209 UE32 GEAR WILL NOT RETRACT ELECTRICALLY. LT MLG ACTUATOR FAILURE. REMOVED AND REPLACED LT MLG ACTUATOR IAW CHAP 32 BMM. (M ) 2 L 7 2 4T RT A24CE 1998072400324 19980724 00324 CE 1998 7 24 98ZZZM484 1 19980515 A 6123 5038912129 SWITCH BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A JJBA K NONE L NO TEST IN INSP/MAINT 1 EA 01 845CA UE47 RIGHT AUTO FEATHER INOP. RT ENGINE LOW PRESSURE SWITCH FAILURE. REPLACED RT ENGINE LOW PRESSURE SWITCH IAW CHAP 61 BEE CH MAINTENANCE MANUAL. 2 L 7 2 4T RT A24CE 1998072400325 19980724 00325 CE 1998 7 24 98ZZZM485 1 19980518 A 3234 1013841377 SELECTOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 857CA 813 UE71 LANDING GEAR RETRACT CIRCUIT BREAKER OPENS. LANDING GEAR HANDLE FAILURE. REPLACED LANDING GEAR HANDLE IAW BEECH MAINTE NANCE MANUAL. (M) 2 L 7 2 4T RT A24CE 1998072400326 19980724 00326 CE 1998 7 24 98ZZZM486 1 19980506 A 2620 1143200523 TEE HANDLE BEECH 1900 1900D 1154162 CE COCKPIT FAILED A JJBA K NONE L NO TEST IN INSP/MAINT 1 EA 01 855CA 632 UE61 LT TEE HANDLE WILL NOT ILLUMINATE AT AMP TEST. TEE HANDLE FAILURE. REMOVED AND REPLACED TEE HANDLE. 2 L 7 2 4T RT A24CE 1998072400327 19980724 00327 NM 1998 7 24 TAOA059815 1 19980601 A 2121 10608551 FAN BOEING 727 727254 138408L NM A/C BAY SHORTED A TAOA H B DEACTIVATE SYST/CIRCUITS EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 914TS 20251 FLT 6480 - DCA-LGA - GASPER FAN CIRCUIT BREAKER POPPED FOLLOWED BY BURNING SMELL FROM GASPER FAN VENTS. GASPER FAN SWIT CH WAS PLACED TO OFF. REPLACED GASPER FAN IAW MM CHAPTER 21-23-1. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998072400328 19980724 00328 NM 1998 7 24 TAOA059816 1 19980528 A 2420 9JY20AA1 TRANSFORMER BOEING 727 727227 1384078 NM NR 2 GENERATOR SHORTED A TAOA O OTHER O OTHER IN INSP/MAINT 1 EA 15 926TS 20774 REPEATER ITEM, DIFFERENTIAL FAULT ON GENERATOR NR 2. TRIPPED FIELD AND GENERATOR BREAKER ALSO DIFFERENTIAL FAULT ON SEC OND OFFICERS PANEL. FOUND WIRE FROM GENERATOR CURRENT TRANSFORMERS TO GROUND W200-456-4 (T6) SHORTING TO SENSE LINE ON PRESSURIZATION BLEED CONTROL VALVE. REPLACED WIRE HARNESS AND REPLACED CURRENT TRANSFORMERS T62, T63, T64 AND ELECTRICA L SHELF. REPLACED CURRENT TRANSFORMERS T71, T72, T73 FOR NR 2 ESSENTAIL BUS. ALL GENERATORS CHECK NORMAL ON TEST FLIGH T. (M) 2 L 7 3 4F A3WE 1998072400329 19980724 00329 EU 1998 7 24 WTAA980082 1 19980525 A 7710 31024766 TRANSMITTER BAG JETSTM JETSTM3101 1500215 EU RT ENGINE OUT OF ADJUST A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 WP 17 107XV 723 FAT - RIGHT ENGINE FAILED TO MAKE MINIMUM STATIC POWER DURING TAKEOFF ROLL. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENA NCE ADJUSTED RIGHT ENGNIE TORQUE SIGNAL CONDITIONER. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4T RT A21EU 1998072400330 19980724 00330 SO 1998 7 24 WTAA980083 2 19980525 A 7261 OIL SYSTEM EMB 120 EMB120RT SO LT ENGINE REQ SERVICE A WTAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 17 268UE 120207 ACV - OIL PRESSURE WARNING ON LEFT ENGINE DURING TAKEOFF ROLL. TAKEOFF ABORTED. MAINTENANCE SERVICED ENGINE OIL TO PRO PER LEVEL. OPERATIONAL CHECKS SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400331 19980724 00331 EU 1998 7 24 WTAA980081 1 19980521 A 5101 STRUCTURE BAG JETSTM JETSTM3101 1500215 EU AIRFRAME BIRDSTIKE A WTAA K NONE C F.O.D. CL CLIMB 1 WP 17 331CA 793 SMF - BIRD STRIKE AFTER ROTATION REPORTED. MAINTENANCE INSPECTED AREA FOR DAMAGE. NO DAMAGE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998072400332 19980724 00332 NM 1998 7 24 PCAA9800773 1 19980530 A 2913 O-RING DHAV DHC8 DHC8102 2809003 NM HYD PUMP DAMAGED A PCAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 13 834EX 285 AFTER TAKEOFF FROM BWI, NR 1 HYDRAULIC QUANTITY FELL TO ZERO AND THE NR 1 ENGINE HYDRAULIC PUMP LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED INTO MDT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND O-RING CUT ON THE PRESSURE LINE . REMOVED AND REPLACED O-RING AND HYDRAULIC ENGINE DRIVEN PUMP IAW DHC PROCEDURES. COMPLIED WTH DHC HYDRAULIC LOSS CHE CK IAW CHAPTER 05. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998072400333 19980724 00333 NM 1998 7 24 F3LA98074 1 19980527 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 912-947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO BAY STRINGER 27R, RBL 5, BS 912-947. MAINTENANCE REMOV ED CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, 51-30-5, 53-10-1 AND 53-10-3. (M) 2 L 7 2 4F A16WE 1998072400334 19980724 00334 NM 1998 7 24 F3LA98075 1 19980527 A 5330 SKIN BOEING 737 737201 1384454 NM BS 980-1012 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SKIN AND DOUBLER AT BS 980-1012, STRINGER 27R. MAINTENANCE REMOV ED CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0478. (M) 2 L 7 2 4F A16WE 1998072400335 19980724 00335 NM 1998 7 24 F3LA98076 1 19980529 A 5311 FRAME BOEING 737 737201 1384454 NM BS 360 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON FRAME AND SHEAR TIE AT BS 360, RBL 8-13, BETWEEN STRINGER 27R AND 28R. MAINTENANCE REMOVED DAMAGED AREA (6 INCH BY 4 INCH BY .006 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-4. (M) 2 L 7 2 4F A16WE 1998072400336 19980724 00336 NM 1998 7 24 F3LA98071 1 19980527 A 5720 DOUBLER BOEING 737 737201 1384454 NM LT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED LEFT WING FIXED LEADING EDGE SKIN DOUBLER CRACKED AT NR 3 SLAT OUTBOARD AUXILL IARY TRACK CUTOUT. MAINTENANCE REMOVED DAMAGED DOUBLER AND REPAIRED PER ER 98-0483 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998072400337 19980724 00337 NM 1998 7 24 F3LA98072 1 19980527 A 5330 SKIN BOEING 737 737201 1384454 NM BS 103 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED CRACKS ON UPPER SKIN SURFACE AT RIGHT WING, BL 103.5, TWO INCHES FORWARD OF AF T SPAR. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-57-1144. (M) 2 L 7 2 4F A16WE 1998072400338 19980724 00338 NM 1998 7 24 F3LA98073 1 19980527 A 5320 FRAME BOEING 737 737201 1384454 NM GALLEY DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 217US 20215 PAE - DURING C-CHECK, INSPECTION REPORTED A 1.25 INCH CRACK IN FORWARD GALLEY DOOR AFT FRAME, 4 INCHES DOWN FROM TOP COR NER OUTBOARD RADIUS. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER DRAWING 69-69887-3-4-5 AND SB 737-52-1070. (M) 2 L 7 2 4F A16WE 1998072400339 19980724 00339 NM 1998 7 24 F3LA98070 1 19980529 A 5320 SHEAR TIE BOEING 737 737201 1384454 NM BS 294 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED 1.8 INCH CRACK IN SHEAR TIE AT BS 294 BETWEEN STRINGER 12L AND 14L. MAINTENAN CE FABRICATED NEW SHEAR TIE AND REPAIRED PER SRM 51-10-2 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1998072400340 19980724 00340 NM 1998 7 24 F3LA98078 1 19980529 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 295 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN CROWN OF STRINGER 7L, BS 295. MAINTENANCE REMOVED DAMAGED AREA, FABR ICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3, FIG 1. (M) 2 L 7 2 4F A16WE 1998072400341 19980724 00341 NM 1998 7 24 F3LA98077 1 19980529 A 5730 SKIN BOEING 737 737201 1384454 NM LT WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK, INSPECTION REPORTED 1 INCH CRACK IN SKIN ABOVE NR 1 ENGINE PYLON, LEFT WING LEADING EDGE. MAINTEN ANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 57-30-04. (M) 2 L 7 2 4F A16WE 1998072400342 19980724 00342 NM 1998 7 24 F3LA98079 1 19980529 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 294 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK 1 INCH ABOVE STRINGER 12L, BS 294.5. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, 51-40-3, FIG 1 AND 53-10-4. (M) 2 L 7 2 4F A16WE 1998072400343 19980724 00343 NM 1998 7 24 PCAA9800772 1 19980521 A 5542 SKIN DHAV DHC8 DHC8102 2809003 NM FWD RUDDER TORN A PCAA K NONE O OTHER NR NOT REPORTED 1 EA 13 808EX 299 TRAILING RUDDER HAD HOLE TORN IN LEFT LOWER SKIN. HOLE WAS CAUSED BY CLOSING PLATE ON THE BOTTOM OF THE FORE RUDDER COM ING OFF. THE CLOSING PLATE WAS MISSING, RIVETS WERE STILL PRESENT. THE FORE AND AFT RUDDERS WERE REPLACED IAW DHC PROC EDURES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998072400345 19980724 00345 NM 1998 7 24 USAASB98126 1 19980528 A 7931 TRANSMITTER BOEING 737 7372B7 1384560 NM NR 2 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 EA 19 270AU 22882 SAV - FL1896 - CAPTAIN REPORTED THE NR 2 ENGINE INDICATED HIGH OIL PRESSURE WAS IN THE YELLOW BAND. POWER WAS REDUCED A ND OIL PRESSURE DROPPED SLOWLY TO THE BOTTOM OF THE YELLOW BAND. FLIGHT DIVERTED TO SAV AND LANDED WITHOUT FURTHER INCI DENT. AN EMERGENCY WAS DECLARED. NO ENGINE SHUTDOWN OCCURRED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL PR ESSURE TRANSMITTER AND THE OIL PRESSURE REGULATOR. OPERATIONAL CHECK GOOD. ALL ENGINE PARAMETERS NORMAL. (M) 2 L 7 2 4F A16WE 1998072400346 19980724 00346 NM 1998 7 24 98ZZZM487 1 19980528 A 7931 REGULATOR BOEING 737 7372B7 1384560 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 EA 19 270AU 22882 SAV - FL1896 - CAPTAIN REPORTED THE NR 2 ENGINE INDICATED HIGH OIL PRESSURE WAS IN THE YELLOW BAND. POWER WAS REDUCED A ND OIL PRESSURE DROPPED SLOWLY TO THE BOTTOM OF THE YELLOW BAND. FLIGHT DIVERTED TO SAV AND LANDED WITHOUT FURTHER INCI DENT. AN EMERGENCY WAS DECLARED. NO ENGINE SHUTDOWN OCCURRED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE OIL PR ESSURE TRANSMITTER AND THE OIL PRESSURE REGULATOR. OPERATIONAL CHECK GOOD. ALL ENGINE PARAMETERS NORMAL. (M) 2 L 7 2 4F A16WE 1998072400347 19980724 00347 WP 1998 7 24 TWAA9808201 1 19980522 A 4990 OIL SYSTEM DOUG DC9 DC983 3022083 WP APU LEAKING A TWAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 05 931TW 49527 JFK - FLT 412 - AFTER LANDING SMOKE APPEARED IN THE CABIN. PLACARDED THE APU MFG P/N 381276-1 INOP DUE TO AND OIL LEAK. (M) 2 L 7 2 4F RT A6WE 1998072400348 19980724 00348 WP 1998 7 24 TWAA9808202 1 19980522 A 2612 59585701 FIRE LOOP DOUG DC9 DC982 3022082 WP RT ENGINE MALFUNCTIONED A TWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 05 953U 49267 IND - DLT 295 - DURING CRUISE, RT ENGINE FIRE WARNING CAME ON BOTH LOOPS. ACCOMPLISHED FLIGHT HAND BOOK PROCEDURES. RE PLACED FIRE WARNING LOOPS MFG P/N 5958570-1. (M) 2 L 7 2 4F A6WE 1998072400349 19980724 00349 WP 1998 7 24 TWAA9808204 1 19980523 A 2130 77530K VALVE DOUG DC9 DC982 3022082 WP CABIN PRESS CONT MALFUNCTIONED A TWAA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 05 906TW 4645 49160 MCI - FLT 326 - DURING CRUISE, AT FL 280, THE CABIN ALTITUDE ROSE TO 12,000 FT. REPLACED THE LEFT AND RIGHT FLOW PILOT REGULATOR VALVES MFG P/NS 77530K AND 25251X RESPECTIVELY. (M) 2 L 7 2 4F A6WE 1998072400350 19980724 00350 WP 1998 7 24 98ZZZM488 1 19980523 A 2130 25251X VALVE DOUG DC9 DC982 3022082 WP CABIN PRESS CONT MALFUNCTIONED A TWAA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 05 906TW 4437 49160 MCI - FLT 326 - DURING CRUISE, AT FL 280, THE CABIN ALTITUDE ROSE TO 12,000 FT. REPLACED THE LEFT AND RIGHT FLOW PILOT REGULATOR VALVES MFG P/NS 77530K AND 25251X RESPECTIVELY. (M) 2 L 7 2 4F A6WE 1998072400351 19980724 00351 WP 1998 7 24 TWAA9808205 1 19980524 A 3260 39396741 SENSOR DOUG DC9 DC982 3022082 WP LT MLG MALFUNCTIONED A TWAA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 904TW 49156 STL - FLT 649 - AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR AND DOOR LIGHT REMAINED ON. CYCLED GEAR AND LIGHTS WENT OUT. ADJUSTED LEFT MAIN LANDING GEAR DOOR POSITION SENSOR TARGET MFG P/N 3939674-1. (M) 2 L 7 2 4F A6WE 1998072400352 19980724 00352 WP 1998 7 24 TWAA9808206 1 19980526 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9413T 53188 STL - FLT 296 - DURING PREFLIGHT, FOUND EGRESS LIGHTS INOP AT ROW 3C. REPLACED LAMP MODULE ASSEMBLY MFG P/N 0105606-003 . (M) 2 L 7 2 4F RT A6WE 1998072400353 19980724 00353 WP 1998 7 24 TWAA9808301 1 19980525 A 2530 50381 OVEN DOUG DC9 DC982 3022082 WP AFT GALLEY MALFUNCTIONED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 919TW 000049 49368 STL - FLT 100 - DURING CRUISE, THE COACH GALLEY OVEN L2 EMITTED STRONG ELECTRICAL FUMES. REPLACED THE AFT GALLEY L2 OVE N MFG P/N 50381. (M) 2 L 7 2 4F A6WE 1998072400354 19980724 00354 NM 1998 7 24 TWAA9808401 1 19980527 A 2913 A003362 PUMP BOEING 727 727231 1384079 NM 'B' HYD SYSTEM FAILED A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 54352 327146 21984 STL - FLT 484 - DURING CRUISE, LOST 'B' HYDRAULIC SYSTEM PRESSURE. REPLACED 'B' SYSTEM HYDRAULIC PUMPS NR 1 AND NR 2 MF G P/N A00336-2. (M) 2 L 7 3 4F A3WE 1998072400355 19980724 00355 NM 1998 7 24 98ZZZM489 1 19980527 A 2913 A003362 PUMP BOEING 727 727231 1384079 NM 'B' HYD SYSTEM FAILED A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 54352 37066A 21984 STL - FLT 484 - DURING CRUISE, LOST 'B' HYDRAULIC SYSTEM PRESSURE. REPLACED 'B' SYSTEM HYDRAULIC PUMPS NR 1 AND NR 2 MF G P/N A00336-2. (M) 2 L 7 3 4F A3WE 1998072400356 19980724 00356 WP 1998 7 24 TWAA9808501 1 19980527 A 3350 58222 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 978Z 47250 STL - FLT 281 - DURING PREFLIGHT CHECK, FOUND L1 AND R1 EMERGENCY EXIT LIGHTS AND EGRESS LIGHTS IN AREA OF ROW 7 INOP. R EPLACED POWER SUPPLY MFG P/N 5822-2 AND FLOOR FLEX CABLE MFG P/N 5853-1 RESPECTIVELY. (M) 2 L 7 2 4F A6WE 1998072400357 19980724 00357 WP 1998 7 24 TWAA9808701 1 19980522 A 5330 SKIN DOUG DC9 DC932 3022066 WP CARGO DOORWAY DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 920L 47734 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT CARGO DOOR CUTOUT SKIN DAMAGED ON LOWER FORWARD SIDE. REPAIRED SKIN AND INSTALLED DOUBLER PER SRM 53-05, PAGE 261. (M) 2 L 7 2 4F A6WE 1998072400358 19980724 00358 WP 1998 7 24 TWAA9808702 1 19980522 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 920L 47734 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT PRESSURE BULKHEAD, UPPER ANGLE CRACKED ONE INCH AT 9 O'CLOCK POSITION, F ORWARD SIDE OF AFT PRESSURE BULKHEAD. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998072400359 19980724 00359 WP 1998 7 24 TWAA9808703 1 19980528 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 920L 47734 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LOWER ANGLE CRACKED ONE INCH AT 3 O'CLOCK POSITION ON FORWARD SIDE OF AFT PR ESSURE BULKHEAD. REPAIRED ANGLE WITH DOUBLER PER SRM 53-01, PAGE 10. (M) 2 L 7 2 4F A6WE 1998072400360 19980724 00360 WP 1998 7 24 USAAD98089 1 19980517 A 2781 INDICATOR DOUG DC9 DC981 3022081 WP COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 828US 48028 TPA - FL 382, DURING CLIMB-OUT, THE SLAT DISAGREE LIGHT ILLUMINATED. AFTER CYCLING THE SLATS THE LIGHT REMAINED ON. TH E CREW ELECTED TO RETURN TO THE FIELD AND LANDED WITHOUT INCIDENT. THE LANDING WEIGHT WAS 132,500 LBS. MAINTENANCE LUB RICATED THE SLAT DRUM ASSEMBLY, INSPECTED ALL LEADING EDGE SLATS FOR PROPER POSITION, AND OPERATED THE SLATS/FLAPS NUMER OUS TIMES. THE SYSTEM WORKED NORMAL. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED, NO DEFECTS NOTED. (M) 2 L 7 2 4F A6WE 1998072400361 19980724 00361 1998 7 24 USAAD98088 4 19980515 A 3414 45501607 LINE DOUG DC9 DC931 3022065 WP LT COCKPIT LEAKING A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 980VJ 48156 DCA-SDF - FL 201, THE CAPTAINS ALTIMETER WAS ERRATIC WITH A 500 FT DROP IN CORRECTED MODE. THE DIFFERENTIAL DECREASED W ITH A DECREASE IN ALTITUDE. THE AIRCRAFT WAS DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAC H AIRSPEED INDICATOR AND A LEAKING STATIC LINE AT THE MACH SPEED INDICATOR. BOTH ALTIMETERS WERE ALSO REPLACED AS A PRE CAUTIONARY MEASURE. (M) 2 L 7 2 4F A6WE 1998072400362 19980724 00362 1998 7 24 98ZZZM490 4 19980515 A 3414 B220081104 AIRSPEED IND DOUG DC9 DC931 3022065 WP LT COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 980VJ 48156 DCA-SDF - FL 201, THE CAPTAINS ALTIMETER WAS ERRATIC WITH A 500 FT DROP IN CORRECTED MODE. THE DIFFERENTIAL DECREASED W ITH A DECREASE IN ALTITUDE. THE AIRCRAFT WAS DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAC H AIRSPEED INDICATOR AND A LEAKING STATIC LINE AT THE MACH SPEED INDICATOR. BOTH ALTIMETERS WERE ALSO REPLACED AS A PRE CAUTIONARY MEASURE. (M) 2 L 7 2 4F A6WE 1998072400363 19980724 00363 1998 7 24 98ZZZM491 4 19980515 A 3416 A4086910121 ALTIMETER DOUG DC9 DC931 3022065 WP LT COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 980VJ 48156 DCA-SDF - FL 201, THE CAPTAINS ALTIMETER WAS ERRATIC WITH A 500 FT DROP IN CORRECTED MODE. THE DIFFERENTIAL DECREASED W ITH A DECREASE IN ALTITUDE. THE AIRCRAFT WAS DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE MAC H AIRSPEED INDICATOR AND A LEAKING STATIC LINE AT THE MACH SPEED INDICATOR. BOTH ALTIMETERS WERE ALSO REPLACED AS A PRE CAUTIONARY MEASURE. (M) 2 L 7 2 4F A6WE 1998072400364 19980724 00364 WP 1998 7 24 USAAD98093 1 19980520 A 2150 FITTING DOUG DC9 DC982 3022082 WP LT PACK LOOSE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 824US 49143 CLT - FLT 306 - DURING CLIMB-OUT, AT 15,000 FT THE CABIN PRESSURE CONTINUED TO CLIMB. THE AIRCRAFT RETURNED TO THE FIEL D AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED A LOOSE FITTING AT THE LEFT AIRCONDITIONING PACK FLOW CONTROL VALV E. (M) 2 L 7 2 4F A6WE 1998072400365 19980724 00365 WP 1998 7 24 USAAD98095 1 19980522 A 3350 P4010020 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 976VJ 48147 DCA - THE GALLEY SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F A6WE 1998072400366 19980724 00366 WP 1998 7 24 USAAD98096 1 19980526 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 LGA - THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE AND THE REMOTE TAILCONE LOW LEVEL LIGHT RECE IVER GREEN LIGHT DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT BATTERY AND THE REMOTE TAILCONE LOW LEVEL LIGHT RECEIVER. (M) 2 L 7 2 4F A6WE 1998072400367 19980724 00367 WP 1998 7 24 98ZZZM492 1 19980526 A 3350 8732030153 BATTERY DOUG DC9 DC982 3022082 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 LGA - THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE AND THE REMOTE TAILCONE LOW LEVEL LIGHT RECE IVER GREEN LIGHT DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT BATTERY AND THE REMOTE TAILCONE LOW LEVEL LIGHT RECEIVER. (M) 2 L 7 2 4F A6WE 1998072400368 19980724 00368 WP 1998 7 24 USAAD98086 1 19980531 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 974VJ 47130 PIT - THE COCKPIT AND FORWARD FLIGHT ATTENDANT OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE SECURED A LOOSE WIRE TO THE POWER SUPPLY AND REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998072400369 19980724 00369 WP 1998 7 24 USAAD98087 1 19980515 A 3350 41B030F00101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 956VJ 47588 CMH - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT BATTERY . (M) 2 L 7 2 4F A6WE 1998072400370 19980724 00370 WP 1998 7 24 USAAD98091 1 19980515 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 829US 49429 THE PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998072400371 19980724 00371 WP 1998 7 24 USAAD98090 1 19980517 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 931VJ 47188 CMH - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 5 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998072400372 19980724 00372 WP 1998 7 24 USAAD98092 1 19980513 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 931VJ 47188 CMH - THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998072400373 19980724 00373 WP 1998 7 24 USAAD98085 1 19980513 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 MCO - THE EMERGENCY LIGHTS AT THE AFT OVERWING EXITS AND THE AFT FLIGHT ATTENDENT POSITION WERE INOPERATIVE. MAINTENANC E REPLACED THE AFT OVERWING EXIT LIGHT POWER SUPPLY AND THE AFT FLIGHT ATTENDANT POSITION LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998072400374 19980724 00374 WP 1998 7 24 98ZZZM493 1 19980513 A 3350 L201919 LIGHT DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 MCO - THE EMERGENCY LIGHTS AT THE AFT OVERWING EXITS AND THE AFT FLIGHT ATTENDENT POSITION WERE INOPERATIVE. MAINTENANC E REPLACED THE AFT OVERWING EXIT LIGHT POWER SUPPLY AND THE AFT FLIGHT ATTENDANT POSITION LIGHT ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998072400375 19980724 00375 WP 1998 7 24 USAAD98094 1 19980521 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 993VJ 47332 CMH - THE MID CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE MID CABIN CEI LING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998072400376 19980724 00376 NM 1998 7 24 USAA980225 1 19980519 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 31045 24411 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND 1.5 INCH LONG CRACK LOWER FUSELAGE BS 727D PLUS 1B LBL 1 SKIN. REMOVED DAMAGED NDT CONFIRM CRACK CONTAINMENT, INSTALLED AND COMPLETED REPAIR PER SRM 53-00-01. (M) 2 L 7 2 4F A16WE 1998072400377 19980724 00377 NM 1998 7 24 USAA980224 1 19980519 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 529AU 31045 24411 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .5 INCH LONG CRACK FORWARD SIDE OF BS 727D FRAME RBL 2 FRAME. CUTOUT DA MAGED AREA, INSTALLED DOUBLER, REPAIRED PER 737-300 SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F A16WE 1998072400378 19980724 00378 NM 1998 7 24 USAASB98118 1 19980519 A 3260 655825029 CIRCUIT BOEING 737 7374B7 1384702 NM E/E BAY FAILED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 426US 24548 ROC - FL 391 - ON APPROACH TO ROC, THE NOSE GEAR GREEN LIGHT FLICKERED WHEN SELECTING THE GEAR DOWN AND THE WARNING HORN SOUNDED WHEN FLAPS WERE SELECTED TO 15 DEGREES. RECYCLED GEAR AND ON THIRD GEAR EXTENSION RECEIVED ALL THREE GREEN LIG HTS AND NO HORN AT ANY FLAP SETTING. GEAR WAS VERIFIED DOWN ALL THREE TIMES THROUGH SIGN GLASS/VIEWING PORT. FLIGHT LA NDED W/O FURTHER INCIDENT WITH NO EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED THE M983 CIRCUIT CARD INSIDE THE E11 LANDING GEAR LOGIC SHELF. SLUGGED NOSE LANDING GEAR SWITCHES AND GREASED GEAR. PERFORMED TEST FLIGHT. GEAR OPERA TIONAL CHECK GOOD IN ASSOCIATION WITH MM. (M) 2 L 7 2 4F RT A16WE 1998072400379 19980724 00379 WP 1998 7 24 HALA9800165 1 19980614 A 2450 CIRCUIT BREAKER DOUG DC10 DC1010 3022110 WP CB PANEL TRIPPED A HALA K NONE J WARNING INDICATION CR CRUISE 1 WP 13 160AA 46710 FLT 482 - PPT - LEFT EMERGENCY AC BUS OFF LIGHT ILLUMINATED. FOLLOWING CHECKS AND FOUND CIRCUIT BREAKER B-20 (TR 1 INPU T) POPPED. RESET, SYSTEM RETURNED TO NORMAL AT TIME OF FAILURE ST. ELMO'S FIRE WAS OBSERVED. AFTER THE ABOVE EVENT, T HE FLAP LIMIT CHANNEL INOP LIGHT ILLUMINATED AND REMAINED ILLUMINATED. SYSTEM TEST OF LEFT EMERGENCY AC BUS, CHECKED OK . OK FOR SERVICE. RESET NR 1 AND NR 2 FLAP LIMIT AND ELEVATOR LOAD FEEL CIRCUIT BREAKER, OPS CHECK OK. RESET NR 1 AND NR 2 ELEVATOR LOAD FEEL AND FLAP CIRCUIT BREAKER, OPERATIONAL CHECK OK. (M) 2 L 7 3 4F A22WE 1998072400380 19980724 00380 NM 1998 7 24 98ZZZM494 1 19980527 A 3350 60132171 POWER SUPPLY BOEING 737 7372H5 138448E NM CABIN INOPERATIVE A E9WA K NONE L NO TEST IN INSP/MAINT 1 SO 05 221US 20454 FORWARD LEFT (PAX) AND RT SERVICE DOOR EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTS POWER SUPPLY PACK, S/N ON 1715, S/N OFF 15002, P/N 60-1321-1, IAW MM 33-51-71. (M) 2 L 7 2 4F A16WE 1998072400381 19980724 00381 NM 1998 7 24 98ZZZM495 1 19980522 A 3350 1315 BULB BOEING 737 7372H5 138448E NM CABIN FAILED A E9WA K NONE L NO TEST IN INSP/MAINT 1 SO 05 220US 20453 FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BULB. (M) 2 L 7 2 4F A16WE 1998072400382 19980724 00382 NM 1998 7 24 98ZZZM496 1 19980522 A 3397 WIRE BOEING 737 7372H5 138448E NM CABIN CHAFED A E9WA K NONE L NO TEST IN INSP/MAINT 1 SO 05 220US 20453 EMERGENCY EXIT LIGHT PATH INOP. REPAIRED BROKEN WIRE UNDER SEAT 2ABC. (M) 2 L 7 2 4F A16WE 1998072400383 19980724 00383 NM 1998 7 24 EIAA980199 1 19980511 A 3260 LIGHT BOEING 747 747273C 1384896 NM NLG DOOR ILLUMINATED A EIAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 09 471EV 20651 ABORTED TAKEOFF AFTER NOSE DOOR LIGHT ILLUMINATED ON TAKEOFF ROLL. OPENED AND CLOSED NOSE DOOR TWICE. VERIFIED AND CHE CKED VISUALLY ALL LATCHES PINS PRIOR TO DEPARTURE. (M) 2 L 7 4 4F A20WE 1998072400384 19980724 00384 WP 1998 7 24 EIAA980198 1 19980505 A 2170 WW148 CLAMP DOUG DC9 DC933F 302207A WP RT WATER SEP LOOSE A EIAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 945F 47279 AIRCRAFT RETURNED TO BOISE, AIRCRAFT WAS PRESSURIZED ON GROUND. PROBLEM WAS FOUND TO BE A DUCT DISCONNECTED AT RT WATER SEPARATER. FOUND CLAMP OFF DUCT ON OUTLET SIDE OF RT WATER SEPARATER. REINSTALLED CLAMP. OP'S CHECK AND LEAK CHECK G OOD. (M) 2 L 7 2 4F A6WE 1998072400385 19980724 00385 NM 1998 7 24 BJNA980501 1 19980524 A 2613 65528087 OVERHEAT LIGHT BOEING 737 737214 138446R NM LT WING/BODY ILLUMINATED A BJNA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 LEFT WING BODY OVERHEAT LIGHT CAME ON EN ROUTE. REMOVED AND REPLACED COMP OVERHEAT UNIT PER BMM 26-17-0, OPS TEST PERFO RMED PER BMM 26-18-0, TEST OK. (M) 2 L 7 2 4F A16WE 1998072400386 19980724 00386 NM 1998 7 24 BJNA980502 1 19980525 A 2613 CONNECTOR BOEING 737 737214 138446R NM LT WING/BODY DIRTY A BJNA O OTHER N FALSE WARNING DE DESCENT 1 WP 11 457TM 20156 LEFT WING BODY OVERHEAT LIGHT CAME ON DURING DESCENT. CLEANED CONNECTORS OF SENSING ELEMENT ON LEFT ENGINE STRUT CAVITY TESTED WING AND LOWER AFT BODY OVERHEAT DETECTION SYSTEM PER BMM 26-18-0, PAGE 501, TO 502, TEST OK. (M) 2 L 7 2 4F A16WE 1998072400387 19980724 00387 NM 1998 7 24 BJNA980506 1 19980528 A 2613 OVERHEAT LIGHT BOEING 737 737214 138446R NM LT WING/BODY ILLUMINATED A BJNA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 LEFT WING BODY OVERHEAT LIGHT ILLUMINATED DURING THE DESCENT INTO KEKO. AIRCRAFT RELEASED PER MEL 26-12, DMI 10508, ITE M PLACARDED AND TRANSFERRED TO DMI LOG. (M) 2 L 7 2 4F A16WE 1998072400388 19980724 00388 NM 1998 7 24 BJNA980505 1 19980527 A 2612 655280915 FIRE DETECTOR BOEING 737 737214 138446R NM LT WING/BODY MALFUNCTIONED A BJNA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 LEFT WING BODY OVERHEAT ILLUMINATES, QRH PROCEDURE, LIGHT WENT OUT THEN CONTINUED FLICKERING DURING DESCENT. CHECKED AL L LOOPS WITH OHM METER AND MAGER, FOUND NO PROBLEM CHANGED FIRE DETECT ASSY UNIT TEST FLEW AIRCRAFT COULD NOT DUPLICATE PROBLEM. (M) 2 L 7 2 4F A16WE 1998072400389 19980724 00389 NM 1998 7 24 BJNA980504 1 19980527 A 3610 CLAMP BOEING 737 737214 138446R NM LT WING/BODY LOOSE A BJNA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 11 457TM 20156 LEFT WING BODY OVERHEAT LIGHT ILLUMINATED, FOLLOWED QRH PROCEDURE AND AFTER A FEW MOMENTS THE OVERHEAT LIGHT WENT OUT. R ETORQUED CLAMP ON INBOARD END OF AIR CLEANER AT FORWARD END OF LEFT A/C BAY PER BMM 36-19-11, GRUOND CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1998072400390 19980724 00390 NM 1998 7 24 BJNA980503 1 19980526 A 2613 CONNECTOR BOEING 737 737214 138446R NM LT WING/BODY DIRTY A BJNA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 11 457TM 20156 LEFT WING BODY OVERHEAT ILLUMINATES INTERMITTENTLY. CLEANED CONNECTORS ON FORWARD AND AFT KEEL BEAM SENSOR, OPS CHECK N ORMAL. OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1998072400391 19980724 00391 EU 1998 7 24 98ZZZM497 1 19980527 A 2120 AIR DISTRIBUTION AIRBUS 310 A310324 3930206 EU COCKPIT SMOKE A AJLF A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 23 837AB 674 AFTER TAKEOFF, AVIONICS SMOKE ALARM APPEARED ON ECAM WIHT A STRONG SMELL NOTED IN THE COCKPIT. ECAM ACTION CARRIED OUT AND WARNING DISAPPEARED AFTER TWENTY SECONDS. AIRCRAFT RETURNED TO RAMP FOR RECTIFICATION. AIRCRAFT HAD A HIGH ENERGY STOP CAUSING TWO BLOWN TYPE FUSES AND FOUR BRAKES SEIZED. THE CAUSE OF THE SMOKE IN THE CABIN IS STILL BEING INVESTIGAT ED. 2 L 7 2 4F RT A35EU 1998072400392 19980724 00392 1998 7 24 ASAA9880096 4 19980531 A 2565 D29982107 SLIDE DOUG DC9 DC983 3022083 WP L1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 949AS 2008 53022 PHX - DURING C-CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1998072400393 19980724 00393 WP 1998 7 24 ASAA9880095 1 19980531 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN AND TAILCONE AREA WERE FOUND INOPERATI VE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400394 19980724 00394 WP 1998 7 24 ASAA9880093 1 19980526 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 943AS 53018 ANC - FLT 194 - PRIOR TO DEPARTURE, THE FORWARD FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WI RING IN FORWARD FLOOR TRACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400395 19980724 00395 WP 1998 7 24 ASAA9880092 1 19980525 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP AFT CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING MAINTENANCE CHECK, THE AFT TWO OVERHEAD EMERGENCY EXIT LIGHTS AND LOWER TAILCONE LIGHTS WERE FOUND INOPERAT IVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400396 19980724 00396 WP 1998 7 24 ASAA9880090 1 19980524 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP L-1 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING MAINTENANCE CHECK, THE PORTABLE EMERGENCY EXIT LIGHT AT THE L-1 DOOR WAS FOUND INOPERATIVE. RELAMPED AND L IGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400397 19980724 00397 WP 1998 7 24 ASAA9880089 1 19980522 A 3350 0105606003 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 931AS 49232 SEA - FLT 231 - PRIOR TO DEPARTURE, CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTING HAS LOOSE WIRING AND IS MISSING A LAMP AT ROW 2. REPLACED LAMP MODULE AND SECURED WIRING AT ROW 2, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998072400398 19980724 00398 WP 1998 7 24 ASAA9880088 1 19980522 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 948AS 53021 SEA - FLT 414 - PRIOR TO DEPARTURE, CREW REPORTED EMERGENCY EXIT FLOOR TRACK LIGHTS FROM SEAT 1-D FORWARD WERE INOPERATI VE. REPLACED TWO LAMP MODULES AT SEAT 1-D AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400399 19980724 00399 WP 1998 7 24 ASAA9880085 1 19980517 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPAIRED WIRI NG TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400400 19980724 00400 WP 1998 7 24 ASAA9880084 1 19980517 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 943AS 53018 SEA - AFTER ARRIVAL OF FLT 104, CREW REPORTED THE OVERHEAD EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400401 19980724 00401 NM 1998 7 24 ASAA9810039 1 19980522 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, THE FIRST CLASS EMERGENCY EXIT FLOOR TRACK LIGHT LEFT TRANSMITTER WAS FOUND TO BE INOPER ATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998072400402 19980724 00402 NM 1998 7 24 AALA981088 1 19980530 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 649AA 24607 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT MID GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998072400403 19980724 00403 NM 1998 7 24 AALA981087 1 19980530 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 649AA 24607 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT OVERWING EXITS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT OVERWING EXITS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998072400404 19980724 00404 NM 1998 7 24 AALA981078 1 19980527 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 306AA 22312 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 30H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECT OR AT SEAT 30H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400405 19980724 00405 NM 1998 7 24 AALA981030 1 19980526 A 3397 WIRE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 617AM 24525 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN MID CABIN INOPERATIVE. RECONNECTED LOOSE JUMP ER WIRES ON TRACK LIGHT STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998072400406 19980724 00406 NM 1998 7 24 AALA981028 1 19980526 A 3350 SOCKET BOEING 767 767223 1385123 NM CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324AA 22325 SFO - DURING OVERNIGHT MAINTENANCE, LEFT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CORROSION FROM LEFT FORWARD EMERGENCY EXIT LIGHT SOCKET AND RELAMPED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400407 19980724 00407 NM 1998 7 24 AALA981027 1 19980526 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39356 24037 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERHEAD LIGHT AT COCKPIT DOOR DOSE NOT WORK WITH SWITCH. SECURED LOOSE G ROUND WIRE ON EMERGENCY OVERHEAD LIGHT AT COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400408 19980724 00408 NM 1998 7 24 AALA981026 1 19980526 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 39356 24037 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT ROW 38J INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT CONNECTOR AT SEAT ROW 38J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400409 19980724 00409 NM 1998 7 24 AALA981021 1 19980524 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352AA 24033 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT ROW 24AB INOPERATIVE. REPAIRED EMERGENCY EXIT LIG HT WIRE AT SEAT ROW 24AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400410 19980724 00410 NM 1998 7 24 AALA980931 1 19980509 A 3350 1001141 LIGHT BOEING 727 727227 1384078 NM CABIN MALFUNCTIONED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722AA 20730 DFW - DURNIG OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT IS BLINKING OFF AND ON. REPLACED AFT AIRSTAIR EMERGENCY EX IT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400411 19980724 00411 NM 1998 7 24 AALA980820 1 19980422 A 3350 10060091101 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6818 19493 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERHEAD EXIT SIGN LIGHT AT L2 SERVICE DOOR INOPERATIVE. REPLACED L2 EMER GENCY OVERHEAD EXIT SIGN LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400412 19980724 00412 NM 1998 7 24 AALA980941 1 19980510 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 898AA 22014 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN CABIN INOPERATIVE. REPAIRED WIRING IN CABIN F ORWARD OF SEATS. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400413 19980724 00413 NM 1998 7 24 AALA980714 1 19980407 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT COACH INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LGHT STRIP IN AFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400414 19980724 00414 NM 1998 7 24 AALA980711 1 19980407 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 881AA 21520 DFW - DURING OVERNIGHT MAINTENANCE, AFT SECTION OF COACH EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERG ENCY EXIT FLOOR PATH LIGHT STRIP IN AFT COACH SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400415 19980724 00415 NM 1998 7 24 AALA980964 1 19980513 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 875AA 21387 TPA - EMERGENCY EXIT LIGHT OVERHEAD IN AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IN AFT STAIRS. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400416 19980724 00416 NM 1998 7 24 AALA980737 1 19980410 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 873AA 21385 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY PATH FLOOR LIGHTING FLICKERED WHEN TESTED. REPLACED SHORTED CONNECTOR AT SEAT ROW 27ABC. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400417 19980724 00417 NM 1998 7 24 AALA980921 1 19980507 A 3350 AAP2661 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 873AA 21385 TPA - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN MID-CABIN CEILING INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IN MI D-CABIN CEILING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400418 19980724 00418 NM 1998 7 24 AALA980743 1 19980410 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 872AA 21384 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT VENTRAL STAIRWAY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400419 19980724 00419 NM 1998 7 24 AALA980954 1 19980511 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 847AA 20988 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FORWARD GALLEY INOPERATIVE. REPLAC ED EMEREGNCY EXIT FLOOR PATH LIGHTING STRIP NEXT TO FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400420 19980724 00420 NM 1998 7 24 AALA980938 1 19980509 A 3350 3107311 LIGHT BOEING 727 727223 1384074 NM LT WING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 843AA 20984 DFW - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT AFT OVERWING EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400421 19980724 00421 NM 1998 7 24 AALA9800877 1 19980504 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 726AA 20733 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FORWARD CABIN INOPERATIVE. REPAIRED EMERGENCY E XIT FLOOR PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400422 19980724 00422 NM 1998 7 24 AALA980936 1 19980509 A 3350 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722AA 20730 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400423 19980724 00423 NM 1998 7 24 AALA981011 1 19980521 A 3350 1001141 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 718AA 20611 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN AFT AIRSTAIRS INOPERATIVE. REPLACED EMERGENCY EXIT ASSEMBLY LIGHT IN AFT AIRSTAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400424 19980724 00424 EU 1998 7 24 AALA980988 1 19980517 A 3350 2LA00535821 LIGHT FOKKER F28 F28MK0100 4990807 EU RT WING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1447L 11456 ORD - DURING OVERNIGHT MAINTENANCE, RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED RIGHT AFT OVERWING EMERGEN CY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998072400425 19980724 00425 NM 1998 7 24 AALA981020 1 19980523 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702AA 22460 TPA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS ABOVE AFT DOOR AND IN VENTRAL STAIRWAY INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY ABOVE AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400426 19980724 00426 NM 1998 7 24 AALA981079 1 19980527 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 895AA 22011 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT BOTTOM OF AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT ASSEMBLY AT THE BOTTOM OF AFT STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400427 19980724 00427 NM 1998 7 24 AALA981090 1 19980531 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 705AA 9122 22462 TPA - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400428 19980724 00428 NM 1998 7 24 AALA980928 1 19980509 A 2133 10328051 VALVE BOEING 727 727223 1384074 NM ACM BAY DIRTY A AALA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 6835 20188 ORD - FLT 1691 - EN ROUTE ORD-MIA - DURING CLIMB-OUT, COULD NOT CONTROL CABIN PRESSURE. RAN RAPID DEPRESSURIZATION CHEC K LIST WITH NO EFFECT. AIR INTERRUPTED BACK TO ORD, DECLARED EMEREGNCY DUE TO AN OVERWEIGHT CONDITION. LANDED ORD WITH OUT INCIDENT. REMOVED DEBRIS FROM RIGHT CABIN PRESSURE CONTROL OUTFLOW VALVE. PRESSURIZED AIRCRAFT, SYSTEM GROUND CHEC KED NORMAL OPERATION. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION WITH NO DISCREPANCIES NOTED. (M) 2 L 7 3 4F A3WE 1998072400429 19980724 00429 NM 1998 7 24 AALA980994 1 19980515 A 2781 DT2RV212A7 SWITCH BOEING 727 727223 1384074 NM LE FLAP ACT LOOSE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 883AA 21522 MIA - FLT 925 - DURING CLIMB-OUT, FLAPS RETRACTED TO 2 DEGREES AND A LEADING EDGE AMBLER LIGHT ILLUMINATED. POSITION TE ST INDICATED THE NR 3 LEADING EDGE FLAP WAS IN TRANSITION. FLIGHT AIR INTERRUPTED AND RETURNED TO MIA WITHOUT FURTHER I NCIDENT. MAINTENANCE FOUND NR 3 LEADING EDGE ACTUATOR SWITCH LOOSE. NR 3 LEADING EDGE SWITCH WAS TIGHTENED, ADJUSTED, AND CLEANED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998072400430 19980724 00430 WP 1998 7 24 98ZZZM498 1 19980625 A 2910 76140291336 LINE DOUG DC8 DC8F54 3021926 WP LT MLG WW BROKEN A FXLA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 54FA 45637 IN CRUISE BOG TO MIA EXPERIENCED LOSS OF HYDRAULIC QTY. EXECUTED ABNORMAL PROCEDURES AND LANDED MIA WITHOUT INCIDENT. A IRCRAFT TOWED OFF RUNWAY. INSPECTION REVEALED A BROKEN HYDRAULIC LINE IN THE LEFT WHEEL WELL. REPLACED HYDRAULIC LINE, SERVICED SYSTEM AND OPS CHECKED NORMAL. RETURNED TO SERVICE. (M) 2 L 7 4 4F 4A25 1998072400431 19980724 00431 NM 1998 7 24 98ZZZM499 1 19980607 A 5311 FRAME BOEING 737 73733A 1384673 NM BS 616 CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 172AW 23631 DURING 'C' CHECK INSPECTION DISCOVERED CRACKING CONDITIONS ON THE BOTTOM OF THE INNER FRAME CHORD ON BOTH LEFT (LBL 70.5 3) AND RIGHT (RB 70.53) SIDES OF THE AIRCRAFT AT BS 616. REPAIRED BY INSPECTING THE AFFECTED AREA PER SERVICE BULLETIN NUMBER 737-53-1182 SECTION III AND FIGURE 2, REMOVING THE CHORDS, TRIMMING OUT THE CRACKS, FABRICATING AND INSTALLING RE PAIR ANGLES PER INSTALLING CHORDS WITH FASTENERS PER SRM. ACCOMPLISHED IAW AWAA, ENGINEERING REPAIR 3-53-15-23. (M) 2 L 7 2 4F RT A16WE 1998072400432 19980724 00432 NM 1998 7 24 98ZZZM500 1 19980601 A 5312 BULKHEAD FITTING BOEING 727 72723 1384004 NM BS 870 CORRODED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 930FT 58594 19387 DURING C-CHECK INSPECTION, DISCOVERED CORROSION ON THE RIGHT BULKHEAD TERMINAL FITTING AT STATION 870. REPAIRED BY BLEN DING AWAY THE CORROSION, HFEC NDT INSPECTING, FLAP PEENING BLENDED AREA, ALODINING AND DOUBLE PRIMING BARE ALUMINUM AREA S. REPAIRED IAW EVIAA CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N930FT-57-002-EAC. (M) 2 L 7 3 4F A3WE 1998072400433 19980724 00433 NM 1998 7 24 98ZZZM501 1 19980601 A 5730 SKIN BOEING 727 72723 1384004 NM WS 155 CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 930FT 58594 19387 DURING C-CHECK INSPECTION DISCOVERED A CRACK IN THE FIXED LEADING EDGE SKIN AT RIGHT WING LEADING EDGE STATION 155. REP AIRED BY TRIMMING OUT THE CRACK, HFEC NDT INSPECTING, FABRICATING AND INSTALLING A REPAIR DOUBLER AND FILLER WITH BLUEPR INT TYPE FASTENERS. REPAIRED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N930FT-57-006-EAC. ( M) 2 L 7 3 4F A3WE 1998072400434 19980724 00434 NM 1998 7 24 98ZZZM502 1 19980601 A 5313 LONGERON BOEING 727 72723 1384004 NM BS 947/910 WORN B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 930FT 19387 DURING C-CHECK INSPECTION DISCOVERED WEAR MARKS ON THE LEFT AND RIGHT KEEL BEAM LONGERONS AT THE MAIN LANDING GEAR DOOR HINGES, STATION 947 LEFT AND STATION 910 RIGHT. REPAIRED BY BLENDING AWAY THE DAMAGED AREAS, FLAP PEENED, ALODINED, PRI MED AND CORROSION PREVENTATIVE TREATED. REPAIRED IAW EVERGREEN AIR CENTER, ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N 930FT-53-016-EAC. (M) 2 L 7 3 4F A3WE 1998072400435 19980724 00435 WP 1998 7 24 ASAA9880106 1 19980616 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 OAK - DURING 15K CHECK, GOUGE WAS FOUND IN AFT CARGO COMPARTMENT DOOR EDGE ABOVE AFT UPLOCK LATCH FITTING. REMOVED DAMA GED AREA AND INSTALLED REPAIR ANGLE DOUBLER IAW ASA EA 5210-01070. (M) 2 L 7 2 4F RT A6WE 1998072400436 19980724 00436 WP 1998 7 24 ASAA9880107 1 19980616 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 OAK - DURING 15K CHECK, DENT WAS FOUND IN FORWARD CARGO COMPARTMENT DOOR EDGE INBOARD OF AFT UPLOCK LATCH. REMOVED DAMA GED AREA AND INSTALLED REPAIR ANGLE DOUBLER IAW ASA EA 5210-01070. (M) 2 L 7 2 4F RT A6WE 1998072400437 19980724 00437 SO 1998 7 24 C2XA98IA223 1 19980630 A 5320 12006665003 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT CENTER FLOOR SUPPORT BEAM CORRODED FROM FRAMES 28 TO 39. MAINTENANCE REMOVE D AND REPLACED THE DAMAGED SECTION OF THE FLOORBEAM BUTTSTRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400438 19980724 00438 EU 1998 7 24 C2XA98BT041 1 19980619 A 2440 M535061 RECEPTACLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 BTV - ON THE GROUND DAMAGE REPORTED ON GPU RECEPTACLE. REPAIRED GPU RECEPTACLE BOX AND REPLACED RECEPTACLE IAW ATR SRM 53-11-28. OPERATIONALLY CHECKED GOOD AND PRESSURIZATION LEAKED CHECKED GOOD, NO LEAKS NOTED. (M) 2 H 7 2 4T RT A53EU 1998072400439 19980724 00439 EU 1998 7 24 C2XA98BT043 1 19980610 A 7712 311192801 SENSOR AEROSP ATR42 ATR42320 8680930 EU RT ENGINE INTERMITTENT A C2XA E D ENGINE SHUTDOWN RETURN TO BLOCK R J Y PARTIAL RPM/PWR LOSS WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 SW 09 26826 172 EWR - CRE REPORTED RIGHT ENGINE TORQUE GAUGE WENT TO ZERO AT APPROXIMATELY 400 FT AFTER TAKEOFF. APPROXIMATELY 40 PERCE NT AND SHUTDOWN ENGINE ON RETURN FOR LANDING. MAINTENANCE REMOVED AND REPLACED AN INTERMITTENT TORQUE SENSOR ON THE RIG HT ENGINE, OPERATIONALLY CHECKED ON THE GROUND AND TEST FLOWN SATISFACTORILY. (M) 2 H 7 2 4T RT A53EU 1998072400440 19980724 00440 SO 1998 7 24 C2XA98CL047 1 19980629 A 3230 12043270501 RELAY EMB 120 EMB120RT SO COCKPIT FAILED A C2XA O OTHER J WARNING INDICATION DE DESCENT 1 SW 09 12703 5388 120084 CLE - FLT 3259 - CREW REPORTED THAT ON DESCENT THE LANDING GEAR DID NOT EXTEND NORMALLY, THE ELECTRIC OVERRIDE SYSTEM WA S USED TO EXTEND THE GEAR WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THAN REMOVED AND REPLACED THE LA NDING GEAR RELAY BOX IAW EMB-120 MM 32-31-02. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400441 19980724 00441 SO 1998 7 24 C2XA98IA213 1 19980630 A 5320 12006157003 CREASE BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CREASE BEAM CORRODED AT FRAME NR 44. MAINTENANCE REMOVED AND REPLACED THE CREASE BEAM FROM FRAME NR 39 TO 44 IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400442 19980724 00442 SO 1998 7 24 C2XA98IA214 1 19980630 A 5320 12022670002 ANGLE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE VERTICAL FLOOR SUPPORT ANGLE CRACKED AT FRAME NR 13. MAINTENANCE INST ALLED A REPAIR DOUBLER IAE EMB-120 SRM 51-10-02 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400443 19980724 00443 SO 1998 7 24 C2XA98IA215 1 19980630 A 5320 12022670001 ANGLE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE VERTICAL FLOOR SUPPORT ANGLE CRACKED AT FRAME NR 13. MAINTENANCE INSTA LLED A REPAIR DOUBLER IAW EMB-120 SRM 51-1002 AND 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400444 19980724 00444 SO 1998 7 24 C2XA98IA216 1 19980630 A 5347 12015995003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOOR SEAT TRACK CORRODED BETWEEN FRAMES 13 TO 32. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998072400445 19980724 00445 SO 1998 7 24 C2XA98IA217 1 19980630 A 5347 12016000003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLOOR SEAT TRACK CORRODED BETWEEN FRAMES 13 TO 32. MAINTENANCE REMOVE D AND REPLACED THE DAMAGED SECTION OF SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A31SO 1998072400446 19980724 00446 SO 1998 7 24 C2XA98IA218 1 19980630 A 5315 12008972001 FLOORBEAM EMB 120 EMB120RT SO AFT CARGO CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT FLOOR AT CARGO DOOR THRESHOLD CORRODED. MAINTENANCE REMOVE D AND REPLACED THE DAMAGED SECTION IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400447 19980724 00447 SO 1998 7 24 C2XA98IA219 1 19980630 A 5347 12015994003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE WALL SEAT TRACK CORRODED FROM FRAME 18 TO 34. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53--01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400448 19980724 00448 SO 1998 7 24 C2XA98IA220 1 19980630 A 5320 12004170004 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE CENTER 'T' PROFILE AT FRAME 38 CRACKED ON INBOARD SIDE. MAINTENANCE R EMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400449 19980724 00449 SO 1998 7 24 C2XA98IA221 1 19980630 A 5347 12015997003 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE WALL SEAT TRACK CORRODED FROM FRAME 14 TO 34. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW EMB-120 MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400450 19980724 00450 SO 1998 7 24 C2XA98IA222 1 19980630 A 5320 12007053003 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND CENTER FLOOR SUPPORT BEAM CORRODED BETWEEN FRAMES 28 TO 39. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE FLOORBEAM BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400451 19980724 00451 SO 1998 7 24 C2XA98IA224 1 19980630 A 5320 12006647001 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 36. MAINTENANCE REMOVED AN D REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400452 19980724 00452 SO 1998 7 24 C2XA98IA225 1 19980630 A 5320 12014149001 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 38. MAINTENANCE REMOVED AND REP LACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400453 19980724 00453 SO 1998 7 24 C2XA98IA226 1 19980630 A 5320 12007053003 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND CENTER FLOORBEAM CORRODED FROM FRAMES 39 TO 44. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF FLOORBEAM BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400454 19980724 00454 SO 1998 7 24 C2XA98IA228 1 19980630 A 5320 12004449001 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT CENTER FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 36. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400455 19980724 00455 SO 1998 7 24 C2XA98IA227 1 19980630 A 5320 12004166001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOOR SUPPORT BEAM CORRODED FROM FRAMES 34 TO 38. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE FLOORBEAM BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400456 19980724 00456 SO 1998 7 24 C2XA98IA229 1 19980630 A 5320 12004449001 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT CENTER FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 38. MAINTENANCE REMOVED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400457 19980724 00457 SO 1998 7 24 C2XA98IA230 1 19980630 A 5320 12006169001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLOOR SUPPORT BEAM CORRODED FROM FRAME 34 TO 44. MAINTENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE FLOOR SUPPORT BEAM BUTT-STRAP IAW EMB-120 SRM 51-40-01. THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400458 19980724 00458 SO 1998 7 24 C2XA98IA231 1 19980630 A 5320 12004149002 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT OUTBOARD FLOOR SUPPORT 'T' PROFILE CORRODED AT FRAME 40. MAINTENANCE REMOV ED AND REPLACED THE 'T' PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400459 19980724 00459 SO 1998 7 24 C2XA98IA232 1 19980630 A 5753 12011990001 RIB EMB 120 EMB120RT SO LT TE FLAP CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP CRACKED ON OUTBOARD NOSE RIB. MAINTENANCE STOP-DRILLED THE CRA CK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 54-20-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400460 19980724 00460 SO 1998 7 24 C2XA98IA233 1 19980630 A 5411 12024718001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME 9 CRACKED ON THE OUTBOARD UPPER AFT SIDE. MAINTENANCE STOP DR ILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998072400461 19980724 00461 SO 1998 7 24 C2XA98IA234 1 19980630 A 5400 12037317001 SUPPORT EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP OUTBOARD RIB LOWER SKIN SUPPORT CRACKED. MAINTENANCE STOP DRIL LED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400462 19980724 00462 SO 1998 7 24 C2XA98IA235 1 19980630 A 5713 12004363001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER STRINGER NR 8 CRACKED ON INBOARD END NEAR THE AREA OF ACCESS 522E B. MAINTENANCE REMOVED THE DAMAGED SECTION OF THE STRINGER AND FABRICATED AND INSTALLED A STRINGER SPLICE IAW EMB-120 S RM 57-20-03 AND CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5710-01010. THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400463 19980724 00463 SO 1998 7 24 C2XA98IA236 1 19980630 A 5730 12033270001 SKIN EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER SKIN CRACKED AT THE AFT OUTBOARD CORNER OF ACCESS 522EB. MAINTEN ANCE FABRICATED AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998072400464 19980724 00464 SO 1998 7 24 C2XA98IA237 1 19980630 A 5730 12033270001 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER SKIN CRACKED OUTBOARD AFT OF ACCESS 622EB BETWEEN RIBS 8 AND 9. MAINTENANCE INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400465 19980724 00465 SO 1998 7 24 C2XA98IA238 1 19980630 A 5713 12004363002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LOWER STRINGER NR 8 CRACKED OUTBOARD OF RIB 8. MAINTENANCE REMOVED TH E DAMAGED SECTION OF STRINGER AND INSTALLED A REPAIR SPLICE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZAT ION (ECRA) EC5710-01010. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400466 19980724 00466 SO 1998 7 24 C2XA98IA239 1 19980630 A 3211 20696 TRUNNION EMB 120 EMB120RT SO LT MLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 18289 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT MAIN LANDING GEAR OLEO STRUT, LOWER TRUNNION CORRODED AT SECONDARY LOCKING S TRUT ATTACHMENT. MAINTENANCE REMOVED AND REPLACED THE TRUNNION IAW EMB-120 CMM 32-12-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998072400467 19980724 00467 SO 1998 7 24 C2XA98IA240 1 19980630 A 5713 12016085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER STRINGER NR 10 CRACKED IN TWO PLACES ON INBOARD SIDE OF WING NEAR ACCESS 544EB AND 144GB. MAINTENANCE REMOVED THE DAMAGED SECTION OF STRINGER AND INSTALLED A REPAIR SPLICE IAW CONTINEN TAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5710-01010. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998072400468 19980724 00468 1998 7 24 C2XA98CL046 4 19980609 A 3417 7014700918 ADC EMB 145 EMB145 SO COCKPIT CONTAMINATED A C2XA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 SW 09 14940 1275 97071326 145033 SDF - FLT 4042 - AIRCRAFT DIVERTED INTO SDF DUE TO A UNCOMMANDED LEFT ENGINE SHUT DOWN. WHILE TROUBLE SHOOTING THE AIRC RAFT MAINTENANCE FOUND ADC FAULTS ON THE MFD CAUSING FADEC FAILURES. THE LEFT ENGINE FAILED WHEN ALT FADEC WAS SELECTED . MAINTENANCE ALSO FOUND MACH NUMBERS SPLIT WHILE DOWN LOADING THE FADEC AND CMC. THE AIR DATA COMPUTER STATIC LINES W ERE DRAINED OF MOISTURE, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY IAW EMB-145 MM 34-13-00. THE LEFT ENGINE OPERATI ONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998072400469 19980724 00469 EU 1998 7 24 C2XA98BT045 1 19980626 A 6120 8088777 PCU AEROSP ATR72 ATR72212 EU NR 1 ENGINE FAILED A C2XA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 09 69902 3918 385 EWR - FLT 3308 - ON TAKEOFF FROM NEWARK, AIRCRAFT NR 1 ENGINE STARTED TO FEATHER, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND THE PROPELLER CONTROL UNIT TO BE CAUSING THE PROBLEM. REMOVED AND REPLACED PCU WITH SERVICEABLE UNIT, OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998072400470 19980724 00470 EU 1998 7 24 C2XA98BT044 1 19980626 A 2731 E0242A26A0 RELAY AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAILED A C2XA C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 SW 09 18814 103 EWR - DURING TAKEOFF CREW FOUND BOTH CAPTAINS AND FIRST OFFICERS NOSE DOWN ELEVATOR TRIM DIDN'T WORK. AIRCRAFT RETURNED TO NEWARK AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH RELAYS 16CG AND 24CG TO BE INOPERATIVE. REMOVED AND REP LACED RELAYS, OPERATIONALLY CHECKED GOOD AND RETURNED AIRCRAFT TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998072400471 19980724 00471 EU 1998 7 24 C2XA98BT042 1 19980615 A 3350 3011180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 97841 280 BTV - DURING 3A INSPECTION FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AND OPERATIO NALLY CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998072400472 19980724 00472 NM 1998 7 24 BJNA980604 1 19980628 A 2613 INSULATOR BOEING 737 737214 138446R NM APU MISLOCATED A BJNA K NONE N FALSE WARNING IN INSP/MAINT 1 WP 11 457TM 20156 ON GROUND LEFT WING BODY OVERHEAT ILLUMINATED. IN THE APU COMPARTMENT, THE OVERHEAT LOOP ELEMENT IS POSITIONED A FEW IN CHES ABOVE THE BLEED AIR SUPPLY DUCT. THIS ELEMENT IS HELD IN POSITION BY NUMEROUS CLAMPS WITH INSULATORS DURING TROUBL ESHOOTING, AN INSULATOR WAS FOUND TO BE POSITIONED AS TO WHERE THE ELEMENT WOULD INTERMITTENTLY GIVE A FALSE WARNING DUE TO THE TRANSFER OF HEAT FROM THE SUPPLY DUCT TO THE ELEMENT. THIS OVERHEAT PROBLEM WAS CORRECTED WHEN THE CLAMP INSULA TOR WAS REPOSITIONED. (M) 2 L 7 2 4F A16WE 1998072400473 19980724 00473 NM 1998 7 24 BJNA980602 1 19980626 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 20336 R-2 EMERGENCY EXIT INTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY HOLDER ON LIGHT UNIT PER BMM 33-51-01. (M) 2 L 7 2 4F A16WE 1998072400474 19980724 00474 NM 1998 7 24 BJNA980603 1 19980626 A 2613 DETECTOR BOEING 737 737214 138446R NM APU OUT OF POSITION A BJNA K NONE N FALSE WARNING CL CLIMB 1 WP 11 457TM 20156 NR 1 WING BODY OVERHEAT ILLUMINATED INTERMITTENTLY AFTER TAKEOFF AT BFF WITH BLEEDS OFF, APU ON TAKEOFF, REMAINED OFF AF TER BLEEDS RECONFIGURED. DISCOVERED OVERHEAT DETECTOR AGAINST APU BLEED SUPPLY DUCT, RELOCATED AND RAN APU AT MAX TEMP FOR 40 MIN, NO DISCREPANCIES NOTED IAW BMM 49-11-0. (M) 2 L 7 2 4F A16WE 1998072400475 19980724 00475 EA 1998 7 24 98ZZZM503 1 19980610 A 7110 COWL DHAV DHC6 DHC6300 EA LT ENGINE CRACKED A ASWA K NONE O OTHER IN INSP/MAINT 1 WP 07 72GC 264 264 FOUND CRACKS IN LEFT LOWER COWLING SKIN NEAR EXHAUST OPENING. REPAIRED IAW S/B 6/322, INCORPORATED MODIFICATION NR 6/14 97. (M) 1 H 7 2 3T A9EA 1998072400476 19980724 00476 EA 1998 7 24 98ZZZM504 1 19980603 A 5414 C6W150025 SKIN DHAV DHC6 DHC6300 EA RT NACELLE GOUGED A ASWA K NONE O OTHER IN INSP/MAINT 1 WP 07 227SA 517 DURING SCHEDULED INSPECTION, FOUND ENGINE BLEED AIR DUCT CLAMP THREADED STUD HAD GOUGED A HOLE IN RT NACELLE INBOARD INN ER SKIN SECTION. MAINTENANCE REMOVED AND REPLACED SKIN SECTION WITH IDENTICAL PIECE. (M) 1 H 7 2 3T A9EA 1998072400478 19980724 00478 WP 1998 7 24 ASAA9880087 1 19980517 A 5240 BEARING DOUG DC9 DC983 3022083 WP SERVICE DOOR WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - ARRIVAL OF FLT 88, CREW REPORTED THE L2 DOOR WOULD NOT FULLY OPEN. REPLACED THE UPPER HINGE TORQUE TUBE BEARING A ND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400479 19980724 00479 WP 1998 7 24 ASAA9880086 1 19980517 A 5610 PIN DOUG DC9 DC982 3022082 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 955AS 48080 ANC - AFTER ARRIVAL OF FLIGHT 173, CREW REPORTED THE FLIGHT COMPARTMENT LT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WIND OW GUIDE PIN IN TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998072400480 19980724 00480 WP 1998 7 24 ASAA9880098 1 19980603 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 200-299 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 OAK - DURING C-CHECK, DENT WAS FOUND IN FUSELAGE SKIN AFT OF L1 DOOR ABOVE FLOOR LINE. SPLICED IN NEW SECTION OF SKIN F ROM STATION 200 TO 229 LONGERON 16L TO CUSP IAW ASA EA 5330-01319. (M) 2 L 7 2 4F A6WE 1998072400481 19980724 00481 WP 1998 7 24 ASAA9880099 1 19980603 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1338 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 951AS 49111 OAK - DURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN AT STATION 1338 LONGERON 6R. REMOVED DAMAGED AREA AND INSTALLED INTE RNAL FINGER DOUBLER AND FILLER IAW ASA EA 5330-01320. (M) 2 L 7 2 4F A6WE 1998072400482 19980724 00482 WP 1998 7 24 ASAA9880104 1 19980607 A 5610 PANEL DOUG DC9 DC983 3022083 WP COCKPIT MISALIGNED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 939AS 49657 ANC - AFTER ARRIVAL OF FLT 104, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN COMPLETELY. REPOS ITIONED THE WINDOW TRIM PANEL AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400483 19980724 00483 WP 1998 7 24 ASAA9880102 1 19980529 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 37-69 BIRD STRIKE A ASAA K NONE O OTHER AP APPROACH 1 NM 01 982AS 53473 SEA - DURING APPROACH OF FLT 537, CREW REPORTED STRIKING AN EAGLE ON THE FORWARD FUSELAGE AREA AT 3,000 FEET MSL. FOUND DAMAGE CONTAINED WITHIN THE UNPRESSURIZED AREA FROM FS 37 TO FS 69.55 FROM THE FRP TO Z-30. REMOVED DAMAGED STRUCTURES AND INSTALLED NEW STRUCTURES IAW ASA EA 5330-01322. (M) 2 L 7 2 4F RT A6WE 1998072400484 19980724 00484 WP 1998 7 24 ASAA980103 1 19980605 A 5240 BRACKET DOUG DC9 DC982 3022082 WP SERVICE DOOR LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 955AS 48080 LAX - AFTER GROUND SERVICING THE R1 DOOR WOULD NOT CLOSE. TIGHTENED LOOSE BOLTS FOR THE MIDDLE DOOR STOP BRACKET AND OP ERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998072400485 19980724 00485 WP 1998 7 24 ASAA9880105 1 19980613 A 5610 PIN DOUG DC9 DC983 3022083 WP RT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT RT SLIDING WINDOW WAS FOUND DIFFICULT TO OPEN. ADJUSTED THE WIND OW GUIDE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998072400486 19980724 00486 WP 1998 7 24 ASAA9880109 1 19980621 A 5610 WINDOW DOUG DC9 DC982 3022082 WP LT COCKPIT LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 SEA - AFTER ARRIVAL OF FLT 543, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. LUBRICATED THE WINDOW MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998072400487 19980724 00487 1998 7 24 RAIA980604 4 19980608 A 3442 6227337001 RT UNIT BAG JETSTM JETSTM3201 1500217 EU E/E COMPT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 424AM 9718 865 FLT 7067 - STL - WEATHER RADAR INDICATION IS INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED WEATHER RADAR RECEIVER TRA NSMITTER. (M) 2 L 7 2 4T RT A56EU 1998072400488 19980724 00488 EU 1998 7 24 RAIA980603 1 19980606 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO COMPT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 555HK 41072 FLT 7413 - STL - POD SMOKE WARNING ILLUMINATED DURING CLIMB, CREW PERFORMED EMERGENCY LANDING. MAINTENANCE INSPECTED PO D FOR SMOKE/FIRE DAMAGE, NO DAMAGE NOTED. REPLACED FAULTY POD SMOKE DETECTOR. (M) 2 L 7 2 4T RT A41NM 1998072400489 19980724 00489 1998 7 24 RAIA980602 4 19980603 A 3425 7003360944 AHRS AEROSP ATR42 ATR42300 8680920 EU E/E BAY FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 424TE 11033 124 FLT 7148 - STL - RIGHT ATTITUDE HEADING REFERENCE COMPUTER FAILED AND HEADING COMPARATOR WARNING ILLUMINATED. MAINTENAN CE REPLACED RIGHT ATTITUDE HEADING REFERENCE COMPUTER. (M) 2 H 7 2 4T RT A53EU 1998072400490 19980724 00490 EU 1998 7 24 RAIA980513 1 19980525 A 2422 559012AS INVERTER AEROSP ATR72 ATR72202 8680940 EU COCKPIT FAILED A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 722TE 220 STL - FLT 7170 - ELECTRIC SMELL/SMOKE IN COCKPIT, AIRCRAFT DIVERTED TO SPI. MAINTENANCE INSPECTED AND REPLACED NR 1 INV ERTER. (M) 2 H 7 2 4T RT A53EU 1998072400491 19980724 00491 EU 1998 7 24 RAIA980512 1 19980523 A 7933 83161030010 SENSOR AEROSP ATR42 ATR42300 8680920 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 425TE 12262 125 FLT 7140 - STL - RIGHT ENGINE OIL TEMPERATURE GAUGE READS BELOW ZERO. MAINTENANCE REPLACED RIGHT OIL TEMPERATURE SENSOR . (M) 2 H 7 2 4T RT A53EU 1998072400492 19980724 00492 EU 1998 7 24 RAIA980509 1 19980513 A 6120 1680640 MONOPOLE BAG JETSTM JETSTM3201 1500217 EU PROP GOV FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 340TE 2801 939 FLT 7394 - STL - CREW REPORTS LEFT SRL INOPERATIVE, SRL CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED LEFT PROP GOVERNOR MONOPOLE. (M) 2 L 7 2 4T RT A56EU 1998072400493 19980724 00493 EU 1998 7 24 RAIA980510 1 19980519 A 7712 31024766 TQ SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 435AM 2531 889 FLT 7468 - STL - LEFT ENGINE REACHED TEMPERATURE LIMIT BEFORE TARGET TORQUE WAS ACHIEVED. MAINTENANCE REPLACED LEFT ENG INE TORQUE SIGNAL CONDITIONER. (M) 2 L 7 2 4T RT A56EU 1998072400494 19980724 00494 EU 1998 7 24 RAIA980519 1 19980530 A 7930 1241012 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 568HK 4955 41086 FLT 7789 - JFK - LEFT ENGINE OIL PRESSURE FLUCTUATING IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE OIL PRESSURE TRANSDUC ER. (M) 2 L 7 2 4T RT A41NM 1998072400495 19980724 00495 1998 7 24 RAIA980518 4 19980530 A 3417 7000700967 ADC JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 568HK 6574 41086 FLT 7789 - JFK - CAPTAINS AIR DATA COMPUTER FAILED IN FLIGHT. MAINTENANCE REPLACED CAPTAINS AIR DATA COMPUTER. (M) 2 L 7 2 4T RT A41NM 1998072400496 19980724 00496 1998 7 24 RAIA980516 4 19980529 A 3422 7010133000 VALVE JETAIR JETSTM JETSTM4101 1500501 EU LT HORIZ STAB FAILED A RAIA C ABORTED TAKEOFF I J FLT. ATTITUDE INST. WARNING INDICATION TO TAKEOFF 1 CE 03 556HK 6518 41073 FLT 7219 - STL - AHRS HEADING COMPARATOR WARNING ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED LEFT FLUX VALVE. (M ) 2 L 7 2 4T RT A41NM 1998072400497 19980724 00497 EU 1998 7 24 RAIA980515 1 19980529 A 2121 M4941Z7A FAN BAG JETSTM JETSTM3201 1500217 EU CARGO BAY FAILED A RAIA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 436AM 12762 891 FLT 7090 - STL - ON TAXI FROM GATE CABIN FILLED WITH SMOKE. MAINTENANCE INSPECTED AND REPLACED RECIRCULATION FAN. (M) 2 L 7 2 4T RT A56EU 1998072400498 19980724 00498 1998 7 24 RAIA980520 4 19980531 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU E/E COMP FAILED A RAIA A UNSCHED LANDING I J FLT. ATTITUDE INST. WARNING INDICATION CR CRUISE 1 CE 03 564HK 4266 41081 FLT 7516 - STL - CAPTAINS AHRS FAILED IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED CAPTAINS AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1998072400499 19980724 00499 EU 1998 7 24 RAIA980522 1 19980531 A 2730 AS105 PULLEY BAG JETSTM JETSTM3201 1500217 EU BS 463 STICKING A RAIA O OTHER F FLT CONT AFFECTED CR CRUISE 1 CE 03 338TE 12480 932 FLT 7430 - STL - INFLIGHT ELEVATOR CONTROL STICKS. MAINTENANCE INSPECTED AND REPLACED ELEVATOR CONTROL CABLE PULLEY AT AIRFRAME STATION 463. (M) 2 L 7 2 4T RT A56EU 1998072400500 19980724 00500 WP 1998 7 24 RAIA980601 2 19980601 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311UA 01502 WP LEFT BIRD STRIKE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 CE 03 426AM 13014 874 66147 FLT 7486 - STL - ON TAKEOFF ROLL, LEFT ENGINE INCURRED FOREIGN OBJECT DAMAGE DUE TO BIRD STRIKE. MAINTENANCE REPLACED L EFT ENGINE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998072400501 19980724 00501 NM 1998 7 24 MASA98120 1 19980605 A 3350 MS1557081 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE, FOUND THE LEFT AFT FUSELAGE EMERGENCY LIGHT AND NR 1 AND NR 2 OVERHEAD CENTER AISLE LIGHTS N OT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED A BULB IN THE AFT FUSELAGE LAMP ASSEMBLY AND TWO BULBS IN THE OVERHEA D AISLE LIGHT ASSEMBLIES. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998072400502 19980724 00502 NM 1998 7 24 98ZZZM506 1 19980605 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE, FOUND THE LEFT AFT FUSELAGE EMERGENCY LIGHT AND NR 1 AND NR 2 OVERHEAD CENTER AISLE LIGHTS N OT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED A BULB IN THE AFT FUSELAGE LAMP ASSEMBLY AND TWO BULBS IN THE OVERHEA D AISLE LIGHT ASSEMBLIES. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998072400503 19980724 00503 NM 1998 7 24 MASA98121 1 19980605 A 3350 6138443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE, FOUND THE FORWARD TWO RED TRACK LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED T HE NR 3 EMERGENCY POWER SUPPLY AND THE FORWARD TRACK LGHT SECTION. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998072400504 19980724 00504 NM 1998 7 24 98ZZZM507 1 19980605 A 3350 6519020 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE, FOUND THE FORWARD TWO RED TRACK LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED T HE NR 3 EMERGENCY POWER SUPPLY AND THE FORWARD TRACK LGHT SECTION. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998072400505 19980724 00505 NM 1998 7 24 MASA98126 1 19980616 A 3350 PR4 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 DURING ROUTINE MAINTENANCE, PORTABLE EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. ( M) 2 H 7 2 4T RT A13NM 1998072400506 19980724 00506 WP 1998 7 24 AALA981115 1 19980602 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 408AA 49319 DFW - FLT 789 - AFTER GEAR WAS RAISED THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED. PERFORMED ABNORMAL PROCEDURES INDIC ATING ALL ELSE NORMAL. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE GEAR LOCK SENSOR, CYCLED GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998072400507 19980724 00507 EU 1998 7 24 AALA980924 1 19980508 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT 3R INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR P ATH LIGHT WIRING AT 3R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998072400508 19980724 00508 EU 1998 7 24 AALA980925 1 19980508 A 3397 WIRE AIRBUS 300 A300B4605R 3930308 EU CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT 3L INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR P ATH LIGHT WIRING AT 3R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998072400509 19980724 00509 NM 1998 7 24 AALA980825 1 19980423 A 3350 L204961 LIGHT DOUG MD11 MD11 3023602 NM CABIN BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1762B 48552 DFW - DURING OVERNIGHT MAINTENANCE, AFT EMERGENCY EXIT LIGHT FIXTURE BROKEN AT L2 DOOR. REPLACED AFT EMERGENCY EXIT LIG HT FIXTURE BROKEN AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998072400510 19980724 00510 NM 1998 7 24 AALA980993 1 19980514 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE CHECK, RIGHT EMEREGNCY FLOOR PATH LIGHTING STAYS ILLUMINATED FROM FIRST CLASS THROUGH BUSINESS CLASS. REPAIRED EMERGENCY EXIT FLOOR PATH JUMPER WIRE CONNECTION AT SEAT ROW 15. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 3 4F RT A22WE 1998072400511 19980724 00511 NM 1998 7 24 AALA980986 1 19980516 A 3350 A3060841 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1756 48491 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FORWARD OF L2 DOOR INOPERATIVE. REPLACED EMERGEN CY EXIT FLOOR PATH LIGHT STRIP AT L2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998072400512 19980724 00512 NM 1998 7 24 AALA981081 1 19980528 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1765B 48596 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR TRACK LIGHT BULB INOPERATIVE AT SEAT ROW 37G. REPLACED EMERGENCY EX IT FLOOR TRACT LIGHTING LAMP ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998072400513 19980724 00513 NM 1998 7 24 AALA981012 1 19980521 A 3350 CONNECTOR DOUG MD11 MD11 3023602 NM CABIN MISINSTALLED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1767A 48598 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE OR VERY DIM ON LEFT SIDE OF FIRST AND BUSINESS CLASS SECTION OF CABIN. REVERSED POLARITY ON EMERGENCY EXIT FLOOR PATH LIGHTING CONNECTOR IN FIRST CLASS SEC TION OF CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998072400514 19980724 00514 NM 1998 7 24 AALA981116 1 19980603 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359AA 24040 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 26 A AND B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT LEG 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400515 19980724 00515 NM 1998 7 24 AALA981142 1 19980606 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 362AA 24043 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 30HJ INOPERATIVE. RECONNECTED SEAT 30HJ CONNECTOR. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400516 19980724 00516 NM 1998 7 24 AALA981143 1 19980606 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 606AA 27057 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BY RIGHT AFT LAVATORY INOPERATIVE. REPLACED EMER GENCY EXIT FLOOR PATH LIGHT STRIP BY RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998072400517 19980724 00517 NM 1998 7 24 AALA981144 1 19980607 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366AA 25193 ORY - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTING AT SEAT 24B INOPERATIVE. REPAIRED EMERGENCY EXIT ESCAPE L IGHTING WIRE AT SEAT BASE CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400518 19980724 00518 NM 1998 7 24 AALA981139 1 19980605 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 7H INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR AT SEAT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998072400519 19980724 00519 WP 1998 7 24 AALA981135 1 19980606 A 3610 CLAMP DOUG DC9 DC982 3022082 WP TAIL COMP LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 495AA 49733 BOS - FLT 1527 - AFTER TAKEOFF BOS, TAIL COMPARTMENT HIGH LIGHT ILLUMINATED. TAIL COMPARTMENT HIGH LIGHT EXTINGUISHED A FTER PACK SWITCH TURNED OFF. RETURNED BOS AND LANDED WITHOUT INCIDENT. REMOVED LEFT HAND AUGMENTATION VALVE CLAMP, CLE ANED VALVE SURFACE. REINSTALLED LEFT AUGMENTATION VALVE CLAMP. RAN ENGINE AT LOW POWER CHECKED NORMAL. RAN ENGINE AT TAKEOFF POWER WITH NO LEAKS NOTED. ACCOMPLISHED LEAK CHECK PER MAINTENANCE MANUAL. SYSTEM GROUND CHECKED NORMAL OPERAT ION. (M) 2 L 7 2 4F A6WE 1998072400520 19980724 00520 WP 1998 7 24 AALA981016 2 19980520 A 7200 ENGINE DOUG DC9 DC982 3022082 WP LEFT FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 70524 49916 DFW - DURING TAKEOFF, CREW REPORTED STRONG BURNING RUBBER SMELL IN CABIN AND COCKPIT. AIRCRAFT AIR INTERRUPTED AND RETU RNED AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE AND ACCOMPLISHED PACK BURN OUT. GROUND RAN ENGINES AT TAKEOFF WITH NO LEAKS OR SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATIONS. (M) 2 L 7 2 4F A6WE 1998072400521 19980724 00521 WP 1998 7 24 AALA981022 1 19980524 A 3260 SENSOR DOUG DC9 DC983 3022083 WP MLG OUT OF ADJUST A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 567AM 53293 ORD - FLT 575 - DURING CLIMB-OUT AT FL 20,000 FT, GEAR DOOR WARNING LIGHT ILLUMINATED. CREW TURNED ENGINE DRIVEN HYDRAU LIC PUMPS TO HIGH AND LIGHT EXTINGUISHED. FLT CONTINUED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND RIGHT MAIN GEAR DOOR SENSOR OUT OF ADJUSTMENT. ADJUSTED RIGHT MAIN GEAR DOOR SENSOR. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A6WE 1998072400522 19980724 00522 WP 1998 7 24 AALA981023 1 19980526 A 3241 4062575 TRANSDUCER DOUG DC9 DC982 3022082 WP MLG LOOSE A AALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 215AA 49163 DFW - FLT 1203 - DURING TAKEOFF ROLL AT APPROX 100 KTS, THE WHEEL NOT TURNING LIGHT ILLUMINATED. TAKEOFF ABORTED AND LI GHT EXTINGUISHED. MAINTENANCE FOUND ANTI-SKID TRANSDUCER LOOSE. SECURED TRANSDUCERS AND AS A PRECAUTIONARY, REPLACED A NTI-SKID CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998072400523 19980724 00523 WP 1998 7 24 AALA981080 1 19980528 A 2120 AIR DISTRIBUTION DOUG DC9 DC982 3022082 WP CABIN ODOR A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 465A 49595 DFW - FLT 1684 - DURING TAKEOFF, CREW NOTICED SEWAGE SMELL FOLLOWED BY A BURNING SMELL. FLIGHT AIR INTERRUPTED AND RETU RNED DFW AND LANDED OVERWEIGHT WITHOUT INCIDENT. ACCOMPLISHED OVERWEIGHT INSPECTION WITH NO DAMAGE NOTED. PACKS INSPEC TED FOR POSSIBLE INGESTION WITH NO INGESTION NOTED. GROUND RAN ENGINES AT POWER UTILIZING BLEED AIR FOR PACK, UNABLE TO DUPLICATE ORDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998072400524 19980724 00524 EU 1998 7 24 PLGA980414A 1 19980414 A 2120 CONNECTOR SAAB SF340 SF340A 7850100 EU CABIN AIR MISWIRED A PLGA K NONE W INADEQUATE Q C CR CRUISE 1 NE 05 335BE 340A146 BOS - FLT 4316 - CREW REPORTED THAT WHEN THE LEFT CABIN AIR RECIRCULATION FAN WAS SELECTED OFF, THE RT CABIN RECIRCULATI ON FAN INDICATOR LIGHT WOULD ILLUMINATE AND VICE VERSA. MAINTENANCE FOUND LT AND RT CABIN RECIRCULATION FAN SPEED SENSO R WIRING HARNESSES REVERSED AT AIRFRAME RECEPTICALS. CONNECTORS WERE CORRECTLY INSTALLED AND SYSTEM TESTED GOOD. (X) 2 L 7 2 4T RT A52EU 1998072400525 19980724 00525 1998 7 24 PLGA980319A 4 19980319 A 3425 AHC8566361901 AHRS SAAB SF340 SF340A 7850100 EU LEFT MALFUNCTIONED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 335BE 576 340A146 LGA - FLT 4501 - AFTER TAKEOFF, THE LEFT AHRS FAILED. AIRCRAFT RETURNED TO LGA. MAINTENANCE REPLACED THE LEFT AHRS. S YSTEM TESTED GOOD. (X) 2 L 7 2 4T RT A52EU 1998072400526 19980724 00526 EU 1998 7 24 98ZZZX2413 1 19980323 A 2913 4018502 PUMP ABEX PMP05VC05402 SAAB SF340 340B 7860101 EU HYDRAULIC SYSTEM FAILED A NVEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 03 347SB 340B347 PIT - FLT 4918 - INTRANSIT LIGHT WOULD NOT EXTINGUISH. HYDRAULIC PUMP CIRCUIT BREAKERS TRIPPED WHEN PUMP WOULD NOT RUN. EMERGENCY GEAR EXTENSION PERFORMED. AIRCRAFT FERRY TO MNTC BASE. 2 L 7 2 4T RT A52EU 1998072400527 19980724 00527 CE 1998 7 24 PLGA980413A 1 19980413 A 3260 GE387 BULB CESSNA 340 340A 2076405 CE NLG FAILED A PLGA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 NE 05 339BE 340A044 BOS - FLT 4260 - WHEN LANDING GEAR WAS SELECTED DOWN FOR LANDING, THE CREW DID NOT RECEIVE A DOWN AND LOCKED INDICATION FOR THE NOSE GEAR. CREW REPLACED LANDING GEAR INDICATOR LIGHT BULBS FOR NOSE GEAR. SYSTEM TESTED GOOD. (X) 1 L 7 2 3O 3A25 1998072400528 19980724 00528 WP 1998 7 24 AALA980896 1 19980506 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7543A 53025 MSP - DURING OVERNIGHT CHECK, FORWARD HALF OF EMERGENCY EXIT FLOOR PATH TRACK LIGHTING INOPERATIVE. REPLACED SECTION OF FLAT WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998072400529 19980724 00529 NM 1998 7 24 98ZZZX2414 1 19980513 A 3350 S106 BATTERY BOEING 737 737222 1384473 NM CABIN DISCHARGED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 737AP 19956 AFT OVER AISLE EMERGENCY EXIT LIGHT INOPERATIVE. FOUND BATTERY VOLTAGE LOW. REMOVED AND REPLACED BATTERIES. OPERATION S CHECK OK IAW BOEING MM 33-51-81. (X) 2 L 7 2 4F A16WE 1998072400530 19980724 00530 NM 1998 7 24 98ZZZX2415 1 19980513 A 3350 58791 CONNECTOR BOEING 737 737222 1384473 NM CABIN FAILED A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 737AP 19956 AFT SECTION OF TRACK FLOOR EMERGENCY LIGHTING FROM OVERWING EXIT TO BACK INOPERATIVE. FOUND BAD PIN IN CONNECTOR AT AFT END OF TRACK LIGHTING. REPLACED PIN. OPERATIONS CHECK OK IAW BOEING MM, CHAPTER 33-51-01. 2 L 7 2 4F A16WE 1998072400531 19980724 00531 SO 1998 7 24 98ZZZX2416 1 19980503 A 3350 M8372375R1624N CONNECTOR EMB 145 EMB145 SO CABIN DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16944 145045 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. MAINTENANCE CLEANED TH E CANNON PLUG ON THE LIGHT CONTROLLER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1998072400532 19980724 00532 SO 1998 7 24 SIMA981011 1 19980411 A 3260 355022002 LGEU PARKER EMB 145 EMB145ER SO COCKPIT INOPERATIVE A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 600BK 1085 145044 CLE - FLT 9767 - PREVIOUS OCCURRENCE, 4-10-98. LANDING GEAR LEVER DISAGREE. FOLLOWED QRH PROCEDURES. RETURNED TO CLE PER MOC. PERFORMED TROUBLESHOOTING PROCEDURES DUE TO LANDING GEAR LEVER DISAGREE DISPLAY ON EICAS. INSTALLED SELECTOR LANDING SOLENOID VALVE AND LANDING PROXIMITY SWITCHES. REPLACED LANDING GEAR ELECTRONICAL UNIT. RETRACTION TEST GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT T00011AT 1998072400533 19980724 00533 NM 1998 7 24 ASAA9840061 1 19980421 A 5210 MECHANISM BOEING 737 737490 1384715 NM L1 DOOR LACK OF LUBE A ASAA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 01 788AS 28885 LAX - PRIOR TO FLT 103, THE L-1 DOOR WAS FOUND EXTREMELY HARD TO MOVE. LUBRICATED L-1 DOOR AND THE DOOR OPERATED NORMAL LY. (X) 2 L 7 2 4F RT A16WE 1998072400534 19980724 00534 NM 1998 7 24 98ZZZX2417 1 19980511 A 5510 BACB30NF419 BOLT BOEING 737 73749R 1384406 NM HORIZ STAB MISINSTALLED A L P9OA K NONE O OTHER IN INSP/MAINT 1 NM 01 460PR 28881 PER BOEING TELEX M-7200-98-01560, 5-5-98, PRO AIR ELECTED TO ACCOMPLISH A ONE-TIME INSP OF THE HORIZ STAB/ELEVATOR ATTAC H FITTINGS TO IDENTIFY ANY FASTENERS INSTALLED DURING MANUFACTURING THAT HAD INCORRECT GRIP LENGTH. AS A RESULT OF THIS INSP, ALL 20 FASTENERS ON SUBJECT ACFT WERE BACB30NF4-19, AND WERE NOT OF ACCEPTABLE GRIP LENGTH, IN ADDITION TO BEING OUT OF CONFIGURATION PER BOEING/PRR IPC 55-50-00-08. CORRECTIVE ACTION TAKEN TO REPLACE ALL FASTENERS WITH CORRECT P/N BACB30NF4-21 PER TELEX METER AND IPC55-50-00-08. NO LOOSE OR MISSING FASTENERS FOUND DURING ACCOMPLISHMENT OF TASK. CO MP P/N 69-56027-1, P/N 69-562073. 2 L 7 2 4F RT A16WE 1998072400535 19980724 00535 EA 1998 7 24 MASA98099 1 19980508 A 3350 GE1317 BULB BRUCE BM10006002 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37178 7178 WHILE PERFORMING ROUTINE MAINTENANCE, FOUND LT AFT EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED BULB. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A21EA 1998072400536 19980724 00536 WP 1998 7 24 TWAA9809005 1 19980607 A 7714 2CM9ABY7 GENERATOR DOUG DC9 DC983 3022083 WP LT ENGINE FAILED A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 9616G HV1027 53563 STL - FLT 659 - DURING CLIMB, LEFT ENGINE N1 INDICATOR WENT BLANK. REPLACED ENGINE DISPLAY UNIT, MFG PN 301EDP1-4 AND N 1 TACH GENERATOR, MFG PN 2CM9ABY7, OP-16 7-1-97 NEW. (X) 2 L 7 2 4F RT A6WE 1998072400537 19980724 00537 NM 1998 7 24 TWAA9809004 1 19980607 A 3350 LIGHT BOEING 757 757231 1384950 NM CABIN LOOSE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 705TW 28479 JFK - FLT 35 - LOG WRITE-UP - EXIT INDICATOR PULLED UP FROM FLOOR AT FORWARD MAIN CABIN AREA. SECURED TO FLOOR. OP-15 2-15-97 NEW. (X) 2 L 7 2 4F RT A2NM 1998072400538 19980724 00538 NM 1998 7 24 GAIA9860 1 19980610 A 2750 CONNECTOR BOEING 727 727223 1384074 NM TE FLAPS DIRTY A GAIA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 6821 19496 GEG/SEA - EN ROUTE DURING FLAP OPERATION, OUTBOARD FLAPS STUCK AT 2 DEGREES AND WOULD NOT MOVE. PROCEEDED TO SEA AND LA NDED WITHOUT FURTHER DIFFICULTY. CLEANED AND SECURED CONTROL VALVE CANNON PLUG. CYCLED FLAPS SEVERAL TIMES. FLAP SYST EM OPERATES NORMALLY. OPERATIONALLY CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998072400539 19980724 00539 WP 1998 7 24 ORJA98116 1 19980611 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 836RA 53046 EMERGENCY LIGHT OUT AT 15D. RECONNECT CANNON PLUG. OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998072400540 19980724 00540 WP 1998 7 24 ORJA98115 1 19980612 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 EMERGENCY LIGHT AT SEAT 7D INOPERATIVE. SECURED BAD CONNECTION. OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998072400541 19980724 00541 WP 1998 7 24 ORJA98114 1 19980614 A 3397 WIRE DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 755RA 49727 EMERGENCY LIGHTS AT 10W 20D INOPERATIVE. RE-INSTALLED WIRE INTO CONNECTOR. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1998072400542 19980724 00542 WP 1998 7 24 ORJA98110 1 19980612 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS ROWS 21, 22, 23, 24 INOPERATIVE. FOUND SHORTED WIRES ON 23, REPLACED WIRING, REPLACED LT AFT EXIT EMER GENCY BATTERY PACK. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1998072400543 19980724 00543 WP 1998 7 24 ORJA98109 1 19980613 A 3350 60030451 BATTERY DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY EXIT LIGHTS AT ROWS 11, 12, 13 - STAY ON. REPLACED BATTERY PACK FOR ROWS 11, 12, AND 13. OPS CHECK GOOD. (X ) 2 L 7 2 4F RT A6WE 1998072400544 19980724 00544 WP 1998 7 24 ORJA98113 1 19980501 A 3350 DC36L1065H29 CONNECTOR DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 SEAT 26D (AISLE SEAT) EMERGENCY LIGHT INOPERATIVE. REPAIRED CONNECTOR ON BOTTOM OF SEAT. (X) 2 L 7 2 4F RT A6WE 1998072400545 19980724 00545 WP 1998 7 24 ORJA98111 1 19980618 A 3220 5930194505 DEFLECTOR DOUG DC9 DC983 3022083 WP NLG LOOSE A ORJA K NONE N FALSE WARNING NR NOT REPORTED 1 WP 11 872RA 49793 LAS - NOSE GEAR LIGHT (RED) REMAINS ON WITH GEAR HANDLE UP. ENTERED DMI 13924. NOSE WHEEL SPRAY DEFLECTOR BOLT MISSING LT SIDE. SPRAY DEFECTOR REMOVED. NOSE GEAR OPS NORMALLY PER CDL32-20-01 AND MM 32-30-0. INSTALLED LT NLG SPRAY DEFLE CTOR AND SECURED HARDWARE. OK FOR SERVICE. THIS ACTION CLEARS DMI NR 13924. (X) 2 L 7 2 4F RT A6WE 1998072400546 19980724 00546 NM 1998 7 24 MASA98129 1 19980618 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING ROUTINE MAINTENANCE, FOUND NEARLY ALL EMERGENCY LIGHTS INOPERATIVE. REPLACED ALL SIX POWER SUPPLIES. OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998072400547 19980724 00547 NM 1998 7 24 MASA98127 1 19980527 A 3350 AML91A85 BULB AML51G60GY DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 DURING ROUTINE MAINTENANCE, FOUND THE FLIGHT ATTENDANT'S EMERGENCY LIGHT PUSH BUTTON GREEN LIGHT INOPERABLE. REPLACED T HE BULB IN THE SWITCH, OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998072400548 19980724 00548 NM 1998 7 24 MASA98128 1 19980618 A 3350 S48C15564A4EA BULB GRIMES 6519024 DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 DURING ROUTINE MAINTENANCE, FOUND FOURTH SECTION OF EMERGENCY ESCAPE PATH LIGHTING INOPERABLE. REPLACED BULB, OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998072400555 19980724 00555 NM 1998 7 24 EIAA980210 1 19980618 A 5412 56B9041227 BULKHEAD FRAME BOEING 747 747212B 1384886 NM NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 HKG - LOG PAGE: F08701 - DURING B-CHECK, NR 2 PYLON AFT MOUNT BULKHEAD OTBD WEBS (FWD AND AFT) WERE FOUND CRACKED. REP AIRED, REPLACED BULKHEAD WEB AND FRAMES PER SB 747-54-2065, RS R54-53-33775, AS APROVED ON ECRA 482-54-122-1. (X) 2 L 7 4 4F A20WE 1998072400556 19980724 00556 NM 1998 7 24 EIAA980209 1 19980618 A 5270 SWITCH BOEING 747 747132 1384882 NM CARGO DOOR OUT OF ADJUST A EIAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 09 481EV 19896 MNL - LOG PAGE: F66950 - AT FL 390, MAIN DECK SIDE, CARGO DOOR WARNING LIGHT ILLUMINATED. DIVERTED TO MNL. NOTE: LIG HT FLASHED MOMENTARILY DURING TURBULENCE. ADJUSTED MAIN CARGO DECK CARGO DOOR WARNING SWITCH PER MM 52-32-00. CHECKED WIRING FROM PLUG D4732 TO DOOR MODULE. OPERATIONALLY CHECKED GOOD IN COCKPIT AND MASTER CONTROL PANEL. (X) 2 L 7 4 4F A20WE 1998072400557 19980724 00557 NM 1998 7 24 EIAA980208 1 19980618 A 3231 65B109027 ROD BOEING 747 747SR46 NM LT MLG DOOR BROKEN A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 478EV 21033 LAX - LOG PAGE: F81751 - DURING FLIGHT AFTER GEAR RETRACTION, GEAR 'DOOR OPEN' LIGHT REMAINED ILLUMINATED WITH BOTH LT WING GEAR DOOR OPEN LIGHTS ALSO ILLUMINATED. RECYCLED GEAR, PROBLEM REMAINED. RETURNED TO LAX. REPLACED INBD DOOR LIN KAGE ROD LOWER ROD END AND ADJUSTED PER MM 32-12-00. DOOR OPS CHECKED, AND ALL INDICATIONS CHECKED GOOD. (X) 2 L 7 4 4F A20WE 1998072400558 19980724 00558 WP 1998 7 24 EIAA980207 1 19980617 A 3350 60030431 POWER SUPPLY DOUG DC9 DC915F 3022037 WP COCKPIT FAILED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 915F 47061 SYR - LOG PAGE: F66485 - COCKPIT OVERHEAD EMERGENCY LIGHT FAILED TO LIGHT DURING ROUTINE CHECK. REPLACED COCKPIT OVERH EAD EMERGENCY LIGHT BATTERY POWER SUPPLY MM 33-50-0. OPS CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1998072400559 19980724 00559 NM 1998 7 24 EIAA980206 1 19980616 A 2910 65B9017082 LINE BOEING 747 747273C 1384896 NM NR 3 HYD SYSTEM CHAFED A EIAA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 09 471EV 20651 NGU - LOG PAGE: F80966 - DURING CLIMB, LOST NR 3 HYDRAULIC SYSTEM, QUANTITY WENT TO ZERO, AND PRESSURE WAS FLUCTUATING DOWN TO 2,200 PSI. TURNED SYSTEM OFF. DIVERTED TO JFK. REPLACED HYDRAULIC LINE UNDER GAP COVER IN PYLON AND LEAK CHEC KED GOOD. MM 29-11-00. (X) 2 L 7 4 4F A20WE 1998072400560 19980724 00560 NM 1998 7 24 EIAA980205 1 19980614 A 7110 COWLING BOEING 747 747SR46 NM NR 2 NACELLE SEPARATED A EIAA J A DUMP FUEL UNSCHED LANDING D W INFLIGHT SEPARATION INADEQUATE Q C CL CLIMB 1 NM 09 478EV 21033 LAX - LOG PAGE: F81472 - AFTER TAKEOFF FROM LAX, ATC REPORTED DEBRIS FALLING FROM AIRCRAFT. ENGINE COWLING DEBRIS WAS FOUND ON RUNWAY 25R. CREW PERFORMED APPROPRIATE CHECKS, DUMPED FUEL AND RETURNED TO LAX. DURING DESCENT, NR 2 THROTTLE STUCK AT IDLE. NR 2 ENGINE SIDE COWLS WERE FOUND MISSING AFTER LANDING. (X) 2 L 7 4 4F A20WE 1998072400561 19980724 00561 NE 1998 7 24 EISA98135 2 19980612 A 7310 MOISTURE TRAP BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE CONTAMINATED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6826 19704 AIRBORNE RETURN TO SOUTHEND, ENGLAND (SNN), DUE TO FLUCTUATIONS ON ENGINE VALUES, NR 1 EPR, NR 1 N1, AND NR 1 N2, NR 1 F UEL FLOW. PILOT REPORT. CARRIED OUT T/S PER BOEING MM 72-00. INSPECTED INLET AND EXHAUST, REMOVED AND CLEANED PS4 MOI STURE TRAP. CREW CARRIED OUT ENGINE RUNS AT TAKEOFF POWER AND SUSTAINED CLIMB POWER. NO DEFECTS NOTED. (X) 2 L 7 3 4F 4 F A3WE E2EA 1998072400562 19980724 00562 NM 1998 7 24 98ZZZX2420 1 19980612 A 6120 78249050 PCU DHAV DHC8 DHC8103 1386005 NM NR 2 ENGINE INOPERATIAVE A ERAA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 03 881EA 18645 233 NR 2 ENGINE PROPELLER RPM FLUCTUATING BETWEEN 1032 AND 1088. UNABLE TO CONTROL PROP RPM. SHUT DOWN ENGINE AND MADE UNEV ENTFUL LANDING AT ANC. REPLACED NR 2 PCU, GROUND CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998072400563 19980724 00563 NM 1998 7 24 98ZZZX2421 1 19980619 A 3260 CONNECTOR DORNER DO32 DO328100 2996000 NM RT MLG DIRTY A EQGA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 19 340LS 3040 DFW/CUU - FLT 445 - AFTER TAKING POSITION ON THE ACTIVE RUNWAY AND PRIOR TO TAKEOFF ROLL, CREW RECEIVED A 'PROXI LOCK FA IL' AND 'PROXI HYD FAIL' EICAS MESSAGE AND CAUTION CHIME. CREW CANCELLED TAKEOFF CLEARANCE AND TAXIED OFF RUNWAY AND BA CK TO GATE. PROXI PROBLEM RECURRED TWICE EN ROUTE TO GATE. DURING T/S MAINT REMOVED CANNON PLUG ON RT GEAR DOWNLOCK AN D FOUND IT CONTAMINATED. MAIN CLEANED OUT DEBRIS AND RE-INSTALLED CANNON PLUG, PEROFMRED PLUG, PERFORMED OPS CHECKS AND TAXI CHECKS, ALL SATISFACTORY IAW MFG MM. ACFT RETURNED TO REVENUE SERVICE. 2 H 7 2 4T RT A45NM 1998072400564 19980724 00564 NM 1998 7 24 98ZZZX2422 1 19980613 A 3260 870004 PSEU DORNER DO32 DO328100 2996000 NM COCKPIT FAILED A EQGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 19 335PH 7530 20 31A 3013 DFW/TYS - FLT 376 - WHILE IN CLIMB-OUT FROM DFW EN ROUTE TO TYS, A CAUTION SOUNDED AND THE CAS SHOWED 'PROXI SYS' AMBER MESSAGE AND A 'PROXI HYD SINGLE' BLUE MESSAGE. ALSO, THE HYDRAULIC PAGE SHOWED A 'PROXI SYS FAIL' AND 'PROXI WOW FAIL' MESSAGE. CREW ATTEMPTED TO CLEAR MESSAGES BY CYCLING PROXI SYSTEM CIRCUIT BREAKERS, BUT WERE UNSUCCESSFUL. CREW NOTIFI ED MAINTENANCE AND FLIGHT CONTROL. MAINT ADVISED CREW TO RETURN TO DFW. ACFT LANDED WITHOUT INCIDENT. MAINT INSPECTED ACFT AND DETERMINED PSEU HAD FAILED. MAINT REPLACED PSEU AND PERFORMED OPS CHECKS IAW DORNIER MM 32-61-12. ALL CHECKS SATISFACTORY. ACFT RETURNED TO REVENUE SERVICE. 2 H 7 2 4T RT A45NM 1998072400565 19980724 00565 NM 1998 7 24 BJNA980601 1 19980616 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 456TM 20336 PASSENGER CABIN R1 DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT R1 DOOR PER BMM 33-51 -101, PAGE 201 THROUGH 203. (X) 2 L 7 2 4F A16WE 1998072400566 19980724 00566 EA 1998 7 24 98ZZZX2423 1 19980608 A 5512 C6TP10054 SKIN C6TP1001 DHAV DHC6 DHC6300 EA HORIZ STAB CRACKED A ASWA K NONE O OTHER IN INSP/MAINT 1 WP 07 331SA 39072 537 337 FOUND SPANWISE CRACK IN HORIZONTAL STABILIZER LEADING EDGE SKIN BETWEEN STA 98.00 AND STA 103.00. CRACK POSSIBLY CAUSED BY FATIGUE TO THIN SKIN CAUSED BY REPETITIVE REPLACEMENT AND ROLLING DOWN OF EDGES OR STABILIZER DEICER BOOT. 1 H 7 2 3T A9EA 1998072400567 19980724 00567 WP 1998 7 24 GTIA9800064 1 19980606 A 3350 1315 BULBS DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 DTW - AFT COMPARTMENT FLOOR EMERGENCY LIGHTS BURNED OUT. REMOVED AND REPLACED EMERGENCY LIGHT LAMPS AS REQUIRED IAW DC9 MM CHAPTER 33-50-0. (X) 2 L 7 2 4F A6WE 1998072400568 19980724 00568 WP 1998 7 24 GTIA9800065 1 19980607 A 3350 6003045 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 20310 47326 FOUND BROKEN WIRE AND BAD TERMINAL STRIP ON BATTERY POWER SUPPLY PACK AT 5-32. REMOVED AND REPLACED BATTERY POWER SUPPL Y PACK PER DC-9 MM 33-53-0 AND REPAIRED BROKEN WIRE PER DC-9 MM 20-50-1, OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A6WE 1998072400569 19980724 00569 NM 1998 7 24 GAIA9859 1 19980608 A 3350 1000677 LIGHT BOEING 727 727224 1384076 NM CABIN INOPERATIVE A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE 'A' CHECK, MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE LT FORWARD ENTRANCE DOOR INOPERATIVE. MA INTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSY IAW BOEING 727 MM 33-50. SYSTEM OPERATIONAL TEST CARRIED O UT SATISFACTORY. ACFT WAS THEN RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998072400570 19980724 00570 WP 1998 7 24 HALA9800141 1 19980604 A 2612 FIRE LOOP DOUG DC10 DC1010 3022110 WP NR 1 ENGINE MALFUNCTIONED A HALA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 WP 13 171AA 46906 SFO - FLT 15 - (LOG PAGE NR 4620938) - NR 1 ENGINE FIRE DETECTION LOOP 'A' LIGHT ON AFTER TAKEOFF. WENT OUT AFTER CLIMB POWER. REPLACED NR 1 ENGINE CONTROL BOX. (X) 2 L 7 3 4F A22WE 1998072400571 19980724 00571 CE 1998 7 24 98ZZZX2424 1 19980602 A 3040 503800703 CONVERTER BEECH 1900 1900D 1154162 CE FUSELAGE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 854CA 10065 02055 UE60 WINDSHIELD WIPERS INOPERABLE. COVERTER FAILURE. REPLACED WINDSHIELD WIPER CONVERTER AND FLEX DRIVES. 2 L 7 2 4T RT A24CE 1998072400572 19980724 00572 WP 1998 7 24 REXA98095 2 19980506 A 7250 31033101 TURBINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP RT ENGINE FIALED A REXA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 SO 25 318PX P63024 689 RIGHT ENGINE SHUT DOWN ON APPROACH TO MEM. CHANGED ENGINE DUE TO TURBINE FAILURE. (X) 2 L 7 2 4T 4 T RT A21EU E4WE 1998072400573 19980724 00573 NE 1998 7 24 REXA98096 2 19980521 A 7260 5078T36P01 SEAL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE FAILED A REXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 402BH 340A058 LEFT ENGINE LOST OIL PRESSURE. REMOVED AND REPLACED LEFT BB AXIS SEAL AND RUNNER. REF: OPERATOR CONTROL NR 98ZZZX2425 . (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1998072400575 19980724 00575 NE 1998 7 24 REXA98097 2 19980526 A 7320 78550034 HMU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LT ENGINE FAILED A REXA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 25 325PX UDAJ7280 340A051 GEE367231KU LEFT ENGINE TORQUE WENT TO ZERO AND ITT WENT TO 900 DEGREES AT 1,500 FEET. SHUT DOWN ENGINE. PERFORMED ENGINE INSPECTI ON, NO DISCREPANCIES NOTED. CHANGED HMU PER GE RECOMMENDATION FOR TROUBLESHOOTING PURPOSES. (X) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998072400576 19980724 00576 EU 1998 7 24 REXA98099 1 19980608 A 2910 1379305A77 LINE BAG JETSTM JETSTM3101 1500215 EU RT HYD PUMP LEAKING A REXA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 333PX 704 ON APPROACH TO MEM, AIRCRAFT LOST HYDRAULIC POWER. REMOVED AND REPLACED RIGHT PUMP PRESSURE LINE. (X) 2 L 7 2 4T RT A21EU 1998072400577 19980724 00577 EU 1998 7 24 RAIA980606 1 19980614 A 2120 137925FL419 DUCT BAG JETSTM JETSTM3201 1500217 EU LT ACM FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 343TE 11775 955 STL - FLT 7356 - AIRCRAFT WILL NOT PRESSURIZE ABOVE 1 PSID. MAINTENANCE INSPECTED AND REPLACED LEFT WATER SEPARATOR TO CABIN DUCT ASSEMBLY. (X) 2 L 7 2 4T RT A56EU 1998072400578 19980724 00578 NM 1998 7 24 MZZA98163 1 19980514 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 1148 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 817520 (SEQ NR 01148) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON AFT C ARGO COMPARTMENT BS 1148 FRAME SHEAR TIE BETWEEN S27L AND S27R. THE CORRODED SHEAR TIE WAS REMOVED AND REPAIRED PER B72 7 SRM 53-10-4. (X) 2 L 7 3 4F A3WE 1998072400579 19980724 00579 NM 1998 7 24 MZZA98164 1 19980512 A 5320 WEB BOEING 727 727227 1384078 NM BS 1223 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TN - HNRC: 817401 (SEQ NR 01065) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON AFT AIRSTAIR RT TORQUE BOX UPPER WEB AT BS 1223. INSTALLED REINFORCEMENT STIFFENER ANGLE AT THE AFT AIRSTAIR RT TORQUE BOX WEB OIL CANNING AREA PER B727 SRM 51-40-2. (X) 2 L 7 3 4F A3WE 1998072400580 19980724 00580 NM 1998 7 24 MZZA98165 1 19980513 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 480-510 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 816457 (SEQ NR 01073) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FORW ARD CARGO COMPARTMENT STR 28R BETWEEN BS 486 AND BS 492. THE CORRODED STR 28R FROM BS 480 TO BS 510 WAS TRIMMED OUT AN D REPAIRED PER B727 SRM 53-10-03 FIGURE 1. (X) 2 L 7 3 4F A3WE 1998072400581 19980724 00581 NM 1998 7 24 MZZA98166 1 19980513 A 5330 SKIN BOEING 727 727227 1384078 NM BS 490 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 816459 (SEQ NR 01075) - DURING 1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FORWA RD CARGO COMPARTMENT FUSELAGE SKIN INNER SURFACE AT S28R BETWEEN BS 484 AND BS 500. THE CORRODED FUSELAGE SKIN 1 INCH B Y 16 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3 FIGURE 3A. (X) 2 L 7 3 4F A3WE 1998072400582 19980724 00582 NM 1998 7 24 MZZA98167 1 19980512 A 5730 SKIN BOEING 727 727227 1384078 NM RT WING CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 817158 (SEQ NR 01069) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON WING CENTER SECTION LOWER SKIN LOWER SURFACE AT RBL 21 BETWEEN S4C AND S5C. THE CORRODED SKIN WAS CLEANED UP AND REPAIRED PE R B727 SRM 57-30-3 FIGURE 8. (X) 2 L 7 3 4F A3WE 1998072400583 19980724 00583 NM 1998 7 24 MZZA98168 1 19980519 A 5753 SKIN BOEING 727 727227 1384078 NM RT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 816631 (SEQ NR 06078) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON R T WING T/E INBOARD FORE FLAP LOWER SKIN AT WBL 72. THE DAMAGED SKIN 2 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIR ED PER B727 SRM 51-40-6. (X) 2 L 7 3 4F A3WE 1998072400584 19980724 00584 NM 1998 7 24 MZZA98169 1 19980518 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 400 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 840800 (SEQ NR 02430) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON PASS ENGER CABIN FLOORBEAM UPPER CHORD AT BS 400 RBBL 36. THE CORRODED FLOORBEAM UPPER CHORD FORWARD FLANGE 1 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-8 FIGURE 8. (X) 2 L 7 3 4F A3WE 1998072400585 19980724 00585 NM 1998 7 24 MZZA98170 1 19980520 A 5753 SKIN BOEING 727 727227 1384078 NM RT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 816635 (SEQ NR 06084) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMIANTION WAS FOUND ON RT WING T/E OUTBOARD AFT FLAP T/E LOWER SKIN AT WBL 398. THE DAMAGED SKIN 2 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (X) 2 L 7 3 4F A3WE 1998072400586 19980724 00586 NM 1998 7 24 MZZA98171 1 19980514 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 970 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 817517 (SEQ NR 01129) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 970 FRAME SHEAR TIE AT S27R. THE CORRODED SHEAR TIE WAS REMOVED AND REPAIRED PER B727 SRM 53-10-4. (X) 2 L 7 3 4F A3WE 1998072400587 19980724 00587 NM 1998 7 24 MZZA98172 1 19980514 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 817518 (SEQ NR 01145) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME SHEAR TIE BETWEEN S28L AND S29R. THE CORRODED SHEAR TIE WAS REMOVED AND REPAIRED PER B7 27 SRM 53-10-4. (X) 2 L 7 3 4F A3WE 1998072400588 19980724 00588 NM 1998 7 24 MZZA98173 1 19980515 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1158 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 817507 (SEQ NR 01158) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STR 30 AT BS 1152. THE CORRODED STR 30 FROM BS 1150 TO BS 1166 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. (X) 2 L 7 3 4F A3WE 1998072400589 19980724 00589 NM 1998 7 24 MZZA98174 1 19980514 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1148 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 817519 (SEQ NR 01147) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1148 FRAME FORWARD FLANGE (OUTBOARD CHORD FLANGE) AT S30. THE CORRODED FRAME OUTBOARD CHORD FLANGE 1 INCH BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-1 FIGURE 1. (X) 2 L 7 3 4F A3WE 1998072400590 19980724 00590 NM 1998 7 24 MZZA98175 1 19980514 A 5313 655612910 STRINGER BOEING 727 727227 1384078 NM BS 950/976 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 89427 21365 TNN - HNRC: 817516 (SEQ NR 01127) - DURING '1/2D' CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FUSE LAGE STR 27R OUTBOARD CHORD AT BS 950E PLUS 8.75 AND BS 976.75. THE CORRODED FUSELAGE STR 27R OUTBOARD CHORD WAS CLEANE D UP AND REPAIRED PER EC/RA NR 5310-03733 DATED 5-28-98. (X) 2 L 7 3 4F A3WE 1998072400591 19980724 00591 NM 1998 7 24 K3HA980091 1 19980714 A 3230 65195197 FITTING BOEING 727 727225 1384077 NM LT MLG BINDING A K3HA O OTHER J WARNING INDICATION LD LANDING 1 EA 25 356PA 1193 20626 LEFT GEAR STAYED RED WHEN GEAR EXTENDED. UPON CYCLING GEAR, GEAR EXTENDED NORMAL. REMOVED AND REPLACED LEFT HAND MAIN LANDING GEAR OPERATED SEQUENCE VALVE, DUE TO SUSPECTED FAULT PER MM 32-32-21, NO HELP. FOUND UNIVERSAL FITTING AT LEFT HAND MAIN LANDING GEAR SIDE STRUT FAILED. REMOVED AND REPLACED BOTH UNIVERSAL FITTING AND LOWER SEGMENT (SIDE STRUT) AS SEMBLY PER MM 32-11-41. PERFORMED MAIN LANDING GEAR EXTENSION AND RETRACTED TEST PER MM 32-32-0. CYCLED MAIN LANDING G EAR AND NOSE LANDING GEAR 20 TIMES, SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 1998072400592 19980724 00592 NM 1998 7 24 CALA9801272 1 19980720 A 5753 RIB BOEING 727 727227 1384078 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 2 INCH CRACK IN RT WING INBOARD FLAP OUTBOARD CABLE ATTACH RIB (MIDFLAP). THE MIDFLAP WAS REMOVED AN D REPLACED IAW WORK CARD 07-5750-1-4703. 2 L 7 3 4F A3WE 1998072400593 19980724 00593 NM 1998 7 24 CALA9801273 1 19980720 A 5753 SKIN BOEING 727 727227 1384078 NM LT TE FOREFLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND LT I/B FOREFLAP UPPER SKIN INBOARD END DELAMINATED. THE FOREFLAP WAS REMOVED, REPAIRED AND REINSTALLED IAW WORK CARD 07-5750-1-2801. 2 L 7 3 4F A3WE 1998072400594 19980724 00594 NM 1998 7 24 CALA9801274 1 19980720 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 500 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND SHEAR TIE CORRODED AT STA 500, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A SHEAR TIE REPAIR WAS FAB RICATED AND INSTALLED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1998072400595 19980724 00595 NM 1998 7 24 CALA9801275 1 19980720 A 5753 SKIN BOEING 727 727227 1384078 NM RT TE AFT FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND RT I/B AFT FLAP DELAMINATED AT 15 INCHES O/B OF I/B END AT UPPER SURFACE. THE AFT FLAP WAS REMOVED, RE PAIRED AND REINSTALLED IAW WORK CARD 07-5750-1-2802. 2 L 7 3 4F A3WE 1998072400596 19980724 00596 NM 1998 7 24 CALA9801276 1 19980720 A 5530 STRINGER BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER NR 7 RIB LT NR 9 STRINGER. THE CRACKED AREA WAS REMOVED IAW SR M 55-30-2. A STRINGER SECTION WAS FABRICATED AND INSTALLED IAW SRM 55-30-4. 2 L 7 3 4F A3WE 1998072400597 19980724 00597 NM 1998 7 24 CALA9801277 1 19980720 A 5530 STRINGER BOEING 727 727227 1384078 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN STRINGERS 6L, 8L, AND 9L AT VERTICAL STABILIZER NR 9 RIB. THE CRACKED AREAS WERE C UT OUT IAW SRM 55-30-04. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 55-30-04 AND 51-10-2. 2 L 7 3 4F A3WE 1998072400598 19980724 00598 NM 1998 7 24 CALA9801278 1 19980720 A 5754 RIB BOEING 727 727227 1384078 NM NR 4 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A .375 INCH CRACK AT O/B RIB WHERE LT WING NR 4 SLAT ACTUATOR FORWARD ROD END ATTACHES INSIDE SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998072400599 19980724 00599 WP 1998 7 24 CALA9801279 1 19980720 A 5210 DOOR BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND A .375 INCH CRACK IN MAIN CABIN DOOR NR 1 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1998072400600 19980724 00600 NM 1998 7 24 CALA9801280 1 19980720 A 5530 ANGLE BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .5 INCH CRACK IN FRAME ATTACH ANGLE INSIDE LT SIDE OF VERTICAL STABILIZER AT STRINGER 5L. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-4. 2 L 7 3 4F A3WE 1998072400601 19980724 00601 NM 1998 7 24 CALA9801281 1 19980720 A 5330 SKIN BOEING 727 727224 1384076 NM L1 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 2.75 INCH CRACK IN FUSELAGE SKIN AT L-1 DOOR LOWER HINGE CUTOUT. THE CRACKED AREA WAS CUT OUT, A REP AIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-20-4. 2 L 7 3 4F A3WE 1998072400602 19980724 00602 WP 1998 7 24 CALA9801282 1 19980720 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP BS 756-680 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND FLOOR PANEL DELAMINATED AT STA 756 TO 680. A NEW FLOOR PANEL WAS FABRICATED AND INSTALLED IAW SRM 53-0 5 AND 51-10-3. 2 L 7 2 4F A6WE 1998072400603 19980724 00603 WP 1998 7 24 CALA9801283 1 19980720 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A 1 INCH CRACK COMING FROM RIVET HOLE IN FORWARD CARGO DOOR AT STA 425. THE CRACK WAS STOP DRILLED, A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 52-03, 52-31-0 AND 51-70-2. 2 L 7 2 4F A6WE 1998072400604 19980724 00604 NM 1998 7 24 CALA9801284 1 19980717 A 5330 BULKHEAD WEB BOEING 727 727227 1384078 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN PRESSURE WEB SKIN AT STA 1183 BULKHEAD, RT SIDE, WL 188. THE CRACKED AREA WAS CUT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW EA 553A0022. 2 L 7 3 4F A3WE 1998072400605 19980724 00605 NM 1998 7 24 CALA9801285 1 19980717 A 5330 SKIN BOEING 727 727227 1384078 NM BS 680 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 680, STRINGER 27R TO 28R. THE CORRODED AREA WAS CUT OUT, DOUBLER AND FIL LER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, 51-10-2 AND 51-30-3. 2 L 7 3 4F A3WE 1998072400606 19980724 00606 NM 1998 7 24 CALA9801286 1 19980717 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND FUSELAGE SKIN AND STRINGER CORRODED AT STA 720, STRINGER 28L. THE CORRODED AREA OF SKIN AND STRINGER W ERE CUT OUT IAW SRM 53-30-3 AND 53-10-3. SKIN AND STRINGER SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-30. 2 L 7 3 4F A3WE 1998072400607 19980724 00607 NM 1998 7 24 CALA9801287 1 19980717 A 5330 SKIN BOEING 727 727227 1384078 NM BS 500 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 500 STRINGER 28R. THE CRACKED AREA WAS CUT OUT, STRINGER SPLI CE AND SKIN DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1998072400608 19980724 00608 NM 1998 7 24 CALA9801288 1 19980712 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT FS 1110, RBL 30. THE CORRODED AREA WAS CUT OUT, REPAIR PARTS WERE FABRICA TED AND INSTALLED IAW SRM 53-10-8, PAGE 18 AND 19. 2 L 7 3 4F A3WE 1998072400609 19980724 00609 NM 1998 7 24 CALA9801289 1 19980712 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND FORWARD ENTRANCE WAY FLOORBEAM CORRODED AT STA 344, LBL 29 TO 60. THE CORRODED AREA WAS CUT OUT, A T-A NGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998072400610 19980724 00610 NM 1998 7 24 CALA9801290 1 19980717 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 640 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND FLOOR SUPPORT CORRODED IN FORWARD CARGO COMPARTMENT AT STA 640, STRINGER 27L. THE CORRODED AREA WAS CU T OUT, REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 3 AND 51-10-2. 2 L 7 3 4F A3WE 1998072400611 19980724 00611 SO 1998 7 24 COMA9810161 1 19980719 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 266CA 14200 250 120258 EMERGENCY LIGHTS ROW 1 AND 2 ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998072400612 19980724 00612 EA 1998 7 24 COMA9860183 1 19980720 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 EA RT MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 952CA 7092 GEAR DISAGREE WARNING WHEN LANDING GEAR SELECTED UP. TIGHTENED LOOSE UPLOCK PROXIMITY SENSOR TARGET AT RIGHT HAND MLG. 2 L 7 2 4F RT A21EA 1998072400613 19980724 00613 EA 1998 7 24 COMA9860184 1 19980719 A 3260 172825 TARGET CNDAIR CL600 CL6002B19 EA MLG LOOSE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 954CA 7100 RIGHT HAND MLG DISAGREE WARNING, WHEN GEAR SELECTED UP. TIGHTENED LOOSE PROXIMITY TARGET ON RIGHT HAND MLG UPLOCK. 2 L 7 2 4F RT A21EA 1998072400614 19980724 00614 WP 1998 7 24 UPS98827175 1 19980708 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 76.25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, RT WING L/E LOWER SKIN AT WS XFS 76.25 HAS CORROSION BLEND OUT OF LIMITS. REPAIRED IAW DHC SK 708-74 6. 2 L 7 4 4F RT 4A25 1998072400615 19980724 00615 EU 1998 7 24 QXEA9800906 1 19980531 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 24 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CRACK EXTENDING FROM FRAME CLIP REPAIR TO ANOTHER CRACK EXTENDING FROM RIVET BACKTAIL LOCATED AFT SIDE OF FRAME 24-2 STR INGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1998072400616 19980724 00616 EU 1998 7 24 QXEA9800907 1 19980604 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 TWO CRACKS IN CLIP IN FRAME 20075 AT STRINGER 39. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 5 FIGURE 3 AND FOKKER SRM 51-3 1-01. 2 L 7 2 4F RT A20EU 1998072400617 19980724 00617 EU 1998 7 24 QXEA9800908 1 19980525 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PROTRUDING DENT ON LEFTHAND LOWER SKIN OF EXTERIOR FUSELAGE, 7 AFT OF FRAME 17065 AND 1 OUTBOARD OF STRINGER 1. REPAIRE D IAW FOKKER SRM 53-02-02, FIGURE 1. 2 L 7 2 4F RT A20EU 1998072400618 19980724 00618 EU 1998 7 24 QXEA9800909 1 19980609 A 5320 BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CHAFE DAMAGE ON APU VERTICAL BEAM 425R AT UPPER STIFFENER JUST AFT OF FRAME 17565 ATTACH POINT. REPAIRED IAW HORIZON AI R EA 4-53-454. 2 L 7 2 4F RT A20EU 1998072400619 19980724 00619 EU 1998 7 24 QXEA9800910 1 19980604 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 18075 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CHAFE ON FRAME 18075 FROM WIRE BUNDLE JUST ABOVE STRINGER 12. REPAIRED IAW HORIZON AIR EA 4-53-457. 2 L 7 2 4F RT A20EU 1998072400620 19980724 00620 EU 1998 7 24 QXEA9800911 1 19980527 A 5755 SKIN FOKKER F28 F28MK4000 4990810 EU LT SPEEDBRAKE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 INSIDE SKIN JOINT OF LEFTHAND SPEED BRAKE CENTER UPPER SECTION HAS SEVERAL FASTENERS WORKING LOOSE. THERE APPEARS TO BE GRINDER MARKS ON SKIN. REPAIRED IAW HORIZON AIR EA 4-53-451. 2 L 7 2 4F RT A20EU 1998072400621 19980724 00621 EU 1998 7 24 QXEA9800912 1 19980531 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 24 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CRACK IN FRAME AT RADIUS AROUND STRINGER 41 FRAME 24-2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 8, FIGURE 6, FOKKER SRM 51-30-02, SRM 51-31-01 AND SRM 53-10-05. 2 L 7 2 4F RT A20EU 1998072400622 19980724 00622 EU 1998 7 24 QXEA9800913 1 19980614 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERT STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 TOP EDGE RIGHTHAND SIDE OF VERTICAL STABILIZER SKIN HAS CHAFE DAMAGE FROM HORIZONTAL STABILIZER RUBBING AGAINST IT. REP AIRED IAW HORIZON AIR EA 4-55-72. 2 L 7 2 4F RT A20EU 1998072400623 19980724 00623 EU 1998 7 24 QXEA9800914 1 19980528 A 5551 FITTING FOKKER F28 F28MK4000 4990810 EU HORIZ STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 BOTTOM RIGHTHAND INBOARD MOUNT LUG FACE FOR HORIZONTAL STABILIZER JUNCTION FITTING HAS HEAVY SCARING AND PITTING. REPAI RED IAW HORIZON AIR EA 4-55-71. 2 L 7 2 4F RT A20EU 1998072400624 19980724 00624 EU 1998 7 24 QXEA9800915 1 19980605 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERT STAB DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 VERTICAL STABILIZER PANEL 56G HAS 2 SCREW HOLES GOUGED AND REAMED OUT. REPAIRED IAW HORIZON AIR EA 4-55-66. 2 L 7 2 4F RT A20EU 1998072400625 19980724 00625 EU 1998 7 24 QXEA9800916 1 19980515 A 5542 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 DELAMINATION OF LEFTHAND RUDDER SKIN AT STATION 21.6 TO 30.6. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1998072400626 19980724 00626 EU 1998 7 24 QXEA9800917 1 19980623 A 5730 FUEL PANEL FOKKER F28 F28MK4000 4990810 EU RT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 RIGHTHAND WING FUEL PANEL 74D HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON EA'S 4-57-131 AND 4-57-13 6. 2 L 7 2 4F RT A20EU 1998072400627 19980724 00627 EU 1998 7 24 QXEA9800918 1 19980623 A 5730 FUEL PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FUEL PANEL 74C HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA'S 4-57-131, 4-57-131A AND 4-57-13 6. 2 L 7 2 4F RT A20EU 1998072400628 19980724 00628 EU 1998 7 24 QXEA9800919 1 19980623 A 5730 FUEL PANEL FOKKER F28 F28MK4000 4990810 EU WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FUEL PANEL 74B HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA'S 4-57-131, 4-57-131A AND 4-57-13 6. 2 L 7 2 4F RT A20EU 1998072400629 19980724 00629 EU 1998 7 24 QXEA9800920 1 19980619 A 5730 FUEL PANEL FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 INBOARD FASTENER HOLE ON MATING FLANGE FOR FUEL PANEL 74C HAS CRACK. REPAIRED IAW HORIZON AIR EA 4-57-127. 2 L 7 2 4F RT A20EU 1998072400630 19980724 00630 EU 1998 7 24 QXEA9800921 1 19980622 A 5730 FUEL PANEL FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 CRACK LOCATED AT INBOARD SIDE OF MATING FLANGE FOR FUEL PANEL 72A. REPAIRED IAW HORIZON AIR EA 4-57-125. 2 L 7 2 4F RT A20EU 1998072400631 19980724 00631 EU 1998 7 24 QXEA9800922 1 19980619 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PANEL REBATE 74C HAS 4 CRACKS ON INBOARD AND OUTBOARD SIDES, 3 FRETTING AND ONE BORE HOLE. REPAIRED IAW HORIZON EA 4-57 -127. 2 L 7 2 4F RT A20EU 1998072400632 19980724 00632 EU 1998 7 24 QXEA9800923 1 19980622 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 PANEL REBATE 72A HAS ON FRETTING CRACK, INBOARD SIDE. REPAIRED IAW HORIZON AIR EA 4-57-125. 2 L 7 2 4F RT A20EU 1998072400633 19980724 00633 EU 1998 7 24 QXEA9800924 1 19980622 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 FUEL PANEL REBATE AREA HAS ON CRACK NEXT TO A SCREW HOLE. REPAIRED IAW HORIZON AIR EA 4-57-135. 2 L 7 2 4F RT A20EU 1998072400634 19980724 00634 EU 1998 7 24 QXEA9800925 1 19980603 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 DEEP SCRATCH ON UPPER SIDE OF WING LOWER SKIN, JUST AFT OF LEFTHAND WING REAR SPAR. REPAIRED IAW HORIZON AIR EA 4-57-12 6. 2 L 7 2 4F RT A20EU 1998072400635 19980724 00635 NM 1998 7 24 SCNA98071 1 19980718 A 2750 TORQUE TUBE BOEING 727 727225 1384077 NM RT TE FLAP DISCONNECTED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 282SC 22558 AFTER DEPARTURE, THE RIGHT OUTBOARD FLAP EXTENDED TO APPROXIMATELY 35 DEGREES. RETURNED TO LTO. FOUND THE OUTBOARD FLA P TORQUE TUBE DISCONNECTED AT THE RIGHT WHEEL WELL AREA. RECONNECTED THE TORQUE TUBE AND OPERATED FLAPS WITH NO DEFECTS NOTED IN ACCORDANCE WITH B727 MAINTENANCE MANUAL 275111. 2 L 7 3 4F A3WE 1998072400636 19980724 00636 NM 1998 7 24 SCNA98072 1 19980712 A 3610 39271631 MODULATING VALVE BOEING 727 7272J4 1384006 NM NR 1 ENGINE FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 285SC 5099 21676 THE NUMBER ONE ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED FOLLOWING COM PROCEDURES AND AIRCRAFT DIVERT ED TO ATL. THE NUMBER ONE ENGINE PYLON INSPECTED FOR LEAKS WITH NONE FOUND. BLEED VALVE AT 13TH STAGE FOUND CLOSED. R EMOVED AND REPLACED NUMBER ONE ENGINE 13TH STAGE MODULATING VALVE, OPERATIONAL AND LEAK CHECK GOOD IN ACCORDANCE WITH MA INTENANCE MANUAL 361242. 2 L 7 3 4F RT A3WE 1998072400637 19980724 00637 WP 1998 7 24 SCNA98073 1 19980714 A 3260 PROXIMITY SENSOR DOUG DC10 DC1015 3022118 WP NLG INOPERATIVE A SCNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 153SY 48276 DURING CLIMB, THE RED NOSE GEAR LIGHT CAME ON. PERFORMED COM CHECKLIST WITH ALL GEAR DOWN INDICATIONS NORMAL. DIVERTED TO MIA. FOUND TARGET ON DOWNLOCK PROXIMITY SENSOR OUT OF ADJUSTMENT. ADJUSTED DOWN LOCK SENSORS IN ACCORDANCE WITH MA INTENANCE MANUAL 326103, FUNCTIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1998072400638 19980724 00638 NE 1998 7 24 SWIA971213 2 19980706 A 7310 FUEL FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 299SW 120329 LEFT FUEL FILTER LIGHT ILLUMINATED IN FLIGHT. DIVERTED FROM FAT TO ACV. REPLACED LEFT ENGINE FUEL FILTER WITH SERVICEA BLE UNIT. OPS CHECKS GOOD WITH NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998072400640 19980724 00640 SO 1998 7 24 SWIA971215 1 19980709 A 3610 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT MALFUNCTIONED A SWIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 209SW 120269 AFTER DEPARTURE WITH APU ASSIST TAKEOFF WHEN SWITCHING TO ENGINE BLEED, DUCT LEAK ILLUMINATED. LIGHT EXTINGUISHED AT 3 MINUTES. RETURNED TO SLC. REMOVED AND REPLACED LEFT SIDE PRESSURE VALVE WITH SERVICEABLE UNIT, IAW MM 30-10-06. OPS C HECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998072400642 19980724 00642 SO 1998 7 24 SWIA971217 1 19980709 A 2751 FCU EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS TRIPPED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 1117H 120117 CONTROL FAULT WARNING CAME ON IN FLIGHT. TRIED RESET, NOT SUCCESSFUL. RETURNED TO PDX. RERACKED FCU AND CONTROL FAULT WENT AWAY, OPS CHECKS NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1998072400643 19980724 00643 EA 1998 7 24 SWIA971218 1 19980709 A 5350 RADOME CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE FWD FUSELAGE BIRD STRIKE A SWIA A UNSCHED LANDING C F.O.D. CL CLIMB 1 NM 07 409SW 7056 HIT A BIRD ON CLIMBOUT AND RETURNED FOR LANDING. PERFORMED BIRD STRIKE INSPECTION, FOUND NOSE RADOME RIGHT LOWER CORNER DAMAGED. REPLACED RADOME. 2 L 7 2 4F 4 F RT A21EA E15NE 1998072400644 19980724 00644 SO 1998 7 24 SWIA971219 1 19980709 A 7714 INDICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 197SW 120186 LEFT ENGINE NL ON TAKEOFF SHOWED 110 PERCENT TO 115 PERCENT. RETURNED TO SLC. REPLACED LEFT HAND NL/NH INDICATOR. RAN ENGINE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998072400645 19980724 00645 NM 1998 7 24 CKSA98503 1 19980712 A 3397 WIRE BOEING 747 747146 NM CABIN DAMAGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 703CK 19727 RT AFT EMERGENCY EXIT AND FLOOR LIGHTING IS INOP. REPAIRED E PATH LIGHTING AT ZONE D AND E RT SIDE IAW BAC WDM STANDARD PRACTICE. SYSTEM OPS CHECKS NORMAL IAW B747 MM CHAPTER 33 AND 25. 2 L 7 4 4F A20WE 1998072400646 19980724 00646 WP 1998 7 24 TC8A98042 1 19980718 A 2910 FITTING DOUG DC8 DC8F54 3021926 WP SPOILER CRACKED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 802CK 45679 ON TAXI UPON FLIGHT CONTROL CHECK, SPOILER PUMP PRESSURE INDICATION WENT TO ZERO. FOUND FITTING AT SPOILER SUPPLY LINE CRACKED. REPLACED FITTING IAW MM 27-62-0, OPS CHECK NORMAL. 2 L 7 4 4F 4A25 1998072400672 19980724 00672 CE 1998 7 24 98ZZZX2451 1 19980617 A 3233 08421042 BELLCRANK CESSNA 401 401 207590C CE NLG ACTUATOR FAILED A A HBCA K NONE O OTHER TX TAXI/GRND HDL 1 SW 11 2GE 6623 4010088 WHILE TAXIING IN, THE PILOT HEARD A 'POPPING' NOISE IN THE NOSE LANDING GEAR AREA. A CLOSE INSPECTION REVEALED A BROKEN ADJUSTING BELLCRANK (CESSNA P/N 0842104-2). THE BELLCRANK WAS BROKEN WHERE THE WHEEL WELL ACTUATING ROD IS ATTACHED. S UBMITTER STATED UNABLE TO TELL WHAT CAUSED THIS BREAK. THE BREAK APPEARS TO BE A FRESH, CLEAN, NEW BREAK AND THE GEAR D OES NOT SHOW ANY SIGNS OF STRESS. 1 L 7 2 3O A7CE 1998072400689 19980724 00689 CE 1998 7 24 98ZZZX2469 1 19980604 A 3510 C1660070108 BOTTLE BRACKET CESSNA 208 208B 2073701 CE BS 336.85 CRACKED A S ASWA K NONE O OTHER IN INSP/MAINT 1 WP 07 1203S 3340 208B0439 DURING ROUTINE INSPECTION, THE OXYGEN BOTTLE SADDLE BRACKETS WERE FOUND CRACKED. THE LEFT BRACKET WAS CRACKED INTO TWO PIECES. THE RIGHT CRACKED ON ONE SIDE. THE AIRCRAFT HAS NO HISTORY OF A HARD LANDING. 1 H 7 1 3T A37CE 1998072400692 19980724 00692 GL 1998 7 24 98ZZZX2472 2 19980618 A 7250 ENGINE BELL 206 206L1 1182107 SW ALLSN 250C 250C28 03013 GL HOT SECTION FAILED A HEEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 03 16938 17897 497 45157 CAE860015 DURING TAKEOFF, TOT LIGHT CAME ON. PILOT RETURNED TO OFFSHORE PLATFORM AND MADE AN UNEVENTFUL LANDING. DURING HOT-END INSPECTION, ENGINE COMPONENTS FOUND OUT OF LIMITS. MAINTENANCE REPLACED ENGINE ASSEMBLY. 1 G 7 1 3U 3 U H2SW E1GL 1998072400720 19980724 00720 NM 1998 7 24 98ZZZX2499 1 19980531 A 3350 LIGHT BOEING 727 727251 138408H NM CABIN FAILED A P9RA K NONE L NO TEST IN INSP/MAINT 1 SW 09 281US 21160 REMOVED OVERHEAD EMERGENCY EXIT LIGHT ASSY, INOPERATIVE. FOUND WHEN PLACING ACFT IN SHORT TERM STORAGE. 2 L 7 3 4F A3WE 1998072400740 19980724 00740 WP 1998 7 24 TWAA9809811 1 19980616 A 5753 SPAR DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING INBD TE FLAP HINGE CASTING ATTACH HOLES WITH .75 INCH LONG CRACK IND ICATION ON SPAR WEB AT LOWER INBD MOUNT HOLE. INSTALLED REPAIR DOUBLER PER JO 6027 REAR SPAR REPAIR DRAWING. TOTAL TIM E: 72,210 HOURS. TOTAL CYCLES: 84,221. (X) 2 L 7 2 4F A6WE 1998072400741 19980724 00741 WP 1998 7 24 TWAA9809810 1 19980616 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 544 BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK FOUND STA 544 FORMER RING FOOT BENT BEYOND LIMITS, BETWEEN LONGERONS 28R AND 29R. R EPLACED FORMER FOOT PER SRM 53-03, FIG 3 AND SRM 53-04, FIG 38. TOTAL TIME: 72,210 HOURS. TOTAL CYCLES: 84,221. (X) 2 L 7 2 4F A6WE 1998072400742 19980724 00742 WP 1998 7 24 TWAA9809809 1 19980616 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BLENDED BEYOND LIMITS AT STA 200, RBL 22, FLOOR TRACK. REPLACED C ORRODED TRACK SECTION PER SRM 51-01, PG 1 ITEM C. STA 200 TO STA 265. TOTAL TIME: 77,783. TOTAL CYCLES: 84,471. (X ) 2 L 7 2 4F A6WE 1998072400743 19980724 00743 WP 1998 7 24 TWAA9809808 1 19980616 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1022-1041 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK FOUND CORROSION ON NR 1 CHAIR TRACK, STA 1022 TO STA 1041, UNDER AND AROUND SPLICE SCREW HEADS. REPLACED TRACK AND SPLICED REPAIR, STA 1022 TO STA 1136 PER SRM 53-05 FIG 4F, AND SRM 51-01 PAGE 2, PARA C . REF: SERVICE REWORK DRAWING SR0930085. TOTAL TIME: 28,425 HOURS. TOTAL CYCLES: 17,789. (X) 2 L 7 2 4F A6WE 1998072400744 19980724 00744 WP 1998 7 24 TWAA9809807 1 19980616 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 13R CRACKED AT STA 965. CUT AND REMOVED LONGERON FROM JUST AFT OF WINDOW BELT TO STA 972, APPROXIMATELY, TO REMOVE DAMAGED AREA. REPLACED SECTION PER SRM 51-01, PAGE 1 ITEM 6, AND REPAI RED AT SPLICE PER SRM 53-02, FIG 18, PAGES 1, 4, 5, AND 6. REPLACED FORWARD 2 FASTENERS IN SPLICE THROUGH SKIN PER SRM 51-30-5, FIG 4 AND 4A HILOCK PIN CROSS INDEX, AS THESE FASTENERS WERE CAD. PLATED AND WENT THROUGH 'A' TITANIUM DOUBLER FROM A PAST SKIN REPAIR. ALSO SSRM 51-40-501. TOTAL TIME: 77,210 HOURS. TOTAL CYCLES: 84,221. (X) 2 L 7 2 4F A6WE 1998072400745 19980724 00745 NM 1998 7 24 TWAA9809806 1 19980608 A 5330 SKIN BOEING 727 727231 1384079 NM BS 870 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54345 21632 MCI - DURING CHECK-C, MAINTENANCE FOUND COROSION ON RT SIDE OF FUSELAGE SKIN AT STA 870, STR 10R. REMOVED CORROSION PER SRM 51-10-6. CUT OUT CORROSION AND INSTALLED DOUBLER AND FILLER PER SRM 53-30-3, PAGE 14D. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: 30,953. (X) 2 L 7 3 4F A3WE 1998072400746 19980724 00746 NM 1998 7 24 TWAA9809805 1 19980608 A 5315 FLOORBEAM BOEING 727 727231 1384079 NM BS 370-418 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54345 21632 MCI - DURING CHECK-C, MAINTENANCE FOUND CORROSION ON RT FLOOR SUPPORT ANGLE FROM STA 370 TO STA 418, AT RT SERVICE DOOR THRESHOLD. REPLACED ANGLE PER SRM 51-10-1, AND TWA STD PRACTICES. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: 30,953. ( X) 2 L 7 3 4F A3WE 1998072400747 19980724 00747 NM 1998 7 24 TWAA9809804 1 19980609 A 5730 SKIN BOEING 727 727231 1384079 NM RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54345 21632 MCI - DURING CHECK-C, MAINTENANCE FOUND RT WING LE WITH CRACKS IN SKIN AND RIVETS CRACKED AND LOOSE, 19 INCHES OTBD OF N R 5 LE SLAT OTBD 'UP' STOP. REMOVED CRACKED SKIN AND REPAIRED PER SRM 57-30-4, PAGES 10 AND 11. TOTAL TIME: 47,795 HO URS. TOTAL CYCLES: 30,953. (X) 2 L 7 3 4F A3WE 1998072400748 19980724 00748 NM 1998 7 24 TWAA9809803 1 19980606 A 5315 FLOORBEAM BOEING 727 727231 1384079 NM BS 418 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54345 21632 MCI - DURING CHECK-C, MAINTENANCE FOUND CABIN FLOOR SUPPORT AT STA 418 WITH CORROSION FROM RBL 44 INTO OTBD END OF SUPPO RT. NEW SUPPORT INSTALLED PER SRM 51-10-1, PAGES 4 AND 4A. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: 30,953. (X) 2 L 7 3 4F A3WE 1998072400749 19980724 00749 NM 1998 7 24 TWAA9809802 1 19980609 A 5320 DOOR STOP BOEING 727 727231 1384079 NM CABIN CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54331 20309 JFK - EDDY CURRENT FOUND LT NR 1 CABIN DOOR TOP AFT DOOR STOP CRACKED. REMOVED AND REPLACED STOP FITTING PER 727 SRM 51 -10-1. CHECK-C 5-10-98 JFK. TOTAL TIME: 70,079 HOURS. TOTAL CYCLES: 46,814. (X) 2 L 7 3 4F A3WE 1998072400750 19980724 00750 NM 1998 7 24 TWAA9809801 1 19980609 A 5730 SKIN BOEING 727 727231 1384079 NM RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54345 21632 MCI - DURING CHECK-C MAINTENANCE FOUND ON RT WING LE A CRACK IN THE SKIN AT RIVETS, AND THE RIVETS WERE CRACKED AND LOOS E, 11 IN OTBD OF NR 5 LE SLAT OTBD UP-STOP. REMOVED CRACKED SKIN AND REPAIRED PER SRM 57-30-4, PAGES 10 AND 11. TOTAL TIME: 47,795 HOURS. TOTAL CYCLES: 30,953. (X) 2 L 7 3 4F A3WE 1998072400751 19980724 00751 WP 1998 7 24 TWAA9809705 1 19980612 A 5320 TIE DOUG DC9 DC932 3022066 WP BS 167 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND STR 30 CORRODED AT TIE CLIP, FS 167. REMOVED CORROSION IN STRINGER PER SRM 51-10-3, PARA 35, PAGE 21. REMOVED STRINGER TIE, DRILLED, DEBURRED, AND INSTALLED NEW TIE PER SRM 51-01, PAGE 1, ITEM C AND SRM 51-30-2, PAGE 1. TOTAL TIME: 77,783 HOURS. TOTAL CYCLES: 84,471. (X) 2 L 7 2 4F A6WE 1998072400752 19980724 00752 WP 1998 7 24 TWAA9809704 1 19980612 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND 2 EACH CRACKS AT STA 200, LONGERON 4L. REMOVED AND REPLACED 4L LONGERON FRO M STA 128 TO STA 229. INSTALLED LONGERON REPAIR SPLICE AT STA 190, L4L, PER SRM 53-02, FIG 18. TOTAL TIME: 77,783 HOUR S. TOTAL CYCLES: 84,471. (X) 2 L 7 2 4F A6WE 1998072400753 19980724 00753 WP 1998 7 24 TWAA9809703 1 19980612 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 180 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FORMER CRACKED AT STA 180, LONGERON 3R. REPAIRED FORMER RING PER SRM 53-03, CLASS 1, FIG 4, PG 5. TOTAL TIME: 77,783 HOURS. TOTAL CYCLES: 84,471. X) 2 L 7 2 4F A6WE 1998072400754 19980724 00754 WP 1998 7 24 TWAA9809702 1 19980612 A 5320 TIE DOUG DC9 DC932 3022066 WP BS 167 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND STRINGER 29R CORRODED AT TIE CLIP, FS 167. REMOVED CORRODED TIE, ORDERED NE W TIE, DRILLED, DEBURRED, AND INSTALLED NEW TIE PER SRM 51-01, PAGE 1 ITEM C, AND SRM 51-30-2 PAGE 1. TOTAL TIME: 77,78 3 HOURS. TOTAL CYCLES: 84,471. (X) 2 L 7 2 4F A6WE 1998072400761 19980724 00761 1998 7 24 VJ9800231 4 19980721 A 2561 5928729511 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 913VV 47318 COVER DISLODGED ON EMERGENCY EVACUATION SLIDE ASSEMBLY OF GALLEY DOOR. REINSTALLED SLIDE COVER AND PERFORMED REQUIRED I NSPECTIONS. 2 L 7 2 4F A6WE 1998072400762 19980724 00762 NM 1998 7 24 K3HA980092 1 19980718 A 2612 FIRE DETECTOR BOEING 727 727225 1384077 NM NR 1 ENGINE OUT OF POSITION A K3HA O OTHER N FALSE WARNING TO TAKEOFF 1 EA 25 8880Z 21453 NR 1 FIRE BELL SOUNDED AFTER 120 KTS ON TAKEOFF ROLL. NO FIRE LIGHTS OR ABNORMAL INDICATIONS NOTED. THIRTY MINUTES AFT ER TAKEOFF, NR 3 GROUND FAULT LIGHT ON, NR 1 CSD OIL TEMP INDICATE 150 DEGREES) IN 25C RISE ON CLIMBOUT, GEN ISOLATED TE MP RETURNED TO NORMAL AFTER 30 MINUTES. FOUND GASKET BLOWN ON CSD EJECTOR VALVE, LINES TO CSD COOLER REPLACED, GASKET L EAK CHECKED NR 1 ENGINE AT PART POWER, FOUND NO LEAKS, OK FOR SERVICE. NR 3 FAULT DETECTORREPOSTIONED, OPS CHECK OK. F OUND NR 1 CSD SERVICED TO OVER FULL, DRAINED TO PROPER LEVEL, RAN ENGINE LEAK OPS CHECK OK. 2 L 7 3 4F A3WE 1998072400763 19980724 00763 WP 1998 7 24 IXXA9800062 1 19980721 A 3260 H141002 SWITCH DOUG DC8 DC871F 302199D WP LT MLG DEFECTIVE A IXXA K NONE N FALSE WARNING AP APPROACH 1 GL 23 826BX 2748 45998 ON APPROACH, DURING GEAR EXTENSION FOR LANDING,THE LEFT MAIN GEAR INDICATOR LIGHT FAILED TO ILLUMINATE IN THE DOWN POSIT ION, ACCOMPANIED BY AN ILLUMINATED GEAR UNSAFE WARNING LIGHT. THE CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAI NED THE SAME. WHILE TURNING THE AIRCRAFT, THE LEFT MAIN GEAR DOWN AND LOCK LIGHT ILLUMINATED AND THE AIRCRAFT CONTINUED FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE LANDING GEAR INDICATION SYSTEM WHICH REVEALED THE LEFT MAIN GEAR DOWNLOCK SWITCH DEFECTIVE. MAINTENANCE REPLACED THE SWITCH, SYSTEM CHECK GOOD IN ACCORDANCE WITH THE MAINTENANCE MANUAL . 2 L 7 4 4F RT 4A25 1998072400764 19980724 00764 NM 1998 7 24 AWXA9800155 1 19980716 A 5330 SKIN BOEING 737 737277 1384570 NM BS 770 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 185AW 22652 FUSELAGE SKIN CRACK BELOW STRINGER 17L AT BS 770. REMOVED DAMAGE AREA AND INSTALLED REPAIR DOUBLER PER SRM 53-30-03 FIG 25. 2 L 7 2 4F RT A16WE 1998072400765 19980724 00765 1998 7 24 AWXA9800156 2 19980714 A 7261 SCAVENGE LINE BOEING 757 7572S7 1384962 NM NR 1 ENGINE LOOSE A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 901AW 23321 EICAS MESSAGE AND LOW OIL PRESSURE LIGHT ON NR 1 ENGINE. ENGINE SHUT DOWN IN FLIGHT, AIR TURNBACK. OPENED COWLING AND C-DUCTS, FOUND SCAVENGE LINE LOOSE. RETIGHTENED AND SAFETIED. CHECKED MAGNETIC CHIP DETECTORS REF MM 79-21-03. CHECKE D SCAVENGE AND PRESSURE FILTERS REF MM 79-32-00. NO DEFECTS NOTED. SERVICED OIL, ACCOMPLISHED ENGINE RUNS. NO LEAKS N OTED, CLOSED COWLS AND C-DUCTS. 2 L 7 2 4F RT A2NM 1998072400766 19980724 00766 SO 1998 7 24 RAAA98E8022 1 19980720 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 PAX ROW 9 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998072400767 19980724 00767 SO 1998 7 24 RAAA98E8023 1 19980720 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FWD LT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998072400768 19980724 00768 SO 1998 7 24 RAAA98E8024 1 19980720 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FWD RT AND AFT LT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT ASS YS DUE FAILED. 2 L 7 4 4T 4A22 1998072400769 19980724 00769 NM 1998 7 24 CALA9801291 1 19980712 A 5720 BEAM BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A .25 INCH CRACK IN LT WING TRAILING EDGE FLAP CORE AREA J BEAM JUST FORWARD OF NR 7 SPOILER CASTING. T HE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5750-02914, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998072400770 19980724 00770 NM 1998 7 24 CALA9801292 1 19980706 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 848-1130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM SUPPORT BRACE AT STA 848, BL 0 AND A 2 INCH CRACK WAS FOUND IN SUPPORT BRA CE AT STA 1110 TO 1130, LBL 36. THE SUPPORTS WERE REMOVED IAW SRM 51-10-1. NEW SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-6, AND 51-40-5. 2 L 7 3 4F A3WE 1998072400771 19980724 00771 NM 1998 7 24 CALA9801293 1 19980706 A 5320 BRACE BOEING 727 727227 1384078 NM BS 1070-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND FLOORBEAM SUPPORT BRACE AT STA 1070 TO 1110, RBL 64 AND AT STA 1130, RBL 16 CORRODED. THE SUPPORT BRAC ES WERE REMOVED IAW SRM 51-30-21. NEW SUPPORT BRACES WERE FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, 5 1-10-1, AND 51-10-6. 2 L 7 3 4F A3WE 1998072400772 19980724 00772 NM 1998 7 24 CALA9801294 1 19980712 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 344,1025 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1025, RBL 54 AND LT SEAT TRACK WAS CORRODED BETWEEN STA 344 AND 360, LBL 44. 2 L 7 3 4F A3WE 1998072400773 19980724 00773 NM 1998 7 24 CALA9801295 1 19980712 A 5347 SEAT TRACK BOEING 727 727227 1384078 NM BS 380-1135 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND SEAT TRACKS CORRODED AT STA 1110 TO 1135, RBL 24 AND AT STA 380 TO 420, RBL 27. THE CORRODED SEAT TRAC KS WERE REMOVED AND NEW SECTIONS OF SEAT TRACK WERE FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2, AND 51-4 0-5. 2 L 7 3 4F A3WE 1998072400774 19980724 00774 NM 1998 7 24 CALA9801296 1 19980712 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN STRINGER 15L AT STA 720B. THE CRACKED AREA WAS CUT OUT IAW SRM 53-10-32. REPAIR P ARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-3, 51-10-6, AND 53-10-3. 2 L 7 3 4F A3WE 1998072400775 19980724 00775 NM 1998 7 24 CALA9801297 1 19980706 A 5320 PANEL BOEING 727 727227 1384078 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1 INCH CRACK IN TOP RT NOSE WHEEL WELL PANEL. THE CRACKED AREA WAS CUT OUT, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998072400776 19980724 00776 NM 1998 7 24 CALA9801298 1 19980717 A 5713 STRINGER BOEING 727 727224 1384076 NM WS 171.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1.375 INCH CRACK IN RT WING VENT BOX STRINGER 19 AT WS 171.5, NR 2 TANK. THE CRACKED AREA WAS CUT OU T, A REPAIR DOUBLER, FILLER, AND ANGLE WERE FABRICATED AND INSTALLED IAW SRM 57-10-4, 51-10-2, 51-30-2, 51-10-6, AND 51- 20-4. 2 L 7 3 4F A3WE 1998072400777 19980724 00777 NM 1998 7 24 CALA9801299 1 19980717 A 5532 SKIN BOEING 727 727224 1384076 NM BS 1215 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .75 INCH CRACK THROUGH FASTENER HOLE OF SKIN AT LT SIDE OF VERTICAL STABILIZER AROUND ACCESS PANEL 95 23 ABOVE BS 1215. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-0, 55-30-3, 51-10-2, 51-30-2, AND 51-00-00. 2 L 7 3 4F A3WE 1998072400778 19980724 00778 NM 1998 7 24 CALA9801300 1 19980717 A 5320 PANEL BOEING 727 727224 1384076 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND CRACKS IN THE NLG WHEEL WELL TOP LEFT AND TOP RIGHT SKIN PANELS. THE CRACKS WERE .75 TO 1 INCH LONG. T HE SKIN WAS REMOVED IAW SRM 51-10-1. WEB SKIN WAS FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998072400779 19980724 00779 NM 1998 7 24 CALA9801301 1 19980721 A 3350 BPS73 BATTERY PACK RADIANT BOEING 757 757224 1384958 NM CABIN DISCHARGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18112 27302 INSPECTION FOUND EMERGENCY AISLE PATH LIGHTING ON SEATS INOPERATIVE AT ROW 7 TO 25. THE BATTERY PACK AT ROW 9 PSU WAS R EMOVED AND REPLACED. A BROKEN POWER WIRE AT ROW 14 WAS REPLACED. OPERATION OF THE LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A2NM 1998072400780 19980724 00780 NM 1998 7 24 CALA9801302 1 19980717 A 5330 SKIN BOEING 727 727224 1384076 NM R-1 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 2.75 INCH CRACK IN LOWER AFT FUSELAGE SKIN CUTOUT AT R-1 DOOR. THE CRACK WAS STOP DRILLED, A DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW ECRA 5307-01141. 2 L 7 3 4F A3WE 1998072400781 19980724 00781 NM 1998 7 24 CALA9801303 1 19980702 A 5230 DOOR BOEING 727 727224 1384076 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO C-2 DOOR BOTTOM AFT CORNER. THE CORNER OF C-2 DOOR WAS REMOVED AND REPLA CED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 1998072400782 19980724 00782 NM 1998 7 24 CALA9801304 1 19980702 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 328-380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FLOORBEAM CORROSION AT STA 328, LBL 30 AND 45, STA 344, STA 380, RBL 32 TO 42. THE CORRODED AREAS OF F LOORBEAM WERE CUT OUT. REPAIRS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, AND 51-40-4. 2 L 7 3 4F A3WE 1998072400783 19980724 00783 NM 1998 7 24 CALA9801305 1 19980702 A 5320 WEB BOEING 727 727224 1384076 NM BS 700 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND STA 700 SUPPORT WEBS CRACKED AT S22L, S23L, S23R, AND S25R. THE CRACKS WERE 1 TO 1.5 INCH LONG. THE C RACKED AREAS WERE CUT OUT. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998072400784 19980724 00784 NM 1998 7 24 CALA9801306 1 19980702 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FORWARD LAV FLOORBEAM AT STA 344, RBL 24 CORRODED. THE CORRODED AREA OF FLOORBEAM WAS REMOVED, A NEW F LOORBEAM SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998072400785 19980724 00785 NM 1998 7 24 CALA9801307 1 19980702 A 5240 HOUSING BOEING 727 727224 1384076 NM R-2 DOOR HINGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1.5 INCH CRACK IN R-2 DOOR CUTOUT UPPER HINGE HOUSING. THE HINGE HOUSING WAS REMOVED IAW SRM 51-10-1 . A NEW HOUSING WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998072400786 19980724 00786 NM 1998 7 24 CALA9801308 1 19980702 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1.25 INCH CRACK IN STRINGER 15R AND A 2 INCH CRACK IN STRINGER 15L AT STA 720B. REPAIRS WERE FABRICA TED AND INSTALLED IAW SRM 53-10-00, 53-10-3, AND 51-10-2. 2 L 7 3 4F A3WE 1998072400787 19980724 00787 NM 1998 7 24 CALA9801309 1 19980702 A 5330 SKIN BOEING 727 727224 1384076 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FUSELAGE BELLY SKIN CORRODED AT BS 720 TO 720A, BL 0. A DOUBLER AND SHEAR TIE WERE FABRICATED AND INST ALLED IAW SRM 53-30-3, 53-30-4, AND 53-10-4. 2 L 7 3 4F A3WE 1998072400788 19980724 00788 NM 1998 7 24 CALA9801310 1 19980702 A 5311 FRAME BOEING 727 727224 1384076 NM BS 680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .5 INCH CRACK IN FORWARD CARGO COMPARTMENT FRAME AT BS 680 BETWEEN STRINGER 23L AND 24L. THE CRACK W AS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND 51-10-2. 2 L 7 3 4F A3WE 1998072400789 19980724 00789 NM 1998 7 24 CALA9801311 1 19980702 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 400-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND SEAT TRACK CORRODED BETWEEN STA 400 AND 420, RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED IA W SRM 51-30-2. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1998072400790 19980724 00790 NM 1998 7 24 CALA9801312 1 19980702 A 5320 SIDEWALL BOEING 727 727224 1384076 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 THE NLG WHEEL WELL RIGHT SIDEWALL AND TOP CENTER PANEL HAD CRACKS MEASURING .5 TO 1 INCH LONG. THE CRACKED AREAS WERE C UT OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998072400791 19980724 00791 NM 1998 7 24 CALA9801313 1 19980702 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FLOORBEAM CORRODED AT STA 380 BETWEEN RBL 32 AND RBL 42. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT IA W SRM 53-10-8. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, AND 51-40-4. 2 L 7 3 4F A3WE 1998072400792 19980724 00792 NM 1998 7 24 CALA9801314 1 19980702 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 303-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FLOORBEAM CORRODED AT STA 303 TO 344, LBL 28. THE CORROSION WAS REMOVED IAW SRM 51-10-8. ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-8. 2 L 7 3 4F A3WE 1998072400793 19980724 00793 NM 1998 7 24 CALA9801315 1 19980702 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 380-400/1150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 380 TO 400, RBL 16 AND STA 1150, RBL 18. THE FLOOR SUPPORTS WERE REMOVE D, NEW FLOOR SUPPORTS WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-10-1. 2 L 7 3 4F A3WE 1998072400794 19980724 00794 NM 1998 7 24 UPS98227179 1 19980716 A 5753 TRACK BOEING 727 72730C 1384009 NM NR 3 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, NR 3 FLAP TRACK CENTER MOUNT BOLT IS CORRODED ON THE AFT SIDE CORROSION (C57-581-06.00-03) AND CORRO SION (C57-581-06.00-03) NR 3 FLAP TRACK IS CORRODED ON THE SPOILER BEAM MOUNT PAD. FLAP TRACK REMOVED AND SENT TO OUTSI DE SERVICES FOR REPAIR. REINSTALLED AFTER REPAIR. 2 L 7 3 4F A3WE 1998072400795 19980724 00795 NM 1998 7 24 UPS98227180 1 19980716 A 5753 TRACK BOEING 727 72730C 1384009 NM NR 1 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, NR 1 FLAP TRACK FWD MOUNT BOLT LUGS ARE CORRODED. REMOVED FLAP TRACK AND SENT TO OUTSIDE SERVICES F OR REPAIR AND REINSTALLED AFTER REPAIR. 2 L 7 3 4F A3WE 1998072400796 19980724 00796 NM 1998 7 24 UPS98227181 1 19980716 A 5753 TRACK BOEING 727 72730C 1384009 NM NR 7 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C57-581-06.00-04) NR 7 FLAP TRACK FWD LUG HAS RUST AROUND BOLT HOLE. REMOVED FLAP TRACK AND SENT TO OUTSIDE SERVICES FOR REPAIR AND REINSTALLED AFTER REPAIR. 2 L 7 3 4F A3WE 1998072400797 19980724 00797 NM 1998 7 24 UPS98227182 1 19980717 A 5320 STIFFENER BOEING 727 72730C 1384009 NM BS 336 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, WHILE WORKING FUSELAGE 88 CUSTOMER ID NR 832295 FOUND CORROSION ON NLG WHEEL WELL STIFFENER BS 336, LBL 14, WL 158. OUT OF LIMITS. REPAIRED PER SRM 51-10-6, 53-10-1, 53-10-2, 51-30-2, 51-20-151. 2 L 7 3 4F A3WE 1998072400798 19980724 00798 NM 1998 7 24 UPS98227185 1 19980707 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 243.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, CRACK BS 243.7 RT SIDE AT WL 222 APPROX ON FUSELAGE SKIN. CRACK REMOVED PER SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1998072400799 19980724 00799 NM 1998 7 24 UPS98227186 1 19980707 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 211.8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, CRACK BS 211.8 RT SIDE AT WL 219.5 ON FUSELAGE SKIN. CRACK REMOVED PER SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1998072400800 19980724 00800 NM 1998 7 24 UPS98227187 1 19980707 A 5230 CASTING BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, TOP AFT CORNER CASTING CRACKED ON MAIN CARGO DOOR. TOP AFT CORNER FITTING ON MAIN CARGO DOOR REPLACE D IAW SRM 51-30-2, REF BOEING DWG NR 65-25337. 2 L 7 3 4F A3WE 1998072400801 19980724 00801 NM 1998 7 24 UPS98527176 1 19980716 A 5347 BAC1520792 SEAT TRACK BOEING 757 75724APF 1384969 NM BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE-C, CORROSION ON SEAT TRACK AT BS 1180 LBL 45 WL 208 AROUND NUT PLATES. REMOVED CORRODED SEAT TRACK FROM BS 1180 TO 1320 AND INSTALLED NEW SEAT TRACK FROM BS 1180 TO 1320. ALL WORK DONE IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 1998072400802 19980724 00802 NM 1998 7 24 UPS98527177 1 19980715 A 5320 BAC15061108 BEAM BOEING 757 75724APF 1384969 NM BS 900-1040 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE-C, CORROSION ON LONGITUDINAL BEAM BS 900 TO 1040 AROUND NUT PLATES, LBL 45, WL 208. REMOVED CORROSION F OUND TO BE OUT OF LMITS PER SRM 53-00-51. REMOVED AND REPLACED LONGITUDINAL BEAM PER SRM 51-40-02, EO 757-53-0048. 2 L 7 2 4F RT A2NM 1998072400803 19980724 00803 NM 1998 7 24 UPS98527178 1 19980715 A 5320 BAC15061108 BEAM BOEING 757 75724APF 1384969 NM BS 1040-1076 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 406UP 23728 INSPECTION TYPE-C, CORROSION ON LONGITUDINAL BEAM BS 1040 TO 1076 LBL 45, WL 208 AROUND NUT PLATES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-00-51. REMOVED AND REPLACED LONGITUDINAL BEAM IAW SRM 51-40-02. 2 L 7 2 4F RT A2NM 1998072400804 19980724 00804 WP 1998 7 24 UPS98827183 1 19980627 A 5320 JAMB DOUG DC8 DC871F 302199D WP SERVICE DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, RT AFT SERVICE DOOR HAS TWO CRACKS IN AFT UPPER DOOR JAMB CORNER, ON THE INNER DOUBLER 2.5 EMANATING FROM EDGE. REPAIRED IAW SRM 52-2-0. 2 L 7 4 4F RT 4A25 1998072400805 19980724 00805 NM 1998 7 24 UPS98227189 1 19980709 A 5753 ANGLE BOEING 727 72731C 1384011 NM LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, LWR CHORD ANGLE ON LT INB MIDFLAP INB CARRIAGE SUPPORT STRUCTURE CRACKED. LWR CHORD ANGLE REPLACED I AW SRM 51-30-02. 2 L 7 3 4F A3WE 1998072400806 19980724 00806 NM 1998 7 24 UPS98227190 1 19980709 A 5520 BRACKET BOEING 727 72731C 1384011 NM LT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, LT ELEVATOR BRACKET ON REAR SPAR AT ELEV STA 66.5 APPROX CRACKED. OPENED ELEVATOR SKIN IAW SRM 51.30 .2, ANGLE BRACKET REPLACED IAW DRAWING NR 69-19144 ELEVATOR SKIN CLOSED IAW DRAWING NR 65-25635. 2 L 7 3 4F A3WE 1998072400807 19980724 00807 NM 1998 7 24 UPS98227191 1 19980709 A 5753 CASTING BOEING 727 72731C 1384011 NM NR 5 TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, NR 5 FLAP CARRIAGE LWR DEAD WEIGHT ROLLER CASTING CRACKED. FITTING AND ASSOCIATED HARDWARE REPLACED IAW OHM 57-58-02. 2 L 7 3 4F A3WE 1998072400808 19980724 00808 NM 1998 7 24 UPS98227192 1 19980710 A 5412 FIREWALL BOEING 727 72731C 1384011 NM BS 1387.85 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, WEB OVER NR 2 ENGINE HORIZONTAL FIREWALL RT SIDE AT BS 1387.85 IS CRACKED. WEB FABRICATED AND INSTAL LED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1998072400809 19980724 00809 NM 1998 7 24 UPS98227194 1 19980709 A 5753 CASTING BOEING 727 72731C 1384011 NM NR 4 TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, NR 4 FLAP TRACK TEAR DROP FAIRING SPIGOT CASTING CRACKED. REPLACED CASTING IAW MM 27-50-00. 2 L 7 3 4F A3WE 1998072400810 19980724 00810 NM 1998 7 24 UPS98227195 1 19980708 A 5753 RIB BOEING 727 72731C 1384011 NM LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, SUSPECT CRACK IN LT I/B FLAP I/B CARRIAGE SUPPORT STRUCTURE. RIB CHORD REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998072400811 19980724 00811 NM 1998 7 24 UPS98227196 1 19980707 A 5230 CASTING BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, TOP FWD CORNER CASTING CRACKED ON MAIN CARGO DOOR. TOP FWD CORNER FITTING ON MAIN CARGO DOOR REPLACE D IAW SRM 51-30-2, ALSO REF BOEING DWG NR 65-25337. 2 L 7 3 4F A3WE 1998072400812 19980724 00812 NM 1998 7 24 UPS98227197 1 19980709 A 5510 65245711 BEAM BOEING 727 72731C 1384011 NM LT HORIZ STAB CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, SURFACE CORROSION ON LT STAB UPPER T/E BEAM FROM I/B TO O/B END. T/E BEAM REPLACED IAW DRAWING NR 65 -22987. 2 L 7 3 4F A3WE 1998072400813 19980724 00813 NM 1998 7 24 UPS98227198 1 19980709 A 5510 65245712 BEAM BOEING 727 72731C 1384011 NM RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, RT STAB UPPER SURFACE T/E BEAM HAS SEVERAL AREAS OF CORROSION FROM I/B TO O/B. CORROSION REMOVED AND FOUND TO BE OUT OF LIMITS IAW SRM 55-10-1. BEAM REPLACED IAW DRAWING NR 65-22987. 2 L 7 3 4F A3WE 1998072400814 19980724 00814 WP 1998 7 24 UPS98827199 1 19980629 A 5320 3754066503 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, TORQUE BOX FS 1220 L-33R FITTING CORRODED. REMOVED, FABRICATED AND REPLACED FITTING IAW DHC SK 708-5 59. 2 L 7 4 4F RT 4A25 1998072400815 19980724 00815 WP 1998 7 24 UPS98827201 1 19980626 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 598 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 708UP 46048 INSPECTION TYPE-C, RT WING L/E LWR SKIN AT WS XFS 598 IS CRACKED. REPAIRED IAW DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 1998072400816 19980724 00816 EU 1998 7 24 QXEA9801030 1 19980718 A 3397 WIRE GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 EXIT SIGN ABOVE GALLEY IS INOPERATIVE IN THE EVAC POSITION. MAINTENANCE REPAIRED A BROKEN WIRE AT THE CANNON PLUG, OPER ATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998072400817 19980724 00817 EU 1998 7 24 QXEA9801031 1 19980719 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 AFT EXIT EVACUATION LIGHTS REMAIN ON WHEN BATTERY IS SWITCHED OFF. MAINTENANCE REPLACED POWER SUPPLY IN AFT CARGO HOLD, OPERATIONALLY TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998072400818 19980724 00818 EU 1998 7 24 QXEA9801032 1 19980720 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 EMERGENCY EXIT LIGHT IN ROW 9E OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998072400819 19980724 00819 EU 1998 7 24 QXEA9801033 1 19980718 A 2750 LINE FOKKER F28 F28MK4000 4990810 EU TE FLAP DRIVE FAILED A QXEA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 09 488US 11240 EN ROUTE, NR 1 HYD FLUID QUANTITY DEPLETED. CREW PERFORMED ALTERNATE GEAR EXTENSION. LANDED WITH DOORS DOWN. MAINTENA NCE INSPECTED AND FOUND A HYDRAULIC RETURN LINE ON THE FLAP DRIVE GEARBOX BROKEN. INSTALLED A FLEX LINE, SERVICED HYDRA ULIC SYSTEM, LEAK CHECKED GOOD WITH NO OTHER HYDRAULIC SYSTEM DEFECTS NOTED. MAINTENANCE FOUND THE DOORS UP CABLE BROKEN . THE CABLE WAS REMOVED AND REPLACED. THE RIGHT HAND MAIN LANDING GEAR DOOR WAS REMOVED AND REPLACED. THE LEFT HAND M AIN LANDING GEAR DOOR WAS REPAIRED. THE ALTERNATE RETRACTION SYSTEM CABLE FOR INBOARD MAIN LANDING GEAR WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A20EU 1998072400820 19980724 00820 EU 1998 7 24 QXEA9801034 1 19980716 A 3350 TERMINAL FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 LEFT AND RIGHT WING ROOT EVACUATION LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CORRODED POSITIVE TERMINAL END AT BOTH LEFT AND RIGHT LIGHT FIXTURES, OPERATIONALLY TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998072400821 19980724 00821 NM 1998 7 24 QXEA9801035 1 19980719 A 3232 ACTUATOR DHAV DHC8 DHC8102 2809003 NM GEAR DOOR OUT OF ADJUST A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 814PH 43 AFTER GEAR SELECTED UP THE AMBER DOOR LIGHT REMAINED ON. VISUALLY VERIFIED THAT THE GEAR DOOR WAS OPEN. CYCLED LANDING GEAR AND ALL LIGHTS WENT OUT. ADJUSTED AFT GEAR DOOR ACTUATOR ROD END IAW MM MANUAL 32-10-36. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998072400822 19980724 00822 WP 1998 7 24 ABXA9800633 1 19980719 A 3260 38981571 TARGET DOUG DC8 DC863 302198A WP RT MLG WW OUT OF ADJUST A ABXA O OTHER N FALSE WARNING CR CRUISE 1 GL 23 816AX 46093 WITH GEAR UP AND NO GEAR UNSAFE LIGHT ON, DOOR 'NOT LATCHED' LIGHT ILLUMINATED WHEN RIGHT DOOR SELECTED. RECYCLED GEAR, LIGHT REMAINED ON. REPOSITIONED TARGET ON DOOR ROLLER IAW DC8 MM 32-60-00, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998072400823 19980724 00823 WP 1998 7 24 ABXA9800634 1 19980720 A 3230 5715316 FITTING DOUG DC8 DC861 3021952 WP LT/RT MLG WORN A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 848AX 46032 RED GEAR UNSAFE LIGHT ILLUMINATED INTERMITTENTLY AFTER GEAR RETRACTION. RECYCLED GEAR AND LIGHT DID NOT ILLUMINATE AGAI N. REPLACED BOTH LEFT AND RIGHT MAIN LANDING GEAR DRAG BRACE FITTING. PERFORMED OPS CHECK OF GEAR, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998072400824 19980724 00824 WP 1998 7 24 ABXA9800635 1 19980721 A 2170 21D101 COALESCER BAG DOUG DC9 DC941 302207N WP CABIN MISINSTALLED A ABXA O OTHER B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C AP APPROACH 1 GL 23 969AX 47464 AFT SMOKE DETECTOR ILLUMINATED ON SHORT FINAL. EVACUATED AIRCRAFT AFTER LANDING. SMOKE WAS OBSERVED IN AFT UPPER COMPA RTMENT. FIRE DEPT CLEARED AIRCRAFT, REPLACED NR 11 SMOKE DETECTOR. INSPECTED AND FOUND RIGHT COALESCER BAG NOT PROPERL Y INSTALLED. REPLACED COALESCER BAG. INSPECTED DUCTING IN AFT CARGO COMPARTMENT. NO DEFECTS NOTED. INSPECTED FREIGHT WITH NO CAUSE OF SMOKE FOUND. SUSPECT SMOKE WAS ACTUALLY MOISTURE/CONDENSATION. 2 L 7 2 4F A6WE 1998072400825 19980724 00825 WP 1998 7 24 MWEA98812 1 19980715 A 3231 5955992 BRACKET DOUG DC9 DC915 3022036 WP LT MLG DOOR BROKEN A MWEA O OTHER O OTHER LD LANDING 1 GL 31 300ME 45718 ON GEAR EXTENSION UPON LANDING, LEFT MAIN GEAR DOOR FREE SWUNG HITTING PAVEMENT. MTC FOUND BRACKET ON MAIN GEAR DOOR BR OKE. REMOVED AND REPLACED DOOR. 2 L 7 2 4F A6WE 1998072400826 19980724 00826 WP 1998 7 24 SCNA98531 1 19980721 A 3350 LIGHT DOUG DC10 DC1015 3022118 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, THE EMERGENCY EXIT LIGHTING AT AFT A ZONE AND FWD B ZONE ARE FOUND TO BE INOPERATIVE. THE FEEDS DO NOT HAVE POWER. REMOVED AND REPLACED TWO EEL BATTERIES, TWO DIODES, AND TWO EEL FEEDS. OPERATIONAL CHECK GOOD PER MM 3 35300 (SUPPLEMENTAL BINDER). 2 L 7 3 4F A22WE 1998072400827 19980724 00827 WP 1998 7 24 SCNA98532 1 19980721 A 5720 FITTING DOUG DC10 DC1015 3022118 WP LT WING CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 152SY 48289 DURING HEAVY CHECK, DEEP PITTING CORROSION WAS DISCOVERED ON THE FRONT SPAR, ON THE LEFT WING, FOOTSTOOL FITTING ATTACH HOLES NR 4 AND NR 6 (AROUND HOLES ON FORWARD FACE). REPAIRED PER BCAG FAX DATED 6/30/98, ACTION NR 373025 AND DWGS SBX SBA 98 0170TR, 0177TR, 0185TR AND APPROVED BY 8110 3 DATED 7/2/98 AND SCA ENGINEERING ORDER 57 5604 1. 2 L 7 3 4F A22WE 1998072400828 19980724 00828 WP 1998 7 24 SCNA98533 1 19980721 A 5711 SPAR CAP DOUG DC10 DC1015 3022118 WP WS 415 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, THE LEFT WING REAR SPAR CAP SPLICE WAS FOUND TO EXHIBIT A 2 INCH CRACK AT STA XORS 415 .00. REMOVED AND REPLACED THE SPAR TANG AFT AT STA XORS 415.00 AT THE LEFT REAR SPAR PER SRM 513301. 2 L 7 3 4F A22WE 1998072400829 19980724 00829 WP 1998 7 24 RRXA98254 1 19980320 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 2 SPOILER GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND LEFT WING, NR 2 SPOILER GOUGED, ON LOWER SIDE. REMOVED DAMAGED SECTION, FABRICATED AN D INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 51-188, 51-1-16 AND TPS 1001. 2 L 7 4 4F RT 4A25 1998072400830 19980724 00830 WP 1998 7 24 RRXA98255 1 19980319 A 5712 RIB DOUG DC8 DC873F 302199F WP LT WING CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND LEFT WING LEADING EDGE RIB CRACKED AT BOTTOM END, FORWARD OF PANEL 518A. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400831 19980724 00831 WP 1998 7 24 RRXA98256 1 19980331 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR PUNCTURED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND LOWER CARGO DOOR, SKIN PUNCTURED AT STA 980 LOWER EDGE. FABRICATED AND INSTALLED REPA IR DOUBLER IAW DC-8 SRM 52-2-0, FIGURE 4. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400832 19980724 00832 WP 1998 7 24 RRXA98257 1 19980410 A 5230 SUPPORT DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND C-2 CARGO DOOR, UPPER ROLLER SUPPORT FLANGE CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 52-4-1, FIGURE 3. TREATED AERA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400833 19980724 00833 WP 1998 7 24 RRXA98258 1 19980420 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 80 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND FRAME CRACKED AT STA 80 AND LONGERON 21 RIGHT. REMOVED DAMAGED SECTION, FABRICATED AN D INSTALLED REPAIR DOUBLER AND FILLERS, BONDED IAW DC-8 SRM 53-2-0 AND 51-1-21. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400834 19980724 00834 WP 1998 7 24 RRXA98260 1 19980328 A 5320 DOOR FRAME DOUG DC8 DC873F 302199F WP CARGO DOORWAY MISREPAIRED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND CARGO DOOR JAMB WITH PREVIOUS REPAIR IN PSE AREA THAT IS NOT APPROVED, AT STA 520 LOWE R JAMB AREA. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGE SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53- 2-0 FIGURE 4, AND 52-4-1 FIGURE 2 AND 51-9-0 FIGURE 68A. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400835 19980724 00835 WP 1998 7 24 RRXA98261 1 19980331 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND LEFT WING FLAP OUTBOARD SKIN CHAFED AT STA 98. REMOVED DAMAGED SECTION IAW DC-8 SRM 5 1-1-21. FABRICATED AND INSTALLED NEW SKIN SECTION IAW 57-7-1 AND DAC DWG 5642960. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400836 19980724 00836 WP 1998 7 24 RRXA98262 1 19980318 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 133 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND RIGHT WING INBOARD FLAP, OUTBOARD BOTTOM EDGE AT INNER CONNECT LINKS CLOSING RIB CRACK ED, WITH 2 EXISTING REPAIRS, AT STA 133. REMOVED EXISTING REPAIRS AND DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW DAC DGW 5652396 AND DC-8 SRM 57-2-0 FIGURE 2, NOTE 2. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400837 19980724 00837 WP 1998 7 24 RRXA98263 1 19980401 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 300-320 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 33 LEFT, AT STA 300 TO STA 320. REMOVED DAMAGED LONGERON 33L, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON IAW 53-2-0, FIGURE 1F. 2 L 7 4 4F RT 4A25 1998072400838 19980724 00838 WP 1998 7 24 RRXA98264 1 19980326 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 860 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND SEAT TRACK CRACKED AT STA 860. REMOVED DAMAGED SEAT TRACK FROM STA 848 TO STA 872 IAW DC-8 SRM 51-3-0. FABRICATED AND INSTALLED NEW SEAT TRACK AND SPLICE REPAIR DOUBLER IAW DC-8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998072400839 19980724 00839 WP 1998 7 24 RRXA98265 1 19980330 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1220 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND SEAT TRACK WORN BEYOND LIMITS IAW DC-8 SRM 51-3-0, AT STA 1220. REMOVED WORN SECTION OF SEAT TRACK. FABRICATED AND INSTALLED NEW SECTION IAW DC-8 SRM 53-2-3 FIGURE 14. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400840 19980724 00840 WP 1998 7 24 RRXA98266 1 19980328 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1420 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND SEAT TRACK WORN AT STA 1420. REMOVED WORN SECTION OF SEAT TRACK. FABRICATED AND INST ALLED NEW SECTION IAW DC-8 SRM 53-2-3. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400841 19980724 00841 WP 1998 7 24 RRXA98267 1 19980325 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1600-1640 WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND SEAT TRACK WORN BETWEEN STA 1600 TO STA 1640. REMOVED WORN SECTION OF SEAT TRACK, FAB RICATED AND INSTALLED NEW SECTION IAW DC-8 SRM 53-2-3. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400842 19980724 00842 WP 1998 7 24 RRXA98268 1 19980325 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 975 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND SEAT TRACK CRACKED AT STA 975. REMOVED DAMAGED SECTION OF SEAT TRACK FROM STA 929 TO STA 975. FABRICATED AND INSTALLED NEW SECTION IAW DC-8 SRM 53-2-3 PAGE 12. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400843 19980724 00843 WP 1998 7 24 RRXA98269 1 19980402 A 5230 SKIN DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 796FT 46104 DURING A MAINTENANCE VISIT, FOUND LOWER CARGO DOOR EXTERIOR SKIN CRACKED AT STA 1220. REMOVED DAMAGED SECTION, FABRICAT ED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 52-2-0. TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998072400844 19980724 00844 WP 1998 7 24 RRXA98270 1 19980720 A 3246 26014112 WHEEL DOUG DC8 DC863F 302198F WP MLG BROKE OFF A RRXA K NONE O OTHER LD LANDING 1 WP 15 921R 46145 ON LANDING, THE NR 1 MLG WHEEL AND TIRE ASSEMBLY BROKE FROM AXLE. TIRE ASSEMBLY ROLLED INTO PARKED EQUIPMENT. AIRCRACF T WAS TOWED TO RAMP FOR INSPECTION. *S/D* REMOVED AND REPLACED NR 1 MAIN WHEEL AND TIRE ASSEMBLY, REPLACED NR 1 MAIN B RAKE ASSEMBLY, REPLACED MLG ANTI-SKID TRANSDUCER AND REPLACED LT MAIN BOGIE ASSEMBLY. 2 L 7 4 4F 4A25 1998072400845 19980724 00845 NM 1998 7 24 VNAA9807007 1 19980716 A 3080 3280013AMENDA CONTROL PANEL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FLIGHT DECK FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 441JS 49068 3059 DURING THE TAXI PRIOR TO TAKEOFF, A PITOT HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MA INTENANCE INSPECTED AND REPLACED THE ICE SYSTEMS CONTROL PANEL (17VE) , IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31 -12-13. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998072400846 19980724 00846 1998 7 24 VNAA9807008 4 19980720 A 3418 861EF1 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 436JS 76846 3052 AN ANGLE OF ATTACK FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GAT E. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND ANGLE OF ATTACK SENSOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MAN UAL 27-33-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998073000001 19980730 00001 NM 1998 7 30 98UAL900292 1 19980516 A 5754 114W251218 BRACKET BOEING 777 777222 1385219 NM PWA 4084 PW4084 NE NR 8 LE SLAT BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 795UA 26927 FOUND (P/N 114W2512-18) SKIRT EXTENSION BRACKET, FOR THE MAIN RIBS INBOARD NR 8 SLAT, BROKEN IN HALF AND CRACKED AT THE FASTENER AREA AT END. *S/D* DAMAGED PART REPLACED AT LHR. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998073000002 19980730 00002 NE 1998 7 30 98UAL900314 2 19980710 A 7320 FUEL CONTROL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE MALFUNCTIONED A UALA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 576UA 26690 ON TAKEOFF, MAX POWER OF 1.42 EPR SET, LEFT ENGINE WAS 1.42. RIGHT ENGINE 1.38 TO 1.39 EPR. RIGHT ENGINE FUEL FLOW SEV ERAL HUNDRED POUNDS LESS THAN LEFT ENGINE. LEFT ENGINE HAD THROTTLE REMAINING. RIGHT ENGINE THROTTLE AGAINST THE FIREW ALL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998073000003 19980730 00003 NM 1998 7 30 DL72L981458 1 19980713 A 3350 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 507DA 21309 AFT CABIN EMER TRACK LIGHT SECTION INOP. REPLACED BATTERY PACK AND CHARGER, OPS CK OK. 2 L 7 3 4F A3WE 1998073000004 19980730 00004 NM 1998 7 30 DL72L981476 1 19980715 A 3350 BATTERY 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 506DA T4282 21308 RT WING FWD EMER EXT LIGHT WILL NOT LIGHT. REPLACED M655 BATT AND PWR SUPP. 2 L 7 3 4F A3WE 1998073000005 19980730 00005 WP 1998 7 30 ARWA980798 1 19980715 A 7830 TR COWL LKHEED 1011 10113851 WP NR 2 ENGINE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 308GB 1133 NR 2 ENGINE TRANSLATING COWL EXTERIOR SKIN AT 6 O'CLOCK POSITION CRACKED. REPAIRED DAMAGED SKIN AS PER EO NR 2112543001 . WORK ACCOMPLISHED UNDER ARROW AIR FORM M3, L/P 12689, ITEM 3M. 2 L 7 3 4F RC A23WE 1998073000006 19980730 00006 NE 1998 7 30 DL757981483 2 19980716 A 7200 ENGINE 45100 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SO 27 641DL 392 23995 716480 ON CLIMB-OUT, FL 260, LT ENG STALLED AND QUIT ALL ENG IND WENT BLANK CLB 2 SELECTED SHUTDOWN CK LIST C/W RETURNED TO CVG . REPLACED NR 1 ENG PMA AND ROTOR SHAFT CKS, OK. 2 L 7 2 4F 4 F RT A2NM E17NE 1998073000007 19980730 00007 NM 1998 7 30 DL72L981486 1 19980716 A 3350 POWER PACK RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 507DA 4576 21309 EMERGENCY TRACK LIGHTING FROM ROW 27 AFT INOP. REPLACED POWER PACK. 2 L 7 3 4F A3WE 1998073000008 19980730 00008 NM 1998 7 30 P5CA9801174 1 19980713 A 3350 S1356B37 BATTERY PACK BOEING 747 747249F 1384849 NM BS 400 DISCHARGED A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 920FT 22237 RIGHT CREW DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-00, OPS CHECK OK. 2 L 7 4 4F A20WE 1998073000010 19980730 00010 EU 1998 7 30 AALA980922 1 19980507 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1470K 2444 11506 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ON FLOOR TRACK INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998073100015 19980731 00015 NM 1998 7 31 TAOA069804 1 19980617 A 7931 NUT BOEING 727 727227 1384078 NM NR 1 ENGINE LOOSE A TAOA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 15 927TS 20837 DCA/LGA - FLT 6420 - DURING CLIMB-OUT, NR 1 ENGINE OIL PRESSURE DECREASED BELOW 35 PSI, OIL TEMPERATURE CLIMBED TO ABOVE 120 DEGREES. FOLLOWED ACM PROCEDURES SHUT DOWN NR 1 ENGINE. REPLACED OIL FILTER, FOUND LOOSE B-NUT ON OIL LINE TO LOW PRESSURE SWITCH AND TRANSMITTER. SECURED LINE, REPLACED CHAFED OIL LINE FROM FUEL OIL COOLER. RAN NR 1 ENGINE AT TAKE OFF POWER. OIL TEMPERATURE AND OIL PRESSURE CHECKED NORMAL, LEAK CHECK OK IAW MM 79-32-0 AND 79-34-0. (X) 2 L 7 3 4F A3WE 1998073100016 19980731 00016 CE 1998 7 31 RU3A98004 1 19980506 A 5330 SKIN LEAR 60 60LEAR 5170707 CE FUSELAGE LIGHTNING STRIKE A RU3A K NONE O OTHER AP APPROACH 1 SW 21 54 009 GJT - N4 ON ILS WAS HIT BY LIGHTNING ON 5-6-98. POST-FLIGHT INSPECTION WAS CONDUCTED BY THE MAINTENANCE FACILITY AT GJT AND A SPECIAL FLIGHT PERMIT WAS ISSUED 5-12-98 FROM GJT TO OKC. THE AIRCRAFT WAS INSPECTED AND REPAIRED IAW THE AFTER LIGHTNING STRIKE INSPECTION IN THE APPROVED MM (CARD NR 0302). A TOTAL OF FIVE RIVETS WERE REPLACED AND THE AIRCRAFT RE TURNED FOR SERVICE ON 5-15-98. REF: RU3A09002 - ORIGINAL. (X) 2 L 7 2 4F RT A10CE 1998073100017 19980731 00017 EU 1998 7 31 REXA98100 1 19980613 A 2612 899253 FIRE DETECTOR SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A REXA F E ACTIVATE FIRE EXT. ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 327PX 340A059 RIGHT ENGINE FIRE INDICATION RIGHT ENGINE SHUT DOWN IN-FLIGHT. REMOVED AND REPLACED RIGHT FIRE DETECTION FIRE OVER HEAT DETECTOR. (X) 2 L 7 2 4T RT A52EU 1998073100018 19980731 00018 EU 1998 7 31 REXA98101 1 19980604 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO BAY MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 110PX 340A023 CARGO LIGHT CAME ON IN-FLIGHT. REMOVED AND REPLACED CARGO SMOKE DETECTOR. (X) 2 L 7 2 4T RT A52EU 1998073100019 19980731 00019 EU 1998 7 31 REXA98102 1 19980607 A 2612 FIRE LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A REXA K NONE N FALSE WARNING CR CRUISE 1 SO 25 327PX 340A059 RIGHT FIRE DETECT FAIL ON CWP CAME ON IN-FLIGHT FOR ABOUT 5 MINUTES THEN WENT OUT. CLEANED AND INSPECTED FIRE DETECT LO OP. NO CHAFING NOTED. (X) 2 L 7 2 4T RT A52EU 1998073100020 19980731 00020 NM 1998 7 31 P2EA98108 1 19980525 A 3230 TORSION LINK BOEING 737 737222 1384473 NM NLG BROKEN A P2EA C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CE 05 208AU 19547 MDW - FLT 424 - ON INITIAL TAKEOFF ROLL, ENCOUNTERED NOSE WHEEL SHIMMY, ABORTED TAKEOFF. AIRCRAFT STOPPED AND WAS UNABL E TO TAXI BACK TO GATE DUE TO STEERING PROBLEM. AIRCRAFT TOWED BACK TO GATE. FOUND LOWER TORSION LINK BROKEN. REPLACE D UPPER AND LOWER TORSION LINKS AND LINK PINS, LINK APEX BOLT, BOTH NLG WHEEL ASSYS, NLG PISTON POSITION SPRING CARTRIDG E AND CRANKSHAFT ASSY, PER MM 32-21-31, S/B 737-32-1033, S/B 737-32-1129 AND MM 32-45-21. (M) 2 L 7 2 4F A16WE 1998073100021 19980731 00021 NM 1998 7 31 P2EA98110 1 19980617 A 5320 ANGLE BOEING 737 737222 1384473 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION PER WORK CARD NR J2C-46-5223C, A CRACK WAS NOTED ON BEAM NR 8 AFT ANGLE OF THE L 1 DOOR. THE CRACK WAS 4 INCHES LONG. INSTALLED ANGLE REPAIR PER SRM 51-40-3 FIG 1. REF: COOPESA W.O. NR LI-0630, VAM 100-240, 208SDA007. (X) 2 L 7 2 4F A16WE 1998073100022 19980731 00022 NM 1998 7 31 P2EA98109 1 19980611 A 5311 FRAME BOEING 737 737222 1384473 NM BS 400 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK, ROUTINE INSPECTION PER CARD NR J2C 51 2525, NOTED CRACK ON FUSELAGE FRAME AT BS 400 BETWEEN STR 25 AND 26 LT. CRACK WAS .250 INCH IN LENGTH. CRACK WS REPAIRED IAW SRM 53-10-4 FIG 6. COOPESA W.O. NR L1-0630, NR VAM 1 00-225, 208SDA006. (X) 2 L 7 2 4F A16WE 1998073100023 19980731 00023 NM 1998 7 31 USAASB98150 1 19980616 A 2131 CONTROLLER BOEING 737 7372B7 1384560 NM LT PACK MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 266AU 22878 PHL - FLT 993 - AIRCRAFT DEPARTED PHL WITH THE LEFT PACK ON MEL DUE TO A LEFT PACK TRIP OFF LIGHT THAT WOULD NOT RESET. ON CLIMB-OUT OF PHL, AIRCRAFT WOULD NOT PRESSURIZE. CREW WENT THROUGH CHECK LIST WITH NO HELP. FLIGHT RETURNED TO FIE LD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PRESSURIZED AIRCRAFT ON GROUND W ITH APU AND RIGHT PACK TO 6 PSI DIFFERENTIAL. CHECKS GOOD WITH NO EXTERNAL LEAKS. CLEARED LEFT PACK MEL BY RUNNING LEF T PACK ON GROUND FOR ONE HOUR. PRESSURIZED AIRCRAFT ON GROUND. OPERATIONAL CHECK OF LEFT PACK GOOD. (X) 2 L 7 2 4F A16WE 1998073100024 19980731 00024 1998 7 31 AALA981187 4 19980616 A 2565 D30545203 SLIDE AIRCRUISERS AIRBUS 300 A300B4605R 3930308 EU R2 DOOR DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7083A 0085 645 BOS - DURING OVERNIGHT MAINTENANCE R2 DOOR HARD TO ARM. SNAPS ON SLIDE WHERE BUSTLE ATTACHES BROKEN AND INTERFERRING WI TH SLIDE ARMING OPERATION. REPLACED R2 DOOR SLIDE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998073100025 19980731 00025 WP 1998 7 31 AALA981163 1 19980609 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1155-1211 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 428AA 49340 TUL - AFT CARGO DOOR BEAM CORRODED VERTICAL AND HORIZONTAL SURFACES. REMOVED CORROSION PER SRM 51-10-03, PERFORMED THIC KNESS CHECK, MANUFACTURED AND INSTALLED DOUBLER TO STA 1174 - STA 1209 PER SRM'S 53-10-00-16, 53-10-00-8, AND 53-10-00-3 . TST: 35,019.40 HOURS. CYCLES: 19,379. (X) 2 L 7 2 4F A6WE 1998073100026 19980731 00026 NM 1998 7 31 AALA981194 1 19980618 A 5511 SPAR CAP BOEING 727 727223 1384074 NM RT HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 707AA 22464 TUL - RIGHT HORIZONTAL STABILIZER T/E SPAR CAP HAS CORROSION UNDER DOUBLER, BETWEEN NR 6 AND NR 7 ELEVATOR HINGES. TREA TED, PRIMED, AND PAINTED AREA, INSTALLED FILLER AND DOUBLER IAW SRM 55-10-6 AND ESO 11-6-97, DATED 6-3-98. TST: 46,450 . CYCLES: 24,085. (X) 2 L 7 3 4F A3WE 1998073100027 19980731 00027 EU 1998 7 31 AALA981157 1 19980608 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU CARGO BAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - ROLLER TRACK NR 6 IS CORRODED ON THE OUTBOARD FLANGE. REPLACED ROLLER TRACK PER AARD 51-10-00-3. TAT: 27,196 HOU RS. CYCLES: 10,843. (X) 2 L 7 2 4F RT A35EU 1998073100028 19980731 00028 EU 1998 7 31 AALA981183 1 19980612 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU BS 58-60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - ROLLER TRACK NR 6 CORRODED UNDER FORWARD GUIDE ROLLER AT FRAME 60 JUST AFT OF FORWARD DOOR JAM. REPLACED DAMAGED ROLLER TRAY PER SRM 51-72-10-0. TST: 27,196 HOURS. CYCLES: 10,843. (X) 2 L 7 2 4F RT A35EU 1998073100029 19980731 00029 EU 1998 7 31 AALA981151 1 19980605 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 27 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - NR 6 ROLLER TRAY CORRODED ON INBOARD PANEL LANDING AT FR 27. REPLACED ROLLER TRAY SECTION BETWEEN FRAME BAYS PER SRM 53-10-15. TST: 27,196.14 HOURS. CYCLES: 10,843. (X) 2 L 7 2 4F RT A35EU 1998073100030 19980731 00030 EU 1998 7 31 AALA981150 1 19980605 A 5347 TRACK AIRBUS 300 A300B4605R 3930308 EU BS 38 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - THRE IS CORROSION ON THE ROLLER TRACK FLANGE ON TRACK NR 5 AT FR 38.1. TRIMMED OUT CORRODED PIECE AND INSTALLED R EPAIR DOUBLER PER 53-10-15-2. TREATED AND PAINTED PER 51-21-00. TST: 27,196.14 HOURS. CYCLES: 10,843. (X) 2 L 7 2 4F RT A35EU 1998073100031 19980731 00031 EU 1998 7 31 AALA981153 1 19980608 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - CORROSION ON ROLLER TRAY NR 6 AT FR 58. REPLACED ROLLER TRAY NR 6 FROM FR C58 TO C55 PER 51-72-10-0, 51-21-10-0 M M, 51-23-10 MM. TST: 27,196.14 HOURS. CYCLES: 10,843. (X) 2 L 7 2 4F RT A35EU 1998073100032 19980731 00032 EU 1998 7 31 AALA981119 1 19980603 A 5347 GUIDE AIRBUS 300 A300B4605R 3930308 EU BS 33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - SPRING LATCH GUIDE, CENTER ROLLER TRAY AT FR 33, HAS CORROSION UNDER LATCH AREA BETWEEN TRAYS 3/4. REMOVED CORROS ION PER SRM 51-74-10-2. INSTALLED NEW FITTING SPRING LATCH GUIDE, TREATED, PRIMED AREA, PAINTED PER 51-21-00. TST: 27, 196.14 HOURS. CYCLES: 10,843. (X)(X) 2 L 7 2 4F RT A35EU 1998073100033 19980731 00033 NM 1998 7 31 F3LA98087 1 19980529 A 5730 SKIN BOEING 737 737201 1384454 NM WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 3321 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ABOVE NR 2 LEADNG EDGE PYLON. MAINTENANCE REMOVED DAMAGED AREA, FABRICA TED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-10-1, 51-30-2, AND 57-30-4. CYCLES: 2,451.0. (X) 2 L 7 2 4F A16WE 1998073100034 19980731 00034 EU 1998 7 31 AALA981120 1 19980603 A 5347 ROLLER TRAY AIRBUS 300 A300B4605R 3930308 EU BS 56/58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - NR 1 ROLLER TRAY CORRODED AT FRAMES 56 AND 58. REPLACED ROLLER TRAY SECTIONS PER SRM 51-72-10-0. TST: 27,196.14 H OURS. CYCLES: 10,843. (X) 2 L 7 2 4F RT A35EU 1998073100035 19980731 00035 NM 1998 7 31 F3LA98088 1 19980529 A 5230 FRAME BOEING 737 737201 1384454 NM CARGO DOOR CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 2451 19421 PAE - DURING C-CHECK INSPECTION REPORTED CRACK IN FORWARD CARGO DOOR LOWER FORWARD FRAME IN OUTBOARD RADIUS OF LATCH ARM . MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1100 AND MM 52-31-0. CYCLES: 2,451. (X) 2 L 7 2 4F A16WE 1998073100036 19980731 00036 NM 1998 7 31 EIAA980215 1 19980629 A 3230 RETRACT MECH BOEING 747 747273C 1384896 NM LT MLG MALFUNCTIONED A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 470EV 20653 HKG - LOG PAGE: F08753 - AFTER TAKEOFF, LEFT WING GEAR FAILED TO GO UP, RECYCLED GEAR ONCE, NO HELP. RETURNED TO HKG. RIGGING CHECK ACCOMPLISHED WITH NO ADJUSTMENTS PERFORMED, ALL TENSION WITHIN LIMITS PER MM 32-31-00. RETRACTION AND EX TENSION CHECKS CARRIED OUT AND NO FAULTS FOUND. RETURNED AIRCRAFT TO SERVICE WITH NO FURTHER PROBLEMS REPORTED. (X) 2 L 7 4 4F A20WE 1998073100037 19980731 00037 WP 1998 7 31 98ZZZX2500 1 19980324 A 5711 59121241 SPAR CAP DOUG DC9 DC951 3022051 WP WS 229-235 CRACKED B ERKR K NONE O OTHER IN INSP/MAINT 1 WP 07 679HA 39781 47662 DURING C-CHECK INSPECTION, DISCOVERED A CRACK ON THE FRONT SPAR UPPER CAP (PN 5912124-1) OF THE LEFT HAND WING FLAP LOCA TED BETWEEN XF229.00 AND SF235.00. REPAIRED BY TRIMMING OUT THE CRACK, NDT INSPECTED, FABRICATED AND INSTALLED NESTED S TEEL ANGLE WITH HILOKS. REPAIRED IAW EVERGREEN AIR CENTER - ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N679HA-57-002-EA C. (X) 2 L 7 2 4F RT A6WE 1998073100038 19980731 00038 WP 1998 7 31 98ZZZX2501 1 19980324 A 5711 5911305502 SPAR CAP DOUG DC9 DC951 3022051 WP WS 111.5 MISDRILLED B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 679HA 39781 47662 DURING C-CHECK, INSPECTION, DISCOVERED NUMEROUS OVERSIZE FASTENER HOLES IN THE REAR LOWER RIGHT HAND SPAR CAP FORWARD LO WER FLANGE AT XRS111.5 (PN 5911305-502) AND LOWER AFT WING SKIN/STRINGERS (P/N 3919224-2). REPAIRED BY OVERSIZE FASTENE R HOLES, FABRICATING AND INSTALLING REPAIR BUSHINGS, INTERNAL REPAIR DOUBLER, REPAIR ANGLES, REPAIR STRAPS, AND MODIFIED SHEAR CLIPS. REPAIRS ARE CONSIDERED TEMPORARY FOR ONE YEAR PENDING DTA/NDT REVIEW. REPAIRED IAW EVERGREEN AIR CENTER - ENGINEERING CHANGE/REPAIR AUTHROZIATION NR N679HA-57-008-EAC. (X) 2 L 7 2 4F RT A6WE 1998073100039 19980731 00039 WP 1998 7 31 98ZZZX2502 1 19980324 A 5320 59529653 DOUBLER DOUG DC9 DC951 3022051 WP COCKPIT WINDOW MISDRILLED B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 679HA 39781 47662 DURING C-CHECK INSPECTION, DISCOVERED OVERSIZE FASTENER HOLES COMMON TO THE LEFT HAND AND RIGHT HAND FLIGHT COMPARTMENT, OVERHEAD WINDOW, UPPER AFT CORNER OUTER RETAINERS (PN 5952965-3/-4) AND UNDERLYING STRUCTURE. REPAIRED BY CLEANING UP DISCREPANT HOLES TO THE MINIMUM DIAMETER, HFEC NDT INSPECTED, DISCARDED AND INSTALLED NEW DOUBLERS (PN 5952965-3/-4) AND STEEL DOUBLERS (PN 5952965-27/-28) WITH OVERSIZE DRAWING TYPE FASTENERS, FABRICATING AND INSTALLING ALUMINUM REPAIR BUS HINGS FOR ALUMINUM PARTS USING RETAINER WASHERS WITH DRAWING TYPE FASTENERS. REPAIRED IAW EVERGREEN AIR CENTER ENGINEE RING CHANGE/REPAIR AUTHORIZATION NR N679HA-53-10-EAC. (X) 2 L 7 2 4F RT A6WE 1998073100040 19980731 00040 WP 1998 7 31 98ZZZX2503 1 19980324 A 5512 5922578501 SKIN DOUG DC9 DC951 3022051 WP HORIZ STAB MISDRILLED B ERKR K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 07 679HA 39781 47662 DURING C-CHECK INSPECTION DISCOVERED OVERSIZED FASTENER HOLE IN THE HORIZONTAL STABILIZER UPPER AFT SKIN PANELS/STRINGER S (PN 5922578-501) REFERENCED IN DAC SB 55-42R1 AND AD 96-10-11. REPAIRED BY OVERSIZING HOLE, SPLIT-SLEEVE COINING THE OVERSIZED HOLE, FABRICATING AND INSTALLING A REPAIR BUSHING AND STANDARD DIAMETER HILOK. REPAIRED IAW EVERGREEN AIR CEN TER - ENGINEERING CHANGE/REPAIR AUTHORIZATION NR N679HA-55-001-EAC. (X) 2 L 7 2 4F RT A6WE 1998073100041 19980731 00041 WP 1998 7 31 GTIA9800067 1 19980612 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 969ML 47268 DTW - FLT 558 - EMERGENCY CEILING LIGHTS, FIRST FIVE OR SO, NEED NEW LIGHT BULBS. RELAMPED, OPERATIONAL CHECK GOOD. (X ) 2 L 7 2 4F A6WE 1998073100042 19980731 00042 WP 1998 7 31 GTIA9800069 1 19980614 A 3350 FUSE DOUG DC9 DC932 3022066 WP CABIN BLOWN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12505 45788 DTW - TAIL CONE CATWALK EMERGENCY TRACK LIGHTING INOPERATIVE. INSTALLED FUSE IN BATTERY PACK, OPERATIONAL CHECK GOOD. ( X) 2 L 7 2 4F A6WE 1998073100043 19980731 00043 WP 1998 7 31 GTIA9800068 1 19980615 A 3350 60030431 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 182 1941 47326 GTIA - EMERGENCY EXIT LIGHT ABOVE VENTRAL DOOR WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK. EMERGENCY EXIT LIGHT ABOVE VENTRAL DOOR WILL NOT EXTINGUISH. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A6WE 1998073100044 19980731 00044 NM 1998 7 31 GAIA9862A 1 19980615 A 3610 CLAMP BOEING 727 727224 1384076 NM CABIN FAILED A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 69739 20667 MKE - AFTER DEPARTING JUST PRIOR TO FLAP RETRACTION, THE NR 1 FIRE WARNING CAME ON. FIREWARNING LIGHT WENT OUT AFTER NR 1 THROTTLE WAS RETARDED. AIRCRAFT RETURNED TO MKE AND MADE UNEVENTFUL LANDING. FOUND 8TH STAGE BLEED VALVE, AFT CLAMP UNSECURED. SECURED CLAMP AS REQUIRED. FIRE WARNING SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE WITH NO FURTHER DISCREPANCIES NOTED. (X) 2 L 7 3 4F A3WE 1998073100045 19980731 00045 NM 1998 7 31 GAIA9861A 1 19980612 A 2751 18129932 INDICATOR BOEING 727 727224 1384076 NM TE FLAPS STICKS A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 69739 20667 AFTER FLAPS RETRACTED, RT INBOARD FLAP ASYMMETRY SPLIT. ONE IS AT 15 DEGREES, AND THE OTHER AT ZERO. ON APPROACH, FLAP S LOCKED OUT AT 4 DEGREES ON INBOARD AFTER FLAPS MOVED TO 15 DEGREES. INBOARD FLAPS RE-SYNCED AND FLAPS OPERATED NORMAL LY. AIRCRAFT MADE AN UNEVENTFUL LANDING AT MSP. REMOVED AND REPLACED INBOARD FLAP INDICATOR AND PERFORMED ADJUST/TEST PER B727 MM 27-51-0. FLAP SYSTEM TEST GOOD WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998073100046 19980731 00046 CE 1998 7 31 98ZZZX2504 1 19980603 A 3260 1013841379 SWITCH BEECH 1900 1900D 1154162 CE GEAR HANDLE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 838CA 11093 297 UE34 GEAR HANDLE LIGHT INTERMITTENT. GEAR HANDLE SWITCH ASSY FAILURE. REPLACED GEAR HANDLE SWITCH ASSY. (X) 2 L 7 2 4T RT A24CE 1998073100047 19980731 00047 1998 7 31 98ZZZX2505 4 19980608 A 3418 1143800511 TRANSDUCER SAFEFLIGHT BEECH 1900 1900D 1154162 CE LT WING FAILED A JJBA K NONE L NO TEST IN INSP/MAINT 1 EA 01 854CA 13311 5972 513 UE60 STALL WARNING WILL NOT TEST. FAILED LIFT TRANSDUCER. REPLACED LIFT TRANSDUCER. 2 L 7 2 4T RT A24CE 1998073100048 19980731 00048 CE 1998 7 31 98ZZZX2506 1 19980608 A 3231 1148100461 CAM BEECH 1900 1900D 1154162 CE LT GEAR DOOR FAILED A JJBA K NONE J WARNING INDICATION IN INSP/MAINT 1 EA 01 837CA UE16 LEFT NLG WOULD NOT RETRACT FOLLOWING TAKEOFF. LEFT GEAR DOOR CAM ASSY FAILED. REPLACED LT GEAR DOOR CAM ASSY. OPS SAT ISFACTORY. (X) 2 L 7 2 4T RT A24CE 1998073100049 19980731 00049 NM 1998 7 31 F3LA98123 1 19980705 A 3350 BATTERY PACK BOEING 737 7372L9 1384497 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 271FL 8 22734 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EXTERIOR MOUNTED FORWARD ENTRY AND FORWARD SERVICE DOOR ESCAPE SLIDE LI GHTS INOPERATIVE. MAINTENANCE REPLACED M 571 BATTERY PACK PER MM 33.51.71 AND CHECKED OKAY. (X) 2 L 7 2 4F RT A16WE 1998073100050 19980731 00050 NM 1998 7 31 98ZZZX2507 1 19980628 A 3350 362624 LIGHT BOEING 737 737222 1384473 NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 737AP 19956 NR 14 INCH EMERGENCY FLOOR TRACK LIGHT STRIP INOPERATIVE. REPLACED NR 14 INCH FLOOR LAMP ASSEMBLY (FLEX) STRIP IAW B737 MM 33-50. (X) 2 L 7 2 4F A16WE 1998073100051 19980731 00051 WP 1998 7 31 ASAA9880118 1 19980630 A 5210 HOOK DOUG DC9 DC982 3022082 WP PASSENGER DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 SEA - PRIOR TO DEPARTURE OF FLIGHT 356, CREW REPORTED THE L1 DOOR WOULD NOT RELEASE FROM THE LATCHED OPEN POSITION. REP LACED THE L1 DOOR HOLD OPEN HOOK AND SHAFT AND OPERATED NORMALLY. ACFT TT: 36,222 HOURS. ACFT TC: 23,242. (X) 2 L 7 2 4F A6WE 1998073100052 19980731 00052 WP 1998 7 31 ASAA9880121 1 19980705 A 5610 CAM DOUG DC9 DC983 3022083 WP COCKPIT OUT OF TRACK A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 963AS 53077 LAX - AFTER ARRIVAL OF FLIGHT 180, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOWS WAS DIFFICULT TO OPEN. FOUND WINDOW FOLLOWER CAM OUT OF TRACK. POSITIONED CAM INTO TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1998073100053 19980731 00053 WP 1998 7 31 ASAA9880114 1 19980626 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - PRIOR TO DEPARTURE OF FLT 119, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED WIRING IN FLOOR TRACK AT ROW 3 AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1998073100054 19980731 00054 WP 1998 7 31 ASAA9880115 1 19980626 A 5210 LATCH DOUG DC9 DC983 3022083 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 974AS 53450 SFO - PRIOR TO DEPARTURE OF FLIGHT 420, CREW REPORTED THE L1 DOOR WOULD NOT LATCH OPEN. LUBRICATED THE DOOR HOLD OPEN L ATCH MECHANISM AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1998073100055 19980731 00055 1998 7 31 ASAA9880116 4 19980626 A 2565 SLIDE DOUG DC9 DC983 3022083 WP R1 DOOR MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OAK - DURING C-CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (X) 2 L 7 2 4F RT A6WE 1998073100056 19980731 00056 WP 1998 7 31 ASAA9880117 1 19980626 A 5311 9911812101 FRAME DOUG DC9 DC983 3022083 WP BS 1485 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 OAK - DURING C-CHECK, A 2 INCH CRACK WAS FOUND IN FUSELAGE CANTED FRAME AT STA 1485 ADJACENT TO THE AFT ENTRANCE STAIR D OOR JAMB RT SIDE AT THE VENTRAL STAIR ACTUATOR MOUNT BRACKET ATTACH POINT. REMOVED DAMAGED AREA AND SPLICED IN NEW MATE RIAL IAW ASA E.A. 5310-01588. (X) 2 L 7 2 4F RT A6WE 1998073100057 19980731 00057 WP 1998 7 31 ASAA9880110 1 19980624 A 5610 WINDOW DOUG DC9 DC983 3022083 WP RT COCKPIT STIFF A ASAA K NONE O OTHER TX TAXI/GRND HDL 1 NM 01 963AS 53077 SEA - AFTER ARRIVAL OF FLT 339, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WAS DIFFICULT TO OPEN. ADJUSTED THE WINDOW MECHANISM AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1998073100058 19980731 00058 NE 1998 7 31 G6OA023 2 19980702 A 7321 665038062826 ECU DOUG DC10 DC1030F 3023504 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE LIGHTNING STRIKE A G6OA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 27 600GC 46965 517837 DURING CLIMB-OUT FROM CDG, THE FLIGHT CREW REPORTED LIGHTNING STRIKE. NR 1 ENGINE PARAMETERS WERE OUTSIDE THE NORMAL PA RAMETERS. NR 1 ENGINE WAS SHUT DOWN, FUEL DUMPED IAW AOM VOL 1 AND RETURNED TO CDG. GROUND MAINTENANCE ACCOMPLISHED LI GHTNING STRIKE INSPECTION IAW MM 05-53-00. NO DAMAGE NOTED. PERFORMED POWER ASSURANCE CHECK. AS A RESULT, REPLACED TH E MEC IAW MM 73-20-01. (X) 2 L 7 3 4F 4 F RT A22WE E23EA 1998073100059 19980731 00059 NM 1998 7 31 EIAA980211 1 19980619 A 2612 21562B FIRE DETECTOR BOEING 747 747273C 1384896 NM CARGO BAY MALFUNCTIONED A EIAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 471EV 20651 FJR - LOG PAGE: F80971 - ON CLIMB-OUT, FORWARD LOWER CARGO COMPARTMENT FIRE LIGHT ILLUMINATED. NO CARGO LOADED. NO SM OKE OR FIRE OBSERVED. RETURNED TO FJR. REPLACED FORWARD LOWER CARGO AFT SMOKE DETECTOR, AND OPS CHECKED SYSTEM PER MM 26-14-02. (X) 2 L 7 4 4F A20WE 1998073100060 19980731 00060 NE 1998 7 31 EIAA980218 2 19980629 A 7200 ENGINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 4 FAILED A EIAA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 NM 09 479EV 19898 HNL - LOG PAGE: F40104 - DURING CLIMB-OUT APPROXIMATELY 20 MINUTES INTO FLIGHT, NR 4 ENGINE OIL QUANTITY SLOWLY DECREAS ED TO ZERO, ENGINE SHUT DOWN. PER EIA PROCEDURES, ENGINE WINDMILLED AT APPROXIMATELY 9 PSI OIL PRESSURE FOR 13 MINUTES, AND REDUCED TO 3 PSI FOR APPROXIMATELY 30 MINUTES. ENGINE SN 662617 TO BE REMOVED FROM AIRCRAFT. AWAITING SHOP REPORT . (X) 2 L 7 4 4F 4 F A20WE E20EA 1998073100061 19980731 00061 NE 1998 7 31 EIAA980217 2 19980629 A 7261 693905 LINE BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE LOOSE A EIAA E A ENGINE SHUTDOWN UNSCHED LANDING K J Y FLUID LOSS WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 NM 09 479EV 19898 HNL - LOG PAGE: F40104 - DURING CLIMB-OUT, NR 4 ENGINE OIL QUANTITY SLOWLY DECREASED TO ZERO, ENGINE SHUT DOWN PER EIA PROCEDURES, ENGINE WINDMILLED AT APPROXIMATELY 20 PSI OIL PRESSURE FOR 35 MINUTES. SERVICED ENGINE OIL AND MOTORED, FOU ND OIL DRAINING FROM OVERFLOW DRAIN AND 1 EACH LINE. REPLACED OIL CAP AND TIGHTENED OIL LINE TO GEARBOX. ACCOMPLISHED WINDMILL INSPECTION PER MM 72-00-00. CHECKED OIL FILTER AND CHIP DETECTORS, NO FINDINGS IN EITHER. RETURNED AIRCRAFT T O SERVICE. (X) 2 L 7 4 4F 4 F A20WE E20EA 1998073100062 19980731 00062 EA 1998 7 31 98ZZZX2508 1 19980619 A 6120 8190024 SWITCH DHAV DHC6 DHC6300 EA RT ENGINE FAILED A ASWA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 07 140SA 267 SHORTLY AFTER LEAVING RUNWAY ON TAKEOFF FROM GRAND CANYON, AZ, LEFT PROPELLER FEATHERED UNCOMMANDED BY CREW. FLIGHT ABO RTED AND A SAFE LANDING WAS MADE AT VALLE AIRPORT, AZ. MAINTENANCE REPLACED DEFECTIVE TORQUE PRESSURE SWITCH ON RIGHT E NGINE. 1 H 7 2 3T A9EA 1998073100063 19980731 00063 WP 1998 7 31 GTIA9800070 1 19980622 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 DTW - EMERGENCY FLOOR TRACK LIGHTING 2 BULBS INOPERATIVE. REPLACED 2 BULBS IN EMERGENCY FLOOR TRACK LIGHTING. OPERATIO NAL CHECK GOOD. (X) 2 L 7 2 4F A6WE 1998073100064 19980731 00064 1998 7 31 GTIA9800073 4 19980623 A 2565 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR SEPARATED A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 132NK 47202 DTW - FLT 172 - RIGHT GALLEY PACK SLIDE OFF. INSTALLED L2 DOOR SLIDE PACK IAW DC9 MM 25-61-0. RII ACCOMPLISHED. (X) 2 L 7 2 4F A6WE 1998073100065 19980731 00065 1998 7 31 GTIA9800074 4 19980626 A 2565 SLIDE DOUG DC9 DC931 3022065 WP PASSENGER DOOR SEPARATED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 934ML 47526 TPA - FLT 341 - PASSENGER ENTRANCE DOOR SLIDE PACK FELL OFF. RE-INSTALLED PASSENGER DOOR ENTRANCE SLIDE PACK IAW DC9 MM 25. (X) 2 L 7 2 4F A6WE 1998073100066 19980731 00066 WP 1998 7 31 GTIA9800075 1 19980626 A 3350 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 17535 47111 OKC - FLT 902 - EMERGENCY FLOOR TRACK BROKE BETWEEN ROWS 11-15. REPAIRED FLOOR TRACK AND LIGHTING IAW DC-9 MM 33-51. O PERATIONAL CHECKS GOOD. (X) 2 L 7 2 4F A6WE 1998073100067 19980731 00067 1998 7 31 MALA976166 4 19980714 A 3442 6227337001 RT UNIT SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 15 99XJ 099 DURING FLIGHT RADAR INOP, PAINTS WHOLE SCREEN. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED WEATHER RADAR R/T. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998073100068 19980731 00068 NM 1998 7 31 UPS98227202 1 19980709 A 5753 651926920 TRACK BOEING 727 72731C 1384011 NM LT TE FLAP DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, LT WING INB FLAP INB FLAP TRACK DAMAGED DUE TO SHEARED DEAD WEIGHT ROLLER. REMOVED NR 4 FLAP TRACK I AW MM 27-51-31. INSTALLED NEW TRACK IAW MM 27-51-31. 2 L 7 3 4F A3WE 1998073100069 19980731 00069 NM 1998 7 31 UPS98227203 1 19980721 A 3350 96310322 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 946UP 19721 EMER EXIT LIGHT ON AFT OVERWING DOOR, RIGHT SIDE WILL NOT TEST. REPLACED EMER EXIT LIGHT ASSY CHECKS OK, PN ON 96-3-103 2-2 SN ON 1033 PN OFF 96-3-1032-2 SN OFF 1012. 2 L 7 3 4F A3WE 1998073100070 19980731 00070 NM 1998 7 31 UPS98227204 1 19980721 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 ALL EMER EXIT LIGHTS INOP. REPLACED EMERG EXIT LIGHT BATTERY PACKS. ALL LIGHTS CHECK OK FOR SERVICE. 2 L 7 3 4F A3WE 1998073100071 19980731 00071 WP 1998 7 31 UPS98827205 1 19980713 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 50 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 814UP 46090 CORROSION ON FUSELAGE BELLY APPROX STA 50, CORROSION ON CIRCUM. STA 70, CRACK ON CIRCUM STA 70 STRINGER 34. REPLACED B ELLY SKIN TEMP. REPAIR ACCOMPLISHED ON CIRCUM FRAME IAW E/O DC8531010158A. 2 L 7 4 4F RT 4A25 1998073100072 19980731 00072 EU 1998 7 31 QXEA9800966 1 19980627 A 5312 BULKHEAD WEB FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - AT FRONT PRESSURE BULKHEAD WEB AND UPPER AREA ALONG HORIZONTAL BEAM VIII BETWEEN OUTBOARD RIVETS 8-9 UPPER ROW AND 9-10 LOWER ROW. THERE IS A 10 MM CRACK. REPAIRED IAW FOKKER SRM 53-07-18, PAGE 35, FIGURE 13, 51-31-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 1998073100073 19980731 00073 EU 1998 7 31 QXEA9800967 1 19980630 A 5320 RIVETS FOKKER F28 F28MK4000 4990810 EU NR 2 WINDOW POST CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - AT AFT SIDE OF FRAME 1890 AT NR 2 WINDOW POST RIGHT SIDE THERE ARE 3 RIVETS WITH CRACKS FROM HEAD ON FRAME CLIP. R EPAIRED IAW FOKKER SRM 51-31-01 AND 51-30-02. 2 L 7 2 4F RT A20EU 1998073100074 19980731 00074 EU 1998 7 31 QXEA9800968 1 19980627 A 2510 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - BASE OF COCKPIT PEDESTAL CORRODED BELOW STAB SERVO DRIVE SPROCKET. REPAIRED IAW FOKKER SRM 51-10-4 AND EA 4-53-48 1. 2 L 7 2 4F RT A20EU 1998073100075 19980731 00075 EU 1998 7 31 QXEA9800969 1 19980627 A 2510 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - LIGHT CORROSION ON CENTER PEDESTAL FRAME ADJACENT TO CO-PILOTS LEFTHAND RUDDER PEDAL FOOTREST. REPAIRED IAW FOKKE R SRM 51-10-4, PAGE 8, PARAGRAPH 3 A-C AND EA 4-53-481. 2 L 7 2 4F RT A20EU 1998073100076 19980731 00076 EU 1998 7 31 QXEA9800970 1 19980624 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - CORROSION AROUND FASTENER RECEPTACLE ON CENTER FLOOR SUPPORT BEAM BETWEEN LEFTHAND INBOARD AND RIGHTHAND INBOARD S EAT TRACK BEAMS. REPAIRED IAW HORIZON AIR EA 4-53-476. 2 L 7 2 4F RT A20EU 1998073100077 19980731 00077 EU 1998 7 31 QXEA9800971 1 19980624 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - CORROSION ON FUSELAGE SKIN UNDER LOWER ATC ANTENNA. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 4. 2 L 7 2 4F RT A20EU 1998073100078 19980731 00078 EU 1998 7 31 QXEA9800972 1 19980625 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - CORROSION ON FUSELAGE SKIN UNDER NR 2 VHF COMM ANTENNA. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 4. 2 L 7 2 4F RT A20EU 1998073100079 19980731 00079 EU 1998 7 31 QXEA9800973 1 19980618 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 MISDRILLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - FORWARD CARGO BAY FRAME 5305 HAS 2 LARGE HOLES DRILLED IN FRAME AND NO FASTENERS ABOVE STRINGERS 70 AND 71. REPAI RED IAW HORIZON AIR EA 4-53-471. 2 L 7 2 4F RT A20EU 1998073100080 19980731 00080 EU 1998 7 31 QXEA9800974 1 19980615 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - FRAME CLIP CRACKED FROM EDGE THROUGH FIRST RIVET HOLE AT FRAME 13815B BETWEEN STRINGERS 73 AND 72. REPAIRED IAW F OKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998073100081 19980731 00081 EU 1998 7 31 QXEA9800975 1 19980615 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13018 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - CRACK EMITTING FROM RIVET HOLE AT FRAME CLIP AT FRAME 13018 BETWEEN STRINGERS 2 AND 3. REPAIRED IAW FOKKER SRM 51 -31-01. 2 L 7 2 4F RT A20EU 1998073100082 19980731 00082 EU 1998 7 31 QXEA9800976 1 19980629 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - EXTRUDED SKIN AND NUTPLATE MOST FORWARD POSITION LOCATED IN THE AFT CARGO DOOR APERATURE WHERE DOOR HINGE ATTACHES . REPAIRED IAW FOKKER SRM 51-30-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 1998073100083 19980731 00083 EU 1998 7 31 QXEA9800977 1 19980709 A 5320 PANEL FOKKER F28 F28MK4000 4990810 EU CARGO COMPT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - FORWARD CARGO BAY ALUMINUM REINFORCING PANELS HAVE SURFACE CORROSION. INSTALLED REINFORCEMENT PANEL. REMOVED COR ROSION AND TREATED. 2 L 7 2 4F RT A20EU 1998073100084 19980731 00084 EU 1998 7 31 QXEA9800978 1 19980625 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX- INTERGRANLAR CORROSION FOUND AT FRAME 13815B BETWEEN STRINGER 1 AND 74 ON FRAME SPLICE. REPAIRED IAW HORIZON EA 4- 53-477, FOKKER SRM 51-31-01 AND 51-30-02. 2 L 7 2 4F RT A20EU 1998073100085 19980731 00085 EU 1998 7 31 QXEA9800979 1 19980615 A 5230 RIB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 487US 11238 PDX - FORWARD CARGO DOOR HAS RIB WITH FIGURE 8 HOLE. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 52-30-00, PAGE 3 IT EM 175. 2 L 7 2 4F RT A20EU 1998073100086 19980731 00086 EU 1998 7 31 QXEA9800980 1 19980615 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 487US 11238 PDX - FORWARD CARGO PIT DOOR INNER SKIN REQUIRES REPLACEMENT DUE TO MISDRILLED RIVET HOLE AND VARIOUS DENTS. REPAIRED I AW FOKKER SRM 52-30-00, PAGE 3, ITEM 420 AND EO 4-52-05E. 2 L 7 2 4F RT A20EU 1998073100088 19980731 00088 NM 1998 7 31 98FDEA00464 1 19980723 A 2612 894120 FIRE LOOP BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE DAMAGED A FDEA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 25 203FE 22925 NR 1 ENGINE FIRE LIGHT AND BELL ON INTERMITTENTLY, ALL ENGINE INDICATIONS NORMAL. DETECTOR NR 1 INOP LIGHT ON CIRCUIT B REAKER PANEL ON AS WELL. PULLED ENGINE DETECTION A NR 1 CIRCUIT BREAKER SYSTEM NORMAL. *S/D* FOUND NR 1 ENG FIRE LOOP DAMAGED IN 2 PLACES CAUSING LOOP TO SHORT. REMOVED AND REPLACED NR 1 ENG FIRE LOOP. TEST AS PER M/M 26-11-01. RAN NR 1 ENG AT HIGH POWER AS PRECAUTION, NO FALSE WARNINGS. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998073100089 19980731 00089 NM 1998 7 31 98FDEA00465 1 19980723 A 5315 65163169 FLOORBEAM BOEING 727 72721C 138400M NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 CORROSION (C53-224-06) IN SEVERAL AREAS ON THE UPPER CHORD OF THE BS 344 FLOORBEAM FROM LBL 63 TO RBL 21. REMOVED, FABR ICATED AND INSTALLED FLOORBEAM UPPER CHORD AT BS 344, LBL 65 TO RBL 65 IAW FEDEX SRDM 27-53-007. 2 L 7 3 4F A3WE 1998073100090 19980731 00090 NM 1998 7 31 98FDEA00466 1 19980723 A 5320 651597514 FITTING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR0479 STA-PAE - CRACK INDICATION NOTED IN HOLE NR 1 OF ROW 3, BS 870 RIGHT TERMINAL FITTING. REPAIRED HOLE NR 1 OF RO W 3, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911. 2 L 7 3 4F A3WE 1998073100091 19980731 00091 NM 1998 7 31 98FDEA00467 1 19980723 A 5320 651597513 FITTING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR0420 STA-PAE - CRACKS NOTED BY NDI IN HOLE NR 1 AND NR 2 OF ROW 2 BS 870 LEFT TERMINAL FITTING. REPAIRED LEFT TERMIN AL FITTING AT BS 870 HOLE NR 1 AND NR 2 OF ROW 2 PER EA NR 7-5310-39910. 2 L 7 3 4F A3WE 1998073100092 19980731 00092 NM 1998 7 31 98FDEA00468 1 19980723 A 5320 651597513 FITTING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR 0421 STA-PAE - MECHANICAL DAMAGE NOTED IN HOLES NR 1 THROUGH 5 OF ROW 3 BS 870 LEFT TERMINAL FITTING. REPAIRED MECH DAMAGED HOLES IN LEFT TERMINAL FITTING AT BS 870 HOLE NR 1 THROUGH NR 5 OF ROW 3 PER EA NR 7-5310-39910. 2 L 7 3 4F A3WE 1998073100093 19980731 00093 NM 1998 7 31 98FDEA00469 1 19980723 A 5320 651597514 FITTING BOEING 727 72725C 138400H NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR 0478 STA-PAE - VISUAL DAMAGE, CRACK AND CORROSION INDICATION NOTED IN HOLES NR 1 THROUGH 5 OF ROW 2 BS 870 RIGHT TER MINAL FITTING. REPAIRED HOLES NR 1 - 5 OF ROW 2, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911. 2 L 7 3 4F A3WE 1998073100094 19980731 00094 GL 1998 7 31 98UAL900209 2 19980522 A 7260 9609M89P11 GEAR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL GEARBOX FAILED A UALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT NR NOT REPORTED 1 WP 29 1847U 32113 48263 451424 NR 2 ENGINE FLAMED OUT AND WAS SHUT DOWN. FLIGHT CONTINUED TO SFO UNDER AMBER ALERT. ENGINE WAS CHANGED FROM AIRCRAFT. UPON TEAR DOWN OF THE INLET GEARBOX, A MAIN BEVEL GEAR WAS FOUND FAILED. 2 L 7 3 4F 4 F A22WE E23EA 1998073100095 19980731 00095 WP 1998 7 31 98UAL900315 1 19980710 A 2121 FAN DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 1844U 48260 ELECTRICAL BURNING SMELL AND SMOKE REPORTED AT ROW 15. ALSO A GRINDING NOISE HEARD. NR 4 RECIRCULATING FAN TRIPPED OFF AND THE ODOR DISSIPATED. THE FAN WAS RESET AND FLIGHT CONTINUED TO IAD. 2 L 7 3 4F 4 F A22WE E23EA 1998073100096 19980731 00096 NM 1998 7 31 98UAL900316 1 19980712 A 3397 W2076L509320 WIRE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 160UA 21237 NA DOOR 1 RIGHT EMERGENCY SLIDE LIGHT STAYS ON WITH EMERGENCY LIGHT SWITCH IN THE ARM POSITION. FOUND WIRE W2076-L5093-20 BROKEN AT DOOR SILL. WIRE PULLED OUT OF CONDUIT ABOVE SILL. REPLACED SLIDE LIGHT HARNESS AT DOOR 1R, OPS CHECKED OK. 2 L 7 4 4F 4 F A20WE E20EA 1998073100097 19980731 00097 NM 1998 7 31 98UAL900317 1 19980712 A 2910 NAS1611020 O-RING BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT ENGINE TORN A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 571UA 26681 LANDED MCI UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC FLUID. *S/D* FLUID LEAKING AT TORN O-RING FOUND ON ENGINE H YDRAULIC LINE QUICK DISCONNECT FITTING. REPLACED O-RING. 2 L 7 2 4F 4 F RT A2NM E17NE 1998073100099 19980731 00099 NM 1998 7 31 98UAL900319 1 19980711 A 2120 AIR DISTRIBUTION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7292U 21570 FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE IN FIRST CLASS CABIN. SMELL WENT AWAY WHEN GALLEY POWER WAS TURNED OFF. 2 L 7 3 4F 4 F A3WE E2EA 1998073100102 19980731 00102 NM 1998 7 31 98UAL900322 1 19980711 A 2613 655966810 OVERHEAT DET BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT WING/BODY FAILED A UALA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 WP 29 386UA 24661 RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. *S/D* FOUND RIGHT WING LEADING EDGE OVERHEAT DETECTOR (M1204) SHORTED. REPLACED THE DETECTOR AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998073100104 19980731 00104 NM 1998 7 31 98UAL900324 1 19980714 A 3260 ACCESSORY UNIT BOEING 655281123 BOEING 737 737222 1384473 NM PWA JT8 JT8D7B 52053 NE E/E COMPT FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 9009U M00008 19047 BOTH TRANSPONDERS ARE INOPERATIVE. *S/D* THE CAUSE FOR THE APPARENT FAILURE OF BOTH TRANSPONDERS IS BELIEVED TO HAVE B EEN AN AIR/GROUND SENSING PROBLEM AS IT WAS ALSO REPORTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE. ALSO, NOTED BY ENGINE ERING, THE AIRCRAFT OFF TIME WAS NOT REPORTED BY ACARS. TWO DAYS LATER, THE AIRCRAFT WAS REPORTED INTERMITTENTLY IN GRO UND MODE IN FLIGHT. THE LANDING GEAR ACCESSORY UNIT WAS REPLACED AND THE PROBLEM HAS NOT REOCCURRED. 2 L 7 2 4F 4 F A16WE E2EA 1998073100105 19980731 00105 NM 1998 7 31 98UAL900325 1 19980714 A 2130 PRESSURIZATION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7293U 21571 CABIN KEPT CLIMBING TO 12000, ACTUAL ALTITUDE 27000. TRIED STANDBY AND MANUAL AC-DC. NO HELP. OUTFLOW VALVE CLOSED AL L THE TIME. DESCENDED AND RETURNED TO OAK. 2 L 7 3 4F 4 F A3WE E2EA 1998073100106 19980731 00106 NM 1998 7 31 98UAL900326 1 19980708 A 2130 PRESSURIZATION BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 WP 29 7284U 21562 RAPID DECOMPRESSION LOSS. DESCENDED TO 9000 FEET AND DIVERTED TO LNK. 2 L 7 3 4F 4 F A3WE E2EA 1998073100107 19980731 00107 NM 1998 7 31 98UAL900327 1 19980705 A 2751 BAC10613173 TRANSMITTER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT TE FLAP MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7443U 21897 RETURNED TO BOI DUE TO FLAPS SHOWED ASYMMETRY PROBLEM UPON RETRACTION. CHECKED VISUALLY AND CONFIRMED. *S/D* REPLACED LEFT HAND OUTBOARD TRAILING EDGE FLAP TRANSMITTER. 2 L 7 3 4F 4 F A3WE E2EA 1998073100108 19980731 00108 NM 1998 7 31 98UAL900328 1 19980706 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7279U 21557 EMERGENCY LIGHT LEFT HAND OVERWING AND AFT AIR STAIR INOPERATIVE. *S/D* REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1998073100109 19980731 00109 NM 1998 7 31 98UAL900329 1 19980713 A 3350 900542U1 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7292U 21570 BOTH THE RIGHT HAND OVERWING EMERGENCY EXIT LIGHTS STAY ON WITH POWER OFF THE AIRCRAFT. *S/D* REPLACED M1086 MOD, AND BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1998073100110 19980731 00110 NM 1998 7 31 98UAL900330 1 19980716 A 2421 IDG SUNDSTRAND MR24113 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 FAILED A UALA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 WP 29 564UA C0744 26666 CREW DIVERTED TO DEN DUE TO LOSS OF NUMBER 2 GENERATOR. *S/D* THE IDG STATOR ASSEMBLY HAD SHIFTED WHICH CAUSED A CRACK IN A CONTROL CURRENT TRANSFORMER CONNECTION INTERNAL TO THE GENERATOR. REPLACED NUMBER 2 INTEGRATED DRIVE GENERATOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1998073100111 19980731 00111 WP 1998 7 31 MWEA98813 1 19980722 A 2560 113313 SLIDE DOUG DC9 DC932 3022066 WP FWD GALLEY FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 204ME 47680 THE GALLEY SLIDE FELL OFF. MAINTENANCE RESECURED THE GALLEY SLIDE. 2 L 7 2 4F A6WE 1998073100112 19980731 00112 WP 1998 7 31 DLL17981507 1 19980720 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 765DA 193H1206 ON LAYOVER, CHECK FOUND AFT LEFT HAND OVERHEAD EMERGENCY LIGHTS WON'T TEST. REPLACED ASSOCIATED BATTERY PACK AT 2L AND ADDITIONAL PACK AT 3R. ALL EMER LIGHTS TEST GOOD. 2 L 7 3 4F A23WE 1998073100113 19980731 00113 NM 1998 7 31 DL72W981509 1 19980720 A 5350 SKIN BOEING 727 727247 138408F NM DORSAL FIN CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 .25 INCH CRACK DORSAL FIN SKIN LEFT SIDE BELOW PANEL 9523. REPAIRED PER M/M 54-30-0 PG 804. 2 L 7 3 4F A3WE 1998073100114 19980731 00114 NM 1998 7 31 DL73E981510 1 19980717 A 5330 6545768237 SKIN BOEING 737 737247 138448D NM BS 470 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 377DL 23604 FUSELAGE SKIN C1 DOOR SURROUND, LOWER AFT CORNER. REPAIR FOR SKIN GOUGE. THE LOWER AFT CORNER OF THE C1 DOOR CUTOUT WA S DAMAGED BY GROUND EQUIPMENT. THE SKIN ASSY AND UNDERLYING BEAR STRAP WAS DENTED AND TORN. THE DAMAGE WAS TRIMMED A WAY AND HFEC INSPECTED. THE DAMAGE WAS EVALUATED AS ACCEPTABLE FOR TIME-LIMITED SERVICE PER ER/A 365274-14. 2 L 7 2 4F A16WE 1998073100115 19980731 00115 NM 1998 7 31 DL72S981511 1 19980721 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 9960 21074 LEFT WING OVERWING AFT EMERGENCY LIGHT ASSY BULB BLINKS INTERMITTENTLY. REPLACED BATTERY PACK. OPS CKS NORMAL. 2 L 7 3 4F A3WE 1998073100116 19980731 00116 WP 1998 7 31 DLL14981513 1 19980607 A 5210 MECHANISM 1282T100017 LKHEED 1011 1011385115 5265015 WP PAX DOOR OUT OF ADJUST A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 740DA 193C1244 COUNTER BALANCE REPLACE, WAS SLOW TO OPERATE IN MANUAL, (EMERGENCY MODE). S/N NR OFF 1095, S/N NR ON 1194. 2 L 7 3 4F A23WE 1998073100117 19980731 00117 NM 1998 7 31 DL72S981521 1 19980619 A 5753 652163262 DOUBLER BOEING 727 727232 1384082 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 REPAIR DOUBLER IS CRACKED AT LWR AFT SPAR 21 AND 35 FROM I/B END. THIS DAMAGE WAS REPAIRED PER M/M 57-52-0, FIG 802. T HIS DAMAGED WAS RECORDED ON N/R 007474 AND 007475. 2 L 7 3 4F A3WE 1998073100118 19980731 00118 NM 1998 7 31 DL72S981522 1 19980618 A 5753 652163262 SKIN BOEING 727 727232 1384082 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 416DA 21258 COVE SKIN IS CRACKED 32 FROM I/B END. THIS DAMAGED WAS RECORRED ON SHOP N/R 007470 AND REPAIRED PER M/M 57-52-0 FIG 809 . 2 L 7 3 4F A3WE 1998073100119 19980731 00119 NM 1998 7 31 DL72W981525 1 19980701 A 5320 FORMER BOEING 727 727247 138408F NM BS 1070 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 CORROSION TASK C53-113-01, CORROSION CRACK AFT SIDE OF FORMER 1070 JUST OUTBD OF STR 28 LT. REPAIRED PER SRM 53-10-4 F IG 27. 2 L 7 3 4F A3WE 1998073100120 19980731 00120 NM 1998 7 31 DL72W981526 1 19980630 A 5240 FRAME BOEING 727 727247 138408F NM SERVICE DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 R-1 DOOR AFT FRAME CRACKED .5 VISIBLE, JUST ABOVE AFT LOWER STOP CASTING. REPAIRED PER M/M 52-12-0 FIG 804. 2 L 7 3 4F A3WE 1998073100121 19980731 00121 NM 1998 7 31 DL72W981527 1 19980722 A 5320 WEB BOEING 727 727247 138408F NM BS 1227 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 .125 INCH CRACK ON LIGHTING HOLE FOR AIRSTAIR CUTOUT AT STA 1227 LEFT. REPAIRED PER M/M 53-11-00 PG 828. 3/16 IN CRACK ON LIGHTNING HOLE FOR AIRSTAIR CUTOUT AT STA 1238 LEFT. REPAIRED PER M/M 53-11-00 PG 828. .3/8 INCH CRACK ON LIGHTNIN G HOLE FOR AIRSTAIR CUTOUT AT STA 1228 LEFT. REPAIRED PER M/M 53-11-00 PG 832. 2 L 7 3 4F A3WE 1998073100122 19980731 00122 NM 1998 7 31 DL72W981529 1 19980722 A 5530 STRINGER BOEING 727 727247 138408F NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 291WA 22109 FOUND DURING C2 LETTER CHECK, CRACK AT FASTENER, VERT STAB STA 180.6 STR 10 LEFT SIDE AND CRACK AT FASTENER, VERT STAB STA 180.6 STR 9 LT SIDE. BOTH REPAIRED PER ERA 365310-14. 2 L 7 3 4F A3WE 1998073100123 19980731 00123 WP 1998 7 31 VJ9800232 1 19980712 A 5320 1A350781 SUPPORT DOUG DC9 DC932 3022066 WP BS 408-427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 LEFT LOWER GIL LINER SUPPORT IS CORRODED BETWEEN STA 408-427. REMOVED CORROSION, OUT OF LIMITS, DEPTH GAUGE A-2042, IAW DC9 SRM 51-10-3, 53-01 FIG 1 (.045 MATERIAL LOSS). FABBED NEW SECTION 7075-0-.063 (1A-35078-1). HEAT TREATED TO T-6 I AW DC-9 SRM 53-21-0 FIG 2A, LOCATED, DRILLED, PRIMED AND INSTALLED NEW SECTION IAW DC-9 SRM 51-10-4 51-30-2, AND 51-10-3 . 2 L 7 2 4F A6WE 1998073100124 19980731 00124 WP 1998 7 31 VJ9800233 1 19980717 A 5347 29559781200 CARGO TRACK DOUG DC9 DC932 3022066 WP BS 270-390 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 FWD CARGO LT STA 270-390 HAS SURFACE CORROSION. MECH REMOVED CORROSION 100 PERCENT BEYOND LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED CARGO TIE DOWN TRACK MATERIAL 2955978-1200 102.5 BY 1 IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1998073100125 19980731 00125 EU 1998 7 31 JBXA980044 1 19980707 A 2612 SENSOR FOKKER F28 F28MK0100 4990807 EU APU BAY MALFUNCTIONED A JBXA F ACTIVATE FIRE EXT. J WARNING INDICATION LD LANDING 1 SO 05 107ML 11450 AIRCRAFT WAS LANDING AT MCO WHEN THE CREW RECEIVED APU FIRE WARNING. DISPATCHED THE BOTTLE. UPON LANDING, MAINTENANCE INSPECTED THE AIRCRAFT, NO SIGNS OF FIRE. APU WAS PLACED ON DMI. (X) 2 L 7 2 4F RT 1998073100126 19980731 00126 EU 1998 7 31 JBXA980045 1 19980723 A 2612 FIRE LOOP FOKKER F28 F28MK0100 4990807 EU APU MALFUNCTIONED A JBXA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SO 05 109ML 11485 APU FIRE INDICATION (L) MFDU ON DESCENT. USED APU FIRE BOTTLE. INSPECTED APU COMPARTMENT, NO EVIDENCE OF ANY FIRE. ASS IGNED TO DMI 05457 PER MEL 49-00-1 - APU INOPERATIVE. (X) 2 L 7 2 4F RT 1998073100127 19980731 00127 EU 1998 7 31 JBXA980043 1 19980704 A 3242 50118091 BRAKE FOKKER F28 F28MK0100 4990807 EU RT MLG OVERHEATED A JBXA C ABORTED TAKEOFF B M J SMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 05 132ML 2492 DEC950289 11321 AFTER LANDING IN RDU AND TAXIING TO THE GATE, THE FLIGHT CREW NOTICED NR 3 BRAKE TEMPERATURE HAVING A HIGH INDICATION. G ROUND CREW NOTICED SMOKE COMING FROM BRAKE AREA. RAMP USED EXTINGUISHERS ON THE BRAKE, NO FLAME WAS VISIBLE. MAINTENAN CE PERFORMED INSPECTION AFTER BRAKE OVERHEAT ON RT GEAR. THE BRAKE QD WAS IN THE OFF POSITION. PART TOTAL CYCLES: 1,8 85. 2 L 7 2 4F RT 1998073100128 19980731 00128 WP 1998 7 31 CALA9801316 1 19980722 A 3350 L2019115 LIGHT LUMINATOR DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 71828 49488 INSPECTION FOUND EMERGENCY LIGHT IN FIRST CLASS CABIN AT STA 252 INOPERATIVE. THE LIGHT ASSEMBLY WAS REPLACED. 2 L 7 2 4F A6WE 1998073100129 19980731 00129 NM 1998 7 31 CALA9801317 1 19980702 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 400/760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A 1 CRACK IN FLOORBEAM SUPPORT AT STA 400-420, BL 0. A 2 CRACK WAS FOUND IN FLOORBEAM SUPPORT AT STA 7 60, BL 0. THE FLOOR SUPPORT AT STA 400-420 WAS REMOVED IAW SRM 51-30-2. A NEW FLOOR SUPPORT WAS FABRICATED AND INSTALL ED IAW SRM 51-10-2, 51-10-1, 51-40-5, AND 51-30-2. THE CRACKED AREA OF FLOOR SUPPORT AT STA 760 WAS CUT OUT. AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-6. 2 L 7 3 4F A3WE 1998073100130 19980731 00130 WP 1998 7 31 CALA9801318 1 19980721 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 237/803 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND SEAT TRACKS CORRODED AT STA 237 RT O/B AND STA 803-845, LBL 48. THE CORRODED SECTIONS OF SEAT TRACKS W ERE CUT OUT. NEW SEAT TRACKS, SPLICES, AND PLATES WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 4F AND 51-30-1. 2 L 7 2 4F A6WE 1998073100131 19980731 00131 WP 1998 7 31 CALA9801319 1 19980720 A 5230 FITTING DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .375 INCH CRACK IN AFT CARGO DOOR NR 2 BEAM AFT END FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51- 30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998073100132 19980731 00132 WP 1998 7 31 CALA9801320 1 19980721 A 5210 L30825502 MOTOR DOUG DC10 DC1010 3022110 WP R-3 DOOR INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68041 73459 46900 THE R-3 DOOR FAILED PNEUMATIC CHECK. THE R-3 DOOR AIR MOTOR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1998073100133 19980731 00133 WP 1998 7 31 CALA9801321 1 19980721 A 5320 RAIL DOUG DC9 DC982 3022082 WP BS 1060-1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND RT TIEDOWN RAIL CORRODED AT STA 1060-1155. A NEW TIEDOWN RAIL WAS INSTALLED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1998073100134 19980731 00134 WP 1998 7 31 CALA9801322 1 19980722 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 636/1155 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND CORROSION ON MID BAG BIN Z BEAM AT THRESHOLD, STA 636-693. CORROSION WAS ALSO FOUND ON AFT BAG BIN Z B EAM AT THRESHOLD STA 1155-1212. REPAIRS WERE INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998073100135 19980731 00135 WP 1998 7 31 CALA9801323 1 19980723 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 229-237 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 229-237 ABOVE CUSP LINE. A REPAIR WAS INSTALLED IAW ECRA 5330-02687. 2 L 7 2 4F A6WE 1998073100136 19980731 00136 NM 1998 7 31 CALA9801324 1 19980722 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 907-947 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND RT INBOARD SEAT TRACK CORRODED AT STA 907-947. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-00 -52, FIGURE 204. 2 L 7 2 4F RT A16WE 1998073100137 19980731 00137 NM 1998 7 31 CALA9801325 1 19980722 A 3350 60B5003737 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14024 20534 INSPECTION FOUND EMERGENCY LIGHT IN CEILING ABOVE ROW 23 HKL INOPERATIVE. THE EMERGENCY LIGHT ASSEMBLY AND BATTERY WERE REPLACED IAW MM 33-51-07, PAGE 201-202, ITEM 3. 2 L 7 4 4F A20WE 1998073100138 19980731 00138 WP 1998 7 31 CALA9801326 1 19980723 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A CALA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 09 16894 49393 THE NLG DID NOT RETRACT AFTER TAKEOFF. BOTH THE RED NOSE GEAR LIGHT AND YELLOW GEAR DOOR OPEN LIGHT REMAINED ILLUMINATE D. THE FAULT WAS ACCOMPANIED BY LOUD WIND NOISE AND VIBRATION. THE GEAR WAS CYCLED AND THE NOSE GEAR RETRACTED WITH GO OD INDICATIONS. THE FLIGHT WAS CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. THE GEAR WAS SWUNG SEVERAL TIMES WIT H NO FAULTS NOTED. THE NLG STRUT WAS SERVICED IAW MM 32-21-02. 2 L 7 2 4F A6WE 1998073100139 19980731 00139 NM 1998 7 31 CALA9801327 1 19980723 A 3213 654610217 TORSION LINK BOEING 737 737291 138448W NM LT MLG SHEARED A CALA K NONE O OTHER LD LANDING 1 SW 09 17252 72307 20362 THE LT MLG LOWER TORSION LINK SHEARED AFTER LANDING IN EWR. THE LT MLG LOWER TORSION LINK WAS REMOVED AND REPLACED. IN ADDITION, THE SHIMMY DAMPER AND BOTH INBOARD AND OUTBOARD GUIDE BRACKETS WERE REPLACED. A GEAR SWING WAS PERFORMED AND OPERATION CHECKED GOOD. 2 L 7 2 4F A16WE 1998073100140 19980731 00140 WP 1998 7 31 CALA9801328 1 19980722 A 3350 EMSE299A BATTERY PACK ENGMAGNETICS DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 37078 46926 THE EMERGENCY TRACK LIGHTING FAILED TEST. THE MID GALLEY BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GO OD. 2 L 7 3 4F A22WE 1998073100141 19980731 00141 WP 1998 7 31 CALA9801329 1 19980723 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A 1.5 CRACK IN AFT PRESSURE BULKHEAD ATTACH T-ANGLE AT STA 996, LONGERON 15L. THE T-ANGLE WAS REMOVED AND REPLACED IAW SRM 53-03, FIGURE 37A. 2 L 7 2 4F A6WE 1998073100142 19980731 00142 WP 1998 7 31 CALA9801330 1 19980723 A 5311 BELTFRAME DOUG DC9 DC932 3022066 WP BS 180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND E/E BELTFRAME CORRODED AT BS 180 BETWEEN LONGERON 24 AND 25L. THE CORRODED SECTION WAS CUT OUT AND A D OUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 4. 2 L 7 2 4F A6WE 1998073100143 19980731 00143 WP 1998 7 31 CALA9801331 1 19980723 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND CRACKS ON AFT PRESSURE BULKHEAD SKIN SPLICE AT BS 996, LONGERONS 7-10L. AN EXTERNAL DOUBLER, INTERNAL FINGER DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW EA 5361-01001. 2 L 7 2 4F A6WE 1998073100144 19980731 00144 WP 1998 7 31 CALA9801332 1 19980724 A 5311 BELTFRAME DOUG DC9 DC932 3022066 WP BS 148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND BELTFRAME CORRODED AT STA 148, LONGERON 26L. THE CORROSION WAS CUT OUT AND A BELTFRAME REPAIR WAS INST ALLED IAW SRM 53-03, FIGURE 2. 2 L 7 2 4F A6WE 1998073100145 19980731 00145 NM 1998 7 31 CALA9801333 1 19980724 A 5741 BOTTLE PIN BOEING 727 727227 1384078 NM LT WING/FUS CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND LT FORWARD WING TO FUSELAGE BOTTLE PIN BLEEDING RUST AT SEALANT AREA. THE BOTTLE PIN WAS REMOVED AND R EPLACED IAW MM 57-41-1. 2 L 7 3 4F A3WE 1998073100146 19980731 00146 NM 1998 7 31 CALA9801334 1 19980724 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 967 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND CORROSION AROUND FASTENER HOLES ON FLOORBEAM AT STA 967, RBL 27.5 TO LBL 41.5. A REPAIR STRAP WAS INST ALLED IAW SRM 53-00-51, FIGURE 203. 2 L 7 2 4F RT A16WE 1998073100147 19980731 00147 NM 1998 7 31 CALA9801335 1 19980723 A 2133 40631997201AA OUTFLOW VALVE BOEING 737 737524 1384721 NM AFT/TAIL MALFUNCTIONED A CALA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 SW 09 11641 3049 28902 THE AIRCRAFT PRESSURE COULD NOT BE CONTROLLED IN AUTO, ALTERNATE, OR MANUAL AFTER TAKEOFF FROM MEX. THE OXYGEN MASKS WE RE DEPLOYED AND THE AIRCRAFT WAS RETURNED TO MEX WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AFT OUTFLOW VALVE AND BOTH CABIN PRESSURE CONTROLLERS. MAINTENANCE FOUND THAT THE 02 GENERATORS IN LAVS AND SEAT ROWS 1 AB, 3AB, 3EF, AND 19L HAD NOT FIRED. ALL O2 GENERATORS WERE REMOVED AND REPLACED AND THE O2 MASKS WERE REPACKED. 2 L 7 2 4F RT A16WE 1998073100148 19980731 00148 SO 1998 7 31 COMA9810162 1 19980714 A 3246 300604 WHEEL BFGOODRICH 314461 EMB 120 EMB120 3260201 SO MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 156 1262 MECHANIC REMOVED WHEEL ASSEMBLY FROM A/C DUE TO LOW PRESSURE. WHEEL SHOP INSPECTED WHEEL AND FOUND INBOARD HALF WAS CRA CKED AT THE BOTTOM OF A KEY INSERT BOSS AREA. CRACK IS APPROXIMATELY .5 INCH LONG. INBOARD WHEEL ASSEMBLY HAS BEEN REM OVED FROM SERVICE AND SENT TO BFG. 2 L 7 2 4T RT A31SO 1998073100149 19980731 00149 SO 1998 7 31 COMA9810163 1 19980721 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 258CA 120247 EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998073100150 19980731 00150 EA 1998 7 31 COMA9860185 1 19980721 A 3397 WIRE CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 SOME OF THE EMERGENCY FLOOR LIGHTS ARE INOP. SECURED LOOSE WIRING CONNECTOR AT TRACK LIGHTING. 2 L 7 2 4F RT A21EA 1998073100151 19980731 00151 EA 1998 7 31 COMA9860186 1 19980721 A 2720 CONTROLS CNDAIR CL600 CL6002B19 EA RUDDER SYST MALFUNCTIONED A COMA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 01 920CA 7022 AFTER TAKEOFF, AIRCRAFT YAWED LT/RT AT SPEEDS ABOVE 210 KTS. INSPECTED RUDDER SYSTEM, FOUND NO DEFECTS. A/C FLIGHT CHE CK SATISFACTORY. 2 L 7 2 4F RT A21EA 1998073100152 19980731 00152 NM 1998 7 31 SWAA981355 1 19980713 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED C1 CHECK, FOUND L1 DOOR VERTICAL EMERGENCY EXIT LIGHT HAS SOME BULBS INOP. REMOVED AND REPLACED LIGHT BULBS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100153 19980731 00153 NM 1998 7 31 SWAA981356 1 19980713 A 5220 WINDOW BOEING 737 7373H4 1384600 NM LT EMER EXIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED C1 CHECK, FOUND LT EMERGENCY EXIT HATCH INNER PANE CRACKED. REMOVED AND REPLACED LIGHT INNER PANE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100154 19980731 00154 NM 1998 7 31 SWAA981357 1 19980713 A 5320 RACK BOEING 737 7373H4 1384600 NM E/E COMP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED C1 CHECK, FOUND CRACKED E1 RACK RT FWD STANCHION. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100155 19980731 00155 NM 1998 7 31 SWAA981358 1 19980713 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL AND L ANGLE CRACKED AT BS 295 LBL 53 WL 252. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100156 19980731 00156 NM 1998 7 31 SWAA981359 1 19980713 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 295 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D CHECK, FOUND STRINGER GOUGED AT BS 295 STR 11 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100157 19980731 00157 NM 1998 7 31 SWAA981360 1 19980713 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294-312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D CHECK, FOUND DENTED UPPER HALF OF INTERCOSTAL AT BS 294-312, RBL 44, WL 208. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998073100158 19980731 00158 NM 1998 7 31 SWAA981361 1 19980713 A 3320 LIGHT BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D CHECK, FOUND NO SMOKING LIGHT OUT ON AFT WALL BY AFT ENTRY DOOR. REPAIRED WIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100159 19980731 00159 NM 1998 7 31 SWAA981362 1 19980713 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 336SW 23940 DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR WEB AT BS 178, RBL 25-29, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100160 19980731 00160 NM 1998 7 31 SWAA981363 1 19980713 A 2560 SLIDE BOEING 737 7373Q8 1384670 NM PAX DOOR REQD SERVICE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING WALKAROUND CHECK, FOUND FRONT ENTRY DOOR SLIDE NEEDS TO BE REPACKED. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100161 19980731 00161 1998 7 31 SWAA981364 4 19980713 A 2565 SLIDE BOEING 737 7372T4 1384492 NM PAX DOOR LOW PRESSURE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING WALKAROUND CHECK, FOUND REAR ESCAPE SLIDE PRESS LOW. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998073100162 19980731 00162 1998 7 31 SWAA981365 4 19980713 A 2565 61620468 SLIDE BOEING 737 7373H4 1384600 NM SERVICE DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING WALKAROUND CHECK, FOUND FWD SVC DOOR HAS NO EMERGENCY EXIT SLIDE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100163 19980731 00163 NM 1998 7 31 SWAA981366 1 19980713 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 967-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED C4 CHECK, FOUND CORRODED AFT LOWER LOBE 5-27L, ON STRINGER FROM BS 967-1006. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998073100164 19980731 00164 NM 1998 7 31 SWAA981367 1 19980713 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED .25D CHECK, FOUND CRACKED L ANGLE LT SIDE OF 3-2 RACK AT BS 312. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998073100165 19980731 00165 NM 1998 7 31 SWAA981368 1 19980713 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 685SW 22731 DURING SCHEDULED C4 CHECK, FOUND DOOR UPLATCH INTERCOSTAL CRACKED. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998073100166 19980731 00166 NM 1998 7 31 SWAA981369 1 19980713 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM BS 727-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23401 DURING SCHEDULED 1/2D CHECK, FOUND LT TRANSITION ANGLE CORRODED AT BS 727D-727E.; BS 727E-747; BS 747-767; AND 727-727B. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100167 19980731 00167 NM 1998 7 31 SWAA981370 1 19980713 A 5720 STRAP BOEING 737 7373Q8 1384670 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23401 DURING SCHEDULED 1/2D CHECK, FOUND STRAP FOR I/B PYLON PANEL CRACKED. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100168 19980731 00168 NM 1998 7 31 SWAA981371 1 19980713 A 5720 CHANNEL BOEING 737 7373Q8 1384670 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23401 DURING SCHEDULED 1/2D CHECK, FOUND U CHANNEL SUPPORT FOR I/B PYLON PANEL CRACKED. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100169 19980731 00169 NM 1998 7 31 SWAA981372 1 19980713 A 5720 ANGLE BOEING 737 7373Q8 1384670 NM LT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23401 DURING SCHEDULED 1/2D CHECK, FOUND PYLON SUPPORT ANGLE FOR PANEL WORN JUST BELOW HYD LINES NR 3 JACKSCREW CANOE FAIRING. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100171 19980731 00171 NM 1998 7 31 SWAA981374 1 19980714 A 5240 HINGE BOEING 737 7372H4 138448C NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED 1/4 D CHECK, FOUND AFT SERVICE DOOR UPPER HINGE CUTOUT HAS .25 INCH CRACK AT TOP FWD CORNER. REPAIRED PER SWA RA NR 1-253-1852. 2 L 7 2 4F A16WE 1998073100172 19980731 00172 NM 1998 7 31 SWAA981375 1 19980714 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 336 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED 1/4 D CHECK, FOUND SKIN CRACKED AT BS 336, STR 17L, WITH EXTENSION APPROX 1/4 BEYOND FASTENER HOLE. RE PAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998073100173 19980731 00173 NM 1998 7 31 SWAA981376 1 19980714 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 988 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED 1/4 D CHECK, FOUND CORRODED Z ANGLE AT BS 988. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998073100174 19980731 00174 NM 1998 7 31 SWAA981377 1 19980714 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR UPLOCK INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100175 19980731 00175 NM 1998 7 31 SWAA981378 1 19980714 A 5240 SKIN BOEING 737 7373G7 1384595 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED EXTERNAL SKIN FWD SERVICE DOOR, AFT CORNER, RBL 66.5 WL 210. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998073100176 19980731 00176 NM 1998 7 31 SWAA981379 1 19980714 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CORRODED AROUND NUTPLATE HOLES UPPER CHORD FLOORBEAM AT BS 967, RBL 5, 28 + 37, WL 208; AND DOUBLE HOLE AT BS 947, WL 208, LBL 42. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100177 19980731 00177 NM 1998 7 31 SWAA981380 1 19980714 A 5320 SHEAR WEB BOEING 737 7373G7 1384595 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CORRODED SHEAR WEB AT BS 1016, LBL 27 WL 208; AND 500A-500B, LBL 65, WL 208. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100178 19980731 00178 NM 1998 7 31 SWAA981381 1 19980714 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 991 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR WEB AT BS 991, RBL 45, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100179 19980731 00179 NM 1998 7 31 SWAA981382 1 19980714 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 312-328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL AT BS 312-328, LBL 47, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100180 19980731 00180 NM 1998 7 31 SWAA981383 1 19980714 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 294.5-312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 294.5-312, RBL 12, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100181 19980731 00181 NM 1998 7 31 SWAA981384 1 19980714 A 5315 FLOORBEAM BOEING 737 737317 138447P NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOORBEAM AT BS 986, RBL 32; BS 986, RBL 36; AND BS 986, RBL 40. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100182 19980731 00182 NM 1998 7 31 SWAA981385 1 19980715 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 790 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN 0.15 INCH LONG AT BS 790 LBL 2. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998073100183 19980731 00183 NM 1998 7 31 SWAA981386 1 19980715 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN .25 INCH LONG AT BS 420 RBL 3. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998073100184 19980731 00184 NM 1998 7 31 SWAA981387 1 19980715 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN 0.15 INCH LONG AT BS 480 RBL 2. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998073100185 19980731 00185 NM 1998 7 31 SWAA981388 1 19980715 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SKIN 0.15 INCH LONG AT BS 520 RBL 1. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998073100186 19980731 00186 NM 1998 7 31 SWAA981389 1 19980719 A 3230 RETRACT MECH BOEING 737 7373H4 1384600 NM LANDING GEAR MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 383SW 26589 AIR RETURN, DUE TO LANDING GEAR WOULD NOT RETRACT NORMALLY AFTER TAKEOFF. OVERRIDE WAS REQUIRED TO MOVE GEAR HANDLE TO UP. PRESSURIZATION WAS NORMAL AND THERE WAS NO TAKEOFF WARNING HORN WHEN THE FLAPS WERE RETRACTED. EXTENSION WAS NORMA L. AIRCRAFT MADE AN UNEVENTFUL LANDING. ADJUSTED GROUND/AIR SENSE TELEFLEX CABLE AS PER BOEING MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998073100187 19980731 00187 NM 1998 7 31 SWAA981390 1 19980717 A 7921 749965 OIL COOLER BOEING 737 7372H4 138448C NM NR 2 ENGINE FAILED A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 085SW 22826 AIR RETURN, DUE ON CLIMB-OUT APPRX 17,000 NR 2 ENG OIL TEMP REACHED 125 DEG, QRH ITEMS COMPLETED DISPATCH ADVISED. AIRC RAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED FUEL OIL COOLER ON NR 2 ENG AND LK CHECK PER BOEING MM. OIL TEMP OPS CK NORMAL. 2 L 7 2 4F A16WE 1998073100188 19980731 00188 NM 1998 7 31 SWAA981391 1 19980715 A 3350 LIGHTS BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702SW 22054 DURING SCHEDULED RON CHECK, FOUND BOTH AFT EXTERIOR SLIDE EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED EMERG BATTERY PACK PER BOEING MM. EMERG LIGHTS OPS NORMAL. 2 L 7 2 4F A16WE 1998073100189 19980731 00189 NM 1998 7 31 SWAA981392 1 19980715 A 5320 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO DOOR FRAME INSIDE DOOR FWD OF AFT I/B STOP. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100190 19980731 00190 NM 1998 7 31 SWAA981393 1 19980715 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED C4 CHECK, FOUND CORRODED BELL FRAME CLIP AT BS 986 STR 17R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100191 19980731 00191 NM 1998 7 31 SWAA981394 1 19980715 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED BC4 CHECK, FOUND CRACKED FWD CARGO INTERCOSTAL. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100192 19980731 00192 NM 1998 7 31 SWAA981395 1 19980715 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 294.5-303.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED INTERCOSTAL WEB AT LBL 62, STR 16, WL 216, BETWEEN BS 294.5-303.9; AND BS 277+1 , RBL 54 STR 14. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100193 19980731 00193 NM 1998 7 31 SWAA981396 1 19980715 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 291.5-295.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED ATTACH ANGLE AT BS 291.5- 295.5, WL208, RBL 54 THAT ATTACHED FLOORBEAM TO MOPSIL L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100194 19980731 00194 NM 1998 7 31 SWAA981397 1 19980715 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED ANGLE AT BS 290, RBL 63, WL 253. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100195 19980731 00195 NM 1998 7 31 SWAA981398 1 19980715 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 277-291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 277-291, RBL 59-63, WL 253. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100196 19980731 00196 NM 1998 7 31 SWAA981399 1 19980715 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 312, LBL 45, RBL 12, WL 208. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998073100197 19980731 00197 NM 1998 7 31 SWAA981400 1 19980715 A 5320 WEB BOEING 737 7373Y0 1384671 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23826 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT DOOR OPENING BS 440, STR 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100198 19980731 00198 NM 1998 7 31 SWAA981401 1 19980716 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C1 CHECK, FOUND BULLNOSE EMERGENCY LIGHT ASSY LOOSE AT SEAT 9ABC. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998073100199 19980731 00199 NM 1998 7 31 SWAA981402 1 19980716 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 637SW 27710 DURING WALKAROUND CHECK, FOUND EGRESS LIGHTS MID CABIN CAME LOOSE. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100200 19980731 00200 NM 1998 7 31 SWAA981403 1 19980716 A 5320 CHORD BOEING 737 7373G7 1384595 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CORRODED Z CHORD AT BS 270, LBL 11 RBL 11, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100201 19980731 00201 NM 1998 7 31 SWAA981404 1 19980716 A 5330 SKIN BOEING 737 737317 138447P NM BS 500 BUCKLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BUCKLED/WARPED AROUND FASTENERS ON LOWER LOBE AT BS 500C, STR 28L. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100202 19980731 00202 NM 1998 7 31 SWAA981405 1 19980716 A 5312 BULKHEAD BOEING 737 737317 138447P NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BS 178 LT BULKHEAD CHORD ANGLE WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100203 19980731 00203 NM 1998 7 31 SWAA981406 1 19980715 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 1000 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED TRANSITION CHECK, FOUND ANGLE BS 1000, RBL 45, WL 208 HAS ELONGATED FASTENER HOLE. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100204 19980731 00204 NM 1998 7 31 SWAA981407 1 19980716 A 5320 WEB BOEING 737 737301 1384611 NM BS 279 MISDRILLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 660SW 23230 DURING SCHEDULED TRANSITION CHECK, FOUND PREVIOUSLY PLUGED HOLE IN WEB AT BS 279 WL 192 LBL 16. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100205 19980731 00205 NM 1998 7 31 SWAA981408 1 19980717 A 2780 RETRACT MECH BOEING 737 7373G7 1384595 NM NR 4 LE FLAP OUT OF ADJUST A SWAA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 670SW 23784 NR 4 LEADING EDGE SLAT SHOWED UNSAFE INFLIGHT. COULD SEE NR 4 SLAT DROOPING ABOUT ONE INCH. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED AND PERFORMED OPERATIONAL CHECK ON FLAP AND LEADING EDGE DEVICES SYSTEM PER BOEING MM. OPS CH OK. 2 L 7 2 4F RT A16WE 1998073100206 19980731 00206 NM 1998 7 31 SWAA981409 1 19980720 A 2560 SLIDE BOEING 737 7372H4 138448C NM PAX DOOR OUT OF POSITION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 095SW 23054 DURING SCHEDULED CI CHECK, FOUND ESCAPE SLIDE GAUGE NOT VISIBLE. REPOSITIONED SLIDE GAUGE FOR PROPER VISIBILITY PER BOE ING MM. 2 L 7 2 4F A16WE 1998073100207 19980731 00207 NM 1998 7 31 SWAA981410 1 19980720 A 3350 END CAP BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED CI CHECK, FOUND EMERGENCY EXIT TRACK LIGHTING FWD END CAP MISSING. INSTALLED MISSING EGRESS LIGHTING E ND CAP AT FWD END PER BOEING MM. 2 L 7 2 4F RT A16WE 1998073100208 19980731 00208 NM 1998 7 31 SWAA981411 1 19980720 A 5320 WEB BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED CI CHECK, FOUND NOSE GEAR ACTUATOR VERTICAL WEB ATTACH CRACKED 2 LONG, 6 IN FROM FWD END. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100209 19980731 00209 NM 1998 7 31 SWAA981412 1 19980720 A 5320 WEB BOEING 737 7373H4 1384600 NM NLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING SCHEDULED CI CHECK, FOUND UPPER WEB CRACKED AT NUT PLATE HOLE RIVET RT AND LT. REPAIRED PER BOEING TI-A53-001. 2 L 7 2 4F RT A16WE 1998073100210 19980731 00210 NM 1998 7 31 SWAA981413 1 19980720 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 381 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 381 BELOW STR 15L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100211 19980731 00211 NM 1998 7 31 SWAA981414 1 19980720 A 5400 BRACKET BOEING 737 7373G7 1384595 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED NR 1 PYLON UPR AFT END, L BRACKET ON I/B SIDE OF SUPPORT BETWEEN ACCESS PANELS 5 735L AND 5736L AND AFT SIDE PANEL SUPPORT AT THE AFT END OF ACCESS PANEL 5736L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100212 19980731 00212 NM 1998 7 31 SWAA981415 1 19980720 A 5400 SUPPORT BOEING 737 7373G7 1384595 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED NR 1 PYLON LWR AFT END L SUPPORT ON I/B SIDE OF PYLON. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100213 19980731 00213 NM 1998 7 31 SWAA981416 1 19980720 A 5400 SUPPORT BOEING 737 7373G7 1384595 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND CRACKED NR1 PYLON 'L' ANGLE SUPPORT ON I/B AFT SIDE ON LWR SIDE OF FLAP CUTOUT IS GOUGE D BEYOND LIMITS. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100214 19980731 00214 NM 1998 7 31 SWAA981417 1 19980720 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 294.5-303.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL WEB CRACKED AT STRINGER 12, WL 244, LBL 62, BETWEEN BS 294.5-303.9. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100215 19980731 00215 NM 1998 7 31 SWAA981418 1 19980720 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 277-294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED AT FLOOR PNL HOLES AT LBL 11 BS 277 TO 294.5. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100216 19980731 00216 NM 1998 7 31 SWAA981419 1 19980720 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND LWR FLOOR BEAM FLANGE INTERCOSTAL CRACKED, LBL 12 AT BS 312 ON INBD AND O/B EDGES, AN D LBL 12 AT BS 328 O/B EDGE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100217 19980731 00217 NM 1998 7 31 SWAA981420 1 19980720 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D CHECK, FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT FASTENER HOLES AT BS 344 RBL 12 TO LBL 12 TOP AND BOTTOM SIDES; AND BS 344 LBL 12 - LBL 58. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998073100218 19980731 00218 NM 1998 7 31 UPS98227206 1 19980714 A 5280 FITTING BOEING 727 72731C 1384011 NM LT MLG DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, LT MLG WING DOOR AFT HINGE FITTING ON NR 4 FLAP TRACK CRACKED. HINGE FITTING REPLACED IAW SRM 51-30- 03 AND MM 21-80-01. 2 L 7 3 4F A3WE 1998073100219 19980731 00219 NM 1998 7 31 UPS98227207 1 19980709 A 5755 6598924 FITTING BOEING 727 72731C 1384011 NM WS 491.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, NR 12 SPOILER SUPPORT FITTING CRACKED AT I/B CORNER OF CASTING. REPLACED SUPPORT FITTING IAW DRAWING 65-16201. 2 L 7 3 4F A3WE 1998073100220 19980731 00220 NM 1998 7 31 UPS98227208 1 19980710 A 5755 65413077 CASTING BOEING 727 72731C 1384011 NM WS 450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, ON REMOVAL OF NR 4 SPOILER ACTUATOR SUPPORT CASTING, CASTING FOUND TO BE BADLY CORRODED. CASTING REP LACED IAW DRAWING 65-17351 AND SUPPORT ANGLES REPLACED IAW DRAWING 65-16201. 2 L 7 3 4F A3WE 1998073100221 19980731 00221 NM 1998 7 31 UPS98227209 1 19980712 A 5753 65413425 FITTING BOEING 727 72731C 1384011 NM WS 330.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, NR 6 FLAP TRACK MIDFAIRING FWD HINGE CASTING HAS LIGHT SURFACE CORROSION FITTING REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998073100222 19980731 00222 NM 1998 7 31 UPS98227210 1 19980712 A 5230 WEB BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, ON GAINING ACCESS TO CRACKED CENTER WEB OF FWD CARGO DOOR, DISCOVERED WEBS FWD AND AFT CRACKED. ALSO , WEBS REPLACED IAW DRAWING 65-18620. 2 L 7 3 4F A3WE 1998073100223 19980731 00223 NM 1998 7 31 UPS98227211 1 19980709 A 5755 ANGLE BOEING 727 72731C 1384011 NM WS 445 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C NR 4 SPOILER ACTUATOR CASTING OUTBD SUPPORT ATTACH ANGLE HOLES BADLY ELONGATED. REPLACED ATTACH ANGLE S IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998073100224 19980731 00224 NM 1998 7 31 UPS98227212 1 19980708 A 5230 WEB BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, SUSPECT CRACK ON INNER UPPER WEB OF FWD LOWER CARGO DOOR WEB. REPLACED IAW DRAWING 65-18620. 2 L 7 3 4F A3WE 1998073100225 19980731 00225 NM 1998 7 31 UPS98227214 1 19980708 A 5230 BEAM BOEING 727 72731C 1384011 NM CARGO DOOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C ON REMOVAL ON MAIN CARGO DOOR CORROSION DISCOVERED ON UPPER BEAM. BEAM REPLACED IAW SRM 51-30-2 AND S RM 51-10-06 AND SRS EO 98-22-002, REF UPS ENGINEERING FILE NUMBER 727-52-0191. 2 L 7 3 4F A3WE 1998073100226 19980731 00226 NM 1998 7 31 UPS98227215 1 19980714 A 5320 FITTING BOEING 727 72731C 1384011 NM BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, CRACK FOUND ON LT BS 940 FITTING ROW ONE SECOND HOLE AFT CRACK. REMOVED AND RETAINED IAW SRM 51-10-1 . REFER TO SRS EO 98-22-0 07, REFERENCE UPS ENGINEERING FILE NUMBER 727-53-2049, FOR COMPLETION OF REPAIR. 2 L 7 3 4F A3WE 1998073100227 19980731 00227 NM 1998 7 31 UPS98227217 1 19980722 A 5315 6515940140 FLOORBEAM BOEING 727 72730C 1384009 NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION (C53-224-01.05-02) AND CHAFFING ON UPPER BS 740 FLOORBEAM UPPER FLANGE, RBL 0-45, WL 208, M ARKED. REMOVED COROSION FOUND TO BE OUT OF LIMITS, REPLACED CHORD AS PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998073100228 19980731 00228 NM 1998 7 31 UPS98227219 1 19980713 A 5520 652564056 TIP BOEING 727 72731C 1384011 NM RT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, CORROSION ON LOWER SKIN RT ELEVATOR TIP IN AREA OF STATIC WICK. ELEVATOR SKIN PANEL REPLACED IAW DRA WING 65-25640. 2 L 7 3 4F A3WE 1998073100229 19980731 00229 NM 1998 7 31 UPS98227220 1 19980718 A 5320 65405124 FITTING BOEING 727 72731C 1384011 NM BS 487.1 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, MAIN CARGO DOOR SUPPORT LATCH FITTING AT BS 487.1 CRACKED. LATCH SUPPORT FITTING REPLACED IAW B727-5 310-0437. 2 L 7 3 4F A3WE 1998073100230 19980731 00230 NM 1998 7 31 UPS98227221 1 19980708 A 5320 65405121 FITTING BOEING 727 72731C 1384011 NM BS 580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, MAIN CARGO DOOR SUPPORT LATCH FITTING AT BS 580 CRACKED. LATCH SUPPORT FITTING REPLACED IAW B727-531 0-0437. 2 L 7 3 4F A3WE 1998073100231 19980731 00231 NM 1998 7 31 UPS98227222 1 19980714 A 5330 SKIN BOEING 727 72731C 1384011 NM BS 740 CUT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C EXISTING CUTOUT ON FUSELAGE SKIN AT BS 740 BETWEEN STR 17 RT AND 18 RT REPAIR CARRIED OUT IAW SRS EO 98-22-009, REF UPS ENGINEERING FILE NUMBER 727-53-2050. 2 L 7 3 4F A3WE 1998073100232 19980731 00232 NM 1998 7 31 UPS98227223 1 19980710 A 5754 SKIN BOEING 727 72731C 1384011 NM NR 5 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C SUSPECT CRACK ON NR 5 KREUGER FLAP OUTER SURFACE AT BULLNOSE MID HINGE CUTOUT. KREUGER FLAP REPLACED IAW MM 27-81-01. 2 L 7 3 4F A3WE 1998073100233 19980731 00233 NM 1998 7 31 UPS98227224 1 19980721 A 5522 SKIN BOEING 727 72731C 1384011 NM RT ELEVATOR CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, ON REMOVAL OF RT ELEVATOR STATIC DISCHARGER ELEVATOR SKIN FOUND CORRODED. ELEVATOR SKIN PANEL REPLAC ED IAW DRAWING 65-25640. 2 L 7 3 4F A3WE 1998073100234 19980731 00234 NM 1998 7 31 UPS98227225 1 19980712 A 5753 FAIRING BOEING 727 72731C 1384011 NM NR 1 TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, NR 1 FLAP TRACK MID FAIRING FWD HINGE CASTING CORRODED. CASTING REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998073100235 19980731 00235 NM 1998 7 31 UPS98227226 1 19980709 A 5755 ANGLE BOEING 727 72731C 1384011 NM NR 3 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, NR 3 SPOILER ACTUATOR CASTING INBD SUPPORT ATTACH ANGLE CRACKED. REPLACED SUPPORT ANGLES IAW DRAWING 65-16201, BOTH ANGLES REPLACED TO CASTING REPLACEMENT. 2 L 7 3 4F A3WE 1998073100236 19980731 00236 NM 1998 7 31 UPS98227227 1 19980706 A 5754 ANGLE BOEING 727 72731C 1384011 NM NR 1 LE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE:C, SUSPECT CRACK IN NR 1 KREUGER FLAP ACTUATOR MOUNT SUPPORT STRUCTURE. REPLACED PART WITH NEW FABRICAT ED ANGLE IAW SRM 51-10-1, PAGE 4. 2 L 7 3 4F A3WE 1998073100237 19980731 00237 EU 1998 7 31 QXEA9801036 1 19980721 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 GEG - EMERGENCY SIGN OVER COCKPIT DOOR IS OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998073100238 19980731 00238 EU 1998 7 31 QXEA9801037 1 19980722 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 PDX - EMERGENCY LIGHTING OVER WINDOW AT ROW 9 IS INTERMITTENT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998073100239 19980731 00239 EU 1998 7 31 QXEA9801038 1 19980722 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 SEA - EMERGENCY EXIT LIGHT AT ROW 9 IS OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998073100240 19980731 00240 NM 1998 7 31 QXEA9801039 1 19980722 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 361PH 7259 155 516 SEA - CLIMBING THROUGH 18,000 FEET, THE MASTER WARNING AND SMOKE WARNING LIGHTS CAME ON FOR ABOUT 3 SECONDS, THEN THE SM OKE LIGHT WENT OUT. VISUAL CHECK OF THE BAGGAGE COMPARTMENT FOUND NO EVIDENCE OF SMOKE OR FIRE. REPLACED THE NR 2 SMOK E DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998073100241 19980731 00241 WP 1998 7 31 ABXA9800636 1 19980717 A 3230 5759112501 DRAG LINK DOUG DC8 DC863 302198A WP LT MLG WORN A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 815AX 46097 RED GEAR UNSAFE LIGHT ILLUMINATED DURING GEAR UPLATCH CHECK ACCOMPANIED BY NOT LATCHED LIGHT ON LEFT GEAR. RECYCLED GEA R, NO HELP. REPLACED WORN DRAG LINK KNUCKLES ON LEFT AND RIGHT GEAR IAW DC8 MM 32-11-03. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998073100242 19980731 00242 WP 1998 7 31 TC8A98044 1 19980723 A 3240 INDICATOR DOUG DC8 DC862 3021970 WP NR 1 BRAKE TRIPPED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 181SK 45910 TRIP NR 02197, DISCREP: ITEM NR 1, HYDRAULIC BRAKE PRESSURE ONLY 2300 PSI. RESET HYD BRAKE IND. OPS CHECKED NORMAL IAW M/M 32-42-5. 2 L 7 4 4F 4A25 1998073100243 19980731 00243 WP 1998 7 31 TC8A98045 1 19980723 A 2110 207001001 INDICATOR DOUG DC8 DC862 3021970 WP NR 2 TURBOCOMP FAILED A TC8A D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 23 181SK 10 45910 TRIP NR 02197, DISCREP: ITEM NR 2, T/C NR 2 DOES NOT TEST. ENTER ON DMI 8628 IAW MEL 21-3 CAT C. REMOVED AND REPLACED T/C INDICATOR IAW MM 21-1-2, OPS CHECKS OK, CLEARED DMI. 2 L 7 4 4F 4A25 1998073100244 19980731 00244 WP 1998 7 31 98ZZZX2509 1 19980628 A 2612 WIRE DOUG DC8 DC851 3021920 WP NR 3 ENGINE CHAFED A FXLA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 507DC 69393 45855 SAL - ON TAKEOFF, EXPERIENCED FIRE WARNING ON NR 3 ENGINE. RETARDED THROTTLE AND FIRE WARNING CEASED. RETURNED TO SAL AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED FIRE DETECTOR WIRING CHAFING ON FORWARD INBOARD COWLING. REPAIRED WIR ING - SYSTEM CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES: 31,341. (X) 2 L 7 4 4F 4A25 1998073100245 19980731 00245 WP 1998 7 31 98ZZZX2510 1 19980627 A 2612 37711523 AMPLIFIER DOUG DC8 DC851 3021920 WP NR 4 ENGINE MALFUNCTIONED A FXLA E A ENGINE SHUTDOWN UNSCHED LANDING N Y FALSE WARNING ENGINE STOPPAGE TO TAKEOFF 1 SO 19 507DC 69392 45855 SAL - AFTER TAKEOFF, EXPERIENCED FIRE WARNING ON NR 4 ENGINE. RETARDED THROTTLE AND FIRE WARNING CEASED. SHUT DOWN ENG INE, RETURNED TO SAL AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A DEFECTIVE FIRE WARNING AMPLIFIER. REPLACED AMP LIFIER AND SYSTEM CHECK NORMAL. RETURNED AIRCRAFT TO SERVICE. PART TOTAL CYCLES: 31,340. (X) 2 L 7 4 4F 4A25 1998073100246 19980731 00246 NM 1998 7 31 EIAA980223 1 19980701 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 380 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 73984 20651 SIN - DURING B-CHECK, BS 380 UPPER DECK FLOORBEAM WAS FOUND CRACKED AT THE UPPER CHORD, RT OUTBOARD END. ACCOMPLISHED T IME LIMITED REPAIR, PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 18 MONTHS OR 1500 CYCLES, WHICHEVER COMES FIRST PER TEL EX SCO-QUG-98-0016RE, AD 98-09-17. ECRA 471-53-1771. GENERATED TO TRACK REPAIR. (M) 2 L 7 4 4F A20WE 1998073100247 19980731 00247 NM 1998 7 31 EIAA980222 1 19980702 A 5210 SKIN BOEING 747 747273C 1384896 NM LT DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 HKG - DURING B-CHECK, L1 DOOR UPPER HINGE, DOOR SKIN CRACKED AT HINGE CUTOUT. REPAIRED DOOR SKIN PER BOEING TELEX EVR-H KG-98-0100RE AND APPROVED ON 8110-3 DATED JUNE 22, 1998. ECRA 470-52-97-1. (M) 2 L 7 4 4F A20WE 1998073100248 19980731 00248 NM 1998 7 31 EIAA980221 1 19980702 A 5320 FITTING BOEING 747 747273C 1384896 NM LT/RT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 73644 20653 HKG - DURING B-CHECK, LT AND RT BODY LANDING GEAR TRUNNION SUPPORT FITTINGS, CORROSION WAS FOUND IN THE BOLT HOLES AND B EARING SURFACES. THE LEFT INBOARD AND OUTBOARD LOWER TRUNNION CAPS ALSO HAVE CORROSION. REPAIRED TRUNNION FITTINGS PER BOEING TELEX PAO-HKG-98-0102RE/0103RE/0105RE APPROVED ON 8110-3, DATED JUNE 26, 1998, ECRA 470-53-99-1. (M) 2 L 7 4 4F A20WE 1998073100249 19980731 00249 NM 1998 7 31 EIAA980220 1 19980701 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 440 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 73644 20653 HKG - DURING B-CHECK, BS 440 UPPER DECK FLOORBEAM WAS FOUND CRACKED AT THE UPPER CHORD, RT OUTBOARD END RUNNING INBOARD .040 INCH. ACCOMPLISHED TIME LIMITED REPAIR, PERMENANT REPAIR TO BE ACCOMPLISHED PRIOR TO 18 MONTHS OR 1500 CYCLES, WHI CHEVER COMES FIRST PER TELEX EVR-HKG-98-0091TE, AD 98-09-17, ECRA 470-53-98-1 GENERATED TO TRACK REPAIR. (M) 2 L 7 4 4F A20WE 1998073100250 19980731 00250 NM 1998 7 31 EIAA980216 1 19980629 A 7722 8DJ163LYT4 INDICATOR BOEING 747 747273C 1384896 NM COCKPIT FAILED A EIAA E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE NR NOT REPORTED 1 NM 09 470EV 7815 20653 ANC - LOG PAGE: F08754 - IN-FLIGHT, NR 2 EGT GAUGE FAILED, AN IN-FLIGHT SHUT DOWN WAS PERFORMED AS A PRECAUTION, OIL PR ESSURE STAYED ABOVE 5 PSI AT ALL TIMES. REPLACED EGT INDICATOR PER MM 77-21-03. CARRIED OUT WINDMILL INSPECTION PER MM 72-00-00. OPS CHECKED EGT INDICATION PER MM 77-21-03 SATISFACTORY. (X) 2 L 7 4 4F A20WE 1998073100251 19980731 00251 NE 1998 7 31 PLGA980518A 3 19980518 A 6111 6607132886 BLADE SAAB SF340 340B 7860101 EU ROTOL R389 R3894123F25 NE 18324 CRACKED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 356BE 4143 SF340132598 340B275 DRG189989 ALB - LEFT PROPELLER WAS REMOVED DUE TO EXECESSIVE BLADE MOVEMENT. UPON INSPECTION, THE FOLLOWING WAS DISCOVERED: THE NR 1 BLADE ROOT OUTER SLEEVE WAS CRACKED COMPLETELY AROUND BLADE AND WAS GROOVED DUE TO EXCESS BLADE MOVEMENT. THE NR 1 BLADE PORT SEAL GROOVE OUTER WALL WAS DAMAGED; GOUGES AND HIGH METAL. BLADES 2, 3, AND 4 WERE FOUND TO HAVE GROOVED BL ADE ROOTS. (X) 2 L 7 2 4T RT A52EU 6 C P30NE 1998073100252 19980731 00252 NE 1998 7 31 C2XA98CL040 3 19980527 A 6114 8147211 HUB EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE RT ENGINE BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 6438 1870 120084 CLE - DURING A SCHEDULED TIME CHANGE ON THE RIGHT HAND ENGINE PROPELLER HUB, ONE OF THE ATTACHMENT STUDS BROKE WHILE THE FINAL TORQUE WAS BEING APPLIED. PLEASE REFER TO SDR NR C2XA98CL041 FOR FAILURE OF THE SECOND HUB. THE HUB WAS REMOVED AND REPLACED IAW HAMILTON STANDARD MM 61-10-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR S ERVICE. (X) 2 L 7 2 4T RT A31SO 6 C P11NE 1998073100253 19980731 00253 NE 1998 7 31 C2XA98CL041 3 19980527 A 6114 8147211 HUB EMB 120 EMB120RT SO HAMSTD 14RF 14RF9 NE RT ENGINE BROKEN STUD A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 2008 389 120084 CLE - DURING A SCHEDULED PROPELLER HUB TIME CHANGE, THE FIRST HUB HAD AN ATTACHMENT STUD BREAK DURING TORQUING. REFER T O SDR NR C2XA98CL040. THE SECOND REPLACEMENT HUB ALSO HAD AN ATTACHMENT STUD BREAK DURING THE FINAL TORQUE PROCEDURE. T HE HUB WAS REMOVED AND REPLACED IAW HAMILTON STANDARD 61-10-0, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 6 C P11NE 1998073100254 19980731 00254 NE 1998 7 31 GAIA9857A 2 19980527 A 7261 79522 SEAL BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE WORN A GAIA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 07 6827 20180 DFW - AFTER DEPARTING, NR 2 ENGINE OIL PRESSURE LOW, (LOSS OF PRESSURE). ENGINE SHUT DOWN. AIRCRAFT MADE AN UNEVENTFUL RETURN TO DFW. INSPECTED ENGINE WITH NO DEFECTS NOTED. NO DEFECTS NOTED IN OIL SCREEN. GARLOCK SEAL FOR STARTER REPL ACED FOR OIL QUANTITY LOSS. RE-SERVICED OIL PER PRATT & WHITENEY MM 72-00. ENGINE RUN COMPLETED WITH NO DEFECTS OR LEA KS NOTED. OIL QUANTITY SERVICE CHECKED GOOD AFTER ENGINE RUN. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1998073100255 19980731 00255 SO 1998 7 31 C2XA98IA184 1 19980524 A 7797 23062387 WIRE HARNESS EMB 145 EMB145 SO NR 2 ENGINE FAILED A C2XA O OTHER J WARNING INDICATION CR CRUISE 1 SW 09 16944 145045 IAH - FLT 4153 - THE PILOT REPORTED THE NR 2 ENGINE HAD A LOW N1 INDICATION. AN AUTO SHUT DOWN OCCURRED AND THE CREW WA S ABLE TO RE-START THE ENGINE AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ITT 'A' SYSTEM MAIN HARNESS. THE AIRCRAFT WAS TEST FLOWN SATISFACTORILY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (X) 2 L 7 2 4F RT T00011AT 1998073100256 19980731 00256 WP 1998 7 31 EIAA980213 1 19980626 A 5315 FLOORBEAM DOUG DC9 DC932F 3022067 WP BS 229 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK, MAIN DECK FLOORBEAM AT BS 229 HAS CORROSION AT RBL 23. REPAIRED FLOORBEAM PER SRM 53-40-00 FIG 6L . (M) 2 L 7 2 4F A6WE 1998073100257 19980731 00257 WP 1998 7 31 EIAA980212 1 19980626 A 5551 59124811 FITTING DOUG DC9 DC932F 3022067 WP HORIZ STAB CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK, HORIZONTAL STABILIZER CENTER SECTION LOWER AFT FITTING HAS CORROSION. REPLACED FITTING PER SB 55- 32. (M) 2 L 7 2 4F A6WE 1998073100258 19980731 00258 WP 1998 7 31 TWAA9810401 1 19980627 A 3350 105606004 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9630A 53561 STL - FLT 201 - TWO SECTIONS OF EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE TWO LAMP MODULE ASSEMBLES. CHECK-C 6-7- 98 STL. (X) 2 L 7 2 4F RT A6WE 1998073100259 19980731 00259 EU 1998 7 31 SIMA981871 1 19980406 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 11829 0209 ORD - FLT 4055 - THREE EMERGENCY FLOOR PROXIMITY LIGHTS AND THE TWO FORWARD EMERGENCY EXIT SIGNS DO NOT ILLUMINATE. REM OVED AND REPLACED EMERGENCY LIGHTING POWER SUPPLY BATTERY. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1998073100260 19980731 00260 EU 1998 7 31 SIMA981881 1 19980707 A 3350 7012211 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 017 ORD - FORWARD EMERGENCY EXIT SIGN DOES NOT FULLY ILLUMINATE. REMOVED AND REPLACED BULBS FOR EXIT LIGHT. OPERATIONAL CH ECK GOOD. (X) 2 H 7 2 4T RT A53EU 1998073100261 19980731 00261 EU 1998 7 31 SIMA981821 1 19980701 A 2611 72111211000 SMOKE DETECTORS SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 244AE A3724 340B244 SYR - FLT 4898 - CARGO SMOKE WARNING LIGHT ILLUMINATED ON CLIMB-OUT. FIRED NR 1 CARGO FIRE EXTINGUISHER. RETURNED TO F IELD. MEL'D CARGO SMOKE DETECT SYSTEM NR 070002 DM. REPOSITIONED AIRCRAFT TO JFK WHERE BOTH CARGO SMOKE DETECTORS AND T HE NR 1 CARGO FIRE EXTINGHISHER WERE REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR 98Z ZZX2511. (X) 2 L 7 2 4T RT A52EU 1998073100262 19980731 00262 EU 1998 7 31 98ZZZX2511 1 19980701 A 2611 72111211000 SMOKE DETECTORS SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 244AE A2337 340B244 SYR - FLT 4898 - CARGO SMOKE WARNING LIGHT ILLUMINATED ON CLIMB-OUT. FIRED NR 1 CARGO FIRE EXTINGUISHER. RETURNED TO F IELD. MEL'D CARGO SMOKE DETECT SYSTEM NR 070002 DM. REPOSITIONED AIRCRAFT TO JFK WHERE BOTH CARGO SMOKE DETECTORS AND T HE NR 1 CARGO FIRE EXTINGHISHER WERE REMOVED AND REPLACED. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SI MA98182-1. 2 L 7 2 4T RT A52EU 1998073100263 19980731 00263 EU 1998 7 31 SIMA981831 1 19980702 A 2611 005W500 WARNING UNIT SAAB SF340 340B 7860101 EU E/E/ BAY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 21 244AE 1251 340B244 ROC - FLT 4902 - CARGO SMOKE WARNING LIGHT CAME ON IN-FLIGHT. FIRED NR 1 CARGO FIRE EXTINGUISHER. RETURNED TO FIELD. I NSPECTED CARGO COMPARTMENT WITH NO DISCREPANCIES NOTED. DEFERRED CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM. REMOVED AND REPLACED (WARNING ELECTRONIC UNIT) WEU. OPERATIONAL CHECK GOOD. CLEARED CARGO COMPARTMENT FIRE EXTINGUISHER MEL. (X) 2 L 7 2 4T RT A52EU 1998073100264 19980731 00264 EU 1998 7 31 SIMA981841 1 19980703 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 256AE 340B256 DFW - FLT 5183 - EMERGENCY LIGHTS AT ROWS 9, 10, AND 11 DO NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY. OPERATIO NAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998073100265 19980731 00265 EU 1998 7 31 SIMA981731 1 19980622 A 5320 S5367800826801 SUPPORT AEROSP ATR72 ATR72212 EU BS 38-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND FLOOR SUPPORT CHANNEL BETWEEN FRAMES 38 AND 39, UNDER PASSENGER DOOR SILL PLATE, CO RRODED. INSTALLED NEW FLOOR CHANNEL SUPPORT BETWEEN FRAMES 38 AND 39. (X) 2 H 7 2 4T RT A53EU 1998073100266 19980731 00266 EU 1998 7 31 SIMA981732 1 19980622 A 5347 S5367001226 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 29-36 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND LEFT AFT INBOARD SEAT TRACK CORRODED FROM FRAME 29 TO FRAME 36. REMOVED AND INSTA LLED NEW SEAT TRACK BETWEEN FRAME 29 AND FRAME 36. (X) 2 H 7 2 4T RT A53EU 1998073100267 19980731 00267 EU 1998 7 31 SIMA981733 1 19980622 A 5315 S5362406208 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND FLOORBEAM 36 CORRODED. REMOVED AND REPLACED FLOORBEAM 36. (X) 2 H 7 2 4T RT A53EU 1998073100268 19980731 00268 EU 1998 7 31 SIMA981734 1 19980622 A 5347 S367001224 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 29-36 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND LEFT AFT OUTBOARD SEAT TRACK CORRODED BETWEEN FRAME 29 AND FRAME 36. REMOVED AND I NSTALLED NEW LEFT AFT OUTBOARD SEAT TRACK BETWEEN FRAMES 29 AND FRAME 36. (X) 2 H 7 2 4T RT A53EU 1998073100269 19980731 00269 EU 1998 7 31 SIMA981735 1 19980622 A 5320 S5367131828001 SILL AEROSP ATR72 ATR72212 EU SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND SERVICE DOOR SILL PLATE CORRODED. REMOVED AND INSTALLED NEW SERVICE DOOR SILL PLAT E. (X) 2 H 7 2 4T RT A53EU 1998073100270 19980731 00270 EU 1998 7 31 SIMA981736 1 19980622 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT'S SEAT TRACK TO HAVE CORROSION BETWEEN FLOORBEAM 36 AND FLOOR BEAM 39. REMOVED AND REPLACED LEFT FLIGHT ATTENDANT'S SEAT TRACK BETWEEN FLOORBEAM 36 AND FLOORBEAM 39. (X) 2 H 7 2 4T RT A53EU 1998073100271 19980731 00271 EU 1998 7 31 SIMA981737 1 19980622 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND PASSENGER DOOR SILL PLATE TO HAVE CORROSION. REMOVED AND REPLACED PASSENGER DOOR S ILL PLATE. (X) 2 H 7 2 4T RT A53EU 1998073100272 19980731 00272 EU 1998 7 31 SIMA981738 1 19980622 A 5320 S5367121729801 GULLEY AEROSP ATR72 ATR72212 EU PAX DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 407AT 407 SAW - DURING CPCP8 INSPECTION, FOUND RAIN GULLEY ON PASSENGER DOOR SILL PLATE TO HAVE CORROSION. REMOVED AND REPLACED R AIN GULLEY ON PASSENGER DOOR SILL PLATE. (X) 2 H 7 2 4T RT A53EU 1998073100273 19980731 00273 EU 1998 7 31 SIMA981754 1 19980624 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 971NA 14871 017 GRR - EMERGENCY FLOOR PROXIMITY LIGHTS AT SEAT MID-CABIN DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK FOR MID-C ABIN FLOOR PROXIMITY LIGHTS. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A53EU 1998073100274 19980731 00274 EU 1998 7 31 SIMA981792 1 19980628 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 144DD 15381 074 GRR - EMERGENCY BATTERY PACK AT 3 WR IS DISCHARGED. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPERATIONAL CHECK NOR MAL. (X) 2 H 7 2 4T RT A53EU 1998073100275 19980731 00275 EU 1998 7 31 SIMA981802 1 19980629 A 5512 SKIN SAAB SF340 340B 7860101 EU HORIZ STABILIZER CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 268AE 340B268 ABI- DURING COMPLIANCE OF SB 34-53-042, INSTALLATION OF PROTECTION PLATE ON LT FUSELAGE AT HORIZONTAL STABILIZER, A CHA FE WAS DISCOVERED BEYOND SRM LIMITATIONS. BLENDED AREA. PERFORMED EDDY CURRENT INSPECTION. INSTALLED EXTERNAL DOUBLER 11.0 INCHES BY 10.75 INCHES IAW SAAB STATEMENT 72SDS1044. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998073100276 19980731 00276 EU 1998 7 31 SIMA981803 1 19980629 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 268AE 340B268 ABI - DURING HMBV INSPECTION, FOUND FUSELAGE DENTS AND OIL CANNING BENEATH AND AFT OF LEFT ICE SHIELD. CUT OUT DAMAGED AREA. PERFORMED EDDY CURENT INSPECTION. INSTALED 10.0 INCH BY 26.0 INCH EXTERNAL DOUBLER AND 7.5 INCH BY 24.0 INCH RIPL ER IAW SAAB STATEMENT 72SD1038. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998073100277 19980731 00277 EU 1998 7 31 SIMA981801 1 19980629 A 3350 7239410001 HOLDER SAAB SF340 SF340A 7850100 EU CABIN BROKEN A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 312AE 312 SBP - CABIN EMERGENCY FLOOR PROXIMITY LIGHT LENSE HOLDERS AT SEATS 3B AND 11B ARE BROKEN. REMOVED AND REPLACED FLOOR PR OXIMITY LIGHT LENSE HOLDERS AT SEAT 3B AND 11B. (X) 2 L 7 2 4T RT A52EU 1998073100278 19980731 00278 EU 1998 7 31 SIMA981761 1 19980625 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 317AE 340B317 JFK - THREE OVERHEAD EMERGENCY LIGHTS AT SEATS 7A, 8BC, AND 10BC DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY POWE R SUPPLY. OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4T RT A52EU 1998073100279 19980731 00279 NE 1998 7 31 SABA290033 2 19980626 A 7210 310212701 GASKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE LEAKING A SABA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 33 881CC 294 CLT - FLT 5122 - ON FLIGHT FROM CLT TO PGV, NR 2 ENGINE OIL PRESSURE WAS INDICATING 50 POUNDS OF PRESSURE. OIL PRESSURE WARNING CAPTION LIGHT ILLUMINATED. AIRCRAFT RETURNED TO CLT. NO IN-FLIGHT EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO CLT WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE NR 2 PROP SHAFT THRUST BEARING COVER GASKET LEAKING. REMOVED AND REPLACED GASKET. SERVICED ENGINE OIL. LEAK AND OPS CHECKED GOOD. (X) 2 H 7 2 4T 4 T RT A13NM E20NE 1998073100280 19980731 00280 NM 1998 7 31 RAAA98B2038 1 19980724 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 LT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998073100281 19980731 00281 NM 1998 7 31 CALA9801336 1 19980724 A 3230 CIRCUIT BREAKER BOEING 737 7373T0 1384582 NM LEVER LATCH POPPED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 69333 23571 THE GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOU T INCIDENT. TROUBLESHOOTING BY MAINTENANCE IAW MM 32-31-21, DUPLICATED CONTROL LEVER LOCK ON GROUND. THE LEVER LATCH C IRCUIT BREAKER WAS FOUND POPPED. THE CIRCUIT BREAKER WAS RESET. GEAR OPERATION WAS SIMULATED AND THE LEVER LOCK OPERATE D NORMALLY WITH THE LEVER LATCH CIRCUIT BREAKER REMAINING IN. 2 L 7 2 4F RT A16WE 1998073100282 19980731 00282 NM 1998 7 31 CALA9801337 1 19980724 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT DOORS AND OVERWING EXITS AND AFT SECTION OF LIGHTS WAS DIM. SEVER AL WIRES WERE FOUND SHORTED. THE WIRING WAS REPAIRED IAW WIRING DIAGRAM 33-51, OPERATIONAL CHECKS WERE GOOD IAW MM 33-5 0. 2 L 7 3 4F A3WE 1998073100283 19980731 00283 NM 1998 7 31 CALA9801338 1 19980724 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.5 INCH CRACK IN ANGLE AT STA 1183 BETWEEN STRINGER 18R AND 19R, RBL 45. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998073100284 19980731 00284 NM 1998 7 31 CALA9801339 1 19980724 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 1.2 INCH CRACK IN VERTICAL SUPPORT AT STA 1183, RBL 50. THE CRACK WAS STOP DRILLED, TWO ANGLES WERE FABRICATED AND INSTALLED IAW ECRA 5310-03748. 2 L 7 3 4F A3WE 1998073100285 19980731 00285 WP 1998 7 31 CALA9801340 1 19980724 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 794 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND FUSELAGE BELLY SKIN TORN WITH CORROSION AT STA 794, LONGERON 30. A DOUBLER WAS INSTALLED IAW SRM 53-04 , FIGURE 12B PAGE 39. 2 L 7 2 4F A6WE 1998073100286 19980731 00286 WP 1998 7 31 CALA9801341 1 19980724 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 718 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE CROWN SKIN AT STA 718, LONGERON 1L. THE CRACKED AREA WAS CUT OUT, INTERNA L AND EXTERNAL DOUBLERS WERE INSTALLED IAW ECRA 5330-02688. 2 L 7 2 4F A6WE 1998073100287 19980731 00287 WP 1998 7 31 CALA9801342 1 19980724 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND LONGERON 22L CORRODED AT STA 150. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 18 PAGE 48. 2 L 7 2 4F A6WE 1998073100288 19980731 00288 WP 1998 7 31 CALA9801343 1 19980724 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 680-756 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT AND RT WHEEL WELL KEEL SKIN AREA CORRODED AT STA 680 TO 756. THE CORRODED SECTION OF KEEL SKIN WAS REMOVED IAW SRM 53-04, FIGURE 42. A NEW SECTION OF SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-2, AND 53-04, FIGURE 42. 2 L 7 2 4F A6WE 1998073100289 19980731 00289 WP 1998 7 31 CALA9801344 1 19980724 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 530 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND A DENT IN LT LOWER WING SKIN AT XRS 530. THE AREA WAS REPAIRED IAW SRM 57-03, PAGE 23. 2 L 7 2 4F A6WE 1998073100290 19980731 00290 WP 1998 7 31 CALA9801345 1 19980727 A 5754 SKIN DOUG DC9 DC932 3022066 WP NR 1 LE SLAT DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 18544 47219 INSPECTION FOUND LT LEADING EDGE SLAT NR 1 SKIN DENTED AT STA XIS 136 AND XIS 132. REPAIRED IAW SRM 57-09, FIGURE 10 AN D 10A. 2 L 7 2 4F A6WE 1998073100291 19980731 00291 NM 1998 7 31 CALA9801346 1 19980726 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 947.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND FLOORBEAM CORRODED AROUND FASTENER HOLES AT STA 947.5 SPAN OF BEAM, WL 208.1. A NEW SECTION OF UPPER T WAS SPLICED IN IAW ECRA 5321-01018 AND SRM 53-00-51, FIGURE 202. 2 L 7 2 4F RT A16WE 1998073100292 19980731 00292 WP 1998 7 31 CALA9801347 1 19980724 A 5350 TAIL CONE DOUG DC9 DC982 3022082 WP AFT FUSELAGE WARPED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10834 49494 THE FORCE REQUIRED TO RELEASE TAIL CONE DURING FUNCTIONAL CHECK WAS EXCESSIVE. THE TAIL CONE HUNG UP ON RIGHT SIDE LATC H PINS. A SERVICEABLE TAIL CONE WAS INSTALLED AND ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998073100293 19980731 00293 EA 1998 7 31 COMA9860192 1 19980724 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 940CA 7048 EMERGENCY LIGHT AT ROW 10 IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1998073100294 19980731 00294 EA 1998 7 31 COMA9860191 1 19980722 A 2421 M83248121B SEAL CNDAIR CL600 CL6002B19 EA RT IDG LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 951CA 7091 RIGHT HAND ENGINE OIL PRESSURE WARNING. FOUND IDG TO BE LEAKING. REPLACED IDG O-RING SEALS. 2 L 7 2 4F RT A21EA 1998073100295 19980731 00295 EA 1998 7 31 COMA9860190 1 19980719 A 5320 601R3520521 BRACKET CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 DURING C-CHECK, FOUND BOTH CARGO STEP BRACKETS BROKEN. REPLACED BRACKETS. 2 L 7 2 4F RT A21EA 1998073100296 19980731 00296 EA 1998 7 31 COMA9860189 1 19980718 A 5320 601R9720413 HEAT SHIELD CNDAIR CL600 CL6002B19 EA APU COMPT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 DURING C-CHECK, FOUND THE APU HEAT SHIELD TO BE CRACKED. REPLACED HEAT SHIELD. 2 L 7 2 4F RT A21EA 1998073100297 19980731 00297 EA 1998 7 31 COMA9860188 1 19980718 A 2750 601R93106107 FLEX SHAFT CNDAIR CL600 CL6002B19 EA LT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 DURING C-CHECK, FOUND CT NR 1 FLAP FLEX SHAFT UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED FLEX SHAFT. 2 L 7 2 4F RT A21EA 1998073100298 19980731 00298 EA 1998 7 31 COMA9860187 1 19980718 A 5741 600101497 BUSHING CNDAIR CL600 CL6002B19 EA RT WING MIGRATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 914CA 7012 DURING C-CHECK, FOUND RIGHT FORWARD WING TO FUSELAGE FITTING AFT BUSHING TO HAV E MIGRATED .020. TEMPORARILY REPAIRED I N ACCEPTANCE WITH CANADAIR REPAIR ENGINEERING ORDER NR 601R-57-21-032. 2 L 7 2 4F RT A21EA 1998073100299 19980731 00299 EA 1998 7 31 COMA9860193 1 19980722 A 2750 857SD100501 FLEX SHAFT CNDAIR CL600 CL6002B19 EA LT TE FLAP BROKEN A COMA K NONE O OTHER AP APPROACH 1 SO 01 965CA 7131 FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE LEFT HAND WING NR 5 FLAP FLEX DRIVE CABLE. CABLE WAS COR RODED AND BROKEN. 2 L 7 2 4F RT A21EA 1998073100300 19980731 00300 EA 1998 7 31 COMA9860194 1 19980722 A 3231 601R751461 VALVE CNDAIR CL600 CL6002B19 EA NLG DOOR MALFUNCTION A COMA K NONE O OTHER AP APPROACH 1 SO 01 914CA 7012 NLG DID NOT EXTEND, PERFORMED MANUAL EXTENSION PER QRH. REPLACED THE NLG DOORS SELECTOR VALVE. 2 L 7 2 4F RT A21EA 1998073100301 19980731 00301 EA 1998 7 31 COMA9860195 1 19980723 A 3230 864806 PSEU CNDAIR CL600 CL6002B19 EA E/E COMPT FAILED A COMA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 SO 01 962CA 5742 2300 7123 PROXIMITY SYSTEM FAULT WARNING. FLAPS FAIL MESSAGE. LANDING GEAR WOULD NOT EXTEND ANTI-SKID AND NOSE STEER FAIL MESSAG ES. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1998073100302 19980731 00302 EA 1998 7 31 COMA9860196 1 19980725 A 2612 47259701 CONTROL BOX CNDAIR CL600 CL6002B19 EA E/E COMPT FAILED A COMA K NONE N FALSE WARNING DE DESCENT 1 SO 01 940CA 7048 LEFT ENGINE FIRE, APU FIRE, AND RIGHT JET PIPE OVERHEAT WARNINGS. FIRE FAIL MESSAGE ON EICAS. REPLACED THE FIRE WARNIN G CONTROL BOX. 2 L 7 2 4F RT A21EA 1998073100303 19980731 00303 NE 1998 7 31 COMA9860197 2 19980724 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 951CA 7091 807324 RIGHT HAND ENGINE OIL PRESSURE GRADUALLY DECREASED WITH FLUCTUATIONS DURING FLIGHT, AT TIME OF OIL PRESSURE WARNING, ENG INE WAS SHUT DOWN. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998073100304 19980731 00304 SO 1998 7 31 COMA9810164 1 19980726 A 2121 FAN EMB 120 EMB120RT SO CABIN FAILED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 243CA 19875 2200 120212 SMOKE FILLED THE COCKPIT AND CABIN AFTER TAKEOFF, AIRCRAFT RETURNED TO THE GATE SAFELY. REPLACED OVERHEATED GASPER FAN. 2 L 7 2 4T RT A31SO 1998073100305 19980731 00305 SO 1998 7 31 COMA9810165 1 19980726 A 5230 12023348005 SEAL EMB 120 EMB120RT SO CARGO DOOR DAMAGED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 268CA 120262 RAPID CABIN DEPRESSURIZATION DURING CLIMBOUT. REPLACED CARGO DOOR SEAL. 2 L 7 2 4T RT A31SO 1998073100306 19980731 00306 NM 1998 7 31 UPS98227230 1 19980703 A 2782 ANGLE BOEING 727 72731C 1384011 NM NR 2 LE FLAP ACT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, SUSPECT CRACK IN NR 2 KRUEGER FLAP ACTUATOR MOUNT SUPPORT STRUCTURE. REPLACED PART WITH NEWLY FABRIC ATED ANGLE IAW SRM 51-10-10, ANGLE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998073100307 19980731 00307 NM 1998 7 31 UPS98227231 1 19980707 A 5320 CHORD BOEING 727 72731C 1384011 NM BS 340-351 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, CORROSION AT WALKWAY LEVEL LT SIDE ON T-CHORD AT BS 351 TO 340 APPROX. REPAIRED CHORD IAW SRM 51-40- 4. 2 L 7 3 4F A3WE 1998073100308 19980731 00308 NM 1998 7 31 UPS98227232 1 19980709 A 5320 HINGE BOEING 727 72731C 1384011 NM CARGO DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, ON REMOVAL OF MAIN CARGO DOOR, DEEP CORROSION FOUND ON HINGE SECTIONS OF FUSELAGE. MAIN CARGO DOOR F USELAGE ATTACH HINGE SECTIONS (6 OFF) REPLACED IAW DRAWING 65-25337. 2 L 7 3 4F A3WE 1998073100309 19980731 00309 NM 1998 7 31 UPS98227234 1 19980710 A 5753 FAIRING BOEING 727 72731C 1384011 NM TE FLAP TRACK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, NR 5 FLAP TRACK AFT FAIRING CRACK AT AFT INBOARD CORNER. FLAP FAIRING REPAIRED IAW UPS EO B727-5750- 3837. 2 L 7 3 4F A3WE 1998073100310 19980731 00310 NM 1998 7 31 UPS98227236 1 19980708 A 5230 FRAME BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, CRACK IN TOP FRAME OF FWD CARGO DOOR. FRAME REPLACED IAW DRAWING 65-18620. 2 L 7 3 4F A3WE 1998073100311 19980731 00311 NM 1998 7 31 UPS98227237 1 19980723 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE-N/A, TURNING ON NO SMOKING SWT ILLUMINATED THE EMERGENCY LTS ABOVE THE COCKPIT DOOR AND THE FWD ENTRY. R EPLACED BOTH EMERGENCY LT ASSYS AND PERFORMED FUNCTIONAL CHECK. 2 L 7 3 4F A3WE 1998073100312 19980731 00312 NM 1998 7 31 UPS98227239 1 19980707 A 5312 BULKHEAD FITTING BOEING 727 72731C 1384011 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, BULKHEAD FITTING BS 740 RT HAS CRACKS. RT BULKHEAD FITTING REPLACED IAW EO B727-5310-7477. 2 L 7 3 4F A3WE 1998073100313 19980731 00313 NM 1998 7 31 UPS98227240 1 19980707 A 5312 BULKHEAD FITTING BOEING 727 72731C 1384011 NM BS 740 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, (CHORD ANGLE) BULKHEAD FITTING BS 740 LT HAS CRACKS. LT BULKHEAD FITTING REPLACED IAW EO B727-5310-7 477. 2 L 7 3 4F A3WE 1998073100314 19980731 00314 NM 1998 7 31 UPS98227241 1 19980708 A 5347 SEAT TRACK BOEING 727 72731C 1384011 NM BS 480-620 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 927UP 19232 INSPECTION TYPE-C, SURFACE CORROSION ON SEAT TRACK BS 480 AND 620 APPROX LBL 62.5. NEW SECTION OF SEAT TRACK FABRICATED FROM EXTRUSION STOCK. SEAT TRACK REPAIRED IAW SRM 53-10-5, FIG 3. 2 L 7 3 4F A3WE 1998073100315 19980731 00315 NM 1998 7 31 UPS98227242 1 19980724 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, POSITION 9L, EMER EXIT LT INOP. REMOVED AND REPLACED BATTERY PACK, OPS OK (P/N 96-2-1015) TAG 1857 70 ON/OFF. 2 L 7 3 4F A3WE 1998073100316 19980731 00316 WP 1998 7 31 UPS98827228 1 19980623 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1240-1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, RIGHT HAND AFT LOWER CARGO PIT FLOOR TRACK AT STATION 1240 TO 1280, LONGERON 21 RIGHT HAS CORROSIO N. REMOVED DAMGED SECTION OF TRACK STATION 970 TO 1580 DRILLED NEW SECTION OF TRACK AND SPLICES IAW DC8 SRM 514. INSTA LLED NEW SECTION OF TRACK AND SPLICES IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998073100317 19980731 00317 WP 1998 7 31 UPS98827229 1 19980709 A 2612 AMPLIFIER DOUG DC8 DC871F 302199D WP CARGO COMPT FAILED A IPXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 702UP 45902 INSPECTION TYPE-N/A, FL 350 CARGO SMOKE LIGHT ILLUMINATED AND SHOWED SMOKE IN ALL POSITIONS. COMPLETED QRH. REMOVED AN D REPLACED FIRE DETECTION SYSTEM CONTROL AMPLIFIER (P/N 30-303A) (S/N 9056) OFF, (P/N 30-326-4) (S/N 43852) ON OPS CHECK S GOOD. 2 L 7 4 4F RT 4A25 1998073100318 19980731 00318 NM 1998 7 31 QXEA9801044 1 19980723 A 3230 82970018009 ACTUATOR DHAV DHC8 DHC8102 2809003 NM LT MLG GEAR MALFUNCTION A QXEA K NONE O OTHER CL CLIMB 1 NM 09 814PH 14947 43 DURING LANDING GEAR RETRACTION, THE LEFT GEAR DOOR LIGHT STAYED ON AND THE GEAR DOOR WAS NOTICED TO BE OPEN. CYCLED THE LANDING GEAR AND THE DOOR OPERATED PROPERLY. REPLACED THE FORWARD GEAR DOOR ACTUATOR AND PERFORMED GEAR SWINGS, OPERAT IONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998073100319 19980731 00319 WP 1998 7 31 ABXA9800637 1 19980722 A 2110 5614845517 TURBO COMP DOUG DC8 DC861 3021952 WP NR 2 DEFECTIVE A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 853AX 367 46037 NR 2 CTC BEGAN TO HOWL ON DESCENT, ACCOMPANIED BY SMELL LIKE BURNING RUBBER. *S/D* REPLACED NR 2 CTC IAW DC8 MM 21-10- 01. 2 L 7 4 4F 4A25 1998073100320 19980731 00320 WP 1998 7 31 ABXA9800639 1 19980724 A 3260 0080004003 PROX CONTROL DOUG DC9 DC941 302207N WP E/E COMPT MALFUNCTION A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 964AX 47781 AFTER LANDING GEAR RETRACTION, RIGH GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, LIGHT REMAINED ON. REPLACED PROX CONTROL BOX, OPS CHECKED GOOD IAW DC9 MM 32-60-00. 2 L 7 2 4F A6WE 1998073100321 19980731 00321 NM 1998 7 31 MWEA98817 1 19980724 A 2560 D29982107 GIRT BAR DOUG MD88 MD88 3023688 NM CABIN DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE MAIN CABIN DOOR SLIDE GIRT BAR CAME OFF. MTC REINSTALLED GIRT BAR LANYARD. 2 L 7 2 4F RT A6WE 1998073100322 19980731 00322 WP 1998 7 31 DLL14981531 1 19980723 A 5312 BULKHEAD LKHEED 1011 1011385115 5265015 WP BS 1363 MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 740DA 193C1244 DURING REWORK OF THE 1363 BULKHEAD PER S/B 093-53-268, SEVERAL FASTENER HOLES WERE MISDRILLED AND SEVERAL FASTENERS WERE INSTALLED WHICH DEVIATE FROM THE S/B. REPAIRED PER ERA 331959-14. 2 L 7 3 4F A23WE 1998073100323 19980731 00323 NM 1998 7 31 DL72S981533 1 19980723 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1297 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 A .25 INCH CRACK ON FRAME LIGHTENING HOLE AT STA 1297 LT. REPAIRED PER M/M 53-11-0 PG 832. 2 L 7 3 4F A3WE 1998073100324 19980731 00324 NM 1998 7 31 DL72S981534 1 19980723 A 5311 FRAME BOEING 727 727232 1384082 NM BS 910 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 A 1 INCH VISIBLE CRACK O/B RADIUS STA 910 FRAME. REPAIRED PER M/M 53-11-0, NR 20. 2 L 7 3 4F A3WE 1998073100325 19980731 00325 NM 1998 7 31 DL72S981535 1 19980723 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 REPLACED SPAR STIFFENER PER M/M 57-20-21. 2 L 7 3 4F A3WE 1998073100326 19980731 00326 NM 1998 7 31 DL72S981537 1 19980723 A 5754 RIB BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 FOUND ON C-1 LETTER CHECK, 1.5 INCH CRACK IN I/B SLAT ACTUATOR ATTACH NOSE RIB ON NR 1 SLAT. INSTALLED DOUBLER PER M/M 57-54-0 NR 4. 2 L 7 3 4F A3WE 1998073100327 19980731 00327 NM 1998 7 31 DL73E981539 1 19980723 A 3350 BATTERY PACK 20131A BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 378DL 23605 OVERHEAD EMERGENCY LIGHT SIGN INOP IN MID CABIN OVERWING EXITS. REPLACED BATT PACK PER M/M. 2 L 7 2 4F A16WE 1998073100328 19980731 00328 NM 1998 7 31 DL72S981541 1 19980720 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 536DA 22049 THE FWD EMER EXIT SIGN IN THE COACH CABIN INOP. FOUND BROKEN GRD WIRE AT C/P FOR LIGHT ON LIGHT SIDE. REPAIRED WIRE, E MER LIGHTS CK OK. 2 L 7 3 4F A3WE 1998073100329 19980731 00329 NM 1998 7 31 DL72L981542 1 19980722 A 5720 DOUBLER BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 RIGHT WING LEADING EDGE FILLET PANEL DOUBLER CRACKED. REMOVED FILLET PANEL AND REPLACED DOUBLER PER SRM 51-40-3. REINS TALLED PANEL. 2 L 7 3 4F A3WE 1998073100330 19980731 00330 WP 1998 7 31 DLL10981543 1 19980723 A 5241 SEAL LKHEED 1011 10113851 5265010 WP GALLEY DOOR DAMAGED A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 727DA 15910 193C1167 UNABLE TO PRESSURIZE AIRCRAFT. LOUD AIR NOISE IN LOWER GALLEY. FOUND SEAL RETAINER UPPER LT AND RT CORNERS DAMAGED AND TWO INCH SECTION OF SEAL MISSING. REPAIRED RETAINER AND REPLACED SEAL. 2 L 7 3 4F A23WE 1998073100331 19980731 00331 NM 1998 7 31 DLM88981544 1 19980723 A 3320 2232 LIGHT DOUG MD88 MD88 3023688 NM CABIN CONTAMINATED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 940DL 49813 READING LIGHT 29E OVERHEATED, A LITTLE SMOKE COMING FROM THAT AREA OF OVHD AND EXCESSIVE HEAT AROUND LIGHT. FOUND BUBBL E GUM WRAPPER INSIDE LIGHT COVER HAD BEEN BURNING. REMOVED GUM WRAPPER, ALL OK. 2 L 7 2 4F RT A6WE 1998073100332 19980731 00332 NM 1998 7 31 DL72S981546 1 19980724 A 5330 SKIN BOEING 727 727232 1384082 NM BS 211.8 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 FOUND AT B-2 LETTER CK, .5 INCH CRACK, FUSELAGE SKIN AT L-4 WINDOW SCREW LOWER INBD CORNER. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1998073100333 19980731 00333 NM 1998 7 31 DL72L981547 1 19980724 A 2433 TRANSFORMER 2299 BOEING 727 727232 1384082 NM NR 2 FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 507DA 21309 STRONG ELECTRICAL SMELL IN COCKPIT AND FWD CABIN FL 310. FOUND ESSENTIAL T/R AT FAULT. SWAPPED WITH NR 2 T/R AND PUT N R 2 T/R ON MCO. 2 L 7 3 4F A3WE 1998073100334 19980731 00334 NM 1998 7 31 DL73K981548 1 19980724 A 3350 1619 BULB BOEING 737 737232 1384475 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 304DL 23076 R2 SLIDE LIGHT INOP. RELAMPED. 2 L 7 2 4F RT A16WE 1998073100335 19980731 00335 NM 1998 7 31 DL72K981549 1 19980724 A 3350 BATTERY 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 412DA 1104 21232 FWD BULLNOSE EMERG LIGHT INOP. REPLACED BATT AND RACK M1088, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1998073100336 19980731 00336 NM 1998 7 31 DL72W981550 1 19980723 A 5240 SKIN BOEING 727 727247 138408F NM R 2 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 FOUND ON MV1 CHECK, 1 CRACK THRU RIVET IN R2 DOOR SKIN LWR FWD CORNER JUST ABOVE GATE HINGE. FABRICATED DOUBLER PER ERA 365315-14 AND INSTALLED DOUBLER. 2 L 7 3 4F A3WE 1998073100337 19980731 00337 NM 1998 7 31 DL72S981551 1 19980724 A 3350 LIGHT 1315 BOEING 727 727225 1384077 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8882Z 21579 EMERGENCY LIGHT INOP ABOVE AFT AIRSTAIR BOTTOM STEP IN CEILING. RELAMPED AND CLEANED SOCKET, CHECKS OK. 2 L 7 3 4F A3WE 1998073100338 19980731 00338 NM 1998 7 31 DL72S981552 1 19980724 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8882Z 14397 21579 EXTERIOR EMERGENCY LIGHT INOP RT SIDE 2ND LIGHT AFT OF OVERWING ESCAPE HATCHES. REPLACED BULBS, BATTERY PACK, CLEANED S OCKETS AND CHECKS OK. 2 L 7 3 4F A3WE 1998073100339 19980731 00339 NM 1998 7 31 DL72S981553 1 19980709 A 3350 BULB 1691 BOEING 727 727232 1384082 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 485DA 20865 EMERGENCY EXIT LIGHT INOP OVERWING EXIT. REPLACED LIGHT BULBS. 2 L 7 3 4F A3WE 1998073100340 19980731 00340 NM 1998 7 31 DLM88981555 1 19980726 A 3350 079123 LIGHT DOUG MD88 MD88 3023688 NM CABIN MISSING A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 939DL 49812 RED EMERGENCY LIGHT AT 25D MISSING. REPLACED SOCKET, BULB AND LENS, CKS NORMAL. 2 L 7 2 4F RT A6WE 1998073100341 19980731 00341 NM 1998 7 31 DL72S981556 1 19980702 A 5320 FORMER BOEING 727 727232 1384082 NM BS 970 BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FORMER BENT AND DAMAGED, STA 970, ABOVE 26L. REMOVED DAMAGE PER SRM 53-10-4. FABRICATED REPAIR PER SRM 53-10-4. DYE C HECKED REMOVED AREA FOR CRACKS, NO CRACKS FOUND PER PS 900-6-3. INSTALLED REPAIR DOUBLER PER SRM 53-10-3. 2 L 7 3 4F A3WE 1998073100342 19980731 00342 NM 1998 7 31 SCNA98077 1 19980726 A 5210 DOOR BOEING 727 7272J4 1384006 NM CABIN OPEN A SCNA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 GL 15 285SC 21676 AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE. FOUND THE R1 DOOR TOP CORNER NOT LATCHED PROPERLY. RECLOSED DOOR AND PERFORMED OPERATIONAL CHECK OF DOOR AND PRESSURIZATION. OPERATIONALLY CHECKED GOOD IN ACCORDANCE WITH MAINTENANCE MANU AL 2100 AND 5200. 2 L 7 3 4F RT A3WE 1998073100343 19980731 00343 WP 1998 7 31 SCNA98078 1 19980718 A 3350 EMSA299A BATTERY PACK EMBS1392 DOUG DC10 DC1015 3022118 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 153SY 69318 48276 DURING EMERGENCY LIGHT SELF TEST IN THE COCKPIT THE AFT EMERGENCY LIGHTS POWER SUPPLY FAILS. REMOVED AND REPLACED THE A FT CABIN EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK PER MAINTENANCE MANUAL 332301, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A22WE 1998073100344 19980731 00344 WP 1998 7 31 SCNA98079 1 19980723 A 3350 EMSA299A BATTERY EMBS1392 DOUG DC10 DC1015 3022118 WP CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 154SY 64945 48259 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT TEST FROM THE COCKPIT FAILS TEST. REMOVED AND REPLACED BOTH BATTER Y CHARGER UNIT AND BATTERY IN AFT POSITION. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A22WE 1998073100345 19980731 00345 WP 1998 7 31 SCNA98080 1 19980727 A 3244 50003064 TIRE DOUG DC10 DC1015 3022118 WP LT MLG FAILED A SCNA O OTHER O OTHER TO TAKEOFF 1 GL 15 152SY 456 48289 CREW WAS INFORMED AFTER DEPARTURE THAT THE LEFT OUTBOARD (2) MAIN TIRE FAILED. REMOVED AND REPLACED THE NUMBER ONE, TWO AND SIX MAIN WHEEL ASSEMBLIES IN ACCORDANCE WITH MAINTENANCE MANUAL 324101. ALSO, REMOVED AND REPLACED THE NUMBER TWO BRAKE ASSEMBLY IN ACCORDANCE WITH 324301. NO DAMAGE TO THE AIRCRAFT WAS NOTED. 2 L 7 3 4F A22WE 1998073100346 19980731 00346 NM 1998 7 31 SCNA98081 1 19980718 A 2530 OVEN BOEING 727 727259 138408J NM GALLEY DIRTY A SCNA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 289SC 22475 SMOKE WAS OBSERVED COMING OUT FROM A SPACE ABOVE THE NUMBER TWO OVEN IN THE FORWARD GALLEY. CLEANED HEATER ELEMENT AND OPERATED THE OVEN. OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F A3WE 1998073100347 19980731 00347 1998 7 31 DHL98802001 4 19980725 A 3441 INS DOUG DC8 DC873F 302199F WP NR 1/2 MALFUNCTIONED A DHLA A J UNSCHED LANDING DUMP FUEL O OTHER CR CRUISE 1 SO 01 802DH 46076 NR 1 INS DISPLAY FLASHING, ALL OTHER FUNCTIONS NORMAL. NR 2 INS DOES NOT RESPOND TO INPUTS. REALIGNED NR 1 AND NR 2 IN S. 2 L 7 4 4F RT 4A25 1998073100348 19980731 00348 WP 1998 7 31 RRXA98271 1 19980723 A 2612 899097 FIRE LOOP DOUG DC8 DC871 302199A WP NR 1 ENGINE MALFUNCTIONED A RRXA K NONE N FALSE WARNING DE DESCENT 1 WP 15 811AL 46099 NR 1 ENG SHORT CIRCUIT LIGHT FOR FIRE WARNING SYSTEM ILLUMINATED DURING DESCENT. W/N TEST FIRE WARNING SYSTEM, ALL ENG IND NORMAL. INTERMIT FIRE WARNING THROUGH OUT APPROACH, WITH BOTH FIRE AND SHORT LIGHT FLASHING ON AND OFF. REMOVED AN D INSTALLED NEW FIRE LOOPS AND AMP. OPS CHK GOOD AT THIS TIME. CHANGED FWD LT, RT AND AFT RT FIRE LOOPS. 2 L 7 4 4F 4A25 1998073100349 19980731 00349 NE 1998 7 31 ARWA9807130 2 19980725 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21152402 54555 NE NR 1 VIBRATION A ARWA A UNSCHED LANDING E B VIBRATION/BUFFET SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 19 306GB 193U1138 14579 MIA - FLT 501 - GOT 2.4 VIB AT TAKEOFF, NR 1 ENGINE. ABORTED TAKEOFF. ENGINE NR 1 WILL BE REMOVED AND REPLACED. DISCR EPANCIES FINDING WILL BE ACCOMPLISHED DURING ENGINE TEAR DOWN. 2 L 7 3 4F 4 F A23WE E12EU 1998073100353 19980731 00353 1998 7 31 CA980402005 4 19980328 A 6122 B210161C SHAFT WOODWARD DHAV DHC8 DHC8102 2809003 NM PROP GOVERNOR SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 1201 2133123D (CAN) DRIVE SHAFT BETWEEN OVERSPEED GOVERNOR AND REDUCTION GEARBOX WAS FOUND SHEARED DURING TROUBLESHOOTING OF A SLOW TO FEATHER SNAG. PART TOTAL CYCLES: 1,276. 2 H 7 2 4T RT A13NM 1998073100354 19980731 00354 1998 7 31 CA980402008 4 19980313 A 2200 AFCS AIRBUS A319 A319114 NM COCKPIT FAILED W K NONE J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 CA (CAN) CAT3 APPROACH COMPLETED, FLIGHT MODE ANNUNCIATOR FLARE, A/C DID NOT FLARE WHICH RESULTED IN A VERY FIRM 3-POINT LA NDING. AUTOLAND NOT ACCEPTABLE. AUTOFLIGHT SYSTEM TEST CARRIED OUT, NO FAULT FOUND. 2 L 7 2 4F RT A28NM 1998073100355 19980731 00355 WP 1998 7 31 CA980402012 1 19980227 A 2530 OVEN DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 54009 (CAN) ELECTRICAL FUMES DETECTED ON CLIMB-OUT. ELECTRICAL FIRE DRILL CARRIED OUT. GALLEY POWER SWITCHED OFF. SMELL DISS IPATED. THE MIDDLE OVEN POSITION NR 16 FOUND TO BE THE CAUSE OF THE PROBLEM AND WAS ISOLATED. OVEN RECEPTACLE CHANGED A ND CHECKED SERVICEABLE. 2 L 7 2 4F A6WE 1998073100356 19980731 00356 EU 1998 7 31 CA980402013 1 19980127 A 5347 D53112782200 SEAT TRACK AIRBUS 320 A320211 3930320 EU CABIN CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NR 4 AND NR 5 SEAT TRACKS CORRODED UNDER NR 2 GALLEY. SEAT TRACKS CORRODED BEYOND S.R.M. LIMITS. SEAT TRACKS REP LACED OR REPAIRED FOR SINGLE POINTS. 2 L 7 2 4F RT A28NM 1998073100357 19980731 00357 EU 1998 7 31 CA980402014 1 19980127 A 5347 D53112728000 SEAT TRACK AIRBUS 320 A320211 3930320 EU CABIN CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NR 3 SEAT TRACK CORRODED UNDER NR 2 GALLEY. SEAT TRACK REPLACED FOR NUMEROUS CORRODED PLACES OR REPAIRED. 2 L 7 2 4F RT A28NM 1998073100358 19980731 00358 EA 1998 7 31 CA980402015 1 19980306 A 3350 LIGHT ASSY CNDAIR CL600 CL6002B19 EA COCKPIT BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 6330 (CAN) SMOKE IN COCKPIT AND A STRONG ELECTRICAL BURNING SMELL, SMOKE BEGAN TO DISSIPATE AND FLIGHT CONTINUED. GALLEY WAL L CEILING LIGHT ASSY FOUND SHORTED. PART TOTAL CYCLES: 5,289. 2 L 7 2 4F RT A21EA 1998073100359 19980731 00359 EA 1998 7 31 CA980402016 1 19980306 A 3340 LIGHT ASSY CNDAIR CL600 CL6002B19 EA COCKPIT BURNT W K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 6325 (CAN) BURNING SMELL AND THEN NAVIGATION LIGHT CIRCUIT BREAKER TRIPPED. CIRCUIT BREAKER RESET AND BULB REPLACED. UNABLE TO FIND ANYTHING ELSE WRONG. PART TOTAL CYCLES: 5,285. 2 L 7 2 4F RT A21EA 1998073100362 19980731 00362 NM 1998 7 31 CA980403001 1 19980326 A 5522 85520088 PANEL 8552002 DHAV DHC8 DHC8102 2809003 NM ELEVATOR DENTED W A K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 7004 (CAN) PILOT SNAGGED A STIFF ELEVATOR TRIM CONTROL. THE ELEVATOR TRIM LINK P/N 82760164-101 WAS CONTACTING THE ACCESS COV ER WHEN THE ELEVATOR WAS MOVED TO THE FULL NOSE UP OR NOSE DOWN POSITION AND THE ELEVATOR TRIM WAS SET JUST OUT OF THE T AKE OFF POSITION IN THE NOSE DOWN DIRECTION. PANELS WERE TRIMMED.. PART TOTAL CYCLES: 4,846. 2 H 7 2 4T RT A13NM 1998073100364 19980731 00364 NM 1998 7 31 CA980403003 1 19980327 A 5730 SKIN DHAV DHC8 DHC8301 NM LT WING DAMAGED W K NONE C F.O.D. AP APPROACH 1 CA 21096 (CAN) POSSIBLE BIRD STRIKE LEFT WING. LEADING EDGES AND NR 4 AND NR 5 BOOTS DAMAGED. 2 H 7 2 4T RT A13NM 1998073100365 19980731 00365 NM 1998 7 31 CA980403004 1 19980327 A 2910 82970010405 HYD LINE DHAV DHC8 DHC8301 NM MLG FAILED W K NONE K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CA (CAN) SIGNIFICANT AMOUNT OF HYDRAULIC FLUID NOTED ON THE RIGHT ENGINE NACELLE, GEAR DOORS AND TIRES. HYDRAULIC TUBE ASS EMBLY FOR THE MLG DOWN PRESSURE SYSTEM NR 2 REPLACED. 2 H 7 2 4T RT A13NM 1998073100369 19980731 00369 EA 1998 7 31 CA980406004 1 19980320 A 3233 DSC252B40124 LINE DHAV DHC8 DHC8311 1386006 EA NLG RUPTURED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF, LOSS OF NR 2 HYDRAULIC SYSTEM FLUID. AIRCRAFT RETURNED. INSPECTION FOUND FLEX LINE TO NLG DOWNLOC K ACTUATOR BURST. LINE AND HYDRAULIC PUMP REPLACED. 2 H 7 2 4T RT A13NM 1998073100370 19980731 00370 EA 1998 7 31 CA980406005 1 19980319 A 2910 82970010389 LINE DHAV DHC8 DHC8311 1386006 EA HYD SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) DURING INSPECTION, FOUND NR 2 HYDRAULIC SEQUENCE VALVE LINE LEAKING. 2 H 7 2 4T RT A13NM 1998073100371 19980731 00371 EU 1998 7 31 CA980406007 1 19980315 A 5414 HC572H03000024 SKIN BAG BAE146 BAE146200A 1500266 EU NR 1 NACELLE PUNCTURED W A UNSCHED LANDING C F.O.D. CL CLIMB 1 CA 22354 (CAN) AFTER TAKEOFF, AIRCRAFT STRUCK A CANADA GOOSE. LEADING EDGE OUTBOARD OF THE NR 1 ENGINE HAD TO BE REPLACED.. PAR T TOTAL CYCLES: 25,175. 2 H 7 4 4F RT A49EU 1998073100372 19980731 00372 EU 1998 7 31 CA980406009 1 19980324 A 2760 SENSOR BAG BAE146 BAE146200A 1500266 EU MLG CONTAMINATED W D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CA (CAN) ON TAXI, THE MANUAL SPOILER CAUTION LIGHT CAME ON. WOW SENSORS CLEANED AND FAULT CLEARED. 2 H 7 4 4F RT A49EU 1998073100374 19980731 00374 NM 1998 7 31 CA980406011 1 19980323 A 3260 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM LT MLG OUT OF ADJUST W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) AFTER TAKEOFF, THE WOW CAUTION LIGHT CAME ON. LEFT MAIN LANDING GEAR PROXIMITY SENSOR GAP WAS FOUND OUT OF TOLERA NCE. 2 H 7 2 4T RT A13NM 1998073100375 19980731 00375 NM 1998 7 31 CA980406013 1 19980330 A 2613 FIRE LOOP BOEING 737 7372T2 1384491 NM NR 2 ENGINE FAULTY W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 43096 (CAN) DURING CLIMB, NR 2 ENGINE OVERHEAT LIGHT FLICKERED CONTINUOUSLY. NR 2 ENGINE LOWER FIRE DETECTION LOOP WAS REPLAC ED AND THE AIRCRAFT RETURNED TO SERVICE.. PART TOTAL CYCLES: 26,033. 2 L 7 2 4F RT A16WE 1998073100376 19980731 00376 EU 1998 7 31 CA980406014 1 19980327 A 2910 D29010052004 LINE AIRBUS 320 A320211 3930320 EU HYDRAULIC SYS LEAKING W A H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 15609 (CAN) ECAM LOW YELLOW HYDRAULIC QUANTITY INDICATION. ACTION ECAM PROCEDURE LEVEL STABILIZED ABOVE MINIMUM WARNING LEVEL . T/R YELLOW SYSTEM LINE TO T/R IN NR 2 PYLON FOUND DAMAGED CAUSED BY SHEARED RIVET ATTACH BRACKET WEARING INTO LINE. R EPLACED LINE. 2 L 7 2 4F RT A28NM 1998073100377 19980731 00377 NM 1998 7 31 CA980406015 1 19980324 A 3030 856AE13 PITOT HEAT ROSEMOUNT 856AE13 BOEING 737 737275 1384485 NM FUSELAGE FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) AIRCRAFT RETURNED DUE TO LT ELEVATOR PITOT HEAT INOPERATIVE. REPLACED. 2 L 7 2 4F A16WE 1998073100378 19980731 00378 NM 1998 7 31 CA980406016 1 19980401 A 7931 42D107A1 SWITCH BOEING 737 737275 1384485 NM ENGINE MALFUNCTIONED W A B E UNSCHED LANDING EMER. DESCENT ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CA 6742 (CAN) IN CRUISE AN ENGINE OIL BYPASS LIGHT ILLUMINATED. THRUST WAS REDUCED AND THE AIRCRAFT DIVERTED. THE LIGHT WAS ON WHEN THE ENGINE WAS SHUTDOWN. WHEN THE CONNECTION WAS REMOVED THE LIGHT WENT OUT. THE ENGINE OIL FILTER WAS CHECKED FO R CONTAMINATION AND WAS FOUND CLEAR. ENGINE OIL FILTER AND OIL PRESSURE SWITCH WERE REPLACED AND THE AIRCRAFT WAS RETURN ED TO SERVICE. 2 L 7 2 4F A16WE 1998073100379 19980731 00379 NM 1998 7 31 CA980406017 1 19980327 A 5312 69737723 BRACKET BOEING 737 737275 1384485 NM NLG BLKHD IMPROPER PART W H DEACTIVATE SYST/CIRCUITS W INADEQUATE Q C TX TAXI/GRND HDL 1 CA 106 (CAN) A/C GROUNDED DUE TO DAMAGE AT AFT NLG PRESSURE BULKHEAD OF NOSE WHEEL WELL. BRACKET MOUNTED, 69-73772-3 IS A 737- 300 PART AND NOT APPLICABLE TO A 200 SERIES A/C. DAMAGE OCCURRED WHEN LANDING GEAR RETRACTED. PAN NOT REPAIRABLE, REPL ACED.. PART TOTAL CYCLES: 48. 2 L 7 2 4F A16WE 1998073100390 19980731 00390 EU 1998 7 31 CA980406050 1 19980226 A 3240 CZ29284E VALVE AIRBUS 320 A320212 EU NR 1 BRAKE FAILED W O OTHER M OVER TEMP TX TAXI/GRND HDL 1 CA 3865 (CAN) AFTER LANDING, BRAKE NR 1 SERVO VALVE , FIN 15 GG. REPLACED VALVE AND PRESSURE TRANSDUCER. ALSO, REPLACED BRAKE AND STEERING CONTROL UNIT AS A PRECAUTIONARY MEASURE. 2 L 7 2 4F RT A28NM 1998073100397 19980731 00397 NM 1998 7 31 CA980713013 1 19980623 A 2710 CLUTCH DHAV DHC8 DHC8301 NM AILERON MALFUNCTIONED W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA (CAN) AT MAIN LANDING GEAR TOUCHDOWN, A ROLL DISCONNECT OCCURRED. ON ROLLOUT EVERYTHING BACK TO NORMAL, AND RE-ENGAGEME NT AND PROPER ROLL CONTROL OPERATION. SYSTEM CLEANED. 2 H 7 2 4T RT A13NM 1998073100398 19980731 00398 EA 1998 7 31 CA980713028 1 19980622 A 2497 WIRE DHAV DHC6 DHC6300 2802606 EA AUX BATTERY CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) WHILE UNLOADING CARGO, THE HANDLER NOTICED A GLOWING WIRE AT THE AUXILIARY BATTERY COMPARTMENT. THE POSITIVE BATT ERY CABLE WAS FOUND TO BE CHAFED AGAINST THE BATTERY CASE. THIS WAS POSSIBLY DUE TO DISPLACEMENT BY CARGO AND WAS SHORT ED OUT AGAINST THE CASE. 1 H 7 2 3T RT A9EA 1998073100399 19980731 00399 NM 1998 7 31 CA980714016 1 19980624 A 2710 ANGLE DHAV DHC8 DHC8301 NM AILERON INTERFERING W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA (CAN) ROLL DISCONNECT SOMETIMES GETS CAUGHT UP ON THE ANGLE BRACKET THAT MAKES UP THE SUPPORT BOX, WHICH HOLDS THE LEVER ASSY IN PLACE. IT CATCHES WHEN GOING FROM DISCONNECT TO CONNECT. IT CATCHES BETWEEN THE PLATE ASSY ON TOP AND THE EY E END OF THE CABLE. THUS, KEEPING THE CLUTCH FROM FULLY ENGAGING AND CATCHING ON THE FORWARD INBOARD TOP OF THE BOX ANGL E BRACKET. 2 H 7 2 4T RT A13NM 1998073100400 19980731 00400 NM 1998 7 31 CA980714017 1 19980706 A 2710 853104971011103 ANGLE DHAV DHC8 DHC8301 NM AILERON FAILED W K NONE F FLT CONT AFFECTED LD LANDING 1 CA (CAN) THE ANGLE BRACKET FOR THE AILERON SYSTEM HAD BEEN REWORKED PER RD8-53-3620, BUT ROLL DISCONNECT HAPPENED AGAIN. T HE BRACKET WAS AGAIN REWORKED AND AGAIN ON TOUCHDOWN, THE ROLL DISCONNECT HAPPENED. 2 H 7 2 4T RT A13NM 1998073100401 19980731 00401 EU 1998 7 31 MALA976167 1 19980723 A 3350 CONNECTOR SAAB SF340 SF340A 7850100 EU CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 115XJ 340A115 DURING INSPECTION NOTED SEVERAL EMERGENCY EXIT SIGNS INOP. MAINTENANCE RESECURED CANNON PLUG BEHIND GALLEY SWINGOUT. O PS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998073100402 19980731 00402 EU 1998 7 31 MALA976168 1 19980723 A 3260 WEU SAAB SF340 SF340A 7850100 EU E/E COMPT TRIPPED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 109XJ 340A109 AFTER TAKEOFF, THE GEAR HANDLE SELECTED UP, ALL 3 GREEN LIGHTS WENT OUT; HOWEVER, THE AMBER IN TRANSIT HANDLE LIGHT REMA INED ON. HYDRAULIC PUMP CONTINUED TO RUN, PULLED CIRCUIT BREAKER E-8, RECYCLED GEAR. RECEiVED SAME RESULT, NO DRAG EFF ECTS NOTICED, OUT GEAR DOWN AND RETURNED TO DTW. MAINTENANCE COULD NOT DUPLICATE PROBLEM, INSPECTED UPLOCK, DOWNLOCK AN D WOW SWITCHES. NO DAMAGE NOTED. RESET WEU AND PERFORMED WEU CHECK AND GEAR SWING. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998073100403 19980731 00403 NM 1998 7 31 MALA976169 1 19980725 A 2424 51608002 GCU DHAV DHC8 DHC8102 2809003 NM LEFT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 827MA 331 LEFT AC BUS ILLUMINATED UPON CLIMBOUT AFTER TAKEOFF. QRH COMPLETED AND VERFIED CONDITION COULD NOT GET BACK ON LINE. A IRCRAFT RETURNED TO MSP. MAINTENANCE CLEANED CANNON PLUGS ON LEFT AC CONTACTOR BOX AND REPLACED LEFT AC GCU. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998073100404 19980731 00404 NM 1998 7 31 K3HA980093 1 19980726 A 3350 08163000108 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 FORWARD TRACK LIGHTING ONE FOOT SECTION WON'T STAY IN SLOT OR TRACK, LIGHT IS OK. REMOVED AND REPLACED WITH NEW STRIP R EPLACED IAW WITH 33-59-00. 2 L 7 3 4F A3WE 1998073100405 19980731 00405 NM 1998 7 31 AWXA9800157 1 19980724 A 3350 1060091101 LIGHT BOEING 737 737112 1384412 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 EMERGENCY LIGHT SIGN ABOVE DOOR R2 BLINGKING ON AND OFF. REMOVED AND REPLACED EMERGENCY LIGHT ASSY. 2 L 7 2 4F A16WE 1998073100406 19980731 00406 NM 1998 7 31 AWXA9800158 1 19980726 A 5330 SKIN BOEING 737 737277 1384570 NM BS 764 CRACKED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 182AW 22649 SKIN CRACKED AT TRR 17 LT STA 764. REPAIRED PER SRM 53-30-03 FIG 25. 2 L 7 2 4F RT A16WE 1998073100407 19980731 00407 WP 1998 7 31 CALA9801348 1 19980727 A 5312 BULKHEAD FITTING DOUG DC9 DC932 3022066 WP BS 69 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A 3 INCH CRACK IN TIE FITTING ON FORWARD SIDE OF BS 69 BULKHEAD AT TOP OF LT INTERCOSTAL AND A 3 INCH C RACK WAS FOUND IN TIE FITTING ON FORWARD SIDE OF BS 69 BULKHEAD AT TOP OF RT INTERCOSTAL. THE TIE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-10-02 AND 53-11-1. 2 L 7 2 4F A6WE 1998073100408 19980731 00408 WP 1998 7 31 CALA9801349 1 19980727 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A 1 INCH CRACK IN RT LAV ANGLE, LOWER SIDE OF Z-63 FROM END FASTENER AT AFT PRESSURE BULKHEAD. THE ANG LE WAS REPAIRED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998073100409 19980731 00409 WP 1998 7 31 CALA9801350 1 19980727 A 5210 PAN DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .5 INCH CRACK AT UPPER RADIUS OF MAIN CABIN DOOR PAN UPPER HINGE CUTOUT. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 33. 2 L 7 2 4F A6WE 1998073100410 19980731 00410 WP 1998 7 31 CALA9801351 1 19980728 A 5312 BULKHEAD TEE DOUG DC9 DC932 3022066 WP BS 996 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .5 INCH CRACK IN AFT PRESSURE BULKHEAD TEE CAP AT RT LAV BETWEEN LONGERON 15R AND 16R, STA 996. THE TEE CAP WAS REPLACED IAW SRM 53-03, FIGURE 37A. 2 L 7 2 4F A6WE 1998073100411 19980731 00411 NM 1998 7 31 CALA9801352 1 19980727 A 5730 PANEL BOEING 757 757224 1384958 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57111 27301 INSPECTION FOUND THE RT WING LEADING EDGE CRACKED IN TWO PLACES BETWEEN SLATS NR 7 AND NR 8. THE CRACKS WERE 5.5 AND 9. 5 INCHES LONG. THE SURFACE WAS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPECTION AND PERMANENT REPAIR PER ECRA 5720-01662, REV A. 2 L 7 2 4F RT A2NM 1998073100412 19980731 00412 NM 1998 7 31 CALA9801353 1 19980727 A 5730 PANEL BOEING 757 757224 1384958 NM LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 57111 27301 INSPECTION FOUND A 10.5 INCH CRACK IN LT WING LEADING EDGE AT THE OUTBOARD END OF NR 1 LEADING EDGE SLAT. THE SURFACE W AS PREPARED IAW SRM 51-70-06. THE AREA WAS REPAIRED IAW ECRA 5720-01662. A DIP WAS ISSUED FOR FOLLOW-UP INSPECTION AND PERMANENT REPAIR PER ECRA 5720-01662. 2 L 7 2 4F RT A2NM 1998073100413 19980731 00413 NM 1998 7 31 CALA9801354 1 19980728 A 5730 PANEL BOEING 757 757224 1384958 NM RT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12114 27556 INSPECTION FOUND A 10 INCH LONGITUDINAL CRACK ALONG UPPER SURFACE OF RT WING LEADING EDGE BETWEEN SLAT NR 7 AND NR 8. T HE AREA WAS REPAIRED IAW ECRA 5720-01665. A DIP WAS INITIATED TO INSPECT FOR DELAMINATION AND WEAR EACH 1000 HOURS AND ACCOMPLISH A PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK, WHICHEVER OCCURS FIRST. 2 L 7 2 4F RT A2NM 1998073100414 19980731 00414 NM 1998 7 31 CALA9801355 1 19980728 A 5730 PANEL BOEING 757 757224 1384958 NM LT WING LE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12114 27556 INSPECTION FOUND A 7 INCH LONGITUDINAL CRACK ALONG UPPER SURFACE OF LT WING LEADING EDGE BETWEEN SLAT NR 3 AND NR 4. TH E AREA WAS REPAIRED IAW ECRA 5720-01665. A DIP WAS INITIATED TO INSPECT FOR DELAMINATION AND WEAR EACH 1000 HOURS AND A CCOMPLISH PERMANENT REPAIR WITHIN 18 MONTHS OR NEXT C-CHECK, WHICHEVER OCCURS FIRST. 2 L 7 2 4F RT A2NM 1998073100415 19980731 00415 1998 7 31 COMA9810166 2 19980727 A 7532 97962641 BLEED VALVE EMB 120 EMB120RT SO RT ENGINE MALFUNCTION A COMA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 261CA 18325 357 120254 RIGHT HAND BLEED AIR OVERHEAT WARNING ON. REPLACED THE HIGH PRESSURE BLEED VALVE. 2 L 7 2 4T RT A31SO 1998073100416 19980731 00416 WP 1998 7 31 UPS98827243 1 19980725 A 5230 DOOR DOUG DC8 DC873F 302199F WP CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-B CK, NR 2 PIT DOOR, FWD UPPER CORNER CRACKED WHERE ROLLER SUPPORT BOLTS TO DOOR FRAME. REPAIRED PER DC 8 52-02-0 PG 13. 2 L 7 4 4F RT 4A25 1998073100417 19980731 00417 WP 1998 7 31 UPS98827244 1 19980725 A 3350 BULB DOUG DC8 DC873F 302199F WP CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 814UP 46090 INSPECTION TYPE-N/A, MAIN ENTRY DOOR EMERG LIGHTS INOP. RELAMPED EMER LIGHTS, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1998073100418 19980731 00418 NM 1998 7 31 98FDEA00470 1 19980723 A 5753 6521630188 SKIN BOEING 727 72725C 138400H NM RT TE FOREFLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR 0455 005 STA-PAE: STEEL RUBSTRIP IS DISBONDED ON R/W I/B FOREFLAP I/B END. *** S/D *** REPAIRED R/W I/B FO REFLAP I/B END UPR & LWR SURFACES PER FEDEX SRM 51-40-6 & DRAWING 65-32738. 2 L 7 3 4F A3WE 1998073100419 19980731 00419 NM 1998 7 31 98FDEA00471 1 19980723 A 5320 65196044 WEB BOEING 727 72721C 138400M NM BS 1136 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 WHILE WORKING NR 0840, FOUND CORROSION ON SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 ON UNDER SURFACE OF WEB. *S/D* R EPAIRED SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 IAW FED-EX SRM 51-40-2. 2 L 7 3 4F A3WE 1998073100420 19980731 00420 NM 1998 7 31 98FDEA00472 1 19980724 A 3230 SENSOR BOEING 727 727233 138408A NM LT MLG FAILED A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 281FE 22348 ON INITIAL T/O, LANDING GEAR HANDLE COULD NOT BE RAISED PAST LEVER LOCK. RAN LANDING GEAR LEVER LATCH FAIL TO RELEASE C HECKLIST TO STEP 7 AND RETRACTED GEAR USING GEAR LEVER LATCH TRIGGER. DISCONNECTED SAFETY SENSOR AT LT MAIN GEAR. DISC ONNECTED NOSE GEAR. PERFORMED OPERATIONAL CHECK OF LAND GEAR HANDLE GEAR LEVER LATCH RELEASE NORMAL. OPERATIONAL CHECK NORMAL ON GROUND MEM. RECONNECTED SAFETY SENSOR AND NOSE GEAR MAINTENANCE MANUAL 32-31-0. 2 L 7 3 4F RT A3WE 1998073100421 19980731 00421 EU 1998 7 31 98FDEA00474 1 19980727 A 7930 684V100 BYPASS VALVE AIRBUS 310 A310222 3930315 EU NR 2 ENGINE FAILED A FDEA C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN J WARNING INDICATION TO TAKEOFF 1 SO 25 422FE 346 T/O ABORT NR 2 ENGINE OIL TEMP WENT TO 250 DEG C, AT THROTTLE ADVANCE. TEMP REMAINED AT 185 DURING TAXI IN. ENGINE SHU T DOWN. REMOVED AND REPLACED FUEL OIL COOLER BYPASS VLV PER M/M 79-21-05, REMOVED AND REPLACED OIL TEMP SENSOR BULB PER 79-32-11. CHECKED OIL CHIP DETECTOR IS CLEAN, ALSO REMOVED AND REPLACED SYSTEM DATA ANALOG CONVERTER PER M/M 31-50-00 ENGINE RUN PER JET RUN HANDBOOK, INDICATION NORMAL. ACFT RELEASED TO SERVICE. 2 L 7 2 4F RT A35EU 1998073100422 19980731 00422 NM 1998 7 31 98UAL900331 1 19980717 A 2421 IDG SUNDSTRAND MR24114 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 654UA G0540 25392 RIGHT ENGINE GENERATOR INOP LIGHT ILLUMINATED IN FLIGHT. RETURNED TO LHR. *S/D* REPLACED RIGHT (NR 2) INTEGRATED DRI VE GENERATOR IDG, MR24114 DASH G0540 HAD INTERNAL PISTON FAILURE. 2 L 7 2 4F 4 F RT A1NM E24NE 1998073100423 19980731 00423 NM 1998 7 31 98UAL900332 1 19980720 A 3350 LIGHTS AIRBUS A319 A319131 NM CABIN FAILED TEST A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 759 AIRCRAFT EMERGENCY LIGHTS OPERATE NORMALLY USING COCKPIT SWITCH, BUT WILL NOT TEST THRU THE CIDS. 2 L 7 2 4F RT A28NM 1998073100424 19980731 00424 NM 1998 7 31 98UAL900333 1 19980717 A 3350 LIGHT BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 991UA 21981 SERVICE DOOR EMERGENCY EXIT LIGHT IS INOP. 2 L 7 2 4F 4 F A16WE E2EA 1998073100425 19980731 00425 NM 1998 7 31 98UAL900334 1 19980720 A 2613 356802255 DETECTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE OUT OF POSITION A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 WP 29 7253U 21400 ON TAKEOFF, NR 2 ENGINE LOWER AFT BODY OVERHEAT LIGHT CAME ON. REDUCED POWER AND LIGHT WENT OUT. BY KEEPING REDUCED PO WER, LIGHT STAYED OUT. RETURNED TO DEN. *S/D* MAINTENANCE RAN ENGINE, APU AND OPERATED A/C PACKS, NO LEAKS FOUND. RE POSITIONED EMPENNAGE DETECTOR. NO FURTHER PROBLEM REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1998073100426 19980731 00426 NM 1998 7 31 98UAL900335 1 19980719 A 3350 6012541LB BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7453U 21907 EMERGENCY EXIT SIGN ABOVE AFT EXIT DOOR INOPERATIVE. *S/D* REPLACED CHARGER AND BATTERY. 2 L 7 3 4F 4 F A3WE E2EA 1998073100428 19980731 00428 NM 1998 7 31 98UAL900337 1 19980718 A 2120 SENSOR ROSEMOUNT 123CH1A BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT COOLING SYST FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 317UA 23949 RIGHT EQUIPMENT COOLING SUPPLY EXHAUST OFF LIGHT ILLUMINATED DURING CLIMB, LEVEL OFF, AND THE FIRST PART OF DESCENT. SE LECTING ALTERNATE DID NOT WORK-IN NORMAL. ON THE GROUND THE LIGHT EXTINGUISHES. COULD ONLY DUPLICATE IN FLIGHT. *S/D* PROBLEM WAS CAUSED BY THE LOW FLOW SENSOR. AFTER REPLACEMENT OF THE LOW FLOW SENSOR, SYSTEM OPERATED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1998073100429 19980731 00429 NM 1998 7 31 98UAL900338 1 19980701 A 2560 131W18401101 GIRT BAR BOEING 777 777222 1385219 NM PWA SLIDE/ RAFT CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 DURING EXAMINATION OF FOUR SLIDE RAFT ASSEMBLIES IN THE OVERHAUL WORK CENTER, THREE EACH (P/N 31W1840-1101) GIRT BARS WE RE FOUND TO HAVE CRACKS IN THE ALUMINUM TUBE. CRACK LENGTHS RANGE BETWEEN 1 AND 3 INCHES AND RUN LONGITUDINALLY ALONG T HE WELD SEAM BETWEEN THE RIVETS. *S/D* PRELIMINARY EVALUATION SUGGESTS CRACKING RESULTED FROM PRELOADING OF THE GIRT B AR TUBE BY RIVET ATTACHMENT OF THE END FITTINGS IN ASSOCIATION WITH PROTRUDING WELD SEAMS. THE AFFECTED -1101 PARTS WER E REPLACED WITH LATEST -1103 CONFIGURATION GIRT BARS. DEFECTIVE PARTS HAVE BEEN SENT TO BOEING FOR FURTHER ANALYSIS. 2 L 7 2 4F RT T0001SE 1998073100430 19980731 00430 NM 1998 7 31 98UAL900339 1 19980720 A 2150 213W31303 TORQUE TUBE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT RAM AIR DOOR SHEARED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 774UA 2585 26936 LOUD VIBRATION ON CLIMBOUT. RETURNED TO LHR. PRELIMINARY INVESTIGATION AT LHR FOUND DAMAGED LEFT PACK RAM DOOR. *S/D* FOUND LT PACK RAM AIR INLET DOOR TORQUE TUBE ASSY (213W3130-3) SHAFT SHEARED. REPLACED TORQUE TUBE ASSY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998073100431 19980731 00431 NM 1998 7 31 98UAL900340 1 19980720 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 FORWARD COACH CEILING EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED BATTERY. 2 L 7 3 4F 4 F A3WE E2EA 1998073100432 19980731 00432 NM 1998 7 31 98UAL900341 1 19980720 A 2530 CONTROL PANEL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY FAILED A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7294U 21572 FLIGHT ATTENDANT NOTICED SMOKE AND SPARKS COMING FROM THE ELECTRICAL CONTROL PANEL ON THE FORWARD GALLEY ABOVE THE HOT P LATE. 2 L 7 3 4F 4 F A3WE E2EA 1998073100433 19980731 00433 NE 1998 7 31 98UAL900343 2 19980720 A 7230 COMPRESSOR BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING Y ENGINE STOPPAGE CR CRUISE 1 WP 29 104UA 2105 26902 727742 NR 3 ENGINE BANGED AND SPOOLED DOWN FL330. *S/D* HIGH PRESSURE COMPRESSOR FAILURE. SUSPECT 5TH STAGE BLADE FAILED. E NGINE SENT TO PRATT WHITNEY FOR WARRANTY REPAIR AND FAILURE ANALYSIS. 2 L 7 4 4F 4 F RT A20WE E24NE 1998073100434 19980731 00434 NM 1998 7 31 98UAL900344 1 19980721 A 2781 CONNECTOR BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 1 LE FLAP LOOSE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK F FLT CONT AFFECTED TO TAKEOFF 1 WP 29 155UA 20104 DURING TAKEOFF, NR 1 LT LEADING EDGE AMBER AND GREEN LIGHT FLICKERED, ALONG WITH INTERMITTENT WARNING HORN. ABORTED TAK EOFF AT 90 KTS. *S/D* THE INDICATION PROBLEM WAS CAUSED BY A LOOSE PIN (PIN 9) IN CONNECTOR DM876B FOR THE M876 PNEUMA TIC DRIVE UNIT. THE PIN WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1998073100435 19980731 00435 NM 1998 7 31 98UAL900345 1 19980722 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 EMERGENCY EXIT SIGN ABOVE DOOR 1L DIM AND THEN FADES OUT. *S/D* REMOVED AND REPLACED BATTERIES. 2 L 7 3 4F 4 F A3WE E2EA 1998073100436 19980731 00436 NM 1998 7 31 98UAL900346 1 19980722 A 3350 900835A BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7442U 21896 LEFT FORWARD EMERGENCY OVERWING ILLUMINATION LIGHT INOPERATIVE. *S/D* REPLACED BATTERY ASSEMBLY, OPS CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998073100437 19980731 00437 NM 1998 7 31 98UAL900347 1 19980703 A 5330 SKIN BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE BS 1290 CORRODED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 608UA 21869 SUSPECT CORROSION BETWEEN TWO EXISTING REPAIRS AT STA 1290, BELLY OF AIRCRAFT FORWARD OF NR 3 VHF ANTENNA. 2 L 7 2 4F 4 F RT A1NM E3NE 1998073100438 19980731 00438 NM 1998 7 31 98UAL900348 1 19980722 A 7603 315T304014 CONTROL BOX BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT THROTTLE FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 610UA 21871 709669 AFTER DEPARTURE BOS, LEFT THROTTLE FROZEN APPROX 2 INCHES FROM FIREWALL. DIVERTED ORD. OVERWEIGHT LANDING. NO ALERTS D ECLARED. *S/D* THE PROBLEM WAS ISOLATED TO BINDING WITHIN THE FUEL CONTROL PUSH-PULL CONTROL BOX. THE CONTROL BOX WAS REPLACED AND THE THROTTLES RERIGGED PER 767-200 MM 76-11-02. THERE HAS BEEN NO FURTHER REPORTS OF PROBLEMS WITH THIS S YSTEM. 2 L 7 2 4F 4 F RT A1NM E3NE 1998073100439 19980731 00439 NM 1998 7 31 98UAL900349 1 19980722 A 2824 VALVE J C CARTER C 405744 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 CROSSFEED STUCK A UALA A J UNSCHED LANDING DUMP FUEL O OTHER NR NOT REPORTED 1 WP 29 7458U 21912 RETURNED TO ORD AFTER DUMPING FUEL DUE TO CROSSFEED PROBLEMS. *S/D* NR 1 CROSSFEED VALVE STUCK IN THE OPEN POSITION. R EPLACED THE NR 1 CROSSFEED VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998073100440 19980731 00440 NM 1998 7 31 98UAL900350 1 19980722 A 2910 HYD FLUID BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE B-HYD SYST LOST A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7278U 21425 LOST B-SYSTEM HYDRAULIC PRESSURE AND QUANTITY. 2 L 7 3 4F 4 F A3WE E2EA 1998073100441 19980731 00441 NM 1998 7 31 98UAL900352 1 19980724 A 3510 9F576750524 FITTING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7277U 21424 CREW REPORTED SMALL POPPING SOUND FOLLOWED BY A LOSS OF CREW OXYGEN. *S/D* BULKHEAD FITTING ON HOSE FROM O2 REGULATOR TO BULKHEAD WAS FOUND BROKEN. HOSE WAS REPLACED AND SYSTEM PRESSURE CHECKED. 2 L 7 3 4F 4 F A3WE E2EA 1998073100442 19980731 00442 WP 1998 7 31 ABXA9800640 1 19980723 A 2510 56410321F SEAT ASSY DOUG DC8 DC863 302198A WP COCKPIT FAILED A ABXA K NONE O OTHER CL CLIMB 1 GL 23 818AX 2445 46075 FLIGHT ENGINEER'S SEAT WOULD NOT HOLD IN VERTICAL POSITION. SEAT FELL SEVERAL TIMES DURING DIFFERENT PHASES OF FLIGHT. REPLACED FLIGHT ENGINEER'S SEAT ASSEMBLY. 2 L 7 4 4F 4A25 1998073100443 19980731 00443 WP 1998 7 31 ABXA9800638 1 19980726 A 7931 779606 RELIEF VALVE DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE MALFUNCTION A ABXA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 GL 23 821AX 46116 669301 NR 4 ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED ON DESCENT. OIL PRESSURE READ 30 PSI. THROTTLE WAS IN IDLE. SHUT DOWN NR 4 ENGINE. WINDMILLING OIL PRESSURE WAS 3 PSI. REPLACED OIL PRESSURE RELIEF VALVE IAW PRATT AND WHITNEY MM 72-00 AN D ADJUSTED OIL PRESSURE. GROUND RAN ENGINE, OPS CHECKED GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1998073100444 19980731 00444 NM 1998 7 31 DHL98706003 1 19980624 A 3246 26045611 WHEEL BOEING 727 72722C 138400F NM NR 4 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 706DH 19192 ON SERVICE CHECK, FOUND NR 4 WHEEL AND TIRE ASSY BROKEN LUGS HITTING BRAKE ASSY. INSPECTED, INNER WHEEL HALF CRACKED AN D BROKEN. REMOVED AND REPLACED NR 4 MAIN TIRE AND WHEEL AND NR 4 BRAKE PER MM 32-45 AND 32-41. INSPECTED AXLE SLEEVE, NO DEFECT NOTED. INSPECTED FOR HARD LANDING PER 5-51-61. NO DEFECTS NOTED. 2 L 7 3 4F A3WE 1998073100445 19980731 00445 WP 1998 7 31 DHL98805002 1 19980728 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 140-160 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 FUSELAGE LT O/B BETWEEN FS 140 TO STA 160 APPROX LONGERONS L-25L AND L-26L HAS A CRACK. CUT OUT DAMAGED SECTION BETW EEN FS 140 AND 160. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998073100446 19980731 00446 WP 1998 7 31 DHL98807005 1 19980727 A 2752 FITTING DOUG DC8 DC873F 302199F WP WS 98 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 RIGHT WING I/B FLAP ACTUATOR SUPPORT FITTING FOUND BROKEN AT STA 98. REMOVED AND REPLACED FITTING PER DC-8 MM 27-51- 9. 2 L 7 4 4F RT 4A25 1998073100447 19980731 00447 WP 1998 7 31 DHL98807006 1 19980728 A 5730 COVER DOUG DC8 DC873F 302199F WP WS 98 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 807DH 45990 RT WING I/B FLAP ACTUATOR SUPPORT COVER PANEL DAMAGED WING LOWER SURFACE STA 98. REMOVED DAMAGED PANEL, CUT OUT DAMAGE D SECTION OF INTERNAL AND EXTERNAL SKIN, EXTERNAL SKIN FILLER, 3.75 X 2.5, EXTERNAL DOUBLER, 6 X 6.25 INTERNAL FILLER 4. 25 X 4.125. FABRICTED AND INSTALLED PARTS PER SRM 51-1-9. 2 L 7 4 4F RT 4A25 1998073100448 19980731 00448 CE 1998 7 31 BIER9804052 1 19980716 A 5312 50221004849 RIB CESSNA 421 421B 2076014 CE LT&RT WING CRACKED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 69924 421B0553 FOUND RIB CRACKED AS REFERENCED IN CESSNA SL ME76-2. INSTALLED KIT SK414-8E. 1 L 7 2 3O A7CE 1998073100449 19980731 00449 WP 1998 7 31 AALA981024 1 19980526 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 203AA 49145 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN AFT CABIN INOPERATIVE. REPLACED EMEREGENCY EXIT FLOOR PATH LIGHT STRIP CONNECTORS IN AFT CABIN AND AS A PRECAUTIONARY. REPLACED BATTERY PACKS. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998073100450 19980731 00450 NM 1998 7 31 AALA981118 1 19980603 A 5280 6517563205 SEAL BOEING 727 727223 1384074 NM NLG DOOR STUCK A AALA K NONE O OTHER AP APPROACH 1 SW 07 868AA 21373 ORD - FLT 1523 - DURING APPROACH, WHEN GEAR HANDLE MOVED TO DOWN POSITION BOTH MAIN LANDING GEARS EXTENDED NORMALLY. NO SE GEAR REMAINED RETRACTED FOR SEVERAL SECONDS MORE FOLLOWED BY A LOUD BANG AND THEN NORMAL NOSE GEAR EXTENSION. LANDED ORD WITHOUT INCIDENT. REMOVED EXCESSIVE PAINT ON NOSE GEAR DOOR SEAL. REPAINTED DOOR SEAL, DOES'NT RUB. LUBED NOSE G EAR STRUT AND ACCOMPLISHED RETRACTION AND EXTENSION CHECK PER MM. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998073100451 19980731 00451 NM 1998 7 31 MASA98094 1 19980422 A 2910 82970010477 HYDRAULIC LINE DHAV DHC8 DHC8202 2809007 NM LT ENGINE SPLIT A MASA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 449YV 449 FLT 7544 - DEN-DRO - AFTER TAKEOFF, THE CREW RAISED THE FLAPS AND NOTICED THAT THE NR 1 HYDRAULIC SYSTEM WAS LOSING PRES SURE AND FLUID. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC RETURN LINE AND ENGINE DRIVEN HYDRAULIC PUMP. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998073100452 19980731 00452 NM 1998 7 31 MASA98101 1 19980508 A 3350 6515002 SIGN DHAV DHC8 DHC8202 2809007 NM CABIN MISSING A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 445YV 445 FLT 7600 - DEN-GJT - CREW REPORTED LOWER EMERENCY EXIT SIGN. MAINTENANCE REPLACED PLACARD. AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A13NM 1998073100453 19980731 00453 NM 1998 7 31 MASA98119 1 19980603 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A MASA K NONE L NO TEST CR CRUISE 1 SW 07 454YV 454 FLT 9454 - TERMINATING IN GJT, CREW REPORTED THE PORTABLE EMERGENCY LIGHT WAS INOP. GJT MAINTENANCE REPLACED THE LIGHT ASSEMBLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998073100454 19980731 00454 CE 1998 7 31 MASA98123 1 19980605 A 5210 1294000371 SEAL BEECH 1900 1900D 1154162 CE DOOR WORN A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 64YV UE64 FLT 5506 - JAX-FLL, AT 13,000 FT, THE PASSENGER DOOR ANNUNCIATOR ILLUMINATED. PILOT NOTED THE DOOR SEAL HAD BEEN WHISTL ING THROUGH 10,000 FT. CREW DECLARED AN EMERGENCY AND RETURNED TO JAX WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AN D REPLACED THE DOOR SEAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998073100455 19980731 00455 CE 1998 7 31 MASA98125 1 19980609 A 3242 11480083 BRAKE ASSY BEECH 1900 1900D 1154162 CE RT MLG UNSERVICEABLE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 3YV UE3 FLT 5021 - IFP-PHX - IN PHX, CREW REPORTED THE RIGHT BRAKES WOULD NOT PROVIDE ADEQUATE BRAKING ACTION. MAINTENANCE REPL ACED THE RIGHT BRAKE AND BLED THE BRAKES. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998073100456 19980731 00456 NM 1998 7 31 MASA98122 1 19980604 A 5542 85540021 COVER PLATE DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 447YV 447 DUE TO OTHER ACFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE. A/C'S RUDDER WAS INSPECTED IN PALM SPRINGS. FWD RUDDER LWR RIB END CAP ACCESS PNL COVER PLATE HAD SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCE SS PNL COVER PLATE. DEHAV WAS CONTACTED AND ADAR APPROVED REPAIR DRAWING WAS GENERATED TO ALLOW THIS AIRCRAFT TO CONTIN UE OPS FOR 100 FLT CYCLES. THE A/C CONTINUED OPS FOR 8.9 HOURS, THEN THE FORE AND AFT RUDDERS WERE REMOVED. A NEW ACCE SS PANEL COVER PLATE WAS FABRICATED AND INSTALLED. THE RIB END CAP WAS REPLACED IAW MESA AIRLINES, INC REPAIR ORDER NR DHC82-55-0001-GJT. THE RUDDERS WERE REINSTALLED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998073100457 19980731 00457 NM 1998 7 31 98ZZZM508 1 19980604 A 5541 85540026101 RIB DHAV DHC8 DHC8202 2809007 NM RUDDER CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 447YV 447 DUE TO OTHER ACFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE. A/C'S RUDDER WAS INSPECTED IN PALM SPRINGS. FWD RUDDER LWR RIB END CAP ACCESS PNL COVER PLATE HAD SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCE SS PNL COVER PLATE. DEHAV WAS CONTACTED AND ADAR APPROVED REPAIR DRAWING WAS GENERATED TO ALLOW THIS AIRCRAFT TO CONTIN UE OPS FOR 100 FLT CYCLES. THE A/C CONTINUED OPS FOR 8.9 HOURS, THEN THE FORE AND AFT RUDDERS WERE REMOVED. A NEW ACCE SS PANEL COVER PLATE WAS FABRICATED AND INSTALLED. THE RIB END CAP WAS REPLACED IAW MESA AIRLINES, INC REPAIR ORDER NR DHC82-55-0001-GJT. THE RUDDERS WERE REINSTALLED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998073100458 19980731 00458 NM 1998 7 31 98ZZZM509 1 19980527 A 5541 85540026101 RIB DHAV DHC8 DHC8202 2809007 NM RUDDER DAMAGED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 446YV 446 DUE TO OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE, A/C'S RUDDER WAS INSPECT ED WHILE THE AIRCRAFT WAS INSPECTED DURING ROUTINE MAINTENANCE. THE FORWARD RUDDER LOWER RIB END CAP ACCESS PANEL COVER PLATE WAS NOTED TO HAVE SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCESS PANEL COVER PLATE AND THE RIB END CAP HAD SE VERAL CRACKS. THE FORE AND AFT RUDDERS WERE REMOVED, A NEW ACCESS PANEL COVER PLAT FABRICATED AND INSTALLED AND THE RIB END CAP WAS REPLACED IAW RO NR DHC82-55-0001-GJT. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVIC E. (M) 2 H 7 2 4T RT A13NM 1998073100459 19980731 00459 NM 1998 7 31 98ZZZM510 1 19980527 A 5541 85540026101 RIB DHAV DHC8 DHC8202 2809007 NM RUDDER CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 437YV 437 DUE TO THE OTHER AIRCRAFT BEING NOTED WITH FORE RUDDER LOWER RIB END CAP AND/OR COVER PLATE DAMAGE. A/C'S RUDDER WAS IN SPECTED WHILE THE A/C WAS INSPECTED DURING THE NORMAL FLIGHT SCHEDULE IN DEN BY A MECHANIC DISPATCHED OUT OF THE PRIMARY MAINTENANCE FACILITY. THE FWD RUDDER LOWER RIB END CAP ACCESS PANEL COVER PLATE WAS NOTED TO HAVE SEVERAL RIVETS THAT WERE PULLED THROUGH THE ACCESS PANEL COVER PLATE AND THE RIB END CAP HAD SEVERAL CRACKS. THE AIRCRAFT WAS FERRIED TO GR AND JUNCTION WHERE THE FORE AND AFT RUDDERS WERE REMOVED. A NEW ACCESS PANEL COVER PLATE WAS FABRICATED AND INSTALLED A ND THE RIB END CAP WAS REPLACED IAW RO NR DHC82-55-0001-GJT. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETURNED 2 H 7 2 4T RT A13NM 1998073100460 19980731 00460 NM 1998 7 31 98ZZZM511 1 19980527 A 5541 85540062101 RIB DHAV DHC8 DHC8202 2809007 NM RUDDER CRACKED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 454YV 454 DEN LINE MX PERSONNEL WERE REPLACING A TAIL NAV BULB WHEN THEY NOTICED A PIECE OF THE FORE RUDDER HANGING DOWN ON THE TA ILCONE OF THE AIRCRAFT. FURTHER INSPECTION, FOUND THE FORE RUDDER LOWER RIB END CAP HAD SEVERAL CRACKS AND THE ACCESS P ANEL COVER PLATE HAS ALMOST ALL OF THE ATTACHING RIVETS PULLED THROUGH. ALLOWING THE COVER PLATE TO HANG DOWN ON THE TA ILCONE OF THE AIRCRAFT. THE AIRCRAFT WAS FERRIED TO GJT, WHERE THE FORE AND AFT RUDDERS WERE REMOVED. A NEW ACCESS PAN EL COVER PLATE FABRICATED AND INSTALLED AND THE RIB END CAP WAS REPLACED IAW RO NR DHC82-55-0001 GJT. THE RUDDERS WERE REINSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998073100461 19980731 00461 NM 1998 7 31 MZZA98177 1 19980612 A 2910 07291030145 LINE BOEING 727 727227 1384078 NM MAIN HYD SYSTEM CHAFFED A MZZA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 13 89427 21365 GUM - FLT 953 - AFTER DEPARTURE AT CRUISE FLT 310, HYD SYSTEM 'A' QTY BEGAN TO DROP SLOWLY. THE QTY DROPPED STEADILY FR OM 4.3 GALLONS TO 2.6 GALLONS IN APPROX 20 MINUTES. THE QTY STABILIZED AT 2.6 GALLONS. AIR RETURN TO GUAM. MAINTENANC E T/S SYSTEM FOUND RIGID LINE ON 'B' SYSTEM SUPPLY LINE CHAFING. REMOVED FAULTY LINE AND INSTALLED SERVICEABLE FLEX-LIN E (HOSE) PER MM SEC 29-00. SERVICED AS REQUIRED, OPS CNA LEAK CHECKED GOOD. NEEDS TO ISSUE DIP TO REPLACE FLEX LINE WI TH RIGID LINE. (M) 2 L 7 3 4F A3WE 1998073100462 19980731 00462 NM 1998 7 31 MZZA98159 1 19980522 A 2780 07278030010 SWITCH BOEING 727 727224 1384076 NM NR 1 LE FLAP MALFUNCTIONED A MZZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 69742 22251 FLT 956 - GUM - AFTER AIRBORNE, CREW CALLED TO ADVISED AIR RETURN DUE TO NR 1 LEADING EDGE FLAPS PROBLEM. NR 1 LE FLAPS DISAGREEMENT WITH FLAP HANDLE POSITION, RED INTRANSIT LIGHT STAYS ON. S/O PANEL SHOWS NR 1 LE FLAPS SHOWS DISAGREEMENT WITH FLAP HANDLE. MAINTENANCE T/S SYSTEM CONFIRMED BAD LE FLAPS SWITCH. REPLACED SWITCH AND OPS CHECK PER MM 27-82-1, GROUND CHECK IS GOOD. AIRCRAFT RELEASED FOR FLIGHT WITH NO FURTHER INCIDENT. (M) 2 L 7 3 4F A3WE 1998073100463 19980731 00463 NM 1998 7 31 MZZA98160 1 19980527 A 2782 651781820 ACTUATOR BOEING 727 727264 138408M NM LT LE FLAPS RUPTURED A MZZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 13 625DH 55449 20780 MNL - FLT 876/27 - AIRCRAFT AIR RETURNED DUE TO LOSS OF A-SYSTEM HYDRAULIC FLUID. FOUND NR 1 LE FLAP ACT RUPTURED. LOG PAGE REMAINS OPEN AND NOT ENTERED, AWAITING SPARES. FLIGHT CONTINUED USING AIRCRAFT 435. (X) 2 L 7 3 4F A3WE 1998073100464 19980731 00464 NM 1998 7 31 MZZA98176 1 19980608 A 5610 5893543129 WINDOW BOEING 727 727224 1384076 NM COCKPIT CRACKED A MZZA A J UNSCHED LANDING DUMP FUEL O OTHER CR CRUISE 1 WP 13 79743 22252 GUM - FLT 956 - AIR RETURN DUE TO PILOT WINDSHIELD CRACKED. MAINTENANCE REMOVED AND REPLACED L-1 WINDOW PER MM 56-11-11 . RESTORED AIRCRAFT TO ORIGINAL CONFIGURATION. RELEASED AIRCRAFT FOR SERVICE. (M) 2 L 7 3 4F A3WE 1998073100465 19980731 00465 NM 1998 7 31 AALA981199 1 19980619 A 2560 SWITCH BOEING 767 767223 1385123 NM LT WING FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 302AA 22308 LAX - FLT 10 - AFTER TAKEOFF LAX, AIR INTERRUPTURED WITH LEFT WING EVACUATION SLIDE EICAS MESSAGE. RETURN AND LANDED LA X WITHOUT INCIDENT. REPLACED AND ADJUSTED BOTH PROXIMITY SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998073100466 19980731 00466 WP 1998 7 31 AALA981211 1 19980619 A 3230 AYG70505507 VALVE DOUG DC10 DC1030 3023501 WP RT MLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 144AA 47848 HNL - FLT 102 - AFTER TAKEOFF HNL, RT MAIN GEAR DOOR WOULD NOT CLOSE. RECYCLED GEAR DOOR, REMAINED OPEN. RETURNED HNL AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR SELECTOR CONTROL VALVE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 3 4F A22WE 1998073100467 19980731 00467 1998 7 31 AALA981170 4 19980610 A 2565 CBB3334501 SLIDE BOEING 727 727223 1384074 NM R1 DOOR MALFUNCTIONED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 710AA A4743 22467 MIA - FLT 1531 - AT GATE PRIOR TO DEPARTURE, THE R1 DOOR SLIDE CAME APART AND DID NOT INFLATE. REPLACED R1 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998073100468 19980731 00468 NM 1998 7 31 AALA981195 1 19980618 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 335AA 22333 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 20B INOPERATIVE. REPLACED CONNECTOR AT SEAT 20B. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998073100469 19980731 00469 NM 1998 7 31 AALA981166 1 19980610 A 2560 H205213 LATCH BOEING 767 767323 1385205 NM LT OW DOOR FAILED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING SLIDE COMPARTMENT DOOR DIFFICULT TO OPEN. REPLACED TWO LEFT OVERWING SLIDE COMPARTMENT DOOR LATCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998073100470 19980731 00470 NM 1998 7 31 AALA981169 1 19980610 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 26AB INOPERATIVE. REPAIRED WIRE FOR EMERGENCY EXIT SE AT LIGHTS AT 26AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998073100471 19980731 00471 NM 1998 7 31 AALA981168 1 19980610 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 23AB INOPERATIVE. REINSTALLED PUSHBACK PIN IN SEAT CO NNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998073100472 19980731 00472 NM 1998 7 31 AALA981161 1 19980609 A 3350 BR7131401 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 323AA 22324 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN FIRST CLASS GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT LIG HT ASSEMBLY IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998073100473 19980731 00473 NM 1998 7 31 AALA981160 1 19980609 A 3350 85130768811 SWITCH BOEING 757 757223 1384957 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 643AA 24601 ORD - FLT 861 - DURING TURNAROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHT PANEL UNARMED SWITCH CAPSULE BROKEN. REPLACED EMERGENCY EXIT LIGHT PANEL UNARMED SWITCH CAPSULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998073100474 19980731 00474 NM 1998 7 31 AALA981184 1 19980616 A 3350 BATTERY PACK BOEING 767 767323 1385205 NM CABIN DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380AN 25449 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT SEAT 20 THROUGH 31 INOPERATIVE. REPLACED TWO EMERGENC Y EXIT SEAT LIGHT CONNECTORS AND BATTERY PACKS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998073100475 19980731 00475 WP 1998 7 31 AALA981175 1 19980614 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445AA 49471 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998073100476 19980731 00476 WP 1998 7 31 AALA981177 1 19980614 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 218AA 49168 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998073100478 19980731 00478 NE 1998 7 31 USAASB98153 2 19980621 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE LEFT OVERTEMP A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 236US 56446 22352 665724 PIT - FLT 1894 - AFTER TAKEOFF FROM PIT, THE NR 1 ENGINE ENCOUNTERED HIGH OIL TEMPERATURE. FLT RETURNED TO FIELD AT PIT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. THE ENGINE WAS NOT SHUT DOWN IN FLT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSY. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998073100479 19980731 00479 EU 1998 7 31 SIMA981697 1 19980618 A 5315 S5367240620801 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAMS 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100480 19980731 00480 EU 1998 7 31 98ZZZM512 1 19980618 A 5315 S5367240725201 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAMS 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100481 19980731 00481 EU 1998 7 31 SIMA981696 1 19980618 A 5320 S5367121733601 SUPPORT AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE SUPPORT AND DRAIN TRACK CORRODED AT FRAME 37. REMOVED AND REPLACED THE SILL PLATE SUPPORT AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100482 19980731 00482 EU 1998 7 31 98ZZZM513 1 19980618 A 5320 536800920102 DRAIN AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE SUPPORT AND DRAIN TRACK CORRODED AT FRAME 37. REMOVED AND REPLACED THE SILL PLATE SUPPORT AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100483 19980731 00483 EU 1998 7 31 SIMA981655 1 19980614 A 5320 S5367121729402 SILL AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, FOUND THE PAX DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE SILL P LATE AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100484 19980731 00484 EU 1998 7 31 98ZZZM514 1 19980614 A 5320 S5367121729801 DRAIN AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, FOUND THE PAX DOOR SILL PLATE AND DRAIN TRACK CORRODED. REMOVED AND REPLACED THE SILL P LATE AND DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100485 19980731 00485 EU 1998 7 31 SIMA981654 1 19980614 A 5347 S53375001212 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100486 19980731 00486 EU 1998 7 31 98ZZZM515 1 19980614 A 5347 S53375001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100487 19980731 00487 EU 1998 7 31 98ZZZM516 1 19980614 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100488 19980731 00488 EU 1998 7 31 98ZZZM517 1 19980614 A 5347 S53375001202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100489 19980731 00489 EU 1998 7 31 98ZZZM518 1 19980614 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100490 19980731 00490 EU 1998 7 31 98ZZZM519 1 19980614 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100491 19980731 00491 EU 1998 7 31 98ZZZM520 1 19980614 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100492 19980731 00492 EU 1998 7 31 98ZZZM521 1 19980614 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100493 19980731 00493 EU 1998 7 31 98ZZZM522 1 19980614 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT AFT INBOARD. THE LEFT AND RIGHT MIDDLE INBOARD AND OUTBOARD AND THE LEFT AND RIGHT AFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLAC ED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100494 19980731 00494 EU 1998 7 31 SIMA981672 1 19980614 A 2120 AIR DISTRIBUTION AEROSP ATR72 ATR72212 EU CABIN ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 448AM 448 DFW - FLT 3535 - FLT ATTENDANT REPORTS AN ELECTRICAL SMOKE SMELL IN THE CABIN. INSPECTED AND FOUND NO EVIDENCE OF SMOKE /SMELL IN CABIN. ALL LIGHTS WORKING OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998073100495 19980731 00495 EU 1998 7 31 SIMA981666 1 19980611 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 529AM 0627 529 ORD - FLT 4374 - VARIOUS CABIN EMERGENCY LIGHTS WILL NOT EXTINGUISH. REMOVED AND REPLACED BATTERY PACK AT SEAT 4B. OPE RATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998073100496 19980731 00496 EU 1998 7 31 SIMA981633 1 19980612 A 3350 167006 BULB AEROSP ATR42 ATR42300 8680920 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 213AT 211 ORD - FLT 4290 - SEVERAL EMERGENCY FLOOR PROXIMITY LIGHTS AT ROW 2 DO NOT ILLUMINATE. REMOVED AND REPLACED TWO FLOOR PR OXIMITY LIGHT BULBS AT ROW 2. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998073100497 19980731 00497 EU 1998 7 31 SIMA981669 1 19980615 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 339SB 340B339 DFW - FLT 5320 - PASSENGER EMERGENCY LIGHT OVER SEAT 11A DOES NOT ILLUMINATE. REMOVED AND REPLACED PASSENGER EMERGENCY LIGHT OVER SEAT 11A. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998073100498 19980731 00498 EU 1998 7 31 PLGA980527A 1 19980527 A 7603 C821464 CONTROL CABLE SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A PLGA O OTHER J WARNING INDICATION AP APPROACH 1 NE 05 743BA 219 340A093 PWM - FLT 4592 - WHILE ON APPROACH, THE LEFT PROPELLER BLADES WENT TOWARD FLAT PITCH. CREW ADVANCED POWER AND ALL CONDI TIONS RETURNED TO NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND POWER LEVER CABLE BETWEEN HMU AND PCU HA D FAILED INTERNALLY AND THE ROD END HAD DISCONNECTED. THE CABLE WAS REPLACED AND ENGINE GROUND RAN WITH ALL SYSTEMS CHE CKING NORMAL. (M) 2 L 7 2 4T RT A52EU 1998073100499 19980731 00499 EU 1998 7 31 PLGA980519A 1 19980519 A 3234 D49410001 HANDLE SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A PLGA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 NE 05 341BE 1241086 340A063 BOS - FLT 4470 - WHEN THE LANDING GEAR WAS SELECTED UP, ALL THREE DOWN AND LOCKED LIGHTS REMAINED ILLUMINATED AND THE GE AR DID NOT RETRACT. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTRO L HANDLE. SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998073100500 19980731 00500 EU 1998 7 31 PLGA980507A 1 19980507 A 3260 ATG130902 SWITCH SAAB SF340 340B 7860101 EU LT MLG FAILED A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 361BE 340B290 HPN - FLT 4382 - WHEN LANDING GEAR WAS SELECTED UP AFTER TAKEOFF, THE LEFT MAIN GEAR DOWN AND LOCKED INDICATION REMAINED ILLUMINATED. IT WAS CONFIRMED THAT GEAR WAS RETRACTED. AIRCRAFT RETURNED TO HPN AND LANDED WITHOUT INCIDENT. MAINTEN ANCE REPLACED THE LEFT DOWN AND LOCKED SWITCH. SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998073100501 19980731 00501 EU 1998 7 31 PLGA980503A 1 19980503 A 5310 STRUCTURE SAAB SF340 340B 7860101 EU FUSELAGE BIRD STRIKE A PLGA K NONE C F.O.D. DE DESCENT 1 NE 05 361BE 340B290 LGA - FLT 4517 - INBOUND TO LGA, THE CREW EXPERIENCED A BIRD STRIKE JUST BELOW THE RIGHT WINDSHIELD. AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND NO DAMAGE. AIRCRAFT WAS RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 1998073100502 19980731 00502 EU 1998 7 31 PLGA980504A 1 19980504 A 3260 GE327 BULB SAAB SF340 340B 7860101 EU RT MLG FAILED A PLGA L ABORTED APPROACH L P NO TEST NO WARNING INDICATION AP APPROACH 1 NE 05 364BE 340B294 BOS - FLT 4479 - CREW SELECTED LANDING GEAR DOWN FOR LANDING AND REPORTED THAT THERE WAS NO DOWN AND LOCKED INDICATION F OR RIGHT MAIN GEAR. THE APPROACH WAS ABORTED AND CREW TESTED THE LANDING GEAR INDICATION SYSTEM. FOUND BOTH INDICATOR LIGHT BULBS FOR RIGHT GEAR WERE BURNED OUT. CREW REPLACED BOTH BULBS AND ALL INDICATION WAS NORMAL. (M) 2 L 7 2 4T RT A52EU 1998073100503 19980731 00503 EU 1998 7 31 PLGA980528A 1 19980528 A 2430 8484001116 RELAY SAAB SF340 340B 7860101 EU E/E BAY FAILED A PLGA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 NE 05 358BE 340B279 BOS - FLT 4253 - AFTER TAKEOFF, THE RIGHT MAIN ELECTRICAL BUS INTERMITTENTLY FELL OFF LINE. AIRCRAFT RETURNED TO BOS AN D LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT TIME DELAY RELAY (PC72). SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998073100504 19980731 00504 EU 1998 7 31 PLGA980527B 1 19980527 A 2913 401852 PUMP SAAB SF340 340B 7860101 EU HYDRAULIC SYSTEM FAILED A PLGA O OTHER J WARNING INDICATION AP APPROACH 1 NE 05 359BE 146 340B285 BGR - FLT 4408 - THE HYDRAULIC PUMP FAILED WHILE ON APPROACH INTO BGR AND THE LANDING GEAR HAD TO BE EXTENDED USING THE HAND PUMP. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC PUMP. (M) 2 L 7 2 4T RT A52EU 1998073100505 19980731 00505 NM 1998 7 31 USAASB98154 1 19980624 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 249US 22756 CMH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PAC K. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998073100506 19980731 00506 EU 1998 7 31 USAAF98052 1 19980630 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 860US 11295 IND - EMERGENCY EXIT SIGN ABOVE GALLEY DOOR WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NR 9 POWER SUPPLY. (M) 2 L 7 2 4F RT 1998073100507 19980731 00507 1998 7 31 USAASB98160 4 19980626 A 3417 HG480B13 ADC BOEING 737 737201 1384454 NM E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 232US 35592 22018 CLT - FLT 8036 - DURING CRUISE, CREW REPORTED A TOTAL NR 1 AIR DATA COMPUTER FAILURE. CREW PULLED AND RESET RN 1 CADC C IRCUIT BREAKERS. SYSTEM RESETS, THEN FAILS AGAIN. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMER GENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 1 AIR DATA COMPUTER PER MM. ACCOMPLISHED FUNCTIONAL CHECK OF NR 1 ADC. CHECKS GOOD. (M) 2 L 7 2 4F A16WE 1998073100508 19980731 00508 WP 1998 7 31 USAAD98114 1 19980625 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 810US 48042 IND - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F A6WE 1998073100509 19980731 00509 WP 1998 7 31 USAAD98115 1 19980625 A 3350 14597101 BATTERIES DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 810US 48042 IND - FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998073100510 19980731 00510 NE 1998 7 31 USAAD98116 2 19980628 A 7261 515107 PUMP DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN K M FLUID LOSS OVER TEMP CL CLIMB 1 EA 19 938VJ 34784 48119 655139 CVG - FLT 1530 - AFTER TAKEOFF FROM IND, CREW NOTED OIL TEMPERATURE ON NR 1 ENGINE RISING. AS THE TEMPERATURE ROSE, THE OIL QTY AND PRESSURE BEGAN TO DROP. CREW SECURED THE ENGINE. FLT DIVERTED TO CVG AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE MAIN OIL PUMP. (M) 2 L 7 2 4F 4 F A6WE E2EA 1998073100511 19980731 00511 NM 1998 7 31 USAASB98131 1 19980530 A 2120 469658 FILTER BOEING 737 737301 1384611 NM A/C BAY DIRTY A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 585US 23930 LAX - FLT 29 - FLT ATTENDANT REPORTED AN ODOR IN THE CABIN DURING FLIGHT WHICH SMELLED LIKE WARM PLASTER OR AN INSULATIO N/ELECTRICAL BURN SMELL. CREW TURNED OFF RECIRCULATION FAN AND ODOR DISSIPATED. FLIGHT LANDED WITHOUT FURTHER INCIDENT . MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FAN FILTER WHICH WAS FOUND TO BE EXTREMELY DIRTY. CHECKED RECIRCU LATION FAN FOR OPERATION. CHECKED OK. NO FURTHER ODOR NOTED. (M) 2 L 7 2 4F RT A16WE 1998073100512 19980731 00512 EU 1998 7 31 USAAF98053 1 19980617 A 3260 858202 PSEU FOKKER F28 F28MK0100 4990807 EU E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 882US 11334 CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EV ERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ING ELECTRONIC UNIT, NR 3 AND NR 4 GND/FLT SENSOR, AND RIGHT MAIN GEAR GND/FLT HARNESS. REF: OPERATOR CONTROL NR 98ZZZ X2829 THROUGH 98ZZZX2831. (X) 2 L 7 2 4F RT 1998073100513 19980731 00513 NM 1998 7 31 USAA980281 1 19980623 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 46491 22275 INT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK BS 727 RBL 6.5 ATTACH ANGLE. REPAIRED PER SRM 51-10-1. ( M) 2 L 7 2 4F A16WE 1998073100514 19980731 00514 NM 1998 7 31 USAA980280 1 19980623 A 5320 BEAM BOEING 737 737201 1384454 NM BS 663-727 FRETTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 46491 22275 INT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 20 INCH FRETTED AREA BETWEEN BS 663-727 BEAM. INSTALLED REPAIR STRAP AN D REPAIRED PER EA 44092. (M) 2 L 7 2 4F A16WE 1998073100515 19980731 00515 NM 1998 7 31 USAA980276 1 19980618 A 5720 694490310 FORMER BOEING 737 7372Q9 138448M NM WS 219 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 231US 48746 21976 CLT - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 10 INCH CRACK IN ANGLE FORMER RT WING L/E AT W STATION 219. INSTALLE D MODIFIED PART. (M) 2 L 7 2 4F A16WE 1998073100516 19980731 00516 NM 1998 7 31 USAASB98156 1 19980625 A 7930 1163P181 SWITCH BOEING 737 737201 1384454 NM OIL BYPASS FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 19 240AU 22355 PHL - FLT 452 - ON CLIMB-OUT FROM PHL, AT APPROX 5,000 FT, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. LIGHT R EMAINED ON WHEN POWER WAS REDUCED TO IDLE THRUST ON THE NR 1 ENGINE. CREW SHUTDOWN THE NR 1 ENGINE IN FLIGHT AND RETURN ED TO FIELD AT PHL WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. MAIN TENANCE REMOVED AND INSPECTED THE NR 1 ENGINE OIL FILTER. NO CONTAMINATION FOUND. INSTALLED NEW OIL FILTER (P/N 056306 -06) AND REPLACED OIL FILTER BYPASS SWITCH. ENGINE RUN CHECKS GOOD. (M) 2 L 7 2 4F A16WE 1998073100517 19980731 00517 NM 1998 7 31 USAASB98158 1 19980626 A 3020 655812310 DUCT BOEING 737 7372B7 1384560 NM NR 1 ENGINE CRACKED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 269AU 22881 TPA - FLT 940 - DURING CLIMB-OUT FROM TPA AT FL200, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CAPTAIN RETARDED THROTT LE ON THE NR 1 ENGINE TO IDLE AND THE LIGHT EXTINGUISHED. CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO FIELD AT TPA. F LT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE FOUND THE NR 1 ENGINE COWL ANTI-ICE DUCT CRACKED AT BELL OWS. REMOVED AND REPLACED DUCT ASSEMBLY. RAN ENGINE. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998073100518 19980731 00518 NM 1998 7 31 USAASB98159 1 19980626 A 3230 BACH8B04EE0207T HYDRAULIC LINE BOEING 737 737201 1384454 NM NLG LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 246US 22753 BOS - FLT 354 - AFTER TAKEOFF FROM BOS, CREW RECEIVED A NOSE LANDING GEAR RED LIGHT ALONG WITH A VIBRATION. CREW DECIDE D TO RETURN TO FIELD TO BOS. RECEIVED THREE GEAR GREEN LIGHTS WHEN GEAR WAS LOWERED. FLIGHT LANDED WITHOUT FURTHER INC IDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NOSE LANDING GEAR LOCK ACTUATOR HYDRAULIC LINE LEAKING. REMOV ED AND REPLACED HYDRAULIC LINE. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998073100519 19980731 00519 NM 1998 7 31 USAA980275 1 19980618 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 231US 74846 21976 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2.50 INCH CRACK IN SKIN STA 727B JUST BELOW STR 15L. INSTALLED DOUBL ER PER TYPICAL REPAIR NR 53-30-14. (X) 2 L 7 2 4F A16WE 1998073100520 19980731 00520 NM 1998 7 31 USAA980278 1 19980618 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 231US 48746 21976 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 3.75 INCH CRACK IN THE SKIN AT STATION 727B STRIGNER 17R. INSTALLED DOUBLER PER TYPICAL REPAIR NR 53-30-14. (M) 2 L 7 2 4F A16WE 1998073100521 19980731 00521 NM 1998 7 31 USAA980273 1 19980608 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 351US 32052 23554 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK IN THE SKIN AFT OF THE EQUIPMENT EXHAUST AT STATION 3 80 BETWEEN STRINGER 28L AND BL 0. INSTALLED DOUBLER PER REPAIR DOCUMENT EA NR 44097. (M) 2 L 7 2 4F RT A16WE 1998073100522 19980731 00522 NM 1998 7 31 USAA980274 1 19980622 A 5512 65C274946 SKIN BOEING 737 7374B7 1384702 NM BS 125 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 443US 22436 24842 CLT - DURING INTERIOR MOD CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK IN LOWER SKIN RT HORIZ STAB STATION 125.5 AND HO RIZ STAB FRONT SPAR. INSTALLED DOUBLER PER TYPICAL REPAIR 55-10-07. (M) 2 L 7 2 4F RT A16WE 1998073100523 19980731 00523 NM 1998 7 31 USAASB98155 1 19980624 A 2612 6678 DETECTOR BOEING 737 737301 1384611 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 19 346US 23515 SBN - FLT 7002 - ABOUT 60 MILES OUT OF SBN, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. AFTER GOING THROUGH CHECKLIST, CAPTAIN ELECTED TO RETURN TO FIELD AT SBN. AN EMERGENCY WAS DECLARED WITH THE TOWER. WHEN THE CREW PULLED BACK THE POW ER ON THE NR 2 ENGINE, THE OVERHEAT LIGHT EXTIGUISHED. THE ENGINE REMAINED AT IDLE UNTIL LANDING BACK IN SBN. CAPTAIN NOTED THAT THE NR 2 ENGINE WAS HARD TO START OUT OF MKE BUT FINE OUT OF SBN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FIRE DETECTION SYSTEM CORE DETECTOR PER MM 26-11-11. PERFORMED HIGH POWER ENGINE RUN WITH NO FAULTS OR OVERHEATS NOTED. 'A' FIRE DETECTION TESTS CHECK GOOD. ALSO, SECURED LOOSE PIN CONNECTOR ON E3 SHELF AT THE M279 MODULE. 'B' FI 2 L 7 2 4F RT A16WE 1998073100524 19980731 00524 NE 1998 7 31 REXA98098 2 19980527 A 7200 ENGINE OIL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE LEFT FAILED A REXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 922MA 340A077 GEE367218 LEFT ENGINE OIL PRESSURE FLUX AND LOW OIL PRESSURE CWP LIGHT ILLUMINATED. SHUTDOWN ENGINE. REMOVED AND REPLACED LEFT E NGINE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998073100525 19980731 00525 WP 1998 7 31 USAAD98104 1 19980609 A 5240 GUIDE TRACK DOUG DC9 DC931 3022065 WP SERV DOOR FOD A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 960VJ 47505 PIT - FLT 841 - COULD NOT OPEN FORWARD SERVICE DOOR. MAINTENANCE FOUND A PIECE OF PLASTIC FROM THE HANDLE COVER IN THE GUIDE TRACK IMPEDING MOTION OF THE CAM AND ROLLER. THE PLASTIC WAS REMOVED. (M) 2 L 7 2 4F A6WE 1998073100526 19980731 00526 1998 7 31 TWRA9835 4 19980617 A 2564 D23835289 LIFE RAFT BOEING 747 747131 1384881 NM 3L DOOR MISMANUFACTURED A TWRA K NONE W INADEQUATE Q C IN INSP/MAINT 1 EA 15 608FF 19672 DURNG A DITCHING TRAINING DRILL (OFF AIRCRAFT), A 42 MAN LIFE RAFT FAILED TO FULLY DEPLOY. THE RAFT WAS INSPECTED AND R EMOVED SERVICEABLE FROM AIRCRAFT FOR TRAINING PURPOSE. CAUSE OF THE RAFT NOT TO FULLY DEPLOY WAS A 1 INCH NYLON STRAP T IED AROUND THE RAFT UNDER THE OUTER LACING COVERING. THE STRAP WAS NOT VISIBLE TO THE DITCHING TEAM AND IS NOT PART OF THE RAFT ASSY. (M) 2 L 7 4 4F A20WE 1998073100527 19980731 00527 EU 1998 7 31 SIMA981331 1 19980513 A 5347 S53375001204 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED OUT OF LIMITS. THE LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, RIGHT FORWARD OUTBOARD, RIGHT MIDDLE OUTBOARD AN D RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998073100528 19980731 00528 EU 1998 7 31 98ZZZM523 1 19980513 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED OUT OF LIMITS. THE LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, RIGHT FORWARD OUTBOARD, RIGHT MIDDLE OUTBOARD AN D RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998073100529 19980731 00529 EU 1998 7 31 98ZZZM524 1 19980513 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED OUT OF LIMITS. THE LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, RIGHT FORWARD OUTBOARD, RIGHT MIDDLE OUTBOARD AN D RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998073100530 19980731 00530 EU 1998 7 31 98ZZZM525 1 19980513 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED OUT OF LIMITS. THE LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, RIGHT FORWARD OUTBOARD, RIGHT MIDDLE OUTBOARD AN D RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998073100531 19980731 00531 EU 1998 7 31 98ZZZM526 1 19980513 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED OUT OF LIMITS. THE LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, RIGHT FORWARD OUTBOARD, RIGHT MIDDLE OUTBOARD AN D RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998073100532 19980731 00532 EU 1998 7 31 98ZZZM527 1 19980513 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED OUT OF LIMITS. THE LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, RIGHT FORWARD OUTBOARD, RIGHT MIDDLE OUTBOARD AN D RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998073100533 19980731 00533 EU 1998 7 31 98ZZZM528 1 19980513 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 209AT 0209 SAW - DURING CPCP-4 INSPECTION, MAINTENANCE REPORTED THE FOLLOWING SEAT TRACKS CORRODED OUT OF LIMITS. THE LEFT FORWARD OUTBOARD, LEFT MIDDLE INBOARD, LEFT MIDDLE OUTBOARD, LEFT AFT INBOARD, RIGHT FORWARD OUTBOARD, RIGHT MIDDLE OUTBOARD AN D RIGHT AFT INBOARD. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1998073100534 19980731 00534 NM 1998 7 31 AALA981017 1 19980521 A 2421 IDG BOEING 767 767323 1385205 NM LT GENERATOR FAILED A AALA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SW 07 39356 24037 GRU - DEFERRED LEFT IDG INOP AS PER MEL REF SERVICED BOTH IDGS AND APU OIL AS PER MEL REQUIRED. MIC SHEET ENTERED AND P LACARDED. REMOVED AND REPLACED LEFT ENGINE IDG PER MM EMP NR 486574. OPS CHECK GOOD. LEAK CHECK GOOD. CLEARED MEL 24 -01. AUTH 5-320DC-B. CLEARED MIC SHEET. (M) 2 L 7 2 4F RT A1NM 1998073100535 19980731 00535 WP 1998 7 31 ASAA9880091 1 19980522 A 5310 SKIN DOUG DC9 DC983 3022083 WP NLG WW DAMAGED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 974AS 53450 SEA - LEFT FORWARD CORNER OF NOSE LANDING GEAR WHEEL WELL WAS DAMAGED DURING PUSHBACK BY A TUG. THE DAMAGE WAS FOUND TO BE WITHIN SRM LIMITS. REPLACED LOOSE BLIND FASTENERS PER THE SRM AND RELEASED AIRCRAFT PER PLT DEFERRAL, WITH REINSPEC TIONS TO BE ACCOMPLISHED AT 'A' CHECKS. DURING 15K CHECK, REPLACED THE FRAME SEGMENT AND MADE REPAIRS TO THE SKIN PER S RM 53-14-1. (M) 2 L 7 2 4F RT A6WE 1998073100536 19980731 00536 WP 1998 7 31 ASAA9880094 1 19980528 A 5610 PIN DOUG DC9 DC982 3022082 WP COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 SEA - FLT 583 - AFTER ARRIVAL, CREW REPORTED THE CAPTAINS SLIDING WINDOW DIFFICULT TO OPEN. FOUND UPPER GUIDE PIN OUT O F TRACK. REPOSITIONED PIN AND RESEQUENCED WINDOW LINKAGE. WINDOW OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998073100537 19980731 00537 WP 1998 7 31 ARWA980609 1 19980629 A 3241 BRAKE DOUG DC8 DC862 3021970 WP NLG OUT OF ADJUST A ARWA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 19 810BN 45905 KRDU - FLT 810 - AFTER TAKEOFF AND GEAR RETRACTION LOUD NOISE AND VIBRATION COMING FROM NOSE GEAR AREA. INSPECTED NOSE, WHEEL SKIN BRAKE, FOUND IN IDLE POSITION, REPOSITION PER DC-8 MM 32-41-3. (M) 2 L 7 4 4F 4A25 1998073100538 19980731 00538 WP 1998 7 31 ARWA980608 1 19980622 A 5210 STRIKER DOUG DC8 DC862F 3021972 WP PASS DOOR LOOSE A ARWA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 791AL 46150 MIA - FLT 627 - AT 24,000 FEET LIGHT ON DOOR, (DOOR WARNING LIGHT ON) PERFORMED ACCORDING ABNORMAL CHECKLIST, DOES NOT C URE, RETURNED TO LICZ. T/S CHECKED MAIN GEAR DOOR UPLATCH RIGGING, FOUND LEFT DOOR STRICKER LOOSE, SECURED STRICKER, OP S CHECK NORMAL ON GROUND IAW 32-31-4. (M) 2 L 7 4 4F 4A25 1998073100539 19980731 00539 NM 1998 7 31 USAABB98067 1 19980617 A 3350 86210066 BATTERY PACK BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 621AU 27200 LAX - FOUND SEVEN EMERGENCY LOW LEVEL LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998073100540 19980731 00540 NM 1998 7 31 USAA980250 1 19980617 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 727 A PLUS 7 INCH STRINGER 17R SKIN. INSTALLED DOUBLERS , REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998073100541 19980731 00541 NM 1998 7 31 USAA980264 1 19980610 A 5330 SKIN BOEING 737 737201 1384454 NM BS 797/767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 48249 22018 PHL - DURING RON, FOUND 2 CRACKS, IN EACH LONG RIGHT SIDE FUSELAGE SKIN BETWEEN STATION 797 AND 767 BETWEEN STRINGER 18R T AND 19RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M) 2 L 7 2 4F A16WE 1998073100542 19980731 00542 NM 1998 7 31 USAA980265 1 19980610 A 5330 SKIN BOEING 737 737201 1384454 NM BS 400/420 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 48249 22018 PHL - DURING RON FOUND 2 INCH CRACK IN FUSELAGE SKIN RIGHT SIDE BETWEEN STATION 400 AND STATION 420 BETWEEN STRINGER 23R T AND 24RT. INSTALLED TEMPORARY EXTERNAL DOUBLER PER SRM 53-30-3 PAGE 2E, FIG 1. (M) 2 L 7 2 4F A16WE 1998073100543 19980731 00543 NM 1998 7 31 USAA980241 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 320-336 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL (HFEC) INSPECTION, FOUND 3 CRACKS 3 FASTENERS HOLES CRACKED APPROX .125 INCH EACH, BS 320- BS 336, STRINGER 20 STRINGER. SPLICED IN NEW SECTION OF STRINGER, SRM 53-10-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998073100544 19980731 00544 NM 1998 7 31 USAA980242 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 304 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 3 INCH CORRODED AREA TWO PLACES BS 304, STRINGER 25L, BS 286.5 , STRINGER 25L STRINGER. INSTALLED STRINGER SPLICE BS 304 AND 286.5 STRINGER 25L, REPAIRED PER SRM 53-10-3 FIG 1 SHEET 8. CORROSION TASK NR C53-202-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998073100545 19980731 00545 NM 1998 7 31 USAA980243 1 19980617 A 5240 SKIN BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK RIGHT FORWARD SERVICE DOOR LOWER AFT CORNER SKIN. INSTA LLED EXTERNAL DOUBLER, REPAIRED DRAWING 65C27287 AND TYPICAL REPAIR 53-10-19 REV A. (M) 2 L 7 2 4F A16WE 1998073100546 19980731 00546 NM 1998 7 31 USAA980244 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 410-463 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SURFACE CORRSION ON STRINGER STATION 410-463 STRINGER 3R, .5 INCH BY 1.0 625. REMOVED AND REPLACED STRINGER 3R FROM STATION 410-463, REPAIRED PER SRM 53-10-3 FIG 3. CORROSION TASK NR C-53-107 -01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998073100547 19980731 00547 NM 1998 7 31 USAA980245 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 420-440 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION ON STRINGER STATION 420-440 STRINGER 7R, 1 FT BY 3 INC H. REMOVED AND REPLACED STRINGER 7R FROM STRINGER 420-440. (M) 2 L 7 2 4F A16WE 1998073100548 19980731 00548 NM 1998 7 31 USAA980259 1 19980617 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK .0625 INCH LONG FORWARD ENTRY DOOR SKIN SCUFF PLATE. INSTALLED RE PAIR DOUBLERS AND TRIPLER, REPAIRED PER EA 44026 AND BOEING DRWING 65C27257. (M) 2 L 7 2 4F A16WE 1998073100549 19980731 00549 NM 1998 7 31 USAA980258 1 19980617 A 5311 FRAME BOEING 737 737201 1384454 NM BS 344 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 344 STRINGER 27R FRAME. INSTALLED REPAIR DOU BLER AND FILLER, REPAIRED PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998073100550 19980731 00550 NM 1998 7 31 USAA980257 1 19980617 A 5311 FRAME BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION,K FOUND 3 INCH CRACK IN FUSELAGE FRAME BS 747 BETWEEN STRINGER 13/14L. INSTALL ED FRAME REPAIR AND REPAIR PER SRM 53-40-4. (M) 2 L 7 2 4F A16WE 1998073100551 19980731 00551 WP 1998 7 31 VJ9800054 1 19980322 A 3340 8906K1665 SWITCH DOUG DC9 DC932 3022066 WP COCKPIT FAILED A VJ6A O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 11 907VJ 47444 DURING FLT, SMOKE COMING FROM THE WING LANDING LIGHT SWITCHES WHEN POSITIONED TO EXT AND ON. SMOKE SUBSIDED WHEN SWITCH ES WERE TURNED OFF. REPLACED THE SWITCH. OPS CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1998073100552 19980731 00552 1998 7 31 USAAF98051 4 19980619 A 2211 6227478411 COMPUTER FOKKER F28 F28MK0100 4990807 EU AVIONICS BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 861US 11297 CLT - FLT 1635 - AT APPROXIMATELY 4000 FT IN CLIMB-OUT FROM CLT, CREW RECEIVED THE FOLLOWING MESSAGES ON THE MULTIFUNCTI ON DISPLAY, 'STAB TRIM 1 AND 2, YD 1 AND 2, RUDDER 1 AND 2'. FLT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. M AINTENANCE REPLACED THE FLIGHT AUGMENTATION COMPUTER. (M) 2 L 7 2 4F RT 1998073100553 19980731 00553 EU 1998 7 31 USAAF98049 1 19980606 A 3350 4TL112B INVERTER FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 858US 11291 GSO - LEFT SIDE OVERWING EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT POWER SUPPLY, BA TTERY PACK, AND INVERTER. (M) 2 L 7 2 4F RT 1998073100554 19980731 00554 EU 1998 7 31 98ZZZM529 1 19980606 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 858US 11291 GSO - LEFT SIDE OVERWING EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT POWER SUPPLY, BA TTERY PACK, AND INVERTER. (M) 2 L 7 2 4F RT 1998073100555 19980731 00555 EU 1998 7 31 98ZZZM530 1 19980606 A 3350 6104789 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 858US 11291 GSO - LEFT SIDE OVERWING EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE NR 5 EMERGENCY LIGHT POWER SUPPLY, BA TTERY PACK, AND INVERTER. (M) 2 L 7 2 4F RT 1998073100556 19980731 00556 EU 1998 7 31 USAAF98050 1 19980611 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 858US 11291 GSO - NR 2 CEILING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT LIGHT FIXTURE. (M) 2 L 7 2 4F RT 1998073100557 19980731 00557 NM 1998 7 31 USAASB98121 1 19980524 A 3350 AD20131A BATTERY BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 534AU 24516 IND - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY EXIT SIGNS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY SUPPL Y IN CHARGER UNIT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100558 19980731 00558 NM 1998 7 31 USAASB98123 1 19980518 A 3350 30043229 LIGHT BOEING 737 7373B7 1384580 NM FUSELAGE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 510AU 23385 TPA - DURING B-CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT AT THE AFT SERVICE DOOR INOP. MAINTENANCE FOUND TH E LIGHT SOCKET WAS BROKEN DUE TO EXCESSIVE CORROSION. REPLACED ENTIRE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100559 19980731 00559 NM 1998 7 31 USAASB98145 1 19980608 A 3350 LIGHT BOEING 737 737401 1384701 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 412US 23881 MCI - PILOT REPORTED THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOP. MAINTENANCE INSPECTED AND RESEATED THE LIGHT ASS Y. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100560 19980731 00560 NM 1998 7 31 USAASB98149 1 19980612 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 392US 23314 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHT AT THE AFT LEFT ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTE RY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100561 19980731 00561 NM 1998 7 31 USAASB98140 1 19980603 A 2410 CSD BOEING 737 7374B7 1384702 NM NR 1 ENGINE OVERSERVICED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 435US 24557 BDL - FLT 1837 - FLT WAS CLIMBING OUT OF BOS WHEN THE NR 1 ENGINE CSD OIL TEMPERATURE LIGHT FLICKERED. OIL TEMPERATURE WENT TO MAXIMUM. CREW DISCONNECTED THE NR 1 ENGINE CSD AND SINCE THE APU WAS ON MEL, THE FLT DIVERTED TO BDL. NO EMERG ENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE CSD OVERSERVICED. REPLACED CSD OIL COOLER (LINE) FILTER (P/N AC9780F15Y6) AND INSPECTED CSD INTERNAL (CHARGE) FILTER AND MAGNETIC CHIP DETECTOR. N O METAL CONTAMINATION FOUND. REPLACED OIL "IN' TEMPERATURE BULB (P/N 102-00002). SERVICED CSD OIL TO PROPER LEVEL. RA N ENGINE WITH FULL GENERATOR LOAD. CSD TEMPERATURE STABILIZED AT 85 DEGREES, RISE 3-4 DEGREES. OPERATIONAL CHECK AND 2 L 7 2 4F RT A16WE 1998073100562 19980731 00562 NM 1998 7 31 USAA980260 1 19980617 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 378 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 391US 37280 23313 INT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 INCH CRACK STATION 378 AND LBL 6 (LOWER LOBE) SKIN. INSTALLED DOUBLER AND REPAIRED PER DRAWING 65C33930 AND SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1998073100563 19980731 00563 NM 1998 7 31 USAASB98141 1 19980604 A 3230 189929 SWITCH BOEING 737 7373B7 1384580 NM RT MLG WW OUT OF ADJUST A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 390US 23312 PHL - FLT 701 - AFTER TAKEOFF OUT OF BTV, THE LANDING GEAR WOULD NOT RETRACT. CREW TRIED TO RECYCLE GEAR BUT IT WOULD N OT RETRACT. USED LANDING GEAR OVERRIDE TRIGGER AND GEAR RETRACTED. FLIGHT PROCEEDED ON NORMAL FLGHT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE MAIN LANDING GEAR AIR GROUND SENSE SAFETY SWITCH PER MM 32-09-01. PERFORME D RETRACTION AND EXTENSION CHECK OF LANDING GEAR. SYSTEM CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100564 19980731 00564 NM 1998 7 31 USAASB98136 1 19980603 A 2133 322684003 OUTFLOW VALVE BOEING 737 737301 1384611 NM PRESS CONT SYS FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 590US 23935 PHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HO RN BEGAN TO SOUND. CREW DECLARED AN EMERGENCY AND DIVERTED INTO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO OXYGE N MASKS WERE DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT OUTFLOW VALVE AND THE CABIN PRESSURE CONTRO LLER. PERFORMED OPERATIONAL TEST PER MM 21-31-00 AND 21-43-11. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100565 19980731 00565 NM 1998 7 31 98ZZZM531 1 19980603 A 2133 7110033 OUTFLOW VALVE BOEING 737 737301 1384611 NM PRESS CONT SYS FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 590US 23935 PHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HO RN BEGAN TO SOUND. CREW DECLARED AN EMERGENCY AND DIVERTED INTO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO OXYGE N MASKS WERE DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT OUTFLOW VALVE AND THE CABIN PRESSURE CONTRO LLER. PERFORMED OPERATIONAL TEST PER MM 21-31-00 AND 21-43-11. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100566 19980731 00566 NM 1998 7 31 98ZZZM532 1 19980603 A 2131 7638101 PRESS CONTROLLER BOEING 737 737301 1384611 NM PRESS CONT SYS FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 590US 23935 PHL - FLT 1975 - CLIMBING OUT OF EWR AT APPROXIMATELY FL 135, THE AUTO PRESSURIZATION SYSTEM FAILED. SYSTEM SWITCHED TO STANDBY PRESSURIZATION AND IT FAILED ALSO. THE MANUAL MODE THEN BECAME EXTREMELY DIFFICULT TO CONTROL AND THE CABIN HO RN BEGAN TO SOUND. CREW DECLARED AN EMERGENCY AND DIVERTED INTO PHL WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO OXYGE N MASKS WERE DEPLOYED. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT OUTFLOW VALVE AND THE CABIN PRESSURE CONTRO LLER. PERFORMED OPERATIONAL TEST PER MM 21-31-00 AND 21-43-11. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100567 19980731 00567 NM 1998 7 31 USAASB98135 1 19980602 A 2130 8012403 TURBOFAN BOEING 737 737301 1384611 NM RT A/C BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 563AU 23551 PIT - FLT 1597 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF FROM PIT. FLIGHT RETURNED TO FIELD AND LANDED WIT HOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT TURBOFAN AND THE LEFT MIX ING CONTROL VALVE ASSY. OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD ON GROUND. (M) 2 L 7 2 4F RT A16WE 1998073100568 19980731 00568 NM 1998 7 31 98ZZZM533 1 19980602 A 2130 39811611 CONTROL VALVE BOEING 737 737301 1384611 NM LT A/C BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 563AU 23551 PIT - FLT 1597 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF FROM PIT. FLIGHT RETURNED TO FIELD AND LANDED WIT HOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT TURBOFAN AND THE LEFT MIX ING CONTROL VALVE ASSY. OPERATIONAL CHECK AND PRESSURIZATION CHECK GOOD ON GROUND. (M) 2 L 7 2 4F RT A16WE 1998073100569 19980731 00569 NM 1998 7 31 USAA980256 1 19980617 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 722 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION FOUND CRACK .25 INCH LONG STATION 722 TO 725 BL '0' LONGITUDINAL FLOORBEAM. IN STALLED DOUBLER, REPAIRED PER SRM 51-40-2 AND BOEING DRAWING 65C34537. (M) 2 L 7 2 4F A16WE 1998073100570 19980731 00570 NM 1998 7 31 USAA980255 1 19980617 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 707-714 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH LONG CRACK STATION 707 TO 714 LBL 25 INCHES LONGITUDIAL FLOORBEAM . INSTALLED DOUBLER, REPAIRED PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998073100571 19980731 00571 NM 1998 7 31 USAA980254 1 19980617 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 661 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK BL '0' AT BS 661 FLOORBEAM. INSTALLED REPAIR ANGLES, REP AIRED PER BOEING REPAIR DRAWING 65C34537. (M) 2 L 7 2 4F A16WE 1998073100572 19980731 00572 NM 1998 7 31 USAA980253 1 19980617 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 707-714 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK BS 707-714 25 INCH RBL WL 203.5 LONGITUDIAL FLOORBEAM WEB. CUTOUT CRACKED AREA AND INSTALLED WEB REPAIR, REPAIRED SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998073100573 19980731 00573 NM 1998 7 31 USAA980252 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION ON STRINGER 8R STATION 365, 1 INCH BY 3 INCH. SPLICES IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-2 FIG 3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998073100574 19980731 00574 NM 1998 7 31 USAA980251 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 358-360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND 2 INCH CORRODED AREA BS 358-360 UPPER SIDE OF STRINGER 27L. INSTALLED N EW SPLICE ANGLE AND REPAIRED PER SRM 51-10-1. CORROSION TASK NR C53-202-02, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998073100575 19980731 00575 NM 1998 7 31 USAA980249 1 19980617 A 5330 SKIN BOEING 737 737201 1384454 NM BS 378 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CRACK .5 INCH LONG STATION 378 BL '0' SKIN. INSTALLED DOUBLER, REPAIRED PER TYPICAL REPAIR 53-30-04. (M) 2 L 7 2 4F A16WE 1998073100576 19980731 00576 NM 1998 7 31 USAA980248 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 460-480 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER 7R AND STRINGER 5R BS 460-480, .75 INCH BY 2 INCH. INSTALLED STRINGER REPAIRS AND REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998073100577 19980731 00577 NM 1998 7 31 USAA980247 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 440-460 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS .25 INCH BY .25 INCH EACH STRINGER 3R BS 440 TO B S 460. SPLICED IN NEW SECTION OF STRINGER, REPAIRED PER SRM 53-10-3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998073100578 19980731 00578 NM 1998 7 31 USAA980246 1 19980617 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 425-470 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 229US 49570 21818 INT - DURING Q-5 CEHCK VISUAL INSPECTION, FOUND SURFACE CORROSION ON STRINGER STATION 425 TO 470 STRINGER 4R, 2 INCH BY 1.5 INCH. REMOVED AND REPLACED STRINGER 4R FROM 425-470, REPAIRED PER SRM 53-10-3 FIG 3. CORROSION TASK NR C53-107-01, CORROSION LEVEL 2. (M) 2 L 7 2 4F A16WE 1998073100579 19980731 00579 NM 1998 7 31 USAA980271 1 19980616 A 5320 65458293 BEAM BOEING 737 737301 1384611 NM BS 326 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 37826 23228 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH AREA OF CORROSION AT BS 326 STRINGER 27 LEFT BEAM. R EPLACED CORRODED AREA OF BEAM PER EA 61852. (M) 2 L 7 2 4F RT A16WE 1998073100580 19980731 00580 NM 1998 7 31 USAA980270 1 19980616 A 5315 6545808159 FLOORBEAM BOEING 737 737301 1384611 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 37826 23228 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM UPPER FLANGE STATION 294 RBBL 1.0. CORROSION TAS K CARD NR C 53-107-01. REPLACED 'T' CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998073100581 19980731 00581 NM 1998 7 31 USAA980269 1 19980616 A 5315 6545815110 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 37826 23228 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM UPPER FLANGE STATION 344 FROM BL 0 TO RT GALLEY D OOR. CORROSION TASK CARD NR C53-107-01. REPLACED 'T' CAP PER TR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998073100582 19980731 00582 NM 1998 7 31 USAA980268 1 19980616 A 5315 6545815110 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 37826 23228 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM STATION 344 FROM LBBL 13.0 TO 28. 0. CORROSION TASK CARD NR C53-107-01. REPLACED 'T' CAP PER TR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998073100583 19980731 00583 NM 1998 7 31 USAA9802267 1 19980616 A 5315 65458123 FLOORBEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 37826 23228 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM UPPER CHORD. CORROSION TASK CARD NR C53-107-01. REPLACED 'T' CAP PER TYPICAL REPAIR NR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998073100584 19980731 00584 NM 1998 7 31 USAA980234 1 19980616 A 5315 654581083 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 300AU 37826 23228 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM STATION 312 AT BL 0 UPPER CHORD. CORROSION TASK CARD NR C53-107-01. INSTALLED DOUBLER REPAIR PLATES ON UPPER FLANGE (FWD) PER REPAIR DOCUMENT SRM 51-70 -12. (M) 2 L 7 2 4F RT A16WE 1998073100585 19980731 00585 NM 1998 7 31 USAABB98063 1 19980607 A 3350 20131ALP BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 606AU 22202 LAX - AFT SECTION OF EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT A2NM 1998073100586 19980731 00586 NM 1998 7 31 USAABB98064 1 19980612 A 3350 8731002511REV9 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 626AU 27303 LAX - FOUND R1, R2 AND L1 DOOR EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. (M) 2 L 7 2 4F RT A2NM 1998073100587 19980731 00587 WP 1998 7 31 USAAD98112 1 19980621 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 993VJ 47332 CMH - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998073100588 19980731 00588 WP 1998 7 31 USAAD98111 1 19980620 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913VJ 45846 IND - THE TAIL COMPARTMENT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE TAIL COMPARTMENT EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998073100589 19980731 00589 NM 1998 7 31 USAASB98152 1 19980619 A 2150 8012403 TURBOFAN BOEING 737 7374B7 1384702 NM RT A/C BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 428US 25739 24550 PIT - FLT 481 - CAPTAIN COULD NOT GET AIRCRAFT TO PRESSURIZE SO HE DECIDED TO RETURN TO FIELD AT PIT. FLIGHT LANDED WIT HOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE RIGHT TURBOFAN SEIZED. REPLACED SAME. OPERATIONAL CH ECK AND PRESSURIZATION CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998073100590 19980731 00590 WP 1998 7 31 USAAD98103 1 19980609 A 3230 UPLATCH DOUG DC9 DC931 3022065 WP LT MLG OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 952VJ 47574 PIT - FLT 305 - AFTER TAKEOFF, CREW RECEIVED A LEFT MAIN LANDING GEAR UNSAFE LIGHT. FLIGHT RETURNED TO PIT AND LANDED W ITH NO FURTHER INCIDENT. MAINTENANCE ADJUSTED THE UPLATCH ON THE LEFT MAIN LANDING GEAR. (M) 2 L 7 2 4F A6WE 1998073100591 19980731 00591 WP 1998 7 31 USAAD98110 1 19980621 A 3260 92743643 RELAY DOUG DC9 DC931 3022065 WP BS 110 FAILED A USAA L ABORTED APPROACH J WARNING INDICATION DE DESCENT 1 EA 19 956VJ 47588 DTW - FLT 388 - DURING LANDING GEAR EXTENTION ON DESCENT THE THREE GREEN GEAR DOWN LIGHTS DID NOT ILLUMINATE. THE CREW RECYCLED THE LANDING GEAR AND THEN HAD THREE RED UNSAFE LIGHTS. THE GEAR WAS MANUALLY EXTENDED, THE CREW VISUALLY CHECK ED THE DOWN LOCK INDICATORS, AND THEN FLEW BY THE TOWER TO CONFIRM THE GEAR WAS DOWN. THE AIRCRAFT LANDED WITHOUT INCID ENT. MAINTENANCE REPLACED THE LANDING GEAR LEVER RELAY AND THE THROTTLE TRANSFER RELAY IN THE LANDING GEAR INDICATION C IRCUIT. (M) 2 L 7 2 4F A6WE 1998073100592 19980731 00592 WP 1998 7 31 USAAD98109 1 19980617 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 997VJ 47336 PIT - THE AFT FUSELAGE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT FUSELAGE EMERGENCY LIGHT BATTERI ES. (M) 2 L 7 2 4F A6WE 1998073100593 19980731 00593 WP 1998 7 31 USAAD98108 1 19980608 A 3350 8732030153 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 DCA - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. ( M) 2 L 7 2 4F A6WE 1998073100594 19980731 00594 WP 1998 7 31 USAAD98107 1 19980607 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 997VJ 47336 CMH - THE RIGHT NACELLE EVACUATION LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT NACELLE EVACUATION LIGHT BATTE RY. (M) 2 L 7 2 4F A6WE 1998073100595 19980731 00595 WP 1998 7 31 USAAD98106 1 19980607 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 981VJ 48157 IND - THE AFT CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN CEILING EMERGENCY LIG HT BATTERIES. (M) 2 L 7 2 4F A6WE 1998073100596 19980731 00596 WP 1998 7 31 USAAD98105 1 19980603 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925VJ 48145 DTW - THE GALLEY ARE OVERHEAD EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE GALLEY AREA OVERHEAD EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998073100597 19980731 00597 EU 1998 7 31 SABA290032 1 19980622 A 3230 7445B VALVE BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 961AE LK8509194 961 BLT/CGS - FLT 5052 - ON TAKEOFF FROM CHARLOTTE, THE NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO CHARLOTTE. NO EM ERGENCY WAS DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND A BAD GEAR RELEASE VALVE. REMOVED AND REPLACED VALVE. GEAR OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A56EU 1998073100598 19980731 00598 EU 1998 7 31 SABA290034 1 19980706 A 3260 9EN1C11HB2BB2 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG LOOSE A SABA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 33 959AE 959 CLT/SOP - FLT 5089 - ON TAKEOFF FROM CLT, THE RT MAIN GEAR UNSAFE LIGHT CAME ON. THEN THE LIGHT WOULD GO OUT THEN BACK ON. AIRCRAFT RETURNED TO CHARLOTTE. NO EMERGENCY WAS DECLARED. AIRCRAFT MADE A SAFE LANDING WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE JAM NUT ON THE UPLOCK SWITCH LOOSE. RE-TORQUED THE UPLOCK SWITCH, SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A56EU 1998073100599 19980731 00599 EU 1998 7 31 REXA98094 1 19980503 A 5610 810441 BOLTS SAAB SF340 SF340A 7850100 EU LT WINDSHIELD LOOSE A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 108PX 741 340A012 LEFT SIDE WINDOW, WINDSHIELD FRAME HAS SEVERAL LOOSE BOLTS. REMOVED AND REPLACED LT SIDE WINDSHIELD. (X) 2 L 7 2 4T RT A52EU 1998073100600 19980731 00600 EU 1998 7 31 REXA98093 1 19980423 A 3230 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG BROKEN A REXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 404BH 340A061 AFTER TAKEOFF, LOST ALL HYDRAULIC (MAIN) PRESSURE. FOUND RT MLG SWIVEL BROKEN. REMOVED AND REPLACED SWIVEL. (X) 2 L 7 2 4T RT A52EU 1998073100601 19980731 00601 EU 1998 7 31 REXA98092 1 19980430 A 2810 FUEL CELL SAAB SF340 SF340A 7850100 EU WS 42 CORRODED A REXA K NONE O OTHER IN INSP/MAINT 1 SO 25 346AM 340A032 CORROSION FOUND IN FUEL CELL AT WS 42.30. REPAIRED RT WING RIB SECTION AT WS 42.30 BY CUTTING OFF FLANGES AT RADIUS. F ABRICATED AND INSTALLED 7075-T6, 0.100 INCH DOUBLER ANGLE. REPAIR WORK IAW SAAB DOCUMENT 72SD0955. (X) 2 L 7 2 4T RT A52EU 1998073100602 19980731 00602 WP 1998 7 31 ORJA98123 1 19980625 A 3010 DUCT DOUG DC9 DC982 3022082 WP A/C MACHINE CRACKED A ORJA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 11 822RA 49932 AIR TURN BACK DUE TO TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON DURING CLIMB. COMPLIED WITH EMERGENCY PROCEDURES. COULD EXTINGUISH LIGHT WITH POWER REDUCTION ONLY AND SO RETURNED FOR PRECAUTIONARY LANDING. FOUND CRACKED DUCT ABOVE A/C MACH INE AFT SIDE RT, ASSIGNED TO DMI 13988 PER MEL 21-1. A/C IS SINGLE PACK OPERATION. REMOVED AND REPLACED RT ACM, DMI 13 988 CLOSED. (M) 2 L 7 2 4F A6WE 1998073100603 19980731 00603 WP 1998 7 31 ORJA98125 1 19980625 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 AFT VENTRAL EMERGENCY EXIT LIGHT INOPERABLE. AFT VENTRAL OVERHEAD LIGHT IS DISPLACED AND HAS BROKEN WIRE. REMOVED AND REPLACED LIGHT ASSY AND REATTACHED LIGHT ASSY TO PANEL AND REPAIRED BROKEN WIRE. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998073100604 19980731 00604 NM 1998 7 31 98ZZZX2512 1 19980628 A 3350 1102833 LIGHT GRIMES 900835A BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 13547 22435 LOG PAGE 20132 - ON PRE-FLIGHT TRANSIT CHECK, FOUND AFT AIRSTAIRS EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT SYSTEM, FOUN D LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY IAW 33-50-00. OPS CHECKED GOOD. (X) 2 L 7 3 4F A3WE 1998073100605 19980731 00605 CE 1998 7 31 98ZZZX2513 1 19980625 A 5210 12951407619 HANDLE BEECH 1900 1900D 1154162 CE PASSENGER DOOR BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 840CA 10920 UE38 CABIN DOOR HANDLE BROKEN. REPLACED CABIN DOOR HANDLE. TEST NORMAL. (X) 2 L 7 2 4T RT A24CE 1998073100606 19980731 00606 CE 1998 7 31 98ZZZX2514 1 19980626 A 3240 5058002643 CONTROL CABLE BEECH 1900 1900D 1154162 CE PARK BRAKE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 861CA 62746 UE164 PARKING BRAKE INOPERATIVE. CONTROL CABLE FAILURE. REPLACED PARKING BRAKE CONTROL CABLE. OPS SATISFACTORY IAW CHAPTER 32. (X) 2 L 7 2 4T RT A24CE 1998073100607 19980731 00607 NE 1998 7 31 98ZZZX2515 2 19980626 A 7314 1143890425 FUEL PUMP ROMEC B108 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 853CA 1678 UE56 RIGHT ENGINE OIL LEAK. FUEL PUMP SEAL FAILURE. REPLACED RT ENGINE FUEL PUMP AND GARLOCK SEAL. LEAK CHECK SATISFACTORY IAW P & W MM CHAPTERS 12 AND 13. 2 L 7 2 4T 4 T RT A24CE E26NE 1998073100608 19980731 00608 NE 1998 7 31 98ZZZX2516 2 19980625 A 7310 A29002 FUEL LINE STRATOFLEX BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE FAILED A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 854CA 10188 UE60 RIGHT ENGINE FUEL LEAK. FUEL LINE FAILURE. REPLACED FUEL LINE. 2 L 7 2 4T 4 T RT A24CE E26NE 1998073100609 19980731 00609 EU 1998 7 31 JBXA980042 2 19980626 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 MALFUNCTIONED A JBXA C ABORTED TAKEOFF M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 05 103ML 11444 17636 DURING TAKEOFF ROLL AT 90-100 KNOTS, NR 1 ENGINE TGT CLIMBED TO 870 DEGREES FOR APPROXIMATELY 2-3 SECONDS. TAKEOFF WAS DISCONTINUED. REMOVED AND REPLACED NR 1 ENGINE IAW MIDWAY AIRLINES WC F4602, F4603, AND F4004. OPERATIONAL CHECK GOOD. PART TOTAL CYCLES: 8,892. (X) 2 L 7 2 4F 4 F RT 1998073100610 19980731 00610 WP 1998 7 31 HALA9800199 1 19980706 A 7830 5958782503 DRIVER LINK DOUG DC9 DC951 3022051 WP NR 2 ENGINE CRACKED A HALA K NONE J WARNING INDICATION LD LANDING 1 WP 13 709HA HAL0026 47764 ITO - FLT 141 - (LOG PAGE NR A144265) - AFTER LANDING IN HILO, RIGHT THRUST REVERSER UNLOCK LIGHT ADVISORY LIGHT WOULD N OT EXTINGUISH. FOUND NR 2 ENGINE BOTTOM BUCKET INBD LOWER DRIVER LINK CRACKED. REPLACED DRIVER LINK PER MM 78-31-5. V ISUALLY INSPECTED THRUST REVERSER, NO VISUAL DEFECTS NOTED, OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998073100611 19980731 00611 WP 1998 7 31 HALA9800168 1 19980621 A 3350 41B004A00763 BATTERIES DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 674MC 47735 47735 HNL - (LOG PAGE NR A145652) - M.E.D. EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERIES, OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998073100612 19980731 00612 WP 1998 7 31 HALA9800170 1 19980622 A 4930 PACKING DOUG DC9 DC951 3022051 WP FUEL MANIFOLD FAILED A HALA K NONE O OTHER TX TAXI/GRND HDL 1 WP 13 679HA 47662 HNL - FLT 114 - (LOG PAGE NR A145677) - FUEL SMELL IN CABIN. REMOVED AND REPLACED PACKING ON APU FUEL MANIFOLD FITTING AND BOTH WATER SEPARATORS. LEAK CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998073100613 19980731 00613 NM 1998 7 31 98ZZZX2517 1 19980626 A 3211 65B1059532 FITTING BOEING 747 747273C 1384896 NM LT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 CORROSION BLEND-OUT/RE-WORK ON TRUNNION SUPPORT FITTINGS - LT INBD TRUNNION CAP FITTING 65B1059532. OPERATOR CONTROL NR 98ZZZX2518 THROUGH 98ZZZX2520. 2 L 7 4 4F A20WE 1998073100615 19980731 00615 NM 1998 7 31 98ZZZX2519 1 19980626 A 3211 65B105953534 FITTING BOEING 747 747273C 1384896 NM LT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 CORROSION BLEND-OUT/RE-WORK ON TRUNNION SUPPORT FITTINGS - INBD TRUNNION VERTICAL SUPPORT FITTING 65B1059535-34. OPERA TOR CONTROL NR 98ZZZX2817 THROUGH 98ZZZX2520. 2 L 7 4 4F A20WE 1998073100616 19980731 00616 NM 1998 7 31 98ZZZX2520 1 19980626 A 3211 65B104624344 FITTING BOEING 747 747273C 1384896 NM LT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 CORROSION BLEND-OUT/RE-WORK ON TRUNNION SUPPORT FITTINGS - OTBD TRUNNION VERTICAL SUPPORT FITTING 65B104624344. OPERA TOR CONTROL NR 98ZZZX2817 THROUGH 98ZZZX2519. 2 L 7 4 4F A20WE 1998073100617 19980731 00617 WP 1998 7 31 TWAA9810315 1 19980620 A 5312 BULKHD FITTING DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - THE UPPER END FITTING ON AFT PRESSURE BULKHEAD LT Z24 RIB WAS CRACKED AT TEE FITTING. REMOVED AND REPLACED END FI TTING PER ARA 15188. CHECK-C 3-12-98 STL. (X) 2 L 7 2 4F A6WE 1998073100618 19980731 00618 WP 1998 7 31 TWAA9810313 1 19980618 A 5311 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - THE Z48 RADIAL FORMER RT SIDE WAS FOUND CRACKED 1 INCH LONG ON OTBD END. REPAIRED FORMER PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100619 19980731 00619 WP 1998 7 31 TWAA9810312 1 19980620 A 5312 BULKHEAD SKIN DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - FOUND BULKHEAD SKIN CRACKED .25 INCH AT LT BULKHEAD AT Z24L, ON OTBD TOP SIDE, SECOND HOLE FORM END. REPAIRED SKI N PER ARA 15189. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100620 19980731 00620 WP 1998 7 31 TWAA9810311 1 19980619 A 5311 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - ON THE LT Z34 RADIAL UPPER OTBD HOLE ON THE FORWARD SIDE, A CRACK INDICATION WAS SHOWN BY EDDY CURRENT. REPAIRED PER TWA ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100621 19980731 00621 WP 1998 7 31 TWAA9810310 1 19980623 A 5311 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - ON LT Z14 RADIAL OTBD LOWER HOLE ON THE FORWARD SIDE, A .25 INCH CRACK WAS INDICATED BY EDDY CURRENT IN THE ATTACH ANGLE. REPAIRED PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100622 19980731 00622 NM 1998 7 31 MASA98132 1 19980628 A 3350 AML91LA85 BULB HUNTNG AML51G60G4 DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING ROUTINE MAINTENANCE INSPECTION, MAINTENANCE PERSONNEL FOUND THE FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH NOT ILLUM INATING. REPLACED BULB, OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998073100623 19980731 00623 NM 1998 7 31 AALA984145 1 19980612 A 5311 FRAME BOEING 767 767323 1385205 NM BS 1285 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 373AA 25200 AFW - BLENDED OUT CORROSION AT NUTPLATES. BLEND OUTS EXCEED SRM LIMITS. REFINISHED BLENDED AREAS. APPROVED FOR CONTIN UED SERVICE WITH NOTED CONDITION OF ENGINEERING PER MRB767-1643. TST: 27,257.02 HOURS. CYCLES: 4,345. (X) 2 L 7 2 4F RT A1NM 1998073100624 19980731 00624 NM 1998 7 31 AALA984144 1 19980612 A 5311 FRAME BOEING 767 767323 1385205 NM BS 1263 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 373AA 25200 AFW - FLAP CORRODED. BLEND-OUT EXCEEDS SRM LIMITS. REFINISHED BLENDED AREAS. APPROVED FOR CONTINUED SERVICE WITH NOTE D CONDITION BY ENGINEERING PER MRB 767-1645. TST: 27,257.02 HOURS. CYCLES: 4,345. (X) 2 L 7 2 4F RT A1NM 1998073100625 19980731 00625 NM 1998 7 31 AALA984142 1 19980612 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 373AA 25200 AFW - FOUND FLOORBEAM CORRODED FOUND DAMAGE TO EXCEED SRM LIMITS AFTER BLENDING. ALODINED BLENDED AREA. FABRICATED A ND INSTALLED REPAIR STRAP USING 0.050 INCH 301 1/2 HARD STAINLESS STEEL. APPROVED BY ENGINEERING PER MRB 767-1646. TST : 27,257.02 HOURS. CYCLES: 4,345. (X) 2 L 7 2 4F RT A1NM 1998073100626 19980731 00626 NM 1998 7 31 AALA9811204 1 19980621 A 2560 416T20521 CAM BOEING 767 767223 1385123 NM LT WING SLIDE BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 327AA 22327 SFO - DURING OVERNIGHT MAINTENANCE, LEFT HAND OVER WING SLIDE COMPARTMENT INFLATION CABLE DISCONNECT CAM BROKEN. REPLAC ED LEFT HAND OVER WING SLIDE CAM ASSEMBLY AND PRECAUTIONARY REPLACED LEFT HAND OVER WING SLIDE BOTTLE. SYSTEM GROUND CH ECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998073100627 19980731 00627 WP 1998 7 31 TWAA9810309 1 19980621 A 5311 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - FOUND LT Z14 RADIAL OTBD UPPER HOLE ON THE FORWARD SIDE WITH .3750 INCH CRACK INDICATION BY EDDY CURRENT. REMOVED AND REPLACED END CLIP PER SRM 51-30-5, AND ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100628 19980731 00628 WP 1998 7 31 TWAA9810308 1 19980621 A 5320 FITTING DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - FOUND UPPER END FITTING ON AFT PRESSURE BULKHEAD RT Z34 RADIAL CRACKED .1250 INCH AT TEE FITTING. REPAIRED PER AR A 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100629 19980731 00629 WP 1998 7 31 TWAA9810307 1 19980621 A 5311 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - THE RT Z34 RADIAL WAS CRACKED ON END ABOUT 1 INCH. REPAIRED PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,63 9 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100630 19980731 00630 WP 1998 7 31 TWAA9810305 1 19980620 A 5311 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - THE LT Z24 RADIAL, UPPER INBD HOLE ON THE FORWARD SIDE SHOWED CRACK INDICATION BY EDDY CURRENT. REMOVED AND REPLA CED FITTING PER ARA 15188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100631 19980731 00631 WP 1998 7 31 TWAA9810306 1 19980621 A 5311 FRAME DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - THE RT Z34 RADIAL OUTBOARD LOWER HOLE ON FORWARD SIDE SHOWED CRACK INDICATION BY EDDY CURRENT. REPAIRED PER ARA 1 5188. CHECK-C 3-12-98 STL. ACFT TT: 66,639 HOURS. ACFT TC: 80,202. (X) 2 L 7 2 4F A6WE 1998073100632 19980731 00632 NM 1998 7 31 TWAA9810304 1 19980627 A 3350 20131A BATTERY PACK BOEING 767 767231 1385131 NM FUSELAGE DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 608TW 22571 JFK - FLT 904 - THREE EXTERIOR EMERGENCY LIGHTS INOPERATIVE ABOVE RT WING. REPLACED EMERGENCY BATTERY PACK RT SIDE STA 430. CHECK-C 5-4-98 LAX. (X) 2 L 7 2 4F RT A1NM 1998073100633 19980731 00633 NM 1998 7 31 TWAA9810303 1 19980627 A 3350 58225 POWER SUPPLY BOEING 727 727231 1384079 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 54336 20490 STL - FLT 611 - EGRESS LIGHTING AFT OF ROW 22 CAME ON IN-FLIGHT. REPLACED EGRESS POWER SUPPLY ABOVE SEAT 24. CHECK-C 1 0-21-97 MCI. (X) 2 L 7 3 4F A3WE 1998073100634 19980731 00634 WP 1998 7 31 TWAA9810302 1 19980627 A 3350 595723215 BATERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 414EA 47746 STL - FLT 27 - EGRESS LIGHTS OUT FROM FRONT OF CABIN TO ABOUT ROW 10. REPLACED FORWARD BATTERY PACK AND REPAIRED FEEDER STRIP. CHECK-C 6-9-98 STL. (X) 2 L 7 2 4F RT A6WE 1998073100635 19980731 00635 WP 1998 7 31 TWAA9810301 1 19980626 A 3310 G033411 LIGHT DOUG DC9 DC931 3022065 WP COCKPIT SHORTED A TWAA H DEACTIVATE SYST/CIRCUITS B A SMOKE/FUMES/ODORS/SPARKS FLAME/FIRE NR NOT REPORTED 1 CE 05 989Z 47135 STL - FLT 579 - FIRST OFFICER'S LIGHT ON YOKE STARTED TO SMOKE AND ARC. REPLACED CHART HOLDER. CHECK-C 6-13-98 STL. ( X) 2 L 7 2 4F A6WE 1998073100636 19980731 00636 EU 1998 7 31 98ZZZX2521 1 19980519 A 5260 14860011 ACTUATOR AEROSP SA365 AS365N2 8680815 EU STOP FAILED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365WM 1789 16544 6429 STEP ACTUATOR INOPERATIVE. REMOVED AND REPLACED ACTUATOR. 1 G 7 2 3U RT H10EU 1998073100637 19980731 00637 EU 1998 7 31 98ZZZX2522 1 19980623 A 6320 4639311005 SHAFT BOLKMS 105 BO105LSA3 5626020 EU M/R DRIVE DEFECTIVE A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 202LF 1198 2014 RECEIVED SHAFT UNIT IN NEW CONDITION AND FOUND THE PLATING WAS PEELING OFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998073100638 19980731 00638 EU 1998 7 31 98ZZZX2523 1 19980623 A 6320 4639311005 SHAFT BOLKMS 105 BO105LSA3 5626020 EU M/R DRIVE DEFECTIVE A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 202LF 1238 2014 RECEIVED UNIT IN NEW CONDITION AND FOUND THE PLATING WAS PEELING OFF. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998073100639 19980731 00639 EU 1998 7 31 98ZZZX2524 1 19980607 A 2810 FTA017521E TANK BOLKMS 105 BO105LSA3 5626020 EU MAIN FUEL LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 203LF 44 46483 2015 FUEL TANK LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1998073100640 19980731 00640 NE 1998 7 31 98ZZZX2525 2 19980529 A 7321 8080803011 EEC DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE ENGINE FAILED A R7MA K NONE L NO TEST IN INSP/MAINT 1 NM 11 901CF 2494 C96010028 90000012 PCE206042 EEC FAILED TO PASS OVERSPEED TEST. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1998073100641 19980731 00641 SW 1998 7 31 98ZZZX2526 1 19980404 A 6230 206010443001 BEARING 206010450113 BELL 206 206L1 1182107 SW SWASHPLATE FAILED B L ZV1R K NONE O OTHER IN INSP/MAINT 1 SW 03 2654 15079 GDJG9483 45482 SWASHPLATE DUPLEX BEARING, SN 19247, FAILED AT 367.3 HOURS TIME SINCE NEW. DAMAGED OUTER RING, PN 206-010-453-0009, S/N GD9083-7 AND CAP, P/N 206-010-444-001. 1 G 7 1 3U H2SW 1998073100642 19980731 00642 EU 1998 7 31 98ZZZX2527 1 19980126 A 3340 4171072 LIGHT AEROSP SA365 SA365N 8680669 EU LANDING LIGHT FAILED A ZYWA K NONE O OTHER IN INSP/MAINT 1 GL 09 365SJ 3141 20359 6018 LANDING LIGHT INOPERATIVE. REMOVED AND REPLACED LANDING LIGHT. 1 G 7 2 3U H10EU 1998073100661 19980731 00661 SW 1998 7 31 HEEA0015179 1 19980713 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX SEPARATED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 403PH 804 53177 MAIN ROTOR GEARBOX MOUNT SEPARATED BEYOND LIMITS. 1 G 7 1 3U O H2SW 1998073100716 19980731 00716 1998 7 31 TWAA9812001 4 19980724 A 3442 MI5920412 RT UNIT BOEING 727 727231 1384079 NM NR 1 FAILED A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 54354 21986 SMOKE REPORTED TO BE COMING FROM BEHIND THE FIRST OFFICERS INSTRUMENT PANEL. FLIGHT DIVERTED TO ABQ. FOUND WEATHER RAD AR CIRCUIT BREAKER POPPED. REPLACED WEATHER RADAR NR 1 RECEIVER/TRANSMITTER. CHECKED ELECTRICAL WIRE BUNDLES IN ELECTR ONIC COMPT, CHECKED AREA BETWEEN RUDDER PEDALS, SHOOK DOWN WIRE BUNDLES WHILE WINDSHIELD HEAT IN OPERATION, OPERATED ALL COCKPIT LIGHTING AND RADIOS. UNABLE TO DUPLICATE OR FIND EVIDENCE OF SMOKE OR BAD WIRING. DID FIND RADAR R/T AND RACK DAMP. CLEANED RACK. CHECK-C 5-21-98 MCI. 2 L 7 3 4F A3WE 1998073100717 19980731 00717 WP 1998 7 31 TWAA9812002 1 19980715 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND A CRACK IN FUSELAGE SKIN LEFT SIDE JUST BELOW THE LEFT PYLON STA 965. AREA HAD AN INTER IM REPAIR WITH BLIND FASTENERS. ACCOMP EDDY CURRENT AND NO CRACKS FOUND, REF 51-00-03. INSTALLED DOUBLER PER SRM 53-04 , PAGE 93. 2 L 7 2 4F A6WE 1998073100718 19980731 00718 WP 1998 7 31 TWAA9812003 1 19980715 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 965, FORMER S29L TO S29R. SPLICE REPAIRED FORMER PER SRM 53-03, FIG 2A . 2 L 7 2 4F A6WE 1998073100719 19980731 00719 WP 1998 7 31 TWAA9812004 1 19980720 A 5312 BULKHEAD DOUBLER DOUG DC9 DC932 3022066 WP BS 965 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND SPAR WEB DOUBLER ON AFT SIDE OF BULKHEAR WEB, STA 965 RT SIDE, CRACKED. REPAIRED WITH . 090 DOUBLER 2024-T3 AND INSTALLED PER MO 72J15, PHASE K AND DAC DRAWING 4709532 AND 5936993. 2 L 7 2 4F A6WE 1998073100720 19980731 00720 WP 1998 7 31 TWAA9812005 1 19980720 A 5312 BULKHEAD WEB DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND BULKHEAD 965 RBL 58, APPROX 28 IN ABOVE FLOOR LINE WITH CRACK IN WEB. STOP DRILLED AND INSTALLED DOUBLER. INSTALLED NEW WEB PER MO 72J15, PHASE K, PER DRAWING 4709532 REV A, AND 5936993 REV D. 2 L 7 2 4F A6WE 1998073100721 19980731 00721 WP 1998 7 31 TWAA9812006 1 19980717 A 5512 SKIN DOUG DC9 DC932 3022066 WP LT HORIZ STAB DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND LT HORIZ STAB, LEADING EDGE OF STAB DAMAGED AND FILLET DETERIORATED APPROX 20 IN FROM O/ B END. INSTALLED DOUBLER PER SRM 55-03, FIG 3 PG 5. 2 L 7 2 4F A6WE 1998073100722 19980731 00722 WP 1998 7 31 TWAA9812007 1 19980717 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND FRAME WITH APPROX 1 IN CRACK AT STA 980, LONGERON 17R. ACCOMPLISHED FRAME REPAIR BY CUT TING DAMAGED SECTION OUT BETWEEN L14R AND L16R, AND FLOOR LINE. INSTALLED NEW SECTIONS OF FRAME AND SPLICED PER SRM 53- 03, FIG 32, SHEETS 1 THRU 5. 2 L 7 2 4F A6WE 1998073100723 19980731 00723 WP 1998 7 31 TWAA9812008 1 19980717 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 1010 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND INTERCOASTAL CRACKED AT AFT END OF PULLEY CLUSTER AT STA 1010, RBL 20 INCHES. NEW SUPPO RT FABRICATED IN SHOP PER DRAWING 9915540, DRILLED NEW PART AND INSTALLED AND SEALED PER SRM 53-03. 2 L 7 2 4F A6WE 1998073100724 19980731 00724 WP 1998 7 31 TWAA9812009 1 19980717 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 815 WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND FUSELAGE SKIN WORN AT LONGERON 26L, STA 815, UNDER FUSELAGE FAIRING. TRIMMED DAMAGED AR EA WHICH IS FOR A LAP SEAM. INSTALLED REPAIR PER SRM 53-04 FIG 12B. 2 L 7 2 4F A6WE 1998073100725 19980731 00725 WP 1998 7 31 TWAA9812010 1 19980713 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND LONGERON 17R CRACKED AT STA 965. REPLACED CRACKED LONGERON PER SRM 53-02, PG 48 TO 53. INSTALLED RIVETS COMMON TO SKIN AND LONGERON PER SRM 51-30, PG 1 AND 6. USED MS 20615-M-4 AND AN960B4 WASHERS. 2 L 7 2 4F A6WE 1998073100726 19980731 00726 WP 1998 7 31 TWAA9812011 1 19980713 A 5400 ANGLE DOUG DC9 DC931 3022065 WP NR 1 PYLON CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND LOWER ATTACH ANGLE AT FUSELAGE CRACKED 1.5 IN AT FWD END OF NR 1 PYLON. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE FROM 177PH STEEL, .040 IN. INSTALLED WITH MONEL RIVETS REF DWG 5923062. 2 L 7 2 4F A6WE 1998073100727 19980731 00727 WP 1998 7 31 TWAA9812012 1 19980713 A 5512 SKIN DOUG DC9 DC931 3022065 WP RT HORIZ STAB CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND RT STAB L/E CRACKED 3 INCHES IN UPPER FLANGE OF L/E SECT AT XFS 40. FABRICATED DOUBLER AND INSTALLED PER SRM 55-01, PAGE 8. 2 L 7 2 4F A6WE 1998073100728 19980731 00728 WP 1998 7 31 TWAA9812013 1 19980713 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 945 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND CRACK IN FORMER FOOT STA 945, BETWEEN L14L AND L15L. REMOVED AND DISCARDED FORMER FRAME , INSTALLED NEW TWA STOCK NR 16-0585 FRAME PER SRM 53-03, FIG 3. 2 L 7 2 4F A6WE 1998073100729 19980731 00729 WP 1998 7 31 TWAA9812014 1 19980715 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 446 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND FLOOR SUPPORT CAP, ATTACH TO FORMER, CRACKED AT FS 446 ABOVE LONGERON 28. REMOVED FLOOR SUPPORT, WELDED PER SHOP TAG NR 795242. REINSTALLED FLOOR SUPPORT. 2 L 7 2 4F A6WE 1998073100730 19980731 00730 WP 1998 7 31 TWAA9812015 1 19980714 A 5744 CASTING DOUG DC9 DC931 3022065 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND CRACK ON RT WING T/E FLAP O/B HINGE CASTING, I/B UPPER ATTACH FRAME. REPLACED CRACKED F RAME WITH NEW FRAME AND INSTALLED FASTENERS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998073100731 19980731 00731 WP 1998 7 31 TWAA9812016 1 19980714 A 5744 CASTING DOUG DC9 DC931 3022065 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND 1 INCH CRACK ON RT WING T/E FLAP O/B HINGE CASTING, O/B UPPER ATTACH FLANGE. REPLACED C RACKED FRAME WITH PART NR 165489. INSTALLED FASTENERS PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998073100732 19980731 00732 WP 1998 7 31 TWAA9812017 1 19980714 A 5330 DOUBLER DOUG DC9 DC931 3022065 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND DOUBLER ABOVE LONGERON 16R AT STA 980 WAS CRACKED. REMOVED DAMAGED PART, FORMED NEW PAR T ONE GAUGE HEAVIER, PAINTED AND INSTALLED WITH FASTENERS LIKE REMOVED. 2 L 7 2 4F A6WE 1998073100733 19980731 00733 WP 1998 7 31 TWAA9812018 1 19980716 A 5315 FLOORBEAM DOUG DC9 DC931 3022065 WP BS 996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FS 996, LBL 21 TO LBL 41, CORROSION REMOVED ON FLOORBEAM CAP WAS BEYOND LIMITS. INSTALLED REP AIR DOUBLER PER SRM 53-05, FIG 20A. 2 L 7 2 4F A6WE 1998073100734 19980731 00734 WP 1998 7 31 TWAA9812019 1 19980716 A 5280 HINGE DOUG DC9 DC931 3022065 WP LT MLG DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND LT MLG STRUT DOOR HINGE, NR 5 HINGE LUG ON WING SIDE OF HINGE, CRACKED. CONFIRMED WITH EDDY CURRENT. REPLACED DOOR HINGE MFG (P/N 2924290-501) PER DWG 5910484. TORQUE FASTENERS PER SRM 51-30-1P PG 13. REA MED HOLES PER SRM 51-10-4, PAGE 4. 2 L 7 2 4F A6WE 1998073100735 19980731 00735 WP 1998 7 31 TWAA9812020 1 19980717 A 5320 DOOR FRAME DOUG DC9 DC931 3022065 WP BS 363.5 MISDRILLED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND .5 IN DIA HOLE AT FS 363.5, L29R, FORMER FOR DOOR FRAME CAP. REPAIRED PER ARA 92227. 2 L 7 2 4F A6WE 1998073100736 19980731 00736 WP 1998 7 31 TWAA9812101 1 19980713 A 5330 SKIN DOUG DC9 DC931 3022065 WP E/E COMP DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, NEC COMPLY WITH ET NR 016 ON ELECTRONIC COMPT ACCESS DOOR CUTOUT. REPAIRED PER ARA 9222. 2 L 7 2 4F A6WE 1998073100737 19980731 00737 WP 1998 7 31 TWAA9812102 1 19980708 A 5320 PAN DOUG DC9 DC931 3022065 WP EMER EXIT DRWAY DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, NEC COMPLY WITH ET NR 018 ON RT FWD EMERGENCY EXIT DOOR PAN. REPAIRED EMERGENCY EXIT DOOR PER SRM 52-05, PG 300, CONFIG 7003. 2 L 7 2 4F A6WE 1998073100738 19980731 00738 WP 1998 7 31 TWAA9812103 1 19980713 A 5320 PAN DOUG DC9 DC931 3022065 WP EMER EXIT DRWAY DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, NEC COMPLY WITH ET NR 018 ON RT AFT EMERGENCY EXIT DOOR PAN. REPAIRED EMERG EXIT DOOR PAN PER SRM 52-05 CONFIG -7003. 2 L 7 2 4F A6WE 1998073100739 19980731 00739 WP 1998 7 31 TWAA9812104 1 19980714 A 5312 BULKHEAD FITTING DOUG DC9 DC982 3022082 WP AFT PRESS BLKHD DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 922TW 48013 DURING CHECK-C MAINT, FOUND THE AFT BULKHEAD T-FITTING DAMAGED. CRACK WAS 2.5 BY 1.7 AT AREA OF AFT JACK POINT. REMOV ED AND REPLACED T AS PER SRM 53-03, FIG 37A. 2 L 7 2 4F A6WE 1998073100740 19980731 00740 NM 1998 7 31 TWAA9812105 1 19980719 A 5330 SKIN BOEING 767 767231 1385131 NM BS 428-470 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DUE TO DAMAGE INCIDENT THE LT SIDE OF FUSELAGE WAS DENTED FROM STA 428 TO 470, STR 34L TO 37L, WITH A SKIN TEAR 14 IN B Y 6 IN. REPAIRED PER ARA 11576. CHECK-C 4-20-98 LAX. 2 L 7 2 4F RT A1NM 1998073100741 19980731 00741 NM 1998 7 31 TWAA9812106 1 19980719 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 456 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DUE TO A DAMAGE INCIDENT STR 36L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03 DETAIL III. 2 L 7 2 4F RT A1NM 1998073100742 19980731 00742 NM 1998 7 31 TWAA9812107 1 19980719 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 456 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DUE TO A DAMAGE INCIDENT STR 35L WAS CRACKED AT STA 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III. 2 L 7 2 4F RT A1NM 1998073100743 19980731 00743 NM 1998 7 31 TWAA9812108 1 19980719 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 429-456 BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DUE TO A DAMAGE INCIDENT STR 37L WAS BENT AND TWISTED AND RIVETS POPPED. CENTER STRAP TWISTED BETWEEN STA 429 AND 456. REPAIRED PER 767 SRM 53-00-03, DETAIL III, AND ARA 11576. 2 L 7 2 4F RT A1NM 1998073100744 19980731 00744 NM 1998 7 31 TWAA9812109 1 19980719 A 5330 SKIN BOEING 767 767231 1385131 NM BS 430-440 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DUE TO A DAMAGE INCIDENT FOUND 14 IN BY 1 IN DEEP DENT ON FUSELAGE SKIN, STA 430 TO 440, LOCATED BETWEEN STR 35L AND 37L . REPAIRED PER ARA 11576. 2 L 7 2 4F RT A1NM 1998073100745 19980731 00745 NM 1998 7 31 TWAA9812110 1 19980719 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DUE TO A DAMAGE INCIDENT STRINGER 36L SPLICE AREA CRACKED AT STA 434. REPAIRED PER 767 SRM 53-00-03 DETAIL III. 2 L 7 2 4F RT A1NM 1998073100746 19980731 00746 NM 1998 7 31 TWAA9812111 1 19980719 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 460 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DURING WORK ON A DAMAGE INCIDENT FOUND STRINGER 34L WITH SURFACE CORROSION AT STA 460, JUST FWD OF FORMER. REPAIRED PER SRM 53-00-03, DETAIL III. CHECK-C 4-20-98 LAX. 2 L 7 2 4F RT A1NM 1998073100747 19980731 00747 NM 1998 7 31 TWAA9812112 1 19980719 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 448 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 FOUND DURING DAMAGE REPAIRS STRINGER 33L HAD CORROSION AT STA 448. REPAIRED PER SRM 53-00-03 DETAIL III. CHECK-C 4-20- 98 LAX. 2 L 7 2 4F RT A1NM 1998073100748 19980731 00748 NM 1998 7 31 TWAA9812113 1 19980719 A 5320 SPLICE BOEING 767 767231 1385131 NM BS 434 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DURING DAMAGE REPAIRS FOUND SPLICE PLATE CRACKED AT RIVET HOLE TO MATERIAL EDGE AT STA 434, STR 36. REPAIRED PER ARA 11 576. 2 L 7 2 4F RT A1NM 1998073100749 19980731 00749 NM 1998 7 31 TWAA9812114 1 19980719 A 5320 STRAP BOEING 767 767231 1385131 NM BS 456 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 STRAP CRACKED AND TORN AT RIVET HOLES STA 456, BETWEEN S35 AND S36. REPAIRED PER ARA 11576. 2 L 7 2 4F RT A1NM 1998073100750 19980731 00750 WP 1998 7 31 TWAA9812115 1 19980722 A 5320 TIE DOUG DC9 DC932 3022066 WP BS 994 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND STRINGER END TIE CORRODED AT STA 994, STR 27R AND 28R. REMOVED AND REPLACED 2 (P/N 4912 515-1), INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-05. 2 L 7 2 4F A6WE 1998073100751 19980731 00751 WP 1998 7 31 TWAA9812116 1 19980722 A 5312 BULKHEAD CHORD DOUG DC9 DC932 3022066 WP BS 604 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND AT FS 604, THE AFT BULKHEAD OF THE FWD CARGO COMPT, THE BOTTOM CHORD AT STA 30 HAD AREA OF CORROSION. REMOVED CORROSION PER SRM 51-10-03. REPAIRED PER SRM 53-03, FIG 10 ITEM 503. 2 L 7 2 4F A6WE 1998073100752 19980731 00752 WP 1998 7 31 TWAA9812117 1 19980723 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK LONGERON 23L HAD 1.5 IN CRACK IN O/B FLANGE RUNNING DOWN INTO RADIUS AT FS 200. CONFIRMED BY E DDY CURRENT. REMOVED CRACKED LONG, INSTALLED NEW LONG FROM FACTORY SPLICE TO FACTORY SPLICE, INSTALLED FASTENERS PER SR M 51-30-0 AND 51-30-02. 2 L 7 2 4F A6WE 1998073100753 19980731 00753 WP 1998 7 31 TWAA9812118 1 19980723 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 465-579 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND RT CENTER CABIN FLOOR PANEL AT FS 465 TO 579 WITH 5 CRACKS AT U-CHANNELS ON BOTTOM SIDE, NR 39 PANEL. NEW PANEL FABRICATED PER SSRM 53-00-104. 2 L 7 2 4F A6WE 1998073100754 19980731 00754 WP 1998 7 31 TWAA9812119 1 19980723 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, ON RT WING UPPER SURFACE WING SKIN FOUND CRACK AT O/B AFT CORNER OF FUEL TANK ACCESS PLATE NR 1410A. STOP DRILLED CRACK, INSTALLED DOUBLER PER DRW 5951593RE. ACCOMP NDT CRACK CONTAINMENT CHECK PER 51-00-03. 2 L 7 2 4F A6WE 1998073100755 19980731 00755 WP 1998 7 31 TWAA9812120 1 19980721 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, 6 IN LBL TO 6 IN RBL. REMOVED CORROSION B Y CUTTING OUT CORRODED SECTION PER SRM 53-03, FIG 9 PAGE 12B. INSTALLED DOUBLER PER SRM 53-03, FIG 9. 2 L 7 2 4F A6WE 1998073100756 19980731 00756 WP 1998 7 31 TWAA9812121 1 19980721 A 5330 SKIN DOUG DC9 DC932 3022066 WP RT MLG WW CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND AT BOTTOM OF FUSELAGE SKIN AT FWD END OF RT WHEEL WELL, CORROSION THRU WHERE HINGE PIN S HIELD COVERS. REMOVED CORROSION PER SRM 51-10-03. REPAIRED PER SRM 53-04, FIG 38. REINSTALLED BATH TUB FITTING AND RE LATED PARTS PER SRM 51-30-0, PG 1. 2 L 7 2 4F A6WE 1998073100757 19980731 00757 WP 1998 7 31 TWAA9812122 1 19980720 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965. REPLACED SECTION OF LONGERON FROM FS 955 TO 996, PER S RM 51-10, PG 1 ITEM C, AND INSTALLED LONGERON SPLICE PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1998073100758 19980731 00758 WP 1998 7 31 TWAA9812123 1 19980720 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP FUSELAGE MISINSTALLED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND REPAIR INSTALLED WITH BLIND FASTENERS ON FUSELGE SKIN AND NO DOUBLER AT STA 965 AND 970 BETWEEN LONG 16L AND 17L. REPLACED BLIND FASTENERS AND INSTALLED FINGER DOUBLER PER SRM 53-04, PAGE 93. 2 L 7 2 4F A6WE 1998073100759 19980731 00759 WP 1998 7 31 TWAA9812124 1 19980720 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 965-980 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL AT 29R BADLY CORRODED AT STA 965 TO 980. MADE NEW PER SRM 51-01, FABRICATED INTERCOSTAL FROM 7075-0 AND HEAT TREATED PER SRM 53-11-3 PAGE 108. REMOVED CORROSION BY REPLACING INTERCOSTAL PER SRM 51-01, PAGE 1 ITEM C. INSTALLED RIVETS PER SRM 51-30-02. SMOOTHED AND FINISH PAINTED PER STD PRACTICE. 2 L 7 2 4F A6WE 1998073100760 19980731 00760 WP 1998 7 31 TWAA9812125 1 19980721 A 5522 SKIN DOUG DC9 DC931 3022065 WP RT ELEVATOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND RT ELEVATOR LOWER O/B SKIN PANEL WITH 2 CREASES. REMOVED AND REPLACED LOWER O/B SKIN PA NEL PER DWG 5910412-516. 2 L 7 2 4F A6WE 1998073100761 19980731 00761 WP 1998 7 31 TWAA9812126 1 19980720 A 5754 SKIN DOUG DC9 DC932 3022066 WP NR 1 LE FLAP DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND DENT ON NR 1 L/E SLAT, LT WING, EXCEEDING ALLOWABLE LIMITS PER SRM 57-03, PG 20A. DENT IS 2.5 BY 17 IN BY .150 DEEP. CUT OUT DAMAGED SKIN AND INSTALLED REPAIR PER SRM 57-09, FIG 10F. 2 L 7 2 4F A6WE 1998073100762 19980731 00762 WP 1998 7 31 TWAA9812127 1 19980718 A 5320 ATTACT TEE DOUG DC9 DC982 3022082 WP APU COMPT DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 922TW 48013 DURING CHECK-C MAINT, FOUND APU RT SIDEWALL ATTACH T WITH END FLANGE CUT OFF WITH 3 ATTACH HOLES TO GAIN ACCESS. INSTAL LED FILLERS AND DOUBLERS PER ARA 15416 AND 15416A. 2 L 7 2 4F A6WE 1998073100763 19980731 00763 WP 1998 7 31 TWAA9812128 1 19980722 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 658 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OVERNIGHT MAINT, FOUND LONGERON 6R AT STA 658 WITH .750 IN CRACKS AT FRAME ATTACH POINTS. FOUND ACCOMPLISHING WO RK SHEET MC8-AD-AM. REPAIRED LONGERON PER SRM 53-02 AS REQUIRED. CHECK-C 1-8-98 STL. 2 L 7 2 4F A6WE 1998073100764 19980731 00764 WP 1998 7 31 TWAA9812129 1 19980722 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 680 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OVERNIGHT MAINT, FOUND LONGERON 6R AT STA 680 WITH .750 INCH CRACKS AT FRAME ATTACH POINTS. FOUND ACCOMPLISHING WORK CARD MC8-AD-AM. REPAIRED LONGERON PER SRM 53-02. CHECK-C 1-8-98 STL. 2 L 7 2 4F A6WE 1998073100765 19980731 00765 NM 1998 7 31 TWAA9812130 1 19980724 A 5753 SKIN BOEING 767 767205 1385121 NM LT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, FOUND LT WING O/B FLAP LOWER SKIN WITH 2 IN CRACK APPROX 18 IN FROM I/B END AND APPROX 12 IN FROM T/E. CUT OUT DAMAGED AREA AND INSTALLED FIBER GLASS 250 DEG CURE HOT BOND REPAIR PER SRM 57-53-01 AND 51-70-07. 2 L 7 2 4F RT A1NM 1998073100766 19980731 00766 NM 1998 7 31 TWAA9812131 1 19980721 A 5755 SKIN BOEING 767 767205 1385121 NM NR 5 SPOILER TORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, FOUND NR 5 SPOILER T/E 1.5 IN TEAR IN SPOILER PANEL. REPAIRED PER SRM. INSTALLED LAYER ADHESIVE AND LAYER FABRIC AND HOT BOND 6 BY 6 PER SRM 51-70-17, FIG 19 ITEM 3H. 2 L 7 2 4F RT A1NM 1998073100767 19980731 00767 WP 1998 7 31 TWAA9812132 1 19980723 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 200-205 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORT AT FS 200 TO 205, RBL 53. REMOVED CORRODED FLOOR SUPPO RT FROM STA 160 TO 205. MADE NEW PART, INSTALLED WITH SAME TYPE AND SIZE FASTENERS PER SRM 53-11-1, PG 47 ITEM 10. 2 L 7 2 4F A6WE 1998073100768 19980731 00768 WP 1998 7 31 TWAA9812133 1 19980720 A 5347 FLOOR TRACK DOUG DC9 DC931 3022065 WP BS 200-240 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR TRACK NR 4, FS 200 TO 240. INSTALLED NEW TRACK STA 200 TO FACT ORY SPLICE STA 267. 2 L 7 2 4F A6WE 1998073100769 19980731 00769 WP 1998 7 31 TWAA9812134 1 19980720 A 5347 FLOOR TRACK DOUG DC9 DC931 3022065 WP BS 200-240 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR TRACK NR 3, FS 200 TO 240. REMOVED CORRODED FLOOR TRACK AND RE PLACED WITH NEW FROM STA 200 TO FACTORY SPLICE AT STA 267. 2 L 7 2 4F A6WE 1998073100770 19980731 00770 WP 1998 7 31 TWAA9812135 1 19980720 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 180-195 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND CABIN FLOOR SUPPORT GROUND OUT OF LIMITS AT LBL 49, STA 180 TO 195. FABRICATED NEW FLOO R SUPPORT FROM 70757-6 EXT PER SRM 53-11-1, PAGE 47 ITEM 10. 2 L 7 2 4F A6WE 1998073100771 19980731 00771 WP 1998 7 31 TWAA9812202 1 19980724 A 5522 SKIN DOUG DC9 DC931 3022065 WP LT ELEVATOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND LT ELEVATOR O/B LOWER SKIN PANEL WITH 2 REPAIRS. INSTALLED NEW LOWER PANEL, O/B END PER DAC DWG 5910412-1. 2 L 7 2 4F A6WE 1998073100772 19980731 00772 WP 1998 7 31 TWAA9812203 1 19980722 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND LONGERON 16L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTIO N AND SPLICED PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1998073100773 19980731 00773 WP 1998 7 31 TWAA9812204 1 19980724 A 5522 SKIN DOUG DC9 DC931 3022065 WP LT ELEVATOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND LT ELEVATOR O/B T/E WITH STRIPPER DAMAGE. REMOVED AND REPLACED THE T/E PER DAC DWG 5910 412-1. 2 L 7 2 4F A6WE 1998073100774 19980731 00774 WP 1998 7 31 TWAA9812205 1 19980724 A 5522 SKIN DOUG DC9 DC931 3022065 WP LT ELEVATOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND LT ELEVATOR O/B TOP SKIN PANEL WITH REPAIR. FABRICATED NEW PANEL PER DAC SRM 55-03, PG 23 AND 24. INSTALLED NEW PANEL PER DAC DWG 5910412-1. 2 L 7 2 4F A6WE 1998073100775 19980731 00775 WP 1998 7 31 TWAA9812206 1 19980722 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965, AFT SIDE OF BULKHEAD. REPLACED CRACKED LONGERON SECTIO N AND SPLICED PER SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1998073100776 19980731 00776 WP 1998 7 31 TWAA9812207 1 19980723 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 994 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 976Z 47248 DURING CHECK-C, FOUND BULGE IN SKIN AT STA 994, STR 25L. REPLACED CORRODED TIE WITH NEW TIE USING RIVETS AND HI-LOKS PE R SRM 51-01, PG 4, 51-30-5, AND TWA DRAWING 5911423. 2 L 7 2 4F A6WE 1998073100777 19980731 00777 NM 1998 7 31 TWAA9812208 1 19980717 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 680 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54335 20462 DURING CHECK-C, FOUND FUSELAGE STRINGERS CORRODED AT FS 660 TO 680, S27L TO S27R. REMOVED 3 T ANGLE STIFFENERS, REMOVED CORROSION BY ABRASIVE SANDING AND RE-INSTALLED PER SRM 51-10-6, PG 5. 2 L 7 3 4F A3WE 1998073100778 19980731 00778 NM 1998 7 31 TWAA9812209 1 19980722 A 5712 RIB BOEING 727 727231 1384079 NM RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54335 20462 DURING CHECK-C, FOUND CRACK 17 IN LONG AT BOTTOM OF RT WING RIB WEB ANGLE, 27 IN O/B OF WING BODY FAIRING, FWD. REMOVED AND REPLACED WEB ANGLE AT O/B END OF WING BODY FAIRING, PER SRM 51-10-1, AND 51-40-3. 2 L 7 3 4F A3WE 1998073100779 19980731 00779 NM 1998 7 31 TWAA9812210 1 19980721 A 5313 STRINGER BOEING 727 727231 1384079 NM BS 720 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54335 20462 DURING CHECK-C, FOUND FS 720, S28L WITH CORROSION. HEAVY CORROSION ON STRINGER, LIGHT SKIN CORROSION. REMOVED SKIN COR ROSION PER SRM 51-10-6, AND FABRICATED NEW STRINGER AND INSTALLED PER SRM 51-10-1. 2 L 7 3 4F A3WE 1998073100780 19980731 00780 NM 1998 7 31 TWAA9812211 1 19980722 A 5330 SKIN BOEING 727 727231 1384079 NM LT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54335 20462 DURING CHECK-C, FOUND 14 IN BY 2 IN BY .375 IN HOLE IN LT WING L/E ABOVE LANDING LIGHT. ACCOMP FLUSH REPAIR PER SRM 57- 30-4, PAGES 2B, 3, AND 4, FIG 2. 2 L 7 3 4F A3WE 1998073100781 19980731 00781 NM 1998 7 31 TWAA9812212 1 19980722 A 5753 SKIN BOEING 727 727231 1384079 NM RT TE FOREFLAP WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54335 20462 DURING CHECK C, FOUND RT WING RT O/B FOREFLAP WITH ROUND DEPRESSION WORN IN I/B LEADING EDGE. INSTALLED 2024-T42 DOUBLE R PER SRM 57-50-4, PG 2B. 2 L 7 3 4F A3WE 1998073100782 19980731 00782 WP 1998 7 31 TWAA9812213 1 19980721 A 5522 SKIN DOUG DC9 DC931 3022065 WP RT ELEVATOR DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND RT ELEVATOR O/B TRAILING EDGE DELAMINATED. REMOVED AND REPLACED THE O/B TRAILING EDGE P ER DWG 5910412-516. 2 L 7 2 4F A6WE 1998073100783 19980731 00783 NM 1998 7 31 K3HA980094 1 19980727 A 3350 BC50087 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 REPAIR EMERGENCY PATH LIGHTING TRACK AT POSITION FORWARD OF SEAT ROW 2ABC. REMOVED AND REPLACED 2.5 FEET OF EMERGENCY P ATH TRACK LIGHTING. OPS CHECK GOOD REF MM 33-50. 2 L 7 3 4F A3WE 1998073100784 19980731 00784 WP 1998 7 31 9809839948 1 19980725 A 3260 SENSOR DOUG DC9 DC931 3022065 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 8929E 45866 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. FLIGHT CREW CONFIRMED VISUALLY THROUGH PEEP H OLE THAT GEAR WAS DOWN AND LOCKED. EMERGENCY EQUIPMENT WAS REQUESTED ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED WITHO UT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK SENSOR BROKEN. REPLACED SENSOR. OPERATIONAL CHECK NORMAL ON GEAR SW ING. 2 L 7 2 4F A6WE 1998073100785 19980731 00785 WP 1998 7 31 9809849916 1 19980727 A 2910 FITTING DOUG DC9 DC932 3022066 WP RT MLG WW LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 01 949N 47566 DURING CRUISE FLIGHT, RIGHT HYDRAULIC SYSTEM QUANTITY DROPPED TO 4 QUARTS. FLIGHT CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FITTING LEAKING AT RIGHT WHEEL WELL PRIO RITY VALVE. REPLACED PACKING, LEAK CHECK WAS NORMAL. 2 L 7 2 4F A6WE 1998073100786 19980731 00786 NM 1998 7 31 UPS98527245 1 19980724 A 2750 113N23631 BEAM BOEING 757 75724APF 1384969 NM RT TE FLAPS BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 411UP 23851 INSPECTION TYPE-N/A ON WALKAROUND, FOUND RT I/B AFT FLAP JAMMED AND RT I/B BELLCRANK SPROCKET BEAM ASSY BROKEN. FOUND L EFT I/B FLAP BELLCRANK SPROCKET BEAM ASSY BROKEN. REMOVED AND REPLACED LEFT I/B BELLCRANK BEAM ASSY PER M/M 27-51-13, ( P/N 113N2363-1) FLAP SYS NEED OPS CHECK. 2 L 7 2 4F RT A2NM 1998073100787 19980731 00787 EU 1998 7 31 QXEA9801045 1 19980727 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 LIGHTS ON EMERGENCY EXIT AT 9A INOPERATIVE. MAINTENANCE RELAMPED LIGHT ASSEMBLY, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998073100788 19980731 00788 NM 1998 7 31 DHL98707003 1 19980728 A 2782 1U1110 ACTUATOR BOEING 727 72722 1384002 NM NR 1 LE FLAP LEAKING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 707DH 18321 AFTER TAKEOFF WITH GEAR AND FLAPS UP, THE A- SYSTEM QUANTITY DECREASED TO ZERO. CRANKED GEAR DOWN, EXTENDED FLAPS AND LED WITH ALTERNATE SYSTEM. A-SYSTEM SHUT OFF 7 MINUTES. ABNORMAL PROCEDURES COMPLIED WITH. FOUND NR 1 LEADING EDGE FL AP ACTUATOR LEAKING. REMOVED AND REPLACED PER MM 27-81-22. 2 L 7 3 4F A3WE 1998073100789 19980731 00789 NM 1998 7 31 CALA9801356 1 19980728 A 5730 PANEL BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND A 5 AND 10 INCH CRACK ON TOP OF LT WING LEADING EDGE PANEL BETWEEN SLATS NR 3 AND NR 4. REPAIRED IAW S RM 51-20-01 AND 51-70-17. 2 L 7 2 4F RT A2NM 1998073100790 19980731 00790 NM 1998 7 31 CALA9801357 1 19980728 A 5730 114N210620 PANEL BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17104 27294 INSPECTION FOUND A 5 AND 10 INCH CRACK ON TOP OF RT WING LEADING EDGE PANEL BETWEEN SLATS NR 7 AND NR 8. THE PANEL WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A2NM 1998073100791 19980731 00791 NM 1998 7 31 CALA9801358 1 19980728 A 5730 PANEL BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND A 3, 8 AND 2.5 INCH CRACK IN RT WING UPPER SURFACE OF LEADING EDGE COMPOSITE PANEL AT SLAT NR 7, NR 8, STA OSS 421. REPAIR PLIES WERE CUT OUT, SANDED, AND INSTALLED IAW ECRA 5720-01661. A DIP WAS ISSUED TO INSPECT THE REP AIR EVERY SIX DAYS UNTIL PERMANENT REPAIR IS ACCOMPLISHED WITHIN 30 DAYS OR 50 CYCLES. 2 L 7 2 4F RT A2NM 1998073100792 19980731 00792 NM 1998 7 31 CALA9801359 1 19980728 A 5730 PANEL BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17105 27295 INSPECTION FOUND A 9 INCH CRACK IN LT WING UPPER SURFACE OF LEADING EDGE COMPOSITE PANEL AT SLAT NR 3, NR 4 STA OSS 421. REPAIR PLIES WERE CUT OUT AND INSTALLED IAW ECRA 5720-01661. A DIP WAS ISSUED TO INSPECT THE REPAIR EVERY SIX DAYS UN TIL PERMANENT REPAIR IS ACCOMPLISHED WITHIN 30 DAYS OR 50 CYCLES. 2 L 7 2 4F RT A2NM 1998073100793 19980731 00793 WP 1998 7 31 CALA9801360 1 19980728 A 5320 CLIP DOUG DC9 DC932 3022066 WP BS 1109 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A 2 INCH CRACK IN CLIP AT STA 1109, LONGERON 2R. THE CLIP WAS REPLACED IAW SRM 51-60-0. 2 L 7 2 4F A6WE 1998073100794 19980731 00794 NM 1998 7 31 MWEA98818 1 19980726 A 2560 D29982107 GIRT BAR DOUG MD88 MD88 3023688 NM CABIN DOOR SLIDE OUT OF POSITION A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 601ME 49762 THE FORWARD DOOR SLIDE NEEDS TO BE REDONE. MTC REROUTED GIRT BAR CORRECTLY. 2 L 7 2 4F RT A6WE 1998073100795 19980731 00795 WP 1998 7 31 MWEA98819 1 19980727 A 5330 5911424505 SKIN DOUG DC9 DC932 3022066 WP BS 935-965 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND THREE DENTS ON AFT FUSELAGE SKIN FROM FS 935 TO 965 BETWEEN LONGERON 24R TO 25R. MTC FABRICATED AND INSTALLED DOU BLERS. 2 L 7 2 4F A6WE 1998073100796 19980731 00796 WP 1998 7 31 MWEA98820 1 19980727 A 5320 99194021 TRAP PANEL DOUG DC9 DC932 3022066 WP LEFT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CRACK ON LEFT TRAP PANEL UPPER OUTBOARD FLANGE FROM FORWARD EDGE TO JUST PAST THE THIRD BOLT HOLE. MTC TRIMMED TO FOURTH HOLE. 2 L 7 2 4F A6WE 1998073100797 19980731 00797 WP 1998 7 31 MWEA98821 1 19980727 A 5210 59141215 PAN DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CRACK IN UPPER FORWARD CORNER PASSENGER DOOR PAN. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998073100798 19980731 00798 WP 1998 7 31 MWEA98822 1 19980727 A 5400 995815957 ANGLE DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CRACK ON LEFT PYLON LOWER AFT BOX CORNER ANGLE. MTC FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 1998073100799 19980731 00799 WP 1998 7 31 MWEA98823 1 19980727 A 5210 99557523 BEAM DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CRACK ON AFT END OF PASSENGER DOOR NUMBER ONE BEAM. MTC FABRICATED AND INSTALLED DOUBLER AND REPLACED DOOR STOP A SSEMBLY. 2 L 7 2 4F A6WE 1998073100800 19980731 00800 WP 1998 7 31 MWEA98824 1 19980727 A 5313 49122611 LONGERON DOUG DC9 DC932 3022066 WP BS 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON LONGERON 27L AT STATION 218. MTC FABRICATED AND INSTALLED NEW LONGERON SPLICE. 2 L 7 2 4F A6WE 1998073100801 19980731 00801 WP 1998 7 31 RRXA98278 1 19980520 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 DURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND DC-8 LIMITS, AT STA 960. REMOVED DAMAGED FI TTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-1-20D. 2 L 7 4 4F 4A25 1998073100802 19980731 00802 WP 1998 7 31 RRXA98279 1 19980521 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 DURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND DC-8 SRM LIMITS, AT STA 920. REMOVED FITTIN G, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW 53-1-0, PAGE 1. 2 L 7 4 4F 4A25 1998073100803 19980731 00803 WP 1998 7 31 RRXA98280 1 19980521 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 DURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT FITTING CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 940. REMOVED FI TTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-1-0, PAGE 1. 2 L 7 4 4F 4A25 1998073100804 19980731 00804 WP 1998 7 31 RRXA98281 1 19980511 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1480-4500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 DURING A MAINTENANCE VISIT, FOUND LONGERON 24 RIGHT CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 1480 TO 1500. REMOVED L ONGERON 24 RIGHT, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED NEW SECTION OF LONGERON IAW DC-8 SRM 53-2-2, FIGU RE 10. 2 L 7 4 4F 4A25 1998073100805 19980731 00805 WP 1998 7 31 RRXA98282 1 19980516 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 990CF 46068 DURING A MAINTENANCE VISIT, FOUND HORIZONTAL STABILIZER LEADING EDGE RIGHT SIDE WITH EXFOLIATION CORROSION BEYOND DC-8 S RM LIMITS, AT STA XFS 178 TO STA XFS 200. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND IN STALLED REPAIR DOUBLER IAW DC-8 SRM 55-2-1, PAGE 17. 2 L 7 4 4F 4A25 1998073100806 19980731 00806 NM 1998 7 31 VNAA9807011 1 19980727 A 3241 ACM30662 TRANSDUCER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG BRAKE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 424JS 83162 3033 DURING THE TAXI PRIOR TO TAKEOFF, A ANTI-SKID FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MA INTENANCE INSPECTED AND REPLACED THE LEFT HAND INBOARD WHEEL SPEED TRANSDUCER, IN ACCORDANCE WITH DORNIER MAINTENANCE MA NUAL 32-42-11. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998080700001 19980807 00001 WP 1998 8 7 TWAA9810314 1 19980618 A 5312 BULKHD FITTING DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 491SA 45799 STL - THE LOWER END FITTING ON AFT PRESSURE BULKHEAD LT Z34 RIB HAD A .3750 INCH CRACK AT TEE FITTING. REPAIRED PER TWA ARA 15188. CHECK-C 3-12-98 STL. (X) 2 L 7 2 4F A6WE 1998080700011 19980807 00011 SW 1998 8 7 98ZZZX2539 1 19980615 A 6720 212011710001 PITCH LINK 20901170017 BELL 205 205A1 1181414 SW TAIL ROTOR BROKEN A GDMA R AUTOROTATION F FLT CONT AFFECTED HO HOVERING 1 NM 09 66HJ AHN00215 30239 PITCH LINK FAILED WHILE IN HOVER FLIGHT. PILOT EXECUTED HOVERING AUTOROTATION SUCCESSFULLY. TAIL ROTOR ASSY COMPLETE, 90 DEGREE GEARBOX, AND 42 DEGREE GEARBOX WERE REPLACED AS A PRECAUTION, FOR INSPECTION. 1 G 7 1 4U H1SW 1998080700016 19980807 00016 WP 1998 8 7 AALA981029 1 19980526 A 3350 LIGHT GRIMES DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 423AA 49335 DFW - DURING MAINTENANCE CHECK, LEFT HAND OVER WING EMERGENCY LIGHT INOPERATIVE. REPAIRED LOOSE CONTACT IN EMERGENCY EX IT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998080700017 19980807 00017 WP 1998 8 7 AALA981117 1 19980603 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7543A 53025 DFW - DURING OVERNIGHT CHECK, FORWARD COACH CABIN EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998080700018 19980807 00018 EU 1998 8 7 98ZZZX2544 1 19980526 A 5540 D55471001 RUDDER AIRBUS 320 A320214 EU EMPENNAGE DAMAGED A AJLF K NONE O OTHER IN INSP/MAINT 1 SO 23 630AJ 630 AIRCRAFT'S RUDDER TOP END DAMAGED AS IT CAME IN CONTACT WITH CRANE SUPPORT BEAM OF THE HANGAR ROOF. THIS INCIDENT TOOK PLACE WHEN THE AIRCRAFT WAS BEING POSITIONED FOR DOCKING IN THE HANGAR TO REPAIR THE RIGHT HAND ELEVATOR AND HORIZONTAL STABILIZER (REF: MOR 20-10-98). FOLLOWING THE REPAIRS OR REPLACEMENT OF COMPONENTS, THE AIRCRAFT WILL BE RELEASED FOR FURTHER SERVICE. REF: 20-11-98. 2 L 7 2 4F RT A28NM 1998080700019 19980807 00019 CE 1998 8 7 COEA9801875 1 19980507 A 3240 06111800 CYLINDER CESSNA 208 208B 2073701 CE RT MLG BRAKE LEAKING A COEA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 NM 13 875FE 3603 2640 208B0206 WHILE TURNING OUT OF PARKING SPOT TO REPOSITION AIRCRAFT, PILOT REPORTED RT BRAKE PEDAL WENT TO FLOOR AND BRAKING ACTION WENT TO ZERO ON RT SIDE. PILOT SHUT DOWN AIRCRAFT AND SAW THAT RT BRAKE CYLINDER HAD STARTED LEAKING BRAKE FLUID. MAI NTENANCE WAS NOTIFIED. REPLACED BRAKE CYLINDER. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 1 H 7 1 3T A37CE 1998080700020 19980807 00020 WP 1998 8 7 HALA9800182 1 19980624 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP CABIN CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 171AA 46906 TULE - (LOG PAGE NR 0116521). CORROSION ON RT FORWARD LAVATORY FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT FOR FORWARD LAVATORY PER AARD 51-00-00-05. (X) 2 L 7 3 4F A22WE 1998080700021 19980807 00021 NE 1998 8 7 MASA98098 2 19980502 A 7321 5071T98P03 EEC CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE E/E BAY FAILED A MASA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 37208 691 7208 STL/PHL - FLT 5764 - AFTER TAKEOFF, LEFT N1 GAUGE BEGAN FLUCTUATING MINUS 20 PERCENT, CLIMB THRUST AND ITT WENT TO MOMEN TARY RED LINE. CREW DID NOT DECLARE AN EMERGENCY, BUT THE FIRE TRUCKS WERE DISPATCHED BY THE TOWER AS A PRECAUTIONARY M EASURE. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE DEFERRED THE ENGINE SPEED CONTROL SYSTEM PER MEL 76-11-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE LT ENGINE CONTROL AMPLIFIER WAS REMOVED AND REPLACED. (X) 2 L 7 2 4F 4 F RT A21EA E15NE 1998080700023 19980807 00023 NM 1998 8 7 98ZZZX2546 1 19980702 A 2910 B-NUT BOEING 727 7272J0 138407E NM NR 1 ENGINE LOOSE A S84A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 21 284KH 21108 AIRCRAFT DIVERTED INTO KFLL. DUE LOSS OF A-SYSTEM HYDRAULIC FLUID, FOUND B-NUT NR 1 ENGINE MAIN HYDRAULIC LINE LOOSE. T IGHTENED B-NUT, CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASE AIRCRAFT. 2 L 7 3 4F RT A3WE 1998080700024 19980807 00024 EU 1998 8 7 SIMA981511 1 19980531 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 204NE A3794 340B204 APF - FLT 5727 - ON APPROACH AT 4,000 FEET, CARGO SMOKE LIGHT ILLUMINATED. FIRE BOTTLES WERE PULLED. NO EVIDENCE OF FI RE IN CARGO. CONTRACT MAINTENANCE INSPECTED CARGO COMPARTMENT AND ISSUED MEL 26-4. MIA MAINTENANCE. CLOSED MEL. REPL ACED BOTH FIRE BOTTLES AND BOTH CARGO SMOKE DETECTORS. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR: 98ZZZ X2547. (X) 2 L 7 2 4T RT A52EU 1998080700025 19980807 00025 EU 1998 8 7 98ZZZX2547 1 19980531 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 204NE A4418 340B204 APF - FLT 5727 - ON APPROACH AT 4,000 FEET, CARGO SMOKE LIGHT ILLUMINATED. FIRE BOTTLES WERE PULLED. NO EVIDENCE OF FI RE IN CARGO. CONTRACT MAINTENANCE INSPECTED CARGO COMPARTMENT AND ISSUED MEL 26-4. MIA MAINTENANCE. CLOSED MEL. REPL ACED BOTH FIRE BOTTLES AND BOTH CARGO SMOKE DETECTORS. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL SIMA981511 . 2 L 7 2 4T RT A52EU 1998080700026 19980807 00026 EU 1998 8 7 SIMA981632 1 19980612 A 3350 CONNECTOR SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AE 340B313 DFW - FLT 5113 - EMERGENCY FLOOR PROXIMITY ESCAPE PATH SIGNS AT ROWS 9, 11, 12, AND 14 DO NOT ILLUMINATE. INSTALLED CAN NON PLUG AT AFT POWER SUPPLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998080700027 19980807 00027 EU 1998 8 7 SIMA981674 1 19980608 A 3320 BV0330002 SOCKET SAAB SF340 340B 7860101 EU CABIN SHORTED A SIMA F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 SW 21 393AE 340B393 MAF - FLT 3559 - OVERHEAD LAMP ABOVE SEAT 14B BURNED/SHORTED, AND CAUGHT FIRE. FLIGHT ATTENDANT DISCHARGED HAND-HELD HA LON FIRE EXTINGUISHER. MAINTENANCE REMOVED BULB AND OPENED MEL FOR OVERHEAD LIGHT SYSTEM. FERRIED AIRCRAFT TO DFW FOR EXTINGUISHER BOTTLE REPLACEMENT. CLOSURE OF MEL NR 060033 IS PENDING LAMP SOCKET REPLACEMENT. REMOVED AND REPLACED AFT (14B) OVERHEAD FLUORESCENT LAMP SOCKET/HOLDER. OPERATIONAL CHECK GOOD. MEL NR 060033 CLEARED ON 6-17-98. (X) 2 L 7 2 4T RT A52EU 1998080700028 19980807 00028 EU 1998 8 7 SIMA981393 1 19980519 A 3350 3013000 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 538AM 0485 538 IND - EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT THE FOLLOWING LOCATIONS. 61WL. PERFORMED OPERATIONAL CHE CK SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998080700029 19980807 00029 SO 1998 8 7 SIMA981385 1 19980518 A 2611 PU90431R1 SMOKE DETECTOR EMB 145 EMB145LR SO BAGGAGE COMPT FAILED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 602AE 145048 CVG - FLT 4096 - RECEIVED BAGGAGE SMOKE WARNING. CARRIED OUT CHECKLIST ACTIONS. REQUIRED FIRE EXTINGUISHER AGENT DISCH ARGE. REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS. OPS CHECK GOOD IAW 26-15-01. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4T RT T00011AT 1998080700030 19980807 00030 NM 1998 8 7 TWAA9808203 1 19980522 A 2150 68064043 ACM BOEING 757 7572Q8 1384972 NM CABIN FAILED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 709TW 28168 BWI - FLT 176 - DURING APPROACH, LT AIR CYCLE MACHINE MADE A BURNED SMELL IN THE CABIN. REPLACED THE LT AIR CYCLE MACHI NE MFG PN 680640-4-3. OP-15. 5-14-97. NEW. (X) 2 L 7 2 4F RT A2NM 1998080700031 19980807 00031 WP 1998 8 7 TWAA9808101 1 19980520 A 2150 39271411 VALVE DOUG DC9 DC983 3022083 WP RT PACK FAILED A TWAA K NONE O OTHER LD LANDING 1 CE 05 9620D 004567 53591 JFK - FLT 763 - RIGHT AIR CONDITIONER PACK FAILED AFTER TAKEOFF. THIRTY-FIVE MINUTES AFTER TAKEOFF, PACK VALVE OPENED T O 10 PSI. SIX MINUTES LATER, VALVE OPENED COMPLETELY. PACK THEN FAILED ON LANDING. REPLACED AIR PRESSURE REGULATOR VA LVE P/N 293-0033. OP-15. 10-01-97. NEW. (X) 2 L 7 2 4F RT A6WE 1998080700032 19980807 00032 EA 1998 8 7 VTZA98179 1 19980430 A 2170 7536893 COALESCER BAGS CNDAIR CL600 CL6002B19 EA LT/RT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 625BR 7214 IAD/JAX - FLT 6751 - DURING CLIMB, AT 0750 HRS ON 4-30-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LAV SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BOTH FCS COALESER BAGS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998080700033 19980807 00033 WP 1998 8 7 VJ9800055 1 19980325 A 3350 20131A BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN TRIPPED A VJ6A K NONE O OTHER IN INSP/MAINT 1 SO 11 948VV 47559 AFT EMERGENCY LIGHT STUCK ON. RESET THE EMERGENCY HIGH BATTERY PACK. OPS CHECKED GOOD. (X) 2 L 7 2 4F A6WE 1998080700034 19980807 00034 EU 1998 8 7 98ZZZX2548 1 19980428 A 5347 S53375001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION, PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND FORWARD LEFT INBOARD SEAT TRACK FLOORBOARD CLIP HOLES CORRODED BETWEEN FRAMES 13 AND 16. INSTALLED SEAT TRACK PER SRM 51-21-04. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2 H 7 2 4T RT A53EU 1998080700035 19980807 00035 EU 1998 8 7 98ZZZX2549 1 19980428 A 5315 S5367240720201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND CORROSION ON FLOORBEAM 38. INSTALLED FLOORB EAM PER SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2 H 7 2 4T RT A53EU 1998080700036 19980807 00036 EU 1998 8 7 98ZZZX2550 1 19980428 A 5311 S53672406200 FRAME AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND FRAME 36 CORRODED AT FLOOR LEVEL RIGHT SIDE. REPAIRED FRAME 36 IAW ATR 42 SRM 53-61-40, FIGURE 407. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY/GALLEY SPILL. AIRCR AFT TT: 18,688.4 HOURS. TAC: 23,278. 2 H 7 2 4T RT A53EU 1998080700037 19980807 00037 EU 1998 8 7 98ZZZX2551 1 19980428 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RIGHT AFT INBOARD SEAT TRACK CORRODED FO RWARD OF FRAME 35. COMPLETE REPLACMENT OF RT AFT INBOARD SEAT TRACK BY COUNTERSINK HOLES, INSTALLED HILOCKS, AND RIVETS ON AFT SUPPORT BRACKETS IAW ATR 42 SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY, GALLEY SPILL. AIRCRAFT TT : 18,688.4 HOURS. TAC: 23,278. 2 H 7 2 4T RT A53EU 1998080700038 19980807 00038 EU 1998 8 7 98ZZZX2552 1 19980428 A 5315 S5367240620802 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND NUT PLATE HOLES CORRODED ON FLOORBEAM 36. I NSTALLED REPLACEMENT FLOORBEAM 36 IAW ATR 42 SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOUR S. TAC: 23,278. 2 H 7 2 4T RT A53EU 1998080700039 19980807 00039 EU 1998 8 7 98ZZZX2553 1 19980428 A 5242 S5387500001800 DOOR AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND LIGHT CORROSION ON AFT AVIONICS DOOR FLANGES (FWD AND AFT). REMOVED AND REPLACED WITH NEW DOOR IAW ATR 42 SRM 20-21-00. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY, GALLEY SPILL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2 H 7 2 4T RT A53EU 1998080700040 19980807 00040 EU 1998 8 7 98ZZZX2554 1 19980428 A 5347 S53678001214 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LAVATORY WALL SEAT TRACK BETWEEN FRAMES 39 AND 41 CLIP NUT HOLE CORRODED AFT AREA. INSTALLED SERVICEABLE SEAT TRACK BETWEEN FRAMES 39 AND 41 LAVATORY WALL IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE: ENVIRONMENTAL, LAVATORY/GALLEY SPILL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,27 8. 2 H 7 2 4T RT A53EU 1998080700041 19980807 00041 EU 1998 8 7 98ZZZX2555 1 19980428 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LEFT F/A SEAT TRACK CORRODED AT FRAME 39 . INSTALLED NEW LEFT SEAT TRACK PER SRM 51-25-04. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2 H 7 2 4T RT A53EU 1998080700042 19980807 00042 NM 1998 8 7 MBXA9800015 1 19980627 A 3240 CONNECTOR DORNER DO32 DO328100 2996000 NM BRAKE SYSTEM DIRTY A M8XA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 03 336PH 3014 DEN - FLT 7407 - EN ROUTE FROM DEN TO DRO, THE FLIGHT CREW REPORTED THE 'EMERGENCY/PARKING BRAKE ACCUMULATOR' LOW PRESSU RE ANNUNCIATION LIGHT ILLUMINATED IN-FLIGHT. CREW PERFORMED CHECK LIST ITEM IAW FLIGHT STANDARDS MANUAL, HOWEVER, LIGHT ILLUMINATED ONCE AGAIN A SHORT TIME LATER. CREW ELECTED TO RETURN TO DENVER. AIRCRAFT LANDED IN DENVER WITHOUT FURTH ER INCIDENTS. DENVER MAINTENANCE CLEANED CANNON PLUG CONNECTOR ON THE PRESSURE SWITCH. UNABLE TO DUPLICATE DISCREPANCY . AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A45NM 1998080700043 19980807 00043 WP 1998 8 7 TWAA9812301 1 19980727 A 5350 TAIL CONE DOUG DC9 DC982 3022082 WP AFT FUSELAGE DEFORMED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 922TW 48013 DURING C-CHECK, THE TAIL CONE FAILED TO RELEASE DURING ROUTINE CHECK. FOUND THE UPPER SECTION OF THE TAIL CONE WAS DIST ORTED SO THAT THE FOUR ATTACH POINTS DID NOT ALIGN WITH THE ATTACHMENT PINS. WAS NECESSARY TO CUT BACK THE TOP OF THE T AIL CONE, DRAW THE PIECES TOGETHER, AND HOT BOND REPAIR INSIDE AND OUT. THE FRAMES WERE CUT AND FORMED TO THE NEW CONTO UR, AND SPLICES WERE INSTALLED AT THE 4 CUTS. FIBERGLAS REPAIRS PER SRM 51-90-0. FRAME REPAIRS PER ARA 15449. 2 L 7 2 4F A6WE 1998080700044 19980807 00044 WP 1998 8 7 TWAA9812302 1 19980717 A 5311 FORMER DOUG DC9 DC932 3022066 WP BS 1038 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND FORMER CORRODED AT INBD ANGLE STA 1038, BETWEEN S15R AND S17R. CORROSION GROUND TO A DE PTH OF .090. REMOVED CORROSION PER SRM 51-10-3. REPAIRED FORMER 1038 PER ARA 15366A. INSTALLED FORMER 2014-T6 L ANGLE WITH HI-LOCKS. 2 L 7 2 4F A6WE 1998080700045 19980807 00045 WP 1998 8 7 IXXA9800063 1 19980730 A 3610 3F17271502 SENSE LINE DOUG DC8 DC871F 302199D WP NR 3 ENGINE CHAFED A IXXA K NONE O OTHER TO TAKEOFF 1 GL 23 823BX 46064 DURING CLIMB-OUT FROM TOL TO DEN, THE NUMBER THREE ENGINE SHORT CIRCUIT LIGHT AND MASTER FIRE LIGHT ILLUMINATED. A FEW SECONDS LATER, THE FIRE WARNING LIGHT AND BELL CAME ON. THE CREW SHUTDOWN ENGINE AND DISCHARGED ONE FIRE AGENT BOTTLE A ND THE AIRCRAFT RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE HIGH PRESSURE REGULATOR SENSE LINE CHAFFED THROUGH AT THE CLAMP LETTING HOT BLEED AIR VENT ON TO THE FIRE LOOP. MAINTENANCE REPLACED SENSE LINE. THE SYSTEM CHECK WAS GOOD IN ACCORDANCE WITH THE MAINTENANCE MANUAL, AND THE AIRCRAFT WAS RETURNED TO SERV ICE. 2 L 7 4 4F RT 4A25 1998080700046 19980807 00046 NM 1998 8 7 AWXA9800159 1 19980727 A 3350 20121 POWER SUPPLY BOEING 757 757225 1384959 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 915AW 22209 DURING ROUTINE MAINTENANCE CHECK, FOUND AFT SECTION OF EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER POWE R SUPPLY. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998080700047 19980807 00047 NM 1998 8 7 CALA9801361 1 19980728 A 2131 71211997101AA CONTROLLER BOEING 737 737524 1384721 NM E/E COMPT INOPERATIVE A CALA G O2 MASK DEPLOYED O OTHER CR CRUISE 1 SW 09 33637 27540 THE A/C LOST PRESSURE AT FL 370 WHILE EN ROUTE FROM IAH TO MDW. A DESCENT WAS BEGUN AND CONTROL OF THE CABIN WAS REGAIN ED AT FL 240 USING ALT. OXYGEN MASKS WERE DEPLOYED. A/C LANDED AT MDW W/O FURTHER PROBLEM. BOTH CABIN PRESS CONTROLLE RS AND THE CABIN PRESS SELECT PNL WERE REMOVED AND REPLACED. A BITE CHECK WAS NORM IAW MM 21-31-21. MX FOUND OXYGEN MA SKS IN LAVS AND AT SOME SEATS OF ROWS 6, 7, 9, 10, 14, 18, AND 19 DROPPED BUT DID NOT FIRE. OXYGEN GENERATORS WERE REPL ACED AND MASKS WERE STOWED IAW MM 35-22-11 AND 35-22-31. THE INSTALLATION OF OXYGEN GENERATORS AND MASKS WERE INSPECTED AND ALL FOUND SERVICEABLE AND CORRECT IAW MM 35-22. MANUAL MASK ACTUATION TEST WAS PERFORMED IAW MM 35-22 AND NO PROBL 2 L 7 2 4F RT A16WE 1998080700048 19980807 00048 WP 1998 8 7 CALA9801362 1 19980729 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 756-935 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND AFT CARGO FLOOR PANEL AT STA 756-935 CRACKED AND WORN IN SEVERAL PLACES. A NEW PANEL WAS FABRICATED AN D INSTALLED IAW SRM 53-21-0. 2 L 7 2 4F A6WE 1998080700049 19980807 00049 WP 1998 8 7 CALA9801363 1 19980729 A 5720 ANGLE DOUG DC9 DC932 3022066 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND A .5 INCH CRACK IN ANGLE TO RT WING INBOARD BUTE DOOR STIFFENER ATTACHMENT POINT. AN ANGLE WAS FABRICA TED AND INSTALLED IAW SRM 51-10-2, FIGURE 1. 2 L 7 2 4F A6WE 1998080700050 19980807 00050 WP 1998 8 7 CALA9801364 1 19980729 A 5730 PANEL DOUG DC9 DC932 3022066 WP RT WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND RT WING LEADING EDGE PANEL NR 1248 GOUGED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-01, FIGURE 3, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998080700051 19980807 00051 WP 1998 8 7 CALA9801365 1 19980729 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 935 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND FLOOR PANEL SPLICE PLATE IN AFT CARGO PIT AT STA 935 CORRODED. A NEW FLOOR PANEL SPLICE PLATE WAS FABR ICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998080700052 19980807 00052 NM 1998 8 7 CALA9801366 1 19980729 A 5730 114N210619 PANEL BOEING 757 757224 1384958 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND A 10 CRACK IN LT WING FIXED LEADING EDGE PANEL AFT OF NR 4 LEADING EDGE SLAT AND A 6.75 INCH CRACK WAS FOUND AFT OF NR 3 LEADING EDGE SLAT. THE AREAS WERE REPAIRED IAW ECRA 5720-01666. A DIP WAS ISSUED IAW ECRA 5720-01666 . 2 L 7 2 4F RT A2NM 1998080700053 19980807 00053 NM 1998 8 7 CALA9801367 1 19980729 A 5730 114N210620 PANEL BOEING 757 757224 1384958 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 21108 27298 INSPECTION FOUND THREE CRACKS AFT OF NR 8 LEADING EDGE SLAT AND THREE CRACKS AFT OF NR 7 LEADING EDGE SLAT IN RT WING FI XED LEADING EDGE. THE CRACKS WERE 2 TO 12.5 INCHES LONG. THE AREAS WERE REPAIRED AND A DIP WAS ISSUED IAW ECRA 5720-01 667. 2 L 7 2 4F RT A2NM 1998080700054 19980807 00054 WP 1998 8 7 CALA9801368 1 19980729 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 980 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND CORROSION AROUND FLOORBEAM NUT PLATES AT RT AFT LAV, STA 980, APPROXIMATELY 18 INCHES FROM RT SIDE OF F USELAGE. THE FLOORBEAM WAS REPAIRED IAW SRM 53-05, FIGURE 20A. 2 L 7 2 4F A6WE 1998080700056 19980807 00056 EA 1998 8 7 COMA9860199 1 19980728 A 5210 1078461 SPRING CNDAIR CL600 CL6002B19 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 916CA 7014 CABIN DOOR OUTER HANDLE WARNING MESSAGE DURING FLIGHT. REPLACED HANDLE LATCH SPRING. 2 L 7 2 4F RT A21EA 1998080700057 19980807 00057 EA 1998 8 7 COMA9860200 1 19980728 A 3350 64643 LAMP CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 938CA 7046 FIRST SECTION OF EMERGENCY FLOOR LIGHTING STRIP IS INOPERABLE. REPLACED LIGHTING STRIP. 2 L 7 2 4F RT A21EA 1998080700058 19980807 00058 EA 1998 8 7 COA9860201 1 19980724 A 5320 601R9720419 HEAT SHIELD CNDAIR CL600 CL6002B19 EA APU COMPT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 DURING C-CHECK, FOUND THE APU HEAT SHIELD TO BE CRACKED. REMOVED AND REPLACED WITH SERVICEABLE UNIT. 2 L 7 2 4F RT A21EA 1998080700059 19980807 00059 EA 1998 8 7 COMA9860202 1 19980725 A 4980 1079900004 CLAMP CNDAIR CL600 CL6002B19 EA APU COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 DURING C-CHECK, FOUND APU EXHAUST CLAMP TO BE BROKEN. REPLACED EXHAUST CLAMP. 2 L 7 2 4F RT A21EA 1998080700060 19980807 00060 EA 1998 8 7 COMA9860203 1 19980725 A 4980 1097500000 DUCT CNDAIR CL600 CL6002B19 EA APU COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 DURING C-CHECK, FOUND APU EXHAUST DUCT ASSY TO HAVE BROKEN TABS. REPLACED APU EXHAUST DUCT ASSEMBLY. 2 L 7 2 4F RT A21EA 1998080700061 19980807 00061 EA 1998 8 7 COMA9860204 1 19980725 A 2750 601R93106503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP FLEXSHAFT TO BE UNSERVICEABLE DUE TO STRAND SEPARATION. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998080700062 19980807 00062 EA 1998 8 7 COMA9860205 1 19980725 A 2750 601R93106108 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP STRIPPED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 7158 DURING C CHECK, FOUND RIGHT INBOARD FLAP FLEXSHAFT TO HAVE STRIPPED CASING THREADS. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998080700063 19980807 00063 EA 1998 8 7 COMA9860206 1 19980725 A 7830 1217545 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TR UNIT SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 978CA 3851 7158 DURING C-CHECK, FOUND RIGHT THRUST REVERSER FLEXSHAFT AT 5 O'CLOCK POSITION TO BE UNSERVICEABLE. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998080700064 19980807 00064 EA 1998 8 7 COMA9860207 1 19980729 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 912CA 7011 FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED STRIP LIGHT. 2 L 7 2 4F RT A21EA 1998080700065 19980807 00065 EA 1998 8 7 COMA9860208 1 19980729 A 3350 364911 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 948CA 7079 SEVERAL SECTIONS OF EMERGENCY FLOOR LIGHTING ARE INOPERABLE. REPLACED TWO SECTIONS OF FLOOR TRACK LIGHTING. 2 L 7 2 4F RT A21EA 1998080700066 19980807 00066 EU 1998 8 7 QXEA9801040 1 19980725 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 GEG - EMERGENCY EXIT LIGHT OUT AT 9A. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998080700067 19980807 00067 WP 1998 8 7 ABXA9800641 1 19980714 A 5312 5910130275 BULKHEAD WEB DOUG DOUG DC9 DC915 3022036 WP BS 817 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD WEB CORRODED BETWEEN LONGERON 26L TO 30L. REPAIRED I AW ABX REA D953-24142MR. 2 L 7 2 4F A6WE 1998080700068 19980807 00068 WP 1998 8 7 ABXA9800642 1 19980720 A 5312 8917633507 BULKHEAD BRACKET DOUG DOUG DC9 DC915 3022036 WP BS 817 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH 'C' INSPECTION, FOUND THE AFT FACE OF THE AFT PRESSURE BULKHEAD HAD A CRACKED BRACKET AT LOWER LEFT CORNER OF DOOR JAMB. REPLACED BRACKET IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998080700069 19980807 00069 WP 1998 8 7 ABXA9800643 1 19980720 A 5315 99581883 FLOORBEAM DOUG DOUG DC9 DC915 3022036 WP BS 801 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND A FLOORBEAM CORRODED ALONG LOWER FLANGE AT FS801 AND LBL44. REPAIRED FLOORBEAM IAW ABX REA D953-24225MR. 2 L 7 2 4F A6WE 1998080700070 19980807 00070 WP 1998 8 7 ABXA9800644 1 19980709 A 5711 59113022 SPAR DOUG DOUG DC9 DC915 3022036 WP WS 410-460 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND THE RIGHT WING FORWARD UPPER SPAR CAP CORRODED FROM XFS 410 TO 406. REPAIRED R IGHT WING FRONT SPAR CAP IAW ABX REA D957-24091MR. 2 L 7 2 4F A6WE 1998080700071 19980807 00071 WP 1998 8 7 ABXA9800645 1 19980722 A 5311 99155902 FRAME DOUG DOUG DC9 DC915 3022036 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND FUSELAGE FRAME 544 RIGHT CRACKED AT TRANSVERSE FLOORBEAM. REPLACED FUSELAGE FR AME IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998080700072 19980807 00072 WP 1998 8 7 ABXA9800646 1 19980709 A 5312 59174637 BULKHEAD JAMB DOUG DOUG DC9 DC915 3022036 WP BS 817 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB UPPER RIGHT CORNER CRACKED. REPAIRED IAW A BX REA D953-24119. 2 L 7 2 4F A6WE 1998080700073 19980807 00073 WP 1998 8 7 ABXA9800647 1 19980714 A 5511 5918000501 SPAR DOUG DOUG DC9 DC915 3022036 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER UPPER REAR SPAR CORRODED AT XE 147. REPLACED SP AR SECTION IAW DC-9 SRM CHAPTER 55-02. 2 L 7 2 4F A6WE 1998080700074 19980807 00074 WP 1998 8 7 ABXA9800648 1 19980715 A 5711 5911306507 SPAR DOUG DOUG DC9 DC915 3022036 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND THE LEFT WING UPPER FRONT SPAR CRACKED BETWEEN TWO SCREW HOLES 10 OUTBOARD OF X CW 58. REPAIRED CRACK IAW ABX REA D957-24108MR. 2 L 7 2 4F A6WE 1998080700075 19980807 00075 WP 1998 8 7 ABXA9800649 1 19980717 A 5320 5956879501 WEB DOUG DOUG DC9 DC915 3022036 WP BS 206 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND A WEB CRACKED BETWEEN LONGERON 8L AND 9L AT FS206. REPAIRED WEB IAW ABX REA D9 53-24104. 2 L 7 2 4F A6WE 1998080700076 19980807 00076 WP 1998 8 7 ABXA9800650 1 19980715 A 5711 5911306508 SPAR DOUG DOUG DC9 DC915 3022036 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 927AX 45717 WHILE COMPLYING WITH C INSPECTION, FOUND A CRACK IN THE RIGHT UPPER SPAR TEE CAP AT XCW 58. REPAIRED CRACK IAW ABX REA D957-24102MR. 2 L 7 2 4F A6WE 1998080700077 19980807 00077 WP 1998 8 7 MWEA98825 1 19980729 A 5320 39146541 FITTING DOUG DC9 DC932 3022066 WP BS 990 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CRACK ON END FITTING AT LONGERON 23L AT STATION 990. MX FABRICATED AND INSTALLED NEW END FITTING. 2 L 7 2 4F A6WE 1998080700078 19980807 00078 WP 1998 8 7 MWEA98826 1 19980729 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 908 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON AFT CARGO COMPARTMENT FRAME SPLICE AT FS 908 UNDER NUT PLATE AT LONGERON 28L. MX FABRICATED AND INST ALLED NEW SUPPORT SPLICE. 2 L 7 2 4F A6WE 1998080700079 19980807 00079 WP 1998 8 7 MWEA98827 1 19980729 A 5320 3913291 SPLICE DOUG DC9 DC932 3022066 WP BS 837 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND AFT CARGO COMPARTMENT LONGERON SPLICE AT 28L AND FS 837 CORRODED AND CRACKED ON AFT END. MX FABRICATED AND INSTAL LED LONGERON SPLICE. 2 L 7 2 4F A6WE 1998080700080 19980807 00080 NM 1998 8 7 DL72W981557 1 19980723 A 5330 SKIN BOEING 727 727247 138408F NM BS 550 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 FUSELAGE SKIN FS 540-560 L 0, REPAIR FOR SKIN CORROSION CUTOUTS, TWO AREAS OF CORROSION WERE FOUND IN THE FUSELAGE BELLY SKIN AT APPROX BL 0 BETWEEN FS 540 AND 560. THE CORROSION WAS CUT OUT OF THE SKIN WITH A 7.5 BY 2.12 CUTOUT AND A 2 .25 BY 2 CUTOUT. THE CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM EXTERNAL DOUBLER AND TRIPLER REPAIR PER ER/A 365224-1 4, REV B. 2 L 7 3 4F A3WE 1998080700081 19980807 00081 NM 1998 8 7 DL72W981561 1 19980727 A 3350 RPS1 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 291WA 22109 FOUND ROWS 10-19 EMERGENCY ESCAPE PATH LIGHTING INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998080700082 19980807 00082 NM 1998 8 7 DL72S981562 1 19980728 A 3350 6104789 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 525DA 21585 FWD SLIDES EMERGENCY LIGHTS INOP. REPLACED BATTERY. OPS GOOD. 2 L 7 3 4F A3WE 1998080700083 19980807 00083 NM 1998 8 7 DLM88981564 1 19980728 A 3350 61020 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 925DL 49712 EMERGENCY FLASHLIGHT AT AFT ATTENDANTS JUMPSEAT BATTERY LOW. REPLACED FLASHLIGHT. 2 L 7 2 4F RT A6WE 1998080700084 19980807 00084 NM 1998 8 7 DL73K981566 1 19980729 A 5230 DOOR BOEING 737 737232 1384475 NM CARGO COMPT NOT LATCHED A DALA K NONE J WARNING INDICATION LD LANDING 1 SO 27 308DL 23080 FWD CARGO DOOR LIGHT ILLUMINATE UPON TOUCH DOWN. FOUND DOOR OPEN, CHECKED DOOR LATCHES AND ALL WARNING SYS ALL CKS NML. 2 L 7 2 4F RT A16WE 1998080700085 19980807 00085 NM 1998 8 7 DL73K981567 1 19980728 A 3350 BATTERY BPS73 BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 315DL 1735 23087 FOUND LAST THREE LEFT SIDE AISLE EMERGENCY LIGHTS INOP. FOUND BATTERY BAD FOR PWR SUPPLY. REPLACED PWR SUPPLY, AND NEW BATTERY. 2 L 7 2 4F RT A16WE 1998080700086 19980807 00086 NM 1998 8 7 DL757981568 1 19980728 A 3350 333780100 PWR SUPPLY BOEING 757 757232 1384965 NM CARGO COMPT INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 680DA 26956 ON L/O, FOUND EMERGENCY LIGHTS AT 4C, 5C AND C-2 CARGO DOOR INOP. REPLACED TEE-OFF HARNESS ON 4C AND LAMP ASSEMBLY ON 5 C OPS CHECK GOOD. REPLACED BATTERY PACK AND CHARGER (M736). ALL EMERGENCY LIGHTS CHECK LIGHTS CHECK GOOD IAW MM. 2 L 7 2 4F RT A2NM 1998080700087 19980807 00087 NM 1998 8 7 DL757981569 1 19980728 A 3350 337101963 BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 680DA 26956 ON LAYOVER, FOUND EMERGENCY LIGHTS AT 4C, 5C AND C-2 CARGO DOOR INOP. REPLACED TEE-OFF HARNESS ON 4C AND LAMP ASSEMBLY ON 5C OPS CHECK GOOD. REPLACED BATTERY PACK AND CHARGER (M736). ALL EMERGENCY LIGHTS CHECK GOOD IAW MM. 2 L 7 2 4F RT A2NM 1998080700088 19980807 00088 NM 1998 8 7 DL72S981570 1 19980702 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 DURING SHOP VISIT, THE NR 3 MIDFLAP, SN DL15, WAS FOUND WITH A CRACKED REAR CHORD ANGLE. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998080700089 19980807 00089 NM 1998 8 7 DL72S981571 1 19980702 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 THE MIDFLAP REAR CHORD ANGLE WAS FOUND CRACKED 37 AND 31 FROM IB END DURING SHOP VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998080700090 19980807 00090 NM 1998 8 7 DL72S981572 1 19980702 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 DURING SHOP VISIT, THE REAR CHORD ANGLE WAS FOUND CRACKED 17 AND 22 FROM IB END OGF FLAP. THE ANGLE WAS REPAIRED PER 72 7MM 57-52-0 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998080700091 19980807 00091 NM 1998 8 7 DL72S981573 1 19980702 A 5753 SKIN BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 DURING SHOP VISIT, THE COVE SKIN WAS FOUND CRACKED 31 FROM IB END OF FLAP. THE SKIN WAS REPAIRED PER 727 MM 57-52-0, FI G 809, BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FILLER. 2 L 7 3 4F A3WE 1998080700092 19980807 00092 NM 1998 8 7 DL72S981574 1 19980729 A 2910 6517844144 LINE BOEING 727 727232 1384082 NM A-HYD SYST FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 416DA 21258 20 MIN AFTER TAKEOFF FROM ABQ, HAD TOTAL LOSS OF A SYSTEM HYDRAULICS. C/W POM PROCEDURES. DIVERTED TO DFW. REPLACED BROKEN LINE TO A SYSTEM HYDRAULIC MODULE. REPLACED NR 1 ENGINE DRIVEN HYD PUMP. PRESSURE AND LEAK CHECK OK. 2 L 7 3 4F A3WE 1998080700093 19980807 00093 WP 1998 8 7 DLL14981575 1 19980726 A 5240 7424283 CABLE LKHEED 1011 1011385115 5265015 WP L3 DOOR BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 741DA 193C1245 L-3 DOOR TRACK LOCK PIN MECHANISM CABLE BROKEN UNABLE TO ACCOPMPLISH EMERGENCY OPS CHECK INSIDE AND OUTSIDE HANDLES. RE PLACED CABLE. 2 L 7 3 4F A23WE 1998080700094 19980807 00094 NM 1998 8 7 DL72S981577 1 19980722 A 5312 BULKHEAD ANGLE BOEING 727 727232 1384082 NM BS 740 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 FWD B/B STA 740 BLKH LWR ANGLE/CORRODED LOC BETWEEN STA 27R AND 28R. NOTE, FOUND DURING OK TO INST STG 27R REPAIR N/R 1 349. BEGAN REMOVING ANGLE, CONT REMOVING ANGLE. REMOVED ANGLE BEGAN INSTALLATION OF NEW ANGLE. DRILLED UP NEW ANGLE. DRILLED UP ANGLE DOUBLER PER M/M 53-11-0, FIG 826. OK TO INSTALL. BEGAN INSTALLATION OF ANGLE. COMPLETED INST OF ANG LE. 2 L 7 3 4F A3WE 1998080700095 19980807 00095 NM 1998 8 7 DL72S981578 1 19980729 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 NR 5 SLAT ANGLE CRACKED AT O/B SIDE OF ACTUATOR ATTACH RIB. REMOVED PANELS 6501, 6573 AND 6502 FOR ACCESS. REPAIRED PE R MM 57-54-0, FIG 804. INSTALLED PANELS 6501, 6573 AND 6502. 2 L 7 3 4F A3WE 1998080700096 19980807 00096 NM 1998 8 7 DL72S981579 1 19980729 A 5754 RIB BOEING 727 727232 1384082 NM NR 7 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 NR 7 SLAT O/B ACTUATOR ATTACH RIB HAS BEEN STOP DRILLED TWICE INDICATING THAT CRACK HAS CONTINUED TO GROW. REMOVED ACCE SS PANELS TO RIB. FABRICATED DOUBLER. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER MM 57-54-0 FIG 804. REPAIR OK PER M/M. OK TO CLOSE SLAT PANEL. CLOSED SLAT ACCESS PANELS. 2 L 7 3 4F A3WE 1998080700097 19980807 00097 WP 1998 8 7 DLL10981580 1 19980729 A 2520 251044006 SPRING LKHEED 1011 10113851 5265010 WP CABIN SEAT BROKEN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 729DA 193C1180 CENTER DOUBLE STEW SEAT AT L2/R2 CROSSOVER SEAT BOTTOM WON'T AUTO RETRACT. FOUND RT SPRING BROKE REPLACED SAME CKS OK R EF IPC 25-21-09 FIG 2 PG 0 ITEM 210. 2 L 7 3 4F A23WE 1998080700101 19980807 00101 SW 1998 8 7 CA980407005 1 19980324 A 2497 WIRE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313 01514 WP WS 81 FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 25559 P54214 (CAN) NR 4 BUS WIRES FOUND ARCED AND SHORTED IN LT LEADING EDGE WING JUST FWD OF OUTBOARD SIDE OF BATTERY AT WS 81.17. W IRE NR'S 122A4, 122B4, 123A4, AND 123B4. A/C HAD BEEN PREVIOUSLY INVOLVED IN AN ACCIDENT. WHILE DOING SOME SHEET META L REPAIRS, A TECH NOTED THAT ONE OF THE WIRES HAD NO INSULATION AND A HOLE HAD BEEN ARCED INTO BLEED AIR DUCT. ONE OF T HE WIRES HAD THE INSULATION CHAFED OFF WHICH CONTACTED DUCT. THIS LEAD TO DAMAGE TO OTHER WIRES AS BLEED AIR LEAKED ON WIRE BUNDLE AND OVERHEATING. THIS IS APPARENTLY SECOND TIME OPERATOR HAS SEEN WIRES BURNED IN THIS AREA. SEE SB 24-00- 2, AS WELL AS PHASE INSP PROGRAM LTR CHECK PROGRAM. 2 L 7 2 4T 4 T RT A8SW E4WE 1998080700103 19980807 00103 NE 1998 8 7 CA980407011 2 19980214 A 7250 TURBINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE SEIZED W K NONE O OTHER IN INSP/MAINT 1 CA 22212 1464 120544 (CAN) ALTHOUGH PROPELLER AND FRONT END OF THE ENGINE TURNED NORMALLY BY HAND, WHEN A START WAS ATTEMPTED, THE ENGINE WOU LD NOT ROTATE. THE TURBINE SECTION WAS SEIZED. PWC TECH REP BORESCOPED THE ENGINE AND THERE WAS NO VISIBLE ANOMALLY. T HERE WAS A SLIGHT RUB HEARD WHEN THE ENGINE WAS MANUALLY ROTATED. THE ENGINE WAS REMOVED AS A PRECAUTIONARY PROCEDURE A ND SENT TO PWC FOR INVESTIGATION. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700107 19980807 00107 EU 1998 8 7 CA980407017 1 19980302 A 2910 T2C50060500 HOSE BRAERO 748 HS7482A 4231001 EU HYDRAULIC SYS LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) AFTER TAKEOFF, CREW OBSERVED LOW HYDRAULIC FLUID PRESSURE CAUTION LIGHT. A/C RETURNED AND LANDED WITHOUT INCIDENT . HP HYDRAULIC HOSE CHAFED AT BULKHEAD FROM FILTER. REPLACED. 2 L 7 2 3T A24EU 1998080700112 19980807 00112 NE 1998 8 7 CA980415002 2 19980402 A 7320 7863916 HMU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE MALFUNCTIONED W O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 2524 120658 (CAN) AFTER TAKEOFF, NR 1 ENGINE HAD A 20 PERCENT TORQUE ROLLBACK. POWER LEVER WAS ADVANCED TO RESTORE POWER. AFTER CR UISE ESTABLISHED, THERE WAS AN ABRUPT UNCOMMANDED INCREASE IN TORQUE. AFTER NORMAL ARRIVAL, THE HYDRO MECHANICAL UNIT, THE FUEL PUMP WERE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700113 19980807 00113 EA 1998 8 7 CA980415003 1 19980306 A 2820 MS2452433 SWITCH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE FUEL SYSTEM FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 123133 (CAN) AFTER TAKEOFF, FUEL WOULD NOT TRANSFER FROM TANK 1 TO TANK 2. FUEL TRANSFER SWITCH FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700114 19980807 00114 NM 1998 8 7 CA980415004 1 19980406 A 2422 DH103024600CSI INVERTER PHOENIX DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AC SYSTEM FAILED W K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 3726 AA2020S8 120833 (CAN) PRIMARY INVERTER FAIL CAUTION LIGHT ON, ACCOMPANIED BY ELECTRICAL SMOKE. CIRCUIT BREAKER F8/115VAC BUS TIE TRIPPE D. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700115 19980807 00115 EU 1998 8 7 CA980415005 1 19980402 A 3230 UPLOCK AIRBUS 320 A320211 3930320 EU MLG WARNING W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) UNSAFE LANDING INDICATION. A/C RETURNED TO BASE. MAINTENANCE CHECK REVEALED LANDING UPLOCK HOUSING FILLED WITH GREASE. UPLOCK CLEANED AND LANDING RETRACTION TESTS CARRIED OUT, SERVICEABLE. 2 L 7 2 4F RT A28NM 1998080700117 19980807 00117 NM 1998 8 7 CA980415007 1 19980413 A 3230 037280375 BEARING 654462514 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE MLG SEPARATED W K NONE J WARNING INDICATION AP APPROACH 1 CA 47589 19994 4721 702735 (CAN) ON APPROACH, TWO SELECTIONS WERE MADE IN ORDER TO INDICATE NOSE GEAR DOWN AND LOCKED. DOWNLOCK ACTUATOR LOWER BEA RING SEPARATED FROM ACTUATOR HOUSING. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998080700118 19980807 00118 NM 1998 8 7 CA980415009 1 19980413 A 8012 1G38616927 SWITCH PARKERHANFIN 2730426 BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE STARTER FAILED W A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CA 43023 1140 2019 708827B (CAN) AIRCRAFT RETURNED TO RAMP DUE TO STARTER VALVE LIGHT ON. VALVE REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998080700125 19980807 00125 EU 1998 8 7 CA980415018 1 19980408 A 8200 SP90014 SEAL BRAERO 748 HS7482B 1500248 EU RROYCE DART DART5342 EU WATER INJECTOR LEAKING W E D ENGINE SHUTDOWN RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 19068 (CAN) LEAK OCCURRED WHEN WATER METHANOL PUMPS TURNED ON PRIOR TO DEPARTURE. A/C INFORMED OF LEAK WHILE HOLDING SHORT. E NGINE SHUTDOWN AND A/C TOWED. SEAL LEAKING AT FIREWALL DISCONNECT SUPPLY LINE. SEAL REPLACED. 2 L 7 2 3T 4 T A24EU A196 1998080700131 19980807 00131 NM 1998 8 7 CA980416004 1 19980330 A 7997 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE OIL PRESSURE SYS FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 120542 (CAN) CREW REPORTED LEFT OIL PRESSURE WOULD OCCASIONALLY DROP OFF OUT OF GREEN, WITH NO ASSOCIATED OIL LOW PRESSURE LIGH T. SOMETIMES DURING START AND SOMETIMES IN CRUISE. NUMEROUS ENGINE COMPONENTS WERE REPLACED WITH NO SUCCESS. FINALLY, LEFT OIL PRESSURE SYSTEM WIRING REPLACED FROM ENGINE FIREWALL TO COCKPIT INDICATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700132 19980807 00132 NM 1998 8 7 CA980416006 1 19980404 A 3233 DSC252B40124 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG RUPTURED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA 120795 (CAN) AFTER TAKEOFF, THE GEAR DID NOT RETRACT AND NR 2 HYDRAULIC QUANTITY WENT TO ZERO. HYDRAULIC LINE AT NOSE DRAG STR UT ACTUATOR FOUND RUPTURED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700137 19980807 00137 NE 1998 8 7 CA980416011 2 19980325 A 7320 87600520001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA TM120851 (CAN) CONDITION LEVER CABLE TO RIGHT HAND ENGINE FOUND WITH BROKEN STRANDS. CABLE WORN ALONG THE PART THAT CROSSES THE ENGINE FIRE WALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700141 19980807 00141 1998 8 7 CA980417004 4 19980328 A 3431 LOCALIZER BOEING 747 747238B 1384828 NM PWA JT9 JT9D7F 52054 NE COCKPIT VOR MALFUNCTIONED W K NONE O OTHER CR CRUISE 1 CA P685912 (CAN) ON ILS APPROACH, CAPTAIN'S GLIDE SLOPE SHOWED FULL SCALE HIGH. ON PASSING NDB/BEACON AT WHAT SHOULD HAVE BEEN FL 230, AIRCRAFT WAS BELOW GLIDE SLOPE, FIRST OFFICER'S INDICATOR SHOWED FULL SCALE BELOW GLIDE SLOPE. CORRECTION MADE AND A/C LANDED. FOUND PIN NR 52 BROKEN AND PIN PUSHED BACK 24R ON CONNECTOR D2012P. NEW VOR/LOCALIZER INSTALLED AND NEW R OLL COMPUTER INSTALLED. SERVICEABLE. 2 L 7 4 4F 4 F A20WE E20EA 1998080700142 19980807 00142 EU 1998 8 7 CA980417005 1 19980402 A 2750 CONTROL UNIT AIRBUS 320 A320211 3930320 EU FLAP/SLAT SYS FAILED W K NONE F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA (CAN) FLAPS STOPPED FROM ZERO AND 1 UNIT. FLAP CONTROL COMPUTER RESET, CLEARED WARNING, PRESSURIZED HYDRAULIC SYSTEMS, CYCLED FLAPS, AND SLATS, OPERATION NORMAL. 2 L 7 2 4F RT A28NM 1998080700143 19980807 00143 EU 1998 8 7 CA980417006 1 19980402 A 2133 OUTFLOW VALVE AIRBUS 320 A320211 3930320 EU CABIN PRESS SYS FAILED W B D EMER. DESCENT RETURN TO BLOCK O OTHER CR CRUISE 1 CA (CAN) AFTER TAKEOFF, A/C OVERPRESSURIZED DUE TO FAULTY NR SYSTEM AND NR SYSTEM DID NOT TAKE CONTROL. ALSO, DIFFICULTY ENCOUNTERED WITH MANUAL CONTROL. CLIMB-OUT OF FLIGHT LEVEL 320 LOST CONTROL OF CABIN, FIRST DESCENDED, THEN FULL CLIMB AT 3,700 FEET PER MINUTE, CONTROL REGAINED, OK IN MANUAL. A/C RETURNED TO DEPARTURE TERMINAL. MAINTENANCE ACTION INVO LVED CHANGING OUT FLOW VALVE ASSEMBLY AND OPERATIONALLY CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998080700144 19980807 00144 EU 1998 8 7 CA980417007 1 19980405 A 3230 SENSOR AIRBUS 320 A320211 3930320 EU NLG FAILED W K NONE J WARNING INDICATION AP APPROACH 1 CA (CAN) TWO ATTEMPTS WERE MADE BEFORE ALL THREE LANDING GEAR EXTENDED. CHANGED SENSOR 37G NOSE GEAR DOOR OPEN, RETRACTION S CARRIED OUT, CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998080700145 19980807 00145 EU 1998 8 7 CA980417008 1 19980405 A 2750 CONTROL UNIT AIRBUS 320 A320211 3930320 EU TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) FLAPS LOCKED OUT DURING EXTENSION ON APPROACH. SLAT/FLAP CONTROL COMPUTER RESET CARRIED OUT AND SYSTEM CHECKED N ORMAL. 2 L 7 2 4F RT A28NM 1998080700146 19980807 00146 EA 1998 8 7 CA980417009 1 19980405 A 2150 LOCKWIRE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COOLING VALVE BROKEN W A UNSCHED LANDING O OTHER TO TAKEOFF 1 CA 4496 807389 (CAN) UNABLE TO PRESSURIZE AFTER TAKEOFF. FLIGHT RETURNED. INSPECTION FOUND OUTBOARD COOLING VALVE LOCKWIRE BROKEN, RES ECURED INBOARD AND OUTBOARD VALVE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998080700147 19980807 00147 EA 1998 8 7 CA980417010 1 19980403 A 2611 DETECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE CARGO BAY MALFUNCTIONED W F ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 CA 6048 807295 (CAN) AURAL RED WARNING CARGO SMOKE AFTER TAKEOFF. ON APPROACH, WARNING REAPPEARED. NORMAL AND STANDBY CARGO BOTTLES D ISCHARGED. SMOKE DETECTORS AND RELAY K11HL REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1998080700148 19980807 00148 NM 1998 8 7 CA980417011 1 19980403 A 3244 32600151 TREAD BOEING 767 767333 NM PWA 4060 PW4060 52119 NE NR 3 TIRE SEPARATED W K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 CA P724736 (CAN) NR 3 TIRE TREAD THROWN DURING TAKEOFF. DAMAGE TO NR 7 SPOILER PANEL, BODY FAIRING, AND WING PANEL. PARTS REPLACED . 2 L 7 2 4F 4 F RT A1NM E24NE 1998080700149 19980807 00149 NM 1998 8 7 CA980417012 1 19980401 A 2120 DUCT BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE CARGO BAY BLOWN W K NONE O OTHER AP APPROACH 1 CA P709698 (CAN) AFTER TAKEOFF, ENGINE INDICATION AND CREW ALERTING SYSTEM MESSAGE, BODY DUCT LEAK WITH LOSS OF PRESSURIZATION AT A BOUT 6,000 FEET. QUICK REF. HAND BOOK DRILL ACCOMPLISHED AND A/C RETURNED. FOUND DUCT IN C2 CARGO TO WHEEL WELL AREA B LOWN. NEW DUCT INSTALLED AND LEAK CHECK CARRIED OUT. 2 L 7 2 4F 4 F RT A1NM E3NE 1998080700150 19980807 00150 NE 1998 8 7 CA980417013 2 19980401 A 7261 LINE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE ENGINE OIL CHAFED W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 731532 (CAN) ON CLIMBOUT, NR 2 ENGINE OIL QUANTITY NOTICED DECREASING. PRESSURE AND TEMPERATURE NORMAL. JUST AFTER QUANTITY W ENT TO ZERO, OIL PRESSURE STARTED TO DROP. ENGINE SHUT DOWN. AIRCRAFT GROUND RUN AND FOUND OIL PRESSURE LINE TO NR 5 B EARING CHAFED. LINE REPLACED AND GROUND CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A28NM E29NE 1998080700151 19980807 00151 WP 1998 8 7 CA980417014 1 19980327 A 7430 792081 SWITCH DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE IGNITION SYSTEM FAILED W C F ABORTED TAKEOFF ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657244D (CAN) DURING TAXIING OUT FOR TAKEOFF, SMOKE AND FIRE OBSERVED COMING FROM OVERHEAD ELECTRICAL PANEL IN COCKPIT. EMERGEN CY EVACUATION DRILL CARRIED OUT AND PORTABLE FIRE EXTINGUISHER DISCHARGED INTO FIRE AREA AND FIRE EXTINGUISHED. MAINTEN ANCE INVESTIGATION REVEALED WIRING BURNT IN VICINITY OF THE ENGINE IGNITION ELECTRICAL SWITCH WHICH HAD FAILED INTERNALL Y. WIRING AND SWITCH REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1998080700152 19980807 00152 EU 1998 8 7 CA980417015 1 19980330 A 3233 ACTUATOR AIRBUS A340 A340313 EU NLG INOPERATIVE W A UNSCHED LANDING O OTHER TO TAKEOFF 1 CA (CAN) LOUD BANGING NOISE HEARD FROM NOSE AREA DURING TAKEOFF. THIRD TIME REPEAT. A/C RETURNED TO BASE. MAINTENANCE RE PLACED NOSE LANDING GEAR UPLATCH AND ACTUATOR. 2 L 7 4 4F RT A197 1998080700155 19980807 00155 EU 1998 8 7 CA980421006 1 19980409 A 2910 373Q2277 LINE BRAERO 748 HS7482A 4231001 EU HYDRAULIC SYS CRACKED W K NONE K FLUID LOSS CR CRUISE 1 CA 979 (CAN) EN ROUTE, THE FLIGHT CREW NOTICED THE PORT AND STARBOARD HYDRAULIC FLOW LIGHTS ON. THE MAIN HYDRAULIC SYSTEM PRES SURE WAS SEEN TO BE FALLING. AIRCRAFT LANDED OK. PORT HYDRAULIC PRESSURE LINE FROM THE PORT EDP HAD FRACTURED AT THE I NLET TO THE HIGH PRESSURE FILTER ALLOWING THE LOSS OF FLUID. THE FRACTURE COULD NOT BE SEEN UNLESS THE LINE WAS REMOVED . FRACTURE WAS UNDER THE 'B' NUT. NEW LINE INSTALLED. 2 L 7 2 3T A24EU 1998080700156 19980807 00156 SW 1998 8 7 CA980421008 1 19980407 A 2612 PROBE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT ENGINE SHORTED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 33747 P54082 (CAN) AFTER DEPARTURE, RIGHT ENGINE FIRE WARNING ON. ENGINE SHUTDOWN AND AIRCRAFT RETURNED. NOTHING FOUND. TWO DAYS L ATER DURING TAXI, LIGHT ON AGAIN. COWLINGS REMOVED ONE AT A TIME AND LOWER ENGINE PROBE WAS FOUND SHORTING TO THE METAL COVERING OF AN ENGINE OIL LINE. 2 L 7 2 4T 4 T RT A8SW E4WE 1998080700157 19980807 00157 SW 1998 8 7 CA980421010 1 19980417 A 5711 WEB SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP CENTER SPAR CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA 31931 P54276 (CAN) FAIRCHILD RECENTLY REVISED ITS AIRFRAME INSPECTION MANUAL TO INCLUDE A DETAILED INSPECTION OF THE WING CENTER SPAR INNER WEB. CRACKS HAVE BEEN FOUND ON THE WEB. TWO OTHER AIRCRAFT WITH SIMILAR FINDINGS. 2 L 7 2 4T 4 T RT A8SW E4WE 1998080700158 19980807 00158 SW 1998 8 7 CA980421011 1 19980417 A 5711 WEB SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313 01514 WP CENTER SPAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 26289 P54214 (CAN) FAIRCHILD RECENTLY REVISED ITS AIRFRAME INSPECTION MANUAL TO INCLUDE A DETAILED INSPECTION OF THE WING CENTER SPAR INNER WEB. CRACKS FOUND ON THE WEB. TWO OTHER AIRCRAFT WITH SIMILAR PROBLEM. 2 L 7 2 4T 4 T RT A8SW E4WE 1998080700160 19980807 00160 NM 1998 8 7 CA980421013 1 19980406 A 2910 82970410119 NUT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PRESS MANIFOLD LOOSE W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 120804 (CAN) DURING CLIMB, NR 1 HYDRAULIC CAUTION LIGHT CAME ON AND NR 1 HYDRAULIC FLUID LEVEL WENT TO ZERO. INLET PRESSURE LI NE FROM EDP TO PRESSURE MANIFOLD FITTING NUT FOUND LOOSE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700161 19980807 00161 NE 1998 8 7 CA980421014 3 19980408 A 6111 SFA13M1 BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE LT PROPELLER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 120273 LH10007 (CAN) DURING WALK-AROUND, THE NR 3 BLADE OF THE LEFT HAND PROPELLER WAS FOUND CRACKED ON THE FACE OF THE NICKEL SHEATH. THE CRACK WAS LOCATED 4.8750 INCHES FROM THE EDGE OF THE DE-ICER BOOT. THE BLADE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1998080700162 19980807 00162 NM 1998 8 7 CA980421015 1 19980408 A 2731 TAB DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ELEVATOR DAMAGED W K NONE C F.O.D. CR CRUISE 1 CA 120273 (CAN) AIRCRAFT REPORTED FAILURE OF FDR. CREW UNSURE IF THEY WERE HIT BY LIGHTNING, SINCE A VIBRATION/SHUDDER AND FLASH WAS OBSERVED. THEY WERE FLYING IN PRECIPITATION. LIGHTNING ENTRY POINT FOUND ON THE LOWER SURFACE OF THE RADOME. PIN HOLE AND SEVERAL PATCHES EXPOSED ON OUTER LAMINATE. EXIT POINT DISCOVERED ON THE RIGHT HAND ELEVATOR TRIM TAB, AND A ON E INCH HOLE ON THE TRAILING EDGE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700163 19980807 00163 NM 1998 8 7 CA980421016 1 19980408 A 3246 L812148 BEARING BFGOODRICH 314352 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 WHEEL DAMAGED W K NONE M OVER TEMP TX TAXI/GRND HDL 1 CA AO78M 120382 (CAN) AFTER LANDING AND GATE ARRIVAL, NR 1 WHEEL CHECKED AND FOUND WITH WHEEL BEARING OVERHEATED AND FAILED. AXLE NUT C AP FOUND ON RUNWAY. OUTBOARD BEARING IS THE MOST DAMAGED. ROLLER CAGES AND SEALS ARE DESTROYED. WHEEL DID NOT SEIZE. W HEEL BEARING RACES WERE DAMAGED AND MELTED. NR 1 BRAKE UNIT FOUND SEIZED. METAL RAM WHEEL ASSY FOUND MELTED ON TO TWO STATORS OF BRAKE. BRAKE UNIT WORE GROOVES IN WHEEL ASSY. AXLE ON THE MAIN STRUT FOUND SCORED, AND GROOVED AND SHOWED H EAT DAMAGE. INBOARD P/N L713049. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700164 19980807 00164 NE 1998 8 7 CA980421017 3 19980409 A 6111 SFA13M1OA BLADE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROP DEBONDED W K NONE O OTHER IN INSP/MAINT 1 CA 120382 LH1896 (CAN) ON INSPECTION, NR 3 AND NR 4 (P/N SFA13G1OA) PROPELLER BLADES WERE FOUND DEBONDED AT THE TIP AREA OF THE FACE OF T HE BLADES. THE DEBONDING WAS APPROXIMATELY 2 INCHES IN LENGTH, RUNNING TO TIP CENTER OF BLADE FACE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1998080700170 19980807 00170 EA 1998 8 7 98ZZZX2603 2 19980615 A 7414 10349237 GEAR BEECH 60 60 1153602 CE LYC O541 TIO541E1A4 41536 EA RT MAGNETO STRIPPED A TIMA K NONE E R VIBRATION/BUFFET PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 NM 07 604BH P38 PILOT REPORTED ROUGH RUNNING ENGINE. REMOVED FUEL CONTROL FLOW, CHECKED. FOUND BAD RIGHT MAGNETO. TEETH STRIPPED FROM DISTRIBUTER GEAR. 1 L 7 2 3O 3 O A12CE E10EA 1998080700188 19980807 00188 NM 1998 8 7 W7NA9800001 1 19980528 A 2710 BACC2A6B00408EG CONTROL CABLE BOEING 737 7372Y5 1384554 NM LT AILERON FRAYED A W7NA O OTHER O OTHER TX TAXI/GRND HDL 1 NM 07 118RW 23040 EKO - FLT 9988 - AILERON BUS CABLE FRAYED. CABLE ROUTED WRONG AROUND CABLE GUARD. REMOVED AND REPLACED CABLE. ROUTED P ROPERLY IAW MM 27-11-11, 27-11-101, AND 27-11-71. AILERON FUNCTIONALLY CHECKED GOOD. AIRCRAFT REUTRNED TO SERVICE. (X ) 2 L 7 2 4U RT A16WE 1998080700219 19980807 00219 NE 1998 8 7 98ZZZX2556 2 19980702 A 7321 5001739629 FUEL CONTROL AMD FALC20 FALCON 2720302 EU GE CF700 CF7002D2 30010 NE ENGINE MISADJUSTED A JOGA O OTHER X ENGINE FLAMEOUT NR NOT REPORTED 1 SW 01 45MR 7851 3566 GAT46085 123 30418380 FLAME-OUT OCCURRED DUE TO A LOW FUEL DENSITY SETTING. ONCE PROPER DENSITY IS SET, NO FURTHER PROBLEMS OCCURRED. 2 L 7 2 4F 4 F A7EU E7EA 1998080700230 19980807 00230 WP 1998 8 7 98ZZZX2566 2 19980625 A 7200 ENGINE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RT ENGINE FAILED A VLLA O OTHER J WARNING INDICATION AP APPROACH 1 GL 05 108RB 8113 140 097 P74544 ON APPROACH, RT ENGINE LOST OIL PRESSURE. FOUND SOME METAL IN SCREW AND OIL. SUSPECT INTERNAL ENGINE OR GEARBOX FAILUR E. 2 L 7 2 4F 4 F A10CE E6WE 1998080700234 19980807 00234 NE 1998 8 7 98ZZZX2570 2 19980701 A 7200 ENGINE CESSNA 500 500CESSNA 2076602 CE PWA JT15 JT15D1 52060 NE LT ENGINE FAILED A ESMA E ENGINE SHUTDOWN J K WARNING INDICATION FLUID LOSS DE DESCENT 1 SO 11 102AD 5000280 WHILE DESCENDING FOR THE APPROACH, THE LEFT ENGINE LOST OIL PRESSURE AND A PRECAUTIONARY SHUT DOWN WAS ACCOMPLISHED. TH E PROBLEM WAS IDENTIFIED BY A DROP IN THE OIL PRESSURE GAUGE AND THE ILLUMINATION OF THE 'OIL LOW' ANNUNCIATOR. APPAREN T CAUSE: LOSS OF OIL OUT THE BACK OF THE ENGINE. THE AIRCRAFT WAS LANDED SUCCESSFULLY AND WITHOUT INCIDENT. 1 L 7 2 4F 4 F A22CE E1NE 1998080700235 19980807 00235 NE 1998 8 7 98ZZZX2571 2 19980621 A 7240 RK48932 COMBUSTION CAN FOKKER F27 F27MK500 4990629 EU RROYCE DART DART5327R 54509 NE AFT FLAME TUBE CRACKED A OIZA K NONE O OTHER IN INSP/MAINT 1 WP 19 284MA 1516 15060 14121 DURING A SCHEUDLED INSPECTION, THE NR 1 COMBUSTION CAN ASSY ON THE LEFT ENGINE WAS REJECTED DUE TO AN OUTER CASING BURN- THROUGH NEAR THE AFT END. UPON CAN REMOVAL, THE FLAME TUBE WAS FOUND CRACKED 360 DEGREES AND SEPARATED APPROXIMATELY 4 INCHES - 5 INCHES FROM THE AFT END. NO DOWN STREAM IMPACT OR TEMPERATURE DISTRESS NOTED. THE DAMAGED PARTS WILL BE REP LACED. THE COMBUSTION CAN WILL BE SENT TO RR. 2 H 7 2 4T 4 T A817 E297 1998080700264 19980807 00264 WP 1998 8 7 TWAA9812401 1 19980730 A 3350 3350002621 BATTERY PACK DOUG DC9 DC934 302207E WP CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 928L 48124 EMERGENCY EGRESS LIGHTS IN CABIN FLOOR WERE ILLUMINATED ALL THE TIME WITH THE SWITCH IN THE ARMED POSITION. REPLACED NR 4 BATTERY PACK FOR EMERGENCY LIGHTS. CHECK-C 3-22-98 STL. 2 L 7 2 4F RT A6WE 1998080700265 19980807 00265 WP 1998 8 7 TWAA9812402 1 19980629 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 389 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK, FOUND FUSELAGE SKIN CRACKED AT STA 389, LONGERON 28 AND 29R. REMOVED PREVIOUS REPAIR AND INST ALLED NEW REPAIR PER SRM 53-04, FIG 12B SHEET 3, AND ARA 9223 WHICH REMOVED SLOT 3 IN BY 1 IN IN AREA OF CRACK. 2 L 7 2 4F A6WE 1998080700266 19980807 00266 NM 1998 8 7 RAAA98B1086 1 19980729 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 FWD RT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998080700267 19980807 00267 NE 1998 8 7 CALA9801369 2 19980729 A 7230 809407 C-7 BLADE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE BROKEN A CALA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SW 09 72822 49482 696414 THE TOWER REPORTED THAT THE NR 1 ENGINE HAD SPARKS COMING FROM EXHAUST AREA AFTER TAKEOFF. THE CREW REPORTED THAT THERE WERE NO UNUSUAL NR 1 ENGINE INSTRUMENT INDICATIONS AND OPERATION APPEARED NORMAL. THE ENGINE WAS NOT SHUTDOWN. THE AI RCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. *S/D* ENGINEER ING CONCLUDED THAT THE PRIMARY CAUSE OF ENGINE FAILURE WAS DUE TO A BROKEN C-7 BLADE. 2 L 7 2 4F 4 F A6WE E9NE 1998080700268 19980807 00268 WP 1998 8 7 CALA9801370 1 19980730 A 5730 PANEL DOUG DC9 DC932 3022066 WP LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND CORROSION ON TOP SIDE LEFT WING PANEL NR 1122A. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-01, PAGE 8, 57-31-1, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998080700269 19980807 00269 WP 1998 8 7 CALA9801371 1 19980730 A 2760 5954283501 TORSION BAR DOUG DC9 DC932 3022066 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND RT WING INBOARD TORSION BAR CORRODED. THE TORSION BAR WAS REMOVED AND REPLACED AND OPERATION CHECKED G OOD IAW MM 27-61-6. 2 L 7 2 4F A6WE 1998080700270 19980807 00270 WP 1998 8 7 CALA9801372 1 19980730 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND FUSELAGE SKIN HAD ELONGATED HOLES AT LT VERTICAL FIN ATTACH ANGLE AREA. ALL HOLES WERE REAMED, FILLER WAS FABRICATED AND INSTALLED, AND EDDY CURRENT WAS PERFORMED IAW ECRA 5330-02692. 2 L 7 2 4F A6WE 1998080700271 19980807 00271 WP 1998 8 7 CALA9801373 1 19980730 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 1068 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .5 INCH CRACK IN LONGERON 2R AT STA 1068. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 8. 2 L 7 2 4F A6WE 1998080700272 19980807 00272 WP 1998 8 7 CALA9801374 1 19980730 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1019 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND TWO .5 INCH CRACKS AT FASTENERS IN LEFT FUSELAGE SKIN AT STA 1019 ABOVE PYLON. THE AREA WAS REPAIRED I AW SRM 53-04, FIGURE 27. 2 L 7 2 4F A6WE 1998080700273 19980807 00273 WP 1998 8 7 CALA9801375 1 19980731 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 1059 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE ATTACH ANGLE AT STA 1059, LONGERON 15R. A DOUBLER WAS FABRICATED AND INST ALLED IAW SRM 55-01, FIGURE 2. 2 L 7 2 4F A6WE 1998080700274 19980807 00274 NM 1998 8 7 CALA9801376 1 19980730 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 440 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17344 23582 INSPECTION FOUND FUSELAGE SKIN GOUGED AT STA 440, STRINGER 23R. THE GOUGE WAS BLENDED AND A DOUBLER REPAIR WAS INSTALLE D IAW SRM 53-00-01, 51-10-02, AND 53-00-01, FIGURE 201. 2 L 7 2 4F RT A16WE 1998080700275 19980807 00275 NM 1998 8 7 CALA9801377 1 19980730 A 5330 SKIN BOEING 727 727224 1384076 NM PAX DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .5 INCH CRACK AT LEFT SIDE OF FUSELAGE AT CUTOUT FOR L-1 DOOR UPPER HINGE ARM. THE CRACKED AREA WAS CUT OUT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5330-02675, SRM 51-10-2 AND SRM 51-30-2, AND SERVICE BU LLETIN 727-53-0198. 2 L 7 3 4F A3WE 1998080700276 19980807 00276 WP 1998 8 7 CALA9801378 1 19980730 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 906 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 76073 46940 INSPECTION FOUND AN 8 INCH CRACK ON LEFT WING LEADING EDGE SKIN AT WING STA XOS 906.00. REPAIRED IAW ECRA 5731-01009. 2 L 7 3 4F A22WE 1998080700277 19980807 00277 WP 1998 8 7 9809859620 1 19980728 A 2613 SENSOR DOUG DC9 DC932 3022066 WP TAIL COMPT FAILED A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 620NW 47533 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT WAS RETURNE D TO OKC. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT TAIL COMPARTMENT TEMPERATURE SENSOR. OPERA TIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998080700278 19980807 00278 NM 1998 8 7 UPS98227246 1 19980729 A 3350 BATTERY BOEING 727 727185C 138406N NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 ENTRY DOOR EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY, OPS CHECK OK. 2 L 7 3 4F A3WE 1998080700279 19980807 00279 NM 1998 8 7 UPS98227249 1 19980728 A 2750 CABLE BOEING 727 72725C 138400H NM RT TE MIDFLAP BROKEN A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 948UP 19357 FOL UNEVENTFUL 340 KT CLIMB, .80M/330 IAS SET. AFTER APROX 10 MIN, MOD VIBS STARTED AND WERE AIRSPEED. A/S REDUCED 263 KTS BEFORE VIBS ABATED. FLR COMPLIED BELOW 260 KTS. FOUND CABLE BROKEN IN MID FLAP TO AFT FLAP ASSY RT INBD T/E FLAP S EE LOG PAGE 267071 ITEM 1 FOR REPAIR. 2 L 7 3 4F A3WE 1998080700280 19980807 00280 NM 1998 8 7 UPS98227250 1 19980729 A 2761 ACTUATOR BOEING 727 727247 138408F NM SPOILER FAILED A IPXA O OTHER E VIBRATION/BUFFET CL CLIMB 1 SO 01 208UP 21701 A/C STARTED TO VIBRATE CLIMBING THROUGH FL 250 AT 280 KTS LEVELED AT FL 260 AT MAINTAINED 270 KTS EXCERCISED SPEEDBRAKE LEVER BUT VIBRATION CONTINUED WHEN ABOVE 280 KTS, VIBRATION TO DIMISH IN TURNS. REMOVED AND REPLACED OUTBOARD FLIGHT SP OILER NR 3 ACTUATOR IN REF TO MM 27-61-81. OP CK OK FOR SERVICE AT THIS TIME P/N ON 21450-11, SN OFF 355227A P/N OFF 21 450-14 SN OFF 419826. 2 L 7 3 4F A3WE 1998080700281 19980807 00281 NM 1998 8 7 UPS98227251 1 19980728 A 3350 BATTERY BOEING 727 72725C 138400H NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 931UP 19858 ENTRY DOOR EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK. OP'S CHK'S GOOD. 2 L 7 3 4F A3WE 1998080700282 19980807 00282 EU 1998 8 7 QXEA9801050 1 19980730 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 GEG - THE 28 VOLT SIGNS AT THE COCKPIT DOOR, THE CABIN ENTRANCE, AND THE FORWARD FACING LIGHT AT ROW 8 ARE ALL DIM. MAI NTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998080700283 19980807 00283 EU 1998 8 7 QXEA9801051 1 19980729 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 SEA - EXIT LIGHT AT SEAT 9A IS OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998080700284 19980807 00284 WP 1998 8 7 98FDEA00475 1 19980729 A 7120 AUB70251 FITTING DOUG DC10 DC1010 3022110 WP NR 1 P6YLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 386FE 46620 SNRM 042 STA-LAX - CORROSION FOUND TO EXCEED LIMITS ON NR 1 PYLON AFT MOUNT BULKHEAD FITTING. REMOVED AND REPLACED NR 1 PYLON AFT BULKHEAD FITTING PER SRM 51-00-01. 2 L 7 3 4F A22WE 1998080700285 19980807 00285 NM 1998 8 7 98FDEA00477 1 19980728 A 5711 6521641T SPAR CHORD BOEING 727 72721C 138400M NM WS 456-467 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 CORROSION (C57-562-02) RT WING SPAR LOWER CHORD HORIZONTAL LEG FS 456 TO 457. *S/D* REPAIRED RT WING FRONT SPAR LOWER SPAR CHORD AT FS 456 TO 467 IAW FED-EX EA 7-5710-35089. 2 L 7 3 4F A3WE 1998080700286 19980807 00286 NM 1998 8 7 98FDEA00479 1 19980730 A 5711 6595600763 SPAR CHORD BOEING 727 72721C 138400M NM BS 745 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 CORROSION (C53-132-01-1) ON WING CENTER SECTION SPAR CHORD (LOWER) AT BS 745, RBL 12 TO RBL 30, WL 160. *S/D* REMOVED AND REPLACED LOWER SPAR CHORD, BS 745 IAW FED-EX DRAWING 65C21537. 2 L 7 3 4F A3WE 1998080700287 19980807 00287 EU 1998 8 7 98FDEA00480 1 19980730 A 3234 224TS05Y CONTROL HANDLE AIRBUS 310 A310221 3930310 EU LANDING GEAR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 448FE 260 98-0188 STA-IND - AFTER T/O LANDING GEAR WOULD NOT RETRACT UNLOCK AND GREEN DIAMONDS ON ALL 6 INDICATORS. BOTH SYS 1 A ND SYS 2 ON POSITION DETECTOR SWITCH TRIED MULTIPLE TIMES. REMOVED AND REPLACED LAND GEAR CONTROL HANDLE MODULE PER M/M 32-30. PERFORMED GEAR SWING 8 CYCLES, 4 ON SYS 1 AND 4 ON SYS 2. OPS CHECK GOOD RII REQUIRED RII NR 0859 16. 2 L 7 2 4F RT A35EU 1998080700288 19980807 00288 NM 1998 8 7 98FDEA00481 1 19980731 A 2612 CONNECTOR BOEING 727 72722 1384002 NM COCKPIT CONTAMINATED A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 149FE 19087 98-0188 STA-MEM - SHORTLY AFTER GEAR SELECTED DOWN HAD FIRE WARN BELL WITH NO ASSOCIATED LIGHTS. LANDED AND MEMPHIS FI RE CREW INSP A/C, FOUND NO EVIDENCE OF FIRE. APPROXIMATELY 30 SECONDS AFTER GEAR EXTENSION. FOUND CONDENSATION ON CONN ECTOR. DISCONNECTED AND CLEANED WITH CONTACT CLEANER OPERATIONAL CHECKED SYSTEM AS PER AIRCRAFT M/M CHAPTER 26 REFERENC E. SYSTEM OPERATION CHECKED NORMAL AT THIS TIME. AIRCRAFT OK FOR RETURN TO SERVICE. 2 L 7 3 4F A3WE 1998080700289 19980807 00289 WP 1998 8 7 ABXA9800651 1 19980521 A 5311 5750180451 FRAME DOUG DOUG DC8 DC863F 302198F WP BS 1040 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STATION 1040 FRAME UPPER CHORD, LOWER SURFACE AFT SIDE, AT LONGERON 31R AND 32R HAS HEAVY EXFOLIATION CORROSION AND IS C RACKED. REPAIRED IAW ABX REA D853-22857, SRM 51-1-21, 51-1-20D AND 51-1-11. 2 L 7 4 4F 4A25 1998080700290 19980807 00290 WP 1998 8 7 ABXA9800652 1 19980501 A 5320 3450257IN FITTING DOUG DOUG DC8 DC863F 302198F WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 STATION 600-620, STRINGER 31R SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DWG 3750257 AND DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1998080700291 19980807 00291 WP 1998 8 7 ABXA9800653 1 19980427 A 5712 5769496 RIB DOUG DOUG DC8 DC863F 302198F WP WS 716025 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING LEADING EDGE AT STATION XFS 716.250. THE UPPER RIB IS CRACKED AT THE AFT END. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998080700292 19980807 00292 WP 1998 8 7 ABXA9800654 1 19980430 A 5320 561032617 ANGLE DOUG DOUG DC8 DC863F 302198F WP BS 380 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 FORWARD AND AFT SIDES OF STATION 380 FLOORBEAM LBL 11 AND RBL 11. THE INTERCOSTAL ATTACH ANGLES ARE CRACKED. REMOVED, FABRICATED AND REPLACED ANGLES IAW DWG 5610326 AND SRM 51-1-21. 2 L 7 4 4F 4A25 1998080700293 19980807 00293 WP 1998 8 7 ABXA9800655 1 19980523 A 5320 SRO85700095 ANGLE DOUG DOUG DC8 DC863F 302198F WP WS 857 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 CRACK IN LEFT WING REAR SPAR LOWER CAP STATION 857 LBL 70 INBOARD APPROXIMATELY 9 LEFT MLG WHEEL WELL, FORWARD, LOWER, O UTBOARD. REPAIRED IAW DWG SR08570009 AND DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998080700294 19980807 00294 WP 1998 8 7 ABXA9800656 1 19980523 A 5720 3648143501 FITTING DOUG DOUG DC8 DC863F 302198F WP BS 495 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 ATTACH FITTING AT CANTED STATION XRS 495 TO STRINGER 63 (UPPER SKIN) HAS CRACK AT LAST FASTENER HOLE. FABRICATED REPLAC EMENT ATTACH FITTING IAW DWG 3648143 AND ABX REA 857-22859. 2 L 7 4 4F 4A25 1998080700295 19980807 00295 WP 1998 8 7 ABXA9800657 1 19980603 A 5312 56121595 BULKHEAD WEB DOUG DOUG DC8 DC863F 302198F WP BS 1890 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 24763 1 .5 INCH CRACK AT AFT BULKHEAD STATION 1890, UPPER RIGHT CORNER ABOVE BRACKET WITH MOUNT BOLT FOR RUDDER POWER MECHANIS M. REPAIRED IAW DC8 SRM 52-2-0. 2 L 7 4 4F 4A25 1998080700296 19980807 00296 WP 1998 8 7 ABXA9800658 1 19980527 A 5712 97532771 BULKHEAD DOUG DOUG DC8 DC863F 302198F WP WS 508.977 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 LEFT WING CANTED BULKHEAD LOWER FLANGE CRACKED AT XRS 508.977 BETWEEN STRINGERS 63-64. REPAIRED IAW ABX REA D853-22858M R AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998080700297 19980807 00297 WP 1998 8 7 ABXA9800659 1 19980715 A 5320 D0489841 CUSP DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 966AX 47510 DURING C-CHECK, FOUND CUSP WEB CRACKED AT LONGERON 18R, FS 1041. REPLACED CUSP WEB FS 946 TO 1041 IAW DC9 SRM 51-30-2, 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998080700298 19980807 00298 WP 1998 8 7 ABXA9800660 1 19980724 A 5320 59114279 STIFFENER DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 WHILE COMPLYING WITH C INSPECTION, FOUND STATION 965 LONGERON L17 CRACKED UNDER SPLICE STIFFENER. REPAIRED IAW DC-9 SRM AND DWG K05864. 2 L 7 2 4F A6WE 1998080700299 19980807 00299 WP 1998 8 7 ABXA9800671 1 19980729 A 5610 4440940505 SPRING DOUG DC9 DC932 3022066 WP COCKPIT WEAK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 988AX 47084 DURING PREFLIGHT WAS UNABLE TO OPEN CAPTAIN'S CLEARVIEW WINDOW. REPLACED AFT LOWER LATCH HOOK RETURN SPRING AND LUBRICA TED WINDOW. 2 L 7 2 4F A6WE 1998080700300 19980807 00300 WP 1998 8 7 ABXA9800672 1 19980730 A 5610 561321718 WINDOW DOUG DC8 DC863 302198A WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 817AX 45928 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT SLIDE OPEN COMPLETELY. READJUSTED CLEARVIEW WINDOW IAW DC8 MM . 2 L 7 4 4F 4A25 1998080700301 19980807 00301 WP 1998 8 7 ABXA9800673 1 19980730 A 3250 57698711 PIVOT ARM DOUG DC8 DC861 3021952 WP LT MLG BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 DURING POST FLIGHT INSP, FOUND LEFT MAIN LANDING GEAR BOGIE SWIVEL MECHANISM PIVOT ARM BROKEN. REPLACED BOGIE SWIVEL AR M IAW DC8 MM 32-51-04. 2 L 7 4 4F 4A25 1998080700302 19980807 00302 WP 1998 8 7 ABXA9800661 1 19980618 A 5730 5611340 SKIN DOUG DOUG DC8 DC861F 3021953 WP WS 74 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 RIGHT WING TOP SKIN AT STATION XRS 74 IS CRACKED AT STRINGER 9, 10, AND 11. REPAIRED RIGHT WING SKIN DC-8 SRM 57-2-1. 2 L 7 4 4F 4A25 1998080700303 19980807 00303 WP 1998 8 7 ABXA9800662 1 19980617 A 5320 37502571 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 440 & 460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 31L SPLICE FITTING BETWEEN STATION 440 AND 460 CRACKED. REPLACED LONGERON SPLICE FITTING IAW DC8 SRM 53-1-0 AN D 51-1-20D. 2 L 7 4 4F 4A25 1998080700304 19980807 00304 WP 1998 8 7 ABXA9800663 1 19980617 A 5320 37533061 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 980-1000 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 STATION 980 - 1000 LONGERON 23L END FITTING CRACKED. REPLACED END FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998080700305 19980807 00305 WP 1998 8 7 ABXA9800664 1 19980617 A 5320 5710350DD ANGLE DOUG DOUG DC8 DC861F 3021953 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 DRIVE LINK FITTING STIFFENER ANGLE CRACKED, LEFT WING, FLAP STATION 3.00. REPAIRED IAW DC8 SRM 53-8-1 AND 51-1-20. 2 L 7 4 4F 4A25 1998080700306 19980807 00306 WP 1998 8 7 ABXA9800665 1 19980616 A 5320 36471172N FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FS 960 FITTING CRACKED BETWEEN LONGERON 24L AND THE PRESSURE WEB. REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-3-0. 2 L 7 4 4F 4A25 1998080700307 19980807 00307 WP 1998 8 7 ABXA9800666 1 19980613 A 5320 3750257503N FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 31L SPLICE FITTING CRACKED AT STATION 1040-1060. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998080700308 19980807 00308 WP 1998 8 7 ABXA9800667 1 19980614 A 5320 5750322502 SPLICE DOUG DOUG DC8 DC861F 3021953 WP BS 1140-1160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 34R CRACKED STATION 1140-1160. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1998080700309 19980807 00309 WP 1998 8 7 ABXA9800668 1 19980613 A 5320 37502571N FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 31L SPLICE FITTING CRACKED STATION 600-620. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998080700310 19980807 00310 WP 1998 8 7 ABXA9800669 1 19980624 A 5320 97549453 WEB DOUG DOUG DC8 DC861F 3021953 WP BS 1210-1250 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 HEAVY CORROSION ON TORQUE BOX WEB AT STATION 1210-1250. REPAIRED WEB IAW DWG 9754945, DC8 SRM 53-2-0 AND 51-1-21. 2 L 7 4 4F 4A25 1998080700311 19980807 00311 WP 1998 8 7 ABXA9800670 1 19980627 A 5720 5655441 STRAP DOUG DOUG DC8 DC861F 3021953 WP WS 610 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 RIGHT WING LEADING EDGE AT STATION XFS 610.000, UPPER RIB TRAILING EDGE STRAP IS CRACKED. REPLACED STRAP IAW DWG 565544 1 AND DC8 SRM 51-1-21A. 2 L 7 4 4F 4A25 1998080700312 19980807 00312 NM 1998 8 7 SCNA98082 1 19980730 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE AFT ENTRY BULLNOSE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLAC ED THE BATTERY PACK. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998080700313 19980807 00313 WP 1998 8 7 SCNA98083 1 19980729 A 3397 WIRE DOUG DC10 DC1015 3022118 WP CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 151SY 48295 DURING A LINE MAINTENANCE CHECK, THE MID CABIN RIGHT SIDE EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. FOUND A BRO KEN WIRE. WIRE REPAIRED AND LIGHTS OPERATIONALLY CHECK GOOD IN ACCORDANCE WITH 3300. 2 L 7 3 4F A22WE 1998080700314 19980807 00314 NM 1998 8 7 DHL98712003 1 19980729 A 3260 SWITCH BOEING 727 72729 1384007 NM NLG DIRTY A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 712DH 19401 LANDING GEAR NOSE GREEN LIGHT FAILED TO ILLUMINATE TWICE ON EXTENSION. THIRD ATTEMPT AT EXTENSION WAS SUCESSFUL. RED UNSAFE LIGHTS CYCLED NORMALLY, PRESS TO TEST WAS NORMAL. CLEANED DOWN LOCK SWITCH AND LUBED NOSE GEAR. JACKED NOSE GE AR AND CYCLES SEVERAL TIMES. OPS CHECK OK PER MM 32-61-21. 2 L 7 3 4F A3WE 1998080700315 19980807 00315 NM 1998 8 7 P5CA9801182 1 19980722 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING DELAMINATION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT WING UPPER SURFACE FWD INBOARD TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998080700316 19980807 00316 NM 1998 8 7 P5CA9801183 1 19980723 A 5753 SKIN BOEING 747 747132 1384882 NM LT TE FLAP DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT OUTBOARD TRAILING EDGE AFT FLAP LOWER SURFACE 4 FOOT DELAMINATION. REPAIRED PER SRM 51-40-07. 2 L 7 4 4F A20WE 1998080700317 19980807 00317 NM 1998 8 7 P5CA9801184 1 19980723 A 5280 SKIN BOEING 747 747132 1384882 NM RT MLG DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT WING GEAR DOOR 5 INCH DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998080700318 19980807 00318 NM 1998 8 7 P5CA9801185 1 19980723 A 5280 SKIN BOEING 747 747132 1384882 NM LT MLG DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT WING GEAR DOOR CORNER DELAMINATED. REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998080700319 19980807 00319 NM 1998 8 7 P5CA9801186 1 19980723 A 5730 PANEL BOEING 747 747132 1384882 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT WING UPPER SURFACE FIXED TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998080700320 19980807 00320 NM 1998 8 7 P5CA9801187 1 19980723 A 7110 COWL BOEING 747 747132 1384882 NM NR 2 ENGINE CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 2 ENGINE INBD CORE COWL PREVIOUS REPAIR CHAFFED THROUGH. REPAIRED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1998080700321 19980807 00321 NM 1998 8 7 P5CA9801188 1 19980723 A 7110 COWL BOEING 747 747132 1384882 NM NR 1 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 1 ENGINE OUTBD CORE COWL MOST AFT LATCH HOUSING CRACKED AND DAMAGED. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998080700322 19980807 00322 NM 1998 8 7 P5CA9801189 1 19980723 A 5755 SKIN BOEING 747 747132 1384882 NM NR 4 SPOILER DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 4 SPOILER UPPER SURFACE DELAMINATED. REMOVED AND REPLACED SPOILER PANEL PER MM 27-61-02. 2 L 7 4 4F A20WE 1998080700323 19980807 00323 NM 1998 8 7 P5CA9801190 1 19980723 A 5280 HINGE BOEING 747 747132 1384882 NM RT MLG DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT CENTER GEAR DOOR HINGE LIGHT SURFACE CORROSION. REPAIRED BY SRM 51-10-02 AND 51-10-06. 2 L 7 4 4F A20WE 1998080700324 19980807 00324 NM 1998 8 7 P5CA9801191 1 19980723 A 7110 COWL BOEING 747 747132 1384882 NM NR 1 ENGINE LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 1 ENGINE OUTBOARD CORE COWL TOP AFT CORNER LOOSE FASTENERS. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998080700325 19980807 00325 NM 1998 8 7 P5CA9801192 1 19980723 A 7110 COWL BOEING 747 747132 1384882 NM NR 2 ENGINE LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 2 ENGINE CORE COWL 3RD LATCH AREA HAS LOOSE FASTENERS. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998080700326 19980807 00326 NM 1998 8 7 P5CA9801193 1 19980723 A 5730 PANEL BOEING 747 747132 1384882 NM LT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 LEFT WING UPPER SURFACE PANEL DELAMINATED INBD 2ND FROM ROOT AREA. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998080700327 19980807 00327 NM 1998 8 7 P5CA9801194 1 19980723 A 7110 RIB BOEING 747 747132 1384882 NM NR 2 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 2 ENGINE INBOARD POWER COWL RIB CRACKED. REPAIRED PER SRM 51-30-02 AND 51-10-01. 2 L 7 4 4F A20WE 1998080700328 19980807 00328 NM 1998 8 7 P5CA9801195 1 19980723 A 7110 COWL BOEING 747 747132 1384882 NM NR 2 ENGINE DAMAGE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 2 ENGINE INBOARD POWER COWL LOWER CORNER SKIN DAMAGED. REPAIRED PER SRM 54-30-03 AND 51-10-02. 2 L 7 4 4F A20WE 1998080700329 19980807 00329 NM 1998 8 7 P5CA9801196 1 19980723 A 7110 FAIRING BOEING 747 747132 1384882 NM NR 4 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 4 ENGINE DOG HOUSE FAIRING TORN/DAMAGED. REPAIRED TO SRM 51-40-02. 2 L 7 4 4F A20WE 1998080700330 19980807 00330 NM 1998 8 7 P5CA9801197 1 19980723 A 7810 EXHAUST SLEEVE BOEING 747 747132 1384882 NM NR 3 ENGINE LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 3 ENGINE EXHAUST SLEEVE A 1 O'CLOCK POSITION LOOSE FASTENERS. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998080700331 19980807 00331 NM 1998 8 7 P5CA9801198 1 19980723 A 5245 FASTENER BOEING 747 747132 1384882 NM AIR COND DOOR MISSING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 PANEL 191NL MISSING FASTENERS. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998080700332 19980807 00332 NM 1998 8 7 P5CA9801199 1 19980723 A 7830 STINGER BOEING 747 747132 1384882 NM NR 1 ENGINE LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 1 ENGINE STINGER ASSY LOOSE AND MISSING FASTENERS. REPAIRED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998080700333 19980807 00333 NM 1998 8 7 P5CA9801200 1 19980723 A 5245 FAIRING BOEING 747 747132 1384882 NM AIR COND DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 3 PACK EXIT DOOR FAIRING PANEL DELAMINATED. REPAIRED PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998080700334 19980807 00334 NM 1998 8 7 P5CA9801201 1 19980723 A 5400 65B907074 FAIRING BOEING 747 747132 1384882 NM NR 4 PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 4 PYLON V FAIRING DELAMINATED. REMOVED AND REPLACED FAIRING SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998080700335 19980807 00335 NM 1998 8 7 P5CA9801202 1 19980723 A 7110 ANGLE BOEING 747 747132 1384882 NM NR 1 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 1 ENGINE INBOARD CORE COWL MOST AFT RIB ASSY HAS CRACKED ANGLE. REPAIRED PER SRM 51-10-01 AND 51-30-01. 2 L 7 4 4F A20WE 1998080700336 19980807 00336 NM 1998 8 7 P5CA9801203 1 19980723 A 5730 PANEL BOEING 747 747132 1384882 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 RIGHT WING UPPER SURFACE TRAILING EDGE PANEL DELAMINATED. REPAIRED PER SRM 51-40-15 AND 51-24-11. 2 L 7 4 4F A20WE 1998080700337 19980807 00337 NM 1998 8 7 P5CA9801204 1 19980723 A 5400 FAIRING BOEING 747 747132 1384882 NM NR 3 PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 3 PYLON V FAIRING DELAMINATED. REPAIRED PER SRM 51-30-07. 2 L 7 4 4F A20WE 1998080700338 19980807 00338 NM 1998 8 7 P5CA9801205 1 19980723 A 5245 SKIN BOEING 747 747132 1384882 NM AIR COND DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 3 AIR CONDITIONING BAY DOOR DELAMINATED. REPAIRED PER SRM 51-24-11 AND 51-40-15. 2 L 7 4 4F A20WE 1998080700339 19980807 00339 NM 1998 8 7 P5CA9801206 1 19980723 A 5412 BULKHEAD BOEING 747 747132 1384882 NM NR 4 PYLON DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 NR 4 PYLON INTERNAL AT BULKHEAD LINE PASS THROUGH ELONGATED. REPAIRED PER SRM 54-10-03 AND MM 20-11-05. 2 L 7 4 4F A20WE 1998080700340 19980807 00340 NE 1998 8 7 P5CA9801207 2 19980726 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 FLAMED OUT A P5CA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 WP 23 851FT 19756 662552 NR 2 ENGINE FLAMED OUT FL350. ENG RESTART AT FL 290. RESTART NORMAL. PERFORMED FUEL CONTAMINATION CHECK PER MM 73-00- 00 PG 201. VERIFIED FUEL REMAIN NR 2 TANK VIA STICK 17 AT 20.0, 10,962 LBS. SUMPED TANKS FOR EVIDENCE OF WATER, VERIFI ED CONDITON MOTOR OPERATIONAL. VERIFIED FUEL PUMP PRESS PER MM 76-00-46 PROCEDURE 1. CHECKED INLET AND EXHAUST FOR FOD DAMAGE. DRY MOTORED THE WET MOTORED. ENG STARTED NORMAL. CHECK AND REPLACE FUEL FILTER, NO CONTAMINATION FOUND ALL C HECK NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1998080700341 19980807 00341 NM 1998 8 7 P5CA9801208 1 19980722 A 2612 WIRE BOEING 747 747122 1384872 NM FE PANEL CHAFED A P5CA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 23 851FT 19756 REJECTED TAKEOFF FROM RTA DUE TO AFT CARGO FIRE INDICATION AND FIRE BELL DURING T/O ROLL. PARKED AND INSPECTED FOR FIRE . NO SMOKE OR FIRE NOTED. TRANSFERED TO DMI NR 20623 AND 20624. REMOVED AND REPLACED SMOKE DETECTOR PANEL P-4 FOR T/S PER MM 26-16-00 DMI OK TO CONTINUE. LOWER CARGO FIRE DETECT LIGHT INTERMIT DURING TURBULENCE AND LANDING AT JFK. FOUN D CHAFFED WIRE BEHIND F/E PANEL. REPAIRED WIRING PER MM 20-10-13 CHECK OK PER 26-16-00 DMI CLEARED. 2 L 7 4 4F A20WE 1998080700342 19980807 00342 WP 1998 8 7 RRAX98292 1 19980428 A 5720 5615090 FITTING DOUG DC8 DC873F 302199F WP FRONT SPAR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT FOUND INNER FRONT SPAR SPLICE FITTING (PN: 5615090) CRACKED. REMOVED FITTING, FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUBSTITUTION IAW FAA APPROVED TIMCO DER REO-04751. 2 L 7 4 4F RT 4A25 1998080700343 19980807 00343 WP 1998 8 7 RRXA98289 1 19980605 A 5311 5615700 FRAME DOUG DC8 DC873F 302199F WP BS 190 & 200 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAMES WITH MISS-DRILLED HOLES, AT STA 190 ALSO STA 200, BETWEEN LONGERONS 7 RIGHT TO 16 RIGHT AND LONGERON 6 LEFT. REMOVED DAMAGED SECTIONS, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR STRAPS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04725. 2 L 7 4 4F RT 4A25 1998080700344 19980807 00344 WP 1998 8 7 RRXA98290 1 19980605 A 5311 5750174 FRAME DOUG DC8 DC873F 302199F WP BS 430 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 430 AND LONGERON 13 LEF T. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04720. 2 L 7 4 4F RT 4A25 1998080700345 19980807 00345 WP 1998 8 7 RRXA98291 1 19980522 A 5522 565497033 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND LEFT ELEVATOR SKIN ASSEMBLY AND TE CLOSING CHANNEL AT STA XE=200.258 HAD A DOUBLER DRI LLED HOLE. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR STRAP AND FILLER IAW FAA APPROVED TIMCO DER ENGINEE RING SKETCH REO-04741. 2 L 7 4 4F RT 4A25 1998080700346 19980807 00346 WP 1998 8 7 RRXA98293 1 19980526 A 5311 577278737 FRAME DOUG DC8 DC873F 302199F WP BS 270 & 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND MAIN CARGO DOOR JAMB FRAMES WITH MIS-DRILLED HOLES, AT STA 270 AND STA 280. REMOVED D AMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH ENGINEERING SKETC H REO-04753. 2 L 7 4 4F RT 4A25 1998080700347 19980807 00347 WP 1998 8 7 RRXA98294 1 19980522 A 5311 5750835501 FRAME DOUG DC8 DC873F 302199F WP BS 1080 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME WITH MIS-DRILLED HOLES, AT STA 1080 BETWEEN LONGERONS 5 LEFT TO 8 LEFT. REMOVED DAMAGED SECTIONS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04762. 2 L 7 4 4F RT 4A25 1998080700348 19980807 00348 WP 1998 8 7 RRXA98295 1 19980526 A 5315 561214257 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1700 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1700. REMOVED DAMA GED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGIN EERING SKETCH REO-04764. 2 L 7 4 4F RT 4A25 1998080700349 19980807 00349 WP 1998 8 7 RRXA98296 1 19980522 A 5320 46111811 FITTING DOUG DC8 DC873F 302199F WP BS 70-80 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND LONGERON 14 LEFT END FITTING (4611181-1) CRACKED, BETWEEN STA 70 TO STA 80. REMOVED F ITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUBSTITUTION, IAW FAA APPROV ED TIMCO DER ENGINEERING SKETCH REO-04765. 2 L 7 4 4F RT 4A25 1998080700350 19980807 00350 WP 1998 8 7 RRXA98297 1 19980522 A 5320 46111811 FITTING DOUG DC8 DC873F 302199F WP BS 55-70 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND LONGERON 14 RIGHT END FITTING (PN: 4611181-1) CRACKED, BETWEEN STA 55 AND STA 70. REM OVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUBSTITUTION IAW FAA A PPROVED TIMCO DER ENGINEERING SKETCH REO-04766. 2 L 7 4 4F RT 4A25 1998080700351 19980807 00351 WP 1998 8 7 RRXA98298 1 19980605 A 5311 5759216 FRAME DOUG DC8 DC873F 302199F WP BS 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 300 BETWEEN LONGERONS 5 LEFT AND 6 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRCATED AND INSTALLED REPAIR IAW FAA AP PROVED TIMCO DER ENGINEERING SKETCH REO-04778. 2 L 7 4 4F RT 4A25 1998080700352 19980807 00352 WP 1998 8 7 RRXA98299 1 19980605 A 5311 9755500 FRAME DOUG DC8 DC873F 302199F WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS, AT STA 1260 AND LONGERON 4 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER R EO-04779. 2 L 7 4 4F RT 4A25 1998080700353 19980807 00353 WP 1998 8 7 RRXA98300 1 19980527 A 5320 4611284502 FITTING DOUG DC8 DC873F 302199F WP BS 70 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND LONGERON 11 RIGHT END FITTING (PN: 4611284-502) CRACKED, AT STA 70. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUBSTITUTION IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04780. 2 L 7 4 4F RT 4A25 1998080700354 19980807 00354 WP 1998 8 7 RRXA98301 1 19980527 A 5312 57535221 BULKHEAD DOUG DC8 DC873F 302199F WP AFT PRESS BLKHD DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, ONE EACH FASTENER HOLE WAS DAMAGED DURING DRILLING OPERATION OF DC-8 SRM 53-2-5 FIGURE 14A, SHEET 4, REPAIR TO AFT PRESSURE BULKHEAD BETWEEN LONGERONS 10 LEFTAND 12 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04786. 2 L 7 4 4F RT 4A25 1998080700355 19980807 00355 WP 1998 8 7 RRXA98302 1 19980528 A 2750 37511591 LINK DOUG DC8 DC873F 302199F WP LT TE FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND LEFT WING, FLAP LINK GOUGED, AT STA 340. AFTER DAMAGE BLEND-OUT, NO DC-8 SRM LIMITS G IVEN. LIMITATIONS APPROVED IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-4787. 2 L 7 4 4F RT 4A25 1998080700356 19980807 00356 WP 1998 8 7 RRXA98303 1 19980605 A 5311 5753322 FRAME DOUG DC8 DC873F 302199F WP BS 100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 100 AND LONGERON 30 RIG HT. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04788. 2 L 7 4 4F RT 4A25 1998080700357 19980807 00357 WP 1998 8 7 RRXA98304 1 19980605 A 5311 561548 FRAME DOUG DC8 DC873F 302199F WP BS 200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 200 AND LONGERON 17 RIG HT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVE D TIMCO DER ENGINEERING SKETCH REO-04789. 2 L 7 4 4F RT 4A25 1998080700358 19980807 00358 WP 1998 8 7 RRXA98305 1 19980601 A 5320 56119433 ANGLE DOUG DC8 DC873F 302199F WP BS 70 CUT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, STA 70, FWD CAP ANGLE REQUIRES SPLICE REPAIR, BETWEEN LONGERONS 25 LEFT TO 26 LEFT, AND RIGH T SIDE. DC-8 SRM 53-2-5, FIGURE 8C GIVES INSTRUCTIONS TO ACCOMPLISH THE SPLICE AT LOWER LOCATION. FAA APPROVED TIMCO D ER REO-04801, ALSO PROVIDES ADDITIONAL INSTRUCTIONS TO PERFORM REPAIR. 2 L 7 4 4F RT 4A25 1998080700359 19980807 00359 WP 1998 8 7 RRXA98306 1 19980601 A 5711 55978292 SPAR CAP DOUG DC8 DC873F 302199F WP RT WING CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, AFT SPAR CAP WITH CORROSION BEYOND LIMITS IAW DC-8 SRM, AT STA 63. REMOVE D DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEE RING SKETCH REO-04804. 2 L 7 4 4F RT 4A25 1998080700360 19980807 00360 WP 1998 8 7 RRXA98307 1 19980605 A 5311 5640235 FRAME DOUG DC8 DC873F 302199F WP BS 1520 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1520 AND LONGERON 8 RIG HT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04807. 2 L 7 4 4F RT 4A25 1998080700361 19980807 00361 WP 1998 8 7 RRXA98308 1 19980601 A 5320 57510409 JAMB DOUG DC8 DC873F 302199F WP L2 DOOR CUT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, L-2 DOOR JAMB PAN, AFT LOWER CORNER NEEDS TO BE REMOVED TO FACILITATE OTHER MAINTENANCE. RE PLACED PANEL BY SPLICE REPAIR IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-04810. 2 L 7 4 4F RT 4A25 1998080700362 19980807 00362 WP 1998 8 7 RRXA98309 1 19980604 A 5311 5614945535 FRAME DOUG DC8 DC873F 302199F WP BS 300 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FRAME DENTED/CRACKED BEYOND LIMITS IAW DC-8 SRM, STA 300 AND LONGERON 15 RIGHT. REMOV ED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINE ERING SKETCH REO-04843. 2 L 7 4 4F RT 4A25 1998080700363 19980807 00363 WP 1998 8 7 RRXA98310 1 19980608 A 5210 5615775127 SKIN DOUG DC8 DC873F 302199F WP PAX DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND AFT ENTERANCE DOOR SKIN WITH CRACK BEYOND LIMITS IAW DC-8 SRM, AT STA 1640. REMOVED D AMAGED SECTION, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETC H REO-04857. 2 L 7 4 4F RT 4A25 1998080700364 19980807 00364 WP 1998 8 7 RRXA98311 1 19980609 A 5320 4611181 FITTING DOUG DC8 DC873F 302199F WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND FITTING (4611181) WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 70 AND LONG ERON 17 RIGHT. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING BY MATERIAL SUB STITUTION IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04863. 2 L 7 4 4F RT 4A25 1998080700365 19980807 00365 WP 1998 8 7 RRXA98312 1 19980622 A 5230 2363572 CAM DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND MAIN CARGO DOOR LATCH CAM (2363572) WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED CAM, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW CAM IAW FAA APPROVED TIMCO DER EN GINEERING SKETCH REO-04932. 2 L 7 4 4F RT 4A25 1998080700366 19980807 00366 WP 1998 8 7 RRXA983138 1 19980522 A 5320 97585211 ANGLE DOUG DC8 DC873F 302199F WP BS 280 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CROSS SLIDE DOOR, COVER ATTACH ANGLE WITH CORROSION BEYOND LIMITS IAW DC-8 SRM, AT STA 280 BETWEEN LONGERONS 27 RIGHT AND 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-04758. 2 L 7 4 4F RT 4A25 1998080700367 19980807 00367 WP 1998 8 7 CKSA98493 1 19980730 A 2612 D5020 FIRE LOOP DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 1 ENGINE OUT OF ADJUST A CKSA K NONE N FALSE WARNING AP APPROACH 1 GL 23 815CK 46151 678969 ENGINE FIRE INDICATION NR 1, BOTTLE NR 1 DISCHARGED, HANDLE LIGHT REMAINED ILLUMINATED, BOTTLE NR 2 DISCHARGED, LIGHT RE MAINED ILLUMINATED, ON POST FLIGHT, NO VISABLE INDICATION OF FIRE. REMOVED AND REPLACED NR 1 ENGINE FIRE LOOP AS PER MM 26-10-1 GROUND GOOD AS PER MM 26-10-0. REMOVED AND REPLACED LT INBOARD AND OUTBOARD ENGINE FIRE BOTTLES AS PER MM 26-2 0-1. INSTALLED SQUIBS ON LT OUTBOARD FIRE BOTTLE AS PER MM 26-20-2 FIRE SENSING SYSTEM TEST GOOD AS PER 26-10-0 RAN NR 1 ENGINE, NO PNEUMATIC LEAK NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1998080700368 19980807 00368 1998 8 7 CALA9801379 4 19980731 A 2210 4020952906 YAW DAMPER BOEING 737 7373T0 1384582 NM E & E COMPT MALFUNCTIONED A CALA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SW 09 12319 23370 WHILE CLIMBING THROUGH 5,000 FEET WITH THE AUTOPILOT OFF, THE AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL. THE YAW DAMPER I NDICATOR PEGGED FULL RIGHT. THE YAW DAMPER WAS TURNED OFF AND THE FLIGHT WAS CONTINUED. THE YAW DAMPER WAS TURNED ON W HILE AT CRUISE WITH AUTOPILOT ON AND OPERATION WAS NORMAL. MAINTENANCE REMOVED AND REPLACED THE MAIN RUDDER PCU, THE ST ANDBY RUDDER PCU, AND THE YAW DAMP COUPLER. *S/D* SHOP TEARDOWN REVEALED THE FOLLOWING (1) YAW DAMPER COUPLER (P/N 403 0952-906) RATE GYRO ROUGH RUNNING. (2) STANDBY RUDDER PCU (P/N 1U1150-1) ROD SEAL LEAKAGE WITH PACKING WORN, FOUND BOLTS , CORRODED. (3) MAIN RUDDER PCU (P/N 65C37052-9) LEVER ASSEMBLIES AND ROD END BEARINGS WORN, MANIFOLD CORRODED. 2 L 7 2 4F RT A16WE 1998080700369 19980807 00369 WP 1998 8 7 CALA9801380 1 19980731 A 5400 ANGLE DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND A CRACK IN NR 1 PYLON TRAILING EDGE PANEL INTERCOSTAL ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-3, AND 51-00. 2 L 7 2 4F A6WE 1998080700370 19980807 00370 WP 1998 8 7 CALA9801381 1 19980731 A 7830 BRACKET DOUG DC9 DC932 3022066 WP NR 1 TR UNIT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND NR 1 THRUST REVERSER PANEL BRACKET GOUGED. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND I NSTALLED IAW SRM 51-10-1, 51-10-2A, AND 51-30-2. 2 L 7 2 4F A6WE 1998080700371 19980807 00371 WP 1998 8 7 CALA9801382 1 19980731 A 5400 STRAP DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND A 3 INCH CRACK IN NR 1 PYLON TRAILING EDGE PANEL DOUBLER STRAP. A NEW DOUBLER WAS FABRICATED AND INSTA LLED IAW SRM 54-30-0. 2 L 7 2 4F A6WE 1998080700372 19980807 00372 WP 1998 8 7 CALA9801383 1 19980801 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 13891 49102 THE PULL FROM CLIPS AT INTERIOR TAIL CONE RELEASE HANDLE WAS HIGH AT 50 POUNDS. THE TAIL CONE HANDLE CLIPS WERE ADJUSTE D IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998080700373 19980807 00373 SO 1998 8 7 COMA9810167 1 19980731 A 2751 WARNING EMB 120 EMB120RT SO TE FLAPS ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 152CA 120152 FLAP SYSTEM WARNING DURING TAKEOFF. COULD NOT DUPLICATE, SYSTEM TEST NORMAL. 2 L 7 2 4T RT A31SO 1998080700374 19980807 00374 EA 1998 8 7 COMA9860209 1 19980801 A 2613 356024310 OVERHEAT ELEMENT CNDAIR CL600 CL6002B19 EA LT PYLON MALFUNCTIONED A COMA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 959CA 7116 LEFT HAND STAGE BLEED DUCT LEAK WARNING. REPLACED THE BLEED LEAK SENSING ELEMENT IN LEFT HAND ENGINE PYLON. 2 L 7 2 4F RT A21EA 1998080700375 19980807 00375 EA 1998 8 7 COMA9860210 1 19980728 A 3222 16120NLGQC STRUT CNDAIR CL600 CL6002B19 EA NLG MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 915CA 54 54 7013 NLG SLOW TO RETRACT GEAR DISAGREE WARNING. REPLACED THE NLG SHOCK STRUT. 2 L 7 2 4F RT A21EA 1998080700376 19980807 00376 EA 1998 8 7 COMA9860211 1 19980731 A 2540 TRASH BIN CNDAIR CL600 CL6002B19 EA LAVATORY FIRE A COMA A F UNSCHED LANDING ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 SO 01 918CA 7018 EMERGENCY LANDING DUE TO FIRE IN LAVATORY. INSPECTED LAVATORY TRASH BIN AND FIRE EXTINGUISHER, FOUND TO BE SERVICEABLE. 2 L 7 2 4F RT A21EA 1998080700377 19980807 00377 NM 1998 8 7 UPS98227266 1 19980803 A 5711 SPAR BOEING 727 72727C 138400J NM RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 909UP 19115 INSPECTION TYPE-N/A, RT WING REAR SPAR U-CHANNEL CRACKED BETWEEN LIGHTENING HOLES DIRECTLY OVER RT MAIN LANDING GEAR STR UT, (MARKED IN RED). REPAIRED CRACKED AREA AS PER EO B727-5720-10177-A, INSTALLED REPAIR DOUBLER. 2 L 7 3 4F A3WE 1998080700378 19980807 00378 NE 1998 8 7 UPS98427265 2 19980802 A 7320 CONNECTOR PIN BOEING 747 747121 1384871 NM PWA JT9 JT9D7 52054 NE NR 1 ENGINE BENT A IPXA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 SO 01 681UP 19661 662872 INSPECTION TYPE-N/A, CREW REPORTED AT 500 FT AGL ON FINAL APPROACH, NR 1 ENGINE FLAMED OUT. NORMAL LANDING ACCOMPLISHED . INFLIGHT START NOT INITIATED DUE TO DISTANCE FROM RUNWAY. FOUND PIN 6 ON NR 1 ENG FIREWALL CONN D0014P BENT AND TOUC HING PIN 17 CAUSING FUEL CONTROL ACTUATOR TO MALFUNCTION. REMOVED AND REPLACED CONDITION ACTUATOR AND STRAIGHTENED PIN. ACT FUNCTION AND ENGINE RUN WERE SATISFACTORY. 2 L 7 4 4F 4 F A20WE E20EA 1998080700379 19980807 00379 WP 1998 8 7 UPS98827253 1 19980731 A 5230 146915 SOLENOID VALVE DOUG DC8 DC871F 302199D WP CARGO DOOR LEAKING A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 752UP 45952 INSPECTION TYPE-N/A BLOCK TURNBACK, CREW HAD SMOKE IN COCKPIT. FOUND HYD LEAK IN LWR E & E, SUSPECT MAIN CARGO DOOR CON TROL VALVE HYD SUPPLY LINE. FOUND UPPER CARGO DOOR SOLENOID VALVE TO BE LEAKING ONTO PNUEMATIC DUCT. REMOVED AND REPLA CED FWD UPPER CARGO DOOR SOLENOID SOV PER MM 52-36-00. 2 L 7 4 4F RT 4A25 1998080700380 19980807 00380 WP 1998 8 7 UPS98827254 1 19980719 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 283.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT WS XFS 283.250. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998080700381 19980807 00381 WP 1998 8 7 UPS98827255 1 19980718 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS I6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LT WING L/E LWR SURFACE CRACKED AT WS XOLDI 6.225 ON SKIN. REPAIRED IAW UPS EO 5720-4087 APPN C. 2 L 7 4 4F RT 4A25 1998080700382 19980807 00382 WP 1998 8 7 UPS98827256 1 19980720 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 822.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, RT WING L/E AT WS XFS 822.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-1. 2 L 7 4 4F RT 4A25 1998080700383 19980807 00383 WP 1998 8 7 UPS98827257 1 19980714 A 5320 3757794504 JAMB DOUG DC8 DC873F 302199F WP CARGO DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C-3, AFT CARGO STA 1160 FWD DOOR LWR JAMB HAS CORROSION. REMOVED FITTING, FOUND OUT OF LIMITS IAW DC8 S RM 53-2-0, REVEL NEW FITTING (P/N 3757794-504). LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-2 4. INSTALLED FITTING IA W DC8 SRM 51-1-200. 2 L 7 4 4F RT 4A25 1998080700384 19980807 00384 WP 1998 8 7 UPS98827258 1 19980721 A 5320 37592201 SPLICE DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LONG 33L SPLICE FITTING CRACKED FS 1260 TO 1280. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITT ING IAW SRM 51-1-21 AND DWG 3759220. 2 L 7 4 4F RT 4A25 1998080700385 19980807 00385 WP 1998 8 7 UPS98827259 1 19980720 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 341.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, RT WING L/E SKIN (LWR) AT WS XFS 341.5 HAS NUMEROUS CRACKS. REPAIRED IAW UPS EO DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 1998080700386 19980807 00386 WP 1998 8 7 UPS98827260 1 19980719 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 576.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER WS 576.75. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998080700387 19980807 00387 WP 1998 8 7 UPS98827261 1 19980724 A 5320 37502571N SPLICE DOUG DC8 DC871F 302199D WP BS 600-620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, FS 600 TO 620 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700388 19980807 00388 WP 1998 8 7 UPS98827262 1 19980721 A 5320 37502571N SPLICE DOUG DC8 DC871F 302199D WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LONG 31R SPLICE FITTING CRACKED FS 1040 TO 1060. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700389 19980807 00389 WP 1998 8 7 UPS98827263 1 19980719 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 697.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED WS XFS 697.5. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998080700390 19980807 00390 WP 1998 8 7 UPS98827264 1 19980718 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LT WING UPPER SKIN HAS 2 CRACKS JUST I/B OF WS XRS 74 FWD AND AFT LEG OF STR 11. REPAIRED IAW SRM 57 -3-1. 2 L 7 4 4F RT 4A25 1998080700391 19980807 00391 WP 1998 8 7 UPS98827267 1 19980713 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, SEAT TRACK D HAS AREAS OF CORR FROM 1240 TO 1400. REMOVED AND REPLACED SEAT TRACK IAW DC8 SRM 51- 1-8, 52-2-3, 51-3-0 FROM STA 1330 TO 1270. 2 L 7 4 4F RT 4A25 1998080700392 19980807 00392 WP 1998 8 7 UPS98827268 1 19980720 A 5320 3755843 FITTING DOUG DC8 DC873F 302199F WP BS 1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, LONG 35R AND 34R ZEE FITTING AT FS 1200 HAS CORROSION. REMOVED CORRODED FITTING, ALODINED AND PRI MED ZEE FITTING. INSTALLED FITTINGS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700393 19980807 00393 WP 1998 8 7 UPS98827269 1 19980713 A 5320 37558472 FITTING DOUG DC8 DC873F 302199F WP BS 1160 & 1228 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, REMOVE FITTING (P/N 36755847-2) TO FOM. REMOVED FITTING, FITTING FOUND TO BE CRACKED, RECEIVED AN D INSTALLED NEW FITTING IAW DC8-SRM 51-1-24. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700394 19980807 00394 WP 1998 8 7 UPS98827270 1 19980718 A 5320 37549301 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, NR 2 BACK-UP FITTING CORRODED. REMOVED FITTING, FABBED FITTING IAW DAC 3754930. TRIMMED FITTING IAW DC8 SRM 53-2-0 FIG 2D. DRILLED FITTING AND CLIPS TO FIT IAW DC8 SRM 5 1-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8 AND INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700395 19980807 00395 WP 1998 8 7 UPS98827271 1 19980714 A 5320 375404150IN FITTING DOUG DC8 DC873F 302199F WP BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, FITTING AT LONGERON 26L AT FS 320 CRACKED IN RADIUS AT CROSS SLIDE DOOR BUMPER STOP. REMOVED CRAC KED FITTING IAW DC8 SRM 51-1-20D. DRILLED AND LOCATED NEW FITTING IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700396 19980807 00396 WP 1998 8 7 UPS98827272 1 19980714 A 5320 56905201 FITTING DOUG DC8 DC873F 302199F WP BS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, LONG 26L AND STA 300 FITTING IS CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, RECEIVED, LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700397 19980807 00397 WP 1998 8 7 UPS98827273 1 19980710 A 5320 3755843IN FITTING DOUG DC8 DC873F 302199F WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, AFT PIT FWD DOOR TORQUE BOX FITTING IS CORRODED STA 1160 BETWEEN LONG 32R AND 33R. REMOVED FITTIN G, REVD FITTING, FABBED DOUBLERS AND CUT FITTING, ALODINED AND PRIMED AS REQUIRED IAW DC8 SRM 51-1-8, 55-2-0. INSTALLED IAW DC8 SRM 54-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998080700398 19980807 00398 WP 1998 8 7 UPS98827274 1 19980723 A 5320 3755841501 FITTING DOUG DC8 DC873F 302199F WP BS 1180 & 1200 REPAIRED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, 2 Z-FITTINGS AND STA 1180 AND 1200 L33R TO L34R INSTALLED NOT PER SRM. FABBED 2 501 FITTING IAW D AC DWG 3755841, LOCATED AND DRILLED FITTINGS IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FI TTING IAW DC8 SRM 53-2-0 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700399 19980807 00399 WP 1998 8 7 UPS98827275 1 19980712 A 5320 3648667 FITTING DOUG DC8 DC873F 302199F WP BS 55 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, STA 55 LONG 30 R HAS CORROSION EMITTING FROM DOME NUT. REMOVED CORRODED DOME NUT IAW DC8 SRM 51-1 -21. REMOVED CORROSION FROM L30 R AND STA 35. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED LONG 30R FS 8 TO FS 70. REMOVED INTERCOSTAL AND END FITTING L30R STA 8 TO 26 TO FOM RECEIVED LOCATED AND DRILLED LONG IAW DC8 SRM 51-1-24. AL ODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED LONG AND END FITTING IAW 51-1-21. 2 L 7 4 4F RT 4A25 1998080700400 19980807 00400 WP 1998 8 7 UPS98827276 1 19980713 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1152 & 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, REMOVE FITTING (P/N 3755847-1) TO FOM. REMOVED FITTING, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53- 2-0. RECEIVED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 3755847. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700401 19980807 00401 WP 1998 8 7 UPS98827277 1 19980713 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, LONG 33 R AND 34 R FS 1180 HAS TWO FITTING CRACKED. REMOVED FITTING, FABRICATED NEW DOUBLERS, ALO DINED AND PRIMED IAW DC8 S RM 51-1-8. INSTALLED DOUBLERS AND FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700402 19980807 00402 WP 1998 8 7 UPS98827278 1 19980710 A 5320 WEB DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, RT WW/ I/B FALSE SPAR AREA WEB CRACKED. FAB WEB IAW DOUGLAS DWG 5643117 ALODINED AND PRIMED IAW D C8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998080700403 19980807 00403 WP 1998 8 7 UPS98827279 1 19980710 A 5320 5894282502 FITTING DOUG DC8 DC873F 302199F WP BS 1168 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, AFT PIT FWD DOOR TORQUE BOX FITTING CRACKED AND CORRODED STA 1168 BETWEEN LONG 32R AND 33R. REMOV ED CRACKED AND CORRODED FAB BACK-UP FITTING ON PRINTED OP 50002 IAW DAC DWG 375493. RECVD REPAIR FITTING, DRILLED UP IA W DC8 SRM 51-1-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700404 19980807 00404 WP 1998 8 7 UPS98827280 1 19980710 A 5320 5894282501 FITTING DOUG DC8 DC873F 302199F WP BS 1200 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C CK, AFT LOWER CARGO AT STATION 1200, L32R FITTING CRACKED. REMOVED FITTING, FABBED FITTING, DRILLED F ITTING AND CLIPS TO FIT ALODINED, PRIMED AND INSTALLED. 2 L 7 4 4F RT 4A25 1998080700405 19980807 00405 WP 1998 8 7 MWEA98828 1 19980730 A 2560 591769037 SLIDE COVER DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 207ME 47794 THE GALLEY SLIDE COVER FELL OFF. MTC INSTALLED GALLEY DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998080700406 19980807 00406 WP 1998 8 7 MWEA98829 1 19980730 A 5330 59114123 SKIN DOUG DC9 DC914 3022034 WP BS 427 TORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 THE FUSELAGE SKIN IS TORN AT STATION 427 L26 AND L25. MTC FABRICATED AND INSTALLED NEW SKIN AND DOUBLER. 2 L 7 2 4F A6WE 1998080700407 19980807 00407 WP 1998 8 7 MWEA98830 1 19980730 A 5730 59559113 SKIN DOUG DC9 DC914 3022034 WP LT WING DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 600ME 45725 FOUND LEFT WING LOWER INBOARD FLAP AREA CONTACTING THE FUSELAGE SKIN. MTC REMOVED AND REPLACED SKIN. 2 L 7 2 4F A6WE 1998080700408 19980807 00408 WP 1998 8 7 DLL17981582 1 19980730 A 2910 31914920 O-RING LKHEED 1011 10113853 5265020 WP D-HYD SYST TORN A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 767DA 193H1209 UPON STARTING NR 3 ENGINE, EXPERIENCED RAPID LOSS OF 'D' SYSTEM HYDRAULIC FLUID. FOUND O-RING ON D-SYSTEM HYDRAULIC MUL E FITTING TORN, REF IPC 29-11-35 ITEM 85. REPLACED SAME. SERVICED AND LEAK CHECKED HYDRAULIC SYSTEM. OK FOR SERVICE. 2 L 7 3 4F A23WE 1998080700409 19980807 00409 WP 1998 8 7 DLL14981585 1 19980731 A 3510 OXYGEN BOTTLE 80137500 LKHEED 1011 1011385115 5265015 WP COCKPIT LEAKING A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 737D 255200 193C1228 COCKPIT OXYGEN BOTTLE PRESSURE READS ZERO PSI. REPLACED OXYGEN BOTTLE. LEAK CHECKED AT BOTTLE CONNECTIONS AND AT MASK, ALL OK. 2 L 7 3 4F A23WE 1998080700410 19980807 00410 NM 1998 8 7 DL733981588 1 19980801 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 400 GOUGED A DALA K NONE C F.O.D. IN INSP/MAINT 1 SO 27 951WP 22951 REPAIRED GOUGE ON FUSELAGE SKIN AT STA 400 BELOW STRINGER 19 LEFT PER SRM 53-00-01 FIG 210. 2 L 7 2 4F RT A16WE 1998080700411 19980807 00411 NM 1998 8 7 DL76L981589 1 19980801 A 3350 POWER SUPPLY BPS73 BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST LD LANDING 1 SO 27 172DN 6508 24775 DURING OVERWATER 2 CHECK, FOUND EMERGENCY PATH LIGHTS NEAR LT AND RT OVERWING EXITS INOP. REPLACED LT SIDE BATTERY AND POWER SUPPLY CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1998080700412 19980807 00412 NM 1998 8 7 DLM88981591 1 19980802 A 2910 HYD LINE DOUG MD88 MD88 3023688 NM NR 2 ENGINE CHAFED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 980DL 53267 000000 ON DEPARTURE, FELT VIBRATION FOLLOWED BY RT SYS HYD FAILURE. FOUND HYD PRESS LINE CHAFED NR 2 ENG PYLON. REPLACED LINE , INSPECTED AND REPLACED NR 2 ENG HYD PUMP FILTERS. RAN ENG PER PFHB, NO LEAKS FOUND. NR 2 ENG HYD PUMP CKS OK. 2 L 7 2 4F RT A6WE 1998080700413 19980807 00413 NE 1998 8 7 SCNA98084 2 19980729 A 7320 POWER STOP BOEING 727 727259 138408J NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE NOT STOWED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 15 289SC 22475 DURING TAKEOFF ROLL FOLLOWING A MAINTENANCE CHECK, THE AIRCRAFT WOULD NOT REACH TAKEOFF POWER ON THE NUMBER THREE ENGINE . FOUND THE PART POWER STOP IN THE PART POWER STOP POSITION. STOWED AND SAFETIED THE PART POWER STOP. ENGINE OPERATIO NALLY CHECKS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998080700414 19980807 00414 NM 1998 8 7 SCNA98085 1 19980730 A 2782 1U11032 ACTUATOR BOEING 727 727259 138408J NM NR 5 LE SLAT FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 289SC 10088 22475 DURING CLIMB, THE NUMBER FIVE LEADING EDGE SLAT AND THE NUMBER SIX LEADING EDGE FLAP WOULD NOT RETRACT. REMOVED AND REP LACED THE NUMBER FIVE LEADING EDGE SLAT ACTUATOR PER MAINTENANCE MANUAL 278132 AND INSTALLED A NUMBER SIX LEADING EDGE F LAP INDICATION EMERGENCY HARNESS PER 2788201. 2 L 7 3 4F A3WE 1998080700415 19980807 00415 NM 1998 8 7 SCNA98086 1 19980721 A 7711 2045051 EPR INDICATOR BOEING 727 7272J4 1384006 NM NR 1 ENGINE INOPERATIVE A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 15 284SC 7262 21438 ON TAKEOFF ROLL, THE NUMBER ONE ENGINE WOULD NOT DEVELOP MORE THAN 1.60 EPR. OTHER INDICATIONS WERE CONSISTENT WITH LOW POWER. ABORTED THE TAKEOFF AT 90 KNOTS. REMOVED AND REPLACED THE EPR INDICATOR. RAN ENGINE AND ALL INDICATIONS NORMA L. 2 L 7 3 4F RT A3WE 1998080700416 19980807 00416 WP 1998 8 7 RRXA98317 1 19980618 A 5311 5615753573 FRAME DOUG DC8 DC862 3021970 WP BS 620 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 620 AND LONGERON 21 LEFT. 2 L 7 4 4F 4A25 1998080700417 19980807 00417 WP 1998 8 7 RRXA98318 1 19980618 A 5311 5610416519 FRAME DOUG DC8 DC862 3021970 WP BS 640 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 21 LEFT. 2 L 7 4 4F 4A25 1998080700418 19980807 00418 WP 1998 8 7 RRXA98319 1 19980618 A 5311 5615754515 FRAME DOUG DC8 DC862 3021970 WP BS 660 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 660 AND LONGERON 21 LEFT. 2 L 7 4 4F 4A25 1998080700419 19980807 00419 WP 1998 8 7 RRXA98320 1 19980618 A 5311 5750129501 FRAME DOUG DC8 DC862 3021970 WP BS 759 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 759 BETWEEN LONGERONS 19 LEFT TO 20 LEFT. 2 L 7 4 4F 4A25 1998080700420 19980807 00420 WP 1998 8 7 RRXA98321 1 19980625 A 5311 5642861503 FRAME DOUG DC8 DC862 3021970 WP BS 834 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 834 AND LONGERON 15 RIGHT. 2 L 7 4 4F 4A25 1998080700421 19980807 00421 WP 1998 8 7 RRXA98322 1 19980624 A 5311 5754002501 FRAME DOUG DC8 DC862 3021970 WP BS 560 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 560 BETWEEN LONGERONS 7 LEFT TO 8 LEFT. 2 L 7 4 4F 4A25 1998080700422 19980807 00422 WP 1998 8 7 RRXA98323 1 19980624 A 5311 57544271 FRAME DOUG DC8 DC862 3021970 WP BS 580 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLE, AT STA 580 AND LONGERON 9 LEFT. 2 L 7 4 4F 4A25 1998080700423 19980807 00423 WP 1998 8 7 RRXA98324 1 19980624 A 5311 5613466505 FRAME DOUG DC8 DC862 3021970 WP BS 640 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 7 LEFT. 2 L 7 4 4F 4A25 1998080700424 19980807 00424 WP 1998 8 7 RRXA98325 1 19980624 A 5311 5610049 FRAME DOUG DC8 DC862 3021970 WP BS 270 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 270 BETWEEN LONGERONS 12 RIGHT TO 14 RIGH T. 2 L 7 4 4F 4A25 1998080700426 19980807 00426 WP 1998 8 7 RRXA98327 1 19980624 A 5311 5615749523 FRAME DOUG DC8 DC862 3021970 WP BS 420 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 420 BETWEEN LONGERONS 7 RIGHT TO 8 RIGHT. 2 L 7 4 4F 4A25 1998080700427 19980807 00427 WP 1998 8 7 RRXA98328 1 19980624 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 440 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 440 AND LONGERON 16 RIGHT. 2 L 7 4 4F 4A25 1998080700428 19980807 00428 WP 1998 8 7 RRXA98329 1 19980624 A 5311 5642859507 FRAME DOUG DC8 DC862 3021970 WP BS 822 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 822 AND LONGERON 3 LEFT. 2 L 7 4 4F 4A25 1998080700429 19980807 00429 WP 1998 8 7 RRXA98330 1 19980618 A 5311 57511111 FRAME DOUG DC8 DC862 3021970 WP BS 520 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 520 AND LONGERON 21 LEFT. 2 L 7 4 4F 4A25 1998080700430 19980807 00430 WP 1998 8 7 RRXA98331 1 19980618 A 5311 5751121 FRAME DOUG DC8 DC862 3021970 WP BS 540 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 540 AND LONGERON 21 LEFT. 2 L 7 4 4F 4A25 1998080700431 19980807 00431 WP 1998 8 7 RRXA98332 1 19980618 A 5311 5754002501 FRAME DOUG DC8 DC862 3021970 WP BS 560 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 560 AND LONGERON 21 LEFT. 2 L 7 4 4F 4A25 1998080700432 19980807 00432 NE 1998 8 7 VNAA9807012 2 19980730 A 7532 311671504 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 426JS 61194 3038 116162 DURING THE TAXI OUT, THE AIRCRAFT RETURNED TO THE GATE ON TWO OCCASIONS FOR ECU FAIL WARNING MESSAGES. THE FIRST GATE R ETURN, MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND 1.8 SENSOR, (P/N 8720194), AND THE LEFT HAND NP SENSOR, (P/N 87 20190). OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. THE FLIGHT RETURNED TO THE GA TE WITH ANOTHER ECU FAIL INDICATION. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND INTERCOMPRESSOR BLEED VALVE, IN A CCORDANCE WITH DORNIER MAINTENANCE MANUAL 75-31-01. OPERATION CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998080700433 19980807 00433 NM 1998 8 7 VNAA9807013 1 19980729 A 3233 2412500000 ACTUATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT MLG FAILED A VNAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 07 328JS 86114 3030 WHEN THE LANDING GEAR WAS SELECTED DOWN DURING APPROACH, THE RT MAIN GEAR UNLOCK LIGHT REMAINED ILLUMINATED. THE ACFT C LIMBED TO 8000 FT AND MADE ANOTHER ATTEMPT TO EXTEND THE GEAR. THE LANDING GEAR EXTENDED AND A NORMAL LANDING WAS MADE. MX INSPECTED AND APPROVED THE ACFT FOR A GEAR DOWN FERRY FLIGHT TO PIT. THE FERRY FLIGHT WAS CARRIED OUT WITHOUT ANY PROBLEMS. MX INSPECTED AND REPLACED THE LANDING GEAR SELECTOR VALVE, (P/N HP848800-1), THE RT MAIN GEAR ACTUATING CYLIN DER, (P/N 24125-000-00) AND THE RT DOWN LOCK ASSIST ACTUATOR, (P/N 22455-000-00). ABOVE PARTS TIMES WERE FHR: 8611.4 C YCLES: 8202. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998080700434 19980807 00434 NE 1998 8 7 USAAD98084 2 19980509 A 7261 11738701 SEAL SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENG GEARBOX LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 111PX 340A024 MCO-SYR - FLT 2226 - AFTER ONE HOUR OF FLT, THE RIGHT ENGINE OIL QTY BEGAN TO DROP FROM 16 QUARTS. THE OIL QUANTITY DRO PPED APPROXIMATELY 1 QT PER 10 MINUTES AT CRUISE POWER. ALL OTHER ENGINE GAUGES WERE NORMAL. THE FLT DIVERTED TO ORF. DURING FLT IDLE DESCENT THERE WAS NO NOTICEABLE OIL LOSS. THE FLT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE R IGHT ENGINE CSD GARLOCK SEAL. DURING ENGINE RUN THE OIL QTY REMAINED NORMAL. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998080700435 19980807 00435 NE 1998 8 7 AALA980939 2 19980510 A 7320 11337701 SEAL BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A AALA E ENGINE SHUTDOWN K X FLUID LOSS ENGINE FLAMEOUT CR CRUISE 1 SW 07 863AA 21090 DFW - FLT 795 - DURING CRUISE, EN ROUTE STL-DFW NR 1 ENGINE REQUIRED 1500 LBS MORE FUEL FLOW THAN NR 2 AND 3 ENGINES TO MAINTAIN CRUISE POWER. NR 1 ENGINE WENT TO IDLE AND THAN FLAMED OUT. LANDED DFW WITHOUT INCIDENT. REPLACED SEAL TO P AND D VALVE. ACCOMPLISHED ENGINE RUN-UP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998080700436 19980807 00436 GL 1998 8 7 ZIAA98002 2 19980118 A 7200 ENGINE LKHEED 188 188C 5262604 SO ALLSN 501D 501D13 03004 GL NR 1 FAILED A ZIAA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 23 286F 188C1146 CYYT - UPON APPROACH INTO CYYT, NR 1 ENIGNE RPM DECAYED TO ZERO, PULLED SHUTDOWN HANDLE. MAINTENANCE INSPECTION REVEALE D NR 1 ENGINE APPEARS TO BE DE-COUPLED. AIRCRAFT THREE ENGINED FERRIED TO YIP, FOR NR 1 ENGINE REPLACEMENT. ENGINE WAS REPLACED ON 1-28-98 IAW ZIAA L-188 MIP ONE-120. (M) 2 L 7 4 4T 4 T 4A22 E282 1998080700437 19980807 00437 NE 1998 8 7 PLGA980505A 2 19980505 A 7320 CONNECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE FUEL CONTL DIRTY A PLGA K NONE N FALSE WARNING CR CRUISE 1 NE 05 366BE 340B303 BOS - FLT 4366 - WHILE AT CRUISE, CREW REPORTED A TORQUE SURGE AND N1 FLUCTUATION ON LEFT ENIGNE WHILE ALL OTHER ENGINE PARAMETERS WERE NORMAL. ENGINE WAS PUT IN TORQUE MOTOR LOCKOUT AND AIRCRAFT CONTINUED TO BOS AND LANDED WITHOUT INCIDEN T. MAINTENANCE CLEANED ELECTRICAL CONNECTOR 162UP ON FIREWALL AND CONNECTOR FOR FORWARD NP SENSOR. ENGINE WAS GROUND R UN WITH NO PROBLEMS FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998080700438 19980807 00438 NE 1998 8 7 98ZZZM534 2 19980514 A 7314 043890425 PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 858CA UE72 LEFT ENGINE FUEL LEAK NOTED. LEFT ENGINE LOW PRESURE PUMP LEAKING. REPLACED LT ENGINE LOW PRESSURE FUEL PUMP. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1998080700439 19980807 00439 NE 1998 8 7 98ZZZM535 2 19980506 A 7314 1143890425 FUEL PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE LEAING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 858CA UE72 FUEL LEAK UNDER LT COWL. FUEL PUMP LEAKING. REMOVED AND REPLACED FUEL PUMP. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1998080700440 19980807 00440 NE 1998 8 7 98ZZZM536 2 19980515 A 7314 1143890425 FUEL PUMP BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 855CA UE61 LEFT GEAR DOORS SHOW SIGNS OF FLUID LEAKAGE. LEFT ENGINE DRIVEN FUEL PUMP LEAKING. REPLACED LT ENGINE DRIVEN FUEL PUMP P/N 114-389042-5 IAW CHP 71 BEECH MM. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1998080700441 19980807 00441 NE 1998 8 7 MZZA98162 2 19980603 A 7320 451077 PS4 LINE BOEING 727 727224 1384076 NM PWA JT8 JT8* 52044 NE NR 2 ENGINE RUPTURED A MZZA A J UNSCHED LANDING DUMP FUEL M R J OVER TEMP PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 13 79743 22252 FLT 956 - KSA - DURING STAGE 2 CLIMB SEGMENT AT POWER REDUCTION TO CLIMB POWER, EPR DROPPED .30, FUEL FLOW DROPPED TO 10 00 PPH, AND EGT ROSE TO NEAR REDLINE. AIR RETURN TO KSA. MAINTENANCE FOUND PRBC PS-4 LINE LEAKS 1PC 75-30-0-1, ITEM 30 PG-0/FIG-1. REMOVED AND REPLACE PS-4 LINE WITH SERVICEABLE LINE. REMOVED AND REPLACED P AND D VALVE FOR PRECAUTIONARY PER MM 73-12-1. AIRCRAFT RELEASED FOR SERVICE AND NO FURTHER INCIDENT. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998080700442 19980807 00442 NE 1998 8 7 P2EA98104 2 19980507 A 7230 633731A4434 COVER BOEING 737 737244 138448U NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE CRACKED A P2EA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 620PC 19708 FLT 804 - MDW - NO EMERGENCY DECLARED LANDING NORMAL. GOT HAZY VAPOR IN CABIN DURING FLIGHT. FOUND NR 1 BEARING ACCESS ORY COVER CRACKED ON NR 1 ENGINE, REPLACED COVER PER PWA M/M 72-23. PERFORMED ENGINE RUN NO LEAKS OR HAZE NOTED. (M) 2 L 7 2 4F 4 F A16WE E2GL 1998080700443 19980807 00443 NE 1998 8 7 ORJA9889 2 19980505 A 7320 FUEL CONTROL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RT ENGINE MALFUNCTIONED A ORJA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 WP 11 822RA 49932 ENGINE SHUT DOWN DUE TO THE FACT THAT THE RIGHT ENIGNE WOULD NOT IDLE BELOW 68 PERCENT N2. ENTERED DMI NR 13546. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998080700444 19980807 00444 NE 1998 8 7 REXA98089 2 19980418 A 7530 6058T80P03 AIR VALVE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LEFT INOP A REXA K NONE J WARNING INDICATION CL CLIMB 1 SO 25 111PX 340A024 LEFT AIR VALVE LIGHT ILLUMINATED DURING CLIMB-OUT. REMOVED AND REPLACED LEFT HAND ASIBV. GROUND RUN CHECKS GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998080700445 19980807 00445 WP 1998 8 7 VTZA98175 2 19980428 A 7314 8974007 FUEL PUMP BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 473UE 828 FLT 6531 - IAD-ORF - DURING CRUISE, MADE A UNSCHEDULED LANDING AT IAD DUE TO RT FUEL PSI LOW. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS MAINTENANCE INSPECTED AND REMOVED AND REPLACED FUEL PUMP. OPS CHECK OK. AIRCRAFT WAS RELEASE D AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A21EU E3WE 1998080700446 19980807 00446 NE 1998 8 7 P2EA98107 2 19980516 A 7200 ENGINE BOEING 737 737281 138448P NM GE CFM56 CFM56* 13802 NE NR 2 OVERTEMP A P2EA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 CE 05 219US 20414 FLT 823 - ON TAKEOFF FROM MCI, THE NR 2 ENGINE EGT RAN HOT. PERFORMED WATER WASH ON NR 2 ENGINE PER AMM 71-00-PG 703D, VISUALLY INSPECTED WIRING REF 77-21-0, OPERATED NR 2 ENGINE AT TAKEOFF POWER MAX EGT NOTED WAS 570 DEGREES, MAX ALLOWABL E EGT IS 590 DEGREE REF AMM 71-09-100 PAGE 218G, 71-09-226 PG 209. (M) 2 L 7 2 4F 4 F A16WE E2GL 1998080700447 19980807 00447 NE 1998 8 7 USAASB98107 2 19980505 A 7260 717000 N2 GEARBOX BOEING 737 737201 1384454 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K M J FLUID LOSS OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 241US 19595 22443 BWI - FLT 2400 - CREW DECLARED AN EMERGENCY AND SHUT DOWN THE NR 1 ENGINE IN FLT DUE TO LOSS OF OIL QTY AND PRESSURE AND TEMPERATURE INDICATIONS. FLT RETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. AIRCRAFT TAXIED TO THE GAT E NORMALLY. TOTAL SINGLE ENGINE TIME WAS 14 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE N2 GEARBOX ASSY. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2GL 1998080700448 19980807 00448 NE 1998 8 7 AALA981025 2 19980524 A 7321 7696068 FUEL CONTROL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE FAILED A AALA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION AP APPROACH 1 SW 07 7517A A3051 49894 LAX - FLT 7 - DURING FINAL APPROACH LAX AT 5,000 FEET, THROTTLES WERE RETARDED AND RIGHT ENGINE SHUT DOWN IN FLT. FLIGH T CREW ACCOMPLISHED ENGINE OUT PROCEDURES AND LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED RIGHT ENGINE FUEL CONTROL U NIT AND AS A PRECAUTIONARY, REPLACED RIGHT ENGINE FUEL PUMP. RIGGED RIGHT ENGINE FUEL CONTROL UNIT PER PROCEDURES. RIG HT ENGINE WAS GROUND RUN AT VARIOUS POWER SETTINGS WITH NO LEAKS OR UNCOMMANDED SHUT DOWNS. SYSTEM GROUND CHECKED NORMA L OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998080700449 19980807 00449 WP 1998 8 7 RAIA980514 2 19980518 A 7261 31058703 PUMP JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A RAIA E A ENGINE SHUTDOWN UNSCHED LANDING K J Y FLUID LOSS WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 CE 03 569HK 4422 41088 FLT 7796 - PIT - RIGHT ENGINE OIL PRESSURE FLUCTUATING, LOW OIL PRESSURE CAPTION ILLUMINATED. CREW PERFORMED ENGINE SHU TDOWN. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE DRIVEN OIL PUMP ASSY. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1998080700450 19980807 00450 WP 1998 8 7 USAAD98113 1 19980623 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 921VJ 48141 IND - THE CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE CEILING EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998080700451 19980807 00451 SO 1998 8 7 C2XA98CL048 1 19980629 A 7540 M1160140242 SENSOR EMB 120 EMB120RT SO LT WING MALFUNCTIONED A C2XA K NONE N FALSE WARNING AP APPROACH 1 SW 09 17728 120182 GRR - FLT 3069 - CREW REPORTED THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED DURING APPROACH, ALOS THE LIGHT WOULD NOT EXT INGUISH ON THE GROUND. AIRCRAFT WAS MAINTENANCE FERRIED TO CLE AND THE LEFT WING/FUSELAGE FAIRING DUCT LEAK SENSOR WS R EMOVED AND REPLACED IAW EMB-120 MM 36-20-01. OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB-120MM 36-20-00. AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700452 19980807 00452 WP 1998 8 7 AALA981152 1 19980608 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1176-1309 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 428AA 49340 TUL - FOUND CORROSION ON SEAT TRACK. REPLACED TRACK. (M) 2 L 7 2 4F A6WE 1998080700453 19980807 00453 WP 1998 8 7 AALA981124 1 19980602 A 2550 ROLLER TRAY DOUG DC10 DC1030 3023501 WP BS 1666 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION IN ROLLER TRAY NR 1 AT ROLLER BRAKE LOCATION STATION 1666. REMOVED AND REPLACED NR 1 ROLLER TRAY FROM STATION 1621 TO STATION 1781 PER SRM 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998080700454 19980807 00454 WP 1998 8 7 AALA981122 1 19980603 A 5320 TIE DOWN DOUG DC10 DC1030 3023501 WP BS 840-860 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION AT AFT GALLEY TIE DOWN LUGS. NEW SECTION INSTALLED PER ESO 7349, DATED 5/28/98. (M) 2 L 7 3 4F A22WE 1998080700455 19980807 00455 WP 1998 8 7 AALA981121 1 19980603 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 433 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSIN ON LOWER WING SKIN AROUND CASTNER AT REAR SPAR NEAR STATION XORS 433. REPAIRED PER ESO 7349, DATED 6-2-98. (M) 2 L 7 3 4F A22WE 1998080700456 19980807 00456 WP 1998 8 7 AALA981156 1 19980606 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1997 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FRAME ANGLE AFT SIDE OF FRAME 1997 HAS HEAVY CORROSION BETWEEN LONGER 47L AND 48R. SPLICED IN NEW SECTION OF 'J' ANGLE PER SRM 53-30-00 VOL 11. (M) 2 L 7 3 4F A22WE 1998080700457 19980807 00457 WP 1998 8 7 AALA981155 1 19980606 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FRAME AT STATION 1841 BETWEEN LONGER 43L AND 42L HAS CORROSION. INSTALLED REPAIR AFTER CORROSION REMOVAL, PER SRM 53-30-00 PAGE 14. (M) 2 L 7 3 4F A22WE 1998080700458 19980807 00458 WP 1998 8 7 AALA981154 1 19980606 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1997-2005 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FUSELAGE BELLY SKIN HAS CORROSION 2 PLACES ON SIDES OF LONGERON 44L STATION 2000 TO 2005. REPAIRED AREA PER ESO 7 349, DATED 05/28/98 AND SRM 51-21-01 VOL 2. (M) 2 L 7 3 4F A22WE 1998080700459 19980807 00459 WP 1998 8 7 AALA981149 1 19980509 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1868 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION ON FUSELAGE SKIN UNDER L48L STATION 1868 STRINGER 48L. INSTALLED EXTERNAL REPAIR DOUBLER PER ESO 7349, DATED 6/1/98. (M) 2 L 7 3 4F A22WE 1998080700460 19980807 00460 WP 1998 8 7 AALA981137 1 19980605 A 5320 SHEAR TIE DOUG DC10 DC1030 3023501 WP BS 1967 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - SHEAR TIE IS ONE PIECE FROM 47L-47R EACH TIE TO SKIN HAS CORROSION. REMOVED AND REPLACED SHEAR TIE STRIP PER AARD 51-01-00-05. (M) 2 L 7 3 4F A22WE 1998080700461 19980807 00461 WP 1998 8 7 AALA981138 1 19980605 A 3211 TRUNNION DOUG DC10 DC1030 3023501 WP BS 1461 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND CORROSION ON LEFT AND RT AFT TRUNNION BOLT SPOT FACE SURFACES, TOP SIDES. REMOVED CORROSION, CASTING BEYOND LIMITS. REPAIRED PER ESO 7349, DATE 6-5-98. (M) 2 L 7 3 4F A22WE 1998080700462 19980807 00462 WP 1998 8 7 AALA981132 1 19980604 A 5320 SPLICE DOUG DC10 DC1030 3023501 WP BS 1853 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FOUND LONGERON SPLICE FITTING CORRODED BETWEEN STATION 1853-1871 AT LONGERON 48L. SPLICED IN NEW SECTION OF LONGE RON PER SRM 53-10-00 PAGE 9. (M) 2 L 7 3 4F A22WE 1998080700463 19980807 00463 NM 1998 8 7 AALA981146 1 19980606 A 5330 SKIN BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - STATION 950F STRINGER 28R BELLY SKIN HAS CORROSION. INSTALLED SKIN REPAIR PER ESO 11697, DATED 5-11-98. (M) 2 L 7 3 4F A3WE 1998080700464 19980807 00464 NM 1998 8 7 AALA981147 1 19980606 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 877AA 21389 TUL - OUTBOARD SIDE OF STRINGER 28R IS CORRODED STATION 950F TO 970. REPAIRED STRINGER PER ESO 11697, DATED 5-11-98. ( M) 2 L 7 3 4F A3WE 1998080700465 19980807 00465 NM 1998 8 7 AALA984134 1 19980604 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 373AA 25200 AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE UPPER CAP OF FLOORBEAM. THE BLENDOUT EXCEEDED SRM MAX ALLOWABLE LIMITS. ALODINED BLENDOUT. FABRICATED AND INSTALLED REPAIR STRAP USING .050 301.5 HARD STAINLESS STEEL. FI LLED AND PRIMED AS REQUIRED. APPROVED BY ENGINEERING PER MRB 767-1647. (M) 2 L 7 2 4F RT A1NM 1998080700466 19980807 00466 SO 1998 8 7 C2XA98IA211 1 19980617 A 3350 3011151 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE FORWARD FLOOR EMERGENCY LIGHTS FAILED TO ILLUMINATE. MAINTENANCE REMOVED AND REPLA CED THE EMERGENCY LIGHT BATTERY PACK FOR THE AFFECTED LIGHTS IAW EMB120 MM CH 33-50-02, AND THE AIRCRAFT WAS APPROVED FO R RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700467 19980807 00467 SO 1998 8 7 C2XA98IA210 1 19980617 A 5320 12006159501 CREASE BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 39 AND 44. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700468 19980807 00468 SO 1998 8 7 C2XA98IA209 1 19980617 A 5320 12006158003 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP WAS FOUND TO BE CORRODED BETWEEN FRAMES 38-44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700469 19980807 00469 SO 1998 8 7 C2XA98IA208 1 19980617 A 5320 12027929003 BUTTSTRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP BETWEEN FRAMES 34 AND 38 WAS FOUND TO BE CORRODED. MAINTENA NCE REMOVED AND REPLACED THE EFFECTED SECTION OF BUTTSTRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RE TURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700470 19980807 00470 SO 1998 8 7 C2XA98IA207 1 19980617 A 5320 12005779001 T-PROFILE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 40 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE EFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700471 19980807 00471 SO 1998 8 7 C2XA98IA206 1 19980617 A 5320 12004149001 TEE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE T-PROFILE AT FRAME 38 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE EFFECTED T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700472 19980807 00472 SO 1998 8 7 C2XA98IA205 1 19980617 A 5347 12026864607 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMVOED AND REPLA CED THE EFFECTED SEAT TRACK IAW EMBL-120 SRM 51-21-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700473 19980807 00473 SO 1998 8 7 C2XA98IA204 1 19980617 A 5720 12004342008 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING NUMBER TWO UPPER SKIN SUPPORT AT RIB 21 WAS FOUND TO BE CRACKED. MAINTE NANCE REMOVED AND REPLACED THE EFFECTED SKIN SUPPORT IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700474 19980807 00474 SO 1998 8 7 C2XA98IA200 1 19980617 A 5530 12015374601 ANGLE EMB 120 EMB120RT SO VERT STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE LEFT DRAG ANGLE ON THE VERTICLE STABILIZER WAS FOUND TO BE CRACKED. MAINTENANCE RE MOVED THE DAMAGED SECTION OF THE DRAG ANGLE AND INSTALLED A REPAIR SPLICE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5530-01013, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700475 19980807 00475 SO 1998 8 7 C2XA98IA198 1 19980617 A 5320 12022670001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLE D THE CRACK AND INSTALLED A DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700476 19980807 00476 SO 1998 8 7 C2XA98IA199 1 19980617 A 5320 12022670002 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 47722 120166 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILL ED THE CRACK AND INSTALLED A DOUBLER REPAIR IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1998080700477 19980807 00477 EU 1998 8 7 C2XA98BT040 1 19980610 A 3350 3011180A BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 21837 202 BTV - DURING 1A INSPECTION, FOUND EMERGENCY LIGHTS FORWARD BATTERY PACK INOP. FORWARD EXIT AND HALF OF FWD FLOOR LIGHTS INOP. REMOVED AND REPLACED FWD AND MID PWR SUPPLY, IAW ATR 42 MM 33-50-00. OPS CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998080700478 19980807 00478 EU 1998 8 7 C2XA98IA197 1 19980610 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14829 181 IAH - DURIGN 'A' CHECK INSPECTION, THE EMERGENCY LIGHT BATTERY PACK AT 29WL WOULD NOT ILLUMINATE ITS ASSOCIATED EMERGENC Y LIGHTS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW ATR-42 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998080700479 19980807 00479 EU 1998 8 7 C2XA98IA196 1 19980610 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14829 181 IAH - DURING 'A' CHECK INSPECTION, THE EMERGENCY BATTERY AT LOCATION 3WL FAILED TO ILLUMINATE ITS ASSOCIATED EMERGENCY L IGHTS. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998080700480 19980807 00480 NE 1998 8 7 C2XA98IA202 2 19980616 A 7200 310440001 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 SEIZED A C2XA K NONE J Y WARNING INDICATION ENGINE STOPPAGE AP APPROACH 1 SW 09 93840 271 PCE120526 IAH - DURING APPROACH ON FLT 401A, THE PILOT REPORTED THE NR 2 ENGINE SEIZED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDE NT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998080700481 19980807 00481 SO 1998 8 7 C2XA98IA201 1 19980614 A 2611 FAU751A3 SMOKE DETECTOR EMB 120 EMB120RT SO CABIN MALFUNCTIONED A C2XA K NONE N FALSE WARNING CR CRUISE 1 SW 09 16723 120169 IAH - DURING FLT 3952 - THE CREW REPORTED A FALSE LAVATORY SMOKE INDICATION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDEN T WHERE MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR PANEL AND THE AIRCRAFT WAS APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700482 19980807 00482 SO 1998 8 7 C2XA98IA203 1 19980614 A 3350 FD2A250V1A FUSE EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59708 120098 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHTS AT ROW 6 WOULD NOT ILLUMINATE. MAIN TENANCE REMOVED AND REPLACED THE AFFECTED FUSE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700483 19980807 00483 SO 1998 8 7 C2XA98CL043 1 19980601 A 2121 EVAC2322C2 COOLING FAN EMB 120 EMB120RT SO RT A/C BAY FAILED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 17728 15690 596 120182 CLE - FLT 3204 - CREW REPORTED THAT DURING TAXI OUT THEY OBSERVED SMOKE IN THE COCKPIT AND CABIN, AIRCRAFT RETURNED TO T HE GATE WITHOUT FURTER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE RIGHT GROUND COOLING FAN IAW EMB-120 MM 21-51-03. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700484 19980807 00484 SO 1998 8 7 C2XA98CL045 1 19980608 A 2150 17185613 HOSE EMB 120 EMB120RT SO RT ACM RUPTURED A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 15713 120114 CLE - FLT 3079 - CREW REPORTED THAT THE COCKPIT AND CABIN FILLED WITH SMOKE DURING TAXI OUT, AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED A BLOWN HOSE AND CLEANED OIL FROM THE RIGHT ACM. OPERATIONAL AND LEAK CHECKS WERE SAT ISFACTORY IAW EMB-120 MM 21-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998080700485 19980807 00485 NM 1998 8 7 USAABB98061 1 19980603 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 LAX - FOUND EMERGENCY LIGHTS INOPERATIVE AT ROWS 1, 4 AND 6. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998080700486 19980807 00486 NM 1998 8 7 USAABB98062 1 19980603 A 3350 873100151REV9 LIGHT BOEING 757 7572B7 1384964 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 LAX - FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 23. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998080700487 19980807 00487 NM 1998 8 7 USAASB98139 1 19980603 A 2120 AIR DISTRIBUTION BOEING 737 737401 1384701 NM CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 406US 23876 CHA - FLT 598 - AT FL 350, APPROX 60 MILES EAST OF CHA, FLT ATTENDANT IN AFT CABIN CALLED FLT CREW TO INFORM THEM OF A B URNING TYPE DOOR. FIRST OFFICER PROCEEDED TO REAR OF CABIN AND CONFIRMED ODOR. ODOR WAS SIMILAR TO AN ELECTRICAL TYPE FIRE BUT NO SMOKE OR FIRE WAS PRESENT. ODOR SPREAD THROUGHOUT CABIN AND INTO COCKPIT. CAPTAIN DECLARED AN EMERGENCY AN D DIVERTED INTO CHA WITHOUT INCIDENT. A/C TAXIED TO GATE AND PASSENGERS WERE DEPLANED. MX INSPECTED COCKPIT, CABIN, CA RGO BINS, E/E COMPT AND CABIN LIGHTING AND FOUND NO DISCREPANCIES. RAN BOTH ENGINES AND PACKS. NO DISCREPANCIES NOTED. COULD NOT DUPLICATE ODOR. (M) 2 L 7 2 4F RT A16WE 1998080700488 19980807 00488 WP 1998 8 7 MWEA98637 1 19980603 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP GALLEY DR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 502ME 48132 MKE - FLT 712 - THE GALLEY DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY DOOR SLIDE COVER. (M) 2 L 7 2 4F A6WE 1998080700489 19980807 00489 WP 1998 8 7 MWEA98638 1 19980602 A 2913 AS66411L5666 HYD PUMP DOUG DC9 DC914 3022034 WP LT ENGINE INOPERATIVE A MWEA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CR CRUISE 1 GL 31 700ME MX196217R 45696 MKE - FLT 527 - THE LEFT HYDRAULIC PRESSURE WENT TO ZERO WITH PUMP ON HIGH OR LOW. MAINTENANCE REMOVED AND REPLACED LEF T ENGINE DRIVEN HYDRAULIC PUMP. (M) 2 L 7 2 4F A6WE 1998080700490 19980807 00490 WP 1998 8 7 TWAA9808601 1 19980529 A 2120 AIR DISTRIBUTION DOUG DC9 DC983 3022083 WP CABIN ODOR A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 9619V 53566 ABQ - FLT 649 - STRONG ELECTRICAL BURNING SMELL IN AREA OF CABIN ROW 5, ABOVE RT SEATS. REMOVED PANELS AND THOROUGHLY I NSPECTED AREA FROM ROW 1 THROUGH 8. NO DEFECT NOTED. (M) 2 L 7 2 4F RT A6WE 1998080700491 19980807 00491 WP 1998 8 7 TWAA9808602 1 19980529 A 3320 B615 BALLAST DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 9619V 53566 STL - FLT 572 - ELECTRICAL FUMES AND SMOKE CAME FROM SIDE WALL LIGHT AREA ABOVE CABIN ROW 5, RT SEATS. ON LANDING SIDE WALL LIGHTS FLICKERED THEN WENT OUT. REPLACED LIGHT SOCKET AT FWD FLOURESCENT LAMP, AFT POSITION, AND REPLACED LIGHT BA LLAST. BALLAST MFG B6-15. (M) 2 L 7 2 4F RT A6WE 1998080700492 19980807 00492 WP 1998 8 7 98ZZZM537 1 19980529 A 3320 D77311001 SOCKET DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 9619V 53566 STL - FLT 572 - ELECTRICAL FUMES AND SMOKE CAME FROM SIDE WALL LIGHT AREA ABOVE CABIN ROW 5, RT SEATS. ON LANDING SIDE WALL LIGHTS FLICKERED THEN WENT OUT. REPLACED LIGHT SOCKET AT FWD FLOURESCENT LAMP, AFT POSITION, AND REPLACED LIGHT BA LLAST. BALLAST MFG B6-15. (M) 2 L 7 2 4F RT A6WE 1998080700493 19980807 00493 WP 1998 8 7 TWAA9808603 1 19980529 A 3350 58222 BATTERY PACK DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 491SA 45799 STL - FLT 404 - EMERGENCY EXIT SIGNS AT R1 AND L1 DOORS CAME ON IN FLIGHT. WOULD NOT RESET UNTIL SHORT FINAL. REPLACED FWD EMERGENCY EXIT SIGN BATTERY PACK. (M) 2 L 7 2 4F A6WE 1998080700494 19980807 00494 WP 1998 8 7 TWAA9808604 1 19980522 A 5320 PRESSURE DECK DOUG DC9 DC933F 302207A WP BS 82 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 937F 47409 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION AND MISSING FASTENERS AT A PREVIOUS REPAIR TO PRESSURE DECK, STATI ON 82 RBL 20. REMOVED PREVIOUS REPAIR, CUT OUT CORROSION AREA PER SRM 51-10-03, AND REPAIRED PER STANDARD PRACTICES AND ARA 11011A. (M) 2 L 7 2 4F A6WE 1998080700495 19980807 00495 NM 1998 8 7 TWAA9808605 1 19980519 A 5753 SKIN BOEING 767 767231 1385131 NM RT TE FLAP DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 LAX - DURING C-CHECK MAINTENANCE, FOUND RT WING INBOARD TE FLAP, TOP SIDE HAD 4 INCH BY 5 INCH BY .125 INCH DEEP DENT, J UST OUTBOARD OF FLAP CANOE. REPAIRED FLAP DENT PER SRM 51-70-10. INSTALLED 8.5 INCH BY 8.5 INCH PATCH AND NEW HONEYCOM B. (M) 2 L 7 2 4F RT A1NM 1998080700496 19980807 00496 SO 1998 8 7 MASA98112 1 19980601 A 3350 D36604001 BATTERY PACK EMB 120 EMB120RT SO CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 221YV 120221 DURING MAINTENANCE, AFT EMERGENCY LIGHTS, RT AFT SIDE, FAILED TO TEST. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PAC K, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1998080700497 19980807 00497 CE 1998 8 7 MASA98106 1 19980518 A 5210 12951410649 SNUBBER BEECH 1900 1900D 1154162 CE CABIN DOOR FAILED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 195YV UE195 FLT 5236 - PHX-YUM - PRIOR TO DEPARTURE, CREW REPORTED THAT THE CABIN DOOR WAS DIFFICULT TO CLOSE. MAINTENANCE REMOVED AND REPLACED THE DOOR SNUBBER. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998080700498 19980807 00498 CE 1998 8 7 MASA98105 1 19980517 A 5220 115430100107 STOP BEECH 1900 1900D 1154162 CE RT EMERG EXIT OUT OF ADJUST A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 23YV UE23 DURING ROUTINE INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR NOT FLUSH WITH EXTERIOR SURFACE. MAINTENANCE RERIGGED DOOR STOPS. PRESSURE CHECKED, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A24CE 1998080700499 19980807 00499 NM 1998 8 7 MASA98109 1 19980526 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING ROUTINE MAINTENANCE, FOUND RT FWD EMERGENCY EXIT SIGN HAD SEVERAL LIGHT BULBS THAT DID NOT ILLUMINATE. REMOVED A ND REPLACED BULBS, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998080700500 19980807 00500 WP 1998 8 7 ORJA98102 1 19980518 A 3350 59306431 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY LIGHTS IN ROWS 15-18 REMAIN ON WHEN EMERGENCY LIGHT SWITCH IS SELECTED TO OFF. REPLACED BATTERIES IN BATTERY PACK FOR ROW 15-18. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998080700501 19980807 00501 WP 1998 8 7 ORJA98101 1 19980523 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS INOP ROW 21 THROUGH 24, AND ROWS 1 THROUGH 8. REMOVED AND REPLACED FORWARD GALLEY AND ENTRANCE DOOR CH ARGER. REPLACED BATTERY IN AFT EMERGENCY DOOR CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998080700502 19980807 00502 WP 1998 8 7 98ZZZM538 1 19980523 A 3350 59306431 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS INOP ROW 21 THROUGH 24, AND ROWS 1 THROUGH 8. REMOVED AND REPLACED FORWARD GALLEY AND ENTRANCE DOOR CH ARGER. REPLACED BATTERY IN AFT EMERGENCY DOOR CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998080700503 19980807 00503 WP 1998 8 7 ORJA98103 1 19980528 A 3350 208347 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 A SECTION OF EMERGENCY EXIT LIGHTS INOP IN COACH. REMOVED AND REPLACED LEFT AFT OVERWING EXIT LAMP ASSY. OPS CHECK NOR MAL AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 1998080700504 19980807 00504 WP 1998 8 7 ORJA98104 1 19980502 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP CABIN DEFECTIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 ROW 4-6 LIGHTS INOP. REMOVED AND REPLACED FORWARD GALLEY LIGHT CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998080700505 19980807 00505 WP 1998 8 7 ORJA98105 1 19980524 A 3350 208347 LIGHT DOUG DC9 DC983 3022083 WP CABIN MALFUNCTIONED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY LIGHTS CAME ON AT ROWS 3, 4, 5 AND WOULD NOT EXTINGUISH. REMOVED AND REPLACED EMERGENCY EXIT LAMP SIGN ROWS 3 , 4, 5. (M) 2 L 7 2 4F RT A6WE 1998080700506 19980807 00506 NM 1998 8 7 ORJA98106 1 19980523 A 3350 2608C1011 CHARGER DOUG MD90 MD9030 3023690 NM CABIN INOPERATIVE A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 905RA 53573 BURNED ELECTRICAL THROUGHOUT FORWARD PART OF CABIN AND COCKPIT. REMOVED AND REPLACED TWO A/C BATTERIES IAW MM 24. REMO VED AND REPLACED BATTERY CHARGER UNIT IAW MM 24. (M) 2 L 7 2 4F RT A6WE 1998080700507 19980807 00507 NM 1998 8 7 98ZZZM539 1 19980523 A 3350 260BA1011 BATTERY PACK DOUG MD90 MD9030 3023690 NM CABIN DISCHARGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 905RA 53573 BURNED ELECTRICAL THROUGHOUT FORWARD PART OF CABIN AND COCKPIT. REMOVED AND REPLACED TWO A/C BATTERIES IAW MM 24. REMO VED AND REPLACED BATTERY CHARGER UNIT IAW MM 24. (M) 2 L 7 2 4F RT A6WE 1998080700509 19980807 00509 EU 1998 8 7 VTZA98212 1 19980604 A 2931 S214160K GAUGE BAG JETSTM JETSTM3201 1500217 EU COCKPIT MALFUNCTIONED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 486UE 905 FLT 6414 - IAD-GSO - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO LEFT AND RIGHT HYDRAULIC PRESSURE FLUCTUATION. A IRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PRESSURE GA UGE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700510 19980807 00510 EU 1998 8 7 VTZA98211 1 19980606 A 7714 P146A7210035 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 307UE 41021 FLT 6265 - IAD-BTV - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT RPM GAUGE FAILED. AIRCRAFT RETURN ED TO GATE AT WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLENAED AND RESEATED RT MONOPOLE CANNON PLUG. OPS CH ECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700511 19980807 00511 EU 1998 8 7 VTZA98190 1 19980512 A 2422 2XBY RELAY BAG JETSTM JETSTM3201 1500217 EU E/E COMPT LOOSE A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 492UE 790 FLT 6247 - IAD-BGM - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT IAD DUE TO THE RED INVERTER WARNING LIGHT ILLUMINATED . AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET 28V MAIN DC BUS AND RESECURE D RELAY 2XB7, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700512 19980807 00512 1998 8 7 VTZA98205 4 19980529 A 3425 7004545911 COMPENSATOR JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 323UE 41059 FLT 6277 - BWI-BOS - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 HEADING COMPAITOR WARNING LIGHT ILL UMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 REMO TE COMPENSATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700513 19980807 00513 EU 1998 8 7 VTZA98203 1 19980527 A 3230 ROD JETAIR JETSTM JETSTM4101 1500501 EU NLG OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 301UE 41012 FLT 6572 - IAD-SCE - DURING TAKEOFF, THE CREW EXPERIENCED A NLG INTRANSIT LIGHT THAT REMAINED ON. A/C RETURNED TO IAD W HERE MX CONTROL WAS NOTIFIED AND DISPATCHED MAINTENANCE. MAINTENANCE INSPECTED THE NOSE LANDING GEAR SYSTEM IAW MM AND FOUND THAT THE ROD ENDS ATTACHED TO THE GEAR LEG ASSY NEEDED TO BE ADJUSTED. A/C WAS MOVED TO THE HANGAR WHERE THE ROD ENDS WERE ADJUSTED AND THE LANDING GEAR WAS FUNCTIONALLY CHECKED FOR PROPER OPERATION. ALL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700514 19980807 00514 EU 1998 8 7 VTZA98197 1 19980520 A 2932 S12211143 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU LT HYD SYSTEM FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 476UE 884 FLT 6546 - IAD-ROA - DURING CRUISE, A/C MADE A UNSCHEDULED LANDING DUE TO HYDRAULIC FLUCTUATION ON BOTH LEFT AND RT PSI GAUGE. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND BLEED RT HYDRAULIC PUMP AND R EMOVED AND REPLACED LT HYDRAULIC PUMP TRANSMITTER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700515 19980807 00515 EU 1998 8 7 VTZA98187 1 19980509 A 3411 PITOT LINE BAG JETSTM JETSTM3201 1500217 EU FUSELAGE CONTAMINATED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 477UE 890 FLT 6281 - IAD-HPN - DURING CRUISE, AIRCRAFT DIVERTED TO EWR DUE TO NR 1 ALTIMETER FAILURE. AIRCRAFT WENT TO THE GATE W ITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEARED PITOT STATIC LINES OF MOISTURE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700516 19980807 00516 EU 1998 8 7 VTZA98209 1 19980602 A 3260 BULB JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA O OTHER P NO WARNING INDICATION LD LANDING 1 EA 27 325UE 41063 FLT 6199 - BDL-IAD - DURING LANDING, AIRCRAFT LANDED ON SCHEDULE WITH ONE DISCREPANCY WHICH WS NO RT MLG INDICATION. AI RCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LIGHT BULB AND PERFORMED G EAR SWING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700519 19980807 00519 NM 1998 8 7 WRLA98087 1 19980610 A 2820 VALVE DOUG MD11 MD11 3023602 NM TAIL FUEL TANK MALFUNCTIONED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 276WA 48632 DURING TAXI OUT, FLT CREW RECEIVED A 'TAIL TANK TRANSFER' FAULT. FLIGHT CREW ELECTED TO RETURN TO GATE FOR MAINTENANCE. A/C RETURNED TO GATE WITHOUT FURTHER INCIDENT AS NOTED ON LOGPAGE NR 87916. MAINTENANCE PERSONNEL UNABLE TO DUPLICATE FAULT. RECYCLED THE TAIL TANK NR 1 FILL VALVE, AND PERFORMED A RETURN TO SERVICE TEST OF FUEL SYSTEM WITH NO FAULTS NO TED. SUSPECT EVENT WAS A SPURIOUS DIGITAL SIGNAL. A/C RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998080700520 19980807 00520 NM 1998 8 7 USAABB98055 1 19980510 A 2530 OVEN BOEING 757 7572B7 1384964 NM GALLEY SMOKE A USAA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 631AU 27809 SEA - FLT 116 - IN THE FORWARD, NR 2 OVEN, A PIECE OF PAPER WAS LEFT ON A WARNING TRAY AND BEGAN TO SMOLDER. THE CREW U SED A HALON EXTINGUISHER ON THE TRAY. MAINTENANCE CHECKED THE OVEN FOR SAFE OPERATION. (M) 2 L 7 2 4F RT A2NM 1998080700521 19980807 00521 WP 1998 8 7 ORJA98112 1 19980617 A 2421 GENERATOR DOUG DC9 DC983 3022083 WP RT ENGINE MALFUNCTIONED A ORJA K NONE O OTHER NR NOT REPORTED 1 WP 11 873RA 53093 AFTER START, RIGHT ENGINE GENERATOR WOULD NOT COME ON LINE. APU GEN POWER BLUE LIGHT REMAINED 'ON' ON RIGHT DISTRIBUTIO N SYSTEM EVEN THOUGH APU WAS SHUT DOWN. DEENERGIZED APU RT POWER RELAY. APU GEN AND CONTROL SYSTEM IS INOP. ENTERED D MI 13916 WPC 18492. APU OPERATIONAL, DMI CLEARED. OPERATIONS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998080700522 19980807 00522 NE 1998 8 7 TWAA9809701 2 19980617 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE RT ENGINE STALLED A TWAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 CE 05 919TW 49368 1207 DCA - FLT 797 - AT FL 330 TO 350 RT ENGINE HAD SEVERAL STALLS. REDUCED THROTTLE TO IDLE AND STALLS STOPPED. DECLARED E MERGENCY AND DIVERTED TO DCA. REPLACED ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998080700523 19980807 00523 1998 8 7 98ZZZM542 4 19980207 A 2565 SLIDE ASSY AIRBUS 310 A310324 3930206 EU PAX DOOR FAILED A L AJLF K NONE O OTHER IN INSP/MAINT 1 SO 23 838AB 676 DOOR 3L SLIDE WAS DEPLOYED AS PART OF AIR JAMAICA'S SAMPLING PROGRAM. THE SLIDE WAS EJECTED BUT DID NOT INFLATE. AN AT TEMPT OF MANUAL INFLATION ALSO PROVED FUTILE. (M) 2 L 7 2 4F RT A35EU 1998080700524 19980807 00524 EU 1998 8 7 VTZA98183 3 19980505 A 6112 P110264170117 DE-ICE JETAIR JETSTM JETSTM4101 1500501 EU RT PROP ASSY FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 301UE 41012 FLT 6150 - IAD-EWR - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT PROP HEAT FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT PROP ASSY, OPS CHECK OK. AIRCRAFT WAS RELEASED ADN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700525 19980807 00525 EU 1998 8 7 VTZA98186 1 19980508 A 3310 13730323K406 BULB BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING L NO TEST CR CRUISE 1 EA 27 477UE 890 FLT 6387 - IAD-SYR - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO BURNING SMELL IN COCKPIT. AIRCRAFT RETURNED TO T HE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RELAMPED FO'S SKIRT PANEL LIGHTS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700526 19980807 00526 EU 1998 8 7 VTZA98185 1 19980507 A 3060 P110264170117 DEICE JETAIR JETSTM JETSTM4101 1500501 EU LT PROP ASSY MALFUNCTIONED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 302UE 41013 FLT 6612 - IAD-JFK - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT PROP HEAT FAILURE. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND CHECKED LEFT PROP HEAT AND COULD NOT DUPLICATE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700527 19980807 00527 EU 1998 8 7 VTZA98184 1 19980508 A 3060 C40648 DEICE JETAIR JETSTM JETSTM4101 1500501 EU LT PROP ASSY FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 309UE 41022 FLT 6326 - IAD-ROC - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT PROP HEAT FAILURE. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT PROP DEICE LEAD, OPS CHECK OF. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700528 19980807 00528 1998 8 7 VTZA98206 4 19980529 A 3442 7008420922 RT UNIT JETAIR JETSTM JETSTM4101 1500501 EU E/E COMPT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 308UE 41013 FLT 6306 - IAD-JFK - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO WEATHER RADAR FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WEATHER RADAR RT, OPS CHECK OK. AIRC RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700529 19980807 00529 EU 1998 8 7 VTZA98188 1 19980510 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY FAILED A VTZA K NONE N FALSE WARNING AP APPROACH 1 EA 27 302UE 41013 FLT 6941 - BWI-RIC - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS SMOKE DETECTOR W ARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND REMOVED AND REPLACED POD SMOKE DETECTOR, OPS CHECK OK. AIRCRAFT WA S RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700530 19980807 00530 EU 1998 8 7 VTZA98219 1 19980619 A 2611 722111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 326UE 41064 FLT 6173 - BOS-IAD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO POD SMOKE WARNIGN LIGHT ILLUMINATED. AI RCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 57054, MEL 26-1. MAINTENANCE CL OSED DMI 57054 ON 06-19-98 BY REMOVING AND REPLACING SMOKE DETECTOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700531 19980807 00531 EU 1998 8 7 VTZA98220 1 19980615 A 3350 6134051 BATTERY JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCHARGED A VTZA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 27 322UE 41058 FLT 6591 - IAD-ROA - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO EMERGENCY LIGHTS INOP. MAINTENANCE INSPECTED AND REM OVED AND REPLACED EMERGENCY BATTERIES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700532 19980807 00532 EU 1998 8 7 VTZA98217 1 19980610 A 2913 QA03044 FILTER BAG JETSTM JETSTM3201 1500217 EU HYD SYSTEM FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 497UE 904 FLT 6330 - IAD-BOS - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO LANDING GEAR SLOW TO RETRACT. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ALL THREE HYDRAULIC FIL TER AND PERFORMED GEAR SWING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700533 19980807 00533 EU 1998 8 7 VTZA98216 1 19980611 A 3210 14132003 GUARD JETAIR JETSTM JETSTM4101 1500501 EU RT MLG LOOSE A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 308UE 41023 FLT 6543 - EWR-IAD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT GEAR WARNING LIGHT STAYED ON AFTER G EAR RETRACTION. AIRCRAFT RETURNED TO GATE AT EWR WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND RT WHEEL WE LL MUD GUARD LOOSE AND RESECURED AND PERFORMED GEAR SWING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700534 19980807 00534 EU 1998 8 7 VTZA98213 1 19980606 A 5270 WARNING BAG JETSTM JETSTM3201 1500217 EU PAX DOOR ACTIVATED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 497UE 904 FLT 6584 - BOS-SWF - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING AT BDL DUE TO PAX DOOR WARNING LIGHT ILLUMINATE D. AIRCRAFT DIVERTED TO BDL AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 56392, MEL 52-1. MAINTENANCE CLOSED DMI 56392 ON 6-6-98 BY PERFORMING OPERATION CHECK ON PASSENGER DOOR WARNING SYSTEM. COULD NO T DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700535 19980807 00535 EU 1998 8 7 VTZA98189 1 19980510 A 2910 1379305A77 LINE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE CHAFED A VTZA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 27 495UE 818 FLT 6373 - SYR-IAD - DURING CRUISE, MADE AN UNSCHEDULED LANDING AT IAD WITH ONE DISCREPANCY WHICH WAS LOSS OF ALL HYDRAU LIC PUMP PRESSURE. LANDING GEAR WAS PUMPED DOWN. AIRCRAFT WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSP ECTED AND REMOVED AND REPLACED HYDRAULIC LINE TO HYDRAULIC PUMP, OPS CHECK OL. AIRCRAFT WAS RELEASED AND RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A56EU 1998080700536 19980807 00536 1998 8 7 VTZA98204 4 19980528 A 3416 4016341905 INDICATOR JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 333UE 41101 FLT 6547 - IAD-ROA - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 ALTITUDE INDICATOR FAILED. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 ALTITUDE INDICATOR. O PS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700537 19980807 00537 EU 1998 8 7 VTZA98196 1 19980519 A 2750 51481M185 HANDLE BAG JETSTM JETSTM3101 1500215 EU TE FLAP FAILED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 473UE 828 FLT 6410 - IAD-MDT - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO FLAPS NEVER RETRACTED AND FELL TO 35 DEGREES. AIRCRAFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ARE STILL IN THE PROCESS OF TROUBLESHOOTING PROBLEM. MAINTENANCE FINISHED TROUBLESHOOTING AIRCRAFT AND REMOVED AND REPLACED FLAP SELECTOR VALVE HANDLE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998080700538 19980807 00538 EU 1998 8 7 VTZA98198 1 19980520 A 2750 8661D VALVE BAG JETSTM JETSTM3101 1500215 EU TE FLAPS FAILED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 473UE 828 FLT 6568 - IAD-SCE - DURING TAKEOFF CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FLAPS STUCK AT 35 DEGREES. AIRCR AFT RETURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLAP SELECTOR VALVE A ND PERFORMED MAINTENANCE ACCEPTANCE FLIGHT. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998080700539 19980807 00539 EU 1998 8 7 VTZA98193 1 19980516 A 7722 6940019002 SENSOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 471UE 821 FLT 6193 - IAD-JFK - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE EGT FLUCTUATION. AIRCRAFT RE TURNED TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 56342, MEL 76-1 ON SRL. MAINTENANCE CLOSED DMI 56324 ON 5-17-98 BY REMOVING AND REPLACING TEMPERATURE SENSOR. OPS CHECK OK AIRCRAFT WAS RELEASED AND RETURN ED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700540 19980807 00540 EU 1998 8 7 VTZA98191 1 19980511 A 7722 94959411 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE DIRTY A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT DE DESCENT 1 EA 27 491UE 911 FLT 6524 - ROC-JFK - DURING DESCENT, MADE AN SCHEDULED LANDING AT JFK WITH ONE DISCREPANCY WHICH WAS LEFT ENGINE FLAMED OUT. CREW SHUT DOWN ENGINE. AIRCRAFT WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE FERRIED AIRCRAFT TO IAD W HERE MAINTENANCE INSPECTED AND OPENED DMI 50218 MEL 76-2 ON TTL. MAINTENANCE CLOSED DMI 50218 ON 5-18-98 BY CLEANING CA NNON PLUG AT ZONE 2 CONNECTION. OPS CHECK OK AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700541 19980807 00541 EU 1998 8 7 VTZA98194 1 19980517 A 5210 1415201641 SEAL JETAIR JETSTM JETSTM4101 1500501 EU MAIN DOOR DISPLACED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 301UE 41012 FLT 6225 - IAD-BOS - AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR SEAL FAILED AND AIRCRAFT WOULD NOT HOLD PRESSURIZATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REINSTALLED DOOR SEAL IN TO CHANNEL, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998080700542 19980807 00542 EU 1998 8 7 VTZA98182 1 19980505 A 7931 1241013 GAUGE BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 484UE 899 FLT 6195 - IAD-MDT - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO RT OIL PSI GAUGE PEGGED OUT. AIRCRAFT RETURNED T O THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL, PSI GAUGE. OPS CHECK OK. AIR CRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998080700543 19980807 00543 EU 1998 8 7 VTZA98165 1 19980417 A 2611 MP5 WIRE BAG JETSTM JETSTM3201 1500217 EU SMOKE DET FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 481UE 895 FLT 6168 - IAD-LYH - DURING CLIMB, EXPERIENCED A DISCREPANCY WITH THE CARGO SMOKE DETECTOR ILLUMINATING. AIRCRAFT RETUR NED TO IAD AND NOTIFIED MAINTENANCE CONTROL IAD MAINTENANCE WAS DISPATCHED MAINTENANCE DEFERRED THE CARGO SMOKE DETECTOR UNDER MEL 26-4. MAINTENANCE CLOSED DMI 50706 ON 4-18-98 BY REPAIRING SHORTED WIRE. AIRCRAFT WAS THEN RELEASED FOR SER VICE. (M) 2 L 7 2 4T RT A56EU 1998080700544 19980807 00544 EU 1998 8 7 98ZZZM543 1 19980507 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND THE RIGHT CENTER INBOARD SEAT TRACK CORRODED IN SEVERAL AREAS. REMOVED AND INSTALLED SEAT TRACK IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE, ENVIROMENTAL. 2 H 7 2 4T RT A53EU 1998080700545 19980807 00545 EU 1998 8 7 98ZZZM544 1 19980507 A 5347 S53678001200201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND THE LEFT OUTBOARD SEAT TRACK, AFT CABIN CORRO DED IN SEVERAL AREA. REMOVED AND INSTALLED SEAT TRACK IAW ATR 42 SRM 53-61-00. CAUSE OF DAMAGE, ENVIROMENTAL. 2 H 7 2 4T RT A53EU 1998080700546 19980807 00546 EU 1998 8 7 98ZZZM545 1 19980507 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND THE LEFT CENTER OUTBOARD SEAT TRACK CORRODED IN SEVERAL AREAS. INSTALLED SEAT TRACK IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE, ENVIROMENTAL. (M) 2 H 7 2 4T RT A53EU 1998080700547 19980807 00547 EU 1998 8 7 98ZZZM546 1 19980507 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND THE RIGHT FORWARD OUTBOARD SEAT TRACK CORRODED IN SEVERAL AREAS. INSTALLED SEAT TRACK IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE, ENVIRONMENTAL. (M) 2 H 7 2 4T RT A53EU 1998080700548 19980807 00548 EU 1998 8 7 98ZZZM547 1 19980507 A 5347 S53375001203 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND THE RIGHT FWD INBOARD SEAT TRACK CORRODED IN SEVERAL AREAS. REMOVED AND INSTALLED NEW SEAT TRACK IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE, ENVIROMENTAL. (M) 2 H 7 2 4T RT A53EU 1998080700549 19980807 00549 EU 1998 8 7 98ZZZM548 1 19980507 A 5347 S53678001201222 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED A AMR EAGLE MAINTENANCE CENTER FOUND THE RIGHT OUTBOARD SEAT TRACK, AFT CABIN, CORR ODED IN SEVERAL AREAS. REMOVED AND INSTALLED SEAT TRACK IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE, ENVIRONMENTAL. (M) 2 H 7 2 4T RT A53EU 1998080700550 19980807 00550 EU 1998 8 7 98ZZZM549 1 19980507 A 5347 S53375001204 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND THE LEFT FOWARD OUTBOARD SEAT TRACK CORRODED IN SEVERAL AREAS. REMOVED AND INSTALLED NEW SEAT TRACK IAW ATR 42 SRM 51-25-04. CAUSE OF DAMAGE, ENVIRONMENTAL. (M) 2 H 7 2 4T RT A53EU 1998080700551 19980807 00551 EU 1998 8 7 98ZZZM550 1 19980508 A 5320 S5367800821602 ZEE MEMBER AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND CORROSION ON THE RIGHT Z MEMBER BETWEEN FRAME S 39 AND 41. REMOVED AND INSTALLED Z MEMBER IAW ATR 42 SRM 51-25-02. CAUSE OF DAMAGE, ENVIROMENTAL. (M) 2 H 7 2 4T RT A53EU 1998080700552 19980807 00552 EU 1998 8 7 98ZZZM551 1 19980508 A 5320 S5367800821602 ZEE MEMBER AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 271AT 273 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER FOUND FLOORBEAM CORRODED AT SCREW HOLE NEAR LEFT AF T F/A SEAT TRACK. SPLICED IN INSERT OF FLOORBEAM 38 IAW ATR 42 SRM 53-00-00 FIG 429 AND 51-25-02. CAUSE OF DAMAGE, ENV IRONMENTAL. (M) 2 H 7 2 4T RT A53EU 1998080700553 19980807 00553 NM 1998 8 7 TSAA9833379 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 4 POSITION EMERGENCY LIGHT ASSY BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700554 19980807 00554 NM 1998 8 7 TSAA9833380 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700555 19980807 00555 NM 1998 8 7 TSAA9833381 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700556 19980807 00556 NM 1998 8 7 TSAA9833382 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700557 19980807 00557 NM 1998 8 7 TSAA9833383 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700558 19980807 00558 NM 1998 8 7 TSAA9833384 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700559 19980807 00559 NM 1998 8 7 TSAA9833315 1 19980611 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 LEFT FORWARD PASSENGER DOOR EXIT IDENTIFIER 'ALL'S WELL' LIGHT INOP. REPLACED IDENTIFIER. OPS CHECKED OK. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700560 19980807 00560 NM 1998 8 7 TSAA9833316 1 19980611 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 FORWARD SERVICE DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700561 19980807 00561 NM 1998 8 7 TSAA9833317 1 19980615 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REMOVED AND REPLACED NR 3 SEAT LIGHT ASSY BATTERY PACK DUE TO FAILING CHECK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1998080700562 19980807 00562 NM 1998 8 7 TSAA9833361 1 19980703 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 4 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO NO TESTING. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998080700563 19980807 00563 NM 1998 8 7 TSAA9833362 1 19980703 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700564 19980807 00564 NM 1998 8 7 TSAA9833363 1 19980704 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998080700565 19980807 00565 NM 1998 8 7 TSAA9833364 1 19980704 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 4 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO NO TESTING. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998080700566 19980807 00566 NM 1998 8 7 TSAA9833365 1 19980707 A 3350 8731002511 LIGHT BOEING 737 737297 1384480 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED FORWARD ENTRY DOOR EXIT IDENTIFICATION LIGHT ASSY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F A16WE 1998080700567 19980807 00567 NM 1998 8 7 TSAA9833367 1 19980708 A 3350 90031 LIGHT BOEING 737 737297 1384480 NM CABIN BROKEN A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED LEFT SIDE OVERWING EMERGENCY LIGHT ASSY DUE TO BEING CRACKED/BROKEN. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F A16WE 1998080700568 19980807 00568 NM 1998 8 7 TSAA9833366 1 19980707 A 3350 0221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED BATTERY PACK FOR AFT ENTRY DOOR EXIT LIGHT DUE TO BEING INOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700569 19980807 00569 NM 1998 8 7 TSAA9853368 1 19980629 A 5330 SKIN BOEING 737 737297 1384480 NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 FUSELAGE SKIN CRACK APPROXIMATELY 1.75 INCHES IN LENGTH AT BS 727 PLUS 12 INCHES AND STRINGER 16R. VERIFIED BY HFEC. R EPAIRED CRACK PER BOEING SRM 53-30-3 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998080700570 19980807 00570 NM 1998 8 7 TSAA9826355 1 19980624 A 2612 CONNECTOR BOEING 737 7372M6C 1384708 NM NR 2 FIRELOOP LOOSE A TSAA K NONE N W FALSE WARNING INADEQUATE Q C NR NOT REPORTED 1 WP 13 805AL 21809 FIRE WARNING WENT OFF MOMENTARILY IN FLIGHT NR 2 ENGINE AND APU FIRE DETECTION SYSTEM WOULD NOT TEST THEREAFTER. INSPEC TED NR 2 ENGINE AND FOUND LOOSE CONNECTOR ON LOWER FIRE LOOP. SECURED AND SAFETY-TIED CONNECTOR. OPS CHECK OK. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700571 19980807 00571 NM 1998 8 7 TSAA9832356 1 19980625 A 3240 SRDL7G INDICATOR BOEING 737 737230 NM HYD SYSTEM FAILED A TSAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 818AL 22117 SYSTEM 'B' HYDRAULIC BRAKE PRESSURE IS LOW AT 2300 PSI AFTER TAKEOFF. HYDRAULIC SYSTEM PRESSURE IS NORMAL AND 'A' BRAKE PRESSURE NORMAL. REPLACE INDICATOR AND TRANSMITTER. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998080700572 19980807 00572 NM 1998 8 7 TSAA9833354 1 19980627 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY IN NR 1 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F A16WE 1998080700573 19980807 00573 NM 1998 8 7 USAA980287 1 19980630 A 5311 146N10141 FRAME BOEING 757 757225 1384959 NM BS 460 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND FRAME CORROSION 36 INCHES ON TOP OF FRAME AND SIDES ARE CORRODED STATION 1460 RBL 4 TO LBL 14. INSTALLED NEW FRAME SECTION PER SRM 53-00-07 AND SRM 53-10-11. (M) 2 L 7 2 4F RT A2NM 1998080700574 19980807 00574 NM 1998 8 7 USAA980288 1 19980630 A 5315 141N51121 FLOORBEAM BOEING 757 757225 1384959 NM BS 365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION ON FLOORBEAM BS 365 LBL 30 RBL 62. FABRICATED NEW 'T' CAP, DOUBLERS AND ANGLES PER TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1998080700575 19980807 00575 NM 1998 8 7 USAA980289 1 19980630 A 5320 141N51111 BEAM BOEING 757 757225 1384959 NM BS 345 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION BS 345 LBL 16, RBL 01 ON BEAM. FAB RICATED NEW 'T' CAP, DOUBLER AND ANGLES PER TYPICAL REPAIR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1998080700576 19980807 00576 NM 1998 8 7 USAA980290 1 19980630 A 5320 140N2006161 SHEAR TIE BOEING 757 757225 1384959 NM BS 1300 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH AREA OF CORROSION SHEAR TIE BS 1300 STRINGER 29L. (M ) 2 L 7 2 4F RT A2NM 1998080700577 19980807 00577 NM 1998 8 7 USAA980291 1 19980630 A 5320 140N2006161 SHEAR TIE BOEING 757 757225 1384959 NM BS 1300 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH AREA OF CORROSION SHEAR TIE BS 1300 STRINGER 29R. (M ) 2 L 7 2 4F RT A2NM 1998080700578 19980807 00578 NM 1998 8 7 USAA980284 1 19980630 A 5311 146N101715 FRAME BOEING 757 757225 1384959 NM BS 1520 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 3 INCH AND 2 INCH BY 27 INCH ON FRAME STATION 1520 ASSY BOTT OM. REPAIRED LOWER FRAME SECTION REMOVED AND REPLACED PER SRM 53-00-07. (M) 2 L 7 2 4F RT A2NM 1998080700579 19980807 00579 NM 1998 8 7 USAA980285 1 19980630 A 5311 146N10452 FRAME BOEING 757 757225 1384959 NM BS 1500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION BS 1500 LBL 04-LBL 19 ON FRAME ASSY . INSTALLED NEW FRAME PER SRM 51-10-00 BAC DWG 146N1045. (M) 2 L 7 2 4F RT A2NM 1998080700580 19980807 00580 NM 1998 8 7 USAA980292 1 19980630 A 5313 146N3110184 STRINGER BOEING 757 757225 1384959 NM BS 1410 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION BS 1410 STRINGER 29L. INSTALLED ST RINGER REPAIR KIT CC6341806 PER SRM 53-00-03 PAGE 201, FIGURE 201. (M) 2 L 7 2 4F RT A2NM 1998080700581 19980807 00581 NM 1998 8 7 USAA980293 1 19980630 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM BS 377 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION BS 377 LBL 45 SEAT TRACK. FABRICAT ED SEAT TRACK PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1998080700582 19980807 00582 NM 1998 8 7 USAA980283 1 19980630 A 5320 141N29321 CHORD BOEING 757 757225 1384959 NM BS 324 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCY BY 1 INCH AREA OF CORROSION BS 324 RBL 42, RBL 48 ON UPPER CHOR D. INSTALLED UPPER CHORD SPLICE PER EA 61784. (M) 2 L 7 2 4F RT A2NM 1998080700583 19980807 00583 NM 1998 8 7 USAA980272 1 19980630 A 5311 146N10115 FRAME BOEING 757 757225 1384959 NM BS 1400 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION BS 1400 STRINGER 28L-28R ON FRAME A SSY BOTTOM. INSTALLED NEW FRAME FROM BOEING PER SRM 51-10-00. (M) 2 L 7 2 4F RT A2NM 1998080700584 19980807 00584 NM 1998 8 7 USAA980235 1 19980630 A 5330 146N3430 SKIN BOEING 757 757225 1384959 NM BS 1495 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION BETWEEN FILLER AND DOUBLER STATION 1495 BETWEEN STRINGER 28L A ND STRINGER 29L ON SKIN. REPLACED EXISTING FILLER AND DOUBLER PER SRM 53-00-01 FIG 208. (M) 2 L 7 2 4F RT A2NM 1998080700585 19980807 00585 NM 1998 8 7 USAA980279 1 19980625 A 5320 146N852247 ANGLE BOEING 757 7572B7 1384964 NM BS 1380/1400 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 633AU 10295 27811 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION AT LWR THRESHOLD CHORD ANGLE AFT CARGO DOOR BETWEEN STATION 13 80 AND 1400 OUTBOARD CHORD. BLENDED CORRODED AREA PER EA NR 61989. (M) 2 L 7 2 4F RT A2NM 1998080700586 19980807 00586 NM 1998 8 7 USAA980282 1 19980630 A 5320 6546921528 FRAME BOEING 737 737301 1384611 NM CARGO DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 35551 23237 CLT - DURING CX-6 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK FWD SIDE OF FWD CARGO DOOR. INSTALLE D MODIFIED PART. (M) 2 L 7 2 4F RT A16WE 1998080700587 19980807 00587 NM 1998 8 7 USAA980299 1 19980707 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 48368 22018 CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK ON FUSELAGE SKIN 1 INCH FORWARD OF BS 727B .5 INCH ABOVE ST RINGE R16R. INSTALLED EXTERNAL REPAIR DOUBLER PER EA 62067. (M) 2 L 7 2 4F A16WE 1998080700588 19980807 00588 NM 1998 8 7 USAA980300 1 19980629 A 5320 6546921528 FRAME BOEING 737 737301 1384611 NM CARGO DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 340US 35551 23237 CLT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK FWD SIDE OF DOOR FRAME OF FWD CARGO DOOR. INSTALLED M ODIFIED PART. (M) 2 L 7 2 4F RT A16WE 1998080700589 19980807 00589 NM 1998 8 7 USAA980313 1 19980707 A 5230 6547952524M SKIN BOEING 737 7373B7 1384580 NM CARGO DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 518AU 33953 23704 DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION FOUND A .25 INCH CRACK IN AFT CARGO DOOR SKIN AT THE AFT UPPER CORN ER FOR HANDLE. INSTALLED DOUBLER PR SRM 52-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1998080700590 19980807 00590 WP 1998 8 7 USAA980261 1 19980706 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1018 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 966VJ 73788 47420 PIT - DURING RON VISIT, FOUND 5.5 INCH CRACK IN SKIN AT STATION 1018 ABOVE LAP JOINT 23L. INSTALLED DOUBLER PER SRM 53- 04 FIG 18. (M) 2 L 7 2 4F A6WE 1998080700591 19980807 00591 NM 1998 8 7 USAASB98157 1 19980625 A 3350 30043229 LIGHT BOEING 737 7373B7 1384580 NM FUSELAGE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 375US 22954 SYR - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT JUST AFT OF THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE EXTERIOR EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998080700592 19980807 00592 WP 1998 8 7 USAAD98117 1 19980630 A 5241 DOOR DOUG DC9 DC982 3022082 WP GALLEY NOT CLOSED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 825US 49237 CLT - FLT 237 - AFTER TAKEOFF, CREW REPORTED THEY COULD NOT PRESSURIZE THE AIRCRAFT. FLIGHT ATTENDANTS REPORTED THAT TH E L2 DOOR WAS NOT CLOSED PROPERLY AND WAS MAKING A LOUD NOISE. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDE NT. MAINTENANCE INSPECTED THE DOOR AND FOUND NO DEFECTS. DOOR WAS CLOSED AND AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F A6WE 1998080700593 19980807 00593 NM 1998 8 7 USAA980286 1 19980630 A 5315 141N51131 FLOORBEAM BOEING 757 757225 1384959 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 41669 22192 CLT - DURIGN C-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION ON FLOORBEAM AT BS 377 LBL 61 RBL 1 2. FABRICATED NEW 'T' CAP, DOUBLERS AND ANGLES PER TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1998080700594 19980807 00594 NM 1998 8 7 USAASB98166 1 19980702 A 2530 1539B1 OVEN BOEING 737 737201 1384454 NM GALLEY OVERHEATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 259AU 22806 PGV - FLT 1077 - AT FL 350 EN ROUTE TO JAX FROM LGA, THE FORWARD GALLEY OVEN CAUGHT FIRE. THE FLIGHT ATTENDANT USED A F IRE EXTINGUISHER AND PUT OUT THE FIRE. THIRTY MINUTES LATER THE FIRE RESTARTED AND SMOKE ENTERED THE COCKPIT. CAPTAIN DECLARED AN EMERGENCY AND FLIGHT ATTENDANT EXTINGUISHED FIRE AGAIN. FLIGHT DIVERTED TO PGV AND LANDED WITHOUT FURTHER I NCIDENT. MAINTENANCE FOUND THE OVEN FAN MOTOR WAS BURNED OUT. REPLACED THE OVEN AND INSPECTED THE AREA. NO FURTHER DA MAGE WAS FOUND. (M) 2 L 7 2 4F A16WE 1998080700595 19980807 00595 WP 1998 8 7 TWAA9812501 1 19980803 A 2822 3980001 BOOST PUMP DOUG DC9 DC982 3022082 WP CENTER TANK WORN A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 914TW 49185 ABOVE FL 300 COULD NOT PUMP FUEL FROM CENTER TANK. TURNED OFF LEFT TANK PUMPS AND DESCENDED IN ALTITUDE AND CENTER TANK STARTED FEEDING. RETURNED TO MCI. REPLACED BOTH CENTER TANK FUEL BOOST PUMPS. CHECK-C 2-28-98 MCI. 2 L 7 2 4F A6WE 1998080700596 19980807 00596 NM 1998 8 7 TWAA9812502 1 19980728 A 5730 SKIN BOEING 767 767231 1385131 NM LT WING DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 605TW 22568 DURING CHECK-C MAINT, FOUND DELAMINATION ON LT WING UPPER LE 2.5 FEET BEHIND NR 6 LE SLAT, OTBD END, 5 INCHES LONG. REP AIRED SURFACE WITH A 3 IN BY 5 IN HOT BOND REPAIR PER SRM 51-70-08, PG 6 THRU 32. 2 L 7 2 4F RT A1NM 1998080700597 19980807 00597 NM 1998 8 7 TWAA9812503 1 19980731 A 5730 SKIN BOEING 767 767231 1385131 NM RT WING DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 608TW 22571 DURING CHECK-C MAINT, FOUND ON RT WING THE LE PANEL UNDER NR 7 LE SLAT, APPROX 2/3 DISTANCE FROM INBD END OF STRUT, HAD .5 IN BY 2.5 IN LONG DELAMINATED LOOKING CRACK. INSTALLED REPAIR SIZE 2 IN BY 3 IN AND HOT BOND REPAIR PER SRM 51-70-17 . 2 L 7 2 4F RT A1NM 1998080700598 19980807 00598 WP 1998 8 7 TWAA9812504 1 19980803 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND CORROSION ON L-ANGLE AT PRESSURE BULKHEAD UNDER REPAIR 6 IN LBL TO 6 IN RBL. REMOVED L- ANGLE DOUBLER NR 9915661-33 FOR REPLACEMENT PER SRM 51-10-01, PG 1 ITEM C. INSTALLED NEW L-ANGLE DOUBLER 9915561-33 PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998080700599 19980807 00599 WP 1998 8 7 TWAA9812505 1 19980803 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 996, LONGERON 28 AND 29R. REPAIRED CRACK AS REQUIRED P ER SRM 53-04, FIG 12B, AND ARA 15299. 2 L 7 2 4F A6WE 1998080700600 19980807 00600 WP 1998 8 7 TWAA9812506 1 19980803 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND REINFORCING DOUBLER ABOVE JACK PAD ABOVE SKIN WITH CORROSION, FS 996 LONGERON 28L TO L28 R. REMOVED DOUBLER FOR REPLACEMENT PER SRM 51-01, PG 1 ITEM C. INSTALLED NEW 991561-73 DOUBLER PER DOUGLAS BLUEPRINT N R 9915561 AND SRM 53-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998080700601 19980807 00601 WP 1998 8 7 TWAA9812507 1 19980726 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 192 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND SKIN CRACKED AT STA 192, STR 22L, .1875 IN LONG AT 10 O'CLOCK. REMOVED CRACK PER SRM 53 -04, P33 NOTE NR 1. INSTALLED REPAIR PER MO 71N61 PHASE A. 2 L 7 2 4F A6WE 1998080700602 19980807 00602 WP 1998 8 7 TWAA9812508 1 19980803 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 950 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND CORROSION ON TOP OF LONG 30 AT FS 950. REPLACED LONGERON FROM FS 931 TO 955, PER 51-01, PAGE 4. SEALED PER SRM 51-20-0. 2 L 7 2 4F A6WE 1998080700603 19980807 00603 WP 1998 8 7 TWAA9812509 1 19980803 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 871 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND DENT IN FUSELAGE AT FS 871, BETWEEN LONG 29 AND 30 RT, 4 IN BY 6 IN BY .125 IN. REPAIRE D PER SRM 53-04, FIG 12B, PAGE 25. 2 L 7 2 4F A6WE 1998080700604 19980807 00604 WP 1998 8 7 TWAA9812510 1 19980803 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 800 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 800, LONG 16R. INSTALLED CLASS I REPAIR DOUBLER PER SR M 53-04, FIG 12B. 2 L 7 2 4F A6WE 1998080700605 19980807 00605 WP 1998 8 7 TWAA9812511 1 19980803 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 495-505 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND EXTERNAL DOUBLER INSTALLED AT FS 495 TO 505, LONG 19 TO 20R. REPAIRED PER DC9 SRM 53-04 , FIG 12B SHEET 6. 2 L 7 2 4F A6WE 1998080700606 19980807 00606 WP 1998 8 7 TWAA9812512 1 19980728 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 294 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CRACKED 3 INCHES FWD OF STA 294, AT ZERO BL. FABRICATED NEW INTERCOSTAL FRO M 2024-0 ALUM MATERIAL HEAT TREATED TO 2024T3 PER REMOVED INTERCOSTAL. INSTALLED IN ACFT USING HI-LOKS AND MS20470AD RI VETS, PER DOUGLAS PRINT 3913577. 2 L 7 2 4F A6WE 1998080700607 19980807 00607 WP 1998 8 7 TWAA9812513 1 19980729 A 5240 SKIN DOUG DC9 DC932 3022066 WP LAV SERVICE DOOR CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND ON LOWER FUSELAGE CORROSION AND FASTENER HEADS MISSING AT LOWER FWD CORNER OF THE AFT LA V DUMP SERVICE DOOR. CUT OUT CORRODED MATERIAL FOR REPAIR PER ACFT SRM 51-10-03. REPAIRED PER ARA 15367 PAGE 1 OF 1. 2 L 7 2 4F A6WE 1998080700608 19980807 00608 WP 1998 8 7 TWAA9812514 1 19980729 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 993 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION CLEAN UP BEYOND MANUAL LIMITS, 30 PERCENT REMOVED, AT FS 993, LONGERO N 29L ON FUSELAGE SKIN. REPAIRED DAMAGED AREA BY BLENDING OUT AREA AND INSTALLING A DOUBLER PER SRM 53-04, FIG 38 PAGE 209, CONDITION 3. 2 L 7 2 4F A6WE 1998080700609 19980807 00609 WP 1998 8 7 VJ9800259 1 19980522 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 832 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 AFT CARGO COMPARTMENT CORRODED AT STA 832, L28R. REMOVED SUPPORT, NUT PLATE AND COROSION ON UPPER FLANGE. CORROSION LO SS OF .028 BEYOND LIMIT. INSTALLED SUPPORT IAW DC9 SRM 51-30-2, AT STA 832, L28R, AFTER ALODINING AND PRIMING IAW DC9 S RM 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998080700610 19980807 00610 WP 1998 8 7 VJ9800261 1 19980526 A 5330 1A34569 SKIN DOUG DC9 DC932 3022066 WP BS 360-365 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 FWD CARGO PIT, RH REPAIR DOUBLER AND SKIN CORRODED BEYOND LIMIT AT FS 360, L30-27R. REMOVED CORROSION, FABRICATED REPLA CEMENT DOUBLER FROM 2024T3 .025 INCH, IAW DC9 SRM 53-04, TREATED, PRIMED AND INSTALLED PLUS APPLIED SEALANT. 2 L 7 2 4F A6WE 1998080700611 19980807 00611 WP 1998 8 7 VJ9800262 1 19980527 A 5320 1A3458434585 SUPPORT DOUG DC9 DC932 3022066 WP BS 996-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 RT FLOOR SUPPORT CORRODED BEYOND LIMIT AT STA 996 TO 965. REMOVED CORROSION AND FOUND SKIN CORRODED OUT OF LIMIT IN Z-A NGLE. FABRICATED SKIN FROM 7075T6, .032, AND Z-ANGLE FROM 7075T6, .032. DRILLED AND DEBURRED SKIN AND Z-ANGLE IAW DC9 S RM 51-10-2, 51-10-4. TREATED, PRIMED AND INSTALLED SKIN AND Z-ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998080700613 19980807 00613 WP 1998 8 7 VJ9800264 1 19980528 A 5320 1A345721 WEB DOUG DC9 DC932 3022066 WP BS 218-228 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 LT FWD CARGO PIT WEB CRACKED AND CORRODED BEYOND LIMIT AT STA 218 TO 228, LBL 40 TO 58, IAW DC9 SRM 53-01 FIG 1. REMOVE D LT O/B FLOOR PANEL AFT OF FWD ENTRY DOOR, REMOVED WEB AND FABRICATED WEB PANEL FROM 7075T6, .020, IAW DC9 SRM 53-10-2, FIG 5. TREATED AND PRIMED IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1998080700614 19980807 00614 WP 1998 8 7 VJ9800265 1 19980530 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 503 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 FS 503 FRAME LONGERON 29R TO 29L CORRODED BEYOND LIMIT. INSTALLED REPAIR PARTS AND REPAIRED IAW DC9 SRM 53-03 FIG 5 PG 6 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1998080700615 19980807 00615 WP 1998 8 7 VJ9800266 1 19980601 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 900 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 OUTFLOW VALVE CUTOUT CORRODED BEYOND LIMIT AT STA 900, LT L22. FABRICATED NEW SPLICE FROM 7075T651 IAW DWG 3914675. TR EATED, PRIMED AND INSTALLED NEW SPLICE IAW SRM 53-01, FIG 1, 51-10-3, 51-30-5. REINSTALLED FLOOR SUPPORT, FRAME, SPLICE AND STIFFENER IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998080700616 19980807 00616 WP 1998 8 7 VJ9800267 1 19980605 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 915 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 AFT CARGO PIT LT SIDE, AFT AND BELOW CABIN AIR OUTFLOW VALVE, FRAME CORRODED BEYOND LIMIT. REMOVED STRUT AND INSTALLED NEW STRUT IAW DC9 SRM 51-10-4, 51-10-2, 51-10-3, AND 53-11-3. 2 L 7 2 4F A6WE 1998080700617 19980807 00617 WP 1998 8 7 VJ9800268 1 19980612 A 5315 1A34801 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 AFT PIT FLOORBEAM HAS CORROSION BEYOND LIMIT UNDER NUT PLATES AT FS 965, BL17L AND 19L. REMOVED AND REPLACED FLOORBEAM AND 2 Z-ANGLES IAW DC9 SRM 51-10-3, 51-10-4, 51-30-2, 51-30-5 AND 53-11-3. REINSTALLED, RIGGED AND OPS CHECKED STAB TR IM CABLES AND ENGINE TR CABLES IAW DC9 MM 27-40-0 AND 78-00. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998080700618 19980807 00618 WP 1998 8 7 VJ9800269 1 19980728 A 5313 3914677501N LONGERON DOUG DC9 DC932 3022066 WP BS 794-813 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 SPLICE CORRODED BEYOND LIMIT AT STA 794 TO 813, L30. REMOVED SPLICE AND CORROSION IAW DC9 SRM 51-30-2 AND 51-10-3. ORD ERED NEW SPLICE, DRILLED, DEBURRED AND INSTALLED SPLICE IAW DC9 SRM 51-10-4, 51-30-5. 2 L 7 2 4F A6WE 1998080700619 19980807 00619 WP 1998 8 7 VJ9800270 1 19980803 A 2150 39271411 SHUTOFF VALVE DOUG DC9 DC932 3022066 WP RT PACK MALFUNCTIONED A ZZDA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 15 919VV 47260 AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED OVERHEAT SMELL AFTER FULL HOT HAD BEEN SELECTED TO COMPENSATE FOR AN OVER CHILL IN AIRCRAFT PASSENGER CABIN. SMOKE DETECTOR WARNING RECEIVED. FLIGHT CREW SHUTDOWN RT PACK AND SMELL ALONG WITH SMOKE DETECTION WARNING DISSIPATED. AS PRECAUTIONARY MEASURE, FLIGHT CREW ELECTED TO RETURN TO BASE. INSPECTED AND CHECKED SMOKE DETECTOR, LAVATORY, HOT WATER HEATER, LAV MOTOR, LIGHTS AND RT AIR CONDITIONING PACK. PLACED AC PACK ON MEL AND S UBSEQUENTLY AS PRECAUTIONARY MEASURE REPLACED RT PACK PRESSURE REGULATOR SHUTOFF VALVE IAW MM 21-50, OPS CHECKED SERVICE ABLE. 2 L 7 2 4F A6WE 1998080700620 19980807 00620 WP 1998 8 7 VJ9800271 1 19980803 A 7603 AN540411150433 BOLT DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE RT ENGINE MISSING A ZZDA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 15 930VV 47723 ON TAKEOFF, RT EGT IN CAUTION RANGE AND RT THROTTLES DID NOT RESPOND TO THROTTLE MOVEMENT, ENGINE REMAINED AT TAKEOFF PO WER. FLIGHT CREW SHUTDOWN ENGINE AND RETURNED TO ATL MAINTENANCE BASE. VISUAL INSPECTION OF NR 2 ENGINE REVEALED ENGI NE THROTTLE ROD END BOLT MISSING. INSTALLED AND SAFTIED BOLT IAW MM 76-00. 2 L 7 2 4F 4 F A6WE E2EA 1998080700621 19980807 00621 1998 8 7 MALA976170 2 19980728 A 7260 CHIP LIGHT SAAB SF340 SF340A 7850100 EU RT ENGINE ILLUMINATED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 142XJ 142 RIGHT CHIP DETECT LIGHT CAME ON IN FLIGHT, COMPLIED WITH QRH AND RETURNED TO STW. MAINTENANCE REMOVED RIGHT ENGINE CHIP DETECTOR AND FOUND ONE SMALL SLIVER, CHIP WAS ALLOWABLE. INSPECTED SUMP, NO DEBRIS FOUND. RAN AIRCRAFT, CHECKS GOOD. ALL WORK DONE IAW GEMM 72-00-00. 2 L 7 2 4T RT A52EU 1998080700622 19980807 00622 NM 1998 8 7 MALA976171 1 19980730 A 3350 OL3071BPEGPL LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 846MA 344 DURING INSPECTION, EXIT LIGHT OVER ROW 4A LOOSE ON PANEL. MAINTENANCE INSTALLED SERVICEABLE EXIT LIGHT, ALL CHECKS GOOD . 2 H 7 2 4T RT A13NM 1998080700623 19980807 00623 NM 1998 8 7 MALA976172 1 19980729 A 2611 CONNECTOR DHAV DHC8 DHC8102 2809003 NM COCKPIT DIRTY A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 832MA 341 SMOKE WARNING LIGHT ILLUMINATES INTERMITTENTLY. MAINTENANCE CLEANED CANNON PLUGS ON SMOKE DETECTORS, CYCLED AIRCRAFT PO WER. SMOKE WARNING TEST SATISFACTORY. SMOKE LIGHT REMAINS OUT, OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998080700624 19980807 00624 EU 1998 8 7 MALA976173 1 19980803 A 3230 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 418XJ 418 UPON GEAR DOWN SELECTION THE HYDRAULIC PUMP RAN, GEAR INTRANSIT ILLUMINATED, NO 3 GREEN. CREW RETRIED AFTER ATTEMPTING HYDRAULIC CONTROL BREAKER RESET, BREAKER REPOPPED, SUCCESSFUL RESET ON 3RD ATTEMPT, THREE GREEN. GROUND PERSONEL COMPLA INED OF HEAVY ELECTRICAL BURNING SMELL. MAINTENANCE INSPECTED AND REPLACED CB 7GA. CLEANED CANNON PLUGS IN BOTH GEARWE LLS. OPS CHECK OF EXTENSION AND RETRACTION SYSTEM GOOD. 2 L 7 2 4T RT A52EU 1998080700625 19980807 00625 1998 8 7 MALA976174 4 19980731 A 3418 861CAR STALL VANE SAAB SF340 SF340A 7850100 EU LT FUSELAGE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 115XJ 340A115 LEFT STALL VANE FAIL LIGHT KEPT CYCLING ON/OFF AFTER TAKEOFF. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT STALL VANE. PERFORMED OPS CHECK OF STALL SYSTEM, OPS AND SECURITY CHECK GOOD. 2 L 7 2 4T RT A52EU 1998080700626 19980807 00626 EU 1998 8 7 MALA976175 1 19980731 A 3350 1317 LAMP SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 48XJ 048 DURING WALK AROUND, OVERHEAD EMERGENCY LIGHT AT SEAT 3CD INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998080700627 19980807 00627 SO 1998 8 7 LR7A35 1 19980723 A 5320 3723221 ANGLE LKHEED 382 382G 526414U SO BS 257 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 12363 4606 EXFOILATION CORROSION STA 258 RT CHINE, INSPECTED DAMAGED AREA PER ENGINEERING IN DIRECTIVE EDF07-1 STEP 1 AND STEP 2 DA MAGE WITHIN PERMISABLE LIMITS PER STEP 2 OK FOR INTENDED FERRY FLT RT CHINE ANGLE, FS 257, BLR 61, WL 146, (P/N 372322-1 ). REPAIRED IAW SMP 583 FIG 53-40-26 PG 69. RT RING SEGMENTS (2 EA) FS 250 AND FS 260, BLR 61, WL 146, (P/N 371653-39) . REPAIRED IAW SMP 583 FIG 51-140-21 PG 60. RT TIE FITTING FS 245 TO 251, BLR 61, WL 146 (P/N 373838-4). REPLACED IAW SMP 583 CHP 51-10 PG 5. RT END FITTING FS 245, BLR 61, WL 146 (P/N 373188-1). REPLACED IAW SMP 583 CH 51-10 PG 5. 2 H 7 4 4T A1SO 1998080700628 19980807 00628 SO 1998 8 7 LR7A9831 1 19980723 A 2910 HYD LINE LKHEED 382 382G 526414U SO NLG BROKEN A LR7A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 402LC 1119 4698 LOSS OF UTILITY HYD SYSTEM. REMOVED AND REPLACED LAND GEAR DOWN HYD LINE WHICH WAS BROKEN. ALSO, REPLACED THE EMERGENC Y DOWN HYD LINE, WEATHER BEATING BAD. PRESSURE TESTED GOOD IAW LOCKHEED MM CHAPTER 32. REFILLED HYD RES UTILITY HYD SY STEM. 2 H 7 4 4T A1SO 1998080700629 19980807 00629 SO 1998 8 7 LR7A9832 1 19980724 A 3230 3588005 UPLOCK LKHEED 382 382G 526414U SO NLG CRACKED A LR7A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 402LC 10979 4698 LOSS OF UTILITY HYD SYSTEM. NLG UPLOCK ASSY REPLACED IAW 32-30 PG 231-232. LEAK CHECK GOOD, OPS CHECK GOOD IAW 32-32 P G 201. EMERGENCY EXT OPS CHECK GOOD IAW 32-00 PG 201. 2 H 7 4 4T A1SO 1998080700630 19980807 00630 SO 1998 8 7 LR7A9833 1 19980724 A 7921 5A527000 OIL COOLER LKHEED 382 382G 526414U SO NR 2 ENGINE INOPERATIVE A LR7A E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION DE DESCENT 1 AL 03 401LC 12414 4606 SHUTDOWN NR 2 ENG DUE TO HIGH OIL TEMP. REMOVED AND REPLACED NR 2 ENG OIL COOLER, SEE SPAR WO NR 20-431-101-001. INOPE RATIVE THERMOSTATIC BYPASS AND RELIEF VALVE. 2 H 7 4 4T A1SO 1998080700631 19980807 00631 SO 1998 8 7 LR7A9834 1 19980725 A 2130 CLAMP LKHEED 382 382G 526414U SO RT MLG WW LOOSE A LR7A A UNSCHED LANDING M OVER TEMP CL CLIMB 1 AL 03 403LC 1588 4590 CARGO COMPARTMENT REFRIG OVERHEAT LIGHT CAME ON IN CLIMBOUT. SWITCHED CARGO COMPARTMENT AIR CONDITION SHUT OFF TO OFF P ER EMERG CHECKLIST. OVERHEAT LIGHT WENT OUT. TIGHTENED CLAMP ON CARGO COMPT FLOW CONTROL VALVE SYS LK, OP AND PRESS CK GOOD PER MM CHAP 21-30 201. 2 H 7 4 4T A1SO 1998080700632 19980807 00632 NM 1998 8 7 AWXA9800160 1 19980728 A 3350 417N52101 BATTERY PACK BOEING 757 757225 1384959 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 915AW 22209 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP AT AFT ROWS 26 - 31. REMOVED AND REPLACED AFT BATTERY PAC K. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998080700633 19980807 00633 NM 1998 8 7 AWXA9800161 1 19980728 A 3350 413N3302 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 913AW 22207 DURING ROUTINE MAINTENANCE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHTS INOP ROW 27 TO 30. REPLACED LIGHT ASSEMBLIES AS R EQUIRED. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998080700634 19980807 00634 NM 1998 8 7 AWXA9800163 1 19980729 A 2612 0007460 CONNECTOR BOEING 737 737297 1384480 NM NR 2 ENGINE LOOSE A AWXA F ACTIVATE FIRE EXT. N FALSE WARNING IN INSP/MAINT 1 WP 28 147AW 22630 NR 2 FIRE WARNING LIGHT AND BELL WENT OFF ABOUT 50 MILES PRIOR TO LAND QRH PROCEDURES COMPLETE AND ENGINE SECURED. BOTH FIRE BOTTLES EXPENDED INTO NR 2 ENGINE. BELL CONTINUED TO SOUND AND FIRE LIGHT CONTINUED TO ILLUMINATE LONG AFTER LAND ING AND TAXI IN. REMOVED AND REPLACED BOTTLES IAW MM26-21-11. OPS CKD NORMAL T/S FIRE INDICATION INTERMITTENT CONNECTO R ON FIRE DETECTION LOOP B AFT C/P. 2 L 7 2 4F A16WE 1998080700635 19980807 00635 NM 1998 8 7 AWXA9800164 1 19980724 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 344-360 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 STR 23L STA 344-360 IN E AND E COMPARTMENT HAD SEVERE CORROSION. REMOVED AND REPLACED STR PER SRM 53-10-03 FIG 1. 2 L 7 2 4F RT A16WE 1998080700636 19980807 00636 NM 1998 8 7 AWXA9800165 1 19980720 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 659 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 UPON CLEANING AND OK TO CLOSE FLOOR PANELS, FOUND CRACKS NOTED FLOORBEAM AT STA 659, BLO. REMOVED DAMAGED SECTION NDT E XISTING HOLES, NO CRACKS NOTED. FABRICATED REPAIR PARTS INSTALLED PER SB737-57-1210. 2 L 7 2 4F RT A16WE 1998080700637 19980807 00637 NM 1998 8 7 AWXA9800166 1 19980724 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 CORROSION IN FLOORBEAM TOP FLANGE STA 967 BL-0 TO RBL-30. REPAIRED PER SRM 53-10-09. 2 L 7 2 4F RT A16WE 1998080700638 19980807 00638 NM 1998 8 7 AWXA9800167 1 19980724 A 5320 CHORD BOEING 737 737277 1384570 NM BS 639 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 CABIN STA 639 LT CHORD AND OUTER WEB CRACKED. REMOVED AND REPLACED PER SRM 53-10-03, REPAIRED PER SB53-1061. 2 L 7 2 4F RT A16WE 1998080700640 19980807 00640 NM 1998 8 7 AWXA9800169 1 19980724 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 181AW 22648 CORROSION FLOORBEAM TOP FLANGE STA 986 RBL-15. REPAIR PER SRM 53-10-09. 2 L 7 2 4F RT A16WE 1998080700641 19980807 00641 NM 1998 8 7 AWXA9800170 1 19980729 A 2913 3508807 PUMP BOEING 757 7572S7 1384962 NM LT ENGINE FAILED A AWXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 904AW 28124 1615 23566 INBOUND TO BOSTON LEFT HYDRAULIC ENGINE DRIVEN PUMP LOW OIL PRESSURE LIGHT ILLUMINATED. PUMP WAS TURNED OFF. LEFT SYST EM QUANTITY WENT TO ZERO. REPLACED LEFT ENGINE DRIVEN PUMP. REPLACED PRESS AND SUPPLY QUICK DISCONNECT. REPLACED FILT ERS ON EDP AND ACMP. REPLACED LEFT HYDRAULIC SYSTEM PRESS TUBE ABOVE LEFT PYLON PRESS MODULE, LEAK CHECKS GOOD. SERVIC ED LEFT HYDRAULIC RESERVOIR. 2 L 7 2 4F RT A2NM 1998080700642 19980807 00642 NM 1998 8 7 UPS98227282 1 19980630 A 5311 FRAME BOEING 727 72730C 1384009 NM BS 294 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-221-01.00-01) ON FRAME AT STA 294 LBL 57 WL 236 TO 239. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998080700643 19980807 00643 NM 1998 8 7 UPS98227283 1 19980731 A 5312 BULKHEAD BOEING 727 72730C 1384009 NM BS 1183 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON BS 1183 BULKHEAD RBL 15 WL 178. REMOVED CORROSION AND ACCOMPLISHED EO B727-5311-0635 WITH THE ADDITION OF EXTENDING THE RBL 8 BULKHEAD DOUBLER TO ENCOMPASS THE CORRODED AREA. 2 L 7 3 4F A3WE 1998080700644 19980807 00644 NM 1998 8 7 UPS98227284 1 19980728 A 5330 6518382298 SKIN BOEING 727 72730C 1384009 NM BS 1120-1150 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, DISHED RIVETS AND PILLOWED SKIN STA 1120 TO 1150 LT 3 STR TO STR 4 LT AND 3 STR RT TO 4 STR RT. REP LACED SKIN PER EO 98-2608. 2 L 7 3 4F A3WE 1998080700645 19980807 00645 NM 1998 8 7 UPS98227285 1 19980617 A 5320 69144925 SPLICE BOEING 727 72730C 1384009 NM BS 442-436 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 25L SPLICE AT BS 442, BS 436. CORROSION FOUND TO BE OUT OF LIMI TS PER SRM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-2, 51-30-5, AND SRM 51-30-6. 2 L 7 3 4F A3WE 1998080700646 19980807 00646 NM 1998 8 7 UPS98227286 1 19980617 A 5320 69144925 SPLICE BOEING 727 72730C 1384009 NM BS 443 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STR 25R SPLICE AT BS 443. CORROSION FOUND TO BE OUT OF LIMITS PER S RM 53-10-1. INSTALLED NEW SPLICE PER SRM 51-30-5, 51-30-2, AND MM 51-30-00. 2 L 7 3 4F A3WE 1998080700647 19980807 00647 NM 1998 8 7 UPS98227287 1 19980617 A 5320 69162761 BRACKET BOEING 727 72730C 1384009 NM BS 203.8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON NOSE COMPARTMENT DOOR STOP BRACKET, FWD SIDE OF BS 203.8 BRACKET, LB L 8. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. NEW FITTING INSTALLED IAW SRM 52-40-21 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998080700648 19980807 00648 NM 1998 8 7 UPS98227288 1 19980711 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON NUT PLATES AT BS 740 FLOORBEAM RBL 60 TO LBL 60 WL 208. REMOVED FLO ORBEAM AT BS 740 LBL 6, RBL 60, INSTALLED FABRICATED FLOORBEAM IAW SRM 51-30-2, 53-104. 2 L 7 3 4F A3WE 1998080700649 19980807 00649 NM 1998 8 7 UPS98227289 1 19980731 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM ON AND AT NUT PLATES BS 760 TO 848 LBL 45 WL 208. CORRODED PART OUT OF LIMITS. FABRICATED AND INSTALLED NEW REPAIR PARTS IAW SRM 51-30-2, 51-10-2, 51-20 -21, 51-20-151, 51-30-4. 2 L 7 3 4F A3WE 1998080700650 19980807 00650 NM 1998 8 7 UPS98227290 1 19980706 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 760-848 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-02) ON FLANGES OF LONGITUDINAL FLOORBEAM AND NUT PLATES BS 760 TO 848, WL 2 08 RBL 45. REPLACED LONGITUDINAL FLOORBEAM AND SEAT TRACK (NRC 832504) BS 760 TO 848 PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998080700651 19980807 00651 NM 1998 8 7 UPS98227291 1 19980710 A 5320 ANGLE BOEING 727 72730C 1384009 NM BS 804 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, POSSIBLE CRACK IN FLOORBEAM SUPPORT ANGLE BS 804, LBL 46, WL 206. FLOORBEAM SUPPORT CRACKED, VERIFI ED BY NDI. REPLACED SUPPORT ANGLE PER 727 SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1998080700652 19980807 00652 NM 1998 8 7 UPS98227292 1 19980618 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON UPPER CHORD OF FLOORBEAM AT FASTENER HOLE BS 312, LBL 3, WL 208. CO RROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW SRM 53-10-8, 51-30-5, 51-30-2, A ND MM 51-20-151. 2 L 7 3 4F A3WE 1998080700653 19980807 00653 WP 1998 8 7 UPS98827281 1 19980714 A 5320 3755822502 FITTING DOUG DC8 DC873F 302199F WP BS 350 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE-C-CK, AFT SIDE OF STA 350, L36 TO L35L FITTING CRACKED. REMOVED FITTING, DRILLED AND INSTALLED NEW ONE IAW DC8 SRM 53-2-0 AND 51-1-21. 2 L 7 4 4F RT 4A25 1998080700654 19980807 00654 WP 1998 8 7 UPS98827293 1 19980719 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 297.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT WS XFS 297.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998080700655 19980807 00655 NM 1998 8 7 98FDEA00484 1 19980804 A 3230 656021123 CONTROL MODULE BOEING 727 7272S2F 1384O81 NM E/E COMPT INOPERATIVE A FDEA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 25 217FE 22938 DURING LANDING GEAR RETRACTION, GEAR HANDLE WOULD NOT RAISE PAST OFF. COMPLIED WITH RED TABS. LANDED WITH DOWN IN GREE N. *S/D* DUPLICATED PROBLEM. REMOVED AND REPLACED LAND GEAR CONTROL MODULE PER M/M 32-09-121, TESTS NORMAL. REMOVED AND REPLACED LANDING GEAR LOCK SOLENOID PER M/M 32-31-16, TESTS NORMAL. CLEANED AIR/GROUND SENSORS. SYSTEM CHECKS NORM AL. PER M/M OPERATON CHECKS. 2 L 7 3 4F A3WE 1998080700656 19980807 00656 NM 1998 8 7 98FDEA00485 1 19980804 A 5313 6534144109 LONGERON BOEING 727 72725C 138400H NM BS 760 - 857 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 STA-PAE: CORROSION ON LONGITUDINAL BS 836 AND 839, RBL 45, WL 208.1. *S/D* REMOVED DAMAGE LONG BEAM FROM BS 760-850, RBL 45, WL 208.1 AND REPLACED PER FEDEX DRAWING 65-34144. 2 L 7 3 4F A3WE 1998080700657 19980807 00657 WP 1998 8 7 98FDEA00486 1 19980803 A 5313 LONGERON DOUG DC10 DC1010F 3022111 WP BS 1811 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 056FE 47810 STA-LAX: AFT CARGO COMPT 6 INCH CRACK IN LONGERON 47L AT BS 1811. *S/D* ROUTED OUT DAMAGE AREA, VERIFY CRACK REMOVE B Y NDT HFEC INSP. FABRICATE FILLER STRAPS, INNER AND OUTER DOUBLER PER EA 8-5330-38595. INSTALL PARTS PER EA 8-5330-385 95. 2 L 7 3 4F A22WE 1998080700658 19980807 00658 NM 1998 8 7 98FDEA00487 1 19980803 A 5330 65401398 BEAR STRAP BOEING 727 72721C 138400M NM BS 475 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 144FE 19137 STA-PAE: CORROSION (C53-224-02) INNER SKIN EMANATING FROM UNDER BEAR STRAP AT BS 475 BETWEEN STRINGER 3 AND 4 LT. 2 L 7 3 4F A3WE 1998080700659 19980807 00659 NM 1998 8 7 98UAL900353 1 19980725 A 2750 MECHANISM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT TE FLAP OUT OF ADJUST A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 7460U 21914 AT 20,000 FEET AND 350 KNOTS GOT RIGHT FLAP FLUTTER. PASSENGER SAW RIGHT HAND OUTBOARD AFT FLAP FLUTTER 4 INCHES WITH F LAPS UP. RETURNED TO DEN. *S/D* ADJUSTED OUTBOARD TRAILING EDGE FLAP ECCENTRICS. SYSTEM CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998080700660 19980807 00660 NM 1998 8 7 98UAL900354 1 19980725 A 3610 9750025001 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 BLEED AIR FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7258U 21405 NR 2 BLEED OVERHEAT LIGHT ILLUMINATED. RETURNED TO ORD. *S/D* REPLACED AIR DUCT OVER TEMPERATURE SWITCH. 2 L 7 3 4F 4 F A3WE E2EA 1998080700661 19980807 00661 NM 1998 8 7 98UAL900355 1 19980724 A 2910 FITTING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE B-HYD SYST LOOSE A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 309UA 23670 B-HYDRAULIC SYSTEM LOW PRESSURE LIGHT CAME ON IN FLIGHT AFTER LOSS OF B-HYDRAULIC SYSTEM QUANTITY. *S/D* AIRCRAFT MAIN TENANCE TECHNICIAN FOUND T-FITTING LEAKING IN THE RIGHT WHEEL WELL. SECURED FITTING. FILLED AND PRESSURE CHECKED, NO L EAKS FOUND. ALSO, REPLACED B-SYSTEM ELECTRIC AND ENGINE DRIVEN PUMP, BOTH B-SYSTEM CASE DRAIN FILTERS. OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1998080700662 19980807 00662 NE 1998 8 7 98UAL900356 2 19980712 A 7230 COMPRESSOR PWA PW4077 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 ENGINE FOD A UALA H DEACTIVATE SYST/CIRCUITS B E SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET DE DESCENT 1 WP 29 774UA 777034 26936 777034 CREW REPORTED AT TOP OF DESCENT WHEN THROTTLES RETARDED, SMOKE FILLED CABIN AND COCKPIT. TURNED OFF NR 1 BLEED AND PACK . SMOKE CLEARED. ENGINE VIBRATION ALSO REPORTED. ENGINE REPLACED AT IAD FOR OIL IN THE GAS PATH. ON ENGINE DISASSEMB LY A FOREIGN OBJECT WAS FOUND IN THE OIL SYSTEM. A PIECE OF CARDBOARD ABOUT ONE INCH SQUARE WAS FOUND LOOSE IN THE NR 1 - NR 2 BEARING COMPARTMENT AREA. THE CARDBOARD WAS REMOVED. THE ENGINE WAS REASSEMBLED, TESTED AND RETURNED TO SERVIC E WHERE IT HAS BEEN OPERATING NORMALLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998080700663 19980807 00663 NM 1998 8 7 98UAL900357 1 19980724 A 3350 LIGHT BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 180UA 25224 EMERGENCY LIGHT ASSEMBLY PANEL INOP IN DOOR 1 LEFT. REPLACED ASSEMBLY AND OP'S CHECKED OK. 2 L 7 4 4F 4 F RT A20WE E24NE 1998080700664 19980807 00664 NM 1998 8 7 98UAL900358 1 19980725 A 3350 POWER PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 175UA 24382 UPPER DECK LEFT EMERGENCY EXIT LIGHT WILL NOT TURN OFF. REPLACED POWER PACK. 2 L 7 4 4F 4 F RT A20WE E24NE 1998080700665 19980807 00665 NM 1998 8 7 98UAL900359 1 19980725 A 3350 BATTERY BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 161UA 21352 OUTBOARD EMERGENCY FLASHLIGHT AT FLIGHT ATTENDANTS SEAT NEXT TO DOOR 3 RIGHT NEEDS TO BE REPLACED. REPLACED BATTERY AND REINSTALLED FLASHLIGHT, OP'S CHECKED GOOD. 2 L 7 4 4F 4 F A20WE E20EA 1998080700666 19980807 00666 NM 1998 8 7 98UAL900360 1 19980727 A 3350 POWER SUPPLY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 650UA 25287 EMERGENCY EXIT FLOOR LIGHTS DAMAGED ROWS 30 TO 36. FLOOR LIGHTS TURN ON AND OFF. *S/D* REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A1NM E24NE 1998080700667 19980807 00667 NE 1998 8 7 98UAL900361 2 19980728 A 7230 1B7306 BLADE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE RT ENGINE CRACKED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 559UA 4080 26657 717982 THREE LOUD JOLTS CAME FROM RIGHT ENGINE DURING CLIMB. *S/D* ENGINE WAS REPLACED AND A FAILED 6TH STAGE HPC BLADE WAS D ISCOVERED AFTER ENGINE DISASSEMBLY. THE UA INVESTIGATION FOUND THAT A 6TH STAGE BLADE HAD FAILED DUE TO FATIGUE CRACKIN G ORIGINATING 2/3 OF THE WAY DOWN THE CONVEX AIRFOIL MID SPAN. THE BLADE IS BEING RETURNED TO PWA FOR INVESTIGATION. 2 L 7 2 4F 4 F RT A2NM E17NE 1998080700668 19980807 00668 NE 1998 8 7 98UAL900362 2 19980727 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE STALLED A UALA A J UNSCHED LANDING DUMP FUEL R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 643UA 27027 8772 25093 724462 NR 2 ENGINE HEAVY COMPRESSOR STALL AT 200 FEET AGL. REDUCED THRUST TO FLIGHT IDLE, JETTISONED FUEL. RETURNED TO MIA AM BER ALERT, OVERWEIGHT LANDING. *S/D* ENGINE SURGE WAS DUE TO GENERAL DETERIORATION OF THE HIGH PRESSURE COMPRESSOR. T HE ENGINE WAS REMOVED AND WILL BE REFURBISHED TO PHASE 3 STANDARDS. 2 L 7 2 4F 4 F RT A1NM E24NE 1998080700669 19980807 00669 EU 1998 8 7 98UAL900363 1 19980727 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 403UA 442 EMERGENCY EXIT LIGHT TEST FAILED. MESSAGE LEFT COM, EXTERNAL FAULT CODE ON EPSU. 2 L 7 2 4F 4 F RT A28NM E40NE 1998080700670 19980807 00670 NE 1998 8 7 98UAL900364 2 19980728 A 7530 LVDT HAMILTON STD BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 3 ENGINE FAILED A UALA O OTHER X ENGINE FLAMEOUT NR NOT REPORTED 1 WP 29 104UA F18799 26902 727304 POSSIBLE BIRD STRIKE ON NR 3 ENG FOLLOWED BY FLAME OUT. EGT MAX WAS ABOUT 510 DEGS. *S/D* ENGINE FLAME OUT IN DESCENT DUE TO STATOR VANE ACTUATOR LVDT FAILURE. ACTUATOR HAS NOT BEEN TESTED OR DISASSEMBLED YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998080700671 19980807 00671 EU 1998 8 7 98UAL900366 1 19980729 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 EMERGENCY ESCAPE PATH LIGHTS INOP AT 16ABC, 17, 18, 22, 23, 24ABC. 2 L 7 2 4F 4 F RT A28NM E40NE 1998080700672 19980807 00672 EU 1998 8 7 98UAL900367 1 19980728 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 416UA 479 EMERGENCY LIGHT BROKEN OFF. 2 L 7 2 4F 4 F RT A28NM E40NE 1998080700674 19980807 00674 EU 1998 8 7 98UAL900369 1 19980728 A 3260 LGICU AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 405UA 452 LANDING GEAR FAILED TO RETRACT. NR 1 LGICU FAULT. RETURNED TO ATL. NORMAL LANDING. *S/D* FOUND TARGET FOR PROX SENS OR 24GA LOOSE OR MISSING. RETORQUED BOLT AT BRACKET, OP CHECKS GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 1998080700675 19980807 00675 WP 1998 8 7 ABXA9800674 1 19980620 A 5730 5643000 SKIN DOUG DOUG DC8 DC861F 3021953 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 CRACK IN TRAILING EDGE SKIN FORWARD OF NR 2 SPOILER BOARD OUTBOARD CENTER HINGE. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998080700676 19980807 00676 WP 1998 8 7 ABXA9800675 1 19980618 A 5320 5616306 WEB DOUG DOUG DC8 DC861F 3021953 WP BS 870 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT MAIN GEAR WHEEL WELL LOWER SUPPORT WEB CRACKED AT FS 870. REPAIRED WEB IAW DC8 SRM 53-2-0 AND 51-1-21. 2 L 7 4 4F 4A25 1998080700677 19980807 00677 WP 1998 8 7 ABXA9800676 1 19980618 A 5320 5751452 WEB DOUG DOUG DC8 DC861F 3021953 WP PAX DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT AFT ENTRY DOOR LOWER FORWARD CORNER WEB IS CRACKED. REPAIRED WEB IAW DC8 SRM 52-01 FIG 8. 2 L 7 4 4F 4A25 1998080700678 19980807 00678 WP 1998 8 7 ABXA9800677 1 19980618 A 5320 5615463219 WEB DOUG DOUG DC8 DC861F 3021953 WP PAX DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT FORWARD ENTRY DOOR WEB IS CRACKED BELOW LOWER HINGE CUTOUT. REPLACED LOWER WEB IAW DRAWING 5615463 AND DC8 SRM 51- 1-21. 2 L 7 4 4F 4A25 1998080700679 19980807 00679 WP 1998 8 7 ABXA9800678 1 19980618 A 5730 57189634 SKIN DOUG DOUG DC8 DC861F 3021953 WP WS 6.225 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 RIGHT WING LEADING EDGE LOWER SKIN AT STATION XOLDI 6.225 IS CRACKED. REPAIRED LEADING EDGE SKIN IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1998080700680 19980807 00680 WP 1998 8 7 ABXA9800679 1 19980618 A 5320 37502571 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 31R BETWEEN STATION 1040 TO 1060 SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 53-1-0 AND 51- 1-20D. 2 L 7 4 4F 4A25 1998080700681 19980807 00681 WP 1998 8 7 ABXA9800680 1 19980618 A 5320 37502571 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 31R SPLICE FITTING BETWEEN STATION 440 TO 460 IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 53-1-0 AND 51-1- 20D. 2 L 7 4 4F 4A25 1998080700682 19980807 00682 WP 1998 8 7 ABXA9800681 1 19980618 A 5320 9754069 MEMBRANE DOUG DOUG DC8 DC861F 3021953 WP BS 1480-1500 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT CUSP MEMBRANE AT STATION 1480 TO 1500 IS CRACKED. REPAIRED CUSP MEMBRANE IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998080700683 19980807 00683 WP 1998 8 7 ABXA9800682 1 19980618 A 5712 57695723 RIB DOUG DOUG DC8 DC861F 3021953 WP WS 716.250 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT WING LEADING EDGE RIB AT STATION XFS 716.250 IS CRACKED AT AFT LOWER END. REPAIRED RIB IAW DRAWING K05056. 2 L 7 4 4F 4A25 1998080700684 19980807 00684 WP 1998 8 7 ABXA9800683 1 19980618 A 5712 576957123 RIB DOUG DOUG DC8 DC861F 3021953 WP WS 778.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT WING LEADING EDGE RIB AT STATION XFS 778.750 IS CRACKED AT THE AFT LOWER END. REPAIRED RIB IAW DRAWING K05056. 2 L 7 4 4F 4A25 1998080700685 19980807 00685 NM 1998 8 7 VNAA9807014 1 19980731 A 7712 3037603 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 426JS 22969 45 3038 AN ECU FAIL WARNING MESSAGE ILLUMINATED DURING CLIMB. THE CREW ATTEMPTED A RESET OF THE ECU. THE ATTEMPT FAILED AND TH E AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED THE 1.8 SENSOR IN ACCORDANCE WITH DORNIER MAINTENA NCE MANUAL 73-21-02. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998080700837 19980807 00837 NM 1998 8 7 TWAA9812601 1 19980804 A 3350 0202175007 LIGHT BOEING 767 767330 NM CABIN WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 DURING OVERNIGHT MAINT FOUND EGRESS LIGHT STRIP FWD OF AFT LAV WAS INOPERATIVE. REPLACED LIGHT STRIP. CHECK-C 5-23-98 LAX. 2 L 7 2 4F RT A1NM 1998080700838 19980807 00838 WP 1998 8 7 VJ9800272 1 19980717 A 5347 29559781200 CARGO TRACK DOUG DC9 DC932 3022066 WP BS 270-390 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 FORWARD LT CARGO TRACK CORRODED BEYOND LIMIT AT STA 270-390. REMOVED CORROSION IAW DC9 SRM 53-01, FIG 1, AND FABRICATED TIE DOWN TRACK MATERIAL, 102 1/2 BY 1 INCH, IAW DC9 SRM 53-21-0. TREATRED CARGO TIE DOWN TRACK IAW DC9 SRM 51-10-3. 2 L 7 2 4F A6WE 1998080700839 19980807 00839 WP 1998 8 7 VJ9800273 1 19980728 A 5330 1A3566835670 SKIN DOUG DC9 DC932 3022066 WP BS 579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 INTERNAL SKIN IN FWD PIT CORRODED AT STA 579. REMOVED END CAPS FROM 25L TO 25R, FRAME AND SHEAR TIES AT STA 579 AND COR ROSION IAW DC9 SRM 51-10-3. FABRICATED AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW DC9 SRM 53-04, FIG 43, AND RES 981100. REPLACED CRACKED LONGERON AND CAPS 25L, 26L AND 30L. REINSTALLED ALL REMOVED PARTS IAW DC9 SRM 51-30-2 AND 51- 30-5. 2 L 7 2 4F A6WE 1998080700840 19980807 00840 WP 1998 8 7 VJ9800274 1 19980731 A 5313 1A3551835519 LONGERON DOUG DC9 DC932 3022066 WP BS 346 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 FWD CARGO COMPARTMENT UPPER FLANGE OF LONGERON 27R, FS 346, CORRODED BEYOND LIMIT. CUT OUT CORRODED SECTION OF LONGERON AND SPLICED IN NEW SECTION IAW DC9 SRM 51-10-4, 51-10-3, 53-02, FIG 18. 2 L 7 2 4F A6WE 1998080700841 19980807 00841 WP 1998 8 7 VJ9800275 1 19980731 A 5311 1A3360235408 FRAME DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 CABIN FRAME BETWEEN CABIN FLOOR AND CENTER TANK AT STA 617, RBL 58, CRACKED. HFEC INSPECTION VERIFIED CRACK IN RADIUS T O BE TWO INCHES FROM LOWER END OF PART. STOP DRILLED CRACK IAE EO 9-53-006. HFEC VERIFIED STOP DRILLED CRACKS, SHOT PE ENED ENTIRE FRAME, TREATED AND PRIMED FRAME STA 617 IAW DC9 SRM 51-10-3. BONDED CHANNNEL 2014 AND CLIP 202 PER AIW EO 9 -53-006. INSTALLED WINDOW FRAME STA 598-617 598-617. 2 L 7 2 4F A6WE 1998080700842 19980807 00842 NE 1998 8 7 PNSA980801 2 19980803 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 685PA 212 785533 DURING CLIMB, LT ENGINE ITT BEGAN TO FLUCTUATE. CREW WAS UNABLE TO CONTROL FLUCTUATION. ENGINE WAS SECURED AND AIRCRAF T RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. 2 L 7 2 4T 4 T RT A52EU E8NE 1998080700843 19980807 00843 NM 1998 8 7 CALA9801384 1 19980802 A 3260 LOGIC CARDS BOEING 737 7373T0 1384582 NM E/E COMPT INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 14342 23580 THE LANDING GEAR HANDLE WOULD NOT MOVE ABOVE THE OFF POSITION AFTER TAKEOFF. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE GEAR HANDLE RAISED. MAINTENANCE REMOVED AND REPLACED THE M990 AND M991 LOGIC CARDS IAW MM 32-09-20. OPERATION OF THE LANDING GEAR CONTROL LEVER LOCK SOLENOID WAS CHECKED IAW MM 32-31-31 AND ALL TESTED NORMAL. 2 L 7 2 4F RT A16WE 1998080700844 19980807 00844 WP 1998 8 7 CALA9801385 1 19980803 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1087 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND A .75 INCH CRACK IN FUSELAGE SKIN AT STA 1087, LONGERON 2L. REPAIRED IAW SRM 53-04, FIGURE 27. 2 L 7 2 4F A6WE 1998080700845 19980807 00845 WP 1998 8 7 CALA9801386 1 19980804 A 5320 FLANGE DOUG DC10 DC1010 3022110 WP BS 1129 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND CORROSION ON CAC LOWER FLANGE AT STA 1129 BETWEEN LONGERON 50L AND 50R. THE CORRODED AREA WAS CLEANED. THE AREA WAS REWORKED AND REINFORCED WITH TWO FRAME SPLICES IAW SRM 53-30-00, FIGURE 5, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998080700846 19980807 00846 WP 1998 8 7 CALA9801387 1 19980805 A 5720 WEB DOUG DC10 DC1010 3022110 WP WS 46 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND CRACKS IN CENTER WING BOX WEBS AT STA XCWR46, XCWL46, XCWR17, AND XCWL18. ALL CRACKS WERE TRIMMED AND BLENDED OUT. REWORKED AREAS AND REINFORCED WITH DOUBLERS AND FILLERS IAW SRM 57-00-01, FIGURE 1, 51-21-03, AND 51-30-02 . 2 L 7 3 4F A22WE 1998080700847 19980807 00847 WP 1998 8 7 CALA9801388 1 19980805 A 5414 SKIN DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL UPPER SKIN HOLES ELONGATED AND CRACKED. THE PYLON UPPER SKIN WAS REMOVE D, NEW SKIN WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998080700848 19980807 00848 WP 1998 8 7 CALA9801389 1 19980804 A 5414 SKIN DOUG DC9 DC932 3022066 WP NR 1 PYLON CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND NR 1 PYLON TRAILING EDGE PANEL LOWER SKIN DELAMINATED AND CORRODED. SKIN AND FINGER DOUBLERS WERE FABR ICATED AND INSTALLED IAW SRM 54-30-0, 51-30-8, AND 51-30-2. 2 L 7 2 4F A6WE 1998080700849 19980807 00849 WP 1998 8 7 CALA9801390 1 19980805 A 2550 SKIN DOUG DC9 DC932 3022066 WP BARRIER DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15525 47531 INSPECTION FOUND AFT CARGO BARRIER DOOR SKIN CRACKED AND DELAMINATED ON INBOARD SIDE WITH A PUNCTURE ON OUTBOARD SIDE. T HE DOOR WAS DISASSEMBLED. THE OUTER SKIN WAS REMOVED AND THE PUNCTURED AREA WAS TRIMMED OUT. NEW SKIN AND DOUBLERS WER E FABRICATED AND INSTALLED IAW SRM 53-21, FIGURE 15. THE DOOR WAS REASSEMBLED IAW MM 51-70-2 AND 51-30-2. 2 L 7 2 4F A6WE 1998080700850 19980807 00850 WP 1998 8 7 UPS98827294 1 19980717 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 304 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, RT WING L/E TOP SKIN AT WS XFS 304.0 FRONT SPAR HAS HEAVY CORROSION, UNDER THE SURFACE. REPAIRED IAW DHC SK 755-816. 2 L 7 4 4F RT 4A25 1998080700851 19980807 00851 WP 1998 8 7 UPS98827295 1 19980722 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, FS 1520 LONGERON 33R INTERCOSTAL HAS CRACK. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOST AL IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700852 19980807 00852 WP 1998 8 7 UPS98827296 1 19980714 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 300 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE C-CK, FS 300 BETWEEN LONG 36 AND 35L HAS CRACKED FITTING. REMOVED FITTING IAW DC8 SRM 52-1-20D, RECEIVE D AND CUT FITTING AS NEEDED FOR REPLACEMENT IAW DC8 SRM 52-2-0 FIG 2D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTA LLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700853 19980807 00853 WP 1998 8 7 UPS98827297 1 19980714 A 5320 3755826501N FITTING DOUG DC8 DC873F 302199F WP BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 804UP 46004 INSPECTION TYPE C-CK, FS 340 AT LONG 31L FITTING HAS CRACK. REMOVED FITTING AND FOUND TO BE CRACKED IAW 51-1-20D. RECE IVED, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-24 AND 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998080700854 19980807 00854 NM 1998 8 7 QXEA9801052 1 19980802 A 3231 54C546349 VALVE DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR MALFUNCTION A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 814PH 667 43 LEFT MAIN GEAR DOOR REMAINED OPEN AFTER LANDING GEAR RETRACTION. AFTER CYCLING GEAR, THE DOOR CLOSED NORMALLY. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN PDX, REPLACED THE NR 1 MAIN GEAR DOOR PROXIMITY SENSOR AND THE SEQUENCE VALVE . OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998080700855 19980807 00855 EU 1998 8 7 QXEA9801053 1 19980802 A 3310 BULB FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 488US 11240 SMOKE CAME OUT OF FIRST OFFICER'S GLARESHIELD. AFTER TURNING OFF ALL LIGHT RHEOSTATS AND SWITCHES THE SMOKE STOPPED. M AINTENANCE FOUND THE FIRST OFFICER'S GLARESHIELD RED TUBE LIGHT BURNT. REMOVED AND REPLACED RED TUBE LIGHT. TURNED ON ALL GLARESHIELD LIGHTING AND OPERATIONALLY TESTED WITH NO DEFECTS NOTED. 2 L 7 2 4F RT A20EU 1998080700856 19980807 00856 EU 1998 8 7 QXEA9801054 1 19980731 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 480AU 11229 SEVERAL LIGHTS OUT ON CENTER CABIN OVERHEAD EXIT SIGN. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998080700857 19980807 00857 EU 1998 8 7 QXEA9801055 1 19980802 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 OVERHEAD EMERGENCY EXIT SIGN AT ROW 8, FACING AFT IS INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998080700858 19980807 00858 1998 8 7 98FDEA00488 2 19980805 A 7200 ENGINE BOEING 727 727233 138408A NM NR 2 MALFUNCTIONED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 220FE 20934 NR 2 ENGINE JUST AFTER LIFTOFF OIL PRESSURE WENT TO 5 PSI WITH GOOD OIL QUANTITY. OIL FILTER BYPASS/LOW OIL PRESSURE LI GHT CAME ON. *S/D* REMOVED ACCESSORY DRIVE GEARBOX OIL FILTER AND MAIN OIL PUMP. REMOVED AND REPLACED NR 2 ENG FIREWA LL PLUG AND NR 2 ENG PER WORK CARD 70T0002. ENG RUN AND LEAK CK GOOD. 2 L 7 3 4F RT A3WE 1998080700859 19980807 00859 NM 1998 8 7 DL72S981592 1 19980801 A 5330 65545644 SKIN BOEING 727 727232 1384082 NM BS 560 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 CORROSION WAS FOUND IN THE SKIN AT THE STRINGER 26L LAP SPLICE. THE CORRODED AREA WAS TRIMMED OUT AND AN EXTERNAL ALUMI NUM REPAIR DOUBLER WAS INSTALLED. THE SKIN LAP WAS SEPARATED AND INSPECTED FWD AND AFT OF THE DAMAGED AREA AND WAS REST ORED WITH PROTRUDING HEAD OVERSIZE RIVETS PER THE B727 SRM. THE REPAIR WAS ACCOMPLISHED PER ER/A 365312-14 REV C. 2 L 7 3 4F A3WE 1998080700860 19980807 00860 NM 1998 8 7 DL72S981593 1 19980731 A 5330 65545644 SKIN BOEING 727 727232 1384082 NM BS 660 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 484DA 20864 THE FUSELAGE SKIN WAS FOUND CORRODED AT THE STRINGER 26L LAPSPLICE. THE CORRODED AREA WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 365330-14, REV B. 2 L 7 3 4F A3WE 1998080700861 19980807 00861 NM 1998 8 7 DL72S981594 1 19980731 A 5330 6518420483 SKIN BOEING 727 727232 1384082 NM BS 295 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 419DA 21272 THE FUSELAGE SKIN WAS BADLY DENTED AT FS 295 BETWEEN STR 12L AND 13L DUE TO A BIRD STRIKE. THE DAMAGED AREA WAS CUTOUT AND REPAIRED PER THE B727 SRM 53-30-3, FIG 1 WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS DOCUMENTED PER ER /A 365361-14 WHICH ADDED A DTA REQUIREMENT TO THE REPAIR. 2 L 7 3 4F A3WE 1998080700862 19980807 00862 NM 1998 8 7 DL757981595 1 19980730 A 5330 148N32145 SKIN BOEING 757 757232 1384965 NM BS 1720 TORN A DALA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 27 615DL 22822 THE FUSELAGE SKIN WAS BADLY GOUGED/TORN AT THE SKIN BUTT SPLICE AT FS 1720. THE DAMAGED AREA OF SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 365333-14, REV A. THE DAMAGED WAS CAUSED BY OVER ROTATION ON TAKEOFF. 2 L 7 2 4F RT A2NM 1998080700863 19980807 00863 NM 1998 8 7 DL72L981596 1 19980731 A 5521 657278419 SPAR BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 A TYPICAL CRACK WAS FOUND IN THE REAR SPAR OF THE LT ELEVATOR EXTENDING FROM UNDER THE SHEAR PLATE OF THE MIDDLE TAB FIT TING. THE CRACK EXTENDS .125 LONG BEYOND THE FITTING. THE CRACK WAS STOP DRILLED PER BAC S/B 727-55-0089 AND WILL BE R E-INSPECTED WITHIN 1600 HOURS WITH THE TERMINATING MOD ACCOMPLISHED IN 3200 HOURS. THE REPAIR WAS DOCUMENTED PE R ER/A 365359-14AD. 2 L 7 3 4F A3WE 1998080700864 19980807 00864 NM 1998 8 7 DL733981597 1 19980803 A 5330 SKIN BOEING 737 7373B7 1384580 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 951WP 22951 R1 DOOR CUTOUT SKIN CRACKED AT AFT LWR CORNER. INSTALLED REPAIR PER SRM 53-10-01 FIG 202. 2 L 7 2 4F RT A16WE 1998080700865 19980807 00865 NM 1998 8 7 DL76L981600 1 19980804 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 172DN 24775 EMERGENCY EXIT LIGHTS AT MID CABIN OVERWING DOOR INOP ON BOTH SIDES. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A1NM 1998080700866 19980807 00866 NM 1998 8 7 DL72L981601 1 19980804 A 2910 000AE954D0157 HOSE BOEING 727 727232 1384082 NM LT ELEVATOR LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 511DA 21313 AFTER T/O, LOST A-SYS HYD FLUID. RETURNED TO MSY. FOUND LEAKING SUPPLY LINE AT LEFT ELEVATOR PCU. REPLACED LINE. 2 L 7 3 4F A3WE 1998080700867 19980807 00867 NM 1998 8 7 DL72S981602 1 19980804 A 5320 FRAME BOEING 727 727232 1384082 NM R2 SERV DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 A 1 INCH CRACK FUSELAGE FRAME FWD SIDE AFT RT SVC DOOR UPPER STOP PAD. REPAIR PER M/M 53-13-0. 2 L 7 3 4F A3WE 1998080700868 19980807 00868 NM 1998 8 7 DL72S981603 1 19980728 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 FOUND DURING MV1 CORROSION VISIT NRC 78, 1.5 INCH CRACK AT STA 870 BULKHEAD AT LOWER SIDE OF APU AIR DUCT CUTOUT. REPAI RED PER SRM 53-10-9 FIG 5. 2 L 7 3 4F A3WE 1998080700869 19980807 00869 NM 1998 8 7 VNAA9808001 1 19980801 A 3240 AC69963 METERING UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE MLG BRAKES FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 438JS 66949 9701 3056 THE CREW REPORTED THAT THE BRAKES WOULD PULSATE ON AND OFF, WHEN THEY WERE APPLIED DURING TAXI. THE AIRCRAFT RETURNED T O THE GATE. MAINTENANCE INSPECTED AND REPLACED THE BRAKE METERING UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 3 2-42-03. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998080700870 19980807 00870 NM 1998 8 7 VNAA9808002 1 19980802 A 5101 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AIRFRAME BIRD STRIKE A VNAA K NONE C F.O.D. AP APPROACH 1 GL 07 442JS 3060 DURING APPROACH, THE CREW HEARD A BANG NOISE, AND SAW A FLOCK OF BIRDS FLY AWAY FROM THE AIRCRAFT. THE AIRCRAFT LANDED NORMALY, WITHOUT FURTHER PROBLEMS. MAINTENANCE INSPECTED THE AIRCRAFT FOR DAMAGE FROM A BIRD STRIKE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-51-00. NO DAMAGE WAS FOUND AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998080700871 19980807 00871 NM 1998 8 7 98UAL900059 1 19980210 A 2120 AIR DISTRIBUTION BOEING 777 777222 1385219 NM CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 795UA 26927 DURING FLIGHT AN OZONE SMELL WOULD OCCUR OFF AND ON, FOR ENTIRE FLIGHT. ALTITUDES WERE FL 370 AND 410. SUPPLEMENTAL DA TA UPDATE ON GROUND AT MIAMI, THE ODOR STILL PERSISTED UNTIL THE AIR CONDITIONING SYSTEM BURNOUT WAS PERFORMED. THERE WERE NO FURTHER REPORTS OF BAD ODOR ON SUBSEQUENT FLIGHTS. THE ODOR/SMELL PROBABLY CAME FROM A DIFFERENT SOURCE THAN OZ ONE BECAUSE THE SMELL PERSISTED ON THE GROUND AS WELL. ALSO, FLIGHT 733 FROM SFO TO MIA ON THAT PARTICULAR DAY OF THE Y EAR, AT FLIGHT LEVEL 370 TO 410 WAS NOT EXPOSED TO HIGH CONCENTRATION OF OZONE. 2 L 7 2 4F RT T0001SE 1998080700872 19980807 00872 NM 1998 8 7 DL73K981505 1 19980720 A 2910 LINE 000AE908T06 BOEING 737 737232 1384475 NM RROYCE ENGINE RUPTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 314DA 23086 LOSS OF A/B HYDRAULICS RESULTED IN DIVERSION BACK TO MCO. FOUND 01 ENG PRESS LINE RUPTURED. REPLACED SAME, LEAK CKS OK . REPLACED ALL CASE DRAIN FILTERS. 2 L 7 2 4F RT A16WE 1998080700873 19980807 00873 NM 1998 8 7 DL72S981514 1 19980721 A 5320 WEB BOEING 727 727225 1384077 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 VERTICLE WEB DAMAGED AT LIGHTNING HOLE RT SIDE STA 1263- 2. VERTICLE WEB DAMAGED AT LIGHTNING HOLE RT SIDE STA 1228. R EPAIRED PER M/M 53-11-0 PG 828. 2 L 7 3 4F A3WE 1998080700874 19980807 00874 NM 1998 8 7 DL72S981515 1 19980721 A 5320 WEB BOEING 727 727225 1384077 NM BS 1240 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 VERTICLE WEB CRACKED APPROX .25 INCH LONG AT LIGHTNING HOLE STA 1240. REPAIRED PER M/M 53-11-0 PG 832. 2 L 7 3 4F A3WE 1998080700875 19980807 00875 NM 1998 8 7 DL72S981516 1 19980721 A 5320 WEB BOEING 727 727225 1384077 NM BS 1224 PART A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 VERTICLE WEB CRACKED STA 1224 LBL 24 ABOVE EXISTING REPAIR. REPAIRED PER M/M 53-11-0 PG 832. 2 L 7 3 4F A3WE 1998080700876 19980807 00876 WP 1998 8 7 VJ9800234 1 19980718 A 5320 5924053015 BRACKET DOUG DC9 DC932 3022066 WP FWD LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 CORROSION DUST PARTICLES EMANATING FROM UNDER I/B WAS OF FWD LAVATORY AFT DOOR. THE CORROSION WAS FOUND TO BE LEVEL 2. REPLACED CORROSION BRACKET UNDER I/B WALL OF FED AV AFT DOOR AND ASSEMBLED COMPONETS IAW DC-9 MM 25-42-1. 2 L 7 2 4F A6WE 1998080700877 19980807 00877 WP 1998 8 7 ARWA9807129 1 19980722 A 2150 2680307MSF VALVE LKHEED 1011 10113851 WP AC COMPT STUCK OPEN A ARWA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LD LANDING 1 SO 19 306GB 1138 50 FT ABOVE TOUCH DOWN, ALL SMOKE DETECTORS AND MASTER SMOKE WARNING HORN AND LTS CAME ON. VERFIED SMOKE IN MAIN CABIN. AIRCRAFT LANDED IN MIAMI WITHOUT INCIDENT. NO EVIDENCE OF FIRE. RAN NR 1, 2, AND 3 ACM'S SEPARATELY AT HIGH POWER AF TER CHANGING ALL WATER SEPARATOR BAGS AND ZONE TRIM VALVE. NO SMOKE IN CABIN IAW MM 21-60-00, 21-50-00 AND 21-40-00. 2 L 7 3 4F RC A23WE 1998080700878 19980807 00878 WP 1998 8 7 VJ980238 1 19980726 A 2560 COVER DOUG DC9 DC932 3022066 WP R1 DOOR LOOSE A ZZDA K NONE O OTHER UK UNKNOWN 1 SO 15 935VV 47534 R1 DOOR EMERGENCY EVACUATION SLIDE CAME LOOSE FROM DOOR. INSTALLED SLIDE COVER LANYARD PINS IAW 25-62-0. NO OTHER DEFE CTS NOTED. 2 L 7 2 4F A6WE 1998080700879 19980807 00879 NM 1998 8 7 DL72L981530 1 19980722 A 5751 SKIN 570369002 BOEING 727 727232 1384082 NM LT AILERON DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 ON T/C, FOUND LEFT O/B AILERON DELAMINATED BEYOND SRM LIMITS. REPLACED LT O/B AILERON TRAILING EDGE WEDGE. 2 L 7 3 4F A3WE 1998080700880 19980807 00880 EU 1998 8 7 98FDEA00473 1 19980725 A 3610 9354M37G01 DUCT AIRBUS 310 A310203 EU NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 426FE 245 CLIMBING THRU 10,000 FT GOT NR 1 ENG NACELLE TEMP ADVISORY, TEMP AT 95 CELSIUS. CLOSED BLEED, NO HELP. OPENED NR 1 BLE ED AND RETARDED THROTTLE AND TEMP DECREASED. RESUMED CLIMB POWER AND TEMP AGAIN INCREASED TO 110C. FOUND HPT RECOUP D UCT BLOWN. REMOVED AND REPLACED DUCT. RAN ENGINE PER JRH. OPS CHECK OK. 2 L 7 2 4F RT A35EU 1998080700881 19980807 00881 WP 1998 8 7 TWAA9812201 1 19980728 A 3350 010560001 COVER DOUG DC9 DC983 3022083 WP CABIN LOOSE A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 EIBWD 49575 THE ESCAPE PATH LIGHTING NEAR REAR GALLEY HAD A LOOSE COVER. INSTALLED TRACK COVER. CHECK-C 2-6-98 MCI. 2 L 7 2 4F RT A6WE 1998081400001 19980814 00001 NM 1998 8 14 AALA981304 1 19980703 A 5320 ANGLE BOEING 727 727227 1384078 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND CRACK IN CORNER ANGLE INBOARD OF APU AIR BOX FLANGE. REMOVED AND REPLACED ANGLE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998081400002 19980814 00002 NM 1998 8 14 AALA981359 1 19980703 A 5320 DOUBLER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - LIGHT HOUSING AND SKIN DOUBLER CORRODED. TREATED AND PRIMED DOUBLER PER SRM 51-20-0, INSTALLED NEW LIGHT HOUSING PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998081400003 19980814 00003 NM 1998 8 14 AALA981261 1 19980619 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND HEAVY CORROSION ON STRINGER 27L AT STATION 560. INSTALLED NEW STRINGER SECTION AND 2 DOUBLERS PER SRM. (M) 2 L 7 3 4F A3WE 1998081400004 19980814 00004 NM 1998 8 14 AALA981260 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND BELL FRAME DENTED STATION 660 BETWEEN STRINGER 24R AND 25R. INSTALLED DOUBLER PER SRM 53-10-4 PAGE 5. (M) 2 L 7 3 4F A3WE 1998081400005 19980814 00005 NM 1998 8 14 AALA981259 1 19980619 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 360-445 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND CORROSION ON TOP OF CREASE ANGLE RBL 55, FS 360 TO 445. REMOVED AND REPLACED WITH NEW CREASE ANGLE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998081400006 19980814 00006 1998 8 14 ASAA9840071 4 19980522 A 2330 RECORDER BOEING 737 737490 1384715 NM CABIN MALFUNCTIONED A ASAA H DEACTIVATE SYST/CIRCUITS O OTHER NR NOT REPORTED 1 NM 01 768AS 27082 SEA - FLT 517 - DURING FLT SNA-SEA, CREW NOTICED ACRID SMELL IN FLT DECK. CO-PILOT INVESTIGATED AND OBSERVED PASSENGER ADDRESS TAPE REPORDUCER SMOKING. CREW PULLED TAPE REPRODUCER CIRCUIT BREAKER AND SMOKE STOPPED. AIRCRAFT LANDED IN SE A WITHOUT INCIDENT. MAINTENANCE VERIFIED CIRCUIT BREAKER PULLED AND COLLARED. AIRCRAFT WAS RELEASED PER MEL 25-10. MA INTENANCE SUBSEQUENTLY REPLACED TAPE REPRODUCER ON 5/29/98, OPS NORMAL. ORIGINAL TAPE REPORDUCER WAS SENT TO ASA AVIONI CS SHOP FOR TROUBLESHOOTING AND REPAIR. (M) 2 L 7 2 4F RT A16WE 1998081400007 19980814 00007 NM 1998 8 14 ASAA9810048 1 19980704 A 3350 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 16 WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998081400008 19980814 00008 NM 1998 8 14 ASAA9810047 1 19980702 A 3350 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - FLT 152 - PRIOR TO FLT, THE EMERGENCY EXIT LIGHTS ON PALLET NR 8 WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASS Y AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998081400009 19980814 00009 NM 1998 8 14 ASAA9810046 1 19980629 A 3350 BATTERY PACK BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THR GITH AFT PALLET EMERGENCY EXIT LIGHTS REMAINED ILLUMINATED WITH THE SWITCH 'OFF'. R EPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998081400010 19980814 00010 NM 1998 8 14 ASAA9810045 1 19980625 A 3350 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - PRIOR TO FLT 30, THE EMERGENCY EXIT LIGHTS ON PALLET 8-2 WOULD NOT EXTINGUISH. REPLACED BATTERY AND LIGHTS OPERAT ED NORMALLY. (M) 2 L 7 2 4F A16WE 1998081400011 19980814 00011 NM 1998 8 14 ASAA9810044 1 19980620 A 3350 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE NR 5 PALLET EMERGENCY EXIT TRACK LGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTE RY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998081400012 19980814 00012 NM 1998 8 14 ASAA9810043 1 19980620 A 3350 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE NR 2 PALLET EMERGENCY EXIT TRACK LIGHTS WOULD NOT EXTINGUISH WHEN TURNED OFF. REPLA CED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998081400013 19980814 00013 NM 1998 8 14 ASAA9810042 1 19980618 A 3350 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERA TED NORMALLY. (M) 2 L 7 2 4F A16WE 1998081400014 19980814 00014 NM 1998 8 14 ASAA9810041 1 19980612 A 3350 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998081400015 19980814 00015 NM 1998 8 14 ASAA9810040 1 19980607 A 3350 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE FORWARD WINDSCREEN 'EXIT TO REAR' LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTE RY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998081400016 19980814 00016 NM 1998 8 14 ASAA9840075 1 19980630 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 SEA - PRIOR TO FLT 68, THE AFT 5 EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998081400017 19980814 00017 NM 1998 8 14 ASAA9840073 1 19980622 A 3397 WIRE BOEING 737 7374Q8 NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE ILLUMINATING WITHOUT ANY MOVEMENT OF SWITCH. RESEATED WIRE IN EMERGENCY LIGHT SWITCH CANNON PLUG AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998081400018 19980814 00018 NM 1998 8 14 ASAA9840072 1 19980610 A 3350 CONNECTOR BOEING 737 7374Q8 NM CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 760AS 25098 KTN - FLT 73 - PRIOR TO FLT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROW 22-25 WOULD NOT ILLUMINATE DURING TEST. SECUR ED LOOSE CONNECTOR AT ROW 25 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998081400019 19980814 00019 WP 1998 8 14 ASAA9880120 1 19980705 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998081400020 19980814 00020 WP 1998 8 14 ASAA9880119 1 19980704 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 9 WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998081400021 19980814 00021 WP 1998 8 14 ASAA9880113 1 19980626 A 3350 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SFO - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WOULD NOT EXTINGUISH WHEN CONTROL SWIT CH PLACED TO OFF POSITION, WOULD EXTINGUISH WHEN SWITCH PLACED TO ARMED POSITION. REPLACED THE POWER SUPPLY AND OPERATE D NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998081400022 19980814 00022 WP 1998 8 14 ASAA9880112 1 19980625 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 942AS 53052 SEA - DURING MAINTENANCE CHECK, THE TAILCONE JETTISON HANDLE LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSY AND OPERA TED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998081400023 19980814 00023 WP 1998 8 14 ASAA9880111 1 19980625 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 27 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998081400024 19980814 00024 WP 1998 8 14 ASAA9880108 1 19980618 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998081400025 19980814 00025 WP 1998 8 14 ASAA9880101 1 19980604 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND DIM. REPLACED SECOND FROM FORWARD LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998081400026 19980814 00026 WP 1998 8 14 ASAA9880100 1 19980604 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE RED EMERGENCY FLOOR TRACK LIGHT AT THE AFT GALLEY WAS FOUND INOPERATIVE. REPLACED L AMP MODULE AT AFT GALLEY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998081400027 19980814 00027 WP 1998 8 14 ASAA9880097 1 19980603 A 3350 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998081400028 19980814 00028 NM 1998 8 14 TSAA9833346 1 19980625 A 3350 1000679 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED FORWARD SERVICE EXIT EMERGENCY LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400029 19980814 00029 NM 1998 8 14 TSAA9833347 1 19980625 A 3350 8731002511 LIGHT BOEING 737 737297 1384480 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED FORWARD SERVICE EXIT EMERGENCY LIGHT ASSY DUE TO NOT TESTING. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400030 19980814 00030 NM 1998 8 14 TSAA9833348 1 19980625 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 6 POSITION EMERGENCY LIGHT BATTERY PACK REPLACED DUE TO BEING INOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400031 19980814 00031 NM 1998 8 14 TSAA9833349 1 19980625 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 4 POSITION EMERGENCY LIGHT BATTERY PACK REPLACED DUE TO BEING INOP. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400032 19980814 00032 NM 1998 8 14 TSAA9833350 1 19980625 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 1 POSITION EMERGENCY LIGHT BATTERY PACK REPLACED DUE TO BEING INOP. OPS CHECKED GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1998081400033 19980814 00033 NM 1998 8 14 TSAA9833351 1 19980626 A 3350 9221009 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY BATTERY PACK DUE TO INOP. OPS CHECKED OK. AIRCRAFT RE TURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998081400034 19980814 00034 NM 1998 8 14 TSAA9833352 1 19980626 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 1998081400035 19980814 00035 NM 1998 8 14 TSAA9833353 1 19980626 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 3 POSITION EMERGENCY EXIT LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998081400036 19980814 00036 NM 1998 8 14 TSAA9833360 1 19980701 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 2 POSITION EMERGENCY LIGHT ASSY BATTERY PACK DUE TO FAILING CHECK. OPS CHECKED OK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 1998081400037 19980814 00037 NM 1998 8 14 TSAA9833359 1 19980629 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400038 19980814 00038 NM 1998 8 14 TSAA9833358 1 19980629 A 3350 963100211 LIGHT BOEING 737 7372S2C 138448G NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400039 19980814 00039 NM 1998 8 14 TSAA9833357 1 19980629 A 3350 963100211 LIGHT BOEING 737 737297 1384480 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT ASSY DUE TO LIGHT STAYING ON. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998081400040 19980814 00040 NM 1998 8 14 TSAA9853342 1 19980602 A 5320 STIFFENER BOEING 737 737230C 1384472 NM BS 328 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 STIFFENER CRACKED ON THE FLOORBEAM AT BS 328 AND RBL 32. REPLACED MANUFACTURED AND REPLACED STIFFENER IAW BOEING SRM 53 -10-2. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400041 19980814 00041 NM 1998 8 14 TSAA9853343 1 19980602 A 5347 SEAT TRACK BOEING 737 737230C 1384472 NM BS 716 DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 SEAT TRACK AT BS 716 AND BL 24L DAMAGED BEYOND LIMITS. REPLACED SEAT TRACK PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1998081400042 19980814 00042 NM 1998 8 14 TSAA9853344 1 19980602 A 5347 SEAT TRACK BOEING 737 737230C 1384472 NM BS 597 DAMAGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 SEAT TRACK AT BS 597 AND BL 48R DAMAGED BEYOND LIMITS. REPLACED SEAT TRACK PER SRM 53-10-5. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1998081400043 19980814 00043 NM 1998 8 14 TSAA9853345 1 19980603 A 5320 CHANNEL BOEING 737 737230C 1384472 NM BS 328 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 CHANNEL ATTACHED TO FLOORBEAM WAS FOUND TO BE CRACKED IN 2 PLACES. CHANNEL LOCATED AT BS 328 AND BL 32R. REPAIRED IAW SRM 53-10-2 FIGURE 7. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400044 19980814 00044 NM 1998 8 14 TSAA9833369 1 19980702 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED BATTERY IN NR 3 POSITION FLOOR PROXIMITY LIGHT ASSY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F A16WE 1998081400045 19980814 00045 NM 1998 8 14 TSAA9833370 1 19980706 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400046 19980814 00046 NM 1998 8 14 TSAA9833371 1 19980706 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400047 19980814 00047 NM 1998 8 14 TSAA9833372 1 19980706 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998081400048 19980814 00048 NE 1998 8 14 PNSA980801A 2 19980803 A 7320 HMU WOODWARD 6068T72P09 SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE MALFUNCTIONED A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 685PA WYG54848 212 785533 DURING CLIMB, LT ENGINE ITT BEGAN TO FLUXUATE. CREW WAS UNABLE TO CONTROL FLUXUATION. ENGINE WAS SECURED AND AIRCRAFT RETURNED TO AIRPORT FOR AN UNEVENTFUL LANDING. REPLACED FUEL CONTROL (HMU) OPERATIONAL CHECK OK. 2 L 7 2 4T 4 T RT A52EU E8NE 1998081400049 19980814 00049 NM 1998 8 14 RAAA98B2039 1 19980804 A 3350 873100212 SIGN BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED EGRESS IDENTIFIER ASSY DUE FAILED. 2 L 7 3 4F A3WE 1998081400050 19980814 00050 NM 1998 8 14 CALA9801391 1 19980805 A 2420 CONNECTOR BOEING 737 7373T0 1384582 NM NR 2 GENERATOR FAILED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 59338 23576 THE NR 2 AND NR 3 TRANSFORMER RECTIFIER CIRCUIT BREAKERS POPPED ACCOMPANIED BY AN ELECTRICAL SMELL IN THE CABIN DURING C RUISE AT FL 310. THE AIRCRAFT LANDED AT CLE WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 GENERATOR D410 FIREWALL CANNO N PLUG BURNT. THE D410 PLUG AND A PIN SOCKET AND THE FIREWALL GENERATOR RECEPTACLE D3026 AND A PIN WERE REPLACED IN REF ERENCE TO WIRING DIAGRAM 24-21-21 AND STANDARD WIRE PRACTICES MANUAL 20-62-26. OPERATION OF THE NR 2 GENERATOR CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998081400051 19980814 00051 NM 1998 8 14 CALA9801392 1 19980805 A 5720 ANGLE BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND 2.5 INCH CRACK AT CURVED ANGLE AT OUTBOARD SIDE OF LT WING FIXED LEADING EDGE RIB SLAT STA 0. THE ANGL E WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3. 2 L 7 3 4F A3WE 1998081400052 19980814 00052 NM 1998 8 14 CALA9801393 1 19980805 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 380-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND SEAT TRACK CORRODED AT INBOARD AND OUTBOARD LEGS AND ALONG TOP AT BS 380 TO 420, RBL 45. THE SEAT TRAC K WAS REMOVED AND A NEW ONE WAS FABRICATED AND INSTALLED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998081400053 19980814 00053 NM 1998 8 14 CALA9801394 1 19980806 A 5320 SIDEWALL BOEING 727 727224 1384076 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN RT SIDEWALL OF NLG WHEEL WELL. THE CRACKED AREA WAS CUT OUT, A DOUBLER AND FITTING WERE FABRICATED AND INSTALLED IAW SRM 53-10-1. 2 L 7 3 4F A3WE 1998081400054 19980814 00054 NM 1998 8 14 CALA9801395 1 19980806 A 5320 SIDEWALL BOEING 727 727224 1384076 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 0.3 CRACK IN TOP LT PANEL OF NLG WHEEL WELL. THE AREA WAS REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998081400055 19980814 00055 NM 1998 8 14 CALA9801396 1 19980806 A 5320 HAT CHANNEL BOEING 727 727224 1384076 NM BS 320 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND FLOOR SUPPORT HAT CHANNEL CORRODED AT FORWARD LAV AREA, BS 320, RBL 15. THE HAT CHANNEL WAS REMOVED AN D A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-40-4. 2 L 7 3 4F A3WE 1998081400056 19980814 00056 NM 1998 8 14 CALA9801397 1 19980806 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 1129-1176 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND ANGLE AT LT AFT LAV FIXED FLOOR CORRODED AT BS 1129 TO 1176, RBL 25 TO 63. A DOUBLER WAS FABRICATED AN D INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998081400057 19980814 00057 NM 1998 8 14 CALA9801398 1 19980806 A 5320 PANEL BOEING 727 727224 1384076 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND THREE .5 INCH CRACKS IN TOP CENTER PANEL OF NLG WHEEL WELL. THE AREA WAS REPAIRED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998081400058 19980814 00058 NM 1998 8 14 CALA9801399 1 19980806 A 5320 CLIP BOEING 727 727224 1384076 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 1 INCH CRACK IN TIE CLIP IN AFT CARGO COMPARTMENT AT STA 1183, 36 INCHES BELOW LBL 9 BULKHEAD FITTING . THE TIE CLIP WAS REMOVED, A NEW TIE CLIP WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998081400059 19980814 00059 WP 1998 8 14 9809869878 1 19980802 A 3231 LATCH DOUG DC9 DC951 3022051 WP LT MLG DOOR INOPERATIVE A NWAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 GL 01 787NC 48149 DURING APPROACH, THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED WITH LANDING GEAR EXTENDED. THE FLIGHT CREW PERFORMED COM REFERENCE 2.32.3, INITIATED A GO-AROUND PROCEDURE, RECYCLED THE LANDING GEAR SYSTEM, AND LANDED AT DTW WITHOUT INCIDENT . NORMAL LANDING GEAR POSITION INDICATIONS WERE ACHIEVED WITH THE LANDING GEAR DOOR LIGHT ILLUMINATED. MAINTENANCE REP LACED THE LEFT MAIN LANDING GEAR UPLOCK ROLLER SPRING ASSEMBLY, THE LEFT AND RIGHT MAIN LANDING GEAR DOOR SKID PADS, AND REPAIRED THE LEFT AND RIGHT MAIN LANDING GEAR DOOR ASSEMBLIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998081400060 19980814 00060 SO 1998 8 14 COMA9810168 1 19980805 A 3397 W272000924 WIRE EMB 120 EMB120RT SO CABIN SHORTED A COMA K NONE L NO TEST NR NOT REPORTED 1 SO 01 179CA 120179 EMERGENCY FLOOR LIGHT SYSTEM CIRCUIT BREAKER TRIPPED. WOULD NOT RESET. REPAIRED SHORTED WIRE NR W272-0009-24. 2 L 7 2 4T RT A31SO 1998081400061 19980814 00061 SO 1998 8 14 COMA9810169 1 19980805 A 3350 1317 BULB EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 249CA 120230 EMERGENCY LIGHT AT ROW 7 IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 1998081400062 19980814 00062 SO 1998 8 14 COMA9810170 1 19980804 A 3350 1317 BULB EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 243CA 120212 CEILING EMERGENCY LIGHT ROW 6 IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 1998081400063 19980814 00063 EA 1998 8 14 COMA9860212 1 19980731 A 3040 16591 CONTROLLER CNDAIR CL600 CL6002B19 EA LT WINDSHIELD FAILED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 917CA 10413 5559 7017 LEFT WINDSHIELD HEAT INOPERABLE. REPLACED HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 1998081400064 19980814 00064 1998 8 14 UPS98527321 2 19980805 A 7532 BVCU BOEING 757 75724APF 1384969 NM RT ENGINE FAILED A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT LD LANDING 1 SO 01 452UP 25473 INSPECTION TYPE-N/A, RT ENG FLAMEOUT, RESTART NOT ATTEMPTED FOLLWING NORMAL APPROACH AND LANDING AFTER THRUST REVERSER S TOW. PERFORMED BITE TEST PROCEDURE PER MM 75-32-OOP201, FOUND RT ENG BVCU FAULTS. REPLACED BVCU FLT CREW RAN ENG GROUN D IDLE. CHECK PERFORMED BVCU BITE TEST AFTER RUN, NO FAULTS NOTED, FOUND SATISFACTORY. (P/N C8E38-12) (S/N 3005) ON, ( S/N 3069). 2 L 7 2 4F RT A2NM 1998081400065 19980814 00065 WP 1998 8 14 UPS98827299 1 19980727 A 5320 37502571 SPLICE DOUG DC8 DC871F 302199D WP BS 600-620 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LONG 31R SPLICE FITTING CRACKED FS 600 TO 620. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21D AND DWG 3750257-1N. 2 L 7 4 4F RT 4A25 1998081400066 19980814 00066 WP 1998 8 14 UPS98827300 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 847.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E RIB CRACKED AT WS XFS 847.5 UPPER AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400067 19980814 00067 WP 1998 8 14 UPS98827301 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 385.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E AT WS XFS385.25 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW 57-2-0. 2 L 7 4 4F RT 4A25 1998081400068 19980814 00068 WP 1998 8 14 UPS98827302 1 19980725 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS XFS 628.750 APPROX 2 FWD FROM T/E. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998081400069 19980814 00069 WP 1998 8 14 UPS98827303 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E AT WS 778.750 THE UPPER L/E RIB IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0 . 2 L 7 4 4F RT 4A25 1998081400070 19980814 00070 WP 1998 8 14 UPS98827304 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 691.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E AT WS 691.250 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400071 19980814 00071 WP 1998 8 14 UPS98827305 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 778.750 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER WS XFS 778.750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400072 19980814 00072 WP 1998 8 14 UPS98827306 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 697.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E AT WS XFS 697.5 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400073 19980814 00073 WP 1998 8 14 UPS98827307 1 19980727 A 5320 SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LONGERON SPLICE FITTING CRACKED FS 440 TO 460 L-31R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998081400074 19980814 00074 WP 1998 8 14 UPS98827308 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E AT WS XFS 597.5 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400075 19980814 00075 WP 1998 8 14 UPS98827309 1 19980725 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT XFS 610 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998081400076 19980814 00076 WP 1998 8 14 UPS98827310 1 19980725 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS 597.500 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998081400077 19980814 00077 WP 1998 8 14 UPS98827311 1 19980725 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS XFS 616.25 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998081400078 19980814 00078 WP 1998 8 14 UPS98827312 1 19980725 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 603.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS 603.75 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998081400079 19980814 00079 WP 1998 8 14 UPS98827313 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 397.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E AT WS XFS 397.75 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400080 19980814 00080 WP 1998 8 14 UPS98827314 1 19980725 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E SKIN IS CRACKED AT WS XFS 304.00. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400081 19980814 00081 WP 1998 8 14 UPS98827315 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 772.5. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400082 19980814 00082 WP 1998 8 14 UPS98827316 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 810.000. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998081400083 19980814 00083 WP 1998 8 14 UPS98827317 1 19980727 A 5320 3750257503 SPLICE DOUG DC8 DC871F 302199D WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, FS 1040 TO 1060 STRINGER 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 1998081400084 19980814 00084 WP 1998 8 14 UPS98827318 1 19980731 A 5320 37502571N SPLICE DOUG DC8 DC871F 302199D WP BS 1040-1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, LONG 31R SPLICE FITTING CRACKED FS 1040 TO 1060. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998081400085 19980814 00085 WP 1998 8 14 ABXA9800684 1 19980731 A 5320 5912285513 RETAINER DOUG DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING AIRCRAFT C-CHECK, A CRACK WAS FOUND ON THE LOWER AFT CORNER OF THE WINDOW RETAINER LOCATED AT STATION 656R. CRAC K MEASURES APPROXIMATELY .5. REPAIRED IAW ABX REA NR D 953-24234. 2 L 7 2 4F A6WE 1998081400086 19980814 00086 WP 1998 8 14 ABXA9800685 1 19980728 A 2742 2706386505 JACKSCREW DOUG DOUG DC8 DC861 3021952 WP HORIZ STAB WORN A ABXA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 23 851AX 45940 DURING TEST FLIGHT FOR FLIGHT CONTROL PROBLEMS, AT SPEEDS ABOVE 280 KTS, BRIEF SHARP ELEVATOR INPUT INDUCED ELEVATOR OSC ILLATIONS. SELF INDUCED OSCILLATION OCCURRED ON SEVERAL OCCASIONS. SMALL CONTROL INPUT CAUSED OSCILLATION TO CEASE IMM EDIATELY. FOUND BOTH JACKSCREWS AND GIMBLES WORN DUE TO CORROSION. REPLACED LEFT AND RIGHT HORIZONTAL STABILIZER JACK SCREW ASSEMBLIES IAW DC8 MM 27-41-1. LEFT JACKSCREW (P/N 2706383503). 2 L 7 4 4F 4A25 1998081400087 19980814 00087 WP 1998 8 14 ABXA9800686 1 19980803 A 5320 991015585 PRESSURE WEB DOUG DOUG DC9 DC933F 302207A WP RT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE CEILING PRESSURE PANEL STATION 737 EXFOLIATED ABOVE LONGERON 20. REPAIRED PRESSURE PANEL IAW ABX REA NR D 953-24434-MR. 2 L 7 2 4F A6WE 1998081400088 19980814 00088 WP 1998 8 14 ABXA9800687 1 19980803 A 5210 591008123 DOUBLER DOUG DOUG DC9 DC933F 302207A WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE LEFT ENTRY DOOR EXTERNAL DOUBLER CRACKED AROUND THE HANDLE. REPLACED DOUBLER IAW DC9 SRM 51-3 0-2 AND DACO DWG 5910081. 2 L 7 2 4F A6WE 1998081400089 19980814 00089 WP 1998 8 14 ABXA9800688 1 19980803 A 5320 9922042505 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE FRAME FITTING AT STATION 945 AND LONGERON 24L CRACKED ON INBOARD END OF LOWER FLANGE. REPLACE D FRAME FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998081400090 19980814 00090 WP 1998 8 14 ABXA9800689 1 19980803 A 5311 99220421 FRAME DOUG DOUG DC9 DC933F 302207A WP BS 794 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE FRAME AT STATION 794 CRACKED AT LONGERON 24L ON UPPER FLANGE. REPLACED FRAME FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998081400091 19980814 00091 WP 1998 8 14 ABXA9800690 1 19980803 A 5313 592Y878501N LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 756-840 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND LONGERON 30 CORRODED BETWEEN FRAMES AT STATIONS 775 AND 794 AND AT STATION 756. REPLACED LONGERON BETWEEN STATIONS 756 AND 840 IAW DC9 SRM 51-30-5 AND 51-30-1. 2 L 7 2 4F A6WE 1998081400092 19980814 00092 WP 1998 8 14 ABXA9800691 1 19980803 A 5320 99100733 PRESSURE WEB DOUG DOUG DC9 DC933F 302207A WP NLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND NOSE LANDING GEAR WHEEL WELL PRESSURE PANEL CRACKED AT STATION 83, RIGHT SIDE. REPAIRED PANEL IAW DC9 S/B 58-187. 2 L 7 2 4F A6WE 1998081400093 19980814 00093 WP 1998 8 14 ABXA9800692 1 19980803 A 5320 39573171AX FITTING DOUG DOUG DC9 DC933F 302207A WP BS 362-370 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE FITTING BETWEEN STATIONS 370 AND 362 AT LONGERON 30 CRACKED. REPLACED FITTING IAW DC9 SRM 51- 30-5. 2 L 7 2 4F A6WE 1998081400094 19980814 00094 WP 1998 8 14 ABXA9800693 1 19980803 A 5320 991075521 WEB DOUG DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND CUSP WEB CRACKED JUST FORWARD OF STATION 965, OUTBOARD OF RBL 54. REPAIRED CUSP WEB IAW DC9 SRM 5 3-01. 2 L 7 2 4F A6WE 1998081400095 19980814 00095 WP 1998 8 14 ABXA980694 1 19980803 A 5320 99107555 WEB DOUG DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND CUSP WEB CRACKED OUTBOARD OF LBL 54 JUST FORWARD OF STATION 965. REPAIRED CUSP WEB IAW DC9 SRM 53 -01. 2 L 7 2 4F A6WE 1998081400097 19980814 00097 WP 1998 8 14 ABXA9800696 1 19980803 A 5320 991075516 WEB DOUG DOUG DC9 DC933F 302207A WP BS 755 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND CUSP WEB CORRODED BETWEEN RBL 44 AND 55 AT STATION 755. REPLACED CUSP WEB IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998081400098 19980814 00098 WP 1998 8 14 ABXA9800707 1 19980801 A 3350 60030431 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 941AX 731 47419 EMERGENCY LIGHTS WERE EXTREMELY DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1998081400099 19980814 00099 WP 1998 8 14 ABXA9800708 1 19980805 A 3350 1032200 SWITCH DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 EMERGENCY LIGHT POWER SWITCH OPERATION WAS INTERMITTENT. REPLACED EMERGENCY LIGHT POWER SWITCH. 2 L 7 2 4F A6WE 1998081400100 19980814 00100 WP 1998 8 14 MWEA98831 1 19980805 A 5320 991960325 SPLICE DOUG DC9 DC932 3022066 WP BS 889 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION BEYOND LIMITS ON SPLICE CAP AT FS 889 LONGERON 26L TO 29L. MTC FABRICATED AND INSTALLED NEW SPLICE CAP. 2 L 7 2 4F A6WE 1998081400101 19980814 00101 WP 1998 8 14 MWEA98832 1 19980805 A 5312 5910130119 BULKHEAD WEB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD DEFORMED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND LOWER AFT PRESSURE BULKHEAD DEFORMED AND WITH TOOLING MARKS FROM LONGERON 27L TO 27R. MTC FABRICATED AND INSTALLE D REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998081400102 19980814 00102 WP 1998 8 14 MWEA98833 1 19980805 A 5330 5911424505 SKIN DOUG DC9 DC932 3022066 WP BS 958 & 964 SCRATCHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND SCRATCHES ON FUSELAGE SKIN BETWEEN LONGERON 21 AND 22 RIGHT AT STATION 958 AND 964. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1998081400103 19980814 00103 WP 1998 8 14 MWEA98834 1 19980805 A 5313 5920302507 LONGERON DOUG DC9 DC932 3022066 WP BS 880-895 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON AFT CARGO COMPARTMENT LONGERON 29R FROM FS 880 TO 895. MTC FABRICATED AND INSTALLED SPLICED PIECE OF LONGERON. 2 L 7 2 4F A6WE 1998081400104 19980814 00104 WP 1998 8 14 MWEA98835 1 19980805 A 5320 39145901 FITTING DOUG DC9 DC932 3022066 WP BS 990 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON END FITTING AT LONGERON 24L STATION 990. MTC FABRICATED AND INSTALLED NEW END FITTING. 2 L 7 2 4F A6WE 1998081400105 19980814 00105 WP 1998 8 14 MWEA98836 1 19980805 A 5320 49144541 CLIP DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON END CLIP AT LEFT SIDE FUSELAGE AT STATION 996 BETWEEN LONGERON 18L AND 20L. MTC FABRICATED AND INST ALLED END CLIP. 2 L 7 2 4F A6WE 1998081400106 19980814 00106 WP 1998 8 14 MWEA98837 1 19980805 A 5220 DO602775 LOCKPIN SOCKET DOUG DC9 DC932 3022066 WP EMERGENCY EXIT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND BOTH LEFT AFT EMERGENCY EXIT LOCKPIN SOCKETS CRACKED. MTC REMOVED AND REPLACED LOCKPIN SOCKETS. 2 L 7 2 4F A6WE 1998081400107 19980814 00107 WP 1998 8 14 MWEA98838 1 19980805 A 5311 3912237513 FRAME DOUG DC9 DC932 3022066 WP BS 870 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON AFT CARGO COMPARTMENT FUSELAGE FRAME FS 870 AT LONGERON 29L TO 29R. MTC FABRICATED AND INSTALLED REP AIR SPLICES. 2 L 7 2 4F A6WE 1998081400108 19980814 00108 WP 1998 8 14 MWEA98839 1 19980805 A 2510 9957871 SEAT RAIL DOUG DC9 DC932 3022066 WP COCKPIT WORN A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND THE CAPTAINS SEAT RAIL HOLES ARE WORN. MTC FOUND RAIL WEAR WITHIN LIMITS AND FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998081400109 19980814 00109 WP 1998 8 14 MWEA98840 1 19980805 A 5320 995791745 FORMER DOUG DC9 DC932 3022066 WP BS 937 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND FORMER BENT AT STATION 937 IN BETWEEN L30 TO L29R TO L28R. MTC STRAIGHTENED OUT FORMER AND INSTALLED FASTENERS. 2 L 7 2 4F A6WE 1998081400110 19980814 00110 WP 1998 8 14 MWEA98841 1 19980805 A 5330 5919707501 SKIN DOUG DC9 DC932 3022066 WP BS 870 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 209ME 47730 FOUND DOUBLE DRILLED HOLE AT FS 870 BETWEEN LONGERON 30 AND 29L ON SKIN. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998081400111 19980814 00111 WP 1998 8 14 MWEA98842 1 19980801 A 5312 591016343 BLKHD STIFFENER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND CRACKED STIFFENER AT INBOARD EDGE ON AFT PRESSURE BULKHEAD AFT SIDE. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998081400112 19980814 00112 NM 1998 8 14 DL72S981604 1 19980729 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 990-1010 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 493DA 21062 FOUND DURING MV1 CORROSION VISIT NRC 121, CORROSION ON STR 29 LT OUTBOARD LEG AFT OF STA 990 TO STA 1010. REPAIRED PER SRM 53-10-11 FIG 3. 2 L 7 3 4F A3WE 1998081400113 19980814 00113 NM 1998 8 14 DL72S981606 1 19980805 A 3510 OXYGEN BOTTLE 80130700 BOEING 727 727232 1384082 NM E/E COMPT EMPTY A DALA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 27 497DA 072373 21077 CREW OXYGEN READS ZERO, SUSPECT REGULATOR AT JUMPSEAT STUCK IN EMERGENCY POSITION. FREED JUMPSEAT 02 SWITCH, REPLACED C REW O2 BOTTLE LEAK AND OPS CKS OK. 2 L 7 3 4F A3WE 1998081400114 19980814 00114 NM 1998 8 14 DL72S981607 1 19980722 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 STA 1303 INSIDE OF VERT RT SIDE CTR OF BULKHEAD WEB CRACKED AT CUTOUT FOR STR. REMOVED SECTION OF ANTI-ICE DUCT FOR ACC ESS, REMOVED HORT SUPPORT BRACE FOR ACCESS, REMOVED EXISTING FASTENER AND DOUBLER. STOP DRILLED CRACK, FAB AND DRILLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17. REPAIRED PER SRM 53-10-4 FIG 17. REINSTALLED ANTI-ICE DUCT AND HORT SUPPORT BRA CE. 2 L 7 3 4F A3WE 1998081400115 19980814 00115 NM 1998 8 14 DL72S981608 1 19980722 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 STA 1303 INSIDE OF VERT LOWER LT CORNER OF BULKHEAD WEB CRACKED. REMOVED EXISTING FASTENERS, STOP DRILLED CRACK, FAB AN D DRILLED REPAIR DOUBLER PER SRM 53-10-4 FIG 17. REPAIRED PER SRM 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1998081400116 19980814 00116 NM 1998 8 14 SCNA98087 1 19980731 A 3350 900835A BATTERY PACK BOEING 727 727282 138408T NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS OVER BOTH RIGHT OVERWING EXITS WERE FOUND TO FLASH ON AND OFF. RE MOVED AND REPLACED THE BATTERY PACK AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998081400117 19980814 00117 NM 1998 8 14 DHL98705001 1 19980804 A 2720 65178231 MODULE 10617441 BOEING 727 72722C 138400F NM RUDDER LEAKING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 705DH MX457988 19191 HYDRAULIC SYSTEM-A FAILURE. ZERO PRESSURE AND QUANTITY. REPLACED A-SYSTEM RUDDER MODULE AND BOTH ENG DRIVEN PUMPS. 2 L 7 3 4F A3WE 1998081400118 19980814 00118 NM 1998 8 14 DHL98708002 1 19980805 A 5754 CASTING BOEING 727 72725 1384006 NM NR 2 LE FLAP BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 NR 2 LEADING EDGE FLAP HAS BROKEN CASTING AT ACTUATOR MOUNT ON FLAP. REPLACED FLAP PER MM 27-81-1. 2 L 7 3 4F A3WE 1998081400119 19980814 00119 NM 1998 8 14 VNAA9808003 1 19980801 A 3240 BRAKES DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG REQD SERVICE A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 423JS 3032 THE LEFT HAND BRAKES WERE REPORTED FROM THE CREW AS SPONGEY WHEN SELECTED, DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RE TURNED TO THE GATE. MAINTENANCE INSPECTED AND BLED THE BRAKE SYSTEM, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-4 2-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998081400120 19980814 00120 NM 1998 8 14 VNAA9808005 1 19980804 A 3241 AE20768 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ANTI-SKID SYST FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 436JS 77953 3052 AN ANTI-SKID FAIL WARNING MESSAGE OCCURRED, DURING TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANC E INSPECTED AND REPLACED THE ANTI-SKID CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-11. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998081400128 19980814 00128 SO 1998 8 14 98ZZZX2660 1 19980709 A 5610 562023 WINDOW PIPER PA42 PA42 7104202 SO COPILOT CRACKED A S TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 175AA 2178 93308H7283 428001017 COPILOT WINDOW HAS CRACKED. 1 L 7 2 4T A23SO 1998081400149 19980814 00149 CE 1998 8 14 98ZZZX2681 1 19980711 A 8011 539800 CLUTCH SPRING 643259A CESSNA 207 207 2073602 CE STARTER ADAPTER BROKE A KCQA K NONE O OTHER IN INSP/MAINT 1 GL 13 1518U 1294 4965 20700118 STARTER ADAPTER SPRING BROKE. 1 H 7 1 3O A16CE 1998081400153 19980814 00153 1998 8 14 98ZZZX2685 4 19980618 A 3421 G550A GYRO ARC CESSNA 414 414A 2075907 CE INSTRUMENT PANEL FAILED A GJAA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 NM 01 6562C 12 446700008 414A0015 GYRO HORIZON/FLIGHT DIRECTOR FAILED IN-FLIGHT. THE GYRO GASKET BETWEEN THE FRONT FACE AND INSTRUMENT STARTED LEAKING AN D PREVENTED OPERATION OF GYRO. UNABLE TO RESTORE OPERATION. FLIGHT FOR 135 OPERATIONS WAS DISCONTINUED. 1 L 7 2 3O A7CE 1998081400175 19980814 00175 NM 1998 8 14 98ZZZX2710 1 19980702 A 2910 B NUT BOEING 727 7272J0 138407E NM A HYD SYSTEM LOOSE A S84A A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 21 284KH 21108 AIRCRAFT DIVERTED INTO KFLL DUE LOSS OF A-SYSTEM HYDRAULIC FLUID: FOUND B-NUT NR 1 ENGINE MAIN HYD LINE LOOSE. TIGHTEN ED B-NUT. CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASED AIRCRAFT. 2 L 7 3 4F RT A3WE 1998081400177 19980814 00177 EA 1998 8 14 98ZZZX2711 2 19980113 A 7320 3008787 ROD END BEECH 99 99A 1154003 CE PWA PT6 PT6A27 52043 EA FCU BINDING A KCQA K NONE O OTHER IN INSP/MAINT 1 GL 13 499CZ U81 PCE40501 ENGIEN POWER WOULD NOT DECREASE DUE TO BINDING ROD END CONNECTOR CAM BOX TO FCU. TAT: 30,824 HOURS. ENG TSN: 4,295 H OURS. ENG TSO: 1,129 HOURS. 1 L 7 2 3T 4 T A14CE E4EA 1998081400178 19980814 00178 CE 1998 8 14 98ZZZX2712 1 19980709 A 2930 LINE LEAR 25 25D 5170514 CE WHEEL WELL FAILED A KKFA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 GL 23 95CK 11613 248 WHILE EN ROUTE, HYDRAULIC PRESSURE INDICATION WENT TO ZERO. AIRCRAFT DIVERTED TO TYS FOR LONGER RUNWAYS, A NORMAL LANDI NG WAS MADE. INSPECTION REVEALED A BROKEN INDICATOR CAPILLARY LINE. LINE WAS REPLACED. HYDRAULIC SYSTEM WAS SERVICED AND INSPECTED. 2 L 7 2 4J A10CE 1998081400179 19980814 00179 CE 1998 8 14 98ZZZX2713 1 19980708 A 2133 24800045 OUTFLOW VALVE LEAR 25 25 5170506 CE CABIN PRESSURE FAILED A VLLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 05 294NW 8446 011 031 ON CLIMB-OUT OF MWO, PILOTS REPORTED THAT CABLE PRESSURIZATION COULD NOT BE CONTROLLED BY CABIN RATE CONTROL. RETURNED TO MWO. REMOVED CABIN OUTFLOW AND RATE CONTROL. SENT TO LEAR JET FOR TEST/REPAIR. 2 L 7 2 4J A10CE 1998081400183 19980814 00183 CE 1998 8 14 98ZZZX2717 1 19980713 A 8010 1009800231 BRACKET BEECH 100 B100 1152919 CE LT STARTER FAILED A A EGQA K NONE O OTHER IN INSP/MAINT 1 EA 17 400AC 9896 BE12 PILOT REPORTED LT ENG STARTER WOULD NOT CRANK ENG. STARTER REPLACED. NEW STARTER TESTED, AND WOULD NOT CRANK ENG. VOL TAGE AT THE STARTER CHECKED AND FND TO BE 48 VOLTS INSTEAD OF THE NORMAL 24 VOLTS. START CONTROL PANEL WAS INSPECTED AN D FND TO HAVE ARCED RELAY CONTACTS. START CONTROL PANEL REPLACED WITH NEW UNIT. VOLTAGE AT STARTER CONFIRMED TO BE 24V , BUT ENG STILL WOULD NOT CRANK. INSP OF GROUND WIRES REVEALED THE BRACKET THAT ATTACHES GROUND WIRES TO FIREWALL HAD B ROKEN OFF FIREWALL. BRACKET REMAINED IN CONTACT WITH FIREWALL TO ALLOW VOLTAGE CHECK TO SHOW 24V, BUT WITHOUT A SOLID C ONNECTION, THE CURRENT REQUIRED BY THE STARTER COULD NOT FLOW THROUGH THE FAILED GROUNDING POINT. 1 L 7 2 4T A14CE 1998081400189 19980814 00189 CE 1998 8 14 98ZZZX2723 1 19980706 A 2730 1156100100325 TORQUE TUBE BEECH 99 99 1154002 CE ELEVATOR CONTROL CRACKED A KCQA K NONE O OTHER IN INSP/MAINT 1 GL 13 199CZ U30 ELEVATOR CONTROL SYSTEM TORQUE TUBE ASSEMBLY FOUND CRACKED AT TAPER PIN HOLE. 1 L 7 2 3T A14CE 1998081400190 19980814 00190 CE 1998 8 14 98ZZZX2724 1 19980701 A 2730 115610010325 TORQUE TUBE BEECH 99 99 1154002 CE ELEVATOR CONTROL CRACKED A KCQA K NONE O OTHER IN INSP/MAINT 1 GL 13 299CZ U74 ELEVATOR CONTROL SYSTEM TORQUE TUBE ASSY FOUND CRACKED AT TAPER PIN HOLE. 1 L 7 2 3T A14CE 1998081400192 19980814 00192 WP 1998 8 14 TWAA9812701 1 19980805 A 3350 58531 LIGHT DOUG DC9 DC915 3022036 WP CABIN LOOSE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 491SA 45799 THE FIRST CLASS AND FWD SECTION OF COACH HAD EGRESS LIGHTING INOPERATIVE. FOUND POWER FEEDER LEAD LOOSE. RESECURED CON NECTOR. CHECK-C 3-12-98 STL. 2 L 7 2 4F A6WE 1998081400193 19980814 00193 NM 1998 8 14 TWAA9812703 1 19980804 A 3350 20131A BATTERY PACK BOEING 767 767205 1385121 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 650TW 23057 MAINT FOUND EMERGENCY LIGHT EQUIPMENT NRS L308, L311, L333 WERE INOPERATIVE ON TEST. REPLACED BATTERY PACK. CHECK-C 7-2 1-98 LAX. 2 L 7 2 4F RT A1NM 1998081400194 19980814 00194 NM 1998 8 14 TWAA9812705 1 19980805 A 7120 BRACKET BOEING 757 757231 1384950 NM NR 1 ENGINE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 705TW 28479 DURING CHECK-C, THE NR 1 ENG STRUCTURE MOUNT BRACKET WAS CRACKED AT FWD LOWER CORNER INSIDE PANEL 435AR. FABRICATED AND INSTALLED NEW PART FROM 310 1/2 HARD .020 THICK PER SRM 51-10-00. 2 L 7 2 4F RT A2NM 1998081400195 19980814 00195 NM 1998 8 14 TWAA9812706 1 19980805 A 7120 BRACKET BOEING 757 757231 1384950 NM NR 1 ENGINE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 705TW 28479 DURING CHECK-C, FOUND NR 1 ENG STRUCTURE MOUNT BRACKET CRACKED AT LOWER AFT CORNER INSIDE PANEL 435AR. FABRICATED AND I NSTALLED NEW PART PER SRM 51-10-00, FROM 2024 T3 .071 THICK. 2 L 7 2 4F RT A2NM 1998081400196 19980814 00196 WP 1998 8 14 TWAA9812707 1 19980803 A 5320 FRAME DOUG DC9 DC931 3022065 WP AIRSTAIR DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 DURING OP 15 MAINT CHECK AT FWD AIRSTAIR, FOUND CORROSION ON DOOR CUTOUT INSIDE SURFACE AT CENTER AND AFT CORNER OF DOOR . REPLACED FRAME AND WEB WITH NEW PARTS, INSTALLED FASTENERS PER SRM 51-60-0, 51-30-02, AND SSRM 51-40-501. 2 L 7 2 4F A6WE 1998081400197 19980814 00197 NM 1998 8 14 TWAA9812708 1 19980805 A 5730 SKIN BOEING 757 757231 1384950 NM LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 705TW 28479 DURING CHECK-C, FOUND LT WING LE TOP, AFT OF NR 4 OTBD SLAT, HONEY COMB PANEL CRACKED 8 IN LONG. INSTALLED FIBERGLAS RE PAIR 7 IN BY 11 IN WITH HOT BOND PER SRM 51-70-07, REPLACED REMOVED FASTENERS AND SMOOTHED AREA. 2 L 7 2 4F RT A2NM 1998081400198 19980814 00198 NM 1998 8 14 AWXA9800172 1 19980718 A 5320 SUPPORT BOEING 757 7572S7 1384962 NM BS 330 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN FLOOR SUPPORT AT STA 330, RBL 5 CORRODED. REMOVED AND REPLACED FLOOR S UPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 1998081400199 19980814 00199 NM 1998 8 14 AWXA9800173 1 19980718 A 5315 FLOORBEAM BOEING 757 7572S7 1384962 NM BS 365.35 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 DURING SCHEDULED C-6 INSPECTION, FOUND CABIN FLOORBEAM AT BS 365.35 CORRODED AT RBL 38, 45, 53 AND 59. REMOVED AND REPL ACED FLOORBEAM PER SRM 53-00-51. 2 L 7 2 4F RT A2NM 1998081400200 19980814 00200 NM 1998 8 14 AWXA9800174 1 19980718 A 5315 FLOORBEAM BOEING 757 7572S7 1384962 NM BS 365.25 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 901AW 23321 DURING SCHEDULED C-6 INSPECTION, FOUND CABIN FLOORBEAM AT BS 365.25 CORRODED AT RBL 5, 12, 16, 20 AND 29. REMOVED AND R EPLACED FLOORBEAM PER SRM 53-00-51. 2 L 7 2 4F RT A2NM 1998081400201 19980814 00201 NM 1998 8 14 AWXA9800175 1 19980718 A 5320 SUPPORT BOEING 757 7572S7 1384962 NM BS 345-365 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN STATION 345 - 365 RBL - 0 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. 2 L 7 2 4F RT A2NM 1998081400202 19980814 00202 NM 1998 8 14 AWXA9800176 1 19980718 A 5320 SUPPORT BOEING 757 7572S7 1384962 NM BS 367-375 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN STATION 367 - 375 LBL 60 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-10-00. 2 L 7 2 4F RT A2NM 1998081400203 19980814 00203 NM 1998 8 14 AWXA9800177 1 19980718 A 5320 CHANNEL BOEING 757 7572S7 1384962 NM BS 335-345 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING SCHEDULED C-6 INSPECTION, FOUND FWD CABIN STATION 335 - 345 LBL 60 FLOOR CHANNEL CORRODED. REMOVED AND REPLACED FLOOR CHANNEL PER 51-10-00. 2 L 7 2 4F RT A2NM 1998081400204 19980814 00204 NM 1998 8 14 AWXA9800178 1 19980718 A 5320 SUPPORT BOEING 757 7572S7 1384962 NM BS 324-365.25 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 902AW 23322 DURING SCHEDULED C-6 INSPECTION, FOUND FLOOR SUPPORT CHANNEL AT NR 1 R CABIN SERVICE DOOR, BETWEEN BS 324 TO 365.25 RBL 62L, CORRODED WITH HOLES AND CORROSION ON TOP SURFACE (CHANNEL IS TWO PIECES). REMOVED AND REPLACED FLOOR SUPPORT CHANN ELS PER SRM 51-10-00. 2 L 7 2 4F RT A2NM 1998081400205 19980814 00205 NM 1998 8 14 AWXA9800179 1 19980716 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 967 CORRODED A AWXA O OTHER O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 FOUND DURING SCHEDULED INSPECTION, FLOORBEAM 967 LBL 44 CORROSION AT NUT PLATE HOLES. REPAIRED PER SRM 53-00-51 FIG 202 . 2 L 7 2 4F RT A16WE 1998081400206 19980814 00206 NM 1998 8 14 AWXA9800180 1 19980716 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 918 MISREPAIRED A AWXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 28 311AW 24712 FOUND DURING SCHEDULE INSPECTION, FLOORBEAM REPAIR STATION 981 BL O NOT TYPICAL REPAIR. REPAIRED PER SRM 53-00-51. 2 L 7 2 4F RT A16WE 1998081400207 19980814 00207 NM 1998 8 14 AWXA9800181 1 19980716 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 FOUND DURING SCHEDULED INSPECTION, CORROSION AT NUTPLATE HOLE FLOORBEAM STA 947 RBL 17. REPAIRED PER SRM 53-00-51 FIG 2 02. 2 L 7 2 4F RT A16WE 1998081400208 19980814 00208 NM 1998 8 14 AWXA9800182 1 19980716 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 918 DAMAGED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 FOUND DURING SCHEDULED INSPECTION, UPPER CHORD OF FLOORBEAM AT STATION 981 RBL 24 HAD ELONGATED FASTENER HOLE. PREVIOUS REPAIR REPAIRED TEE CAP PER SRM 53-00-51 FIG 202. 2 L 7 2 4F RT A16WE 1998081400209 19980814 00209 NM 1998 8 14 AWXA9800183 1 19980716 A 5320 6545855101 THRESHOLD BOEING 737 7373G7 1384595 NM BS 947-987 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 311AW 24712 FOUND DURING SCHEDULED INSPECTION, R-2 DOOR THRESHOLD CHORD CORRODED BEYOND LIMITS. REPLACED WITH FABRICATED CHORD PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1998081400210 19980814 00210 NM 1998 8 14 CALA9801400 1 19980806 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 970-990 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL WEB TOP ANGLE AT FORWARD SCREW HOLE BETWEEN FLOORBEAMS AT BS 970-990, BL 0. THE TOP ANGLE WAS REMOVED. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-40-3. 2 L 7 3 4F A3WE 1998081400211 19980814 00211 NM 1998 8 14 CALA9801401 1 19980806 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1030-1120 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND CORROSION AT INBOARD AND OUTBOARD LEGS OF SEAT TRACK AT BS 1030-1120, LBL 45. THE SEAT TRACK WAS REMOV ED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998081400212 19980814 00212 NM 1998 8 14 CALA9801402 1 19980806 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 1130-1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND FLOOR PANEL SUPPORT ANGLE CORRODED AT BS 1130-1148, RBL 12. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-4, 51-10-2, AND 51-40-5. 2 L 7 3 4F A3WE 1998081400213 19980814 00213 NM 1998 8 14 CALA9801403 1 19980806 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND CORROSION ON TOP OF FLOORBEAM AT BS 344, LBL 41-53. THE CORRODED AREA WAS CUT OUT. NEW PARTS WERE FAB RICATED AND INSTALLED IAW SRM 53-10-8 AND 51-10-2. 2 L 7 3 4F A3WE 1998081400214 19980814 00214 NM 1998 8 14 CALA9801404 1 19980806 A 5320 WEB BOEING 727 727224 1384076 NM BS 1175 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND FLOOR WEB CORRODED AT BS 1175, RBL 65, OUTBOARD OF RT AFT LAV DUMP CHUTE FLANGE. THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-30-2. 2 L 7 3 4F A3WE 1998081400215 19980814 00215 NM 1998 8 14 CALA9801405 1 19980807 A 5321 FLOOR BOEING 727 727224 1384076 NM BS 1129-1176 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND RT AFT LAV FIXED FLOOR CORRODED INCLUDING AROUND DUMP CHUTE AT BS 1129-1176, RBL 25-63. THE CORROSION WAS REMOVED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-40-5, AND 51-10-6. 2 L 7 3 4F A3WE 1998081400216 19980814 00216 NM 1998 8 14 CALA9801406 1 19980807 A 5320 ANGLE BOEING 727 727224 1384076 NM RT LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND RT AFT LAV FLOOR ANGLE CORRODED OUTBOARD OF DUMP CHUTE AREA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-10-1, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1998081400217 19980814 00217 NM 1998 8 14 CALA9801407 1 19980806 A 5321 FLOOR BOEING 727 727232 1384082 NM BS 950 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A PUNCTURE IN AFT CARGO FLOOR PANEL AT STA 950E. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 , 53-10-7, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998081400218 19980814 00218 NM 1998 8 14 CALA9801408 1 19980806 A 5321 FLOOR BOEING 727 727232 1384082 NM BS 640-720 PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A HOLE IN FORWARD PIT FLOOR PANEL AT STA 640-720. THE DAMAGED AREA WAS CUT OUT. TWO DOUBLERS AND REPA IR FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-7, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998081400219 19980814 00219 NM 1998 8 14 CALA9801409 1 19980806 A 5720 TIP BOEING 727 727232 1384082 NM LT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT WING TIP INBOARD ACCESS PANEL 8112 DEFORMED AND CRACKED. A NEW PANEL WAS FABRICATED AND INSTALLED I AW SRM 51-20-01. 2 L 7 3 4F A3WE 1998081400220 19980814 00220 NM 1998 8 14 CALA9801410 1 19980806 A 5320 STRAP BOEING 727 727232 1384082 NM BS 540 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FORWARD CARGO PIT FLOOR SUPPORT STRAP CORRODED WITH ELONGATED HOLES AT STA 540. A SUPPORT STRAP WAS FA BRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2. 2 L 7 3 4F A3WE 1998081400221 19980814 00221 NM 1998 8 14 CALA9801411 1 19980806 A 5744 BRACKET BOEING 727 727224 1384076 NM NR 5 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A 1 CRACK IN RT NR 5 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET AT UPPER OUTBOARD LEADING EDGE. THE MOUN T BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998081400222 19980814 00222 NM 1998 8 14 CALA9801412 1 19980807 A 5744 BRACKET BOEING 727 727224 1384076 NM NR 2 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A .75 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 2 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED IAW SRM 51-30-2. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998081400223 19980814 00223 NM 1998 8 14 CALA9801413 1 19980807 A 5744 BRACKET BOEING 727 727224 1384076 NM NR 1 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A .5 INCH CRACK IN INBOARD BRACKET WHERE LT WING NR 1 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET W AS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998081400224 19980814 00224 NM 1998 8 14 CALA9801414 1 19980807 A 5754 SKIN BOEING 727 727224 1384076 NM NR 4 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A .15625 AND .09375 CRACK IN LT WING NR 4 SLAT LOWER TRAILING EDGE SKIN AT RADIUS OUTBOARD OF INBOARD T RACK, 36.5 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-50-3 , 51-10-2, AND 51-40-5. 2 L 7 3 4F A3WE 1998081400225 19980814 00225 WP 1998 8 14 CALA9801415 1 19980807 A 5350 CABLES DOUG DC9 DC932 3022066 WP TAILCONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 THE FORCE REQUIRED TO DROP TAILCONE USING INTERIOR HANDLE WAS EXCESSIVE AT 45 POUNDS. THE FORCE REQUIRED USING EXTERIOR HANDLE WAS LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-3. 2 L 7 2 4F A6WE 1998081400226 19980814 00226 NM 1998 8 14 QXEA9801056 1 19980804 A 2611 473054 SMOKE DETECTOR DHAV 82522710001 DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTION A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 357PH 709 504 SEA - INTERMITTENT SMOKE WARNING LIGHT IN FLIGHT. CHECKED BAGGAGE COMPARTMENT NO EVIDENCE OF FIRE OR SMOKE NOTED. ALL OTHER INDICATIONS NORMAL. REPLACED NR 1 SMOKE DETECTOR IN THE BAGGAGE COMPARTMENT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998081400227 19980814 00227 NM 1998 8 14 QXEA9801057 1 19980803 A 3231 69210 VALVE DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR MALFUNCTION A QXEA K NONE O OTHER CL CLIMB 1 NM 09 814PH 14963 4963 43 SEA - LEFT GEAR DOOR LIGHT REMAINED ON WHEN THE LANDING GEAR WAS RETRACTED. DOOR VISUALLY INSPECTED AND VERFIED TO BE O PEN. WHEN GEAR CYCLED THE LIGHT WENT OUT. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN PDX, RIGGED THE ALTERNATE EXTENSION SYSTEM AND REPLACED THE HYDRAULIC MANIFOLD (S/N: 0040, TSN/CSN 28478/38930, TSR/CSR 12555/17633), AND THE MECH ANICAL SEQUENCE VALVE. PERFORMED GEAR SWINGS AND TEST FLIGHT, BOTH SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998081400228 19980814 00228 WP 1998 8 14 ABXA9800697 1 19980806 A 2760 3954558501 LINK DOUG DOUG DC9 DC933F 302207A WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE LEFT OUTBOARD SPOILER DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 SMM 27-61-1 AND MM 27-6 1-0. 2 L 7 2 4F A6WE 1998081400229 19980814 00229 WP 1998 8 14 ABXA9800698 1 19980806 A 2760 39515571 LINK DOUG DOUG DC9 DC933F 302207A WP LT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE LEFT INBOARD SPOILER DRIVE LINK CRACKED. REPLACED DRIVE LINK IAW DC9 SMM 27-61-1 AND MM 27-61 -0. 2 L 7 2 4F A6WE 1998081400230 19980814 00230 WP 1998 8 14 ABXA9800699 1 19980806 A 5320 99220421 FITTING DOUG DOUG DC9 DC933F 302207A WP BS 775 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND THE FRAME FITTING AT STATION 775 AT LONGERON 24L CRACKED ON UPPER FLANGE. REPLACED FITTING IAW DC 9 SRM 53-30-5, 51-30-2, 51-30-8 AND 51-30-1. 2 L 7 2 4F A6WE 1998081400231 19980814 00231 WP 1998 8 14 ABXA9800700 1 19980806 A 5313 59114279 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND LONGERON 17L CRACKED AT STATION 980. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998081400232 19980814 00232 WP 1998 8 14 ABXA9800701 1 19980806 A 5313 59114279 LONGERON DOUG DOUG DC9 DC933F 302207A WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT AFT SIDE OF PYLON BULKHEAD STATION 965. REPAIRED LONGERON IAW DC9 SRM 53- 02. 2 L 7 2 4F A6WE 1998081400233 19980814 00233 WP 1998 8 14 ABXA9800702 1 19980623 A 5320 5755600 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 1140 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 FLOORBOARD ATTACH ANGLE CRACKED AT STATION 1140, RBL 55. REPAIRED IAW ABX REA NR D853-22888 AND DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1998081400234 19980814 00234 WP 1998 8 14 ABXA9800703 1 19980623 A 5712 57695892 RIB DOUG DOUG DC8 DC861F 3021953 WP WS 6.225 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 RIGHT WING LEADING EDGE AT STATION XOLDI 6.225, UPPER LEADING EDGE RIB HAS A 4 CRACK. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F 4A25 1998081400235 19980814 00235 WP 1998 8 14 ABXA9800704 1 19980621 A 5320 9755584507 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 1070 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT LOWER FRAME TO CUSP FITTING CRACKED AT STATION 1070. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 9755584. 2 L 7 4 4F 4A25 1998081400236 19980814 00236 WP 1998 8 14 ABXA9800705 1 19980621 A 5320 5646444 WEB DOUG DOUG DC8 DC861F 3021953 WP LT MLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT WHEEL WELL AFT TORQUE BOX WEB CRACKED. REPAIRED IAW DC8 SRM 53-2-0, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 1998081400237 19980814 00237 WP 1998 8 14 ABXA9800706 1 19980621 A 5320 3754473501N FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 1300-1320 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 SPLICE FITTING CRACKED AT STATION 1300 - 1320 STRINGER 31L. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998081400238 19980814 00238 WP 1998 8 14 ABXA9800709 1 19980619 A 5320 3754220503 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 180-200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 31L SPLICE FITTING IS CRACKED AT STATION 180 - 200. REPLACED SPLICE FITTING IAW DC8 SRM 51-11-20D. 2 L 7 4 4F 4A25 1998081400239 19980814 00239 WP 1998 8 14 ABXA9800710 1 19980617 A 5320 46455172 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 680 BULKHEAD SEAT TRACK ATTACH FITTING CRACKED AT BL-0. REPLACED FITTING IAW DWG 4645517 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998081400240 19980814 00240 WP 1998 8 14 ABX9800711 1 19980619 A 5313 575499227 LONGERON DOUG DOUG DC8 DC861F 3021953 WP BS 640-680 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LONGERON 31R AT STATION 640-680 HAS CORROSION. REPAIRED IAW ABX REA D853-22883MR. 2 L 7 4 4F 4A25 1998081400241 19980814 00241 WP 1998 8 14 ABXA9800712 1 19980626 A 5320 4645517502 ANGLE DOUG DOUG DC8 DC861F 3021953 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 680 BULKHEAD UPPER ATTACH FITTING TO FLOOR BOARD FRAME CRACKED AT RBL24. REPLACED FLOOR SUPPORT ANGLE IAW DWG 4645517 A ND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998081400242 19980814 00242 WP 1998 8 14 ABXA9800713 1 19980620 A 5320 37505451 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 STATION 1040-1060 LONGERON 35L SPLICE FITTING IS CRACKED. REPLACED SPLICE FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998081400243 19980814 00243 WP 1998 8 14 ABXA9800714 1 19980712 A 5320 37532351 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 980-1000 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 STATION 980-1000 STRINGER 22R END FITTING WAS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-8 AND DWG 37532351. 2 L 7 4 4F 4A25 1998081400244 19980814 00244 WP 1998 8 14 ABXA9800715 1 19980617 A 5320 37533061 FITTING DOUG DOUG DC8 DC861F 3021953 WP BS 980-1000 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 STATION 980-1000 STRINGER 23R END FITTING IS CRACKED. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 3753306. 2 L 7 4 4F 4A25 1998081400245 19980814 00245 WP 1998 8 14 ABXA9800716 1 19980623 A 5720 576947622 ANGLE DOUG DOUG DC8 DC861F 3021953 WP WS 766.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 RIGHT WING LEADING EDGE AT STATION XFS 766.250, THE INTERNAL DOUBLER ANGLE FORWARD OF ACCESS HOLE HAS A 5 CRACK. REPAIR ED IAW DC8 SRM 51-1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998081400246 19980814 00246 WP 1998 8 14 ABXA9800717 1 19980623 A 5712 576954551 RIB DOUG DOUG DC8 DC861F 3021953 WP WS 816.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 849AX 45891 LEFT WING LEADING EDGE LOWER RIB ARM CRACKED BY AFT FASTENER AT STATION XFS 816.250. REPAIRED IAW DC8 SRM 57-2-0 AND 51 -1-21. 2 L 7 4 4F 4A25 1998081400247 19980814 00247 WP 1998 8 14 ABXA9800718 1 19980804 A 3260 7000010101 SWITCH DOUG DC8 DC863 302198A WP LT MLG WORN A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 LEFT MAIN LANDING GEAR UPLATCH FAILED DURING CLIMB. RECYCLED GEAR SEVERAL TIMES, NO CHANGE. AFTER ENCOUNTERING TURBULE NCE, LIGHT WENT OUT AND REMAINED OUT. REPLACED LEFT MAIN LANDING GEAR UPLATCH SWITCH IAW DC8 MM 32-60-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998081400248 19980814 00248 WP 1998 8 14 ARWA980803 1 19980805 A 2910 NUT DOUG DC8 DC862 3021970 WP HYDRAULIC SYSTEM LOOSE A ARWA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 802BN 45909 KELP - FLT 045 - DURING CLIMB-OUT, HYDRAULIC FLUID LOSS, PRESSURE FLUCTUATING, EMERGENCY CHECK LIST COMPLETED, 6 GALLONS REMAINING. RETURNED TO KELP. TIGHTENED LOOSE B-NUT ON RT AILERON ACTUATOR SWIVEL GLAND NUT, LEAK AND OPS CHECK NORMAL IAW 27-10-0. HYDRAULICS SERVICED. (X) 2 L 7 4 4F 4A25 1998081400249 19980814 00249 NM 1998 8 14 VNAA9808006 1 19980805 A 7603 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 433JS 3047 WHEN THE AIRCRAFT TOOK THE ACTIVE RUNWAY, THE CREW ADVANCED THE POWER LEVERS FOR TAKEOFF. THE LEFT POWER LEVER WOULD N OT ADVANCE PAST THE FLIGHT IDLE DETENT. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND LUBED THE LEFT POWER LEVER RELEASE AND LOCK SYSTEM. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVI CE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998081400250 19980814 00250 WP 1998 8 14 TC8A98046 1 19980806 A 2110 CONNECTOR DOUG DC8 DC8F54 3021926 WP NR 1 TURBO COMP DIRTY A TC8A D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 23 802CK 45679 TRIP NR 02268, NR 1 TURBO COMPRESSOR WOULD NOT TEST. CLEANED CANNON PLUG AND RESET, OPS CHECK GOOD IAW M/M 21-10-2. 2 L 7 4 4F 4A25 1998081400251 19980814 00251 1998 8 14 TC8A98047 4 19980806 A 3421 258733511 GYRO VERTICAL DOUG DC8 DC862 3021970 WP E/E COMPT INOPERATIVE A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 181SK 45910 TRIP NR 02270, FO VERTICAL GYRO INOP, ATTITUDE FLAG IN VIEW. REPLACED NR 2 VG, SYSTEM CHECKED SATISFACTORY 34-25-0. 2 L 7 4 4F 4A25 1998081400252 19980814 00252 1998 8 14 TC8A98048 4 19980806 A 3497 WIRE DOUG DC8 DC862 3021970 WP E/E COMPT BROKEN A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 181SK 45910 TRIP NR 02270, INTERMITTENT ATT FLAG DURING TAXI ON F/O SIDE VERTICAL GYRO. REPAIRED BROKEN WIRE, P/N: 2F21DABLY AT INS T RACK 2 AS PER M/M 20-51-0 AND W/D 34-2-2, SYSTEM OPS CHECKED NORMAL ON GROUND IAW M/M 34-25-0. 2 L 7 4 4F 4A25 1998081400253 19980814 00253 EU 1998 8 14 98ZZZX2727 1 19980106 A 2450 TERMINAL BOARD BAG BAE146 BAE146200A 1500266 EU NR 1 PYLON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 1 PYLON TERMINAL BOARD J ON AFT PYLON BULKHEAD CORRODED. CLEANED TERMINAL BOARD ON NR 1 PYLON. 2 H 7 4 4F RT A49EU 1998081400259 19980814 00259 EU 1998 8 14 98ZZZX2733 1 19980102 A 2710 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU LT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 AILERON INTERCONNECT CABLES ARE CORRODED AT LR WING ROOT PULLEYS. REMOVED AND REPLACED BOTH CENTER SECTIONS OF THE AILE RON INTERCONNECT CABLE CIRCUIT AND ADJUSTED IAW MM 27-11-00. W/C 5023 GENERATED FOR FUNCTIONAL CHECK. 2 H 7 4 4F RT A49EU 1998081400260 19980814 00260 EU 1998 8 14 98ZZZX2734 1 19980102 A 5344 FLANGE BAG BAE146 BAE146200A 1500266 EU BS 14-15 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FORWARD VESTIBULE RT SIDE SERVICE DOOR LOWER HINGE PIN DIAPHRAGM IS CRACKED AT UPPER FLANGE BETWEEN FR 14 AND FR 1 5. REPAIRED FLANGE IAW SRM 51-71-11. 2 H 7 4 4F RT A49EU 1998081400261 19980814 00261 EU 1998 8 14 98ZZZX2735 1 19980102 A 7120 MOUNT BAG BAE146 BAE146200A 1500266 EU NR 2 PYLON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 2 PYLON YOKE HAS SLIGHT SURFACE CORROSION IN CENTER OF YOKE. REMOVED CORROSION FROM SURFACE OF NR 2 PYLON YOKE CENTER AND COATED SURFACE WITH CARBOLINE. 2 H 7 4 4F RT A49EU 1998081400262 19980814 00262 EU 1998 8 14 98ZZZX2736 1 19980106 A 5320 SILL BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - AFT SERVICE DOOR SILL PLATE HAS SEVERAL SPOTS OF LIGHT SURFACE CORROSION. NOTE: MARKED IN BLACK MARKER. REMOVED SURFACE CORROSION, TREATED, PRIMED AND PAINTED SERVICE DOOR SILL PLATE. 2 H 7 4 4F RT A49EU 1998081400263 19980814 00263 EU 1998 8 14 98ZZZX2737 1 19980106 A 2810 BOLTS BAG BAE146 BAE146200A 1500266 EU WING TANK LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - DURING GV INSPECTION OF WING, CENTER TANK EVIDENCE OF LOOSE JO BOLTS. NO CORROSION FOUND. REPORTED DETAILS OF FA STENERS TO RDO. C/W GEN VISUAL INSPECTION OF WING TANK JO BOLTS. C/W BOLT TORQUE CHECK TO FASTENERS, EXCEPT THOSE INSI DE THE VERTICAL BOX AREA. REPORTED ALL DETAILS TO BAE RDO FOR ASSESSMENT. REF: DJR/RJ0001-98. REPORTED LOOSE JO BOLT S ACCEPTABLE. 4000 FLT REINSP REQUIRED. 2 H 7 4 4F RT A49EU 1998081400264 19980814 00264 EU 1998 8 14 98ZZZX2738 1 19980128 A 5230 SEAL CAGE BAG BAE146 BAE146200A 1500266 EU CARGO DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FRONT CARAGO BAY DOOR; LOWER FORWARD SEAL CAGE DENTED AND CRACKED LOWER AFT SEAL CAGE CRACKED. REPLACED BOTH LOWE R SEAL CAGES. 2 H 7 4 4F RT A49EU 1998081400265 19980814 00265 EU 1998 8 14 98ZZZX2739 1 19980105 A 7120 MOUNT BAG BAE146 BAE146200A 1500266 EU NR 1 PYLON DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 1 PYLON LORD MOUNT ATTACH BRACKET CENTER RIVET SHEARED. INSTALLED BOLT AT CENTER LORD MOUNT RACKET POSITION. R EF: FAX PJN/1196R-92. REPLACED BOTH LORD MOUNT RUBBER BUSHINGS. 2 H 7 4 4F RT A49EU 1998081400266 19980814 00266 EU 1998 8 14 98ZZZX2740 1 19980105 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU BS 41-44 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FLOORBEAMS AND SUPPORT STRUCTURE FRAMES 41-44 HAS SEVERAL SPOTS OF LIGHT SURFACE CORROSION ON TOP OF GUSSET PLATES AND INTERCOSTALS. ALL SPOTS ARE MARKED WITH BLACK MARKER. CLEANED AND REMOVED SURFACE CORROSION. TREATED, PRIMED AND PAINTED AFT VEST FLOORBEAMS SUPPORT STRUCTURE FRAMES 41-44 GUSSET PLATES AND INTERCOSTALS. 2 H 7 4 4F RT A49EU 1998081400267 19980814 00267 EU 1998 8 14 98ZZZX2742 1 19980106 A 7120 MOUNT BAG BAE146 BAE146200A 1500266 EU NR 3 PYLON DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 3 PYLON SHOULDER COWL LORD MOUNT BRACKET CENTER RIVET HEAD SHEARED OFF. REPLACED NR 3 PYLON LORD MOUNT BRACKET CENTER FASTENER IAW BAE FAX PJN/1196R-92. 2 H 7 4 4F RT A49EU 1998081400268 19980814 00268 EU 1998 8 14 98ZZZX2743 1 19980106 A 5400 BRACKET BAG BAE146 BAE146200A 1500266 EU NR 3 NACELLE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 3 ENGINE SHOULDER COWL - TERMINAL BOARD SUPPORT BRACKET FORWARD, CRACKED. REPLACED NR 3 ENGINE FORWARD TERMINA L BOARD SUPPORT BRACKET ON SHOULDER COWL. 2 H 7 4 4F RT A49EU 1998081400269 19980814 00269 EU 1998 8 14 98ZZZX2744 1 19980107 A 5320 THRESHOLD BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - AFT PASSENGER DOOR SILL PLATE AND THRESHOLD HAS ONLY A COUPLE SPOTS OF LIGHT SURFACE CORROSION. NOTE: MARKED WITH BLACK MARKER. REMOVED CORROSION ON AFT PASSENGER DOOR SILL PLATE AND THRESHOLD. TREATED AREA, PRIMED AND PAINTED. 2 H 7 4 4F RT A49EU 1998081400270 19980814 00270 EU 1998 8 14 98ZZZX2745 1 19980108 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU BS 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - MLG BAY PRESSURE DIAPHRAM ROOF HAS A FLOORBEAM, (NR 19), AT FR 29 RT SIDE UNDER OUTBOARD SEAT RAIL IN CABIN THAT H AS A SMALL CRACK DEVELOPING AROUND A FASTENER HEAD. REPAIRED RT BEAM NR 19 AT FR 29 IAW BAE DRAWING HC536H92 11 AND BAE FAX DJR/RJ0207-97. 2 H 7 4 4F RT A49EU 1998081400271 19980814 00271 EU 1998 8 14 98ZZZX2746 1 19980113 A 5320 BRACKET BAG BAE146 BAE146200A 1500266 EU CABIN BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - IN CABIN AT RT SIDE BETWEEN FRAMES 39 AND 40 JUST BELOW SERVICE DOOR, UPPER LONGERON, IS A BRACKET THAT IS BROKEN WHICH SECURES THE OUTER PSU SUPPORT RAILS AFT END. REMOVED AND REPLACED CRACKED BRACKET WITH NEW BRACKET AFT RT PSU SUP PORT RAIL JUST FORWARD OF RT SERVICE DOOR. (X) 2 H 7 4 4F RT A49EU 1998081400272 19980814 00272 EU 1998 8 14 98ZZZX2747 1 19980113 A 5320 SUPPORT BAG BAE146 BAE146200A 1500266 EU BS 26 DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FLOOR SUPPORT SIDE RAILS ON BOTH LT AND RT SIDES OF CABIN AT FRAME 26 HAVE SHEARED RIVETS. REMOVED AND REPLACED R IVETS ON LT AND RT FLOOR SUPPORT SIDE RAILS AFT FRAME 26. 2 H 7 4 4F RT A49EU 1998081400273 19980814 00273 EU 1998 8 14 98ZZZX2748 1 19980114 A 7110 FRAME BAG BAE146 BAE146200A 1500266 EU COWL DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 1 ENGINE RT FORWARD COWL DOOR. LOWER AFT FRAME CHAFED. REPAIRED NR 1 ENGINE RT FORWARD COWL DOOR AFT LOWER FR AME IAW SRM 54-10-11. 2 H 7 4 4F RT A49EU 1998081400274 19980814 00274 EU 1998 8 14 98ZZZX2749 1 19980119 A 7110 FRAME BAG BAE146 BAE146200A 1500266 EU COWL DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 NR 4 ENGINE RT FORWARD COWL DOOR, LOWER AREA OF AFT FRAME CHAFED. REPAIRED LOWER AFT FRAME CHAFE IAW SRM 54-10-11, NR 4 RT FORWARD COWL DOOR. 2 H 7 4 4F RT A49EU 1998081400275 19980814 00275 EU 1998 8 14 98ZZZX2750 1 19980116 A 7110 SKIN BAG BAE146 BAE146200A 1500266 EU COWL DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 NR 4 ENGINE LFT FORWARD COWL DOOR, AFT INNER SKIN CHAFED. REPAIRED NR 4 ENGINE LT FORWARD COWL DOOR INNER SKIN IAW SRM 51-71-11. 2 H 7 4 4F RT A49EU 1998081400276 19980814 00276 EU 1998 8 14 98ZZZX2751 1 19980116 A 7110 SKIN BAG BAE146 BAE146200A 1500266 EU COWL DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 3 ENGINE LT FORWARD COWL DOOR. INNER SKIN FORWARD SECTION CHAFED. REPAIRED NR 3 ENGINE LT FORWARD COWL DOOR I NNER SKIN FORWARD SECTION IAW SRM 51-71-11. 2 H 7 4 4F RT A49EU 1998081400277 19980814 00277 EU 1998 8 14 98ZZZX2752 1 19980120 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FORWARD CANOPY SKIN HAS A RIVET HEAD UNDER THE NR 5 FOR '656' AT C/L THAT HAS AN OLD LIGHTNING STRIKE PIT MEASURIN G APPROXIMATELY .030 INCH - .035 INCH DEEP WITHOUT PAINT BEING REMOVED. REPLACED RIVET PER AVRO FAX REF DJR/RJ0028-98. 2 H 7 4 4F RT A49EU 1998081400278 19980814 00278 EU 1998 8 14 98ZZZX2753 1 19980120 A 7110 SKIN BAG BAE146 BAE146200A 1500266 EU COWL DOOR CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 3 ENGINE LT AFT COWL DOORS INNER SKIN CHAFED AT PAN AREA. REPLACED NR 3 ENGINE LT AFT COWL DOOR DISHING PANEL. 2 H 7 4 4F RT A49EU 1998081400279 19980814 00279 EU 1998 8 14 98ZZZX2754 1 19980112 A 5250 HINGE BAG BAE146 BAE146200A 1500266 EU LAVATORY DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FORWARD LAVATORY DOOR HINGE POST CORRODED ON BOTTOM END. REMOVED CORROSION, TREATED, PRIMED AND PAINTED. 2 H 7 4 4F RT A49EU 1998081400280 19980814 00280 EU 1998 8 14 98ZZZX2755 1 19980122 A 2540 SPRING BAG BAE146 BAE146200A 1500266 EU LAVATORY BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 FORWARD LAVATORY TRASH BIN LID SPRINGS BROKEN. REPLACED SPRINGS AS NEEDED, OPS CHECKED GOOD. 2 H 7 4 4F RT A49EU 1998081400281 19980814 00281 EU 1998 8 14 98ZZZX2756 1 19980108 A 5411 RIB BAG BAE146 BAE146200A 1500266 EU NR 3 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 3 PYLON BOX STRUCTURE AT RIB 4 OTBD BOTTOM FLANGE HAS A CRACK DEVELOPING THAT IS APPROXIMATELY .3750 INCH LONG. NR 3 PYLON CRACKING RIB 4 LOWER FLANGE .3750 INCH LONG IS ACCEPTABLE AND MAY CONTINUE IN SERVICE. 1,000 CYCLE REPEAT INSPECTION. DETAILS REPORTED TO BAE RDO - REF RIL HC546H9018, GENERATED W/C FOR REINSPECT. 2 H 7 4 4F RT A49EU 1998081400282 19980814 00282 EU 1998 8 14 98ZZZX2757 1 19980119 A 3340 LIGHT BAG BAE146 BAE146200A 1500266 EU AFT FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - TAIL NAVIGATION LAMP CASTING CHAFED ON LT SIDE AND SHOWS LARGE GAP TO AIRBRAKE ON RT SIDE. BLENDED OUT CHAFED TO A SMOOTH DEPRESSION, PERFORMED LIQUID PENETRANT INSPECTION. REF: WC 3046, NO CRACKS NOTED, RE-PROTECTED AREA WITH ALOC ROM, PRIMER AND PAINT PER FAX GB/RJ022-94. ADJUSTED TRIPOD ASSY TO CENTER OF AIRBRAKE. 2 H 7 4 4F RT A49EU 1998081400283 19980814 00283 EU 1998 8 14 98ZZZX2758 1 19980202 A 5320 ANGLE BAG BAE146 BAE146200A 1500266 EU FUSELAGE BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 CAMLOCK RECEPTICAL AT FORWARD ATTACH SUPPORT STRUCTURE UNDER PANEL 286FT BROKEN OFF (BASE METAL BROKEN). REMOVED AND RE PLACED ANGLE BRACKET, DRILLED AND LOCATED HOLES. INSTALLED BRACKET AND NUT PLATES AND CAMLOC RECEPTACLES. OPS CHECK GO OD. 2 H 7 4 4F RT A49EU 1998081400284 19980814 00284 EU 1998 8 14 98ZZZX2759 1 19980106 A 5260 STEP BAG BAE146 BAE146200A 1500266 EU AIRSTAIR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FORWARD AIRSTAIRS THIRD STEP FROM TOP CORRODED. REPLACED STEP. 2 H 7 4 4F RT A49EU 1998081400285 19980814 00285 EU 1998 8 14 98ZZZX2760 1 19980108 A 5411 FRAME BAG BAE146 BAE146200A 1500266 EU NR 4 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 4 PYLON BOX STRUCTURE AT RIB NR 4 BOTTOM OTBD FLANGE HAS CRACK APPROXIMATELY .3750 INCH LONG. NR 4 PYLON CRACK ING RIB 4 LOWER FLANGE .3750 INCH LONG IS ACCEPTABLE AND MAY CONTINUE IN SERVICE. 1,000 CYCLE REPEAT INSPECTION. DETAI LS REPORTED TO BAE RDO. REF: RIL HC546H9018. GENERATED W/C FOR REINSPECT. 2 H 7 4 4F RT A49EU 1998081400286 19980814 00286 EU 1998 8 14 98ZZZX2761 1 19980102 A 2710 CABLE BAG BAE146 BAE146200A 1500266 EU LT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - LEFT WING CLAD AILERON INTERCONNECT CABLE IS CORRODED AND NEEDS CHANGING. REMOVED AND REPLACED LT OUTBOARD AILERO N INTERCONNECT CABLE AND ADJUSTED IAW MM 27-11-00. W/C 5023 GENERATED FOR FUNCTIONAL CHECK. 2 H 7 4 4F RT A49EU 1998081400287 19980814 00287 EU 1998 8 14 98ZZZX2762 1 19980123 A 5720 TIP BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - CLOSE OUT FAIRING AT RIB 20, LT WING TIP AREA CRACKED. PATCHED SAID CRACKED AREA IAW BAE SRM, PAINTED AND FOUND S ERVICEABLE. 2 H 7 4 4F RT A49EU 1998081400288 19980814 00288 EU 1998 8 14 98ZZZX2763 1 19980116 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - LT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD BETWEEN RIBS 7 AND 8. REMOVED AND REPLACED WITH NEW PART AT TRAI LING EDGE AT SKIN STIFFENERS BETWEEN RIBS 7 AND 8, LT WING. 2 H 7 4 4F RT A49EU 1998081400289 19980814 00289 EU 1998 8 14 98ZZZX2764 1 19980123 A 5730 SKIN BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 QTW - RT WING OUTER TIP FAIRING PLATE ASSY IS CRACKED. NOTE - LOOKS REPAIRABLE. LOCATED AT RIB 20. INSTALLED PATCH ON CRACKED AREA IAW BAE SRM, PAINTED AND FOUND SERVICEABLE. 2 H 7 4 4F RT A49EU 1998081400290 19980814 00290 EU 1998 8 14 98ZZZX2765 1 19980102 A 5411 RIB BAG BAE146 BAE146200A 1500266 EU NR 2 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - NR 2 PYLON RIB 4 LOWER FLANGE HAS .125 INCH LONG CRACK ON INBOARD SIDE OF CUT-OUT. CRACK MAY CONTINUE IN SERVICE WITH REPETITIVE INSPECTIONS IAW RIL HC546H9018. REPORTED DETAILS TO BAE RDO. GEN W/C FOR REINSPECT. 2 H 7 4 4F RT A49EU 1998081400291 19980814 00291 EU 1998 8 14 98ZZZX2766 1 19980105 A 7120 MOUNT BAG BAE146 BAE146200A 1500266 EU NR 1 ENGINE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 NR 1 MOTOR YOKE ASSEMBLY HAS SLIGHT SURFACE CORROSION AT CENTER AREA OF YOKE. CLEANED AREA AND REMOVED SURFACE CORROSIO N FROM NR 1 ENGINE MOUNT YOKE IAW A46 SRM 51-20-11. COATED AREA. REF: 51-20-11. 2 H 7 4 4F RT A49EU 1998081400292 19980814 00292 EU 1998 8 14 98ZZZX2767 1 19980116 A 2910 BRACKET BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - RT WING T/E LOWER HYDRAULIC LINE CLAMP BRACKET CRACKED AT RIB NR 5. LOCALLY MANUFACTURED PART PER DRAWING HC932H0 211 AND REMOVED AND REPLACED HYDRUALIC CLAMP BRACKET AT RT RIB 5. 2 H 7 4 4F RT A49EU 1998081400293 19980814 00293 EU 1998 8 14 98ZZZX2768 1 19980102 A 2710 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU RT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - RIGHT CLAD COVERED AILERON INTERCONNECT CABLE IS CORRODED AT OUTBOARD PULLEY. REMOVED AND REPLACED RIGHT OUTBOARD AILERON INTERCONNECT CABLE AND ADJUSTED IAW MM 27-11-00. W/C 5023 GENERATED FOR FUNCTIONAL CHECK. 2 H 7 4 4F RT A49EU 1998081400295 19980814 00295 EU 1998 8 14 98ZZZX2770 1 19980120 A 5730 SKIN BAG BAE146 BAE146200A 1500266 EU RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - RIGHT WING BOTTOM SKIN FUEL PANEL NR 611DB RECESS HAS SMALL SPORTS OF SURFACE CORROSION, SPOTS MARKED WITH BLACK M ARKER. CLEANED CORROSION WITH MINOR BLENDING, RE-TREATED RECESS AS REQUIRED. 2 H 7 4 4F RT A49EU 1998081400296 19980814 00296 EU 1998 8 14 98ZZZX2771 1 19980121 A 5730 SKIN BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - RIGHT WING TOP SKIN FORWARD EDGE OVER THE FRONT SPAR INBOARD OF RIB 2 APPROXIMATELY 6 INCHES, HAS A CRACK THAT IS 1.75 INCHES LONG THAT RUNS FOR AND AFT BETWEEN 2 FASTENERS, CRACK WAS VERIFIED USING EDDY CURENT INSPECTION TECHNIQUE. R EPAIRED IAW BAE REPAIR DRAWING HC573H9018 BAE FAX REF DJR/RJ0031-98, DJR/RJ0024-98, DJR/RJ0890-97, AND JM/RJ0901/97. 2 H 7 4 4F RT A49EU 1998081400297 19980814 00297 EU 1998 8 14 98ZZZX2772 1 19980314 A 2761 4101H2 ACTUATOR BAG BAE146 BAE146300A 1500267 EU SPOILER FAILED A A6WA K NONE E VIBRATION/BUFFET CR CRUISE 1 GL 31 615AW 6842 FYH157973 E3141 MKE - FLT 619 - AIRFRAME VIBE AT 280 KNOTS WAS WRITTEN ON TERMINATION ATW LAST NIGHT, EXTENSIVE T/S REVEALED NO DEFECT. MAINTENANCE REQUESTED CHECK FLIGHT AND CONFIRMED VIBE WHEN ROLLING TO RIGHT, SUSPECT SPOILER. REMOVED AND REPLACED RT ROLL SPOILER ACTUATOR, OPS CHECKED GOOD. 2 H 7 4 4F RT A49EU 1998081400298 19980814 00298 EU 1998 8 14 98ZZZX2773 1 19980317 A 2750 676801007 COMPUTER BAG BAE146 BAE146200A 1500266 EU E/E BAY MALFUNCTIONED A A6WA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 31 181US 2497 DRG101382 E2042 DEN -- FLT 661 - FLAP FAULT AND FLAPS INOPERABLE INDICATION, FLAPS FROZEN AT 18 DEGREES AFTER TAKEOFF. REMOVED AND REPL ACED FLAP COMPUTER, OPS CHEKCED GOOD, INSPECTED FLAP DRIVE UNITS, CLEANED ALL FLAP CONTROL AND INDICATORS, CANNON PLUGS. OPS CHECKED GOOD MANY TIMES. 2 H 7 4 4F RT A49EU 1998081400299 19980814 00299 EU 1998 8 14 98ZZZX2774 1 19980107 A 2761 BOLT BAG BAE146 BAE146200A 1500266 EU SPOILER CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - LEFT WING OUTER LIFT SPOILER AFT JACK BOLT CORRODED AND PLATING COMING OFF. REMOVED AND REPLACED BOLT. 2 H 7 4 4F RT A49EU 1998081400300 19980814 00300 EU 1998 8 14 98ZZZX2775 1 19980120 A 5320 BOLT BAG BAE146 BAE146200A 1500266 EU MLG CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ATW - MLG BAY LOWER LONGERON AFT INNER BOLT IS CORRODED AND PROTECTIVE COATING IS WORN OFF. REPLACED MLG BAY LOWER LONG ERON AFT INNER BOLT AT THIS TIME WITH A NEW ONE. INSTALLATION C/W UPON COMPLETION OF SSI 53200141C. 2 H 7 4 4F RT A49EU 1998081400301 19980814 00301 NE 1998 8 14 PLGA980513A 2 19980513 A 7200 6053T88G01 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LEFT OVERTEMP A PLGA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NE 05 751BA 340A157 GEE367337 LGA - FLT 4562 - AFTER TAKEOFF, THE LEFT ENGINE OVERTEMP WARNING ILLUMINATED FOLLOWED BY A POWER SURGE. THE OVERTEMP WA RNING REMAINED ILLUMINATED FOR 4 SECONDS THEN EXTINGUISHED. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. MAIN TENANCE REPLACED THE LEFT ENGINE DUE TO EXCESS OVERTEMP. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1998081400302 19980814 00302 EU 1998 8 14 C2XA98IA256 1 19980710 A 5712 S5721158100000 RIB AEROSP ATR42 ATR42320 8680930 EU RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING LEADING EDGE SUPPORT AT RIB NR 30 CRACKED. MAINTENANCE STOP DRILLED T HE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400303 19980814 00303 1998 8 14 C2XA98CL053 3 19980712 A 6140 1143800663 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 09 81538 5102 375 UE199 CLE - FLT 3287 - THE CREW REPORTED THAT DURING TAXI OUT, THE RIGHT HAND PROP RPM INDICATOR WAS READING ZERO. THE AIRCRA FT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND PROP RPM INDICATOR IA W B1900 MM 77-10-00. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A24CE 1998081400304 19980814 00304 SO 1998 8 14 C2XA98CL052 1 19980712 A 3232 20725 ACTUATOR EMB 120 EMB120RT SO NLG OUT OF ADJUST A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 34712 18525 149 120111 ROC - FLT 3119 - THE CREW REPORTED THE NOSE GEAR DOORS WOULD NOT CLOSE AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO FIEL D WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR ACTUATOR IAW EMB-120 MM 32-30-00. OPERATIONAL C HECKS WERE SATISFACTORY IAW EMB-120 MM 32-30-00. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 1998081400305 19980814 00305 SO 1998 8 14 C2XA98CL051 1 19980706 A 2121 EVAC2322C2 FAN EMB 120 EMB120RT SO NR 2 PACK FAILED A C2XA D RETURN TO BLOCK B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 51726 13413 583 120174 CLE - FLT 3290 - CREW REPORTED THAT DURING TAXI, THE SMOKE LIGHT ILLUMINATED ON THE M.A.P. AND ON THE FLIGHT ATTENDANT'S SMOKE ALARM PANEL. THE CREW ALSO SMELLED SMOKE IN THE CABIN AND COCKPIT WITH BOTH PACKS IN LOW. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE NR 2 GROUND COOLING FAN IAW EMB-120 MM 21-51-03, OPERATIONAL CHECKS WERE SAT ISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 1998081400306 19980814 00306 EU 1998 8 14 C2XA98IA247 1 19980707 A 3350 0341516 FUSE AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FORWARD EMERGENCY EXIT LOWER LIGHTING ASSEMBLY INOPERATIVE. MAINTENANCE REM OVED AND REPLACED A BLOWN FUSE IN THE EMERGENCY LIGHT BATTERY PACK. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( X) 2 H 7 2 4T RT A53EU 1998081400307 19980814 00307 EU 1998 8 14 C2XA98IA248 1 19980707 A 5315 S5317310300100 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU COCKPIT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING C-CHECK INSPECTION, FOUND FLOOR STRUCTURE AT CAPTAIN'S SIDE SEAT ATTACHMENT AREA CORRODED. MAINTENANCE REM OVED AND REPLACED THE FLOOR STRUCTURE IAW ATR-42 SRM 51-25-02 AND SRM 53-17-70. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TAT: 17,634.1 HOURS. TC: 20,767. (X) 2 H 7 2 4T RT A53EU 1998081400308 19980814 00308 EU 1998 8 14 C2XA98IA249 1 19980707 A 5315 S53173206201 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU COCKPIT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING C-CHECK INSPECTION, FOUND FLOOR STRUCTURE AT FIRST OFFICER'S SIDE SEAT ATTACHMENT AREA CORRODED. MAINTENAN CE REMOVED AND REPLACED THE FLOOR STRUCTURE IAW ATR-42 SRM 51-25-02 AND SRM 53-17-70. THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. TT: 17,634.1 HOURS. TC: 20,767. (X) 2 H 7 2 4T RT A53EU 1998081400309 19980814 00309 EU 1998 8 14 C2XA98IA250 1 19980707 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU BS 34-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE INBOARD AFT SEAT TRACK CORRODED BEYOND LIMITS FROM FRAMES 34 TO 36. M AINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW ATR-42 SRM 51-25-04. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (X) 2 H 7 2 4T RT A53EU 1998081400310 19980814 00310 EU 1998 8 14 JBXA980046 1 19980723 A 2760 233005 ACTUATOR FOKKER F28 F28MK0100 4990807 EU SPEED BRAKE CRACKED A JBXA K NONE K FLUID LOSS DE DESCENT 1 SO 05 132ML MC089 11321 DURING GEAR EXTENSION, LOST NR 1 HYDRAULIC SYSTEM. LANDED WITH GEAR DOORS EXTENDED. HYDRAULIC QUANTITY READS ZERO. IN SPECTED AND FOUND SPEED BRAKE ACTUATOR FILTER HOUSING CRACKED. REMOVED AND REPLACED SPEEDBRAKE ACTUATOR IAW F-100 MM 27 -61-02. OPERATIONAL AND LEAK CHECKS GOOD, OKAY FOR SERVICE. (X) 2 L 7 2 4F RT 1998081400311 19980814 00311 SO 1998 8 14 COMA9810171 1 19980806 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT LATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 205CA 120205 SERVICE DOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR UNLATCHED. SECURED DOOR CLOSED AND AIRCRAFT RETURNED TO S ERVICE. 2 L 7 2 4T RT A31SO 1998081400312 19980814 00312 NM 1998 8 14 UPS98227335 1 19980724 A 5315 FLOORBEAM BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI CORROSION ON FLANGES OF LONGITUDINAL FLOORBEAM. REPLACED PER DWG 65-34144. 2 L 7 3 4F A3WE 1998081400313 19980814 00313 NM 1998 8 14 UPS98227336 1 19980727 A 5320 LINK BOEING 727 72730C 1384009 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI, CORROSION ON EXPANSION LINK BS 870 RBL 25. REPLACED PER DRAWING 65-34144. 2 L 7 3 4F A3WE 1998081400314 19980814 00314 NM 1998 8 14 UPS98227337 1 19980728 A 5347 SEAT TRACK BOEING 727 72730C 1384009 NM BS 760-785 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI, SEAT TRACK CORRODED BS 760-785 RBL 25. REPLACED TRACK PER SRM 53-10-5. 2 L 7 3 4F A3WE 1998081400315 19980814 00315 NM 1998 8 14 UPS98227338 1 19980706 A 5320 EXPANSION LINK BOEING 727 72730C 1384009 NM BS 860 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI, WHILE WORKING INTERIOR 140 CUST NR 832471 FOUND STA 860 RBL 45 EXPANSION LINK CORRODED. REMOVED COR ROSION FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-1. 2 L 7 3 4F A3WE 1998081400316 19980814 00316 NM 1998 8 14 UPS98227339 1 19980728 A 5320 BRACKET BOEING 727 72730C 1384009 NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 906UP 19314 INSPECTION TYPE:SI, CORROSION AROUND EXPANSION LINK BRACKET. REPLACED BRACKET PER SRM 53-10-1. 2 L 7 3 4F A3WE 1998081400317 19980814 00317 WP 1998 8 14 UPS98827319 1 19980727 A 5320 37502571N SPLICE DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, LONGERON 31L SPLICE FITTING CRACKED FS 440-460. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998081400318 19980814 00318 WP 1998 8 14 UPS98827320 1 19980725 A 5720 36412572 DOUBLER DOUG DC8 DC871F 302199D WP WS 828.75 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, RT WING L/E AT W/S XFS 828.75, THE INTERNAL DOUBLER HAS HEAVY CORROSION AT FWD END OF ACCESS PANEL. R EMOVED AND REPLACED DOUBLER IAW SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998081400319 19980814 00319 WP 1998 8 14 UPS98827322 1 19980725 A 5730 ACCESS PANEL DOUG DC8 DC871F 302199D WP LT WING TANK CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, LT WING NR 2 MAIN TANK INBD AFT ACCESS PANEL LAND CRACKED AT OTBD AFT CORNER. REPAIRED IAW SRM 57-2- 1. 2 L 7 4 4F RT 4A25 1998081400320 19980814 00320 WP 1998 8 14 UPS98827323 1 19980727 A 5320 3754473501 SPLICE DOUG DC8 DC871F 302199D WP BS 380-400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, LONGERON 31L SPLICE FITTING CRACKED FS 380-400. REMOVED AND REPLACED FITTING IAW SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998081400321 19980814 00321 WP 1998 8 14 UPS98827324 1 19980724 A 5347 5759223513 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 980-1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, FS 980-1070 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998081400322 19980814 00322 WP 1998 8 14 UPS98827325 1 19980724 A 5347 5759233513 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 980-1070 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, FS 980-1070 ABOVE STR 33R, CARGO TRACK AND SPLICE HAVE HEAVY CORROSION. REMOVED AND REPLACED CARGO T RACK IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998081400323 19980814 00323 WP 1998 8 14 UPS98827326 1 19980724 A 5347 5759223523 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 1330-1410 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, FS 1330-1410 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLA CEMENT CARGO TRACK IAW SRM 51-3-0 AND DWG 5751516. 2 L 7 4 4F RT 4A25 1998081400324 19980814 00324 WP 1998 8 14 UPS98827327 1 19980724 A 5347 5716454295 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 1240-1320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, FS 1240-1320 ABOVE STR 33R, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPL ACEMENT TRACK IAW SRM 51-3-0 AND DWG 5751516. 2 L 7 4 4F RT 4A25 1998081400325 19980814 00325 WP 1998 8 14 UPS98827328 1 19980724 A 5347 5759223513 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 1410-1490 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, FS 1410-1490 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPL ACEMENT TRACK IAW SRM 51-3-0 AND DWG 5151516. 2 L 7 4 4F RT 4A25 1998081400326 19980814 00326 WP 1998 8 14 UPS98827329 1 19980726 A 5320 57508683 FITTING DOUG DC8 DC871F 302199D WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, TAIL SKID INTERNAL MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20. 2 L 7 4 4F RT 4A25 1998081400327 19980814 00327 WP 1998 8 14 UPS98827330 1 19980728 A 5313 1415997 LONGERON DOUG DC8 DC871F 302199D WP BS 1700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, LONGERON 36 FS 1700 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-2 -2. 2 L 7 4 4F RT 4A25 1998081400328 19980814 00328 WP 1998 8 14 UPS98827331 1 19980726 A 5320 564932955 DOUBLER DOUG DC8 DC871F 302199D WP BS 1776 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, FS 1776 DOOR 62 DOUBLER SEVERE EXFOLIATED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IA W SRM 51-1- 20 AND DWG 5649329. 2 L 7 4 4F RT 4A25 1998081400329 19980814 00329 WP 1998 8 14 UPS98827332 1 19980725 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 240-260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, BETWEEN FS 240-260, L-34L TO L-35L 8 CRACK IN OUTER PLATING FUSELAGE SKIN. REPAIRED IAW DHC SK 715-6 33. 2 L 7 4 4F RT 4A25 1998081400330 19980814 00330 WP 1998 8 14 UPS98827333 1 19980728 A 5720 1416644 ANGLE DOUG DC8 DC871F 302199D WP BS 798 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, WING CENTER SECTION ( UPPER ) AT FS 798 RBL 44, CHORD ANGLE HAS HEAVY CORROSION. REMOVED AND REPLACE D CHORD ANGLE IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998081400331 19980814 00331 WP 1998 8 14 UPS98827334 1 19980725 A 5720 36412572 DOUBLER DOUG DC8 DC871F 302199D WP WS 797.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C, RT WING L/E AT W/S XFS 797.500, THE INTERNAL DOUBLER HAS HEAVY CORROSION AT O/B END OF ACCESS PANEL. REMOVED AND REPLACED DOUBLER IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998081400332 19980814 00332 EU 1998 8 14 QXEA9801058 1 19980805 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 475AU 11222 BOI - OVERHEAD EMERGENCY EVACUATION LIGHT AT ROW 7 IS INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TEST SHOWS NORMAL OPERATION. 2 L 7 2 4F RT A20EU 1998081400333 19980814 00333 EU 1998 8 14 QXEA9801059 1 19980804 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 BOI - EMERGENCY EXIT LIGHT ABOVE COCKPIT IS INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TEST SHOWS NORM AL OPERATION. 2 L 7 2 4F RT A20EU 1998081400334 19980814 00334 EU 1998 8 14 QXEA9801060 1 19980805 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 BOI - EMERGENCY EXIT LIGHT AT ROW 9 IS INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TEST SHOWS NORMAL OP ERATION. 2 L 7 2 4F RT A20EU 1998081400335 19980814 00335 EU 1998 8 14 QXEA9801061 1 19980806 A 3350 5515800106 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 GEG - EMERGENCY EXIT LIGHT IN FORWARD CABIN IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LIGHT ASSEMBLY AND OPERATI ONALLY TESTED, TEST SHOWS NORMAL OPERATION. 2 L 7 2 4F RT A20EU 1998081400336 19980814 00336 EU 1998 8 14 98FDEA00489 1 19980806 A 3234 224TS05Y MODULE AIRBUS 300 A300F4605R 3930327 EU LANDING GEAR INOPERATIVE A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 658FE 752 98-193 - GEAR WOULD NOT RETRACT. STOPPED MID POSITION. TRIED BOTH SYSTEMS. REMOVED AND REPLACED LANDING GEAR HANDLE C ONTROL MODULE PER M/M 32-31-11-4 RETRACTION CHECK OK. R11 012823 2 L 7 2 4F RT A35EU 1998081400337 19980814 00337 NM 1998 8 14 98FDEA00490 1 19980807 A 2612 893851 FIRE LOOP BOEING 727 7272S2F 1384O81 NM NR 1 ENGINE MALFUNCTIONED A FDEA F H ACTIVATE FIRE EXT. DEACTIVATE SYST/CIRCUITS N FALSE WARNING DE DESCENT 1 SO 25 203FE 22925 FIFTEEN TO TWENTY MILES FROM MEM, NR 1 ENG FIRE WARN AND BELL CAME ON. RAN ENG FIRE/SEVERE DMG CHECKLIST AND LIGHT REMA IN ON. BOTH FIRE BOTTLES FIRED, LIGHT ON. NR 1 HYDRAULIC A-SYSTEM CLOSED. FWD TO MEL/CDL: 26 - 6A CAT: C EXP: 17AUG98 FOUND A LOOP DEFECT. REMOVED AND REPLACED ENG LOOP, NO HELP. SUSPECT FIREWALL LOOP. ALSO, REMOVED AND REPLACED DETEC TOR UNIT, NO HELP. REINSTALLED ORIG ENG LOOP AND DETECT UNIT. REMOVED AND REPLACED RT AND LT ENG FIRE BOTTLES PER 727 M/M 26-21-1. REMOVED AND REPLACED NR 1 ENG FIREWALL LOOP AS M/M 26-11-12, OK FOR SERVICE. 2 L 7 3 4F A3WE 1998081400338 19980814 00338 NM 1998 8 14 98FDEA00491 1 19980807 A 5313 655623632 STRINGER BOEING 727 727227 1384078 NM BS 670 - 672 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION (C53-113-01,1) ON STRINGER 28 LT, BS 670-672 FWD CARGO BAY. *S/D* STRINGER 28 LT, BS 680-480 WAS BEING REPLA CED ON NR 140, NO FURTHER ACTION REQUIRED. 2 L 7 3 4F A3WE 1998081400339 19980814 00339 WP 1998 8 14 98FDEA00492 1 19980807 A 5720 BOLT DOUG DC10 DC1010F 3022111 WP BS 118-115 SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 061FE 46973 FOUND 3 BOLTS SHEARED AT BS XCW 118 TO XCW 115 RT AFT SPAR TOP SURFACE. *S/D* REMOVED AND REPLACED BOLT AND TORQUED. I NSP AND NDT, MEASURE BOLT HOLE, SPOT FACE AREA. 2 L 7 3 4F A22WE 1998081400340 19980814 00340 NM 1998 8 14 98FDEA00493 1 19980807 A 5313 655623632 STRINGER BOEING 727 727227 1384078 NM BS 557 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION (C53-113-0,1) ON STRINGER 28 LT, BS 557 FWD CARGO BAY. *S/D* REMOVED AND REPLACED STR 28 LT, BS 480-680 IAW FEDEX SRM 51-10-3. 2 L 7 3 4F A3WE 1998081400341 19980814 00341 WP 1998 8 14 MWEA98843 1 19980806 A 2560 113317 SLIDE COVER DOUG DC9 DC932 3022066 WP CABIN DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE GALLEY SERVICE DOOR SLIDE COVER FELL OFF, MAINTENANCE RE-INSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1998081400342 19980814 00342 WP 1998 8 14 MWEA98844 1 19980809 A 5230 59101417 PAN DOUG DC9 DC914 3022034 WP CARGO DOOR DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 700ME 45696 FOUND 2 HOLES IN FORWARD CARGO DOOR LOWER PAN. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998081400343 19980814 00343 WP 1998 8 14 MWEA98845 1 19980810 A 5312 99155617 BULKHEAD SUPPORT DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD MISINSTALLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 4 BOT ORIG HOLES ON VERTICLE JACK PAD SUPPORT WILL CREATE BELOW MINIMUM EDGE DISTANCE IN VERTICLE LEG ON AFT PRESS BULK TEE. MAINTENANCE FABRICATED AND INSTALLED DOUBLER ANGLE REPAIR. 2 L 7 2 4F A6WE 1998081400344 19980814 00344 WP 1998 8 14 MWEA98846 1 19980810 A 5311 9911843501 FRAME DOUG DC9 DC932 3022066 WP BS 1168 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND THE MOST AFT CANTED FRAME AT STATION 1168 CRACKED AT THE 9 O'CLOCK POSITION. MAINTENANCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998081400345 19980814 00345 WP 1998 8 14 MWEA98847 1 19980810 A 5320 5917497501 SUPPORT DOUG DC9 DC932 3022066 WP BS 996 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND JACK SUPPORT BRACKET BENT AT STATION 996 AT LONGERON 30. MAINTENANCE REMOVED AND REPLACED JACK SUPPORT BRACKET. 2 L 7 2 4F A6WE 1998081400346 19980814 00346 WP 1998 8 14 MWEA98848 1 19980810 A 5312 5910130387 BULKHEAD TEE DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND AFT PRESSURE BULKHEAD LOWER TEE DENTED BETWEEN LONGERON 29L-29R ON FORWARD LOWER LEG AND BETWEEN 29L-30 ON AFT LOW ER LEG. MAINTENANCE REMOVED AND REPLACED TEE. 2 L 7 2 4F A6WE 1998081400347 19980814 00347 WP 1998 8 14 MWEA98849 1 19980810 A 5320 9912243219 FORMER DOUG DC9 DC932 3022066 WP BS 965 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND FORMER BENT AT STATION 965 FROM L26L TO L26R. MAINTENANCE REMOVED AND REPLACED FORMER. 2 L 7 2 4F A6WE 1998081400348 19980814 00348 WP 1998 8 14 MWEA98850 1 19980810 A 5320 49176501 CLIP DOUG DC9 DC932 3022066 WP BS 995 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND SHOVEL CLIP CRACKED AT STATION 995 FROM L29L. MAINTENANCE REMOVED AND REPLACED SHOVEL CLIP. 2 L 7 2 4F A6WE 1998081400349 19980814 00349 WP 1998 8 14 MWEA98851 1 19980810 A 5320 991551735 FORMER DOUG DC9 DC932 3022066 WP BS 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND 2 CRACKS ON FORMER AT STATION 996 LONGERON 24L TO 25R. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 1998081400350 19980814 00350 WP 1998 8 14 MWEA98852 1 19980810 A 5311 995773937 FRAME DOUG DC9 DC932 3022066 WP BS 945 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND FRAME AT STATION 945 AFT LEG BENT UP BETWEEN L29R AND L28R ALSO BETWEEN L30 AND L29R AFT LOWER LEG. MAINTENANCE F ABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998081400351 19980814 00351 WP 1998 8 14 MWEA98853 1 19980810 A 5311 995791739 FRAME DOUG DC9 DC932 3022066 WP BS 937 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND FRAME AT STATION 937 BETWEEN L30 AND L29R LOWER AFT LEG BENT UP. MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUB LER. 2 L 7 2 4F A6WE 1998081400352 19980814 00352 WP 1998 8 14 MWEA98854 1 19980810 A 5512 5910625 PANEL DOUG DC9 DC981 3022081 WP RT HORIZ STAB MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 809ME 48071 THE HORIZONTAL STABILIZER RIGHT HAND LEADING EDGE PANEL HOLES DO NOT MATCH NEW SECTION. MAINTENANCE FABRICATED AND INST ALLED NEW LEADING EDGE PANEL. 2 L 7 2 4F A6WE 1998081400353 19980814 00353 WP 1998 8 14 MWEA98855 1 19980810 A 5511 59225802 SPAR CAP DOUG DC9 DC981 3022081 WP RT HORIZ STAB ELONGATED HOLES A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND SEVERAL ELONGATED HOLES IN RT HORIZONTAL STAB LEADING EDGE UP AND LWR SPAR CAP. MAINTENANCE REAMED UP AND LWR SPA R CAP AND FABRICATED AND INSTALLED SALVAGE BUSHINGS. 2 L 7 2 4F A6WE 1998081400354 19980814 00354 WP 1998 8 14 MWEA98856 1 19980810 A 5730 593050383 SKIN DOUG DC9 DC981 3022081 WP LT WING MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 809ME 48071 FOUND UNACCEPTABLE PREVIOUS REPAIR ON LEFT WING LOWER SKIN AT STATION 531.700. MAINTENANCE FABRICATED AND INSTALLED DOU BLER. 2 L 7 2 4F A6WE 1998081400355 19980814 00355 WP 1998 8 14 MWEA98857 1 19980810 A 5730 593050383 SKIN DOUG DC9 DC981 3022081 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND LEFT WING LOWER SKIN BLEND OUT BEYOND LIMITS AT AFT SPAR STATIONS 236XRS AND 392XRS. MAINTENANCE FABRICATED AND I NSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998081400356 19980814 00356 WP 1998 8 14 MWEA98858 1 19980810 A 5730 593050383 SKIN DOUG DC9 DC981 3022081 WP WS 60-64 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 48071 FOUND LEFT WING LOWER SKIN BLENDING AND CORROSION AT FORWARD EDGE OF AFT SKIN PANEL STRINGER 17 FROM XCW60-64. MAINTENA NCE FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998081400357 19980814 00357 NM 1998 8 14 P5CA9801215 1 19980727 A 5280 SKIN BOEING 747 747132 1384882 NM LT MLG DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT BODY MLG INBD AND OTBD STRUT DOOR ASSEMBILES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REMOVED MINOR SURFACE CORROSION IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1998081400358 19980814 00358 NM 1998 8 14 P5CA9801222 1 19980804 A 5280 SKIN BOEING 747 747132 1384882 NM RT MLG DOOR CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT BODY MLG BOTH INBOARD AND OUTBOARD STRUT DOOR ASSEMBLIES HAVE MANY SPOTS WITH LOST FINISH AND SURFACE CORROSION. REM OVED MINOR SURFACE CORROSION IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1998081400359 19980814 00359 NM 1998 8 14 P5CA9801224 1 19980712 A 5321 FLOOR BOEING 747 747122 1384872 NM BS 2020 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 BULK CARGO BS2020 LBL 48 AND 52 FLOOR PANEL SUPT HAT SECTION CRACKED. REPAIRED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998081400360 19980814 00360 NM 1998 8 14 P5CA9801225 1 19980721 A 5330 SKIN BOEING 747 747122 1384872 NM BS 530&570 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION ON FUSELAGE SKIN STA 530 AND 570 BELOW VHF ANTENNA. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-0 1 AND 51-10-02. 2 L 7 4 4F A20WE 1998081400361 19980814 00361 NM 1998 8 14 P5CA9801226 1 19980721 A 5330 SKIN BOEING 747 747122 1384872 NM BS 740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION ON FUSELAGE SKIN STA 740 STR 42-44R. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01 AND SRM 51-10 -02. 2 L 7 4 4F A20WE 1998081400362 19980814 00362 NM 1998 8 14 P5CA9801227 1 19980721 A 5330 SKIN BOEING 747 747122 1384872 NM BS 800-840 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION ON FUSLEAGE SKIN STA 800-840 BELLY STR 44L-44R. CORROSION REMOVED AND REPROTECTED PER SRM 51-01-01 AN D SRM 51-10-02. 2 L 7 4 4F A20WE 1998081400363 19980814 00363 NM 1998 8 14 P5CA9801228 1 19980727 A 5730 SKIN BOEING 747 747122 1384872 NM RT WING CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION ON RT WING UPPER WING SKIN SURFACE FORWARD AND OUTBOARD OF NR 7 SPOILER. REMOVED, PEENED AND REPROTEC TED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998081400364 19980814 00364 NM 1998 8 14 P5CA9801229 1 19980729 A 5330 PANEL BOEING 747 747122 1384872 NM BS 1040 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 AIR CONDITIONING PANEL BS 1040 BL 10-30 HAS CORRSOION. CORROSION REMOVED AND SURFACE REPROTECTED PER SRM 51-10-00 AND 5 1-10-02. 2 L 7 4 4F A20WE 1998081400365 19980814 00365 NM 1998 8 14 P5CA9801230 1 19980729 A 5320 69B031461 BRACKET BOEING 747 747122 1384872 NM BS 1500 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 SUPPORT BRACKET AT BS 1500 STR 21-22 RIGHT FOUND CRACKED. REPLACED SUPPORT BRACKET PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998081400366 19980814 00366 NM 1998 8 14 P5CA9801231 1 19980729 A 5311 FRAME BOEING 747 747122 1384872 NM BS 780 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 MAIN DECK BODY FRAME RADIUS FOUND CRACKED AT STR 6L BS 780. REPAIRED BODY FRAME PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998081400367 19980814 00367 NM 1998 8 14 P5CA9801232 1 19980730 A 5330 SKIN BOEING 747 747122 1384872 NM RT MLG WW CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION RT BODY GEAR WHEEL WELL SKIN WEB. REMOVED CORROSION AND REPROTECTED PER SRM 51-40-02 FIG 1. 2 L 7 4 4F A20WE 1998081400368 19980814 00368 NM 1998 8 14 P5CA9801233 1 19980728 A 5320 PANEL BOEING 747 747122 1384872 NM KEEL BEAM CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 KEEL BEAM ACCESS PANEL 191KK REAR ATTACH SUPPORT LOWER CHORD HAS SURFACE CORROSION. REMOVED CORROSION AND REPROTECTED P ER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998081400369 19980814 00369 NM 1998 8 14 P5CA9801234 1 19980731 A 5400 FAIRING BOEING 747 747122 1384872 NM NR 3 PYLON DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 3 PYLON NAC STA 320 SAIL BOAT RT FAIRING 474D HAS OUTER SKIN DELAMINATION. HOT BOND REPAIR PER SRM 51-40-06 FIG 13. 2 L 7 4 4F A20WE 1998081400370 19980814 00370 NM 1998 8 14 P5CA9801235 1 19980731 A 5311 FRAME BOEING 747 747122 1384872 NM BS 820 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 BS 820 STR 3L BODY FRAME RADIUS CRACKED. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1998081400371 19980814 00371 NM 1998 8 14 P5CA9801236 1 19980801 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION AT BS 2100 STR 3L. REMOVED CORROSION AND BLENDED AREA AND REPROTECTED PER SRM 51-10-01, 53-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998081400372 19980814 00372 NM 1998 8 14 P5CA9801237 1 19980801 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2080 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS 2080 STR 2L. REMOVED CORROSION AND RETREATED AREA PER SRM 51-10-01, 51-10-02 AND MM 51-24 -11. 2 L 7 4 4F A20WE 1998081400373 19980814 00373 NM 1998 8 14 P5CA9801238 1 19980801 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1960-2220 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT SKIN LAP JOINT BS 1960-2220 STR 12L. CLEANED CORROSION, BLENDED AREA AND REPROTECTED PER SRM 51-10-01, 53-30-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998081400374 19980814 00374 NM 1998 8 14 P5CA9801239 1 19980801 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2060 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION STRINGER L1. REMOVED CORROSION AND BLENDED AREA AND RETREATED PER SRM 51-10-01, 51-10-02 AND MM 51-24 -04. 2 L 7 4 4F A20WE 1998081400375 19980814 00375 NM 1998 8 14 P5CA9801240 1 19980801 A 5314 KEEL BEAM BOEING 747 747122 1384872 NM BS 1240-1260 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION ON RIVET HEADS ON KEEL BEAM AT BS 1240 TO 1260. REMOVED CORROSION, BLENDED AREA AND TREATED SURFACE P ER SRM 51-10-01, 51-10-02 AND 51-24-11. 2 L 7 4 4F A20WE 1998081400376 19980814 00376 NM 1998 8 14 P5CA9801241 1 19980801 A 5314 KEEL BEAM BOEING 747 747122 1384872 NM BS 1220 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON KEEL BEAM LOWER WEB BS 1220-40 BL R9-L9. REMOVED AND BLENDED CORROSION SURFACE PER SRM 51-10 -01, 51-10-02 AND 51-24-11. 2 L 7 4 4F A20WE 1998081400377 19980814 00377 NM 1998 8 14 P5CA9801242 1 19980801 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT MAIN DECK BS1960 STRINGER R12. BLENDED OUT AND REMOVED CORROSION PER SRM 51-10-02 AND 51-24- 11. 2 L 7 4 4F A20WE 1998081400378 19980814 00378 NM 1998 8 14 P5CA9801243 1 19980801 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2020-2180 CORRSODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT SKIN LAP JOINT AREA BS 2020-2180 STR 4R. REMOVED CORROSION, BLENDED AND REPROTECTED PER SRM 51-10-01, 53-30-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998081400379 19980814 00379 NM 1998 8 14 P5CA9801244 1 19980801 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2100 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS 2100 STR 3L. REMOVED CORROSION, BLENDED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998081400380 19980814 00380 NM 1998 8 14 P5CA9801245 1 19980801 A 5311 FRAME BOEING 747 747122 1384872 NM BS 600 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 BS 600 RT BODY FRAME RADIUS FOUND CRACKED. REPAIRED FRAME PER RS5322-33811, SRM 51-10-01, 51-30-02. 2 L 7 4 4F A20WE 1998081400381 19980814 00381 NM 1998 8 14 P5CA9801246 1 19980806 A 5320 SUPPORT BOEING 747 747132 1384882 NM BS 340 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION AT SUPPORT CHANNEL FOR DRAIN PAN AT BS 340. CORROSION REMOVED FROM SUPPORT CHANNEL AT STA 340 IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998081400382 19980814 00382 NM 1998 8 14 P5CA9801247 1 19980806 A 5320 SUPPORT BOEING 747 747132 1384882 NM CABIN CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION FOUND UNDER F/E SEAT FLOOR PANEL SUPPORT BEAM. REMOVED SURFACE CORROSION ON SUPPORT BEAM AND TREATED IAW SRM 51-10-06. 2 L 7 4 4F A20WE 1998081400383 19980814 00383 NM 1998 8 14 P5CA9801248 1 19980806 A 5315 FLOORBEAM BOEING 747 747132 1384882 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION FOUND ON BOTTOM OF FLOORBEAM BS 600. REMOVED SURFACE CORROSION IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998081400384 19980814 00384 NM 1998 8 14 P5CA9801249 1 19980806 A 7110 SKIN BOEING 747 747132 1384882 NM NR 3 ENG COWL CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 3 ENG O/B FAN COWL CRACK ON UPPER FWD AND AFT HINGE CUTOUT. BLENDED OUT CRACKED AREA AROUND FORWARD HINGE. CRACK WI THIN SRM LIMITS PER SRM 51-40-06 FIG 2. REPAIRED PER SRM 51-40-06. 2 L 7 4 4F A20WE 1998081400385 19980814 00385 NM 1998 8 14 P5CA9801250 1 19980806 A 5280 DOOR BOEING 747 747132 1384882 NM LT MLG CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION LEFT FLYING DOOR LOWER SECTION ALONG LOWER EDGE OF ITS INNER SURFACE AROUND BOLD HEADS. REMOVED AND R EPLACED FASTENERS AND CLEANED AREAS IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998081400393 19980814 00393 SW 1998 8 14 98ZZZX2784 1 19980528 A 2910 AE99115J COUPLING BELL 214 214ST 1182106 SW HYDRAULIC SYSTEM LEAKING A HEEA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 03 3897N 28106 HYDRAULIC LIGHT ILLUMINATED IN CRUISE FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEAK AT B-NUT ATTACHING HYDRA ULIC QUICK DISCONNECT. TIGHTENED CONNECTION. REF: 214ST IPC, FIGURE 29-4, ITEM 82. 2 G 7 2 4U H10SW 1998081400404 19980814 00404 GL 1998 8 14 98ZZZX2795 2 19980522 A 7322 25246429 FUEL CONTROL BENDIX BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL ENGINE FAILED A HEEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS HO HOVERING 1 SW 03 911BR 8709 159 334872 S719 CAE834412 AFTER PICKING AIRCRAFT UP TO A HOVER TO REPOSITION, NR 1 ENGINE DECELLED. LANDED WITHOUT INCIDENT. SUSPECT INTERNAL F/ C FAILURE. MAINTENANCE REPLACED FUEL MANAGEMENT SYTEM. 1 G 7 2 3U 3 U H3EU E4CE 1998081400419 19980814 00419 NM 1998 8 14 K3HA980095 1 19980807 A 2150 39854021 VALVE BOEING 727 727225 1384077 NM RT PACK STUCK A K3HA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 25 354PA 20624 UNABLE TO CONTROL PRESSURE IN AUTO OR MANUAL. INSPECTED PNEUMATIC SYSTEM. FOUND RIGHT HAND FORWARD PACK VALVE STUCK OP EN. REMOVED AND REPLACED RIGHT HAND FORWARD PACK VALVE. REF 21-51-61 TESTED PRESSURE CONTROL REF 21-30-0, OPS CHECK OK . 2 L 7 3 4F A3WE 1998081400420 19980814 00420 NM 1998 8 14 K3HA980096 1 19980808 A 3350 106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 EMERGENCY CEILING LIGHT INOP. REMOVED AND REPLACED EMERGENCY CEILING LIGHT BATTERIES IAW 33-50-01. OPS CHECK GOOD 2 L 7 3 4F A3WE 1998081400421 19980814 00421 NM 1998 8 14 AWXA9800184 1 19980720 A 3350 849029 BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 322AW 25400 EMERGENCY ESCAPE PATH LIGHTING INOP, ROWS 1 TO 5. REMOVED AND REPLACED POWER SUPPLY, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1998081400422 19980814 00422 NM 1998 8 14 AWXA9800185 1 19980724 A 3350 20121 CHARGER BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 322AW 25400 EMERGENCY ESCAPE PATH LIGHTING INOP, ROWS 1 TO 5. REMOVED AND REPLACED BATTERY CHARGER ASSY. 2 L 7 2 4F RT A16WE 1998081400423 19980814 00423 NM 1998 8 14 AWXA9800186 1 19980730 A 3350 FUSE BOEING 737 7373G7 1384595 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 322AW 25400 EMERGENCY ESCAPE PATH LIGHTING INOP, ROWS 1 TO 5. REMOVED AND REPLACED FUSE ON BATTERY. 2 L 7 2 4F RT A16WE 1998081400424 19980814 00424 NM 1998 8 14 AWXA9800171 1 19980716 A 5210 LATCH BOEING 757 7572S7 1384962 NM PAX DOOR OUT OF ADJUST A AWXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 28 901AW 23321 LEFT AFT ENTRY DOOR HANDLE WOULD NOT STAY SECURE IN FLIGHT. DOOR POPPED OPEN ON TOUCHDOWN. NO EMERGENCY DECLARED BY FL IGHT CREW. AIR RETURN TO LAS WITHOUT INCIDENT. INSPECTED DOOR AND FOUND SOFT DOOR HANDLE. C/W ADJUSTMENT AND TEST IAW MM 52-11-00 501. ADJUSTED DOOR LATCH CAMS AND HANDLE MECHANISM. FUNCTION TEST GOOD. 2 L 7 2 4F RT A2NM 1998081400425 19980814 00425 NM 1998 8 14 AWXA9800187 1 19980805 A 3350 FUSE BOEING 737 73733A 1384673 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 169AW 23630 SEAT MOUNTED EMERGENCY EXIT LIGHTS INOP AT ROWS 19 THROUGH 23 LEFT. FOUND BLOWN FUSE ON BATTERY CHARGER. REPLACED FUSE , CORRECTED SHORTING CONDITION. OPS CK GOOD. 2 L 7 2 4F RT A16WE 1998081400426 19980814 00426 WP 1998 8 14 CALA9801416 1 19980807 A 2910 B NUT DOUG DC9 DC982 3022082 WP RT MLG BRAKE LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 14814 49112 THE RT HYDRAULIC SYSTEM FLUID QUANTITY DROPPED TO 1.5 QUARTS ON CLIMB-OUT OF DCA EN ROUTE TO EWR. THE RIGHT PUMP AND AU X PUMP WERE TURNED OFF. THE GEAR WAS MANUALLY EXTENDED AND THE AIRCRAFT LANDED AT EWR WITH GEAR DOORS OPEN. THE RIGHT GEAR DOOR SUSTAINED DAMAGE. THE RIGHT GEAR DOOR WAS REPLACED IAW MM 32-31-04. MAINTENANCE FOUND B NUT LOOSE ON HYDRAUL IC LINE TO RIGHT SYSTEM BRAKE ACCUMULATOR. THE B NUT WAS TIGHTENED AND LEAK CHECK WAS GOOD. THE RT HYDRAULIC SYSTEM WA S SERVICED TO FULL. GEAR DOOR OPERATION AND INDICATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998081400427 19980814 00427 NE 1998 8 14 CALA9801417 2 19980807 A 7510 ANTI-ICE DUCT BOEING 727 727224 1384076 NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE BLOWN A CALA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SW 09 69735 20664 674266 THE FIRE WARNING BELL SOUNDED FOLLOWED BY ILLUMINATION OF THE NR 3 ENGINE FIRE WARNING LIGHT ON CLIMB-OUT OF IAH AT ABOU T 900 FEET. THE NR 3 ENGINE POWER WAS REDUCED AND THE FIRE WARNINGS CEASED. A VALID FIRE TEST WAS RUN. THE LIGHT AND BELL CAME ON AGAIN WHEN ENGINE WAS RETURNED TO CLIMB POWER. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH FOR A NORMAL LANDING WITH NR 3 ENGINE AT REDUCED POWER. MAINTENANCE FOUND THE NR 3 ENGINE ANTI-ICE DUCT BLOWN. THE DUCT WAS REMOVED AND REPLACED. THE NR 3 ENGINE WAS RUN WITH NO LEAKS NOTED AND OPERATION CHECKED GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1998081400428 19980814 00428 NM 1998 8 14 CALA9801418 1 19980809 A 3230 189915 SENSOR BOEING 737 7373T0 1384582 NM LANDING GEAR INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 14342 23580 THE LANDING GEAR WOULD NOT RETRACT; THE LEVER WOULD NOT GO ABOVE THE OFF POSITION AFTER TAKEOFF FROM SFO. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE AIR SAFETY SENSOR AND PERFOR MED ADJUSTMENT AND TEST IAW MM 32-09-01. THE TELEFLEX CABLE WAS RIGGED. THE R276 AIR SENSE RELAY WAS ALSO REPLACED. T HE AIRCRAFT WAS JACKED AND A GEAR RETRACT ADJUSTMENT/TEST WAS PERFORMED IAW MM 32-32-00. THE GEAR WAS CYCLED FIVE TIMES AND GEAR HANDLE OPERATION WAS NORMAL. 2 L 7 2 4F RT A16WE 1998081400429 19980814 00429 NM 1998 8 14 CALA9801419 1 19980807 A 5320 SPLICE BOEING 727 727232 1384082 NM CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND BUTT SPLICE NR 2 IN FORWARD CARGO COMPARTMENT ON RT SIDE CORRODED. A NEW BUTT SPLICE WAS FABRICATED AN D INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998081400430 19980814 00430 NM 1998 8 14 CALA9801420 1 19980807 A 5320 SPLICE BOEING 727 727232 1384082 NM CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND BUTT SPLICE NR 3 IN FORWARD CARGO COMPARTMENT ON RT SIDE CORRODED. A NEW BUTT SPLICE WAS FABRICATED AN D INSTALLED IAW MM 51-20-1, 51-10-2, AND 51-20-12. 2 L 7 3 4F A3WE 1998081400431 19980814 00431 NM 1998 8 14 CALA9801421 1 19980808 A 5320 STRAP BOEING 727 727232 1384082 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND BUTT STRAP CORRODED IN AFT PIT AT STA 950A. A NEW STRAP WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, PAGE 7, 51-10-2, PAGE 4, AND MM 51-20-12, PAGE 710. 2 L 7 3 4F A3WE 1998081400432 19980814 00432 NM 1998 8 14 CALA9801422 1 19980808 A 5320 STRAP BOEING 727 727232 1384082 NM BS 555-630 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND BUTT STRAP IN FORWARD CARGO PIT CORRODED AT LT STA 555-630. A NEW BUTT STRAP WAS FABRICATED AND INSTAL LED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998081400433 19980814 00433 NM 1998 8 14 CALA9801423 1 19980708 A 5280 SKIN BOEING 727 727232 1384082 NM NLG DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A DENT IN AFT LOWER OUTBOARD SKIN OF NLG LT FORWARD DOOR. THE DOOR WAS REPAIRED IAW SRM 52-80-2 AND 51 -30-2. 2 L 7 3 4F A3WE 1998081400434 19980814 00434 NM 1998 8 14 CALA9801424 1 19980807 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .75 INCH CRACK IN RT WING INBOARD MIDFLAP LOWER CUTOUT FOR INBOARD ACTUATING ROD. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998081400435 19980814 00435 NM 1998 8 14 CALA9801425 1 19980807 A 5720 ANGLE BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .15625 CRACK IN SUPPORT ANGLE FOR LT WING TRAILING EDGE PANEL FORWARD OF OUTBOARD AILERON, OUTBOARD O F AILERON LOCKOUT. THE CRACKED AREA WAS ROUTED OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-40-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998081400436 19980814 00436 NM 1998 8 14 CALA9801426 1 19980807 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN LT INBOARD MIDFLAP LOWER TRAILING EDGE SKIN, 32 INCHES FROM INBOARD END. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-6 AND 51-10-1. 2 L 7 3 4F A3WE 1998081400437 19980814 00437 NM 1998 8 14 CALA9801427 1 19980807 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN LT INBOARD FLAP AFT SEGMENT LEADING EDGE SKIN, 64 INCHES FROM OUTBOARD END. THE CRA CKED AREA WAS REMOVED. A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND 51-10-6. 2 L 7 3 4F A3WE 1998081400438 19980814 00438 NM 1998 8 14 CALA9801428 1 19980807 A 5720 ANGLE BOEING 727 727224 1384076 NM WS 150 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN FORWARD ANGLE AT RT WING LEADING EDGE FLAP WELL LOWER STIFFENER, FS 150. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998081400439 19980814 00439 NM 1998 8 14 CALA9801429 1 19980807 A 5711 SPAR WEB BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .25 INCH CRACK IN SECOND FROM AFT VERTICAL WEB AT RT WING FRONT SPAR CHORD INBOARD AREA JUST FORWARD OF BOTTLE PIN. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2. 2 L 7 3 4F A3WE 1998081400440 19980814 00440 WP 1998 8 14 CALA9801430 1 19980807 A 5210 SKIN DOUG DC10 DC1030 3023501 WP L4 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 87070 48292 INSPECTION FOUND A SMALL CRACK WITH SOME PULLED RIVETS IN TOP EDGE OF DOOR L-4 SKIN. REPAIRED IAW ECRA 5210-01332. 2 L 7 3 4F A22WE 1998081400441 19980814 00441 WP 1998 8 14 CALA9801431 1 19980809 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 824 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND SEAT TRACK CORRODED AT STA 824, RBL 70. THE CORRODED AREA WAS TRIMMED AND BLENDED OUT. STRAP AND FILL ER WERE USED TO REINFORCE THE AREA IAW SRM 53-70-00, FIGURE 18. 2 L 7 3 4F A22WE 1998081400442 19980814 00442 WP 1998 8 14 CALA9801432 1 19980809 A 3213 AXLE SLEEVE DOUG DC10 DC1010 3022110 WP LT MLG BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND LT MLG NR 2 AXLE SLEEVE LOCK KEY BROKEN. THE NR 2 AXLE SLEEVE WAS REMOVED AND REPLACED IAW CMM 32-12-0 1. 2 L 7 3 4F A22WE 1998081400443 19980814 00443 NM 1998 8 14 CALA9801433 1 19980810 A 5530 STRINGER BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK AT ATTACH BOLT IN NR 7 STRINGER OF RT VERTICAL STABILIZER INNER COMPARTMENT AT NR 4 RIB . THE CRACKED SECTION WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-4. 2 L 7 3 4F A3WE 1998081400444 19980814 00444 NM 1998 8 14 CALA9801434 1 19980810 A 5230 BRACKET BOEING 727 727224 1384076 NM C2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 1 INCH CRACK AT LOWER AFT END OF AFT CARGO C-2 DOOR FRAME SIDE BRACKET. THE DOOR FRAME BRACKET WAS R EMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998081400445 19980814 00445 NM 1998 8 14 CALA9801435 1 19980810 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 380-420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND SEAT TRACK CORRODED AT BS 380-420, RBL 24. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS FABRICATED A ND INSTALLED IAW SRM 53-10-5 AND 51-10-5. 2 L 7 3 4F A3WE 1998081400446 19980814 00446 NM 1998 8 14 CALA9801436 1 19980810 A 5720 WEB BOEING 727 727224 1384076 NM WS 171.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN WEB PANEL NEXT TO BOOST PUMP INSIDE NR 2 FUEL TANK AT LT WS 171.50. THE WEB PANEL W AS REPAIRED IAW SRM 51-40-2, FIGURE 1. 2 L 7 3 4F A3WE 1998081400447 19980814 00447 NM 1998 8 14 CALA9801437 1 19980810 A 5311 CIRCUMFERENTIAL BOEING 727 727224 1384076 NM BS 219 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND CORROSION ON FORWARD AND AFT FACE OF CIRCUMFERENTIAL AT LOWER FORWARD NOSE COMPARTMENT, BS 219 BETWEEN STRINGER 24R AND 26R. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998081400448 19980814 00448 NM 1998 8 14 CALA9801438 1 19980811 A 5753 FITTING BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 0.6 CRACK IN FITTING AT RT INBOARD MIDFLAP RIB LEADING EDGE JUST OUTBOARD OF NR 5 CARRIAGE. THE FITT ING WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. FASTENERS WERE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998081400449 19980814 00449 NM 1998 8 14 CALA9801439 1 19980811 A 5320 STIFFENER BOEING 727 727224 1384076 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 0.3 INCH CRACK IN AFT CARGO COMPARTMENT STIFFENER AT STA 950A, LONGERON 30R. THE STIFFENER WAS REMOV ED AND REPLACED IAW SRM 51-30-2 AND 51-40-4. 2 L 7 3 4F A3WE 1998081400677 19980814 00677 WP 1998 8 14 HALA9800184 1 19980705 A 3350 POWER SUPPLY DOUG DC10 DC1010 3022110 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 153AA 46708 HNL - FLT 03 - LOG PAGE NR 4824872 - EMERGENCY LIGHT MID-POWER SUPPLY FAILED TEST. (X) 2 L 7 3 4F A22WE 1998081400678 19980814 00678 EU 1998 8 14 VTZA98215 1 19980609 A 3097 WIRE JETAIR JETSTM JETSTM4101 1500501 EU LEFT CHAFED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 311UE 41029 IAD/LVH - FLT 6310 - DURING CLIMB AT 2020 HOURS ON 6-9-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT ICE OBSERVATI ON CIRCUIT BREAKER TRIPPED. AIRCRAFT RETURNED TO GATE AT IAD WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPAI RED CHAFED WIRE. OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998081400679 19980814 00679 EU 1998 8 14 UF6A980519 1 19980527 A 3350 P4010021 BATTERY BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 ORD - DURING DAILY INSPECTION, THE FORWARD F/A EMERGENCY FLASHLIGHT WAS FOUND INOPERABLE. MAINTENANCE REMOVED AND REPLA CED POWER PACK. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1998081400680 19980814 00680 NE 1998 8 14 UF6A980518 2 19980527 A 7261 3006084 CAP BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE LOOSE A UF6A E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 GL 31 858AW 2035 124394 SBN - FLT 5751 - NR 2 ENGINE LOW OIL RPESSURE CWP ILLUMINATED DURING FLIGHT. ENGINE WAS SHUT DOWN PER EMERGENCY CHECKLI ST. MAINTENANCE PERFORMED INSPECTION OF NR 2 ENGINE AND FOUND OIL SERVICING CAP UNSECURED. CAP WAS SECURED AND ALL PAR AMETERS OPS CHECKED GOOD. (X) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998081400681 19980814 00681 EU 1998 8 14 UF6A980516 1 19980521 A 2710 JD270J0423000 PIN BAG ATP ATP EU AILERON FAILED A UF6A K NONE J WARNING INDICATION AP APPROACH 1 GL 31 857AW 2034 ORD - FLT 5708 - CSC CWP ILLUMINATED ON FINAL ALONG WITH AILERON SPLIT AND ENGAGED LIGHTS. MAINTENANCE REMOVED AND REPL ACED AILERON SHEAR PIN. SYSTEM OPS CHECKED GOOD. ACFT TT: 12,683 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400682 19980814 00682 EU 1998 8 14 UF6A980515 1 19980521 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - FLT 5762 - EMERGENCY LIGHT IN GALLEY INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 1998081400683 19980814 00683 EU 1998 8 14 UF6A980514 1 19980521 A 3350 L1R LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - FLT 5762 - EMERGENCY LIGHTING AT 12CD AND 14CD INOPERATIVE. MAINTENANCE SECURED LOOSE GROUND WIRE AT TERMINAL L1R . SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1998081400684 19980814 00684 EU 1998 8 14 UF6A980513 1 19980520 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 9683 349 16106 2021 SBN - LEFT HAND OVERWING EMERGENCY EXIT LIGHT INSIDE CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY. S YSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1998081400685 19980814 00685 EU 1998 8 14 98ZZZX2813 1 19980519 A 3350 58731 LIGHT BAG ATP ATP EU BS 234 LOOSE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 ORD - EMERGENCY FLOOR PROXIMITY LIGHTING COMING UP AT SEAT 1CD TO 5CD. MAINTENANCE RE-ATTACHED STRIPS. ACFT TT: 15,54 3 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400686 19980814 00686 EU 1998 8 14 98ZZZX2814 1 19980601 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FLT 5706 - FORWARD PASSENGER DOOR LOWER EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. ACFT TT: 12,617 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400687 19980814 00687 EU 1998 8 14 UF6A980602 1 19980602 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 SBN - FLT 5751 - RIGHT SIDE AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. ACFT TT: 1 2,292 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400688 19980814 00688 NE 1998 8 14 98ZZZX2815 2 19980604 A 7321 7919002002 EEC HAMSTD BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE FAILED A UF6A A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 GL 31 852AW 6102 90073615 2021 124403 ORD - FLT 5712 - DURING CLIMB AT FL 180, NR 1 ENGINE LOST 20 PERCENT TORQUE AND INCREASED 40 DEGREES ITT. MAINTENANCE R EMOVED AND REPLACED THE NR 1 EEC. SYSTEM OPS CHECKED GOOD. ACFT TT: 13,951 HOURS. ENGINE TT: 9,933. (X) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998081400689 19980814 00689 EU 1998 8 14 UF6A980604 1 19980608 A 3231 5D11580 ROD BAG ATP ATP EU NLG DOOR FAILED A UF6A A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 31 852AW 2021 AFTER TAKEOFF, VIBRATION FELT FROM NOSE GEAR AREA. MAINTENANCE REPLACED THE NOSE GEAR DOOR CONNECTING ROD. OPS CHECK G OOD. (X) 2 L 7 2 4T RT A27NM 1998081400690 19980814 00690 EU 1998 8 14 UF6A980608 1 19980616 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - RIGHT HAND OVERWING EXIT LAMP FILAMENT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. ACFT TT: 13,655 H OURS. (X) 2 L 7 2 4T RT A27NM 1998081400691 19980814 00691 EU 1998 8 14 UF6A980612 1 19980618 A 3350 6104781 BATTERY PACK GRIMES BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 ORD - UPON DAILY INSPECTION, FOUND LEFT HAND AFT EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 7 BATTER Y PACK. SYSTEM OPS CHECKED GOOD. ACFT TT: 13,668 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400692 19980814 00692 EU 1998 8 14 UF6A980607 1 19980615 A 5320 6017902 ANGLE BAG ATP ATP EU FUSELAGE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - CORROSION AND CRACKS FOUND ON AFT T-ANGLE. MAINTENANCE REPLACED AFT T-ANGLE. ACFT TT: 14,252 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400693 19980814 00693 EU 1998 8 14 UF6A980605 1 19980609 A 2421 BA03304 GENERATOR LUCAS BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 GL 31 852AW 7084 888 2026CA 2021 ORD - FLT 5711 - NR 1 GENERATOR FAILED ON TAKEOFF. MAINTENANCE REMOVED AND REPLACED THE NR 1 GENERATOR. OPS CHECK GOOD . ACFT TT: 13,971 HOURS. ENGINE TT: 9,953 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400694 19980814 00694 EU 1998 8 14 UF6A980606 1 19980615 A 5311 JD533J0187000 FRAME BAG ATP ATP EU BS 270 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 2022 SBN - CORROSION ON TOP SURFACE OF FRAME STATION 270 AS FROM OUTBOARD OF RIGHT HAND SEAL RAIL TO OUTBOARD OF LEFT HAND SE AT RAIL. ACFT TT: 14,252 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400695 19980814 00695 EU 1998 8 14 UF6A980610 1 19980616 A 3350 P4010021 BATTERY PACK BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECKED GOOD. A CFT TT: 13,063 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400696 19980814 00696 EU 1998 8 14 UF6A980611 1 19980619 A 5315 10D11498 FLOORBEAM BAG ATP ATP EU BS 378 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 853AW 14252 2022 SBN - FLOORBEAM AT FORMER BS 378 HAS CORROSION. MAINTENANCE CUT OUT SECTION OF CORROSION AND FABRICATED NEW ANGLE FROM 2024-T3 .183 INCH IAW ENGINNERING REPORT NR 98-080. ACFT TT: 14,252 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400697 19980814 00697 EU 1998 8 14 UF6A980616 1 19980629 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 10946 395 16997 2035 ORD - AFT EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY. OPS CHECKED GOOD. ACFT TT: 12,423 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400698 19980814 00698 EU 1998 8 14 UF6A980617 1 19980629 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 12032 564 16675 2020 SBN - NR 1 EMERGENCY POWER SUPPLY INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY. OPS CHECKED GOOD. ACFT TT: 12,770 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400699 19980814 00699 EU 1998 8 14 UF6A980613 1 19980620 A 5620 JD562J0013002W WINDOW BAG ATP ATP EU FUSELAGE DAMAGED A UF6A K NONE O OTHER CL CLIMB 1 GL 31 856AW 2032 ORD - FLT 5719 - ROW 3AB OUTER PASSENGER COMPARTMENT WINDOW HAS HOLE IN IT. MAINTENANCE REMOVED AND REPLACED OUTER WIND OW. SYSTEM OPS CHECKED GOOD. ACFT TT: 13,088 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400700 19980814 00700 EU 1998 8 14 UF6A980614 1 19980625 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 SBN - LEFT OUTER OVERWING EXIT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. ACFT TT: 12,404 HOU RS. (X) 2 L 7 2 4T RT A27NM 1998081400701 19980814 00701 EU 1998 8 14 UF6A980318 1 19980311 A 5753 86F10471 BEARING TORRINGTON BAG ATP ATP EU NR 2 TE FLAP WORN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 857AW 12349 2034 SBN - DURING B-CHECK INSPECTION, FOUND DAMAGE TO NR 2 FLAP, NR 2 OUTBOARD FLAP TRACK. MAINTENANCE INSPECTED AND FOUND N R 2 OUTBOARD FLAP TRACK LATERAL BEARING WORN. REMOVED AND REPLACED BEARING. SYSTEM OPS CHECKED GOOD. ACFT TT: 12,348 .8 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400702 19980814 00702 1998 8 14 UF6A980508 4 19980515 A 3140 EICAS BAG ATP ATP EU COCKPIT MALFUNCTIONED A UF6A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 857AW 2034 ORD - FLT 5751 - CWP AURAL WARNING ON TAKEOFF WITH NO VISUAL WARNING PRESENT. MAINTENANCE PERFORMED OPS CHECKS OF SYST EM AS WELL AS HIGH SPEED TAXI. NO DEFECTS NOTED. ACFT TT: 12,047 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400703 19980814 00703 EU 1998 8 14 UF6A980506 1 19980513 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - RIGHT HAND EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. ACFT TT: 13,48 4.6 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400704 19980814 00704 EU 1998 8 14 UF6A980507 1 19980514 A 3350 GE1317 BULB GE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - FLT 5751 - OVERHEAD EMERGENCY LIGHT IN GALLEY IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. ACFT TT: 1 3,484.6 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400705 19980814 00705 EU 1998 8 14 UF6A980511 1 19980518 A 3350 GE1317 BULB BAG ATP ATP EU COCKPIT FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 SBN - FLIGHT DCK EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. ACFT TT: 12,878 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400706 19980814 00706 1998 8 14 UF6A980510 4 19980518 A 3444 959960718501 TRANSPONDER BAG ATP ATP EU RADIO ALTIMETER FAILED A UF6A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 856AW 10971 1021 2032 SBN - FLT 5764 - EFIS CWP AND BLANK T.C.A.S. MAINTENANCE REMOVED AND REPLACED RAD ALT TRANSCEIVER. SYSTEM OPS CHECKED GOOD. ACFT TT: 12,8778 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400707 19980814 00707 EU 1998 8 14 UF6A980501 1 19980506 A 5330 JD539J0002263 SKIN BAG ATP ATP EU BS 408-418 DAMAGED A UF6A K NONE C F.O.D. NR NOT REPORTED 1 GL 31 859AW 12476 2036 SBN - FLT 5762 - AIRCRAFT HAD BIRD STRIKE ON RIGHT HAND SIDE OF NOSE DURING FLIGHT. MAINTENANCE INSPECTED AIRCRAFT. FO UND DAMAGE TO BE BETWEEN FORMER 408F TO 422F. DAMAGE WAS INSPECTED IAW TOR 001635 AND FOUND ACCEPTABLE FOR FLIGHT WITH A 25-CYCLE REINSPECTION REQUIRED AND 250 HOURS TERMINATION TIME. ACFT TT: 12,475.5 HOURS. (X) 2 L 7 2 4T RT A27NM 1998081400708 19980814 00708 NM 1998 8 14 EISA98158 1 19980628 A 5320 WEB BOEING 727 727223 1384074 NM BS 1183 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF CPCP WORK CARD, C3-224-08, FOUND CRACK INSIDE FS 1183 WALL AT LBL 50 EXTENDING FROM LIGHTENING HOLE IN WEB. REMOVED DAMAGED AREA IN WEB. FABRICATED REPAIR PER SRM 51-40-2 AND INSTALLED REPAIR PER SRM 57-30-02. TT : 72,562.53 HOURS. TC: 49,761. (X) 2 L 7 3 4F A3WE 1998081400709 19980814 00709 NM 1998 8 14 EISA98157 1 19980628 A 5542 SKIN BOEING 727 727223 1384074 NM RUDDER SPLIT A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LOWER RUDDER AT BOTTOM TRAILING EDGE SPLIT. REPAIRED TRAILING EDGE SPLIT PER SRM 51-40-6. TT: 72,562.53 HOURS. TC: 49.761. (X) 2 L 7 3 4F A3WE 1998081400710 19980814 00710 NM 1998 8 14 EISA98156 1 19980628 A 5542 SKIN BOEING 727 727223 1384074 NM RUDDER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LOWER RUDDER DELAMINATED AT TOP RIGHT HAND SIDE. REPAIRED HON EY-COMB WITH POTTED REPAIR PER SRM 51-40-6. FABRICATED SKIN DOUBLER AND INSTALLED PER SRM 55-40-8 AND INSTALLED FIBERGL ASS OVERLAY PER SRM 51-40-8. TT: 72,562.53 HOURS. TC: 49,761. (X) 2 L 7 3 4F A3WE 1998081400711 19980814 00711 NM 1998 8 14 EISA98155 1 19980628 A 5755 SKIN BOEING 727 727223 1384074 NM NR 8 SPOILER DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, RIGHT WING NR 8 SPOILER PANEL DELAMINATED. REPAIRED SPOILER PER SRM 51-40-6 AND SRM 51-10-8 FIBERGLASS OVERLAY. TT: 72562:53 HOURS. TC: 49,761. (X) 2 L 7 3 4F A3WE 1998081400712 19980814 00712 NM 1998 8 14 EISA98154 1 19980628 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 560 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CORROSION AROUND .25 INCH DIAMETER HOLE IN FLOOR STRUCTURE AT STR 29R FS 560, FWD CARGO PIT. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 53-10-2 AND SRM 53-10-1. TT: 72,562:53 HOURS. TC: 49,761. (X) 2 L 7 3 4F A3WE 1998081400713 19980814 00713 NM 1998 8 14 EISA98153 1 19980628 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 640 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON STR 29R AT FS 640, FORWARD CARGO PIT. REMOVED CO RROSION AREA, FABRICATED FILLER AND DOUBLER AND INSTALLED PER SRM 53-10-2 AND SRM 51-30-0. TT: 72,562:53 HOURS. TC: 4 9,761. (X) 2 L 7 3 4F A3WE 1998081400714 19980814 00714 NM 1998 8 14 EISA98152 1 19980628 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1464 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF CPCP WORK CARD C53-100-01, FOUND SKIN CRACKED AROUND FASTENER AT FS 1464 RIGHT HAND SIDE, FWD O F NR 2 ENGINE. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-10-2 AND SRM 53-30-3. TT: 72,562:53 HOURS. TC: 49, 761. (X) 2 L 7 3 4F A3WE 1998081400715 19980814 00715 NM 1998 8 14 EISA98151 1 19980628 A 5752 SKIN BOEING 727 727223 1384074 NM RT AILERON TAB DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND RIGHT WING OTBD AILERON CONTROL TAB DELAMINATED IN SEVERAL PLA CES. REMOVED SKIN OVER DAMAGED AREA, FABRICATED FILLERS AND INSTALLED WITH FIBERGLASS OVERLAY PER SRM 51-40-6 AND SRM 5 1-40-8. TT: 72,562:53 HOURS. TC: 49,761. (X) 2 L 7 3 4F A3WE 1998081400716 19980814 00716 EU 1998 8 14 C2XA98IA263 1 19980710 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLIGHT ATTENDANT'S SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLA CED THE SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400717 19980814 00717 EU 1998 8 14 C2XA98IA264 1 19980710 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLIGHT ATTENDANT'S SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17852.4 HOURS. TC: 2 0,381. (X) 2 H 7 2 4T RT A53EU 1998081400718 19980814 00718 EU 1998 8 14 C2XA98IA262 1 19980710 A 5320 S5367131120601 ANGLE AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FAIL SAFE ANGLE AT FRAME 37, STR 17, CORRODED. MAINTENANCE REMOVED AN D REPLACED THE FAIL SAFE ANGLE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400719 19980814 00719 EU 1998 8 14 C2XA98IA257 1 19980710 A 5315 S5367240720202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BEAM AT FRAME 38 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FL OOR BEAM IAW ATR 42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400720 19980814 00720 EU 1998 8 14 C2XA98IA258 1 19980710 A 5315 S53240820802 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BEAM AT FRAME 36 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FL OORBEAM IAW STR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,381. ( X) 2 H 7 2 4T RT A53EU 1998081400721 19980814 00721 EU 1998 8 14 C2XA98IA259 1 19980710 A 5315 S5367240720201 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND FLOOR SUPPORT BEAM AT FRAME 39 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FL OORBEAM IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,381. ( X) 2 H 7 2 4T RT A53EU 1998081400722 19980814 00722 EU 1998 8 14 C2XA98IA260 1 19980710 A 5320 S5367800821602 ZEE CHANNEL AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLOOR SUPPORT Z-CHANNEL CORRODED FROM FRAMES 39 TO 41. MAINTENANCE RE MOVED AND REPLACED THE Z-CHANNEL IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852. 4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400723 19980814 00723 EU 1998 8 14 C2XA98IA261 1 19980710 A 5320 S5367240600861 BEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FRAME 36 FLOOR SUPPORT I-BEAM CORRODED. MAINTENANCE REMOVED AND REPLA CED THE I-BEAM IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20 ,381. (X) 2 H 7 2 4T RT A53EU 1998081400724 19980814 00724 EU 1998 8 14 C2XA98BT049 1 19980708 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST CR CRUISE 1 SW 09 19812 99 EWR - FLIGHT CREW REPORTED 'LAST ROW OF EMERGENCY LIGHTS REMAIN ILLUMINATED IN-FLIGHT/BATTERY LOW NEEDS CHARGING'. MAIN TENANCE REMOVED AND REPLACED POWER SUPPLY MODULE AND OPERATIONALLY CHECKED SYSTEM GOOD. ACFT TT: 23,251.6 HOURS. ACFT CYCLES: 24,960. (X) 2 H 7 2 4T RT A53EU 1998081400725 19980814 00725 EU 1998 8 14 C2XA98IA251 1 19980710 A 5313 S5337140021402 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 15-16 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND STR 20 RIGHT BETWEEN FRAMES NR 15 AND NR 16 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE STRINGER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,85 2.4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400726 19980814 00726 EU 1998 8 14 C2XA98IA252 1 19980710 A 2750 S5751065500141 FITTING AEROSP ATR42 ATR42320 8680930 EU RT FLAP CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD FLAP, INBOARD AFT HINGE FITTING AT RIB NR 5, ATTACHMENT FASTENER HO LE ELONGATED. MAINTENANCE REPAIRED THE HINGE FITTING BY INSTALLING A REPAIR BUSHING IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5750-01-16. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS . TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400727 19980814 00727 EU 1998 8 14 C2XA98IA253 1 19980710 A 5320 S53337129320001 CHANNEL AEROSP ATR42 ATR42320 8680930 EU CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND FORWARD CARGO DOOR THRESHOLD DRAIN CHANNEL CORRODED. MAINTENANCE REMOVED AND REP LACED THE DRAIN CHANNEL IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400728 19980814 00728 EU 1998 8 14 C2XA98IA254 1 19980710 A 5320 S5337122622001 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND FORWARD DOOR THRESHOLD PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED THE THRE SHOLD PLATE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,852.4 HOURS. TC: 20,38 1. (X) 2 H 7 2 4T RT A53EU 1998081400729 19980814 00729 EU 1998 8 14 C2XA98IA255 1 19980710 A 5320 S53971402218 SPLICE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 11835 194 IAH - DURING C-CHECK INSPECTION, FOUND BELLY FAIRING SUPPORT FRAME NR 27 CORRODED AT CENTER WEB SPLICE. MAINTENANCE INS TALLED A REPAIR DOUBLER ON THE WEB SPLICE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT : 17,852.4 HOURS. TC: 20,381. (X) 2 H 7 2 4T RT A53EU 1998081400730 19980814 00730 NM 1998 8 14 AWXA9800188 1 19980806 A 2730 BACB10ET06 CAM BEARING BOEING 757 757225 1384959 NM ELEVATOR CONTROL LACK OF LUBE A AWXA O OTHER F FLT CONT AFFECTED LD LANDING 1 WP 28 913AW 22207 DURING FLAIR ON LANDING AND AT GATE, ELEVATOR MOVEMENT FOR ELEVATOR 'UP' (YOKE BACK) WAS VERY STIFF. BETTER WITH ONLY L EFT SYS POWERED. INSPECTED ELEVATOR CONTROL SYS FOR DAMAGE OBSTRUCTION AND BINDING OR JAMMING. INSPECTED CABLE RUNS, T ORQUE TUBES AND QUAD. NO OBVIOUS DAMAGE. PERFORMED ELEVATOR FEEL SYSTEM FORCES TEST BMM 27-31-00 EXCEPT STEP S725-140 (7) A-K DUE TO INABILITY TO CHECK BOTH PITOT SYS'S AT ONCE. FOUND FROZEN BEARING IN ELEVATOR FEEL AND CENTERING UNIT. I NSPECTED, LUBED AND FREED UP FROZEN BEARING. PERFORMED OPS CHECK OF ELEVATOR FEEL SYSTEM FORCES PER BMM 27-31-00 WITH E XCEPTION TO S725-140 A-K. SYSTEM OPS CHECK GOOD. R/R'D BEARING, PERFORMED FUNCTIONAL TEST PER BMM 27-31-17, PG 2, 14 2 L 7 2 4F RT A2NM 1998081400731 19980814 00731 NM 1998 8 14 CALA9801440 1 19980810 A 5320 PAN BOEING 727 727232 1384082 NM BS 740-760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND AFT EDGE OF PRESSURE PAN CRACKED APPROXIMATELY TWO INCHES AT FASTENER HOLE STA 740-760, LT SIDE. A REP AIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998081400732 19980814 00732 NM 1998 8 14 CALA9801441 1 19980810 A 5711 SPAR CHANNEL BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND U-CHANNEL AT REAR SPAR OF LT WING LOWER SURFACE JUST INBOARD OF SECOND OUTBOARD FLAP TRANSMISSION WORN AND CRACKED OUT OF NUT PLATE HOLE. THE CHANNEL WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIG URE 1 AND 51-30-2. 2 L 7 3 4F A3WE 1998081400733 19980814 00733 NM 1998 8 14 CALA9801442 1 19980810 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN AT STA 1183, WL 189, RBL 30. A DOUBLER AND TRIPLER WERE FABRICATED AND INSTALLED IAW BOEING 727 DRAWING NR 65C31446-3. 2 L 7 3 4F A3WE 1998081400734 19980814 00734 NM 1998 8 14 CALA9801443 1 19980811 A 5753 BRACKET BOEING 727 727232 1384082 NM NR 7 FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN RT WING INBOARD NR 7 FLAP TRACK TRAILING EDGE ATTACH BRACKET. THE ATTA CH BRACKET WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1998081400735 19980814 00735 NM 1998 8 14 CALA9801444 1 19980811 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 2 INCH CRACK IN RT INBOARD END OF FLOOR SUPPORT AT BS 760, BL 0. THE CRACKED SECTION OF FLOOR SUPPOR T WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 1998081400736 19980814 00736 NM 1998 8 14 CALA9801445 1 19980811 A 5512 PANEL BOEING 727 727224 1384076 NM LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND THREE CRACKS IN LT HORIZONTAL STABILIZER BALANCE PANEL NR 9116. THE CRACKS WERE STOP DRILLED IAW SRM 5 1-10-1. TWO EACH DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 55-20-3. 2 L 7 3 4F A3WE 1998081400737 19980814 00737 NM 1998 8 14 CALA9801446 1 19980811 A 5720 ANGLE BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A .5 INCH CRACK IN RT WING TRAILING EDGE UPPER ATTACH ANGLE ABOVE NR 6 GEARBOX FOR FLAP. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-10-6. 2 L 7 3 4F A3WE 1998081400738 19980814 00738 WP 1998 8 14 CALA9801447 1 19980812 A 5350 SLIDING BLOCKS DOUG DC9 DC982 3022082 WP TAILCONE INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 THE TAILCONE HUNG UP DURING RELEASE CHECK, HANDLE PULL WAS GOOD. BOTH UPPER SLIDING BLOCKS WERE REPLACED. A TAILCONE D ROP/FUNCTIONAL CHECK WAS PERFORMED IAW MM 53-53-01 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998081400739 19980814 00739 NE 1998 8 14 9809875534 2 19980809 A 7200 ENGINE BOEING 757 757251 1384970 NM PWA 2037 PW2037 NE NR 2 FAILED A NWAA E ENGINE SHUTDOWN X ENGINE FLAMEOUT AP APPROACH 1 GL 01 534US 24265 716473 DURING FINAL APPROACH AT 1000 FEET, NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL AND FLAMED OUT. AN UNEVENTFUL SINGLE ENG INE LANDING WAS PERFORMED. MAINTENANCE FOUND TRACE OF METAL IN THE TAILPIPE AND REPLACED THE ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998081400740 19980814 00740 WP 1998 8 14 9809889885 1 19980809 A 3260 0080004003 PROX SWITCH DOUG DC9 DC951 3022051 WP LANDING GEAR INOPERATIVE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 401EA 5503 1000 47682 AFTER TAKEOFF, ALL THREE LANDING GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE FLIGHT CREW RECYCLED THE LANDING GEAR WITH UNSAFE LIGHTS REMAINING ILLUMINATED. LANDING GEAR UNSAFE LIGHTS EXTINGUISHED DURING FLI GHT DESCENT. AIRCRAFT LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR PROXIMITY SWITCH ELECTRONI CS UNIT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998081400741 19980814 00741 WP 1998 8 14 9809899918 1 19980808 A 3610 CLAMP DOUG DC9 DC932 3022066 WP LT ACM DUCT BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 940N 47572 TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED T O MSP. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CLAMP BROKEN AT LEFT AIR CYCLE MACHINE INLET DUCT. REPLACE D CLAMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998081400742 19980814 00742 SO 1998 8 14 COMA9810172 1 19980810 A 3246 1014021 WHEEL 314461 EMB 120 EMB120RT SO MLG CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 2486 120225 DURING TEARDOWN VISUAL INSPECTION FOR TIRE CHANGE, THE INNER HALF OF THE MAIN WHEEL ASSY WAS FOUND TO HAVE A CRACK APPRO XIMATELY 2 INCHES IN LENGTH RUNNING INWARD IN THE WEB AREA, STARTING FROM UNDER THE BEARING CUP. THE WHEEL WAS REMOVED FROM SERVICE AT THIS TIME. 2 L 7 2 4T RT A31SO 1998081400743 19980814 00743 EA 1998 8 14 COMA9860216 1 19980801 A 5753 601R1430342 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 C-CHECK TASK 27-680-100. RIGHT INBOARD FLAP VANE HAS CHAFE DAMAGE. REPLACED FLAP VANE LEADING EDGE SKIN PANEL. 2 L 7 2 4F RT A21EA 1998081400744 19980814 00744 EA 1998 8 14 COMA9860215 1 19980801 A 2710 600908002 PULLY CNDAIR CL600 CL6002B19 EA RT AILERON FROZEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 DURING C-CHECK INSPECTION, FOUND RIGHT AILERON CABLE PULLY IS FROZEN. REPLACED PULLY. 2 L 7 2 4F RT A21EA 1998081400745 19980814 00745 EA 1998 8 14 COMA9860214 1 19980801 A 2710 272953 LINKS CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 C-CHECK TASK 002-27-690-100, RIGHT AILERON PCU LINKS ARE WORN AND CHAFED. REPLACED LINKS. 2 L 7 2 4F RT A21EA 1998081400746 19980814 00746 EA 1998 8 14 COMA9860213 1 19980802 A 2710 601R130002 BEARINGS CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 916CA 7014 DURING C-CHECK INSPECTION, FOUND RIGHT AILERON HAS WORN BEARINGS. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998081400747 19980814 00747 EU 1998 8 14 QXEA9801063 1 19980809 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 BOI - EXIT LIGHT ABOVE FORWARD GALLEY OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998081400748 19980814 00748 NM 1998 8 14 QXEA9801065 1 19980809 A 3350 1013079 BULB DHAV 82520977001 DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 816PH 54 PDX - EMERGENCY FLOOR PROXIMITY LIGHTING RED BULB INOP (4TH BULB FROM FORWARD). RELAMPED PROXIMITY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998081400749 19980814 00749 EU 1998 8 14 QXEA9801066 1 19980808 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 SEA - RIGHT AFT OVERWING EXIT HAS A BURNT OUT BULB. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998081400750 19980814 00750 EU 1998 8 14 QXEA9801067 1 19980809 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 SEA - BOTH OVERWING EXIT EVACUATION LIGHTS ON RIGHT HAND SIDE ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BA TTERY POWER SUPPLY AT ROW 8, OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998081400751 19980814 00751 EU 1998 8 14 QXEA9801068 1 19980807 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 GEG - EMERGENCY EXIT LIGHT OUT AT ROW 8 C,D,E. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998081400752 19980814 00752 EU 1998 8 14 QXEA9801069 1 19980808 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 GEG - EXIT LIGHT AT 9E OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998081400753 19980814 00753 EU 1998 8 14 QXEA9801070 1 19980808 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 GEG - EXIT LIGHT OVER COCKPIT DOOR IS OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998081400754 19980814 00754 EU 1998 8 14 QXEA9801071 1 19980807 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 BOI - AISLE EVACUATION LIGHT AT 4B OUT. MAINTENANCE REPAIRED A BROKEN WIRE, RESECURED BUNDLE, AND OPERATIONALLY TESTED, TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998081400755 19980814 00755 EU 1998 8 14 98FDEA00494 1 19980810 A 7722 500652101 THERMOCOUPLE AIRBUS 310 A310222 3930315 EU NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 420FE 339 98-195 - ON CLIMB-OUT THROUGH 140 NR 1 EGT FLUCTUATED PLUS/MINUS 20 DEG AT LEVEL OFF EGT CLIMB TO 1025 DEG MAX. CKLIST RAN NOTED ENG SHUTDOWN PROC EGT, THEN STAB BELOW MAX, THEN WENT TO ZERO RETURN TO BASE. WITH NR 1 ENG SHUTDOWN EGT IND NORM. PERFORM RESISTANCE AND MV TEST WHILE SHAKING EGT HARNESS, NO PROBLEM NOTED AND INSPECTED EGT HARNESS AND PROBES. VISUALLY CKS NORM. FOUND SEV LOOSE TERM AND NR 4 PROBE HAD 1/2 BROKEN STUD AND 2 LOOSE TERM. REMOVED AND REPLACED NR 1 ENG THERMOCOUPLE NR 4 PER M/M 77-21-04. RUN UP NR 1 ENG PER A310 JRH, ALL IND NORM. 2 L 7 2 4F RT A35EU 1998081400756 19980814 00756 NM 1998 8 14 98FDEA00495 1 19980811 A 3260 SWITCH BOEING 727 727233 138408A NM LANDING GEAR FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 218FE 21101 98-19 - GEAR WARNING HORN (STEADY) AFTER GEAR RETRACTION WITH FLAP AT 15 AND WENT OUT WITH GEAR DOWN. REMOVED AND REPLA CED AND ADJUST FLAP LAND WARN SWITCH PER M/M 31--26-12, WIR DIAG MANUAL 32-64-03. REMOVED AND REPLACED LAND GEAR ACC PE R M/M 32-09-121. TEST NORM. 2 L 7 3 4F RT A3WE 1998081400757 19980814 00757 NM 1998 8 14 98FDEA00496 1 19980811 A 2781 651781823 SWITCH BOEING 727 72727C 138400J NM NR 2 LE SLAT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 145FE 19109 98-0197 - NR 2 SLAT STILL IND OUT WHEN FLAP RETRACT TO ZERO POSITION TEST ALL AMBER LEADING EDGE SLATS ILLUM). AIRPLANE DID NOT HOWEVER ROLL LEFT. REQUIRES UNUSUAL CONTROL INPUTS TO KEEP WINGS LEVEL. FOUND NR 2 SLAT ACTUATOR POSITION SWI TCH TO BE BAD. REPLACED SWITCH PER M/M 27-81-32. OPS CHK GOOD. 2 L 7 3 4F A3WE 1998081400758 19980814 00758 1998 8 14 98FDEA00497 4 19980811 A 3418 COMPUTER BOEING 727 72722 1384002 NM E/E COMPT MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 190FE 19083 STICK SHAKER AFTER TAKEOFF DURING FIRST FLAP RETRACTION 165 KIAS. OCCURRED INTERMITTENTLY AT ALL ALTITUDES AND AIRSPEED S UNTIL LANDING, PITCH APPROX 8 DEG UP. *S/D* REMOVED AND REPLACED STALL WARN COMP AND ANGLE ATTACK SENSOR RIGHT, TEST OK. 2 L 7 3 4F A3WE 1998081400759 19980814 00759 NM 1998 8 14 98FDEA00498 1 19980811 A 3610 CLAMP BOEING 727 72722 1384002 NM NR 3 ENGINE LOOSE A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 195FE 19144 98-0199 - DURING CLIMB-OUT PASSING 10K FT, ENG 3 STRUT LGT ILLUM. RT PACK WAS TURNED OFF AND ENG 3 BLEED CLOSED. WHILE REFERENCING RED TABS, LGT EXT LGT TESTED OK. RED TABS COMPLETE. FOUND NR 3 ENG BLEED VLV IN 3 STRUT WITH LOOSE CLAMPS . AIR LEAK. RESECURED CLAMPS, RAN ENG, OPS CHK NORM. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998081400760 19980814 00760 NM 1998 8 14 98FDEA00499 1 19980811 A 3260 SOCKET BOEING 727 72725 1384006 NM NLG MALFUNCTIONED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 133FE 19851 98-200 - ON SHORT FINAL, NOSE GEAR MAIN GREEN LIGHTS BOTH WENT OUT. AFTER GO AROUND RECYCLED GEAR AND BOTH LIGHTS KEPT FLICKERING. BULBS TESTED GOOD. INSPECTED LIGHT SOCKET, FOUND THAT MOVEMENT ON LENS CAUSE LIGHT TO FLICKER THEN GO OUT. REMOVED AND REPLACED BULB AND CLEAN SOCKET. MOVEMENT OF LENS NO LONGER CAUSE FLICKER. NO OTHER DEFECT FOUND. 2 L 7 3 4F A3WE 1998081400761 19980814 00761 EU 1998 8 14 98FDEA00500 1 19980811 A 7722 636002581 INDICATOR AIRBUS 310 A310222 3930315 EU PWA 4152 PW4152 NE NR 1 ENGINE INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 420FE 339 98-201 - DURING CLIMB-OUT PASS 17000 MSL, NR 1 EGT PEG OUT HIGH FOR 5-10 SEC. ALL OTHER PARAMETERS NORM AND WITHIN RANG E. REDUCE PWR AND EGT CONT PLUS/MINUS 10 DEG OF NEEDLE TRAVEL. EGT INOP RETURN TO SIN. VISUAL CK EXHAUST DUCT. REAR OF FRONT COMPRESS DRIVE TURBINE FOR BURN DISTORT METAL PART. REMOVED AND REPLACED EGT IND C/OUT ENG RUN PER JRH. ALL P ARAMETER NML. 2 L 7 2 4F RT A35EU E24NE 1998081400762 19980814 00762 NM 1998 8 14 98FDEA00501 1 19980812 A 2910 BACH8A08NN0164 HYDRAULIC LINE BOEING 727 7272S2F 1384O81 NM B HYD SYST RUPTURED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 25 203FE 22925 98-202 - LOST 'B' SYS HYD QUANTITY AND PRESSURE ON TAKEOFF. INSPECTED AND FOUND NR 1 'B' PUMP PRESS LINE RUPTURED. REMO VED AND REPLACED LINE WITH NEW ALT LINE PER ENG AUTH 7-2914-38376. OPERATION AND LEAK CHK GOOD PER B-727 M/M 29-12-0. 2 L 7 3 4F A3WE 1998081400763 19980814 00763 NM 1998 8 14 98FDEA00502 1 19980811 A 2742 AJH7349505 JACK SCREW DOUG MD11 MD11F 3023600 NM HORIZ STAB WORN A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 612FE 48605 EXCESSIVE FREE PLAY IN HORIZ STAB RT JACK SCREW NUT. CHANGE RT HORIZ STAB JACK SCREW REF M/M 27-44-04-4 PERFORM ADJUST AND TEST PER MM 27-40-00-5. ALL BEAR AND BUSH CK WITHIN LIMIT PER DAC DRAWINGS ALC 8050 AND AJH 7135. 2 L 7 3 4F RT A22WE 1998081400764 19980814 00764 NM 1998 8 14 98FDEA00503 1 19980811 A 5210 507945238 BEAM BOEING 727 727227 1384078 NM PAX DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 FWD ENTRY DOOR LOWER GATE BEAM IS CRACKED ABOVE BOTTOM FWD STOP PIN FITTING. *S/D* REPAIRED FORWARD ENTRY DOOR LOWER G ATE BEAM IAW FED-EX DRAWING SR 27-52-015. 2 L 7 3 4F A3WE 1998081400765 19980814 00765 NM 1998 8 14 98FDEA00504 1 19980811 A 5311 6515931 FRAME BOEING 727 727227 1384078 NM BS 560 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CRACK IN FRAME BS 560, LBL 8, WL 155 FWD CARGO BAY. *S/D* REPAIRED CRACKED FRAME AT BS 560, LBL 8, WL 155 PER FEDEX SR M 51-40-3. ALODINED, PRIMED AND PAINTED PER FEDEX MM 51-20-151. 2 L 7 3 4F A3WE 1998081400766 19980814 00766 WP 1998 8 14 ABXA9800734 1 19980811 A 2910 61105360301 HYD HOSE DOUG DC8 DC861 3021952 WP RT MLG RUPTURED A ABXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 GL 23 843AX 46017 ON TAKEOFF FROM ILN, LOST ALL HYDRAULIC PRESSURE. UNABLE TO RAISE FLAPS. RETURNED TO ILN. REPLACED RIGHT BOGIE TRIM H YDRAULIC LINE. LEAK CHECKED GOOD IAW DC8 MM. 2 L 7 4 4F 4A25 1998081400767 19980814 00767 WP 1998 8 14 MWEA98859 1 19980810 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN BROKEN A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 215ME 47744 THE FORWARD ENTRANCE DOOR EMERGENCY LIGHT MOUNT PIN BROKE AND DOES NOT STAY SECURE. MAINTENANCE REMOVED AND REPLACED EM ERGENCY LIGHT ASSEMBLY. 2 L 7 2 4F A6WE 1998081400768 19980814 00768 WP 1998 8 14 MWEA98860 1 19980810 A 5320 39148671 FITTING DOUG DC9 DC932 3022066 WP BS 990 CORROSDED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND LONGERON 25L END FITTING AT STATION 990 WITH A BLOWN OUT HOLE AND CORROSION. MAINTENANCE FABRICATED AND INSTALLED NEW END FITTING. 2 L 7 2 4F A6WE 1998081400769 19980814 00769 WP 1998 8 14 MWEA98861 1 19980810 A 5330 59197073N SKIN DOUG DC9 DC932 3022066 WP BS 810-996 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 REMOVED AFT BELLY SKIN FROM FS 810-996 TO GET AT DAMAGE AND TO REPLACE BELLY SKIN. MAINTENANCE REMOVED AND REPLACED BEL LY SKIN AND FINGER DOUBLERS. 2 L 7 2 4F A6WE 1998081400770 19980814 00770 NM 1998 8 14 P5CA9801257 1 19980811 A 5751 SKIN BOEING 747 747132 1384882 NM LT AILERON PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 HOLE IN LOWER SURFACE OF LEFT INBOARD AILERON. CLEANED AREA, REMOVED DAMAGED MATERIAL, AND REPAIRED WITH FIBERGLASS OVE RLAYS IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998081400771 19980814 00771 NM 1998 8 14 P5CA9801258 1 19980811 A 5753 FAIRING BOEING 747 747132 1384882 NM NR 3 TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 3 FLAP CANOE TRAILING EDGE DAMAGED. REMOVED DAMAGED AREA AND APPLIED FIBERGLASS LAY UP OF 3 PLY SKINS IAW SRM 51-40- 15. 2 L 7 4 4F A20WE 1998081400772 19980814 00772 NM 1998 8 14 P5CA9801259 1 19980811 A 5311 FRAME BOEING 747 747132 1384882 NM BS 1780 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FRAME AT STA 1780 RIGHT SIDE HAS DEEP GOUGE CAUSED FROM GILL LINER SUBSTRUCTURE AT LONGERON 21R. BLENDED GOUGE AT FRAME IAW SRM 51-10-01. INSTALLED DOUBLER REPAIR IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998081400773 19980814 00773 NM 1998 8 14 P5CA9801260 1 19980811 A 5311 FRAME BOEING 747 747132 1384882 NM BS 2060 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 FRAME AT STA 2060 HAS SEVERAL GOUGES FROM GILL LINER SUBSTRUCTURE AT LONGERON 14R TO 21R. REPAIRED FRAME IAW SRM 51-10- 03. INSTALLED DOUBLER IAW SRM 51-30-02. 2 L 7 4 4F A20WE 1998081400774 19980814 00774 NM 1998 8 14 P5CA9801261 1 19980810 A 5753 SKIN BOEING 747 747132 1384882 NM RT TE MIDFLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT I/B MIDFLAP HAS DEEP GOUGE AT LEADING EDGE I/B CARRIAGE CUT OUT. REWORKED GOUGES IAW SRM 57-50-01. TREATED AND PRIM ED IAW SRM 51-10-02. 2 L 7 4 4F A20WE 1998081400775 19980814 00775 NM 1998 8 14 P5CA9801262 1 19980810 A 5330 SKIN BOEING 747 747132 1384882 NM FUSELAGE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEVEL 1 CORROSION, FOUND UNDER BOTH ATC ANTENNAS. REMOVED CORROSION IAW SRM 51-10-06. 2 L 7 4 4F A20WE 1998081400776 19980814 00776 NM 1998 8 14 P5CA9801263 1 19980810 A 5753 FITTING BOEING 747 747132 1384882 NM RT TE MIDFLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT I/B MIDFLAP AFT SUPPORT FITTING GOUGED. REMOVED AND REPLACED RT O/B MIDFLAP AFT SUPPORT FITTING IAW SB 747-27-2280. 2 L 7 4 4F A20WE 1998081400777 19980814 00777 NM 1998 8 14 P5CA9801264 1 19980810 A 5320 ANGLE BOEING 747 747132 1384882 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 L ANGLE BELOW SPLICE FITTING AT RIGHT BODY GEAR WHEEL WELL STA 1480 CRACKED. REMOVED AND REPLACED L ANGLE IAW SRM 51-10 -01 AND 51-30-02. 2 L 7 4 4F A20WE 1998081400778 19980814 00778 1998 8 14 P5CA9801265 4 19980809 A 3452 ANTENNA BOEING 747 747132 1384882 NM NR1 & NR2 ATC CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 1 AND NR 2 ATC ANTENNAS HAVE SURFACE CORROSION. REPLACED BOTH NR 1 AND NR 2 ATC ANTENNAS. OPS CHECKED GOOD IAW 3450 -01-01. 2 L 7 4 4F A20WE 1998081400779 19980814 00779 NM 1998 8 14 P5CA9801266 1 19980809 A 5753 SKIN BOEING 747 747132 1384882 NM LT TE MIDFLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT INBOARD MIDFLAP HAS HOLE IN UPPER SURFACE JUST AFT OF INBOARD CARRIAGE. REMOVED DAMAGED SKIN AND REPAIRED WITH FIB ERGLASS DOUBLERS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998081400780 19980814 00780 NM 1998 8 14 P5CA9801267 1 19980809 A 5753 FAIRING BOEING 747 747132 1384882 NM NR 2 TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 2 FLAP FAIRING CANOE HAS HOLE DAMAGE INSIDE. APPLIED FIBERGLASS OVERLAYS AND REPAIRED IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998081400781 19980814 00781 NM 1998 8 14 P5CA9801268 1 19980809 A 5753 SKIN BOEING 747 747132 1384882 NM NR 2 TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 2 LEFT AFT FLAP TRAILING EDGE DAMAGED. REPAIRED DAMAGE AT AFT T/E FLAP IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998081400782 19980814 00782 NM 1998 8 14 P5CA9801269 1 19980809 A 7110 COWLING BOEING 747 747132 1384882 NM NR 4 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 ENG INBOARD T/R TRAILING EDGE AT 8 O'CLOCK POSITION SKIN DAMAGED AND PEELING IN THREE AREAS. REPAIRED SKIN ROUTED SMALL CRACK AND REBONDED SKIN IAW 51-40-05. 2 L 7 4 4F A20WE 1998081400783 19980814 00783 NM 1998 8 14 P5CA9801270 1 19980809 A 5280 SKIN BOEING 747 747132 1384882 NM RT MLG DOOR DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RIGHT FLYING DOOR LOWER SECTION HAS SPOTS OF DELAMINATION ON ITS INNER SURFACE AT DENT LOCATION. SANDED AND REMOVED DAM AGED AREA AND REPAIRED IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998081400784 19980814 00784 NM 1998 8 14 P5CA9801271 1 19980809 A 5753 PIN BOEING 747 747132 1384882 NM RT TE FLAP CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RIGHT WING NR 7 SPINDLE AFT BOGIE O/B SUPPORT PIN CORRODED. REPLACED O/B SUPPORT PIN ON NR 7 SPINDLE AFT BOGIE IAW 747 OHM 27-51-75. 2 L 7 4 4F A20WE 1998081400785 19980814 00785 NM 1998 8 14 P5CA9801272 1 19980811 A 5313 LONGERON BOEING 747 747132 1384882 NM BS 2330 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 STA 2330 LONGERON 17R IS CRACKED. REMOVED CRACKED STRINGERS AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED ST RINGER AND SPLICE IAW SRM 53-30-02 FIG 4 AND 51-30-02. 2 L 7 4 4F A20WE 1998081400786 19980814 00786 NM 1998 8 14 P5CA9801273 1 19980811 A 5313 STRINGER BOEING 747 747132 1384882 NM BS 2330 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 STA 2330 LONGERON 14R IS CRACKED. REMOVED CRACKED STRINGER AND SPLICE. FABRICATED, TREATED, PRIMED AND REINSTALLED STR INGER AND SPLICE IAW SRM 53-10-03 FIG 4 AND 54-30-02. 2 L 7 4 4F A20WE 1998081400787 19980814 00787 NM 1998 8 14 P5CA9801274 1 19980812 A 5753 FRAME BOEING 747 747132 1384882 NM RT TE MIDFLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RT I/B MIDFLAP INBOARD MOST FRAME CRACKED. STOPPED DRILLED CRACK AND FABRICATED DOUBLER AND TREATED, PRIMED AND INSTALL ED IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1998081400788 19980814 00788 NM 1998 8 14 P5CA9801275 1 19980812 A 5313 LONGERON BOEING 747 747132 1384882 NM BS 1900 DAMAGE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 STA 1900 LONGERON 19R TO 26R FRAME HAS SERVERAL GOUGES ON I/B LIP. REPAIRED FRAME IAW SRM 51-40-03. 2 L 7 4 4F A20WE 1998081900001 19980819 00001 NM 1998 8 19 DL72S981558 1 19980724 A 5320 65561014 FRAME BOEING 727 727225 1384077 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8875Z 21293 FUSELAGE C1 DOOR CUTOUT AFT (STA 620) DOOR JAMB FRAME INNER CHORD S-25R, SPLICE REPAIR. THE INNER CHORD OF THE C1 DOOR CUTOUT AFT JAMB FRAME AT FS 620 WAS FOUND BADLY CORRODED BELOW S-25R. THE INNER CHORD WAS CUT NEAR S-25R AND A NEW LOWE R SECTION INSTALLED. THE NEW CHORD WAS SPLICED IN WITH TITANIUM REPAIR ANGLES AND STRAPS ON A TIME-LIMITED BASIS PER ER/A 365301-14, REV B. 2 L 7 3 4F A3WE 1998081900004 19980819 00004 WP 1998 8 19 VJ9800235 1 19980428 A 5320 1A32468 STRIP DOUGLAS DOUG DC9 DC932 3022066 WP BS 595 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 939VV 47089 FWD PIT AFT RT FS 595 LWR FLOOR PANEL/GILLINER MOUNT STRIP CORRODED BETWEEN 28R AND 23R AND LWR LEG AT LONG 30. FWD PIT AFT RT FS 595 LWR FLOOR PANEL GILL MOUNT STRIP, MECH. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABBED 1EA ANGLE H EAT TREATED, DRILLED, COUNTERSUNK, TRAETED AND PRIMED AND INSTALLED 7075-0-.050. TREATED, 7075-T6 IAW DC-9 SRM 51-11-2, 51-10-2, AND 51-30-2. 2 L 7 2 4F A6WE 1998081900005 19980819 00005 WP 1998 8 19 VJ9800236 1 19980721 A 2560 5168MA MEGAPHONE DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 918VV 47320 EMERGENCY MEGAPHONE DOES NOT WORK. REPLACED FWD MEGAPHONE. 2 L 7 2 4F A6WE 1998081900006 19980819 00006 WP 1998 8 19 VJ9800237 1 19980724 A 3350 AD4002P BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 967VV 47170 AFT OVERHEAD CABIN EMERGENCY LIGHTS INOP. REPLACED EMERGENCY POWER SUPPLY BATTERIES PER MM 33-50. OPS CHECK GOOD. 2 L 7 2 4F A6WE 1998081900007 19980819 00007 WP 1998 8 19 VJ9800249 1 19980718 A 5311 1A34936 FRAME DOUGLAS DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 AFT PIT FRAME SPLICE STA 938 28L IS CORRODED. CORROSION FOUND BEYOND SRM LIMITS, FABBED REPAIR REQUIRED. REMOVED FRAME SPLICE, FABBED REPAIR FRAME SPLICE OUT OF 7075-0.063 P NR 1A-34396-1. HEAT TREATED TO T-6. TREATED AND PRIMED REPAIR. INSTALLED REPAIR FROME SPLICE IAW DC-9 SRM 53-30-5, 51-10-2, 51-10-2A, 51-10-3, AND 51-30-5. 2 L 7 2 4F A6WE 1998081900008 19980819 00008 WP 1998 8 19 VJ9800250 1 19980718 A 5320 592405315 BRACKET DOUGLAS DOUG DC9 DC932 3022066 WP LAV DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 CORROSION DUST/PARTICLES EMANATING FROM UNDER I/B WASS OF FWD LAV, AFT OF DOOR CORROSION LEVEL 2. REPLACED CORRODED BRA CKET UNDER I/B WALL OF FWD LAV, AFT OF DOOR AND ASSEMBLED COMPONENTS IAW DC-9 MM 25-42-1. 2 L 7 2 4F A6WE 1998081900009 19980819 00009 WP 1998 8 19 VJ9800251 1 19980723 A 5330 1A35688 SKIN DOUGLAS DOUG DC9 DC932 3022066 WP BS 889-897 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 AFT CARGO COMPT FLOOR SUPPORT FRAME AND SKIN HAVE CORROSION FS 889-897 L30-L29R. CLEANED CORROSION FOUND TO BE OUT OF L IMITS IAW DC-9 SRM 53-04 CONDITION 3, 20 PERCENT TO 50 PERCENT. FABBED INTERNAL DOUBLER IAW DC-9 SRM 2024-T3.032 5.40X5 .50X.032. DRILLED AND DEBURRED IAW DC-9 RM 51-10-4. TREATED AND PRIMED IAW DC-9 51-10-3. INSTALLED DOUBLER NICA METHO D IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998081900010 19980819 00010 WP 1998 8 19 VJ9800252 1 19980721 A 5330 1A35100 SKIN DOUGLAS DOUG DC9 DC932 3022066 WP BS 935 28R CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 CORROSION ON INNER SKIN UNDER LONG 28R STA 935. REMOVED LONG 28R AND INNER SKIN FOUND CORROSION OUT OF LIMITS, FABBED N EW INNER SKIN 2024-T3.025. EXTERNAL SKIN CORROSION OUT OF LIMITS, FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INST ALLED LONG. 28R. 2 L 7 2 4F A6WE 1998081900011 19980819 00011 WP 1998 8 19 VJ9800253 1 19980721 A 5330 1A35100 SKIN DOUGLAS DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 CORROSION ON INNER SKIN STA 935 UNDER LONGERON 29R. REMOVED LONG 29R AND INNER SKIN FOUND CORROSION OUT OF LIMITS. FAB BED NEW INNER SKIN 2024-T3.025 EXTERNAL SKIN CORROSION OUT OF LIMITS FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND IN STALLED LONG 29R. 2 L 7 2 4F A6WE 1998081900012 19980819 00012 WP 1998 8 19 VJ9800254 1 19980719 A 5320 1A350661 INTERCOSTAL DOUGLAS DOUG DC9 DC932 3022066 WP BS 851-870 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 INTERCOSTAL STA 851-870 LONG 27L IS CORRODED AND BUBBLED ON LONGERON. REMOVED INTERCOSTAL AND FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED NEW INTERCOSTAL 18 1/8X5 USING 7075-0.050 IAW SRM 51-10-2 AND 53-11 FIG 3A. HEAT TRE ATED IAW DC-9 SRM 51-10-2A. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED INTERCOSTAL IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998081900013 19980819 00013 WP 1998 8 19 VJ0900247 1 19980718 A 5320 5924053015 BRACKET DOUG DC9 DC932 3022066 WP LAV DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 DURING C CHECK, FOUND DUST/PARTICLES EMANATING FROM UNDER I/B WAS OF FWD LAV AFT OF DOOR CORROSION LEVEL 2. REPLACED CO RROSION BRACKET UNDER I/B WALL OF FWD LAV, AFT DOR AND ASSEMBLED COMPONENTS IAW DC-9 MM 25-42-1. 2 L 7 2 4F A6WE 1998081900014 19980819 00014 WP 1998 8 19 VJ9800239 1 19980726 A 3260 SENSOR DOUG DC9 DC932 3022066 WP RT MLG DIRTY A ZZDA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 15 947VV 47555 RIGHT MLG RED UNSAFE LIGHT ALONG WITH DOOR WARNING LIGHT. AIRCRAFT AIR RETURNED. FOUND RT MLG UPLOCK SENSOR DIRTY AND PAINTED OVER. CLEANED SENSOR AND OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998081900015 19980819 00015 WP 1998 8 19 VJ9800240 1 19980727 A 3230 5224280105 BUNGEE CYLINDER DOUG DC9 DC932 3022066 WP RT MLG FAILED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 947VV 47555 MAIN LANDING GEAR RT UNSAFE LIGHT ON WITH DOOR WARNING LIGHT. AIRCRAFT AIR RETURNED. REMOVED AND REPLACED RT MLG BUNGE E CYLINDER GEAR SWING IAW 32-30-0. 2 L 7 2 4F A6WE 1998081900016 19980819 00016 WP 1998 8 19 VJ9800241 1 19980723 A 2120 DUCT DOUG DC9 DC932 3022066 WP RT PACK LOOSE A ZZDA O OTHER M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 15 935VV 47534 TAIL COMPARTMENT HI TEMP LIGHT ILLUMINATED IN FLIGHT CLIMB 18,000. FOLLOWED EMERGENCY PROCEDURES AND ISOLATED THE RIGHT SYSTEM. THE LIGHT EXTINGUISH. AIRCRAFT AIR RETURNED. FOUND LOOSE DUCT ON RT PACK SUPPLY, RE-SECURED DUCT IAW MM 21-0 0 AND 36-00. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998081900017 19980819 00017 WP 1998 8 19 VJ9800242 1 19980719 A 5320 1A350681 INTERCOASTAL DOUG DC9 DC932 3022066 WP BS 813-832 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 DURING C CHECK, FOUND INTERCOSTAL STA 813 - 832 27L HAS CORROSION. REMOVED INTERCOSTAL AND FOUND IT TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED NEW INTERCOASTAL 18.5 X 5 USING 7075-0-.040 IAW DC-9 SRM 51-10-3. HEAT TREATED IAW D C-9 SRM 51-10-2A. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED INTERCOASTAL IAW 51-30-2. 2 L 7 2 4F A6WE 1998081900018 19980819 00018 WP 1998 8 19 VJ9800243 1 19980721 A 5320 1A35686 SUPPORT DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 DURING C CHECK, FOUND AFT CABIN CENTER FLOOR BOARD SUPPORT HAS CORROSION ON TOP AT STA 965. REMOVED CORROSION 100 PERCE NT OF THE MATERIAL STA 965 BLO. REMOVED SECTION OUT OF LIMITS. FABBED REPAIR ANGLES 4 EA FROM 7075-T6 .032 2 EA 9.5 X 1X 1, 2 EA. 7.5 X 1 X 1 AND EXTRUSION 2652479, DRILLED, DEBURRED, COUNTERSUNK, TREATED, AND PRIMED IAW DC-9 SRM 53-01 FI G 2 PAG 4, 53-11-2, 51-10-4, 51-10-2, AND 51-10-3. INSTALLED EXTRUSION AND ANGLES IAW DC-9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998081900019 19980819 00019 WP 1998 8 19 VJ9800244 1 19980724 A 5320 1A35671 INTERCOASTAL DOUG DC9 DC932 3022066 WP BS 332 & 351 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 DURING C CHECK, FOUND INTERCOASTAL CORRODED BETWEEN STA 332 AND 351 LEVEL 2. REMOVED INTERCOASTAL FOUND TO BE OUT OF LI MITS. FABBED AND FORMED NEW INTERCOASTAL 19.5 X 1 X .5 X 27/8 FROM 7075 .050. HEAT TREATED TO 7075-T6 .050. TRIMMED T O FIT, DRILLED, DEBURRED, TREATED, AND PRIMED, IAW DC-9SRM 53-11-2, 51-10-2, 51-30-2, 51-30-3, AND 51-10-3. 2 L 7 2 4F A6WE 1998081900020 19980819 00020 WP 1998 8 19 VJ9800245 1 19980721 A 5320 1A356641 PAN DOUG DC9 DC932 3022066 WP GALLEY DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 DURING C CHECK, FOUND FWD GALLEY RT OUTBOARD PAN AT FWD INB CORNER OF R-1 DOOR FS 160 LONG 18 R B/L 55R HAS EXFOLIATED C ORROSION LEVEL 2. R-1 FWD ENTRY FLOOR PANEL, TRANSITION PLATE AND LOWER SIDE WALL CLOSEOUT PANEL STA 160- 20 RBL 40-TO 55 FOR ACCESS IAW DC-9 SRM 51-30-1, MM 25-50-1. FABRICATED NEW TRANSITION PANEL FROM 2024-T3 .025, 4' 10 X 3.25 X 2 IAW DC-9 SRM 51-10-2, 53-21 FIG 2D, LOCATED, TRIMMED, DRILLED, AND DIMPLED IAW DC-9 SRM 51-10-4 TREATED, PRIMED, AND INSTAL LED. 2 L 7 2 4F A6WE 1998081900021 19980819 00021 WP 1998 8 19 VJ9800246 1 19980712 A 5320 1A350781 SUPPORT DOUG DC9 DC932 3022066 WP BS 408-427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 LEFT LOWER LINER GILLINER SUPPORT IS CORRODED BETWEEN STA 408-427. REMOVED CORROSION, OUT OF LIMITS, DEPTH GAUGE A-2024 , IAW DC-9 SRM 51-10-3, 53-01 FIG 1 (.045 MATERIAL LOSS). FABBED NEW SECTION 7075-0-.063 (1A-35078), HEAT TREATED TO T 6 IAW DC-9 SRM 53-21-0 FIG 2A, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW SECTION IAW DC-9 SRM 51-10-4, 51-30- 2, 51-10-3. 2 L 7 2 4F A6WE 1998081900022 19980819 00022 WP 1998 8 19 VJ9800248 1 19980722 A 5320 1A34922 SPLICE DOUG DC9 DC932 3022066 WP BS 937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 AFT PIT FRAME SLICE STA 937 28L IS CORRODED. REMOVED CORROSION MATERIAL LOSS WAS 90 PERCENT AND BEYOND LIMITS. REMOVED FLOOR SUPPORT AND SPLICE CAP. CUT FRAME, FABBED REPAIR OUT OF 7075-0 .050 AND 2 EA SPLICES OUT OF 7075-0.071 AND 0.050 . FABBED REPAIR DOUBLER OUT OF 7075-T-6 .050 DRILLED, DEBURRED, TREATED, AND PRIMED. INSTALLED REPAIR PART AT STA 932 28L IAW DC-9 51-30-2, 51-10-3, 53-03 PAG 4, 51-10-4. 2 L 7 2 4F A6WE 1998081900023 19980819 00023 WP 1998 8 19 98FDEA00478 1 19980722 A 5711 SPAR DOUG DC10 DC1010 3022110 WP LT WING CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 388FE 46622 STA-GYR: WHILE WORKING EO 8-5710-7-3314 PARTS 5,6,7, AND 8 FOUND LEFT NR 2 AND RT NR 4 HOLES IN PYLON FITTINGS AND WING SPAR CORRODED. CORROSION WAS REMOVED AND HOLES ARE WITHIN BLUEPRINT TOLERANCE. 2 L 7 3 4F A22WE 1998081900024 19980819 00024 NM 1998 8 19 P5CA9801209 1 19980731 A 7110 PANEL GUIDE BOEING 747 747249F 1384849 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 CRACKED NR 4 ENGINE PANEL GUIDE AT 11:30 POSITION AT FAN EXIT. FABRICATED NEW PANEL GUIDE PER BOEING SRM 51-40-00. 2 L 7 4 4F A20WE 1998081900025 19980819 00025 NM 1998 8 19 P5CA9801210 1 19980731 A 7110 COWL BOEING 747 747249F 1384849 NM NR 1 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 DAMAGED AND BENT LOWER CORNER ON NR 1 ENGINE FAN COWL. REMOVED DAMAGED AREA FABRICATED NEW FILLER AND DOUBLER PER BOEIN G SRM 51-40-05 2 L 7 4 4F A20WE 1998081900026 19980819 00026 NM 1998 8 19 P5CA9801211 1 19980730 A 7810 EXHAUST SLEEVE BOEING 747 747249F 1384849 NM NR 4 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 CRACKED NR 4 ENGINE EXHAUST SLEEVE AT 1:00 AND 6: POSITIONS. REPAIRED CRACK PER BOEING SRM 54-30-3. 2 L 7 4 4F A20WE 1998081900027 19980819 00027 NM 1998 8 19 P5CA9801212 1 19980730 A 5753 SKIN BOEING 747 747249F 1384849 NM LT TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 CRACKED AND DAMAGED AREA ON INBOARD EDGE NR 9 VARIABLE CAMBER FLAP. BLENDED DAMAGED AREA AND FOUND WITHIN LIMITS PER BO EING SRM 57-50-01. 2 L 7 4 4F A20WE 1998081900028 19980819 00028 NM 1998 8 19 P5CA9801213 1 19980728 A 5753 SKIN BOEING 747 747249F 1384849 NM RT TE FLAP CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 CRACKED AND BENT AREA ON INBOARD EDGE NR 17 VARIABLE CAMBER FLAP. BLENDED DAMAGED AREA AND FOUND WITHIN LIMITS PER BOEI NG SRM 57-50-01. 2 L 7 4 4F A20WE 1998081900029 19980819 00029 NM 1998 8 19 P5CA9801214 1 19980731 A 7110 COWL BOEING 747 747249F 1384849 NM NR 2 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 DENTED AND DELAMINATION NR 2 ENGINE INBOARD FAN COWL EXTERNAL SKIN AT LOWER CENTER. REPAIRED PER BOEING SRM 51-40-06. 2 L 7 4 4F A20WE 1998081900030 19980819 00030 WP 1998 8 19 VJ9800255 1 19980731 A 2560 5928730503 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR DETACHED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 915VV 47443 L1 DOOR EMERGENCY SLIDE PACK FELL OF DOOR. REINSTALLED SLIDE AND COVER PER MM. 2 L 7 2 4F A6WE 1998081900031 19980819 00031 WP 1998 8 19 VJ9800256 1 19980731 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR DETACHED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 966VV 47168 R1 DOOR EMERGENCY SLIDE FELL OFF DOOR. SLIDE LANYARD DISCONNECTED. REINSTALLED R1 DOOR SLIDE IAW MM 25-60. 2 L 7 2 4F A6WE 1998081900032 19980819 00032 WP 1998 8 19 VJ9800257 1 19980731 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 914VV 47486 R1 DOOR EMERGENCY SLIDE APPEARS LOOSE. RESECURED R1 DOOR SLIDE PER MM 25-60. 2 L 7 2 4F A6WE 1998081900033 19980819 00033 WP 1998 8 19 VJ9800258 1 19980801 A 3350 110049 BATTERY CHARGER DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 919VV 47260 ROW 24 AND AFT EPL LIGHTING INOP. REMOVED AND REPLACED AFT OVERHEAD BATTERY PACK CHARGER IAW MM 25-60. 2 L 7 2 4F A6WE 1998081900034 19980819 00034 NM 1998 8 19 DLM90981581 1 19980729 A 2730 CABLES DOUG MD90 MD9030 3023690 NM ELEVATOR CONTROL LOCKED UP A A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 913DN 53393 ON FINAL IN LANDING CONFIGURATION CONTROL COLUMN LOCKED APPROX 6 INCHES FWD OF NEUTRAL AIRSPEED 145 TO 150 KNOTS COLUMN WAS FORCEFULLY PUSHED FORWARD. RELEASE OCCURRED, BUT LOCKED ON A SECOND TRY COULD NOT DUPLICATE ON THE GROUND. REMARKS - AS OF 2130E/30 ITEM IS STILL IN WORK CABLES BEING RIGGED,T.E COLUMN OVERRIDE MECHANISM HAS BEEN RESET. 2 L 7 2 4F RT A6WE 1998081900035 19980819 00035 NM 1998 8 19 DL72L981583 1 19980730 A 5320 WEB BOEING 727 727232 1384082 NM BS 1225 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 FOUND ON F1 LETTER CK, CRACK IN VERTICAL WEB STA 1225 FROM FASTENER HOLE. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998081900036 19980819 00036 WP 1998 8 19 MWEA98639 1 19980603 A 5250 39178531 CHANNEL DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 MKE - FOUND CRACK ON VENTRAL DOOR LOWER LEFT DOOR FRAME CHANNEL. MAINTENANCE FABRICATED AND INSTALLED NEW DOOR CHANNEL. (M) 2 L 7 2 4F A6WE 1998081900037 19980819 00037 WP 1998 8 19 MWEA98640 1 19980603 A 2560 591769037 COVER DOUG DC9 DC932 3022066 WP GALLEY DR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 204ME 47680 MKE - FLT 584 - THE GALLEY DOOR SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY SLIDE COVER. (M) 2 L 7 2 4F A6WE 1998081900038 19980819 00038 WP 1998 8 19 VJ9800260 1 19980525 A 5313 27779485 LONGERON DOUG DC9 DC932 3022066 WP BS 231-246 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 CORROSION IN FORWARD PIT AT FS 231, L29R BEYOND LIMITS. REMOVED CORROSION, RT LONGERON 29, FS 231 TO 246. DRILLED NEW SECTION OF LONGERON AND LONGERON SPLICES IAW DC9 SRM 53-02, FIG 18. DEBURRED, TREATED AND INSTALLED LONGERON AND SPLICE S AND SHIMS IAW DC9 SRM 53-02, FIG 18. 2 L 7 2 4F A6WE 1998081900046 19980819 00046 EU 1998 8 19 98ZZZX2741 1 19980105 A 5320 RIVET BAG BAE146 BAE146200A 1500266 EU FRAME 14 MISSING A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 156TR E2156 ATW - FORWARD VESTIBULE RT SIDE AT FR 14 AND INTERCOSTAL. THREE MISSING RIVETS FROM PRODUCTION WITH CLECO STILL INSTALL ED. INSTALLED 3 RIVETS. 2 H 7 4 4F RT A49EU 1998081900047 19980819 00047 NM 1998 8 19 P5CA9801216 1 19980803 A 5730 PANEL BOEING 747 747249F 1384849 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 RIGHT WING UPPER SURFACE OF FLYING PANEL HAS A 2X2 AREA OF DELAMINATION AT TITANIUM COFFIN DOUBLER. REMOVED AND REPLACE D RIGHT HAND WING FLYING PANEL IAW SRM 57-22-89, 51-30-02 AND POLAR MA A5730-02:01. 2 L 7 4 4F A20WE 1998081900048 19980819 00048 NM 1998 8 19 P5CA9801217 1 19980801 A 5330 SKIN BOEING 747 747249F 1384849 NM FUSELAGE CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 LEVEL 1 CORROSION UNDER THE ATC ANTENNAS. REMOVED CORROSION FROM UNDER A/C ATC ANTENNAS WITH MINIMAL MATERIAL LOSS IAW SRM 51-10-01. 2 L 7 4 4F A20WE 1998081900049 19980819 00049 NM 1998 8 19 P5CA9801218 1 19980731 A 7810 EXHAUST SLEEVE BOEING 747 747249F 1384849 NM NR 4 ENGINE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 NR 4 ENGINE EXHAUST SLEEVE INNER SKIN DELAMINATED AT 6 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENG EXHAUST SLEEVE A SSY IAW MM 78-11-02. 2 L 7 4 4F A20WE 1998081900050 19980819 00050 NM 1998 8 19 P5CA9801219 1 19980802 A 5321 FLOOR BOEING 747 747249F 1384849 NM UPPER DECK DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 LEVEL 1 CORROSION ON FLOOR PANEL UNDER LT UPPER DECK SLIDE CARRIAGE DELAMINATED AND MINOR CORROSION. FOUND MINOR SURFAC E CORROSION, REMOVED IAW SRM 51-10-06 AND REPAIRED DELAMINATION IAW SRM 51-40-05. 2 L 7 4 4F A20WE 1998081900051 19980819 00051 1998 8 19 P5CA9801220 4 19980731 A 3452 ANTENNA BOEING 747 747249F 1384849 NM FUSELAGE CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 LEVEL 1 CORROSION ON THE NR 1 AND NR 2 ANTENNA BODY. REPLACED NR 1 AND NR 2 ATC ANTENNAS IAW MM 34-53-03. 2 L 7 4 4F A20WE 1998081900052 19980819 00052 NM 1998 8 19 P5CA9801221 1 19980803 A 5280 PANEL BOEING 747 747249F 1384849 NM RT MLG DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 RIGHT WING GEAR FLYING DOOR PANEL CRACKED. REPAIRED PANEL IAW 747 SRM 51-40-09. 2 L 7 4 4F A20WE 1998081900053 19980819 00053 NM 1998 8 19 P5CA9801223 1 19980801 A 5320 SUPPORT BOEING 747 747249F 1384849 NM BS 860 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 FWD LOWER CARGO COMPARTMENT STA 860 CENTER GUIDE FLOOR SUPPORT DAMAGED. REMOVED DAMAGED FLOOR SUPPORT AND WEB REINSTALL ED PERMANENT REPAIR IAW SRM 51-40-02. 2 L 7 4 4F A20WE 1998082100001 19980821 00001 EU 1998 8 21 VTZA98207 3 19980531 A 6112 10364160116 DEICE JETAIR JETSTM JETSTM4101 1500501 EU LT PROP ASSY FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 327UE 41080 FLT 6267 - IAD-BTV - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT PROP DEICE FAILED IN ICING CONDITIO N. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT PROP ASSY. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998082100002 19980821 00002 WP 1998 8 21 TWAA9810718 1 19980624 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND CLASS 3 REPAIR INSTALLED AT AFT END OF REAR CARGO DOOR CUT-OUT. INSTALLED C LASS 1 REPAIR PER SRM 53-05, FIG 80. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X) 2 L 7 2 4F A6WE 1998082100003 19980821 00003 1998 8 21 USAAF98060 4 19980601 A 2565 60049101 SLIDE FOKKER F28 F28MK0100 4990807 EU ENTRY DOOR RUPTURED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 854US 11282 PIT - DURING AN ANNUAL ESCAPE SLIDE OPERATION CHECK SAMPLING PROGRAM, THE FORWARD ENTRY DOOR SLIDE FAILED TO HOLD INFLAT ION PRESSURE DUE TO TWO HOLES IN THE SLIDE. THE SLIDE DEPLOYED NORMALLY AND ALL SLIDE LIGHTS ILLUMINATED. IT COULD NOT BE DETERMINED IF THE HOLES WERE CAUSED DURING THE DEPLOYMENT OR IF THEY EXISTED PRIOR TO DEPLOYMENT. THE SLIDE WAS ROU TED TO THE REPAIR SHOP. (X) 2 L 7 2 4F RT 1998082100004 19980821 00004 NM 1998 8 21 USAASB98187 1 19980718 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 393US 23315 ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY/EVACUATION LIGHTS INOPERATIVE. BULLNOSE EVACUATION LIGHT AT SEAT ROW 1, ESCAPE SLIDE LIGHT FOR FORWARD PASSENGER DOOR, EXIT SIGN OVER FORWARD SERVICE DOOR AND COCKPIT EVACUATION LIGHT. MAINT ENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998082100005 19980821 00005 1998 8 21 USAAF98061 4 19980719 A 2565 60049101 SLIDE FOKKER F28 F28MK0100 4990807 EU ENTRY DOOR MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 869US 11314 PIT - DURING AN ANNUAL ESCAPE SLIDE OPERATIONAL CHECK SAMPLING PROGRAM, THE FORWARD ENTRY DOOR ESCAPE SLIDE DID NOT FULL Y INFLATE. ACCORDING TO THE INSPECTOR THAT WITNESSED THE DEPLOYMENT, THE SLIDE INITIALLY WAS HUNG UP IN THE DOORWAY. W HEN THE MANUAL HANDLE WAS PULLED, THE SLIDE DEPLOYED VERTICALLY, BUT DID NOT APPEAR TO FULLY INFLATE. HOWEVER, THE SLID E DID HOLD ITS PRESSURE. THE SLIDE WAS ROUTED TO THE REPAIR SHOP. (X) 2 L 7 2 4F RT 1998082100006 19980821 00006 1998 8 21 UF6A980609 3 19980615 A 6140 3039242 SENSOR BAG ATP ATP EU NR 2 ENG NR 1 FAILED A UF6A K NONE O OTHER CR CRUISE 1 GL 31 858AW 11874 CH8898 2035 IN CRUISE AT 14,000 FEET, NR 1 NH INDICATED 107 PERCENT. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 PULSE PROBE PIC K-UPS. TEST FLIGHT WAS SATISFACTORY. REF: OPERATOR CNTRL NR 98ZZZX2827. (X) 2 L 7 2 4T RT A27NM 1998082100007 19980821 00007 1998 8 21 98ZZZX2827 3 19980615 A 6140 3039242 SENSOR BAG ATP ATP EU NR 2 ENG NR 2 FAILED A UF6A K NONE O OTHER CR CRUISE 1 GL 31 858AW 11874 CH8909 2035 IN CRUISE AT 14,000 FEET, NR 1 NH INDICATED 107 PERCENT. MAINTENANCE REMOVED AND REPLACED NR 1 AND NR 2 PULSE PROBE PIC K-UPS. TEST FLIGHT WAS SATISFACTORY. REF: OPERATOR CNTRL NR UF6A980609. 2 L 7 2 4T RT A27NM 1998082100008 19980821 00008 WP 1998 8 21 TWAA9811506 1 19980716 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINTENANCE CHECK AT STA 965, THE BULKHEAD WEB HAD 2 EACH CRACKS APPROX 2 INCHES LONG AT WL 200, JUST INBD OF LONGERON 18R. REPLACED FULL BULKHEAD WEB WITH SAME AS ORIGINAL .032 INCH 7075T6 ALUMINUM MATERIAL. ATTACHED WITH MS L0470AD RIVETS AND HLT HI LOKS, ALL FASTENERS AND PARTS INSTALLED WITH FAYING SURFACE SEALANT. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100009 19980821 00009 WP 1998 8 21 TWAA9811505 1 19980713 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DUIRNG OP 16 MAINTENANCE CHECK, FOUND LONGERON 17R AT STA 980 WITH .50 INCH CRACK AT ATTACH HOLE TO FORMER. REPLACED SE CTION OF LONGERON FROM STA 956 TO STA 996. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 18. CFT TT: 77,783 H OURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100010 19980821 00010 WP 1998 8 21 TWAA9811503 1 19980709 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 914 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR ANGLE WITH EXFOLIATION AT FS 914, S29R. REMOVED EXFOLIATED SECTION OF ANGLE AND REPAIRED AREA PER SRM 53-01, FIG 2 SHEET 4. AFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100011 19980821 00011 WP 1998 8 21 TWAA9811502 1 19980714 A 5210 SKIN DOUG DC9 DC982 3022082 WP PASSENER DOOR BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 902TW 49153 DURING OVERNIGHT MAINTENANCE, FOUND THE L-1 CABIN DOOR LOWER FORWARD CORNER OF DOOR SKIN BENT INWARD 9 INCHES. AREA CUT OUT, FILLER AND DOUBLER INSTALLED PER SRM 52-05, FIG 32. CHECK-C 2-1-98 STL. ACFT TT: 48,075 HOURS. ACFT TC: 24,89 6. (X) 2 L 7 2 4F A6WE 1998082100012 19980821 00012 WP 1998 8 21 TWAA9811402 1 19980715 A 5240 49157461 ROD DOUG DC9 DC982 3022082 WP R-1 DOOR BROKEN A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 913TW 49184 A CATERER REPORTED BEING UNABLE TO OPEN THE R-1 CABIN DOOR. FOUND A BROKEN CONTROL ROD FOR THE DOOR LOWER GATE. REPLAC ED ROD. CHECK-C 12-30-97 MCI. ACFT TT: 45,209 HOURS. ACFT TC: 23,365. (X) 2 L 7 2 4F A6WE 1998082100013 19980821 00013 WP 1998 8 21 TWAA9811401 1 19980715 A 2910 LINE DOUG DC9 DC983 3022083 WP HYDRAULIC SYSTEM CHAFED A TWAA A UNSCHED LANDING K H J FLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 05 9307R 49663 THE LT GENERATOR TRIPPED OFF AND THERE WAS A LOSS OF LT HYDRAULIC SYSTEM FLUID. FLT 249 MADE AN UNSCHEDULED LANDING AT MCI. FOUND GENERATOR FEEDER CABLE RUBBED AN ELEVATOR RETURN HYDRAULIC LINE IN THE TAIL COMPARTMENT CAUSING FAILURE OF B OTH SYSTEMS. REPLACED HYDRAULIC LINE AND SPLICED SECTION OF THE GENERATOR FEEDER CABLE. CHECK-C 11-29-97 MCI. REF: O PERATOR CONTROL NR 98ZZZX2828. (X) 2 L 7 2 4F RT A6WE 1998082100014 19980821 00014 WP 1998 8 21 98ZZZX2828 1 19980715 A 2420 WIRE DOUG DC9 DC983 3022083 WP GENERATOR WORN A TWAA A UNSCHED LANDING K H J FLUID LOSS ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 05 9307R 49663 THE LT GENERATOR TRIPPED OFF AND THERE WAS A LOSS OF LT HYDRAULIC SYSTEM FLUID. FLT 249 MADE AN UNSCHEDULED LANDING AT MCI. FOUND GENERATOR FEEDER CABLE RUBBED AN ELEVATOR RETURN HYDRAULIC LINE IN THE TAIL COMPARTMENT CAUSING FAILURE OF B OTH SYSTEMS. REPLACED HYDRAULIC LINE AND SPLICED SECTION OF THE GENERATOR FEEDER CABLE. CHECK-C 11-29-97 MCI. REF: O PERATOR CONTROL NR TWAA9811401. 2 L 7 2 4F RT A6WE 1998082100015 19980821 00015 NM 1998 8 21 TWAA9811301 1 19980625 A 5330 SKIN BOEING 767 767231 1385131 NM FUSELAGE GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 601TW 22564 DURING CHECK-C, MAINTENANCE FOUND FUSELAGE SKIN GOUGE 3 FEET BELOW AFT EDGE OF THE R-1 CABIN DOOR. INSTALLED DOUBLER WI TH HI-LOCKS (WEST) 8.50 INCHES BY 10 INCHES EXTERNAL PATCH REPAIR ER SRM 53-00-01, PAGE 204 FIGURE 201. ACFT TT: 63,367 HOURS. ACFT TC: 12,994. (X) 2 L 7 2 4F RT A1NM 1998082100016 19980821 00016 WP 1998 8 21 TWAA9811202 1 19980713 A 2530 50198A COFFEEMAKER DOUG DC9 DC932 3022066 WP GALLEY MALFUNCTIONED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 996Z 47028 THE OTBD COFFEEMAKER PRODUCED A LARGE SPARK AND ELECTRICAL SMELL. CIRCUIT BREAKERS WERE PULLED. REPLACED COFFEEMAKER. CHECK-C 9-16-97 STL. ACFT TT: 78,249 HOURS. ACFT TC: 84,997. (X) 2 L 7 2 4F A6WE 1998082100017 19980821 00017 NM 1998 8 21 TWAA9811201 1 19980713 A 3350 CAP BOEING 767 7673Y0 NM CABIN LOOSE A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 632TW 24953 EGRESS LIGHT STRIP CAP WAS LOOSE AT THE AFT GALLEY, EXPOSING WIRING. SECURED LIGHT STRIP AND WIRES. CHECK-C 6-3-98 LAX . (X) 2 L 7 2 4F RT A1NM 1998082100018 19980821 00018 NM 1998 8 21 TWAA9811101 1 19980712 A 3350 57781 COVER BOEING 727 727231 1384079 NM CABIN CRACKED A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 64339 20844 IN THE AFT CABIN, A FOUR-INCH SECTION OF TH EGRESS LIGHT COVER WAS FOUND BROKEN AND A PIECE MISSING. REPLACED SECTION O F COVER. CHECK-C 5-25-98 JFK. 2 L 7 3 4F A3WE 1998082100019 19980821 00019 WP 1998 8 21 TWAA9811008 1 19980707 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LEFT FLANGE OF LONGERON 4L CRACKED AT ATTACHMENT TO FORMER AT FS 200. REPLA CED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN USING NAS 1097 AD-6. ACFT TT: 69,860 HO URS. ACFT TC: 81,151. (X) 2 L 7 2 4F A6WE 1998082100020 19980821 00020 WP 1998 8 21 TWAA9811006 1 19980707 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT FS 200. REPLACED LONGERON PER SRM 53-02, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN AND LONGERON WITH NAS 1097-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X) 2 L 7 2 4F A6WE 1998082100021 19980821 00021 WP 1998 8 21 TWAA9811007 1 19980707 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 980Z 47344 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND LONGERON 4L WITH CRACKED FLANGES AT STA 160. REPLACED LONGERON PER SRM 53-0 2, PG 48 TO PG 53. REPLACED FASTENERS COMMON TO SKIN USING NAS 1097-6. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X) 2 L 7 2 4F A6WE 1998082100022 19980821 00022 WP 1998 8 21 TWAA9811005 1 19980707 A 5730 SKIN DOUG DC9 DC932 3022066 WP RT WING DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WING SKIN WITH HOLE WORN THROUGH SKIN INBD OF NR 1 SLAT TRACK, L. E. OF WING TO END OF WING TO NR 3 SLAT TRACK HAD WORN SKIN. BLENDED WEAR AREA OTBD OF CENTER TRACK CUT-OUT PER SRM 57-0 1 PAGE 5, FIG 1. INSTALLED 3 DOUBLER REPAIRS PER SRM 57-06A, FIG 4. ACFT TT: 77,783 HOURS. ACFT TC: 84, 471. (X) 2 L 7 2 4F A6WE 1998082100023 19980821 00023 WP 1998 8 21 TWAA9811003 1 19980707 A 5753 RIB DOUG DC9 DC932 3022066 WP TE FLAP BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING FLAP, TWO RIBS INSIDE LOWER INBD ACCESS PLATE WERE BENT. INSTALL ED REPAIR DOUBLER PER ARA 15361. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100024 19980821 00024 WP 1998 8 21 TWAA9811002 1 19980708 A 2910 VALVE DOUG DC9 DC982 3022082 WP HYD SYSTEM FAILED A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 CE 05 908TW 49169 IAD - FLT 30 - MADE UNSCHEDULED LANDING DUE TO LT HYDRAULIC SYSTEM PRESSURE AND QUANTITY LOSS. DECLARED AN EMERGENCY. R EPLACED THE SPOILER SHUT OFF VALVE ON LT SIDE, MFG P/N 147425-3, AND THE LT POWER TRANSFER SHUT OFF VALVE MFG P/N 240695 -2. CHECK-C 2-16-98 STL. (X) 2 L 7 2 4F A6WE 1998082100025 19980821 00025 NM 1998 8 21 TWAA9811001 1 19980709 A 3350 532243 BATTERY PACK BOEING 767 767231 1385131 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 608TW 22571 STL - DURING MAINTENANCE, FOUND LT SIDE OF CABIN EGRESS LIGHTING WAS LIGHT WITH SYSTEM IN ARM OR ON POSITION. CHANGED P OWER PACKS AT ROW 12 AND ROW 31 ON LEFT SIDE. CHECK-C 5-4-98 LAX. (X) 2 L 7 2 4F RT A1NM 1998082100026 19980821 00026 WP 1998 8 21 TWAA9810903 1 19980707 A 3350 60030451LB BATTERY PACK DOUG DC9 DC951 3022051 WP TAIL DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 417EA 47753 STL - DURING MAINTENANCE, FOUND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. REPLACED TAIL COMPARTMENT LIGHTS NICAD B ATTERIES. CHECK-C 4-3-97 STL. (X) 2 L 7 2 4F RT A6WE 1998082100027 19980821 00027 NM 1998 8 21 TWAA9810902 1 19980707 A 3350 LIGHT BOEING 727 727231 1384079 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54349 21968 STL - DURING MAINTENANCE FOUND EGRESS FLOOR LIGHTS INOPERATIVE AT OVERWING EXIT. RECONNECTED FLOOR LAMP AT OVERWING EXI T. CHECK-C 10-20-97 JFK. (X) 2 L 7 3 4F A3WE 1998082100028 19980821 00028 NM 1998 8 21 TWAA9810901 1 19980707 A 3350 1619 LAMP BOEING 727 727231 1384079 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54349 21968 STL - DURING MAINTENANCE, FOUND FWD GALLEY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LIGHT. CHECK-C 10-20-97 JFK. (X) 2 L 7 3 4F A3WE 1998082100029 19980821 00029 NM 1998 8 21 TWAA9810809 1 19980623 A 5754 SKIN BOEING 767 767231 1385131 NM LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING CHECK-C, MAINTENANCE FOUND ON LT WING NR 5 L.E. SLAT INBD SIDE WITHSKIN DELAMINATION ON AFT SIDE. INSTALL ED 2 INCH BY 3 INCH IN HOT BONDED FLUSH DOUBLER PER SRM 57-43-02 AND SRM 51-70-10. (X) 2 L 7 2 4F RT A1NM 1998082100030 19980821 00030 WP 1998 8 21 TWAA9810808 1 19980629 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING UPPER REAR SPAR CAP, AN 'EYE BROW' CRACK ABOVE BOTH THE INBD AND OTBD STUD HOLES. CRACK LENGTH WAS 0.75 INCH ABOVE THE INBD HOLE AND 0.5 INCH ABOVE THE OTBD HOLE. INSTALLED DOUBLER PE R ARA 15291 AND BLUE PRINT JO60272, AND STD PRACTICES. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100031 19980821 00031 WP 1998 8 21 TWAA9810807 1 19980624 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP CARGO DOORWAY MISINSTALLED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 980Z 47344 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND AFT CARGO DOOR, AFT JAMB WITH DOUBLER INSTALLED USING BLIND FASTENERS. INST ALLED DOUBLER PER SRM 53-05, FIG 80. ACFT TT: 69,860 HOURS. ACFT TC: 81,151. (X) 2 L 7 2 4F A6WE 1998082100032 19980821 00032 WP 1998 8 21 TWAA9810806 1 19980618 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 929-945 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DOUBLER AT RBL 58, FLOOR LINE, CORRODED AT STA 929 TO STA 945. REMOVED CORR OSION PER 51-10-03, PARA 30 TO PARA 42. REPAIRED PER SRM 53-01, PG 9. INSTALLED NEW DOUBLER. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100033 19980821 00033 WP 1998 8 21 TWAA9810805 1 19980702 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 744 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI- DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR MEMBRANE CRACKED AT FS 744, RBL 50. REPLACED MEMBRANE WITH NEW PART PER SRM 51-01 PAGE 04. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100034 19980821 00034 WP 1998 8 21 TWAA9810804 1 19980624 A 5754 SPLICE DOUG DC9 DC932 3022066 WP NR 1 SLAT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING A CRACK IN WING L.E. ON SPLICE DOUBLER. LOCATED OTBD END OF NR 1 SLAT. INSTALLED SPLICE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100035 19980821 00035 NM 1998 8 21 TWAA9801803 1 19980623 A 5754 DOUBLER BOEING 767 767231 1385131 NM LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING CHECK-C, MAINTENANCE ON LT WING DOUBLER REMOVED ON FWD SIDE, INBD END OF NR 5 L.E. SLAT, AND FOUND DELAMINA TION ON AFT SIDE. INSTALLED 8 INCH BY 7 INCH HOT BONDED DOUBLER PER SRM 567-43-02 AND SRM 51-70-10. ACFT TT: 63,613 H OURS. ACFT TC: 14,886. (X) 2 L 7 2 4F RT A1NM 1998082100036 19980821 00036 NM 1998 8 21 TWAA9810802 1 19980625 A 5753 FLAP BOEING 767 767231 1385131 NM RT WING TE CONTAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING CHECK-C, MAINTENANCE FOUND ON RT WING NR 4 TE FLAP INBD AFT SIDE WITH INDICATION OF WATER. AFTER WATER REM OVED, INSTALLED 12 BY 30 PANEL AND ADHESIVE HOT BOND PER SRM 51-70-07, AND LIMITS PER 57-53-01. ACFT TT: 63,613 HOURS. ACFT TC: 14,886. (X) 2 L 7 2 4F RT A1NM 1998082100038 19980821 00038 WP 1998 8 21 TWAA9810717 1 19980623 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND IN CABIN DYE CHECK SHOWING 2 EACH CACKS IN LOWER FLANGE OF LONGERON 16R, AT STA 965 FORMER FRAME. REMOVED CRACKED SECTION OF L16R AND FITTED AND INSTALLED NEW SECTION OF LONGERON PER SRM 53-02, F IG 18. ACFT T: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100039 19980821 00039 WP 1998 8 21 TWAA9810716 1 19980624 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 237 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR PANEL SUPPORT HAT SECTION WITH APPROXIMATELY 1.5 INCH CRACK AT STA 237 , RBL 2 INCHES. REPAIRED PER SRM 51-01, PAGE 1, ITEM C, TWA STD PRACTICES, AND SRM 51-30-2, SRM 51-01 PAGE 4 FIG 1. AC FT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100040 19980821 00040 WP 1998 8 21 TWAA9810715 1 19980625 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 937-946 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR TRACK NR 3, FS 937 TO FS 946. REMOVED OLD TRACK FROM STA 929 TO STA 965. INSTALLED NEW TRACK PER SRM 53-05-10C, AND SRM 51-01 PAGE 1 ITEM C. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100041 19980821 00041 WP 1998 8 21 TWAA9810714 1 19980629 A 5720 SPLICE DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING 10 INCHES OTBD OF INBD END OF NR 3 SLAT, LE OF WING SPLICE PLATE, CRACKED. REMOVED CRACKED SPLICE PLATE AND INSTALLED NEW PART, DRILLED IN, INSTALLED AD RIVETS AND TENSION HI LOCKS PER SRM 51-30-0 PG 1. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100042 19980821 00042 WP 1998 8 21 TWAA9810713 1 19980629 A 5320 TIE DOUG DC9 DC932 3022066 WP BS 585 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACKED STRINGER TIE AT FS 585, AND STR 26R. REMOVED FORMER RING AT STA 579 FROM S25L TO S25R TO GAIN ACCESS TO STRINGER TIE. REPLACED CRACKED STRINGER TIE PER SRM 51-30. (X) 2 L 7 2 4F A6WE 1998082100043 19980821 00043 WP 1998 8 21 TWAA9810712 1 19980701 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOND FORMER FOOT STA 980 CRCKED BELOW LONGEORN 14R AND ABOVE 16R. REPLACED FORMER PER MO 72J14. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100044 19980821 00044 WP 1998 8 21 TWAA9810711 1 19980701 A 5521 RIB DOUG DC9 DC932 3022066 WP LT ELEVATOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND LOWER SURFACE AT DAMPER CUT OUT LOWER RIB CAP CRACKED ON LT ELEVATOR. REPLA CED LOWER RIB CAP PER DAC DWG 9918535. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100045 19980821 00045 WP 1998 8 21 TWAA9810709 1 19980629 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, A DYE CHECK SHOWED A ONE INCH CRACK IN LOWER FLANGE OF LONGERON 13R, AT FASTENER A T STA 965 FORMER FRAME. REMOVED CRACKED SECTION OF LONGERON 13R. INSTALLED NEW SECTION OF LONGERON AND INCORPORATED L ONGERON SPLICE REPAIR PER SRM 53-02. ACFT TT: 77,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100046 19980821 00046 WP 1998 8 21 TWAA9810708 1 19980628 A 5311 FRAME DOUG DC9 DC983 3022083 WP BS 313 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9303K 49529 JFK - THE FUSELAGE WAS DAMAGED AT FS 313, FORMER BETWEEN LONGERON 21 AND LONGERON 22R. DAMAGED AREA 6 INCHES WIDE BY 15 INCHES LONG. INSTALLED CLASS 2 REPAIR PER MD80 SRM 53-04, PG 47, FIG 12B SHEET 8. CHECK-C 11-8-97 MCI. ACFT TT: 35, 201 HOURS. ACFT TC: 17,425. (X) 2 L 7 2 4F RT A6WE 1998082100047 19980821 00047 WP 1998 8 21 TWAA9810707 1 19980630 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 794 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 STL - DURING ROUTINE MAINTENANCE, FOUND .50 INCH CRACK AT FASTENER AT STA 794, LONGERON 2R. SPLICED IN NEW SECTION OF L ONGERON 20 INCHES LONG PER SRM 53-02, FIG 18. CHECK-C 12-23-97 STL. ACFT TT: 49,615 HOURS. ACFT TC: 45,404. (X) 2 L 7 2 4F RT A6WE 1998082100048 19980821 00048 EU 1998 8 21 98ZZZX2829 1 19980617 A 3260 201072294 HARNESS FOKKER F28 F28MK0100 4990807 EU E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 882US 11334 CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EV ERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ING ELECTRONIC UNIT, NR 3 AND NR 4 GND/FLT SENSOR, AND RIGHT MAIN GEAR GND/FLT HARNESS. REF: OPERATOR CONTROL NR USAAF 98053, AND, 98ZZZX2830 THROUGH 98ZZZX2831. 2 L 7 2 4F RT 1998082100049 19980821 00049 EU 1998 8 21 98ZZZX2830 1 19980617 A 3260 201073201 SENSOR FOKKER F28 F28MK0100 4990807 EU E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 882US 11334 CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EV ERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ING ELECTRONIC UNIT, NR 3 AND NR 4 GND/FLT SENSOR, AND RIGHT MAIN GEAR GND/FLT HARNESS. REF: OPERATOR CONTROL NR USAAF 98053, AND, 98ZZZX2829 THROUGH 98ZZZX2831. 2 L 7 2 4F RT 1998082100050 19980821 00050 EU 1998 8 21 98ZZZX2831 1 19980617 A 3260 201073604 SENSOR FOKKER F28 F28MK0100 4990807 EU E/E BAY FAILED A USAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 EA 19 882US 11334 CLT - FLT 1458 - AFTER TAKEOFF, 'GND/FLT CONTROL' MESSAGE ALONG WITH MASTER CAUTION LIGHT WOULD INTERMITTENTLY APPEAR EV ERY 2-3 MINUTES. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SWITCH ING ELECTRONIC UNIT, NR 3 AND NR 4 GND/FLT SENSOR, AND RIGHT MAIN GEAR GND/FLT HARNESS. REF: OPERATOR CONTROL NR USAAF 98053, AND, 98ZZZX2829 THROUGH 98ZZZX2830. 2 L 7 2 4F RT 1998082100052 19980821 00052 WP 1998 8 21 TWAA9810705 1 19980623 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1288-1309 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOOR SUPPORT AT ZERO BL, STA 1288 TO STA 1309, WITH SEVERAL CRACKS IN UPPER FLANGE. INSTALLED REPAIR ANGLE PER ARA 15294A. ACFT TT: 28,425 HOURS. ACFT TC: 17,789. (X) 2 L 7 2 4F A6WE 1998082100053 19980821 00053 WP 1998 8 21 TWAA9810704 1 19980706 A 3340 8906K1268 SWITCH DOUG DC9 DC982 3022082 WP COCKPIT FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CE 05 913TW 49184 DCA - FLT 209 - AT 6,000 FEET WHEN EXTENDING AND TURNING ON WING LANDING LIGHTS, SMOKE CAME FROM UNDER CAPTAIN'S GLARE S HIELD. TURNED SWITCHES OFF IMMEDIATELY. DEFERRED CORR PER MEL. ON LAY OVER, REPLACED LT LANDING LIGHT SWITCH. CHECK- C 12-30-97 MCI. (X) 2 L 7 2 4F A6WE 1998082100054 19980821 00054 WP 1998 8 21 TWAA9810703 1 19980706 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 417EA 47753 STL - DURING MAINTENANCE, FOUND EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. REPLACED EXTERIOR OVERWING EMERGENCY LI GHT POWER SUPPLY, MFG PART NR 60-1177-5, AND BATTERY PACK. CHECK-C 4-3-97 STL. (X) 2 L 7 2 4F RT A6WE 1998082100055 19980821 00055 WP 1998 8 21 TWAA9810702 1 19980705 A 3350 BATTERY DOUG DC9 DC934 302207E WP CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 928L 48124 STL - FLT 655 - EMERGENCY FLOOR LIGHTING INTERMITTENTLY ON DURING FLIGHT, ROW 9 AND AFT. CHARGED EGRESS POWER SUPPLY BAT TERIES. CHECK-C 3-22-98 STL. (X) 2 L 7 2 4F RT A6WE 1998082100056 19980821 00056 WP 1998 8 21 TWAA9810701 1 19980705 A 3350 CONNECTOR DOUG DC9 DC934 302207E WP CABIN LOOSE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 928L 48124 DFW - FLT 655 - THE ESCAPE PATH LIGHTS, ROW 10 TO ROW 14, ILLUMINATED DURING FLIGHT. RE-SEATED CANNON PLUG ON BATTERY P ACK. CHECK-C 3-22-98 STL. (X) 2 L 7 2 4F RT A6WE 1998082100057 19980821 00057 WP 1998 8 21 TWAA9810615 1 19980625 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 234 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND A .50 INCH CRACK IN MEMBRANE AT LONGERON 18L, STA 234. REMOVED MEMBRANE AT L18L, FS 218 TO FS 237 PER DAC SRM 51-61 PAGE 1. FABRICATED COMPLETE PART FROM SAME MATERIAL PER DAC SRM 53-10-2, FIG 4 SHEETS 1 AND 2, ITEM 3. INSTALLED RIVETS PER DAC SRM 51-30-2 PAGE 1, AND BOLTS PER DAC SRM 51-30-1 FIG 1. ACFT TT: 7 7,783 HOURS. ACFT TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100058 19980821 00058 WP 1998 8 21 TWAA9810614 1 19980625 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 256 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, ON LOWER FUSELAGE, FOUND LONGERON 25L WITH CRACK AT FASTENER AT STA 256 FORMER FRA ME. INSTALLED NEW LONGERON SECTION AND TWO LONGERON REPAIR SPLICES PER SRM 53-02, FIG 18. ACFT TT: 77,783 HOURS. ACF T TC: 84,471. (X) 2 L 7 2 4F A6WE 1998082100059 19980821 00059 WP 1998 8 21 TWAA9810613 1 19980625 A 5744 CASTING DOUG DC9 DC932 3022066 WP RT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING, THE CENTER AND INBD FWD FLAP HINGE CASTING HAD BADLY PITTED MOUNT HOLES. INSTALLED NEW FLAP HINGE CASTING PER MM 57-40-01, PG 201 TO PG 205. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100060 19980821 00060 WP 1998 8 21 TWAA9811909 1 19980715 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 24L WITH INNER GRANULAR CORROSION ON ATTACH FITTING AT FWD SIDE OF FS 996 . REMOVED CORROSION PER SRM 51-10-03, STEP 35, PAGE 21. ALODINED AND PRIMED PER TWA STD PROCEDURES. INSTALLED NEW ATT ACH FITTING PER SRM 51-01. INSTALLED NEW RIVETS PER SRM 51-30-2. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100061 19980821 00061 WP 1998 8 21 TWAA9811908 1 19980713 A 5312 BULKHEAD CLIP DOUG DC9 DC932 3022066 WP BS 1143 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND 2 INCH CRACK ON STA 1143 CANTED BULKHEAD WEB CLIP, RT SIDE A RUDDER TRIM CABLE CUT -OUT. REPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100062 19980821 00062 WP 1998 8 21 TWAA9811907 1 19980713 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 513 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND INTERCOSTAL AT STA 513 ABOVE S27R CRACKED. REPAIRED PER SRM 53-01, PG 10. INSTAL LED DOUBLER REPAIR. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100063 19980821 00063 WP 1998 8 21 TWAA9811906 1 19980710 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 575-604 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND SKIN PILLOWING AT FS 575 TO FS 604, L27R THROUGH LONGERON 27L. REMOVED FRAMES FRO M FS 579 TO FS 604. REMOVED LONGERONS 26L TO 26R. REMOVED DOUBLERS, BLASTED PARTS PER SRM 51-10-03, ITEM 35D. REPLACE D DOUBLER FROM STA 580 TO STA 604, L26R TO 30. REMOVED CORROSION ON SKIN PER 51-10-3 ITEM 358. INSTALLED ALL PARTS WIT H NEW FASTENERS. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100064 19980821 00064 WP 1998 8 21 TWAA9811905 1 19980710 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 578 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 30 CRACKED JUST FORWARD OF STA 578 FRAME. INSTALLED NEW LONGERON END PER INSTL DWG 592176 PER SRM 51-01, PG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER SRM 51-60-0 AND INSTL DWG 592176. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100065 19980821 00065 WP 1998 8 21 TWAA9811904 1 19980710 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 578 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29L CRACKED JUST FORWARD OF STA 578 FRAME. REMOVED AND REPLACED LONGERON END PER INSTL DWG 592176 PER SRM 51-01, ITEM C. INSTALLED NEW STRINGER PER INSTL DWG 592176 AND SRM 51-60-0. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X) 2 L 7 2 4F A6WE 1998082100066 19980821 00066 WP 1998 8 21 VJ9800279 1 19980811 A 3350 9145155 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 967VV 47170 EMERGENCY PATH LIGHTING AT PASSENGER SEAT ROWS 19 - 23A INOP. REPLACED BATTERIES AT RT AFT LAV; OPS CHECKED GOOD IAW MM 33-00. 2 L 7 2 4F A6WE 1998082100067 19980821 00067 WP 1998 8 21 VJ9800280 1 19980727 A 5720 ANGLE DOUG DC9 DC932 3022066 WP WS 164 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 SPAR CAP XRS AT INBRD FLAP HINGE STUD HOLE HAS A .25 INCH CRACK ON FWD FACE RUNNING VERTICALLY FROM TOP EDGE OF HOLE. F ABRICATED ANGLE FROM 2024, 26 1/4 BY 3 INCHES. LOCATED AND DRILLED TWO OTHER ANGLES. INSTALLED REPAIRS IAW DC9 SRM 51- 30-5 AND DWG J0602T1. 2 L 7 2 4F A6WE 1998082100068 19980821 00068 WP 1998 8 21 VJ9800281 1 19980812 A 3530 DP3113 PBE DOUG DC9 DC932 3022066 WP CABIN DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 940VV 47523 PBE HAS HOLE IN BAG. REPLACED PBE. 2 L 7 2 4F A6WE 1998082100069 19980821 00069 EU 1998 8 21 MALA976180 1 19980809 A 2611 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO BAY FAILED A MALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 15 31XJ 031 DURING FLIGHT, THE CARGO SMOKE WARNING LIGHT ILLUMINATED, CARGO IRE EXTINGUISHER SWITCHED ON, CARGO SMOKE WARNING LIGHT WENT OUT SHORTLY AFTER, QRH COMPLETED. AIRCRAFT RETURNED TO MSP, LANDED WITHOUT DISCREPANCY. MAINTENANCE INSPECTED CAR GO COMPARTMENT AND DETERMINED TO BE INDICATION PROBLEM. MX REPLACED CARGO SMOKE DETECTOR IAW 26-13-15 AMM. OPS CHECK G OOD. REPLACED FIRE BOTTLE AND CARTRIDGE, FUNCTIONAL TEST GOOD. 2 L 7 2 4T RT A52EU 1998082100070 19980821 00070 EU 1998 8 21 MALA976181 1 19980805 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 119XJ 119 DURING INSPECTION, EMERGENCY OVERHEAD LIGHT INOP AT SEAT 8CD. MAINTENANCE RELAMPED. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998082100071 19980821 00071 EU 1998 8 21 MALA976182 1 19980809 A 2421 31342001 GENERATOR SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 GL 15 407XJ 340B407 DURING FLIGHT, THE RIGHT AC GENERATOR WENT OFF LINE. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT AC GENER ATOR AND AC GENERATOR CONTROL (PN 51634-002), IAW SAAB 340 AMM, GROUND RAN AIRCRAFT FOR 15 MINUTES ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998082100072 19980821 00072 NM 1998 8 21 UPS98227394 1 19980811 A 2910 BACH8C08NN0290 HOSE BOEING 727 72762C 138402C NM B-HYD SYST RUPTURED A IPXA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 913UP 19245 IN FLIGHT, 'B' HYD SYS QUANTITY SHOWED 0, AND NR 2 PUMP LOW PRESS LIGHT ILLUMINATED, AOM PROCEDURES ACCOMPLISHED, 10 MIN LATER, NR 1 B PUMP LOW PRESS LITE ILLUMINATED ALONG WITH 'B' SYS RUDDER AND ELEVETOR LIGHTS AND ELEV FEEL DRIFT LIGHT, AOM ACCOMPLISHED, AFTER LANDING, 'A' SYS QTY CONTINUED TO DECREASE TP 1.5 GAL AT SHUTDOWN. FOUND 'B' PUMP NR 2 PRESS LI NE RUPTURED (CHAFFED ON CLAMP). REMOVED AND REPLACED 'B' PUMP NR 2 PRESSURE LINE, LK CK GOOD, SERVICED ALL SYSTEMS PER MM 12-12 -00. 2 L 7 3 4F A3WE 1998082100073 19980821 00073 NM 1998 8 21 UPS98227395 1 19980811 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 207UP 21699 COCKPIT EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE WHEN TESTED FROM PILOT'S OVERHEAD PANEL. INSTALLED FRESHLY SERVICED BA TTERIES IN REPLACEMENT COCKPIT EMERG EXIT LIGHT ASSY AND INSTALLED AND TESTED LIGHT, IAW MM 33-50-101, TEST GOOD, PN ON- OFF 10-0067-9. SN OFF 28163 SN ON 12740. 2 L 7 3 4F A3WE 1998082100074 19980821 00074 WP 1998 8 21 UPS98827380 1 19980715 A 5320 3575843502N FITTING DOUG DC8 DC871F 302199D WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 1160 AT STR 35R, THE TORQUE BOX FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FIT TING IAW SRM 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1998082100075 19980821 00075 WP 1998 8 21 UPS98827381 1 19980721 A 5320 47799401 FITTING DOUG DC8 DC871F 302199D WP BS 1050 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D HEAVY CORROSION ON STA 1050 BUTT SPLICE ATTACH FITTING AT LONG 31. REMOVED AND REPLACED FITTING IAW D WG 4779940 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100076 19980821 00076 WP 1998 8 21 UPS98827382 1 19980722 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 25-70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 25-70 AT RBL 54, THE CUSP WEB HAS HEAVY CORROSION. REMOVED CORRODED AREA AND SPLICED IN NEW AREA IAW SRM 53-2-0 FIG 1B. 2 L 7 4 4F RT 4A25 1998082100077 19980821 00077 WP 1998 8 21 UPS98827383 1 19980722 A 5320 37799782 FITTING DOUG DC8 DC871F 302199D WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D INTERCOSTAL END FITTING AT LONG 13L JUST AFT OF STA 759 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100078 19980821 00078 WP 1998 8 21 UPS98827384 1 19980723 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP BS 440-460 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 440-460, STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100079 19980821 00079 WP 1998 8 21 UPS98827385 1 19980801 A 5320 3773077501 FITTING DOUG DC8 DC871F 302199D WP BS 200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 200 AT STR 27L, THE FLOORBEAM SUPPORT FITTING IS CORRODED. REMOVED, FABRICATED AND REPLACED FITTI NG IAW DWG 3773077 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100080 19980821 00080 WP 1998 8 21 UPS98827386 1 19980722 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1480-1500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 1480-1500, STR 32L HAS HEAVY CORROSION ON INNER FLANGE. REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1998082100081 19980821 00081 WP 1998 8 21 UPS98827387 1 19980721 A 5313 97585083 LONGERON DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 1260-1280, LONGERON 36 IS CRACKED. REPAIRED AREA IAW DHC SK755-547. 2 L 7 4 4F RT 4A25 1998082100082 19980821 00082 WP 1998 8 21 UPS98827388 1 19980721 A 5320 5704908 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1480-1500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 1480-1500 AT LONG 2L, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IA W DWG 5704908 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100083 19980821 00083 WP 1998 8 21 UPS98827389 1 19980722 A 5320 577327558 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 680 AT RBL 24, THE FLOORBEAM ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IA W DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100084 19980821 00084 WP 1998 8 21 UPS98827390 1 19980721 A 5320 3755841501 FITTING DOUG DC8 DC871F 302199D WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 1180 AT LONG 34R, THE SHEAR TIE FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FIT TING IAW DWG 3755841 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100085 19980821 00085 WP 1998 8 21 UPS98827391 1 19980717 A 5320 577327558 ANGLE DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 680 AT LBL24, THE FLOORBEAM SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100086 19980821 00086 WP 1998 8 21 UPS98827392 1 19980727 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 1540, LONG 33L IS CORRODED. REMOVED DAMAGED SECTION OF LONGERON AND REPLACED SECTION IAW SRM 53-5 -0. 2 L 7 4 4F RT 4A25 1998082100087 19980821 00087 WP 1998 8 21 UPS98827396 1 19980730 A 5720 5769858 ANGLE DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D LT WING L/E AT STA XS 250.089, THE VERTICAL STIFFNENER ANGLE IS CRACKED AT THE LWR END. REMOVED, FABR ICATED AND REPLACED ANGLE IAW DWG 5769859 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100088 19980821 00088 WP 1998 8 21 UPS98827397 1 19980724 A 5720 56422052 FITTING DOUG DC8 DC871F 302199D WP WS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C RT AUX SPAR AREA, THE REAR SPAR TO AUX SPAR LWR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLA CED FITTING IAW DHC SK 715-421 AND DWG 5642205. 2 L 7 4 4F RT 4A25 1998082100089 19980821 00089 WP 1998 8 21 UPS98827398 1 19980724 A 5720 36433192 FITTING DOUG DC8 DC871F 302199D WP WS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C RT WING T/E AT STA 98.00, THE REAR SPAR VERTICAL STIFFNER FITTING WHICH TIES TO THE FLAP CYCLINDER FIT TING IS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3643319 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100090 19980821 00090 WP 1998 8 21 UPS98827399 1 19980730 A 5320 4641324N FITTING DOUG DC8 DC871F 302199D WP WS 1690 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1690, LONG 28 LT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51- 1-20D. 2 L 7 4 4F RT 4A25 1998082100091 19980821 00091 WP 1998 8 21 UPS98827400 1 19980726 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C FUSELAGE SKIN IS CRACKED AROUND FWD ENTRY DOOR HOLD OPEN ROD (STA 25 ). REPAIRED IAW SRM 53-3-3 FIG 1 . 2 L 7 4 4F RT 4A25 1998082100092 19980821 00092 WP 1998 8 21 UPS98827401 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 329 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C RT WING L/E AT STA XFS 329.000- THE LWR L/E RIB IS CRACKED AT MID SPAN. STOP DRILLED CRACK AND REPAIR ED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998082100093 19980821 00093 WP 1998 8 21 UPS98827402 1 19980725 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 347.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C RT WING L/E LWR SKIN AT STA XFS347.500 IS CRACKED IN 2 PLACES. REPAIRED AREA IAW SRM 57-2-1 FIG 2. 2 L 7 4 4F RT 4A25 1998082100094 19980821 00094 WP 1998 8 21 UPS98827403 1 19980728 A 5320 5779936 DOUBLER DOUG DC8 DC871F 302199D WP BS 1541-1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1541-1580 AT STR 31R, THE FINGER DOUBLER IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REPLACE D FINGER DOUBLER IAW DWG 5779936 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998082100095 19980821 00095 WP 1998 8 21 UPS98827404 1 19980724 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 283.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C RY WING L/E SECTION BTWN PYLONS AT STA XFS283.250, THE L/E SKIN IS CRACKED AT THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 1998082100096 19980821 00096 WP 1998 8 21 UPS98827405 1 19980724 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 683 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C FWD ACC COMP AT STA 683 AND STR 30R, THE FRAME CHORD IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 53-2-5 FIG 14. 2 L 7 4 4F RT 4A25 1998082100097 19980821 00097 WP 1998 8 21 UPS98827406 1 19980725 A 5720 36412571 DOUBLER DOUG DC8 DC871F 302199D WP WS 728 & 741 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C LT WING L/E INTERNAL DOUBLER HAS HEAVY CORROSION AT STA XFS 728. 750 AND XFS741.250. REMOVED, FABRIC ATED AND REPLACED DOUBLER IAW DWG 3641257 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100098 19980821 00098 WP 1998 8 21 UPS98827407 1 19980726 A 5320 4641324 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1690, STR 30L END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1998082100099 19980821 00099 WP 1998 8 21 UPS98827408 1 19980726 A 5320 4641324 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1690, LONG 34R END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 1998082100100 19980821 00100 WP 1998 8 21 UPS98827409 1 19980803 A 5320 975406931 ANGLE DOUG DC8 DC871F 302199D WP BS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 380 AT STR 21R, THE CUSP ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9754069 AND SRM 51- 1-21D. 2 L 7 4 4F RT 4A25 1998082100101 19980821 00101 WP 1998 8 21 UPS98827410 1 19980727 A 5320 975584503 FITTING DOUG DC8 DC871F 302199D WP BS 1290 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1290 AT STR 21L, THE FRAME TO CUSP TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTI NG IAW DWG 975584 AND SRM 5 1-1-20D. 2 L 7 4 4F RT 4A25 1998082100102 19980821 00102 WP 1998 8 21 UPS98827411 1 19980727 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1260-1280, STR 34R IS CRACKED ON UNDERSIDE OF RT FLANGE. REPAIRED AREA IAW DHC SK 715-548. 2 L 7 4 4F RT 4A25 1998082100103 19980821 00103 WP 1998 8 21 UPS98827412 1 19980727 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1400 FRAME BTWN STR 35L-36 IS CRACKED ON END. REPAIRED AREA IAW DHC SK 715-883. 2 L 7 4 4F RT 4A25 1998082100104 19980821 00104 WP 1998 8 21 UPS98827413 1 19980727 A 5320 5758571503 FITTING DOUG DC8 DC871F 302199D WP BS 1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 1280 ABOVE STR 33R, THE SEAT TRACK SUP[PORT FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5758571 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100105 19980821 00105 WP 1998 8 21 UPS98827414 1 19980725 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 3 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C RT WING T/E RIB AT STA XW 3.00, IS CRACKED IN 4 PLACES. REPAIRED AREA IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998082100106 19980821 00106 WP 1998 8 21 UPS98827415 1 19980810 A 5320 5612298 DOUBLER DOUG DC8 DC871F 302199D WP BS 10-20 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C COCKPIT SUB-FLOOR FINGER DOUBLER AT STA -10 TO-20 BLB50 HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5612298 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998082100107 19980821 00107 WP 1998 8 21 UPS98827416 1 19980728 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 55 AT STR 24L, THE FRAME IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 3. 2 L 7 4 4F RT 4A25 1998082100108 19980821 00108 WP 1998 8 21 UPS98827417 1 19980728 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE:C STA 55 AT STR 24R, THE FRAME IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 3. 2 L 7 4 4F RT 4A25 1998082100109 19980821 00109 NM 1998 8 21 UPS98227419 1 19980811 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 EMER LIGHTS FOUND LEFT ON WHEN CHECKED ALL WERE INOP. REMOVED AND REPLACED ALL EMER LGIHT BATTERIES PER MM 33-50-22, OP S CHK GOOD. 2 L 7 3 4F A3WE 1998082100110 19980821 00110 NM 1998 8 21 UPS98227420 1 19980812 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 RT AFT OVERWING EXIT LIGHT INOP. REMOVED AND REPLACED RT AFT OVERWING EMER EXIT LIGHT ASSY. OPS CHKS NORMAL PER MM 33- 50-61. 2 L 7 3 4F A3WE 1998082100111 19980821 00111 WP 1998 8 21 UPS98827418 1 19980722 A 5320 3779659501 FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D LONGERON 4L END FITTING CRACKED JUST FWD OF F/S 857. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT F ITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100112 19980821 00112 WP 1998 8 21 UPS98827421 1 19980813 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 EMER LIGHTS BATTERY AND RELAY UNIT CHANGED PER MMOC REQUEST (CAUTIONARY). REMOVED AND REPLACED EMER LIGHTS BATTERY PACK AND RELAY UNIT PER 33-50-01, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1998082100113 19980821 00113 WP 1998 8 21 UPS98827422 1 19980810 A 5330 SKIN DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 TWO RIVETS POPPED ON FUSELAGE SKIN ABOUT SIX FEET AFT OF NR 4 PIT DOOR. COMPLIED WITH EO DC8-5330-10186A. 2 L 7 4 4F RT 4A25 1998082100114 19980821 00114 WP 1998 8 21 UPS98827424 1 19980812 A 3397 WIRE DOUG DC8 DC871F 302199D WP CABIN BROKEN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 NO LIGHT ON AFTER EMER EXIT LIGHTS DISARMED. SEE PREVIOUS WRITE UP P 294088. RECONNECTED BROKEN WIRE AT CONNECTOR P1-1 345 PINS 7 AND 11 AT BATTERY PACK. OPS CK SYS NORMAL. 2 L 7 4 4F RT 4A25 1998082100115 19980821 00115 NE 1998 8 21 QXEA9801064 2 19980809 A 7200 ENGINE DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE HAMSTD 14SF 14SF23 NE NR 2 MALFUNCTIONED A QXEA E ENGINE SHUTDOWN E VIBRATION/BUFFET DE DESCENT 1 NM 09 351PH 490 PCEAG0057 961123 (REVISED) AT ABOUT 13,000 FEET, DESCENDING INTO SEA, NR 2 ENGINE GOT VERY LOUD, FOLLOWED BY AN AIRCRAFT VIBRATION. NR 2 ENGINE TORQUE INDICATION PEGGED AND ITT INDICATED 1000 DEGREES CELSIUS. PLACED NR 2 ENGINE CONTROL TO START/FEATHER A ND SHUT DOWN NR 2 ENGINE. DECLARED AN EMERGENCY, AND AIRCRAFT LANDED WITHOUT INCIDENT. SUBMITTER STATES, NR 2 ENGINE M ANUAL FUEL CONTROL UNIT (MFCU). MAINTENANCE REPLACED ENGINE AND PROPELLER. AWAITING SHOP FINDINGS ON ENGINE AND PROPEL LER. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1998082100116 19980821 00116 EU 1998 8 21 QXEA9801072 1 19980810 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 GEG - OVERHEAD EXIT LIGHT OUT AT ROW 8. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED, ASSEMBLY TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998082100117 19980821 00117 EU 1998 8 21 QXEA9801073 1 19980811 A 2612 8934100450 CONTROL UNIT KIDDE FOKKER F28 F28MK4000 4990810 EU NR 2 ENGINE MALFUNCTIONED A QXEA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 499US 11182 GEG - CREW REPORTED NR 2 ENGINE FIRE WARNING IN FLIGHT. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO INDICATION OF FIR E OR OVERHEAT. FIRE WARNING FOUND TO BE AN INDICATION PROBLEM. TROUBLE SHOT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANC E MANUAL. FOUND INBOARD PIGTAIL AND OUTBOARD AFT PIGTAIL OF FIRE LOOP TO HAVE CORRODED CONNECTIONS. REMOVED AND REPLAC ED FIRE WARNING LOOP AND CONTROL UNIT. SYSTEM OPERATIONALLY TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998082100118 19980821 00118 NM 1998 8 21 DHL98741003 1 19980813 A 2613 OVERHEAT LOOP BOEING 727 7272Q9 138448M NM AFT BODY OUT OF POSITION A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 741DH 21931 DURING CLIMB LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. ABNORMAL CHECKILIST ACCOMPLISHED AND AT ONE MINUTE WITH NR 1 EN G BLEED CLOSED, LIGHT EXTIGUISHED. TROUBLE SHOT SYSTEM PER 26-14-00. FOUND AFT LEFT LOOP TOUCHING STRUTURE. REPOSITIO NED LOOP, RAN AIRCRAFT. LEAK CHECKED ALL DUCTS AND CLAMPS. NO LEAKS FOUND OPS CHECK GOOD PER M/M. 2 L 7 3 4F RT A3WE 1998082100119 19980821 00119 1998 8 21 VNAA9808007 4 19980807 A 3140 7013348913 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 440JS 82488 285 3058 ON TAXI OUT FOR TAKEOFF, ANGLE OF ATTACK/SHAKER FAIL WARNING MESSAGES ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 DATA AQUISITION UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-42-0 0. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100120 19980821 00120 NM 1998 8 21 VNAA9808008 1 19980810 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AFT RT FUSE DENTED A VNAA K NONE O OTHER IN INSP/MAINT 1 GL 07 440JS 3058 THE AIRCRAFT WAS STRUCK BY A CATERING TRUCK, WHILE PARKED AT THE GATE. THE DAMAGE WAS NEAR THE GALLEY SERVICE DOOR AREA . MAINTENANCE INSPECTED THE DAMAGE AND APPROVED THE AIRCRAFT FOR RETURN TO SERVICE, UNDER DORNIER SPR 14457. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100121 19980821 00121 NM 1998 8 21 VNAA9808009 1 19980811 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA O OTHER L NO TEST IN INSP/MAINT 1 GL 07 433JS 56095 724 3047 DURING THE PRE-FLIGHT INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 4,5, AND SIX WERE NOTED TO BE INOPERATIVE. OUTSTAT ION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY FURTHER PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE 5LK BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100122 19980821 00122 EU 1998 8 21 C2XA98IA246 1 19980707 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU BS 36-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14830 184 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLIGHT ATTENDANT'S SEAT TRACK CORRODED BEYOND LIMITS BETWEEN FRAMES 36 AND 39. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 17,634.1 HOURS. TC: 20,767. (X) 2 H 7 2 4T RT A53EU 1998082100123 19980821 00123 GL 1998 8 21 C2XA98BT048 2 19980706 A 7200 23054002 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL NR 1 OVERTEMP A C2XA H DEACTIVATE SYST/CIRCUITS X J ENGINE FLAMEOUT WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 13935 1588 145022 CAE310078 EWR - AFTER LANDING, NR 1 ENGINE FLAMED OUT. MAINTENANCE DOWNLOADED CMC. FOUND ITT LIMITS 1,050 DEGREES CELSIUS FOR 3 SECONDS. REMOVED AND REPLACED ENGINE DUE TO OVERTEMP. ACFT TT: 2,104.8 HOURS. ACFT TC: 1,413. (X) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1998082100124 19980821 00124 EU 1998 8 21 C2XA98BT050 1 19980711 A 2421 20032 GENERATOR AEROSP ATR42 ATR42320 8680930 EU NR 1 ENGINE FAILED A C2XA K NONE J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 14822 14394 2672 197003 163 EWR - ON APPROACH INTO EWR, NR 1 ACW GENERATOR FAILED WITH AN ACCOMPANIED SMOKE SMELL IN CABIN AND COCKPIT. EMERGENCY D ECLARED. AIRCRAFT LANDED WITH NO FURTHER DIFFICULTY. THE NR 1 ACW GENERATOR WAS REMOVED AND REPLACED IAW ATW MM 24-22- 84-RAI 10000-002. OPS AND LEAK CHECK SATISFACTORY. (X) 2 H 7 2 4T RT A53EU 1998082100125 19980821 00125 SO 1998 8 21 C2XA98IA243 1 19980630 A 3260 922AA2YA6PZ722 SWITCH EMB 120 EMB120RT SO LT MLG CONTAMINATED A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 09 17720 120142 IAH - FLT 3772 - PILOT REPORTED THE LEFT GEAR WOULD NOT RETRACT PROPERLY. THE AIRCRAFT LANDED WITHOUT INCIDENT AND MAIN TENANCE SERVICED THE LANDING GEAR ACCUMULATOR. THE AIRCRAFT WAS RELEASED TO SERVICE AND ENCOUNTERED THE SAME DISCREPANC Y ON FLT 3777 WHERE THE PILOT REPORTED THE LEFT GEAR WOULD NOT RETRACT PROPERLY. THE AIRCRAFT LANDED AT IAH WITHOUT INC IDENT. MAINTENANCE CLEANED THE LEFT GEAR UPLOCK PROXIMITY SENSOR CONNECTIONS, RESECURED THEM, AND RELEASED THE AIRCRAFT FOR SERVICE. (X) 2 L 7 2 4T RT A31SO 1998082100126 19980821 00126 SO 1998 8 21 C2XA98IA245 1 19980703 A 3230 12032943001 SEQUENCE VALVE EMB 120 EMB120RT SO LT MLG WW OUT OF ADJUST A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 09 17720 120142 IAH - FLT 3725 - PILOT REPORTED THE LEFT GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT . MAINTENANCE FOUND A LOOSE CONNECTION AT THE LANDING GEAR RELAY BOX, AND THE LEFT GEAR INBD SEQUENCE VALVE TO BE OUT O F ADJUSTMENT. MAINTENANCE TIGHTENED THE AFFECTED CANNON PLUG AND PERFORMED AN ADJUSTMENT TO THE LEFT GEAR INBD SEQUENCE VALVE. THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998082100127 19980821 00127 SO 1998 8 21 C2XA98IA244 1 19980630 A 3260 922AA2YA6PZ722 SWITCH EMB 120 EMB120RT SO RT MLG CONTAMINATED A C2XA K NONE J WARNING INDICATION CL CLIMB 1 SW 09 57734 120199 IAH - FLT 3786 - PILOT REPORTED THE RIGHT GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDEN T. MAINTENANCE REMOVED MOISTURE FROM THE RIGHT GEAR UPLOCK PROXIMITY SWITCHES. THE GEAR OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998082100128 19980821 00128 SO 1998 8 21 C2XA98IA242 1 19980630 A 3230 12038594001 CONTROL UNIT EMB 120 EMB120RT SO MLG INOPERATIVE A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 09 16710 120106 IAH - FLT 3684 - THE PILOT REPORTED A SEVERE VIBRATION WAS FELT AFTER THE LANDING GEAR WAS SELECTED TO THE UP POSITION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT AND MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CON TROL BOX, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998082100129 19980821 00129 EU 1998 8 21 C2XA98BT046 1 19980630 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST CR CRUISE 1 SW 09 34817 152 EWR - CREW REPORTS 'EMERGENCY EXIT LIGHTS ON IN FLIGHT'. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY CONTROL UNIT. 2 H 7 2 4T RT A53EU 1998082100130 19980821 00130 SO 1998 8 21 C2XA98IA241 1 19980629 A 3350 1317 BULB EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59708 120098 IAH - FLT 3901 - DURING POST-FLIGHT INSPECTION, CREW REPORTED RT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB, EMERGENCY LIGHTING SYSTEM CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998082100131 19980821 00131 SO 1998 8 21 C2XA98CL049 1 19980703 A 7920 1593731 LINE EMB 120 EMB120RT SO LT ENGINE SPLIT A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 16731 120190 CLE - FLT 33259 - THE CREW REPORTED THAT DURING CLIMB-OUT, THE LEFT HAND ENGINE LOST OIL PRESSURE. THE CREW SUCCESSFULL Y COMPLETED A PRECAUTIONARY ENGINE SHUT DOWN, AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE INSPECTED THE ENGINE THEN REM OVED AND REPLACED A SPLIT LINE ON THE LEFT HAND ENGINE OIL COOLER IAW EMB-120 MM 79-21-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. ACFT TT: 15,849.9 HOURS. TOTAL CYCLES: 21,630. (X) 2 L 7 2 4T RT A31SO 1998082100132 19980821 00132 NM 1998 8 21 BJNA980701 1 19980707 A 2613 356254255 SENSOR BOEING 737 737214 138446R NM APU COMPARTMENT MALFUNCTIONED A BJNA K NONE O OTHER NR NOT REPORTED 1 WP 11 457TM 20156 LEFT WING BODY OVERHEAT LIGHT ILLUMINATED. AIRCRAFT RELEASED PER MEL 26-12, DMI 701, ITEM TRANSFERRED TO DMI LOG AND PL ACARDED. REF: DMI 701, REMOVED AND REPLACED OVERHEAT LOOP IN APU COMPARTMENT IAW 26-18. OPS CHECKS NORMAL. (LOG PAGE 10721). (X) 2 L 7 2 4F A16WE 1998082100133 19980821 00133 NM 1998 8 21 AALA981206 1 19980621 A 3530 1190030 PBE BOEING 727 727227 1384078 NM CABIN DISCHARGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 729AA 20736 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY PORTABLE BREATHING EQUIPMENT DEPLETED. REPLACED PORTABLE BREATHING EQ UIPMENT. SYSTEM GROUND CHECKED NORMAL. (X) 2 L 7 3 4F A3WE 1998082100134 19980821 00134 NM 1998 8 21 AALA981295 1 19980630 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 708AA 22465 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRWAY EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPLACED AFT STAIRWAY EMERG ENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100135 19980821 00135 NM 1998 8 21 AALA981301 1 19980702 A 3350 AAP2661 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 883AA 21522 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN CEILING NEAR ROW 25 INOPERATIVE. REPLACED EMERGENCY EXIT CE ILING LIGHT PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100136 19980821 00136 NM 1998 8 21 AALA981188 1 19980615 A 3350 CONTACTS BOEING 727 727227 1384078 NM BATTERY PACK DIRTY A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721AA 20729 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. CLEANED CONTACTS ON BATTER Y PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100137 19980821 00137 EU 1998 8 21 AALA981140 1 19980605 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1452B 11464 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT HAND AFT LAVATORY EMERGENCY LIGHT INOPERATIVE. REPLACED AFT RIGHT HAND LAVATO RY EMERGENCY LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998082100138 19980821 00138 NM 1998 8 21 AALA981141 1 19980605 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 708AA 22465 IAH - DURING OVERNIGHT CHECK, AFT STAIR OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED AFT STAIRWAY EMERGENCY LIGHT. S YSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100139 19980821 00139 NM 1998 8 21 AALA981145 1 19980607 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 878AA 21390 DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT SEGMENT IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SEGMENT IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100140 19980821 00140 EU 1998 8 21 AALA981176 1 19980613 A 3350 A47011407 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1453D 11465 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY SIDEWALL LIGHT AT LEFT OVERWING EXIT BROKEN. REPLACED EMERGENCY SIDEWALL EXIT LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998082100141 19980821 00141 EU 1998 8 21 AALA981201 1 19980620 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1412A 11370 DFW - DURING OVENRIGHT MAINTENANCE, RIGHT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BROKEN WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998082100142 19980821 00142 NM 1998 8 21 AALA981265 1 19980624 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 848AA AA13 20989 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ABOVE AFT STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ABOVE AF T STAIRS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100143 19980821 00143 NM 1998 8 21 AALA981203 1 19980620 A 3397 WIRE BOEING 727 727227 1384078 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 726AA 20733 DFW - DURING OVERNIGHT MAINTENANCE, LOWER HALF OF AFT AIR STAIR LIGHTS INOPERATIVE. REPAIRED WIRE ON LOWER HALF OF AFT STAIR LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100144 19980821 00144 NM 1998 8 21 AALA981180 1 19980615 A 3350 1001141 LIGHT GRIMES BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 726AA 20733 ORD - DURING OVERNIGHT INSPECTION, AFT STAIR WELL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT IN AF T STAIR WELL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100145 19980821 00145 NM 1998 8 21 AALA981202 1 19980620 A 3350 1001141 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 723AA 20731 DFW - DURING OVERNIGHT MAINTENANCE, THE AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AIRSTAIR EMERGENCY EXIT LIG HT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998082100146 19980821 00146 WP 1998 8 21 AALA981278 1 19980627 A 4990 O-RING DOUG DC9 DC982 3022082 WP APU FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 221AA 49172 ORD - FLT 1631 - ODOR IN CABIN BOTH ON GROUND AND IN AIR. AFTER TAKEOFF, ODOR WAS STRONGER AND A SMOKY APPEARANCE WAS N OTED THROUGHOUT CABIN. LANDED ORD WITHOUT INCIDENT. REPLACED APU OIL COOLER SUPPLY LINE O-RING. ACCOMPLISHED BURN OUT OF HIGH PRESSURE PNEUMATIC DUCTING PER MM. REPLACED COALESCER BAGS. NO SMOKE NOTED. SYSTEM GROUND CHECKED, NORMAL OP ERATION. (X) 2 L 7 2 4F A6WE 1998082100147 19980821 00147 WP 1998 8 21 AALA981274 1 19980623 A 2720 VALVE DOUG DC9 DC982 3022082 WP RUDDER LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 70425 49337 SJC - FLT 1041 - DURING APPROACH TO SJC, HAD HYDRAULIC FLUID LOSS ON RIGHT HAND SYSTEM. THE LANDING GEAR WAS EXTENDED A ND BACKED UP WITH THE ALTERNATE GEAR EXTENSION. PRESSURE AND QUANTITY WENT TO ZERO. CREW FOLLOWED THE CHECKLIST AND LA NDED AT SJC WITH GEAR DOORS DOWN (WOULD NOT RETRACT). REPLACED PACKING ON RUDDER HYDRAULIC POWER SHUT OFF VALVE. SERVI CED RIGHT HAND HYDRAULIC SYSTEM. RAN RIGHT HAND ENGINE AND PERFORMED LEAK CHECK. RUDDER HYDRAULIC SHUT OFF VALVE CHECK S NORMAL FOR SERVICE. CHECKED GEAR DOORS FOR DAMAGE, NO DAMAGE NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100148 19980821 00148 1998 8 21 AALA981299 4 19980701 A 2565 29985103 SLIDE AIRCRUISERS A3593 DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 440AA 49549 ORD - FLT 1928 - AFT GALLEY EMERGENCY SLIDE DEPLOYMENT WIRE BROKEN. REPLACED AFT GALLEY DOOR EMERGENCY SLIDE PER MM. S YSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100149 19980821 00149 WP 1998 8 21 AALA981293 1 19980630 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 405A 49316 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD LEFT HAND DOOR INOPERATIVE. REPAIRED WIRE ON LEFT HAND FORWARD SIDE ABOVE ENTRY DOOR FOR EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED, NORMAL O PERATION. (X) 2 L 7 2 4F A6WE 1998082100150 19980821 00150 WP 1998 8 21 AALA981302 1 19980702 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7532A 49924 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED CORRODED EMERGEN CY EXIT FLOOR PATH LIGHT STRIP IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100151 19980821 00151 WP 1998 8 21 AALA981284 1 19980628 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 462AA 49592 DFW - DURING OVENRIGHT MAINTENANCE, AFT AIR STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRING FOR AFT AIR STAIR E MERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100152 19980821 00152 WP 1998 8 21 AALA981276 1 19980625 A 3350 D77311001 BALLAST DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 597AA 53287 DFW - DURING OVERNIGHT MAINTENANCE, LEFT HAND SIDE WALL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LEFT HAND SIDE WALL EMERGENCY EXIT LIGHT BALLAST. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998082100153 19980821 00153 WP 1998 8 21 AALA981272 1 19980626 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 586AA 53249 DFW - DURING OVERNIGHT MAINTENANCE, THE SIDEWALL FORWARD POSITION AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED SPLICE AT SIDEWALL FORWARD POSITION AFT STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 2 4F A6WE 1998082100154 19980821 00154 WP 1998 8 21 AALA981273 1 19980626 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 278AA 49294 DFW - DURING OVERNIGHT MAINTENANCE, THE AFT ENTRY TAIL CONE EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED WIRE AT AFT ENTR Y TAIL CONE EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100155 19980821 00155 WP 1998 8 21 AALA981275 1 19980626 A 3244 TIRE BFGOODRICH DOUG DC10 DC1010 3022110 WP NR 4 MLG FAILED A AALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 126AA 46947 SFO - FLT 0020 - AFTER TAKEOFF SFO, 5 KNOTS PRIOR TO V1, AIRPLANE VIBRATED EXCESSIVELY. AFTER GEAR RETRACTION, ALL THRE E RED LIGHTS STAYED ILLUMINATED. GEAR HANDLE POPPED OUT AND THEN BACK INTO THE UP DEFAULT. VISUAL INSPECTION SHOWED RI GHT MAIN GEAR DOORS OPEN SLIGHTLY. ALTERNATE GEAR EXTENSION WAS PERFORMED WITH SUBSEQUENT INSPECTION OF THE TIRES. NR 4 MAIN TIRE WAS FOUND SHREDDED. RETURNED AND LANDED SFO WITHOUT INCIDENT. REPLACED NR 4 MLG TIRE PER MM. STRAIGHTENED FOLLOW-UP DOOR SEAL. PERFORMED GEAR SWING SEVERAL TIMES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1998082100156 19980821 00156 WP 1998 8 21 AALA981205 1 19980621 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 73444 49470 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS BETWEEN FIRST CLASS AND COACH INOPERATIVE. REPLACE D JUMPER WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100157 19980821 00157 WP 1998 8 21 AALA981209 1 19980622 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 453AA 49558 PHX - DURING OVERNIGHT MAINTENANCE, FORWARD FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPAIRED FOR WARD FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100158 19980821 00158 WP 1998 8 21 AALA981264 1 19980624 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 428AA 49340 ORD - DURING OVERNIGHT CHECK, AFT STAIR EMERGENCY EXIT LIGHT ON RIGHT HAND WALL INOPERATIVE. REPAIRED WIRES FOR AFT STA IR EMERGENCY EXIT LIGHT ON RIGHT HAND WALL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100159 19980821 00159 NE 1998 8 21 AALA981253 2 19980620 A 7261 AC9806F65 FILTER RUSSEL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE CLOGGED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 7546A 53028 DFW - FLT 2083 - EN ROUTE DFW/IAH IN CRUISE, RIGHT ENGINE OIL STRAINER CLOGGIN G LIGHT ILLUMINATED. OIL TEMPERATURE WAS 128 DEGREES AND OIL PRESSURE 45 PSI. RETARDED THROTTLE AND LIGHT WENT OUT. DECLARED AN EMERGENCY AND AIR INTERRUPTED. ACCOMPLISHED REDUCED THRUST APPROACH TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE OIL FILTER, DRAINED AN D SERVICED OIL TO FULL. RAN ENGINE AT HIGH POWER, NO DISCREPANCIES NOTED, LEAK CHECK GOOD. SYSTEM GROUND CHECKED, NORM AL OPERATION. (X) 2 L 7 2 4F 4 F A6WE E9NE 1998082100160 19980821 00160 WP 1998 8 21 AALA981207 1 19980620 A 3260 D128 SENSOR ELDEC DOUG DC9 DC982 3022082 WP MLG OUT OF ADJUST A AALA K NONE N FALSE WARNING CR CRUISE 1 SW 07 429AA 49341 ORD - FLT 0321 - EN ROUTE, DURING CRUISE, GEAR DOOR OPEN LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE, TURNING ON RI GHT ENGINE HYDRAULIC PUMP TO HIGH TO EXTINGUISH LIGHT. LANDED ORD WITHOUT INCIDENT. POSITIONED MAIN GEAR DOORS' SENSOR S AND TARGETS TO PROPER POSITION PER MM. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998082100161 19980821 00161 NM 1998 8 21 AALA981167 1 19980610 A 3397 WIRE DOUG MD11 MD11 3023602 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, BUSINESS CLASS EMERGENCY EXIT FLOOR PATH LIGHTING ON RIGHT SIDE ILLUMINATED ALL THE TIME. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE IN BUSINESS CLASS ON RIGHT SIDE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998082100162 19980821 00162 NM 1998 8 21 AALA981186 1 19980616 A 2612 4208030000 HARNESS SIMMONDS DOUG MD11 MD11 3023602 NM NR 1 ENGINE FAILED A AALA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 SW 07 1756 48491 MIA - FLT 0901 - AFTER TAKEOFF, EN ROUTE MIA/EZE, WITH THRUST SET AT TAKEOFF POWER, THE CREW RECEIVED A NR 1 FIRE WARNIN G. CREW ACCOMPLISHED FULL FIRE CHECKLIST PROCEDURE. DUMPED FUEL TO MAXIMUM LANDING WEIGHT AND RETURNED TO MIA AND LAN DED WITHOUT INCIDENT. TROUBLESHOT AND FOUND EXCESSIVE RESISTANCE ON UPPER RIGHT HAND A-LOOP. REPLACED UPPER RIGHT HAND A-LOOP AND RIGHT HAND HARNESS AFT AND UPPER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998082100163 19980821 00163 NM 1998 8 21 AALA981200 1 19980620 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 339AA 22336 SFO - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY CROSS AISLE EMERGENCY LIGHTS INOPERATIVE. REPLACED SPLICE ON FORWARD GALLEY CROSS AISLE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998082100164 19980821 00164 NM 1998 8 21 AALA981266 1 19980624 A 2530 46700017 COFFEEMAKER BOEING 767 767223 1385123 NM CABIN MALFUNCTIONED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 317AA 22319 LHR - FLT 0142 - EN ROUTE JFK/LHR FIRST CLASS NR 1 COFFEEMAKER EMITTED SPARKS BEHIND BUTTON LABELED 'HOT'. TURNED OFF C OFFEEMAKER. LANDED LHR WITHOUT INCIDENT. REPLACED NR 1 COFFEEMAKER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998082100165 19980821 00165 WP 1998 8 21 AALA981173 1 19980609 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1977 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FRAME ANGLE FORWARD SIDE HAS CORROSION STA 1977 FROM LONGERON 48L TO LONGEORN 52. REPAIRED PER ESO 7349, DATED 6 -8-98. TST: 96,680.24 HOURS. CYCLES: 18,100. (X) 2 L 7 3 4F A22WE 1998082100166 19980821 00166 WP 1998 8 21 AALA981172 1 19980610 A 5320 FRAME DOUG DC10 DC1030 3023501 WP CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - CORROSION ON CENTER CARGO DOOR CUT-OUT FORWARD LOWER CORNER OF JAMB STA 1701, L43R. INSTALLED DOUBLER STRAP OVER BLENDED AREA PER ESO7349 DATED 6-10-98. TST: 96,680.24 HOURS. CYCLES: 18,100. (X) 2 L 7 3 4F A22WE 1998082100167 19980821 00167 WP 1998 8 21 AALA981171 1 19980610 A 5744 BRACKET DOUG DC10 DC1030 3023501 WP WS 736 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - CORROSION IN 2 EACH BOLT HOLES AND ON FACE OF OUTBOARD FLAP, OUTBOARD HINGE BRACKET SIDE LOAD SUPPORT BOSS. RE-WO RKED OUTBOARD FLAP OUTBOARD HINGE SIDE LOAD SUPPORT BOSS BORES PER CMM 57-44-09 AND ESO'S 7327 AND 7349 DATED 6-10-98. T ST: 96,680.24 HOURS. CYCLES: 18,100. (X) 2 L 7 3 4F A22WE 1998082100168 19980821 00168 WP 1998 8 21 AALA981098 1 19980530 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887-1897 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - CORROSION ON AFT END OF LAVATORY F SUPPORT. INSTALLED FABRICATED LUG PER SRM 53-60-01 AND DOUBLER PER SRM 53-60-0 1. TST: 96,680.24 HOURS. CYCLES: 18,100. (X) 2 L 7 3 4F A22WE 1998082100169 19980821 00169 WP 1998 8 21 AALA981099 1 19980530 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887-1897 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 137AA 47847 TUL - FLOORBOARD SUPPORT HAS CORROSION AT 1887-1897 APPROXIMATELY 40 INCHES RIGHT OF CENTERLINE. INSTALLED FABRICATED R EPAIR PER SRM 53-60-01 AND DOUBLER PER SRM 53-60-01. TST: 96,680.24 HOURS. CYCLES: 18,100. (X) 2 L 7 3 4F A22WE 1998082100170 19980821 00170 NM 1998 8 21 AALA981249 1 19980619 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - CORROSION ALONG DOME NUT. STA 720B TO STA 720C. CUT OUT CORROSION AND INSTALLED FLUSH REPAIR PER 53-30-3. TST: 68,331. CYCLES: 45,099. (X) 2 L 7 3 4F A3WE 1998082100171 19980821 00171 NM 1998 8 21 AALA981248 1 19980527 A 5330 SKIN BOEING 727 727227 1384078 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - CORROSION ON EXTERIOR OF BELLY SKIN AT FS 680 AT STR 27R. REPAIRED EXTERIOR BELLY SKIN AT FS 680 AT STR 27R PER S RM 53-30-3 FIG 3A. TST: 68,331. CYCLES: 45,099. (X) 2 L 7 3 4F A3WE 1998082100172 19980821 00172 NM 1998 8 21 AALA981247 1 19980608 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1166-1183 DELAMINATED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FUSELAGE SKIN DELAMINATION AROUND AFT LAVATORY SERVICE PANEL CUT-OUT AS SEEN FROM INSIDE AFT CARGO. REPAIRED PER ESO 11697 DATED JUNE 3, 1998. TST: 68,331. CYCLES: 45,099. (X) 2 L 7 3 4F A3WE 1998082100173 19980821 00173 NM 1998 8 21 AALA981246 1 19980619 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - STR 15L CRACKED JUST AFT OF ICE LIGHT. REPAIRED PER SRM 53-10-3 FIG 5. FINISHED INSTALLING FASTENERS. TST: 68, 331. CYCLES: 45,099. (X) 2 L 7 3 4F A3WE 1998082100174 19980821 00174 NM 1998 8 21 AALA981311 1 19980703 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - STRINGER CRACKED 15L STA 720B FORWARD OF ICE LIGHT HOUSING AT END OF STRINGER. REPAIRED STR 15L FORWARD OF ICE LI GHT STA 720B PER SRM 53-10-3. TST: 70,062 HOURS. CYCLES: 49,889. (X) 2 L 7 3 4F A3WE 1998082100175 19980821 00175 NM 1998 8 21 AALA981310 1 19980703 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - STRINGER CRACKED 15L STA 720C AFT SIDE OF ICE LIGHT AT END OF STRINGER. REPAIRED STR 15 LT AFT SIDE OF ICE LIGHT STA 720C PER SRM 53-10-3. TST: 70,062 HOURS. CYCLES: 49,889. (X) 2 L 7 3 4F A3WE 1998082100176 19980821 00176 NM 1998 8 21 AALA981309 1 19980703 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - TOP AFT STRINGER CRACKED, STA 656.56 AT FLANGE HOLE. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER SB 727-57 A 159 REV 5. TST: 70,062 HOURS. CYCLES: 49,889. (X) 2 L 7 3 4F A3WE 1998082100177 19980821 00177 NM 1998 8 21 AALA981308 1 19980703 A 5320 WEB BOEING 727 727227 1384078 NM BS 874 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - TWO EACH CRACKS IN WEB SKIN FORWARD END RT APU CUT-OUT. STOP DRILLED CRACKS. INSTALLED REPAIR DOUBLER IAW SRM 51 -40-2. TST: 70,062 HOURS. CYCLES: 49,889. (X) 2 L 7 3 4F A3WE 1998082100178 19980821 00178 NM 1998 8 21 AALA981307 1 19980703 A 5320 ANGLE BOEING 727 727227 1384078 NM BS 950 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - NR 2 CARGO DOOR FRAME UPPER CHORD ANGLE WORN AND CRACKED JUST AFT STR 26R (MARKED) (FORWARD EDGE OF DOOR). STOP D RILLED CRACK, FABRICATED DOUBLER REPAIR AND INSTALLED IAW SRM 51-40-4. (X) 2 L 7 3 4F A3WE 1998082100179 19980821 00179 NM 1998 8 21 AALA981306 1 19980619 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1130-1150 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - SKIN DENTED AND GOUGED BETWEEN STA 1130 - STA 1150, STR 3R - STR 4R (DUE TO DOCK STRIKE). INSTALLED REPAIR DOUBLE R PER SRM 53-30-3 CUTTING OUT DAMAGE AND INSTALLING FILLER WITH SCAB EXT DOUBLER. (X) 2 L 7 3 4F A3WE 1998082100180 19980821 00180 NM 1998 8 21 AALA981305 1 19980703 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1143-1149 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - RIVETS PULLING THROUGH, HEADS CRACKED, STA 1143 TO STA 1149, STR 23L, 4 EACH FASTENERS. FOUND CORROSION BETWEEN D OUBLER SKIN (WHEN REMOVING FASTENERS). REMOVED CORROSION, REPAIRED AREA, INSTALLED DOUBLER AND TRIPLER PER ECO 11697 DA TED 6-24-98, REVISED 6-25-98. TST: 70,062 HOURS. CYCLES: 49,889. (X) 2 L 7 3 4F A3WE 1998082100181 19980821 00181 WP 1998 8 21 CALA9801448 1 19980812 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A 1 CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. A NEW BEAM WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082100182 19980821 00182 NM 1998 8 21 CALA9801449 1 19980813 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 760 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 5/8 CRACK IN OUTBOARD END OF FLOORBOARD SUPPORT AT BS 760, RBL 45.5. THE FLOORBOARD SUPPORT WAS REMO VED AND REPLACED IAW SRM 51-30-5 AND 51-30-2. 2 L 7 3 4F A3WE 1998082100183 19980821 00183 NM 1998 8 21 CALA9801450 1 19980813 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 8 TE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND APPROXIMATELY A 2 CRACK IN RT WING NR 8 FLAP TRACK INBOARD TRAILING EDGE ATTACH ANGLE. A NEW ATTACH AN GLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100184 19980821 00184 NM 1998 8 21 CALA9801451 1 19980813 A 5730 ACCESS PLATE BOEING 727 727232 1384082 NM CENTER WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND WING CENTER SECTION LOWER SKIN PLENUM ASSEMBLY INSPECTION ACCESS PLATE CORRODED ON FORWARD RT SIDE. A NEW ACCESS PLATE WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-10-2, 51-20-1, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100185 19980821 00185 NM 1998 8 21 CALA9801452 1 19980813 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND APPROXIMATELY A 2 CRACK IN LT WING LEADING EDGE SLAT NR 2 INBOARD SLAT TRACK OUTBOARD SIDE L ANGLE. TH E ANGLE WAS REPLACED IAW SRM 57-30-4, 51-20-12, AND 51-30-2. 2 L 7 3 4F A3WE 1998082100186 19980821 00186 WP 1998 8 21 CALA9801453 1 19980814 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1289 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND A 2 CRACK IN FLOORBEAM AT STA 1289 ADJACENT TO L-3 DOOR THRESHOLD. THE CRACKED AREA WAS TRIMMED OUT. A NEW FLOORBEAM SECTION WITH SPLICE CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998082100187 19980821 00187 WP 1998 8 21 CALA9801454 1 19980814 A 5532 SKIN DOUG DC10 DC1010 3022110 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68043 46902 INSPECTION FOUND A 1 CRACK IN LOWER VERTICAL STABILIZER SKIN (NR 2 ENGINE INTAKE DUCT). THE AREA WAS REPAIRED IAW ECRA 5530-01213 AND A DIP WAS ISSUED TO PERFORM A VISUAL INSPECTION OF THE REPAIR IAW PART 2 OF ECRA 5530-01213 AT EVERY C CH ECK. 2 L 7 3 4F A22WE 1998082100188 19980821 00188 SO 1998 8 21 COMA9810173 1 19980807 A 2130 720159001410 INDICATOR EMB 120 EMB120RT SO COCKPIT MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 248CA 17270 4356 120228 PRESSURIZATION SYSTEM DOES NOT WORK. REPLACED THE CABIN PRESSURE TRIPLE INDICATOR. 2 L 7 2 4T RT A31SO 1998082100189 19980821 00189 1998 8 21 COMA9810174 4 19980809 A 3425 6227711003 DPU EMB 120 EMB120RT SO RT COCKPIT FAILED A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 463CA 18453 120267 CO-PILOTS EAD1 AND EHS1 FAILED DURING TAKEOFF. REPLACED THE DPU-86H. 2 L 7 2 4T RT A31SO 1998082100190 19980821 00190 SO 1998 8 21 COMA9810175 1 19980811 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 256CA 120245 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN ASSY. 2 L 7 2 4T RT A31SO 1998082100191 19980821 00191 SO 1998 8 21 COMA9810176 1 19980810 A 2150 1945463 HEAT EXCHANGER EMB 120 EMB120RT SO LT ACM SMOKING A COMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 189CA 21660 1187 120189 SMOKE FILLED COCKPIT AND CABIN DURING BOARDING. REPLACED THE LEFT ACM HEAT EXCHANGER. 2 L 7 2 4T RT A31SO 1998082100192 19980821 00192 EA 1998 8 21 COMA9860217 1 19980808 A 3020 CONNECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED A COMA O OTHER M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 01 935CA 7043 DURING CRUISE FLIGHT, THE LEFT COWL ANTI-ICE CAUTION MESSAGE CAME ON. THE BLEED AIR CONNECTION AT THE THRUST REVERSER M OTOR CAME OFF CAUSING EXTENSIVE HEAT DAMAGE TO ENGINE AND COWLING. REPLACED ENGINE AND COWLING. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082100193 19980821 00193 EA 1998 8 21 COMA9860218 1 19980809 A 7897 WIRE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE CHAFED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 935CA 1 7043 LEFT ENGINE THRUST REVERSER UNLOCKED MESSAGE AFTER TAKEOFF. REPAIRED CHAFED WIRE AT CONNECTOR P28EZ. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082100194 19980821 00194 EA 1998 8 21 COMA9860219 1 19980808 A 3230 PIN CNDAIR CL600 CL6002B19 EA LANDING GEAR INSTALLED A COMA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 01 976CA 7151 LANDING GEAR DISAGREE MESSAGE AFTER TAKEOFF. REMOVED DOWN LOCK SAFETY PIN. 2 L 7 2 4F RT A21EA 1998082100195 19980821 00195 EA 1998 8 21 COMA9860220 1 19980812 A 5240 H50002064115 LATCH CNDAIR CL600 CL6002B19 EA OXY SERVICE DR BROKEN A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 973CA 7146 LOUD UNUSUAL NOISE IN COCKPIT. STALL FAIL/MESSAGE ON EICAS. REPLACED BROKEN LATCH ON OXYGEN SERVICE DOOR. 2 L 7 2 4F RT A21EA 1998082100196 19980821 00196 NM 1998 8 21 98FDEA00505 1 19980811 A 5320 6516340 SHEAR TIE BOEING 727 727227 1384078 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION (C53-113-02) SHEAR TIE AT BS 990, RBL 2, WL 138. *S/D* REPAIRED SHEAR TIE AT 990, RBL 2, WL 138 PER FED-EX S RM 53-10-4. 2 L 7 3 4F A3WE 1998082100197 19980821 00197 NM 1998 8 21 98FDEA00506 1 19980812 A 3610 652244143 DUCT BOEING 727 727233 138408A NM NR 3 ENGINE FAILED A FDEA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 25 274FE 22039 98-203 AFTER T/O NR 3 FIRE WARN LIGHT CAME ON. SHUT DOWN NR 3 ENGINE. NR 3 FIRE LOOPS TEST GOOD. FND APPROX 1.75 CRA CK IN THE 13TH STAGE SADDLE DUCT ON NR 3 ENG AT CTR BOOSTER. REMOVED AND REPLACED DUCT PER BAC OHM 71-02-01 PG 578J, LE AK CHECKED DUCT CK OK. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998082100198 19980821 00198 WP 1998 8 21 98FDEA00507 1 19980812 A 5245 STRIKER DOUG DC10 DC1010F 3022111 WP AC DOOR OUT OF ADJUST A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 050FE 47804 A/C DOORS CAUTION LT ILLUM IN FLT FOR 25 SEC. FOLLOW RED TABS AND DIVERTED TO DEN. T/S SYS VERF SWITCH OPS, RELAY FUNC TION AND WIRING, NO PROBLEM FOUND. STRIKER PLATE THROW ON RIGHT DOOR OUT OF LIMITS. ADJUSTED STRIKER PER M/M 52-42-01- 2. DOOR OPS AND LIGHT IND NORMAL. REMOVED MEL NR 39037. 2 L 7 3 4F A22WE 1998082100199 19980821 00199 NM 1998 8 21 VNAA9808010 1 19980806 A 6120 DOLN511F07SND01 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 459PS 3070 THE LEFT PROPELLER OVERSPEED TEST FAILED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTEN ANCE INSPECTED AND REPLACED THE LEFT PROPELLER OVERSPEED GOVERNOR CANNON PLUG, IN ACCORDANCE WITH DORNIER MAINTENANCE MA NUAL 61-01-03. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100200 19980821 00200 NM 1998 8 21 VNAA9808012 1 19980812 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE BIRD STRIKE A VNAA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 GL 07 431JS 3028 THE CREW REPORTED THAT A BIRD STRIKE OCCURRED ABOVE THE F/O'S FORWARD WINDOW, DURING TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND CLEANED UP THE REMAINS OF THE BIRD, IN ACCORDA NCE WITH DORNIER MAINTENANCE MANUAL 52-11-02. NO DAMAGE WAS NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100201 19980821 00201 1998 8 21 VTZA98232 4 19980630 A 3418 601RS20221 SENSOR CNDAIR CL600 CL6002B19 EA E/E BAY FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 623BR 7192 IAD/BNA - FLT 6702 - DURING CLIMB, AT 1300 HRS ON 6-30-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING DUE TO LT AOA WARNING LI GHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED AO A SENSOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998082100202 19980821 00202 EU 1998 8 21 VTZA98231 1 19980630 A 2621 330000103 FIRE BOTTLES JETAIR JETSTM JETSTM4101 1500501 EU RT/LT ENGINE FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 319UE 41042 EWR/IAD - FLT 6468 - DURING TAXI AT 0740 HRS ON 6-30-98, AIRCRAFT RETURNED TO GATE DUE TO RT ENGINE FIRE INDICATION. MA INTENANCE INSPECTED AND FOUND BAD RT ENGINE ZONE 1 FIRE LOOP. MAINTENANCE REMOVED AND REPLACED RT ENGINE FIRE LOOP AND BOTH FIRE BOTTLES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: OPER CONTROL NR 98ZZ ZX2833. (X) 2 L 7 2 4T RT A41NM 1998082100203 19980821 00203 EU 1998 8 21 98ZZZX2833 1 19980630 A 2612 D2370240 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 319UE 41042 EWR/IAD - FLT 6468 - DURING TAXI AT 0740 HRS ON 6-30-98, AIRCRAFT RETURNED TO GATE DUE TO RT ENGINE FIRE INDICATION. MA INTENANCE INSPECTED AND FOUND BAD RT ENGINE ZONE 1 FIRE LOOP. MAINTENANCE REMOVED AND REPLACED RT ENGINE FIRE LOOP AND BOTH FIRE BOTTLES. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. REF: OPER CONTROL NR VTZA 98231. 2 L 7 2 4T RT A41NM 1998082100204 19980821 00204 EU 1998 8 21 VTZA98229 1 19980628 A 5270 91SE13 SWITCHES BAG JETSTM JETSTM3201 1500217 EU PASSENGER DOOR DIRTY A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 497UE 904 EWR/IAD - FLT 6461 - DURING CRUISE AT 2100 HOURS ON 6-28-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT EWR DUE PASSENGER D OOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DM I 56397, MEL 52-2. MAINTENANCE CLOSED DMI 56397 ON 6-29-98 BY CLEANING AND LUBING ALL MICROSWITCHES ON PASSENGER DOOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100205 19980821 00205 EU 1998 8 21 VTZA98227 1 19980629 A 3230 9005EN38 DOWNLOCK BAG JETSTM JETSTM3201 1500217 EU LT MLG DIRTY A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 494UE 810 JFK/BOS - FLT 6478 - DURING APPROACH AT 1020 HOURS ON 6-29-98, AIRCRAFT MADE A SCHEDULED LANDING AT BOS WITH ONE DISCREP ANCY WHICH WAS LT GEAR DOWNLOCK INDICATION FLICKERS ON AND OFF. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTE NANCE INSPECTED AND CLEANED DOWNLOCK SYSTEM AND COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT RELEASED AND RETUR NED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100206 19980821 00206 1998 8 21 VTZA98225 4 19980625 A 2211 7003360948 AHRS COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 321UE 41045 IAD/MBT - FLT 6388 - DURING CRUISE AT 0945 HRS ON 6-25-98. AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 2 AHRS FAILED . AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTION AND REMOVED AND REPLACED NR 2 AHRS COMPU TER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1998082100207 19980821 00207 1998 8 21 VTZA98221 4 19980622 A 6122 8210263 GOVERNOR BAG JETSTM JETSTM3201 1500217 EU LT PROP FLUCTUATION A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 EA 27 472UE 823 PHL/IAD - FLT 6614 - AT 1540 HOURS ON 6-22-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING DUE TO LT ENGINE FLUCTUATION. CREW SHUT DOWN LT ENGINE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED PROPELLER GOVERNOR. OPS CHECK OK. AIRCRAFT WAS RE LASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100208 19980821 00208 EU 1998 8 21 VTZA98222 1 19980624 A 2750 AIR87390 VALVE BAG JETSTM JETSTM3201 1500217 EU TE FLAPS FAILED A VTZA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 EA 27 482UE 897 BOS/SWF - FLT 6584 - DURING CLIMB AT 0910 HOURS ON 6-24-98, MADE AN UNSCHEDULED LANDING DUE TO FLAPS DROOPING IN-FLIGHT (UNCONTROLLED). AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLA P SELECTOR VALVE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100209 19980821 00209 1998 8 21 VTZA98224 4 19980624 A 3418 C771075 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT/RT WINGS OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 496UE 900 IAD - FLT 6243 - DURING CLIMB AT 6243 HOURS ON 6-24-98, AIRCRAFT MADE AN UNSCHEDULED LANDING AT IAD DUE TO LT STALL WARN ING AND STICK SHAKER INTERMITTENT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUS TED LIFT TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100210 19980821 00210 EU 1998 8 21 VTZA98230 1 19980629 A 2120 13792471 DUCT BAG JETSTM JETSTM3201 1500217 EU CABIN LOOSE A VTZA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 EA 27 471UE 821 IAD/JFK - FLT 6193 - DURING TAXI AT 0730 HOURS ON 6-29-98, AIRCRAFT RETURNED TO GATE DUE TO SMOKE IN COCKPIT. MAINTENAN CE INSPECTED AND FOUND LOOSE DUCT AT ROW 1A AND 2A GIVING OFF WATER CONDENSATION. MAINTENANCE RESECURED DUCT. OPS CHEC K OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100211 19980821 00211 EU 1998 8 21 SIMA981842 1 19980703 A 5220 13S52277001000A0 SADDLE AEROSP ATR42 ATR42300 8680920 EU EMERG EXIT DOOR BROKEN A SIMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 21 424MQ 1099 045 ORD - FLT 4094 - DURING TAKE OFF, THE LEFT EMERGENCY EXIT DOOR AT ROW 1 FELL INTO THE CABIN. FOUND THE LEFT HAND SADDLE BROKEN ON THE EXIT DOOR. REMOVED AND REPLACED LEFT HAND EMERGNECY EXIT DOOR AT ROW 1. ACFT TT: 23,440.1 HOURS. ACFT TC: 30,310. (X) 2 H 7 2 4T RT A53EU 1998082100212 19980821 00212 EU 1998 8 21 VTZA98218 1 19980610 A 2620 330000103 EXTINGUISHER BAG JETSTM JETSTM3201 1500217 EU NR 2 ENGINE MALFUNCTIONED A VTZA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 EA 27 485UE 901 RDU/IAD - FLT 6358 - DURING CRUISE AT 1,300 HOURS ON 6-10-98, MADE A SCHEUDLED LANDING WITH ONE DISCREPANCY WHICH WAS NR 2 ENGINE FIRE BOTTLE INADVERTENLY ACTIVATED IN-FLIGHT. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE IN SPECTED AND REMOVED AND REPLACED NR 2 FIRE BOTTLE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100213 19980821 00213 NE 1998 8 21 VTZA98214 2 19980607 A 7260 5725109162 DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RT ENGINE MALFUNCTIONED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 310UE 41028 BOS/IAD - FLT 6218 - DURING TAKEOFF AT 1800 HRS ON 6-7-98, ABORTED TAKEOFF DUE TO RT ENGINE OIL CONTAMINATION WARNING LI GHT ILLUMINATED. AIRCRAFT RETURNED TO GATE AT BOS WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND NO METAL O N CHIP DETECTOR THEN CLEANED AND REINSTALLED, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERIVCE. ( X) 2 L 7 2 4T 4 T RT A41NM E18NE 1998082100214 19980821 00214 EU 1998 8 21 VTZA98226 1 19980628 A 2422 HB3501B13 INVERTER BAG JETSTM JETSTM3201 1500217 EU E/E BAY FAILED A VTZA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 EA 27 492UE 790 IAD/PHL - FLT 6237 - DURING CRUISE AT 1314 HOURS ON 6-28-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING AT IAD DUE TO INVERTER FAIL WARNING LIGHT IN-FLIGHT. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED A ND REPLACED INVERTER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998082100215 19980821 00215 NM 1998 8 21 TWRA9836 1 19980616 A 3610 CLAMP BOEING 747 747136 1384883 NM NR 4 PDU LOOSE A TWRA K NONE M OVER TEMP DE DESCENT 1 EA 15 606FF 20273 AT START OF DESCENT TO SJU FROM FL 37,000 FEET, THRUST LEVER AT IDLE, LEFT WING OVERHEAT LIGHT CAME ON. ABNORMAL PROCED URES FOR WING OVERHEAT COMPLETED, LIGHT WENT OUT AFTER 8 MINUTES. THRUST LEVER AT IDLE, SYSTEM NORMAL AND LIGHT NEVER C AME BACK ON. FOUND LOOSE CLAMP ON NR 4 PDU LT WING. TIGHTENED CLAMP, LEAK CHECK OK PER MM 26-18-00, PAGE 101. (X) 2 L 7 4 4F A20WE 1998082100216 19980821 00216 NM 1998 8 21 TAOA079801 1 19980701 A 7714 8DJ81LWM2 INDICATOR GE BOEING 727 727225 1384077 NM COCKPIT N1 TACH MALFUNCTIONED A TAOA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 15 918TS Z4610 20445 LGA/BOS - FLT 6040 - NR 1 THROTTLE WAS AGAINST THE FORWARD STOP AND N1 WAS BELOW TAKEOFF POWER SETTING. NEEDED 93.3 PER CENT AND HAD 89.6 PERCENT. TAKEOFF ABORTED AT 95 KNOTS. CHANGED NR 1 ENGINE N1 TACHOMETER PER MM 77-12-0, RAN ENGINE PER 71-00-57, CHECKED OK. EPR SYSTEM TO CONTINUE ON CONTROL ITEM M847709. (X) 2 L 7 3 4F A3WE 1998082100217 19980821 00217 NM 1998 8 21 TAOA079802 1 19980703 A 2782 1U11032 ACTUATOR RONSON BOEING 727 727225 1384077 NM NR 3 LE SLAT LEAKING A TAOA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 EA 15 918TS 72 20445 BOS/LGA - FLT 6101 - LOST HYDRAULIC FLUID A-SYSTEM ON TAXI OUT. REPLACED NR 3 SLT ACTUATOR PER MM 27-81-32. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (X) 2 L 7 3 4F A3WE 1998082100218 19980821 00218 EU 1998 8 21 SIMA981822 1 19980702 A 3240 MS287786 O-RING SAAB SF340 340B 7860101 EU RT BRAKE DAMAGED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 272AE 340B272 DFW - FLT 3576 - REQUIRES A LOT OF RIGHT FOOT PRESSURE TO GET THE RIGHT BRAKES TO ACTIVATE. SEEMS AT TIMES THERE IS LIT TLE OR NO RIGHT BRAKE. REMOVED AND REPLACED CUT O-RING ON NR 4 BRAKE BLEED PORT TO HOUSING FITTING. BLED RIGHT BRAKE A SSY. LEAK AND OPERATIONAL CHECK NORMAL. (X) 2 L 7 2 4T RT A52EU 1998082100219 19980821 00219 NM 1998 8 21 EIAA980230 1 19980716 A 3310 LIGHT BOEING 747 747273C 1384896 NM COCKPIT SMOKING A EIAA K NONE O OTHER NR NOT REPORTED 1 NM 09 470EV 20653 KWRA - LOG PAGE: F67062 - CAPTAIN'S FLUORESCENT LIGHT ON GLARE SHIELD SMOKING WITH POWER ON. TRANSPORTED TO DMI 260 PE R MEL 33-1 CAT C DUE 7-25-98. CAPTAIN'S FLUORESCENT LIGHT CIRCUIT BREAKER PULLED. (X) 2 L 7 4 4F A20WE 1998082100220 19980821 00220 EU 1998 8 21 SIMA981982 1 19980717 A 5320 S5367121729402 SILL PLATE AEROSP ATR72 ATR72212 EU PASSENGER DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PASSENGER DOORSILL PLATE AND COVER PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH PLATES IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX2834 . ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. (X) 2 H 7 2 4T RT A53EU 1998082100221 19980821 00221 EU 1998 8 21 98ZZZX2834 1 19980717 A 5320 S5367121729602 COVER PLATE AEROSP ATR72 ATR72212 EU PASSENGER DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PASSENGER DOORSILL PLATE AND COVER PLATE CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH PLATES IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. REF: OPER CONTROL NR SIMA981982. 2 H 7 2 4T RT A53EU 1998082100222 19980821 00222 EU 1998 8 21 SIMA981983 1 19980717 A 5210 S5217620420602 PAN AEROSP ATR72 ATR72212 EU PASSENGER DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PASSENGER DOOR UPPER PAN CORRODED. MAINTENANCE REMOVED AND REP LACED THE PAN IAW SRM 52-11-00. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. (X) 2 H 7 2 4T RT A53EU 1998082100223 19980821 00223 EU 1998 8 21 SIMA981984 1 19980717 A 5320 S5367131828001 SILL PLATE AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND DRAIN GULLEY CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL PLATE AND DRAIN GULLEY IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER C ONTROL NR 98ZZZX2835. ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. (X) 2 H 7 2 4T RT A53EU 1998082100224 19980821 00224 EU 1998 8 21 98ZZZX2835 1 19980717 A 5320 S536712172801 DRAIN GULLEY AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE SERVICE DOOR SILL PLATE AND DRAIN GULLEY CORRODED. MAINTENANCE REMOVED AND REPLACED THE SILL PLATE AND DRAIN GULLEY IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 11 ,704.9 HOURS. ACFT TC: 12,665. REF: OPER CONTROL NR SIMA981984. 2 H 7 2 4T RT A53EU 1998082100225 19980821 00225 EU 1998 8 21 SIMA981985 1 19980717 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, LEFT AFT INBOARD AND THE LEFT MIDDLE OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS IAW SRM 51-25-04. MAINTENANCE REPAIRED THE LEFT MIDDLE OUTBOARD SEAT TRACK IAW SRM 53-00-00, F IGURE 434. AIRCRAF RETURNED TO SERVICE. REF: OPER CACFT TT: 11704.9 HOURS. ACFT TC: 12,665. CONTROL NR 98ZZZX____ THROUGH 98 ZZZX____. (X) 2 H 7 2 4T RT A53EU 1998082100226 19980821 00226 EU 1998 8 21 98ZZZX2836 1 19980717 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, LEFT AFT INBOARD AND THE LEFT MIDDLE OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS IAW SRM 51-25-04. MAINTENANCE REPAIRED THE LEFT MIDDLE OUTBOARD SEAT TRACK IAW SRM 53-00-00, F IGURE 434. AIRCRAF RETURNED TO SERVICE. OPER ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. REF: CONTROL NR SIMA98198- 5 , AND, 98ZZZX____ THROUGH 98 ZZZX____. 2 H 7 2 4T RT A53EU 1998082100227 19980821 00227 EU 1998 8 21 98ZZZX2837 1 19980717 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, LEFT AFT INBOARD AND THE LEFT MIDDLE OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS IAW SRM 51-25-04. MAINTENANCE REPAIRED THE LEFT MIDDLE OUTBOARD SEAT TRACK IAW SRM 53-00-00, F IGURE 434. AIRCRAF RETURNED TO SERVICE. ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. REF: OPER CONTROL NR SIMA98198- 5 , AND, 98ZZZX____ THROUGH 98 ZZZX____. 2 H 7 2 4T RT A53EU 1998082100228 19980821 00228 EU 1998 8 21 98ZZZX2838 1 19980717 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT FLIGHT ATTENDANT, RIGHT FLIGHT ATTENDANT, LEFT AFT INBOARD AND THE LEFT MIDDLE OUTBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED BOTH FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS IAW SRM 51-25-04. MAINTENANCE REPAIRED THE LEFT MIDDLE OUTBOARD SEAT TRACK IAW SRM 53-00-00, F IGURE 434. AIRCRAF RETURNED TO SERVICE. ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. REF: OPER CONTROL NR SIMA98198- 5 , AND, 98ZZZX____ THROUGH 98 ZZZX____. 2 H 7 2 4T RT A53EU 1998082100229 19980821 00229 EU 1998 8 21 SIMA981986 1 19980717 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36 CORRODED. MAINTENANCE REMOVED AND REPLACED FLOORBEAM 36 IAW SRM 51-25-02. AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 11,704.9 HOURS. ACFT TC: 12,665. (X) 2 H 7 2 4T RT A53EU 1998082100230 19980821 00230 NM 1998 8 21 EIAA980219 1 19980701 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 440 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 73644 20653 HKG - DURING B-CHECK, BS 440 UPPER DECK FLOORBEAM WAS FOUND CRACKED AT THE UPPER CHORD, LEFT OUTBOARD END RUNNING INBOAR D .040 INCH. ACCOMPLISHED TIME LIMITED REPAIR, PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 18 MONTHS OR 1500 CYCLES, W HICHEVER COMES FIRST PER TELEX EVR-HKG-98-0091TE, AD 98-09-17, ECRA 470-53-98-1 GENERATED TO TRACK REPAIR. (M) 2 L 7 4 4F A20WE 1998082100231 19980821 00231 WP 1998 8 21 98ZZZX2839 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 37, BS 419. REF: OPER CONTROL NR EIAA980214, AND, 98ZZ ZX2840 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100232 19980821 00232 WP 1998 8 21 98ZZZX2840 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 37, BS 510. REF: OPER CONTROL NR EIAA980214, AND, 98ZZ ZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100233 19980821 00233 WP 1998 8 21 98ZZZX2841 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 37, BS 601. REF: OPER CONTROL NR EIAA980214, AND, 98ZZ ZX2839 THROUGH 2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100234 19980821 00234 WP 1998 8 21 98ZZZX2842 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 37, BS 792 REF: OPER CONTROL NR EIAA980214, AND, 98ZZZ X2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100235 19980821 00235 WP 1998 8 21 98ZZZX2843 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 37, BS 983. REF: OPER CONTROL NR EIAA980214, AND, 98ZZ ZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100236 19980821 00236 WP 1998 8 21 98ZZZX2844 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 37, BS 1074. REF: OPER CONTROL NR EIAA980214, AND, 98Z ZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100237 19980821 00237 WP 1998 8 21 98ZZZX2845 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 37, BS 1165. REF: OPER CONTROL NR EIAA980214, AND, 98Z ZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100238 19980821 00238 WP 1998 8 21 98ZZZX2846 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 16.25, BS 419. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100239 19980821 00239 WP 1998 8 21 98ZZZX2847 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 16.25, BS 510. REF: OPER CONTROL NR EIAA980214, AND, 98ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100240 19980821 00240 WP 1998 8 21 98ZZZX2848 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 16.25, BS 601. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100241 19980821 00241 WP 1998 8 21 98ZZZX2849 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 16.25, BS 792. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100242 19980821 00242 WP 1998 8 21 98ZZZX2850 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 16.25, BS 983. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100243 19980821 00243 WP 1998 8 21 98ZZZX2852 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN LBL 16.25, BS 1165. REF: OPER CONTROL NR EIAA980214, AND, 98ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100244 19980821 00244 WP 1998 8 21 98ZZZX2853 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 8.5, BS 510. REF: OPER CONTROL NR EIAA980214, AND, 98Z ZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100245 19980821 00245 WP 1998 8 21 98ZZZX2854 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 8.5, BS 601. REF: OPER CONTROL NR EIAA980214, AND, 98Z ZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100246 19980821 00246 WP 1998 8 21 98ZZZX2855 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 8.5, BS 792. REF: OPER CONTROL NR EIAA980214, AND, 98Z ZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100247 19980821 00247 WP 1998 8 21 98ZZZX2856 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 8.5, BS 983. REF: OPER CONTROL NR EIAA980214, AND, 98Z ZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100248 19980821 00248 WP 1998 8 21 98ZZZX2857 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 8.5, BS 1165. REF: OPER CONTROL NR EIAA980214, AND, 98 ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100249 19980821 00249 WP 1998 8 21 98ZZZX2858 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 33.25, BS 237. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100250 19980821 00250 WP 1998 8 21 98ZZZX2859 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 33.25, BS 328. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100251 19980821 00251 WP 1998 8 21 98ZZZX2860 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 33.25, BS 510. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100252 19980821 00252 WP 1998 8 21 98ZZZX2861 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 33.25, BS 792. REF: OPER CONTROL NR EIAA980214, AND, 9 8ZZZX2839 THROUGH 98ZZZX2862. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100253 19980821 00253 WP 1998 8 21 98ZZZX2862 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 328-1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACKS WERE FOUND WORN IN RBL 33.25, BS 1165. REF: OPER CONTROL NR EIAA980214, AND, 98ZZZX2839 THROUGH 98ZZZX2861. REPAIRED SEAT TRACKS PER SRM 53-05 FIGURE 4A. 2 L 7 2 4F A6WE 1998082100254 19980821 00254 WP 1998 8 21 TWAA9813001 1 19980815 A 3350 58222 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 927TW 49358 EMERGENCY ESCAPE PATH LIGHTS WERE ON WITH SWITCH SELECTED TO ARM POSITION. LIGHTS WERE ON FROM OVERWING EXIT TO REAR G ALLEY RT SIDE. REPLACED NR 3 EGRESS LIGHT BATTERY PACK. CHECK-C 12-10-97 MCI. 2 L 7 2 4F RT A6WE 1998082100255 19980821 00255 NM 1998 8 21 RAAA98B1087 1 19980806 A 3350 1000679 LIGHT BOEING 727 72722C 138400F NM VENTRAL STAIR FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 VENTRAL STAIR OVERHEAD EMERGENCY EXIT LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED AND WATER CONTAMINATIO N AND CHANGED 2 BATTERIES DUE LOW CHARGE. 2 L 7 3 4F A3WE 1998082100256 19980821 00256 NM 1998 8 21 RAAA98B1088 1 19980814 A 3350 873100212 SIGN BOEING 727 72722C 138400F NM CABIN BROKEN A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 FOUND FWD LT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT COVER BROKEN ON SERVICE CHECK. CHANGED LIGHT ASSY DUE COVER BROKEN. 2 L 7 3 4F A3WE 1998082100257 19980821 00257 SO 1998 8 21 RAAA98E4018 1 19980813 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 LT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998082100258 19980821 00258 SO 1998 8 21 RAAA98E8025 1 19980815 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 PAX ROW 17 EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998082100259 19980821 00259 SO 1998 8 21 RAAA98E8026 1 19980815 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 AFT LT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT DUE FAILED. 2 L 7 4 4T 4A22 1998082100260 19980821 00260 WP 1998 8 21 UPS98827426 1 19980813 A 3350 LIGHT DOUG DC8 DC873F 302199F WP CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 801UP 46101 EMER EXIT LIGHTS INOP. ALLOWED SUFFICIENT TIME FOR BATTERY PACK TO R-CHARGE, SYS OPS CHK NORMAL. 2 L 7 4 4F RT 4A25 1998082100261 19980821 00261 NM 1998 8 21 UPS98227428 1 19980814 A 2613 OVERHEAT LOOP BOEING 727 72762C 138402C NM ENGINE LOOSE A IPXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 01 912UP 19244 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED DURING FLT. ENGINE WAS SHUTDOWN FOR REMAINDER OF FLIGHT. FOUND BACKSHELL LOOSE ON OVERHEAT LOOP AT STATION NR 48. RAN ENGINE AND OPS CKS OK. 2 L 7 3 4F A3WE 1998082100262 19980821 00262 NM 1998 8 21 UPS98227429 1 19980813 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:SI CORROSION (C53-224-01.05-01) FLOOR BEAM BS 680 WL 208 LBL 2-15. REMOVED CORROSION FOUND OUT OF LIMIT S. REPAIRED PER 51-10-6, 53-10-1, 51-30-02, 53-10-08, 51-10-02, 51-20-15 SRM. 2 L 7 3 4F A3WE 1998082100263 19980821 00263 NM 1998 8 21 UPS98227430 1 19980813 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:SI CORROSION (C53-224-01.05-01), ON FLOORBEAM BS 344 LBL 60 RBL 5 WL 208. REMOVED CORROSION FOUND OUT O F LIMITS REPAIRED IAW SRM 53-10-01, 53-10-08, 51-30-02, 51-20-31. 2 L 7 3 4F A3WE 1998082100264 19980821 00264 NM 1998 8 21 UPS98227431 1 19980814 A 5320 CREASE BEAM BOEING 727 727247 138408F NM BS 418 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:SI CORROSION (C53-224-01.00-01), ON CREASE BEAM AT BS 418 RBL 60 WL 208. REPLACED CREASE BEAM PER 727 S RM 51-30-2. 2 L 7 3 4F A3WE 1998082100265 19980821 00265 NM 1998 8 21 UPS98227432 1 19980811 A 5311 FRAME BOEING 727 727247 138408F NM BS 377 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:SI WHILE WORKING CUST CARD 816656 (INTERIOR 105), FOUND CORROSION ON FRAME AT BS 377 RBL 60 WL 209. REM OVED DAMAGED AREA AND INSTALLED REPAIR PARTS AS PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998082100266 19980821 00266 NM 1998 8 21 UPS98227433 1 19980814 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 EMER EXIT LIGHT FAILED TEST RT OVERHEAD AISLE SEAT ROW 11 DEF PLUS AFT RT OVERWING EXIT DOOR. REMOVED AND REPLACED BATT ERY PACKS OPS OK PART NR 96-2-1033. 2 L 7 3 4F A3WE 1998082100267 19980821 00267 NM 1998 8 21 UPS98227434 1 19980814 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 EMER EXIT LIGHTS FAILED TEST, GALLEY AISLE FWD OVERHEAD LIGHT GALLEY DOOR PLUS LT GALLEY BULKHEAD FWD ENTRY AISLE OVERHE AD. REMOVED AND REPLACED BATTERY PACKS OPS OK PART NR 96-2-1024 96-2-1015. 2 L 7 3 4F A3WE 1998082100268 19980821 00268 NM 1998 8 21 UPS98227435 1 19980814 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 EMER EXIT LIGHTS FAILED TEST, SEAT ROWS NR 6 ABC PLUS 17 ABC FWD BULKHEAD AISLE OVERHEAD 11 DEF. REMOVED AND REPLACED B ATTERY PACKS OPS OK PART NR 96-2-1015. 2 L 7 3 4F A3WE 1998082100269 19980821 00269 NM 1998 8 21 UPS98527427 1 19980813 A 2424 734284F GCU BOEING 757 75724APF 1384969 NM LT GENERATOR MALFUNCTIONED A IPXA O OTHER H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 01 439UP 25470 AT VI INTERMITENT LEFT GEN OFF LIGHT ILLUM. LEFT AC BUSS FAILED, RIGHT BUS DID NOT PICK UP LEFT BUS. SHORLTY THERE AFT ER THE R AC BUS FAILED. MULTIPLE WARNINGS DISPLAYED. RESET R GEN, R BUS POWER BACK ON. FIRED APU L BUS POWERED. SHOR TLY AFTER L BUS POWER WAS INTERMITTENT. RETURNED TO GDL AIRPORT. PERFORMED BPCU BITE TEST AND SHOWED AUX CONTACTS/BPCU /GCU MES. SWAPPED APU GCU TO LEFT GCU. RUN ENGINES AND ATTEMPTED TO DUPLICATE PROBLEM. SYSTEM OPS CK NORMAL. DEFERRE D APU PER MEL. 2 L 7 2 4F RT A2NM 1998082100270 19980821 00270 WP 1998 8 21 UPS98827436 1 19980721 A 5320 9755536501 FITTING DOUG DC8 DC871F 302199D WP BS 1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D LT LWR CUSP FITTING CRACKED STA 1280. REMOVED AND REPLACED FITTING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998082100271 19980821 00271 WP 1998 8 21 UPS98827437 1 19980722 A 5320 3779658502 FITTING DOUG DC8 DC871F 302199D WP BS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D LONG 10L END FITTING CRACKED JUST AFT OF STA 902. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100272 19980821 00272 WP 1998 8 21 UPS98827438 1 19980721 A 5320 9754002122 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D HEAVY CORROSION ON TORQUE BOX VERTICAL SUPPORT ANGLE STA 1220 AT LONG 27L. REMOVED, FABRICATED, AND R EPLACED FITTING IAW DAC DWG 9754002 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100273 19980821 00273 WP 1998 8 21 UPS98827439 1 19980721 A 5320 9755584504 FITTING DOUG DC8 DC871F 302199D WP BS 1325 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D LT LWR CUSP FITTING CRACKED AT STA 1325. REMOVED, FABRICATED, AND REPLACED FITTING IAW DAC DWG 975558 4 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100274 19980821 00274 WP 1998 8 21 UPS98827440 1 19980723 A 5320 47504191 FITTING DOUG DC8 DC871F 302199D WP BS 1228 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE:D STA 1228 AT LONG 19R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D . 2 L 7 4 4F RT 4A25 1998082100275 19980821 00275 1998 8 21 98FDEA00508 2 19980814 A 7261 OIL FITTING BOEING 727 727233 138408A NM NR 3 GEARBOX LOOSE A FDEA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 270FE 22035 98-205 - LOST OIL QTY ON ENG NR 3 IN FLT. SHUT DOWN ENG PER RED TABS. FOUND FITTING LOOSE IN GEARBOX ON OIL LINE RUN T O FILTER BYPASS SWITCH. REMOVED AND REPLACED FITTING AND MAIN ENG OIL SCREEN. RAN NR 3 ENG CKS GOOD. PRESS NORMAL. E NG RUN PER 727 JET RUN HDBK. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998082100276 19980821 00276 NM 1998 8 21 98FDEA00509 1 19980811 A 5312 BULKHEAD BEAM BOEING 727 727233 138408A NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 266FE 21672 NR 0875, BS 1183 BLKD, RBL 36.83, WL 237 VERTICAL BEAM CRACKED BOTH SIDES OF AFT RADIUS. STOP DRILLED CRACK PER SRM 51- 10-1 AND INSTALLED REPAIR DOUBLERS PER DRAWING 65-C34406. 2 L 7 3 4F RT A3WE 1998082100277 19980821 00277 NM 1998 8 21 98FDEA00510 1 19980810 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 990 MISDRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 266FE 21672 NR 0888 - MISDRILLED HOLE IN FLOORBEAM TOP FWD, FLANGE BS 990, RBL 23. INSTALLED DOUBLER, TRIPLER AND FILLER IN ACCORDA NCE WITH AARD 53-10-0702. 2 L 7 3 4F RT A3WE 1998082100278 19980821 00278 NM 1998 8 21 98FDEA00511 1 19980803 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 950 MISDRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 266FE 21672 NR 0887- MISDRILLED HOLE IN FLOORBEAM BS 950E, RBL 26 ON FWD TOP FLANGE. INSTALLED DOUBLER, TRIPLER AND FILLER IN ACCOR DANCE WITH AARD 53-10-07-02. 2 L 7 3 4F RT A3WE 1998082100279 19980821 00279 NM 1998 8 21 98FDEA00512 1 19980805 A 5311 BELLFRAME BOEING 727 727233 138408A NM BS 1010 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 273FE 22038 NR 0546 - LOWER AFT CARGO COMP FS 1010 BELLFRAME BETWEEN STRINGERS 25L AND 26L CREASED. REMOVED DAMAGED AREA. FABRICAT ED DOUBLERS, TREATED, PRIMED AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-4. 2 L 7 3 4F RT A3WE 1998082100280 19980821 00280 WP 1998 8 21 ABXA9800744 1 19980813 A 3350 5708458503 BATTERY PACK DOUG DC8 DC862 3021970 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 804AX 45987 DURING PRE-DEPARTURE CHECK, FOUND THAT COCKPIT EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHTING BATTERY P ACK IAW DC8 MM 33-50-01. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998082100281 19980821 00281 WP 1998 8 21 MWEA98862 1 19980812 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 207ME 47794 FOUND BOTH LEFT AND RIGHT FORWARD EMERGENCY EXIT LIGHTS VERY DIM. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998082100282 19980821 00282 WP 1998 8 21 MWEA98863 1 19980813 A 5313 591142517 LONGERON DOUG DC9 DC932 3022066 WP BS 980 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND LONGERON 30 BENT AT STATION 980. MAINTENANCE FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 1998082100283 19980821 00283 WP 1998 8 21 MWEA98864 1 19980813 A 5320 591015843 DOUBLER DOUG DC9 DC932 3022066 WP CARGO DOOR JAMB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CORROSION ON DOUBLERS AT AFT CARGO DOOR JAMB. MAINTENANCE FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1998082100284 19980821 00284 WP 1998 8 21 MWEA98865 1 19980813 A 5330 5920321501 SKIN DOUG DC9 DC932 3022066 WP BS 345-360 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND CREASES ON FUSELAGE SKIN AT FS 345-360 AND LONGERON 24R. MAINTENANCE FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1998082100285 19980821 00285 WP 1998 8 21 MWEA98866 1 19980813 A 5320 99155047 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 980-996 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND INTERCOSTAL BENT FROM STATION 980 TO 996 AT L28L. MAINTENANCE REMOVED AND REPLACED INTERCOSTAL. 2 L 7 2 4F A6WE 1998082100286 19980821 00286 WP 1998 8 21 MWEA98867 1 19980813 A 5311 995823837 FRAME DOUG DC9 DC932 3022066 WP BS 980 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND BENT FRAME AT STATION 980 AT L26L TO L26R. MAINTENANCE FABRICATED AND INSTALLED SPLICED PARTS. 2 L 7 2 4F A6WE 1998082100287 19980821 00287 WP 1998 8 21 MWEA98868 1 19980813 A 5313 591142515 LONGERON DOUG DC9 DC932 3022066 WP BS 980 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND LONGERON 29L AND 29R BENT AT STATION 980. MAINTENANCE FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 1998082100288 19980821 00288 WP 1998 8 21 MWEA98869 1 19980813 A 5313 59114259 LONGERON DOUG DC9 DC932 3022066 WP BS 985 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND LONGERON 28LC AND 28R DENTED AT STATION 985. MAINTENANCE FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 1998082100289 19980821 00289 WP 1998 8 21 MWEA98870 1 19980813 A 5311 9912243105 FRAME DOUG DC9 DC932 3022066 WP BS 965 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND STATION 965 FRAME BENT FROM L26L TO L26R. MAINTENANCE FABRICATED AND INSTALLED FRAME SPLICES. 2 L 7 2 4F A6WE 1998082100290 19980821 00290 WP 1998 8 21 MWEA98871 1 19980813 A 5313 59114257 LONGERON DOUG DC9 DC932 3022066 WP BS 985 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 FOUND LONGERON 27L AND 27R DENTED AT STATION 985. MAINTENANCE FABRICATED AND INSTALED LONGERON. 2 L 7 2 4F A6WE 1998082100291 19980821 00291 WP 1998 8 21 CKSA98499 1 19980717 A 3260 PIN DOUG DC8 DC861 3021952 WP LT UPLATCH SW NOT SEATED A CKSA K NONE N FALSE WARNING CL CLIMB 1 GL 23 24UA 45963 AFTER GEAR UP DURING CLIMB, LEFT GEAR UNSAFE LIGHT AND GEAR NOT LATCHED LIGHT REMAINED ON. FOLLOWED ABNORMAL PROCEDURES PER FOM. DETERMINED THAT DOOR WAS LATCHED AND GEAR WAS NOT LATCH. FOLLOWED FOM PROCEDURES. FOUND PUSHED PIN AT LEFT GEAR UP LATCH SWITCH RESEATED PIN AS REQUIRED CHECKS NORMAL DC8 MM 32-60. 2 L 7 4 4F 4A25 1998082100292 19980821 00292 WP 1998 8 21 CKSA98504 1 19980717 A 3260 DIODE DOUG DC8 DC861 3021952 WP LT MLG SHORTED A CKSA K NONE N FALSE WARNING CL CLIMB 1 GL 23 24UA 45963 AFTER GEAR UP DURING CLIMB, LEFT GEAR UNSAFE LIGHT AND GEAR NOT LATCHED LIGHT REMAINED ON. FOLLOWED ABNORMAL PROCEDURES PER FOM. DETERMINED THAT DOOR WAS LATCHED AND GEAR WAS NOT LATCHED. FOLLOWED FOM PROCEDURES. TROUBLESHOT WIRING. FO UND DIODE BETWEEN POST 27 AND POST 25 GROUNDING AGAINST RIVET BEHIND TERMINAL STRIP S3-39. TEST OF UPLATCH SYSTEM FAILE D FIRST. OPS CHECK GOOD AFTER REPOSITIONING DIODE. GEAR INDICATIONS OPS CHECK GOOD IAW MM 32-60-0. 2 L 7 4 4F 4A25 1998082100293 19980821 00293 WP 1998 8 21 CKSA98505 1 19980712 A 3260 SWITCH DOUG DC8 DC863F 302198F WP RT MLG DOOR NOT SECURED A CKSA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 811CK 46147 AFTER TAKEOFF FROM MIA, LANDING GEAR FAILED UPLATCH CHECK. MX NOTE: COMPLETED UPLATCH CHECK LIST AND FOUND WHEN LOWERIN G LANDING GEAR RIGHT MAIN GEAR GREEN LIGHT INTERMITTENTLY ON. TROUBLESHOT AND FOUND RT MAIN GEAR DOOR SWITCH NOT SECURE D. SECURED DOOR SWITCH AND PERFORMED LANDING GEAR DOOR AND GEAR UP LIMIT SWITCH. TEST IAW MM DC8 32-60-0. 2 L 7 4 4F 4A25 1998082100294 19980821 00294 WP 1998 8 21 CKSA98506 1 19980811 A 3610 DUCT DOUG DC8 DC861 3021952 WP NR 1 ENGINE MISALIGNED A CKSA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 GL 23 816CK 45892 AT FL330 JUST AFTER LEVEL OFF AND POWER REDUCTION TO CRUISE POWER 3 OF 4 T/C'S: NR 1,2, AND 4 STARTED STALLING AND OVERH EATING, PNEUMATIC SWITCHES WERE ON HIGH, MANIFOLD PRESSURE WAS AT APPROXIMATELY 12 PSI, CABIN CLIMBED OVER 5,000 FEET PE R MINUTE TO 14,000 FEET, MANUAL CONTROLLER WAS FULLY CLOSED, WAS UNABLE TO CONTROL CABIN UNTIL BELOW 22,000 FEET. EMERG ENCY DESCENT ACCOMPLISHED. FOUND LARGE AIR LEAK AT NR 1 ENGINE UPPER PNEUMATIC DUCT REPOSITIONED DUCT AND SECURED CLAMP S NO LONGER LEAKS. ACCOMPLISHED GROUND PRESSURIZATION CHECKS GOOD. 2 L 7 4 4F 4A25 1998082100296 19980821 00296 NM 1998 8 21 AWXA9800088 1 19980330 A 3350 849029 BATTERY BOEING 757 7572S7 1384962 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 904AW 23566 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS ON A/C RIGHT AFT INOP. RESET BATTERY, LIGHT OPS GOOD. 2 L 7 2 4F RT A2NM 1998082100297 19980821 00297 NM 1998 8 21 AWXA9800189 1 19980811 A 5330 SKIN BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 181AW 22648 LEFT FUSELAGE IS CRACKED APPROX 9 INCHES AFT OF WING SCAN LIGHT, CRACK WAS VARIFIED 1.4 INCHES. REPAIRED PER 53-30-03 F IG 1. 2 L 7 2 4F RT A16WE 1998082100298 19980821 00298 WP 1998 8 21 CALA9801455 1 19980814 A 3020 DE-ICE DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE BLOWN A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 35832 49492 717410 THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED DURING CLIMBOUT. THE NR 2 ENGINE WAS RETARDED TO IDLE AND THE FIR E WARNING CEASED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE NOSE COWL ANTI-ICE DUCT BLOWN WITH DAMAGE TO THE UPPER COWL. THE ANTI-ICE DUCT AND UPPER COWL WERE REPLACED. IN ADDIT ION, THE ANTI-ICE VALVE WAS REPLACED DUE TO METAL PARTICLES FOUND IN THE VALVE. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F 4 F A6WE E9NE 1998082100299 19980821 00299 WP 1998 8 21 CALA9801456 1 19980816 A 2611 1024003 SMOKE DETECTOR DOUG DC10 DC1030 3023501 WP CARGO COMPT INOPERATIVE A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 14079 46927 THE AFT CARGO FIRE WARNING LIGHT AND SMOKE DETECTOR LIGHT ILLUMINATED WHILE ENROUTE. EMERGENCY PROCEDURES WERE COMPLIED WITH AND THE LIGHTS EXTINGUISHED. BOTH CARGO FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS DIVERTED TO SJU WHERE I T LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THE MASTER WARNING CONTROLLER WAS REMOVED AND REPLAC ED. THE CARGO FIRE BOTTLES WERE REMOVED AND REPLACED. IN ADDITION, THE AFT CARGO NR 1 SMOKE DETECTOR WAS REMOVED AND R EPLACED. 2 L 7 3 4F A22WE 1998082100300 19980821 00300 WP 1998 8 21 CALA9801457 1 19980814 A 5530 ANGLE DOUG DC9 DC982 3022082 WP LT VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14840 49580 INSPECTION FOUND A .25 INCH CRACK IN AFT FUSELAGE LEFT VERTICAL STABILIZER ATTACH ANGLE. THE ANGLE WAS REPLACED IAW EA 5340-01012. 2 L 7 2 4F A6WE 1998082100301 19980821 00301 NM 1998 8 21 CALA9801458 1 19980814 A 5320 PAN WEB BOEING 727 727232 1384082 NM LT AFT LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT AFT LAV PAN WEB CORRODED. THE CORRODED AREA WAS REMOVED IAW SRM 51-10-6. A REPAIR WAS FABRICATED A ND INSTALLED IAW SRM 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100302 19980821 00302 NM 1998 8 21 CALA9801459 1 19980815 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 344-384 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FORWARD END OF LT INBOARD SEAT TRACK CORRODED AT STA 344 TO 384. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5, 51-10-2, 51-30-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1998082100303 19980821 00303 NM 1998 8 21 CALA9801460 1 19980815 A 5720 ANGLE BOEING 727 727232 1384082 NM WS 130 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A CRACK ON THE INBOARD SIDE OF L/E CAVITY BULKHEAD LOWER ANGLE APPROXIMATELY TWENTY INCHES AFT OF KRUEG ER FLAP HINGE LINE AT LT WING LEADING EDGE STA 130. THE ANGLE WAS REMOVED AND A NEW REPAIR ANGLE WAS FABRICATED AND INS TALLED IAW SRM 51-40-3, 51-30, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100304 19980821 00304 NM 1998 8 21 CALA9801461 1 19980815 A 5720 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND TWO ATTACH ANGLES CRACKED UNDER OUTBOARD END OF NR 12 SPOILER AT SUPPORT ROD LOWER ATTACH POINT OF RT W ING TRAILING EDGE. THE ATTACH ANGLES WERE REMOVED. TWO NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10 -2, 51-30-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1998082100305 19980821 00305 NM 1998 8 21 CALA9801462 1 19980815 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND THREE CRACKS IN UPPER FLANGE OF INTERCOSTAL BETWEEN FS 720 AND 720A. A REPAIR WAS FABRICATED AND INSTA LLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100306 19980821 00306 NM 1998 8 21 CALA9801463 1 19980815 A 7830 FAIRING BOEING 737 7372C0 1384488 NM NR 1 ENGINE CHAFED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A HOLE CHAFED THROUGH NR 1 ENGINE THRUST REVERSER EXTENSION UPPER CLOSE OUT FAIRING. THE AREA WAS REPA IRED IAW SRM 51-20-1, FIGURE 7. 2 L 7 2 4F A16WE 1998082100307 19980821 00307 NM 1998 8 21 CALA9801464 1 19980815 A 5413 LONGERON BOEING 737 7372C0 1384488 NM NR 2 NACELLE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 2.5 INCH CRACK ON END CAP (LONGERON) PANEL NR 2 ENGINE FAIRING. THE LONGERON WAS REMOVED AND A NEW L ONGERON WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998082100308 19980821 00308 NM 1998 8 21 CALA9801465 1 19980815 A 5400 FAIRING BOEING 737 7372C0 1384488 NM WS 181 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 181.0. THE CRACK WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2 A ND 51-40-2, FIGURE 1. 2 L 7 2 4F A16WE 1998082100309 19980821 00309 NM 1998 8 21 CALA9801466 1 19980815 A 5400 FAIRING BOEING 737 7372C0 1384488 NM WS 183.4 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 1 INCH CRACK ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 183.4. THE CRAC K WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2, 51-40-2, FIGURE 1 , AND 51-30-2. 2 L 7 2 4F A16WE 1998082100310 19980821 00310 WP 1998 8 21 CALA9801467 1 19980817 A 3297 WIRE DOUG DC9 DC932 3022066 WP RT MLG DOOR BROKEN A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 18544 47219 THE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED, BUT THE GEAR DOOR OPEN LIGHT CAME ON. THE GEAR WAS CYCLED TO UP AND THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE GEAR INDI CATIONS WERE NORMAL AFTER CYCLING THE GEAR THE THIRD TIME. MAINTENANCE FOUND WIRES TO RT MLG DOOR UP SWITCH BROKEN. TH E RT MLG DOOR UP SWITCH CANNON PLUG WAS REPLACED. THE NOSE GEAR POSITION SWITCH CANNON PLUG PINS WERE CLEANED. A GEAR SWING WAS PERFORMED AND ALL OPERATION AND INDICATIONS CHECKED GOOD. 2 L 7 2 4F A6WE 1998082100311 19980821 00311 NM 1998 8 21 CALA9801468 1 19980815 A 5320 ANGLE BOEING 737 7372C0 1384488 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A .5 INCH CRACK IN FORWARD ANGLE IN AFT CARGO COMPARTMENT AT STA 727, BL 0, STRINGER 29L. THE ANGLE WA S REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998082100312 19980821 00312 WP 1998 8 21 CALA9801469 1 19980816 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND APPROXIMATELY A 2 INCH CRACK IN LONGERON 17R AT LAV WALL STA 965. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1998082100313 19980821 00313 WP 1998 8 21 CALA9801470 1 19980816 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 996 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND CUSP MEMBRANE CORRODED AT STA 996, LONGERON 18L. THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 25. 2 L 7 2 4F A6WE 1998082100314 19980821 00314 WP 1998 8 21 CALA9801471 1 19980815 A 5312 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A 1.5 INCH CRACK IN AFT PRESSURE BULKHEAD DOUBLER ON LT SIDE BELOW DOOR OPENING. REPAIRED IAW SRM 53-0 5, FIGURE 39. 2 L 7 2 4F A6WE 1998082100315 19980821 00315 WP 1998 8 21 CALA9801472 1 19980817 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A 1 INCH CRACK IN LONGERON 16L AT LT LAV WALL STA 965. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1998082100316 19980821 00316 NM 1998 8 21 CALA9801473 1 19980817 A 5320 SILL BOEING 727 727232 1384082 NM R-2 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND R-2 DOOR LOWER SILL CORRODED AT BS 1065. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100317 19980821 00317 NM 1998 8 21 CALA9801474 1 19980817 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FUSELAGE FRAME ANGLE CORRODED AT STA 360 BETWEEN STRINGER 17R AND 20R. THE ANGLE WAS REMOVED IAW SRM 5 1-30-2. THE CORROSION WAS REMOVED IAW SRM 51-10-6. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998082100318 19980821 00318 SO 1998 8 21 COMA0810177 1 19980815 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 462CA 14396 700 120264 EMERGENCY LIGHTS INOPERABLE. REPLACED BATTERY. 2 L 7 2 4T RT A31SO 1998082100319 19980821 00319 EA 1998 8 21 COMA9860221 1 19980815 A 3350 362624 LIGHT CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 918CA 7018 SECOND SECTION OF FLOOR PATH EMERGENCY LIGHTING IS INOPERABLE. REPLACED LUMINESCENT STRIPS (P/N 6464-5 & 36262-4). 2 L 7 2 4F RT A21EA 1998082100320 19980821 00320 EA 1998 8 21 COMA9860222 1 19980815 A 5270 WARNING SYST CNDAIR CL600 CL6002B19 EA CABIN DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 966CA 7132 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED DOOR WARNING SYSTEM PER MEL. 2 L 7 2 4F RT A21EA 1998082100321 19980821 00321 EA 1998 8 21 COMA9860223 1 19980813 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT MALFUNCTIONED A COMA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 916CA 7014 CARGO SMOKE WARNING. FALSE WARNING CARGO SMOKE DETECTORS DEFERRED PER MEL. 2 L 7 2 4F RT A21EA 1998082100322 19980821 00322 EA 1998 8 21 COMA9860224 1 19980807 A 2710 601R130001 CONTROL MECH CNDAIR CL600 CL6002B19 EA LT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 9658 7048 CHECK INSPECTION, LEFT AILERON HAS EXCESSIVE PLAY. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998082100323 19980821 00323 EA 1998 8 21 COMA9860225 1 19980807 A 2710 601R130002 HINGE CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 SO 01 940CA 9658 7048 C-CHECK INSPECTION, RIGHT HAND AILERON HINGE POINTS HAS EXCESSIVE PLAY. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998082100324 19980821 00324 EA 1998 8 21 COMA9860226 1 19980816 A 2710 279253 LINK CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 DURING C-CHECK, FOUND RIGHT AILERON PCU LINKS TO HAVE EXCESSIVE PLAY. REPLACED BOTH LINKS. 2 L 7 2 4F RT A21EA 1998082100325 19980821 00325 EA 1998 8 21 COMA9860227 1 19980808 A 2750 601R93106505 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 DURING C-CHECK, FOUND RIGHT OUTBOARD FLAP FLEX SHAFT TO BE WORN. REPLACED FLEX SHAFT. 2 L 7 2 4F RT A21EA 1998082100326 19980821 00326 EA 1998 8 21 COMA9860228 1 19980809 A 2752 601R931017 ACTUATOR CNDAIR CL600 CL6002B19 EA RT TE FLAP WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 9942 7044 DURING C-CHECK, FOUND RIGHT INBOARD FLAP ACTUATOR TO HAVE EXCESSIVE PLAY. REPLACED ACTUATOR. 2 L 7 2 4F RT A21EA 1998082100327 19980821 00327 EA 1998 8 21 COMA9860229 1 19980809 A 2752 601R93104 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 6904 7044 DURING C-CHECK, FOUND LEFT OUTBOARD FLAP, OUTBOARD ACTUATOR TO HAVE EXCESSIVE PLAY. REPLACED ACTUATOR. 2 L 7 2 4F RT A21EA 1998082100328 19980821 00328 EA 1998 8 21 COMA9860230 1 19980809 A 2720 10231007 DAMPENER CNDAIR CL600 CL6002B19 EA RUDDER LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 937CA 2982 7044 LEFT OUTBOARD ELEVATOR FLUTTER DAMPENER IS LEAKING FLUID. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1998082100329 19980821 00329 EA 1998 8 21 COMA9860231 1 19980808 A 5320 601R3520521 BRACKET CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 DURING C-CHECK, FOUND CARGO DOOR STEP PLATE BRACKET BROKEN. REPLACED BRACKET. 2 L 7 2 4F RT A21EA 1998082100330 19980821 00330 EA 1998 8 21 COMA9860232 1 19980807 A 5753 601R1430341 VANE CNDAIR CL600 CL6002B19 EA LT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 7048 C-CHECK INSPECTION, LEFT WING INBOARD FLAP VANE HAS CHAFE DAMAGE AT WS 56.30. REPLACED FLAP VANE LEADING EDGE. 2 L 7 2 4F RT A21EA 1998082100331 19980821 00331 EA 1998 8 21 COMA9860233 1 19980808 A 5753 601R1430342 VANE CNDAIR CL600 CL6002B19 EA RT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 7048 C-CHECK INSPECTION TASK 27-680-100, RIGHT HAND INBOARD VANE HAS CHAFE DAMAGE AT WS 56.30. REPLACED FLAP VANE LEADING ED GE. 2 L 7 2 4F RT A21EA 1998082100332 19980821 00332 NM 1998 8 21 UPS98227456 1 19980730 A 5330 SKIN BOEING 727 72751C 1384015 NM BS 243.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK AT RT BS 243.7 WL 226 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3. 2 L 7 3 4F A3WE 1998082100333 19980821 00333 NM 1998 8 21 UPS98227457 1 19980730 A 5330 SKIN BOEING 727 72751C 1384015 NM BS 235.8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK AT RT BS 235.8 WL 222 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3. 2 L 7 3 4F A3WE 1998082100334 19980821 00334 NM 1998 8 21 UPS98227458 1 19980730 A 5330 SKIN BOEING 727 72751C 1384015 NM BS 203.8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK LOCATED AT RT BS 203.8 WL 222 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3. 2 L 7 3 4F A3WE 1998082100335 19980821 00335 NM 1998 8 21 UPS98227459 1 19980730 A 5330 SKIN BOEING 727 72751C 1384015 NM BS 243.7 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK LOCATED AT LT BS 243.7 WL 220 FUSELAGE SKIN. REPAIR CARRIED OUT IAW SRM 53-30-03 FIG 3. 2 L 7 3 4F A3WE 1998082100336 19980821 00336 NM 1998 8 21 UPS98227460 1 19980731 A 7830 BRACKETS BOEING 727 72751C 1384015 NM NR 3 ENG TR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, ENGINE NR 3 THRUST REV FAIRING MID AND AFT SUPPORT BRACKETS CRACKED. BRACKETS REPLACED IAW MM 78-30- 00. 2 L 7 3 4F A3WE 1998082100337 19980821 00337 NM 1998 8 21 UPS98227461 1 19980730 A 5312 BULKHEAD BOEING 727 72751C 1384015 NM BS 178 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, SUSPECT CRACKS ON FWD FACE OF B/H 178 WL 204 APPROX. DEFECT REPAIRED IAW DRW 65C36289 USING EO B727- 5310-4290. 2 L 7 3 4F A3WE 1998082100338 19980821 00338 NM 1998 8 21 UPS98427423 1 19980810 A 5330 SKIN BOEING 747 747121 1384871 NM CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 682UP 20349 AFT UPPER CORNER OF BULK CARGO DOOR FUSELAGE SKIN CRACKED. REPAIRING PER EO BH747-5330-10189. 2 L 7 4 4F A20WE 1998082100339 19980821 00339 WP 1998 8 21 UPS98827441 1 19980807 A 5320 4758514517 FITTING DOUG DC8 DC871F 302199D WP BS 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, INTERCOSTAL AFT END FITTING FOUND TO BE CRACKED AT FWD SIDE OF FS 1140 FRAME AT LONG 33R. REMOVED AN D REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100340 19980821 00340 WP 1998 8 21 UPS98827442 1 19980722 A 5320 JAMB DOUG DC8 DC871F 302199D WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, APPROX .25 INCH CRACK NOTED AT UPPER FORWARD DOOR JAMB CORNER OF AFT CARGO DOOR. REPAIRED IAW SRM 53 -2-0 FIG 21. 2 L 7 4 4F RT 4A25 1998082100341 19980821 00341 WP 1998 8 21 UPS98827443 1 19980721 A 5320 37584951 FITTING DOUG DC8 DC871F 302199D WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, INTERCOSTAL END FITTING CRACKED STA 1240 AT LONG 35L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100342 19980821 00342 WP 1998 8 21 UPS98827444 1 19980727 A 5313 37585931 LONGERON DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-D, STA 1260 TO 1280, STR 35L IS CRACKED ON THE UNDERSIDE. REPAIRED AREA IAW DHC SK 715-547. 2 L 7 4 4F RT 4A25 1998082100343 19980821 00343 WP 1998 8 21 UPS98827445 1 19980731 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1440-1450 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 1440 TO 1450 AT STR 31R, THE SKIN IS CORRODED BEYOND LIMITS. REPAIRED AREA IAW SRM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 1998082100344 19980821 00344 WP 1998 8 21 UPS98827446 1 19980807 A 5320 3610130501N FITTING DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, A/C COMP AT STA 70, STR 21R TIE FITTING UNDER CUSP HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998082100345 19980821 00345 WP 1998 8 21 UPS98827447 1 19980807 A 5313 3615532501 LONGERON DOUG DC8 DC871F 302199D WP BS 35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, A/S COMP, STA 35, STR 36 IS CRACKED AND CORRODED. REMOVED FABRICATED AND INSTALLED LONGERON IAW DWG 3615532 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100346 19980821 00346 WP 1998 8 21 UPS98827448 1 19980810 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 520 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 520 AT STR 32R, THE TORQUE BOX WEB IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 AND DWG 5616520. 2 L 7 4 4F RT 4A25 1998082100347 19980821 00347 WP 1998 8 21 UPS98827449 1 19980724 A 5320 37551721 FITTING DOUG DC8 DC871F 302199D WP BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, NR 1 PIT, THE LWR AFT T-BOLT FITTING IS CRACKED (STA 320). REMOVED AND REPLACED FITTING IAW SRM 51-3 -0. 2 L 7 4 4F RT 4A25 1998082100348 19980821 00348 WP 1998 8 21 UPS98827450 1 19980727 A 5320 575352227 BRACKET DOUG DC8 DC871F 302199D WP BS 1756-1766 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 1756 TO 1766 AT BL O, THE T-BRACKET HAS HEAVY CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND I NSTALLED REPLACEMENT BRACKET IAW DWG 5753522 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100349 19980821 00349 WP 1998 8 21 UPS98827451 1 19980808 A 5320 5615374139 DOUBLER DOUG DC8 DC871F 302199D WP BS 1541-1590 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 1541 TO 1590 AT STR 31L, THE FINGER DOUBLER IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REP LACED DOUBLER IAW DWG 5615674 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998082100350 19980821 00350 WP 1998 8 21 UPS98827452 1 19980728 A 5320 9612650N FITTING DOUG DC8 DC871F 302199D WP BS 8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 8.00, STR 33L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9612650 AND SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1998082100351 19980821 00351 WP 1998 8 21 UPS98827453 1 19980804 A 5313 36428381 LONGERON DOUG DC8 DC871F 302199D WP BS 8-25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 8 TO 25, LONG 33L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 3 642838 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998082100352 19980821 00352 WP 1998 8 21 UPS98827454 1 19980806 A 5320 97537927 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1240-1260 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C STA 1240 TO 1260 AT STR 33L, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753792 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100353 19980821 00353 WP 1998 8 21 UPS98827455 1 19980728 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 702 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 702, RBL 45 TO 50 (WING CENTER SECTION) THE FLOORBEAM WEB HAS A 4 INCH CRACK. REPAIRED AREA IAW DHC SK 715-054. 2 L 7 4 4F RT 4A25 1998082100354 19980821 00354 WP 1998 8 21 UPS98827462 1 19980731 A 5313 3646771228 LONGERON DOUG DC8 DC871F 302199D WP BS 1440-1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 1440 TO 1520, LONG 31R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SECTION OF LO NGERON IAW DWG 3646771 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998082100355 19980821 00355 WP 1998 8 21 UPS98827463 1 19980728 A 5320 561537273 DOUBLER DOUG DC8 DC871F 302199D WP BS 1440-1520 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 1440 TO 1520 AT LONG 31R, THE FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615372 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998082100356 19980821 00356 WP 1998 8 21 98FDEA00513 1 19980813 A 5270 SWITCH DOUG DC10 DC1010F 3022111 WP NR 1 PACK DOOR FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 060FE 46970 AIR COND DOORS LIGHT CAME ON IN FLT STAYED ON TILL ESTABLISH IN DESCENT TO DIVERT FIELD. A/C RELEASE FOR SERVICE PER ME L/CDL. DEFER ITEM PER MEL 52-4D CONT NR 39124, 3 DOOR CONFIRM LOCKED. REPLACED PACK 1 DOOR LIGHT SW. OPS CK OK PER M/ M 52-42-01. SECURED DOORS. 2 L 7 3 4F A22WE 1998082100357 19980821 00357 WP 1998 8 21 98FDEA00514 1 19980816 A 5270 LIGHT DOUG DC10 DC1030F 3023504 WP AC DOOR INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 310FE 48299 IN CRUISE FLT LEVEL 370, AIR COND DOOR LIGHT ILLUM. CONSULT RED TABS, RETURNED TO ANC. DOOR LIGHT WENT OUT AT 6.5 PSI. BEG TO BLINK WHEN INCREASE PSI AT 7.0 PSI. A/C RELEASED PER MEL 52-4D. A/C COND DOOR CAUTION LIGHT INOP. C/W MSP 52 -4C, DOORS ARE VERIFIED CLOSED AND LOCKED. 2 L 7 3 4F RT A22WE 1998082100358 19980821 00358 EU 1998 8 21 98FDEA00515 1 19980816 A 5270 ABS030901 SWITCH AIRBUS 300 A300* EU CARGO DOOR DIRTY A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 655FE 742 REJECTED T/O ATL DUE TO AFT CARGO DOOR WARN. TAXI BACK FOR VISUAL. CK GOOD LIGHT OUT, CAME ON AGAIN DURING LAND IN MEM . CLEAN SWITCH 32WS AND INSP SWITCH 34WS, SWITCH CKS GOOD. CARGO DOOR IND GOOD. PRESS ACFT WITH NO DOOR IND PROBLEM. 2 L 7 2 4F RT A35EU 1998082100359 19980821 00359 NM 1998 8 21 98FDEA00516 1 19980817 A 5330 651237038 SKIN BOEING 727 72725C 138400H NM BS 440-680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 BS 440 TO 680, STR 1 TO STR 3 LT SHOWS SIGN OF CORROSION DUE TO SKIN PILLOWING AND DISHED RIVET HEADS. *S/D* REMOVED A ND REPLACED CROWN SKIN AT STA 440 TO 740, STR 4 LT- STR 4 RT PER FED EX EA 7-5330-42276. 2 L 7 3 4F A3WE 1998082100360 19980821 00360 NM 1998 8 21 98FDEA00517 1 19980817 A 5320 651634112 SHEAR TIE BOEING 727 727227 1384078 NM BS 990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION (C53-113-02) SHEAR TIE AT BS 990, LBL 18, WL 139. *S/D* REPLACED SHEAR TIE AT BS 990, LBL 18, WL 139 IAW FED -EX SRM 53-10-4. 2 L 7 3 4F A3WE 1998082100361 19980821 00361 NM 1998 8 21 98FDEA00518 1 19980817 A 5313 65526236100 STRINGER BOEING 727 727227 1384078 NM BS 670-675 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION (C53-113-01,1) ON STR 28 RT, BS 670 TO 675 FWD CARGO BAY. *S/D* REPAIRED STR 28 RT, BS 666 TO 680 PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1998082100362 19980821 00362 NM 1998 8 21 98FDEA00519 1 19980817 A 5313 655623620 STRINGER BOEING 727 727227 1384078 NM BS 682 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION (C53-113-01,1) ON STRINGER 27 RT, BS 682 FORWARD CARGO BAY. *S/D* REPAIRED STR 27 RT, BS 680 TO 690 IAW FEDE X SRM 53-10-3 FIG 1, DETAIL 1. 2 L 7 3 4F A3WE 1998082100363 19980821 00363 NM 1998 8 21 98FDEA00520 1 19980817 A 5315 65163169 FLOORBEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 WHILE WORKING NR 0173 FOUND FLOORBEAM AT BS 344, RBL 14, WL 208.1 CORRODED. *S/D* REPAIRED FLOORBEAM AT BS 344, RBL 14 , WL 208.1 PER FEDEX REPAIR DRAWING SR 27-53-007. 2 L 7 3 4F A3WE 1998082100364 19980821 00364 NM 1998 8 21 98FDEA00521 1 19980817 A 5313 655624540 STRINGER BOEING 727 727227 1384078 NM BS 700-720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 CORROSION ON STRINGER 28L BETWEEN BS 700 TO 720. *S/D* REPAIRED STR 28L BETWEEN BS 700 TO 720 IAW FED-EX SRM 53-10-3. 2 L 7 3 4F A3WE 1998082100365 19980821 00365 NE 1998 8 21 98UAL900220 2 19980524 A 7230 BLADE PWA BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 ENGINE C5 FAILED A UALA A F J UNSCHED LANDING ACTIVATE FIRE EXT. DUMP FUEL A FLAME/FIRE CL CLIMB 1 WP 29 191UA 26880 727333 NR 1 ENGINE FAILED DEPARTING LAX CLIMBING THRU 13,000 FT. FLT ATTENDANT REPORTED SPARKS COMING FROM FRONT AND REAR OF E NGINE. ZERO OIL PRESSURE, ZERO N2, HIGH EGT. ENG FIRE CHECKLIST ACCOMPLISHED. BOTH BOTTLES FIRED. DUMPED FUEL. OVER WEIGHT LANDING IN LAX, PER SFOLM LAND WEIGHT 673.0 LBS. *S/D* ENGINE IS NOT YET DISASSEMBLED. PRELIMINARY INDICATIONS ARE HIGH PRESSURE COMPRESSOR STAGE 5 BLADE FAILURE. ENGINE SHOWS NO INDICATION OF FIRE. MORE DETAIL TO FOLLOW AFTER E NGINE DISASSEMBLY. 2 L 7 4 4F 4 F RT A20WE E24NE 1998082100366 19980821 00366 NM 1998 8 21 98UAL900373 1 19980801 A 3397 58631 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7458U 21912 EMERGENCY ESCAPE PATH LIGHTING EXIT SIGN BY DOOR NR 1 LEFT IS INOPERATIVE. *S/D* REPLACED EEL CABLE BETWEEN FWD EEL ST RIP AND DOOR 1-LEFT EXIT SIGN, CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998082100367 19980821 00367 NE 1998 8 21 98UAL900379 2 19980809 A 7321 863210 MEC WOODWARD GOV 3560056 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE FAILED A UALA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 WP 29 358UA 31438 31438 24379 723161 ON DESCENT, NUMBER 1 ENGINE FLAMED OUT. *S/D* REPLACED MAIN ENGINE CONTROL (MEC) ON ENGINE. ENGINE TESTED SUCCESSFULL Y. FOUND GOVERNOR PLUG ON MEC DISBONDED. INCORPORATING SERVICE BULLETIN 73-117. 2 L 7 2 4F 4 F RT A16WE E2GL 1998082100368 19980821 00368 NM 1998 8 21 98UAL900380 1 19980807 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7456U 21910 LEFT FORWARD EXTERIOR EMERGENCY LIGHT BATTERY CHARGER IS INOPERATIVE. *S/D* REPLACED BATTERY PACK, OP CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998082100369 19980821 00369 NM 1998 8 21 98UAL900381 1 19980807 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7290U 21568 LEFT OVERWING CENTER EMERGENCY LIGHT INOPERATIVE. *S/D* INSTALLED NEW BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1998082100370 19980821 00370 NM 1998 8 21 98UAL900382 1 19980811 A 2752 240863 MOTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 29 7260U 21407 LOST ALL A-SYSTEM HYDRAULIC QUANTITY DURING CLIMB. RETURNED TO ORD. *S/D* FLAP DRIVE MOTOR FOUND LEAKING HYDRAULIC FL UID. REPLACED FLAP DRIVE MOTOR SYSTEM, OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998082100371 19980821 00371 NM 1998 8 21 98UAL900383 1 19980811 A 3610 VALVE AIRESEARCH 12355814 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA A UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 WP 29 7446U 21900 IMMEDIATELY AFTER TAKEOFF, THE NR 3 STRUT OVERHEAT LIGHT CAME ON. SHUT DOWN NR 3 ENGINE AND RETURNED TO LGA. *S/D* RE PLACED NR 3 ENGINE 8TH STAGE VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998082100373 19980821 00373 NM 1998 8 21 98UAL900385 1 19980812 A 3350 S106 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 AIRSTAIR EMERGENCY LIGHT INOPERATIVE. *S/D* REPLACED BATTERY, OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998082100374 19980821 00374 NM 1998 8 21 98UAL900386 1 19980813 A 3260 INDICATION BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE LANDING GEAR MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 988UA 21750 RETURNED TO DENVER DUE TO LANDING GEAR INDICATION PROBLEMS. *S/D* LUBED GEAR HANDLE AND JACKED AIRCRAFT PER 32-60-05 A ND SYSTEM CHECKS OK. 2 L 7 2 4F 4 F A16WE E2EA 1998082100375 19980821 00375 NM 1998 8 21 98UAL900387 1 19980813 A 3230 RELAY BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LANDING GEAR MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 947UA 26688 RETURNED TO STL DUE TO TAKEOFF WARNING HORN, AND GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. *S/D* REPLACED M991, M 983, AND R432. CHECKED PER MM 31-26-00. 2 L 7 2 4F 4 F RT A16WE E2GL 1998082100376 19980821 00376 WP 1998 8 21 ABXA9800735 1 19980728 A 5313 5919238 STRINGER DOUG DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND STRINGER 16 CORRODED. REPAIRED IAW ABX REA D 957 24455 MR. 2 L 7 2 4F A6WE 1998082100377 19980821 00377 WP 1998 8 21 ABXA9800736 1 19980729 A 5315 991224359 FLOORBEAM DOUG DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON UPPER FLOORBEAM CAP FS 965. FABRICATED REPAIR STRAP AND REPAIR ANGLE IAW ABX REA D 953 24462 MR AND INSTALLED REPAIR IAW ABX REA D 953 24462 MR. 2 L 7 2 4F A6WE 1998082100378 19980821 00378 WP 1998 8 21 ABXA9800737 1 19980810 A 5313 591142527 LONGERON DOUG DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND LONGERON 17R CRACKED. REPLACED LONGERON 17R IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082100379 19980821 00379 WP 1998 8 21 ABXA9800738 1 19980728 A 5313 5919237501 STRINGER DOUG DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND STRINGER 15 CORRODED. REPAIRED IAW ABX REA D 957 24455 MR. 2 L 7 2 4F A6WE 1998082100380 19980821 00380 WP 1998 8 21 ABXA9800739 1 19980728 A 5313 5919236501 STRINGER DOUG DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND STRINGER 14 CORRODED. REPAIRED IAW ABX REA D 957 24455 MR. 2 L 7 2 4F A6WE 1998082100381 19980821 00381 WP 1998 8 21 ABXA9800740 1 19980720 A 5320 9910755 CUSP WEB DOUG DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND CUSP WEB CRACKED AT LONGERON 18R FS 965. REPLACED CUSP WEB IAW ABX REA D 953 24241 MR. 2 L 7 2 4F A6WE 1998082100382 19980821 00382 WP 1998 8 21 ABXA9800741 1 19980720 A 5320 59148657 ANGLE DOUG DOUG DC9 DC932 3022066 WP PRESS PANEL CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND ANGLE ON FORWARD SIDE OF PRESSURE PANEL CRACKED. REPLACED ANGLE ON FORWARD SIDE OF PRESSURE PANEL IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082100383 19980821 00383 WP 1998 8 21 ABXA9800742 1 19980717 A 5311 59353803 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK FOUND CRACKED FRAME FS 965 LONGERON 15L. REPLACED FRAME SECTION FS 965 LONGERON 15L IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998082100384 19980821 00384 WP 1998 8 21 ABXA9800743 1 19980720 A 5320 D0489835 WEB DOUG DOUG DC9 DC932 3022066 WP BS 990 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND CUSP WEB CRACKED AT FS 990 LONGERON 18L. REPLACED CUSP WEB IAW REA D 953 24241 MR. 2 L 7 2 4F A6WE 1998082100385 19980821 00385 WP 1998 8 21 ABXA9800745 1 19980815 A 5720 99193691 T-CAP DOUG DOUG DC9 DC932 3022066 WP WS 58.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 983AX 47257 DURING C-CHECK, FOUND LEFT T-CAP CRACKED AT STATION XCW-58.500. REPLACED LEFT WING T-CAP IAW ABX EA 12182 AND DC9 SRM 5 1-30-5. 2 L 7 2 4F A6WE 1998082100386 19980821 00386 WP 1998 8 21 MWEA98872 1 19980813 A 2560 113317 SLIDE COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 THE GALLEY SLIDE COVER COMES OFF EASILY. MTC READJUSTED TOP CHANNEL ON DOOR. 2 L 7 2 4F A6WE 1998082100387 19980821 00387 WP 1998 8 21 MWEA98873 1 19980816 A 5730 59358221 SKIN DOUG DC9 DC981 3022081 WP WS 164-214 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND SEVERAL BLENDOUT BETWEEN XRS 164 AND XRS 214 BEYOND LIMITS ON LEFT WING LOWER PLATING SKIN. MTC FABRICATED AND IN STALLED DOUBLERS. 2 L 7 2 4F A6WE 1998082100388 19980821 00388 WP 1998 8 21 MWEA98874 1 19980813 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 THE COCKPIT EMERGENCY EXIT LIGHTS DO NOT COME ON WITH EMERGENCY LIGHTS SWITCH IN ON POSITION. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998082100389 19980821 00389 WP 1998 8 21 MWEA98875 1 19980814 A 7931 39610051D1 INDICATOR DOUG DC9 DC932 3022066 WP LT ENGINE INOPERATIVE A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 207ME 47794 LEFT ENGINE OIL PRESSURE DROPPED TO 38 PSI DURING TO ROLL. REMOVED AND REPLACED LEFT ENGINE OIL PRESSURE INDICATOR, OPS GOOD. 2 L 7 2 4F A6WE 1998082100390 19980821 00390 WP 1998 8 21 MWEA98876 1 19980815 A 3350 60117759 BATTERY PACK DOUG DC9 DC914 3022034 WP AFT CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 600ME 45725 LT EMERGENCY NACELLE LIGHT INOP. REMOVED AND REPLACED NACELLE LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1998082100391 19980821 00391 NM 1998 8 21 MWEA98877 1 19980816 A 2612 878239 CONNECTOR DOUG MD88 MD88 3023688 NM APU COMPART DIRTY A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 31 601ME 49762 APU FIRE DETECTOR LOOP CAME ON LOOP-B AT 90 KB ABOARD TAKEOFF. CLEANED OIL FROM LOOP CONNECTORS, OPS CHECK GOOD. 2 L 7 2 4F RT A6WE 1998082100392 19980821 00392 NM 1998 8 21 DL73K981610 1 19980806 A 3350 POWER SUPPLY BPS73 BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 312DL 1669 23084 EMERGENCY LIGHTS FLASHING RT AISLE AND AFT BULKHEAD. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A16WE 1998082100393 19980821 00393 NM 1998 8 21 DL72S981612 1 19980806 A 5311 651592231 FRAME BOEING 727 727232 1384082 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 A CRACK WAS FOUND IN THE FRAME AT FS 380 AND WL 280, JUST ABOVE THE R1 DOOR CUTOUT. REPAIRED PER ERA 331909-14. 2 L 7 3 4F A3WE 1998082100394 19980821 00394 NM 1998 8 21 DL72S981613 1 19980806 A 5330 65184201031 SKIN BOEING 727 727232 1384082 NM BS 990 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 L1 DOOR SURROUND BEAR STRAP WAS FOUND CRACKED IN THE LWR AFT CORNER OF THE DOOR. CRACK WAS TRIMMED OUT THRU THE SKIN, B ONDED DOUBLER AND BEAR STRAP. REPAIRED PER ERA 331987-14. 2 L 7 3 4F A3WE 1998082100395 19980821 00395 NM 1998 8 21 DL72S981614 1 19980806 A 5311 655612910 FRAME BOEING 727 727232 1384082 NM BS 95-960 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 523DA 21583 CORROSION WAS FOUND ON THE O/B FLANGE OF THE O/B CHORD OF THE C2 DOOR SILL. APPROX 0.060 OF MATERIAL FROM THE UPPER SUR FACE OF THE FLANGE WAS REMOVED. REPAIRED PER ERA 331905-14. 2 L 7 3 4F A3WE 1998082100396 19980821 00396 NM 1998 8 21 DL72S981616 1 19980806 A 3350 BATTERY PACK RPS1B BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 529DA 8134 21703 ALL 1ST CABIN SEAT MOUNTED EMERGENCY EXIT LIGHT AND ROWS 10 AND 11 EMERGENCY EXIT PATH LIGHTS INOP DURING STBY POWER CHE CK. REPLACED BATTERY PACK AND BATTERY RACK OPS CKS OK. 2 L 7 3 4F A3WE 1998082100397 19980821 00397 NM 1998 8 21 DL767981617 1 19980806 A 3350 BPS73 POWER SUPPLY BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 107DL 22219 RT OVERWING EGRESS LIGHTS INOP. REPLACED BATTERY POWER SUPPLY, CKS GOOD. 2 L 7 2 4F RT A1NM 1998082100398 19980821 00398 NM 1998 8 21 DL757981618 1 19980807 A 5414 SKIN BOEING 757 757232 1384965 NM NR 2 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 634DL 23615 DURING INSPECTION OF A PREVIOUSLY ACCOMPLISHED REPAIR, AN ADDITIONAL CRACK WAS FOUND EMANATING FROM A PREVIOUS CUTOUT AT THE FWD UPPER CORNER OF THE ACCESS HOLE ON THE NR 2 ENGINE STRUT SKIN, AT THE OUTBD SIDE OF NAC STA 107.7. REPAIRED PE R ERA 365391-14. 2 L 7 2 4F RT A2NM 1998082100399 19980821 00399 NM 1998 8 21 DLM88981619 1 19980807 A 3350 BATTERY 61020 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 913DL 49544 AFT CABIN FLASHLIGHT NOT FLICKERING. REPLACED BATT AND BULB, OP CKS GOOD. 2 L 7 2 4F RT A6WE 1998082100400 19980821 00400 NM 1998 8 21 DL72S981620 1 19980626 A 5753 6502163262 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED IN 21 PLACES AT I/B CUTOUT FOR I/B AFT FLAP DRIVE. T HE ANGLE WAS REPAIRED BY STOP DRILLING THE CRACKS AND INSTALLING A DOUBLER PER 727 MM 57-52-0, PG 807. 2 L 7 3 4F A3WE 1998082100401 19980821 00401 1998 8 21 DLL14981623 4 19980808 A 3442 TR UNIT 20704100101 LKHEED 1011 1011385115 5265015 WP NR 2 RADAR FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 1738D 3070 193C1234 ELECTRICAL BURNING/SMOKE SMELL IN COCKPIT. NO SECONDARY INDICATIONS. FOUND ELEC SMELL IN FESC COMING FROM NR 2 RADAR T RANSCEIVER. REPLACED NR 2 RADAR TRANSCEIVER, CHECKS GOOD. 2 L 7 3 4F A23WE 1998082100402 19980821 00402 WP 1998 8 21 DLL10981625 1 19980808 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 720DA 193C1136 EMERGENCY EXTERIOR LIGHTS INOP LEFT FWD. REPLACED BATTERY AND PWR SUPPLY, SYS NOW CKS OK. 2 L 7 3 4F A23WE 1998082100403 19980821 00403 NM 1998 8 21 DLM88981628 1 19980809 A 3350 LIGHT P20700030 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 948DL 49879 ON PREFLIGHT, FOUND EMER FLASHLIGHT AT FWD F/A STATION TEST INOP. REPLACED FLASHLIGHT AND BATT. 2 L 7 2 4F RT A6WE 1998082100404 19980821 00404 NM 1998 8 21 DLM88981629 1 19980809 A 3350 BATTERY 61020 DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 948DL 49879 ON PREFLIGHT, FOUND EMER FLASHLIGHT AT FWD FLT ATTEND STA NOT TESTING. REPLACED BATT. 2 L 7 2 4F RT A6WE 1998082100405 19980821 00405 NM 1998 8 21 DL72S981630 1 19980801 A 5741 FITTING BOEING 727 727232 1384082 NM LT WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 LEFT WING FWD WING FITTING BORE HAS CORROSION AND SCORING, FOUND WHEN BUSHING REMOVED. REMOVED BTL PIN ON R/C 59, OPN 5 508AD AND REMOVED FWD BUSHING PER M/M 57-41-11. FOUND CORROSION TO BE WITHIN .15 OF INNER EDGE OF TERMINAL FITTING AT 1 0 AND 11 O'CLOCK POSITION FACING AFT. MACHINE BORE TO 3500 PER SRM 53-40-01 PG 13. CORR REMOVAL COMPLETE, OK TO TREAT BORE. TREATED BORE, TURNED AND TREATED BUSHING, INSTALLED BUSHING. 2 L 7 3 4F A3WE 1998082100406 19980821 00406 NM 1998 8 21 DLM90981631 1 19980809 A 3244 TIRE DOUG MD90 MD9030 3023690 NM NR 3 MAIN FAILED A DALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SO 27 909DA 53389 NR 3 MAIN TIRE LOST TREAD DURING T/O ROLL, LEFT GEAR EXTENDED. RETURNED FOR UNEVENTFUL LANDING. RECAP SEPARATED FROM T IRE CAUSING EXTENSIVE DAMAGE TO RT I/B FLAP AND NR 2 ENGINE. 2 L 7 2 4F RT A6WE 1998082100407 19980821 00407 NM 1998 8 21 DL73K981632 1 19980808 A 5312 6546547215 BULKHEAD CHORD BOEING 737 737232 1384475 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 A 0.5 INCH CRACK WAS FOUND IN THE MLG WHEEL WELL BLKHD AT STA 727. THE CRACK WAS LOCATED IN THE UPPER FLANGE OF THE COM PRESSION CHORD AT BL 0.0 AND RUNS THRU A FASTENER HOLE. REPAIRED PER ERA 365406-14. 2 L 7 2 4F RT A16WE 1998082100408 19980821 00408 NM 1998 8 21 DL73K981633 1 19980807 A 5315 654541039 FLOORBEAM BOEING 737 737232 1384475 NM BS 678 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 LBL AND RBL 24 CABIN FLOORBEAMS OVERLYING THE MAIN WHEEL WELL AT APPROX STA 678 WERE FOUND WITH CRACKS IN THE WEB AND WE B DOUBLER. REPAIRED PER ERA 332046-14. 2 L 7 2 4F RT A16WE 1998082100409 19980821 00409 NM 1998 8 21 DL73K981634 1 19980807 A 5320 654795919 STRAP BOEING 737 737232 1384475 NM BS 783 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 THE REINFORCEMENT STRAP FOR THE C2 DOOR CUTOUT FWD FRAME WAS CORRODED AT THE NUT PLATE HOLES AT APPROX S25R. REPAIRED P ER ERA 332025-14. 2 L 7 2 4F RT A16WE 1998082100410 19980821 00410 NM 1998 8 21 DL73K981635 1 19980807 A 5315 6545410224 FLOORBEAM BOEING 737 737232 1384475 NM BS 664 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 BL 0 FLOORBEAM OF THE WING CENTER SECTION IS CRACKED AT BS 664. NO CRACKS FOUND IN THE WEB. REPAIRED PER ERA 331996-14 . 2 L 7 2 4F RT A16WE 1998082100411 19980821 00411 NM 1998 8 21 DL73K981636 1 19980807 A 5311 FRAME BOEING 737 737232 1384475 NM BS 380 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 FS 380 FRAME WAS GOUGED APPROX 3 ABOVE S27L IN THE UPPER FREE FLANGE. REPAIRED PER ERA 332007-14. 2 L 7 2 4F RT A16WE 1998082100412 19980821 00412 NM 1998 8 21 DL73K981637 1 19980807 A 5330 SKIN BOEING 737 737232 1384475 NM CARGO DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 AFT EDGE OF C2 DOOR CUTOUT WAS FOUND CRACKED AT APPROX 10 BELOW THE SKIN LAP SPLICE. REPAIRED PER ERA 332013-14. 2 L 7 2 4F RT A16WE 1998082100413 19980821 00413 NM 1998 8 21 DLM88981638 1 19980810 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 996DL 53363 A CRACK WAS FOUND AT L2L AND L2R AT STA 1418, IN THE FRAME. REPAIRED PER ERA 332005-14. 2 L 7 2 4F RT A6WE 1998082100414 19980821 00414 NM 1998 8 21 DL73K981643 1 19980807 A 5315 6545410224 FLOORBEAM BOEING 737 737232 1384475 NM BS 670 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 334DL 23105 CRACKS WERE FOUND IN THE UPPER CHORD OF THE LBL 24 AND RBL 24 OVERWING FLOORBEAMS AT APPROX STA 670 TO 675. THE CRACKS EMINATED FROM THE SEAT TRACK FASTENER CUTOUTS. CRACKING IS DUE TO FATIGUE. REPAIRED PER ERA 332012-14. 2 L 7 2 4F RT A16WE 1998082100415 19980821 00415 NM 1998 8 21 DLM88981647 1 19980807 A 5320 JAMB DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 925DL 49712 THE LOWER JAMB PAN OF THE C1 DOOR CUTOUT WAS FOUND CORRODED. THE SECTION OF PAN BETWEEN THE FWD AND AFT CORNERS WAS CUT AND REMOVED. A NEW SECTION OF PAN WAS SPLICED IN PER THE MD-88 SRM 53-05 FIG 44 AND DOCUMENTED PER ER/A 365399-14. 2 L 7 2 4F RT A6WE 1998082100416 19980821 00416 NM 1998 8 21 DL72S981648 1 19980810 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 532DA 22045 EMERGENCY TRACK LIGHTING SECTION IN FWD COACH AREA DOES NOT ILLUMINATE. REPAIRED SECTION OF WIRE. 2 L 7 3 4F A3WE 1998082100417 19980821 00417 NM 1998 8 21 DL73E981649 1 19980807 A 5330 SKIN BOEING 737 737247 138448D NM BS 380 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 374DL 23521 THE FUSELAGE SKIN AT FS 380 WAS DAMAGED BY GROUND EQUIPMENT BETWEEN STRINGERS 17L AND 18L. THE DAMAGED AREA WAS CUTOUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED PER ER/A 365386-14. 2 L 7 2 4F A16WE 1998082100418 19980821 00418 NM 1998 8 21 DL72S981650 1 19980808 A 5312 6516350339 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 543DA 22392 THE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH CRACK AT RBL 25 AND WL 169. THE CRACK WAS REPAIRED WITH A TITANIUM REP AIR DOUBLER ON A TEMPORARY BASIS WITH REPETITIVE INSPECTIONS. THE PERMANENT REPAIR WILL ACCOMPLISH A WEB MODIFICATION P ER BAC S/B 727-53-0215. THE REPAIR WAS ACCOMPLISHED PER ER/A 365397-14. 2 L 7 3 4F A3WE 1998082100419 19980821 00419 NM 1998 8 21 DLM88981652 1 19980804 A 4990 38005041 APU DOUG MD88 MD88 3023688 NM APU COMPT FAILED A DALA A UNSCHED LANDING B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CR CRUISE 1 SO 27 903DE 7615 53380 P126 IN CRZ AT FL330, SMOKE IN CABIN WHEN AIRFOIL A/I TURNED ON. SMOKE DISSIPATED WHEN A/I TURNED OFF. FOUND APU TO BE LEAK ING OIL AND DISTRIBUTED INTO PNEUMATIC SYSTEM, RENDERED APU INOP. RAN ENGINES TO TAKEOFF POWER, ALL OK. REPLACED APU. 2 L 7 2 4F RT A6WE 1998082100420 19980821 00420 NM 1998 8 21 DL72S981653 1 19980724 A 5753 652163361 RIB BOEING 727 727232 1384082 NM NR 1 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 P126 DURING SHOP INSPECTION, THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED AT LOWER AFT CORNER. THE RIB WAS REPAIRED PER 727 MM 57-52-0, FIG 808 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FILLER. 2 L 7 3 4F A3WE 1998082100421 19980821 00421 NM 1998 8 21 DL72W981658 1 19980811 A 3230 SEQUENCE VALVE 1U10851 BOEING 727 727247 138408F NM RT MLG CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 2809W 1538A 20581 DURING CLIMBOUT, LOST 'A' SYSTEM HYDRAULIC PRESSURE AND FLUID QTY. FOUND RIGHT MLG DOOR SEQUENCING VALVE CRACKED. REPL ACED VALVE. LEAK CHECK AND GEAR SWING GOOD. 2 L 7 3 4F A3WE 1998082100422 19980821 00422 NM 1998 8 21 DLM90981659 1 19980810 A 5330 SKIN DOUG MD90 MD9030 3023690 NM BS 1353 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 907DA 53387 THE FUSLEAGE SKIN AT FS 1353 WAS DENTED AND CREASED BETWEEN STRINGERS 28L AND 28R. STRINGER 29L WAS ALSO DENTED. THE S KIN DAMAGE WAS REMOVED WITH A 18.75 X 20.75 CUTOUT AND A 4 INCH SECTION OF THE DAMAGED STRINGER WAS REMOVED. THE SKIN W AS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER THE MD-90SRM (CLASS 2 REPAIR) AND THE STRINGER WAS SPLICED WITH PER TH E MD-90 SRM. THE REPAIR WAS DOCUMENTED PER ER/A 365416-14. 2 L 7 2 4F RT A6WE 1998082100423 19980821 00423 NM 1998 8 21 DLM11981661 1 19980812 A 2530 CHILLER 2676 DOUG MD11 MD11 3023602 NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 810DE 1757 48565 AFT GALLEY CHILLER G8 HAS SMOKE COMING OUT OF IT. REPLACED CHILLER. 2 L 7 3 4F RT A22WE 1998082100424 19980821 00424 NM 1998 8 21 DLM90981662 1 19980812 A 3350 BULB 2232 DOUG MD90 MD9030 3023690 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 909DA 53389 LEFT OVERWING EMERGENCY EVACUATION LIGHT FAILED TO TEST ON LAYOVER CHECK. RELAMPED, TESTS GOOD. 2 L 7 2 4F RT A6WE 1998082100425 19980821 00425 NM 1998 8 21 DL72W981663 1 19980812 A 3350 BATTERY PACK S106 BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2815W 20871 R-1 DOOR EMERG LIGHT INOP. REPLACED BATT PACK, OPS NOW OK. 2 L 7 3 4F A3WE 1998082100426 19980821 00426 NM 1998 8 21 DL72L981664 1 19980812 A 5530 STRINGER BOEING 727 727232 1384082 NM VERTICAL STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 502DA 21304 A 1 INCH CRACK AT BOLT TO EDGE ON STR 8 FIN STA 157.2 RT SIDE. REPAIRED PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1998082100427 19980821 00427 NM 1998 8 21 DL73S981665 1 19980812 A 3350 BPS73 POWER SUPPLY BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 323DL 23095 ON L/O-2 CHECK FOUND EMERGENCY EXIT LIGHT ABOVE RT OVERWING DOOR INOP, M1135 POSITION. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A16WE 1998082100428 19980821 00428 NM 1998 8 21 DL767981666 1 19980812 A 3350 20131A BATTERY PACK BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 111DN 22223 L1 SLIDE LIGHT INOP, ALSO BOTH LT OVERWING SLIDE LIGHTS INOP. REPLACED BOTH BATTERIES. 2 L 7 2 4F RT A1NM 1998082100429 19980821 00429 NM 1998 8 21 DL72S981669 1 19980723 A 5754 RIB BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 AT HMV FOUND, RIBS CRACKED I/B AND O/B OF GUIDE TRACK NR 6 SLAT I/B GUIDE TRACK. REMOVED ARM, FABRICATED DOUBLER MM 57- 54-00 PG 813A, INSTALLED DOUBLER PER SAME. 2 L 7 3 4F A3WE 1998082100430 19980821 00430 NM 1998 8 21 DL72E981670 1 19980306 A 5753 652163254A SKIN BOEING 727 727247 138408F NM NR 3 TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 DURING SHOP INSPECTION, A CRACK WAS DISCOVERED AT THE CORNER OF THE CUTOUT IN THE COVE SKIN FOR THE I/B AFT FLAP DRIVE R OD. THE COVE SKIN WAS REPAIRED PER MM 57-52-0 FIG 809 BY REMOVING THE DAMAGE AND INSTALLING A FILLER AND DOUBLER. 2 L 7 3 4F A3WE 1998082100431 19980821 00431 NM 1998 8 21 DL72S981671 1 19980813 A 2782 SUPPORT BOEING 727 727232 1384082 NM NR 8 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 NR 8 SLAT ACTUATOR SUPPORT CRACKED I/B SIDE. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998082100432 19980821 00432 NM 1998 8 21 DL72S981672 1 19980813 A 5522 PANEL BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 NR 2 LT BALANCE BOARD CLOSE OUT PANEL HAS A 2 INCH CRACK AT O/B END. REPAIRED PER SRM 55-20-3. 2 L 7 3 4F A3WE 1998082100433 19980821 00433 NM 1998 8 21 DL72S981673 1 19980813 A 5320 WEB BOEING 727 727232 1384082 NM BS 1275 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 478DA 20755 RT VERTICAL TORQUE BOX WEB CRACKED .25 INCH PAST ROUTE OUT AT LIGHTNING HOLE STA 1275 RT UPPER HOLE. REPAIRED PER M/M 5 3-11-0 FIG 819. 2 L 7 3 4F A3WE 1998082100434 19980821 00434 1998 8 21 DLL19981675 2 19980814 A 7314 RB211524B4I FUEL PUMP PAC102MK4B4I LKHEED 1011 10113853 5265020 WP NR 1 ENGINE FAILED A DALA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SO 27 759DA B1374C 193Y1176 NR 1 ENG FLAME-OUT AT FL 31.0, OIL FILTER PRESSURE LIGHT NOT ON. N3 ABOVE 20 PERCENT OTHER PARAMETERS WIND MILL NORMAL. USING CROSSFEED NR 3 TO NR 1 AT TIME WITH NR 1 FUEL BOOST PUMP OFF FUEL PRESS LIGHT ON MOMENTERILY ON FE AND PILOTS AN NUNCIATOR PANEL. RELIGHT SUCCESSFUL. REPLACED ENGINE FUEL PUMP. 2 L 7 3 4F A23WE 1998082100435 19980821 00435 NM 1998 8 21 DL72S981676 1 19980814 A 5712 6518522 RIB BOEING 727 727232 1384082 NM BS 760 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 DURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERTICAL FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHOR D. THE CRACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE 2 FWD MOST FASTENER HOLES AND TRAVELS DOWN, THRU THE ENTIR E THICKNESS OF THE HORIZ FLANGE. REPAIRED PER ERA 332037-14AD. 2 L 7 3 4F A3WE 1998082100436 19980821 00436 NM 1998 8 21 DL73E981677 1 19980811 A 5330 SKIN BOEING 737 737247 138448D NM LT COCKPIT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 THE UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW WAS FOUND WITH A .75 INCH LONG CRACK IN THE SKIN AND UNDERLYING GUSSET A LONG THE C-D WINDOW POST. THE GUSSET CRACK WAS STOP DRILLED AND THE SKIN CRACK TRIMMED OUT. AN EXTERNAL STEEL DOUB LER AND ALUMINUM TRIPLER WERE INSTALLED TO REPAIR THE DAMAGE. THE REPAIR WAS ACCOMPLISHED PER ER/A 365422-14. 2 L 7 2 4F A16WE 1998082100437 19980821 00437 NM 1998 8 21 DL76L981678 1 19980812 A 5400 SHIM BOEING 767 767332 1382001 NM NR 1 PYLON MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 A SHIM WAS FOUND MIGRATED .25 FROM BENEATH THE STRUT LOWER SPAR FITTING ON THE NR 1 PYLON. THE CONDITION IS DESCRIBED I N BAC S/B 767-54-0070. THE LOCAL FASTENERS WERE REPLACED AND THE MIGRATED SHIM WAS TRIMMED FLUSH PER THE TEMPORARY REPA IR INSTRUCTIONS OF THE SERVICE BULLETIN. THE PERMANENT MOD WILL BE ACCOMPLISHED AT THE NEXT HMV. THE REPAIR WAS DOCUME NTED PER ER/A 365445-14. 2 L 7 2 4F RT A1NM 1998082100438 19980821 00438 WP 1998 8 21 DLL19981680 1 19980813 A 3350 5165741 POWER SUPPLY LKHEED 1011 10113853 5265020 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 753DA 193W1189 F/C CABIN EMERGENCY TRACK LIGHTS GO OFF AFTER APPROX 1.5 MINUTES. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998082100439 19980821 00439 NM 1998 8 21 DL72W981684 1 19980815 A 3350 1001141 LIGHT BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2819W 21057 OVERHEAD EMERGENCY LIGHTS AT AFT AIRSTAIRS INOP. MTC REPLACED LIGHT ASSY, OPS CKS. OK. 2 L 7 3 4F A3WE 1998082100440 19980821 00440 NM 1998 8 21 DLM88981685 1 19980815 A 3350 P2070003001 LIGHT DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 906DL 49537 EMER FLASHLIGHT AT FWD F/A JUMPSEAT INOP. REPLACED FLASHLIGHT. 2 L 7 2 4F RT A6WE 1998082100441 19980821 00441 NM 1998 8 21 DLM88981686 1 19980814 A 2760 3924649501 LINK DOUG MD88 MD88 3023688 NM RT INBD SPOILER WORN A DALA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 27 925DL 49712 AT 20,000 FT AND 300 KTS ATTEMPED TO DEPLOY SPEEDBRAKES, AIRCRAFT_ROLLED RIGHT. SPEED BRAKE RETRACTION STOPPED ROLL. RE PLACED RT INBOARD FLIGHT SPOILER LINK. 2 L 7 2 4F RT A6WE 1998082100442 19980821 00442 NM 1998 8 21 DLM90981689 1 19980815 A 2612 FIRE LOOP 2460170 DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE FAILED A DALA K NONE N FALSE WARNING LD LANDING 1 SO 27 909DA 53389 20205 AFTER TAKEOFF, RIGHT ENGINE FIRE LIGHT FLICKERS. ON SHORT, FINAL FIRE WARNING 4 TIMES UNTIL LANDING. REPLACED ELEMENT. 2 L 7 2 4F 4 F RT A6WE E40NE 1998082100443 19980821 00443 NM 1998 8 21 DL72S981692 1 19980810 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 FOUND DURING MV1 CORROSION VISIT NRC 31, CORROSION AT CLIP NUT HOLES UPPER AND LOWER SIDE OF FLOORBEAM STA 344 BL 0 RBL 24 AREA RBL 18 TO RBL 24 WITHIN LIMITS SRM 53-10-1. AREA RBL 18 TO BL 0 WORKED ON NRC 40 SRM 53-10-8. 2 L 7 3 4F A3WE 1998082100444 19980821 00444 NM 1998 8 21 DL72S981693 1 19980810 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 FOUND DURING MV1 CORROSION VISIT NRC 40, CORROSION AT FLOORBEAM STA 344 FROM BL 0 TO LBL 60. WORKED WITH NRC 31. REPAI RED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998082100445 19980821 00445 NM 1998 8 21 DL72K981694 1 19980816 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 480DA 20860 ON L/O, FOUND AISLE EMERGENCY LIGHT OUT AT ROW 9. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998082100446 19980821 00446 NM 1998 8 21 DL72S981696 1 19980814 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 478DA 20755 EMERGENCY EXIT FLOOR LIGHTS DO NOT WORK FROM ROW 28 BACK. REPAIRED BROKEN WIRES AT END OF TRACK. 2 L 7 3 4F A3WE 1998082100447 19980821 00447 NM 1998 8 21 DL72W981697 1 19980814 A 3350 900542 BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2814W 20870 EMERGENCY EXIT LIGHTS AT RT WING INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998082100448 19980821 00448 NM 1998 8 21 DL76S981698 1 19980812 A 5730 111T30131 SKIN BOEING 767 767332 1382001 NM CENTER WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 124DE 23438 CORROSION WAS FOUND ON THE WING CENTER SECTION. DAMAGE LOCATED ON AFT SKIN PANEL, FWD EDGE ON THE LT OUTBD END. REPAIR ED PER ERA 331990-14. 2 L 7 2 4F RT A1NM 1998082100449 19980821 00449 NM 1998 8 21 DL72S981699 1 19980814 A 5711 65192923 SPAR WEB BOEING 727 727232 1384082 NM CENTER WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 THE CENTER WING REAR SPAR WEB WAS FOUND WITH 5 CRACKS NEAR UPPER SPAR CAP. THE CRACKS ARE TYPICAL OF THOSE IN BAC S/B 727-57A0182. THE SPAR WEB WAS MODIFIED PER THE S/B WITH A CHANGE TO THE REPAIR AT RBL 20 WHERE A PREVIOUS LOCAL REPAIR WAS INSTALLED. THE REPAIR/MODIFICATION WAS ACCOMPLISHED PERER/A 365428-14AD. 2 L 7 3 4F A3WE 1998082100450 19980821 00450 NM 1998 8 21 SCNA98088 1 19980809 A 3397 WIRE BOEING 727 727225 1384077 NM CABIN BROKEN A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR LIGHTING SEGMENT IN THE AFT CABIN WAS FOUND TO BE INOPERATIVE. FOU ND A BROKEN WIRE AFT OF SEAT ROW 27 AND REPAIRED. OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1998082100451 19980821 00451 SO 1998 8 21 BIER05053 1 19980818 A 5511 4007514 SPAR PIPER PA31 PA31350 7103110 SO LT HORIZ STAB CRACKED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 3521S 100 317952107 DURING INSP IAW PIPER SB998A, FOUND LEFT STAB SPAR CRACKED ON O/B BOTTOM AREA OF SPAR. CRACK ONLY VISIBLE USING BORESCO PE DUE TO LOCATION. 1 L 7 2 3O A20SO 1998082100452 19980821 00452 SO 1998 8 21 BIER9806054 1 19980818 A 2730 81262109 LINK PIPER PA31 PA31350 7103110 SO ELEVATOR DAMAGED B BIEA K NONE O OTHER IN INSP/MAINT 1 EA 21 3521S 100 317952107 FOUND ELEVATOR BALANCE SPRING FWD LINK HOLE ELONGATED AT POINT SPRING ATTACHES TO LINK. 1 L 7 2 3O A20SO 1998082100453 19980821 00453 SO 1998 8 21 SWIA971230 1 19980809 A 3620 DUCT LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT PACK ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 215SW 120281 LEFT DUCT LEAK LIGHT ON MAP CAME ON 7 MIN AFTER TAKEOFF. RETURNED TO AIRPORT AND LIGHT EXTINGUISHED JUST BEFORE TOUCHDO WN. DEFERRED LEFT A/C PACK PER MEL 36-21-1. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082100454 19980821 00454 SO 1998 8 21 SWIA971232 1 19980809 A 3620 DUCT LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE ILLUMINATED A SWIA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 NM 07 214SW 120280 LEFT ENGINE BLEED DUCT LEAK ON IN FLIGHT. SCENARIO B IN QRH LEFT ENGINE SHUTDOWN IN FLIGHT. PERFORMED LEAK CHECK OF LE FT ENGINE BLEED AIR SYSTEM WITH ENGINE AND SHOP AIR. COULD NOT DUPLICATE PROBLEM. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082100455 19980821 00455 SO 1998 8 21 SWIA971233 1 19980809 A 7712 311694201 TORQUE SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 294SW 120321 RIGHT TORQUE GAUGE FAILED SHORTLY AFTER TAKEOFF. ENGINE FEATHERED BUT UNFEATHERED ON ITS OWN. REMOVED AND REPLACED RIG HT ENGINE TORQUE SENSOR. RAN ENGINE FOR 20 MINUTES AT VARIOUS POWER SETTINGS AND TORQUE INDICATION NORMAL WITH NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082100456 19980821 00456 SO 1998 8 21 SWIA971234 1 19980801 A 2720 RUDDER LIGHT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE COCKPIT ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 212SW 120276 RUDDER LIGHT ON MAP ASSOCIATED WITH RUDDER OVER BOOST ON OVER HEAD ILLUMINATED IN FLIGHT. RETURNED TO SLC. PERFORMED R UDDER OVER BOOST TEST IAW MM 27-22-00. INSPECTED IAW FAULT ISOLATION MANUAL 27-24-90 WITH PITOT STATIC PRESSURE. NO FA ULT FOUND AT THIS TIME. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082100457 19980821 00457 1998 8 21 SWIA971235 4 19980803 A 3425 AHRS EMB 120 EMB120RT SO PWA 118 PW118 NE NR 1 & 2 OUT OF ADJUST A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 130G 120130 RECEIVED HEADING FLAG, RMI FLAG BOTH SIDES WITH GYRO PRECESSING ALL THE TIME INFLIGHT. RETURNED TO LAX. RE-ORIENTED N R 1 AND NR 2 AHRS IAW MM 34-00-00. OPERATED SYSTEM ON GROUND AND ALL CHECKS OK. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082100458 19980821 00458 NE 1998 8 21 SWIA971236 2 19980803 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT FAILED A SWIA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 NM 07 221SW 120290 RIGHT ENGINE FAILED IN FLIGHT. RETURNED TO LAX. REMOVED AND REPLACED RIGHT ENGINE ASSEMBLY WITH A SERVICEABLE UNIT PER MM 71-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082100459 19980821 00459 NE 1998 8 21 VNAA9808013 2 19980813 A 7532 4067B000 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 439JS 69309 3057 DURING THE TAXI FOR TAKEOFF, A HIGH PRESSURE BLEED SYSTEM FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO TH E GATE. OUTSTATION MAINTENANCE INSPECTED AND DEFERRED THE LEFT HAND ENGINE HP BLEED SYSTEM, IN ACCORDANCE WITH THE MINU MUM EQUIPMENT LIST. ON 17 AUG 98 MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND HIGH PRESSURE BLEED VALVE IN ACCORDAN CE WITH DORNIER MAINTENANCE MANUAL 36-11-07. OPERATIONAL CHECKS WERE COMPLETED AND THE DEFERRAL WAS REMOVED FROM THE AI RCRAFT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100460 19980821 00460 NM 1998 8 21 VNAA9808014 1 19980816 A 2612 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE LOOSE A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 425JS 3037 A RIGHT HAND ENGINE FIRE DETECT WARNING LIGHT ILLUMINATED, DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GA TE. MAINTENANCE INSPECTED AND RESECURED THE RIGHT HAND ENGINE FIRE LOOP SENSOR WIRE CANNON PLUG, IN ACCORDANCE WITH DOR NIER MAINTENANCE MANUAL 26-11-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100461 19980821 00461 1998 8 21 CKSA98507 4 19980727 A 2564 D30170533 SLIDE RAFT LKHEED 1011 1011385115 5265015 WP R 2 DOOR DEPLOYED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 108CK 193N1204 R2 DOOR SLIDE FOUND INFLATED UPON ARRIVAL AT AIRCRAFT. REMOVED AND REPLACED R2 DOOR EVACUATION SLIDE RAFT PER MM 25-61- 10. DOOR OPS CHECKS GOOD. 2 L 7 3 4F A23WE 1998082100462 19980821 00462 NM 1998 8 21 USAA980294 1 19980630 A 5347 SEAT TRACK BOEING 757 757225 1384959 NM BS 377 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 600AU 22192 DURING C-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION BS 377 LBL 45 SEAT TRACK. FABRICATED SEA T TRACK PER SERM 51-10-00. 2 L 7 2 4F RT A2NM 1998082100463 19980821 00463 NM 1998 8 21 TSAA9833378 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 3 POSITION EMERGENCY LIGHT ASSY BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082100464 19980821 00464 NM 1998 8 21 TSAA9833377 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 2 POSITION EMERGENCY LIGHT ASSY BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082100465 19980821 00465 NM 1998 8 21 TSAA9833376 1 19980709 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 1 POSITION EMERGENCY LIGHT ASSY BATTERY PACK DUE TO CONDITION LED'S INOP. OPS CHECKED OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082100466 19980821 00466 NM 1998 8 21 TSAA9833375 1 19980706 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECKED GOOD. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998082100467 19980821 00467 NM 1998 8 21 TSAA9833374 1 19980706 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998082100468 19980821 00468 NM 1998 8 21 TSAA9833373 1 19980706 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998082100469 19980821 00469 EU 1998 8 21 VTZA982243 1 19980625 A 3230 S2700003 RELAY JETAIR JETSTM JETSTM4101 1500501 EU LT MLG INTERFERING A VTZA A D UNSCHED LANDING RETURN TO BLOCK O OTHER CL CLIMB 1 EA 27 311UE 41029 FLT 6260 - IAD-BUF - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WOULD NOT RETRACT. AIRCRAFT RETURNE D TO GATE AT IAD WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND SCRAPPER RING INTERFERING WITH AOG RELAY. M AINTENANCE PROPOSITIONED AOG RELAY. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998082100470 19980821 00470 EA 1998 8 21 98ZZZM552 1 19980524 A 2460 8801K23 SWITCH DHAV DHC6 DHC6300 EA COCKPIT FAILED A ASWA A UNSCHED LANDING N B FALSE WARNING SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 07 140SA 267 CREW REPORTED THAT APPROXIMATELY 2 MINUTES AFTER TAKEOFF, THE RIGHT GENERATOR DROPPED OFF LINE, WOULD NOT RESET. THE TH E NR 1 RADIO AND GPWS INOP LIGHTS STARTED TO FLASH AND A BURNING SMELL WAS IN THE COCKPIT. AIRCRAFT RETURNED TO AIRPORT OF DEPARTURE. MAINTENANCE PERSONNEL REPLACED SHORTED LT AVIONICS MASTER SWITCH. GENERATORS AND AVIONICS CHECKED NORMA L. (M) 1 H 7 2 3T A9EA 1998082100471 19980821 00471 NM 1998 8 21 USAASB98170 1 19980706 A 3020 655812313 ANTI-ICE DUCT BOEING 737 7372B7 1384560 NM NR 2 ENGINE BLOWN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 268AU 22880 PHL - FLT 993 - AFTER TAKEOFF FROM PHL, CREW OBSERVED A RAPID RISE IN THE NR 2 ENGINE CSD OIL TEMPERATURE FOLLOWED BY A NR 2 ENGINE OVERHEAT LIGHT. CREW REDUCED THRUST ON ENGINE AND OVERHEAT LIGHT WENT OUT. AIRCRAFT WAS AT FL 080 WHEN CRE W MADE DECISION TO RETURN TO FIELD AT PHL. FLT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANC E REMOVED AND REPLACED A BLOWN ANTI-ICE DUCT FOR THE NOSE COWL ANTI-ICE ON THE RIGHT SIDE OF THE NR 2 ENGINE. GROUND RU N, OPERATIONAL CHECK AND LEAK CHECK GOOD. THE NR 2 ENGINE CSD REMAINED ON MEL. (M) 2 L 7 2 4F A16WE 1998082100472 19980821 00472 NM 1998 8 21 USAASB98173 1 19980707 A 2133 7110033 OUTFLOW VALVE BOEING 737 7372B7 1384560 NM CABIN FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 276AU 22888 PHL - FLT 221 - AIRCRAFT DEPARTED PHL WITH THE RIGHT AIR CONDITIONING PACK ON MEL. AFTER TAKEOFF, CREW COULD NOT GET TH E LEFT PACK TO PRESSURIZE AIRCRAFT. DECISION WAS MADE TO RETURN TO FIELD AT PHL. FLT LANDED WITHOUT INCIDENT. NO EMER GENCY WAS DECLARED. MAINTENANCE FOUND THE AFT OUTFLOW VALVE NOT DRIVING THE FORWARD OUTFLOW VALVE CLOSED. REMOVED AND REPLACED THE AFT OUTFLOW VALVE ASSY PER MM. OPERATED OUTFLOW VALVE IN MANUAL AC AND DC AND IN STANDBY PRESSURIZATION. O PERATIONAL CHECK NORMAL PER MM 21-31-11. RAN ENGINES AT IDLE AND PRESSURIZED AIRCRAFT UP TO 3.5 PSI, ALTERNATING LEFT A ND RIGHT PACKS. BOTH PACKS OPERATE AND CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100473 19980821 00473 NM 1998 8 21 USAASB98163 1 19980630 A 3610 39271611 SHUT OFF VALVE BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 254AU 22796 PIT - FLT 296 - CREW ADVISED VIA ACARS WERE ENCOUNTERING PROBLEMS WITH THE DUCT PRESSURES. AT CLIMB POWER, THE LEFT DUC T PRESSURE READS 80 PSI WHILE THE RIGHT READS 38 PSI. THE DECISIION WAS MADE TO DIVERT TO PIT. NO EMERGENCY WAS DECLAR ED AND THE FLIGHT LANDED WITHOUT FURHTER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE 13TH STAGE MODULATI NG AND SHUTOFF VALVE. OPERATIONAL CHECKS NORMAL PER MM. (M) 2 L 7 2 4F A16WE 1998082100474 19980821 00474 NM 1998 8 21 USAASB98174 1 19980709 A 7312 320115 HEAT VALVE BOEING 737 7372B7 1384560 NM NR 2 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 EA 19 281AU 36248 23114 MSY - FLT 1184 - ON CLIMB-OUT FROM MSY, THE NR 2 ENGINE FUEL HEAT VALVE TRANSIT LIGHT ILLUMINATED. THE NR 2 ENGINE OIL TEMPERATURE WAS IN THE YELLOW BAND. CRWE COULD NOT CONTROL FUEL HEAT VALVE WITH SWITCH AND TRIED RESETTING CIRCUIT BREA KER WITH NO HELP. REDUCING POWER SENT OIL TEMPERATURE TO RED LINE. CREW SHUTDOWN THE NR 2 ENGINE IN FLIGHT AND DECLARE D AN EMERGENCY. FLIGHT RETURNED TO FIELD TO MSY AND LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 M INUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL HEAT VALVE IN ASSOCIATION WITH MAINTENANCE MANUAL. OPERA TIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100475 19980821 00475 NM 1998 8 21 USAABB98071 1 19980625 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 LAX - FOUND R1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998082100476 19980821 00476 NM 1998 8 21 USAABB98068 1 19980610 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 LGA - FOUND THE FLOOR LEVEL EMERGENCY LIGHTS AT ROWS 9 AND 13 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLIES. ( M) 2 L 7 2 4F RT A2NM 1998082100477 19980821 00477 NM 1998 8 21 USAABB98070 1 19980618 A 3350 FUSE BOEING 757 757225 1384959 NM CABIN BLOWN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 LAX - ROW 24 AND 26 EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE M735 POWER SUPPLY. (M) 2 L 7 2 4F RT A2NM 1998082100478 19980821 00478 NM 1998 8 21 USAABB98069 1 19980618 A 3350 20121 CHARGER BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 607AU 22203 LAX - AFT SECTION OF OVERHEAD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER. (M) 2 L 7 2 4F RT A2NM 1998082100479 19980821 00479 NM 1998 8 21 USAASB98169 1 19980705 A 3230 654462514 LOCK ACTUATOR BOEING 737 7373B7 1384580 NM NLG FAILED A USAA L ABORTED APPROACH J WARNING INDICATION CL CLIMB 1 EA 19 371US 22950 ROC - FL 1795 - SHORTLY AFTER RAISING THE LANDING GEAR AFTER TAKEOFF FROM DCA, THE NOSE LANDING GEAR GREEN LIGHT REMAINE D ON ALONG WITH THE RED UNSAFE LIGHT. COCKPIT NOISE INDICATED THE GEAR DOORS WERE STILL OPEN. RECYCLED GEAR AND RECEIV ED ALL THREE GEAR GREEN LIGHTS WITH ALL NORMAL INDICATIONS. PROCEEDED TO ROC AND REQUESTED TOWER FLYBY. GEAR EXTENSION AND TOWER FLYBY WERE NORMAL. FLIGHT LANDED WITHOUT INCIDENT AND NO EMERGENCY BEING DECLARED. MAINTENANCE FERRIED THE AIRCRAFT TO PIT FOR REPAIR AND REPLACED THE NOSE LANDING GEAR LOCK ACTUATOR PER MM 32-33-21. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998082100480 19980821 00480 NM 1998 8 21 USAABB98072 1 19980705 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 623AU 27244 LGA - FOUND FOUR LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998082100481 19980821 00481 NM 1998 8 21 USAABB98073 1 19980705 A 3350 8731002511REV9 SIGN BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 630AU 27808 BDL - FOUND L1 DOOR EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998082100482 19980821 00482 NM 1998 8 21 USAABB98074 1 19980701 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 605AU 22201 LAX - FOUND EMERGENCY LOW LEVEL LIGHT AT ROW 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998082100483 19980821 00483 WP 1998 8 21 USAAD98123 1 19980714 A 5240 4954341501 SPRING DOUG DC9 DC981 3022081 WP AFT SERVICE DOOR BROKEN A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 805US 48053 ORD - FLT 247 - DURING CLIMB, THE AIRCRAFT BEGAN TO LOSE PRESSURIZATION AND THE AFT SERVICE DOOR WARNING LIGHT ILLUMINAT ED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT SERVICE DOOR NOT CLOSED PROPERLY CAUSED BY A BROKEN INTERLOCK SPRING. THE INTERLOCK SPRING WAS REPLACED AND DOOR OPERATION WAS NORMAL. (M) 2 L 7 2 4F A6WE 1998082100484 19980821 00484 EU 1998 8 21 USAASB98164 2 19980630 A 7250 TURBINE BOEING 737 737401 1384701 NM CFMINT CFM56 CFM563B2 13802 EU LT ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 404US 23886 720406 FLL - FLT 1638 - AFTER TAKEOFF AT 800 FT, THE NR 1 ENGINE EXPERIENCED A TURBINE FAILURE. CREW SHUT DOWN THE NR 1 ENGINE IN FLIGHT. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT FLL WITHOUT FURTHER INCIDENT. TOTAL SINGLE E NGINE TIME WAS 17 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSY. OPERATIONAL CHECK AND LEAK CHECK GOO D. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1998082100485 19980821 00485 NE 1998 8 21 USAAD98118 2 19980702 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE RIGHT FAILED A USAA O OTHER J X WARNING INDICATION ENGINE FLAMEOUT AP APPROACH 1 EA 19 974VJ 47130 DCA - FLT 998 - ON FINAL ON DCA, SEVEN MILES OUT AND AT 2000 FT IN A RIGHT TURN, CREW RECEIVED A CROSS TIE LOCKOUT WARNI NG, LOST THE RIGHT ENGINE AND FIRST OFFICERS INSTRUMENTS, AND EXPERIENCED SOME PRESSURIZATION PROBLEMS. THE CREW STARTE D THE APU AND REGAINED THE RIGHT ENGINE BEFORE LANDING. AN EMERGENCY WAS DECLARED. MAINTENANCE WAS UNABLE TO DUPLICATE THE ENGINE SHUTDOWN. AS PRECAUTION THE ENGINE DRIVE FUEL PUMP, FUEL CONTROL UNIT, AND FUEL HEATER WERE REPLACED. (M) 2 L 7 2 4F 4 F A6WE E2EA 1998082100486 19980821 00486 WP 1998 8 21 USAAD98100 1 19980602 A 2150 49560771 SEAL DOUG DC9 DC931 3022065 WP LT PACK FAILED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 941VJ 47054 ATL-PHL - FLT 1786 - DURNIG CRISE AT 33,000 FT THE CABIN ALT STARTED TO CLIMB SLOWLY AT ABOUT 100 FT/MIN. WHEN THE CREW REDUCED ENGINE POWER THE CABIN ALT STARTED TO INCREASE RAPIDLY. THE CREW DECLARED AN EMERGENCY WITH ATC AND CHANGED AI RCRAFT ALTITUDE TO 10,000 FT. DURING DESCENT THE CABIN ALT EXCEEDED 10,000 FT AND THE OXYGEN MASKS DEPLOYED. THE AIRCR AFT DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT AIR CONDITIONING PACK ACM, AND PACK CONT ROL SWITCH. ALSO, THE PRESSURE SEAL IN THE RIGHT WHEEL WELL FOR THE DUAL BRAKE CONTROL VALVE CABLES WAS REPLACED. (M) 2 L 7 2 4F A6WE 1998082100487 19980821 00487 NM 1998 8 21 AALA981245 1 19980608 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1166-1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - STRINGER 227 CORRODED AT BS 1166-1183. REPAIRED DAMAGE STRINGER PER SRM 53-10-3. ALODINED AND PRIMED PER MM 51-2 0-0. (M) 2 L 7 3 4F A3WE 1998082100488 19980821 00488 NM 1998 8 21 AALA981244 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 728AA 20735 TUL - FOUND BELL FRAME HAS 3 DEEP DENTS ON TOP OF FRAME BETWEEN STRINGER 22L AND 25L AT STATION 500 FWD WEB OF FRAME DIS TORTED. INSTALLED BELL FRAME REPAIR PER SRM 93-10-A. (M) 2 L 7 3 4F A3WE 1998082100489 19980821 00489 WP 1998 8 21 AALA981243 1 19980619 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 420 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 228AA 49178 TUL - FOUND FRAME 420 BELLFRAME CRACKED AT HORIZONTAL DOOR FRAME STIFFENER ATTACH POINT HI-LOK STRINGER 20R, VIEWED FROM UNDER SIDE OF COLLAR. INSTALLED DOUBLER AND FILLER AND FASTENERS PER SRM 53-10-4. (M) 2 L 7 2 4F A6WE 1998082100490 19980821 00490 NM 1998 8 21 AALA981242 1 19980527 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 675 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND STRINGER 27R AND STRINGER SPLICE HAVE HEAVY CORROSION AT STATION 675. INSTALLED STRINGER SPLICE PER ESO 116 97. (M) 2 L 7 3 4F A3WE 1998082100491 19980821 00491 NM 1998 8 21 AALA981241 1 19980619 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND STRINGER 28R OUTBOARD LEG CORRODED AT STATION 720C. INSTALLED A FILLER AND STRAP WITH SEALANT AND HI-LOKS P ER ESO 11697, DATED 6/3/98. (M) 2 L 7 3 4F A3WE 1998082100492 19980821 00492 NM 1998 8 21 AALA981240 1 19980619 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 460 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - HEAVY CORROSION ON TOP OF FLOORBEAM RBL 55 TO 62, STATION 460. TOP CAP OF FLOORBEAM RBL 55 TO 62. REMOVED FLOORB EAM, REPAIR PERFORMED PER 53-10-8 PAGE 9A. (M) 2 L 7 3 4F A3WE 1998082100493 19980821 00493 NM 1998 8 21 AALA981239 1 19980619 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 474 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND STRINGER 19R AT FS 474 HEAVILY CORRODED. CUTOUT CORRODED AREA AND INSTALLED REPAIR PER SRM 53-10-34 AND 51- 10-2. (M) 2 L 7 3 4F A3WE 1998082100494 19980821 00494 NM 1998 8 21 AALA981238 1 19980619 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND STRINGER 15R CRACKED JUST FWD OF ICE LIGHT. FINISHED DRILLING PARTS, ALODINED, PRIMED SEALED PARTS AND INST ALLED PER SRM 53-10-3 FIG 5, PAGE 12. (M) 2 L 7 3 4F A3WE 1998082100495 19980821 00495 NM 1998 8 21 AALA981237 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 540 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 725AA 20732 TUL - BELL FRAME HAD 2 DEEP DENTS AT STATION 540 BETWEEN STRINGER 25L AND STRINGER 24L. CUTOUT DAMAGE, INSTALLED DOUBLE R PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998082100496 19980821 00496 NM 1998 8 21 AALA981236 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - BELTFRAME DENTED AT STATION 700 BETWEEN STRINGER 24L AND 23L, FORWARD WEB OF FRAME DISTORTED. INSTALLED DOUBLER O VER DAMAGE CUTOUT ON BELTFRAME AT STATION 780 BETWEEN STRINGE R23L AND 24L PER SRM 53-10-4, PAGE 3. (M) 2 L 7 3 4F A3WE 1998082100497 19980821 00497 NM 1998 8 21 AALA981235 1 19980619 A 5320 SPLICE BOEING 727 727227 1384078 NM BS 700 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - BELL FRAME SPLICE HAS DEEP GOUGE AT STATION 700 BETWEEN STRINGER 25R AND STRINGER 21R. REMOVED AND REPLACED SPLIC E PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998082100498 19980821 00498 NM 1998 8 21 AALA981234 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - BELL FRAME DENTED AT STATION 680 BETWEEN STRINGER 24R AND STRINGER 23R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998082100499 19980821 00499 NM 1998 8 21 AALA981233 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - BELL FRAME DENT AND FORWARD WEB DISTORTED AT STATION 700, BETWEEN STRINGER23R AND 24R. CUT OUT DAMAGED INSTALLED FRAME REPAIR PER 53-10-4. (M) 2 L 7 3 4F A3WE 1998082100500 19980821 00500 NM 1998 8 21 AALA981232 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND BELL FRAME DENTED STATION 620 BETWEEN STRINGER 25L AND 24L. REPAIRED BELL FRAME PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998082100501 19980821 00501 NM 1998 8 21 AALA981231 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - STATION 380 BELL FRAME CRACKED AT HORIZONTAL DOOR FRAME STIFFENER ATTACH POINT HI-LOK, STRINGER 20R. INSTALLED DO UBLER AND FILLER AND FASTENERS PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998082100502 19980821 00502 NM 1998 8 21 AALA981230 1 19980619 A 5312 BULKHEAD BOEING 727 727227 1384078 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - STATION 1183 BULKHEAD CRACKED LBL 35, WL 188 BELOW LEFT CENTER DUCT CUTOUT. REPAIRED BULKHEAD PER BOEING SB 727-5 3-0217, DOUBLER/TRIPLER WITH HI-LOKS. (M) 2 L 7 3 4F A3WE 1998082100503 19980821 00503 NM 1998 8 21 AALA981229 1 19980619 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1169 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND CORROSION BULGING BETWEEN EXT SKIN AND LAV SVC PAN AT AFT LAV PANEL ACCESS DOOR. REMOVED LAV PAN, REMOVED C ORROSION PER 51-10-6. REPLACED PAN SUPPORT FRAME AND RE-INSTALLED PAN. (M) 2 L 7 3 4F A3WE 1998082100504 19980821 00504 NM 1998 8 21 AALA981228 1 19980619 A 5720 BULKHEAD BOEING 727 727227 1384078 NM LT WING TIP CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - LEFT WING TIP BULKHEAD CRACKED, UPPER FLANGE AT 3 RIVETS, OUTBOARD SIDE PANEL VENT BOX. REPAIRED LT BULKHEAD UPPE R FLAGNE CRACKS AT 3 RIVETS PER SRM 51-40-2 PAGE 3. (M) 2 L 7 3 4F A3WE 1998082100505 19980821 00505 NM 1998 8 21 AALA981227 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - BELL FRAME CRACKED UNDER UPPER FLANGE AT FS STATION 500 BETWEEN STRINGER 21R AND 22R. INSTALLED DOUBLER AND FILLR PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998082100506 19980821 00506 NM 1998 8 21 AALA981226 1 19980619 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 BELL FRAME DENTED AND FWD WEB DISTORTED AT STATION FS 500 BETWEEN STRINGER 24R AND 25R. INSTALLED DOUBLER AND FILLER PE R SRM 51-40-3 FIG 1 SHT 3. (M) 2 L 7 3 4F A3WE 1998082100507 19980821 00507 NM 1998 8 21 AALA981225 1 19980619 A 5320 BEAM BOEING 727 727227 1384078 NM BS 740-780 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 FOUND CORROSION ON BOTTOM AND INSIDE OF DELTA BEAM FS 740 TO FS 780, LBL 7 TO RBL 7. REMOVED CORROSION, TREATED AND PRI MED PER ESO 11697. (M) 2 L 7 3 4F A3WE 1998082100508 19980821 00508 NM 1998 8 21 AALA981224 1 19980619 A 5320 HOUSING BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND CORROSION AROUND FASTENERS ON ICE LIGHT HOUSING, STATION 720B TO 720C BETWEEN STRINGER 14R AND STRINGER 16R. INSTALLED NEW ICE LIGHT HOUSING AND SEALED PER SRM 51-30-2 AND SRM 51-20-4. (M) 2 L 7 3 4F A3WE 1998082100509 19980821 00509 NM 1998 8 21 AALA981223 1 19980619 A 5320 BRACKET BOEING 727 727227 1384078 NM BS 560-580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND CORROSION ON BOTH SIDES OF WEB AND ATTACHING BRACKETS. REMOVED CORROSION PER SRM 51-10-6 PAGE 23. TREATED AND PRIMED WEB PER SRM 51-10-2 PAGE 1-6. REINSTALLED WEB USING HI-LOKS PER SRM 51-30-2 PAGES 30-36. REMOVED AND REPLAC ED ATTACHING BRACKET PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1998082100510 19980821 00510 NM 1998 8 21 AALA981222 1 19980619 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND SHEAR TIE CORRODED. REMOVED CORRODED SHEAR TIE AND REPLACED PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998082100511 19980821 00511 NM 1998 8 21 AALA981221 1 19980619 A 5320 HOUSING BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND CORROSION EMITTING FROM UNDER ICE LIGHT HOUSING. REMOVED ICE LIGHT HOUSING AND BLENDED CORROSION PER SRM 51 -10-6 ALODINED AND PRIMED PER SRM 51-10-2. RESEALED AND INSTALLED NEW ICE LIGHT HOUSING LEFT. (M) 2 L 7 3 4F A3WE 1998082100512 19980821 00512 NM 1998 8 21 AALA981220 1 19980528 A 5320 SPLICE BOEING 727 727227 1384078 NM BS 1170 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND STRINGER 22R STATION 1166-1183 PLUS FACTORY STRINGER END SPLICE ON SAME SECTION IS CORRODED. REMOVED AND RE PLACED STRINGER SPLICE. REMOVED CORRODED SECTION OF STRINGER AND SPLICED NEW SECTION PER SRM 51-10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1998082100513 19980821 00513 NM 1998 8 21 AALA981219 1 19980619 A 5320 CASTING BOEING 727 727227 1384078 NM BS 1035 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND FIGURE 8 HOLE AT FUSELAGE TORQUE TUBE UPPER CASTING AT FASTENER HOLE. APPLIED SEALANT PER SRM 51-20-4 TO FI XING SURFACE ON NEW CASTING NR 65-57535-9 AND INSTALLED PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998082100514 19980821 00514 NM 1998 8 21 AALA981218 1 19980619 A 5320 FRAME BOX BOEING 727 727227 1384078 NM BS 1035 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND LEFT AFT SERVICE DOOR UPPER HINGE FRAME BOX CRACKED. APPLIED SEALANT PER SRM 51-20-46 FIXING SURFACES ON NE W CASTING NR 65-57534-1 AND INSTALLE4D PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998082100515 19980821 00515 NM 1998 8 21 AALA981217 1 19980619 A 5320 CLIP BOEING 727 727227 1384078 NM BS 277 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND STRINGER CLIP CRACKED BEHIND F/E DESK AT STRINGER 15R AT STATION 277. REMOVED AND REPLACED STRINGER CLIP AS PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998082100516 19980821 00516 NM 1998 8 21 AALA981216 1 19980619 A 5320 DOOR FRAME BOEING 727 727227 1384078 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 728AA 20735 TUL - FOUND DOOR CUTOUT SKIN CRACKED AT JOGGLE OUTBOARD OF UPPER FORWARD CAM LATCH PLATE. REMOVED AND REPLACED UPPER FW D DOOR FRAME FITTING PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998082100517 19980821 00517 WP 1998 8 21 AALA981352 1 19980706 A 2612 5938323508 FIRE DETECTOR DOUG DC9 DC982 3022082 WP E/E BAY MALFUNCTIONED A AALA E ENGINE SHUTDOWN N Y FALSE WARNING ENGINE STOPPAGE CR CRUISE 1 SW 07 478AA 49653 DFW - FLT 434 - EN ROUTE PHX-DFW - LEFT ENGINE FIRE INDICATION WARNING CAME ON. COULD NOT SILENCE FIRE WARNING WITH BUT TON. SHUT ENGINE DOWN AND FIRE WARNING STOPPED. LANDED DFW WITHOUT INCIDENT. REPLACED LEFT ENGINE FIRE DETECTOR AMPLI FIER A2-7 AND LEFT ENGINE FIRE DETECTOR LOOP. ACCOMPLISHED CHECKS OF LEFT ENGINE FIRE WARNING SYSTEM. SYSTEM GROUND CH ECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998082100518 19980821 00518 WP 1998 8 21 AALA981344 1 19980708 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7526A 49918 DFW - DURING OVERNIGHT CHECK, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED PORTABLE LIGHT AT F ORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998082100519 19980821 00519 WP 1998 8 21 AALA981343 1 19980708 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 554AA 53084 DFW - DURING OVERNIGHT CHECK, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT WAS INOPERATIVE. REPLACED PORTABLE LIGHT AT F ORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998082100520 19980821 00520 NM 1998 8 21 AALA981208 1 19980622 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374AA 25201 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 21B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT SEA T 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082100521 19980821 00521 NE 1998 8 21 AALA981254 2 19980621 A 7250 840001 BLADE BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A AALA A E UNSCHED LANDING ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 SW 07 859AA 21086 666197 DFW - FLT 392 - ON TAKEOFF FROM DFW, EN ROUTE DFW-IAD, EXPERIENCED SEVERE VIBRATION FROM NR 2 ENGINE. VIBRATION WAS NOT ICED IN THE CABIN AND COCKPIT. N2 ROLLED BACK TO ZERO. ACCOMPLISHED PRECAUTIONARY SHUTDOWN CHECKLIST. DECLARED AN EME RGENCY AND RETURNED DFW AND LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. DI SASSEMBLY REVEALED DAMAGE TO THE 1ST STAGE HIGH PRESSURE TURBINE BLADES. VISUAL INSPECTION REVEALED MINIMAL SIGNS OF SU LFIDATION IN ONE EACH THE LIGHTENING HOLES. FAILURE INDICATES THAT THE BLADE MATERIAL UNDERWENT CREEP AND STRESS RUPTUR E. ONE EACH BLADE WAS EVALUATED FOR OVERTEMP SHOWING A METAL TEMP OF LESS THAN 2000 DEG F (LIMIT = 2000 DEG F, AT THE B 2 L 7 3 4F 4 F A3WE E2EA 1998082100522 19980821 00522 NM 1998 8 21 AALA981198 1 19980619 A 3260 106122629 SENSOR BOEING 727 727223 1384074 NM RT MLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 846AA 20987 IAH - FLT 1798 - AFTER TAKEOFF IAH, WHILE RAISING GEAR HANDLE THE RIGHT MAIN GEAR RED LIGHT ILLUMINATED. RECYCLED GEAR AND STILL HAD GEAR RED LIGHT ILLUMINATED. LOWERED GEAR AND GOT SAFE INDICATION. RETURNED AND LANDED IAH WITHOUT INCIDE NT. PERFORMED SPECIAL FERRY FLIGHT TO DFW WITH GEAR DOWN FOR FURTHER EVALUATION. REPLACED RIGHT MAIN LANDING GEAR UPLO CK SENSOR. SWUNG GEAR, SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998082100523 19980821 00523 WP 1998 8 21 AALA981339 1 19980707 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 596AA 53286 ORD - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998082100524 19980821 00524 WP 1998 8 21 AALA981331 1 19980704 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 593AA 53256 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACT LIGHTING IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR TRACK LIGHT STRIP IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998082100525 19980821 00525 WP 1998 8 21 AALA981334 1 19980705 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7533A 49987 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY PORTABLE FLASH LIGHT AT L1 DOOR INOPERATIVE. REPLACED EMERGENCY FLASH LIG HT AT L1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998082100526 19980821 00526 WP 1998 8 21 AALA981341 1 19980706 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 579AA 53156 LAS - DURING OVERNIGHT CHECK, COACH CLASS EMERGENCY EXIT LIGHTS INOPERATIVE. SECURED LOOSE WIRE IN COACH CLASS EMERGENC Y EXIT LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998082100527 19980821 00527 WP 1998 8 21 AALA981337 1 19980706 A 2120 CLAMP DOUG DC9 DC982 3022082 WP RT PACK BROKEN A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 453AA 49558 DFW - DURING TAKEOFF, TAIL COMPARTMENT TEMP LIGH TILLUMINATED AND REMAINED ON WITH THROTTLES RETARDED. AIRCRAFT AIR INT ERRUPTED AND RETURNED TO DFW AND LANDED OVERWEIGHT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A BROKEN CLAMP AT RIGHT AIR CONDITIONING PACK TURBINE. REPLACED BROKEN CLAMP AT RIGHT AIR CONDITIONING PACK TURBINE. OVERWEIGHT INSPECTION REV EALED NO DISCREPANCIES. GROUND RAN ENGINES AT POWER AND NO LEAKS WERE NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 1998082100528 19980821 00528 WP 1998 8 21 AALA981329 1 19980706 A 3260 49548192 SUPPORT DOUG DC9 DC983 3022083 WP RT MLG BROKEN A AALA K NONE J WARNING INDICATION AP APPROACH 1 SW 07 566AA 49348 SJC - FLT 1157 - DURING APPROACH SJC, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. GEAR WAS CYCLED WI TH NO CHANGE. AIRCRAFT LANDED WITHOUT AND STOPPED ON TAXI WAY FOR LANDING GEAR DOOR INSPECTION. GEAR DOORS WERE FOUND IN THE UP AND LOCKED POSITION AND AIRCRAFT TAXIED TO GATE. MAINTENANCE FOUND R IGHT MAIN LANDING GEAR DOOR TARGET BRACK ET BROKEN. REPLACED RIGHT MAIN LANDING GEAR DOOR TARGET BRACKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998082100529 19980821 00529 WP 1998 8 21 AALA981325 1 19980701 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 550-555 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 427AA 49339 TUL - FOUND CORROSION AROUND FASTENERS LEFT CUSP. INSTALLED DOUBLERS IAW AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 1998082100530 19980821 00530 WP 1998 8 21 AALA981290 1 19980629 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 178-186 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 427AA 49339 TUL - FOUND CORROSION ON SUBFLOOR 5 INCHES INBOARD OF FWD PAX DOOR. CUT OUT CORROSION AND INSTALLED DOUBLER IAW SRM 53- 04 FIG 4. (M) 2 L 7 2 4F A6WE 1998082100531 19980821 00531 WP 1998 8 21 AALA981342 1 19980706 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 430AA 49342 TUL - FOUND CORROSION UNDER STAINLESS DOUBLER ON AFT CARGO ENTRYWAY DOOR BEAM. REPLACED ENTIRE AFT CARGO LOWER DOOR BEA M FLOOR STATION 1117 TO 1250 ALONG LONGERON 28 RT. (M) 2 L 7 2 4F A6WE 1998082100532 19980821 00532 NM 1998 8 21 AALA981324 1 19980703 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 620 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND CORROSION ON STRINGER 27R OUTBOARD LEG (VERTICAL) AT STATION 620. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PGS 4C-4E. REMOVED CORROSION PER SRM 51-10-6, TREATED AND PRIMED AREA. (M) 2 L 7 3 4F A3WE 1998082100533 19980821 00533 NM 1998 8 21 AALA981323 1 19980616 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND CORROSION ON INNER SKIN JUST INBOARD OF STRINGER 28L, STATION 720C TO STATION 720C PLUS 5 INCHES. INSTALLED DOUBLER AS PER SRM 53-30-3 AND 51-20-1 AND PER AARD 53-30-03-3 PAGE 1. (M) 2 L 7 3 4F A3WE 1998082100534 19980821 00534 NM 1998 8 21 AALA981322 1 19980703 A 5320 BEAM BOEING 727 727227 1384078 NM BS 744 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND LOWER SKIN ON DELTA BEAM CORRODED AND BLOWN OUT STATION 744 FWD END. REMOVED DAMAGED WEB. INSTALLED WEB RE PAIR PER SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 1998082100535 19980821 00535 NM 1998 8 21 AALA981321 1 19980703 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 360 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND CORROSION ON TOP FLANGE OF FLOORBEAM STATION 360 LBL 10 INCHES AT NUTCLIP HOLE. REMOVED DAMAGED SECTION AND REPAIRED PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998082100536 19980821 00536 NM 1998 8 21 AALA981320 1 19980703 A 5320 WEB BOEING 727 727227 1384078 NM BS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND CORROSION ON CHORD STATION 1183 RBL 20. FOUDN AFTER FASTENER REMOVAL OF CHORD ANGLE, CHORD ANGLE DISPLACED. REPLACED ALL FASTENERS TO RESTORE STRUCTURE AT HAT CHANNEL FLOOR PANS AND CHORD ANGLE. REPLACED FLOOR PAN AREA COMMON TO CHORD ANGLE IAW 51-40-2, 16 BY 12 AREA. (M) 2 L 7 3 4F A3WE 1998082100537 19980821 00537 NM 1998 8 21 AALA981319 1 19980703 A 5320 FITTING BOEING 727 727227 1384078 NM BS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - STRINGER END FITTING CORRODED, STRINGER 5R STATION 1183. REPLACED END FITTING 65-24276-10, STRINGER 5 NEW END FIT TING PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998082100538 19980821 00538 NM 1998 8 21 AALA981318 1 19980608 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 678 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND STRINGER 25R CORRODED ON LOWER VERTICAL LEG AT STATION 678. REMOVED STRINGER FROM STATION 675 TO 690 AND IN STALLED NEW STRINGER SPLICE PER ESO 11697, DATED 6-4-98 TITLED BS 680, STRINGER 25R REPAIR RT SIDE. (M) 2 L 7 3 4F A3WE 1998082100539 19980821 00539 NM 1998 8 21 AALA981317 1 19980703 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - DENT IN FRAME AT 950F STRINGER 25 AND 24 RT. REMOVED DAMAGED AREA. INSTALLED DOUBLER PER AARD 53-10-07-3. (M) 2 L 7 3 4F A3WE 1998082100540 19980821 00540 NM 1998 8 21 AALA981316 1 19980703 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND CRACK IN BELTFRAME AT 950F BETWEEN STRINGER 26L AND 27L. STOP DRILLED CRACK. INSTALLED DOUBLER PER AARD 53 -10-07-3. (M) 2 L 7 3 4F A3WE 1998082100541 19980821 00541 NM 1998 8 21 AALA981315 1 19980602 A 5330 SKIN BOEING 727 727227 1384078 NM BS 420 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND SCRATCH AND DENT IN FUSELAGE STATION 420. REMOVED DAMAGED SKIN AND INSTALLED REPAIR PER SRM 53-30-3 FIG 3 P AGE 12. (M) 2 L 7 3 4F A3WE 1998082100542 19980821 00542 NM 1998 8 21 AALA981314 1 19980703 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - UPPER STRINGER CRACKED, 3RD TAB AFT OUTBOARD SIDE STATION 656.5. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR P ER SB 727-57 A159 REV 5. (M) 2 L 7 3 4F A3WE 1998082100543 19980821 00543 NM 1998 8 21 AALA981313 1 19980703 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - TOP FORWARD STRINGER CRACKED AT STATION 656.5 OUTBOARD SIDE. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PER S B 727-57A159 REV 5. (M) 2 L 7 3 4F A3WE 1998082100544 19980821 00544 NM 1998 8 21 AALA981312 1 19980703 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 719AA 20612 TUL - FOUND STRINGER CRACKED 4TH TAB AFT OUTBOARD SIDE STATION 656.5. REMOVED DAMAGED TAB. INSTALLED DOUBLER REPAIR PE R SB 727-57A 159 REV 5. (M) 2 L 7 3 4F A3WE 1998082100545 19980821 00545 NM 1998 8 21 F3LA98116 1 19980629 A 5320 CHORD BOEING 737 737301 1384611 NM BS 520 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK, INSPECTION REPORTED FAIL/SAFE CHORD CRACKED AT FASTENER LOCATION, BS 520, RBL 8, WL 149. MAINTENA NCE REMOVED DAMAGED AREA OF FAIL/SAFE CHORD (1 INCH BY .7 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-4 0-2, 53-00-07 AND ER NR 98-0610. (M) 2 L 7 2 4F RT A16WE 1998082100546 19980821 00546 NM 1998 8 21 F3LA98115 1 19980629 A 5314 KEEL BEAM BOEING 737 737301 1384611 NM BS 500 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED KEEL BEAM OUTBOARD LOWER FLANGE CORRODED AT BS 500D PLUS 4 INCH, WL 149. MAIN TENANCE REMOVED CORRODED AREA (.9 INCH BY 4.8 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2 AND 53-3 0-12, FIG 202-206. (M) 2 L 7 2 4F RT A16WE 1998082100547 19980821 00547 NM 1998 8 21 F3LA98114 1 19980629 A 5311 FRAME BOEING 737 737301 1384611 NM BS 787 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON FRAME AT BS 787, RBL 23, WL 156. MAINTENANCE REMOVED CORROSION ( 25 INCH BY 1 INCH BY .005 INCH AREA). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-01, 53-00-07 AND ERO NR 9 8-0607. (M) 2 L 7 2 4F RT A16WE 1998082100548 19980821 00548 NM 1998 8 21 F3LA98113 1 19980628 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 727 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON CARGO FLOOR SUPPORTS AT BS 727D PLUS 13 INCHES, 792, 794, 817, RB L 7.5. MAINTENANCE BLENDED CORROSION AT BS 792 (2.25 INCH BY .009 INCH BY .070 INCH), BS 794 (2 INCH BY 1 INCH BY .009 INCH BY .070 INCH). REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2 AND 53-00-53. (M) 2 L 7 2 4F RT A16WE 1998082100549 19980821 00549 NM 1998 8 21 F3LA98112 1 19980628 A 5320 CREASE BEAM BOEING 737 737301 1384611 NM BS 618 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CREASE BEAM WEB CRACKED BETWEEN FASTENERS AT BS 618, RBL 65, WL 208.1. MAINTE NANCE REMOVED DAMAGED WEB, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-40-2 AND SB 737-531122. (M) 2 L 7 2 4F RT A16WE 1998082100550 19980821 00550 NM 1998 8 21 F3LA98111 1 19980628 A 5320 STRAP BOEING 737 737301 1384611 NM BS 794 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON STRAP UNDER FRAME AT BS 794.5, RBL 23, WL 156. MAINTENANCE REMOV ED CORROSION (1 INCH BY 8 INCH BY .025 INCH), AND REPAIRED PER SRM 51-40-02 AND 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998082100551 19980821 00551 NM 1998 8 21 F3LA98110 1 19980626 A 5754 SKIN BOEING 737 737301 1384611 NM NR 2 SLAT CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 2 SLAT OUTBOARD LOWER TRAILING EDGE SKIN NEAR UPSTOP. MAINTENANCE REMOV ED DAMAGED AREA. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-02, DRAWING 65C30133. (M) 2 L 7 2 4F RT A16WE 1998082100552 19980821 00552 NM 1998 8 21 F3LA98109 1 19980626 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 500 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN STRINGER 16L, BS 500C PLUS 4 INCHES. MAINTENANCE REMOVED 14.5 INCH O F STRINGER 16L FROM BS 500B PLUS 10 INCH TO BS 500C PLUS 5 INCHES, FABRICATED REPLACEMENTS PARTS AND REPAIRED PER SRM 51 -40-2, 53-30-03. (M) 2 L 7 2 4F RT A16WE 1998082100553 19980821 00553 NM 1998 8 21 F3LA98107 1 19980623 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 308 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ON INTERCOSTAL AND STRAP BETWEEN FRAMES 303-312, BS 308, STRINGER 4L. M AINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-02 AND 53-00-04. (M) 2 L 7 2 4F RT A16WE 1998082100554 19980821 00554 NM 1998 8 21 F3LA98106 1 19980623 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 807 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON SHEAR TIE AND FRAME AT BS 807, LBL 2 - RBL 3, STRINGER 27L AND 27 R. MAINTENANCE REMOVED CORRODED AREA (2 INCH BY 3 INCH), FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-20-01, 51 -30-2, 53-00-07 AND 53-60-07. (M) 2 L 7 2 4F RT A16WE 1998082100555 19980821 00555 NM 1998 8 21 F3LA98105 1 19980623 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 986 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON FLOORBEAM. UNDER SIDE OF UPPER FRAME AT BS 986.5, LBL 45, WL 208 . MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-00-51, PAGES 212 AND 213 AND SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1998082100556 19980821 00556 NM 1998 8 21 F3LA98104 1 19980623 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON FLOORBEAM AT BS 328, RBL 15-42. MAINTENANCE REMOVED CORROSION AT RBL 15 (1.8 INCH BY 1.2 INCH BY .012 INCH), RBL 22 (1.3 INCH BY 1 INCH BY .013 INCH), RBL 29 (1.4 INCH BY 1 INCH BY .01 5 INCH) RBL 36 (1.5 INCH BY 1.2 BY .012 INCH), AND RBL 43 (1.7 INCH BY 7 INCH BY .016 INCH). FABRICATED REPLACEMENT PAR TS AND REPAIRED PER SRM 53-00-51, FIG 203. (M) 2 L 7 2 4F RT A16WE 1998082100557 19980821 00557 NM 1998 8 21 F3LA98103 1 19980623 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 825/867 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON CARGO FLOOR SUPPORT AT BS 825 AND BS 867. MAINTENANCE REMOVED CO RROSION (.023 INCH AND .013 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, 53-00-53 AND 53-60-53. ( M) 2 L 7 2 4F RT A16WE 1998082100558 19980821 00558 NM 1998 8 21 F3LA98102 1 19980623 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 500 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN END OF STRINGER 16R AT BS 500C PLUS 4 INCHES. MAINTENANCE REMOVED DA MAGED AREA, FABRICATED REPLACEMENTS PARTS AND REPAIRED PER SRM 51-40-2, 53-00-03. (M) 2 L 7 2 4F RT A16WE 1998082100559 19980821 00559 NM 1998 8 21 F3LA98101 1 19980623 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 1006 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 1006, RBL 10, WL 208. MAINTENAN CE REMOVED CORROSION (1.4 INCH BY 1.1 INCH BY .062 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER ERO 98-0567, SR M 51-40-2 AND SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1998082100560 19980821 00560 NM 1998 8 21 F3LA98100 1 19980623 A 5330 SKIN BOEING 737 737301 1384611 NM BS 946 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DURING C-CHECK INSPECTION, REPORTED A 1 INCH CRACK IN AFT GALLEY DOOR SURROUND STRUCTURE INNER SKIN AT BS 946, STRINGER 11R TO 12R THROUGH A HI-LOK HOLE. MAINTENANCE REPAIRED CRACK PER BOEING SB 737-53-1094 AND ER 00017. (M) 2 L 7 2 4F RT A16WE 1998082100561 19980821 00561 NM 1998 8 21 F3LA98099 1 19980623 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 772 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON CARGO FLOOR SUPPORT AT BS 772 AND BS 727E PLUS 3 INCH, LBL 2.5. M AINTENANCE REMOVED CORROSION ON FLOOR SUPPORT AT BS 727E PLUS 3 INCH, LBL 2.5 (1 INCH BY 3 INCH BY .018 INCH) AND BS 772 , LBL 2.5 (1 INCH BY 3 INCH BY .015 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, 53-00-53 AND 53-6 0-53. (M) 2 L 7 2 4F RT A16WE 1998082100562 19980821 00562 NM 1998 8 21 F3LA98098 1 19980623 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 772 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON CARGO FLOOR SUPPORT AT BS 772, LBL 12. MAINTENANCE REMOVED CORRO SION (1 INCH BY 3 INCH BY .022 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, 53-00-53 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1998082100563 19980821 00563 NM 1998 8 21 F3LA98097 1 19980623 A 5320 SUPPORT BOEING 737 737301 1384611 NM BS 727 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ARUOND NUT HOLE PLATES IN SIDEWALL SUPPORT STRAP AT BS 747 - BS 727C MINUS 2 INCH, RBL 19.5 - RBL 23. MAINTENANCE REMOVED CORRODED AREA. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2 AND 53-60-53. (M) 2 L 7 2 4F RT A16WE 1998082100564 19980821 00564 NM 1998 8 21 F3LA98096 1 19980623 A 5311 FRAME BOEING 737 737301 1384611 NM BS 747 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON SHEAR TIE FRAME AT BS 747, STRINGER 27L. MAINTENANCE REMOVED COR ROSION ON SHEAR TIE FRAME (1 INCH BY 2 INCH BY .012 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2, 5 3-00-07 AND 53-60-07. (M) 2 L 7 2 4F RT A16WE 1998082100565 19980821 00565 NM 1998 8 21 F3LA98095 1 19980623 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION AROUND NUT HOLE PLATES AT BS 344 FLOORBEAM UPPER CHORD, LBL 10 TO RB L 2, WL 208. MAINTENANCE REMOVED CORROSION AROUND NUT PLATE HOLES AT BS 344 FLOORBEAM UPPER CHORD, RBL 2 (2 INCH BY 1 I NCH BY .030 INCH), LBL 8 (2 INCH BY 1 INCH BY .025 INCH), LBL 20 (2 INCH BY 1 INCH BY .020 INCH) LBL 50 (2 INCH BY 1 INC H BY .031 INCH), AND RBL 15 (2 INCH BY 1 INCH BY .032 INCH). FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2 AND 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998082100566 19980821 00566 NM 1998 8 21 F3LA98094 1 19980623 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 294 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON FLOORBEAM AT BS 294.5 RBL 10 TO LBL 10, WL 208. MAINTENANCE REMO VED CORROSION, FABRICATED REPLACEMENT PARS AND REPAIRED PER SRM 51-40-2, 53-10-8 AND 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998082100567 19980821 00567 NM 1998 8 21 F3LA98093 1 19980623 A 5315 FLOORBEAM BOEING 737 737301 1384611 NM BS 312 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED 1.5 INCH BY 1 INCH BY .070 INCH AREA OF CORROSION ON FLOORBEAM AT BS 312, RBL 34. MAINTENANCE REMOVED CORRODED AREA, FABRICATED REPLACEMENT PARTS AND INSTALLED PER SRM 51-40-2, 53-10-51 AND 53-10-5 7. (M) 2 L 7 2 4F RT A16WE 1998082100568 19980821 00568 NM 1998 8 21 F3LA98092 1 19980623 A 5320 INTERCOSTAL BOEING 737 737301 1384611 NM BS 327 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ON TOP FLANGE OF INTERCOSTAL AT BS 327, RBL 31, RUNNING 1.5 INCH THROUGH RADIUS. MAINTENANCE FABRICATED REPLACEMENT INTERCOSTAL AND REPAIRED PER SRM 51-40-2 AND 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998082100569 19980821 00569 NM 1998 8 21 F3LA98091 1 19980623 A 5347 SEAT TRACK BOEING 737 737301 1384611 NM BS 336 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED .5 INCH BY 2 INCH BY .45 INCH AREA OF CORROSION ON SEAT TRACK AT BS 336, RBL 2 2. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACEMENT SEAT TRACK AND REPAIRED PER SRM 51-40-2 AND 53-00-52. (M) 2 L 7 2 4F RT A16WE 1998082100570 19980821 00570 NM 1998 8 21 F3LA98090 1 19980623 A 5511 SPAR BOEING 737 737301 1384611 NM HORIZ STAB CORROSION A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURIGN C-CHECK INSPECTION, REPORTED CORROSION ON THREE AREAS OF LT HORIZONTAL STABILIZER UPPER REAR SPAR CHORD AT OUTBOARD END AND 24 INCHES AND 28 INCHES INBOARD FROM OUTBOARD END. MAINTENANCE BLENDED CORROSION, FABRICATED REPLACEME NT PARTS AND REPAIRED PER ER 98-0578, OHM 20-10-3, AND SRM 51-20-6 AND 55-10-0. (M) 2 L 7 2 4F RT A16WE 1998082100571 19980821 00571 NM 1998 8 21 F3LA98089 1 19980605 A 5320 ANGLE BOEING 737 737201 1384454 NM BS 353 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON MAIN EQUIPMENT BAY RIGHT INTERCOSTAL LOWER OUTBOARD SUPPORT ANGLE AT BS 353, RBL 12, WL 146. MAINTENANCE REPAIRED PER EO 98-0502. (M) 2 L 7 2 4F A16WE 1998082100572 19980821 00572 NM 1998 8 21 F3LA98086 1 19980529 A 5320 SPLICE BOEING 737 737201 1384454 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN BS 727 BULKHEAD TO FLOORBEAM SUPPORT SPLICE AFT FLANGE, LBL 25, WL 20 2. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-1, 51-10-2, 51-20-1 AND 51 -30-2. (M) 2 L 7 2 4F A16WE 1998082100573 19980821 00573 NM 1998 8 21 F3LA980529 1 19980529 A 5320 FRAME BOEING 737 737201 1384454 NM CARGO DOORWAY CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD CARGO DOOR UPPER AFT FRAME. MAINTENANCE REMOVED DAMAGED FRAM E. FABRICATED REPLACEMENT PART AND REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998082100574 19980821 00574 NM 1998 8 21 F3LA98084 1 19980529 A 5320 DOUBLER BOEING 737 737201 1384454 NM BS 270 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON INNER MOUNTING DOUBLER FOR FORWARD LAVATORY DRAIN TUBE, BS 270, S TRINGER 23R. MAINTENANCE REMOVED DAMAGED DOUBLER, FABRICATED REPLACMENT PART AND REPAIRED PER SRM 51-20-4, 51-30-2 AND 53-10-1. (M) 2 L 7 2 4F A16WE 1998082100575 19980821 00575 NM 1998 8 21 F3LA98083 1 19980529 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM BS 294 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK ON INTERCOSTAL, AFT SIDE AT BS 294.5 STRINGER 7L. MAINTENANCE REMOVED I NTERCOSTAL, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND 53-10-3 FIG 2. (M) 2 L 7 2 4F A16WE 1998082100576 19980821 00576 NM 1998 8 21 F3LA98081 1 19980529 A 5330 SKIN BOEING 737 737201 1384454 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK IN FORWARD ENTRY DOOR OUTER SKIN, LOWER HINGE CUTOUT, UPPER AFT CORNER. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SB 737-52-1096 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998082100577 19980821 00577 NM 1998 8 21 F3LA98108 1 19980623 A 5314 KEEL BEAM BOEING 737 737301 1384611 NM BS 594-639 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED 5 LONGITUDINAL BEAM NUT PLATE HOLES DAMAGED AT BS 594-639, RBL 25, WL 208 AT I NBOARD SIDE OF FLANGE. MAINTENANCE BLENDED CORROSION AT NUTPLTE HOLES AT BS 594 (1.5 INBH BY 1 INCH BY .032 INCH) BS 60 0 (1 INCH BY 7 INCH), BS 627 (.7 INCH BY .6 INCH), BS 649 (1.3 INCH BY .8 INCH), AND BS 639 (.5 INBH BY .5 INCH BY .002 INCH) AND REPAIRED PER ERO NR 98-0571. (M) 2 L 7 2 4F RT A16WE 1998082100578 19980821 00578 WP 1998 8 21 AALA981158 1 19980608 A 2170 21D101 COALESCER BAG DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 70401 49312 RDU - FLT 1287 - AFTER TAKEOFF RDU AN ODOR, LIKE BURNING RUBBER, ENTERED THE CABIN AND COCKPIT. RETURNED RDU AND LANDED WITHOUT INCIDENT. REPLACED BOTH COALESCER BAGS DUE TO OILY FILTHY CONDITION. ACCOMPLISHED REQUIRED PACK BURNOUT PROCE DURE PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. NO SMEL OR ODOR AFTER CHECK. (M) 2 L 7 2 4F A6WE 1998082100579 19980821 00579 WP 1998 8 21 TWAA9811903 1 19980713 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 587 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29R CRACKED JUST FORWARD ON STATION 587 FRAME. REMOVED AND REPLACED LONG ERON END PER DWG INST 592176 PER SRM 51-01 PAG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER DOUGLAS INST DWG 592176 AND S RM 51-60-0. (M) 2 L 7 2 4F A6WE 1998082100580 19980821 00580 WP 1998 8 21 TWAA9811902 1 19980708 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING OP 16 MAINTENANCE CHECK, FOUND FORWARD CABIN FLOOR PANEL NR 40 WITH HAT SECTIONS CRACKED IN SEVERAL PLACES. REPL ACED CRACKED HAT SECTIONS IN FLOOR PANEL NR 40 PER SRM 53-00-104, PAGE 201 FIG 201. (M) 2 L 7 2 4F A6WE 1998082100581 19980821 00581 WP 1998 8 21 TWAA9811901 1 19980723 A 3350 0105601003PA57 COVER DOUG DC9 DC983 3022083 WP CABIN DAMAGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9405T 53141 THE EGRESS LIGHT STRIP COVER WAS REPORTED DAMAGED AT CABIN ROW 7. REPLACED COVER, CHECK-C 11-16-97 MCI. (M) 2 L 7 2 4F RT A6WE 1998082100582 19980821 00582 WP 1998 8 21 TWAA9811801 1 19980721 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 902TW 49153 THE AFT EGRESS LIGHT STRIP, AFT OF LAST PAX SEAT, WAS INOP AND COVER BROKEN. REPAIRED LIGHT STRIP AND REPLACED LIGHT CO VER, CHECK-C 2-1-98 STL. (M) 2 L 7 2 4F A6WE 1998082100583 19980821 00583 WP 1998 8 21 TWAA9811802 1 19980722 A 2923 DC62E2410SN CONNECTOR DOUG DC9 DC982 3022082 WP PUMP SHORTED A TWAA K NONE A FLAME/FIRE IN INSP/MAINT 1 CE 05 951U 49245 DURING CHECK-C MAINTENANCE, WHILE OPERATING THE AUX HYD PUMP THE ELECTRICAL CONNECTOR ON THE PUMP SHORTED, BURNING THE C ONNECTOR CONTACTS AND CAUSING A SMALL FIRE AT THE CONNECTOR. REPLACED THE AUX HYD PUMP CONN AND THE PUMP. (M) 2 L 7 2 4F A6WE 1998082100584 19980821 00584 NM 1998 8 21 WRLA98088 1 19980711 A 3610 ARM7009508 LINE DOUG MD11 MD11F 3023600 NM NR 1 ENGINE LOOSE A WRLA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 274WA 48633 DURING TAXI FOR DEPARTURE, FLIGHT CREW RECEIVED NR 1 ENGINE BLEED 'INOP ALERT'. FLIGHT CREW ELECTED TO RETURN TO GATE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. NOTED ON LOG PAGE 100802. MAINTENANCE FOUND PNEUMATIC LINE LOOSE ON NR 1 ENGINE PNUEMATIC PILOT VALVE. RETORQUE FITTING. GROUND CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998082100585 19980821 00585 WP 1998 8 21 USAAD98119 1 19980708 A 5270 834003 SENSOR DOUG DC9 DC981 3022081 WP DOOR FRAME DAMAGED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 801US 48037 CLT - FLT 514 - AFTER TAKEOFF THE MID CARGO DOOR WARNING LIGHT ILLUMINATED AND THE CABIN WOULD NOT PRESSURIZE. THE AIRC RAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. LANDING WEIGHT WAS 129,300 LB. MAINTENANCE INSPECTED THE MID C ARGO DOOR FOR DAMAGE, NONE NOTED. HOWEVER, THE DOOR WARNING SENSOR WAS FOUND DAMAGED AND WAS REPLACED. THE PRESSURIZAT ION SYSTEM WAS TESTED PER THE MM. THE AIRCRAFT WAS PRESSURIZED SATISFACTORILY WITH NO EXCESSIVE HULL LEAKAGE NOTED. AN OVERWEIGHT LANDING CHECK WAS PERFORMED. (M) 2 L 7 2 4F A6WE 1998082100586 19980821 00586 EU 1998 8 21 USAAF98054 1 19980507 A 3231 200444004 DAMPER FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 860US 11295 PIT - FLT 434 - AFTER TAKEOFF FROM PIT, 'L MLG DOOR' MESSAGE APPEARED ON DISPLAY. CREW RECYCLED GEAR WITH SAME RESULT. FLT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN GEAR UPSTOP DAMPER. GEAR SWING WAS NORMAL. (M) 2 L 7 2 4F RT 1998082100587 19980821 00587 NM 1998 8 21 TWAA9810706 1 19980625 A 5751 AILERON BOEING 767 767231 1385131 NM RT WING CONTAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 LAX - DURING C-CHECK, MAINTENANCE FOUND ON RT WING TOP OF OUTBOARD AILERON WITH INDICATION OF WATER ON THE WHOLE SURFACE . AFTER WATER REMOVED, INSTALLED WET LAYUP PER SRM 51-70-17, PAGE 67 AND PAINTED AREAS. (M) 2 L 7 2 4F RT A1NM 1998082100588 19980821 00588 NM 1998 8 21 USAASB98168 1 19980703 A 3350 6104789 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 281AU 23114 RDU - MAINTENANCE FOUND THE RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY AND REPOSITIONED WIRE ON LIGHT SOCKET AT SERVICE DOOR. SYSTEM OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100589 19980821 00589 NM 1998 8 21 98ZZZM553 1 19980703 A 3350 6013211 POWER SUPPLY BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 281AU 23114 RDU - MAINTENANCE FOUND THE RIGHT AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE POWER SUPPLY AND REPOSITIONED WIRE ON LIGHT SOCKET AT SERVICE DOOR. SYSTEM OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100590 19980821 00590 NM 1998 8 21 USAASB98172 1 19980706 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 234US 22274 ALB - MAINTENANCE FOUND THE FOLLOWING EMERGENCY EVACUATION LIGHTS INOP, LEFT OVERWING EXIT HATCH SIDEWALL EXIT LIGHT, TH E LEFT OUTSIDE EXIT HATCH WING LIGHT AND THE LEFT GRUOND ILLUMINATION LIGHTS. MAINTENANCE REMOVED AND REPLACED THE BATT ERY PACK IN THE AFT CARGO BAY, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100591 19980821 00591 WP 1998 8 21 USAAD98122 1 19980710 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 PIT - THE LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE LIGHT AT ROW 16 WAS INOPERATIVE. MAINTENANCE REPLACED ALL THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE LIGHT ASSEMBLY AT ROW 16. (M) 2 L 7 2 4F A6WE 1998082100592 19980821 00592 WP 1998 8 21 98ZZZM554 1 19980710 A 3350 9731045 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 PIT - THE LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE LIGHT AT ROW 16 WAS INOPERATIVE. MAINTENANCE REPLACED ALL THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE LIGHT ASSEMBLY AT ROW 16. (M) 2 L 7 2 4F A6WE 1998082100593 19980821 00593 WP 1998 8 21 USAAD98121 1 19980712 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 956VJ 47588 IND - THE CEILING EMERGENCY LIGHTS AT ROWS 5 THROUGH 11 WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERIES. (M) 2 L 7 2 4F A6WE 1998082100594 19980821 00594 WP 1998 8 21 USAAD98120 1 19980712 A 3350 114597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 955VJ 47593 IND - THE TAIL COMPARTMENT CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES FOR THE TAIL COMPARTME NT CEILING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998082100595 19980821 00595 NM 1998 8 21 USAASB98165 1 19980630 A 3350 AD20311A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 391US 23313 PIT - MAINTENANCE FOUND THE MID CABIN CENTER AISLE EMERGENCY EXIT SIGN AND THE LEFT OVERWING EMERGENCY EXIT SIGN INOP. M AINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998082100596 19980821 00596 NM 1998 8 21 98ZZZM555 1 19980630 A 3350 20121 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 391US 23313 PIT - MAINTENANCE FOUND THE MID CABIN CENTER AISLE EMERGENCY EXIT SIGN AND THE LEFT OVERWING EMERGENCY EXIT SIGN INOP. M AINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND THE BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998082100597 19980821 00597 NM 1998 8 21 USAASB98151 1 19980617 A 3350 20121 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 505AU 23380 LGA - MAINTENANCE FOUND THE AFT SECTION OF FLOOR EMERGENCY LIGHTS INOP. MAINTENACE REMOVED AND REPLACED THE BATTERY CHA RGER AND BATERY PACK AND REPAIRED BURNED WIRES IN THE OVERHEAD ABOVE THE AFT GALLEY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998082100598 19980821 00598 NM 1998 8 21 98ZZZM556 1 19980617 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 505AU 23380 LGA - MAINTENANCE FOUND THE AFT SECTION OF FLOOR EMERGENCY LIGHTS INOP. MAINTENACE REMOVED AND REPLACED THE BATTERY CHA RGER AND BATERY PACK AND REPAIRED BURNED WIRES IN THE OVERHEAD ABOVE THE AFT GALLEY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998082100599 19980821 00599 NM 1998 8 21 USAASB98184 1 19980715 A 3350 POWER SUPPLY BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 423US 23990 CLE - MAINTENANCE FOUND THE EMERGENCY LIGHT POWER SUPPLY AT STATION 753L WILL NOT HOLD A CHARGE. MAINTENANCE REMOVED AN D REPLACED THE POWER SUPPLY AT STATION 753L. OPERATIONAL CHECK NORMAL 2 L 7 2 4F RT A16WE 1998082100600 19980821 00600 NM 1998 8 21 USAASB98182 1 19980713 A 3350 S106 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 229US 21818 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT LEFT SERVICE DOOR INOP DURING THE TRANSIT CHECK. MAINTEN ANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100601 19980821 00601 NM 1998 8 21 USAASB98180 1 19980712 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM COCKPIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 224US 21666 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT IN THE COCKPIT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMB LY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100602 19980821 00602 NM 1998 8 21 USAASB98175 1 19980710 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 235US 22275 ALB - MAINTENANCE FOUND THE AFT ENTRY AND AFT SERVICE DOOR EXTERIOR EVACUATION LIGHTS AND THE INTERIOR SIDEWALL EMERGENC Y EXIT SIGNS BY EACH DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE RIGHT SIDE OF THE AFT CARGO CO MPARTMENT BEHIND THE COCKPIT VOICE RECORDER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082100603 19980821 00603 WP 1998 8 21 TWAA9810612 1 19980619 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP16 MAINTENANCE CHECK, FOUND FWD ENTRY DOOR AREA LONGERON CRACKED AT STATION 200, L2L. REMOVED CRACKED LO NGERON. INSTALLED NEW LONGERON PER SRM 51-06, PAGE 1, ITEM C, AND INSTALLED FASTENERS PER SRM 51-30-05. (M) 2 L 7 2 4F A6WE 1998082100604 19980821 00604 WP 1998 8 21 TWAA9810611 1 19980622 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 699 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP16 MAINTENANCE CHECK, EDDY CURRENT INDICATED .125 INCH LONG CRACK RUNNING AFT FROM UNDER RIVET RBL 13 IN, STATION 699, TOP FUSELAGE SKIN. ACCOMP HFEC PER SRM 51-00-2 FOR CRACK CONTAINMENT. NO CRACK INDICATED. REPAIRED PER DAC REWORK DRAWING SR09530129 AS PER WORK SHEET MC8-AD-AM, ITEM 6. (M) 2 L 7 2 4F A6WE 1998082100605 19980821 00605 WP 1998 8 21 TWAA9810610 1 19980624 A 5712 RIB DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND A CRACK IN AFT FASTENER RIB, 18 IN OUTBOARD OF NR 5 SLAT CENTER TRACK RIB IN LE OF LEFT WING. REPLACED RIB PER SRM 51-01, PAGE 1 ITEM C. REPLACED HI-LOKS PER SRM 51-30-5. REPLACED RIVETS PER S RM 51-30-5. (M) 2 L 7 2 4F A6WE 1998082100606 19980821 00606 WP 1998 8 21 TWAA9810609 1 19980618 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT SEVENTH FASTENER ABOVE LAP SEAM, LONGERON 14, AT FS 1076 ABOVE RT E NGINE PYLON. CRACK IN BEYOND STOP DRILL, UNDER PREVIOUS REPAIR. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 53-04, FIG 18. (M) 2 L 7 2 4F A6WE 1998082100607 19980821 00607 WP 1998 8 21 TWAA9810608 1 19980618 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 604 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SUPPORT ANGLE TO FRONT SPAR CRACKED AT BULKHEAD STATION 604, BETWEEN LONGERO N 23R AND 24R. REPLACED CRACKED SUPPORT ANGLE, PER SRM 51-01 PAGE 1, ITEM C, AND INSTALLED FASTENERS PER SRM 51-30-2. ( M) 2 L 7 2 4F A6WE 1998082100608 19980821 00608 WP 1998 8 21 TWAA9810607 1 19980618 A 5320 FASTENERS DOUG DC9 DC932 3022066 WP BS 700 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STATION 700, LEFT SIDE, BOTTOM AND TOP FORWARD FASTENERS ON INNER STRINGE R FRAME THAT HOLDS WINDOW INNER SEAL SPACER RUBBER, CRACKED. INNER FRAME REMOVED AND NEW FRAME INSTALLED PER SRM 51-01, PAGE 1 ITEM C. (M) 2 L 7 2 4F A6WE 1998082100609 19980821 00609 WP 1998 8 21 TWAA9801606 1 19980617 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 MCI - DURIN GOP 16 MAINTENANCE CHECK, FOUND LEFT WING TE FIXED UPPER WING PANEL CRACKED AT REAR SPAR, JUST FORWARD AND I NBOARD OF INBOARD SPOILER. ACCOMP HFEC CRACK CONTAINMENT PER TWA NDT PART 6 AND 51-00-03. STOP DRILLED END OF CRACK PE R SRM 57-01 AND INSTALLED DOUBLER REPAIR PER SRM 51-01, FIG 23 SHEET 2, PAGE 8. (M) 2 L 7 2 4F A6WE 1998082100610 19980821 00610 WP 1998 8 21 TWAA9810605 1 19980617 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION TOP SIDE OF FLOORBEAM, STATION 996 RBL 22 IN TO RBL 50 INC H. REPLACED ANGLE PER SRM 51-01 AND STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998082100611 19980821 00611 WP 1998 8 21 TWAA9810604 1 19980617 A 5312 BULKHEAD DOUG DC9 DC932 3022066 WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND TIE ANGLE FOR FLOORBEAM, FORMER RING AND PRESSURE BULKHEAD CRACKED AT STATIO N 996, RBL 58.6 INCHES. VERIFIED BY NDT. REPLACED TIE PALTE PER SRM 51-01 AND STD PRACTICES. (M) 2 L 7 2 4F A6WE 1998082100612 19980821 00612 WP 1998 8 21 TWAA9810603 1 19980601 A 5240 SKIN DOUG DC9 DC951 3022051 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 414EA 47746 STL - DURING CHECK-C MAINTENANCE, FOUND RT FORWARD SERVICE DOOR WITH .25 INCH IN CRACK IN UPPER AFT CORNER OF DOOR. INS TALLED DOUBLER PER SRM 52-05 FIG 25. (M) 2 L 7 2 4F RT A6WE 1998082100613 19980821 00613 WP 1998 8 21 TWAA9810602 1 19980704 A 3350 14597101 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 924L 47324 STL - DURING MAINTENANCE CHECK, FOUND SEVERAL OVERHEAD EMERGENCY LIGHTS INOP IN CABIN AISLE, AND RT AFT OVERWING EXIT LI GHT INOP. REPLACED CELL PACK B5-25. CHECK-C, 8-6-97 MCI. (M) 2 L 7 2 4F A6WE 1998082100614 19980821 00614 WP 1998 8 21 TWAA9810601 1 19980705 A 3350 LIGHT DOUG DC9 DC934 302207E WP CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 928L 48124 STL - FLT 655 - AFT THIRD OF CABIN FLOOR ESCAPE PATH LIGHT INTERMITTENTLY CAME ON IN FLIGHT. RESEATED RIBBON ON FLOOR E SCAPE LIGHTS. CHECK-C 3-22-98 STL. (M) 2 L 7 2 4F RT A6WE 1998082100615 19980821 00615 WP 1998 8 21 TWAA9810504 1 19980702 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9412W 53187 EWR - FLT 707 - DURING PREFLIGHT, FOUND EGRESS LIGHTS INOPERATIVE AT ROW 21 SIDE. RELAMPED AND REPLACED LENS AND REPAIR ED TRACK COVER. (M) 2 L 7 2 4F RT A6WE 1998082100616 19980821 00616 WP 1998 8 21 TWAA9810503 1 19980701 A 3320 LIGHT DOUG DC9 DC982 3022082 WP CABIN SMOKING A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 05 912TW 49183 STL - FLT 603 - DURING TAKEOFF, CABIN ATTENDANT NOTICED SMOKE AT OVERHEAD GALLEY LIGHT. REPLACED LAMP. SUSPECTED OVEN RESIDUE. (M) 2 L 7 2 4F A6WE 1998082100617 19980821 00617 NM 1998 8 21 TWAA9810502 1 19980630 A 3350 LIGHT BOEING 727 727231 1384079 NM CABIN LOOSE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54344 21631 JFK - FLT 361 - EGRESS FLOOR STRIP LIGHTING COMING LOOSE AT ROW 15 LEFT SIDE. FLOOR STRIP WAS SECURED. (M) 2 L 7 3 4F A3WE 1998082100618 19980821 00618 NM 1998 8 21 TWAA9810501 1 19980630 A 3397 WIRE BOEING 767 7673Y0 NM CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 JFK - FLT 884 - DURING ROUTINE GROUND MAINTENANCE, FOUND EGRESS LIGHTS AT THE FORWARD GALLEY RT AISLE SIDE. REPAIRED A BROKEN WIRE. (M) 2 L 7 2 4F RT A1NM 1998082100619 19980821 00619 EU 1998 8 21 SIMA981981 1 19980717 A 5320 S5367121701200 BRACKET AEROSP ATR72 ATR72212 EU BS 36-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR HANDRAIL BRACKET, TEE FITTING ON PAX DOOR SILL PLATE A ND FLOOR SUPPORT BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED ALL THREE ITEMS IAW SRM 51-25-02. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082100620 19980821 00620 EU 1998 8 21 98ZZZM557 1 19980717 A 5320 S5367129034801 TEE FITTING AEROSP ATR72 ATR72212 EU BS 36-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR HANDRAIL BRACKET, TEE FITTING ON PAX DOOR SILL PLATE A ND FLOOR SUPPORT BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED ALL THREE ITEMS IAW SRM 51-25-02. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082100621 19980821 00621 EU 1998 8 21 98ZZZM558 1 19980717 A 5320 S5367800826801 SUPPORT AEROSP ATR72 ATR72212 EU BS 36-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 355AT 355 SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE PAX DOOR HANDRAIL BRACKET, TEE FITTING ON PAX DOOR SILL PLATE A ND FLOOR SUPPORT BETWEEN FRAMES 36 AND 39 CORRODED. MAINTENANCE REMOVED AND REPLACED ALL THREE ITEMS IAW SRM 51-25-02. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082100622 19980821 00622 EU 1998 8 21 REXA98103 1 19980618 A 2150 PACK SAAB SF340 340B 7860101 EU CABIN DEFECTIVE A REXA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 25 364PX 340B262 STRONG SMOKE ODOR IN COCKPIT AND CABIN (NO DETECT ON CWP) FLOWS BLOW EXTREMELY HOT ON LAST TEN MINUTES OF FLT. GROUND R AN BOTH ENGINES. LEFT BLEED CHECKS GOOD IN AUTO AND MANUAL MODE. RT BLEED BLOWS HOT. DEFER RT AIR CONDITIONING PACK P ER MEL 21-50-01 CAT C PER D. PLACARD INSTALLED. NO SMOKE ODOR NOTED. (M) 2 L 7 2 4T RT A52EU 1998082100623 19980821 00623 EU 1998 8 21 REXA98105 1 19980703 A 3260 SWITCH SAAB SF340 SF340A 7850100 EU NLG OUT OF ADJUST A REXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 401BH 340A057 WHEN GEAR SELECTED UP, AMBER LIGHT IN HANDLE STAYS ON. ADJUSTED NOSE DOWNLOCK SWITCH. (M) 2 L 7 2 4T RT A52EU 1998082100624 19980821 00624 SO 1998 8 21 MASA98142 1 19980707 A 3350 3071BPE BULB EMB 120 EMB120RT SO CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 180YV 120180 DURING ROUTINE MAINTENANCE, FOUND ONE BULB IN THE EMERGENCY FLOOR TRACK LIGHTING AT SEAT 5A WOULD NOT ILLUMINATE. REMOV ED AND REPLACED BULB. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1998082100625 19980821 00625 SO 1998 8 21 MASA98141 1 19980710 A 3350 12021299001 LIGHT EMB 120 EMB120ER 3260203 SO FUSELAGE INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 298YV 120298 DURING ROUTINE MAINTENANCE, FOUND RT AFT EXTERNAL EMERGENCY LIGHT ABOVE INBOARD FLAP WOULD NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A31SO 1998082100626 19980821 00626 NM 1998 8 21 EIAA0211 1 19980619 A 2611 21562B SMOKE DETECTOR BOEING 747 747273C 1384896 NM CARGO BAY FAILED A EIAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 09 471EV 20651 FJR - LOG PAGE: F80971 - ON CLIMB-OUT, FORWARD LOWER CARGO COMPARTMENT FIRE LIGHT ILLUMINATED. NO CARGO LOADED. NO SM OKE OR FIRE OBSERVED. RETURNED TO FJR. REPLACED FORWARD LOWER CARGO AFT SMOKE DETECTOR, AND OPS CHECKED SYSTEM PER MM 26-14-02. (X) 2 L 7 4 4F A20WE 1998082100627 19980821 00627 NE 1998 8 21 DKAA98008 2 19980610 A 7230 COMPRESSOR AMD FALC20 FALCOND 2720304 EU GE CF700 CF7002D 30010 NE NR 1 ENGINE FOD A DKAA A E UNSCHED LANDING ENGINE SHUTDOWN C X F.O.D. ENGINE FLAMEOUT TO TAKEOFF 1 GL 23 226R 10757 245372 226 245372 NR 1 ENGINE FLAMED OUT DURING FIRST POWER REDUCTION AFTER TAKEOFF. FOUND NR 1 ENGINE TO HAVE COMPRESSOR FOD. REPLACED NR 1 ENGINE PER RAI CARD NR 1-7100-01 AND AMD 71-00-01. OPERATIONAL AND LEAK CHECKS GOOD ON GROUND RUN (IND). AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F 4 F A7EU E7EA 1998082100628 19980821 00628 EU 1998 8 21 USAAF98058 1 19980720 A 2133 1313745 AIR FILTER FOKKER F28 F28MK0100 4990807 EU E/E BAY CONTAMINATED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 893US 11373 CLT - FLT 2053 - EN ROUTE PHL/BNA, AT FL 310, CREW RECEIVED THE CABIN PRESSURE CONTROL CHANNEL FAULT MESSAGE ON THE MFDU . THE CABIN ALTITUTDE BEGAN TO CLIMB AT APPROXIMATELY 2,000 FPM. THE CREW COULD NOT SATISFACTORILY CONTROL THE PRESSUR IZATION IN MANUAL MODE. THE FLIGHT DESCENDED AND THEN DIVERTED TO CLT, AND LANDED WITH NO FURTHER INCIDENT. MAINTENANC E FOUND THE OUTFLOW VALVE FILTER IN ZONE 165 CONTAMINATED AND REPLACED IT. (X) 2 L 7 2 4F RT 1998082100629 19980821 00629 EU 1998 8 21 USAAF98057 1 19980718 A 3230 MLG FOKKER F28 F28MK0100 4990807 EU MLG WW FAILED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 882US 11334 PIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RESULT. FLIGHT RETURNED TO PIT. ON APPROACH TO PIT, CREW USED THE ALTERNATE GEA R EXTENSION PROCEDURE. ALL GEAR EXTENDED NORMALLY. FLIGHT LANDED PIT WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F RT 1998082100630 19980821 00630 EU 1998 8 21 98ZZZX2863 1 19980718 A 5280 A11320425 DOOR FOKKER F28 F28MK0100 4990807 EU LT MLG DAMAGED A USAA A UNSCHED LANDING O OTHER AP APPROACH 1 EA 19 882US 11334 PIT - FLT 671 - ON APPROACH TO CRW WHEN THE LANDING GEAR WAS SELECTED DOWN, THE MAIN LANDING GEAR DID NOT EXTEND. CREW RECYCLED THE GEAR HANDLE WITH THE SAME RESULT. FLIGHT RETURNED TO PIT. ON APPROACH TO PIT, CREW USED THE ALTERNATE GEA R EXTENSION PROCEDURE. ALL GEAR EXTENDED NORMALLY. FLIGHT LANDED PIT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND TURN BUCKLE MISSING FROM RMLG SEQUENCING VALVE. THEY REPLACED THE TURNBUCKLE. MAINTENANCE ALSO FOUND THE LMLG GEAR DOOR DAM AGED DUE TO ALTERNATE EXTENSION PROCEDURE. THEY REPLACED THE DOOR. TURNBUCKLE: MPN A82670-401. GEAR DOOR: MPN A11320 -425. REF: OPERATOR CONTROL NR USAAF98057. 2 L 7 2 4F RT 1998082100631 19980821 00631 WP 1998 8 21 USAAD98128 1 19980720 A 3230 VALVE PULLEY DOUG DC9 DC931 3022065 WP MLG BLOCKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 912VJ 47020 PIT - FLT 972 - AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE GEAR WAS CYCLED TWICE, BUT WOULD NOT RETRACT. T HE FLIGHT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPOSITIONED A TEMPORARY HYDRAULIC LINE IN THE RIGHT WHEEL WELL THAT WAS CATCHING ON THE LANDING GEAR CONTROL VALVE PULLEY. (X) 2 L 7 2 4F A6WE 1998082100632 19980821 00632 NM 1998 8 21 USAA980318 1 19980726 A 5311 654659588 FRAME BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 37440 23314 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1.50 INCH CRACK 727D BETWEEN STRINGERS 27 LT AND RT OF FRAME. INSTALL ED DOUBLER, NEW SHEAR TIES AND FLOOR ANGLE SUPPORTS PER SRM 53-00-07 FIG 203. (X) 2 L 7 2 4F RT A16WE 1998082100633 19980821 00633 NM 1998 8 21 USAA980319 1 19980726 A 5315 6545818510 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 37440 23314 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 4 INCH AREA OF CORROSION TOP OF FLANGE FLOORBEAM AT STA 312 RBL 30. C ORROSION TASK NR C53-107-01. INSTALLED SPLICE PER SRM 53-10-03. (X) 2 L 7 2 4F RT A16WE 1998082100634 19980821 00634 NM 1998 8 21 USAA980320 1 19980726 A 5315 6545818510 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 392US 37440 23314 CLT - DURING Q-3 CHECK VISUAL INSPECTION FOUND A 4 INCH BY 4 INCH CORROSION TOP OF FLANGE STA 312 CENTERLINE FLOORBEAM. CORROSION TASK NR C 53-107-01. INSTALLED SPLICE PER REPAIR DOCUMENT SRM 53-10-03. (X) 2 L 7 2 4F RT A16WE 1998082100635 19980821 00635 NM 1998 8 21 USAASB98192 1 19980725 A 2121 215201 FAN BOEING 737 7372B7 1384560 NM A/C BAY FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 277AU 22889 MIA - FLT 2649 - CAPTAIN REPORTED A SULFUR SMELL IN CABIN DURING FINAL APPROACH INTO MIA. MAINTENANCE FOUND THE GASPER FAN CIRCUIT BREAKER POPPED, AND REPLACED THE FAN. (M) 2 L 7 2 4F A16WE 1998082100636 19980821 00636 NM 1998 8 21 USAASB98189 1 19980722 A 2121 5007024620 FAN BOEING 737 7372B7 1384560 NM RT PACK FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 286AU 29666 23133 JAX - FLT 2606 - EN ROUTE FLL/BWI, CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. CREW SECURED THE GASPER FAN AND RIGHT PACK. THE SMOKE APPEARED TO ABATE. FLIGHT DIVERTED TO JAX AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE GASPER FAN CIRCUIT BREAKER TRIPPED AND THE FAN AT FAULT FOR THE PROBLEM. THE FAN WAS REPLACED. (X) 2 L 7 2 4F A16WE 1998082100637 19980821 00637 NM 1998 8 21 USAA980314 1 19980718 A 5330 SKIN BOEING 737 737201 1384454 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 40302 22866 CLT - DURING VISUAL CHECK INSPECTION, FOUND A 2.25 INCH CRACK AT BS 767 AND STR 19R ON SKIN. TRIMMED OUT DAMAGE AND INS TALLED DOUBLER PER SRM 53-30-3 FIGURE 1. (X) 2 L 7 2 4F A16WE 1998082100638 19980821 00638 NM 1998 8 21 USAA980262 1 19980711 A 5330 SKIN BOEING 737 737201 1384454 NM BS 757 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 256AU 40920 22798 PHL - DURING RON, FOUND SMALL 1 INCH CRACK VERIFIED BY DYE CHECK ON SKIN ABOVE STR 18R AND STA 757 JUST AFT OF WING-TO-B ODY FAIRING. INSTALLED EXTERNAL REPAIR PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1998082100639 19980821 00639 NM 1998 8 21 USAASB98179 1 19980711 A 7930 1163P181 SWITCH BOEING 737 737201 1384454 NM NR 1 FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 232US 2057 22018 BOS - FLT 921 - ON CLIMB-OUT FROM BOS, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. ENGINE WAS BROUGHT BACK TO IDLE AND AN EMERGENCY WAS DECLARED. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS S HUT DOWN AFTER LANDING. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE OIL FILTER (P/N 056306-06). NO CONTAMINATION WAS FOUND. REMOVED AND REPLACED THE NR 1 ENGINE OIL FILTER BYPASS SWITCH. RAN ENGINE. OPS CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998082100640 19980821 00640 NM 1998 8 21 USAA980302 1 19980714 A 5320 68353521 TIE CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STA 807 STR 10R TIE CLIP. REPLACED CLIP PER EO 539 3G227 (AD 93-08-04, SB 737-53-1085). (X) 2 L 7 2 4F A16WE 1998082100641 19980821 00641 NM 1998 8 21 USAA980303 1 19980714 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .025 INCH CRACK AT STA 727B, STRINGER 1 FRAME TO TIE CLIP. REPLACED C LIP PER EP 5393G227 (AD 93-08-04, SB 737-53-1085). (X) 2 L 7 2 4F A16WE 1998082100642 19980821 00642 NM 1998 8 21 USAA980304 1 19980714 A 5320 69414371 CLIP BOEING 737 7372B7 1384560 NM BS 664 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING A Q-6 CHECK VISUAL INSPECTION, FOUND A .025 INCH CRACK AT STA 664, STR 10L, FRAME TIE CLIP. REPLACED CLIP PER EO 5393G227 (AD 93-08-04, SB 737-53-1085. (X) 2 L 7 2 4F A16WE 1998082100643 19980821 00643 NM 1998 8 21 USAA980297 1 19980622 A 5315 FLOORBEAM BOEING 737 737201 1384454 NM BS 1008 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 46491 22275 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1.3750 INCH AREA OF CORROSION ON FLOORBEAM STA 106 LBL 18. I NSTALLED T-CAP PER TR 53-10-05C. (X) 2 L 7 2 4F A16WE 1998082100644 19980821 00644 NM 1998 8 21 USAA980295 1 19980703 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 41064 22888 CLT - DURING CX-2 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN SKIN RIGHT AFT SERVICE DOOR LOWER HINGE CUT-OUT. INSTAL LED DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 33. (X) 2 L 7 2 4F A16WE 1998082100645 19980821 00645 NM 1998 8 21 USAA980301 1 19980703 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 41064 22888 CLT - DURING CX-2 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN SKIN RT AFT SERVICE DOOR LOWER HINGE CUT-OUT ON SKIN. I NSTALLED DOUBLER AND TRIPPLER PER SRM 53-30-3 FIG 33. (X) 2 L 7 2 4F A16WE 1998082100646 19980821 00646 NM 1998 8 21 USAA980296 1 19980703 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 276AU 41058 22888 CLT - DURING A DROP-IN VISUAL INSPECTION, FOUND A CRACK AT FORWARD ENTRY DOOR SKIN AT LOWER AFT CUT-OUT. INSTALLED DOUB LER/TRIPLER PER EA 41616. (X) 2 L 7 2 4F A16WE 1998082100647 19980821 00647 NM 1998 8 21 TAOA079809 1 19980716 A 2612 356644400 FIRE LOOP BOEING 727 727254 138408L NM LT/RT MLG WW MALFUNCTIONED A TAOA E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 15 916TS 20437 FLT 6480 - DCA-LGA - WHEEL WELL FIRE WARNING LIGHT CAME ON IN FLIGHT FOLLOWED EMERGENCY PROCEDURES. REPLACED NOSE WHEEL WELL FIRE LOOP ALSO REPLACED MAIN LEFT AND RIGHT WHEEL WELL FIRE LOOP. REPLACED FIRE AND OVERHEAT CONTROL BOX. PERFOR MED RESISTANCE CHECK FROM WHEEL WELLS TO FIRE OVERHEAT CONTROL BOX. OPERATION CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998082100648 19980821 00648 CE 1998 8 21 98ZZZX2864 1 19980719 A 3260 SWITCH BEECH 1900 1900C 1154161 CE NLG OUT OF ADJUST A GUUA K NONE O OTHER NR NOT REPORTED 1 SO 19 154GA UB25 PBI/MIA - FLT 9319 - NOSE GEAR LIGHT ILLUMINATED APPROXIMATELY 1-1/2 MINUTES AFTER MAIN GEAR WITH GEAR SELECTED DOWN. A IRCRAFT LANDED SAFELY. ADJUSTED NOSE GEAR MICROSWITCH. 2 L 7 2 4T RT A24CE 1998082100649 19980821 00649 CE 1998 8 21 98ZZZX2865 1 19980716 A 2150 ACM BEECH 1900 1900 1154160 CE LT WING MALFUNCTIONED A GUUA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SO 19 194GA UB8 RSW/MIA - FLT 9283 - ON TAKEOFF, SMOKEY SMELL WHEN ACM IS SELECTED. SMELL DISSIPATED AFTER 30 SECONDS. RAN AIRCRAFT EN GINES WITH ACM RUNNING. COULD NOT DUPLICATE. (X) 2 L 7 2 4T RT A24CE 1998082100650 19980821 00650 CE 1998 8 21 98ZZZX2866 1 19980710 A 3260 SWITCH BEECH 1900 1900C 1154161 CE MLG OUT OF ADJUST A GUUA K NONE O OTHER NR NOT REPORTED 1 SO 19 154GA UB25 MIA/TPA - FLT 9440 - NOSE GEAR INDICATOR DID NOT ILLUMINATE WHEN GEAR WAS SELECTED DOWN. AIRCRAFT LANDED SAFELY AND WAS FERRIED TO MIA. ADJUSTED NOSE GEAR DOWNLOCK SWITCH. (X) 2 L 7 2 4T RT A24CE 1998082100651 19980821 00651 CE 1998 8 21 98ZZZX2867 1 19980716 A 3230 1003810061 SWITCH BEECH 1900 1900C 1154161 CE MLG FAILED A GUUA K NONE O OTHER NR NOT REPORTED 1 SO 19 155GA UB55 JAX/TPA - FLT 9461 - LANDING GEAR INDICATOR TRIPPED AND COULD NOT RESET. REMOVED AND REPLACED NOSE LANDING GEAR DOWNLOC K SWITCH. (X) 2 L 7 2 4T RT A24CE 1998082100652 19980821 00652 CE 1998 8 21 98ZZZX2868 1 19980624 A 5410 1149800211 KEEL BEECH 1900 1900C 1154161 CE LT NACELLE DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 195GA 25503 UB65 AT SCHEDULED INSPECTION, DETERMINED THE LEFT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVIC E BULLETIN 54-3071 PART II. VISUAL INSPECTIONS PROVED SATISFACTORY PER PART I OF SAME BULLETIN. SCHEDULED REPETITIVE V ISUAL INSPECTIONS UNTIL KEEL IS REPLACED. SCHEDULED KEEL REPLACEMENT PER RAYTHEON SB 54-3071. (X) 2 L 7 2 4T RT A24CE 1998082100653 19980821 00653 CE 1998 8 21 98ZZZX2869 1 19980521 A 7120 118910025121 MOUNT BEECH 1900 1900C 1154161 CE NR 2 NACELLE CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 155GA UB55 DURING R.O.N. INSPECTION, APPROXIMATELY 1 INCH CRACK WAS FOUND ON FORWARD UPPER INBOARD SUPPORT TUBE ON NR 2 ENGINE TRUS S MOUNT. PERFORMED WELD REPAIR IAW FAA APPROVED DATA FOUND IN BEECHCRAFT SRM. (X) 2 L 7 2 4T RT A24CE 1998082100654 19980821 00654 CE 1998 8 21 98ZZZX2870 1 19980524 A 3230 H111541 SWITCH BEECH 1900 1900C 1154161 CE COCKPIT FAILED A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 19 153GA UB34 TPA/MIA - FLT 7485 - LANDING GEAR INDICATOR CIRCUIT BOARD TRIPS WHEN GEAR RETRACTS AND WILL NOT RESET UNTIL GEAR IS DOWN AND LOCKED. REMOVED AND REPLACED GEAR UP LIMIT SWITCH. (X) 2 L 7 2 4T RT A24CE 1998082100655 19980821 00655 CE 1998 8 21 98ZZZX2871 1 19980519 A 2810 10138901165 VALVE BEECH 1900 1900C 1154161 CE PURGE TANK INOPERATIVE A GUUA O OTHER O OTHER NR NOT REPORTED 1 SO 19 86UE UC86 TCB/MIA - FLT 7253 - PILOT DISCREPANCY: FUEL SMELL DURING ATTITUDE CHANGES. REMOVED AND REPLACED FUEL PURGE TANK, CHEC K VALVE. (X) 2 L 7 2 4T RT A24CE 1998082100656 19980821 00656 CE 1998 8 21 98ZZZX2872 1 19980719 A 3260 1145801141 LINE BEECH 1900 1900C 1154161 CE MLG WW CRACKED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 197GA UB16 TCB/MIA - FLT 9138 - GEAR WARNING INOPERABLE. REMOVED AND REPLACED MANUAL BLEED VALVE LINE AT LANDING GEAR POWER PACK. (X) 2 L 7 2 4T RT A24CE 1998082100657 19980821 00657 CE 1998 8 21 98ZZZX2873 1 19980720 A 3233 1123802223 ACTUATOR 503 BEECH 1900 1900C 1154161 CE NLG FAILED A GUUA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 154GA UB25 FPO/FLL - FLT 9149 - NOSE GEAR INDICATOR FAILED TO ILLUMINATE WITH GEAR EXTENDED. AIRCRAFT LANDED SAFELY AND WAS FERRIE D TO MIAMI. REMOVED AND REPLACED NOSE GEAR ACTUATOR. (X) 2 L 7 2 4T RT A24CE 1998082100658 19980821 00658 CE 1998 8 21 98ZZZX2874 1 19980716 A 3260 35133790007 ANNUNCIATOR BEECH 1900 1900C 1154161 CE COCKPIT MALFUNCTIONED A GUUA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 154GA UB25 TPA/TLH - FLT 9197 - NOSE GEAR LIGHT WOULD NOT ILLUMINATE WITH GEAR SELECTED DOWN. AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED GEAR DOWN AND LOCKED ANNUNCIATOR. (X) 2 L 7 2 4T RT A24CE 1998082100659 19980821 00659 NM 1998 8 21 GAIA9871 1 19980717 A 3260 656021132 ACCESSORY UNIT BOEING 727 727214 138407R NM E/E BAY INOPERATIVE A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 750US 21512 OKC - DURING SCHEDULED TEST FLIGHT AFTER C-CHECK WHEN GEAR WAS RETRACTED, RT GEAR UNSAFE LIGHT (RED) REMAINED ON. THE C REW THEN RECYCLED THE GEAR AND THE LIGHT REMAINED ILLUMINATED. RIGHT HAND GEAR UNSAFE LIGHT EXTINGUISHED ON GEAR EXTENS ION, AND ALL INDICATIONS SHOW NORMAL. THE CREW THEN LANDED BACK AT OKC AND MADE A SAFE AND UNEVENTFUL LANDING. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. CARRIED OUT GEAR SWING IAW BOEING MM 32-30, GROUND CHECKED NORMAL. THE AIRC RAFT WAS THEN RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998082100660 19980821 00660 EU 1998 8 21 C2XA98BT051 1 19980717 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 BTV - DURING 2A INSPECTION, FOUND EMERGENCY LIGHTS FAILED TEST WITH SWITCH 2WL IN 'ARM' POSITION. REMOVED AND REPLACED BATTERY PACK WITH SERVICEABLE UNIT. OPERATIONALLY CHECKED GOOD. (X) 2 H 7 2 4T RT A53EU 1998082100661 19980821 00661 EU 1998 8 21 C2XA98BT052 1 19980716 A 2911 FITTING AEROSP ATR42 ATR42320 8680930 EU HYD SYSTEM LEAKING A C2XA O OTHER K FLUID LOSS CL CLIMB 1 SW 09 15827 175 EWR - CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT, GREEN HYDRAULIC LO-LEVEL LIGHT ILLUMINATED. MAINTENANCE FOUND L EAKING 'TEE' FITTING AT THE GREEN HYDRAULIC ACCUMULATOR. REMOVED AND REPLACED WITH SERVICEABLE UNIT. OPS CHECKED/LEAK CHECKED GOOD ON GEAR RETRACTION. (X) 2 H 7 2 4T RT A53EU 1998082100662 19980821 00662 EU 1998 8 21 C2XA98IA266 1 19980720 A 3397 3351214CF20 WIRE AEROSP ATR42 ATR42500 EU CABIN BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING MAITNENANCE VISIT INSPECTION, THE LOWER LEFT HAND AFT EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. MAINTENAN CE REPAIRED WIRE NR 3351214CF20, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998082100663 19980821 00663 SO 1998 8 21 C2XA98IA275 1 19980720 A 3234 12038594001 GEAR HANDLE EMB 120 EMB120RT SO COCKPIT INOPERATIVE A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 15721 120160 IAH - FLT 3994 - DURING FLIGHT, PILOT REPORTED THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT I NCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE GEAR HANDLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X ) 2 L 7 2 4T RT A31SO 1998082100664 19980821 00664 EU 1998 8 21 C2XA98IA267 1 19980717 A 5210 S52176404200 FRAME AEROSP ATR42 ATR42320 8680930 EU PASSENGER DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR STEP FRAME WAS FOUND CRACKED IN THE CENTER UNDER PANEL 834BZ. MAINT ENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR 42 SRM 51-71-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998082100665 19980821 00665 EU 1998 8 21 C2XA98IA268 1 19980717 A 5320 S53678008268 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT AT FRAME 36 WAS FOUND CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA S AND APPLIED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998082100666 19980821 00666 EU 1998 8 21 C2XA98IA269 1 19980717 A 5311 S5367134820001 FRAME AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, FRAME 37 WAS FOUND CORRODED ABOVE AND BELOW THE CREASE BEAM ON THE RIGHT HAND SIDE. MA INTENANCE REMOVED THE CORROSION AND APPLIED REPAIR DOUBLERS IAW AIR REPAIR DRAWING 16S536R0054, AND THE AIRCRAFT WAS APP ROVED FOR RETURN TO SERVICE. AIRCRAFT TT: 23,397 HOURS. CYCLES: 24,780. (X) 2 H 7 2 4T RT A53EU 1998082100667 19980821 00667 EU 1998 8 21 C2XA98IA270 1 19980717 A 5320 S5367131831001 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOVED THE CORROSION, AN D APPLIED REPAIR DOUBLERS IAW ATR42 SRM'S 51-21-42, 51-70-00, AND 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 23,397. CYCLES: 24,780. (X) 2 H 7 2 4T RT A53EU 1998082100668 19980821 00668 EU 1998 8 21 C2XA98IA271 1 19980717 A 5320 S5367121729801 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, THE U-CHANNEL UNDER THE PASSENGER DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOV ED AND REPLACED THE U-CHANNEL IAW ATR42 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 33 ,397 HOURS. CYCLES: 24,780. (X) 2 H 7 2 4T RT A53EU 1998082100669 19980821 00669 EU 1998 8 21 C2XA98IA272 1 19980717 A 5320 S53681004204 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, THE U-CHANNEL FLOOR SUPPORT BEAM BETWEEN FRAMES 39 AND 40 ON THE LEFT HAND SIDE OF THE FUSELAGE WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT BEAM IAW ATR42 SRM 51-70-00, AND SRM 52-25-02 , AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT T: 23,397 HOURS. CYCLES: 24,780. (X) 2 H 7 2 4T RT A53EU 1998082100670 19980821 00670 EU 1998 8 21 C2XA98IA273 1 19980717 A 5320 S53672406208 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14813 100 IAH - DURING C-CHECK INSPECTION, THE FLOOR SUPPORT BEAM BETWEEN FRAMES 36 AND 38 WAS FOUND CORRODED. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED FLOOR SUPPORT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ACFT TT: 23,397 HOURS. CYCLES: 24,780. (X) 2 H 7 2 4T RT A53EU 1998082100671 19980821 00671 1998 8 21 C2XA98CL054 4 19980716 A 3417 7014700918 ADC EMB 145 EMB145 SO COCKPIT FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 16927 214 97071304 145006 CLE - FLT 4101 - CREW REPORTED THAT WHILE IN CRUISE FLIGHT, THE NR 2 ADC CAUSED NUMEROUS PROBLEMS WITH AIRSPEED AND ALTI TUDE. THE CREW ALSO HAD THE NR 1 ENGINE CONTROL A/B FAIL AND THE NR 2 ENGINE B CONTROL FAIL, WHICH WOULD NOT RESET. AI RCRAFT DIVERTED INTO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ADC IAW EMB-145 MM 34-13-0 0, 34-15-00 AND 34-15-01. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998082100672 19980821 00672 SO 1998 8 21 C2XA98IA265 1 19980709 A 2150 24540150 CLAMP EMB 120 EMB120RT SO ACM BAY BROKEN A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 16723 120169 IAH - FLT 3884 - PILOT REPORTED SMOKE HAD ACCUMULATED IN THE COCKPIT, THE AIRCRAFT LANDED AT IAH WITHOUT ANY FURTHER INC IDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RAM AIR DOOR SWITCH IN THE WRONG POSITION AND TWO WORM GEAR CLA MPS BROKEN ON THE LEFT PACK. THE AFFECTED CLAMPS WERE REPLACED AND THE AIRCRAFT OPERATIONALLY CHECKED GOOD AND WAS RELE ASED TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998082100673 19980821 00673 NM 1998 8 21 HNAA9891731 1 19980705 A 3231 DOOR DHAV DHC8 DHC8102 2809003 NM NLG OUT OF ADJUST A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 917HA 075 CLT/EWN - FLT 3284 - AFTER GEAR UP SELECTION, NOSE GEAR DOORS OPENED. CYCLED GEAR, NOSE GEAR DOORS OPENED AGAIN. AIR T URNBACK TO CLT. ADJUSTED NOSE GEAR DOORS, ACTUATOR END ONE TURN OUT. CYCLED GEAR, OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998082100674 19980821 00674 NM 1998 8 21 HNAA9891729 1 19980705 A 3231 54C546347 VALVE DHAV DHC8 DHC8102 2809003 NM NLG WW FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 917HA 30244 42 075 CLT/HHH - FLT 3172 - AFTER GEAR RETRACTION, NOSE GEAR DOOR AMBER LIGHT CAME ON. CREW CYCLED GEAR AND LIGHT ON AGAIN. A IR TURNBACK TO CLT. REMOVED AND REPLACED SOLENOID SEQUENCE VALVE, OPS CHECKED GOOD. (X) 2 H 7 2 4T RT A13NM 1998082100675 19980821 00675 NM 1998 8 21 98ZZZX2875 1 19980714 A 3350 1102833 LIGHT GRIMES 900835A BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 972 22435 LOG PAGE: 27320 - ON PRE-FLIGHT TRANSIT, FOUND AFT ENTRY OVERHEAD EMERGENCY LIGHT ASSEMBLY DID NOT ILLUMINATE. TROUBLE SHOT SYSTEM, FOUND LIGHT ASSY INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY IAW 33-50-00. OPS CHECKED GOOD. (X) 2 L 7 3 4F A3WE 1998082100676 19980821 00676 NM 1998 8 21 98ZZZX2876 1 19980718 A 3350 36262R014 LIGHT GRIMES 72914 BOEING 727 727231 1384079 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 808MA 21988 LOG PAGE: 24839: ON PRE-FLIGHT TRANSIT, FOUND ESCAPE PATH LIGHTING R2 DOOR NOT LIGHTING. TROUBLESHOT SYSTEM. REPAIRE D WIRING. OPS CHECKED OK IAW 33-50-01. (X) 2 L 7 3 4F A3WE 1998082100677 19980821 00677 NM 1998 8 21 98ZZZX2877 1 19980716 A 2612 65249203 CONTROL UNIT BOEING 727 727231 1384079 NM E/E COMPARTMENT MALFUNCTIONED A MYWA O OTHER N FALSE WARNING CR CRUISE 1 SO 19 808MA M00187 21988 LOG PAGE: 24836 - DURING CRUISE, WHEEL WELL FIRE WARNING LIGHT AND BELL CAME ON. COMPLETED AOM PROCEDURES AND INDICATIO N DID NOT RETURN. THE NGU TROUBLESHOT SYSTEM, INSPECTED LOOPS, WIRING, GROMMETS, AND FASTENERS IN L/R WHEELS. NO DEFEC TS NOTED. REMOVED WATER CONTAMINATION FROM L/R WHEEL WELL DISCONNECT C/P. SYSTEM CHECK OK IAW MM 2612-1. LOG PAGE 248 40 IN ERW R/R FIRE DETECTOR CONTROL UNIT FOR COMPANY CONVENIENCE. OPS CHECK OK IAW 26/14/11. (X) 2 L 7 3 4F A3WE 1998082100678 19980821 00678 NM 1998 8 21 EISA98167 1 19980707 A 2611 STRUT BOEING 727 727223 1384074 NM NR 1 MLG WW OVERHEAT A EISA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 314NE 19495 AT 1,000 FEET, AGL ON REDUCED POWER TAKEOFF OUT OF DFW, AIRCRAFT INDICATED NR 1 STRUT OVERHEAT. LIGHT EXTINGUISHED 2 MI NUTES AFTER THROTTLE RETARDED. GENERATED FROM PILOT REPORT. REMOVED NR 1 STRUT PANELS AND INSPECTED. NO DEFECTS NOTED . ALSO, TIGHTENED STRUT AIR DUCTS. OPS CHECK NORMAL. (X) 2 L 7 3 4F A3WE 1998082100679 19980821 00679 NM 1998 8 21 EISA98174 1 19980721 A 2133 VALVE BOEING 727 72731 1384010 NM CABIN OUT FLOW DIRTY A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 240NE 18906 PHL - AFTER TAKEOFF, AIRCRAFT WOULD NOT PRESSURIZE IN ANY MODE OR BLEED CONFIGURATION. RETURNED TO PHL. GENERATED FROM PILOT REPORT. FROUND LEFT OUT FLOW VALVE DIRTY. CLEANED VALVE AREA. OPS CHECK ON GROUND. ALL NORMAL DEFECTS NOTED MM 21-00. (X) 2 L 7 3 4F A3WE 1998082100680 19980821 00680 NM 1998 8 21 EISA98175 1 19980711 A 2130 10328051 VALVE BOEING 727 72725 1384006 NM CABIN FAILED A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 300NE 45619 18974 CLIMBING THROUGH 17,000 FEET, LOSS OF ALL PRESSURIZATION, CABIN CLIMBED TO 14,000 FEET. NO CONTROL IN ANY MODE. INITIA TED DESCENT TO 9,000 FEET. CABIN ALTITUDE CAUGHT AIRCRAFT ALTITUDE, STILL NO CONTROL OF PRESSURIZATION, RETURNED TO BDL . GENERATED FROM PILOT REPORT. REMOVED AND REPLACED SAFETY VALVE IAW 21-30-51. OPS CHECK ON GROUND GOOD. (X) 2 L 7 3 4F A3WE 1998082100681 19980821 00681 NM 1998 8 21 EISA98176 1 19980711 A 2750 GEARBOX BOEING 727 7272A7 138407K NM TE FLAPS CONTAMINATED A EISA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 310NE 20241 AFTER TAKEOFF FROM IND WHILE RETRACTING FLAPS, OUTBOARD FLAPS DID NOT RETRACT FROM 2 DEGREES TO UP. PERFORMED PROCEDURE AND PROBLEM REMAINED. RETURNED TO IND. GENERATED FROM PILOT REPORT. CYCLED FLAPS, FLUSHING ANY POSSIBILITY OF AIR, I NSPECTED FLAPS, FLAP OUTBOARD GEARBOX FLUSHED, AND FILLED WITH 5606, TEST GOOD ON GROUND, IAW MM CHAPTER 27. (X) 2 L 7 3 4F A3WE 1998082100682 19980821 00682 WP 1998 8 21 EISA98177 1 19980709 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 950VJ 47564 FOUND GALLEY DOOR MOUNTED SLIDE LIGHT DIM. GENERATED MAINTENANCE REPORT. REPLACED GALLEY DOOR MOUNTED SLIDE. RIGHT BA TTERY PER MM 33-50-1. (X) 2 L 7 2 4F A6WE 1998082100683 19980821 00683 NM 1998 8 21 EISA98178 1 19980710 A 2434 976J1A12 GENERATOR BOEING 727 727231 1384079 NM NR 2 MALFUNCTIONED A EISA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 74318 PA4829 20051 DURING CRUISE FLIGHT, CREW NOTICED ALL LIGHTS IN COCKPIT, RADAR SCREEN, AND GPS SCREEN WOULD FLASH ON AND OFF EVERY FEW MINUTES. KILOWATTS ON THE NR 1 WOULD SPIKE TO 25 TO 30 KILOWATTS. NR 2 GENERATOR WOULD DO THE SAME THING. BTB ILLUMIN ATED. COULD NOT BRING NR 2 GEN ON-LINE. DURING DESCENT, CREW WAS AWARE OF STRONG ELEC SMOKE IN COCKPIT. REMOVED AND REPLACED NR 1 AND NR 2 GENERATORS, 3 VOLTAGE REGULATORS. ON NR 2 GEN FOUND FIELD WIRE TERMINALS LOOSE. CHECKED WIRING BEHIND ELEC RACK. FOUND NO DEFECTS. RAN ALL 3 ENG IN-FLIGHT MODE WITH ALL EQUIP ON. NO DEFECTS. NOTED: PERFORMED O PER CHK OF ACFT AC AND DC GEN PER MM 24-20-0, PAGES 501 TO 504. REF OPER CNTRL NR 98ZZZX2878, AND, NR 98ZZZX2879. (X) 2 L 7 3 4F A3WE 1998082100684 19980821 00684 NM 1998 8 21 98ZZZX2878 1 19980710 A 2434 976J1A12 GENERATOR BOEING 727 727231 1384079 NM NR 1 MALFUNCTIONED A EISA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 74318 MO6354 20051 DURING CRUISE FLIGHT, CREW NOTICED ALL LIGHTS IN COCKPIT, RADAR SCREEN, AND GPS SCREEN WOULD FLASH ON AND OFF EVERY FEW MINUTES. KILOWATTS ON THE NR 1 WOULD SPIKE TO 25 TO 30 KILOWATTS. NR 2 GENERATOR WOULD DO THE SAME THING. BTB ILLUMIN ATED. COULD NOT BRING NR 2 GEN ON-LINE. DURING DESCENT, CREW WAS AWARE OF STRONG ELEC SMOKE IN COCKPIT. REMOVED AND REPLACED NR 1 AND NR 2 GENERATORS, 3 VOLTAGE REGULATORS. ON NR 2 GEN FOUND FIELD WIRE TERMINALS LOOSE. CHECKED WIRING BEHIND ELEC RACK. FOUND NO DEFECTS. RAN ALL 3 ENG IN-FLIGHT MODE WITH ALL EQUIP ON. NO DEFECTS. NOTED: PERFORMED O PER CHK OF ACFT AC AND DC GEN PER MM 24-20-0, PAGES 501 TO 504. REF OPER CNTRL NR EISA98178, AND, NR 98ZZZX2879. 2 L 7 3 4F A3WE 1998082100685 19980821 00685 NM 1998 8 21 98ZZZX2879 1 19980710 A 2436 905D9774 VOLTAGE REG BOEING 727 727231 1384079 NM E/E BAY MALFUNCTIONED A EISA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 74318 YY4471A 20051 DURING CRUISE FLIGHT, CREW NOTICED ALL LIGHTS IN COCKPIT, RADAR SCREEN, AND GPS SCREEN WOULD FLASH ON AND OFF EVERY FEW MINUTES. KILOWATTS ON THE NR 1 WOULD SPIKE TO 25 TO 30 KILOWATTS. NR 2 GENERATOR WOULD DO THE SAME THING. BTB ILLUMIN ATED. COULD NOT BRING NR 2 GEN ON-LINE. DURING DESCENT, CREW WAS AWARE OF STRONG ELEC SMOKE IN COCKPIT. REMOVED AND REPLACED NR 1 AND NR 2 GENERATORS, 3 VOLTAGE REGULATORS. ON NR 2 GEN FOUND FIELD WIRE TERMINALS LOOSE. CHECKED WIRING BEHIND ELEC RACK. FOUND NO DEFECTS. RAN ALL 3 ENG IN-FLIGHT MODE WITH ALL EQUIP ON. NO DEFECTS. NOTED: PERFORMED O PER CHK OF ACFT AC AND DC GEN PER MM 24-20-0, PAGES 501 TO 504. REF OPER CNTRL NR EISA98178, AND, NR 98ZZZX2878. 2 L 7 3 4F A3WE 1998082100686 19980821 00686 NM 1998 8 21 EISA98179 1 19980717 A 2432 CA72720 BATTERY BOEING 727 727223 1384074 NM BATTERY BAY OVERHEAT A EISA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 6815 9603224 19490 WHEN PARKING AIRCRAFT AT EDI, FLIGHT DECK FILLED WITH SMOKE. IT WAS DETERMINED BATTERY WAS OVERHEATING. FIRE DEPARTMEN T REMOVED BATTERY FROM AIRCRAFT. GENERATED FROM PILOT REPORT. MAIN BATTERY AND BATTERY CHARGER REPLACED. CHECKED SATI SFACTORY IAW MM 24-30-11. (X) 2 L 7 3 4F A3WE 1998082100687 19980821 00687 NM 1998 8 21 EISA98180 1 19980722 A 2611 CONNECTOR BOEING 727 72725 1384006 NM SMOKE DETECTOR CONTAMINATED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 300NE 18974 DURING PRE-FLIGHT, THE SECOND FROM THE LEFT BUTTON, MAIN CARGO SMOKE DETECTOR SYSTEM WOULD NOT TEST. GENERATED FROM PIL OT REPORT. CLEANED CANNON PLUG PER MM CHAPTER 26. OPS CHECK NORMAL. (X) 2 L 7 3 4F A3WE 1998082100688 19980821 00688 1998 8 21 EISA98142 4 19980618 A 3418 STICK SHAKER BOEING 727 727227 1384078 NM E/E BAY MALFUNCTIONED A EISA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 07 308AS 22002 DURING TAKEOFF ROLL, STICK SHAKER ACTIVATED. DISCONTINUED TAKEOFF AT 70 KNOTS. GENERATED FROM PILOT REPORT. OPS CHECK ED STALL WARNING IAW BMM CHAPTER 34-18-01, PAGES 502 THROUGH 504. NO DEFECTS NOTED. (X) 2 L 7 3 4F A3WE 1998082100689 19980821 00689 NM 1998 8 21 EISA98140 1 19980612 A 5310 STRUCTURE BOEING 727 727231 1384079 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 12305 19562 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD NR 269, INSPECTION OF PLENUM CHAMBERS. OBSERVED CORROSION AT STR S4C AND LBL 29.9 AND LBL 31.8 AND STR S3C RBL 16.5 AND STR S4C AT RBL 32.0. BOEING REPAIR NR EOIR980527 AND EOIR980529. (X) 2 L 7 3 4F A3WE 1998082100690 19980821 00690 NM 1998 8 21 EISA98139 1 19980619 A 2782 1U11032 ACTUATOR BOEING 727 727223 1384074 NM NR 5 SLAT MALFUNCTIONED A A EISA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 316NE 4177A 19475 AFTER TAKEOFF FROM DFW DURING FLAP/SLAT RETRACTION, NR 5 SLAT FAILED TO RETRACT. RECYCLED NR 5 SLAT, STILL DID NOT RETR ACT. RETURNED TO DFW. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED NR 5 SLAT ACTUATOR WITH SERVICEABLE PART. GR OUND OPS CHECK GOOD. NO OTHER DEFECTS NOTED. (X) 2 L 7 3 4F A3WE 1998082100691 19980821 00691 NM 1998 8 21 EISA98137 1 19980619 A 2780 H1010271 SLAT BOEING 727 727223 1384074 NM NR 5 SLAT MALFUNCTIONED A A EISA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 316NE 7712 19475 DURING FLAP ROTATION AFTER TAKEOFF FROM DFW, NR 5 SLAT FAILED TO RETRACT. RECYCLED FLAPS, DID NOT RETRACT, RETURNED TO DFW FOR LANDING. GENERATED FROM PILOT REPORT. REMOVED NR 5 SLAT AND INSPECTED SLAT AND BEARINGS AND ALL ATTACHED FITTI NGS. NO DEFECTS. (X) 2 L 7 3 4F A3WE 1998082100692 19980821 00692 NM 1998 8 21 EISA98136 1 19980618 A 3232 731414 ACTUATOR BOEING 727 727223 1384074 NM LT M LG DOOR FAILED A EISA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SW 07 6826 AA15 19704 ON TAKEOFF FROM BRUSSELS (BRU), A-SYSTEM HYDRAULIC QUANTITY WENT TO 2.0 GALLONS AND LOW LEVEL LIGHT ILLUMINATED. RETURN ED FOR LANDING TO (BRU). GENERATED FROM PILOT REPORT. REMOVED AND REPLACED LEFT MAIN LANDING GEAR DOOR ACTUATOR IAW M M CHAPTER 32. OPS CHECK GOOD. (X) 2 L 7 3 4F A3WE 1998082100693 19980821 00693 NM 1998 8 21 EISA98134 1 19980614 A 2612 DETECTOR BOEING 727 727223 1384074 NM LT MLG WW FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312NE 20193 DURING PRE-FLIGHT, FOUND WHEEL WELL FIRE DETECTOR SYSTEM INOPERATIVE. GENERATED FROM MAINTENANCE REPORT. REMOVED AND R EPLACED LEFT WHEEL WELL. FIRE DETECTOR ELEMENT AND SYSTEM OPS CHECKS NORMAL IAW MM 26-12-00. (X) 2 L 7 3 4F A3WE 1998082100694 19980821 00694 NM 1998 8 21 EISA98133 1 19980527 A 5311 65C3627936 FRAME BOEING 727 727231 1384079 NM BS 760 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 12305 65287 19562 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD SEQ 237, RIGHT SIDE STA 760.95 FOUND FRAME CRACKED. INSTALLED BOEIN G REPAIR KIT PER SB 53-0197. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X) 2 L 7 3 4F A3WE 1998082100695 19980821 00695 NM 1998 8 21 EISA98132 1 19980527 A 5320 FITTING BOEING 727 727231 1384079 NM BS 740 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 12305 65287 19562 DURNG ACCOMPLISHMENT OF ROUTINE WORK CARD 045 OR SB 53-62 R6, INSPECTION OF 740 FITTINGS FOUND RIGHT HAND 740 FITTING CR ACKED. REPLACED RIGHT-HAND 740 FITTING PER SB 53-0062. USED BOEING KIT 65C13724-96. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X) 2 L 7 3 4F A3WE 1998082100696 19980821 00696 NM 1998 8 21 EISA98131 1 19980527 A 5712 RIB 65C3320299 BOEING 727 727231 1384079 NM WS 70.5 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 12305 65287 19562 DURING ACCOMPLISHMENT OF ROUTINE WORK CARD FOR C-CHECK SEQ 237, FOUND UPPER RIB CHORD CRACKED AT BBL 70.5 STA 760.95 ON LEFT HAND SIDE OF AIRCRAFT. INSTALLED REPAIR KIT PER SB 57-112 R5. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X) 2 L 7 3 4F A3WE 1998082100697 19980821 00697 NM 1998 8 21 EISA98130 1 19980527 A 5320 6595600253 FITTING BOEING 727 727231 1384079 NM BS 1170 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 12305 65287 19562 DURING ACCOMPLISHMENT OF C-CHECK, CPCP CARD NR C53-100-01, BS 1170 LEFT HAND SIDE AT AFT LAV DOOR AREA STR 20 FOUND BULG E, OPENED SKIN FOUND CRACK AND CORROSION ON FITTING. REMOVED CORROSION AND REPLACED STRINGER PER MM 53-10-3. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X) 2 L 7 3 4F A3WE 1998082100698 19980821 00698 NM 1998 8 21 EISA98119 1 19980525 A 2432 2301 BATTERY CHARGER BOEING 727 727231 1384079 NM E/E BAY FAILED A EISA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 74318 248 20051 ON POST-FLIGHT INSPECTION, FOUND THE BATTERY VOLTAGE TO BE ZERO. AFTER CONSULTING WITH MAINTENANCE (BRUSSELS), FOUND A 50-AMP CIRCUIT BREAKER IN LOWER 48 LABELED BATTERY CHARGER. WHEN CIRCUIT BREAKER WAS RESET, BATTERY POWER RESTORED, HOW EVER, AFTER 2 MINUTES, COCKPIT FILLED WITH ELECTRICAL SMOKE. EVACUATION OF CREW WAS ACCOMPLISHED. DE-POWERED AIRCRAFT. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED MAIN BATTERY IAW MM 24 CHECKS GOOD. REMOVED AND REPLACED BATTERY C HARGER IAW MM 24. OPS CHECK GOOD IAW MM24. (X) 2 L 7 3 4F A3WE 1998082100699 19980821 00699 NE 1998 8 21 EISA98147 2 19980616 A 7230 COMPRESSOR BOEING 727 727223 1384074 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE STALLED A EISA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 313NE 657163 19702 FROM JFK - AT APPROXIMATELY 100 KNOTS, TAEKOFF ROLL NR 2 ENGINE COMPRESSOR STALL. RECOVERED. AFTER, THROUGH 400 FEET, COMPRESSOR STALL (NR 2) AGAIN AND RECOVERED. WIND 140/4 TEMP 18 DEGREES CELSIUS. ON SECOND COMPRESSOR STALL, ENGINE NE ARLY FLAMED OUT. BOTH ENGINE FAIL LIGHTS CAME ON. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED NR 2 ENGINE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1998082100700 19980821 00700 NM 1998 8 21 USAASB98176 1 19980710 A 3230 CIRCUIT BREAKER BOEING 737 7374B7 1384702 NM COCKPIT TRIPPED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 435US 24557 DCA - FLT 1950 - AFTER TAKEOFF, CREW COULD NOT RETRACT THE LANDING GEAR. FLIGHT RETURNED TO FIELD AT DCA AND LANDED WIT HOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PINNED THE GEAR AND PLACED THE AIRCRAFT IN THE AIR MODE. PROBLE M WAS DUPLICATED. FOUND 'LANDING GEAR LEVER LATCH AND PRESSURE WARNING' CIRCUIT BREAKER ON THE P6-2 PANEL TRIPPED. RES ET CIRCUIT BREAKER AND TESTED SYSTEM PER MM 32-31. OPERATIONAL CHECK GOOD. REMOVED GEAR PINS. (X) 2 L 7 2 4F RT A16WE 1998082100701 19980821 00701 WP 1998 8 21 TWAA9811504 1 19980715 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DEFECTIVE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE UPPER AND LOWER SKIN THICKNESS MEASURED BY NDT WAS .024 INCH. SKIN THICK NESS IS .063 INCH AT STA 815, L26R. REPAIRED SKIN PER SRM 53-04, FIG 12B, PAGE 45. ACFT TT: 77,783 HOURS. ACFT TC: 8 4,471. (X) 2 L 7 2 4F A6WE 1998082100702 19980821 00702 NM 1998 8 21 USAASB98183 1 19980714 A 3234 A42006028305 SOLENOID BOEING 737 7374B7 1384702 NM COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 426US 24548 PIT - FLT 1265 - AFTER TAKEOFF, CREW WAS UNABLE TO RAISE THE LANDING GEAR. LANDING GEAR LEVER WOULD NOT MOVE UP. CHECK LIST WAS ACCOMPLISHED AND THE GEAR WAS RAISED USING THE OVERRIDE. AFTER THE GEAR CAME UP AND CLIMB POWER WAS ADDED, THE TAKEOFF CONFIGURATION WARNING HORN SOUNDED WHEN THE FLAPS WERE FULLY RETRACTED. CREW DECLARED AN EMERGENCY AND RETURNE D TO FIELD AT PIT. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER LATCH SOLENOID PER MM 32-31-31. PERFORMED OPERATIONAL CHECK. OPS CHCK GOOD. (X) 2 L 7 2 4F RT A16WE 1998082100703 19980821 00703 NM 1998 8 21 USAASB98185 1 19980715 A 3260 SENSOR BOEING 737 7374B7 1384702 NM NLG WW OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 426US 24548 CLT - FLT 1100 - AFTER TAKEOFF, CREW UNABLE TO MOVE LANDING GEAR HANDLE TO THE 'UP' POSITION TO RAISE THE GEAR. ABNORMA L PROCEDURES FOLLOWED AND RETURNED TO CLT. CLT MAINT CONTACTED BY THE FLIGHT VIA RADIO AND PROVIDED ADVICE ABOUT CIRCUI T BREAKER OPERATION. CREW RESET A CIRCUIT BREAKER AND RECEIVED 3 GREEN LIGHTS TO VERIFY GEAR POSITION. A TOWER FLYBY C ONFIRMED GEAR WAS DOWN. FLIGHT LANDED CLT WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINT FOUND THE AIR/GROUND SAFETY SENSOR S106 (P/N 1-899-29) TARGET GAP EXCESSIVE. ADJUSTED SENSOR PER MM 32-09-01. DUPLICATED FAILURE OF M991 AIR/GROUN D SENSOR CARD. REPLACED CARD PER MM 32-09-20. ACCOMPLISHED SEVERAL GEAR SWINGS, NORMAL OPERATION. (X) 2 L 7 2 4F RT A16WE 1998082100704 19980821 00704 EU 1998 8 21 USAAF98059 1 19980403 A 3350 71050301 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU ESCAPE SLIDE DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 891US 11366 GSO - THE FORWARD SERVICE DOOR ESCAPE SLIDE LIGHTS FAILED TO ILLUMINATE DURING THE ANNUAL ESCAPE SLIDE OPERATIONAL CHECK SAMPLING PROGRAM. THE SLIDE DEPLOYED NORMALLY. TWO OTHER AIRCRAFT SCHEDULED FOR THE SERVICE DOOR POSITION PASSED THE TEST. THE SLIDE BATTERY PACK WAS DISCHARGED RESULTING IN LIGHT FAILURE. THE REPAIR SHOP REPLACED THE BATTERY PACK AND REPACKED THE SLIDE. (X) 2 L 7 2 4F RT 1998082100705 19980821 00705 NE 1998 8 21 98ZZZX2880 2 19980503 A 7250 111052019 SHROUD BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE 1ST STAGE NOZZEL CRACKED A GDMA K NONE O OTHER IN INSP/MAINT 1 NM 09 58HJ 7942 2546 30314 LE07205X IT WAS NOTED DURING OPERATION, ENGINE EGT WAS OBSERVED TO BE ABOVE NORMAL. UPON TEARDOWN OF HOT SECTION, THE FIRST STAG E TURBINE NOZZLE OUTER SHROUD WAS FOUND SEVERELY CRACKED. (X) 1 G 7 1 4U 4 U H1SW E17EA 1998082100706 19980821 00706 SW 1998 8 21 98ZZZX2881 1 19980523 A 6230 430340036101 BEARING BELL 430 430 1182150 SW MAST SPALLED B SL3R K NONE J WARNING INDICATION NR NOT REPORTED 1 NE 01 430TX 5723 ZV5015 49005 MAST BEARING CHIP LIGHT IN-FLIGHT. FOUND THRUST SIDE OF INNER RACE SPALLED. 1 G 7 2 3U RT H9SW 1998082100707 19980821 00707 SW 1998 8 21 98ZZZX2882 1 19980528 A 6230 430310450101 BEARING BELL 430 430 1182150 SW SWASHPLATE FAILED B SL3R K NONE O OTHER IN INSP/MAINT 1 NE 01 430TX 572 49005 DUPLEX BEARING FAILED. NEW BEARING INSTALLED. 1 G 7 2 3U RT H9SW 1998082100708 19980821 00708 SW 1998 8 21 98ZZZX2883 1 19980528 A 6230 430310453101 SEAL BELL 430 430 1182150 SW SWASHPLATE DAMAGED B SL3R K NONE K FLUID LOSS IN INSP/MAINT 1 NE 01 430TX 572 49005 DURING REPLACEMENT OF DUPLEX BEARING, THE SEAL WAS FOUND DAMAGED. NEW SEAL INSTALLED. THIS IS THE LOWER SEAL IN THE CA P. 1 G 7 2 3U RT H9SW 1998082100709 19980821 00709 SW 1998 8 21 98ZZZX2884 1 19980610 A 6321 206340301103 CALIPER BELL 407 407 SW ROTOR BRAKE LEAKING B IIFR K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PR 189 810 53232 ROTOR BRAKE LEAKING. NO TECHNICAL DATA TO REPAIR. 1 G 7 1 3U O H2SW 1998082100710 19980821 00710 SW 1998 8 21 98ZZZX2885 1 19980610 A 6520 406312106101 BOOT BELL 407 407 SW TAIL ROTOR LEAKING B IIFR K NONE K FLUID LOSS IN INSP/MAINT 1 SW 03 407PR 189 53232 HOLE IN BOOT ALLOWING OIL AND GREASE TO FLOW OUT. SEALS 2 EACH B56-40-2 AND ONE EACH 26001-7023 WERE REPLACED DUE TO LE AKING. 1 G 7 1 3U O H2SW 1998082100711 19980821 00711 SW 1998 8 21 98ZZZX2886 1 19980701 A 6300 406010426101 LINK ASSY BELL 407 407 SW M/R DRIVE FAILED B IIFR K NONE O OTHER IN INSP/MAINT 1 SW 03 407JR 99 AFS1399 53245 DRIVE LINK LOWER STUD SHEARED DUE TO CRACK/CORROSION. REMOVED DRIVE LINK P/N 406-010-426-101, S/N A-FS1399. INSTALLED S/N A-FS1777 TTO NEW DRIVE LINK. 1 G 7 1 3U O H2SW 1998082100712 19980821 00712 NM 1998 8 21 TWAA9813201 1 19980817 A 3350 CIRCUIT BREAKER BOEING 727 727231 1384079 NM CABIN TRIPPED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 54340 20845 THE EMERGENCY LIGHTS BATTERY CHARGER POPPED CIRCUIT BREAKER. CHECKED BATTERY CHARGER AND WIRING, NO PROBLEM FOUND. REP LACED 115V C/B. CHECK-C 9-5-97 MCI. 2 L 7 3 4F A3WE 1998082100713 19980821 00713 NM 1998 8 21 TWAA9813202 1 19980818 A 3350 1102833 POWER SUPPLY BOEING 727 727231 1384079 NM BS 400 INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54340 20845 EMERGENCY LIGHTS BATTERY CHARGER CIRCUIT BREAKER WAS POPPING. REPLACED BATTERY POWER SUPPLY. CHECK-C 9-5-97. 2 L 7 3 4F A3WE 1998082100714 19980821 00714 WP 1998 8 21 TWAA9813204 1 19980813 A 3350 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9303K 49529 DURING MAINT FOUND EMERGENCY OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACK AND POWER SUPPLY. BATTERY PACK E02899-1 AND POWER SUPPLY 33000794-05. CHECK-C 11-8-97 MCI. 2 L 7 2 4F RT A6WE 1998082100715 19980821 00715 WP 1998 8 21 TWAA9813205 1 19980813 A 3350 3350002621 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9303K 49529 DURING MAINT FOUND FWD CABIN EGRESS LIGHTS INOP. REPLACED BATTERY PACK. CHECK-C 11-8-97 MCI. 2 L 7 2 4F RT A6WE 1998082100716 19980821 00716 WP 1998 8 21 TWAA9813207 1 19980813 A 5312 BULKHEAD JAMB DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 995Z 47027 DURING CHECK-C MAINT, AN INTERIM REPAIR WAS FOUND ACCOMPLISHED WITH BLIND FASTENERS ON A CRACK AT THE AFT PRESS BLKHD DO OR JAMB, RT SIDE. INSTALLED DOOR JAMB PERMANENT REPAIR PER ARA 15365 AND SRM 53-05 FIG 30. 2 L 7 2 4F A6WE 1998082100717 19980821 00717 WP 1998 8 21 VJ9800282 1 19980723 A 5310 1A35688 STRUCTURE DOUG DC9 DC932 3022066 WP BS 889-897 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 AFT CARGO COMPARTMENT FLOOR SUPPORT FRAME AND SKIN CORRODED BEYOND LIMIT AT FS 889-897, L30-29R. CLEANED CORROSION IAW DC9 SRM 53-04, FABRICATED INTERNAL DOUBLER FROM 2024-T3.032, 5.4 X 5.5 X.032, IAW DC9 SRM. DRILLED AND DEBURRED IAW DC9 SRM 51-10-4. TREATED AND PRIMED IAW DC9 51-10-3. INSTALLED DOUBLER NACA METHOD IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998082100718 19980821 00718 WP 1998 8 21 VJ9800283 1 19980729 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 522 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 902VJ 47177 CORROSION BEYOND LIMIT AT FS 522, 28L-28R. REMOVED FASTENERS TO ACCESS CORRSION IAW DC9 SRM 51-10-3. TREATED AND PRIME D AREA IAW DC9 SRM 53-01 FIG 1. TREATED AND PRIMED AREA IAW DC9 SRM 51-10-3 AND REPLACED FASTENERS IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082100719 19980821 00719 WP 1998 8 21 CALA9801475 1 19980818 A 3260 SWITCH DOUG DC9 DC932 3022066 WP RT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 12510 47799 THE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE LIGHT EXTINGUISHED. TH E FLIGHT CONTINUED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE RT MLG DOWNLOCK SWITCH IAW MM 32-60-1, CODE 8, PAGE 201-203. OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998082100720 19980821 00720 WP 1998 8 21 CALA9801476 1 19980818 A 5311 BELTFRAME DOUG DC9 DC931 3022065 WP BS 408 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A 4 INCH CRACK IN BELTFRAME AT STA 408, LONGERON 5L. THE BELTFRAME WAS REPAIRED IAW SRM 53-03, FIGURE 4. 2 L 7 2 4F A6WE 1998082100721 19980821 00721 WP 1998 8 21 CALA9801477 1 19980818 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND A CRACK IN LONGERON 16R AT RT LAV WALL, STA 965. THE CRACKED SECTION OF LONGERON WAS REMOVED AND REPLA CED IAW SRM 53-02, FIGURE 18, PAGE 48. 2 L 7 2 4F A6WE 1998082100722 19980821 00722 NM 1998 8 21 CALA9801478 1 19980818 A 5230 WEB BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1.5 INCH CRACK AT AFT LIGHTENING HOLE OF C-1 CARGO DOOR WEB. THE CRACK WAS STOP DRILLED. A REPAIR W AS FABRICATED AND INSTALLED IAW SRM 51-10-1, PAGE 6B, 51-40-2, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100723 19980821 00723 NM 1998 8 21 CALA9801479 1 19980818 A 5320 SPLICE BOEING 727 727232 1384082 NM CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND BUTT SPLICE CORRODED, DENTED, AND GOUGED AT NR 3 RT CARGO AREA. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3 AND 51-10-2. 2 L 7 3 4F A3WE 1998082100724 19980821 00724 NM 1998 8 21 CALA9801480 1 19980818 A 5311 FRAME BOEING 727 727232 1384082 NM BS 219.8 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND WEB CORRODED AT FLIGHT DECK FS 219.8, RT FRAME, DIRECTLY BELOW R-2 SLIDING WINDOW. THE WEB WAS REMOVED IAW SRM 51-30-2. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100725 19980821 00725 NM 1998 8 21 CALA9801481 1 19980818 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1136, RBL 25. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABRICATE D AND INSTALLED IAW SRM 53-10-5, 51-30-5, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082100726 19980821 00726 NM 1998 8 21 CALA9801482 1 19980818 A 5712 RIB BOEING 737 7372C0 1384488 NM LT WING GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A GOUGE IN LT WING LEADING EDGE RIB INBOARD OF NR 3 SLAT. A REPAIR ANGLE DOUBLER AND FILLER WERE FABRI CATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-21-31. 2 L 7 2 4F A16WE 1998082100727 19980821 00727 EU 1998 8 21 9809903201 1 19980813 A 3241 HARNESS AIRBUS 320 A320211 3930320 EU RT MLG MISROUTED A NWAA K NONE W INADEQUATE Q C LD LANDING 1 GL 01 301US 31 DURING LANDING ROLLOUT, RIGHT MAIN LANDING GEAR BRAKES BECAME INEFFECTIVE CAUSING THE AIRCRAFT TO PULL LEFT ALLOWING LEF T MAIN LANDING GEAR TO DEPART RUNWAY SURFACE. NO AIRCRAFT DAMAGE WAS SUSTAINED. MAINTENANCE REROUTED ANTI-SKID TRANSD UCER WIRING HARNESS WHICH WAS FOUND CROSSED BETWEEN NR 3 AND NR 4 WHEELS. HIGH SPEED TAXI AND BRAKE OPERATIONALLY TESTE D OK. 2 L 7 2 4F RT A28NM 1998082100728 19980821 00728 WP 1998 8 21 9809919951 1 19980816 A 3260 PROX SENSOR DOUG DC9 DC932 3022066 WP NOSE GEAR BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 9347 45827 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW RECYCLED GEAR TWICE WITH SAME RESULTS. EMERGENCY GEAR EXTENSION PRODUCERS WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. RED EMERGENCY WAS DECLARED BY THE CAPTAIN . MAINTENANCE FOUND NOSE GEAR PROXIMITY SENSOR BROKEN. REPLACED SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998082100729 19980821 00729 1998 8 21 COMA9810178 4 19980814 A 3425 6226190204 AHRS AHC85 EMB 120 EMB120RT SO NR 1 MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 266CA 24256 607 120258 ATTITUDE DISPLAY WARNING DURING TAKEOFF. REPLACED THE NR 1 AHRS. 2 L 7 2 4T RT A31SO 1998082100730 19980821 00730 WP 1998 8 21 UPS98827464 1 19980727 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 1200-1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 1200-1220 ABOVE STR 35R, THE TORQUE BOX WEB HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLAC ED WEB IAW SRM 53-2-0 FIG1D. 2 L 7 4 4F RT 4A25 1998082100731 19980821 00731 WP 1998 8 21 UPS98827465 1 19980717 A 5347 5759223170 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 120 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK I AW DWG 5151516 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998082100732 19980821 00732 WP 1998 8 21 UPS98827466 1 19980723 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 1180-1200 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, STA 1180-1200 AT LONG 34R, THE TORQUE BOX WEB HAS HEAVY CORROSION. REPAIRED AREA IAW DC8-5350-7876-A . 2 L 7 4 4F RT 4A25 1998082100733 19980821 00733 WP 1998 8 21 UPS98827467 1 19980527 A 5230 WEB DOUG DC8 DC873F 302199F WP CARGO DOOR BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, MAIN CARGO DOOR FWD BETWEEN LIGHTENING HOLES 4, 5 HAVE EDGES BROKEN OUT INSIDE. FABRICATED WEB RE PAIR, FRAME REPAIR ANGLE AND REPAIR SPLICE ANGLE IAW REO 04929, INSTALLED WEB REPAIR AND ANGLE IAW REO 04929 AND DC8 SR M 51-1-20D, AND 51-1-21. 2 L 7 4 4F RT 4A25 1998082100734 19980821 00734 WP 1998 8 21 UPS98827468 1 19980522 A 5230 SKIN DOUG DC8 DC873F 302199F WP L-2 DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, L-2 DOOR AT FWD LOWER CORNER HAS CRACKED LINE ABOUT 4 INCHES LONG. CUT OUT DAMAGED IAW REO 04856, FABRICATED FILLERS IAW DC8 SRM 53-2-0, 51-1-24, AND REO 04856. FABRICATED DOUBLERS IAW DC8 SRM 53-2-0 AND REO 04856 AN D INSTALLED FILLERS AND DOUBLERS IAW DC8 SRM 53-2-0, 51-1-20D AND REO 04856. 2 L 7 4 4F RT 4A25 1998082100735 19980821 00735 WP 1998 8 21 UPS98827469 1 19980525 A 5530 STRAP DOUG DC8 DC873F 302199F WP VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, VERTICAL STABILIZER TO FUSELAGE STRAP, RIGHT HAND SIDE HAS A CRACK AT FASTENERS HOLE FUSELAGE STAT ION 1765. FABRICATED REPAIR ANGLE AND FILLERS AND ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FILLER AND REPAIR A NGLE IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082100736 19980821 00736 WP 1998 8 21 UPS98827470 1 19980529 A 5751 WEB DOUG DC8 DC873F 302199F WP LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, LEFT HAND INBOARD AILERON, INBOARD WEB, CENTER ACCESS PANEL MATING SURFACE OF THE WEB IS TORN AND CRACKED. FABRICATED REPAIR DOUBLERS AND ALODINED AND PRIMED IAW REO 04825 AND DC8 SRM 51-1-8. INSTALLED REPAIR IAW REO 04825 AND DC8 SRM 51-1-21, 51-1-21A. 2 L 7 4 4F RT 4A25 1998082100737 19980821 00737 EU 1998 8 21 QXEA9801074 1 19980814 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 EMERGENCY LIGHT AT ROW 9AB INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998082100738 19980821 00738 EU 1998 8 21 QXEA9801075 1 19980814 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 CEILING EMERGENCY LIGHT INOPERATIVE AT ROW 8. MAINTENANCE RELAMPED, OPERATIONALY TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998082100739 19980821 00739 EU 1998 8 21 QXEA9801076 1 19980815 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 FORWARD FACING EMERGENCY EXIT SIGN IS OUT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY, OPERATONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998082100740 19980821 00740 EU 1998 8 21 QXEA9801077 1 19980816 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 COCKPIT ENTRY WAY EMERGENCY LIGHT OUT. MAINTENANCE RELAMPED, OPERATIONALLY TESTED AND RESULTS WERE NORMAL. 2 L 7 2 4F RT A20EU 1998082100741 19980821 00741 1998 8 21 QXEA9801078 4 19980815 A 3442 RDR1E INDICATOR FOKKER F28 F28MK4000 4990810 EU COCKPIT RADAR FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 480AU 2697 11229 CREW REPORTED ACRID ELECTRICAL SMELL COMING FROM JUST ABOVE THE RADAR SCREEN. MAINTENANCE REMOVED AND REPLACED THE RADA R INDICATOR, OPERATION TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998082100742 19980821 00742 EU 1998 8 21 QXEA9801079 1 19980808 A 4900 APU FOKKER F28 F28MK4000 4990810 EU APU COMPT FAILED A QXEA K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 491US 1167 11156 DURING CLIMB LAVATORY SMOKE DETECTOR WENT OFF. NO SMOKE OR FIRE WAS FOUND BY CREW INSPECTION OF LAVATORY. MAINTENANCE NOTED BLUE HAZE IN CABIN WITH THE APU RUNNING. SUSPECT APU BLEED AIR TO HAVE CAUSED WARNING. PLACED APU ON MEL. ON 8/ 9/98 BOI MAINTENANCE REMOVED AND REPLACED THE APU. OPERATIONAL TEST NORMAL. CLEAR MEL. 2 L 7 2 4F RT A20EU 1998082100743 19980821 00743 WP 1998 8 21 ABXA9800746 1 19980730 A 5311 3425610088 FRAME DOUG DOUG DC8 DC862 3021970 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 LOWER FLANGE OF FRAME 280 CRACKED AT LONGERON 12R. REPAIRED IAW DWG K04888 AND DC8 SRM 51-1-21D. 2 L 7 4 4F 4A25 1998082100744 19980821 00744 WP 1998 8 21 ABXA9800747 1 19980730 A 5712 RIB DOUG DOUG DC8 DC862 3021970 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION XILAI 7-295 THE UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DC8 S RM 51-1-8. 2 L 7 4 4F 4A25 1998082100745 19980821 00745 WP 1998 8 21 ABXA9800748 1 19980730 A 5712 97532923 RIB DOUG DOUG DC8 DC862 3021970 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION XS 250-089 UPPER RIB IS CRACKED ABOVE PNEUMATIC DUCT. FABRICATED REPAIR ANGLE IAW DC 8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998082100746 19980821 00746 WP 1998 8 21 ABXA9800749 1 19980730 A 5712 97532933 RIB DOUG DOUG DC8 DC862 3021970 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 LEFT WING LEADING EDGE RIB AT STATION XS 250-089 IS CRACKED ABOVE PNEUMATIC DUCT. FABRICATED REPAIR ANGLE IAW DC8 SRM 5 7-2-0. 2 L 7 4 4F 4A25 1998082100747 19980821 00747 WP 1998 8 21 ABXA9800750 1 19980727 A 5720 97532937 ANGLE DOUG DOUG DC8 DC862 3021970 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 LEFT INBOARD SLOT BOX, AFT OUTBOARD VERTICAL ANGLE IS CRACKED. FABRICATED AND INSTALLED REPLACEMENT VERTICAL ANGLE IAW DC8 SRM 51-1-20D AND DWG 9753293. 2 L 7 4 4F 4A25 1998082100748 19980821 00748 WP 1998 8 21 ABXA9800751 1 19980727 A 5720 4206309462 DOUBLER DOUG DOUG DC8 DC862 3021970 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING TRAILING EDGE RIB IS CRACKED IN 2 PLACES AT FLAP STATION 3.00. INSTALLED NEW RIB DOUBLER INTERCOSTAL IAW DC8 SRM 51-1-21, 51-1-20D AND 57-2-0. 2 L 7 4 4F 4A25 1998082100749 19980821 00749 WP 1998 8 21 ABXA9800752 1 19980727 A 5720 576958935 DOUBLER DOUG DOUG DC8 DC862 3021970 WP WS 6.225 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION XOL 6.225, INTERNAL DOUBLER IS CRACKED ON EACH SIDE OF TRIPLER. REPAIRED IAW DC8 SRM 51-1-21 AND DWG 5769589. 2 L 7 4 4F 4A25 1998082100750 19980821 00750 WP 1998 8 21 ABXA9800753 1 19980727 A 5320 37507571N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 LONGERON 31R SPLICE FITTING CRACKED AT STATION 600-620. REPLACED LONGERON 31R SPLICE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998082100751 19980821 00751 WP 1998 8 21 ABXA9800754 1 19980725 A 5720 56412532 DOUBLER DOUG DOUG DC8 DC862 3021970 WP WS 354 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT INBOARD UNDER WING FUEL ADAPTER, XFS 354.000, INTERNAL DOUBLER HAS SEVERE CORROSION. REPAIRE D IAW DACO DWG 5641253 AND DC8 SRM 51-1-20 AND 51-1-21. 2 L 7 4 4F 4A25 1998082100752 19980821 00752 WP 1998 8 21 ABXA9800755 1 19980723 A 5313 5753159 LONGERON DOUG DOUG DC8 DC862 3021970 WP BS 1180-1200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 STATION 1180-1200 LONGERON 34R IS CRACKED ON OUTBOARD FLANGE UNDERSIDE, CRACK IS 3.5 INCHES LONG. REPAIRED IAW DC8 SRM 53-2-2 AND ABX REA NR D 853-22894 MR. 2 L 7 4 4F 4A25 1998082100753 19980821 00753 WP 1998 8 21 MWEA98878 1 19980814 A 7931 3961005101 INDICATOR DOUG DC9 DC932 3022066 WP LT ENGINE MALFUNCTIONED A MWEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 31 207ME 47794 THE LEFT ENGINE OIL PRESSURE WENT INTO THE YELLOW ON TAKEOFF ROLL. MTC REMOVED AND REPLACED THE LEFT OIL PRESSURE INDIC ATOR. 2 L 7 2 4F A6WE 1998082100754 19980821 00754 WP 1998 8 21 MWEA98879 1 19980817 A 2560 11331DGDME COVER DOUG DC9 DC914 3022034 WP GALLEY SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 800ME 45842 THE GALLEY SLIDE COVER FELL OFF. MTC REINSTALLED GALLEY SLIDE COVER. 2 L 7 2 4F A6WE 1998082100755 19980821 00755 WP 1998 8 21 MWEA98880 1 19980818 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 205ME 47601 FORWARD ENTRANCE SLIDE CAME OUT OF PACK. MTC RESECURED SLIDE COVER TO FORWARD ENTRANCE DOOR. 2 L 7 2 4F A6WE 1998082100756 19980821 00756 NM 1998 8 21 SCNA98089 1 19980718 A 2750 TORQUE TUBE BOEING 727 727225 1384077 NM RT TE FLAP DISCONNECTED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 282SC 22558 AFTER DEPARTURE THE RIGHT OUTBOARD FLAP EXTENDED TO APPROXIMATELY 35 DEGREES. AIR RETURNED TO LTO. INSPECTED THE AIRCR AFT AND FOUND THE OUTBOARD FLAP TORQUE TUBE DISCONNECTED AT THE RIGHT WHEEL WELL AREA. RECONNECTED THE TORQUE TUBE AND OPERATED THE FLAPS WITH NO DEFECTS NOTED DURING OPERATION. TESTED IAW B727 MM 27-51-11. 2 L 7 3 4F A3WE 1998082100757 19980821 00757 NM 1998 8 21 VNAA9808015 1 19980815 A 2130 22260A020201 CONTROL PANEL 22260A020201 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT MALFUNCTIONED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 430JS 81095 111 3044 DURING THE TAXI FOR TAKEOFF, THE AIRCRAFT DISPLAYED CPCS MISCOMPAIR AND PUSHER / SHAKER FAIL WARNING MESSAGES. THE AIRC RAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE PRESSURIZATION CONTROL PANEL (P/N 22260A020201). MAI NTENANCE ALSO INSPECTED AND REPLACED THE LEFT HAND ANGLE OF ATTACK PROBE, IN ACCORDANCE WITH THE DORNIER MAINTENANCE MAN UAL. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082100758 19980821 00758 NM 1998 8 21 VNAA9808016 1 19980817 A 7603 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 433JS 3047 WHEN THE POWER LEVERS WERE ADVANCED FOR TAKEOFF, THE RIGHT HAND POWER LEVER WOULD NOT MOVE PAST THE FLIGHT IDLE POSITION . THE AIRCRAFT ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBED THE RIGHT HAND POWER LEVE R FLIGHT IDLE LOCK GATE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-21. NO OTHER DEFECTS WERE NOTED, AND THE A IRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082700001 19980827 00001 EU 1998 8 27 98FDEA00476 1 19980730 A 3230 RETRACT MECH AIRBUS 310 A310203 EU LANDING GEAR MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 425FE 264 98-0187 STA-ATL - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF SYSTEM 1 OR SYSTEM 2, INTERLOCK ENGAGED. 2 L 7 2 4F RT A35EU 1998082700002 19980827 00002 1998 8 27 TWAA9812702 4 19980805 A 2565 SLIDE DOUG DC9 DC983 3022083 WP PAX DOOR DEPLOYED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9405T 53141 PARKED ON THE GATE, THE AFT LEFT CABIN DOOR WAS OPENED FOR COOLING WITHOUT REMOVING THE ESCAPE SLIDE GIRT BAR. THE ESCA PE SLIDE ONLY PARTIALLY DEPLOYED. BOTTLE PRESSURE WAS REPORTED EMPTY. CHECK-C 11-16-97 MCI. 2 L 7 2 4F RT A6WE 1998082700003 19980827 00003 WP 1998 8 27 TWAA9812704 1 19980802 A 5712 RIB DOUG DC9 DC983 3022083 WP WS 610 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9620D 53591 DURING MAINT, FOUND RT WING RIB DAMAGED AT SLAT TRACK OPENING XOS=610, IDLER TRACK NR 15. REMOVED AND REPLACED RIBS PER SRM 51-20-2, 51-30-5, AND 51-30-8, AND STANDARD MAINTENANCE PRACTICES. 2 L 7 2 4F RT A6WE 1998082700004 19980827 00004 NE 1998 8 27 SWIA971220 2 19980708 A 7321 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 129AM 120119 ON CLIMB-OUT LEFT EEC RED LIGHT/WHITE MANUAL REVERSION LIGHT WITH LEFT ENGINE SURGE. DURING EEC FAILURE CHECK LIST TORQ UE INDICATED 115 PERCENT AND NP 45 PERCENT THEN INCREASED TO TORQUE 130 PERCENT AND NP APPROXIMATELY 21 PERCENT. PRECAU TIONARY ENGINE SHUT DOWN PERFORMED ON LEFT ENGINE. HIGH TORQUE INDICATION FOR APPROXIMATELY 1 MINUTE. CHECKED RGB CHIP DETECTOR SCAVENGE OIL FILTER FOR CHIPS. NO PROBLEMS FOUND. RAN ENGINE IAW MM 71-00-00. OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700005 19980827 00005 SO 1998 8 27 SWIA971221 1 19980708 A 2751 FLAP INDICATION EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 195SW 120127 TAKEOFF PLUS 3 MINUTES GOT FLAP DISAGREEMENT WHEN INITIATED FLAP RETRACTION AFTER TAKEOFF. RETURNED TO SLC. RESET FLAP SYSTEM AND RAN FLAPS SEVERAL TIMES. OPS CHECKS NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700006 19980827 00006 SO 1998 8 27 SWIA971222 1 19980708 A 2150 PACK EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 212SW 120276 ON TAKEOFF LEFT BLEED OVERHEAT ILLUMINATED AND EXTREMELY HOT AIR CAME OUT OF AIR CONDITIONING VENTS AND BLEED EYELETS. R ETURNED TO SLC. OPERATED BOTH PACKS FROM APU BLEED. NO FAULT FOUND. PACKS OPERATE NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700007 19980827 00007 EA 1998 8 27 SWIA971223 1 19980708 A 3244 TIRE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 403SW 7028 HEARD LOUD BANG AT ROTATION ON TAKEOFF ON RUNWAY 34L. HAD TOWER CHECK FOR DEBRIS ON RUNWAY AND TOWER CONFIRMED TIRE DEB RIS ON RUNWAY SURFACE. RETURNED FOR LANDING WHICH WAS UNEVENTFUL. POST FLIGHT SHOWED A THROWN CAP ON RIGHT NOSE GEAR. INSPECTED AIRCRAFT PER ST CARD AND REPLACED BOTH NOSE WHEEL TIRE ASSEMBLIES. SERVICED THE WHEEL ASSEMBLIES IAW MM 32-4 2-01. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082700008 19980827 00008 SO 1998 8 27 SWIA971224 1 19980708 A 5280 BRACKET EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 MAIN GEAR WOULD NOT RETRACT. CYCLED HANDLE, STILL DOWN INDICATION. NOSE GEAR RETRACTED FINE. INSTALLED NEW GEAR DOOR HINGE BRACKET ON RIGHT GEAR INBOARDD FORWARD DOOR. ADJUSTED AND SWUNG GEAR 20 TIMES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700009 19980827 00009 NE 1998 8 27 SWIA971225 2 19980706 A 7510 WATER SEPARATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT DE-ICE SYST MALFUNCTIONED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 218SW 120287 ON CLIMB-OUT, LEFT DUCT LEAK LIGHT CAME ON. FOLLOWED QRH AND SHUT THE LEFT ENGINE DOWN. REPLACED LEFT DE-ICE WATER SEP ARATOR. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700010 19980827 00010 1998 8 27 SWIA971226 4 19980706 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE STALL WARNING FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 408SW 7055 STALL FAIL MESSAGE CAME ON DURING INITIAL CLIMB OUT. RETURNED TO SLC. REPLACED STALL WARNING COMPUTOR. OPS CHECKS GOO D. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082700011 19980827 00011 SO 1998 8 27 SWIA971227 1 19980707 A 2751 CONTROL PANEL EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS TRIPPED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 1117H 120117 UPON FLAP RETRACTION WE GOT FLAP DISAGREEMENT AND THE OUTBOARD PAIR APPEARED MORE EXTENDED THAN THE REST ON THE FLAP PA NEL. RETURNED TO SEA. RESET FLAP PANEL. FLAPS OPS CHECKS GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700012 19980827 00012 SO 1998 8 27 SWIA971228 1 19980707 A 3230 12038594001 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 221SW 120290 AFTER TAKEOFF, LEFT MAIN LANDING GEAR DID NOT RETRACT. MADE A STRANGE NOISE (SURGING HYDRAULIC AND/OR WIND NOISE). LOW ERED GEAR AND LANDED NORMALLY AFTER RETURNING TO LA. REPLACED LANDING CONTROL BOX. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700013 19980827 00013 SO 1998 8 27 SWIA971229 1 19980809 A 2910 FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE GREEN HYD SYST DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 218SW 120287 GREEN HYDRAULIC FILTER LIGHT CAME ON AFTER TAKEOFF. RETURNED TO SLC. REPLACED GREEN SYSTEM PRESSURE AND RETURN FILTERS . NO VISIBLE CONTAMINATION FOUND (RETURN PIN WAS POPPED). RAN BOTH HYDRAULIC SYSTEMS 15 MINUTES AND ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998082700014 19980827 00014 WP 1998 8 27 TWAA9812901 1 19980807 A 5720 TIP DOUG DC9 DC983 3022083 WP RT WING DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9620D 53591 THE RT WING TIP AND TIP TRAILING EDGE WERE DAMAGED WHEN STRUCK ON THE GROUND. REPLACED WING TIP ASSY AND INSTALLED NEW TRAILING EDGE, PER SRM 51-30-1 AND STANDARD MAINT PRACTICES. 2 L 7 2 4F RT A6WE 1998082700015 19980827 00015 WP 1998 8 27 VTZA98192 2 19980516 A 7260 31035992 DIAPHRAGM BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE331* 01514 WP RT ENGINE SEPARATED A VTZA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 EA 27 496UE 900 P66048 FLT 6377 - IAD-CRW - DURING APPROACH, MADE A SCHEDULED LANDING AT CRW WITH ONE DISCREPANCY WHICH WAS RT ENGINE FLAMED OU T. CREW SHUT DOWN ENGINE. AIRCRAFT WENT TO THE GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND IDLER S PUR GEAR DIAPHRAGM SEPARATED FROM ASSEMBLY. MAINTENANCE REMOVED AND REPLACED DIAPHRAGM. OPS CHECK OK. AIRCRAFT WAS RE LEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E2WE 1998082700016 19980827 00016 WP 1998 8 27 AALA981289 1 19980630 A 5320 DOOR FRAME DOUG DC9 DC982 3022082 WP BS 1174 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 435AA 49453 TUL - AFT CARGO DOOR LOWER DOOR BEAM AT AFT DOOR STOP, DOOR STOP BOLT HOLE IN SILL FRAME HAS NO EDGE DISTANCE ON OUTBOAR D SIDE OF HOLE. INSTALLED DOUBLER ON AFT BOTTOM DOOR STOP BOLT HOLE AND DOOR BEAM PER AARD 53-10-00-16. (M) 2 L 7 2 4F A6WE 1998082700017 19980827 00017 NM 1998 8 27 EISA98129 1 19980612 A 5320 FITTING BOEING 727 727231 1384079 NM BS 740 MISMANUFACTURED A EISA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 12305 65287 19562 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD 045R, FOUND RIGHT HAND 740 FITTING CRACKED. DURING REPLACEMENT OF 74 0 FITTING, FOUND THAT REPLACEMENT FITTING WAS DIFFERENT. THE EDGE DISTANCE WAS TOO CLOSE. BOEING ENGINEERING SUPPLIED DRAWING AND INFORMATION TO CORRECT PROBLEM. REF E01 R980609DTD AND E01-DAL 98-0021RR AND 8110-3 FORM. ACFT TT: 65,287 :32 HOURS. ACFT TC: 44,162. (X) 2 L 7 3 4F A3WE 1998082700018 19980827 00018 WP 1998 8 27 TWAA9813203 1 19980810 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 EIBWD 49575 DURING MAINT FOUND CEILING EMERGENCY LIGHT AT SEAT ROW 33D INOP. REPLACED BATTERY PACK. CHECK-C 2-6-98. 2 L 7 2 4F RT A6WE 1998082700019 19980827 00019 WP 1998 8 27 TWAA9813206 1 19980810 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 439 SCRATCHED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9621A 53592 ON LT FUSELAGE FOUND DENT AND SCRATCH AT LONGERON 21, STA 439 TO 470, 1.5 INCH WIDE BY 36 INCH LONG AND .070 DEEP, PARAL LEL TO LONGERON. FABRICATED AND INSTALLED EXTERNAL DOUBLER PER SRM 53-04, FIG 12B, PG 39. ENGR CONCURRENCE A3250800082 AND A3250800087. ----CLOSED----- 2 L 7 2 4F RT A6WE 1998082800001 19980828 00001 SO 1998 8 28 C2XA98BT047 1 19980706 A 3350 7287103503 CONTROLLER EMB 145 EMB145 SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15941 145035 EWR - CREW REPORTED 'EMERGENCY LIGHTS WILL NOT SHUT OFF. MAINTENANCE FOUND A FAULTY EMERGENCY LIGHT CONTROLLER. REMOVE D AND REPLACED UNIT. OPS CHECKED GOOD. (X) 2 L 7 2 4F RT T00011AT 1998082800002 19980828 00002 NM 1998 8 28 TWAA9813301 1 19980818 A 3397 WIRE BOEING 767 7673Y0 NM CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 EGRESS LIGHTS FLOOR STRIP IN FIRST CLASS GALLEY AND AT REAR GALLEY WERE FOUND INOPERATIVE. REPAIRED BROKEN WIRE TO EG RESS LIGHTS IN BOTH AREAS. CHECK-C 6-3-98 LAX. 2 L 7 2 4F RT A1NM 1998082800003 19980828 00003 WP 1998 8 28 TWAA9813302 1 19980814 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 1285 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9616G 53563 DURING CHECK-C MAINT, FOUND A DENT AT STA 1285 BETWEEN STR 24L AND 25L, RUNNING FROM STR TO STA, 6 IN BY 4 IN BY .070 DE EP. CUT OUT DAMAGED AREA AND INSTALLED EXTERNAL DOUBLER AND FASTENERS PER SRM 53-04 GENERAL FUSELAGE REPAIR FOR PLATING , FIG 12B, CLASS 1 REPAIR. 2 L 7 2 4F RT A6WE 1998082800004 19980828 00004 EU 1998 8 28 MALA976183 1 19980816 A 3230 HP848430721 VALVE SAAB SF340 340B 7860101 EU GEAR BAY FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 422XJ 422 WHILE INBOUND, LANDING GEAR WOULD NOT COME DOWN AFTER PULLING LANDING GEAR HANDLE. NOTICED LANDING GEAR CONTROL CIRCUIT BREAKER POPPED. REST NUMEROUS TIMES, TRIED PUMPING GEAR DOWN, UNSUCCESSFU. PULLED EMERGENCY LANDING HANDLE, COMPLETED EMERGENCY GEAR EXTENSION, 3 GREEN LIGHTS. LANDED WITHOUT ANY GEAR PROBLEMS. MAINTENANCE REPLACED LANDING GEAR CONTROL VALVE. ALL OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998082800005 19980828 00005 EU 1998 8 28 MALA976184 1 19980816 A 2432 40787 BATTERY SAAB SF340 SF340A 7850100 EU LT & RT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 106XJ 106 DURING FLIGHT WITH EXTERNAL POWER MELED, LEFT AND RIGHT BATTERY TEMPS RUNNING HIGH. AIRCRAFT RETURNED TO MSP. MAINTENA NCE REPLACED RT AND LT BATTERIES, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998082800006 19980828 00006 EU 1998 8 28 MALA976185 1 19980815 A 7930 523535 INDICATOR SAAB SF340 340B 7860101 EU COCKPIT STICKING A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 233CH 233 EN ROUTE, RIGHT PROP OIL TEMP INDICATOR ROSE TO 100 DEGREES, RETURNED TO MSP. MAINTENANCE REPLACED RT PGB OIL PSI/TEMP INDICATOR. GROUND RUNS AND OPS GOOD. 2 L 7 2 4T RT A52EU 1998082800007 19980828 00007 EU 1998 8 28 MALA976186 1 19980813 A 5753 SPAR SAAB SF340 SF340A 7850100 EU LT & RT TE FLAPS CRACKED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 991XJ 091 DURING 4,000 HOUR CHECK, CRACKS IN FLAP REAR SPAR AND LOWER SKIN AT WS 142 LT AND RT FLAPS. MAINTENANCE COMPLETED EO NR S57007. STOP DRILLED THE CRACKS IN BOTH END IN ACCORDANCE TO CH 51-70-03 AND SEALED STOP HOLES. INSTALLED A DOUBLER P LATE AND SHIMMED. SURFACE TREATED. INSTALLED NEW FASTENERS ACCORDING TO THE SP 51-40-21. 2 L 7 2 4T RT A52EU 1998082800008 19980828 00008 EU 1998 8 28 MALA976187 1 19980811 A 5414 SKIN SAAB SF340 SF340A 7850100 EU LT NACELLE CHAFED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 991XJ 091 DURING 4,000 HOUR CHECK, CHAFING WAS FOUND ON LT I/B NACELLE SKIN. MAINTENANCE COMPLETED EO NR S54009, BLEND OUT THE CH AFING AREA SMOOTHLY, REINFORCED WITH DOUBLER, SEALED DOUBLER WITH NEW FASTENERS INSTALLED PER NAS1669-3 IAW SRM 51-20-42 /43. 2 L 7 2 4T RT A52EU 1998082800009 19980828 00009 EU 1998 8 28 AWXA9800190 1 19980815 A 2121 EVT3454G FAN AIRBUS 320 A320231 3930325 EU E/E COMPT FAILED A AWXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 WP 28 627AW 23317 12110 66 DURING CLIMBOUT, EXPERIENCED A VIBRATION THAT SEEMED TO ORIGINATE IN THE AREA BELOW THE FLIGHT DECK, FOLLOWED BY AN ELEC TRICAL SMOKE SMELL. SHUT DOWN OF VENTILATION BLOWER FAN, STOPPED ALL NOISES, VIBRATIONS AND SMELLS. REPLACED AVIONICS COOLING FAN, SYSTEM OPS NORMAL. 2 L 7 2 4F RT A28NM 1998082800010 19980828 00010 NM 1998 8 28 RAAA98B1089 1 19980818 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998082800011 19980828 00011 NM 1998 8 28 CALA9801483 1 19980819 A 3230 69141064 CYLINDER BOEING 737 737524 1384721 NM NLG INOPERATIVE A CALA K NONE O OTHER AP APPROACH 1 SW 09 14645 17586 28906 WHEN LANDING GEAR WAS LOWERED ON APPROACH, THE NOSE GEAR APPEARED TO HANG UP FOR SEVERAL SECONDS AND THEN SLAMMED DOWN H ARD. THREE GREEN GEAR LIGHTS WERE INDICATED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR TRANSFER CYLINDER AT FAULT. THE NLG TRANSFER CYLINDER WAS REMOVED AND REPLACED IAW MM 32-33-41. THE GEAR WAS SWUNG SEV ERAL TIMES WITH OPERATION CHECKING GOOD AND NO LEAKS WERE NOTED. 2 L 7 2 4F RT A16WE 1998082800012 19980828 00012 NM 1998 8 28 CALA9801484 1 19980819 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 560 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOOR ATTACH ANGLE IN FORWARD CARGO PIT CORRODED AT STA 560, RBL 20. THE CORRODED AREA WAS CUT OUT, AN ANGLE AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, FIGURE 1. 2 L 7 3 4F A3WE 1998082800013 19980828 00013 NM 1998 8 28 CALA9801485 1 19980819 A 5320 BRACKET BOEING 727 727232 1384082 NM BS 251.8 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CORROSION ON TWO L-ANGLE BRACKETS AT AFT SIDE OF STA 251.8, UP SIX INCHES AND TWELVE INCHES FROM FLOOR LEFT SIDE OF COCKPIT. TWO NEW L-ANGLE BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 53-10-2, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082800014 19980828 00014 NM 1998 8 28 CALA9801486 1 19980819 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 15 AND LBL 20. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998082800015 19980828 00015 NM 1998 8 28 CALA9801487 1 19980820 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344, LBL 30 TO 20. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998082800016 19980828 00016 SO 1998 8 28 COMA9810179 1 19980818 A 3230 12032943001 SEQUENCE VALVE EMB 120 EMB120RT SO NLG FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 256CA 17215 120245 NLG WOULD NOT RETRACT. REPLACED THE LEFT HAND NLG DOOR SEQUENCE VALVE. 2 L 7 2 4T RT A31SO 1998082800017 19980828 00017 SO 1998 8 28 COMA9810180 1 19980818 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 205CA 13693 650 120205 AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998082800018 19980828 00018 EA 1998 8 28 COMA9860234 1 19980817 A 2430 P600A803E014 CONTROLLER CNDAIR CL600 CL6002B19 EA BATTERY COMPT FAILED A COMA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 918CA 7018 TRU NR 2 FAILED FOLLOWED BY ELECTRICAL BURNING SMELL. REPLACED BURNED MAIN BATTERY POWER CONTROLLER IN JB5. 2 L 7 2 4F RT A21EA 1998082800019 19980828 00019 EA 1998 8 28 COMA9860235 1 19980818 A 2421 IDG CNDAIR CL600 CL6002B19 EA RIGHT FAILED A COMA K NONE H ELECT. POWER LOSS-50 PC CR CRUISE 1 SO 01 932CA 7038 RIGHT HAND GENERATOR CAUTION MESSAGE. DEFERRED THE RIGHT HAND IDG PER MEL. 2 L 7 2 4F RT A21EA 1998082800020 19980828 00020 NM 1998 8 28 UPS98227472 1 19980811 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOORBEAM BS 312 LBL 3 TO 25 WL 208. REMOVED OUT OF LIMITS CORRODED FLOORBEAM, FABRICATED NEW FLOORBEAM AND REPAIR PARTS IAW SRM 53-10-8, 51-30-2, INSTALLED PARTS IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998082800021 19980828 00021 NM 1998 8 28 UPS98227473 1 19980804 A 5314 652355567 KEEL BEAM BOEING 727 727247 138408F NM BS 750 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, SEVERAL RIVETS SHOW SIGNS OF CORROSION EMANATING FROM FASTENER HOLES, THIRD HOLE AFT ON KEEL BEAM, L OWER FWD CHORD, (MARKED) (C53-123-01.03-01) STA 750 BL 0. LOWER CHORD FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10- 1. INSTALLED NEW LOWER CHORD PER SRM 51-40-4. 2 L 7 3 4F A3WE 1998082800022 19980828 00022 NM 1998 8 28 UPS98227474 1 19980817 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 720 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) FLOORBEAM BS 720D LBL 5 TO 25 WL 208. REMOVED CORROSION FOUND OUT OF L IMITS. REPAIRED IAW SRM 53-10-02, 53-10-8, 51-40-02, 51-30-02. 2 L 7 3 4F A3WE 1998082800023 19980828 00023 NM 1998 8 28 UPS98227475 1 19980731 A 5320 655614870 CREASE BEAM BOEING 727 727247 138408F NM BS 1048-1058 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-224-06-1B) ON MOP SILL OUTER FLANGE AT LEFT HAND AFT SERVICE DOOR CUTOUT BS 1048 TO 1 058 LBL 66 WL 209. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED NEW CREASE BEAM PER SRM 51-30-5, MM 51-20-21, AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998082800024 19980828 00024 NM 1998 8 28 UPS98227476 1 19980816 A 5347 BAC1520780 SEAT TRACK BOEING 727 727247 138408F NM BS 655-668 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION ON SEAT TRACK BS 655 TO 668, LBL 45, WL 208. REMOVED CORROSION FROM SEAT TRACK BS 668 TO 655, FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK BS 480 TO 685, ALL WORK PERFORMED IAW SRM 51-10-06, 53-10-01, 51-30 -02, 53-10-05. 2 L 7 3 4F A3WE 1998082800025 19980828 00025 NM 1998 8 28 UPS98227477 1 19980817 A 5320 SUPPORT BOEING 727 727247 138408F NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-224-01.05-01) ON FLOOR SUPPORT BS 344 LBL 30 WL 208. REPLACED FLOOR SUPPORT PER 727 SRM 51-30-2 AND 51-20-4. 2 L 7 3 4F A3WE 1998082800026 19980828 00026 NM 1998 8 28 UPS98227478 1 19980817 A 5320 CLIP BOEING 727 727247 138408F NM BS 540 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, FWD BAY STR 23L, BS 540 HAS A CRACKED AND CORRODED STRINGER CLIP. REPLACED STRINGER CLIP PER 727 SR M 51-30-2. 2 L 7 3 4F A3WE 1998082800027 19980828 00027 NM 1998 8 28 UPS98227479 1 19980817 A 5320 SUPPORT BOEING 727 727247 138408F NM BS 312-322 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION ON (C53-224-01.05-01) FLOOR SUPPORT BS 312 TO 322 LBL 30 WL 208. REPLACED FLOOR SUPPORT P ER 727 SRM 51-20-4 AND 51-30-2. 2 L 7 3 4F A3WE 1998082800028 19980828 00028 NM 1998 8 28 UPS98527486 1 19980820 A 3260 67410332206 BULB BOEING 757 75724APF 1384969 NM LT & RT MLG FAILED A IPXA K NONE L NO TEST CR CRUISE 1 SO 01 436UP 25467 INSPECTION TYPE-N/A, EN ROUNTE DID A LIGHT TEST AND OBSERVE RIGHT MAIN GEAR LIGHT INOP. CALLED MMOC TO CHANGE LIGHTS AN D OBSERVED BOTH MAIN GEAR LIGHTS WERE INOP. DID A FLY-BY IN DSM. AIRCRAFT NEEDS SPARE BULBS (387). BITE PSEU AND FOU ND NO FAULTS. REMOVED AND REPLACED LT AND RT MAIN GEAR IND LAMP ASSY'S IAW MM33-16-02. OP CK NORMAL. (P/N 674-1033-22 06) 2 L 7 2 4F RT A2NM 1998082800029 19980828 00029 WP 1998 8 28 UPS98827471 1 19980724 A 5311 56417832 FRAME DOUG DC8 DC871F 302199D WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, BULGING AT THE CUSP STA 8 AT LONG 21R. REMOVED FASTENERS FOUND STA 8 FRAME CORRODED OUT OF LIMITS. C UT OUT DAMAGED FRAME, FABRICATED AND REPLACED FRAME PER DAC DWG 5641783 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082800030 19980828 00030 WP 1998 8 28 UPS98827480 1 19980805 A 5320 PLUG DOUG DC8 DC873F 302199F WP BS 860-880 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, SEAT TRACK D BETWEEN STA 860 AND 880 HAS CORRODED SEAT TRACK PLUG ON BOTTOM SIDE. REMOVED AND REP LACED PLUG AND SPLICE IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998082800031 19980828 00031 WP 1998 8 28 UPS98827481 1 19980805 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 800-1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, SEAT TRACK G HAS CORROSION AT STA 800 TO STA 1100 AS MARKED. REMOVED CORROSION ON SEAT TRACK IAW DC8 SRM 51-1-8 AND INSTALLED 3 SEAT TRACK PLUG ON STA 941, 917, 816 IAW DC8 SRM 53-2-3 FIG 6D. TREATED ALODINED AND PRI MED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998082800032 19980828 00032 WP 1998 8 28 UPS98827482 1 19980805 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 759-1100 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, SEAT TRACK E CORRODED FS 759 TO 1100. REMOVED CORROSION IAW DC8 SRM 511-8, 53-2-3. FOUND AT FS 1 040, OUT OF LIMITS CORROSION. REMOVED SEAT TRACK FROM 1030 TO 1050, FABBED, DRILLED, INSTALLED NEW SECTION IAW DC8 SRM 53-2-3 AND 51-1-8. 2 L 7 4 4F RT 4A25 1998082800033 19980828 00033 WP 1998 8 28 UPS98827483 1 19980804 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 70 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, LONG 33 RT END SPLICE TO FRAME CORRODED STA 70. REMOVED CORROSION IAW DC8 SRM 51-1-8. ALODINED A ND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998082800034 19980828 00034 WP 1998 8 28 UPS98827485 1 19980724 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 603.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, RT WING L/E SKIN (UPPER) HAS 4 CRACKS AT STA XFS603.750. REPAIRED AREA IAW SRM 57-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 1998082800035 19980828 00035 EU 1998 8 28 QXEA9801080 1 19980818 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 477AU 11226 EMERGENCY EXIT LIGHTS OUT AT ROW 8E. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998082800036 19980828 00036 NM 1998 8 28 QXEA9801081 1 19980817 A 2611 473054 SMOKE DETECTOR DHAV 82523211001 DHAV DHC8 DHC8202 2809007 NM CABIN MALFUNCTIONED A QXEA K NONE N FALSE WARNING CL CLIMB 1 NM 09 350PH 488 SMOKE DETECTOR GOES OFF IN LAVATORY WHEN NR 2 BLEED AIR IS TURNED ON, STOPS AFTER ABOUT 1 MINUTE. INSPECTED NR 2 BLEED SYSTEM, NO DEFECTS NOTED. REPLACED THE LAVATORY SMOKE DETECTOR, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998082800037 19980828 00037 EU 1998 8 28 98FDEA00522 1 19980818 A 2420 FC3400KE4835P CONNECTOR AIRBUS 310 A310203 EU NR 2 ENGINE BURNED A FDEA A UNSCHED LANDING G H J MULTIPLE FAILURE ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 25 443FE 283 AFTER T/O ALL INSTR PWR BY NR 2 ENG GEN SYS START SPIKING, LIGHT FLICKER. NR 2 FUEL FLOW IND AND NR 2 N2 FLUCT. FUEL P UMPS FAIL. A/C DIVERTED TO ATL. MX FOUND BURNED PIN ON NR 2 ENG GEN FEEDER HARNESS CONNECTOR VC4955P. REPLACED THE NR 2 GEN LINE. MX FOUND ECAM FREQ IND INOP. 2 L 7 2 4F RT A35EU 1998082800038 19980828 00038 NM 1998 8 28 98FDEA00523 1 19980818 A 5315 651631526 FLOORBEAM BOEING 727 727227 1384078 NM BS 328 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 WHILE WORKING NR 0170 FOUND CORROSION ON FLOORBEAM BS 328, RBL 14, WL 208. *S/D* REPAIRED FLOORBEAM BS 328, RBL 14, WL 208 PER FED-EX SRM 53-10-8 FIG 9. 2 L 7 3 4F A3WE 1998082800039 19980828 00039 NM 1998 8 28 98FDEA00524 1 19980819 A 3230 SWITCH BOEING 727 72725C 138400H NM LT MLG FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 119FE 19301 AFTER T/O, THE LAND GEAR WOULD NOT RETRACT. APPROPRIATE RED TABS FOLLOW WITH NEG RESULT. FOUND THE LT MAIN LAND GEAR G ROUND SAFETY SWITCH OVER CTR IN WRONG POSITION. REPOSITIONED AND PERFORMED TRIPLE GEAR SWING PER FEDEX M/M 32-32-0, OPS CK GOOD. 2 L 7 3 4F A3WE 1998082800040 19980828 00040 NM 1998 8 28 DHL98741004 1 19980820 A 4900 380678111 APU BOEING 727 7272Q9 138448M NM APU COMPT MALFUNCTIONED A DHLA A F UNSCHED LANDING ACTIVATE FIRE EXT. J B WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 741DH 21931 DEPARTED SMF WITH 13TH STAGE MOD VALVE DMI TO OPEN POSITION, NR 1 BLEED OFF, LEFT PACK OFF. WHEN LEFT PACK TURNED ON IN FLIGHT, NOTICED A STRONG ODOR IN COCKPIT. THE ODOR INCREASED AS WE TURNED BACK FOR LANDING. RECEIVED APU FIRE INDICA TION, PULLED HANDLE AND DISCHARGED FIRE BOTTLE. PUT ON EXTERNAL AIR ON AIRCRAFT, APPLIED BOTH PACKS AND 100 AMP LOAD. G ROUND RAN ALL ENGINES AND PACKS WITH 100 AMP LOAD, OPS CHECK NORMAL. INSPECTED WHEEL WELL AREA FOR EVIDENCE OF FIRE, S MOKE AND ELECTICAL DAMAGE, NONE NOTED . 2 L 7 3 4F RT A3WE 1998082800041 19980828 00041 WP 1998 8 28 RRXA98335 1 19980816 A 2150 8212C HEAT EXCHANGER DOUG DC8 DC862F 3021972 WP RIGHT CRACKED A RRXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 15 997CF 46154 AFT T/O GEAR RETRACTION LOUD VIBRATION TYPE NOISE COMING FROM NOSE AREA. NOISE BECAME WORSE WITH SPEED. FOUND RT HEAT EXCHANGER INLET AND OUTLET HEADER ASSEMBLY'S CRACKED. UPON DISASSEMBLY FOUND EXCHANGER FOULED WITH FEATHER. CHANGED HE AT EXCHANGER AND HEADER ASSEMBLYS IAW DC-8 MM CH 21-54-1. LEAK CKS GOOD. 2 L 7 4 4F 4A25 1998082800064 19980828 00064 EU 1998 8 28 98ZZZX2960 1 19980722 A 3250 SD37303ZZXA HOSE STBROS SD3 SD360 8100606 EU NLG STEERING LEAKING A DATA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 13 124CA 24704 SH3652 AFTER DEPARTURE FROM ADF, THE LT AND RT HYDRAULIC CWP LIGHTS CAME ON. THE HYDRAULIC SYSTEM PRESSURE AND CONTENTS SHOWED 15 PERCENT. THE CREW PUT THE LANDING GEAR DOWN AND FOLLOWED EMERGENCY PROCEDURES. THE CREW DID NOT DECLARE AN EMERGEN CY WITH THE TOWER AND LANDED IN CRW WITH NO INCIDENT. THE NOSE WHEEL STEERING FLEX LINES WERE REPLACED, P/N SD3-73-0311X A AND P/N SD 3-73-031SXA. THE HYDRAULICS SERVICED, GROUND RAN AND TAXI CHECK OKAY. OPS CHECK GOOD. 2 H 7 2 4T A41EU 1998082800066 19980828 00066 CE 1998 8 28 98ZZZX2962 1 19980723 A 5280 207100 DOOR BEECH 18 C45H 1151018 CE NLG DAMAGED A KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 231SK AF856 NOSE GEAR DOORS DAMAGED DUE TO HIGH WINDS. REMOVED GEAR DOORS FOR MAINTENANCE FERRY FLIGHT TO YIP. REPLACED NOSE GEAR DOORS WITH SERVICEABLE UNITS. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR AND RIGGED AS REQUIRED. WINDS WERE EXPERIENCE D DURING LANDING - GUSTS UP TO 70 KNOTS. 1 L 7 2 3R A765 1998082800067 19980828 00067 CE 1998 8 28 98ZZZX2963 1 19980723 A 5280 207101 DOOR BEECH 18 C45H 1151018 CE NLG DAMAGED A KKFA K NONE O OTHER IN INSP/MAINT 1 GL 23 231SK AF856 NOSE GEAR DOORS DAMAGED DUE TO HIGH WINDS. REMOVED GEAR DOORS FOR MAINTENANCE FERRY FLIGHT TO YIP. REPLACED NOSE GEAR DOORS WITH SERVICEABLE UNITS. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR AND RIGGED AS REQUIRED. WINDS WERE EXPERIENCE D DURING LANDING - GUSTS UP TO 70 KNOTS. 1 L 7 2 3R A765 1998082800074 19980828 00074 NM 1998 8 28 98ZZZX2970 1 19980610 A 3230 69181946 SUPPORT BOEING 727 727225 1384077 NM NLG UPLOCK CRACKED A C8GA A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS LD LANDING 1 SO 15 808EA 22439 AFTER NORMAL LANDING, GEAR EXTENSION AND NORMAL EXTENSION OF 'LANDING FLAPS' HYDRAULIC SYSTEM 'A' QUANTITY DROPPED TO ZE RO. BOTH LOW PRESSURE LIGHTS ILLUMINATED. UPON INSPECTION, FOUND NOSE GEAR UPLOCK ACTUATOR CHANNEL (SUPPORT) CRACKED. REMOVED AND REPLACED CHANNEL PER 32-33-11. PERFORMED NORMAL AND MANUAL NOSE GEAR EXTENSION, OPS CHECKED NORMAL. FOUND ACTUATOR HYDRAULIC LINES DAMAGED, REPLACED SAME. 2 L 7 3 4F A3WE 1998082800081 19980828 00081 GL 1998 8 28 98ZZZX2976 2 19980720 A 7321 3300588 FCU CVAC 440 440 2422902 WP ALLSN 501D 501D13H 03004 GL LT ENGINE FAILED A ERAA E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 AL 03 565EA 792 399 501685 IN CRUISE AT 18,000 FEET, LEFT ENGINE GRADUALLY LOST POWER. HP DROPPED FROM 2,000 TO ZERO, TIT FROM 847 TO 450, FF FROM 1,110 TO 600. TRIED TD NULL OFF, POWER LOSS GOT WORSE. TRIED ENGINE HEAT, NO EFFECT. SHUT ENGINE DOWN. DISCONNETED EDC PER CHECKLIST. TIME FROM START TO POWER LOSS TO ENGINE SHUT DOWN WAS APPROXIMATELY 7 MINUTES. THERE WERE NO OTHER ABNORMAL ENGINE INDICATIONS. 2 L 7 2 4R 4 T 6A6 E282 1998082800086 19980828 00086 CE 1998 8 28 98ZZZX2982 1 19980714 A 2820 510010877 LINE CESSNA 402 402B 207590P CE LT WING INBD CHAFED A A HBCA K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS IN INSP/MAINT 1 SW 11 6350X 7413 402B1317 WHILE READING THE ACFT HOUR METER, A STRONG FUEL SMELL WAS NOTICED. A FUEL STAIN WAS NOTICED UNDER THE LEFT WING STARTI NG AT THE INBD ENGINE NACELLE AND SEEPING DOWN THE MAIN WING SPAR TO THE INBD MAIN GEAR DOOR. CROSS-FEED FUEL LINE HAD BEEN CHAFED AFT OF THE TURBOCHARGER BY A STRINGER AND WAS LEAKING. UNFORTUNATELY, THESE LINES MAINTAIN A POSITIVE PRESS URE ON THEM WITH NO WAY TO TURN OFF THE FUEL. IT IS SUBMITTER'S RECOMMENDATION THAT CESSNA PROVIDE SOME MEANS TO ENABLE THE PILOT TO TURN OFF THE FUEL SUPPLY TO THESE FUEL LINES. 1 L 7 2 3O A7CE 1998082800095 19980828 00095 WP 1998 8 28 TWAA9813401 1 19980806 A 5240 BEAM DOUG DC9 DC951 3022051 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 410EA 47731 DURING CHECK-C MAINT, THE FWD RT SERVICE DOOR BEAM HAD A 2 IN CRACK AT FWD END. REPLACED BEAM IN SHOP ON TICKET 836667 PER SRM 52-05, FIG 25 AND 51-10. 2 L 7 2 4F RT A6WE 1998082800096 19980828 00096 WP 1998 8 28 TWAA9813402 1 19980808 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 294 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 410EA 47731 DURING CHECK-C MAINT, FOUND .25 INCH CRACK IN FLANGE OF LONGERON 24L AT STA 294. CUT OUT DAMAGED SECTION OF LONGERON AN D INSTALLED NEW SECTION AND SPLICE PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 1998082800097 19980828 00097 WP 1998 8 28 TWAA9813403 1 19980808 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 287 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 410EA 47731 DURING CHECK-C MAINT, FOUND .25 INCH CRACK IN FLANGE OF LONGERON 23L AT STA 287. CUT OUT DAMAGED SECTION OF LONGERON, A ND INSTALLED NEW SECTION AND SPLICE PER SRM 53-02, FIG 18. 2 L 7 2 4F RT A6WE 1998082800098 19980828 00098 WP 1998 8 28 TWAA9813404 1 19980812 A 5320 FITTING DOUG DC9 DC951 3022051 WP BS 1167 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 410EA 47731 DURING CHECK-C MAINT, FOUND LONGERON 20R, LONGERON 21R, LONGERON 22R, HAD END FITTINGS CORRODED AT STA 1167 BULKHEAD. R EPLACED END FITTINGS AT STA 1167 AND LONGERON 22R, LONGERON 20R, AND LONGERON 21R PER SRM 51-30-2. 2 L 7 2 4F RT A6WE 1998082800099 19980828 00099 NM 1998 8 28 VJ9800284 1 19980819 A 3350 2013A1A BATTERY PACK BOEING 737 7372P6 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 EICJW 21355 FWD EMERGENCY LIGHT BATTERY PACK FAILED DURING LAY OVER CHECK. REPLACED THE FWD BATTERY PACK. 2 L 7 2 4F RT A16WE 1998082800100 19980828 00100 NM 1998 8 28 K3HA980097 1 19980818 A 3350 079123 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 BULB AND LENSE MISSING. REPLACED LIGHT MODULE ASSEMBLY AND BULB, P/N 3071BPEGPL. OPS CHECK GOOD PER MM 33-59-00. 2 L 7 3 4F A3WE 1998082800101 19980828 00101 GL 1998 8 28 LR7A9836 2 19980820 A 7261 SEAL LKHEED 382 382G 526414U SO ALLSN 501D 501D22A 03006 GL NR 2 ENGINE FAILED A LR7A E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 403LC 555 4590 550338 NR 2 ENG SHUTDOWN IN FLIGHT DUE TO OIL LOSS STARTER GARLOC SEAL LEAKING. REPLACED STARTER GARLOC SEAL IAW 501-D22 MM 72 -0 PG 221. REPLACED SCAVANGE OIL FILTER IAW 501-D22 72-2-5 DUE TO PIN BEING POPPED (BYPASS). 2 H 7 4 4T 4 T A1SO E282 1998082800102 19980828 00102 NM 1998 8 28 CALA9801488 1 19980820 A 2910 HYD LINE BOEING 737 737524 1384721 NM TE FLAPS LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 13624 27528 THE AIRCRAFT HAD ASSYMETRIC LOCKOUT BETWEEN FLAPS 2 AND 5 ON APPROACH TO IAH. THE ALTERNATE FLAP SYSTEM WAS USED AND TH E AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FLAP HYDRAULIC LINE LEAKING IN LT FORWARD AIR CONDITIONING BAY. T HE HYDRAULIC LINE WAS REPAIRED AND LEAK CHECK WAS GOOD. NO OTHER DEFECTS WERE NOTED. 2 L 7 2 4F RT A16WE 1998082800103 19980828 00103 NM 1998 8 28 CALA9801489 1 19980819 A 5400 CASTING BOEING 737 7372C0 1384488 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND NR 1 ENGINE PYLON PANEL LOWER SIDE NUT PLATE AREA CRACKED AND FOUND A 1 CRACK IN INBOARD FORWARD ATTACH CASTING. THE CASTING WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10- 2, AND MM 51-20-11. A NEW CASTING WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998082800104 19980828 00104 NM 1998 8 28 CALA9801490 1 19980820 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1050-1060 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1050-1060. A NEW SEAT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5 , FIGURE 1. 2 L 7 3 4F A3WE 1998082800105 19980828 00105 NM 1998 8 28 CALA9801491 1 19980820 A 5210 SUPPORT BOEING 727 727232 1384082 NM R-1 DOOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND R-1 DOOR FORWARD SUPPORT CORRODED. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTAL LED IAW SRM 52-10-1 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082800106 19980828 00106 NM 1998 8 28 CALA9801492 1 19980820 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 950-950A. THE SEAT TRACK WAS REMOVED. A NEW SEAT TRACK WAS FAB RICATED AND INSTALLED IAW SRM 53-10-5, FIGURE 1 AND 7, 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1998082800107 19980828 00107 NM 1998 8 28 CALA9801493 1 19980820 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 990-1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT OUTBOARD SEAT TRACK CORRODED AT STA 990-1030. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS F ABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-5, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082800108 19980828 00108 NM 1998 8 28 CALA9801494 1 19980820 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND SEAT TRACK CORRODED AT STA 950A-950B, LBL 46. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS FABR ICATED AND INSTALLED IAW SRM 51-30-2, 51-10-5, FIGURE 1, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998082800109 19980828 00109 NM 1998 8 28 CALA9801495 1 19980820 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND STIFFENER CRACKED AT LT WING TRAILING EDGE FALSE SPAR WHERE FLAP TRACK NR 3 IS LOCATED. THE STIFFENER WAS REMOVED IAW SRM 51-30-2. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW SRM 51-20-1, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998082800110 19980828 00110 NM 1998 8 28 UPS98227488 1 19980813 A 5741 69139017 BOTTLE PIN BOEING 727 72751C 1384015 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D LT BS 750 BOTTLE PIN FOUND WITH LIGHT PITTING CORROSION. PIN REPLACED IAW MM 57-41-00. 2 L 7 3 4F A3WE 1998082800112 19980828 00112 NM 1998 8 28 UPS98227491 1 19980729 A 5754 RIB BOEING 727 72751C 1384015 NM NR 2 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, NR 2 LE SLAT RIB CRACKED ADJACENT TO ANTI-ICE DUCT (TELESCOPIC). NR 2 SLAT RIB REPAIRED IAW SRM 51-4 0-2. 2 L 7 3 4F A3WE 1998082800113 19980828 00113 NM 1998 8 28 UPS98227492 1 19980806 A 7830 WEB BOEING 727 72751C 1384015 NM NR 1 TR UNIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, ENGINE NR 1 THRUST REV AFT VERTICAL WEB SUSPECT CRACK AT 12 O'CLOCK POSITION AT HYD PIPE BRACKET ATTA CH. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998082800114 19980828 00114 NM 1998 8 28 UPS98227493 1 19980730 A 5412 FIREWALL WEB BOEING 727 72751C 1384015 NM BS 1387.85 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, WEB AT BS 1387.85 LT OVER NR 2 HORIZONTAL FIREWALL IS CRACKED. NEW WEB FABRICATED AND INSTALLED IAW DRAWING NR 65-17555. 2 L 7 3 4F A3WE 1998082800115 19980828 00115 NM 1998 8 28 UPS98227494 1 19980730 A 5754 SKIN BOEING 727 72751C 1384015 NM NR 8 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, CRACKS AT NR 8 SLAT UPPER SIDE AT AFT I/B HOOK ATTACH HOLE. REPAIR CARRIED OUT IAW SRM 57-50-3. 2 L 7 3 4F A3WE 1998082800116 19980828 00116 NM 1998 8 28 UPS98227495 1 19980807 A 5320 WEB BOEING 727 72751C 1384015 NM BS 830 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, COROSION ON WEB RBL 10 BS 830 APPROX. REPAIR CARRIED OUT IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998082800117 19980828 00117 NM 1998 8 28 UPS98227496 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998082800118 19980828 00118 NM 1998 8 28 UPS98227497 1 19980803 A 5210 SKIN BOEING 727 72751C 1384015 NM PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, CRACK ON FWD ENTRY DOOR SKIN .25 EITHER SIDE OF RIVET AT BS 344 STR 9. REPAIR CARRIED OUT IAW SRS E O 98-24-007 UPS ENGINEERING FILE NO 727- 52-0195. 2 L 7 3 4F A3WE 1998082800119 19980828 00119 NM 1998 8 28 UPS98227498 1 19980802 A 5741 69139004 BOTTLE PIN BOEING 727 72751C 1384015 NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, LT BS 740 BOTTLE PIN FOUND WITH PITTING CORROSION. PIN REPLACED IAW MM 57-41-00. 2 L 7 3 4F A3WE 1998082800120 19980828 00120 NM 1998 8 28 UPS98227499 1 19980807 A 5320 FITTING BOEING 727 72751C 1384015 NM BS 360-380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D, 9G BARRIER NET ATTACH FITTING ON FLOOR LBL 20 BETWEEN BS 360-380 HAS SEVERE CORROSION. 9G FITTING AT LBL 20 REPLACED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998082800121 19980828 00121 EU 1998 8 28 QXEA9801082 1 19980818 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 PDX - RIGHT EMERGENCY LIGHT INOPERATIVE AT ROW 9. MAINTENANCE RELAMPED. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998082800122 19980828 00122 EU 1998 8 28 QXEA9801083 1 19980817 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 GEG - FOUND CABIN EMERGENCY EXIT LIGHTS OUT. MAINTENANCE RELAMPED. OPERATION CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998082800123 19980828 00123 NM 1998 8 28 DL72S981702 1 19980818 A 2530 OVEN 11228 BOEING 727 727232 1384082 NM FWD GALLEY SMOKING A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 467DA 20744 FWD GALLEY OVENS EMITTED BURNING PLASTIC SMELL AND VISABLE SMOKE AFTER TURNING ON. FOUND PLASTIC SHIPPING LABEL ON SIDE OF FOOD CARRIER. REMOVED AND REPLACED CARRIER. 2 L 7 3 4F A3WE 1998082800124 19980828 00124 NM 1998 8 28 DL72S981705 1 19980819 A 5720 6483386 CHORD BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 UPPER CHORD ANGLE OF THE RT WING AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS WERE LOCATED AT FASTENER HOLES ON TH E HORIZ FLANGE OF THE CHORD ANGLE UNDER STRINGERS 16 AND 19. ALSO, THE S18 TAB WAS CRACKED. REPAIRED PER ERA 332040-14 . 2 L 7 3 4F A3WE 1998082800125 19980828 00125 NM 1998 8 28 DL767981707 1 19980819 A 5315 141T511183 FLOORBEAM BOEING 767 767232 1385132 NM BS 287 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 110DL 22222 CORROSION WAS FOUND ON THE UPPER SURFACE OF THE BS 287 FLOORBEAM UPPER CHORD. IN ADDITION, AN EXISTING REPAIR WAS ALSO LOCATED IN THE SAME AREA. REPAIRED PER ERA 332044-14. 2 L 7 2 4F RT A1NM 1998082800126 19980828 00126 NM 1998 8 28 DL73S981712 1 19980819 A 3350 BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 323DL 23095 RT O/W EMERGENCY SIGN INOP. REPLACED BATT PK. 2 L 7 2 4F RT A16WE 1998082800127 19980828 00127 NM 1998 8 28 DL75A981716 1 19980819 A 3350 BULB 7839 BOEING 757 757212 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 751AT 23125 ON L/O, FOUND FIRST CLASS EMERGENCY LIGHTS INOP. FOUND SHORTED BULB AT SEAT 2AB. REPLACED SAME. OPS CHECKS NORMAL. 2 L 7 2 4F RT A2NM 1998082800128 19980828 00128 WP 1998 8 28 DLL13981721 1 19980820 A 3350 POWER PACK 5165741 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 786DL 3763561471 193A1123 LOWER GALLEY EMERGENCY CEILING LIGHT AND R2 DOOR EXITS AND CEILING LIGHT INOP. REPLACED 2 EACH POWER PACKS. 2 L 7 3 4F A23WE 1998082800129 19980828 00129 NM 1998 8 28 DLM88981723 1 19980821 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 997DL 53364 CRACK FOUND AT L2R ON THE FUSELAGE STA 1418 FRAME. CRACK WAS 1 INCH IN LENGTH. REPAIRED PER ERA 332078-14. 2 L 7 2 4F RT A6WE 1998082800130 19980828 00130 NM 1998 8 28 DL72S981724 1 19980821 A 5712 6483385 RIB BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 UPPER CHORD OF THE LT WING RIB AT WS 171.5 WAS FOUND W/CRACKS. THE CRACKS WERE LOCATED EMANATING FROM FASTENER HOLES ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER WING STRINGERS 17 AND 20. REPAIRED PER ERA 332081-14. 2 L 7 3 4F A3WE 1998082800131 19980828 00131 NM 1998 8 28 DL767981726 1 19980821 A 5315 111T50483 FLOORBEAM BOEING 767 767232 1385132 NM BS 850 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 110DL 22222 CORROSION DAMAGE WAS FOUND ON THE UPPER CAP OF THE OVERWING LONGITUDINAL FLOORBEAM AT RBL 54, FROM BS 850 TO THE AFT END OF THE UPPER CAP AT APPROX BS 1000. THE UPPER CAP WAS REPLACED, BUT THE ORIGINAL EXTRUSION COULD NOT BE OBTAINED. REP AIRED PER ERA 332058-14. 2 L 7 2 4F RT A1NM 1998082800132 19980828 00132 WP 1998 8 28 RRXA98336 1 19980803 A 5311 56121509 FRAME DOUG DC8 DC871F 302199D WP BS 1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING A MAINTENANCE VISIT, FOUND FRAME LOWER SECTION WITH CORROSION DAMAGE, AT STA 1580 BETWEEN LONGERONS 35 LEFT TO 35 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DE R TIMCO ENGINEERING SKETCH REO-05167. 2 L 7 4 4F RT 4A25 1998082800133 19980828 00133 WP 1998 8 28 RRXA98337 1 19980805 A 5311 561630617 FRAME DOUG DC8 DC871F 302199D WP BS 867 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING A MAINTENANCE VISIT, FOUND FRAME CRACKED, AT STA 867 AND BL 51 L. REMOVED DAMAGED SECTION, FABRICATED AND INSTA LLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-05179. 2 L 7 4 4F RT 4A25 1998082800134 19980828 00134 WP 1998 8 28 RRXA98338 1 19980806 A 5313 577991523 LONGERON DOUG DC8 DC871F 302199D WP BS 1080 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING A MAINTENANCE VISIT, FOUND LONGERON 31 RIGHT WITH CORROSION DAMAGE, AT STA 1080. REMOVED DAMAGED SECTION, TREATE D AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-0 5194. 2 L 7 4 4F RT 4A25 1998082800135 19980828 00135 WP 1998 8 28 RRXA98339 1 19980806 A 5330 564932959 SKIN DOUG DC8 DC871F 302199D WP BS 1890 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING A MAINTENANCE VISIT, FOUND BELLY SKIN WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1890 BETWEEN LONGE RONS 36 TO 32 RIGHT. REMOVED CORROSION DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBL ER IAW FAA APPROVED DER TIMCO ENGINEERING SKETCH REO-05195. 2 L 7 4 4F RT 4A25 1998082800136 19980828 00136 WP 1998 8 28 RRXA98340 1 19980821 A 5330 5611380531 SKIN DOUG DC8 DC871F 302199D WP LT WING DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING A MAINTENANCE VISIT, FOUND LEFT WING, PANEL 57-88 MOD, SKIN DOUBLER WITH 2 EACH ELONGATED HOLES. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05260. 2 L 7 4 4F RT 4A25 1998082800137 19980828 00137 WP 1998 8 28 RRXA98341 1 19980817 A 5751 5705334354 SKIN DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, INBOARD AILERON UPPER O/B SKIN, CRACKED. REMOVED DAMAGED SECTION, FABRIC ATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05281. 2 L 7 4 4F RT 4A25 1998082800138 19980828 00138 NM 1998 8 28 VNAA9808017 1 19980818 A 4980 001A498A0300000 EXHAUST DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AFT FUSELAGE DENTED A VNAA D RETURN TO BLOCK C F.O.D. TX TAXI/GRND HDL 1 GL 07 425JS 84239 3037 DURING THE TAXI FOR TAKEOFF, THE AIRCRAFT WAS STRUCK BY A FREE ROLLING WORK STAND ON WHEELS. THE TOWER REPORTED THAT IT LOOKED AS IF AN ENGINE STAND ROLLED INTO THE AIRCRAFT AS IT TAXIED BY. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE APU EXHAUST ASSEMBLY, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 49-00-00. OPERATIONAL C HECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082800139 19980828 00139 NM 1998 8 28 CA980421018 1 19980410 A 3260 SENSOR 841101 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT MLG INOPERATIVE W K NONE J WARNING INDICATION AP APPROACH 1 CA 21468 120458 (CAN) RIGHT HAND DOWNLOCK LANDING GEAR SENSOR WIRE CHAFED AT ZONE G611 BETWEEN PLUG 7700 P2 AND CONNECTOR 2/J17 AGAINST THE METAL CONDUIT. ON APROACH, THE GEAR WAS SELECTED DOWN. THE RED UNSAFE LIGHT AND RIGHT MAIN LANDING GEAR DOOR CYCLE D. WIRE NR 3261-28A22-2. PART TC: 22,422. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800140 19980828 00140 NM 1998 8 28 CA980421019 1 19980413 A 5730 85740149005 COVER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LEFT SIDE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 120323 (CAN) THREE SCREWS LOOSE ON THE COVER ASSY CAUSING WEAR ON THE PART OF THE PANEL THE COUNTER SUNK SCREW HEADS HOLD AGAIN ST. IF THE PANELS WERE TO WEAR TO THE POINT THAT THE SCREWS COULD PULL THROUGH, THE PANEL COULD MOVE INBOARD AND POSSIB LY JAM AGAINST THE AILERON GAP STRIP CAUSING THE AILERON TO BE HARD TO MOVE. RIGHT HAND SIDE OK. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800147 19980828 00147 NM 1998 8 28 CA980421030 1 19980408 A 7921 28E997 COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE OIL LEAKING W E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 CA 7168 120459 (CAN) OIL COOLER LEAKED IN-FLIGHT. PART TC: 7,921. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800148 19980828 00148 NM 1998 8 28 CA980421031 1 19980406 A 3230 MS21251B3L TURNBUCKLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 26038 120760 (CAN) TURNBUCKLES, CLEVIS ENDS AND PINS WERE FOUND WITH EXTENSIVE CORROSION. PINS WORN THROUGH APPROXIMATELY 25 PERCENT . PART TC: 29,986. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800149 19980828 00149 NM 1998 8 28 CA980422006 1 19980417 A 2710 CLUTCH DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE AILERON DISCONNECTED W A O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 123010 (CAN) ON LANDING IN A LEFT CROSSWIND, THE AILERONS DISCONNECTED AT TOUCHDOWN. PILOT SIDE ONLY, COPILOT'S AILERONS STILL CONNECTED. CAPTAIN'S AILERONS RECONNECTED AT ROLLOUT. NO FAULT FOUND. HOWEVER, MOD. 8/2342--SB 8-27-79 WAS PREVIOUSL Y ACCOMPLISHED, BUT DISCONNECT STILL OCCURRED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800150 19980828 00150 NE 1998 8 28 CA980422007 2 19980417 A 7320 87600520001 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 21101 120370 (CAN) DURING 400-HOUR INSPECTION. FOUND THE RIGHT HAND ENGINE CONDITION LEVER CABLE FRAYED BEYOND LIMITS. CABLE FRAYED AT PULLEY, FORWARD OF ENGINE FIREWALL. PART TC: 17,896. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800155 19980828 00155 NE 1998 8 28 CA980424005 2 19980411 A 7532 10746012 VALVE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE NR 1 ENGINE FAILED W O B OTHER EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA 30690 (CAN) ENGINE HIGH STAGE EICAS MESSAGE CAUSED FLIGHT CREW COMPLETE QRH CHECKLIST AND SELECT NR 1 ENGINE BLEED TO OFF. A PPROXIMATELY ONE HOUR LATER, CREW NOTICED CABIN ALTITUDE AT 10,000 FEET RISING SLOWLY. DESCENT INITIATED AND NORMAL PRE SSURIZATION RECOVERED AT APPROXIMATELY FL 270. POST-FLIGHT INVESTIGATION REVEALED A FAULT WITH THE NR 1 ENGINE HIGH STAG E PILOT VALVE. THE VALVE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998082800160 19980828 00160 NM 1998 8 28 CA980424010 1 19980401 A 5350 SKIN BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE RADOME DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA P707548 (CAN) RADOME DELAMINATED DUE TO LIGHTNING STRIKE. REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998082800161 19980828 00161 EU 1998 8 28 CA980424012 1 19980319 A 2750 SENSOR AIRBUS 320 A320211 3930320 EU TE FLAPS FAILED W A O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) FLAPS LOCKED AND ALIGNMENT FAULT APPEARED ON ELECTRONIC CENTRALIZED A/C MONITORING AT SELECTION OF FLAPS. TWO ECM PROCEDURES CARRIED OUT AND NORMAL LANDING COMPLETED. FLAP WING TIP BRAKE RESET. ON WALK AROUND, FOUND RIME ICE NEAR S ENSORS ON FLAPS, SUSPECT THIS CAUSE OF FAULT. SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998082800162 19980828 00162 NM 1998 8 28 CA980424013 1 19980318 A 5230 HANDLE AIRBUS A319 A319114 NM CARGO DOOR LOOSE W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF, AT 11,000 FEET, A NOISE WAS HEARD FOLLOWED BY AFT CARGO DOOR OPEN WARNING. AIRCRAFT RETURNED TO DE PARTURE TERMINAL. MAINTENANCE CHECK REVEALED DOOR HANDLE POPPED SLIGHTLY. DOORS INDICATION CHECKED OK, BITE CHECK CARR IED OUT ON BOTH LANDING CONTROL INTERFACE UNIT AND GROUND PROXIMITY WARNING SYSTEM, TESTED OK. 2 L 7 2 4F RT A28NM 1998082800163 19980828 00163 NM 1998 8 28 CA980424014 1 19980321 A 2530 SWITCH BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE GALLEY MALFUNCTIONED W K NONE O OTHER CR CRUISE 1 CA P709651 (CAN) FLIGHT ATTENDANT RECEIVED SHOCK FROM A CONTROL SWITCH ON THE FORWARD GALLEY HEATER PAD. REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998082800164 19980828 00164 WP 1998 8 28 CA980424015 1 19980327 A 2530 OVEN DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA P656802D (CAN) ELECTRICAL FUMES DETECTED ON CLIMB-OUT. ELECT FIRE DRILL CARRIED OUT. GALLEY POWER SWITCHED OFF. SMELL DISSIPAT ED WITHIN ONE MINUTE. GALLEY OVEN 16 FOUND TO BE THE CAUSE. FAULTY RECEPTACLE CHANGED. 2 L 7 2 4F 4 F A6WE E2EA 1998082800165 19980828 00165 NM 1998 8 28 CA980424016 1 19980312 A 2510 APU AIRBUS A319 A319114 NM COCKPIT FUMES W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) BURNING SMELL DETECTED IN COCKPIT DURING RAMP CHECK. APU RAN FOR ONE HOUR. BOTH PACKS ON AND ALL DOORS CLOSED. N O BURNING SMELL DETECTED. SUSPECT CAUSE MAY HAVE BEEN GROUND HEATING UNIT. 2 L 7 2 4F RT A28NM 1998082800170 19980828 00170 NE 1998 8 28 CA980424022 2 19980411 A 7532 32143042 VALVE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE NR 2 ENGINE FAILED W O B OTHER EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA 31383 (CAN) ENGINE HIGH STAGE EICAS MESSAGE CAUSED THE FLIGHT CREW TO COMPLETE QRH CHECKLIST AND SELECT NR 1 ENGINE BLEED TO O FF. APPROXIMATELY ONE HOUR LATER, CREW NOTICED CABIN ALTITUDE AT 10,000 FEET RISING SLOWLY. DESCENT INITIATED AND NORM AL PRESSURIZATION RECOVERED AT APPROXIMATELY FL 270. POST-FLIGHT INVESTIGATION REVEALED A FAULT WITH THE NR 1 ENGINE HI GH STAGE PILOT VALVE. THE VALVE WAS REPLACED. SUBSEQUENT INVESTIGATION REVEALED A FAULT WITH THE NR 2 ENGINE BLEED, WH ICH WAS FOUND TO HAVE LOW PRESSURE FLOW WHEN OPERATING AT LOW STAGE SETTINGS. THE NR 2 ENGINE HP SHUTOFF VALVE WAS ALSO REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998082800173 19980828 00173 SW 1998 8 28 CA980430012 1 19980422 A 5311 2722018003 FRAME SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313 01514 WP BS 272 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 26289 P54214 (CAN) WHILE OPENING AREA TO REPAIR CRACKED WEBS, THE RIGHT HAND FRAME AT NR 11 STRINGER POSITION WAS FOUND CRACKED. FRA ME AND CHANNEL P/N 27-22116-006 WERE CRACKED THROUGH BOTH LAYERS RUNNING FROM THE STRINGER CUT-OUT TO THE EDGE OF THE FR AME. PART TC: 26,289. 2 L 7 2 4T 4 T RT A8SW E4WE 1998082800177 19980828 00177 NM 1998 8 28 CA980430016 1 19980419 A 2910 82950010273 LINE A44700009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120249 (CAN) CREW CALLED IN HYDRAULIC SYSTEM. A HYDRAULIC LEAK FOUND AT INBOARD ROLL SPOILER ACTUATOR AREA, LEFT HAND. HYDRA ULIC LINE FOR THE LIFT DUMP PRESSURE CRACKED AT THE BEND. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800178 19980828 00178 NM 1998 8 28 CA980430017 1 19980419 A 2910 82950010275 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYS CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120249 (CAN) DURING REPLACEMENT OF ADJACENT HYDRAULIC TUBE ON LEFT HAND INBOARD SPOILER ROLL ACTUATOR, A PRESSURE LINE WAS FOUN D CHAFING AGAINST THE ACTUATOR BODY. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800179 19980828 00179 NM 1998 8 28 CA980430018 1 19980420 A 8010 AA4N103 CONTACTOR DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE STUCK W H DEACTIVATE SYST/CIRCUITS B M J SMOKE/FUMES/ODORS/SPARKS OVER TEMP WARNING INDICATION IN INSP/MAINT 1 CA 123010 (CAN) ON STARTING NR 2 ENGINE, STARTER STAYED IN START MODE AND OVERHEATED. EMERGENCY EVACUATION CARRIED OUT. SUSPECT CONTACTOR STUCK CLOSED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800186 19980828 00186 NM 1998 8 28 CA980430028 1 19980224 A 5521 6522901 RIB BOEING 727 727260 NM PWA JT8 JT8D17 52049 NE ELEVATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P689955 (CAN) TWO 1 INCH GRACKS FOUND ON ELEVATOR INPUT QUADRANT RIB. REPLACED. 2 L 7 3 4F 4 F RT A3WE E2EA 1998082800187 19980828 00187 NM 1998 8 28 CA980430029 1 19980410 A 3231 54C546347 VALVE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG SEPARATED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA TM120797 (CAN) DURING CLIMB, NR 2 HYDRAULIC PRESSURE AND QUANTITY. NLG DOOR SEQUENCING VALVE HAD SEPARATED FROM VALVE CAUSING A MAJOR LEAK OF HYDRAULIC FLUID. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800188 19980828 00188 WP 1998 8 28 CA980430031 1 19980417 A 7160 SPINNER LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE LOOSE W E A ENGINE SHUTDOWN UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 CA 10059 (CAN) NR 2 ENGINE WAS SHUTDOWN ON CLIMB-OUT DUE TO HIGH VIBRATION AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE. P OST-FLIGHT INSPECTION FOUND OIL IN THE ENGINE SPINNER AND TWO BOLTS OF THE SPINNER CAP WERE FOUND LOOSE. THE SPINNER CAP AND ANTI-ICE TUBES WERE CROOKED (BENT) WHICH INCREASED THE VIBRATION. A SURVEY CONDUCTED INDICATED THE VIBRATIION WAS INCREASING OVER A PERIOD OF TIME. THE SPINNER, SPINNER CAP AND ANTI-ICE TUBES WERE REPLACED. THE FAN TRIM BALANCED. HI GH POWER RUNUP CARRIED OUT SERVICEABLE, WITH VIBRATION WITHIN LIMITS AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1998082800190 19980828 00190 NE 1998 8 28 CA980430033 2 19980422 A 7310 KB27134 O-RING LK57864 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 2 ENGINE DAMAGED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 14829 (CAN) DURING SERVICING CHECK, NR 2 ENGINE FUEL TUBES WERE FOUND LEAKING. BOTH O-RING SEALS WERE FOUND LEAKING. THE SEA LS WERE REPLACED, A LEAK CHECK WAS CARRIED OUT SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1998082800194 19980828 00194 NM 1998 8 28 CA980504009 1 19980426 A 7712 310507601 SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MALFUNCTIONED W D RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 657 120293 (CAN) DURING TAKEOFF ROLL, THE NR ENGINE TORQUE GAUGE FLUCTUATED UP AND DOWN RAPIDLY. AIRCRAFT RETURNED TO THE GATE. T HE NR 2 TORQUE PROBE WAS REPLACED AND THE GAP ADJUSTED PER THE MAINTENANCE MANUAL. THE ENGINE WAS GROUND RUN SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800201 19980828 00201 NM 1998 8 28 CA980504024 1 19980423 A 5610 141T480 WINDSCREEN BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E437 54555 NE COCKPIT CRACKED W K H NONE DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 CA 30680 (CAN) FOLLOWING INITIAL LEVEL OFF AT 37,000 FEET, FIRST OFFICER'S WINDSHIELD CRACKED. WINDSHIELD HEAT DEACTIVATED. WIN DSHIELD AND CONTROLLER REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998082800204 19980828 00204 EA 1998 8 28 CA980506002 1 19980427 A 7603 87600520003 CABLE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 15569 123028 (CAN) CONDITION CABLE FRAYED AT PULLEY 4 TO 6 INCHES FORWARD OF FIREWALL PULLEY. PART TC: 11,752. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800206 19980828 00206 NM 1998 8 28 CA980506011 1 19980427 A 2910 AE70421640 HOSE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE HYDRAULIC SYS RUPTURED W O OTHER K FLUID LOSS CR CRUISE 1 CA 666281 (CAN) A SYSTEM HYDRAULIC FLUID LOSS EN ROUTE, RETURNED TO NORMAL WHEN LANDING GEAR LOWERED. FOUND NR 2 ENGINE DRIVEN PU MP PRESSURE HOSE CHAFED AND RUPTURED. HOSE REPLACED AND AIRCRFT RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998082800214 19980828 00214 NE 1998 8 28 CA980512004 2 19980427 A 7314 TF38003CL FUEL PUMP TRW CNDAIR CL215 CL2151A10 EA PWA R2800 CA3 52026 NE HAMSTD 43E 43E60 NE NR 2 ENGINE FAULTY W A E UNSCHED LANDING ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 CA TF4698911W P31460 N182596 (CAN) ON CLIMB OUT AFTER TAKEOFF, FUEL PRESSURE ON NR 2 ENGINE STARTED TO INCREASE BEYOND LIMITS. THE ENGINE WAS SHUTDO WN AND THE AIRCRAFT RETURNED TO BASE. NR 2 ENGINE FUEL PUMP WAS REPLACED AND THE ENGINE WAS GROUND RUN SERVICEABLE. 2 H 7 2 4R 4 R A14EA E231 6 C P871 1998082800215 19980828 00215 GL 1998 8 28 CA980512005 1 19980504 A 2434 BRUSH LUCAS B1816 DHAV DHC1 DHC1B2S5 2801739 GL NR 1 GENERATOR FAILED W A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA 672 (CAN) DURING FLIGHT, ALL RADIOS FUNCTIONING OK AND THEN MODE 'C' NOT PUTTING OUT SHORTLY AFTER VOLTMETER DROPPED AND LOR AN WENT DEAD. COULD NOT TRANSMIT. RADAR ALERT PATTERNS WERE FLOWN. AIRCRAFT THEN LANDED OK. FOUND THE PIGTAIL LEAD O N ONE GENERATOR BRUSH BENT OVER THE FRAME THAT THE BRUSH SLIDES IN. THE BRUSH WAS NOT MAKING GOOD CONTACT, ALLOWING ARC ING TO OCCUR. IT WAS BURNT, NOT ALLOWING A PROPER GENERATOR OUTPUT. GENERATOR ITSELF WAS OK. 1 L 7 1 3O EXPA1L71 1998082800220 19980828 00220 EA 1998 8 28 CA980512015 1 19980423 A 2450 K1XD RELAY CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE E/E BAY FAILED W K NONE N FALSE WARNING IN INSP/MAINT 1 CA 7991 807157 (CAN) AC ESSENTIAL BUS CAUTION MESSAGE ON INTERMITTENTLY. CREW REPORTED FAULT OCCURRED ON 3 OF THE LAST 5 LEGS. EMERGE NCY LIGHTS ON WHEN FAULT OCCURRED. RELAY K1XD AND NR 1 DATA CONCENTRATOR REPLACED. PART TC: 6,937. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082800221 19980828 00221 EA 1998 8 28 CA980512016 1 19980423 A 2750 FCU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE TE FLAPS FAILED W K NONE F FLT CONT AFFECTED TO TAKEOFF 1 CA 7818 807317 (CAN) FLAP SYSTEM FAILED AFTER TAKEOFF. LANDED OK WITH ZERO DEGREE FLAPS. FLAP ELECTRONIC CONTROL UNIT RESET. PART TC : 6,973. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082800222 19980828 00222 WP 1998 8 28 CA980512017 1 19980421 A 2530 RECEPTACLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE GALLEY MALFUNCTIONED W O OTHER O OTHER CR CRUISE 1 CA P657446D (CAN) ELECTRICAL SHOCK FELT WHEN REMOVING OVEN GALLEY TROLLEY FROM RECEPTACLE, POSITION NR 17. TROLLEY REMOVED FOR FURT HER TESTING AT ACCESSORY SHOP. VISUAL INSPECTION OF RECEPTACLE CARRIED OUT, NO ARCING SIGNS PRESENT. RE-INSPECTED IN A PRIL AND FOUND 3 PHASES AND GROUND PRESENT AT CONNECTOR. NO ARCING VISIBLE. OVENS CONSIDERED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998082800223 19980828 00223 EA 1998 8 28 CA980512018 1 19980421 A 3250 CONTROL BOX CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG STEERING INOPERATIVE W O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 5704 808307 (CAN) CREW REPORTED STEERING INOPERATIVE, SYSTEM RESET, UNSUCCESSFUL. AIRCRAFT LANDED WITHOUT NOSEWHEEL STEERING AND HA D TO BE TOWED TO GATE. ELECTORNIC CONTROL UNIT AND SERVO VALVE REPLACED. PART TC: 5,075. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082800224 19980828 00224 EA 1998 8 28 CA980512019 1 19980415 A 2750 POTENTIOMETER CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE TE FLAPS OUT OF ADJUST W O OTHER J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 CA 7938 807157 (CAN) CREW SELECTED 20 FLAPS THEN THE FLAPS FAILED, LIGHT CAME ON. AIRCRAFT LANDED WITH 20 DEGREE FLAP. MAINTENANCE A DJUSTED FLAP ELECTRONIC CONTROL UNIT POTENTIOMENTERS NUMBERS 5 TO 8. PART TC: 6,891. 2 L 7 2 4F 4 F RT A21EA E15NE 1998082800225 19980828 00225 EU 1998 8 28 CA980512020 1 19980414 A 2130 RELIEF VALVE AIRBUS A340 A340313 EU NR 1 ENGINE LEAKING W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) NACELLE TEMPERATURE ADVISORY AND FLASHING NR 1 NACELLE ON TAKE-OFF THRU 1500 FEET. TEMPERATURE ABOVE 240 DEGREES. MAINTENANCE REVEALED OVERPRESSURE RELIEF VALVE LEAKING AT SHAFT. VALVE REPLACED, BANJO FITTING REPAIRED, AND LEAK CHE CK CARRIED OUT SERVICEABLE. 2 L 7 4 4F RT A197 1998082800226 19980828 00226 EU 1998 8 28 CA980512021 1 19980415 A 3610 DUCT SEAL AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 2 ENGINE MISSING W O OTHER J WARNING INDICATION CL CLIMB 1 CA 731598 (CAN) ON DEPARTURE, NR 2 ENG FIRE LIGHT ILLUMINATED. WHEN NR 2 ENGINE THRUST LEVER AT IDLE, ENGINE LIGHT WENT OUT. ENG INE WAS NOT SHUT DOWN. MAINTENANCE FOUND SEAL MISSING FROM HIGH PRESSURE DUCT FLANGE AT 7 O'CLOCK POSITION AND FLANGE A T 4 O' CLOCK POSITION LOOSE. NEW SEAL INSTALLED AND DUCT FLANGES TIGHTENED AND SYSTEM CHECKED SERVICEABLE ON GROUND RUN -UP. 2 L 7 2 4F 4 F RT A28NM E29NE 1998082800228 19980828 00228 NM 1998 8 28 CA980512025 1 19980501 A 3246 1702092 INSERT BFGOODRICH 214664 DHAV DHC8 DHC8102 2809003 NM MLG WHEEL LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 23591 0398 (CAN) INSERT MIGRATED FROM ITS POSITION ON THE WHEEL AND MADE HEAVY CONTACT WITH THE BRAKE ASSY WHICH HAD TO BE SCRAPPED . PART TC: 27,150. 2 H 7 2 4T RT A13NM 1998082800229 19980828 00229 NM 1998 8 28 CA980512026 1 19980501 A 3246 83240011S101 SEAT BFGOODRICH DHAV DHC8 DHC8102 2809003 NM WHEEL CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 0119 (CAN) CORROSION FOUND ON THE BEAD SEAT AREA OF THE WHEEL. WHEEL SCRAPPED. 2 H 7 2 4T RT A13NM 1998082800230 19980828 00230 NM 1998 8 28 CA980512027 1 19980501 A 3246 8324001S101 SEAT BFGOODRICH DHAV DHC8 DHC8102 2809003 NM WHEEL CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 0282 (CAN) CORROSION FOUND ON THE BEAD SEAT AREA OF THE WHEEL. WHEEL SCRAPPED. 2 H 7 2 4T RT A13NM 1998082800231 19980828 00231 NM 1998 8 28 CA980512028 1 19980504 A 3244 H31X975X13 TIRE DUNLOP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG BURST W K NONE O OTHER TX TAXI/GRND HDL 1 CA 96281005 120398 (CAN) WHILE TAXIING TO POSITION FOR TAKEOFF, THE NR 1 TIRE BURST. BOTH NR 1 AND NR 2 MAIN WHEELS REPLACED. PART TC: 478. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800232 19980828 00232 NM 1998 8 28 CA980512029 1 19980506 A 3244 TIRE DUNLOP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG BURST W K NONE O OTHER TX TAXI/GRND HDL 1 CA 120383 (CAN) NR 3 TIRE SIDEWALL BURST DURING TAXI. BOTH NR 3 AND NR 4 MAIN WHEELS REPLACED. PART TC: 464. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800233 19980828 00233 NM 1998 8 28 CA980512030 1 19980505 A 3244 96261170 TIRE GOODYEARAERO DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG BURST W K NONE O OTHER TX TAXI/GRND HDL 1 CA 96261170 120190 (CAN) NR 1 MAIN WHEEL TIRE SIDE WALL BURST DURING TAXI. BOTH NR 1 AND NR 2 MAIN WHEEL TIRES REPLACED. PART TC: 460. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800237 19980828 00237 1998 8 28 CA980513005 4 19980415 A 2211 6225796339 COMPUTER COLLINS DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA AFCS MALFUNCTIONED W B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 5339 2499 PCE42181 (CAN) ON DESCENT WITH AUTOPILOT COUPLED, A STRONG SMELL OF SOMETHING ELECTRICAL NOTED. EMERGENCY DECLARED AND AIRCRAFT LANDED OK. INSPECTION FOUND THAT THE AUTOPILOT COMPUTER WAS GETTING WARM AND THE SMELL WAS DUPLICATED. 1 H 7 2 3T 4 T A9EA E4EA 1998082800240 19980828 00240 NM 1998 8 28 CA980513013 1 19980413 A 3260 88343 WOW TARGET DHAV DHC8 DHC8101 2809002 NM PWA 120 PW120A NE NLG LOOSE W K NONE N FALSE WARNING LD LANDING 1 CA 120830 (CAN) ON LANDING, WEIGHT- ON-WHEEL CAUTION LIGHT CAME ON. ONE TARGET ON NOSE LANDING GEAR TRAILING ARM WAS MISSING AND THE OTHER WAS READY TO DEPART. THESE TARGETS ARE GLUED ON THE CASTING OF THE TRAILING ARM. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800241 19980828 00241 1998 8 28 CA980513014 4 19980422 A 3416 10220011821 ENCODER AEROSONIC DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA COCKPIT MALFUNCTIONED W K NONE O OTHER NR NOT REPORTED 1 CA 63 WA2099 PCE40367 (CAN) MODE 'C' INFORMATION BEING GIVEN TO ATC GIVES INCORRECT ALTITUDES. PILOT TOOK SOME READINGS. ALTIMETER INDICATO R AT 4,500, WHILE MODE C' AT 4,400, AND SO ON UP TOTAL. INDICATION AT 10,500 WHILE MODE 'C' AT 9,300. DURING DESCENT, MODE 'C' WAS SHOWING A CLIMB. COPILOT'S ALTIMETER WITHIN 50 FEET OF THE ENCODING ALTIMETER READING. 1 H 7 2 3T 4 T A9EA E4EA 1998082800242 19980828 00242 1998 8 28 CA980513015 4 19980429 A 3416 10220011821 ENCODER AEROSONIC DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA COCKPIT MALFUNCTIONED W K NONE O OTHER NR NOT REPORTED 1 CA 9 WA2022 PCE40367 (CAN) INDICATION OF ENCODING ALTIMETER HAD AN ERROR OF 151 FEET AS COMPARED TO ONLY 10 FEET ON THE COPILOTS. AT ALTITUD ES THIS ALTIMETER WAS NEVER WITHIN 200 FEET OF THE COPILOTS ALTIMETER. 1 H 7 2 3T 4 T A9EA E4EA 1998082800249 19980828 00249 NM 1998 8 28 CA980519012 1 19980501 A 7921 DSC2841 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE OIL COOLER LEAKING W E ENGINE SHUTDOWN K R FLUID LOSS PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 120896 (CAN) POWER WAS REDUCED IN-FLIGHT AND THEN NR 2 ENGINE WAS SHUTDOWN DUE TO REDUCING OIL PRESSURE. POST-FLIGHT MAINTENAN CE IDENTIFIED PROBLEM AS AN OIL LINE LEAK AT THE OIL COOLER. NR 2 ENGINE WAS REPLACED DUE TO PREVIOUS PROBLEMS WITH FOU R OIL COOLERS AND THREE FUEL HEATERS. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800250 19980828 00250 NM 1998 8 28 CA980519013 1 19980510 A 5320 85320980101 COUPLING DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE LAVATORY CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 18985 123021 (CAN) FIVE AREAS ON TOP SURFACE OF LAV COUPLING MACHINED FITTING FOUND CORRODED. DEPTHS RANGING FROM 0.005 INCH TO 0.11 0 INCH. PART TC: 20,969. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800259 19980828 00259 EA 1998 8 28 CA980521009 2 19980513 A 7322 229164 DISCHARGE TUBE PRECISION 105217 CESSNA 172 172N 2072434 CE LYC O320 O320D2G 41508 EA MCAULY 1C160 1C160DTM GL CARBURETOR MISSING W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 1383 75005314 L1725139A 728858 (CAN) WHILE PRACTICING FORCED APPROACHES, FULL POWER WAS APPLIED FOR A GO-AROUND. THE ENGINE DID NOT RESPOND AND STARTE D TO COUGH, POWER WAS REDUCED AND THE AIRCRAFT LANDED. POST-FLIGHT INSPECTION FOUND A SMALL PIECE OF BRASS TUBING IN TH E NR 1 SPARK PLUG. FURTHER INVESTIGATION FOUND THE CARBURETOR ACCELERATOR PUMP DISCHARGE TUBE WAS MISSING. THE CARBURE TOR WAS REPLACED. 1 H 7 1 3O 3 O NT 3A12 E274 5 N P910 1998082800264 19980828 00264 EA 1998 8 28 CA980525007 1 19980416 A 5753 C6WF1100 RIB C6WF10023 DHAV DHC6 DHC6300 EA PWA PT6 PT6A27 52043 EA TE FLAP LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 22960 589 PCE41110 (CAN) EXCESSIVE LOOSENESS BETWEEN THE TWO HALVES OF THE FLAP AT THE CENTER HINGE ARM POSITION. THE RIBS ON EITHER SIDE OF THE HINGE ARM ARE ASSEMBLED TO THE ARM BY THE USE OF LONG MS20470AD5 SOLID RIVETS. IT WOULD APPEAR THAT THERE HAS BE EN SOME WORKING BETWEEN THE RIVETS AND THE RIBS WHICH HAS CAUSED A SLIGHT WEARING OF THE RIVET HOLES IN THE RIBS. PART TC: 25,447. 1 H 7 2 3T 4 T A9EA E4EA 1998082800272 19980828 00272 NM 1998 8 28 CA980529013 1 19980515 A 7603 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 5341 120370 (CAN) LEFT HAND CONDITION LEVER CABLE ASSEMBLY FRAYED WHERE CABLE RUNS OVER PULLEY - FORWARD OF ENGINE FIREWALL. PART T C: 4,914. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800277 19980828 00277 EU 1998 8 28 CA980602002 1 19980410 A 3230 201138606 BAULK LEVER ROTOL 201138002 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NLG BROKEN W O OTHER O OTHER AP APPROACH 1 CA DRG771286 LF05491A (CAN) ON APPROACH, A LOUD BANG WAS HEARD WHEN GEAR SELECTED DOWN. NO NOSE GEAR INDICATION. FLY-BY SHOWED NOSE GEAR NOT DOWN AND NOSE GEAR DOORS CLOSED. ALTERNATE EXTENSION CARRIED OUT. BAULK LEVER FOUND BROKEN OFF. PART TC: 14,320. 2 H 7 4 4F 4 F RT A49EU E6NE 1998082800278 19980828 00278 NM 1998 8 28 CA980602003 1 19980423 A 6123 944215B653323 SWITCH AEROOPTICS 944215B65 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE PROP CONTROL STUCK W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 24000 120156 870601 (CAN) AFTER TAKEOFF, UNABLE TO DE-SELECT AUTO FEATHER SWITCH ASSY. REPLACED. PART TC: 33,600. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1998082800279 19980828 00279 NM 1998 8 28 CA980602005 1 19980421 A 5230 85230009115 SEAL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CARGO DOOR LOOSE W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 120229 (CAN) UNABLE TO MAINTAIN MAX. PRESSURIZATION IN MANUAL OR AUTO MODE. TOP OF BAGGAGE DOOR SEAL WAS FOUND POPPED OUT OF SE AL RETAINER. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800280 19980828 00280 NM 1998 8 28 CA980602006 1 19980415 A 2997 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PTU CHAFED W K NONE L NO TEST IN INSP/MAINT 1 CA 24229 120322 (CAN) POWER TRANSFER UNIT WOULD NOT FUNCTION, CIRCUIT BREAKER FOUND CHAFED IN THE LEFT HAND ARMPIT JUNCTION. PART TC: 3 3,666. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800281 19980828 00281 NM 1998 8 28 CA980602009 1 19980512 A 6123 V319 SWITCH HONEYWELL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AUTO FEATHER FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 120833 891003 (CAN) WHEN TAKEOFF POWER APPLIED, THE AUTOFEATHER SYSTEM DID NOT ARM. POWER LEVER SWITCH REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1998082800283 19980828 00283 NM 1998 8 28 CA980602012 1 19980527 A 2421 31708001A GENERATOR LEARSIEGLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 AC GEN FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 1303 829 120229 (CAN) AFTER TAKEOFF, NR 2 AC GENERATOR FAILED, AIRCRAFT RETURNED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998082800285 19980828 00285 NE 1998 8 28 CA980602015 2 19980414 A 7314 384300 PUMP HAMSTD 7436024 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE FUEL SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CA 21957 434A P709475B (CAN) AIRCRAFT RETURNED TO GATE DUE TO FLUCTUATING ENGINE PARAMETERS. THE FUEL PUMP AND FUEL CONTROL UNIT WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1998082800286 19980828 00286 WP 1998 8 28 CA980602016 1 19980414 A 2760 ABH73401 ROD ABH7185505 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE SPOILER BENT W K NONE F FLT CONT AFFECTED IN INSP/MAINT 1 CA 517958 (CAN) BINDING OF SPOILER CONTROL REPORTED. IT WAS FOUND THAT THE INPUT ROD FOR THROTTLE INTERLOCK WAS BENT AND INTERFERI NG ON THE CROSS SHAFT. 2 L 7 3 4F 4 F A22WE E23EA 1998082800287 19980828 00287 NM 1998 8 28 CA980602017 1 19980415 A 7931 1163P181 SWITCH BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 7729XX P708808B (CAN) AIRCRAFT DIVERTED AFTER ENGINE SHUTDOWN DUE TO OIL BYPASS LIGHT ILLUMINATION. REPLACED OIL PRESSURE SWITCH AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1998082800288 19980828 00288 EU 1998 8 28 CA980602018 1 19980415 A 5320 D5337160300 BEAM AIRBUS 320 A320211 3930320 EU PAX DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING SLIDE ASSEMBLY REMOVAL, FOUND O/W SLIDE SUPPORT BEAM RH SIDE CRACKED FROM FORWARD END TO FORWARD END SLIDE MOUNT FASTENER HOLE. 2 L 7 2 4F RT A28NM 1998082800289 19980828 00289 NM 1998 8 28 CA980602019 1 19980421 A 5210 6044551 SHAFT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE PAX DOOR HANDLE SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 34429 687733 (CAN) RIGHT AFT DOOR EXTERIOR HANDLE CAME OFF WHEN ATTEMPTING TO OPEN BY COMMISSARY STAFF. SPLINE SHAFT SHEARED AT NEC K TO SPLINE. REPLACED. PART TC: 57,780. 2 L 7 2 4F 4 F A16WE E2EA 1998082800290 19980828 00290 WP 1998 8 28 CA980602020 1 19980428 A 3610 8986263 VALVE ALIDSIGNAL 8986263 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE PNEU SYSTEM FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 50951 15791 P1527 517926 (CAN) TAKEOFF ROLL ABORTED DUE TO NR 3 ENGINE THROTTLE ADVANCED WITH NO INCREASE IN POWER. THE PR VALVE WAS REPLACED BE CAUSE THE SENSE LINE OF THE VALVE WAS WORN THROUGH. ENGINE RUN CARRIED OUT SERVICEABLE. 2 L 7 3 4F 4 F A22WE E23EA 1998082800291 19980828 00291 1998 8 28 CA980602021 4 19980501 A 2565 SLIDE BFGOODRICH 7A1323107 BOEING 747 747475 NM PAX DOOR DEPLOYED W K NONE W INADEQUATE Q C TX TAXI/GRND HDL 1 CA (CAN) UPPER DECK R/H SLIDE ASSY ACCIDENTLY DEPLOYED DUE FLIGHT CREW L/H AND R/H UPPER DECK DOORS ARMED UPON ARRIVAL. SL IDE DEPLOYED CAUSING DAMAGE TO PACK BOARD. DAMAGE CAUSED BY LANYARD PIN INSTALLED INCORRECTLY ALLOWING BOTTLES TO INIT IATE INFLATION PRIOR TO SLIDE RELEASE FROM PACK. PACK PUSHED THROUGH PACK BOARD RIPPING FITTINGS FROM BOARD. DAMAGE TO FITTINGS ALSO CAUSED BY SLIDE LOAD DURING DEPLOYMENT, 2 BRACKETS DAMAGED. SLIDE REPLACED. 2 L 7 4 4F RT A20WE 1998082800292 19980828 00292 EU 1998 8 28 CA980602022 1 19980501 A 5510 D551800000 STABILIZER CASA D551800000 AIRBUS 320 A320211 3930320 EU HORIZ STAB DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA CG1851 (CAN) DURING POST HMV ENGINE RUNS, A LARGE PIECE OF ASPHALT DISLODGED STRIKING THE TRIMMABLE HORIZONTAL STABILIZER LT SI DE CAUSING UNREPAIRABLE DAMAGE. T.H.S. REPLACED AND REPAIR TO FUSELAGE SKIN CARRIED OUT. INSPECTIONS TO SURROUNDING ST RUCTURES AND VERTICAL FIN CARRIED OUT AND A/C TEST FLOWN ON REQUEST BY AIRBUS. 2 L 7 2 4F RT A28NM 1998082800293 19980828 00293 NM 1998 8 28 CA980602025 1 19980525 A 2613 SENSOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE LT WING FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 702657 (CAN) AIRCRAFT TURNED BACK DUE TO L/H WING OVERHEAT LIGHT ON AND MASTER CAUTION LIGHT FLICKERING ON. FOUND SENSOR TOUCHI NG BLEED DUCT AND A LOOSE GROUND WIRE TO SENSOR. REPOSITIONED SENSOR AND CHECKED CONNECTIONS. ENGINE RUN OK. 2 L 7 2 4F 4 F A16WE E2EA 1998082800296 19980828 00296 NM 1998 8 28 CA980602032 1 19980526 A 2780 69355413 PCU 654456113 BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE LE FLAP CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 21994 0454 P678085 (CAN) ON CLIMB, B-SYSTEM FAILED WITH LOSS OF FLUID AND PRESSURE. FLIGHT WAS TURNED BACK. DURING APPROACH WITH FLAPS 15 AND GEAR SELECTED DOWN, THE AIRCRAFT CONTINUED TO ROLL. CREW USED A COMBINATION OF AILERON, RUDDER AND DIFFERENTIAL TH RUST TO CONTINUE TO LAND WITHOUT FURTHER INCIDENT. ON THE GROUND, THE NR 7 FLIGHT SPOILER WAS FOUND IN THE FLIGHT POSIT IION. INVESTIGATION REVEALED CRACKED CAP ON SPOILER PCU. REPLACED. PART TC: 14,370. 2 L 7 2 4F 4 F A16WE E2EA 1998082800299 19980828 00299 NM 1998 8 28 TWAA9813501 1 19980821 A 3350 LIGHT BOEING 767 767231 1385131 NM CABIN MALFUNCTIONED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 608TW 22571 FLOOR EGRESS LIGHTS ILLUMINATED ON LT SIDE, ROWS 12 THROUGH 13, AND ROWS 22 THROUGH 30, WHEN SWITCH PLACED IN ARM POSN. EGRESS LIGHT MALFUNCTIONS WERE DEFERRED PER MEL. AT THE NEXT STATION THE LIGHTS WERE FOUND TO OPERATE NORMALLY. CHEC K-C 8-1-98 LAX. 2 L 7 2 4F RT A1NM 1998082800300 19980828 00300 WP 1998 8 28 TWAA9813502 1 19980821 A 5350 STOPS DOUG DC9 DC983 3022083 WP TAIL CONE OUT OF POSITION A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 9402W 53138 TAIL CONE UNSAFE LIGHT CAME ON DURING DEPARTURE OUT OF BWI. MADE UNSCHEDULED LANDING AT DCA. FOUND CABLE BALL STOPS HA D BECOME UNSEATED. REINSTALLED CABLE BALL STOPS AT UNSAFE LIGHT SWITCH. CHECK-C 10-29-97 LAX. 2 L 7 2 4F RT A6WE 1998082800301 19980828 00301 NM 1998 8 28 VJ9800286 1 19980824 A 3350 6104781 BATTERY PACK BOEING 737 7372E1 138448F NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 461AT 20976 FORWARD LT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK; OPS CHECKED GOOD. 2 L 7 2 4F A16WE 1998082800302 19980828 00302 WP 1998 8 28 VJ9800287 1 19980822 A 3350 41B004ADO763 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 921VV 47284 MAIN CABIN DOOR PORTABLE EMERGENCY LIGHTS INOP. REPLACED NICAD BATTERIES; OPS CHECKED GOOD IAW MM 33-50. 2 L 7 2 4F A6WE 1998082800303 19980828 00303 WP 1998 8 28 VJ9800288 1 19980823 A 3340 5557 TAXI LIGHT DOUG DC9 DC932 3022066 WP NLG WW SMOKING A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 931VV 47674 DURING TAKEOFF, AT MSL 1000, FLIGHT CREW OBTAINED A FAINT SMELL OF SMOKE AND ELECTED TO RETURN TO IAD MAINTENANCE BASE. INSPECTION OF AIRCRAFT INDICATED SMOKE MAY HAVE EMANATED FROM TAXI LIGHT GROUND WIRE. REPLACED RT NOSE TAXI LIGHT AND OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998082800304 19980828 00304 WP 1998 8 28 VJ9800289 1 19980820 A 5320 1A353411 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 FLOORBOARD HAS SURFACE CORROSION BEYOND LIMIT AND CHAFED ON BOTTOM SIDE AROUND SCREW HOLES AT STA 180, BL 44 RT, AND COR RODED BEYOND LIMIT AT STA 160, RBL 1-21. REMOVED CORROSION AND BLENDED CHAFED AREA IAW DC9 SRM 51-10-3, 53-01, FIG 1. F AB'D REPAIR DOUBLER FROM 7075T6 .032. DRILLED, COUNTERSUNK, DEBURRED, TREATED AND PRIMED. INSTALLED IAW DC9 SRM 53-05, FIG 1, 51-10-4, 51-10-3 AND 51-30-2. FAB'D NEW SUPPORT IAW DC9 SRM 51-10-1, FIG 22, 53-11-1, ITEM 10, AND 51-10-1. CU T AND TRIMMED TO FIT. FITTED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED SUPPORT ANGLE IAW DC9 SRM 51-10-2, 51-10 -4, 51-10-3 AND 51-30-2. INSTALLED FLOORBOARD STA 160 CENTER IAW DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998082800305 19980828 00305 WP 1998 8 28 VJ9800290 1 19980821 A 5320 1A353291 SUPPORT DOUG DC9 DC932 3022066 WP BS 170 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 GALLEY FLOOR SUPPORT Z STRUCTURE HAS CORROSION BEYOND LIMIT RT CABIN STA 170. REMOVED Z ANGLE TO ACCESS CORROSION IAW D C9 SRM 51-30-2 AND 51-30-8. REMOVED CORROSION IAW DC9 SRM 51-10-3 AND EXCESSIVE MATERIAL LOSS IAW DC9 SRM 53-01, FIG 1. CUT AND TRIMMED Z ANGLE FROM 2024T3, .050. DRILLED AND DEBURRED IAW DC9 SRM 51-10-2, 51-10-4, AND EO 981200. TREATED AND PRIMED IAW DC9 SRM 51-10-2, 51-10-3. INSTALLED REPAIR IAW DC9 SRM 51-30-8. 2 L 7 2 4F A6WE 1998082800306 19980828 00306 WP 1998 8 28 VJ9800291 1 19980821 A 5320 1A353501 HAT CHANNEL DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 CABIN FLOORBOARD CORRODED BEYOND LIMIT AROUND SCREW HOLES, HAT CHANNELS AND CHAFED IN CONTACT AREA AT STA 160 - 200, LBL 0 - 44. REMOVED CORROSION IAW DC9 SRM 51-10-3, 53-01. FABRICATED FLOORBOARD FROM 7075T6, .025 IAW DC9 SRM 53-21-0. F ABRICATED 4 EACH HAT CHANNEL FROM 2912282 IAW SRM 53-21-0, PG 6M AND 6N. TREATED AND PRIMED BOTH REPAIRS IAW DC9 SRM 51 -10-3, INSTALLED HAT CHANNELS IAW DC9 51-30-2 AT FLOORBOARD. 2 L 7 2 4F A6WE 1998082800307 19980828 00307 WP 1998 8 28 VJ9800292 1 19980821 A 5320 1A353341 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 600-610 & 710 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 HORIZONTAL INTERCOASTAL CORRODED BEYOND LIMIT AT FS 600-610, L16, AN FS 710, L16. REMOVED CORROSION IAW DC9 SRM 51-30-3 . LOSS LIMITS IAW DC9 SRM 53-01, FIG 1. CUT, TRIMMED AND FABRICATED INTERCOASTAL FROM 7075-0, 040, IAW DC9 SRM 53-11-3 , FIG 1. HEAT TREATED IAW DC9 SRM 51-10-2A. LOCATED, DRILLED AND DEBURRED INTERCOASTAL IAW DC9 SRM 51-10-4. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082800308 19980828 00308 WP 1998 8 28 VJ9800293 1 19980822 A 5320 591342123 FLANGE DOUG DC9 DC932 3022066 WP BS 105 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 NLG AFT DOOR FUSELAGE FLANGE CORRODED BEYOND LIMIT AT BS 105, BL 10R. REMOVED FLANGE AND ORDER NEW PART IAW DC9 SRM 53- 05. DRILLED HOLES IAW DC9 SRM 51-10-4. PRIMED IAW DC9 SRM 51-10-3 AND INSTALLED FRAME IAW DC9 SRM 51-30-1, 51-30-2, 51 -30-5, 51-30-8 AND 51-20-0. 2 L 7 2 4F A6WE 1998082800309 19980828 00309 NM 1998 8 28 K3HA980098 1 19980819 A 3350 CONNECTOR BOEING 727 727225 1384077 NM CABIN LOOSE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 FORWARD EMERGENCY LIGHTING ON OVERHEAD LIFE RAFT COMPARTMENT WON'T LIGHT BATTERY LOCATED IN AFT RAFT COMPARTMENT. FOUND POWER SUPPLY CANNON PLUG CONNECTOR LOOSE RESECURED, TESTED 33-50-01. OPS CHECK OK. 2 L 7 3 4F A3WE 1998082800310 19980828 00310 WP 1998 8 28 9809929101 1 19980818 A 2822 6550934 BOOST PUMP DOUG DC9 DC915 3022036 WP RIGHT FAILED A NWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 GL 01 91S 56053 40628 47063 AFTER TAKEOFF, THE RIGHT AC ELECTRICAL SYSTEM FAILED CAUSING MALFUNCTION OF SEVERAL SYSTEMS AND COMPONENTS. FLIGHT WAS RETURNED TO ICT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT AFT FUEL BOOST PUMP INOPERATIVE WHICH CAUSED TRIP OF A PHASE CIRCUIT BREAKER. REPLACED PUMP. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998082800311 19980828 00311 WP 1998 8 28 9809939938 1 19980816 A 2780 T-DUCT DOUG DC9 DC931 3022065 WP RT WING BINDING A A NWAA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 GL 01 1798U 47369 SLAT DISAGREEMENT LIGHT ILLUMINATED WITH LEFT AIRCRAFT ROLL DURING APPROACH INTO GFK. CAPTAIN DECLARED A YELLOW EMERGEN CY AND AIRCRAFT WAS LANDED SAFELY USING FLAPS ONLY. MAINTENANCE REPLACED THE RIGHT WING ANTI-ICE TELESCOPE DUCT. OPERA TIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998082800312 19980828 00312 NM 1998 8 28 EISA98138 1 19980620 A 2761 H1010262 SWITCH BOEING 727 727223 1384074 NM NR 5 L/E FLAP FAILED A EISA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 316NE F4998 19475 DURING FLAP RETRACTION FROM 5 DEGREES - 2 DEGREES ON TAKEOFF FROM DFW, AMBER LEADING EDGE FLAPS LIGHT REMAINED ILLUMINAT ED. RECYCLED FLAPS. FAILED TO EXTINGUISH LIGHT. NR 5 KRUEGER FLAP IN TRANSIT LIGHT ILLUMINATED. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED NR 5 LEADING EDGE POSITION SWITCH WITH SERVICEABLE PART. GROUND OPS CHECK GOOD. (X) 2 L 7 3 4F A3WE 1998082800313 19980828 00313 EU 1998 8 28 98ZZZX2991 1 19980428 A 5320 S5367800821602 ZEE MEMBER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE Z-MEMBER CORRODED IN THE RIGHT AFT BAGGAGE COMPARTMENT AT FLOORBOARD AREA. INSTALLED RIGHT Z-MEMBER IAW ATR SRM 51-25-03. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRC RAFT TT: 18,688.4 HOURS/TAC: 23,278. (X) 2 H 7 2 4T RT A53EU 1998082800315 19980828 00315 EU 1998 8 28 98ZZZX2993 1 19980428 A 5315 S53872700223 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LEFT SIDE STR 21 BETWEEN FRAMES 44 AND 4 5 CORRODED. REMOVED AND REPLACED STR 21 LT IAW ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688 .4 HOURS/TAC: 23,278. (X) 2 H 7 2 4T RT A53EU 1998082800316 19980828 00316 EU 1998 8 28 98ZZZX2994 1 19980428 A 5315 S53872700222 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RT SIDE STR 21 BETWEEN FRAMES 44 AND 45 CORRODED. REMOVED AND REPLACED STR 21 RT IAW ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688. 4 HOURS/TAC: 23,278. (X) 2 H 7 2 4T RT A53EU 1998082800317 19980828 00317 EU 1998 8 28 98ZZZX2995 1 19980428 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RIGHT F/A SEAT TRACK CORRODED AT FRAME 3 9. INSTALLED NEW SEAT TRACK IAW ATR SRM 51-25-04. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS/ TAC: 23,278. 2 H 7 2 4T RT A53EU 1998082800318 19980828 00318 EU 1998 8 28 98ZZZX2996 1 19980428 A 5347 S535678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RT AFT OUTBOARD SEAT TRACK CORRODED FORW ARD FRAME 35. REMOVED AND INSTALLED AFT OUTBOARD SEAT TRACK WITH NEW IAW ATR SRM 53-63-00. CAUSE OF DAMAGE: ENVIRONME NTAL, LAVATORY/GALLEY SPILLS. AIRCRAFT TT: 18,688.4/TAC: 23,278. 2 H 7 2 4T RT A53EU 1998082800319 19980828 00319 EU 1998 8 28 98ZZZX2997 1 19980428 A 5320 S53874001202 CLIP AEROSP ATR42 ATR42300 8680920 EU TAIL FUSELAGE CORRODED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND 7 NUT PLATES CORRODED AND UNDERNEATH THEM, A LSO TEARSTRAP CLIPS. TREATED PER 51-21-31. REMOVED AND INSTALLED NUT PLATES PER SRM 51-25-00, AND INSTALLED 1 EACH NEW CLIPS TAIL CONE ATTACH POINTS (BOTTOM) PER SRM 51-25-01. CAUSE OF DAMAGE: LAVATORY/GALLEY SPILLS. AIRCRAFT TT: 18,6 88.4 HOURS/TAC: 23,278. 2 H 7 2 4T RT A53EU 1998082800320 19980828 00320 NM 1998 8 28 USAASB98167 1 19980702 A 5240 SEAL BOEING 737 737201 1384454 NM SERVICE DOOR OUT OF POSITION A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 236US 22352 PIT - FLT 856 - AFTER TAKEOFF FROM PIT, AIRCRAFT FAILED TO PRESSURIZE. A LOUD AIR NOISE WAS HEARD COMING FROM DOOR R1. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RE-INSTALLED THE R1 DOOR SEAL AND SECURED THE SERVICE DOOR. PRESSURE TESTED GOOD. (X) 2 L 7 2 4F A16WE 1998082800321 19980828 00321 SO 1998 8 28 C2XA98CL044 1 19980606 A 3350 7287103503 CONTOL UNIT EMB 145 EMB145 SO CABIN FAILED A C2XA K NONE L NO TEST CR CRUISE 1 SW 09 13935 0062 145022 CLE - FLT 4004 - CREW REPORTED THE EMERGENCY LIGHTS ILLUMINATED DURING FLIGHT. MAINTENANCE REMOVED AND REPLACED THE EME RGENCY LIGHTS CONTROL MODULE IAW EMB-145 MM 33-21-01. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVI CE. ACFT TT: 1,894.5 HOURS. TOTAL CYCLES: 1,269. (X) 2 L 7 2 4F RT T00011AT 1998082800322 19980828 00322 NM 1998 8 28 98ZZZX2998 1 19980525 A 3260 869701 PROX SENSOR DORNER DO32 DO328100 2996000 NM RT MLG DEFECTIVE A EQGA K NONE N FALSE WARNING CL CLIMB 1 SW 19 338PH 3029 DFW/CUU - FLT 445 - DURING CLIMB AFTER TAKEOFF FROM DFW AFTER GEAR RETRACTION, 'PROXI SYSTEM FAIL' CAS MESSAGE APPEARED AND ON HYDRAULIC PAGE 'PROXI FAIL' AND 'PROXI LOCK'. AT THE SAME TIME, THE RT MAIN GREEN GEAR DOWN INDICATOR WAS ON WIT H GEAR UP. CREW CYCLED GEAR SEVERAL TIMES AND THE PROBLEM REMAINED. CREW CONTACTED FLT AND MAINT CONTROL AND RETURNED TO DFW. ACFT LANDED WITHOUT INCIDENT. MAINT INSPECTED THE ACFT AND DETERMINED THE PROXI SWITCH B ON THE RT SIDE WAS FA ULTY. MAINT REPLACED THE EFFECTED PROXI SENSOR AND PERFORMED OPERATIONAL CHECKS. ALL CHECKS SATISFACTORY. MAINT CHECK FLIGHT PERFORMED WITH NUMEROUS GEAR SWINGS CONDUCTED. ALL TESTS SATISFACTORY. ACFT RELEASED TO REVENUE SERVICE. 2 H 7 2 4T RT A45NM 1998082800323 19980828 00323 NM 1998 8 28 98ZZZX2999 1 19980525 A 3350 231430 BATTERY PACK DORNER DO32 DO328100 2996000 NM CABIN DISCHARGED A EQGA K NONE L NO TEST IN INSP/MAINT 1 SW 19 335LS 1562 10456 3035 DFW/TYS - FLT 373 - DURING PREFLIGHT, CREW NOTICED THE EMERGENCY EXIT LIGHTS OVER SEAT 9A WERE INOPERABLE. CREW NOTIFIE D MAINTENANCE. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE EMERGENCY LIGHT BATTERY POWER PACK WAS DEAD. MAIN TENANCE REPLACED THE POWER PACK AND PERFORMED OPERATIONAL CHECKS. ALL CHECKS SATISFACTORY. AIRCRAFT WAS RELEASED TO RE VENUE SERVICE. 2 H 7 2 4T RT A45NM 1998082800324 19980828 00324 WP 1998 8 28 AALA981351 1 19980704 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 503-598 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 427AA 49339 TUL - CORROSION ON BOTTOM SIDE OF CUSP. REPAIRED IAW 53-00-00-02. TST: 35,040 HOURS. CYCLES: 19,474. (X) 2 L 7 2 4F A6WE 1998082800325 19980828 00325 WP 1998 8 28 AALA981350 1 19980702 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 422 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 427AA 49339 CORROSION ON CUSP OTBD OF NR 1 SEAT TRACK. REPAIRED IAW 53-00-00-02. TST: 35,040 HOURS. CYCLES: 19,474. (X) 2 L 7 2 4F A6WE 1998082800327 19980828 00327 NM 1998 8 28 AALA981303 1 19980703 A 2530 2510000405 OVEN BOEING 767 767323 1385205 NM GALLEY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 39356 24037 LHR - FLT 0136 - EN ROUTE LAX/LHR, SMOKE EMITTING FROM FIRST CLASS GALLEY OVENS. LANDED LHR WITHOUT INCIDENT. CLEANED BOTH FIRST CLASS OVENS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998082800328 19980828 00328 NM 1998 8 28 AALA981283 1 19980629 A 2530 46700017 COFFEE MAKER BOEING 767 767223 1385123 NM GALLEY FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 313AA 22316 LHR - FLT 0046 - EN ROUTE ORD/LHR - BUSINESS CLASS NR 3 COFFEE MAKER EMITTED SMOKE. TURNED OFF COFFEE MAKER. LANDED LHR WITHOUT INCIDENT. REPLACED NR 3 COFFEE MAKER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998082800329 19980828 00329 EU 1998 8 28 AALA981162 1 19980609 A 3260 D11320409 DOOR FOKKER F28 F28MK0100 4990807 EU LT MLG OUT OF ADJUST A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 1440A 11435 ORD - FLT 0702 - AFTER TAKOEFF, LEFT MLG WOULD NOT RETRACT. RECYCLED GEAR SEVERAL TIMES, BUT GEAR WOULD NOT RETRACT. L ANDED ORD WITHOUT INCIDENT. ADJUSTED LEFT MLG DOOR AND DOOR STOP PER MM. CYCLED MLG SEVERAL TIMES. SYSTEM GROUND CHEC KED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998082800330 19980828 00330 SW 1998 8 28 98ZZZX3000 1 19980723 A 8200 CAWI FRCHLD SA227 SA227DC 3377521 SW ENGINE INOPERATIVE A EQGA K NONE O OTHER TO TAKEOFF 1 SW 19 853LS DC853B DFW/PNC - FLT 1263 - WITH A PASSENGER LOAD OF 19, PERFORMANCE REQUIRED THE USE OF CAWI ON TAKEOFF. CREW TESTED THE SYST EM AND IT TESTED CORRECTLY. WHEN THE CREW TURNED IT ON PRIOR TO TAKEOFF ROLL, THE CAWI SYSTEM DID NOT ACTIVATE. CREW A BORTED TAKEOFF, AND TAXIED BACK TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE CAWI SYSTEM WAS INOP ERATIVE. MAINTENANCE DEFERRED THE CAWI SYSTEM IAW MEL 82-1-2, CONTROL NR 2077. 2 L 7 2 4T RT A18SW 1998082800331 19980828 00331 SW 1998 8 28 98ZZZX3001 1 19980802 A 8200 CAWI FRCHLD SA227 SA227DC 3377521 SW ENGINE INOPERATIVE A EQGA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SW 19 854LS DC854B DFW/CUU- FLT 445 - CREW ACTIVATED CAWI AT 40 PERCENT TORQUE AND RECEIVED TWO CAWI PUMP LIGHTS AND A TORQUE RISE TO 80 PE RCENT. CREW ADVANCED POWER. AT APPROXIMATELY 70 KNOTS IAS, TORQUE DROPPED TO 80 PERCENT AND EGT WENT TO 645-650 DEGREE S CELSIUS. CREW ABORTED TAKEOFF. CREW CONTACTED OPERATIONS AND MAINTENANCE CONTROL AND ADVISED THEY WERE RETURNING TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND ATTEMPTED TO FIRE THE CAWI SYSTEM. CAWI SYSTEM DETERMINED TO BE INOPE RATIVE. MAINTENANCE DEFERRED THE CAWI SYSTEM IAW MEL 82-1-2, CONTROL NR 2105. AIRCRAFT RETURNED TO REVENUE SERVICE. 2 L 7 2 4T RT A18SW 1998082800332 19980828 00332 NE 1998 8 28 98ZZZX3002 2 19980728 A 7250 TURBINE BOEING 737 7372H5 138448E NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A E9WA A E UNSCHED LANDING ENGINE SHUTDOWN D Y INFLIGHT SEPARATION ENGINE STOPPAGE TO TAKEOFF 1 SO 05 220US 44626 2432 20453 665973 ON TAKEOFF FROM GSO ON FLT 405 AT 500 FEET AGL, THE NR 1 ENGINE SHUT DOWN DUE TO APPARENT LPT FAILURE. THE TURBINE WAS CONTAINED AND NO FIRE OR OTHER DAMAGE OCCURRED. THE FLIGHT CREW CONTINUED TO 2,000 FEET, DECLARED EMERGENCY TO GSO TOWE R, WAS CLEARED VISUAL, RETURNED TO GSO, AND LANDED SAFELY SINGLE-ENGINE. 2 L 7 2 4F 4 F A16WE E2EA 1998082800333 19980828 00333 WP 1998 8 28 G6OA027 1 19980806 A 2510 1056J10004505 CONTROL UNIT DOUG DC10 DC1030 3023501 WP CAPTAIN'S SEAT FAILED A G6OA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 27 606GC 47929 IST - ON CLIMB-OUT, THE FLIGHT CREW NOTICED SMOKE AROMA IN THE COCKPIT. THE SOURCE OF THE SMOKE WAS DETERMINED TO BE TH E CAPTAIN'S SEAT CONTROL UNIT ASSEMBLY. THE CAPTAIN'S SEAT CONTROL CIRCUIT BREAKERS WERE PULLED AND THE AIRCRAFT RETURN ED TO IST. GROUND MAINTENANCE TROUBLESHOT THE SYSTEM. FOUND FAILED CONTROL UNIT ASSEMBLY. (X) 2 L 7 3 4F A22WE 1998082800334 19980828 00334 CE 1998 8 28 98ZZZX3003 1 19980801 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG WW FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 852CA 0699A UE55 NO DOWNLOCK INDICATION ON LT MLG. SUSPECTED ACTUATOR ZIGGING. REPLACED LT MLG ACTUATOR. 2 L 7 2 4T RT A24CE 1998082800451 19980828 00451 NM 1998 8 28 AWXA9800191 1 19980807 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 312 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 FOUND DURING SCHEDULED INSP, CORROSION OUT OF LIMITS AT NUT PLATE HOLES, STATION 312 RBL 10 TO LBL 10. REPAIRED PER SRM UPPER CHORD SPLICE PER 53-10-51, 51-40-02. 2 L 7 2 4F RT A16WE 1998082800452 19980828 00452 NM 1998 8 28 AWXA9800192 1 19980807 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 FOUND DURING SCHEDULED INSPECTION, CORROSION OUT OF LIMITS AT NUT PLATE HOLES AT FLOORBEAM STATION 328 RBL 30 TO RBL 34. REPAIRED PER SRM 53-10-51, 51-40-02. 2 L 7 2 4F RT A16WE 1998082800453 19980828 00453 NM 1998 8 28 AWXA9800193 1 19980807 A 5320 65458770 CHORD BOEING 737 7373G7 1384595 NM BS 294.5-328 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING SCHEDULED C INSPECTION, FOUND CORROSION OUT OF LIMITS ON R-1 LOWER DOOR CHORD. REPLACED CHORD PER SRM 51-40-02. 2 L 7 2 4F RT A16WE 1998082800454 19980828 00454 NM 1998 8 28 AWXA9800194 1 19980807 A 5320 6517588100 CHORD BOEING 737 7373G7 1384595 NM BS 312-344 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 322AW 25400 DURING SCHEDULED C INSPECTION, FOUND L-1 LOWER CHORD CORRODED BEYOND LIMITS. REPAIRED PER ER 3-53-12-30, EAC MZJ-98-0 8 110-3 DATED 8-11-98. 2 L 7 2 4F RT A16WE 1998082800455 19980828 00455 EU 1998 8 28 AWXA9800195 1 19980820 A 3350 321452 POWER SUPPLY AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 635AW 25341 25349 092 DURING ROUTINE WEEKLY MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS FAILED ON RIGHT SIDE OF AIRCRAFT. FOUND BATTERY FAILED AND CHARGER INOP. REMOVED AND REPLACED BATTERY AND CHARGER, BATTERY ASSEMBLY - 321430. 2 L 7 2 4F RT A28NM 1998082800456 19980828 00456 NM 1998 8 28 AWXA9800196 1 19980820 A 3350 20121 CHARGER BOEING 737 73733A 1384673 NM CABIN INOPERATIVE A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 165AW 23626 EMERGENCY EXIT LIGHTS FROM ROW 19 TO 23 ON PAX SEATS INOP. REPLACED AFT BATTERY CHARGER, CHECK OK. 2 L 7 2 4F RT A16WE 1998082800457 19980828 00457 NM 1998 8 28 RAAA98B2040 1 19980823 A 2782 1U1110 ACTUATOR BOEING 727 72722C 138400F NM NR 5 LE FLAP FAILED A RAAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 832RV 6110 19098 DURING CLIMBOUT, LE FLAP STATUS DISAGREEMENT LIGHT ON AFTER FLAPS RETRACTED. RETURNED TO UUS AND LANDED WITHOUT INCIDEN T. FOUND NR 5 LE FLAP WOULD NOT RETRACT. CHANGED NR 5 LE FLAP ACTUATOR AND SHUTTLE VALVE DUE ACTUATOR FAILED IN EXTEND ED POSITION. 2 L 7 3 4F A3WE 1998082800458 19980828 00458 WP 1998 8 28 CALA9801496 1 19980822 A 3260 SWITCH DOUG DC9 DC932 3022066 WP RT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 12510 47799 THE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR HANDLE WAS IN THE UP POSITION AND THE GEA R DOOR OPEN LIGHT WAS EXTINGUISHED. CYCLING THE GEAR DID NOT HELP. THE FLIGHT LANDED AT IAH WITHOUT INCIDENT. MAINTEN ANCE FOUND THE RT UPLOCK SWITCH AT FAULT. THE SWITCH WAS REMOVED AND REPLACED IAW MM 32-60-1. OPERATION AND INDICATION S CHECKED GOOD. 2 L 7 2 4F A6WE 1998082800459 19980828 00459 WP 1998 8 28 CALA9801497 1 19980823 A 3241 392492 VALVE DOUG DC9 DC982 3022082 WP RT ANTISKID LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 938AS 29230 49365 THE RT HYDRAULIC SYSTEM QUANTITY DECREASED DURING CLIMBOUT. QRH PROCEDURES WERE FOLLOWED FOR HYDRAULIC QUANTITY LOSS AN D ALTERNATE GEAR EXTENSION WAS USED FOR RETURN TO MCO WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOARD ANTI-SKID DUAL CONTROL VALVE LEAKING. THE ANTI-SKID DUAL CONTROL VALVE WAS REMOVED AND REPLACED IAW MM 32-4 3-03, PAGE 202A. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998082800460 19980828 00460 NM 1998 8 28 CALA9801498 1 19980823 A 2913 6507506 HYD PUMP BOEING 737 737130 1384435 NM NR 2 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 77204 17287 19021 THE NR 2 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AFTER TAKEOFF. THE NR 1 ENGINE A-HYD PUMP LOW PRESSURE LIGHT ILLUMINATED AND THE EMERGENCY CHECKLIST FOR LOSS OF HYD WAS COMPLETED. THE AIRCRAFT WAS RETURNED AND LANDED WITHOUT INC IDENT. MAINTENANCE FOUND FLUID LEAKING FROM CASE DRAIN OF THE NR 2 ENGINE A-HYD PUMP. THE PUMP WAS REMOVED AND REPLACE D IAW MM 29-10-32, PAGE 401. IN ADDITION, THE NR 1 ENGINE DRIVEN HYD PUMP WAS REMOVED AND REPLACED. THE A-HYD SYSTEM W AS SERVICED TO FULL. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1998082800461 19980828 00461 EA 1998 8 28 COMA9860236 1 19980816 A 3230 TORQUE LINKS CNDAIR CL600 CL6002B19 EA NLG DISCONNECTED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 926CA 7027 NLG DID NOT RETRACT. FOUND NLG TORQUE LINKS DISCONNECTED. CONNECTED TORQUE LINKS AND AIRCRAFT RETUNRED TO SERVICE. 2 L 7 2 4F RT A21EA 1998082800462 19980828 00462 WP 1998 8 28 ABXA9800780 1 19980821 A 5210 5615403225 DOOR DOUG DOUG DC8 DC861 3021952 WP CABIN OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45940 DURING POST FLIGHT INSPECTION WAS UNABLE TO OPEN MAIN CABIN DOOR. MADE VERTICAL ADJUSTMENT IAW DC8 MM, OPS CHECKED GOOD . 2 L 7 4 4F 4A25 1998082800463 19980828 00463 WP 1998 8 28 MWEA98881 1 19980822 A 5730 59358221 SKIN DOUG DC9 DC982 3022082 WP WS 111-125 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND 5 AREAS OF BLENDOUT AND CORROSION ON LEFT WING LOWER SKIN AT AFT SPAR ATTACH AREA FROM XRS 111-XRS125. MTC FABRIC ATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998082800464 19980828 00464 NM 1998 8 28 MWEA98882 1 19980821 A 2560 956953503 COVER DOUG MD88 MD88 3023688 NM PAX DOOR SLIDE LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 601ME 49762 FWD ENTRY DOOR EMERGENCY SLIDE COVER LOOSE. RESECURED EMERGENCY SLIDE COVER. 2 L 7 2 4F RT A6WE 1998082800465 19980828 00465 WP 1998 8 28 MWEA98883 1 19980822 A 5280 5910161502 SKIN DOUG DC9 DC914 3022034 WP RT MLG DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND RIGHT MAIN INBOARD LANDING GEAR DOOR DENTED IN AT THE BUMPER. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998082800467 19980828 00467 WP 1998 8 28 MWEA98885 1 19980822 A 5280 59175282 FRAME DOUG DC9 DC914 3022034 WP RT MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND CRACK ON RIGHT MAIN LANDING GEAR DOOR. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998082800468 19980828 00468 WP 1998 8 28 MWEA98886 1 19980822 A 5280 5910161501 SKIN DOUG DC9 DC914 3022034 WP LT MLG DOOR DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND LEFT MAIN INBOARD LANDING GEAR DOOR DENTED IN AT THE BUMPER AND HAS SKIN DAMAGE ON FORWARD BUMPER. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998082800469 19980828 00469 WP 1998 8 28 RRXA98342 1 19980807 A 5244 5614438 DOOR DOUG DC8 DC873F 302199F WP FUS PNEU ACCESS CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND GROUND PNEUMATIC ACCESS DOOR, INTERNAL DOUBLER CORRODED AND CRACKED. REMOVED CORRODED REPAIR DOUBLER, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW FAA APPROVED TIMCO DER ENGI NEERING SKETCH REO-05072. 2 L 7 4 4F RT 4A25 1998082800470 19980828 00470 WP 1998 8 28 RRXA98343 1 19980720 A 5320 56150402 FITTING DOUG DC8 DC873F 302199F WP BS 980 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FITTING (P/N 5615040-2), AT STA 980 AND LONGERON 22 RIGHT FOUND DAMAGED. REMOVED FITTING, F ABRICATED NEW FITTING BY MATERIAL SUBSTITUTION. ORIGINAL MATERIAL 7075-T411, SUBSTITIUTED WITH 7075T-T6 IAW FAA APPROVE D TIMCO ENGINEERING SKETCH REO-05079. FABRICATED AND INSTALLED NEW FITTING IAW DWG 56150T0 AND DWG 5615041 AND DPS4.999 . 2 L 7 4 4F RT 4A25 1998082800471 19980828 00471 WP 1998 8 28 RRXA98344 1 19980731 A 5414 9754906 PLATING DOUG DC8 DC873F 302199F WP NR 3 PYLON CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND NUMBER 3 PYLON, LEADING EDGE WITH .5 INCH CRACK. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05083. 2 L 7 4 4F RT 4A25 1998082800472 19980828 00472 WP 1998 8 28 RRXA98345 1 19980727 A 5315 3773157502 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND INBOARD FLANGE OF FLOORBEAM AND FRAME, STRUT WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1480, BLR. REMOVED DAMAGED SECTION, TREATED AREA IAW DC08 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05094. 2 L 7 4 4F RT 4A25 1998082800473 19980828 00473 WP 1998 8 28 RRXA98346 1 19980807 A 5311 3773157502 FRAME DOUG DC8 DC873F 302199F WP BS 1460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND INBOARD FLANGE OF FLOORBEAM AND FRAME, STRUT WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1460, BLR. REMOVED DAMAGED SECTION, TREATED AREA IAW DC08 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05098. 2 L 7 4 4F RT 4A25 1998082800474 19980828 00474 WP 1998 8 28 RRXA98347 1 19980807 A 5315 37731572 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLANGE OF FLOORBEAM AND FRAME, STRUT WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1520, BLR. REMOVED DAMAGED SECTION, TREATED AREA IAW DC08 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05099. 2 L 7 4 4F RT 4A25 1998082800475 19980828 00475 WP 1998 8 28 RRXA98348 1 19980724 A 5330 57503223 SKIN DOUG DC8 DC873F 302199F WP BS 1050-1084.5 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND SKIN/PLATING WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1050 TO 1084.5 A ND LONGERON 35 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLE R IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05103. 2 L 7 4 4F RT 4A25 1998082800476 19980828 00476 WP 1998 8 28 RRXA98349 1 19980724 A 5315 3773077509 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND INBOARD FLANGE OF FLOORBEAM AND FRAME, STRUT WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1320, BLR. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05111. 2 L 7 4 4F RT 4A25 1998082800477 19980828 00477 WP 1998 8 28 RRXA98350 1 19980727 A 5311 3773077509 FRAME DOUG DC8 DC873F 302199F WP BS 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND INBOARD FRAME, STRUT WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1240, BL L. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO D ER ENGINEERING SKETCH REO-05118. 2 L 7 4 4F RT 4A25 1998082800478 19980828 00478 WP 1998 8 28 RRXA98351 1 19980728 A 5315 3773077 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 380 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND INBOARD FLANGE OF FLOORBEAM AND FRAME, STRUT WITH TOOL DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 380, BLL. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FA A APPROVED TIMCO DER ENGINEERING SKETCH REO-05129. 2 L 7 4 4F RT 4A25 1998082800479 19980828 00479 WP 1998 8 28 RRXA98352 1 19980728 A 5320 36169442 FITTING DOUG DC8 DC873F 302199F WP BS 832 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FITTING (P/N 3616944-2), AT STA 832 AND LONGERON 21 RIGHT FOUND DAMAGED. REMOVED FITTING, F ABRICATED NEW FITTING BY MATERIAL SUBSTITUTION. ORIGINAL MATERIAL 7075-T411, SUBSTITUTED WITH 7075T-T6 IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05130. FABRICATED AND INSTALLED NEW FIITING IAW DWG 3616944-2 AND DPS4.999. 2 L 7 4 4F RT 4A25 1998082800480 19980828 00480 WP 1998 8 28 RRXA98353 1 19980728 A 5315 3773449503 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 781.5 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 781.5 AND BLL 2 TO BLL 10. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TI MCO DER ENGINEERING SKETCH REO-05135. 2 L 7 4 4F RT 4A25 1998082800481 19980828 00481 WP 1998 8 28 RRXA98354 1 19980729 A 5753 5642960 HINGE DOUG DC8 DC873F 302199F WP RT TE FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND RIGHT INBOARD FLAP, HINGE, (P/N 5642960), GOUGED. REPAIRED HINGE BY BLENDOUT, FABRICA TED 6 FILLERS, 4 RUB STRAPS AND INSTALLED IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05139. 2 L 7 4 4F RT 4A25 1998082800482 19980828 00482 WP 1998 8 28 RRXA98355 1 19980807 A 5311 5616521 FRAME DOUG DC8 DC873F 302199F WP BS 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FRAME CHANNEL, WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 520 AND LONGER ON 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05142. 2 L 7 4 4F RT 4A25 1998082800483 19980828 00483 WP 1998 8 28 RRXA98356 1 19980807 A 5320 5887442 ANGLE DOUG DC8 DC873F 302199F WP BS 180 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FRAME ANGLE CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 180 AND LONGERON 30 LEFT. REM OVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGI NEERING SKETCH REO-05145. 2 L 7 4 4F RT 4A25 1998082800484 19980828 00484 WP 1998 8 28 RRXA98357 1 19980807 A 5311 5640914 FRAME DOUG DC8 DC873F 302199F WP BS 980 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLE, AT STA 980 AND LONGERON 7 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-0149. 2 L 7 4 4F RT 4A25 1998082800485 19980828 00485 WP 1998 8 28 RRXA98358 1 19980807 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1480-1600 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM, UPPER FLANGE WITH MULTIPLE ELONGATED HOLES, AT STA 1480 TO 1600. FABRICATE D AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05150. 2 L 7 4 4F RT 4A25 1998082800486 19980828 00486 WP 1998 8 28 RRXA98359 1 19980807 A 5400 57530541 FASTENER DOUG DC8 DC873F 302199F WP NR 2 PYLON TRAPPED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, TRAPPED FASTENER UNDER DRAG ANGLE AND A FASTENER INTERFERS WITH REPLACEMENT OF FOOTSTOOL FIT TING AT NR 2 PYLON. DELTED TRAPPED FASTENER FROM FOOTSTOOL, INSTALLED AND MODIFIED FOOTSTOOL TO AVOID INTERFERENCE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05152. 2 L 7 4 4F RT 4A25 1998082800487 19980828 00487 WP 1998 8 28 RRXA98360 1 19980807 A 5400 57530542 FASTENER DOUG DC8 DC873F 302199F WP NR 3 PYLON TRAPPED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, TRAPPED FASTENER UNDER DRAG ANGLE AND A FASTENER INTERFERS WITH REPLACEMENT OF FOOTSTOOL FIT TING AT NR 3 PYLON. DELTED TRAPPED FASTENER FROM FOOTSTOOL, INSTALLED AND MODIFIED FOOTSTOOL TO AVOID INTERFERENCE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05153. 2 L 7 4 4F RT 4A25 1998082800488 19980828 00488 WP 1998 8 28 RRXA98361 1 19980807 A 5315 2772345 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 200 AND BLR 45. RE MOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05159. 2 L 7 4 4F RT 4A25 1998082800489 19980828 00489 WP 1998 8 28 RRXA98362 1 19980807 A 5315 9753796 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 620. REMOVED DAMAG ED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINE ERING SKETCH REO-05169. 2 L 7 4 4F RT 4A25 1998082800490 19980828 00490 WP 1998 8 28 RRXA98363 1 19980807 A 5315 2773274 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 822 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM, UPPER SURFACE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 822 AND BLL 15. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05170. 2 L 7 4 4F RT 4A25 1998082800491 19980828 00491 WP 1998 8 28 RRXA98364 1 19980807 A 5311 9755884 FRAME DOUG DC8 DC873F 302199F WP BS 1080 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FRAME LOWER SURFACE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1080 AND LONGERON 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FA A APPROVED TIMCO DER ENGINEERING SKETCH REO-05171. 2 L 7 4 4F RT 4A25 1998082800492 19980828 00492 WP 1998 8 28 RRXA98365 1 19980807 A 5311 5779772 FRAME DOUG DC8 DC873F 302199F WP BS 1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FRAME LOWER SURFACE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1060 AND LONGERON 35 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05172. 2 L 7 4 4F RT 4A25 1998082800493 19980828 00493 WP 1998 8 28 RRXA98366 1 19980807 A 5311 3706962 FRAME DOUG DC8 DC873F 302199F WP BS 1120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FRAME LOWER SURFACE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1120 AND LONGERON 33 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05177. 2 L 7 4 4F RT 4A25 1998082800494 19980828 00494 WP 1998 8 28 RRXA98367 1 19980807 A 5315 3773077510 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM TO FRAME STRUT WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 380, BLL. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMC O DER ENGINEERING SKETCH REO-05178. 2 L 7 4 4F RT 4A25 1998082800495 19980828 00495 WP 1998 8 28 RRXA98368 1 19980805 A 5320 37558401 FITTING DOUG DC8 DC873F 302199F WP BS 834 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FITTING (P/N 3755840-1), AT STA 834 AND LONGERON 21 RIGHT FOUND DAMAGED. REMOVED FITTING, F ABRICATED NEW FITTING BY MATERIAL SUBSTITUTION. ORIGINAL MATERIAL 7075-T411, SUBSTITUTED WITH 7075T-T6 IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05192. FABRICATED AND INSTALLED NEW FIITING IAW DWG 5615040 AND DPS4.999. 2 L 7 4 4F RT 4A25 1998082800496 19980828 00496 WP 1998 8 28 RRXA98369 1 19980807 A 5315 2759472 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM, UPPER SURFACE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1580 AND BLL 50. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FA A APPROVED TIMCO DER ENGINEERING SKETCH REO-05200. 2 L 7 4 4F RT 4A25 1998082800497 19980828 00497 WP 1998 8 28 RRXA98370 1 19980807 A 5315 2773274 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 834 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM, UPPER SURFACE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 834 AND BLL 24. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05201. 2 L 7 4 4F RT 4A25 1998082800498 19980828 00498 WP 1998 8 28 RRXA98371 1 19980821 A 5730 5769857395 SKIN DOUG DC8 DC873F 302199F WP WS 526.76 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, LEADING EDGE, LOWER SKIN SURFACE WITH .55 INCH CRACK, AT STA XFS 526.76. R EMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05316. 2 L 7 4 4F RT 4A25 1998082800499 19980828 00499 WP 1998 8 28 RRXA98372 1 19980820 A 5320 56161322 FITTING DOUG DC8 DC873F 302199F WP MLG WW DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FITTING (P/N 5616132-2), AT WHEEL WELL AND LONGERON 24 RIGHT FOUND DAMAGED. REMOVED FITTING , FABRICATED NEW FITTING BY MATERIAL SUBSTITUTION. ORIGINAL MATERIAL 7075-T411, SUBSTITUTED WITH 7075T-T6 IAW FAA APPRO VED TIMCO ENGINEERING SKETCH REO-05079. FABRICATED AND INSTALLED NEW FITTING IAW DWG 5616132 AND DWG 5616429 AND DPS4.9 99. 2 L 7 4 4F RT 4A25 1998082800500 19980828 00500 WP 1998 8 28 ARWA980811 1 19980823 A 5270 SENSOR DOUG DC8 DC862F 3021972 WP PAX DOOR MALFUNCTIONED A ARWA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 19 791AL 46150 MIA - FLT 627 - REJECTED T/O DUE MAIN CABIN DOOR LIGHT AND MASTER WARNING LIGHTS COMES ON INTERMITTENT. CHECK DOOR VISU AL AS NORMAL, OPEN AND CLOSE AGAIN LIGHTS GOES OUT. DEPART, ACCORDING AOM BRAKE COOLING CHART. CHECK MAIN CABIN DOOR O PEN AND CLOSE FEW TIMES WARNING LIGHT OK MM 52-10-0. (M) 2 L 7 4 4F 4A25 1998082800501 19980828 00501 WP 1998 8 28 TC8A9052 1 19980825 A 3251 ACTUATOR DOUG DC8 DC862F 3021972 WP NLG STEERING FAILED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 187SK 46022 UNABLE TO STEER AIRCRAFT, TOW BACK TO THE RAMP. REMOVED AND REPLACED LT STEERING ACTUATOR, OPS CHECK AND LEAK CHECK OK IAW MM 32-32-12. 2 L 7 4 4F 4A25 1998082800502 19980828 00502 WP 1998 8 28 TC8A98050 1 19980825 A 3260 H2015 SWITCH DOUG DC8 DC862F 3021972 WP LT MLG STRUT FAILED A TC8A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 183SK 45904 AFTER T/O AND CLIMB CK, TAKEOFF WARNING HORN CAME ON, UNABLE TO SILENCE. GROUND COOLING BLOWAWAY JET LIGHT ON. PULL GR OUND CONTROL RELAY, WAS ABLE TO RESET. REMOVED AND REPLACED LT GROUND CONTROL OLEO SWITCH IAW DC8 MM 24-52-2, 32-62-0, OPS CHECK GOOD. CHECKED OPERATION AND RIGGING OF GROUND SHIFT MECHANISM. ADJUSTED CABLE TENSION IAW DC8 MM 32-52-8. L UBRICATED LINKAGES IAW DC8 MM CHPT 12-00. CHECKED FOR BROKEN PULLEYS AND BINDING LINKAGES IN GROUND SHIFT SYSTEM, ALL C OMPONENTS FOUND IN GOOD CONDITION. NO BINDING IN SYSTEM. SERVICED NOSE GEAR STRUT IAW DC8 MM 32-21-2. 2 L 7 4 4F 4A25 1998082800503 19980828 00503 WP 1998 8 28 TC8A98051 1 19980825 A 3251 37666395507 CYLINDER DOUG DC8 DC861F 3021953 WP NLG STEERING FAILED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 184SK 45981 AFTER PUSHBACK, AIRCRAFT WOULD ONLY TURN SEVERAL DEGREES LEFT WITH NOSE WHEEL STEERING. FOUND RT STEERING CYLINDER FAIL ED DURING PUSHBACK. REPLACED RT STEERING CYLINDER AND FUNCTIONAL CHECK AND LEAK CHECK GOOD IAW 32-52-2. 2 L 7 4 4F 4A25 1998082800529 19980828 00529 WP 1998 8 28 TWAA9813601 1 19980823 A 3246 3910797 WHEEL DOUG DC9 DC941 302207N WP RT MLG SEPARATED A TWAA O OTHER O OTHER LD LANDING 1 CE 05 933L 47617 DURING LANDING ROLLOUT THE RT I/B TIRE AND WHEEL ASSEMBLY SEPARATED FROM THE AXLE. INSTALLED NEW TIRE AND WHEEL ASSEMBL Y. THERE WAS NO AXLE DAMAGE. THE WHEEL ASSEMBLY HAD BEEN INSTALLED THE PREVIOUS DAY, BUT THE SPACER AND AXLE NUT WERE NOT RECOVERED, SO A DETERMINATION OF THE CAUSE COULD NOT BE MADE. CHECK-C 2-16-98 STL. 2 L 7 2 4F A6WE 1998082800530 19980828 00530 NM 1998 8 28 TWAA9813602 1 19980824 A 3510 15830AC REGULATOR BOEING 767 767231 1385131 NM LT COCKPIT LEAKING A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 601TW 22564 CREW OXYGEN PRESSURE WENT TO ZERO, NOTICED AT TOP OF CLIMB. RETURNED TO JFK. FOUND CAPT OXY REGULATOR FAULTY. REPLACE D REGULATOR AND OXY BOTTLE. CHECK-C 7-9-98 LAX. 2 L 7 2 4F RT A1NM 1998082800531 19980828 00531 WP 1998 8 28 TWAA9813603 1 19980630 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 794 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 405EA 47688 DURING MAINT, A .5 IN CRACK WAS FOUND AT FASTENER AT STA 794, LONG 2R. SPLICED IN NEW SECTION OF LONG 20 IN LONG. ALL WORK DONE PER SRM 53-02, FIG 18. CHECK-C 12-13-97 STL. 2 L 7 2 4F RT A6WE 1998082800532 19980828 00532 WP 1998 8 28 TWAA9813604 1 19980819 A 5347 TIE DOWN TRACK DOUG DC9 DC951 3022051 WP CARGO COMPT CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 DURING CHECK-C MAINT, FOUND IN AFT CARGO COMPT THE RT TIE DOWN TRACK, AFT OF CARGO DOOR, WITH CORROSION IN CHANNEL. REP LACED RT TIE DOWN TRACK AFT OF DOOR PER SRM 51-01, PAGE 4. 2 L 7 2 4F RT A6WE 1998082800533 19980828 00533 WP 1998 8 28 TWAA9813605 1 19980714 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 370-389 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 915TW 49186 FOUND ONE INCH HOLE APPROX 9 IN LONG ON LT SIDE OF FUSELAGE AT LONGERON 2L AND STA 370 TO 389. REPAIRED DAMAGE PER SRM 53-04, PAGE 43 FIG 12B. CHECK-C 5-17-98 STL. 2 L 7 2 4F A6WE 1998082800534 19980828 00534 NM 1998 8 28 VJ9800294 1 19980825 A 3350 1000679 LIGHT BOEING 737 737284 138448R NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 470AT 21501 L-2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED L-2 DOOR PORTABLE EMERGENCY LIGHT IAW BMM 33-51-101. 2 L 7 2 4F A16WE 1998082800535 19980828 00535 WP 1998 8 28 VJ9800295 1 19980818 A 5321 1A353231 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 DURING C-CHECK AT 31J, FOUND CABIN FLOOR BOARD STA 160 TO 200 RBL 44 TO 54 HAS CORROSION. MECHANICALLY REMOVED CORROSIO N AND FOUND TO BE OUT OF LIMITS WITH 100 PERCENT OF THE MATERIAL LOSS AROUND THE NET PLATE HOLE. CRACK ALSO FOUND WHEN CLEANING AREA FOR REPAIR. STOP DRILLED CRACK AND FABBED REPAIR, IAW SRM 53-01 FIG 2. HFEC CRACK CONTAINED AT STOP HOLE DC-9 SRM NTM PART 06. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED REPAIR IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998082800536 19980828 00536 WP 1998 8 28 CALA9801499 1 19980821 A 5711 SPAR CAP DOUG DC9 DC931 3022065 WP WS 364.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND RT WING AFT LOWER SPAR CAP CORRODED AT WS XRS 364.5. THE AFT LOWER SPAR CAP WAS REPAIRED IAW SRM 57-09 , FIGURE 11. 2 L 7 2 4F A6WE 1998082800537 19980828 00537 NM 1998 8 28 CALA9801500 1 19980821 A 5754 SKIN BOEING 727 727232 1384082 NM RT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND TWO 2.5 INCH CRACKS AT RIVET HEADS FORWARD OF OUTBOARD SEQUENCE CARRIAGE ATTACH POINT OF RT INBOARD FOR EFLAP. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30. 2 L 7 3 4F A3WE 1998082800538 19980828 00538 NM 1998 8 28 CALA9801501 1 19980824 A 5313 STRINGER BOEING 737 7373T0 1384582 NM BS 1006-1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69348 23586 INSPECTION FOUND STRINGER CORRODED JUST BELOW RT AFT LAV DUMP CHUTE FROM STA 1006 TO 1016. THE CORRODED SECTION OF STRI NGER WAS REMOVED AND A NEW SECTION OF STRINGER AND SHIM WERE FABRICATED AND INSTALLED IAW ECRA 5360-01018. 2 L 7 2 4F RT A16WE 1998082800539 19980828 00539 EA 1998 8 28 COMA9860237 1 19980814 A 5753 601R14303042 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 C-CHECK INSPECTION, RIGHT HAND INBOARD FLAP VANE HAS CHAFE DAMAGE. INSTALLED NEW FLAP VANE LEADING EDGE. 2 L 7 2 4F RT A21EA 1998082800540 19980828 00540 EA 1998 8 28 COMA9860238 1 19980814 A 5753 601R14303041 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 C-CHECK INSPECTION, LEFT HAND INBOARD FLAP VANE IS DAMAGED. REPLACED FLAP VANE LEADING EDGE SKIN. 2 L 7 2 4F RT A21EA 1998082800541 19980828 00541 EA 1998 8 28 COMA9860239 1 19980817 A 2710 272955 LINK CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 917CA 7017 C-CHECK INSPECTION, RIGHT HAND AILERON OUTBOARD PCU LINK HAS EXCESS PLAY. REPLACED LINK. 2 L 7 2 4F RT A21EA 1998082800542 19980828 00542 EU 1998 8 28 QXEA9801087 1 19980820 A 2611 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAVATORY MALFUNCTIONED A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 494US 11167 LAVATORY SMOKE DETECTOR INTERMITTENTLY ACTIVATES. NO SMOKE NOTED BY CREW. MAINTENANCE REMOVED AND REPLACED THE LAVATOR Y SMOKE DETECTOR, OPERATIONAL CHECK GOOD. NO SMOKE WAS NOTED. 2 L 7 2 4F RT A20EU 1998082800543 19980828 00543 EU 1998 8 28 QXEA9801088 1 19980821 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 EMERGENCY EXIT SIGNS AT ROW 9 HAVE SEVERAL 28 VOLT BULBS OUT. MAINTENANCE REPLACED SIGN ASSEMBLY, OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A20EU 1998082800544 19980828 00544 EU 1998 8 28 QXEA9801089 1 19980822 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 FORWARD EMERGENCY EXIT SIGN HAS SEVERAL 28 VOLT BULBS OUT. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998082800545 19980828 00545 EU 1998 8 28 QXEA9801090 1 19980822 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 EVACUATION LIGHTS ON SEATS 5, 6, 8, 10 AND 11B INOP. MAINTENANCE SECURED WIRE CONNECTOR UNDER SEAT 9, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998082800546 19980828 00546 EU 1998 8 28 QXEA9801091 1 19980822 A 3350 5515900004 CURCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 493US 11161 LIGHTS ARE DIM IN EXIT SIGN ON PASSENGER CABIN CEILING AT ROWS 8 AND 9. MAINTENANCE REPLACED CIRCUIT BOARD FOR CEILING EXIT SIGN AT ROWS 8 AND 9, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998082800547 19980828 00547 NM 1998 8 28 98FDEA00526 1 19980824 A 5330 65545406 SKIN BOEING 727 727227 1384078 NM BS 680-692 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 NR-0510 - WHILE WORKING NRO434 FOUND CORROSION ON BELLY SKIN OUT OF LIMITS AT BS 680 - 692 WL 149 RBL 11-12 IAW FEDEX SRM 53-30-1. REPAIRED BELLY SKIN AT BS 680 TO 692 WL149, RBL 11-12 IAW FEDEX SRM 53-30-3. 2 L 7 3 4F A3WE 1998082800548 19980828 00548 NM 1998 8 28 98FDEA00527 1 19980825 A 5314 6556441 KEEL BEAM BOEING 727 727227 1384078 NM BS 950-990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 NR 0444 - CORROSION ON LT KEEL BEAM AT BS 950F PLUS 5 TO BS 990, LBL 6, WL 138. REMOVED CORROSION ON LT KEEL BEAM AT B S 950F PLUS 5 TO BS 990, LBL 6, WL 138 PER SR 27-53-023. ALL REPAIR WORK ACCOMPLISHED PER EA 7-5310-39912A. 2 L 7 3 4F A3WE 1998082800549 19980828 00549 NM 1998 8 28 98FDEA00528 1 19980824 A 5320 651633925 SHEAR TIE BOEING 727 727227 1384078 NM BS 970 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 NR 0453 CORROSION (C53-113-02) SHEAR TIE AT BS 970, LBL 7, WL 138. REMOVED AND REPLACED SHEAR TIE AT BS 970, LBL 7, WL 138 IAW FEDEX SRM 53-10-4. 2 L 7 3 4F A3WE 1998082800550 19980828 00550 NM 1998 8 28 98FDEA00529 1 19980824 A 5320 69648411 SUPPORT BOEING 727 727227 1384078 NM BS 740 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 491FE 21529 740 BULKHEAD IN A/C BAYS WHERE KEEL BEAMS ATTACH (BOTH LT AND RT KEEL BEAMS) IS CORRODED. * S/D* REMOVED AND REPLACED BS 740 RT SKIN FORMER FROM RBL 7 TO 15 PER FEDEX SRM 51-30-2. REMOVED AND CORROSION ON BS 740 LT AT LBL 7, WL 144. ALO DINED AND RESTORED PROTECTIVE FINISH TO ALL BARE METAL PER FEDEX M/M 51-20-151. 2 L 7 3 4F A3WE 1998082800551 19980828 00551 NM 1998 8 28 98UAL900377 1 19980804 A 2841 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE REFUELING PANEL DIRTY A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 7453U 21907 AFTER DEPARTURE ALL FUEL QUANTITY GAUGES DROPPED TO ZERO. RESETTING CIRCUIT BREAKER DID NOT SOLVE PROBLEM. FLIGHT WAS DIVERTED TO SYR. *S/D* SUSPECTED REFUELING PANEL POWER SWITCH. CLEANED POWER SWITCH AT REFUELING PANEL. NO SUBSEQUEN T WRITE-UPS. 2 L 7 3 4F 4 F A3WE E2EA 1998082800552 19980828 00552 NE 1998 8 28 98UAL900388 2 19980816 A 7261 1A281101 MANIFOLD BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE CRACKED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 WP 29 501UA 24622 726553 MADE AN UNSCHEDULED LANDING INTO DEN, BECAUSE THE NUMBER 2 ENGINE WAS SHUTDOWN DUE TO LOSS OF OIL. *S/D* FOUND CRACKED OIL BREATHER MANIFOLD. REPLACED MANIFOLD AND RELEASED A/C BACK INTO SERVICE AFTER WINDMILLING INSPECTION PER 757 MM. M ANIFOLD HAS BEEN RETURNED TO PWA FOR INVESTIGATION. 2 L 7 2 4F 4 F RT A2NM E17NE 1998082800553 19980828 00553 1998 8 28 98UAL900389 4 19980816 A 2230 AUTO THROTTLE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT & RT ENGINE MALFUNCTIONED A UALA O OTHER O OTHER DE DESCENT 1 WP 29 424UA 506 ON DESCENT, NO THROTTLE RESPONSE WITH AUTO THROTTLES ON. AUTO THROTTLE SWITCHED OFF, NO THROTTLE RESPONSE IN MANUAL, FL X OR CLIMB. APPLIED T/O G/A POWER AND GOT THROTTLE RESPONSE- BOTH ENGINES. *S/D* ENGINES TESTED AT HI-PWR. AFS AND L AND TEST PER MM 22-97-00 ACCOMPLISHED WITH NO FAULTS DETECTED. AIRCRAFT RETURNED TO SERVICE. TO DATE (9/25/98) NO MORE AUTO THROTTLE PROBLEMS HAVE HAPPEDNED. 2 L 7 2 4F 4 F RT A28NM E40NE 1998082800554 19980828 00554 EU 1998 8 28 98UAL900390 1 19980815 A 2611 PAI280001 SMOKE DETECTOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CARGO COMPT DEFECTIVE A UALA F ACTIVATE FIRE EXT. N FALSE WARNING UK UNKNOWN 1 WP 29 409UA 462 FORWARD CARGO SMOKE INDICATION ON UPPER ECAM FLASHED INTERMITTENTL, THEN CAME ON CONTINUOUSLY. DISCHARGED AGENT. RETUR NED TO FIELD. *S/D* DEFECTIVE SMOKE DETECTOR COUPLED WITH OPEN GROUND 1999UT TERMINAL BLOCK. REPLACED SMOKE DETECTOR CONTROL UNIT AND SMOKE DETECTORS. CHECKED WIRING AND TEST FLEW A/C. 2 L 7 2 4F 4 F RT A28NM E40NE 1998082800555 19980828 00555 EU 1998 8 28 98UAL900391 1 19980813 A 3260 ABS012110 PROX SENSOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 416UA 479 ECAM MESSAGE SHOCK ABSORBER FAULT. CB RESETS ON LGCIU'S, NO HELP. DIVERTED TO DENVER AMBER ALERT. *S/D* CFDS INDICAT ED PROX SENSOR 24GA AT FAULT. REPLACED SENSOR PER MM 32-31-73. 2 L 7 2 4F 4 F RT A28NM E40NE 1998082800556 19980828 00556 NM 1998 8 28 98UAL900392 1 19980814 A 3350 LIGHT BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT EXTERIOR MALFUNCTIONED A UALA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 WP 29 663UA 27160 AIRCRAFT RETURNED TO BLOCKS WITH REPORT OF LEFT AFT EXTERIOR EMERGENCY LIGHTS ILLUMINATED. *S/D* PERFORMED EXTERIOR EMER GENCY LIGHTS TEST PER MM. NO PARTS REPLACED, NO FURTHER REOCCURRENCE OF DISCREPANCY. 2 L 7 2 4F 4 F RT A1NM E24NE 1998082800557 19980828 00557 NM 1998 8 28 98UAL900393 1 19980813 A 3350 BATTERY PACK BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 174UA 24381 LEFT SIDE UPPER DECK DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK AND WORKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 1998082800558 19980828 00558 EU 1998 8 28 98UAL900394 1 19980818 A 2913 MR29142 PUMP AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 404UA 450 CREW REPORT, GREEN EDP LOW PRESSURE AND LOW GREEN SYSTEM PRESSURE. QUANTITY IS INDICATING ZERO AMBER ALERT. RETURNED T O DENVER. *S/D* GREEN SYSTEM HYD PUMP REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 1998082800559 19980828 00559 NM 1998 8 28 98UAL900395 1 19980818 A 2620 DISCHARGED LIGHT AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE APU ILLUMINATED A UALA O OTHER J WARNING INDICATION IN INSP/MAINT 1 WP 29 814UA 0862 APU FIRE DISCHARGE LIGHT IS ILLUMINATED. RED DISCHARGE INDICATOR IS PRESENT ON AIRCRAFT. 2 L 7 2 4F 4 F RT A28NM E40NE 1998082800560 19980828 00560 NM 1998 8 28 98UAL900396 1 19980818 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7456U 21910 OVERWING EMERGENCY EXIT LIGHTS AT LEFT SIDE ROW 15 AND 17 WILL NOT EXTINGUISH. *S/D* RESET BATTERY PACK, OPS CHECKS GO OD. 2 L 7 3 4F 4 F A3WE E2EA 1998082800561 19980828 00561 NM 1998 8 28 98UAL900397 1 19980818 A 2150 ACM AIRESEARCH 2040751MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA O OTHER J WARNING INDICATION DE DESCENT 1 WP 29 7297U 21892 CABIN PRESSURE CANNOT BE MAINTAINED IN AUTO. CABIN ALTITUDE RISES IN DESCENT. *S/D* AIR CYCLE MACHINE FAILED. REPLAC ED AIR CYCLE MACHINE. 2 L 7 3 4F 4 F A3WE E2EA 1998082800562 19980828 00562 NE 1998 8 28 98UAL900398 2 19980819 A 7532 51D271 PIN PWA 51D048 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE NR 1 BLEED VALVE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 780UA 9453 9453 26944 777014 UNABLE TO OBTAIN CLIMB THRUST ON NR 1 ENGINE. FLIGHT RETURNED TO ORD. NR 1 ENGINE OVERTEMP ON CLIMB POWER AT 1.15 EPR AND 620 DEGREES (C). RIGHT ENGINE WAS 1.23 EPR AT 590 DEGREES (C). REPLACED NR 1 ENGINE. CAUSE WAS ATTRIBUTED TO BROK EN 2.5 BLEED BELLCRANK PIVOT PIN. PART WAS PRE-SB PW4G-112-72-60. PROJECT IS UNDERWAY TO UPGRADE BLEED DESIGN TO SUBSE QUENT SB PW4G-112-72-106. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998082800563 19980828 00563 NM 1998 8 28 98UAL900399 1 19980820 A 2130 WARNING BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN ACTIVATED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 766UA 26917 CABIN ALTITUDE WARNING. CABIN CLIMBED TO 10,000 FEET. FLIGHT RETURNED TO LAX. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998082800564 19980828 00564 NM 1998 8 28 98UAL900400 1 19980803 A 2910 65C26840 TUBE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE BS 727 WORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 385UA 24660 THE BRAKE ACCUMULATOR B-SYSTEM PRESSURE HYDRAULIC TUBE 65C26840-1058 (IPC: 29-20-00-001D INDEX 155) TUBE IS WORN. THE W EAR IS CAUSED BY INTERFERENCE BETWEEN HYDRAULIC TUBE AND COMPOSITE PANEL. (COMPOSITE PANEL SHOWN ON BLUE PRINT 65-4844 0 SHEET 802 ZONE 11). REPLACED DAMAGED HYDRAULIC TUBE WITH NEW TUBE ASSEMBLY. 2 L 7 2 4F 4 F RT A16WE E2GL 1998082800565 19980828 00565 WP 1998 8 28 ABXA9800770 1 19980811 A 5730 57696005 SKIN DOUG DOUG DC8 DC862 3021970 WP WS 304 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION XFS 304.0 UPPER LEADING EDGE SKIN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED IA W DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1998082800566 19980828 00566 WP 1998 8 28 ABXA9800771 1 19980811 A 5712 5769603 RIB DOUG DOUG DC8 DC862 3021970 WP WS 360.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION XFS 360.250 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K0505 6 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998082800567 19980828 00567 WP 1998 8 28 ABXA9800772 1 19980811 A 5712 5718963 RIB DOUG DOUG DC8 DC862 3021970 WP WS 316.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION 316.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DRAWING K 050 56 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998082800568 19980828 00568 WP 1998 8 28 ABXA9800773 1 19980808 A 5320 46461631 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1020-1040 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT MAIN CABIN SPLICE FITTING CRACKED BETWEEN STATION 1020 TO 1040 LONGERON 7R. REPAIRED IAW DWG 4646163-1, DC8 SRM 5 1-1-20D AND SRM 51-1-8. 2 L 7 4 4F 4A25 1998082800569 19980828 00569 WP 1998 8 28 ABXA9800774 1 19980807 A 5320 37558242 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 500 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 BACK UP FITTING FORWARD SIDE OF TORQUE BOX, STATION 500, LONGERON 34R AND 33R IS CRACKED. REPAIRED IAW DC8 SRM 53-1-0 A ND 51-1-20D. 2 L 7 4 4F 4A25 1998082800570 19980828 00570 WP 1998 8 28 ABXA9800775 1 19980805 A 5712 5769545 RIB DOUG DOUG DC8 DC862 3021970 WP WS 722.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION XFS 722.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW ABX DWG K 05056 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998082800571 19980828 00571 WP 1998 8 28 ABXA9800776 1 19980805 A 5340 4773146 FITTING DOUG DOUG DC8 DC862 3021970 WP SERVICE DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 EXFOLIATED FITTING INSIDE LOWER AFT TORQUE BOX WEB AT RIGHT AFT SERVICE DOOR. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 477 3146. 2 L 7 4 4F 4A25 1998082800572 19980828 00572 WP 1998 8 28 ABXA9800777 1 19980805 A 5712 57696006 RIB DOUG DOUG DC8 DC862 3021970 WP WS 560 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION XFS 560.00 UPPER LEADING EDGE RIB IS CRACKED. REPAIRED IAW DC8 SRM 57-3-2 AND DWG K 5056. 2 L 7 4 4F 4A25 1998082800573 19980828 00573 WP 1998 8 28 ABXA9800778 1 19980803 A 5730 97510821 SKIN DOUG DOUG DC8 DC862 3021970 WP WS 74 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 LEFT WING LEADING EDGE UPPER SURFACE AT THE FORWARD SPAR STATION XFS 74.0 HAS HEAVY CORROSION. REPAIRED IAW ABX REA D 8 57- 22899 MR AND DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1998082800574 19980828 00574 WP 1998 8 28 ABXA9800779 1 19980821 A 5720 97532937 ANGLE DOUG DOUG DC8 DC862 3021970 WP WS 250 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE INTERIOR, VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM OUTBOARD END OF INBOARD SLOT BOX STATION XS 250.089. REPLACED ANGLE IAW DWG 9753293 AND DC8 SRM 51-1-20 AND 51-1-21. 2 L 7 4 4F 4A25 1998082800575 19980828 00575 WP 1998 8 28 RRXA98386 1 19980818 A 5720 5616481 TRAP PANEL DOUG DC8 DC873F 302199F WP LT MLG WW DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING GROUND SERVICE, FOUND AILERON BUS CABLE CUT THROUGH LEFT SIDE OF TRAPEZOIDAL PANEL, (P/N 5616481), LEFT WHEEL WE LL AT STA 865. REMOVED AND REPLACED CABLE SECTION. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05292. 2 L 7 4 4F RT 4A25 1998082800576 19980828 00576 1998 8 28 VNAA9808019 4 19980822 A 6122 PCUAEFS144 GOVERNOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROP DEFECTIVE A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 422JS 30247 3018 WHILE TAXIING TO RUNWAY, CREW PERFORMED PROPELLER OVERSPEED TEST. TEST FAILED. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE PROPELLER OVERSPEED GOVERNOR DEFECTIVE. REPLACED GOVERNOR IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 61-21-04. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998082800586 19980828 00586 SO 1998 8 28 98ZZZX3037 2 19980730 A 8520 6461401 STUD 643202 CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO NR 6 CYL PAD FAILED A HBCA K NONE O OTHER IN INSP/MAINT 1 SW 11 5040Q 300 402B0347 275073H DURING 100-HOUR INSPECTION, MECHANIC NOTICED RIGHT ENGINE, NR 6 CYLINDER, PER MOST AFT AND THE LOWER TWO MOST AFT STUDS HAD BROKEN OFF FLUSH WITH THE CYLINDER BASE/SKIRT. THE CASE WAS INSPECTED FOR CRACKS, AND A CRACK APPROXIMATELY A .50 INCH LONG WAS OBSERVED COMING FROM THE LOWER STUD HOLE (JUST FORWARD OF THE MOST AFT LOWER STUD) WAS CRACKED IN THE DIRE CTION OF THE CENTER OF THE ENGINE CASE. SUBMITTER STATED TO HAVING HAD THIS PROBLEM IN THE PAST AND HAD STARTED REPLACI NG THE CYLINDER BASE STUDS AT ENGINE OVERHAUL. UNFORTUNATELY, THESE STUDS WERE REPLACED AND HAVE APPROXIMATELY 300 HOUR S TISN. 1 L 7 2 3O 3 O A7CE E8CE 1998082800587 19980828 00587 NM 1998 8 28 GAIA9870 1 19980707 A 5320 FITTING BOEING 727 727223 1384074 NM BS 1183 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-100-01 - 2-24 END FITTING CORRODED AT BS 1 183 BULKHEAD. REMOVED AND REPLACED END FITTING IAW B727 SRM 51-10-1 AND SRM 51-30-2. REF: OPER CONTROL NR 98ZZZX3038 THROUGH 98ZZZX3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING I T ON THE KHA OPERATING CERTIFICATE. (X) 2 L 7 3 4F A3WE 1998082800588 19980828 00588 NM 1998 8 28 98ZZZX3038 1 19980707 A 5311 FRAME BOEING 727 727223 1384074 NM BS 211 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-111-01 - BS 211.8 LT FRAME TO DOOR FRAME C ORRODED. REMOVED AND REPLACED CORRODED ANGLE IAW B727 SRM 51-10-1. REF: OPER CONTROL NR GAIA9870 THROUGH 98ZZZX3049 A ND 98ZZZX3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING IT ON T HE KHA OPERATING CERTIFICATE. 2 L 7 3 4F A3WE 1998082800589 19980828 00589 NM 1998 8 28 98ZZZX3039 1 19980707 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-224-01 - BS 702A-720D, RBL SEAT TRACK CORRO DED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-4 AND SRM 51-30-2. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX3038 AND 98ZZZX3946. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING IT ON THE KHA OPERATING CERTIFICATE. 2 L 7 3 4F A3WE 1998082800590 19980828 00590 NM 1998 8 28 98ZZZX3040 1 19980707 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1010-1130 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C-53-224-01 - BS 1010-1130, RBL 25 SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-30-2 AND SRM 53-10-5. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX 3038 AND 98ZZZX3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING I T ON THE KHA OPERATING CERTIFICATE. 2 L 7 3 4F A3WE 1998082800591 19980828 00591 NM 1998 8 28 98ZZZX3041 1 19980707 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 783-804 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-224-01 - BS 738-804, LBL 25 AND 45, SEAT T RACK CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW B727 SRM 51-30-2 AND SRM 53-10-5. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX3038 AND 98ZZZX3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PU TTING IT ON THE KHA OPERATING CERTIFICATE. 2 L 7 3 4F A3WE 1998082800592 19980828 00592 NM 1998 8 28 98ZZZX3042 1 19980707 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 783-848 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-224-01 - BS 783-848, RBL 25, SEAT TRACK CO RRODED. REMOVED AND REPLACED SEAT TRACKS IAW B727 SRM 51-30-2 AND SRM 53-10-5. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX 3038 AND 98ZZZX3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING I T ON THE KHA OPERATING CERTIFICATE. 2 L 7 3 4F A3WE 1998082800593 19980828 00593 NM 1998 8 28 98ZZZX3043 1 19980707 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 783-848 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: B53-224-01 - BS 738-848, RBL 45, SEAT TRACK CO RRODED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-30-2 AND SRM 53-10-5. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX3 038 AND 98ZZZX3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING IT ON THE KHA OPERATING CERTIFICATE. 2 L 7 3 4F A3WE 1998082800594 19980828 00594 NM 1998 8 28 98ZZZX3044 1 19980707 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 480 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-224-01 - BS 480, RBL 45, SEAT TRACK CORROD ED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-30-2 AND SRM 53-10-5. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX3038 AND 98ZZZX 3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING IT ON THE KHA OPERATING CERTIFICATE. 2 L 7 3 4F A3WE 1998082800595 19980828 00595 NM 1998 8 28 98ZZZX3045 1 19980707 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 560 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-224-01 - BS 560, RBL 65 FLOOR ATTACH ANGLE CORRODED. INSTALLED REPAIR IAW SRM 51-40-3. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX3038 AND 98ZZZX3046. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING IT ON THE KHA OPERATING CERTIFICATE . 2 L 7 3 4F A3WE 1998082800596 19980828 00596 NM 1998 8 28 98ZZZX3046 1 19980707 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1130 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6821 19496 DURING CPC INSPECTION, THE FOLLOWING LEVEL 2 CORROSION ITEMS WERE NOTED: C53-224-01 - BS 1130, LBL 25, SEAT TRACK CORRO DED. REMOVED AND REPALCED SEAT TRACK IAW B727 SRM 53-10-5. OPER CONTROL NR GAIA9870 THROUGH 98ZZZX3038 AND 98ZZZX3045. NOTE: THESE CPC ITEMS WERE FOUND DURING A PHASE-IN INSPECTION OF THIS AIRCRAFT PRIOR TO PUTTING IT ON THE KHA OPERATIN G CERTIFICATE. 2 L 7 3 4F A3WE 1998082800610 19980828 00610 SW 1998 8 28 98ZZZX3060 1 19980721 A 3244 850108PLY TIRE GOODYEARAERO GULSTM 500 500S 0141107 SW TREAD GROOVE SEPARATION A EHSA K NONE O OTHER IN INSP/MAINT 1 WP 07 4664E 694 43141279 17869 INSPECTION FOUND CORD SEPARATION OCCURRING IN TIRE. 1 H 7 2 3O 6A1 1998082800633 19980828 00633 EU 1998 8 28 SIMA981892 1 19980708 A 5347 S5357020300 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AT 451 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800634 19980828 00634 EU 1998 8 28 98ZZZM559 1 19980708 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AT 451 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800635 19980828 00635 EU 1998 8 28 98ZZZM560 1 19980708 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AT 451 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800636 19980828 00636 EU 1998 8 28 98ZZZM561 1 19980708 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 451AT 451 SAW - DURING CPCP-8 INSPECTION, MAINTENANCE REPORTED THE LEFT MIDDLE INBOARD, LEFT AFT INBOARD, LEFT AFT OUTBOARD, RIGHT MIDDLE INBOARD, RIGHT MIDDLE OUTBOARD AND RIGHT AFT INBOARD SEAT TRACKS CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACKS IAW SRM 51-25-04. A/C WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800637 19980828 00637 EU 1998 8 28 SIMA981941 1 19980713 A 3350 1311 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 297AE 340B297 DFW - FLT 5020 - FLIGHT ATTENDANT REPORTS AN EMERGENCY LIGHT BURNED OUT OVERHEAD 11A. RAI EMERGENCY LIGHT BULB OVERHEAD SEAT 11A. OPS CHECK GOOD. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800638 19980828 00638 SO 1998 8 28 MASA98140 1 19980703 A 3350 10130115 LIGHT ASSY EMB 120 EMB120RT SO CABIN CRACKED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 221YV 120221 DURING ROUTINE MAINTENANCE, FOUND RIGHT REAR EMERGENCY EXIT COVER CRACKED. REPLACED LIGHT ASSEMBLY, OPS CHECK GOOD. (M ) 2 L 7 2 4T RT A31SO 1998082800639 19980828 00639 NM 1998 8 28 MASA98139 1 19980712 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 455YV 455 DURING ROUTINE MAINTENANCE, FOUND SECOND OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998082800640 19980828 00640 SO 1998 8 28 MASA98138 1 19980705 A 3350 GE1317 BULB EMB 120 EMB120ER 3260203 SO FUSELAGE FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 298YV 120298 WHILE PERFORMING LINE CHECK, FOUND LEFT FORWARD OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. REPLACED LIGHT BULB, OPS CHECK. (M) 2 L 7 2 4T RT A31SO 1998082800641 19980828 00641 NM 1998 8 28 MASA98137 1 19980710 A 3350 SGR3S63AAE LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE, THE FORWARD EMERGENCY ESCAPE PATH LIGHT SECTION WOULD NOT ILLUMINATE. MAINTENANCE REMOVED A ND REPLACED THE LIGHT STRIP AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998082800642 19980828 00642 SO 1998 8 28 MASA98136 1 19980710 A 3350 12021299001 LIGHT EMB 120 EMB120ER 3260203 SO FUSELAGE INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 298YV 120298 DURING NIGHT MAINTENANCE, FOUND THE RIGHT FUSELAGE AFT EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND RE PLACED THE EMERGENCY LIGHT ASSY. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A31SO 1998082800643 19980828 00643 NM 1998 8 28 MASA98135 1 19980628 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING ROUTINE INSPECTION, MAINTENANCE PERSONNEL FOUND THE LEFT FWD EMERGENCY EGRESS LIGHT NOT ILLUMINATING. REMOVED AN D REPLACED THE NR 1 EMERGENCY LIGHT POWER SUPPLY, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998082800644 19980828 00644 CE 1998 8 28 MASA98134 1 19980707 A 3230 1143880007 POWER PACK BEECH 1900 1900D 1154162 CE LT WING LEAKING A MASA K NONE O OTHER CL CLIMB 1 SW 07 144ZV 5898 UE144 FLT 5258 - LEB-LGA - ON CLIMB-OUT AT 160 KNOTS, THE CREW NOTICED THE GEAR HANDLE ILLUMINATED. THE FIRST OFFICER SAW THE RT MAIN LANDING GEAR FULLY EXTENDED. THE CREW HEARD THE HYDRAULIC POWER PACK CYCLE AND THE GEAR RETRACTED. COMPLETED FLIGHT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REPLACED THE POWER PACK. OPS CHECK GOOD, AIRRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998082800645 19980828 00645 CE 1998 8 28 98ZZZM562 1 19980713 A 7714 50389057 TACH GEN BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 860CA UE134 RIGHT N TACH INOPERATIVE. RIGHT N TACH GEN FAILED. REPLACED RT N TACH GEN. 2 L 7 2 4T RT A24CE 1998082800646 19980828 00646 CE 1998 8 28 98ZZZM563 1 19980707 A 2435 23078019 START/GEN BEECH 1900 1900D 1154162 CE LT NACELLE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 831CA 8552 92110 UE20 LT GENERATOR INOP. GENERATOR FAILURE. REPLACED LEFT START/GEN. 2 L 7 2 4T RT A24CE 1998082800647 19980828 00647 WP 1998 8 28 HALA9800242 1 19980715 A 3350 BATTERY DOUG DC9 DC951 3022051 WP TAIL CONE DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 420EA 47689 HNL - TAIL CONE EMERGENCY LIGHTS DIM. FAILED TEST. RELAMPED AND REPLACED BATTERIES, CLEANED CONTACTS. OPS CHECK OK. ( M) 2 L 7 2 4F RT A6WE 1998082800648 19980828 00648 WP 1998 8 28 HALA9800244 1 19980716 A 2910 LINE DOUG DC9 DC951 3022051 WP RT HYD SYSTEM LEAKING A HALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 699HA 47763 LIH - FLT 382 - ON TAXI NOTICED RIGHT HYD QTY GAUGE READS 0. LOST ALL RIGHT HYD FLUID ON TAXI OUT. RETURNED TO RAMP. I NSPECTED RIGHT THRUST REVERSER HYD FILTERS AND RT AUX PUMP FILTERS. CHECKED OK. REPLACED PRESSURE LINE ON AUX PUMP. GR OUND RUN OPS CHECK OK. LEAK CHECK OK, OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 1998082800649 19980828 00649 WP 1998 8 28 HALA9800220 1 19980710 A 3230 CONTROL CABLE DOUG DC9 DC951 3022051 WP MLG OUT OF ADJ A HALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 13 601AP 47658 FLT 241 - HNL - UNABLE TO RAISE LANDING GEAR HANDLE AFTER TAKEOFF. ABNORMAL PROCEDURES ADHERED TO GEAR WAS RETRACTED, N O GROUND MODE PROBLEM, FLIGHT NORMAL. ADJUSTED ANTI-RETRACTION CABLE SYSTEM PER DC-9 MM 32-31-1. OPS AND GEAR SWING CH ECK OK. (M) 2 L 7 2 4F RT A6WE 1998082800650 19980828 00650 WP 1998 8 28 98ZZZM564 1 19980720 A 5743 56114252 FITTING DOUG DC8 DC8F54 3021926 WP RT MLG CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 56FA 45663 FOUND RIGHT MAIN LANDING GEAR SUPPORT FITTING CRACKED. REMOVED AND REPLACED RIGHT MAIN GEAR FITTING PER IAW DOUGLAS DC8 MLG FITTING REPLACEMENT GUIDE AND RECOVERY AND MOD SERVICES NR CI-735. (M) 2 L 7 4 4F 4A25 1998082800651 19980828 00651 NM 1998 8 28 P2EA98127 1 19980719 A 3397 WIRE BOEING 737 737244 138448U NM CABIN BROKEN A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 620PC 19708 MCI - FLT 303 - EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH IN ARM POSITION. REPAIRED BROKEN WIRE ON EMERGENCY EXIT SWITC H IN AFT GALLEY, OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998082800652 19980828 00652 NE 1998 8 28 98ZZZM565 2 19980710 A 7261 602260005 LINE FOKKER F27 F27MK500 4990629 EU RROYCE DART DART5327R 54509 NE LT GEARBOX LOOSE A OIZA K NONE O OTHER CR CRUISE 1 WP 19 284MA 10560 14121 DURING CRUISE, LEFT GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. (M) 2 H 7 2 4T 4 T A817 E297 1998082800653 19980828 00653 NM 1998 8 28 MASA98143 1 19980715 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 DURING ROUTINE MAINTENANCE, FOUND GALLEY OVERHEAD EMERGENCY EXIT SIGN DIM. REPLACED BURNED OUT BULBS, OPS CHECK GOOD. ( M) 2 H 7 2 4T RT A13NM 1998082800654 19980828 00654 EU 1998 8 28 COEA9801729 1 19980714 A 3250 AC61906 VALVE FOKKER F27 F27MK600 4990706 EU NLG WW LEAKING A COEA K NONE O OTHER CL CLIMB 1 NM 13 729FE 10385 ON CLIMB-OUT FROM LAS, WHILE SELECTING GEAR UP CREW SAW PNEUMATIC PRESSURES ON MAIN AND BRAKE BOTTLES DROP INTO YELLOW A RC. THE CREW SELECTED GEAR DOWN AND LOCKED AND RETURNED TO LAS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE WHE EL STEERING FOLLOW UP CONTROL VALVE LEAKING. MAINTENANCE REPLACED FOLLOW UP CONTROL VALVE. PNEUMATICS WERE SERVICED, S YSTEM LEAK CHECKED GOOD. NOSE WHEEL STEERING SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 1998082800655 19980828 00655 WP 1998 8 28 AALA981165 1 19980609 A 2131 21171803 CONTROLLER DOUG DC9 DC982 3022082 WP FUSELAGE MALFUNCTIONED A AALA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 SW 07 294AA 49306 DFW - FLT 689 - EN ROUTE ORD, ELP DURING CRUISE AT 28,000 FT FLOW LIGHT ILLUMINATED. PROCEDURES WERE ACCOMP, NO HELP. C ABIN ASCENT COULD NOT BE STOPPED IN MANUAL MODE. PERFORMED EXPLOSIVE REPRESSURIZATION PROCEDURE AND DIVERTED TO DFW. PA X'S O2 MASKS DROPPED CORRECTLY. LANDED DFW WITHOUT INCIDENT. REPLACED BOTH PRESSURE CONTROLLERS AND PERFORMED REQUIRED OPERATION CHECKS. PRESSURIZED A/C USING ENGINES AND APU AND PERFORMED LEAK CHECK FOR A/C. INSPECTED OUTFLOW VALVES AN D LINKAGES AND PERFORMED FUNCTIONAL CHECK OF AUTO PACK TRIP SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998082800656 19980828 00656 WP 1998 8 28 AALA981181 1 19980615 A 2822 60324 BOOST PUMP DOUG DC9 DC982 3022082 WP FUEL TANK FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 70524 49916 RDU - FLT 470 - AFTER LEVEL OFF, EN ROUTE MIA-YUL, AT 33,000 FT THE CENTER FUEL TANK OPERATION BECAME UNRELIABLE. CENTE R TANK WOULD FEED SOMETIMES AND WINGS WOULD FEED AT OTHER TIMES. WHEN WING TANK PUMPS WERE TURNED ON, THE INLET FUEL PR ESSURE LIGHTS ILLUMINATED. AIR INTERRUPTED AND LANDED RDU WITHOUT INCIDENT. REPLACED CENTER AFT FUEL BOOST PUMP. PERF ORMED ENGINE RUN AND FUEL TRANSFER CHECK USING CENTER PUMPS AND PRESSURE SOURCE. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F A6WE 1998082800657 19980828 00657 WP 1998 8 28 AALA981185 1 19980616 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 293AA 49305 ORD - AFTER TAXI TO HANGAR THE SLIDE EMERGENCY LIGHTS WOULD NOT EXTINGUISH. REPAIRED WIRE ON EMERGENCY LIGHT PACK B5-28 . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998082800658 19980828 00658 NM 1998 8 28 AALA981193 1 19980619 A 5510 ANGLE BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - UPPER T/E CHORD ON RT HORIZ STAB HAS CORROSION APPROX 16 INCHES INBOARD OF NR 7 ELEV HINGE. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER ESO DATED 6/10/98. (M) 2 L 7 3 4F A3WE 1998082800659 19980828 00659 EU 1998 8 28 AALA981093 1 19980530 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU BS 69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND STRINGER 48L CORRODED AT FRAME 69. REMOVED AND BLENDED OUT CORROSION, TREATED AND PAINTED. REPAIRED PER SR M 53-10-14, PAGE 203/204 FIG 201. (M) 2 L 7 2 4F RT A35EU 1998082800660 19980828 00660 EU 1998 8 28 AALA981113 1 19980529 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 72-74 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND LAV V FLOOR SUPPORT BEAM ATTACH POINT AND CORRODED. REMOVED AND REPLACED LAV SUPPORT BEAM PER SRM 51-72-10- 0. (M) 2 L 7 2 4F RT A35EU 1998082800661 19980828 00661 EU 1998 8 28 AALA981112 1 19980602 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - AT FRAME 69 THE UNDERSIDE OF THE FLOOR SUPPORT IS EXFOLIATED LEFT SIDE 2ND INBOARD. REMOVED CORRODED SECTION AND REPLACED WITH NEW PIECE PER A300 SRM 51-72-10 AND 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998082800662 19980828 00662 EU 1998 8 28 AALA981096 1 19980601 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU BS 56 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND FRAME 56 TRAY SUPPORT, TOP OF FRAME EXFOLIATED. REMOVED CORROSION PER SRM 51-74-00. INSTALLED NEW SECTION OF FLOOR SUPPORT AND INSTALLED SPLICE DOUBLER PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1998082800663 19980828 00663 EU 1998 8 28 AALA981101 1 19980530 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 14-15 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CORROSION ON SEAT TRACK NR 4 JUST FORWARD OF SEAT LOCK DOWN LUGS, 6 INCHES FORWARD OF FRAME 15. REMOVED COR ROSION PER SRM 51-74-10. ALODINED, PRIMED AND INSTALLED REPAIR PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998082800664 19980828 00664 EU 1998 8 28 AALA981102 1 19980526 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1194 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CORROSION ON SEAT TRACK FLOORBOARD FLANGE AT SCREW HOLES, TRACK NR 6. REPAIRED FLANGE PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998082800665 19980828 00665 EU 1998 8 28 AALA981094 1 19980529 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND FLOOR SUPPORT UNDER ROLLER TRAY 6 CORROODED AT FRAME 58. INSTALLED NEW SECTION OF FLOOR SUPPORT PER SRM 53- 10-15-2. (M) 2 L 7 2 4F RT A35EU 1998082800666 19980828 00666 EU 1998 8 28 AALA981095 1 19980528 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND FRAME 58 INBOARD OF ROLLER TRAY 1 FLOOR SUPPORT IS EXFOLIATED. SPLICED IN NEW SECTION OF FLOOR SUPPORT PER SRM 53-10-15-2. (M) 2 L 7 2 4F RT A35EU 1998082800667 19980828 00667 EU 1998 8 28 AALA981127 1 19980603 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 71-72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT BEAM, BETWEEN FRAME 71 AND 72 IN LINE WITH SEAT TRACK NR 7. REMOVED AND INS TALLED SUPPORT BEAM PER 51-71-50-2. (M) 2 L 7 2 4F RT A35EU 1998082800668 19980828 00668 EU 1998 8 28 AALA981128 1 19980602 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU WS 538 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - L/W BOTTOM SKIN JUST OUTBOARD OF NR 1 PYLON FWD ATTACH POINT HAS HEAVY INTERGRANULAR CORROSION WITH SEVERAL RIVETS SHEARED. ROUTED OUT CORROSION AND INSTALLED FILLER AND DOUBLER PER ESO 30595 DATED 6-2-98. (M) 2 L 7 2 4F RT A35EU 1998082800669 19980828 00669 EU 1998 8 28 AALA981129 1 19980603 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 33-34 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CRACK INDICATION AT LIGHTNING STRIKES AT FRAME 33 TO 34 AT STRINGER 45. INSTALLED DOUBLER REPAIR PER SRM 53 -10-12-2. (M) 2 L 7 2 4F RT A35EU 1998082800670 19980828 00670 EU 1998 8 28 AALA981130 1 19980603 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 29-30 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CRACK INDICATED AT LIGHTNING STRIKES AT FRAMES 29 AND 30, STRINGER 44R TO 47R. INSTALLED RIVETS PER ESO 305 95 6-2-98. INSTALLED DOUBLER PER SRM 53-10-12-2. (M) 2 L 7 2 4F RT A35EU 1998082800671 19980828 00671 EU 1998 8 28 AALA981131 1 19980603 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 31-32 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CRACK INDICATIONS AT LIGHTNING STRIKES AND FRAMES 31 TO 32, STRINGER 45R TO 46R. INSTALLED DOUBLER PER SRM 53-10-12-2 AND INSTALLED RIVETS PER ESO 30595, 6-2-98. (M) 2 L 7 2 4F RT A35EU 1998082800672 19980828 00672 EU 1998 8 28 AALA981133 1 19980604 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 25 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FLOOR SUPPORT ON FRAME 25 AT NR 1 ROLLER TRAY HAS CORROSION. INSTALLED TOP CAP BEAM REPAIR PER SRM 53-10-15 FIG 2 15. (M) 2 L 7 2 4F RT A35EU 1998082800673 19980828 00673 EU 1998 8 28 AALA981148 1 19980605 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CORROSION ON STRINGER 54L AT FRAME 59. CUT OUT CORRODED SECTION OF STRINGER, INSTALLED NEW STRINGER SECTION AND SPLICES PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998082800674 19980828 00674 EU 1998 8 28 AALA981174 1 19980610 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU BS 63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CORROSION ON FRAME 63 AND DOWN ON TO STRINGER 46R. REPAIRED AS PER ESO 30595, DATED 6/8/98. (M) 2 L 7 2 4F RT A35EU 1998082800675 19980828 00675 EU 1998 8 28 98ZZZM566 1 19980610 A 5313 LONGERON AIRBUS 300 A300B4605R 3930308 EU BS 63 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CORROSION ON FRAME 63 AND DOWN ON TO STRINGER 46R. REPAIRED AS PER ESO 30595, DATED 6/8/98. (M) 2 L 7 2 4F RT A35EU 1998082800676 19980828 00676 EU 1998 8 28 AALA981111 1 19980525 A 5320 BEAM AIRBUS 300 A300B4605R 3930308 EU BS 474 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7062A 474 TUL - FOUND CORROSION ON LAV V AFT INBOARD MOUNT BEAM BORE. REPLACED MOUNT BEAM PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998082800677 19980828 00677 NM 1998 8 28 AALA981192 1 19980619 A 5510 ANGLE BOEING 727 727227 1384078 NM LT HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 718AA 20611 TUL - FOUND LEFT UPPER T/E CHORD ON LEFT HORIZ STAB HAS CORROSION APPROX 16 INCHES INBOARD OF NR 6 ELEV HINGE. CUT OUT CORRODED AREA AND INSTALLED DOUBLER PER ESO 11697, DATED 6/10/98. (M) 2 L 7 3 4F A3WE 1998082800678 19980828 00678 WP 1998 8 28 AALA981164 1 19980608 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 313-332 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 428AA 49340 TUL - FOUND DENT IN SKIN AT STATION 313-332 AND L24 LT THREE INCHES IN DIAMETER, AND .25 INCH DEEP. DENTED SKIN REPAIRE D BY INSTALLING INTERNAL DOUBLER PER SRM 53-04. (M) 2 L 7 2 4F A6WE 1998082800679 19980828 00679 WP 1998 8 28 98ZZZM567 1 19980608 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 313-332 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 428AA 49340 TUL - FOUND DENT IN LONGERON AT STATION 313-332 AND L24 LT THREE INCHES IN DIAMETER, AND .25 INCH DEEP. LONGERON SPLICE D PER SRM 53-02. (M) 2 L 7 2 4F A6WE 1998082800680 19980828 00680 EU 1998 8 28 AALA981126 1 19980603 A 5542 STRIP AIRBUS 300 A300B4605R 3930308 EU RUDDER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70073 516 TUL - FOUND SMALL AREA OF CORROSION ON RUDDER T/E LEFT SIDE APPROX TWO-THIRDS UP. REPAIRED APEX STRIP PER ESO 30595, 4- 13-98. (M) 2 L 7 2 4F RT A35EU 1998082800681 19980828 00681 EU 1998 8 28 AALA981125 1 19980603 A 5542 STRIP AIRBUS 300 A300B4605R 3930308 EU RUDDER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70073 516 TUL - FOUND SMALL AREA OF CORROSION ON RUDDER T/E ON LEFT SIDE LITTLE MORE THAN HALF WAY UP. REPAIRED APEX STRIP PER ES O 30595, 4-13-98. (M) 2 L 7 2 4F RT A35EU 1998082800682 19980828 00682 NM 1998 8 28 EISA98145 1 19980622 A 2610 FIRE LOOP BOEING 727 72725 1384006 NM NR 3 ENGINE MALFUNCTIONED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 290NE 18972 NR 3 ENGINE FIRE WARNING TEST IMPROPERLY. GENERATED FROM MAINTENANCE REPORT. REPAIRED WIRE TO NR 3 ENGINE FIRE LOOP. O PS CHECK GOOD PER MM 26-00. (M) 2 L 7 3 4F A3WE 1998082800683 19980828 00683 WP 1998 8 28 EISA98144 1 19980620 A 3350 P4010020 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 950VJ 47564 EMERGENCY SLIDE MAINTENANCE ENTRANCE LIGHT INOP, DEAD BATTERY PACK. GENERATED FROM MAINTENANCE REPORT. REMOVED AND REP LACED BATTERY PACK IAW MM CHAPTER 33-50-01. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998082800684 19980828 00684 NM 1998 8 28 EISA98149 1 19980701 A 3610 CLAMP BOEING 727 727223 1384074 NM NR 2 ENGINE LOOSE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 DFW - DURING CLIMB-OUT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, REDUCED POWER, CLOSED NR 1 ENGINE BLEED PER ABNORMAL CHEC KLIST, LIGHT EXTINGUISHED. TIGHTENED CLAMP TO DUCT. START LEAK TEST, OK FOR SERVICE IAW MM 26-14. (M) 2 L 7 3 4F A3WE 1998082800685 19980828 00685 NM 1998 8 28 EISA98150 1 19980703 A 2611 SMOKE DETECTORS BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 290NE 18972 CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT COMPLETED ABNORMAL PROCEDURE PER AOM. THE WARNING LIGHT EXTINGUISHED IN DESCENT . COULD NOT DUPLICATE MALFUNCTION, CARGO SMOKE DETECTORS. OPS CHECKED GOOD PER AERONAUTICAL MANUAL. (M) 2 L 7 3 4F A3WE 1998082800686 19980828 00686 NM 1998 8 28 EISA98146 1 19980610 A 3244 26045611 TIRE BOEING 727 7272A7 138407K NM RT MLG FAILED A EISA C ABORTED TAKEOFF D INFLIGHT SEPARATION TO TAKEOFF 1 SW 07 310NE 20241 RIGHT MAIN TIRES BLEW POSSIBLY ON TAKEOFF FROM ICT. ICT TOWER REPORTED RUBBER ON RUNWAY. REPAIRED AND REPLACED NR 3 AN D NR 4 MAIN WHEEL ASSEMBLIES IAW 32-45-1. NR 4 TIRE IS THE TIRE THAT BLEW OUT. (M) 2 L 7 3 4F A3WE 1998082800687 19980828 00687 NM 1998 8 28 EISA98143 1 19980620 A 2611 302842 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 300NE 18974 MAIN CARGO SMOKE DETECTOR INDICATOR 'CARGO SMOKE' ILLUMINATED WILL NOT EXTINGUISH. WILL NOT TEST. REPLACED NR 3 SMOKE DETECTOR, SYSTEM CHECKED NORMAL PER MM 26-10-00, REMOVED PLACARD. (M) 2 L 7 3 4F A3WE 1998082800688 19980828 00688 EU 1998 8 28 SIMA981971 1 19980716 A 3350 OL3042BPE BULB AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AE 494 ORD - FLT 4107 - REAR MOST FLOOR PROX LIGHT INOP. RAI'D BULB. PERFORMED OPERATION CHECK SATISFACTORILY AND RETURNED A/ C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800689 19980828 00689 EU 1998 8 28 SIMA981991 1 19980717 A 5320 S5367121721001 PLATE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AT 417 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT AFT OUTBOARD SEAT TRACK JUNCTION PLATE BETWEEN FRAME 35 AND 36 TO BE COR RODED. REMOVED AND REPLACED THE JUNCTION PLATE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800690 19980828 00690 EU 1998 8 28 SIMA9819810 1 19980717 A 5347 S53375001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AT 417 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT FORWARD AND AFT OUTBOARD, LEFT AND RIGHT AFT INBOARD AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800691 19980828 00691 EU 1998 8 28 98ZZZM568 1 19980717 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AT 417 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT FORWARD AND AFT OUTBOARD, LEFT AND RIGHT AFT INBOARD AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800692 19980828 00692 EU 1998 8 28 98ZZZM569 1 19980717 A 5347 S53678001226 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AT 417 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT FORWARD AND AFT OUTBOARD, LEFT AND RIGHT AFT INBOARD AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800693 19980828 00693 EU 1998 8 28 98ZZZM570 1 19980717 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AT 417 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT FORWARD AND AFT OUTBOARD, LEFT AND RIGHT AFT INBOARD AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800694 19980828 00694 EU 1998 8 28 98ZZZM571 1 19980717 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 417AT 417 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT FORWARD AND AFT OUTBOARD, LEFT AND RIGHT AFT INBOARD AND THE RIGHT MIDDLE OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800695 19980828 00695 EU 1998 8 28 SIMA982031 1 19980722 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 273AE 340B273 DFW - FLT 3652 - EMERGENCY OVERHEAD LIGHT AT SEAT 9A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB AT SEAT 9A. OPERAT IONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998082800696 19980828 00696 EU 1998 8 28 SIMA981989 1 19980717 A 3350 66363 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 382AE 340B382 DFW - FLT 3598 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROW 9/10 DO NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY L IGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998082800697 19980828 00697 EU 1998 8 28 SIMA981987 1 19980717 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AT 16021 327 GRR - CENTER SECTION OF CABIN EMERGENCY FLOOR LIGHTING DOES NOT ILLUMINATE. REMOVED AND REPLACED BATTERY FOR POWER SUPP LY 18WH. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998082800698 19980828 00698 EU 1998 8 28 SIMA982002 1 19980719 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 494AE 494 GRR - FLT 5067 - EMERGENCY LIGHTS STAY ON. REMOVED AND REPLACED BATTERY PACKS AT 73WL, 63WL, AND 61WL. OPERATIONAL CHE CK GOOD. (M) 2 H 7 2 4T RT A53EU 1998082800699 19980828 00699 EU 1998 8 28 SIMA981921 1 19980711 A 2612 89905201 CONTROL BOX SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA K NONE N FALSE WARNING AP APPROACH 1 SW 21 359SB 0439 340B359 DFW - FLT 3661 - THE RIGHT FIRE DETECT LIGHT CAME ON THREE TIMES JUST PRIOR TO LANDING. REMOVED AND REPLACED FIRE DETEC TION CONTROL BOX. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998082800700 19980828 00700 EU 1998 8 28 SIMA982001 1 19980719 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 174AE 17834 340B174 TPA - FLT 9875 - EMERGENCY LIGHTS GO OFF AFTER TEN SECONDS. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT 21LN. OPERA TIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998082800701 19980828 00701 EU 1998 8 28 REXA98106 1 19980713 A 2121 EVCTA465A RECIRC FAN SAAB SF340 340B 7860101 EU CABIN FAILED A REXA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 361PX 815 340B249 SMOKE SMELL IN CABIN. REMOVED AND REPLACED LEFT RECIRC FAN. (M) 2 L 7 2 4T RT A52EU 1998082800702 19980828 00702 EU 1998 8 28 REXA98104 1 19980701 A 2910 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG LEAKING A REXA B EMER. DESCENT K FLUID LOSS CL CLIMB 1 SO 25 344AM 340A030 ON CLIMB AFTER TAKEOFF, GEAR HANDLE WAS SELECTED UP. HYDRAULIC QTY WENT TO ZERO WITH HYDRAULIC CWP LIGHT. REMOVED AND REPLACED RT HYDRAULIC SWIVEL AND SERVICED HYD SYSTEM. (M) 2 L 7 2 4T RT A52EU 1998082800703 19980828 00703 EU 1998 8 28 PLGA980710A 1 19980710 A 2751 CIRCUIT BREAKER SAAB SF340 340B 7860101 EU FLAP INDICATOR TRIPPED A PLGA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 NE 05 358BE 340B279 BOS - FLT 4264 - WHEN FLAPS WERE SELECTED DOWN FOR LANDING AT BOS, THE CREW REPORTED THERE WAS NO FLAP INDICATION. CREW PERFORMED A MISSED APPROACH AND FOUND THE FLAP INDICATOR CIRCUIT BREAKER OPEN. THE BREAKER WAS RE-SET AND AIRCRAFT LAN DED WITHOUT INCIDENT. (M) 2 L 7 2 4T RT A52EU 1998082800704 19980828 00704 EU 1998 8 28 PLGA980610A 1 19980610 A 6120 12J63125 CLAMP SAAB SF340 340B 7860101 EU RT ENGINE LOOSE A PLGA A UNSCHED LANDING M N OVER TEMP FALSE WARNING CL CLIMB 1 NE 05 353BE 340B242 BTV - FLT 4262 - DURING CLIMB-OUT CREW NOTICED RT ITT RISING. AIRCRAFT RETURNED TO BTV WITHOUT INCIDENT. MAINTENANCE F OUND CLAMP ON HIGH PRESSURE BLEED LINE HAD COME OFF AT ENGINE BOSS. CLAMP WAS REPLACED. ALL CHECKS SATISFACTORY. AIRC RAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800705 19980828 00705 EU 1998 8 28 PLGA980612A 1 19980612 A 2612 WIRE SAAB SF340 SF340A 7850100 EU RT NACELLE BROKEN A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 344BE 340A104 LGA - FLT 4524 - DURING FLT, RIGHT ENGINE FIRE WARNING LIGHT FLICKERED. AIRCRAFT DIVERTED BACK TO LGA WITHOUT INCIDENT. MAINTENANCE REPAIRED BROKEN WIRE IN RIGHT NACELLE. ALL CHECKS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800706 19980828 00706 EU 1998 8 28 PLGA980612B 1 19980612 A 2420 51634002 AC GCU SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A PLGA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 NE 05 345BE 431 340A108 ALB - FLT 4520 - DURING FLIGHT YOW TO LGA, THE LEFT AC GENERATOR FAILED. AIRCRAFT DIVERTED TO ALB DUE TO WEATHER. MAIN TENANCE REMOVED AND REPLACED THE LEFT AC GENERATOR AND AC GCU. ALL CHECKS SATISFACTORY. AC GEN, P/N 31342-001, S/N 678 . (M) 2 L 7 2 4T RT A52EU 1998082800707 19980828 00707 EU 1998 8 28 PLGA980615A 1 19980615 A 7931 IPTE1191000200D1 TRANSDUCER SAAB SF340 340B 7860101 EU RIGHT ENGINE FLUCTUATING A PLGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 359BE 46488187 340B285 BOS - FLT 4400 - DURING FLIGHT, RIGHT ENGINE OIL PRESSURE WARNING LIGHT ON CWP ILLUMINATED INTERMITTENTLY WITH ASSOCIATE D RIGHT OIL PRESSURE INDICATOR FLUCTUATING PLUS/MINUS PSI. AIRCRAFT DIVERTED TO BOS AND LANDED WITHOUT INCIDENT. MAINT ENANCE REMOVED AND REPLACED RIGHT ENGINE PRESSURE TRANSDUCER AND PRESSURE SWITCH. ALL CHECKS SATISFACTORY. AIRCRAFT RE TURNED TO SERVICE. PRESSURE SWITCH P/N 8346-5, S/N 995WPL. (M) 2 L 7 2 4T RT A52EU 1998082800708 19980828 00708 EU 1998 8 28 PLGA980616A 1 19980616 A 2121 C209690C FAN SAAB SF340 SF340A 7850100 EU CABIN FAILED A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NE 05 341BE 31595 340A063 HPN - FLT 4235 - DURING CLIMB-OUT OF HPN CREW REPORTED STRONG ELECTRICAL SMELL IN CABIN. AIRCRAFT DIVERTED TO HPN AND L ANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT RECIRC FAN BURNED OUT. FAN WAS DEFERRED PER MEL 21-20-1. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800709 19980828 00709 EU 1998 8 28 PLGA980619A 1 19980619 A 2730 7239056504 HANDLE SAAB SF340 SF340A 7850100 EU COCKPIT SEIZED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 340BE 340A062 BGR - DURING HEAVY MAINTENANCE INSPECTION, AN OPERATION TEST OF THE PITCH DISCONNECT SYSTEM WAS BEING PERFORMED. DURING THIS TEST THE PITCH DISCONNECT HANDLE WOULD NOT PULL OUT. MAINTENANCE REMOVED AND REPLACED ASSY PER MM. OPERATIONAL C HECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998082800710 19980828 00710 EU 1998 8 28 PLGA980620A 1 19980620 A 2421 31342001 AC GENERATOR SAAB SF340 340B 7860101 EU LT ENGINE FAILED A PLGA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 NE 05 347BE 704 340B187 BOS - FLT 4253 - DURING CLIMB-OUT, THE LEFT AC GENERATOR FAILED. AIRCRAFT RETURNED TO BOS. MAINTENANCE REPLACED LEFT A C GENERATOR. ALL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800711 19980828 00711 EU 1998 8 28 PLGA980621A 1 19980621 A 2910 AE7064588 HYD LINE SAAB SF340 340B 7860101 EU NLG LEAKING A PLGA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NE 05 358BE 340B279 PVD - FLT 4573 - AFTER TAKEOFF WHEN LANDING GEAR WAS SELECTED UP, HYDRAULIC PUMP RAN CONTINUOUSLY AND HYDRAULIC FLUID QT Y DECREASED. CREW SELECTED GEAR DOWN AND DIVERTED TO PVD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NLG RET RACT ACTUATOR UP LINE AND SERVICED HYDRAULIC SYSTEM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800712 19980828 00712 EU 1998 8 28 PLGA980625A 1 19980625 A 7722 4078T09P02 T4.5 TRIMMER SAAB SF340 340B 7860101 EU LT ENGINE FAILED A PLGA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 NE 05 357BE GDB00694 340B277 BOS - FLT 4252 - CREW NOTICED LEFT ENGINE TEMPS HIGHER THAN RIGHT, BUT NOT OUT OF LIMITS. CREW REDUCED POWER TO MATCH T EMPS AND LEFT ENGINE DID NOT MAKE CHARTED TORQUE. AIRCRAFT RETURNED TO BOS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLA CED THE T4.5 TRIMMER IAW GE MM. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800713 19980828 00713 NM 1998 8 28 P2EA98129 1 19980711 A 5754 SLAT BOEING 737 737247 138448D NM WS 373 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - LEFT WING NR 1 SLAT LEADING EDGE DENTED AT SS 373. REPAIRED NR 1 SLAT SKIN SECTION BETWEEN SS 373 AND SS 382 PER SRM 57-50-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998082800714 19980828 00714 NM 1998 8 28 P2EA98128 1 19980724 A 5230 FRAME BOEING 737 737247 138448D NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FORWARD CARGO DOOR BEAM NR 5 CRACKED IN AFT SECTION DEFECT SIZE L=1.375 INCH. REPAIRED FORWARD CARGO DOOR BEAM NR 5 PER BOEING SERVICE BULLETIN 737-52-1100 REV 2 DATED MARCH 31, 1994, SECTION 111, PAR 'C' FIG 6, DETAIL II. (M) 2 L 7 2 4F A16WE 1998082800715 19980828 00715 WP 1998 8 28 ORJA98124 1 19980621 A 3350 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 ROA 20B EMERGENCY RED LIGHT INOP. FOUND LOOSE WIRE AT 20B EMERGENCY LIGHT. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 1998082800716 19980828 00716 WP 1998 8 28 ORJA98159 1 19980708 A 3350 59306431 BATTERIES DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 LAST THREE ROWS AND AFT DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998082800717 19980828 00717 WP 1998 8 28 ORJA98160 1 19980711 A 3350 6011779 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 LOWER AFT RIGHT OVERWING EMERGENCY EXIT LAMP INOP. REMOVED AND REPLACED BATTERY LIGHT POWER PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998082800718 19980828 00718 WP 1998 8 28 ORJA98161 1 19980711 A 3350 59306431 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 EMERGENCY EVACUATION FLOOR LIGHTING (ON SEATS) INOPERABLE, ROWS 21-24. INSPECTED AIRCRAFT FOR A ONE TIME FERRY PERMIT F OR FURTHER TROUBLESHOOTING OF EMERGENCY LIGHT SYSTEM. REF; LOG PAGE 165764. EMERGENCY EVACUATION FLOOR LIGHTING (ON SE ATS) INOP ROWS 21-24. REMOVED AND REPLACED BATTERIES. (M) 2 L 7 2 4F RT A6WE 1998082800719 19980828 00719 WP 1998 8 28 ORJA98162 1 19980712 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 EMERGENCY EXIT ROW LIGHTING AT EMERGENCY EXIT DOOR INOPERABLE. REMOVED AND REPLACED SEAT LIGHTING POWER SUPPLY. OPS CH ECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998082800720 19980828 00720 WP 1998 8 28 ORJA98164 1 19980714 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 OVERHEAD EMERGENCY LIGHTS OUT BY EMERGENCY EXIT. REPLACED BATTERY PACK IN OVERHEAD BIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998082800721 19980828 00721 WP 1998 8 28 ORJA98163 1 19980711 A 3350 59306431 BATTERY DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY EXIT LIGHTS INOPERABLE AT ROWS 9-14 AND 21-25. REMOVED AND REPLACED EMERGENCY BATTERIES. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998082800722 19980828 00722 WP 1998 8 28 ORJA98165 1 19980714 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 EMPENNAGE EMERGENCY LIGHTS OUT. REMOVED AND REPLACED BULBS. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998082800723 19980828 00723 WP 1998 8 28 ORJA98166 1 19980704 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 ROW 2C EMERGENCY PATH LIGHT INOPERABLE. FOUND BROKEN WIRE. REPAIRED WIRE. OPS CHECK GOOD. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A6WE 1998082800724 19980828 00724 WP 1998 8 28 ORJA98167 1 19980701 A 3350 LIGHT DOUG DC9 DC987 3022087 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 ROW 9 EMERGENCY FLOOR TRACK LIGHT INOPERABLE. REPAIRED BROKEN WIRES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998082800725 19980828 00725 WP 1998 8 28 ORJA98170 1 19980718 A 2760 ANNUNCIATOR DOUG DC9 DC983 3022083 WP TE FLAP MALFUNCTIONED A ORJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 834RA 53124 ABORTED TAKEOFF DUE TO SPOILED FLAP EXT ANNUNCIATOR CAME ON DURING TAKEOFF ROLL AT ABOUT 90 KTS. SYSTEM OPERATIONS CHEC K WAS NORMAL PER MM 27-60-00. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 1998082800726 19980828 00726 WP 1998 8 28 ORJA98171 1 19980719 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERABLE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 EMERGENCY WHITE LIGHTS INOP AT ROWS 18 AND 20. FOUND BAD WIRE, SECURED. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 1998082800727 19980828 00727 WP 1998 8 28 ORJA98172 1 19980721 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 EMERGENCY EXIT LIGHTS INOP IN SEATS 17-20. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD PER MM. ( M) 2 L 7 2 4F A6WE 1998082800728 19980828 00728 1998 8 28 G60A025 4 19980717 A 2565 119821003 SENSOR DOUG DC10 DC1030F 3023504 WP SLIDE FAILED A G6OA K NONE L NO TEST IN INSP/MAINT 1 EA 27 600GC 46965 THE L1 DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS TO TEST SWITCH WAS INOPERATIVE. THIS WAS DEFERRED IAW MEL 25-24. GR OUND MAINTENANCE REMOVED AND REPLACED THE PRESSURE SENSE ASSY IAW MM 25-60-03. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F RT A22WE 1998082800729 19980828 00729 NM 1998 8 28 USAA980312 1 19980714 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 927 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 927 STRINGER 9R TIE CLIP. INSTALLED PART PER S RM 51-40 AND EO 5393G227. (M) 2 L 7 2 4F A16WE 1998082800730 19980828 00730 NM 1998 8 28 USAA980311 1 19980714 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727, STRINGER 4L TIE CLIP. INSTALLED PART PER SRM 51-40 AND EO 5393G227. (M) 2 L 7 2 4F A16WE 1998082800731 19980828 00731 NM 1998 8 28 USAA980310 1 19980714 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 2R TIE CLIP. INSTALLED PART PER S RM 51-40 AND EO 5393G227. (M) 2 L 7 2 4F A16WE 1998082800732 19980828 00732 NM 1998 8 28 USAA980309 1 19980714 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 787 STRINGER 10R TIE CLIP. INSTALLED PART PER SRM 51-40 AND EO 5393G227. (M) 2 L 7 2 4F A16WE 1998082800733 19980828 00733 NM 1998 8 28 USAA980308 1 19980714 A 5315 6545808171 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 VISUAL INSPECTION, FOUND A 1 INCH BY 10 INCH AREA OF CORROSION AT STATION 294 LBBL 12 FLOORBEAM 'T' CAP CHORD. CORROSION TASK CARD NR C53-202-02. FABRICATED NEW 'T' CAP, DOUBLER AND STRAPS AND INSTALLED PER TYPICAL REPAIR NR 53-10-04B. (M) 2 L 7 2 4F A16WE 1998082800734 19980828 00734 NM 1998 8 28 USAA980307 1 19980714 A 5320 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .025 INCH CRACK AT STATION 727A STRINGER 7L TIE CLIP. REPLACED CLIP P ER EO 5393G227 9AD 93-08-04, SB 737-53-1085. (M) 2 L 7 2 4F A16WE 1998082800735 19980828 00735 NM 1998 8 28 USAA980306 1 19980714 A 5320 6935352505 CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .075 INCH CRACK AT STATION 616 AND STRINGER 4R TIE CLIP. REPLACED CLI P PER EO 5393G227 (AD 93-08-04, SB 737-53-1085). (M) 2 L 7 2 4F A16WE 1998082800736 19980828 00736 NM 1998 8 28 USAA980305 1 19980714 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 271AU 42781 22883 CLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .075 INCH CRACK AT STATION 639 AND STRINGER 1L FRAME TIE CLIP. REPLAC ED CLIP PER EO 5393G227 9AD 93-08-04, SB 737-53-1085). (M) 2 L 7 2 4F A16WE 1998082800737 19980828 00737 EU 1998 8 28 USAAF98062 1 19980726 A 3241 60042725 CONTROL BOX FOKKER F28 F28MK0100 4990807 EU E/E BAY FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 887US 16791 11349 CLT - FLT 476 - AFTER TAKEOFF FROM CLT, WHEN LANDING GEAR WAS RETRACTED, 'ANTI-SKID' FAULT MESSAGE APPEARED. FLIGHT RET UREND TO CLT. MESSAGE REMAINED ON UNTIL LANDING GEAR WAS EXTENDED THEN MESSAGE EXTINGUISHED. FLIGHT LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE REPLACED THE ANTI-SKID CONTROL BOX. (M) 2 L 7 2 4F RT 1998082800738 19980828 00738 NM 1998 8 28 USAA980323 1 19980730 A 5313 BAC1506626 STRINGER BOEING 737 737301 1384611 NM BS 1100 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 32422 23553 CLT - DURING A PILOTS REPORT READING INSPECTION, FOUND A 1 INCH BY 1 INCH WARP AREA STRINGER STATION 1100. REPLACED WIT H IDENTICAL PART PER BAC DRAWING 65-46579. (M) 2 L 7 2 4F RT A16WE 1998082800739 19980828 00739 NM 1998 8 28 USAA980324 1 19980730 A 5313 BAC1506626 STRINGER BOEING 737 737301 1384611 NM BS 1100 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 32422 23553 CLT - DURING DROP IN CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH WARPED AREA HEAT DAMAGE STATION 1100 APU TORQUE B OX STRINGER. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1998082800740 19980828 00740 NM 1998 8 28 USAA980325 1 19980730 A 5313 BAC1506626 STRINGER BOEING 737 737301 1384611 NM BS 1113-1123 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 32422 23553 CLT - DURING A PILOTS REPORT READING VISUAL INSPECTION, FOUND A 1 INCH BY .5 INCH CORROSION AREA STATION 1113 AND STATIO N 1123 RIGHT SIDE TORQUE BOX STRINGER. REPLACED WITH IDENTICAL PART PER SRM 51-40-02 AND BAC DRAWING 6546579. (M) 2 L 7 2 4F RT A16WE 1998082800741 19980828 00741 NM 1998 8 28 USAA980263 1 19980711 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 36873 23315 CLT - DURING CX-5 CHECK VISUAL AND EDDY CURRENT, FOUND A 1.625 INCH CRACK IN SKIN STATION 380 BL 3L EQUIP COOLING DUCT O UTLET CUTOUT. INSTALLED DOUBLER PER T/R 53-30-04 AND EA 62079A. (M) 2 L 7 2 4F RT A16WE 1998082800742 19980828 00742 NM 1998 8 28 USAASB98186 1 19980717 A 2120 65553473 CHECK VALVE BOEING 737 7373B7 1384580 NM CABIN AIR LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 391US 23313 PIT - FLT 1665 - AFTER TAKEOFF FROM PIT, AIRCRAFT WOULD NOT PRESSURIZE IN AUTO, STANDBY OR MANUAL AC. OUTFLOW VALVE IND ICATED CLOSED. CREW WENT THROUGH PROCEDURES AND ADVISED TOWER THAT THEY WERE RETURNING TO FIELD TO PIT. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CONDITIONED AIR HOOKUP DUCT CHECK VA LVE ASSY. OPERATIONAL CHECK GOOD. WORK ACCOMPLISHED PER MM 21-21-12. (M) 2 L 7 2 4F RT A16WE 1998082800743 19980828 00743 NM 1998 8 28 USAASB98197 1 19980727 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 783AU 25022 IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE AFT LEFT ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998082800744 19980828 00744 NM 1998 8 28 USAASB98198 1 19980727 A 3350 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 393US 23315 PIT - DURING TRANSIT CHECK, MAINTENANCE FOUND TWO ADJACENT FLOOR TRACK EMERGENCY LIGHTS INOP. MAINTENANCE REPAIRED BROK EN WIRES AT WIRE SPLICES FOR BOTH LOCATIONS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998082800745 19980828 00745 NM 1998 8 28 USAASB98191 1 19980725 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 519AU 23705 SYR - FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER AND BATTERY PAC K. (M) 2 L 7 2 4F RT A16WE 1998082800746 19980828 00746 NM 1998 8 28 USAASB98190 1 19980725 A 3350 MS24266R16B24SN CONNECTOR BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 519AU 23705 SYR - FOUND AFT SECTIN OF FLOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPAIRED WIRING AND REPLACED A CANNON PLUG ON THE AFT SECTION OF THE TRACK LIGHTING. (M) 2 L 7 2 4F RT A16WE 1998082800747 19980828 00747 NM 1998 8 28 USAABB98076 1 19980726 A 3350 20121 BATTERY CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 646US 23898 CDG - FOUND EMERGENCY LIGHTS AT R2 DOOR INOPERATIVE. MAINTENANCE SWAPPED THE M1209 POWER SUPPLY WITH THE M738 POWER SUP PLY (EXTERIOR LIGHTS, LEFT SIDE) AND RESTRICTED THE AIRCRAFT TO DAYLIGHT OPERATIONS. THE M738 MODULE WAS SUBSEQUENTLY R EPLACED IN PHL. (M) 2 L 7 2 4F RT A1NM 1998082800748 19980828 00748 NM 1998 8 28 USAABB98078 1 19980729 A 3350 20121 BATTERY CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 650US 23902 CDG - FOUND LEFT AND RIGHT FORWARD EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE SWAPPED THE M1208 MODULE (INTERIOR LIGHTS) WITH THE M738 MODULE (EXTERIOR LIGHTS) AND RESTRICTED THE AIRCRAFT TO DAYLIGHT OPERATIONS. THE M738 MODULE WAS SUBSEQU ENTLY REPLACED THE PHL. (M) 2 L 7 2 4F RT A1NM 1998082800749 19980828 00749 NM 1998 8 28 USAABB98081 1 19980818 A 3350 8731002511REV9 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 BOS - R4 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998082800750 19980828 00750 WP 1998 8 28 USAAD98125 1 19980717 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 814US 48094 PHL - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERY PACKS . (M) 2 L 7 2 4F A6WE 1998082800751 19980828 00751 WP 1998 8 28 USAAD98124 1 19980707 A 3350 110049 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 977VJ 48155 DAY - THE AFT SECTION OF THE FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR TRACK LIGHTING PO WER SUPPLY AND THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998082800752 19980828 00752 WP 1998 8 28 98ZZZM572 1 19980707 A 3350 20131ALP POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 977VJ 48155 DAY - THE AFT SECTION OF THE FLOOR TRACK LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR TRACK LIGHTING PO WER SUPPLY AND THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998082800753 19980828 00753 NM 1998 8 28 USAASB98200 1 19980728 A 3350 1012623 LIGHT BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 274US 22886 PHL - WHILE TESTING EMERGENCY LIGHT SYSTEM, MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 9A WITHOUT A LENSE AND SMOKING. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 9A. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998082800754 19980828 00754 NM 1998 8 28 USAABB98077 1 19980715 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED ALL ASSOCIATED BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998082800755 19980828 00755 NM 1998 8 28 USAABB98080 1 19980721 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 614AU 27145 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 23. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998082800756 19980828 00756 WP 1998 8 28 USAAD98126 1 19980718 A 3350 14597101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 PIT - THE EMERGENCY LIGHTS AT ROW 25 AND THE AFT TAIL COMPARTMENT LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EME RGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998082800757 19980828 00757 WP 1998 8 28 USAAD98131 1 19980731 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816US 48096 LGA - THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND POWER SUPPLY FOR THE FORWA RD ENTRY AND FIRST CLASS CEILING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998082800758 19980828 00758 WP 1998 8 28 98ZZZM573 1 19980731 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816US 48096 LGA - THE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES AND POWER SUPPLY FOR THE FORWA RD ENTRY AND FIRST CLASS CEILING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998082800759 19980828 00759 WP 1998 8 28 USAAD98127 1 19980720 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919VJ 48139 PIT - THE FLOOR LEVEL EMERGENCY LIGHTS ROW 16 THROUGH ROW 21 AND THE CEILING EMERGENCY LIGHTS ROW 9 THROUGH ROW 12 WERE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN BUTT SPLICE FOR THE FLOOR LEVEL EMERGENCY LIGHTS AND REPLACED FLOOR LEVEL AN D CEILING EMERGENCY BATTERIES. (M) 2 L 7 2 4F A6WE 1998082800760 19980828 00760 EU 1998 8 28 USAAF98063 1 19980730 A 2900 HYDRAULIC SYSTEM FOKKER F28 F28MK0100 4990807 EU HORIZONTAL STAB FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 882US 11334 CLT - FLT 281 - ON CLIMB-OUT FROM CLT, SYSTEM 1 HORIZONTAL STABILIZER HYDRAULICS FAILED. SEVERAL MINUTES LATER, SYSTEM 2 HORIZONTAL STABILIZER HYDRAULICS FAILED. FLIGHT RETURNED TO CLT WITHOUT DECLARING AN EMERGENCY AND LANDED WITHOUT FUR THER INCIDENT. MAINTENANCE ACTION PENDING. (X) 2 L 7 2 4F RT 1998082800761 19980828 00761 NM 1998 8 28 TSAA9833436 1 19980728 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED BATTERY PACK FOR NR 2 POSITION FLOOR LIGHT ASSY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1998082800762 19980828 00762 NM 1998 8 28 TSAA9833435 1 19980725 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECK OK. AIRCRAFT RETURN ED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082800763 19980828 00763 NM 1998 8 28 TSAA9833434 1 19980723 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 FORWARD ENTRY EXIT IDENTIFIER INOP ON TEST. REPLACED EXIT IDENTIFIER. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998082800764 19980828 00764 NM 1998 8 28 TSAA9833433 1 19980722 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY AT NR 6 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F A16WE 1998082800765 19980828 00765 NM 1998 8 28 TSAA9833432 1 19980717 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECKED OK. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082800766 19980828 00766 NM 1998 8 28 TSAA9833431 1 19980717 A 3350 1000679 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED BATTERY PACK ON RIGHT SIDE FORWARD EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1998082800767 19980828 00767 NM 1998 8 28 TSAA9833430 1 19980717 A 3350 100679 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED BATTERY PACK ON LEFT SIDE FORWARD EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1998082800768 19980828 00768 NM 1998 8 28 TSAA9833429 1 19980717 A 3350 6013211 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 RIGHT FORWARD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4U RT A16WE 1998082800769 19980828 00769 NM 1998 8 28 TSAA9833428 1 19980717 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082800770 19980828 00770 NM 1998 8 28 TSAA9833427 1 19980717 A 3350 873100151 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 SEAT EMERGENCY LIGHT ASSEMBLY DUE TO NOT RECEIVING TRANSMITTING SIGNAL. OPS CHECKED OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082800771 19980828 00771 NM 1998 8 28 TAOA079815 1 19980731 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 20415 FLT 6530 - DCA-LGA - RIGHT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER AND BATTERY PAC K, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998082800772 19980828 00772 NM 1998 8 28 TSAA9833426 1 19980717 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 5 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998082800773 19980828 00773 EU 1998 8 28 SIMA982096 1 19980728 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 TO BE CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800774 19980828 00774 EU 1998 8 28 98ZZZM574 1 19980728 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 TO BE CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800775 19980828 00775 EU 1998 8 28 98ZZZM575 1 19980728 A 5315 S53676208202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 TO BE CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800776 19980828 00776 EU 1998 8 28 SIMA982095 1 19980728 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT AFT OUTBOARD, THE RIGHT AFT INBOARD AND THE RIGHT FORWARD OUTBO ARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800777 19980828 00777 EU 1998 8 28 98ZZZM576 1 19980728 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT AFT OUTBOARD, THE RIGHT AFT INBOARD AND THE RIGHT FORWARD OUTBO ARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800778 19980828 00778 EU 1998 8 28 98ZZZM577 1 19980728 A 5347 S53678001246 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT AFT OUTBOARD, THE RIGHT AFT INBOARD AND THE RIGHT FORWARD OUTBO ARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800779 19980828 00779 EU 1998 8 28 98ZZZM578 1 19980728 A 5347 S53375001200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT AFT OUTBOARD, THE RIGHT AFT INBOARD AND THE RIGHT FORWARD OUTBO ARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800780 19980828 00780 EU 1998 8 28 SIMA982097 1 19980728 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURNG CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FLIGHT ATTENDANT, LEFT AND RIGHT MIDDLE OUTBOARD, THE RIGHT MIDD LE INBOARD, AND THE LEFT FORWARD INBOARD AND OUTBOARD SEAT TRACKS GOUGED AT FEET ATTACH POINT. REMOVED AND REPLACED SEA T TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800781 19980828 00781 EU 1998 8 28 98ZZZM579 1 19980728 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURNG CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FLIGHT ATTENDANT, LEFT AND RIGHT MIDDLE OUTBOARD, THE RIGHT MIDD LE INBOARD, AND THE LEFT FORWARD INBOARD AND OUTBOARD SEAT TRACKS GOUGED AT FEET ATTACH POINT. REMOVED AND REPLACED SEA T TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800782 19980828 00782 EU 1998 8 28 98ZZZM580 1 19980728 A 5347 S53575001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURNG CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FLIGHT ATTENDANT, LEFT AND RIGHT MIDDLE OUTBOARD, THE RIGHT MIDD LE INBOARD, AND THE LEFT FORWARD INBOARD AND OUTBOARD SEAT TRACKS GOUGED AT FEET ATTACH POINT. REMOVED AND REPLACED SEA T TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800783 19980828 00783 EU 1998 8 28 98ZZZM581 1 19980728 A 5347 S53375001214 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURNG CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FLIGHT ATTENDANT, LEFT AND RIGHT MIDDLE OUTBOARD, THE RIGHT MIDD LE INBOARD, AND THE LEFT FORWARD INBOARD AND OUTBOARD SEAT TRACKS GOUGED AT FEET ATTACH POINT. REMOVED AND REPLACED SEA T TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800784 19980828 00784 EU 1998 8 28 98ZZZM582 1 19980728 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURNG CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FLIGHT ATTENDANT, LEFT AND RIGHT MIDDLE OUTBOARD, THE RIGHT MIDD LE INBOARD, AND THE LEFT FORWARD INBOARD AND OUTBOARD SEAT TRACKS GOUGED AT FEET ATTACH POINT. REMOVED AND REPLACED SEA T TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800785 19980828 00785 EU 1998 8 28 98ZZZM583 1 19980728 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURNG CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FLIGHT ATTENDANT, LEFT AND RIGHT MIDDLE OUTBOARD, THE RIGHT MIDD LE INBOARD, AND THE LEFT FORWARD INBOARD AND OUTBOARD SEAT TRACKS GOUGED AT FEET ATTACH POINT. REMOVED AND REPLACED SEA T TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800786 19980828 00786 EU 1998 8 28 98ZZZM584 1 19980728 A 5347 S53570201202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURNG CPCP-4 INSPECTION, FOUND THE LEFT AND RIGHT FLIGHT ATTENDANT, LEFT AND RIGHT MIDDLE OUTBOARD, THE RIGHT MIDD LE INBOARD, AND THE LEFT FORWARD INBOARD AND OUTBOARD SEAT TRACKS GOUGED AT FEET ATTACH POINT. REMOVED AND REPLACED SEA T TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998082800787 19980828 00787 EU 1998 8 28 SIMA982093 1 19980728 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 209AT 11724 0209 SAW - DURING PS-2 INSPECTION, THE AFT EMERGENCY EXIT SIGN AND AFT FLOOR PROXIMITY LIGHTS DID NOT ILLUMINATE. REMOVED AN D REPLACED THE EMERGENCY LIGHT BATTERY PACK AT 18WL. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998082800788 19980828 00788 NE 1998 8 28 SIMA981823 2 19980701 A 7210 GEARBOX AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENGINE DAMAGED A SIMA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SW 21 260AE 263 127100 HRL - FLT 3724 - AFTER TAKEOFF, CREW SELECTED 'CLIMB' ON POWER MGMNT PANEL AND BEGAN TO BRING CONDITION LEVERS BACK TO 8 6 PERCENT NP WHEN THE NR 1 ENGINE BEGAN TO SURGE, THEN TORQUE WENT TO ZERO. NP STABILIZED AT 30 PERCENT AND NH AT 45 PE RCENT. SHUT DOWN THE ENGINE AS PRECAUTIONARY MEASURE. A/C RETURNED TO FIELD. PAX DEPLANED NORMALLY. REMOVED AND REPL ACED NR 1 ENGINE ASSY. EXTENSIVE DAMAGE TO VARIOUS RGB COMPONENTS. THIS MIGHT HAVE BEEN CAUSED BY AC GENERATOR FAILURE , WHEREBY THE DRIVESHAFT DID NOT SHEAR AND IT CAUSED SUDDEN RGB STOPPAGE AND SUBSEQUENT COMPONENT DAMAGE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998082800789 19980828 00789 NM 1998 8 28 PCAA9800777 1 19980721 A 3230 841005 PSEU DHAV DHC8 DHC8102 2809003 NM MLG FAILED A PCAA O OTHER J WARNING INDICATION CR CRUISE 1 EA 13 838EX 220 FLT 3842 - DURING CRUISE, LANDING GEAR BEGAN AN UNSELECTED EXTENSION. DOORS OPENED THEN CLOSED. GEAR HANDLE INTRANSIT LIGHT AND AMBER GEAR DOOR OPEN LIGHTS ILLUMINATED MOMENTARILY. LANDING GEAR REMAINED UP, DID NOT EXTEND. PERFORMED PRO XIMITY SWITCH ELECTRONICS UNIT TEST AND INSPECTED WIRING. NO FAULTS FOUND. PERFORMED NUMEROUS RETRACT AND EXTENSION CY CLES. COULD NOT DUPLICATE. REPLACED PSEU AND LANDING GEAR CONTROL HANDLE AS PRECAUTIONARY MEASURE. A/C RETURNED TO SE RVICE. (M) 2 H 7 2 4T RT A13NM 1998082800790 19980828 00790 EU 1998 8 28 PLGA980729A 1 19980729 A 7540 51533172 SENSOR SAAB SF340 340B 7860101 EU RT NACELLE MALFUNCTIONED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NE 05 348BE 340B190 MNT - FLT 4400 - WHILE IN FLIGHT, THE RIGHT ENGINE BLEED AIR LEAK LIGHT ILLUMINATED. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT DIVERTED TO MNT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT NACELLE AND WING ROOT LEAK SENSOR AT FAULT CAUSING A FALSE WARNING. THE LEAK SENSOR LOOP WAS REPLACED. SYSTEM TESTED GOOD AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998082800791 19980828 00791 NM 1998 8 28 P2EA98136 1 19980714 A 5312 BULKHEAD BOEING 737 737247 138448D NM BS 294 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FUSELAGE BULKHEAD WEB CRACKED AT BS 294.5, LBL 16 INCHES, WL 165 (E/E COMPT). REPAIRED WEB AT BS 294.5, LBL 13 TO LBL 18, BETWEEN WL 170 AND WL 160 PER BOEING FAX COO-SJO-98-0491RR DATED JULY 21, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1998082800792 19980828 00792 NM 1998 8 28 P2EA98137 1 19980713 A 5330 SKIN BOEING 737 737247 138448D NM BS 380 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FUSELAGE SKIN DENTED AT BS 380 BETWEEN STRINGER 17 LT AND STRINGER 18 LT. DEFECT SIZE LENGTH 4 INCHES WIDTH 2 INC HES. REPAIRED FUSELAGE SKIN SECTION BS 376 AND BS 387, BETWEEN STRINGER 17 LT AND 19 LT PER SRM 53-30-3 FIG 17 DETAIL V . (M) 2 L 7 2 4F A16WE 1998082800793 19980828 00793 NM 1998 8 28 P2EA98135 1 19980711 A 5210 SKIN BOEING 737 737247 138448D NM PAX DOOR DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - MAIN ENTRY DOOR (L1) OUTER SKIN BETWEEN BEAM 4 AND BEAM 5 OIL CANNED. REPAIRED MAIN ENTRY DOOR SKIN SECTION BETWE EN BEAM 4 AND BEAM 5 PER SRM 52-00-3 FIG 6 SHEET 1 OF 2. (M) 2 L 7 2 4F A16WE 1998082800794 19980828 00794 NM 1998 8 28 P2EA98134 1 19980711 A 5320 SPLICE BOEING 737 737247 138448D NM BS 1016 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - FUSELAGE FRAME SPLICE SECTION CORRODED BEYOND LIMITS AT BS 1016, BETWEEN STRINGER 25RT AND STRINGER 25LT. REPAIRE D FUSELAGE FRAME SPLICE SECTION AT BS 1016, BETWEEN STRINGER 25 RT AND 25 LT PER SRM 51-10-5, PAGE 5 AND SRM 51-30-2. ( M) 2 L 7 2 4F A16WE 1998082800795 19980828 00795 WP 1998 8 28 ORJA98177 1 19980618 A 5320 WEB DOUG DC9 DC983 3022083 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 881RA 49941 LEVEL 3 CORROSION, CUSP WEB CORRODED RIGHT STATION 1200 JUST AFT OF AFT CARGO DOOR. REMOVED CORRODED CUSP WEB RIGHT STA TION 117 TO 1174 AND FABRICATED NEW CUSP WEB AND INSTALLED IAW DC-9 SRM 51-30-2 AND ACTION NR 372194. FILE NR 98-06-19- 022. (M) 2 L 7 2 4F RT A6WE 1998082800796 19980828 00796 WP 1998 8 28 ORJA98181 1 19980720 A 3240 26088911 BRAKE DOUG DC9 DC982 3022082 WP NR 4 FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 821RA 49931 AT SNA, NR 4 BRAKE MALFUNCTION OCCURRED, CAUSING A RETURN TO GATE. REMOVED AND REPLACED WHEEL BRAKE ASSY AS PER MM 32-4 2-01, CHECKS OK. (M) 2 L 7 2 4F A6WE 1998082800797 19980828 00797 WP 1998 8 28 ORJA98178 1 19980720 A 3242 26088921 BRAKE DOUG DC9 DC982 3022082 WP NR 4 FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 821RA 49931 AT SNA, NR 4 BRAKE MALFUNCTION, REQUIRING A RETURN TO GATE. REMOVED AND REPLACED WHEEL BRAKE ASSEMBLY AS PER MM 32-42-0 1. CHECKS OK. (M) 2 L 7 2 4F A6WE 1998082800798 19980828 00798 WP 1998 8 28 ORJA98180 1 19980725 A 3350 EM1267 BATTERIES DOUG DC9 DC982 3022082 WP SEATS 17-14 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 AT RENO, EMERGENCY LIGHTS AT SEATS 17 THROUGH 24 WERE INOPERABLE. REMOVED AND REPLACED BAD BATTERIES. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998082800799 19980828 00799 WP 1998 8 28 ORJA98179 1 19980725 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 880RA 53186 AT RNO, EMERGENCY EXIT LIGHTS AT SEATS 12 THROUGH 16 (RT) WERE INOPERABLE. REPLACED EMERGENCY EXIT BATTERY CHARGER AT S EAT 20A. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998082800800 19980828 00800 NM 1998 8 28 98ZZZM585 1 19980805 A 2612 356644400 FIRE LOOP BOEING 727 727231 1384079 NM MLG WW MALFUNCTIONED A MYWA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 808MA 21988 PASSING THROUGH FL190 ON TAKEOFF WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCED URES. FIRE WARNING LIGHT EXTINGUISHED WITH GEAR EXTENSION. IN MIA REMOVED AND REPLACED LEFT AND RIGHT WHEEL WELL FIRE WARNING SENSOR LOOPS IAW 26-12-1. OPS CHECK OK. CLEANED AND RESEATED NOSE WHEEL WELL SENSOR LOOP. OPS CHECK OK IAW 26 -11. (M) 2 L 7 3 4F A3WE 1998082800801 19980828 00801 NM 1998 8 28 98ZZZM586 1 19980802 A 2612 FIRE LOOP BOEING 727 727231 1384079 NM MLG WW MALFUNCTIONED A MYWA O OTHER N FALSE WARNING CL CLIMB 1 SO 19 808MA 21988 PASSING THROUGH FL190 WHEEL WELL FIRE WARNING LIGHT ILLUMINATED. FOLLOWED COMPANY EMERGENCY CHECKLIST PROCEDURES. FIRE WARNING LIGHT EXTINGUISHED WITH GEAR EXTENSION. ON ARRIVAL PERFORMED VISUAL INSPECTION OF DETECTOR LOOPS, SENSORS, WHE EL WELL AND LANDING GEAR AREA. NO DAMAGE OR FAULT FOUND. PERFORMED WHEEL WELL FIRE DETECTION ADJUSTMENT TEST IAW MM 26 -12-00. (M) 2 L 7 3 4F A3WE 1998082800802 19980828 00802 CE 1998 8 28 98ZZZM587 1 19980724 A 3260 90422912 ANNUNCIATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 843CA UE43 NOSE GEAR LIGHT INOPERATIVE. DEFECTIVE LANDING GEAR ANNUNCIATOR. REPLACED LANDING GEAR ANNUNCIATOR. (M) 2 L 7 2 4T RT A24CE 1998082800803 19980828 00803 1998 8 28 98ZZZM588 4 19980729 A 3442 6228439003 RADAR BEECH 1900 1900D 1154162 CE E/E COMPT FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 833CA 6971 925 UE24 WEATHER RADAR INOPERATIVE. RTA-852 FAILURE. REPLACED RTA-852. (M) 2 L 7 2 4T RT A24CE 1998082800804 19980828 00804 CE 1998 8 28 98ZZZM589 1 19980724 A 3260 1148200773 BRACKET BEECH 1900 1900D 1154162 CE NLG WW BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 854CA UE60 RED GEAR HANDLE, NO NOSE GEAR GREEN. BROKEN NOSE GEAR DOWN LOCK ACTUATOR BRACKET, REPLACED. (M) 2 L 7 2 4T RT A24CE 1998082800805 19980828 00805 NM 1998 8 28 AALA981368 1 19980711 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380AN 25449 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS AT SEAT 33H INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR LIGHT CONNECTOR AT SEAT 33H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082800806 19980828 00806 NM 1998 8 28 AALA981367 1 19980711 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380AN 25449 SFO - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR LIGHTS AT SEAT 41B INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR L IGHT CONNECTOR AT SEAT 41B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082800807 19980828 00807 NM 1998 8 28 AALA981366 1 19980711 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 380AN 25449 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS AT SEAT 21B INOPERATIVE. REPAIRED WIRE AT SEAT 21B. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082800808 19980828 00808 NM 1998 8 28 AALA981338 1 19980706 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 21B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CON NECTOR AT PAX SEAT 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082800809 19980828 00809 NM 1998 8 28 AALA981348 1 19980707 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 389AA 27449 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH ESCAPE LIGHTING AT SEAT ROW 25 INOPERATIVE. RECONNECTED E MERGENCY EXIT FLOOR PATH ESCAPE LIGHT STRIP CONNECTOR AT SEAT ROW 25. SYSTEM GROUND CHECKED NROMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082800810 19980828 00810 NM 1998 8 28 AALA981391 1 19980715 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHTS AT 36AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR A ND PINS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082800811 19980828 00811 NM 1998 8 28 AALA981356 1 19980709 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 36 A/B INOPERATIVE. REPLACED CONNECTOR ON LOWER S EAT LEG OF SEAT 36. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998082800812 19980828 00812 NM 1998 8 28 AALA981270 1 19980627 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 360AA 24041 SFO - FLT 1539 - EN ROUTE MIA-SFO - DURING CRUISE, ALL EMERGENCY EXIT AND FLOOR LIGHTS ILLUMINATED FOR APPROX 30 SECONDS THEN WERE EXTINGUISHED BY RESETTING THE EMERGENCY EXIT LIGHTS AT FLIGHT ATTENDANTS STATION. SITUATION OCCURRED AGAIN D URING FLIGHT. LANDED SFO WITHOUT INCIDENT. SECURED CONNECTOR AT FLT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPER ATION. (M) 2 L 7 2 4F RT A1NM 1998082800813 19980828 00813 NE 1998 8 28 ARWA9807133 2 19980730 A 7210 GEAR BOX DOUG DC8 DC863 302198A WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE LEAKING A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 345JW 46042 BLD - FLT 505 - AFTER TAKEOFF OF BDL CREW PHONE LOST OIL QTY NR 2 ENGINE SHUT DOWN A/C DIVERTED TO MIAMI. AFTER LANDING , NR 2 ENGINE WAS OIL SERVICE, MOTORIZED. FOUND GEAR BOX LEAKING. ENGINE WILL BE REPLACED. (M) 2 L 7 4 4F 4 F 4A25 1E8 1998082800814 19980828 00814 NM 1998 8 28 EISA98170 1 19980707 A 3610 CLAMP BOEING 727 727223 1384074 NM NR 1 STRUT LOOSE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 AFTER TAKEOFF FROM MCI WHILE CLIMBING THROUGH 3200 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AOM ABNORMAL ACCOM PLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLT, EVEN AFTER NR 1 THR OTTLE RETURNED TO NORMAL. GENERATED BY PILOT REPORT. REMOVED AND REPLACED AFT 8TH STAGE VALVE CLAMP. NO OTHE RLEAKS N OTED. (M) 2 L 7 3 4F A3WE 1998082800815 19980828 00815 NM 1998 8 28 EISA98171 1 19980707 A 3610 CLAMP BOEING 727 727223 1384074 NM NR 1 STRUT LOOSE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 AFTER TAKEOFF FROM LAX WHILE CLIMBING THROUGH 5000 FEET, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCO MPLISHED. OVERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLIGHT, EVEN AFTER NR 1 THROTTLE RETURNED TO NORMAL. GENERATED FROM PILOT REPORT. REPOSITIONED AND TIGHTENED 8TH STAGE CLAMPS. (M) 2 L 7 3 4F A3WE 1998082800816 19980828 00816 NM 1998 8 28 EISA98169 1 19980707 A 8012 CLAMP BOEING 727 727223 1384074 NM NR 1 ENGINE LOOSE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 AFTER TAKEOFF FROM IND WHILE CLIMBING THROUGH APPROXIMATELY 5000 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM A BNORMALS ACCOMPLISHED. OVERHEAT LIGHT EXTINGUISHED AFTER APPROXIMATELY 2 MINUTES COOLING PERIOD, LIGHT REMAINED OFF FOR REMAINDER OF FLIGHT EVEN AFTER THROTTLE REPLACED TO NORMAL POSITION. GENERATED FROM PILOT REPORT. FOUND CLAMP TO STAR TER DUCT LOOSE AND LEAKING REPOSITION CLAMP, GROUND RUN AIRCRAFT WITH CREW, LEAK CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998082800817 19980828 00817 NM 1998 8 28 EISA98172 1 19980707 A 3610 BACC100U35UAB CLAMP BOEING 727 727223 1384074 NM NR 1 STRUT FAILED A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 ON CLIMB-OUT OF PDX AT APPROXIMATELY 4500 FT, NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED, AOM ABNORMAL ACCOMPLISHED. O VERHEAT LIGHT EXTINGUISHED AS SOON AS THROTTLE RETARDED. LIGHT REMAINED OFF REST OF FLIGHT, EVEN AFTER NR 1 THROTTLE RE TURNED TO NORMAL. REMOVED AND REPLACED 8TH STAGE BLEED AIR BAND CLAMP. OPS CHECK GOOD IAW 36-10. (M) 2 L 7 3 4F A3WE 1998082800818 19980828 00818 NM 1998 8 28 EISA98173 1 19980708 A 3610 131961 LINE BOEING 727 727223 1384074 NM NR 1 STRUT FAILED A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 315NE 20190 AFTER DEPARTURE FROM LAX, PASSING 4500 FT, NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, PERFORMED CHECKLIST LIGHT EXTINGUISHED . FOUND LEAKING SENSE LINE AT 13TH STAGE MODULATION VALVE. REPLACED LINE, OPS CHECK GOOD PER MM 36-10-00, 36-12-00, NO OTHER LEAKS NOTED. (M) 2 L 7 3 4F A3WE 1998082800819 19980828 00819 CE 1998 8 28 98ZZZM590 1 19980624 A 5400 1149800211 KEEL WEB BEECH 1900 1900C 1154161 CE LT NACELLE DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 195GA UB65 AT SCHEDULED INSPECTION, DETERMINED THE LEFT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVIC E BULLETIN 54-3071 PART 2, VISUAL INSPECTIONS PROVED SATISFACTORY PER PART 1 OF SAME BULLETIN. SCHEDULED REPETITIVE VIS UAL INSPECTIONS UNTIL KEEL IS REPLACED. SCHEDULED KEEL REPLACEMENT PER RAYTHEON SERVIEC BULLETIN 54-3071. (M) 2 L 7 2 4T RT A24CE 1998082800820 19980828 00820 CE 1998 8 28 98ZZZM591 1 19980624 A 5400 1149800212 KEEL WEB BEECH 1900 1900C 1154161 CE RT NACELLE DAMAGED A GUUA K NONE O OTHER IN INSP/MAINT 1 SO 19 195GA 25503 UB65 AT SCHEDULED INSPECTION DETERMINED THE RIGHT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVIC E BULLETIN 54-3071 PART 2. VISUAL INSPECTIONS PROVED SATISFACTORY PER PART 1 OF SAME BULLETIN. SCHEDULED REPETITIVE VI SUAL INSPECTIONS UNTIL KEEL IS REPLACED. SCHEDULED KEEL REPLACEMENT PER RAYTHEON SERVICE BULLETIN 54-3071. (M) 2 L 7 2 4T RT A24CE 1998082800821 19980828 00821 NM 1998 8 28 P2EA98111 1 19980617 A 5210 ANGLE BOEING 737 737222 1384473 NM L1 DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-46-5223C, A CRACK WAS NOTED ON BEAM NR 7 ANGLE, OF THE L 1 DOOR. THE CRACK WAS 1.25 INCHES LONG. INSTALLED ANGLE REPAIR AS PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 1998082800822 19980828 00822 EU 1998 8 28 UF6A980615 1 19980627 A 3150 3085003004 PBSI BAG ATP ATP EU COCKPIT FAILED A UF6A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 31 855AW 13240 2029 ORD - FLT 5708 - WHEN SELECTING ANY MODE ON POWER SELECTOR RATING 'TAKEOFF' PBSI STAYS ENGAGED. MAINTENANCE REPLACED 'T AKEOFF' PBSI. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998082800823 19980828 00823 NM 1998 8 28 USAASB98178 1 19980711 A 3411 STATIC LINE BOEING 737 7374B7 1384702 NM AIR DATA COMP LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 436US 24558 CLT - FLT 549 - ON CLIMB-OUT FROM CLT, THE CAPTAINS ALTIMETER AND AIRSPEED INDICATOR BECAME INOP. FLIGHT RETURNED TO FI ELD AT CLT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESEATED/RERACKED THE NR 1 AIR DATA COM PUTER (P/N 4061100-901). BITE TEST AND OPERATIONAL CHECK GOOD. ITEM REPEATED MAINTENANCE REPAIR NR 1 AIRDATA SYSTEM ST ATIC LEAK. (M) 2 L 7 2 4F RT A16WE 1998082800824 19980828 00824 EU 1998 8 28 USAAF98055 1 19980713 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN MALFUNCTIONED A USAA K NONE O OTHER CL CLIMB 1 EA 19 857US 11289 PIT - FLT 671 - AFTER TAKEOFF FROM PIT, THE EMERGENCY EXIT LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR WAS RETRACTED. MAINTENANCE RESEATED RELAY K2618A AND THE SYSTEM OPERATED NORMALLY. THEY PROGRAMMED THE RELAY FOR CHANGE AS A PRECAUT IONARY MAINTENANCE ACTION. (M) 2 L 7 2 4F RT 1998082800825 19980828 00825 NM 1998 8 28 USAASB98177 1 19980710 A 2150 3964421 VALVE BOEING 737 737301 1384611 NM LT PACK FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 351US 26319 23554 CLT - FLT 1065 - AFTER TAKEOFF FROM CLT, THE AUTO PRESSURIZATION SYSTEM FAILED. CREW WAS UNABLE TO PRESSURIZE AIRCRAFT OR CONTROL CABIN IN STANDBY OR MANUAL OPERATION. DECISION WAS MADE TO RETURN TO FIELD AT CLT. FLIGHT LANDED WITHOUT IN CIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT FLOW CONTROL VALVE. PRESSURIZED AIRCRAFT . OPERATIONAL CHECK GOOD PER MM 21-31-00. (M) 2 L 7 2 4F RT A16WE 1998082800826 19980828 00826 EU 1998 8 28 RAIA980720 1 19980703 A 5320 S53572103200 CLIP AEROSP ATR72 ATR72202 8680940 EU BS 37 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 14975 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT SERVICE DOOR CLIP FRAME 37. MAINTENANCE REPLACED CLIP AT SERVICE DOO R FRAME 37 IAW ATR 72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800827 19980828 00827 EU 1998 8 28 RAIA980719 1 19980703 A 5347 S536780001000 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU BS 36 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 14975 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT RIGHT OUTBOARD SEAT TRACK FRAME 36. MAINTENANCE REPAIRED SEAT TRACK AT FRAME 36 IAW ATR 72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800828 19980828 00828 EU 1998 8 28 RAIA980718 1 19980702 A 5347 S536780001000 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU BS 34-36 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 14974 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT RIGHT INBOARD SEAT TRACK AT FRAMES 34 AND 36. MAINTENANCE REPAIRED S EAT TRACK SECTION BETWEEN FRAMES 34 AND 36 IAW ATR 72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800829 19980828 00829 EU 1998 8 28 RAIA980717 1 19980702 A 5320 S53572103200 CLIP AEROSP ATR72 ATR72202 8680940 EU BS 39 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 14975 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 39 SERVICE DOOR SILL CLIP. MAINTENANCE REPLACED SILL PLATE CLI P IAW ATR 72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800830 19980828 00830 EU 1998 8 28 RAIA980716 1 19980702 A 5320 S53371294202 SILL PLATE AEROSP ATR72 ATR72202 8680940 EU BS 39 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 14975 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FRAME 39 SERVICE DOOR SILL PLATE. MAINTENANCE REPLACED SERVICE DOOR SILL PLATE IAW ATR 72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800831 19980828 00831 1998 8 28 RAIA980710 4 19980711 A 3417 7000700967 COMPUTER JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 570HK 4567 41089 FLT 7789 - JFK - LEFT AIR DATA COMPUTER FAILED. MAINTENANCE REPLACED LEFT AIR DATA COMPUTER. (M) 2 L 7 2 4T RT A41NM 1998082800832 19980828 00832 EU 1998 8 28 RAIA980709 1 19980711 A 7722 30738461 SENSOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 568HK 4390 41086 FLT 7780 - JFK - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED RIGHT ENGINE EGT ALUMEL TERMINAL END. (M) 2 L 7 2 4T RT A41NM 1998082800833 19980828 00833 EU 1998 8 28 RAIA980708 1 19980711 A 3230 1379305A155 HOSE BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A RAIA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CE 03 860AE 15370 860 FLT 4734 - FAT - HYDRAULIC SYSTEM PRESSURE WENT TO '0'. MAINTENANCE REPLACED RIGHT MAIN GEAR RADIUS ROD RETRACT HOSE. ( M) 2 L 7 2 4T RT A56EU 1998082800834 19980828 00834 EU 1998 8 28 RAIA980713 1 19980714 A 2422 1B3501B13 INVERTER BAG JETSTM JETSTM3201 1500217 EU E/E BAY FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 340TE 10893 939 FLT 7418 - STL - ESSENTIAL INVERTER FAILED IN FLIGHT. MAINTENANCE REPLACED INVERTER. (M) 2 L 7 2 4T RT A56EU 1998082800835 19980828 00835 EU 1998 8 28 RAIA980714 1 19980714 A 7331 696219 INDICATOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 425AM 10597 870 FLT 7468 - STL - RIGHT FUEL PRESSURE GAUGE READS NEGATIVE. MAINTENANCE REPLACED RIGHT FUEL PRESSURE GAUGE. (M) 2 L 7 2 4T RT A56EU 1998082800836 19980828 00836 EU 1998 8 28 RAIA980712 1 19980713 A 2610 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 557HK 3267 41074 FLT 7761 - JFK - SMOKE CAPTION ILLUMINATED AFTER TAKEOFF. MAINTENANCE REPLACED SMOKE DETECTOR. (M) 2 L 7 2 4T RT A41NM 1998082800837 19980828 00837 1998 8 28 RAIA980711 3 19980713 A 6140 31056294 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 556HK 41073 FLT 7260 - STL - RIGHT BETA CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT BETA PRESSURE SWITCH. (M) 2 L 7 2 4T RT A41NM 1998082800838 19980828 00838 WP 1998 8 28 RAIA980613 2 19980625 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP LEFT MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 433AM 885 FLT 7045 - STL - LEFT ENGINE SINGLE RED LINE COMPUTER CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE DEFERRED 76-1 CA T C. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998082800839 19980828 00839 1998 8 28 RAIA980707 4 19980708 A 3416 066306202 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 426AM 12302 874 STL - FLT 7508 - NR 1 ALTIMETER FLAGGED. REPLACED ALTIMETER. (M) 2 L 7 2 4T RT A56EU 1998082800840 19980828 00840 WP 1998 8 28 RAIA980706 2 19980708 A 7320 31081961 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP NR 1 ENGINE LEAKING A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 430AM 6529 880 66128 STL - FLT 7348 - NR 1 ENGINE WOULD NOT PRODUCE TARGET TORQUE. REPLACED BLEED AIR GASKET. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998082800841 19980828 00841 NE 1998 8 28 RAIA980705 2 19980706 A 7320 7863927 HMU AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE NR 1 ENGINE MALFUNCTIONED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 425TE 17034 125 121021 STL - FLT 7417 - NR 1 WOULD NOT PRODUCE TAKEOFF TORQUE. REPLACED HYDRO-MECHANICAL UNIT. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998082800842 19980828 00842 EU 1998 8 28 RAIA980615 1 19980630 A 5320 S53671217376 ANGLE AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 14975 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT PASSENGER CABIN SILL PLATE T-ANGLE BETWEEN FLOORBEAM 36 AND 37. MAIN TENANCE REPLACED T-ANGLE IAW ATR 72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800843 19980828 00843 EU 1998 8 28 RAIA980616 1 19980629 A 5347 S536780001000 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FLIGHT ATTENDANT SEAT TRACK. MAINTENANCE REPLACED SEAT TRACK IAW ATR 72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800844 19980828 00844 EU 1998 8 28 RAIA980617 1 19980630 A 5320 S53572103200 CLIP AEROSP ATR72 ATR72202 8680940 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 721TE 14975 217 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT RIGHT SIDE FLOORBEAM 41. MAINTENANCE REPLACED CLIP AT FLOORBEAM 41 I AW ATR72 SRM. (M) 2 H 7 2 4T RT A53EU 1998082800845 19980828 00845 NM 1998 8 28 TWAA9811701 1 19980721 A 3350 1102837 LIGHTS BOEING 727 727231 1384079 NM CABIN INOPERATIVE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54351 21983 DURING OVERNIGHT MAINTENANCE, FOUND THE AFT AIRSTAIR EMERGENCY LIGHTS INOP. REPLACED THE LIGHT ASSEMBLY. CHECK-C 10-31 -97. (M) 2 L 7 3 4F A3WE 1998082800846 19980828 00846 WP 1998 8 28 TWAA9811601 1 19980718 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 414EA 47746 DURING PREFLIGHT, CREW REPORTED THE FIRST CLASS AND FWD CABIN FLOOR EGRESS LIGHTS WERE INOPERATIVE. FOUND CONN TO FIRST CLASS FEEDER STRIP WAS OFF. REINSTALLED CONN, CHECK-C 6-9-98. (M) 2 L 7 2 4F RT A6WE 1998082800847 19980828 00847 NM 1998 8 28 TSAA9833398 1 19980708 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 2 POSITION FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT A16WE 1998082800848 19980828 00848 NM 1998 8 28 TSAA9833399 1 19980708 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 5 POSITION FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT A16WE 1998082800849 19980828 00849 NM 1998 8 28 TSAA9833400 1 19980708 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 6 POSITION FLOOR PROXIMITY EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT A16WE 1998082800850 19980828 00850 NM 1998 8 28 TSAA9833402 1 19980716 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998082800851 19980828 00851 NM 1998 8 28 TSAA9833403 1 19980616 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998082800852 19980828 00852 NM 1998 8 28 TSAA9833404 1 19980616 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION LED'S INOP. REPLACED BATTERY. OPS CHECK GOOD. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998082800853 19980828 00853 WP 1998 8 28 TWAA9813701 1 19980824 A 3240 222704 CONTROL VALVE DOUG DC9 DC915 3022036 WP RT HYD SYST FAILED A TWAA O OTHER O OTHER LD LANDING 1 CE 05 971Z 45773 WHEN LANDING THE RT BRAKE WAS INOPERATIVE WHEN THE RT HYD SYSTEM WAS SELECTED. BRAKING NORMAL WHEN LT HYD SYS SELECTED. REPLACED THE RT BRAKE CONTROL VALVE PER MAINT MANUAL 32-42-2. CHECK-C 7-6-98 STL. 2 L 7 2 4F A6WE 1998082800854 19980828 00854 NM 1998 8 28 TWAA9813702 1 19980719 A 5753 SKIN BOEING 767 767231 1385131 NM RT TE FLAP DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 603TW 22566 DURING ROUTINE CHECK OF ACFT, FOUND RT O/B TE FLAP, I/B OF I/B CANOE, WITH LEADING EDGE DAMAGED 18 IN BY 8 IN. REPAIRED DAMAGE PER SRM 57-53-01 AND 57-70-17. CHECK-C 6-28-98 LAX. 2 L 7 2 4F RT A1NM 1998082800855 19980828 00855 NM 1998 8 28 K3HA980099 1 19980824 A 2910 106056341 LINE BOEING 727 727225 1384077 NM NR 1 ENGINE LEAKING A K3HA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 25 356PA 20626 NO A-HYDRAULIC SYSTEM PRESSURE DUE TO NR 1 AND NR 2 ENGINE HYDRAULIC PUMP FAILURE. NO FLUID LOSS. GEARS MANUALLY EXTEN DED. LUGGAGE RACK INHIBITED MANUAL GEAR EXTENSION. FOUND LEAKING NR 1 ENGINE HYDRAULIC PUMP PRESSURE LINE AND FIRE WAL L COUPLING. REPLACED LINE, COUPLING, NR 1 AND NR 2 HYDRAULIC PUMPS IAW B727 MM 29-11-33 AND 20-10-5. REPLACED HYDRAULI C QUANTITY GAUGE IAW MM 29-11-0. ADJUSTED LUGGAGE RACK IN COCKPIT. 2 L 7 3 4F A3WE 1998082800856 19980828 00856 WP 1998 8 28 IXXA9800065 1 19980812 A 3230 MECHANISM DOUG DC8 DC863F 302198F WP LANDING GEAR MISRIGGED A IXXA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 GL 23 867BX 28 46049 AFTER TAKEOFF, WHEN THE FLIGHT CREW RETRACTED THE LANDING GEAR, THE CONTROL HANDLE WOULD NOT POSITION TO THE UP POSITION . THE CREW RETURNED THE GEAR HANDLE TO THE DOWN POSITION, RECEIVING THREE DOWN AND LOCK INDICATIONS. A SECOND ATTEMPT TO RETRACT THE GEAR WAS UNSUCCESSFUL AND THE AIRCRAFT RETURNED TO DFW. MAINTENANCE INSPECTED THE AIRCRAFT, FINDING THE LANDING GEAR ANTI-RETRACT LATCH MECHANISM MISRIGGED. MAINTENANCE RIGGED THE SYSTEM IN ACCORDANCE WITH THE DOUGLAS MAINT ENANCE MANUAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1998082800857 19980828 00857 WP 1998 8 28 IXXA9800066 1 19980811 A 2612 92274473 RELAY DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A IXXA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 828BX 2699 45993 DURING CLIMBOUT, THE NR 1 ENG FIRE WARNING SOUNDED WITH THE MASTER FIRE WARNING LIGHT ILLUMINATED. THE FLT CREW SECURED THE ENG FOLLOWING COMPANY PROCEDURES AND DISCHARGED THE FIRE BOTTLE. THE FIRE WARNING LIGHT EXTINGUSHED FOLLOWING FIRE BOTTLE DISCHARGE. THE FLT RETURNED TO DFW FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENG AND FOUND NO EVIDE NCE OF A FIRE. THE FIRE WARNING LOOPS AND ASSOCIATED WIRING WERE INSPECTED LOCATING CORROSION ON THE FIRE WALL CANNON P LUG AND A DEFECTIVE RESET RELAY. THE RELAY WAS REPLACED AND THE CANNON PLUG WAS CLEANED. MAINTENANCE PERFORMED A SUCCE SSFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. 2 L 7 4 4F RT 4A25 1998082800858 19980828 00858 NM 1998 8 28 CALA9801502 1 19980825 A 5320 SUPPORT BOEING 727 727224 1384076 NM LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LT AFT LAV AISLE SIDEWALL FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-10-1. A NE W FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, PAGE 4. 2 L 7 3 4F A3WE 1998082800859 19980828 00859 NM 1998 8 28 CALA9801503 1 19980825 A 5532 PLATE BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 4 INCH CRACK IN VERTICAL STABILIZER INNER COMPARTMENT NR 1 RIB LOWER LT CORNER PLATE JUST AFT OF S-DU CT. THE RIVETS WERE REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998082800860 19980828 00860 NM 1998 8 28 CALA9801504 1 19980825 A 5530 STRINGER BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK AT ATTACH BOLT IN STRINGER 9R AT VERTICAL STABILIZER INNER COMPARTMENT NR 9 RIB. THE C RACKED AREA WAS REMOVED IAW SRM 55-30-4. A REPAIR WAS INSTALLED IAW SRM 55-20-4, FIGURE 1, SHEET 5, AND SRM 51-10-2. 2 L 7 3 4F A3WE 1998082800861 19980828 00861 NM 1998 8 28 CALA9801505 1 19980825 A 5330 SKIN BOEING 727 727224 1384076 NM CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND FORWARD LOWER C-3 DOOR CUTOUT CORRODED IN AFT CARGO COMPARTMENT BETWEEN LONGERON 25R AND 26R. THE CORR ODED AREA WAS REMOVED IAW SRM 51-30-2. A DOUBLER WAS INSTALLED IAW SRM 53-10-1, PAGE 5, FIGURE 1. 2 L 7 3 4F A3WE 1998082800862 19980828 00862 NM 1998 8 28 CALA9801506 1 19980825 A 5320 BRACKET BOEING 727 727224 1384076 NM BS 910 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .0781 INCH CRACK AT UPPER FORWARD LEG OF LT GEAR UPLOCK SUPPORT BRACKET WHERE IT MOUNTS TO FUSELAGE B S 910 BETWEEN STRINGER 18A LEFT AND 18L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4. 2 L 7 3 4F A3WE 1998082800863 19980828 00863 NM 1998 8 28 CALA9801507 1 19980825 A 5320 WEB BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LT LAV FLOOR WEB CORRODED AT STA 1130, LBL 27. THE CORRODED AREA WAS CUT OUT IAW SRM 51-40-2. A DOUBL ER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, SHEET 6. 2 L 7 3 4F A3WE 1998082800864 19980828 00864 NM 1998 8 28 CALA9801508 1 19980825 A 5320 WEB BOEING 727 727224 1384076 NM BS 1148-1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND CORROSION ON TOP OF AFT CABIN FLOOR SUPPORT WEB AT BS 1148 TO 1183, RBL 25 TO LBL 25. THE CORRODED ARE A WAS CUT OUT IAW SRM 51-40-2. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1. 2 L 7 3 4F A3WE 1998082800865 19980828 00865 NM 1998 8 28 CALA9801509 1 19980825 A 5330 SKIN BOEING 727 727224 1384076 NM BS 680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 2 INCH CRACK IN LT FUSELAGE SKIN BETWEEN WINDOWS NR 16 AND NR 17 AT STA 680. THE CRACKED AREA WAS RE PAIRED IAW SRM 51-40-00, 51-10-6, AND 51-10-2. 2 L 7 3 4F A3WE 1998082800866 19980828 00866 NM 1998 8 28 CALA9801510 1 19980825 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1180 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT AFT LAV FLOOR LEVEL ANGLE CORRODED AT FS 1180. A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND 51-20-4. 2 L 7 3 4F A3WE 1998082800867 19980828 00867 NM 1998 8 28 CALA9801511 1 19980825 A 5320 WEB BOEING 727 727232 1384082 NM BS 740 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 3 AND 4 INCH CRACK IN LT CABIN ATTACH WEB AT STA 740, LBL 45. THE CRACKS WERE STOP DRILLED, A DOUBLE R WAS INSTALLED IAW SRM 51-10-1, 51-40-2, 53-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998082800868 19980828 00868 NM 1998 8 28 CALA9801512 1 19980825 A 5210 SKIN BOEING 727 727232 1384082 NM PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND L-1 DOOR INNER SKIN CRACKED JUST AFT OF WINDOW OPENING. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS IN STALLED IAW SRM 51-40-2 FIGURE 1, 51-30-2, 52-10-1 FIGURE 1, 51-30-6, 51-30-8, AND 51-40-2 FIGURE 1. 2 L 7 3 4F A3WE 1998082800869 19980828 00869 NM 1998 8 28 CALA9801513 1 19980825 A 5311 FRAME BOEING 727 727232 1384082 NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 312 BELOW SRTINGER 13R. THE CRACKED SECTION OF FRAME WAS REMOVED. A RE PAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 4 AND 51-30-2. 2 L 7 3 4F A3WE 1998082800870 19980828 00870 NM 1998 8 28 CALA9801514 1 19980825 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT UPPER WING TO BODY FAIRING SUPPORT STRUCTURE CRACKED ON LOWER ANGLE AND WEB AT FS 950. THE CRACK WA S 2 INCHES LONG. THE ANGLE WAS REMOVED AND THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-40-3 , 51-10-2, 51-00-0 FIGURE 23 AND MM 51-20-1. 2 L 7 3 4F A3WE 1998082800871 19980828 00871 NM 1998 8 28 CALA9801515 1 19980825 A 5720 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND TWO .625 INCH CRACKS IN RT WING TRAILING EDGE SUPPORT ANGLE UNDER NR 13 SPOILER OUTBOARD END AT SUPPORT ROD LOWER ATTACH POINT. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-3 0-2. 2 L 7 3 4F A3WE 1998082800872 19980828 00872 NM 1998 8 28 CALA9801516 1 19980825 A 5720 ANGLE BOEING 727 727232 1384082 NM WS 92.8 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT WING FORWARD RIB ATTACH ANGLE CRACKED AT WS 92.8. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALL ED IAW SRM 51-30-2, 57-20-2, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998082800873 19980828 00873 NM 1998 8 28 CALA9801517 1 19980825 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 410-430 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND SEAT TRACK CORRODED AT STA 410 TO 430, RBL 24. THE SEAT TRACK WAS REPLACED IAW SRM 53-10-5, FIGURE 7. 2 L 7 3 4F A3WE 1998082800874 19980828 00874 NM 1998 8 28 CALA9801518 1 19980825 A 5720 BEAM BOEING 727 727224 1384076 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A .5 INCH CRACK IN J-BEAM APPROXIMATELY 1.5 INCHES ABOVE NR 7 SPOILER ACTUATOR AT CUTOUT ABOVE INBOARD END OF AFT FALSE SPAR. PANELS AND A FITTING WERE REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5740-02914 AND SRM 51-10-2 , AND 51-10-6. THE PANELS AND FITTING WERE REINSTALLED. 2 L 7 3 4F A3WE 1998082800875 19980828 00875 NM 1998 8 28 CALA9801519 1 19980825 A 5720 BRACKET BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A 0.4 INCH CRACK IN RT WING LEADING EDGE FLAP NR 6 ACTUATOR MOUNT BRACKET. THE MOUNT BRACKET WAS REMOV ED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998082800876 19980828 00876 WP 1998 8 28 CALA9801520 1 19980824 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 636-693 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14818 49478 INSPECTION FOUND CORROSION ON THE LOWER HORIZONTAL LEG OF THE MAIN BAGGAGE BIN Z-ANGLE AT LOWER THRESHOLD OF DOOR CUTOUT AT STA 636 TO 693. A Z-ANGLE REPAIR WAS INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998082800877 19980828 00877 WP 1998 8 28 CALA9801521 1 19980825 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14818 49478 INSPECTION FOUND AFT CARGO Z-ANGLE CORRODED AROUND HI-SHEARS AND DOOR STOPS FROM STA 1155 TO 1212. A REPAIR DOUBLER AND SPACER WERE INSTALLED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998082800878 19980828 00878 NM 1998 8 28 CALA9801522 1 19980825 A 5315 FLOORBEAM BOEING 737 7372C0 1384488 NM BS 663 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM WEB AT STA 663, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5710-01931. 2 L 7 2 4F A16WE 1998082800879 19980828 00879 NM 1998 8 28 CALA9801523 1 19980825 A 5320 ANGLE BOEING 737 7372C0 1384488 NM LT WING/FUS CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 3 INCH CRACK IN LT FORWARD WING TO BODY FAIRING ATTACH ANGLE. THE ANGLE WAS REMOVED AND A REPAIR ANG LE WAS INSTALLED IAW ECRA 5350-01227 AND 51-30-2. 2 L 7 2 4F A16WE 1998082800880 19980828 00880 WP 1998 8 28 CALA9801524 1 19980824 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 775 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 INSPECTION FOUND FUSELAGE SKIN CORRODED AT AFT BAGGAGE BIN STA 775, LONGERON 30 TO 29R. A DOUBLER WAS INSTALLED IAW ECR A 5331-01028. 2 L 7 2 4F A6WE 1998082800881 19980828 00881 WP 1998 8 28 9809949623 1 19980823 A 3260 SENSOR DOUG DC9 DC932 3022066 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 623NW 47591 NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CAPTAIN DECLARED AN EMERGENCY AND AIRCRAFT LANDED WITH OUT INCIDENT. NOSE GEAR WAS PINNED ON RUNWAY AND AIRCRAFT WAS TOWED TO GATE. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PROX IMITY SENSOR BROKEN. REPLACED SENSOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998082800882 19980828 00882 WP 1998 8 28 9809951155 1 19980619 A 5730 SKIN DOUG DC10 DC1040 3023508 WP LT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 155US 46764 DURING M-CHECK, FOUND TWO INCH CRACK IN INBOARD EDGE OF LEADING EDGE FLEX SKIN. REPAIRED PER EA 11-155651. 2 L 7 3 4F A22WE 1998082800883 19980828 00883 WP 1998 8 28 9809961155 1 19980701 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1510-1531 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 155US 46764 DURING M-CHECK, FOUND CORROSION ON OUTER SKIN FROM FS 1510 TO 1531, STR 45R TO 45L. REPAIRED PER EA 11-158670. 2 L 7 3 4F A22WE 1998082800884 19980828 00884 WP 1998 8 28 9809979997 1 19980823 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 1155 CANTED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8933E 47142 DURING M-CHECK, FOUND CANTED FRAME AT FS 1155 RBL 25. REPAIRED PER EA 99-160044. 2 L 7 2 4F A6WE 1998082800885 19980828 00885 WP 1998 8 28 9809989990 1 19980825 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 261 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8950E 47186 DURING H-CHECK, FOUND FINGER DOUBLER CRACKED FROM EDGE OF LAP TO FASTENER AT FS 261, LONGERON 1. REPAIRED PER EA 99-160 260. 2 L 7 2 4F A6WE 1998082800886 19980828 00886 NM 1998 8 28 UPS98227425 1 19980812 A 5313 STRINGER BOEING 727 72725C 138400H NM BS 360 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 937UP 19302 INSPECTION TYPE-N/A, EVIDENCE OF CORROSION LEFT SIDE STA 360 APPROX S24-S25. DEFERRED CORROSION AT STATION 360 STRINGER 24 AND 25 IN ACCORDANCE WITH FERRY PERMIT NR 9052. REMOVED FASTENER TO INVESTIGATE, VISUALLY INSPECTED FASTENER HOLES. NO CORROSION FOUND, ILLEGIBLE 66193 12 AUG 98. INSP ALL INTERNAL STRUCTURE NO CORROSION NOTED ILLEGIBLE 90851. INSTA LL FASTENERS, THIS CLEARS D-157185. 2 L 7 3 4F A3WE 1998082800887 19980828 00887 NM 1998 8 28 UPS98627513 1 19980820 A 5541 RIB BOEING 767 76734AF 1385212 NM RUDDER DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 309UP 27740 INSPECTION TYPE-E, TOP DAMAGE CAUSED TO BULLNOSE RIB WEB AT RUDDER STA 181.034. RUDDER ASSEMBLY WAS REMOVED AND REPLACE D ON CARD NR 745375. 2 L 7 2 4F RT A1NM 1998082800888 19980828 00888 NM 1998 8 28 UPS98627514 1 19980820 A 5541 SPAR WEB BOEING 767 76734AF 1385212 NM RUDDER PUNCTURE A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 309UP 27740 INSPECTION TYPE-N/A, RUDDER FRONT SPAR WEB IS PUNCTURED AT RUDDER STATION 189, THREE INCHES LEFT OF CENTER LINE. REMOVE D AND REPLACED RUDDER ASSEMBLY ON CARD NR 745375. 2 L 7 2 4F RT A1NM 1998082800889 19980828 00889 NM 1998 8 28 UPS98627515 1 19980821 A 5541 SPAR BOEING 767 76734AF 1385212 NM RUDDER DELAMINATED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 309UP 27740 INSPECTION TYPE-N/A, RUDDER FRONT SPAR AT RUDDER STATION FRONT SPAR STATION 189 HAS 2 X 6 AREA OF DELAMINATION. REMOVED RUDDER ASSEMBLY, INSTALLED SERVICEABLE RUDDER ASSEMBLY IAW MM 27-21-01. 2 L 7 2 4F RT A1NM 1998082800890 19980828 00890 WP 1998 8 28 UPS98827512 1 19980818 A 5320 47117221 FITTING DOUG DC8 DC871F 302199D WP BS 8 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, STA 8 STR 22R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4711722 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998082800891 19980828 00891 NM 1998 8 28 UPS98227517 1 19980814 A 5712 RIB BOEING 727 72751C 1384015 NM NR 4 SLAT ACT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, ON REMOVAL OF NR 4 SLAT ACTUATOR EYE END BOLT FROM SLAT BOTH RIBS EITHER SIDE OF MOUNT POINT FOUND CR ACKED. REPLACED RIBS IAW SRM AND DRAWING 657276, REINSTALLED NR 4 SLAT EYE BOLT IAW MM 27-81-32. 2 L 7 3 4F A3WE 1998082800892 19980828 00892 NM 1998 8 28 UPS98227518 1 19980810 A 5311 FRAME BOEING 727 72751C 1384015 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, SLIDING FAIRING 2ND AFT FRAME HAS A CRACK AT THE UPPER SLIDING TRACK ATTACH POINT. CRACK STOP DRILLE D PER SRM 51-10-1, REPAIRED FRAME IAW SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1998082800893 19980828 00893 NM 1998 8 28 UPS98227519 1 19980807 A 5330 SKIN BOEING 727 72751C 1384015 NM BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, SUSPECT CORROSION BETWEEN SKIN AND CUSP ANGLE BS 1180 STR 17R. CORRODED SKIN AT BS 1180 STR 17R REPA IRED PER SRS EO 98-24-006 REF UPS ENGINEERING FILE NR 727-53-2063. 2 L 7 3 4F A3WE 1998082800894 19980828 00894 NM 1998 8 28 UPS98227520 1 19980729 A 2782 MOUNT BOEING 727 72751C 1384015 NM NR 2 LE SLAT ACT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, NR 2 LE SLAT ACTUATOR VERY LOOSE IN MOUNTING STRUCTURE. REPLACED MOUNTING IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998082800895 19980828 00895 NM 1998 8 28 UPS98227521 1 19980730 A 2710 65217271 PUSH ROD BOEING 727 72751C 1384015 NM LT AILERON CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CORROSION ON LT O/B AILERON PUSH ROD ATTACH LUG. REPLACED PUSH ROD ATTACH WG CASTING IAW DRAWING NR 65-21766. 2 L 7 3 4F A3WE 1998082800896 19980828 00896 NM 1998 8 28 UPS98227522 1 19980730 A 5730 SKIN BOEING 727 72751C 1384015 NM WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, SUSPECT CRACK IN UPPER T/E SKIN PANEL ADJACENT TO NR 5 SPOILER PANEL O/B HINGE CUTOUT. REPAIR CARRIE D OUT IAW SRM 57-30-04 FIG 10. 2 L 7 3 4F A3WE 1998082800897 19980828 00897 NM 1998 8 28 UPS98227523 1 19980802 A 5320 STIFFENER BOEING 727 72751C 1384015 NM BS 750 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, LIGHT SURFACE CORROSION AT BS 750 APPROX LT SIDE WL 1675 APPROX AT STR 27 POSITIONS. REPLACED STIFFE NER IAW DRW 64-08333. 2 L 7 3 4F A3WE 1998082800898 19980828 00898 NM 1998 8 28 UPS98227524 1 19980802 A 5741 69139004 BOTTLE PIN BOEING 727 72751C 1384015 NM BS 740 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, RT BS 740 BOTTLE PIN FOUND WITH PITTING CORROSION. PIN REPLACED IAW MM 57-41-00. 2 L 7 3 4F A3WE 1998082800899 19980828 00899 NM 1998 8 28 UPS98227525 1 19980803 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 560-580 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, BS 560 TO 580 LT STR 20 HAS DENT IN FUSELAGE. REPAIR CARRIED OUT IAW EO 98-24-003 UPS ENGINEERING FI LE NR 727-53 -2060. 2 L 7 3 4F A3WE 1998082800900 19980828 00900 NM 1998 8 28 UPS98227526 1 19980804 A 5320 BRACKET BOEING 727 72751C 1384015 NM BS 745 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CORROSION ON BRACKET STIFFENER AT LBS 745 APPROX STR 24 POSITION WL 167.5. REPLACED BRACKET IAW DRAW ING 64-08333. 2 L 7 3 4F A3WE 1998082800901 19980828 00901 NM 1998 8 28 UPS98227527 1 19980807 A 5720 CLIP BOEING 727 72751C 1384015 NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT LBL 25. REPLACED SHEAR TIE CLIP IAW DRAWING 64-08333. 2 L 7 3 4F A3WE 1998082800902 19980828 00902 NM 1998 8 28 UPS98227528 1 19980807 A 5720 CLIP BOEING 727 72751C 1384015 NM CENTER WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, WING CENTER SECTION FWD TANK FWD WALL SHEAR TIE CLIP CRACKED AT RBL 25. REPLACED SHEAR TIE CLIP IAW DRW 64-08333. 2 L 7 3 4F A3WE 1998082800903 19980828 00903 NM 1998 8 28 UPS98227529 1 19980807 A 5320 WEB BOEING 727 72751C 1384015 NM BS 885 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK ON VERTICAL WEB ABOVE KEEL BEAM RBL BS 885 APPROX. VERTICAL WEB ABOVE KEEL BEAM REPAIRED IAW S RM 51-40-02. 2 L 7 3 4F A3WE 1998082800904 19980828 00904 NM 1998 8 28 UPS98227531 1 19980804 A 2810 CLAMP RING BOEING 727 72751C 1384015 NM WS 185 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, NR 2 TANK ACCESS PANEL RT WING SHOWING EVIDENCE OF FRETTING CORROSION ON CLAMP RING. CLAMP RING REPL ACED PER TC NR C57-571-01-2D. 2 L 7 3 4F A3WE 1998082800905 19980828 00905 NM 1998 8 28 UPS98227533 1 19980806 A 5753 SPINDLE BOEING 727 72751C 1384015 NM TE FLAP TRACK CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, SURFACE CORROSION IN BORE OF SPINDLE OF NR 3 FLAP TRACK CARRIAGE. FLAP TRACK CARRIAGE REPLACED REF O HM 57-58-11. 2 L 7 3 4F A3WE 1998082800906 19980828 00906 NM 1998 8 28 UPS98227534 1 19980826 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-224-04.00-01) ON MAIN DECK FLOORBEAM UPPER CHORD AT BS 1130, RBL 18, WL 208 UNDER SHE AR WEB. REPAIRED IAW ENGINEERING REPAIR NR 98-2760. 2 L 7 3 4F A3WE 1998082800907 19980828 00907 NM 1998 8 28 UPS98227535 1 19980826 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-224-04.00-01) ON MAIN DECK FLOORBEAM UPPER CHORD TOP FLANGE BS 1130, RBL 22, WL 208 A T SMALL DRILLED HOLE (NR 40 BIT). REPAIRED PER ENGINEERING REPAIR NR 98-2760. 2 L 7 3 4F A3WE 1998082800908 19980828 00908 NM 1998 8 28 UPS98227536 1 19980806 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION BETWEEN SEAT TRACK AND EXPANSION LINK FLANGES AT BS 850 RBL 25 WL 208. REPLACED SEAT TRAC K AND EXPANSION LINK AS PER SRM 51-30-5. 2 L 7 3 4F A3WE 1998082800909 19980828 00909 NM 1998 8 28 UPS98227538 1 19980826 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 1130 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON LOWER CHORD OF BS 1130 FLOORBEAM BETWEEN LBL 2 AND RBL 51 WL 201. R EPAIRED CORROSION WITH NEW PART IAW ENGINEERING REPAIR NR 98-2760. 2 L 7 3 4F A3WE 1998082800910 19980828 00910 NM 1998 8 28 UPS98227539 1 19980819 A 5320 FITTING BOEING 727 727247 138408F NM BS 850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION ON LONGITUDINAL BEAM AT I/B FLOOR SUPPORT FITTING ATTACH POINT BS 850 LBL 45 WL 208. REMO VED CORRODED PART, INSTALLED NEW PART IAW SRM 51-30-2, 51-30-5. 2 L 7 3 4F A3WE 1998082800911 19980828 00911 NM 1998 8 28 UPS98227540 1 19980819 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 740 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION ON EXPANSION LINK UPPER SEAT TRACK O/B FLANGE UNDER STRAP AFT OF BS 740 LBL 45 WL 208. RE MOVED CORRODED SEAT TRACK, FABRICATED AND INSTALLED NEW SEAT TRACK IAW 51-30-2. 2 L 7 3 4F A3WE 1998082800912 19980828 00912 WP 1998 8 28 UPS98827516 1 19980720 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 755UP 46055 INSPECTION TYPE-D, RT WING L/E AT STA XFS653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND R EPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998082800913 19980828 00913 WP 1998 8 28 UPS98827530 1 19980726 A 5313 5649329 LONGERON DOUG DC8 DC871F 302199D WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, HEAVY CORROSION ON LONGERON 30L FS 1700. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20D AND DWG 5649329. 2 L 7 4 4F RT 4A25 1998082800914 19980828 00914 WP 1998 8 28 UPS98827532 1 19980726 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1717 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 715UP 45915 INSPECTION TYPE-C, HEAVY CORROSION ON LONGERON 34R FS 1717. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW S RM 53-5-1. 2 L 7 4 4F RT 4A25 1998082800915 19980828 00915 NM 1998 8 28 98FDEA00530 1 19980826 A 2613 OVERHEAT LIGHT BOEING 727 727233 138408A NM LWR AFT BODY MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 218FE 21101 CLIMBING THRU 16,000 LWR AFT BODY OVERHEAT LIGHT CAME ON. CLOSED NR 1 BLD AND LT PACK, WENT TO IDLE PWR ON NR 1 ENG. RA N BOTH PACK WITH APU AND WITH NR 1 AND 3 ENG, COULDN'T DUP. CK TEMP GUN FOR HOT SPOT, NONE FOUND. LEAK CHK GOOD AT HIG H POWER CW (144405). 2 L 7 3 4F RT A3WE 1998082800916 19980828 00916 NM 1998 8 28 98FDEA00531 1 19980821 A 3610 1897403 PRECOOLER DOUG MD11 MD11 3023602 NM PNEU SYSTEM FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 583FE 48421 DURING CLIMB, AIR MANIFOLD NR 2 FAIL ALERT CAME ON, W/I 10 TO 15 SECONDS OF THE NR 2 MANIFOLD FAIL ALERT, GOT THE NR 3 B LEED AIR OFF ALERT. FOUND THE PRECOOLER LEAKING INTERNALLY. REMOVED AND REPLACED THE PRECOOLER, ALSO REMOVED AND REPLA CED 14A AND B MANIFOLD SENSE ELEMENTS, MANIFOLD DECAY CHECK WAS GOOD PER THE JRH. 2 L 7 3 4F RT A22WE 1998082800917 19980828 00917 NM 1998 8 28 98FDEA00532 1 19980825 A 5320 65196063 SHEAR WEB BOEING 727 72725C 138400H NM BS 116-1174 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 CORROSION (C53-224-08) ON SHEAR WEB BS 1166 TO 1174, LBL 37, WL 208. *S/D* REPAIRED SHEAR WEB AT BS 1166 TO 1174, LBL 37, WL 208 PER FED-EX SRM 51-40-2. 2 L 7 3 4F A3WE 1998082800918 19980828 00918 WP 1998 8 28 ABXA9800794 1 19980825 A 5610 5613217507 WINDOW DOUG DC8 DC863 302198A WP LT COCKPIT JAMMED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 822AX 46079 DURING PREFLIGHT, FOUND CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) DIFFICULT TO OPEN AND WAS OCCASIONALLY JAMMING. LUBRICA TED LINKAGE. WINDOW OPERATES NORMAL. 2 L 7 4 4F 4A25 1998082800919 19980828 00919 WP 1998 8 28 ABXA9800781 1 19980806 A 5320 991224369 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT FS 1021 BELOW LONGERON 14 RT. REPAIRED SHEAR TIE IAW DC9 SRM 53-03, FIG 6. 2 L 7 2 4F A6WE 1998082800920 19980828 00920 WP 1998 8 28 ABXA9800782 1 19980814 A 5320 9912243227 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1056 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, FOUND SHEAR TIE CRACKED AT FS 1056 BETWEEN LONGERON 14L AND 16L. REPLACED SHEAR TIE AND CLIPS IAW DC9 S RM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082800921 19980828 00921 WP 1998 8 28 ABXA9800783 1 19980807 A 5320 995773925N SHEAR TIE DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, FOUND CRACKED SHEAR TIE AT FS 1021 BETWEEN LONGERON 14L AND 15L. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082800922 19980828 00922 WP 1998 8 28 ABXA9800784 1 19980807 A 5320 995773925N SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, FOUND A CRACKED SHEAR TIE AT FS 1021 BETWEEN LONGERON 15L AND 16L. REPLACED SHEAR TIE IAW DC9 SRM 51-30 -2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082800923 19980828 00923 WP 1998 8 28 ABXA9800785 1 19980811 A 5230 WEB DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR STRUCTURE CRACKED ABOVE THE FORWARD HINGE. REPLACED WEB AND FITTING IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998082800924 19980828 00924 WP 1998 8 28 ABXA9800786 1 19980812 A 5311 56410082 FRAME DOUG DOUG DC8 DC862 3021970 WP BS 798 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 FRAME STATION 798 RIGHT BELOW CUSP AREA CORRODED OUT ON FORWARD AND AFT SIDE OF FITTING. REPAIRED IAW DWG 5641008 AND A BX REA D853-22904 MR. 2 L 7 4 4F 4A25 1998082800925 19980828 00925 WP 1998 8 28 ABXA9800787 1 19980812 A 5320 5615328 DOUBLER DOUG DOUG DC8 DC862 3021970 WP BS 879 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 LONGERON 24R AT STATION 879 HAS A 3.6 INCH LONG CRACK RUNNING FORWARD AND AFT OF FITTING LOCATION. REPAIRED IAW DC8 SRM 53-2-2 AND 51-1-20D. 2 L 7 4 4F 4A25 1998082800926 19980828 00926 WP 1998 8 28 ABXA9800788 1 19980812 A 5320 47731462 FITTING DOUG DOUG DC8 DC862 3021970 WP BS 340-350 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT UPPER CUSP MEMBRANE FITTING HAS HEAVY CORROSION FS 340 TO 350. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998082800927 19980828 00927 WP 1998 8 28 ABXA9800789 1 19980812 A 5720 5769545 ANGLE DOUG DOUG DC8 DC862 3021970 WP WS 778.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT WING LEADING EDGE AT STATION 778.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K 05056-7 003. 2 L 7 4 4F 4A25 1998082800928 19980828 00928 WP 1998 8 28 ABXA9800790 1 19980812 A 5320 4641326N FITTING DOUG DOUG DC8 DC862 3021970 WP BS 1520 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 LONGERON END FITTING AT FRAME STATION 1520, LONGERON 28 LEFT AT MANUFACTURE SPLICE WAS CRACKED AND CORRODED. REPLACED F ITTING IAW DC8 SRM 51-3-0 AND SRM 51-1-20. 2 L 7 4 4F 4A25 1998082800929 19980828 00929 WP 1998 8 28 ABXA9800791 1 19980811 A 5320 5753159 INTERCOSTAL DOUG DOUG DC8 DC862 3021970 WP BS 1500 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 CORRODED AND CRACKED INTERCOSTAL AT FUSELAGE STATION 1500 LONGERON 29R AFT ACCESSORY COMPARTMENT. REPAIRED IAW DC8 SRM 53-4-1, 51-1-8 AND 51-1-21. 2 L 7 4 4F 4A25 1998082800930 19980828 00930 WP 1998 8 28 ABXA9800792 1 19980811 A 5753 5769859 VANE DOUG DOUG DC8 DC862 3021970 WP RT TE FLAP CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 RIGHT INBOARD SLOT VANE OUTBOARD END HAS HEAVY CORROSION UNDER THE SURFACE IN 2 PLACES. REPAIRED SLOT VANE IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1998082800931 19980828 00931 WP 1998 8 28 ABXA9800793 1 19980811 A 5315 9753798501 FLOORBEAM DOUG DOUG DC8 DC862 3021970 WP BS 1540 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 FLOORBEAM 1540 CORRODED FROM LBL 24 TO RBL 38 LOWER FLANGE. REPAIRED FLOORBEAM IAW ABX REA D853-22918 MR. 2 L 7 4 4F 4A25 1998082800932 19980828 00932 WP 1998 8 28 MWEA98909 1 19980817 A 5753 5910041503 VANE DOUG DC9 DC914 3022034 WP LT TE FLAP BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 LEFT INBOARD FLAPVANE INBOARD EDGE IS GOUGED UP TO RIVET HOLE AND EDGE IS BENT. MTC FABRICATED AND INSTALLED DOUBLER RE PAIR. 2 L 7 2 4F A6WE 1998082800933 19980828 00933 WP 1998 8 28 MWEA98910 1 19980817 A 5720 4991149975 CLIP DOUG DC9 DC914 3022034 WP WS 111.5 UNAPPROVED PART A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 400ME 45727 FOUND MATERIAL SUBSTITUTION CLIP ON RIGHT WING ANTENNA STATION XRS 111.5 BETWEEN STRINGER 13 AND 14. MTC FABRICATED AND INSTALLED STRINGER CLIP. 2 L 7 2 4F A6WE 1998082800934 19980828 00934 WP 1998 8 28 MWEA98911 1 19980817 A 5753 2645424537 BUSHINGS DOUG DC9 DC914 3022034 WP LT TE FLAP PITTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND 4 HAT BUSHINGS PITTED ON LEFT FLAP INBOARD HINGE. MTC REMOVED AND REPLACED UPPER BUSHING. 2 L 7 2 4F A6WE 1998082800935 19980828 00935 WP 1998 8 28 MWEA98912 1 19980817 A 5711 99574431 SPAR DOUG DC9 DC914 3022034 WP LT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 40ME 45727 FOUND BARE METAL AND CHAFING ON LEFT WING FRONT SPAR UPPER AND LOWER CHORDS. MTC REWORKED CHAFED AREAS. 2 L 7 2 4F A6WE 1998082800936 19980828 00936 WP 1998 8 28 MWEA98913 1 19980817 A 5320 99101545 CUSP DOUG DC9 DC914 3022034 WP BS 786 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND CRACKED CUSP MEMBRANE ON LEFT SIDE FORWARD OF STATION 786. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998082800937 19980828 00937 WP 1998 8 28 MWEA98914 1 19980817 A 5311 99118775 FRAME DOUG DC9 DC914 3022034 WP BS 953 LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 01 45727 FOUND LOOSE RIVETS IN HARNESS BRACKET AT AFT ACCESSORY COMPARTMENT CANTED FRAME RIGHT SIDE STATION 953. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998082800938 19980828 00938 WP 1998 8 28 MWEA98915 1 19980817 A 5320 9957739 SHEAR TIE DOUG DC9 DC914 3022034 WP BS 766 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 CRACKED SHEAR TIE AFT LEG STA 766 BETWEEN LONG 15 AND 16L. MTC FABRICATED AND INSTALLED SHEAR TIE. 2 L 7 2 4F A6WE 1998082800939 19980828 00939 WP 1998 8 28 MWEA98916 1 19980817 A 5753 995806 SKIN DOUG DC9 DC914 3022034 WP LT TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 LT WING FLAP TRAIL END SEGMENT NUMBER 2 LOWER OUTBOARD EDGE CHAFED. FABBED NEW WEB ALODINED PRIMED AND INSTALLED. 2 L 7 2 4F A6WE 1998082800940 19980828 00940 WP 1998 8 28 MWEA98917 1 19980817 A 5320 591032 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 370-389 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FORWARD LOWER CARGO PIT STATION 370 389 L29L INTERCOSTAL BENT AND DISTORTED. MTC FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 1998082800941 19980828 00941 WP 1998 8 28 MWEA98918 1 19980817 A 5320 591012 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 379-389 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 400ME 45727 FORWARD LOWER CARGO PIT STATION 379 389 L29R INTERCOSTAL MISDRILLED HOLES. MTC FABRICATED AND INSTALLED INTERCOSTAL. 2 L 7 2 4F A6WE 1998082800942 19980828 00942 WP 1998 8 28 MWEA98919 1 19980817 A 5320 9957914501 INTERCOSTAL DOUG DC9 DC914 3022034 WP BS 351-370 BENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FORWARD LOWER CARGO PIT STATION 351 370 CENTER CEILING INTERCOSTAL BENT AND DISTORTED. MTC FABRICATED AND INSTALLED INT ERCOSTAL. 2 L 7 2 4F A6WE 1998082800943 19980828 00943 WP 1998 8 28 MWEA98920 1 19980817 A 5230 DOOR DOUG DC9 DC914 3022034 WP CARGO COMPT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND CRACK IN FORWARD CARGO PIT LOWER FORWARD EDGE OF CARGO DOOR. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998082800944 19980828 00944 WP 1998 8 28 MWEA98921 1 19980817 A 5720 9957757501 WEB DOUG DC9 DC914 3022034 WP WING CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 WEB AT UPPER WING TRAILING EDGE IS CRACKED AT OUTBOARD END NUMBER 2 SPOILER PANEL. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998082800945 19980828 00945 WP 1998 8 28 MWEA98922 1 19980817 A 5311 995821519 FRAME DOUG DC9 DC914 3022034 WP BS 737 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 AFT CARGO FRAME AT STA 737 L30 HAS DRILL DAMAGE. MTC FABRICATED AND INSTALLED ANGLE FILLER DOUBLER AND SPACER. 2 L 7 2 4F A6WE 1998082800946 19980828 00946 WP 1998 8 28 MWEA98923 1 19980817 A 5753 9910010153 SPAR DOUG DC9 DC914 3022034 WP RT TE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 RIGHT WING FLAP FORWARD SPAR BETWEEN INBOARD FLAP TRACK OUTBOARD MOVEABLE VANE MENCHANISM EXCESSIVE BARE METAL. MTC FAB RICATED AND INSTALLED WEB. 2 L 7 2 4F A6WE 1998082800947 19980828 00947 WP 1998 8 28 MWEA98924 1 19980817 A 5313 2779224 LONGERON DOUG DC9 DC914 3022034 WP BS 786 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 CRACK VERTICAL LEGS OF LONGERON 17 RIGHT STATION 786 AFT SIDE OF BULKHEAD. MTC FABRICATED AND INSTALLED LONGERON AND SP LICES. 2 L 7 2 4F A6WE 1998082800948 19980828 00948 WP 1998 8 28 MWEA98925 1 19980817 A 5414 995822024 SKIN DOUG DC9 DC914 3022034 WP NR 2 PYLON CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 NUMBER 2 PYLON INBOARD SIDE OF LEADING EDGE AIRCRAFT SKIN CHAFED AT BOTTOM. MTC FABRICATED AND INSTALLED DOUBLER REPAIR . 2 L 7 2 4F A6WE 1998082800949 19980828 00949 WP 1998 8 28 MWEA98926 1 19980817 A 5210 59100817 SKIN DOUG DC9 DC914 3022034 WP PAX DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 XRAY INDICATION CRACK UNDER REPAIR FORWARD TOP CORNER L1 DOOR. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998082800950 19980828 00950 WP 1998 8 28 MWEA98927 1 19980817 A 5312 5910163 BULKHD DOUBLER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 PASSENGER CABIN AFT PRESS BULKHEAD FORWARD FACE GOUGE AT DOUBLER REPAIR. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1998082800951 19980828 00951 WP 1998 8 28 MWEA98928 1 19980817 A 5330 591140089 SKIN DOUG DC9 DC914 3022034 WP BS 101 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 EXTERNAL FUSELAGE SKIN DENTED AT STATION 101 L19L. MTC FABRICATED AND INSTALLED DOUBLER FILLER AND FINGER. 2 L 7 2 4F A6WE 1998082800952 19980828 00952 WP 1998 8 28 MWEA98930 1 19980817 A 5311 9911538506N FRAME DOUG DC9 DC914 3022034 WP BS 604 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 INSPECT REPAIR FOR CRACK GROWTH AS PER SB 53-100 ON FRAME STA 604 RIGHT MAIN LANDING GEAR WHEEL WELL. MTC REMOVED AND R EPLACED FRAME. 2 L 7 2 4F A6WE 1998082800953 19980828 00953 WP 1998 8 28 MWEA98931 1 19980817 A 5330 59114017 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 EXTERNAL SKIN AROUND DRAIN HOLE L21-22R CORRODED. MTC REMOVED AND REPLACED FASTENERS. 2 L 7 2 4F A6WE 1998082800954 19980828 00954 WP 1998 8 28 MWEA98932 1 19980817 A 5210 5910082 ANGLE DOUG DC9 DC914 3022034 WP PAX DOOR GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FORWARD ENTRANCE DOOR GOUGED AT ATTACH ANGLE AT TOP AFT CORNER OF DOOR TORQUE BOX FS 200. MTC FABRICATED AND INSTALLED ANGLE. 2 L 7 2 4F A6WE 1998082800955 19980828 00955 WP 1998 8 28 MWEA98933 1 19980817 A 5330 9958220C SKIN DOUG DC9 DC914 3022034 WP BS 758 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FUSELAGE SKIN STA 758 AT LEFT LEADING EDGE PYLON HAS AREA OF CHAFING. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998082800956 19980828 00956 WP 1998 8 28 MWEA98934 1 19980817 A 5532 5912166 SKIN DOUG DC9 DC914 3022034 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 VERTICAL STABILIZER APPROXIMATE STATION ZY 115 0 CRACK HAS CONTINUED TO CRACK PAST STOP DRILL LEFT SIDE APPROXIMATE 6 IN CHES FROM TRAILING EDGE SEAM. MTC REMOVED AND REPLACED SPLICE. 2 L 7 2 4F A6WE 1998082800957 19980828 00957 NM 1998 8 28 DLM88981727 1 19980821 A 3231 BRACKET DOUG MD88 MD88 3023688 NM LT MLG DOOR BROKEN A DALA O OTHER O OTHER LD LANDING 1 SO 27 993DL 53345 DURING DESCENT, GEAR DOOR LIGHT CAME ON AFTER LOWERING GEAR. A/C WAS MET ON THE RUNWAY AND THE DOORS TIED UP SO THAT TH E A/C COULD TAXI TO THE GATE. FOUND LT GEAR DOOR PROX SWITCH BRACKET BROKEN. REPLACED SAME. 2 L 7 2 4F RT A6WE 1998082800958 19980828 00958 NM 1998 8 28 DLM88981729 1 19980821 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM BS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 997DL 53364 FUSELAGE SKIN WAS FOUND DENTED AT APPROX FS 218 BETWEEN L18L AND L19L. REPAIRED PER ERA 332080-14. 2 L 7 2 4F RT A6WE 1998082800959 19980828 00959 NM 1998 8 28 DL72S981730 1 19980821 A 5720 65583758 CHORD BOEING 727 727232 1384082 NM BS 761 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 DURING ACCOMPLISHMENT OF 4-58560-3AD, A CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSELAGE UPPER ATTACH CHORD. C RACK PROPAGATES FROM THE EDGE OF THE CHORD ABOVE THE TWO FWD MOST FASTENER HOLES AND TRAVELS DOWN. REPAIRED PER ERA 332 062-14AD. 2 L 7 3 4F A3WE 1998082800960 19980828 00960 NM 1998 8 28 DL733981732 1 19980821 A 2910 LINE AS11608026 BOEING 737 737347 1384647 NM B-HYD SYST PUNCTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 3301 23181 EN ROUTE EXPERIENCED TOTAL HYD SYS-B FAILURE CONTACTED ATL. MTC AND DISPATCH ADVISED LANDING IN LAS. T/S B-HYD SYS FOU ND PIN HOLE IN FLEX HOSE FROM PUMP TO PRESS MODULE. INSTALLED APPROVED INTERIM HYD HOSE. 2 L 7 2 4F RT A16WE 1998082800961 19980828 00961 NM 1998 8 28 DL72S981733 1 19980818 A 5330 SKIN BOEING 727 727232 1384082 NM BS 680 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 515DA 21431 AN AREA OF CORROSION WAS FOUND IN THE BELLY SKIN AT FS 680 AND STR 28R. THE CORROSION WAS REMOVED WITH A SKIN CUTOUT. T HE CUTOUT WAS NEAR TWO PREVIOUS REPAIRS WHICH WERE REMOVED AND ONE LARGER ALUMINUM EXTERNAL SKIN DOUBLER WAS INSTALLED P ER THE GUIDELINES OF B727 SRM 53-30-3 AND S/B 727-53A203. THE REPAIR WAS DOCUMENTED PER ER/A 365455-14AD. 2 L 7 3 4F A3WE 1998082800962 19980828 00962 NM 1998 8 28 DL72E981734 1 19980223 A 5753 ANGLE BOEING 727 727247 138408F NM NR 2 TE MIDFLAP CRACKED A DALA O OTHER O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 DURING SHOP VISIT THE AFT CHORD ANGLE WAS FOUND CRACKED IN 3 LOCATIONS 19, 33 AND 37 FROM I/B END OF FLAP. THE ANGLE WA S REPAIRED PER MM 57-52-0, FIG 802 BY REMOVING DAMAGED SECTION OF ANGLE AND SPLICING IN A NEW SECTION. 2 L 7 3 4F A3WE 1998082800963 19980828 00963 NM 1998 8 28 DL72W981735 1 19980821 A 5754 ANGLE BOEING 727 727247 138408F NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 FOUND ON B2 LETTER CK, .5 INCH CRACK COVE SKIN ATTACH ANGLE I/B SIDE OF I/B UPSTOP NR 4 SLAT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998082800964 19980828 00964 NM 1998 8 28 DL72W981736 1 19980821 A 5320 WEB BOEING 727 727247 138408F NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 297WA 22534 FOUND DURING B-2 LETTER CHECK, VERT WEB ABOVE S- DUCT AT STA 1303 HAS A .5 INCH CRACK ON RT SIDE AT CUTOUT FOR STR. REP AIRED PER SRM 53-10-4 FIG 7. 2 L 7 3 4F A3WE 1998082800965 19980828 00965 NM 1998 8 28 DL72S981737 1 19980822 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 516DA 21432 AFT OVERHEAD EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPS CK GOOD. 2 L 7 3 4F A3WE 1998082800966 19980828 00966 NM 1998 8 28 DL72W981738 1 19980819 A 3350 BATTERY 900835A BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2815W 4577 20871 OVERWING EMERGENCY EXIT LIGHTS FLASHING. REPLACED RACK AND BATTERY, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998082800967 19980828 00967 NM 1998 8 28 DLM11981739 1 19980822 A 3397 0201720005 WIRE HARNESS DOUG MD11 MD11 3023602 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 808DE 48479 EMERGENCY LIGHT AT SEAT 37B INOP. REPLACED LIGHT/HARNESS ASSY. 2 L 7 3 4F RT A22WE 1998082800968 19980828 00968 NM 1998 8 28 DL72E981740 1 19980823 A 3350 900542 RACK BOEING 727 727247 138408F NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 LT OVERWING EMERGENCY LIGHT INOP. REPLACED RACK. 2 L 7 3 4F A3WE 1998082800969 19980828 00969 NE 1998 8 28 DLL10981741 2 19980823 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 3 FAILED A DALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 735D 54295 193C1226 010607 NR 3 ENG SHUT DOWN, LOW OIL PRESS. FOUND METAL ON CHIP DETECTORS. REPLACED ENGINE. 2 L 7 3 4F 4 F A23WE E12EU 1998082800970 19980828 00970 NM 1998 8 28 DL72S981742 1 19980823 A 7930 BYPASS LIGHT BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE ILLUMINATED A DALA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 27 475DA 20752 700438 NR 3 ENG FILTER BYPASS LIGHT ILLUM. ENG WAS SHUTDOWN. ENG WINDMILLED FOR REST OF FLT. REMOVED AND INSPECTED NR 3 OIL FILTER, NO MATERIAL IN FILTER. CHIP DETECTOR ALSO CLEAN. FWD OIL BYPASS SYS TO MCO AND PLAC PER 79-00-02. WINDMILLING OK PER MM 71-00 PG 2. 2 L 7 3 4F 4 F A3WE E2EA 1998082800971 19980828 00971 NM 1998 8 28 DL72W981743 1 19980823 A 2150 SWITCH BOEING 727 727247 138408F NM LT PACK FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 2810W 20648 ON DESCENT, MOMENTARY WHITE SMOKE ON COCKPIT AND A MUSTY OILY SMELL IN CABIN AND COCKPIT. GALLEYS AND GASPER FANS TURNE D OFF CABIN RAISED TO 9500 FT SMOKE AND SMELL DISSIPATED. RAN ENGINES FOUND LEFT PACK OVERHEATING BUT WOULD NOT TRIP. R EPLACED TURBINE INLET OVER HEAT SWITCH AND TURBINE INLET OVERHEAT SWITCH AND DUCT OVERHEAT 250 DEGREE SWITCH. RAN ENGIN ES, LEFT PACK OPS CKS OK. 2 L 7 3 4F A3WE 1998082800972 19980828 00972 NM 1998 8 28 DL73E981744 1 19980822 A 2721 BEARING 65709736 BOEING 737 737247 138448D NM RUDDER TRIM WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 377DL 23604 RUDDER TRIM AND CENTERING UNIT, (P/N 65-70973-6) FOUND WORN BEARING, (P/N BACB10B257R) ITEM 220, FIG 1, 27-20-4-1. ALSO , FOUND ARM ASSY (P/N 69-51251-6) HAD SEPARATION OF SIDE PLATE ON END WITH BRG (P/N B538DDFS464). REPAIRED SAME. 2 L 7 2 4F A16WE 1998082800973 19980828 00973 NM 1998 8 28 DLM88981746 1 19980824 A 5330 2953657501 SKIN DOUG MD88 MD88 3023688 NM BS 39 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 997DL 53364 TWO DENTS WERE FOUND IN THE UNPRESSURIZED AREA OF THE NOSE SKIN JUST AFT OF THE RADOME. THE DAMAGE WAS REMOVED WITH A 6 BY 17 CUTOUT. REPAIRED PER ERA 363630-14. 2 L 7 2 4F RT A6WE 1998082800974 19980828 00974 NM 1998 8 28 DL72L981748 1 19980824 A 5330 65545664 SKIN BOEING 727 727232 1384082 NM BS 490 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THE SKIN WAS FOUND CORRODED BETWEEN FS 480 AND 500 AT STRINGER 28R. THE CORROSION WAS CUTOUT RESULTING IN A 16.75 LONG X 3.25 WIDE CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER, INSTALLED PER PROCEDURES OUTLINED IN B72 7 SRM 53-30-3, FIG 3 AND DOCUMENTED PER ER/A 365500-14, REV B . 2 L 7 3 4F A3WE 1998082800975 19980828 00975 NM 1998 8 28 DL72L981749 1 19980824 A 5330 65C13913 SKIN BOEING 727 727232 1384082 NM BS 1055 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THE FUSELAGE SKIN AT FS 1055 AND STRINGER 29L WAS FOUND WITH CORROSION RESULTING IN A 2 X 3 CUTOUT TO REMOVE THE DAMAGE. THE CUTOUT WAS ADJACENT TO TWO OTHER EXISTING SKIN REPAIRS. ONE OF THE EXISTING REPAIRS WAS REMOVED AND REPLACED WITH A NEW EXTERNAL ALUMINUM DOUBLER TO INCORPORATE PREVIOUS DAMAGES AND TO OVERLAP AN EXISTING REPAIR. ALL REPAIRS WILL BE REMOVED AT NEXT MV AND A NEW SKIN INSTALLED. 2 L 7 3 4F A3WE 1998082800976 19980828 00976 NM 1998 8 28 DL72L981750 1 19980824 A 5330 65C139131 SKIN BOEING 727 727232 1384082 NM BS 990 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THE FUSELAGE SKIN AT FS 990 AND STRINGER 28R WAS FOUND CUTOUT TO REMOVE CORROSION OVER A 2 X 3 AREA. THE CUTOUT WAS ADJ ACENT TO AN EXISTING REPAIR INSTALLED TO REPAIR ANOTHER SKIN CORROSION CUTOUT. THE EXISTING REPAIR WAS REMOVED AND A NE W EXTERNAL ALUMINUM DOUBLER AND TRIPLER WAS INSTALLED TO REPAIR BOTH CUTOUTS. THE REPAIR WAS ACCOMPLISHED PER ER/A 2 31173-14, REV D. 2 L 7 3 4F A3WE 1998082800977 19980828 00977 WP 1998 8 28 DLL10981751 1 19980822 A 5711 1503230103 SPAR CAP LKHEED 1011 10113851 5265010 WP BS 1103 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 728DA 193C1173 THE UPPER SPAR CAP OF THE FS 1103 INTERMEDIATE SPAR WAS FOUND WITH TYPICAL CRACKING AT LEFT END. THE CRACK WAS BEYOND T HE ALLOWABLE LIMITS SPECIFIED IN LAC S/B 093-57-087. THE CAP WAS CUT I/B OF LBL 94.5 AND A NEW SECTION WAS SPLICED IN W ITH STEEL REPAIR ANGLES AND STRAPS PER ER/A 365477-14, REV B. 2 L 7 3 4F A23WE 1998082800978 19980828 00978 NM 1998 8 28 DL72S981754 1 19980824 A 5240 STRAP BOEING 727 727232 1384082 NM L-2 DOOR OUT OF POSITION A DALA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 27 527DA 21587 YELLOW BARRIER STRAP CAUGHT HALF WAY OUT L2 DOOR, UNABLE TO RETRACT IN FLIGHT. AIR TURNBACK. REMOVED YELLOW SAFETY STR AP FROM DOOR JAMB. 2 L 7 3 4F A3WE 1998082800979 19980828 00979 NM 1998 8 28 DL72W981755 1 19980824 A 5320 WEB BOEING 727 727247 138408F NM BS 1293 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 RT VERTICAL TORQUE BOX WEB UPPER LIGHTENING HOLE HAS .375 INCH CRACK AT STA 1293. REPAIRED PER M/M 53-11-0 FIG 819. 2 L 7 3 4F A3WE 1998082800980 19980828 00980 NM 1998 8 28 DLM88981756 1 19980824 A 2424 GCU 947F9453 DOUG MD88 MD88 3023688 NM E/E COMPT FAILED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 27 988DL XJ2131B 53339 ON T/O ROLL (115 KTS), LT AC BUS FAIL WITH AC CROSSTIE LOCK-OUT. ABORTED T/O. CHECKED LT AND RT CSD OIL SERV AND FILTE R BUTTON FOUND LT ENG GEN CONT UNIT DIST FAULT ILLUM. CHECKED LT GEN SYS DPCTS. CKS OK INSP GEN LEADS ON LT ENG. NO D EFECTS NOTED. REPLACED LT GCU, RAN ENGS X-TIES AND GEN OPN NORMAL. 2 L 7 2 4F RT A6WE 1998082800981 19980828 00981 NM 1998 8 28 DL767981757 1 19980822 A 3350 LIGHT BOEING 767 767232 1385132 NM CABIN DAMAGED A DALA K NONE O OTHER TX TAXI/GRND HDL 1 SO 27 103DA 22215 EMERGENCY TRACK LIGHTING DAMAGED BY 2L DOOR. INSPECTED ALL EMERGENCY TRACK LIGHTING, REPAIRED DAMAGE, CKS OK. 2 L 7 2 4F RT A1NM 1998082800982 19980828 00982 NM 1998 8 28 DL73E981758 1 19980825 A 5320 6545410225 DOUBLER BOEING 737 737247 138448D NM BS 682 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 DURING RTN INSP PER SI3-56673-12 OF THE LH AND RH LONGITUDINAL OVERWING FLOORBEAMS, CRACKS WERE FOUND IN THE WEB DOUBLER S. THE CRACKS ARE LOCATED IN THE DOUBLERS IN THE UPPER AFT CORNER OF THE AILERON CONTROL QUADRANT CUTOUTS AT THE LBL/RB L 24.82 AND APPROX STA 682. AT BOTH LOCATIONS THE CRACKS EXTEND FROM THE UPPER EDGE OF THE DOUBLER TO THE CONTROL QUAD OPENING AND SEPARATE THE WEB INTO TWO PIECES. REWORKED PER ERA 332082-14AD. 2 L 7 2 4F A16WE 1998082800983 19980828 00983 NM 1998 8 28 DL757981759 1 19980824 A 5754 WEDGE BOEING 757 757232 1384965 NM NR 3 LE FLAP DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 THE NR 3 SLAT TRAILING EDGE WEDGE WAS FOUND DENTED FROM A BIRD STRIKE. THE WEDGE WAS REPAIRED PER B757 SRM 51-70-10 (AS REFERENCED IN SRM 57-43-02). SINCE THE SLAT WEDGES ARE THE SUBJECT OF AD T91-22-51, THE REPAIR WAS DOCUMENTED PER ER/A 365517-14AD. 2 L 7 2 4F RT A2NM 1998082800984 19980828 00984 NM 1998 8 28 DL72L981760 1 19980821 A 5521 657278419 SPAR BOEING 727 727232 1384082 NM RT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 THE REAR SPAR OF THE RT ELEVATOR WAS FOUND WITH A .1875 INCH TYPICAL CRACK AT CENTER HINGE BRACKET SHEAR PLATE. THE CRA CK WAS STOP DRILLED PER THE REQUIREMENTS OF AD 96-06-05 AND S/B 727-55-0089. THE REPAIR WAS DOCUMENTED PER ER/A 365499- 14AD WHICH ESTABLISHES A RE-INSPECT OF THE REAR SPAR WITHIN 1600 CYCLES AND TERMINATING MODIFICATION WITHIN 3200 CYCLES. 2 L 7 3 4F A3WE 1998082800985 19980828 00985 NM 1998 8 28 DL72W981761 1 19980822 A 5753 SHIM BOEING 727 727247 138408F NM LT TE FLAP MIGRATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 THE I/B TRACK OF THE LT WING I/B FLAP WAS FOUND WITH THE LAMINATED SHIM MIGRATED .25 AS TYPICAL OF S/B 727-57-0178 AND AD 90-07-05. THE SHIM WAS REPLACED PER THE REQUIREMENTS OF THE S/B AND DOCUMENTED PER ER/A 365509-14AD. 2 L 7 3 4F A3WE 1998082800986 19980828 00986 NM 1998 8 28 DLM88981762 1 19980824 A 3244 TIRE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RT MLG FAILED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION TO TAKEOFF 1 SO 27 934DL 49721 725921 NUMEROUS COMPRESSOR STALLS ON RIGHT ENGINE AFTER LIFTOFF. NR 4 MAIN TIRE RECAP, SEPARATED FROM OUTBOARD PORTION OF TIR E AND CAUSED FOD DAMAGE TO NR 2 FAN, NOSE COWL AND LOWER COWL DOOR. FOUND EXTENSIVE DAMAGE TO FAN AND COMPRESSOR SECTIO N AND REQUIRED ENGINE CHANGE. 2 L 7 2 4F 4 F RT A6WE E9NE 1998082800987 19980828 00987 NM 1998 8 28 DL72S981764 1 19980824 A 3350 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 407DA 14180 21151 ON L/O, AFT OVERWING ESCAPE LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998082800988 19980828 00988 NM 1998 8 28 DL72S981765 1 19980825 A 2782 BRACKET BOEING 727 727232 1384082 NM LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 NR 1 L/E FLAP ACTUATOR ATTACH BRACKET CRACKED O/B LOWER END. FOUND ON D1 LETTER CK. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998082800989 19980828 00989 NM 1998 8 28 DL767981766 1 19980825 A 3350 0201720002 LIGHT BOEING 767 767232 1385132 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 102DA 22214 AFT EMERGENCY LIGHT ON SEAT 25F INOP. REPLACED LIGHT ASSY, CKS GOOD. 2 L 7 2 4F RT A1NM 1998082800990 19980828 00990 NM 1998 8 28 SCNA98711 1 19980810 A 5320 SHEAR WEB BOEING 727 7272J4 1384006 NM BS 700-720 CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING A HEAVY MAINT CHECK, A CRACK WAS FOUND IN THE UPPER CHORD OF THE SHEAR WEB BETWEEN FLOORBEAMS STA 700 AND 720. R EMOVED CRACKED SHEAR WEB IN UPPER CHORD. FABRICATED NEW SHEAR WEB FROM BAC14902785 7075 T3 .050 IAW B727 SRM 531002. TR EATED AND PRIMED IAW B727 SRM 511002 MM 512002. INSTALLED SHEAR WEB IAW B727 SRM 513001. 2 L 7 3 4F RT A3WE 1998082800991 19980828 00991 WP 1998 8 28 RRXA98387 1 19980727 A 5320 S2537716 DOUBLER DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT FOUND FRAME DOUBLER WITH CORROSION DAMAGE, AND WITH MISDRILLED HOLES. REMOVED PREVIOUS DOUBL ER REPAIR, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER REPAIR IAW FAA APPROVED TIMCO DER ENG INEERING SKETCH REO-05106. 2 L 7 4 4F RT 4A25 1998082800992 19980828 00992 WP 1998 8 28 RRXA98388 1 19980727 A 5553 SKIN DOUG DC8 DC871F 302199D WP LT TE FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND LEFT WING OUTBOARD FLAP WEDGE HAD PREVIOUS BLENDOUT ON TOP INBOARD CORNER AT THE ATTAC H SEAM GOUGED, BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND I NSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05117. 2 L 7 4 4F RT 4A25 1998082800993 19980828 00993 WP 1998 8 28 RRXA98389 1 19980727 A 5542 5655077 SKIN DOUG DC8 DC871F 302199D WP RUDDER DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND RUDDER, LEFT SIDE, SKIN GOUGE/DENTED, AT STA=XR 90. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-051 19. 2 L 7 4 4F RT 4A25 1998082800994 19980828 00994 WP 1998 8 28 RRXA98390 1 19980727 A 5320 5644011501 ANGLE DOUG DC8 DC871F 302199D WP FUSELAGE CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM ATTACHMENT ANGLE WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 85 7 BLL 16 AND WL -1. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05125. 2 L 7 4 4F RT 4A25 1998082800995 19980828 00995 WP 1998 8 28 RRXA98391 1 19980728 A 5311 S2537716 FRAME DOUG DC8 DC871F 302199D WP BS 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT FOUND FRAME FLANGE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM, AT STA 1140 AND LONGERON 35 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APP ROVED TIMCO DER ENGINEERING SKETCH REO-05132. 2 L 7 4 4F RT 4A25 1998082800996 19980828 00996 WP 1998 8 28 RRXA98392 1 19980729 A 5311 S2537716 FRAME DOUG DC8 DC871F 302199D WP BS 1080 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLES, AT STA 1080 AND LONGERON 29 LEFT. REMOVED DAMAGED SECTIO N, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKE TCH REO-05133. 2 L 7 4 4F RT 4A25 1998082800997 19980828 00997 WP 1998 8 28 RRXA98393 1 19980730 A 5320 5755564 DOOR FRAME DOUG DC8 DC871F 302199D WP BS 474. MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT FOUND R1 DOOR JAMB FRAME WITH MISDRILLED HOLE, AT STA 474.347. REMOVED DAMAGED SECTION, TREA TED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO -05138. 2 L 7 4 4F RT 4A25 1998082800998 19980828 00998 WP 1998 8 28 RRXA98394 1 19980729 A 5320 56122987 PRESSURE PANEL DOUG DC8 DC871F 302199D WP BS 60 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND PRESSURE PANEL WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA -60 AND BLL 30. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED T IMCO DER ENGINEERING SKETCH REO-05143. 2 L 7 4 4F RT 4A25 1998082800999 19980828 00999 WP 1998 8 28 RRXA98395 1 19980729 A 5320 56122987 PRESSURE PANEL DOUG DC8 DC871F 302199D WP BS 15-29 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND PRESSURE PANEL WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA -15 TO STA -29 AND BLR 30. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05144. 2 L 7 4 4F RT 4A25 1998082801000 19980828 01000 WP 1998 8 28 RRXA98396 1 19980729 A 5313 5611546061 LONGERON DOUG DC8 DC871F 302199D WP BS 160 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND LONGERON 20 RIGHT WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 160. REMOVE D DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05147. 2 L 7 4 4F RT 4A25 1998082801001 19980828 01001 WP 1998 8 28 RRXA98397 1 19980806 A 3232 4649765501 FITTING DOUG DC8 DC871F 302199D WP MLG DOOR ACT MISMANUFACTURED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, PERFORMED REQUIREMENTS IAW SB 32-171, LEFT AND RIGHT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING NEEDED TO BE SPOTFACED TO INSTALL FASTENERS. 2 L 7 4 4F RT 4A25 1998082801002 19980828 01002 WP 1998 8 28 RRXA98398 1 19980731 A 2750 56537498 FITTING DOUG DC8 DC871F 302199D WP RT TE FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, FLAP, EXHAUST GATE ACTUATING FITTING GOUGED BEYOND LIMITS IAW DC-8 SRM. R EMOVED DAMAGE, INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05157. 2 L 7 4 4F RT 4A25 1998082801003 19980828 01003 WP 1998 8 28 RRXA98399 1 19980731 A 5753 57699332 VANE DOUG DC8 DC871F 302199D WP RT TE FLAP WORN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, OUTBOARD SLOT VANE ATTACHMENT HOLES WORN AND OUT OF ROUND. REMOVED DAMAGE D SECTIONS, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05160. 2 L 7 4 4F RT 4A25 1998082801004 19980828 01004 WP 1998 8 28 RRXA98400 1 19980805 A 5315 5644657 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM, VERTICAL FLANGE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 920 AND LONGERON 21 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05175. 2 L 7 4 4F RT 4A25 1998082801005 19980828 01005 WP 1998 8 28 RRXA98401 1 19980805 A 5311 3614944 FRAME DOUG DC8 DC871F 302199D WP BS 1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FRAME FLANGE WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1060 AND LONGERO N 26 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05187. 2 L 7 4 4F RT 4A25 1998082801006 19980828 01006 WP 1998 8 28 RRXA98402 1 19980806 A 5311 564022231 FRAME DOUG DC8 DC871F 302199D WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FRAME UPPER FLANGE WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 1260 BETWEE N LONGERONS 34 LEFT AND 35 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH R EO-05188. 2 L 7 4 4F RT 4A25 1998082801007 19980828 01007 WP 1998 8 28 RRXA98403 1 19980810 A 5320 97794801502 DOUBLER DOUG DC8 DC871F 302199D WP BS 1216 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND INNER DOUBLER WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 1216 BETWEEN LON GERONS 34 RIGHT TO LONGERON 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RE PAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05202. 2 L 7 4 4F RT 4A25 1998082801008 19980828 01008 WP 1998 8 28 RRXA98404 1 19980812 A 5315 2707460 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM, UPPER FLANGE WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1300. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED TI MCO ENGINEERING SKETCH REO-05217. 2 L 7 4 4F RT 4A25 1998082801009 19980828 01009 WP 1998 8 28 RRXA98405 1 19980811 A 5311 S2537716 FRAME DOUG DC8 DC871F 302199D WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FRAME INBOARD FLANGE WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM AT STA 1260 BET WEEN LONGERONS 25 LEFT AND 26 LEFT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05224. 2 L 7 4 4F RT 4A25 1998082801010 19980828 01010 WP 1998 8 28 RRXA98406 1 19980811 A 5243 56496351 PANEL DOUG DC8 DC871F 302199D WP HYD SERVICE DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT FOUND LEFT WING, HYDRAULIC SERVICE DOOR, PANEL (-3), CRACKED AND CHAFED ON FLANGE. REMOVED D AMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05230. 2 L 7 4 4F RT 4A25 1998082801011 19980828 01011 WP 1998 8 28 RRXA98407 1 19980817 A 5311 58229291 FRAME DOUG DC8 DC871F 302199D WP BS 1000 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FRAME WITH ELONGATED HOLES, AT STA 1000 AND FOUND LONGERON 35 LEFT WITH CORROSION DAMA GE. REMOVED DAMAGED SECTIONS FROM FRAME, AND CORROSION FROM LONGERON 35L, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05276. 2 L 7 4 4F RT 4A25 1998082801012 19980828 01012 WP 1998 8 28 RRXA98408 1 19980818 A 5320 5641008502 FITTING DOUG DC8 DC871F 302199D WP BS 798 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND FITTING (P/N 5641008-502) WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 798. REMOVED DAMAGED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW FITTING BY MATERIAL SUBSTITUTION, INSTALLED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05278. 2 L 7 4 4F RT 4A25 1998082801013 19980828 01013 WP 1998 8 28 RRXA98409 1 19980817 A 5753 564297032 SKIN DOUG DC8 DC871F 302199D WP RT TE FLAP CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND RIGHT WING, OUTBOARD FLAP, LOWER SKIN WITH CHAFING CAUSED BY FAIRING RUBBING THE SKIN. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED T IMCO DER ENGINEERING SKETCH REO-05280. 2 L 7 4 4F RT 4A25 1998082801014 19980828 01014 WP 1998 8 28 RRXA98410 1 19980821 A 5320 57794952 SUPPORT DOUG DC8 DC871F 302199D WP FUSELAGE DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND PREVIOUS REPAIR TO FLOOR SUPPORT STRUT, DAMAGED CAUSED BY IMPACT FROM CARGO. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO ENGINEERING SKETCH REO-05298. 2 L 7 4 4F RT 4A25 1998082801015 19980828 01015 WP 1998 8 28 RRXA98411 1 19980820 A 5530 STIFFENER DOUG DC8 DC871F 302199D WP VERT STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND VERTICAL STABILIZER, INNER SPAR STIFFENER WITH CORROSION BEYOND LIMITS IAW DC-8 SRM. R EMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMC O DER ENGINEERING SKETCH REO-05303. 2 L 7 4 4F RT 4A25 1998082801016 19980828 01016 WP 1998 8 28 RRXA98412 1 19980821 A 3210 4649496 BUSHING DOUG DC8 DC871F 302199D WP RT MLG DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND RIGHT SIDE, MAIN LANDING GEAR, SIDE BRACE, LINK ASSEMBLY, BORE BUSHING WAS REMOVED TO REMOVE CORROSION, DURING PROCEDURES OVERSIZED HOLE. REPAIRED HOLE AND BUSHING, IAW FAA APPROVED TIMCO DER ENGINEERING S KETCH REO-05311. 2 L 7 4 4F RT 4A25 1998082801017 19980828 01017 WP 1998 8 28 RRXA98413 1 19980825 A 5330 57799114797794 DOUBLER DOUG DC8 DC871F 302199D WP BS 330 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8076U 45941 DURING A MAINTENANCE VISIT, FOUND EXTEROIR, SKIN DOUBLER GOUGED AND TORN, AT STA 330 AND LONGERON 36. REMOVED DAMAGED S ECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERIN G SKETCH REO-05348. 2 L 7 4 4F RT 4A25 1998090300001 19980903 00001 1998 9 3 98FDEA00525 2 19980716 A 7261 O-RING BOEING 727 727233 138408A NM NR 1 ENGINE MISSING A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 25 219FE 21102 98-210 - NR 1 ENG PRIOR TO PUSH HAD OIL QTY OF 4 PLUS GAL AND GAUGE NORM. DURING T/O ROLL PRIOR TO 80 KTS, ALL 3 OIL QT Y GAUGE READ 3.5 GAL AFT ROTATION NR 1 OIL QTY WAS 2.5 CONT TO DROP 1.5. TEST NORM. FOUND OIL SERV CAP O-RING DISPLACE D. REINSTALLED O-RING ON CAP. SERV ENG TO PROPER LIMITS. INSP TAIL PIPE AND ENG NO DEFECT. REF PRATT AND WHITNEY M/M 70-00 PAGE 203. 2 L 7 3 4F RT A3WE 1998090400003 19980904 00003 CE 1998 9 4 CA980325029 1 19980302 A 5713 26220064 STRINGER CESSNA 208 208B 2073701 CE WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1491 (CAN) SAME STRINGER IN EACH WING CRACKED WHERE THE STRINGER ATTACHES TO THE RIB. APPROX .500 INCH LONG ORIGINATING AT R IVET HOLE. 1 H 7 1 3T A37CE 1998090400004 19980904 00004 CE 1998 9 4 CA980325030 1 19980307 A 5713 262200063 STRINGER CESSNA 208 208B 2073701 CE WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1797 (CAN) SAME STRINGER IN EACH WING CRACKED WHERE THE STRINGER ATTACHES TO THE RIB. APPROX .500 INCH LONG ORIGINATING AT RIVET HOLE. 1 H 7 1 3T A37CE 1998090400011 19980904 00011 SW 1998 9 4 CA980415001 1 19980401 A 5551 106997 BRACKET AIRTRC 302272 AIRTRC AT802 AT802 0390305 SW HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 188 (CAN) DURING INSPECTION, A CRACK WAS NOTED ON THE WELD AT THE RIGHT AFT HORIZONTAL STABILIZER LOCATION. REPLACED. 1 L 7 1 3T NC A19SW 1998090400028 19980904 00028 EA 1998 9 4 CA980602034 1 19980314 A 3260 SWITCH DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG INTERMITTENT W B EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 123061 (CAN) AT 25,000 FEET, TURBULENCE ENCOUNTERED RESULTING IN NOSE LANDING GEAR DOOR LIGHT ON. CREW SLOWED AIRCRAFT AND DES CENDED TO 21,000 FEET. DURING DESCENT, THE HIGH BLEEDS TURNED ON AND SHORTLY AFTER, CABIN FILLED WITH SMOKE. CREW TURN ED OFF NR 1 BLEED WHICH CLEARED SMOKE. AT LOWER ALTITUDE, PILOT SELECTED GEAR DOWN TO TRY AND PUT LIGHT OUT, BUT IT STA YED ON. SMOKE DIFFICULTY COULD NOT BE FOUND. DOOR LIGHT PROBLEM FOUND THAT PROXIMITY SWITCH WAS INTERMITTENT, AS A RES ULT OF TURBULENCE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400029 19980904 00029 SW 1998 9 4 CA980602053 1 19980407 A 6310 212040001059 TRANSMISSION BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA OIL JETS LEAKING W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 15605 CPPS6131 (CAN) FOLLOWING INSTALLATION, OIL WAS FOUND LEAKING FROM THE UPPER OIL JETS. O-RING WAS NOT INSTALLED ON THE JET. 1 G 7 1 4U 4 U H4SW E22EA 1998090400032 19980904 00032 1998 9 4 CA980602060 4 19980528 A 3452 TR2061A TRANSPONDER BENDIX BX2000 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP COCKPIT FAILED W H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 3245 P54183 (CAN) CREW REPORTED SMOKE COMING FROM BEHIND THE LEFT HAND INSTRUMENT PANEL JUST ABOVE THE TRANSPONDER, ACCOMPANIED BY E LECTRICAL BURNING SMELL. NR 1 TRANSPONDER TURNED OFF AND SMOKE DISSIPATED. CIRCUIT BOARD OF NR 1 TRANSPONDER BADLY BUR NED. 2 L 7 2 4T 4 T RT A8SW E4WE 1998090400033 19980904 00033 EA 1998 9 4 CA980602064 2 19980415 A 7230 GEAR BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA ENGINE MISALIGNED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 53 PCE50587 (CAN) NEWLY OVERHAULED ENGINE REMOVED DUE TO NOISE IN THE COMPRESSOR. ENGINE RETURNED TO OVERHAUL SHOP. NR 1 AND NR 2 BEARINGS WERE SENT FOR A SPIN CHECK. THE BEARINGS WERE REJECTED DUE TO EXCESSIVE VIBRATION. NEW BEARINGS WERE INSTALLED AND THE NR 1 BEARING SUPPORT ADAPTER HOUSING WAS REPLACED, THE ENGINE WAS RETURNED AND INSTALLED. AFTER 53.2 HOURS ,TH E ENGINE WAS AGAIN REMOVED DUE TO VIBRATION AND NOISE. THE ENG WAS AGAIN RETURNED TO THE OVERHAUL SHOP. THE ADAPTER AS SEMBLY WAS REPLACED AGAIN DUE TO ALIGNMENT AND THE HIGH SPEED BEARING BOSS WAS FOUND OUT OF CONCENTRICITY. THE SUBMITTE R STATES THAT THE REPAIRS WERE NOT DONE PROPERLY. 1 L 7 2 3T 4 T A14CE E4EA 1998090400034 19980904 00034 SW 1998 9 4 CA980602068 1 19980519 A 2435 2762113001 DUCT APC 300SG119Q SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE STARTER/GEN SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 305 12981 880393 (CAN) NOISE HEARD ON START. STARTER GENERATOR COOLING DUCT HAD SEPARATED FROM THE STARTER GENERATOR. PART TC: 412. 2 L 7 2 4T RT A8SW 6 C 3PNE 1998090400037 19980904 00037 NM 1998 9 4 CA980602078 1 19980512 A 2910 5509808 PUMP ABEX 5509808 BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE HYDRAULIC SYS LEAKING W K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA 163610K P678085 (CAN) TWENTY MINUTES BACK FROM YFB, NR 1 PUMP ON 'A' SYSTEM INDICATED LOW PRESSURE DURING COMPLETION OF CHECK LIST. NR 2 PUMP ON 'A' SYSTEM INDICATED LOW PRESSURE. AIRCRAFT LANDED WITHOUT INCIDENT. NR 1 'A' PUMP RIPPLE DAMPENER LEAKING. NR 1 AND NR 2 PUMPS REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998090400038 19980904 00038 NM 1998 9 4 CA980602080 1 19980526 A 2782 ACTUATOR BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE LE FLAP CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA P678085 (CAN) AFTER DEPARTURE, THE AIRCRAFT EXPERIENCED A 'B' SYS FAILURE AND RETURNED TO BLOCKS. DURING FLAP AND GEAR SELECTIO N, THE AIRCRAFT ENTERED AN UNCOMMANDED RIGHT ROLL WHICH THE CREW WAS ABLE TO COMPENSATE FOR. THE OUTBOARD FLIGHT SPOILE R WAS PARTIALLY DEPLOYED AND THE ACTUATOR HAD A CRACKED HOUSING. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998090400041 19980904 00041 NM 1998 9 4 CA980602086 1 19980522 A 2760 82970010327 FITTING DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE SPOILER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 123152 (CAN) HYDRAULIC LEAK FOUND IN THE RIGHT HAND WHEEL WELL. FITTING ON SPOILER LIFT DUMP LINE FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400042 19980904 00042 NM 1998 9 4 CA980602087 1 19980526 A 2932 APT7510004000SW TRANSMITTER AEB2151011 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 0332A 120816 (CAN) DURING WALKAROUND, HYDRAULIC LEAK NOTED COMING FROM NR 1 NACELLE. PRESSURE TRANSDUCER SWITCH BODY WAS LEAKING FOR THE ENGINE DRIVEN PUMP (EDP). 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400051 19980904 00051 EU 1998 9 4 CA980603007 1 19980413 A 3010 BOOT BAG JETSTM JETSTM4112 EU HORIZ STAB CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 6752 (CAN) CREW UNABLE TO ENGAGE RUDDER GUSTLOCK. INVESTIGATION FOUND THAT IT WAS SEIZED. THIS WAS ATTRIBUTED TO THE ANTI-IC E BOOT BEING CRACKED. PART TC: 9,914. 1 L 7 2 4T RT A196 1998090400052 19980904 00052 NM 1998 9 4 CA980603008 1 19980428 A 2731 82760160003002 ELEVATOR TRIM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HORIZ STAB JAMMED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 120175 (CAN) ON ROTATION, F.O. REPORTED EXCESSSIVE BACK PRESSURE ON CONTROL COLUMN. HE THEN INPUT FULL FORWARD ELEVATOR TRIM T O COUNTERACT PITCH UP. ELEVATOR TRIMLOCKED IN FULL FORWARD POSITION AFTER INPUT. REQUIRED EXCESSIVE FORCE TO OVERCOME THE JAM. ON INITIAL INSPECTION, ICE BUILD-UP NOTED ON UPPER SURFACE WHICH WOULD CAUSE HEAVY ELEVATOR CONTROLS. MFG NO TED THAT IF EXCESSIVE FORCE WAS APPLIED IN THE FULL UP OR FULL DOWN POSITION OF THE SCREW JACKS, THEN INITIAL ADDITIONAL FORCE WOULD BE REQUIRED TO RETURN THE SCREW JACKS TOWARDS NEUTRAL. DEHAVILLAND HAS ISSUED AOM 481 TO COVER AND WILL BE TAKING FURTHER ACTION FOR THE OPERATING MANUAL AND INSPECTIONS. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400053 19980904 00053 1998 9 4 CA980603009 4 19980505 A 3421 2587335114 GYRO HONEYWELL BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 29959 8102 82063604 LF05842A (CAN) CREW REPORTED THEY COULD SMELL AN ELECTRICAL OVERHEAT IN-FLIGHT. VERTICAL GYRO FOUND OVERHEATED. PART TC: 39,06 1. 2 H 7 4 4F 4 F RT A49EU E6NE 1998090400054 19980904 00054 NM 1998 9 4 CA980603010 1 19980510 A 7712 3034945 TSCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA 17150 1825 120176 (CAN) ON TAKEOFF ROLL , NR 2 ENGINE TORQUE INDICATION FAILED. NR 2 TORQUE SIGNAL CONDITIONING UNIT (TSCU) WAS REPLACED AND THE SYSTEM TESTED SERVICEABLE. PART TC: 20,787. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400055 19980904 00055 NE 1998 9 4 CA980603011 2 19980512 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE COMP MALFUNCTIONED W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA 20219 14453 120698 (CAN) AN UNUSUAL SOUND AND VIBRATION WAS NOTICED DURING ENGINE START. THE ENGINE WAS REPLACED. PART TC: 24,744. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400062 19980904 00062 EA 1998 9 4 CA980608009 1 19980530 A 2430 XD4N023 RELAY CNDAIR CL600 CL6001A11 1900302 EA DC SYSTEM FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 CA 7045 (CAN) BATTERY CHARGER ANNUNCIATOR ILLUMINATED DURING GROUND OPERATION. RELAY KP7A FOUND FAULTY. WHEN RELAY IS LATCHED BY A DC SENSE CIRCUIT, IT, IN TURN, WILL ALLOW THE AC BUS TO OPERATE BATTERY CHARGER. PART TC: 4,348. 2 L 7 2 4F RT A21EA 1998090400065 19980904 00065 WP 1998 9 4 CA980608013 1 19980519 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE BS 609-629 CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 10256 (CAN) DURING INSPECTION, CORROSION FOUND AROUND OUTFLOW VALVE CUT OUT SKIN, FS 609-629 AND STR 42-35. REPAIRED PER SRM. 2 L 7 3 4F 4 F A23WE E12EU 1998090400066 19980904 00066 NE 1998 9 4 CA980608018 2 19980427 A 7230 522194 SPACER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE NR 2 ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 65842 P656929D (CAN) THE NR 2 ENGINE WAS REMOVED FROM THE AIRCRAFT DUE TO METAL CONTAMINATION IN THE OIL FILTER. ON DISASSEMBLY, THE S PACER BETWEEN THE THIRD AND FOURTH STAGE ON THE LOW PRESSURE COMPRESSOR WAS FOUND CRACKED IN SEVERAL PLACES. THE LARGES T CRACK EXTENDED RADIALLY FROM THE SIDE FLANGE INNER LIP THROUGH THE BUSHED TIE ROD HOLE TO THE EXTERIOR BARREL. THIS CR ACK WHICH WAS 1.6 INCHES OF THE 2.75 INCHES TOTAL BARREL WIDTH, HAD OPENED APPROXIMATELY 0.010 INCH. THERE WERE FIVE OT HER TIGHT CRACKS EXTENDING FROM THE SIDE INNER LIP TO THE BUSHED TIE ROD HOLE. PART TC: 66,106. 2 L 7 2 4F 4 F A6WE E2EA 1998090400067 19980904 00067 EU 1998 9 4 CA980608019 1 19980520 A 2750 RETRACT MECH AIRBUS 320 A320211 3930320 EU TE FLAP MALFUNCTIONED W L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 CA 25734 (CAN) FLAP OVERSPEED AT FULL FLAP ON APPROACH. FLAP AND SLAT OVERSPEED INSPECTION AND OPERATION CARRIED OUT. NO FAULT FOUND, A/C SERVICEABLE. 2 L 7 2 4F RT A28NM 1998090400069 19980904 00069 WP 1998 9 4 CA980608021 1 19980519 A 4900 49700010118 APU DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT PACK LEAKING W K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA P657314D (CAN) DURING CLIMB OUT, AN OILY SMELL WAS DETECTED IN BUSINESS CLASS SECTION OF PASSENGER COMPARTMENT. SMELL DISSIPATED AFTER LEFT HAND AIR CONDTIONER PACK TURNED OFF. MAINTENANCE CHECK REVEALED AUXILIARY POWER UNIT WAS CONTAMINATING LEFT AIR CONDITIONER PACK. AUXILIARY POWER UNIT REPLACED AND OPERATIONAL CHECK CARRIED OUT, SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998090400070 19980904 00070 EA 1998 9 4 CA980608022 1 19980521 A 3234 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE MLG FAILED W K NONE J WARNING INDICATION TO TAKEOFF 1 CA 7741 807173 (CAN) GEAR DISAGREE WARNING AT RETRACTION AFTER TAKEOFF. REPLACED MAIN LANDING GEAR SELECTOR VALVE. PART TC: 6,940. 2 L 7 2 4F 4 F RT A21EA E15NE 1998090400071 19980904 00071 EA 1998 9 4 CA980608023 1 19980523 A 5210 SUPPORT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE PAX DOOR OUT OF ADJUST W K NONE O OTHER IN INSP/MAINT 1 CA 7767 807242 (CAN) CABIN MAIN PASSENGER DOOR DIFFICULT TO OPEN. AFT UPPER FRAME, FIXED BEARING SUPPORT FOR ROTARY LATCH CAM ADJUSTED . PART TC: 6,698. 2 L 7 2 4F 4 F RT A21EA E15NE 1998090400072 19980904 00072 EU 1998 9 4 CA980608025 1 19980514 A 2530 OVEN AIRBUS A340 A340313 EU GALLEY CONTAMINATED W F ACTIVATE FIRE EXT. A FLAME/FIRE CR CRUISE 1 CA (CAN) FIRE OCCURRED IN MIDDLE GALLEY OVEN. FIRE EXTINGUISHED BY CREW. IT WAS DETERMINED FIRE WAS CAUSED BY FOOD PAPER WRAPPING. OVEN CHECKED OKAY, NO FAULT FOUND. 2 L 7 4 4F RT A197 1998090400074 19980904 00074 EA 1998 9 4 CA980608028 1 19980503 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE FLAP CONTROL FAILED W K NONE F FLT CONT AFFECTED LD LANDING 1 CA 5348 807343 (CAN) FLAPS FAILED ON LANDING. REPLACED BRAKE POSITION SENSOR UNIT AND FLAP ELECTRONIC CONTROL UNIT (P/N 860D10018ABC). PART TC: 4,662. 2 L 7 2 4F 4 F RT A21EA E15NE 1998090400075 19980904 00075 EU 1998 9 4 CA980608029 1 19980510 A 2611 UNKNOWN AIRBUS 320 A320211 3930320 EU GALLEY SMOKE W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA (CAN) ECAM WARNING, SMOKE IN LAVATORY. AIRCRAFT RETURNED TO DEPARTURE TERMINAL. MAINTENANCE TECHS OPERATED BOTH AIR CO NDITIONERS FOR 30 MINUTES AND WERE UNABLE TO DUPLICATE PROBLEM, NO EVIDENCE OF SMOKE. LAVATORY SMOKE DETECTION SYSTEM C HECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998090400076 19980904 00076 NM 1998 9 4 CA980608030 1 19980510 A 2133 VALVE AIRBUS A319 A319114 NM CABIN PRESSURE FAILED W B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA (CAN) DURING CRUISE, FLT LEVEL 370, UNUSUAL CABIN ALTITUDE IN AUTO SYSTEM 2 OF 6,500 FEET. SAFETY VALVE OPENED TWICE FO R A BRIEF PERIOD, APPROXIMATELY 2 MINUTES LATER, CABIN DEPRESSURIZED AND EMERGENCY DESCENT CARRIED OUT. CONTROL REGAINE D IN MANUAL MODE AT FLT. LEVEL 200. OUTFLOW VALVE REPLACED. SYSTEMS 1 AND 2 TESTED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998090400077 19980904 00077 EU 1998 9 4 CA980608031 1 19980508 A 3231 LINKAGE PIN AIRBUS 320 A320211 3930320 EU NLG DOOR MISSING W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) ON CLIMB, DURING GEAR UP SELECTION, ECAM WARNING LANDING GEAR AND INTERFACE UNIT FAULT AND GEAR DOOR NOT CLOSED AT NOSE LANDING GEAR. A/C RETURNED TO DEPARTURE TERMINAL. MAINTENANCE CHECK REVEALED NOSE GEAR DOOR ACTUATOR EYE AND LIN KAGE PIN MISSING. NEW BOLT INSTALLED AND RETRACTION TEST CARRIED OUT SERVICABLE. 2 L 7 2 4F RT A28NM 1998090400078 19980904 00078 EU 1998 9 4 CA980608032 1 19980503 A 2780 SLAT AIRBUS 320 A320211 3930320 EU WING INOPERATIVE W K NONE F FLT CONT AFFECTED AP APPROACH 1 CA (CAN) SLATS DID NOT EXTEND WHEN SELECTED. MAINTENANCE ACTION INVOLVED CHANGING WING TIP BRAKE. 2 L 7 2 4F RT A28NM 1998090400079 19980904 00079 WP 1998 9 4 CA980608033 1 19980502 A 2761 ACTUATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE SPOILER FAILED W K NONE F FLT CONT AFFECTED AP APPROACH 1 CA P654059D (CAN) UNABLE TO ARM GROUND SPOILERS ON APPROACH AND SPOILERS DID NOT DEPLOY MANUALLY ON LANDING. REPLACED SPOILER CONTR OL ACTUATOR AND SPOILER CONTROL BOX. SPOILERS ADJUSTED AND CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998090400080 19980904 00080 NM 1998 9 4 CA980608035 1 19980501 A 5610 WINDSHIELD AIRBUS A319 A319114 NM COCKPIT SHATTERED W J A DUMP FUEL UNSCHED LANDING O OTHER CR CRUISE 1 CA (CAN) CAPTAIN'S WINDOW SHATTERED IN-FLIGHT. MAINTENANCE CHANGED WINDSHIELD AND WINDSHIELD HEAT CONTROLLER. 2 L 7 2 4F RT A28NM 1998090400081 19980904 00081 1998 9 4 CA980608036 4 19980501 A 2350 AUDIO PANEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE COCKPIT INOPERATIVE W K NONE O OTHER AP APPROACH 1 CA P653684D (CAN) LOSS OF VHF COMMUNICATION ON APPROACH TO AIRPORT, SOME TRANSMISSIONS TOO WEAK TO BE READ BY AIR TRAFFIC CONTROL CE NTER. MAINTENANCE REPAIRED THREE BROKEN WIRES ON CAPTAIN'S AUDIO CONTROL PANEL CONNECTOR. 2 L 7 2 4F 4 F A6WE E2EA 1998090400082 19980904 00082 EA 1998 9 4 CA980608037 1 19980430 A 2750 PROX SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT WING FAILED W O OTHER O OTHER AP APPROACH 1 CA 5330 807343 (CAN) ON APPROACH, THE FLAPS LOCKED AT 30 DEGREES. AIRCRAFT LANDED OK WITH FLAPS AT 30. REPLACED LEFT HAND BRAKE PROX IMITY SENSOR UNIT AND FLEX CABLE TO BRAKE PROXIMITY SENSOR UNIT. PART TC: 4,647. 2 L 7 2 4F 4 F RT A21EA E15NE 1998090400083 19980904 00083 EA 1998 9 4 CA980608038 1 19980429 A 2750 FECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS LOCKED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 5325 807343 (CAN) FLAPS FAULT MESSAGE AND FLAPS LOCKED AT 30 DEGREES ON LANDING. FLAP ELECTRONIC CONTROL UNIT REPLACED. PART TC: 4,643. 2 L 7 2 4F 4 F RT A21EA E15NE 1998090400088 19980904 00088 NM 1998 9 4 CA980610008 1 19980531 A 3241 PLGA1250010 PLUG DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BRAKE SYS LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 24403 120421 (CAN) ANTI-SKID VALVE PLUG FOUND LOOSE ALLOWING FLUID TO LEAK. ANTI-SKID VALVE REPLACED. PART TC: 26,063. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400089 19980904 00089 NM 1998 9 4 CA980610009 1 19980527 A 3250 89769 TRANSDUCER DOWTY 89607 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE STEERING FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TX TAXI/GRND HDL 1 CA 78451 121075 (CAN) NOSE WHEEL STEERING WOULD KICK OFF AS SOON AS NOSE STEERING SWITCH SELECTED. CAUTION LIGHT ON. FOUND LDVT TRANSD UCER DEFECTIVE. THE SHAFT WAS BENT. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400091 19980904 00091 NM 1998 9 4 CA980610011 1 19980601 A 7603 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE CONDITION FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 19001 120439 (CAN) DURING ENGINE ILNSPECTION, THE RIGHT HAND LOWER CONDITION LEVER CABLE WAS FOUND FRAYED AT THE PULLEY, FORWARD OF T HE ENGINE FIREWALL. PART TC: 19,167. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400094 19980904 00094 NE 1998 9 4 CA980629018 2 19980601 A 7230 522194 SPACER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 62719 P656927D (CAN) DURING DISASSEMBLY OF A TIME EXPIRED ENGINE, THE FRONT COMPRESSOR ROTOR THIRD TO FOURTH STAGE SPACER WAS FOUND CRA CKED. THERE WERE 8 CRACKS EXTENDING FROM THE TIE ROD SLEEVE HOLES TO THE INSIDE, AND THERE WAS ONE SMALL CRACK STARTING FROM THE TIE ROD SLEEVE TO THE OUTSIDE DIAMETER. THE PARTS WERE REMOVED FROM SERVICE AND WILL BE EVALUATED. A MORE DET AILED SDR WILL BE SUBMITTED TO IDENTIFY THE ROOT CAUSE. PART TC: 61,431. 2 L 7 2 4F 4 F A6WE E2EA 1998090400103 19980904 00103 WP 1998 9 4 TWAA9813801 1 19980826 A 3250 CONTROL CABLE DOUG DC9 DC951 3022051 WP NLG STEERING BROKEN A TWAA O OTHER O OTHER TX TAXI/GRND HDL 1 CE 05 411EA 47732 DURING TAXI TOWARD THE GATE IN A 90 DEGREE RIGHT ANGLE TURN CREW HEARD LOUD SNAP AND LOST NOSE WHEEL STEERING. ACFT WAS TOWED INTO GATE. REPLACED BROKEN STEERING CABLE 124C PER MNT MANUAL 32-51-1. CHECK-C, 7-19-97 STL. 2 L 7 2 4F RT A6WE 1998090400104 19980904 00104 NM 1998 9 4 VJ0900298 1 19980826 A 3350 6013211 BATTERY CHARGER BOEING 737 737214 138446R NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 RT OVERWING EMERGENCY LIGHTS INOP. REPLACED THE LIGHT BATTERY CHARGER ASSY. 2 L 7 2 4F A16WE 1998090400105 19980904 00105 NM 1998 9 4 VJ9800297 1 19980825 A 3350 1000679 LIGHT BOEING 737 7372L9 1384497 NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 R-1 DOOR EMERGENCY LIGHT (INTERIOR) INOP. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A16WE 1998090400106 19980904 00106 EU 1998 9 4 MALA976188 1 19980824 A 3350 1012621 LIGHT BAC 146 AVRO146RJ85A 1500097 EU CABIN BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 501XJ E2208 DURING INSPECTION, EMERGENCY EXIT LIGHT ASSEMBLY BROKEN AT MAIN PASSENGER EXIT. MAINTENANCE REPLACED LIGHT ASSEMBLY, AL L CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998090400107 19980904 00107 EU 1998 9 4 MALA976189 1 19980823 A 3350 LENSE SAAB SF340 340B 7860101 EU CABIN LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 586MA 340B165 DURING INSPECTION, EXIT SIGN ABOVE SEAT 6A THE FORWARD HALF OF PLASTIC SIGN HAS COME APART. MAINTENANCE RESECURED LENS, SEC CHECK GOOD. 2 L 7 2 4T RT A52EU 1998090400108 19980904 00108 WP 1998 9 4 IXXA9800067 1 19980825 A 2130 PRESSURE SYST DOUG DC8 DC871F 302199D WP CABIN MALFUNCTIONED A IXXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 824BX 45946 EN ROUTE AT FLIGHT LEVEL 35.0, THE AIRCRAFT CABIN BEGAN TO CLIMB RAPIDLY, MANUAL CONTROL OF PRESSURIZATION WAS ATTEMPTED . PACK FLOWS WERE INCREASED TO 90 PERCENT CAPACITY WITH MINIMAL DECREASE IN CABIN. DESCENT INITIATED AND AT LEVEL OFF CABIN COULD BE MAINTAINED AT 5,000 FT. CREW ACCOMPLISHED COMPANY PROCEDURES FOR PRESSURIZATION LOSS AND ELECTED TO LAN D THE AIRCRAFT AT SLC. FOLLOWING THE UNEVENTFUL LANDING AT SLC, MAINTENANCE ACCOMPLISHED A OPERATIONAL CHECK OF BOTH TH E MANUAL AND AUTOMATIC PRESSURIZATION SYSTEMS AND A CABIN PRESSURE DECAY CHECK IAW THE AIRCRAFT MM AND FOUND NO DEFECTS. 2 L 7 4 4F RT 4A25 1998090400109 19980904 00109 NM 1998 9 4 CALA9801525 1 19980825 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOOR SUPPORT ANGLE CORRODED AT DOGHOUSE, STA 294.5. THE FLOOR SUPPORT ANGLE WAS REMOVED AND A NEW ANG LE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400110 19980904 00110 NM 1998 9 4 CALA9801526 1 19980825 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 950 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND AFT PIT FLOORBEAM CRACKED AT BS 950E ABOVE STRINGER 29L. THE CRACKED SECTION OF FLOORBEAM WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-40-4, 51-30-2, 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1998090400111 19980904 00111 NM 1998 9 4 CALA9801527 1 19980825 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 460-480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND SEAT TRACK CORRODED AT STA 460 TO 480, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLE D IAW SRM 53-10-5, FIGURE 1, 51-10-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998090400112 19980904 00112 NM 1998 9 4 CALA9801528 1 19980825 A 5311 FRAME BOEING 727 727232 1384082 NM BS 560 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT FUSELAGE FRAME GOUGED AT STA 560, WL 294. A REPAIR WAS INSTALLED IAW SRM 53-10-4, FIGURE 1, 51-30-2 , 51-10-2, AND MM 51-20-0. 2 L 7 3 4F A3WE 1998090400113 19980904 00113 NM 1998 9 4 CALA9801529 1 19980825 A 5311 FRAME BOEING 727 727232 1384082 NM BS 340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT FUSELAGE FRAME CORRODED AT STA 340. A REPAIR WAS INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 1998090400114 19980904 00114 NM 1998 9 4 CALA9801530 1 19980826 A 5720 CHORD BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A 1.5 INCH CRACK IN RT WING TRAILING EDGE LOWER CHORD AT NR 8 SPOILER ACTUATOR CASTING. THE CRACKED SE CTION OF CHORD WAS REMOVED IAW SRM 51-30-2. A REPAIR WAS INSTALLED IAW SRM 51-10-1 AND ECRA 5720-01675. 2 L 7 3 4F A3WE 1998090400115 19980904 00115 NM 1998 9 4 CALA9801531 1 19980826 A 5343 FITTING BOEING 727 727224 1384076 NM NLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND NOSE GEAR RT TRUNNION FITTING AND CAP CORRODED. THE STIFFENERS AND FITTING WERE REMOVED AND THE AREA W AS REPAIRED IAW SRM 51-10-2 AND 51-10-6. 2 L 7 3 4F A3WE 1998090400116 19980904 00116 NM 1998 9 4 CALA9801532 1 19980826 A 5343 FITTING BOEING 727 727224 1384076 NM NLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND NOSE GEAR LT TRUNNION FITTING AND CAP CORRODED IN AREAS OF BUSHING RECESS. THE FACES AND BORE OF LT NL G TRUNNION AND CAP ASSEMBLY WERE MACHINED IAW SRM 53-40-1 AND ECRA 5340-01323. 2 L 7 3 4F A3WE 1998090400117 19980904 00117 NM 1998 9 4 CALA9801533 1 19980826 A 5720 CHORD BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A 1.5 INCH CRACK IN LOWER FORWARD CHORD OF LT WING BELOW NR 7 SPOILER ACTUATOR. THE CRACKED SECTION WA S CUT OUT, A REPAIR WAS INSTALLED IAW ECRA 5720-01675. 2 L 7 3 4F A3WE 1998090400118 19980904 00118 NM 1998 9 4 CALA9801534 1 19980826 A 5720 ANGLE BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 66734 20663 INSPECTION FOUND A 1 INCH CRACK IN L-ANGLE OF LT WING J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE ANGLE WAS REMOVED AND A N EW ANGLE WAS INSTALLED IAW SRM 51-10-1, PAGE 4 AND 51-30-2. 2 L 7 3 4F A3WE 1998090400119 19980904 00119 NM 1998 9 4 CALA9801535 1 19980825 A 5315 FLOORBEAM BOEING 737 7372C0 1384488 NM BS 675 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM LOWER CHORD AT STA 675, BBL 0.07. THE LOWER CHORD WAS REMOVED AND A NEW LO WER CHORD ANGLE AND TWO REINFORCING SPLICE ANGLES WERE INSTALLED IAW ECRA 5710-01929. 2 L 7 2 4F A16WE 1998090400120 19980904 00120 NM 1998 9 4 CALA9801536 1 19980825 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 178 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A .0625 AND 1.5 INCH CRACK IN FUSELAGE SKIN DOUBLER FORWARD OF COCKPIT WINDOW AT STA 178, BL 0. THE SK IN DOUBLER WAS REMOVED IAW SRM 51-30-2. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND ECRA 5310-03754. 2 L 7 2 4F A16WE 1998090400121 19980904 00121 SO 1998 9 4 COMA9810181 1 19980827 A 2820 12008729009 FUEL LINE EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 462CA 120264 WHILE REPLACING LEAKING RIVET IN RIGHT OUTBOARD WING, FOUND RE-FUEL LINE (P/N 120-08728-009) CRACKED AT BEND RADIUS. RE PLACED CRACKED FUEL LINE. 2 L 7 2 4T RT A31SO 1998090400122 19980904 00122 SO 1998 9 4 COMA9810182 1 19980825 A 2720 421120963 DIODE BLOCK EMB 120 EMB120RT SO E/E COMPT FAILED A COMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SO 01 264CA 120256 RUDDER OVERBOOST WARNING AT 190 KTS. REPLACED DIODE BLOCK. 2 L 7 2 4T RT A31SO 1998090400123 19980904 00123 SO 1998 9 4 COMA9810183 1 19980824 A 3350 1013073 LIGHT EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 189CA 120189 EMERGENCY FLOOR LIGHT BY GALLEY IS BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4T RT A31SO 1998090400124 19980904 00124 EA 1998 9 4 COMA9860240 1 19980825 A 5270 CIRCUIT BREAKERS CNDAIR CL600 CL6002B19 EA DOOR WARN SYST TRIPPED A COMA K NONE N FALSE WARNING DE DESCENT 1 SO 01 946CA 7072 CABIN DOOR, SERVICE DOOR AND CARGO DOOR WARNINGS. RESET CIRCUIT BREAKERS, CLEARED FAULTS FROM PSEU. SYSTEM TEST SATISF ACTORY. 2 L 7 2 4F RT A21EA 1998090400125 19980904 00125 EA 1998 9 4 COMA9860241 1 19980824 A 3230 864806 PSEU CNDAIR CL600 CL6002B19 EA AVIONICS MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 933CA 6841 7040 LANDING GEAR WILL NOT EXTEND. USED FREE FALL SYSTEM TO LOWER GEAR. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1998090400126 19980904 00126 NM 1998 9 4 UPS98227541 1 19980728 A 5320 FITTING BOEING 727 72751C 1384015 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACKS FOUND ON BS 870 TERMINAL FITTING LT AND RT. BOTH BS 870 LT AND RT TERMINAL FITTINGS REPLACED. 2 L 7 3 4F A3WE 1998090400127 19980904 00127 NM 1998 9 4 UPS98227542 1 19980729 A 5320 6559742 FITTING BOEING 727 72751C 1384015 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, REPLACE RT BS 870 TERMINAL FITTING. FITTING REPLACED IAW UPS EO B727-5310-3056 AND DRAWING 65C23231. 2 L 7 3 4F A3WE 1998090400128 19980904 00128 NM 1998 9 4 UPS98227543 1 19980804 A 5730 106003162 PANELS BOEING 727 72751C 1384015 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, LT WING NR 18 TANK ACCESS PANEL BOLT ON TYPE SEAL GROOVE CORRODED, ALSO NR 17 AND NR 19. PANELS REP LACED, THEN CLOSED PER TC C57-571-01-1D. 2 L 7 3 4F A3WE 1998090400129 19980904 00129 NM 1998 9 4 UPS98227544 1 19980805 A 5753 BOLT BOEING 727 72751C 1384015 NM WS 224.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, NR 5 FLAP TRACK ATTACH BOLT CORRODED. BOLT CHANGED IAW MM 27-51-31. 2 L 7 3 4F A3WE 1998090400130 19980904 00130 NM 1998 9 4 UPS98227545 1 19980804 A 5753 BOLT BOEING 727 72751C 1384015 NM NR 2 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, NR 2 FLAP TRACK ATTACH BOLT AND BARRELL NUT CORRODED. BOLT AND BARRELL NUT REPLACED PER MM27-51-31. 2 L 7 3 4F A3WE 1998090400131 19980904 00131 NM 1998 9 4 UPS98227546 1 19980804 A 5753 BOLT BOEING 727 72751C 1384015 NM NR 4 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, NR 4 FLAP TRACK ATTACH BOLTS AND NUT CORRODED. NUT AND BOLTS REPLACED IAW MM 20-80-01. 2 L 7 3 4F A3WE 1998090400132 19980904 00132 NM 1998 9 4 UPS98227547 1 19980804 A 5753 BARRELL NUT BOEING 727 72751C 1384015 NM NR 1 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, NR 1 FLAP TRACK BARRELL NUT CORRODED AND WASHER UNDER HEAD OF ATTACH BOLT CORRODED. BARRELL NUT AND WASHER CHANGED PER MM. 2 L 7 3 4F A3WE 1998090400133 19980904 00133 NM 1998 9 4 UPS98227548 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 420 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, STRINGER 23R BROKEN AT STA 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1 DETAIL 2. 2 L 7 3 4F A3WE 1998090400134 19980904 00134 NM 1998 9 4 UPS98227549 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK AT FASTENER HOLE OF STRINGER 21R AT STATION 420. STRINGER REPAIRED IAW SRM 53-10-2, FIG 1, DET AIL 2. 2 L 7 3 4F A3WE 1998090400135 19980904 00135 NM 1998 9 4 UPS98227550 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, SUSPECT CRACK ON S22R FASTENER HOLE ST STA 380. REPAIRED CRACK IAW SRM 51-10-3 FIG 2. 2 L 7 3 4F A3WE 1998090400136 19980904 00136 NM 1998 9 4 UPS98227551 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK IN FASTENER HOLE AND FASTENER MISSING ON S21R AT BS 400. REPAIRED CRACK IAW SRM 51-10-3, FIG 2 . 2 L 7 3 4F A3WE 1998090400137 19980904 00137 NM 1998 9 4 UPS98227552 1 19980730 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, SUSPECT CRACK IN FRAME 600 JUST ABOVE STR 18 RT. REPAIRED CRACK AT STATION 600, STR 18 RT IAW SRM 53 -10-4. 2 L 7 3 4F A3WE 1998090400138 19980904 00138 NM 1998 9 4 UPS98227553 1 19980731 A 5730 9611503000 PANELS BOEING 727 72751C 1384015 NM WS 519-656.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CORROSION IN SEAL RECESS ON RT WING FUEL TANK BOLT ON ACCESS DOORS NR 15, 16, 17, 18 AND 19. PANELS REPLACED AND THEN CLOSED PER TC C57-571-01-2D. 2 L 7 3 4F A3WE 1998090400139 19980904 00139 NM 1998 9 4 UPS98227554 1 19980731 A 5730 BAC10600313002 PANEL BOEING 727 72751C 1384015 NM WS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, NR 1 FRONT SPAR TANK ACCESS PANEL CORRODED, RT WING. REFER TO TC C57-571-01-2D FOR ACCESS PANEL AND CLAMP RING REPLACEMENT/INSTALLATION. 2 L 7 3 4F A3WE 1998090400140 19980904 00140 NM 1998 9 4 UPS98227555 1 19980730 A 5753 TRACK BOEING 727 72751C 1384015 NM NR 6 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, PITTING CORROSION ON UPPER SURFACE OF NR 6 FLAP TRACK AT ATTACH POINT TO AUXILIARY SPAR. SHIM MANUFA CTURED AND INSTALLED PER SRS ENGINEERING ORDER 98-24-009 REF UPS ENGINEERING FILE NUMBER 727-57-2000. 2 L 7 3 4F A3WE 1998090400141 19980904 00141 NM 1998 9 4 UPS98227556 1 19980729 A 5320 65159741 FITTING BOEING 727 72751C 1384015 NM BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, REPLACE LT BS 870 TERMINAL FITTING. FITTING REPLACED IAW UPS EO B727-5310-3056 AND DRAWING 65C23231. 2 L 7 3 4F A3WE 1998090400142 19980904 00142 NM 1998 9 4 UPS98227557 1 19980730 A 5753 TRACK BOEING 727 72751C 1384015 NM NR 3 FLAP TRACK CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, PITTING CORROSION ON UPPER SURFACE OF NR 3 FLAP TRACK AT ATTACH POINT TO AUXILIARY SPAR. SHIM FABRIC ATED AND INSTALLED IAW SRS 98-24-008, REF UPS ENGINEERING FILE NUMBER 727-57-2001. 2 L 7 3 4F A3WE 1998090400143 19980904 00143 NM 1998 9 4 UPS98227558 1 19980802 A 5711 6518540 SPAR BOEING 727 72751C 1384015 NM LT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CORROSION ON LT WING CENTER SECTION FRONT SPAR LOWER CHORD AT APPROX LBL 100. REPLACED FRONT LOWER CENTER TANK CHORD IAW DRAWING 64-8333. 2 L 7 3 4F A3WE 1998090400144 19980904 00144 NM 1998 9 4 UPS98227559 1 19980802 A 5230 FRAME BOEING 727 72751C 1384015 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, AFT CARGO DOOR LOWER FORWARD FRAME CRACKED. FRAME REPLACED IAW DRAWING 65C16422. 2 L 7 3 4F A3WE 1998090400145 19980904 00145 NM 1998 9 4 UPS98227560 1 19980807 A 5347 65227977 TRACK BOEING 727 72751C 1384015 NM BS 1010 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CARGO TRACK SECTION BS 1010 RT SIDE HAS SIZEABLE CRACK. RT FWD TRACK REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400146 19980904 00146 NM 1998 9 4 UPS98227561 1 19980812 A 5712 RIB BOEING 727 72751C 1384015 NM WS 656.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 10 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS EO B7 27-5710-0314 FIG 13. 2 L 7 3 4F A3WE 1998090400147 19980904 00147 NM 1998 9 4 UPS98227562 1 19980730 A 5230 FITTING BOEING 727 72751C 1384015 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, AFT CARGO DOOR NUMBER ONE FITTING CRACKED (NR 1 FWD FITTING). NEW FITTING INSTALLED IAW DRAWING 65C1 8422. 2 L 7 3 4F A3WE 1998090400148 19980904 00148 NM 1998 9 4 UPS98227563 1 19980805 A 5320 ANGLE BOEING 727 72751C 1384015 NM BS 740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CHORD ANGLE AT BS 740 LT (P/N 65-15940-24) HAS CORROSION ON O/B SECTION. CHORD REPAIRED IAW DRAWING 65C13724 AND SRS ENGINEERING ORDER 98-24- 004, REF UPS ENGINEERING FILE NUMBER 727-53-2064. 2 L 7 3 4F A3WE 1998090400149 19980904 00149 NM 1998 9 4 UPS98227564 1 19980812 A 5712 RIB BOEING 727 72751C 1384015 NM BS 656.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, CRACK ON RIB ATTACH TAB ON NR 13 STRINGER AT WING STATION 656.5 RT. REPAIR CARRIED OUT IAW UPS B727- 5710-0314. 2 L 7 3 4F A3WE 1998090400150 19980904 00150 NM 1998 9 4 UPS98227565 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 380 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, S21L HAS CRACK AT FASTENER HOLE AT STATION 380. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1. 2 L 7 3 4F A3WE 1998090400151 19980904 00151 NM 1998 9 4 UPS98227566 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-D, STRINGER 23L AT STATION 400 CRACKED AT FASTENER HOLE. STRINGER REPAIRED IAW SRM 53-10-3, FIG 1. 2 L 7 3 4F A3WE 1998090400152 19980904 00152 EU 1998 9 4 QXEA9801092 1 19980823 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 LIGHT IN OVERWING EXIT SIGN ON LEFT SIDE, ROW 8 IS OUT. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998090400153 19980904 00153 EU 1998 9 4 QXEA9801093 1 19980824 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 LIGHT IN OVERWING EXIT SIGN AT ROW 9E IS OUT. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998090400154 19980904 00154 EU 1998 9 4 QXEA9801094 1 19980824 A 5210 BUSHING FOKKER F28 F28MK4000 4990810 EU PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 MAINTENANCE REPORTS, THE MAIN CABIN DOOR IS HARD TO OPEN FROM THE OUTSIDE. INSPECTED AND FOUND EXTERIOR MAIN CABIN DOOR HANDLE RUBBING ON FUSELAGE. REMOVED AND REPLACED PIVOT PIN AND BUSHINGS FOR HANDLE, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998090400155 19980904 00155 WP 1998 9 4 ABXA9800795 1 19980826 A 5250 AR25291GR41 DOOR HANDLE DOUG DC8 DC862 3021970 WP COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 803AX 45917 DURING PREFLIGHT, FOUND THAT THE COCKPIT DOOR WOULD NOT OPEN FROM CABIN SIDE. REPAIRED COCKPIT DOOR HANDLE AS REQUIRED, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998090400156 19980904 00156 NM 1998 9 4 SCNA98712 1 19980814 A 5347 SEAT TRACK BOEING 727 7272J4 1384006 NM BS 720 BROKEN A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING A HEAVY MAINT CHECK, A SEAT TRACK WAS FOUND BROKEN APPROX 4 INCHES LONG ON I/B SIDE OF TRACK AT STATION 720A WL 2 08 LBL 46. CUT OUT SEAT TRACK IAW SRM B727 531005. FABRICATED NEW SEAT TRACK IAW SRM PER B727 531005 FROM EXTRUSTION B AC 1520 792. TREATED AND PRIMED IAW SRM B727 511006. INSTALLED IAW SRM B727 531005 FIGURE 7. 2 L 7 3 4F RT A3WE 1998090400157 19980904 00157 WP 1998 9 4 RRXA98414 1 19980825 A 2612 FIRE DETECTOR DOUG DC8 DC873F 302199F WP NR 4 ENGINE MALFUNCTIONED A RRXA K NONE N FALSE WARNING DE DESCENT 1 WP 15 2674U 46062 ON DESCENT, NR 4 FIRE HANDLE AND FE'S FIRE WARN LIGHT AND BELL ILLUMINATED INTERMITTENTLY. LATER ON DESCENT ENG NR 4 SH ORT CIRCUIT LIGHT ILLUMINATTED INTERMITTENTLY. INSTALLED COMPLETE SET OF FIRE DET ELEMENT ASSY'S ON NR 4 ENG FIRE WARN BELL/LIGHT AND SHORT CIRCUIT CHECKS NORMAL. 2 L 7 4 4F RT 4A25 1998090400158 19980904 00158 WP 1998 9 4 RRXA98415 1 19980826 A 2410 CSD DOUG DC8 DC873F 302199F WP NR 2 DIRTY A RRXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 15 796FT 46104 DURING CRUISE, NR 2 BUS PWR FAIL AND LT EMERG BUSS FAIL W/GEN UNPARAL LIGHT ILLUMINATED. VOLTS/FREQS - 0. RESTORED BUS PWR MAN QRH. ON SHORT FINAL LOST NR 2 BUSS PWR AGAIN AND SMELLED ELECTRICAL BURNING. INSPECTED GCU, BTR, GR CT'S, AND WIRING, NO DEFECTS NOTED. CLEANED OIL FROM CSD DISCONNECT, ALL GENS AND BUSSES OPS CK OK ON GROUND RUN. 2 L 7 4 4F RT 4A25 1998090400159 19980904 00159 NM 1998 9 4 VNAA9808022 1 19980823 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE BIRD STRIKE A VNAA K NONE O OTHER LD LANDING 1 GL 07 422JS 3018 DURING ROLLOUT, HEARD 2 THUMPS AND SAW BIRDS STRIKE THE AIRCRAFT BELOW THE CO-PILOTS WINDSHIELD. MAINTENANCE INSPECTED THE AIRCRAFT PROPELLERS, INLETS, FUSELAGE AND FLIGHT CONTROLS FOR DAMAGE, NO DAMAGED FOUND. CLEANED AIRCRAFT AND APPROV ED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998090400160 19980904 00160 NM 1998 9 4 VNAA9808024 1 19980824 A 3010 29S7D524004 DEICE BOOT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WING DEFECTIVE A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 441JS 3059 DURING TAXI FOR TAKEOFF, CREW RECEIVED AIRFRAME DEICE FAIL MESSAGE. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED A IRCRAFT AND DEFERRED RT MIDDLE WING DEICE BOOT. AIRCRAFT WAS RELEASED AND FLOWN TO PIT. PIT MAINTENANCE REPLACED RT MI DDLE AIRFRAME LEADING EDGE IN ACCORDANCE WITH THE DORNIER MAINTENANCE MANUAL 57-40-00. OPERATIONAL CHECK OF THE DEICE B OOT SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-10-00 CHECKED GOOD. DEFERRAL WAS CLEARED AND THE AIRCRAFT A PPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998090400161 19980904 00161 NM 1998 9 4 VNAA9808025 1 19980825 A 3240 HP16131001 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE BRAKE DEFECTIVE A VNAA A D UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 GL 07 425JS 3037 DURING CLIMB, CREW RECEIVED EMERGENCY PARKING BRAKE ACCUMULATOR CAS MESSAGE. CREW CONSULTED CHECK LIST WHICH REQUIRES L ANDING AT NEAREST AVAILABLE AIRPORT. AIRCRAFT RETURNED TO CAK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE A IRCRAFT AND FOUND THE EMERGENCY PARKING BRAKE SELECTOR VALVE DEFECTIVE. MAINTENANCE REPLACED THE VALVE IN ACCORDANCE WI TH THE DORNIER MAINTENANCE MANUAL 29-21-03. OPERATIONAL AND LEAK CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998090400162 19980904 00162 SW 1998 9 4 98ZZZX3083 1 19980812 A 6710 2120013231 BOLT BELL 412 412 1182202 SW CYCLIC CONTROL CORRODED D A K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 19 411DE 36030 DURING A 300-HOUR INSPECTION, DISCOVERED ONE OF THE BOLTS IN THE 'BOOSTED CYCLIC' CONTROL SYSTEM WAS WORN AND NEEDED TO BE REPLACED. A NEW BOLT, P/N 212-001-323-001, WAS DRAWN OUT OF SPARES SUPPLY TO REPLACE THE WORN ITEM. UPON OPENING TH E SEALED PACKAGE, NOTICED WHAT APPEARED TO BE ETCHING OR CORROSION DAMAGE ON THE 'NEW' BOLT SHANK AREA. THE REMAINING 3 PACKAGES OF THE P/N BOLTS CHECKED AND FOUND 2 MORE WITH SIMILAR ETCHING/CORROSION DAMAGE. SUBMITTER CONTACTED BELL HEL ICOPER QUALITY CONROL MONITOR WHO WANTED BOLTS RETURNED ASAP. THE 'REJECTED' BOLTS AND ALL THE DOCUMENTATION HAVE BEEN PACKAGED-UP AND SENT TO BELL HELICOPTER. 1 G 7 2 4U H4SW 1998090400163 19980904 00163 EU 1998 9 4 98ZZZX3084 1 19980713 A 5610 M1052330122 WINDOW BOLKMS 105 BO105LSA3 5626020 EU PILOT SLIDER DEPARTED D O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 WP 07 203LF 2015 PILOT'S SLIDING WINDOW WAS OPEN. WINDOW TRIM DEBONDED FROM WINDOW ALLOWING WINDOW SLIDER TO DEPART AIRCRAFT. THIS IS T HE SECOND OCCURRENCE AT THIS CONTRACT LOCATION. FIRST ONE WAS CAUGHT IN TIME AND WINDOW TRIM WAS REBONDED. FIRST ONE W AS ON BK117B1, COPILOT'S WINDOW. WINDOW PART NUMBER NOT VISIBLE ON PART. 1 G 7 2 3U H3AU 1998090400164 19980904 00164 NE 1998 9 4 98ZZZX3085 1 19980807 A 3260 7655200904041 SWITCH SKRSKY S76 S76A 8143006 NE MLG SHORTED A HEEA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 SW 03 15459 760222 ON APPROACH TO OFFSHORE PLATFORM WHEN GEAR WAS EXTENDED FOR LANDING, SAFE LIGHT WOULD NOT ILLUMINATE. RETURNED TO SHORE BASE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWN LIMIT SWITCH SHORTED. REPLACED HARNESS ASSY. REF: S-76 IPC, CHAPTER 32-30-05, FIG 1, ITEM 4. 1 G 7 2 3U H1NE 1998090400168 19980904 00168 EU 1998 9 4 98ZZZX3089 1 19980604 A 7722 56375600010 INDICATOR SNIAS 350 AS350B2 8680813 EU ENG T4 FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 96LG 261 2817 INDICATOR INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400169 19980904 00169 NE 1998 9 4 98ZZZX3090 2 19980612 A 7412 9550164470 EXCITER HE900 SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE IGNITION FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 6099P 102 2818 9365 EXCITER INOPERATIVE. WILL NOT SPARK AT PROPER FREQUENCY. UNIT HAS CONTINUOUS SPARK MOST OF THE TIME. REPLACED WITH NE W UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 1998090400181 19980904 00181 EU 1998 9 4 98ZZZX3102 1 19980408 A 2460 SP461300 SWITCH BOLKMS 117 BK117A3 5626015 EU DC SYSTEM MISMANUFACTURED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 127HH 7060 TOGGLE SWITCH REJECTED, NEW OUT-OF-BOX. WILL NOT LOCK IN THE 'ON' POSITION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998090400182 19980904 00182 EU 1998 9 4 98ZZZX3103 1 19980323 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 349 12052 S754 PRESSURE TRANSMITTER UNIT INOPERATIVE. INDICATING HIGH PRESSURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1998090400183 19980904 00183 EU 1998 9 4 98ZZZX3104 1 19980702 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 257 12936 S754 PRESSURE TRANSMITTER HAS ERRATIC INDICATIONS. INSTALLED S/N COULD BE 12917. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1998090400184 19980904 00184 EU 1998 9 4 98ZZZX3105 1 19980411 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 115 12966 S754 PRESSURE TRANSMITTER UNIT INOPERATIVE. FUEL PRESURE INDICATOR MAXING OUT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1998090400185 19980904 00185 EU 1998 9 4 98ZZZX3106 1 19980612 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 181 S789 PRESSURE TRANSMITTER PEGGED TO HIGH SIDE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1998090400186 19980904 00186 EU 1998 9 4 98ZZZX3107 1 19980218 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 48 12795 S789 PRESSURE TRANSMITTER PEGGED TO HIGH SIDE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1998090400187 19980904 00187 EU 1998 9 4 98ZZZX3108 1 19980706 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 293 12799 S789 PRESSURE TRANSMITTER PEGGED TO HIGH SIDE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1998090400188 19980904 00188 EU 1998 9 4 98ZZZX3109 1 19980616 A 2840 DK040 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 825LF 193 8352 796 PRESSURE TRANSMITTER HAS HIGH PRESSURE READINGS. JUST UNDER RED LINE. REPLACED WITH NEW UNIT, OCRRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1998090400189 19980904 00189 EU 1998 9 4 98ZZZX3110 1 19980716 A 2460 SP461310 SWITCH BOLKMS 117 BK117A3 5626015 EU DC SYSTEM STUCK A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 315 7017 TOGGLE SWITCH STICKS IN CLOSED POSITION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998090400190 19980904 00190 EU 1998 9 4 98ZZZX3111 1 19980720 A 2700 10195193 BELLOWS BOLKMS 117 BK117A3 5626015 EU FLT CONT WRONG PART A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 951AM 7017 BELLOWS REJECTED, NEW OUT-OF-BOX. INCORRECTLY PACKAGED. PARTS DO NOT MATCH PART NUMBER ON LABEL. REPLACED WITH 3 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998090400192 19980904 00192 EU 1998 9 4 98ZZZX3113 1 19980606 A 7400 50181100010 RELIGHT UNIT AEROSP AS355 AS355F1 8680810 EU ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 53LH 85 5093 ENGINE RE-LIGHT SYSTEM ACTUATES INTERMITTENTLY DURING FLIGHT. ALSO, WILL ACTUATE ON GROUND WHILE ENGINE IS NOT RUNNING. REPLACED WITH NEW UNIT, CORRECTED UNIT. 1 G 7 2 3U H11EU 1998090400193 19980904 00193 EU 1998 9 4 98ZZZX3114 1 19980513 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 309 2404 TAIL ROTOR BEARING ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400194 19980904 00194 EU 1998 9 4 98ZZZX3115 1 19980717 A 6410 704A33633171G HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911LR 317 2404 LAMINATED HINGE (HINGE), ELASTOMERICS WORN BEYOND SERVICABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400195 19980904 00195 EU 1998 9 4 98ZZZX3116 1 19980708 A 6240 614764021 INDICATOR SNIAS 350 AS350B2 8680813 EU ROTOR NR STICKS A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 117 480 2728 TACHOMETER NR NEEDLE STICKS. REPLACED IWTH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400196 19980904 00196 EU 1998 9 4 98ZZZX3117 1 19980422 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 244 2728 LAMINATED TAIL ROTOR BEARING, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS 4 EACH, CORRECTED PR OBLEM. 1 G 7 1 3U H9EU 1998090400197 19980904 00197 EU 1998 9 4 98ZZZX3118 1 19980617 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 151 2728 T/R LAMINATED BEARING, ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 4 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400198 19980904 00198 EU 1998 9 4 98ZZZX3119 1 19980722 A 6410 704A33633171G HINGE SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 94LG 283 2728 LAMINATED HINGE (GREEN), ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM . 1 G 7 1 3U H9EU 1998090400199 19980904 00199 EU 1998 9 4 98ZZZX3120 1 19980522 A 7332 1130021089 SWITCH SNIAS 350 AS350B2 8680813 EU FUEL PRESSURE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 484 2917 PRESSURE SWITCH UNIT INOPERATIVE. FAILS TO INDICATE ANY PRESSSURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400200 19980904 00200 EU 1998 9 4 98ZZZX3121 1 19980619 A 6720 350A33200405 SPIDER SNIAS 350 AS350B2 8680813 EU T/R PITCH CHANGE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 547 MA0542 2917 T/R PITCH CHANGE SPIDER, SEALS DETERIORATED AND WORN BEYOND SERVICEABLE LIMITS. EXCESSIVE PLAY WITHIN SPLIT BUSHINGS. R EPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400201 19980904 00201 EU 1998 9 4 98ZZZX3122 1 19980619 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 547 2917 T/R PTICH CONTROL ROD WORN BEYOND SERIVCEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998090400202 19980904 00202 EU 1998 9 4 EYJA5660 1 19980802 A 2612 WIRE AEROSP AS355 AS355F1 8680810 EU NR 1 ENGINE BROKEN A EJYA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 07 911TX 5073 NR 1 ENGINE FIRE WARNING ILLUMINATED IN-FLIGHT. REPAIRED BROKEN WIRE AT FIRE DETECTOR. (X) 1 G 7 2 3U H11EU 1998090400203 19980904 00203 1998 9 4 HALA9800181 4 19980629 A 3418 SENSOR DOUG DC10 DC1010 3022110 WP FUSELAGE MALFUNCTIONED A HALA A UNSCHED LANDING E N VIBRATION/BUFFET FALSE WARNING CL CLIMB 1 WP 13 152AA 46707 LAS - FLT 03 - (LOG PAGE NR 4622639) - AFER ROTATION STICK SHAKER (CAPT AND FO'S) WENT OFF. STAYED ON CONSTANTLY UNTIL CLEAN UP AT 250 KNOTS. ACFT MADE UNEVENTFUL LANDING IN LAS. ON SECOND ATTEMPT, SAME PROBLEM OCCURRED, P15-STICK SHAKER ACTIVATED AFTER ROTATION, APPEARS TO BE BOTH CHANNELS. PULLED BOTH CB'S. FOUND RT AOA SENSOR BAD, REPLACED RT AOA SEN SOR PER MM 23-33-01, OPS CHECK GOOD. (ON SECOND AIR TURN BACK), REPAIRED BROKEN WIRE ON LT INBD FLAP POSITION TRANSMITT ER CONNECTOR. REPLACED LT INLET TRANSMITTER, ACCOMPLISHED ADJUSTMENT AND TEST PER MM. ACCOMPLISHED STALL WARNING TEST AND BITE CHECK BOTH AUTOTHROTTLE SPEED CONTROL COMPUTERS, NO FAULTS NOTED, CHECK NORMAL. (X) 2 L 7 3 4F A22WE 1998090400204 19980904 00204 NE 1998 9 4 98ZZZX3123 2 19980731 A 7314 1143830425 PUMP ROMEC BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 831CA 10060 4112 B981 UE20 FUEL LEAK FROM LT COWLING. FUEL PUMP, ENGINE DRIVEN, LEAKING. REPLACED FUEL PUMP. 2 L 7 2 4T 4 T RT A24CE E26NE 1998090400205 19980904 00205 EU 1998 9 4 AALA981210 1 19980622 A 2910 O-RING FOKKER F28 F28MK0100 4990807 EU NR 1 ENGINE FAILED A AALA K NONE K FLUID LOSS CR CRUISE 1 SW 07 1405J 11356 ORD - FLT 1795 - DURING CRUISE, EN ROUTE MSP/ORD, SYSTEM 1 HYDRAULIC LOW QUANTITY ALERT ON RIGHT MFDU ILLUMINATED. SYST EMS 1 AND 2 PUMPS TURNED OFF WITH 35 PERCENT QUANTITY REMAINING IN SYSTEM. ALTERNATIVE GEAR PROCEDURE USED. LANDED ORD WITHOUT INCIDENT. REPLACED NR 1 ENGINE PRESSURE LINE O-RING ON HYDRAULIC PUMP. SYSTEM GROUND CHECKED, NORMAL OPERATIO N. (X) 2 L 7 2 4F RT 1998090400206 19980904 00206 EU 1998 9 4 AALA981353 1 19980706 A 4900 QACF100 APU FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1406A P145C 11359 YYZ - FLT 1084 - AFTER TAKEOFF YYZ EN ROUTE TO LGA ON CLIMB-OUT, SMOKE WAS OBSERVED IN COCKPIT WITH BURNING SMELL. SMOK E APPEARED AFTER APU WAS SHUT DOWN IN-FLIGHT. AIRCRAFT RETURNED AND LANDED YYZ WITHOUT INCIDENT. REPLACED APU PER MM. ACCOMPLISHED OPERATIONS CHECK AND LEAK CHECK. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F RT 1998090400207 19980904 00207 NM 1998 9 4 AALA984159 1 19980625 A 5311 FRAME BOEING 767 767223 1385123 NM BS 36 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 308AA 22314 AFW - J-CAP AT STATION 36F HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACE. BLENDED AND REFINISHED THE AREA PER SRM 53 -00-07 FIG 101. THE FRAME IS ACCEPTABLE TO RETURN TO SERVICE. (M) 2 L 7 2 4F RT A1NM 1998090400208 19980904 00208 NM 1998 9 4 AALA984157 1 19980629 A 5311 FRAME BOEING 767 767223 1385123 NM BS 544 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 308AA 22314 AFW - CORROSION BLENDED BEYOND LIMITS AT TWO LOCATIONS ON FRAME STA 544. BLENDED OUT CORROSION. APPLIED ALODINE AND TW O COATS OF PRIMER TO BLENDED AREA. FORWARD BLENDED AREA WITH BMS5-95 TO RESTORE A FLUSH FINISH. TST: 50,291.20 HOURS. CYCLES: 15,033. (X) 2 L 7 2 4F RT A1NM 1998090400209 19980904 00209 NM 1998 9 4 AALA984156 1 19980625 A 5311 FRAME BOEING 767 767223 1385123 NM BS 412 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 308AA 22314 AFW - FRAME AT STA 412 HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACE. BLENDED AND REFINISHED AREA PER SRM 53-00-07 F IG 101. THE FRAME IS ACCEPTABLE TO RETURN TO SERVICE. TST: 50,291.20 HOURS. CYCLES: 15,033. (X) 2 L 7 2 4F RT A1NM 1998090400210 19980904 00210 NM 1998 9 4 AALA981360 1 19980710 A 5330 SKIN BOEING 727 727223 1384074 NM BS 178-209 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - AIRCRAFT SUSTAINED DAMAGE TO RADOME AND WRINKLES TO LT FUSELAGE. STA 178 TO STA 208, STR 17L TO STR 24L. SUSPECT AFT AIRSTAIR OUT OF RIG. REPAIRED RADOME, FUSELAGE DAMAGE. REPAIRED PER SRM 53-30-3. RIGGED AND ADJUSTED VENTRICAL S TAIR PER MM. ALL WORK ACCOMPLISHED ON W.O. NR 320 DATED 7-1-98. TULSA BOW 320-71-98. REF: OPERATOR CONTROL NR 98ZZZX 3702. (X) 2 L 7 3 4F A3WE 1998090400211 19980904 00211 WP 1998 9 4 AALA981404 1 19980718 A 3230 PIN DOUG DC9 DC982 3022082 WP MLG INSTALLED A AALA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SW 07 469AA 49599 ORD - FLT 1731 - AFTER TAKEOFF DTW, UNABLE TO RAISE MAIN LANDING GEAR. LANDED ORD WITHOUT INCIDENT. REMOVED MAIN LANDI NG GEAR DOWNLOCK PINS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998090400212 19980904 00212 WP 1998 9 4 AALA981405 1 19980717 A 3260 PSEU ELDEC DOUG DC9 DC982 3022082 WP E/E/ BAY MALFUNCTIONED A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 402A 49313 ORD - FLT 0475 - UPON GEAR EXTENSION, ALL THREE GEAR LIGHTS INDICATED UNSAFE. CREW VISUALLY INSPECTED GEARS, ALL WERE D OWN AND LOCKED. LANDED ORD WITHOUT INCIDENT. REPLACED PROXIMITY UNIT. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998090400213 19980904 00213 NM 1998 9 4 AALA981378 1 19980713 A 3510 CDB1012501 ADAPTER BOEING 767 767323 1385205 NM COCKPIT LOOSE A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 355AA 24036 LHR - FLT 0095 - EN ROUTE DURING CRUISE, THE CREW OXYGEN DROPPED FROM 1100 PSI TO 960 PSI. DIVERTED TO LHR AND LANDED W ITHOUT INCIDENT. TROUBLESHOT SYSTEM AND FOUND SEEPAGE FROM MAIN OXYGEN CONNECTOR. REPLACED OXYGEN BOTTLE AND RETORQUED ADAPTER. ACCOMPLISHED LEAK CHECK. SYSTEM GROUND CHECKED, NORMAL OPERATION. 2 L 7 2 4F RT A1NM 1998090400214 19980904 00214 NM 1998 9 4 AALA984160 1 19980715 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 374AA 25201 AFW - FLOORBEAM AT STA 347 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINED BLENDED AREA. FABRICATED STRAP FROM STAINL ESS STEEL. APPLIED 2 COATS PRIMER TO STRAP AND FLOORBEAM AND BLENDED AREA. INSTALLED STRAP WET WITH SEALANT WITH HI-L0 KS. TST: 27,816.33 HOURS. CYCLES: 4,326. (X) 2 L 7 2 4F RT A1NM 1998090400215 19980904 00215 NM 1998 9 4 AALA984161 1 19980715 A 5320 FRAME J CAP BOEING 767 767323 1385205 NM BS 1285 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 374AA 25201 AFW - CHORD (J-CAP) HAS CORROSION REMOVAL IN UPPER AND LOWER SURFACE. MATERIAL REMAINING IS BEYOND SRM LIMITS. REMOVED ALL CORROSION, ENSURED BLENDOUTS IN AREA OF NUTPLATES ARE FLAT TO ALLOW PROPER SEATING WHEN INSTALLED. REFINISHED BLEN DED AREA PER SRM 53-00-07, FIG 1D1. TST: 27,816.53 HOURS. CYCLES: 4,326. (X) 2 L 7 2 4F RT A1NM 1998090400216 19980904 00216 NM 1998 9 4 AALA984162 1 19980716 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 371AA 25198 AFW - FLOORBEAM AT STA 347 RBL 46 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINED THE BLENDED AREA, FABRICATED STRAP FROM 0.50301-1/2 HARD STEEL. APPLIED TWO COATS OF PRIMER TO THE STRAP AND FLOORBEAM. FILLED THE BLENDED AREA WITH BMS5 -92 TYPE NRS 1 AND 3. TST: 27,711.57 HOURS. CYCLES: 4,361. (X) 2 L 7 2 4F RT A1NM 1998090400219 19980904 00219 NM 1998 9 4 98ZZZX3126 1 19980814 A 7603 CONTROL CABLE PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA RT THROTTLE MALFUNCTIONED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 3645T 600852816124 646648A PILOT REPORTED NO RESPONSE FROM RT THROTTLE CONTROL. SUSPECT RT THROTTLE CABLE. CAUSE NOT YET KNOWN. 1 M 7 2 3O 3 O RT A17WE 1E4 1998090400247 19980904 00247 NE 1998 9 4 TWAA9813901 2 19980827 A 7261 RD21891 TUBE DOUG DC9 DC934 302207E WP PWA JT8 JT8D15 52051 NE NR 6 BEARING FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 05 927L 48123 1602 ENGINE OIL PRESSURE AND QUANTITY DROPPED. LOW OIL PRESSURE LIGHT CAME ON. SHUT DOWN ENGINE, DECLARED AN EMERGENCY AND MADE UNSCHEDULED LANDING AT IND. NR 6 OIL BEARING LINE IN THE TAIL HAD FAILED. REPLACED LINE. CHECK-C 1-4-98 STL. 2 L 7 2 4F 4 F RT A6WE E2EA 1998090400248 19980904 00248 WP 1998 9 4 TWAA9813902 1 19980827 A 3320 BULB DOUG DC9 DC982 3022082 WP GALLEY LOOSE A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 904TW 49156 FLIGHT ATTENDANT RECEIVED AN ELECTRICAL SHOCK WHEN TOUCHING A FLOURSCENT LIGHT IN THE FORWARD GALLEY. THE LIGHT FIXTURE END CAP HAD OPENED AND THE BULB SLIPPED PARTIALLY OUT. REINSERTED BULB AND SECURED THE CAP. CHECK-C 4-1-98 STL. 2 L 7 2 4F A6WE 1998090400249 19980904 00249 NM 1998 9 4 VJ9800304 1 19980826 A 3350 1619 BULB BOEING 737 7372L9 1384497 NM CABIN FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 465AT 21528 DURING LAY OVER CHECK, FOUND EMERGENCY LIGHT ON OUTSIDE OF THE AIRCRAFT AFT OF L-1 DOOR INOP. REPLACED LIGHT BULB CLEAN ED CONNECTIONS AND OPS CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998090400250 19980904 00250 WP 1998 9 4 VJ9800305 1 19980821 A 5320 9560321 FITTING DOUG DC9 DC932 3022066 WP BS 238 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 LT AND RT LOWER FLOOR SUPPORT FITTINGS ARE CORRODED FS 238 BETWEEN LOG 27 AND 28 IN FWD CARGO COMPT. REMOVED EXISTING F ITTINGS, REMOVED AND BLENDEDCORROSION PER DC-9 SRM 51-10-3. CORROSION BEYOND LIMITS PER DC-9 SRM 53-01 FIG 1. REPLACED EXISTING FITTINGS WITH NEW IAW DC-9 SRM 51-30-05. 2 L 7 2 4F A6WE 1998090400251 19980904 00251 WP 1998 9 4 VJ9800306 1 19980818 A 5320 1A35595 ANGLE DOUG DC9 DC932 3022066 WP BS 427 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FWD C-1 DOOR CUT-OUT SUPPORT ANGLE HAS EXFOLIATED CORROSION FS 427. MECHANICALLY REMOVED CORROSION IAW DC-9 SRM 51-10-3 . FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. FABBED NEW SPLICE IAW DC-9 SRM 51-10-2, 53-11 FIG 2D. TREATED, PRIMED, AND INSTALLED NEW SPLICE IAW DC-9 SRM 51-10-3, 51-30-2. 2 L 7 2 4F A6WE 1998090400252 19980904 00252 NM 1998 9 4 K3HA980101 1 19980826 A 2612 106037713 FIRE LOOP BOEING 727 727225 1384077 NM NR 2 ENGINE FAILED A K3HA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 25 8880Z 21453 IN TAKEOFF POSITION WITH 1.7 EPR FIRE BELL CAME ON WITH NO FIRE LIGHT SILENCE BELL RETURNED TO GATE. REMOVED AND REPLAC ED NR 2 ENGINE FIRE WALL SENSOR P/N 1050-806-585, S/N 74200 AND NR 2 ENGINE FIRE LOOP. OPS CHECKED GOOD NORMAL PER MM 2 6-11-00. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998090400253 19980904 00253 NM 1998 9 4 CALA9801538 1 19980826 A 5720 BEAM BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .75 INCH CRACK IN RT WING TRAILING EDGE J BEAM JUST ABOVE NR 8 SPOILER MOUNT. REPAIR PARTS WERE INST ALLED IAW ECRA 5720-01676. 2 L 7 3 4F A3WE 1998090400254 19980904 00254 NM 1998 9 4 CALA9801539 1 19980826 A 5754 SKIN BOEING 727 727224 1384076 NM NR 6 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 SLAT AT OUTBOARD HOOK. A REPAIR WAS ACCOMPLISHED IAW SRM 57-50-3, FIGU RE 10. 2 L 7 3 4F A3WE 1998090400255 19980904 00255 NM 1998 9 4 CALA9801540 1 19980826 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .875 INCH AND .25 INCH CRACK IN LT OUTBOARD FOREFLAP LEADING EDGE CUTOUT ABOVE NR 1 FLAP TRACK. THE FLAP WAS REPAIRED IAW SRM 57-50-4, FIGURE 1. 2 L 7 3 4F A3WE 1998090400256 19980904 00256 NM 1998 9 4 CALA9801541 1 19980826 A 5751 652172519 SKIN BOEING 727 727224 1384076 NM LT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND AREAS OF DELAMINATED SKIN ON TOP AND BOTTOM OF LT WING OUTBOARD AILERON OUTBOARD TRAILING EDGE WEDGE PA NEL. THE WEDGE PANEL WAS REMOVED AND REPAIRED IAW SRM 57-50-5. THE PANEL WAS REINSTALLED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998090400257 19980904 00257 NM 1998 9 4 CALA9801542 1 19980826 A 5320 SIDEWALL BOEING 727 727224 1384076 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .125 INCH CRACK IN LEFT SIDEWALL OF NLG WHEEL WELL. THE CRACKED AREA WAS CUT OUT IAW SRM 51-20-1. D OUBLER AND FITTINGS WERE INSTALLED IAW ECRA 5310-03759. 2 L 7 3 4F A3WE 1998090400258 19980904 00258 NM 1998 9 4 CALA9801543 1 19980826 A 5530 BOLTS BOEING 727 727224 1384076 NM VERT STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND FOUR VERTICAL STABILIZER TENSION TIE BOLTS CORRODED AT TOP OF STABILIZER. THE FOUR BOLTS WERE REMOVED AND REPLACED IAW SRM 55-20-00. 2 L 7 3 4F A3WE 1998090400259 19980904 00259 NM 1998 9 4 CALA9801544 1 19980827 A 5312 BULKHEAD BEAM BOEING 727 727224 1384076 NM BS 1183 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND TWO 1.5 CRACKS IN AFT BULKHEAD VERTICAL SUPPORT BEAM AT AFT CARGO COMPARTMENT, BS 1183, RBL 46.93. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5310-03758. 2 L 7 3 4F A3WE 1998090400260 19980904 00260 NM 1998 9 4 CALA9801545 1 19980827 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LEFT WING UPPER TRAILING EDGE SKIN TORN AT ALL THREE HINGES OF NR 6 SPOILER. THE TORN AREAS WERE CUT O UT IAW SRM 57-30-4. A DOUBLER WAS INSTALLED AT EACH OF THE THREE HINGES IAW SRM 57-30-4, FIGURE 10, SHEET 3. 2 L 7 3 4F A3WE 1998090400261 19980904 00261 NM 1998 9 4 CALA9801546 1 19980827 A 5720 ANGLE BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LT WING INBOARD NR 7 SPOILER ACTUATOR SUPPORT FITTING LOWER ANGLES (TWO EACH) RIB PANEL SUPPORTS CRACKE D. THE CRACKS WERE .5 INCH LONG. THE INBOARD AND OUTBOARD ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51 -10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998090400262 19980904 00262 NM 1998 9 4 CALA9801547 1 19980826 A 5755 651434874A SKIN BOEING 727 727224 1384076 NM NR 6 SPOILER DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND THE LT WING NR 6 SPOILER LOWER SKIN DEBONDED AT FORWARD END. THE NR 6 SPOILER WAS REMOVED AND REPLACED IAW MM 57-00 AND 27-60-1. 2 L 7 3 4F A3WE 1998090400263 19980904 00263 NM 1998 9 4 CALA9801548 1 19980826 A 5755 651734781A SKIN BOEING 727 727224 1384076 NM NR 4 SPOILER DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LT WING NR 4 SPOILER DEBONDED AT LOWER SKIN. THE NR 4 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1. 2 L 7 3 4F A3WE 1998090400264 19980904 00264 NM 1998 9 4 CALA9801549 1 19980827 A 5752 652172641K SKIN BOEING 727 727224 1384076 NM LT AILERON TAB DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LT OUTBOARD AILERON TAB TRAILING EDGE DEBONDED 41.5 INCHES FROM INBOARD END. THE OUTBOARD AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41. 2 L 7 3 4F A3WE 1998090400265 19980904 00265 NM 1998 9 4 CALA9801550 1 19980827 A 5753 6521630187 SKIN BOEING 727 727224 1384076 NM LT TE FOREFLAP DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LT INBOARD FOREFLAP DEBONDED ON LOWER SURFACE ABOVE NR 4 CARRIAGE. THE FOREFLAP WAS REMOVED AND REPLAC ED IAW MM 27-51-2. 2 L 7 3 4F A3WE 1998090400266 19980904 00266 NM 1998 9 4 CALA9801551 1 19980827 A 5753 6521634150 SKIN BOEING 727 727224 1384076 NM RT TE AFT FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND RT WING INBOARD AFT FLAP LOWER SURFACE DELAMINATED AT MID OUTBOARD AREA. THE AFT FLAP WAS REMOVED AND REPLACED IAW MM 27-51-10. 2 L 7 3 4F A3WE 1998090400267 19980904 00267 NM 1998 9 4 CALA9801552 1 19980827 A 5523 657279946 SKIN BOEING 727 727224 1384076 NM RT ELEV TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND RT ELEVATOR CONTROL TAB INBOARD TRAILING EDGE DELAMINATED. THE ELEVATOR CONTROL TAB WAS REMOVED AND RE PLACED IAW MM 27-30-11. 2 L 7 3 4F A3WE 1998090400268 19980904 00268 NM 1998 9 4 CALA9801553 1 19980827 A 5720 BEAM BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN J BEAM AT CUTOUT AREA ABOVE NR 7 SPOILER. THE J BEAM WAS REPAIRED IAW ECRA 5780-029 14. 2 L 7 3 4F A3WE 1998090400269 19980904 00269 NM 1998 9 4 CALA9801554 1 19980827 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .25 INCH CRACK IN FUSELAGE SKIN JUST FORWARD OF CAPTAIN'S WINDSHIELD WIPER AREA. THE CRACKED AREA WAS CUT OUT IAW SRM 51-10-1. A DOUBLER, TRIPLER, AND FILLER WERE INSTALLED IAW SRM 51-30-2, 51-20-4, AND ECRA 5330-02698. 2 L 7 3 4F A3WE 1998090400270 19980904 00270 NM 1998 9 4 CALA9801555 1 19980827 A 5751 RIB BOEING 727 727224 1384076 NM RT AILERON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN RT OUTBOARD AILERON LEADING EDGE RIB JUST OUTBOARD OF NR 3 HINGE. THE RIB WAS REMOVE D AND REPLACED IAW SRM 51-10-1, PAGE 4. 2 L 7 3 4F A3WE 1998090400271 19980904 00271 NM 1998 9 4 CALA9801556 1 19980827 A 5753 651926920 BOLT BOEING 727 727224 1384076 NM NR 5 FLAP TRACK CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND RT WING FLAP TRACK NR 5 CORRODED AT FORWARD ATTACH BOLT. THE NR 5 FLAP TRACK AND ATTACH BOLT WERE REMO VED AND REPLACED IAW MM 57-50-0. 2 L 7 3 4F A3WE 1998090400272 19980904 00272 NM 1998 9 4 CALA9801557 1 19980827 A 5551 FITTING BOEING 727 727224 1384076 NM HORIZ STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND LT AND RT HORIZONTAL STABILIZER ATTACH FITTING CORRODED. THE CORROSION WAS REMOVED BY BORING HOLES. N EW BUSHINGS AND BEARINGS WERE INSTALLED. THE BEARINGS WERE TORQUED AND SAFETIED IAW ECRA 5550-01033. 2 L 7 3 4F A3WE 1998090400273 19980904 00273 NM 1998 9 4 CALA9801558 1 19980827 A 5741 69139017 BOTTLE PIN BOEING 727 727224 1384076 NM RT WING BODY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND RT AFT BOTTLE PIN CORRODED. THE BOTTLE PIN AND FORWARD AND AFT BUSHINGS WERE REMOVED AND REPLACED, THE N SAFETIED AND SEALED IAW MM 57-41-1. 2 L 7 3 4F A3WE 1998090400274 19980904 00274 WP 1998 9 4 CALA9801559 1 19980826 A 5730 SKIN DOUG DC10 DC1030 3023501 WP WS 683 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19072 46576 INSPECTION FOUND A 1.5 CRACK IN LT WING LEADING EDGE SKIN AT STA XORS 683. THE SKIN WAS REPAIRED IAW SRM 57-10-00, FIGU RE 49 AND FIGURE 68, SHEET 10. 2 L 7 3 4F A22WE 1998090400275 19980904 00275 NM 1998 9 4 CALA9801560 1 19980826 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1010 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBOARD SUPPORT CORRODED WITH TWO .5 INCH CRACKS AT BS 1010 BETWEEN STRINGERS 27R AND 28R. A DOUBLE R WAS INSTALLED IAW SRM 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 1998090400276 19980904 00276 NM 1998 9 4 CALA9801561 1 19980826 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1166 ABOVE STRINGER 29R. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS INS TALLED IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998090400277 19980904 00277 NM 1998 9 4 CALA9801562 1 19980826 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 480 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBEAM CORRODED AT STA 480, RBL 24-65. A CHORD, ANGLES, STRAPS, AND STIFFENERS WERE INSTALLED IAW S RM 53-10-8, FIGURE 1. 2 L 7 3 4F A3WE 1998090400278 19980904 00278 NM 1998 9 4 CALA9801563 1 19980826 A 5712 RIB BOEING 727 727232 1384082 NM LT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN LT WING TIP RIB AT PANEL NR 8110. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400279 19980904 00279 NM 1998 9 4 CALA9801564 1 19980826 A 5320 FRAME BOEING 727 727232 1384082 NM CARGO DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 CRACK AT FASTENER HOLE OF WEB AT NR 2 CARGO DOORWAY FORWARD FRAME BS 950E. A REPAIR WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400280 19980904 00280 NM 1998 9 4 CALA9801565 1 19980827 A 5311 FRAME BOEING 727 727232 1384082 NM BS 372 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FUSELAGE FRAME CORRODED ON FORWARD SIDE AT STA 372 BETWEEN STRINGER 17R AND 20R. THE CORRODED SECTION WAS REMOVED AND A FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-40-3 AND 51-30-2. 2 L 7 3 4F A3WE 1998090400281 19980904 00281 WP 1998 9 4 CALA9801566 1 19980828 A 3230 UPLATCH MECH DOUG DC9 DC932 3022066 WP RT MLG OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 18544 47219 THE RT MLG UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING IAH. THE GEAR WAS CYCLED AND THE LIGHT EXTIN GUISHED, BUT THE GEAR DOOR OPEN LIGHT REMAINED ON. THE AIRCRAFT WAS RETURNED TO IAH. BOTH THE LT AND RT MLG DOORS WERE DAMAGED ON LANDING. THE MLG DOORS WERE REMOVED AND REPLACED IAW MM 32-12-1. TROUBLESHOOTING FOUND THE RT MLG UPLATCH MECHANISM OUT OF ADJUSTMENT. THE UPLATCH MECHANISM WAS ADJUSTED IAW MM 32-31-4. A GEAR SWING WAS PERFORMED AND ALL OPE RATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998090400282 19980904 00282 WP 1998 9 4 CALA9801567 1 19980827 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 294 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14818 49478 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 294, LONGERON 23L AND 25L. THE DENTED AREAS WERE CUT OUT AND A REPAIRS WER E INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1998090400283 19980904 00283 WP 1998 9 4 CALA9801568 1 19980827 A 5350 CLIPS DOUG DC9 DC931 3022065 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14564 47490 THE FORCE REQUIRED TO RELEASE TAILCONE EXTERIOR HANDLE FROM CLIPS WAS LOW AT 15 POUNDS. THE CLIPS WERE REPLACED AND ADJ USTED IAW MM 53-50-3. 2 L 7 2 4F A6WE 1998090400284 19980904 00284 NM 1998 9 4 CALA9801569 1 19980827 A 5320 ANGLE BOEING 737 7372C0 1384488 NM BS 294-325 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND ANGLE CORRODED AT STA 294.5 TO 325.38, LBL 8. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 5 1-30-5. 2 L 7 2 4F A16WE 1998090400285 19980904 00285 NM 1998 9 4 CALA9801570 1 19980827 A 3350 6013211 POWER SUPPLY GRIMES BOEING 737 737291 138448W NM CABIN INOPERATIVE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10251 20361 INSPECTION FOUND SECTION OF EMERGENCY FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. MAINTENANCE FOUND THE M913 POWER SU PPLY AT STA 776 AT FAULT. THE M913 POWER SUPPLY WAS REMOVED AND REPLACED AND OPERATION OF THE EMERGENCY FLOOR PATH LIGH TING WAS RESTORED. 2 L 7 2 4F A16WE 1998090400286 19980904 00286 NM 1998 9 4 UPS98227567 1 19980824 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 850 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:SI CORROSION BETWEEN SEAT TRACK AND EXPANSION LINK FLANGES BS 850 LBL 45 WO L208. REPLACED SEAT TRACK O N EXPANSION LINK PER 727 SRM 51-30-2, 51-20-151 51-30-5, 51-10-1. 2 L 7 3 4F A3WE 1998090400287 19980904 00287 NM 1998 9 4 UPS98227568 1 19980819 A 5311 FRAME BOEING 727 727247 138408F NM BS 294.5 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:SI CORROSION (C53-111-03.00-01) ON FRAME WEB AT BS 294.5 WL 167-169 RBL 35-40 FABRICATED NEW WEB AND INSTALLED WORK DONE IAW SRM 53-10-1, 51-40-2 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998090400288 19980904 00288 NM 1998 9 4 UPS98227569 1 19980820 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 1070 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE:SI CORROSION ON SEAT TRACK UPPER AND LOWER FLANGES STA 1070-1130 RBL 45 WL 208. REMOVED CORRODED SEAT T RACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-30-2, 53-10-5. 2 L 7 3 4F A3WE 1998090400289 19980904 00289 NM 1998 9 4 UPS98227571 1 19980808 A 5320 STRAP BOEING 727 72751C 1384015 NM WINDOW POST CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D ON ACCOMPLISHMENT OF EDDY CURRENT INSPECTION OF RT E-F WINDOW POST PER EO B727-5310-0012, CRACKS FOUND ON 3 HOLES COMMON TO REPAIR STRAP. REPAIR CARRIED OUT IAW SRS ENGINEERING ORDER 98-24-012, REF UPS ENGINEERING FILE NU MBER 727-5310-2066. 2 L 7 3 4F A3WE 1998090400290 19980904 00290 NM 1998 9 4 UPS98227572 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 440 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D SUSPECT CRACK ON STRINGER 23R AT STA 440. REPLACED PART WITH 69-14492-5 IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400291 19980904 00291 NM 1998 9 4 UPS98227573 1 19980811 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 420 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D CRACK ON UPPER FLANGE OF FRAME AT BS 420, BL 0. REPAIR CARRIED OUT ON UPPER FLANGE IAW SRM 51-40-3, F IG 1. 2 L 7 3 4F A3WE 1998090400292 19980904 00292 NM 1998 9 4 UPS98227574 1 19980812 A 5313 STRINGER BOEING 727 72751C 1384015 NM BS 260-277 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D STRINGER ON TOP OF NOSE WHEEEL WELL AT BL 0, BS 260 TO 277 IS CORRODED. STRINGER SECTION REPAIRED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1998090400293 19980904 00293 NM 1998 9 4 UPS98227575 1 19980804 A 5311 FRAME BOEING 727 72751C 1384015 NM BS 560 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D SUSPECT CRACK IN OUTER FLANGE OF FRAME 560 RT. FLANGE REPAIRED IN IAW SRM 53-10-4, FIG 11. 2 L 7 3 4F A3WE 1998090400294 19980904 00294 NM 1998 9 4 UPS98227576 1 19980804 A 5730 PANEL BOEING 727 72751C 1384015 NM WS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D LT WING TANK FROMT SPAR ACCESS PANEL NR 1 CORRODED. PANEL REPLACED IAW MM 28-11-21. 2 L 7 3 4F A3WE 1998090400295 19980904 00295 NM 1998 9 4 UPS98227577 1 19980727 A 2782 MOUNTING BOEING 727 72751C 1384015 NM NR 2 LE SLAT ACT WORN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE:D NR 2 L/E SLAT ACTUATOR VERY LOOSE IN MOUNTING STRUCTURE. MOUNTING REPLACED IAW EO B727-5720-1058. 2 L 7 3 4F A3WE 1998090400296 19980904 00296 NM 1998 9 4 UPS98627570 1 19980825 A 5720 ANGLE BOEING 767 76734AF 1385212 NM WS 512-500 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 310UP 27762 INSPECTION TYPE:ETOP LEFT WING NR 6 SLAT LOWER TE COVE SUPPORT ANGLES CRACKED AT POSITIONS 3, 4, 5, 6 AND 7 FROM OUTBOAR D END. REMOVED CRACKED SUPPORT ANGLES, FABRICATED AND INSTALLED NEW SUPPORT ANGLES IAW SRM 51-30-01, SRM 51-21-01, SRM 51-40-02. 2 L 7 2 4F RT A1NM 1998090400297 19980904 00297 EU 1998 9 4 QXEA9801095 1 19980825 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 490US 11152 PDX - EMERGENCY LIGHT OVER 9E IS OUT. MAINTENANCE REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998090400298 19980904 00298 EU 1998 9 4 QXEA9801096 1 19980825 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 11156 BOI - EXIT SIGN ABOVE GALLEY DOOR WAY IS INOPERATIVE. MAINTENANCE RELAMPED EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD . 2 L 7 2 4F RT A20EU 1998090400299 19980904 00299 NM 1998 9 4 98FDEA00533 1 19980826 A 5230 651862013 CHANNEL BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR0424 FWD CARGO DOOR #4 TRANSVERSE BEAM (FROM BOTTOM) IS CRACKED IN OUTBOARD RADIUS. *** S/D ***R&R FWD CARGO DOO R #4 TRANSVERSE BEAM IAW FEDEX DRAWING 65-18620. 2 L 7 3 4F A3WE 1998090400300 19980904 00300 NM 1998 9 4 98FDEA00534 1 19980826 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A FDEA O OTHER L NO TEST CR CRUISE 1 SO 25 119FE 19301 NR 0468 ON TEST HOP FOUND MAIN CABIN DOOR EMER EXIT LIGHT BATTERY TO BE VERY LOW. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CK GOOD PER FED-EX M/M 33-10-0. 2 L 7 3 4F A3WE 1998090400301 19980904 00301 NM 1998 9 4 98FDEA00535 1 19980827 A 5230 651862068 SKIN BOEING 727 72725C 138400H NM CARGO DOOR CREASED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 FWD CARGO DOOR OUTER SKIN IS DENTED 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM. *S/D* REPAIRED FWD CARGO DOOR 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM, PER FEDEX SRM 52-00-3. 2 L 7 3 4F A3WE 1998090400302 19980904 00302 WP 1998 9 4 ABXA9800796 1 19980807 A 5531 9918901 RIB DOUG DOUG DC9 DC941 302207N WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 975AX 47512 DURING C-CHECK, FOUND RIB CRACKED IN THE VERTICAL STABILIZER LEADING EDGE. REPLACED RIB IAW DC9 SRM CHAPTERS 51-30-2 AN D 51-30-5. 2 L 7 2 4F A6WE 1998090400303 19980904 00303 WP 1998 9 4 ABXA9800797 1 19980825 A 5400 995815963 ANGLE DOUG DOUG DC9 DC941 302207N WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND ANGLE CRACKED INSIDE NR 1 PYLON ABOVE AFT OUTBOARD CORNER OF PANEL 8105. REPLACED ANGLE IAW DC9 S RM 54-01 AND 51-30-2. 2 L 7 2 4F A6WE 1998090400304 19980904 00304 WP 1998 9 4 ABXA9800798 1 19980825 A 5313 76378133 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 389 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATION 389. REPLAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998090400305 19980904 00305 WP 1998 9 4 ABXA9800799 1 19980825 A 5320 995766412 FRAME DOUG DOUG DC9 DC941 302207N WP CARGO DOORWAY CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR FRAME CRACKED FORWARD OF AFT HINGE. REPLACED FRAME WEB I AW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998090400306 19980904 00306 WP 1998 9 4 ABXA9800800 1 19980825 A 5510 5922578503 STRINGER DOUG DOUG DC9 DC941 302207N WP LT HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND THE THIRD STRINGER UPPER FLANGE EXFOLIATED IN INTERIOR OF THE LEFT HORIZONTAL STABILIZER AT STATIO N XHR 7. REPAIRED IAW ABX REA D955-24651 MR. 2 L 7 2 4F A6WE 1998090400307 19980904 00307 WP 1998 9 4 ABXA9800801 1 19980825 A 5313 592480225 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 237-256 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT STATIONS 237, 256 AND 313. REPLACED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998090400308 19980904 00308 WP 1998 9 4 ABXA9800802 1 19980825 A 5320 99577397 SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT STATION 1021 AND LONGERONS 15R AND 16R. REPLACED SHEAR TIE IA W DC9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1998090400309 19980904 00309 WP 1998 9 4 ABXA9800803 1 19980825 A 5313 59364369 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND LONGERON 13L CRACKED AT HI-LOCK AT STATION 1041. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998090400310 19980904 00310 WP 1998 9 4 ABXA9800804 1 19980825 A 5320 995773925N SHEAR TIE DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND FUSELAGE FRAME SHEAR TIE STATION 1021 CRACKED BETWEEN LONGERONS 15L - 16L AND 14R - 15R. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-05. 2 L 7 2 4F A6WE 1998090400311 19980904 00311 WP 1998 9 4 ABXA9800805 1 19980825 A 5320 49177013 INTERCOSTAL DOUG DOUG DC9 DC941 302207N WP BS 1244 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND INTERCOSTAL CRACKED AT STATION 1244, LEFT SIDE BELOW SERVICE LIGHT SWITCH. REPLACED INTERCOSTAL I AW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998090400312 19980904 00312 WP 1998 9 4 ABXA9800806 1 19980825 A 5313 591140513 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998090400313 19980904 00313 WP 1998 9 4 ABXA9800807 1 19980825 A 5312 59364369 BULKHEAD WEB DOUG DOUG DC9 DC941 302207N WP BS 1117 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND BULKHEAD WEB AT STATION 1117 CRACKED AT LONGERON 13L. REPAIRED BULKHEAD WEB IAW DC9 SRM 53-11 AND DWG 9912246. 2 L 7 2 4F A6WE 1998090400314 19980904 00314 WP 1998 9 4 ABXA9800808 1 19980825 A 5412 59177177 ANGLE DOUG DOUG DC9 DC941 302207N WP BS 1117 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND ANGLE ON AFT FACE OF THE LEFT AFT PYLON BULKHEAD STATION 1117 AT LONGERON 15L CRACKED. REPLACED A NGLE IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998090400315 19980904 00315 WP 1998 9 4 ABXA9800809 1 19980825 A 5312 49191471 FITTING DOUG DOUG DC9 DC941 302207N WP BS 1117 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 969AX 47464 DURING C-CHECK, FOUND FITTING ON AFT FACE OF THE LEFT AFT PYLON BULKHEAD, STATION 1117, AT LONGERON 15L CRACKED. REPLA CED FITTING IAW DC9 SRM 51-30-1, 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998090400316 19980904 00316 WP 1998 9 4 SCNA98091 1 19980814 A 3350 EMBS1392 POWER SUPPLY DOUG DC10 DC1015 3022118 WP CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 154SY 48259 DURING A LINE MAINTENANCE CHECK, THE MID CABIN EMERGENCY LIGHTING POWER SUPPLY FAILED SELF TEST. REMOVED AND REPLACED M ID CABIN EMERGENCY LIGHTING (OVERHEAD) POWER SUPPLY AND BATTERY. EMERGENCY LIGHTING BITE TESTS GOOD AND OPERATIONALLY C HECKS NORMAL. 2 L 7 3 4F A22WE 1998090400317 19980904 00317 NM 1998 9 4 SCNA98092 1 19980819 A 3350 6104781 BATTERY PACK BOEING 727 7272A1 138407F NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EVACUATION SLIDE LIGHTS WERE FOUND TO BE INOPERATIVE AT DOOR L2 AND R2. R EMOVED AND REPLACED THE BATTERY PACK FOR THE EVACUATION SLIDE LIGHTS AT DOORS L2 AND R2. 2 L 7 3 4F A3WE 1998090400318 19980904 00318 NM 1998 9 4 SCNA98093 1 19980819 A 3350 6104781 BATTERY PACK BOEING 727 7272A1 138407F NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 286SC 21601 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY EVACUATION SLIDE LIGHTS WERE FOUND TO BE INOPERATIVE AT DOOR L1 AND R1. R EMOVED AND REPLACED THE BATTERY PACK FOR THE EVACUATION SLIDE LIGHTS AT DOORS L1 AND R1. 2 L 7 3 4F A3WE 1998090400319 19980904 00319 NM 1998 9 4 SCNA98090 1 19980819 A 2910 LINE BOEING 727 7272A1 138407F NM ELEVATOR RUPTURED A SCNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 15 286SC 21601 AFTER DEPARTURE LOSS OF A SYSTEM HYDRAULIC QUANTITY UPON GEAR RETRACTION. PERFORMED ALL COM PROCEDURES AND DUMPED FUEL. RETURNED TO MSP. FOUND RUPTURED LINE ON ELEVATOR ACCESSORY. REMOVED AND REPLACED LINE WITH FOLLOWING LEAK AND OPERAT IONAL CHECKS GOOD. 2 L 7 3 4F A3WE 1998090400320 19980904 00320 NM 1998 9 4 SCNA98094 1 19980819 A 2612 656020911 FIRE BELL BOEING 727 7272J4 1384006 NM COCKPIT INOPERATIVE A SCNA O OTHER P NO WARNING INDICATION IN INSP/MAINT 1 GL 15 285SC 783 21676 DURING A LINE MAINTENANCE CHECK, THE FIRE WARNING BELL IN THE COCKPIT WAS FOUND TO BE INOPERATIVE DURING A FIRE TEST. R EMOVED AND REPLACED THE ENGINE FIRE DETECTION UNIT. OPERATIONALLY CHECKS GOOD PER MAINTENANCE MANUAL CHAPTER 261101. 2 L 7 3 4F RT A3WE 1998090400321 19980904 00321 NM 1998 9 4 SCNA98095 1 19980819 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, RIGHT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLA CED THE BATTERY PACK FOR THE LIGHT. OPERATIONALLY CHECKS GOOD PER MAINTENANCE MANUAL 335022. 2 L 7 3 4F RT A3WE 1998090400322 19980904 00322 NM 1998 9 4 SCNA98096 1 19980826 A 3350 1000677 LIGHT BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE L1 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD PER MAINTENANCE MANUAL 3350101. 2 L 7 3 4F A3WE 1998090400323 19980904 00323 WP 1998 9 4 RRXA98416 1 19980815 A 5320 5711283516 FITTING DOUG DC8 DC871F 302199D WP BS 985 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 500MH 45812 DURING A MAINTENANCE VISIT, (BER) LOWER AFT, CARGO SEPARATOR FIITING (PN: 5711283-516), AT STA 985. MANUFACTURED NEW FI TTING IAW DWG DAC 5711283, DPS4.999 AND DC-8 SRM 51-1-1A. USE FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05273 FOR M ATERIAL SUBSTITUTION, IT IS ACCEPTABLE TO USE 7075-T6511 ALUMINUM ALLOY EXTRUDED BAR PER QQ-A-200/11 IN PLACE OF 7075 FO RGING TO FABRICATE FITTING. 2 L 7 4 4F RT 4A25 1998090400324 19980904 00324 WP 1998 9 4 RRXA98417 1 19980827 A 5330 5750322123 SKIN DOUG DC8 DC873F 302199F WP BS 1260-1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FUSELAGE, INTERIOR SKIN WITH CORROSION DAMAGED BEYOND LIMITS IAW DC-8 SRM, AT STA 1260 TO STA 1280 AND LONGERON 36. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPA IR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05269. 2 L 7 4 4F RT 4A25 1998090400325 19980904 00325 WP 1998 9 4 RRXA98418 1 19980825 A 5330 5773863125127 SKIN DOUG DC8 DC873F 302199F WP BS 70-130 DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND FUSELAGE EXTERIOR SKIN WITH MULTIPLE DENTS IN VARIOUS ARES, DAMAGED IS BEYOND LIMITS I AW DC-8 SRM, AT STA 70 TO STA 130 LEFT SIDE. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05277. 2 L 7 4 4F RT 4A25 1998090400326 19980904 00326 NM 1998 9 4 K3HA980100 1 19980826 A 3350 0816901 LIGHT MODULE BOEING 727 727225 1384077 NM R-2 DOOR MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 EMERGENCY PATH TRACK LIGHT AT R-2 DOOR, RED LENS SOCKET MISSING. INSTALLED NEW RED LENS (P/N 07912-3), NEW SOCKET (P/N 08169-01) AND LAMP (P/N 307). OPS CHECK OK. 2 L 7 3 4F A3WE 1998090400327 19980904 00327 1998 9 4 CALA9801571 4 19980827 A 2565 LIGHT BFGOODRICH DOUG DC9 DC931 3022065 WP R1 DOOR SLIDE INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14564 2258 47490 THE R-1 DOOR EMERGENCY EVACUATION SLIDE FAILED SLIDE LIGHT TEST. THE R-1 DOOR SLIDE WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1998090400328 19980904 00328 WP 1998 9 4 CALA9801572 1 19980828 A 3230 PANEL DOUG DC9 DC982 3022082 WP COCKPIT MISMANUFACTURED A CALA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SW 09 83870 48056 THE LANDING GEAR HANDLE COULD NOT BE RAISED AFTER TAKEOFF. QRH CHECKLIST PROCEDURES WERE FOLLOWED TO NO AVAIL. THE AIR CRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT A BURR ON CENTER INSTRUMENT PANEL CU TOUT WAS CAUSING THE GEAR HANDLE TO STICK. THE BURR WAS REMOVED. THE LANDING GEAR WAS SWUNG SEVERAL TIMES AND OPERATIO N CHECKED GOOD. 2 L 7 2 4F A6WE 1998090400329 19980904 00329 NM 1998 9 4 CALA9801573 1 19980827 A 5330 SKIN BOEING 727 727224 1384076 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND FUSELAGE SKIN CORRODED AT LT SIDE, STA 1166, TWO INCHES ABOVE TOP OF FLOORBEAM. THE CORRODED AREA WAS CUT OUT, A DOUBLER WAS INSTALLED IAW ECRA 5330-02699. 2 L 7 3 4F A3WE 1998090400330 19980904 00330 NM 1998 9 4 CALA9801574 1 19980827 A 5320 STIFFENER BOEING 727 727224 1384076 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO STIFFENER AT STA 950A, LONGERON 29R. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2, 51-10-1, 51-10-2. 2 L 7 3 4F A3WE 1998090400331 19980904 00331 NM 1998 9 4 CALA9801575 1 19980827 A 2752 BRACKET BOEING 727 727224 1384076 NM LT TE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .375 INCH CRACK IN SUPPORT BRACKET FOR LT WING NR 1 LEADING EDGE FLAP ACTUATOR. A NEW BRACKET WAS IN STALLED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998090400332 19980904 00332 NM 1998 9 4 CALA9801576 1 19980827 A 5720 CHANNEL BOEING 727 727224 1384076 NM WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 1.25 INCH CRACK IN CHANNEL INSIDE TRAILING EDGE AT UPPER SKIN OUTBOARD END OF AFT FALSE SPAR ABOVE NR 3 FLAP TRANSMISSION. A NEW CHANNEL WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400333 19980904 00333 NM 1998 9 4 CALA9801577 1 19980827 A 5754 RIB BOEING 727 727224 1384076 NM NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A 1 INCH CRACK IN NR 5 SLAT ACTUATOR INBOARD ATTACH RIB. THE CRACK WAS STOP DRILLED, A REPAIR WAS INST ALLED IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1998090400334 19980904 00334 NM 1998 9 4 CALA9801578 1 19980827 A 2782 BRACKET BOEING 727 727224 1384076 NM NR 2 LE SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 32725 20655 INSPECTION FOUND A .5 INCH CRACK IN SUPPORT BRACKET FOR LT WING NR 2 LEADING EDGE FLAP ACTUATOR. A NEW BRACKET WAS INST ALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400335 19980904 00335 NM 1998 9 4 CALA9801579 1 19980828 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 477 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND STRINGER 23R CORRODED AT STA 477. THE CORRODED AREA OF STRINGER WAS REMOVED IAW SRM 53-10-3. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998090400336 19980904 00336 NM 1998 9 4 CALA9801580 1 19980828 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 970-990 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND .5 TO 1 INCH CRACKS IN INTERCOSTAL UPPER ANGLE AT FS 970 TO 990, BL 0. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400337 19980904 00337 NM 1998 9 4 CALA9801581 1 19980828 A 5754 TRACK GUIDE BOEING 727 727232 1384082 NM NR 3 LE SLAT GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND THE OUTBOARD TRACK GUIDE FOR NR 3 SLAT INBOARD TRACK GOUGED. THE TRACK GUIDE WAS REMOVED AND A NEW GUI DE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400338 19980904 00338 NM 1998 9 4 CALA9801582 1 19980828 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 29.5. THE CORRODED AREA OF FLOORBEAM WAS CUT OUT. DOUBLERS AND A T EE WERE INSTALLED IAW SRM 53-10-8, 51-10-2, 51-40-3, 51-30-2, AND MM 51-20-1. 2 L 7 3 4F A3WE 1998090400339 19980904 00339 NM 1998 9 4 CALA9801583 1 19980828 A 5313 STIFFENER BOEING 737 7372C0 1384488 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 2 INCH CRACK AT LOWER ATTACH POINT OF VERTICAL STIFFENER AT AFT CARGO FORWARD PRESSURE BULKHEAD STA 7 27, LBL 18. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998090400340 19980904 00340 WP 1998 9 4 CALA9801584 1 19980828 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 549 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14818 49478 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 549, LONGERON 25R. REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 28. 2 L 7 2 4F A6WE 1998090400341 19980904 00341 WP 1998 9 4 CALA9801585 1 19980828 A 5230 SKIN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR SKIN AT LOWER AFT CORNER. THE CRACKED AREA WAS CUT OUT AND A DOUB LER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 4. 2 L 7 2 4F A6WE 1998090400342 19980904 00342 WP 1998 9 4 CALA9801586 1 19980828 A 5320 CLIP DOUG DC9 DC932 3022066 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 2 INCH CRACK IN SHEAR TIE CLIP AT LT AFT CABIN STA 965 UNDER LONGERON 13L. THE CRACK WAS REMOVED AND A CLIP REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 28. 2 L 7 2 4F A6WE 1998090400343 19980904 00343 WP 1998 9 4 CALA9801587 1 19980828 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14818 49478 INSPECTION FOUND A .625 INCH SQUARE INCH AREA OF MAIN CABIN DOOR EXTERIOR SKIN LOWER AFT CORNER TORN OUT. REPAIRED IAW SRM 52-05, FIGURE 37 AND 51-10-3. 2 L 7 2 4F A6WE 1998090400344 19980904 00344 WP 1998 9 4 9810011160 1 19980825 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 160US 46769 CENTER LANDING GEAR WHEEL WELL REAR SHELF AREA HAS EXPOSED METAL AND CORROSION AT FS 1509 TO 1521 FROM LEFT KEEL WEB TO RIGHT KEEL WEB. REPAIRED PER EA 11-158662. 2 L 7 3 4F A22WE 1998090400345 19980904 00345 WP 1998 9 4 9810021155 1 19980825 A 5540 BRACKET DOUG DC10 DC1040 3023508 WP RUDDER CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 155US 46764 DURING M-CHECK, FOUND CORROSION IN UPPER FASTENER BRACKET IN RUDDER. REPAIRED PER EA 11-160285. 2 L 7 3 4F A22WE 1998090400346 19980904 00346 WP 1998 9 4 9809999621 1 19980826 A 3260 SENSOR DOUG DC9 DC932 3022066 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 621NW 47544 DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW PERFORMED EMERGENCY GEAR EXTENSI ON PROCEDURES AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PROXIMITY SENSOR BROKEN. REPL ACED SENSOR. ALSO REPLACED THE LEFT MAIN GEAR DOOR DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998090400347 19980904 00347 SO 1998 9 4 COMA9810184 1 19980830 A 3230 12043270501 RELAY BOX EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 168CA 16510 6071 120168 LANDING GEAR DID NOT RETRACT. REPLACED THE LANDING GEAR RELAY BOX. 2 L 7 2 4T RT A31SO 1998090400348 19980904 00348 SO 1998 9 4 COMA9810185 1 19980830 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE UNLATCHED A COMA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 01 256CA 120245 DOORS WARNING AFTER TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT SECURED. CLOSED AND LATCHED DOOR. 2 L 7 2 4T RT A31SO 1998090400349 19980904 00349 SO 1998 9 4 COMA9810186 1 19980822 A 6120 78249046 PCU EMB 120 EMB120RT SO RT PROPELLER OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 463CA 11440 120267 RIGHT HAND ENGINE NP WAS 102 PERCENT DURING CLIMB. ADJUSTED THE PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A31SO 1998090400350 19980904 00350 EA 1998 9 4 COMA9860242 1 19980829 A 3830 CD1398503 DRAIN CNDAIR CL600 CL6002B19 EA GALLEY NOISY A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 946CA 7072 NOISE FROM CABIN DOOR AREA. REPLACED THE GALLEY DRAIN ASSY. 2 L 7 2 4F RT A21EA 1998090400351 19980904 00351 EA 1998 9 4 COMA9860243 1 19980827 A 2750 860D10018AB FECU CNDAIR CL600 CL6002B19 EA E/E COMPT FAILED A COMA O OTHER O OTHER AP APPROACH 1 SO 01 969CA 6676 7141 FLAPS FAILED WHEN SELECTED FOR LANDING. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1998090400352 19980904 00352 EA 1998 9 4 COMA9860244 1 19980827 A 3233 17008109 ACTUATOR CNDAIR CL600 CL6002B19 EA LT MLG LEAKING A COMA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 963CA 5312 7127 NR 3 HYDRAULIC SYSTEM QUANTITY IS LOW. REPLACED THE LEFT HAND MLG RETRACT ACTUATOR. 2 L 7 2 4F RT A21EA 1998090400353 19980904 00353 EA 1998 9 4 COA9860245 1 19980821 A 2910 601R7514771 LINE CNDAIR CL600 CL6002B19 EA NR 3 HYD SYST LEAKING A COMA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 01 914CA 7012 NR 3 HYDRAULIC SYSTEM FAILED DURING FLIGHT. REPLACED LEAKING BALL ATTENUATOR LINE ON PUMP 3A. 2 L 7 2 4F RT A21EA 1998090400354 19980904 00354 NM 1998 9 4 UPS98227581 1 19980828 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT OUT AT GALLEY EXIT. REMOVED AND REPLACED BATTERY PACK AT GALLEY EXIT FOR EMER GENCY LIGHTS. 2 L 7 3 4F A3WE 1998090400355 19980904 00355 WP 1998 9 4 UPS98827578 1 19980530 A 5320 JAMB DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, MAIN CARGO DOOR AFT JAMB DRILLED HOLE IS CRACKED AND A PIECE IS BROKEN OFF. MATERIAL ID FOR REPAI R .063 2024 T4 IAW DOUGLAS DWG 57772787, HEAT TREATED MATERIAL FROM 2024-0 TO 2024 T4 IAW TPS-1003 REV A. MATERIAL ID F ILLER .063 2024 T4 IAW DOUGLAS 5772787. FAB DRILLED DOUBLER AND FILLER FROM 2024 T4 IAW DC8 SRM 53-2-00. ALODINED AN D PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER AND A FILLER IAW DC8 SRM. 2 L 7 4 4F RT 4A25 1998090400356 19980904 00356 WP 1998 9 4 UPS98827579 1 19980527 A 5730 SKIN DOUG DC8 DC873F 302199F WP CENTER WING DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, RT WING CENTER LEADING EDGE INBOARD UPPER SKIN 2 SCREW COUNTERSUNK DAMAGED. FABRICATED BUSHING IA W REO 04899, FABRICATED REPAIR DOUBLER IAW REO 04899. INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-21, INSTALLED REPAIR BU SHING IAW DC8 SRM 51-1-25. 2 L 7 4 4F RT 4A25 1998090400357 19980904 00357 WP 1998 9 4 UPS98827580 1 19980521 A 5320 PAN DOUG DC8 DC873F 302199F WP R1 DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, R1 DOOR JAMB AFT LOWER PAN REPAIR IS CRACKED. REMOVED DAMGED SECTION, FABRICATED PAN SECTION SPLI CE ANGLE IAW RE O 04777. FABRICATED SEAL DEPRESSOR IAW DAC 5615700. RECEIVED EXTERNAL STRAP FROM SHOP (P/N 3887438-501 ) PER REO 04777 AND OP 50025. FABRICATED INNER SKIN IAW DAC DWG 5615700. FABRICATED EXTERNAL STRAP IAW DC8 SRM 51-3-2. INSTALLED INNER SKIN PAN, EXTERNAL STRAP. 2 L 7 4 4F RT 4A25 1998090400358 19980904 00358 NM 1998 9 4 98FDEA00536 1 19980828 A 5230 65186256 BEAM BOEING 727 72725C 138400H NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR 0072 AFT CARGO DOOR #4 TRANSVERSE BEAM HAS CRACK INDICATION AT OUTBOARD FLANGE. *** S/D *** R&R #4 TRANSVERS E BEAM IN AFT CARGO DOOR IAW FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1998090400359 19980904 00359 WP 1998 9 4 ABXA9800810 1 19980826 A 3350 60030431 SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 943AX 47528 COCKPIT EMERGENCY LIGHT TEST WAS DIM. REPLACED EMERGENCY LIGHT POWER SUPPLY. 2 L 7 2 4F A6WE 1998090400360 19980904 00360 WP 1998 9 4 MWEA98935 1 19980817 A 5320 5956026 ANGLE DOUG DC9 DC914 3022034 WP BS 360-484 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FORWARD LOWER CARGO PIT STN 360 TO 484 L27L TO 28L FLOOR SUPPORT ANGLE CORRODED. MTC FABRICATED AND INSTALLED NEW SUPPO RT ANGLE. 2 L 7 2 4F A6WE 1998090400361 19980904 00361 WP 1998 9 4 MWEA98936 1 19980817 A 5320 5956026 ANGLE DOUG DC9 DC914 3022034 WP BS 237-360 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FORWARD LOWER CARGO IT STN 237 TO 360 L27L TO 28L FLOOR PANEL SUPPORT ANGLE CORRODED. MTC FABRICATED AND INSTALLED NEW SUPPORT ANGLE. 2 L 7 2 4F A6WE 1998090400362 19980904 00362 WP 1998 9 4 MWEA98938 1 19980817 A 5720 9910009 TEE CAP DOUG DC9 DC914 3022034 WP WS 585 REPLACEMENT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 RIGHT SIDE TEE CAP REPLACEMENT AT STATION XCW 58 5. MTC REMOVED AND REPLACED TEE CAP. 2 L 7 2 4F A6WE 1998090400363 19980904 00363 WP 1998 9 4 MWEA98939 1 19980817 A 5730 591356016 SKIN DOUG DC9 DC914 3022034 WP RT WING CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND RIGHT FLAP INBOARD LEADING EDGE PANEL SKIN CHAFING. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998090400364 19980904 00364 WP 1998 9 4 MWEA98940 1 19980817 A 5312 9911520 BULKHEAD DOUG DC9 DC914 3022034 WP BS 218 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 400ME 45727 FOUND MULTIPLE NON SRM REPAIRS 17 EACH ON FORWARD BULKHEAD STATION 218 LOWER PIT. MTC FABRICATED AND INSTALLED FORWARD BULKHEAD. 2 L 7 2 4F A6WE 1998090400365 19980904 00365 WP 1998 9 4 MWEA98941 1 19980817 A 5754 591356015 SKIN DOUG DC9 DC914 3022034 WP LT LE FLAP CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 LEFT FLAP INBOARD LEADING EDGE EXTERIOR SKIN IS GOUGED AND CHAFED. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998090400366 19980904 00366 WP 1998 9 4 MWEA98942 1 19980826 A 5330 591141063 SKIN DOUG DC9 DC932 3022066 WP BS 218 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 FOUND GOUGES ON FUSELAGE SKIN LEFT SIDE BETWEEN LONGERON 18 LEFT AND 19 LEFT STATION 218. MTC BLENDED DAMAGED AREA, FAB RICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998090400367 19980904 00367 WP 1998 9 4 MWEA98943 1 19980826 A 5330 59114015 SKIN DOUG DC9 DC914 3022034 WP FUSELAGE CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND MODERATE CORROSION ON FUSELAGE SKIN FORWARD OF E AND E DOOR JAMB BETWEEN LONGERONS 29 LEFT AND 30. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998090400368 19980904 00368 NM 1998 9 4 SCNA98713 1 19980807 A 5522 SKIN BOEING 727 7272J4 1384006 NM LT ELEVATOR CRACKED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 288SC 20765 DURING A HEAVY MAINT CHECK, X-RAY INSPECTION OF THE LEFT HAND ELEVATOR REVEALED SEVERAL CRACKS AT THE TRAILING EDGES. C UT OUT CRACKED AREA OF SKIN IAW SRM B727 552003 FIGURE 2. FABRICATED DOUBLERS FROM 2024 T3 .032 PER SRM B727 552003 FIG URE 2. ALODINED AND PRIMED PER SRM 511002 AND MM 512002. INSTALLED REPAIR PER SRM 552003 AND 513002. NO BALANCE REQUI RED AS PER 518007 PAGE 12 FIGURE 2. 2 L 7 3 4F RT A3WE 1998090400369 19980904 00369 NM 1998 9 4 DHL9872101D 1 19980708 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 1 ENG LOWER COWL GEN COOLING EXHAUST DOUBLER HAS CHAFED FLANGE ON COWLING INTERIOR. REPLACED CHAFED FL ANGE PER SRM 51-40-3, 20 X 2.5. N/R 7556. 2 L 7 3 4F A3WE 1998090400370 19980904 00370 NM 1998 9 4 DHL9872102D 1 19980708 A 7110 COWL BOEING 727 727228 NM NR 3 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 3 ENG LOWER COWLING SKIN IS DENTED AT O/B SIDE 10 INCHES BELOW NR 3 HINGE CUTOUT. CUT OUT DAMAGED SECTIO N, INSTALLED REPAIR PER SRM 54-10-3, 6 DOUBLER, FILLER 2. N/R 7508. 2 L 7 3 4F A3WE 1998090400371 19980904 00371 NM 1998 9 4 DHL9872103D 1 19980709 A 7110 COWL BOEING 727 727228 NM NR 2 ENGINE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 2 ENG LEFT HAND AFT COWL FWD PIN RECEPTACLE BENT. CUT OUT DAMAGED SECTION, INSTALLED REPAIR PER SRM 54-1 0-3, 12.5 X 4, SPLICE SECTION 8.5 X 3.5. N/R 5690. 2 L 7 3 4F A3WE 1998090400372 19980904 00372 NM 1998 9 4 DHL9872104D 1 19980709 A 7110 COWL BOEING 727 727228 NM NR 2 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 2 ENG LT AFT COWL NR 7 RIB HOLE CHAFED THROUGH. CUT OUT DAMAGED AREA ON NR 2 ENG LT AFT COWL. INSTALLED REPAIR PER SRM 54-10-3, 4 X 11. N/R 6589. 2 L 7 3 4F A3WE 1998090400373 19980904 00373 NM 1998 9 4 DHL9872105D 1 19980708 A 7110 COWL BOEING 727 727228 NM NR 3 ENGINE GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 3 ENG LOWER COWL INTERIOR RIB NR 10 IS GOUGED. INSTALLED REPAIR PER SRM 54-10-3, 7 X 3. N/R 6529. 2 L 7 3 4F A3WE 1998090400374 19980904 00374 NM 1998 9 4 DHL9872106D 1 19980708 A 7110 COWL STIFFENER BOEING 727 727228 NM NR 3 ENGINE BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 3 ENG LOWER COWL, STIFFENER AT I/B EDGE OF GEN COOLING EXHAUST IS BENT AND GOUGED. REPLACED STIFFENER PE R SRM 54-10-2, 20 X 2.5. N/R 6527. 2 L 7 3 4F A3WE 1998090400375 19980904 00375 NM 1998 9 4 DHL9872107D 1 19980715 A 5210 FRAME BOEING 727 727228 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, MAIN ENTRY DOOR LOWER INNER FRAME HOLES ELONGATED, CRACKED AND CORNERS BENT. REPLACED PLATE PER SRM 51-10- 1, 5 X 33. N/R 5179. 2 L 7 3 4F A3WE 1998090400376 19980904 00376 NM 1998 9 4 DHL9872108D 1 19980714 A 5320 ANGLE BOEING 727 727228 NM BS 804.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, VERT ANGLE HAS A CRACK AT UPPER END BELOW NR 2 SEAT TRACK O/B FLANGE STA 804.5. REMOVED AND REPLACED VERTI CAL ANGLE PER SRM 53-10-1, 8.5 X 2.5 X 1. N/R 5147. 2 L 7 3 4F A3WE 1998090400377 19980904 00377 NM 1998 9 4 DHL9872109D 1 19980714 A 5320 ANGLE BOEING 727 727228 NM BS 825 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, VERT ANGLE HAS CRACKS AT UPPER AND LOWER ENDS BELOW NR 2 SEAT TRACK O/B FLANGE STA 825. REMOVED AND REPLACE D VERT ANGLE PER SRM 51-30-2, 10.5' X 1' X 2.5. N/R 5144. 2 L 7 3 4F A3WE 1998090400378 19980904 00378 NM 1998 9 4 DHL9872110D 1 19980710 A 5320 SUPPORT BOEING 727 727228 NM BS 283 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, FLOOR SUPPORT FASTENERS LOOSE AND REPAIR CRACKED IN COCKPIT FLOOR AT APPROX FS 283 LBL 6. INSTALLED DOUBLE R IN FLOOR SUPPORT 7 X 8 PER SRM 51-10-1. N/R 5075. 2 L 7 3 4F A3WE 1998090400379 19980904 00379 NM 1998 9 4 DHL9872111D 1 19980715 A 5542 SKIN BOEING 727 727228 NM RUDDER DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, UPPER RUDDER, LT TRAILING EDGE HAS IMPACT DAMAGE. INSTALLED REPAIR PER SRM 51-40-2, 6 X 4. N/R 4763. 2 L 7 3 4F A3WE 1998090400380 19980904 00380 NM 1998 9 4 DHL9872112D 1 19980714 A 5315 FLOORBEAM BOEING 727 727228 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 BS 560 FLOORBEAM LBL 10 LIGHT CORROSION. CUT OUT DAMAGED SECTION, INSTALLED UPPER CHORD REPAIR PER SRM 53-10-8, 10.75. N/R 5188. 2 L 7 3 4F A3WE 1998090400381 19980904 00381 NM 1998 9 4 DHL9872113D 1 19980712 A 5720 66147351 BRACKET BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, L/W LOWER TRAILING EDGE PANEL SUPPORT BRACKET CRACKED AT I/B SIDE OF NR 6 SPOILER ACTUTOR CASTING. REPLACED BRACKET PER SRM 51-10-1. N/R 1385. 2 L 7 3 4F A3WE 1998090400382 19980904 00382 NM 1998 9 4 DHL9872114D 1 19980721 A 2780 ANGLE BOEING 727 727228 NM NR 3 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LEFT WING NR 3 L/E SLAT, I/B UPSTOP I/B ATTACH ANGLE CRACKED IN WING L/E. REPLACED UPSTOP ATTACH ANGLE PER SRM 51-40-3, 7 X 4. N/R 1305. 2 L 7 3 4F A3WE 1998090400384 19980904 00384 NM 1998 9 4 DHL9872116D 1 19980710 A 5720 TIP BOEING 727 727228 NM LT WING CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LT WING TIP AFT OUTER FAIRING SECTION FWD CROSS RIB IS CHAFED WITH WORN OFF RIVET HEADS AND SECTION OF RIB MISSING ON AFT SIDE. REMOVED AND REPLACED WEB SECTION PER SRM 51-10-1, 10 X 6. N/R 1290. 2 L 7 3 4F A3WE 1998090400385 19980904 00385 NM 1998 9 4 DHL9872117D 1 19980713 A 5720 ANGLE BOEING 727 727228 NM LT WING TIP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, WING TIP LOWER FWD ATTACH ANGLE CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-3 0-2. N/R 1399. 2 L 7 3 4F A3WE 1998090400386 19980904 00386 NM 1998 9 4 DHL9872118D 1 19980713 A 5720 ANGLE BOEING 727 727228 NM LT WING TIP CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, WING TIP LOWER FWD ATTACH ANGLE CORRODED IN SEVERAL PLACES. REMOVED ATTACH ANGLE AND REPLACED PER SRM 51-3 0-2. N/R 1399. 2 L 7 3 4F A3WE 1998090400387 19980904 00387 NM 1998 9 4 DHL9872119D 1 19980710 A 5713 STRINGER BOEING 727 727228 NM BS 180 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING FIXED L/E INTERIOR LOWER L/E STRINGER IS CORRODED ALONG THE UPPER INSIDE, LOCATED JUST O/B OF SUPPO RT RIB AT FWD END L/E STA 180.9. CUT OUT DAMAGED SECTION, INSTALLED ANGLE REPAIR PER SRM 51-10-3. N/R 2465. 2 L 7 3 4F A3WE 1998090400388 19980904 00388 NM 1998 9 4 DHL9872120D 1 19980710 A 5712 651626418 RIB BOEING 727 727228 NM RT WING CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING FIXED L/E SUPPORT RIB ON THE O/B SIDE AT FWD END IS CORRODED. FABRICATED AND AND INSTALLED ATTACH FITTING PER SRM 51-30-2. CUT OUT RIB SUPPORT AND INSTALLED RIB REPAIR PER SRM 51-40-2, 6 X 4'. N/R 2462. 2 L 7 3 4F A3WE 1998090400389 19980904 00389 NM 1998 9 4 DHL9872121D 1 19980710 A 5720 WEB BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING FIXED L/E INTERIOR VERTICAL WEB AT WBL 92.8 IS CRACKED AT AFT LOWER ATTACH BOLTS. STOP DRILLED END OF CRACK. INSPECT STOP DRILL, INSTALLED WEB REPAIR PER SRM 51-40-2, 3 X 6. N/R 3454. 2 L 7 3 4F A3WE 1998090400390 19980904 00390 NM 1998 9 4 DHL9872122D 1 19980710 A 5754 HEAT SHIELD BOEING 727 727228 NM NR 5 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, 35 L/E FLAP HEAT SHIELD AT THE 3 RD BAY FROM I/B SIDE IS CRACKED AND LOOSE AT LOWER ATTACH RIVETS. REMOVED AND REPLACED PER SRM 51-30-2, 11 X 8. N/R 2467. 2 L 7 3 4F A3WE 1998090400391 19980904 00391 NM 1998 9 4 DHL9872123D 1 19980710 A 5754 HEAT SHIELD BOEING 727 727228 NM NR 5 LE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING FIXED L/E INTERIOR HEAT SHIELD IS DAMAGED ABOVE THE NR 5 L/E FWD FLAP ACTUATOR FITTING. CUT OUT D AMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 57-30-4, 4 X 5'. N/R 2472. 2 L 7 3 4F A3WE 1998090400392 19980904 00392 NM 1998 9 4 DHL9872124D 1 19980710 A 5754 HEAT SHIELD BOEING 727 727228 NM NR 5 LE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 5 L/E FLAP HEAT SHIELD AT 4TH BAY FROM I/B SIDE IS CRACKED. REPLACED HEAT SHIELD PER SRM 51-30-2, 11 X 8. N/R 2466. 2 L 7 3 4F A3WE 1998090400393 19980904 00393 NM 1998 9 4 DHL9872125D 1 19980710 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, CORROSION UNDER NUT PLATES IN AFT BAGGAGE BIN AT FLOOR PANEL ATTACH INTERCOSTAL BETWEEN STA 950A AND 950B LB L 26. REPLACED ANGLE PER SRM 53-10-2, 1 X 1 X 18. N/R 3237. 2 L 7 3 4F A3WE 1998090400394 19980904 00394 NM 1998 9 4 DHL9872126D 1 19980714 A 5313 STRINGER BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, SPOT OF CORROSION AT STRINGER 18L BETWEEN BS 950E AND 950F. CUT OUT DAMAGED SECTION OF STRINGER, INSTALLED REPAIR PER SRM 53-10-3 FROM 950E THROUGH 950F. N/R 3242. 2 L 7 3 4F A3WE 1998090400395 19980904 00395 NM 1998 9 4 DHL9872127D 1 19980714 A 5313 STRINGER BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, SPOT OF CORROSION FROM STA 950D TO 950E AT STR 18L. REMOVED DAMAGED AREA, INSTALLED REPAIR PER SRM 53-10-3, 9 X 2.5. N/R 3249. 2 L 7 3 4F A3WE 1998090400396 19980904 00396 NM 1998 9 4 DHL9872128D 1 19980714 A 5311 FRAME BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, AFT BAGGAGE ATTACH FRAME CRACKED AT BS 950F ABOVE STR 26L. STOP DRILLED FRAME, INSTALLED REPAIR PER SRM 51- 40-2, 6 X 3. N/R 3244. 2 L 7 3 4F A3WE 1998090400397 19980904 00397 NM 1998 9 4 DHL9872129D 1 19980714 A 5320 CLIP BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, AFT BAGGAGE BIN SIDE WALL ATTACH CLIP CRACKED AT BS 950F FRAME ABOVE STR 25L. REPLACED CLIP PER SRM 51-402 , 2 X 1.5. N/R 3245. 2 L 7 3 4F A3WE 1998090400398 19980904 00398 NM 1998 9 4 DHL9872130D 1 19980719 A 5311 FRAME BOEING 727 727228 NM BS 1040 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, CORROSION AT LOWER FUSELAGE FRAME BS 1040 BETWEEN STR 22L AND 23L. REMOVED AND REPLACED FRAME PER SRM 51-30 -2. N/R 3259. 2 L 7 3 4F A3WE 1998090400399 19980904 00399 NM 1998 9 4 DHL9872131D 1 19980714 A 5311 FRAME BOEING 727 727228 NM BS 1050 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, AFT BAGGAGE BIN SIDE WALL TO FLOOR ATTACH FRAME IS CRACKED AT FASTENER HOLE BS 1050 RBL 25. INSTALLED DOUBL ER REPAIR PER SRM 51-40-2, 1 X 17. N/R 3261. 2 L 7 3 4F A3WE 1998090400400 19980904 00400 NM 1998 9 4 DHL9872132D 1 19980714 A 5230 DOOR BOEING 727 727228 NM CARGO DOOR BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, CARGO DOOR EDGE IS BENT FWD LOWER SIDE. CUT OUT DAMAGED AREA, INSTALLED ANGLE REPAIR PER SRM 51-40-3, 5 X 1 .75. N/R 3271. 2 L 7 3 4F A3WE 1998090400401 19980904 00401 NM 1998 9 4 DHL9872133D 1 19980713 A 5320 ANGLE BOEING 727 727228 NM BS 870 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT FORGING STA 870 BEHIND BULKHEAD I/B SIDE OF RIGHT AFT BOTTLE PIN HAS CORROSION ON ITS ATTACHING ANGLE. REMOVED AND REPLACED ATTACH ANGLE PER SRM 57-10-2, 2 LONG. N/R 3279. 2 L 7 3 4F A3WE 1998090400402 19980904 00402 NM 1998 9 4 DHL9872134D 1 19980712 A 5320 PANEL BOEING 727 727228 NM TAIL SKID CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, TAIL SKID OPENING AFT INTERNAL PANEL CRACKED AT LT TOP. REPLACED PANEL PER SRM 51-40-2, 9 X 10. N/R 3164. 2 L 7 3 4F A3WE 1998090400403 19980904 00403 NM 1998 9 4 DHL9872135D 1 19980711 A 5220 SKIN BOEING 727 727228 NM EMER EXIT DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT FWD EMERGENCY EXIT DOOR AFT TE SURFACE SKIN DAMAGED. ROUTED OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 52-20-2, 4 X 8. N/R 3076. 2 L 7 3 4F A3WE 1998090400404 19980904 00404 NM 1998 9 4 DHL9872136D 1 19980711 A 5324 SIDE WALL BOEING 727 727228 NM BS 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LOWER FWD CARGO FLOOR TO SIDE WALL PANEL CRACKED AT BS 600 STR 26L. REMOVED SIDE WALL PANEL PER 25-52-2. I NSTALLED SIDE WALL AT BS 600 PER SRM 51-40-2, 6 X 48. N/R 3125. 2 L 7 3 4F A3WE 1998090400405 19980904 00405 NM 1998 9 4 DHL9872137D 1 19980711 A 5320 ANGLE BOEING 727 727228 NM BS 717 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, CORROSION ON FLOOR SUPPORT ANGLE BS 717 LBL 10 LOWER FWD CARGO COMPT. FABRICATED AND INSTALLED PANEL PER S RM PER SRM 51-10-1, 2' X 1'. N/R 3120. 2 L 7 3 4F A3WE 1998090400406 19980904 00406 NM 1998 9 4 DHL9872138D 1 19980711 A 5324 PANEL BOEING 727 727228 NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LOWER FWD CARGO COMPT RT FLOOR TO SIDE WALL PANEL CRACKED BS 720 STR 26. INSTALLED PANEL PER SRM 51-10-1, 2' X 1'. N/R 3130. 2 L 7 3 4F A3WE 1998090400407 19980904 00407 NM 1998 9 4 DHL9872139D 1 19980712 A 5320 WEB BOEING 727 727228 NM BS 1323 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, AFT AIRSTAIRS AREA HORIZ WEB FOR TORQUE BOX LT AFT OF BS 1323 WEB UNDER ACCESS PLATE CRACKED. STOP DRILL CR ACK, HFEC, INSTALLED WEB REPAIR PER SRM 51-40-2, 4' X 2.25. N/R 3145. 2 L 7 3 4F A3WE 1998090400408 19980904 00408 NM 1998 9 4 DHL9872140D 1 19980712 A 5720 STIFFENER BOEING 727 727228 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LT WING ROOT ACCESS THRU PANEL 6302 VERTICAL STIFFENER BETWEEN FWD WING BOTTLE PIN CASTING AND ANIT-ICING D UCT SECTION CRACK. STOP DRILLED CRACK, INSTALLED DOUBLER 7 X 3 PER SRM 51-40-3. N/R 3147. 2 L 7 3 4F A3WE 1998090400409 19980904 00409 NM 1998 9 4 DHL9872141D 1 19980712 A 5330 SKIN BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, TAIL SKID OPENING AFT INTERNAL PANEL CRACKED AT LT TOP. REPLACED PANEL PER SRM 51-40-2, 9 X 10. N/R 3164. 2 L 7 3 4F A3WE 1998090400410 19980904 00410 NM 1998 9 4 DHL9872142D 1 19980713 A 5320 SUPPORT BOEING 727 727228 NM BS 420-440 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, 2 FLOOR SUPPORT CHANNELS IN E & E COMPT, BETWEEN STA 440 AND 420 CRACKED. CUT OUT DAMAGED AREA AND INSTALLE D ANGLE REPAIR AT STA 420 PER SRM 51-40-3, 4 X 1' X 1'. REPLACED FLOOR SUPPORT CHANNEL AT STA 440 PER SRM 51-30-2, 16 L ONG. N/R 3170. 2 L 7 3 4F A3WE 1998090400411 19980904 00411 NM 1998 9 4 DHL9872143D 1 19980714 A 5320 CLIP BOEING 727 727228 NM BS 700 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 700 STR TIE CLIP IS CRACKED. REMOVED AND INSTALLED NEW TIE CLIP PER SRM 53-10-2, 3 X 4. N/R 3209. 2 L 7 3 4F A3WE 1998090400412 19980904 00412 NM 1998 9 4 DHL9872144D 1 19980714 A 5320 CLIP BOEING 727 727228 NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 720A STR 7R TIE CLIP IS CRACKED. REMOVED AND INSTALLED TIE CLIP PER SRM 53-10-2, 3 X 4. N/R 3210. 2 L 7 3 4F A3WE 1998090400413 19980904 00413 NM 1998 9 4 DHL9872145D 1 19980714 A 5311 FRAME BOEING 727 727228 NM BS 560 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 560 FRAME, INNER FLANGE BETWEEN RT 5R AND 6R DENTED. CUT OUT DAMAGED AREA AND INSTALLED REPAIR PER SRM 53-10-4, 10 X 4.5. N/R 3215. 2 L 7 3 4F A3WE 1998090400414 19980904 00414 NM 1998 9 4 DHL9872146D 1 19980714 A 5320 CLIPS BOEING 727 727228 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 480 STR 6L AND 5L TIE CLIPS TO RIB ARE BENT AND CRACKED. REMOVED AND REPLACED TIE CLIPS PER SRM 51-10- 2. N/R 3221. 2 L 7 3 4F A3WE 1998090400415 19980904 00415 NM 1998 9 4 DHL9872147D 1 19980710 A 5330 SKIN BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, TWO RIVET HEADS SHEARED OFF AND SKIN BULGED AT HORIZONTAL LAP JOINT STRINGER 20L STA 950E. REMOVED CORROSIO N, CUT OUT DAMAGED AREA AT STA 950E. CUT OUT OUTER LAP SKIN, INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 11 X 6. N/R 30 53. 2 L 7 3 4F A3WE 1998090400416 19980904 00416 NM 1998 9 4 DHL9872148D 1 19980710 A 5753 SKIN BOEING 727 727228 NM RT TE FOREFLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING O/B FOREFLAP ATTACHING POINT 53 FROM I/B EDGE CRACKED AND RIVETS LOOSE. FABRICATED DOUBLER PER SRM 57-40-4, 3.75 X 3.5. N/R 2546. 2 L 7 3 4F A3WE 1998090400417 19980904 00417 NM 1998 9 4 DHL9872149D 1 19980712 A 5720 STIFFENER BOEING 727 727228 NM WS 621 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING REAR SPAR VERT STIFFENER CRACKED WS 621. REMOVED VERTICAL STIFFENER, FABRICATED NEW STIFFENER PER SRM 57-10-2, 12 X 2 X 2. N/R 2557. 2 L 7 3 4F A3WE 1998090400418 19980904 00418 NM 1998 9 4 DHL9872150D 1 19980707 A 5320 ANGLE BOEING 727 727228 NM FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, TAIL SKID COMPT, VERTICAL ANGLE HAS CORROSION AT UPPER AND LOWER END. REPLACED ANGLE 7 X 1.5 PER SRM 52-10 -1. N/R 3050. 2 L 7 3 4F A3WE 1998090400419 19980904 00419 NM 1998 9 4 DHL9872151D 1 19980709 A 5320 6747464 FITTING BOEING 727 727228 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LEFT SIDE STA 1183 DOOR FRAME NR 7 STOP FITTING CRACKED. REMOVED AND REPLACED STOP FITTING PER SRM 51-30-2. N/R 3051. 2 L 7 3 4F A3WE 1998090400420 19980904 00420 NM 1998 9 4 DHL9872152D 1 19980710 A 5720 652165830 BRACKET BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RIGHT WING BELOW NR 12 SPOILER PANEL COVE SUPPORT BRACKET CRACKED WS 505. REMOVED AND REPLACED BRACKET PER SRM 51-10-1. N/R 2509. 2 L 7 3 4F A3WE 1998090400421 19980904 00421 NM 1998 9 4 DHL9872153D 1 19980710 A 5720 HEAT SHIELD BOEING 727 727228 NM RT WING DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RIGHT WING FIXED L/E INTERIOR HEAT SHIELD IS DAMAGED AT FWD END. CUT OUT DAMAGED AREA, INSTALLED DOUBLER RE PAIR PER SRM 57-30-4, 3.5 X 4.5. N/R 2464. 2 L 7 3 4F A3WE 1998090400422 19980904 00422 NM 1998 9 4 DHL9872154D 1 19980714 A 5311 FRAME BOEING 727 727228 NM BS 520 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 520 FRAME INNER FLANGE BETWEEN STR 17R AND 16R HAS DENTS. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA , INSTALLED FRAME REPAIR PER SRM 53-10-4, 16 X 5 X 1. N/R 3220. 2 L 7 3 4F A3WE 1998090400423 19980904 00423 NM 1998 9 4 DHL9872155D 1 19980713 A 5753 SKIN BOEING 727 727228 NM LT TE AFT FLAP DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LEFT I/B AFT FLAP HAS A DENT ON UPPER SURFACE. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-50-4, 7 X 4.5. N/R 1414. 2 L 7 3 4F A3WE 1998090400424 19980904 00424 NM 1998 9 4 DHL9872156D 1 19980710 A 5712 RIB BOEING 727 727228 NM LT WING TIP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LT WING TIP OUTER RIB CENTER VERTICAL SUPPORT BRACKET HAS CHAFED AREA OF FWD SIDE, SMALL BULB SEAL DETERIORA TED TOP FLANGE OF BRACKET IS CRACKED WITH ONE NUT PLATE BROKEN OFF. REPLACED VERTICAL SUPPORT BRACKET AT LT WING TIP OU TER RIB PER SRM 51-30-2. N/R 1281. 2 L 7 3 4F A3WE 1998090400425 19980904 00425 NM 1998 9 4 DHL9872157D 1 19980714 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 950 BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, AFT BAGGAGE FLOOR INTERCOSTAL WEB BENT AND VERTICAL STIFFENER CRACKED AT BL-0 BETWEEN STA 950F AND 970. IN STALLED NEW VERTICAL STIFFENER PER SRM 51-40-3, 12 X 12 X 12. INSTALLED WEB REPAIR PER SRM 51-30-2. N/R 3241. 2 L 7 3 4F A3WE 1998090400426 19980904 00426 NM 1998 9 4 DHL9872158D 1 19980714 A 5311 FRAME BOEING 727 727228 NM BS 660 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 660 FRAME INNER FLANGE BETWEEN STR 17R AND 16R HAS DENTS. CUT OUT DAMAGED AREA, INSTALLED FRAME REPAIR PER SRM 53-10-4, 16 X 5 X 1. N/R 3219. 2 L 7 3 4F A3WE 1998090400427 19980904 00427 NM 1998 9 4 DHL9872159D 1 19980707 A 2710 6524440018 CASTING BOEING 727 727228 NM RT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING O/B AILERON GEARBOX SUPPORT CRACKED ON UPPER SIDE. REMOVED AND REPLACED CASTING PER SRM 51-10-1. N /R 2410. 2 L 7 3 4F A3WE 1998090400428 19980904 00428 NM 1998 9 4 DHL9872160D 1 19980714 A 5311 FRAME BOEING 727 727228 NM BS 600 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 600 FRAME INNER FLANGE BETWEEN STR 5R AND 6R DENTED. CUT OUT DAMAGED AREA, INSTALLED FRAME REPAIR PER S RM 53-10-4, 8 X 3' X 1. N/R 3218. 2 L 7 3 4F A3WE 1998090400429 19980904 00429 NM 1998 9 4 DHL9872161D 1 19980713 A 5720 ANGLE BOEING 727 727228 NM WS 294 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING UPPER SURFACE BULGED AT REAR SPAR UPPER CHORD ANGLE WS 294. REMOVED UPPER CHORD RIGHT WING FROM ST A 70.5 TO 348 AND REPLACED PER AVITAS EO 98PMSI233RO-Z. N/R 2564. 2 L 7 3 4F A3WE 1998090400430 19980904 00430 NM 1998 9 4 DHL9872162D 1 19980714 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 1010-1030 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, CORROSION PRESENT AT INTERCOSTAL BETWEEN BS 1010 AND 1030 STRINGER 27R. REMOVED AND REPLACED INTERCOSTAL PE R SRM 53-10-1, 20 X 10. N/R 3254. 2 L 7 3 4F A3WE 1998090400431 19980904 00431 NM 1998 9 4 DHL9872163D 1 19980709 A 5320 65577665 FITTING BOEING 727 727228 NM SERVICE DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LEFT AFT SERVICE DOOR CUTOUT FWD STOP FITTING FROM THE BOTTOM CRACKED. REMOVED AND REPLACED FITTING PER SRM 53-10-1. N/R 3041. 2 L 7 3 4F A3WE 1998090400432 19980904 00432 NM 1998 9 4 DHL9872164D 1 19980709 A 5754 SKIN BOEING 727 727228 NM NR 6 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 6 LE SLAT ABOVE ANTI-ICE DUCT ANGLE CRACKED I/B END. STOP DRILL, HFEC, FABRICATED DOUBLER PER SRM 57-50- 3, 7 X 6. N/R 2423. 2 L 7 3 4F A3WE 1998090400433 19980904 00433 NM 1998 9 4 DHL9872165D 1 19980711 A 3230 65244805 FITTING BOEING 727 727228 NM LT MLG CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LEFT MLG UPLOCK SUPPORT FITTING CRACKED AT AFT MOUNT LUG. REMOVED AND REPLACED FITTING PER SRM 51-14-1. N/ R 7591. 2 L 7 3 4F A3WE 1998090400434 19980904 00434 NM 1998 9 4 DHL9872166D 1 19980713 A 5521 RIB BOEING 727 727228 NM LT ELEVATOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, X-RAY INSP SHOWS INTERNAL LOWER RIB CRACKED, DAMAGE TO THE LT ELEVATOR SKIN SEEN THROUGHT ACCESS PANEL 9309 . REMOVED AND REPLACED ELEVATOR SKIN PANEL PER SRM 51-30-2. REBALANCED ELEVATOR PER SRM 51-80-7. INSTALLED ELEVATOR A ND RIGGED PER MM 27-30-1. N/R 4746. 2 L 7 3 4F A3WE 1998090400435 19980904 00435 NM 1998 9 4 DHL9872167D 1 19980713 A 5311 FRAME BOEING 727 727228 NM LAVATORY CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, CORROSION AT RIGHT FORWARD LAVATORY FLOOR FRAME AREA JUST BELOW AFT LAV WALL. REPLACED HAT CHANNEL PER SRM 51-40-4. N/R 5132. 2 L 7 3 4F A3WE 1998090400436 19980904 00436 NM 1998 9 4 DHL9872168D 1 19980808 A 7110 66144652 BRACKET BOEING 727 727228 NM NR 3 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 3 ENGINE FWD FIXED COWL UPPER FWD SUPPORT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM 51-10- 1. N/R 6713. 2 L 7 3 4F A3WE 1998090400437 19980904 00437 NM 1998 9 4 DHL9872169D 1 19980714 A 5400 S-DUCT BOEING 727 727228 NM NR 2 ENGINE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 2 ENGINE INLET DUCT AFT END HAS PULLED RIVETS AND SKIN CRACKED. CUT OUT DAMAGED AREA AT 12 O'CLOCK AFT E ND. CUT OUT DAMAGED SECTION OF INTERNAL STRAP AT TOP OF AFT END, 12 INCHES LONG. FABRICATED AND INSTALLED FILLER AND D OUBLER 7 X 4 PER SRM 54-10-3. INSTALLED FABRICATED STRAP PER SRM 54-10-3, 12 X 2. N/R 6658/6710. 2 L 7 3 4F A3WE 1998090400438 19980904 00438 NM 1998 9 4 DHL9872170D 1 19980710 A 5712 RIB BOEING 727 727228 NM LT WING TIP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, LT WING TIP OUTER RIB HAS CRACK EXTENDING OUT FROM OVAL ACCESS PANEL OPENING, LOWER AFT CORNER. ACCOMPLISH ED HFEC, INSTALLED DOUBLER REPAIR PER SRM 51-40-3, 4 X 10 X 1. N/R 1283. 2 L 7 3 4F A3WE 1998090400439 19980904 00439 NM 1998 9 4 DHL9872171D 1 19980709 A 2710 196057004 BRACKET BOEING 727 727228 NM RT AILERON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT I/B AILERON TURN AROUND PULLEY SUPPORT BRACKET ASSY HAS CORROSION PITTING AROUND PULLEY PIVOT BOLT HOLE L OWER SIDE AND LOWER O/B BOLT. REMOVED AND REPLACED BRACKET PER MM 27-10-1. N/R 2418. 2 L 7 3 4F A3WE 1998090400440 19980904 00440 NM 1998 9 4 DHL9872172D 1 19980710 A 5330 SKIN BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING UPPER SURFACE CUTOUT FOR THE NR 11 SPOILER O/B HINGE IS CRACKED. STOP DRILLED CRACK, REMOVED RT WIN G SKIN PLATE AT SPOILER CUTOUT PER SRM. INSTALLED NEW PLATE FROM WS 438 TO 530 PER SRM 57-30-4, 91 X 4. N/R 2525. 2 L 7 3 4F A3WE 1998090400441 19980904 00441 NM 1998 9 4 DHL9872173D 1 19980710 A 5753 LINK BOEING 727 727228 NM RT TE FOREFLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RT WING LOWER FOREFLAP CENTER ATTACHING LINK LOWER SURFACE GOUGED AND CORRODED. CUT OUT DAMAGED AREA, INSTA LLED DOUBLER REPAIR PER SRM 57-50-4, 5 X 5. N/R 2547. 2 L 7 3 4F A3WE 1998090400442 19980904 00442 NM 1998 9 4 DHL9872174D 1 19980806 A 2760 53621441 PULLEY BOEING 727 727228 NM WS 253 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, PULLEY FOUND CRACKED FOR SPOILER AT WS 253 RT WING. REMOVED AND REPLACED PULLEY PER MM 20-20-4. N/R 2664. 2 L 7 3 4F A3WE 1998090400443 19980904 00443 NM 1998 9 4 DHL9872175D 1 19980713 A 5753 SKIN BOEING 727 727228 NM RT TE AFT FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, RIGHT O/B AFT FLAP L/E LOWER SURFACE HAS CRACK ON SKIN AT FITTING, 2 FT FROM I/B END. HFEC CONFIRM CRACK C ONTAINMENT. INSTALLED DOUBLER REPAIR PER SRM 57-50-4, 6.25 X 4.5. N/R 2565. 2 L 7 3 4F A3WE 1998090400444 19980904 00444 NM 1998 9 4 DHL9872176D 1 19980710 A 5330 SKIN BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, B-SYSTEM HYD COMPARTMENT, DOUBLER REPAIR JUST BELOW B-SYS MODULE NEEDS TO BE CHECKED. REMOVED DOUBLER REPAI R. FOUND CRACKED ATTACH ANGLE SUPPORT AT STA 950C. CUT OUT DAMAGED SECTION OF VERTICAL ANGLE AND INSTALLED DOUBLER REP AIR PER SRM 51-40-2, 4 X 3. FABRICATED DOUBLER REPAIR AND FILLER FOR SKIN REPAIR 16 X 12 FILLER, DOUBLER 22 X 18 PER S RM 51-10-2. N/R 3073. 2 L 7 3 4F A3WE 1998090400445 19980904 00445 NM 1998 9 4 DHL9872177D 1 19980715 A 5315 FLOORBEAM BOEING 727 727228 NM BS 560 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, STA 560 FLOORBEAM TOP CHORD AFT FLANGE LOWER FURFACE LBL 23 HAS CORROSION. CUT OUT DAMAGED AREA, INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8, 2 FT LONG. N/R 3348. 2 L 7 3 4F A3WE 1998090400446 19980904 00446 1998 9 4 DHL98873001 4 19980826 A 2210 2588787904 COMPUTER DOUG DC8 DC873F 302199F WP E/E COMPT FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 873SJ 46091 YAW DAMPER EXECUTED HARD OVER LEFT AFTER LEAVING 25,000 FT. RESET BY TURNING YAW DAMPER OFF, ANOTHER HARD OVER OCCURRED AT 30,000 FT. REMOVED AND REPLACED YAW CHANNEL COMPUTER. PERFORMED OPS CHECK PER MM 27-21-5. 2 L 7 4 4F RT 4A25 1998090400447 19980904 00447 WP 1998 9 4 DHL98873002 1 19980828 A 2913 3051157040 SEAL DOUG DC8 DC873F 302199F WP NR 4 ENGINE WORN A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 873SJ 46091 NR 4 ENGINE OIL QUANTITY INDICATION GOING TO ZERO, SHUT DOWN ENGINE AS PRECAUTIONARY. REPLACED HYDRAULIC PUMP PAD SEAL PER MM CHAP 29. 2 L 7 4 4F RT 4A25 1998090400448 19980904 00448 NE 1998 9 4 TC8A98053 2 19980822 A 7532 560339 BLEED VALVE DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE REPLACED A TC8A A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 802CK 301 45679 642841 MULTIPLE COMPRESSOR STALLS ON CLIMBOUT, 6,000 FT ON NR 1 ENG. REMOVED AND REPLACED NR 1 PRBC VALVE, OPS CHECKS OK IAW 7 5-30-3. 2 L 7 4 4F 4 F 4A25 1E8 1998090400449 19980904 00449 1998 9 4 TC8A98054 4 19980829 A 3420 2588533901 AMPLIFIER DOUG DC8 DC862F 3021972 WP CABIN REPLACED A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 187SK 674 46022 AFTER TAXI OUT, F/O'S HEADING FLAG ON COMPASS BECAME DISPLAYED. REMOVED AND REPLACED INSTRUMENT AMPLIFIER RACK NR 2. O PS CHECK NORMAL PER MM 34-21-0. 2 L 7 4 4F 4A25 1998090400450 19980904 00450 SW 1998 9 4 98ZZZX3154 1 19980810 A 5610 407706301107 WINDOW BELL 407 407 SW LT SLIDER DEPARTED A A HEEA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SW 03 437PH 53072 WHILE IN-FLIGHT, LT SLIDING WINDOW DEPARTED AIRCRAFT. AIRCRAFT CONTINUED TO LAND BASE. AFTER LANDING, A 'NICK' WAS DIS COVERED ON THE INBOARD TRAILING EDGE OF ONE T/R BLADE. REMOVED BLADE ASSEMBLY FOR REPAIR. REF: IPC, (407) FIGURE 152-8 , ITEM 11. 1 G 7 1 3U O H2SW 1998090400669 19980904 00669 SW 1998 9 4 HEEA0015787 1 19980826 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DETERIORATED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 402PH 53159 MAIN ROTOR GEARBOX RUBBER MOUNTS DETERIORATED. 1 G 7 1 3U O H2SW 1998090400733 19980904 00733 1998 9 4 HEEA0015880 4 19980827 A 3197 75028515 INDICATOR BELL 206 206L1 1182107 SW CAUTION PANEL SHORTED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50182 45242 INDICATOR FOR ENG. OUT SEGMENT AND ROTOR LOW RPM SEGMENT. 1 G 7 1 3U H2SW 1998090400804 19980904 00804 EU 1998 9 4 UF6A980502 1 19980506 A 5320 JD539J0199001 ANGLE BAG ATP ATP EU CARGO DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 13884 2021 SBN - FORWARD BAGGAGE DOOR LANDING ANGLE IS DAMAGED ON FORWARD AND AFT SHOOT BOLT PLATES. MAINTENANCE REPAIRED DAMAGE I AW TOR 001634. (M) 2 L 7 2 4T RT A27NM 1998090400805 19980904 00805 EU 1998 9 4 UF6A980509 1 19980515 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 2020 ORD - EMERGENCY LIGHTS INOP AT ROWS 9 AND 10. MAINTENANCE REMOVED AND REPLACED NR 6 EMERGENCY BATTERY PACK. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998090400806 19980904 00806 EU 1998 9 4 UF6A980505 1 19980510 A 3350 GE1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 855AW 2029 SBN - RIGHT AFT EXTERIOR OVEWING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998090400807 19980904 00807 EU 1998 9 4 UF6A980504 1 19980508 A 3350 GE1317 BULB BAG ATP ATP EU CARGO BAY FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 SBN - RIGHT AFT BAGGAGE DOOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998090400808 19980904 00808 NM 1998 9 4 TAOA079806 1 19980710 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 20415 FLT 6790 - DCA-LGA - RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL PER MM 33-50. (M) 2 L 7 3 4F A3WE 1998090400809 19980904 00809 NM 1998 9 4 TAOA079807 1 19980710 A 3350 90052 CHARGER UNIT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 20415 FLT 6790 - DCA-LGA - RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. REPLACED BATTERY BASE CHARGER UNIT, OPERATIONAL CH ECK NORMAL PER MM 33-50. (M) 2 L 7 3 4F A3WE 1998090400810 19980904 00810 NM 1998 9 4 TAOA079805 1 19980710 A 2150 32176431 VALVE BOEING 727 727254 138408L NM RT PACK MALFUNCTION A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 914TS 20251 FLT 6420 - DCA-LGA - RIGHT PACK OVERHEATED ON TAXI OUT WITH RIGHT PACK SWITCH IN OFF POSITION. REPLACED RIGHT PACK SHUT OFF VALVE. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998090400811 19980904 00811 NE 1998 9 4 SIMA981824 2 19980701 A 7210 RGB AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 1 ENGINE DAMAGED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 SW 21 260AE 263 127100 HRL - FLT 3724 - AFTER TAKEOFF FROM HRL THE FLT CREW SELECTED 'CLIMB' ON THE POWER MANAGEMENT PANEL AND BEGAN TO BRING T HE CONDITION LEVERS BACK TO ACHIEVE 86 PERCENT NP WHEN THE NR 1 ENGINE BEGAN TO SURGE AND THEN THE TQ WENT TO ZERO. THE NP STABILIZED AT 30 PERCENT AND THE NH AT 45 PERCENT. THE ENGINE WAS SHUT DOWN AS A PRECAUTION MEASURE. A/C RETURNED TO HRL SAFELY. CFR WAS CALLED AND FOLLOWED THE AIRCRAFT TO THE GATE. PAX DEPLANED NORMALLY. MX INSPECTED ENG AND FOUN D EVIDENCE OF DAMGE TO RGB COMPONENTS. PERFORMED SYSTEM AND ENGINE CHANGE CHECKS SATISFACTORILY. A/C WAS RETURNED TO S ERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998090400812 19980904 00812 NM 1998 9 4 98ZZZM592 1 19980705 A 3350 20131A BATTERY PACK BOEING 727 72789 1384028 NM CABIN DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 511DB 19139 NUMEROUS EMERGENCY EXI TAND FLOOR LEVEL LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT BATTERY PACKS AT STATIONS 460 AN D 1140. (M) 2 L 7 3 4F A3WE 1998090400813 19980904 00813 1998 9 4 98ZZZM593 4 19980619 A 2564 5WD230600203 SLIDE DOUG DC10 DC1010 3022110 WP PAX DOOR FAILED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 572SC DD204 46977 DURING FAA MINI EVACUATION DEMONSTRATION, THE R3 DOOR SLIDE/RAFT FAILED TO DEPLOY FULLY. THE RAFT PORTION OF THIS TWO P ART ASSEMBLY IS THE ONLY PART TO FAIL. THE SLIDE PORTION PERFORMED ITS INTENDED FUNCTION. (M) 2 L 7 3 4F A22WE 1998090400814 19980904 00814 NM 1998 9 4 P2EA98126 1 19980702 A 5330 SKIN BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD J2C-50-5325C, A CRACK WAS FOUND ON THE SKIN AT BS 727B PLUS 2. THE CRACK WAS 1.5 INCH IN LENGTH. DUE TO OTHER REPAIRS IN THE AREA, IT WAS DETERMINED BY BOEING TO REPLACED THE SKIN S ECTION FROM BS 727 TO BS 757 BETWEEN STRINGER 14L TO 20L. DETAILS OF REPLACEMENT CAN BE FOUND ON COOPSEA EO NR COO-3-53 -351-98. (M) 2 L 7 2 4F A16WE 1998090400815 19980904 00815 NM 1998 9 4 P2EA98124 1 19980701 A 5712 RIB BOEING 737 737222 1384473 NM RT WING CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK, WHILE REMOVING RT WING INBOARD MID-FLAP TO FACILITATE OTHER MAINTENANCE OBSERVED TWO RIBS CRACKED AT WBL 87.7. NEWS RIBS FABRICATED BY COOPESA MACHINE SHOP AS PER COOPESA EO NR C00-3-57-330-98. INSTALLED IAW SRM 51-1 0-1 PAGE 5 AND 51-30-2. (M) 2 L 7 2 4F A16WE 1998090400816 19980904 00816 NM 1998 9 4 P2EA98123 1 19980630 A 5720 ANGLE BOEING 737 737222 1384473 NM BS 575-615 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-50-5325C, A CRACK WAS NOTED ON AN ANGLE LOCATED ON THE W ING CENTER SECTION AT LBL 52.5. THE CRACK WAS 1.5 INCH IN LENGTH. REPAIRED ANGLE AT WING CENTER SECTION BETWEEN BS 575 AND 615, LBL 52, IAW SRM 51-40-30, FIG 1. RIVETS REPLACED IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998090400817 19980904 00817 NM 1998 9 4 P2EA98122 1 19980629 A 5712 RIB BOEING 737 737222 1384473 NM WS 83 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-10-5726C, A CRACK WAS FOUND ON A RIB OF THE RT WING, INB OARD MID-FLAP. THE CRACK WAS LOCATED AT WBL 83 AND WAS 1 INCH IN LENGTH. THE RIB WAS REPLACED IAW SRM 51-10-1 PAGE 6. RIVETS REPLACED IAW SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998090400818 19980904 00818 NM 1998 9 4 P2EA98121 1 19980701 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK, WHILE PERFORMING SKIN REPLACEMENT AT BS 727, A CRACK WAS FOUND ON STRINGER 19L. REPAIRED CRACK IA W SRM 53-10-3 FIG 2. (M) 2 L 7 2 4F A16WE 1998090400819 19980904 00819 NM 1998 9 4 P2EA98120 1 19980629 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 520-540 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD J2C-51-2125, CORROSION WAS FOUND ON STRINGER 28 LEFT BETWEEN BS 520 AND BS 540. THE CORROSION WAS OUT OF LIMITS AS PER SRM, (MORE THAN 10 PERCENT REMOVED). REPAIRED AS PER COOPESA E O NR C00-3-53-328-98. APPROVED AND SUBMITTED BY FAA DER. (M) 2 L 7 2 4F A16WE 1998090400820 19980904 00820 NM 1998 9 4 P2EA98119 1 19980628 A 5230 BEAM BOEING 737 737222 1384473 NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION, A CRACK WAS FOUND ON THE NR 5 BEAM OF THE FORWARD CARGO COMPARTMENT DOOR, FORWA RD SECTION LENGTH 1.5 INCH. REPAIRED CRACK AS PER BOEING S/B 737-52-1100. (M) 2 L 7 2 4F A16WE 1998090400821 19980904 00821 NM 1998 9 4 P2EA98118 1 19980621 A 5711 SPAR BOEING 737 737222 1384473 NM WS 525 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION WHILE PERFORMING WORK CARD NR J2C-10-5726C. A CRACK WAS FOUND ON THE VERTICAL A NGLE ON THE FRONT WING SPAR AT FSS 525. THE LENGTH WAS .187 INCH. ANGLE WAS REPLACED AS PER SRM 51-10-1, PAGE 5. FABR ICATED ANGLE IAW SRM 51-20-1, 51-10-1, HEAT TREATED IAW BAC 5602 AND SRM 51-10-3. CORROSION PROTECTION APPLIED AS PER S RM 51-10-2 MATERIAL USED, 7075 T6, .125 INCH. (M) 2 L 7 2 4F A16WE 1998090400822 19980904 00822 NM 1998 9 4 P2EA98117 1 19980621 A 5312 BULKHEAD BEAM BOEING 737 737222 1384473 NM AFT PRESS BLKHD CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-51-2525, A CRACK WAS NOTED ON THE FORWARD CARGO COMPT, A FT PRESSURE BULKHEAD, VERTICAL BEAM, RBL 15, WL 167.5 (FRONT SPAR, WING CENTER SECTION). REPLACED BEAM AS PER SRM 51-1 0-1, PAGE 5. (M) 2 L 7 2 4F A16WE 1998090400823 19980904 00823 NM 1998 9 4 P2EA98113 1 19980611 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 480 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD J2C-51-2525, A CRACK WAS FOUND AT BS 480 BETWEEN STRINGER NR 26 AND NR 27 RT. THE CRACK WAS REPAIRED AS PER SRM 53-10-4. (M) 2 L 7 2 4F A16WE 1998090400824 19980904 00824 NM 1998 9 4 P2EA98112 1 19980611 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 493-514 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING C-CHECK ROUTIN EINSPECTION AS PER WORK CARD J2C-51-2525, A CRACK WAS FOUND ON STRINGER NR 23 RT, BETWEEN BS 493 AND BS 514. THE CRACK WAS .25 INCH LONG. THE CRACK WAS REPAIRED AS PER SRM 53-10-03. (M) 2 L 7 2 4F A16WE 1998090400825 19980904 00825 NM 1998 9 4 PCAA9800775 1 19980623 A 3230 DSC252B40124 HOSE DHAV DHC8 DHC8102 2809003 NM NLG WW FAILED A PCAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 13 816EX 329 DURING CLIMB-OUT FROM MDT, UPON GEAR RETRACTIO NLEFT MAIN GEAR UNSAFE, NOSE, AND RIGHT MAIN DOOR LIGHTS REMAINED ILLUMIN ATED. GEAR RETRACTED FULLY AFTER APPROXIMATELY 1 MINUTE. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAIN TENANCE TROUBLESHOT AND FOUND A HYDRAULIC LINE LEAK IN NOSE GEAR WELL. REMOVED AND REPLACED THE HYDRAULIC LINE TO DRAG STAY ACTUATOR AND O-RING IAW DHC PROCEDURES. RETRACTION TEST SATISFACTORY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998090400826 19980904 00826 NM 1998 9 4 PCAA9800774 1 19980601 A 3260 864202 SWITCH DHAV DHC8 DHC8102 2809003 NM NLG WW FAILED A PCAA K NONE N FALSE WARNING CR CRUISE 1 EA 13 813AW 247 DURING CRUISE FLIGHT, NOSE GEAR LIGHT AND GEAR HANDLE LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE NOSE GEAR DRAG BRACE PROXIMITY SWITCH AT FAULT. THE SWITCH WAS REPLACED IAW DHC PROCE DURES AND RETRACTION TEST WAS SATISFACTORY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998090400827 19980904 00827 CE 1998 9 4 98ZZZM594 1 19980706 A 7714 1303800445 GAUGE BEECH 1900 1900D 1154162 CE COCKPIT FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 859CA 2377 496 UE128 RT N GAUGE INOPERATIVE. N1 GAUGE FAILURE. REPLACED N1 GAUGE. (M) 2 L 7 2 4T RT A24CE 1998090400828 19980904 00828 1998 9 4 98ZZZM595 4 19980708 A 6122 311849601 GOVERNOR BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 857CA UE71 RIGHT ENGINE SURGING IN TORQUE. RIGHT PROPELLER GOVERNOR FAILURE. REPLACED RT PROPELLER GOVERNOR. (M) 2 L 7 2 4T RT A24CE 1998090400829 19980904 00829 WP 1998 9 4 HALA9800218 1 19980406 A 5320 SPLICE DOUG DC9 DC951 3022051 WP BS 598-579 CORRODED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 601AP 47658 HNL - MODERATE/HEAVY CORROSION, ON LONGERON 30 SPLICE BETWEEN STATION 598 AND 579. REPLACED SPLICE PER HAL 105, FILE NR 59125. (M) 2 L 7 2 4F RT A6WE 1998090400830 19980904 00830 WP 1998 9 4 HALA9800205 1 19980707 A 7711 TUBE DOUG DC9 DC951 3022051 WP NR 2 ENGINE CRACKED A HALA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 13 603DC 47784 HNL - FLT 110 - NR 2 ENGINE COULD NOT MAKE TAKEOFF POWER. RIGHT ENGINE EPR LOW WITH TAKEOFF POWER APPLIED, APPROX 1.7 E PR AND 95 PERCENT N1. ALL OTHER ENGINE PARAMETERS NORMAL. FOUND TUBE ASSY FOR PT7 OUTER INTERNAL HOSE BROKEN. REPLACE D DURING CLOSE UP OF SHROUD COVER. FOUND BROKEN BOLT. (M) 2 L 7 2 4F RT A6WE 1998090400831 19980904 00831 WP 1998 9 4 GTIA9800079 1 19980701 A 2560 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 947ML 47514 MAIN CABIN DOOR ESCAPE SLIDE FELL OUT DUE TO JET BLAST. REINSTALLED ESCAPE SLIDE AS REQUIRED. NO DEFECTS NOTED AT THIS TIME IAW DC9 MM 25-61-0. ALL ACCOMPLISHED. (M) 2 L 7 2 4F A6WE 1998090400832 19980904 00832 WP 1998 9 4 GTIA9800078 1 19980705 A 2560 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR LOOSE A GTIA K NONE O OTHER AP APPROACH 1 GL 23 132NK 47202 ATL - FLT 810 - GALLEY DOOR SLIDE PACK DISLODGED ARRIVAL ATL FLT 810 ACY-ATL. RESECURED SLIDE IAW 25-60. RII ACCOMPLIS HED. (M) 2 L 7 2 4F A6WE 1998090400833 19980904 00833 NM 1998 9 4 F3LA98139 1 19980713 A 5320 STRAP BOEING 737 737301 1384611 NM BS 847 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON STRAP UNDER UPPER ANGLE OF FRAME AT BS 847, RBL 14-30. MAINTENA NCE REMOVED AND REPLACED STRAP PER SRM 51-40-2 AND 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998090400834 19980904 00834 NM 1998 9 4 F3LA98135 1 19980713 A 3222 CYLINDER BOEING 737 737301 1384611 NM NLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED NOSE LANDING GEAR OUTER CYLINDER THREADS ARE CORRODED AND HAVE SHARP EDGES. M AINTENANCE REPAIRED PER SRM 32-21-58, OHM 20-50-3 AND OHM 20-42-10. (M) 2 L 7 2 4F RT A16WE 1998090400835 19980904 00835 NM 1998 9 4 F3LA98136 1 19980713 A 5320 WEB BOEING 737 737301 1384611 NM BS 294 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CRACK AND CORROSION ON WEB AROUND FASTENER AT BS 294.5, WL 208, LBL 56. MAINT ENANCE REMOVED DAMAGED WEB, FABRICATED REPLACEMENT PART AND REPAIRED PER SRM 51-30-01 AND 51-40. (M) 2 L 7 2 4F RT A16WE 1998090400836 19980904 00836 NM 1998 9 4 F3LA98137 1 19980713 A 5343 FITTING BOEING 737 737301 1384611 NM RT MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK INSPECTION, REPORTED CORROSION ON RT MAIN LANDING GEAR STABILIZER BEAM AFT FITTING. MAINTENANCE BL ENDED CORROSION. REMOVED AND REPLACED BEAM AND AFT FITTING PER OHM 57-41-01 AND MM 32-13-21. (M) 2 L 7 2 4F RT A16WE 1998090400837 19980904 00837 NM 1998 9 4 F3LA98138 1 19980713 A 5320 FRAME BOEING 737 737301 1384611 NM CARGO DOORWAY CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON AFT CARGO DOOR FRAME, BS 794.5, RBL 24. MAINTENANCE REMOVED CORR OSION (4.5 INCH BY 39 INCH) AND REMOVED AND REPLACED FRAME FROM STRINGER 16R TO 27R PER SRM 53-60-15, SRM 51-40-2, SB 73 7-53-1096, AND DRAWING 65C35243. (M) 2 L 7 2 4F RT A16WE 1998090400838 19980904 00838 NM 1998 9 4 F3LA98140 1 19980713 A 5343 BEAM BOEING 737 737301 1384611 NM LT MLG CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON LT MAIN LANDING GEAR BEAM LOWER SURFACE AND DAMAGED PANEL MOUNT H OLE OUTBOARD OF STABILIZER LINK MOUNT POINT. MAINTENANCE REMOVED CORROSION, FABRICATED REPLACMENT PARTS AND REPAIRED PE R SRM 51-20-10 AND ERO 98-0597. (M) 2 L 7 2 4F RT A16WE 1998090400839 19980904 00839 NM 1998 9 4 98ZZZM596 1 19980701 A 2611 302313 SMOKE DETECTOR DHAV DHC8 DHC8103 1386005 NM CARGO BAY CONTAMINATED A ERAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 881EA 233 CARGO COMPARTMENT SMOKE DETECTOR WARNING AFTER TAKEOFF, FOR APPROX 3 MINUTES. MADE UNEVENTFUL PRECAUTIONARY LANDING AT ENG. CAUTION LIGHT WENT OUT PRIOR TO LANDING. CLEANED SMOKE DETECTOR ELECTRICAL CONNECTORS AND REPLACED FWD SMOKE DETE CTOR. GROUND OPERATIONAL CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998090400840 19980904 00840 NM 1998 9 4 EIAA980227 1 19980713 A 2612 FIRE LOOP BOEING 747 747273C 1384896 NM NR 1 ENGINE MALFUNCTIONED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 CTS - AFTER TAKEOFF NR 1 ENGINE A LOOP OFF-SCALE WITH FAULT LIGHT ILLUMINATED. SWITCHED TO B LOOP, TESTED NORMAL. THEN IN CRUISE B LOOP INDICATED FAULT. PERFORMED IN FLIGHT SHUTDOWN. OIL PRESSURE NOT BELOW 10 PSI. REPAIRED B LOOP UPPER ELEMENT CONNECTOR, OPS CHECKED GOOD PER MM 26-11-0. REPLACED A-13 CARD DUE TO PRECAUTIONARY MEASURE. PERFORMED WINDMI LL INSPECTION PER MM 72-00-00, NO DEFECTS NOTED. (M) 2 L 7 4 4F A20WE 1998090400841 19980904 00841 WP 1998 9 4 EIAA980224 1 19980702 A 5711 SPAR CHORD DOUG DC9 DC932F 3022067 WP WS 156 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK, LEFT WING 11 ELONGATED HOLES AT XRS 156.75 ON THE LOWER AFT SPAR CHORD. REPAIRED PER ECRA 932-57- 037-2. (M) 2 L 7 2 4F A6WE 1998090400842 19980904 00842 WP 1998 9 4 EIAA980225 1 19980702 A 5711 SPAR CHORD DOUG DC9 DC932F 3022067 WP WS 156 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47355 MZJ - DURING C-CHECK, RIGHT WING 1 ELONGATED HOLE AT XRS 156.75 ON THE LOWER AFT SPAR CHORD. REPAIRED PER ECRA 932-57-0 38-2. (M) 2 L 7 2 4F A6WE 1998090400843 19980904 00843 NM 1998 9 4 98ZZZM597 1 19980702 A 3211 FITTING BOEING 747 747273C 1384896 NM RT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 20653 HKG - DURING B-CHECK, LEFT AND RIGHT BODY LANDING GEAR TRUNNION SUPPORT FITTINGS, CORROSION WAS FOUND IN THE BOLT HOLES AND BEARING SURFACES. THE LEFT INBOARD AND OUTBOARD LOWER TRUNNION CAPS ALSO HAVE CORROSION. REPAIRED TRUNNION FITTING S PER BOEING TELEX PAO-HKG-98-0102RE/0103RE/0105RE APPROVED ON 8110-3 DATED JUN 26, 1998. (M) 2 L 7 4 4F A20WE 1998090400844 19980904 00844 1998 9 4 EISA98166 4 19980707 A 3422 172652A DIRECTIONAL GYRO BOEING 727 72731 1384010 NM COCKPIT INOPERATIVE A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 240NE 18906 NR 2 HSI AND NR 1 COMPASS (RMI) INOPERATIVE, AIR TURN BACK TO BRADLEY. INSTALLED SERVICEABLE NR 2 DIRECTIONAL GYRO. OP S CHECK SATISFACTORY. (M) 2 L 7 3 4F A3WE 1998090400845 19980904 00845 NM 1998 9 4 EISA98168 1 19980630 A 7930 42D107A2 SWITCH BOEING 727 727231 1384079 NM NR 3 ENGINE INOPERATIVE A EISA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 74318 D18N 20051 NR 3 OIL FILTER BYPASS LIGHT CAME ON WHEN TAKEOFF POWER WAS SET. EXTINGUISHED AFTER CLEARING RUNWAY. GENERATED FROM PI LOT REPORT. REMOVED AND REPLACED NR 3 ENGINE OIL FILTER BYPAS SWITH IAW MM CHAPTER 79. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998090400846 19980904 00846 NM 1998 9 4 EISA98165 1 19980628 A 5543 SKIN BOEING 727 727223 1384074 NM RUDDER TAB DELAMINTATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND LOWER RUDDER TAB DELAMINATED AT TRAILING EDGE LOWER CORNER. R EPAIRED DELAMINATION PER SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998090400847 19980904 00847 NM 1998 9 4 EISA98164 1 19980628 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF CPCP CARD C53-224-05, FOUND CRACK IN FUSELAGE FRAME AT FS 500 WL 214. REMOVED DAMAGED AREA. F ABRICATED REPAIR PER SRM 51-40-3 AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998090400848 19980904 00848 NM 1998 9 4 EISA98163 1 19980628 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF CPCP CARD C53-224-05, FOUND CRACK IN FUSELAGE FRAME AT FS 520 WL 214. REMOVED DAMAGED AREA. F ABRICATED REPAIR PER SRM 51-40-3 AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998090400849 19980904 00849 NM 1998 9 4 EISA98162 1 19980628 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 848-870 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CORROSION ON RIGHT OUTBOARD SEAT TRACK AT FS 848-870. REMOVED CORRODED TRACK AND INSTALLED NEW TRACK FROM FS 848.95 TO FS 870. (M) 2 L 7 3 4F A3WE 1998090400850 19980904 00850 NM 1998 9 4 EISA98161 1 19980628 A 5320 FITTING BOEING 727 727223 1384074 NM LT MLG CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING REPLACEMENT OF LEFT MAIN LANDING GEAR, FOUND FORWARD TRUNNION BEARING ATTACH FITTING CRACKED AT LOWER INBOARD BUS HING HOLE. REMOVED DAMAGED FITTING. INSTALLED NEW FITTING PER SRM 51-10-1 AND 51-30-1. (M) 2 L 7 3 4F A3WE 1998090400851 19980904 00851 NM 1998 9 4 EISA98160 1 19980628 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND STRINGER 24L CRACKED JUST FORWARD OF FS 950A. REMOVED DAMAGED AREA. FABRICATED REPAIR PER SRM 53-10-3 AND INSTALLED PER SRM 53-10-03. (M) 2 L 7 3 4F A3WE 1998090400852 19980904 00852 NM 1998 9 4 EISA98159 1 19980628 A 5230 BRACKET BOEING 727 727223 1384074 NM CARGO DOOR CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 315NE 20190 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FORWARD CARGO DOOR LOWER AFT CORNER, ANGLE BRACKET EXFOLIATED. REMOVED BRACKET. FABRICATED AND INSTALLED NEW BRACKET PER SRM 53-10-02. (M) 2 L 7 3 4F A3WE 1998090400853 19980904 00853 EU 1998 9 4 SABA290035 1 19980715 A 5270 SENSOR BAG JETSTM JETSTM3201 1500217 EU PAX DOOR MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 33 957AE 957 GSP - FLT 5156 - ON FLIGHT FROM AVL TO RDU, THE MAIN ENTRY DOOR LIGHT CAME ON. THE AIRCREW DIVERTED TO THE NEAREST AIRP ORT WHICH WAS GSP. AIRCRAFT LANDED AT GSP WITH NO OTHER PROBLEMS. AIRCREW CONTACTED MAINTENANCE IN CHARLOTTE. THEY WE RE TOLD TO TRY RESETTING THE CIRCUIT BREAKER. LIGHT IN COCKPIT WOLD NOT GO OUT. THE CREW WAS ALSO DIRECTED TO CHECK TH E DOOR LOCK ALIGNMENT MARKINGS. DOOR WAS OPENED AND CLOSED SEVERAL TIMES. ALL LOCK INDICATORS WERE GOOD. DISCREPANCY WAS DEFERRED TO MSL 071598-01C. (M) 2 L 7 2 4T RT A56EU 1998090400854 19980904 00854 NM 1998 9 4 TWRA9837 1 19980712 A 3610 CLAMP BOEING 747 7472F6B 1384807 NM NR 1 NACELLE LOOSE A TWRA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 15 623FF 22382 FLT 92 - SJU-MIA - ON CLIMB, NR 1 ENGINE FIRE SWITCH ILLUMINATED AND FIRE BELLSOUNDED. ENGINE SHUT DOWN. WHEN START LE VER WAS CUT OFF THE FIRE SWITCH LIGHT STOPPED ILLUMINATION. NACELLE TEMP DROPPED. FIRE BOTTLE WAS NOT DISCHARGED. AIR TURN BACK TO SJU. FOUND DUCT CLAMP CONNECTING 14TH STAGE MANIFOLD OFF, SECURED CLAMP. INSPECTION ENGINE INLET AND EXH AUST AREA. ENGINE REVERSER COWLING AND ASSOCIATED WIRING. NO DAMAGE FOUND. INSPECTED OIL SCREEN, FOUND OK ACCOMPLISHE D HI POWER RUN. OPS AND LEAK CHECK OK PER MM 71-00-00. (M) 2 L 7 4 4F A20WE 1998090400855 19980904 00855 NM 1998 9 4 TWRA9838 1 19980629 A 5220 DOOR SEAL BOEING 747 747121 1384871 NM EMERG DOOR LOOSE A TWRA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 617FF 19650 FLT 513 - OXT- CAI, AIR TURN BACK TO OXT, DUE UNABLE TO PRESSURIZE AIRCRAFT, COCKPIT HATCH DOOR DOES NOT SEAL PROPERLY. FOUND DOOR SEAL OUT OF GROOVE, REINSTALLED DOOR SEAL, OPS AND PRESSURIZATION CHECK OK PER MM 52-20. (M) 2 L 7 4 4F A20WE 1998090400856 19980904 00856 NM 1998 9 4 TWRA9839 1 19980719 A 3610 CLAMP BOEING 747 7472F6B 1384807 NM NR 1 NACELLE LOOSE A TWRA K NONE N FALSE WARNING CL CLIMB 1 EA 15 623FF 22382 NR 1 ENGINE FIRE WARNING MOMENTARILY INDICATED ON CLIMB-OUT FROM TLV, RETARDED THRUST LEVER TO IDLE BEFORE ANY ACTION TA KEN. LIGHT/HORN EXTINGUISHED, OTHER INDICATIONS NORMAL. 'A' LOOP DROPPED TO NORMAL. 'B' LOOP CONTINUED TO RUN ABOVE ' A' LOOP. FOUND PNEUMATIC LEAK AT HIGH STAGE VALVE CLAMP. RESET AND TIGHTENED CLAMPS. PERFORMED RUN UP AND LEAK CHECK PER MM 71-00-00, TESTS 1, 3 AND 4. NO LEAKS NOTED. OPS CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1998090400857 19980904 00857 CE 1998 9 4 98ZZZM598 1 19980730 A 5610 10138402522 WINDSHIELD BEECH 1900 1900D 1154162 CE COCKPIT CRACKED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 845CA 96118H6687 UE47 RIGHT WINDSHIELD CRACKED IN OUTER PANE. SUSPECT STRESS OVERLAP. REPLACED RT WINDSHIELD. 2 L 7 2 4T RT A24CE 1998090400858 19980904 00858 1998 9 4 98ZZZM599 4 19980730 A 6122 311849601 GOVERNOR BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 862CA 6201 2457416 UE180 A/C YAWS LEFT ON LANDING AT IDLE POWER. PROP GOVERNOR FAILURE. REPLACED PROP GOVERNOR. (M) 2 L 7 2 4T RT A24CE 1998090400859 19980904 00859 NM 1998 9 4 USAASB98195 1 19980722 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 575US 23740 ROC - MAINTENANCE FOUND ALL THE EMERGENCY LIGHTS CONTROLLED BY POWER SUPPLY M1132 FAIL AFTER 10-15 SECONDS OF OPERATION. ALSO FOUND THE AISLE BULLNOSE EMERGENCY LIGHT AT STATION 590L INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN POWER SUPPLY M1132 AND RELAMPED THE AISLE BULLNOSE LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998090400860 19980904 00860 NM 1998 9 4 USAASB98196 1 19980724 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 337US 23235 IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE AFT RIGHT SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED T HE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998090400861 19980904 00861 NM 1998 9 4 USAA980333 1 19980731 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 32 INCH CORRODED AREA AROUND FLOORBOARD SCREW HOLES IN 'T' C AP FLOORBEAM STATION 344 RBL 10 TO LBL 22. CORROSION TASK NR C53-107-02. INSTALLED NEW 'T'CAP PER T/R 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998090400862 19980904 00862 NM 1998 9 4 USAA980332 1 19980731 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 380 BETWEEN STRINGER 8 LT AND STRINGER 9 LEFT ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 BAC ADVISORY 737258. (M) 2 L 7 2 4F RT A16WE 1998090400863 19980904 00863 NM 1998 9 4 USAA980331 1 19980731 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 400 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 400 BETWEEN STRINGER 8 LT AND STRINGER LT ON FR AME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M) 2 L 7 2 4F RT A16WE 1998090400864 19980904 00864 NM 1998 9 4 USAA980330 1 19980731 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 440 BETWEEN STRINGER 8 LT AND STRINGER 9 LT ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M) 2 L 7 2 4F RT A16WE 1998090400865 19980904 00865 NM 1998 9 4 USAA980329 1 19980731 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STATION 827, STRINGER 8 RIGHT, STRINGER 9 RIGHT ON FRA ME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M) 2 L 7 2 4F RT A16WE 1998090400866 19980904 00866 NM 1998 9 4 USAA980328 1 19980731 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867 BETWEEN STRINGER 8 RT AND STRINGER 9 RT FRAM E. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M) 2 L 7 2 4F RT A16WE 1998090400867 19980904 00867 NM 1998 9 4 USAA980327 1 19980731 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 867 BETWEEN STRINGER 8 LEFT AND STRINGER 9 LEFT FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. BAC ADVISORY 737258. (M) 2 L 7 2 4F RT A16WE 1998090400868 19980904 00868 NM 1998 9 4 USAA980326 1 19980731 A 5311 65465323 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .12 5INCH CRACK STATION 480 BETWEEN 5-8 RIGHT AND 5-9 RIGHT BODY FRAME. INSTALLED DOUBLER PER SRM 53-00-07 FIG 202 AND BAC ADVISORY 737258. (M) 2 L 7 2 4F RT A16WE 1998090400869 19980904 00869 NM 1998 9 4 USAA980266 1 19980522 A 5315 146N509012 FLOORBEAM BOEING 757 757225 1384959 NM BS 1661 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 607AU 41850 22203 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM AT CLIP NUT HOLES STATION 1661 FROM BL 0 TO RBBL 55. CORROSION CARD NR C53-251-03. INSTALLED REPAIR 'T' CAP AND STRAPS. PARTIAL 'T' CAP REPLACED FROM LBL 25 TO LBL 64 ALSO INSTALLED REPLACEMENT CHORD/REPAIR ANGLES PER SRM 53-00-51 FIG 201. (M) 2 L 7 2 4F RT A2NM 1998090400870 19980904 00870 NM 1998 9 4 USAABB98083 1 19980804 A 2133 566918 VALVE BOEING 757 757225 1384959 NM E/E BAY FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 603AU 22198 LAX - FLT 41 - EN ROUTE CLT-LAX, CREW RECEIVED THE EICAS MESSAGE 'CABIN ALTITUDE' AND ASSOCITED LIGHTS. FLIGHT DESCENDE D TO FL 280 AND USED MANUAL MODE TO MAINTAIN 8000 FEET CABIN ALTITUDE. FLIGHT CONTINUED TO LAX AND LANDED WITH NO FURTH ER INCIDENT. MAINTENANCE IN LAX REPLACED THE CABIN PRESSURE SELECTOR PANEL. SUBSWQUENTLY, IN PHL, THE OUTFLOW VALVE WA S REPLACED FOR LEAKING AND OVERBOARD EQUIPMENT COOLING VALVE WAS REPLACED FOR BEING STUCK IN THE OPEN POSITION. (M) 2 L 7 2 4F RT A2NM 1998090400871 19980904 00871 NM 1998 9 4 USAABB98082 1 19980804 A 2133 60683218 OUTFLOW VALVE BOEING 757 757225 1384959 NM FUSELAGE FAILED A USAA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 603AU 22198 CLT - FLT 1190 - EN ROUTE MCO-PHL, AIRCRAFT LOST PRESSURIZATION IN AUTO MODE, AND EICAS MESSAGE 'CABIN ALTITUDE' ILLUMIN ATED. AIRCRAFT DESCENDED TO 10,000 FT, AND PRESSURIZATION CONTROL WAS REGAINED USING MANUAL MODE. FLIGHT DIVERTED TO C LT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE OUTFLOW VALVE. (M) 2 L 7 2 4F RT A2NM 1998090400872 19980904 00872 NE 1998 9 4 USAAD98137 2 19980805 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT NACELLE FAILED A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 EA 19 824US 49143 696369 BUF - FLT 433 - AFTER TAKEOFF THE RIGHT ENGINE EXPERIENCED TWO COMPRESSOR STALLS, THE EGT INCREASED AND THE ENGINE WAS U NRESPONSIVE TO THROTTLE MOVEMENT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THERE WAS NO RESPONS E TO REVERSE THRUST FROM THE RIGHT ENGINE. MAINTENANCE REPLACED THE RIGHT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998090400873 19980904 00873 NE 1998 9 4 USAABB98084 2 19980808 A 7230 BLADES BOEING 767 7672B7 1385107 NM GE CF6 CF680C2B2 30025 NE RT ENGINE DAMAGED A USAA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 EA 19 653US 24894 695144 PHL - FLT 42 - AT TAKEOFF FROM PHL, CAPTAIN SAW A BIRD PASS BENEATH THE AIRCRAFT. AS THE GEAR RETRACTED, THE CREW NOTED A STRANGE NOISE FROM THE RIGHT ENGINE. ALL INDICATIONS WERE NORMAL, BUT THE NOISE CONTINUED. FLIGHT RETURNED TO PHL A ND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE BORESCOPE INSPEED THE RIGHT ENGINE AND FOUND DAMAGE ON THE 1ST, 11TH, 1 2TH, 13TH AND 14TH STAGE COMPRESSOR BLADES. THE ENGINE WAS REPLACED. (M) 2 L 7 2 4F 4 F RT A1NM E13NE 1998090400874 19980904 00874 EU 1998 9 4 USAAF98066 1 19980802 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 897US 11392 GSO - FORWARD EMERGENCY LIGHTS WEAK. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1998090400875 19980904 00875 EU 1998 9 4 USAAF98067 1 19980811 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 856US 11286 IND - FORWARD ENTRY DOOR EXIT SIGN INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1998090400876 19980904 00876 EU 1998 9 4 USAAF98064 1 19980726 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 893US 11373 GSO - FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK. (M) 2 L 7 2 4F RT 1998090400877 19980904 00877 EU 1998 9 4 98ZZZM600 1 19980726 A 3350 6040681 POWER SUPPLY FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 893US 11373 GSO - FORWARD ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK. (M) 2 L 7 2 4F RT 1998090400878 19980904 00878 WP 1998 9 4 USAAD98129 1 19980730 A 5270 SENSOR DOUG DC9 DC981 3022081 WP CARGO DOOR OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 806US 48038 PIT - FLT 2032 - AFTER TAKEOFF, THE FORWARD CARGO DOOR CAUTION LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AN D LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR WARNING SENSOR TARGET SLIGHTLY OUT OF POSITION. TH E TARGET WAS STRAIGHTENED AND THE PROXIMITY UNIT CHECKED, ALL WAS NORMAL. (M) 2 L 7 2 4F A6WE 1998090400879 19980904 00879 WP 1998 9 4 USAA980334 1 19980730 A 5311 CC1192874 FRAME DOUG DC9 DC931 3022065 WP BS 1104 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 960VJ 47505 PIT - DURING C-4 CHECK, FOUND 6 1 INCH CRACKS IN FRAME AT STATION 1104 CANTED, FRAME AT STRINGERS 3L AND 3R, 4L AND 4R A ND 5L AND 5R. REPLACED 1104 FRAME ASSY PER MFG DWG. (M) 2 L 7 2 4F A6WE 1998090400880 19980904 00880 WP 1998 9 4 USAAD98132 1 19980803 A 3231 NAS13047D BOLT DOUG DC9 DC931 3022065 WP LT MLG WW FAILED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 920VJ 48140 BOS - FLT 409 - DURING LANDING, THE FLIGHT CREW EXECUTED A GO-AROUND AFTER THE LANDING GEAR DOOR OPEN LIGHT ILLUMINATED. THE AIRCRAFT THEN LANDED AND STOPPED ON THE RUNWAY UNTIL MAINTENANCE PINNED THE LANDING GEAR AND DOORS. THE AIRCRAFT THEN TAXIED TO THE TERMINAL. MAINTENANCE REPLACED THE BOLT AND NUT FOR THE LEFT MAIN GEAR FOLLOW-UP SYSTEM DRIVE FOR TH E TORQUE TUBE TO DOR UPLATCH. THE MAIN GEAR DOOR SKIDS WERE REPLACED AND AN EXTENSION AND RETRACTION AND FREE FALL CHEC K OF ALL GEARS WAS PERFORMED. (M) 2 L 7 2 4F A6WE 1998090400881 19980904 00881 WP 1998 9 4 USAAD98130 1 19980731 A 2910 836SD620 FUSE DOUG DC9 DC982 3022082 WP LT MLG WW BROKEN A USAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 EA 19 829US 49429 TPA - FLT 1622 - DURING CRUISE, THE LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED WITH THE QTY INDICATING 4 QTS. THE AI RCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE LANDING WEIGHT WAS 132,000 LBS. MAINTENANCE REPLACED THE UPPER HYDRAULIC FUSE IN THE LEFT WHEEL WELL AND PERFORMED AND OVERWEIGHT LANDING INSPECTION. (M) 2 L 7 2 4F A6WE 1998090400882 19980904 00882 WP 1998 9 4 USAAD98133 1 19980805 A 3231 DOOR DOUG DC9 DC981 3022081 WP NLG OPEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 807US 48039 BOS - FLT 1924 - AIRCRAFT EXPERIENCED HEAVY VIBRATION FROM NOSE WHEEL AREA AFTER GEAR RETRACTION. MAINTENANCE FOUND THE RIGHT NOSE GEAR DOOR OPEN. THE DOOR WAS SECURED CLOSED AND THE AIRCRAFT DISPATCHED. (M) 2 L 7 2 4F A6WE 1998090400883 19980904 00883 WP 1998 9 4 USAAD98134 1 19980805 A 2170 WATER SEPARATOR DOUG DC9 DC931 3022065 WP AC BAY CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 926VJ 48146 IND - FLT 1242 - AFTER TAKEOFF A STRONG FUEL SMELL WAS EVIDENT IN BOTH THE CABIN AND COCKPIT. THE FLIGHT RETURNED TO TH E FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RAN BOTH ENGINES AND THE APU, NO OIL OR FUEL LEAKS WERE NOTED. THE TAIL COMPARTMENT, WHEEL WELLS AND FUSELAGE BELLY WERE CHECK FOR FLUID LEAKS, NONE FOUND. THE SHROUD DRAINS WERE ALSO INSPECTED. THE AIR CONDITIONING WATER SEPARATOR BAGS WERE REPLACED AND THE APU AND ENGINES RUN WITH THE PACKS ON. NO SMELL NOTED AT ANY POWER SETTING. (M) 2 L 7 2 4F A6WE 1998090400884 19980904 00884 WP 1998 9 4 USAAD98136 1 19980805 A 2130 94840213 AMPLIFIER DOUG DC9 DC931 3022065 WP E/E BAY FAILED A USAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 19 955VJ 47593 PIT - FLT 1132 - DURING CRUISE AT 33,000 FEET THE CABIN ALTITUDE WARNING ACTIVATED. THE FLIGHT CREW INITIATED AN EMERGE NCY DESCENT AND GAINED CONTROL OF THE CABIN PRESSURE USING THE MANUAL CONTROL SYSTEM. THE CABIN OXYGEN MASKS DID NOT DE PLOY. MAINTENANCE REPLACED THE CABIN PRESSURE AMPLIFIER. (M) 2 L 7 2 4F A6WE 1998090400885 19980904 00885 NM 1998 9 4 USAA980335 1 19980730 A 5320 65465784 WEB BOEING 737 737301 1384611 NM BS 1088/BS1121 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 32422 23553 CLT - DURING DROP IN CHECK VISUAL AND EDDY CURRENT, FOUND A 40 INCH SQUARE HEAT DAMAGED AREA APU TORQUE BOX UPPER WEB BS 1088 - BS 1121 LBL 40 RBL 40 WEB CENTER. INSTALLED NEW FLOOR WEB SECTION PER SRM 53-80-13. (X) 2 L 7 2 4F RT A16WE 1998090400886 19980904 00886 NM 1998 9 4 TSAA9833440 1 19980805 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 1 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4F RT A16WE 1998090400887 19980904 00887 NM 1998 9 4 TSAA9833441 1 19980729 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 5 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400888 19980904 00888 NM 1998 9 4 TSAA9833442 1 19980729 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 6 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400889 19980904 00889 NM 1998 9 4 TSAA9833443 1 19980730 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LED'S BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1998090400890 19980904 00890 NM 1998 9 4 TSAA9833444 1 19980730 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LED'S BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1998090400891 19980904 00891 NM 1998 9 4 TSAA9833445 1 19980730 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY PACK AT NR 1 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F A16WE 1998090400892 19980904 00892 NM 1998 9 4 TSAA9833446 1 19980730 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY PACK AT NR 2 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F A16WE 1998090400893 19980904 00893 NM 1998 9 4 TSAA9833447 1 19980730 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400894 19980904 00894 NM 1998 9 4 TSAA9833448 1 19980730 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING NOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1998090400895 19980904 00895 NM 1998 9 4 TSAA9833449 1 19980730 A 3350 6013211 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED LEFT SIDE AFT EXTERIOR SLIDE EMERGENCY BATTERY PACK DUE TO BATTERY BEING DEAD. OPS CHECKED OK. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998090400896 19980904 00896 NM 1998 9 4 TSAA9833450 1 19980731 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998090400897 19980904 00897 NM 1998 9 4 TSAA9833453 1 19980813 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998090400898 19980904 00898 NM 1998 9 4 TSAA9833454 1 19980813 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998090400899 19980904 00899 NM 1998 9 4 TSAA9833455 1 19980813 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998090400900 19980904 00900 NM 1998 9 4 TSAA9833439 1 19980705 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED BATTERY PACK AT NR 5 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400901 19980904 00901 NM 1998 9 4 TSAA9833406 1 19980718 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 2 FLOOR PROX LIGHT ASSY SHOWS NO BATTERY LED'S ON TEST. REPLACED BATTERY, TESTED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400902 19980904 00902 NM 1998 9 4 TSAA9833407 1 19980718 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 AND NR 5 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400903 19980904 00903 NM 1998 9 4 TSAA9833408 1 19980718 A 3350 873100151 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . (M) 2 L 7 2 4F RT A16WE 1998090400904 19980904 00904 NM 1998 9 4 TSAA9833409 1 19980719 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED AFT ENTRY DOOR EMERGENCY ID LIGHT ASSY BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400905 19980904 00905 NM 1998 9 4 TSAA9833410 1 19980718 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 4 AND NR 6 EXIT FLOOR LIGHT BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400906 19980904 00906 NM 1998 9 4 TSAA9833411 1 19980719 A 3350 8731002511 LIGHT BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED AFT ENTRY DOOR EMERGENCY ID LIGHT ASSY S/N 2436, ON 2540. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400907 19980904 00907 NM 1998 9 4 TSAA9833412 1 19980718 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 5 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998090400908 19980904 00908 NM 1998 9 4 TWRA9841 1 19980804 A 3350 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 AFT GALLEY EGRESS LIGHT INOP. REPLACED DAMAGED SECTION OF LIGHT STRIP. OPS CHECK OK MM 33-51-00. (M) 2 L 7 4 4F A20WE 1998090400909 19980904 00909 NM 1998 9 4 TAOA089802 1 19980809 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 927TS 20837 FLT 6070 - BOS-LGA - FOUND ON LS, LEFT FORWARD EXTERIOR OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OP ERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998090400910 19980904 00910 EU 1998 9 4 SIMA982181 1 19980806 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBO ARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400911 19980904 00911 EU 1998 9 4 98ZZZM601 1 19980806 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBO ARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400912 19980904 00912 EU 1998 9 4 98ZZZM602 1 19980806 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBO ARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400913 19980904 00913 EU 1998 9 4 98ZZZM603 1 19980806 A 5347 S53575001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBO ARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400914 19980904 00914 EU 1998 9 4 98ZZZM604 1 19980806 A 5347 S53575001214 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBO ARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400915 19980904 00915 EU 1998 9 4 98ZZZM605 1 19980806 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLIGHT ATTENDANT, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT FORWARD OUTBO ARD AND RIGHT MIDDLE SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400916 19980904 00916 EU 1998 9 4 SIMA982221 1 19980809 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 DFW - FLT 5324 - EMERGENCY LIGHT AT SEAT 11A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4T RT A52EU 1998090400917 19980904 00917 EU 1998 9 4 SIMA9822212 1 19980809 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 329AE 340B329 FLT 5055 - CREW FOUND EMERGENCY LIGHT SWITCH WAS LEFT IN THE ARM POSITION, ALL AIRCRAFT EMERGENCY LIGHTS DO NOT ILLUMINA TE. REMOVED AND REPLACED ALL EMERGENCY LIGHT POWER SUPPLY'S . OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998090400918 19980904 00918 EU 1998 9 4 SIMA982131 1 19980801 A 5315 S5367240620801 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAM 36 CORRODED. REMOVED AND REPLACED FLOORBEAM 36. AIRCRAFT RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400919 19980904 00919 NM 1998 9 4 AALA981440 1 19980728 A 5311 FRAME BOEING 727 727227 1384078 NM BS 990 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - BELL FRAME BENT AT STATION 990 BETWEEN STRINGER 25L-26L. INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998090400920 19980904 00920 NM 1998 9 4 AALA981439 1 19980728 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1030 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - DENT AT STATION 1030 STRINGER 25-26R. INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998090400921 19980904 00921 NM 1998 9 4 AALA981451 1 19980728 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FRAME 1130 DAMAGED AT STRINGER 27R. STOP DRILLED DAMAGEA AREA AND INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998090400922 19980904 00922 NM 1998 9 4 AALA981450 1 19980728 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FRAME 1110 DAMAGED AT STRINGER 27L. STOP DRILLED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998090400923 19980904 00923 NM 1998 9 4 AALA981449 1 19980728 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - BELL FRAME BENT STATION 990 STRIGNER 26L MARKED (WEB BULGED). CUT OUT DAMAGE AND INSTALLED 'Z' ANGLE DOUBLER REPA IR PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998090400924 19980904 00924 NM 1998 9 4 AALA981448 1 19980728 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1090 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - BELL FRAME DENTED WEB BULGED STATION 1090 STRINGER 26L MARKED. CUT OUT DAMAGED ARE OF BELL FRAME. INSTALLED 'Z' ANGLE DOUBLER REPAIR PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998090400925 19980904 00925 NM 1998 9 4 AALA981447 1 19980728 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - RIGHT WING UPPER SKIN PANEL BULGING ARUOND FASTENERS JUST FORWARD OF APU EXHAUST CUT OUT 6 INCH AREA. REMOVED AND REPLACED WING SKIN PANEL WITH 8130 PANEL. (M) 2 L 7 3 4F A3WE 1998090400926 19980904 00926 NM 1998 9 4 AALA981446 1 19980728 A 5320 CASTING BOEING 727 727223 1384074 NM BS 304 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FOUND CORROSION ON TOP OF UPPER HINGE CASE FRAME ON FWD ENTRY DOOR CUT OUT. REMOVED AND REPLACED UPPER HINGE CAST ING PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998090400927 19980904 00927 NM 1998 9 4 AALA981444 1 19980728 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-1010 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FOUND CORROSION IN STRINGER CHANNEL, STATION 950B TO 1010, STRINGER 27L. REMOVED STRINGER 27 FROM 950B TO 1010. I NSTALLED NEW STRINGER AND STRINGER CLIPS. (M) 2 L 7 3 4F A3WE 1998090400928 19980904 00928 NM 1998 9 4 AALA981443 1 19980728 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - FOUND CORROSION ON FLOORBEAM AT STATION 340 RBL 22 TO 24, RBL 13 TO 15, TOP AND BOTTOM SIDE OF TOP FLANGE RBL 14 T O 20, LBL 22. FLOORBEAM REPAIR COMPLETED AS PER SRM 53-10-8 PAGE49-52. (M) 2 L 7 3 4F A3WE 1998090400929 19980904 00929 NM 1998 9 4 AALA981442 1 19980728 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 360 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - CORROSION ON FLOORBEAM STATION 360 RBL 13 TO RBL 15. REPAIRED AREA OUT OF LIMIT PER SRM 53-10-08 PAGE 9C, 9D, 9E. (M) 2 L 7 3 4F A3WE 1998090400930 19980904 00930 NM 1998 9 4 AALA981441 1 19980728 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 874AA 21386 TUL - DENT IN UPPER FLANGE AT BELL FRAME STATION 620, BETWEEN STATION 24-25L. REMOVED DAMAGED AREA AND INSTALLED DOUBLE R PER SRM 51-40-3, FIG 1 SHEET 3 PAGE 3. (M) 2 L 7 3 4F A3WE 1998090400931 19980904 00931 NM 1998 9 4 AALA981438 1 19980729 A 5754 SKIN BOEING 727 727223 1384074 NM LE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - FOUND CORROSION BEHIND DATA PLATE ON NR 1 AND NR 6 L/E FLAPS. REMOVED DATA PLATE. REMOVED CORROSION AND INSTALLE D DOUBLERS PER SRM 57-50-3. (M) 2 L 7 3 4F A3WE 1998090400932 19980904 00932 WP 1998 9 4 AALA981453 1 19980729 A 5320 FITTING DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70529 49921 TUL - FOUND CORROSION ON LONGERON END FITTING STATION 1338, L24L BEYOND LIMITS. INSTALLED NEW END CAP. (M) 2 L 7 2 4F A6WE 1998090400933 19980904 00933 EU 1998 9 4 AALA981279 1 19980624 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND CORROSION ON SEAT TRACK, FLOOR BOARD SUPPORT AT FRAME 31Y STATION 78 RT. INSTALLED STRAP REPAIR PER AARD 53 -20-00-2 AND SRM 51-22-00-0. ALODINED, PRIMED AND PAINTED. (M) 2 L 7 2 4F RT A35EU 1998090400934 19980904 00934 EU 1998 9 4 AALA981287 1 19980626 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 69 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND STRINGER 48L HAS CORROSION FORWARD OF FRAME 69. SPLICED IN NEW STRINGER SECTION PER SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998090400935 19980904 00935 EU 1998 9 4 AALA981286 1 19980627 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND CORROSION ALONG TRACK FROM FRAME 31-32 IN TRACK NR 8. REMOVED AND REPLACED SECTION OF SEAT TRACK PER SRM 53 -10-16. (M) 2 L 7 2 4F RT A35EU 1998090400936 19980904 00936 EU 1998 9 4 AALA981257 1 19980622 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 30-33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND CORROSION ON SEAT TRACK FROM FRAME 39A TO 33Y STATION 58, LEFT SIDE. REMOVED AND REPLACED CORRODED SEAT TRA CK WITH SERVICEABLE TRACK PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998090400937 19980904 00937 EU 1998 9 4 AALA981258 1 19980622 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 90070 513 TUL - FOUND CORROSION JUST FORWARD OF FRAME 33Y STATION 78 LEFT ON LAV SUPPORT AND SEAT TRACK. REMOVED AND REPLACED SEA T TRACK SECTION JUST FORWARD OF FRAME 34 TO FWD OF FRAME 33 PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998090400938 19980904 00938 EU 1998 9 4 AALA981285 1 19980626 A 5320 STIFFENERS AIRBUS 300 A300B4605R 3930308 EU BS 54 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - THE POD STOP STIFFENERS UNDER FORWARD END OF TRACK NR 5 CORRODED. INSTALLED NEW SECTION OF TRACK PER SRM 53-10-15 . (M) 2 L 7 2 4F RT A35EU 1998090400939 19980904 00939 EU 1998 9 4 AALA981288 1 19980626 A 5311 FRAME AIRBUS 300 A300B4605R 3930308 EU BS 61 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION ON TOP AND BOTTOM FRAME BETWEEN ROLLER TRAY 5 AND 6. INSTALLED NEW ANGLE PER SRM 51-72-10, PRIMED AND PAINTED PER SRM 51-75-10. (M) 2 L 7 2 4F RT A35EU 1998090400940 19980904 00940 EU 1998 9 4 AALA981190 1 19980616 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 200 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION ON FLOOR BOARD SUPPORT BETWEEN FRAME 11 AND 12, RT CENTER RAIL JUST AFT OF COCKPIT. REMOVED AND R EPLACED FLOOR BOARD SUPPORT RT SIDE OF COCKPIT DOOR FROM FRAME 11 TO FRAME 12 PER SRM 51-72-10. ALODINED, PRIMED AND PA INTED PER SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1998090400941 19980904 00941 EU 1998 9 4 AALA981191 1 19980618 A 5400 RIB AIRBUS 300 A300B4605R 3930308 EU NR 2 PYLON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - RIB 16A HAS CORROSION ON LANDING SURFACE. REPLACED RIB ASSY PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998090400942 19980904 00942 EU 1998 9 4 AALA981215 1 19980619 A 5347 CARGO TRACK AIRBUS 300 A300B4605R 3930308 EU BS 58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION IN SPLICE OF TRACK NR 6 AT FRAME 58. INSTALLED NEW SECTION OF TRACK PER SRM 53-10-15. (M) 2 L 7 2 4F RT A35EU 1998090400943 19980904 00943 EU 1998 9 4 AALA981214 1 19980619 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 61 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - CUTOUT DAMAGED AREA SPLICED IN NEW ONE PER SRM 53-10-15-2. ALSO, ALODINED, PRIMED AND PAINTED PER SRM 51-75-10. ( M) 2 L 7 2 4F RT A35EU 1998090400944 19980904 00944 EU 1998 9 4 AALA981213 1 19980618 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 66-68 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION ON NR 2 SEAT TRACK IN BETWEEN FRAME 66 AND 68 AT 2 SEPARATE AREAS. DRILLED UP 7076-T6 METAL FOR B RACKETS PER SRM 51-10-16-2 ALODINE, PRIMED AND PAINTED BRACKETS AND AREA CORROSION WAS REMOVED PER SRM 51-21-00. NO CRA CKS FOUND INSTALLED BRACKETS TO SUPPORT AREA CORROSION WAS REMOVED PER SRM 51-10-16-2. (M) 2 L 7 2 4F RT A35EU 1998090400945 19980904 00945 EU 1998 9 4 AALA981212 1 19980619 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU BS 57 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION AT JOINT OF VERTICAL PANEL AND BOTTOM OF TRACK NR 6 AT FRAME 57. INSTALLED NEW ANGLE TO BOTTOM OF TRACK PER SRM 51-75-10. (M) 2 L 7 2 4F RT A35EU 1998090400946 19980904 00946 EU 1998 9 4 AALA981255 1 19980622 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1498-1658 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION ON TOP LUGS OF NR 10 SEAT TRACK BETWEEN FRAME 21 AND FRAME 24, 3 PLACES. BLENDED OUT CORROSION, A LODINED, PRIMED AND PAINTED IAW ESO 30595, DATED 5/22/98. (M) 2 L 7 2 4F RT A35EU 1998090400947 19980904 00947 EU 1998 9 4 AALA981256 1 19980622 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1658 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - FOUND CORROSION ON TOP LUGS OF SEAT TRACK NR 9 AT FRAME 24. BLENDED OUT CORROSION, ALODINED, PRIMED AND PAINTED I AW ESO, 30595 DATED 6/22/98. (M) 2 L 7 2 4F RT A35EU 1998090400948 19980904 00948 EU 1998 9 4 AALA981280 1 19980624 A 5754 FLAP AIRBUS 300 A300B4605R 3930308 EU LE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14068 511 TUL - KRUGER FLAP HAS CORROSION THROUGHOUT INTERNAL STRUCTURE. REPLACED KRUGER FLAP PER A-300MM 27-87-11-4. (M) 2 L 7 2 4F RT A35EU 1998090400949 19980904 00949 WP 1998 9 4 AALA981431 1 19980724 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7533A 49987 TUL - FOUND EXTERIOR DOOR SKIN HAS LARGE DENT AT TOP FORWARD EDGE. INSTALLED DOUBLER IAW ESO 80172. (M) 2 L 7 2 4F A6WE 1998090400950 19980904 00950 WP 1998 9 4 AALA981430 1 19980724 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1271 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7533A 49987 TUL - FOUND CORROSION ON 'J' FRAME L-30 AT FS 1271. REPAIRED IAW 53-03 FIG 2A. (M) 2 L 7 2 4F A6WE 1998090400951 19980904 00951 EU 1998 9 4 AALA981381 1 19980714 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 69-70 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - STRINGER 54L BETWEEN FRAMES 69 AND 70 HAS DEEP CORROSION. CUT OUT CORRODED AREA AND REPAIRED AS PER SRM 53-10-14- 2. TREATED, PRIMED AND PAINTED AS PER SRM 51-21-10. (M) 2 L 7 2 4F RT A35EU 1998090400952 19980904 00952 EU 1998 9 4 AALA981382 1 19980714 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 63-64 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - STRINGER 53R CORRODED BETWEEN FRAME 63 AND FRAME 64. REMOVED CORRODED SECTION OF STRINGER 53R AND SPLICE IN NEW S ECTION IAW SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998090400953 19980904 00953 EU 1998 9 4 AALA981383 1 19980713 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 31-33 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION UNDER LAV. REMOVED AND REPLACED SECTION TRACK 53-10-16-2. (M) 2 L 7 2 4F RT A35EU 1998090400954 19980904 00954 EU 1998 9 4 AALA981384 1 19980715 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 30-31 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FLOOR SUPPORT BEAM SEAT TRACK 3 WAS FOUND TO BE CORRODED. BLENDED OUT CORROSION PER 51-74-10. REPAIRED PER AARD 53-20-00-2. (M) 2 L 7 2 4F RT A35EU 1998090400955 19980904 00955 EU 1998 9 4 AALA981380 1 19980714 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 71-72 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION AROUND 2 FASTENER HOLES IN FLOOR SUPPORT BETWEEN FRAMES 71 AND72 AND A/C CENTER LINE AND SEAT TRAC K NR 7. REMOVED AND REPLACED FLOOR SUPPORT PER 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998090400956 19980904 00956 EU 1998 9 4 AALA981406 1 19980717 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 66 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER FITTING UNDER DUCT IS CORRODED. REMOVED CORRODED STRINGER 48R FITTING AND INSTALLED NEW FITTING. ( M) 2 L 7 2 4F RT A35EU 1998090400957 19980904 00957 EU 1998 9 4 AALA981407 1 19980717 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 66 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER 48R CORRODED JUST FORWARD OF FRAME 66. REMOVED CORRODED PORTION OF STRINGER 48R AND REPAIRED AREA IAW 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998090400958 19980904 00958 EU 1998 9 4 AALA981412 1 19980718 A 5320 CLIP AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER CLIP CORRODED. ALODINED, PRIMED AND PAINTED AREA PER SRM 51-75-10-2. INSTALLED NEW STRINGER END P ER SRM 51-72-10-0 WITH SPLICE PER SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998090400959 19980904 00959 EU 1998 9 4 AALA981413 1 19980718 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER CLIP CORRODED. ALODINED, PRIMED AND PAINTED AREA PER SRM 51-75-10-2. INSTALLED NEW STRINGER END P ER SRM 51-72-10-10 W/SPLICE PER SRM 53-10-14-2. (M) 2 L 7 2 4F RT A35EU 1998090400960 19980904 00960 EU 1998 9 4 AALA981398 1 19980715 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 14-16 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FLOOR SUPPORT BEAM BETWEEN FRAME 14-16 CORRODED ENTIRE LENGTH. REPLACED ENTIRE LENGTH OF FLOOR SUPPORT UPPER CAP ENTIRE LENGTH PER SRM 53-70-00. (M) 2 L 7 2 4F RT A35EU 1998090400961 19980904 00961 EU 1998 9 4 AALA981397 1 19980716 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 64-65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - STRINGER 55L BETWEEN FRAMES 64 AND 65 HAS DEEP CORROSION. INSTALLED STRINGER REPAIR PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998090400962 19980904 00962 EU 1998 9 4 AALA981396 1 19980716 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 63-64 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - STRINGE R55L BETWEEN FRAMES 63 AND 64 HAS DEEP CORROSION. INSTALLED STRINGER REPAIR FROM FRAME 63 TO FRAME 65 PER SRM 53-10-14. (M) 2 L 7 2 4F RT A35EU 1998090400963 19980904 00963 EU 1998 9 4 AALA981395 1 19980716 A 5320 FITTING AIRBUS 300 A300B4605R 3930308 EU BS 63-65 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER END FITTING AT STRINGER 55L BETWEEN FRAMES 65 TO 63 HAS DEEP CORROSION. INSTALLED STRINGER REPAIR FROM FRAME 63 TO FRAME 65 PER SRM 53-10-14, ALSO INSTALLED NEW END FITTING AT FRAME 65. (M) 2 L 7 2 4F RT A35EU 1998090400964 19980904 00964 EU 1998 9 4 AALA981394 1 19980716 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 65-66 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER 51L BETWEEN FRAMES 65 AND 66 HAS DEEP CORROSION. REPAIRED STRINGER PER SRM 53-10-14-2. TREATED AN D PAINTED PER SRM 51-21-01 AND INSTALLED NEW FASTENERS. (M) 2 L 7 2 4F RT A35EU 1998090400965 19980904 00965 EU 1998 9 4 AALA981418 1 19980722 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 57-58 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER 52L AT FRAME 57.3 TO 58 HAS CORROSION. REMOVED STRINGER SPLICE THAT IS AFT OF CORROSION DAMAGED ON STRINGER. INSTALLED NEW STRINGER SPLICE THAT IS APPROX 9 INCHES LONGER AND EXTENDS 6 FASTENER HOLES FORWARD AND PAST D AMAGED AREA ON STRINGER AS PER SRM 51-72-10-0. TREATED, PRIMED AND PAINTED PER SRM 51-21-10. (M) 2 L 7 2 4F RT A35EU 1998090400966 19980904 00966 EU 1998 9 4 AALA981419 1 19980722 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59-60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER 55L AT FRAME 59 TO 60 HAS CORROSION. REPLACED DAMAGED SECTION OF STRINGER ADDED NEW SPLICE ON AFT END OF NEW SECTION. REINSTALLED SPLICE ON FWD END AS PER SRM 51-72-10-0. TREATED, PRIMED AND PAINTED PER SRM 51-21-10. (M) 2 L 7 2 4F RT A35EU 1998090400967 19980904 00967 EU 1998 9 4 AALA981420 1 19980722 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59-60 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - STRINGER 54L AT FRAME 59 TO 60 HAS CORROSION. REPLACED DAMAGED SECTION OF STRINGER ADDED NEW SPLICE ON AFT END OF NEW SECTION. REINSTALLED FORWARD SPLICE AS PER SRM 51-72-10-0. TREATED, PRIMED AND PAINTED PER SRM 51-21-10. (M) 2 L 7 2 4F RT A35EU 1998090400968 19980904 00968 EU 1998 9 4 AALA981421 1 19980722 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON STRINGER 53L, 1 INCH FORWARD OF FRAME 59. REPLACED DAMAGED SECTION OF STRINGER ADDED NEW SPLIC E ON AFT END ON NEW SECTION. REINSTALLED FORWARD SPLICE AS PER SRM 51-72-10-0. TREATED, PRIMED AND PAINTED PER SRM 51- 21-10-0. (M) 2 L 7 2 4F RT A35EU 1998090400969 19980904 00969 EU 1998 9 4 AALA981422 1 19980721 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND STRINGER HAS CORROSION. CUT OUT CORRODED SECTION OF STRINGER AND REPAIRED AS PER SRM 53-10-14-2. TREATED, PRIMED AND PAINTED AS PER SRM 51-20-00. (M) 2 L 7 2 4F RT A35EU 1998090400970 19980904 00970 EU 1998 9 4 AALA981424 1 19980721 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - STRINGER HAS CORROSION. CUT OUT CORRODED SECTION OF STRINGER AND REPAIRED AS PER SRM 53-10-14-2. TREATED, PRIMED AND PAINTED AS PER SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1998090400971 19980904 00971 EU 1998 9 4 AALA981423 1 19980721 A 5313 STRINGER AIRBUS 300 A300B4605R 3930308 EU BS 59 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - STRINGER HAS CORROSION. CUT OUT CORRODED SECTION OF STRINGER AND REPAIRED AS PER SRM 53-10-14-2. TREATED, PRIMED AND PAINTED AS PER SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1998090400972 19980904 00972 EU 1998 9 4 AALA981429 1 19980723 A 5315 FLOORBEAM AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FLOORBEAM NR 63 RIGHT AT NR 6 LOAD TRAY HAS CORROSION. REMOVED DAMAGED SECTION OF FRAME FROM SPLICE B/H OUTBOARD END. RESPLICED DAMAGED SECTION PER SRM 51-72-10-0. TREATED, PRIMED AND PAINTED PER SRM 51-21-10-0. (M) 2 L 7 2 4F RT A35EU 1998090400973 19980904 00973 EU 1998 9 4 AALA981428 1 19980723 A 5540 STRAP AIRBUS 300 A300B4605R 3930308 EU RUDDER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - APEX STRAP HAS AREAS OF CORROSION ON LEFT AND RT SIDE OF RUDDER. REMOVED AREA OF CORROSION AND SPLICED IN NEW SEC TION PER ESO 30595 DATED 4-13-98. (M) 2 L 7 2 4F RT A35EU 1998090400974 19980904 00974 EU 1998 9 4 AALA981427 1 19980723 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU CABIN CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON FLOORBOARD SUPPORT APPROX 20 INCH FROM COCKPIT. REPAIRED SUPPORT PER ESO 30595, DATED 7-17-98. (M) 2 L 7 2 4F RT A35EU 1998090400975 19980904 00975 NM 1998 9 4 WRLA98090 1 19980807 A 2450 66586F0 CONNECTOR DOUG MD11 MD11 3023602 NM NR 2 ENGINE CONTAMINATED A WRLA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 272WA 48437 DURING TAXI FOR TAKEOFF, FLIGHT CREW WAS UNABLE TO OBTAIN ELECTRICAL POWER FROM NR 2 ENGINE IDG. FLIGHT CREW ELECTED TO RETURN TO GATE FOR MAINTENANCE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL FOUND ELECT RICAL CANNON PLUG ON FIREWALL (CORE-6 POSITION) WAS CONTAMINATED WITH DIRT, AND NOT ALLOWING PROPER CONTACT. MAINTENANC E PERSONNEL CLEANED CANNON PLUG AND PERFORMED ENGINE RUN. IDG CAME ON LINE WITH NO FAULTS. A/C RETURNED TO SERVICE. ( M) 2 L 7 3 4F RT A22WE 1998090400976 19980904 00976 EU 1998 9 4 SIMA982121 1 19980731 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED EME RGENCY LIGHT BATTERY PACK AT 10WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998090400977 19980904 00977 NM 1998 9 4 ASAA9810071 1 19980724 A 5311 FRAME BOEING 737 737298C 1384490 NM BS 500 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND MATERIAL DAMAGE IN TWO PLACES AT STATION 500, BETWEEN STRINGER 22L AND 21L, AND ADJACENT TO STRINGER 22L. REPAIRED PER ASA EA 5310-01582. (M) 2 L 7 2 4F RT A16WE 1998090400978 19980904 00978 NM 1998 9 4 ASAA9810072 1 19980724 A 5320 FRAME BOEING 737 737298C 1384490 NM CARGO DOORWAY MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND MAIN CARGO DOOR FRAME HAS MISDRILLED HOLE AT STATION 480, STRINGER 18R. REPAIRED PER ASA EA 5310-01591. (M) 2 L 7 2 4F RT A16WE 1998090400979 19980904 00979 EU 1998 9 4 USAAF98065 1 19980804 A 2612 33100007 DETECTOR FOKKER F28 F28MK0100 4990807 EU APU BAY MALFUNCTIONED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 886US 11346 TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING AN NUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENE RATOR WAS ON MEL. FLT LANDED TYS WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE APU AREA AND FOUND NO EVIDENCE OF FIRE. REPLACED THE APU FIRE BOTTLE, NR 1 GENERATOR AND NR 1 GENERATOR CONTROL UNIT. MAINTENANCE ALSO PROGRAMMED THE A PU ENCLOSURE SEALS TO BE REPLACED. (M) 2 L 7 2 4F RT 1998090400980 19980904 00980 EU 1998 9 4 98ZZZM606 1 19980804 A 2421 740508 IDG FOKKER F28 F28MK0100 4990807 EU APU BAY FAILED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 886US 11346 TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING AN NUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENE RATOR WAS ON MEL. FLT LANDED TYS WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE APU AREA AND FOUND NO EVIDENCE OF FIRE. REPLACED THE APU FIRE BOTTLE, NR 1 GENERATOR AND NR 1 GENERATOR CONTROL UNIT. MAINTENANCE ALSO PROGRAMMED THE A PU ENCLOSURE SEALS TO BE REPLACED. (M) 2 L 7 2 4F RT 1998090400981 19980904 00981 EU 1998 9 4 98ZZZM607 1 19980804 A 2420 740514C GCU FOKKER F28 F28MK0100 4990807 EU APU BAY FAILED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 886US 11346 TYS - FLT 1633 - ON APPROACH TO TYS DESCENDING THROUGH 4000 FEET, WHEN SPEEDBRAKES WERE DEPLOYED THE APU FIRE WARNING AN NUNCIATED. THE APU AUTOMATICALLY SHUT DOWN AND THE FIRE BOTTLE DISCHARGED. THE APU WAS BEING RUN BECAUSE THE NR 1 GENE RATOR WAS ON MEL. FLT LANDED TYS WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE APU AREA AND FOUND NO EVIDENCE OF FIRE. REPLACED THE APU FIRE BOTTLE, NR 1 GENERATOR AND NR 1 GENERATOR CONTROL UNIT. MAINTENANCE ALSO PROGRAMMED THE A PU ENCLOSURE SEALS TO BE REPLACED. (M) 2 L 7 2 4F RT 1998090400982 19980904 00982 EU 1998 9 4 98ZZZM608 1 19980729 A 5230 180061 SEAL AMD FALC20 FALCON 2720302 EU CARGO DOOR FAILED A DKAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 227R 227 CARGO DOOR SEAL FAILED CLIMBING THROUGH FLIGHT LEVEL 22,500. REPLACED DOOR SEAL ON FRAME ALONG BOTTOM. OPERATIONAL CHE CKS GOOD ON GROUND CHECKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A7EU 1998090400983 19980904 00983 NM 1998 9 4 P2EA98156 1 19980811 A 5280 6550520504 DOOR BOEING 737 737205 NM RT NLG CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 412CE 20412 MCI - RIGHT NLG DOOR LOWER FORWARD CORNER HAS DAMAGE. INSPECT RIGHT NLG DOOR FORWARD HINGE FITTING FOR CRACKS. REPLACE D RIGHT NLG DOOR AND PERFORMED GEAR SWING PER MM 32-22-11. WHILE RIGHT NLG DOOR WAS REMOVED, PERFORMED VISUAL AND DYE P ENETRANT INSPECTION OF FWD HINGE FITTING. NO DAMAGE NOTED. (M) 2 L 7 2 4F A16WE 1998090400984 19980904 00984 NM 1998 9 4 P2EA98155 1 19980808 A 3242 26010425 BRAKE BENDIX BOEING 737 737247 138448D NM LT MLG DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP B3816AD 19607 MCI - FLT 815 - THE FOLLOWING WAS NOTED DURING POST FLIGHT WALKAROUND, NR 2 BRAKE LINE QUICK DISCONNECT, METERING VALVE, IS BROKEN OFF OF THE BRAKE ASSY. MAINTENANCE ENTRY REPLACED LEFT MLG DUE TO DAMAGE AT NR 2 BRAKE. REPLACED BRAKE LINE AND QUICK DISCONNECT (METERING VALVE) PER MM CHAPTER 32. REPLACED LEFT MLG ASSY PER CARD J232-11-01-C AND MM 32-11-00. (M) 2 L 7 2 4F A16WE 1998090400985 19980904 00985 NM 1998 9 4 P2EA98154 1 19980805 A 5330 SKIN BOEING 737 737244 138448U NM BS 188 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - UPPER FUSELAGE BS 188, DOUBLER BELOW LEFT WINDSHIELD CENTER POST CRACKED. REPAIRED IAW BOEING S/B 737-53-1059. ( M) 2 L 7 2 4F A16WE 1998090400986 19980904 00986 NM 1998 9 4 P2EA98153 1 19980805 A 5320 ANGLE BOEING 737 737244 138448U NM NR 2 GALLEY CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PASSENGER CABIN FORWARD NR 2 GALLEY FLOOR ANGLE WITH CORROSION. REPLACED ANGLE IN REFERENCE TO SRM 51-10-1 PAGE 5 . (M) 2 L 7 2 4F A16WE 1998090400987 19980904 00987 NM 1998 9 4 P2EA98152 1 19980805 A 5330 SKIN BOEING 737 737244 138448U NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - REPAIR INTERNAL DOUBLER AT BS 727A STRINGER 16R. REPAIRED FUSELAGE SKIN DUE TO CRACK FROM BS 727 PLUS 11 INCHES T O BS 727 PLUS 4 INCHES, BETWEEN STRINGERS 15R AND 19R IN REFERENCE TO SRM 53-30-3 FIG 17 DETAIL 5. (M) 2 L 7 2 4F A16WE 1998090400988 19980904 00988 NM 1998 9 4 P2EA98151 1 19980805 A 5330 SKIN BOEING 737 737244 138448U NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - CRACKED SKIN AROUND FASTENER, EXTERNAL FUSELAGE BS 727A BETWEEN STRINGER 14R AND 15R. REPAIRED FUSELAGE SKIN CRAC K AT BS 727A BETWEEN STRINGER 14R AND 15R IN REFERENCE TO SRM 53-30-3 FIGURE 17. (M) 2 L 7 2 4F A16WE 1998090400989 19980904 00989 NM 1998 9 4 P2EA98150 1 19980806 A 5330 SKIN BOEING 737 737244 138448U NM BS 854-881 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - EXTERNAL FUSELAGE SKIN WITH MATERIAL LOSS MORE THAN 10 PERCENT IN SEVERAL PLACES DUE TO CORROSION AT STRINGER 20L FROM BS 767 TO BS 887. REMOVED CORROSION FROM FUSELAGE SKIN FROM BS 747 TO BS 832 AND BS 854 TO BS 881 AT STRINGER 20L IN REFERENCE TO SRM 51-10-6 PAGE 12, WITH IN LIMITS REFERENCE SRM 53-30-1 FIG 1, DETAIL 2 ORIGINAL .036, REMAINING .034. REPAIRED FUSELAGE SKIN BETWEEN BS 832 AND BS 854 AT STRINGER 20L IN REFERENCE TO SRM 53-30-3 FIG 16. (M) 2 L 7 2 4F A16WE 1998090400990 19980904 00990 NM 1998 9 4 P2EA98149 1 19980804 A 5330 SKIN BOEING 737 737244 138448U NM BS 312-318 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - REPAIR L1 LOWER DOUBLER, FORWARD LOWER CORNER. REPAIRED FORWARD ENTRY DOOR EXTERNAL SKIN CRACK AT FORWARD LOWER C ORNER BETWEEN BS 312 AND BS 318 FROM WL 212 TO WL 218 IN REFERENCE TO SRM 52-00-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998090400991 19980904 00991 EU 1998 9 4 PLGA980810B 1 19980810 A 2610 72111211000 DETECTOR SAAB SF340 SF340A 7850100 EU CARGO BAY MALFUNCTIONED A PLGA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 NE 05 344BE A3847 340A104 BOS - FLT 4358 - WHLE DESCENDING INTO BOS, THE CREW RECEIVED A SMOKE WARNING IN BOTH CARGO AND LAVATORY COMPARTMENTS. C REW DECLARED AN EMERGENCY AND FOLLOWED PROCEDURES. THE CARGO COMPARTMENT FIRE EXTINGUISHER WAS DISCHARGED AFTER WHICH B OTH WARNING LIGHTS EXTINGUISHED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED BOTH COMPARTMENTS AND FOUND N O EVIDENCE OF FIRE, SMOKE OR HEAT DAMAGE. BOTH CARGO AND LAVATORY COMPARTMENT SMOKE DETECTORS WERE REPLACED ALONG WITH FIRE EXITNGUISHER BOTTLE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998090400992 19980904 00992 EU 1998 9 4 PLGA980810A 1 19980810 A 2610 WIRE SAAB SF340 SF340A 7850100 EU RT ENGINE CHAFED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING N Y FALSE WARNING ENGINE STOPPAGE CL CLIMB 1 NE 05 341BE 340A063 BTV - FLT 4479 - TEN MINUTES AFTER DEPARTURE FROM BTV, THE CREW RECEIVED A RIGHT TAIL PIPE HOT WARNING. THE CREW FOLLOW ED PROCEDURES AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT RETURNED TO BTV AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A CHAFED WIRE ON AIRFRAME SIDE OF TAIL PIPE HOT INDICATION SYSTEM. WIRE WAS REPAIRED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998090400993 19980904 00993 WP 1998 9 4 NOCA1798 1 19980801 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 INSPECTION OF E-PATH LIGHTING FOUND INOPERATIVE AT ROWS 12 THROUGH 16. FOUND LOOSE CONNECTOR AT ROW 12. CONNECTOR REAT TACHED. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998090400994 19980904 00994 WP 1998 9 4 ORJA98188 1 19980804 A 3350 EM1267 BATTERIES DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 RNO - O/H EMERGENCY LIGHTS INOP BETWEEN ROWS 18A-21AC, LEFT SIDE. REMOVED AND REPLACED BATTERIES, OPS CHECK OK. (M) 2 L 7 2 4F A6WE 1998090400995 19980904 00995 WP 1998 9 4 ORJA98187 1 19980803 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 SJC - EMERGENCY LIGHTS AT ROW 21 ILLUMINATE AT ALL TIMES. REMOVED BATTERY PACK RIGHT AFT EMERGENCY DOOR, OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A6WE 1998090400996 19980904 00996 WP 1998 9 4 ORJA98186 1 19980803 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 SJC - LEFT AND RIGHT AFT EMERGENCY EXI TLIGHTS INOP, UPPER. REMOVED AND REPLACED AFT EMERGENCY BATTERY PACK, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1998090400997 19980904 00997 WP 1998 9 4 ORJA98185 1 19980803 A 3350 PPSIB CHARGER DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY FLOOR PATH, ROWS 19-21, AIRCRAFT RIGHT, CAME ON IN FLIGHT. STAYED ON 30 MINUTES AND WENT OUT. LIGHTS DO NOT TEST ON GROUND AT ORD. REPLACED BATTERY/CHARGER PACK FOR EMERGENCY FLOOR PATH LIGHTS AT RENO 21, SEAT F IAW BRUCE INDUS TRIES MM400-079. OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A6WE 1998090400998 19980904 00998 WP 1998 9 4 ORJA98184 1 19980802 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 751RA 49779 AT SJC, EMERGENCY LIGHTS INOPERATIVE, ROWS 20-23. REMOVED AND REPLACED R/A AG BATTERY PACK/CHARGER. OPS CHECK GOOD. ( M) 2 L 7 2 4F RT A6WE 1998090400999 19980904 00999 WP 1998 9 4 ORJA98183 1 19980801 A 3350 EM1267 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 AT SJC, EMERGENCY LIGHTS INOPERATIVE AT ROWS 22-25. REMOVED AND REPLACED BATTERY CHARGER. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998090401000 19980904 01000 WP 1998 9 4 ORJA98182 1 19980801 A 3350 EM1267 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 AT RENO, EMERGENCY LIGHTS INOPERATIVE AT ROWS 8-12. REPLACED BATTERY. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998090401001 19980904 01001 CE 1998 9 4 98ZZZM609 1 19980803 A 2130 1143810035 SWITCH BEECH 1900 1900D 1154162 CE LT WING ROOT FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 859CA 115L UE128 LEFT ENVIRONMENTAL FAIL ON TAKEOFF. OVERPRESSURE SWITCH FAILURE. REPLACED LT ENVIRONMENTAL OVERPRESSURE SWITCH. (M) 2 L 7 2 4T RT A24CE 1998090401002 19980904 01002 CE 1998 9 4 98ZZZM610 1 19980804 A 5210 1295140533 LEVER BEECH 1900 1900D 1154162 CE FUSELAGE BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 838CA UE34 AIRSTAIR DOOR LEVER ASSY BROKEN. REPLACED LEVER ASSY IAW CHAP 56 RAYTHEON MM. (M) 2 L 7 2 4T RT A24CE 1998090401003 19980904 01003 CE 1998 9 4 98ZZZM611 1 19980802 A 2130 1813800213 SOLENOID BEECH 1900 1900D 1154162 CE FUSELAGE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 840CA UE38 PRESSURIZATION INOPERATIVE. RESET AND DUMP SOLENOID DEFECTIVE. REPLACED RESET AND DUMP SOLENOIDS. (M) 2 L 7 2 4T RT A24CE 1998090401005 19980904 01005 NM 1998 9 4 GAIA98078 1 19980810 A 3610 32146451 VALVE BOEING 727 727223 1384074 NM NR 3 ENGINE LEAKING A GAIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 854AA 20995 AFTER DEPARTING TOL, NR 3 STRUT OVERHEAT LIGHT ILLUMINATED AT 100 FT AGL, AND REMAINED ILLUMINATED UNTIL THRUST RETARDED BELOW 70 PERCENT N-1. AIRCRAFT RETURNED TO TOL AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 3 ENGINE BLEED VALVE AND HIGH PRESSURE WING TAI VALVE GASKETS. RAN NR 3 ENGINE WITH NO LEAKS NOTED. STRUT OVERHEAT, OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998090401006 19980904 01006 WP 1998 9 4 GAIA9873 1 19980724 A 5315 FLOORBEAMS CVAC 240 240D 2422660 WP BS 414-691 BENT A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 94279 101 DURING C-CHECK INSPECTION, THE AFT CARGO FLOOR SUPPORT BEAMS AT FS 414 TO 691 WERE FOUND BENT DOWN ON THE TOP EDGES WHER E FREIGHT LOADS HAD BEEN DROPPED. THE AREAS ABOVE WERE REPAIRED IAW KHA EA NR CV-53-36 APPROVED BY 8110-3 NR 98399 PREP AIRED BY DER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R RT A793 1998090401007 19980904 01007 WP 1998 9 4 GAIA9874 1 19980725 A 3231 39567851 LINK DOUG DC9 DC915F 3022037 WP NLG OUT OF ADJUST A GAIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 07 562PC 48138 47012 KHA - FLT 613 LRD TO MMGDL - ON TAKEOFF FROM LRD, THE FLIGHT CREW NOTICED MODERATE VIBRATION AFTER GEAR RETRACTION. THE FLIGHT CREW RETURNED TO LRD. UPON GEAR EXTENSION, THE VIBRATION STOPPED. AN UNEVENTFUL LANDING WAS MADE. AFTER PARKIN G, DISCOVERED THE FORWARD NOSE GEAR DOORS WERE OPEN. FURTHER INVESTIGATION REVEALED THE NOSE GEAR DOORS WERE OUT OF ADJ USTMENT. THE AIRCRAFT WAS FERRIED WITH THE GEAR DOWN FROM LRD TO DFW WHERE THE NOSE GEAR DOORS WERE ADJUSTED PER DC-9 M M. THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F A6WE 1998090401008 19980904 01008 WP 1998 9 4 GTIA9800081 1 19980718 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - FLT 417 - ON PREFLIGHT, FOUND FORWARD EMERGENCY OVERHEAD LIGHTS INOPERATIVE. REMOVED AND REPLACED FORWARD NR 2 AN D NR 4 BATTERIES IN BATTERY PACK ON EMERGENCY OVERHEAD LIGHTS. OPERATIONAL CHECK ON EMERGENCY LIGHTS GOOD DC-9 MAINTENA NCE MANUAL 33-50-0. (M) 2 L 7 2 4F A6WE 1998090401009 19980904 01009 WP 1998 9 4 GTIA9800087 1 19980809 A 3350 1315 BULB DOUG DC9 DC931 3022065 WP CABIN MISSING A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 DTW - FLT 418 - LIGHT BULB MISSING FROM RED AISLE PATH LIGHT AT ROW 14. RELAMPED EMERGENCY TRACK LIGHT AT ROW 14. OPER ATIONAL CHECK GOOD. REFERENCE DC-9 MM CHAPTER 33-50-00. (M) 2 L 7 2 4F A6WE 1998090401010 19980904 01010 WP 1998 9 4 GTIA9800088 1 19980802 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 EWR - FLT 264 - CABIN LOG ITEM NR 3, FLOOR PATH LIGHTING AT EXIT ROW IS MISSING A RED LIGHT. REPLACED LIGHT AND LENS CO VER, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998090401011 19980904 01011 CE 1998 9 4 98ZZZM612 1 19980726 A 2751 SWITCH BEECH 1900 1900 1154160 CE FLAP LIMIT OUT OF ADJUST A GUUA K NONE O OTHER NR NOT REPORTED 1 SO 19 188GA UB14 FLT 9472 - TLH-TPA - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS IN APPROACH POSITION. ADJUSTED APPROACH LIMITS SWI TCH. OPERATIONAL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1998090401012 19980904 01012 CE 1998 9 4 98ZZZM613 1 19980725 A 2750 LEVER BEECH 1900 1900 1154160 CE COCKPIT OUT OF ADJUST A GUUA K NONE J WARNING INDICATION AP APPROACH 1 SO 19 188GA UB14 FLT 9483 - MIA-MCO - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS MOVED INTO APPROACH. REPOSITIONED FLAP SELECTOR LE VER GUARD. OPERATIONAL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1998090401013 19980904 01013 CE 1998 9 4 98ZZZM614 1 19980731 A 3260 SWITCH BEECH 1900 1900C 1154161 CE RT MLG LOOSE A GUUA K NONE O OTHER NR NOT REPORTED 1 SO 19 155GA UB55 FLT 2020 - FLL-MIA - GEAR UNSAFE LIGHT ILLUMINATED AND RIGHT GEAR DOWN AND LOCKED ANNUNCIATOR EXTINGUISHES ON GROUND WHE N RIGHT BRAKE IS DEPRESSED. SECURED RIGHT MAIN GEAR DOWNLOCK SWITCH. (M) 2 L 7 2 4T RT A24CE 1998090401014 19980904 01014 SW 1998 9 4 98ZZZM615 1 19980809 A 8200 CAWI FRCHLD SA227 SA227DC 3377521 SW COCKPIT INOPERATIVE A EQGA C D ABORTED TAKEOFF RETURN TO BLOCK R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 SW 19 853LS DC853B FLT 163 - DFW-PNS - CREW WAS RELEASED FOR TAKEOFF OUT OF DFW EN ROUTE TO PNS, AS THE CREW BROUGHT UP POWER, CAPTAIN CALL ED FOR CAWI ON. CREW RECEIVED 2 LIGHTS, BUT NO TORQUE RISE. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE IN SPECTED THE AIRCRAFT AND ATTEMPTED TO FIRE THE CAWI SYSTEM. CAWI SYSTEM DETERMINED TO BE INOPERATIVE. MAINTENANCE DEFE RRED THE CAWI SYSTEM IAW MEL 82-1-2. CONTROL NR 2130. AIRCRAFT RETURNED TO REVENUE SERVICE. (M) 2 L 7 2 4T RT A18SW 1998090401015 19980904 01015 WP 1998 9 4 ASAA9880125 1 19980711 A 5610 NUT DOUG DC9 DC982 3022082 WP WINDOW DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 ANC - PRIOR TO DEPARTURE OF FLT 104, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WAS DIFFICULT TO CLOSE. R EPLACED NUT ON UPPER AFT ROLLER OF SLIDING WINDOW MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998090401016 19980904 01016 WP 1998 9 4 TWAA9814001 1 19980824 A 5312 BULKHEAD TEE DOUG DC9 DC982 3022082 WP BS 1338 CREASED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 919TW 49368 DURING CHECK-C MAINT, FOUND CREASE ON BULKHEAD TEE STA 1338, BETWEEN LONGERON 29R AND 29L. REMOVED AND REPLACED TEE PER SRM 53-03, FIG 37A. 2 L 7 2 4F A6WE 1998090401017 19980904 01017 WP 1998 9 4 VJ9800307 1 19980826 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 541 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FORWARD PIT FRAME CORRODED TOP AND BOTTOM AT FS 541, L27L-28L. REMOVED CORROSON IAW DC9 SRM 51-10-3, SRM 53-01, FIG 1. REMOVED FLOOR SUPPORT FROM LONGERON 24R-24L IAW DC9 SRM 51-30-2. FABRICATED FLOOR SUPPORT FROM 7075-0, .063, TREATED, LOCATED, DRILLED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-2, 51-10-2A, 51-10-4, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998090401018 19980904 01018 WP 1998 9 4 VJ9800308 1 19980827 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 44 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 LOWER FORWARD AREA SKIN ATTACHMENT ANGLE AT RT NOSE WHEEL AREA HAS CORROSION BEYOND LIMIT. REMOVED CORROSION AND ATTACH ANGLE IAW DC9 SRM 51-10-3 AND SRM 53-01, FIG 1. FABRICATED REPAIR DOUBLER AND PRIMED IAW DC9 SRM 51-10-2, 51-10-3, 51- 30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998090401019 19980904 01019 WP 1998 9 4 VJ9800309 1 19980827 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 465 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FORWARD PIT FRAME CORRODED BEYOND LIMIT AT FS 465, L30. REMOVED FASTENERS AND CORROSION IAW DC9 SRM 51-30-1. FABRICATE D REPAIR, CLIP FILLER AND DOUBLERS IAW DC9 SRM 53-08, FIG 2A, 51-10-3, 51-30-2 AND 51-30-5. HEAT TREATED, ALODINED, PRI MED AND INSTALLED FABRICATED PARTS AND FASTENERS IAW DC9 SRM 51-10-2A, 51-10-3 AND 51-30-5. 2 L 7 2 4F A6WE 1998090401020 19980904 01020 WP 1998 9 4 VJ9800310 1 19980828 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FORWARD PIT FRAME, WHERE CLIP NUTS TO LOWER PART OF FRAME, CORRODED BEYOND LIMIT AT FS 579, L26R-26L. REMOVED CORROSION IAW DC9 SRM 53-01, FIG 1. FABRICATED FRAME, HEAT TREATED, TRIMMED, DEBURRED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-21 , 51-10-4, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998090401021 19980904 01021 WP 1998 9 4 VJ9800311 1 19980828 A 5320 9915561353 WEB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 AFT PIT WEB CORRODED BEYOND LIMIT AT FS 996. REMOVED CORROSION, DRILLED, DEBURRED, ALODINED, AND PAINTED NEW WEBS IAW D C9 SRM 51-10-2, 51-10-3 AND 51-10-4. 2 L 7 2 4F A6WE 1998090401022 19980904 01022 WP 1998 9 4 VJ9800312 1 19980828 A 5320 99155617 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 JACKPAD STRUT CORRODED BEYOND LIMIT AT FS 996, L30. REMOVED CORROSION FROM JACKPAD FITTING AND ALODINED, PRIMED, REPAIN TED, DRILLED AND DEBURRED NEW STRUT IAW DC9 SRM 51-10-3 AND 51-10-4. 2 L 7 2 4F A6WE 1998090401023 19980904 01023 WP 1998 9 4 VJ9800313 1 19980828 A 5320 SHROUD DOUG DC9 DC932 3022066 WP APU COMPT CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 APU GENERATOR ACCESS INNER ATTACH COVER OPENING HAS POPPED FASTENERS AND DEEP CHAFE MARKS BEYOND LIMIT. REMOVED SHROUD, DRILLED OFF HEAT BLANKET TO GAIN ACCESS TO WORK AREA IAW DC9 SRM 53-01, FIG 1. FABRICATED NEW SHROUD PER DC9 SRM 51-10 -2, 51-10-4 AND RES 981200. TREATED, PRIMED AND INSTALLED COVER IAW DC9 SRM 51-10-3 AND 51-30-1. 2 L 7 2 4F A6WE 1998090401024 19980904 01024 WP 1998 9 4 VJ9800314 1 19980828 A 5400 5958666171921 SEAL DOUG DC9 DC932 3022066 WP NR 1 ENGINE CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 NR 1 ENGINE SPRING SEAL ON LOWER SURFACE APRON HAS WEAR BEYOND LIMIT DUE TO CHAFING IAW DC9 SRM 53-01, FIG 1. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW SPRING SEALS IAW DC9 SRM 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1998090401025 19980904 01025 NM 1998 9 4 VJ9800315 1 19980830 A 3350 370067001 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 467AT 22055 R1 AND R2 PORTABLE EXIT LIGHTS INOP. REPLACED BATTERIES; OPS CHECKED GOOD IAW MM 33-10. 2 L 7 2 4F A16WE 1998090401026 19980904 01026 WP 1998 9 4 CALA9801588 1 19980831 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP CARGO COMPT LEAKED A CALA O OTHER K J B FLUID LOSS WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 16894 49393 SMOKE APPEARED IN THE CABIN AFTER TAKEOFF AND BEGAN CLEARING WITHIN 2-3 MINUTES. THE SMOKE HAD COMPLETELY DISSIPATED WI THIN 10-15 MINUTES. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A HYDRAULIC LINE IN THE AFT CARGO COMPARTMENT LEAKING CAUSING HYDRAULIC FLUID TO BE INGESTED BY APU. THE LINE WAS REPAIRED IAW GENERAL MAINTENANCE MANUAL 10-799-78. AN ENGINE RUN WAS PERFORMED WITH PACKS OPERATING AND NO SMOKE WAS NOTED. 2 L 7 2 4F A6WE 1998090401027 19980904 01027 NM 1998 9 4 CALA9801589 1 19980831 A 3260 387 BULB BOEING 737 737130 1384435 NM NLG FAILED A CALA L ABORTED APPROACH L P NO TEST NO WARNING INDICATION AP APPROACH 1 SW 09 77204 19021 NO NOSE GEAR INDICATION WAS RECEIVED WHEN GEAR WAS EXTENDED ON APPROACH. A GO-AROUND WAS INITIATED AND THE NOSE GEAR LI GHTS DID NOT TEST. THE NOSE GEAR INDICATOR LIGHT BULBS WERE REPLACED AND TESTED GOOD. GOOD INDICATIONS WERE RECEIVED W ITH GEAR EXTENDED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. 2 L 7 2 4F A16WE 1998090401028 19980904 01028 NM 1998 9 4 CALA9801590 1 19980828 A 5311 FRAME BOEING 727 727232 1384082 NM BS 910 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN LT INTERIOR FUSELAGE FRAME AT FS 910 AT STRINGER 15L. THE CRACKED AREA WAS TRIMMED OUT, A REPAIR WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090401029 19980904 01029 NM 1998 9 4 CALA9801591 1 19980829 A 5532 PANEL BOEING 727 727232 1384082 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN LT VERTICAL STABILIZER SLIDER PANEL AND A .75 INCH CRACK IN RT VERTICAL STABILIZER S LIDER PANEL. BOTH PANELS WERE REPLACED IAW SRM 51-20-1, FIGURE 7, 51-10-2, AND MM 51-20-2. 2 L 7 3 4F A3WE 1998090401030 19980904 01030 NM 1998 9 4 CALA9801592 1 19980829 A 5311 FRAME BOEING 727 727232 1384082 NM BS 375 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 AND 1.5 INCH CRACK IN DOOR FRAME AT FS 375 JUST FORWARD OF R-1 DOOR CUTOUT STRINGER 17R ABOVE FLOOR LINE. A DOUBLER, TRIPLER, AND FILLERS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1, 51-30, 51-10-2, AND MM 51-20. 2 L 7 3 4F A3WE 1998090401031 19980904 01031 NM 1998 9 4 CALA9801593 1 19980829 A 5320 SUPPORT BOEING 727 727232 1384082 NM CARGO COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1.5 INCH CRACK IN SIDEWALL SUPPORT ON RT SIDE AFT OF C-1 DOOR. THE CRACKED SECTION OF SUPPORT WAS RE MOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-0. 2 L 7 3 4F A3WE 1998090401032 19980904 01032 NM 1998 9 4 CALA9801594 1 19980830 A 5330 SKIN BOEING 727 727232 1384082 NM BS 373 DAMAGED A CALA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN AT BS 373 BETWEEN STRINGER 22R AND 23R. THE DAMAGED AREA WAS CUT OUT IAW SRM 53-30-3. A REPAIR WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998090401033 19980904 01033 NM 1998 9 4 CALA9801595 1 19980830 A 5330 SKIN BOEING 727 727232 1384082 NM STA 389 DAMAGED A CALA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT STA 389 BETWEEN STRINGERS 23R AND 24R. THE DAMAGED AREA WA S REMOVED IAW SRM 53-30-3. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-1 AND 51-20-4. 2 L 7 3 4F A3WE 1998090401034 19980904 01034 NM 1998 9 4 CALA9801596 1 19980831 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1030 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CABIN SEAT TRACK CORRODED AT BS 1030, RBL 24. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED. A REPAI R WAS INSTALLED IAW SRM 51-30-2 AND MM 51-20-12. 2 L 7 3 4F A3WE 1998090401035 19980904 01035 WP 1998 9 4 9810039990 1 19980828 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 149 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8950E 47186 DURING H-CHECK, FOUND CORROSION ON FLOOR WEB AT FS 149, RBL 4.5 INCHES UNDER FLOOR PANEL NR 13. REPAIRED PER EA 99-1596 93. 2 L 7 2 4F A6WE 1998090401036 19980904 01036 WP 1998 9 4 9810041155 1 19980714 A 5320 ANGLE DOUG DC10 DC1040 3023508 WP BS 1708 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 155US 46764 DURING M-CHECK, FOUND LOWER CHORD ANGLE CORRODED ON INBOARD END. REPAIRED PER EA 11-158027. 2 L 7 3 4F A22WE 1998090401037 19980904 01037 SO 1998 9 4 COMA9810187 1 19980830 A 3230 PIN EMB 120 EMB120RT SO NLG INSTALLED A COMA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 SO 01 263CA 120255 NLG DID NOT RETRACT. REMOVED NLG DOWN LOCK SAFETY PIN. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1998090401038 19980904 01038 SO 1998 9 4 COMA9810188 1 19980830 A 3411 PITOT TUBE EMB 120 EMB120RT SO LT SYSTEM LOOSE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 259CA 120252 A 40 KT DIFFERENCE BETWEEN PILOT AND CO-PILOT AIRSPEED INDICATION. TIGHTENED LOOSE CONNECTION AT FRAME 8 IN PILOTS PITO T SYSTEM. LEAK CHECK SATISFACTORY. 2 L 7 2 4T RT A31SO 1998090401039 19980904 01039 EA 1998 9 4 COMA9860246 1 19980831 A 3230 7179015 RETRACT MECH CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 709CA 7238 LANDING GEAR DID NOT RETRACT WHEN SELECTED UP. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE GEAR SELECTOR HANDLE FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1998090401040 19980904 01040 NM 1998 9 4 UPS98427585 1 19980831 A 5330 SKIN BOEING 747 747121 1384871 NM BS 860 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-N/A, APPROX 4 INCH CRACK ON BELLY SKIN LAP SEAM, LEFT SIDE STA 860 UNDER FILLET PANEL. ABOVE ITEM TO BE ACCOMPLISHED WITH EO B747-5330-10196-A. 2 L 7 4 4F A20WE 1998090401041 19980904 01041 NM 1998 9 4 UPS98427586 1 19980830 A 5330 SKIN BOEING 747 747121 1384871 NM BS 480 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-N/A, FUSE SKIN CORRODED THRU AT STA 480 BETWEEN S47L AND S47R. REPAIRED IAW EO B747-5330-10196. 2 L 7 4 4F A20WE 1998090401042 19980904 01042 WP 1998 9 4 UPS98827582 1 19980816 A 5320 3641125502 FITTING DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, MAIN CABIN STA 759XC-46 AT TOP OF L/W TANK FLOORBEAM ATTACH FITTING CRACKED. REMOVED AND REPLACED CRACKED FITTING. 2 L 7 4 4F RT 4A25 1998090401043 19980904 01043 WP 1998 9 4 UPS98827583 1 19980806 A 5230 DOOR DOUG DC8 DC873F 302199F WP CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, AFT LOWER CARGO DOOR HAS CRACK ON FORWARD UPPER AREA. STOP DRILLED CRACK, FAB DOUBLER, ALODINE, P RIMED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 52-2-0, 52-4-1, 51-1-8, AND 51-1-11. 2 L 7 4 4F RT 4A25 1998090401044 19980904 01044 WP 1998 9 4 UPS98827584 1 19980806 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP CABIN CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, SEAT TRACK NR C AT POSITION NR 3 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW DC 8 SRM 51-3 -0. 2 L 7 4 4F RT 4A25 1998090401045 19980904 01045 WP 1998 9 4 MWEA98944 1 19980831 A 5320 59147923 PAN DOUG DC9 DC932 3022066 WP SERVICE DOORWAY CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 FOUND CHAFE DAMAGE ON AFT LAV TOILET SERVICE DOOR PAN. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F A6WE 1998090401046 19980904 01046 WP 1998 9 4 MWEA98945 1 19980830 A 2530 50226 OVEN DOUG DC9 DC932 3022066 WP GALLEY DIRTY A MWEA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 212ME 47701 THE LEFT OVEN STARTED TO SMOKE AND FLIGHT ATTENDANT TURNED OFF. MTC CLEANED AND OPS CHECKED OVEN. 2 L 7 2 4F A6WE 1998090401047 19980904 01047 WP 1998 9 4 MWEA98946 1 19980830 A 3260 DREF4286 LINKAGE DOUG DC9 DC932 3022066 WP NLG DISCONNECTED A MWEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 31 602ME 48133 THE STALL INDICATION FAILURE LIGHT CAME ON AUTO SPOILER DO NOT USE LIGHT WITH SMELL IN CABIN. PERFORMED AIR TURNBACK. M AINTENANCE FOUND GROUND SHIFT LINKAGE DISCONNECTED AND RECONNECTED. 2 L 7 2 4F A6WE 1998090401048 19980904 01048 NM 1998 9 4 DL73E981767 1 19980826 A 5330 SKIN BOEING 737 737247 138448D NM CARGO DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 DURING INSP OF THE C1 DOOR CUTOUT PER RTN OPN 8706, AN EXISTING DOUBLER WAS REMOVED TO ACCOMMODATE THE INSPECTION. UPON REMOVING THE DOUBLER, ADDITIONAL SKIN DAMAGE WAS FOUND. REPAIRED PER ERA 332066-14. 2 L 7 2 4F A16WE 1998090401049 19980904 01049 NM 1998 9 4 DL73E981768 1 19980826 A 5330 6545768134 SKIN BOEING 737 737247 138448D NM CARGO DOORWAY GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 239WA 23187 THE UPPER AFT PORTION OF THE C1 DOOR CUTOUT WAS FOUND TO HAVE A GOUGE APPROX 10.5 BY 2.5. REPAIRED PER ERA 332098-14. 2 L 7 2 4F A16WE 1998090401050 19980904 01050 NM 1998 9 4 DL72S981769 1 19980826 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 475DA 20752 FOUND LEFT OVERWING EMERGENCY EXIT LIGHT FWD POS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998090401051 19980904 01051 NM 1998 9 4 DL72S981770 1 19980826 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 475DA 20752 FIRST CLASS CEILING EMERGENCY LIGHT OUT. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998090401052 19980904 01052 NM 1998 9 4 DL72S981772 1 19980827 A 2781 SWITCH H1010272 BOEING 727 727232 1384082 NM NR 1 LE SLAT FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 401DA 21145 AMBER LEADING EDGE FLAP LIGHT WOULD NOT EXTINGUISH WHEN FLAPS WERE MOVED FROM 5 TO 2 DEGREES. REPLACED RETRACT SWITCH O N NR 1 SLAT ACTUATOR. 2 L 7 3 4F A3WE 1998090401053 19980904 01053 NM 1998 9 4 DL733981773 1 19980827 A 3230 LINE BACCH8A00250 BOEING 737 737347 1384647 NM RT MLG RUPTURED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 308WA 23441 LOST A-SYS HYD PRESS AND QTY JUST AFTER RAISING GEAR ON T/O. FOUND RT GEAR UP LINE TO ACT RUPTURED. REPLACED LINE, BOT H A-SYS CASE DRAIN CHECK OK. LEAK CHECKED PUMPS, CHECK OK. 2 L 7 2 4F RT A16WE 1998090401054 19980904 01054 NM 1998 9 4 DL757981775 1 19980827 A 2913 SEAL BOEING 757 757232 1384965 NM NR 1 ENGINE TORN A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 690DL 27585 LT HYD QTY EICAS MSG, STATUS PAGE SHOWED FLUID DECREASING. RAN THROUGH LOSS OF FLUID PROCEDURE. COULD NOT ISOLATE TO A NY SINGLE PUMP. WITH BOTH PUMPS OFF FLUID QTY DECREASED TO .14. FOUND TORN SEAL ON LEFT ENG HYD PUMP. REPLACED SEAL, RAN ENG, LEAK CK LEFT HYD SYSTEM. INSPECTED FILTERS AND NO METAL FOUND. 2 L 7 2 4F RT A2NM 1998090401055 19980904 01055 NM 1998 9 4 DL72S981776 1 19980827 A 3350 BATTERIES S016 BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8873Z 21291 2L DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES. 2 L 7 3 4F A3WE 1998090401056 19980904 01056 NM 1998 9 4 DL73K981778 1 19980827 A 5330 SKIN BOEING 737 737232 1384475 NM BS 520 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 301DL 23073 A CRACK WAS FOUND IN THE SKIN AT FS 520 AND STR 16L. THE UNDERLYING STRINGER WAS FOUND WITH A TYPICAL CRACK AT THE END OF THE STRINGER AS OUTLINED IN BAC S/B 737-53-1145. THE SKIN WAS REPAIRED WITH AN EXTERNAL DOUBLER PER SRM PROCEDURE AN D THE STRINGER WAS REPAIRED PER THE S/B. THE REPAIR WAS DOCUMENTED PER ER/A 365541-14. 2 L 7 2 4F RT A16WE 1998090401057 19980904 01057 NM 1998 9 4 DL72S981779 1 19980826 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1067 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 538DA 22076 THE FUSELAGE SKIN AT FS 1067 WAS FOUND DENTED JUST O/B OF STRINGER 29R. THE DAMAGE WAS ADJACENT TO AND EXISTING DOUBLER REPAIR FOR ANOTHER SKIN CUTOUT. THE DENT WAS CUT OUT OF THE SKIN, THE EXISTING DOUBLER REMOVED, AND A NEW EXTERNAL ALU MINUM DOUBLER WAS INSTALLED TO REPAIR BOTH CUTOUTS. THE REPAIR WAS ACCOMPLISHED PER ER/A 365529-14, REV A. 2 L 7 3 4F A3WE 1998090401058 19980904 01058 NM 1998 9 4 DL72S981780 1 19980828 A 3230 1U1085 VALVE BOEING 727 727225 1384077 NM RT MLG CRACKED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 8875Z 21293 AIR RETURN, HYD FAILURE RT MAIN GEAR UPLOCK SEQUENCING VLV. HOUSING CRACKED. REPLACED VALVE. 2 L 7 3 4F A3WE 1998090401059 19980904 01059 NM 1998 9 4 DL72S981781 1 19980826 A 5312 6516350371 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 403DA 21147 TWO CRACKS OF .75 INCH LENGTH OR LESS WERE FOUND IN THE FS 1183 BULKHEAD WEB AT RBL 18 BETWEEN WL 166 AND 169 AND ONE .3 75 INCH CRACK WAS FOUND IN THE WEB AT LBL 25, WL 169. THE CRACKS WERE REPAIRED WITH A DOUBLER PER ER/A 365537-14 AND SE T UP FOR REPETITIVE INSPECTIONS UNTIL ACCOMPLISHMENT OF PERMANENT S/B MODIFICATIONS PRIOR TO 60,000 TOTAL AIRCRAFT CYCLE S. 2 L 7 3 4F A3WE 1998090401060 19980904 01060 NM 1998 9 4 DL72W981782 1 19980824 A 5320 651751090 CHORD BOEING 727 727247 138408F NM BS 1274 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 THE 65-17510-90 INNER CHORD OF THE VENTRAL STAIRWAY TORQUE BOX WAS FOUND WITH A CRACK AT FS 1274. THE CRACK IS TYPICAL OF BAC S/B 53-0129. THE CRACKED CHORD WAS REPAIRED WITH A REPAIR ANGLE AND STRAPS PER THE PROCEDURES OUTLINED IN THE B AC S/B. THE REPAIR WAS DOCUMENTED PER ER/A 365521-14AD. 2 L 7 3 4F A3WE 1998090401061 19980904 01061 NM 1998 9 4 DLM88981783 1 19980825 A 5330 29524621 SKIN DOUG MD88 MD88 3023688 NM BS 245 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 936DL 49723 THE FUSELAGE SKIN WAS FOUND CORRODED AROUND THE TCAS ANTENNA CUTOUT BETWEEN FS 237 AND 256 OVER STRINGERS 29L AND 30. T HE TCAS STRUCTURE WAS REMOVED AND THE SKIN CUT OUT OVER A 17.5 X 14.5 AREA. AN EXTERNAL ALUMINUM REPAIR DOUBLER AND INT ERNAL FINGER DOUBLERS WERE INSTALLED TO REPAIR THE CUT OUT PER ER/A 365510-14. THE TCAS STRUCTURE WAS RE-INSTALLED AFTE R THE REPAIR. 2 L 7 2 4F RT A6WE 1998090401062 19980904 01062 NM 1998 9 4 DL757981785 1 19980828 A 3230 273N20873 VALVE BOEING 757 757232 1384965 NM LT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 637DL 23760 LANDING GEAR WOULD NOT COME UP AFTER TAKEOFF. HANDLE WENT TO OFF, BUT WOULD NOT GO TO UP. GREEN GEAR LIGHTS STAYED ON. REPLACED LT MAIN GEAR TRUCK POSITIONING SHUTTLE VALVE. 2 L 7 2 4F RT A2NM 1998090401063 19980904 01063 NM 1998 9 4 DLM11981786 1 19980828 A 3350 6044113 POWER SUPPLY DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 805DE 48476 NR 3 EMERGENCY BATTERY PACK TESTED LOW DURING SYSTEM MAINT TEST. REPLACED POWER SUPPLY. 2 L 7 3 4F RT A22WE 1998090401064 19980904 01064 NE 1998 9 4 DLL10981789 2 19980829 A 7530 MR102MM8 SLAVE RAM LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 1 ENGINE DEFECTIVE A DALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 27 722DA 10658 193C1147 10658 NR 1 THROTTLE FAILED TO DEVELOP T/O THRUST WITH HIGH N2. REPLACED NR 1 ENG MASTER AND SLAVE RAM, RAN PER PFHB TEST NR 4 ALL CKS NORMAL. 2 L 7 3 4F 4 F A23WE E12EU 1998090401065 19980904 01065 NM 1998 9 4 DL72S981790 1 19980829 A 2150 SWITCH 694859832 BOEING 727 727232 1384082 NM COCKPIT INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 520DA DL60 21471 RT PACK SWITCH FAULTY. INFLT BUMPED SWITCH TO INTERMEDIATE POS, CAUSING PACK TO NOT OPERATE AT FL 330. PAC APPEARED TO BE ON, BUT ACTUALLY WAS OFF. RESULT WAS DEPRESSURIZATION TO ABOVE 10,000 FT, CABIN ALT O2 DROPPED. CABIN ALT REGAINED IN STBY MODE AND SWITCH PHYSICALLY PUSHED UP. FOUND RT PACK SWITCH FAULTY, REPLACED AIR COND CONTROL PANEL. RAN PACS AND PRESSURIZED A/C TO 7 PSI. CABIN LK CK GOOD. STOWED AND RESET O2 SYSTEM. 2 L 7 3 4F A3WE 1998090401066 19980904 01066 NM 1998 9 4 DL73E981791 1 19980829 A 3350 BATTERY PACK 20131A BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 375DL 23602 MID AISLE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F A16WE 1998090401067 19980904 01067 NM 1998 9 4 DLM88981792 1 19980828 A 3350 POWER SUPPLY RPS1 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 904DL 0762 49535 AFT PATH LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 1998090401068 19980904 01068 NM 1998 9 4 DL73K981793 1 19980829 A 3350 POWER SUPPLY BPS73 BOEING 737 737232 1384475 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 316DL 3588 23088 MID PATH LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A16WE 1998090401069 19980904 01069 NM 1998 9 4 DL73S981794 1 19980830 A 2742 ACTUATOR R1631 BOEING 737 737232 1384475 NM STAB TRIM FAILED A DALA L ABORTED APPROACH F FLT CONT AFFECTED LD LANDING 1 SO 27 330DL 840203 23102 RUNAWAY STAB TRIM ON SHORT FINAL. GO-AROUND MADE. REPLACED STAB TRIM ACTUATOR. 2 L 7 2 4F RT A16WE 1998090401070 19980904 01070 NM 1998 9 4 DL76L981796 1 19980830 A 3350 0201720001 LIGHT BOEING 767 767332 1382001 NM CABIN MISSING A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 197DN 28454 EMERGENCY ESCAPE PATH LIGHT (1 WHITE) MISSING AT SEAT 10B. REPLACED MISSING LIGHT ASSY AT 10B, OPS CKS GOOD. 2 L 7 2 4F RT A1NM 1998090401071 19980904 01071 NM 1998 9 4 DLM88981797 1 19980830 A 3350 LIGHT P2070003 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 49543 FWD FLASHLIGHT AT THE AFT FLIGHT ATTENDANT STATION INOP. REPLACED FLASHLIGHT ASSY AND BATTERY. 2 L 7 2 4F RT A6WE 1998090401072 19980904 01072 NM 1998 9 4 DL72S981798 1 19980724 A 5753 652163262 SPAR BOEING 727 727232 1384082 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 AFT SPAR RAIL CRACKED 37 INCHES FROM I/B END OF FLAP. REPAIRED ON SO 529555 PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998090401073 19980904 01073 NM 1998 9 4 DLM88981799 1 19980828 A 3350 POWER SUPPLY RPS1 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 940DL 762 49813 AFT CABIN EMERGENCY TRACK LIGHTING INOP. REPLACED REAR PATH LIGHTING POWER SUPPLY, OPS CK NORMAL. 2 L 7 2 4F RT A6WE 1998090401074 19980904 01074 1998 9 4 DL767981800 4 19980830 A 3418 RVDT 3A1260A BOEING 767 767232 1385132 NM LT WING INTERMITTANT A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 105DA 0054 22217 AFTER TAKEOFF, L/E CAUTION AND L/E SLAT ASSY EICAS MSG. RETURNED TO LAX. REPLACED M548 RVDT PER MM, ALL OPS NORMAL. 2 L 7 2 4F RT A1NM 1998090401075 19980904 01075 NM 1998 9 4 DL72S981805 1 19980831 A 2121 215201 FAN BOEING 727 727232 1384082 NM COCKPIT FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 416DA 21258 SMOKE AND FUMES IN COCKPIT AND CABIN, RAN CK LIST AND COULD NOT FIND SOURCE. ALSO, ELECTRICAL BURNT PLASTIC SMELL. INS PECTED COALESCER BAGS, CKS GOOD. INSPECTED E & E AREA, CKS GOOD. INSPECTED GALLEY AREA, CKS GOOD. FOUND SMELL COMING FROM GASPER FAN, RAN PACKS W/ENGINES AND GASPER FAN OFF. NO BURNING SMELL. FWD GASPER FAN TO MCO PER MEL 21-00-24. PU LLED AND COLLARED C/B. REPLACED GASPER FAN. 2 L 7 3 4F A3WE 1998090401076 19980904 01076 NM 1998 9 4 DHL9872178D 1 19980708 A 7110 COWL BOEING 727 727228 NM NR 3 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 721DH 19545 AT D-CHECK, NR 3 ENG LOWER COWL INT SKIN IS DENTED JUST I/B OF GENERATOR EXHAUST PORT AT AFT END. CUT OUT DAMAGED SECTI ON, INSTALLED REPAIR PER SRM 54-10-3, 8.5 X 7. N/R 6526. 2 L 7 3 4F A3WE 1998090401077 19980904 01077 NM 1998 9 4 P5CA9801369 1 19980827 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1368-1371 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL OUTBOARD STRINGER BS 1368 TO 1371 STR R33. CORROSION REMOVED PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998090401078 19980904 01078 NM 1998 9 4 P5CA9801370 1 19980827 A 5720 BEAM BOEING 747 747123 1384873 NM BS 280 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEFT WING TRAILING EDGE BEAM UPPER CHORD INBOARD END CRACKED. REPAIRED PER SRM 51-40-14 FIG 2. 2 L 7 4 4F A20WE 1998090401079 19980904 01079 NM 1998 9 4 P5CA9801371 1 19980827 A 5730 SKIN BOEING 747 747123 1384873 NM WS 586 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION FOUND ON LEFT WING UPPER SKIN AT REAR SPAR AREA. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998090401080 19980904 01080 NM 1998 9 4 P5CA9801372 1 19980827 A 5320 BRACKET BOEING 747 747123 1384873 NM BS 1352 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL WELL BRACKET AT BS 2352L WL 160. REMOVED CORROSION PER SRM 51-10-01 AND 5 1-10-02. 2 L 7 4 4F A20WE 1998090401081 19980904 01081 NM 1998 9 4 P5CA9801373 1 19980827 A 5320 BEAM BOEING 747 747123 1384873 NM BS 1352 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION ON RT BODY GEAR WW OUTBOARD BEAM BS 1352 TO 1353 BL R70-R80. CORROSION REMOVED PER SRM 51-10-01 AND 5 1-10-02. 2 L 7 4 4F A20WE 1998090401082 19980904 01082 NM 1998 9 4 P5CA9801374 1 19980827 A 5320 BRACKET BOEING 747 747123 1384873 NM BS 1380R CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION FOUND ON RT BODY GEAR WW VALVE SUPPORT BRACKET. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998090401083 19980904 01083 NM 1998 9 4 P5CA9801375 1 19980827 A 5320 ANGLE BOEING 747 747123 1384873 NM BS 1373 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION FOUND ON RT BODY GEAR WHEEL OUTBOARD CHORD ANGLE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998090401084 19980904 01084 NM 1998 9 4 P5CA9801376 1 19980827 A 5314 KEEL BEAM BOEING 747 747123 1384873 NM BS 1290-1280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 859FT 20326 LEVEL 1 CORROSION FOUND ON RT WING GEAR WHEEL WELL INBOARD KEEL BEAM UPPER SURFACE. REMOVED CORROSION PER SRM 51-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998090401085 19980904 01085 NE 1998 9 4 P5CA9801377 2 19980830 A 7230 COMPRESSOR BOEING 747 747124 1384874 NM PWA JT9 JT9D7A 52054 NE ENGINE STALLED A P5CA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 23 855FT 19733 ON TAKEOFF ROLL, A LOUD BANG OCCURRED AT SPEED OF 80 KNOTS. RETURNED TO BLOCKS. VISUAL INSPECTION OF ALL ENGINE INTAKE S, AND EXHAUST PER MM 72-00-00, FOUND NOTHING. CHECKED EXTERIOR OF A/C AND FOUND NOTHING ABNORMAL. AIRCRAFT DEPARTED O N TIME. 2 L 7 4 4F 4 F A20WE E20EA 1998090401086 19980904 01086 NM 1998 9 4 VNAA9808026 1 19980828 A 3150 TRIM WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ELEVATOR ACTIVATED A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 GL 07 457PS 3048 THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE, FOLLOWING A TAKEOFF CONFIG FAIL WARNING MESSAGE. THE CREW SUSPEC TED THAT AN UNCOMMANDED ELEVATOR TRIM CHANGE CAUSED THE EVENT. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS O F THE ELEVATOR TRIM SYSTEM. ALSO A HIGH SPEED TAXI CHECK WAS COMPLETED. NO DEFECTS WERE FOUND IN ACCORDANCE WITH DORNI ER MAINTENANCE MANUAL 27-32-00, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998090401087 19980904 01087 WP 1998 9 4 CKSA98508 1 19980828 A 3610 DUCT DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE LOOSE A CKSA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 GL 23 6161C 45856 644999 ON CLIMBOUT APPROXIMATELY 2,000 FT, NR 1 ENGINE FIRE WARNING CAME ON. DURING POWER LEVER REDUCTION LIGHT EXTINGUISHED. PERFORMED ENGINE FIRE CHECKLIST, SHUTDOWN NR 1 ENGINE, NO FIRE BOTTLES USED. NR 1 ENGINE FIRE LIGHT TESTED OK. OIL PR ESSURE 15 PSI AFTER SHUTDOWN. SECURED LOOSE PNEUMATIC DUCTING AND CLEANED DIRTY CONNECTOR ON FIRE LOOP. RAN ENGINE THR EE TIMES TO TAKEOFF POWER FOR 5 MINS EACH TIME WITH NO FIRE WARNING FAULT. CONFIRMED FIRE WARNING SYSTEM TEST NORMAL IA W DC8 MM 26-2-0. 2 L 7 4 4F 4 F 4A25 1E8 1998090401088 19980904 01088 WP 1998 9 4 98ZZZX3204 1 19980529 A 5310 STRUCTURE DOUG DC9 DC983 3022083 WP FUSELAGE DAMAGED A AJLF O OTHER C F.O.D. IN INSP/MAINT 1 SO 23 191AJ 53191 UVF/MBJ - FLT JM 090 - WHILE AIRCRAFT WAS PARKED DURING TRANSIT, IT WAS HIT AT THE FORWARD LEFT-HAND SIDE IN THE VACINIT Y OF THE TOILET SERVICE PANEL BY A TOILET SERVICE TRUCK. A DENT MEASURING .75 INCH DEEP AND 3 INCHES BY 4 INCHES WAS RE PAIRED IAW AIRCRAFT SRM CHAPTER 53-04, PAGE 35. UPON COMPLETION OF THE NECESSARY CHECKS/INSPECTION, THE AIRCRAFT WAS RE LEASED FOR FURTHER SERVICE. 2 L 7 2 4F RT A6WE 1998090401089 19980904 01089 EU 1998 9 4 98ZZZX3205 1 19980615 A 5414 SKIN AIRBUS 320 A320214 EU NR 1 NACELLE DAMAGED A AJLF K NONE O OTHER IN INSP/MAINT 1 SO 23 626AJ 626 MIA/MBJ - FLT JM 036 - ON WALK-AROUND INSPECTION, BIRD STRIKE FOUND ON NR 1 ENGINE. NO REPORT OF ABNORMAL ENGINE PARAME TERS. THE FOLLOWING STEPS, HOWEVER, WERE TAKEN: BIRD STRIKE INSPECTION CARRIED OUT PER AMM CHAPTER 72-00-00, PAGES 601 -606. THERE WAS NO EVIDENCE OF ENGINE DAMAGE. ALSO, BORESCOPE INSPECTION WAS CONDUCTED IAW AMM CHAPTER 72-31-00. THIS REVEALED SATISFACTORY. RESULTS. 2 L 7 2 4F RT A28NM 1998090401091 19980904 01091 CE 1998 9 4 98ZZZX3207 1 19980611 A 7797 WIRE CESSNA 402 402C 207590R CE RT ENGINE CHAFED A BQTA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 NE 05 402ME 402C0010 THE PILOT MADE A PRECAUTIONARY LANDING AT THE ROCHESTER, NY AIRPORT AS THE RIGHT HAND ENGINE'S CYLINDER HEAD TEMPERATURE BEGAN TO FLUCTUATE AND EVENTUALLY FELL TO ZERO BEFORE LANDING. AN INSPECTION OF THE ENGINE'S BAFFLING, EXHAUST MANIFOL D, AND CYLINDERS REVEALED NO ABNORMALITIES. FURTHER INSPECTION REVEALED A CHAFED WIRE ADJACENT TO THE EXHAUST HEADER HE AT SHIELD, THE 22 GAUGE AIRFRAME CHT INDICATION SYSTEM WIRE WAS SPLICED USING A SP0704 INSULATED SPLICE CONNECTOR, EGT S YSTEM OPERATION, AND INDICATIONS WERE OPS CHECKED AND FOUND NORMAL. 1 L 7 2 3O A7CE 1998090401092 19980904 01092 CE 1998 9 4 98ZZZX3208 1 19980603 A 8011 EQ6642 SPRING CESSNA 402 402C 207590R CE RT ENG STARTER BROKEN A BQTA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 NE 05 402ME 1500 402C0010 THE RIGHT ENGINE OIL PRESSURE DROPPED INTO THE YELLOW ARC DURING FLIGHT. THE AIRCRAFT MADE A PRECAUTIONARY LANDING (DID NOT SHUT DOWN ENGINE). INVESTIGATION REVEALED THE SPRING BROKE IN THE STARTER ADAPTER AND PIECES BECAME LODGED UNDER T HE RELEIF VALVE. THE START ADAPTER WAS REPLACED. FLUSHED OIL SYSTEM, OPENED FILTER AFTER GROUND RUN FOR 30 MINUTES. N O METAL NOTED IN FILTER. 1 L 7 2 3O A7CE 1998090401093 19980904 01093 SO 1998 9 4 C2XA98IA274 1 19980718 A 2740 701700082404 COMPUTER EMB 145 EMB145 SO COCKPIT MALFUNCTIONED A C2XA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SW 09 14947 145054 LFT - FLT 4129 - THE PILOT REPORTED AN UNCOMMANDED PITCH-TRIM ON TAKEOFF. THE ACFT LANDED AT LFT WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER CONTROL UNIT AND WAS RELEASED BACK TO SERVICE. THE UNCOMMAN DED PITCH-TRIM FAULT RECURRED ON THE GROUND AT AMA ON 7-20-98, FLT 4210. MAINTENANCE REMOVED AND REPLACED THE NR 1 IC60 0 COMPUTER, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. NO FURTHER INCIDENTS HAVE BEEN REPORTED TO-DATE. (X) 2 L 7 2 4F RT T00011AT 1998090401094 19980904 01094 NE 1998 9 4 JBXA980038 2 19980520 A 7320 CONNECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE NR 2 ENGINE DIRTY A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 572ML 7224 AT FL 240, AND 300 KIAS, NR 2 ENGINE N1 ADVANCED TO 101 PERCENT RPM AND AIRFRAME RUMBLE OCCURRED. PULLED POWER TO IDLE, INDICATIONS. RETURNED TO NORMAL. LEFT POWER AT IDLE AND LANDED. N2 AND ITT WERE RISING WITH N1. INSPECTED NR 2 ENGIN E IAW AMM 71-00-00 FAN ROTOR (N1) OVERSPEED LIMITS AREA B SUB A TABLE 503. NO DEFECTS NOTED AT THIS TIME. DISCONNECTED NR 2 ENGINE ALTERNATOR STATOR HARNESS, INSPECTED AND CLEANED HARNESS. RECONNECT IAW AMM 73-21-07. PERFORMED ENGINE RUN , N1 SPEED CONTROL, AMPLIFIER DISABLE CHK, APR OPS CHECK AND POWER ASSURANCE CHK IAW AMM 71-00-00. OPERATIONAL CHK GOOD , NO FAULTS NOTED. (X) 2 L 7 2 4F 4 F RT A21EA E15NE 1998090401095 19980904 01095 CE 1998 9 4 98ZZZX3209 1 19980603 A 3260 ISEI3 SWITCH 50410011 CESSNA 402 402A 207590M CE RT MLG LACK OF LUBE A KCQA O OTHER N FALSE WARNING LD LANDING 1 GL 13 727CA 16195 402A0102 LANDING GEAR RIGHT MAIN WOULD NOT INDICATE DOWN AND LOCK. RIGHT SIDE LANDING MAIN GEAR DOWN AND LOCKED LIGHT WOULD NOT ILLUMINATE. ON TOUCH DOWN, GEAR LIGHT ILLUMINATED. LUBED, CLEANED, AND CHECKED GEAR, FOUND OK. 1 L 7 2 3O A7CE 1998090401096 19980904 01096 EU 1998 9 4 SIMA981392 1 19980519 A 3350 3013017 BATTERY AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 538AT 0609 538 IND - EMERGENCY LIGHTS INOPERATIVE. REPLACED ONE POWER SUPPLY AND BATTERY. OPERATIONAL CHECK PERFORMED SATISFACTORILY. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998090401097 19980904 01097 EU 1998 9 4 SIMA981687 1 19980617 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 0604 540 GRR - SOME EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACKS FOR POWER SUPPLIES 62 AND 73 WL . OPERATIONAL CHECK GOOD. REF: OPERATOR CONTROL NR 98ZZZX3210. 2 H 7 2 4T RT A53EU 1998090401098 19980904 01098 EU 1998 9 4 98ZZZX3210 1 19980617 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 540AM 0597 540 GRR - SOME EMERGENCY FLOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACKS FOR POWER SUPPLIES 62 AND 73 WL . OPERATIONAL CHECK GOOD. REF: OPERATOR CONTROL NR SIMA981687. 2 H 7 2 4T RT A53EU 1998090401099 19980904 01099 EU 1998 9 4 SIMA981673 1 19980612 A 3350 167006 BULB AEROSP ATR72 ATR72212A 8680902 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 548 ORD - FLT 4083 - FLOOR PROXIMITY LIGHT ADJACENT TO SEAT 13B DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB AT 13B. OPE RATIONAL CHECK GOOD. MEL NR 060144 CLEARED. (X) 2 H 7 2 4T RT A53EU 1998090401100 19980904 01100 EU 1998 9 4 SIMA981942 1 19980713 A 3350 6013211 POWER SUPPLIES GRIMES SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 18301 340B319 DFW - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND INSPECTED POWER SUPPLIES AT POSITION 122AZ, 161AZ, 131CT, 141AZ, 141BZ IAW SAAB AMM. PERFORMED OPERATIONAL CHECK SATISFACTORILY A ND RETURNED AIRCRAFT TO SERVICE. REF: OPER CNTRL NR 98ZZZX3211 THROUGH 98ZZZX3214. (X) 2 L 7 2 4T RT A52EU 1998090401101 19980904 01101 EU 1998 9 4 98ZZZX3211 1 19980713 A 3350 6013211 POWER SUPPLIES GRIMES SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 18303 340B319 DFW - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND INSPECTED POWER SUPPLIES AT POSITION 122AZ, 161AZ, 131CT, 141AZ, 141BZ IAW SAAB AMM. PERFORMED OPERATIONAL CHECK SATISFACTORILY A ND RETURNED AIRCRAFT TO SERVICE. REF: OPER CNTRL NR SIMA981942, AND, 98ZZZX3212 THROUGH 98ZZZX3214. 2 L 7 2 4T RT A52EU 1998090401102 19980904 01102 EU 1998 9 4 98ZZZX3212 1 19980713 A 3350 6013211 POWER SUPPLIES GRIMES SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 19500 340B319 DFW - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND INSPECTED POWER SUPPLIES AT POSITION 122AZ, 161AZ, 131CT, 141AZ, 141BZ IAW SAAB AMM. PERFORMED OPERATIONAL CHECK SATISFACTORILY A ND RETURNED AIRCRAFT TO SERVICE. REF: OPER CNTRL NR SIMA981942, AND, 98ZZZX3211 THROUGH 98ZZZX3214. 2 L 7 2 4T RT A52EU 1998090401103 19980904 01103 EU 1998 9 4 98ZZZX3213 1 19980713 A 3350 6013211 POWER SUPPLIES GRIMES SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 18317 340B319 DFW - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND INSPECTED POWER SUPPLIES AT POSITION 122AZ, 161AZ, 131CT, 141AZ, 141BZ IAW SAAB AMM. PERFORMED OPERATIONAL CHECK SATISFACTORILY A ND RETURNED AIRCRAFT TO SERVICE. REF: OPER CNTRL NR SIMA981942, AND, 98ZZZX3211 THROUGH 98ZZZX3214. 2 L 7 2 4T RT A52EU 1998090401104 19980904 01104 EU 1998 9 4 98ZZZX3214 1 19980713 A 3350 6013211 POWER SUPPLIES GRIMES SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 905AE 18976 340B319 DFW - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS ILLUMINATED INTERMITTENTLY. REMOVED AND INSPECTED POWER SUPPLIES AT POSITION 122AZ, 161AZ, 131CT, 141AZ, 141BZ IAW SAAB AMM. PERFORMED OPERATIONAL CHECK SATISFACTORILY A ND RETURNED AIRCRAFT TO SERVICE. REF: OPER CNTRL NR SIMA981942, AND, 98ZZZX3211 THROUGH 98ZZZX3213. 2 L 7 2 4T RT A52EU 1998090401105 19980904 01105 NM 1998 9 4 TWAA9811501 1 19980716 A 5730 PANEL BOEING 757 7572Q8 1384972 NM LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 704X 28163 DURING CK-C01, FOUND LT WING TOP L/E PANEL AT OTBD END OF NR 4 L/E SLAT HAS A 7 INCH CRACK. DRESSED OUT DAMAGED AREA AN D INSTALLED HOT BOND REPAIR PER SRM 51-70-07 PG 40 AND SRM 57-41-01 PG 20. (X) 2 L 7 2 4F RT A2NM 1998090401106 19980904 01106 WP 1998 9 4 TWAA9811004 1 19980707 A 5230 SKIN DOUG DC9 DC983 3022083 WP CARGO DOOR DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9615W 53562 MCI - DURING CHECK-C, MAINTENANCE FOUND FORWARD CARGO DOOR, OUTSIDE AT HANDLE, HAD DENT AND PRY MARK. DENT 2 INCHES ACR OSS BY .75 INCH BY 0.187 INCH DEEP. REPAIRED DENT PER SRM 52-05, PAGE 159, INSTALLING CRES STEEL SCUFF PLATE TO HANDLE AREA USING HILOKS, WASHERS AND NUTS, AND SEALING. (X) 2 L 7 2 4F RT A6WE 1998090401107 19980904 01107 1998 9 4 VTZA98228 4 19980627 A 2213 COMPUTER CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 627BR 7233 IAD/BNA - FLT 6704 - DURING CRUISE AT 1755 HRS ON 6-27-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO ALTITUDE ALERT SO UNDED CONTINUOUSLY. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED CHECKED OF FCC SYSTEM AND COULD NOT DUPLICATE PROBLEMS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998090401108 19980904 01108 NE 1998 9 4 98ZZZX3215 2 19980329 A 7250 212107135 SPACER CNDAIR CL600 CL6001A11 1900302 EA LYC ALF502 ALF502L2 41580 NE NR 1 ENGINE MISINSTALLED A UWUA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NE 03 818TH 4204 1069 LF031195 HPN - NORMAL TAKEOFF EN ROUTE BAHAMAS. APPROX 1 HR EN ROUTE AT FL 310, PILOT NOTED NR 1 ENG VIBRATION INCREASE FROM .3 M/S TO .6 M/S AND INCREASE IN ENG NOISE. ALL OTHER ENG INDICATIONS WITHIN NORMAL PARAMETERS. ENG NOISE SUBSIDED THEN I NCREASE IN ENG VIBRATION FROM .6 M/S TO .9 M/S, WITHIN NORMAL LIMITS. PILOT DISCONTINUED FLT, PRECAUTIONARY LANDING AT ISP. BORESCOPE INSP REVEALED NR 2 TURB DISC DAMAGE. ENG REMOVED AND REPLACED. UPON ENG DISASSY AND REPAIR, ALLIED SI GNAL NOTED A GAS PRODUCER SPACER WAS INSTALLED. SPACER CONFIG IS NOT COMPATIBLE WITH ALF502L-2C ENGINES AND THEY SUSPEC T ENG DAMAGE A DIRECT RESULT OF INSTALL OF INCORRECT GAS PRODUCER SPACER CONFIG. ENG REPAIRED AND RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E6NE 1998090401109 19980904 01109 EA 1998 9 4 VTZA9821D 1 19980605 A 3030 AOA HEAT CNDAIR CL600 CL6002B19 EA LT WING FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 625BR 7214 IAD/BNA - FLT 6700 - DURING CRUISE AT 0830 HRS ON 6-5-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT AOA HEAT INOPER ABLE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM, OPS C HECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998090401110 19980904 01110 EU 1998 9 4 98ZZZX3216 1 19980710 A 5753 BRACKET 257WF3AB BRAERO DH125 HS125700A 4230170 EU LT TE FLAP CRACKED A L KKYA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 NE 03 81KA 11152 DHB75 NA0227 PN POST-FLIGHT AT OXC, FOUND LT WING SHROUD BENT, THE FLAP VANE MISSING, AND THE TWO BRACKETS THAT ATTACH THE VANE TO TH E FLAP WERE BROKEN. THE AIRCRAFT HAD A 48 MONTH 2400 HOUR INSPECTION IN 1-98 AND THE FLAPS AND VANES WERE X-RAYED AT TH AT TIME. WILL REVIEW THE X-RAYS AND SEE IF THIS PARTICULAR AREA WAS INCLUDED. THESE FINDINGS WILL COME IN A FOLLOW-UP REPORT WHEN THE RESEARCH IS COMPLETE. 2 L 7 2 4F A3EU 1998090401111 19980904 01111 NM 1998 9 4 AALA981297 1 19980629 A 3210 654T00083 MLG BOEING 767 767323 1385205 NM LEFT FAILED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 374AA 25201 ORD - FLT 0037 - ON TAKEOFF UPON RAISING THE GEAR, THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. FOLLOWED ABNORMAL PROCEDURES. THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED EVEN WHEN THE GEAR WAS DOWN AND LOCKED. GEAR WAS LEFT IN THE DOWN AND LOCKED POSITION AND AN EMERGENCY LANDING AT ORD WAS ACCOMPLISHED WITHOUT INCIDENT. REPLACED MLG ASSY. SW UNG GEAR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401112 19980904 01112 WP 1998 9 4 AALA981370 1 19980713 A 3350 HARNESS DOUG DC9 DC982 3022082 WP TAIL CONE FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 242AA 49255 DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN TAIL CONE INOPERATIVE. REPLACED UPPER POWER HARNESS ASSY. SYSTEM GROU ND CHECKED, NORMAL OPERATION. 2 L 7 2 4F A6WE 1998090401113 19980904 01113 WP 1998 9 4 AALA981371 1 19980712 A 2613 4TL1413D SENSORS DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 7522A 49899 DFW - FLT 1676 - AFTER TAKEOFF DFW, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. STAYED ON STEADY FOR ABOUT 30 SECONDS. ACCOMPLISHED EMERGENCY PROCEDURES CHECK LIST. THE LIGHT FLICKERED ON AND OFF FOR ABOUT 2 MINUTES. DECISI ON TO LAND BACK AT DFW WAS MADE AND THE LAST 7 MINUTES THERE WAS NO FURTHER INDICATION OF THE LIGHT. LANDED DFW WITHOUT INCIDENT. RAN ENGINES, APU AND PACKS AND COULD NOT DUPLICATE. CHECKED TAIL COMPARTMENT DUCTING FOR LEAKS, NO LEAKS NO TED. REPLACED BOTH TAIL COMPARTMENT TEMPERATURE SENSORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998090401114 19980904 01114 NM 1998 9 4 AALA981282 1 19980628 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372AA 25199 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 31H INOPERATIVE. RESET EMERGENCY EXIT SEAT LIGHT CONNE CTOR AT SEAT 31H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401115 19980904 01115 NM 1998 9 4 AALA981292 1 19980701 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTING AT SEATS 33H AND 39B INOPERATIVE. REPLACED EMERGENCY E XIT SEAT LIGHT CONNECTORS AT SIDEWALL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401116 19980904 01116 NM 1998 9 4 AALA981291 1 19980701 A 3350 HARNESS BOEING 767 767323 1385205 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354AA 24035 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTING AT SEAT 37H INOPERATIVE. RECONNECTED EMERGENCY EXIT SE AT LIGHT HARNESS AT SIDEWALL. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401117 19980904 01117 NM 1998 9 4 AALA981333 1 19980704 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 335AA 22333 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 23B WOULD NOT ILLUMINATE. SECURED LOSE EMERGENCY E XIT LIGHT CONNECTOR AT SEAT ROW 28B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401118 19980904 01118 NM 1998 9 4 AALA981388 1 19980715 A 3350 CONNECTOR PIN BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 320AA 22321 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTING AT SEAT 26B INOPERATIVE. RESECURED PUSHED BACK PIN AT SEAT HARNESS FOR EMERGENCY EXIT LIGHTING AT SEAT 26B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401119 19980904 01119 NM 1998 9 4 AALA981332 1 19980704 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 317AA 22319 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 30AB WOULD NOT ILLUMINATE. SECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT SEAT ROW 30AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401120 19980904 01120 NM 1998 9 4 AALA981281 1 19980628 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 315AA 22317 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 23H INOPERATIVE. RELOCKED EMERGENCY EXIT SEAT LIGHT CO NNECTOR AT SEAT 23H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401121 19980904 01121 NM 1998 9 4 AALA981294 1 19980630 A 3350 P4010051 MODULE BOEING 757 757223 1384957 NM CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659AA 24617 DFW - DURING OVERNIGHT MAINTENANCE, L2 DOOR EMERGENCY EXIT LIGHT OVERHEAD INOPERATIVE. RESEATED L2 DOOR OVERHEAD EMERGE NCY EXIT LIGHT ASSEMBLY MODULE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998090401122 19980904 01122 NM 1998 9 4 AALA981296 1 19980630 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659AA 24617 DFW - DURING OVERNIGHT MAINTENANCE, MID-GALLEY EMERGENCY EXIT LIGHT ASSEMBLY INOPERATIVE. REPAIRED WIRING ON EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998090401123 19980904 01123 NM 1998 9 4 AALA981403 1 19980718 A 3350 PR010051112 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 617AM BBGJFKJ 24525 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT MODULE INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT MODULE. S YSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998090401124 19980904 01124 NM 1998 9 4 AALA984163 1 19980717 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 764 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 371AA 25198 AFW - FLOORBEAM HAS CORROSION ON UPPER SURFACE. REMOVED ALL CORROSION. REFINISHED PER SRM 53-00-01. FILLED BLENDS WIT H BMS5-92. TST: 27,711.57 HOURS. CYCLES: 4,361. (X) 2 L 7 2 4F RT A1NM 1998090401125 19980904 01125 NM 1998 9 4 AALA981414 1 19980722 A 2530 2510000405 OVEN BOEING 767 767223 1385123 NM GALLEY DIRTY A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 321AA 22322 LHR - FLT 0092 - DURING CRUISE, FIRST CLASS RIGHT SIDE NR 2 OVEN SMOKED WHEN OVEN ON. DISCONTINUED USE OF OVEN. LANDED LHR WITHOUT INCIDENT. CLEANED FIRST CLASS RIGHT SIDE NR 2 OVEN. GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401126 19980904 01126 WP 1998 9 4 AALA981392 1 19980716 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3507A 49801 SAT - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 28 THROUGH 33 INOPERATIVE. REPLACED EMERGEN CY EXIT FLOOR LIGHT STRIP AND ONE CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998090401127 19980904 01127 WP 1998 9 4 AALA981393 1 19980716 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 492AA 49730 RDU - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS SECTION OF THE CABIN AND COACH TO THE EMERGENCY OVERWING EXIT INOPERATIVE. REPLACED SECTION OF EMERGENCY EXIT FLOOR PATH LIGHTING AT FORWARD SECTION OF C OACH AND BOTH BATTERY PACKS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998090401128 19980904 01128 WP 1998 9 4 AALA981425 1 19980723 A 3230 ARG7765511 CYLINDER DOUG DC10 DC1010 3022110 WP RT MLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 134AA CPT0113 47829 JFK - FLT 0015 - AFTER TAKEOFF JFK, EN ROUTE TO SFO, GEAR HANDLE WOULD NOT RAISE AND GEAR WOULD NOT RETRACT. ABNORMAL P ROCEDURE WAS FOLLOWED WITHOUT SUCCESS. RETURNED JFK AND LANDED WITHOUT INCIDENT. REPLACED RIGHT HAND GEAR LEVELING CYL INDER AND TRIM CYLINDER LOCK-OUT FUSE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A22WE 1998090401129 19980904 01129 NM 1998 9 4 AALA981401 1 19980717 A 5330 SKIN BOEING 727 727223 1384074 NM BS 500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 882AA 21521 TUL - REMOVED CORROSION. INSTALLED DOUBLER PER SRM 53-30-3 PAGE 12 FIGURE 3. TST: 52,996 HOURS. CYCLES: 32,076. (X ) 2 L 7 3 4F A3WE 1998090401130 19980904 01130 NM 1998 9 4 AALA981399 1 19980717 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 882AA 21521 TUL - BELLFRAME DAMAGED FROM CONTACT WITH SCREW AT TIE DOWN FITTING STA 1070, STR 27R. INSTALLED BELLFRAME REPAIR PER S RM 51-40-3 PAGES 1-6. TST: 52,996 HOURS. CYCLES: 32,076. (X) 2 L 7 3 4F A3WE 1998090401131 19980904 01131 NM 1998 9 4 AALA981400 1 19980717 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 620-626 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 882AA 21521 TUL - STR 27R CORRODED BETWEEN BS 620 - BS 626. REMOVED CORROSION PER 51-10-6 AND INSTALLED U-CHANNEL DOUBLER IN STR 27R FROM BS 620 - BS 626 PER ESO 11697 DATED 6-30-98. TST: 52,996 HOURS. CYCLES: 32,076. (X) 2 L 7 3 4F A3WE 1998090401132 19980904 01132 NM 1998 9 4 AALA981328 1 19980703 A 2752 MS9391130ZE4C DRIVE VICKERS BOEING 727 727223 1384074 NM RT TE FLAPS LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 897AA MX346749 22013 MIA - FLT 0733 - DURING CLIMB-OUT, CREW NOTICED SYSTEM A-HYDRAULIC QUANTITY DECREASED TO 1 GALLON AND WHEN ISOLATED, DEC REASED TO 1/4 GALLON FOLLOWED BY LOSS OF SYSTEM A-HYDRAULICS. AIRCRAFT AIR INTERRUPTED AND LANDED WITHOUT INCIDENT MIA. MAINTENANCE FOUND RT TRAILING EDGE FLAP DRIVE MOTOR LEAKING. REPLACED RT TRAILING EDGE FLAP DRIVE MOTOR AND SERVICED SYSTEM A-HYDRAULICS. FLAPS WERE CYCLED SEVERAL TIMES OPERATING NORMALLY WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED, NO RMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998090401133 19980904 01133 NE 1998 9 4 AALA981182 2 19980615 A 7261 799331 OIL PUMP BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LOOSE A AALA E A ENGINE SHUTDOWN UNSCHED LANDING K M FLUID LOSS OVER TEMP CR CRUISE 1 SW 07 860AA 21087 TPA - FLT 1029 - EN ROUTE DCA-MIA - AT 33,000 FEET, NR 1 OIL TEMP WENT INTO CAUTION ZONE AND OIL QTY DECREASED TO 1 GALL ON. OIL QTY CONTINUED TO DECREASE, OIL TEMP STAYED IN THE CAUTION FOR 15 MINUTES AND NR 1 ENGINE WAS SHUTDOWN. DELCARE D AN EMERGENCY AND DIVERTED TO TPA. LANDED TPA WITHOUT INCIDENT. REPLACED NR 1 ENGINE, SYSTEM GROUND CHECKED NORMAL OP ERATION. THE CAUSE FOR ENGINE REMOVAL AND SHUTDOWN WAS FAILURE OF THE 4/5 SCAVENGE PUMP. AT ENGINE TEAR DOWN, THE 4/5 SCAVENGE PUMP HOUSING ASSY MOUNTING BOLTS WERE FOUND LOOSE. FINDINGS DURING DISASSEMBLY REVEALED ONE EACH MOUNT BOLTS L YING IN THE NR 4 BEARING HOUSING WITH SAFETY WIRE BROKEN, AND THE OTHER TWO MOUNT BOLTS WERE HAND TIGHT. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998090401134 19980904 01134 NM 1998 9 4 AALA981330 1 19980703 A 2133 CLAMP BOEING 727 727223 1384074 NM SHUT OFF VALVE LOOSE A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 849AA 20990 BNA - FLT 0405 - DURING CLIMB-OUT PASSING FL 300, CREW NOTICED LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLI SHED EMERGENCY CHECK LIST, AIR INTERRUPTED AND LANDED BNA WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND AFT RIGHT CLAMP A T FLOW CONTROL SHUT-OFF VALVE LOOSE. TIGHTENED LOOSE CLAMP AT FLOW CONTROL SHUT-OFF VALVE. ACCOMPLISHED ENGINE RUN WIT H NO LEAKS NOTED. SYTSEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998090401135 19980904 01135 NE 1998 9 4 AALA981298 2 19980628 A 7261 391009 PACKING BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE NR 3 ENGINE DEFECTIVE A AALA A UNSCHED LANDING K M FLUID LOSS OVER TEMP CL CLIMB 1 SW 07 859AA 21086 666102 DFW - FLT 1614 - 10 MINS AFTER TAKEOFF DFW, WHILE ACCELERATING TO CLIMB POWER, THE NR 3 THROTTLE STARTED BINDING 2 KNOB WIDTHS SHORT OF CLIMB POWER. AT SAME TIME, NR 3 ENGINE OIL QTY STARTED TO DECREASE TO 0 AND THE NR 3 ENGINE OIL TEMPERA TURE WENT TO 160 DEGREES CELSIUS. NR 3 OIL PRESSURE DECREASED TO 0 PSI. NR 3 LOW OIL PRESSURE LIGHT ILLUMINATED. NR 3 ENGINE WAS SHUT DOWN PER EMERGENCY PROCEDURES. ENGINE 1 AND 2 INDICATIONS WERE NORMAL. RETURNED AND LANDED DFW WITHOU T INCIDENT. REPLACED ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. ENGINE TEAR DOWN REVEALED THAT THE NR 4 BEARING PRESSURE LINE PACKING WAS DETERIORATED. THE PACKING MATERIAL IN THE ID WAS TORN. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998090401136 19980904 01136 NM 1998 9 4 AALA981345 1 19980708 A 3230 AAP2448A ACCESSORY UNIT BOEING 727 727223 1384074 NM E/E BAY MALFUNCTIONED A AALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 873AA R00709 21385 DTW - FLT 1768 - DURING LANDING APPROACH, GREEN GEAR DOWN AND LOCKED INDICATOR CHANGED TO RED. GEAR WAS RECYCLED AND THE RED GEAR UNSAFE INDICATOR REMAINED ILLUMINATED. CREW FLEW TO SAFE ALTITUDE AND VISUALLY CHECKED GEAR INDICATORS WHICH INDICATED GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED DTW WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LANDING GEAR AC CESSORY UNIT AND AS A PRECAUTIONARY, LUBRICATED NOSE LANDING GEAR, AND CLEANED DOWNLOCK POSITION SWITCHES. SYSTEM GROUN D CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F A3WE 1998090401137 19980904 01137 1998 9 4 AALA981408 4 19980717 A 2565 D29982125 SLIDE AIRCRUISERS DOUG DC9 DC982 3022082 WP PASSENGER DOOR MALFUNCTIONED A AALA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 449AA BBCMZPZ 49475 PVD - FLT 1974 - FORWARD ENTRY DOOR SLIDE FOUND ON FLOOR WITH PINS POPPED OUT. DID NOT INFLATE. INSTALLED NEW DOOR SLI DE PACK. SYSTEM GROUND CHECKED NORMAL. (X) 2 L 7 2 4F A6WE 1998090401138 19980904 01138 EU 1998 9 4 AALA981415 1 19980722 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 14068 511 LGW - FLT 0120 - DURING CRUISE, COACH NR 8 OVEN SMOKES WHEN OVEN IS ON. DISCONTINUED USE OF OVEN. LANDED LGW WITHOUT I NCIDENT. CLEANED COACH NR 8 OVEN. GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998090401139 19980904 01139 EU 1998 9 4 AALA981355 1 19980709 A 2530 2510000405 OVEN AIRBUS 300 A300B4605R 3930308 EU GALLEY DIRTY A AALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 70073 516 LHR - FLT 0108 - EN ROUTE BOS/LHR WHILE HEATING MEALS, SMOKE WAS OBSERVED FROM NR 1 AND NR 2 FIRST CLASS OVENS. SHUT OV ENS OFF AND SMOKE DISSIPATED. LANDED LHR WITHOUT INCIDENT. CLEANED OVENS, SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A35EU 1998090401140 19980904 01140 NM 1998 9 4 AALA981417 1 19980721 A 3350 S283N00219 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 620AA 24578 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. ATTACHED LEADS TO FORWARD L EFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998090401141 19980904 01141 NM 1998 9 4 AALA981416 1 19980721 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313AA 22316 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 37B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGH T CONNECTOR AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401142 19980904 01142 NM 1998 9 4 AALA981390 1 19980715 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHTS AT 7HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT TERMINAL CON NECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A1NM 1998090401143 19980904 01143 SO 1998 9 4 RAAA98E4019 1 19980822 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 PAX ROW 13 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998090401144 19980904 01144 SO 1998 9 4 RAAA98E9021 1 19980829 A 5720 ANGLE LKHEED 188 188C 5262604 SO WS 167 BROKEN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK WHILE GAINING ACCESS TO REPAIR FUEL LEAK (M-54 NR 11), RT MLG RIB FORGING LOWER NR 4 WING PA NEL ATTACH ANGLE INADVERTENTLY BROKEN OFF AT WS 167. REPAIRED PER LDS DWG 188339. M-54 NR 293. 2 L 7 4 4T 4A22 1998090401145 19980904 01145 SO 1998 9 4 RAAA98E9022 1 19980829 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 167-169 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK WHILE GAINING ACCESS TO REPAIR FUEL LEAK (M-54 NR 11) RT WING LOWER SURFACE NR 4 PANEL, NR 2 2 RISER INADVERTENTLY CRACKED IN RADUS, APPROX 2.00 IN, AT WS 167 TO 169. REPAIRED PER LDS DWG 188339. M-54 NR 292. 2 L 7 4 4T 4A22 1998090401146 19980904 01146 SO 1998 9 4 RAAA98E9023 1 19980829 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 135-155 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK PER CARD 42.03.66, FOUND RT WING LOWER SURFACE NR 8 PANEL CORRODED AT WS 135 TO 155. REPAIR ED PER DWG TSG/83-7002 AND SRM 57-2-1. M-54 NR 64. 2 L 7 4 4T 4A22 1998090401147 19980904 01147 SO 1998 9 4 RAAA98E9024 1 19980829 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 309 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK PER CARD 42.036.55, FOUND FS 309 FRAME CORRODED AT STR 32 TO 41. REPAIRED PER SRM 53-2-3. M -54 NR 148. 2 L 7 4 4T 4A22 1998090401148 19980904 01148 SO 1998 9 4 RAAA98E9025 1 19980829 A 5414 SKIN LKHEED 188 188C 5262604 SO NR 3 NACELLE CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK PER CARD 42.03.78, FOUND NR 3 NACELLE I/B SKIN CRACKED, APPROX .75 IN, AT NAC STA -30, NAC W L -8. REPAIRED PER SRM 54-2-1. M-54 NR 215. 2 L 7 4 4T 4A22 1998090401149 19980904 01149 SO 1998 9 4 RAAA98E9026 1 19980829 A 5330 SKIN LKHEED 188 188C 5262604 SO BS 265 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK PER CARD 42.03.55, FOUND FUSELAGE SKIN DENTED AND GOUGED BEYOND SRM LIMITS AT FS 265, STR 51 TO 52. REPAIRED PER SRM 53-2-1. M-54 NR 290. 2 L 7 4 4T 4A22 1998090401150 19980904 01150 SO 1998 9 4 RAAA98E9027 1 19980829 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 321 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK AND ACCESS FOR M-54 NR 290, REPAIR FOUND FS 321 FRAME CORRODED AT STR 52. REPAIRED PER SRM 53-2-3. M-54 NR 317. 2 L 7 4 4T 4A22 1998090401151 19980904 01151 SO 1998 9 4 RAAA98E9028 1 19980829 A 5320 DOUBLER LKHEED 188 188C 5262604 SO BS 375-415 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK PER CARD 42.03.55, FOUND FUSELAGE SKIN DOUBLER CORRODED AT FS 375 TO 415, STR 33 TO 40. REP LACED DOUBLER PER SRM 53-2-1, FIG 2, SHEET 3. M-54 NR 84. 2 L 7 4 4T 4A22 1998090401152 19980904 01152 SO 1998 9 4 RAAA98E9029 1 19980829 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 321 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK AND ACCESS FOR M-54 NR 84, REPAIR FOUND FS 321 FRAME CORRODED AT STR 27 TO 45. REPAIRED PER SRM 53-2-3. M-54 NR 123. 2 L 7 4 4T 4A22 1998090401153 19980904 01153 SO 1998 9 4 RAAA98E9030 1 19980829 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 407 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 1968R 188C2007 DURING SCHEDULED NR 3 CHECK AND ACCESS FOR M-54 NR 84, REPAIR FOUND FS 407 FRAME CORRODED AT STR 33 TO 40. REPAIRED PER SRM 53-2-3. M-54 NR 281. 2 L 7 4 4T 4A22 1998090401154 19980904 01154 NM 1998 9 4 UPS98227587 1 19980824 A 5313 STRINGER BOEING 727 727247 138408F NM BS 1016 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, CORROSION (C53-111-01-3D) ON STRINGER BS 1016 WL 150 RBL 28. STRINGER REPAIRED BS 1006 TO BS 1016 P ER 727 SRM 53-10-3 AND 51-30-2. 2 L 7 3 4F A3WE 1998090401155 19980904 01155 NM 1998 9 4 UPS98227588 1 19980824 A 5755 652162225 FITTING BOEING 727 727247 138408F NM NR 11 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 210UP 21697 INSPECTION TYPE-SI, NR 11 SPOILER FITTING CORRODED AT MOUNT HOLE. REPLACED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998090401156 19980904 01156 NM 1998 9 4 UPS98227589 1 19980817 A 5320 WEB BOEING 727 72727C 138400J NM NLG WW CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 908UP 19114 INSPECTION TYPE-C, NLG W/W CEILING HAS VISUAL CRACK INDICATION AT RIVET HOLE STA 288 BL 0. REMOVED AND REPLACED DAMAGED SECTION OF WEB NWW CELING BS 288 TO 270 BL 9 LT TO BL 9 RT AS PER B727 SRM 53-10-2 FIG 2 AND 51-30-2. MATERIAL USED 70 75-T6 .040 18 X 18 LOT 219081 P O 8312438. 2 L 7 3 4F A3WE 1998090401157 20010116 01157 NM 2001 1 16 QXEA9801200 1 19980826 A 2612 360188100039035 FIRE LOOP DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE DAMAGED A QXEA K NONE J WARNING INDICATION NR NOT REPORTED 1 NM 09 351PH 490 NR 2 ENGINE FIRE DETECTION LOOP-A LIGHT ILLUMINATED. FOUND THE PRIMARY DETECTION LOOP-A BAD. SWAPPED TO THE SPARE A SE NSOR. REMOVED AND REPLACED THE FIRE LOOP-A, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998090401158 19980904 01158 NM 1998 9 4 QXEA9801201 1 19980829 A 2612 BULB DHAV 82410175021 DHAV DHC8 DHC8202 2809007 NM NR 2 FIRE DET FAILED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 361PH 516 NR 2 FIRE DETECTION SYSTEM FAULT LIGHT B ILLUMINATED. INSPECTED AND FOUND THE NR 2 SYSTEM A BULB BLOWN CAUSING THE B-LO OP TO FAIL. REPLACED LAMP AND RESET B CIRCUIT BREAKER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998090401159 19980904 01159 EU 1998 9 4 QXEA9801097 1 19980815 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 5805 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 STRINGERS 15 AND 16 HAVE NICKS AT SKIN FLANGE RADIUS IN AREA OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-06 PAGE 9 FIG URE 4. 2 L 7 2 4F RT A20EU 1998090401160 19980904 01160 EU 1998 9 4 QXEA9801099 1 19980809 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16660 FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 ONE INCH BREAK IN FRAME CASTELLATION AT FRAME 16660 OUTBOARD OF STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2 P AGE 4. 2 L 7 2 4F RT A20EU 1998090401161 19980904 01161 EU 1998 9 4 QXEA9801100 1 19980807 A 5312 BULKHEAD WEB FOKKER F28 F28MK4000 4990810 EU FWD PRESS BLKHD PUNCTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 SMALL PUNCTURE (.025) IN SKIN AT LEFT HAND END OF FRAME NR 7 ON FRONT PRESSURE BULKHEAD. REPAIRED IAW FOKKER SRM 53-02- 02, PAGE 2. 2 L 7 2 4F RT A20EU 1998090401162 19980904 01162 EU 1998 9 4 QXEA9801101 1 19980807 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME 13815B AT STRINGER 74 HAS A CRACK UNDER GILL LINER SUPPORT CONNECTION BRACKET. REPAIRED IAW HORIZON AIR EA 4-53-5 24. 2 L 7 2 4F RT A20EU 1998090401163 19980904 01163 EU 1998 9 4 QXEA9801102 1 19980805 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME 7805 IS CRACKED. DIRECTLY ABOVE STRINGER 73. REPAIRED IAW HORIZON AIR EA 4-53-522. 2 L 7 2 4F RT A20EU 1998090401164 19980904 01164 EU 1998 9 4 QXEA9801103 1 19980723 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CORROSION AT NUT PLATE HOLE IN FRAME 5305 AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 9 FIGURE 3 SECTION D-D . 2 L 7 2 4F RT A20EU 1998090401165 19980904 01165 EU 1998 9 4 QXEA9801104 1 19980816 A 5320 COVER FOKKER F28 F28MK4000 4990810 EU NLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK AT NOSE GEAR BAY TOP COVER, STATION 2475. REPAIRED IAW HORIZON AIR EA 4-53-532. 2 L 7 2 4F RT A20EU 1998090401166 19980904 01166 EU 1998 9 4 QXEA9801105 1 19980727 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU NLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK ON NOSEGEAR ATTACH FITTING INBOARD OF NOSE GEAR ACTUATOR ATTACH BRACKET. REPAIRED IAW HORIZON AIR EA 4-53-503. 2 L 7 2 4F RT A20EU 1998090401167 19980904 01167 EU 1998 9 4 QXEA9801106 1 19980723 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU BS 3870 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 BOTH FLOOR SUPPORT ANGLES CRACKED ON FUSELAGE KEEL BEAM AT BL600R, FRAME 3870. REPAIRED IAW FOKKER SRM 51-31-01 AND 51- 30-02. 2 L 7 2 4F RT A20EU 1998090401168 19980904 01168 EU 1998 9 4 QXEA9801107 1 19980803 A 5320 STRIP FOKKER F28 F28MK4000 4990810 EU NLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 TYPE 2 CRACKS (LEFT AND RIGHT) AT INNER FRAME STRIP AFT SIDE OF NOSE LANDING GEAR WHEEL BAY. REPAIRED IAW HORIZON AIR E O 4-53-33B. 2 L 7 2 4F RT A20EU 1998090401169 19980904 01169 EU 1998 9 4 QXEA9801108 1 19980728 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK ON CLIP TO FUSELAGE ATTACH POINT, STATION 13815B. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 7 AND 8. 2 L 7 2 4F RT A20EU 1998090401170 19980904 01170 EU 1998 9 4 QXEA9801109 1 19980728 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK ON CLIP TO FUSELAGE ATTACH POINT, STATION 13815B, NEAR LEFT CORNER WHERE PANEL 98H IS INSTALLED. REPAIRED IAW FOK KER SRM 53-02-01, PAGE 7 AND 8. 2 L 7 2 4F RT A20EU 1998090401171 19980904 01171 EU 1998 9 4 QXEA9801110 1 19980803 A 5320 STIFFENER FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK AT BOTTOM OF STIFFENER 4TH STIFFENER FROM FRAME 11905, RIGHT SIDE, IN BLEED AIR TUNNEL, UNDER PANEL 26A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401172 19980904 01172 EU 1998 9 4 QXEA9801111 1 19980802 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK IN FRAME 11905 IN BLEED AIR TUNNEL AT 5 O'CLOCK POSITION. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 8, 51-10-4 AND 51-31-01. 2 L 7 2 4F RT A20EU 1998090401173 19980904 01173 EU 1998 9 4 QXEA9801112 1 19980805 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME 16660 CASTELLATION AT STRINGER 1 HAS A TWO INCH CRACK IN RADIUS. REPAIRED IAW FOKKER SRM 53-02-12 AND 51-31-01. 2 L 7 2 4F RT A20EU 1998090401174 19980904 01174 EU 1998 9 4 QXEA9801113 1 19980728 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME CASTELLATION AT FRAME 13815B BETWEEN STRINGER 2 AND 3 HAS A 1.5 INCH CRACK IN RADIUS AND IS CRACKED AT THE RIVET. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998090401175 19980904 01175 EU 1998 9 4 QXEA9801114 1 19980728 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME CASTELLATION AT FRAME 13815B BETWEEN STRINGER 72 AND 73 HAS A 1.5 INCH CRACK IN RADIUS AND A 1 INCH CRACK AT RIVET . REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998090401176 19980904 01176 EU 1998 9 4 QXEA9801115 1 19980808 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 AFT CARGO DOOR OUTER SKIN LOWER AFT CORNER AT DOOR HINGE ATTACHMENT HAS TOOLING DAMAGE. REPAIRED IAW HORIZON AIR EA 4-5 2-150. 2 L 7 2 4F RT A20EU 1998090401177 19980904 01177 EU 1998 9 4 QXEA9801116 1 19980806 A 2750 CABLES FOKKER F28 F28MK4000 4990810 EU TE FLAPS RUSTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FOUR SEGMENTS OF FLAP DRIVE CABLES IN HYDRAULIC TUNNEL HAVE RED RUST CORROSION FROM FRONT BULKHEAD TO SWITCH UNIT. REPA IRED IAW FOKKER SRM 20-30-09 AND SRM 27-51-00, PARAGRAPH B, STEPS 1 THRU 54. 2 L 7 2 4F RT A20EU 1998090401178 19980904 01178 EU 1998 9 4 QXEA9801117 1 19980813 A 3232 ACTUATOR FOKKER F28 F28MK4000 4990810 EU LT MLG DOOR FAILED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 BOTH LEFT-HAND INBOARD GEAR DOOR ACTUATOR BEARINGS FELL OUT. REPLACED LEFT-HAND FORWARD AND AFT ACTUATORS IAW FOKKER SR M 32-32-14, PAGE 201, 3A, B, C AND D STEP 1. 2 L 7 2 4F RT A20EU 1998090401179 19980904 01179 EU 1998 9 4 QXEA9801118 1 19980722 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FORWARD CARGO BAY CLIP CRACK AT FRAME 7305 STRINGER 66. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, 51-10-09, PAGE 9, PAR AGRAPH 4, A-C AND 51-31-01, PAGE 13-17. 2 L 7 2 4F RT A20EU 1998090401180 19980904 01180 EU 1998 9 4 QXEA9801119 1 19980808 A 5230 DOOR FOKKER F28 F28MK4000 4990810 EU CARGO COMPT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 AFT CARGO DOOR HAS CORROSION AT WEB AT AFT LOWER CORNER. REPAIRED IAW FOKKER SRM 52-01-01. 2 L 7 2 4F RT A20EU 1998090401181 19980904 01181 EU 1998 9 4 QXEA9801120 1 19980805 A 5230 WEB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CARGO A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 AFT CARGO DOOR HAS A CRACK WEB JUST INSIDE BEAR FRAME. REPAIRED IAW FOKKER SRM 52-30-00, 51-31-01 AND 51-30-02. 2 L 7 2 4F RT A20EU 1998090401182 19980904 01182 EU 1998 9 4 QXEA9801121 1 19980803 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 AFT CARGO DOOR FORWARD LOWER BEAM FRAME HAS CRACK AT NUT PLATE. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 52-30-00 . 2 L 7 2 4F RT A20EU 1998090401183 19980904 01183 EU 1998 9 4 QXEA9801122 1 19980808 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 AFT CARGO DOOR INNER BEAM HAVE IMPACT DAMAGE NEXT TO HINGE ASSEMBLY. REPAIRED IAW HORIZON AIR EA 4-52-150. 2 L 7 2 4F RT A20EU 1998090401184 19980904 01184 EU 1998 9 4 QXEA9801123 1 19980808 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 AFT CARGO DOOR FORWARD LOWER CORNER HAS IMPACT DAMAGE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998090401185 19980904 01185 EU 1998 9 4 QXEA9801124 1 19980809 A 5230 BEAM FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 AFT CARGO DOOR HAS IMPACT DAMAGE ON UPPER BEAM AFT CORNER. REPAIRED IAW HORIZON AIR EA 4-52-150. 2 L 7 2 4F RT A20EU 1998090401186 19980904 01186 EU 1998 9 4 QXEA9801125 1 19980722 A 5320 SIDE WALL FOKKER F28 F28MK4000 4990810 EU BS 2570 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 NOSE WHEEL BAY LEFT-HAND STATION 2570 HAS CRACKS FROM A RIVET IN THE SIDE WALL SKIN. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9. 2 L 7 2 4F RT A20EU 1998090401187 19980904 01187 EU 1998 9 4 QXEA9801126 1 19980722 A 5320 SIDE WALL FOKKER F28 F28MK4000 4990810 EU BS 2570 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 NOSE WHEEL BAY RIGHT-HAND STATION 2570 HAS CRACKS FROM A RIVET IN THE SIDE WALL SKIN. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9. 2 L 7 2 4F RT A20EU 1998090401188 19980904 01188 EU 1998 9 4 QXEA9801127 1 19980722 A 5320 SIDE WALL FOKKER F28 F28MK4000 4990810 EU BS 2970 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 RIGHT-HAND NOSE BAY SIDE WALL STATION 2970 HAS CRACKS FROM A RIVET. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9. 2 L 7 2 4F RT A20EU 1998090401189 19980904 01189 EU 1998 9 4 QXEA9801128 1 19980803 A 2150 EXHAUST FOKKER F28 F28MK4000 4990810 EU RT ACM CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 RIGHT-HAND ACM EXHAUST DUCT CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-05. 2 L 7 2 4F RT A20EU 1998090401190 19980904 01190 EU 1998 9 4 QXEA9801129 1 19980811 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU SERVICE DOORWAY DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 SERVICE EMERGENCY DOOR OPENING LOWER LEFT HAND CORNER HAS A TOOLING CUT .25 WIDE BY .1875 DEEP IN THE 3RD AND 4TH SHEETM ETAL LAYERS. REPAIRED IAW HORIZON AIR EA 4-53-527. 2 L 7 2 4F RT A20EU 1998090401191 19980904 01191 EU 1998 9 4 QXEA9801130 1 19980808 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 6305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 DENT .055 INCH PROTRUDING OUT ON LEFT-HAND SIDE OF FUSELAGE SKIN 9 AFT OF FRAME 6305. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, RIG 1 AND SRM 53-01-01, PAGE 9, 6 A-D. 2 L 7 2 4F RT A20EU 1998090401192 19980904 01192 EU 1998 9 4 QXEA9801131 1 19980720 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME CLIP CRACKED AT FRAME 8305 STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401193 19980904 01193 EU 1998 9 4 QXEA9801132 1 19980720 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME CLIP CRACKED AT FRAME 9305A STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401194 19980904 01194 EU 1998 9 4 QXEA9801133 1 19980720 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305 AT STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401195 19980904 01195 EU 1998 9 4 QXEA9801134 1 19980720 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305A AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401196 19980904 01196 EU 1998 9 4 QXEA9801135 1 19980724 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME14755-15205 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 RIGHT-HAND INBOARD SEAT TRACK INNER FLOOR BOARD FLANGE HAS CORROSION FROM FRAME 14755 TO 15205. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998090401197 19980904 01197 EU 1998 9 4 QXEA9801136 1 19980731 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 RIGHT-HAND INBOARD SEAT TRACK INBOARD FLANGE 6 FORWARD OF FRAME 13815B HAS A .014 GOUGE .053 THICK. REPAIRED IAW FOKKER SRM 53-02-15, PAGES 3 AND 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998090401198 19980904 01198 EU 1998 9 4 QXEA9801137 1 19980724 A 5220 PINS FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 THREE LATCHING PINS HAVE DAMAGE AT THE ENGAGEMENT ENDS. REPLACED LATCHING PINS IAW HORIZON AIR EO 4-52-79A. 2 L 7 2 4F RT A20EU 1998090401199 19980904 01199 EU 1998 9 4 QXEA9801138 1 19980801 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME4610 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK IN THE CASTELLATION AT FRAME 4610 AND STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401200 19980904 01200 EU 1998 9 4 QXEA9801139 1 19980728 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 RIGHT-HAND INBOARD SEAT TRACK BETWEEN FRAME 9305B AND 9305 HAS CHAFE DAMAGE INSIDE OF TRACK. REPAIRED IAW FOKKER SRM 53 -02-15. 2 L 7 2 4F RT A20EU 1998090401201 19980904 01201 EU 1998 9 4 QXEA9801140 1 19980719 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305C AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401202 19980904 01202 EU 1998 9 4 QXEA9801141 1 19980719 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305C AT STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401203 19980904 01203 EU 1998 9 4 QXEA9801142 1 19980719 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305C AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401204 19980904 01204 EU 1998 9 4 QXEA9801143 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305A AT STRINGER 47. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401205 19980904 01205 EU 1998 9 4 QXEA9801144 1 19980719 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305 AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401206 19980904 01206 EU 1998 9 4 QXEA9801145 1 19980720 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305 AT STRINGER 48A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401207 19980904 01207 EU 1998 9 4 QXEA9801146 1 19980719 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 9305C AT STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401208 19980904 01208 EU 1998 9 4 QXEA9801147 1 19980719 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 8805 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998090401209 19980904 01209 EU 1998 9 4 QXEA9801148 1 19980717 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 7805 AT STRINGER 32. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401210 19980904 01210 EU 1998 9 4 QXEA9801149 1 19980717 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 7805 AT STRINGER 38. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401211 19980904 01211 EU 1998 9 4 QXEA9801150 1 19980717 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 7805 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401212 19980904 01212 EU 1998 9 4 QXEA9801151 1 19980716 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5808 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 5805 AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401213 19980904 01213 EU 1998 9 4 QXEA9801152 1 19980716 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 5805 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401214 19980904 01214 EU 1998 9 4 QXEA9801153 1 19980716 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 5805 AT STRINGER 42. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401215 19980904 01215 EU 1998 9 4 QXEA9801154 1 19980716 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 5805 AT STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401216 19980904 01216 EU 1998 9 4 QXEA9801155 1 19980716 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 5805 AT STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401217 19980904 01217 EU 1998 9 4 QXEA9801156 1 19980717 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACKED AT FRAME 5805 AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401218 19980904 01218 EU 1998 9 4 QXEA9801157 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CLIP CRACK AT FRAME 16060 AND STRINGER 55A. REPAIRED IAW FOKKER 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401219 19980904 01219 EU 1998 9 4 QXEA9801158 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACKED CLIP AT FRAME 16060 AND STRINGER 55. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401220 19980904 01220 EU 1998 9 4 QXEA9801159 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACKED CLIP AT FRAME 16060 AND STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1998090401221 19980904 01221 EU 1998 9 4 QXEA9801160 1 19980807 A 5320 BRACKET FOKKER F28 F28MK4000 4990810 EU BS 1700 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACK IN RADIUS/NECK OF T-ATTACH BRACKET FOR Z STRINGER 2.18, STATION 1700R. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998090401222 19980904 01222 EU 1998 9 4 QXEA9801161 1 19980815 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT TE FLAP DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 LEFT-HAND OUTBOARD LEADING EDGE DELAMINATING AT PREVIOUS REPAIR. REPAIRED IAW FOKKER SRM 51-70-00, PAGE 15. 2 L 7 2 4F RT A20EU 1998090401223 19980904 01223 EU 1998 9 4 QXEA9801162 1 19980801 A 5720 ANGLE FOKKER F28 F28MK4000 4990810 EU LT MLG WW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 LEFT-HAND WING UPPER LEFT-HAND MLG CONNECTION ANGLE (FROM WING TO MLG) CRACKED IN RADIUS. REPAIRED IAW FOKKER SRM 57-02 -05. 2 L 7 2 4F RT A20EU 1998090401224 19980904 01224 EU 1998 9 4 QXEA9801163 1 19980813 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 LEFT-HAND WING INBOARD FLAP VANE HAS ROCK DAMAGE TO LOWER SKIN AT FIRST 48 INCHES FROM INBOARD EDGE. REPAIRED IAW FOKKE R SRM 51-70-00, PARAGRAPH 5A(2), SRM 51-70-0 METHOD 1 PARAGRAPH 7, HORIZON AIR EA 4-57-152 AND MAINTENANCE MANUAL 27-50- 02. 2 L 7 2 4F RT A20EU 1998090401225 19980904 01225 EU 1998 9 4 QXEA9801164 1 19980814 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 DENT IN LOWER WING SKIN AFT OF NR 2 LIFT DUMPER BELL CRANK. REPAIRED IAW FOKKER SRM 57-02-04, PAGE 2, FIGURE 1 AND SRM 51-31-04. 2 L 7 2 4F RT A20EU 1998090401226 19980904 01226 EU 1998 9 4 QXEA9801166 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73J OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401227 19980904 01227 EU 1998 9 4 QXEA9801167 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73H OPENING HAS FRETTING CORROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401228 19980904 01228 EU 1998 9 4 QXEA9801168 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73G OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401229 19980904 01229 EU 1998 9 4 QXEA9801169 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73E OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401230 19980904 01230 EU 1998 9 4 QXEA9801170 1 19980728 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73D HAS FRETTING EROSION AROUND SCREW HOLE. REPAIRED IAW HORIZON AIR EA 4-57-154. 2 L 7 2 4F RT A20EU 1998090401231 19980904 01231 EU 1998 9 4 QXEA9801171 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73D OPENING HAS FRETTING EROSION AROUND SCREW HOLE. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401232 19980904 01232 EU 1998 9 4 QXEA9801172 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 71A OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401233 19980904 01233 EU 1998 9 4 QXEA9801173 1 19980728 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 71A HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154. 2 L 7 2 4F RT A20EU 1998090401234 19980904 01234 EU 1998 9 4 QXEA9801174 1 19980728 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73B HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154. 2 L 7 2 4F RT A20EU 1998090401235 19980904 01235 EU 1998 9 4 QXEA9801175 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73B OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401236 19980904 01236 EU 1998 9 4 QXEA9801176 1 19980728 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73A HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154. 2 L 7 2 4F RT A20EU 1998090401237 19980904 01237 EU 1998 9 4 QXEA9801177 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73A OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401238 19980904 01238 EU 1998 9 4 QXEA9801178 1 19980728 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73C HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-154. 2 L 7 2 4F RT A20EU 1998090401239 19980904 01239 EU 1998 9 4 QXEA9801179 1 19980812 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING FRETTING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FUEL PANEL 73C OPENING HAS FRETTING EROSION AROUND SCREW HOLES. REPAIRED IAW HORIZON AIR EA 4-57-162. 2 L 7 2 4F RT A20EU 1998090401240 19980904 01240 EU 1998 9 4 QXEA9801180 1 19980818 A 5720 FAIRING FOKKER F28 F28MK4000 4990810 EU WS 1800 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 DENT IN SKIN PLANE FAIRING WEB RIGHT-HAND LOWER WING APPROXIMATELY STATION 1800. REPAIRED IAW HORIZON AIR EA 4-57-138. 2 L 7 2 4F RT A20EU 1998090401241 19980904 01241 EU 1998 9 4 QXEA9801181 1 19980731 A 5712 RIB FOKKER F28 F28MK4000 4990810 EU WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 LEADING EDGE RIB BETWEEN PANEL 92J AND 62A IS CHAFED IN SEVERAL PLACES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAG RAPH 4 A-C AND HORIZON AIR EA 4-57-1573. 2 L 7 2 4F RT A20EU 1998090401242 19980904 01242 EU 1998 9 4 QXEA9801182 1 19980805 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 THERE ARE TWO DENTS BELOW AND FORWARD OF SCAB PATCH ABOVE LAV SERVICE PANEL STATION 18870. REPAIRED IAW FOKKER SRM 53-0 2-02, FIGURE 1. 2 L 7 2 4F RT A20EU 1998090401243 19980904 01243 EU 1998 9 4 QXEA9801183 1 19980729 A 2722 HOUSING FOKKER F28 F28MK4000 4990810 EU RUDDER BROKEN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 RUDDER ACTUATOR TO RUDDER POST RETAINING BOLT ANTI ROTATION HOUSING IS BROKEN. REPAIRED IAW HORIZON AIR EA 4-27-52. 2 L 7 2 4F RT A20EU 1998090401244 19980904 01244 EU 1998 9 4 QXEA9801184 1 19980804 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 18870 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 SCAB PATCH ABOVE LAV SERVICE PANEL STATION 18870 HAS DENT IN PATCH. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 2. 2 L 7 2 4F RT A20EU 1998090401245 19980904 01245 EU 1998 9 4 QXEA9801185 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 498US 11181 PREVIOUS CLIP REPAIR ON FRAME 17565 AT STRINGER 21 HAS IMPROPER FASTENERS PER FOKKER SRM 53-02-13. REPLACED FASTENERS I AW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 1998090401246 19980904 01246 EU 1998 9 4 QXEA9801186 1 19980811 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 DENT .069 INCH DEEP, 6 INCHES AFT OF FRAME 18075 AT STRINGER 51. REPAIRED IAW FOKKER SRM 53-02-06 PAGE 6 AND 7, FIGURE 3, SRM 51-31-01, SRM 51-30-02, PAGE 10. 2 L 7 2 4F RT A20EU 1998090401247 19980904 01247 EU 1998 9 4 QXEA9801187 1 19980722 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 THERE ARE TWO CRACKED FRAME CLIPS ON THE BACK SIDE OF FRAME 20075 BETWEEN STRINGERS 33 AND 41. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 10. 2 L 7 2 4F RT A20EU 1998090401248 19980904 01248 EU 1998 9 4 QXEA9801188 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 24-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 TWO CRACKED FRAME CLIPS ON THE BACK SIDE OF OBLIQUE FRAME 24-2 AT STRINGERS 46 AND 29. REPAIRED IAW FOKKER SRM 53-02-13 , FIGURE 5. 2 L 7 2 4F RT A20EU 1998090401249 19980904 01249 EU 1998 9 4 QXEA9801189 1 19980729 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 BACKSIDE OF FRAME 41-2 THERE IS A CRACKED FRAME CLIP AT STRINGER 29. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998090401250 19980904 01250 EU 1998 9 4 QXEA9801190 1 19980723 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 MISREPAIRED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 ON BACKSIDE OF FRAME 41-2 THERE IS A PREVIOUS REPAIR THAT IS NOT IN CONFORMITY WITH FOKKER SRM 53-02-13 AT STRINGER 44. REPAIRED IAW FOKKER SRM 51-30-13, FIGURE 6. 2 L 7 2 4F RT A20EU 1998090401251 19980904 01251 EU 1998 9 4 QXEA9801191 1 19980724 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 ON BACKSIDE OF OBLIQUE FRAME 50-2 THERE ARE CRACKED FRAME CLIPS AT STRINGERS 25, 27 AND 29. REPAIRED IAW FOKKER SRM 53- 02-13, FIGURE 3 AND MM 53-10-5, PAGE 601-604. 2 L 7 2 4F RT A20EU 1998090401252 19980904 01252 EU 1998 9 4 QXEA9801192 1 19980723 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 ON BACKSIDE OF FRAME 50-2 THERE ARE CRACKED FRAME CLIPS AT STRINGERS 49, 51 AND 52. REPAIRED IAW FOKKER SRM 51-31-01, 5 1-10-4, 53-02-3 FIGURE 3 AND F-28 MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998090401253 19980904 01253 EU 1998 9 4 QXEA9801193 1 19980723 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 22293 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 FRAME 22293 IS CRACKED IN TWO PLACES ON THE FORWARD RIGHT-HAND SIDE BETWEEN STRINGERS 55 AND 56. REPAIRED IAW HORIZON A IR EA 4-53-498, STEPS 1, 3-7, AND FOKKER SRM 51-30-01. 2 L 7 2 4F RT A20EU 1998090401254 19980904 01254 EU 1998 9 4 QXEA9801194 1 19980721 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 PREVIOUS REPAIR ON FORWARD SIDE OF FRAME 17565 BETWEEN STRINGERS 51 AND 52 IS CRACKED. REPAIRED IAW FOKKER SRM 53-02-13 , FIGURE 3. 2 L 7 2 4F RT A20EU 1998090401255 19980904 01255 EU 1998 9 4 QXEA9801195 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 THERE ARE TWO CRACKED FRAME CLIPS ON THE FORWARD SIDE OF FRAME 17565 AT STRINGERS 49 AND 50. REPAIRED IAW FOKKER SRM 53 -02-13, FIGURE 3 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1998090401256 19980904 01256 EU 1998 9 4 QXEA9801196 1 19980721 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 175465 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 498US 11181 THERE IS A PREVIOUS CLIP REPAIR ON FRAME 17565 AT STRINGER 21 THAT HAS IMPROPER FASTENERS PER FOKKER SRM 53-02-13. REMO VED AND REPLACED FASTENERS IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 1998090401257 19980904 01257 EU 1998 9 4 QXEA9801197 1 19980827 A 2611 SMOKE DETECTOR FOKKER F28 F28MK4000 4990810 EU LAVATORY ACTIVATED A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 480AU 11229 AIRCRAFT RETURNED TO FIELD WITH BOTH SMOKE DETECTORS IN THE LAVS GOING OFF. CREW NOTED THAT THE APU WAS OFF ON TAKEOFF AND CLIMB. PURGED BLEED AIR DUCTS AND CHANGED WATER SEPARATOR FILTER SOCKS. GROUND RAN AIRCRAFT, OPERATIONAL CHECK GOO D. NO SMOKE NOTED. AIRCRAFT TEST FLIGHT SATISFACTORY. 2 L 7 2 4F RT A20EU 1998090401258 19980904 01258 EU 1998 9 4 QXEA9801198 1 19980827 A 3350 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 RIGHT FORWARD OVERWING EXIT LIGHT INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998090401259 19980904 01259 EU 1998 9 4 QXEA9801199 1 19980828 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CARGO COMPT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 209 11167 RIGHT AFT EMERGENCY EXIT LIGHT OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY POWER SUPPLY IN THE AFT CARGO COMPARTM ENT. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998090401260 19980904 01260 EU 1998 9 4 QXEA9801202 1 19980830 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 486US 11237 TWO EVENTS OF THE EMERGENCY EXIT LIGHT AT ROW 8CDE REPORTED BURNT OUT. IN BOTH CASES MAINTENANCE RELAMPED AND OPERATION ALLY TESTED. RESULTS WERE NORMAL. 2 L 7 2 4F RT A20EU 1998090401261 19980904 01261 WP 1998 9 4 98FDEA00537 1 19980831 A 5753 ARC1457402 VANE DOUG DC10 DC1010 3022110 WP RT TE FLAP VANE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 375FE 46613 RT O/B FLAP VANE UPPER EXTERNAL SURFACE BY NR 4 TRACK IS CRACKED APPROX 4 INCHES LONG AT THE EDGE OF RUB STRIP DOT NR 2. *S/D* REPAIRED PER SERVICE BULLETIN A57-110 PG 40. REPAIR IS IN COMPLIANCE WITH EO 8-5750-7-4319 PART 3 EOCN E4. 2 L 7 3 4F A22WE 1998090401262 19980904 01262 NM 1998 9 4 98UAL900401 1 19980822 A 3350 POWER SUPPLY BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 603UA 21864 EMERGENCY LIGHTS ON ROW 14 TO AFT END RIGHT INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F 4 F RT A1NM E3NE 1998090401263 19980904 01263 WP 1998 9 4 98UAL900402 1 19980823 A 3232 ACTUATOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE LT MLG DOOR ACT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 1858U 46987 LEFT GEAR DOOR LIGHT ON AT BOTH PANELS. VISUALLY CONFIRMED DOOR OPEN. RETURNED TO SFO. *S/D* LEFT MAIN LANDING GEAR DOOR ACTUATOR EYEBOLT ASSEMBLY WAS FOUND SEPARATED FROM THE ACTUATOR PISTON ASSEMBLY. THE DOOR ACTUATOR WAS REPLACED. O PERATIONAL CHECK WAS PERFORMED SATISFACTORILY. 2 L 7 3 4F 4 F A22WE E23EA 1998090401264 19980904 01264 NM 1998 9 4 98UAL900403 1 19980823 A 3350 BATTERY BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 662UA 27159 EMERGENCY FLOOR LIGHTS FLICKER ON AND OFF. REPLACED BATTERIES, OPS CHECK OK. 2 L 7 2 4F 4 F RT A1NM E24NE 1998090401265 19980904 01265 NM 1998 9 4 98UAL900404 1 19980821 A 3260 853502 PROX CARD ELDEC 849704 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE E & E COMPT FAILED A UALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 WP 29 644UA 25094 ON TAKEOFF ROLL 100 KT, FLAP CONFIG WARNING LIGHT ON EICAS AND HORN. CONTINUED TAKEOFF. FALSE STICK SHAKER AT 170 KTS AND L/E SLAT ASYM ON EICAS. COULD NOT RETRACT SLATS WITH FLAP HANDLE UP. EXTENDED FLAPS USING ALTERNATE SYSTEM. LANDE D FLAPS 20 DEG AT 330,000 POUNDS. *S/D* FAULTY LOGIC FROM THE PSEU CAUSED FALSE WARNING INDICATIONS DURING TAKEOFF INC LUDING FLAP CONFIGURATION, SLAT ASYMMETRY AND STALL WARNING. WHEN THE SLAT ASYMMETRY INDICATION WAS SENSED BY THE FLAP/ SLAT ELEC UNIT FSEU. SLATS WERE POSITIONED ELECTRICALLY. REPLACED M14 PROX CARD AND M10 DRIVER CARD ASSEMBLIES IN PSEU AND THE S300 SLAP POSITION SENOR SWITCH PER MM. 2 L 7 2 4F 4 F RT A1NM E24NE 1998090401266 19980904 01266 NM 1998 9 4 98UAL900406 1 19980821 A 3350 LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 354UA 24360 DOOR 1 LEFT EXTERIOR EMERGENCY EXIT EGRESS LIGHT INOP. *S/D* REFLECTOR ASSEMBLY AND LAMP REPLACED. REFLECTOR ASSEMBLY (P/N 31-1498-1), LAMP (P/N 1619). 2 L 7 2 4F 4 F RT A16WE E2GL 1998090401267 19980904 01267 NM 1998 9 4 98UAL900407 1 19980823 A 2760 CONTROL CABLE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE SPOILER LOOSE A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 389UA 24664 AIRPLANE AIR-GROUND SWITCH STUCK IN GROUND MODE. *S/D* SECURED GROUND SPOILER INTERLOCK CABLE TO TORSION LINK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998090401268 19980904 01268 NM 1998 9 4 98UAL900408 1 19980824 A 2782 755299A ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LE SLAT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 528UA 25018 RETURNED TO ORD DUE TO A LEADING EDGE FLAP PROBLEM. *S/D* POSITION NUMBER 15 LEADING EDGE SLAT ACTUATOR WAS FOUND WITH AN INTERMITTENT PROBLEM CAUSING THE EICAS MESSAGE AND LOCKOUT OF THE LEADING EDGE SLATS. REPLACED NUMBER 15 LEADING ED GE SLAT ACTUATOR AND RETURNED AIRCRAFT TO SERVICE WITH NO FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A2NM E17NE 1998090401269 19980904 01269 NM 1998 9 4 DHL98702003 1 19980828 A 5210 GATE BOEING 727 72730C 1384009 NM PAX DOOR DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 702DH 19793 DURING AIRCRAFT PRESSURIZATION FOUND FWD ENTRY DOOR LOWER FWD GATE DAMAGED AND SEAL LEAKING. REMOVED AND REPLACED LOWE R GATE PER MM 52-11-71. LP 125348. 2 L 7 3 4F A3WE 1998090401270 19980904 01270 SO 1998 9 4 SWIA971237 1 19980805 A 6121 PROP SYNCH EMB 120 EMB120RT SO PWA 118 PW118A NE RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 289YV 120289 RIGHT ENGINE STARTED SURGING, TQ FLUCTUATIONS AT 9,000 FT. RETURNED TO LAX. TQ FLUCTUATING CONTINUED AS MUCH AS 10 PER CENT. TURNED OFF EEC PER QRH WITH NO CHANGES. NOTIFIED LAX MX. DECLARED EMERGENCY VIA ATC FOR ENGINE SURGING. DID NO T SHUT DOWN ENGINE. RAN AIRCRAFT IN TAKEOFF/CLIMB AND CRUISE CONFIGURATIONS, NP AND TQ BOTH STABLE. DURING 20 + MIN RU N AT 65 PERCENT TQ AND 85 PERCENT NP, FLUCTUATION (MINOR) WAS NOTED TO STABLE SYNC ON. TURNING OFF PROP SYNC RETURNED N P TO STABLE CONDITION, TQ ALSO CHECKS GOOD. FUEL FLOW, NH/NL, T6 ALL MATCHED AND STABLE. ALL ENGINE OPERATIONAL PARAM ETERS OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998090401272 19980904 01272 SO 1998 9 4 SWIA971239 1 19980802 A 5230 SEAL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CARGO DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 212SW 120276 CLIMBING THROUGH F230, CABIN ALTITUDE STARTED A 2500-3500 MINUTE CLIMB. SWITCHED TO MANUAL, NO HELP. CABIN CONTINUED C LIMB. PERFORMED DESCENT, MASKS FELL. LANDED UNPRESSURIZED. NO DOOR LIGHTS NO OTHER UNUSUAL WITH A/C PERFORMANCE. FOU ND CARGO DOOR SEAL BLOWN OUT ON LOWER SIDE OF CARGO DOOR. REPLACED BENT RETAINING STRIP FOR CARGO DOOR SEAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1998090401273 19980904 01273 SO 1998 9 4 SWIA971240 1 19980802 A 2750 FCU EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 128AM 120109 OUTBOARD FLAPS CONTROL FAULT AND WILL NOT RESET. RETURNED TO PDX. REPLACED FLAP CONTROL UNIT IAW MM 27. 2 L 7 2 4T 4 T RT A31SO E20NE 1998090401274 19980904 01274 NE 1998 9 4 P5CA9801378 2 19980829 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 1 FAILED A P5CA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 23 851FT 19756 662276 DURING CLIMBOUT PASSING FL120, ACFT EXPERIENCED LOUD NOISE AND SHUDDER AND FLASH OF LIGHT FOLLOWED BY INCREASE IN NR 1 E NG EGT TO 960 DEGREES. ENGINE SHUT DOWN. DUMPED FUEL AND RETURNED TO SNN. REPLACED NR 1 ENGINE PER BMM 71-00-02 AND P AC M7100-002/M7111-001, M783-007 AND M7100-001. 2 L 7 4 4F 4 F A20WE E20EA 1998090401275 19980904 01275 NE 1998 9 4 TC8A98055 2 19980901 A 7200 ENGINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 4 SURGED A TC8A C D E ABORTED TAKEOFF RETURN TO BLOCK ENGINE SHUTDOWN O OTHER TO TAKEOFF 1 GL 23 183SK 45904 669478 DURING T/O ROLL 90 KNTS, NR 4 ENGINE SURGED, FOLLOWED BY EXTREMELY HIGH EGT 700 DEGREES. ABORTED TAKEOFF AND SHUTDOWN N R 4 ENGINE. 2 L 7 4 4F 4 F 4A25 1E8 1998090900002 19980909 00002 1998 9 9 VJ9800285 4 19980819 A 2565 SLIDE BOEING 737 7372L9 1384497 NM L-2 DOOR DEPLOYED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 464AT 21278 INADVERTENT DEPLOYMENT OF THE L-2 DOOR SLIDE. FERRIED AIRCRAFT TO MCO, DOOR SLIDE WAS INSTALLED ON THE L-2 DOOR. 2 L 7 2 4F RT A16WE 1998090900003 19980909 00003 WP 1998 9 9 UPS98827487 1 19980820 A 2752 57756935019 FITTING DOUG DC8 DC873F 302199F WP GE CFM CFM562 GL LT TE FLAP GOUGED A IPXA K NONE F FLT CONT AFFECTED LD LANDING 1 SO 01 805UP 46117 FLAP SPLIT AFTER REACHING 35 DEG POSITION. AT 35 DE. FLAPS WERE WITHIN 4 DEG. FOUND LEFT CENTER FLAP ACTUATOR DISCONNE CTED AT ROD END, BOLT MISSING. LEFT CENTER FLAP FITTING GOUGED. REPLACING ACTUATOR AND FITTING. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998090900004 19980909 00004 NM 1998 9 9 DL72E981711 1 19980306 A 5753 SPAR BOEING 727 727247 138408F NM NR 3 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 283WA 21485 CRACK AFT SPAR RAIL DOUBLER 38 FROM I/B END OF FLAP. AFT SPAR AND SEAL RETAINER DAMAGED 33 FROM O/B END OF FLAP AFT SPA R RAIL CRACKED 55 FROM I/B END OF FLAP. ALL REPAIRED PER M/M 57-52-0 FIG 802 REF N/R CARDS 005808, 005812 AND 005810. 2 L 7 3 4F A3WE 1998090900005 19980909 00005 NM 1998 9 9 DL72L981717 1 19980820 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 FOUND ON F-1 LETTER CHECK NRC NR 61, TWO 1 INCH CRACKS, LOWER TORQUE BOX LT WEB UPPER EDGE ABOVE LIGHTENING HOLE STA 122 3. INSTALLED DOUBLER PER M/M 53-11-0 PG 832. 2 L 7 3 4F A3WE 1998090900006 19980909 00006 NM 1998 9 9 DL72L981718 1 19980820 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 995 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 509DA 21311 STRINGER 29R FS 995 CORRODED BEYOND LIMITS. REPAIRED PER SRM 53-10-11 FIG 3. 2 L 7 3 4F A3WE 1998090900007 19980909 00007 NM 1998 9 9 DL73E981719 1 19980820 A 3350 BATTERY PACK 20131A BOEING 737 737247 138448D NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 243WA 41940 23517 EMERGENCY LIGHT ABOVE 23 DEF INOP. REPLACED BATTERY PACK. 2 L 7 2 4F A16WE 1998090900011 19980909 00011 WP 1998 9 9 MWEA98929 1 19980817 A 5210 595251225 DOUBLER DOUG DC9 DC914 3022034 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 AFT BULKHEAD PLUG DOOR DOUBLER REPAIR CRACKED AT RIVET UPPER SECTION OF DOOR. MTC FABRICATED AND INSTALLED DOUBLER REPA IR. 2 L 7 2 4F A6WE 1998091100006 19980911 00006 NE 1998 9 11 98ZZZX3222 2 19980801 A 7530 30B1668B TUBE BRAERO 1000 BAE1251000 1500287 EU PWA 305 PW305 NE RT ENG P3 LINE BROKEN A DXTA K NONE O OTHER IN INSP/MAINT 1 GL 07 513QS NA1004 305053 RIGHT HAND ENGINE OUTBOARD BLEED AIR VALVE P3 LINE FOUND BROKEN AT WELDED 'L' FITTING. BY VISUAL INSPECTION, SUSPECTED CAUSE IS VIBRATION AND FATIGUE AND POSSIBILITY OF FLAW IN WELD. 2 L 7 2 4F 4 F RT A3EU E35NE 1998091100023 19980911 00023 CE 1998 9 11 98ZZZX3238 1 19980819 A 2913 12808451 POWER PACK CESSNA 210 210L 2073448 CE CABIN DEFECTIVE A FPIA K NONE O OTHER NR NOT REPORTED 1 SO 15 640AJ 13 696 21060758 WHILE SELECTING LANDING GEAR DOWN, SYSTEM HAD TO BE CYCLED 4-5 TIMES, AND CIRCUIT BREAKER TRIPPED. WHEN ACFT WAS PUT ON JACKS, THE 5TH CYCLE, LANDING GEAR WOULD NOT COME DOWN. SHUTTLE VALVE STUCK IN THE UP POSITION (SPECIFIC PART P/N 128 0802-1, MANIFOLD BODY ASSY, L/G. 1 H 7 1 3O 3A21 1998091100029 19980911 00029 CE 1998 9 11 98ZZZX3244 1 19980801 A 2510 SEAT BELT PACIFICSCIEN CESSNA 172 172M 2072418 CE COCKPIT MALFUNCTIONED A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 1753V 17263738 THIS BELT WAS INSTALLED IN BACK SEAT OF AIRCRAFT. A 200 PLUS POUND PERSON PUT ON SEAT BELT, AND WHILE MOVING AROUND, BE LT WOULD LOOSEN UP NUMEROUS TIMES. NO CURLING EFFECT ON BELT. P/N LL01-AL24AB40AA-001. 1 H 7 1 3O NT 3A12 1998091100070 19980911 00070 WP 1998 9 11 TWAA9814101 1 19980901 A 2150 20220142 VALVE DOUG DC9 DC941 302207N WP RT PACK WORN A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 935L 47603 CREW REPORTED SLOW PRESSURIZATION LOSS IN FLIGHT. REGAINED CABIN PRESSURIZATION IN DESCENT FROM BETWEEN 11000 AND 16000 FT. FLIGHT RETURNED TO STL. REPLACED RT PACK FLOW CONTROL VALVE, 2022014-2, AND PRESS RATIO SHUT OFF VALVE, 392714-1- 1. CHECK-C 6-24-97 STL. 2 L 7 2 4F A6WE 1998091100071 19980911 00071 WP 1998 9 11 TWAA9814102 1 19980901 A 2910 61971 FUSE DOUG DC9 DC983 3022083 WP RT HYD SYST FAILED A TWAA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 CE 05 9306T 49567 THE RT HYD SYSTEM FAILED DURING GEAR RETRACTION AFTER TAKEOFF. COMPLETE FLUID LOSS FROM RT SIDE. RT HYD PUMP LATER FAIL ED. FLT RETURNED TO STL. REPLACED NR 3 BRAKE HYD FUSE LIMITER AS INITIAL CAUSE. CHECK-C 3-16-98 MCI. 2 L 7 2 4F RT A6WE 1998091100072 19980911 00072 NM 1998 9 11 TWAA9814103 1 19980826 A 5753 SKIN BOEING 767 7673Y0 NM NR 3 TE FLAP DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING CHECK-C MAINT, FOUND RT WING NR 3 FWD FLAP TE WEDGE LOWER SURFACE HAD 4 IN BY 5 IN BY .0625 IN DEEP DENT LOCATED 9 IN OTBD OF INBD END. REPAIRED DAMAGED AREA PER SRM 51-70-0 WITH PATCH 4 IN BY 12 IN, AND PAINTED AREA. 2 L 7 2 4F RT A1NM 1998091100073 19980911 00073 NM 1998 9 11 TWAA9814104 1 19980826 A 5753 SKIN BOEING 767 7673Y0 NM NR 3 TE FLAP DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING CHECK-C, MAINT FOUND 5 IN BY 4 IN BY .0625 IN DEEP DENT IN RT WING TE FLAP NR 3, FWD OF AFT FLAP, FWD FLAP TE WED GE LOWER SURFACE 33 IN FROM INBD END. FABRICATED PATCH 5 IN BY 5 IN AND INSTALLED PER SRM 51-70-05 AND PAINTED AREA. 2 L 7 2 4F RT A1NM 1998091100074 19980911 00074 NM 1998 9 11 TWAA9814105 1 19980826 A 5753 SKIN BOEING 767 7673Y0 NM NR 3 TE FLAP DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 DURING CHECK-C, MAINT FOUND RT WING NR 3 TE FLAP, AFT WEDGE LOWER SURFACE HAD 2 IN BY 4 IN DENT LOCATED 26 IN FROM INBD END. FABRICATED 4 IN BY 5 IN PATCH AND INSTALLED PER SRM 51-70-05 AND PAINTED AREA. 2 L 7 2 4F RT A1NM 1998091100075 19980911 00075 WP 1998 9 11 TWAA9814106 1 19980829 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 160-200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 992Z 47095 DURING CHECK-C, FOUND LONGERON 4L CRACKED AT STA 160 AND 200. CRACKED ONE INCH AT EACH LOCATION. REMOVED AND REPLACED SECTION OF LONGERON AND FASTENERS. INSTALLED PER SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998091100076 19980911 00076 WP 1998 9 11 TWAA9814107 1 19980828 A 5220 PAN DOUG DC9 DC951 3022051 WP LT EMER EXIT DR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 DURING CHECK-C, MAINT FOUND INTERIM REPAIR INSTALLED PER ARA 11885 AT THE LT AFT EMERGENCY EXIT DOOR PAN. REPLACED SECT ION OF PAN PER SRM 52-05, FIG 51. 2 L 7 2 4F RT A6WE 1998091100077 19980911 00077 WP 1998 9 11 TWAA9814108 1 19980828 A 5220 PAN DOUG DC9 DC951 3022051 WP RT EMER EXIT DR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 DURING CHECK-C, MAINT FOUND INTERIM REPAIR INSTALLED PER ARA 11885 AT RT AFT EMERGENCY EXIT DOOR PAN. REPLACED SECTION OF PAN PER SRM 52-05, FIG 51. 2 L 7 2 4F RT A6WE 1998091100078 19980911 00078 WP 1998 9 11 TWAA9814109 1 19980821 A 7120 ANGLE DOUG DC9 DC951 3022051 WP ENGINE MOUNT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 DURING CHECK C, MAINT FOUND CRACKED SUPPORT ANGLE INSIDE ACCESS PLATE NR 8111A AT UPPER AFT ENG MOUNT. MADE AND INSTAL LED NEW SUPPORT ANGLE WITH EXISTING ORIGINAL HARDWARE AFTER PRIMING. 2 L 7 2 4F RT A6WE 1998091100079 19980911 00079 NM 1998 9 11 K3HA980102 1 19980829 A 3350 1000679 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 L-1 EXIT DOOR PORTABLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED L-1 EXIT DOOR PORTABLE EMERGENCY LIGHT REF MM 33-50-0 1. 2 L 7 3 4F A3WE 1998091100080 19980911 00080 NM 1998 9 11 K3HA980103 1 19980829 A 3350 38931002 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 AFT STAIR EMERGENCY PATH LIGHT INOP. FOUND BATTERIES INOP, REPLACED BATTERIES, BATTERY NICAD P/N 211-9324, S/N NOV-26, OPS CHECK OK REF 33-59. 2 L 7 3 4F A3WE 1998091100081 19980911 00081 NM 1998 9 11 K3HA980104 1 19980829 A 3350 20131A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 CENTER AISLE EMERGENCY PATH BATTERY PACK INOP. REMOVED AND REPLACED BATTERY PACK FOR EMERGENCY PATH LIGHT PER MM 33-51- 0. OPS CHECKS OK. 2 L 7 3 4F A3WE 1998091100082 19980911 00082 WP 1998 9 11 IXXA9800068 1 19980828 A 3260 H146 SWITCH DOUG DC8 DC862 3021970 WP LT GEAR DEFECTIVE A IXXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 728PL 74987 1152 45918 EN ROUTE FROM BWI TO WRI, WHEN THE LANDING GEAR WAS RETRACTED, THE LANDING GEAR UNSAFE LIGHT REMAINED ON. THE CREW CYCL ED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT CONTINUED TO WRI FOR AN UNEVENTFUL LANDING. MAINT ENANCE INSPECTED THE LANDING GEAR AND INDICATION SYSTEMS LOCATING A DEFECTIVE LEFT MAIN GEAR UPLATCH SWITCH. MAINTENANC E REPLACED THE SWITCH IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL AND A SUCCESSFUL OPERATIONAL CHECK RETURNED THE AIRCRAFT TO SERVICE. 2 L 7 4 4F 4A25 1998091100083 19980911 00083 WP 1998 9 11 CALA9801597 1 19980831 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14818 49478 THE FORCE REQUIRED TO PULL TAILCONE EXTERIOR RELEASE HANDLE FROM CLIPS WAS UNDER 25 POUNDS. THE CLIPS AND SUPPORTS WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998091100084 19980911 00084 WP 1998 9 11 CALA9801598 1 19980901 A 2910 HYD LINE DOUG DC9 DC982 3022082 WP RT TR UNIT LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 57837 49582 THE RT HYDRAULIC PRESSURE LOW LIGHT AND MANUAL RUDDER CONTROL LIGHT ILLUMINATED DURING CLIMB OUT OF ANC. THE RT HYDRAUL IC PUMP PRESSURE WAS ZERO WITH QUANTITY DECREASING. THE HYDRAULIC QUANTITY LOSS CHECKLIST WAS ACCOMPLISHED AND THE AIRC RAFT LANDED AT SEA WITHOUT INCIDENT. MAINTENANCE FOUND B-NUT TO HYDRAULIC PRESSURE LINE FROM ENGINE TO RIGHT THRUST REV ERSER MODULE HAD COME OFF. THE HYDRAULIC LINE WAS SECURED AND THE ENGINE WAS RUN WITH NO LEAKS NOTED. THE RT MLG DOOR SKID AND SKIN WERE DAMAGED. THE DOOR WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 52-01, 52-84-0, AND MM 32-12-00. OP ERATION OF THE DOOR CHECKED GOOD. 2 L 7 2 4F A6WE 1998091100085 19980911 00085 NM 1998 9 11 CALA9801599 1 19980901 A 2751 285N001140 FSEU BOEING 757 757224 1384958 NM E/E BAY INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 13110 11724 27300 BOTH THE LE AND TE AMBER LIGHTS ILLUMINATED AND BOTH LE AND TE DISAGREE EICAS MESSAGES ILLUMINATED AFTER SELECTING FLAPS 25 FROM FLAPS 20 ON APPROACH TO EWR. ALTERNATE FLAPS WERE USED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 FSEU AT FAULT. THE NR 1 FSEU WAS REMOVED AND REPLACED. BITE TEST WAS GOOD. THE FLAPS WERE SUCCESSFULLY CYCLED SEVERAL TIMES. A FLAP LOAD LIMIT TEST AND LEFT AND RIGHT ADC TEST WERE PERFORMED AND ALL TESTS WERE GOOD. 2 L 7 2 4F RT A2NM 1998091100086 19980911 00086 WP 1998 9 11 CALA9801600 1 19980901 A 3260 POSITION SWITCH DOUG DC9 DC932 3022066 WP NLG INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14534 47110 THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. QRH PROCEDURE WAS FOLLOWED, BUT GREEN LIGHT STILL DID NOT ILLUMINATE. THE NOSE GEAR WAS VISUALLY CONFIRMED DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDE NT. THE NLG DOWNLOCK SWITCH AND CANNON PLUG WERE INSPECTED AND THE PLUG INSULATION APPEARED DAMAGED. THE POSITION SWIT CH AND CANNON PLUG WERE REMOVED AND REPLACED. THE GEAR WAS SWUNG SEVERAL TIMES IAW MM 32-60-1 AND NO DEFECTS WERE NOTED . 2 L 7 2 4F A6WE 1998091100087 19980911 00087 WP 1998 9 11 CALA9801601 1 19980831 A 5512 SKIN DOUG DC10 DC1030 3023501 WP RT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 19072 46576 INSPECTION FOUND A 1 CRACK IN SKIN OF RT HORIZONTAL STABILIZER LEADING EDGE ON SECOND SECTION NEAR THE LOWER EXTERNAL CO RNER. THE AREA WAS REPAIRED IAW ECRA 5513-01001. 2 L 7 3 4F A22WE 1998091100088 19980911 00088 NM 1998 9 11 CALA9801602 1 19980831 A 5320 CLIP BOEING 737 7372C0 1384488 NM BS 277 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND SHEAR CLIP CORRODED AT STA 277, LBL 17. THE SHEAR CLIP WAS REMOVED AND REPLACED IAW SRM 53-10-2 AND 51 -30-2. 2 L 7 2 4F A16WE 1998091100089 19980911 00089 NM 1998 9 11 CALA9801603 1 19980901 A 5313 LONGERON BOEING 737 7372C0 1384488 NM BS 287 DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND NLG WHEEL WELL LONGERON 28L DELAMINATED AT BS 287. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-30 -2, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 2 4F A16WE 1998091100090 19980911 00090 NM 1998 9 11 CALA9801604 1 19980901 A 5320 ANGLE BOEING 737 7372C0 1384488 NM BS 277 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND VERTICAL ANGLE CORRODED AT FS 277. THE VERTICAL ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998091100091 19980911 00091 NM 1998 9 11 CALA9801605 1 19980901 A 5753 WEB BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT WING O/B MID FLAP INBOARD WEB CRACKED AT INBOARD JACKSCREW FAIRING MOUNT BRACKET. THE CRACK WAS .75 LONG. THE CRACKED AREA WAS REMOVED. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, 57-50-1, 51-10-2, 51-30-2, AND MM 51-20- 11. 2 L 7 3 4F A3WE 1998091100092 19980911 00092 NM 1998 9 11 CALA9801606 1 19980901 A 5350 FAIRING BOEING 727 727232 1384082 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK AT NUT PLATE HOLE OF LT BODY FAIRING PANEL NR 3337. THE CRACKED SECTION WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 53-40-3, FIGURE 1, 51-10-2, 51-30-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998091100093 19980911 00093 NM 1998 9 11 CALA9801607 1 19980901 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND TOP OF FLOORBEAM CORRODED AT FS 328, LBL 29.5. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT. REPAIR PARTS WERE INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100094 19980911 00094 NM 1998 9 11 CALA9801608 1 19980901 A 7110 COWL BOEING 727 727232 1384082 NM NR 3 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 BY .25 INCH PIECE OF SKIN CRACKED OUT BY NOSE COWL OF NR 3 ENGINE UPPER FORWARD END OF FIXED COWL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-2, 51-10-2, 51-20-4, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100095 19980911 00095 NM 1998 9 11 CALA9801609 1 19980901 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 360-380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND STRINGER 21R CORRODED BETWEEN STA 360 AND 380. THE CORRODED AREA WAS CUT OUT AND A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3 AND 53-10-4. 2 L 7 3 4F A3WE 1998091100096 19980911 00096 WP 1998 9 11 CALA9801610 1 19980901 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 2 INCH CRACK IN LONGERON 17L AT ANGLE MOUNT, STA 965. THE CRACKED SECTION OF LONGERON WAS CUT OUT IA W SRM 53-02, FIGURE 18. A NEW LONGERON SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998091100097 19980911 00097 NM 1998 9 11 CALA9801611 1 19980901 A 5313 LONGERON BOEING 727 727232 1384082 NM BS 965 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK LONGERON 13R AT ATTACH ANGLE, STA 965. THE CRACKED AREA WAS CUT OUT IAW SRM 53-02, FIGU RE 18. A REPAIR LONGERON AND TWO SPLICES WERE INSTALLED IAW SRM 51-30. 2 L 7 3 4F A3WE 1998091100098 19980911 00098 NM 1998 9 11 CALA9801612 1 19980901 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN FORWARD END OF LT OUTBOARD SEAT TRACK AT STA 344. THE SEAT TRACK WAS REMOVED AND A N EW SEAT TRACK WAS INSTALLED IAW SRM 53-10-5, FIGURE 7. 2 L 7 3 4F A3WE 1998091100099 19980911 00099 NM 1998 9 11 CALA9801613 1 19980901 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK AT FASTENER ON OUTBOARD SKIN APPROXIMATELY 28 INCHES FROM AFT END OF RT OUTBOARD MID FLA P OUTBOARD JACKSCREW FAIRING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998091100100 19980911 00100 NM 1998 9 11 CALA9801614 1 19980901 A 5311 FRAME BOEING 727 727232 1384082 NM BS 340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT FUSELAGE FRAME CORRODED AT STA 340. THE CORRODED AREA WAS REMOVED. REPAIR PARTS WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-02, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100101 19980911 00101 NM 1998 9 11 CALA9801615 1 19980901 A 5520 ANGLE BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1.5 INCH CRACK IN LT ELEVATOR ATTACH ANGLE. AN ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091100102 19980911 00102 NM 1998 9 11 CALA9801616 1 19980902 A 2910 FLEX LINE BOEING 727 727227 1384078 NM ELEVATOR PCU FAILED A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 09 15774 21242 THE A HYDRAULIC SYSTEM WAS LOST AFTER TAKEOFF FROM IAH. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDE NT. MAINTENANCE FOUND A HOLE IN ELEVATOR LEFT PCU PRESSURE FLEX LINE. THE FLEX LINE WAS REMOVED AND REPLACED. IN ADDI TION, THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. THE HYDRAULIC SYSTEM W AS SERVICED TO FULL. OPERATIONAL CHECKS WERE GOOD WITH NO LEAKS NOTED. 2 L 7 3 4F A3WE 1998091100103 19980911 00103 NM 1998 9 11 CALA9801617 1 19980901 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 727 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14241 20070 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE KEEL BEAM LOWER SKIN AT STA 727, RBL 5. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-03, FIGURE 40. 2 L 7 2 4F A16WE 1998091100104 19980911 00104 NM 1998 9 11 CALA9801618 1 19980902 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 304-280 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND COCKPIT FLOOR PANEL ATTACH ANGLE CORRODED AT BS 304-280, WL 208.1, LBL 40. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091100105 19980911 00105 WP 1998 9 11 CALA9801619 1 19980902 A 5312 BULKHEAD STRAP DOUG DC9 DC932 3022066 WP BS 737 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1 INCH CRACK IN LOWER SUPPORT STRAP OF FORWARD BULKHEAD WALL IN AFT PIT, FS 737. THE SUPPORT STRAP W AS REMOVED AND A NEW SUPPORT STRAP WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1998091100106 19980911 00106 WP 1998 9 11 CALA9801620 1 19980902 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1062 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A .25 INCH CRACK AT FASTENER IN TAIL SECTION SKIN AT STA 1062 APPROXIMATELY FOUR INCHES BELOW LONGERON 15L. THE FASTENER WAS REMOVED IAW SRM 51-30-2 AND THE CRACKED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 28. A DOUBLER REP AIR WAS INSTALLED IAW 51-10-3. 2 L 7 2 4F A6WE 1998091100107 19980911 00107 WP 1998 9 11 CALA9801621 1 19980902 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 370 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND WEB CORRODED AT FORWARD CARGO DOOR, STA 370, STRINGER 28R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-0 1, FIGURE 2. 2 L 7 2 4F A6WE 1998091100108 19980911 00108 EA 1998 9 11 COMA9860247 1 19980902 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR LACK OF LUBE A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 973CA 7146 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. LUBED OUTER HANDLE LATCH BUTTON. A/C RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1998091100109 19980911 00109 1998 9 11 COMA9860248 4 19980902 A 3417 8220372115 ADC CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA K NONE O OTHER CL CLIMB 1 SO 01 940CA 11656 527 7048 EFIS COMP MON AND AIRSPEED WARNINGS. REPLACED THE NR 2 ADC. 2 L 7 2 4F RT A21EA 1998091100110 19980911 00110 EA 1998 9 11 COMA9860249 1 19980821 A 5753 601R1430342 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 C-CHECK INSPECTION, RIGHT INBD FLAP VANE LEADING EDGE HAS CHAFE DAMAGE. REPLACED FLAP VANE LEADING EDGE. 2 L 7 2 4F RT A21EA 1998091100111 19980911 00111 EA 1998 9 11 COMA9860250 1 19980821 A 5753 601R1430341 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP VANE CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 912CA 7011 C-CHECK INSPECTION, LEFT INBD FLAP VANE HAS CHAFE DAMAGE. REPLACED FLAP VANE LEADING EDGE. 2 L 7 2 4F RT A21EA 1998091100112 19980911 00112 NE 1998 9 11 COMA9860251 2 19980901 A 7230 COMPRESSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE DIRTY A COMA C D ABORTED TAKEOFF RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 SO 01 917CA 7017 807076 DURING TAKEOFF, RT ENGINE ITT REACHED 900 DEGREES. TAKEOFF ABORTED. COMPRESSOR WASH ENGINE AND FOUND ITT WITHIN LIMITS . 2 L 7 2 4F 4 F RT A21EA E15NE 1998091100113 19980911 00113 EA 1998 9 11 COMA9860252 1 19980901 A 3350 60205 SIGN CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 965CA 7131 EMERGENCY EXIT SIGN AT GALLEY SERVICE DOOR IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4F RT A21EA 1998091100114 19980911 00114 NM 1998 9 11 QXEA9801203 1 19980826 A 2612 CIRCUIT BREAKER DHAV DHC8 DHC8202 2809007 NM NR2 ENG FIRE DET TRIPPED A QXEA K NONE J WARNING INDICATION UK UNKNOWN 1 NM 09 361PH 516 EAT- NR 2 ENGINE FIRE DETECTION FAULT B LIGHT ILLUMINATED. FOUND CIRCUIT BREAKER FOR FIRE DETECTOR POPPED. RESET CIRCU IT BREAKER. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998091100115 19980911 00115 1998 9 11 QXEA9801204 2 19980901 A 7532 310848803 VALVE DHAV DHC8 DHC8202 2809007 NM ENG P2.5/P3 MALFUNCTION A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 355PH 500 PDX - STRONG ACRID SMELL NOTICED FROM THE VENTILATION SYSTEM. REPLACED THE P2.5/P3 SWITCHING VALVE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998091100116 19980911 00116 WP 1998 9 11 98FDEA00538 1 19980901 A 5414 ACCESS PANEL DOUG DC10 DC1010F 3022111 WP NR 3 PYLON TORN A FDEA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SO 25 049FE 47803 98-213 - NR 3 ENG PYLON PNL 400GL TORN OFF ON INBD SIDE. AIRCRAFT LANDED EWR WITHOUT INCIDENT. REPLACED ACCESS PANEL. ALL NUTPLATES APPEAR TO BE IN GOOD WORKING ORDER. 2 L 7 3 4F A22WE 1998091100117 19980911 00117 NM 1998 9 11 98FDEA00539 1 19980902 A 5753 6521634148 SKIN BOEING 727 727247 138408F NM RT TE AFT FLAP DELAMINATED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 NR 0243 - RIGHT WING INBD AFT FLAP IS DELAMINATED AND DAMAGED AT INBD AND OUTBD ENDS. 2 L 7 3 4F A3WE 1998091100118 19980911 00118 NM 1998 9 11 98FDEA00540 1 19980902 A 5320 651986219 CHORD BOEING 727 727247 138408F NM BS 312-351 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 CORROSION (C53-111-03-1/2) IN NUMEROUS AREAS OF MID NOSE CHORD HORIZ FLANGE BS 312 TO 351, LBL 15, WL 169. *S/D* REMOV ED AND REPLACED NOSE CHORD BS 294 TO 351, WL 169, LBL 16 IAW DRW 65-18415 AND FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1998091100119 19980911 00119 WP 1998 9 11 98FDEA00541 1 19980901 A 5754 FAIRING DOUG DC10 DC1010F 3022111 WP NR 1 LE SLAT DEPARTED A FDEA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 25 057FE 48264 98-214 - LT WING NR 1 SLAT WING TO BODY FAIRING DEPARTED A/C ON ROTATION OUT OF MEM. 2 L 7 3 4F A22WE 1998091100120 19980911 00120 WP 1998 9 11 MWEA98947 1 19980831 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 502ME 48132 FOUND FORWARD EMERGENCY ENTRANCE LIGHT INOP. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY ENTRANCE LIGHT ASSEMBLY . 2 L 7 2 4F A6WE 1998091100121 19980911 00121 WP 1998 9 11 MWEA98948 1 19980901 A 2560 113319 COVER DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 THE FORWARD GALLEY SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED THE SLIDE COVER. 2 L 7 2 4F A6WE 1998091100122 19980911 00122 SO 1998 9 11 SWIA971241 1 19980604 A 5320 SILL EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LAVATORY DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 189SW 120048 RIGHT FORWARD SILL BY LAVATORY HAS CORROSION. REMOVED AND REPLACED THE RIGHT FORWARD SILL IAW SRM 51-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998091100123 19980911 00123 EA 1998 9 11 SWIA971242 1 19980809 A 5320 SILL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE SERVICE DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CORROSION AROUND SERVICE DOOR SILL AREA ON ANGLES. REMOVED AND REPLACED SERVICE DOOR SILL AREA ANGLE IAW CJR SRM 51-00- 00. 2 L 7 2 4F 4 F RT A21EA E15NE 1998091100124 19980911 00124 EA 1998 9 11 SWIA971243 1 19980809 A 5320 SILL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PAX DOOR CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 412SW 7101 CORROSION AROUND PASSENGER DOOR SILL AREA ON ANGLES. REMOVED AND REPLACED PASSENGER DOOR SILL AREA ANGLE IAW EMB SRM 51 -00-00. 2 L 7 2 4F 4 F RT A21EA E15NE 1998091100125 19980911 00125 EA 1998 9 11 SWIA971244 1 19980804 A 5320 STRAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BS 280-400 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 408SW 7055 THERE IS CORROSION IN A NUMBER OF PLACES IN BUTT STRAPS RBL 9, RBL 27, LBL 27 FROM STATION 280, STATION 400. REMOVED A ND REPLACED BUTT STRAP, REMOVED CORROSION ON OTHER AREAS, IAW SRM 51-10-00. 2 L 7 2 4F 4 F RT A21EA E15NE 1998091100126 19980911 00126 EA 1998 9 11 SWIA971245 1 19980802 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BS 330 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 AREA AROUND NUT PLATE LBL 27, FS 330 INBOARD SIDE HAS CORROSION OUT OF LIMITS. REPLACED AREA AROUND NUT PLATE IAW MM. 2 L 7 2 4F 4 F RT A21EA E15NE 1998091100127 19980911 00127 EA 1998 9 11 SWIA971246 1 19980802 A 5315 FLOORBEAM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE BS 335 & 345 CORRODED A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 409SW 7056 AREA NEXT TO INSERTS CENTER OF LBL 9, FS 335 AND 345 HAS LIGHT CORROSION. CUT OUT DAMAGED AREA, FABRICATED A L-ANGLE AN D FILLERS AND INSTALLED ON LBL 9, FS 335 AND 345 IAW MM . 2 L 7 2 4F 4 F RT A21EA E15NE 1998091100128 19980911 00128 WP 1998 9 11 ARWA980901 1 19980901 A 2740 909036019 CONTROL CABLE DOUG DC8 DC862 3021970 WP HORIZ STAB TRIM BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 WHEEL LONGITUDINAL TRIM WILL NOT TRIM NOSE UP, SUITCASE HANDLE ARE SPLIT LEFT HANDLE FULL AFT. RIGHT HANDLE IN NEUTRAL POSITION. FOUND LONGITUDINAL TRIM CABLE 113A BROKEN. REMOVED AND REPLACED CABLE IAW DC-8 91-10-0 AND 91-10-2. INSTALL ED CABLE PER MM 27-40-0, ADJUSTMENT, TENSION AND OPS. CHECK OK IAW 27-40-0. ASSY CABLE PER 20-11-0. 2 L 7 4 4F 4A25 1998091100129 19980911 00129 WP 1998 9 11 ARWA980902 1 19980902 A 3260 801813 PROX SWITCH LKHEED 1011 10113851 WP RT MLG DOOR BROKEN A ARWA O OTHER N FALSE WARNING LD LANDING 1 SO 19 308GB 1133 ON LANDING GEAR EXTENSION GOT 3 GREEN, RED DOOR AND IN TRANS, LIGHT ALSO GOT RT GEAR DOOR LIGHT ON F/E ANUNCIATOR. FOUN D RT GEAR DOOR PROX SWITCH BROKEN. REMOVED AND REPLACED PROX SWITCH AND CONDUIT IAW 32-6-1, OPS CHECK NORMAL. 2 L 7 3 4F RC A23WE 1998091100130 19980911 00130 NM 1998 9 11 VNAA9808027 1 19980822 A 3350 321473 POWER SUPPLY DIEHL 321430 DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 433JS 62645 2772 10469 3047 DURING THE PRE-FLIGHT INSPECTION, THE FLOOR PATHWAY EMERGENCY LIGHTING AT ROWS FIVE AND SIX WERE NOTED TO BE INOPERATIVE . MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY FOR THE AFFECTED LIGHTS. OPERATIONAL CHECKS WERE COMPLETED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091100131 19980911 00131 NM 1998 9 11 VNAA9808028 1 19980827 A 6120 WIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE BROKEN A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 433JS 3047 DURING THE TAXI FOR TAKEOFF, THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RETU RNED TO THE GATE. MAINTENANCE INSPECTED AND REPAIRED BROKEN WIRES AT THE OVERSPEED GOVERNOR CANNON PLUG CONNECTOR, IN A CCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-04. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091100132 19980911 00132 NM 1998 9 11 VNAA9808029 1 19980829 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE BIRD STRIKE A VNAA K NONE O OTHER AP APPROACH 1 GL 07 442JS 3060 DURING THE FLAIR FOR LANDING, THE CREW NOTED THAT THE AIRCRAFT MAY HAVE TAKEN A BIRD STRIKE. OUTSTATION MAINTENANCE WAS CALLED OUT TO INSPECT THE AIRCRAFT. OUTSTATION MAINTENANCE INSPECTED AND FOUND REMAINS OF A BIRD STRIKE ON THE FUSELAG E LEFT SIDE SPONSON, BELOW THE LANDING GEAR. THE AREA WAS CLEANED AND INSPECTED, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-29-00. NO FURTHER DAMAGE WAS NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091100133 19980911 00133 NE 1998 9 11 COEA9802711 2 19980612 A 7532 312124803 BLEED VALVE CESSNA 208 208B 2073701 CE PWA PT6 PT6A114 52043 NE ENGINE FAILED A COEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 13 711FX 3145 4Y152 208B0433 19163 PILOT REPORTS AS HE WAS CLIMBING THROUGH 7,000 FEET, 10 MILES NORTH OF THE MFR AIRPORT, HE NOTICED 200 POUND DROP IN TOR QUE AND 40 DEGREE RISE IN ITT. AT THIS TIME, PILOT ELECTED TO RETURN TO MFR. NO EMERGENCY WAS DECLARED. MAINTENANCE T ROUBLESHOT THE SYSTEM AND FOUND A FAILED BLEED VALVE. PART WAS REPLACED. GROUND RUN CHECKED GOOD. AIRCRAFT RETURNED T O SERVICE. (X) 1 H 7 1 3T 3 T A37CE E4EA 1998091100134 19980911 00134 NM 1998 9 11 TCAA9833418 1 19980724 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LOW VOLTAGE CONDITION. OPS CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. TAT: 45,503.9 HOURS. TAC: 60,299. (X) 2 L 7 2 4F A16WE 1998091100135 19980911 00135 NM 1998 9 11 TSAA9833417 1 19980723 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REPLACED NR 1 POSITION EMERGENCY LIGHT ASSY BATTERY PACK DUE TO BEING INOPERABLE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. TAT: 40,564.9 HOURS. TAC: 52,457. (X) 2 L 7 2 4F RT A16WE 1998091100136 19980911 00136 NM 1998 9 11 TSAA9833424 1 19980727 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LOW VOLTAGE CONDITION. OPS CHECK GOOD. AIRCRAFT RETUR NED TO SERVICE. TAT: 45,503.9 HOURS. TAC: 60,299. (X) 2 L 7 2 4F A16WE 1998091100137 19980911 00137 NM 1998 9 11 TSAA9833425 1 19980727 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECKED OK. AIRCRAFT RET URNED TO SERVICE. TAT: 33,645.6 HOURS. TAC: 63,576. (X) 2 L 7 2 4F RT A16WE 1998091100138 19980911 00138 EU 1998 9 11 RAIA980521 1 19980531 A 5210 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR MALFUNCTIONED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 859AE 859 FLT 4705 - PSP - PASSENGER DOOR CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED AND DEFERRED PASSENGER DOOR WARNIN G PER MEL 52-2 CAT C. (M) 2 L 7 2 4T RT A56EU 1998091100139 19980911 00139 EU 1998 9 11 RAIA980605 1 19980610 A 3220 NOSE WHEEL BAG JETSTM JETSTM3201 1500217 EU NLG SEPARATED A RAIA B EMER. DESCENT D INFLIGHT SEPARATION CL CLIMB 1 CE 03 429AM 879 FLT 7438 - STL - LEFT NOSE WHEEL SEPARATED FROM NOSE GEAR AXLE AFTER TAKEOFF, CREW PERFORMED EMERGENCY LANDING. MAINTEN ANCE IS IN WORK. (M) 2 L 7 2 4T RT A56EU 1998091100140 19980911 00140 EU 1998 9 11 RAIA980612 1 19980625 A 3244 31485 TIRE BAG JETSTM JETSTM3201 1500217 EU LT MLG FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 337TE 42 929 FLT 7067 - STL - LEFT MAIN TIRE BLEW OUT ON TAKEOFF ROLL. MAINTENANCE INSPECTED LEFT MAIN WHEEL AXLE FOR DAMAGE, NO DAM AGE NOTED. REPLACED LEFT MAIN WHEEL ASSY. (M) 2 L 7 2 4T RT A56EU 1998091100141 19980911 00141 WP 1998 9 11 HALA9800247 1 19980720 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 10926 47654 HNL - LOG PAGE NR A147940 - PER FLEET CAMPAIGN, THE FOLLOWING EMERGENCY LIGHTS FAILED; FLOOR, FUSELAGE, AFT, OVERWING EX IT AT ROW 17 LT AND RT; OVERWING AT ROW 18 LT AND RT; CABIN, AND TAIL CONE. REPLACED BATTERIES, 3 EACH. REF: OPERATO R CONTROL NR 98ZZZX3285 AND NR 98ZZZX3286. (X) 2 L 7 2 4F RT A6WE 1998091100142 19980911 00142 WP 1998 9 11 98ZZZX3285 1 19980720 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 10928 47654 HNL - LOG PAGE NR A147940 - PER FLEET CAMPAIGN, THE FOLLOWING EMERGENCY LIGHTS FAILED; FLOOR, FUSELAGE, AFT, OVERWING EX IT AT ROW 17 LT AND RT; OVERWING AT ROW 18 LT AND RT; CABIN, AND TAIL CONE. REPLACED BATTERIES, 3 EACH. REF: OPERATOR CONTROL NR HALA9800247 AND NR 98ZZZX3286. 2 L 7 2 4F RT A6WE 1998091100143 19980911 00143 WP 1998 9 11 98ZZZX3286 1 19980720 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 9009 47654 HNL - LOG PAGE NR A147940 - PER FLEET CAMPAIGN, THE FOLLOWING EMERGENCY LIGHTS FAILED; FLOOR, FUSELAGE, AFT, OVERWING EX IT AT ROW 17 LT AND RT; OVERWING AT ROW 18 LT AND RT; CABIN, AND TAIL CONE. REPLACED BATTERIES, 3 EACH. REF: OPERATOR CONTROL NR HALA9800247 AND NR 98ZZZX3285. 2 L 7 2 4F RT A6WE 1998091100144 19980911 00144 WP 1998 9 11 HALA9800257 1 19980722 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 660HA 1304 48122 HNL - LOG PAGE NR A164796/A164794 - PER FLEET CAMPAIGN, OVERHEAD LIGHTS FROM ROWS 13 TO 17 AND AFT TAIL EMERGENCY LIGHTS FAILED CHECK. REPLACED BATTERY, OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1998091100145 19980911 00145 WP 1998 9 11 HALA9800264 1 19980723 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 661HA 47796 HNL - LOG PAGE NR A143926 - EMERGENCY LIGHTS CEILING BATH ABOVE ROW 10 HAS A WEAK BATTERY. REPLACED BATTERY, OPS CHECK GOOD. (X) 2 L 7 2 4F RT A6WE 1998091100146 19980911 00146 NM 1998 9 11 GAIA9864 1 19980623 A 7830 653784279 FAIRING BOEING 727 727223 1384074 NM NR 2 THRUST REV CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6810 19485 DURING ROUTINE C-CHECK, A CRACK WAS FOUND ALONG NR 2 THRUST REVERSER, AFT FAIRING ASSEMBLY AT THE 1:00 O'CLOCK POSITION. THE CRACK WAS STOPPED DRILLED USING AN 0.187 INCH HOLE. THE CRACK WAS THEN NDT TO ENSURE CRACK LIMITATION. REPAIR DO UBLER WAS INSTALLED USING FLIGHT VEHICLES, INC., DRAWING 54-98301-2 REV NEW DATED 6-9-98 BY AAR IN OKLAHOMA CITY. (X) 2 L 7 3 4F A3WE 1998091100147 19980911 00147 NM 1998 9 11 GAIA9868 1 19980623 A 5754 6516227 FLAP BOEING 727 727223 1384074 NM WING CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6810 19485 DURING ROUTINE C-CHECK INSPECTION. CORROSION WAS FOUND ALONG THE NR 1 KRUGER FLAP BULLNOSE WHERE THE JUMPER CABLE IS AT TACHED. THE CORROSION WAS REMOVED BY BLENDING OUT. THE JUMPER ATTACH HOLE WAS RELOCATED IN THE MAIN FLAP BODY FORWARD 1.0 INCH WHILE MAINTAINING A 0.40 INCH EDGE MARGIN. THE AREA WAS REPAIRED IAW BOEING ENGINEERING LETTER AOC-OKC-98-053R R DATED 6-2-98 BY AAR OKLAHOMA CITY. THE AREA WAS RESTORED TO NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998091100148 19980911 00148 WP 1998 9 11 ARWA9807131 1 19980730 A 3231 CONNECTOR DOUG DC8 DC862 3021970 WP LT MLG DOOR LOOSE A ARWA C J ABORTED TAKEOFF DUMP FUEL N FALSE WARNING TO TAKEOFF 1 SO 19 802BN 45909 DAY - FLT 046 - AFTER TAKEOFF, GEAR DOOR NOT LATCH LIGHT ILLUMINATED, ABNORMAL CHECK LIST COMPLETED. DOOR NOT LATCH LIG HT REMAINED ILLUMINATED. RETURNED TO DAY, FUEL DUMPED APPROX 4,000 POUNDS. RESECURED CANNON PLUG ON LT MAIN DOOR SWITC H, CYCLED SYSTEM IAW DC-8 MM 32-60-00. OPS CHECK GOOD ON GROUND. (X) 2 L 7 4 4F 4A25 1998091100149 19980911 00149 1998 9 11 SIMA982094 4 19980728 A 2213 6227491210 FCC SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A A SIMA K NONE F FLT CONT AFFECTED CR CRUISE 1 SW 21 253AE 1935 340B253 LAX - FLT 3386 - UNCOMMANDED PITCH MOVEMENTS IN-FLIGHT WITH OR WITHOUT AUTOPILOT. VERIFIED THE FLAPS DID NOT APPEAR TO BE MOVING. REMOVED AND REPLACED THE FLIGHT CONTROL COMPUTER. OPERATIONAL CHECK AND TEST FLIGHT PERFORMED WITH NO FURTH ER PROBLEMS NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998091100150 19980911 00150 EU 1998 9 11 SIMA982082 1 19980727 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT S53672406208 270 SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX3287 AND 98ZZZX3288. (X) 2 H 7 2 4T RT A53EU 1998091100151 19980911 00151 EU 1998 9 11 98ZZZX3287 1 19980727 A 5315 S5367240725200 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT S53672406208 270 SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA982082 AND 98ZZZX3288. 2 H 7 2 4T RT A53EU 1998091100152 19980911 00152 EU 1998 9 11 98ZZZX3288 1 19980727 A 5315 S5367240825402 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT S53672406208 270 SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAMS 36, 38, AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA982082 AND 98ZZZX3287. 2 H 7 2 4T RT A53EU 1998091100153 19980911 00153 EU 1998 9 11 SIMA982062 1 19980725 A 5347 S53375001212 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX3289 THROUGH NR 98ZZZX3298. (X) 2 H 7 2 4T RT A53EU 1998091100154 19980911 00154 EU 1998 9 11 98ZZZX3289 1 19980725 A 5347 S53375001210 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, 98ZZZX3290 AND NR 98ZZZX3298. 2 H 7 2 4T RT A53EU 1998091100155 19980911 00155 EU 1998 9 11 98ZZZX3290 1 19980725 A 5347 S53570203202 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 AND 98ZZZX3298. 2 H 7 2 4T RT A53EU 1998091100156 19980911 00156 EU 1998 9 11 98ZZZX3291 1 19980725 A 5347 S53678001224 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 98. 2 H 7 2 4T RT A53EU 1998091100157 19980911 00157 EU 1998 9 11 98ZZZX3292 1 19980725 A 5347 S53678001226 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 98. 2 H 7 2 4T RT A53EU 1998091100158 19980911 00158 EU 1998 9 11 98ZZZX3293 1 19980725 A 5347 S53375001210 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 98. 2 H 7 2 4T RT A53EU 1998091100159 19980911 00159 EU 1998 9 11 98ZZZX3294 1 19980725 A 5347 S53678001212 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 98. 2 H 7 2 4T RT A53EU 1998091100160 19980911 00160 EU 1998 9 11 98ZZZX3295 1 19980725 A 5347 S53378001228 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 98. 2 H 7 2 4T RT A53EU 1998091100161 19980911 00161 EU 1998 9 11 98ZZZX3296 1 19980725 A 5347 S53678001245 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 98. 2 H 7 2 4T RT A53EU 1998091100162 19980911 00162 EU 1998 9 11 98ZZZX3297 1 19980725 A 5347 S53570203200 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 98. 2 H 7 2 4T RT A53EU 1998091100163 19980911 00163 EU 1998 9 11 98ZZZX3298 1 19980725 A 5347 S53570203202 SEAT TRACKS AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW - DURING CPCP-4 INSPECTION, FOUND THE LT AND RT FLIGHT ATTENDANT, LT FORWARD INBD AND OTBD, LT MIDDLE AND AFT OTBD, LT AFT INBD, RT AFT CARGO, RT MIDDLE AND AFT OTBD, AND THE RT MIDDLE INBD SEAT TRACKS CORRODED. REMOVED AND REPLACED TH E SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98206-2, AND, NR 98ZZZX3289 THROUGH NR 98ZZZX32 97. 2 H 7 2 4T RT A53EU 1998091100164 19980911 00164 EU 1998 9 11 SIMA982061 1 19980725 A 5730 S524105372000 PANEL AEROSP ATR72 ATR72212 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 DURING CPCP-4 INSPECTION, FOUND THE RT WING FEEDER TANK AND CENTER WING TANK ACCESS PANELS CORRODED. REMOVED AND REPLAC ED BOTH PANELS. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR 98ZZZX3299. (X) 2 H 7 2 4T RT A53EU 1998091100165 19980911 00165 EU 1998 9 11 98ZZZX3299 1 19980725 A 5730 S524105570000 PANEL AEROSP ATR72 ATR72212 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 DURING CPCP-4 INSPECTION, FOUND THE RT WING FEEDER TANK AND CENTER WING TANK ACCESS PANELS CORRODED. REMOVED AND REPLAC ED BOTH PANELS. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SIMA982061. 2 H 7 2 4T RT A53EU 1998091100166 19980911 00166 EU 1998 9 11 SIMA982051 1 19980724 A 5320 S5367131826001 ZEE MEMBER AEROSP ATR72 ATR72212 EU BS 39-40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW DURING MBV-1 INSPECTION, FOUND THE LT AND RT AFT ZEE MEMBERS AND LT WEB BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED BOTH ZEE MEMBERS AND WEB. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX3300 AND NR 98ZZZX33 01. (X) 2 H 7 2 4T RT A53EU 1998091100167 19980911 00167 EU 1998 9 11 98ZZZX3300 1 19980724 A 5320 S53678008200 ZEE MEMBER AEROSP ATR72 ATR72212 EU BS 39-40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW DURING MBV-1 INSPECTION, FOUND THE LT AND RT AFT ZEE MEMBERS AND LT WEB BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED BOTH ZEE MEMBERS AND WEB. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98205-1 AND NR 98ZZZX3 301. 2 H 7 2 4T RT A53EU 1998091100168 19980911 00168 EU 1998 9 11 98ZZZX3301 1 19980724 A 5320 S53671217204 ZEE MEMBER AEROSP ATR72 ATR72212 EU BS 39-40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 270AT 270 SAW DURING MBV-1 INSPECTION, FOUND THE LT AND RT AFT ZEE MEMBERS AND LT WEB BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED BOTH ZEE MEMBERS AND WEB. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA98205-1 AND NR 98ZZZX3 300. 2 H 7 2 4T RT A53EU 1998091100169 19980911 00169 NM 1998 9 11 TSAA9833437 1 19980729 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED BATTERY IN NR 2 POSITION FLOOR PROXIMITY LIGHT ASSY DUE TO BEING INOPERABLE. OPS CHECKED OK. AIRCRAFT RETURNE D TO SERIVCE. TAT: 47,255.7 HOURS. TAC: 62,000. (X) 2 L 7 2 4F A16WE 1998091100170 19980911 00170 NM 1998 9 11 TSAA9833413 1 19980627 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY IN NR 6 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOPERABLE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. TAT: 43,068.7 HOURS. TAC: 59.345. (X) 2 L 7 2 4F A16WE 1998091100171 19980911 00171 NM 1998 9 11 TSAA9833414 1 19980722 A 3350 873100151 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. AIRCRAFT RETURNED TO SERVICE. TAT: 31,618 .2 HOURS. TAC: 38,510. (X) 2 L 7 2 4F RT A16WE 1998091100172 19980911 00172 NM 1998 9 11 TSAA9833415 1 19980722 A 3350 873100151 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 1 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . TAT: 31,618.2 HOURS. TAC: 38,510. (X) 2 L 7 2 4F RT A16WE 1998091100173 19980911 00173 NM 1998 9 11 TSAA9833416 1 19980722 A 3350 873100151 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPALCED NR 2 SEAT EMERGENCY LIGHT BATTERY PACKS DUE TO UNIT WILL NOT TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE . TAT: 31,618.2 HOURS. TAC: 38,510. (X) 2 L 7 2 4F RT A16WE 1998091100174 19980911 00174 NM 1998 9 11 USAASB98199 1 19980730 A 2613 6131508551 HARNESS BOEING 737 7373B7 1384580 NM NR 2 ENGINE FAILED A USAA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 19 390US 23312 IAH - FLT 1934 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE OVERHEAT LIGHT AND THE MASTER CAUTION LIGHT ILLUMINATED. CREW W ENT THROUGH EMERGENCY PROCEDURES, DISCHARGED BOTH ENGINE FIRE BOTTLES AND SHUT DOWN THE NR 2 ENGINE. FLIGHT RETURNED TO FIELD AT IAH AND LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGI NE TIME WAS 17 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE CORE HARNESS AND THE TWO ENGINE FIRE BOTTLES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998091100175 19980911 00175 NM 1998 9 11 USAA980321 1 19980730 A 5320 ANGLE BOEING 737 737301 1384611 NM BS 1092 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 32422 23553 CLT - DURING A PILOT'S REPORT READING VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH WARP. SPLICED IN NEW SECTION OF CHORD ANGLE PER SRM 53-80-13 AND BAC DRAWING 65-46579. (X) 2 L 7 2 4F RT A16WE 1998091100176 19980911 00176 NM 1998 9 11 USAA980322 1 19980730 A 5313 6541579552 STRINGER BOEING 737 737301 1384611 NM BS 1113 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 350US 32422 23553 CLT - DURING A PILOT'S REPORT READING INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION. REPLACED WITH IDENTICAL P ART PER BAC DRAWING 65-46579. (X) 2 L 7 2 4F RT A16WE 1998091100177 19980911 00177 NM 1998 9 11 EIAA980232 1 19980722 A 2613 ENGINE BOEING 747 747273C 1384896 NM NR 1 NACELLE OVERTEMP A EIAA E ENGINE SHUTDOWN M J Y OVER TEMP WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 NM 09 470EV 20653 JFK - LOG PAGE: F73265 - EN ROUTE FROM KLCK TO KJFK, NR 1 ENGINE NACELLE TEMP WENT TO 720 DURING CLIMB, INCREASED TO 82 0. ACCOMPLISHED NAC OVERTEMP PROCEDURE, NO HELP. ACCOMPLISHED IN-FLIGHT SHUT DOWN CHECK LIST. WINDMILL TIME, 1 HOUR N AC TEMP, WENT TO ZERO AFTER SHUT DOWN, POSITIVE OIL PRESSURE. (X) 2 L 7 4 4F A20WE 1998091100178 19980911 00178 NM 1998 9 11 P2EA98148 1 19980731 A 3250 BACC10AP38787 CONTROL CABLE BOEING 737 737222 1384473 NM NLG STEERING BROKEN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 209US 19548 MDW - FLT 821 - NOSE WHEEL STEERING FAILED ON TAXI, PRIOR TO DEPARTURE. MAINTENANCE FOUND NOSE WHEEL STEERING CABLE BRO KEN. CABLE WAS REPLACED AND SYSTEM TESTED GOOD IAW MM 32-51-31A AND MM 32-51-0. (X) 2 L 7 2 4F A16WE 1998091100179 19980911 00179 NM 1998 9 11 P2EA98147 1 19980802 A 5744 FITTING BOEING 737 737247 138448D NM SPOILER CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - C-CHECK ITEM - OUTBOARD SUPPORT FITTING RT WING SPOILER NR 5 CRACKED. DEFECT SIZE L = 2.5 INCHES. REPLACED NR 5 GROUND SPOILER OUTBOARD HINGE PER SRM 51-10-1 PAGE 5. FABRICATED FITTING PER COOPESA E.O. COO3-57-377-98 DATED DOCUMENT ED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER ROBERT M MANASH, DESIGNATION SW-180. SEE COOPESEA W.O. L1-061 6-6-67, VAM 100 NR 602. (X) 2 L 7 2 4F A16WE 1998091100180 19980911 00180 NM 1998 9 11 P2EA98146 1 19980711 A 5320 PRESSURE WEB BOEING 737 737247 138448D NM BS 278 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - C-CHECK ITEM - NOSE LANDING GEAR WHEEL WELL CRACKED AT BS 278, WL 200, RBL 7. DEFECT SIZE L- 2.5 INCHES. REPAIRE D NOSE WHEEL WELL UPPER WEB SECTION AT BS 274 THROUGH BS 281, RBL 6 INCHES AND RBL 14 INCHES PER COOPSEA E.O. COO3-53-36 998 DATED JULY 21, 1998, AND BOEING FAX COO-SJO-98-0488RR DATED 7-20-98. DOCUMENTED ON FAA FORM 8110-3. APPROVED AND SU BMITTED BY FAA DER B.R. FRAKES DESIGNATION NM02256 DATED JULY 24, 1998. SEE COOPSEA W.O. L1-0616-1-42, VAM 100 NR 361. (X) 2 L 7 2 4F A16WE 1998091100181 19980911 00181 NM 1998 9 11 P2EA98142 1 19980721 A 5330 SKIN BOEING 737 737247 138448D NM BS 294 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - C-CHECK ITEM. REF: VAM 54 NR 050, REPLACED TIME LIMITED SKIN REPAIR AT BS 294, STR 23R. INSTALLED PERMANENT REP AIR AT BS 281 THROUGH BS 298 BETWEEN STR 21R AND STR 24R PER SRM 53-30-3 FIG 1. SEE COOPESA W.O. L1-0616-9-9, VAM 54 NR 50. (X) 2 L 7 2 4F A16WE 1998091100182 19980911 00182 NM 1998 9 11 P2EA98141 1 19980712 A 5720 STIFFENER BOEING 737 737247 138448D NM WS 395 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - C-CHECK ITEM - RIGHT WING L/E CAVITY WBL 321. FSS 395, STIFFENER CRACKED. DEFECT SIZE L=0.950 INCH. REPLACED CR ACKED ANGLE AT FRONT SPAR, BS 395 PER SRM 51-10-1 PAGE 5, AND SRM 51-30-2. SEE COOPESA W.O. L1-0616-6-40, VAM 100 NR 28 9. (X) 2 L 7 2 4F A16WE 1998091100183 19980911 00183 NM 1998 9 11 P2EA98140 1 19980711 A 5330 DOUBLER BOEING 737 737247 138448D NM BS 178 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - C-CHECK ITEM. FUSELAGE SKIN REPAIR DOUBLER MISSING MATERIAL AT BS 178. ACCOMPLISHED PREVENTATIVE MODIFICATION ON FUSELAGE CONTROL CABIN SKIN AT WINDSHIELD CENTER POST PER SB 737-53-1059 SECT 3, FIG 2, DATED ON 11-17-80, REV 1 DATED 5-17-90. SEE COOPESA W.O. L1-0616-1-69, VAM 100 NR 402. (X) 2 L 7 2 4F A16WE 1998091100184 19980911 00184 NM 1998 9 11 P2EA98139 1 19980712 A 5330 SKIN BOEING 737 737247 138448D NM BS 977-998 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - C-CHECK ITEM. FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR (L2) CUT OUT BETWEEN BS 977 AND BS 998, STR 15L THROUGH STR 18L. REPAIRED SKIN SECTION BETWEEN BS 977 AND BS 998, STR 15L THROUGH STR 18L PER BOEING FAX COO-SJO-98-0494RR. DOCUM ENTED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER D.L. JENSEN DESIGNATION NR NM-2605 DATED JULY 28, 1998. SE E COOPESA W.O. L1-0616-2-170, VAM 100 NR 443. (X) 2 L 7 2 4F A16WE 1998091100187 19980911 00187 NM 1998 9 11 P2EA98138 1 19980714 A 5313 STRINGER BOEING 737 737247 138448D NM BS 529 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 SJO - C-CHECK ITEM - FUSELAGE STRINGER 10L CRACKED AT BS 529.5. DEFECT SIZE L - 0.095 INCH. REPAIRED STRINGER 10L BETW EEN BS 278 AND BS 302 PER SRM 53-10-3 FIG 3 SHEET 4. SEE COOPESA W.O. L1-0616-2-204, VAM 100 NR 555. (X) 2 L 7 2 4F A16WE 1998091100188 19980911 00188 WP 1998 9 11 HALA9800265 1 19980724 A 3350 6011777 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 699HA 576 47763 HNL - LOG PAGE NR A147883/147884 - PER FLEET CAMPAIGN, FUSELAGE EXTERIOR AND AFT ACCY EMERGENCY LIGHTS FAILED TEST. REP LACED BATTERY, OPS CHECK GOOD. REF: OPERATOR CONTROL NR 98ZZZX3304. (X) 2 L 7 2 4F RT A6WE 1998091100189 19980911 00189 WP 1998 9 11 98ZZZX3304 1 19980724 A 3350 6011777 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 699HA 599 47763 HNL - LOG PAGE NR A147883/147884 - PER FLEET CAMPAIGN, FUSELAGE EXTERIOR AND AFT ACCY EMERGENCY LIGHTS FAILED TEST. REP LACED BATTERY, OPS CHECK GOOD. REF: OPERATOR CONTROL NR HALA9800265. 2 L 7 2 4F RT A6WE 1998091100214 19980911 00214 SW 1998 9 11 HEEA0015967 1 19980904 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX DETERIORATED E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 405PH 53207 RUBBER DELAMINTATED ON MAIN ROTOR GEARBOX MOUNT. 1 G 7 1 3U O H2SW 1998091100234 19980911 00234 WP 1998 9 11 TWAA9814201 1 19980903 A 3350 CONNECTOR DOUG DC9 DC915 3022036 WP CABIN DIRTY A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 971Z 45773 THE OVERWING EXIT SECTION OF THE EGRESS LIGHTS WERE COMING ON INTERMITTENTLY IN FLIGHT. FOUND CONNECTOR FOR THAT SECTIO N WAS DIRTY. CLEANED ELECTOR CONNECTOR. CHECK-C 7-6-98 STL. 2 L 7 2 4F A6WE 1998091100235 19980911 00235 WP 1998 9 11 TWAA9814202 1 19980831 A 5312 BULKHEAD CAP DOUG DC9 DC951 3022051 WP AFT PRESS BLKHD CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 DURING CHECK-C, MAINT FOUND CRACK INDICATION BETWEEN STR 10L AND 11L, REAR PRESS BULKHEAD T-CAP. REMOVED AND REPLACED T -CAP. SPLICED IN PER SRM 53-03, FIG 37A. 2 L 7 2 4F RT A6WE 1998091100236 19980911 00236 WP 1998 9 11 TWAA9814203 1 19980901 A 5347 TRACK DOUG DC9 DC951 3022051 WP CARGO COMPT CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 DURING CHECK-C, MAINT FOUND CORROSION IN AFT CARGO COMPT, LT TIE DOWN TRACK, FROM FWD END TO AFT END OF BIN. TRACK WAS REMOVED AND REPLACED. INSTALLED PER SRM 53-01, PG 10 FIG 2 SHEET 4. 2 L 7 2 4F RT A6WE 1998091100237 19980911 00237 NM 1998 9 11 VJ9800316 1 19980901 A 3350 6013211 POWER SUPPLY BOEING 737 737214 138446R NM CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 RT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F A16WE 1998091100238 19980911 00238 1998 9 11 VJ9800317 4 19980904 A 2561 P0723E105PC LIFE VEST DOUG DC9 DC932 3022066 WP CABIN DAMAGED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 940VV 47523 AFT RT FLT ATTENDANTS LIFE VEST COVER TORN. INSTALLED SERVICEABLE LIFE VEST. 2 L 7 2 4F A6WE 1998091100239 19980911 00239 EU 1998 9 11 MALA976190 1 19980827 A 3260 LGCU SAAB SF340 340B 7860101 EU E/E COMPT MALFUNCTIONED A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 433XJ 433 LANDING GEAR TRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED DOWN WITH NO DOWN INDICATION. HYDRAULIC PUMP CONTINUED TO RU N, LANDING GEAR CONTROL CIRCUIT BREAKER RESET CAUSED GEAR TO EXTEND NORMALLY. MAINTENANCE PERFORMED GEAR SWINGS, COULD NOT DUPLICATE. REPLACED RELAY 15GA AND LANDING GEAR CONTROL UNIT FOR PRECAUTIONARY MEASURES. PERFORMED GEAR SWINGS ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998091100240 19980911 00240 EU 1998 9 11 MALA976191 1 19980828 A 7603 RELAY SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 411XJ 411 AFTER TAKEOFF, THE FLIGHT IDLE STOP OPEN LIGHT CAME ON. AIRCRAFT RETURNED TO MSP. DURING LANDING THE ANTI SKID INOP LI GHT CAME ON WHEN GEAR WAS PUT DOWN. DURING TAXI INTO THE GATE THE FLIGHT IDLE STOP OPEN AND FLIGHT IDLE STOP LIGHTS WER E BOTH ON. MAINTENANCE REPLACED RELAYS 20GN, 19GA, 15GA AND SERVICED STRUTS. TEST FLIGHT AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A52EU E8NE 1998091100241 19980911 00241 NM 1998 9 11 K3HA980105 1 19980829 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CARGO DOOR DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 AFT CARGO DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK OK REF 33-50-71. 2 L 7 3 4F A3WE 1998091100242 19980911 00242 NM 1998 9 11 K3HA980106 1 19980829 A 3350 081691 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY PATH LIGHT RED LIGHT AT ROW 30-31 IS INOP. RELAMPED, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998091100243 19980911 00243 NM 1998 9 11 K3HA980107 1 19980829 A 3350 081691 LENSE BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 353PA 20622 FORWARD EMERGENCY PATH LIGHTING HAS ONE RED LENS MISSING. REPLACED EMERGENCY RED LENS. 2 L 7 3 4F A3WE 1998091100244 19980911 00244 NM 1998 9 11 K3HA980108 1 19980831 A 3350 328 BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 EGRESS TRACK LIGHTS AT R-2 AFT EXIT INOP 2 EACH. RELAMPED 2 SOCKET AND REPLACED 2 LENSES (RED LIGHT MODULE 2 EACH 07912 -3). 2 L 7 3 4F A3WE 1998091100245 19980911 00245 WP 1998 9 11 IXXA9800069 1 19980902 A 3231 RETRACT MECH DOUG DC8 DC863F 302198F WP NLG DOOR OUT OF ADJUST A IXXA K NONE O OTHER CL CLIMB 1 GL 23 867BX 46049 AFTER TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOISE AND VIBRATION COMING FROM THE NOSE WH EEL WELL AREA. THE CREW CYCLED THE GEAR BUT THE VIBRATION CONDITION WAS STILL PRESENT. THE AIRCRAFT RETURNED TO TOL FO R AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE RIGHT AFT NOSE GEAR DOOR OUT OF RIG. MA INTENANCE RIGGED THE NOSE GEAR DOOR IN ACCORDANCE WITH THE DOUGLAS MAINTENANCE MANUAL AND PERFORMED A SUCCESSFUL NOSE GE AR SWING. 2 L 7 4 4F 4A25 1998091100246 19980911 00246 WP 1998 9 11 IXXA9800070 1 19980902 A 2433 6RS741Y1 TRU DOUG DC8 DC871F 302199D WP COCKPIT DEFECTIVE A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 830BX 45973 EN ROUTE, THE FLIGHT CREW SENSED A SMOKE ODOR IN THE COCKPIT. THE FLIGHT ENGINEER NOTICED THE NUMBER THREE DC LOAD MONI TOR WAS READING AN EXCESSIVE LOAD. THE NUMBER THREE TRANSFORMER RECTIFIER CIRCUIT BREAKER WAS OPENED AND THE ODOR SUBSI DED. MAINTENANCE INVESTIGATED AND FOUND THE TRANSFORMER RECTIFIER DEFECTIVE. MAINTENANCE DEFERRED THE NUMBER THREE TRA NSFORMER RECTIFIER. 2 L 7 4 4F RT 4A25 1998091100247 19980911 00247 NE 1998 9 11 PNSA980802 2 19980825 A 7412 103815501 IGNITER BOX CESSNA 208 208 2073702 CE PWA PT6 PT6A114 52043 NE ENGINE INOPERATIVE A PNSA O OTHER O OTHER IN INSP/MAINT 1 AL 03 9481F 20800070 LOADED PASSENGERS, ENGINE WOULD NOT START. DEPLANED PAX. REPLACED IGNITER BOX, OPS CHECK OK. 1 H 7 1 3T 3 T NT A37CE E4EA 1998091100248 19980911 00248 EU 1998 9 11 PNSA980803 1 19980825 A 3230 7232360151 SPRING SAAB SF340 340B 7860101 EU LT MLG BROKEN A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 685PA 212 DURING PREFLIGHT AT GATE, PILOT NOTICED A BROKEN UPLOCK ASSIST SPRING ON LT MAIN GEAR. SPRING REPLACED, GEAR SWING NORM AL. 2 L 7 2 4T RT A52EU 1998091100249 19980911 00249 EU 1998 9 11 PNSA980903 1 19980903 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A PNSA O OTHER N FALSE WARNING DE DESCENT 1 AL 03 685PA 212 LAV SMOKE DETECT LIGHT ILLUMINATED IN FLIGHT. FLIGHT CREW INVESTIGATED AND DID NOT SMELL SMOKE. AIRCRAFT LANDED UNEVEN TFULLY. MAINTENANCE INVESTIGATED AND COULD NOT DETERMINE SOURCE. IT WAS NOTICED THAT THE OVER HEADLIGHT FLICKERED INTE RMITTANTLY WHEN DOOR WAS CLOSED. HOWEVER, IT DID NOT EMIT SMOKE. LAMP WAS REPLACED ANYWAY AND NO FURTHER PROBLEMS NOTE D WITH SYSTEM. SYSTEM TESTS WERE NORMAL. 2 L 7 2 4T RT A52EU 1998091100250 19980911 00250 SO 1998 9 11 RAAA98E9031 1 19980903 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 FWD CABIN EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSEMBLY DUE FAILED. 2 L 7 4 4T 4A22 1998091100251 19980911 00251 NM 1998 9 11 CALA9801622 1 19980903 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 620 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CORROSION AND A .75 INCH CRACK IN L-ANGLE IN FORWARD PIT AFT OF DOOR AT STA 620, STRINGER 27R. THE ANG LE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-20-1, 51-10-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998091100252 19980911 00252 NM 1998 9 11 CALA9801623 1 19980903 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND STRINGER 24R CORRODED AT STA 1166. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 53-10 -3, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100253 19980911 00253 NM 1998 9 11 CALA9801624 1 19980903 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 219.8 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND INSIDE OF SKIN CORRODED IN LT WHEEL WELL AT STA 219.8, STRINGER 27L. THE CORROSION WAS REMOVED AND A R EPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-6, 53-10-1, 53-30-3, 51-10-2, AND MM 51-11-20. 2 L 7 2 4F A16WE 1998091100254 19980911 00254 WP 1998 9 11 CALA9801625 1 19980903 A 5210 SKIN DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND A .5 INCH CRACK IN SKIN AT LOWER FORWARD CORNER OF MAIN ENTRY DOOR. A DOUBLER WAS INSTALLED IAW SRM 53 -05, FIGURE 32. 2 L 7 2 4F A6WE 1998091100255 19980911 00255 NM 1998 9 11 CALA9801626 1 19980904 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 435-440 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14241 20070 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 435 TO 440, STRINGER 24R. A DOUBLER WAS INSTALLED IAW SRM 53-30-3. 2 L 7 2 4F A16WE 1998091100256 19980911 00256 NM 1998 9 11 CALA9801627 1 19980904 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 950 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND INTERCOSTAL WEB GOUGED AT RT FUSELAGE STA 950B BETWEEN STRINGER 29L AND 30L. THE INTERCOSTAL WEB WAS R EMOVED. A NEW INTERCOSTAL AND THREE EACH L-ANGLE STIFFENERS WERE INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51 -20-0. 2 L 7 3 4F A3WE 1998091100257 19980911 00257 NM 1998 9 11 CALA9801628 1 19980904 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT FUSELAGE FLOORBEAM CORRODED AT STA 1070. THE CORRODED AREA WAS CUT OUT, TWO ANGLES AND FILLER WERE INSTALLED IAW SRM 53-10-8, FIGURE 8. 2 L 7 3 4F A3WE 1998091100258 19980911 00258 NM 1998 9 11 CALA9801629 1 19980904 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1030-1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT FUSELAGE SEAT TRACK CORRODED AT STA 1030 TO 1136. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK W AS INSTALLED IAW SRM 53-10-5. 2 L 7 3 4F A3WE 1998091100259 19980911 00259 NM 1998 9 11 CALA9801630 1 19980905 A 5311 FRAME BOEING 727 727232 1384082 NM BS 804.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 804.5, STRINGER 14L. A 1.5 INCH CRACK WAS FOUND IN FRAME AT STA 804.5, STRINGER 14R. AN ANGLE WAS INSTALLED AT EACH LOCATION IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091100260 19980911 00260 WP 1998 9 11 CALA9801631 1 19980906 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND A 1 INCH CRACK IN MAIN CABIN DOOR NR 1 BEAM. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 31, SECTION U-U, PAGE 179. 2 L 7 2 4F A6WE 1998091100261 19980911 00261 WP 1998 9 11 CALA9801632 1 19980905 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1900 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1900, LBL 6 AND RBL 6. THE FLOOR SUPPORTS WERE REMOVED AND NEW PART S WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998091100262 19980911 00262 WP 1998 9 11 CALA9801633 1 19980905 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 460 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 460, RBL 20. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998091100263 19980911 00263 WP 1998 9 11 CALA9801634 1 19980905 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1887 BETWEEN RBL 0 - RBL 25, RBL 25 - 35, RBL 35 - 60, AND RBL 60 - 90. THE FLOOR SUPPORTS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998091100264 19980911 00264 WP 1998 9 11 CALA9801635 1 19980905 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1887 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1887 BETWEEN LBL 35 & 45 AND BETWEEN LBL 45 & 90. THE FLOOR SUPPORTS WE RE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998091100265 19980911 00265 EA 1998 9 11 COMA9860253 1 19980904 A 3230 864806 PSEU CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTION A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 932CA 2403 2100 7038 PROX SYSTEM FAULT MESSAGE. LANDING GEAR WOULD NOT EXTEND NORMAL. REPLACED THE PSEU. 2 L 7 2 4F RT A21EA 1998091100266 19980911 00266 EA 1998 9 11 COMA9860254 1 19980904 A 3350 59465 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN INOPERATIVE A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 916CA 7014 AFT SECTION OF FLOOR PATH EMERGENCY LIGHTING IS INOPERABLE. REPLACED LIGHT STRIP CONNECTOR. 2 L 7 2 4F RT A21EA 1998091100267 19980911 00267 EA 1998 9 11 COMA9860255 1 19980904 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 964CA 7129 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT HAND BPSU. 2 L 7 2 4F RT A21EA 1998091100268 19980911 00268 NM 1998 9 11 UPS98227595 1 19980902 A 5330 SKIN BOEING 727 727247 138408F NM BS 1050 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 209UP 21698 INSPECTION TYPE-N/A, CORROSION ON FUSELAGE SKIN APPROX STA 1050 STR 27L, BULGE AND SEVERAL POPPED FASTENERS. REPAIRED P ER SRM 53-30-3 FIG 3, FIG 1. 2 L 7 3 4F A3WE 1998091100269 19980911 00269 NM 1998 9 11 UPS98227596 1 19980902 A 5330 SKIN BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 209UP 21698 INSPECTION TYPE-N/A, CORROSION ON FUSELAGE SKIN APPROX STA 1130 STR 29L. BULGE AND SEVERAL POPPED FASTENERS. REPAIRED SKIN PER SRM 53-30-3 FIG 3. 2 L 7 3 4F A3WE 1998091100270 19980911 00270 WP 1998 9 11 UPS98827593 1 19980524 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 290 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, LONGERON 35 LEFT CRACKED FUSELAGE STATION 290. REMOVED AND REPLACED LONGERON 35 LEFT IAW DC8 SRM 51-1-20D AND 51-1-24. 2 L 7 4 4F RT 4A25 1998091100271 19980911 00271 WP 1998 9 11 UPS98827594 1 19980525 A 5510 LINKAGE BOX DOUG DC8 DC873F 302199F WP HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-C/CK, LEFT HAND HORIZONTAL STABILIZER OUTBOARD GEAR TAB LINKAGE BOX CRACKED AND GOUGED XRS 216. REMOVED TAB LINKAGE COVER IAW DC8 SRM 51-1-21, WELDED BOX IAW DC8 1 0.301 AND DAC DWG 5652086, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, REINSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998091100272 19980911 00272 WP 1998 9 11 UPS98827597 1 19980817 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 857 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, LWR FRAME AT FS 857 LT HAS CORROSION AND CRACK ON RADIUS ON INTERCOSTAL (ABF SENSE ANTENNA SUPPORT ATTACHMENT ANGLE). REMOVED AND REPLACED INTERCOSTAL AND REPAIRED RIB WITH STACKED ANGLE REPAIR IAW REO-05372 DC8 SRM 5 3-2-0 FIG 1B. ALODINED AND PRIMED PARTS IAW DC8 SRM 51-1-8. INSTALLED EO A/C AFFECTED PARTS IAW DC8 SRM 51-3 -0, 51-1- 21, 51-1-21D. 2 L 7 4 4F RT 4A25 1998091100273 19980911 00273 WP 1998 9 11 UPS98827598 1 19980809 A 5320 364711724 FITTING DOUG DC8 DC873F 302199F WP BS 960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-C CK, AFT CARGO UPPER FITTING AT FS 960 ABOVE LONGERON 24L HAS CRACK IN ATTACHMENT HOLE. REMOVED EXISTI NG FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON UPS N/R 840692. 2 L 7 4 4F RT 4A25 1998091100274 19980911 00274 WP 1998 9 11 UPS98827599 1 19980809 A 5320 3646956 FITTING DOUG DC8 DC873F 302199F WP BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, UPPER FITTING AT FS 940 ABOVE LONGERON 24 HAS CRACK IN ATTACHMENT HOLES. REMOVED EXISTING FITTING AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON N/R 840692. 2 L 7 4 4F RT 4A25 1998091100275 19980911 00275 WP 1998 9 11 UPS98827600 1 19980809 A 5320 5753113501 FITTING DOUG DC8 DC873F 302199F WP BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, UPPER FITTING AT FS 920 ABOVE LONG 24L HAS CRACK. REMOVED EXISTING FITTING, DRILLED NEW FITTING I AW DC8 SRM 51-3-2. FITTING INSTALLATION TO BE COMPLETED ON UPS N/R 840692. 2 L 7 4 4F RT 4A25 1998091100276 19980911 00276 WP 1998 9 11 UPS98827601 1 19980807 A 5320 37739061 CLIP DOUG DC8 DC873F 302199F WP BS 822 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 822 XCW-29 UNDER SEAT TRACK E FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITT ING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 373906-1) PO NR 267866 IAW DC8 SRM 51-3-2. IN STALLED NEW FITTING IAW DC8 SRM 51-1-2 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998091100277 19980911 00277 WP 1998 9 11 UPS98827602 1 19980807 A 5320 37739061 FITTING DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 781 XCWX29 UNDER SEAT TRACK C FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITT ING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 3773906-1), PO NR 267861 IAW DC8 SRM 51-3- 2. INSTALLED NEW FITTING IAW DC8 SRM 51-1-2 & 51-1-20D. 2 L 7 4 4F RT 4A25 1998091100278 19980911 00278 WP 1998 9 11 UPS98827603 1 19980819 A 5320 37739062 CLIP DOUG DC8 DC873F 302199F WP BS 781 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK E STA 781 XCW-29 FRAME ATTACH CLIP CRACKED. REMOVED AND REPLACED SEAT TRACK E IAW 51-1 -20, DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100279 19980911 00279 WP 1998 9 11 UPS98827604 1 19980807 A 5320 37552221 CLIP DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 759 XCW-26 UNDER AFT SIDE SEAT TRACK E FITTING FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP (FITTING) IAW DC8 SRM 51-1-2 & 51-1-20D. LOCATED AND DRILLED NEW FITTING (P/N 375522-1) PO NR 267866 IAW D C8 SRM 51-3-2. INSTALLED NEW FITTING IAW SRM 51-1-2 & 51-1-20D. 2 L 7 4 4F RT 4A25 1998091100280 19980911 00280 WP 1998 9 11 UPS98827605 1 19980819 A 5320 37552222 CLIP DOUG DC8 DC873F 302199F WP CABIN CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK FRAME ATTACH CLIP CRACKED. REMOVED ATTACH CLIP FITTING IAW DC8 SRM 51-3-0. INSTALLED NEW FITTING SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100281 19980911 00281 WP 1998 9 11 UPS98827606 1 19980806 A 5320 3755826504N FITTING DOUG DC8 DC873F 302199F WP BS 340 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, STA 340 L31L Z FITTING HAS CORROSION EMITTING FROM FASTENER. REMOVED CORROSION FOUND TO BE OUT OF LIMITS DC8 SRM 51-1-8 AND 53-2-0. REMOVED FITTING, FABBED DOUBLERS, REINSTALLED FITTING IAW DC8 SRM 5 3-2-0. ALODINED , PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D. FILLETED SEALED IAW DC8 SRM 51-1-16. 2 L 7 4 4F RT 4A25 1998091100282 19980911 00282 WP 1998 9 11 UPS98827607 1 19980817 A 5347 53B003501 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK STA 1300 C TRACK HAS CORROSION. REMOVED DAMAGED AREA OF SEAT TRACK, SPLICED NEW TRACK IAW DC8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998091100283 19980911 00283 WP 1998 9 11 UPS98827608 1 19980805 A 5320 STANCION DOUG DC8 DC873F 302199F WP BS 440 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, FLC STA 440 LT SIDE STANCION CORRODED AROUND NUT PLATES. FABRICATED REPAIR ANGLE AND INSTALLED IA W DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998091100284 19980911 00284 WP 1998 9 11 UPS98827609 1 19980805 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 798 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK D STA 798 FLOORBEAM HAS CORROSION AROUND BOLT HOLES. REPAIRED IAW REO 05232. 2 L 7 4 4F RT 4A25 1998091100285 19980911 00285 WP 1998 9 11 UPS98827610 1 19980805 A 5320 3750257503N SPLICE DOUG DC8 DC873F 302199F WP BS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, FLC LONG 31R STA 610 SPLICE CRACKED. REMOVED AND REPLACED (P/N 3750257-503N) LONGERON SPLICE FITT ING ON LONGERON 31R AT STA 610 IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998091100286 19980911 00286 WP 1998 9 11 UPS98827611 1 19980805 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1460-1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK F HAS CORROSION STA 1460 TO 1580. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGED SECTION OF TRACK IAW DC8 SRM 51-3-0, MAT ID S4889185. DOUBLE SEAT TRACK 7075 T6 PO NR 1085 84 IAW DC8 SRM 53-2-3. FAB SEAT TRACK REPAIR IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 51-1-8. INSTALLED IAW DC 8 SRM 53-2-3. 2 L 7 4 4F RT 4A25 1998091100287 19980911 00287 WP 1998 9 11 UPS98827612 1 19980805 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 70-280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK HAS CORROSION STA 70 TO STA 280. CORROSION OUT OF LIMITS ON TRACK F STA 85 IAW DC8 SRM 53-2-3. REMOVED DOUBLE SEAT TRACK MAT ID 54889485 7075-T6 IAW DC8 SRM 53-2-3 PO NR 10 8589. FAB SEAT TRACK IAW DC8 SR M 53-2-3. DRILLED SEAT TRACK IAW DC8 SRM 51-3-2. ALODINED AND PRIMED SEAT TRACK IAW DC8 SRM 51-1-8. INSTALLED SEAT TR ACK IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100288 19980911 00288 WP 1998 9 11 UPS98827613 1 19980805 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 280-520 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK E HAS CORROSION STA 280 TO STA 520. REMOVED CORROSION FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3 MAT ID IAW DC8 SRM 53-2-3 AND SPLICES IAW DC8 SRM 53-7-3. LOCATED, DRILLED NEW SEAT TRACK AND SPLICES IAW DC8 SR M 53-2-3 & 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAT TRACK AND SPLICES IAW DC8 SRM 53 -2-3 A ND 51-3-0. 2 L 7 4 4F RT 4A25 1998091100289 19980911 00289 WP 1998 9 11 UPS98827614 1 19980805 A 5347 53B003501 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 70-280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK E HAS CORROSION STA 70 TO 280. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-3 FIG 12 AT FS 130 TO 270. REMOVED CORROSION AT FS 70 TO 80 IAW DC8 SRM 51-1-8 AND 53-2-3 FIG 12. ALODIN ED AND PRIMED IAW DC8 SRM 51. REMOVED TRACK FROM 130 TO 270 MAT ID 527726607075-T6 IAW DC8 SRM 53-2-3 AND 51-2-0. DRIL LED AND INSTALLED IAW DC8 SRM 53-2-3, 51-3-0, 51-1-8, 51-1-14. 2 L 7 4 4F RT 4A25 1998091100290 19980911 00290 NM 1998 9 11 UPS98227616 1 19980904 A 5330 SKIN BOEING 727 727247 138408F NM BS 1130 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 209UP 21698 INSPECTION TYPE-N/A, CORROSION ON FUSELAGE SKIN APPROX STA 1130 STR 29L BULGE AND SEVERAL POPPED FASTENERS. TRANSFERRE D TO NON-ROUTINE TALLY SHEET AND NON ROUTINE NR 544150. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1998091100291 19980911 00291 NM 1998 9 11 UPS98227617 1 19980904 A 5330 SKIN BOEING 727 727247 138408F NM BS 1050 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 209UP 21698 INSPECTION TYPE-N/A, CORROSION SKIN APPROX STA 1050 STR 27L, BULGE AND SEVERAL POPPED FASTENERS. TRANSFERRED TO NON-ROU TINE TALK SHEET AND NON ROUTINE NR 544152. REPAIRED PER SRM 53-10-3. 2 L 7 3 4F A3WE 1998091100292 19980911 00292 NM 1998 9 11 UPS98227624 1 19980904 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, EMERGENCY LIGHTS AT ROW 9 DOES NOT SHUT OFF WITH COCKPIT SWITCH. REPLACED EMERGENCY LIGHT, CHECKS OK. 2 L 7 3 4F A3WE 1998091100293 19980911 00293 1998 9 11 UPS98827615 4 19980903 A 3441 INU DOUG DC8 DC871F 302199D WP LEFT FAILED A IPXA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION TO TAKEOFF 1 SO 01 707UP 45907 INSPECTION TYPE-N/A, AIR TURNBACK CPATS INS FAILED ON T/O ROLL (DUMP FUEL DOWN TO 46.00). REMOVED AND REPLACED NR 1 INU PER M/M 34-44-03, OPS CK GOOD. (S/N 1172) OFF, (P/N 463001-6110-0412) OFF, (S/N 1307) ON, (P/N 463001-6130-0412) ON. 2 L 7 4 4F RT 4A25 1998091100294 19980911 00294 WP 1998 9 11 UPS98827618 1 19980806 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 130-220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 130 TO 220 SEAT TRACK B HAS CORROSION. REMOVED CORRODED SECTION OF TRACK B STA 50 TO 220. TRIMMED, LOCATED, DRILLED NEW SECTION IAW DC8 SRM 53-2-3 & 51-1-24. ALODINED AND PRIMED TRACK AND AREA IAW DC8 SRM 51-1-8. INSTALLED TRACK IAW DC8 RM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100295 19980911 00295 WP 1998 9 11 UPS98827619 1 19980807 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 879-1080 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 879 TO 1080 SEAT TRACK A HAS CORROSION. REMOVED CORROSION IAW DC8 SRM 51-1-8. NOT WITHIN LIMITS IAW DC8 SRM 53-2-3. REMOVED DAMAGED SECTION OF SEAT TRACK STA 590 TO 1030, DRILLED NEW SECTION IAW DC8 S RM 51-1-4. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SECTION OF TRACK IAW DC8 SRM 53-2-3 AND 51-3-0. REIN STALLED FLOOR PANELS IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100296 19980911 00296 WP 1998 9 11 UPS98827620 1 19980804 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 90 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, STA 90 ABOVE L33R INTERCOSTAL CRACKED TOP FLANGE. REMOVED AND REPLACED INTERCOSTAL IAW DC8 SRM 51 -1-21. FABRICATED INTERCOSTAL IAW DAC DWG 5750726. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998091100297 19980911 00297 WP 1998 9 11 UPS98827621 1 19980804 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 25 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, STA 25 FLOOR SUPPORT CORRODED CUSP TO CUSP. REMOVED DAMAGED FLOOR SUPPORT AT STA 25 CUSP TO CUSP, FAB NEW SUPPORT IAW DC8 53-3-2 AND DOUGLAS DWG 5888367. ALODINED AND PRIMED FLOOR SUPPORT IAW DC8 SRM 51-1-8. INSTAL LED FLOOR SUPPORT IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-21A. 2 L 7 4 4F RT 4A25 1998091100298 19980911 00298 WP 1998 9 11 UPS98827622 1 19980810 A 5320 ANGLE DOUG DC8 DC873F 302199F WP LAVATORY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, LAV SEAT CONTAINER BOTTOM ATTACH ANGLES HAS CORROSION AND BARE METAL ON BOTTOM SIDE. REMOVED CORR OSION IAW DC8 SRM 51-1-8, FAB ANGLES IAW DOUGLAS DWG DC-8- 380-001. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998091100299 19980911 00299 WP 1998 9 11 UPS98827623 1 19980807 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 781 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 781 XCW0 FRAME HAS CORROSION AT SEAT TRACK ATTACH POINT. REMOVED BOLT STA 781 IAW DC8 SRM 51-3-0. REMOVED CORROSION IAW DC8 SRM 51-1-8. MAT REMOVED OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB FLOORBEAM REP AIR ANGLE, SUPPORT REPAIR ANGLE FILLER AND REPAIR STRAP IAW REO 05229 REV A. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. I NSTALLED BOLTS IN SEAT TRACK IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100300 19980911 00300 WP 1998 9 11 UPS98827625 1 19980807 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 781 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 781 SCW-29 AND -36 FLOORBEAM HAS CORROSION AROUND PLATE. REMOVED DAMAGED AREA IAW REO 05223, FABBED FILLER AND L-ANGLE IAW REO 0 5223. LOCATED AND DRILLED UP L-ANGLE AND FILLER IAW REO 05223. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FILLER AND L-ANGLE IAW DC8 SRM 51-1-2 0D AND REO 05223. 2 L 7 4 4F RT 4A25 1998091100301 19980911 00301 WP 1998 9 11 UPS98827626 1 19980807 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 822 CORROSION A IPXA O OTHER O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 822 XCW-30 FLOORBEAM HAS CORROSION. REMOVED CORROSION AND DOCUMENTED REMAINING MAT THICK ON REO 05281, MAT ID .190 7075-T6 PO 234881 FOR FILLER AND 60-4139 L-ANGLE EXTRUSION 7075-T6 511 FOR REPAIR ANGLE . TRIMMED DAMAGE, FABBED FILLER FOR UPPER FLANGE AND FAB, DRILLED REPAIR ANGLE IAW REO 05231. ALODINED AND PRIMED IAW 51-1-8. INSTALLED IAW REO 05231. 2 L 7 4 4F RT 4A25 1998091100302 19980911 00302 WP 1998 9 11 UPS98827627 1 19980807 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 902 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 902 FLOORBEAM AT XCW-39 CRACKED AND HAS CORROSION. BLENDED OUT CORROSION TO UPPER FWD FLANGE LWR SURFACE IAW DC8 SRM 53 -2-0 MAT ID 7075-T6 .125 REPAIR STRAP, FILLER 7075-T6 .090 PO 248989 , 263213. FA B REPAIR STRAP IAW REO 05238. ALODINED AND PRIMED IAW DC8 SRM 51-1 -8. INSTALLED REPAIR STRAP IAW REO 05238 AND SRM 51 -1-11. 2 L 7 4 4F RT 4A25 1998091100303 19980911 00303 WP 1998 9 11 UPS98827629 1 19980807 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 920 FLOORBEAM AT SCW-40 CRACKED AND HAS CORROSION. CUT OUT DAMAGED AREA IAW REO 05 244, FAB AND DRILLED REPAIR ANGLE, STRAP AND FILLER IAW REO 05244. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED R EPAIR ANGLE STRAP AND FILLER IAW REO 05244 REV A AND DC8 SRM 51-1-20 AND 51-3-0. 2 L 7 4 4F RT 4A25 1998091100304 19980911 00304 WP 1998 9 11 UPS98827630 1 19980806 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 920 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, FLOORBEAM UPPER FLANGE LOWER SURFACE HAS CORROSION STA 920 X=+59 D OT P788. REPAIRED FLOORBEAM IA W REO 05246. 2 L 7 4 4F RT 4A25 1998091100305 19980911 00305 WP 1998 9 11 UPS98827631 1 19980806 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 580 FLOORBOARD B SPLICES HAVE CORROSION. REMOVED SPLICES FROM FLOORBOARDS AND REMO VED CORROSION IAW DC8 SRM 51-1-8. NOT WITHIN LIMITS IAW DC8 SRM 53-2-0. FAB NEW SPLICES IAW DC8 SRM 53-7-0 AND 51-1-24 . ALODINED AND PRIMED IAW DC8 SRM 51-1-21 AND REINSTALLED SPLICES IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100306 19980911 00306 WP 1998 9 11 UPS98827632 1 19980806 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 1000 FLOORBOARD C SPLICES HAVE CORROSION. REMOVED CORROSION FROM SPLICES IAW DC8 S RM 51-1-8. FOUND SPLICES TO BE OUT OF LIMTIS IAW DC8 SRM 53-2-0 MAT ID IAW DC8 SRM 53-7-3 7075T6 .090 PO 263213. FAB P ART IAW DC8 SRM 53-7-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-18. REINSTALLED SPLICE AT STA 1000 FLOORBOARD C. 2 L 7 4 4F RT 4A25 1998091100307 19980911 00307 WP 1998 9 11 UPS98827633 1 19980807 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 1000 FLOORBOARD B SPLICE HAS CORROSION. REMOVED CORROSION FROM SPLICES IAW DC8 SRM 51-1-8. FOUND SPLICES TO BE OUT OF LIMITS MAT ID IAW DC8 SRM 53-7-3 7075-T6 .090 PO 263213. FABRICATED PARTS IAW DC8 SRM 53-7-3. ALODINED AND PRIMED IAW DC8 SRM 51-1- 8. REINSTALLED AT STA 1000 FLOORBOARD B. 2 L 7 4 4F RT 4A25 1998091100308 19980911 00308 WP 1998 9 11 UPS98827634 1 19980805 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 92 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK D STA 920 AT FWD MOUNT BOLT FLOORBEAM IS CRACKED. FABBED REPAIR STRAP IAW REO 05207, A LODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. NO CRACK NOTED, PART WAS CORRODED. 2 L 7 4 4F RT 4A25 1998091100309 19980911 00309 WP 1998 9 11 UPS98827635 1 19980804 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1480 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 1480 LONG 21R FRAME CRACKED. REMOVED GILLINER FOR ACCESS. REMOVED DAMAGED CLIP, F AB REPLACEMENT CLIP IAW DAC DWG 5773480. HEAT TREATED CLIP IAW TPS-1003, DRILLED DEBURNED CLIP, TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED CLIP IAW DC8 SRM 51-1-20D & 51-1-9. REINSTALLED GILLINER IAW DC8 SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1998091100310 19980911 00310 WP 1998 9 11 UPS98827636 1 19980819 A 5320 CLIP DOUG DC8 DC873F 302199F WP BS 759 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 759 SEAT TRACK E ATTACH CLIP CRACKED. REMOVED 7 REPLACED ATTACH CLIP FITTING IAW D C8 SRM 51-1-2, 51-1-20D. 2 L 7 4 4F RT 4A25 1998091100311 19980911 00311 WP 1998 9 11 UPS98827637 1 19980817 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 865 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, FRAME SUPPORT ANGLE STA 865 HAS CORROSION IN LOWER LEG, DOUBLER HAS CORROSION OUTER AND INNER SKIN PANEL. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0 FOR MED INTERCOSTAL IAW DC8 SRM 51-1-4 A ND DAC DWG 5616306. FAB DOUBLER IAW DC8 SRM 53-4-1, 51-1-24, FAB CLIP IAW DAC DWG 5616306, HEAT TREATED INTERCOSTAL FRO M 2004-0 TO 2024T3, FAB INTERCOSTAL IAW DAC DWG 5616306. ALODINED AND PRIMED IAW 51-1-8. INSTALLED IAW 51-1-20D AND 51 -1-21A. 2 L 7 4 4F RT 4A25 1998091100312 19980911 00312 NM 1998 9 11 QXEA9801228 1 19980902 A 3350 1013079 LIGHT DHAV 82520977001 DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 351PH 490 FLOOR EMERGENCY PROXIMITY LIGHTING SEGMENT IS INOP. REPLACED LIGHT SECTION, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998091100313 19980911 00313 EU 1998 9 11 QXEA9801267 1 19980902 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 11237 FORWARD EMERGENCY EXIT SIGN ABOVE CENTER AISLE AT ROW 8 HAS SEVERAL 28V EMERGENCY BULBS OUT. MAINTENANCE REMOVED AND RE PLACED THE CIRCUIT BOARD, OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998091100314 19980911 00314 EU 1998 9 11 QXEA9801268 1 19980901 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 4 AND 13. MAINTENANCE RELAMPED BOTH, OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998091100315 19980911 00315 EU 1998 9 11 QXEA9801269 1 19980801 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 490US 11152 EMERGENCY EXIT LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE RELAMPED AND TESTED, OPERATIONAL TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998091100316 19980911 00316 NM 1998 9 11 98FDEA00542 1 19980903 A 5230 655714051 WEB BOEING 727 727247 138408F NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 WHILE WORKING NR-0059, FOUND 3RD WEB FROM FWD EDGE OF NR 1 CARGO DOOR TO BE CORROED. *S/D* REMOVED AND REPLACED 3RD WE B FROM FWD EDGE OF NR 1 CARGO DOOR IAW FEDEX SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1998091100317 19980911 00317 NM 1998 9 11 98FDEA00543 1 19980903 A 5230 655714051 WEB BOEING 727 727247 138408F NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 WHILE WORKING NR-0059, FOUND 4TH WEB FROM FWD EDGE OF NR 1 CARGO DOOR TO BE CRACKED. *S/D* REMOVED AND REPLACED 4TH WE B FROM FWD EDGE OF NR 1 CARGO DOOR IAW FED-EX SRM 51-10-1, 51-30-2. 2 L 7 3 4F A3WE 1998091100318 19980911 00318 NM 1998 9 11 98FDEA00544 1 19980903 A 5230 655714051 WEB BOEING 727 727247 138408F NM CARGO DOOR CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 NR 1 CARGO DOOR HAS CORROSIOIN ON WEB 2ND FROM FWD EDGE OF DOOR, FOUND UPON REMOVAL OF SEAL DEPRESSOR ON NR-0059. *S/D* REMOVED AND REPLACED 2ND WEB FROM FWD EDGE OF NR 1 CARGO DOOR. WORK DONE IAW FED-EX SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1998091100319 19980911 00319 NM 1998 9 11 98FDEA00545 1 19980903 A 3260 7500355 ANNUNCIATOR PNL BOEING 727 72725 1384006 NM LANDING GEAR FAILED A FDEA O OTHER P NO WARNING INDICATION AP APPROACH 1 SO 25 156FE 18289 LT MLG GREEN LIGHT DID NOT COME ON AFTER GEAR EXTENSION. RAISED GEAR AND REPLACED LEFT GEAR BULBS AND TESTED LIGHTS. T HE LT GEAR GREEN LIGHTS TESTED GOOD BUT NOSE GEAR DID NOT TEST. REPLACED NOSE GEAR BULBS STILL DID NOT TEST BUT LOWERED GEAR AND GOT ALL GREEN. SUSPECT TEST MODULE BAD. REMOVED AND REPLACED LANDING GEAR ANNUNCIATOR PANEL, HAVE ALL E GREE N/SAFE LIGHTS AND TEST FUNCTION WORKS NORMALLY NOW. 2 L 7 3 4F A3WE 1998091100320 19980911 00320 EU 1998 9 11 98FDEA00546 1 19980903 A 2611 CG7G0 DETECTOR AIRBUS 300 A300* EU E/E COMPT FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 653FE 736 AVIONICS SMOKE ECAM AND CRG AT 1500 FT AFTER T/O. NO ODOR WITH SNIFFER OR SMOKE IN COCKPIT. WARNING CONTINUED, DECLARE D EMERGENCY AND RETURNED FOR LANDING. NOT OVERWEIGHT. NOTICED SLIGHT ELECTRICAL SMELL IN CABIN AFTER SHUTDOWN. FOUND SMOKE DETECTOR FAILED. REMOVED AND REPLACED 11WA DETECTOR PER MM 26-15-12-4, OPS TEST GOOD. NO HINT OF SMOKE IN AVIONI CS COMPARTMENT, OK FOR SERVICE. 2 L 7 2 4F RT A35EU 1998091100321 19980911 00321 NM 1998 9 11 SCNA98100 1 19980901 A 3297 WIRE BOEING 727 727227 1384078 NM RT MLG BROKEN A SCNA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 275AF 22092 ON DESCENT HAD AN UNSAFE GEAR INDICATION ON THE RIGHT MAIN LANDING GEAR. FOLLOWED COM PROCEDURES AND LANDED UNEVENTFULL Y. FOUND A BROKEN WIRE UNDERNEATH A CLAMP IN THE RIGHT MAIN WHEEL WELL. REPAIRED WIRE AND GEAR POSITION INIDCATING SYS TEM OPERATIONALLY CHECKS GOOD PER BMM 326101 ON GEAR SWING. 2 L 7 3 4F A3WE 1998091100322 19980911 00322 1998 9 11 SCNA98097 4 19980830 A 3414 B024781107 INDICATOR BOEING 727 7272J4 1384006 NM LT COCKPIT FAILED A SCNA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 285SC 21676 ON CLIMBOUT, CAPTAIN'S AIRSPEED INDICATOR FAILED. RETURNED TO MSP FOR CHANGE. REMOVED AND REPLACED CAPTAIN'S AIRSPEED INDICATOR IAW MM 341221. OPERATIONALLY CHECKED NORMAL IAW MM 34120. 2 L 7 3 4F RT A3WE 1998091100323 19980911 00323 NM 1998 9 11 SCNA98098 1 19980901 A 2130 PRESSURIZATION BOEING 727 7272J4 1384006 NM CABIN MALFUNCTIONED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 288SC 20765 ON CLIMBOUT COULD NOT CONTROL THE CABIN PRESSURIZATION IN ANY MODE. PERFORMED AN OPERATIONAL CHECK OF THE PRESSURIZATIO N SYSTEM PER 3600 PAGE 501 AND OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1998091100324 19980911 00324 NM 1998 9 11 SCNA98099 1 19980829 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA A UNSCHED LANDING L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE LEFT MID OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND RE PLACED THE BATTERY PACK, OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1998091100325 19980911 00325 NE 1998 9 11 DHL98722001 2 19980901 A 7314 378200 PUMP BOEING 727 727228 NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A DHLA A J L UNSCHED LANDING DUMP FUEL ABORTED APPROACH X ENGINE FLAMEOUT CL CLIMB 1 SO 01 722DH 19861 655480 AFTER TAKEOFF, NR 2 ENGINE FLAMED OUT. DUMPED FUEL, RETURNED FOR LANDING. FORCED TO MAKE GO- AROUND. LANDED AFTER SEC OND APPROACH. FOUND FUEL PUMP FAILED. 2 L 7 3 4F 4 F A3WE E2EA 1998091100326 19980911 00326 NM 1998 9 11 DHL98722002 1 19980901 A 3211 6516206 TRUNNION BOEING 727 727228 NM PWA JT8 JT8D7B 52053 NE RT MLG FAILED A DHLA A J L UNSCHED LANDING DUMP FUEL ABORTED APPROACH D INFLIGHT SEPARATION LD LANDING 1 SO 01 722DH 19861 655480 AFTER LANDING, RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FAILED, CAUSING LANDING GEAR TO SEPARATE FROM THE AIRCRA FT. 2 L 7 3 4F 4 F A3WE E2EA 1998091100327 19980911 00327 WP 1998 9 11 ARWA980903 1 19980904 A 2750 FLAPS LKHEED 1011 1011385115 5265015 WP WING MALFUNCTIONED A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 306GB 193U1138 MIA - FLT 501 - FLAPS WILL NOT GO DOWN, NO INDICATION. UNLOCKED FLAPS AT FLAP BRAKE, OPS CHECK GOOD IAW MM 27-51-00. ( M) 2 L 7 3 4F A23WE 1998091100328 19980911 00328 NM 1998 9 11 VNAA9809001 1 19980901 A 5350 NOSE CONE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE BIRD STRIKE A VNAA O OTHER C F.O.D. AP APPROACH 1 GL 07 461PS 3075 THE CREW REPORTED THAT THEY MAY HAVE TAKEN A BIRD STRIKE ON THE NOSE CONE, DURING SHORT FINAL APPROACH. THE AIRCRAFT CO NTINUED THE APPROACH AND LANDED WITHOUT INCIDENT. OUTSTATION MAINTENANCE WAS CALLED AND INSPECTED THE AIRCRAFT, IN ACCO RDANCE WITH DORNIER MAINTENANCE MANUAL 05-57-07. GROUND ENGINE RUNS WERE ALSO PERFORMED ON BOTH ENGINES. NO DAMAGE WAS FOUND. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091100329 19980911 00329 NM 1998 9 11 VNAA9809002 1 19980902 A 3240 HANDLE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARKING BRAKE OUT OF ADJUST A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 437JS 3055 DURING THE TAXI FOR TAKEOFF, A BRAKE OVERHEAT WARNING MESSAGE ILLUMINATED, FOR ALL FOUR BRAKES. THE AIRCRAFT RETURNED T O THE GATE. MAINTENANCE INSPECTED, ADJUSTED AND LUBED THE EMERGENCY PARK BRAKE HANDLE, IN ACCORDANCE WITH DORNIER MAINT ENANCE MANUAL 32-43-02. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091100330 19980911 00330 WP 1998 9 11 CKSA98509 1 19980902 A 5347 SEAT TRACK LKHEED 1011 10113851 5265010 WP BS 1107-1125 WORN A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 103CK 293C1212 POSTFLIGHT FOUND LT O/B MAIN DECK SEAT TRACK WORN BETWEEN FS 1107 AND FS 1125. REMOVED AND REPLACED WORN SEAT TRACK IAW MM 25-10-03. 2 L 7 3 4F A23WE 1998091100331 19980911 00331 WP 1998 9 11 TC8A98056 1 19980904 A 7931 42D491C SWITCH DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE FAILED A TC8A A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 GL 23 181SK 45910 669217 ON CLIMBOUT, NR 2 ENGINE LOW OIL PRESSURE LIGHT ON. CHECK LIST COMPLETED AND LIGHT STILL ON. SHUT DOWN NR 2 ENGINE PRE CAUTIONARY. CREW DEBRIEF REVEALED NO OIL PRESSURE LOSS AND NO OIL QTY LOSS. DISCOVERED OIL DIFFERENTIAL PRESSURE SWITC H LEAKING. REMOVED AND REPLACED PRESSURE SWITCH IAW DC8 MM 79-33-1. INSPECTED MAIN OIL FILTER FOR CONTAMINATION, NO CO NTAMINATION NOTED. AS PRECAUTIONARY MEASURE, REMOVED AND REPLACED MAIN OIL FILTER IAW DC8 MM 79-20-1, OPS AND LEAK CHEC K OF OIL FILTER AND PRESSURE SWITCH GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1998091100332 19980911 00332 WP 1998 9 11 TC8A98057 1 19980908 A 2781 WIRE DOUG DC8 DC862F 3021972 WP LE FLAPS FAILED A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 187SK 46022 WING SLOT LIGHT DOES NOT ILLUMINATE DURING T/O FLAP SELECTION. TRANSFERRED TO DMI IAW MEL 27-8 CAT C, DMI NR 8693, PLAC ARD INSTALLED ON 9/8/98. REPAIRED WIRING AT UP FLAP LIMIT SWITCH AS PER M/M 20-50-1. SYSTEM CHECKED NORMAL IAW M/M 27- 52-3. DMI CLEARED. 2 L 7 4 4F 4A25 1998091100333 19980911 00333 WP 1998 9 11 ASAA9880133 1 19980716 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 229 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OAK - DURING 15K CHECK, GOUGE AND CRACK WAS FOUND IN FUSELAGE SKIN AT STATION 229, LONGERON 18L. INSTALLED FLUSH DOUBLE R IAW DC9 SRM 53-04 FIG 47. (M) 2 L 7 2 4F RT A6WE 1998091100334 19980911 00334 WP 1998 9 11 ASAA9880134 1 19980716 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 219 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 OAK - DURING 15K CHECK, DENT WAS FOUND IN FUSELAGE SKIN AT STATION 219 BETWEEN LONGERON 17L AND CUSP. REMOVED DAMAGED A ND INSTALLED FLUSH REPAIR DOUBLER IAW ASA EA 5330-01326. (M) 2 L 7 2 4F RT A6WE 1998091100335 19980911 00335 WP 1998 9 11 ASAA9880131 1 19980715 A 5610 PIN DOUG DC9 DC982 3022082 WP COCKPIT OUT OF TRACK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 931AS 49232 OAK - AFTER ARRIVAL OF FLIGHT 456, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. FOUND WINDO W AFT HINGE PIN MIGRATED OUT OF POSITION. REPOSITIONED PIN INTO HINGE AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998091100336 19980911 00336 1998 9 11 ASAA9880128 4 19980712 A 2565 BOTTLE DOUG DC9 DC983 3022083 WP SLIDE INOP A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 963AS 53077 PDX - DURING MAINTENANCE CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLAC ED THE TAILCONE EMERGENCY EVACUATION SLIDE ASSY. (M) 2 L 7 2 4F RT A6WE 1998091100337 19980911 00337 WP 1998 9 11 ASAA9880135 1 19980716 A 5610 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 963AS 53077 PDX - AFTER ARRIVAL OF FLIGHT 497, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. FREED JAMMED WINDOW MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091100338 19980911 00338 WP 1998 9 11 ASAA9880130 1 19980714 A 5610 PIN DOUG DC9 DC983 3022083 WP COCKPIT OUT OF TRACK A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 963AS 53077 SEA - AFTER ARRIVAL OF FLIGHT 419, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. FOUND WIND OW UPPER GUIDE PIN OUT OF TRACK. REPOSITIONED PIN INTO TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091100339 19980911 00339 NM 1998 9 11 ASAA9810053 1 19980724 A 5320 CLIP BOEING 737 737298C 1384490 NM BS 351 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND STRINGER CLIP CORRODED AT STATION 351, STRINGER 22L. REPAIRED PER SRM 51-10-6. (M) 2 L 7 2 4F RT A16WE 1998091100340 19980911 00340 NM 1998 9 11 ASAA9810054 1 19980724 A 5320 WEB BOEING 737 737298C 1384490 NM BS 847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND INBOARD SIDE OF WEB CORRODED AT STATION 847, STRINGER 22L. REPAIRED PER SRM 51-10-6 AND SRM 51-10-30. (M) 2 L 7 2 4F RT A16WE 1998091100341 19980911 00341 NM 1998 9 11 ASAA9810055 1 19980724 A 5320 WEB BOEING 737 737298C 1384490 NM BS 500 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND FLOOR WEB CRACKED AT STATION 500, 8 INCH INBOARD OF STRINGER 17R. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1998091100342 19980911 00342 NM 1998 9 11 ASAA9810056 1 19980724 A 5311 FRAME BOEING 737 737298C 1384490 NM BS 986 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND FRAME CORRODED AT STATION 986, STRINGER 27L. REPAIRED PER SRM 51-30-2 AND SRM 51-40-3. (M) 2 L 7 2 4F RT A16WE 1998091100343 19980911 00343 NM 1998 9 11 ASAA9810057 1 19980724 A 5313 STRINGER BOEING 737 737298C 1384490 NM BS 495-540 MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND STRINGER 23R HAS TWO HOLES IN RADIUS AT STATION 495-540. REPAIRED PER SRM 51-20-2. (M) 2 L 7 2 4F RT A16WE 1998091100344 19980911 00344 NM 1998 9 11 ASAA9810058 1 19980724 A 5313 STRINGER BOEING 737 737298C 1384490 NM BS 420-440 MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND STRINGER 22R HAS TWO OVERSIZED HOLES AT STATION 420-440. REPAIRED PER SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1998091100345 19980911 00345 NM 1998 9 11 ASAA9810059 1 19980724 A 5313 STRINGER BOEING 737 737298C 1384490 NM BS 360-440 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND STRINGER 21R AT STATION 360-440 HAS HAD NUMEROUS BLENDOUTS AND REPAIRS. REPAIRED PER SRM 51 -30-0. (M) 2 L 7 2 4F RT A16WE 1998091100346 19980911 00346 NM 1998 9 11 ASAA9810060 1 19980724 A 5320 SPLICE BOEING 737 737298C 1384490 NM BS 500 MISMANUFACTURED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND FILLER AND HOLES WITH INADEQUATE EDGE DISTANCE ON FRAME SPLICE AT STATION 500B, STRINGER 25R . REPAIRED PER SRM 51-40-3. (M) 2 L 7 2 4F RT A16WE 1998091100347 19980911 00347 NM 1998 9 11 ASAA9810061 1 19980724 A 5313 STRINGER BOEING 737 737298C 1384490 NM BS 500 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND STRINGER 25R CRACKED AT STATION 500B. REPAIRED PER SRM 53-10-2. (M) 2 L 7 2 4F RT A16WE 1998091100348 19980911 00348 NM 1998 9 11 ASAA9810062 1 19980724 A 5313 STRINGER BOEING 737 737298C 1384490 NM BS 727 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND STRINGER 20L AT STATION 727 HAS RIVET HOLE CORRODED. REPAIRED PER SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 1998091100349 19980911 00349 NM 1998 9 11 ASAA9810063 1 19980724 A 5347 SEAT TRACK BOEING 737 737298C 1384490 NM BS 747-947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND LEFT SECOND FROM OUTBOARD SEAT TRACK CORRODED FROM STATION 747-947, BL 25L. REPAIRED PER SR M 53-10-2 AND SRM 53-10-5. (M) 2 L 7 2 4F RT A16WE 1998091100350 19980911 00350 NM 1998 9 11 ASAA9810064 1 19980724 A 5315 FLOORBEAM BOEING 737 737298C 1384490 NM BS 500 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND LOWER SURFACE OF FLOORBEAM CORRODED AT STATION 500, LBL 0- LBL 42. REPAIRED PER EA 5310-015 83. (M) 2 L 7 2 4F RT A16WE 1998091100351 19980911 00351 NM 1998 9 11 ASAA9810065 1 19980724 A 5315 FLOORBEAM BOEING 737 737298C 1384490 NM BS 460 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND LOWER SURFACE OF FLOORBEAM CORRODED AT STATION 460, LBL 23-LBL 42. REPAIRED PER SRM 51-10-2 AND ASA EA 5310-01584. (M) 2 L 7 2 4F RT A16WE 1998091100352 19980911 00352 NM 1998 9 11 ASAA9810066 1 19980724 A 5347 SEAT TRACK BOEING 737 737298C 1384490 NM BS 655-706 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND LOWER SIDE OF CENTER FLOOR TRACK CORRODED STATION 655-706, BL 0. REPAIRED PER SRM 53-10-2 A ND SRM 53-10-5. (M) 2 L 7 2 4F RT A16WE 1998091100353 19980911 00353 NM 1998 9 11 ASAA9810067 1 19980724 A 5320 SUPPORT BOEING 737 737298C 1384490 NM BS 540-706 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND FLOOR TRACK UPPER SUPPORT BEAM CORRODED AT STATION 540-706, LBL 24.75. REPAIRED PER ASA EA 5310-01587. (M) 2 L 7 2 4F RT A16WE 1998091100354 19980911 00354 NM 1998 9 11 ASAA9810068 1 19980724 A 5320 DOOR SILL BOEING 737 737298C 1384490 NM BS 474 DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND LEFT FUSELAGE MAIN CARGO DOOR SILL, LONGERON 17 AT STATION 474 DENTED. REPAIRED PER ASA EA 5330-01323. (M) 2 L 7 2 4F RT A16WE 1998091100355 19980911 00355 NM 1998 9 11 ASAA9810069 1 19980724 A 5320 SUPPORT BOEING 737 737298C 1384490 NM BS 758 CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND SEAT TRACK SUPPORT CRACKED AT STATION 758, RBL 25. REPAIRED PER ASA EA 5310-01585. (M) 2 L 7 2 4F RT A16WE 1998091100356 19980911 00356 NM 1998 9 11 ASAA9810070 1 19980724 A 5230 SKIN BOEING 737 737298C 1384490 NM CARGO DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND MAIN CARGO DOOR LOWER AFT CORNER CRACKED. REPAIRED PER ASA EA 5320-01082. (M) 2 L 7 2 4F RT A16WE 1998091100357 19980911 00357 EU 1998 9 11 RAIA980809 1 19980813 A 6120 31058993 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 572HK 5348 41091 DCA - FLT 7750- IEC'S FAULTED. REMOVED AND REPLACED NR 2 NTS PRESSURE SWITCH. (M) 2 L 7 2 4T RT A41NM 1998091100358 19980911 00358 EU 1998 9 11 RAIA980808 1 19980812 A 2710 MS14036PK BEARING JETAIR JETSTM JETSTM4101 1500501 EU LT AILERON LOOSE A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 553HK 41066 DURNG PRE-TAKEOFF CHECK, CREW NOTED RESTRICTION IN AILERON MOVEMENT. INSPECTION REVEALED THE ROLLER BEARING MIGRATED OU T OF THE CONTROL LINK. MAINTENANCE INSTALLED A NEW BEARING IAW SRM 51-70-02. (M) 2 L 7 2 4T RT A41NM 1998091100359 19980911 00359 NM 1998 9 11 P2EA98157 1 19980816 A 2612 WIRE BOEING 737 737247 138448D NM APU BAY BROKEN A P2EA A B UNSCHED LANDING EMER. DESCENT N FALSE WARNING NR NOT REPORTED 1 CE 05 204AU 19603 FLT 584 - MCI - EMERGENCY DECLARED, LANDING UNEVENTFUL. APU FIRE WARNING BELL AND LIGHT CAME ON IN FLIGHT. APU REPORTE D TO BE SHUT DOWN WHEN FIRE WARNING SOUNDED. CREW DISCHARGED APU EXTINGUISHER BOTTLE PERFORMED DETAILED VISUAL INSPECTI ON OF APU, SHROUD, STAB CROSS THROUGH AND APU TAILPIPE AREAS. CONFIRMED NO FIRE OCCURRED. REPAIRED BROKEN WIRE AT APU EXHAUST DUCT SENSOR AREA. REPLACED APU FIRE BOTTLE AND DISCHARGE DISK PER MM 26-22-11. OK FOR SERVICE. (M) 2 L 7 2 4F A16WE 1998091100360 19980911 00360 NM 1998 9 11 P2EA98158 1 19980814 A 3350 LIGHT BOEING 737 737247 138448D NM CABIN INOPERATIVE A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 912MP 19607 MCI - FLT 303 - L-1 DOOR EMERGENCY LIGHT INOP REPLACED BAD SPLICE ON WIRE TO L-1 DOOR LIGHT PER STANDARD PRACTICES. O PS NORMAL CLEARED DEFERRAL M912765. (M) 2 L 7 2 4F A16WE 1998091100361 19980911 00361 NM 1998 9 11 MASA98151 1 19980805 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING A ROUTINE MAINTENANCE CHECK, SEVERAL EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE. MAINTENANCE PERSONNEL REPLACED ALL SIX EMERGENCY LIGHT POWER SUPPLIES. SYSTEM OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998091100362 19980911 00362 CE 1998 9 11 MASA98144 1 19980718 A 7110 11891002791 COWLING BEECH 1900 1900D 1154162 CE RT NACELLE LOOSE A MASA E ENGINE SHUTDOWN D Y INFLIGHT SEPARATION ENGINE STOPPAGE AP APPROACH 1 SW 07 218YV UE218 FLT 5499 - JAX-MCO - ON APPROACH, THE CREW NOTICED THE RT PROP PITCH CHANGING UNCOMMANDED. THEY THEN NOTICED THE RT TOP COWLING WAS COMING LOOSE, AND WAS RESTING ON THE PROP GOVERNOR AND BETA VALVE. THE CREW DECLARED AN EMERGENCY, SHUT DO WN THE RT ENGINE, AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESECURED THE COWLING AND PERFORMED AN MAINTENANCE R UN ON THE AIRCRAFT AND SYSTEMS. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998091100363 19980911 00363 NM 1998 9 11 98ZZZM616 1 19980815 A 3350 36262R014 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 804MA 22435 ON PREFLIGHT TRANSIT FOUND LEFT SIDE EMERGENCY PATH LIGHTING INOP FROM L1 DOOR T 30 ABC. TROUBLESHOT SYSTEM, FOUND EPL WET. DRIED AND CLEANED EPL, OPS CHECK OK IAW MM 33-50-1. OPERATIONAL CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998091100364 19980911 00364 NM 1998 9 11 98ZZZM617 1 19980814 A 3350 900835A BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 808MA R3545 21988 ON 'A' SERVICE, FOUND RIGHT OVEWING EMERENCY LIGHT INOPERATIVE. TROUBLESHOT SYTEM. FOUND RIGHT OVERWING BATTERY PACK L OW CHARGE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD IAW MM 33-50-1. (M) 2 L 7 3 4F A3WE 1998091100365 19980911 00365 NM 1998 9 11 98ZZZM618 1 19980813 A 2751 1812993 INDICATOR BOEING 727 727225 1384077 NM COCKPIT MALFUNCTIONED A MYWA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 19 804MA 22435 DURING CLIMB-OUT ON FLAP RETRACTION BETWEEN 2 DEGREES AND FLAPS UP, INBOARD FLAPS LOCKED OUT. LEFT AND RIGHT NEEDLES DI D NOT AGREE. REMOVED AND REPLACED INBOARD FLAP INDICATOR AND ADJUSTED INBOARD TRANSMITTER PER MM 27-52-1. (M) 2 L 7 3 4F A3WE 1998091100366 19980911 00366 NM 1998 9 11 GAIA9881 1 19980811 A 3230 LINK BOEING 727 727251 138408H NM NLG LOOSE A GAIA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 264US 19983 EN ROUTE FROM OKC TO ICT, DURING CLIMB-OUT, THE NOSE LANDING GEAR WOULD NOT RETRCT. CYCLED GEAR WITHOUT SUCCESS. CONTI NUED EN ROUTE TO ICT AND LANDED WITHOUT DIFFICULTIES. INSPECTED NOSE LANDING GEAR AND FOUND THE DOWN LOCK ACTUATOR LINK DISCONNECTED. INSTALLED LINK. OPERATED NORMAL AND MANUAL. OPERATIONALLY CHECKS GOOD IAW B727 MM 32-31-01. RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 1998091100367 19980911 00367 NM 1998 9 11 MASA98149 1 19980727 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 5183 - PHX-TEX - DURING PREFLIGHT CHECK, CREW NOTICED THE HAND HELD EMERGENCY LIGHT WAS INOP. MAINTENANCE REMOVED A ND REPLACED THE HAND HELD EMERGENCY LIGHT ASSY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998091100368 19980911 00368 CE 1998 9 11 98ZZZM619 1 19980811 A 7712 1293800043 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 836CA 11735 130 UE32 RIGHT TORQUE GAUGE INOP. GAUGE FAILURE. REPLACED RT TORQUE GAUGE. (M) 2 L 7 2 4T RT A24CE 1998091100369 19980911 00369 CE 1998 9 11 98ZZZM620 1 19980811 A 3230 1013880083 VALVE BEECH 1900 1900D 1154162 CE LT WING FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 839CA 11245 1780 UE36 LANDING GEAR WILL NOT EXTEND NORMALLY MANUAL EXTENSION ONLY. LANDING GEAR SERVICE VALVE FAILURE. REPLACED GEAR SERVICE VALVE. (M) 2 L 7 2 4T RT A24CE 1998091100370 19980911 00370 CE 1998 9 11 98ZZZM621 1 19980807 A 3231 1148100451 CAM BEECH 1900 1900D 1154162 CE LT MLG DOOR BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 837CA UE16 NR 2 NLG DOOR UPLOCK CAM BROKEN. CAUSE UNKNOWN. REPLACED BROKEN CAM. (M) 2 L 7 2 4T RT A24CE 1998091100371 19980911 00371 CE 1998 9 11 98ZZZM622 1 19980810 A 3260 1003810061 SWITCH BEECH 1900 1900D 1154162 CE NLG WW FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 834CA UE25 RED LGHT IN GEAR HANDLE REMAINS ON. UPLOCK SWITCH (NOSE) FAILURE. REPLACED NOSE GEAR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A24CE 1998091100372 19980911 00372 NM 1998 9 11 HNAA9892233 1 19980724 A 3231 SENSOR DHAV DHC8 DHC8102 2809003 NM LT MLG MALFUNCTIONED A HNAA K NONE J WARNING INDICATION CL CLIMB 1 EA 07 922HA 094 FLT 3270 - CLT-CRW - LEFT MAIN GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION. INSPECTED PROX SENSORS AND WIRING PERFORM ED NEAR/FAR TARGET TEST. PERFORMED SEVERAL GEAR RETRACTIONS. COULD NOT DUPLICATE. (M) 2 H 7 2 4T RT A13NM 1998091100373 19980911 00373 EU 1998 9 11 98ZZZM623 1 19980724 A 2910 LINE STBROS SD3 SD360 8100606 EU HYDRAULIC SYSTEM LEAKING A HSYA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 NM 05 617FB SH3617 BIL - PILOT REPORTED A LOSS OF BRAKING ACTION AND A LOSS OF HYDRAULC FLUID DURING TAXI. LEAKING PRESSURE HYDRAULIC FLUI D LINE TO THE NOSE STEERING ACTUATOR. REMOVED AND REPLACED HOSE ASSY. REPLENISHED HYDRAULIC CONTENTS. LEAK AND FUNCTI ONAL CHECKED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A41EU 1998091100374 19980911 00374 WP 1998 9 11 HALA9800276 1 19980809 A 3242 50043215 BRAKE DOUG DC9 DC951 3022051 WP LT MLG LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 679HA APR940435A 47662 HNL - FLT 536 - ON TAXI OUT TOWER REPORTED VAPOR CLOUD FROM LEFT WHEEL WELL. RIGHT HYDRAULIC SYSTEM SLOWLY DECREASING I N QTY. FOUND LEFT MLG NR 2 POSITION BRAKE LEAKING. REPLACED NR 2 BRAKE, SPIN CHECK OK. SERVICED RIGHT HYDRAULIC SYSTE M WITH FLUID. (M) 2 L 7 2 4F RT A6WE 1998091100375 19980911 00375 WP 1998 9 11 HALA9800274 1 19980807 A 2150 ACM DOUG DC10 DC1010 3022110 WP AC SYSTEM FAILED A HALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 13 122AA 46522 FLT 14 - ON TAXI ADVISED BY CABIN CREW OF SMOKE IN THE CABIN AREA ROWS 23 TO 35. FLT ENGINEER WENT BACK, DESCRIBED FOGG Y OR HAZY. SOME FLT ATTENDANTS DESCRIBED SMELL OF ELECTRICAL, OTHERS AS LIKE A BURNED MATCH SMELL. RETURNED TO GATE. T URBINE INLET TEMP OBSERVED AS 235 DEG F COMPLETED AIR CONDITIONING SMOKE CHECKLIST AND INITIALLY FIRST PART OF ELECTRICA L FIRE OR SMOKE OF UNKNOWN ORIGIN CHECKLIST SINCE WE COULD NOT INITIALLY RULE OUT AN ELECTRICAL COMPONENT AS THE SOURCE OF THE SMOKE. (M) 2 L 7 3 4F A22WE 1998091100376 19980911 00376 WP 1998 9 11 HALA9800285 1 19980816 A 3350 60030451 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 669HA 13876 47654 HNL - OVERHEAD EMERGENCY LIGHTS AT ROW 7-11 ARE INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY, OPS CH ECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998091100377 19980911 00377 WP 1998 9 11 HALA9800283 1 19980815 A 3350 2078C BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 672MC 1050 47661 HNL - CABIN FLOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED CABIN FLOOR EMERGENCY LIGHT BATTER POWER SUPPLY, OPS CHEC K GOOD. (M) 2 L 7 2 4F RT A6WE 1998091100378 19980911 00378 NM 1998 9 11 F3LA98151 1 19980727 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 1006 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM 1006, LBL 14, WL 208. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-30-2, 53-10-1, 53-10-2, AND 53-10-9. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100379 19980911 00379 NM 1998 9 11 F3LA98150 1 19980727 A 5320 INTERCOSTAL BOEING 737 7372L9 1384497 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178.5, LBL 25, WL 194.5. MAINTENANCE REMOVED DAMAGE D INTERCOSTAL AND REPAIRED PER SRM 51-30-2. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100380 19980911 00380 NM 1998 9 11 F3LA98149 1 19980726 A 5511 RIB BOEING 737 7372L9 1384497 NM HORIZONTAL STAB CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAI - DURING C-CHECK, INSPECTION REPORTED CORROSION ON RT HORIZONTAL STABILIZER UPPER CHORD RIB AFT OF REAR SPAR AT BS 2 09.9. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-10-2, 51-20-4, 51-30-2, AND 51-30-5. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100381 19980911 00381 NM 1998 9 11 F3LA98160 1 19980804 A 5730 SKIN BOEING 737 7372L9 1384497 NM WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN NR 4 SLAT OUTBOARD AUXILIARY TRACK LEADING EDGE CUT-OUT SKIN. MAINTE NANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PART AND REPAIRED PER ER 98-0680, ER 98-0680A, SRM'S 51-00-00, 51-30- 2, AND MM 27-81-21. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100382 19980911 00382 NM 1998 9 11 F3LA98159 1 19980803 A 5730 SKIN BOEING 737 7372L9 1384497 NM LE FLAP CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON LT WING INBD MID-FLAP, LEADING EDGE INBD CORNER OF NOSE CHORD. MA INTENANCE REMOVED DAMAGED AREA (2.0 INCHES BY 1.0 INCH), FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-30-2, 51 -10-9, AND ER 98-0707. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100383 19980911 00383 NM 1998 9 11 F3LA98158 1 19980803 A 5730 SKIN BOEING 737 7372L9 1384497 NM WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN NR 2 SLAT CENTER UPSTOP CUT-OUT FIXED LEADING EDGE. MAINTENANCE REMO VED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-1 AND ER 98-06-89. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100384 19980911 00384 NM 1998 9 11 F3LA98157 1 19980802 A 5730 SKIN BOEING 737 7372L9 1384497 NM WING CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CRACK IN NR 5 SLAT CENTER UPSTOP CUT-OUT FIXED LEADING EDGE SKIN. MAINTENANCE REMOVED DAMAGED AREA. FABRICATED REPLACMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0693. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100385 19980911 00385 NM 1998 9 11 F3LA98156 1 19980731 A 5320 INTERCOSTAL BOEING 737 7372L9 1384497 NM BS 178 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT BS 178.5, RBL 25.25, WL 194.5. MAINTENANCE REPLACED DAM AGED INTERCOSTAL PER SRM 51-30-2 AND SRM 51-30-5. CYCLES: 1941. (X) 2 L 7 2 4F RT A16WE 1998091100386 19980911 00386 NM 1998 9 11 F3LA98155 1 19980730 A 5551 CLEVIS BOEING 737 7372L9 1384497 NM HORIZONTAL STAB CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON RT HORIZONTAL STABILIZER REAR LOWER CLEVIS ON FORWARD SIDE AROUND BUSHING. MAINTENANCE BLENDED CORROSION (1 INCH BY .035 INCH BY .081 INCH; .15 INCH BY .4 INCH BY .023 INCH; .15 INCH B Y .7 INCH BY .037 INCH; .3 INCH BY .5 INCH BY .046 INCH; .13 INCH BY .40 INCH BY .049 INCH; .15 INCH BY .40 INCH BY .062 INCH; AND, .10 INCH BY .50 INCH BY .065 INCH). INSTALLED NEW BUSHING AND REPAIRED PER SRM'S 51-10-8, 55-10-1, OHM 20-1 0-3, AND ER 98-0704. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100387 19980911 00387 NM 1998 9 11 F3LA98154 1 19980727 A 5311 FRAME BOEING 737 7372L9 1384497 NM BS 727 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED LEFT 727 CHORD CRACKED. MAINTENANCE REMOVED DAMAGED CHORD AND REPLACED PER SB 737-53-1088, ER 98-0677, SRM'S 51-30-2 ADN 53-10-1. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100388 19980911 00388 NM 1998 9 11 F3LA98153 1 19980727 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 987 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT BS 987, WL 208, LBL 3 TO RBL 20. MAINTENANCE BLENDE D CORROSION (2 INCHES BY 1 INCH BY .018 INCH; 2.5 INCHES BY 1 INCH BY .015 INCH). REMOVED DAMAGED FLOORBEAM, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0695. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100389 19980911 00389 NM 1998 9 11 F3LA98152 1 19980727 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED FORWARD GALLEY DOOR AFT DOOR FRAME CRACKED AT NR 4 STOP PIN FITTING CUT-OUT. M AINTENANCE STOP DRILLED CRACK, FABRICATED DOUBLER AND REPAIRED PER SRM'S 51-10-2, 51-30-2, 52-00-2, AND ER 98-0705. CYC LES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100390 19980911 00390 NM 1998 9 11 F3LA98161 1 19980809 A 5312 PRESSURE BLKHD BOEING 737 737201 1384454 NM NLG WW CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 212US 1533 20212 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 7 INCH/8 INCH CRACK IN NOSE WHEEL WELL PRESSURE WEB. OUTBOARD RT SID E AFT OF DOWNLOCK VIEWER. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED PER SRM 51-40-2, FIG 1. CYCLES: 1,199. (X) 2 L 7 2 4F A16WE 1998091100391 19980911 00391 NM 1998 9 11 F3LA98142 1 19980728 A 5320 SHEAR TIE BOEING 737 7372L9 1384497 NM BS 967 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 22733 PAI - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT BS 967, LBL 14. MAINTENANCE REMOVED DAMAGED SHEAR T IE, FABRICATED REPLACEMENT PART AND REPAIRED PER SRM'S 51-30-2, 51-30-5, AND 53-10-1. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100392 19980911 00392 NM 1998 9 11 F3LA98143 1 19980728 A 3350 BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 EICHH 21 23177 DEN - DURING A-5 CHECK, INSPECTION REPORTED AFT SECTION OF FLOOR PROXIMITY LIGHTING AT R-2 DOOR INOPERATIVE. REPLACED B ATTERY PACK AND SYSTEM CHECKED OKAY. (X) 2 L 7 2 4F RT A16WE 1998091100393 19980911 00393 NM 1998 9 11 F3LA98144 1 19980728 A 3350 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 214AU 18 20214 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LT OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REP LACED BATTERY PACK AND SYSTEM CHECKED OKAY. (X) 2 L 7 2 4F A16WE 1998091100394 19980911 00394 NM 1998 9 11 F3LA98146 1 19980724 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED 3 CRACKS IN AFT LOWER CORNER OF FORWARD SERVICE DOOR CUT-OUT SKIN. REMOVED DA MAGED AREA, FABRICATED REPLACMENT PARTS AND REPAIRED PER SRM'S 51-30-2 AND 53-30-3. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100395 19980911 00395 NM 1998 9 11 F3LA98145 1 19980724 A 5330 SKIN BOEING 737 7372L9 1384497 NM FUSELAGE CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED .25 INCH CRACK IN LOWER HINGE CUT OUT OF FORWARD ENTRY DOOR. MAINTENANCE REMO VED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-20-4, 51-30-2, AND 53-30-3. CYCLES: 1,941. ( X) 2 L 7 2 4F RT A16WE 1998091100396 19980911 00396 NM 1998 9 11 F3LA98147 1 19980725 A 5320 SHEAR TIE BOEING 737 7372L9 1384497 NM BS 947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT BS 947, RBL 3, WL 171. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM'S 51-10-3, 51-30-2, AND 53-10-1. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100397 19980911 00397 NM 1998 9 11 F3LA98148 1 19980725 A 5313 STRINGER BOEING 737 7372L9 1384497 NM BS 969 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 270FL 3225 22733 PAI - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STR 25L, BS 969. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED RE PLACEMENT PARTS AND REPAIRED PER SRM'S 51-10-1, 51-30-2, AND 53-10-3. CYCLES: 1,941. (X) 2 L 7 2 4F RT A16WE 1998091100398 19980911 00398 NM 1998 9 11 EISA98203 1 19980808 A 2780 6963642 BEARING BOEING 727 727223 1384074 NM LE FLAP FAILED A EISA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TO TAKEOFF 1 SW 07 311NE 19703 ON DEPARTURE, RETRACTING FLAPS FROM 2 DEGREES TO 0 DEGREES INBOARD FLAP GAUGE REMAINED AT 2 DEGREES. LEADING EDGE FLAPS INDICATOR LIGHTS DID NOT INDICATE AN AMBER LIGHT NOR DID FLIGHT ENGINEER PANEL SHOW (FLAP POSITION INDICATOR) LEADING E DGE FLAPS OR SLATS EXTENDED. RETURNED TO PDX. GENERATED FROM PILOT REPORTED. REPLACED RIGHT INBOARD FLAP INBOARD JACK SCREW FAIRING BEARING. OPS CHECK GOOD 27-51-0. (M) 2 L 7 3 4F A3WE 1998091100399 19980911 00399 WP 1998 9 11 EISA98202 1 19980806 A 3231 3967851 LINK DOUG DC9 DC931 3022065 WP NLG DOOR DAMAGED A EISA H DEACTIVATE SYST/CIRCUITS E VIBRATION/BUFFET TO TAKEOFF 1 SW 07 977ML 47329 VIBRATION IN NOSHE WHEEL AFTER GEAR RETRACTION, RETURNED TO ELP. GENERATED FROM PILOT REPORT. FOUND RIGHT NOSE GEAR DO OR FORWARD LINK BAD. REMOVED AND REPLACED DOOR LINK. OPS CHECK COMPLETED. NO FURTHER DEFECTS NOTED PER MM 32-22-1. R ETRACTION CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1998091100400 19980911 00400 NM 1998 9 11 EISA98201 1 19980804 A 2611 302842 DETECTOR BOEING 727 72725 1384006 NM CARGO BAY FAILED A EISA O OTHER N FALSE WARNING LD LANDING 1 SW 07 290NE 18972 AFTER LANDING CARGO SMOKE LGHT ILLUMINATED VERIFIED VISUALLY NO SMOKE FOR FIRE, COULD NOT EXTINGUISH LIGHT. GENERATED F ROM PILOT REPORT. TROUBLESHOOTING FOUND LIGHT WOULD GO OUT WITH NR 4 SMOKE DETECTOR DISCONNECTED. REPLACED NR 4 SMOKE DETECTOR. CHECKS NORMAL PER AERONAUTICAL MM CHAPTER 1. (M) 2 L 7 3 4F A3WE 1998091100401 19980911 00401 WP 1998 9 11 EISA98200 1 19980731 A 3350 JA40106001A BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A EISA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 950VJ 47564 RIGHT DOOR EMERGENCY SLIDE INOPERATIVE. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED RIGHT GALLEY DOOR EMERGENCY SLIDE LIGHT BATTERY PER MM 33-50-1. OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998091100402 19980911 00402 NM 1998 9 11 EISA98199 1 19980730 A 2130 39854021 SHUTOFF VALVE BOEING 727 72725 1384006 NM LT PACK FAILED A EISA H DEACTIVATE SYST/CIRCUITS O OTHER TO TAKEOFF 1 SW 07 300NE P3258 18974 AFTER TAKEOFF FROM BDL, AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL GENERATED FROM PILOT REPORT. REMOVED AND REPLACE D LEFT PACK VALVE. REMOVED AND REPLACED OUTFLOW CONTROL VALVE, AND FLOW CONTROL MODULATING VALVE. OPS CHECK NORMAL PER 21-30-00. (M) 2 L 7 3 4F A3WE 1998091100403 19980911 00403 NM 1998 9 11 98ZZZM624 1 19980730 A 2133 1310461 OUTFLOW VALVE BOEING 727 72725 1384006 NM LT PACK FAILED A EISA H DEACTIVATE SYST/CIRCUITS O OTHER TO TAKEOFF 1 SW 07 300NE 11565 18974 AFTER TAKEOFF FROM BDL, AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL GENERATED FROM PILOT REPORT. REMOVED AND REPLACE D LEFT PACK VALVE. REMOVED AND REPLACED OUTFLOW CONTROL VALVE, AND FLOW CONTROL MODULATING VALVE. OPS CHECK NORMAL PER 21-30-00. (M) 2 L 7 3 4F A3WE 1998091100404 19980911 00404 NM 1998 9 11 98ZZZM625 1 19980730 A 2130 39222011 CONTROL VALVE BOEING 727 72725 1384006 NM LT PACK FAILED A EISA H DEACTIVATE SYST/CIRCUITS O OTHER TO TAKEOFF 1 SW 07 300NE P871 18974 AFTER TAKEOFF FROM BDL, AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL GENERATED FROM PILOT REPORT. REMOVED AND REPLACE D LEFT PACK VALVE. REMOVED AND REPLACED OUTFLOW CONTROL VALVE, AND FLOW CONTROL MODULATING VALVE. OPS CHECK NORMAL PER 21-30-00. (M) 2 L 7 3 4F A3WE 1998091100405 19980911 00405 NM 1998 9 11 EISA98198 1 19980730 A 2150 RT PACK BOEING 727 72725 1384006 NM AC BAY MALFUNCTIONED A EISA H DEACTIVATE SYST/CIRCUITS O OTHER TO TAKEOFF 1 SW 07 300NE 18974 AFTER TAKEOFF AIRCRAFT WOULD NOT PRESSURIZE, RETURNED TO BDL. GENERATED FROM PILOT REPORT. RESET RIGHT PACK. (M) 2 L 7 3 4F A3WE 1998091100406 19980911 00406 NM 1998 9 11 EISA98197 1 19980722 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 600 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND SEAT TRACK CORRODED LEFT OUTBOARD AT STATION 600. REPLACED SEAT TR ACK WITH NEW SECTION FROM 560-630 PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1998091100407 19980911 00407 NM 1998 9 11 EISA98196 1 19980722 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 700 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND RIGHT INBOARD SEAT TRACK CORRODED AT FS APPROX 700. REMOVED DAMAGE D TRACK AND REPLACED WITH NEW SECTION FROM FS 580-700 PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1998091100408 19980911 00408 NM 1998 9 11 EISA98195 1 19980722 A 5330 SKIN BOEING 727 727223 1384074 NM BS 420 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND CRACK IN FUSELAGE SKIN AT FS 420 AT STRINGER 22R. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR PER SRM 53-30-3 FIG 23. (M) 2 L 7 3 4F A3WE 1998091100409 19980911 00409 NM 1998 9 11 EISA98194 1 19980722 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 570 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND LEFT OUTBOARD SEAT TRACK EXFOLIATED ON UPPER SIDE OF FS 576 BL 606. REMOVED DAMAGED TRACK AND REPLACED WITH NEW SECTION PER SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1998091100410 19980911 00410 NM 1998 9 11 EISA98193 1 19980722 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 620 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND LEFT OUTBOARD SEAT TRACK AT STATION 620 CORRODED. REPLACED SEAT TR ACK WITH NEW SECTION FROM STATION 560-630 PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998091100411 19980911 00411 NM 1998 9 11 EISA98192 1 19980730 A 5312 PRESSURE BLKHD BOEING 727 727223 1384074 NM NLG CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF C-CHECK CPCP CARD, FOUND CORROSION NOSE LANDING GEAR DOG HOUSE STATION 324 PRESSURE WEB LEFT. R EMOVED AND REPLACED DAMAGED WEB PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998091100412 19980911 00412 NM 1998 9 11 EISA98189 1 19980722 A 5311 FRAME BOEING 727 727223 1384074 NM FUSELAGE CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF C-CHECK CPCP CARD, FOUND 8 INCH LONG SPLIT IN LEFT HORIZONTAL REAR CHORD AND CORROSION. REMOVE D AND REPLACED UPPER CHORD BEAM PER SRM 51-30-2 AND 53-16-5. (M) 2 L 7 3 4F A3WE 1998091100413 19980911 00413 NM 1998 9 11 EISA98190 1 19980722 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 680 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, CORROSION WAS FOUND ON FLOORBEAM AT STATION 680 LBL 52. REMOVED CORROSIO N USING DER DRAWING 53-98395 AND SRM 51-30-02 AND 53-10-08. (M) 2 L 7 3 4F A3WE 1998091100414 19980911 00414 NM 1998 9 11 EISA98191 1 19980730 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 580 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, FOUND SEAT TRACK AT STATION 580 CORRODED. REMOVED AND REPLACED DAMAGED S ECTION OF TRACK FROM 540 TO 680 PER SRM 51-10-5. (M) 2 L 7 3 4F A3WE 1998091100415 19980911 00415 SO 1998 9 11 MASA98133 1 19980630 A 2120 AIR DISTRIBUTION EMB 120 EMB120RT SO RT PACK SMOKE A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 180YV 120180 FLT 5281 - FLL-MIA - CREW REPORTED THAT WITH RT PACK ON, SMOKE ACCUMULATED IN CABIN DURING FLIGHT. AIRCRAFT LANDED IN M IA WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, NO DISCREPANCIES WERE NOTED. AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A31SO 1998091100416 19980911 00416 CE 1998 9 11 98ZZZM626 1 19980717 A 5210 12951410333 DOOR STRUT BEECH 1900 1900D 1154162 CE PAX DOOR BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 852CA UE55 CABIN DOOR STRUT BROKEN. BROKEN STRUT. REPLACED STRUT. (M) 2 L 7 2 4T RT A24CE 1998091100417 19980911 00417 EU 1998 9 11 VTZA98237 1 19980708 A 2120 AIR DISTRIBUTION JETAIR JETSTM JETSTM4101 1500501 EU CABIN FUMES A VTZA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 27 313UE 41026 FLT 6464 - JFK-BOS - DURING CRUISE, AIRCRAFT DIVERTED TO PVD DUE TO FUMES IN THE CABIN. AIRCRAFT WENT TO GATE AT PVD WI TH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND COULD FIND NOT DEFECTS. CREW SUSPECTS PASSENGERS HAD SOMETHING ON TH EM THAT CAUSED SMELL NOT WARNING INDICATED, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M ) 2 L 7 2 4T RT A41NM 1998091100418 19980911 00418 NM 1998 9 11 GAIA9875 1 19980803 A 5714 WING BOX BOEING 727 727214 138407R NM FUSELAGE CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 750US 21512 DURING ACCOMPLISHMENT ON AD 85-24-02, RAM AIR PLENUM CORROSION INSPECTION. CORROSION WAS FOUND ALONG THE LEFT SIDE WING BOX CENTER SECTION AT STRINGER 5C. THE CORROSION WAS BLENDING OUT AND A DOUBLER WAS INSTALLED. THE AREA WAS REPAIRED IAW BOEING ENGINEERING LETTER AOC-OKC-98-051RR DATED 02-JUN-98 BY AAR OKC. STRUCTURAL SUBSTANTIATION OF REPAIR PLAN IS AN AMOC TO AD 85-24-02. THE AREA WAS RESTORED TO NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998091100419 19980911 00419 NM 1998 9 11 ASAA9810075 1 19980724 A 5240 FRAME BOEING 737 737298C 1384490 NM APU BAY MISMANUFACTURED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND APU 'Z' FRAME HAS TOO SHORT OF EDGE DISTANCE ON AFT 10 RIVETS. REPAIRED PER ASA EA 5240-010 32. (M) 2 L 7 2 4F RT A16WE 1998091100420 19980911 00420 WP 1998 9 11 ASAA9880124 1 19980710 A 5210 LATCH DOUG DC9 DC983 3022083 WP PAX DOOR MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WOLD NOT RELEASE FROM THE LATCHED OPEN POSITION. ADJUSTED THE DOOR HOLD OPE N LATCH RELEASE MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091100421 19980911 00421 WP 1998 9 11 ASAA9880132 1 19980715 A 2120 AIR DISTRIBUTION DOUG DC9 DC983 3022083 WP CABIN SMOKE A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 942AS 53052 LAX - AIR TURNBACK OF FLT 537 - CREW REPORTED SMOKE IN CABIN DURING CLIMB-OUT PASSING 18,000 FT, SMOKE ALARMS ACTIVATED IN BOTH AFT LAVATORIES. SMOKE DISSIPATED DURING DESCENT AND LANDED WITHOUT INCIDENT. INSPECTED BOTH ENGINES INLET AND EXHAUST, BOTH AIR CONDITIONING PACKS AND DISCHARGE DUCTS, AND LAVATORIES AND GALLEYS, NO DEFECT NOTED. ACCOMPLISHED RUN UP OF BOTH ENGINES. OPERATED BOTH AIR CONDITIONING PACKS, TURNED ON GALLEY OVENS, AND ACCOMPLISHED AIR QUALITY CHECK, NO SMOKE OR DEFECT NOTED. (M) 2 L 7 2 4F RT A6WE 1998091100422 19980911 00422 WP 1998 9 11 HALA9800272 1 19980806 A 3230 AC670753 BRACKET DOUG DC10 DC1010 3022110 WP NLG WW FAILED A HALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 13 122AA 46522 LAX - FLT 9 - RIGHT NOSE GEAR DOOR DID NOT RETRACT. REMOVED AND REPLACED FORWARD RIGHT DRIVE LINK ASSY. (M) 2 L 7 3 4F A22WE 1998091100423 19980911 00423 EU 1998 9 11 SIMA982104 1 19980729 A 5320 S5367800824602 ZEE MEMBER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 249AT 0249 SAW - DURING CPCP-4 INSPECTION, FOUND RIGHT AFT ZEE MEMBER CORRODED BETWEEN FRAME 39 AND 41. REMOVED AND REPLACED ZEE M EMBER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998091100424 19980911 00424 EU 1998 9 11 SIMA982182 1 19980806 A 5320 S53678008200 ZEE MEMBER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 414WF 414 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT AFT ZEE MEMBER, BETWEEN FRAME 39 AND 40 CORRODED. REMOVED AND REPLACED ZEE M EMBER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998091100425 19980911 00425 WP 1998 9 11 USAAD98139 1 19980806 A 3231 833703 SENSOR DOUG DC9 DC981 3022081 WP LT MLG WW MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 827US 48049 CLT - FLT 995 - AFTER TAKEOFF FROM CLT AND GEAR RETRACTION, THE GEARS DOOR LIGHTS REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR AND RECEIVED THE SAME INDICATION. THE FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANC E REPLACED THE LEFT MAIN LANDING GEAR DOOR OPEN SENSOR. (M) 2 L 7 2 4F A6WE 1998091100426 19980911 00426 NM 1998 9 11 USAASB98181 1 19980712 A 3230 UPLOCK BOEING 737 7372B7 1384560 NM MLG MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 271AU 22883 CLT - FLT 798 - CAPT REPORTED AT FL180 AND 310 KNOTS, ALL THREE LANDING GEAR EXTENDED WITH THE GEAR SELECTOR IN THE 'OFF POSITION. CREW SLOWED A/C DOWN AND RAISED THE GEAR SELECTOR TO THE 'UP' POSITION. NOSE GEAR RETRACTED AND THE MAINS S TAYED DOWN FOR ABOUT 90 SECONDS, THE RETRACTED. CREW DECLARED AN EMEREGNCY AND RETURNED TO FIELD AT CLT. A FLYBY THE T OWER WAS ACCOMP TO DETERMINE IF GEAR WAS IN DOWN POSITION BEFORE LANDING. GEAR WAS CONFIRMED DOWN. FLIGHT LANDED WITHO UT FURTHER INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE INSPECTED LANDING GEARS AND UPLOCK ASSEMBLI ES. VERIFIED NORMAL AND MANUAL EXTENSION AND RETRACTION TEST PER MM 32-34-0 AND 32-32-0. COULD NOT DUPLICATE. GEAR CH 2 L 7 2 4F A16WE 1998091100427 19980911 00427 NM 1998 9 11 USAASB98206 1 19980810 A 3350 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 231US 21976 GSO - MAINTENANCE FOUND THE AFT LEFT SERVICE DOOR EXTERIOR LIGHT INOP. MAINTENANCE FOUND A BAD WIRE SPLICE. REMOVED AN D REPLACED WIRE SPLICE 1724. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998091100428 19980911 00428 NE 1998 9 11 USAAD98141 2 19980809 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT NACELLE MALFUNCTIONED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J Y OVER TEMP WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 EA 19 817US 48097 PIT - FLT 365 - EN ROUTE BUF-CLT - CREW NOTED A RISE IN THE LEFT ENGINE OIL TEMPERATURE, EXCEEDING 165 DEGREES. THE ENG INE STARTED TO VIBRATE. CREW SECURED THE ENGINE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENA NCE REPLACED THE ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998091100429 19980911 00429 NM 1998 9 11 USAA980315 1 19980722 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 42036 22885 CLT - DURING CX-6 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN THE FUSELAGE SKIN FORWARD ENTRY DOOR FRAME LOWER AFT COR NER. INSTALLED DOUBLER OF .063 CRES 301 1/2 HARD AND A TRIPLER OF .063 CRES 301 1/2 HARD PER EA 62121B. (M) 2 L 7 2 4F A16WE 1998091100430 19980911 00430 NM 1998 9 11 USAA980316 1 19980722 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 986-1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 42036 22885 CLT - DURING CX-6 CHECK VISUAL INSPECTION, FOUND HEAVY CORROSION STRINGER 27L STATION 986 TO STATION 1006. REPLACED WIT H NEW SECTION OF STRINGER PER EA 62127 AND SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1998091100431 19980911 00431 NM 1998 9 11 USAA980298 1 19980716 A 5330 657371514 SKIN BOEING 737 737401 1384701 NM BS 120-123 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 420US 27664 23987 CLT - DURING A DROP IN CHECK VISUAL INSPECTION, FOUND A 3.5 INCH CRACK RIGHT HORIZ STABILIZER 120-123, 2 INCHES FORWARD OF REAR SPAR, LOWER IN SPAR SKIN. INSTALLED DOUBLER PER T/P 55-10-07, EA 62085. (M) 2 L 7 2 4F RT A16WE 1998091100432 19980911 00432 NM 1998 9 11 TWRA9846 1 19980806 A 3350 65B5003737 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 EMERGENCY LIGHT ABOVE SEAT 31 HJK INOP. REMOVED AND REPLACED LIGHT ASSY. (M) 2 L 7 4 4F A20WE 1998091100434 19980911 00434 NE 1998 9 11 TWRA9844 2 19980806 A 7250 772832001 TURBINE BOEING 747 747121 1384871 NM PWA JT9 JT9D7F 52054 NE ENGINE CRACKED A TWRA K NONE T ENGINE CASE PENETRATION IN INSP/MAINT 1 EA 15 617FF 19650 662443 DURING ROUTINE INSPECTION, AN .9375 INCH CRACK WAS FOUND ON THE LOW PRESSURE TURBINE CASE EXITING OUT OF THE EGT THERMAL COUPLE PORT AT THE 1 O'CLOCK POSITION. ENGINE WAS REMOVED FROM SERVICE. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998091100435 19980911 00435 NM 1998 9 11 TWRA9843 1 19980731 A 3350 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 B-ZONE AND L-5 MED CEILING LIGHT INOPERATIVE (NR 1). REPLACED LIGHT ASSY. OPS OK. 2 L 7 4 4F A20WE 1998091100436 19980911 00436 NM 1998 9 11 TWRA9842 1 19980731 A 3350 S1356B37 LIGHT BOEING 747 747238B 1384828 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 607PE 20011 R-1 - R-3 BUSSLE LIGHT INOPERABLE (NR1). REPLACED LIGHT ASSY. OPS CHECK OK. R-1 REPAIRED BROKEN WIRE. (X) 2 L 7 4 4F A20WE 1998091100437 19980911 00437 EU 1998 9 11 SIMA982232 1 19980811 A 5320 S5367131831001 SILL AEROSP ATR72 ATR72212 EU SERVICE DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-4 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE CORRODED. REMOVED AND REPLACED SILL PLATE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998091100438 19980911 00438 EU 1998 9 11 SIMA982231 1 19980811 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND THE FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND R EPLACED BOTH SEATS TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998091100439 19980911 00439 EU 1998 9 11 98ZZZM627 1 19980811 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT INBOARD AND THE FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND R EPLACED BOTH SEATS TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998091100440 19980911 00440 EU 1998 9 11 SIMA982233 1 19980811 A 5315 S5367240825402 FLOORBEAM AEROSP ATR72 ATR72212 EU BS 39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 440AM 440 SAW - DURING CPCP-4 INSPECTION, FOUND FLOORBEAM 39 CORRODED AROUND THE NUT PLATE ATTACH POINT ON THE RIGHT SIDE. REPAIR ED FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998091100471 19980911 00471 NM 1998 9 11 CA980616010 1 19980607 A 2760 82950010271 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SPOILER LEAKING W K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 21348 120329 (CAN) NR 1 HYDRAULIC QUANTITY LOW. FOUND A LEAK ON A HYDRAULIC LINE GOING TO THE ROLL SPOILER ACTUATOR. PART TC: 25 ,786. 2 H 7 2 4T 4 T RT A13NM E20NE 1998091100473 19980911 00473 WP 1998 9 11 TWA9814301 1 19980903 A 3320 BV0405501108 SOCKET DOUG DC9 DC982 3022082 WP CABIN WORN A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 905TW 49157 ELECTRICAL SMELL FIRST TWO ROWS OF COACH. LOWER SIDE WALL AND UPPER SIDE WALL LIGHTS WERE TURNED OFF AND ODOR WENT AWA Y. FOUND EVIDENCE OF ARCING ON CABIN ROW 5A UPPER SIDE WALL LIGHT. REPLACED SOCKET. CHECK-C 12-16-97 MCI. 2 L 7 2 4F A6WE 1998091100474 19980911 00474 WP 1998 9 11 TWAA9813419 1 19980902 A 5313 LONGERON DOUG DC9 DC915 3022036 WP BS 130-160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 INTERCOASTAL LONGERON 28L STA 130 TO 160 HAD CORROSION DAMAGE. INSTALLED INTERCOASTAL PER DWG 5910343. COMPLIED WITH A RA 9240 REV A. CHECK-C 11-22-98 STL. 2 L 7 2 4F A6WE 1998091100475 19980911 00475 NM 1998 9 11 TWAA9814302 1 19980904 A 3010 43617241 GASKET BOEING 727 727231 1384079 NM WING ANTI-ICE LEAKING A TWAA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 CE 05 54340 20845 NR 1 STRUT OVERHEAT ILLUMINATED IN FLIGHT. EXTINGUISHED WHEN NR 1 BLEED SELECTED CLOSED. FLIGHT RETURNED TO STL. REPL ACED 2 EA 13TH STAGE WING ANTI-ICE VALVE GASKETS. CHECK-C 8-23-98 MCI. 2 L 7 3 4F A3WE 1998091100476 19980911 00476 NM 1998 9 11 TWAA9814303 1 19980906 A 3350 588224 POWER SUPPLY BOEING 767 767231 1385131 NM CABIN INOPERATIVE A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 610TW 22573 EGRESS LIGHT ON RT SIDE OF FWD CABIN ILLUMINATE INTERMITTENTLY. REPLACED EGRESS POWER SUPPLY. CHECK-C 6-14-98 LAX. 2 L 7 2 4F RT A1NM 1998091100477 19980911 00477 NM 1998 9 11 TWAA9814304 1 19980906 A 3350 CONNECTOR BOEING 767 767231 1385131 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 610TW 22573 FOUND EGRESS LIGHT STRIP INOPERATIVE IN AFT GALLEY AREA DURING MAINTENANCE TEST. FOUND LOOSE CONNECTION. RESEATED FLEX JUMPER TO POWER FLEX CABLE AND SECURED. CHECK-C 6-14-98 LAX. 2 L 7 2 4F RT A1NM 1998091100478 19980911 00478 WP 1998 9 11 TWAA9814305 1 19980906 A 2170 1794609 COALESCER BAG DOUG DC9 DC983 3022083 WP LT & RT DIRTY A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 9305N 49395 STRONG ODOR WITH SMOKY HAZE IN COCKPIT AND CABIN AFTER TAKEOFF. FLT RETURNED TO SFO. CHECKED ALL ACFT COMPARTMENTS, CH ECKED APU CHECK VALVE, AND ACM OUTLETS FOR OIL. NO SIGN OF OIL. CHANGED BOTH WATER SEPARATORS. ALSO ACCOMP ENG RUN AN D PACK BURN OUT PROCEDURE. CHECK-C 8-7-98 MCI. 2 L 7 2 4F RT A6WE 1998091100479 19980911 00479 WP 1998 9 11 TWAA9814306 1 19980827 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 29 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND SLIGHT BULGE IN SKIN WITH STRESSED FASTENERS AND BLIND FASTENERS INSTALLED AT STA 29L, J UST AFT OF ELECTRONIC COMPT DOOR. BLENDED DENT AREA AND INSTALLED .025 TITANIUM INTERNAL DOUBLER PER SRM 53.04, FIG 38 SHEET 28 PAGE 218H. 2 L 7 2 4F A6WE 1998091100480 19980911 00480 WP 1998 9 11 TWAA9814307 1 19980902 A 5753 RIB DOUG DC9 DC931 3022065 WP LT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND LT WING TE O/B RIB CRACKED AT TOP BOLT HOLE INSIDE FLAP AT O/B HINGE ARM. REPLACED O/B RIB PER SRM 57-50-3, PAGE 9 AND 10, IPC 27-50-01, FIG 2B PAGE 0 TO 7. 2 L 7 2 4F A6WE 1998091100481 19980911 00481 WP 1998 9 11 TWAA9814308 1 19980902 A 5753 RIB DOUG DC9 DC931 3022065 WP LT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND LT WING TE, I/B RIB CRACKED IN RADIUS BELOW BOLT HOLE, INSIDE FLAP AT O/B HINGE ARM. RE PLACED I/B RIB PER SRM 57-50-3, PAGES 9 AND 10. IPC 27-50-01, FIG 2B PAGES 0 TO 7. 2 L 7 2 4F A6WE 1998091100482 19980911 00482 WP 1998 9 11 TWAA9814309 1 19980902 A 5220 PAN DOUG DC9 DC931 3022065 WP LT EMER EXIT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND LT FWD EMERGENCY EXIT DOOR PAN CRACKED, WITH INTERIM REPAIR INSTALLED. INSTALLED NEW PA N STOCK NR 63-3273. 2 L 7 2 4F A6WE 1998091100483 19980911 00483 WP 1998 9 11 TWAA9814310 1 19980902 A 5312 BULKHD STIFFENER DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND .75 INCH CRACK AT UPPER RIVET HOLE ON VERT STIFFENER, AFT SIDE OF BULKHEAD, BETWEEN LONG 3L AND 4L. REPLACED TIE CLIP, UPPER END OF STIFFENER, WITH FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 1998091100484 19980911 00484 WP 1998 9 11 TWAA9814311 1 19980902 A 5330 SKIN DOUG DC9 DC915 3022036 WP E/E DOORWAY CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 DURING ROUTINE MAINT, FOUND CORROSION ON ELECTRONIC COMPT DOOR DOUBLER AND EXTERIOR SKIN AROUND DOOR. REMOVED AND REPLA CED SKIN AND DOUBLER PER ARA 9240. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100485 19980911 00485 WP 1998 9 11 TWAA9814312 1 19980902 A 5330 SKIN DOUG DC9 DC915 3022036 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 STA 110 TO 174 BELLY SKIN REMOVED FOR CORROSION DAMAGE FROM LONGERON 26L TO 26R. REMOVED AND REPLACED SKIN PER ARA 9240 . CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100486 19980911 00486 WP 1998 9 11 TWAA9814313 1 19980902 A 5311 FORMER DOUG DC9 DC915 3022036 WP BS 134 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 FORMER RING REMOVED STA 134, LONGERON 24L TO L24R DUE TO CORROSION DAMAGE. INSTALLED NEW FORMER RING REF DOUGLAS DWG 9 911512 AND ARA 9240. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100487 19980911 00487 WP 1998 9 11 TWAA9814314 1 19980902 A 5320 ANGLE DOUG DC9 DC915 3022036 WP BS 110-129 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 CHORD ANGLE REMOVED FOR CORROSION DAMAGE STA 110 TO 129, LBL 14 IN. INSTALLED NEW CHORD ANGLE REF DOUGLAS DWG 5911401. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100488 19980911 00488 WP 1998 9 11 TWAA9814315 1 19980902 A 5320 ANGLE DOUG DC9 DC915 3022036 WP FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 FORMER FOOT ANGLE LONGERON 26L TO 27L REMOVED FOR CORROSION. REMOVED AND REPLACED FORMER FOOT REF DOUGLAS DWG 9911515. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100489 19980911 00489 WP 1998 9 11 TWAA9814316 1 19980902 A 5320 ANGLE DOUG DC9 DC915 3022036 WP BS 160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 FORMER FOOT ANGLE LONGERON 26R TO 27R STA 160 REMOVED FOR CORROSION. REMOVED AND REPLACED FORMER FOOT REF DOUGLAS DWG 9 911515. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100490 19980911 00490 WP 1998 9 11 TWAA9814317 1 19980902 A 5320 JAMB DOUG DC9 DC915 3022036 WP BS 134-160 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 DOOR JAMB STRUCTURE REMOVED AT ELECTRONIC COMPT DOOR FOR CORROSION DAMAGE STA 134 TO 160, LONGERON 28L TO 28R WITH ATTAC H STRUCTURE. ACCOMPLISHED ARA 9240 REV A. INSTALLED DOOR JAMB STRUCTURE PER DWG 5910343. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100491 19980911 00491 WP 1998 9 11 TWAA9814318 1 19980902 A 5320 INTERCOSTAL DOUG DC9 DC915 3022036 WP BS 120-130 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 969Z 47001 INTERCOASTAL 28R RBL 14 IN AT STA 120 TO 130, REMOVED FOR CORROSION AND CRACK. MADE 9911549-2 FROM 7075-0 AND HEAT TRE ATED TO T6 CONDITION AND INSTALLED WITH HI-LOKS AND RIVETS. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091100492 19980911 00492 WP 1998 9 11 TWAA9814401 1 19980903 A 5312 BULKHEAD TEE DOUG DC9 DC951 3022051 WP BS 1147 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 409EA 47728 DURING CHECK-C, MAINT FOUND UPPER T-CAP AT STA 1147 DAMAGED WHEN LT T-CAP WAS REMOVED AT AFT PRESSURE BULKHEAD. SPLICE STRAP, CLIPS AND SHIMS INSTALLED PER ARA 15382. 2 L 7 2 4F RT A6WE 1998091100493 19980911 00493 NM 1998 9 11 AWXA9800198 1 19980828 A 5315 FLOORBEAM BOEING 737 737277 1384570 NM BS 986.5 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 189AW 22656 FLOORBEAM AT STATION 986.5 CORRODED BEYOND LIMITS [PREVIOUSLY REWORKED] FROM RBL 44 TO LBL 16. REMOVED DAMAGED SECTION OF UPPER T-CAP FABRICATED AND INSTALLED NEW T-CAP IAW ER 2-53-15-81. 2 L 7 2 4F RT A16WE 1998091100494 19980911 00494 NM 1998 9 11 AWXA9800199 1 19980826 A 3350 FUSE BOEING 737 7373Y0 1384671 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 329AW 23500 TESTED EMERGENCY EXIT LIGHTS IAW TASK CARD A1C33009, ROWS 20 THROUGH 23 LEFT SEAT MOUNTED LIGHTS DO NOT WORK. REPLACED POWER SUPPLY FUSE, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998091100495 19980911 00495 NM 1998 9 11 AWXA9800200 1 19980827 A 5330 SKIN BOEING 737 737277 1384570 NM BS 727 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 180AW 22647 SKIN CRACK LT FUSELAGE STA 727B STRINGER 16L VERIFIED WITH HFEC. PERFORMED REPAIR IAW SRM 53-30-3 USING BLIND FASTENERS . TRANSFERRED BLIND FASTENERS TO AWM-952 CONTROL NR 981720. REINSPECT FIRST 3000 CYCLES 2500 CYCLES THERE AFTER. TERM INATE AT NEXT C-CK. 2 L 7 2 4F RT A16WE 1998091100496 19980911 00496 WP 1998 9 11 CALA9801636 1 19980904 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1 INCH CRACK AT UPPER MOUNT HOLE OF FRAME AT STA 980, LONGERON 16R. THE CRACKED AREA WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1998091100497 19980911 00497 WP 1998 9 11 CALA9801637 1 19980908 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1920-2007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN STA 1920 AND 2007, RBL 55. THE FLOOR SUPPORT WAS REMOVED. A NEW PART W AS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998091100498 19980911 00498 WP 1998 9 11 CALA9801638 1 19980908 A 5320 SUPPORT DOUG DC10 DC1030 3023501 WP BS 1910 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 1910, LBL 25. THE FLOOR SUPPORT WAS REMOVED AND A NEW PART WAS IN STALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998091100499 19980911 00499 NM 1998 9 11 CALA9801639 1 19980908 A 5754 SKIN BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A 1 INCH CRACK IN NR 8 SLAT INNER SKIN AFT OF ACTUATOR CUTOUT. THE SLAT PANEL WAS REMOVED IAW SRM 51-3 0-2 AND THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091100500 19980911 00500 NM 1998 9 11 CALA9801640 1 19980908 A 5712 RIB BOEING 727 727224 1384076 NM RT WINGTIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 2.75 AND 1 INCH CRACK IN RIB INSIDE RT WINGTIP, ACCESSED THROUGH PANEL NR 8811. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. ANGLE REPAIRS WERE INSTALLED IAW SRM 51-40-3, FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 1998091100501 19980911 00501 NM 1998 9 11 CALA9801641 1 19980908 A 5753 RIB BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 1 INCH CRACK IN RT WING INBOARD MIDFLAP RIB OUTBOARD OF INBOARD CARRIAGE SPINDLE MOUNT. THE CRACK WA S STOP DRILLED IAW SRM 51-10-1. A DOUBLER REPAIR WAS INSTALLED IAW SRM 57-10-5, FIGURE 1. 2 L 7 3 4F A3WE 1998091100502 19980911 00502 NM 1998 9 11 CALA9801642 1 19980908 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND CORROSION IN RT ELEVATOR SKIN UNDER OUTBOARD CENTER STATIC WICK BASE. THE CORRODED AREA WAS CUT OUT, A DOUBLER AND FITTING WERE INSTALLED IAW SRM 55-20-3 FIGURE 2 PAGE 2. 2 L 7 3 4F A3WE 1998091100503 19980911 00503 NM 1998 9 11 CALA9801643 1 19980908 A 5753 651859933 CARRIAGE BOEING 727 727224 1384076 NM NR 5 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WING NR 5 FLAP CARRIAGE SPINDLE CORRODED AT FORWARD AREA. THE NR 5 FLAP CARRIAGE ASSEMBLY WAS REPLA CED IAW MM 57-50-00. 2 L 7 3 4F A3WE 1998091100504 19980911 00504 NM 1998 9 11 CALA9801644 1 19980908 A 5753 651920220 CARRIAGE BOEING 727 727224 1384076 NM NR 2 LE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND NR 2 FLAP CARRIAGE AFT SPINDLE BUSHING CORRODED. THE NR 2 FLAP CARRIAGE ASSEMBLY WAS REMOVED AND REPLA CED IAW MM 57-50-00. 2 L 7 3 4F A3WE 1998091100505 19980911 00505 WP 1998 9 11 CALA9801645 1 19980908 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 448-465 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND A GOUGE IN FUSELAGE SKIN AT STA 448-465, LONGERON 19L TO 20L. A REPAIR DOUBLER WAS INSTALLED IAW SRM 5 3-04, FIGURE 12B. 2 L 7 2 4F A6WE 1998091100506 19980911 00506 WP 1998 9 11 CALA9801646 1 19980908 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 465-489 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND FORWARD BAGGAGE BIN INTERNAL DOUBLERS CORRODED BETWEEN STA 465 AND 489, LONGERONS 24L TO 26L. A DOUBLE R WAS INSTALLED IAW SRM 53-04, FIGURE 12B, PAGE 35. 2 L 7 2 4F A6WE 1998091100507 19980911 00507 NM 1998 9 11 CALA9801647 1 19980908 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBOARD SUPPORT ANGLE IN AFT PIT CORRODED AT STA 1166, LT SIDE. THE CORRODED AREA OF FLOORBOARD SUP PORT ANGLE WAS REMOVED AND REPAIR PARTS WERE INSTALLED IAW SRM 53-10-5, FIGURE 6, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100508 19980911 00508 NM 1998 9 11 CALA9801648 1 19980908 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 535 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FORWARD PIT FLOOR SUPPORT ANGLE CORRODED AT STA 535, RBL 20. THE CORROSION WAS REMOVED AND A REPAIR WA S INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100509 19980911 00509 NM 1998 9 11 CALA9801649 1 19980908 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBEAM CORRODED AT STA 360, RBL 24.75. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR W AS INSTALLED IAW SRM 53-10-08 AND 51-30-02. 2 L 7 3 4F A3WE 1998091100510 19980911 00510 NM 1998 9 11 CALA9801650 1 19980908 A 5530 STRAP BOEING 727 727232 1384082 NM VERT STAB BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT VERTICAL STABILIZER SPAR ATTACH STRAP BROKEN IN HALF AT STA 1213. A DOUBLER AND FILLER WERE INSTALL ED IAW SRM 51-40-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100511 19980911 00511 NM 1998 9 11 CALA9801651 1 19980908 A 5530 BRACKET BOEING 727 727232 1384082 NM BS 1218 & 1228 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CRACKED BRACKETS AT LT LOWER VERTICAL STABILIZER FRONT SPAR FITTING AT FS 1218 AND STA 1228. THE CRACK S WERE 1.5 AND 1 INCH LONG. ANGLES WERE INSTALLED AT BOTH LOCATIONS IAW SRM 51-40-3, FIGURE 1 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091100512 19980911 00512 NM 1998 9 11 CALA9801652 1 19980908 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND L-ANGLE ON TOP OF DOGHOUSE CORRODED AT STA 294.5, LBL 12. THE L-ANGLE WAS REMOVED IAW SRM 51-30-2. A NEW L-ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091100513 19980911 00513 WP 1998 9 11 CALA9801653 1 19980908 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND 1 INCH CRACKS AT CLIP NUT HOLES IN FLOOR PANEL NR 47 FORWAD OF STA 756. A NEW FLOOR PANEL WAS INSTALLE D IAW SRM 53-21, 51-30-2, AND 53-05, FIGURE 1. 2 L 7 2 4F A6WE 1998091100514 19980911 00514 WP 1998 9 11 CALA9801654 1 19980908 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 945 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND TWO 1 INCH CRACKS IN DOUBLER AT STA 945, LONGERON 14R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS I NSTALLED IAW SRM 53-03, FIGURE 28. 2 L 7 2 4F A6WE 1998091100515 19980911 00515 NM 1998 9 11 CALA9801655 1 19980909 A 5712 RIB BOEING 727 727224 1384076 NM LT WING TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 1.5 INCH CRACK IN LT WING TIP RIB UPPER FLANGE BY INBOARD AFT CORNER OF FUEL VENT OUTLET. THE CRACK WAS STOP DRILLED IAW SRM 51-30-2. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, FIGURE 1. 2 L 7 3 4F A3WE 1998091100516 19980911 00516 NM 1998 9 11 CALA9801656 1 19980909 A 5320 SUPPORT BOEING 727 727224 1384076 NM LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FORWARD LAV INBOARD WALL FLOOR SUPPORT CORRODED. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-1, PAGE 4. 2 L 7 3 4F A3WE 1998091100517 19980911 00517 NM 1998 9 11 CALA9801657 1 19980909 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND CORROSION IN RT ELEVATOR SKIN UNDER OUTBOARD MOST STATIC WICK BASE. THE CORRODED AREA WAS CUT OUT. A NEW DOUBLER AND FITTING WERE INSTALLED IAW SRM 55-20-3, FIGURE 2, PAGE 2. 2 L 7 3 4F A3WE 1998091100518 19980911 00518 NM 1998 9 11 CALA9801658 1 19980909 A 5753 TRACK BOEING 727 727224 1384076 NM NR 7 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WING NR 7 FLAP TRACK ROLLER SURFACES CORRODED. THE FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-40-00. 2 L 7 3 4F A3WE 1998091100519 19980911 00519 WP 1998 9 11 CALA9801659 1 19980908 A 5510 FAIRING DOUG DC9 DC932 3022066 WP RT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 4.5 INCH CRACK IN LOWER AFT END OF RT HORIZONTAL STABILIZER LOWER FAIRING. THE CRACK WAS STOP DRILLE D. A DOUBLER WAS INSTALLED IAW SRM 55-11-0 FIGURE 7, 55-01, FIGURE 2, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998091100520 19980911 00520 NM 1998 9 11 UPS98227651 1 19980909 A 3350 S106 BATTERY BOEING 727 72725C 138400H NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 932UP 19856 INSPECTION TYPE-N/A, EMERGENCY LIGHTS GO DIM. REPLACED DRAINED BATTERIES. 2 L 7 3 4F A3WE 1998091100521 19980911 00521 NM 1998 9 11 UPS98527650 1 19980908 A 3350 20131A BATTERY BOEING 757 75724APF 1384969 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 418UP 23905 INSPECTION TYPE P-DP FORWARD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY. 2 L 7 2 4F RT A2NM 1998091100522 19980911 00522 1998 9 11 UPS98827592 2 19980901 A 7321 MEC DOUG DC8 DC871F 302199D WP NR 3 ENGINE FAILED A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 707UP 45907 INSPECTION TYPE-N/A, NR 3 ENG FLAMED OUT IN CRUISE FLT AT FL 350 ON ATTEMPTED RE-IGT, EGT CLIMBED RAPIDLY TO 900 DEG, SH UT DOWN ENG. FOB AT TIME WAS 50.0 WITH 12,750 LBS IN NR 3 MAIN NORMAL CONFIG. REPLACED NR 3 ENG MEC PER MM-73-20-01, T /C 1037/1038 SYSTEM LEAK AND OPS CHK OK. (P/N 8063-211) OFF, (P/N 8063-212) ON, (S/N WYG34934) OFF, (S/N WYG35140) ON. 2 L 7 4 4F RT 4A25 1998091100523 19980911 00523 WP 1998 9 11 UPS98827638 1 19980817 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, FRAME AT FS 870 LOWER LT SKIN PANEL HAS CORROSION AT RB ATTACHMENT. REMOVED DAMAGED SECTION OF FR AME, FORMED FRAME AND SPLICE IAW REO 0530 1 AND DC8 SRM 51-1-4. HEAT TREATED FRAME AND SPLICE, REMOVED INTERCOSTAL TO A LLOW ACCESS. FAB FRAME AND SPLICE IAW REO 05301. REINSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D. FAB -59 ANGLE IAW REO 05301. ALODINED AND PRIMED IAW 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998091100524 19980911 00524 WP 1998 9 11 UPS98827640 1 19980807 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 857 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, LT MLG WHEEL WELL, STA 857 ANGLE ABOVE REAR SPAR HAS CORROSION ON FWD SIP AT JUST O/B OF I/B PRESS URE PANEL 48 IN LT OF C/L. REMOVED CORROSION WAS OUT OF LIMITS. REMOVED AND REPLACED ANGLE IAW DC8 SRM 51-1-8/ 51-1-20 D/ 53-2-0. 2 L 7 4 4F RT 4A25 1998091100525 19980911 00525 WP 1998 9 11 UPS98827641 1 19980807 A 5320 BRACKET DOUG DC8 DC873F 302199F WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, LT MLG WHEEL WELL STA 857 ABOVE REAR SPAR, CORNER BRACKET HAS A VISIBLE CRACK THROUGH RADIUS AND F ASTENER HOLES O/B SIDE OF I/B PRESSURE PANEL. REMOVED AND REPLACED BRACKET IAW DC8 SRM 51-1-24 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998091100526 19980911 00526 WP 1998 9 11 UPS98827642 1 19980806 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK JUST I/B OF XRS 74 STRINGER 51 AFT SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING IAW DC8 SRM 51-1-20D. FABBED FITTING IAW DAC CWG 3724841. 2 L 7 4 4F RT 4A25 1998091100527 19980911 00527 WP 1998 9 11 UPS98827643 1 19980806 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK O/B OF XRS 74 STRINGER 51 AFT SPLICE FITTING IS CRACKED. REMOVED CRACKED F ITTING HAD NEW ONE FABRICATED IAW DAC DWG 3724841 AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-1-23. 2 L 7 4 4F RT 4A25 1998091100528 19980911 00528 WP 1998 9 11 UPS98827644 1 19980806 A 5720 FITTING DOUG DC8 DC873F 302199F WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, INSIDE NR 3 MAIN TANK O/B OF XRS 74 STINGER 51 THE FWD SPLICE FITTING IS CRACKED. REMOVED CRACKED FITTING, FABRICATED NEW FITTING IAW DAC DWG 3704841. INSTALLED FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-1-23. 2 L 7 4 4F RT 4A25 1998091100529 19980911 00529 WP 1998 9 11 UPS98827645 1 19980806 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 320 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, STA 320 F/L/C AFT DOOR STOP FITTING CRACKED L29L AND RUBBER BUMPER MISSING. REMOVED CRACKED FITTI NG, LOCATED AND DRILLED NEW FITTING IAW 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100530 19980911 00530 WP 1998 9 11 UPS98827646 1 19980805 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1400-1580 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, SEAT TRACK G HAS CORROSION AT STA 1400 TO 1580. REMOVED DAMAGED SEAT TRACK MATERIAL ID FOR NEW SE AT TRACK 2772660 EXTRUSION 7075T6 PO 158781. FAB AND DRILLED UP NEW SEAT TRACK AND SPLICE FITTING DC8 53B003-501 TAG 44 7216 IAW DC8 SRM 53-2-3. ALODINED IAW DC8 SRM 51-1-8. PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998091100531 19980911 00531 WP 1998 9 11 UPS98827647 1 19980805 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 50-260 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 50 TO 260 SEAT TRACK A HAS CORROSION. REMOVED CORROSION IAW 1-1-8. NOT WITHIN LIM ITS IAW DC8 SRM 53-2-3. DRILLED NEW SECTION OF SEAT TRACK IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SECTION OF TRACK IAW DC8 SRM 51-3-0 AND 53-2-3. 2 L 7 4 4F RT 4A25 1998091100532 19980911 00532 WP 1998 9 11 UPS98827648 1 19980805 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 50-120 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, MAIN CABIN STA 50 TO 120 SEAT TRACK B CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS I AW DC8 SRM 53-2-3. REPLACED SEAT TRACK ON NR 840844. 2 L 7 4 4F RT 4A25 1998091100533 19980911 00533 WP 1998 9 11 UPS98827649 1 19980804 A 5313 5750198501 LONGERON DOUG DC8 DC873F 302199F WP BS 862 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE C-CK, LT WHEEL WELL LONGERON 24 CRACKED APPROX 2 INCHES AT STA 862. REMOVED AND REPLACED LONGERON 24 IA W TIMCO WORK CARD 90453100. 2 L 7 4 4F RT 4A25 1998091100534 19980911 00534 WP 1998 9 11 UPS98827652 1 19980908 A 3397 WIRE DOUG DC8 DC871F 302199D WP CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-N/A, EMERGENCY LIGHTS DISARM CHECK LIGHT INOP. TIGHTENED LOOSE WIRE ON EMERGENCY DISARM LIGHT SOCKET, O P'S CK GOOD. LIGHT ON WITH SWTICH IN DISARM POS. 2 L 7 4 4F RT 4A25 1998091100535 19980911 00535 NM 1998 9 11 QXEA9801270 1 19980904 A 3350 6038443 POWER SUPPLY DHAV 82410162007 DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 354PH 498 DURING LINE CHECK, FOUND THE FORWARD CABIN CEILING EMERGENCY LIGHTS ARE INOP AND THE LEFT AFT EMERGENCY LIGHTS INOP. RE PLACED THE PS3 BATTERY POWER SUPPLY. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998091100536 19980911 00536 NE 1998 9 11 QXEA9801271 2 19980907 A 7421 CH34487A IGNITOR PLUG DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MALFUNCTION A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 830PH 314 NR 2 ENGINE WOULD NOT START. FUEL SMELL NOTED INSIDE CABIN. REPLACED ENGINE IGNITORS. ENGINE OPERATES AND STARTS NORM ALLY. NO FURTHER SMELL NOTED IN THE CABIN. 2 H 7 2 4T 4 T RT A13NM E20NE 1998091100537 19980911 00537 NM 1998 9 11 QXEA9801272 1 19980907 A 3320 82521446005 LIGHT DHAV DHC8 DHC8102 2809003 NM CABIN MALFUNCTION A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 828PH 287 ELECTRIC SMELL NOTED IN THE CABIN. INSPECTED AND FOUND TO BE CAUSED BY THE CABIN OVERHEAD LIGHTS. DEACTIVATED THE OVER HEAD LIGHTS AND PLACED ON MEL. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED BY REPLACING THE FORWARD LAMP HOLDER AT ROW 7 DE. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998091100538 19980911 00538 NM 1998 9 11 QXEA9801273 1 19980904 A 3350 MS25231316 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 825PH 213 ROW 5 CENTER EMERGENCY LIGHT INOP. RELAMPED OVERHEAD LIGHT. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998091100539 19980911 00539 NM 1998 9 11 98FDEA00547 1 19980909 A 3246 WHEEL BOEING 727 727247 138408F NM NR 1 MISSING A FDEA K NONE D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 234FE 21328 ON WALKAROUND, FOUND NR 1 TIRE MISSING FROM AXLE. *S/D* PERFORM VISUAL INSPECT OF LEFT MAIN GEAR, NO DEFECT NOTED. RE PLACED LEFT O/B AXLE SLEEVE ASSY PER BOEING OVERHAUL MAN 32-12-01. PER HARD LAND INSP PHASE 1 PER M/M 51-51-61. REMOVE D AND REPLACED NR 1 TIRE AND WHEEL ASSY PER M/M 32-45-01. 2 L 7 3 4F A3WE 1998091100540 19980911 00540 NM 1998 9 11 98FDEA00548 1 19980909 A 2761 65C163002 ACTUATOR BOEING 727 727233 138408A NM NR 14 SPOILER LEAKING A FDEA O OTHER K J FLUID LOSS WARNING INDICATION UK UNKNOWN 1 SO 25 223FE 20935 SYS-A HYD QUANTITY WENT TO 0. EXEC RED TABS LANDING UNEVENTFUL. FOUND NR 14 SPLR ACTUATOR LEAK. REMOVED AND REPLACED NR 14 SPLR ACTUATOR PER M/M 27-61-81 PG 501. SERVICED A-SYS RESERVOIR TO FULL PROGRESS REPORT COMPLETED. 2 L 7 3 4F RT A3WE 1998091100541 19980911 00541 NM 1998 9 11 98FDEA00549 1 19980826 A 5330 SKIN BOEING 727 72722 1384002 NM BS 360 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 LOW FREQ EDDY CURRENT IND 15 PERCENT MATERIAL LOSS BS 360 AFT FASTENER ROW STR 4 RT BOTTOM OF SKIN LAP TO ONE INCH BELOW . REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 5. 2 L 7 3 4F A3WE 1998091100542 19980911 00542 NM 1998 9 11 98FDEA00550 1 19980818 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 UPPER LOBE BS 380 HEAVY CORROSION ON FLOORBEAM AT LBL 34. REMOVED CORROSION PER SRM 51-10-6. CORROSION REMOVAL OUT OF LIMITS. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1 AND 2 FIG 3. 2 L 7 3 4F A3WE 1998091100543 19980911 00543 NE 1998 9 11 98UAL900410 2 19980828 A 7530 HPC VANE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE OUT OF ADJUST A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 556UA 19570 6891 26650 726600 RIGHT ENGINE FUEL FLOW AND EPR GAUGES STARTED SURGING PASSING THROUGH FL330 ON CLIMB. CREW ALSO FELT RIGHT ENGINE SURGI NG. FLIGHT DECENDED TO FL250 AND ENGINE RETURNED TO NORMAL INDICATIONS. FLIGHT RETURNED TO SFO WITH EQUIPMENT STANDING BY. *S/D* ENGINE WAS REPLACED DUE TO SURGING. DURING REPAIR AS ORDER NUMBER D345, IT WAS REPAIRED PER SFOEP FIX LETT ER. ACCOMPLISHMENT WAS TO CHECK VSV AND 2.5 SYSTEMS. REMOVED THE FUEL CONTROL AND THE 14 STG CONVERTER VALVE. INVESTI GATIVE FINDINGS FOUND 6TH STG HPC VANES OUT OF RIG / SCHEDULE. THE 2.5 BLEED OUT OF RIG OPEN, AND THE BLEED RING AFT SE AL WORN AND LEAKING DUE TO AIR EROSION FROM BEING MISRIGGED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998091100544 19980911 00544 NM 1998 9 11 98UAL900412 1 19980828 A 5270 693735230 ANNUNCIATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE 1L DOOR FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 305UA 23666 DOOR 1L LIGHT ILLUMINATED. *S/D* REPLACED DOOR WARNING ANNUCIATOR MODULE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100545 19980911 00545 NM 1998 9 11 98UAL900413 1 19980829 A 5270 WARNING LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE CARGO DOOR ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 907UA 25007 FORWARD CARGO WARNING LIGHT ILLUMINATED. *S/D* ADJUSTED TARGET. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100546 19980911 00546 NM 1998 9 11 98UAL900414 1 19980830 A 2913 PACKING BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 1 HYD PUMP FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 WP 29 374UA 24639 NR 1 ENGINE HYDRAULIC PUMP WARNING LIGHT ILLUMINATED. *S/D* REPLACED PACKING FOR A ELECTRIC PUMP ACOUSTIC FILTER REF I PC 29-15-22-001. OPS AND LEAK CK NORMAL. A-SYS SERVICED TO FULL. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100547 19980911 00547 NE 1998 9 11 98UAL900415 2 19980829 A 7200 51D411 DATA PLUG BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT ENGINE MISINSTALLED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 654UA 20 25392 727802 REJECTED TAKEOFF AT 85 KTS, LEFT ENGINE DEVELOPED 1.49 EPR WITH 1.6 SELECTED. *S/D* INCORRECT EEC DATA ENTRY PLUG INST ALLED. REPROGRAMED PLUG TO PROPER CONFIGURATION. CHANGED SHOP MAINTENANCE AND LINE MAINTENANCE DOCUMENTS TO PREVENT RE OCCURENCE. 2 L 7 2 4F 4 F RT A1NM E24NE 1998091100548 19980911 00548 NM 1998 9 11 98UAL900416 1 19980829 A 2612 896768 FIRE DETECTOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 336UA 24240 APU FIRE WARNING INDICATION IN FLIGHT. *S/D* REPLACED APU EXHAUST FIRE SENSING ELEMENT AND OVERHEAT SENSOR AND HARNESS PER MM 26-15-14. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100549 19980911 00549 GL 1998 9 11 98UAL900417 2 19980830 A 7230 COMPRESSOR DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NR 3 ENGINE FAILED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 1844U 48260 451468 CAPT ADVISED AT 80KT EXPERIENCED LOUD EXPLOSION WITH MINOR AIRCRAFT SWERVE AND NR 3 EGT EXCEEDING MAX TEMP. CAPT ABORTE D TAKEOFF AT 90KT WITH NO FURTHER PROBLEMS AND TAXIIED TO THE GATE. BORESCOPE INDICATES FAILURE INITIATED AT STAGE 7 HP C BLADE. REPLACED ENGINE. 2 L 7 3 4F 4 F A22WE E23EA 1998091100550 19980911 00550 NM 1998 9 11 98UAL900420 1 19980830 A 2822 BOOST PUMP PLESSLEY 10620493 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 ENGINE MALFUNCTIONED A UALA K NONE X ENGINE FLAMEOUT AP APPROACH 1 WP 29 917UA 4601A 25384 NR 1 ENGINE FLAME-OUT. ENGINE RESTARTED PRIOR TO LANDING. *S/D* REPLACED NUMBER ONE MAIN TANK FORWARD AND AFT BOOST P UMP. REPLACED FUEL SHUT OFF VALVE AND GATE ASSEMBLY. REPLACED FUEL FILTERS. ACCOMPLISHED FUEL FEED SYSTEM TEST. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100551 19980911 00551 NM 1998 9 11 98UAL900421 1 19980831 A 5270 SENSOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE CARGO DOOR OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 352UA 24320 CARGO DOOR WARNING LIGHT ILLUMINATED. *S/D* ADJUSTED SENSOR TARGET. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100552 19980911 00552 NE 1998 9 11 98UAL900422 2 19980830 A 7230 730786 BEARING BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE FAN CASE WORN A UALA K NONE O OTHER CR CRUISE 1 WP 29 612UA 21873 707527 NR 1 ENGINE EXPERIENCED MULTIPLE STALLS WHILE IN STEADY STATE CONDITION AT CRUISE POWER SETTING IN TURBULENCE AT 39,000 FEET WITH AUTO THROTTLES DISCONNECTED. *S/D* ACCOMPLISHED CHECKS PER MM 71-00-39. FOUND 3.0 BLEED OPERATION WAS ERRA TIC AND COULD NOT BE TRIMMED TO WITHIN OPERATIONAL LIMITS. THE ENGINE WAS REMOVED AND ROUTED TO THE SHOP. IN THE SHOP, A WORN 3.0 BLEED ROD BEARING IN THE FAN CASE WAS FOUND AND REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998091100553 19980911 00553 NM 1998 9 11 98UAL900423 1 19980829 A 3350 BULB BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 176UA 24383 OVERHEAD EMERGENCY LIGHT INOP AT SEAT 33CD AISLE LIGHT. REPLACED 1317 LAMP IN LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F 4 F RT A20WE E24NE 1998091100554 19980911 00554 1998 9 11 98UAL900425 4 19980805 A 2564 TUBE AIR CRUISERS 62772202 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SLIDE/RAFT TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 772UA 0021 26930 DURING FLAT FIRING OF SLIDE RAFT (P/N 62772-202) (S/N 0021) IN CONJUNCTION WITH SHOP OVERHAUL VISIT, A ONE INCH TEAR DEV ELOPED IN THE LOWER TUBE UNDER THE GIRT. UNIT SENT TO VENDOR FOR REPAIR AND EVALUATION. *S/D* AFTER REVIEW BY VENDOR, CAUSE OF FAILURE COULD NOT BE PRECISELY DETERMINED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998091100555 19980911 00555 NM 1998 9 11 98UAL900426 1 19980902 A 2120 FLOW SENSOR ROSEMOUNT 123CH1A BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE E/E COMPT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 312UA 23673 EQUIPMENT COOLING FANS FAILED. *S/D* THE LOW FLOW SENSOR FAILED IN BOTH NORMAL AND ALTERNATE MODES. THE LOW FLOW SENS OR WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100556 19980911 00556 NE 1998 9 11 98UAL900427 2 19980902 A 7530 IVG ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE LOOSE A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 379UA 24654 722420 N2 OVERSPEED ON NUMBER TWO ENGINE. *S/D* REPLACED ENGINE. FOUND LEFT INLET GUIDE VANE BOLT/NUT ATTACHING INLET GUIDE VANE ACTUATION RING TO BELLCRANK ASSEMBLY ROD-END MISSING. NUT: J149P10BOLT: 99970M42P02. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100557 19980911 00557 NM 1998 9 11 98UAL900428 1 19980819 A 2133 10614501 SEAL BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE OUTFLOW VLV MISSING A UALA O OTHER O OTHER CR CRUISE 1 WP 29 7443U 21897 UNABLE TO MAINTAIN CABIN PRESSURE IN EITHER AUTO, STANDBY, OR MANUAL. DESCENDED TO 10,000 FEET AND PROCEEDED TO CLE. * S/D* MAINTENANCE FOUND OUTFLOW VALVE SEAL MISSING. ALSO, FOUND THE SEAL ON DOOR 1 RIGHT OUT OF TRACK. REPOSITIONED SE AL ON DOOR TRACK AND INSTALLED SEAL ON OUTFLOW VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998091100558 19980911 00558 NM 1998 9 11 98UAL900429 1 19980901 A 3610 VALVE AIRESEARCH 39271611 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 BLEED FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7285U 21563 NR 3 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER TAKEOFF. RETURNED TO BOI. *S/D* HISTORY OF HIGH PRESSURE AND OVERHEAT LIGHT INDICATION. MAINTENANCE REPLACED THE HI STAGE MODULATING VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998091100559 19980911 00559 NE 1998 9 11 98UAL900430 2 19980829 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 MALFUNCTIONED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 7945U 21899 NR 2 ENGINE OIL QUANTITY INDICATOR DROPPED TO ZERO. AFTER A FEW MINUTES A TEMPERATURE RISE WAS OBSERVED AND A PRECAUTIO NARY SHUT DOWN WAS PERFORMED. DIVERTED TO PDX WHERE MAINTENANCE WAS AVAILABLE. 2 L 7 3 4F 4 F A3WE E2EA 1998091100560 19980911 00560 NM 1998 9 11 98UAL900431 1 19980828 A 2910 65178494061 LINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE B-HYD SYST LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 7295U 21573 DIVERTED TO JFK WHEN THE HYDRAULIC SYSTEM-B FAILED. *S/D* REMOVED AND REPLACED LEAKING HYD SYSTEM-B LINE AND FILTERS. LEAK CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1998091100561 19980911 00561 NM 1998 9 11 98UAL900432 1 19980830 A 7930 BYPASS LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT ENGINE ILLUMINATED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7466U 21920 THE RIGHT OIL BYPASS LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO SEA. 2 L 7 3 4F 4 F A3WE E2EA 1998091100562 19980911 00562 NM 1998 9 11 98UAL900433 1 19980829 A 3350 6005401LB POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7456U 21910 BOTH LEFT WING EMERGENCY EXIT LIGHTS STAY ON WITH SWITCH OFF. *S/D* REPLACED POWER SUPPLY, CHECKS GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1998091100563 19980911 00563 NM 1998 9 11 98UAL900434 1 19980830 A 3350 1060091102 POWER SUPPLY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7281U 21559 AFT EMERGENCY EXIT SIGN ABOVE CEILING INOPERATIVE. *S/D* REPLACED POWER SUPPLY, OPS CHECK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998091100564 19980911 00564 NM 1998 9 11 98UAL900435 1 19980828 A 5270 1EN1S SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CARGO DOOR OUT OF ADJUST A UALA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING CL CLIMB 1 WP 29 7466U 21920 FORWARD CARGO DOOR LIGHT CAME ON AFTER TAKEOFF. RETURNED TO EWR. *S/D* FORWARD CARGO DOOR OPEN LIGHT SWITCH WAS FOUND TO BE OUT OF ADJUSTEMNT. THE SWITCH WAS ADJUSTED, AN OPERATIONAL CHECK WAS PERFORMED ON THE CARGO DOOR AND SWITCH TO C ONFIRM PROPER OPERATION. 2 L 7 3 4F 4 F A3WE E2EA 1998091100565 19980911 00565 NE 1998 9 11 98UAL900436 2 19980903 A 7530 99970M42P02 IGV ACTUATOR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE LOOSE A UALA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 29 379UA 24654 NR 2 ENGINE NOT GENERATING ENOUGH POWER. *S/D* REPLACED ENGINE. FOUND LEFT INLET GUIDE VANE BOLT/NUT ATTACHING INLET GUIDE VANE ACTUATION RING TO BELLCRANK ASSEMBLY ROD-END MISSING. NUT: J149P10BOLT: 99970M42P02. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091100566 19980911 00566 WP 1998 9 11 ABXA900811 1 19980908 A 5311 995821519 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 917 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING C-CHECK, FOUND CORROSION ON FRAME 917 AT LONGERON 29L-LONGERON 29R. REPAIRED IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998091100567 19980911 00567 WP 1998 9 11 ABXA9800812 1 19980908 A 5313 591140615N LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING C-CHECK, FOUND LONGERON 4 LEFT AT FS 160 CRACKED. REPLACED NEW SECTION OF LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998091100568 19980911 00568 WP 1998 9 11 ABXA9800813 1 19980908 A 5320 99105035 WEB DOUG DOUG DC9 DC931 3022065 WP BS 945 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING C-CHECK, FOUND CUSP WEB CORRODED FS 945, LBL 50-54. REPLACED SECTION OF LEFT CUSP WEB 945L IAW ABX REA 953 24 70 2 MR. 2 L 7 2 4F A6WE 1998091100569 19980911 00569 WP 1998 9 11 ABXA9800814 1 19980908 A 5330 591970731 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 756-760 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING C-CHECK, FOUND CORROSION ON LONGERON 30 AND ADJACENT FUSELAGE SKIN LONGERON 29R TO LONGERON 30R, FS 756-760. REP AIRED FUSELAGE SKIN IAW ABX REA D953 24724. 2 L 7 2 4F A6WE 1998091100570 19980911 00570 WP 1998 9 11 ABXA9800815 1 19980908 A 5330 591142551 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 946-950 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING C-CHECK, FOUND FUSELAGE SKIN CORRODED FS 946-950 LONGERON 27R - LONGERON 29R. REPLACED DOUBLERS FS 945-980 LONGE RON 27R TO LONGERON 29R, IAW DC9 MM 51-30-2. 2 L 7 2 4F A6WE 1998091100571 19980911 00571 WP 1998 9 11 ABXA9800816 1 19980908 A 5311 99196181 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING C-CHECK, FOUND LEFT MAIN FRAME FS 718 CRACKED. REPAIRED LEFT FUSELAGE MAIN FRAME FS 718 IAW ABX REA D953- 24732- SB. 2 L 7 2 4F A6WE 1998091100572 19980911 00572 WP 1998 9 11 ABXA9800817 1 19980908 A 5313 59114279 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 949AX 47325 DURING C-CHECK, FOUND LONGERON 17L CRACKED FS 965. REPLACED SECTION OF LONGERON 17L FS 965 IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998091100573 19980911 00573 NM 1998 9 11 DL73E981806 1 19980901 A 2761 654496116 ACTUATOR BOEING 737 7372J8 1384489 NM NR 8 SPOILER BROKEN A DALA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 235WA 22859 ON TAXI IN, A-SYS HYD WENT TO ONE GALLON. REPLACED NR 8 SPOILER ACTUATOR. 2 L 7 2 4F RT A16WE 1998091100574 19980911 00574 NM 1998 9 11 DLM88981808 1 19980901 A 3350 61020 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 911DL 49542 JUMPSEAT 1L FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED FLAHSLIGHT BATTERY AND BULB. 2 L 7 2 4F RT A6WE 1998091100575 19980911 00575 NM 1998 9 11 DL72S981809 1 19980823 A 7110 COWL BOEING 727 727232 1384082 NM NR 2 PYLON WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FOUND AT HMV, STA 1352 FWD COWLING RING WORN THROUGH AT 6 O'CLOCK POSITION. ROUTED OUT DAMAGE MANFCT BDLER PER MM 53-11 -0 PG 801 AND INSTALLED PER SRM 53-11-0 PG 801. 2 L 7 3 4F A3WE 1998091100576 19980911 00576 NM 1998 9 11 DL72S981810 1 19980901 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FOUND ON B2 LETTER CK, HORIZONTAL TORQUE BOX ANGLE CRACKED RT STA 1273. REPLACED ANGLE PER SRM 53-10-10. 2 L 7 3 4F A3WE 1998091100577 19980911 00577 NM 1998 9 11 DL72S981811 1 19980901 A 5320 WEB BOEING 727 727232 1384082 NM BS 1303 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FOUND ON D2 LETTER CK, 2 EA .5 INCH CRACKS STA 1303 VERT WEB ABOVE S-DUCT RT SIDE. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1998091100578 19980911 00578 NM 1998 9 11 DL72S981812 1 19980901 A 5320 WEB BOEING 727 727232 1384082 NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FOUND ON D2 LETTER CK, RT VERTICAL TORQUE BOX WEB CRACKED .1562 INCH AT LIGHTENING HOLE STA 1243 RT. ROUTED OUT DAMAGED AREA PER MM 53-11-0. 2 L 7 3 4F A3WE 1998091100579 19980911 00579 NM 1998 9 11 DL72S981813 1 19980901 A 5755 651734781A PANEL BOEING 727 727232 1384082 NM NR 2 SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 535DA 22048 FOUND AREA OF DELAMINATION ON NR 2 SPOILER UPPER SURFACE. REPAIRED PER SRM 57-50-6. 2 L 7 3 4F A3WE 1998091100580 19980911 00580 NM 1998 9 11 DL73E981814 1 19980902 A 5754 69598892 HINGE BOEING 737 737247 138448D NM RT LE FLAP FAILED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 373DL 23520 RT I/B LEADING EDGE FLAP SKIN BENT/CRACKED AT UPPER I/B EDGE DUE TO FAILURE OF I/B HINGE. 2 L 7 2 4F A16WE 1998091100582 19980911 00582 NM 1998 9 11 DLM88981818 1 19980903 A 2120 AIR DISTRIBUTION DOUG MD88 MD88 3023688 NM CABIN SMOKE A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 978DL 53259 APPROX ONE TO TWO MINUTES AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED SMOKE IN CABIN. BOTH SMOKE DETECTORS IN REAR OF AIR CRAFT ACTIVATED. CHECKED APU INLET FOUND CLEAR. PERFORMED DUCT BURNOUT PER M/M 36-10-00-5. NO SMOKE IN CABIN ON RUN-U P. OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1998091100583 19980911 00583 NM 1998 9 11 DL72S981821 1 19980903 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 910 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 469DA 20746 REF SHIP 469 TPA LETTER CHK E-2, VERTICAL ANGLE CRACKED RT WHEEL WELL STA 910. REPAIRED PER M/M 53-11-0. 2 L 7 3 4F A3WE 1998091100584 19980911 00584 WP 1998 9 11 DLL14981827 1 19980901 A 5712 1527807102 BULKHEAD FITTING LKHEED 1011 1011385115 5265015 WP WS 503 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 741DA 193C1245 THE RT WING PYLON BACKUP FITTING BULKHEAD WAS FOUND CRACKED. A DOUBLER REPAIR IS INSTALLED. 2 L 7 3 4F A23WE 1998091100585 19980911 00585 WP 1998 9 11 DLL14981828 1 19980903 A 5712 1527032 RIB LKHEED 1011 1011385115 5265015 WP RT & LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 741DA 193C1245 THE RT WING IWS 503 RIB UPPER CAP, LT WING IWS 555 RIB UPPER CAP WERE BOTH FOUND CRACKED. ALL CRACKED PARTS WERE REPLAC ED. 2 L 7 3 4F A23WE 1998091100586 19980911 00586 WP 1998 9 11 DLL14981829 1 19980903 A 5320 1542396 DECK LKHEED 1011 1011385115 5265015 WP BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 741DA 193C1245 THE FUSELAGE HORIZONTAL PRESSURE DECK WAS FOUND CRACKED AT RBL 102 AND FS 380. A DOUBLER/TRIPLER REPAIR WAS ACCOMPLISHE D. 2 L 7 3 4F A23WE 1998091100587 19980911 00587 WP 1998 9 11 DLL14981830 1 19980903 A 5320 1542396 DECK LKHEED 1011 1011385115 5265015 WP BS 395-437 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 741DA 193C1245 THE NOSE LANDING GEAR PRESSURE DECK WAS FOUND CRACKED IN SIX LOCATIONS AT LBL 24 AND RBL 24 BETWEEN STA 395 AND 437. DO UBLER/TRIPLER REPAIRS ARE INSTALLED. 2 L 7 3 4F A23WE 1998091100588 19980911 00588 WP 1998 9 11 DLL14981832 1 19980903 A 5320 1516901101 FRAME LKHEED 1011 1011385115 5265015 WP GALLEY DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 741DA 193C1245 THE FWD GALLEY DOORWAY FRAME WAS CORRODED NEAR THE LOWER SILL AT STR 25. THE DAMAGE WAS REMOVED AND A REPAIR SECTION SP LICED IN. 2 L 7 3 4F A23WE 1998091100589 19980911 00589 NM 1998 9 11 DL76S981833 1 19980903 A 5330 146T32621 SKIN BOEING 767 767332 1382001 NM BS 1197-1221 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 135DL 25145 A CRACK WAS FOUND IN THE FUSELAGE SKIN NEAR AN EXISTING REPAIR. A SECTION OF SKIN PANEL IN THIS REGION WAS REMOVED AND A NEW ONE SPLICED IN BETWEEN STA 1197+77 AND 1197+124 AND BETWEEN STR 36L AND 36R. 2 L 7 2 4F RT A1NM 1998091100590 19980911 00590 NM 1998 9 11 DL73E981834 1 19980902 A 5330 6545768295 SKIN BOEING 737 737247 138448D NM CARGO DOORWAY WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 DURING INSPECTION OF CARGO DOOR CUTOUT, FUSELAGE SKIN DAMAGE WAS FOUND TO THE C1 DOOR CUTOUT AFT EDGE SKIN BETWEEN STRIN GERS 22-23R. THE DAMAGE WAS REPAIRED BY ER/A 332205-14. 2 L 7 2 4F A16WE 1998091100591 19980911 00591 NM 1998 9 11 DL73E981835 1 19980902 A 5330 6545768295 SKIN BOEING 737 737247 138448D NM CARGO DOORWAY WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 THE FUSELAGE SKIN AND BEAR STRAP WAS FOUND WITH WEAR ON THE C1 DOOR CUTOUT FORWARD EDGE JUST ABOVE STRINGER 22R. THE DA MAGE WAS REPAIRED BY ER/A 332204-14. 2 L 7 2 4F A16WE 1998091100592 19980911 00592 NM 1998 9 11 DLM88981836 1 19980904 A 3510 REGULATORS MXP1461 DOUG MD88 MD88 3023688 NM FLT DECK OXYGEN LEAKING A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 927DA 10709 49714 CREW OXYGEN WENT TO ZERO IN FLIGHT. REPLACED CAPT AND OBSV O2 REG BOXES FOR LEAKING REGULATOR. 2 L 7 2 4F RT A6WE 1998091100593 19980911 00593 NM 1998 9 11 DL72L981837 1 19980904 A 5312 65872608 BULKHEAD FITTING BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 501DA 21303 FOUND ON F-2 LETTER CK, RT I/B TENSION TIE FITTING CRACKED AFT OF STA 1183 BULKHEAD. REPLACED FITTING PER BOEING DWG 65 -17509 REV M. 2 L 7 3 4F A3WE 1998091100594 19980911 00594 NM 1998 9 11 DL72S981846 1 19980906 A 3350 BATTERY 900835A BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 421DA 21274 LEFT WING MID BODY FAIRING EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998091100595 19980911 00595 NM 1998 9 11 DL72S981847 1 19980907 A 3350 334701743 LIGHT BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 489DA 21019 EMERGENCY LIGHT EXIT SIGN AT L1 DOOR DIM DURING TEST. REPLACED LIGHT MODULE, CKS OK. 2 L 7 3 4F A3WE 1998091100596 19980911 00596 NM 1998 9 11 DL72L981850 1 19980902 A 5330 SKIN BOEING 727 727232 1384082 NM BS 700 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 700 BETWEEN STR 28R AND 28L. THE CORROSION WAS CUT OUT WITH A 9 X 6.5 CUTOUT . THE CUTOUT WAS ADJACENT TO AN EXISTING REPAIR FOR ANOTHER SKIN CUTOUT. THE EXISTING REPAIR WAS REMOVED AND BOTH SKIN CUTOUTS WERE REPAIRED WITH A SINGLE DOUBLER INSTALLED PER THE GUIDELINES OF B727 SRM 53-30-3, FIG 3. THE REPAIR WAS DO CUMENTED PER ER/A 365586-14AD. 2 L 7 3 4F A3WE 1998091100597 19980911 00597 NM 1998 9 11 DLM11981851 1 19980907 A 5330 SKIN DOUG MD11 MD11 3023602 NM CARGO DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 810DE 48565 FUSELAGE SKIN DAMAGED AT LOWER FWD CORNER OF C-1 DOOR 3 INCHES ABOVE SCUFF PLATE. REPAIRED DAMAGED AREA PER SRM 53-50-0 0-0-7. 2 L 7 3 4F RT A22WE 1998091100598 19980911 00598 NM 1998 9 11 DL72S981854 1 19980907 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 416DA 21258 DURING L/O, FOUND OVERWING EMERGENCY EXIT LIGHTS NOT ILLUM AT LT WING STA 804. REPLACED BATTERY PACK, OP CKS NORMAL. 2 L 7 3 4F A3WE 1998091100599 19980911 00599 WP 1998 9 11 DLL17981855 1 19980908 A 2910 1791421 HYD LINE LKHEED 1011 10113853 5265020 WP RT AILERON LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 766DA 193H1207 HYDRAULIC SYSTEM-B LOW QTY LIGHT CAME ON IN FLIGHT. QUANTITY INDICATED LESS THAN QUARTER FULL. FOUND RT O/B AILERON AC TUATOR PRESSURE LINE LEAKING AT ANGULAR SEAL PLATE (P/N 277203191). REPLACED SEAL, SERVICED HYDRAULICS AND LEAK CHECKS SATISFACTORY. 2 L 7 3 4F A23WE 1998091100600 19980911 00600 NM 1998 9 11 DL76L981856 1 19980908 A 3350 BULB 1317 BOEING 767 767332 1382001 NM LT WING FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 173DN 24800 ON LAYOVER, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BULB. 2 L 7 2 4F RT A1NM 1998091100601 19980911 00601 NM 1998 9 11 DL72W981858 1 19980812 A 5753 652163388A RIB BOEING 727 727247 138408F NM NR 4 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 DURING SHOP VISIT, THE I/B AFT CLOSEOUT RIB WAS FOUND CRACKED. THE RIB WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 808. 2 L 7 3 4F A3WE 1998091100602 19980911 00602 NM 1998 9 11 DL73E981859 1 19980905 A 5330 65458001206 SKIN BOEING 737 737247 138448D NM R1 DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 TOOLING DAMAGE WAS INCURRED TO THE FUSELAGE SKIN AT A FASTENER LOCATION UNDER THE FWD CORNER OF THE R1 DOOR CUTOUT. THE SUBJECT FASTENER WAS LOCATED UNDER THE DOOR LOWER THRESHOLD PLATE. REPAIR PER ER/A 332212-14. 2 L 7 2 4F A16WE 1998091100603 19980911 00603 NM 1998 9 11 DL73E981860 1 19980905 A 5347 6545410224 SEAT TRACK BOEING 737 737247 138448D NM BS 543 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 SEVERAL LIGHTENING HOLES IN THE UPPER SHORD OF THE RBL 25 OVERWING SEAT TRACK WERE DAMAGED DURING REPLACEMENT OF THE PAR T. THE DAMAGED HOLES ARE LOCATED BETWEEN BS 543 TO 769. REPAIRED PER ER/A 332203-14. 2 L 7 2 4F A16WE 1998091100604 19980911 00604 NM 1998 9 11 DLM88981861 1 19980903 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 998DL 53370 CRACKS WERE FOUND ON THE STA 1418 FRAME AT L-2R AND L-2R ON THE STA 1418 FRAME. THE CRACKS WERE TYPICAL OF THOSE FOUND IN DAC S/B 53-184, REV 1. THE CRACKS WERE DUE TO FATIGUE DAMAGE. REPAIRED PER ER/A 332146-14. 2 L 7 2 4F RT A6WE 1998091100605 19980911 00605 NM 1998 9 11 P5CA9801379 1 19980904 A 5320 DECK BOEING 747 747122 1384872 NM BS 1354 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON PRESSURE DECK SKIN BS 1354 BL 113 LEFT. REPAIRED PER REPAIR SCHEME R53-48-33819 AND 8110-03. 2 L 7 4 4F A20WE 1998091100606 19980911 00606 NM 1998 9 11 P5CA9801380 1 19980902 A 5313 LONGERON BOEING 747 747122 1384872 NM BS 1840-1860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON LONGERON AT BS 1840 TO 1860 STR 45 LEFT. CORROSION REMOVED PER SRM 53-10-01. 2 L 7 4 4F A20WE 1998091100607 19980911 00607 NM 1998 9 11 P5CA9801381 1 19980903 A 5330 SKIN BOEING 747 747122 1384872 NM BS 360-520 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FOUND 65 LONGITUDINAL FASTENER HOLES IN SKIN CRACKED. REAMED OUT HOLES, HFEC, FREEZE PLUGS AND REPAIRED SKIN PER SRM 53 -22-72. 2 L 7 4 4F A20WE 1998091100608 19980911 00608 NM 1998 9 11 P5CA9801382 1 19980903 A 5311 FRAME BOEING 747 747122 1384872 NM BS 960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FRAME AT BS 960 STR 5-6 RIGHT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998091100609 19980911 00609 NM 1998 9 11 P5CA9801383 1 19980903 A 5311 FRAME BOEING 747 747122 1384872 NM BS 380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FRAME STRUCTURES AT BS 380 LEFT STR 23-25R FOUND EXTENSIVE CRACKING LEFT AND RIGHT SIDES. REPLACED FRAME ASSY PER PAO-H KG 98-0140 AND HAECO RS 5312-23812 AND 8110-03. 2 L 7 4 4F A20WE 1998091100610 19980911 00610 NM 1998 9 11 P5CA9801384 1 19980803 A 5343 TRUNNION BOEING 747 747122 1384872 NM NLG CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NOSE GEAR TRUNNION FITTING FWD CUTOUT WEB CRACKED LEFT AND RIGHT SIDES. REPAIRED PER SB 53-2293 REPAIR. 2 L 7 4 4F A20WE 1998091100611 19980911 00611 NM 1998 9 11 P5CA9801385 1 19980903 A 5311 FRAME BOEING 747 747122 1384872 NM BS 960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FRAME CHORD AT BS 970 STR 8 AND 9 RIGHT FOUND CRACKS. REPAIRED FRAME PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998091100612 19980911 00612 NM 1998 9 11 P5CA9801386 1 19980904 A 5313 LONGERON BOEING 747 747122 1384872 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 OVERWING LONGERON BULKHEAD FORGING AT BS 1480 STR 32-33R FOUND CRACK 6 INCHES LONG PLUS NUMEROUS MINOR BOLT HOLE CRACKS IN FITTINGS OF ASSOCIATED AREA. REPAIRED PER HAECO REPAIR SCHEME R53-43-33825 AND NUMEROUS 8110-3 FORMS AND BOEING SB 5 3A2390. 2 L 7 4 4F A20WE 1998091100613 19980911 00613 NM 1998 9 11 P5CA9801387 1 19980903 A 5312 BULKHEAD SPLICE BOEING 747 747122 1384872 NM BS 1480 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NUMEROUS BOLT HOLE CRACKS IN COMMON FITTINGS OF THE BODY STATION 1480 BULKHEAD LONGERON SPLICE. REPAIRED PER HAECO REPA IR SCHEME R53-61-33817 AND NUMEROUS 8110 REPORTS AND SB 53A2390. 2 L 7 4 4F A20WE 1998091100614 19980911 00614 NM 1998 9 11 P5CA9801388 1 19980903 A 5320 WEB BOEING 747 747122 1384872 NM BS 1242 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON WING GEAR WHEEL WELL BS 1242 TO 1246 WL 155 RIGHT WEB. REPAIRED PER SRM 53-10-01 FIG 1. 2 L 7 4 4F A20WE 1998091100615 19980911 00615 NM 1998 9 11 P5CA9801389 1 19980904 A 5311 FRAME BOEING 747 747122 1384872 NM BS 960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 FRAME AT BS 960L STR 5 LEFT FOUND CRACKED. REPAIRED PER SRM 53-10-04 FIG 54. 2 L 7 4 4F A20WE 1998091100616 19980911 00616 NM 1998 9 11 P5CA9801390 1 19980904 A 3260 65B4750630 LOGIC MODULE BOEING 747 747122 1384872 NM LANDING GEAR MALFUNCTION A P5CA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 23 852FT 19757 FOLLOWING TAKEOFF HAD GEAR UP WARNING LIGHT AND AUDIBLE WARNING HORN. ALL LANDING GEAR WARNING LTS AT F/E STATION REMAI NED ILL. RETURNED TO HKG. REPLACED LANDING GEAR LOGIC MODULE IAW MM 31-26-03. OPS CHECK OK. 2 L 7 4 4F A20WE 1998091100617 19980911 00617 WP 1998 9 11 RRXA98421 1 19980901 A 2612 FIRE LOOP DOUG DC8 DC863 302198A WP NR 3 ENGINE SHORTED A RRXA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 WP 15 964R 46000 NR 3 ENG FIRE WARNING SOUNDED WITH LIGHT FIRED BOTH BOTTLES. LIGHT REMAINED ON. REMOVED AND REPLACED SHORTED FIRE LOOP SECTION D1-48 PER DC-8 M/M CHAP 26-10-1. 2 L 7 4 4F 4A25 1998091100618 19980911 00618 1998 9 11 RRXA98422 4 19980903 A 3442 RADAR DOUG DC8 DC871F 302199D WP E/E COMPT MALFUNCTIONED A RRXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 15 8079U 45947 AT FLIGHT 31,0 RADAR PAINTS GROUND ON RIGHT SIDE. TRANSFERRED TO DMI NR 809042 IAW MEL 34-21 CATC DUE 9-13-98, PLACARD INSTALLED. 2 L 7 4 4F RT 4A25 1998091100619 19980911 00619 WP 1998 9 11 RRXA98423 1 19980904 A 2612 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 2 ENGINE MALFUNCTIONED A RRXA K NONE N FALSE WARNING CR CRUISE 1 WP 15 8084U 45974 NR 2 ENGINE FIRE WARNING ILLUMINATES INTERMITTENTLY WITH ENGINE RUNNING OR SHUTDOWN. FIRE WARNING TEST NORMAL. REMOVED AND REPLACED RT AND LT FAN COMPARTMENT FIRE LOOPS AND RT AND LT LOWER CORE COMPARTMENT FIRE LOOPS. NR 2 ENGINE FIRE WA RNING OPS CHECKS GOOD STATIC AND ON HIGH POWER RUN IAW MM CHAPTER 77-21-20. CLOSED AND SECURED COWLINGS. 2 L 7 4 4F RT 4A25 1998091100620 19980911 00620 WP 1998 9 11 RRXA98424 1 19980905 A 2761 ACTUATOR DOUG DC8 DC873F 302199F WP SPOILER LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 15 791FT 46045 ON APPROACH WITH GEAR DOWN SPOILER PRESS READS ABOUT 2600 PSI THEN DROPS TO 2400 PSI, DECREASING TO 2000 PSI. TIGHTNED B-NUT TOP OF ACCUMULATOR AND BLED SPOILER RESERVOIR SYSTEM PRESS CK NORMAL ON GROUND. DURING 5 MIN DURATION OF PUMP RU NNING NOTICED SYSTEM PRESS GAUGE IN COCKPIT DROPPED BELOW 2800 PSI. REMOVED AND REPLACED SYS PRESS TRANSMITTER, NO HELP . REMOVED AND REPLACED SPOILER PUMP. LK CK GOOD BUT PROBLEM REMAINS SEE ITEM 3. SPOILER PRESS DROPS FROM 3000 PSI TO AS LOW AS 2400 PSI. REMOVED AND REPLACED SPOILER RESERVOIR IAW MM 27-61-1, LK CK OK. REMOVED AND REPLACED CASE DRAIN A ND PRESS SYS FILTER-SYSTEM OP AND LK CKS OK. 2 L 7 4 4F RT 4A25 1998091100621 19980911 00621 NM 1998 9 11 VNAA9809003 1 19980905 A 2150 GB2001AA1 CHECK VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PACK FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 424JS 3033 A RIGHT HAND AIR CONDITIONING PACK FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETU RNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND NACA DUCT CHECK VALVE, IN ACCORDANCE WITH DORNIER M AINTENANCE MANUAL 21-51-24. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091100622 19980911 00622 1998 9 11 VNAA9809004 4 19980906 A 2350 7013270932 RMU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 FAILED A VNAA O OTHER J WARNING INDICATION CR CRUISE 1 GL 07 427JS 65187 32893 3039 DURING CRUISE FLIGHT, A NUMBER ONE RADIO MANAGEMENT UNIT FAIL WARNING MESSAGE ILLUMINATED. THE CREW UTILIZED THE NUMBER TWO RADIO MANAGEMENT UNIT, AND CONTINUED ON TO AZO. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECT ED AND REPLACED THE NUMBER TWO RADIO MANAGEMENT UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 23-11-00. OPERATION AL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091800001 19980918 00001 WP 1998 9 18 VJ9800318 1 19980429 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 196 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 945VV 47238 MAIN CABIN SUPPORT STA 196 BL 0 - LBL 44 CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT, FABRICATED REPAIR SUPPORT FROM 2652479 EXTRUSION 42.50. LOCATED TRIM TO FIT, DRILLED, DEBURRED, TREATED, AND PRIMED IAW 51-30-2, 53-01-1 FIG 11, 51-10 -2 AND SRM 51-10-4, 51-30-5. 2 L 7 2 4F A6WE 1998091800002 19980918 00002 WP 1998 9 18 VJ9800320 1 19980728 A 5330 1A331661 SKIN DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 945VV 47238 DURING ACCOMPLISHMENT OF AD 88-24-08 INSPECTION PER EO-12-29-B1058I/R, HFEC INDICATES EXTERNAL FUS SKIN CRACK .100 AT CO UNTERSUNK FASTENER HOLE COMMON TO FS 617 RT LONG 1 SHEAR TIE. REMOVED FASTENER, VERIFIED CRACK IN SKIN AT COUNTERSUNK, REMOVED FAST, CUT OUT 2.5 HOLE AT CRACK AREA, FABBED REPAIR FINGER DOUBLER, EXTERIOR DOUBLER AND SKIN FILLER. ALODINED, PRIMED AND INSTALLED DOUBLERS IAW SRM 51-30-2, 53-04 FIG 38, AND 51-10-3 (DIMMENSIONS 6.98 X 7.61 FINGER DOUBLER SKIN F ILLER, EXTERIOR DOUBLER 8.58 X 6.14). 2 L 7 2 4F A6WE 1998091800003 19980918 00003 WP 1998 9 18 VJ9800321 1 19980427 A 5330 1A33157 SKIN DOUG DC9 DC932 3022066 WP BS 639 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 945VV 47238 DURING ACCOMPLISHMENT OF AD 88-24-08 INSP PER EO 12-5330-29-B1058I/R, HFEC INDICATES EXTERNAL FUSELAGE SKIN CRACK .100 A T COUNTERSINK FASTENER HOLE COMMON TO FS 639 RT LONG 5 LOWER SHEAR TIE. REMOVED FASTENER, NDT VERIFIED CRACK AT COUNTER SINK. CUT OUT 2 .125 DIAMETER SKIN WERE CRACK WAS FOUND. FABBED FINGER DOUBLER REPAIR OUT OF MIL-T9064LH .032 P NR 1A- 33157-1. FABBED, TREATED, AND PRIMED FILLER OUT OF 2024 T3 .050. INSTALLED REPAIR DOUBLER AND FILLER TO A/C FS 639 RT STR 5 IAW DC-9 SRM 51-10-3, 51-30-2, AND 53-04 FIG 38, 51-10-45, AND EO12-5330-29-B1058I/R. 2 L 7 2 4F A6WE 1998091800004 19980918 00004 WP 1998 9 18 VJ9800322 1 19980507 A 5753 SKIN DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 945VV 47238 SPOT OF LIGHT CORROSION ON UNDER SIDE OF LEFT WING FLAP L/E AT INTERSECTION OF CENTER AND I/B FIXED VANES. MECHANICALLY REMOVED CORROSION .030 MATERIAL LOSS, OUT OF LIMITS. FABRICATED REPAIR DOUBLER FROM .071 7075 T-6 MEASURING 3 X 4.75 AND INSTALLED IAW SRM 578-01 FIG 3, 51-20-0 AND 51-30-1. 2 L 7 2 4F A6WE 1998091800005 19980918 00005 WP 1998 9 18 VJ9800323 1 19980426 A 5311 1A33160 FRAME DOUG DC9 DC932 3022066 WP BS 1132 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 945VV 47238 CANTED FRAME STA 1132 BETWEEN LONGERON 13R AND 14R CANTED FRAME WEB CRACK 2. REMOVED HAT STIFFENER, DOUBLER AND ANGLE T O GAIN ACCESS TO CORROSION BETWEEN OVERLAPING WEBS REMOVED CORRODED SECTION OF WEB IAW DC-9 SRM 53-10 FIG 1. FABBED DOU BLER REPAIR FROM 7075 T6 .050 9.40 X 8.50 X 7.35 X 7.20 IAW SRM 53-01 FIG 1. TREATED, PRIMED AND INSTALLED IAW SRM 51- 10-3, 53-04 FIG 4 AND INSTALLED INTERNAL SHROUD. 2 L 7 2 4F A6WE 1998091800006 19980918 00006 WP 1998 9 18 VJ9800324 1 19980404 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 201-212 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 SEAT TRACK STA 201-237 BL 45 RT CORRODED BEYOND LIMITS. REMOVED SECTION OF TRACK AND REPLACED IAW SRM 53-05 FIG 10G. 2 L 7 2 4F A6WE 1998091800007 19980918 00007 WP 1998 9 18 VJ9800325 1 19980404 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 579-598 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 CORROSION BULGE STA 598 LONG 30-29 RT. REMOVED, FABRICATED AND INSTALLED INNER DOUBLER STA 579-598 LONG 29 RT TO 29 LT IAW SRM 53-31-0 FIG 8, 51-30-1, 51-30-2 AND 51-10-3. 2 L 7 2 4F A6WE 1998091800008 19980918 00008 WP 1998 9 18 VJ9800326 1 19980404 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 598 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 LEVEL 2 CORROSION BULGE STA 598 LONG 29RT. REMOVED AND REPLACED LONG 29 RT STA 579-578 IAW 51-30-1, 51-30-2, AND 51-10- 3. 2 L 7 2 4F A6WE 1998091800009 19980918 00009 WP 1998 9 18 VJ9800327 1 19980306 A 5320 INTERCOASTAL DOUG DC9 DC932 3022066 WP BS 945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 LEVEL 2 CORROSION IN AFT PIT FS 945 LONG 29R. REMOVED INTERCOASTAL AT FS 945 LONG 29R. FABRICATED NEW INTERCOASTAL, RE PLACED THE INTERCOASTAL, TREATED, PRIMED AREA IAW SRM 53-01 FIG 1, 51-10-2, 51-10-2, AND 51-10-3. 2 L 7 2 4F A6WE 1998091800010 19980918 00010 WP 1998 9 18 VJ9800328 1 19980315 A 5321 99578261 FLOOR DOUG DC9 DC932 3022066 WP BS 140-160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 F/O'S FLOOR PANEL NR 14 CORRODED BEYOND LIMITS IAW SRM 53-01 FIG 1 PG 8. MATERIAL LOSS 100 PERCENT. FORMED NEW FLOOR P ANEL FROM 7075 T6 .040 CLAD IAW DC-9 SRM 51-10-2, 51-10-4, TREATED AND PRIMED PANEL IAW SRM 51-10-3. 2 L 7 2 4F A6WE 1998091800011 19980918 00011 WP 1998 9 18 VJ9800329 1 19980326 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 180-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 REMOVED CORRODED AREA OF FLOOR PANEL WEB STA 180-200 BL 0 TO BL 44 LT. CORROSION LEVEL 2. FABRICATED AND INSTALLED REP AIR DOUBLER IAW SRM 53-01 FIG 4. 2 L 7 2 4F A6WE 1998091800012 19980918 00012 WP 1998 9 18 VJ9800330 1 19980329 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 ON C-CHECK, FOUND FLOOR SUPPORT FS 160 BL 0 TO RBL-52 CORRODED LEVEL 2. REMOVED CORROSION, FOUND REMOVAL TO BE OUT OF L IMITS. REMOVED FLOOR SUPPORT, FABBED SUPPORT, TREATED, PRIMED, AND INSTALLED FLOOR SUPPORT IAW DC-9 SRM 51-10-3, 53-01 FIG 1 AND 51-30-2. 2 L 7 2 4F A6WE 1998091800013 19980918 00013 WP 1998 9 18 VJ9800331 1 19980329 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 FLOOR SUPPORT FS 160 TO 200 RBL 44 CORRODED (LEVEL 2). REMOVED CORROSION AND REMOVAL OUT OF LIMITS. REMOVED FLOOR SUPP ORT, FABBED NEW FLOOR SUPPORT, TREATED, PRIMED, AND INSTALLED FLOOR SUPPORT IAW DC-9 SRM 51-10-3, 51-30-5, 53-01 FIG 1. 2 L 7 2 4F A6WE 1998091800014 19980918 00014 WP 1998 9 18 VJ9800332 1 19980325 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 CABIN FLOORBOARD, BETWEEN RT I/B SEAT TRACK AND RT SIDE WALL AT FS 237, FWD WND IS CRACKED AND CORRODED (LEVEL 2) PANEL NR 21. CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED IAW DC-9 SRM 53-01 FIG AND 51-30-3. 2 L 7 2 4F A6WE 1998091800015 19980918 00015 WP 1998 9 18 VJ9800333 1 19980328 A 5320 991556531 BEAM DOUG DC9 DC932 3022066 WP PAX DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 CORROSION ON LOWER BEAM AFT PAX ENTRY DOOR CUT OUT OF LIMITS IAW DC-9 SRM 52-01 FIG 1. REMOVED AND REPLACED 9915565-31 LOWER BEAM IAW DC-9 SRM 51-10-4, 51-30-1, 51-10-3, AND DC9 OHM 52-63-1. 2 L 7 2 4F A6WE 1998091800016 19980918 00016 WP 1998 9 18 VJ9800334 1 19980326 A 5321 527558981144 FLOOR DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 CORROSION ON FLOOR PANEL AT AFT ENTRANCE (LEVEL 2). FABBED NEW FLOOR PANEL AND HAT CHANNEL SUPPORTS, TREATED, PRIMED FL OOR PANELS AND HAT CHANNELS. INSTALLED NEW AND USABLE ORIG HAT CHANNELS TO NEW FLOOR PANEL AT AFT ENTRANCE. 2 L 7 2 4F A6WE 1998091800017 19980918 00017 WP 1998 9 18 VJ9800335 1 19980227 A 5320 ANGLE DOUG DC9 DC932 3022066 WP AFT GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 FOUND CORROSION ON BTM (2 EA) CORNERS OF NR 4 AFT AFT GALLEY. CLEANED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 5 3-01 PAG 8. REMOVED AND FABRICATED ANGLE FOR BOTTOM OF NR 4 AFT GALLEY FROM S124943T 75 X 1.0 X 11.0 X ANGLE IAW SRM 53 -01 FIG 2, 51-10-4, INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998091800018 19980918 00018 WP 1998 9 18 VJ9800336 1 19980330 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 FOUND CORROSION ON CENTER FLOOR SUPPORT BETWEEN FS 200 AND 237 BL 0. CORROSION BEYOND LIMITS IAW SRM 53-01 FIG 1. REMO VED FLOOR SUPPORT, CUT AND TRIMMED TO FIT NEW SUPPORT. DRILLED, TREATED AND PRIMED. INSTALLED WITH SEALER IAW SRM 51-1 0-3, 51-00, 51-30-5. 2 L 7 2 4F A6WE 1998091800019 19980918 00019 WP 1998 9 18 VJ9800337 1 19980330 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 204-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 FOUND LONGITUGINAL FLOOR SUPPORT HEAVILY CORRODED BETWEEN FS 204 AND 237 (X=-14 R/S). CORROSION BEYOND LIMITS IAW SRM 5 3-01 FIG 1. REMOVED FLOOR SUPPORT, DRILLED, TRIMMED TO FIT, DEBURRED, TREATED AND PRIMED. INSTALLED WITH SEALER IAW SR M 51-30-5, 51-10-3, 51-00. 2 L 7 2 4F A6WE 1998091800020 19980918 00020 WP 1998 9 18 VJ9800338 1 19980404 A 5320 29573151 STRAP DOUG DC9 DC932 3022066 WP STA 908 & 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 CARGO TIE DOWN RING RETAINER STRAPS AFT PIT STA 908 AND 935 CORRODED BEYOND LIMITS IAW DC-9 SRM 53-01 FIG 1. REMOVED AN D REPLACED STRAPS IAW MM 25-52-1. 2 L 7 2 4F A6WE 1998091800021 19980918 00021 WP 1998 9 18 VJ9800339 1 19980302 A 5320 INTERCOASTAL DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 INTERCOASTAL CORRODED BEYOND LIMITS AT FS 965 BETWEEN LONGERON 27LT AND 29 RT. REPLACED CORRODED INTERCOASTAL AT FS 965 , LONGERON 27 LT-29 RT IAW SRM 51-10-2, 51-30-1, 51-30-2. 2 L 7 2 4F A6WE 1998091800022 19980918 00022 WP 1998 9 18 VJ9800340 1 19980328 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 CENTER FLOOR SUPPORT STA 160-200 BL 0 CORRODED BEYOND LIMITS IAW DC-9 SRM 53-01 FIG 1. FABRICATED AND INSTALLED FLOOR S UPPORT IAW DC-9 SRM 51-10-1, 51-10-3, 51-10-4, 51-30-2. 2 L 7 2 4F A6WE 1998091800023 19980918 00023 WP 1998 9 18 VJ9800341 1 19980326 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 REMOVED AND REPLACED 3 CORRODED FLOOR (LEVEL 2) SUPPORTS IAW SRM 51-30-2 FROM STA 200 BL 0 TO BL 57 RT. FLOOR SUPPORTS FABRICATED FROM 60-2576 7075 T6 EXTRUSION IAW DC-9 SRM 51-1-2, 51-1-4, 51-10-3. 2 L 7 2 4F A6WE 1998091800024 19980918 00024 WP 1998 9 18 VJ9800342 1 19980328 A 5320 3917852501 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 REMOVED AND REPLACED LOWER CLOSE OUT ANGLE BOTTOM OF AFT PAX DOOR STA 996 IAW 51-10-1, 51-10-4, 51-30-1. CORROSION ON A NGLE WAS FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 52-01 FIG 1. 2 L 7 2 4F A6WE 1998091800025 19980918 00025 WP 1998 9 18 VJ9800343 1 19980328 A 5320 992948025 PAN DOUG DC9 DC932 3022066 WP PAX DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 AFT PAX DOOR LOWER PAN CORRODED BEYOND LIMITS IAW SRM 52-01 FIG 1. REMOVED AND REPLACED PAN IAW DC-9 SRM 51-10-1, 51-10 -4, 51-30-1, AND OHM 52-63-1. 2 L 7 2 4F A6WE 1998091800026 19980918 00026 WP 1998 9 18 VJ9800344 1 19980328 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 173-193 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 FLOOR SUPPORT STA 173-193 BL 44 LT CORRODED BEYOND LIMITS IAW SRM 53-01 FIG 1. FABRICATED AND INSTALLED FLOOR SUPPORT I AW SRM 51-10-3, 51-10-1, 51-10-4, 51-30-2. 2 L 7 2 4F A6WE 1998091800027 19980918 00027 WP 1998 9 18 VJ9800345 1 19980328 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 198 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 903VJ 47261 FLOOR SUPPORT STA 198 CORRODED BEYOND LIMITS IAW SRM 53-01 FIG 1. FABRICATED AND INSTALLED FLOOR SUPPORT IAW DC-9 SRM 5 1-10-1, 51-10-3, 51-10-4, 51-30-2. 2 L 7 2 4F A6WE 1998091800028 19980918 00028 NM 1998 9 18 AWXA9800201 1 19980904 A 3350 849029 BATTERY BOEING 737 7373G7 1384595 NM CABIN DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 303AW 24010 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS AT ROW 1 THROUGH 5 INOP. REMOVED AND REPLACED BATTERY AND CHAR GER ASSEMBLY. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998091800029 19980918 00029 NM 1998 9 18 AWXA9800202 1 19980904 A 2120 AIR DISTRIBUTION BOEING 737 737277 1384570 NM CABIN ODOR A AWXA K NONE O OTHER DE DESCENT 1 WP 28 184AW 22651 JET FUEL ODOR IN CABIN ON DESCENT. ALSO COULD DETECT ODOR IN COCKPIT AFTER COCKPIT DOOR OPENED AT GATE. FOUND SMALL FU EL LEAK AT RT WING AFT BOOST PUMP BLEED VALVE. RESET BLEED CHECK VALVE ON PUMP. GROUND RUN BOTH ENGINES AND APU. ISOL ATED BOTH PACKS. PRESSURIZED AIRCRAFT. NO FUEL SMELL NOTED IN CABIN AT THIS TIME. 2 L 7 2 4F RT A16WE 1998091800030 19980918 00030 NM 1998 9 18 CALA9801660 1 19980909 A 5230 ANGLE BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN ATTACH ANGLE AT C-1 DOOR FRAME. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INS TALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800031 19980918 00031 NM 1998 9 18 CALA9801661 1 19980909 A 5753 65192497 FLAP TRACK BOEING 727 727224 1384076 NM NR 6 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WING NR 6 FLAP TRACK CORRODED AROUND FORWARD MOUNT HOLES. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00. 2 L 7 3 4F A3WE 1998091800032 19980918 00032 NM 1998 9 18 CALA9801662 1 19980909 A 5752 652172641K SKIN BOEING 727 727224 1384076 NM LT AILERON TAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND LT OUTBOARD AILERON TAB DENTED ON UPPER SURFACE WITH THE TRAILING EDGE BENT. THE AILERON TAB WAS REMOV ED AND REPLACED IAW MM 27-10-41. 2 L 7 3 4F A3WE 1998091800033 19980918 00033 NM 1998 9 18 CALA9801663 1 19980909 A 5321 FLOOR BOEING 727 727224 1384076 NM BS 1178-1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOOR WEB WITH CORROSION RUNNING INTO SPLICE AT FS 1178-1183, RBL 16. THE CORRODED AREA WAS CUT OUT AN D A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, 51-10-2, AND 51-30-2, PARAGRAPH 7. 2 L 7 3 4F A3WE 1998091800034 19980918 00034 NM 1998 9 18 CALA9801664 1 19980909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1130-1150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1130-1150, RBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS I NSTALLED IAW SRM 51-10-6 AND 51-10-2. 2 L 7 3 4F A3WE 1998091800035 19980918 00035 NM 1998 9 18 CALA9801665 1 19980909 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 1 INCH CRACK IN STRINGER 15L AND 15R AT STA 720B. REPAIRS WERE INSTALLED IAW SRM 53-10-3 AND 51-10-2 . 2 L 7 3 4F A3WE 1998091800036 19980918 00036 NM 1998 9 18 CALA9801666 1 19980909 A 5753 65192509 TRACK BOEING 727 727224 1384076 NM NR 1 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND NR 1 FLAP TRACK PAD MOUNT CENTER HOLE CORRODED. THE FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW M M 57-40-00. 2 L 7 3 4F A3WE 1998091800037 19980918 00037 NM 1998 9 18 CALA9801667 1 19980909 A 5753 TRACK BOEING 727 727224 1384076 NM NR 3 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND CORROSION IN BORE WHERE BUSHINGS MOUNT ON LT AND RT SIDES OF NR 3 FLAP TRACK FORWARD CLEVIS. THE FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-40-00. 2 L 7 3 4F A3WE 1998091800038 19980918 00038 NM 1998 9 18 CALA9801668 1 19980909 A 5320 PRESSURE PANEL BOEING 727 727224 1384076 NM BS 930 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .9375 INCH CRACK IN LT MLG WHEEL WELL CEILING PRESSURE PANEL JUST FORWARD OF WHEEL WELL LIGHT AT STA 930, LBL 48. THE CRACK WAS STOP DRILLED IAW BOEING DRAWING 65-89360. A DOUBLER WAS INSTALLED IAW BOEING DRAWING 65-893 60. 2 L 7 3 4F A3WE 1998091800039 19980918 00039 NM 1998 9 18 CALA9801669 1 19980909 A 5753 651920210 SPINDLE BOEING 727 727224 1384076 NM NR 8 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND NR 8 FLAP CARRIAGE AFT SPINDLE CORRODED. THE NR 8 FLAP CARRIAGE ASSEMBLY WAS REMOVED AND REPLACED IAW MM 57-50-00. 2 L 7 3 4F A3WE 1998091800040 19980918 00040 EU 1998 9 18 QXEA9801280 1 19980907 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 481US 11230 AFT FACING EXIT SIGN AT MID CABIN HAS SEVERAL BULBS OUT. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPERATIONAL TESTS WERE P ERFORMED, RESULTS NORMAL. 2 L 7 2 4F RT A20EU 1998091800041 19980918 00041 EU 1998 9 18 QXEA9801281 1 19980907 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 493US 11161 EMERGENCY EXIT LIGHT AT ROW 9 IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INOPERATIVE BULBS. OPERATIONAL TEST S WERE PERFORMED, RESULTS NORMAL. 2 L 7 2 4F RT A20EU 1998091800042 19980918 00042 WP 1998 9 18 MWEA98949 1 19980905 A 5312 49179232 BULKHEAD SUPPORT DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACK IN AFT PRESSURE BULKHEAD UPPER LEFT SUPPORT ATTACHED TO -13 DOUBLER. MTC REMOVED AND REPLACED DOUBLER. 2 L 7 2 4F A6WE 1998091800043 19980918 00043 WP 1998 9 18 MWEA98950 1 19980906 A 5320 591757921 JAMB DOUG DC9 DC932 3022066 WP VENTRAL DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACK ON AFT VENTRAL DOOR JAMB LEFT SIDE ANGLE. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998091800044 19980918 00044 WP 1998 9 18 MWEA98951 1 19980906 A 3350 6011775 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 FOUND RIGHT NACELLE EMERGENCY LIGHT VERY DIM. MTC REMOVED AND REPLACED NACELLE EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1998091800045 19980918 00045 WP 1998 9 18 MWEA98952 1 19980906 A 5246 591479129 DOOR DOUG DC9 DC932 3022066 WP WATER SERVICE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND TEAR IN WATER SERVICE PANEL DOOR ON AFT LOWER CORNER. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998091800046 19980918 00046 WP 1998 9 18 MWEA98953 1 19980906 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND FORWARD PASSENGER DOOR EMERGENCY SLIDE COVER CRACKED. MTC RESECURED LAMINANT COVER TO EMERGENCY SLIDE COVER. 2 L 7 2 4F A6WE 1998091800047 19980918 00047 WP 1998 9 18 MWEA98954 1 19980906 A 3350 6011777 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 FOUND LEFT NACELLE EMERGENCY LIGHT WILL NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998091800048 19980918 00048 WP 1998 9 18 MWEA98955 1 19980907 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE MAIN SLIDE ON FORWARD EXIT FELL OFF. MAINTENANCE REINSTALLED PASSENGER DOOR SLIDE. 2 L 7 2 4F A6WE 1998091800049 19980918 00049 WP 1998 9 18 MWEA98956 1 19980908 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 THE GALLEY SLIDE GIRT BAR FELL OFF DOOR. MTC REINSTALLED GALLEY SLIDE AND COVER. 2 L 7 2 4F A6WE 1998091800050 19980918 00050 WP 1998 9 18 ARWA980904 1 19980910 A 2822 11230311 BOOST PUMP DOUG DC8 DC863 302198A WP NR 4 FAILED A ARWA O OTHER O OTHER CR CRUISE 1 SO 19 345JW 46042 NR 4 ALT BOOST PUMP POPS C/B IN FLIGHT. REMOVED AND REPLACED NR 4 ALT FUEL BOOST PUMP, OPS CHECKED NORMAL IAW MM 28-22- 0. 2 L 7 4 4F 4A25 1998091800051 19980918 00051 1998 9 18 ARWA980905 2 19980910 A 7230 COMPRESSOR DOUG DC8 DC862 3021970 WP NR 2 ENGINE STALLED A ARWA D RETURN TO BLOCK C F.O.D. TX TAXI/GRND HDL 1 SO 19 791AL 46150 BLOCK TURNBACK AFTER SPOOLED AND STABLE NR 1 OR NR 2 ENG COMPRESSOR STALL. FOUND PAPER IN INLET OF NR 2 ENGINE. REMOVE D FOD (PAPER) FROM INLET, STARTED AND SPOOLED UP NR 2 ENGINE IAW DC-8 MM 80-00-0, NO DEFECTS NOTED AT THIS TIME. 2 L 7 4 4F 4A25 1998091800052 19980918 00052 NM 1998 9 18 TWAA9814501 1 19980725 A 5753 SKIN BOEING 727 727231 1384079 NM RT TE MIDFLAP MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 24343 21630 RT WING INBD MID FLAP HAD PIECE OF SKIN MISSING, 4 IN BY 16 IN, TOP OTBD EDGE. REPAIRED RT MID FLAP PER BOEING 727 SRM 51-40-6. CHECK-C 2-13-98 MCI. 2 L 7 3 4F A3WE 1998091800053 19980918 00053 NM 1998 9 18 TWAA9814502 1 19980811 A 5730 PANEL BOEING 727 727231 1384079 NM RT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64347 21634 DURING CHECK-C MAINT, FOUND RT WING UPPER WING PANEL CRACKED AT OTBD END OF OTBD SPOILER. INSTALLED FIBERGLAS REPAIR PE R SRM 57-20-4 AND 51-40-6. 2 L 7 3 4F A3WE 1998091800054 19980918 00054 WP 1998 9 18 TWAA9814503 1 19980828 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 170-175 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 FOUND 5 .250 INCH CRACKS IN FUSELAGE SKIN EXTENDING FROM RIVETS STA 170 TO 175, LONG 22L. REPAIRED PER SRM 53-04, FIG 1 2B. 2 L 7 2 4F A6WE 1998091800055 19980918 00055 NM 1998 9 18 TWAA9814504 1 19980818 A 5330 SKIN BOEING 727 727231 1384079 NM BS 660 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54334 20461 DURING CHECK-C MAINT, FOUND FUSELAGE ON RT SIDE PELLOWING, PULLED, AND POPPED RIVET HEADS AT STA 660, S28R AND 28L. COR ROSION REMOVED, INSTALLED DOUBLER OVER AREA OF SKIN THAT WAS BEYOND LIMITS OF CORROSION REMOVAL. ALSO, INCORPORATED EXI STING REPAIR PER SRM 53-30-3 PAGE 5. 2 L 7 3 4F A3WE 1998091800056 19980918 00056 NM 1998 9 18 TWAA9814505 1 19980818 A 5347 SEAT TRACK BOEING 727 727231 1384079 NM BS 1100 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64347 21634 DURING CHECK-C, FOUND CORROSION ON NR 1 CHAIR TRACK, LBL 46 IN AT STA 1100. REMOVED CORRODED TRACK AND INSTALLED NEW TR ACK AND FASTENERS PER SRM 53-10-5. 2 L 7 3 4F A3WE 1998091800057 19980918 00057 NM 1998 9 18 TWAA9814506 1 19980812 A 5320 INTERCOSTAL BOEING 727 727231 1384079 NM BS 700 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 64347 21634 DURING CHECK-C, MAINT FOUND CORROSION ON VERTICAL INTERCOSTAL AT FS 700, STR 28L, BOTTOM MOUNTING FLANGE, BELOW FWD CARG O COMPT FLOOR LEVEL. CORRODED PARTS REMOVED AND REPLACED WITH NEW PARTS MADE OF 7075T6. TREATED, PAINTED, SEALED AND I NSTALLED WITH RIVETS. 2 L 7 3 4F A3WE 1998091800058 19980918 00058 WP 1998 9 18 TWAA9814601 1 19980909 A 5210 SAFETY STRAP DOUG DC9 DC983 3022083 WP PAX DOOR OUT OF POSITION A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 9306T 49567 ON CLIMB-OUT, R1 DOOR HAD AN AIR NOISE. SAFETY STRAP CAUGHT IN DOOR. STRAP WAS STOWED. CHECK-C1. 2 L 7 2 4F RT A6WE 1998091800059 19980918 00059 NM 1998 9 18 TWAA9814602 1 19980909 A 3350 1317 LAMP BOEING 757 7572Q8 1384972 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 704X 28163 EMERGENCY AISLE LIGHT INOP AT ROW 17 FED, RELAMPED. CHECK-C 01, 7-19-98 LAX. 2 L 7 2 4F RT A2NM 1998091800060 19980918 00060 NM 1998 9 18 TWAA9814603 1 19980909 A 3350 65801003 CONNECTOR BOEING 757 7572Q8 1384972 NM CABIN DAMAGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 704X 28163 EGRESS LIGHTS INOP IN FRONT OF LAV DOOR LT BEHIND FIRST CLASS. REPAIRED FLEX CABLE ASSY CONNECTORS MFG PN'S 65801-003 A ND 97F9705. CHECK-C 01. 2 L 7 2 4F RT A2NM 1998091800061 19980918 00061 NM 1998 9 18 TWAA9814604 1 19980909 A 3350 CONNECTOR BOEING 757 7572Q8 1384972 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 704X 28163 EGRESS LIGHT INOP BY L-1 DOOR. SECURED CONNECTOR AND TRACK COVER. CHECK-C 01, 7-19-98 LAX. 2 L 7 2 4F RT A2NM 1998091800062 19980918 00062 NE 1998 9 18 TWAA9814605 2 19980907 A 7200 ENGINE BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 05 54349 21968 3962 TEN MINUTES PRIOR TO LANDING NR 2 ENG OIL QUANTITY WENT DOWN TO 1/8 GAL. PRESSURE DOWN TO 35 PSI. ENG FAILURE PREC. R EPLACED NR 2 ENG. CHECK-C 02, 10-29-97 JFK. 2 L 7 3 4F 4 F A3WE E2EA 1998091800063 19980918 00063 WP 1998 9 18 VJ9800346 1 19980818 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 CABIN FLOOR BOARD CORRODED BEYOND LIMIT AT STA 160-200, RBL 44-54. STOP DRILLED CRACK AND FABRICATED REPAIR IAW DC9 SRM 53-01, FIG 2. HFEC CRACK CONTAINED AT STOP HOLE DC9 SPM NTM PART 06. TREATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALL ED REPAIR IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998091800064 19980918 00064 WP 1998 9 18 VJ9800347 1 19980818 A 5321 135320 FLOOR DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 FLOOR BOARD CORRODED BEYOND LIMIT AT STA 160 - 220, LBL 44-54 AND HAT CHANNELS ON BOTTOM SIDE WORN AND BARE METAL. REMO VED CORROSION IAW DC9 SRM 53-01, FIG 1 AND FABRICATED NEW SKIN IAW DC9 SRM 53-21-1, 51-10-4 AND 53-21-0, FIG 2. 2 L 7 2 4F A6WE 1998091800065 19980918 00065 WP 1998 9 18 VJ9800348 1 19980819 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 227 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 CENTER LT FLOOR BOARD CORRODED BEYOND LIMIT. FOUND 5 HAT CHANNELS CRACKED AFTER FLOOR BOARD AND DOUBLER REMOVED; STOP D RILLED 9 EACH IAW DC9 SRM 53-01, FIG 1. NDT VERIFIED ALL CRACKS TERMINATED IAW DC9 NTSPM PT-08 PER HFEC INSPECTION. FA BRICATED NEW DOUBLER IAW DC9 SRM 53-01, FABRICATED NEW HAT CHANNEL DOUBLER. INSTALLED NEW DOUBLERS AND FLOOR BOARD IAW DC9 SRM 51-30-1, 51-30-2 AND 53-20-1. 2 L 7 2 4F A6WE 1998091800066 19980918 00066 WP 1998 9 18 VJ9800349 1 19980823 A 5260 FRAME DOUG DC9 DC932 3022066 WP RT AFT STAIR CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 938VV 47442 AFT STAIR RT FRAME HAS 2 INCH GOUGE MIDWAY DOWN AND CHAFFING AGAINST FUSELAGE. OUT OF LIMIT IAW DC9 SRM 52-01, CALIPER MEASURE A NR 1729. FABRICATED REPAIR ANGLES IAW DC9 52-01, FIG 2 AND INSTALLED WITH SEALANT. 2 L 7 2 4F A6WE 1998091800067 19980918 00067 WP 1998 9 18 VJ9800368 1 19980828 A 5320 392405509N END CAP DOUG DC9 DC932 3022066 WP BS 598-600 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 END CAPS STA 598 - 600, L30, 29L AND 29R CORRODED BEYOND LIMIT. REMOVED END CAPS AND DETERMINED CORRODED OUT OF LIMIT IAW SRM 53-01, FIG 1. DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED NEW END CAPS IAW DC9 SRM 51-10-3, 51-10-4, 51- 30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998091800068 19980918 00068 WP 1998 9 18 VJ9800369 1 19980828 A 5230 ACCESS PANEL DOUG DC9 DC932 3022066 WP CARGO DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 ACCESS PANEL C2 DOOR, FWD SIDE, CORRODED BEYOND LIMIT AND CORROSION UNDER NUTPLATES. CUT OUT CORRODED AREA IAW DC9 SRM 51-01, FIG 1. FABRICATED REPAIR DOUBLER AND SPLICE, HEAT TREATED, PRIMED, DRILLED AND INSTALLED IAW DC9 SRM 51-10-3, 51 -10-4, 51-30-1, 51-30-2 AND 51-30-8. 2 L 7 2 4F A6WE 1998091800069 19980918 00069 NM 1998 9 18 VJ9800350 1 19980804 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 328-312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 L-1 DOOR SILL LOWER SUPPORT ANGLE BETWEEN STA 328-312 HAS 100 PERCENT MATERIAL LOSS. REMOVED SUPPORT ANGLE AND CLEANED CORROSION, MATERIAL LOSS 100 PERCENT OUT OF LIMITS IAW 737 SRM 53-10-1, 51-10-6. FABRICATED REPAIR ANGLE LS980-2. DRIL LED, TRIMMED, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW 737 SRM 51-40-3. INSTALLED SUPPORT IAW 737 SRM 51-30-2. 2 L 7 2 4F A16WE 1998091800070 19980918 00070 NM 1998 9 18 VJ9800351 1 19980802 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 296 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 AFT ALV AT STA 296 BUTT LINE LBL35 ON REMOVAL OF SUPPORT ANGLE, LOWER SUPPORT U CHANNEL HAS CORROSION BEYOND LIMITS. RE MOVED LOWER CHANNEL SUPPORT IAW B 737 SRM 51-30-2. FABRICATED REPAIR SUPPORT CHANNEL IAW 737 SRM 51-40-4. TREATED AND PRIMED IAW 737 SRM 51-10-2 AND MM 51-51-51. INSTALLED REPAIR IAW 51-30-2. 2 L 7 2 4F A16WE 1998091800071 19980918 00071 NM 1998 9 18 VJ9800352 1 19980729 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 300 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 UPON REMOVAL OF FWD AFT LAV AFT WALL ATTACH ANGLE, AT BS 300, LOWER HAT SUPPORT HAS IG CORROSION. REMOVED HAT SUPPORT F OUND CORROSION BEYOND LIMTS IAW SRM 53-10-1 MADE REPAIR EXTRUDED PART OUT OF BAC-1510-335 IAW SRM 51-40-4. ALODINED IAE STM 51-10-2, PRIMED IAW MM 51-21-31, INSTALLED REPAIR IAW SRM 51-40-4. 2 L 7 2 4F A16WE 1998091800072 19980918 00072 NM 1998 9 18 VJ9800353 1 19980731 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 1006 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 AFT CARGO AREA AROUND STA 1006-1016 UNDER LT AFT LAV CORROSION BETWEEN THE FLOORBEAMS AND FLOOR BOARDS. REMOVED CORRODE D AREA STA 1006-1016 WITHIN LIMITS. REMOVED CORROSION OUT OF LIMITS AT STA 1006 IAW SRM 53-10-1 FIG 1. FABRICATED ANGL ES FROM 7075 -0 .080 IAW SRM 53-10-9 FIG 7. HEAT TREATED IAW BAC 5602. INSTALLED FLOORBEAM IAW STM 53-10-9 FIG 7. 2 L 7 2 4F A16WE 1998091800073 19980918 00073 NM 1998 9 18 VJ9800354 1 19980730 A 5320 ANGLE BOEING 737 737297 1384480 NM LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 AFT TOILET FWD WALL TIE DOWN ANGLE IS CORRODED. REMOVED CORROSION OUT OF LIMTS, MAT LOSS .045 IAW SRM 53-10-1. REMOVED BRACKET TO FABRICATE NEW ANGLE IAW SRM 51-40-3. FABBED REPAIR ANGLE (BRACKET) AND PRIMED IAW SRM 51-40-3, 51-10-2, MM 51-21-51. INSTALLED ON AIRCRAFT IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998091800074 19980918 00074 NM 1998 9 18 VJ9800355 1 19980731 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 300 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 CORROSION FOUND ON FWD LAV AFT WALL ATTACH ANGLE BS 300 LB 35. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS IAW SRM 53-1 0-1. REMOVED ATTACH ANGLE IAW SRM 51-30-2. FABRICATED REPAIR ANGLE IAW SRM 51-40-3. TREATED AND PRIMED IAW 51-10-2 AN D MM 51-21-51. INSTALLED ATTACH ANGLE TO CHANNEL IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998091800075 19980918 00075 NM 1998 9 18 VJ9800356 1 19980806 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 328 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 EXFOLIATED CORROSION ON BS 328 FLOORBEAM CAP UNDER TAPERED SHIN RBL 54. REMOVED CORROSION IAW SRM 51-10-6. MATERIAL LO SS TO BE OUT OF LIMITS. REMOVED T CHORD STA 328 LBL 15 RBL 65 IAW SRM 51-30-2 AND 53-10-9. FABRICATED REPAIR SECTION A ND REPAIR ANGLES IAW SRM 53-10-4 FIG 5. ALODINED AND PRIMED REPAIR PARTS 1A-344431-1 AND 1A-34433-1,2. INSTALLED REPAI R PARTS IAW SRM 51-10-2, MM 51-21-21, AND 51-30-2. 2 L 7 2 4F A16WE 1998091800076 19980918 00076 NM 1998 9 18 VJ9800357 1 19980804 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 326 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 EXFOLIATED CORROSION AROUND NUT PLATE ON UNDERSIDE OF CUSP ANGLE AT L-1 DOOR THRESHOLD, BS 326. REMOVED SUPPORT ANGLE A ND REMOVED CORROSION, LOSS FOUND TO BE OUT OF LIMITS IAW B737 SRM 51-10-6, AND 53-10-1. FABRICATED REPAIR ANGLE FROM LS 980-2. TRIMMED, DRILLED, DEBURRED, TREATED, AND PRIMED IAW SRM 51-40-3. INSTALLED SUPORT ANGLE IAW 51-30-2. 2 L 7 2 4F A16WE 1998091800077 19980918 00077 NM 1998 9 18 VJ9800358 1 19980804 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 312-344 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 FILLER STRIPS ON TOP SIDE OF CUSP ANGLE AT L-1 DOOR THRESHOLD CORRODED BS 312-344. REMOVED CORROSION ON THRESHOLD, FOUN D TO BE OUT OF LIMITS IAW SRM 53-10-01 AND 51-10-6. REMOVED ANGLE AND FORMED REPAIR ANGLE FROM 7075-0-.080. HEAT TREAT ED TO T6 IAW SRM 51-40-3 AND BAC5602. TRIMMED, DRILLED, DEBURRED, TREATED AND PRIMED REPAIR ANGLE IAW SRM 51-40-3. INS TALLED REPAIR IAW 737 SRM 51-30-2. 2 L 7 2 4F A16WE 1998091800078 19980918 00078 NM 1998 9 18 VJ9800359 1 19980805 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 L-1 DOOR FWD GIRT BAR ATTACH BRACKET BLOCK CORRODED ON BS 312 FLOORBEAM. REMOVED CORRODED ATTACH BRACKET IAW SRM 51-30- 1. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR ANGLE FROM 7075-0 .070 IAW SRM 51-40-3. DRILLED, TRIM MED, AND COUTER SUNK REPAIR ANGLE IAW SRM 51-30-5. TREATED AND PRIMED REPAIR ANGLE IAW SRM 51-10-2. INSTALLED REPAIR A NGLE AND ATTACH BRACKET IAW SRM 51-30-1. 2 L 7 2 4F A16WE 1998091800079 19980918 00079 NM 1998 9 18 VJ9800360 1 19980807 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 962 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 AFT CARGO STRINGER 27R AT STA 962 AT FASTENER HOLE CORRODED. MAT LOSS IN THE BASE OF STRINGER AT STA 951-967 (27R) OUT OF LIMITS IAW SRM 53-10-1. CUT OUT CORRODED SECTION STRINGER IAW SRM 53-10-3. FORMED 1 V CHANNEL AND 2 ANGLE REPAIR 70 75-0 HEAT TREATED BAC 5602. DRILLED, TRIMMED, DEBURRED, TREATED, AND PRIMED IAW 53-10-3, 51-10-2. REMOVED AND RE-INSTA LLED 2 ANGLE REPAIR, 1 V CHANNEL, 1 STRINGER FILLER IAW SRM 53-10-3 AND 53-10-4. OPS CK OK IAW MM 21-32-21. 2 L 7 2 4F A16WE 1998091800080 19980918 00080 NM 1998 9 18 VJ9800361 1 19980801 A 5320 ANGLE BOEING 737 737297 1384480 NM BS 1016 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 AFT TOILET FLOOR SUPPORT AT BL 12 L BS 1016 IS CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-30-1. REMOVED CORROSION IAW SRM 51-10-6. FOUND TO BE OUT OF LIMITS. FABRICATED ANGLE REPAIR FROM 7075-0 .100 IAW SRM 51-40-3. DRILLED, TRIMMED, A ND DEBURRED ANGLE REPAIR IAW SRM 51-30-1. PRIMED AND TREATED IAW SRM 51-10-2 AND MM 51-20-11. INSTALLED REPAIR ANGLE A T FLOOR SUPPORT IAW SRM 51-30-1. RE-INSTALLED FLOOR SUPPORT IAW SRM 51-30-1. 2 L 7 2 4F A16WE 1998091800081 19980918 00081 NM 1998 9 18 VJ9800362 1 19980728 A 5320 SUPPORT BOEING 737 737297 1384480 NM BS 1016 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 AFT TOILET UNDER FLOOR SUPPORT AT BL0 BS 1016 IS CORRODED. REMOVED CORROSION IAW SRM 51-10-2. FLOOR SUPPORT FOUND TO B E OUT OF LIMITS IAW SRM 53-10-1 AND 51-10-1. REPAIRED EXTRUDED SECTION IAW SRM 51-40-4 FROM 7075 T6 511. INSTALLED FLO OR SUPPORT REPAIR IAW SRM 51-40-4. 2 L 7 2 4F A16WE 1998091800082 19980918 00082 NM 1998 9 18 VJ9800363 1 19980807 A 5315 FLOORBEAM BOEING 737 737297 1384480 NM BS 294.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 FUSELAGE INTERIOR, FLOORBEAM AT BS 294.5 IS CORRODED ON TOP AT RBL 12. REMOVED CORROSION .024 TO .041 MATERIAL LOSS OUT OF LIMITS. GAUGE NR A-0358 IAW SRM 51-10-6 AND 53-10-1. REMOVED STIFFENERS AND UPPER CHORD FROM RL 26 TO LBL 20 NECES SARY TO INSTALL CHORD SPLICES IAW SRM 53-10-9. TRIMMED, DRILLED, DEBURRED, TREATED, AND PRIMED T CHORD AND REPAIR SPLIC ES IAW SRM 53-10-9. INSTALLED T CHORD, REPAIR SPLICES, AND STIFFENERS IAW SRM 53-10-9. 2 L 7 2 4F A16WE 1998091800083 19980918 00083 NM 1998 9 18 VJ9800364 1 19980807 A 5320 INTERCOASTAL BOEING 737 737297 1384480 NM BS 312 & 294.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 FUSELAGE INTERIOR BETWEEN BS 312 AND 294.5, INTERCOSTAL AT RBL 24 IS CORRODED ON TOP. REMOVED CORROSION OUT OF LIMITS I AW SRM 53-10-1 AND 51-10-6. REMOVED INTERCOSTAL AND FABRICATED REPAIR FROM 7075 T6 .080 17 BY 2 1/1 BY 1. DRILLED, DEB URRED, TREATED AND PRIMED IAW SRM 51-40-3. INSTALLED INTERCOASTAL IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998091800084 19980918 00084 NM 1998 9 18 VJ9800365 1 19980731 A 5313 STRINGER BOEING 737 737297 1384480 NM BS 986-1010 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 AFT CARGO STRINGER 27L FROM APPROX 986-1010 HAS NUMBEROUS SURFACE CORROSION ON THE CHANNEL AND ON LT SIDE AND ON THE BEL LY SKIN. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1 FROM 2 PLACES AT STR 27L STA 986-1006. REMOVED CORROSION WITH IN LIMITS FROM STA 947-967. TREATED AND PRIMED AREA IAW SRM 51-10-2 AND MM 51-21-31. FABRICATED 2 REPAIR STR SPLICES, TREATED, PRIMED AND INSTALLED IAW SRM 51-10-2, 51-21-31 AND SRM 53-10-3. 2 L 7 2 4F A16WE 1998091800085 19980918 00085 NM 1998 9 18 VJ9800366 1 19980727 A 5330 PANEL BOEING 737 737297 1384480 NM BS 492-520 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 FWD CARGO PTI, STA 492.4 TO 520 RT SIDE TRANSITION PANEL HAS CORROSION OVER TOP OF STRINGER 26 RT. REMOVED CORROSION OU T OF LIMITS. FABRICATED TRANSITIONS PANEL FROM 2024 T3 .040, TREATED AND PRIMED AND INSTALLED IAW SRM 51-10-2, 51-20-11 , AND 51-40-2. 2 L 7 2 4F A16WE 1998091800086 19980918 00086 NM 1998 9 18 VJ9800367 1 19980806 A 5330 SKIN BOEING 737 737297 1384480 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 462AT 22631 CORROSION ON SIDE MOUNT AREA FOR EYE BROW WINDOW NR 5. REMOVED CORROSION OUT OF LIMITS, FABRICATED REPAIR DOUBLER FROM 2024 T-3 .063 ABD STRAP REPAIR FROM 7075 T-6 .032 IAW TSR NR B737-53-009, B737 --56-002 AND DWG B737-980006. TREATED AN D PRIMED IAW SRM 51-30-1, TSR NR B737-56-002, B737-53-009, DWG 98-0006. 2 L 7 2 4F A16WE 1998091800087 19980918 00087 WP 1998 9 18 VJ9800370 1 19980719 A 5320 INTERCOASTAL DOUG DC9 DC932 3022066 WP BS 851-870 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 INTERCOSTAL STA 851-870 LONG 27L AND BUBBLED ON LONG. REMOVED INTERCOSTAL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01 F IG 1. FABBED NEW INTERCOASTAL 18 1/8 BY 5 USING 7075-0-.050 IAW DC-9 SRM 51-10-2 AND 53-11 FIG 3A. HEAT TREATED IAW SR M 51-10-2A. TREATED AND PRIMED IAW SRM 51-10-3. INSTALLED INTERCOSTAL IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998091800088 19980918 00088 WP 1998 9 18 VJ9800371 1 19980721 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 CORROSION ON INNER SKIN STA 935 UNDER LONGERON 29R. REMOVED LONGERON 29R AND INNER SKIN FOUND CORROSION OUT OF LIMITS. FABBED NEW INNER SKIN FROM 2024 - T3 .025 EXTERNAL SKIN CORROSION OUT OF LIMITS, FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106 AND INSTALLED LONNG 29R. 2 L 7 2 4F A6WE 1998091800089 19980918 00089 WP 1998 9 18 VJ9800372 1 19980721 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 935 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 CORROSION ON INNER SKIN UNDER LONGERON 28R STA 935. REMOVED LONG 28R AND INNER SKIN FOUND TO BE OUT OF LIMITS. FABBED NEW INNER SKIN 2024 T-3 .025 EXTERNAL SKIN CORROSION OUT OF LIMITS. FABBED REPAIR DOUBLER IAW AIRTRAN RES 981106. 2 L 7 2 4F A6WE 1998091800090 19980918 00090 WP 1998 9 18 VJ9800373 1 19980719 A 5320 1A350681 INTERCOASTAL DOUG DC9 DC932 3022066 WP BS 813-832 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 INTERCOASTAL STA 813-832 LONG 27L HAS CORROSION. REMOVED INTERCOASTAL AND FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1 . FABBED NEW INTERCOASTAL 18.5 BY 5 USING 7075 -0 .040 IAW DC-9 SRM 53-11-3. HEAT TREATED IAW SRM 51-10-2A. TREATED A ND PRIMED IAW SRM 51-10-3. INSTALLED INTERCOSTAL IAW DC-9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998091800091 19980918 00091 WP 1998 9 18 VJ9800374 1 19980728 A 5320 3914677501N SPLICE DOUG DC9 DC932 3022066 WP BS 794-813 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 LONGERON 30 SPLICE CORRODED OUT OF LIMITS, STA 794-813. REMOVED SPLICE IAW SRM 51-30-2, REMOVED CORROSION IAW SRM 51-1 0-3, MATERIAL LOSS .030 IAW AERO CORP GAUGE NR A-2039, OUT OF LIMITS IAW SRM 53-01 FIG 1. SPLICE P/N 3914677-501N, DRIL LED AND DEBURRED NEW SPLICE IAW SRM 51-10-4, INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998091800092 19980918 00092 WP 1998 9 18 VJ9800375 1 19980728 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 889 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 FLOOR SUPPORT DOUBLERS CORRODED UNDER STA 889-908 LONGERON 29L-27L. FABRICATED SUPPORT DOUBLER FROM 7075 T6 .063 3.5 BY 3. INSTALLED REPAIR IAW DC-9 SRM 51-10-3, 53-01 FIG 1 AND 51-30-1. 2 L 7 2 4F A6WE 1998091800093 19980918 00093 WP 1998 9 18 VJ9800376 1 19980722 A 5313 1A374411 LONGERON DOUG DC9 DC932 3022066 WP BS 935-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 912VV 47359 LONGERON 30 SPLICE CORRODED STA 935-965. REMOVED 2 SPLICE CORRODED. REMOVED 32 .125 FORMED SECTION LONGERON CORRODED, FABRICATED NEW LONGERON FROM EXTRUSION S1242886, IAW SRM 53-02 FIG 15, DRILLED, TRIMMED AND DEBURRED LONGERON AND SPLICE REPAIRS IAW DC-9 SRM 51-10-4. TREATED AND PRIMED LONGERON IAW SRM 51-10-3. INSTALLED LONGERON AND SPLICE REPAIRS IAW SRM 53-02 FIG 15. 2 L 7 2 4F A6WE 1998091800094 19980918 00094 NM 1998 9 18 K3HA980109 1 19980903 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 OVERWING EXIT LEFT SIGNS DO NOT ILUMINATE IN EMERGENCY POSITION. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD PER MM 33-50-01. 2 L 7 3 4F A3WE 1998091800095 19980918 00095 NM 1998 9 18 K3HA980110 1 19980904 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 FORWARD EXTERIOR OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK REF MM 33-50-22. OPS CHECK OK 2 L 7 3 4F A3WE 1998091800096 19980918 00096 NM 1998 9 18 CALA9801670 1 19980909 A 2910 6578444017 HYD LINE BOEING 727 727227 1384078 NM A-HYD SYST LEAKING A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 76752 21248 THE A HYDRAULIC SYSTEM WAS LOST ON FINAL APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE A SYSTEM HYDRAULIC PRESSURE LINE IN AFT AIRSTAIRS TO FIREWALL LEAKING. THE HYDRAULIC PRESSURE LINE WAS REMO VED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A3WE 1998091800097 19980918 00097 WP 1998 9 18 CALA9801671 1 19980909 A 2910 HYD LINE DOUG DC10 DC1030 3023501 WP NR 2 HYD SYST PUNCTURED A CALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 14079 46927 THE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE WAS LOST ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAI NTENANCE FOUND A HOLE IN HYDRAULIC PRESSURE LINE TO LEFT HYDRAULIC PUMP AND THE RIGHT PUMP WAS LEAKING HYDRAULIC FLUID O UT DRAIN MAST. THE HYDRAULIC LINE AND PUMP WERE REPLACED. LEAK AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998091800098 19980918 00098 NM 1998 9 18 CALA9801672 1 19980909 A 5320 MOUNT BOEING 727 727224 1384076 NM BS 312-344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FORWARD LAV FLOORBOARD MOUNT FRAME AT STA 312-344 HAD CORROSION AROUND MOUNTING HOLES. THE MOUNT FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F A3WE 1998091800099 19980918 00099 NM 1998 9 18 CALA9801673 1 19980909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1140, LBL 12. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALL ED IAW SRM 51-10-2, 51-10-1, AND 51-30-2. 2 L 7 3 4F A3WE 1998091800100 19980918 00100 NM 1998 9 18 CALA9801674 1 19980909 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1050 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOORBEAM CORRODED AT TOP FLANGE SCREW HOLE FS 1050, RBL 35. THE CORRODED AREA WAS REMOVED AND A NEW S ECTION OF FLOORBEAM WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 53-10-5, FIGURE 7. 2 L 7 3 4F A3WE 1998091800101 19980918 00101 NM 1998 9 18 CALA9801675 1 19980909 A 5320 WEB BOEING 727 727224 1384076 NM BS 1122 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WEB CORRODED AT FS 1122, RBL 65. THE CORRODED AREA WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-2, 51-10-1, PAGE 4, AND 51-30-2. 2 L 7 3 4F A3WE 1998091800102 19980918 00102 NM 1998 9 18 CALA9801676 1 19980909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1034 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 24-45. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INST ALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2. 2 L 7 3 4F A3WE 1998091800103 19980918 00103 NM 1998 9 18 CALA9801677 1 19980909 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1067 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 1067, RBL 12-24 AND RBL 45-65. THE FLOOR SUPPORTS WERE REMOVED AND A NEW SUPPORTS WERE INSTALLED IAW SRM 51-30-1AND 51-10-2. 2 L 7 3 4F A3WE 1998091800104 19980918 00104 NM 1998 9 18 CALA9801678 1 19980909 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .375 CRACK IN ANGLE AT INTERCOSTAL AT BS 950A-950B, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SR M 51-40-3, FIGURE 1 AND 51-30-2. 2 L 7 3 4F A3WE 1998091800105 19980918 00105 NM 1998 9 18 CALA9801679 1 19980909 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 22.5 TO 24.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A N EW SECTION WAS INSTALLED IAW SRM 53-10-8 AND 51-30-2. 2 L 7 3 4F A3WE 1998091800106 19980918 00106 NM 1998 9 18 CALA9801680 1 19980909 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1166, STRINGER 29R. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS INSTALLE D IAW SRM 53-10-5, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800107 19980918 00107 NM 1998 9 18 CALA9801681 1 19980909 A 5531 SPAR BOEING 727 727232 1384082 NM BS 1218 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1.5 CRACK IN BRACKET AT RT LOWER VERTICAL STABILIZER FRONT SPAR, FS 1218 AN ANGLE WAS INSTALLED IAW S RM 51-40-3, FIGURE 1 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800108 19980918 00108 NM 1998 9 18 CALA9801682 1 19980909 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBOARD SUPPORT ANGLE CORRODED AT STA 1166 IN AFT PIT, LT SIDE. THE CORRODED SECTION OF SUPPORT ANG LE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-10-5, FIGURE 6, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800109 19980918 00109 NM 1998 9 18 CALA9801683 1 19980910 A 5512 SKIN BOEING 727 727232 1384082 NM LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 2.5 CRACK IN LT HORIZONTAL STABILIZER UPPER AFT TRAILING EDGE SKIN AT HS STA 195. A DOUBLER WAS INST ALLED IAW SRM 51-20-1, 51-40-5, 51-30, AND 51-20-4. 2 L 7 3 4F A3WE 1998091800110 19980918 00110 WP 1998 9 18 CALA9801684 1 19980909 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 370 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 370 BETWEEN LONGERON 27L AND 28L. A REPAIR WAS INSTALLED IAW SRM 53-04, FI GURE 38, SHEET 22. 2 L 7 2 4F A6WE 1998091800111 19980918 00111 WP 1998 9 18 CALA9801685 1 19980909 A 5320 HAT CHANNEL DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 3 CRACK IN HAT CHANNEL AT FLOORBOARD PANEL, LT SIDE, STA 756. A NEW HAT CHANNEL SECTION WAS INSTALLE D IAW SRM 53-05, PAGE 1 AND 51-30-2. 2 L 7 2 4F A6WE 1998091800112 19980918 00112 WP 1998 9 18 CALA9801686 1 19980909 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 917 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND SUPPORT BRACKET CORRODED AT STA 917, STRINGER 28L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10- 3, 51-10-4, AND 51-30-1. 2 L 7 2 4F A6WE 1998091800113 19980918 00113 NM 1998 9 18 CALA9801687 1 19980910 A 5720 BEAM BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A .375 INCH CRACK IN RT WING J BEAM FORWARD OF SPOILER NR 8 ACTUATOR MOUNT FITTING. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-07914. 2 L 7 3 4F A3WE 1998091800114 19980918 00114 NM 1998 9 18 CALA9801688 1 19980910 A 5330 SKIN BOEING 727 727232 1384082 NM R-1 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A 1.9 CRACK IN R-1 DOOR LOWER AFT CUTOUT. A DOUBLER WAS INSTALLED IAW SRM 51-30-21, 51-10-2, 51-40-5, AND ECRA 5307-01141, FIGURE 4. 2 L 7 3 4F A3WE 1998091800115 19980918 00115 WP 1998 9 18 CALA9801689 1 19980910 A 3230 49516351 SPRING DOUG DC9 DC981 3022081 WP NLG BROKEN A CALA K NONE O OTHER AP APPROACH 1 SW 09 13881 48045 A LOUD SNAP SOUND WAS HEARD COMING FROM NOSE GEAR AREA WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. ALL THREE GREEN GEAR LIGHTS CAME ON AND THE GEAR DOOR OPEN LIGHT WAS EXTINGUISHED. THE AIRCRAFT LANDED SAFELY WITH GEAR WORKING NORMALLY AND THE AIRCRAFT TAXIIED TO THE GATE. MAINTENANCE FOUND THE RT UPPER LOCK LINK EXTENSION SPRING FOR NLG BROKEN. THE SPRIN G WAS REMOVED AND REPLACED. THE GEAR WAS SWUNG AND OPERATION CHECKED GOOD IAW MM 32-21-03. 2 L 7 2 4F A6WE 1998091800116 19980918 00116 NM 1998 9 18 CALA9801690 1 19980910 A 5753 651920216 CARRIAGE BOEING 727 727224 1384076 NM NR 7 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND NR 7 FLAP OUTBOARD FLAP INBOARD CARRIAGE CORRODED. THE FLAP CARRIAGE WAS REMOVED AND REPLACED IAW MM 5 7-53-2. 2 L 7 3 4F A3WE 1998091800117 19980918 00117 NM 1998 9 18 CALA9801691 1 19980910 A 5522 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT ELEVATOR SKIN LOWER SURFACE CORRODED. THE CORRODED AREA WAS CUT OUT AND A NEW FITTING AND DOUBLER W ERE INSTALLED IAW SRM 55-20-3, FIGURE 2, PAGE 2, 51-10-2, AND 51-40-5. 2 L 7 3 4F A3WE 1998091800118 19980918 00118 NM 1998 9 18 CALA9801692 1 19980910 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1034 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 1034, RBL 45-65. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INST ALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800119 19980918 00119 NM 1998 9 18 CALA9801693 1 19980910 A 5320 HAT CHANNEL BOEING 727 727224 1384076 NM BS 1150 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND HAT CHANNEL CORRODED AT FS 1150, LBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED I AW SRM 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998091800120 19980918 00120 NM 1998 9 18 CALA9801694 1 19980910 A 2752 BRACKET BOEING 727 727224 1384076 NM NR 5 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .5 INCH CRACK IN OUTBOARD BRACKET WHERE RT WING NR 5 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998091800121 19980918 00121 NM 1998 9 18 CALA9801695 1 19980910 A 5753 TRACK BOEING 727 727224 1384076 NM NR 8 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WING NR 8 FLAP TRACK FORWARD ATTACH LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-00. 2 L 7 3 4F A3WE 1998091800122 19980918 00122 NM 1998 9 18 CALA9801696 1 19980910 A 5320 BRACKET BOEING 727 727232 1384082 NM C2 DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND C2 DOOR FRAME AFT SIDEWALL ATTACH BRACKET CORRODED WITH A .25 INCH CRACK AT RIVET. A REPAIR WAS INSTAL LED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800123 19980918 00123 NM 1998 9 18 CALA9801697 1 19980910 A 5730 SKIN BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 CRACK IN LEADING EDGE SKIN AT LT WING NR 3 SLAT TRACK. THE CRACK WAS STOP DRILLED. A REPAIR WAS I NSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800124 19980918 00124 1998 9 18 CALA9801698 2 19980910 A 7510 DUCT DOUG DC9 DC982 3022082 WP NR 2 ENGINE RUPTURED A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 72822 49482 THE RT FIRE DETECTOR LOOP LIGHT ILLUMINATED, FOLLOWED BY THE RT FIRE WARNING LIGHT AND BELL WHILE EN ROUTE FROM IAH TO C LE. THE RIGHT ENGINE POWER WAS REDUCED AND THE FIRE WARNINGS CEASED. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ANTI-ICE DUCT ON TOP OF NR 2 ENGINE RUPTURED. THE ANTI-ICE DUCT WAS REMOVED AN D REPLACED. IN ADDITION, THE NR 2 ENGINE UPPER COWLING WAS REMOVED AND REPLACED DUE TO HEAT DAMAGE CAUSED BY RUPTURE OF THE ANTI-ICE DUCT. LEAK CHECKS WERE GOOD AND A FIRE DETECTION TEST WAS NORMAL. 2 L 7 2 4F A6WE 1998091800125 19980918 00125 1998 9 18 COMA9810189 4 19980909 A 3421 CONNECTOR EMB 120 EMB120RT SO COCKPIT LOOSE A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 168CA 120168 EAD1 AND EHS1 TUBES FAILED DURING TAKEOFF. REPAIRED LOOSE WIRE CONNECTION AT CIRCUIT BREAKER CB0256. 2 L 7 2 4T RT A31SO 1998091800126 19980918 00126 SO 1998 9 18 COMA9810190 1 19980906 A 3080 DEICE INDICATION EMB 120 EMB120RT SO RT COCKPIT MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 168CA 120168 ABNORMAL DEICE, F/O FCP AND FO EFIS TUBE INDICATIONS DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNE D TO SERVICE. 2 L 7 2 4T RT A31SO 1998091800127 19980918 00127 EA 1998 9 18 COMA9860256 1 19980908 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 716CA 280 7250 FLAPS FAILED WHEN SELECTED FOR LANDING. COULD NOT DUPLICATE DISCREPANCY, FLAP SYSTEM CHECKS SATISFACTORY. NEXT FLIGHT FLAPS FAILED AGAIN. REPLACED THE LEFT BPSU. 2 L 7 2 4F RT A21EA 1998091800128 19980918 00128 NM 1998 9 18 UPS98227657 1 19980909 A 3350 BATTERIES BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 948UP 19357 EMER EXIT LIGHT BY MAIN CABIN DOOR INOP. REMOVED AND REPLACED EMER EXIT BATTERIES AT MAIN CABIN DOOR, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1998091800129 19980918 00129 WP 1998 9 18 UPS98827653 1 19980828 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 297.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C LT WING L/E RIB AT W/S XFS 297.5 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998091800130 19980918 00130 WP 1998 9 18 UPS98827654 1 19980827 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 76 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C RT WING UPPER SKIN CRACKED AT STA 76 STR 10 AFT ROW OF FASTENERS. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998091800131 19980918 00131 WP 1998 9 18 UPS98827655 1 19980826 A 5330 SKIN DOUG DC8 DC871F 302199D WP CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C THE FUSELAGE SKIN IS CRACKED AT THE UPPER FWD CORNER OF THE D PIT DOOR CUTOUT. REPAIRED IAW SRM 53-2- 0. 2 L 7 4 4F RT 4A25 1998091800132 19980918 00132 WP 1998 9 18 UPS98827656 1 19980827 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 360-385 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C RT WING L/E UPPER SURFACE CRACKED IN 2 PLACES FWD OF TE XFS 360.25 AND 385.25. REPAIRED IAW SRM 57-2- 1. 2 L 7 4 4F RT 4A25 1998091800133 19980918 00133 WP 1998 9 18 UPS98827658 1 19980829 A 5320 37558401 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1160 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C SHEAR TIE LWR FLANGE LWR SURFACE HAS MODERATE CORROSION F/S 1160 L-34R TO L-33R. REMOVED AND REPLACED FITTING IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998091800134 19980918 00134 WP 1998 9 18 UPS98827659 1 19980831 A 5320 37592581N SPLICE DOUG DC8 DC871F 302199D WP BS 1260-1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C STRINGER SPLICE FITTING CRACKED FS 1260-1280 L-35L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998091800135 19980918 00135 WP 1998 9 18 UPS98827660 1 19980828 A 5720 97532935 ANGLE DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C RT WING I/B SLOT O/B VERTICAL ANGLE CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND DWG 9753293. 2 L 7 4 4F RT 4A25 1998091800136 19980918 00136 NM 1998 9 18 UPS98227661 1 19980908 A 5347 SEAT TRACK BOEING 727 727247 138408F NM BS 514 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:C SEAT TRACK CRACKED BS 514 AND ELONGATED TEETH AT BS 526, RBL 25 WL 208. REPLACED SEAT TRACK BS 480 TO 530 PER SRM 53-10-5. 2 L 7 3 4F A3WE 1998091800137 19980918 00137 NM 1998 9 18 UPS98227662 1 19980907 A 5320 WEB BOEING 727 727247 138408F NM BS 720-725 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE:C WHILE WORKING TC NO CL2-224-03 DISCOVERED CORROSION AT BS 720E TO 725F LBL 65-70 WL 208. REMOVED, FAB RICATED AND INSTALLED NEW SHEAR WEB IAW SRM 51-20-01, 51-30-05, 51-30-07, MM 51-20-151. 2 L 7 3 4F A3WE 1998091800138 19980918 00138 WP 1998 9 18 UPS98827663 1 19980828 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 314-310 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C RT WING L/E LWR SKIN CRACKED 2 PLCS XFS 304-310 7 FWD OF TE AND 5 FWD OF T/E. REPAIRED IAW DC8-5720-4 087-B. 2 L 7 4 4F RT 4A25 1998091800139 19980918 00139 WP 1998 9 18 UPS98827664 1 19980910 A 3350 BATTERY DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 EMER LIGHTS DISARM CHECK INOP REF 120346 HISTORY. REMOVED AND REPLACED BATTERY PACK, OPS CK GOOD. 2 L 7 4 4F RT 4A25 1998091800140 19980918 00140 NE 1998 9 18 QXEA9801274 2 19980907 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 1 FAILED A QXEA E ENGINE SHUTDOWN J WARNING INDICATION UK UNKNOWN 1 NM 09 821PH 25456 3584 104 PCE120141 BOI- NR 1 ENGINE INDICATED OIL PRESSURE WAS BELOW 40 PSI. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. AWAITING TEARDOWN RESULTS OF ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998091800141 19980918 00141 NM 1998 9 18 98FDEA00551 1 19980909 A 5311 65163517 FRAME BOEING 727 727247 138408F NM BS 424 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 CORROSION (C53-224-03-1/2) ON E & E BAY DOOR CUTOUT FWD FRAME. *S/D* REMOVED AND REPLACED E & E BAY DOOR CUTOUT FWD F RAME PER FED-EX SRM 51-30-2 AND FED-EX DRAWING 65-16351. 2 L 7 3 4F A3WE 1998091800142 19980918 00142 NM 1998 9 18 98FDEA00552 1 19980909 A 5311 65168431 FRAME BOEING 727 727247 138408F NM BS 1050 GOUGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 DAMAGE TO THE TOP FLANGE OF THE BS 1050 FRAME AT LBL 20, WL 151. *S/D* REPAIRED DAMAGE TO THE TOP FLANGE OF THE BS 10 50 FRAME AT LBL 20, WL 151 IAW FED-EX SRM 53-10-1. 2 L 7 3 4F A3WE 1998091800143 19980918 00143 NM 1998 9 18 98FDEA00553 1 19980909 A 5313 651622040 STRINGER BOEING 727 727247 138408F NM BS 484 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 CORROSION ON STRINGER NR 27 RT, BS 484 FWD CARGO BAY. 2 L 7 3 4F A3WE 1998091800144 19980918 00144 NM 1998 9 18 98FDEA00554 1 19980909 A 5330 6572702 SKIN BOEING 727 727247 138408F NM BS 351 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 NR 0480, CRACK IN SKIN AT 351, LBL 22, WL 140 CIRCLED IN RED. REPAIRED CRACK IN SKIN AT BSA 351, LBL 22, WL 140 CIRCLED IN RED PER FEDEX SRM 51-10-1 AND PER 53-30-2. POURED LEVEL COMPOUND OVER INTERVAL PORTION OF FASTENERS PER FEDEX M/M 2 0-60-1. 2 L 7 3 4F A3WE 1998091800145 19980918 00145 NM 1998 9 18 98FDEA00555 1 19980909 A 5311 651916017 FRAME BOEING 727 727247 138408F NM BS 420 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 WHILE WORKING NR 0164, FOUND CORROSION ON BS 420 FRAME LBL 15 - RBL 15, WL 135-133. *S/D* REPAIRED FRAME AT BS 420, LB L 15-RBL 15, WL 135-133 PER FED-EX SRM 51-40-3. 2 L 7 3 4F A3WE 1998091800146 19980918 00146 NM 1998 9 18 98FDEA00556 1 19980909 A 5330 SKIN BOEING 727 72722 1384002 NM BS 886 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 NR 0342 - UPPER LOBE BS 886 HEAVY CORROSION AT WINDOW BELT AND ON SKIN 8 ABOVE STR 14L. REMOVED CORROSION FRAME WAS TAK EN OUT OF LIMITS. WINDOW FRAME REPLACED FOR EA 7-5330-29636 AND SRM 51-30-2 DOUBLER INSTALL PER EA 7-5330-29636. 2 L 7 3 4F A3WE 1998091800147 19980918 00147 NM 1998 9 18 98FDEA00557 1 19980909 A 5330 SKIN BOEING 727 72722 1384002 NM BS 360 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 NR 0698 - LFEC IND 10 PERCENT MATERIAL LOSS JUST ABOVE STR 23 LT, 2 AFT OF BS 360 FRAME. DAMAGED AREA, REMOVED AND REPL ACED DOUBLER INSTALLED PER SRM 53-30-3 PG 14B-14D. 2 L 7 3 4F A3WE 1998091800148 19980918 00148 NM 1998 9 18 98FDEA00558 1 19980909 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1010 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 0811 - CORROSION ON FLOORBEAM LWR FLANGE SEEN FROM LWR AFT CARGO BS 1010, RBL 45 TO LBL 45. CUT OUT CORROSION REMOVE D BEYOND LIMITS AT LBL 12 AND LBL 20 TO LBL 45. INSTALLED DOUBLER REPAIR PER SRM 53-10-8 PG 44 THROUGH PG 48. 2 L 7 3 4F RT A3WE 1998091800149 19980918 00149 NM 1998 9 18 98FDEA00559 1 19980909 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 NR 0936 - UPPER LOBE, FLOORBEAM BS 680 CORROSION ON UPPER FLANGE LBL 10- RBL 6. CORROSION REMOVAL OUT OF LIMITS AT LBL 5 FWD SIDE OF FLANGE. INSTALLED ANGLE DOUBLER PER AARD 53-10-07-2. 2 L 7 3 4F A3WE 1998091800150 19980918 00150 NM 1998 9 18 98FDEA00560 1 19980909 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 560 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 1119 - DAMAGE TO FLOORBEAM OVERSIZED HOLES NOT IN USE AT BS 560 BLO. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1,2,3 A ND FIG 1. 2 L 7 3 4F RT A3WE 1998091800151 19980918 00151 NM 1998 9 18 98FDEA00561 1 19980909 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 580 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 1120, OVERSIZED HOLES NOT IN USE IN FLOORBEAM AT BS 580 BLO. INSTALLED REPAIR PER AARD 53-10-07-2 PG 1,2,3 AND FIG 1 . 2 L 7 3 4F RT A3WE 1998091800152 19980918 00152 NM 1998 9 18 98FDEA00562 1 19980909 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 0380, UPPER LUBE CORROSION FLOORBEAM BS 620, BL O TO RBL 25. REPAIRED FLOORBEAM PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 1998091800153 19980918 00153 NM 1998 9 18 98FDEA00563 1 19980910 A 5320 651627910 CHORD BOEING 727 727247 138408F NM BS 760-850 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 CORROSION LUMINATING FROM UNDER SEAT TRACK AT BS 760 TO 850, LBL 25, WL 208. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM UPPER CHORD, BS 760 TO 850, LBL 25, WL 208 IAW DWG 65-16279 AND FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800154 19980918 00154 WP 1998 9 18 98FDEA00564 1 19980909 A 5320 FRAME DOUG DC10 DC1030 3023501 WP CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 CENTER CARGO COMPARTMENT, DOOR CUTOUT AFT EDGE LOWER CORNER FOUND WITH CUT/CRACK (ADJACENT TO COMPARTMENT FLOOR LEVEL). OPENED UP AREA, FOUND ADDITIONAL DAMAGE. REQUEST ENGINEERING EVALUATION. *S/D* CARRIED OUT REPAIR AS PER EA 8-5310-4 0362 AND SRM 53-50-00 FIG 9 VOL 1. 2 L 7 3 4F A22WE 1998091800155 19980918 00155 NM 1998 9 18 98FDEA00565 1 19980908 A 2612 224W9726517 FIRE LOOP DOUG MD11 MD11F 3023600 NM NR 2 FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 25 617FE 48748 98-219 - FIRE DET 2 FAIL ILLUM ON T/O B LOOP WAS PLACARD INOP FOR DISPATCH. REMOVED AND REPLACED A LOOP HARNESS 224W972 6-517. REMOVED AND REPLACED UPPER LT DET ASSY P/N 224-9743-509, SYS, OPS CHECK GOOD. 2 L 7 3 4F RT A22WE 1998091800156 19980918 00156 WP 1998 9 18 98FDEA00566 1 19980910 A 5753 GUIDE VANE DOUG DC10 DC1010 3022110 WP RT TE FLAP MISSING A FDEA O OTHER D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 397FE 46631 98-220, RT INBD FLAP OUTBD FLAP GUIDE VANE STOP MISSING. INSTALL GUIDE VANE STOP AND ADJUST PER M/M 27-50-03-2 PG 205. CK FLAP (INBD) FOR DAMAGE NONE NOTED. RETURN TO SERVICE. 2 L 7 3 4F A22WE 1998091800157 19980918 00157 EU 1998 9 18 98FDEA00567 1 19980910 A 2410 CSD AIRBUS 310 A310* EU LT ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 417FE 333 DURING CRUISE, IDG OIL OUTLET FLASHING ADVISORY CAME ON NR 2 DISCONN START TEMP AROUND 135 DEG CELSIUS. AIR/OIL COOLER INOP. SECURE OPEN RAN ENG AT 85 PERCENT N1 TEMP AT 48C, DEFERRED OIL COOLER VALVE PER MEL 75-1B. *S/D* REMOVED AND RE PLACED AIR/OIL HEAT EXCHANGE VALVE, LT CSD FUEL/OIL COOLER, IDG PER MM 24-11-24, 24-11-26, 24-11-11. LEAK CHECK GOOD. 2 L 7 2 4F RT A35EU 1998091800158 19980918 00158 WP 1998 9 18 ABXA9800818 1 19980908 A 5250 AR25291GR41 LATCH DOUG DC9 DC931 3022065 WP COCKPIT BINDING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 941AX 47419 COCKPIT DOOR LATCHING MECHANISM BINDING AND STICKS IN CLOSED POSITION. DISASSEMBLED, CLEANED, LUBRICATED AND REASSEMBL ED LATCH ASSEMBLY. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998091800159 19980918 00159 WP 1998 9 18 MWEA98958 1 19980909 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP GALLEY DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 302ME 47102 THE GALLEY SLIDE COVER FELL OFF. MAINTENANCE REINSTALLED GALLEY SLIDE. 2 L 7 2 4F A6WE 1998091800160 19980918 00160 WP 1998 9 18 MWEA98959 1 19980910 A 3350 6011777 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 THE LEFT NACELLE EMERGENCY LIGHT FOUND INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK FOR LEFT NACELLE EMERGENCY L IGHT. 2 L 7 2 4F A6WE 1998091800161 19980918 00161 NM 1998 9 18 DHL98712004 1 19980829 A 5330 SKIN BOEING 727 72729 1384007 NM BS 1343 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 RIVETS WORKING AND SKIN WAVING AT BS 1343 RT AT WL 259.5 ABOVE NR 2 ENGINE COWL DOOR. CUT OUT DAMAGED SECTION OF SKIN, INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 5 X 7. N/R 6681. 2 L 7 3 4F A3WE 1998091800162 19980918 00162 NM 1998 9 18 DHL98712005 1 19980830 A 5330 SKIN BOEING 727 72729 1384007 NM BS 269 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 DENT OF FUSELAGE SKIN STA 269 AT S-24 LT. CUT OUT DAMAGED SKIN PER SRM 51-30-2. INSTALLED DOUBLER REPAIR PER SRM 53-30 -3, 12 X 12. N/R 6690. 2 L 7 3 4F A3WE 1998091800163 19980918 00163 NM 1998 9 18 DHL98712006 1 19980829 A 5280 WEB BOEING 727 72729 1384007 NM NLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 712DH 19401 CRACKS AT CUTOUT ABOVE FWD HINGE LEFT OF NOSE GEAR DOOR. REMOVED DAMAGED WEB PER SRM 51-30-2. REPLACED WEB PER SRM 51- 10-1, 8 X 12. N/R 6672. 2 L 7 3 4F A3WE 1998091800164 19980918 00164 WP 1998 9 18 ARWA980906 1 19980911 A 2761 ACTUATOR DOUG DC8 DC862 3021970 WP SPOILER DIRTY A ARWA O OTHER J WARNING INDICATION LD LANDING 1 SO 19 791AL 46150 NO SPOILER DEPLOYMENT WITH REAR WHEELS SPIN UP. SPOILER HANDLE STIFF TO ACTUATE. FOUND BELL CRANK AND SPOILER HYD. AC TUATOR HAD EXCESSIVE BUILD-UP OF ANTI-CORROSION PAINT. REMOVED BUILD UP AND LUBE CRANK. SPOILER SYSTEM, OPS CHECKED GO OD IAW DC-8 M/M 27-60-0. AUTO SPOILERS OPS CHECKED GOOD IAW DC-8, M/M 27-60-2. 2 L 7 4 4F 4A25 1998091800165 19980918 00165 NM 1998 9 18 VNAA9809005 1 19980903 A 2750 1050A000003 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE TE FLAPS MALFUNCTIONED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 424JS 63186 35228 3033 WHILE AWAITING CLEARANCE FOR TAKEOFF, A FLAP CONTROL FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GAT E. OUTSTATION MAINTENANCE PERFORMED A RE-RACK OF THE FLAP CONTROL UNIT AND COMPLIED WITH OPERATIONAL CHECKS, IN ACCORDA NCE WITH DORNIER MAINTENANCE MANUAL 27-52-00. THE OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED T O SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091800166 19980918 00166 NM 1998 9 18 VNAA9809006 1 19980908 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE BIRD STRIKE A VNAA K NONE C F.O.D. CR CRUISE 1 GL 07 430JS 3044 EN ROUTE TO TRI, THE AIRCRAFT ENCOUNTERED A BIRD STRIKE, BELOW THE AREA OF THE FIRST OFFICERS WINDOW. THE FLIGHT CONTIN UED TO TRI AND LANDED WITHOUT FURTHER INCIDENT. OUTSTATION MAINTENANCE INSPECTED THE AIRCRAFT FOR DAMAGE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-57-07. NO DAMAGE WAS NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091800167 19980918 00167 NM 1998 9 18 CKSA98510 1 19980813 A 5230 SKIN BOEING 747 7472B4B 138481B NM CARGO DOOR DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 710CK 21097 ON T/S CHECK, FOUND LOWER AFT CORNER OF AFT BELLY CARGO DOOR DAMAGED. REPAIRED PER 747 SRM 52-00-03 FIG 3. 2 L 7 4 4F RT A20WE 1998091800168 19980918 00168 1998 9 18 CKSA98512 4 19980905 A 2565 D30170555 SLIDE LKHEED 1011 1011385115 5265015 WP L1 DOOR DEPLOYED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 109CK 193N1205 UPON ARRIVAL AT A/C, FOUND L1 DOOR SLIDE LYING ON TOP OF AIRSTAIRS. DOOR OPENED INCORRECTLY BY OGDEN CATERING. REMOVED AND REPLACED L1 DOOR SLIDE ASSEMBLY IAW L1011 MM CHAPTER 25-61-01, OPS CHECK NORMAL IAW SAME. 2 L 7 3 4F A23WE 1998091800169 19980918 00169 WP 1998 9 18 CKSA98513 1 19980729 A 3350 BATTERY LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A CKSA K NONE L NO TEST IN INSP/MAINT 1 GL 23 109CK 193N1205 EMERGENCY EXIT LIGHT AT R2 PAX DOOR, BATTERY HAS NO CHARGE. INSTALLED BATTERY IAW CHAPTER 35. 2 L 7 3 4F A23WE 1998091800328 19980918 00328 SO 1998 9 18 SWIA971247 1 19980804 A 2722 3081401003 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RUDDER FAILED A A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 218SW 120287 AFTER DEPARTURE RIGHT RUDDER PEDALS REFUSED FURTHER MOVEMENT BEYOND NEUTRAL POSITION. RETURNED FOR LANDING. REPLACED G REEN SYSTEM RUDDER ACTUATOR IAW MM 27. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998091800329 19980918 00329 SO 1998 9 18 SWIA971248 1 19980909 A 2913 PUMP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 07 205SW 120260 GREEN HYDRAULIC SYSTEM LOSS OF FLUID WITH SUBSEQUENT LOW PRESSURE INDICATION. REMOVED AND REPLACED LEFT ENGINE HYDRAULI C PUMP. RAN ENGINE AND SYSTEM OPS CHECKS GOOD. SERVICED GREEN SYSTEM. 2 L 7 2 4T 4 T RT A31SO E20NE 1998091800330 19980918 00330 SO 1998 9 18 SWIA971249 1 19980808 A 3260 RELAY EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 NM 07 205SW 120260 INBOUND ANTISKID LIGHT ILLUMINATED JUST AFTER GEAR WAS SELECTED DOWN. THIS OCCURED ON APPROACH TO OXR WHICH HAS A RUNWA Y THAT IS TOO SHORT, SO RETURNED TO LAX. REMOVED AND REPLACED K0021 AND K0255 LANDING GEAR POSITION RELAYS WITH SERVICE ABLE UNITS. PERFORMED LANDING GEAR RETRACTION TESTS MULTIPLE TIMES. OPS CHECKS GOOD WITH NO DISCREPANCIES NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998091800331 19980918 00331 SO 1998 9 18 SWIA971250 1 19980809 A 3233 1959500007 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 RIGHT MAIN GEAR INTRANSIT LIGHT (A & B SYSTEMS) ON. TOWER REPORTED RIGHT MAIN DID NOT RETRACT. COULD HEAR HYDRAULIC CY CLING IN NOSE. RETURNED TO FAT. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR IAW MM 32-32-10. GEAR SWING SAT ISFACTORY. 2 L 7 2 4T 4 T RT A31SO E20NE 1998091800332 19980918 00332 NM 1998 9 18 P5CA9801391 1 19980804 A 5320 CLIP BOEING 747 747122 1384872 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND ON TIE CLIP BS 1580, STR 3L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 53-1 0-02. 2 L 7 4 4F A20WE 1998091800333 19980918 00333 NM 1998 9 18 P5CA9801392 1 19980804 A 5320 SHEAR TIE BOEING 747 747122 1384872 NM BS 1580 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND MAIN DECK BS 1580 SHEAR TIE AFT FACE, BETWEEN S4R AND S7R. CORROSION REMOVED AND AREA REPROTE CTED AS PER SRM 51-10-01, 53-10-01, 51-10-02. 2 L 7 4 4F A20WE 1998091800334 19980918 00334 NM 1998 9 18 P5CA9801393 1 19980804 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1625 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND BS 1625 STRINGER 2L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02, AN D 53-10-01. 2 L 7 4 4F A20WE 1998091800335 19980918 00335 NM 1998 9 18 P5CA9801394 1 19980804 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT LAP JOINT AREA OF STR 12R, BS 1620-1640. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 53-30-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998091800336 19980918 00336 NM 1998 9 18 P5CA9801395 1 19980804 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1620 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT BS 1620 STR 1R. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND M M 51-24-11. 2 L 7 4 4F A20WE 1998091800337 19980918 00337 NM 1998 9 18 P5CA9801396 1 19980804 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT MAIN DECK BS 1740-1820 STR 4R LAP JOINT. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND 53-30-01. 2 L 7 4 4F A20WE 1998091800338 19980918 00338 NM 1998 9 18 P5CA9801397 1 19980801 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1960-2180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON STRINGER 19R FROM BS 1960-2180 AT LAP JOINT AREA. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02, 51-24-11. 2 L 7 4 4F A20WE 1998091800339 19980918 00339 NM 1998 9 18 P5CA9801398 1 19980805 A 5313 LONGERON BOEING 747 747122 1384872 NM BS 1580 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 MAIN DECK BS 1580 STR 5L FOUND CRACKED. REPAIRED AS PER SRM 53-10-03 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800340 19980918 00340 NM 1998 9 18 P5CA9801399 1 19980805 A 5313 LONGERON BOEING 747 747122 1384872 NM BS 1495 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 MAIN DECK BS 1495 STR 2L FOUND CRACKED. REPAIRED AS PER SRM 53-10-03 FIGURE 5. 2 L 7 4 4F A20WE 1998091800341 19980918 00341 NM 1998 9 18 P5CA9801400 1 19980805 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT MAIN DECK BS 1520 SKIN, STRINGER 19L. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51 -10-01, 51-10-02 AND 53-40-01. 2 L 7 4 4F A20WE 1998091800342 19980918 00342 NM 1998 9 18 P5CA9801401 1 19980803 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1580 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 MAIN DECK BS 1580 STRINGER 5R CRACK FOUND. REPAIRED PER SRM 53-10-03. 2 L 7 4 4F A20WE 1998091800343 19980918 00343 NM 1998 9 18 P5CA9801402 1 19980803 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1650 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON MAIN DECK BS 1650 12L LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 53-30-01, 52-10-0 1, 53-10-02. 2 L 7 4 4F A20WE 1998091800344 19980918 00344 NM 1998 9 18 P5CA9801403 1 19980803 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1960-2180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT STRINGER 12R FROM STA 1960 TO 1280 RIGHT LAP JOINT. CORROSION REMOVED AND REPROTECTED AREA P ER SRM 51-10-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800345 19980918 00345 NM 1998 9 18 P5CA9801404 1 19980805 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1725 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT MAIN DECK BS 1725 STR 12L LAP JOINT AREA. CORROSION REMOVED AND AREA REPROTECTED AS PER SR M 51-10-01, 51-10-02, 53-30-01 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800346 19980918 00346 NM 1998 9 18 P5CA9801405 1 19980805 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2200-2280 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT MAIN DECK CROWN BS 2200-2280 STR 4R LAP JOINT AREA. CORROSION REMOVED AND AREA REPROTECTED AS PER SRM 51-10-01, 51-10-02 AND 53-30-01. 2 L 7 4 4F A20WE 1998091800347 19980918 00347 NM 1998 9 18 P5CA9801406 1 19980803 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1940-1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT MAIN DECK CROWN BS 1940-1960 STR 4R LAP JOINT SEALANT AREA. REMOVED CORROSION AND REPROTECTE D. 2 L 7 4 4F A20WE 1998091800348 19980918 00348 NM 1998 9 18 P5CA9801407 1 19980805 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 UPPER DECK BS 380-390 STR 7R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998091800349 19980918 00349 NM 1998 9 18 P5CA9801408 1 19980805 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 380 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 UPPER DECK BS 380-390 S5R-6R INTERCOSTAL FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998091800350 19980918 00350 NM 1998 9 18 P5CA9801409 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 545-560 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION AND CRACK FOUND AT UPPER DECK RBL 23 SEAT TRACK OUTBOARD FLANGE, BS 545-560. CORROSION REMOVED, ARE A REPAIRED AND REPROTECTED AS PER SRM 51-10-01, 51-10-02, AND 53-10-01. 2 L 7 4 4F A20WE 1998091800351 19980918 00351 NM 1998 9 18 P5CA9801410 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK, BS 600-700, WL 300. CORROSION REMOVED AND AREA REPAIRED AS PER S RM 51-10-01, 51-10-02, 53-10-01, AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800352 19980918 00352 NM 1998 9 18 P5CA9801411 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT CROWN AREA OF UPPER DECK LT SEAT TRACK, BS 600-700, WL 300. CORROSION REMOVED AND AREA REP AIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-01. 2 L 7 4 4F A20WE 1998091800353 19980918 00353 NM 1998 9 18 P5CA9801412 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSIN FOUND AT UPPER DECK RT SEAT TRACK, BS 600-710, WL 300, RBL 64. CORROSION REMOVED AND AREA REPAIRED A S PER SRM 51-10-01, 51-10-02 AND 53-10-01. 2 L 7 4 4F A20WE 1998091800354 19980918 00354 NM 1998 9 18 P5CA9801413 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT UPPER DECK RT SEAT TRACK, BS 600-700, WL 300, BL R27. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-05. 2 L 7 4 4F A20WE 1998091800355 19980918 00355 NM 1998 9 18 P5CA9801414 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK CROWN SURFACE, BS 600-710, WL 300. CORROSION REMOVED AND SEAT TRA CK REPLACED AS PER SRM 51-10-01, 53-10-01, 53-10-05 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800356 19980918 00356 NM 1998 9 18 P5CA9801415 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT UPPER DECK LT SEAT TRACK CROWN AREA, BS 600-710, WL 300, LBL 46. CORROSION REMOVED AND ARE A REPAIRED AS PER SRM 51-10-01, 51-10-02 AND 53-10-05. 2 L 7 4 4F A20WE 1998091800357 19980918 00357 NM 1998 9 18 P5CA9801416 1 19980803 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2120 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS 2120 STR 2L. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND 51-24-11. 2 L 7 4 4F A20WE 1998091800358 19980918 00358 NM 1998 9 18 P5CA9801417 1 19980805 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 600 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL ONE CORROSION FOUND AT UPPER DECK RT SEAT TRACK, BS 600-710, WL 300, BL R46. CORROSION REMOVED AND AREA REPAIRED AS PER SRM 51-10-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800359 19980918 00359 NM 1998 9 18 P5CA9801418 1 19980803 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2080-2160 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON MAIN DECK BS 2080-2160 STR 4L LAP JOINT AREA. REMOVED CORROSION AND REPROTECTED PER SRM 51-1 0-01, 51-10-02, 53-30-01. 2 L 7 4 4F A20WE 1998091800360 19980918 00360 NM 1998 9 18 P5CA9801419 1 19980803 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2258 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION ON MAIN DECK CROWN SKIN BS 2258 S2R. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800361 19980918 00361 NM 1998 9 18 P5CA9801420 1 19980803 A 5330 SKIN BOEING 747 747122 1384872 NM BS 2180-2200 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND ON MAIN DECK CROWN BS 2180-2200 STR 12R LAP JOINT. REMOVED CORROSION AND REPROTECTED PER SRM 51 -10-01, 51-10-02 AND 53-30-01. 2 L 7 4 4F A20WE 1998091800362 19980918 00362 NM 1998 9 18 P5CA9801421 1 19980803 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1960-2180 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND FROM BS 1960-2180 STRINGER 19L LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 5 1-10-02 AND 53-30-01. 2 L 7 4 4F A20WE 1998091800363 19980918 00363 NM 1998 9 18 P5CA9801422 1 19980804 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1565 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS 1565 STR 12L. REPAIRED CORROSION AND REPROTECTED PER SRM 51-10-01, 53-10-01 AND 51-10-02. 2 L 7 4 4F A20WE 1998091800364 19980918 00364 NM 1998 9 18 P5CA9801423 1 19980804 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1800-1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND BS 1800-1960 STR 12R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AN D MM 51-24-11. 2 L 7 4 4F A20WE 1998091800365 19980918 00365 NM 1998 9 18 P5CA9801424 1 19980804 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1740-1820 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS1740-18820 STR 12R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800366 19980918 00366 NM 1998 9 18 P5CA9801425 1 19980804 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1960 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS 1960 STR 12R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND MM 51-24-11. 2 L 7 4 4F A20WE 1998091800367 19980918 00367 NM 1998 9 18 P5CA9801426 1 19980804 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1740 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS 1740 STR 19R LAP JOINT. CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01, 51-10-02 AND 53-30-01. 2 L 7 4 4F A20WE 1998091800368 19980918 00368 NM 1998 9 18 P5CA9801427 1 19980804 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1520 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 LEVEL 1 CORROSION FOUND AT BS 1520R STR 12R LAP JOINT. REMOVED CORROSION AND REPROTECTED PER SRM 51-10-01, 53-30-01 AN D 51-10-02. 2 L 7 4 4F A20WE 1998091800378 19980918 00378 SO 1998 9 18 98ZZZX3313 1 19980818 A 3230 AN4 BOLT PIPER PA32 PA32R300 7103213 SO LYC O540 IO540K1A5 41532 EA NLG ACTUATOR SHEARED A DKBA O OTHER O OTHER LD LANDING 1 SO 09 8337C 32R7680101 RETRACT ACTUATOR BOLT AT GEAR SHEARED IN-FLIGHT. NOSE GEAR EXTENDED AND LOCKED DOWN BY INDICATION OF GREEN LIGHT. PILO T MOVED HANDLE TO DOWN POSITION AND LT AND RT MLG EXTENDED AND LOCKED DOWN, AND, LANDED WITHOUT INCIDENT. BOLT REPLACED AND RETRACT PERFORMED. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. 1 L 7 1 3O 3 O A3SO 1E4 1998091800438 19980918 00438 SW 1998 9 18 HEEA0016028 1 19980911 A 7714 212075037113 INDICATOR BELL 412 412 1182202 SW ENGINE N1 STICKING E HEEA K NONE L NO TEST IN INSP/MAINT 1 SW 03 142PH 408 33150 N1 STICKS DURING ENGINE START. 1 G 7 2 4U H4SW 1998091800448 19980918 00448 NM 1998 9 18 SWAA981804 1 19980820 A 3350 BULB BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED RON CHECK, FOUND EGRESS LIGHT INOP AT LEFT WING TRAILING EDGE. CLEANED SOCKET AND RELAMPED PER BOEING MM, OPS CHECK OK. 2 L 7 2 4F A16WE 1998091800449 19980918 00449 NM 1998 9 18 SWAA981805 1 19980820 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 337 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN AT BS 337 DENTED 3 BELOW STR 17 LT FWD ENTRY DOOR LOWER THRESHOLD. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800450 19980918 00450 NM 1998 9 18 SWAA981806 1 19980821 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AROUND NUT PLATE AT BS 727-947, RBL 3, WL 159. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800451 19980918 00451 NM 1998 9 18 SWAA981807 1 19980821 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FLOOR TO BULKHEAD SUPPORT ANGLE CORRODED AT BS 947, LBL 21, RBL 21, WL 180. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800452 19980918 00452 NM 1998 9 18 SWAA981808 1 19980821 A 5320 FASTENERS BOEING 737 7373H4 1384600 NM FUSELAGE OVERSIZE A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE ABOVE STRINGER 23 RT HAS OVERSIZED FASTENER HOLES AT BS 727D AND BS 727D-727D+ 10. PERFORMED MODIFICATION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800453 19980918 00453 NM 1998 9 18 SWAA981809 1 19980821 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 827, LBL 46, WL 173. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800454 19980918 00454 NM 1998 9 18 SWAA981810 1 19980821 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 989-1016 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND NUMEROUS SCRATCHES AND GOUGES IN SKIN AT BS 989 TO BS 1016, WL 233 - WL 241 LEFT SIDE. R EMOVED AND REPLACED PER TRAMCO EWO NR 98-0676. 2 L 7 2 4F RT A16WE 1998091800455 19980918 00455 NM 1998 9 18 SWAA981811 1 19980821 A 5512 SKIN BOEING 737 7373H4 1384600 NM LT HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND LEFT HORIZ STAB L/E DENTED BETWEEN STABILIZER AT BS 0 AND STABILIZER AT BS 57.93. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800456 19980918 00456 NM 1998 9 18 SWAA981812 1 19980821 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 1126.56 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND LEFT SKATE ANGLE CHAFED AT BS 1126.56. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800457 19980918 00457 NM 1998 9 18 SWAA981813 1 19980821 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 922-924 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21722 DURING SERVICE CHECK, FOUND 2 INCH CRACK AT BS 922 TO 924 ABOVE STR 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800458 19980918 00458 NM 1998 9 18 SWAA981814 1 19980821 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D-CHECK, FOUND CRACK INDICATION AT BS 178 BULKHEAD WEB AT WL 218 AND RBL 11 AT RADAR SUPPORT. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800459 19980918 00459 NM 1998 9 18 SWAA981815 1 19980821 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 787-791 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL CORRODED AT BS 787-791, STR 25R IN AFT CARGO BAY. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800460 19980918 00460 NM 1998 9 18 SWAA981816 2 19980821 A 7200 ENGINE BOEING 737 7372T4 1384492 NM NR 1 MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 721SW 22697 AIR RETURN DUE TO NR 1 ENGINE EGT WAS AT REDLINE FOR T/O AND REQUIRED REDUCING THROTTLE SIGNIFICANTLY TO MAINTAIN IN LIM ITS. A/C MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 ENGINE ASSY AS PER SAM FORMS 104, 111, 117, 636. INSTA LLED STAGE II MOTOR. PERFORMED TRIM RUN AND ALL PARAMETER WERE WITHIN BOEING MM LIMITS. 2 L 7 2 4F A16WE 1998091800461 19980918 00461 NM 1998 9 18 SWAA981817 1 19980821 A 5310 STRUCTURE BOEING 737 7373H4 1384600 NM FWD FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 364SW 26575 AIRCRAFT STRUCK BY CONTINENTAL AIRLINES MX TRUCK. DURING INSP FOUND RIGHT SIDE NOSE AREA SKIN DAMAGED. INSPECTED AND F OUND OK FOR MX FERRY FLT TO DAL. DURING WALKAROUND IN DAL DISCOVERED DAMAGE TO AIRCRAFT NOSE GEAR AREA TO INCLUDE LEF T NOSE GEAR DOOR AND LOWER FUSELAGE FWD OF THE NOSE GEAR WHEEL WELL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800462 19980918 00462 1998 9 18 SWAA981818 2 19980822 A 7200 ENGINE BOEING 737 7372T4 1384492 NM NR 2 BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 130SW 22699 AIR TURNBACK DUE TO BIRD STRIKE ON NR 2 ENGINE ON ROTATION. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED PER BOEING MM, NO DAMAGED NOTED. 2 L 7 2 4F A16WE 1998091800463 19980918 00463 NM 1998 9 18 SWAA981819 1 19980821 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 907 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FRAME DENTED AT BS 907, WL 172, LBL 24. REMOVED AND REPLACED PER TRAMCO EWO NR 98-0774 . 2 L 7 2 4F RT A16WE 1998091800464 19980918 00464 NM 1998 9 18 SWAA981820 1 19980821 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 616, WL 201, LBL 65. REMOVED AND REPLACED PER TRAMCO EWO NR 98-074 3. 2 L 7 2 4F RT A16WE 1998091800465 19980918 00465 NM 1998 9 18 SWAA981821 1 19980821 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 538 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOOR STIFFENER CRACKED AT BS 538, RBL 2, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800466 19980918 00466 NM 1998 9 18 SWAA981822 1 19980821 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 312-328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 312-328, LBL 12, WL 208 CRACKED. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091800467 19980918 00467 NM 1998 9 18 SWAA981823 1 19980821 A 3350 COVER BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 624SW 27934 DURING SCHEDULED C2 CHECK, FOUND EMERGENCY FLOOR LIGHT TRACK COVER MISSING AT CENTER LOUNGE. INSTALLED MISSING TRACK C OVER BETWEEN EMERGENCY FLOOR LIGHTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800468 19980918 00468 NM 1998 9 18 SWAA981824 1 19980821 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT OUT. REPLACED BULB AT FWD EXTERIOR SERVICE DOO R EMERGENCY EXIT LIGHT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800469 19980918 00469 NM 1998 9 18 SWAA981825 1 19980822 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 080SW 22675 DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OUTSIDE FWD ENTRY AND GALLEY INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM, OPS CKS GOOD. 2 L 7 2 4F A16WE 1998091800470 19980918 00470 NM 1998 9 18 SWAA981826 1 19980822 A 5320 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT FWD FRAME CLOSEOUT PANEL DAMAGED AT BS 794, RBL 25. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800471 19980918 00471 NM 1998 9 18 SWAA981827 1 19980822 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 787 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 787, RBL 24-25, WL 158. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800472 19980918 00472 NM 1998 9 18 SWAA981828 1 19980822 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AROUND NUT PLATE AT BS 727-947, LBL 12.5, WL 159; BS 727-947, L BL 8, WL 159; BS 727-947, LBL 3, WL 159 AND BS 727-947, RBL 8, WL 159. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800473 19980918 00473 NM 1998 9 18 SWAA981829 1 19980822 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 LT, BS 867; STR 8 & 9 LT, BS 827 & STR 8 AND 9 LT, BS 787. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800474 19980918 00474 NM 1998 9 18 SWAA981830 1 19980822 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 LT, BS 747. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800475 19980918 00475 NM 1998 9 18 SWAA981831 1 19980822 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED SIDE CHORD AT BS 178, RBL 29, WL 207 AND BS 178, LBL 29 WL 207. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800476 19980918 00476 NM 1998 9 18 SWAA981832 1 19980822 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 349 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 349, WL 217, LBL 64. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800477 19980918 00477 NM 1998 9 18 SWAA981833 1 19980822 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED BELOW STRINGER AT BS 360, STR 13 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800478 19980918 00478 NM 1998 9 18 SWAA981834 1 19980822 A 5230 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 519SW 23959 DURING SCHEDULED BC4 CHECK, FOUND AFT CARGO DOOR UP LATCH INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800479 19980918 00479 NM 1998 9 18 SWAA981835 1 19980823 A 5730 SKIN BOEING 737 7373H4 1384600 NM WING LE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 330SW 23694 DURING SCHEDULED C4 CHECK, FOUND LEADING EDGE SKIN CRACKED AT I/B END OF HINGE CUTOUT OF SPRING LOADED DOOR. REPAIRED P ER ACO NR 6820-57. 2 L 7 2 4F RT A16WE 1998091800480 19980918 00480 NM 1998 9 18 SWAA981836 1 19980822 A 5230 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED C2 CHECK, FOUND CARGO DOOR LATCH BRACKET INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800481 19980918 00481 NM 1998 9 18 SWAA981837 1 19980822 A 5320 WINDOW POST BOEING 737 7373H4 1384600 NM COCKPIT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND HFEC REVELS CRACKED TOP OF F/O CORNER WINDOW POST. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800482 19980918 00482 NE 1998 9 18 SWAA981838 2 19980824 A 7321 378200 FUEL CONTROL BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A SWAA O OTHER J WARNING INDICATION DE DESCENT 1 SW 07 85SW 22826 AT CRUISE, NR 2 ENGINE ROLLED BACK TO 1.56 EPR, 79 PERCENT N1, 83.5 PERCENT N2 2150 FF AND FROZE THERE. ENGINE DID NOT RESPOND TO THROTTLE MOVEMENT, ENGINE SHUTDOWN ACCOMPLISHED AND SINGLE-ENGINE LANDING ACCOMPLISHED. REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL ASSY PER BOEING MM. 2 L 7 2 4F 4 F A16WE E2EA 1998091800483 19980918 00483 NM 1998 9 18 SWAA981840 1 19980824 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22732 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE AFT F/A COMM PANEL NOT SECURED. RESECURED LIGHT PER BOEING MM. 2 L 7 2 4F A16WE 1998091800484 19980918 00484 NM 1998 9 18 SWAA981841 1 19980823 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 LT AT BS 500C. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800485 19980918 00485 NM 1998 9 18 SWAA981842 1 19980824 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400 & 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8 AND 9 RT AT BS 500A AND BS 400. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800486 19980918 00486 NM 1998 9 18 SWAA981843 1 19980824 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 315.5 & 324 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 315.5 AND 324, RBL 10, WL 208. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998091800487 19980918 00487 NM 1998 9 18 SWAA981844 1 19980824 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 305.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 305.5 AND RBL 10, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800488 19980918 00488 NM 1998 9 18 SWAA981845 1 19980824 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 312, LBL 39, 33, 20, 14 RBL 8, WL 208 AND WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800489 19980918 00489 NM 1998 9 18 SWAA981846 1 19980824 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 326 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND STABILIZER STRAP CRACKED AT BS 326, RBL 32, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800490 19980918 00490 NM 1998 9 18 SWAA981847 1 19980824 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED BS 178 BULKHEAD AT WL 200, LBL 5, FWD SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800491 19980918 00491 NM 1998 9 18 SWAA981848 1 19980824 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS OF BS 178 BULKHEAD, UNDER STRAP AT LBL 6.7, WL 212-213. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800492 19980918 00492 NM 1998 9 18 SWAA981849 1 19980824 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS OF BS 178 BULKHEAD, UNDER STRAP AT RBL 4.7, WL 200.5 TO 201.5. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800493 19980918 00493 NM 1998 9 18 SWAA981850 1 19980824 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACK INDICATIONS OF BS 178 BULKHEAD, UNDER STRAP AT RBL 4.7, WL 197.5 TO 198.5. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800494 19980918 00494 NM 1998 9 18 SWAA981851 1 19980824 A 5321 FLOOR BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR WEB AT BS 178, LBL 25-29 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800495 19980918 00495 NM 1998 9 18 SWAA981852 1 19980824 A 5321 FLOOR BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED FLOOR WEB AT BS 178, RBL 25-29 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800496 19980918 00496 NM 1998 9 18 SWAA981853 1 19980824 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGER 8 AND 9 RIGHT AT BS 827. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800497 19980918 00497 NM 1998 9 18 SWAA981854 1 19980824 A 5320 SHEAR WEB BOEING 737 7373H4 1384600 NM BS 386 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR WEB AT BS 386, BL 0, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800498 19980918 00498 NM 1998 9 18 SWAA981855 1 19980824 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 1015 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED SUPPORT AT BS 1015, LBL 39, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800499 19980918 00499 NM 1998 9 18 SWAA981856 1 19980824 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND ANGLE TO BS 178 BULKHEAD CRACKED, LBL 26-29 AT STR 17 LT AND RBL 26-29, AT STR 17 RT. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800500 19980918 00500 NM 1998 9 18 SWAA981857 1 19980824 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 182 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 182, RBL 17, WL 181. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800501 19980918 00501 NM 1998 9 18 SWAA981858 1 19980824 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 181 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 181, LBL 6, WL 187. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800502 19980918 00502 NM 1998 9 18 SWAA981859 1 19980824 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM UPPER CHORD AT BS 986.5, RBL 5, 22, 23, 26, 43.5, LBL 4.5, 14, 43.5, WL 208 AND WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800503 19980918 00503 NM 1998 9 18 SWAA981860 1 19980824 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 340 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 340, RBL 11, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800504 19980918 00504 NM 1998 9 18 SWAA981861 1 19980823 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND REMOVED EGRESS LIGHTING FOM. INSTALLED EGRESS LIGHTING AND OPS CHECKS GOOD PER BOEI NG MM. 2 L 7 2 4F RT A16WE 1998091800505 19980918 00505 NM 1998 9 18 SWAA981862 1 19980825 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING STRIP ROW 12 LOOSE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800506 19980918 00506 NM 1998 9 18 SWAA981863 1 19980825 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED A2 CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT IS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT L IGHT ASSY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800507 19980918 00507 NM 1998 9 18 SWAA981864 1 19980825 A 3350 BULB BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 528SW 26570 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY LIGHT AT OVERHEAD BIN ROW 8 INOP. RELAMPED LIGHT, OPS CHECK GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800508 19980918 00508 NM 1998 9 18 SWAA981865 1 19980824 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28036 DURING SCHEDULED C3 CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT IS INOP. RELAMPED PER BOEING MM, OPS CHECK G OOD. 2 L 7 2 4F RT A16WE 1998091800509 19980918 00509 NM 1998 9 18 SWAA981866 1 19980825 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD UPPER SURFACE FWD EDGE GOUGED AT BS 986, WL 208, RBL 44. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800510 19980918 00510 NM 1998 9 18 SWAA981867 1 19980825 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD UPPER SURFACE CORRODED AT BS 986.5, WL 208, LBL 4.75, LBL 13.5 & L BL 30.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800511 19980918 00511 NM 1998 9 18 SWAA981868 1 19980825 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1008 & 1014 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD UPPER SURFACE CORRODED AT BS 1008 & 1014, WL 208, LBL 30.5 & LBL 6 .0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800512 19980918 00512 NM 1998 9 18 SWAA981869 1 19980825 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 992 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT CORRODED AT BS 992, WL 208, LBL 24. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800513 19980918 00513 NM 1998 9 18 SWAA981870 1 19980825 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CORROSION ON CREASE BEAM WEB AT BS 727A-727B, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800514 19980918 00514 NM 1998 9 18 SWAA981871 1 19980825 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CORRODED ON CREASE BEAM WEB AT BS 727B-727C, WL 208, LBL 60. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800515 19980918 00515 NM 1998 9 18 SWAA981872 1 19980825 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 986.5 - 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 986.5 - 1016, LBL 35-45, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800516 19980918 00516 NM 1998 9 18 SWAA981873 1 19980826 A 2131 7638101 CONTROLLER BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 687SW 23388 AIRCRAFT ROUTED FROM MCO TO PVD DIVERTED TO BWI. WHILE CRUSING AT FL 370, CABIN ALT WARNING HORN SUDDENTLY CAME ON, CAB IN PRESSURIZATION WAS RAPIDLY CLIMBING THROUGH 10,000 FT. EMERGENCY DESCENT COMMENCED, OUTFLOW VALVE CLOSED MANUALLY. P ACKS WERE PUT ON HIGH, THE CABIN STAB PASSING 28,000 FT A/C LEVELED AT 23,000 FT. PRESSURIZATION THEN MAINTAINED USING STANDBY MODE. FLIGHT ATTENDANT REPORTED AIR RUSHING OUT REAR OF A/C BY THE DOORS. CABIN ALT MAXED OUT AT 11,000 FT, SO MASK DID NOT DROP. A/C MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED CABIN PRESSURE CONTROLLER AND PRESSURIZATION CONTROL PANEL AND ACCOMPLISHED SYSTEM TESTS PER BOEING MM. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800517 19980918 00517 NE 1998 9 18 SWAA981874 2 19980827 A 7200 ENGINE BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 63SW 22061 AIR TURNBACK DUE TO BIRD STRIKE, NR 2 ENGINE DURING TAKEOFF ROLL. AIRCRAFT MADE AN UNEVENTFUL LANDING. AIRCRAFT INSPEC TED, NR 2 ENGINE AND PS3 FILTER. NO DAMAGE. C/W ENGINE RUN PER BOEING MM. REPAIRED PER BOEING SRM. 2 L 7 2 4F 4 F A16WE E2EA 1998091800518 19980918 00518 NM 1998 9 18 SWAA981875 1 19980826 A 5320 WEB BOEING 737 7372H4 138448C NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED AT STRINGER 4L AND BS 294. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800519 19980918 00519 NM 1998 9 18 SWAA981876 1 19980826 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND AT BS 727 COMPRESSION CHORD CRACKED AT BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800520 19980918 00520 NM 1998 9 18 SWAA981877 1 19980826 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 178-188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND INTERCOSTAL CRACKED AT BS 178 TO 188, LBL 26. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800521 19980918 00521 NM 1998 9 18 SWAA981878 1 19980826 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND SURFACE CORRODED AT BS 967, STR 25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800522 19980918 00522 NM 1998 9 18 SWAA981879 1 19980826 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1145 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND SKIN/PLATE WORN UNDER FWD SLIDING SEAL RETAINER AT BS 1145. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800523 19980918 00523 NM 1998 9 18 SWAA981880 1 19980826 A 5320 WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND WATER LINE 207, RBL 28.5 WEB CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800524 19980918 00524 NM 1998 9 18 SWAA981881 1 19980827 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4D CHECK, FOUND EDDY CURRENT SHOWS CRACK COMING FROM FASTENER HEAD LBL 10, WL 234 FWD SIDE OF BULKHEA D. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800525 19980918 00525 NM 1998 9 18 SWAA981882 1 19980826 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 343 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 343 BETWEEN STR 19 AND 20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800526 19980918 00526 NM 1998 9 18 SWAA981883 1 19980826 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 984 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CORRODED SUPPORT ANGLE AT BS 984, LTBL 53, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800527 19980918 00527 NM 1998 9 18 SWAA981885 1 19980826 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 270 Z ANGLE, LBL 12 TO RBL 12. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800528 19980918 00528 NM 1998 9 18 SWAA981886 1 19980826 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 344, LBL 60, WL 208 ON GIRT BAR BRACKET MOUNT PAD. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800529 19980918 00529 NM 1998 9 18 SWAA981887 1 19980826 A 5312 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND VERTICAL CHORD CRACKED ON AFT SIDE OF 178 BULKHEAD, LBL 5.7, WL 184. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091800530 19980918 00530 NM 1998 9 18 SWAA981888 1 19980826 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED LBL 1, WL 186. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800531 19980918 00531 NM 1998 9 18 SWAA981889 1 19980826 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 890 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AT BS 890 BETWEEN STRINGERS 25-26 RT. REPAIRED PER BOEING SRM. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800532 19980918 00532 NM 1998 9 18 SWAA981890 1 19980827 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED BS 178 BULKHEAD, RBL 4, WL 199-202. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800533 19980918 00533 NM 1998 9 18 SWAA981884 1 19980827 A 3350 LIGHT BOEING 737 7373A4 1384585 NM CABIN MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 680SW 23505 DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS TRACK LIGHTING MISSING SEVERAL LIGHTS. REPLACED LIGHT & LENS ASSY'S AS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800534 19980918 00534 NM 1998 9 18 SWAA981892 1 19980827 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 1142 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND STRINGER 5 RT LOWER CHORD CRACKED AT BS 1142. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800535 19980918 00535 NM 1998 9 18 SWAA981893 1 19980827 A 5311 FRAME BOEING 737 7373H4 1384600 NM FUSELAGE GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY FWD DOOR FRAME NR 5 STOP PAD FITTING WITH DEEP GOUGES. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800536 19980918 00536 NM 1998 9 18 SWAA981894 1 19980827 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 907 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND DAMAGED SHEAR TIE BETWEEN STR 21R AND 22R AT BS 907. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091800537 19980918 00537 NM 1998 9 18 SWAA981895 1 19980827 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 907 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND DAMAGED SHEAR TIE BETWEEN STR 22R AND 23R AT BS 907 AND STR 23R AND 24R AT BS 907. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800538 19980918 00538 NM 1998 9 18 SWAA981896 1 19980828 A 3241 39353 LIGHT BOEING 737 7373H4 1384600 NM ANTISKID SYST INOPERATIVE A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 610SW 27696 AIRCRAFT DIVERTED TO STL ANTISKID LIGHT CAME ON AFTER TAKEOFF. WOULD NOT RESET AIRBORNE. AIRCRAFT MADE AN UNEVENTFUL L ANDING. DEFERRED PER MEL 32-2. 2 L 7 2 4F RT A16WE 1998091800539 19980918 00539 NM 1998 9 18 SWAA981897 1 19980827 A 5314 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 712.5-725 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM FLANGE RT OUT BOARD CHAFED AROUND FASTENER HOLES AT BS 712.5 TO 725, RBL 6. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800540 19980918 00540 NM 1998 9 18 SWAA981898 1 19980828 A 5400 ANGLE BOEING 737 7373H4 1384600 NM NR 1 PYLON DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND NR 1 PYLON ANGLE LOWER EDGE OF I/B FLAP CUTOUT DAMAGED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800541 19980918 00541 NM 1998 9 18 SWAA981899 1 19980828 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND 9L AT BS 867. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800542 19980918 00542 NM 1998 9 18 SWAA981900 1 19980828 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER 8R AT BS 344. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800543 19980918 00543 NM 1998 9 18 SWAA981901 1 19980828 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 294-312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOOR SUPPORT AT BS 294-312, LBL 12, WL 208 CORRODED. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998091800544 19980918 00544 NM 1998 9 18 SWAA981902 1 19980828 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 390 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER SURFACE OF WEB AT WL 208, BS 390, RBL 70. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091800545 19980918 00545 NM 1998 9 18 SWAA981903 1 19980828 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT STR 7L, BS 295 FWD OF FWD ENTRY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800546 19980918 00546 NM 1998 9 18 SWAA981904 1 19980828 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 367 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 367, 1 BELOW STR 5L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800547 19980918 00547 NM 1998 9 18 SWAA981905 1 19980828 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND BULKHEAD SUPPORT ANGLE AT BS 500D, RBL 24 TO LBL 24, WL 156 CORRODED SURFACE AROUND NUT PLATE . REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800548 19980918 00548 NM 1998 9 18 SWAA981906 1 19980828 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED IN AFT CARGO BAY AT BS 867, STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800549 19980918 00549 NM 1998 9 18 SWAA981907 1 19980827 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 365SW 26576 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT TRACK LOOSE. REMOVED AND REPLACED TRACK LOOSE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800550 19980918 00550 NM 1998 9 18 SWAA981908 1 19980828 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING WALKAROUND CHECK, FOUND FWD ENTRY EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED FWD ENTRY EMERGENCY EXIT LIG HT, OPS CKS OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800551 19980918 00551 NM 1998 9 18 SWAA981909 1 19980828 A 2560 SLIDE BOEING 737 7375H4 138449D NM CABIN DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING WALKAROUND CHECK, FOUND EMERGENCY ESCAPE SLIDE FELL OUT OF FIBERGLASS SHELL. F/A WAS UNABLE TO ATTACH GIRT BAR. REINSTALLED SLIDE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800552 19980918 00552 NM 1998 9 18 SWAA981910 1 19980829 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4 D-CHECK, FOUND VERTICAL T-CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED PER TRAMCO T1-253-031 . 2 L 7 2 4F A16WE 1998091800553 19980918 00553 NM 1998 9 18 SWAA981911 1 19980829 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED STR 27L AT BS 947 UNDER THE FRAME. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800554 19980918 00554 NM 1998 9 18 SWAA981912 1 19980829 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 335SW 23939 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY EXIT LIGHT ASSY LOOSE ABOVE 5D. REPAIRED EMERGENCY LIGHT ASSY PER BOEING MM. \N\N\N\N\N\N\N\NREPLACED LIGHT & LENS ASSY'S AS PER BOEING MM.\N\N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM.\N\N\N\N\N\N\N \N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800555 19980918 00555 NM 1998 9 18 SWAA981913 1 19980829 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO COMPT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 322SW 23343 DURING SCHEDULED C1 CHECK, FOUND AFT CARGO COMPT INTERCOSTAL BROKEN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800556 19980918 00556 NM 1998 9 18 SWAA981914 1 19980829 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED AT BS 178 BULKHEAD, LBL 4, WL 199-202. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800557 19980918 00557 NM 1998 9 18 SWAA981915 1 19980829 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 1006 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND FRAME WITH EIGHT HOLES AT BS 1006 WL 300, RBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800558 19980918 00558 NM 1998 9 18 SWAA981916 1 19980829 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED 178 BULKHEAD, RBL 6-7, WL 199. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800559 19980918 00559 NM 1998 9 18 SWAA981917 1 19980829 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 308 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 308, RBL 11, WL 208. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091800560 19980918 00560 NM 1998 9 18 SWAA981918 1 19980829 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 616 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND FRAME TO FLOORBEAM SUPPORT DAMAGED FASTENER AT BS 616, LBL 64.5, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800561 19980918 00561 NM 1998 9 18 SWAA981919 1 19980829 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 616 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND FRAME TO FLOORBEAM SUPPORT DAMAGED FASTENER AT BS 616, RBL 64.5, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800562 19980918 00562 NM 1998 9 18 SWAA981920 1 19980830 A 5320 ANGLE BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND AFT GALLEY SERVICE DOORWAY THRESHOLD Z ANGLES CORRODED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800563 19980918 00563 NM 1998 9 18 SWAA981921 1 19980830 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 787 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP MECHANICALLY DAMAGED AT BS 787, STR 21 RT. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998091800564 19980918 00564 NM 1998 9 18 SWAA981922 1 19980830 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 500B TO 500C, RBL 26, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800565 19980918 00565 NM 1998 9 18 SWAA981923 1 19980830 A 3350 LIGHT BOEING 737 7373G7 1384595 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FWD END OF FLOOR TRACK LIGHTS OFF. RESECURED FWD END FLOOR TRACK LIGHTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800566 19980918 00566 NM 1998 9 18 SWAA981924 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 400 BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800567 19980918 00567 NM 1998 9 18 SWAA981925 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 440 BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800568 19980918 00568 NM 1998 9 18 SWAA981926 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 480 BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800569 19980918 00569 NM 1998 9 18 SWAA981927 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500A BELOW STR 8 LT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800570 19980918 00570 NM 1998 9 18 SWAA981928 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500C BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800571 19980918 00571 NM 1998 9 18 SWAA981929 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 500A BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800572 19980918 00572 NM 1998 9 18 SWAA981930 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 440 BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800573 19980918 00573 NM 1998 9 18 SWAA981931 1 19980831 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 380 BELOW STR 8 RT. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800574 19980918 00574 NM 1998 9 18 SWAA981932 1 19980831 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 727 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND (AFT CARGO BAY) SUPPORT BRACE BRACKETS BROKEN AT BS 727, LBL 1 AND RBL 2 (2) PLACES, WL 163. REMOVED AND REPLACED PER BOEING SRM.\N\N\N\N\N\N\N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800575 19980918 00575 NM 1998 9 18 SWAA981933 1 19980831 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 293-298 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED WEB R1 DOOR AT BS 293-298, WL 208, RBL 55. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800576 19980918 00576 NM 1998 9 18 SWAA981934 1 19980831 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 330-332 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED SUPPORT L-ANGLE FWD GALLEY DOOR SUB T-HOLD AT BS 330-332 BOTTOM SIDE. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800577 19980918 00577 NM 1998 9 18 SWAA981935 1 19980831 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 950, LBL 26 TO 44, WL 208; BS 947 TO 967, LBL 17, WL 208 AND BS 967 TO 987, LBL 17 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800578 19980918 00578 NM 1998 9 18 SWAA981936 1 19980831 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 951 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 951, LBL 12.5, WL 208 AND BS 951, LBL 23, WL 208. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800579 19980918 00579 NM 1998 9 18 SWAA981937 1 19980831 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 375 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4 D-CHECK, FOUND DENTED FUSELAGE SKIN AT BS 375 BETWEEN 22R AND 23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800580 19980918 00580 NM 1998 9 18 SWAA981938 1 19980831 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 178-188 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED INTERCOSTAL BS 178 TO 188, RBL 26. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800581 19980918 00581 NM 1998 9 18 SWAA981939 1 19980831 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN PLATE I/B OF LT HORIZ STAB GOUGED/WORN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800582 19980918 00582 NM 1998 9 18 SWAA981940 1 19980831 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN PLATE I/B OF RT HORIZ STAB GOUGED/WORN. REMOVED AND REPLACED PER BOEING SRM.\N \N\N\N\N\N\N\N\N\N\N\N\N\N\NREPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800583 19980918 00583 NM 1998 9 18 SWAA981941 1 19980831 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 950 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 950, RBL 40. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800584 19980918 00584 NM 1998 9 18 SWAA981942 1 19980831 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 986-1006, BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800585 19980918 00585 NM 1998 9 18 SWAA981943 1 19980831 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 947-967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 947-967, LBL 18 AND 947-967, RBL 18. REPA IRED PER BOEING SRM. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800586 19980918 00586 NM 1998 9 18 SWAA981944 1 19980831 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CLIP NUT HOLE AT BS 947, LBL 15 AND BS 947, RBL 15. REPAIRED PER TI-A53-04 . REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800587 19980918 00587 NM 1998 9 18 SWAA981945 1 19980831 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED STR CLIP AT BS 947 STR 24L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800588 19980918 00588 NM 1998 9 18 SWAA981946 1 19980831 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED RT AFT TRANSITION ANGLE AT BS 500A TO 500D. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091800589 19980918 00589 NM 1998 9 18 SWAA981947 1 19980902 A 2612 FIRE WARNING BOEING 737 7372H4 138448C NM WHEEL WELL ACTIVATED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 085SW 22826 CREW REPORTED WHEEL WELL FIRE INDICATION IN FLIGHT, LOWERED LANDING GEAR, LIGHT AND HORN WENT OUT NORMAL LANDING ACCOMPL ISHED. AIRCRAFT DIVERTED EN ROUTE TPA-BNA, MADE AN UNEVENTFUL LANDING. PERFORMED OPERATIONAL CHECK OF WHEEL WELL FIRE LOOP CONNECTIONS IN WHEEL WELL. FOUND OK PER BOEING MM. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800590 19980918 00590 NM 1998 9 18 SWAA981948 1 19980901 A 5320 FASTENER BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND FASTENER AT BS 967, RBL 17. REPAIRED PER BOEING TI-A53-14. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800591 19980918 00591 NM 1998 9 18 SWAA981949 1 19980901 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 420-440 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED TRANSITION ANGLE RT AT BS 420-440. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800592 19980918 00592 NM 1998 9 18 SWAA981950 1 19980901 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 1006-1016, LBL 7. REMOVED AND REPLACED PER BOEING SRM. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800593 19980918 00593 NM 1998 9 18 SWAA981951 1 19980901 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 847 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED AND DENTED WEB AT BS 847, STR S24 AND S25R. REPAIRED PER BOEING SRM. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800594 19980918 00594 NM 1998 9 18 SWAA981952 1 19980901 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT FASTENER HOLE WL 234, RBL 8. REPAIRED PER BOEING TI-A53-015. 2 L 7 2 4F RT A16WE 1998091800595 19980918 00595 NM 1998 9 18 SWAA981953 1 19980901 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294-312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED IN AND AROUND HOLES IN INTERCOSTAL AT BS 294 TO 312, LBL 11. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800596 19980918 00596 NM 1998 9 18 SWAA981954 1 19980901 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT FASTENER HOLE WL 234, RBL 10; WL 234, RBL 11 AND WL 234, LBL 9. REMOVED AND REPLACED PER BOEING SRM. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800597 19980918 00597 NM 1998 9 18 SWAA981955 1 19980901 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 967-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL CLIP NUT HOLES AT BS 967-986, LBL 18. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800598 19980918 00598 NM 1998 9 18 SWAA981956 1 19980902 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 440-500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED LT TRANSITION ANGLE NUT PLATE HOLES AT BS 440-500. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800599 19980918 00599 NM 1998 9 18 SWAA981957 1 19980902 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 460 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP AT BS 460, STR 24L DAMAGED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800600 19980918 00600 NM 1998 9 18 SWAA981958 1 19980902 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 328 & 344 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL BETWEEN BS 328 AND 344 RBL 11. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800601 19980918 00601 NM 1998 9 18 SWAA981959 1 19980902 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED L-ANGLE FOR FLOORBOARD AND CENTER BULKHEAD PANEL AT BS 500D, STR 25L TO 25R . REMOVED AND REPLACED PER BOEING SRM. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800602 19980918 00602 NM 1998 9 18 SWAA981960 1 19980902 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED T-ANGLE AT BS 500A TO 500D. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800603 19980918 00603 NM 1998 9 18 SWAA981961 1 19980902 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 294-312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED IN AND AROUND HOLES IN ANGLE AT BS 294 TO 312, RBL 16. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800604 19980918 00604 NM 1998 9 18 SWAA981962 1 19980902 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 328-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION IN AND AROUND HOLES IN INTERCOSTAL AT BS 328 - 344, LBL 11. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800605 19980918 00605 NM 1998 9 18 SWAA981963 1 19980901 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT RT SIDE OF FUSELAGE 36 FWD OF OUT FLOW VALVE. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800606 19980918 00606 NM 1998 9 18 SWAA981964 1 19980901 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED AT LEFT SIDE OF FUSELAGE 3 INCHES ABOVE AND 3 INCHES AFT OF WATER SERVICE PANEL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800607 19980918 00607 NM 1998 9 18 SWAA981965 1 19980901 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 976 & 941 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 976 ABOVE STR 22L AND AT BS 941 ABOVE 25R. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998091800608 19980918 00608 NM 1998 9 18 SWAA981966 1 19980901 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4 D-CHECK, FOUND RT SIDE CHORD CRACKED AT BS 178, RBL 32, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800609 19980918 00609 NM 1998 9 18 SWAA981967 1 19980901 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED 1/4 D-CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, LBL 32, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800610 19980918 00610 NM 1998 9 18 SWAA981968 1 19980901 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 759 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 759, STR 18L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800611 19980918 00611 NM 1998 9 18 SWAA981969 1 19980901 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED C1 CHECK, FOUND INTERCOSTAL BROKEN AT SUPPORT UPLOCK LATCH. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800612 19980918 00612 NM 1998 9 18 SWAA981970 1 19980901 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND STR 9L AT BS 727D. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800613 19980918 00613 NM 1998 9 18 SWAA981971 1 19980901 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND STR 9L AT BS 747. REPAIRED PER TRAMCO EWO NR 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800614 19980918 00614 NM 1998 9 18 SWAA981972 1 19980901 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8L AND STR 9L AT BS 827. REPAIRED PER TRAMCO EWO NR 98-0751. 2 L 7 2 4F RT A16WE 1998091800615 19980918 00615 NM 1998 9 18 SWAA981973 1 19980901 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 & 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8R AND STR 9R AT BS 867 AND BS 827. REPAIRED PER TRAMCO EWO N R 98-0751. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800616 19980918 00616 NM 1998 9 18 SWAA981974 1 19980901 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME BETWEEN STR 8R AND STR 9R AT BS 727D AND BS 727B. REPAIRED PER TRAMCO EWO NR 98-0751. 2 L 7 2 4F RT A16WE 1998091800617 19980918 00617 NM 1998 9 18 SWAA981975 1 19980901 A 5320 STABILIZER BOEING 737 7373H4 1384600 NM BS 314 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOOR STABILIZER CRACKED AT BS 314, LBL 12, WL 198.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800618 19980918 00618 NM 1998 9 18 SWAA981976 1 19980901 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 314 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM AT BS 294.5, RBL 47, WL 208 CORRODED ON UPPER FLANGES. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091800619 19980918 00619 NM 1998 9 18 SWAA981977 1 19980901 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT FASTENER HOLE BS 727 TO 847, LBL 3, WL 160. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091800620 19980918 00620 NM 1998 9 18 SWAA981978 1 19980901 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED BC1 CHECK, FOUND EMERGENCY FLOOR PATH LIGHT STRIP CRACKED AT 1AB. REMOVED AND REPLACED EMERGENCY FLOOR PATH LIGHT STRIP PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800621 19980918 00621 NM 1998 9 18 SWAA981979 1 19980902 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 241 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 241, WL 170, LBL 59. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800622 19980918 00622 NM 1998 9 18 SWAA981980 1 19980902 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 342 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 342, WL 205 BETWEEN STRINGER 17 AND 18 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800623 19980918 00623 NM 1998 9 18 SWAA981981 1 19980902 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 348 & 346 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND TWO DENTS IN SKIN AT BS 348 AND 346, WL 200 BETWEEN STRINGERS 17 AND 18 RT. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800624 19980918 00624 NM 1998 9 18 SWAA981982 1 19980902 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 468 & 474 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND TWO DENTS IN FUSELAGE SKIN AT BS 468 AND 474 BETWEEN STRINGER 22 AND 23 LT. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800625 19980918 00625 NM 1998 9 18 SWAA981983 1 19980902 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE GOUGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOORWAY FUSELAGE TORQUE TUBE CAVITY GOUGE ON INSIDE OF SKIN. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800626 19980918 00626 NM 1998 9 18 SWAA981984 1 19980902 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT STR 16L, BS 295 FWD OF FWD ENTRY DOORWAY. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091800627 19980918 00627 NM 1998 9 18 SWAA981985 1 19980902 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 428 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND DENTED INTERCOSTAL AT BS 428, LBL 45, WL 166. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800628 19980918 00628 NM 1998 9 18 SWAA981986 1 19980902 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CRACKED L-BRACKET AT BS 344, STR 12R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800629 19980918 00629 NM 1998 9 18 SWAA981987 1 19980902 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 429 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER SURFACE OF WEB AT BS 429, WL 208, RBL 70. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091800630 19980918 00630 NM 1998 9 18 SWAA981988 1 19980902 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 442 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED SKIN, LOWER FWD CORNER OF FWD CARGO DOOR CUTOUT, BS 442, RBL 32, WL 145. RE PAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800631 19980918 00631 NM 1998 9 18 SWAA981989 1 19980902 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED BRACKET AT BS 312, WL 208, LBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800632 19980918 00632 NM 1998 9 18 SWAA981990 1 19980902 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 360, WL 208, LBL 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800633 19980918 00633 NM 1998 9 18 SWAA981991 1 19980902 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 967 - 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED INTERCOSTAL AT BS 967 TO 987, LBL 3, WL 208. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998091800634 19980918 00634 NM 1998 9 18 SWAA981992 1 19980902 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500-520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED ANGLE OF FLOOR SUPPORT FROM BS 500-520, BL 0, WL 208. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091800635 19980918 00635 NM 1998 9 18 SWAA981993 1 19980902 A 5730 SKIN BOEING 737 7372T4 1384492 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND SKIN CRACKED AT NR 3 SLAT CUTOUT FOR ACTUATOR. REPAIRED PER TI-257-017. 2 L 7 2 4F A16WE 1998091800636 19980918 00636 NM 1998 9 18 SWAA981994 1 19980902 A 5320 ANGLE BOEING 737 7372T4 1384492 NM LT MLG DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND LEFT GEAR FWD, DOOR CUTOUT ANGLE CRACKED AT BS 680. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800637 19980918 00637 NM 1998 9 18 SWAA981995 1 19980903 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT LOOSE IN OVERHEAD BIN 16DEF. TIGHTENED EMERGENCY EXIT LIGHT PER B OEING MM. 2 L 7 2 4F RT A16WE 1998091800638 19980918 00638 NM 1998 9 18 SWAA981996 1 19980908 A 2612 FIRE WARNING BOEING 737 7372H4 138448C NM NR 2 ENGINE ACTIVATED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 094SW 23053 AIR TURNBACK DUE TO NR 2 ENG FIRE WARNING LT CAME ON INTERMITTANTLY INFLT. RETARDED THROTTLE, LIGHT WENT OUT. TESTED C IRCUIT TESTED OK. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED NR 2 ENG FOR EVIDENCE OF FIRE OR OVERHEAT CONDITIONS, OK TO CONTINUE PER MEL. (LG PG 190147). 2 L 7 2 4F A16WE 1998091800639 19980918 00639 NM 1998 9 18 SWAA981997 1 19980903 A 3350 BULB BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 509SW 24186 DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY FLOOR TRACK LIGHT IS INOP. RELAMPED AND OP'S CK'D GOOD PER BOEING M M. 2 L 7 2 4F RT A16WE 1998091800640 19980918 00640 NM 1998 9 18 SWAA981998 1 19980903 A 3350 LIGHT BOEING 737 7373G7 1384595 NM CABIN DETACHED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED BC4 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ASSY DETATCHED, 20 DEF. REPLACED BULLNOSE EMERGENCY EXI T LIGHT ASSY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800641 19980918 00641 NM 1998 9 18 SWAA981999 1 19980903 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED SERVICE CHECK, FOUND AFT EGRESS LIGHTING INOP. RESECURED BATTERY PACK AND CHARGED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800642 19980918 00642 NM 1998 9 18 SWAA982000 1 19980903 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 291.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE AT BS 291.5, STR 12R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800643 19980918 00643 NM 1998 9 18 SWAA982001 1 19980903 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT RBL 5.7. WL 198.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800644 19980918 00644 NM 1998 9 18 SWAA982002 1 19980903 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CANNED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN OIL CANNED AT BL 0 WL 201 TO WL 195. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800645 19980918 00645 NM 1998 9 18 SWAA982003 1 19980903 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 SKIN CRACKED AT LBL 5.7, WL 197 - 205 AND RBL 5.7, WL 201. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998091800646 19980918 00646 NM 1998 9 18 SWAA982004 1 19980903 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 305-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED Z ANGLE AT BS 305 TO 344, LBL 64. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800647 19980918 00647 NM 1998 9 18 SWAA982005 1 19980903 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 460 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP AT BS 460, STR 23L DAMAGED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800648 19980918 00648 NM 1998 9 18 SWAA982006 1 19980903 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 639 BELTFRAME I/B L-ANGLE CRACKED AT STR 17R. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091800649 19980918 00649 NM 1998 9 18 SWAA982007 1 19980903 A 5311 BELTFRAME BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND BS 639 BELTFRAME WEB CRACKED IN TWO LOCATIONS AT STR 17R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800650 19980918 00650 NM 1998 9 18 SWAA982008 1 19980903 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM AFT CARGO BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND AFT CARGO DOOR INTERCOSTAL BROKEN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800651 19980918 00651 NM 1998 9 18 SWAA982009 1 19980903 A 5330 SKIN BOEING 737 7372T4 1384492 NM LEFT AFT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722SW 22698 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED IN THE LEFT AFT SECTION BEHIND WING TO BODY FAIRING. REPAIRED PE R BOEING SRM. 2 L 7 2 4F A16WE 1998091800652 19980918 00652 NM 1998 9 18 SWAA982010 1 19980903 A 5312 DOUBLER BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND ULTRA SONIC CRACK INDICATIONS UNDER ANGLE STIFFENER FWD SIDE OF BULKHEAD RBL 12, WL 218. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800653 19980918 00653 NM 1998 9 18 SWAA982011 1 19980903 A 5312 CHORD BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND VERTICAL CHORD CRACKED AT BS 178 LBL 5.5 WL 184, AFT SIDE. REPAIRED PER BOEING TI 2 53-031. 2 L 7 2 4F A16WE 1998091800654 19980918 00654 NM 1998 9 18 SWAA982012 1 19980903 A 5320 INTERCOSTAL BOEING 737 7372T4 1384492 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND INSIDE INTERCOSTAL AT LBL 26, WL 195 CRACKED FWD END. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998091800655 19980918 00655 NM 1998 9 18 SWAA982013 1 19980903 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED 1/4 D-CHECK, FOUND 2 INCH CRACK AT STRINGER 15L AT BS 727B. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800656 19980918 00656 NM 1998 9 18 SWAA982014 1 19980904 A 3350 A3060761005 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 394SW 27380 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FWD ENTRY SLIDE SINGLE LIGHT INOP. SLIDE (P/N 61620-468) (S/N 0712A) R EPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800657 19980918 00657 NM 1998 9 18 SWAA982016 1 19980904 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800658 19980918 00658 NM 1998 9 18 SWAA982017 1 19980904 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 639 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND FRAME TO STRINGER WEB CRACKED ON BOTTOM SIDE AT BS 639, STR 15L. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800659 19980918 00659 NM 1998 9 18 SWAA982018 1 19980904 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ROW NR 3 LT INOP. RELAMPED OPS CHECK NORMAL PER BOEING M M. 2 L 7 2 4F RT A16WE 1998091800660 19980918 00660 NM 1998 9 18 SWAA982019 1 19980904 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 320SW 23341 DURING SCHEDULED A1 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT ROW NR 5 RT INOP. RELAMPED OPS CHECK NORMAL PER BOEING M M. 2 L 7 2 4F RT A16WE 1998091800661 19980918 00661 NM 1998 9 18 SWAA982020 1 19980904 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND STRINGER 16 RT AND 16 LT CRACKED AT BS 500 + 4. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1998091800662 19980918 00662 NM 1998 9 18 SWAA982021 1 19980904 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 292 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED BOTTOM SIDE OF WEB AT BS 292, WL 207, RBL 52. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800663 19980918 00663 NM 1998 9 18 SWAA982022 1 19980904 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 328, LBL 49, TO RBL 45, WL 208. REMOVED AND REPLACED PER SR M. 2 L 7 2 4F RT A16WE 1998091800664 19980918 00664 NM 1998 9 18 SWAA982023 1 19980904 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 312, RBL 23, WL 208. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800665 19980918 00665 NM 1998 9 18 SWAA982024 1 19980904 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 329 - 332 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED INTERCOSTAL AT BS 329 TO 332, RBL 24, WL 208. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800666 19980918 00666 NM 1998 9 18 SWAA982025 1 19980904 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 304 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 304, LBL 29, WL 208. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800667 19980918 00667 NM 1998 9 18 SWAA982026 1 19980904 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 328, LBL 11, WL 208. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800668 19980918 00668 NM 1998 9 18 SWAA982027 1 19980904 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 302 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED INTERCOSTAL AT BS 302, RBL 15, WL 208. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800669 19980918 00669 NM 1998 9 18 SWAA982028 1 19980904 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 325 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED AFT SUPPORT WEB AT BS 325, WL 208 FWD GALLEY DOOR. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800670 19980918 00670 NM 1998 9 18 SWAA982033 1 19980904 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 696 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED BOTTOM SIDE OF BRACKET AT BS 696, RBL 67, WL 208. REMOVED AND REPLACED PER SRM. 2 L 7 2 4F RT A16WE 1998091800671 19980918 00671 NM 1998 9 18 SWAA982029 1 19980904 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 1113 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED VERTICAL STIFFENER INTERIOR OF TORQUE BOX AT BS 1113 FWD SIDE OF APU AIR INL ET CUTOUT RBL 12. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1998091800672 19980918 00672 NM 1998 9 18 SWAA982030 1 19980904 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 1112-1124 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED HORIZONTAL STIFFENER BETWEEN BS 1112 AND BS 1124 LOWER SIDE OF APU AIR INLET CUTOUT ON TORQUE BOX RBL 13. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1998091800673 19980918 00673 NM 1998 9 18 SWAA982031 1 19980904 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 777 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED 1/4 D-CHECK, FOUND FOUR HOLES IN FLOORBEAM AT BS 777, RBL 8. REPAIRED PER SRM. 2 L 7 2 4F RT A16WE 1998091800674 19980918 00674 NM 1998 9 18 SWAA982032 1 19980904 A 3350 LIGHTS BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 715SW 27849 DURING SCHEDULED SERVICE CHECK, FOUND ROW 16 EMERGENCY LIGHTS INOP. RELAMPED LIGHT TRACK SECTION, OPS CHECK OK PER BOEI NG MM. 2 L 7 2 4F RT A16WE 1998091800675 19980918 00675 NM 1998 9 18 SWAA982034 1 19980905 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 663.75 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND FRAME UPPER FLANGE CRACKED AT BS 663.75, STR 3R. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1998091800676 19980918 00676 NM 1998 9 18 SWAA982035 1 19980905 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED SHEAR TIE AT BS 360 BETWEEN STR 14 AND 13 RT. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1998091800677 19980918 00677 NM 1998 9 18 SWAA982036 1 19980905 A 5320 DOUBLER BOEING 737 7372H4 138448C NM BS 950 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND CRACKED AT BS 950, STR 10 DOOR FRAME. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1998091800678 19980918 00678 NM 1998 9 18 SWAA982037 1 19980905 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT SEAT ROW NR 3. REMOVED AND REPLACED BATTERY PACK PER MM. 2 L 7 2 4F A16WE 1998091800679 19980918 00679 NM 1998 9 18 SWAA982038 1 19980905 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 606SW 27926 DURING SCHEDULED SERVICE CHECK, FOUND ROW 14 FLOOR TRACK LIGHTING INOP. RELAMPED PER MM. 2 L 7 2 4F RT A16WE 1998091800680 19980918 00680 NM 1998 9 18 SWAA982039 1 19980905 A 5321 FLOOR BOEING 737 7373Q8 1384670 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED 1/4 D-CHECK, FOUND FLOOR PANEL TRANSITION ANGLE CORRODED ALONG UPPER SURFACE AT BS 860, LBL 21, RBL 21. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800681 19980918 00681 NM 1998 9 18 SWAA982040 1 19980906 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CENTER SECTION FLOOR WEB CRACKED AT BS 663, LBL 22. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800682 19980918 00682 NM 1998 9 18 SWAA982041 1 19980906 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY TRACK LIGHT INOP ON ROW 15. REMOVED AND REPLACED LIGHT SOCKET PER BOEIN G MM. 2 L 7 2 4F RT A16WE 1998091800683 19980918 00683 NM 1998 9 18 SWAA982042 1 19980906 A 5320 BOW TIE BOEING 737 7373Q8 1384670 NM LT HORIZ STAB WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED 1/4 D-CHECK, FOUND LT BOW TIE WORN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800684 19980918 00684 NM 1998 9 18 SWAA982043 1 19980906 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED 1/4 D-CHECK, FOUND FWD BULKHEAD DIAGONAL SUPPORT CRACKED AT BS 727, BL 0. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998091800685 19980918 00685 NM 1998 9 18 SWAA982044 1 19980907 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 770 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED 1/4 D-CHECK, FOUND CORRODED FLOORBEAM AND SEVERAL HOLES AT BS 770, RBL 3. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998091800686 19980918 00686 NM 1998 9 18 SWAA982045 1 19980906 A 3350 BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING INT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, SYS OPS NORMAL PER BOEING MM, PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800687 19980918 00687 NM 1998 9 18 SWAA982046 1 19980907 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 758.8-761.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 056SW 21811 DURING SCHEDULED RON CHECK, FOUND 2.65 INCH CRACK AT BS 758.8 TO BS 761.5 STR 24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091800688 19980918 00688 NM 1998 9 18 SWAA982047 1 19980907 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM AT BS 773, LBL 5 CORRODED AT NUT PLATE HOLES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800689 19980918 00689 NM 1998 9 18 SWAA982048 1 19980907 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT CARGO FLOOR SUPPORT BEAM AT BS 773, RBL 5 CORRODED AT NUT PLATE HOLES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800690 19980918 00690 NM 1998 9 18 SWAA982049 1 19980907 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 338SW 23960 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD, UPPER SURFACE FWD EDGE GOUGED AT BS 986.5, WL 208, LBL 49. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800691 19980918 00691 NM 1998 9 18 SWAA982050 1 19980907 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 620SW 28036 DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK EGRESS LIGHTING INOP AT ROWS 5-9. RELAMPED EGRESS LIGHTS AT ROW 5-9 PER BO EING MM. 2 L 7 2 4F RT A16WE 1998091800692 19980918 00692 NM 1998 9 18 SWAA982051 1 19980907 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 639SW 27712 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR LIGHTS BY LEFT EMERGENCY EXIT DOOR INOP. RECONNECTED LOOSE CONNEC TIONS TO LIGHTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800693 19980918 00693 NM 1998 9 18 SWAA982052 1 19980907 A 3350 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHTS ARE MISSING AT SEATS 22DEF, 13DEF. REPAIRED WIRES AND RELAMPED LIGH TS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800694 19980918 00694 NM 1998 9 18 SWAA982054 1 19980908 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 360. CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 16L CRACKED AT BS 360. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800695 19980918 00695 NM 1998 9 18 SWAA982055 1 19980908 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED RAMER ANGLE AT BS 294.5 STR 5-7R IN TOP CORNER. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998091800696 19980918 00696 NM 1998 9 18 SWAA982056 1 19980909 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED DOUBLER AT BS 663, RBL 65. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800697 19980918 00697 NM 1998 9 18 SWAA982057 1 19980909 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED DOUBLER BS 663, LBL 65. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800698 19980918 00698 NM 1998 9 18 SWAA982058 1 19980909 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 375 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB ATTACH T-ANGLE CRACKED AT BS 375, STR 17L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800699 19980918 00699 NM 1998 9 18 SWAA982059 1 19980909 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 360 - 380 BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB BENT AT STR 17L BETWEEN BS 360 AND 380. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800700 19980918 00700 NM 1998 9 18 SWAA982060 1 19980909 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 927-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND RT Z-ANGLE CORRODED ON SURFACE FROM BS 927-1016. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800701 19980918 00701 NM 1998 9 18 SWAA982061 1 19980909 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN CRACKED AT BS 727, STR 19R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800702 19980918 00702 NM 1998 9 18 SWAA982062 1 19980909 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND SKIN CORRODED AT DME ANT FWD CARGO LOWER SKIN. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800703 19980918 00703 NM 1998 9 18 SWAA982063 1 19980909 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 706 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT BELTFRAME BS 706, STR 11R AND BS 727A, STR 15R. REMOVED AN D REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800704 19980918 00704 NM 1998 9 18 SWAA982064 1 19980909 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 667 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 667 STR 10R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800705 19980918 00705 NM 1998 9 18 SWAA982065 1 19980909 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED AT CLIP NUT HOLE AT BS 986, RBL 44. REMOVED AND REPLACED PER TYPICAL REPAI R TI-A53-014. 2 L 7 2 4F RT A16WE 1998091800706 19980918 00706 NM 1998 9 18 SWAA982066 1 19980909 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 640SW 27713 DURING SCHEDULED SERVICE CHECK, FOUND LAST THREE EMERGENCY EXIT FLOOR LIGHTS IN CABIN INOP. RESECURED WIRE AND LIGHTS O PS CK OK. 2 L 7 2 4F RT A16WE 1998091800707 19980918 00707 NM 1998 9 18 SWAA982067 1 19980908 A 5320 WEB BOEING 737 7373Q8 1384670 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 688SW 23254 DURING SCHEDULED 1/4 D-CHECK, FOUND WEB DAMAGED AT FWD LOWER CORNER OF AFT CARGO DOORWAY. REPAIRED PER TII-A53-35. 2 L 7 2 4F RT A16WE 1998091800708 19980918 00708 NM 1998 9 18 SWAA982068 1 19980908 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 727-747 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 695SW 23506 DURING SCHEDULED SERVICE CHECK, FOUND GOUGE IN ACFT SKIN ON RT SIDE BETWEEN BS 727 AND 747 BETWEEN STR 24R AND 23R. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800709 19980918 00709 NM 1998 9 18 SWAA982069 1 19980908 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED SERVICE CHECK, FOUND ROW 12 TO 15 FLOOR TRACK LIGHTING INOP. RECONNECTED LOOSE WIRES PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800710 19980918 00710 NM 1998 9 18 DHL98712007 1 19980911 A 5610 SPRING BOEING 727 72729 1384007 NM L-2 WINDOW OUT OF POSITION A DHLA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 712DH 19401 ON CLIMBOUT AT APPROX 24,000, THE L-2 WINDOW SPARKED AND POPPED REPEATEDLY AND EMMITTED SMOKE. EMERGENCY PROCEDURES AC COMPLISHED, DIVERTED TO IAD AND EVACUATED AIRCRAFT. FOUND SPRING HOLD DOWN FOR LEFT SLIDING WINDOW INTERFERRING WITH LEAD. REPOSITIONED SPRING, OPS CHECK SYSTEM PER MM 30-41-01. 2 L 7 3 4F A3WE 1998091800711 19980918 00711 NM 1998 9 18 UPS98427666 1 19980912 A 3350 LIGHT BOEING 747 747212B 1384886 NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 INSPECTION TYPE:W, END EEL ABOVE ESCAPE HATCH DOOR IN COCKPIT INOP, NR X325-X326. CLEANED CONECTOR, OP'S CHECK NORMAL. 2 L 7 4 4F A20WE 1998091800712 19980918 00712 NM 1998 9 18 UPS98627672 1 19980911 A 5310 STRUCTURE BOEING 767 76734AF 1385212 NM AIRFRAME DAMAGED A IPXA K NONE O OTHER LD LANDING 1 SO 01 316UP 27744 ON LANDING, A/C SKIDDED OFF THE RUNWAY. THE A/C HAS STRUCTURAL DAMAGE TO THE RT MAIN GEAR WELL AREA, RT WING FWD AND TR AILING EDGES, RT PYLON, AND ENGINE AREAS, FOUND AT THIS TIME MORE DETAILS TO COME AS THEY BECOME AVAILABLE. 2 L 7 2 4F RT A1NM 1998091800713 19980918 00713 WP 1998 9 18 UPS98827667 1 19980905 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE:PRFL, EEL FAILED CHECK ON PRE-FLIGHT. REMOVED AND REPLACED EMERGENCY BATT PACK. 2 L 7 4 4F RT 4A25 1998091800714 19980918 00714 WP 1998 9 18 UPS98827668 1 19980831 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 258 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C, LT WING L/E AY STA XW258.00 IS CRACKED AT A FASTENER HOLE. REPAIRED AREA IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998091800715 19980918 00715 WP 1998 9 18 UPS98827669 1 19980831 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 360.25 & 379 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C, LT WING L/E UPPER SKIN AT STA XFS 360.250 AND XFS 379.000 IS CRACKED AT 2 FASTENERS. REPAIRED AREAS IAW DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 1998091800716 19980918 00716 WP 1998 9 18 UPS98827670 1 19980901 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 484.895 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C, LT WING L/E RIB AT STA XS484.895 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998091800717 19980918 00717 WP 1998 9 18 UPS98827671 1 19980901 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 572.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C, LT WING L/E LWR SKIN IS CRACKED AT STA XFS572.500, JUST AFT OF THE DRAIN HOLE. STOP DRILLED CRACK AN D REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998091800718 19980918 00718 WP 1998 9 18 UPS98827673 1 19980901 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 709.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE:C, LT WING L/E SKIN AT STA XFS 709.500 HAS HEAVY CORROSION AND IS CRACKED AT THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 28. 2 L 7 4 4F RT 4A25 1998091800719 19980918 00719 WP 1998 9 18 UPS98827674 1 19980828 A 5720 97532937 ANGLE DOUG DC8 DC871F 302199D WP WS 246.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE:C, LT WING L/E I/B SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM, (STA.XS246.089). REMOVED AND REPLACED ANGLE IAW DWG 9753293. 2 L 7 4 4F RT 4A25 1998091800720 19980918 00720 WP 1998 9 18 MWEA98960 1 19980910 A 3350 6011777 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 FOUND RIGHT NACELLE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED RIGHT NACELLE EMERGENCY LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1998091800721 19980918 00721 NM 1998 9 18 DL72S981868 1 19980909 A 5720 STIFFENER BOEING 727 727232 1384082 NM LE SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 FOUND ON F1 LETTER CK, NR 6 SLAT O/B TRACK O/B SPAR STIFFENER CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998091800722 19980918 00722 NM 1998 9 18 DLM11981869 1 19980909 A 3350 BATTERY PACK 6044113 DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 809DE 00040395 48480 EMER LIGHTS BATTERY PACKS 2 AND 4 FAIL TEST. REPLACED BATTERY PACKS 2 AND 4. ALL CHECKS GOOD PER M/M. 2 L 7 3 4F RT A22WE 1998091800723 19980918 00723 NM 1998 9 18 DL73K981870 1 19980909 A 3350 20131A BATTERY PACK BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 308DL 23080 AFT RIGHT SERVICE DOOR SLIDE LIGHT INOP. REPLACED BATTERY PACK. CKS GOOD. 2 L 7 2 4F RT A16WE 1998091800724 19980918 00724 NM 1998 9 18 DLM88981874 1 19980910 A 4920 APU DOUG MD88 MD88 3023688 NM AFT FUSELAGE LEAKING A DALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TO TAKEOFF 1 SO 27 904DE 6190 53409 UNK AFTER T/O, CABIN FILLED WITH ENOUGH HAZE TO SETOFF ALL LAV SMOKE DETECTORS. FLT ATTENDANT REPORTED NO SMOKY SMELL, JUST HAZE IN CABIN, ALSO REPORTED ON SHORT FINAL WITH POWER CHANGES. FOUND APU OIL LEAKING INTO INLET FWD TO MCO/PLAC PER M EL 49-00-01A. RAN BOTH ENGINES AT TAKEOFF PWR. RAN PACKS ISOLATED BLEEDS, ALL CHECKED OK FOR SERVICE. 2 L 7 2 4F RT A6WE 1998091800725 19980918 00725 NM 1998 9 18 DL72S981875 1 19980910 A 5400 DUCT BOEING 727 727232 1384082 NM PYLON BENT A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 DOGHOUSE AFT LIP, ON AIRINTAKE DUCT 360 DEGREES AREA, BENT AND DISTORTED. HEAVY ACCUMULATION OF SEALER. REMOVED DAMAGE DOUBLER, BEGAN DRILLING NEW DOUBLER. COMPLETED FABRICATION OF NEW DOUBLER PER SRM 54-10-3 FIG 13 D. OK TO INSTALL DOU BLER. INSTALLED REPAIR PER SRM 54-10-3 FIG 13. 2 L 7 3 4F A3WE 1998091800726 19980918 00726 NM 1998 9 18 DL72S981876 1 19980910 A 5280 DOOR BOEING 727 727232 1384082 NM NLG DEPARTED A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 528DA 21702 NOSE GEAR DOORS TORN FROM ACFT ON GEAR RETRACTION. REPLACED DOORS. REPAIRED NR 2 AND NR 3 SLATS. REPAIRED HOLE IN FUS ELAGE. REPLACED CUT TIRE. 2 L 7 3 4F A3WE 1998091800727 19980918 00727 NM 1998 9 18 DLM88981878 1 19980910 A 2130 PRESSURE SYST DOUG MD88 MD88 3023688 NM CABIN MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 938DL 49811 ON CLIMB-OUT, LOST CABIN PRESSURE, THE PACKS OVER TEMPED AND SHUT OFF. THE A/C DECREASED ALT AND RETURNED TO PHX. FOU ND NO DUCT LEAKS. BOTH PACKS OPERATED NORMAL. PRESSURIZEDTO 5 PSID WITH EACH PACK, THEN WITH BOTH PACKS. REPAIRED THE A/C FOR FERRY FLT TO DFW FOR OXY CANISTER MTC. 2 L 7 2 4F RT A6WE 1998091800728 19980918 00728 NM 1998 9 18 DL72S981880 1 19980910 A 5511 RIB BOEING 727 727232 1384082 NM LT HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 LT ELEV HINGE SUPPORT RIB CRACKED, ELEV STA 99.79 AFT I/B END. REPAIRED PER MM 55-10-31 FIG 802. 2 L 7 3 4F A3WE 1998091800729 19980918 00729 NM 1998 9 18 DL72S981881 1 19980910 A 5311 FRAME BOEING 727 727232 1384082 NM BS 910 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 482DA 20862 REF SHIP NR 482, TPA, LETTER CHK D2, CRACK AT STA 910 FRAME FWD OUTBOARD RADIUS. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998091800730 19980918 00730 NM 1998 9 18 DL72W981884 1 19980909 A 5330 65545662 SKIN BOEING 727 727247 138408F NM BS 620 DAMAGE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 DURING REPLACEMENT OF BELLY SKIN, A FASTENER HOLE SUSTAINED TOOLING DAMAGE NEAR THE C-1 DOOR CUTOUT. REPAIR PER ERA 332 149-14. 2 L 7 3 4F A3WE 1998091800731 19980918 00731 NM 1998 9 18 DL767981885 1 19980910 A 5730 111T30131 SKIN BOEING 767 767232 1385132 NM CENTER WING CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 113DA 22225 CORROSION DAMAGE WAS FOUND DURING ROUTINE INSPECTION OF THE CENTER WING UPPER SKIN OVERLYING THE REAR SPAR. CORROSION W AS LOCATED AT LBL 68 NEAR THE DRAIN AT LBL 75. REPAIRED PER ERA 332134-14. 2 L 7 2 4F RT A1NM 1998091800732 19980918 00732 NM 1998 9 18 DL767981886 1 19980909 A 5315 FLOORBEAM BOEING 767 767232 1385132 NM BS 835-910 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 113DA 22225 CORROSION WAS FOUND ON THE UPPER CAP OF THE RBL 33 LONGITUDINAL OVERWING FLOORBEAM BETWEEN FS 835 AND 910. A SECTION OF UPPER CAP WILL BE REPLACED WITH A SPLICE REPAIR ON EACH END OF THE REPLACEMENT SECTION. REPAIRED PER ERA 332139-14. 2 L 7 2 4F RT A1NM 1998091800733 19980918 00733 NM 1998 9 18 DL72W981887 1 19980811 A 5754 HEAT SHIELD BOEING 727 727247 138408F NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 CRACKS IN HEAT SHIELD, NR 6 LE SLAT, ONE IS JUST OUTBOARD OF ACTUATOR ATTACH RIB, THE OTHER IS JUST OUTBOARD OF OUTBOARD TRACK. MANUFACTURED AND INSTALLED DOUBLERS ON HEAT SHIELD SKIN PER MM 57-54-0 FIG 803A. MANUFACTURED AND INSTALLED DO UBLER ON HEAT SHIELD SKIN PER MM 57-54-0 FIG 803A. STOP DRILLED AREAS. OK TO INSTALL DOUBLERS. 2 L 7 3 4F A3WE 1998091800734 19980918 00734 NM 1998 9 18 DL72S981888 1 19980911 A 2612 FIRE LOOP BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 2 ENGINE FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 496DA 21076 700797 ENG NR 2 FIRE WARNING CAME ON DURING CLIMB-OUT SHORTLY AFTER T/O, LIGHT STAYED ON AFTER GOING OUT INITIALLY. FOLLOWING THROTTLE BEING REDUCED TO IDLE. SHUT DOWN ENG. BOTH BOTTLES DISCHARGED. REPLACED FIREWALL LOOP, CKS OK. NO FIRE. 2 L 7 3 4F 4 F A3WE E2EA 1998091800735 19980918 00735 NM 1998 9 18 DL767981889 1 19980911 A 3350 BATTERY PACK BPS73 BOEING 767 767232 1385132 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 106DA 42513 22218 MSU T/S EMERGENCY LIGHT PROBLEM. FOUND M735 BATTERY CHARGER BAD. REPLACED CHARGER AND BATTERY PACK. CKS NML. 2 L 7 2 4F RT A1NM 1998091800736 19980918 00736 NM 1998 9 18 DL76L981891 1 19980911 A 3397 WIRE BOEING 767 767332 1382001 NM CABIN BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 199DN 28456 SEAT MOUNTED EMERGENCY LIGHT AT 29F INOP. WIRES BROKEN IN AREA OF UNDERSEAT BAGGAGE STORAGE. SPLICED WIRES AND RELOCAT ED. 2 L 7 2 4F RT A1NM 1998091800737 19980918 00737 1998 9 18 DL73E981894 4 19980912 A 2350 AUDIO ACC UNIT 655280479 BOEING 737 7372S3 NM E/E COMPT FAILED A DALA O OTHER O OTHER CL CLIMB 1 SO 27 367DL M01020 21774 COMM RADIO FAILURE IN FLIGHT OCCURED 5 MIN AFTER T/O. RADIOS RESTORED AFTER APU STARTED AND TRANSFERED NR 2 BUS TO AP U. RAN ENGS ALL COMRADIOS CK GOOD. INSPECTED STATIC WICKS AND ANTS. ALL OK. REPLACED AUDIO ACC UNIT. ALL RADIO FUNC TIONS NORMAL. 2 L 7 2 4F RT A16WE 1998091800738 19980918 00738 NM 1998 9 18 DL72S981896 1 19980913 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 528DA 21702 FOUND ON L/O CK, NR 4 SLAT O/B ACTUATOR ATTACH RIB CRACKED AT FWD END. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998091800739 19980918 00739 NE 1998 9 18 DL72S981899 2 19980913 A 7320 714810 P & D VALVE BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A DALA K NONE X ENGINE FLAMEOUT CR CRUISE 1 SO 27 400DA 21144 111797 NR 3 ENG FAILED INITIALLY FELT SLIGHT SWERVE AND EPR DROPPED WHEN THE THROTTLE WAS ADVANCED. THE ENG CONTINUED TO SPOOL DOWN TO WINDMILLING. REPLACED P/D VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998091800740 19980918 00740 NM 1998 9 18 DL757981900 1 19980912 A 5510 182N720171 FAIRING BOEING 757 757232 1384965 NM LT HORIZ STAB GAPPED A DALA K NONE E VIBRATION/BUFFET CL CLIMB 1 SO 27 645DL 24216 AIRFRAME BUFFET AFTER TAKEOFF. WORSE WITH INCREASE IN ALT AND SPEED FELT THROUGH CONTROLS FIRST THEN UP THROUGH SEAT. F /A FELT ALL THE WAY TO BACK OF PLANE. INSPECTED FUSELAGE AND WINGS INCLUDING FLT CONTROLS AND FLAPS AND ALSO EMPENNAGE. FOUND LT LWR STAB FAIRING GAPPED, SHIMMED FAIRING. PERFORMED TEST FLT PER SP 4080, NO DISCREPANCIES NOTED BY FLT CREW OR INSPECTOR DURING TEST FLT. 2 L 7 2 4F RT A2NM 1998091800741 19980918 00741 NM 1998 9 18 DL72S981902 1 19980823 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 STRINGER CRACKED. VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 157.2 STR 8L. CRACK RAN FROM CTR OF HOLE TO EDGE OF STRINGER. FABRICATED REPAIR ANGLE PER MM 55-30-0 FIG 803 OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 FI G 803. 2 L 7 3 4F A3WE 1998091800742 19980918 00742 NM 1998 9 18 DL72S981903 1 19980823 A 5530 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 STRINGER CRACKED VERTICAL STAB INTERIOR, STRINGER CRACKED AT FIN STA 180.6 STA 9L. CRACK RUNS FROM HOLE TO EDGE OF PART . NO STOP DRILL REQUIRED. FABRICATED REPAIR PER M/M 55-30-0 FIG 803. IK INSTALL. BEGAN INSTALL OF REPAIR PER M/M 55- 30-0 FIG 803. FINISHED INSTALL OF REPAIR PER M/M 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1998091800743 19980918 00743 NM 1998 9 18 DL72W981904 1 19980913 A 2782 ACTUATOR 269002917 BOEING 727 727247 138408F NM NR 1 LE SLAT FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 2814W DL483X 20870 AFTER T/O, LOST 'A' SYS HYD QTY AND PRESS IND ZERO. PROCEDURES COMPLIED WITH ALT FLAP SW USED GPWS INHIBITED. GEAR PIN INSTALLED BY MTC. REMOVED AND REPLACED NR 1 SLAT ACT. OPS AND LEAK CKS GOOD. 2 L 7 3 4F A3WE 1998091800744 19980918 00744 NM 1998 9 18 TWAA9814701 1 19980910 A 3350 582243 BATTERY PACK BOEING 767 767231 1385131 NM CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 610TW 22573 EGRESS LIGHTS WERE REPORTED AS FLASHING WITH SWITCH IN ARMED POSITION. REPLACED BATTERY PACK. CHECK-C 6-14-98 LAX. 2 L 7 2 4F RT A1NM 1998091800745 19980918 00745 WP 1998 9 18 TWAA9814702 1 19980910 A 3350 58222 POWER SUPPLY DOUG DC9 DC915 3022036 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 969Z 47001 FLOOR EGRESS LIGHTS REPORTED INOP ROWS 12 TO 16. REPLACED POWER SUPPLY. CHECK-C 11-22-97 STL. 2 L 7 2 4F A6WE 1998091800746 19980918 00746 NM 1998 9 18 TWAA9814703 1 19980911 A 3350 58224 BATTERY PACK BOEING 767 767231 1385131 NM CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 608TW 22571 ESCAPE PATH LIGHTS IN RT AISLE ROWS 8 TO 45 ILLUMINATED INTERMITTENTLY. REPLACED RT EGRESS LIGHT BATTERY PACK. CHECK-C 8-1-98 LAX. 2 L 7 2 4F RT A1NM 1998091800747 19980918 00747 WP 1998 9 18 TWAA9814704 1 19980912 A 5610 5912290501 WINDSHIELD DOUG DC9 DC932 3022066 WP LT COCKPIT CRACKED A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 923L 47109 THE CAPTAIN'S NR 1 WINDOW CRACKED WITH ARCING VISIBLE. FLIGHT RETURNED TO STL. REPLACED WINDOW. CHECK-C 3-2-98 STL. 2 L 7 2 4F A6WE 1998091800748 19980918 00748 WP 1998 9 18 TWAA9814705 1 19980912 A 4990 3812761 OIL SYST DOUG DC9 DC982 3022082 WP APU OVERSERVICED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 954U 49426 IN CLIMB EXPERIENCED HEAVY BURNING SMELL IN ACFT. TURNED OFF RT PACK. SMELL RETURNED WHEN WAITING FOR A GATE ON THE GR OUND. FOUND OIL LEAKING ON INLET SIDE OF APU DUCT. PLACARDED APU INOP. LATER CLEANED APU COMPT AND SURROUNDING AREA. RAN APU FOR 2 HOURS AND NO LEAKS OR ODOR. POSSIBLE SERVICING PROBLEM. CHECK-C 8-2-98 STL. 2 L 7 2 4F A6WE 1998091800749 19980918 00749 WP 1998 9 18 TWAA9814706 1 19980603 A 5321 FLOOR DOUG DC9 DC982 3022082 WP BS 921 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 940AS 49825 DURING OP 16 MAINT CHECK, FOUND CABIN FLOOR MEMBRANE CORRODED AND CRACKED AT FS 921, RBL 58. REMOVED CORROSION PER SRM 51-10-3. INSTALLED DOUBLER REPAIR PER SRM 53-01 PAGE 8. 2 L 7 2 4F A6WE 1998091800750 19980918 00750 WP 1998 9 18 TWAA9814707 1 19980911 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND LONGERON 4L CRACKED AT STA 200. REPLACED LONGERON USING FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 1998091800751 19980918 00751 WP 1998 9 18 TWAA9814708 1 19980911 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 200-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 CHAIR TRACK GROUND BEYOND LIMITS TO REMOVE CORROSION AT STA 200 TO 237, RBL 23 IN. REMOVED CHAIR TRACK AND REPLACED WIT H NEW TRACK. INSTALLED WITH FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 1998091800752 19980918 00752 WP 1998 9 18 VJ9800377 1 19980912 A 3520 11503911 MANIFOLD DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA G O2 MASK DEPLOYED O OTHER IN INSP/MAINT 1 SO 15 945VV 47238 ALL PASSENGER OXYGEN MASKS DEPLOYED WHEN CREW TURNED ON OXYGEN. REPLACED REGULATOR (P/N 900-002-007-6), (S/N 425). SUS EQUENTLY REPACKED MASKS AND PERFORMED OXYGEN MASK DROP AND ALL EXCEPT PASSENGER SEAT ROW 24DEF SUCESSFULLY DEPLOYED. RE PLACED PASSENGER OXYGEN MANIFOLD (P/N 115039-11), (SN 11578) AND REPACKED OXYGEN MASKS, OPS CHECKED GOOD IAW MM 35-00. 2 L 7 2 4F A6WE 1998091800753 19980918 00753 WP 1998 9 18 VJ9800378 1 19980913 A 3350 S103 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 923VV 47529 EMERGENCY LIGHTS ABOVE TAIL CONE SLIDE DIDN'T ILLUMINATE. REPLACED NICAD BATTERIES IN EMERGENCY BATTERY PACK, OPS CHECK ED GOOD. 2 L 7 2 4F A6WE 1998091800754 19980918 00754 WP 1998 9 18 VJ9800379 1 19980913 A 2612 207865 CONNECTOR DOUG DC9 DC932 3022066 WP NR 1 ENGINE DIRTY A ZZDA O OTHER N FALSE WARNING CR CRUISE 1 SO 15 967VV 47170 NR 1 ENGINE B-LOOP LIGHT ILLUMINATED IN FLIGHT, A-LOOP OK. CLEANED ELECTRICAL CONNECTOR ON NR 1 ENGINE IAW MM 26-00, OP S CHECKED GOOD. 2 L 7 2 4F A6WE 1998091800755 19980918 00755 WP 1998 9 18 VJ9800380 1 19980914 A 3350 60030451 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 924VV 47278 RT AND LT EXIT SIGNS AT OVERWING DO NOT ILLUMINATE. REPLACED BATTERY POWER SUPPLY IAW MM 33-53. 2 L 7 2 4F A6WE 1998091800757 19980918 00757 NM 1998 9 18 AWXA9800203 1 19980905 A 3230 2670296M1 SEQUENCE VALVE BOEING 757 757225 1384959 NM NLG FAILED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 914AW 22208 ON TAKEOFF DURING GEAR RETRACTION, LEFT HYDRAULIC SYSTEM FLUID LOST EICAS MESSAGE. AIR TURNBACK TO LAS. REMOVED AND RE PLACED NOSE GEAR SEQ VALVE ASSEMBLY IN ACCORDANCE WITH BMM 32-34-06. AIRCRAFT INSPECTED AND FOUND SAFE FOR FLIGHT. 2 L 7 2 4F RT A2NM 1998091800758 19980918 00758 NM 1998 9 18 CALA9801699 1 19980910 A 5753 TRACK BOEING 727 727224 1384076 NM NR 5 TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD LUG AREA CORRODED. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57-40-0 0. 2 L 7 3 4F A3WE 1998091800759 19980918 00759 NM 1998 9 18 CALA9801700 1 19980910 A 5720 PAD BOEING 727 727224 1384076 NM NR 3 FLAP TRACK CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND BOTTOM SURFACE OF SPOILER BEAM PAD CORRODED WHERE NR 3 FLAP TRACK MOUNTS. THE FLAP TRACK MOUNT PAD WAS REMOVED AND REPLACED IAW SRM 51-10-2, PAGE 1 AND 51-30-2, PAGE 14. 2 L 7 3 4F A3WE 1998091800760 19980918 00760 NM 1998 9 18 CALA9801701 1 19980910 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FUSELAGE SKIN AND RIB DENTED JUST AFT OF NLG AFT DOOR. THE RIB AND SKIN WERE REMOVED AND REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998091800761 19980918 00761 NM 1998 9 18 CALA9801702 1 19980910 A 5753 RIB BOEING 727 727224 1384076 NM LT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 1.5 INCH CRACK IN LT O/B MIDFLAP O/B END RIB FORWARD OF MID SPAR. THE CRACK WAS STOP DRILLED. A DOU BLER ANGLE WAS INSTALLED IAW SRM 51-30-2, PAGE 4. 2 L 7 3 4F A3WE 1998091800762 19980918 00762 NM 1998 9 18 CALA9801703 1 19980910 A 5753 DOUBLER BOEING 727 727224 1384076 NM LT I/B FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .5 INCH CRACK IN DOUBLER INSIDE LT INBOARD FLAP AT AFT END OF INBOARD FLAP TRACK CARRIAGE SPINDLE CUT OUT. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998091800763 19980918 00763 NM 1998 9 18 CALA9801704 1 19980910 A 2782 BRACKET BOEING 727 727224 1384076 NM LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .5 INCH CRACK IN BRACKET WHERE RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNTS. THE BRACKET WAS REMOV ED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-40-3, 51-30-2, AND 51-10-2. 2 L 7 3 4F A3WE 1998091800764 19980918 00764 NM 1998 9 18 CALA9801705 1 19980910 A 5720 ANGLE BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 4 INCH CRACK IN ANGLE AND DOUBLER AT RT WING FIXED LEADING EDGE RIB AT SLAT STA 0. THE DOUBLER WAS R EMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-30-2, 51- 10-2, AND 51-40-3, FIGURE 1. 2 L 7 3 4F A3WE 1998091800765 19980918 00765 WP 1998 9 18 CALA9801706 1 19980910 A 5523 TAB DOUG DC9 DC982 3022082 WP RT ELEVATOR DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND RT ELEVATOR GEAR TAB DELAMINATED. THE RT ELEVATOR GEAR TAB WAS REMOVED AND REPLACED IAW MM 27-30-04. 2 L 7 2 4F A6WE 1998091800766 19980918 00766 WP 1998 9 18 CALA9801707 1 19980910 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 218-275 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 49117 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 218 TO 275, LONGERON 17-18L. REPAIRED IAW ECRA 5330-02445. 2 L 7 2 4F A6WE 1998091800767 19980918 00767 NM 1998 9 18 CALA9801708 1 19980910 A 5753 SKIN BOEING 737 7372C0 1384488 NM LT TE FOREFLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND LT INBOARD FOREFLAP GOUGED IN TWO PLACES AT INBOARD SIDE. THE GOUGED AREAS WERE TRIMMED OUT. AN ADHES IVE PRIMER AND BONDED FIBERGLASS REPAIR WAS INSTALLED IAW SRM 51-40-6, 51-40-9, AND MM 51-20-11. 2 L 7 2 4F A16WE 1998091800768 19980918 00768 NM 1998 9 18 CALA9801709 1 19980910 A 5320 STRAP BOEING 727 727232 1384082 NM BS 930 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN LT FUSELAGE SPLICE STRAP AT STA 930, WL 228. THE SPLICE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800769 19980918 00769 NM 1998 9 18 CALA9801710 1 19980910 A 5330 PANEL BOEING 727 727232 1384082 NM BS 530-560 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT TRANSITION PANEL CORRODED IN FORWARD CARGO COMPARTMENT AT STA 530-560. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-20-1, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800770 19980918 00770 NM 1998 9 18 CALA9801711 1 19980910 A 7110 COWL BOEING 737 7372C0 1384488 NM NR 2 ENGINE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE IN NR 2 ENGINE INBOARD ENGINE COWL. THE CRACKED AREA WAS CUT OUT IAW S RM 51-40-2. TWO REPAIR DOUBLERS WERE INSTALLED IAW SRM 51-40-2 AND 51-30-0. 2 L 7 2 4F A16WE 1998091800771 19980918 00771 NM 1998 9 18 CALA9801712 1 19980910 A 5321 FLOOR BOEING 737 7372C0 1384488 NM CARGO COMPT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A 1 INCH CRACK AT SCREW IN FLOOR PANEL AT AFT CARGO COMPARTMENT DOOR ENTRANCE. THE FLOOR PANEL WAS REM OVED IAW SRM 51-30-2. A REPAIR WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-11. THE FLOOR PANEL WAS REINSTALLE D IAW SRM 51-30-2. 2 L 7 2 4F A16WE 1998091800772 19980918 00772 WP 1998 9 18 CALA9801713 1 19980911 A 5720 BEAM DOUG DC10 DC1030 3023501 WP RT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND CORROSION IN UPPER HOLES OF RT MLG WING ATTACH BEAM. REPAIRED IAW DOUGLAS DRAWINGS 90-57-1017 AND 90-5 7-1018. 2 L 7 3 4F A22WE 1998091800773 19980918 00773 WP 1998 9 18 CALA9801714 1 19980911 A 5720 BEAM DOUG DC10 DC1030 3023501 WP LT WING CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND CORROSION IN BOLT HOLES OF LT MLG ATTACH BEAM. REPAIRED IAW DOUGLAS DRAWINGS 90-57-1017 AND 90-57-1018 . 2 L 7 3 4F A22WE 1998091800774 19980918 00774 WP 1998 9 18 CALA9801715 1 19980911 A 5320 ANGLE DOUG DC10 DC1030 3023501 WP BS 1894 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND FLOORBOARD SUPPORT ANGLES CORRODED AT STA 1894. REPAIRED IAW SRM 53-60-01. 2 L 7 3 4F A22WE 1998091800775 19980918 00775 NM 1998 9 18 CALA9801716 1 19980912 A 5720 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN OUTBOARD TRAILING EDGE ATTACH ANGLE AT RT WING NR 8 FLAP TRACK. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-40-3, 51-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800776 19980918 00776 NM 1998 9 18 CALA9801717 1 19980912 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 380 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 380, RBL 44 TO RBL 60. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED A ND A NEW SECTION OF FLOORBEAM AND SPLICE ANGLES WERE INSTALLED IAW SRM 53-10-8, FIGURE 9, 51-20-4, AND 51-10-2. 2 L 7 3 4F A3WE 1998091800777 19980918 00777 NM 1998 9 18 CALA9801718 1 19980912 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN BOTH INBOARD AND OUTBOARD RIBS OF NR 4 SLAT AT ACTUATOR ROD END ATTACH POINT. THE A CCESS PANEL ON NR 4 SLAT WAS REMOVED IAW SRM 51-30-2. THE CRACKED RIBS WERE REMOVED IAW SRM 51-30-2. NEW RIBS WERE INS TALLED IAW SRM 51-30-4 AND 51-30-2. THE ANTI-ICE DUCTS AND ACCESS PANEL WERE REINSTALLED IAW MM 30-11-81 AND SRM 51-30- 2. 2 L 7 3 4F A3WE 1998091800778 19980918 00778 WP 1998 9 18 9810051160 1 19980901 A 5320 SUPPORT DOUG DC10 DC1040 3023508 WP BS 999 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 160US 46769 DURING M-CHECK, FOUND CORROSION ON THE FLOOR SUPPORT ON FRAME 999 ABOVE STR 44L. REPAIRED PER EA 11-160661. 2 L 7 3 4F A22WE 1998091800779 19980918 00779 WP 1998 9 18 9810069998 1 19980908 A 5311 FRAME DOUG DC9 DC931 3022065 WP BS 908 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 952N 47073 DURING PERIODIC CHECK, FOUND HOLE PUNCHED IN FRAME AND CRACK SURROUNDING HOLE AT FS 908, LONGERON 11R. INSTALLED REPAIR DOUBLER PER SRM 51-30-5 AND EA 99-159316. 2 L 7 2 4F A6WE 1998091800780 19980918 00780 EA 1998 9 18 COMA9860257 1 19980910 A 2750 860D10018 FECU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 716CA 284 7250 FLAPS FAILED AFTER TAKEOFF. REPLACED THE FECU. 2 L 7 2 4F RT A21EA 1998091800781 19980918 00781 EA 1998 9 18 COMA9860258 1 19980910 A 2760 4916405 SECU CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 01 916CA 197 7014 CONFIG SPOILER WARNING DURING TAKEOFF. REPLACED THE LT AND RT SECU. 2 L 7 2 4F RT A21EA 1998091800782 19980918 00782 EA 1998 9 18 COMA9860259 1 19980910 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A COMA K NONE J WARNING INDICATION AP APPROACH 1 SO 01 719CA 7253 FLAPS FAILED WHEN SELECTED FOR LANDING. COULD NOT DUPLICATE PROBLEM. REPLACED LT BPSU FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1998091800813 19980918 00813 NE 1998 9 18 98ZZZX3372 2 19980512 A 7250 ROTOR ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TURBINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 2140 501 7127 LE45305E FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES : 4,571.4. 1 G 7 2 3U 3 U H13EU E5NE 1998091800814 19980918 00814 NE 1998 9 18 98ZZZX3373 2 19980305 A 7250 430144801 SEAL BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 128HH 257 81950391 7036 LE45254EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800815 19980918 00815 EU 1998 9 18 98ZZZX3374 1 19980704 A 7714 430106102 PICKUP BOLKMS 117 BK117A3 5626015 EU NR 2 ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 339 97A0198 7058 PICKUP UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998091800816 19980918 00816 EU 1998 9 18 98ZZZX3375 1 19980228 A 7714 430135601 PICKUP BOLKMS 117 BK117A3 5626015 EU NR 2 ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 406 6099117 7104 PICKUP REJECTED PER SB 0163 (IMPROPER MARKINGS AND POSSIBLE REVERSE POLARITY). REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U H13EU 1998091800817 19980918 00817 EU 1998 9 18 98ZZZX3376 1 19980228 A 7714 430135601 PICKUP BOLKMS 117 BK117A3 5626015 EU NR 2 ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 406 6099134 7104 PICKUP REJECTED PER SB 0163 (IMPROPER MARKINGS AND POSSIBLE REVERSE POLARITY). REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U H13EU 1998091800818 19980918 00818 EU 1998 9 18 98ZZZX3377 1 19980519 A 7714 430135601 PICKUP BOLKMS 117 BK117A3 5626015 EU NR 2 ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 591 971907800400 7104 PICKUP HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998091800819 19980918 00819 EU 1998 9 18 98ZZZX3378 1 19980519 A 7714 430135601 PICKUP BOLKMS 117 BK117A3 5626015 EU NR 2 ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 591 971907800389 7104 PICKUP HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998091800820 19980918 00820 NE 1998 9 18 98ZZZX3379 2 19980519 A 7250 430124203 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SECT PITTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 353 1607 7104 LE45218EA BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800821 19980918 00821 NE 1998 9 18 98ZZZX3380 2 19980401 A 7240 413102002 CURL BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE COMB CHAMBER BURNT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 128HH 349 7036 LE45205E CURL ASSY HAS EXCESSIVE BURN IN SOME AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800822 19980918 00822 NE 1998 9 18 98ZZZX3381 2 19980515 A 7240 413102002 CURL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COMB CHAMBER BURNT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 118LF 673 7137 LE45135EA CURL ASSY HAS EXCESSIVE BURN IN SOME AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. CORE SCRAPPED LOCALLY. 1 G 7 2 3U 3 U H13EU E5NE 1998091800823 19980918 00823 NE 1998 9 18 98ZZZX3382 2 19980128 A 7250 410106701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MA 351 7107 LE45078E SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800824 19980918 00824 NE 1998 9 18 98ZZZX3383 2 19980128 A 7250 230307203 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117MA 351 7107 LE45078E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800825 19980918 00825 EU 1998 9 18 98ZZZX3384 1 19980309 A 7700 430136101 HARNESS BOLKMS 117 BK117A3 5626015 EU NR 1 ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 375 691 7058 HARNESS HAS INTERNAL SHORT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998091800826 19980918 00826 NE 1998 9 18 98ZZZX3385 2 19980516 A 7250 410106701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117MV 461 7089 LE45071E SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800827 19980918 00827 NE 1998 9 18 98ZZZX3386 2 19980218 A 7230 430150601 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 611 1705 7115 LE45023E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800828 19980918 00828 NE 1998 9 18 98ZZZX3387 2 19980218 A 7250 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 6115 1190778 7115 LE45023E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800829 19980918 00829 NE 1998 9 18 98ZZZX3388 2 19980218 A 7250 410106701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202HN 611 7115 LE45023E SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800830 19980918 00830 NE 1998 9 18 98ZZZX3389 2 19980218 A 7250 230093303 BEARING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202HN 611 7115 LE45023E BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998091800832 19980918 00832 NM 1998 9 18 98ZZZX3391 1 19980812 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 908-928/940 CRACKED B EF2R K NONE O OTHER IN INSP/MAINT 1 SW 05 59SW 61079 21811 SEVEN EACH FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 908 TO STA 928, STR 14L. TWO EACH FASTENER HOLES CRACKED IN THE FUSELAGE SKIN, STA 940, STR 14L. FUSELAGE SKIN IS CRACKED AT THE AFT ENTRY DOOR LOWER HINGE CUT-OUT (THE BEAR STRA P IS NOT CRACKED). REPAIRED PER DALFORD AEROSPACE XEA X2-53-216 DATED 7-22-98 AND BOEING 737 SRM 53-30-3, FIGURE 42. 2 L 7 2 4F A16WE 1998091800833 19980918 00833 NM 1998 9 18 98ZZZX3392 1 19980812 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 908-927 CRACKED B EF2R K NONE O OTHER IN INSP/MAINT 1 SW 05 59SW 21811 THREE EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 908 TO STA 927, STR 14R. EIGHT EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 932 TO STA 947, STR 14R. BEAR STRAP IS CRACKED AT THE AFT ENTRY DOOR LOWER HINGE CUT-OUT. REPAIR ED PER: DALFORT AEROSPACE, L.P. XEA X2-53-215, REV 1 DATED 7-31-98 AND SB 737-53-1074, REV 3. 2 L 7 2 4F A16WE 1998091800834 19980918 00834 NM 1998 9 18 98ZZZX3393 1 19980812 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 932-947 CRACKED B EF2R K NONE O OTHER IN INSP/MAINT 1 SW 05 59SW 21811 THREE EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 908 TO STA 927, STR 14R. EIGHT EACH FASTENER HOLES CRACKED IN FUSELAGE SKIN AT STA 932 TO STA 947, STR 14R. BEAR STRAP IS CRACKED AT THE AFT ENTRY DOOR LOWER HINGE CUT-OUT. REPAIR ED PER: DALFORT AEROSPACE, L.P. XEA X2-53-215, REV 1 DATED 7-31-98 AND SB 737-53-1074, REV 3. 2 L 7 2 4F A16WE 1998091800835 19980918 00835 EU 1998 9 18 98ZZZX3394 1 19980531 A 7110 221405083DB COWL ROHR AIRBUS 310 A310325 EU LT ENGINE DAMAGED A L AJLF O OTHER C F.O.D. TX TAXI/GRND HDL 1 SO 23 835AB 16246 523 650 KIN - FLT JM001 - ON ARRIVAL, ACFT APPROACHED GATE M24 WITH NORMAL TAXI SPEED FOLLOWING PAPA BOARD SIGNAL LIGHT. ACFT S TOPPED AT A310 POSITION ON CENTERLINE, MOVED FORWARD UNTIL LT ENGINE NOSE COWL STRUCK MOVEABLE JET BRIDGE. CAPTAIN REPO RTED ACFT HAD A BRAKE FAILURE. WEATHER WAS GOOD; VISIBILITY CLEAR. JET BRIDGE MOVED APPROX 5 TO 6 FEET AND WAS ALSO D AMAGED. UNITED A/L MAINT CONTINUES WITH ITS INVESTIGATION. INVEST REVEALED ACFT LOST YELLOW HYD FLUID EN ROUTE LHR. M AINT FND HYD LEAK FROM A DAMAGED PACKING (P/N NAS161206) OF SERVO CNTRL SAMPLING VALVE LOCATED IN THE RT WHEEL WELL. NE W PACKING INSTALLED, YELLOW HYD SYS SERVICED AND LEAK CHECKS OK. CASE DRAIN FILTERS CHECKED AND NO CONTAMINATION FOUND. 2 L 7 2 4F RT A35EU 1998091800836 19980918 00836 WP 1998 9 18 98ZZZX3395 1 19980812 A 3244 34X99 TIRE CVAC 240 2405 2422612 WP MLG SEPARATED A TFAA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 SO 15 295M 64 AFTER AIRCRAFT WAS IN CRUISE, ATC REPORTED THAT ANOTHER AIRCRAFT REPORTED SOME RUBBER ON THE RUNWAY JUST AFTER TAKEOFF. ALL INDICATIONS WERE NORMAL AND CREW CONTINUED TO DESTINATION. (SJU) SAN JUAN FIRE AND RESCUE WERE NOTIFIED AND AIRCRA FT MADE AN UNEVENTFUL LANDING. IT WAS DISCOVERED THAT THE RECAP HAD SEPARATED ON THE NR 1 MAIN TIRE. 2 L 7 2 4R A793 1998091800837 19980918 00837 WP 1998 9 18 NOCA1698 1 19980620 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 183NA 49808 E-PATH LIGHTS INOPERATIVE AT ROWS 3 AND 4. REPLACED FORWARD BATTERY POWER SUPPLY. OPS CHECK OK. (X) 2 L 7 2 4F RT A6WE 1998091800838 19980918 00838 NM 1998 9 18 EISA98184 1 19980801 A 5313 STRINGER BOEING 727 727277 138408S NM BS 660-680 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP CARD C 53-100-01 PART 4 INSPECTION OF LOWER FUSE BS 178 TO BS 1183, DETECTED ROW OF RIVETS RIGHT-HAND SIDE AT S25 STA 680 TO STA 660, SKIN BULGED AND STG CRACKED WITH CORROSION. CORRECTIVE ACTION: REPLACED ST G 25 PER SRH 53-10-03 FIG 1 HEAVY LIFT M/R CARD 905789. TT: 56,343:45 HOURS. TC: 37,111. (X) 2 L 7 3 4F RT A3WE 1998091800839 19980918 00839 NM 1998 9 18 EISA98181 1 19980717 A 3350 1000679 LIGHT BOEING 727 72731 1384010 NM CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 240NE 19617 18906 EMERGENCY EXIT LIGHT INOPERATIVE L1 DOOR. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK GOOD. TT: 61,936:46 HOURS. TC: 45,116. (X) 2 L 7 3 4F A3WE 1998091800840 19980918 00840 NM 1998 9 18 EISA98182 1 19980723 A 2612 7421019007376 FIRE LOOP BOEING 727 727223 1384074 NM NR 1 ENGINE FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 314NE 746 19495 ON PRE-FLIGHT, FOUND NR 1 ENGINE FIRE LIGHT WOULD NOT ILLUMINATE WHEN TESTED. FIRE BELL WORKED OK. GENERATED FROM PILO T REPORT. CORRECTIVE ACTION: REMOVED AND REPLACED NR 1 ENGINE FIRE LOO PER MM CHAPPTER 26-11-12. OPS CHECK GOOD. (X) 2 L 7 3 4F A3WE 1998091800841 19980918 00841 NM 1998 9 18 EISA98183 1 19980727 A 2133 CONNECTOR BOEING 727 727277 138408S NM OUTFLOW VALVE LOOSE A EISA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 275WC 20549 RETURNED TO BRU DUE TO PRESSURIZATION INOPERATIVE. GENERATED FROM PILOT REPORT. CORRECTIVE ACTION: TROUBLESHOT AND FO UND CONNECTOR TO OUTFLOW VALVE LOOSE. RESECURED CONNECTOR SYSTEM. CHECKS GOOD. MM CHAPTER 21. (X) 2 L 7 3 4F RT A3WE 1998091800842 19980918 00842 EU 1998 9 18 JBXA980034 1 19980308 A 3040 EAWTC8803411 CONTROLLER FOKKER F28 F28MK0100 4990807 EU E/E BAY MALFUNCTIONED A JBXA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 05 104ML FBE4043 11445 RDU - FLT 304 - LT WINDOW HEAT FAULTED WHEN POWER APPLIED FOR TAKEOFF. CORRECTIVE ACTION: INSPECTED LT WINDSHIELD AND SIDE WINDOWS. NO DEFECTS NOTED. PERFORMED BITE TEST OF CONTROLLER. ALL ELEMENTS TESTED GOOD AND SENSORS TESTED GOOD. REMOVED AND REPLACED LT WINDSHIELD HEAT CONTROLLER FOR TROUBLESHOOTING. TESTED GOOD IAW F100 AMM 30-45-01. (X) 2 L 7 2 4F RT 1998091800843 19980918 00843 CE 1998 9 18 S2YA98017 1 19980621 A 3260 327 BULB BEECH 1900 1900D 1154162 CE MLG ANNUNCIATOR FAILED A S2YA K NONE N FALSE WARNING AP APPROACH 1 GL 13 118SK UE108 ESC/MQT - FLT 1273 - DURING APPROACH, CREW SELECTED THE LANDING GEAR DOWN, WITH THE GEAR EXTENDED BOTH THE H AND THE R G EAR DOWN AND LOCK ANNUNCIATORS WERE INOPERATIVE. AFTER THE AIRCRAFT MADE AN UNEVENTFUL LANDING, MAINTENANCE INSPECTED T HE AIRCRAFT AND FOUND THE INDICATOR BULBS BURNED OUT. THE BULBS WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. (X ) 2 L 7 2 4T RT A24CE 1998091800844 19980918 00844 NE 1998 9 18 S2YA98018 2 19980621 A 7261 310047001 FITTING BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE RGB CRACKED A S2YA E ENGINE SHUTDOWN K J Y FLUID LOSS WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 GL 13 901SK 2744 UE90 YYZ/GRR - FLT 1123 - DURING CRUISE, CREW NOTICED RED ANNUNCIATOR CAUTION ILLUMINATE, FOUND RT LOW OIL PRESS ANNUNCIATOR ILLUMINATED AND REDUCED ENG POWER TO FLIGHT IDLE. MONITORED OIL PRESS INDICATOR, OIL PRESS ON RT ENG DROPPED STEADILY. FO INSP RT ENG AND NOTICED OIL COMING OUT FROM THE GAP BETWEEN SPINNER AND COWLING. MONITORED OIL PRESS GAUGE WITH NO SIGNS OF OIL PRESS INCREASING, SHUT DOWN ENG. DECLARED AN EMERGENCY. AFTER UNEVENTFUL LANDING AT YXU, MAINT INSPECTED ACFT. FND OIL RPESS LINE ELBOW HAD ONE BOLT BROKEN OFF AND OTHER SIDE OF ELBOW CRACKED. MAINT REPLACED ELBOW, INSP CH IP DETECTOR, AND OIL FILTER, NO DISCREPANCIES NOTED. OIL SERVICED, ENG LEAK CHECKED, RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 T RT A24CE E26NE 1998091800845 19980918 00845 NM 1998 9 18 NOCA1598 1 19980613 A 3350 676 LIGHT BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE AT DOOR L4. RE-LAMPED EXTERIOR EMERGENCY LIGHT AT DOOR L4. OPS CHECK NORMAL. (X) 2 L 7 2 4F RT A2NM 1998091800846 19980918 00846 SO 1998 9 18 98ZZZX3396 1 19980625 A 2913 65WE002241 PUMP EMB 110 EMB110P1 3260122 SO LT ENGINE FAILED A BQTA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 NE 05 790RA C1155C1 110278 AT APPROXIMATELY 6:30 P.M. ON 6-25-98 WHILE EN ROUTE TO SYRACUSE, THE LT HYD SYSTEM PRESSURE DROPPED TO ZERO PSIG. A NO RMAL LANDING ACCOMPLISHED AT SYRACUSE. THE HYD SYS FILTER AND PRESSURE AND SUCTION LINES WERE EXAMINED FOR METAL. NONE FOUND. THE LT PUMP WAS ISOLATED AND A FERRY FLIGHT TO B5B. THE LT PUMP P/N 65WE00224-1 S/N C1-155-C1 REMOVED AND REPL ACED ALONG WITH THE PRIMARY SYSTEM FILTER. THE HYD PUMP AND SYS FUNCTIONAL TESTED SATISFACTORY AND ACFT RETURNED TO SER VICE. (X) 1 L 7 2 4T A21SO 1998091800847 19980918 00847 NM 1998 9 18 GAIA9863 1 19980623 A 5312 BULKHEAD WEB BOEING 727 727223 1384074 NM BS 1183 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6810 19485 DURING ROUTINE C-CHECK, A CRACK WAS FOUND ALONG THE AFT PRESSURE BULKHEAD WEB APPROXIMATELY 1.2 INCHES LONG JUST ABOVE W L 263 AND LBL 26.83, BS 1183. THE CRACK WAS STOP DRILLED USING A 0.187 INCH HOLE. THE CRACK WAS THEN NDT TO ENSURE CRA CK LIMITATION. REPAIR DOUBLER INSTALLED USING FLIGHT VEHICLES, INC., DRAWING 53-98301-1 REV NEW DATED 6-9-98 BY AAR IN OKLAHOMA CITY. (X) 2 L 7 3 4F A3WE 1998091800848 19980918 00848 NM 1998 9 18 GAIA9867 1 19980623 A 5714 WING BOX BOEING 727 727223 1384074 NM WING CTR SECT CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6810 19485 DURING ACCOMPLISHMENT OF AD 85-24-02, RAM AIR PLENUM CORROSION INSPECTION. CORROSION WAS FOUND ALONG THE LEFT SIDE WING BOX CENTER SECTION AT STR 4C AND LBL 36.5. THE CORROSION WAS BLENDED OUT AND A DOUBLER WAS INSTALLED. THE AREA WAS R EPAIRED IAW BOEING ENGINE LETTER AOC-OKC-98-051RR DATED 6-2-98 BY AAR OKLAHOMA CITY. STRUCTURAL SUBSTANTIATION OF REPAI R PLAN IS AN AMOC TO AD 85-24-02. THE AREA WAS RESTORED TO NORMAL AND ACFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998091800849 19980918 00849 NM 1998 9 18 GAIA9866 1 19980623 A 5714 WING BOX BOEING 727 727223 1384074 NM WING CTR SECT CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6810 19485 DURING ACCOMPLISHMENT OF AD 85-24-2, RAM AIR PLENUM CORROSION INSPECTION. CORROSION WAS FOUND ALONG THE RT SIDE WING BO X CENTER SECTION AT STRINGERS S-3C AND S-4C, RBL 36.5 AND STRINGERS 3C AND S-4C, RBL 20.0. THE CORROSION WAS REMOVED BY BLENDING OUT. THE AREA WAS REPAIRED IAW BOEING ENGINEERING LETTER AOC-OKC-98-05044 DATED 6-2-98, BY AAR OKLAHOMA CITY. STRUCTURAL SUBSTANTIATION OF REPAIR PLAN IS AN AMOC TO AD 85-24-02. THE AREA WAS RESTORED TO NORMAL AND ACFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998091800850 19980918 00850 NM 1998 9 18 TAOA079814 1 19980728 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 926TS 11307 20774 BOS/LGA - FLT 6081 - EMERGENCY LIGHTS DO NOT ILLUMINATE AT R-1 DOOR, BOTH OVERWING DOORS ON RT SIDE, OVERHEAD AISLE FORW ARD OF WINGS. REPLACED R-1 DOOR LIGHT ASSY AND BATTERY PACK FOR OVERWING LIGHTS. REPAIRED TWO BROKEN WIRES ON CENTER A ISLE OVERHEAD UNIT. (X) 2 L 7 3 4F A3WE 1998091800851 19980918 00851 EU 1998 9 18 SIMA981851 1 19980704 A 2910 7064588 LINE SAAB SF340 340B 7860101 EU NLG WW BROKEN A SIMA A UNSCHED LANDING K FLUID LOSS TO TAKEOFF 1 SW 21 284AE 340B284 BFL - FLT 3272 - LOST ALL HYD SYSTEM FLUID ON TAKEOFF. FOUND BROKEN LANDING GEAR RETRACT LINE AT NOSE LANDING GEAR DOWN LOCK ACTUATOR. REMOVED LINE, CAPPED PORTS, SERVICED SYSTEM AND FERRIED AIRCRAFT TO LAX FOR REPAIR. REPLACED LINE AT L AX. ALSO, REPLACED BOTH NOSE TIRES FOR FLUID CONTAMINATION. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998091800852 19980918 00852 WP 1998 9 18 TWAA9814801 1 19980914 A 2421 GENERATOR DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A TWAA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CE 05 929TW 48014 AIRCRAFT WAS DISPATCHED WITH THE RT ENG GENERATOR INOPERATIVE PER MEL. AT FL310, THE APU SHUT DOWN. APU RESTARTED AT F L 240. ELECTED TO DIVERT TO MCI. THE RT ENG CSD AND GENERATOR WERE REPLACED. APU OPERATED OK. CSD MFG 696233B AND GE N MFG 976J252-8. CHECK-C 4-1-98 MCI. 2 L 7 2 4F A6WE 1998091800853 19980918 00853 WP 1998 9 18 VJ9800382 1 19980831 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FRAME TO SKIN ATTACHING CLIP AND SKIN IN AFT CARGO COMPARTMENT AT STA 945 HAS CORROSION BEYOND LIMIT. REMOVED CORROSION AT FRAME LOWER CAP IAW DC9 SRM 51-30-2 AND FOUND SHEAR TIE CRACKED IN TWO PLACES AND SKIN OUT OF LIMIT IAW DC9 SRM 53-0 1, FIG 1. FABRICATED SKIN DOUBLER REPAIR IAW DC9 SRM 53-04, FIG 38 AND INSTALLED PARTS IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998091800854 19980918 00854 WP 1998 9 18 VJ9800383 1 19980831 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FORWARD CARGO FRAME STA 218, L26L-L26R CORRODED. REMOVED NUTPLATES FOR ACCESS AND CORROSION IAW DC9 SRM 51-10-3. TREAT ED AND PRIMED FROM LBL 3 TO RBL 40 AND LBL 5 TO LBL29 IAW DC9 SRM 53-01, FIG 1. FABRICATED REPAIR FILLER AND DOUBLER, P RIMED AND INSTALLED IAW DC9 SRM 53-10-0, FIG 808 AND REINSTALLED NUT PLATES IAW DC9 SRM 51-30-2 AND RES 981348. 2 L 7 2 4F A6WE 1998091800855 19980918 00855 WP 1998 9 18 VJ9800384 1 19980831 A 5414 SKIN DOUG DC9 DC932 3022066 WP RT PYLON CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 RT PYLON LOWER TRAILING EDGE SKIN CORRODED ON INBOARD SIDE. REMOVED CORRODED SKIN FROM RT PYLON LOWER TRAILING EDGE IAW DC9 SRM 51-10-2, 51-10-4. INSTALLED NEW SKIN IAW DC9 SRM 51-30-2 AND RES 981313, REINSTALLED TRAILING EDGE ON PYLON IA W DC9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998091800856 19980918 00856 WP 1998 9 18 VJ9800385 1 19980831 A 5311 9919617502N FRAME DOUG DC9 DC932 3022066 WP BS 699 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FRAME 699R AFT SIDE BELOW FLOOR LEVEL CRACKED. REPLACED CRACKED FRAME AT STA 699 RT IAW EO 12-5311-29-B1044. 2 L 7 2 4F A6WE 1998091800857 19980918 00857 WP 1998 9 18 VJ9800386 1 19980831 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 240 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 DENT .048X2X 18 INCHES AT FS 240R, L26-29, OUT OF LIMIT IAW 5304, FIG 38. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DC9 SRM 53-04, FIG 38. 2 L 7 2 4F A6WE 1998091800858 19980918 00858 WP 1998 9 18 VJ9800387 1 19980831 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 250 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 TWO EACH DENTS LOCATED AT FS 250L, L18-17, OUT OF LIMIT. COLD WORKED DENTS AT STA 250-245L, BETWEEN L17-18L, IAW DC9 SR M 53-04, FIG 38. FABRICATED DOUBLER REPAIR IAW DC9 SRM 53-04, FIG 38. DRILLED, TRIMMED AND DEBURRED DOUBLER, TREATED A ND PRIMED DOUBLER AND INSTALLED INTERNAL SKIN DOUBLER REPAIR IAW DC9 SRM 51-10-4, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998091800859 19980918 00859 WP 1998 9 18 VJ9800388 1 19980831 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1153 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 DENTS OUT OF LIMIT AT AFT SECTION OF SKIN AT AFT ENTRY DOOR IAW DC9 SRM 51-50-1, FIG 1. CUT OUT DAMAGED AREA, FABRICATE D SKIN REPAIR AND DOUBLER. FITTED, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-10-4, 51-10- 3, 51-10-2 AND AIRTRAN RES NR 981411. 2 L 7 2 4F A6WE 1998091800860 19980918 00860 WP 1998 9 18 VJ9800389 1 19980914 A 2560 11331 SLIDE DOUG DC9 DC932 3022066 WP R1 DOOR DETACHED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 932VV 47451 DOOR SLIDE DISLODGED FROM GALLEY DOOR. REINSTALLED SLIDE IAW MM 25-00 AND PERFORMED REQUIRED INSPECTIONS. 2 L 7 2 4F A6WE 1998091800861 19980918 00861 NM 1998 9 18 RAAA98B1090 1 19980914 A 5330 SKIN BOEING 727 72722C 138400F NM BS 506.5 PUNCTURED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING CARGO LOADING AT ANC 1.25 INCH BY 2 INCH HOLE PUNCTURED IN BS 506.5 FUSELAGE SKIN BETWEEN STR 20L AND 21L. REPAI RED PER SRM 53-30-3, FIG 1 M-54 NR 1. 2 L 7 3 4F A3WE 1998091800862 19980918 00862 NM 1998 9 18 CALA9801719 1 19980912 A 5400 ANGLE BOEING 727 727232 1384082 NM BS 1203 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN LEFT RIB TO SKIN ATTACH ANGLE AND A 2.5 CRACK IN RIGHT RIB TO SKIN ATTACH ANGLE OF C ENTER ENGINE AIR DUCT HOUSING AT STA 1203. THE ATTACH ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800863 19980918 00863 NM 1998 9 18 CALA9801720 1 19980913 A 5400 ANGLE BOEING 727 727232 1384082 NM BS 1213 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN RT RIB TO SKIN ATTACH ANGLE OF CENTER ENGINE AIR DUCT HOUSING AT STA 1213. THE ATTA CH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800864 19980918 00864 NM 1998 9 18 CALA9801721 1 19980912 A 5320 DOUBLER BOEING 727 727232 1384082 NM AFT AIRSTAIR SEPARATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LEFT AFT AIRSTAIR EXTERNAL SKIN REPAIR DOUBLER SEPARATING WITH A LOOSE RIVET. THE SEPARATING AREA WAS REMOVED. DOUBLER, FILLER, AND AN ANGLE WERE INSTALLED IAW SRM 51-10-2. 2 L 7 3 4F A3WE 1998091800865 19980918 00865 NM 1998 9 18 CALA9801722 1 19980912 A 5311 FRAME BOEING 727 727232 1384082 NM BS 930 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .75 INCH CRACK IN RT FUSELAGE FRAME AT STA 930, WL 230 AND 234. THE FRAME WAS REPAIRED IAW ECRA 5310 -01397, SRM 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998091800866 19980918 00866 NM 1998 9 18 CALA9801723 1 19980912 A 5320 SUPPORT BOEING 727 727232 1384082 NM BS 344-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND DRAG BRACE SUPPORT DECK AND SIDE T-CHORDS CORRODED AT STA 344-360. THE SUPPORT DECK AND CHORDS WERE RE MOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724. 2 L 7 3 4F A3WE 1998091800867 19980918 00867 NM 1998 9 18 CALA9801724 1 19980912 A 5320 T-CHORD BOEING 727 727232 1384082 NM BS 259-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT AND RT FUSELAGE T-CHORDS CORRODED AT STA 259-360. THE T-CHORDS WERE REMOVED AND REPLACED IAW SRM 51 -30-2 AND BOEING DRAWING 65C15724. 2 L 7 3 4F A3WE 1998091800868 19980918 00868 NM 1998 9 18 CALA9801725 1 19980913 A 5330 SKIN BOEING 727 727232 1384082 NM BS 227-360 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT AND RT NOSE SKIN CORRODED AT STA 227-360, STRINGERS 24-29L AND 24-29R. NEW SKIN SECTIONS WERE INSTA LLED IAW SRM 51-30-2 AND BOEING DRAWING 65C15724. 2 L 7 3 4F A3WE 1998091800869 19980918 00869 NM 1998 9 18 CALA9801726 1 19980913 A 5320 SUBFLOOR BOEING 727 727232 1384082 NM BS 340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FORWARD LAV SUBFLOOR CORRODED AT STA 340, RBL 42-60. THE LAV SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-20-1. 2 L 7 3 4F A3WE 1998091800870 19980918 00870 NM 1998 9 18 CALA9801727 1 19980913 A 5311 FRAME BOEING 727 727232 1384082 NM BS 1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CORROSION AT HOLE OF LT UPPER DOOR FRAME STA 1183, WL 273, LBL 19.22. REPAIRED IAW ECRA 5310-03765. 2 L 7 3 4F A3WE 1998091800871 19980918 00871 NM 1998 9 18 CALA9801728 1 19980913 A 5320 BRACKET BOEING 727 727232 1384082 NM BS 303.9 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 2 INCH AND 1.5 INCH CRACK IN CABIN FLOOR SUPPORT BRACKET AT STA 303.9, LBL 12. THE FLOOR SUPPORT BRA CKET WAS REMOVED AND NEW BRACKET WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800872 19980918 00872 NM 1998 9 18 CALA9801729 1 19980913 A 5330 PANEL BOEING 727 727232 1384082 NM BS 530-550 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FORWARD CARGO PIT LT TRANSITION PANEL CORRODED FROM STA 530-550. THE PANEL WAS REMOVED AND REPLACED IA W SRM 51-30-2, 51-10-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998091800873 19980918 00873 NM 1998 9 18 CALA9801730 1 19980913 A 5320 INTERCOSTAL BOEING 727 727232 1384082 NM BS 303.9 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND INTERCOSTAL CORRODED AT FS 303.9, LBL 0 TO 12. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS I NSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998091800874 19980918 00874 WP 1998 9 18 CALA9801731 1 19980912 A 5350 5910233509 TAIL CONE DOUG DC9 DC982 3022082 WP AFT FUSELAGE WARPED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 35888 34748 49117 THE TAILCONE PULL TEST EXCEEDED LIMITS AND THE TAILCONE DID NOT DEPLOY USING EITHER THE INTERIOR OR AFT RELEASE HANDLES. THE TAILCONE WAS REMOVED AND REPLACED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998091800875 19980918 00875 NM 1998 9 18 CALA9801732 1 19980914 A 5523 TAB BOEING 727 727232 1384082 NM LT ELEVATOR DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND LT ELEVATOR TAB INBOARD MOST TRAILING EDGE AREA DEBONDED. THE ELEVATOR TAB WAS REMOVED AND REPLACED IA W MM 27-30-11. 2 L 7 3 4F A3WE 1998091800876 19980918 00876 NM 1998 9 18 CALA9801733 1 19980914 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN AT UPPER OUTBOARD CORNER OF CAPTAIN'S WINDSHIELD CUTOUT AND A .125 INC H CRACK WAS FOUND IN SKIN AT LOWER FORWARD CORNER JUST FORWARD OF CAPTAIN'S SLIDING WINDOW. THE CRACKS WERE STOP DRILLE D AND DOUBLERS WERE INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1998091800877 19980918 00877 NM 1998 9 18 CALA9801734 1 19980914 A 5754 SKIN BOEING 727 727232 1384082 NM NR 8 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A 2 INCH CRACK IN NR 8 SLAT INNER SKIN AT OUTBOARD STRIKER PLATE AREA. THE OUTBOARD STRIKER SKIN PLATE WAS REPLACED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998091800878 19980918 00878 NM 1998 9 18 CALA9801735 1 19980914 A 5320 FRAME BOEING 727 727232 1384082 NM CARGO DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A 3.5 INCH CRACK AT FORWARD LOWER SIDE OF NR 3 CARGO DOOR FRAME BETWEEN STRINGER 25R AND 26R. THE CRAC K WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-10-4. 2 L 7 3 4F A3WE 1998091800879 19980918 00879 NM 1998 9 18 CALA9801736 1 19980914 A 5753 65192709 TRACK BOEING 727 727224 1384076 NM NR 4 FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND NR 4 FLAP TRACK FORWARD CLEVIS CORRODED ON BOTH SIDES. THE FLAP TRACK ASSEMBLY WAS REPLACED IAW MM 57- 40-00. 2 L 7 3 4F A3WE 1998091800880 19980918 00880 NM 1998 9 18 CALA9801737 1 19980914 A 5754 ANGLE BOEING 727 727224 1384076 NM NR 3 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .375 INCH CRACK IN NR 3 SLAT LOWER ATTACH ANGLE FOR PANELS AT ACTUATOR ATTACH AREA. THE CRACK WAS RO UTED OUT. AN ANGLE DOUBLER WAS INSTALLED IAW SRM 51-40-4, FIGURE 3. 2 L 7 3 4F A3WE 1998091800881 19980918 00881 NM 1998 9 18 CALA9801738 1 19980914 A 5754 ANGLE BOEING 727 727224 1384076 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .375 INCH CRACK IN NR 2 SLAT PANEL ATTACH ANGLE BY ANTI-ICE DUCT. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, FIGURE 4. 2 L 7 3 4F A3WE 1998091800882 19980918 00882 NM 1998 9 18 CALA9801739 1 19980914 A 5320 CHANNEL BOEING 727 727224 1384076 NM BS 1140-1170 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND AFT LAV FLOOR HAT CHANNEL CORRODED AT FS 1140-1170, RBL 24. THE HAT CHANNEL WAS REMOVED AND A NEW CHAN NEL WAS INSTALLED IAW SRM 51-30-2, PAGE 2, 51-10-2, AND 51-40-5. 2 L 7 3 4F A3WE 1998091800883 19980918 00883 NM 1998 9 18 CALA9801740 1 19980914 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .3125 INCH CRACK AT RT OUTBOARD FOREFLAP LOWER LEADING EDGE SKIN ABOVE NR 7 FLAP TRACK AREA, 54 INCHE S FROM INBOARD END. A DOUBLER WAS INSTALLED IAW SRM 57-50-4, FIGURE 1, 51-10-6, AND 51-10-2. 2 L 7 3 4F A3WE 1998091800884 19980918 00884 NM 1998 9 18 CALA9801741 1 19980914 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .75 INCH AND .1093 INCH CRACK IN RT WING LOWER TRAILING EDGE OF INBOARD MIDFLAP, 34 INCHES FROM INBOA RD END. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 57-50-4, FIGU RE 1. 2 L 7 3 4F A3WE 1998091800885 19980918 00885 NM 1998 9 18 CALA9801742 1 19980914 A 5522 SKIN BOEING 727 727224 1384076 NM LT ELEVATOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND LT ELEVATOR SKIN UPPER SURFACE CORRODED AROUND STATIC WICK BASE. THE CORRODED AREA WAS REMOVED AND A R EPAIR WAS INSTALLED IAW SRM 55-20-03. 2 L 7 3 4F A3WE 1998091800886 19980918 00886 SO 1998 9 18 COMA9810192 1 19980915 A 5320 12028978005 DOUBLER EMB 120 EMB120RT SO FUSELAGE CRACKED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 164D 21953 1164 DOUBLER ON POST BETWEEN DIRECT VISION WINDOW AND NR 1 WINDOW IS CRACKED BELOW HANDLE. REMOVED DOUBLER AND REPLACED WITH SERVICEABLE DOUBLER. ALSO COMPLIED WITH S/B 120-53-0045 IAW EMB 120 S/B 120-53-0045. 2 L 7 2 4T RT A31SO 1998091800887 19980918 00887 EA 1998 9 18 COMA9860260 1 19980911 A 3350 60206 SIGN CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 EMERGENCY LIGHT IN FRONT ENTRANCE IS BROKEN. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A21EA 1998091800888 19980918 00888 EA 1998 9 18 COMA9860261 1 19980911 A 2613 356024310 DETECTOR CNDAIR CL600 CL6002B19 EA LT BLEED AIR MALFUNCTIONED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 963CA 7127 LEFT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE PYLON LEAK DETECTOR LOOP. 2 L 7 2 4F RT A21EA 1998091800889 19980918 00889 EA 1998 9 18 COMA9860262 1 19980912 A 3222 16040103 STRUT CNDAIR CL600 CL6002B19 EA NLG REQD SERVICE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 940CA 9895 7048 NLG DOORS AND GEAR DISAGREE MESSAGE. SERVICED NLG STRUT, LANDING GEAR RETRACT CHECKS NORMAL. 2 L 7 2 4F RT A21EA 1998091800890 19980918 00890 EA 1998 9 18 COMA9860263 1 19980913 A 7714 5071T98P02 AMPLIFIER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE MALFUNCTIONED A COMA K NONE O OTHER CR CRUISE 1 SO 01 989CA 4867 7215 RT ENGINE N1 AND ITT FLUCTUATIONS WHICH EXCEED LIMITS. COULD NOT DUPLICATE FLUCTUATIONS DURING GROUND RUN. REPLACED CO NTROL AMPLIFIER FOR TROUBLESHOOTING. 2 L 7 2 4F 4 F RT A21EA E15NE 1998091800891 19980918 00891 EA 1998 9 18 COMA9860264 1 19980913 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 713CA 7245 CABIN DOOR OUTER HANDLE MESSAGE. COULD NOT DUPLICATE. OPERATED DOOR SEVERAL TIMES. NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1998091800892 19980918 00892 SO 1998 9 18 COMA9810193 1 19980913 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT SECURED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 258CA 1247 SERVICE DOOR WARNING DURING TAKE-OFF. SECURED SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998091800893 19980918 00893 SO 1998 9 18 COMA9810194 1 19980914 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 152CA 120152 EMERGENCY LIGHT COVER AT 5C IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998091800894 19980918 00894 NM 1998 9 18 UPS98227681 1 19980915 A 5720 DOUBLER BOEING 727 72751C 1384015 NM WS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 905UP 18947 INSPECTION TYPE-N/A, RIGHT WING AFT SPAR LOWER EDGE CORRIGATED DOUBLER CRACKED APROX 2 INCHES AT APROX WS 340 WBL 220. S TOP DRILLED CRACK PER SRM 51-10-1 PG 6B. 2 L 7 3 4F A3WE 1998091800895 19980918 00895 NM 1998 9 18 UPS98527680 1 19980912 A 2510 MXP21000 GOGGLES BOEING 757 75724APF 1384969 NM COCKPIT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 419UP 23906 INSPECTION TYPE-W/E, 1 PAIR OF JUMPSEAT SMOKE GOGGLES CRACKED. INSTALLED SERVICEABLE SMOKE GOGGLES IN JUMPSEAT POSITION . 2 L 7 2 4F RT A2NM 1998091800896 19980918 00896 WP 1998 9 18 UPS98827675 1 19980829 A 5313 575032223 LONGERON DOUG DC8 DC871F 302199D WP BS 1272 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-C, LONGERON 35R IS CRACKED AT STA 1272. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 5750322 AND D WG 3758593. 2 L 7 4 4F RT 4A25 1998091800897 19980918 00897 WP 1998 9 18 UPS98827676 1 19980827 A 5320 97558651 FITTING DOUG DC8 DC871F 302199D WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-C, LONGERON 36 END FITTING AT STA 8 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 9755865. 2 L 7 4 4F RT 4A25 1998091800898 19980918 00898 WP 1998 9 18 UPS98827677 1 19980828 A 5330 SKIN DOUG DC8 DC871F 302199D WP WS 240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-C, LT WING L/E UPPER SKIN AT STA XW240.00 IS CRACKED IN 2 PLACES, NEAR THE L/E AT THE FRONT SPAR. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998091800899 19980918 00899 WP 1998 9 18 UPS98827678 1 19980827 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 78.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-C, RT WING FUEL TANK ACCESS PANEL LAND IS CRACKED AT THE AFT O/B CORNER (XCW 78.5). REPAIRED AREA IAW S RM 57-2-1 FIG 36. 2 L 7 4 4F RT 4A25 1998091800900 19980918 00900 WP 1998 9 18 UPS98827679 1 19980825 A 5330 561386215N1 SKIN DOUG DC8 DC871F 302199D WP BS 58 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-C, EXTERNAL FUSELAGE SKIN AT STA 58 AND LONGERON 34R IS CRACKED AND CORRODED. REMOVED AND REPLACED BELL Y SKIN FROM STA -136 TO 70 IAW DC8-5330 -8942 C. 2 L 7 4 4F RT 4A25 1998091800901 19980918 00901 EU 1998 9 18 QXEA9801282 1 19980909 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 GEG - OVERHEAD EXIT LIGHT ABOVE COCKPIT DOOR HAS LAMPS OUT. MAINTENANCE RELAMPED. OPERATIONAL TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998091800902 19980918 00902 EU 1998 9 18 QXEA9801283 1 19980908 A 3350 2302 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 484US 11234 GEG - OVERHEAD EXIT LIGHT IN GALLEY AND MID CABIN OUT. MAINTENANCE REPLACED EXIT SIGNS. OPERATIONAL TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998091800903 19980918 00903 NM 1998 9 18 98FDEA00569 1 19980311 A 2820 CIRCUIT BREAKER DOUG MD11 MD11F 3023600 NM ACCESSORY COMPT TRIPPED A FDEA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 SO 25 601FE 48401 DURING FUEL SYS STATUS CK WORKCARD 28B1301, L/TAIL TANK TRANSFER PUMP C/B TRIPPED. FIRE STARTED IN AFT ACCESSORY SECTIO N DURING FUEL TRANSFER TEST. C/W REPAIR IAW EA 1-2800-38210 AND WDM 28-22-05. 2 L 7 3 4F RT A22WE 1998091800904 19980918 00904 NM 1998 9 18 98FDEA00570 1 19980914 A 2740 AVR869 RELAY BOEING 727 727227 1384078 NM CONTROL WHEEL FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 489FE 21492 97-223 - CONTROL WHEEL TRIM SWITCHES INOP BOTH SIDES. REPLACED R-29 PHASE SEQUENCE RELAY. SYSTEM G/CS NORMAL. 2 L 7 3 4F A3WE 1998091800905 19980918 00905 1998 9 18 98FDEA00571 2 19980915 A 7200 ENGINE BOEING 727 7272S2F 1384O81 NM NR 2 FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 201FE 22924 WHEN SWITCH FROM BLD NR 1 TO BLD NR 2 AT 18000 FT, THE ENG NR 2 BLD HIGH TEMP LIGHT ILLUM. AFT SWITCH BACK TO NR 1 BLD. THE HIGH TEMP LIGHT WENT OUT APPROX 30 SEC TO 1 MIN LATER. NR 2 ENG PWR SET WAS 2.08 EPR. *S/D* CHGD NR 3 ENG EPR T RANSMITTER, PRECAUTION B/B 77-11-11. REMOVED AND REPLACED NR 2 ENGINE PER WORK CARD 70T0002 AND 70T0301. CK GOOD NO LE AKS NOTED. 2 L 7 3 4F A3WE 1998091800906 19980918 00906 WP 1998 9 18 98FDEA00572 1 19980911 A 5347 TRACK DOUG DC10 DC1030 3023501 WP BS 1871 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 SNRM 0030 - CORRODED TIE DOWN (TWO EACH) ON FLOOR TRACK LOCATED APPROX ALONG BS 1871, 8 INCH LBL. 2 L 7 3 4F A22WE 1998091800907 19980918 00907 WP 1998 9 18 98FDEA00573 1 19980911 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 765 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 318FE 46837 SURFACE CORROSION ON FLOOR TRACK ALONG BS 765, 27 INCH RBL. *S/D* FLOOR TRACK SURFACE CORROSION FOUND EXCEED LIMITS. C ARRIED OUT REPAIR BY INSTALLING FABRICATED FLOOR TRACK AND HAT SECTION SPLICE AS PER SRM 53-70-00 FIG 1 VOL 1 REV 76. 2 L 7 3 4F A22WE 1998091800908 19980918 00908 WP 1998 9 18 ABXA9800819 1 19980910 A 5230 564585717 SKIN DOUG DOUG DC8 DC863 302198A WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 815AX 46097 CARGO DOOR WEB IS CRACKED AT UPPER AFT CORNER AND FLANGE IS BROKEN AT DOOR PAN. REPAIRED INNER SKIN, CARGO DOOR IAW ABX REA D852-24277MR. 2 L 7 4 4F 4A25 1998091800909 19980918 00909 WP 1998 9 18 ABXA9800820 1 19980911 A 5313 591140617N LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING C-CHECK, FOUND LONGERON 4L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 1998091800910 19980918 00910 WP 1998 9 18 ABXA9800821 1 19980911 A 5755 3923258504 FITTING DOUG DOUG DC9 DC932 3022066 WP RT WING SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING C-CHECK, FOUND RIGHT OUTBOARD SPOILER TORSION BAR CENTER SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30 AND 51-30-2. 2 L 7 2 4F A6WE 1998091800911 19980918 00911 WP 1998 9 18 ABXA9800822 1 19980911 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 1998091800912 19980918 00912 WP 1998 9 18 ABXA9800823 1 19980911 A 5313 59114279 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING C-CHECK, FOUND LONGERONS 17L AND 17R CRACKED AT STATION 965 AND 980. REPAIRED LONGERONS IAW DC-9 SRM 53-02. 2 L 7 2 4F A6WE 1998091800913 19980918 00913 WP 1998 9 18 ABXA9800824 1 19980911 A 5312 3917624511 BLKHD STIFFENER DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING C-CHECK, FOUND STIFFENER CRACKED, RIGHT SIDE OF AFT PRESSURE BULKHEAD DOOR JAMB APPROXIMATELY 18 ABOVE FLOOR. RE PLACED STIFFENER IAW DC-9 SRM 51-30-5 AND 51-30-2. 2 L 7 2 4F A6WE 1998091800914 19980918 00914 WP 1998 9 18 ABXA9800825 1 19980911 A 5711 5911300502 SPAR CAP DOUG DOUG DC9 DC932 3022066 WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING C-CHECK, FOUND RIGHT WING UPPER SPAR CAP CORRODED BEYOND LIMITS UNDER AND AROUND THE NUT PLATE JUST OUTBOARD OF R IGHT AILERON. REPAIRED IAW ABX REA D957-24791-MR. 2 L 7 2 4F A6WE 1998091800915 19980918 00915 WP 1998 9 18 ABXA9800826 1 19980911 A 5320 9910073223 MEMBRANE DOUG DOUG DC9 DC932 3022066 WP BS 120 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 DURING C-CHECK, FOUND THE SUBFLOOR MEMBRANE CRACKED AT STATION 120 ABOVE THE AILERON LOAD FEEL CENTERING SPRING ON RIGHT SIDE. REPAIRED SUBFLOOR MEMBRANE IAW DC-9 SRM 53-01. 2 L 7 2 4F A6WE 1998091800916 19980918 00916 WP 1998 9 18 ARWA980907 1 19980915 A 2742 ACTUATOR DOUG DC8 DC862 3021970 WP HORIZ STAB INOPERATIVE A ARWA O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 SO 19 791AL 46150 CONTROL WHEEL SWITCHES ON CAPT AND FO FOR LONGITUDINAL TRIM INOP. ON PREFLIGHT SWAPPED TRIM ACTUATOR, REINSTALLED LOANE R TRIM ACTUATOR, SYS OPS CHECK NORMAL IAW MM 27-43-0. 2 L 7 4 4F 4A25 1998091800917 19980918 00917 1998 9 18 VNAA9809007 4 19980909 A 3130 7013348903 DAU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E COMPT MALFUNCTIONED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 434JS 79229 3051 DURING THE TAXI FOR TAKEOFF, A CHECK DU 3 WARNING MESSAGE ILLUMINATED ON FAULT WARNING COMPUTOR NUMBER TWO. THE AIRCRA FT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND SWAPPED THE DATA ACQUISITION UNITS FOR TROUBLE SHOOTING. OPERATION CHECKS WERE CARRIED OUT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-42-00. THE CHECKS WERE SATISFACTORY, AND THE A IRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091800918 19980918 00918 NM 1998 9 18 VNAA9809008 1 19980910 A 5730 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT WING BIRD STRIKE A VNAA K NONE C F.O.D. AP APPROACH 1 GL 07 461PS 3075 DURING APPROACH, THE AIRCRAFT TOOK A BIRD STRIKE ON THE LEFT WING. THE AIRCRAFT CONTINUED THE APPROACH AND PERFORMED A NORMAL LANDING WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE CLEANED AND INSPECTED THE AIRCRAFT FOR DAMAGE, IN ACCORDANCE W ITH DORNIER MAINTENANCE MANUAL 05-51-07. NO DAMAGE WAS NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998091800919 19980918 00919 NM 1998 9 18 GAIA9876 1 19980806 A 2761 65C163001 ACTUATOR BOEING 727 727223 1384074 NM RT WING LEAKING A GAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 6821 19496 BSM/MCI - EN ROUTE AFTER LEVEL CRUISE, A-SYSTEM HYDRAULICS WENT TO 1.5 GALLONS, THEN QUANTITY DECREASED TO ZERO, AND THE LOW LEVEL LIGHT ILLUMINATED. PERFORMED A-SYSTEM LOSS PROCEDURE, DECLARED EMERGENCY, AND DIVERTED TO DFW. THE AIRCRAFT LANDING IN DFW WITHOUT FURTHER DIFFICULTIES. SERVICED A-SYSTEM HYDRAULICS. FOUND NR 14 SPOILER ACTUATOR LEAKING BADL Y. REPLACED NR 14 SPOILER ACTUATOR PER B727 MM 27-61-81. RE-SERVICED A-SYSTEM HYDRAULIC SYSTEM. OPERATIONAL CHECK GOO D ON GROUND. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998091800920 19980918 00920 NM 1998 9 18 GAIA98079 1 19980810 A 3610 DUCT BOEING 727 727214 138407R NM NR 1 PYLON LEAKING A GAIA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 751US 21513 DURING CLIMB-OUT FROM MCI/PDX, THE NR 1 PYLON STRUT OVERHEAT LIGHT ILLUMINATED IN THE COCKPIT FOLLOWED BY A BURNING SMEL L IN THE COCKPIT. THE CREW THEN REDUCED THE POWER TO THE NR 1 ENGINE AND THE LIGHT EXTINGUISHED. THE CREW RETURNED TO MCI AND MADE A ROUTINE LANDING. INSPECTED NR 1 ENGINE PYLON AND FOUND SEVERAL LEAKS FROM THE 6TH STAGE BLEED AIR DUCT. REMOVED CLAMPS, RE-POSITIONED, RE-TORQUED AND SAFETIED AS NECESSARY. RAN AIRCRAFT TO 80 PERCENT N2 FOR 10 MINUTES WIT H NO LEAKS NOTED. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998091800921 19980918 00921 NM 1998 9 18 GAIA98077 1 19980810 A 3610 SEALS BOEING 727 727223 1384074 NM NR 3 LEAKING A GAIA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 854AA 20995 DURING CLIMB-OUT FROM TOL TO TOL-BDL-EWR, THE NR 3 PYLON STRUT OVERHEAT LIGHT ILLUMINATED IN THE COCKPIT. THE CREW TURN ED OFF THE BLEED AIR AND REDUCED THE POWER TO THE NR 3 ENGINES. THE CREW RETURNED TO TOLEDO AND MADE A ROUTINE LANDING. FOUND 8TH STAGE CHECK VALVE LEAKING. REMOVED AND REPLACED VALVE SEALS. RAN ENGINE WITH NO LEAKS NOTED. STRUT OVERHE AT OPS CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998091800922 19980918 00922 WP 1998 9 18 ARWA980802 1 19980803 A 2810 FUEL CELL DOUG DC8 DC862F 3021972 WP RT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 791AL 46150 MIA - RIGHT WING FORWARD AUXILIARY TANK LOWER SURFACE HAS CORROSION. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AN D INSTALLED PER JOSSAIR CO E.O. 18R572001. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3, ITEM NR 31. (X) 2 L 7 4 4F 4A25 1998091800923 19980918 00923 1998 9 18 ARWA980801 4 19980803 A 3416 A3861910005 ALTIMETER DOUG DC8 DC862 3021970 WP COCKPIT FAILED A ARWA O OTHER O OTHER DE DESCENT 1 SO 19 8968U 294B 46069 JFK - FLT 9974 - INBOUND LOG ITEM: F/O ALTIMETER INTERMITTENT. STICKS AT ALTITUDE THEN ROLLS. REMOVED AND REPLACED AL TIMETER IAW MM 34-16-0. OPS NORMAL. (X) 2 L 7 4 4F 4A25 1998091800924 19980918 00924 NM 1998 9 18 P2EA98133 1 19980710 A 5312 BULKHEAD BOEING 737 737247 138448D NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 C-CHECK ITEM. BS 727 BULKHEAD SKIN CRACKED RBL 32, WL 200.5. DEFECT SIZE - 1.375 INCH. REPAIRED FUSELAGE BULKHEAD WEB AT BS 727, WL 194.25 AND WL 202 BETWEEN RBL 26.5 AND RBL 39.25 PER BOEING FAX COO-SJO-98-0486RR DATED 7-16-98. DOCUMEN TED ON FAA FORM 8110-3. APPROVED AND SUBMITTED BY FAA DER D.L. JENSEN DESIGNATION NM-2605 DATED 7-27-98, AND, COOPESA E .O. COO-SJO-53-366-98 DATED 7-17-98. SEE COOPSEA W.O. L1-01616-1-33, VAM 100 NR 155. (X) 2 L 7 2 4F A16WE 1998091800925 19980918 00925 NM 1998 9 18 P2EA98132 1 19980729 A 5311 FRAME BOEING 737 737247 138448D NM BS 420 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 C-CHECK ITEM. FUSELAGE FRAME CRACKED AT BS 420 BETWEEN STR 20R AND STR 21R. REPAIRED FUSELAGE FRAME SECTION AT BS 420 BETWEEN STR 19R AND 21R PER SRM 53-40-3 FIG 1. SEE COOPESA W.O. L1-0616-1-86, VAM 100 NR 486. (X) 2 L 7 2 4F A16WE 1998091800926 19980918 00926 NM 1998 9 18 P2EA98131 1 19980713 A 5311 FRAME BOEING 737 737247 138448D NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 C-CHECK ITEM. FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FUSELAGE FRAME SECTION AT BS 360 BETWEEN STR 19R AND 21R PER SRM 51-40-3 FIG 1. SEE COOPESA W.O. L1-0616-1-89, VAM 100 NR 499. (X) 2 L 7 2 4F A16WE 1998091800927 19980918 00927 NM 1998 9 18 P2EA98130 1 19980712 A 5330 SKIN BOEING 737 737247 138448D NM BS 943-BS 975 CRRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 19603 C-CHECK ITEM. R2 DOOR CUT-OUT LOWER FORWARD OUTER FUSELAGE SKIN CRACKED. DEFECT SIZE - 2.000 INCH. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 943 AND BS 975, STR 16R AND STR 19R PER SRM 53-30-3 FIG 24. SEE COOPESA W.O. L1-0616-2-171, VAM 100 NR 448. (X) 2 L 7 2 4F A16WE 1998091800928 19980918 00928 NM 1998 9 18 P2EA98116 1 19980620 A 5313 STRINGER BOEING 737 737222 1384473 NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 DURING C-CHECK WHILE PERFORMING SPECIAL ITEM J253-10-12L, STR 18A LEFT, SHEAR BEAM WAS FOUND CRACKED. THE CRACK WAS 1.2 5 INCHES LONG. CRACK REPAIRED IAW SB 737-53-1066 REV 3 DATED 9-24-82. SECTION III PART III. REF: COOPESA W.O. NR L1-0 630-2-154. VAM100-203, 208SDA010, SB 737-53-1066. (X) 2 L 7 2 4F A16WE 1998091800929 19980918 00929 NM 1998 9 18 P2EA98115 1 19980615 A 5320 SUPPORT BOEING 737 737222 1384473 NM BS 500 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 DURING C-CHECK ROUTINE INSPECTION PER WORK CARD J2C-512525, CRACKS WERE FOUND AT THE FOLLOWING LOCATION: ANTENNA SUPPOR T CHANNEL AT BS 500 AND BS 500A, BETWEEN STR 28L AND STR 28R. REPLACED ANTENNA SUPPORT CHANNEL IAW SRM 51-10-1 PG 5. F ABRICATED PARTS IAW SRM'S 51-20-1, 51-10-2, 51-10-1, AND 51-30-2. REF: COOPESA W.O. NR L1-0630-1-23, VAM 100-186, 208S DA009. (X) 2 L 7 2 4F A16WE 1998091800930 19980918 00930 NM 1998 9 18 P2EA98114 1 19980611 A 5313 STRINGER BOEING 737 737222 1384473 NM BS 500/BS 528 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 DURING C-CHECK WHILE PERFORMING ROUTINE INSPECTION PER WORK CARD J2C-512525, CORROSION WAS FOUND AT STR 26 LEFT BETWEEN BS 500 B + 16 INCHES AND BS 528. THE CORROSION WAS OUT OF LIMITS (10 PERCENT REMOVED) PER THE SRM. THE STRINGER WAS RE PAIRED IAW SRM 53-10-03, FIG 1, SHT 6. REF: COOPESA W.O. L1-0630-1-32, VAM100-195, 208SKA005. (X) 2 L 7 2 4F A16WE 1998091800931 19980918 00931 EU 1998 9 18 SABA290036 1 19980720 A 7712 8691691M SENSOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A SABA K NONE O OTHER CR CRUISE 1 SO 33 962AE 2169304 962 LEX/CLT - FLT 5201 - PILOT REPORTED LT TORQUE FLUX 30 TO 40 PERCENT AT 6,000 FEET AND BELOW TORQUE SEEMED OK. AIRCRAFT LANDED AT CHARLOTTE WITH NO PROBLEMS. NO IN-FLIGHT EMERGENCY DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGIN E P-2 SENSOR. SYSTEM RUN AND OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A56EU 1998091800932 19980918 00932 EU 1998 9 18 SABA290037 1 19980721 A 7712 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE LOOSE A SABA K NONE N FALSE WARNING CR CRUISE 1 SO 33 962AE 962 LEX/CLT - FLT 5167 - PILOT REPORTED LT ENGINE TORQUE FLUX ALONG WITH EGT AND RPM. NO IN-FLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED AT CLT WITH NO OTHER PROBLEMS. MAINTENANCE FOUND A LOOSE CANNON PLUG ON THE LEFT TORQUE SIGNAL BRIDGE. TORQUE SIGNAL BRIDGES WERE ALSO SWAPPED OUT. RE-TORQUE CANNON ON LT SIGNAL BRIDGE, GROUND RUN AND OPS CHECKED GOOD. ( X) 2 L 7 2 4T RT A56EU 1998091800933 19980918 00933 EU 1998 9 18 SABA290038 1 19980727 A 3234 SELECTOR BAG JETSTM JETSTM3201 1500217 EU MLG TRIPPED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 961AE 961 RDU - FLT 5142 - ON FLIGHT 5142 FROM RWI TO CLT, THE LANDING GEAR WOULD NOT RETRACT. AIRCRAFT DIVERTED TO RDU. AIRCRAF T LANDED WITH NO OTHER PROBLEMS. NO IN-FLIGHT EMERGENCY DECLARED. MAINTENANCE FROM CLT WAS DEPLOYED TO RDU. LANDING G EAR WAS INSPECTED AND FOUND THE EMERGENCY HYD SELECTOR GEAR RELEASE PIN POPPED. RESET PIN AND OPS CHECKED GEAR. AIRCRA FT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998091800934 19980918 00934 NE 1998 9 18 ORJA98140 2 19980629 A 7313 6A5548 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20040 SJC - MAINTENANCE DISCOVERED NR 2 ENGINE AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENG UPPER AND LOWER C-DU CTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. ACFT FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MA INT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES I N THE BRACKET ASSY (BRACKETS 14, 16, AND 19). MAINT PERFORMED INTERIM REPAIR TO UPPER AND LOWER C-DUCTS AND AFT COWL LA TCH DOOR IAW ROHR ENG DOC NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK (7-98). MAINT REMOVED AND REPLACED DEFE CTIVE FUEL NOZZLE BRACKETS. NOTE: NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800935 19980918 00935 NE 1998 9 18 ORJA98139 2 19980703 A 7313 6A4747 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 902RA 6169 53490 V20049 MAINTENANCE DISCOVERED ON NR 1 ENGINE AT NR'S 2, 16, AND 20 POSITIONS, THE FUEL NOZZLE BRACKETS WERE LOOSE DUE TO ELONGA TIONS OF THE BOLT HOLES. MAINTENANCE REPLACED THE BRACKETS. AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NE VER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800936 19980918 00936 NE 1998 9 18 ORJA98138 2 19980703 A 7313 6A4745 BRACKETS DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 902RA 6169 53490 V20049 MAINTENANCE DISCOVERED ON NR 1 ENGINE, AT NR'S 2, 16, AND 20 POSITIONS. THE FUEL NOZZLE BRACKETS WERE LOOSE DUE TO ELON GATIONS OF THE BOLT HOLES. MAINTENANCE REPLACED THE BRACKETS. AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800937 19980918 00937 NE 1998 9 18 ORJA98137 2 19980629 A 7313 2A1226 GASKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20037 SJC - MAINTENANCE DISCOVERED ON THE NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS WERE DELAMINATED AND DISBONDED BEYOND LIMIT S. AIRCRAFT FERRIED TO RENO FOR REPAIRS. MAINT DISCOVERED THAT 2 EACH GASKETS (FUEL NOZZLE BRACKET GASKET) WERE DEFECT IVE AT THE NR 17 AND NR 18 POSITIONS. MAINT REPLACED THE UPPER C-DUCT AND REPAIRED THE LOWER C-DUCT IAW ROHR ENGINE DOC UMENT 98VN515. THIS IS AN INTERIM REPAIR WHICH WILL BE PERMANENTLY REPAIRED AT C-CHECK (7-98). MAINT REPLACED THE 2 EA CH DEFECTIVE GASKETS. AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800938 19980918 00938 NE 1998 9 18 ORJA98136 2 19980629 A 7313 6A5857 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20037 SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCR AFT FERRIED TO RENO FOR REPAIR. MAINTENANCE DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF TH E BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT REPLACED THE UPPER C-DU CT AND PERFORMED AN INTERIM REPAIR ON THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-C HECK (7-98). AIRCRAFT WAS RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800939 19980918 00939 NE 1998 9 18 ORJA98135 2 19980629 A 7313 6A5548 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20037 SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCR AFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING DEFECTIVE FUEL NOZZLE BRACKETS. MAINTENANCE REPLACED THE UPPER C-DUCT AND PERFORMED AN I NTERIM REPAIR ON THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAF T RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800940 19980918 00940 NE 1998 9 18 ORJA98134 2 19980629 A 7313 6A4747 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20037 SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCR AFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR IN THE LOWER C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK ( 7-98). AIRCRAFT WAS RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800941 19980918 00941 NE 1998 9 18 ORJA98133 2 19980629 A 7313 6A4746 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20037 SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCR AFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT REPLACED THE DEFECTIVE FUEL N OZZLE BRACKETS. MAINT REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR ON THE LOWER C-DUCT IAW ROHR NR 98VN515 . A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVE R BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800942 19980918 00942 NE 1998 9 18 ORJA98132 2 19980629 A 7313 6A4745 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 1 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20037 SJC - MAINTENANCE DISCOVERED ON NR 1 ENGINE, THE UPPER AND LOWER C-DUCTS DELAMINATED AND DISBONDED BEYOND LIMITS. AIRCR AFT FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MAINT DISCOVERED THE FOLLOWING FUEL NOZZLE BRACKETS LOOSE D UE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET CAUSING HOT AIR LEAKAGE AT NR 18, NR 17 FUEL NOZZLE BRACKETS. MAINT R EPLACED THE DEFECTIVE FUEL NOZZLE BRACKETS. MAINT REPLACED THE UPPER C-DUCT AND PERFORMED AN INTERIM REPAIR ON THE LOWE R C-DUCT IAW ROHR NR 98VN515. A PERMANENT REPAIR WILL BE PERFORMED AT C-CHECK (7-98). AIRCRAFT WAS RETURNED TO SERVICE . NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800943 19980918 00943 NE 1998 9 18 ORJA98131 2 19980703 A 7313 6A4745 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 902RA 6169 53490 V20044 MAINTENANCE DISCOVERED ON NR 2 ENGINE, NR 9 FUEL NOZZLE BRACKET LOOSE DUE TO ELONGATED BOLT HOLES. REMOVED AND REPLACED NR 9 FUEL NOZZLE BRACKETS. AIRCRAFT RETURNED TO SERVICE. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800944 19980918 00944 NE 1998 9 18 ORJA98130 2 19980629 A 7313 6A5857 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20040 SJC MAINTENANCE DISCOVERED NR 2 ENGINE AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENGINE UPPER AND LOWER C- DUCTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. AIRCRAFT FERRIED TO RENO FOR REPAIR. MAINT DISCOVERED THE FOL LOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET ASSY (BR ACKET POSITIONS 14, 16, AND 19). MAINT PERFORMED AN INTERIM REPAIR TO THE UPPER AND LOWER C-DUCTS AND THE AFT COWL LATC H DOOR IAW W/ROHR ENG DOCUMENT NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK (7-98). MAINT REMOVED AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. NOTE: FUEL NOZZLES HAVE NEVER BEEN REPLACED. (X) 2 L 7 2 4F 4 F RT A6WE E40NE 1998091800945 19980918 00945 NM 1998 9 18 SWAA981577 1 19980802 A 2133 OUTFLOW VALVE BOEING 737 7373H4 1384600 NM CABIN MALFUNCTIONED A SWAA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 623SW 27933 DURING FLIGHT AT 35,000 FT 10,000 FT HORN CAME ON, (PRESSURIZATION) COULD NOT BE CONTROLLED IN AUTO, ACT, OR MAN. NEVE R GOT AUTO FAIL IN ALT NOSE GOT GREEN LIGHT BUT COULD NOT CONTROL PRESS, IN MANUAL COULD NOT MOVE OUTFLOW VALVE UNTIL 10 ,000 FT THEN IT BROKE LOOSE AND WE COULD CONTROL IN MAN. PASS 02 MASKS DID DEPLOY AUTOMATICALLY AT 14,000. REMOVED AND REPLACED CONTROL, OUTFLOW VALVE AND PRESSURE CONT OVERHEAD. OPS CK GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800946 19980918 00946 NM 1998 9 18 SWAA981578 1 19980731 A 3245 26015711 TIRE BOEING 737 7372H4 138448C NM NR 1 FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 053SW 21535 AIR RETURN WITH NR 1 MAIN TIRE BLEW ON TAKEOFF DAMAGING ATTACHED GEAR DOOR AND PUNCHING HOLE IN INBOUND AFT SECTION OF N R 1 ENGINE NACELLE. FOUND LEFT GEAR CENTER AND INNER DOOR DAMAGE FROM TIRE BURST. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 AND NR 2 MLG TIRE ASSY PER BOEING MM, BITE TEST ANTISKID CK GOOD. REMOVED AND REPLACED LEF T GEAR UPPER CENTER AND INNER DOOR RIGG CK GOOD OPS CK GOOD PER MM. 2 L 7 2 4F A16WE 1998091800947 19980918 00947 NM 1998 9 18 SWAA981580 1 19980803 A 2410 CSD BOEING 737 7372H4 138448C NM NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 056SW 21721 AIR RETURN DUE TO NR 1 GEN LOW OIL PRESSURE LIGHT ILLUMINATED DURING TAKEOFF. DISCONNECTED NR 1 CSD. APU FIRE DETECTIO N SYSTEM INOP. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 CSD ASSYS PER BOEING MM. RAN ENGINE OPS CK'D OK AND CHANGE IN LINE FILTER LEAK CK'D OK. 2 L 7 2 4F A16WE 1998091800948 19980918 00948 NM 1998 9 18 SWAA981581 1 19980731 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING WALKAROUND CHECK, FOUND APPROX 3 SKIN CRACK RIGHT TOP SIDE OF FUSELAGE BETWEEN CABIN WINDOWS 10 AND 11. REPAIRE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800949 19980918 00949 NM 1998 9 18 SWAA981582 1 19980731 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND BS 400 STRINGER CLIP 23L CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800950 19980918 00950 NM 1998 9 18 SWAA981583 1 19980731 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 328-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 328 TO 344 LBL 10. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800951 19980918 00951 NM 1998 9 18 SWAA981584 1 19980731 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 308.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 308.5, RBL 10.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800952 19980918 00952 NM 1998 9 18 SWAA981585 1 19980731 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED BELTFRAME LEG AT BS 500C, RBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800953 19980918 00953 NM 1998 9 18 SWAA981586 1 19980731 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 500 SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND RIVET HEAD SHEARED AT AFT BULKHEAD LOWER ANGLE AT BS 500D RBL 13.5. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800954 19980918 00954 NM 1998 9 18 SWAA981587 1 19980731 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AFT BULKHEAD LOWER ANGLE AT BS 500D, RBL 24, LBL 24. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800955 19980918 00955 NM 1998 9 18 SWAA981588 1 19980731 A 5320 FRAME BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER CORNER AT BS 294.5 AT Z ANGLE. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800956 19980918 00956 NM 1998 9 18 SWAA981589 1 19980731 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED UPPER WEB ANGLE AT BS 767 THRU 793 RBL 22. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800957 19980918 00957 NM 1998 9 18 SWAA981590 1 19980731 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED TRANSITION ANGLE AT BS 727-767, RBL 21 AND BS 727C-827. 2 L 7 2 4F RT A16WE 1998091800958 19980918 00958 NM 1998 9 18 SWAA981591 1 19980731 A 5312 BULKHEAD BRACKET BOEING 737 7373H4 1384600 NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND FWD BULKHEAD PANEL SUPPORT BRACKET CRACKED CENTER BOTTOM NEXT TO BLEED AIR DUCT. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800959 19980918 00959 NM 1998 9 18 SWAA981592 1 19980731 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED TRANSITION ANGLE NUT PLATES HOLES AT BS 727-727C, LBL 21. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800960 19980918 00960 NM 1998 9 18 SWAA981593 1 19980731 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 368SW 26579 DURING SCHEDULED 1/2D CHECK, FOUND REMOVED CABIN EGRESS LIGHTING FOM. INSTALLED EGRESS TRACK LIGHTING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800961 19980918 00961 NM 1998 9 18 SWAA981594 1 19980731 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 502SW 24179 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP AT MID CABIN. RECONNECTED EMERGENCY FLOOR TRACK LIGHT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800962 19980918 00962 NM 1998 9 18 SWAA981595 1 19980801 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED WEB AT BS 179, LBL 32, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800963 19980918 00963 NM 1998 9 18 SWAA981596 1 19980801 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 400-420 BENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND BENT AT BS 400 TO 420 WEB BELOW RT TRANSITION ANGLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800964 19980918 00964 NM 1998 9 18 SWAA981597 1 19980801 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 460-480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND BENT AND CRACKED WEB BELOW LT TRANSITION ANGLE AT BS 460 TO 480. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800965 19980918 00965 NM 1998 9 18 SWAA981598 1 19980801 A 5320 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND 2 STOP PADS CORRODED ON AFT FRAME DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800966 19980918 00966 NM 1998 9 18 SWAA981599 1 19980801 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006, LBL 13; BS 955, RBL 9-17; BS 947-967 RBL 8 AND BS 947 - 967, RBL 18. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800967 19980918 00967 NM 1998 9 18 SWAA981600 1 19980801 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED IN AND AROUND CLIP NUT HOLE AT BS 312, LBL 1 AFT LEG; BS 312 LBL 1 FWD LEG; BS 312, LBL 8, AFT LEG AND BS 312, LBL 8, FWD LEG. REPAIRED FLOORBEAM PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800968 19980918 00968 NM 1998 9 18 SWAA981601 1 19980801 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED IN AND AROUND FASTENER AT BS 312, LBL 12. REPAIRED FLOORBEAM PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998091800969 19980918 00969 NM 1998 9 18 SWAA981602 1 19980801 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 757 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AROUND NUT PLATE HOLE AT FLOORBEAM, BS 757 RBL 14. REPAIRED FLOORBEAM PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998091800970 19980918 00970 NM 1998 9 18 SWAA981603 1 19980801 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STRINGER AT BS 787, 21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800971 19980918 00971 NM 1998 9 18 SWAA981604 1 19980801 A 5754 BRACKET BOEING 737 7375H4 138449D NM RT LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C2 CHECK, FOUND K-FLAP MOST I/B SEAL BRACKET CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800972 19980918 00972 NM 1998 9 18 SWAA981605 1 19980801 A 5400 BRACKET BOEING 737 7375H4 138449D NM PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 524SW 26566 DURING SCHEDULED C2 CHECK, FOUND NR 6 CANOE/PYLON AREA O/B SIDE ANGLE BRACKET CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800973 19980918 00973 NM 1998 9 18 SWAA981606 1 19980802 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND BS 947 RBL 22 LBL 22 AFT BULKHEAD CORNER ANGLE SURFACE CORRODED AROUND FLOORBEAM HOLE . REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800974 19980918 00974 NM 1998 9 18 SWAA981607 1 19980802 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM CARGO COMPT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND O/B FLANGE OF RT CARGO TRACK AT TIE DOWN BROKEN OFF. REPAIRED FLOORBEAM PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998091800975 19980918 00975 NM 1998 9 18 SWAA981608 1 19980802 A 5320 BAFFLE BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND BAFFLE CRACKED BETWEEN BS 500A AND 500B RT SIDE UNDER INTERCOSTAL. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998091800976 19980918 00976 NM 1998 9 18 SWAA981609 1 19980802 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500B, STR 24L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800977 19980918 00977 NM 1998 9 18 SWAA981550 1 19980729 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY DOOR SKIN CRACKED AT LOWER HINGE CUTOUT LWR CORNER. 2 L 7 2 4F A16WE 1998091800978 19980918 00978 NM 1998 9 18 SWAA981610 1 19980803 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITIONAL ANGLE CRACKED AT BS 727C. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800979 19980918 00979 NM 1998 9 18 SWAA981611 1 19980803 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CLIP CRACKED BELOW RT TRANSITION ANGLE AFT AT BS 727A BELTFRAME. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800980 19980918 00980 NM 1998 9 18 SWAA981612 1 19980803 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT BS 178, RBL 32, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800981 19980918 00981 NM 1998 9 18 SWAA981613 1 19980803 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 1006 & 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL BETWEEN BS 1006 AND 1016 LBL 37. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091800982 19980918 00982 NM 1998 9 18 SWAA981614 1 19980803 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 950 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 950, RBL 31 TO RBL 47. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091800983 19980918 00983 NM 1998 9 18 SWAA981615 1 19980803 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT BS 727+13, RBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800984 19980918 00984 NM 1998 9 18 SWAA981616 1 19980803 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636SW 27709 DURING WALKAROUND CHECK, FOUND EGRESS LIGHTING LOOSE ROW 3 AND 4. REPAIRED AND SECURED EGRESS LIGHTING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800985 19980918 00985 NM 1998 9 18 SWAA981617 1 19980804 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 359SW 26573 DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP ROWS 12 TO 15. RELAMPED AND RECONFIGURED PER BOEI NG MM. 2 L 7 2 4F RT A16WE 1998091800986 19980918 00986 NM 1998 9 18 SWAA981618 1 19980804 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 371SW 26598 DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS LIGHTS OUT MID AIRCRAFT WIRING LOOSE AND COVERS. REINSTALLED TRACK LIGH TING WIRING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800987 19980918 00987 NM 1998 9 18 SWAA981619 1 19980804 A 5330 SKIN BOEING 737 7372K6 NM BS 374 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 374 STR 15L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800988 19980918 00988 NM 1998 9 18 SWAA981620 1 19980804 A 5320 ANGLE BOEING 737 7373H4 1384600 NM GALLEY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED LT Z ANGLE AROUND CLIP NUT HOLES. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800989 19980918 00989 NM 1998 9 18 SWAA981621 1 19980804 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 300 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND WEB FWD OF DOOR FRAME AT BS 300 BELOW STR 13 WORN. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998091800990 19980918 00990 NM 1998 9 18 SWAA981622 1 19980804 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER FLANGE AFT AT BS 344, LBL 9. REPAIRED PER TRAMCO TR TI-553-006. 2 L 7 2 4F RT A16WE 1998091800991 19980918 00991 NM 1998 9 18 SWAA981629 1 19980804 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER FWD FLANGE AT BS 344, LBL 7. REPAIRED PER TRAMCO TR TI-553-006. 2 L 7 2 4F RT A16WE 1998091800992 19980918 00992 NM 1998 9 18 SWAA981623 1 19980804 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER FWD FLANGE AT BS 344, LBL 0. REPAIRED PER TRAMCO TR TI-553-006. 2 L 7 2 4F RT A16WE 1998091800993 19980918 00993 NM 1998 9 18 SWAA981624 1 19980804 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT FASTENER HOLE FLOORBEAM UPPER AFT FLANGE AT BS 344, RBL 1; AND UPPER FWD FLANGE AT BS 344, LBL 7. REPAIRED PER TRAMCO TI-553-006. 2 L 7 2 4F RT A16WE 1998091800994 19980918 00994 NM 1998 9 18 SWAA981625 1 19980804 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 277-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT FWD DOORWAY Z ANGLE CORRODED UPPER AND LOWER SURFACE FROM BS 277 TO BS 3 44. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800995 19980918 00995 NM 1998 9 18 SWAA981626 1 19980804 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 911-927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED ON STRINGER 26L AT BS 911-927. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800996 19980918 00996 NM 1998 9 18 SWAA981627 1 19980804 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED 1/2D CHECK, FOUND BARE METAL SURFACE ON WEB CORRODED AT BS 1006-1016. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800997 19980918 00997 NM 1998 9 18 SWAA981628 1 19980804 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND CRACKED BS 178 BULKHEAD WL 188 RBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091800998 19980918 00998 NM 1998 9 18 SWAA981630 1 19980805 A 2424 GCU BOEING 737 7373A4 1384585 NM NR 1 FAILED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 680SW 23505 AIRCRAFT ROUTED FROM BWI TO TPA DIVERTED INTO JAX. IN FLT FL350 SMOKE ENTERED COCKPIT IN VICINITY OF GCU NR 1 AND NR 1 GENERATOR DROPPED OFF LINE. PULLED NR 1 GCU CB AND SMOKE DISSIPATED. APU STARTED AND POWERED NR 1 GEN BUS NORMALLY. A/ C DIVERTED WITH NO FUTHER PROBLEMS. MADE AN UNEVENTFUL LANDING. VERIFIED CSD OIL QTYS AND APU OIL QTY PLACARED NR 1 GE NERATOR PER MEL. REMOVED AND REPLACED NR 1 GCU PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091800999 19980918 00999 NM 1998 9 18 SWAA981631 1 19980805 A 4920 APU BOEING 737 7373H4 1384600 NM AFT FUSELAGE INOPERATIVE A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 647SW 28332 AT GATE NOTICED SMOKE IN CABIN. HEAVY SMOKE OUT OF APU TAILPIPE, APU INOP. REMOVED AND REPLACED APU PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801000 19980918 01000 NM 1998 9 18 SWAA981632 1 19980805 A 3244 TIRE BOEING 737 7372H4 138448C NM NR 4 FAILED A SWAA K NONE O OTHER CL CLIMB 1 SW 07 074SW 22674 DURING TAKEOFF ROLL, NR 4 TIRE BLEW WITH DAMAGE ON RT INBOARD AFT FLAP RT INNER GEAR DOOR. 2 L 7 2 4F A16WE 1998091801001 19980918 01001 NM 1998 9 18 SWAA981633 1 19980805 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 087SW 22903 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY DOOR RT AND LT LIGHTS OUT. REMOVED AND REPLACED OVERWING EMERG ENCY DOOR RT AND LT LIGHT CARTRIDGE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801002 19980918 01002 NM 1998 9 18 SWAA981634 1 19980805 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 760 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN CRACKED BELOW STR 18R AT BS 760. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091801003 19980918 01003 NM 1998 9 18 SWAA981635 1 19980805 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 948-990 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT Z-ANGLE AT BS 948 TO 990. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801004 19980918 01004 NM 1998 9 18 SWAA981636 1 19980805 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED WEB AFT FROM 1016 FLOORBEAM RT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801005 19980918 01005 NM 1998 9 18 SWAA981637 1 19980805 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 767-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AROUND FLOORBOARD HOLES AT BS 767 TO 847. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998091801006 19980918 01006 NM 1998 9 18 SWAA981638 1 19980805 A 5321 FLOORBOARD BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED SURFACE AND FLOORBOARD HOLES LEFT TRANSITION ANGLE AT BS 727E-947. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801007 19980918 01007 NM 1998 9 18 SWAA981639 1 19980805 A 5320 STRAP BOEING 737 7373A4 1384585 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679SW 23291 DURING SCHEDULED BC1 CHECK, FOUND FLOORBEAM SUPPORT STRAP CRACKED LT O/B AT BS 328. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801008 19980918 01008 NM 1998 9 18 SWAA981640 1 19980805 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND FWD GALLEY DOOR LWR AFT INNER DOUBLER CRACKED IN AFT FRAME LOWER CORNER. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801009 19980918 01009 NM 1998 9 18 SWAA981641 1 19980806 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C2 CHECK, FOUND INTERCOSTAL CRACKED CARGO BIN FOR DOOR UPLOCK. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091801010 19980918 01010 NM 1998 9 18 SWAA981642 1 19980806 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702SW 22054 DURING SCHEDULED SERVICE CHECK, FOUND FWD SEVEN EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK AND HOU SING ASSY PER BOEING MM, OPS CHECK NORMAL. 2 L 7 2 4F A16WE 1998091801011 19980918 01011 NM 1998 9 18 SWAA981643 1 19980806 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 988 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED WEB FLOOR LEVEL AT BS 988, RBL 42. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801012 19980918 01012 NM 1998 9 18 SWAA981644 1 19980806 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986.5-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006 BL 0. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801013 19980918 01013 NM 1998 9 18 SWAA981645 1 19980806 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1121 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED SHEAR TIE AT BS 1121, LT INSIDE LIGHTENING HOLE APU CAVITY. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998091801014 19980918 01014 NM 1998 9 18 SWAA981646 1 19980806 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 927-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED WEB UPPER ANGLE AT BS 927 TO 947 BL 0. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801015 19980918 01015 NM 1998 9 18 SWAA981647 1 19980806 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 967-986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL BETWEEN BS 967 AND 986.5 RBL 18. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998091801016 19980918 01016 NM 1998 9 18 SWAA981648 1 19980806 A 5320 ANGLE BOEING 737 7373H4 1384600 NM RT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND ANGLE HAS WASHER WORN THRU JUST I/B OF I/B FOREFLAP. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801018 19980918 01018 NM 1998 9 18 SWAA981650 1 19980806 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 848 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED RON CHECK, FOUND GOUGE AND DENTED FUSELAGE SKIN AT BS 848 STR 18L. REPAIRED CUT OUT DAMAGED SKIN PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998091801019 19980918 01019 NM 1998 9 18 SWAA981651 1 19980806 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 953 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN DENTED 15 BELOW AFT GALLEY DOOR FWD LOWER CORNER BS 953 WL 196 RBL 53. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801020 19980918 01020 NM 1998 9 18 SWAA981652 1 19980806 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1015 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR WEB AT BS 1015 LBL 38 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801021 19980918 01021 NM 1998 9 18 SWAA981653 1 19980806 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM UPPER CHORD BS 328, RBL 29, 33, 35.5 AND RBL 42.5 WL 208 AND WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801022 19980918 01022 NM 1998 9 18 SWAA981655 1 19980806 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FLOOR STIFFENER CRACKED AT BS 328, LBL 45.5, WL 204 AFT SIDE OF FLOORBEAM. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801023 19980918 01023 NM 1998 9 18 SWAA981656 1 19980806 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FLOOR STIFFENER CRACKED AT BS 328, RBL 32, WL 201. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801024 19980918 01024 NM 1998 9 18 SWAA981657 1 19980806 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD AT BS 344, LBL 9, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801025 19980918 01025 NM 1998 9 18 SWAA981658 1 19980806 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 345 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 345, BL 0 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801026 19980918 01026 NM 1998 9 18 SWAA981659 1 19980806 A 5330 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679SW 23191 DURING SCHEDULED D-CHECK, FOUND LOWER FUSELAGE SKIN HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801027 19980918 01027 NM 1998 9 18 SWAA981660 1 19980806 A 3350 LIGHTS BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED SERVICE CHECK, FOUND TWO EMERGENCY LIGHTS INOP IN FLOOR TRACK ROW 10. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801028 19980918 01028 NM 1998 9 18 SWAA981664 1 19980807 A 5330 SKIN BOEING 737 7373A4 1384585 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 673SW 23252 DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR LOWER FUSELAGE HINGE CUTOUT HAS A 1.25 SKIN CRACKED AND A 1 BARE STRAP CRACKED. REPAIRED PER SWA RA 1-353-1869. 2 L 7 2 4F RT A16WE 1998091801029 19980918 01029 NM 1998 9 18 SWAA981665 1 19980807 A 5320 BEAM BOEING 737 7373H4 1384600 NM LEFT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED LEFT HAND STABILIZER BEAM. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801030 19980918 01030 NM 1998 9 18 SWAA981666 1 19980807 A 5320 ANGLE BOEING 737 7373H4 1384600 NM LEFT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED LEFT HAND STABILIZER BEAM PANEL L-ANGLES ARE CHAFED. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801031 19980918 01031 NM 1998 9 18 SWAA981667 1 19980807 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED WEB AT BS 178 WL 218 LBL 11. REPAIRED CUTOUT DAMAGED PER SWA RA NR 13531864. 2 L 7 2 4F RT A16WE 1998091801032 19980918 01032 NM 1998 9 18 SWAA981668 1 19980807 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INDICATIONS AT BS 178 BULKEHAD WL 207 IN WEB BENEATH SUPPORT ANGLE AT RBL 1 W L 207 LBL 1 IN WEB BENEATH SUPPORT. REPAIRED PER SWA RA NR 13531864. 2 L 7 2 4F RT A16WE 1998091801033 19980918 01033 NM 1998 9 18 SWAA981669 1 19980808 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION BELOW STR 28R AT BS 500C + 10. REPAIRED PER SWA RA NR 13531864. 2 L 7 2 4F RT A16WE 1998091801034 19980918 01034 NM 1998 9 18 SWAA981670 1 19980808 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON FLOORBEAM FWD FLANGE AT BS 1016 RBL 11. REPAIRED PER SWA RA NR 1-353-18 64. 2 L 7 2 4F RT A16WE 1998091801035 19980918 01035 NM 1998 9 18 SWAA981671 1 19980808 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INDICATIONS AT BS 178 BULKHEAD WEB, LBL 5.7 AND WL 211. REPAIRED PER SWA RA NR 1-353-1864. 2 L 7 2 4F RT A16WE 1998091801036 19980918 01036 NM 1998 9 18 SWAA981672 1 19980808 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED AT BS 178 BULKHEAD, WL 207, LBL 11. REPAIRED PER SWA RA NR 1-353-1864. 2 L 7 2 4F RT A16WE 1998091801037 19980918 01037 NM 1998 9 18 SWAA981673 1 19980808 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 202 & 204 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND 2 CRACKS UNDER VERTICAL STRAP LBL 5, WL 202 AND 204. ALSO AT RBL 5, WL 202 AND 204 A T FWD SIDE. REPAIRED PER SWA RA NR 1-353-1864. 2 L 7 2 4F RT A16WE 1998091801038 19980918 01038 NM 1998 9 18 SWAA981674 1 19980808 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND 4 INDICATIONS OF CRACKS FROM 3 FASTENER HEADS IN FWD SIDE OF BLKHD WL 234 LBL 9. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801039 19980918 01039 NM 1998 9 18 SWAA981675 1 19980809 A 3350 LIGHT BOEING 737 7372H4 138448C NM PAX DOOR INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY AND FWD SERVICE DOOR EMERGENCY SLIDE LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY PER BOEING MM. 2 L 7 2 4F A16WE 1998091801040 19980918 01040 NM 1998 9 18 SWAA981676 1 19980809 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR LOWER EMERGENCY EXIT LIGHT OUT. REPAIRED PER BOEING MM, OPS CK G OOD. 2 L 7 2 4F A16WE 1998091801041 19980918 01041 NM 1998 9 18 SWAA981677 1 19980809 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED SERVICE CHECK, FOUND ONE RED FLOOR TRACK LIGHT INOP AT CENTER CABIN. REPAIRED PER BOEING MM, OPS CK GO OD. 2 L 7 2 4F A16WE 1998091801042 19980918 01042 NM 1998 9 18 SWAA981678 1 19980809 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 513SW 24190 DURING SCHEDULED SERVICE CHECK, FOUND ONE AFT EMERGENCY FLOOR TRACK LIGHT INOP. REPLACED LIGHT TRACK ASSEMBLY PER BOEIN G MM, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1998091801043 19980918 01043 NM 1998 9 18 SWAA981679 1 19980809 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED LT TRANSITION ANGLE FROM BS 500 TO BS 500D LBL 20. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801044 19980918 01044 NM 1998 9 18 SWAA981680 1 19980809 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 540 LBL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801045 19980918 01045 NM 1998 9 18 SWAA981681 1 19980809 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 767-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 767-847, RBL 13 AROUND TIE DOWNS FLOORBOARDS HOLES ON FLOORBEAM. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801046 19980918 01046 NM 1998 9 18 SWAA981683 1 19980809 A 5321 FLOORBOARD BOEING 737 7373H4 1384600 NM BS 767-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 767-847, LBL 3 AROUND FLOORBOARDS HOLES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801047 19980918 01047 NM 1998 9 18 SWAA981684 1 19980809 A 5321 FLOORBOARD BOEING 737 7373H4 1384600 NM BS 767-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 767-847 LBL 8 AROUND FLOORBOARDS HOLES. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801048 19980918 01048 NM 1998 9 18 SWAA981685 1 19980809 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 847-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 847-947 FLOORBEAM, RBL 13 AROUND TIE DOWNS AND FLOORBOARD HOLES. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801049 19980918 01049 NM 1998 9 18 SWAA981682 1 19980809 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 847-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AT BS 847-947 RBL 7 LBL 12 AROUND FLOORBOARD HOLES. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091801050 19980918 01050 NM 1998 9 18 SWAA981686 1 19980809 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AROUND NUT PLATE HOLE ON FLOORBEAM RBL 8, BS 727E + 2. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801051 19980918 01051 NM 1998 9 18 SWAA981687 1 19980809 A 5320 ANGLE BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND ANGLE CRACKED AT AILERON MIDDLE HINGE WBL 494. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801052 19980918 01052 NM 1998 9 18 SWAA981688 1 19980809 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED RT SIDE CHORD AT BS 178 RBL 32 WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801053 19980918 01053 NM 1998 9 18 SWAA981689 1 19980809 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 522 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND 1.25 INCH CRACK, FUSELAGE SKIN AT BS 522 LBL 5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801054 19980918 01054 NM 1998 9 18 SWAA981690 1 19980809 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED SUPPORT CHANNEL ON PANEL I/B OF NR 5 GROUND SPOILER. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998091801055 19980918 01055 NM 1998 9 18 SWAA981691 1 19980810 A 5730 SKIN BOEING 737 7373H4 1384600 NM BS 213 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED BC3 CHECK, FOUND L/E BS 213 KRUEGER FLAP CUTOUT CRACKED APPROX .625 IN LENGTH. REPAIRED PER SWA ACO 68 20-57. 2 L 7 2 4F RT A16WE 1998091801056 19980918 01056 NM 1998 9 18 SWAA981692 1 19980807 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT OUT. REPAIRED EMERGENCY EXIT LIGHT PER BOEING MM . 2 L 7 2 4F A16WE 1998091801057 19980918 01057 NM 1998 9 18 SWAA981693 1 19980807 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 502SW 24179 DURING WALKAROUND CHECK, FOUND EMERGENCY TRACK LIGHTING AT ROW 5 HAS EXPOSED WIRES. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801058 19980918 01058 NM 1998 9 18 SWAA981694 1 19980808 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A S SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS (4 EA) AT ROW 12-13 INOP. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998091801059 19980918 01059 NM 1998 9 18 SWAA981696 1 19980810 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED ANGLE AT BS 500D, RBL 20, LBL 20. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801060 19980918 01060 NM 1998 9 18 SWAA981697 1 19980810 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 494 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND PANEL AFT OF FWD CARGO DOOR CUTOUT DAMAGED AT BS 494, RBL 22. REPAIRED PER BOEING MM . 2 L 7 2 4F RT A16WE 1998091801061 19980918 01061 NM 1998 9 18 SWAA981698 1 19980810 A 3350 20122 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 674SW 23252 DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED RT AFT BATTERY PACK HOUSIN G PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801062 19980918 01062 NM 1998 9 18 SWAA981699 1 19980810 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 & 787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND LT TRANSITION ANGLE ABOVE STRINGER 25L SURFACE CORRODED BETWEEN BS 727C AND 787. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801063 19980918 01063 NM 1998 9 18 SWAA981700 1 19980810 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT STRINGER 4 LT BS 907. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801064 19980918 01064 NM 1998 9 18 SWAA981701 1 19980810 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT STRINGER 4 RT BS 907. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801065 19980918 01065 NM 1998 9 18 SWAA981702 1 19980810 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 386 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH L-ANGLE CRACKED BS 386 WL 207 BL 0. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998091801066 19980918 01066 NM 1998 9 18 SWAA981703 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 727B. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801067 19980918 01067 NM 1998 9 18 SWAA981704 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 867. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801068 19980918 01068 NM 1998 9 18 SWAA981705 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 500C. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801069 19980918 01069 NM 1998 9 18 SWAA981706 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 440. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801070 19980918 01070 NM 1998 9 18 SWAA981707 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 8R AND 9R AT BS 400. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801071 19980918 01071 NM 1998 9 18 SWAA981708 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 767 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 767, RBL 35, WL 160. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801072 19980918 01072 NM 1998 9 18 SWAA981709 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 727, RBL 34, WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801073 19980918 01073 NM 1998 9 18 SWAA981710 1 19980810 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 727E, LBL 25.5, WL 157. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801074 19980918 01074 NM 1998 9 18 SWAA981711 1 19980810 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 589 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FLOOR PANEL TIE STRAP CORRODED AT BS 589, RBL 18 LBL 21 WL 165. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801075 19980918 01075 NM 1998 9 18 SWAA981712 1 19980810 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 440-492 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB TIE STRAP AT BS 440 TO 492 RBL 22 WL 157. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998091801076 19980918 01076 NM 1998 9 18 SWAA981713 1 19980810 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 807 CREASE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CREASE IN SKIN AT BS 807 BETWEEN STR 27L AND 27R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801077 19980918 01077 NM 1998 9 18 SWAA981714 1 19980810 A 5720 ANGLE BOEING 737 7372T4 1384492 NM LT WING CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 130SW 22699 DURING SCHEDULED SERVICE CHECK, FOUND O/B STABILIZER BAR SUPPORT ANGLE CORRODED ON LUG FACE. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F A16WE 1998091801078 19980918 01078 NM 1998 9 18 SWAA981715 1 19980811 A 5320 STRAP BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED RON CHECK, HFEC INDICATES BEAR STRAP CRACKED AT LOWER FUSELAGE MOUNTED HINGE FITTING AT FWD SERVICE DOO R. REPAIRED PER SWA RA NR 1-253-1871. 2 L 7 2 4F A16WE 1998091801079 19980918 01079 NM 1998 9 18 SWAA981716 1 19980811 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED RON CHECK, FOUND BODY FRAME AT BS 294.5 CRACKED AT LOWER SERVICE DOOR HINGE CUTOUT, ON AFT SIDE OF FRAM E. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091801080 19980918 01080 NM 1998 9 18 SWAA981717 1 19980811 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 917 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 917, STR 24L CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1998091801081 19980918 01081 NM 1998 9 18 SWAA981718 1 19980811 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT FOR AFT SERVICE AND AFT ENTRY WEAK. REMOVED AND REP LACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F A16WE 1998091801082 19980918 01082 NM 1998 9 18 SWAA981719 1 19980811 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 520 MISREPAIRED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND BLIND RIVETS INSTALLED AT BS 520 STR 11-12 LEFT PREVIOUS PATCH REPAIR ON UPPER LOBE. REMOVED AND REPLACED PREVIOUS REPAIR PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801083 19980918 01083 NM 1998 9 18 SWAA981720 1 19980811 A 5314 KEELBEAM BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED KEEL BEAM CHORD AT BS 727 LBL 6. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801084 19980918 01084 NM 1998 9 18 SWAA981721 1 19980811 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 367 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 318SW 23339 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN FWD OF EQUIPMENT COOLING DUCT AT BS 367. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998091801085 19980918 01085 NM 1998 9 18 SWAA981722 1 19980811 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 26583 DURING SCHEDULED D-CHECK, FOUND CRACKED WEB AT BS 178, LBL 5.7 WL 202. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801086 19980918 01086 NM 1998 9 18 SWAA981723 1 19980811 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 26583 DURING SCHEDULED D-CHECK, FOUND CRACKED SKIN AFT SERVICE DOOR HINGE CUTOUT LOWER RADIUS. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801087 19980918 01087 NM 1998 9 18 SWAA981726 1 19980812 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED UPPER CHORD OF FLOORBEAM AT BS 663 BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801088 19980918 01088 NM 1998 9 18 SWAA981727 1 19980812 A 5320 BEAM BOEING 737 7373H4 1384600 NM COCKPIT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED C3 CHECK, FOUND CORROSION UNDER NLG VIEW DOOR SUPPORT BEAM. REPAIRED PER BOEING TR NR T1-A53-024. 2 L 7 2 4F RT A16WE 1998091801089 19980918 01089 NM 1998 9 18 SWAA981728 1 19980812 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 & 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGER 8 AND 9 LT AT BS 727D AND STRI NGERS 8 AND 9 RT AT BS 440. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801090 19980918 01090 NM 1998 9 18 SWAA981729 1 19980812 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND LOWER STUB FRAME CRACKED AT BS 294, WL 208 RBL 54. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801091 19980918 01091 NM 1998 9 18 SWAA981730 1 19980812 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 270 Z-CHORD, RBL 11, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801092 19980918 01092 NM 1998 9 18 SWAA981732 1 19980812 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND RT TRANSITION ANGLE ABOVE STRINGER 25R CORRODED AROUND FASTENER HOLES BETWEEN BS 727 AND 727B AND BETWEEN BS 727B AND 767. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801093 19980918 01093 NM 1998 9 18 SWAA981733 1 19980812 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 767 & 787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND RT TRANSITION ANGLE WEB BETWEEN BS 767 AND 787 HEAVILY CORRODED AND DETERIORATED. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801094 19980918 01094 NM 1998 9 18 SWAA981734 1 19980812 A 5320 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND LOWER FWD CORNER DOOR FRAME CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801095 19980918 01095 NM 1998 9 18 SWAA981735 1 19980812 A 5320 PLATE BOEING 737 7373H4 1384600 NM CARGO DOORWAY GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB PLATE AFT DOOR CUTOUT ABOVE STRINGER 24R GOUGED/WORN. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801096 19980918 01096 NM 1998 9 18 SWAA981736 1 19980812 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND AFT AT BS 727 PRESS BULKHEAD BL 0, LOWER COMP BEAM CRACKED. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801097 19980918 01097 NM 1998 9 18 SWAA981737 1 19980812 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE FWD FLANGE AT BS 986.5, RBL 28, RBL 36, RBL35, RBL 30, RBL 40 AND RBL 43. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801098 19980918 01098 NM 1998 9 18 SWAA981738 1 19980812 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 10-11 INOP. REPLACED DAMAGED FLOOR TRACK SOCKET AT ROW 10 PER SWA MM. 2 L 7 2 4F RT A16WE 1998091801099 19980918 01099 NM 1998 9 18 SWAA981739 1 19980812 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 16-17 INOP. REPLACED SHORTED SOCKET ASSY IN FLOOR TRAC K AT ROW 16 PER SWA MM. 2 L 7 2 4F RT A16WE 1998091801100 19980918 01100 NM 1998 9 18 SWAA981740 1 19980812 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 784 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721SW 22697 DURING SCHEDULED CI CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 784, STR 17L CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1998091801101 19980918 01101 NM 1998 9 18 SWAA981741 1 19980812 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721SW 22697 DURING SCHEDULED CI CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B+7 AT STR 17R CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091801102 19980918 01102 NM 1998 9 18 SWAA981742 1 19980813 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721SW 22697 DURING SCHEDULED CI CHECK, FOUND EMERGENCY EXIT LIGHT OVER AFT SERVICE DOOR FELL OUT OF MOUNTING. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1998091801103 19980918 01103 NM 1998 9 18 SWAA981743 1 19980813 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 277 STR 24R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801104 19980918 01104 NM 1998 9 18 SWAA981744 1 19980813 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006 LBL 12. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801105 19980918 01105 NM 1998 9 18 SWAA981745 1 19980813 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 967-986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 967 TO 986.5 LBL 18. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801106 19980918 01106 NM 1998 9 18 SWAA981746 1 19980813 A 5320 STANCHION BOEING 737 7373H4 1384600 NM E & E COMP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND FWD RIGHT STANCHION CRACKED E-1 RACK. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801107 19980918 01107 NM 1998 9 18 SWAA981747 1 19980813 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT Z-ANGLE AT BS 947 TO 996. REMOVED AND RPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801108 19980918 01108 NM 1998 9 18 SWAA981748 1 19980813 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 927-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND UPPER WEB ANGLE CRACKED AT BS 927-947, BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801109 19980918 01109 NM 1998 9 18 SWAA981749 1 19980814 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED EMERGENC Y EXIT LIGHT ASSEMBLY AND OPS CKD OK PER BOEING MM. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091801110 19980918 01110 NM 1998 9 18 SWAA981751 1 19980813 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 059SW 21811 DURING SPECIAL VISIT TO DALFORT, REMOVED EMERGENCY BATTERY PACK FOM. INSTALLED EMERGENCY EXIT BATTERIES AND OPS CHECKED GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998091801111 19980918 01111 NM 1998 9 18 SWAA981752 1 19980813 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED C4 CHECK, FOUND AFT CARGO DOOR UPLATCH MECHANISM INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091801112 19980918 01112 NM 1998 9 18 SWAA981753 1 19980813 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AFT FLANGE AT BS 986.5, LBL 9. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091801113 19980918 01113 NM 1998 9 18 SWAA981754 1 19980813 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 296 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND SKIN DENTED AND GOUGED AT BS 296 ABOVE STR 19L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801114 19980918 01114 NM 1998 9 18 SWAA981755 1 19980813 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 720 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND WHEEL WELL ATTACH ANGLE CHAFED FASTENER HOLES AT BS 720, RBL 15, WL 152. REMOVED AND RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801115 19980918 01115 NM 1998 9 18 SWAA981756 1 19980813 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT FLOORBOARD FASTENER HOLE AT BS 947, LBL 53.5 WL 208. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801116 19980918 01116 NM 1998 9 18 SWAA981757 1 19980813 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND BS 616 FRAME INBOARD CHORD CRACKED AT LBL 64 WL 201. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801117 19980918 01117 NM 1998 9 18 SWAA981758 1 19980813 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1124 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 1124, 1 INBOARD OF STR 2 LT. REPAIRED PER TRAMCO EWO NR 980696. 2 L 7 2 4F RT A16WE 1998091801118 19980918 01118 NM 1998 9 18 SWAA981759 1 19980813 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1124 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND GOUGED SKIN AT BS 1124, 1 INBOARD OF STR 2 RT. REPAIRED PER TRAMCO EWO NR 980696. 2 L 7 2 4F RT A16WE 1998091801119 19980918 01119 NM 1998 9 18 SWAA981760 1 19980816 A 2130 3964421 PACK VALVES BOEING 737 7373H4 1384600 NM CABIN MALFUNCTIONED A SWAA G A O2 MASK DEPLOYED UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 623SW 27933 AIRCRAFT UNABLE TO HOLD PRESSURE AT FL350 IN AUTO, CABIN PRESSURE CONTROL PROBLEM. O2 MASK DEPLOYED. WILL HOLD PRESS W ITH BOTH PACKS IN HIGH. MANY 02 MASK'S WERE MELTED DURING STORAGE OF THE MASKS IN FLT. A/C DIVERTED, MADE AN UNEVENTFU L LANDING. REMOVED AND REPLACED LEFT AND RIGHT PACK VALVES, RANG OUT WIRING AND CW DECAY CHECK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801120 19980918 01120 NM 1998 9 18 SWAA981761 1 19980814 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND MISDRILLED HOLE AT BS 986.5 FLOORBEAM RBL 2 WL 208. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998091801121 19980918 01121 NM 1998 9 18 SWAA981762 1 19980814 A 3350 610478 BATTERY CHARGER BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353SW 24889 DURING SCHEDULED A2 CHECK, FOUND AFT SECTION FLOOR PROX EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER AND PACK PER BOEING MM, OPS NORMAL. 2 L 7 2 4F RT A16WE 1998091801122 19980918 01122 NM 1998 9 18 SWAA981763 1 19980814 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 395SW 27689 DURING SCHEDULED A2 CHECK, FOUND FLOOR TRACK LIGHTS AT 16 ROW INOP. RELAMPED FLOOR TRACK AT ROW 16 PER BOEING MM. REMO VED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801123 19980918 01123 NM 1998 9 18 SWAA981764 1 19980814 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636SW 27709 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT FLOOR TRACK LIGHTS INOP AT ROW 12 AND 13. RECONNECTED WIRES PER BO EING MM. 2 L 7 2 4F RT A16WE 1998091801124 19980918 01124 NM 1998 9 18 SWAA981766 1 19980815 A 3350 6104791 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING SCHEDULED SERVICE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHTS WON'T ILLUMINATE. REMOVED AND REPLACED BOTH BATTE RY PACK AND SUPPLY FOR RIGHT OVERWING EMERGENCY LIGHTS PER BOEING MM. 2 L 7 2 4F A16WE 1998091801125 19980918 01125 NM 1998 9 18 SWAA981767 1 19980815 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHTS INTERMITTENT FROM ROW 2 AND FWD. REMOVED AND REPLACED FWD LIGHT ASSY PER BOEING MM AND RECONNECTED LOOSE SOCKET AT ROW 2. 2 L 7 2 4F RT A16WE 1998091801126 19980918 01126 NM 1998 9 18 SWAA981768 1 19980815 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 294.5, STR 12L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801127 19980918 01127 NM 1998 9 18 SWAA981769 1 19980815 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386SW 26601 DURING SCHEDULED C1 CHECK, FOUND FWD ENTRY DOOR VERTICAL EMERGENCY EXIT SIGN MISSING TWO BULBS. INSTALLED TWO BULBS IN FWD ENTRY DOOR VERTICAL EMERGENCY EXIT SIGN PER BOEING MM, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1998091801128 19980918 01128 NM 1998 9 18 SWAA981770 1 19980816 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN. INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702SW 22054 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT ABOVE R1 DOOR WILL NOT ILLUMINATE. REMOVED AND REPLACED LIGH T ASSEMBLY PER BOEING MM. 2 L 7 2 4F A16WE 1998091801129 19980918 01129 NM 1998 9 18 SWAA981771 1 19980816 A 3350 SOCKET BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTS AT ROW 10, 17 HAVE SEVERAL LIGHTS INOP. REPLACED SOCKET ASSY A T ROW 10 AND 17 PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801130 19980918 01130 NM 1998 9 18 SWAA981772 1 19980817 A 3350 WIRE BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 511SW 24188 DURING WALKAROUND CHECK, FOUND TWO OVERWING RED STRIP LIGHTS AND TWO WHITE STRIP LIGHTS INOP. REPAIRED WIRE SPLICE 8ABC PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801131 19980918 01131 NM 1998 9 18 SWAA981773 1 19980817 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT R2 EXIT IDENTIFIER BULLNOSE AT 18L AND 20R FLOOR PROX AT 16-19. REPLACED BATTERY PACK AT DOOR R2 POSITION PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801132 19980918 01132 NM 1998 9 18 SWAA981774 1 19980817 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED C3 CHECK, FOUND FWD CARGO DOOR UPLATCH INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998091801133 19980918 01133 NM 1998 9 18 SWAA981775 1 19980817 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND EDDY CURRENT REVEALS CRACKED FWD SIDE OF BULKHEAD, LBL 5 WL 188.5. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998091801134 19980918 01134 NM 1998 9 18 SWAA981776 1 19980817 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND STABILIZER STRAP CRACKED AT BS 344, LBL 45.5 WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801135 19980918 01135 NM 1998 9 18 SWAA981777 1 19980817 A 5320 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 179 CRACKED AT 17 RT RBL 29. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801136 19980918 01136 NM 1998 9 18 SWAA981778 1 19980817 A 5320 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 179 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM AT BS 179 CRACKED AT 17 RT, RBL 29. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801137 19980918 01137 NM 1998 9 18 SWAA981779 1 19980817 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT BS 344, LBL 9. REPAIRED PER BOEING NR TIA53014. 2 L 7 2 4F RT A16WE 1998091801138 19980918 01138 NM 1998 9 18 SWAA981780 1 19980817 A 5320 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND AFT CARGO DOOR CUTOUT, AFT FRAME CLOSEOUT PANEL IS DAMAGED AT BS 847, RBL 25. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801139 19980918 01139 NM 1998 9 18 SWAA981781 1 19980817 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 780-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB TIE STRAP AT BS 780 TO 847, RBL 20, WL 160. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801140 19980918 01140 NM 1998 9 18 SWAA981787 1 19980817 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 787-800 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB LOWER TIE STRAP AT BS 787 TO 800, RBL 20, WL 157. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801141 19980918 01141 NM 1998 9 18 SWAA981782 1 19980817 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 842-852 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED SILL WEB LOWER TIE STRAP AT BS 842 TO 852, RBL 20, WL 162. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801142 19980918 01142 NM 1998 9 18 SWAA981783 1 19980817 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1104 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED SHEAR TIE AT BS 1104 BETWEEN STR 17R AND 18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801143 19980918 01143 NM 1998 9 18 SWAA981784 1 19980817 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM TIE STRAP AT BS 772, RBL 21 LBL 21 WL 162. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801144 19980918 01144 NM 1998 9 18 SWAA981785 1 19980817 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 291 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE STIFFENER AT BS 291, WL 248, RBL 60. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801145 19980918 01145 NM 1998 9 18 SWAA981788 1 19980818 A 2450 CIRCUIT BREAKERS BOEING 737 7372H4 138448C NM AC POWER TRIPPED A SWAA O OTHER H B ELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 105SW 23249 ON GROUND LOSS OF ALL AC POWER, SMELL OF SMOKE MULTIPLE CB'S TRIPPED. APU POWERING BUSSES AT TIME. REMOVED AND REPLACE D C803 BREAKER AND APU GCU. RAN APU ENGINES ALL CHECK NORMAL PER BOEING MM. 2 L 7 2 4F A16WE 1998091801146 19980918 01146 NM 1998 9 18 SWAA981789 1 19980818 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 327 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 23959 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SERVICE DOORWAY AFT LOWER SKIN CUTOUT AT BS 327, WL 210. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801147 19980918 01147 NM 1998 9 18 SWAA981790 1 19980818 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 23959 DURING SCHEDULED D-CHECK, FOUND WEB INTERCOSTAL CRACKED AT BS 294, WL 216, LBL 57. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801148 19980918 01148 NM 1998 9 18 SWAA981791 1 19980818 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 300.9 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 23959 DURING SCHEDULED D-CHECK, FOUND L-ANGLE CRACKED AT BS 300.9 WL 257 LBL 53. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801149 19980918 01149 NM 1998 9 18 SWAA981792 1 19980818 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 23959 DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER CLIP AT BS 380, STR 22L, WL 170. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801150 19980918 01150 NM 1998 9 18 SWAA981793 1 19980818 A 3350 SPLICE BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 511SW 24188 DURING WALKAROUND CHECK, FOUND TWO OVERWING RED STRIP LIGHTS AND TWO WHITE STRIP LIGHTS INOP. REPAIRED WIRE SPLICE AND 8ABC PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801151 19980918 01151 NM 1998 9 18 SWAA981794 1 19980818 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 621SW 28037 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHT (PORT SIDE) AFT OF OW EXIT HAS EXPOSED WIRE AND IS INOP. RECONNECT ED WIRES AND INSTALLED COVER PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801152 19980918 01152 NM 1998 9 18 SWAA981795 1 19980818 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 430 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TIE STRAP DENTED AT BS 430, RBL 10, WL 156. REMOVED AND REPLACED PER BOEING M M. 2 L 7 2 4F RT A16WE 1998091801153 19980918 01153 NM 1998 9 18 SWAA981796 1 19980819 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 19R, WL 192. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801154 19980918 01154 NM 1998 9 18 SWAA981798 1 19980819 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 568 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND RAM AIR INLET DUCT SKATE ANGLE CRACKED AT BS 568 WL 166, LBL 47. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091801155 19980918 01155 NM 1998 9 18 SWAA981797 1 19980819 A 5320 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED D-CHECK, FOUND FWD CARGO BAY DOOR FRAME COVER PLATE DENTED AT BS 492 TO 495, RBL 25 TO 30, WL 169. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998091801156 19980918 01156 NM 1998 9 18 SWAA981799 1 19980819 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986.5-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 986.5 TO 1006, LBL 12. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998091801157 19980918 01157 NM 1998 9 18 SWAA981800 1 19980819 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 967-986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 375SW 26583 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED INTERCOSTAL AT BS 967 TO 986.5, LBL 18. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998091801158 19980918 01158 NM 1998 9 18 SWAA981801 1 19980819 A 3260 SENSOR BOEING 737 7373A4 1384585 NM LT & RT MLG FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 673SW 23251 AIR TURNBACK DUE TO LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. UNSAFE LIGHT WENT OUT UPON GEAR EXTE NSION. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED L/R MLG SENSOR. GEAR SWING PER BOEING MM, OPS CK GOO D PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801159 19980918 01159 NM 1998 9 18 SWAA981803 1 19980819 A 5230 SKIN BOEING 737 737301 1384611 NM CARGO DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND AFT CARGO DOOR SKIN DENTED. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998091801160 19980918 01160 CE 1998 9 18 98ZZZM628 1 19980819 A 5210 12951407619 HANDLE BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR BROKEN A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 843CA UE43 DOOR HANDLE BROKEN. ALUMINUM HANDLE (TUBING) WORN, CRACKED, DRILLED. REPLACED DOOR HANDLE. 2 L 7 2 4T RT A24CE 1998091801161 19980918 01161 EU 1998 9 18 98ZZZM629 1 19980807 A 3241 95427322 VALVE AMD FALC20 FALCON 2720302 EU RT MLG WW INOPERATIVE A DKAA O OTHER O OTHER LD LANDING 1 GL 23 108R 108 NR 3 AND NR 4 TIRES BLOWN ON LANDING, ANTI-SKID SYSTEM DOES NOT APPEAR TO BE OPERATING CORRECTLY (DTW). REPLACED NR 3 A ND NR 4 MAIN WHEEL/TIRE ASSEMBLIES. REPLACED RIGHT ANTI-SKID SERVO VALVE IAW AMD MM 32-42. AIRCRAFT RETURNE TO SERVICE . (M) 2 L 7 2 4F A7EU 1998091801162 19980918 01162 WP 1998 9 18 ASAA9880153 1 19980817 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 PDX - RETURN TO GATE OF FLIGHT 516, CREW REPORTED THE EMERGENCY FLOOR TRACK RED LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. REPLACED WIRE SECTION IN FLOOR TRACK AT ROW 2 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801163 19980918 01163 WP 1998 9 18 ASAA9880152 1 19980816 A 3350 LIGHT DOUG DC9 DC983 3022083 WP FWD CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 1 TO 3 WERE FOUND INOPERATIVE. REPAIRED WIRI NG IN THE FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801164 19980918 01164 WP 1998 9 18 ASAA9880151 1 19980816 A 3350 60030451 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801165 19980918 01165 WP 1998 9 18 ASAA9880150 1 19980815 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 981AS 53472 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK RED LIGHTS FOR THE AFT OVERWING EMERGENCY EXIT WERE FOUND INOP ERATIVE. RESEATED CONNECTORS TO LIGHT ASSEMBLIES AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801166 19980918 01166 WP 1998 9 18 ASAA9880149 1 19980815 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 SEA - PRIOR TO DEPARTURE OF FLIGHT 305, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RESEATED CONNECTOR TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801167 19980918 01167 WP 1998 9 18 ASAA9880146 1 19980812 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. TIGHTENED LOOSE GRO UND IN OVERHEAD PANEL AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801168 19980918 01168 WP 1998 9 18 ASAA9880145 1 19980812 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 961AS 53075 SEA - DURING MAINTENANCE CHECK, THE FORWARD F/A PORTABLE EMERGENCY LIGHT WAS FOUND TO BE BROKEN. REPLACED LIGHT ASSEMBL Y AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801169 19980918 01169 WP 1998 9 18 ASAA9880144 1 19980808 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 LAX - PRIOR TO FLT 258 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FIRST CLASS CABIN WERE INOPERATIVE. REIN STALLED UNPLUGGED SECTION OF LIGHTS AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801170 19980918 01170 WP 1998 9 18 ASAA9880142 1 19980805 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - PRIOR TO DEPARTURE OF FLT 718, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RESEATED CONNECTOR TO LIGHT ASSY AT ROW 1 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801171 19980918 01171 WP 1998 9 18 ASAA9880140 1 19980729 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - PRIOR TO DEPARTURE OF FLIGHT 526, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. SECURED TRACK ASSEMBLY FROM ROW 2 FORWARD AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801172 19980918 01172 WP 1998 9 18 ASAA9880138 1 19980728 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 967AS 49103 OAK - DURING C-CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WERE FOUND DIM. REPLACED THE POWER SUPPLY AND O PERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998091801173 19980918 01173 WP 1998 9 18 ASAA9880136 1 19980725 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 948AS 53021 SEA - PRIOR TO DEPARTURE OF FLIGHT 507, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RESEATED CONNECTOR TO LIGHT ASSEMBLY AT ROW 1 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801174 19980918 01174 WP 1998 9 18 ASAA9880129 1 19980713 A 3350 6011777 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SFO - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY EVACUATION LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801175 19980918 01175 WP 1998 9 18 ASAA9880127 1 19980712 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801176 19980918 01176 WP 1998 9 18 ASAA9880126 1 19980712 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY AND GALLEY AREA WERE FOUND INOPERATIV E. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801177 19980918 01177 WP 1998 9 18 ASAA9880123 1 19980707 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM 13 TO 16 WERE FOUND INOPERATIVE. REPLACED THE BATTER IES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801178 19980918 01178 WP 1998 9 18 ASAA9880122 1 19980706 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - PRIOR TO DEPARTURE OF FLIGHT 137, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998091801179 19980918 01179 NM 1998 9 18 ASAA9840086 1 19980815 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 PDX - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT A SSEMBLY AND RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801180 19980918 01180 NM 1998 9 18 ASAA9840085 1 19980814 A 3350 8100022607 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - DURING MAINTENANCE CHECK, THE FORWARD TWO RED EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801181 19980918 01181 NM 1998 9 18 ASAA9840084 1 19980814 A 3350 20131A BATTERY BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT DOOR EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLA CED THE BATTERY AND BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801182 19980918 01182 NM 1998 9 18 98ZZZM630 1 19980814 A 3350 BPS73 CHARGER BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT DOOR EXIT IDENTIFIER WAS FOUND TO BE INOPERATIVE. REPLA CED THE BATTERY AND BATTERY CHARGER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801183 19980918 01183 NM 1998 9 18 ASAA9840083 1 19980813 A 3350 LIGHT BOEING 737 737490 1384715 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 767AS 27081 PDX - DURING MAINTENANCE CHECK, BOTH AFT RED EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRI NG/LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801184 19980918 01184 NM 1998 9 18 ASAA9840081 1 19980801 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 SEA - PRIOR TO FLT 138, ONE RED EMERGENCY EXIT FLOOR TRACK LIGHT ASSEMBLY WAS FOUND MISSING AT AFT EXIT AND WIRES WERE F OUND TO BE STICKING OUT OF TRACK. REPLACED AFT TWO LIGHT ASSEMBLIES AND SECURED. LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801185 19980918 01185 NM 1998 9 18 ASAA9840080 1 19980825 A 3350 SIGN BOEING 737 7374Q8 NM CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 771AS 25104 ANC - PRIOR TO FLIGHT 534, THE LEFT FLOOR 'EXIT' SIGN AT ROW 14 WAS FOUND TO BE MISSING. REPLACED 'EXIT' SIGN. (M) 2 L 7 2 4F RT A16WE 1998091801186 19980918 01186 NM 1998 9 18 ASAA9840078 1 19980714 A 3350 LIGHTS BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 764AS 25101 SEA - PRIOR TO FLT 330, SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE IN THE AFT CABIN AREA. R EPLACED WIRING HARNESS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801187 19980918 01187 NM 1998 9 18 ASAA9810087 1 19980814 A 3350 8731002142 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE RIGHT AFT EMERGENCY EXIT LIGHTS WAS FOUND TO BE INOPERATIVE. REPLACED LIGHT ASSEMBL Y AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801188 19980918 01188 NM 1998 9 18 ASAA9810086 1 19980808 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR LOWER EMERGENCY EXIT LIGHT WAS FOUND TO BE DIM. REPLACED BATTERY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801189 19980918 01189 NM 1998 9 18 ASAA9810085 1 19980808 A 3350 6104781 BATTERIES BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - PRIOR TO FLT 64, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 AND 14. REPLACED B ATTERIES AT ROWS 12 AND 14, AND REPLACED RECEIVER AT ROW 12. EMERGENCY EXIT FLOOR TRACK LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998091801190 19980918 01190 NM 1998 9 18 98ZZZM631 1 19980808 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - PRIOR TO FLT 64, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 12 AND 14. REPLACED B ATTERIES AT ROWS 12 AND 14, AND REPLACED RECEIVER AT ROW 12. EMERGENCY EXIT FLOOR TRACK LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998091801191 19980918 01191 NM 1998 9 18 ASAA9810084 1 19980806 A 3350 883200312 RECEIVER BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING RECON OF AIRCRAFT, FOUND TWO EMERGENCY EXIT LIGHT INOPERATIVE ON ONE PALLET AND ALL EMERGENCY EXIT LIGHTS I NOPERATIVE ON THE SECOND PALLET. REPLACED BATTERY PACK ON ONE PALLET AND REPLACED THE RECEIVER AND BATTERY PACK ON THE SECOND PALLET. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801192 19980918 01192 NM 1998 9 18 98ZZZM632 1 19980806 A 3350 8821004 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING RECON OF AIRCRAFT, FOUND TWO EMERGENCY EXIT LIGHT INOPERATIVE ON ONE PALLET AND ALL EMERGENCY EXIT LIGHTS I NOPERATIVE ON THE SECOND PALLET. REPLACED BATTERY PACK ON ONE PALLET AND REPLACED THE RECEIVER AND BATTERY PACK ON THE SECOND PALLET. ALL EMERGENCY EXIT LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801193 19980918 01193 NM 1998 9 18 ASAA9810052 1 19980720 A 3350 6005401 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EXIT IDENTIFIER WAS FOUND TO BE DIM, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE, AND THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RESPECTIVE BATTERIES AND ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801194 19980918 01194 NM 1998 9 18 98ZZZM633 1 19980720 A 3350 86210144 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EXIT IDENTIFIER WAS FOUND TO BE DIM, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE, AND THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RESPECTIVE BATTERIES AND ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801195 19980918 01195 NM 1998 9 18 98ZZZM634 1 19980720 A 3350 6013211 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR EXIT IDENTIFIER WAS FOUND TO BE DIM, THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE, AND THE LT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED RESPECTIVE BATTERIES AND ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801196 19980918 01196 NM 1998 9 18 ASAA9810083 1 19980805 A 3350 6104781 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - FLT 61 - DURING PREFLIGHT, THE CREW FOUND THE EMERGENCY EXIT LIGHTS AT ROW 10 INOPERATIVE. REPLACED BATTERY AND L IGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998091801197 19980918 01197 NM 1998 9 18 ASAA9810082 1 19980804 A 3350 6013211 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE DIM. REPLACED BATTERY PACK AN D LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998091801198 19980918 01198 NM 1998 9 18 ASAA9810079 1 19980728 A 3350 1060091102 LIGHT BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, FOUND THE EMERGENCY EXIT LIGHT ABOVE THE AFT AIRSTAIRS INOPERATIVE. REPLACED LIGHT ASSE MBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998091801199 19980918 01199 NM 1998 9 18 ASAA9810078 1 19980728 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998091801200 19980918 01200 CE 1998 9 18 98ZZZM635 1 19980521 A 3233 993880011 ACTUATOR BEECH 99 C99 1154006 CE MLG LEAKING A AJZA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 19 388AV U188 PILOT REPORTED LANDING GEAR CIRCUIT BREAKER POPPED AND GEAR WOULD NOT FULLY EXTEND. PILOT EXTENDED GEAR USING HAND PUMP , AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LEFT RETRACT ACTUATOR LEAKING. PART REMOVED. 1 L 7 2 3T A14CE 1998091801201 19980918 01201 NM 1998 9 18 ASAA9810081 1 19980731 A 5210 6516477 GATE BOEING 737 737298C 1384490 NM PAX DOOR MISDRILLED A ASAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE, THE L1 DOOR WAS FOUND TO BE HARD TO CLOSE. REMOVED DOOR. REPLACED UPPER DOOR GATE DUE TO INT ERFERENCE FIT WITH DOOR FRAME. INSTALLED AND RIGGED DOOR. (M) 2 L 7 2 4F RT A16WE 1998091801202 19980918 01202 NM 1998 9 18 ASAA9810076 1 19980725 A 3350 8821004 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT NR 2 SEAT PALLET. REPLA CED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998091801203 19980918 01203 WP 1998 9 18 USAAD98145 1 19980816 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 821US 49138 JAX - THE LOW LEVEL EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE LOW LEVEL LIGHTING BATTERIES. (M) 2 L 7 2 4F A6WE 1998091801204 19980918 01204 NM 1998 9 18 USAABB98090 1 19980718 A 3350 873100151REV9 LIGHT BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 LAX - FOUND THE EMERGENCY LOW LEVEL LIGHT AT ROW 4 INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998091801205 19980918 01205 NM 1998 9 18 USAA980349 1 19980731 A 5311 654587570 FRAME BOEING 737 7373B7 1384580 NM BS 295-336 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 533AU 30760 24515 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 41 INCH CORRODED AREA RIGHT CREASE BEAM INNER CHORD BS 295 A ND BS 336. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART. (M) 2 L 7 2 4F RT A16WE 1998091801206 19980918 01206 1998 9 18 USAAD98138 4 19980806 A 2211 25878263 COMPUTER DOUG DC9 DC931 3022065 WP E/E BAY MALFUNCTIONED A USAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 19 991VJ 47310 PIT - FLT 1254 - AFTER TAKEOFF THE RUDDER WAS 'KICKING' THE TAIL SECTION AROUND. THE FLIGHT CREW TURNED OFF THE YAW DAM PER BUT THERE WAS NO CHANGE. AFTER TURNING OFF THE AUTO PILOT RUDDER SERVO THE 'KICKING' STOPPED BUT THE AIRCRAFT STILL FELT UNSTABLE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A SATISFACTORY T EST OF THE YAW DAMPER AND STABILITY AUGMENT COMPUTER. THE COMPUTER WAS CHANGED AS A PRECAUTION AND THE AIRCRAFT FLOWN O N A SUCCESSFUL TEST HOP. (M) 2 L 7 2 4F A6WE 1998091801207 19980918 01207 WP 1998 9 18 USAAD98140 1 19980809 A 2420 976J2544 CONTROL DOUG DC9 DC931 3022065 WP E/E BAY FAILED A USAA O OTHER H ELECT. POWER LOSS-50 PC AP APPROACH 1 EA 19 974VJ 47130 PIT - FLT 400 - DESCENDING THROUGH 5000 FEET, THE LEFT GENERATOR DROPPED OFF LINE. WHEN THE CREW TRIED A RESET, THE GEN ERATOR AGAIN TRIPPED OFF LINE AND THE CROSS-TIE RELAY TRIPPED. THE CREW WAS WITHOUT AC POWER. THE APU WAS STARTED AND POWER RESTORED. MAINTENANCE REPLACED THE GENERATOR CONTROL PANEL. (M) 2 L 7 2 4F A6WE 1998091801208 19980918 01208 NM 1998 9 18 USAASB98208 1 19980813 A 2130 3964421 CONTROL VALVE BOEING 737 737301 1384611 NM LT PACK FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 563AU 23551 DEN - FLT 136 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT UPON CLIMB-OUT FROM DEN. FLIGHT RETURNED TO FIELD AT DEN AND LAN DED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK FLOW CONTROL V ALVE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998091801209 19980918 01209 NM 1998 9 18 USAABB98085 1 19980727 A 3350 86210066 BATTERIES BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 601AU 22193 SFO - FOUND EMERGENCY LIGHTS AT ROWS 4, 6, 9, 18 AND 29 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998091801210 19980918 01210 NM 1998 9 18 USAABB98087 1 19980806 A 3350 9221009 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 612AU 27124 LAX - FOUND THE L1 AND R1 DOOR EXIT IDENTIFIERS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998091801211 19980918 01211 WP 1998 9 18 USAAD98147 1 19980817 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 956VJ 47588 ROC - THE RIGHT NACELLE EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F A6WE 1998091801212 19980918 01212 WP 1998 9 18 USAAD98146 1 19980817 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 977VJ 48155 IND - THE PORTABLE EMERGENCY LIGHT NEAR THE MAIN ENTRANCE DOOR WAS DIM. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998091801213 19980918 01213 NM 1998 9 18 USAABB98088 1 19980805 A 3350 LIGHT BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 645US 23897 PIT - FOUND THE LOW LEVEL EMERGENCY LIGHTING INOPERATIVE FROM ROW 5R TO ROW 11R. MAINTENANCE FOUND THE WIRING DISCONNEC TED AT ROW 12 AND RECONNECTED IT. (M) 2 L 7 2 4F RT A1NM 1998091801214 19980918 01214 WP 1998 9 18 USAAD98143 1 19980814 A 3260 SENSOR DOUG DC9 DC981 3022081 WP MLG DIRTY A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 808US 48040 PHL - FLT 1622 - NOSE GEAR LIGHT WAS RED ON GEAR UP. CYCLED GEAR AND THE INDICATION WAS NORMAL. MAINTENANCE RESET PROX BOX AND PERFORMED BITE TEST, ALL NORMAL. CLEANED SENSORS A PRECAUTION. (M) 2 L 7 2 4F A6WE 1998091801215 19980918 01215 NM 1998 9 18 USAABB98089 1 19980808 A 3350 LIGHT BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PIT - FOUND LOW LEVEL EMERGENCY LIGHTS INOPERATIVE AT ROWS 8 THROUGH 10 LEFT AND 28 THROUGH 29 RIGHT. MAINTENANCE RESEA TED CONNECTORS AT THE LAMPHOLDERS. (M) 2 L 7 2 4F RT A1NM 1998091801216 19980918 01216 NM 1998 9 18 TAOA089806 1 19980814 A 3350 1102833 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 926TS 20774 FLT 6531 - LGA-DCA - FOUND ON L/S CHECK, AFT AIRSTAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT A SSEMBLY. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998091801217 19980918 01217 NM 1998 9 18 TAOA089805 1 19980814 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 926TS 3898 20774 FLT 6531 - LGA-DCA - FOUND ON L/S CHECK, RIGHT EXTERIOR FORWARD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK BASE AND BATTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998091801218 19980918 01218 NM 1998 9 18 TAOA089803 1 19980809 A 5240 12715029 BOLT BOEING 727 727225 1384077 NM SERVICE DOOR SHEARED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 919TS 20447 R-1 DOOR UPPER GUIDE ARM ATTACH BOLT SHEARED DURING PREFLIGHT WHEN DOOR WAS OPENED. REPLACED BOLT AND HARDWARE, SERVICE DOOR OPERATIONAL CHECKS NORMAL. (M) 2 L 7 3 4F A3WE 1998091801219 19980918 01219 NM 1998 9 18 TAOA089804 1 19980812 A 5220 LATCH BOEING 727 727225 1384077 NM EMERGENCY DOOR OUT OF ADJUST A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 923TS 20441 DURING TRAINING RIGHT FORWARD OVERWING EMERGENCY EXIT WOULD NOT OPEN. ADJUSTED FORWARD UPPER LATCH FITTING ON RIGHT FOR WARD EMERGENCY EXIT DOOR PER MM 52-21-0. CHECKED HATCH FOR FLUSHNESS AND OPENING AND CLOSING FORCE PER MM 52-21-0. OPE RATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998091801220 19980918 01220 NM 1998 9 18 P2EA98161 1 19980819 A 3260 SWITCH BOEING 737 737222 1384473 NM RT MLG WW OUT OF ADJUST A P2EA K NONE N FALSE WARNING AP APPROACH 1 CE 05 208AU 19547 FLT 588 - WITH FLAPS AT 5 DEGREES AND GEAR UP THE GEAR HORN CAME ON AS NORMAL, WAS SILENCED, AND CAME ON AGAIN. HORN CO NTINUED UNTIL GEAR WAS DOWN AND LOCKED. ADJUSTED FLAP LANDING WARNING SWITCH IN RIGHT WHEEL WELL IAW MM 31-26-12. HORN SOUNDS IN CORRECT POSITION AND IS SILENT IN CORRECT POSITIONS. OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1998091801221 19980918 01221 NE 1998 9 18 ORJA98192 2 19980811 A 7230 776623T1753 PRESSURE TUBE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A ORJA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 WP 11 871RA 18973 49788 725703 AT SJC, ON TAXI OUT, NR 1 ENGINE DECREASED FROM 10 QTS TO 3 QTS. REMOVED AND REPLACED NR 4.5 AND NR 6 BEARING INTERNAL PRESSURE TUBE. PERFORMED ENGINE RUN AND NO LEAKS NOTED. ENGINE MAINTAINED NORMAL OIL QTY. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1998091801222 19980918 01222 WP 1998 9 18 ORJA98193 1 19980813 A 2613 OVERHEAT LOOP DOUG DC9 DC982 3022082 WP TAIL COMPT MALFUNCTIONED A ORJA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 11 822RA 49932 FROM RENO, AIR TURNBACK TO RENO, TAIL COMPT TEMP HIGH LIGHT CAME ON AFTER TAKEOFF. STAYED ON FOR 3 MINUTES. WENT OUT O N FIRST POWER REDUCTION. RAN ENGINES NR 1 AND NR 2 AND APU AT TAKEOFF POWER 3 TIMES. COULD NOT DUPLICATE TAIL TEMP HIG H LIGHT AT THIS TIME. SYSTEM OPS CHECKS NORMAL, AND NO LEAKS NOTED. (M) 2 L 7 2 4F A6WE 1998091801223 19980918 01223 WP 1998 9 18 ORJA98189 1 19980806 A 3610 F17087 CLAMP DOUG DC9 DC983 3022083 WP TAIL COMP FAILED A ORJA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 11 876RA 53183 FROM LAS, AIR RETURN TO LAS, TAIL COMP TEMP HIGH LIGHT CAME ON IN FLIGHT. WENT OUT WHEN RIGHT THROTTLE REDUCED TO IDLE. FOUND CROSS FEED VALVE CLAMP TO BE INOPERATIVE. REMOVED AND REPLACED CLAMP. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998091801224 19980918 01224 WP 1998 9 18 ORJA98191 1 19980809 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 IN RENO, EMERGENCY AFT BATTERY CHARGER/EMERGENCY LIGHTING NEEDS REPLACED. REMOVED AND REPLACED BATTERY CHARGER AND EMER GENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998091801225 19980918 01225 WP 1998 9 18 98ZZZM636 1 19980809 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 IN RENO, EMERGENCY AFT BATTERY CHARGER/EMERGENCY LIGHTING NEEDS REPLACED. REMOVED AND REPLACED BATTERY CHARGER AND EMER GENCY LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998091801226 19980918 01226 WP 1998 9 18 ORJA98190 1 19980808 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 AT RENO, FLOOR EXIT LIGHTS, ROWS 9-12 INOPERATIVE. FOUND RIGHT FORWARD OVERWING EXIT BATTERY PACK DEFECTIVE. REMOVED A ND REPLACED WITH NEW PACK. OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1998091801227 19980918 01227 SW 1998 9 18 98ZZZM637 1 19980804 A 3233 2752010003 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW NLG INOPERATIVE A MEJA O OTHER J WARNING INDICATION CL CLIMB 1 SW 17 3114G AC583 AFTER TAKEOFF OUT OF MIQ, THE CREW HAD TO RECYCLE THE NOSE LANDING GEAR IN ORDER TO GET THE GEAR LIGHT TO EXTINGUISH. T HE RED INTRANSIT LIGHT WENT ON AND OFF 3 TIMES BEFORE EXTINGUISHING. THE AIRCRAFT LANDED AT SJU WITHOUT FURTHER INCIDEN T. MAINTENANCE REMOVED AND REPLACED BOTH THE LEFT AND RIGHT RETRACTION ACTUATORS WITH OVERHAULED UNITS. OPERATIONAL CH ECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998091801228 19980918 01228 WP 1998 9 18 ORJA98173 1 19980718 A 3350 EM1267 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 EMERGENCY EXIT LIGHT IN AFT GALLEY INOP. REPLACED CONTROLLER LIGHT ASSY AND BATTERIES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998091801229 19980918 01229 WP 1998 9 18 98ZZZM638 1 19980718 A 3350 208347 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 872RA 49793 EMERGENCY EXIT LIGHT IN AFT GALLEY INOP. REPLACED CONTROLLER LIGHT ASSY AND BATTERIES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998091801230 19980918 01230 WP 1998 9 18 ORJA98176 1 19980617 A 5320 WEB DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 881RA 49941 LEVEL 3 CORROSION, CUSP WEB CORRODED AND CRACKED BETWEEN STATION 1250 AND 1309 AT STRINGER 19, RIGHT SIDE AFT PIT AREA. REMOVED CORRODED AND CRACKED CUSP WEB BETWEEN STATION 1250 AND 1309 RIGHT. INSTALLED NEW CUSP WEB IAW DC9, SRM 51-30-2 . (M) 2 L 7 2 4F RT A6WE 1998091801231 19980918 01231 WP 1998 9 18 ORJA98175 1 19980621 A 5320 WEB DOUG DC9 DC983 3022083 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 881RA 49941 LEVEL 3 CORROSION ON RIGHT CUSP WEB, STATION 1098 TO 1174 IN CABIN. REMOVED CORRODED AND CRACKED CUSP WEB RIGHT, STATIO N 1098 TO 1179. FABRICATED NEW CUSP WEB AND INSTALLED IAW DC-9 SRM 51-30-2 AND ACTION NR 372194. FILE NR 98-06-19-022. (M) 2 L 7 2 4F RT A6WE 1998091801232 19980918 01232 WP 1998 9 18 ORJA98174 1 19980726 A 3230 SENSOR DOUG DC9 DC982 3022082 WP RT MLG MALFUNCTIONED A ORJA O OTHER N FALSE WARNING CL CLIMB 1 WP 11 823RA 49889 UPON GEAR RETRACTION RIGHT MAIN GEAR INDICATION REMAINED RED. GEAR DOOR OPEN LIGHT ON. RECYCLED GEAR WITH NO CHANGE. M ADE UPLOCK CHECK AND RIGHT GEAR EXTENDED. PUT GEAR HANDLE BACK UP AND ALL INDICATIONS NORMAL. RETURNED TO RENO PER MAI NTENANCE REQUEST. PERFORMED FUNCTIONAL TEST OF PROX BOX. ALL INDICATIONS NORMAL. JACKED AIRCRAFT. PERFORMED 5 RETRAC TIONS AND 6 EXTENSIONS. ALL INDICATIONS NORMAL. COULD NOT DUPLICATE AT THIS TIME. (M) 2 L 7 2 4F A6WE 1998091801233 19980918 01233 WP 1998 9 18 ORJA98169 1 19980716 A 2613 SENSOR DOUG DC9 DC983 3022083 WP TAIL COMP MALFUNCTIONED A ORJA O OTHER N FALSE WARNING CL CLIMB 1 WP 11 836RA 53046 TAIL COMPARTMENT TEMP HIGH, LIGHT ILLUMINATED AFTER TAKEOFF. QRH PROCEDURE ACCOMPLISHED. LIGHT EXTINGUISHED. MAINTENA NCE REMOVED SIDE PANELS. INSPECTED DUCTS WITH PACKS RUNNING. NO LEAKS NOTED. INSPECTED TEMP SENSOR AND AIR OUTLET. C OULD NOT DUPLICATE AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 1998091801234 19980918 01234 NE 1998 9 18 ORJA98158 2 19980712 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE NR 1 MALFUNCTIONED A ORJA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 WP 11 823RA 49889 ABORTED TAKEOFF DUE TO SPOOL UP (1.4 EPR) NR 1 ENGINE WOULD NOT ACCELERATE. AFTER 2-3 SECONDS, PUSHED BOTH THROTTLES UP (1.6 ON RT) AND STILL NO RESPONSE ON NR 1 ENGINE. PERFORMED HIGH POWER ASSURANCE CHECK AND ACCELERATION CHECK IAW MM 7 1-00-00 PAGE 557. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998091801235 19980918 01235 NM 1998 9 18 USAASB98188 1 19980719 A 5241 DOOR BOEING 737 7373B7 1384580 NM SERVICE DOOR OPEN A USAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 19 508AU 23383 CLT - FLT 1475 - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. NOISE WAS HEART FROM AFT SERVICE DOOR ALTHOUGH NO DOOR WA RNING INDICATIONS WERE PRESENT. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED . MAINTENANCE FOUND THE AFT GALLEY SERVICE DOOR NOT CLOSED PROPERLY. INSPECTED AND FUNCTINOALLY CHECKED DOOR. INSPECT ION AND FUNCTIONAL CHECK GOOD. PRESSURIZED AIRCRAFT ON GROUND. NO DISCREPANCIES NOTED. (M) 2 L 7 2 4F RT A16WE 1998091801236 19980918 01236 NM 1998 9 18 TSAA9833422 1 19980726 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE INDICATION. OPS CHECKED OK. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998091801237 19980918 01237 NM 1998 9 18 GAIA9865 1 19980623 A 5512 652298744 SKIN BOEING 727 727223 1384074 NM HORIZ STAB DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6810 19485 DURING ROUTINE C-CHECK, SEVERAL HOLES ALONG THE RIGHT STABILIZER LOWER TRAILING EDGE AT ELEVATOR STATION 99 TO 136, HOLD ING PLASTIC FAIRING WHERE FOUND ENLARGED. EXISTING HOLES WHERE PLUGGED PER SRM. NEW HOLES WHERE MADE 2D FROM PLUGGED H OLES. REINSTALLED PLASTIC FAIRING USING FASTENERS AS REMOVED. REPAIR COMPLIED WITH BY AAR OKLAHOMA, USING FLT VEHICLES , INC REPAIR DRAWING 55-98301-3 REV. NEW DATED 6/9/98. RESTORED AREA AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998091801238 19980918 01238 NE 1998 9 18 MASA98146 2 19980723 A 7321 324485310141516 FUEL CONTROL DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE NR 1 ENGINE FAILED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING R J Y PARTIAL RPM/PWR LOSS WARNING INDICATION ENGINE STOPPAGE TO TAKEOFF 1 SW 07 447YV 5343 447 TMAG0004 FLT 5225 - YUM-PHX - AFTER A NORMAL TAKEOFF RUN, AT ROTATION THE NR 1 ENGINE EXPERIENCED A POWER LOSS. THE NR 1 PROP WE NT INTO AUTOFEATHR, AT 1500 FT AGL THE APPROPRIATE PROCEDURES WERE CARRIED OUT. AN EMERGENCY WAS DECLARED, AND THE AIRC RAFT RETURNED TO THE FIELD WHERE IT LANDED WITHOUT INCIDENT. PASSENGERS WERE BUSSED TO THE TERMINAL. MAINTENANCE REMOV ED AND REPLACED THE HMU. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1998091801239 19980918 01239 NM 1998 9 18 AALA981379 1 19980710 A 5330 SKIN BOEING 727 727223 1384074 NM BS 198-208 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - A/C SUSTAINED DAMAGED TO RADOM AND WRINKLES TO LEFT FUSELAGE STATION 178 TO 208, STRINGER 17L TO 24L, SUSPECT AFT AIR STAIRS OUT OF RIG. REPLACED RADOME, FUSE DAMAGE REPAIRED PER SRM 53-30-3. RIGGED AND ADJUSTED STAIRS PER MM. ALL WORK ACCOMPLISHED ON TUL DROP IN BOW NR 320, DATED 7-1-98. (M) 2 L 7 3 4F A3WE 1998091801240 19980918 01240 EU 1998 9 18 VTZA98236 1 19980705 A 7710 AG44AF TACH GEN BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 479UE 893 FLT 6193 - IAD-JFK - DURING CLIMB, THE FLT CREW EXPERIENCED A FAILURE OF THE LEFT ENGINE RPM INDICATION. CREW NOTIFIED DISPATCH AND MAINTENANCE CONTROL AND RETURNED TO IAD. MAINTENANCE CONTROL NOTIFIED LINE MAINTENANCE OPERATIONS AND MECH ANICS WERE DISPATCHED TO THE AIRCRAFT. MAINTENANCE FOUND THAT THE LEFT ENGINE TACH GENERATOR HAD FAILED. MAINTENANCE R EMOVED AND REPLACED THE TACH GENERATOR, PERFORMED REQUIRED ENGINE RUN VERIFICATIONS AND RELEASED THE AIRCRAFT FOR SERVIC E. (M) 2 L 7 2 4T RT A56EU 1998091801241 19980918 01241 EU 1998 9 18 VTZA98234 1 19980703 A 5210 BOLTS BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 497UE 904 FLT 6247 - IAD-BGM - DURING TAKEOFF, THE FLT CREW EXPERIENCED A PAX DOOR LIGHT ILLUMINATION. CREW NOTIFIED DISPATCH AND MAINTENACNE CONTROL AND RETURNED TO IAD. MAINTENANCE CONTROL, NOTIFIED LINE MAINTENANCE OPERATIONS AND MECHANICS WERE DISPATCHED TO THE AIRCRAFT. MAINTENANCE FOUND THAT THE PAX DOOR SHOOT BOLTS NEEDED TO BE ADJUSTED. MAINTENANCE ADJUSTE D THE SHOOT BOLTS TO PROPER LIMITS, PERFORMED REQUIRED DOOR CLOSURE VERIFICATIONS AND RELEASED THE AIRCRAFT FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998091801242 19980918 01242 EA 1998 9 18 VTZA98233 1 19980630 A 5240 600330121 DOOR CNDAIR CL600 CL6002B19 EA OXYGEN SERV OPEN A VTZA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 27 624BR 7211 FLT 6771 - IAD-GSP - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOUD NOISE COMING FROM COCKPIT RIGHT SIDE . AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SECURED OXYGEN SERVICE DOOR. OPS CHEC K OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998091801243 19980918 01243 EU 1998 9 18 VTZA98239 1 19980710 A 3230 ATG135020 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 311UE 41029 FLT 6210 - BDL-IAD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WOULD NOT RETRACT AFTER TAKEOFF. AI RCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED AOG SWITCH ON LEFT MAI N LANDING GEAR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998091801244 19980918 01244 EU 1998 9 18 VTZA98238 1 19980708 A 7800 14178001409 JET PIPE JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE DAMAGED A VTZA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING M J Y OVER TEMP WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 27 318UE 41041 FLT 6524 - FLT ROC-JFK - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE FIRE WARNING LIGHT ILLUMI NATED AND CREW SHUTDOWN RT ENGINE AND BLEW BOTH FIRE BOTTLES. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROB LEMS. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF FIRE AFT OF ZONE 2, BUT DID FIND EXHAUST DUCT HEAT SHIELD DETERIOR ATED AND SEVERAL HARNESS HEAT SHRUNK DAMAGE. MAINTENANCE REMOVED AND REPLACED BOTH ENGINE FIRE BOTTLES AND RT JET PIPE AND HEAT SHRUNK, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998091801245 19980918 01245 1998 9 18 VTZA98245 4 19980714 A 3417 700007000966 ADC JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 314UE 41027 FLT 6612 - IAD-JFK - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 ADC FAILED. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 ADC. OPS CHECK OK. AIRCRAFT WAS REL EASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998091801246 19980918 01246 EU 1998 9 18 VTZA98244 1 19980719 A 7714 AG44AF TACH GEN BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 478UE 892 FLT 6294 - IAD-ROA - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO RIGHT RPM INDICATION FAILURE. AIRCRAFT LANDED WIT H NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TACH GENERATOR. OPS CHECK OK. AIRCRAFT WAS RELE ASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998091801247 19980918 01247 EU 1998 9 18 VTZA98243 1 19980718 A 3260 ATC135020 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 312UE 41025 FLT 6185 - IAD-RDU - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WOULD NOT RETRACT AFTER TAKEOFF. AI RCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT WOW SWITCH ON LEF T MAIN LANDING GEAR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998091801248 19980918 01248 EU 1998 9 18 VTZA98242 1 19980718 A 2422 PC125123B INVERTER JETAIR JETSTM JETSTM4101 1500501 EU AC SYSTEM FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 330UE 41098 FLT 6521 - IAD-BDL - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT STATIC INVERTER FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT STATIC INVERTER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998091801249 19980918 01249 1998 9 18 VTZA98240 4 19980716 A 3417 70000700966 ADC JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 324UE 41017 FLT 6621 - IAD-ILM - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 2 ADC FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 2 ADC, OPS CHECK OK. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998091801250 19980918 01250 NM 1998 9 18 USAASB98193 1 19980728 A 2781 189929 SENSOR BOEING 737 7374B7 1384702 NM RT WING FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 782AU 25021 LGA - FLT 565 - FLT HAD JUST TAKEN OFF WHEN THE CREW NOTICED THAT THE NR 4 LEADING EDGE INTRANSIT LIGHT WAS ILLUMINATED. CREW WENT THROUGH PROCEDURES TO RECEIVE THE CORRECT INDICATION WITH NO HELP. FLIGHT RETURNED TO FIELD AT LGA AND LAND ED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 4 LEADING EDGE FLAP EXTEND PRO X SENSOR PER MM 27-88-11. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998091801251 19980918 01251 NM 1998 9 18 USAABB98079 1 19980729 A 3350 20121 BATTERY SUPPLY BOEING 767 767201 1385125 NM LT WING DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 646US 23898 CDG - LEFT WING SQUIB TEST FAILED. MAINTENANCE FOUND THE POWER SUPPLY MODULE M962 TO BE AT FAULT AND SWAPPED IT WITH MO DULE M736. M736 WILL BE REPLACED. (M) 2 L 7 2 4F RT A1NM 1998091801254 19980918 01254 EU 1998 9 18 RAIA980610 1 19980622 A 2612 51228801 LOOP JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 551HK 8938 41040 FLT 7516 - STL - RIGHT OVERHEAT LOOP CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND REPLACED RIGHT OVER HEAT LOOP. (M) 2 L 7 2 4T RT A41NM 1998091801255 19980918 01255 EU 1998 9 18 RAIA980609 1 19980623 A 7931 41SG107150G14 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 429AM 14579 879 FLT 7050 - STL - RIGHT ENGINE OIL PRESSURE READS HIGH, 140 PSI. MAINTENANCE INSPECTED AND REPLACED RIGHT ENGINE OIL PRE SSURE TRANSDUCER. (M) 2 L 7 2 4T RT A56EU 1998091801256 19980918 01256 EU 1998 9 18 RAIA980517 1 19980530 A 5270 SP4594 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU AFT CARGO POSITION A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 551HK 41040 FLT 7107 - STL - MAIN BAGGAGE DOOR CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE CYCLED DOOR HANDLE FULLY CLOSED, DO OR CAPTION EXTINGUISHED NORMALLY. (M) 2 L 7 2 4T RT A41NM 1998091801257 19980918 01257 EU 1998 9 18 RAIA980607 1 19980616 A 7933 CA3108R12S3SF80 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 435AM 14393 889 STL - FLT 7096 - RIGHT OIL TEMPERATURE GAUGE READING HIGH. MAINTENANCE INSPECTED AND REPLACED RIGHT OIL TEMPERATURE BUL B CONNECTOR. (M) 2 L 7 2 4T RT A56EU 1998091801258 19980918 01258 EU 1998 9 18 RAIA980527 1 19980518 A 5347 S536780001000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 422TE 106 STL - DURING MAINTENANCE, FOUND RIGHT INBOARD SEAT TRACK CORRODED. MAINTENANCE PERFORMED SPLICE REPAIR IAW ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 1998091801259 19980918 01259 EU 1998 9 18 RAIA980526 1 19980518 A 5320 S2541004120200 THRESHOLD AEROSP ATR42 ATR42300 8680920 EU LAVATORY CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 422TE 106 STL - DURING MAINTENANCE, FOUND LAVATORY THRESHOLD CORRODED AND EXFOLIATED. MAINTENANCE REPLACED LAVATORY THRESHOLD IAW WITH ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 1998091801260 19980918 01260 EU 1998 9 18 RAIA980525 1 19980518 A 5347 S536780001000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 422TE 22361 106 STL - DURING MAINTENANCE, FOUND CORROSION AT LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. MAINTENANCE PERFORMED SPLICE REPAIR AT LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS IAW ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 1998091801261 19980918 01261 EU 1998 9 18 RAIA980524 1 19980518 A 5240 S536720206200 SKIN AEROSP ATR42 ATR42300 8680920 EU SERVICE DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 422TE 22361 106 STL - DURING MAINTENANCE, FOUND CORROSION AT SERVICE DOOR TORQUE BOX. MAINTENANCE REPLACED TORQUE BOX SKIN AT SERVICE D OOR IAW ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 1998091801262 19980918 01262 EU 1998 9 18 RAIA980523 1 19980518 A 5311 S53372413227 FRAME AEROSP ATR42 ATR42300 8680920 EU BS 17 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 422TE 22361 106 STL - DURING MAINTENANCE INSPECTION, FOUND CORROSION AT FRAME 17 CARGO DOOR FLOOR LEVEL. MAINTENANCE PERFORMED SPLICE R EPAIR AT FRAME 17 IAW ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 1998091801263 19980918 01263 EU 1998 9 18 RAIA980611 1 19980625 A 2910 HYD PRESSURE BAG JETSTM JETSTM3201 1500217 EU MLG FAILED A RAIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 03 343TE 955 FLT 7424 - STL - HYDRAULIC PRESSURE WENT TO ZERO, CREW PERFORMED EMERGENCY GEAR EXTENSION, IN WORK 6/25/98. (M) 2 L 7 2 4T RT A56EU 1998091801264 19980918 01264 EU 1998 9 18 RAIA980703 1 19980703 A 7931 8582 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NR 2 ENGINE FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 560HK 5614 41076 JFK - FLT 7698 - NR 2 ENGINE OIL PRESSURE INDICATION DROPPED BELOW RED LINE WITH NO CAP WARNING LIGHT. REMOVED AND REPL ACED OIL PRESSURE TRANSDUCER. (M) 2 L 7 2 4T RT A41NM 1998091801265 19980918 01265 EU 1998 9 18 RAIA980704 1 19980705 A 3230 NAS620121 BOLT BAG JETSTM JETSTM3201 1500217 EU RT MLG BROKEN A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 423AM 15179 858 ALO - FLT 7469 - RIGHT GEAR WOULD NOT RETRACT TO UP AND LOCKED POSITION. REPLACED RT MAIN UPLOCK SWITCH MOUNT BOLT. (M ) 2 L 7 2 4T RT A56EU 1998091801266 19980918 01266 1998 9 18 RAIA980701 3 19980701 A 6140 31056294 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 558HK 1456 41071 FLT 7174 - STL - LEFT AND RIGHT BETA CAPTIONS ILLUMINATED ON TAKEOFF. MAINTENANCE CLEANED RIGHT BETA SWITCH CONNECTOR A ND REPLACED LEFT BETA SWITCH. (M) 2 L 7 2 4T RT A41NM 1998091801267 19980918 01267 NM 1998 9 18 TAOA079808 1 19980713 A 2750 DAS832A4 BEARING BOEING 727 727227 1384078 NM RT JACKSCREW MISSING A TAOA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 15 927TS 20837 FLT 6480 DCA-LGA - INBOARD FLAPS WOULD NOT RETRACT AFTER TAKEOFF FROM DCA, DIVERTED TO BALTIMORE WASHINGTON INTERNATIONA L AIRPORT. REPLACED RIGHT INBOARD FLAP JACKSCREW CARRIAGE BEARING FOR ELEPHANT EAR, REPLACED INBOARD JACKSCREW END CAP, OPERATIONAL CHECK NORMAL PER MM 27-51-27. (M) 2 L 7 3 4F A3WE 1998091801268 19980918 01268 EU 1998 9 18 USAAF98056 2 19980718 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 FAILED A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 EA 19 869US 11314 17368 PIT - FLT 8079 - EN ROUTE TO PHL AT FL33 AND ON DESCENT TO FL29, AS N1 CAME BACK THROUGH 50 PERCENT, NR 1 ENGINE VIBRATI ON INDICATION WENT TO TOP OF ORANGE BAND. THE VIBRATION WAS FELT IN THE COCKPIT FLOOR AND THROTTLE QUADRANT. ALSO, AN AUDIBLE RUMBLE WAS HEARD. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 EN GINE ASSY. (M) 2 L 7 2 4F 4 F RT 1998091801269 19980918 01269 1998 9 18 EIAA980231 4 19980720 A 3418 SENSOR BOEING 747 747212B 1384886 NM E/E BAY MALFUNCTIONED A A EIAA A UNSCHED LANDING J E F WARNING INDICATION VIBRATION/BUFFET FLT CONT AFFECTED NR NOT REPORTED 1 NM 09 482EV 20713 AMS - WHEN FLAPS WERE RETRACTED TO 1 DEGREE DURING ASSENT, STICK SHAKER ACTIVATED, NOSE OSCILLATED UP AND DOWN. SPEED I NCREASED TO 300 KTS PITCH OSCILLATION CONTINUED, FLAPS EXTENDED TO 5 DEGREES, OSCILLATION STOPPED. DECLARED EMERGENCY A ND PREPARED A/C FOR OVERWEIGHT LANDING. (M) 2 L 7 4 4F A20WE 1998091801270 19980918 01270 WP 1998 9 18 98ZZZM639 1 19980717 A 6121 ACTUATOR CVAC 440 440 2422902 WP RT ENGINE FAILED A A ERAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 566EA 381 PROPELLERS WILL NOT SYNC IN K1 POSITION. RIGHT 13500 RPM, LT 14,000 RPM AND RISING. PITCH LOCKED PROPELLER, RPM STILL UNSTABLE. E-HANDLED LT ENGINE AND MADE UNEVENTFUL LANDING AT ANC. REPLACED LT ROTARY ACTUATOR AND REPAIRED BROKEN WIRE TO RT PROP ALTERNATOR. GROUND OPS CHECK GOOD. (M) 2 L 7 2 4R 6A6 1998091801271 19980918 01271 1998 9 18 98ZZZM640 4 19980720 A 6122 8210393 GOVERNOR BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 840CA UE38 LEFT PROP RPM LOW. PROP GOVERNOR FAILURE. REPLACED PROP GOVERNOR IAW CHAP 61, OPS CHECK OK. (M) 2 L 7 2 4T RT A24CE 1998091801272 19980918 01272 1998 9 18 98ZZZM641 4 19980715 A 6122 8210393 GOVERNOR WOODWARD BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 844CA 8474 UE45 A/C YAWS RIGHT ON LANDING. RIGHT PROPELLER GOVERNOR FAILURE. REPLACED RIGHT PROPELLER GOVERNOR. (M) 2 L 7 2 4T RT A24CE 1998091801273 19980918 01273 NM 1998 9 18 USAABB98075 1 19980716 A 3150 EICAS BOEING 767 767201 1385125 NM E/E BAY MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 645US 23897 PHL - FLT 12 - AFTER TAKEOFF FROM PHL, CREW RECEIVED THE EICAS MESSAGE 'FLAP/SLAT ELEC'. CREW CONTACTED MAINTENANCE ON GROUND AND DECIDED TO RETURN TO PHL RATHER THAN FACE MAINTENANCE PROBLEMS IN MAD. FLIGHT LANDED WITH NO FURTHER INCIDEN T. MAINTENANCE PERFORMED A BITE CHECK OF THE SYSTEM AND CYCLED THE FLAPS. NO PROBLEMS WERE FOUND. (M) 2 L 7 2 4F RT A1NM 1998091801274 19980918 01274 WP 1998 9 18 TWAA9810710 1 19980629 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 510 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 998R 47030 MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ROUND INTERIM REPAIR AT THE RADIO ALT ANTENNA AT FS 510, L30. REM OVED PREVIOUS REPAIR. INSTALLED REPAIR DOUBLER AND FINGER DOUBLER PER DWG SRO 9530107 AND SRM 53-04, FIG 44. (M) 2 L 7 2 4F A6WE 1998091801275 19980918 01275 NM 1998 9 18 TSAA9833421 1 19980726 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED THE NR 1 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998091801276 19980918 01276 NM 1998 9 18 TSAA9833420 1 19980726 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 POSITION EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998091801277 19980918 01277 NM 1998 9 18 TSAA9833419 1 19980724 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 2 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BATTERY LAMPS NOT ILLUMINATING. OPS CHECKED OK. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998091801278 19980918 01278 EU 1998 9 18 AALA981377 1 19980713 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1817-1870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70074 517 TUL - DURING C-CHECK, FOUND CORROSION ON NR 10 SEAT TRACK AT FRAME 27 AND 28 IN FORWARD CABIN. REMOVED AND REPLACED COR RODED SECTION OF SEAT TRACK FROM FRAME 25 TO 29, PER SRM 57-72-10-2. (M) 2 L 7 2 4F RT A35EU 1998091801279 19980918 01279 EU 1998 9 18 AALA981363 1 19980709 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 30 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70074 517 TUL - FLOOR SUPPORT BETWEEN SEAT TRACKS 8 AND 9 HAS SOME PITTING. REPLACED BEAM 8A, FLOOR SUPPORT BETWEEN SEAT TRACKS 8 AND 9 PER SRM 51-72-10-0. ALODINED, PRIMED, PAINTED BEAM PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998091801280 19980918 01280 EU 1998 9 18 AALA981364 1 19980709 A 5320 MOUNT AIRBUS 300 A300B4605R 3930308 EU FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70074 517 TUL - LAV MOUNT IN BETWEEN SEAT TRACK 8 AND FLOOR SUPPORT IS CORRODED. REPLACED LAV MOUNT IN BETWEEN SEAT TRACK 8 AND F LOOR SUPPORT PER SRM 51-72-10-0, ALODINED, PRIMED, PAINTED PER SRM 51-21-00-0. (M) 2 L 7 2 4F RT A35EU 1998091801281 19980918 01281 EU 1998 9 18 AALA981386 1 19980714 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 2188-2241 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70074 517 TUL - DURING C-CHECK, FOUND CORROSION ON NR 8 SEAT TRACK BETWEEN FRAME 34 AND 35 IN MID CABIN. REMOVED AND REPLACED SEA T TRACK SECTION BETWEEN FRAME 34 AND 36 PER SRM 53-10-16-2. (M) 2 L 7 2 4F RT A35EU 1998091801282 19980918 01282 EU 1998 9 18 AALA981385 1 19980714 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 1764-1976 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70074 517 TUL - DURING C-CHECK, FOUND CORROSION IN SEVERAL PLACES ON NR 9 SEAT TRACK BETWEEN FRAME 26 AND 30 IN MID CABIN. REMOVE D AND REPLACED CORRODED SEAT TRACK SECTION BETWEEN FRAME 26 TO 30 PER SRM 51-72-10. (M) 2 L 7 2 4F RT A35EU 1998091801283 19980918 01283 WP 1998 9 18 AALA981482 1 19980806 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 710-735 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - REF AC DAMAGE LOG ITEM NR 022 DAMAGE IS OUT OF LIMITS PER SRM 53-20-00 PAGE 116 VOL I. INSTALLED CLASS I REPAIR D OUBLER PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998091801284 19980918 01284 WP 1998 9 18 AALA981493 1 19980805 A 5312 BULKHEAD WEB DOUG DC10 DC1010 3022110 WP BS 2007 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - DURING C-CHECK, FOUND SMALL DENT IN FORWARD FACE OF STATION 2007 BULKHEAD WEB IN CTR OF BULKHEAD 20 INCHES ABOVE L ONGERON NR 52 IN AFT CARGO COMPT. CUT OUT DENT DAMAGE AND INSTALLED DOUBLER REPAIR PER SRM 53-40-00, FIG 9A, VOL I. (M ) 2 L 7 3 4F A22WE 1998091801285 19980918 01285 WP 1998 9 18 AALA981489 1 19980805 A 5753 CASTING DOUG DC10 DC1010 3022110 WP TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION IN BOLT HOLES WHERE TRACK ATTACHES TO FLAP. HOLES BORED OUT TO REMOVE CORROSION AND BUSHINGS INST ALLED (HOLES REAMED TO .4485). (M) 2 L 7 3 4F A22WE 1998091801286 19980918 01286 WP 1998 9 18 AALA981488 1 19980805 A 5753 CASTING DOUG DC10 DC1010 3022110 WP TE FLAP CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION IN BOLT HOLES WHERE TRACK ATTACHES TO FLAP. HOLES BORED OUT TO REMOVED CORROSION AND BUSHINGS INS TALLED (HOLES REAMED TO .4485). (M) 2 L 7 3 4F A22WE 1998091801287 19980918 01287 WP 1998 9 18 AALA981487 1 19980805 A 5753 TRACK DOUG DC10 DC1010 3022110 WP TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION IN BOLT HOLES WHERE TRACK ATTACHES TO FLAP. HOLES BORED OUT TO REMOVE CORROSION AND BUSHINGS INST ALLED (HOLES REAMED TO .4485). (M) 2 L 7 3 4F A22WE 1998091801288 19980918 01288 WP 1998 9 18 AALA981486 1 19980805 A 5753 TRACK DOUG DC10 DC1010 3022110 WP TE FLAPS CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION IN BOLT HOLES WHERE TRACK ATTACHES TO FLAP. HOLES BORED OUT TO REMOVE CORROSION AND BUSHINGS INST ALLED (HOLES REAMED TO .4485). (M) 2 L 7 3 4F A22WE 1998091801289 19980918 01289 WP 1998 9 18 AALA981485 1 19980805 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 840 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION ON HAT SECTION FLOOR SUPPORT BETWEEN TRACK NR 6 OUTBOARD TO FLOOR SUPPORT. FABRICATED NEW HAT TRA CK FROM T-6 EXTRUSION PER SRM 53-60-01, TREATED PER SRM 51-21-01 VOL 2. INSTALLED PER SRM 53-60-01. (M) 2 L 7 3 4F A22WE 1998091801290 19980918 01290 WP 1998 9 18 AALA981484 1 19980808 A 5713 STRINGER DOUG DC10 DC1010 3022110 WP LT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND COMPENSATOR FLANGE HAS CORROSION ON PANEL LANDING. REMOVED AND REPLACED STRINGER 8 PER ESO 7349, DATED 4-23 -98. (M) 2 L 7 3 4F A22WE 1998091801291 19980918 01291 WP 1998 9 18 AALA981483 1 19980808 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1887 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - TEMP DOUBLER REPAIR LOWER FUSELAGE. REMOVED TEMP DOUBLER AND INSTALLED NEW DOUBLER PER SRM VOL 1 53-20-00. (M) 2 L 7 3 4F A22WE 1998091801292 19980918 01292 WP 1998 9 18 AALA981521 1 19980811 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 839 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION BETWEEN SKIN AND STRINGER AT STATION 839 AND STRINGER 461. INSTALLED DOUBLER REPAIR PER SRM 53-20 -00 FIG 6. (M) 2 L 7 3 4F A22WE 1998091801293 19980918 01293 WP 1998 9 18 AALA981524 1 19980812 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 715 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - UPPER FLOOR SUPPORT FRAME 715 BETWEEN ROLLER TRAYS 1 AND 2 IS CORRODED. INSTALLED NEW SUPPORT PER SRM 53-70-00 AN D 51-21-01 VOL II. (M) 2 L 7 3 4F A22WE 1998091801294 19980918 01294 WP 1998 9 18 AALA981523 1 19980813 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1850-1853 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - DURING C-CHECK, FOUND CORROSION ON LOWER FUSELAGE SKIN RUNNING UNDER TEAR STRAP AT STATION 1850-1853 BETWEEN LONGE RONS 46L AND 47L IN AFT CARGO COMPT. CUTOUT CORRODED SKIN AND INSTALLED CLASS I DOUBLER PER SRM 53-20-00, VOL I, FIG 6, SHEET 5 AND SRM 51-21-01, VOL II.(M) 2 L 7 3 4F A22WE 1998091801295 19980918 01295 WP 1998 9 18 AALA981530 1 19980813 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1501 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND STATION 1501 BELLY SKIN CORRODED AROUND 6 DRAINS LONGERON 49L TO 49R. INSTALLED DOUBLER OVER CORRODED AREA STATION 1501 PER SRM 53-40-00. (M) 2 L 7 3 4F A22WE 1998091801296 19980918 01296 EU 1998 9 18 AALA981492 1 19980810 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 13 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 8067A 510 TUL - FOUND CORROSION SHORT FLOOR SUPPORT INBOARD OF TRACK NR 4. REMOVED AND REPLACED FLOOR SUPPORT INBOARD OF TRACK 4 PER SRM 51-72-10-00 AND 51-21-00. (M) 2 L 7 2 4F RT A35EU 1998091801297 19980918 01297 EU 1998 9 18 AALA981491 1 19980805 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU BS 13-14 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 8067A 510 TUL - FOUND CORROSION ON SHORT FLOOR SUPPORT INBOARD OF SEAT TRACK NR 4, FRAME 13-14. REMOVED AND REPLACED FLOOR SUPPOR T INBOARD OF TRACK NR 4 PER SRM 51-72-10-00. (M) 2 L 7 2 4F RT A35EU 1998091801298 19980918 01298 EU 1998 9 18 AALA981490 1 19980807 A 5347 SEAT TRACK AIRBUS 300 A300B4605R 3930308 EU BS 14 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 8067A 510 TUL - FOUND SEAT TRACK HAS CORROSION AT FRAME 14. REMOVED AND REPLACED SEAT TRACK NR 7 FROM FRAME 11-15 PER SRM 51-72-1 0 AND SRM 51-21-00. (M) 2 L 7 2 4F RT A35EU 1998091801299 19980918 01299 EU 1998 9 18 AALA981473 1 19980720 A 5400 ANGLE AIRBUS 300 A300B4605R 3930308 EU NR 1 PYLON CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 40064 507 TUL - FOUND CORROSION ON LOWER FLANGE OF RIB 14A UPPER PYLON TO WING PANEL SUPPORT. INSTALLED NEW FLANGE PER SRM 51-72- 10-0. (M) 2 L 7 2 4F RT A35EU 1998091801300 19980918 01300 NM 1998 9 18 AALA981452 1 19980729 A 5320 WEB BOEING 727 727227 1384078 NM BS 830 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 725AA 20732 TUL - FOUND CRACK IN WEB OF CENTER WING TANK RIGHT WALL STATION 830 APPROX RBL, ABOUT 16 INCHES ABOVE FLOOR, INSIDE 3RD COMPT OF TANK. INSTALLED DOUBLER REPAIR PER ESO 11697, DATED 7/19/98. (M) 2 L 7 3 4F A3WE 1998091801301 19980918 01301 NM 1998 9 18 AALA981520 1 19980812 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 360 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND FLOORBEAM UPPER CAP STATION 360 RBL 10 TO RBL 14. REPAIRED PER AARD 53-10-07-07 FIG 2. (M) 2 L 7 3 4F A3WE 1998091801302 19980918 01302 NM 1998 9 18 AALA981519 1 19980811 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND FLOORBEAM UPPER CAP CORRODED AND CRACKED, STATION 344 RBL 10 TO RBL 22. REMOVED CORRODED SECTION OF FLOORBE AM UPPER CAP STATION 344 RBL 10 TO RBL 58. INSTALLED REPAIR PART PER 53-10-8. (M) 2 L 7 3 4F A3WE 1998091801303 19980918 01303 NM 1998 9 18 AALA984177 1 19980810 A 5320 STRAP BOEING 767 767223 1385123 NM DOOR FRAME CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 305AA 22311 AFW - AFT CARGO DOOR FRAME FAIL/SAFE STRAP HAD CORROSION BLEND ON TOP SURFACE. BLEND ALL CORROSION, ROTO PEEN AREA AND REFINISH IAW TO SRM REQUIREMENTS. (M) 2 L 7 2 4F RT A1NM 1998091801304 19980918 01304 NM 1998 9 18 AALA984176 1 19980807 A 5313 STRINGER BOEING 767 767223 1385123 NM BS 434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 305AA 22311 AFW - AFT END OF 38L AT STATION 434 WAS BADLY CORRODED. REMOVED CORRODED PIECE OF STRINGER. REPLACED WITH SIMILAR LONG ER SPLICE WITHOUT A JOGGLE. (M) 2 L 7 2 4F RT A1NM 1998091801305 19980918 01305 NM 1998 9 18 AALA984175 1 19980807 A 5320 SPLICE BOEING 767 767223 1385123 NM BS 434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 305AA 22311 AFW - STRINGER 33R WAS BADLY CORRODED, AFT OF STATION 434. REMOVE CORRODED PIECE OF STRINGER. REPLACE WITH SIMILAR LON GER SPLICE WITHOUT A JOGGLE. (M) 2 L 7 2 4F RT A1NM 1998091801306 19980918 01306 NM 1998 9 18 AALA984172 1 19980803 A 3221 BEAM BOEING 767 767223 1385123 NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 312AA 22315 AFW - FOUND CORROSION IN THE BORE FOR THE AFT MLG TRUNNION BUSHING. THE BORE WAS HONED OUT TO A DIA OF 8.272 INCH, AFTE R HONING SOME LOCAL PITTING REMAINED WHICH WAS BLENDED AND THE PITTING WAS IN THE 1R O'CLOCK AREA. (M) 2 L 7 2 4F RT A1NM 1998091801307 19980918 01307 NM 1998 9 18 AALA981527 1 19980813 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 384AA 26996 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT PAX SEAT 23H INOPERATIVE. RESEATED LOOSE EMERGENCY EXIT LIG HT CONNECTOR AT PAX SEAT 23H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998091801308 19980918 01308 NM 1998 9 18 AALA981526 1 19980813 A 3350 1265 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312AA 22315 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING LIGHT AT SEAT ROW 7 RIGHT SIDE WOULD NOT ILLUMINATE. REPLACED EME RGENCY CEILING LIGHT ASSEMBLY AT SEAT ROW 7 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998091801309 19980918 01309 NM 1998 9 18 AALA981522 1 19980812 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 363AA 24044 MIA - DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED WIRE IN EMERGENCY EXIT LIGHTS. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998091801310 19980918 01310 NM 1998 9 18 AALA981477 1 19980805 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 632AA 24590 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT COFFEE BAR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT COFFEE BAR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998091801311 19980918 01311 NM 1998 9 18 AALA981528 1 19980813 A 3350 0201922001 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 301AA 22307 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHT AT SEAT ROW 27H WOULD NOT ILLUMINATED. REPLACED EMERGENCY ES CAPE LIGHT ASSEMBLY AT SEAT ROW 27H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998091801312 19980918 01312 WP 1998 9 18 AALA981533 1 19980814 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 560AA 53090 DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED FIRST CLASS EME RGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998091801313 19980918 01313 EU 1998 9 18 AALA981518 1 19980811 A 2913 PV32402F PUMP AIRBUS 300 A300B4605R 3930308 EU ENGINE FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 70079 619 MIA - FLT 915 - DURING CLIMB, YELLOW SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. FLIGHT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE UPPER ENGINE DRIVEN HYDRAULIC PUMP SHAFT SHEARED. REPLACED ENGINE DRIVEN HYDR AULIC PUMP AND MOTORIZED ENGINE WITH NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801314 19980918 01314 EU 1998 9 18 AALA981347 1 19980708 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7076A 610 JFK - DURING OVERNIGHT MAINTENANCE, EMEREGNCY EXIT FLOOR PATH ESCAPE LIGHTING BETWEEN SEAT ROWS 21AB THROUGH 23AB FOUND INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH ESCAPE LIGHT STRIP AT SEAT ROWS 21AB THROUGH 23AB. SYSTEM GROUND CHECK ED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801315 19980918 01315 EU 1998 9 18 AALA981349 1 19980708 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7076A 610 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACT LIGHTING AT L-4 DOOR INOPERATIVE. REPLACED EMERGENCY EXI T LIGHT STRIP AT L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801316 19980918 01316 EU 1998 9 18 AALA981365 1 19980711 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 MIA - DURING OVERNIGHT MAINTENANCE, FOUR FOOT OF EMERGENCY EXIT FLOOR LIGHTING AT ROWS 24B-25B INOPERATIVE. REPLACED EM ERGENCY EXIT FLOOR LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801317 19980918 01317 EU 1998 9 18 AALA981263 1 19980624 A 2840 SIC50773 COMPUTER AIRBUS 300 A300B4605R 3930308 EU BAY FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 7082A 643 MIA - FLT 1153 - EN ROUTE MIA-SJU - PRIOR TO LEVEL OFF BOTH CGCC AND FUEL TO TOTALIZER FAILED. ON LEVEL OFF FUEL TOTAL ON OUTER AND INNER TANKS WAS 10,000 LBS LESS THAN PLANNED. RETURN AND LANDED MIA WITHOUT INCIDENT. ACCOMPLISHED BITE C HECK ON FUEL QUANTITY COMPUTER AND FOUND FAULT ON IT. REPLACED COMPUTER AND RESET FUEL QUALITY CONTROL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801318 19980918 01318 NM 1998 9 18 AALA981387 1 19980714 A 3350 LIGHT DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1756 48491 MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 2G INOPERATIVE. REPAIRED WIRING FOR EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 2G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998091801319 19980918 01319 WP 1998 9 18 AALA981532 1 19980813 A 3350 P2070003001 FLASHLIGHT DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 143AA 46555 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLIGHT ATTENDANT FLASHLIGHT AT L4 SEAT INOPERATIVE. REPLACED EMERGENCY FL IGHT ATTENDANT FLASHLIGHT AT L4 SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1998091801320 19980918 01320 EU 1998 9 18 AALA981458 1 19980731 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59081 639 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS ON LEFT SIDE OF AIRCRAFT INOPERATIVE. REPAIRED WIR E SPLICE ON EMERGENCY EXIT FLOOR PATH LIGHTING ON LEFT SIDE OF AIRCRAFT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801321 19980918 01321 EU 1998 9 18 AALA981271 1 19980626 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7076A 610 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH ESCAPE LIGHTING AT SEAT 23 DISCONNECTED. RECONNECTED EMER GENCY EXIT FLOOR PATH ESCAPE LIGHTING STRIP AT SEAT 23. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801322 19980918 01322 EU 1998 9 18 AALA981268 1 19980626 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT 15AB-20AB INOPERATIVE. REPLACED EMERGENCY EXI T FLOOR PATH LIGHT POWER STRIP FROM SIDEWALL CONNECTOR TO LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801323 19980918 01323 EU 1998 9 18 AALA981267 1 19980626 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT MAINTENANCE, L4 EMERGENCY EXIT FLOOR PATH LIGHTING HAS ONLY ONE LIGHT OPERATIVE. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHT STRIP AT L4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801324 19980918 01324 EU 1998 9 18 AALA981346 1 19980708 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7076A 610 JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR TRACT LIGHTING AT R4 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT 4R DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801325 19980918 01325 EU 1998 9 18 AALA981269 1 19980626 A 3350 LIGHT AIRBUS 300 A300B4605R 3930308 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 3075A 606 JFK - DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY EXIT FLOOR PATH LIGHTING HAS ONLY ONE BULB INOPERATIVE. REPLACED RI GHT EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT 4R. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998091801326 19980918 01326 NM 1998 9 18 AALA981516 1 19980808 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1148-1160 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND STRINGER 30 CORRODED ON RT SIDE AFTER STATION 1148 TO 1160. REMOVED CORRODED AREA OF STRINGER 30. INSTALLE D FILLER AND STRINGER SPLICE AT STRINGER 30, STA 1148 TO 1160 PER SRM 53-10-3 PAGE 4B. (M) 2 L 7 3 4F A3WE 1998091801327 19980918 01327 NM 1998 9 18 AALA981517 1 19980808 A 2810 SPAR BOEING 727 727223 1384074 NM BS 865 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - FOUND CRACK IN REAR SPAR OF NR 2 FUEL TANK CENTER SECTION AT RBL 20 INCH IN RADIUS OF WEB AT TOP CHORD ANGLE. INS TALLED REPAIR DOUBLER PER ESO 11697 DATED 8-6-98. (M) 2 L 7 3 4F A3WE 1998091801328 19980918 01328 NM 1998 9 18 AALA981514 1 19980811 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1110 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - DEEP GROOVE AND SMALL NICKS ON BELLFRAME AT STATION 1110 STRINGER 26R TO STRINGER 27R. INSTALLED DOUBLER ON BELLF RAME PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998091801329 19980918 01329 NM 1998 9 18 AALA981513 1 19980811 A 5311 FRAME BOEING 727 727227 1384078 NM BS 580 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - BELLFRAME IS DENTED AT STATION 580 ABOVE STRINGER 24L. INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998091801330 19980918 01330 NM 1998 9 18 AALA981512 1 19980811 A 5711 SPAR BOEING 727 727227 1384078 NM WS 392 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND CORROSION ON TOP AND BOTTOM OF LE SPAR LOWR CHORD ANGLE AT WING LE STATION 392, BELOW FUEL VALVE. INSTALLED STRIP DOUBLER ON UPPER SIDE OF BLENDED AREA PER AARD 57-30-00-2, 14 INCHES IN LENGTH. (M) 2 L 7 3 4F A3WE 1998091801331 19980918 01331 NM 1998 9 18 AALA981511 1 19980811 A 5330 SKIN BOEING 727 727227 1384078 NM BS 820-835 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - AFT HEAT EXCHANGER PLENUM CORRODED RT SIDE. INSTALLED DOUBLER REPAIR IAW ESO 11697, DATED 7-14-98. (M) 2 L 7 3 4F A3WE 1998091801332 19980918 01332 NM 1998 9 18 AALA981510 1 19980811 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - LIGHTING STRIKE BLEND OUT IS BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER AARD 53-30-3, PAGE 1, 5, 7, 8 OF SRM 53- 30-3. (M) 2 L 7 3 4F A3WE 1998091801333 19980918 01333 NM 1998 9 18 AALA981509 1 19980811 A 5711 SPAR BOEING 727 727227 1384078 NM WS 124 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - CHORD ANGLE CRACKED 3 INCHES FORWARD OF NR 7 SPOILER CASTING. CUT OUT DAMAGED SECTION OF LOWER CHORD ANGLE AND SP LICED IN NEW SECTION PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1998091801334 19980918 01334 NM 1998 9 18 AALA981508 1 19980811 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND CORROSION UNDER INBOARD WALL ATTACH CHANNEL STATION 1130-1136 RBL 19 INCHES TO 24 INCHES, RT AFT LAV. REPAI RED WEB PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998091801335 19980918 01335 NM 1998 9 18 AALA981507 1 19980811 A 5330 SKIN BOEING 727 727227 1384078 NM BS 277 CREASED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL- FUSELAGE SKIN HAS SHARP CREASE STATION 277, STRINGER 17 LEFT OUT OF LIMITS PER SRM 53-30-1. CUT OUT DAMAGE AND INS TALLED DOUBLER PER SRM 53-30-3 PAGE 14B. (B) 2 L 7 3 4F A3WE 1998091801336 19980918 01336 WP 1998 9 18 AALA981506 1 19980915 A 5300 WEB DOUG DC9 DC982 3022082 WP BS 1155-1174 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 432AA 49350 TUL - FOUND CORROSION ON LOWER SIDE OF CUSP MEMBRANE CONTINUING UNDER 'T' EXTRUSION OF GIRT BAR SUPPORT STRUCTURE. REPA IRED IAW AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 1998091801337 19980918 01337 NM 1998 9 18 AALA981505 1 19980511 A 5510 BEAM BOEING 727 727227 1384078 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - UPPER TE BEAM HAS CORROSION ON TOP SURFACE OF BEAM, ABOVE NR 4 RIB SUPPORT CASTING. REF E58 NR 0123429. REMOVED CORROSION PER SRM 51-10-6. INSTALLED BEAM REPAIR PER SRM 55-10-6 AND ESO 11697 DATED 7/14/98. (M) 2 L 7 3 4F A3WE 1998091801338 19980918 01338 WP 1998 9 18 AALA981535 1 19980812 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 525 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 437AA 49455 TUL - CUSP CORRODED. REPAIRED IAW AARD 53-00-00-02. TST: 34,960 HOURS. CYCLES: 17,650. (X) 2 L 7 2 4F A6WE 1998091801339 19980918 01339 NM 1998 9 18 AALA981549 1 19980818 A 5311 FRAME BOEING 727 727223 1384074 NM BS 480 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - BELT FRAME CRACKED 1 INCH LONG FROM RIVET TO STRINGER. CUT OUT RADIUS, STA 1180, STR 26R. INSTALLED REPAIR PER S RM 51-40-2 FIG 1 USING 7075T6 MATERIAL, .063 INCH THICKNESS WITH 2 ROWS FASTENERS, .1875 INCH HI-LOCKS, AROUND DAMAGE, . 75 INCH SPACE BETWEEN FASTENERS. STOP DRILLED CRACK WITH .25 INCH. TST: 53,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801340 19980918 01340 NM 1998 9 18 AALA981550 1 19980818 A 5311 FRAME BOEING 727 727223 1384074 NM BS 580 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - BELT FRAME STA 580 UPPER LIP DENTED BETWEEN STR 24L AND STR 23L (DISTORTED WEB). REPAIRED PER SRM 53-10-4 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801341 19980918 01341 NM 1998 9 18 AALA981551 1 19980818 A 5311 FRAME BOEING 727 727223 1384074 NM BS 380 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - BELL FRAME CRACKED STA 380 BETWEEN STR'S 7-8, RT SIDE. REPAIRED FRAME PER SRM 53-10-4 FIG 2. TST: 53,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801342 19980918 01342 NM 1998 9 18 AALA981552 1 19980818 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - CORROSION AT FLOORBEAM AT STA 344 FROM LBL 24 TO RBL 24. INSTALLED FLOORBEAM REPAIR PER ESO 11697 AT STA 344. ES O DATED 7-28-98. TST: 53,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801343 19980918 01343 NM 1998 9 18 AALA981553 1 19980818 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - STR 27R OUTBOARD LEG CORRODED AT STA 680. REMOVED STRINGER SECTION, SPLICED NEW SECTION PER SRM 53-10-3 FIG 1. T ST: 53,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801344 19980918 01344 NM 1998 9 18 AALA981554 1 19980818 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 595 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - CORROSION ON STR 28R OUTBOARD SIDE STA 595. INSTALLED STRINGER SPLICE SECTION REPAIR PER SRM 53-10-3 FIG 1. TST: 53,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801345 19980918 01345 NM 1998 9 18 AALA981555 1 19980818 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720-740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - STR 27R CORRODED STA 720F + 4 INCHES TO STA 740. INSTALLED STRINGER SPLICE PER SRM 53-10-3 PG HB FIG 1. TST: 53 ,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801346 19980918 01346 NM 1998 9 18 AALA981556 1 19980818 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1076 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - STR 27R CORRODED AT OUTBOARD END STA 1076. INSTALLED STRINGER REPAIR AT STA 1076 PER SRM 53-10-3 FIG 1. TST: 53 ,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801347 19980918 01347 NM 1998 9 18 AALA981557 1 19980818 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - STR 15L CRACKED AT END TO FIRST FASTENER FORWARD 4 INCHES OF FS 720C. REPAIRED PER SRM 53-10-3 FIG 5. TST: 53,2 45 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801348 19980918 01348 NM 1998 9 18 AALA981558 1 19980818 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - STR 15R CRACKED AT END TO FIRST FASTENER AT FS 720B. REPAIRED PER SRM 53-20-3 FIG 5. TST: 53,245 HOURS. CYCLES : 32,117. (X) 2 L 7 3 4F A3WE 1998091801349 19980918 01349 NM 1998 9 18 AALA981559 1 19980818 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 663 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - STR 27R OUTBOARD LEG CORRODED TOP EDGE STA 663. REPAIRED PER SRM 53-10-3 FIG 2. TST: 53,245 HOURS. CYCLES: 32 ,117. (X) 2 L 7 3 4F A3WE 1998091801350 19980918 01350 NM 1998 9 18 AALA981560 1 19980818 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - SKIN UNDER INTERCOSTAL CORRODED JUST OUTBOARD OF FORWARD CARGO. INSTALLED REPAIR PER SRM 53-30-3 FIG 3. TST: 53 ,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801351 19980918 01351 NM 1998 9 18 AALA981561 1 19980818 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1075-1086 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - BELLY SKIN CORROSION UNDER STR 27R, STA 1075 - STA 1086. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. TST: 53,245 HOURS. CYCLES: 32,117. (X) 2 L 7 3 4F A3WE 1998091801352 19980918 01352 EU 1998 9 18 AALA981578 1 19980821 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU BS 56-57 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 8067A 510 TUL - CORROSION ON FUSELAGE SKIN BELOW RIGHT EMERGENCY EXIT DOOR BETWEEN STR 30 AND STR 31 AND BETWEEN FR 56 AND FR 57 R T SIDE. TRIMMED OUT DAMAGED AREA. INSTALLED FILLERS AND DOUBLERS WITH HILOKS. TREATED, PAINTED, AND SEALED PER ESO NR 30595 DATED 8-21-98. TST: 27,784.54 HOURS. CYCLES: 9,942. (X) 2 L 7 2 4F RT A35EU 1998091801353 19980918 01353 WP 1998 9 18 AALA981581 1 19980820 A 5347 TIE DOWN DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7537A 49991 TUL - CORROSION ON RT TIE DOWN TRACK, OUTBOARD FLANGE, STA 1212. REMOVED CORROSION. CUT-OUT DAMAGED AREA. INSTALLED F ILLER AND STRAP REPAIR PER ESO 80559, DATED 8-20-98 AND SRM AARD 53-20-00-13. TST: 23,605.42 HOURS. CYCLES: 12,312. (X) 2 L 7 2 4F A6WE 1998091801354 19980918 01354 WP 1998 9 18 AALA981582 1 19980821 A 5347 TIE DOWN DOUG DC9 DC982 3022082 WP BS 1057 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7537A 49991 TUL - CORROSION ON AFT ARGO TIE DOWN TRACK FROM STA 1025 TO STA 1155. CORROSION REMOVAL EXCEEDED MAXIMUM ALLOWABLE AT S TA 1057. INSTALLED REPAIR STRAP PER AARD 53-20-00-13 AT THIS LOCATION. TST: 23,605 HOURS. CYCLES: 12,312. (X) 2 L 7 2 4F A6WE 1998091801355 19980918 01355 WP 1998 9 18 AALA981583 1 19980821 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 237 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7537A 49991 TUL - DENT AND CREASE IN FUSELAGE SKIN, STA 237 BETWEEN LONGERON 18L AND LONGERON 19L. ALSO, INTERNAL DAMAGE TO FUSELAG E FRAME, BENT AND CRACKED, AT SAME LOCATION. REMOVED DAMAGED SECTION OF FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND FI LLER PER SRM 53-04, FIG 38. REMOVED DAMAGED FORMER. INSTALLED NEW SECTION. TST: 23,605.42 HOURS. CYCLES: 12,312. ( X) 2 L 7 2 4F A6WE 1998091801356 19980918 01356 WP 1998 9 18 AALA981596 1 19980831 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 479AA 49654 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHT STRIP FORWARD OF FIRST CLASS SEATS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP FORWARD OF FIRST CLASS SEATS. SYSTEM GROUND CHECKED, NORMAL OPERATION. ( X) 2 L 7 2 4F A6WE 1998091801357 19980918 01357 NM 1998 9 18 TWRA9850 1 19980829 A 2830 65B821062 SWITCH BOEING 747 747124 1384874 NM LOAD LIMITER MALFUNCTIONED A TWRA O OTHER L NO TEST DE DESCENT 1 EA 15 602FF 700018 19734 DURING FUEL DUMP, NR 3 MAIN JETTISON PUMP PRESSURE LIGHT REMAINED ON WITH BOTH PUMPS ON. DUMP RATE FROM NR 3 WAS ONE-HA LF (50 PERCENT) BELOW NR 2 MAIN. REQUIRED TO CLOSE NR 2 JETTISON PUMP TO MAINTAIN BALANCE. REF: ATB AILERON PROBLEM. CHECKED WIRING OF NR 3 MAIN INBOARD AND OUTBOARD FUEL JETTISON PUMPS CIRCUITS PER WDM 28 42 12 AND 26 31 21. RE-SECURE D LOOSE PRESSURE SWITCH CONNECTION ON NR 3 INBD PUMP. OPS CHECK NORMAL. MM REF 38 31 00. (X) 2 L 7 4 4F A20WE 1998091801358 19980918 01358 CE 1998 9 18 MASA98162 1 19980826 A 3233 1143800415 ACTUATOR 1148100231 BEECH 1900 1900D 1154162 CE LT MLG FAILED A MASA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 SW 07 17YV UE17 PIT/DBE - FLT 5918 - ON APPROACH TO CBE, THE LT GEAR WOULD NOT INDICATE DOWN AND LOCKED. CREW DECLARED AN EMERGENCY, AN D RETURNED TO PIT. AIRCRAFT LANDED WITHOUT INCIDENT AND WAS SUBSEQUENTLY FERRIED TO DUJ WHERE MAINTENANCE REMOVED AND R EPLACED THE MAIN LANDING GEAR ACTUATOR. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998091801359 19980918 01359 CE 1998 9 18 98ZZZX3397 1 19980820 A 5711 1181000229 SPAR CAP ASSY BEECH 1900 1900C 1154161 CE COCKPIT CORRODED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 01 45GL 23613 UC45 FOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN TH E CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR AND WAS DISTRIBUTED IN SMALL AREAS ACROSS SPAR JUST ABOVE THE EDGE OF THE SEALANT THAT IS USED TO SEAL THE SPAR RIVET FLANGE. A SMALL AMOUNT OF PITTING WAS FOUND ON THE HORIZONT AL SURFACE JUST ABOVE AND AFT OF THE FORWARD FACE. DAMAGE WAS DETERMINED TO BE NEGLIGIBLE AFTER CORROSION REMOVAL. 2 L 7 2 4T RT A24CE 1998091801360 19980918 01360 CE 1998 9 18 98ZZZX3398 1 19980823 A 5711 1181000229 SPAR BEECH 1900 1900C 1154161 CE COCKPIT CORRODED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 01 41UE 23461 UC41 FOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN TH E CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR AND WAS DISTRIBUTED IN SMALL AREAS ACROSS THE SPAR JUST AB OVE THE EDGE OF THE SEALANT THAT IS USED TO SEAL THE SPAR RIVET FLANGE. CORROSION WAS FOUND WITHIN THE LIMITS OF NEGLIG IBLE DAMAGE AFTER CORROSION REMOVAL. 2 L 7 2 4T RT A24CE 1998091801361 19980918 01361 CE 1998 9 18 98ZZZX3399 1 19980827 A 3230 MS24171D1 RELAY BEECH 1900 1900C 1154161 CE LT NACELLE CONTAMINATED A YADA O OTHER O OTHER DE DESCENT 1 AL 01 45GL 635 UC45 LANDING GEAR FAILED TO EXTEND WITH GEAR HANDLE SELECTION. LANDING GEAR EXTENDED USING HAND PUMP SYSTEM, GEAR INDICATION S WERE NORMAL. FOUND LANDING GEAR PUMP RELAY CONTAMINATED WITH WATER AND SUSPECT UNIT FROZE IN-FLIGHT AND FAILED TO POW ER ELECTRIC PUMP. SEALED NEW RELAY PLUNGER BODY WITH SILICONE RTV TO PREVENT MOISTURE CONTAMINATION AND INSTALLED IN AI RCRAFT. RETRACT TEST C/W, OK. 2 L 7 2 4T RT A24CE 1998091801362 19980918 01362 NM 1998 9 18 USAASB98223 1 19980830 A 5270 189929 SWITCH BOEING 737 737401 1384701 NM CARGO DOOR OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 418US 23985 SDF - FLT 1732 - DURING CLIMB-OUT, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. CAPTAIN DECIDED TO RETURN TO FIELD AT SDF TO VERIFY SECURITY OF THE CARGO DOOR. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. CAPTAIN NOTE D THAT ON LANDING, THE CARGO LIGHT EXTINGUISHED. MAINTENANCE CHECKED THE FORWARD CARGO DOOR SWITCH, MOUNTING AND WIRING . ADJUSTED PLUNGER ONE TURN. OPERATED DOOR SEVERAL TIMES. OPERATIONAL CHECK OF DOOR WARNING SYSTEM GOOD. (X) 2 L 7 2 4F RT A16WE 1998091801363 19980918 01363 NM 1998 9 18 USAASB98225 1 19980901 A 5242 SEAL BOEING 737 7374B7 1384702 NM E/E DOOR LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 778AU 24980 BWI - FLT 1435 - AFTER TAKEOFF, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT. FLIGHT RETURNED TO FIELD AT BWI AND LANDED WITH OUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE E/E DOOR SEAL OUT OF POSTION. REPOSITIONED E/E DOOR SEAL AND LUBED. PRESSURIZATION CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998091801364 19980918 01364 NM 1998 9 18 TWRA9853 1 19980827 A 3350 LIGHT BOEING 747 747136 1384883 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 606FF 20273 AFTER BLOCK, FLIGHT ATTENDANT NOTED E-ZONE PATH LIGHTING ON RIGHT SIDE, ONE-HALF SECTION OUT. ZONE LEFT SIDE E-PATH LIG HTING OUT. ON RIGHT SIDE, FOUND LOOSE CONNECTION AND SECURED. LEFT SIDE FOUND WATER IN TRACK DRIED OUT, WATER AND WIRE S POS CHECK OK. (X) 2 L 7 4 4F A20WE 1998091801365 19980918 01365 1998 9 18 TWRA9852 4 19980827 A 2564 CABLE BOEING 747 747130 1384880 NM RAFT MISSING A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 PRIOR TO FLIGHT, FLIGHT ATTENDANT REPORTED L3 LIFE RAFT COMPARTMENT DOOR NOT SECURED. FLIGHT CREW WAS NOTIFIED RAFT WAS MOVED TO R3 DOOR. INSPECTED RAFT COMPARTMENT AND FOUND LEFT HAND BALANCE CABLE OFF. REINSTALLED CABLE, PERFORMED OPS CHECK OF DOOR, OK. REINSTALLED LIFE RAFT. (X) 2 L 7 4 4F A20WE 1998091801366 19980918 01366 NM 1998 9 18 TWRA9849 1 19980901 A 2612 21562B DETECTOR BOEING 747 747212B 1384886 NM CARGO BAY FAILED A TWRA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 EA 15 619FF 21316 DURING CRUISE FL 330, AFT CARGO FIRE WARNING LIGHT AND BELL ACTIVATED. BOTH FIRE BOTTLES WERE DISCHARGED. ACCOMPLISHED EMERGENCY CHECK LIST AND AIRCRAFT DIVERTED TO DENVER. AFTER LANDING, FIRE DEPARTMENT CONFIRMED NO FIRE. INSPECTED AFT CARGO AND BULK COMPT, FOUND NO SMOKE OR FIRE. FOUND NR 5 FIRE DETECTOR FAULTY. DISCONNECTED NR 5 DETECTOR, CONTINUED IN O D I. NO CARGO IN LOWER COMPARTMENTS. 2 L 7 4 4F A20WE 1998091801367 19980918 01367 NM 1998 9 18 TAOA099801 1 19980901 A 3350 1315 LIGHT GE BOEING 727 727227 1384078 NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 925TS 21244 BOS/LGA - FLT 6141 - DURING L/S CHECK, FOUND FORWARD AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. RE-LAMPED LIGHT ASSY. OPERATIONAL CHECK NORMAL. (X) 2 L 7 3 4F A3WE 1998091801368 19980918 01368 1998 9 18 S2YA98015 4 19980601 A 3416 066030620000 ENCODER BEECH 1900 1900D 1154162 CE COCKPIT FAILED A S2YA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 GL 13 79SK 66 UE79 MKE/SBN - FLT 1166 - DURING CLIMB-OUT, FLIGHT CREW NOTICED THE PILOT'S ALTIMETER WAS FLAGGED AND ALTITUDE PRE-SELECT WAS ONLY SHOWING DASHES. AFTER AN UNEVENTFUL LANDING IN MKE, MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NR 1 ALTIMET ER INOPERATIVE AND A STATIC LINE GOING TO THE ALTIMETER TWISTED. THE ALTIMETER AND STATIC LINE WERE REPLACED, PITOT STA TIC AND OPERATIONAL CHECKS WERE PERFORMED. (X) 2 L 7 2 4T RT A24CE 1998091801369 19980918 01369 CE 1998 9 18 S2YA98019 1 19980705 A 2750 10152105223 CAM BEECH 1900 1900D 1154162 CE RT TE FLAP MALFUNCTIONED A S2YA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 13 891SK 10377 UE89 CMH/MKE - FLT 1829 - DURING TAKEOFF ROLL, CREW DETECTED SMELL OF SMOKE AND SAW SMOKE IN CABIN. ABORTED T/O, RETURNED TO GATE. MAINT INSPECTED ACFT, FOUND THE FLAP MOTOR DAMAGED FROM OVERHEATING. FLAP SYSTEM WAS PLACED ON MEL AND ACFT RET URNED TO SERVICE. MAINT REPLACED THE FLAP MOTOR AND FND FLAPS DRIVEN UP AGAINST THE STOPS AND FOUND THE FLAP LIMIT SWIT CH CAM PINCH BOLT SHEARED. WHEN CAM BOLT SHEARED, CAM ROTATED OUT OF ALIGN, WHEN CREW HAD SELECTED THE FLAPS UP AT THE END OF PREVIOUS FLIGHT, FLAP MOTOR NEVER SHUT OFF. THIS CAUSED FLAP MOTOR TO OVERHEAT AND FAIL. MAINT REPLACED FLAP MO TOR, ONE FLAP ACTUATOR, AND FLAP LIMIT SWITCH CAM BOX. RIGGED FLAPS, PERFORMED OPER CHK, RETURNED ACFT TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998091801370 19980918 01370 CE 1998 9 18 S2YA98020 1 19980726 A 3233 571302 ACTUATOR BEECH 1900 1900D 1154162 CE LT MLG FAILED A S2YA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 13 87SK 10404 UE87 MKE/DSM - FLT 1838 - DURING CRUISE, CREW NOTICED THE LANDING GEAR HANDLE ILLUMINATE AND THE LANDING GEAR CIRCUIT BREAKER OPEN. MANUALLY EXTENDED GEAR AND RETURNED TO MKE. THEY DID NOT DECLARE EMERGENCY, BUT WERE MET ON THE GROUND BY CFR. MAINTENANCE INSPECTED AIRCRAFT AND FOUND THE HYDRAULIC POWER PACK MOTOR INOPERATIVE. MOTOR REPLACED AND THE GEAR OPS C HECKED GOOD. THE PUMP MOTOR WAS DISASSEMBLED, INSPECTED, AND FOUND A WIRE THAT CONNECTED TWO OF THE BRUSHES TOGETHER WA S MELTED WHERE A TERMINAL JOINED THEM TOGETHER. (X) 2 L 7 2 4T RT A24CE 1998091801371 19980918 01371 1998 9 18 S2YA98022 4 19980811 A 3454 6222506014 INDICATOR BEECH 1900 1900D 1154162 CE COCKPIT FAILED A S2YA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 13 92SK 1930 UE92 DURING PRE-FLIGHT RUN UP, CREW NOTICED SMOKE IN THE COCKPIT COMING FROM THE LT SUB-PANEL AND THE RMI FLAGGED INOPERABLE. AFTER FINISHING THE RUN-UP, THEY RETURNED TO THE GATE AND NOTIFIED MAINTENANCE. AFTER ACFT FERRIED TO MKE WITHOUT INC IDENT, MAINT INSPECTED THE AIRCRAFT AND FOUND THE RMI TO BE THE CAUSE OF THE SMOKE. THE RMI WAS REPLACED AND THE AIRCRA FT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998091801372 19980918 01372 CE 1998 9 18 S2YA98024 1 19980817 A 6120 CONTROL CABLE BEECH 1900 1900D 1154162 CE PROP CONTROL LOOSE A S2YA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 145SK UE145 LSE/MKE - FLT 1090 - WHILE CLIMBING THROUGH 6,700 FEET, THE RT ENGINE TORQUE INCREASED MOMENTARILY AND THEN SLOWLY START ED TO DECREASE. THE CREW SECURED THE ENGINE AS THE TORQUE DROPPED PAST 1,000 FEET/POUNDS. DECLARED AN EMERGENCY AND DI VERTED TO MSN WHERE AN UNEVENTFUL LANDING WAS MADE. MAINT INSPECTED THE OIL FILTER, ENGINE PLUMBING, AND ENGINE CONTROL S. ON THE PROPELLER GOVERNOR THEY NOTICED THE BETA VALVE FULLY EXTENDED, THE OUTER GUIDE ON THE FORWARD SIDE OF THE BET A CABLE WAS FOUND LOOSE, BUT STILL SAFETIED. THEY RIGGED THE ENGINE BETA LINKAGES, FLIGHT IDLE TORQUE, AND GROUND IDLE TORQUE. AFTER ALL CHECKED GOOD ON THE GROUND, THE AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998091801373 19980918 01373 CE 1998 9 18 S2YA98025 1 19980817 A 5310 SKIN BEECH 1900 1900D 1154162 CE FWD FUSELAGE BIRD STRIKE A S2YA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 13 831SK UE83 MKE/CWA - FLT 1071 - JUST AFTER TAKEOFF, AIRCRAFT STRUCK A BIRD JUST ABOVE THE FIRST OFFICER'S WINDSHIELD. THE CREW DEC IDED TO RETURN TO MKE SO THE AIRCRAFT COULD BE INSPECTED FOR DAMAGE. AFTER MAKING AN UNEVENTFUL LANDING, MAINTENANCE IN SPECTED AIRCRAFT AND FOUND NO DAMAGE. AIRCRAFT WAS THEN RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998091801374 19980918 01374 WP 1998 9 18 GTIA9800094 1 19980812 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 DTW - SEVERAL CABIN EMERGENCY LIGHTS BURNED OUT. REMOVED AND REPLACED BURNED OUT CABIN EMERGENCY LIGHTS WITH NEW EMERGE NCY LIGHTS AS REQUIRED IAW DC9 MM 33-53-00, OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4F A6WE 1998091801375 19980918 01375 WP 1998 9 18 GTIA9800096 1 19980814 A 3350 LIGHT DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 132NK 47202 DTW - EMERGENCY FLOOR TRACK LIGHT IN AFT SECTION, LIGHTS NOT WORKING. REPLACED BAD SPLICE. OPERATIONAL CHECK GOOD IAW DC-9 MM 33-50-0. (X) 2 L 7 2 4F A6WE 1998091801376 19980918 01376 WP 1998 9 18 GTIA9800098 1 19980824 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 DTW - FLT 548 - FORWARD SECTION OF EMERGENCY EXIT FLOOR LIGHTING FOUND INOPERATIVE DURING PRE-FLIGHT INSPECTION. FOUND LOOSE WIRE AND SECURED SAID LOOSE WIRE. LIGHTING OPERATIONAL CHECK GOOD. NO DEFECT NOTED AT THIS TIME. IAW DC-9 MM 33 -50-0. (X) 2 L 7 2 4F A6WE 1998091801377 19980918 01377 WP 1998 9 18 GTIA9800095 1 19980816 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 131NK 47605 DTW - EMERGENCY FLOOR PATH LIGHTING INTERMITTENT. FOUND LOOSE WIRE, RE-CRIMPED WIRE IAW DC-9 MM, OPERATIONAL CHECK GOOD . (X) 2 L 7 2 4F A6WE 1998091801378 19980918 01378 NM 1998 9 18 TWAA9814901 1 19980916 A 3397 58531 WIRE BOEING 727 727231 1384079 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54341 21628 DURING MAINT CHECK, FOUND EGRESS LIGHTS INOPERATIVE SEAT ROW 17 TO 23. REPLACED FEEDER CABLE. CHECK-C 1-10-98 JFK. 2 L 7 3 4F A3WE 1998091801379 19980918 01379 WP 1998 9 18 TWAA9814902 1 19980828 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 170-175 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 923L 47109 DURING MAINT, FOUND FIVE .250 INCH CRACKS IN FUSELAGE SKIN EXTENDING FROM RIVETS STA 170 TO 175, LONGERON 22L. REPAIRED PER SRM 53-04, FIG 12B. CHECK-C 3-2-98 STL. 2 L 7 2 4F A6WE 1998091801380 19980918 01380 NM 1998 9 18 TWAA9814903 1 19980907 A 5753 TE WEDGE BOEING 767 767231 1385131 NM RT TE FLAP CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING CHECK-C MAINT, FOUND ON RT WING THE O/B TE FLAP, CENTER TE WEDGE LOWER SURFACE WITH A 4 INCH CRACK. DRESSED OUT DAMAGED AREA AND INSTALLED 3 SKIN HOT BOND REPAIRS 4 IN BY 6 IN PER SRM 51-70-07 FIG 4A. 2 L 7 2 4F RT A1NM 1998091801381 19980918 01381 WP 1998 9 18 TWAA9814904 1 19980911 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 200 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 990Z 47136 DURING CHECK-C MAINT, FOUND .125 INCH CRACK IN LONGERON 4L AT STA 200. SPLICED IN NEW SECTION OF LONGERON PER DC9 SRM 5 3-02, FIG 18. 2 L 7 2 4F A6WE 1998091801382 19980918 01382 WP 1998 9 18 VJ9800400 1 19980818 A 5312 BLKHD STIFFENER DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 BLEED AIR LINE TO LT AIR CONDITIONING SYSTEM CHAFED BEYOND LIMIT AT LEG OF CIRCUMFERENTIAL STIFFENER ANGLE ON LT SIDE OF AFT PRESSURE BULKHEAD BETWEEN L12 AND L13. BLENDED CHAFE IAW DC9 SRM 53-01 AND FABRICATED BULKHEAD STIFFENER REPAIRS F ROM 2024T3, .032, IAW DC9 SRM 53-01-10. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998091801383 19980918 01383 WP 1998 9 18 VJ9800401 1 19980819 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 FLOOR SUPPORT STRUCTURE HAS CORROSION BEYOND LIMIT AROUND FASTENER 20 INCHES RIGHT OF CENTER LINE AT STA 980. BLENDED A ND CUT OUT CORRODED AREA, REPAIR FILLER AND ANGLE IAW DC9 SRM 51-10-3 AND 53-05. INSTALLED REPAIR IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998091801384 19980918 01384 WP 1998 9 18 VJ9800402 1 19980819 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 UPPER AND LOWER MATING SURFACES OF STATIC DISCHARGE ATTACHMENTS CORRODED BEYOND LIMIT. REMOVED CORROSION FROM ATTACH SU RFACES OF STATIC DISCHARGE WICKS ON LT WING TRAILING EDGE BETWEEN AILERON AND WING TIP. CUT OUT CORRODED SKIN, FABRICA TED REPAIR DOUBLERS, TREATED, PRIMED AND INSTALLED DOUBLER REPAIR. CLEANED SEALANT FROM SKIN SURFACE IAW DC9 SRM 57-01- 3, 57-31-3, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998091801385 19980918 01385 WP 1998 9 18 VJ9800403 1 19980820 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 FLOOR SUPPORT ANGLE HAS NUT PLATES CORRODED BEYOND LIMIT AT BS 579, STR 30 AND 27 L. REMOVED FLOOR SUPPORT ANGLE AND NU T PLATES TO DETERMINE CORROSION BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. FABRICATED DOUBLERS, HEAT TREATED, TRIMMED TO FI T, DRILLED, DEBURRED, COUNTERSUNK, ALODINED, PRIMED AND INSTALLED L ANGLES TO FLOOR SUPPORT AND TO FLOOR SUPPORT FRAME A ND REINSTALLED NUT PLATES IAW DC9 SRM 51-30-2, 53-01, FIG 2, AND 51-10-3. 2 L 7 2 4F A6WE 1998091801386 19980918 01386 WP 1998 9 18 VJ9800404 1 19980825 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 83-55 DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 EXTERNAL REPAIR AT FS 83-55 ABOVE LT NOSE WHEEL WELL REQUIRES FLUSH REPAIR BECAUSE IT IS IN A CLASS 1 AERODYNAMIC AREA. REMOVED EXISTING DOUBLER AND FRAME FOR ACCESS IAW RES 981346. FABRICATED TITANIUM INTERNAL DOUBLER AND FLUSH FILLER FR OM 2024T3. ALODINED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED REPAIR IAW DC9 SRM 53-04, FIG 38, 51-30-2 AND RES 981378 . 2 L 7 2 4F A6WE 1998091801387 19980918 01387 WP 1998 9 18 VJ9800405 1 19980826 A 5260 RIB DOUG DC9 DC932 3022066 WP AFT AIRSTAIRS CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 INNER ATTACHING RIB NR 5 ON AFT AIRSTAIRS CORRODED BEYOND LIMIT AT ATTACHING POINTS LT, RT AND CENTER. LT AND RT POINTS CORRODED BEYOND LIMIT IAW DC9 SRM 52-01, PG 3. FORMED REPAIR ANGLES FROM 2024T3, .025, IAW DC9 SRM 52-01, PG9. HEAT T REATED IAW SRM 51-10-2A. DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED ANGLES IAW DC9 SRM 51-10-3, 51-30-2, AND 51- 30-5. 2 L 7 2 4F A6WE 1998091801388 19980918 01388 WP 1998 9 18 VJ9800406 1 19980826 A 5260 RAIL DOUG DC9 DC932 3022066 WP BS 1100 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 AFT ENTRY AIRSTAIRS CORRODED BEYOND LIMIT ON RAIL PANEL AT LT FS 1100. CUT OUT CORRODED AREA IAW DC9 SRM 51-10-3 AND 52 -01. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR ON RAIL IAW DC9 SRM 52-01 AND 52-05. FABRICATED AND INSTALLED STACKED ANGLE REPAIR AND STEP SUPPORT ANGLES IAW 52-01-2 AND 51-30-3. 2 L 7 2 4F A6WE 1998091801389 19980918 01389 WP 1998 9 18 VJ9800407 1 19980826 A 5260 RIB DOUG DC9 DC932 3022066 WP AFT AIRSTAIRS CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 INNER ATTACH RIB, NR 4 FROM TOP, CORRODED BEYOND LIMIT AT LT, RT AND CENTER ATTACH POINTS. REMOVED CORROSION IAW DC9 SR M 52-01, PG 3. FORMED REPAIR ANGLES FROM 2024, .025. HEAT TREATED, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED IA W DC9 SRM 51-10-2A, 51-10-4, 51-10-3, 51-30-2, 51-30-5. 2 L 7 2 4F A6WE 1998091801390 19980918 01390 WP 1998 9 18 VJ9800408 1 19980829 A 5522 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 TRAILING EDGE SKIN LT ELEVATOR, UPPER OUTBOARD AFT CORNER CORRODED BEYOND LIMIT. FABRICATED REPAIR FROM 2024T3, .050. T REATED AND PRIMED AREA, INSTALLED DOUBLER IAW DC9 SRM 51-30-8, 51-10-3, 55-01, 55-03 FIG 14. 2 L 7 2 4F A6WE 1998091801391 19980918 01391 WP 1998 9 18 VJ9800409 1 19980829 A 5522 SKIN DOUG DC9 DC932 3022066 WP LT ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 TRAILING EDGE SKIN OUTBOARD LOWER AFT CORNER LT ELEVATOR CORRODED BEYOND LIMIT. FABRICATED DOUBLER REPAIR, DRILLED, COU NTERSUNK, ALODINED, PRIMED AND INSTALLED DOUBLER IAW DC9 SRM 55-20-0 FIG 3, 51-30-9, 51-10-3, 51-30-8. 2 L 7 2 4F A6WE 1998091801392 19980918 01392 WP 1998 9 18 VJ9800410 1 19980912 A 3230 CONTROL CABLE DOUG DC9 DC932 3022066 WP LANDING GEAR OUT OF ADJ A ZZDA A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 SO 15 912VV 47359 AFTER TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. AS PRECAUTIONARY MEASURE FLIGHT CREW ELECTED TO RETURN TO A TL MAINTENANCE BASE. ADJUSTED ANTI RETRACTION CABLE WHICH WAS FOUND TO BE OUT OF TOLERANCE IAW MM 32-23-1, PERFORMED GE AR SWING AND ALL CHECKS NORMAL. 2 L 7 2 4F A6WE 1998091801393 19980918 01393 NM 1998 9 18 MALA976192 1 19980915 A 3350 MS25231316 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 848MA 346 DURING INSPECTION, OVERHEAD AND OUTSIDE EMERGENCY LIGHTS INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998091801394 19980918 01394 NM 1998 9 18 RAAA98B2041 1 19980912 A 3350 873100112 LIGHT BOEING 727 72722C 138400F NM CABIN ILLUMINATED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 2 FLOOR PROXIMITY EGRESS LIGHT WOULD NOT EXTINGUISH AT GATE. RESET EMERGENCY LIGHTS AND CHECKED OK. 2 L 7 3 4F A3WE 1998091801395 19980918 01395 NM 1998 9 18 CALA9801743 1 19980914 A 5753 PAD BOEING 727 727224 1384076 NM RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND CORROSION AT RT WING AFT FALSE SPAR PAD WHERE NR 5 AND NR 6 FLAP TRACKS MOUNT. THE FLAP TRACK MOUNT PA DS WERE REMOVED IAW SRM 51-30-2. NEW MOUNT PADS WERE INSTALLED IAW SRM 51-10-6, 51-10-1, AND 51-30-2. 2 L 7 3 4F A3WE 1998091801396 19980918 01396 NM 1998 9 18 CALA9801744 1 19980914 A 5753 ANGLE BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT RT INBOARD MIDFLAP JUST OUTBOARD OF NR 5 FLAP CARRIAGE. THE ANGLE WAS REMOV ED AND REPLACED IAW SRM 51-10-1. 2 L 7 3 4F A3WE 1998091801397 19980918 01397 NM 1998 9 18 CALA9801745 1 19980914 A 5730 PANEL BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .375 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 12 SPOILER INBOARD HINGE AREA. THE CRACK WAS ST OP DRILLED IAW SRM 51-10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4 AND 51-30-2. 2 L 7 3 4F A3WE 1998091801398 19980918 01398 WP 1998 9 18 CALA9801746 1 19980914 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 950 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 950, THREE INCHES BELOW LONGERON 14L. THE CRACKED AREA WAS REMO VED IAW SRM 53-04, FIGURE 38. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1998091801399 19980918 01399 WP 1998 9 18 CALA9801747 1 19980914 A 5523 TAB DOUG DC9 DC932 3022066 WP LT ELEVATOR DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND TWO AREAS OF DELAMINATION ON UPPER SURFACE OF LT ELEVATOR CONTROL TAB BETWEEN THIRD AND OUTBOARD HINGES . THE DELAMINATED AREAS WERE TRIMMED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-2. 2 L 7 2 4F A6WE 1998091801400 19980918 01400 WP 1998 9 18 CALA9801748 1 19980914 A 5400 WEB DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND THREE 2 INCH CRACKS ON NR 1 ENGINE PYLON INTERNAL WEB AT STA 1065. THE CRACKS WERE STOP DRILLED IAW SR M 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 54-01, FIGURE 2. 2 L 7 2 4F A6WE 1998091801401 19980918 01401 WP 1998 9 18 CALA9801749 1 19980914 A 5753 FITTING DOUG DC9 DC932 3022066 WP LT TE FLAP VANE GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND FLAP FITTING GOUGED AT AFT END OF LT WING AFT MOVEABLE VANE INBOARD TRACK STA XFLS 65.612 TO 69.125. T HE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998091801402 19980918 01402 WP 1998 9 18 CALA9801750 1 19980914 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 332 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND FRAME GOUGED AT STA 332, LONGERON 29L TO 30. A SPLICE AND PLATE REPAIR WAS INSTALLED IAW SRM 53-03, FI GURE 2A AND 51-10-2A. 2 L 7 2 4F A6WE 1998091801403 19980918 01403 WP 1998 9 18 CALA9801751 1 19980914 A 5510 FAIRING DOUG DC9 DC932 3022066 WP RT HORIZ STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND RT LOWER HORIZONTAL STABILIZER FAIRING DELAMINATED AT FWD END. THE DELAMINATED HONEYCOMB CORE, DOUBLER , AND PLATE WERE REMOVED. BONDED DOUBLER WITH HONEYCOMB CORE AND PLATE TO SKIN FAIRING IAW ECRA 5510-01317, SRM 51-70-2 , 51-30-2. 2 L 7 2 4F A6WE 1998091801404 19980918 01404 WP 1998 9 18 CALA9801752 1 19980914 A 5510 FAIRING DOUG DC9 DC932 3022066 WP LT HORIZ STAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FAIRING DELAMINATED FROM AFT ATTACH POINT FORWARD. REMOVED PAN ON LOWER SURFACE AND REMOVED DELAMINATED HONEYCOMB. NEW HONEYCOMB WAS BONDED IN LOWER PAN AND THEN PAN WAS INSTALLED ON FAIRING AND BONDED IAW SRM 51-70-2 AND ECRA 5510-01316. 2 L 7 2 4F A6WE 1998091801405 19980918 01405 NM 1998 9 18 CALA9801753 1 19980914 A 5320 FLOOR PAN BOEING 727 727232 1384082 NM BS 1173 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CABIN INTERIOR CENTER AISLE FLOOR PAN CORRODED AT BS 1173, RBL 22. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-30-2, 51-10-6, MM 51-20-11. 2 L 7 3 4F A3WE 1998091801406 19980918 01406 NM 1998 9 18 CALA9801754 1 19980914 A 5330 PANEL BOEING 727 727232 1384082 NM BS 620-720D CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT TRANSITION PANEL CORRODED AROUND NUT PLATES IN FORWARD CARGO COMPARTMENT AT STA 620-720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998091801407 19980918 01407 NM 1998 9 18 CALA9801755 1 19980914 A 5330 PANEL BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOOR TRANSITION PANEL CORRODED AT BS 720A-720D, STRINGER 26R. THE PANEL WAS REMOVED AND A NEW PANEL W AS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998091801408 19980918 01408 NM 1998 9 18 CALA9801756 1 19980914 A 5330 PANEL BOEING 727 727232 1384082 NM STA 660-720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT TRANSITION PANEL CORRODED IN FORWARD CARGO PIT AT FS 660 TO 720D. THE PANEL WAS REMOVED AND A NEW P ANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998091801409 19980918 01409 NM 1998 9 18 CALA9801757 1 19980914 A 5320 DOUBLER BOEING 737 7372C0 1384488 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND INTERNAL DOUBLER CORRODED AT STA 294.5 LEFT. THE CORRODED SECTION OF DOUBLER WAS CUT OUT, FILLER AND D OUBLER WERE INSTALLED IAW ECRA 5330-02709. 2 L 7 2 4F A16WE 1998091801410 19980918 01410 NM 1998 9 18 CALA9801758 1 19980914 A 5320 STRAP BOEING 737 7372C0 1384488 NM E & E COMPT PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A HOLE IN STRAP JUST FORWARD OF E & E COMPARTMENT ENTRANCE. A DOUBLER WAS INSTALLED IAW SRM 51-10-2 AN D ECRA 5330-02712. 2 L 7 2 4F A16WE 1998091801411 19980918 01411 NM 1998 9 18 CALA9801759 1 19980914 A 5230 SKIN BOEING 737 7372C0 1384488 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO DOOR SKIN CUTOUT AT LOWER AFT CORNER. THE EXISTING DOUBLERS WERE REMOVED, FILLERS, DOUBLERS, AND TRIPLERS WERE INSTALLED IAW SRM 51-30-2 AND ECRA 5330-02710. 2 L 7 2 4F A16WE 1998091801412 19980918 01412 NM 1998 9 18 CALA9801760 1 19980914 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 312 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND FORWARD GALLEY DOOR CUTOUT UPPER FORWARD CORNER CRACKED AT STA 312. THE CRACKED AREA WAS ROUTED OUT. R EPAIR FILLERS, DOUBLERS, AND TRIPLERS WERE INSTALLED IAW SRM 51-30, ECRA 5330-02703 AND BOEING DRAWING 65C33800. 2 L 7 2 4F A16WE 1998091801413 19980918 01413 NM 1998 9 18 CALA9801761 1 19980914 A 5321 FLOOR BOEING 727 727232 1384082 NM LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND LT AFT SINK DRAIN FLOOR AREA CORRODED. THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1, PAGE 6 AND 51-10-2. 2 L 7 3 4F A3WE 1998091801414 19980918 01414 WP 1998 9 18 CALA9801762 1 19980915 A 5510 CAP DOUG DC10 DC1030 3023501 WP LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND AN 11 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE LOWER OUTBOARD CAP AT L4. THE CAP WAS REMOVE D AND A NEW CAP WAS INSTALLED IAW SRM 51-21-01, 51-31-01, AND 55-12-01, FIGURE 3. 2 L 7 3 4F A22WE 1998091801415 19980918 01415 WP 1998 9 18 CALA9801763 1 19980915 A 5510 CAP DOUG DC10 DC1030 3023501 WP LT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND A 6 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE INBOARD SIDE CAP AT L3. THE CAP WAS REMOVED AN D A NEW CAP WAS INSTALLED IAW SRM 51-33-01 AND 55-12-01. 2 L 7 3 4F A22WE 1998091801416 19980918 01416 WP 1998 9 18 CALA9801764 1 19980915 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1520-1560 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND CENTER CARGO COMPARTMENT INTERIOR SKIN SWELLING AT STA 1520 TO 1560 BETWEEN STRINGER 45R AND 46R. THE SKIN WAS REPAIRED IAW ENGINEERING ORDER MF-MAN-D10-53-86829. 2 L 7 3 4F A22WE 1998091801417 19980918 01417 NM 1998 9 18 CALA9801765 1 19980914 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1034 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED AT FS 1034, RBL 12-24. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WA S INSTALLED IAW SRM 53-00 AND 51-10-2. 2 L 7 3 4F A3WE 1998091801418 19980918 01418 NM 1998 9 18 CALA9801766 1 19980914 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 683-688 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND STRINGER 26R CORRODED IN FORWARD CARGO COMPARTMENT AT STA 683 TO 688. THE CORROSION WAS REMOVED IAW SR M 51-10-6. THE CORRODED AREA WAS CUT OUT IAW SRM 53-30-3, FIGURE 6. A REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 6 A ND 51-10-2. 2 L 7 3 4F A3WE 1998091801419 19980918 01419 NM 1998 9 18 CALA9801767 1 19980914 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1120 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT INTERCOSTAL AT FS 1120, BL 0. THE TOP FLANGE WAS REMOVED AND A NEW SEC TION WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND 51-20-1 FIGURE 7. 2 L 7 3 4F A3WE 1998091801420 19980918 01420 NM 1998 9 18 CALA9801768 1 19980914 A 5320 INTERCOSTAL BOEING 727 727224 1384076 NM BS 970 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .5 INCH CRACK AT TOP FLANGE OF INTERCOSTAL THREE INCHES AFT OF FLOOR FRAME FS 970, BL 0. THE TOP FLA NGE WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-2 AND 51-20-1. 2 L 7 3 4F A3WE 1998091801421 19980918 01421 NM 1998 9 18 CALA9801769 1 19980915 A 5530 ANGLE BOEING 727 727224 1384076 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .25 INCH CRACK IN VERTICAL STABILIZER FORWARD RT DORSAL FIN ATTACH ANGLE. THE ANGLE WAS REMOVED AND REPLACED IAW EA 5340-01012. 2 L 7 3 4F A3WE 1998091801422 19980918 01422 NM 1998 9 18 CALA9801770 1 19980915 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 65 TO LBL 65. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A R EPAIR WAS INSTALLED IAW SRM 51-30-2, 53-10-2, 53-10-8, FIGURE 9, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998091801423 19980918 01423 NM 1998 9 18 QXEA9801284 1 19980913 A 3350 MS25231316 BULB DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 813PH 32 COCKPIT EMERGENCY OVERHEAD LIGHT INOP. RELAMPED, PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTS SYSTEM. ALL LIGHTS OP ERATE NORMALLY. 2 H 7 2 4T RT A13NM 1998091801424 19980918 01424 NM 1998 9 18 QXEA9801285 1 19980911 A 2150 SCREEN DHAV DHC8 DHC8202 2809007 NM ACM DIRTY A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 347PH 480 BLEEDS EMITTING A VERY STRONG ODOR FOR ABOUT 30 SECONDS AFTER BEING TURNED ON. FOUND SCREEN ON ACM DIRTY. CLEANED SCRE EN. GROUND RAN, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998091801425 19980918 01425 NM 1998 9 18 QXEA9801286 1 19980914 A 3350 1013079 BULB GRIMES 82520977001 DHAV DHC8 DHC8102 2809003 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 824PH 157 TWO FLOOR EMERGENCY LIGHTS INOP. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998091801426 19980918 01426 EU 1998 9 18 QXEA9801287 1 19980910 A 2611 SMOKE DETECTOR KIDDIE FOKKER F28 F28MK4000 4990810 EU LAVATORY MALFUNCTIONED A QXEA K NONE N FALSE WARNING NR NOT REPORTED 1 NM 09 496US 11167 LAV SMOKE DETECTOR GOES OFF DURING PRESSURIZATION. MAINTENANCE REPLACED THE DETECTOR AND OPERATIONALLY TESTED BY PRESSU RIZING AIRCRAFT. TEST CHECKED NORMAL. 2 L 7 2 4F RT A20EU 1998091801427 19980918 01427 EU 1998 9 18 QXEA9801288 1 19980914 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 478US 11227 OVERWING EXIT LIGHT AT ROW 9A IS INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998091801428 19980918 01428 EU 1998 9 18 QXEA9801289 1 19980915 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 482US 11231 AFT SIDE OF CENTER EXIT LIGHT HAS A LAMP OUT. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998091801429 19980918 01429 EU 1998 9 18 QXEA9801290 1 19980914 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 EMERGENCY EXIT LIGHT OUT AT ROW 8. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998091801430 19980918 01430 EU 1998 9 18 QXEA9801291 1 19980911 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 OVERHEAD EMERGENCY EXIT LIGHT AT ROW 13 AND 14 INOPERATIVE. MAINTENANCE RELAMPED AND OPERATIONALLY TESTED. TESTS ARE N ORMAL. 2 L 7 2 4F RT A20EU 1998091801431 19980918 01431 NM 1998 9 18 QXEA9801292 1 19980915 A 3350 6038441 POWER SUPPLY DHAV 82410191011 DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 828PH 287 LEFT AFT EMERGENCY EGRESS LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY (S/N 0049) AND POWER SUPPLY OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998091801432 19980918 01432 NM 1998 9 18 98FDEA00574 1 19980915 A 3260 LIGHT BOEING 727 72725 1384006 NM NLG FAILED A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 509FE 18280 NOSE GEAR AND RIGHT GEAR DOWN AND LOCKED (GREEN) LIGHTS DID NOT COME ON UPON GEAR EXTENSION. EXECUTED MISSED APPROACH. CHANGED 4 LIGHT BULBS IN 2 IND. CYCLED GEAR BACK DOWN WITH GOOD IND. LANDED UNEVENTFULLY. *S/D* PER CREW REPORT SYS TEM OPERATIONAL CHECK NORMAL. 2 L 7 3 4F A3WE 1998091801433 19980918 01433 NM 1998 9 18 98FDEA00575 1 19980915 A 5313 65587776 STRINGER BOEING 727 727247 138408F NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 233FE 21327 CORROSION (C53-113-01,11) ON STR 27 RT AT BS 720B+10 FWD CARGO BAY. *S/D* REPAIRED STR 27 RT, BS 720 AT 14 TO 720B+12 PER FED-EX SRM 53-10-3 FIG 1. 2 L 7 3 4F A3WE 1998091801434 19980918 01434 NM 1998 9 18 98UAL900371 1 19980728 A 7110 BRACKET BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE BROKEN A UALA O OTHER O OTHER NR NOT REPORTED 1 WP 29 7448U 21902 700047 NR 3 ENGINE THROTTLE STUCK AT 80 PERCENT NI. *S/D* THE FORWARD COWL HOLD OPEN ROD BRACKET HAD BROKE AND WAS JAMMED IN THE FUEL CONTROL LINKAGE, LIMITING ITS TRAVEL. ONCE THE ROD WAS REMOVED FROM THE LINKAGE, THE ENGINE OPERATED NORMALLY. MANUFACTURED AND INSTALLED NEW BRACKET. 2 L 7 3 4F 4 F A3WE E2EA 1998091801435 19980918 01435 NM 1998 9 18 98UAL900437 1 19980908 A 3610 SENSE LINE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT BLEED AIR DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 29 947UA 26688 RIGHT BLEED TRIPPED RESULTING IN A LOSS OF CABIN PRESSURE. *S/D* WHEN THE RIGHT HAND PACK TRIPPED OFF, THE ISOLATION V ALVE OPENED AND BLEED AIR SUPPLIED FROM THE LEFT HAND PACK ENTERED INTO THE RIGHT SIDE OF THE PNEUMATIC MANIFOLD. A HOL E WAS DETECTED IN THE SENSE LINE CONNECTING THE PRESSURE REGULATING AND SHUTOFF VALVE TO THE 450 THERMOSTAT. THE SENSE LINE WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998091801436 19980918 01436 EU 1998 9 18 98UAL900438 1 19980903 A 3260 LGCIU AIRBUS 320 A320232 3930326 EU IAE V2522 V2522A5 NE NLG DOOR MALFUNCTIONED A UALA O OTHER N FALSE WARNING DE DESCENT 1 WP 29 448UA 842 CREW REPORTS LANDING GEAR DID NOT COMPLETELY EXTEND ON FIRST ATTEMPT. CYCLED GEAR, OPS NORMAL. *S/D* LGCIU REPORTED N LG R DOOR PROX SENSOR 38GA TARGET POSITION. CHECKED GAPS AND FOUND WITHIN TOLERANCE PER AMM 32-31-73. BITE TEST OK. N O FURTHER PROBLEMS. 2 L 7 2 4F 4 F RT A28NM E40NE 1998091801437 19980918 01437 NM 1998 9 18 98UAL900442 1 19980908 A 3230 VALVE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LANDING GEAR FAILED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7295U 21573 RETURNED TO OKC DUE TO A HYDRAULIC SYSTEM INOPERATIVE. *S/D* REPLACED UPLOCK SEQUENCE VALVE. ACCOMPLISHED GEAR SWING, SYSTEM OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998091801438 19980918 01438 1998 9 18 98UAL900443 4 19980907 A 3418 69485938 MODULE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E/E COMPT FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7452U 21906 STALL WARNING ON ROTATION WITH FIRST OFFICER'S STICK SHAKER. RETURNED TO ORD. *S/D* NR 2 STALL WARNING MODULE. REPLA CED NR 2 STALL WARNING MODULE, OPS CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998091801439 19980918 01439 NM 1998 9 18 98UAL900444 1 19980903 A 3350 1001143LBU1 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7279U 21557 AIRSTAIR AFT EMERGENCY EXIT LIGHT INOPERATIVE. *S/D* LIGHT ASSY WAS FOUND TO BE DISCHARGED. THE LIGHT ASSY WAS REPLAC ED AND CHECKED FOR PROPER OPERATION. 2 L 7 3 4F 4 F A3WE E2EA 1998091801440 19980918 01440 NM 1998 9 18 98UAL900445 1 19980903 A 3610 REGULATOR AIRESEARCH 89812611 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 STRUT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7467U 21921 AT FLAP RETRACTION NR 3 STRUT OVERHEAT LIGHT CAME ON, LIGHT WENT OUT WHEN THROTTLE RETARDED. KEPT THROTTLE AT IDLE UNTI L LANDING. RETURNED TO ORD. *S/D* HIGH DUCT PRESSURE. REPLACED HIGH STAGE REGULATOR. 2 L 7 3 4F 4 F A3WE E2EA 1998091801442 19980918 01442 NE 1998 9 18 98UAL900447 2 19980905 A 7510 DUCT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE FAILED A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7281U 21559 WHEN ENGINE ANTI-ICE WAS SELECTED ON THE NR 2 COWL ANTI-ICE DUCT TEMPERATURE CLIMBED TO 230 DEGREES. BEFORE IT WAS SELE CTED AN ACRID SMELL WAS EVIDENT IN THE COCKPIT AND CABIN. 2 L 7 3 4F 4 F A3WE E2EA 1998091801443 19980918 01443 WP 1998 9 18 ABXA9800827 1 19980914 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 982AX 47317 WHEN TESTING EMERGENCY LIGHTS, LIGHTS WENT FROM DIM TO OFF IN 5 SECS. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES. 2 L 7 2 4F A6WE 1998091801444 19980918 01444 WP 1998 9 18 MWEA98961 1 19980911 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 FORWARD ENTRANCE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998091801445 19980918 01445 NM 1998 9 18 P5CA9801429 1 19980824 A 5350 FAIRING BOEING 747 747122 1384872 NM LT WING ROOT DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEFT HAND UNDERWING ROOT PANEL DELAMINATED. REMOVED PANEL AND REPAIRED PANEL AND INSTALLED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998091801446 19980918 01446 NM 1998 9 18 P5CA9801430 1 19980824 A 5350 FAIRING BOEING 747 747122 1384872 NM BS 850 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEFT FUSELAGE BODY FAIRING AT STA 850 IS DELAMINATED. REPAIRED PANEL PER SRM 51-40-07. 2 L 7 4 4F A20WE 1998091801447 19980918 01447 NM 1998 9 18 P5CA9801431 1 19980824 A 5350 FAIRING BOEING 747 747122 1384872 NM BS 900 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEFT FUSELAGE BODY FAIRING AT STA 900 IS DELAMINATED. REPAIRED PANEL PER SRM 51-40-07. 2 L 7 4 4F A20WE 1998091801448 19980918 01448 NE 1998 9 18 P5CA9801432 2 19980829 A 7230 FAN BLADES BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE BROKEN A P5CA K NONE C F.O.D. IN INSP/MAINT 1 WP 23 858FT 20109 DURING TRANSIT CHECK AT DXB FOUND BIRD STRIKE DAMAGE TO NR 2 ENGINE. VARIOUS FAN BLADES BROKEN OFF AT TIPS AND BLADES A LSO BENT. TOTAL 8 BLADES DAMAGED. CARRIED OUT FOD (BIRD STRIKE) INSP PER MM 72-00-00. NO DAMAGE EVIDENT ADJACENT TO C ORE, ONLY FAN BLADES. FAN BLADES REPLACED PER MM 72-31-02 PG 401. ENGINE IDLE RUN CARRIED OUT SATISFACTORY. 2 L 7 4 4F 4 F A20WE E20EA 1998092200002 19980922 00002 NM 1998 9 22 VJ9800296 1 19980823 A 3350 6104789 BATTERY PACK BOEING 737 737214 138446R NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 460AT 20158 RT FUSELAGE EXTERNAL OVERWING EMERGENCY LIGHT FOUND INOPERATIVE DURING LAYOVER CHECK. REPLACED BATTERY PACK. 2 L 7 2 4F A16WE 1998092200003 19980922 00003 1998 9 22 VJ9800299 4 19980825 A 2565 11331 SLIDE DOUG DC9 DC932 3022066 WP R-1 DOOR INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 R-1 DOOR EVAC SLIDE ILLUMINATION LIGHTS DID NOT COME ON WHEN MX CHECKING SLIDE AFTER DEPLOY. PULLED LANDYARD AND LIGHT CAME ON. REPLACED THE SLIDE ASSY. 2 L 7 2 4F A6WE 1998092200004 19980922 00004 WP 1998 9 22 VJ9800300 1 19980825 A 3350 60030431 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 967VV 47170 CEILING EMERGENCY LIGHTS INOP AT MID CABIN. REPLACED THE CEILING LIGHT BATTERY PACK ASSY. 2 L 7 2 4F A6WE 1998092200005 19980922 00005 NM 1998 9 22 CALA9801537 1 19980826 A 3234 1030875 SOLENOID BOEING 737 737222 1384473 NM CONTROL LEVER INOPERATIVE A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 10236 19937 THE LANDING GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION TO UP UNLESS OVERRIDE TRIGGER WAS PULLED AFTER TAKEOFF. MAINTE NANCE FOUND THE LANDING GEAR CONTROL LEVER LOCK SOLENOID AT FAULT. THE LEVER LOCK SOLENOID WAS REMOVED AND REPLACED IAW MM 32-31-31. IN ADDITION, THE AIR/GROUND SAFETY SENSORS WERE ADJUSTED IAW MM 32-09-200. A FULL GEAR RETRACTION WAS PE RFORMED IAW MM 32-32-0 WITH ALL INDICATIONS AND GEAR HANDLE OPERATING NORMALLY. 2 L 7 2 4F A16WE 1998092200006 19980922 00006 WP 1998 9 22 9810001155 1 19980827 A 5320 WEB DOUG DC10 DC1040 3023508 WP BS 1701 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 155US 46764 DURING M-CHECK, FOUND CRACK IN WEB UPPER STRUCTURE IN LOWER RADIUS. REPLACED WEB DOUBLER PER EA 11-159807. 2 L 7 3 4F A22WE 1998092200007 19980922 00007 WP 1998 9 22 MWEA98937 1 19980817 A 5720 9910009 TEE CAP DOUG DC9 DC914 3022034 WP WS 585 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 LEFT SIDE TEE CAP REPLACEMENT AT STATION XCW 58 5. MTC REMOVED AND REPLACED LEFT TEE CAP. 2 L 7 2 4F A6WE 1998092200009 19980922 00009 NM 1998 9 22 P2EA98125 1 19980702 A 5311 FRAME BOEING 737 737222 1384473 NM BS 685 MISREAMED A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 208AU 19547 SJO - AT A/C'S LAST C-CHECK, THE FRAME FITTING AT BS 685 LEFT WAS MISREAMED. BOEING APPROVED RETURN TO SERVICE PENDING REPLACEMENT AT NEXT SCHEDULED C-CHECK. A NON-ROUTINE WORK CARD WAS ISSUED TO ACCOMPLISH REPLACEMENT. FRAME FITTING REP LACEMENT ACCOMPLISHED AS PER COOPESA EO NR C00-3-53-338-98 AND BOEING FAX NR C00-SJO-98-0438RR. (M) 2 L 7 2 4F A16WE 1998092200010 19980922 00010 NE 1998 9 22 DLL17981774 2 19980827 A 7200 ENGINE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 SO 27 769DL 63719 193H1218 014776 NR 2 ENG 2.6 VIBES ON TAKEOFF FOR APPROX 30 SECONDS, VIBES 2.2 ON CLIMBOUT. ON DESCENT, PULLED THROTTLE BACK 3.0 VIBES. SHUTDOWN ENG IN ACCORDANCE WITH ABNORMAL CHECKLIST. REPLACED ENGINE. 2 L 7 3 4F 4 F A23WE E12EU 1998092200011 19980922 00011 EU 1998 9 22 QXEA9801165 1 19980806 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WS 4837.5 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 498US 11181 CRACKED Z STRINGER, LEFT WING, FUEL PANEL 73B, STATION 4837.5, STRINGER 2.13. REPAIRED IAW HORIZON AIR EA 4-57-155. 2 L 7 2 4F RT A20EU 1998092200012 19980922 00012 NM 1998 9 22 98UAL900405 1 19980821 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 153UA 20102 THREE EMERGENCY EXIT SIGNS ABOVE AND AROUND DOOR 1 LEFT IS INOP. REPLACED BATTERY PACK, OP CK OK. 2 L 7 4 4F 4 F A20WE E20EA 1998092200013 19980922 00013 NM 1998 9 22 98UAL900411 1 19980825 A 3020 ANTI-ICE VALVE BOEING 777 777222 1385219 NM PWA 4084 PW4084 NE LT ENGINE OUT OF POSITION A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 785UA 26954 EN ROUTE, CREW GOT INDICATION OF LEFT ENGINE ANTI-ICE VALVE IN CLOSE POSITION. AIRCRAFT DIVERTED TO ORD. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998092200014 19980922 00014 WP 1998 9 22 ARWA980908 2 19980727 A 7261 779606 VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE INOPERATIVE A ARWA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 8968U 46069 NR 3 ENGINE AT IDLE, OIL PRESS 35 PSI, SHUT DOWN ENG, OIL PRESS LIGHT CAME ON. REMOVED AND REPLACED NR 3 ENG OIL PRESS RELIEF VALVE, OPS CHECKED NORMAL IAW 79-32-0. 2 L 7 4 4F 4 F 4A25 1E8 1998092500001 19980925 00001 NM 1998 9 25 TSAA9833508 1 19980809 A 3350 86210066 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 809AL 21720 REPLACED BATTERY IN NR 4 POSITION FLOOR PROXIMITY LIGHT ASSY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F A16WE 1998092500002 19980925 00002 NM 1998 9 25 98ZZZX3400 1 19980826 A 3350 LIGHT 58791 BOEING 727 727225 1384077 NM CABIN INOPERATIVE A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 889MA 21854 ON PRE-FLIGHT TRANSIT, FOUND EPL LIGHT INOPERATIVE FROM ROWS 1-4; ALSO, L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. TROUB LESHOT SYSTEM. FOUND POWER CABLE ASSEMBLY SHORTED. REPLACED CABLE, OPS CHECK GOOD IAW 33-50-01. 2 L 7 3 4F A3WE 1998092500003 19980925 00003 EA 1998 9 25 MASA98165 1 19980827 A 3350 GE1317 BULB BRUCE BC50335902 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77181 7181 WHILE PERFORMING ROUTINE MAINTENANCE, FOUND THE AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB, OPS CHECKED GOOD. (X) 2 L 7 2 4F RT A21EA 1998092500004 19980925 00004 EA 1998 9 25 MASA98166 1 19980828 A 3350 C2233 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5766 - PHL-STL - PRIOR TO DEPARTURE, THE CREW NOTICED THE MIDDLE CEILING EMERGENCY LIGHT WAS INOP. MAINTENANCE DEFE RRED THE ITEM PER MEL 33-51-1 AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1998092500005 19980925 00005 CE 1998 9 25 MASA98167 1 19980830 A 5260 101514076011 LATCH 1294000441 BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR DIRTY A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 93ZV UE93 HII/IFP - FLT 5021 - CAPTAIN CLOSED MAIN PASSENGER DOOR AND NOTED THE CABIN DOOR ANNUNCIATOR STAYED ILLUMINATED. FURTHE R INVESTIGATION SHOWED THE PASSENGER DOOR WAS NOT LOCKING PROPERLY. AIRCRAFT FERRIED TO PHX WHERE THE DOOR LATCH MECHAN ISM WAS CLEANED AND LUBED. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998092500006 19980925 00006 NM 1998 9 25 ASAA9810049 1 19980709 A 3350 6005401 BATTERY GRIMES BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE LT AND RT AFT EMERGENCY EXIT STROBE LIGHTS REMAINED ILLUMINATED AFTER LIGHTS WERE TU RNED OFF. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1998092500007 19980925 00007 NM 1998 9 25 ASAA9810050 1 19980714 A 3350 6005401 BATTERIES GRIMES BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND DIM, R2 DOOR EMERGENCY EXIT IDENTIFIER W AS FOUND INOPERATIVE, AND THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED R1 AND R2 DOOR EMERGEN CY EXIT IDENTIFIER BATTERIES AND THE SMOKE BARRIER LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTR OL NR 98ZZZX3401. (X) 2 L 7 2 4F RT A16WE 1998092500008 19980925 00008 NM 1998 9 25 98ZZZX3401 1 19980714 A 3350 8731002142 LIGHT INTVLV BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 SEA - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT IDENTIFIER WAS FOUND DIM, R2 DOOR EMERGENCY EXIT IDENTIFIER W AS FOUND INOPERATIVE, AND THE SMOKE BARRIER EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED R1 AND R2 DOOR EMERGEN CY EXIT IDENTIFIER BATTERIES AND THE SMOKE BARRIER LIGHT ASSEMBLY. ALL LIGHTS OPERATED NORMALLY. REF: OPERATOR CONTR OL NR ASAA9810050. 2 L 7 2 4F RT A16WE 1998092500009 19980925 00009 WP 1998 9 25 ASAA9880159 1 19980824 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 947AS 53020 SEA - PRIOR TO DEPARTURE OF FLT 622, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED BROKEN WIRE IN FLOOR TRACK AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1998092500010 19980925 00010 1998 9 25 HALA9800297 4 19980822 A 3444 INDICATOR DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A HALA K NONE O OTHER NR NOT REPORTED 1 WP 13 152AA 46707 LAX - FLT 10 - (LOG PAGE 4411752) - CAPTAIN'S RADIO ALTIMETER CYCLES DOWN TO 2500-1500 FEET DURING CLIMB AND CRUISE. OF F FLAG APPEARS IF READ-OUT STAYS AT 25-1500 FOR A FEW SECONDS, OFF FLAG FINALLY STAYED ON FOLLOWED BY GPWS AND WIND SHE AR FAIL LIGHTS. CYCLED R/A CB RESTORED R/A AND GPWS/WINDSHEAR SYSTEMS. R/A CONTINUED TO CYCLED. (X) 2 L 7 3 4F A22WE 1998092500011 19980925 00011 NM 1998 9 25 UIEA9803 1 19980731 A 7722 PROBE BOEING 747 747243B 1384830 NM NR 4 ENGINE MISSING A UIEA K NONE O OTHER IN INSP/MAINT 1 EA 15 516MC 58454 22507 DURING MAINTENANCE SERVICE AT MIA, DISCOVERED THE EGT PROBE AND WELDED BOSS AT THE 12 O'CLOCK POSITION ON NR 4 ENGINE CA SE NEAR THE AFT ENGINE MOUNT WAS MISSING. EXHAUST AIR ESCAPING THROUGH THE RESULTING HOLE IN THE CASE CAUSED DAMAGE TO THE AREA AND STRUT. THERE WERE NO FIRE WARNING DISCREPANCIES DOCUMENTED IN THE AIRCRAFT MAINTENANCE LOG. REQUESTED BOE ING SURVEY TEAM TO EXAMINE ENGINE/PYLON. BOEING DETERMINED THAT PYLON CHANGE WAS REQUIRED. PYLON S/N OFF RN 000124, S/ N ON RN 000265, ENGINE S/N OFF 517718, S/N ON 517589. (X) 2 L 7 4 4F A20WE 1998092500012 19980925 00012 NM 1998 9 25 USAA980348 1 19980824 A 5311 65465251 FRAME BOEING 737 737401 1384701 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND A SMALL CRACK .250 INCH AT RIVET HOLE FUSELAGE FRAME 380 BETWEEN S8L AN D S9L. CUT OUT DAMAGED AREA AND REPAIRED WITH FILLER AND DOUBLER PER SRM 53-00-07 FIG 202. (X) 2 L 7 2 4F RT A16WE 1998092500013 19980925 00013 EU 1998 9 25 USAA980361 1 19980825 A 5315 D28858003 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU CARGO BAY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 893US 15337 11373 PIT - DURING C-CHECK, FOUND TOP SURFACE CORRODED, 1 INCH BY 1 INCH AREA, FWD CARGO ENTRANCE FLOORBEAM. TEMPORARY REPAIR PER EA SBF100-51-009 AND T.R. 53-30-02. ITEM WAS FOUND ON C-CHECK 6-12-98. TEMPORARY REPAIR PER E.O. 49926 BEAM REPLA CED ON Q-CHECK PER SRM 8-21-98. (X) 2 L 7 2 4F RT 1998092500014 19980925 00014 EU 1998 9 25 USAAF98069 1 19980819 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 861US 11297 RIC - FOUND REAR FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (X) 2 L 7 2 4F RT 1998092500015 19980925 00015 EU 1998 9 25 USAAF98070 1 19980820 A 3350 6040681 BATTERY FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 889US 11358 GSO - FOUND FORWARD EMERENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY. (X) 2 L 7 2 4F RT 1998092500016 19980925 00016 EU 1998 9 25 C2XA98IA347 1 19980904 A 3350 NSA931320100 CIRCUIT BREAKER AEROSP ATR42 ATR42500 EU COCKPIT TRIPPED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE RESET THE ASSO CIATED CIRCUIT BREAKER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998092500018 19980925 00018 CE 1998 9 25 98ZZZX3402 1 19980821 A 6123 3037G83 LINE BEECH 1900 1900D 1154162 CE RT ENGINE CRACKED A JJBA O OTHER O OTHER AP APPROACH 1 EA 01 854CA UE60 RT PROPELLER WENT INTO FEATHER ON APPROACH. CRACKED P3 DELIVERY LINE. REPLACED RT P3 DELIVERY LINE. 2 L 7 2 4T RT A24CE 1998092500019 19980925 00019 EU 1998 9 25 C2XA98BT058 1 19980809 A 7312 10718DAF FUEL HEATER AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE NR 2 BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69901 14261 1165 127046 379 127046 BTV - DURING 2A INSPECTION, PLANNING REQUESTED THE NR 2 ENGINE FUEL/OIL HEATER FILTER BE TIME-CHANGED. DURING REMOVAL O F BOWL AND FILTER, FOUND STUD BROKEN ON FILTER BOWL. REMOVED AND REPLACED FUEL/OIL HEATER ASSEMBLY. OPS AND LEAK CHECK S GOOD. (X) 2 H 7 2 4T 4 T RT A53EU E20NE 1998092500020 19980925 00020 NM 1998 9 25 TSAA9727491 1 19980904 A 2761 654456114 ACTUATOR BOEING 737 737297 1384480 NM NR 3 SPOILER LEAKING A TSAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 WP 13 726AL 22426 OGG/HNL - FLT 69 - ON DESCENT FROM OGG, HAD TOTAL LOSS OF A-SYSTEM HYDRAULIC PRESSURE. QUANTITY SHOWED ZERO. ACCOMPLIS HED A-SYSTEM LOSS CHECK LIST. DECLARED EMERGENCY WITH ATC. FOUND NR 3 SPOILER ACTUATOR LEAKING. REMOVED AND REPLACED NR 3 SPOILER ACTUATOR IAW MM 27-61-51. OPS AND LEAK CHECK OK. REPLENISHED FLUID IN HYDRAULIC SYSTEM. INSPECTED AND RE PLACED 'A' CASE DRAIN AND 'B' CASE DRAIN FILTERS. RAN ENGINES. LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998092500021 19980925 00021 NM 1998 9 25 TSAA9833490 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LED'S BEING INOPERABLE. OPS CHECK GOOD. AIRACRAFT RET URNED TO SERVICE. (X) 2 L 7 2 4F A16WE 1998092500022 19980925 00022 NM 1998 9 25 TSAA9833489 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK ASSY DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (X) 2 L 7 2 4F RT A16WE 1998092500023 19980925 00023 NM 1998 9 25 TSAA9833463 1 19980817 A 5311 FRAME BOEING 737 7372S5C 1384499 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 AFT CARGO DOORWAY AFT FRAME CRACKED AT RIVET HOLE AND SEPARATING FROM INTERNAL DOUBLER. REPLACED DOUBLER, INSTALLED WEB AND SCUFF PLATE IAW ECO 1474R6. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X) 2 L 7 2 4F RT A16WE 1998092500024 19980925 00024 NM 1998 9 25 TSAA9833462 1 19980817 A 5311 FRAME BOEING 737 7372S5C 1384499 NM BS 420 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FORWARD CARGO COMPARTMENT LOWER LOBE FRAME CRACKED AT BS 420 BETWEEN S21L AND S22L. INSTALLED REPAIR CHANNEL PER SRM 53 -10-4 PAGE 2B. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X) 2 L 7 2 4F RT A16WE 1998092500025 19980925 00025 NM 1998 9 25 TSAA9833464 1 19980817 A 5751 654645423 AILERON BOEING 737 7372S5C 1384499 NM LT WING CRUSHED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 LEFT AILERON BOTTOM SIDE HAS DENT AND A LARGE SMASH NOTED. REPLACED LT AILERON IAW MM CHAPTER 27-11-0. OPERATIONAL CHE CK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X) 2 L 7 2 4F RT A16WE 1998092500026 19980925 00026 NM 1998 9 25 TSAA9833465 1 19980817 A 7830 1061813 THRUST REVERSER BOEING 737 7372S5C 1384499 NM LT ENGINE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FOUND 2.5 INCH CRACK IN THRUST REVERSER PIPE AT 9 O'CLOCK POSITION. CRACK WELDED IAW BOEING OVERHAUL MANUAL 78-38-43. A IRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X) 2 L 7 2 4F RT A16WE 1998092500027 19980925 00027 NM 1998 9 25 TSAA9833 1 19980831 A 3350 86210066 BATTERY PACK BOEING 737 737297 1384480 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 726AL 22426 REPLACED NR 3 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERV ICE. TAT: 38,602.1 HOURS. TAC: 74,295. (X) 2 L 7 2 4F A16WE 1998092500028 19980925 00028 NM 1998 9 25 TSAA9833475 1 19980827 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK ASSY DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (X) 2 L 7 2 4F RT A16WE 1998092500029 19980925 00029 NM 1998 9 25 TSAA9833476 1 19980829 A 3350 873100151 LIGHT BOEING 737 7372S5C 1384499 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 2 POSITION EMERGENCY FLOOR PROXIMITY LIGHT DUE TO BEING INOPERATIVE. REPLACED LIGHT ASSY. AIRCRAFT RETURNED TO SERV ICE. (X) 2 L 7 2 4F RT A16WE 1998092500030 19980925 00030 NM 1998 9 25 TSAA9833477 1 19980829 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 1 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO BEING INOPERATIVE. REPLACED BATTERY PACK. AIRCRAFT R ETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998092500031 19980925 00031 NM 1998 9 25 98ZZZX3403 1 19980804 A 3350 GE1312 LIGHT BOEING 727 727222 1384073 NM CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 7643U 20037 IND - FLT 738 - EMERGENCY EXIT LIGHTS INADEQUATE. RE-LAMPED EXIT LIGHTS. (X) 2 L 7 3 4F A3WE 1998092500032 19980925 00032 WP 1998 9 25 98ZZZX3404 1 19980812 A 3610 ASM0005511 DUCT DOUG DC10 DC1010 3022110 WP NR 1 ENGINE BROKEN A RYNA O OTHER J WARNING INDICATION DE DESCENT 1 CE 07 572SC 46977 SF/OGG - FLT 0007 - ON DESCENT, FIRE WARNING ON NR 1 ENGINE. THROTTLE TO IDLE WARNING WENT OUT. HIGH PRESSURE BLEED CO NTROL T-DUCT FLANGE AND THRUST REVERSER CROSS-OVER DUCT BROKEN AND LEAKING. REPAIRED BOTH DUCTS. OPERATIONAL CHECK WER E NORMAL. (X) 2 L 7 3 4F A22WE 1998092500033 19980925 00033 NE 1998 9 25 98ZZZX3405 2 19980726 A 7314 371900 PUMP BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 2 ENGINE FAILED A RYNA E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION DE DESCENT 1 CE 07 428EX 19097 654150 PHX/SAN - FLT 619 - AIRCRAFT WAS DIVERTED TO ONT DUE TO WEATHER. ON DESCENT, NR 2 ENGINE BECAME INOPERATIVE. REMOVED A ND REPLACED NR 2 ENGINE DRIVEN FUEL PUMP. 2 L 7 3 4F 4 F A3WE E2EA 1998092500034 19980925 00034 NM 1998 9 25 98ZZZX3406 1 19980531 A 2910 24060600480 LINE BOEING 727 72722C 138400F NM HYDRAULIC SYS RUPTURED A RYNA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CE 07 426EX 19089 IND/RIC - FLT 612 - DIVERTED TO ORF DUE TO LOSS OF HYDRAULIC QUANTITY AND PRESSURE IN THE B-SYSTEM. REMOVED AND REPLACE D HYDRAULIC LINE. SERVICED HYDRAULICS AND BLED SYSTEM OF AIR. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F A3WE 1998092500035 19980925 00035 NM 1998 9 25 98ZZZX3407 1 19980819 A 2612 182523252025 FIRE LOOP WHITTAKER BOEING 727 727222 1384073 NM NR 1 ENGINE FAILED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 7645U 20039 DAY - FLT 0144 - AFTER TAKEOFF, NR 1 FIRE WARNING CAME ON AND BELL, RETURNED TO DAY. REMOVED AND REPLACED NR 1 ENGINE F IRE LOOP. 2 L 7 3 4F A3WE 1998092500036 19980925 00036 EU 1998 9 25 C2XA98IA351 1 19980908 A 5320 S53971402218 SPLICE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE CENTER SPLICE ON THE KEEL BEAM WAS FOUND CORRODED ON THE RIGHT SIDE. MAINTENANCE P ERFORMED A DOUBLER REPAIR IAW ATR42 SRM'S 51-25-04, 51-21-42, 51-24-00, AND 51-21-28, AND THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. TOTAL HOURS: 23,206.6. TOTAL CYCLELS: 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500037 19980925 00037 EU 1998 9 25 C2XA98IA352 1 19980908 A 5320 S53672409218 ANGLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE REINFORCEMENT ANGLE AT FRAME 40 LEFT WAS FOUND CORRODED AT A NUTPLATE. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01037, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. TOTAL HOURS: 23,206.6. TOTAL CYCLES: 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500038 19980925 00038 EU 1998 9 25 C2XA98IA353 1 19980908 A 5315 S53672408202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE RIGHT BEAM WAS FOUND CORRODED AROUND A NUTPLATE AT AT FRAME 39. MAINTENANCE PERFOR MED A DOUBLER REPAIR IAW ATR42 SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TOTAL HOURS: 23,206. 6 HOURS. TOTAL CYCLES: 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500039 19980925 00039 EU 1998 9 25 C2XA98IA354 1 19980908 A 5320 S52176406210 ANGLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR STEP FRAME UPPER AFT CORNER WAS FOUND CRACKED. MAINTENANCE REPAIRED THE TREAD SUPPORT ANGLE IAW ATR42 SRM 52-11-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TOTAL HOURS: 23, 206.6. TOTAL CYCLES: 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500040 19980925 00040 EU 1998 9 25 C2XA98IA357 1 19980908 A 5320 S533712230110000 FITTING AEROSP ATR42 ATR42320 8680930 EU FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE FORWARD CARGO DOOR LATCH FITTING WAS FOUND TO HAVE DEEP GOUGES. MAINTENANCE REMOVE D AND REPLACED THE LATCH FITTING IAW ATR42 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TOTAL HOU RS: 23,206.6. TOTACL CYCLES: 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500041 19980925 00041 EU 1998 9 25 C2XA98IA356 1 19980908 A 5320 S52176406202 ANGLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE CENTER STEP ANGLE FOR THE BOTTOM STEP OF THE PASSENGER DOOR WAS FOUND CRACKED. MAI NTENANCE INSPECTED THE ANGLE AND FOUND THE CRACK TO TERMINATE IN A SCREW HOLE. MAINTENANCE PERFORMED A DOUBLER REPAIR I AW ATR 42 SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TOTAL HOURS: 23,206.6 HOURS. TOTAL CYCLES : 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500042 19980925 00042 EU 1998 9 25 C2XA98IA355 1 19980908 A 5320 S52176406202 ANGLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR STEP FRAME FOR PANEL 834DZ WAS FOUND CRACKED BEHIND THE AFT CENTER N UTPLATE. MAINTENANCE STOP-DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW ATR42 SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TOTAL HOURS: 23,206.6. TOTAL CYCLES: 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500043 19980925 00043 SO 1998 9 25 C2XA98IA330 1 19980908 A 5720 12017063011 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 2 AT RIB 22 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919. 5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500044 19980925 00044 SO 1998 9 25 C2XA98IA329 1 19980908 A 5720 12017062013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 3 AT RIB 22 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500045 19980925 00045 SO 1998 9 25 C2XA98IA328 1 19980908 A 5720 12017062006 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 2 AT RIB 21 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919. 5 HOURS. TC: 23,160. 9X) 2 L 7 2 4T RT A31SO 1998092500046 19980925 00046 SO 1998 9 25 C2XA98IA327 1 19980908 A 5411 12007893001 FRAME EMB 120 EMB120RT SO LT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE OUTBOARD AFT MAIN LANDING GEAR DOOR, AFT HINGE POINT FORWARD FRAME C RACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB-120 SRM 54-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERIVCE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500047 19980925 00047 SO 1998 9 25 C2XA98IA326 1 19980908 A 5713 120168085001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER STR 10 CRACKED IN CENTER WING DRY BAY. MAINTENANCE REMOVED AND R EPLACED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECR) EC5710-010 10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500048 19980925 00048 SO 1998 9 25 C2XA98IA325 1 19980908 A 5411 12007890002 FRAME EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE INBOARD AFT MAIN LANDING DOOR, FORWARD HINGE POINT FRAME CRACKED. M AINTENANCE STOP-DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 54-20-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500049 19980925 00049 EU 1998 9 25 C2XA98IA359 1 19980908 A 5320 S533712230110000 FITTING AEROSP ATR42 ATR42320 8680930 EU FUSELAGE GOUGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE AFT CARGO DOOR LATCH FITTING WAS FOUND TO HAVE DEEP GOUGES. MAINTENANCE REMOVED AN D REPLACED THE LATCH FITTING IAW ATR 42 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 23,206. 6. TOTAL CYCLES: 25,658. (X) 2 H 7 2 4T RT A53EU 1998092500050 19980925 00050 SO 1998 9 25 C2XA98IA339 1 19980908 A 5320 12004449001 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD T-PROFILE AT FRAME 36 CORRODED. MAINTENANCE REMOVED AND REPLACED TH E T-PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,1 60. (X) 2 L 7 2 4T RT A31SO 1998092500051 19980925 00051 SO 1998 9 25 C2XA98IA338 1 19980908 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TR ACK IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500052 19980925 00052 SO 1998 9 25 C2XA98IA337 1 19980908 A 5320 12027929001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FLOORBEAM CORRODED FROM FRAMES 36 TO 38. MAINTENANCE REMOVED AND RE PLACED THE BUTT-STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500053 19980925 00053 SO 1998 9 25 C2XA98IA336 1 19980908 A 5320 12027929001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FLOORBEAM CORRODED FROM FRAMES 33 TO 36. MAINTENANCE REMOVED AND RE PLACED THE BUTT-STRAP IAW EMB-20 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. T C: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500054 19980925 00054 SO 1998 9 25 C2XA98IA335 1 19980908 A 5320 12037024601 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND AFT CARGO DOOR THRESHOLD BUTT-STRAP CORRODED FROM FRAMES 39 TO 44. MAINTENANCE R EMOVED AND REPLACED THE BUTT-STRAPP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12 ,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500055 19980925 00055 SO 1998 9 25 C2XA98IA334 1 19980908 A 5320 12034416001 SUPPORT EMB 120 EMB120RT SO COCKPIT CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INPSECTION, FOUND LEFT SIDE SKIN SUPPORT AT FRAME 9 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23, 160. (X) 2 L 7 2 4T RT A31SO 1998092500056 19980925 00056 SO 1998 9 25 C2XA98IA332 1 19980908 A 5320 12004149001 TEE EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE OUTBOARD T-PROFILE AT FRAME 38 CORRODED. MAINTENANCE REMOVED AND REPL ACED THE T-PROFILE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC : 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500057 19980925 00057 SO 1998 9 25 C2XA98IA333 1 19980908 A 5320 12004416002 SUPPORT EMB 120 EMB120RT SO COCKPIT CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE SKIN SUPPORT AT FRAME 9 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23 ,160. (X) 2 L 7 2 4T RT A31SO 1998092500058 19980925 00058 SO 1998 9 25 C2XA98IA331 1 19980908 A 5720 12017062013 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURINC C-CHECK INSPECTION, FOUND LEFT WING UPPER SKIN SUPPORT BRACKET NR 1 AT RIB 21 CRACKED. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919. 5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500059 19980925 00059 SO 1998 9 25 C2XA98IA345 1 19980908 A 5315 12006157007 FLOORBEAM EMB 120 EMB120RT SO CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT OUTBOARD FLOORBEAM CORRODED FROM FRAMES 44 TO 47. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500060 19980925 00060 SO 1998 9 25 C2XA98IA344 1 19980908 A 5315 12006159501 FLOORBEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT OUTBOARD FLOORBEAM CORRODED FROM FRAMES 38 TO 44. MAINTENANCE REMOVED AND REPLACED THE FLOORBEAM IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERIVCE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500061 19980925 00061 SO 1998 9 25 C2XA98IA343 1 19980908 A 5320 12006159001 BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RT INBOARD FLOOR SUPPORT OMEGA BEAM CORRODED AT FRAME 38. MAINTENANCE REMOVED TH E CORROSION AND INSTALLED A REPAIR DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5340 -01020. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. TT: 12,919.5 HOURS. TC: 23,160. (X) 2 L 7 2 4T RT A31SO 1998092500062 19980925 00062 WP 1998 9 25 TWAA9815001 1 19980916 A 3233 39281375001 ACTUATOR DOUG DC9 DC934 302207E WP NLG WORN A TWAA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CE 05 927L 48123 NOSE GEAR RED UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. RECYCLED LANDING GEAR, NO HELP. RETURNED TO STL. REPLAC ED THE NLG RETRACT ACTUATOR. CHECK-C 1-4-98 STL. 2 L 7 2 4F RT A6WE 1998092500063 19980925 00063 NM 1998 9 25 TWAA9815002 1 19980916 A 5754 SKIN BOEING 767 767231 1385131 NM RT LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 610TW 22573 DURING CHECK-C MAINT, FOUND RT WING NR 11 LE SLAT REPAIR LOOSE IN CENTER AREA, 1.5 IN BY 2.5 IN. REMOVED OLD REPAIR. R EMOVED 1 IN BY 3 IN DELAMINATION ON O/B END OF OLD REPAIR TO SKIN, AND REMOVED DAMAGED CORE. INSTALLED SKIN AND CORE RE PLACEMENT WITH HOT BOND REPAIR PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1998092500064 19980925 00064 WP 1998 9 25 VJ9800390 1 19980811 A 5720 TIP DOUG DC9 DC932 3022066 WP WS 536.8 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 AT WS XW536.8 ON LT WING TIP THERE IS A GOUGE IN THE TRAILING EDGE. BLENDED GOUGE AT STA 536.8 IAW DC-9 SRM 51-10-3. M AT LOSS 100 PERCENT AND OUT OF LIMITS IAW DC9 SRM 57-01 FIG 1. FABRICATED NEW SECTION OF T/E OUT OF 2024 T 3 .020 IAW DC9 SRM 57-31-3 AND 51-10-2. DRILLED, DEBURRED, REPAIR PART IAW DC9 SRM 51-10-4. TREATED AND PRIMED IAW SRM 51-10-3. I NSTALLED REPAIR SECTION OF T/E IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998092500065 19980925 00065 WP 1998 9 25 VJ9800391 1 19980811 A 5320 FRAME DOUG DC9 DC932 3022066 WP CARGO DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 AFT CARGO COMPARTMENT FWD CARGO DOOR FRAME HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-3, ON AFT CARGO COMP FWD DOOR FRAME FOUND TO BE OUT OF LIMITS IAW SRM 53-01 FIG 1, 53-11-3. FABBED NEW WEB REPAIR AND REPAIR DOUBLER, IAW SRM 51-10- 3. TREATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED WEB PANEL AND DOUBLER IAW SRM 53-05 PG 201 FIG 70. 2 L 7 2 4F A6WE 1998092500066 19980925 00066 WP 1998 9 25 VJ9800392 1 19980812 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 945-965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 LT O/B SEAT TRACK CHANNEL AND PRIOR SPLICE FASTENERS BETWEEN STA 945 TO 965 IN CABIN FOUND TO BE CORRODED. REMOVED SECT ION OF SEAT TRACK CHANNEL FROM STA 945 TO 965 LT, FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. CLEANED SUB FLOOR AND FLOORBEAM IAW SRM 51-10-3, MAT LOSS LESS THAN .001, WITHIN LIMITS IAW SRM 53-01 FIG 1. DRILLED, DEBURRED, COUNTERS UNK, ALODINED, PRIMED NEW SEAT TRACK AND SPLICE SEACTION IAW SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998092500067 19980925 00067 WP 1998 9 25 VJ9800393 1 19980813 A 5330 595591520 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 PANEL NR 2208A HAS CORROSION INSIDE EDGES. CORRODED PANEL NR 2208A WAS FOUND TO BE OUT OF LIMITS. RECEIVED NEW PANEL F ROM SUPPLY. DRILLED AND TRIMMED TO FIT. WORK ACCOMPLISHED IAW SRM 51-10-3, 51-01 FIG 1, 51-10-4 AND 51-02. 2 L 7 2 4F A6WE 1998092500068 19980925 00068 WP 1998 9 25 VJ9800394 1 19980815 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 870 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 AFT CARGO COMP STA 870 CORROSION ON FRAME LOWER LIP. REMOVED CORROSION IAW SRM 51-10-3. REMAINING FORMER AND FS 870 BE TWEEN STA 24 AND 25 RT, OUT OF LIMITS IAW SRM 53-01 FIG 1. REMOVED CORRODED FORMER AND FABBED 1 FORMER AND SPLICE PLATE IAW SRM 51-10-4. INSTALLED FORMER AND SPLICE IAW SRM 51-10-4. 2 L 7 2 4F A6WE 1998092500069 19980925 00069 WP 1998 9 25 VJ9800395 1 19980815 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 FLOOR SUPPORT STRUCTURE STA 996, 20 RT OF CL HAS EXFOLIATION CORROSION. CLEANED CORROSION IAW SRM 51-10-3. FOUND TO BE OUT OF LIMITS AND DUE TO EXCESSIVE CORROSION ON LENGTH OF FLOORBEAM CAP, PULLEYS BLOCKED SUPPORT STRUCTURE AND NUT PLAT ES REMOVED. FLOORBEAM CAP FABRICATED NEW BC-9 SRM 53-11-3. INSTALLED NEW BEAM CAP IAW SC-9 SRM 51-30-2 AND 51-30-5. R EINSTALLED ATTACHING HARDWARE AND FLOOR SUPPORT. 2 L 7 2 4F A6WE 1998092500070 19980925 00070 WP 1998 9 25 VJ9800396 1 19980816 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 389-401 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 FINGER DOUBLER, ANTENNA DOUBLER, AND NUT PLATE DOUBLER HAS SURFACE CORROSION FROM BS 3889 TO 401 BETWEEN STRINGERS 29R T O 28L. GAINED ACCESS BY REMOVING PLASTIC SHROUD, ANTENNA DOUBLER, SPACER DOME NUTS, FASTENERS. MECH REMOVED CORROSION FROM DOUBLER AND SPACER, BEYOND LIMITS ALSO ELONGATED HOLES. FABBED 1 ANTENNA DOUBLER, FABBED 1 ANTENNA SPACER DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED, INSTALLED ALL PARTS AND FASTENERS IAW DC-9 SRM 53-01 PG 4 FIG 1, 51-10-3, 51-30-2, 53-31-1 FIG 3. 2 L 7 2 4F A6WE 1998092500071 19980925 00071 WP 1998 9 25 VJ9800397 1 19980817 A 5320 CHANNEL DOUG DC9 DC932 3022066 WP BS 370-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 FWD CARGO COMPARTMENT INNER ATTACHING BRACKET IS CORRODED STA 370R TO 237R. REMOVED CORROSION FROM BS 237 TO 313, LONGE RON 27R AT LINER ATTACH BRACKET. MATERIAL LOSS WAS OUT OF LIMITS FROM BS 313 TO 370 AT LONGERON 27R. FABRICATED NEW SE CTION OF ATTACH BRACKET FROM 7075 .063. HEAT TREATED TO 7075 T6 IAW SRM 51-10-3, 51-10-2A, 53-01 FIG 1, 51-10-4, 51-30- 2. ASSEMBLED NEW ATTACH BRACKET TO ASSEMBLIES AND INSTALLED COMPLETED ASSY IAW SRM 51-30-2, AND 51-30-8. 2 L 7 2 4F A6WE 1998092500072 19980925 00072 WP 1998 9 25 VJ980399 1 19980817 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 934VV 47488 LT AFT BEAMS NUT PLATES HAVE CORROSION UNDER THEM AS MARKED WHEN VIEWED FROM ABOVE FLOOR. REMOVED FLOOR SUPPORT, REMOVE D NUT PLATES, FOUND U-CHANNEL WITHIN FLOOR SUPPORT TO BE CORRODED 90 PERCENT MAT LOSS, BEYOND LIMITS. FABRICATED REPAIR U-CHANNEL FOR 2024 T3 .050. DRILLED, DEBURRED, ALODINED, PRIMED, AND INSTALLED. INSTALLED NEW NUT PLATES AND REINSTAL LED FLOOR SUPPORT IAW SRM 53-01 FIG 2, 53-11-3, AND 51-10-2. 2 L 7 2 4F A6WE 1998092500073 19980925 00073 NM 1998 9 25 CALA9801771 1 19980915 A 5320 STRAP BOEING 727 727232 1384082 NM BS 1050 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND AFT CARGO PIT LT LOWER SIDE WALL PANEL STRAP CORRODED AT STA 1050. A NEW STRAP WAS INSTALLED IAW SRM 5 1-10-6. 2 L 7 3 4F A3WE 1998092500074 19980925 00074 NM 1998 9 25 CALA9801772 1 19980915 A 5400 CHANNEL BOEING 727 727232 1384082 NM NR 3 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1.75 INCH CRACK IN NR 3 ENGINE PYLON UPPER FIXED COWL FORWARD END U-CHANNEL. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998092500075 19980925 00075 NM 1998 9 25 CALA9801773 1 19980915 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1136, LBL 46. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-2, 5 1-10-2, 51-30-2, AND MM 51-20-12. 2 L 7 3 4F A3WE 1998092500076 19980925 00076 NM 1998 9 25 CALA9801774 1 19980915 A 5330 SKIN BOEING 727 727232 1384082 NM BS 380-451 DAMAGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 448 TO 451, STRINGER 25R, AND AT STA 380, STRINGER 23R. DOUBLERS WERE INSTALLED IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1998092500077 19980925 00077 NM 1998 9 25 CALA9801775 1 19980915 A 5230 SKIN BOEING 727 727232 1384082 NM CARGO DOOR IMPACTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO C-1 DOOR SKIN. DOUBLER WAS INSTALLED IAW SRM 52-00-3, FIGURE 4 AND ECRA 523 2-01004. 2 L 7 3 4F A3WE 1998092500078 19980925 00078 NM 1998 9 25 CALA9801776 1 19980915 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND STRINGER 23R CORRODED AT LOWER NOSE WHEEL WELL RT LAP SEAM STA 294.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3, FIGURE 1. 2 L 7 3 4F A3WE 1998092500079 19980925 00079 NM 1998 9 25 CALA9801777 1 19980915 A 5320 CHORD BOEING 727 727232 1384082 NM BS 351.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND SHEAR TIE T-CHORD CORRODED AT STA 351.5, BL 0, WL 148.5. THE T-CHORD WAS REMOVED AND A NEW T-CHORD WAS INSTALLED IAW SRM 51-10-02. 2 L 7 3 4F A3WE 1998092500080 19980925 00080 WP 1998 9 25 CALA9801778 1 19980915 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 259 & 265 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND TOP OF FUSELAGE AFT ADF LOOP ANTENNA MOUNTING SURFACE EXTERNAL SKIN CRACKED AT RT CENTER MOUNT HOLE, ST A 259 LONGERON 1R, BL 0 AND AT RT MOUNT HOLE, STA 265, LONGERON 1R, BL 0. BOTH CRACKS WERE .375 INCH LONG. THE CRACKED AREAS OF SKIN WERE CUT OUT. DOUBLERS WERE INSTALLED IAW SRM 53-04, FIGURE 29 AND 51-10-3. 2 L 7 2 4F A6WE 1998092500081 19980925 00081 NM 1998 9 25 CALA9801779 1 19980916 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 400 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FLOORBEAM CORRODED AROUND MOUNT HOLES AT STA 400, RBL 30. THE CORRODED AREA WAS CUT OUT IAW SRM 53-10- 8. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-10-8. 2 L 7 3 4F A3WE 1998092500082 19980925 00082 NM 1998 9 25 CALA9801780 1 19980916 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 348 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND SEAT TRACK CORRODED AT STA 348, LBL 24. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW S RM 53-10-5 AND 51-10-2. 2 L 7 3 4F A3WE 1998092500083 19980925 00083 NM 1998 9 25 CALA9801781 1 19980916 A 3350 3114981 SOCKET GRIMES BOEING 737 7373T0 1384582 NM CABIN CORRODED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 63305 23356 INSPECTION FOUND THE RT AFT DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. THE LIGHT SOCKET WAS REPLACED DUE TO CORROSION. 2 L 7 2 4F RT A16WE 1998092500084 19980925 00084 NM 1998 9 25 CALA9801782 1 19980916 A 5755 ANGLE BOEING 727 727232 1384082 NM NR 7 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A 1 INCH CRACK IN NR 7 SPOILER SUPPORT BRACKET SIDE BRACE ANGLE. A NEW ANGLE WAS INSTALLED IAW SRM 51- 30-2. 2 L 7 3 4F A3WE 1998092500085 19980925 00085 NM 1998 9 25 CALA9801783 1 19980916 A 5720 BRACKET BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A .5 INCH CRACK IN OUTBOARD ANGLE BRACKET UNDER J-BEAM AT RT WING NR 8 SPOILER. THE BRACKET WAS REMOVE D AND REPLACED IAW SRM 51-10-1 AND 51-30-2. 2 L 7 3 4F A3WE 1998092500086 19980925 00086 NM 1998 9 25 CALA9801784 1 19980916 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND RT ELEVATOR LOWER SKIN CORRODED JUST AFT OF OUTBOARD LEADING EDGE TIP WEIGHT. THE CORRODED SKIN WAS RE MOVED. NEW SKIN WAS INSTALLED IAW SRM 51-30-2 AND 51-40-5. 2 L 7 3 4F A3WE 1998092500087 19980925 00087 NM 1998 9 25 CALA9801785 1 19980916 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1065 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1065, STRINGER 28R. THE CORROSION WAS REMOVED AND FILLER AND DOUBLER WERE IN STALLED IAW SRM 51-40-3 AND 51-10-6. 2 L 7 3 4F A3WE 1998092500088 19980925 00088 NM 1998 9 25 CALA9801786 1 19980916 A 3350 BATTERY GRIMES BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND MAIN CABIN EMERGENCY LIGHT AT ROW 8 HAD A WEAK BATTERY. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IA W MM 33-50-00. 2 L 7 3 4F A3WE 1998092500089 19980925 00089 NM 1998 9 25 CALA9801787 1 19980916 A 5720 BEAM BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A .375 INCH CRACK IN LT WING TRAILING EDGE J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE CRACK WAS STOP DRIL LED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-02914 AND SRM 51-10-6. 2 L 7 3 4F A3WE 1998092500090 19980925 00090 NM 1998 9 25 CALA9801788 1 19980916 A 5755 BRACKET BOEING 727 727232 1384082 NM NR 7 SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND NR 7 SPOILER ATTACH SUPPORT BRACKET CORRODED. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51- 30-2. 2 L 7 3 4F A3WE 1998092500091 19980925 00091 NM 1998 9 25 CALA9801789 1 19980916 A 5752 652173623 SKIN BOEING 727 727232 1384082 NM LT AILERON TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND LT INBOARD AILERON TAB TRAILING EDGE SEPARATED IN TWO AREAS. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-11. 2 L 7 3 4F A3WE 1998092500092 19980925 00092 NM 1998 9 25 CALA9801790 1 19980916 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1090-1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND SEAT TRACK CORRODED AT FS 1090 TO 1130, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS IN STALLED IAW SRM 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998092500093 19980925 00093 WP 1998 9 25 CALA9801791 1 19980916 A 5320 MOUNT DOUG DC9 DC982 3022082 WP BS 598-617 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16893 49392 INSPECTION FOUND NR 1 RADIO ALTIMETER RECEIVER ANTENNA MOUNT LOCATED ON FUSELAGE BELLY BELOW MAIN BAGGAGE BIN AT STA 598 TO 617 CORRODED. THE ANTENNA MOUNT WAS REMOVED AND REPLACED IAW SRM 51-10-3. 2 L 7 2 4F A6WE 1998092500095 19980925 00095 NM 1998 9 25 CALA9801793 1 19980916 A 5753 FITTING BOEING 727 727224 1384076 NM RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND FITTING CORRODED WHERE RT WING NR 5 FLAP TRACK MOUNTS. THE FITTING AND BUSHING WERE REMOVED AND REPLAC ED IAW MM 32-11-51, PAGE 401 TO 403 AND MM 20-70-7. 2 L 7 3 4F A3WE 1998092500096 19980925 00096 SO 1998 9 25 COMA9810195 1 19980909 A 5320 12046158002 BUTTSTRAP EMB 120 EMB120RT SO NR 3 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 145-012 REVEALED RIGHT NR 3 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED A SERV ICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500097 19980925 00097 SO 1998 9 25 COMA9810196 1 19980909 A 5320 12027929003 BUTTSTRAP EMB 120 EMB120RT SO NR 4 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 4 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVIC EABLE PART USING EMB 120SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500098 19980925 00098 SO 1998 9 25 COMA9810197 1 19980909 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO NR 5 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVIC EABLE ONE USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500099 19980925 00099 SO 1998 9 25 COMA9810198 1 19980909 A 5320 12046158003 BUTTSTRAP EMB 120 EMB120RT SO NR 2 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 145-012 REVEALED LEFT NR 2 BUTTSTRAP TO BE CORRODED. REMOVED AND REPLACED BUTTSTRAP WITH SER VICEABLE ONE USING EMB 120 STANDARD PRATICES. 2 L 7 2 4T RT A31SO 1998092500100 19980925 00100 SO 1998 9 25 COMA9810199 1 19980909 A 5320 12005805003 BUTTSTRAP EMB 120 EMB120RT SO NR 1 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER NR 1 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500101 19980925 00101 SO 1998 9 25 COMA9810200 1 19980909 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO NR 5 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICE ABLE PART USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500102 19980925 00102 SO 1998 9 25 COMA9810201 1 19980909 A 5320 12005803001 SILL EMB 120 EMB120RT SO NR 1 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500103 19980925 00103 SO 1998 9 25 COMA9810202 1 19980909 A 5320 12005802001 SILL EMB 120 EMB120RT SO NR 1 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500104 19980925 00104 SO 1998 9 25 COMA9810203 1 19980909 A 5320 12006157005 SILL EMB 120 EMB120RT SO CARGO DOOR CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 163-012 REVEALED LEFT CARGO SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE USIN G EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500105 19980925 00105 SO 1998 9 25 COMA9810214 1 19980909 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO NR 5 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 151-012 REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICE ABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500106 19980925 00106 SO 1998 9 25 COMA9810205 1 19980909 A 5320 12004449002 CROSSBEAM EMB 120 EMB120RT SO FRAME 20 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK5310-131-01I REVEALED RT CROSSBEAM AT FRAME 20 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLE D SERVICEABLE CROSSBEAM USING EMB 120SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500107 19980925 00107 SO 1998 9 25 COMA9810206 1 19980909 A 5320 12006964001 CROSSBEAM EMB 120 EMB120RT SO FRAME 20 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED. REMOVED CROSSBEAM AND INSTALLED SER VICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500108 19980925 00108 SO 1998 9 25 COMA9810204 1 19980909 A 5320 12004449001 CROSSBEAM EMB 120 EMB120RT SO FRAME 23 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK5320-141-03I REVEALED LT CENTER CROSSBEAM AT FRAME 23 TO BE HEAVILY CORRODED. REMOVED CROSSBE AM AND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500109 19980925 00109 SO 1998 9 25 COMA9810207 1 19980909 A 5320 12004149002 CROSSBEAM EMB 120 EMB120RT SO FRAME 16 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM AND INST ALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500110 19980925 00110 SO 1998 9 25 COMA9810208 1 19980909 A 5320 12006962001 CROSSBEAM EMB 120 EMB120RT SO FRAME 16 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 18542 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED C ROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500111 19980925 00111 SO 1998 9 25 COMA9810209 1 19980909 A 5320 12014243001 CROSSBEAM EMB 120 EMB120RT SO FRAME 14 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LT CROSSBEAM AT FRAME 14 TO BE CORRODED. REMOVED CROSSBEAM AND INSTALL ED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500112 19980925 00112 SO 1998 9 25 COMA9810210 1 19980909 A 5320 12008896001 CROSSBEAM EMB 120 EMB120RT SO FRAME 16 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED RIGHT CENTER CROSSBEAM AT FRAME 16 TO BE CORRODED. REMOVED CROSSBEAM A ND INSTALLED SERVICEABLE CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500113 19980925 00113 SO 1998 9 25 COMA9810211 1 19980909 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO NR 5 CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 120228 DURING 2C INSEPCTION, TASK 151-012 REVEALED RIGHT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVIC EABLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500114 19980925 00114 SO 1998 9 25 COMA9810212 1 19980909 A 5320 12046963001 BUTTSTRAP EMB 120 EMB120RT SO LEFT CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT FORWARD BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500115 19980925 00115 SO 1998 9 25 COMA9810213 1 19980909 A 5320 12007089003 BUTTPLATE EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 248CA 120228 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. R EMOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998092500116 19980925 00116 SO 1998 9 25 COMA9810215 1 19980916 A 3350 1317 BULB EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 246CA 120223 1ST OVERHEAD EMERGENCY LIGHT IS INOP. REPLACED BULB. 2 L 7 2 4T RT A31SO 1998092500117 19980925 00117 EA 1998 9 25 COMA9860265 1 19980905 A 5753 601R1430341 VANE CNDAIR CL600 CL6002B19 EA LT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 979CA 7159 C-CHECK TASK 27-580-100, LT I/B FLAP VANE HAS CHAFE DAMAGE. REPLACED FLAP VANE. 2 L 7 2 4F RT A21EA 1998092500118 19980925 00118 EA 1998 9 25 COMA9860266 1 19980916 A 4930 M259882904 FUEL LINE CNDAIR CL600 CL6002B19 EA APU LEAKING A COMA A UNSCHED LANDING K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 976CA 7151 STRONG JET FUEL ODOR IN COCKPIT. REPAIRED LEAKING FUEL LINE CONNECTION AT THE APU. 2 L 7 2 4F RT A21EA 1998092500119 19980925 00119 EA 1998 9 25 COMA9860267 1 19980915 A 2450 ESS CNDAIR CL600 CL6002B19 EA E/E COMPT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 934CA 7042 AFTER TAKEOFF, ESS AUTO TRANSFER FAILED. COULD NOT DUPLICATE, OPERATIONAL CHECK OF AUTO TRANSFER WAS SATISFACTORY. 2 L 7 2 4F RT A21EA 1998092500120 19980925 00120 NM 1998 9 25 98FDEA00576 1 19980916 A 3610 1442M81G06 DUCT DOUG MD11 MD11F 3023600 NM NR 1 ENGINE BLOWN A FDEA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION TO TAKEOFF 1 SO 25 601FE 48401 NR 1 ENG FIRE WARN AND IND. SHUT ENGINE DOWN IAW CKLIST. DISCHARGED NR 1 FIRE BOTTLE. FOUND HIGH PRESSURE TURBINE COO L DUCT BLOWN. REMOVED AND REPLACED DUCT, NR 1 FIRE BOTTLE AND SQUIB. RAN ENGINE, LEAK CHECK GOOD. 2 L 7 3 4F RT A22WE 1998092500121 19980925 00121 NM 1998 9 25 98FDEA00577 1 19980916 A 2910 LINE BOEING 727 727227 1384078 NM A HYD SYST SPLIT A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 478FE 21395 SYS-A HYD FAILURE 5 MIN AFTER T/O QUAN AND PRESS ZERO. FLUID SHUTOFF SWITCH CLOSED. FOUND HYD LINE SPLIT ON A-SYS PRES S TRANSMITTER. REMOVED AND REPLACED SAME. NOTED 1 GAL FLUID IN A-SYS SERVICE TO FULL, RAN BOTH NR 1 AND NR 2 ENG. ALL SYS OPER CK NORM. RESAFTIED FLUID SHUTOFF SWITCH'S. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998092500122 19980925 00122 NM 1998 9 25 98FDEA00578 1 19980917 A 3260 BULB BOEING 727 72722 1384002 NM LANDING GEAR FAILED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 166FE 18863 SHORT FINAL RUNWAY 36R MEM, NORM GEAR EXT CREW OBSERVED NO DOWN GROUND IND ON LEFT MAIN GEAR. NOSE AND R/M IND DOWN NOR M. CAPT PERFORMED GO-AROUND AFTER RECYCLING GEAR TO NO AVAIL. DID MAN GEAR EXT CKLIST AND GOT VISUAL CONFIRMATION FROM TOWER. LANDED, PINNED GEAR AND TAXIED IN. INSP LEFT GEAR WELL, ALL SWITCH AND WIRING NORM. FOUND BULBS BURN OUT FOR LEFT GEAR IND. REMOVED AND REPLACED BULBS AND IND ON LEFT GEAR OPER NORM, OK FOR SERVICE. 2 L 7 3 4F A3WE 1998092500123 19980925 00123 NM 1998 9 25 98FDEA00580 1 19980917 A 3260 SWITCH BOEING 727 727247 138408F NM RT MLG DOOR DIRTY A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 236FE 21330 RIGHT GEAR DOOR LIGHT REMAINED ON AFTER GEAR RETRACTION. RAN RED TABS AND RECYCLE GEAR, DOOR LIGHT EXTINGUISHED. CLEAN ED RIGHT GEAR DOOR LIGHT SWITCH. OPERATED SEVERAL TIMES, OPER CHECKED NORMAL. 2 L 7 3 4F A3WE 1998092500124 19980925 00124 NM 1998 9 25 DL76L981906 1 19980910 A 2121 732591F FAN BOEING 767 767332 1382001 NM E/E COMPT MALFUNCTIONED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 187DN 27582 EQUIP COOLING OVERHEAT LIGHT ILLUMINATED AFTER T/O. STANDBY SELECTED, NO GOOD. OVRD SELECTED, NO COOLING LIGHT ILLUM. CREW NOTICED SOME ELECTRICAL SMELL. AIR TURNBACK TO MUC. BITE CHECKS ALL OK. EICAS MTC MSG FWD EQ SUPPLY FLOW DETECT OR. CLEANED SAME AND REMOVED AND REPLACED FWD EXHAUST FAN. ALL CHECKS GOOD. MCC FOLLOW-UP TO REMOVED AND REPLACED FWD EQUIP FLOW DETECTOR. 2 L 7 2 4F RT A1NM 1998092500125 19980925 00125 NM 1998 9 25 DL72L981909 1 19980912 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 THE FUSELAGE SKIN WAS FOUND WITH SEVERAL SMALL AREAS OF CORROSION AT THE S-26R LAP SPLICE BETWEEN FS 700 AND 720C. THE CORRODED AREAS WERE LOCALLY CUT OUT AND LOCAL REPAIR DOUBLERS WERE INSTALLED. THE REPAIRS WERE ACCOMPLISHED PER ER/ A 365577-14, REV C DATA ANALYSIS WILL BE ACCOMPLISHED WITHIN 12 MONTHS OF THE REPAIR. 2 L 7 3 4F A3WE 1998092500126 19980925 00126 NM 1998 9 25 DL72S981912 1 19980914 A 5320 WEB BOEING 727 727232 1384082 NM BS 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 REF A/C 495 TPA LTR CHECK C-1, VERTICAL WEB CRACKED .5 INCH LT SIDE LWR LIGHTENING HOLE STA 1228. REPAIRED PER MM 53-11 -0. 2 L 7 3 4F A3WE 1998092500127 19980925 00127 NM 1998 9 25 DLM88981913 1 19980914 A 3213 LUG 5935347511 DOUG MD88 MD88 3023688 NM RT MLG STRUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 953DL 9353477 49884 DURING COMPLETION OF TRANS 9T149AD, RT MLG INSPECTION FOUND RT MLG PISTON I/B LUG RADIUS CRACKED. REPLACED STRUT ASSY. 2 L 7 2 4F RT A6WE 1998092500128 19980925 00128 NM 1998 9 25 DLM88981914 1 19980911 A 5311 9919605501 FRAME DOUG MD88 MD88 3023688 NM BS 1271 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 998DL 53370 APPROX 13 OF THE FS 1271 LOWER FRAME WAS FOUND CORRODED BETWEEN L29L AND L29R. REPAIRED PER ERA 332208-14. 2 L 7 2 4F RT A6WE 1998092500129 19980925 00129 NM 1998 9 25 DLM88981915 1 19980911 A 5330 59114063 SKIN DOUG MD88 MD88 3023688 NM BS 216 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 998DL 53370 DENT FOUND IN FUSELAGE SKIN AT FS 211 TO FS 216 JUST BELOW L17L. REPAIRED PER ERA 332143-14. 2 L 7 2 4F RT A6WE 1998092500130 19980925 00130 NM 1998 9 25 DLM88981916 1 19980911 A 5330 5953050 SKIN DOUG MD88 MD88 3023688 NM BS 260 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 998DL 53370 DENT FOUND IN FUSELAGE SKIN AT FS 257 TO FS 265 BETWEEN L18L TO L19L. REPAIRED PER ERA 332142-14. 2 L 7 2 4F RT A6WE 1998092500131 19980925 00131 NM 1998 9 25 DLM88981917 1 19980911 A 5330 29525251 SKIN DOUG MD88 MD88 3023688 NM BS 1210 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 998DL 53370 SKIN AND BEARSTRAP AT THE AFT EDGE OF THE C3 DOOR CUTOUT WAS DAMAGED. DAMAGE IS LOCATED AT FS 1210, 12 ABOVE THE TANGEN T POINT AT THE LWR AFT CORNER. REPAIRED PER ERA 332210-14. 2 L 7 2 4F RT A6WE 1998092500132 19980925 00132 NM 1998 9 25 DL72S981918 1 19980915 A 5712 6483385 RIB BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 UPPER CHORD ANGLE OF THE LT WING RIB AT WS 171.5 WAS FOUND CRACKED. REPAIRED PER ERA 332223-14. 2 L 7 3 4F A3WE 1998092500133 19980925 00133 NM 1998 9 25 DL72S981919 1 19980915 A 3230 BALL NUT 10607441 BOEING 727 727232 1384082 NM NLG RUSTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 AT HMV, LANDING GEAR CHECK OUT THE NOSE GEAR EMERGENCY EXTENSION FAILED TO OPERATE DUE TO THE BALL NUT AND SCREW ASSY BE ING RUSTED AND FROZEN UP. REF IPC 32-31-00-06 ITEM 185 (P/N 10-60744-1). THE ASSY WAS REPLACED AND THE CHECK OUT COMPL ETED SATISFACTORY. 2 L 7 3 4F A3WE 1998092500134 19980925 00134 NM 1998 9 25 DL72W981920 1 19980915 A 5320 WEB BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 REF SHIP 588 TPA LTR CHECK B-2, .25 INCH CRACK AT LIGHTENING HOLE 8AFT OF LT AIRSTAIR UPSTOP PAD. ROUT OUT AND TREAT PER MM 53-11-0. 2 L 7 3 4F A3WE 1998092500135 19980925 00135 NM 1998 9 25 DL72L981922 1 19980915 A 3350 BATTERY PACK 334102487 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 509DA 21311 LAYOVER FOUND L-2 AND R-2 SLIDE EMERGENCY LIGHTS INOP. REPLACED M983 SLIDE LIGHT BATTERY PACK, OPN CKS OK. 2 L 7 3 4F A3WE 1998092500136 19980925 00136 NM 1998 9 25 DL757981923 1 19980915 A 3350 POWER SUPPLY BPS73 BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 655DL 5424 24395 2R DOOR EMERGENCY LIGHTS INOP. REPLACED PWR SUPPLY, OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998092500137 19980925 00137 WP 1998 9 25 DLL10981924 1 19980915 A 3350 POWER SUPPLY 516574 LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 714DA 37684 193C1090 F/C EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY, OPS CHECK NORMAL. 2 L 7 3 4F A23WE 1998092500138 19980925 00138 NM 1998 9 25 DHL98724002 1 19980915 A 2782 1U10957 ACTUATOR BOEING 727 727228 NM NR 7 SLAT FAILED A DHLA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 724DH 19862 WITH FLAP RETRACTED NR 7 SLAT LIGHT REMAINED ON BOTH ON THE FWD AND SECOND OFFICER PANEL. REPLACED NR 7 SLAT ACTUATOR AND SWITCH. 2 L 7 3 4F A3WE 1998092500139 19980925 00139 NM 1998 9 25 DHL98740005 1 19980915 A 2611 SMOKE LIGHT BOEING 727 7272Q9 138448M NM CARGO COMPT ILLUMINATED A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 740DH 21930 CARGO SMOKE DETECTOR LIGHT ON. RELAMPED ALL SMOKE DETECTORS. 2 L 7 3 4F RT A3WE 1998092500140 19980925 00140 WP 1998 9 25 CKSA98514 1 19980910 A 2612 WIRE DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE FAILED A CKSA E J ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 23 6161C 45856 644999 ON CLIMBOUT, NUMBER 1 ENGINE FIRE WARNING SOUNDED. DURING ENGINE SHUTDOWN THE LIGHT IN THE HANDLE EXTINGUISHED. ENGINE FIRE, SEPARATION, SEVERE DAMAGE CHECKLIST ACCOMPLISHED. AGENT WAS NOT DISCHARGED. OIL PRESSURE AT SHUTDOWN 5 PSI. AI RCRAFT FUEL DUMP ACCOMPLISHED. DUMPED APPROX 15,000 POUNDS. LANDED BELOW 240,000 POUNDS. REPAIRED WIRING AT AFT COWL FIRE WARNING LOOP, LEFT SIDE. OPS CHECK NORMAL IAW DC 8 MM 26-20; TIGHTENED NUTS AND BOLTS AT PRESSURE REGULATOR VALVE. PERFORMED LEAK CHECK IAW DC 8 MM 36-1-0, NO LEAKS NOTED. PERFORMED ENGINE RUN-UP IAW DC 8 MM 71-00-00. ALL SYSTEMS C HECKED NORMAL. NOTE: AT BLAST FENCE AT T/O POWER TILL MAX ALLOWABLE TIME. NO FIRE WARNING. 2 L 7 4 4F 4 F 4A25 1E8 1998092500142 19980925 00142 NM 1998 9 25 VNAA9809010 2 19980911 A 7320 3034652 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 457PS 3048 DURING THE TAXI FOR TAKEOFF, AN ECU FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE I NSPECTED AND REPLACED THE LEFT HAND ENGINE 1.8 SENSOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-21-02. OPERATIO NAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998092500143 19980925 00143 NM 1998 9 25 VNAA9809012 1 19980915 A 3243 AC69895 METERING UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT BRAKES FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 442JS 61094 89 3060 THE RIGHTHAND AND LEFTHAND BRAKES STARTED PULSATING, DURING TAXI AND WHEN STOPPED. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND REPLACED THE BRAKE METERING UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-42-03. OPER ATIONAL AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998092500144 19980925 00144 NM 1998 9 25 VNAA9809013 1 19980916 A 3411 0851GW PITOT HEAD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT FUSELAGE BIRD STRIKE A VNAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 07 426JS 84943 3038 JUST AFTER TAKEOFF DURING THE CLIMB, A BIRD STRUCK THE NUMBER TWO PITOT HEAD. THE AIRCRAFT RETURNED TO THE FIELD AND LA NDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO PITOT HEAD, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-11-04. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998092500145 19980925 00145 NE 1998 9 25 TWAA9815101 2 19980916 A 7200 ENGINE DOUG DC9 DC915 3022036 WP PWA JT8 JT8D7A 52053 NE LEFT BIRD STRIKE A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 490SA 45798 SHORTLY AFTER TAKEOFF, SMELLED INITIAL ODOR IN COCKPIT AND CABIN. RESEMBLED BURNING IN OVENS BUT MORE ACRID. LATER DES CRIBED AS CHEMICAL ELECTRICAL SMELL. FLT RETURNED TO STL. FOUND BIRD HAD BEEN INJESTED IN LT ENGINE AFFECTING THE PNEU MATIC SYSTEM. ACCOMPLISHED BIRD STRIKE INSPECTION. NO DAMAGE TO ENGINE. CHECK-C 9-5-97 STL. (X) 2 L 7 2 4F 4 F A6WE E2EA 1998092500146 19980925 00146 NM 1998 9 25 UPS98427686 1 19980918 A 3350 CONNECTOR BOEING 747 747212B 1384886 NM COCKPIT DIRTY A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 522UP 21936 SDF - EEL ABOVE ESCAPE DOOR IN COCKPIT INOPERABLE, NR 325 326. CLEANED CONNECTION, OPS CHECK NORMAL. (X) 2 L 7 4 4F A20WE 1998092500147 19980925 00147 EU 1998 9 25 QXEA9801293 1 19980911 A 4950 APU GTCP364A FOKKER F28 F28MK4000 4990810 EU CABIN SMOKING A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 496US 11167 PDX - AFTER TAKEOFF, THE LAV SMOKE DETECTOR SOUNDED AND CABIN FILLED WITH SMOKE. MAINTENANCE INSPECTED AND FOUND APU AT FAULT. ALSO FOUND OIL IN WATER SEPARATOR ON BOTH NR 1 AND NR 2 PACKS. 2 L 7 2 4F RT A20EU 1998092500148 19980925 00148 EU 1998 9 25 QXEA9801294 1 19980915 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 477AU 11226 GEG - ARROW IN EXIT SIGN OVER COCKPIT DOOR INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS GOOD. 2 L 7 2 4F RT A20EU 1998092500149 19980925 00149 EU 1998 9 25 QXEA9801295 1 19980915 A 3350 XB86484 SIGN FOKKER F28 F28MK4000 4990810 EU CABIN MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 487US 11238 PDX - EMERGENCY PATH LIGHTING COVER FOR 8D IS MISSING. MAINTENANCE REPLACED LIGHT ASSEMBLY. (X) 2 L 7 2 4F RT A20EU 1998092500150 19980925 00150 NM 1998 9 25 QXEA9801296 1 19980915 A 2420 BREAKER PANEL DHAV DHC8 DHC8102 2809003 NM COCKPIT SHORTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 NM 09 812PH 26 SEA - FLASH OF LIGHT AND ACRID SMELL IN COCKPIT ON SHORT FINAL. LIGHT SEEMED TO COME FROM NR 1 SIDE AFT AROUND BREAKER PANEL. INSPECTED UNDER CIRCUIT BREAKER PANELS, GROUND RAN AIRCRAFT, CHECKED AC AND DC ELECTRICAL SYSTEMS WHILE RUNNING. NO FAULT FOUND. OK FOR CONTINUED SERVICE. (X) 2 H 7 2 4T RT A13NM 1998092500151 19980925 00151 NM 1998 9 25 98FDEA00582 1 19980917 A 5320 FITTING BOEING 727 72725 1384006 NM BS 870 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 154FE 18287 DAL - NR 375 - DURING ACCOMPLISHMENT OF REPEAT INSPECTION PER BOEING SB 727-53-194, HOLE NR 1 WAS FOUND ELONGATED. LOCA TED AT BS 870 IN THE TERMINAL FITTING, LEFT SIDE. (X) 2 L 7 3 4F A3WE 1998092500152 19980925 00152 NM 1998 9 25 98FDEA0583 1 19980917 A 5320 65163517 FRAME BOEING 727 72725C 138400H NM E/E DOORWAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 PAE - NR 0546 - CORROSION (C53-100-010) ON E/E DOOR FRAME AT BS 423, RBL 4 - LBL 4, WL 148. (X) 2 L 7 3 4F A3WE 1998092500153 19980925 00153 WP 1998 9 25 ABXA9800828 1 19980917 A 5753 99576004 ANGLE DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE OUTBOARD INTERIOR ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SR M 51-30-1 AND SRM 51-30-2. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500154 19980925 00154 WP 1998 9 25 ABXA9800829 1 19980917 A 5330 5911408125 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DURING C-CHECK, FOUND NR 2 ADF LOOP ANTENNA AREA EXTERIOR FUSELAGE SKIN CRACKED AROUND HOLE FOR ANTENNA LEAD WIRE. REPAIRED SKIN IAW ABX REA D953-24811-MR. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500155 19980925 00155 WP 1998 9 25 ABXA9800830 1 19980917 A 5311 59114279 FRAME DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DURING C-CHECK, FOUND FUSELAGE FS 980 CRACKED AT LONGERON 17R. REPAIRED FRAME IAW DC9 SRM 53-03. ACFT TT: 49,25 8 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500156 19980925 00156 WP 1998 9 25 ABXA9800831 1 19980917 A 5315 991224355 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DURING C-CHECK, FOUND UPPER SURFACE OF FLOORBEAM STA 965 RBL 8.0 TO RBL 21 CORRODED. REPAIRED IAW DC9 SRM 51-10-3 2 AND DWG K05019. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500157 19980925 00157 WP 1998 9 25 ABXA9800832 1 19980917 A 5311 99115173 FRAME DOUG DC9 DC932 3022066 WP BS 180 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DURING C-CHECK, FOUND FUSELAGE FRAME AT STA 180 AND LONGERONS 22R- 27R CORRODED. REPAIRED FRAME IAW DC9 SRM 53-03 . ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500158 19980925 00158 WP 1998 9 25 ABXA9800833 1 19980917 A 5210 3917624517 FITTING DOUG DC9 DC932 3022066 WP LT VENTRAL DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DURING C-CHECK, FOUND LOWER LEFT VENTRAL DOOR STOP SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 AND SRM 51-30-5. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500159 19980925 00159 WP 1998 9 25 ABXA9800834 1 19980917 A 5320 991050313 WEB DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DURING C-CHECK, FOUND CUSP WEB CORRODED AT STA 965 BETWEEN RBL 44 ND RBL 54.5, IN LIGHTENING HOLE AREA BETWEEN STA 945 - STA 965. REPAIRED CUSP WEB IAW ABX REA D953-24862-MR. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500160 19980925 00160 WP 1998 9 25 ABXA9800835 1 19980917 A 5320 99105033 TEE DOUG DC9 DC932 3022066 WP BS 946/980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 939AX 47201 ILN - DUIRNG C-CHECK, FOUND CUSP TEE ANGLES AT LONGERON 18R AND STA 946 - STA 980 CORRODED ON LOWER SIDE. REPAIRED IAW DC9 SRM 53-05. ACFT TT: 49,258 HOURS. AIRCRAFT TOTAL CYCLES: 39,935. (X) 2 L 7 2 4F A6WE 1998092500161 19980925 00161 WP 1998 9 25 MWEA98962 1 19980915 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PASSENGER DOOR LOOSE A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 302ME 47102 MCO - FLT 90 - FORWARD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FWD ENTRY DOOR EVAC SLIDE COVER. (X) 2 L 7 2 4F A6WE 1998092500162 19980925 00162 1998 9 25 MWEA98963 4 19980915 A 2565 D29985107 SLIDE DOUG MD88 MD88 3023688 NM SERVICE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 701ME 0405 49760 MKE - FOUND AFT SERVICE DOOR EVACUATION SLIDE BACK CASING CRACKED. REMOVED AND REPLACED EVACUATION SLIDE. (X) 2 L 7 2 4F RT A6WE 1998092500163 19980925 00163 NM 1998 9 25 DHL98740006 1 19980915 A 3260 4030949906 CONTROL BOEING 727 7272Q9 138448M NM LT MLG SHORTED A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 740DH 21930 ON GEAR EXTENSION, LT MAIN LANDING GEAR (GREEN) LIGHT REMAINED EXTINGUISHED. SECONDARY LEFT MAIN LANDING GEAR LIGHT ON ENGINEER PANEL ILLUMINATED. FOUND MASTER DIMMNG C/B POPPED SEC NR 1. FOUND A/P CONTROL HEAD SHORTED. REPLACED HEAD PE R MM 22-11-181. 2 L 7 3 4F RT A3WE 1998092500194 19980925 00194 NE 1998 9 25 98ZZZX3422 2 19980825 A 8530 STUD 116733CP DOUG DC3 DC3C 3021457 WP PWA R1830 R183092 52020 NE ENGINE SHEARED A VLLA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 05 8187E 12804 804 Y175 25285 144618 AT CRUISE EN ROUTE FROM UCY/DET, LEFT ENGINE OIL PRESSURE STARTED TO DROP. ENIGNE WAS SHUT DOWN AND AIRCRAFT DIVERTED T O BMG. FOUND NR 1 CYLINDER STUDS BROKEN AND NR 1 CYLINDER LOOSE ON MOUNTING PAD. C/W AD 56-06-02(C) BY REPLACING ALL S TUDS ON NR 1 CYLINDER MOUNT PAD AND INSTALLING OVERHAULED CYLINDER ASSEMBLY. 2 L 7 2 4R 4 R A669 5E4 1998092500200 19980925 00200 CE 1998 9 25 98ZZZX3428 1 19980827 A 3097 WIRE BEECH 99 99 1154002 CE COCKPIT FAILED A FSEA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 NE 05 208BH U2 SMOKE CAME OUT AROUND GEAR HANDLE ON TAKEOFF. FOUND RIGHT PITOT HEAT WIRE BURNED DUE TO BAD CONNECTION. 1 L 7 2 3T A14CE 1998092500207 19980925 00207 SO 1998 9 25 98ZZZX3435 1 19980804 A 3244 175X6256 TIRE PIPER PA31 PA31P 7103120 SO NLG FAILED A EKIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 07 6805L 255 31P7 NOSE TIRE BLEW ON TAKEOFF ROLL AT HII. TAKEOFF ABORTED. PROPELLERS CONTACTED RUNWAY WHEN WHEEL WAS GROUND DOWN TO LOWE R STRUT FORK. AIRCRAFT WAS EQUIPPED WITH CLEVELAND 40-140 WHEEL PER AD 97-7-3 AND 10-PLY MICHELIN 17.5X6.25-6 TIRES. TH IS WHEEL AND TIRE COMBINATION ON THE PA31T AND PA31T1 HAS 80 PSI OF INFLATION PRESSURE, BUT ONLY 45 PSI IN THE PA31P. 1 L 7 2 3O A8EA 1998092500218 19980925 00218 NM 1998 9 25 98ZZZX3446 1 19980814 A 3240 980014001 NUT PIPER PA60 PA60600 7106001 NM CONTROL PEDAL LOOSE A DKBA K NONE O OTHER IN INSP/MAINT 1 SO 09 699RF 9108 600169074 JAM NUT HOLDING YOKE TO PEDAL BACKED OFF LETTING SHAFT ROTATE AND COME APART. WHEN ROD END (YOKE) CAME OFF OF BRAKE ACT UATOR, BRAKING ACTION WAS LOST ON LEFT BRAKE. PILOT WAS ABLE TO PARK AIRCRAFT USING STEERING AND LOWER POWER FOR TAXI. RETURN SPRING, YOKE, AND JAM NUT WERE RE-INSTALLED AND AIRCRAFT RETURNED TO SERVICE. 1 M 7 2 3O RT A17WE 1998092500243 19980925 00243 CE 1998 9 25 98ZZZX3471 1 19980814 A 7603 04110914 CONTROL CABLE CESSNA 195 195 2073102 CE JACOBP R755 R755B2 35007 SW ENGINE FAILED A FTTA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NE 05 145V 5400 7135 12200 THROTTLE CABLE BROKE ON APPROACH TO LANDING LEAVING THROTTLE PLATE APPROX ONE-HALF WAY OPEN. A SEMI-UNEVENTFUL LANDING FOLLOWED USING MIXTURE CONTROL. INVEST REVEALED THE CABLE TO HAVE BROKEN AT THREADED BRASS CABLE END WHERE THE 5 INCH L ONG EXTENSION ADAPTER IS ATTACHED. SUBMITTER STATED PILOT MAY HAVE USED EXCESSIVE FORCE TO ENSURE THROTTLE WAS OPEN ON TAKOFF. THE DISTANCE BETWEEN CABLE SUPPORT BRACKET AT ENG AND THROTTLE ARM IS APPROX 1 FOOT LEAVING AREA OF BRASS THREA DS OPPORTUNITY TO FLEX WHEN EXCESSIVE PRESS EXERTED FROM COCKPIT END. TWO OTHER CESSNA 195'S IN THIS FLEET HAVE THROTTL E CABLE STOP COLLARS ON KNOB END. 1 H 7 1 3R 3 R NC A790 E237 1998092500246 19980925 00246 CE 1998 9 25 98ZZZX3474 1 19980826 A 2434 ALT9422 ALTERNATOR BEECH 58 58 1152740 CE ENGINE FAILED A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 329H 56 8030668 TH219 ALTERNATOR CAME WITH NEW ENGINE, FACTORY REMANUFACTURED, JULY, 1998. WHEN ALTERNATOR IS ON-LINE, FUSE FAILS ON FIELD WI RE, WHEN FUSE IS REPLACED, VOLTAGE CHECK OK ON FIELD WIRE UNTIL ENGINE TURNS, FUSE FAILS. 1 L 7 2 3O 3A16 1998092500258 19980925 00258 NE 1998 9 25 ORJA98129 2 19980629 A 7313 6A4746 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 53489 V20040 SJC - MAINTENANCE DISCOVERED NR 2 ENGINE AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENGINE UPPER AND LOWER C -DUCTS HAVE DELAMINATION AND ARE DISBONDED BEYOND LIMITS. AIRCRAFT 901RA WAS FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MAINTENANCE DISCOVERED THAT THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO EL ONGATION OF THE BOLT HOLES IN THE BRACKET ASSEMBLY (BRACKET POSITIONS 14, 16 AND 19) MAINTENANCE. PERFORMED AN INTERMIM REPAIR TO THE UPPER AND LOWER C-DUCTS AND THE AFT COWL LATCH DOOR IN ACC WITH ROHR ENG DOCUMENT NR 98VN515. THIS REPAI R WILL BE PERMANENT AT C-CHECK (JULY 98). MAINTENANCE REMOVED AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. FUEL NOZZLE 2 L 7 2 4F 4 F RT A6WE E40NE 1998092500259 19980925 00259 1998 9 25 ORJA98128 2 19980629 A 7313 6A4747 BRACKET DOUG MD90 MD9030 3023690 NM NR 2 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 53489 SJC - MX DISCOVERED NR 2 ENG AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENG UPPER AND LOWER C-DUCTS HAVE DEL AMINATION AND ARE DISBONDED BEYOND LIMITS. A/C WAS FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MX DISCOVER ED THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKE T ASSEMBLY (BRACKET POSITIONS 14, 16 AND 19). MX PERFORMED AN INTERIM REPAIR TO THE UPPER AND LOWER C-DUCTS AND THE AFT COWL LATCH DOOR IN ACC WITH ROHR ENG DOCUMENT NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK. MX REMOVED AND RE PLACED DEFECTIVE FUEL NOZZLE BRACKETS. FUEL NOZZLES HAVE NEVER BEEN REPLACED. (M) 2 L 7 2 4F RT A6WE 1998092500260 19980925 00260 NE 1998 9 25 ORJA98127 2 19980629 A 7313 6A4745 BRACKET DOUG MD90 MD9030 3023690 NM IAE V2528 V2528D5 NE NR 2 ENGINE DAMAGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 901RA 6186 53489 V20040 SJC - MX DISCOVERED NR 2 ENG AFT COWL LATCH DOOR HAS EVIDENCE OF HEAT DAMAGE. NR 2 ENG UPPER AND LOWER C-DUCTS HAVE DEL AMINATION AND ARE DISBONDED BEYOND LIMITS. AIRCRAFT WAS FERRIED TO RENO FOR REPAIR. UPON FURTHER INVESTIGATION, MAINTE NANCE DISCOVERED THAT THE FOLLOWING FUEL NOZZLE BRACKETS SHOW EVIDENCE OF HOT AIR LEAKAGE DUE TO ELONGATION OF THE BOLT HOLES IN THE BRACKET ASSY (BRACKET POSITIONS 14, 16 AND 19). MX PERFORMED AN INTERIM REPAIR TO THE UPPER AND LOWER C-DU CTS AND THE AFT COWL LATCH DOOR IN ACC W/ROHR ENG, DOCUMENT NR 98VN515. THIS REPAIR WILL BE PERMANENT AT C-CHECK (JULY 98). MAINTENANCE REMOVE AND REPLACED DEFECTIVE FUEL NOZZLE BRACKETS. FUEL NOZZLES HAVE NEVER BEEN REPLACED. (M) 2 L 7 2 4F 4 F RT A6WE E40NE 1998092500261 19980925 00261 NE 1998 9 25 EIAA980226 2 19980706 A 7200 ENGINE BOEING 747 747273C 1384896 NM PWA JT9 JT9D7J 52054 NE NR 2 FAILED A EIAA A E UNSCHED LANDING ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 NM 09 470EV 20653 NAN - DURING CLIMB-OUT AT APPROX 8000 FT AN EXPLOSIVE NOISE WAS HEARD AND A/C YAWED. NR 2 ENGINE S/N 662970 FAILED. AI RCRAFT RETURNED TO NAN WITH NO FURTHER INCIDENT. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998092500262 19980925 00262 NM 1998 9 25 AALA981515 1 19980808 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 847AA 20988 TUL - TOP OF FRAME AT STATION 1130 CRACKED AREA 27R. SCREW DRIVER TURN FRAME AT STATION 1130 STRINGER 27R. CUT OUT DAM AGED AREA IN UPPER FLANGE OF 1130 FRAME. FABRICATED REPAIR FILLER AND DOUBLER AND INSTALLED IAW SRM 51-40-3 2653538. P REPARED AND PLUGGED HOLE IN FRAME IAW SRM 53-10-1. (M) 2 L 7 3 4F A3WE 1998092500263 19980925 00263 EU 1998 9 25 RAIA980721 1 19980721 A 7797 WIRE BAG JETSTM JETSTM3201 1500217 EU LT SRL FAULTY A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 433AM 885 FLT 7378 - STL - LEFT SRL CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPAIRED WIRE AT T2 SENSOR. (M) 2 L 7 2 4T RT A56EU 1998092500264 19980925 00264 EU 1998 9 25 RAIA980715 1 19980715 A 7722 ST3114 TRIM RESISTOR AEROSP ATR42 ATR42300 8680920 EU RT ENGINE CRACKED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 422TE 5363 106 FLT 7391 - FYV - RIGHT ENGINE DID NOT MAKE TARGET TORQUE TEMPERATURE LIMITED. MAINTENANCE REPLACED RIGHT ENGINE EGT COM PENSATING TRIM RESISTOR. (M) 2 H 7 2 4T RT A53EU 1998092500265 19980925 00265 EU 1998 9 25 RAIA980802 1 19980802 A 7722 SRL BAG JETSTM JETSTM3201 1500217 EU RT ENGINE MALFUNCTIONED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 422AM 856 FLT 7375 - UIN - RIGHT SRL CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE PERFORMED POWER ASSURANCE RUN ALL PARAMETER S NORMAL. (M) 2 L 7 2 4T RT A56EU 1998092500266 19980925 00266 EU 1998 9 25 RAIA980725 1 19980729 A 7712 56B17A SENSOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 341TE 950 FLT 7094 - STL - LEFT ENGINE TORQUE DROPPED TO 60 PERCENT ON CLIMB. MAINTENANCE INSPECTED AND REPLACED LEFT ENGINE T2 S ENSOR. (M) 2 L 7 2 4T RT A56EU 1998092500267 19980925 00267 1998 9 25 RAIA980804 2 19980802 A 7230 8676815 SEAL BAG JETSTM JETSTM3201 1500217 EU RT ENGINE LEAKING A RAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 03 926AE 926 FLT 4793 - SAN - SMOKE IN CABIN, OILY SMELL. MAINTENANCE REPLACED RIGHT ENGINE COMPRESSOR SEAL. (M) 2 L 7 2 4T RT A56EU 1998092500268 19980925 00268 EU 1998 9 25 RAIA980801 1 19980802 A 5610 1379628C401 WINDSCREEN BAG JETSTM JETSTM3201 1500217 EU COCKPIT CRACKED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 427AM 876 FLT 7486 - LEX - CAPTAINS FORWARD WINDSCREEN CRACKED IN FLIGHT. CREW DIVERTED TO EVV. MAINTENANCE REPLACED CAPTAINS FO RWARD WINDSCREEN. (M) 2 L 7 2 4T RT A56EU 1998092500269 19980925 00269 EU 1998 9 25 RAIA980807 1 19980807 A 2612 5122417 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 337TE 929 FLT 7478 - STL - RIGHT FIRE DETECT CAPTION INTERMITTENT IN FLIGHT. MAINTENANCE REPLACED RIGHT ENGINE FIRE WIRE LOOP. ( M) 2 L 7 2 4T RT A56EU 1998092500270 19980925 00270 EU 1998 9 25 RAIA980806 1 19980807 A 2610 51653151 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU RT WING FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 337TE 14679 929 FLT 7498 - STL - RIGHT ENGINE FIRE DETECT CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE INSPECTED, NO EVIDENCE OF FIRE. M AINTENANCE REPLACED RIGHT ENGINE FIRE WIRE CONTROLLER. (M) 2 L 7 2 4T RT A56EU 1998092500271 19980925 00271 EU 1998 9 25 RAIA980805 1 19980806 A 7931 1106P0208 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 428AM 14843 877 FLT 7486 - STL - RIGHT ENGINE OIL CAPTION ILLUMINATED IN FLIGHT. MAINTENANCE REPLACED RIGHT OIL PRESSURE SWITCH. (M) 2 L 7 2 4T RT A56EU 1998092500272 19980925 00272 WP 1998 9 25 RAIA980803 2 19980802 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT NACELLE FAILED A RAIA D RETURN TO BLOCK T J Y ENGINE CASE PENETRATION WARNING INDICATION ENGINE STOPPAGE TX TAXI/GRND HDL 1 CE 03 425AM 6232 870 66399R FLT 7478 - STL - LEFT ENGINE FLAMED OUT ON TAXI. MAINTENANCE REPLACED LEFT ENGINE DUE TO GEAR BOX FAILURE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998092500273 19980925 00273 WP 1998 9 25 RAIA980614 2 19980625 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT NACELLE MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 432AM 9613 883 66321 FLT 7506 - STL - BOTH ENGINES WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED LEFT ENGINE DUE TO LOW POWER. MAINTEN ANCE PERFORMED EGT RECOMPENSATION OF RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998092500274 19980925 00274 EU 1998 9 25 RAIA980811 1 19980817 A 7921 HTE860028 ACTUATOR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 436AM 7805 891 FLT 7061 - STL - LEFT OIL COOLER DOOR LIGHT ILLUMINATED AFTER TAKEOFF. MAINTENANCE REPLACED LEFT OIL COOLER FLAP ACTUAT OR. (M) 2 L 7 2 4T RT A56EU 1998092500275 19980925 00275 1998 9 25 RAIA980810 4 19980816 A 3160 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU E/E BAY FAILED A RAIA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 CE 03 550HK 3232 41039 FLT 7669 - JFK - FIRST OFFICERS EHSI AND EADI FLICKER IN FLIGHT. MAINTENANCE REPLACED RIGHT EFIS SYMBOL GENERATOR. (M) 2 L 7 2 4T RT A41NM 1998092500276 19980925 00276 1998 9 25 RAIA980812 3 19980818 A 6140 8659566 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 428AM 12966 877 FLT 7089 - SPI - RIGHT BETA CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT ENGINE BETA PRESSURE SWITCH . (M) 2 L 7 2 4T RT A56EU 1998092500277 19980925 00277 EU 1998 9 25 SIMA982291 1 19980817 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FAILED A SIMA K NONE N FALSE WARNING CR CRUISE 1 SW 21 180AE A2451 340B180 MIA - FLT 5711 - AVIONICS SMOKE LIGHT CAME ON SEVERAL TIMES IN FLIGHT. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998092500278 19980925 00278 NM 1998 9 25 TWRA9840 1 19980725 A 2530 OVEN BOEING 747 747282B 1384860 NM GALLEY DIRTY A TWRA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 15 610FF 20501 IN FLIGHT, FLIGHT ATTENDANT REPORTED SMELL OF ELECTRICAL NATURE IN THE MID GALLEY. ALL POWER TURNED OFF AND ITEM TRANSF ERRED TO ODI 25587. FROM LOG PAGE 25587 OPERATED ALL OVENS, LIGHTS, AND COFFEE MAKERS. ALL OPERATED NORMAL. NO SMOKE, NO SMELL, NO SPARKS, JUST A DIRTY OVEN. CLEANED OVEN, NO FURTHER DEFECTS NOTED. (M) 2 L 7 4 4F A20WE 1998092500279 19980925 00279 NM 1998 9 25 USAABB98086 1 19980813 A 2130 1305027 PRESS SELECTOR BOEING 767 7672B7 1385107 NM COCKPIT FAILED A USAA B EMER. DESCENT G J MULTIPLE FAILURE WARNING INDICATION DE DESCENT 1 EA 19 656US 7914 26847 PHL - FLT 480 - EN ROUTE MCO-PHL - APPROXIMATELY 100 MILES SOUTH OF PHL AND DESCENDING THROUGH FL 240, CREW EXPERIENCED AN AUTO-PRESSURIZATION FAILURE ON BOTH SYSTEMS. CREW PERFORMED AN EMERGENCY DESCENT TO CONTROL THE CABIN ALTITUDE. FLI GHT CONTINUED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CABIN PRESSURE INDICATOR PANEL AND T HE CABIN PRESSURE SELECTOR PANEL. (M) 2 L 7 2 4F RT A1NM 1998092500280 19980925 00280 NM 1998 9 25 USAASB98209 1 19980811 A 3350 AD20131A BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 426US 24548 GSO - MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK . OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998092500281 19980925 00281 NM 1998 9 25 USAASB98211 1 19980817 A 3350 1154551 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 586US 23931 PIT - MAINTENANCE FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT ROW 5C INOP. MAINTENANCE REMOVED AND REPLACED THE B UTTON LIGHT COVER AT SEAT ROW 5C. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998092500282 19980925 00282 NM 1998 9 25 USAASB98210 1 19980813 A 3350 081691 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 510AU 23385 CLT - PILOT REPORTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHT AT ROW 12 IS INOP. MAINTENANCE REMOVED AND REPLACED TWO LAMPHOLDER ASSEMBLIES AT SEAT ROW 12. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998092500283 19980925 00283 NM 1998 9 25 USAASB98202 1 19980802 A 2120 DUCT BOEING 737 7374B7 1384702 NM AC BAY FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 445US 24863 CLT - FLT 287 - AFTER TAKEOFF, AIRCRAFT FAILED TO PRESSURIZE. CREW SWITCHED TO STANDBY PRESSURIZATION SYSTEM AND OUTFLO W VALVE CLOSED BUT AIRCRAFT STILL FAILED TO PRESSURIZE. APU WAS STARTED WITH NO HELP. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND A BLOWN DUCT IN THE LEFT PACK BAY FR OM THE HEAT EXCHANGER TO THE AIR CYCLE MACHINE. REPAIRED DUCT BY WELDING. PRESSURIZED AIRCRAFT TO 4 PSI. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1998092500284 19980925 00284 NM 1998 9 25 USAASB98201 1 19980802 A 2121 65771 COOLING FAN BOEING 737 7374B7 1384702 NM E/E BAY FAILED A USAA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 EA 19 443US 22742 24842 MSY - FLT 943 - EN ROUTE FROM LGA-MSY - FLIGHT ATTENDANT REPORTED A BURNING SMELL IN THE CABIN. NORMAL EQUIPMENT COOLIN G FAN 'OFF' LIGHT CAME ON AND NORMAL BLOWER CIRCUIT BREAKER POPPED. ALTERNATE FAN POSITION WAS SELECTED AND 'OFF' LIGHT EXTINGUISHED. FLIGHT CONTINUED AND LANDED IN MSY WITHOUT FURTHER INCIDENT. MAINTENANCE DETERMINED THAT THE NORMAL EQU IPMENT COOLING FAN HAD FAILED. REPLACED SAME. OPERATIONAL CHECK GOOD. ALTERNATE FAN CHECKS GOOD ALSO. (M) 2 L 7 2 4F RT A16WE 1998092500285 19980925 00285 NM 1998 9 25 USAA980345 1 19980814 A 5315 146N508922 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 615AU 18876 27146 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION (120 INCHES) AT FLOORBEAM STATION 1640 RBL 60 TO LBL 60. INSTALLED NEW 'T' CAP PER TYPICAL REPAIR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1998092500286 19980925 00286 NM 1998 9 25 USAASB98204 1 19980809 A 2410 UA5385512 OIL COOLER BOEING 737 737401 1384701 NM CSD FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 417US 20506 23984 BNA - FLT 1514 - EN ROUTE FROM CLT-MCI, CAPT NOTICED THE NR 1 ENGINE CSD OIL TEMPERATURE READ HIGH AT 160 DEGREES. IMME DIATELY THEREAFTER, THE OVERHEAT LIGHT ILLUMINATED. CREW DISCONNECTED THE CSD THEN TRIED TO BRING APU ON LINE AT FL350 BUT WAS UNABLE. TRIED AGAIN AT FL310, BUT WAS STILL UNABLE. DECISION WAS MADE TO DIVERT TO NEAREST AIRPORT WHICH WAS B NA DUE TO BEING DOWN TO ONE ELECTRICAL POWER SOURCE. CREW DECLARED AN EMERGENCY AND THE FLIGHT LANDED WITHOUT FURTHER I NCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE CSD OIL COOLER. LEAK CHECKED GOOD. ALSO, REMOVED AND REPLAC ED THE NR 1 ENGINE CSD PER MM AS PRECAUTIONARY. OPS AND LEAK CHECK GOOD. APU WAS PLACED ON MEL. NO REPEAT ITEMS. (M) 2 L 7 2 4F RT A16WE 1998092500287 19980925 00287 NM 1998 9 25 USAASB98203 1 19980807 A 2612 5402 FIRE LOOP BOEING 737 737201 1384454 NM APU BAY FAILED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 263AU 22869 PIT - FLT 278 - AIRCRAFT WAS RELEASED WITH THE NR 1 ENGINE GENERATOR ON MEL. WHILE EN ROUTE FROM PHL TO DTW, THE APU FI RE WARNING DETECTOR LIGHT ILLUMINATED NECESSITATING AN APU SHUTDOWN. WITH ONLY ONE ELECTRICAL POWER SOURCE REMAINING, F LIGHT DIVERTED TO NEAREST AIRPORT AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENA NCE FOUND AN OPEN IN THE LOWER APU FIRE DETECTION LOOP. REMOVED AND REPLACED SAME. OPERATIONAL CHECK GOOD. CLEARED NR 1 ENGINE GENERATOR MEL BY REMOVING AND REPLACING THE GENERATOR. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998092500288 19980925 00288 NM 1998 9 25 USAASB98194 1 19980728 A 2530 50049BSB9334 COFFEE MAKER BOEING 737 7372B7 1384560 NM GALLEY FAILED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 277AU 16594 22889 BWI - FLT 7095 - EN ROUTE FROM MIA-BWI, A STRONG ACRID ODOR EMINATED FROM THE AFT RIGHT GALLEY. ODOR WAS ISOLATED TO TH E VENT IN THE AFT RIGHT GALLEY WHICH IS NOT PART OF THE AIR CONDITIONING SYSTEM. TURNED OFF GALLEY POWER AND PULLED GAL LEY COFFEE CIRCUIT BREAKERS. NO NOTICEABLE AFFECT ON ODOR. FLIGHT LANDED IN BWO WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL CABIN BALLASTS FOR OVERHEATING AND SMELL. ALL CHECK GOOD. FOUND AFT LEFT COFFEE MAKER IN THE AFT RIGHT G ALLEY PRODUCING A STRONG ELECTRICAL SMELL DURING BREW CYCLE. REMOVED AND REPLACED SAME. OPS CHECK GOOD. NO BURNING SM ELL NOTED. (M) 2 L 7 2 4F A16WE 1998092500289 19980925 00289 NM 1998 9 25 USAASB98205 1 19980810 A 7933 ACC336F1665 OIL FILTER BOEING 737 7372B7 1384560 NM NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J Y OVER TEMP WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 19 284AU 23131 TPA - FLT 8026 - CLIMBING THROUGH FL270, THE NR 1 ENGINE OIL TEMP STARTED RISING INTO THE YELLOW BAND. OIL PRESS WAS AT TOP OF THE GREEN BAND BUT NOT OUT OF LIMITS. OIL TEMP CONTINUED TO CLIMB AND AT FL290 HAD RISEN INTO THE RED BAND. TH E NR 1 ENGINE WAS PULLED BACK TO FLIGHT IDLE. AFTER TWO MINUTES, OIL TEMP REMAINED IN THE RED BAND AND CAPT SHUT DOWN T HE NR 1 ENG. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO FIELD AT TPA. FLT LANDED WITHOUT FURTHER INCIDENT. T OTAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE REMOVED THE NR 1 ENGINE FUEL HEAT VALVE AND INSPECTED SAME. NO DEF ECTS NOTED. REINSTALLED SAME. REMOVED AND REPLACED NR 1 ENGINE OIL FILTER, OIL TEMP SENSOR AND HEATER DE-ICER. RAN E 2 L 7 2 4F A16WE 1998092500290 19980925 00290 NM 1998 9 25 EIAA980229 1 19980716 A 3230 DOOR BOEING 747 747273C 1384896 NM MLG MALFUNCTIONED A EIAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 470EV 20653 KWRI - AFTER TAKEOFF AT ETAR, RIGHT WING LANDING GEAR DOOR FAILED TO OPEN, GEAR REMAINED DOWN AND LOCKED. REPEATED GEAR RETRACTION, NO HELP. DURING PREP TO RETURN TO ETAR, WITH GEAR HANDLE IN THE 'OFF' POSITION RIGHT BODY GEAR DOOR 'OPEN' LIGHT CAME ON. MOVED GEAR HANDLE TO THE 'UP' POSITION. RIGHT BODY GEAR DOOR LIGHTS EXTINGUISHED, RIGHT WING GEAR DOOR OPEN AND GEAR RETRACTED. DOOR CLOSED. (M) 2 L 7 4 4F A20WE 1998092500291 19980925 00291 NE 1998 9 25 EISA98148 2 19980610 A 7230 COMPRESSOR BOEING 727 7272A7 138407K NM PWA JT8 JT8D9 52048 NE NR 3 ENGINE STALLED A EISA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 310NE 655378 20241 ON TAKEOFF OUT OF ICT NR 3 ENGINE COMPRESSOR STALLED TRIPPING BOTH PACKS ON CLIMB NR 3 REACHED MAX CONT EGT, .10 EPR, BE LOW MAX CLIMB EPR, IN CRUISE ALL ENGINE PARAMETERS NORMAL. ICT TEMP 23 DEGREES CELSIUS WIND 100 AT 7 RUNWAY 19R. GENER ATED FROM PILOT REPORT. REMOVED AND REPLACED NR 3 ENGINE PER EXPRESS ONE ENGINE CHANGE SHEETS. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998092500292 19980925 00292 NE 1998 9 25 USAAD98135 2 19980805 A 7261 ACC336F1665 FILTER DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE RT ENGINE CLOGGED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 817US 48097 PIT-TPA - FLT 219 - THE RIGHT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED DURING CRUISE. AFTER ABNORMAL PROCEDURES FAILED TO EXTINGUISH THE LIGHT THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO CLT. THE AIRCRAFT LANDED WITHOUT INCIDENT . MAINTENANCE REPLACED THE RIGHT ENGINE OIL FILTER. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998092500293 19980925 00293 WP 1998 9 25 GAIA9872 1 19980707 A 3260 HYD LINE CVAC 240 240D 2422660 WP MLG CONTAMINATED A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 94226 48 FLT 184 - INBOUND TO PIT, THE MAIN LANDING GEAR WAS SELECTED TO THE DOWN POSITION THE CREW GOT A MOMENTARY SAFE THEN UNS AFE INDICATION ON THE MLG DOWN AND LOCKED LIGHTS. ATC WAS NOTIFIED EMERGENCY WAS DECLARED. THE MLG WAS CYCLED UP AND D OWN RESULTING IN A SAFE INDICATION OF DOWN AND LOCKED. AN UNEVENTFUL LANDING WAS MADE. INSPECTION FOUND AIR HAD BEEN T RAPPED IN THE HYDRAULIC SYSTEM CAUSING A FALSE READING ON THE HYDRAULIC SIGHT GAUGE, THE HYDRAULIC SYSTEM WAS SERVICED, AN OPERATIONAL CHECK OF THE HYDRAULIC SYSTEM WAS PERFORMED NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4R RT A793 1998092500294 19980925 00294 NM 1998 9 25 AALA981277 1 19980626 A 2120 FILTER BOEING 727 727223 1384074 NM PWA JT8 JT8D9A 52048 NE RT ENGINE DIRTY A AALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SW 07 849AA 20990 RSW - FLT 1383 - DURING CRUISE, EN ROUTE ATL-MIA, LOWER AFT BODY HEAT LIGHT FLICKERED ON AND OFF SEVERAL TIMES. AIR INT ERRUPTED AND LANDED RWS WITHOUT INCIDENT. REPLACED LEFT AIR CLEANER FILTER. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 3 4F 4 F A3WE E2EA 1998092500295 19980925 00295 WP 1998 9 25 VTZA98202 1 19980527 A 7712 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP NR 2 ENGINE CONTAMINATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 471UE 821 FLT 6193 - IAD-JFK - DURING TAKEOFF, EXPERIENCED A TORQUE ROLL BACK ON THE LEFT ENGINE DURING TAKEOFF ROLL. FLIGHT CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE CONTROL WAS NOTIFIED AND MAINTENANCE WAS DISPATCHED WHERE UP ON TROUBLESHOOTING. FOUND THE ZONE 2 CANNON PLUG HAD SOME DEBRIS IN IT. MAINTENANCE CLEANED THE ZONE 2 CANNON PLUG AND PERFORMED REQUIRED MAINTENANCE RUNS OF THE ENGINE. NO FURTHER DISCREPANCY WAS NOTED. AIRCRAFT WAS THEN RELEASED FOR S ERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998092500296 19980925 00296 EU 1998 9 25 USAASB98171 2 19980706 A 7311 3017764020 HEAT EXCHANGER BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 527AU 27505 23862 DEN - FLT 8052 - UPON CLIMB-OUT, JUST BEFORE LEVEL OFF AT FL 290, CREW WAS ALERTED TO HIGH OIL TEMPERATURE ALONG WITH A BURNING SEMLL ON THE NR 1 ENGINE. CREW ACCOMPLISHED CHECKLIST, DECLARED AN EMERGENCY AND INITIATED PROCEDURES IN SHUTTI NG DOWN THE NR 1 ENGINE AFTER THREE MINUTES AT IDLE. FLIGHT RETURNED TO FIELD AT DEN AND LANDED WITHOUT INCIDENT. AIRC RAFT TAXIED TO THE GATE UNDER ITS OWN POWER. TOTAL SINGLE ENGINE TIME WAS ESTIMATED AT EIGHT TO TEN MINUTES. MAINTENAN CE REMOVED AND REPLACED THE NR 1 ENGINE FUEL/OIL HEAT EXCHANGER. RAN ENGINE AT HIGH POWER FOR TEN MINUTES. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1998092500297 19980925 00297 EU 1998 9 25 SIMA982071 1 19980726 A 6120 78249052 PITCH CONT UNIT SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE SURGES A SIMA O OTHER R PARTIAL RPM/PWR LOSS AP APPROACH 1 SW 21 174AE 900674 340B174 GEE785478 FPO - FLT 5711 - RIGHT PROP RPM SURGED IN EXCESS OF 1500 RPM. POWER SETTING 25-35 PERCENT TORQUE POWER REDUCTION BROUGH T SURGE TO 1360-1480 RPM. PROP DID NOT FEATHER ON ENGINE SHUTDOWN AND WILL NOT RESPOND TO FEATHERING PUMP. SURGE IS 80 0-100/1340 WITH CONDITION LEVERS IN MINIMUM POSITION. OIL LEAKING OUT OF COWL AT OIL COOLER DISCHARGE DUCT. REMOVED AN D REPLACED RT PCU AND RT PROP TRANSFER TUBE. OPERATIONAL AND LEAK CHECK GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998092500298 19980925 00298 EU 1998 9 25 SIMA981891 1 19980708 A 3260 1175101 BOLT SAAB SF340 340B 7860101 EU LT/RT MLG WW BLOWN A SIMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 21 375AE 1387 340B375 DFW - FLT 3527 - FLT CREW REPORTED HYD LIGHT CAME ON IN FLIGHT AND MAIN HYD PRESSURE WENT TO ZERO, RAN QRH PROCEDURE, RE TURNED TO DFW. BLEW GEAR DOWN AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED A/C AND FOUND LIQUID SPILLAGE IN AREA OF TERMINAL BLOCK 36VT. CLEANED UP LIQUID SPILLAGE AND REPLACED L/G. EXPLOSIVE BOLTS PERFORMED L/G. EXTENSION CHECK AND OTHER SYSTEM CHECKS WITH NO DISCREPANCIES NOTED. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998092500299 19980925 00299 WP 1998 9 25 RAIA980702 2 19980701 A 7320 NAS1351C3LL6 SCREW BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UAR 01514 WP RT ENGINE LOOSE A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 429AM 634 879 FLT 7466 - STL - RIGHT SPEED LEVER LINKAGE SELF LOCKING ALLEN HEAD FASTENER LOOSENED CAUSING LINKAGE TO SEPARATE FROM UN DER SPEED FUEL GOVERNOR SPLINE. MAINTENANCE REPLACED SCREW PERFORMED RIGGING AND RUN. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998092500300 19980925 00300 NM 1998 9 25 TSAA9853451 1 19980801 A 5320 WEB BOEING 737 7372S5C 1384499 NM BS 664 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FOUND 2 INCH CRACK AT BS 664 AND 52 INCHES TO THE RIGHT OF BL. REPAIRED PER ECO 2917. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998092500301 19980925 00301 NM 1998 9 25 TSAA9853452 1 19980801 A 5320 WEB BOEING 737 7372S5C 1384499 NM BS 664 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 802AL 22148 FOUND 1 INCH CRACK AT BS 664 AND 39.5 INCHES TO THE RIGHT OF BL. REPAIRED PER ECO 2917. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500302 19980925 00302 NM 1998 9 25 TSAA9853439 1 19980725 A 5320 WEB BOEING 737 7372X6C 1384552 NM BS 664 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 FOUND 2 INCH CRACK AT BS 664 AND 52 INCHES TO THE RIGHT OF BL. VERIFIED BY HFEC. REPAIRED CRACK PER ECO 2917. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500303 19980925 00303 NM 1998 9 25 TSAA9853438 1 19980725 A 5320 WEB BOEING 737 7372X6C 1384552 NM BS 664 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 817AL 23292 FOUND 2 INCH CRACK AT BS 664 AND 39.5 INCHES TO THE RIGHT OF BL. VERIFIED BY HFEC. REPAIRED CRACK PER ECO 2917. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500304 19980925 00304 WP 1998 9 25 HALA9800268 1 19980730 A 2711 LINE DOUG DC10 DC1010 3022110 WP LT WING LEAKING A HALA K NONE K FLUID LOSS IN INSP/MAINT 1 WP 13 160AA 46710 FLT 21 - SEA - AFTER TAKEOFF LANDING GEAR LEVER WOULD NOT MOVE. REPLACED LEAKING HOSE ON LEFT TRIM ACTUATOR. RESET HYD RAULIC FUSE, SERVICED AND BLED HYDRAULIC SYSTEM. PERFORMED TRIM ACTUATOR, OPS CHECK PER MM. TEMPORARY HOSE INSTALLED A ND TECH. SERVICES NOTIFIED FOR PERMANENT REPLACEMENT. (M) 2 L 7 3 4F A22WE 1998092500305 19980925 00305 SO 1998 9 25 C2XA98CL057 1 19980803 A 3230 2112600000 ROD EMB 120 EMB120RT SO RT MLG WORN A C2XA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 09 27707 120095 CLE - FLT 3355 - CREW REPORTED THAT AFTER TAKEOFF THE RIGHT MAIN GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD WIT HOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN GEAR ACTUATOR ROD END IAW EMB-120 MM 32-32-10, O PERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 2 4T RT A31SO 1998092500306 19980925 00306 EU 1998 9 25 C2XA98BT053 1 19980725 A 3230 SWITCH AEROSP ATR42 ATR42320 8680930 EU MLG CONTAMINATED A C2XA O OTHER S AFFECT SYSTEMS CL CLIMB 1 SW 09 17831 185 EWR - CREW REPORTED LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT RETURNED UNEVENTFULLY, AIRCRAFT MEL'D RETURN ED TO SERVICE. MAINTENANCE, ON RON, FOUND DIRTY PROXIMITY SWITCHES, CLEANED PERFORMED GEAR RETRACTION OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998092500307 19980925 00307 SO 1998 9 25 C2XA98BT054 1 19980726 A 3350 7287103501 CONTROL MODULE EMB 145 EMB145 SO COCKPIT INOPERATIVE A C2XA K NONE L NO TEST NR NOT REPORTED 1 SW 09 14930 145011 EWR - CREW REPORTED EMERGENCY LIGHT SWITCH ON F/A PANEL WILL NOT ON EMERGENCY LIGHTS. MAINTENANCE FOUND BAD EMERGENCY L IGHT CONTROL MODULE. REMOVED AND REPLACED WITH A SERVICEABLE UNIT AND OPS CHECKED SYSTEM GOOD. (M) 2 L 7 2 4F RT T00011AT 1998092500308 19980925 00308 CE 1998 9 25 C2XA98IA277 1 19980725 A 2612 24409015 FIRE LOOP BEECH 1900 1900D 1154162 CE LT NACELLE MISINSTALLED A C2XA E D ENGINE SHUTDOWN RETURN TO BLOCK N W FALSE WARNING INADEQUATE Q C TX TAXI/GRND HDL 1 SW 09 69548 UE193 IAH - FLT 3920 - DURING TAXI, THE CREW REPORTED A NR 1 ENGINE FIRE LIGHT ILLUMINATION. THE AIRCRAFT RETURNED TO THE GAT E WHERE MAINTENANCE REPOSITIONED THE FIRE DETECTION LOOP AWAY FROM THE EXHAUST PIPE, AND THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998092500309 19980925 00309 SO 1998 9 25 C2XA98IA280 1 19980723 A 5347 12026864001 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16710 120106 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOO SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACE D THE EFFECTED SEAT TRACK IAW EMB-120 SRM 51-21-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500310 19980925 00310 SO 1998 9 25 C2XA98IA279 1 19980723 A 5730 12033270001 SKIN EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16710 120106 IAH - DURING C-CHECK INSPECTION, THE LEFT WING LOWER SKIN WAS FOUND TO BE CRACKED AT THE AFT OUTBOARD CORNER OF PANEL 52 2EB. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW EMB-120 SRM 57-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A31SO 1998092500311 19980925 00311 SO 1998 9 25 C2XA98IA278 1 19980723 A 3350 F02A250V1A LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16710 120106 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY AISLE PATH LIGHTING AFT SECTION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A DEFECTIVE FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500312 19980925 00312 NE 1998 9 25 C2XA98CL055 1 19980725 A 3610 32144143 VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE NR NOT REPORTED 1 SW 09 16731 17168 316 120190 ORF - FLT 3347 - CREW REPORTED THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED IN FLIGHT AND REMAINED ILLUMINATED AFTER THE CHECKLIST WAS ACCOMPLISHED. THE LEFT ENGINE WAS SECURED AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT . THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE, AND THE LEFT ENGINE BLEED PRESSURE REGULATOR/SHUTOFF VALVE WAS REMOVED A ND REPLACED IAW EMB-120 MM 21-50-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998092500313 19980925 00313 NE 1998 9 25 C2XA98CL056 2 19980727 A 7320 7863904 HMU EMB 120 EMB120RT SO PWA 118 PW118 NE RT ENGINE MALFUNCTIONED A C2XA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 09 12709 14392 F12519 120101 CLE - FLT 3206 - CREW REPORTED THE RIGHT ENGINE NP WOULD NOT GO BELOW 20.9 PERCENT DURING MANUAL FEATHER CHECK, AND THE NH RUNS AT 64.3 PERCENT. AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE HMU IAW EMB-120MM 73-21-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY IAW EMB-120MM 71-00-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998092500314 19980925 00314 EU 1998 9 25 AALA981437 1 19980723 A 2820 9815900 VALVE FOKKER F28 F28MK0100 4990807 EU LT WING LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 1452B FRTR016 11464 DFW - FLT 1189 - DURING CLIMB-OUT AUS, FUEL WAS SEEN STREAMING FROM THE LEFT WING TANK AND CONFIRMED BY THE FLIGHT CREW WITH THE COCKPIT FUEL GAUGES. FUEL STOPPED STREAMING FROM THE LEFT WING TANK AFTER A 300 LBS LOSS WAS NOTED BY THE FLIG HT CREW. AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT SNIFFLE VALVE AND AS A PRECAUTIONARY REPLACED LEFT FUEL OVERFLOW OUTLET VALVE. AIRCRAFT CHECKED NORMAL ON A FUNCTIONAL CHECK FLIGHT. SYSTE M FOUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998092500315 19980925 00315 NM 1998 9 25 AALA981468 1 19980803 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 360AA 24041 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT 21A AND 21B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHTS CONNECTOR AT SEAT 21A AND 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998092500316 19980925 00316 NM 1998 9 25 AALA981457 1 19980801 A 3350 CONNECTOR BOEING 767 767323 1385205 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386AA 27060 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT SEAT 29HJ INOPERATIVE. REPLACED CONNECTOR AND HARNESS . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998092500317 19980925 00317 NM 1998 9 25 AALA981470 1 19980803 A 3350 CONNECTOR BOEING 767 767223 1385123 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 332AA 22331 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 33C INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CO NNECTOR AT SEAT 33C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998092500318 19980925 00318 EU 1998 9 25 AALA981467 1 19980801 A 3260 D22376100 HARNESS AIRBUS 300 A300B4605R 3930308 EU RT MLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 3075A 5028 606 MIA - FLT 518 - AFTER TAKEOFF MIA, UNABLE TO RAISE LANDING GEAR IN EITHER HYDRAULIC SYSTEM 1 OR 2. RETURNED MIA AND LAN DED WITHOUT INCIDENT. REPLACED INBOARD HARNESS RIGHT MAIN LANDING GEAR. INSTALLED NEW PROXIMITY DETECTORS ON RIGHT MAI N LANDING EAR. PERFORMED GEAR SWING OPERATION CHECKS NORMAL ON HYDRAULIC SYSTEM 1 AND 2 PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998092500319 19980925 00319 WP 1998 9 25 AALA981469 1 19980803 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 77421 49333 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS BY AFT ENTRY DOOR INOPERATIVE. REPAIRED WIRE ON EMERGENC Y EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998092500320 19980925 00320 WP 1998 9 25 AALA981456 1 19980802 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7517A 49894 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS FORWARD OF FIRST CLASS SEATS INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500321 19980925 00321 WP 1998 9 25 AALA981465 1 19980730 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 76201 53291 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD SECTION AT FIRST CLASS GALLEY EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE . REPAIRED FEED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHT STRIP. (M) 2 L 7 2 4F RT A6WE 1998092500322 19980925 00322 WP 1998 9 25 AALA981464 1 19980729 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7514A 49891 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT AISLE TRACK LIGHT AFT MOST EXIT SIGN INOPERATIVE. REPLACED EMERGENCY EXIT AISLE LIGHT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500323 19980925 00323 WP 1998 9 25 AALA981463 1 19980731 A 2120 CLAMP DOUG DC9 DC982 3022082 WP RT PACK BROKEN A AALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 07 297AA 49309 DFW - FLT 608 - ON CLIMB-OUT DFW, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. FOLLOWED CHECKLIST PROCEDURE AND LIGHT REMAINED ILLUMINATED. A COUPLE OF MINUTES AFTER HIGH PRESSURE BLEED TURNED OFF THE LIGHT EXTINGUISHED. AIR INTE RRUPTED BACK TO DFW AND LANDED WITHOUT INCIDENT. REPLACED RIGHT PACK ACM CLAMP AND PERFORMED LEAK CHECK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500324 19980925 00324 WP 1998 9 25 AALA981436 1 19980724 A 8012 97941011 VALVE DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 SW 07 7518A 5069C 49895 DFW - FLT 1009 - DURING CLIMB THROUGH FL 18, RIGHT START VALVE OPEN LIGHT ILLUMINATED. CREW PERFORMED IN FLIGHT SHUT DO WN OF RIGHT ENGINE AND LANDED DFW OVERWEIGHT WITHOUT FURTHER INCIDENT. AN OVERWEIGHT INSPECTION WAS ACCOMPLISHED WITH N O FINDINGS. REPLACED RIGHT ENGINE START VALVE AND ACCOMPLISHED OPERATIONS CHECK WITH NORMAL OPERATION. SYSTEM GROUND A ND LEAK CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500325 19980925 00325 EU 1998 9 25 AALA981389 1 19980715 A 2842 0209KTU05 PROBE FOKKER F28 F28MK0100 4990807 EU RT WING FAILED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1457B 11469 DFW - FLT 1198 - ON CLIMB-OUT PASSING FL230 CREW NOTICED RIGHT FUEL TANK WAS NOT FEEDING. FOLLOWED THE FUEL IMBALANCE P ROCEDURE AND STILL NO FUEL WAS BEING USED FROM THE RIGHT TANK. CREW DECLARED AN EMERGENCY AND RETURNED TO DFW. WHILE R ETURNING TO DFW THE RIGHT TANK QUANTITY FELL FROM 78000 LBS TO 5800 LBS, THEN OPERATED NORMALLY. DISCONTINUE THE CROSS FEED PROCEDURE. WHEN THE QUANTITY DROPPED TO 5800 LBS RECEIVED A FUEL ASYMMETRY MESSAGE ON THE MFDU. LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED FUEL CAPACITANCE PROBE FOR RIGHT WING FUEL QUANTITY INDICATOR. CONDUCTED OVERWEIGHT INSPEC TION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998092500326 19980925 00326 NM 1998 9 25 ASAA9810073 1 19980724 A 5330 SKIN BOEING 737 737298C 1384490 NM BS 847 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND SKIN CORRODED UNDER FRAME AT STATION 847, STRINGER 24R. REPAIRED PER ASA EA 5330-01324. (M ) 2 L 7 2 4F RT A16WE 1998092500327 19980925 00327 NM 1998 9 25 ASAA9810074 1 19980724 A 5330 SKIN BOEING 737 737298C 1384490 NM BS 360-540 CREASED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 PHX - DURING D-CHECK, FOUND LOWER FORWARD SKIN CREASED STATION 360-540, STRINGER 19R-26R. REPAIRED PER ASA EA 5330-0133 0. (M) 2 L 7 2 4F RT A16WE 1998092500328 19980925 00328 NM 1998 9 25 ASAA9810077 1 19980728 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING C-CHECK, FOUND THE FLOORBEAM CORRODED AT STATION 947, LBL 29.5 TO LBL 35.62. REPAIRED PER EA 5310-01590 AN D BOEING TELEX ASA-SEA-98-0275RR. (M) 2 L 7 2 4F A16WE 1998092500329 19980925 00329 NM 1998 9 25 ASAA9840077 1 19980707 A 5610 MOUNT BOEING 737 7374Q8 NM COCKPIT LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 783AS 25114 SEA - FLT 479 - CREW REPORTED THE CO-PILOTS SLIDING WINDOW WAS DIFFICULT TO OPEN OR CLOSE. TIGHTENED ROLLER BEARING MOU NT SET SCREW AND WINDOW OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998092500330 19980925 00330 EU 1998 9 25 RAIA980722 1 19980722 A 5280 137414B418 GEAR DOOR BAG JETSTM JETSTM3201 1500217 EU RT MLG SEPARATED A RAIA O OTHER D INFLIGHT SEPARATION LD LANDING 1 CE 03 427AM 15227 876 FLT 7372 - UIN - RIGHT MAIN LANDING GEAR DOOR DEPARTED IN FLIGHT. MAINTENANCE INSPECTED AND FERRIED AIRCRAFT TO STL. M AINTENANCE REPLACED RIGHT MAIN LANDING GEAR DOOR. (M) 2 L 7 2 4T RT A56EU 1998092500331 19980925 00331 EU 1998 9 25 RAIA980723 1 19980725 A 3240 AC66867 VALVE BAG JETSTM JETSTM3201 1500217 EU NLG WW FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 426AM 1608 874 FLT 7023 - STL - AIRCRAFT PULLED TO THE RIGHT DURING TAKEOFF ROLL. MAINTENANCE REPLACED BRAKE CONTROL VALVE. (M) 2 L 7 2 4T RT A56EU 1998092500332 19980925 00332 EU 1998 9 25 RAIA980724 1 19980729 A 3234 1005383Y00 SELECTOR VALVE AEROSP ATR42 ATR42300 8680920 EU MLG WW FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 424TE 21962 124 FLT 7403 - FYV - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED LANDING GEAR CONTROL VALVE. (M) 2 H 7 2 4T RT A53EU 1998092500333 19980925 00333 EU 1998 9 25 REXA98107 1 19980727 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU E/E BAY MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 25 346AM A2068 340A032 AVIONICS SMOKE LIGHT IN FLIGHT. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR. (M) 2 L 7 2 4T RT A52EU 1998092500334 19980925 00334 1998 9 25 ARWA980808 4 19980810 A 2213 CONTROLLER DOUG DC8 DC862 3021970 WP AFCS FAILED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 1808E 3136 46105 MIA - FLT 617 - NR 1 AND NR 2 RADAR INOP R/I. A/C RETURNED TO MIAMI, REMOVED AND REPLACED PITCH COMPUTER, OPS CHECKED N ORMAL IAW MM 22-13-0. NR 2 RADAR R/T, P/N 2067151-0153 S/N 2915. (M) 2 L 7 4 4F 4A25 1998092500335 19980925 00335 1998 9 25 ARWA980807 4 19980808 A 3442 20412151102 RADAR DOUG DC8 DC862 3021970 WP COCKPIT INOPERATIVE A ARWA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 SO 19 1808E 2781 46105 MIA - FLT 617 - NR 2 RADAR INOP 'R/T'. REMOVED AND REPLACED NR 2 RADAR SCOPE SYSTEM CHECKED NORMAL IAW MM 34-41-0. (M) 2 L 7 4 4F 4A25 1998092500336 19980925 00336 WP 1998 9 25 ARWA980809 1 19980812 A 2922 FILTER DOUG DC8 DC862 3021970 WP HYDRAULIC SYSTEM CONTAMINATED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 1808E 46105 MIA - FLT 617 - HYD OIL TEMP REACHED 80 PERCENT. REMOVED AND REPLACED LEFT WHEEL WELL FILTERS IAW MM 29-10-00. OPS AND LEAK CHECK NORMAL. NO LEAKS NOTED. (M) 2 L 7 4 4F 4A25 1998092500337 19980925 00337 1998 9 25 ARWA980810 4 19980812 A 3442 20871810501 ANTENNA DOUG DC8 DC862 3021970 WP RADAR SYSTEM FAILED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 1808E 1931 46105 MIA - FLT 617 - NR 1 AND NR 2 RADAR INOP. REMOVED AND REPLACED ANTENNA AND REPLACED BOTH R/T'S REPLACED BOTHS INDICATOR S AND CONTROL HEADS, ACCOMPLISHED OPERATIONAL CHECK IAW MM 34-41-0, OPS CHECK NORMAL DURING 2 HOURS GROUND CHECK. NR 2 RADAR IND CONTROL P/N 2078 S/N 6, INOP. NR 2 RADAR IND P/N 20852680104 S/N 1498, INOP. NR 1 RADAR R/T, P/N 2067157015 S/N 4352, INOP. NR 2 RADAR R/T P/N 2067157015 S/N 6491, INOP. RADAR IND P/N 20852680104 S/N 1322, INOP. (M) 2 L 7 4 4F 4A25 1998092500338 19980925 00338 NM 1998 9 25 EISA98204 1 19980801 A 5330 SKIN BOEING 727 727277 138408S NM BS 660-680 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP CARD C53-100-01 PART 4 INSPECTION OF LOWER FUSE BS 178 TO 1183. DETECTED ROW OF RIVETS RI GHT SIDE AT STRINGER 25 STATION 680 TO 660 SKIN BULGED AND STRINGER CRACKED WITH CORROSION. REPLACED STRINGER 25 PER SR M 53-10-3 FIG 1 HEAVY LIFT N/R CARD 905789. (M) 2 L 7 3 4F RT A3WE 1998092500339 19980925 00339 NM 1998 9 25 EISA98205 1 19980813 A 2720 2588838 SENSOR BOEING 727 72725 1384006 NM RUDDER FAILED A EISA K NONE J WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 300NE 18974 LOWER RUDDER IND FULL LEFT DEFLECTION ALL TIME, ON GROUND. REMOVED AND REPLACED LOWER RUDDER POSITION SENSOR PER 22-11- 51. OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998092500340 19980925 00340 WP 1998 9 25 EISA98207 1 19980816 A 3350 1100049 BATTERY CHARGER DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A EISA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 977ML 1473 47329 AFT SECTION FLOOR MOUNTED EMERGENCY EXIT LIGHTING INOP. REPLACED AFT EMERGENCY LIGHT BATTERY CHARGER IAW MM 33-00. (M) 2 L 7 2 4F A6WE 1998092500341 19980925 00341 1998 9 25 EISA98208 4 19980816 A 2565 1133169 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR FAILED A EISA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 945VJ 82 47066 POST FLIGHT FOUND GALLEY EVAC SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE ASSY MM 25-00 CHECKS OK. (M) 2 L 7 2 4F A6WE 1998092500342 19980925 00342 NM 1998 9 25 EISA98185 1 19980730 A 5320 WEB BOEING 727 727223 1384074 NM BS 350 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF C-CHECK CPCP CARDS, FOUND CORROSION AT STATION 350 RIGHT PRESSURE WEB IN NOSE LANDING GEAR AREA . REMOVED AND REPLACED CORRODED AREA PER SRM 53-10-02 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1998092500343 19980925 00343 NM 1998 9 25 EISA98186 1 19980722 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 1036-1070 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARDS, FOUND SEAT TRACK LEFT INBOARD AND OUTBOARD FROM STATION 1036 TO 1070 COR RODED. REMOVED AND REPLACED DAMAGED SECTION FROM 1036 TO 1070 PER SRM 53-10-02 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1998092500344 19980925 00344 NM 1998 9 25 EISA98187 1 19980722 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 740-850 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARDS, FOUND SEAT TRACK AT STATION 760-850 LEFT INBOARD CORRODED. REMOVED AND REPLACED WITH NEW SECTION STATION 740 TO 815 PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998092500345 19980925 00345 NM 1998 9 25 EISA98188 1 19980722 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 900 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 316NE 19475 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD, LEFT INBOARD SEAT TRACK WAS FOUND CORRODED AT STATION 900. REMOVED AND R EPLACED WITH NEW SECTION STATION 900 PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998092500346 19980925 00346 WP 1998 9 25 ORJA98197 1 19980818 A 3350 EM1267 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 ATSJC, EMERGENCY LIGHTS, FORWARD EMERGENCY EXITS, BOTH SIDES INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998092500347 19980925 00347 WP 1998 9 25 ORJA98196 1 19980815 A 3350 0105611001 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 RENO - EMERGENCY EXIT LIGHTS INOP AT ROWS 12 THROUGH 16 AND EXIT ROW. INSTALLED NEW LIGHT SWITCHING UNIT. OPS CHECK GO OD IAW 33-50-00. OK FOR SERVICE. (M) 2 L 7 2 4F A6WE 1998092500348 19980925 00348 WP 1998 9 25 ORJA98195 1 19980806 A 3610 D17D87 CLAMP DOUG DC9 DC983 3022083 WP TAIL COMPARTMENT FAILED A ORJA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 11 876RA 53183 AIR RETURN TO LAS VEGAS, TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON IN FLIGHT. WENT OUT WHEN RT THROTTLE REDUCED TO IDLE. FOUND RIGHT CROSSFEED CLAMP TO BE INOPERABLE. REMOVED AND REPLACED CLAMP. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998092500349 19980925 00349 NM 1998 9 25 MASA98152 1 19980809 A 2612 6504 CONTROL UNIT DHAV DHC8 DHC8202 2809007 NM RT ENGINE MALFUNCTIONED A MASA K NONE N FALSE WARNING CR CRUISE 1 SW 07 444YV 444 FLT 5077 - PHX-DRO - CREW REPORTED RIGHT ENGINE FIRELOOP 'B' FAULT LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE ACTION WAS DEFERRED PER MEL 26-01. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, SYSTEM WAS TROUBLESHOT. NO DISCR EPANCIES WERE NOTED. THE RT ENGINE FIRE LOOP WAS REMOVED ADN REPLACED AS A PRECAUTION. (M) 2 H 7 2 4T RT A13NM 1998092500350 19980925 00350 NM 1998 9 25 MASA98158 1 19980822 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 5228 - PHX-YUM - ON PREFLIGHT, CREW FOUND THE PORTABLE EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE E MERGENCY LIGHT. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998092500351 19980925 00351 EA 1998 9 25 MASA98160 1 19980825 A 3350 OL3071BPEGPL BULBS CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5791 - CVG-PHL - CREW REPORTED THE EMERGENCY FLOODLIGHT BETWEEN ROW 4 AND 5 INOP. MAINTENANCE ACTION WAS DEFERRED P ER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULBS WERE REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1998092500352 19980925 00352 EU 1998 9 25 SIMA982371 1 19980825 A 5347 9253799383 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 396AE 340B396 ABI - SEAT TRACK AT FUSELAGE STATION 297 BL 18.31 CORRODED. CUT OUT AND REPLACED 11 INCH SECTION OF SEAT TRACK. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998092500353 19980925 00353 EU 1998 9 25 SIMA982381 1 19980826 A 3350 AA3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 37AE 15387 037 GRR - FORWARD FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998092500354 19980925 00354 EU 1998 9 25 PLGA980811A 2 19980811 A 7261 OIL SYSTEM SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A2 30030 NE RT ENGINE OVERSERVICED A PLGA E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE AP APPROACH 1 NE 05 747BA 340A148 BOS - FLT 4358 - WHILE ON APPROACH TO BOS, THE CREW RECEIVED A LOW OIL PRESSURE WARNING ON RIGHT ENGINE. AIRCRAFT CONTI NUED AND LANDED WITHOUT INCIDENT. THE CREW SHUT DOWN THE RIGHT ENGINE AFTER LANDNIG AND TAXIED TO THE GATE. MAINTENANC E FOUND THE RIGHT ENGINE PGB TO BE OVER SERVICED WITH OIL. THE OIL LEVEL WAS ADJUSTED AND ENGINE RAN WITH SYSTEM CHECKI NG GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1998092500355 19980925 00355 NM 1998 9 25 P2EA98159 1 19980817 A 2133 7110033 VALVE BOEING 737 737247 138448D NM FUSELAGE INOP A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 204AU 19603 FLT 701 - MDW - AIR RETURN, NO EMERGENCY DECLARED. LANDING UNEVENTFUL. AUTO AND STANDBY PRESSURIZATION FAILED IN FIGHT AT 5000FT. ONLY DC MANUAL OPERATIONAL. REPLACED OUTFLOW VALVE. OPS CHECK NORMAL PER MM 21-31-11. (M) 2 L 7 2 4F A16WE 1998092500356 19980925 00356 NM 1998 9 25 P2EA98162 1 19980824 A 3350 900835A BATTERY PACK BOEING 737 737222 1384473 NM CABIN DISCHARGED A P2EA K NONE L NO TEST IN INSP/MAINT 1 CE 05 209US 6511 19548 PHX - DURING SCHEDULED MAINTENANCE, IT WAS NOTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHTS ON ROWS 9 THROUGH 17 WERE I NOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998092500358 19980925 00358 EU 1998 9 25 SIMA982311 1 19980819 A 5347 S5367800124602 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 438AT 438 SAW - DURING CPCP-8 INSPECTION, FOUND THE LEFT AFT INBOARD AND OUTBOARD, AND THE RIGHT MIDDLE INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACD BOTH LEFT AFT SEAT TRACKS. REPAIRED BOTH RIGHT MIDDLE SEAT TRACKS. AIRCRAFT RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500359 19980925 00359 EU 1998 9 25 SIMA982312 1 19980819 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 SAW - DURING MBV-1 INSPECTION, FOUND FLOORBEAM 36.38 AND 39 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCRAFT RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500360 19980925 00360 EU 1998 9 25 SIMA982341 1 19980822 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 359SB 340B359 DFW - FLT 3652 - EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 9/10A DOES NOT ILLUMINATE. RESECURED LOOSE LIGHT STRIP. OPERA TIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998092500361 19980925 00361 EU 1998 9 25 SIMA982351 1 19980823 A 3350 2LAD LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 191AE 340B191 MIA - EMERGENCY EXIT SIGN LIGHT AT SEAT 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998092500362 19980925 00362 EU 1998 9 25 SIMA982352 1 19980823 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 280AE 340B280 DFW - FLT 3148 - EMERGENCY LIGHT AT SEAT 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A52EU 1998092500363 19980925 00363 NM 1998 9 25 HNAA9893535 1 19980806 A 3350 6013211X BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 935HA 142 FLT 3169 - DCA-PHL - NR 3 AND NR 4 RED ESCAPE PATH LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY 3352 PS1, OPS CHECK GO OD. (M) 2 H 7 2 4T RT A13NM 1998092500364 19980925 00364 EU 1998 9 25 SIMA982343 1 19980822 A 5320 S53678008200 ZEE MEMBER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 SAW - DURING CPCP-4 INSPECTION, FOUND THE RIGHT AFT ZEE MEMBER CORRODED BETWEEN FRAMES 39 AND 42. REMOVED AND REPLACED THE ZEE MEMBER AND FLOOR CHANNEL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500365 19980925 00365 EU 1998 9 25 SIMA982342 1 19980822 A 5320 S53678008200 ZEE MEMBER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 SAW - DURING CPCP-4 INSPECTION, FOUND THE LEFT AFT ZEE MEMBER AND FLOOR CHANNEL CORRODED BETWEEN FRAMES 39 AND 40. REMO VED AND REPLACED THE ZEE MEMBER AND FLOOR CHANNEL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500366 19980925 00366 EU 1998 9 25 SIMA982344 1 19980822 A 5347 S53375001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 308AE 309 SAW - DURNIG CPCP-4 INSPECTION, FOUND THE LEFT FORWARD INBOARD AND OUTBOARD, LEFT MIDDLE INBOARD AND OUTBOARD, LEFT AFT INBOARD AND OUTBOARD, LEFT AND RIGHT AFT FLIGHT ATTENDANT, RIGHT AFT CARGO, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND OUTBOARD, RIGHT FORWARD INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500367 19980925 00367 EU 1998 9 25 SIMA982353 1 19980823 A 2421 S242100260000 HOUSING AEROSP ATR72 ATR72212 EU LT ENGINE CRACKED A SIMA O OTHER C F.O.D. DE DESCENT 1 SW 21 399AT 399 TUL - FLT 3828 - LEFT ENGINE ACW GENERATOR FAULTED, AND ASSOCIATED ENGINE POWER LEVER WOULD NOT MOVE FROM FLIGHT IDLE FO RWARD. POWER LEVER WOULD MOVE FROM FLT IDLE BACK THROUGH REVERSE. FOUND ACW GENERATOR COVER BROKEN OFF AND JAMMED AGAI NST POWR LEVER CONTROL. REMOVED COVER AND MEL'D GENERATOR. AIRCRAFT WAS RETURNED TO SERVICE AND FLOW TO DFW WHERE THE GENERATOR WAS REMOVED AND REPLACED. (M) 2 H 7 2 4T RT A53EU 1998092500368 19980925 00368 NM 1998 9 25 USAASB98218 1 19980822 A 2133 7110033 OUTFLOW VALVE BOEING 737 7374B7 1384702 NM FUSELAGE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 447US 24874 MIA - FLT 1431 - ON CLIMB-OUT FROM MIA, CREW WAS UNABLE TO PRESSURIZE AIRCRAFT OR CONTROL CABIN IN STANDBY OR MANUAL MOD ES. FLIGHT RETURNED TO FIELD AT MIA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOV ED AND REPLACED THE AFT OUTFLOW VALVE PER MM CHAPTER 21. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998092500369 19980925 00369 NM 1998 9 25 TAOA089807 1 19980823 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 924TS 21041 FLT 6492, FOUND L/S CHECK, EMERGENCY EXIT SIGN AT R-2 DOOR DOES NOT ILLUMINATE DURING TEST. REPLACED BATTERY PACK AT R- 2 DOOR LOCATION. OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998092500370 19980925 00370 NM 1998 9 25 TWRA9848 1 19980821 A 3350 SIGN BOEING 747 747130 1384880 NM CABIN INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 ON PRE-FLIGHT INSPECTION, FOUND EXIT SIGN ABOVE R1 DOOR EVAC LIGHT INOP. REPAIRED BROKEN WIRE, OPS CHECK OK PER MM 33-5 1-00. (M) 2 L 7 4 4F A20WE 1998092500371 19980925 00371 EU 1998 9 25 SIMA982177 1 19980806 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233RM 3652 235 SAW - DURING PS-2 INSPECTION, FOUND SEVERAL FORWARD CABIN FLOOR PROXIMITY LIGHTS THAT DID NOT ILLUMINATE. REMOVED AND R EPLACED EMERGENCY FLOOR LIGHT BATTERY PACK AT 29 WL. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500372 19980925 00372 EU 1998 9 25 SIMA982183 1 19980806 A 3350 LIGHT AEROSP ATR42 ATR42300 8680920 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 144DD 074 FLT 4229 - GRB - PAX DOOR EMERGENCY EXIT LIGHT DOES NOT ILLUMINATE. REPAIRED BROKEN WIRES AT LIGHT SOCKET. OPERATIONAL CHECK NORMAL. (M) 2 H 7 2 4T RT A53EU 1998092500373 19980925 00373 EU 1998 9 25 SIMA982292 1 19980817 A 3320 65111 BALLAST SAAB SF340 340B 7860101 EU LAVATORY FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 21 392AE 581 340B392 MAF - FLT 3630 - AFTER TAKEOFF, FLIGHT ATTENDANT NOTICED A BURNING ELECTRICAL SMELL FROM THE FORWARD PART OF THE CABIN. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. AFTER LANDING THE SMELL HAD DISSIPATED. FOUND LAVATORY LIGHT BALLAS T TO BE THE CAUSE. REMOVED AND REPLACED LAVATORY LIGHT BALLAST. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998092500374 19980925 00374 NM 1998 9 25 USAASB98220 1 19980823 A 3350 S106 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 241US 22443 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE FORWARD PASSENGER ENTRY DOOR INOP. MAINTENANCE REMOVED AND REP LACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998092500375 19980925 00375 NM 1998 9 25 USAASB98219 1 19980823 A 3350 AD20131A BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 530AU 24412 ROC - MAINTENANCE FOUND SEVERAL FORWARD EMERGENCY LIGHTS FAIL AFTER APPROXIMATELY TWENTY SECONDS OF OPERATION. MAINTENA NCE REMOVED AND REPLACED THE BATTERY PACK IN THE M1132 POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998092500376 19980925 00376 NM 1998 9 25 USAASB98216 1 19980813 A 3350 AD20131A BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 577US 23742 PHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT SEAT ROWS 21 AND 22 INOP. MIANTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998092500377 19980925 00377 NM 1998 9 25 USAASB98215 1 19980813 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 225US 21667 PHL - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998092500378 19980925 00378 NM 1998 9 25 USAASB98214 1 19980819 A 3350 S106 BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 268AU 22880 CMH - PILOT REPORTED THE LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT FLICKERS. MAINTENANCE REMOVED AND REPLACED THE BATT ERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998092500379 19980925 00379 NM 1998 9 25 USAA980340 1 19980816 A 5240 SKIN BOEING 737 737301 1384611 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 35161 23510 TPA - DURING A CX-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN OUTER SKIN FWD SERVICE DOOR AFT UPPER CORNER AT L OWR HINGE CUTOUT AT DOOR EXTERNAL SKIN. INSTALLED DOUBLER OF .063 2024-T3 PER EA 62251. (M) 2 L 7 2 4F RT A16WE 1998092500380 19980925 00380 NM 1998 9 25 USAA980341 1 19980816 A 5210 6552873159 SKIN BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 23510 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK IN OUTER SKIN AFT ENTRY DOOR, AFT LWR CORNER OF UPPER HINGE CUTOUT AT EXTERNAL DOOR SKIN. INSTALLED DOUBLER OF .071 2024-73 PER EA 62252. (M) 2 L 7 2 4F RT A16WE 1998092500381 19980925 00381 NM 1998 9 25 USAA980342 1 19980816 A 5210 6552873159 SKIN BOEING 737 737301 1384611 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 35161 23510 TPA - DURING CX-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK IN EXTERNAL SKIN AFT ENTRY DOOR, FWD FL ANGE 1 INCH ABOVE LOWER HINGE CUTOUT. INSTALLED DOUBLER OF .050 2024 T-3 PER SRM 52-00-01 FIG 202. (M) 2 L 7 2 4F RT A16WE 1998092500382 19980925 00382 NM 1998 9 25 USAA980344 1 19980817 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 339US 35858 23236 CLT - DURING DAILY CHECK VISUAL INSPECTION, FOUND A 5 INCH CRACK BL 0 BETWEEN STATION 727D AND 727E ON FUSELAGE SKIN. I NSTALLED DOUBLER PER SRM 53-00-01. (M) 2 L 7 2 4F RT A16WE 1998092500383 19980925 00383 EU 1998 9 25 USAAF98068 1 19980812 A 4990 10200002 SENSOR FOKKER F28 F28MK0100 4990807 EU APU MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING AP APPROACH 1 EA 19 880US 11331 BWI - FLT 281 - EN ROUTE FROM CLT TO EWR, WITH THE NR 1 GENERATOR ON MEL, THE APU INDICATED AN OIL OVER TEMP CONDITION. THE CREW SHUT DOWN THE APU. FLIGHT D IVERTED TO BWI PER SPECIAL PROCEDURES BECAUSE ONLY ONE GENERATOR WAS ON LINE. FL IGHT LANDED BWI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE APU OIL TEMPERATURE SENSOR. (M) 2 L 7 2 4F RT 1998092500384 19980925 00384 NM 1998 9 25 USAA980352 1 19980824 A 5311 65465501 FRAME BOEING 737 737401 1384701 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 787 BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998092500385 19980925 00385 NM 1998 9 25 USAA980351 1 19980824 A 5311 65465551 FRAME BOEING 737 737401 1384701 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 867 BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER PE R SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998092500386 19980925 00386 NM 1998 9 25 USAA980350 1 19980824 A 5311 65465521 FRAME BOEING 737 737401 1384701 NM BS 827 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 827 BETWEEN S8R AND S9R ON FRAME. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998092500387 19980925 00387 CE 1998 9 25 MASA98157 1 19980821 A 5220 1295140012 EMERGENCY DOOR BEECH 1900 1900D 1154162 CE FUSELAGE MIS-ALIGNED A MASA O OTHER O OTHER IN INSP/MAINT 1 SW 07 23YV UE23 FLT 5320 - FLL-TPA - DURIG PRE-FLIGHT WALK AROUND, CREW NOTICED THAT THE RIGHT REAR EMERGENCY EXIT EXTERIOR HANDLE WAS N OT FLUSH WITH THE DOOR. MAINTENANCE REMOVED AND REINSTALLED THE DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998092500388 19980925 00388 CE 1998 9 25 MASA98156 1 19980819 A 7110 118910027689 COWLING BEECH 1900 1900D 1154162 CE RT NACELLE LOOSE A MASA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 SW 07 13ZV UE13 FLT 5425 - ACY-BWI - AFTER DEPARTURE, CREW OBSERVED THE RIGHT UPPER COWLING WAS LOOSE. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. THE COWLING WAS RESECURED AND THE AIRCRAFT WAS RETURNED T O SERVICE. (M) 2 L 7 2 4T RT A24CE 1998092500389 19980925 00389 CE 1998 9 25 MASA98154 1 19980813 A 5260 12951407619 HANDLE BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR BROKEN A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 54YV UE54 FLT 445 - ROW-ABQ - PRIOR TO DEPARTURE, AS THE CREW SECURED THE AIRSTAIR DOOR, THE DOOR HANDLE BROKE. THE DOOR WAS OPEN ED FROM THE OUTSIDE AND THE PASSENGERS WERE DEPLANED. MAINTENANCE REMOVED AND REPLACED THE DOOR HANDLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998092500390 19980925 00390 NM 1998 9 25 EISA98210 1 19980825 A 3230 MLG BOEING 727 72731 1384010 NM RT MLG LACK OF LUBE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 240NE 18906 RIGHT MAIN LANDING GEAR WILL NOT RETRACT, INDICATORS SHOW RIGHT MAIN GEAR UNSAFE AND RIGHT DOOR OPEN WHEN HANDLE IS MOVE D TO OFF RIGHT MAIN SHOWS IMMEDIATE GREEN. PERFORMED GEAR RETRACTION AND EXTENSION TEST. LUBED ALL GEAR FITTINGS PER M M 32. OPS CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998092500391 19980925 00391 NM 1998 9 25 EISA98211 1 19980825 A 3232 FITTING BOEING 727 72731 1384010 NM RT MLG LOOSE A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 240NE 18906 RIGHT MAIN LANDING GEAR WILL NOT RETRACT, INDICATORS SHOW RIGHT MAIN GEAR UNSAFE AND RIGHT DOOR OPEN WHEN HANDLE IS MOVE D TO OFF RIGHT MAIN SHOWS IMMEDIATE GREEN. FOUND BOLTS LOOSE ON RIGHT GEAR DOOR ACTUATOR FITTINGS. TIGHTENED BOLTS TO PROPER TORQUE, RIGGED DOOR OPS CHECK GOOD PER MM 32-12-1 PAGE 504. (M) 2 L 7 3 4F A3WE 1998092500392 19980925 00392 SO 1998 9 25 C2XA98IA324 1 19980829 A 3350 1317 LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURNG PREFLIGHT INSPECTION, THE CREW REPORTED THE LEFT FORWARD FUSELAGE EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAI NTENANCE REMOVED AND REPLACED THE BULB IN THE AFFECTED LIGHT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500393 19980925 00393 SO 1998 9 25 C2XA98IA321 1 19980824 A 3233 1959500007 ACTUATOR EMB 120 EMB120RT SO LT MLG OUT OF ADJUST A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 16719 120138 IAH - DURING FLT 3814, THE PILOT REPORTED THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT. MAINTENANCE FOUND THE LEFT MAIN GEAR ACTUATOR TO BE OUT OF ADJUSTMENT. THE ACTUATOR WAS ADJUSTED AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500394 19980925 00394 SO 1998 9 25 C2XA98IA320 1 19980824 A 3350 W220192522N LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15721 120160 IAH - DURING PREFLIGHT INSPECTION, THE PILOT REPORTED THE MID FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPA IRED A WIRE UNDER THE FLOOR AT FRAME 28, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500395 19980925 00395 CE 1998 9 25 C2XA98IA319 1 19980825 A 6120 A3026 BLOCK UNIT BEECH 1900 1900D 1154162 CE NR 2 PROP FAILED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 09 17534 UE141 IAH - DURING FLIGHT 3992, THE PILOT REPORTED THE NR 2 PROP FEATHERED, UNCOMMANDED, IN FLIGHT. THE AIRCRAFT RETURNED AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BETA BLOCK ASSEMBLY. SUBSEQUENTLY, THE PROPELLER ASSY, AND GOVERNOR ASSY WERE ALSO CHANGED DUE TO FEATHERING IN FLIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A24CE 1998092500396 19980925 00396 EU 1998 9 25 C2XA98IA323 1 19980826 A 5320 1340422103 BRACKET AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19812 99 IAH - DURING C-CHECK INSPECTION, THE FLIGHT ATTENDANTS SEAT WAS FOUND TO BE CORRODED AT THE LEFT LOWER ATTACH POINT. MA INTENANCE REMOVED AND REPLACED THE LOWER LEFT ATTACH POINT BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500397 19980925 00397 NM 1998 9 25 USAA980356 1 19980824 A 5315 65468101 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION ON STATION 967 LBBL 5-0 FLOORBEAM. CORROSI ON TASK NR C53-107-02. REPAIRED ONE FLANGE UPPER CHORD PER SRM 53-00-51 FIG 203. (M) 2 L 7 2 4F RT A16WE 1998092500398 19980925 00398 NM 1998 9 25 USAA980355 1 19980824 A 5315 654581094 FLOORBEAM BOEING 737 737401 1384701 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH AREA OF CORROSION AROUND NUTPLATE HOLES STATION 312 L BL 12 TO RBL 12 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN A NEW 'T' CAP SECTION PER SRM 53-10-51 . (M) 2 L 7 2 4F RT A16WE 1998092500399 19980925 00399 EU 1998 9 25 C2XA98IA322 1 19980826 A 5320 S53678008268 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19812 99 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 36 RIGHT TO CENTER WAS FOUND TO HAVE CORROSION IN THE SCREW HOLE S. MAINTENANCE PERFORMED TWO DOUBLER REPAIRS IAW CONTINENTAL EXPERSS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310 -01037, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500400 19980925 00400 EU 1998 9 25 RAIA980814 1 19980824 A 2721 28456 SWITCH AEROSP ATR42 ATR42300 8680920 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 426TE 17533 228 FLT 7136 - STL - RUDDER TRIM INOPERATIVE. MAINTENANCE REMOVED AND REPLACED RUDDER TRIM SWITCH. (M) 2 H 7 2 4T RT A53EU 1998092500401 19980925 00401 NM 1998 9 25 USAA980354 1 19980824 A 5311 6546595205 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727G BETWEEN STRINGER 8R AND STRINGER 9R FRAME. INS TALLED DOUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1998092500402 19980925 00402 NM 1998 9 25 USAA980353 1 19980824 A 5311 6546595205 FRAME BOEING 737 737401 1384701 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727E BETWEEN S8R AND S9R FRAME. INSTALLED DOUBLER P ER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1998092500403 19980925 00403 NM 1998 9 25 USAA980357 1 19980824 A 5315 654581292 FLOORBEAM BOEING 737 737401 1384701 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AROUND CLIP NUT HOLE .5 INCH BY .5 INCH STATI ON 328 FLOORBEAM UPPER CHORD BL0. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-51 FIG 206. (M) 2 L 7 2 4F RT A16WE 1998092500404 19980925 00404 NM 1998 9 25 USAA980358 1 19980824 A 5311 6546593210 FRAME BOEING 737 737401 1384701 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 408US 29626 23878 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A SMALL CRACK .25 INCH AT RIVET HOLE FUSELAGE FRAME 500A BETWEEN S8L AND S9L. CUT OUT DAMAGE FILL AND DOUBLER PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1998092500405 19980925 00405 WP 1998 9 25 HALA9800298 1 19980822 A 2740 SPRING DOUG DC9 DC951 3022051 WP ELEVATOR BROKEN A HALA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 WP 13 601AP 47658 FLT 282 - HNL - PRIMARY STAB INOP DURING CLIMB-OUT, RESET C/B PER SOP. NO CHANGE. AIRCRAFT MADE AN UNEVENTFUL LANDING IN HNL. FOUND TWO EACH SPRINGS AT ELEVATOR SECTOR BROKEN. REPLACED SPRINGS, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998092500406 19980925 00406 NM 1998 9 25 TSAA9833451 1 19980810 A 3350 873100151 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 4 POSITION EMERGENCY FLOOR LIGHT ASSY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500407 19980925 00407 NM 1998 9 25 TSAA9833452 1 19980811 A 3350 6013211 BATTERY PACK BOEING 737 737230C 1384472 NM DISCHARGED CABIN A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED AFT SLIDE BATTERY POWER SUPPLY DUE TO LIGHT BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998092500408 19980925 00408 NM 1998 9 25 TSAA9833456 1 19980814 A 3350 86210066 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500409 19980925 00409 NM 1998 9 25 TSAA9833457 1 19980814 A 3350 8731002511 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED LEFT FORWARD ENTRY DOOR EXIT IDENTIFIER. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500410 19980925 00410 NM 1998 9 25 TSAA9833458 1 19980814 A 3350 8731002511 SIGN BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER DUE TO BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1998092500411 19980925 00411 NM 1998 9 25 TSAA9833459 1 19980817 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998092500412 19980925 00412 NM 1998 9 25 TSAA9833460 1 19980817 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998092500413 19980925 00413 EU 1998 9 25 C2XA98IA282 1 19980801 A 5210 S5217666400200 BOLT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CHIPPED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND PASSENGER DOOR FORWARD UPPER SHOOT BOLT PLATING CHIPPED. MAINTENANCE REMOVED AND REPLACED THE SHOOT BOLT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500414 19980925 00414 EU 1998 9 25 C2XA98IA283 1 19980801 A 5320 S53971402264 SUPPORT AEROSP ATR42 ATR42320 8680930 EU FAIRING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND BELLY FAIRING SUPPORT FRAME NR 27 CRACKED ON RIGHT SIDE WEB SUPPORT DOUBLER. MAI NTENANCE REMOVED AND REPLACED THE SUPPORT DOUBLER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1998092500415 19980925 00415 EU 1998 9 25 C2XA98IA284 1 19980801 A 5240 S5247764300200 BOLT AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR CHIPPED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND SERVICE DOOR TOP FORWARD SHOOT BOLT PLATING CHIPPED. MAINTENANCE REMOVED AND REP LACED THE SHOOT BOLT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998092500416 19980925 00416 EU 1998 9 25 C2XA98BT062 1 19980819 A 3230 F96GA0102 CONTROL LEVER AEROSP ATR42 ATR42320 8680930 EU COCKPIT FAILED A C2XA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SW 09 26826 172 CREW REPORTED 'UPON GEAR DOWN SELECTION, GEAR WARNING SYSTEM INTERMITTENT. MAINTENANCE FOUND A LANDING GEAR CONTROL LEV ER FAULTY. REMOVED AND REPLACED WITH SERVICEABLE UNIT AND OPS CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1998092500417 19980925 00417 SO 1998 9 25 C2XA98IA318 1 19980820 A 5313 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, STRINGER 10 ON THE RIGHT INBOARD WING WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A SPLICE REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND THE AIRCRAFT WAS AP PROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500418 19980925 00418 SO 1998 9 25 C2XA98IA317 1 19980820 A 5720 12061431607 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHEC INSPECTION, THE NR 4 FROM AFT UPPER SKIN SUPPORT ON RIB 15 OF THE RIGHT WING WAS FOUND TO BE CRACKED . MAINTENANCE REMOVED AND REPLACED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500419 19980925 00419 SO 1998 9 25 C2XA98IA316 1 19980820 A 5320 12006159501 BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED FROM FRAME 34.5 TO 37. MAINTENANCE REMO VED AND REPLACED THE AFFECTED SECTION OF CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500420 19980925 00420 SO 1998 9 25 C2XA98IA315 1 19980820 A 5320 12004471002 BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE SKIRTING SECTION OF THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED AT FRAME 38. MA INTENANCE PERFORMED A SPLICE REPAIR OF THE AFFECTED SECTION, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500421 19980925 00421 SO 1998 9 25 C2XA98IA314 1 19980820 A 5320 12030303003 SUPPORT EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE FLUSH VALVE SUPPORT WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLUSH VALVE SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500422 19980925 00422 SO 1998 9 25 C2XA98IA313 1 19980820 A 5320 12022670001 ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE VERTICLE STIFFENERS WERE FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPA IR IAW EMB120 SRM 51-70-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500423 19980925 00423 SO 1998 9 25 C2XA98IA312 1 19980820 A 5320 12027929001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 38. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500424 19980925 00424 NM 1998 9 25 AALA981496 1 19980811 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 629 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - STRINGER CRACKED ON TOP OF RIB AT WING LT STATION 629 AFT OF FUEL DUMP TUBE 5TH OPENING FROM TIP. INSTALLED STRIN GER REPAIR PER BOEING SB 727-57A159. (M) 2 L 7 3 4F A3WE 1998092500425 19980925 00425 NM 1998 9 25 AALA981495 1 19980811 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - SHEAR TIE CORRODED STATION 720B BETWEEN STRINGER 20R AND 26R. REPLACED SHEAR TIE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998092500426 19980925 00426 NM 1998 9 25 AALA981536 1 19980814 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1050 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND CORROSION ON BELLFRAME STATION 1050 BETWEEN STATION 26L AND 28L. REMOVED CORROSION AND TREATED PER SRM 51-2 0-0 AND REPAIRED PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998092500427 19980925 00427 NM 1998 9 25 TSAA9833466 1 19980817 A 3350 8731002511 LIGHT BOEING 737 7372S5C 1384499 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 RIGHT SIDE EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REPLACED LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1998092500428 19980925 00428 NM 1998 9 25 TSAA9833467 1 19980817 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 RT SIDE EMERGENCY EXIT IDENTIFIER BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500429 19980925 00429 NM 1998 9 25 TSAA9833468 1 19980817 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 2 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500430 19980925 00430 NM 1998 9 25 TSAA9833469 1 19980817 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 3 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500431 19980925 00431 NM 1998 9 25 TSAA9833470 1 19980817 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 4 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500432 19980925 00432 NM 1998 9 25 TSAA9833471 1 19980817 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 5 POSITION EMERGENCY LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500433 19980925 00433 NM 1998 9 25 TSAA9833472 1 19980822 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED BATTERY PACK AT THE RT EMERGENCY DOOR EXIT IDENTIFIER DO TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500434 19980925 00434 NM 1998 9 25 TSAA9833473 1 19980822 A 3350 8731002511 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED RIGHT EMERGENCY EXIT DOOR IDENTIFIER DO TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998092500435 19980925 00435 NM 1998 9 25 TSAA9833474 1 19980823 A 3350 873100151 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998092500436 19980925 00436 NM 1998 9 25 MZZA98186 1 19980720 A 3230 656021132 ACCESSORY UNIT BOEING 727 727264 138408M NM E/E BAY FAILED A MZZA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 623DH 0399 20895 FLT 891 - MNL - AFTER TAKEOFF GEAR LEVER WOULD NOT RETRACT. GEAR HANDLE WOULD NOT PASS OFF POSITION. DUMP FUEL AND RET URN TO MNL. MAINTENANCE T/S SYSTEM FOUND L/G ACCESSORY UNIT AT FAULT. REMOVED AND REPLACED L/G ACCESSORY UNIT AND PERF ORMED OPS CHECKED PER MM 32-09-121. OPS CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 3 4F A3WE 1998092500437 19980925 00437 SO 1998 9 25 C2XA98IA311 1 19980820 A 5320 12046963001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 17 TO FRAME 20. MAINTENANCE RE MOVED AND REPLACED THE AFFECTED BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998092500438 19980925 00438 EU 1998 9 25 REXA98108 1 19980823 A 3230 AIR8641212 DOWNLOCK ACT SAAB SF340 340B 7860101 EU LT MLG LEAKING A REXA O OTHER K FLUID LOSS NR NOT REPORTED 1 SO 25 368PX LK9102058 340B274 LOST MAIN HYD PRESSURE AND QUANTITY GAUGE DROPPED TO ZERO. REMOVED AND REPLACED LEFT DOWN LOCK ACTUATOR. (M) 2 L 7 2 4T RT A52EU 1998092500439 19980925 00439 NM 1998 9 25 P2EA98165 1 19980826 A 5330 SKIN BOEING 737 737297 1384480 NM BS 436-449 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - EVALUATE DENT AFT OF STATION 440 AND RIGHT OF STRINGER 27R, LOWER BELLY SKIN BELOW FORWARD CARGO DOOR THRESHOLD SR M 53-30-1 FIG 1 DETAIL 3. REPAIRED FUSELAGE SKIN DUE TO DENT BETWEEN BS 436 AND BS 449, BETWEEN STRINGERS 26R AND 29R R EF SRM 53-30-3FIG 6. (M) 2 L 7 2 4F A16WE 1998092500440 19980925 00440 NM 1998 9 25 P2EA98164 1 19980827 A 5330 SKIN BOEING 737 737297 1384480 NM BS 945-955 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - EXTERIOR FUSELAGE, AFT ENTRY DOORWAY LOWER HINGE CUTOUT CRACKED. REPAIRED FUSELAGE SKIN AT AFT ENTRY DOOR LOWER H INGE CUTOUT REF SRM 53-30-3 FIG 34. DUE TO CRACK, REPAIRED SKIN BETWEEN BS 945 AND BS 955 FROM STRINGER 13L TO 16L. (M ) 2 L 7 2 4F A16WE 1998092500441 19980925 00441 NM 1998 9 25 PCAA9800779 1 19980811 A 7921 45E041 VALVE DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE FAILED A PCAA E D ENGINE SHUTDOWN RETURN TO BLOCK J Y WARNING INDICATION ENGINE STOPPAGE TO TAKEOFF 1 EA 13 832EX 280 UPON TAKEOFF FROM BOS, THE NR 1 ENG TEMP EXCEEDED 125 DEGREES. THE CREW SECURED THE ENGINE AND RETURNED TO FIELD. LAND ING WAS WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE OIL TEMP SYSTEM. REMOVED AND REPLACED THE OIL COOLER DIVERTER VA LVE, OIL TEMP BULB AND REPAIRED A BROKEN WIRE AT THE NR 1 ENGINE OIL TEMP BULB ELECTRICAL CONNECTOR. GROUND RAN ENGINE. OPERATIONAL AND LEAK CHECKS PROVED SATISFACTORY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998092500442 19980925 00442 1998 9 25 PCAA9800780 4 19980816 A 3442 066308601 INDICATOR DHAV DHC8 DHC8102 2809003 NM RADAR FAILED A PCAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 13 838EX 3143 220 FLT 3770 - AT 13,000 FT, SMOKE REPORTED COMING FROM LOWER INSTRUMENT PANEL BY CO-PILOTS KNEE, SMOKE EVACUATED BY STANDAR D PROCEDURES. AIRCRAFT DIVERTED TO BDL AND LANDED WITHOUT INCIDENT. MAINTENANCE ISOLATED PROBLEM TO RADAR INDICATOR UN IT. INSPECTED WIRING. REPLACED WEATHER RADAR INDICATOR AND OPERATIONALLY TESTED NORMAL. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998092500443 19980925 00443 NM 1998 9 25 PCAA9800781 1 19980826 A 2611 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY MALFUNCTIONED A PCAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 13 817EX 191 EN ROUTE TO ISP, AIRCRAFT DIVERTED INTO ACY DUE TO BAG BAY SMOKE DETECTOR WARNING ILLUMINATED. CREW INSPECTED BAG COMPA RTMENT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. THE FLIGHT ATTENDANT DID REPORT A FOUL SMELL OF AEROSOL THROUGHOUT THE C ABIN. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. REMOVED AND REPLACED THE FORWARD DETECTOR AND INOPPED THE AFT DETECT OR UNDER MEL PROVISIONS AS A PRECAUTIONARY MEASURE. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998092500444 19980925 00444 NM 1998 9 25 MASA98168 1 19980901 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 FLT 5183 - PHX-TEX - CREW REPORTED THE EMERGENCY LIGHTING THROUGHOUT THE CABIN WOULD NOT ILLUMINATE. MAINTENANCE REMOVE D AND REPLACED ALL SIX POWER SUPPLIES. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998092500445 19980925 00445 NM 1998 9 25 MASA98169 1 19980903 A 3350 S102 BATTERIES DHAV DHC8 DHC8202 2809007 NM COCKPIT DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 436YV 436 DURING A ROUTINE MAINTENANCE CHECK, MAINTENANCE PERSONNEL FOUND THE PORTABLE EMERGENCY LIGHT TO BE DIM. MAINTENANCE REM OVED THE BATTERIES, DEEP CYCLED AND REINSTALLED THEM IN THE LIGHT ASSEMBLY. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998092500446 19980925 00446 NM 1998 9 25 MASA98145 1 19980719 A 3350 10005511 LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE, FOUND PORTABLE EMERGENCY LIGHT WOULD NOT ILLUMINATE DUE TO BATTERY LOW VOLTAGE. DEEP CYCLED BATTERIES, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998092500447 19980925 00447 NM 1998 9 25 MASA98148 1 19980727 A 3350 40005130003 SWITCH DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 DURING ROUTINE MAINTENANCE, FOUND THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH WOULD NOT TURN EMERGENCY LIGHTS ON. MAIN TENANCE REPLACED THE SWITCH, OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998092500448 19980925 00448 NM 1998 9 25 MASA98147 1 19980726 A 3350 MS1557081 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 445YV 445 DURING ROUTINE MAINTENANCE, FOUND THE EXTERNAL EMERGENCY EGRESS LIGHT ON THE RIGHT AFT WOULD NOT ILLUMINATE. MAINTENANC E REPLACED THE LIGHT BULB. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998092500449 19980925 00449 NM 1998 9 25 MASA98172 1 19980808 A 5210 NAS428H415 BOLT DHAV DHC8 DHC8202 2809007 NM PAX DOOR OUT OF ADJUST A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 447YV 447 FLT 5225 - YUM-PHX - AFTER ARRIVAL IN PHX, CREW FOUND THE MAIN CABIN DOOR HARD TO OPEN FROM THE OUTSIDE. MAINTENANCE RE SHIMMED THE HANDLE STOP BOLT. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998092500450 19980925 00450 WP 1998 9 25 GTIA9800100 1 19980827 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 937-950 TORN A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 942ML 47478 DTW - AT GATE, BAGGAGE CART DRIVER INTO RT AFT OF AIRCRAFT. PUNCTURE IN SIDE OF FUSELAGE JUST AFT OF BAGGAGE DOOR. PER FORMED FUSELAGE SKIN EXTERNAL RPAIR FROM FS 937 TO FS 950 BETWEEN L23R AND L26R IAW 08-98-53-012 FROM 8-28-98. DRAWING 53-98445-1 PAINTED AREA IAW DC-9 SRM 53-10-3. (M) 2 L 7 2 4F A6WE 1998092500451 19980925 00451 NM 1998 9 25 EISA98213 1 19980827 A 7933 INDICATOR BOEING 727 727223 1384074 NM COCKPIT MALFUNCTIONED A EISA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SW 07 6813 19488 NR 2 ENGINE OIL TEMP EXCEEDED RED LINE DURING FLIGHT. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED PER FLIGHT MANUAL. FO UND NR 2 OIL TEMP BULB GROUND WIRE BROKEN AT TERMINAL BLOCK. SPLICED WIRE ON TERMINAL BLOCK IAW MM CHAPTER 20. (M) 2 L 7 3 4F A3WE 1998092500452 19980925 00452 WP 1998 9 25 ARWA980813 1 19980826 A 3030 851CU1 HEAT DOUG DC8 DC863F 302198F WP PITOT INOPERATIVE A ARWA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 19 441J 139428 45988 SJU - FLT 759 - GROUND TURN BACK, F/O'S PITOT HEAT INOP. REMOVED AND REPLACED PITOT TUBE ASSY. OPS NORMAL IAW MM 30-30 -0. SATISFACTORY LEAK CHECK IAW MM 34-12-0. (M) 2 L 7 4 4F 4A25 1998092500453 19980925 00453 WP 1998 9 25 AALA981575 1 19980821 A 3350 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 495AA 49733 DFW - DURING OVERNIGHT MANTENANCE, BOTH AFT EMERGENCY FLIGHT ATTENDANT FLASHLIGHTS INOPERATIVE. REPLACED THE TWO AFT FL IGHT ATTENDANT EMERGENCY FLASHLIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500454 19980925 00454 WP 1998 9 25 AALA981538 1 19980816 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7546A 53028 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE RELEASE HANDLE EMERGENCY FLOOR LIGHT INOPERATIVE. REPLACED ENVIRONMENTAL SPLICE ON TAIL CONE RELEASE HANDLE EMERGENCY FLOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500455 19980925 00455 WP 1998 9 25 AALA981539 1 19980816 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7546A 53028 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIRS EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. REPAIRED WIRE ON AFT STAIRS EMER GENCY EXIT FLOOR LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500456 19980925 00456 WP 1998 9 25 AALA981540 1 19980813 A 3350 P2070003001 FLASHLIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7546A 53028 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLIGHT ATTENDANT FLASHLIGHT AT FORWARD ENTRY INOPERATIVE. REPLACED EMERGE NCY FLIGHT ATTENDANT FLASHLIGHT AT FORWARD ENTRY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500457 19980925 00457 WP 1998 9 25 AALA981541 1 19980816 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7546A 53028 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM WING EXITS AFT INOPERATIVE. REPAIRED WIRE I N EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500458 19980925 00458 WP 1998 9 25 AALA981569 1 19980819 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 276AA 49273 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500459 19980925 00459 WP 1998 9 25 AALA981571 1 19980819 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7544A 53026 SFO - DURING OVERNIGHT MAINTENANCE, THE EMERGENCY EXIT FLOOR PATH LIGHTS AT 21D INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998092500460 19980925 00460 NM 1998 9 25 AALA984183 1 19980831 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 764 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7375A 25202 AFW - FLOORBEAM AT STATION 764 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINE BLENDED AREA. FABRICATE STRAP FROM STAI NLESS STEEL. APPLY TWO COATS PRIMER TO STRAP AND FLOORBEAM. FILL BLENDED AREA WITH BMS5-92 TYPE 1. (M) 2 L 7 2 4F RT A1NM 1998092500461 19980925 00461 NM 1998 9 25 AALA984182 1 19980831 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 376AN 25445 AFW - FLOORBEAM AT STATION 347 RBL 46 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT ALL CORROSION. ALODINED ALL BARE ALUMINUM SURFACES, APPLIED TWO COATS OF BMS 10-11 PRIMER AND FILLED BLENDS WITH BMS 5-92 PER SRM. (M) 2 L 7 2 4F RT A1NM 1998092500462 19980925 00462 NM 1998 9 25 AALA984181 1 19980831 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 938 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 376AN 25445 AFW - FLOORBEAM AT STATION 938 LBL 33.06 HAD GOUGE BLENDED BEYOND SRM LIMITS. BLENDED OUT GOUGE. ROTO/FLAP PEENED BLEN DED AREA. ALODINED AREA. APPLIED TWO COATS OF BMS 10-11 PRIMER AND FILLED BLENDED AREA WITH BMS 5-92 PER SRM. (M) 2 L 7 2 4F RT A1NM 1998092500463 19980925 00463 NM 1998 9 25 AALA984180 1 19980831 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 376AN 25445 AFW - FLOORBEAM AT STATION 1480 LBL 50 AND 60 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT CORROSION. ALODINED ALL BARE ALUMINUM SURFACES. APPLIED TWO COATS OF BMS 10-11 PRIMER AND FILLED BLENDS WITH BMS 5-92 PER SRM. (M) 2 L 7 2 4F RT A1NM 1998092500464 19980925 00464 NM 1998 9 25 AALA984179 1 19980831 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 376AN 25445 AFW - FLOORBEAM AT STATION 347 RBL 82 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT ALL CORROSION. ALODINED ALL BARE ALUMINUM SURFACES, FINISHED BLENDED AREAS WITH TWO COATS OF BMS 10-11. PRIMED AND FILLED BLENDS WITH BMS 5092 PER SRM 53-00-51 FIG 101. (M) 2 L 7 2 4F RT A1NM 1998092500465 19980925 00465 WP 1998 9 25 AALA981542 1 19980814 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 180 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 437AA 49455 TUL - FWD SERVICE DOOR PAN GOUGED SEVERAL PLACES. BLENDED GOUGED DYE CHECKED, INSTALLED DOUBLER IAW ESO 80559, DATE 8-1 4-98. (M) 2 L 7 2 4F A6WE 1998092500466 19980925 00466 WP 1998 9 25 AALA981579 1 19980817 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 693 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 437AA 49455 TUL - FOUND CRACK IN SKIN AT AFT SIDE OF CX DOOR CUTOUT BETWEEN L23R AND L24R AT ES 693. REPAIRED IAW 53-30-00-6. (M) 2 L 7 2 4F A6WE 1998092500467 19980925 00467 WP 1998 9 25 AALA981580 1 19980817 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 437AA 49455 TUL - LONGERON 2R CRACKED AFT OF FS 1418. REPAIRED IAW 53-30-00-2. (M) 2 L 7 2 4F A6WE 1998092500468 19980925 00468 NM 1998 9 25 TWAA9815301 1 19980917 A 5755 SKIN BOEING 727 727231 1384079 NM NR 3 SPOILER DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54345 21632 FOUND LT WING NR 3 SPOILER WITH TE DELAMINATED APPROX ONE INCH. APOXY FILLED AND INSTALLED TACK RIVETS PER 51-40-6, FIG 26. CHECK-C 6-12-98 MCI. 2 L 7 3 4F A3WE 1998092500469 19980925 00469 WP 1998 9 25 TWAA9815302 1 19980916 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP RT MLG WW CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING CHECK-C MAINT, FOUND IN RT GEAR WHEEL WELL LOWER RT FWD KEEL BEAM SELF SUPPORT CRACKED 60 PERCENT THRU, HAD ONLY BEEN STOP DRILLED. CRACK LOCATED FWD OF WHEEL WELL DOOR ACTUATOR. 2 L 7 2 4F A6WE 1998092500470 19980925 00470 WP 1998 9 25 TWAA9815303 1 19980916 A 5312 BULKHEAD WEB DOUG DC9 DC931 3022065 WP BS 1121 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING CHECK-C MAINT, FOUND AFT FUSELAGE STA 1121 WITH 2 INCH CRACK IN CANTED BULKHEAD WEB BELOW LOUVERS ON LT SIDE. ST OP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 53-01, FIG 2 PAGE 9. 2 L 7 2 4F A6WE 1998092500471 19980925 00471 WP 1998 9 25 TWAA9815304 1 19980916 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 1076 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING CHECK-C MAINT, IN AFT ACCY COMPT FOUND FORMER CRACKED AT ATTACH POINT TO LONGER 2L AT STA 1076. REMOVED DAMAGED SECTION AND INSTALLED DOUBLERS PER DC9 SRM 53-03, FIG 32. 2 L 7 2 4F A6WE 1998092500472 19980925 00472 WP 1998 9 25 TWAA9815305 1 19980917 A 5280 ANGLE DOUG DC9 DC931 3022065 WP RT MLG DOOR DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING CHECK-C MAINT, FOUND RT MAIN LANDING GEAR I/B DOOR DAMAGE WITH CRACK IN FWD Z' ANGLE UPPER FLANGE AND THE BUMPER PUSHED IN. REPAIRED PER SRM 52-05, FIG 14 PAGE 25. ALSO REF DRAWING 5910161, HIGH FREQ EDDY CURRENT AND CRACK CONTAINE D PER 51-00-03 PAGE 17. 2 L 7 2 4F A6WE 1998092500473 19980925 00473 WP 1998 9 25 TWAA9815306 1 19980917 A 5532 SKIN DOUG DC9 DC931 3022065 WP VERT STAB CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING CHECK-C MAINT, FOUND ON VERT STAB LT SIDE, A GROOVE BLENDED BEYOND LIMITS PER SRM 53-01, PG 6 FIG 1, IN SKIN BELO W LT HORIZ STAB. ACCOMP EDDY CURRENT OF AREA PER 51-00-03 AND NO CRACKS FOUND. REPAIRED PER ARA 15375. 2 L 7 2 4F A6WE 1998092500474 19980925 00474 WP 1998 9 25 TWAA9815307 1 19980917 A 5711 SPAR DOUG DC9 DC931 3022065 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 986Z 47589 DURING CHECK-C MAINT, FOUND LT WING AFT SPAR WITH EDDY CURRENT INDICATION OF 1.25 INCH CRACK IN AFT SPAR WEB, .75 INCH B ELOW O/B LOWER BOLT HOLE FOR O/B FLAP HINGE CASTING. INSTALLED REPAIR PER ROD DRAWING 95-12-06-018, AND ARA 15388. 2 L 7 2 4F A6WE 1998092500475 19980925 00475 WP 1998 9 25 TWAA9815308 1 19980916 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 237-313 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT BEAM WITH CORROSION, STA 237 TO 313. REPLACED SUPPORT ANGLE STA 23 7 TO 258. REMOVED CORROSION FROM STA 258 TO 313. 2 L 7 2 4F A6WE 1998092500476 19980925 00476 WP 1998 9 25 TWAA9815309 1 19980916 A 5321 FLOOR DOUG DC9 DC931 3022065 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 19 WITH CORROSION AND SEVERAL BROKEN SUPPORT CHANNELS. REPLACED CABIN FL OOR PANEL SHEET/HAT SECTION PER SRM 53-00-14, PAGE 201. 2 L 7 2 4F A6WE 1998092500477 19980925 00477 WP 1998 9 25 TWAA9815310 1 19980916 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP CABIN BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 34 WITH BROKEN SUPPORT CHANNELS. REMOVED AND INSTALLED NEW SUPPORT CHANN ELS. 2 L 7 2 4F A6WE 1998092500478 19980925 00478 WP 1998 9 25 TWAA9815311 1 19980917 A 5321 FLOOR DOUG DC9 DC931 3022065 WP CABIN CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND FLOOR PANEL NR 20 WAS CORRODED THROUGH AND HAD BROKEN SUPPORT CHANNELS. FABRICATED NEW FLOOR PANEL PER SRM 53-00-64, FIG 201 PAGE 201. 2 L 7 2 4F A6WE 1998092500479 19980925 00479 WP 1998 9 25 TWAA9815312 1 19980917 A 5313 STRINGER DOUG DC9 DC931 3022065 WP BS 200 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND STRINGER 2L CRACKED AT BOTH SIDE FLANGES AT STA 200. REPLACED LONGERON MFG PART NR 5911 406-13, USING FASTENERS PER SRM 51-30-0. 2 L 7 2 4F A6WE 1998092500480 19980925 00480 WP 1998 9 25 VJ9800412 1 19980921 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 914VV 47486 FWD ENTRY DOOR EVAC SLIDE LOOSE FROM CASE. RESECURED SLIDE PACK LATCH AND COVER PER MM 25-51. 2 L 7 2 4F A6WE 1998092500481 19980925 00481 WP 1998 9 25 VJ9800413 1 19980920 A 3350 P4010021 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 925VV 47319 F/A REPORTED LOOSE WIRES SHOWING FLOOR LIGHTS. INSTALLED LOOSE WIRES AND REPLACED PATHWAY BATTERY PACK FOR BLOWN FUSE, OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998092500482 19980925 00482 WP 1998 9 25 VJ9800414 1 19980920 A 3520 11504012 MANIFOLD DOUG DC9 DC932 3022066 WP PAX OXY SYST FAILED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 921VV 47284 PAX O2 SYSTEM INOP. LEAKING O2 BOTTLE OFF FOR PAX SYSTEM. REMOVED AND REPLACED ROW 23B PSU MANIFOLD. RESTOWED MASK PI N IN AFT F/A MASK. 2 L 7 2 4F A6WE 1998092500483 19980925 00483 EU 1998 9 25 MALA976193 1 19980916 A 7933 4053T73P01 TEMP SENSOR SAAB SF340 SF340A 7850100 EU RT PROP FAILED A MALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 GL 15 115XJ 340A115 RIGHT PROP OIL TEMP RED LINED, ALL OTHER PARAMETERS NORMAL. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED RIGHT PGB O IL TEMP SENSOR IAW SF340 AMM 79-30-10. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998092500484 19980925 00484 EU 1998 9 25 MALA976194 1 19980917 A 2520 TRIM PANEL SAAB SF340 SF340A 7850100 EU EMER EXIT DOOR LOOSE A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 79XJ 079 PLASTIC COVER ON EXIT DOOR 6CD IS LOOSE. MAINTENANCE RESECURED TRIM PANEL, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998092500485 19980925 00485 NM 1998 9 25 MALA976195 1 19980917 A 3260 387 BULB DHAV DHC8 DHC8102 2809003 NM LT & RT MLG FAILED A MALA K NONE N FALSE WARNING NR NOT REPORTED 1 GL 15 846MA 344 LEFT AND RIGHT MAIN LANDING GEAR DOWN AND LOCKED GREEN LIGHTS HAVE ONE LIGHT BURNED OUT. MAINTENANCE REPLACED LEFT AND RIGHT MAIN LANDING GEAR DOWN AND LOCKED GREEN LIGHTS, OPS CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998092500486 19980925 00486 NM 1998 9 25 K3HA980111 1 19980915 A 3350 252005 FUSE BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY LIGHT OUT ROW 5 FORWARD. REPLACED FUSE IN BATTERY PACK, OPS CHECK OF LIGHT MM 33-59-0. 2 L 7 3 4F A3WE 1998092500487 19980925 00487 NM 1998 9 25 AWXA9800205 1 19980916 A 2750 6573271 TORQUE TUBE BOEING 737 7373G7 1384595 NM LT TE FLAP WORN A AWXA K NONE F FLT CONT AFFECTED LD LANDING 1 WP 28 160AW 23782 FLAPS DID NOT MOVE AS INDICATED ON FORWARD PANEL. FLAPS SPLIT, RIGHT FLAP 15 DEGREES, LEFT 30 DEGREES. FOUND LEFT FLAP DRIVE TORQUE TUBE COMPLETELY WORN THROUGH BY INTERFERENCE WITH FIRE BOTTLE BRAIDED HOSE. HOSE INSTALLED UPSIDE DOWN. I NSTALLED HOSE CORRECTLY. LEAK CHECKED GOOD. INSTALLED NEW TORQUE TUBE AND SAFETIED. FLAP UPSTOPS 180 DEGREES. FLAPS OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1998092500488 19980925 00488 SO 1998 9 25 RAAA98E9032 1 19980921 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 BOTH LT AND RT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCH ARGED. 2 L 7 4 4T 4A22 1998092500489 19980925 00489 WP 1998 9 25 CALA9801828 1 19980920 A 3610 39271012 VALVE DOUG DC9 DC982 3022082 WP RIGHT INOPERATIVE A CALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 SW 09 13891 30665 49102 WHEN ICE WAS ENCOUNTERED AT 26,000 FEET, THE ENGINE ANTI-ICE AND AIRFOIL ICE PROTECTION SYSTEM WAS ACTIVATED. IMMEDIATE LY AFTERWARDS THE L&R AC TEMP HIGH LIGHTS, L&R ICE PROTECTION HIGH LIGHTS, ICE PROTECTION SUPPLY PRESSURE LIGHT AND AIRF OIL PROTECTION LIGHT ILLUMINATED AND SMOKE ENTERED THE COCKPIT. THE EFFECTED SYSTEMS WERE SHUTDOWN IAW WITH CHECKLIST P ROCEDURES AND THE SMOKE CLEARED. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT AUGMENTATION VALVE AT FAULT. THE RT AUGMENTATION VALVE WAS REMOVED AND REPLACED IAW MM 36-10-01. BOTH ENGINES W ERE RUN AND ALL SYSTEMS CHECKED GOOD. 2 L 7 2 4F A6WE 1998092500490 19980925 00490 NM 1998 9 25 CALA9801829 1 19980919 A 5321 FLOOR BOEING 727 727232 1384082 NM COCKPIT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND COCKPIT LT SIDE FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM ECRA 5320-01448. 2 L 7 3 4F A3WE 1998092500491 19980925 00491 NM 1998 9 25 CALA9801830 1 19980919 A 5754 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 5 SLAT INBOARD AND OUTBOARD RIBS AT ACTUATOR ROD END ATTACH POINT. BOTH THE INBOARD AND OUTBOARD RIBS WERE REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998092500492 19980925 00492 NM 1998 9 25 CALA9801831 1 19980921 A 2910 LINE BOEING 737 737214 138446R NM NR 1 ENGINE LEAKING A CALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 14239 19920 THE A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE WAS LOST AFTER TAKEOFF. A MANUAL GEAR EXTENSION WAS ATTEMPTED. THE NOSE G EAR DID NOT EXTEND ON FIRST PULL OF HANDLE. THE HANDLE WAS PULLED AGAIN AND THE GEAR EXTENDED BUT NOSE EXTENSION CABLE WOULD NOT RETRACT FULLY. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 1 ENG INE HYDRAULIC PRESSURE LINE BLOWN. THE HYDRAULIC LINE WAS REPLACED. THE ENGINE WAS RUN WITH NO LEAKS NOTED. MAINTENAN CE TESTED THE NOSE GEAR MANUAL EXTENSION PER MM 32-35-0. THE GEAR WAS CYCLED SEVERAL TIMES AND OPERATION CHECKED NORMAL . 2 L 7 2 4F A16WE 1998092500493 19980925 00493 NM 1998 9 25 CALA9801832 1 19980920 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 303.9 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND ANGLE CORRODED BELOW FORWARD FLIGHT ATTENDANT'S SEAT AT STA 303.9 FROM LBL 12 TO LBL 50. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-30-5, 53-10-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998092500494 19980925 00494 NM 1998 9 25 CALA9801833 1 19980920 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1132-1136 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1132-113 TO , RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5, FIGURE 7, 51-30-5, 51-10-2, 53-10-4, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998092500495 19980925 00495 NM 1998 9 25 CALA9801834 1 19980920 A 5320 SPLICE BOEING 727 727232 1384082 NM BS 720-730 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT FORWARD CARGO BUTT SPLICE NR 6 AND BUTT SPLICE AT BS 720 TO 730 CORRODED. NEW BUTT SPLICES WERE INS TALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, MM 51-20-11. 2 L 7 3 4F A3WE 1998092500496 19980925 00496 NM 1998 9 25 CALA9801835 1 19980921 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 178 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND NOSE RADOME AREA LOWER L-ANGLE CORRODED AT FS 178, LBL 6 TO RBL 6. THE ANGLE WAS REMOVED AND A NEW ANG LE WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 AND MM 51-20-0. 2 L 7 3 4F A3WE 1998092500497 19980925 00497 WP 1998 9 25 CALA9801836 1 19980919 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 160 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 160, LONGERON 26R. THE DENTED AREA WAS CUT OUT IAW ECRA 5331-01030. DOUBL ERS AND FILLER WERE INSTALLED IAW ECRA 5331-01030, SRM 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998092500498 19980925 00498 WP 1998 9 25 CALA9801837 1 19980919 A 5350 CABLE DOUG DC9 DC981 3022081 WP TAIL CONE OUT OF ADJ A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 THE AFT FUSELAGE TAIL CONE EXTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998092500499 19980925 00499 WP 1998 9 25 CALA9801838 1 19980919 A 5210 HINGE DOUG DC9 DC981 3022081 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 INSPECTION FOUND AFT ENTRY DOOR UPPER HINGE CRACKED. THE HINGE WAS REPLACED IAW SRM 51-00-0. 2 L 7 2 4F A6WE 1998092500500 19980925 00500 NM 1998 9 25 CALA9801839 1 19980921 A 5755 651734754 SKIN BOEING 727 727232 1384082 NM NR 1 SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND NR 1 SPOILER CORRODED ALONG OUTBOARD EDGE AND DELAMINATED ON TOP. THE NR 1 SPOILER WAS REMOVED AND REP LACED IAW MM 27-61-1. 2 L 7 3 4F A3WE 1998092500501 19980925 00501 NM 1998 9 25 CALA9801840 1 19980921 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND LT OUTBOARD AFT FLAP OUTBOARD LOWER CORNER DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-61 -12. 2 L 7 3 4F A3WE 1998092500502 19980925 00502 NM 1998 9 25 CALA9801841 1 19980921 A 5755 SKIN BOEING 727 727232 1384082 NM NR 7 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND NR 7 SPOILER DELAMINATED AT LOWER OUTBOARD AFT TRAILING EDGE. THE NR 7 SPOILER WAS REMOVED AND REPLACE D IAW MM 27-61-1. 2 L 7 3 4F A3WE 1998092500503 19980925 00503 NM 1998 9 25 CALA9801842 1 19980921 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND RT WING INBOARD TRAILING EDGE AFT FLAP DELAMINATED AT OUTBOARD AND INBOARD TRAILING EDGE CORNER. THE F LAP WAS REMOVED AND REPLACED IAW MM 27-51-1. 2 L 7 3 4F A3WE 1998092500504 19980925 00504 NM 1998 9 25 CALA9801843 1 19980921 A 5755 SKIN BOEING 727 727232 1384082 NM NR 2 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND THE NR 2 SPOILER DELAMINATED AFT OF INBOARD HINGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27 -61-1. 2 L 7 3 4F A3WE 1998092500505 19980925 00505 NM 1998 9 25 CALA9801844 1 19980921 A 5755 SKIN BOEING 727 727232 1384082 NM NR 5 SPOILER CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND NR 5 SPOILER CORRODED ALONG TOP EDGES. THE NR 5 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1. 2 L 7 3 4F A3WE 1998092500506 19980925 00506 NM 1998 9 25 CALA9801845 1 19980921 A 5753 SKIN BOEING 727 727232 1384082 NM RT TE MIDFLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND THE RT WING INBOARD MIDFLAP CORRODED AROUND TWO RIVETS ON UPPER SURFACE. THE FLAP WAS REMOVED AND REPL ACED IAW MM 27-51-1. 2 L 7 3 4F A3WE 1998092500507 19980925 00507 1998 9 25 COMA9810218 3 19980921 A 6111 TAPE EMB 120 EMB120RT SO LEFT PROP BLADE LOOSE A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 268CA 120262 CREW HEARD STRANGE NOISE FROM LEFT HAND SIDE OF AIRCRAFT. REPLACED LOOSE EROSION TAPE ON LEFT HAND PROPELLER BLADES. 2 L 7 2 4T RT A31SO 1998092500508 19980925 00508 EA 1998 9 25 COMA9860268 1 19980921 A 3241 428853 CONTROL UNIT CNDAIR CL600 CL6002B19 EA ANTISKID SYST MALFUNCTION A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 941CA 10130 7050 ANTISKID MESSAGE DURING TAXI. REPLACED THE ANTISKID CONTROL UNIT. 2 L 7 2 4F RT A21EA 1998092500509 19980925 00509 1998 9 25 COMA9860269 4 19980921 A 3442 6229302003 ANTENNA CNDAIR CL600 CL6002B19 EA FWD FUSELAGE FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 935CA 9209 9 7043 RADAR FAULT INDICATION. REPLACED ANTENNA. 2 L 7 2 4F RT A21EA 1998092500510 19980925 00510 WP 1998 9 25 UPS98827689 1 19980827 A 5751 5705321510 WEIGHT DOUG DC8 DC871F 302199D WP RT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-C, RT WING I/B AILERON BALANCE WEIGHT IS CORRODED. REMOVED AND REPLACED I/B AILERON IAW MM 27-11-01. 2 L 7 4 4F RT 4A25 1998092500511 19980925 00511 1998 9 25 UPS98827697 2 19980919 A 7200 ENGINE DOUG DC8 DC871F 302199D WP NR 4 FLAMED OUT A IPXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 01 702UP 45902 INSPECTION TYPE-N/A AT FL 310, SET UP SUCTION FEED OFF OF NR 4 ALT TANK FUEL PRESSURE WAS INTIALLY AT 30 PSI THEN PRESSU RE FLUCTUATED FROM 30 PSI TO 0 PSI. FUEL PRESSURE STAYED AT 0 PSI AND THEN NR 4 ENG FLAMED OUT. ENGINE RESTARTED, OTH ER INDICATIONS NORMAL. RAN NR 4 ENG PER MM 71-00-00 AND CHK'D FOR LEAKS AND OPS CK ENGINE DRIVER PUMP PER 73-10-01. SY S TEST NORMAL WITHIN PARAMETER. 2 L 7 4 4F RT 4A25 1998092500512 19980925 00512 EU 1998 9 25 QXEA9801355 1 19980920 A 3350 2302 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 475AU 11222 FORWARD CABIN OVERHEAD EXIT SIGN JUST ABOVE CLOSET HAS SEVERAL BULBS OUT. MAINTENANCE REPLACED THE LIGHT ASSEMBLY, OPER ATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998092500513 19980925 00513 EU 1998 9 25 QXEA9801356 1 19980921 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 THE EMERGENCY EXIT SIGN ABOVE THE COCKPIT DOOR HAS LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED THE EXIT SIGN, OPERATIO NALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998092500514 19980925 00514 EU 1998 9 25 QXEA9801357 1 19980921 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 THE EMERGENCY EXIT SIGN ABOVE ROW 8 IS INOPERATIVE. MAINTENANCE RELAMPED THE EXIT SIGN, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998092500515 19980925 00515 EU 1998 9 25 QXEA9801358 1 19980919 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CARGO COMPT INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 AFT EXTERIOR UNDERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY IN AFT CARGO PIT. OPERATIONALLY TESTED IN ACCORDANCE WITH 33-50-01. NO DEFECTS NOTED. 2 L 7 2 4F RT A20EU 1998092500516 19980925 00516 EU 1998 9 25 QXEA9801359 1 19980919 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CARGO COMPT INOPERATIONS A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 FORWARD EXTERIOR UNDERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY IN FORWA RD CARGO PIT. OPERATIONALLY TESTED IN ACCORDANCE WITH 33-50-01. NO DEFECTS NOTED. 2 L 7 2 4F RT A20EU 1998092500517 19980925 00517 NM 1998 9 25 98UAL900450 1 19980911 A 2120 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E/E COMPT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 594UA 28145 DIVERTED TO DEN WHEN IT BECAME DIFFICULT TO MAINTAIN CABIN PRESSURE. *S/D* EQUIPMENT COOLING OVERBOARD EXHAUST VALVE F AILED. SHOP FOUND MOTOR BEARING FROZEN. SHOP REPLACED BEARING AND VALVE OPERATES CORRECTLY. 2 L 7 2 4F 4 F RT A2NM E17NE 1998092500518 19980925 00518 NM 1998 9 25 98UAL900451 1 19980910 A 2450 50086003 BREAKER BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE E & E BAY FAILED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 7258U 21405 RETURNED TO GATE WITH ELECTRICAL PROBLEMS. FOUND BUS PROTECTION PANEL CIRCUIT BREAKER POPPED AND ELECTRICAL SMELL IN E & E COMPARTMENT. *S/D* REPLACED FAILED NR 3 GENERATOR BREAKER. ALSO, REPLACED BUS PROTECTION PANEL AND GENERATOR CONT ROL UNITS PRECAUTIONARY. NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1998092500519 19980925 00519 1998 9 25 98UAL900452 4 19980905 A 2210 FMGC AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E & E COMPT MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 420UA 489 FMGC 1 AND 2 FROZEN. NO RESPONSE TO INPUTS. USED STANDBY NAV ON THE RMP'S. *S/D* RESET SYSTEM AND PERFORMED CAT III CAPABILITY PER AMM 22-97-00 AND AFFS TEST. ALL TEST PASSED, NO FAULTS PRESENT. CHECK PLR AND PFR WITH NO FAULTS DETECT ED. NO MORE PROBLEMS WITH FMGC SINCE THIS MRR. 2 L 7 2 4F 4 F RT A28NM E40NE 1998092500520 19980925 00520 EU 1998 9 25 98UAL900453 1 19980908 A 2121 FAN TECHNOFAN S EVT3454G AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE E & E COMPT FAILED A UALA H DEACTIVATE SYST/CIRCUITS B E J SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 419UA 3454G 487 HIGH PITCH VIBRATION UNDER FLIGHT DECK FLOOR. ACRID SMOKE SMELL AND ECAM MESSAGE FOR AVIONICS BLOWER FAULT. SWITCHED T O OVERRIDE POSITION. VIBRATION AND SMOKE CLEARED. *S/D* VIBRATION WAS CAUSED BY THE AVIONICS COOLING FAN. VIBRATION AND SMOKE CLEARED AFTER COOLING FAN REPLACEMENT. 2 L 7 2 4F 4 F RT A28NM E40NE 1998092500522 19980925 00522 NM 1998 9 25 98UAL900456 1 19980915 A 2612 3F17785502 FIRE LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU FAILED A UALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 WP 29 322UA 23954 APU FIRE WARNING INDICATION. *S/D* TROUBLESHOOTING FOUND APU LOOP M515 READING 234 OHMS TO GROUND. THIS READING WAS O UT OF LIMITS. REPLACED M9323 APU TAILPIPE DETECTION HARNESS, AND TESTED SYSTEM PER AMM 26-15-00, SYSTEM CHECKED NORMAL. ALSO, REPLACED THE APU FIRE BOTTLE, SQUIB AND DISCHARGE DISC INDICATOR. 2 L 7 2 4F 4 F RT A16WE E2GL 1998092500523 19980925 00523 NM 1998 9 25 98UAL900457 1 19980917 A 2150 ACM ALLIED SIGNA 106050611 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RIGHT FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 927UA 1115572 26649 SMOKE IN THE COCKPIT. *S/D* RIGHT AIR CYCLE MACHINE SEIZED AND THE WATER SEPARATOR COALESCER BAG BECAME SATURATED WITH OIL. REPLACED THE RIGHT AIR CYCLE MACHINE AND WATER SEPARATOR COALESCER BAG. 2 L 7 2 4F 4 F RT A16WE E2GL 1998092500524 19980925 00524 EU 1998 9 25 98UAL900460 1 19980916 A 3240 BRAKE SYST AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LANDING GEAR MALFUNCTIONED A UALA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 29 401UA 435 BRAKE FAILURE ON TAXI. NR 1 ENG RUNNING, SINGLE ENGINE TAXI. WHILE STARTING NR 2 ENG, ALL BRAKES FAILED. RECYCLED ANT I-SKID NWS SWITCH, NO HELP. *S/D* PERFORMED HYD QTY CK, DEPRESSURIZED AND REPRESSURIZED BRAKE ACCUM. BRAKES CHECKED N ORMAL. RAN ENG 1 AND CONFIRMED PUMP PRESS. YELLOW PUMP PRESS ALSO GOOD. NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A28NM E40NE 1998092500525 19980925 00525 WP 1998 9 25 ABXA9800839 1 19980921 A 2120 AIR DISTRIBUTION DOUG DC8 DC863 302198A WP COCKPIT ODOR A ABXA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 824AX 46141 DURING DESCENT AT APPROXIMATELY 12,000 FT, FUMES WERE SMELLED IN THE COCKPIT. DIRTY, MUSTY, ACID SMELL. DONNED OXYGEN MASK FOR REMAINDER OF FLIGHT. INSPECTED ALL AVIONICS EQUIPMENT. NO FUMES NOTED. GROUND RAN ALL CTC'S ONE AT A TIME. N O FUMES NOTED. INSPECTED FORWARD ACCESSORY CONPARTMENT, NO FUMES NOTED. ALL SYSTEMS CHECKED GOOD. 2 L 7 4 4F 4A25 1998092500526 19980925 00526 WP 1998 9 25 MWEA98968 1 19980918 A 2560 5917689103 COVER DOUG DC9 DC914 3022034 WP PAX DOOR SLIDE DETACHED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 80ME 45795 FORWARD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FORWARD ENTRY EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998092500527 19980925 00527 1998 9 25 DHL98726007 4 19980922 A 3420 2588423905AF INSTRUMENT AMP BOEING 727 727228 NM NR 1 MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 726DH 20409 CAPTAINS HSI HAS INTERMITTENT HEADING FLAG, WHEN SELECTING NR 2 DG FLAG PULLS. REMOVED AND REPLACED NR 1 INSTRUMENT AMP . 2 L 7 3 4F A3WE 1998092500528 19980925 00528 NM 1998 9 25 P5CA9801478 1 19980920 A 2710 60B002581 VALVE BOEING 747 747123 1384873 NM RT WING LEAKING A P5CA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 23 858FT 20109 INFLIGHT NR 3 HYDRAULIC QUANTITY DECREASED AT 1 GAL PER HOUR RATE. DEPRESSURIZED SYSTEM, FLUID LOSS STOPPED. SYSTEM DE PRESSURIZED UNTIL DESCENT. TROUBLESHOOTING CONFIRMED LEAK IN RIGHT HAND FLIGHT CONTROL SHUTOFF VALVE. VALVE REPLACED I AW BMM 27-13-01 PG 401, SYSTEM TESTED SATISFACTORY IAW BMM 27-13-01 PG 501. 2 L 7 4 4F A20WE 1998092500529 19980925 00529 NM 1998 9 25 VNAA980919 1 19980919 A 2611 SD9422AOAO DETECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AFT LAV FAILED A VNAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 07 434JS 71677 5201 3051 DURING THE CLIMB AFTER TAKEOFF, A LAV SMOKE WARNING MESSAGE ILLUMINATED IN THE COCKPIT. THE CREW ELECTED TO RETURN TO T HE FIELD AND HAVE IT LOOKED AT BY DAY MAINTENANCE. MAINTENANCE INSPECTED AND DEFERRED THE LAV SMOKE SYSTEM, IN ACCORDAN CE WITH THE DORNIER MINIMUM EQUIPMENT LIST. THE AIRCRAFT WAS RETURNED TO SERVICE. LATER IN THE DAY, PIT MAINTENANCE IN SPECTED AND REPLACED THE LAV SMOKE DETECTOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 26-15-01. OPERATIONAL CHECKS WERE COMPLETED AND FOUND TO BE SATISFACTORY. THE DEFERRAL WAS REMOVED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998092500531 19980925 00531 NM 1998 9 25 VNAA980921 1 19980921 A 3244 TIRE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG LOW PRESSURE A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 458PS 3068 DURING THE TAXI FOR TAKEOFF, THE CREW FROM FLIGHT 4151 RECEIVED A REPORT FROM ANOTHER CREW ON RADIO, THAT THE LEFT MAIN TIRES LOOKED TO BE LOW ON AIR PRESSURE. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND SERVICED THE LEFT HAND INBOARD TIRE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-13-10, AND RETURNED THE AIRCRAFT TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998092500532 19980925 00532 NE 1998 9 25 CKSA98516 2 19980911 A 7200 ENGINE BOEING 747 747146 NM PWA JT9 JT9D7A 52054 NE NR 1 MALFUNCTIONED A CKSA O OTHER O OTHER DE DESCENT 1 GL 23 702CK 65904 2522 20332 685676 DURING ENGINE START, THE NR 1 ENGINE SMOKED. CLEARED AFTER A FEW MOMENTS, ALL INDICATIONS WERE NORMAL. DURING DESCENT AN OILY SMELL CAME THROUGH THE AIR CONDITIONING SYSTEM, WAS ABLE TO STOP THE SMELL BY CLOSING THE NR 1 ENGINE BLEED AIR VALVE. REMOVED AND REPLACED THE NR 1 ENGINE AND TRIMMED IAW AIA WORK CARD 7EC7100. NO DEFECTS NOTED ON GROUND RUN. 2 L 7 4 4F 4 F A20WE E20EA 1998092500533 19980925 00533 NM 1998 9 25 CKSA98517 1 19980913 A 5350 FILLET BOEING 747 747146 NM WING /FUSELAGE CRACKED A CKSA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 702CK 20332 DURING PREFLIGHT, FOUND CRACK 18.5 INCHES LONG IN COMPOSITE PANEL LOCATED IN THE LOWER REAR BODY GEAR/WING TRAILING EDGE FILLET. CRACK IS DIRECTLY BEHIND THE LOWER WATER DRAIN ACCESS HATCH, IN THE LEFT OF THE AIRCRAFT CENTERLINE, BEHIND TH E LEFT BODY GEAR, NEAR AND PARALLEL TO WHERE IT JOINS THE FUSELAGE SKIN. REPAIRED PANEL AS PER ENGINEERING DRAWING B4 - 06125. 2 L 7 4 4F A20WE 1998092500534 19980925 00534 NE 1998 9 25 CKSA98518 2 19980919 A 7200 ENGINE BOEING 747 747269B NM PWA JT9 JT9D7J 52054 NE NR 4 DEFECTIVE A CKSA B E J EMER. DESCENT ENGINE SHUTDOWN DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 23 707CK 42036 21541 685928 NR 4 ENGINE FIRE INDICATION LIGHT AND BELL WENT OFF AT 2135Z, 24,000 FEET. AIRCRAFT GW 764,998 POUNDS, FUEL 264,000. S ECURED ENGINE, DID NOT HAVE TO FIRE BOTTLE, DUMPED 132,000 POUNDS OF FUEL. OIL QUANTITY OBSERVED DECREASING TO HALF IND ICATION PRIOR TO BELL AND LIGHT. SHUT DOWN ENGINE PER CHECKLIST. LANDING WEIGHT 626,000. WINDMILLING FOR 30 MINUTES W ITH WINDMILL PRESSURE OF 25 PSI. REMOVED AND REPLACED NR 4 ENGINE IAW AIA WORK CARD 7EC7100, NO DEFECTS NOTED. 2 L 7 4 4F 4 F RT A20WE E20EA 1998092500535 19980925 00535 WP 1998 9 25 TC8A98060 1 19980918 A 3260 PROX SWITCH DOUG DC8 DC862F 3021972 WP MLG DOOR LACK OF LUBE A TC8A O OTHER N FALSE WARNING CL CLIMB 1 GL 23 187SK 46022 DOORS NOT LATCHED LIGHT REMAINED ON AFTER GEAR RETRACTION, CYCLED TWICE AND LIGHT EXTINGUISHED. LUBRICATED MLG DOOR UPL ATCH MECHANISM AND CLEANED PROXIMITY SWITCHES, OPS ON GROUND NORMAL IAW M/M 32-31-4. 2 L 7 4 4F 4A25 1998092500555 19980925 00555 GL 1998 9 25 98ZZZX3505 2 19980902 A 7250 67844193 SEAL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL TURBINE FAILED A HEEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 03 8197X S808 CAE835389 IN CRUISE FLIGHT, NR 1 ENGINE OIL PRESSURE BEGAN TO DROP. PILOT SECURED ENGINE, PROCEEDED ON TO SHORE BASE AND LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAK AT NR 6 AND NR 7 SCAVAGE STRUT. REF: ALLISON C-20 IPC, CHAPTER 72-50-00, FIGURE 1, ITEM 32. 1 G 7 2 3U 3 U H3EU E4CE 1998092500556 19980925 00556 EU 1998 9 25 98ZZZX3506 1 19980817 A 6520 4619002003 GEARBOX BOLKMS 105 BO105C 5626005 EU TAIL ROTOR FAILED H A K NONE O OTHER IN INSP/MAINT 1 EA 23 90752 3450 1307 S156 GEARBOX WAS REMOVED FOR REPAIR AT EUROCOPTER CANADA LTD. THEY REPLACED ALL BEARINGS AND RETURNED THE REPAIRED GEARBOX. PART WAS INSTALLED IN ACFT AND DURING SUBSEQUENT GROUND MAINTENANCE RUNS, CHIPS APPEARED ON THE CHIP PLUG. ACFT NEVER GOT AIRBORNE. REMOVED GEARBOX FOR REPAIR AGAIN AT ECL. RE-INSTALLED REPAIRED GEARBOX AND AGAIN DURING SUBSEQUENT GROUN D MAINTENANCE RUNS CHIPS APPEARED ON THE CHIP PLUG. REMOVED GEARBOX FOR REPAIR AT ECL. LOANER FROM AEC IS INSTALLED ON ACFT WHICH IS NOW IN SERVICE. 1 G 7 2 3U H3EU 1998092500557 19980925 00557 EU 1998 9 25 HCMA0000203 1 19980805 A 6400 60102RS1MT33CA BEARING SNIAS 350 AS350B 8680801 EU T/R DRIVE ROUGH A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 642BH 637 2495 BEARING IS ROUGH. SPOTS ON OUTER RACE. (X) 1 G 7 1 3U H9EU 1998092500558 19980925 00558 EU 1998 9 25 HCMA0000204 1 19980713 A 6520 350A33215300 BEARING SNIAS 350 AS350B 8680801 EU T/R DRIVE WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 752BH 92 2510 TAIL ROTOR DRIVE IS WORN EXCESSIVELY. (X) 1 G 7 1 3U H9EU 1998092500559 19980925 00559 EU 1998 9 25 HCMA0000205 1 19980317 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R DRIVE WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 972BH 624 2804 T/R ROTOR DRIVE BEARING IS WORN BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1998092500560 19980925 00560 EU 1998 9 25 HCMA0000206 1 19980723 A 6520 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU T/R DRIVE WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 972BH 632 2804 T/R DRIVE BEARING WORN BEYOND LIMITS; TORN. 1 G 7 1 3U H9EU 1998092500562 19980925 00562 NE 1998 9 25 98ZZZX3508 1 19980827 A 6710 7690001880106 AMPLIFIER SKRSKY S76 S76A 8143006 NE DROOP COMP MALFUNCTIONED A HEEA O OTHER O OTHER AP APPROACH 1 SW 03 706AE 29 760275 ON APPROACH FOR LANDING, NR 1 ENGINE STARTED TO YAW. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 DCA AMPLIFIER INOPERABLE, AND THE NR 2 DCA AMPLIFIER ERRATIC. REPLACED BOTH. REF: S-76 IPC, CHAPTER 76-11-00, FIG 1-14 AND FIG 1-16 . 1 G 7 2 3U H1NE 1998092500567 19980925 00567 EU 1998 9 25 HCMA0000213 1 19980730 A 6410 355A09103601 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 197BH 996 2666 TAIL ROTOR BEARING CRACKED BEYOND LIMITS. 1 G 7 1 3U H9EU 1998092500568 19980925 00568 WP 1998 9 25 ARWA9807132 1 19980730 A 2750 472085117 COMPARATOR LKHEED 1011 1011385115 5265015 WP FLAP ASYMMETRY FAILED A ARWA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 SO 19 308GB 144G 193U1133 MIA - FLT 617 - SLAT ASYMMETRY DETECTION FAULT, LIGHT ON AFTER EXTENDING FLAPS. PERFORMED ABNORMAL PROCEDURES. LIGHT R EMAINED ON. RETURNED TO BLOCK. REMOVED AND REPLACED SLAT ASYMMETRY COMPARATOR. OPS CHECK NORMAL IAW MM 27-81-01. (X) 2 L 7 3 4F A23WE 1998092500569 19980925 00569 NM 1998 9 25 ASAA9840074 1 19980623 A 3350 LIGHT BOEING 737 737490 1384715 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 797AS 28892 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 15-17 WERE FOUND INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1998092500570 19980925 00570 SW 1998 9 25 98ZZZX3513 1 19980806 A 5530 NAS660436 BOLT 206020113223 BELL 407 407 SW VERTICAL FIN LOOSE A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL 53230 ON PHASE INSPECTION FOUND 3 OF THE 4 VERTICAL FIN MOUNTING BOLTS LOST TORQUE. 1 G 7 1 3U O H2SW 1998092500571 19980925 00571 SW 1998 9 25 98ZZZX3514 1 19980806 A 5530 NAS660428 BOLT 206020113223 BELL 407 407 SW VERTICAL FIN LOOSE A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL 53230 ON PHASE INSPECTION FOUND 3 OF THE 4 VERTICAL FIN MOUNTING BOLTS LOST TORQUE. 1 G 7 1 3U O H2SW 1998092500572 19980925 00572 SW 1998 9 25 98ZZZX3515 1 19980806 A 5530 NAS660436 BOLT 206020113223 BELL 407 407 SW VERTICAL FIN LOOSE A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 53247 ON DAILY SERVICE CHECK, 4 MOUNTING BOLTS FOR VERTICAL FIN WERE FOUND TO HAVE LOST TORQUE. 1 G 7 1 3U O H2SW 1998092500574 19980925 00574 SW 1998 9 25 98ZZZX3517 1 19980805 A 5530 NAS660428 BOLT 206020113229 BELL 407 407 SW VERTICAL FIN LOOSE A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 587AL 53248 DURING DAILY SERVICE CHECK, FOUND UPPER AND LOWER AFT BOLTS TO HAVE LOST TORQUE. 1 G 7 1 3U O H2SW 1998092500577 19980925 00577 SW 1998 9 25 98ZZZX3520 1 19980623 A 6510 406040340101 DISC PACK 407040302101 BELL 407 407 SW T/R CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 487AL RNFS5006 53204 WHILE PERFORMING A 25 HOUR INSPECTION, DISC PACK NR 7 WAS NOTED TO BE CRACKED. THE CRACKED DISC OF THE 10 DISCS IS THE NR 10 DISC. (THE VERY AFT DISC OF THE NR 7 DISC PACK). 1 G 7 1 3U O H2SW 1998092500579 19980925 00579 NM 1998 9 25 98ZZZX3522 1 19980727 A 2810 4006 PANEL DORNER DO32 DO328100 2996000 NM COCKPIT MALFUNCTION A EQGA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 19 337PH 7657 94050032 3020 DFW/ASE - FLT 427 - APPROXIMATELY 15 MINUTES AFTER TAKEOFF WHILE CLIMBING TO ALTITUDE EN ROUTE TO ASE, BEGAN TO RECEIVE ERRONEOUS FUEL QUANTITY READINGS ON THE RIGHT TANK GROUP AND RECEIVED A FUEL ASYM MESSAGE ON THE EICAS. CONTACTED MAINT ENANCE CONTROL AND FLIGHT CONTROL AND ADVISED OF THE SITUATION. MAINTENANCE CONTROL ADVISED TO RETURN TO DFW. CREW PRO CEEDED TO RETURN TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THE REFUEL/DEFUE L PANEL WAS DEFECTIVE. MAINTENANCE REPLACED THE REFUEL/DEFUEL PANEL AND PERFORMED NECESSARY OPERATIONAL CHECKS. ALL CH ECKS SATISFACTORY. AIRCRAFT REUTRNED TO REVENUE SERVICE. 2 H 7 2 4T RT A45NM 1998092500580 19980925 00580 1998 9 25 98ZZZX3523 4 19980601 A 3425 BREAKER DORNER DO32 DO328100 2996000 NM FDR SYSTEM TRIPPED A EQGA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 19 337PH 3020 DFW/TYS - FLT 371 - IN CRUISE, AFTER TAKEOFF, CREW EXPERIENCED A LOUD HUM IN THE INTERCOM. APPROX 45 MINUTES INTO FLIG HT, SERVICE LIGHTS CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. APPROX 10 MINUTES LATER, CREW RECEIVED AN FDR FAIL CAS MESSAGE AND FDR C/B TRIPPED. WHILE ATTEMPTING TO RESET C/B, GPWS CIRCUIT BREAKER TRIPPED WITH A CORRESPONDING CAS MESSA GE. MAINTENANCE CONTROL ADVISED CREW TO DIVERT TO HOT WHERE THE AIRCRAFT COULD BE INSPECTED. ACFT LANDED IN HOT WITHOU T INCIDENT. MAINT INSPECTED ACFT AND COULD NOT FIND ANY SIGNS OF DAMAGE, FAILURE, OR FAULT. ALL MESSAGES WERE CLEARED. MAINT CLEANED CONNECTORS AND PERFORMED TEST FLIGHT. TEST FLIGHT SATISFACTORY. ACFT RELEASED TO REVENUE SERVICE. (X) 2 H 7 2 4T RT A45NM 1998092500581 19980925 00581 WP 1998 9 25 98ZZZX3524 2 19980821 A 7200 ENGINE ISRAEL 1124 1124 4500102 EU GARRTT TFE731 TFE7313 01518 WP NR 1 BIRD STRIKE A L EV6A E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING C X J F.O.D. ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 WP 07 262WC 7427 262 77285 LARGE BIRD INGESTION NR 1 ENGINE ON TAKEOFF FROM CONCORD CA 8-21-98. 2 M 7 2 4F 4 F A2SW E6WE 1998092500582 19980925 00582 WP 1998 9 25 98ZZZX3525 1 19980511 A 3222 50064451 FORK DOUG DC3 DC3CR183090C 3021466 WP TAIL WHEEL BROKEN A FHCA K NONE O OTHER IN INSP/MAINT 1 SO 21 133FS 27202 AS THE AIRCRAFT PARKED AND THE ENGINES SHUT DOWN, THE TAIL WHEEL FORK CRACKED AND BROKE IN TWO PIECES. AREAS OF CONSIDE RABLE DAMAGE WERE THE LOWER SKIN, FORMERS AND STRINGERS AT STA 664/667. APPARENT CAUSE OF TROUBLE - METAL FATIGUE. 2 L 7 2 4R A669 1998092500583 19980925 00583 1998 9 25 98ZZZX3526 4 19980711 A 3421 GYRO BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A FYWA K NONE O OTHER NR NOT REPORTED 1 AL 05 242RH 903 SITKA - FLT 301 - FIRST OFFICER'S GYRO - HORIZON WOULD NOT ERECT. FERRIED AIRCRAFT SITKA TO KETCHIKAN. REMOVED AND REP LACED F/O GYRO. 2 L 7 2 4T RT A56EU 1998092500584 19980925 00584 EU 1998 9 25 98ZZZX3527 1 19980705 A 3040 WIPER BAG JETSTM JETSTM3201 1500217 EU WINDSCREEN FAILED A FYWA K NONE O OTHER AP APPROACH 1 AL 05 242RH 903 ON FINAL APPROACH TO KETCHIKAN, RT WINDSHIELD WIPER FAILED TO WORK. REMOVED AIRCRAFT FROM SERVICE. REMOVED AND REPLACE D RT HAND WINDSHIELD WIPER MOTOR. OPS CHECK GOOD. 2 L 7 2 4T RT A56EU 1998092500585 19980925 00585 EU 1998 9 25 98ZZZX3528 1 19980707 A 7722 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A FYWA K NONE O OTHER NR NOT REPORTED 1 AL 05 242RH 903 RIGHT EGT GAUGE DROPPED TO ZERO IN-FLIGHT. AIRCRAFT TAKEN OFF-LINE AND FERRIED TO KTN. FOUND COLD SOLDER JOINT RT EGT COMPRESSOR CANNON PLUG. RE-SOLDERED BAD CONNECTION. GROUND RAN RT ENGINE, OPS CHECK GOOD. RETURNED AIRCRAFT TO SERVIC E. 2 L 7 2 4T RT A56EU 1998092500586 19980925 00586 SO 1998 9 25 98ZZZX3529 1 19980623 A 3240 1159H20014 BRAKE LINE GULSTM G1159 G1159 3953505 SO RT MLG CRACKED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 220JR 50 DURING A ROUTINE INSPECTION, HYDRAULIC FLUID WAS FOUND IN THE WHEEL WELLS. THE LEAK WAS TRACED TO A CRACK IN A RIGHT HA ND BRAKE LINE, PN 1159H20014. THE CRACK STARTED IN A SLIGHT GROOVE THAT MAY HAVE BEEN A MANUFACTURER'S TOOLING MARK THA T WAS INFLICTED WHEN THE TUBING WAS MANUFACTURED OR BENT TO FORM THE ASSEMBLY. THE LINE HAS BEEN INSTALLED FOR 30 YEARS . 2 L 7 2 4F RT A12EA 1998092500587 19980925 00587 NM 1998 9 25 MZZA9818 1 19980709 A 8011 383152161 STARTER BOEING 727 727277 138408S NM NR 1 ENGINE DAMAGED A MZZA D RETURN TO BLOCK E VIBRATION/BUFFET TX TAXI/GRND HDL 1 WP 13 627DH 22641 MNL - FLT CS879 - L/P 7911528 - AIRCRAFT GATE RETURNED DUE TO HEAVY VIBRATIONS ON NR 1 ENGINE DURING START CYCLE. FOUND STARTER TURBINE WHEEL MISSING OUTER PORTION OF ALL BLADES. REMOVED AND REPLACED NR 1 ENGINE PNEU STARTER PER MM 80-11- 31. GROUND ENGINE RUN CHECKED GOOD PER MM 72-20-0. (X) 2 L 7 3 4F RT A3WE 1998092500588 19980925 00588 NM 1998 9 25 MZZA98184 2 19980708 A 7510 320115 VALVE BOEING 727 727277 138408S NM NR 3 ENGINE FAILED A MZZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 WP 13 626DH 22644 MNL - FLT CS879 - L/P 7910614 - DURING TAKEOFF ROLL IMMEDIATELY AFTER AN ESPECIALLY HARD JOLT, THE NR 3 FUEL HEAT VALVE LIGHT CAME ON AND OIL TEMPERATURE STARTED RISING. VALVE WAS SELECTED CLOSED AND CYCLING SWITCH WOULD NOT GO FULLY CLOSE D. SUBMITTER SUSPECTED VALVE ONLY PARTIALLY OPENED. JUST ENOUGH TO TURN ON LIGHT AND ALLOW SOME AIR THROUGH. CHECKED WIRING CONNECTION OF NR 3 ENGINE FUEL DE-ICING AT D0412P TO D076 (V7) OF FUEL DE-ICE VALVE AND REMOVED AND REPLACED DE- ICE VALVE PER MM 73-14-11. (X) 2 L 7 3 4F RT A3WE 1998092500589 19980925 00589 CE 1998 9 25 MASA98164 1 19980827 A 5210 10151404721 CAM LOCKS 1294000321 BEECH 1900 1900D 1154162 CE PASSENGER DOOR OUT OF ADJUST A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 173YV UE173 DUJ/PIT - FLT 5954 - CREW REPORTED THE PASSENGER DOOR CAMLOCKS WOULD NOT LATCH COMPLETELY. MAINTENANCE RIGGED THE DOOR CAMLOCKS, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1998092500590 19980925 00590 EU 1998 9 25 PLGA980617A 1 19980625 A 7722 4078T09P02 TRIMMER SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A PLGA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 NE 05 334BE GDB00694 340A158 BOS - FLT 4252 - CREW NOTICED ENGINE TEMPS HIGHER THAN RIGHT, BUT NOT OUT OF LIMITS. CREW REDUCED POWER TO MATCH TEMPS AND LEFT ENGINE DID NOT MAKE CHARTED TORQUE. AIRCRAFT RETURNED TO BOS WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED T HE T4.5 TRIMMER IAW GE MM. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998092500591 19980925 00591 EU 1998 9 25 PLGA980704A 1 19980704 A 3310 4492 POWER SUPPLY SAAB SF340 SF340A 7850100 EU COCKPIT DISCHARGED A PLGA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NE 05 334BE 0806 340A158 YSC - FLT 4219 - WHILE ON DESCENT INTO YQB, THE CREW REPORTED SMOKE IN THE COCKPIT. CREW DECLARED AN EMERGENCY AND DIVE RTED INTO YSC AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED INSTRUMENT LIGHTING POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998092500592 19980925 00592 EU 1998 9 25 98ZZZX3530 1 19980803 A 7110 350A5801160001 COWLING SNIAS 350 AS350B2 8680813 EU ENGINE WARPED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 4060Z 13 CN123 3038 COWLING HAS EXCESSIVE WARPAGE. LARGE VOID ON INSIDE OF COWLING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998092500594 19980925 00594 1998 9 25 98ZZZX3532 4 19980324 A 3457 071015530200 ANTENNA KA92 SNIAS 350 AS350B 8680801 EU GPS FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5771C 12893 1369 GPS SHUTS DOWN WHILE IN USE. ANTENNA INTERNAL RESISTANCE 42 OHMS. NO CRA. 1 G 7 1 3U H9EU 1998092500595 19980925 00595 EU 1998 9 25 98ZZZX3533 1 19980706 A 3350 301 BULB AIRBUS 320 A320231 3930325 EU CABIN FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GCRPH 424 LAVATORY 'D' AND 'E' EMERGENCY LIGHTS INOPERATIVE. RE-LAMPED, BOTH OPERATIONAL CHECKS NORMAL. 2 L 7 2 4F RT A28NM 1998092500596 19980925 00596 1998 9 25 98ZZZX3534 4 19980723 A 2565 25611045 SLIDE AIRCRUISERS AIRBUS 320 A320231 3930325 EU CABIN DEPLOYED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 GCRPH A6043 424 YYZ - FLT 6001 - LEFT NR 1 DOOR EVACUATION SLIDE DEPLOYED. INADVERTENT DEPLOYMENT ON GROUND. REMOVED AND REPLACED EVAC UATION SLIDE. 2 L 7 2 4F RT A28NM 1998092500597 19980925 00597 EU 1998 9 25 98ZZZX3535 1 19980818 A 3520 11701904 OXYGEN MASK AIRBUS 320 A320231 3930325 EU CABIN ACTIVATED A RYNA O OTHER O OTHER CR CRUISE 1 CE 07 GCRPH 424 DEN - SEAT ROW 1R OXYGEN MASK DEPLOYED AND OXYGEN GENERATOR SET OFF. SECURED MODULE DOOR SHUT AND PLACED ON DMI. REPAC KED OXYGEN MASK AND REPLACED OXYGEN GENERATOR. CLEARED DMI 8-20-98. 2 L 7 2 4F RT A28NM 1998092500598 19980925 00598 EU 1998 9 25 98ZZZX3536 1 19980505 A 3350 LIGHT AIRBUS 320 A320231 3930325 EU CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GEPFR MSN437 DEN - FLT 8258 - EMERGENCY SEAT LIGHT INOPERATIVE AT SEAT ROWS 29L, 11R. DEFERRED PER MEL EMERGENCY SEAT LIGHTING AT RO W 29L, 11R. FOUND CANNON PLUG LOOSE AT 29L AND 11R, RE-INSTALLED. LIGHTS OPERATE NORMALLY. 2 L 7 2 4F RT A28NM 1998092500599 19980925 00599 EU 1998 9 25 SIMA982092 1 19980728 A 3350 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 234AE 340B234 DFW - FLT 5046 - OVERHEAD EMERGENCY LIGHT AT SEAT 11A DOES NOT ILLUMINATE. FOUND BULB LOOSE. RE-SEATED BULB. OPERATIO NAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998092500600 19980925 00600 EU 1998 9 25 SIMA981973 1 19980716 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 659 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 326AE 340B326 ABI - SEAT TRACK 18.3L AT STA 659 WAS FOUND CORRODED BEYOND MM LIMITS. CUT OUT 48 INCH SECTION OF SEAT TRACK. FABRICAT ED AND INSTALLED REPAIR SECTION OF SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998092500601 19980925 00601 EU 1998 9 25 SIMA981988 1 19980717 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 338SB 340B338 DFW - FLT 5166 - TWO EMERGENCY OVERHEAD LIGHTS AT ROWS 9 AND 11 DO NOT ILLUMINATE. REMOVED AND REPLACED BULBS AT ROWS 9 AND 11 OVERHEAD LIGHTS. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998092500602 19980925 00602 EU 1998 9 25 SIMA982091 1 19980728 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 338SB 104 340B338 OVERHEAD EMERGENCY LIGHTS AT SEAT 9A AND 11A DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT RO WS 9/10. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998092500603 19980925 00603 EU 1998 9 25 98ZZZX3537 1 19980428 A 5242 DOOR AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND LIGHT CORROSION ON FUSELAGE FLANGES AROUND A FT AVIONICS DOOR (AFT). INSTALLED DOUBLER ON AFT FLANGE OF AVIONICS DOOR IAW AIRAMS/T/ATR/32986/98, FAX COVER SHEET 141 /98/002 AND ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2075T6 - .063 INCH. 2 H 7 2 4T RT A53EU 1998092500604 19980925 00604 EU 1998 9 25 98ZZZX3538 1 19980428 A 5242 DOOR AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND LIGHT CORROSION ON FUSELAGE FLANGES AROUND A FT AVIONICS DOOR (FORWARD). INSTALLED DOUBLER ON FORWARD FLANGE OF AVIONICS DOOR IAW AIRAMS/T/ATR/32986/98, FAX COVER S HEET 141/98/002 AND ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS. TAC: 23,278. 2 075T6 - .063 INCH. 2 H 7 2 4T RT A53EU 1998092500605 19980925 00605 NE 1998 9 25 UIEA9805 2 19980821 A 7250 TURBINE BOEING 747 747243B 1384830 NM GE CF6 CF650E2 30018 NE NR 2 ENGINE FAILED A UIEA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 EA 15 517MC 77542 6315 23300 517482 ANC - AFTER TAKEOFF AT FL 310, NR 2 ENGINE FLAMED OUT IN CRUISE. ATTEMPTED RE-START ENGINE AND NO HELP. NO N2 INDICATI ON. AIRCRAFT DUMPED FUEL AND HAD UNEVENTFUL RETURN TO ANC. DURING INSPECTION OF ENGINE AT ANC, FOUND EVIDENCE OF METAL IN THE TAIL PIPE AND DAMAGE TO 4TH STAGE LOW PRESSURE TURBINE BLADES. ENGINE REPLACED. S/N OFF 517482, S/N ON 530304. (X) 2 L 7 4 4F 4 F A20WE E23EA 1998092500606 19980925 00606 NM 1998 9 25 UIEA9804 1 19980808 A 3230 NLG BOEING 747 7472D7B 1384803 NM NOSE MALFUNCTIONED A UIEA O OTHER J WARNING INDICATION AP APPROACH 1 EA 15 528MC 22472 ANC - DURING APPROACH, 'NOSE GEAR DID NOT EXTEND NORMALLY - MANUAL EXTENSION OK'. CHECKED RIGGING OF NOSE GEAR SEQUENCE VALVE LOCK MECHANISM AND ACTUATOR AND FOUND SAME TO BE NORMAL. PERFORMED GEAR EXTENSION/RETRACTION CHECK PER MM 32-34- 00, AND NO DEFECTS FOUND, OPERATION NORMAL. (X) 2 L 7 4 4F RT A20WE 1998092500607 19980925 00607 NM 1998 9 25 98ZZZX3539 1 19980801 A 3230 69179572 FITTING BOEING 727 7272K5 NM RT MLG DOOR LOOSE A FX7A O OTHER J WARNING INDICATION AP APPROACH 1 SO 19 369FA 21851 MDPC/KMIA - ON FAE - FLT 800 - ON APPROACH, RIGHT MLG FAILED TO EXTEND. CREW ACCOMPLISHED MANUAL EXTENSION. ON GROUND, MAINTENANCE FOUND RIGHT MLG DOOR OUT OF RIG CAUSED BY A LOOSE MLG INBD FITTING. FITTING WAS TIGHTENED, DOOR WAS RIGGE D AND GEAR SWING ACCOMPLISHED PER 32-32-00. AIRCRAFT RETURNED TO SERVICE. 2 L 7 3 4F RT A3WE 1998092500608 19980925 00608 WP 1998 9 25 98ZZZX3540 1 19980511 A 3222 51158621 FORK DOUG DC3 DC3CR183090C 3021466 WP TAIL WHEEL BROKEN A FHCA K NONE O OTHER IN INSP/MAINT 1 SO 21 133FS 27202 AS THE AIRCRAFT PARKED AND THE ENGINES SHUT DOWN, THE TAIL WHEEL FORK CRACKED AND BROKE IN TWO PIECES. AREAS OF CONSIDE RABLE DAMAGE WERE THE LOWER SKIN, FORMERS AND STRINGERS AT STA 664/667. APPARENT CAUSE OF TROUBLE - METAL FATIGUE. 2 L 7 2 4R A669 1998092500609 19980925 00609 EU 1998 9 25 JBXA980047 1 19980724 A 2421 IDG FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 MALFUNCTIONED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 133ML 11330 NR 1 IDG FAULTED ON TAKEOFF ROLL. RESET AND OPS CHECKED NR 1 GEN (IDG) IAW AMM CH 24-11-00, ALL CHECKS GOOD AT THIS TIM E. 2 L 7 2 4F 4 F RT 1998092500610 19980925 00610 NM 1998 9 25 AWXA9800204 1 19980912 A 5313 STRINGER BOEING 737 737277 1384570 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 186AW 22653 FUSELAGE CRACK STR 18R APPROX 7 INCHES LONG AFT OF RT AFT WING TO BODY FAIRING. INSTALLED BLIND FASTENERS USED, REINSPE CT AT 3000 CYC AND THEREAFTER 2500 CYC. REPLACED BLIND FASTENERS RECOMMENDED BY SUBSEQUENT OVERHAUL. BLIND FASTENERS M UST BE REPLACED BY 10,000 FLT CYC AFTER INITIAL INSTALLATION. INSTALLED REPAIR DOUBLER WITH BLIND FASTENERS IAW SRM 53- 30-03 FIG 1. 2 L 7 2 4F RT A16WE 1998092500611 19980925 00611 NM 1998 9 25 CALA9801794 1 19980916 A 5730 PANEL BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND A .5 INCH CRACK IN RT WING UPPER PANEL FORWARD OF NR 7 SPOILER. THE CRACK WAS STOP DRILLED IAW SRM 51- 10-1. DOUBLERS WERE INSTALLED IAW SRM 57-30-4, FIGURE 10, 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998092500612 19980925 00612 NM 1998 9 25 CALA9801795 1 19980916 A 5522 SKIN BOEING 727 727224 1384076 NM LT ELEVATOR CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND CORROSION IN LT ELEVATOR UPPER TRAILING EDGE SKIN BETWEEN STATIC WICKS. THE CORROSION WAS REMOVED, DOU BLERS WERE INSTALLED IAW SRM 55-20-03. 2 L 7 3 4F A3WE 1998092500613 19980925 00613 NM 1998 9 25 CALA9801796 1 19980916 A 5330 SKIN BOEING 727 727232 1384082 NM BS 560-580 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND CORROSION IN FUSELAGE SKIN UNDER RIVET HEAD AT BS 560 TO 580, STRINGER 5R. THE CORRODED AREA OF SKIN W AS CUT OUT AND A DOUBLER STRAP REPAIR WAS INSTALLED IAW SRM 53-30-8, 51-10-6, 51-20-4, AND 51-30-2. 2 L 7 3 4F A3WE 1998092500614 19980925 00614 NM 1998 9 25 CALA9801797 1 19980916 A 5220 MECHANISM BOEING 727 727232 1384082 NM LT EMER EXIT DR OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 THE LT FORWARD OVERWING EMERGENCY EXIT DOOR FAILED PULL CHECK. THE PULL FORCE ON THE DOOR WAS ADJUSTED TO SPECIFICATION IAW MM 52-21-0. 2 L 7 3 4F A3WE 1998092500615 19980925 00615 NM 1998 9 25 CALA9801798 1 19980916 A 5720 ANGLE BOEING 727 727232 1384082 NM WS 491 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT WING NR 3 SPOILER L-ANGLE CORRODED AT INBOARD SIDE OF TRANSMISSION, WS 491. THE ANGLE WAS REMOVED A ND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-10-3. 2 L 7 3 4F A3WE 1998092500616 19980925 00616 WP 1998 9 25 CALA9801799 1 19980916 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16893 49392 INSPECTION FOUND A .75 INCH CRACK IN RADIUS OF FORWARD ENTRY DOOR NR 1 BEAM. THE BEAM WAS REMOVED AND A NEW BEAM WAS IN STALLED IAW SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998092500617 19980925 00617 WP 1998 9 25 CALA9801800 1 19980916 A 5320 ANGLE DOUG DC9 DC982 3022082 WP CARGO COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16893 49392 INSPECTION FOUND AFT CARGO BIN Z-ANGLE CORRODED. THE ANGLE WAS REPAIRED IAW SRM 53-05, FIGURE 63. 2 L 7 2 4F A6WE 1998092500618 19980925 00618 WP 1998 9 25 CALA9801801 1 19980917 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 256 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16893 49392 INSPECTION FOUND A .75 INCH CRACK IN LONGERON 17L AT STA 256 BELTFRAME ATTACHMENT. A LONGERON AND LONGERON SPLICE WERE INSTALLED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1998092500619 19980925 00619 NM 1998 9 25 CALA9801802 1 19980916 A 5330 SKIN BOEING 737 7372C0 1384488 NM BS 294.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 294.5 BETWEEN S26L AND S27L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5330-02708 AND ECRA 5330-02707. 2 L 7 2 4F A16WE 1998092500620 19980925 00620 WP 1998 9 25 CALA9801803 1 19980916 A 5311 FRAME DOUG DC10 DC1030 3023501 WP BS 1721 & 1780 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND CORROSION ON LOWER FLANGE OF FRAMES IN CENTER CARGO COMPARTMENT AT STA 1721 BETWEEN STRINGER 50L AND 50 R AND AT STA 1780 BETWEEN STRINGER 50L AND 50R. THE CORRODED OUTER CAPS OF FRAMES WERE TRIMMED OUT. THE AREAS WERE REI NFORCED WITH OUTER CAPS AND DOUBLERS IAW SRM 57-21-00, FIGURE 8, 53-30-00, FIGURE 5, 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998092500621 19980925 00621 WP 1998 9 25 CALA9801804 1 19980917 A 5720 ANGLE DOUG DC10 DC1030 3023501 WP LT & RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND A 1.6 INCH CRACK ON RT AND LT WING INBOARD ISLAND LOWER AFT INBOARD SPLICE ANGLE OF RIB. THE SPLICE AN GLE WAS REMOVED AND A NEW PART WAS INSTALLED IAW SRM 57-22-01, FIGURE 2, 51-21-01, AND 51-33-01. 2 L 7 3 4F A22WE 1998092500622 19980925 00622 WP 1998 9 25 CALA9801805 1 19980917 A 5712 RIB DOUG DC10 DC1030 3023501 WP WS 1042-1192 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14075 46922 INSPECTION FOUND A 1 INCH CRACK IN LT WING FIXED LEADING EDGE RIB BETWEEN XFS 1042 AND XFS 1192. THE RIB WAS REMOVED. A NEW PART WAS INSTALLED IAW SRM 57-21-00 FIGURE 8, 51-21-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998092500623 19980925 00623 WP 1998 9 25 CALA9801806 1 19980920 A 3230 FUSE DOUG DC10 DC1030 3023501 WP RT MLG TRIM CYL REQD BLEEDING A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12061 47851 THE LANDING GEAR HANDLE WOULD NOT MOVE TO UP POSITION AFTER TAKEOFF. THE APPROPRIATE CHECKLIST WAS COMPLETED WITH NO HE LP. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TRIM CYLINDER INTERLOCK F USE IN THE RT WHEEL WELL AT FAULT. THE TRIM CYLINDER INTERLOCK FUSE WAS BLED IAW MM 32-31-06, PAGE 203 TO 204. THE GEA R HANDLE WAS CYCLED SEVERAL TIMES AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1998092500624 19980925 00624 NM 1998 9 25 CALA9801807 1 19980920 A 3097 WIRE BOEING 747 747238B 1384828 NM R-1 WINDOW FAILED A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14024 20534 ELECTRICAL ARCING IN R-1 WINDOW CAUSED A SMALL AMOUNT OF SMOKE IN THE COCKPIT DURING CLIMBOUT OF GUM. THE AIRCRAFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND POWER WIRE TO R-1 WINDOW BROKEN AND BURNT. THE WIR E WAS REMOVED AND WIRING WAS RESPLICED. AN OPERATIONAL CHECK OF R-1 WINDOW WAS GOOD. 2 L 7 4 4F A20WE 1998092500625 19980925 00625 WP 1998 9 25 CALA9801808 1 19980917 A 5320 BEAM DOUG DC9 DC982 3022082 WP BAGGAGE COMPT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16893 49392 INSPECTION FOUND MAIN BAGGAGE BIN Z-BEAM CORRODED AROUND LOWER DOOR STOPS. A REPAIR WAS INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 1998092500626 19980925 00626 NM 1998 9 25 CALA9801809 1 19980918 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FOREFLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT INBOARD FOREFLAP SKIN DELAMINATED AT LOWER SURFACE INBOARD MOST END. THE FOREFLAP WAS REMOVED AND R EPLACED IAW MM 27-51-11. 2 L 7 3 4F A3WE 1998092500627 19980925 00627 NM 1998 9 25 CALA9801810 1 19980917 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 1140-1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND STRINGER 25R CORRODED AT STA 1140 TO 1183. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-3. 2 L 7 3 4F A3WE 1998092500628 19980925 00628 NM 1998 9 25 CALA9801811 1 19980917 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 340 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND VERTICAL STIFFENER CORRODED AT RT FUSELAGE STA 340. A NEW STIFFENER WAS INSTALLED IAW ECRA 5300-01196 AND SRM 51-30-2. 2 L 7 3 4F A3WE 1998092500629 19980925 00629 WP 1998 9 25 CALA9801812 1 19980917 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 203.9 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND FORWARD COCKPIT CO-PILOT'S SEAT TRACK CORRODED AT STA 203.9. THE SEAT TRACK WAS REMOVED AND REPLACED I AW MM 53-40-1. 2 L 7 2 4F A6WE 1998092500630 19980925 00630 WP 1998 9 25 CALA9801813 1 19980917 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 246 LIGHTNING STRIKE A CALA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND LIGHTNING STRIKE DAMAGE IN LT FUSELAGE SKIN AT STRINGER 25L, STA 246. THE DAMAGED AREA WAS CUT OUT, DO UBLER AND FILLER WERE INSTALLED IAW ECRA 5331-01031. 2 L 7 2 4F A6WE 1998092500631 19980925 00631 NM 1998 9 25 CALA9801814 1 19980918 A 5720 STIFFENER BOEING 727 727232 1384082 NM WS 224 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND LT WING FRONT SPAR STIFFENER CORRODED ON INBOARD SIDE CENTER AT STA 224. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-20-4. 2 L 7 3 4F A3WE 1998092500632 19980925 00632 NM 1998 9 25 CALA9801815 1 19980918 A 5720 CHORD BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A .5 INCH CRACK IN LT WING LOWER CHORD AT NR 7 SPOILER ACTUATOR. THE CRACKED AREA WAS CUT OUT, STRAPS AND CHORD ANGLE WERE INSTALLED IAW ECRA 5720-01680 AND SRM 51-10-2. 2 L 7 3 4F A3WE 1998092500633 19980925 00633 NM 1998 9 25 CALA9801816 1 19980918 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 234 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND A .5 INCH CRACK IN NOSE WHEEL WELL STIFFENER AT STA 234, LBL 20. THE STIFFENER WAS REPAIRED IAW SRM 51 -10-2. 2 L 7 3 4F A3WE 1998092500634 19980925 00634 NM 1998 9 25 CALA9801817 1 19980918 A 5320 CHORD BOEING 727 727232 1384082 NM BS 292 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT UPPER CHORD CORRODED INSIDE NOSE WHEEL WELL AT STA 292, LBL 20. THE CHORD WAS REMOVED AND A NEW CHO RD WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998092500635 19980925 00635 NM 1998 9 25 CALA9801818 1 19980918 A 5330 PANEL BOEING 727 727232 1384082 NM FUSELAGE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .5 INCH CRACK IN PANEL NR 3338. THE CRACKED AREA WAS CUT OUT, A WEB AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998092500636 19980925 00636 NM 1998 9 25 CALA9801819 1 19980918 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1166 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND 8 INCH CRACK IN L-ANGLE AT STA 1166, STRINGER 26L TO 26R. THE ANGLE WAS REMOVED, A REPAIR ANGLE, NUT P LATES, AND RADIUS BLOCK WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998092500637 19980925 00637 NM 1998 9 25 CALA9801820 1 19980918 A 5230 CHANNEL BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND C-1 CARGO DOOR UNDER LOWER LIGHT HAD A PIECE OF PAN CRACKED OUT. THE PAN CHANNEL WAS REMOVED, A REPAIR WAS INSTALLED IAW SRM 52-30-1, 51-10-2, 51-30-2 AND MM 51-20-12. 2 L 7 3 4F A3WE 1998092500638 19980925 00638 NM 1998 9 25 CALA9801821 1 19980918 A 5311 FRAME BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND SIDE WALL SUPPORT FRAME CORRODED AT STA 720D ABOVE STRINGER 26R. THE CORRODED SECTION OF SUPPORT FRAME WAS REMOVED. A REPAIR ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-50-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998092500639 19980925 00639 NM 1998 9 25 CALA9801822 1 19980918 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 26 TO RBL 34 AND LBL 62. THE FLOORBEAM AREAS WERE REPAIRED IAW ECR A 5321-01028 AND ECRA 5321-01027. 2 L 7 3 4F A3WE 1998092500640 19980925 00640 NM 1998 9 25 CALA9801823 1 19980918 A 5320 PRESS PANEL BOEING 727 727232 1384082 NM BS 271 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A .1875 INCH CRACK IN NLG RT SIDE PRESSURE PANEL OUT OF FASTENER HOLE AT BS 271, WL 185. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998092500641 19980925 00641 NM 1998 9 25 CALA9801824 1 19980919 A 5320 WEB BOEING 727 727232 1384082 NM LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT AFT LAV FLOOR WEB CORRODED VANITY PLUMBING FITTING. THE FLOOR WEB WAS REMOVED, A NEW LAV FLOOR WEB, DOUBLER, AND FILLER WERE INSTALLED IAW SRM 51-40-2, 51-30-2, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998092500642 19980925 00642 NM 1998 9 25 CALA9801825 1 19980919 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 900 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 4 INCH CRACK IN STRINGER 14L AT STA 900. THE CRACKED SECTION OF STRINGER WAS REPLACED IAW SRM 51-30- 2. 2 L 7 3 4F A3WE 1998092500643 19980925 00643 NM 1998 9 25 CALA9801826 1 19980919 A 5530 FITTING BOEING 727 727232 1384082 NM VERT STAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND TOP OF VERTICAL STABILIZER LT HORIZONTAL HINGE ATTACH FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, AND ECRA 5550-01033. 2 L 7 3 4F A3WE 1998092500644 19980925 00644 NM 1998 9 25 CALA9801827 1 19980919 A 5320 FRAME BOEING 727 727232 1384082 NM CARGO DOORWAY CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND C-3 CARGO DOOR CUTOUT FORWARD FRAME LOWER CORNER CRACKED OUT OF BOTTOM STOP FITTING UPPER INBOARD BOLT HOLE AND LOWER PART OF FRAME WAS CORRODED. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40- 3. THE CRACK WAS 1.75 INCH LONG. 2 L 7 3 4F A3WE 1998092500645 19980925 00645 SO 1998 9 25 COMA9810216 1 19980917 A 3340 MS25219131683 SOCKET EMB 120 EMB120RT SO NAV LIGHTS SHORTED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 269CA 120263 NAVIGATION LIGHTS CIRCUIT BREAKER TRIPPED TWICE. REPLACED DEFECTIVE LIGHT SOCKET. 2 L 7 2 4T RT A31SO 1998092500646 19980925 00646 SO 1998 9 25 COMA9810217 1 19980917 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT LATCHED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 256CA 120245 SERVICE DOOR WARNING ON DURING FLIGHT. CLOSE AND LATCHED SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998092500647 19980925 00647 NM 1998 9 25 UPS98227692 1 19980918 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMERGENCY FLOOR LIGHT WILL NOT TEST ROW 17. REMOVED AND REPLACED BATT PACK, OPS CKS GOOD. 2 L 7 3 4F A3WE 1998092500648 19980925 00648 NM 1998 9 25 UPS98227693 1 19980918 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMERGENCY FLOOR LIGHT WILL NOT TEST ROW 15. REMOVED AND REPLACED BATT PACK, OPS CK GOOD. 2 L 7 3 4F A3WE 1998092500649 19980925 00649 NM 1998 9 25 UPS98227694 1 19980918 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMERGENCY AREA LIGHT ON FWD WALL ABOVE FLASH LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATT PACK, NO HELP. SECURED RECEPTICAL PINS ON CARRIAGE ASSY, CHECKS GOOD. 2 L 7 3 4F A3WE 1998092500650 19980925 00650 NM 1998 9 25 UPS98227695 1 19980918 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMERGENCY EXIT IDENTIFIER LIGHT WILL NOT TEST LT AFT OVERWING EXIT APPROX 18 INCHES ABOVE FLOOR. R EMOVED AND REPLACED BATT PACK, NO HELP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CKS GOOD. 2 L 7 3 4F A3WE 1998092500651 19980925 00651 NM 1998 9 25 UPS98427688 1 19980920 A 3350 S135610A BATTERY BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-A CHECK, EMERGENCY LIGHT ON MAIN DECK FAILED. REMOVED AND REPLACED BATTERY ASSY, OPS CHECKS OK. 2 L 7 4 4F A20WE 1998092500652 19980925 00652 NM 1998 9 25 UPS98427690 1 19980921 A 3350 BATTERY PACK BOEING 747 747123 1384873 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-N/A, EMERGENCY CEILING LIGHT MAIN DECK STA 300 INOP. REPLACED BATTERY PACK IN EMERGENCY LIGHT ASSY AT S TA 350 RT, OPERATION CHECKS GOOD. 2 L 7 4 4F A20WE 1998092500653 19980925 00653 WP 1998 9 25 UPS98827687 1 19980828 A 5751 5705321509 WEIGHT DOUG DC8 DC871F 302199D WP LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 706UP 46056 INSPECTION TYPE-C, LEFT I/B AILERON I/B BALANCE WEIGHT HAS MODERATE CORROSION. REMOVED AND REPLACED THE I/B AILERON IAW MM 27-11-01. 2 L 7 4 4F RT 4A25 1998092500654 19980925 00654 EU 1998 9 25 QXEA9801297 1 19980917 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 EMERGENCY EXIT SIGN AT ROW 8 HAS SEVERAL 28V BULBS OUT. MAINTENANCE RELAMPED SIGN, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998092500655 19980925 00655 1998 9 25 98FDEA00584 4 19980918 A 2210 ACCESSORY BOX BOEING 727 7272D4 138407U NM AUTOPILOT FAILED A FDEA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 25 287FE 21849 CLIMBOUT, AC ELEV BUMPED IN LEFT TURN. AUTO PILOT SERVO IN AB. AFT LEVEL OF FLT LEVEL 310 ELEV TRIM RAN AWAY. AUTO PI LOT DISCONN AND CRUISE CONT TO RUN. COULD NOT DUP PROBLEM. REMOVED AND REPLACED AUTO PILOT ACCY BOX PER MM 22-11-141 A ND RELAY R102 AUTO PILOT AND STAB TRIM SYS. REPLACED RELAY. AC DOWNGRADED TO NOT CATEGORY 2 CHECK A AND B. 2 L 7 3 4F A3WE 1998092500656 19980925 00656 WP 1998 9 25 98FDEA00585 1 19980528 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1721 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 371FE 46609 UPPER INTERNAL FUSELAGE BS 1721, LONG 13 RT SIDE, FOUND 1 CRACK ABOUT 5 INCHES LONG ON FRAME. REPAIR ACCOMPLISHED WITH INSTALLATION OF REPAIR FRAME SECTION AND NEW SPLICES IAW SRM 53-10-00, FIG 5. (28 AUGUST 1998). 2 L 7 3 4F A22WE 1998092500657 19980925 00657 WP 1998 9 25 98FDEA00586 1 19980919 A 3260 ACG7353 TARGET DOUG DC10 DC1030 3023501 WP NLG FAILED A FDEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SO 25 318FE 46837 NOSE GEAR INDICATED UNSAFE UPON GEAR RETRACTION AFTER ALT GEAR EXTENSION CHECK. AFTER CYCLING NOSE GEAR INDICATED UNSAF E BOTH UP AND DOWN AML NR 865177. *S/D* REMOVED AND REPLACED INSULATION BLANKET, WIRING BUNDLE AND NOSE LAND GEAR LOCK SENSOR TARGET. 2 L 7 3 4F A22WE 1998092500658 19980925 00658 NE 1998 9 25 98FDEA00581 2 19980918 A 7250 TURBINE BOEING 727 727233 138408A NM PWA JT8 JT8D17 52049 NE NR 3 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN T ENGINE CASE PENETRATION CL CLIMB 1 SO 25 282FE 22349 AT ROTATION, HEARD LOUD POP FROM RT SIDE OF A/C. ENG NR 3 HAD ROLL BACK TO EPR, OF 1.80, N1=80 PERCENT, EGT=500 DEG CEL SIUS, N2=80 PERCENT, FUEL FLOW=5,000 LBS. ENG NR 1 AND NR 2 IND NORM PWR, CONT T/O AND CLIMBOUT. ACCOMPLISHED ENG FAIL /SEVERE DAMAGE CKLIST. SHUTDOWN ENG, RETURNED TO IND AND LANDED. *S/D* REMOVED AND REPLACED NR 3 ENG PER FEDEX WORK C ARD NR 70T0001-03. PERFORM ENG CK PER CHAPTER NR 72-00, AND JET RUN HANDBOOK NR 3 ENG OPER CK NORM. 2 L 7 3 4F 4 F RT A3WE E2EA 1998092500659 19980925 00659 WP 1998 9 25 ABXA9800836 1 19980914 A 3350 1437 BULB DOUG DC8 DC863 302198A WP CABIN FAILED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 822AX 46079 DURING PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHT FORWARD OF THE CREW ENTRY DOOR INOP. RELAMPED, OPS CHECKED NORMAL. 2 L 7 4 4F 4A25 1998092500660 19980925 00660 WP 1998 9 25 ABXA9800837 1 19980914 A 3350 501122804 POWER SUPPLY DOUG DC8 DC861 3021952 WP CABIN DEFECTIVE A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 843AX 1250 46017 DURING SERVICE CHECK, FOUND EMERGENCY POWER SUPPLY FAILED CHECK. REMOVED AND REPLACED EMERGENCY POWER SUPPLY PER DC8 MM 24-30. 2 L 7 4 4F 4A25 1998092500661 19980925 00661 WP 1998 9 25 ABXA9800838 1 19980916 A 2110 5614845517 CTC DOUG DC8 DC861 3021952 WP NR 1 SEIZED A ABXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 845AX 46157 AFTER TAKEOFF WHILE CLIMBING THRU FL200, A LOUD CTC HOWL WAS HEARD WITH A STRONG SMELL OF SOMETHING BURNING. OBSERVED N R 1 CTC SURGING. SHUT OFF NR 1 CTC AND BURNING ODOR DISAPPEARED IN APPROXIMATELY 5 MINUTES. NO ADDITIONAL PROBLEMS NOT ED. FOUND NR 1 CTC COMPRESSION FAN SEIZED, NO ROTATION. REPLACED NR 1 CTC IAW DC-8 MM CH 21-50. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998092500662 19980925 00662 WP 1998 9 25 MWEA98964 1 19980917 A 3350 S103 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 FORWARD ATTENDANT PORTABLE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERIES. 2 L 7 2 4F A6WE 1998092500663 19980925 00663 WP 1998 9 25 MWEA98965 1 19980917 A 3350 60030431 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A MWEA K NONE L NO TEST NR NOT REPORTED 1 GL 31 501ME 47132 COCKPIT OVERHEAD PANEL EVACUATION LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY SUPPLY. 2 L 7 2 4F A6WE 1998092500664 19980925 00664 WP 1998 9 25 MWEA98966 1 19980917 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER NR NOT REPORTED 1 GL 31 95 47132 FORWARD ENTRY DOOR EVACUATION SLIDE COVER PARTIALLY OFF. RESECURED FORWARD ENTRY DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998092500665 19980925 00665 WP 1998 9 25 MWEA98967 1 19980917 A 2560 5917689103 COVER DOUG DC9 DC914 3022034 WP PAX DOOR DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 80ME 45795 FORWARD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998092500666 19980925 00666 NM 1998 9 25 DL73K981927 1 19980917 A 2910 LINE BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENG HYD LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 309DL 23081 709166 HYD LEAK A-SYS TOTAL LOSS. FOUND LEAK NR 1 ENG. REPLACED HYD PUMP PRESS AND CASE DRAIN LINES. REPLACED HYD PUMP AS PRE CAUTION. CHECKED CASE DRAIN FILTER FOR CONTAMINATION, NONE FOUND. REPLACED SAME. SERVICED SYS RAN ENGS AND FLT CONTRO LS TO BLEED. ALL CKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2EA 1998092500667 19980925 00667 NM 1998 9 25 DLM88981928 1 19980917 A 2910 LINE DOUG MD88 MD88 3023688 NM LT HYD SYST LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 991DL 53343 LEFT HYD SYS QTY WENT TO ZERO. PRESS WENT TO ZERO. FOUND LT SYSTEM SUPPLY LINE LEAKING. PERMASWAGED LINE. 2 L 7 2 4F RT A6WE 1998092500669 19980925 00669 NM 1998 9 25 DL72S981931 1 19980917 A 2782 ANGLE BOEING 727 727225 1384077 NM NR 3 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 FOUND ON A1 LETTER CK, NR 3 SLAT I/B ACTUATOR ATTACH ANGLE CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998092500670 19980925 00670 NM 1998 9 25 DL72S981932 1 19980917 A 5320 WEB BOEING 727 727225 1384077 NM BS 1223-1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 805EA 22436 FOUND ON A1 LETTER CK, RT VERTICAL WEB IN LOWER TORQUE BOX AREA CRACKED STA 1223 AND 1233 AT LIGHTENING HOLES. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998092500671 19980925 00671 NM 1998 9 25 DL76G981935 1 19980917 A 2710 251T0100353 ROD END BOEING 767 767332 1382001 NM RT AILERON BROKEN A DALA K NONE F FLT CONT AFFECTED DE DESCENT 1 SO 27 169DZ 29689 ROD END ON CONTROL ROD BETWEEN RT AIL LCCA AND RT LCCA TORQUE TUBE BROKEN. REPLACED INPUT ROD ASSY. 2 L 7 2 4F RT A1NM 1998092500672 19980925 00672 NM 1998 9 25 DLM88981936 1 19980917 A 3350 POWER SUPPLY RPS1 DOUG MD88 MD88 3023688 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920DL 557 49644 EMERGENCY EXIT LIGHTS INOP ROW 29 AFT INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F RT A6WE 1998092500673 19980925 00673 NM 1998 9 25 DL72S981938 1 19980916 A 5320 655612671 CHORD BOEING 727 727232 1384082 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 THE C-2 DOOR STA 990 INBOARD CHORD WAS FOUND WITH A GOUGE AT STRINGER 26R. THE GOUGE WAS LOCATED ON THE OUTER CORNER OF THE INTERSECTION OF THE 2 LEGS OF THE L-SHAPED CHORD. REPAIRED PER ER/A 332209-14 REV A. 2 L 7 3 4F A3WE 1998092500674 19980925 00674 NM 1998 9 25 DL72S981939 1 19980916 A 5330 6558607 SKIN BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 A CRACK WAS FOUND IN THE FUSELAGE SKIN, SIMILAR TO S/B 727-53-0172. STRINGER 18A LOWER FLANGE WAS FOUND WITH A CRACK. R EPAIR PER ERA 332141-14. 2 L 7 3 4F A3WE 1998092500675 19980925 00675 NM 1998 9 25 DL72S981940 1 19980916 A 5713 6483386 STRINGER TAB BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 STRINGER 18 TAB ON THE RT WING VENT BOX WAS FOUND CRACKED. REPAIR PER ER/A 332222-14. 2 L 7 3 4F A3WE 1998092500676 19980925 00676 NM 1998 9 25 DL72S981941 1 19980916 A 5320 651592367 CLIP BOEING 727 727232 1384082 NM BS 400 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 FS 400 FRAME CLIP BETWEEN STR 17 AND 18 WAS FOUND CRACKED. REPAIRED PER ER/A 332224-14 REV A. 2 L 7 3 4F A3WE 1998092500677 19980925 00677 NM 1998 9 25 DL72S981942 1 19980916 A 5720 STIFFENER BOEING 727 727232 1384082 NM WS 300 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 WING UPPER SURFACE J STIFFENER REPAIR (STR 17 RT AT WS 300). REPAIR PER ER/A 332215-14 REV A. 2 L 7 3 4F A3WE 1998092500678 19980925 00678 NM 1998 9 25 DL757981946 1 19980919 A 3230 VALVE 2670112 BOEING 757 757232 1384965 NM NLG MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 628DL 2138 22918 GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR RAISED. GEAR PLACED TO OFF AND UP WITH NO STATUS CHANGE. GEAR CYCLED D OWN THEN UP WITH NO STATUS CHANGE. REPLACED NLG DOOR SAFETY VALVE. 2 L 7 2 4F RT A2NM 1998092500679 19980925 00679 NM 1998 9 25 DL73E981948 1 19980920 A 3230 BACC18Z2R CIRCUIT BREAKER BOEING 737 7372S3 NM COCKPIT TRIPPED A DALA K NONE J WARNING INDICATION CL CLIMB 1 SO 27 369DL 21776 AIR TURNBACK DUE TO LANDING GEAR LEVER WOULDN'T MOVE TO UP POS ON T/O. ABNORMAL PROCEDURES RUN TO RAISE LANDING GEAR. L AND GEAR EXT NORMAL ON RETURN. RESET LEVER LATCH C/B. CYCLED LAND GEAR LEVER, ALL IND NORMAL. REPLACED LEVER LATCH C/ B. CYCLED L/G LEVER SEVERAL TIMES, SYS OPS NORMAL. 2 L 7 2 4F RT A16WE 1998092500680 19980925 00680 NM 1998 9 25 DL73K981951 1 19980920 A 7933 TEMP BULB 56B85B BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN M OVER TEMP CL CLIMB 1 SO 27 312DL 002731 23084 717141 SHUT DOWN NR 1 ENGINE IN FLIGHT DUE TO HIGH OIL TEMP. FOUND NR 1 ENG OIL TEMP BULB OPEN. REPLACED TEMP BULB PER M/M, O PN CKD GOOD. LK CK GOOD. RAN ENG PER PFHB. ALL CKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2EA 1998092500681 19980925 00681 NM 1998 9 25 DL757981952 1 19980918 A 5414 311N31108 SKIN BOEING 757 757232 1384965 NM NR 2 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 643DL 23997 THE NR 2 PYLON OUTBD STRUT SKIN WAS FOUND WITH A CRACK IN THE UPPER FWD CORNER OF THE STRUT SKIN CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH A DOUBLER AND TRIPLER PER SRM 54-51-01-2, FIG 203. OVERSIZED FASTENERS WERE AUTHORIZED PER ER/A 365652-14, REV A. 2 L 7 2 4F RT A2NM 1998092500682 19980925 00682 NM 1998 9 25 DL72W981953 1 19980919 A 5330 SKIN BOEING 727 727247 138408F NM L1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 A .25 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUT FOR THE L1 DOOR. THE CRACK WAS REPAIRED PER BAC S/B 53 -0198 EXCEPT COUNTERSUNK HI-LOKS WERE INSTALLED INSTEAD OF PROTRUDING HEAD HI-LOKS. THE REPAIR WAS DOCUMENTED PER ER/A3 65693-14. 2 L 7 3 4F A3WE 1998092500683 19980925 00683 NM 1998 9 25 DLM11981954 1 19980920 A 2611 DETECTOR DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 802DE 48473 LAV 214 SMOKE DETECTOR INOP. REPLACED DETECTOR, CHECKS OK. 2 L 7 3 4F RT A22WE 1998092500684 19980925 00684 NM 1998 9 25 DL733981955 1 19980919 A 3397 WIRE BOEING 737 737347 1384647 NM CABIN LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 3301 23181 TRACK LIGHT AT SEAT 1-C INOP. FOUND WIRE UNHOOKED UNDER SEAT, OPS CK OK NOW. 2 L 7 2 4F RT A16WE 1998092500685 19980925 00685 NM 1998 9 25 DL72S981957 1 19980917 A 5530 65174636 STRINGER BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 STRINGER 8R WAS FOUND WITH A CRACK THROUGH THE INBD FLANGE AT A RIB ATTACH POINT WHICH PROGRESSED TO THE CENTER OF THE S TRINGER WEB. THE CRACK WAS REPAIRED WITH TWO ALUMINUM ANGLES PER ER/A 365679-14, REV A. 2 L 7 3 4F A3WE 1998092500686 19980925 00686 WP 1998 9 25 DLL19981958 1 19980918 A 5311 FRAME LKHEED 1011 10113853 5265020 WP BS 983 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 760DH 193Y1194 THE FS 983 FRAME WAS FOUND WITH THE TYPICAL AD 91-21-51, CRACK AT WL 185 ON THE LT SIDE. THE CRACK WAS ROUTED OUT AND R EPAIRED PER LAC S/B 093-53-266 USING THE LCC-7622-325 REPAIR WITH SOME FASTENER DEVIATIONS. THE REPAIR WAS ACCOMP LISHED PER ER/A 365628-14, REV B. 2 L 7 3 4F A23WE 1998092500687 19980925 00687 NM 1998 9 25 DL72S981959 1 19980918 A 5330 65562312 SKIN BOEING 727 727232 1384082 NM BS 373 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 499DA 21143 THE R1 DOOR SURROUND SKIN ASSY WAS FOUND WITH A 2.25 INCH TYPICAL CRACK IN THE BEAR STRAP AT THE UPPER HINGE CUTOUT. TH E CRACK WAS REPAIRED PER BAC S/B 727-53-0136, REV 3. THE REPAIR WAS DOCUMENTED PER ER/A 365667-14. NOTE: THE BEAR STR AP HAD THE S/B 53-0136 CORNER RADIUS TRIM MODIFICATION ACCOMPLISHED PRIOR TO CRACK INITIATION. 2 L 7 3 4F A3WE 1998092500688 19980925 00688 NM 1998 9 25 SCNA98714 1 19980902 A 5313 STRINGER BOEING 727 727259 138408J NM BS 720 CORRODED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINT CHECK, EXFOILIATION WAS FOUND PRESENT AT STA 720C STR 28R AT BOTTOM OF RIB UNDER LEVELING COMPOUND. REMOVED DAMAGED AREA IAW B727 SRM 513002 AND 531004 FIGURE 13. FABRICATED NEW DOUBLER OUT OF 7075 T6 .071 IAW B727 SR M 531004. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998092500689 19980925 00689 NM 1998 9 25 SCNA98103 1 19980917 A 3350 900835A SIGN BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE LEFT SIDE OVERWING EMERGENCY EXIT SIGNS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER IAW MM 335071 AND LIGHTS OPERATIONALLY CHECK GOOD. 2 L 7 3 4F RT A3WE 1998092500690 19980925 00690 NM 1998 9 25 SCNA98104 1 19980917 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND RE PLACED THE BATTERY PACK IAW MM 335022 AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998092500691 19980925 00691 NM 1998 9 25 SCNA98105 1 19980917 A 3350 20131A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE AFT EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK IAW MM 335071 AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998092500692 19980925 00692 NM 1998 9 25 SCNA98106 1 19980915 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE LEFT CENTER OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPL ACED THE POWER SUPPLY AND BATTERY PACK AT M951, ALL EMERGENCY EXIT LIGHTS CHECK GOOD. 2 L 7 3 4F A3WE 1998092500693 19980925 00693 NM 1998 9 25 SCNA98102 1 19980910 A 3350 1000677 LIGHT BOEING 727 7272J4 1384006 NM R1 DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK THE R1 DOOR PORTABLE EMERGENCY LIGHT ASSEMBLY ILLUMINTAES WHEN POWER REMOVED FROM THE AI RCRAFT WITH THE EMERGENCY LIGHT IN THE OFF POSITION. REMOVED AND REPLACED THE R1 DOOR PORTABLE EMERGENCY LIGHT ASSEMBLY. EMERGENCY LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998092500694 19980925 00694 NM 1998 9 25 SCNA98715 1 19980902 A 5320 SUPPORT BOEING 727 727259 138408J NM BS 320 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINT CHECK, FLOORBOARD SUPPORT FRAME WAS FOUND TO HAVE CORROSION A BS STA 320. CORROSION ON FLOORBOARD SUPPORT BEAM WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. REMOVED DAMAGED FLOORBEAM SUPPORT IAW B727 SRM 513002. FABRICATED NEW FLOOR BEAM SUPPORT FROM 7075 T6, EXTRUSION AND FILLER FROM 7075 T6 .063 IAW B727 SRM 531002 AND SRM 5140 03. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998092500695 19980925 00695 NM 1998 9 25 DHL98717002 1 19980919 A 7312 320115 VALVE BOEING 727 72723 1384004 NM PWA JT8 JT8D7 52053 NE NR 1 ENGINE FAILED A DHLA A E UNSCHED LANDING ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 717DH 19389 ON CLIMBOUT, NR 1 ENG FUEL HEAT VALVE LIGHT CAME ON. OIL TEMP ROSE TO 140 DEGREES CELSIUS. RETARDED THROTTLE AND HEAT ROSE TO 145 DEGREES. INCREASED THROTTLE TO 80 PERCENT N2 AND TEMP DECREASED TO 140 DEGREES AFTER 15 MIN. SHUT DOWN ENG INE PER AOM. OIL TEMP EXCEEDED 120 DEGREES FOR 21 MIN ALL OTHER INDICATIONS NORMAL. REPLACED FUEL HEAT VALVE, REPLACE D OIL AND OIL FILTER PER MM 72-00 RAN ENG FOR 5 MIN, INDICATIONS NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998092500696 19980925 00696 1998 9 25 DHL98801004 4 19980920 A 3442 20675680501 ANTENNA DOUG DC8 DC873F 302199F WP FUSELAGE INOPERATIVE A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 801DH 46033 WEATHER RADAR INOP. REPLACED ANTENNA PER MM. 2 L 7 4 4F RT 4A25 1998092500698 19980925 00698 NM 1998 9 25 P5CA9801461 1 19980921 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 1970-1980 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 35L, BS 1970 TO 1980. REPAIRED AS PER SRM 51-40-03 FIGURE 1. 2 L 7 4 4F A20WE 1998092500699 19980925 00699 NM 1998 9 25 P5CA9801462 1 19980921 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 1980 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 60L, BS 1980. REPAIRED AS PER SRM 51-40-03 FIGURE 1. 2 L 7 4 4F A20WE 1998092500700 19980925 00700 NM 1998 9 25 P5CA9801463 1 19980910 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 2063 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 50L, BS 2063. REPAIRED AS PER SRM 51-40-03 FIGURE 1. 2 L 7 4 4F A20WE 1998092500701 19980925 00701 NM 1998 9 25 P5CA9801464 1 19980910 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 2000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 40R, BS 2000. REPAIRED AS PER SRM 51-40-03 FIGURE 1. 2 L 7 4 4F A20WE 1998092500702 19980925 00702 NM 1998 9 25 P5CA9801465 1 19980910 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS1935-1940 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 BULK CARGO FLOOR SUPPORT FOUND CRACKED BL 20R, BS 1935 TO 1940. REPAIRED AS PER SRM 51-40-03 FIGURE 2. 2 L 7 4 4F A20WE 1998092500703 19980925 00703 NM 1998 9 25 P5CA9801466 1 19980910 A 5320 SHEAR TIE BOEING 747 747122 1384872 NM BS 2320 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 SHEAR TIE FOUND CRACKED BS 2320, STR 18 TO 19R. REPAIRED AS PER SRM 51-10-04 FIGURE 4. 2 L 7 4 4F A20WE 1998092500704 19980925 00704 NM 1998 9 25 P5CA9801467 1 19980910 A 5320 SHEAR TIE BOEING 747 747122 1384872 NM BS 2160 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 SHEAR TIE FOUND CRACKED BS 2160, STR 21-22R. REMOVED AND REPLACED TIE AS PER SRM 51-10-01 PAGE 18. 2 L 7 4 4F A20WE 1998092500705 19980925 00705 NM 1998 9 25 P5CA9801468 1 19980910 A 5320 WEB BOEING 747 747122 1384872 NM BS 2230 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME SUPPORT WEB FOUND CRACKED BS 2230, STR 174. STOP DRILLED, NDT INSPECTED AND REPAIRED AS PER SRM 51-10-04 FIGURE 7 1. 2 L 7 4 4F A20WE 1998092500706 19980925 00706 NM 1998 9 25 P5CA9801469 1 19980910 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 420-440 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME INTERCOSTAL FOUND CRACKED BS 420 TO 440, STR 8-9R. REMOVED AND REPLACED AS PER SRM 51-10-01 PAGE 18. 2 L 7 4 4F A20WE 1998092500707 19980925 00707 NM 1998 9 25 P5CA9801470 1 19980910 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 570 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 SEAT TRACK INTERCOSTAL SUPPORT FOUND CRACKED BS 570, BL 32R. REMOVED AND REPLACED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998092500708 19980925 00708 NM 1998 9 25 P5CA9801471 1 19980910 A 5320 SHEAR TIE BOEING 747 747122 1384872 NM BS 1680 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL ONE CORROSION FOUND ON AFT CARGO COMPARTMENT SHEAR TIE, BS 1680, STR 50-51R. REPAIRED AS PER SRM 53-10-03 FIGURE 3. 2 L 7 4 4F A20WE 1998092500709 19980925 00709 NM 1998 9 25 P5CA9801472 1 19980910 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 610-615 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FLOOR PANEL INTERCOSTAL SUPPORTS (TWO EACH) FOUND BROKEN, FWD CARGO COMPARTMENT BS 610-615, BL 40L. REPLACED SUPPORTS A S PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998092500710 19980925 00710 NM 1998 9 25 P5CA9801473 1 19980910 A 5320 FRAME BOEING 747 747122 1384872 NM L3 DOORWAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FORWARD FRAME UPPER HINGE CUTOUT CRACKED, MAIN DECK L3 DOOR. REPAIRED AS PER HAECO REPAIR ORDER R52-11-33839. 2 L 7 4 4F A20WE 1998092500711 19980925 00711 NM 1998 9 25 P5CA9801474 1 19980910 A 5320 ANGLE BOEING 747 747122 1384872 NM COCKPIT DOORWAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 HINGE SUPPORT FOUND CRACKED AT DOOR ATTACH AREA, COCKPIT ESCAPE HATCH. REPLACED HINGE SUPPORT ANGLE PER MM 52-21-00. 2 L 7 4 4F A20WE 1998092500712 19980925 00712 NM 1998 9 25 P5CA9801475 1 19980910 A 5730 PANEL BOEING 747 747122 1384872 NM RT WING DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 STRESS PANEL NR 688JT FOUND DELAMINATED. HOT BOND REPAIRED AS PER SRM 51-40-06 FIGURE 17A. 2 L 7 4 4F A20WE 1998092500713 19980925 00713 NE 1998 9 25 P5CA9801476 2 19980910 A 7250 FLANGE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 685859 FOUND RADIAL OD LIGHTENING HOLE CRACK, R FLANGE AT 10:00 POSITION. WELD REPAIRED PER MM 72-53-01 REPAIR 22. 2 L 7 4 4F 4 F A20WE E20EA 1998092500714 19980925 00714 WP 1998 9 25 ARWA980910 1 19980919 A 5711 5597838501 SPAR DOUG DC8 DC862 3021970 WP WS 515-526.76 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 RT WING FRONT SPAR LOWER CAP HAS TWO ADJACENT ATTACHMENT HOLES CRACKED BETWEEN STA XFS 515.000 AND XFS 526.760. CUT OU T DAMAGED AREA PER DRA J060232, FABRICATED FILLER, ANGLES AND DOUBLER PER DRG J060232 AND ROD SKETCH 97-02-10-005. LOCA TED, DRILLED AND STRESS COINED HOLES PER DPS 3.67 TREATED AND PRIMED PARTS PER SRM 51-1-8. INSTALLED REPAIR PER DRAWING J060232, ROD SKETCH 97-02-10-005 AND SRM 51-1-20 ACTION NR 379462, FILE NR 98-09-017. 2 L 7 4 4F 4A25 1998092500715 19980925 00715 NM 1998 9 25 VNAA9809015 1 19980917 A 5610 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT BIRDSTRIKE A VNAA K NONE O OTHER CL CLIMB 1 GL 07 432JS 3045 DURING THE CLIMBOUT, THE AIRCRAFT WAS STRUCK BY A BIRD ON THE COCKPIT RIGHT SIDE WINDSHIELD. THE AIRCRAFT CONTINUED TO CLE AND EXECUTED A NORMAL LANDING. OUTSTATION MAINTENANCE IN CLE, INSPECTED THE AIRCRAFT FOR DAMAGE, IN ACCORDANCE WIT H DORNIER MAINTENANCE MANUAL 05-57-07. NO DEFECTS WERE NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998092500716 19980925 00716 WP 1998 9 25 TC8A98058 1 19980918 A 7830 THRUST BRAKE DOUG DC8 DC862F 3021972 WP NR 4 ENGINE LACK OF LUBE A TC8A D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 187SK 46022 ON TAXI OUT, NR 4 THRUST BRAKE LIGHT START FLASHING. UNABLE TO EXTINGUISH IT. TAXI BACK FOR MAINT. CLEANED MICROSWITC H AND LUBE NR 4 ENGINE THRUST BRAKE IAW DC8 M/M 78-30-0, OPS CHECK NORMAL. 2 L 7 4 4F 4A25 1998092500717 19980925 00717 NE 1998 9 25 TC8A98059 2 19980920 A 7530 PRBC LINE DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE LOOSE A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 183SK 45904 671250 NR 2 ENGINE WOULD NOT ACCELERATE. CONTINUOUS COMPRESSOR STALL WHEN THROTTLE WAS PUSHED PAST IDLE. CHECKED PRBC SENSE L INES AND FOUND 1 LOOSE. SECURED LOOSE SENSE LINES IAW M/M 75-30-2. CREW RAN UP ENGINE AND OPS CHECK OF THE PRBC VALVE GOOD. 2 L 7 4 4F 4 F 4A25 1E8 1998092500718 19980925 00718 NM 1998 9 25 CALA9801846 1 19980921 A 3397 WIRE BOEING 727 727232 1384082 NM CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND R-1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT LIGHT A SSEMBLY. 2 L 7 3 4F A3WE 1998092500719 19980925 00719 NM 1998 9 25 CALA9801847 1 19980921 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1166 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT BS 1166, RBL 50 TO RBL 66. THE CORROSION WAS REMOVED AND A REPA IR STRAP WAS INSTALLED IAW SRM 51-30-5, 51-10-2, 51-30-2, AND ECRA 5321-01029. 2 L 7 3 4F A3WE 1998092500720 19980925 00720 WP 1998 9 25 CALA9801848 1 19980921 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 313 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 313, LONGERON 23L. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38. 2 L 7 2 4F A6WE 1998092500721 19980925 00721 WP 1998 9 25 CALA9801849 1 19980915 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 2033 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND A 4.5 INCH CRACK IN LONGERON 9R AND 6R. ALSO, 8 INCH CRACK WAS FOUND IN LONGERON 4L, AT STA 2033. THE CRACKED AREAS OF LONGERON WERE REPAIRED IAW SRM 53-10-00, FIGURE 3. 2 L 7 3 4F A22WE 1998092500722 19980925 00722 WP 1998 9 25 CALA9801850 1 19980915 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 2122 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68060 47850 INSPECTION FOUND 11 INCH CRACK IN LONGERON 13L AT STA 2122. THE LONGERON WAS REPAIRED IAW SRM 53-10-00, FIGURE 3. 2 L 7 3 4F A22WE 1998092500723 19980925 00723 NM 1998 9 25 CALA9801851 1 19980922 A 5330 SKIN BOEING 727 727232 1384082 NM BS 500 LIGHTNING STRIKE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO STATIC PORT SKIN ON RT FUSELAGE FORWARD OF FORWARD PIT DOOR AT STA 500. THE DAMAGE WAS REPAIRED IAW SRM 53-30-03. 2 L 7 3 4F A3WE 1998092500724 19980925 00724 NM 1998 9 25 CALA9801852 1 19980922 A 5753 FITTING BOEING 727 727232 1384082 NM NR 6 FLAP TRACK CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING CORRODED. THE FLAP TRACK FITTING WAS REMOVED AND REPLAC ED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998092500725 19980925 00725 WP 1998 9 25 CALA9801853 1 19980922 A 5753 VANE DOUG DC9 DC932 3022066 WP RT TE FLAP GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 70542 47535 INSPECTION FOUND RT WING UPPER MOVEABLE VANE LEADING EDGE GOUGED. A REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 1, 51-10 -4, 51-10-3, 51-30-2, AND 51-10-2. 2 L 7 2 4F A6WE 1998092500726 19980925 00726 WP 1998 9 25 9810079984 1 19980920 A 3260 SENSOR DOUG DC9 DC932 3022066 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 984US 47383 DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW DECLINED A RED EMERGENCY AND CON FIRMED VISUALLY THAT NOSE GEAR WAS DOWN AND LOCKED. MAINTENANCE REPLACED NOSE GEAR DOWNLOCK PROXIMITY SENSOR. OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998092500727 19980925 00727 WP 1998 9 25 UPS98827698 1 19980902 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-C, STA 680 BULKHEAD HAS MANY CRACKS ON EACH SIDE OF VERTICAL STIFFENERS IN FWD ACC COMP LBL 32 TO RBL 28 . REPAIRED AREA IAW SRM 53-2-5 FIG 13. 2 L 7 4 4F RT 4A25 1998092500728 19980925 00728 WP 1998 9 25 UPS98827699 1 19980912 A 5311 97537518 FRAME DOUG DC8 DC871F 302199D WP BS 680 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-C, STA 680 FRAME HAS CORROSION AT LONG 27 TO 28R. REMOVED, FABRICATED AND REPLACED FRAME SECTION IAW DW G 9753751 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998092500729 19980925 00729 WP 1998 9 25 UPS98827700 1 19980914 A 5320 97537514N WEB DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-C, STA 680 RT LWR WEB FOUND TO BE CRACKED IN RADIUS. REMOVED AND REPLACED WEB SECTION IAW DWG 9753751 A ND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998092500730 19980925 00730 WP 1998 9 25 UPS98827701 1 19980910 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 700-710 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-C, STA 700 TO 710, LONGERON 31R HAS HEAVY CORROSION. REPAIRED AREA IAW DHC SK 709-591. 2 L 7 4 4F RT 4A25 1998092500731 19980925 00731 WP 1998 9 25 UPS98827702 1 19980903 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-C, LT WING NR 2 MAIN TANK AFT UPPER ACCESS PANEL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 3 6. 2 L 7 4 4F RT 4A25 1998092500732 19980925 00732 WP 1998 9 25 UPS98827703 1 19980909 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1400 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-C, THE SKIN PANEL AT THE LOWER AFT CARGO COMP AFT DOOR JAMB IS CRACKED AT THE LOWER FWD CORNER. REPAIRE D AREA IAW DC8-5330-10707-A AND REFERENCE TO DHC SK 709-145. 2 L 7 4 4F RT 4A25 1998092500733 19980925 00733 WP 1998 9 25 UPS98827704 1 19980922 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 812UP 46112 INSPECTION TYPE-N/A, EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS, OPS CK GOOD P ER MM 34-50-01. (P/N 60-1223-5) (S/N 356) ON, (P/N 5708458-503) (S/N UPS2964) OFF. 2 L 7 4 4F RT 4A25 1998092500734 19980925 00734 EU 1998 9 25 QXEA9801298 1 19980826 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 TWO CRACKS LOCATED UNDER PANEL 81BG. REPAIRED IAW HORIZON AIR EA 4-57-170. 2 L 7 2 4F RT A20EU 1998092500735 19980925 00735 EU 1998 9 25 QXEA9801299 1 19980819 A 5753 VANE FOKKER F28 F28MK4000 4990810 EU RT TE FLAP OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 RIGHT-HAND INBOARD FLAP VANE INBOARD TRAILING EDGE GAP IS LESS THAN MINIMUM OF .080. MEASURED GAP IAW HORIZON AIR EA 4-2 7-57. GAP WITHIN LIMITS. 2 L 7 2 4F RT A20EU 1998092500736 19980925 00736 EU 1998 9 25 QXEA9801300 1 19980826 A 5755 PANEL FOKKER F28 F28MK4000 4990810 EU NR 3 SPOILER DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 NR 3 LIFT DUMPER PANEL HAS 3 DENTS ON PANEL ON THE LEFT-HAND WING. REPAIRED IAW FOKKER SRM 51-70-0, PAGE 6-12. 2 L 7 2 4F RT A20EU 1998092500737 19980925 00737 EU 1998 9 25 QXEA9801301 1 19980901 A 5542 SKIN FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 INNER AND OUTER SKIN CRACKED IN TWO PLACES ON RUDDER LEFT-HAND SIDE AT CENTER HINGE RECESSED AREA, JUST BELOW PANEL 57T. REPAIRED IAW FOKKER SRM 55-02-07, PAGE 9, FIGURE 5 AND SRM 51-31-01, PAGE 13, PARAGRAPH 71, 1 THROUGH 5. 2 L 7 2 4F RT A20EU 1998092500738 19980925 00738 EU 1998 9 25 QXEA9801302 1 19980824 A 5532 SKIN FOKKER F28 F28MK4000 4990810 EU VERT STAB CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 VERTICAL STABILIZER RIGHT-HAND TOP SKIN IS CHAFED 7 INCHES WIDE UNDER ICE SCRAPER. REPAIRED IAW HORIZON AIR EA 4-55-81. 2 L 7 2 4F RT A20EU 1998092500739 19980925 00739 EU 1998 9 25 QXEA9801303 1 19980825 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 LEFT-HAND AFT FUSELAGE SKIN IS DENTED. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1. 2 L 7 2 4F RT A20EU 1998092500740 19980925 00740 EU 1998 9 25 QXEA9801304 1 19980821 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 20077 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CRACKED CLIP, STOP DRILLED BUT EXCEEDS LIMITS AT FRAME 20077, AFT SIDE BETWEEN STRINGERS 31 AND 32. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 4. 2 L 7 2 4F RT A20EU 1998092500741 19980925 00741 EU 1998 9 25 QXEA9801305 1 19980812 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CLIP CRACKED ON FORWARD SIDE OF FRAME 16-2 AND STRINGER 26. REPAIRED IAW FOKKER SRM 51-31-01, PAGES 13 THROUGH 17. 2 L 7 2 4F RT A20EU 1998092500742 19980925 00742 EU 1998 9 25 QXEA9801306 1 19980812 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 SMALL CRACK ON FRAME CLIP ON FORWARD SIDE OF FRAME 32-2 AND STRINGER 7. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGUR E 3 AND SRM 51-31-01, PAGE 13. 2 L 7 2 4F RT A20EU 1998092500743 19980925 00743 EU 1998 9 25 QXEA9801307 1 19980812 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 SMALL CRACK ON FRAME CLIP ON AFT SIDE OF FRAME 32-2 AND STRINGER 29. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 THROUGH 17. 2 L 7 2 4F RT A20EU 1998092500744 19980925 00744 EU 1998 9 25 QXEA9801308 1 19980812 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 67-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CLIP CRACKED ON FORWARD SIDE OF FRAME 67-2 AT STRINGER 14. REPAIRED IAW FOKKER SRM 51-31-01, PAGES 13-17. 2 L 7 2 4F RT A20EU 1998092500745 19980925 00745 EU 1998 9 25 QXEA9801309 1 19980827 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 225.65 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 SHARP DENT IN SKIN, DENTED FROM INSIDE TAIL LOCATION STATION 225.65 X BL125L. REPAIRED IAW FOKKER SRM 53-02-02 AND HORI ZON AIR EA 4-53-533. 2 L 7 2 4F RT A20EU 1998092500746 19980925 00746 EU 1998 9 25 QXEA9801310 1 19980909 A 3350 BULB FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11167 FORWARD LEFT EMERGENCY OVERWING LIGHT IS INOP WHEN VIEWED FROM FORWARD GALLEY. RELAMPED THE TWO EMERGENCY OVERWING LIGH TS, OPS CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998092500747 19980925 00747 EU 1998 9 25 QXEA9801311 1 19980901 A 3350 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11167 ALL EVACUATION LIGHTS INOP. REPLACED OVERHEAD AFT BATTERY POWER SUPPLY. 2 L 7 2 4F RT A20EU 1998092500748 19980925 00748 EU 1998 9 25 QXEA9801312 1 19980826 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 TWO DENTED AREAS. REPAIRED IAW HORIZON AIR EA 4-53-453. 2 L 7 2 4F RT A20EU 1998092500749 19980925 00749 EU 1998 9 25 QXEA9801313 1 19980816 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 SCRATCH ON SKIN OF PASSENGER DOOR JUST FORWARD OF HAND GRIP. REPAIRED IAW FOKKER SRM 52-02-01, FIGURE 2. 2 L 7 2 4F RT A20EU 1998092500750 19980925 00750 EU 1998 9 25 QXEA9801314 1 19980815 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 THERE IS A CRACK AT RIB 6305 IN STRINGER 59A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998092500751 19980925 00751 EU 1998 9 25 QXEA9801315 1 19980815 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 THERE IS A CRACK AT RIB 6305 IN STRINGER 59 AT JOGGEL. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998092500752 19980925 00752 EU 1998 9 25 QXEA9801316 1 19980813 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 5305-8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 RIGHT-HAND INBOARD SEAT TRACK REQUIRES REPLACEMENT FROM STATION 5305 TO 8805 DUE TO NUMEROUS CORROSION ON TRACK. INSTAL LED NEW SEAT TRACK SPLICE SECTION IAW FOKKER SRM 53-02-15, FIGURE 1, SHEET 2. 2 L 7 2 4F RT A20EU 1998092500753 19980925 00753 EU 1998 9 25 QXEA9801317 1 19980815 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 6305 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 A PERMANENT REPAIR IS REQUIRED FOR A DENT LOCATED 1.5 INCHES FORWARD OF STA 6305. REPAIRED IAW FOKKER SRM 53-02-02, FIG URE 1. 2 L 7 2 4F RT A20EU 1998092500754 19980925 00754 EU 1998 9 25 QXEA9801318 1 19980815 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 6305 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 A PERMANENT REPAIR IS REQUIRED FOR A DENT LOCATED FOUR INCHES AFT STA 6305. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1. 2 L 7 2 4F RT A20EU 1998092500755 19980925 00755 EU 1998 9 25 QXEA9801319 1 19980824 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 5805 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 A PERMANENT REPAIR IS REQUIRED FOR A DENT LOCATED 3 INCHES FORWARD OF STA 5805. REPAIRED IAW FOKKER SRM 53-02-02, PAGE 2, FIGURE 1. 2 L 7 2 4F RT A20EU 1998092500756 19980925 00756 EU 1998 9 25 QXEA9801320 1 19980825 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 5305 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 A PERMANENT REPAIR IS REQUIRED FOR A DENT LOCATED FORWARD OF STA 5305. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-0 1. 2 L 7 2 4F RT A20EU 1998092500757 19980925 00757 EU 1998 9 25 QXEA9801321 1 19980815 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 16660 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 FRAME 16660 IN AREA BETWEEN STRINGER 32 AND 33 IS DENTED AND HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 4-53-534. 2 L 7 2 4F RT A20EU 1998092500758 19980925 00758 EU 1998 9 25 QXEA9801322 1 19980820 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305-6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CORROSION IN BOTTOM OF SEAT TRACK RIGHT-HAND OUTBOARD SEAT TRACK IN CABIN FRAME 6305 TO 6805. REPAIRED IAW FOKKER SRM 53 -02-15. 2 L 7 2 4F RT A20EU 1998092500759 19980925 00759 EU 1998 9 25 QXEA9801323 1 19980811 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CORROSION IN BEGINNING OF RIGHT-HAND OUTBOARD SEAT TRACK IN CABIN APPROXIMATELY .15 DIAMETER, .02 DEEP AT FRAME 4610. R EPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998092500760 19980925 00760 EU 1998 9 25 QXEA9801324 1 19980901 A 3350 BATTERY PACK FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 496US 11167 EMERGENCY DOOR LIGHT DID NOT COME ON DURING EMERGENCY LIGHT CHECK. INSTALLED UNDER SEAT EMERGENCY LIGHT BATTERY PACKS. 2 L 7 2 4F RT A20EU 1998092500761 19980925 00761 EU 1998 9 25 QXEA9801325 1 19980818 A 5220 JAMB FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 LEFT-HAND AFT OVERWING EMERGENCY EXIT HAS A CRACK IN FORWARD AND AFT CORNERS ON THE OUTSIDE MATING SURFACE AT THE TOP OF THE DOOR. REPAIRED IAW FOKKER SRM 52-02-03 PAGE 5 FIGURE 3. 2 L 7 2 4F RT A20EU 1998092500762 19980925 00762 EU 1998 9 25 QXEA9801326 1 19980825 A 5230 STRUCTURE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR MISMANUFACTURED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 AFT CARGO DOOR INNER STRUCTURE UNDER DOOR HOLD BRACKET INTERCOSTAL WAS OF IMPROPER HEIGHT. REPAIRED IAW FOKKER SRM 51-3 1-01. 2 L 7 2 4F RT A20EU 1998092500763 19980925 00763 EU 1998 9 25 QXEA9801327 1 19980827 A 2720 RUDDER PEDAL FOKKER F28 F28MK4000 4990810 EU RT COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 BASE ON CO-PILOTS RUDDER PEDAL ASSEMBLY IS CORRODED AT AND UNDER BOLT HOLE MOUNTING LOCATIONS. REPAIRED IAW HORIZON AIR EA 4-53-544, ITEM 3. 2 L 7 2 4F RT A20EU 1998092500764 19980925 00764 EU 1998 9 25 QXEA9801328 1 19980822 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 FORWARD LOWER CORNER OF REAR CARGO DOOR HAS A .75 INCH HOLE WITH PREVIOUS REPAIR THAT DOES NOT CONFORM TO SRM REPAIR'S. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998092500766 19980925 00766 EU 1998 9 25 QXEA9801330 1 19980823 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 DENT IN SKIN ON AFT BELLY OF AIRCRAFT. REPAIRED DAMAGE IAW FOKKER SRM 53-02-02 FIGURE 1. 2 L 7 2 4F RT A20EU 1998092500767 19980925 00767 EU 1998 9 25 QXEA9801331 1 19980819 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 STRINGER 5B INBOARD OF THE RIGHT-HAND AIR COLD PACK INTAKE PORT IS CRACKED ON FORWARD FASTENER HOLE. REPAIRED IAW FOKKE R SRM 53-02-01 FIGURE 6 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998092500768 19980925 00768 EU 1998 9 25 QXEA9801332 1 19980820 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 FRAME CLIP IS CRACKED AT FRAME 4610 AND STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998092500769 19980925 00769 EU 1998 9 25 QXEA9801333 1 19980820 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 4610 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 FRAME CLIP IS CRACKED AT FRAME 4610 AND STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 4. 2 L 7 2 4F RT A20EU 1998092500770 19980925 00770 EU 1998 9 25 QXEA9801334 1 19980827 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 REAR CARGO DOOR INNER SKIN HAS NUMEROUS DRILL STARTS. REPAIRED IAW HORIZON AIR EO 4-52-31A. 2 L 7 2 4F RT A20EU 1998092500771 19980925 00771 EU 1998 9 25 QXEA9801335 1 19980830 A 5320 PANEL FOKKER F28 F28MK4000 4990810 EU CARGO COMPT DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 REAR CARGO BAY PANEL 29AE IS DETERIORATED AND THIN IN PLACES. INSPECTED PANEL AND FOUND TO BE GOOD WITH LESS THAN 10 PE RCENT WEAR. 2 L 7 2 4F RT A20EU 1998092500772 19980925 00772 EU 1998 9 25 QXEA9801336 1 19980818 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CRACKED FRAME CLIP ON FRAME 13815B STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998092500773 19980925 00773 EU 1998 9 25 QXEA9801337 1 19980818 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CRACKED FRAME CLIP ON FRAME 13815B AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-11 PAGE 3 FIGURE 1. 2 L 7 2 4F RT A20EU 1998092500774 19980925 00774 EU 1998 9 25 QXEA9801338 1 19980818 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CRACKED FRAME CLIP ON FRAME 13815A AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-11 PAGE 3 FIGURE 1. 2 L 7 2 4F RT A20EU 1998092500775 19980925 00775 EU 1998 9 25 QXEA9801339 1 19980817 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CRACKED FRAME CLIP ON FRAME 14755 STRINGER 3. REPAIRED IAW FOKKER SRM 53-02-13 FIGURE 2. 2 L 7 2 4F RT A20EU 1998092500776 19980925 00776 EU 1998 9 25 QXEA9801340 1 19980828 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 15635 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 INDENTATION ON FRAME 15635 AT STRINGER 70. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 9. 2 L 7 2 4F RT A20EU 1998092500777 19980925 00777 EU 1998 9 25 QXEA9801341 1 19980828 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 15635 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 INDENTATION ON FRAME 15635 AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-01-01 PAGE 9. 2 L 7 2 4F RT A20EU 1998092500778 19980925 00778 EU 1998 9 25 QXEA9801342 1 19980828 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 15935 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 INDENTATION ON FRAME 15635 AT STRINGER 74. REPAIRED IAW FOKKER SRM 53-01-01, PAGE 9. 2 L 7 2 4F RT A20EU 1998092500779 19980925 00779 EU 1998 9 25 QXEA9801343 1 19980811 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CRACK IN UPPER RADIUS OF BEAM 3 LOCATED AT RIGHT-HAND END ON PRESSURE BULKHEAD. REPAIRED IAW HORIZON AIR EA 4-53-518. 2 L 7 2 4F RT A20EU 1998092500780 19980925 00780 EU 1998 9 25 QXEA9801344 1 19980831 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 16660 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 SMALL DENT IN OUTER FUSELAGE SKIN 3.5 INCHES AFT OF FRAME 16660 AND 1 ABOVE STRINGER 6. REPAIRED IAW FOKKER SRM 53-02-0 1 FIGURE 4. 2 L 7 2 4F RT A20EU 1998092500781 19980925 00781 EU 1998 9 25 QXEA9801345 1 19980816 A 5320 WALL FOKKER F28 F28MK4000 4990810 EU ACM COMPT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 LEFT-HAND ACM COMPARTMENT POSSIBLE CRACK IN WALL FORWARD OF FRAME 3050 AT STRINGER 4A. REPAIRED IAW FOKKER SRM 53-11-02 PAGE 3 FIGURE 2 AND SRM 51-31-05 PAGE 8 AND SRM 51-10-09 PAGE 9 PARAGRAPH 4. 2 L 7 2 4F RT A20EU 1998092500782 19980925 00782 EU 1998 9 25 QXEA9801346 1 19980819 A 5320 INTAKE FOKKER F28 F28MK4000 4990810 EU RT AC PACK CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 THE RIGHT-HAND AIR CONDITIONING PACK INTAKE PORT IS CRACKED ALONG LOWER CORNER. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998092500783 19980925 00783 EU 1998 9 25 QXEA9801347 1 19980820 A 5320 INTAKE FOKKER F28 F28MK4000 4990810 EU LT AC PACK CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 LEFT-HAND AIR CONDITIONING PACK INTAKE PORT APPEARS TO BE CRACKED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998092500784 19980925 00784 EU 1998 9 25 QXEA9801348 1 19980826 A 5320 PORT FOKKER F28 F28MK4000 4990810 EU RT AC PACK CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 RIGHT-HAND AIR CONDITIONING PACK EXHAUST PORT IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01 PAGE 13 PARAGRAPH 13. 2 L 7 2 4F RT A20EU 1998092500785 19980925 00785 EU 1998 9 25 QXEA9801349 1 19980818 A 5320 CASTING FOKKER F28 F28MK4000 4990810 EU FRAME 3820 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CRACK IN THE CORNER OF THE NOSE LANDING GEAR CASTING ON FRAME 3820 NEXT TO THE BRACKET FOR THE NOSE GEAR ACTUATOR. REPA IRED IAW HORIZON AIR EA 4-53-509. 2 L 7 2 4F RT A20EU 1998092500786 19980925 00786 EU 1998 9 25 QXEA9801350 1 19980822 A 5610 WINDOW FOKKER F28 F28MK4000 4990810 EU LT EYEBROW DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 PILOTS EYEBROW HAS AREA OF DELAMINATION IN ONE CORNER. REPAIRED IAW HORIZON AIR EO 4-53-56A. 2 L 7 2 4F RT A20EU 1998092500787 19980925 00787 EU 1998 9 25 QXEA9801351 1 19980831 A 5320 POST FOKKER F28 F28MK4000 4990810 EU RT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 NR 3 CO-PILOT WINDOW POST IS CRACKED IN UPPER AFT CORNER. REPAIRED IAW HORIZON AIR EA 4-53-45A. 2 L 7 2 4F RT A20EU 1998092500788 19980925 00788 EU 1998 9 25 QXEA9801352 1 19980826 A 5320 WALL FOKKER F28 F28MK4000 4990810 EU ACM COMPT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 LEFT-HAND ACM COMPARTMENT DENTS IN SIDE WALL BY AFT MOUNTS. REPAIRED IAW FOKKER SRM 53-02-02, FIGURE 1. 2 L 7 2 4F RT A20EU 1998092500789 19980925 00789 EU 1998 9 25 QXEA9801353 1 19980813 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU LT ACM DOORWAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 LEFT-HAND ACM ACCESS OPENING 23B AFT LOWER CORNER APPEARS TO BE CRACKED IN SKIN. REPAIRED IAW HORIZON AIR EA 4-53-515. 2 L 7 2 4F RT A20EU 1998092500790 19980925 00790 EU 1998 9 25 QXEA9801354 1 19980830 A 5320 POST FOKKER F28 F28MK4000 4990810 EU LT COCKPIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 LEFT-HAND WINDOW POST NR 3 CRACKED AT D5 AND D6 ATTACH HOLES. REPAIRED IAW HORIZON AIR EO 4-53-56A. 2 L 7 2 4F RT A20EU 1998092500791 19980925 00791 NM 1998 9 25 DLM88981960 1 19980921 A 4990 APU DOUG MD88 MD88 3023688 NM AFT FUSELAGE LEAKING A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 905DL 15436 49536 80529 AFTER TAKEOFF, THE FLIGHT ATTENDANTS REPORTED THE AFT LAVATORY SMOKE DETECTOR GOING OFF AND REPORTED SMOKE IN THE AFT CA BIN. RETURNED TO GATE. FOUND APU LEAKING OIL INTO INLET, DEFERRED. 2 L 7 2 4F RT A6WE 1998092500792 19980925 00792 NM 1998 9 25 DLM90981962 1 19980921 A 2120 AIR DISTRIBUTION DOUG MD90 MD9030 3023690 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 910DN 53390 ELECTRICAL FUMES SMELLED IN COCKPIT AND AFT CABIN DURING DESCENT. NO SMOKE WAS SEEN. THE SMELL CAME AND WENT TWICE. N OT DETECTABLE AFTER LANDING. INSPECTED CABIN LIGHTING, OPERATED APU AND PACKS AND BOTH ENGINES. GALLEY POWER, VIDEO, ENTERTAINMENT SYSTEM AND ALL LIGHTING SYSTEMS. NO ODOR PRESENT. ALL POWER SYSTEMS CHECKED NORMAL. LOWERED CABIN CEILI NG PANELS, NO TROUBLE FOUND. 2 L 7 2 4F RT A6WE 1998092500793 19980925 00793 NM 1998 9 25 DL72L981963 1 19980921 A 3297 MS18209387 WIRE BOEING 727 727232 1384082 NM RT MLG BROKEN A DALA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 27 510DA 21312 WHEN LANDING GEAR WAS LOWERED THE RLG GREEN DOWN AND LOCKED DIDN'T ILUMINATE. LIGHT DIDN'T PRESS TO TEST. CHANGED BULB S, NO HELP. WENT TO BRIGHT ON BRIGHT/DIM SWITCH AND INDICATION WERE NORMAL. SECURED WIRE ON BACK OF BRIGHT/DIM SWITCH, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1998092500794 19980925 00794 NM 1998 9 25 DL72W981964 1 19980813 A 5753 652163234 SPAR BOEING 727 727247 138408F NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 AFT SPAR RAIL CRACKED 2 PLACES, 21 INCHES FROM I/B END OF FLAP. REPAIRED PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998092500795 19980925 00795 NM 1998 9 25 DLM88981965 1 19980922 A 5330 SKIN DOUG MD88 MD88 3023688 NM C-1 DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DE 53378 THE OUTER FUSELAGE SKIN AT THE C-1 CARGO DOOR CUTOUT WAS FOUND DAMAGED AT THE AFT EDGE. THE DAMAGE IS APPROXIMATELY 0.5 X 1.5. DAMAGE WAS CAUSED BY GROUND DAMAGE. REPAIRED PER ERA 272471-14. 2 L 7 2 4F RT A6WE 1998092500796 19980925 00796 NM 1998 9 25 DL72S981967 1 19980922 A 5720 ANGLE BOEING 727 727232 1384082 NM NR 6 LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 NR 6 L/E FLAP ACT ATTACH ANGLE CRACKED O/B LOWER RADIUS. REPAIRED PER MM 57-20-21 PG 811. 2 L 7 3 4F A3WE 1998092500797 19980925 00797 NM 1998 9 25 DLM88981968 1 19980922 A 2910 299201062 HOSE DOUG MD88 MD88 3023688 NM RT HYD SYSTEM LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 919DE 53422 A/C LOST RT HYD PRESSURE AND FLUID, USED EMERGENCY PROCEDURES. REPLACED RT ENGINE HYD PUMP MAIN PRESSURE LINE. 2 L 7 2 4F RT A6WE 1998092500798 19980925 00798 NM 1998 9 25 DHL98709001 1 19980923 A 7933 10200002 TEMP BULB BOEING 727 72782C 1384026 NM NR 2 ENGINE FAILED A DHLA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CR CRUISE 1 SO 01 709DH 19968 EN ROUTE, NR 2 ENGINE OIL TEMP INDICATION 140 DEGREE CELSIUS AT CRUISE THRUST. REDUCED TO IDLE FOR APPROX 12 MIN, TEMPE RATURE CONTINOUSLY INDICATED 140C, PEAK TEMP 155C. ABNORMAL PROC AND ENGINE SHUT DOWN. REMOVED AND REPLACED TEMP BUL B, OIL AND FILTER. RESERVICED OIL AND GROUND RAN AIRCRAFT. 2 L 7 3 4F A3WE 1998092500799 19980925 00799 WP 1998 9 25 DHL98807007 1 19980922 A 2810 CAP DOUG DC8 DC873F 302199F WP NR 4 FUEL TANK MISSING A DHLA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 807DH 45990 SUSPECT FUEL LEAK IN NR 4 MAIN TANK AS VERIFIED BY VISUAL INDICATIONS AND LOSS OF FUEL BY GAUGE. FOUND OVERWING FUEL C AP MISSING ON PANEL 606A. 2 L 7 4 4F RT 4A25 1998092500800 19980925 00800 NM 1998 9 25 P5CA9801479 1 19980921 A 5414 SKIN BOEING 747 747122 1384872 NM NR 4 PYLON CHAFED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NUMBER FOUR PYLON OUTBOARD SKIRT FOUND CHAFED ON INSIDE SURFACE. REPAIRED PER SRM 54-30-03 FIGURE 35 AND 36. 2 L 7 4 4F A20WE 1998092500801 19980925 00801 NM 1998 9 25 P5CA9801480 1 19980921 A 5347 SEAT TRACK BOEING 747 747122 1384872 NM BS 735 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 SEAT TRACK INTERCOSTAL FOUND CRACKED, BS 735 BL 25L. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998092500802 19980925 00802 NM 1998 9 25 P5CA9801481 1 19980921 A 5314 KEEL BEAM BOEING 747 747122 1384872 NM BS 990-1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL ONE CORROSION FOUND AT KEEL BEAM FORWARD LEFT HAND INNER CHORD, BS 990 TO 1000, BL 8L. BLENDED AREA AND AREA REPR OTECTED PER SRM 53-10-01 AND 51-10-01. 2 L 7 4 4F A20WE 1998092500803 19980925 00803 NM 1998 9 25 P5CA9801482 1 19980921 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 805 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME SUPPORT ANGLE FOUND CRACKED, BS 805L, WL 199.5. REMOVED AND REPLACED ANGLE AS PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998092500804 19980925 00804 NM 1998 9 25 P5CA9801483 1 19980921 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 805 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME SUPPORT ANGLE FOUND CRACKED, BS 805R, WL 199.5. REMOVED AND REPLACED ANGLE AS PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998092500805 19980925 00805 NM 1998 9 25 P5CA9801484 1 19980921 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1600-2060 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL ONE CORROSION FOUND AT LAP SEAM, BS 1600 TO 2060, STR 12L. BLENDED AREA, AREA REPROTECTED AS PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998092500806 19980925 00806 NM 1998 9 25 P5CA9801485 1 19980921 A 5311 FRAME BOEING 747 747122 1384872 NM BS 600 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME RADIUS FOUND CRACKED BS 600, STR 19L. FRAME REPAIRED AS PER HAECO REPAIR SCHEME 53-22-33837. 2 L 7 4 4F A20WE 1998092500807 19980925 00807 NM 1998 9 25 P5CA9801486 1 19980921 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 2350 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL ONE CORROSION AND CRACKS FOUND AT HAT SECTION BOX INTERCOSTALS, BS 2350, LBL 11 - RBL 11. CORROSION REMOVED, INT ERCOSTALS REPAIRED AND REPLACES IAW SRM 53-10-01 AND 51-10-01. 2 L 7 4 4F A20WE 1998092500808 19980925 00808 NM 1998 9 25 P5CA9801487 1 19980921 A 5320 TIE BOEING 747 747122 1384872 NM BS 860 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL ONE CORROSION FOUND BELOW FLOOR SHEAR FITTING TIE, BS 860, BL L47 - R47. CORROSION REMOVED AND AREA REPAIRED IAW SRM 53-10-04 FIG 3A. 2 L 7 4 4F A20WE 1998092500809 19980925 00809 NM 1998 9 25 P5CA9801488 1 19980921 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1955-1963 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL TWO CORROSION FOUND ON STRINGER 51, BS 1955 TO 1963, BL 5 - 7L. REPLACED AND SPLICED STRINGER AS PER SRM 51-10-01 PAGE 18. 2 L 7 4 4F A20WE 1998092500810 19980925 00810 NE 1998 9 25 ARWA980911 2 19980922 A 7261 FITTING DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE LOOSE A ARWA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 19 802BN 45909 671843 TUS - SHUTDOWN NR 4 ENGINE S/N 671443 AT 1345Z DUE TO STEADY OIL PRESS LIGHT AND INDICATED PRESS LESS THAN 35 PSI. WIND MILLING PRESS AT 18 PSI. TIGHTENED LOOS SWIVEL FITTING AT NR 6 BEARING INLET. ENGINE RUN UP. NO LEAKS NOTED. (M) 2 L 7 4 4F 4 F 4A25 1E8 1998092600001 19980926 00001 NM 1998 9 26 DLM90981816 1 19980902 A 2730 POS TRANSMITTER 08BHG36ABJF7 DOUG MD90 MD9030 3023690 NM RT ELEVATOR INOPERATIVE A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 916DN 1068 53396 AT CRUISE, ELEVATOR SPLIT LIGHT ILLUM ON OAP/ DFGC IN NR 1 WAS ON AND LEVEL AT CRUISE, NO PITCH INPUT FOR 5 MINS. FOUND RT ELEVATOR POS TRANSMITTER INOP. REPLACED TRANSMITTER, CK GOOD PER M/M. 2 L 7 2 4F RT A6WE 1998092600002 19980926 00002 NM 1998 9 26 DL73E981831 1 19980828 A 5320 INTERCOSTAL BOEING 737 737247 138448D NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 238WA 23186 THE R1 DOOR FRAME INTERCOSTAL AT STR 8A WAS FOUND CRACKED. THE REPAIR WAS ACCOMPLISHED PER BOEING S/B 737-53A1108 WITH A MINOR DEVIATION ON THE FINISH. 2 L 7 2 4F A16WE 1998092600003 19980926 00003 NM 1998 9 26 DL73S981844 1 19980906 A 4920 MS200730306 BOLT BOEING 737 737232 1384475 NM PWA JT8 JT8D15A 52051 NE APU MISSING A DALA F ACTIVATE FIRE EXT. J WARNING INDICATION AP APPROACH 1 SO 27 328DL 28414 23100 P50152 APU FIRE WARNING WHILE ON APPROACH. FOLLOWED CHECKLIST. FIRED BOTTLE, FIRE WARNING EXTINGUISHED. FOUND BOLT MISSING F ROM FUEL ATOMIZER CAUSING HEAT TO REACH FIRE LOOP. 2 L 7 2 4F 4 F RT A16WE E2EA 1998092600004 19980926 00004 NE 1998 9 26 DL733981852 2 19980907 A 7200 ENGINE BOEING 737 737347 1384647 NM GE CFM56 CFM563B1 13802 NE NR 1 FAILED A DALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 SO 27 308WA 32090 23441 721164 AT 1500 FT NR 1 ENGINE LOUD BANG AND OVERTEMP TO 930 CELSIUS. FOLLOWED BY VIBRATION WITH THROTTLE REDUCED IDLE INDICATI ONS NORM FOR 4-5 MIN THEN VIBRATION IND WENT TO 3. A/C STARTED TO SHAKE. ENG SHUT DOWN. PAX REPORTED FLAMES AT TIME O F COMPRESSOR STALL THEN NONE UNTIL SLIGHTLY BEFORE ENG SHUT DOWN. INFLT SHUTDOWN AND AIR TURNBACK. MTC FOUND OIL IN TA ILPIPE, CAUSE OF FLAMES AND COMPRESSOR AND TURBINE SEIZED. NO VISIBLE DAMAGE TO ENG OR BLADES. 2 L 7 2 4F 4 F RT A16WE E2GL 1998092600005 19980926 00005 WP 1998 9 26 VJ980319 1 19980402 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 944 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 945VV 47238 IN AFT CARGO COMPARTMENT FOUND CORROSION ON SKIN PANEL ADJACENT TO STR 28L I/B SIDE AT STA 944. REMOVED CORROSION AND F OUND TO BE OUT OF LIMITS, MORE THAN 50 PERCENT MAT LOSS IAW SRM 53-01 FIG 1. FABBED DOUBLER, INSTALLED DOUBLER IAW SRM 53-04 FIG 38 (MAT 2024 T-3 .032 5 X 5.5). 2 L 7 2 4F A6WE 1998092600008 19980926 00008 NE 1998 9 26 SWAA981839 2 19980822 A 7321 CONNECTOR BOEING 737 7372H4 138448C NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE EEC LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 705SW 27839 AIRCRAFT WITH NR 2 ENGINE SHUTDOWN, APU ELEC ON LINE, NR 1 THROTTLE AT IDLE, UNCOMMANDED ENG ACCELERATION TO 85 PERCENT N1, APPROX 10 SEC, THEN RETURNED TO IDLE. (LOG PAGE 169881). FOUND J2 CONNECTOR ON EEC LOOSE, CLEANED AND SECURED OPER ATED ENG PER BOEING MM. NO FAULTS FOUND. 2 L 7 2 4F 4 F A16WE E2GL 1998092600009 19980926 00009 NM 1998 9 26 DL72S981863 1 19980908 A 3350 LIGHTS BOEING 727 727225 1384077 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8891Z 21860 EMERGENCY EXIT LIGHTS INOP. TIGHTENED BULB CONNECTORS AND RELAMPED. 2 L 7 3 4F A3WE 1998092600010 19980926 00010 NM 1998 9 26 DL72L981864 1 19980908 A 3234 MODULE BOEING 727 727232 1384082 NM E/E COMPT INOPERATIVE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 501DA 21303 LDG GEAR WOULD NOT RETRACT AFTER TAKEOFF. HANDLE WOULD NOT GO PAST OFF POSITION. RESET LEVER LATCH CB AND CENTERED STE ERING. SAME RESULT. FOUND LANDING GEAR ELECTRICAL MODULE LEVER LATCH FUNCTION INOP. REPLACED MODULE. RAN TEST/ADJ PE R MM 32-09-121 PG 501. . 2 L 7 3 4F A3WE 1998092600011 19980926 00011 NE 1998 9 26 DL757981867 2 19980909 A 7200 ENGINE BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 FAILED A DALA E ENGINE SHUTDOWN K FLUID LOSS AP APPROACH 1 SO 27 621DL 30539 22911 716513 DURING DESCENT, RT ENGINE OIL QTY SHOWED 0. RT ENGINE OIL PRESS LIGHT CAME ON. ENGINE SHUTDOWN PER CHECK LIST. REPLAC ED ENGINE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998092600012 19980926 00012 NM 1998 9 26 DL72L981872 1 19980826 A 5210 FRAME BOEING 727 727232 1384082 NM PAX DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 2 INCH CRACK ON R-1 DOOR AFT FRAME AT LOWER CORNER. REPAIRED PER MM 52-12-0 FIG 804. 2 L 7 3 4F A3WE 1998092600013 19980926 00013 NM 1998 9 26 DL72L981873 1 19980828 A 5320 WEB BOEING 727 727232 1384082 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 A .375 INCH CRACK IN TORQUE BOX VERTICAL WEB STA 1223 LT SIDE, ABOVE STAIRS CLOSE OUT PANEL. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998092600014 19980926 00014 NM 1998 9 26 DL72L981890 1 19980826 A 2782 STIFFENER BOEING 727 727232 1384082 NM NR 5 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 A .625 INCH CRACK IN SPAR STIFFENER AT NR 5 SLAT ACTUATOR INBD ATTACH FITTING. REMOVED OLD STIFFENER. DRILLED UP STIFF ENER PER M/M 57-20-21 PG 813. 2 L 7 3 4F A3WE 1998092600015 19980926 00015 NM 1998 9 26 DL72L981895 1 19980826 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 740 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND DURING MV2 CORROSION VISIT NRC 154, WHILE WORKING NRC 91 FOUND RT SKIN SUPPORT ANGLE CO RRODED UNDER STR 27R STA 740. REPLACED SKIN SUPPORT ANGLE PER M/M 53-11-0 PG 859. 2 L 7 3 4F A3WE 1998092600016 19980926 00016 NM 1998 9 26 DL72L981897 1 19980913 A 5320 WEB BOEING 727 727232 1384082 NM BS 1309 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND ON MV2 CK, 1 INCH AND .5 INCH CRACKS FOUND IN STA 1309 WEB RT SIDE ABOVE S DUCT. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1998092600017 19980926 00017 NM 1998 9 26 DL72L981898 1 19980913 A 5320 WEB BOEING 727 727232 1384082 NM BS 1309 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 507DA 21309 FOUND ON MV2 CK, .5 INCH CRACK IN THE STA 1309 WEB LEFT SIDE ABOVE THE S DUCT. REPAIRED PER SRM 53-10-4. 2 L 7 3 4F A3WE 1998100200001 19981002 00001 WP 1998 10 2 VJ9800417 1 19980922 A 3241 421396 CONTROL BOX DOUG DC9 DC932 3022066 WP E & E COMPT FAILED A ZZDA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 15 912VV 47359 NO BRAKE PRESSURE DURING TAXI WITH ANTISKID SYSTEM ON. REPLACED ANTISKID CONTROL BOX AND OPS CHECKED GOOD IAW MM 32-43. 2 L 7 2 4F A6WE 1998100200002 19981002 00002 WP 1998 10 2 VJ9800418 1 19980923 A 3246 9543401 HUB CAP DOUG DC9 DC932 3022066 WP RH MLG WORN A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 15 935VV 47534 SMOKE ODOR IN CABIN. AIRCRAFT RETURNED TO MCO. FOUND EVIDENCE OF NR 4 TIRE SPINNING IN WHEEL WELL. REPLACED RUBBER HU B CAP. 2 L 7 2 4F A6WE 1998100200003 19981002 00003 WP 1998 10 2 VJ9800419 1 19980924 A 3350 6003 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 946VV 47226 AFT STAIRS EMERGENCY LIGHT INOP. REPLACED BATTERY POWER SUPPLY IAW MM 3350, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998100200004 19981002 00004 WP 1998 10 2 VJ9800420 1 19980924 A 3350 41B004A11073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 946VV 47226 AFT STAIRS EMERGENCY LIGHTING BATTERIES WON'T HOLD A CHARGE. REPLACED NICAD BATTERIES IAW MM 33-50, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998100200005 19981002 00005 NM 1998 10 2 CALA9801854 1 19980917 A 3220 LANDING GEAR BOEING 737 737524 1384721 NM NLG FAILED A CALA O OTHER O OTHER LD LANDING 1 SW 09 20643 28904 THE NOSE LANDING GEAR COLLAPSED ON LANDING AT GDL. ALL GEAR INDICATIONS WERE NORMAL AT TIME OF LANDING. AN EMERGENCY E VACUATION WAS PERFORMED AS A PRECAUTIONARY MEASURE. THERE WERE NO INJURIES. ENGINEERING CONCLUDED THAT THERE WERE NO M ECHANICAL MALFUNCTIONS ASSOCIATED WITH COLLAPSE OF THE NLG. THE CREW HAD EXPERIENCED EXCESSIVE CROSSWINDS DURING LANDIN G AT GDL. 2 L 7 2 4F RT A16WE 1998100200006 19981002 00006 WP 1998 10 2 CALA9801855 1 19980920 A 3610 DUCT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 3 ENGINE RUPTURED A CALA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 09 14063 47864 517504 THE NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED WHILE EN ROUTE. BOTH FIRE BOTTLES WERE DISCHARGED, BUT THE LIGHT REMAINE D ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO SNN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 8T H STAGE PNEUMATIC DUCT RUPTURED. THE DUCT WAS REMOVED AND REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1998100200007 19981002 00007 WP 1998 10 2 CALA9801856 1 19980923 A 3230 3937030501 LINK DOUG DC9 DC982 3022082 WP RT MLG UPLOCK BROKEN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 936AS 49363 THE RT MLG LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING MIA. THE AIRCRAFT WAS DIVE RTED TO MCO WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE RT MLG UP ACTUATOR LOWER LINK BROKEN. THE LINK WAS REMOVED A ND REPLACED IAW MM 32-10-00. A GEAR SWING WAS PERFORMED IAW MM 07-11-00 AND OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998100200008 19981002 00008 WP 1998 10 2 9810089871 1 19980923 A 3260 SOCKET DOUG DC9 DC951 3022051 WP LT MLG BROKEN A NWAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 01 780NC 48102 DURING APPROACH, ALL LANDING GEAR INDICATION LIGHTS DID NOT ILLUMINATE AND THE LANDING GEAR CONTROL CIRCUIT BREAKERS P-2 7 POPPED WHEN LANDING GEAR WAS EXTENDED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARED EMERGENCY, AND LANDED WITHOU T INCIDENT. MAINTENANCE REPAIRED THE ANNUNCIATOR SOCKET FOR THE LEFT HAND LANDING GEAR DOWN AND LOCK INDICATION. OPERA TIONAL CHECK OK. 2 L 7 2 4F RT A6WE 1998100200009 19981002 00009 SO 1998 10 2 COMA9810219 1 19980922 A 3350 12046830005 TRACK EMB 120 EMB120RT SO CABIN DAMAGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 268CA 120262 EMERGENCY FLOOR LIGHT TORN OUT BY WHEEL CHAIR. REPLACED LIGHT ASSY. 2 L 7 2 4T RT A31SO 1998100200010 19981002 00010 EA 1998 10 2 COMA9860271 1 19980914 A 5320 601R800045 BRACKET CNDAIR CL600 CL6002B19 EA CABIN BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 DURING SCHEDULE INSPECTION FOUND BLEED AIR SUPPORT BRACKET CRACKED BELOW FLOOR PANEL 271CLF. REPLACED BRACKET. 2 L 7 2 4F RT A21EA 1998100200011 19981002 00011 EA 1998 10 2 COMA9860270 1 19980919 A 5320 5013501251 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 DURING INSPECTION FOUND A CRACKED ANGLE ON STRINGER 14, AFT SIDE OF 621 BULKHEAD. REPLACED ANGLE. 2 L 7 2 4F RT A21EA 1998100200012 19981002 00012 EA 1998 10 2 COMA9860273 1 19980920 A 5347 601R3103215 SEAT TRACK CNDAIR CL600 CL6002B19 EA CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 DURING SCHEDULED INSPECTION FOUND LEFT FRONT CABIN FLOOR SEAT RAIL CORRODED. REPLACED SEAT RAIL. 2 L 7 2 4F RT A21EA 1998100200013 19981002 00013 EA 1998 10 2 COMA9860272 1 19980919 A 5320 6013501252 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 937CA 7044 DURING SCHEDULED INSPECTION, FOUND A CRACKED ANGLE ON STRINGER 14, AFT SIDE OF 621 BULKHEAD. REPLACED ANGLE. 2 L 7 2 4F RT A21EA 1998100200014 19981002 00014 EA 1998 10 2 COMA9860274 1 19980919 A 5320 FILLER CNDAIR CL600 CL6002B19 EA PAX DOORWAY MISSING A COMA G A O2 MASK DEPLOYED UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SO 01 963CA 7127 LOUD WIND NOISE FROM CABIN DOOR. REPLACED MISSING FILLER MATERIAL AT PREVIOUS REPAIR OF DOOR FRAME SEAL AREA. 2 L 7 2 4F RT A21EA 1998100200015 19981002 00015 EA 1998 10 2 COMA9860275 1 19980922 A 3350 59465 POWER STRIP CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 924CA 7026 EMERGENCY FLOOR LIGHTING ROW 1 THRU 5 IS INOPERABLE. REPLACED FLOOR LIGHTING CONNECTOR STRIP. 2 L 7 2 4F RT A21EA 1998100200016 19981002 00016 NM 1998 10 2 UPS98427706 1 19980922 A 3350 LIGHT BOEING 747 747121 1384871 NM CABIN INOPERATIVE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 681UP 19661 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT MODULE, OPS CHECK OK. 2 L 7 4 4F A20WE 1998100200017 19981002 00017 NM 1998 10 2 UPS98427707 1 19980924 A 3397 WIRE BOEING 747 747123 1384873 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 675UP 20390 INSPECTION TYPE-N/A, ALL 3 EMERGENCY WALNUT LIGHTS UNDER PANEL CENTER LEFT RIGHT INOP. REPAIRED BAD WIRE ON CENTER EMER G/FLOOD LIGHT ASSY, OPS CHECK GOOD PER W/D 33-13-11. 2 L 7 4 4F A20WE 1998100200018 19981002 00018 NM 1998 10 2 QXEA9801360 1 19980917 A 2611 SMOKE LIGHT DHAV DHC8 DHC8202 2809007 NM COCKPIT ILLUMINATED A QXEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 09 357PH 504 AFTER TAKEOFF CLIMBING THROUGH 3,000 FEET, GOT SMOKE WARNING LIGHT. LIGHT CAME ON FOR 2-3 SECONDS AND WENT OUT, CAME BA CK ON IN 15-20 SECOND AND REPEATED ON / OFF CYCLE CONTINUOUSLY DURING RETURN TO FIELD. FLIGHT ATTENDANT REPORTED CAUSTI C ODOR AND BURNING EYES. GROUND RAN AIRCRAFT FOR 1.5 HOURS AT 90 PERCENT TORQUE. CYCLED TEMP BETWEEN HOT AND COLD MANY TIMES WITH NO SMOKE, ODOR OR BURNING EYES NOTICED. TESTED BAGGAGE BAY SMOKE DETECTORS, TESTED GOOD. INSPECTED UNDER B AGGAGE BAY PANELS 144EZ-251HZ AND 251EZ FOR ANY POSSIBLE DEFECTS, NO DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RELEAS ED FOR TEST FLIGHT. TEST FLIGHT SATISFACTORY. 2 H 7 2 4T RT A13NM 1998100200019 19981002 00019 NM 1998 10 2 98FDEA00587 1 19980922 A 3350 1000679 LIGHT BOEING 727 72725 1384006 NM COCKPIT INOPERATIVE A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 154FE 18287 COCKPIT EMERGENCY LIGHT FELL DOWN DURING T/O ROLL. REINSTALLED COCKPIT EMERGENCY EXIT LIGHT, OPER CKS GOOD PER FEDEX M/ M 33-50-00. 2 L 7 3 4F A3WE 1998100200020 19981002 00020 NM 1998 10 2 98FDEA00588 1 19980924 A 3350 1000679 LIGHT BOEING 727 727247 138408F NM COCKPIT INTERMITTENT A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 233FE 21327 NR 0648 - COCKPIT EMERGENCY EXIT LIGHT INTERMITTENT. REMOVED AND REPLACED COCKPIT EMERGENCY EXIT LIGHT PER FEDEX M/M 33 -50-101. EMERGENCY LIGHT TESTED GOOD PER FEDEX MM 33-50-101. 2 L 7 3 4F A3WE 1998100200021 19981002 00021 WP 1998 10 2 98FDEA00589 1 19980924 A 5412 BLKHD FITTING DOUG DC10 DC1010F 3022111 WP NR 3 PYLON CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 057FE 48264 NR 3 PYLON AFT MOUNT BULKHEAD HAS HIGH FREQ EDDY CURRENT IND IN UPPER FLANGE 4TH HOLE FROM LEFT SIDE. *S/D* REPLACED A FT MOUNT BULKHEAD FITTING (P/N AUB 7025-13). LOCATED AND DRILLED NEW FITTING PER DAC DRAWING NR AUB 7025. COMPLIED WIT H EA 8-5410-40219 ON 4TH HOLE FROM LT SIDE OF BULKHEAD. 9-26-98 2 L 7 3 4F A22WE 1998100200022 19981002 00022 WP 1998 10 2 98FDEA00590 1 19980924 A 5412 FIREWALL DOUG DC10 DC1010F 3022111 WP NR 3 PYLON CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 057FE 48264 NR 3 PYLON LWR SPAR FIREWALL AFT I/B END DEEP PITTING CORROSION BS YN 417. 2 L 7 3 4F A22WE 1998100200023 19981002 00023 WP 1998 10 2 MWEA98969 1 19980920 A 3350 276005 SOCKET DOUG DC9 DC914 3022034 WP CABIN SHORTED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 500ME 45711 EMERGENCY FLOOR TRACK LIGHTING INOP ROWS 4-8. FUSE BLOWN ON FWD AND AFT BATTERY PACKS. REPLACED FUSES AND REPAIRED SHO RTED SOCKETS, OPS CHECK GOOD. 2 L 7 2 4F A6WE 1998100200024 19981002 00024 GL 1998 10 2 DHL98803002 2 19980924 A 7320 FUEL CONTROL DOUG DC8 DC873F 302199F WP GE CFM56 CFM562C5 GL NR 4 ENGINE OUT OF ADJUST A DHLA O OTHER X ENGINE FLAMEOUT CR CRUISE 1 SO 01 803DH 46123 CLIMBED FROM FL 290 TO FL 370, AFTER LEVELING OFF NR 4 ENGINE FLAMED OUT. DESCENDED TO 290 AND PERFORMED INFLIGHT RESTA RT. PERFORMED INSPECTION PER CFM MM 71-00-00 FAULT NR 51. FOUND SPECIFIC GRAVITY OFF INDEX MARK. RESET TO PROPER IND EX .87 PER MM 73-21-10. A/C RELEASED FOR FLIGHT. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998100200025 19981002 00025 1998 10 2 SWIA971251 4 19980909 A 2210 6226684006 CONTROL PANEL EMB 120 EMB120RT SO PWA 118 PW118 NE COCKPIT FAILED A A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 156CA 120156 DURING INITIAL CLIMB AT 1000 FT, ELECTRIC TRIM RAN AWAY FORWARD TO STOP. ROLLED TRIM BACK AND IT RAN FORWARD TO STOP AG AIN, EACH TIME SOUNDING AUTO PILOT AURAL WARNING. THE AUTO PILOT WAS NOT ON AT THE TIME. TRIED TO TURN RIGHT, WAS UNAB LE BECAUSE AUTO PILOT SERVOS WERE IN CONTROL. PRESSED AUTO PILOT ENGAGE ON AND OFF SEVERAL TIMES BUT AUTO PILOT WOULD N OT DISENGAGE. DIALING THE HEADING TO THE RIGHT, AIRCRAFT WOULD ROLL LEFT. EVENTUALLY, THE AUTO PILOT DISENGAGED. RETU RNED TO LAX. REMOVED AND REPLACED AUTO PILOT CONTROL PANEL, OPS CHECKS GOOD ON GROUND. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200026 19981002 00026 SO 1998 10 2 SWIA971252 1 19980909 A 2731 TRIM TAB EMB 120 EMB120RT SO PWA 118 PW118 NE ELEVATOR OUT OF POSITION A SWIA K NONE F FLT CONT AFFECTED DE DESCENT 1 NM 07 156CA 120156 DURING DESCENT, AUTO PILOT DISCONNECTED. FOUND TRIM WHEEL AT FORWARD LIMIT AND TRIM INDICATOR AT 1-8 UNITS DOWN. AIRCR AFT SPEED REDUCTION REQUIRED TO REDUCE STICK FORCES TO NORMAL. ACCOMPLISHED ELEVATOR TRIM TAB DEFLECTION CHECK PER MM 2 7-32-00, TRAVEL WITHIN LIMITS AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200027 19981002 00027 SO 1998 10 2 SWIA971253 1 19980909 A 3610 VENTURI TUBE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ACM FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 299SW 120329 LEFT DUCT LEAK LIGHT ILLUMINATED IN FLIGHT. RETURNED TO FAT. INSTALLED SERVICEABLE VENTURI TUBE ON LEFT ACM. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200028 19981002 00028 EA 1998 10 2 SWIA971254 2 19980909 A 7261 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 NM 07 407SW 7034 DURING CRUISE FLIGHT, LT ENGINE OIL PRESS MSG ILLUMINATED ON EICAS. ALSO, LT ENGINE OIL PRESS WAS FLUCTUATING BETWEEN 2 0 AND 40 PERCENT. PERFORMED ALL ITEMS ON ALL PERTINENT CHECK LIST AND SHUT DOWN ENGINE. PERFORMED SINGLE ENGINE LANDIN G. FOUND LT ENGINE HYDRAULIC PUMP CARBON SEAL LEAKING. REMOVED AND REPLACED CARBON SEAL, CLEANED ENGINE, GROUND RUN AT HIGH POWER SETTINGS FOR 30 MIN. NO LEAKS FOUND. MDC SHOWED NO ENGINE, NO OIL PRESS EXCEEDING. NOTED: C/W LOW OR NO OIL PRESSURE, INSPECTION IAW MM 72-00-00, LEAKS CKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100200029 19981002 00029 SO 1998 10 2 SWIA971255 1 19980909 A 3234 12038594501 HANDLE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 224SW 120294 LEFT B-SYSTEM GREEN LIGHT ILLUMINATED IN FLIGHT. RETURNED TO FIELD. REPLACED LANDING GEAR SELECTOR HANDLE. LANDING GE AR INDICATION OPERATES NORMALLY IAW MM 32-60-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200030 19981002 00030 EA 1998 10 2 SWIA971256 1 19980910 A 5270 LIGHT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE CARGO DOOR ILLUMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 403SW 7028 AFTER TAKEOFF, CARGO DOOR LIGHT ILLUMINATED. RETURNED TO GATE. OPERATIONAL CHECK OF CARGO DOOR CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100200031 19981002 00031 SO 1998 10 2 SWIA971257 1 19980910 A 3030 CURRENT SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AOA HEATER FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 AFTER TAKEOFF, RIGHT AOA HEATER CIRCUIT BREAKER POPS. RETURNED TO SLC. REMOVED AND REPLACED RIGHT CURRENT SENSOR ASSEM BLY. TESTED AOA IAW MM 30-32. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200032 19981002 00032 NM 1998 10 2 VNAA9809019 1 19980919 A 3030 0851GW HEAT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PITOT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 430JS 76264 3044 DURING THE TAXI OUT FOR TAKEOFF, THE CREW NOTED A PITOT FAIL WARNING MESSAGE. THE AIRCRAFT RETURNED TO THE GATE. OUTST ATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO DCA TO ACCOMPLISH REPAIR. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY PROBLEMS. IN DCA THE NR 1 PITOT TUBE WAS REPLACED, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-11-04. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100200065 19981002 00065 CE 1998 10 2 98ZZZX3571 1 19980724 A 3230 08421043 BELLCRANK CESSNA 310 310R 2074245 CE NLG WW FAILED A S A AZOA O OTHER O OTHER LD LANDING 1 GL 13 6209X 3720 310R1339 THE BELLCRANK FAILED ALONG FORK BOLT MOUNTING HOLE. THIS IS THE ADJUSTING POINT FOR DOWNLOCK OVERCENTER TENSION. UPON INSTALLATION OF NEW PART, OVERCENTER TENSION WAS CHECKED AND FOUND TO BE NORMAL. DUE TO THE FAILURE, THE NOSE GEAR COLL APSED UPON LANDING. NO FURTHER DEFECTS NOTED. 1 L 7 2 3O 3A10 1998100200077 19981002 00077 EA 1998 10 2 98ZZZX3582 1 19980716 A 2823 C2CE481 HANDLE DHAV DHC2 DHC2MK1 2800102 EA COCKPIT FAILED A SXFA K NONE O OTHER IN INSP/MAINT 1 NM 01 49771 1079 WHEN SELECTING DIFFERENT FUEL TANK, PANEL MOUNTED FUEL SELECTOR VALVE HANDLE-PIN WHICH HOLDS HANDLE TO SHAFT CAME OUT OF POSITION. THIS WOULD NOT ALLOW TANK SELECTION TO BE MADE. SUBMITTER SUGGESTED TO PREVENT RECURRENCE DURING PRE-FLIGHT AND ROUTINE INSPECTION, MOVE HANDLE, AND CHECK PIN FOR LOOSNESS AND PROPER OPERATION. 1 H 7 1 3R A806 1998100200090 19981002 00090 NM 1998 10 2 UPS98227716 1 19980923 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 LEFT AFT EMER EXIT LIGHT OVERWING AT SEAT POS 12 FAILED TEST. REMOVED AND REPLACED BATTERY PACK FOR LEFT AFT OVERWING E XIT, OPS CK NORMAL PER UPS DWG 727-33A-006. 2 L 7 3 4F A3WE 1998100200091 19981002 00091 NM 1998 10 2 UPS98227717 1 19980923 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 AISLE SEAT EMER LIGHTS POS 9-11-15 FAILED TEST. REMOVED AND REPLACED BATTERY PACKS FOR AISLE SEATS EMER LIGHTS, SEAT 9- 11-15, OPS CK NORMAL PER UPS DWG 727-33A-006. 2 L 7 3 4F A3WE 1998100200092 19981002 00092 NM 1998 10 2 UPS98227718 1 19980923 A 3350 BULB BOEING 727 72725C 138400H NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 949UP 19717 AIRSTAIRS EMER LIGHT INOP. RELALMPED AIRSTAIR EMER LIGHT, OPS CKS NORMAL. 2 L 7 3 4F A3WE 1998100200093 19981002 00093 EU 1998 10 2 QXEA9801361 1 19980924 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 484US 11234 GEG - EXIT LIGHT AT ROW 8 INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998100200094 19981002 00094 EU 1998 10 2 QXEA9801362 1 19980923 A 3350 5515800106 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 PDX - EXIT SIGN OVER COCKPIT DOOR HAS SOME BULBS OUT. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LAMP ASSEMBLY, OP ERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998100200095 19981002 00095 NM 1998 10 2 98FDEA00591 1 19980922 A 3244 657276185 TIRE BOEING 727 727223 1384074 NM LT MLG FAILED A FDEA K NONE D INFLIGHT SEPARATION TO TAKEOFF 1 SO 25 245FE 22016 98-234 - NR 1 TIRE MISS OFF A/C UPON LAND AT MEM. REMOVED AND REPLACED LEFT MLG LWR PISTON CYLINDER ASSY AND REPACK STR UT PER M/M 32-11-11. DUE TO NR 1 AXLE DAMAGE. REPLACE NR 1 TIRE AND BRAKE ASSY. REPLACE NR 2 TIRE ASSY AS PRECAUTION PER MM 32-42 AND 32-43. REMOVED AND REPLACED NR 1 ANTI-SKID XDUCER PER MM 32-44 AS PRECAUTION. ALL SYS OPS CKD NORM. 2 L 7 3 4F A3WE 1998100200096 19981002 00096 NE 1998 10 2 98FDEA00592 2 19980924 A 7230 COMPRESSOR BOEING 727 72722 1384002 NM PWA JT8 JT8D7 52053 NE NR 3 ENGINE BIRD STRIKE A FDEA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 25 105FE 19194 98-235 - ON T/O, SUSPECT BIRD STRIKE AT NOSE WHEEL WELL AREA, FOLLOW BY SEVERE VIBRATION IN NR 3 ENG. ENG SHUTDOWN IAW FOM AND EMERG LAND MADE (MEM RETURN). REMOVED AND REPLACED NR 3 ENG COMPRESSOR BLADES DAMAGED IAW WORK CARD 70T0503 AND 70T0301. OPS CHECK GOOD. WRI 05-50-2570. 2 L 7 3 4F 4 F A3WE E2EA 1998100200097 19981002 00097 NM 1998 10 2 98FDEA00593 1 19980924 A 2752 MS9391130ZE DRIVE MOTOR BOEING 727 727223 1384074 NM TE FLAPS FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 220FE 20934 98-236 - AFTER T/O DUR NORM FLAP RETRACTION. OTBD TRAIL EDGE FLAPS STUCK AT 15 DEG. ACCOMPLISH ABNORMAL CKLIST FLAPS O TBD STILL DID NOT MOVE. RETURN FOR LAND. REMOVED AND REPLACED OTBD FLAP BYPASS VALVE PER MM 27-51-151. TROULBE SHOT A S PER MM. REMOVED AND REPLACED HYD FLAP DRIVE MOTOR PER MM 27-51-62. 2 L 7 3 4F A3WE 1998100200098 19981002 00098 WP 1998 10 2 ABXA9800840 1 19980924 A 3260 SWITCH DOUG DC8 DC863 302198A WP LT MLG DOOR LACK OF LUBE A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 DURING GEAR UPLATCH CHECK, GEAR UNSAFE LIGHT ILLUMINATED. RECYCLED GEAR SEVERAL TIMES. DETERMINED THAT LEFT MAIN GEAR DOOR WAS NOT LATCHED. INSPECTED, CLEANED AND LUBRICATED GEAR SWITCHES. OPS CHECKED NORMAL IAW DC8 MM. 2 L 7 4 4F 4A25 1998100200099 19981002 00099 NM 1998 10 2 SCNA98107 1 19980923 A 3350 1102832 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 118 20765 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT AT THE BOTTOM OF THE STAIRS WAS FOUND TO BE I NOPERATIVE. REMOVED AND REPLACED THE LIGHT ASSEMBLY SYSTEM AND OPERATIONALLY CHECKS NORMAL IAW MM CHAPTER 335000. 2 L 7 3 4F RT A3WE 1998100200100 19981002 00100 WP 1998 10 2 DHL9880301C 1 19980809 A 5313 STRINGER DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, STRINGER 35 JUST FWD OF AIR COND COMPT DOOR CUT OUT HAS LT SIDE CORROSION. REMOVED CORRODED INTERCOSTAL BET WEEN 8 AND 35 AND INSTALLED NEW PER SRM 51-1-21. N/R 893. 2 L 7 4 4F RT 4A25 1998100200101 19981002 00101 WP 1998 10 2 DHL9880302C 1 19980813 A 5751 SKIN DOUG DC8 DC873F 302199F WP LT AILERON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, PANEL ON LT FAIRING 564B UPPER AILERON SURFACE OUTER SKIN FWD EDGE CRACKED. STOP DRILLED CRACK, FABRICATED EXTERNAL DOUBLER 1.0 BY 3.5 PER SRM 55-2-0. N/R 1013. 2 L 7 4 4F RT 4A25 1998100200102 19981002 00102 WP 1998 10 2 DHL9880303C 1 19980808 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, MAIN CARGO COMPT AFT LOWER FLOOR AREA AT STA 1700-1730 FLOOR PANELS DETERIORATED AND CORRODED UPPER AND LOWE R SURFACES. FABRICATED REPAIR FOR ANGLE SUPPORT PER SRM 51-1-4, 2 BY 3FT, N/R 808. 2 L 7 4 4F RT 4A25 1998100200103 19981002 00103 WP 1998 10 2 DHL9880304C 1 19980805 A 7110 DEFLECTOR DOUG DC8 DC873F 302199F WP NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, NR 3 ENGINE NOSE COWLING ANTI-ICE DEFLECTOR HAS 6-8 CRACK ACROSS PANEL AT 11 O'CLOCK POSITION. REPAIRED PER SRM 51-1-8. N/R 505. 2 L 7 4 4F RT 4A25 1998100200104 19981002 00104 WP 1998 10 2 DHL9880305C 1 19980805 A 7110 DEFLECTOR DOUG DC8 DC873F 302199F WP NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, NR 2 ENGINE, NOSE COWL ANTI-ICE DEFLECTOR FROM 3 TO 9 O'CLOCK CRACKED. TRIMMED AREA PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998100200105 19981002 00105 WP 1998 10 2 DHL9880306C 1 19980806 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 920 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT WING TO FUSELAGE STA 920 FOUND CRACK ON SUPPORT. REMOVED SUPPORT AND INSTALLED NEW PER SRM 51-1-21. N/R 579. 2 L 7 4 4F RT 4A25 1998100200106 19981002 00106 WP 1998 10 2 DHL9880307C 1 19980806 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 5000 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT WING T/E I/B AREA AT STA 5.000 DEEP GOUGE ON SIDE PLATE I/B FLAP I/B HINGE AREA. REMOVED DAMAGED ANGLE P ER SRM 51-1-21. INSTALLED NEW ANGLE PER SRM 51-1-21. N/R 586. 2 L 7 4 4F RT 4A25 1998100200107 19981002 00107 WP 1998 10 2 DHL9880308C 1 19980806 A 5330 SKIN DOUG DC8 DC873F 302199F WP RT MLG DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT WHELL WELL AREA AFT DOOR CUT OUT ON FUSELAGE SKIN AND INTERNAL ANGLE CRACKED. REMOVED CRACKED WEB AND A NGLE PER SRM 51-1-21, N/R 574. 2 L 7 4 4F RT 4A25 1998100200108 19981002 00108 WP 1998 10 2 DHL9880309C 1 19980806 A 5330 SKIN DOUG DC8 DC873F 302199F WP RT MLG DOORWAY LOOSE A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C-CHECK, RIGHT WHEEL WELL AREA FWD DOOR CUTOUT AREA METAL SKIN LIFTING OFF. REMOVED DAMAGED SKIN AND REPLACED PER SR M 51-1-21. N/R 575. 2 L 7 4 4F RT 4A25 1998100200109 19981002 00109 WP 1998 10 2 DHL9880310C 1 19980813 A 5312 BULKHEAD WEB DOUG DC8 DC873F 302199F WP BS 1766 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, MAIN CARGO AFT PRESSURE BULKHEAD WEB CRACKED IN 2 PLACES BETWEEN L 10L AND L11L, ONE CRACK 3 INCHES LONG FRO M LBL 25 TO LBL 28 AND FROM LBL 34 TO LBL 36. CUT OUT DAMAGED AREA AND FABRICATED NEW REAPIR PER DACO DRWING SR 0853000 7, 16 BY 29. REPAIRED PER S/B 53-73, N/R 643. 2 L 7 4 4F RT 4A25 1998100200110 19981002 00110 WP 1998 10 2 DHL9880311C 1 19980806 A 7110 DEFLECTOR DOUG DC8 DC873F 302199F WP NR 4 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, NR 4 ENGINE DEFLECTOR CRACKED AT 5 O'CLOCK POSITION. TRIMMED CRACK SECTION PER SRM 51-1-8. N/R 658. 2 L 7 4 4F RT 4A25 1998100200111 19981002 00111 WP 1998 10 2 DHL9880312C 1 19980806 A 7110 DEFLECTOR DOUG DC8 DC873F 302199F WP NR 4 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, NR 4 ENGINE DEFLECTOR CRACKED AT 1 O'CLOCK POSITION. TRIMMED DEFLECTOR PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998100200112 19981002 00112 WP 1998 10 2 DHL9880313C 1 19980806 A 5320 FRAME DOUG DC8 DC873F 302199F WP EMER EXIT DRWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C-CHECK, RT AFT LOWER EXIT DOOR CUTOUT FRAME CRACKED. REPAIRED PER SRM 51-1-19. N/R 668. 2 L 7 4 4F RT 4A25 1998100200113 19981002 00113 WP 1998 10 2 DHL9880314C 1 19980806 A 5320 FRAME DOUG DC8 DC873F 302199F WP EMER EXIE DRWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT FWD EMERG EXIT FRAME INTERNAL JAMB CRACKED. REPAIRED PER SRM 51-1-19, N/R 669. 2 L 7 4 4F RT 4A25 1998100200114 19981002 00114 WP 1998 10 2 DHL9880315C 1 19980806 A 5320 FRAME DOUG DC8 DC873F 302199F WP EMER EXIT DRWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, LT LOWER EMERG EXIT DOOR CUTOUT CRACKED. REPAIRED PER SRM 51-1-19, N/R 670. 2 L 7 4 4F RT 4A25 1998100200115 19981002 00115 WP 1998 10 2 DHL9880316C 1 19980816 A 5320 FRAME DOUG DC8 DC873F 302199F WP EMER EXIT DRWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, LT FWD LOWER EMERG EXIT DOOR CUTOUT FRAME CRACKED. REPAIRED FRAME PER SRM 51-1-19, N/R 671. 2 L 7 4 4F RT 4A25 1998100200116 19981002 00116 WP 1998 10 2 DHL9880317D 1 19980809 A 5720 DUMP WELL DOUG DC8 DC873F 302199F WP LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, FUEL DUMP WELL AREA CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR PER SRM 51-1-21, .5 BY 5.5, N/R 755. 2 L 7 4 4F RT 4A25 1998100200117 19981002 00117 WP 1998 10 2 DHL9880318C 1 19980807 A 7830 TRACK DOUG DC8 DC873F 302199F WP NR 3 ENGINE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, THRUST REVERSER NR 3 ENGINE ON O/B TRANSLATING COWL FWD TRACK HAS BROKEN, ON LOWER PORTION. INSTALLED DOUBL ER REPAIR AND FILLER PER SRM 51-1-8, 2 BY .5 BY .5, N/R 747. 2 L 7 4 4F RT 4A25 1998100200118 19981002 00118 WP 1998 10 2 DHL9880319C 1 19980808 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, LT WING UPPER SURFACE AT REAR SPAR STA APPROX 337 MISSING SHEETMETAL. FABRICATED NEW SECTION OF STRIP AND INSTALLED PER SRM 51-1-8, 20 BY .25, N/R 754. 2 L 7 4 4F RT 4A25 1998100200119 19981002 00119 WP 1998 10 2 DHL9880320C 1 19980808 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 25 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, PANEL ON RACK NR 2 FLOOR PLATE, STA 25/45, DOUBLER CRACKED. REMOVED AND REPLACED DOUBLER PER SRM 51-1-4, 7 BY 3. N/R 821. 2 L 7 4 4F RT 4A25 1998100200120 19981002 00120 WP 1998 10 2 DHL9880321C 1 19980808 A 5350 FAIRING DOUG DC8 DC873F 302199F WP RT WING/BODY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT WING TO BODY FAIRING NR 262G CRACKED AT INTERNAL FWD CORNER. FABRICATED REAPAIR DOUBLER, 3 BY 2 PER SRM 53-2-0, N/R 874. 2 L 7 4 4F RT 4A25 1998100200121 19981002 00121 WP 1998 10 2 DHL9880322C 1 19980907 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, L/W INBOARD FLAP EXTERIOR SKIN DAMAGED BELOW NR 1 ICE SHIELD. REMOVED DAMAGED SKIN. INSTALLED NEW SKIN PER SRM 57-7-1, 12.5 BY 26.5, N/R 360. 2 L 7 4 4F RT 4A25 1998100200122 19981002 00122 WP 1998 10 2 DHL9880323C 1 19980820 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 520 PUNCTURED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, AFT LOWER CARGO COMPT FLOOR BETWEEN STA 520- 560 HAS PUNCTURES AND SCRATCHES. REMOVED AND INSTALLED NEW PA NEL PER SRM 25-51-1, N/R 365. 2 L 7 4 4F RT 4A25 1998100200123 19981002 00123 WP 1998 10 2 DHL9880324C 1 19980823 A 7110 DEFLECTOR DOUG DC8 DC873F 302199F WP NR 3 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, NR 3 ENGINE DEFLECTOR CRACKED AT THE 11 O' CLOCK POS. TRIMMED CRACKED SECTION PER SRM 51-1-8, N/R 1076. 2 L 7 4 4F RT 4A25 1998100200124 19981002 00124 WP 1998 10 2 DHL9880325C 1 19980828 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 291.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, LT WING LEADING EDGE LOWER AREA STA XFS 291.5, FOUND SMALL CRACK. REMOVED PREVIOUS REPAIR FROM LEFT WING L /E STA 257 TO 288. CUT OUT CRACKED AREA, FABRICATED REPAIR DOUBLER PER EO NR 18R57610022 AND INSTALLED PER SAME, N/R 10 99. 2 L 7 4 4F RT 4A25 1998100200125 19981002 00125 WP 1998 10 2 DHL9880326C 1 19980817 A 5720 ANGLE DOUG DC8 DC873F 302199F WP BS 178 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT WING T/E FLAP WELL LOWER AREA AT STA 178. FOUND CRACK ON ANGLE SUPPORT INBOARD AREA NEXT TO FAIRING CUTO UT. REMOVED AND FABRICATED NEW ANGLE PER SRM 51-1-21. N/R 1022. 2 L 7 4 4F RT 4A25 1998100200126 19981002 00126 WP 1998 10 2 DHL9880327C 1 19980817 A 5720 COVER DOUG DC8 DC873F 302199F WP WS 204.125 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT T/E FLAP O/B FLAP I/B HINGE SUPPORT BRACKET STA 204.125, UPPER AREA RUB COVER IS CRACKED. REMOVED AND FA BRICATED AND REPLACED COVER PER SRM 51-3-0. N/R 1023. 2 L 7 4 4F RT 4A25 1998100200127 19981002 00127 WP 1998 10 2 DHL9880328C 1 19980817 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, NR 1 PIT DOOR COVER LOWER FILET CORNER INTERCOSTAL CRACKED. REMOVED, FABRICATED AND INSTALLED NEW INTERCOST AL PER SRM 51-1-21. N/R 1025. 2 L 7 4 4F RT 4A25 1998100200128 19981002 00128 WP 1998 10 2 DHL9880329C 1 19980808 A 5320 THRESHOLD DOUG DC8 DC873F 302199F WP SERVICE DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, PANEL ON RACK NR 1 A, B LT AFT SERVICE DOOR THRESHOLD PLATE HAS CRACK AT SIDE OF PREVIOUS WELD REPAIR AND SP OT OF BULGE. REMOVED AND REPAIRED THRESHOLD PLATE PER SRM 51-1-8, N/R 824. 2 L 7 4 4F RT 4A25 1998100200129 19981002 00129 WP 1998 10 2 DHL9880330C 1 19980808 A 5320 THRESHOLD DOUG DC8 DC873F 302199F WP BS 1080 BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, PANEL ON RACK NR 1 RT MID SERVICE DOOR STA 1080 THRESHOLD PLATE INBD EDGE IS BENT AND RT END HAS CRACK. WEL DED PLATE PER DOUGLAS PROCESS STANDARDS 10.225. N/R 825. 2 L 7 4 4F RT 4A25 1998100200130 19981002 00130 WP 1998 10 2 DHL9880331C 1 19980808 A 5330 THRESHOLD DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, RT FWD SERVICE DOOR THRESHOLD PLATE HAS TWO CRACKS. CLEANED AND WELDED PER DPS 10.225. N/R 826. 2 L 7 4 4F RT 4A25 1998100200131 19981002 00131 WP 1998 10 2 DHL9880332C 1 19980808 A 5320 THRESHOLD DOUG DC8 DC873F 302199F WP SERVICE DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, PANEL RACK NR 1 A,B LT MID SERVICE DOOR THRESHOLD PLATE HAS CRACK EDGE. WELDED PER DPS 10.225. N/R 827. 2 L 7 4 4F RT 4A25 1998100200132 19981002 00132 WP 1998 10 2 DHL9880333C 1 19980808 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 50 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 803DH 46123 AT C CHECK, PANEL ON RACK NR 1 A, B FLOOR PANEL NR 5 RT STA 50-62 DIRTY AND CRACKED. FABRICATED DOUBLER REPAIR PER SRM 51-4-1. INSTALLED PER SRM 51-1-21. N/R 826. 2 L 7 4 4F RT 4A25 1998100200133 19981002 00133 SO 1998 10 2 SWIA971258 1 19980909 A 2731 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE LT ELEVATOR TRIM FAILED A SWIA H DEACTIVATE SYST/CIRCUITS F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 NM 07 156CA 120156 IN DESCENT FLIGHT MAP TRIM FAIL AP DISCONNECT. AIRCRAFT PITCHED UP. DIFFICULT TO CONTROL PITCH. TO DESCEND, IT TOOK A LL NOSE DOWN TRIM AND FORWARD YOKE PRESSURE, (AP TRIM SEVO NOT ILLUMINATED WHEN LOOK AT IT). INSPECTED AND FOUND LEFT E LEVATOR TRIM ACTUATOR JAMMING AND NOT ALLOWING FULL NOSE DOWN TRIM. REMOVED AND REPLACED LEFT ELEVATOR TRIM ACTUATOR PE R MM 27-32-02 AND ADJUSTED RIGHT ELEVATOR TRIM TAB. AIRCRAFT TRIM OPERATIONAL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200134 19981002 00134 SO 1998 10 2 SWIA971259 1 19980903 A 6121 SYNCHRONIZER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PROP MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 226SW 120296 PROP SYNC CAUSES 3 PERCENT NP FLUCTUATION ON RIGHT PROPELLER. RETURNED TO LAX, MEL 61-24-1. REPLACED PROP SYNCHROPHASE R IAW MM 61-24-01, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200135 19981002 00135 NE 1998 10 2 SWIA971260 2 19980905 A 7321 EEC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 196SW 120151 RIGHT EEC FAILED AT 400 FT AGL AFTER TAKEOFF. RETURNED TO AIRPORT (EKO) MEL 73-21-1. REPLACED RIGHT EEC. PERFORMED RU N CHECKS AS REQUIRED PER MM 71-00-00. ALL RUNS CHECK GOOD LEFT AND RIGHT ENGINE . 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200137 19981002 00137 NE 1998 10 2 SWIA971262 2 19980906 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT FAILED A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 APPROXIMATELY 5 MINUTES AFTER TAKEOFF, LEFT T6 INCREASED TO CONTINUOUS LIMIT. REDUCED POWER TO CLIMB POWER SETTING, T6 STILL INCREASING. REDUCED POWER TO 60 PERCENT TQ. AT THAT POINT SEVERAL LOUD ENGINE NOISES HEARD AND AIRCRAFT YAWED. P ERFORMED PRECAUTIONARY ENGINE SHUT DOWN AND RETURNED TO WYS. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00. OPS CHE CKS GOOD. NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200138 19981002 00138 SO 1998 10 2 SWIA971263 1 19980907 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 292SW 120319 AT 11,400 CABIN ALTITUDE MAP ILLUMINATED. RETURNED TO FAT. CLEANED AND INSPECTED PUMP, SWITCH, MANUAL CONTROLLER AND T HE INDICATOR. CLEANED DOOR SEALS AND PNEUMATIC VALVE. NO DEFECTS NOTED. REPLACED AUTO ELECTRIC CONTROLLER. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200139 19981002 00139 SO 1998 10 2 SWIA971264 1 19980908 A 2751 ANNUNCIATOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 289UE 120191 FLAPS WILL NOT RESPOND. NO INDICATIONS. RETURNED TO PDX. REPLACED ANNUNCIATOR. OPS CHECK OK. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200140 19981002 00140 SO 1998 10 2 SWIA971265 1 19980909 A 3610 DUCT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 ENGINE LOOSE A SWIA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 568SW 120343 AT 8.500 FT, NR 2 ENGINE DUCT LEAK LIGHT ILLUMINATED. PER QRH PROCEDURE WITH PRECAUTIONARY ENGINE SHUT DOWN. REINSTALL ED DUCT AT DE-ICE PRESSURE REGULATOR. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200141 19981002 00141 NM 1998 10 2 P5CA9801489 1 19980921 A 5320 CLIP BOEING 747 747122 1384872 NM BS 260 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 NOSE LANDING GEAR PRESSURE DECK TO FLOORBEAM, TWO EACH CLIPS FOUND CRACKED, BS 260, LBL 12 AND 24. REMOVED AND REPLACED CLIPS PER SRM 51-10-01 PAGE 18. 2 L 7 4 4F A20WE 1998100200142 19981002 00142 NM 1998 10 2 P5CA9801490 1 19980921 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1760 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME FOUND CRACKED AND DEFORMED AT INBOARD CHORD, BS 1760 STRINGER 10-11R. REPAIRED PER SRM 53-10-04 FIGURE 1. 2 L 7 4 4F A20WE 1998100200143 19981002 00143 NM 1998 10 2 P5CA9801491 1 19980921 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1840 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME FOUND CRACKED AT BS 1840, STR 12R. REPAIRED PER SRM 53-10-04 FIGURE 1. 2 L 7 4 4F A20WE 1998100200144 19981002 00144 NM 1998 10 2 P5CA9801492 1 19980921 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1860 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME FOUND DEEPLY CHAFED AND CRACKED, BS 1860 STR 12R. FRAME REPAIRED PER SRM 53-10-04 FIGURE 1. 2 L 7 4 4F A20WE 1998100200145 19981002 00145 NM 1998 10 2 P5CA9801493 1 19980921 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 255 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 STRINGER FOUND CRACKED ON SPLICE, BS 255 STRINGER 39L. SPLICE REMOVED AND REPLACED AS PER SRM 51-10-01 PAGE 18. 2 L 7 4 4F A20WE 1998100200146 19981002 00146 NM 1998 10 2 P5CA9801494 1 19980921 A 5314 KEEL BEAM BOEING 747 747122 1384872 NM BS 990-1000 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL ONE CORROSION FOUND ON RIGHT KEEL BEAM CHORD, BS 990-1000 BL 9R. REPAIRED PER HAECO REPAIR SCHEME AND BOEING TELE X PAO-HKG-98-0198RE. 2 L 7 4 4F A20WE 1998100200147 19981002 00147 NM 1998 10 2 P5CA9801495 1 19980921 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2178 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 STRINGER FOUND CRACKED, MAIN DECK FUSELAGE, BS 2178 STR 2R. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872 AND SRWS 91463 8. 2 L 7 4 4F A20WE 1998100200148 19981002 00148 NM 1998 10 2 P5CA9801496 1 19980921 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 2178 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 STRINGER FOUND CRACKED, MAIN DECK FUSELAGE BS 2178, STR 3R. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872 AND SRWS 91463 7. 2 L 7 4 4F A20WE 1998100200149 19981002 00149 NM 1998 10 2 P5CA9801497 1 19980921 A 5311 FRAME BOEING 747 747122 1384872 NM FUSELAGE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME SUPPORT WEB FOUND CRACKED, MAIN DECK FUSELAGE STRINGER 17-19L. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872. 2 L 7 4 4F A20WE 1998100200150 19981002 00150 NM 1998 10 2 P5CA9801498 1 19980921 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1670 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME SUPPORT WEB FOUND CRACKED, MAIN DECK FUSELAGE BS 1670, STR 17-19R. REPAIRED PER HAECO REPAIR SCHEME 53-61-33872. 2 L 7 4 4F A20WE 1998100200151 19981002 00151 NM 1998 10 2 P5CA9801499 1 19980921 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1680 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 FRAME SUPPORT WEB FOUND CRACKED, MAIN DECK FUSELAGE BS 1680, STR 23-24R. REPAIRED PER SRM 53-10-04 FIGURE 84 AND HAECO REPAIR SRWS 914630. 2 L 7 4 4F A20WE 1998100200152 19981002 00152 NM 1998 10 2 P5CA9801500 1 19980921 A 5320 STRAP BOEING 747 747122 1384872 NM NR 2 DOORWAY CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 DOOR FRAME INNER CHORD STRAP FOUND CRACKED, NR 2 MAIN DECK DOOR, STRINGER 18L. REPAIRED PER HAECO REPAIR SCHEME 53-21-3 38 AND SRWS 914646. 2 L 7 4 4F A20WE 1998100200153 19981002 00153 WP 1998 10 2 RRXA98426 1 19980122 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 35 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LAV SUPPORT ANGLE BEYOND LIMITS IAW DC-8 SRM, AT STA 35 AND BL 15L . REMOVED ANGLE, FABRICATED AND INSTALLED NEW MANUFACTURED ANGLE IAW DC-8 SRM 51-3-0, FIGURE 52A. TREATED AREA IAW DC- 8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998100200154 19981002 00154 WP 1998 10 2 RRXA98427 1 19980225 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 37-55 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND LAV SUPPORT ANGLE CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 37 TO 55 AND BL-49L. RE MOVED SUPPORT ANGLE, FABRICATED AND INSTALLED NEW MANUFACTURED SUPPORT ANGLE IAW DC-8 SRM 51-3-0 FIGURE 1F. TREATED ARE A IAW DC-8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998100200155 19981002 00155 WP 1998 10 2 RRXA98428 1 19980225 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 661 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 31 LEFT BEYOND LIMITS IAW DC-8 SRM, AT STA 661. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED 2 REPAIR CHANNELS IAW FAA APPROVED TIMCO DER ENGIN EERING SKETCH REO-041871R AND DC-8 SRM 53-2-0 FIGURE 1F. 2 L 7 4 4F RT 4A25 1998100200156 19981002 00156 WP 1998 10 2 RRXA98429 1 19980225 A 5320 INTERCOASTAL DOUG DC8 DC873F 302199F WP BS 260-274 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND INTERCOSTAL CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 260 TO STA 274 AND LONGERON 33 RIGHT. REMOVED DAMAGED INTERCOSTAL, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DAC DWG 9 890702 AND DC-8 SRM 53-2-0 FIGURE 1F. 2 L 7 4 4F RT 4A25 1998100200157 19981002 00157 WP 1998 10 2 RRXA98430 1 19980225 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND SHEAR TIE CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 660 AND LONGERON 34 LEFT. REMOV ED DAMAGED SHEAR TIE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DAC DWG 5616509 AND DC-8 SRM 53-2-0 FIGURE 1F. 2 L 7 4 4F RT 4A25 1998100200158 19981002 00158 WP 1998 10 2 TC8A98061 1 19980922 A 3297 WIRE DOUG DC8 DC862F 3021972 WP LT MLG CHAFED A TC8A O OTHER N FALSE WARNING CL CLIMB 1 GL 23 187SK 46022 DOORS NOT LATCHED LIGHT REMAINED ON AFTER GEAR RETRACTION, CYCLED TWICE AND LIGHT EXTINGUISHED. REPAIRED CHAFFED WIRE A T LEFT PROXIMITY SWITCH. ALSO, FOUND PROXIMITY CONTROL BOX LOOSE, SECURED BOX, CHECKED SYSTEM SATISFACTORY IAW 32-60-0. 2 L 7 4 4F 4A25 1998100200159 19981002 00159 WP 1998 10 2 TC8A98062 1 19980924 A 3260 DOOR LIGHT DOUG DC8 DC862F 3021972 WP LANDING GEAR ILLUMINATED A TC8A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 187SK 46022 ON GEAR RETRACTION, DOOR NOT LATCHED LIGHT ILLUMINATED. RECYCLED GEAR AND LIGHT EXTINGUISHED. 2 L 7 4 4F 4A25 1998100200160 19981002 00160 WP 1998 10 2 TC8A98063 1 19980924 A 2910 FLUID DOUG DC8 DC862F 3021972 WP HYDRAULIC SYST LOST A TC8A A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 23 187SK 46022 LOSS OF HYDRAULIC FLUID AND PRESSURE. ON LANDING, USED AIR BRAKE PRESSURE. 2 L 7 4 4F 4A25 1998100200161 19981002 00161 GL 1998 10 2 98ZZZX3595 2 19980806 A 7230 STUDS SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30 03013 GL COMPRESSOR LOOSE A HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 22342 11510 892 760096 CAE890499S IN CRUISE, 400 FEET, 80 KNOTS, PILOT REPORTED SEVERALS SHUDDERS, THEN NR 2 ENGINE TOT PEGGED TO THE HIGH SIDE. SECURED ENGINE, RETURNED TO BASE AND MADE UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED ENGINE DUE TO N1 AND N2 SEIZURE. SUBMITTER STATED NR 2 COMPRESSOR SCROLL MOUNTING STUDS PULLED OUT. 1 G 7 2 3U 3 U H1NE E1GL 1998100200162 19981002 00162 NE 1998 10 2 98ZZZX3596 1 19980824 A 2612 7630607902104 DETECTOR LOOP SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE BAY FAILED A HEEA F A ACTIVATE FIRE EXT. UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 03 2743E 760155 CAE895213S SHORTLY AFTER TAKEOFF, NR 1 ENGINE FIRE LIGHT ILLUMINATED. PILOT DEPLOYED FIRE BOTTLE AND LANDED WITHOUT INCIDENT. MA INTENANCE FOUND DEFECTIVE FLAME DETECTOR. REF: S-76 IPC, CHAPTER 26-11-00, FIGURE 1, ITEM 21. 1 G 7 2 3U 3 U H1NE E1GL 1998100200164 19981002 00164 NE 1998 10 2 UF6A980520 2 19980829 A 7200 32448411218 MFCU BAG ATP ATP EU PWA PW120 PW126A NE NR 2 ENGINE FAILED A UF6A B E EMER. DESCENT ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 31 851AW 7790 1959 B21672W 2020 124344 ORD - FLT 5753 - NR 2 ENGINE ROLLED BACK TO ZERO PERCENT TORQUE IN-FLIGHT FOLLOWED BY LOW OIL PSI 'CWP'. MAINTENANCE R EMOVED AND REPLACED MFCU. PERFORMED POWER ASSURANCE RUNS, ALL PARAMETERS CHECKED GOOD. (X) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998100200165 19981002 00165 NE 1998 10 2 PLGA980707A 3 19980707 A 6111 6607132886 BLADE SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE OUTER SLEEVE CRACKED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 741BA SF340132938 340A090 DRG59087 ALB - PROPELLER WAS REMOVED TO EVALUATE EXCESS BLADE MOVEMENT. UPON INSPECTION, THE FOLLOWING WAS FOUND: NR 4 BLADE RO OT OUTER SLEEVE WAS CRACKED COMPLETELY AROUND BLADE AND WAS GROOVED. THE NR 4 BLADE PORT SEAL GROOVE OUTER WALL WAS DAM AGED, GOUGES AND HIGH METAL WAS FOUND. NR 4 BLADE WAS REPLACED. (X) 2 L 7 2 4T RT A52EU 6 C P30NE 1998100200166 19981002 00166 SW 1998 10 2 98ZZZX3598 1 19980821 A 5302 407023800118 SUPPORT BELL 407 407 SW TAILBOOM CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 427AL 1988 53107 DURING ROUTINE DAILY INSPECTION FOUND RT UPPER SUPPORT FITTING, FIRST FORWARD SCREW CRACKED CRESCENT SHAPED 1 INCH TO 1. 50 INCHES. THE DRAWING IS OF THE LT HAND CRACK, BUT THE RT HAND CRACK IS IN A SIMILAR LOCATION. 1 G 7 1 3U O H2SW 1998100200167 19981002 00167 SW 1998 10 2 98ZZZX3599 1 19980821 A 5302 407023800117 SUPPORT BELL 407 407 SW TAILBOOM CRACKED A S ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 567AL 714 53246 DURING ROUTINE DAILY INSPECTION, FOUND LT UPPER SUPPORT FITTING, FIRST FORWARD SCREW CRACKED CRESENT SHAPED 1 INCH TO 1. 50 INCHES. 1 G 7 1 3U O H2SW 1998100200168 19981002 00168 EU 1998 10 2 98ZZZX3600 1 19980824 A 2610 B232M FIRE DETECTOR AEROSP AS355 AS355F 8680806 EU RT ENGINE MALFUNCTIONED A ALGA O OTHER O OTHER NR NOT REPORTED 1 SW 03 5773X 5004 IN-FLIGHT, THE RT HAND ENGINE FIRE DETECTION LIGHT ILLUMINATED THEN WENT OFF AND BACK ON AGAIN AND DID NOT GO OUT UNTIL LANDING. AIRCRAFT HAS BEEN SOAKED BY RAIN PRIOR TO THE FIRST FLIGHT OF THE DAY. INSPECTED ENGINES, NO EVIDENCE OF FIRE FOUND. CLEANING MOISTURE FROM FIRE DETECTORS, FOUND SERVICEABLE. 1 G 7 2 3U H11EU 1998100200170 19981002 00170 EU 1998 10 2 OXEA9801293 1 19980911 A 4920 GTCP364A APU FOKKER F28 F28MK4000 4990810 EU APU COMPARTMENT FAILED A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 496US 11169 PDX - FLT 3050 - AFTER TAKEOFF, THE LAVATORY SMOKE DETECTOR SOUNDED AND CABIN FILLED WITH SMOKE. MAINTENANCE INSPECTED AND FOUND APU AT FAULT. ALSO, FOUND OIL IN WATER SEPARATOR ON BOTH NR 1 AND NR 2 PACKS. (X) 2 L 7 2 4F RT A20EU 1998100200171 19981002 00171 EU 1998 10 2 WXEA9801294 1 19980915 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 477AU 11226 GEG - ARROW IN EXIT SIGN OVER COCKPIT DOOR INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS GOOD. (X) 2 L 7 2 4F RT A20EU 1998100200172 19981002 00172 WP 1998 10 2 AALA981600 1 19980817 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 693 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 437AA 49455 TUL - FOUND CRACK IN SKIN AT AFT SIDE OF CX DOOR CUTOUT BETWEEN L23R AND L24R AT FS 693. REPAIRED IAW 53-30-00-6. (M) 2 L 7 2 4F A6WE 1998100200173 19981002 00173 WP 1998 10 2 AALA981601 1 19980817 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 437AA 49455 TUL - FOUND LONGERON 2R CRACKED AFT OF BS 1418. REPAIRED IAW 53-30-00-2. (M) 2 L 7 2 4F A6WE 1998100200174 19981002 00174 WP 1998 10 2 AALA981602 1 19980812 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 525 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 437AA 49455 TUL - FOUND CUSP CORRODED. REPAIRED IAW AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 1998100200175 19981002 00175 WP 1998 10 2 AALA981548 1 19980815 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1871 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION ON INTERIOR SURFACE OF PROTRUDED FUSELAGE SKIN AND FASTENERS PULLING THROUGH AT STATION 1871 ABOVE AND BELOW LONGERON 47R. INSTALLED DOUBLER REPAIR WITH FILLER PIECE IAW SRM 53-20-00 VOL 1. (M) 2 L 7 3 4F A22WE 1998100200176 19981002 00176 WP 1998 10 2 AALA981547 1 19980814 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND SKIN CORRODED AT BELLY DRAIN STATION 1380 BETWEEN LONGERON 51L AND 51R. INSTALLED EXTERNAL DOUBLER PER SRM 53-40-00. (M) 2 L 7 3 4F A22WE 1998100200177 19981002 00177 WP 1998 10 2 AALA981546 1 19980814 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1331 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND STATION 1331, BELLY DRAINS AND SKIN CORRODED. TREATED AREA AND INSTALLED EXTERNAL DOUBLER PER SRM 53-40-00. (M) 2 L 7 3 4F A22WE 1998100200178 19981002 00178 WP 1998 10 2 AALA981545 1 19980814 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1203 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - TWO BELLY DRAINS CORRODED STATION 1203 TO 1209 BETWEEN LONGERON 51R AND 51L. INSTALLED EXTERNAL DOUBLER PER SRM 5 3-40-00. (M) 2 L 7 3 4F A22WE 1998100200179 19981002 00179 WP 1998 10 2 AALA981544 1 19980815 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1139 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 FUSELAGE SKIN BULGED STATION 1139 BETWEEN LONGERONS 47L AND 48L. CUT OUT CORRODED AREA REMOVED TEMP FASTENERS. INSTALL ED FINGER DOUBLERS. SHAVED RIVETS AND APPLIED SEALANT PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998100200180 19981002 00180 WP 1998 10 2 AALA981543 1 19980817 A 5744 BRACKET DOUG DC10 DC1010 3022110 WP RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION IN ONE OF ATTACH BORES TO WRAP AROUND PULLEY BRACKET (RT WING). ENLARGED BORE TO ACCEPT .030 INCH WALL SLEEVE BUSHING NOT EXCEEDING .4340. FABRICATED BUSHING AS PER DC10 SRM FOR SLAT ATTACH LUGS. INSTALLED BUSHING . 4345. WET WITH PRIMER AS PER ESO 7349, DATED 8/14/98. (M) 2 L 7 3 4F A22WE 1998100200181 19981002 00181 WP 1998 10 2 AALA981479 1 19980820 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 899-939 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND SKIN CORRODED BETWEEN SKIN AND STRAP 3 PLACES ON LONGERON 47L, STATION 939, 919, 899. INSTALLED DOUBLER REP AIR PER SRM 53-20-00, 51-21-00. (M) 2 L 7 3 4F A22WE 1998100200182 19981002 00182 WP 1998 10 2 AALA981568 1 19980820 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 875-900 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND SKIN BULGED 3 SEPARATE AREAS ON LONGERON 46L AND 47L FROM STATION 875 TO 900. INSTALLED DOUBLER PER SRM 53- 20-00. (M) 2 L 7 3 4F A22WE 1998100200183 19981002 00183 WP 1998 10 2 AALA981586 1 19980823 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1059-1079 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FUSELAGE SKIN BULGE AND TEMP FASTENERS STATION 1059 AND STATION 1079, LONGERN 45L AND 46L. CUT OUT DAMAGED/CORROD ED AREA INSTALLED DOUBLER PER SRM 53-20-00. (M) 2 L 7 3 4F A22WE 1998100200184 19981002 00184 WP 1998 10 2 AALA981585 1 19980823 A 5330 SKIN DOUG DC10 DC1010 3022110 WP BS 1039 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FUSELAGE SKIN BULGED STATION 1039 BETWEEN LONGERON 46L AND 47. CUT OUT DAMAGED AND INSTALLED DOUBLER PER SRM 53-2 0-00 FIGURE NR 6 TREATED PRIME AND PAINTED REPAIR REF SRM 52-21-01 VOL 1. (M) 2 L 7 3 4F A22WE 1998100200185 19981002 00185 WP 1998 10 2 AALA981584 1 19980823 A 5347 TRAY DOUG DC10 DC1010 3022110 WP BS 1541-1701 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION ALONG NR 1 ROLLER TRAY TOP AND BOTTOM. INSTALLED NEW/FABRICATED TRACK STATION 1541 TO 1701 IAW AA RD 51-10-05. (M) 2 L 7 3 4F A22WE 1998100200186 19981002 00186 NM 1998 10 2 AALA981565 1 19980819 A 5330 SKIN BOEING 727 727223 1384074 NM BS 480-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND CORROSION ON SKIN UNDER INTERCOSTAL AT LBL 8. INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998100200187 19981002 00187 NM 1998 10 2 AALA981564 1 19980818 A 5711 SPAR BOEING 727 727223 1384074 NM WS 300-305 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FRONT SPAR LOWER CHORD CORRODED BELOW NR 1 KRUGER FLAP ACTUATOR FS 300 TO 305. INSTALLED REPAIR PER AARD 57-30-00 -2 PAGE 1-3. (M) 2 L 7 3 4F A3WE 1998100200188 19981002 00188 NM 1998 10 2 AALA981563 1 19980818 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 656 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND CRACK IN STRINGER NR 8 AT RIB ATTACHMENT TOP OF RIB. INSTALLED STRINGER REPAIR PER SB 727-57A159. (M) 2 L 7 3 4F A3WE 1998100200189 19981002 00189 NM 1998 10 2 AALA981562 1 19980818 A 5330 SKIN BOEING 727 727223 1384074 NM BS 580-600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND CORROSION ON FUSELAGE SKIN UNDER INTERCOSTAL AT STRINGER 28R, STATION 580 - STATION 600. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1998100200190 19981002 00190 NM 1998 10 2 USAA980378 1 19980830 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 36695 23318 TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND AN .25 INCH CRACK IN EXTERNAL SKIN AFT OF EQUIPMENT CO OLING DUCT OUTLET STATION 380 LBL 30. INSTALLED DOUBLER OF .100 2024 T-3 PER EA 62368 SB 737-53-1117 REV 1. (M) 2 L 7 2 4F RT A16WE 1998100200191 19981002 00191 NM 1998 10 2 USAA980379 1 19980830 A 5280 6545871523 SKIN BOEING 737 7373B7 1384580 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 36695 23318 TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND .125 INCH CRACK ON DOOR OUTER SKIN FORWARD SERVICE DO OR LOWER HINGE CUTOUT AFT UPPER CORNER. INSTALLED DOUBLER MADE FROM .063 2024 T-3 PER EA 62369 AND SB 737-52-1096. (M) 2 L 7 2 4F RT A16WE 1998100200192 19981002 00192 NM 1998 10 2 USAA980377 1 19980828 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 520AU 34335 23706 TPA - DURING A CX-1 CHECK EDDY CURRENT INSPECTION, FOUND A .625 INCH CRACK BELLY SKIN .063 STA 380. INSTALLED DOUBLER P ER EA 62363 2024 T-3, SB 737-53-1117. (M) 2 L 7 2 4F RT A16WE 1998100200193 19981002 00193 NM 1998 10 2 USAA980374 1 19980826 A 5315 654680977 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 37806 22957 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 BY .5 BY .92 INCH AREA OF CORROSION AROUND SCREW HOLES BS 947 LBL 3 6 TO RBL 56 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED UPPER T-CAP REPAIR PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1998100200194 19981002 00194 NM 1998 10 2 USAA980375 1 19980826 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 37806 22957 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 14 INCH AREA OF CORROSION STATION 967 LBL 30 FLOORBEAM. CORROSION TAS K NR C53-107-20. REPLACED UPPER FLOORBEAM T-CAP PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1998100200195 19981002 00195 NM 1998 10 2 USAA980376 1 19980826 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 22957 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION STATION 1006 LBL 12 FLOORBEAM. CORROSION TAS K NR C53-107-20. SPLICED FLOORBEAM SECTION PER SRM 53-00-51 FIG 202. (M) 2 L 7 2 4F RT A16WE 1998100200196 19981002 00196 NM 1998 10 2 USAA980366 1 19980827 A 5330 65558721 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 36947 23316 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT SERVICE DOOR INSIDE UPPER FRAME SKIN, UPPER HINGE ARM CLOSEOUT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07 AND EA 62249. (M) 2 L 7 2 4F RT A16WE 1998100200197 19981002 00197 NM 1998 10 2 USAA980367 1 19980827 A 5315 6545815569 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 36947 23316 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBOARD SCREW HOLES .5 INCH BY .5 INCH BY 25 INCH ST ATION 344 BETWEEN LBL 14 TO RBL 11 UPPER CHORD FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW 'T' CAP AND SPLI CED ANGLES PER TR 53-10-03 AND EA 62264. (M) 2 L 7 2 4F RT A16WE 1998100200198 19981002 00198 NM 1998 10 2 USAA980368 1 19980827 A 5315 654581292 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 36947 23316 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND FLOORBEAM BOARD SCREW HOLES .5 INBY .5 BY 70 INCH STATI ON 328 BETWEEN RBL 14 TO RBL 56 UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP SECTION PER SRM 53-1 0-51. (M) 2 L 7 2 4F RT A16WE 1998100200199 19981002 00199 NM 1998 10 2 USAA980369 1 19980827 A 5315 654581094 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 23316 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON 'T' CAP OF FLOORBEAM 65 INCH BY 3.5 INCH STATION 312 LBL 8 RBL 56 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. FABRICATED 'T' CAP ANGLES PER TR 53-10-03. (M) 2 L 7 2 4F RT A16WE 1998100200200 19981002 00200 NM 1998 10 2 USAA980370 1 19980827 A 5315 6546568569 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 23316 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 11 INCH AREA OF CORROSION ON UPPER FLOORBEAM CHO RD STATION 1016 LBL 15, CORROSION TASK NR C53-107-02. INSTALLED 11.5 INCH DOUBLER PER SRM 53-00-51 FIG 203. (M) 2 L 7 2 4F RT A16WE 1998100200201 19981002 00201 NM 1998 10 2 USAA980371 1 19980827 A 5320 654587545 BEAM BOEING 737 7373B7 1384580 NM BS 294-331 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 394US 36947 23316 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION ON UPPER SURFACE OF CREASEBEAM INNER CHORD RBBL BETWEEN STATIO N 294.5 TO STATION 331. CORROSION TASK NR C53-107-02. INSTALLED SPLICE PER DRAWING 6545875 AND SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998100200202 19981002 00202 NM 1998 10 2 P2EA98167 1 19980911 A 5330 SKIN BOEING 737 737297 1384480 NM BS 235-242 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - REPAIRED FUSELAGE SKIN BETWEEN BS 235 AND BS 242 BETWEEN STRINGERS 22 AND 24 RIGHT IAW COOPESA EO NR C00-3-53-452- 98, DATED SEPT 4, 1998 AND BOEING FAX COO-SJO-98-0597RR DATED SEPT 4, 1998. DOCUMENTED ON FAA FORM 8110-3 APPROVED AND SUBMITTED BY FAA DER. (M) 2 L 7 2 4F A16WE 1998100200203 19981002 00203 NM 1998 10 2 P2EA98166 1 19980905 A 5313 FRAME BOEING 737 737297 1384480 NM BS 460 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - FORWARD CARGO COMPARTMENT AT BS 460, BETWEEN STRINGER 28 AND 27 RIGHT FRAME CRACKED. REPAIRED FUSELAGE FRAME AT B S 460, BETWEEN STRINGERS 27 AND 28 RIGHT DUE TO CRACK IN REF TO SRM 53-10-4 FIGURE 11. (M) 2 L 7 2 4F A16WE 1998100200204 19981002 00204 NM 1998 10 2 P2EA98163 1 19980905 A 5330 SKIN BOEING 737 737297 1384480 NM BS 934-948 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - REPAIRED FUSELAGE SKIN FROM BS 934 TO BS 948.5 BETWEEN STRINGER 20 AND 22 LEFT IAW COOPESA EO NR C00-3-53-444-98, SEPT 2, 1998 AND BOEING FAC COO-SJO-98-0586RR DATED SEPT 2, 1998. (M) 2 L 7 2 4F A16WE 1998100200205 19981002 00205 1998 10 2 ORJA98203 4 19980820 A 3418 10000165101 TRANSDUCER DOUG DC9 DC983 3022083 WP COCKPIT FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT SJC, STALL INDICATOR FAIL LIGHT CAME ON DURING TAXI. FOUND RN 2 AOA TRANSDUCER AT FAULT. REMOVED AND REPLACED NR 2 AOA TRANSDUCER PER MM 34-19-01. PERFORMED OPERATIONAL TEST OF STALL WARNING SYSTEM PER MM 34-19-00. ALL CHECKS GOOD. P ERFORMED RTS ON NR 1 AND NR 2 DFGS SYSTEMS PER MM 22-01-05. ALL SYSTEMS GO. (M) 2 L 7 2 4F RT A6WE 1998100200206 19981002 00206 1998 10 2 ORJA98202 4 19980820 A 3418 10000165101 TRANSDUCER DOUG DC9 DC983 3022083 WP COCKPIT FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT SJC, SLAT DISAGREEMENT LIGHT WOULD NOT EXTINGUISH. T/S SYSTEM, FOUND CAPTAIN'S STALL WORN. C/B POPS. ISOLATED CAUS E TO CAPTAINS AOA VANE. REMOVED AND REPLACED AOA TRANSDUCER. PROBE CHECKED FLAP/SLAT SYSTEM OPERATION IAW MM 27-81-00. OPS CHECK GOOD. C/B AND AOA CHECKS GOOD. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A6WE 1998100200207 19981002 00207 WP 1998 10 2 ORJA98201 1 19980820 A 5270 SWITCH DOUG DC9 DC983 3022083 WP CABIN CONTAMINATED A ORJA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 WP 11 832RA 53044 AT SJC, AFT GALLEY DOOR LIGHT CAME ON DURING TAXI. CLEANED AFT GALLEY DOOR PROX SWITCH. PERFORMED OPERATION OF AFT GAL LEY DOOR NUMEROUS TIMES. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998100200208 19981002 00208 WP 1998 10 2 ORJA98200 1 19980820 A 3350 BR9687100 BATTERY CHARGER DOUG DC9 DC987 3022087 WP CABIN FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, FLOOR EMERGENCY EGRESS LIGHTS ILLUMINATED WITH SWITCH IN ARMED POSITION AT SEATS, 19, 20, 21 AND 22. REPLACED B ATTERY CHARGER AND BATTERY PACK AT ROWS 19, 20, 21 AND 22. (M) 2 L 7 2 4F RT A6WE 1998100200209 19981002 00209 WP 1998 10 2 ORJA98199 1 19980820 A 7711 2047021 INDICATOR DOUG DC9 DC987 3022087 WP COCKPIT FAILED A ORJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 753RA 49587 AT SJC, TAKEOFF WAS DISCONTINUED AS NR 2 ENGINE EPR INDICATION NEVER GOT ABOVE 1.3, APPROXIMATELY. REMOVED AND REPLACED NR 2 ENGINE EPR GAUGE AND PERFORMED ENGINE RUN IAW MM 71-00-00. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 1998100200210 19981002 00210 NM 1998 10 2 MASA98174 1 19980911 A 3350 GE85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING ROUTINE MAINTENANCE, FOUND THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH 'ON' LIGHT DID NOT ILLUMINATE. MAINTENAN CE FOUND THAT THE LIGHT BULB WAS LOOSE IN THE SWITCH. THE RESECURED THE LIGHT BULB, OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998100200211 19981002 00211 WP 1998 10 2 98ZZZM686 1 19980613 A 2910 LINE DOUG DC8 DC8F54 3021926 WP LT MLG BROKEN A FXLA K NONE K FLUID LOSS TX TAXI/GRND HDL 1 SO 19 56FA 45663 ON TAXI AFTER LANDING MIA, FLT 364 - REPORTED LOSS OF HYDRAULIC QUANTITY TO AUX LEVEL WITH LOW BRAKE PRESSURE LIGHT ILLU MINATED AND NO EFFECTIVE BRAKING OR STEERING. REPLACED BROKEN HYDRAULIC LINE AT LEFT BOGIE TRIM CYLINDER IAW MM 13-6-2. OPS CHECKED NORMAL PER MM 32-10-0 AND 29-0. (M) 2 L 7 4 4F 4A25 1998100200212 19981002 00212 NM 1998 10 2 ASAA9810097 1 19980901 A 7110 RIB BOEING 737 737210C 1384459 NM COWL WORN A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING SCHEDULED C-CHECK, THE NR 1 ENGINE INBOARD COWL 3RD RIB WAS FOUND TO BE WORN. REPAIRED PER EA 7110-01071. (M) 2 L 7 2 4F A16WE 1998100200213 19981002 00213 NM 1998 10 2 ASAA9810096 1 19980901 A 5730 SKIN BOEING 737 737210C 1384459 NM WING CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING SCHEDULED C-CHECK, THE NR 3 LEADING EDGE SLAT ACTUATOR CUTOUT WAS FOUND TO BE CRACKED. REPAIRED PER EA 572 0-01059. (M) 2 L 7 2 4F A16WE 1998100200214 19981002 00214 NM 1998 10 2 ASAA9810095 1 19980901 A 5730 SKIN BOEING 737 737210C 1384459 NM WING CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING SCHEDULED C-CHECK, THE NR 3 LEADING EDGE SLAT UPSTOP CUTOUT WAS FOUND TO BE CRACKED. REPAIRED PER EA 5720- 01059. (M) 2 L 7 2 4F A16WE 1998100200215 19981002 00215 NM 1998 10 2 ASAA9810094 1 19980901 A 5320 BEAM BOEING 737 737210C 1384459 NM RT MLG GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING SCHEDULED C-CHECK, A GOUGE WAS FOUND ON THE RT MAIN LANDING GEAR BEAM FORWARD CORNER. REPAIRED PER EA 5710 -01047 AND BOEING TELEX ASA-SEA-94-0131RR. (M) 2 L 7 2 4F A16WE 1998100200216 19981002 00216 NM 1998 10 2 ASAA9810093 1 19980901 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM BS 947 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING SCHEDULED C-CHECK, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOORBEAM ON BOTH FORWARD AND AFT FLANGES AT STATION 947.5 FROM LBL 30 TO RBL 60. REPAIRED PER EA 5310-01605 AND BOEING TELEX ASA-SEA-95-030RR. (M) 2 L 7 2 4F A16WE 1998100200217 19981002 00217 NM 1998 10 2 ASAA9810092 1 19980901 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING SCHEDULED C-CHECK, FOUND CORROSION IN THE LOWER FORWARD FLANGE OF THE FLOORBEAM AT STATION 787 FROM CENTERL INE TO RBL 63. REPAIRED PER EA 5310-01597. (M) 2 L 7 2 4F A16WE 1998100200218 19981002 00218 NM 1998 10 2 ASAA9810091 1 19980901 A 5315 FLOORBEAM BOEING 737 737210C 1384459 NM BS 787 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING SCHEDULED C-CHECK, FOUND CORROSION IN THE LOWER FORWARD FLANGE OF THE FLOORBEAM AT STATION 787 FROM 0 BBL T O 63 LBL. REPAIRED PER EA 5310-01597. (M) 2 L 7 2 4F A16WE 1998100200219 19981002 00219 1998 10 2 MASA98131 4 19980625 A 3444 9650686001 COMPUTER BEECH 1900 1900D 1154162 CE GPWS MALFUNCTIONED A MASA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 218YV UE218 FLT 5451 - PFN-MCO - ON SHORT FINAL APPROACH TO MCO, CREW RECEIVED A 'TOO LOW GEAR' AURAL WARNING. INITIATED A GO AROUN D AND REQUESTED THE RESCUE TRUCKS STANDBY. ALL OTHER GEAR INDICATIONS WERE NORMAL AND THE GPWS DID NOT ACTIVATE ON THE SECOND APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE GPWS PER MEL 34-18. IN SUBSEQUENT MAI NTENANCE, THE GPWS COMPUTER WAS REMOVED AND REPLACED. (M) 2 L 7 2 4T RT A24CE 1998100200220 19981002 00220 NM 1998 10 2 EISA98212 1 19980829 A 3231 DOOR BOEING 727 72731 1384010 NM RT MLG OUT OF ADJUST A EISA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 240NE 18906 RIGHT MAIN GEAR DOOR OPENS INFLIGHT WITH GEAR LEVER IN OFF POSITION. GENERATED BY PILOT REPORT. FOUND RIGHT MAIN LANDI NG GEAR DOOR MANUAL RELEASE SYSTEM OUT OF ADJUSTMENT, ADJUSTED RIGHT DOOR MANUAL RELEASE SYSTEM PER 32-34-21 MM, OPS CHE CK GOOD. (M) 2 L 7 3 4F A3WE 1998100200221 19981002 00221 WP 1998 10 2 AALA981567 1 19980819 A 5320 FINGER DOUBLER DOUG DC10 DC1010 3022110 WP BS 1701-1720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 133AA 47828 TUL - FOUND CORROSION AT FINGER DOUBLER. DOUBLER LIFTED AT STRAP. INSTALLED FINGER DOUBLER REPAIR PER ESO 7349, DATED 8-18-98. (M) 2 L 7 3 4F A22WE 1998100200222 19981002 00222 NM 1998 10 2 98ZZZM687 1 19980829 A 2150 2040751 ACM BOEING 727 727251 138408H NM RT PACK FAILED A S84A O OTHER O OTHER NR NOT REPORTED 1 EA 21 259US 19978 UNABLE TO MAINTAIN CABIN PRESSURE. AIRCRAFT DIVERTED TO CSO. FOUND RT ACM DEFECTIVE. 2 L 7 3 4F A3WE 1998100200223 19981002 00223 CE 1998 10 2 MASA98161 1 19980826 A 2120 AIR DIST SYSTEM BEECH 1900 1900D 1154162 CE CABIN CONDENSATION A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 35YV UE35 FLT 401 - ROW-ABQ - CREW REPORTED SMOKE IN CABIN IN FLIGHT, AIRCRAFT RETURNED TO ROW. UPON INSPECTION, THE SMOKE PROVED TO BE MOIST AIR FROM THE AIR VENTS, A NORMAL OCCURANCE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998100200224 19981002 00224 WP 1998 10 2 98ZZZM688 1 19980806 A 3350 P2070001214 BATTERY LKHEED 1011 10113851 5265010 WP CABIN DISCHARGED A WRNA K NONE L NO TEST IN INSP/MAINT 1 SO 05 826CR 193A1141 ON PERFORMING 2A CHECK EMERGENCY FLASHLIGHT, FOUND WITH LOW BATTERY. FLASHLIGHT REPLACED. (M) 2 L 7 3 4F A23WE 1998100200225 19981002 00225 CE 1998 10 2 S2YA98027 1 19980905 A 7714 503890571 TACH GEN BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A S2YA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 13 841SK UE84 FLT 1020 - GRB-MKE - ABORTED TAKEOFF DUE TO DECREASE IN PROPELLER RPM FROM 1700 RPM TO 1400 RPM IN FIVE SECONDS. THE A/ C WAS FERRIED BACK TO MKE. MAINTENANCE INSPECTED A/C FOUND RT N2 TACH GENERATOR BAD. REPLACED RT N2 TACH GENERATOR OPS CHECK GOOD. RETURNED A/C TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998100200226 19981002 00226 CE 1998 10 2 S2YA98028 1 19980908 A 2612 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT ENGINE DAMAGED A S2YA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 13 901SK UE90 FLT 1254 - MKE-GRR - ABORTED TAKEOFF DUE TO LT FIRE LOOP ANNUNCIATOR ILLUMINATING DURING TAKEOFF ROLL. MAINTENANCE INSP ECTED A/C FOUND FWD AND AFT FIRE LOOPS BAD. MAINTENANCE REPLACED FWD AND AFT FIRE LOOPS, OPS CHECK GOOD. RETURNED A/C TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998100200227 19981002 00227 CE 1998 10 2 S2YA98029 1 19980908 A 3260 CONNECTOR BEECH 1900 1900D 1154162 CE LT MLG CONTAMINATED A S2YA A UNSCHED LANDING L NO TEST AP APPROACH 1 GL 13 87SK UE87 FLT 1837 - MKE-MSN - DURING APPROACH, THE CREW SELECTED THE LANDING GEAR DOWN. WITH THE GEAR EXTENDED THE LEFT MAIN GEA R DOWN ANNUNCIATOR FAILED TO ILLUMINATE UNTIL 60 SECONDS HAD PASSED. THE CREW DISCONTINUED APPROACH, CYCLED GEAR SEVERA L TIMES, THE ANNUNCIATOR AGAIN FAILED TO ILLUMINATE UNTIL 60 SECONDS HAD PASSED. RETURNED TO MKE AND MADE AN UNEVENTFUL LANDING. DID NOT DECLARE AN EMERGENCY. ONCE AT THE HANGAR MAINTENANCE RIGGED LT MLG DOWNLOCK SWITCH AND CLEANED CANNO N PLUGS FOR LT MLG SWITCHES AND LT ACTUATOR. OPS CHECK GOOD. RETURNED A/C TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998100200228 19981002 00228 CE 1998 10 2 S2YA98026 1 19980819 A 3610 1293800011 VALVE BEECH 1900 1900D 1154162 CE RT ENGINE INTERMITTENT A S2YA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 13 901SK UE90 FLT 1899 - MKE-FNT - THE CREW NOTICED THE RT ENGINE TORQUE FLUCTUATING 300-400 LB FT. NOTIFIED ATC, RETURNED TO MKE. A FTER AN UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED EXTENSIVE TROUBLESHOOTING THE PROBLEM WAS FOUND TO BE AN INT ERMITTENT THROUGH VALVE. AFTER GROUND CHECK, THE AIRCRAFT WAS TEST FLOWN, AND THE ENGINE OPERATED SATISFACTORY. AIRCRA FT WAS RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998100200229 19981002 00229 1998 10 2 SABA290039 4 19980807 A 3442 RADAR DHAV DHC8 DHC8102 2809003 NM COCKPIT CONTAMINATED A SABA A UNSCHED LANDING L NO TEST CR CRUISE 1 SO 33 820PH 063 CLT - FLT 5069 - CLT TO GNV - WEATHER RADAR WENT OUT. AIRCRAFT WAS HEADING INTO WEATHER. AIRCRAFT RETURNED TO CLT FOR MAINTENANCE. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE CHECKED FOR WATE R IN THE SYSTEM, GROUND RUN SYSTEM. A TEST FLIGHT WAS PERFORMED. GROUND TEST AND TEST FLIGHT CHECKED GOOD. AIRCRAFT W AS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998100200230 19981002 00230 EU 1998 10 2 SABA290040 1 19980807 A 2612 51653151 CONTROLLER BAG JETSTM JETSTM3201 1500217 EU LT WING FAILED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 920AE 1854 920 CLT - FLT 5195 - THE LEFT ENGINE FIRE DETECT LIGHT CAME ON. AIRCREW DID NOT SEE ANY FIRE. NO IN FLIGHT EMERGENCY WAS D ECLARED. AIRCRAFT RETURNED TO CLT AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE LEFT ENGINE FIRE DETECT CON TROLUNIT BAD. REMOVED AND REPLACED CONTROLLER. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A56EU 1998100200231 19981002 00231 EU 1998 10 2 RAIA980904 1 19980906 A 3260 AIR136070 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT MLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 570HK 41089 FLT 7701 - JFK - DURING GEAR RETRACTION GEAR HANDLE DISAGREEMENT ILLUMINATED. MAINTENANCE REPLACED LEFT MAIN LANDING GE AR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A41NM 1998100200232 19981002 00232 EU 1998 10 2 RAIA980901 1 19980904 A 2160 4460C000 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 555HK 41072 FLT 7320 - STL - RIGHT AIR OFF CAPTION ILLUMINATED AND RIGHT ECS FAULT. MAINTENANCE REPLACED RIGHT PACK TEMPERATURE SWI TCH. (M) 2 L 7 2 4T RT A41NM 1998100200233 19981002 00233 SO 1998 10 2 C2XA98CL066 1 19980908 A 2750 CONNECTOR EMB 120 EMB120RT SO LT TE FLAPS CONTAMINATED A A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16731 7047 120190 ORF - FLT 3347 - CREW REPORTED THAT DURING CLIMB-OUT THEY RECEIVED A FLAP DISAGREEMENT AND THE OUTBOARD FLAPS WOULD NOT RETRACT, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE LEFT OUTBOARD FLAP ACTUATOR CANNO N PLUG, OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB 120 MM 27-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200234 19981002 00234 NE 1998 10 2 C2XA98CL065 2 19980908 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT NACELLE FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 16710 120106 115141 TOL - FLT 3022 - CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A LEFT ENGINE LOW OIL PRESSURE WARNING, AIRCRAFT RETURNE D TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LEFT ENGINE AND FOUND THE OIL LEVEL TO BE 3 QUARTS L OW. THE ENGINE OIL LEVEL WAS SERVICED UP TO THE PROPER LEVEL IAW EMB-120 MM 12-12-01, AIRCRAFT RELEASED FOR SERVICE. ( M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200235 19981002 00235 EU 1998 10 2 C2XA98BT066 1 19980906 A 3350 3011210 LIGHT AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69901 379 BTV - DURING 3 A INSPECTION FOUND PASSENGER DOOR EMERGENCY LIGHT INOPE RATIVE. REMOVED AND REPLACED LIGHT ASSY. OPS CH ECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998100200236 19981002 00236 EU 1998 10 2 C2XA98BT064 1 19980903 A 3320 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 25811 094 FLT 3357 - RETURNED TO EWR AFTER FLIGHT ATTENDANT NOTED SMOKE IN CABIN NEAR OVERHEAD ON LEFT SIDE. MAINTENANCE INVESTIG ATED FOUND READING LIGHT 11 A/B HAD BURNED POWER SUPPLY. A/C MEL'D IAW MEL 25-36-01-4 PLACARD NR 20719. (M) 2 H 7 2 4T RT A53EU 1998100200237 19981002 00237 EU 1998 10 2 C2XA98IA348 1 19980908 A 3350 7012210 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT EMERGENCY GROUND ILLUMINATION LIGHT WAS FOUND TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED A DEFECTIVE BULB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200238 19981002 00238 EU 1998 10 2 C2XA98IA349 1 19980908 A 5320 S539714230000 CHORD AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE UPPER CHORD ON FRAME 27A WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE DAMAGED CHORD IAW ATR42-320 SRM 51-25-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200239 19981002 00239 EU 1998 10 2 C2XA98IA350 1 19980908 A 5712 S5721158100000 RIB AEROSP ATR42 ATR42320 8680930 EU LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14815 104 IAH - DURING C-CHECK INSPECTION, THE LEFT WING OUTBOARD LEADING EDGE ATTACH RIB ON THE FRONT SPAR WAS FOUND TO BE CRACKE D. MAINTENANCE REMOVED AND REPLACED THE RIB IAW ATR SRM 57-20-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200240 19981002 00240 SO 1998 10 2 C2XA98IA342 1 19980908 A 5320 12006159001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT INBOARD FLOORBEAM CORRODED FROM FRAMES 38 TO 44. MAINTENANCE REMOVED AND R EPLACED THE DAMAGED SECTION OF BUTT STRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1998100200241 19981002 00241 SO 1998 10 2 C2XA98IA341 1 19980908 A 5320 12006158002 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND LEFT INBOARD FLOORBEAM CORRODED FROM FRAME 38 TO 44. MAINTENANCE REMOVED AND REP LACED THE BUTTSTRAP IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200242 19981002 00242 SO 1998 10 2 C2XA98IA340 1 19980908 A 5347 12026865009 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 22727 120177 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT T RACK IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200243 19981002 00243 WP 1998 10 2 98ZZZM689 2 19980813 A 7200 31025403 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT NACELLE FAILED A MEJA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 17 2671V 437 P44114 MIA-ZQA - DURING TAKEOFF, THE RIGHT ENGINE WOULD NOT MAKE CHARTED TORQUE AND THE TAKEOFF WAS ABORTED. MAINTENANCE INSPE CTED THE ARICRAFT AND FOUND IT SAFE FOR A FERRY FLIGHT. AIRCRAFT WAS FERRIED TO OPF FOR MAINTENANCE AND THE RIGHT ENGIN E WAS REMOVED AND REPLACED WITH A CONTINUED TIME UNIT. OPERATIONS CHECK WAS GOOD AND THE AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1998100200244 19981002 00244 EU 1998 10 2 98ZZZM690 1 19980312 A 2150 BLEED AIR BAG BAE146 BAE146200A 1500266 EU CABIN SMOKE A A6WA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 31 183US E2043 AFTER TAKEOFF CABIN AND COCKPIT FILLED WITH FUMES, SMELLED LIKE SOMETHING OVERHEATING, OCCURED WHEN SWITCHING FROM APU T O ENGINE BLEED AIR. AIRCRAFT RETURNED TO DEN AND LANDED OVERWEIGHT. COMPLETED PACK BURNOUT PROCEDURE PER MM ON BOTH EN G AND APU BLEED AIR, NO DISCREPANCIES NOTED. COMPLIED WITH OVERWEIGHT LANDING INSPECTION. (M) 2 H 7 4 4F RT A49EU 1998100200245 19981002 00245 EU 1998 10 2 98ZZZM691 1 19980227 A 2731 TRIM BAG BAE146 BAE146200A 1500266 EU ELEV BINDS A A6WA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 31 607AW E2052 ELEVATOR TRIM BINDS AT ALL SPEEDS, ALL ALTITUDES WHEN MOVED FORWARD OF 3 ON THE TRIM INDICATOR. 2 H 7 4 4F RT A49EU 1998100200246 19981002 00246 EU 1998 10 2 98ZZZM692 1 19980226 A 2731 TRIM BAG BAE146 BAE146200A 1500266 EU ELEV BINDS A A6WA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 31 607AW E2052 AT 20,000 FT 290 KTS ELEV TRIM BINDS WHEN TRYING TO TRIM NOSE DOWN, NOSE UP FEELS NORMAL. PERFORMED ELEV TRIM CIRCUIT F RICTION TST, ALSO PERFORMED CLUTCH FRICTION TEST, INSPECTED CIRCUIT AND INTERCONNECT CIRCUIT AT ELEV, BOTH TESTS AND VIS UAL ACCOMPLISHED WITH NO DEFECTS NOTED. GEN W/C FOR CHANGE OF LT AND RT TRIM SCREW JACKS. DAMPER HTR TESTS OK. (M) 2 H 7 4 4F RT A49EU 1998100200247 19981002 00247 EU 1998 10 2 98ZZZM694 1 19980119 A 7110 COWL DOOR BAG BAE146 BAE146200A 1500266 EU ENT LT FWD DEFECTIVE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 ALL FOUR ENGINES LEFT FORWARD COWL DOORS REQUIRE LOWER FORWARD DOOR FRAME TRIMMED. TRIMMED FRAME END OF ALL FOUR LEFT F ORWARD COWL DOORS IAW FAX KW/1715-91. 2 H 7 4 4F RT A49EU 1998100200248 19981002 00248 SO 1998 10 2 C2XA98CL050 1 19980705 A 2120 CABIN EMB 120 EMB120RT SO AIR DIST SMOKE A C2XA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 09 51726 120174 CLE - FLT 3043 - THE CREW REPORTED THAT DURING TAXI OUT SMOKE FILLED THE CABIN. AIRCRAFT RETURNED TO GHE GATE. MAINTEN ANCE INSPECTED THE AIRCRAFT AND THEN RELEASED IT IAW MEL 21-50-2 CAT C NR 19880. THE AIRCARFT WAS OPERATIONAL CHECKED L ATER IN THE SAME DAY WITHOUT ANY DISCREPANCIES BEING FOUND, AND WAS RELEASED FOR SERVICE AND FROM THE MEL. (M) 2 L 7 2 4T RT A31SO 1998100200249 19981002 00249 SO 1998 10 2 C2XA98IA310 1 19980820 A 5320 12034415002 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, A SKIN SUPPORT AT FRAME 9 RIGHT WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED SKIN SUPPORT IAW EMB120 SRM 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200250 19981002 00250 SO 1998 10 2 C2XA98IA309 1 19980820 A 5347 12026865609 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200251 19981002 00251 SO 1998 10 2 C2XA98IA308 1 19980820 A 5320 12006158007 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP FROM FRAME 36 TO FRAME 40 WAS FOUND TO BE CORRODED. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1998100200252 19981002 00252 SO 1998 10 2 C2XA98IA307 1 19980820 A 5347 12015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE SEAT TRACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200253 19981002 00253 SO 1998 10 2 C2XA98IA306 1 19980820 A 5347 12015994603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REP LACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200254 19981002 00254 SO 1998 10 2 C2XA98IA305 1 19980820 A 5347 12016000603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE SEAT TRACK AND THE AIRCRAFT WS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200255 19981002 00255 SO 1998 10 2 C2XA98IA304 1 19980820 A 5347 12015994603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE RIGHT FORWARD WALL SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND RE PLACED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200256 19981002 00256 SO 1998 10 2 C2XA98IA303 1 19980820 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200257 19981002 00257 SO 1998 10 2 C2XA98CL064 1 19980817 A 3610 CA33020 CLAMP EMB 145 EMB145 SO CARGO BAY BROKEN A C2XA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 15932 145015 BNA - FLT 4048 - CREW REPORTED AFTER TAKEOFF AND AT ABOUT 11,000 FT, HEARD LOUD NOISE AND RECEIVED A NR 1 DUCT LEAK LIGH T AND CARGO SMOKE WARNING. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCARFT AND FOUND A BLEED DUCT UNDER THE CARGO FLOOR HAD SEPARATED AT THE UNION. MAINTENANCE REMOVED AND REPLACED A CLAMP AT THE D UCT UNION IAW EMB-145 MM 36-11-09, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998100200258 19981002 00258 EU 1998 10 2 C2XA98BT059 1 19980812 A 3350 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN MISSING A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 34817 152 EMERGENCY EXIT LIGHT MISSING, CREW REPORTED. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT AND RESECURED PIN ON CANNON PLUG 41WLA. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998100200259 19981002 00259 SO 1998 10 2 C2XA98IA301 1 19980812 A 3350 F02A250V1A LIGHT EMB 120 EMB120RT SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59708 120098 IAH - DURING PRE-FLIGHT INSPECTION, THE PILOT REPORTED THAT THE LEFT AND RIGHT EXTERNAL EMERGENCY LIGHTS WERE INOPERATIV E. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200260 19981002 00260 CE 1998 10 2 C2XA98CL060 1 19980804 A 5730 118110047652 SKIN BEECH 1900 1900D 1154162 CE RT WING DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 81553 UE222 CLE - WHILE A/C WAS PARKED ON RAMP, A RUNWWAY GPU STRUCK THE RIGHT LEADING EDGE AND WING. THE A/C WAS INSPECTED AND FOU ND TO HAVE SEVERAL SCRATCHES IN THE WING SKIN AND TWO DENTS IN THE LEADING EDGE. THE A/C MAINTENANCE FERRIED TO RFD AND RAYTHEON A/C SERVICES REPAIRED THE WING AND LEADING EDGE IAW B1900 SRM 57-90-00. THE AIRCRAFT WAS THEN FLOWN TO CLE, I NSPECTED AND RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998100200261 19981002 00261 SO 1998 10 2 C2XA98CL061 1 19980809 A 3260 MS3470L833S CONNECTOR EMB 120 EMB120RT SO NLG CORRODED A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 12715 120125 CLE - FLT 3344 - CREW REPORTED THAT UPON SELECTION OF GEAR UP, NO GEAR RETRACTION OCCURRED. THE CREW RECEIVED ALL RED A ND ALL GREEN INDICATION LIGHTS WITH THE GEAR SELECTOR IN THE UP POSITION, ALL INDICATION WERE NORMAL WITH GEAR SELECTOR IN THE DOWN POSITION. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LANDING SYSTEM TH EN REMOVED AND REPLACED THE UPLOCK PROX SWITCH CONNECTOR ON THE AIRFRAME SIDE IAW EMB-120 WM 20-50-03. OPERATIONAL CHEC KS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200262 19981002 00262 SO 1998 10 2 C2XA98CL062 1 19980810 A 3610 12024939001 TUBE EMB 120 EMB120RT SO LT ENGINE TORN A C2XA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 16731 120190 MKE - FLT 3293 - THE CREW REPORTED THAT DURING CRUISE, RECEIVED A DUCT LEAK LIGHT ON THE LEFT ENGINE. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE AND THE LEFT ENGINE BLEED AIR TUBE ASS EMBLY WAS REMOVED AND REPLACED IAW EMB-120 MM 36-10-01. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT WAS REL EASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200263 19981002 00263 SO 1998 10 2 C2XA98IA300 1 19980806 A 5720 12004353015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND A WING SKIN SUPPROT CRACKED AT FRAME 19, LEFT WING. MAINTENANCEE REMOVED AND REP LACE THE SUPPORT IAW EMB120ER SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200264 19981002 00264 SO 1998 10 2 C2XA98IA299 1 19980608 A 5320 12004166001 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT BUTT STRAP AT FRAME 40 CORRODED. MAINTENANCE REMOVED THE CORROSION AND INSTALLED A REINFORCING DOUBLER IAW EMB120ER SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200265 19981002 00265 SO 1998 10 2 C2XA98IA298 1 19980806 A 5347 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT LOWER AFT SEAT TRACK WAS CORRODED. MAINTENANCE REMOVED AND REPLACED TH E SEAT TRACK IAW THE EMB120ER A/C MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200266 19981002 00266 SO 1998 10 2 C2XA98IA297 1 19980806 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND THE LEFT AFT LOWER SEAT TRACK HAD CORROSION. MAINTENANCE REMOVED AND REPLACED TH E SEAT TRACK IAW EMB120ER A/C MM 53-01-05. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200267 19981002 00267 SO 1998 10 2 C2XA98IA296 1 19980806 A 5210 12026539001 BELLCRANK EMB 120 EMB120RT SO PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND THE PASSENGER/CREW DOOR EXTERNAL HANDLE, FORWARD BELLCRANK CORRODED. MAINTENANCE REMOVED AND REPLACED THE BELLCRANK IAW EMB120ER 52-10-00, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200268 19981002 00268 SO 1998 10 2 C2XA98IA295 1 19980806 A 5320 12034416001 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND A SKIN SUPPORT BRACKET CRACKED AT FRAME 9 JUST BELOW RIGHT DIRECT VISION WINDOW. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB120ER SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998100200269 19981002 00269 SO 1998 10 2 C2XA98IA294 1 19980806 A 5320 12034416002 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURNG C-CHECK INSPECTION, FOUND A SKIN SUPPORT BRACKET CRACKED AT FRAME 9 JUST BELOW LEFT DIRECT VISION WINDOW. M AINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB120ER SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200270 19981002 00270 SO 1998 10 2 C2XA98IA293 1 19980806 A 5320 12006157007 BUTT STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT CORNER BUTT STRAP CORRODED BETWEEN FRAME 38 AND 47. MAINTENANCE REMOVE D AND REPLACED THE BUTT STRAP SECTION IAW EMB120ER SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1998100200271 19981002 00271 SO 1998 10 2 C2XA98IA292 1 19980806 A 5320 12006144003 SUPPORT EMB 120 EMB120RT SO FUSELAGE BENT A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND A BUTT STRAP VERTICAL SUPPORT BENT FRAME 45. MAINTENANCE REMOVED AND REPLACED TH E VERTICAL SUPPORT IAW EMB120ER SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200272 19981002 00272 SO 1998 10 2 C2XA98IA291 1 19980806 A 5320 12004149002 TEE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND A T-PROFILE AT FRAME 36 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-P ROFILE IAW EMB120ER SRM 51-21-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200273 19981002 00273 SO 1998 10 2 C2XA98IA290 1 19980806 A 5320 12028877001 TEE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING C-CHECK INSPECTION, FOUND A T-PROFILE AT FRAME 33 TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE T-P ROFILE IAW EMB120ER SRM 51-25-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200274 19981002 00274 EU 1998 10 2 C2XA98IA285 1 19980801 A 5320 S53678009201 FITTING AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLOOR SUPPORT FITTING CORRODED BETWEEN FRAMES NR 36 AND NR 38 AT STRIN GER 16R. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW ATR 42 SRM 51-25-02, 03, 04. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200275 19981002 00275 EU 1998 10 2 C2XA98IA286 1 19980801 A 5347 S53678001200 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND AFT RIGHT SIDE FLOOR SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE S EAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200276 19981002 00276 EU 1998 10 2 C2XA98IA287 1 19980818 A 5320 S53981101204 ANGLE AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE WING TO FUSELAGE FAIRING WEB SUPPORT CRACKED AT LOWER ATTACHMENT ANGLE . MAINTENANCE REMOVED AND REPLACED THE ANGLE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200277 19981002 00277 EU 1998 10 2 C2XA98IA288 1 19980801 A 5320 S5337129320201 CHANNEL AEROSP ATR42 ATR42320 8680930 EU CARGO BAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING C-CHECK INSPECTION, FOUND CARGO DOOR THRESHOLD DRAIN CHANNEL CORRODED. MAINTENANCE REMOVED AND REPLACED TH E DRAIN CHANNEL IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200278 19981002 00278 SO 1998 10 2 C2XA98IA289 1 19980729 A 2710 12027655035 CONTROL CABLE EMB 120 EMB120RT 3260202 SO LT AILERON FRAYED A C2XA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 SW 09 15730 120187 SHV - FLT 3776 - THE PILOT REPORTED THE LEFT CONTROL YOKE HAD EXCESSIVE PLAY IN AILERON CONTROL. THE AIRCRAFT LANDED AT SHV WITHOUT INCIDENT WHERE MAINTENANCE FOUND THE LEFT AILERON CONTROL QUADRANT LOWER CABLE TO HAVE BROKEN STRANDS. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED CABLE IAW EMB120 MM CH 27-11-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200279 19981002 00279 EU 1998 10 2 C2XA98BT055 1 19980803 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26826 172 EWR - DURING 1 A INSPECTION, FOUND FORWARD FLOOR EXIT LIGHTS AND CENTER CEILI NG EMERGENCY EXIT LIGHTS INOPERATIVE. REM OVED AND REPLACED A BATTERY PACK AT LOCATION 10 WL FOR CENTER CEILING LIGHTS AND REMOVED AND REPLACED EMERGENCY POWER SU PPLY FOR FORWARD FLOOR EXIT LIGHTS. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998100200280 19981002 00280 EU 1998 10 2 98ZZZM695 1 19980803 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26826 172 EWR - DURING 1 A INSPECTION, FOUND FORWARD FLOOR EXIT LIGHTS AND CENTER CEILI NG EMERGENCY EXIT LIGHTS INOPERATIVE. REM OVED AND REPLACED A BATTERY PACK AT LOCATION 10 WL FOR CENTER CEILING LIGHTS AND REMOVED AND REPLACED EMERGENCY POWER SU PPLY FOR FORWARD FLOOR EXIT LIGHTS. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998100200281 19981002 00281 SO 1998 10 2 C2XACL98058 1 19980805 A 3620 M1160140242 SENSORS EMB 120 EMB120RT SO LT WING FAILED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 SW 09 16731 120190 BUF - FLT 3261 - CREW REPORTED THAT DURING CLIMB THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED, THE LIGHT WOULD NOT EXTING UISH AFTER CHECK LIST COMPLETION AND THE ELFT ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE AND THE LEFT ENGINE DUCT LEAK SENSORS WERE REMOVED AND REPLACED I AW EMB-120 MM 36-20-01, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200282 19981002 00282 SO 1998 10 2 C2XA98CL059 1 19980805 A 5753 12033045501 CHANNEL EMB 120 EMB120RT SO LT TE FLAP CRACKED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16731 120190 BUF - FLT 4377 - CREW REPORTED THAT AFTER TAKEOFF FOR A FERRY FLIGHT TO CLE THEY RECEIVED A FLAP DISAGREEMENT THAT WOULD NOT CORRECT ITSELF, AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS INSPECTED AND FERRIED TO CLE , WHERE THE LEFT OUTBOARD FLAP LOWER CHANNEL WAS REMOVED AND REPLACED ALONG WITH THE INBOARD BEARING AND BRACKET IAW EMB -120 MM 27-50-04. OPERATIONAL CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100200283 19981002 00283 WP 1998 10 2 ASAA9880162 1 19980826 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 1 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998100200284 19981002 00284 WP 1998 10 2 ASAA9880161 1 19980826 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 24 TO 28 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998100200285 19981002 00285 WP 1998 10 2 ASAA9880157 1 19980822 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 PDX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 7 WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998100200286 19981002 00286 WP 1998 10 2 ASAA9880156 1 19980821 A 3350 S103 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 22 TO 24 WERE FOUND INOPERATIVE. REPLACED TH E BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998100200287 19981002 00287 WP 1998 10 2 ASAA9880155 1 19980821 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 22 TO 24 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998100200288 19981002 00288 WP 1998 10 2 ASAA9880154 1 19980820 A 3350 014597101 BATTERIES DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE FORWARD ENTRY WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998100200289 19981002 00289 NM 1998 10 2 ASAA9810089 1 19980819 A 3350 LIGHT BOEING 737 737290C 138448V NM CABIN MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT LIGHT AT ROW 9 WAS FOUND TO BE MISSING. REPLACED LIGHT ASSEMBLY AND LENS, AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998100200290 19981002 00290 NM 1998 10 2 ASAA9810088 1 19980818 A 3350 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 17. RECONNECT ED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998100200291 19981002 00291 NM 1998 10 2 AALA981476 1 19980805 A 3610 8085561 VALVE BOEING 767 767223 1385123 NM LT ENGINE CLOGGED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 324AA 22325 SFO - FLT 682 - AFTER TAKEOFF SFO, EN ROUTE TO ORD SMOKE AND FUMES NOTED IN THE CABIN. RETURNED TO SFO AND LANDED WITHO UT INCIDENT. REPLACED 8TH STAGE CHECK VALVE AND DUCTING TO PRE-COOLER DUE TO LINE BEING PLUGGED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998100200292 19981002 00292 WP 1998 10 2 AALA981494 1 19980810 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 460AA 49565 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT ROWS 25D INOPERATIVE. RESPLICED BROKEN WIR E AT EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 25D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100200293 19981002 00293 WP 1998 10 2 AALA981475 1 19980804 A 2612 FIRE LOOP DOUG DC9 DC982 3022082 WP RT ENGINE LOOSE A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 297AA 49309 DFW - FLT 794 - DURING CRUISE, EN RUOTE PHX-ORD, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIR INTERRUPTED A ND LANDED DFW WITHOUT INCIDENT. RE-TORQUED LOOSE SENSE LINE ON RIGHT AUGMENTATION VALVE TO HIGH STAGE PILOT VALVE LINE. SYSTEM LEAK AND GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100200294 19981002 00294 NM 1998 10 2 AALA981504 1 19980811 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND STRINGER 15 CRACKED AT END STATION 720C. REPAIRED STRINGER 15L, STATION 720C PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998100200295 19981002 00295 NM 1998 10 2 AALA981503 1 19980811 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND CRACK IN STRINGER END STATION 720 PLUS 5 INCHES, STRINGER 15R. REPAIRED STRINGER 15R AT STATION 720B PER SR M 53-10-3. (M) 2 L 7 3 4F A3WE 1998100200296 19981002 00296 NM 1998 10 2 AALA981502 1 19980811 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND STRINGER 15L CRACKED AT END STATION 720B PLUS 3 INCHES. REPAIRED STRINGER 15L, STATION 720B PLUS 3 INCHES P ER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998100200297 19981002 00297 NM 1998 10 2 AALA981501 1 19980811 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 733 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND STATION 720L PLUS 13 INCHES STRINGER 27L OUTBOARD SIDE HAS CORROSION. CUT OUT STRINGER SECTION AND SPLICED IN NEW SECTION PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998100200298 19981002 00298 NM 1998 10 2 AALA981500 1 19980811 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FLOORBEAM CORRODED UNDER SEAT TRACK TOP AND BOTTOM SIDE OF UPPER FLANGES. FLOORBEAM REPAIRED PER SRM 53-10-8. (M ) 2 L 7 3 4F A3WE 1998100200299 19981002 00299 NM 1998 10 2 AALA981499 1 19980811 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FLOORBEAM CORRODED UPPER FLANGE UNDER SEAT TRACK STATION 1110 LBL 24. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SR M 53-10-8. (M) 2 L 7 3 4F A3WE 1998100200300 19981002 00300 NM 1998 10 2 AALA981498 1 19980811 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FLOORBEAM AT STATION 1110 RBL 8 HAS CORROSION ON UPPER FLANGE AROUND FLOORBOARD HOLE. CUT OUT SECTION OF TOP FLAN GE AND REPAIRED PER SRM 53-10-8 PAGE 9A AND 9B. (M) 2 L 7 3 4F A3WE 1998100200301 19981002 00301 NM 1998 10 2 AALA981497 1 19980811 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND FLOORBEAM 1130 RBL 25 CORRODED AT BOLT HOLE. REPAIRED FLOORBEAM PER ESO 11697, DATED 7/19/98. (M) 2 L 7 3 4F A3WE 1998100200302 19981002 00302 WP 1998 10 2 USAA980396 1 19980913 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 465 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 991VJ 75151 47310 PIT - DURING C-5 CHECK, FOUND 1 INCH CRACK JUST AFT OF STATION 465, LONGERON 20 (NEAR VHF ANTENNA) IN FUSELAGE SKIN. DE TECTED VISUALLY AND BY EDDY CURRENT. REPAIRED PER EO NR 5385X016 AND EA NR 50475. (M) 2 L 7 2 4F A6WE 1998100200303 19981002 00303 WP 1998 10 2 USAA980395 1 19980913 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 617 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 991VJ 75151 47310 PIT - DURING C5 CHECK, FOUND CRACK .5 INCH LONG AT STATION 617, 8 RT LONGERON. DETECTED BY EDDY CURRENT. SPLICED IN NE W SECTION LONGERON PER 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1998100200304 19981002 00304 EU 1998 10 2 USAA980389 1 19980904 A 5320 BRACKET FOKKER F28 F28MK0100 4990807 EU RT MLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 862US 19993 11300 PIT - DURING RON, RIGHT FORWARD MLG DOOR ACTUATOR LOOSE 2 INCH CRACK ACTUATOR BRACKET DOUBLER AT RT WHEEL WELL FWD INBOA RD CORNER AT MLG ACTUATOR BRACKET. INSTALLED DOUBLERS, FILLERS TO WEB AREA, NESTED ANGLE REPAIR PER EA 50457. (M) 2 L 7 2 4F RT 1998100200305 19981002 00305 WP 1998 10 2 USAA980393 1 19980701 A 5311 99196182 FRAME DOUG DC9 DC931 3022065 WP BS 718 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 74555 47336 PIT - DURING C-2 CHECK, FOUND 4 INCH FWD POCKET CRACK AND 4 INCH AFT POCKET CRACK TO TRAPAZOIDAL HOLE AT FS 718 FRAME. R EMOVED AND REPLACED MAIN FRAME 718 PER DWG 392031. (M) 2 L 7 2 4F A6WE 1998100200306 19981002 00306 NM 1998 10 2 USAASB98235 1 19980906 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 448US 24892 IAH - MAINTENANCE FOUND THE CENTER CABIN EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998100200307 19981002 00307 NM 1998 10 2 USAASB98230 1 19980904 A 3350 20121 BATTERY CHARGER BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 434US 24556 GSO - MAINTENANCE FOUND ALL THE EMERGENCY EXIT LOCATOR AND THE AISLE LIGHTS INOP AT SEAT ROW 11 ABC AND THE EXTERIOR OVE RWING LEFT AFT EXIT HATCH LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY AT STATION 598R. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998100200308 19981002 00308 NM 1998 10 2 USAASB98229 1 19980903 A 3350 1012721 LIGHT BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 387US 22959 ROC - MAINTENANCE FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT ON SEAT 22 END BAY INOP. MAINTENANCE FOUND THE WIRES PULLED OUT OF LAMPHOLDER. REMOVED AND REPLACED THE LAMPHOLDER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998100200309 19981002 00309 NM 1998 10 2 USAASB98228 1 19980903 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245US 22751 EWR - MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR EMERGENCY EXIT INOP. MAINTENANCE REMOVED AND REPLACED THE MAIN ENTR Y DOOR EXIT LIGHT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998100200310 19981002 00310 NM 1998 10 2 USAASB98227 1 19980903 A 3350 S106 BATTERIES BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 233US 22273 ALB - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE AFT PASSENGER ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLAC ED THE BATTERIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998100200311 19981002 00311 1998 10 2 USAAD98157 4 19980905 A 2565 13621224 SLIDE DOUG DC9 DC931 3022065 WP FUSELAGE FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 965VJ 47374 PIT - THE AFT ESCAPE SLIDE MECHANISM FAILED TO DEPLOY SLIDE DURING FUNCTIONAL TEST. MAINTENANCE REPAIRED THE SLIDE RELE ASE MECHANISM AND REPLACED THE SLIDE ASSY. (M) 2 L 7 2 4F A6WE 1998100200312 19981002 00312 WP 1998 10 2 USAAD98156 1 19980907 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939VJ 48120 DTW - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 9 AND 13 WERE DIM. MAINTENANCE REPLACED BATTERIES FOR THE CEILING EMERG ENCY LIGHTS BETWEEN ROWS 9 TO 13. (M) 2 L 7 2 4F A6WE 1998100200313 19981002 00313 EU 1998 10 2 USAAF98073 1 19980908 A 3350 59257 INVERTER FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 850US 11276 IND - LOW LEVEL EMERGENCY FLOOR LIGHTS INOPERATIVE AFT OF ROW 16. MAINTENANCE REPLACED THE 6 VOLT INVERTER AND TWO BATT ERY PACKS. (M) 2 L 7 2 4F RT 1998100200314 19981002 00314 EU 1998 10 2 98ZZZM696 1 19980908 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 850US 11276 IND - LOW LEVEL EMERGENCY FLOOR LIGHTS INOPERATIVE AFT OF ROW 16. MAINTENANCE REPLACED THE 6 VOLT INVERTER AND TWO BATT ERY PACKS. (M) 2 L 7 2 4F RT 1998100200315 19981002 00315 EU 1998 10 2 SIMA982493 1 19980906 A 5320 S536721729402 PLATE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND PAX DOOR SILL PLATE CORRODED. REMOVED AND REPLACED THE SILL PLATE. AIRCRAFT RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200316 19981002 00316 EU 1998 10 2 SIMA982492 1 19980906 A 5347 S53375001220 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN LT FWD CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING SEAT TRACKS CORRODED. LOCATIONS WERE THE LEFT FORWARD, MIDDLE AND A FT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO TRACKS CORRODED. REMOVED AND REPLACED CORRODED TRACKS. AI RCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200317 19981002 00317 EU 1998 10 2 98ZZZM697 1 19980906 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU RT MID INB-OUTB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING TRACK LOCATIONS. LEFT FORWARD, MIDDLE AND AFT OUTBOARD , LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT A FT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200318 19981002 00318 EU 1998 10 2 98ZZZM698 1 19980906 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212 EU RT AFT CARGO CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING LOCATIONS. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CAR GO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200319 19981002 00319 EU 1998 10 2 98ZZZM699 1 19980906 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU RT FLT ATTEN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND TRACK CORROSION AT THE FOLLOWING LOCATIONS. LEFT FORWARD,MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGH T ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT A FT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200320 19981002 00320 EU 1998 10 2 98ZZZM700 1 19980906 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN RT MID INB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING TRACKS CORRODED. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT IN BOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200321 19981002 00321 EU 1998 10 2 98ZZZM701 1 19980906 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU LEFT FLT ATTEN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING TRACK LOCATIONS. LEFT FORWARD, MIDDLE AND AFT OUTBOARD , LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RI GHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1998100200322 19981002 00322 EU 1998 10 2 98ZZZM702 1 19980906 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN LT AFT INB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING TRACK LOCATIONS. LEFT FORWARDRD, MIDDLE AND AFT OUTBOA RD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO S EAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200323 19981002 00323 EU 1998 10 2 98ZZZM703 1 19980906 A 5347 S53678020102 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN AFT OUTB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING SEAT TRACKS CORRODED. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT A FT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO TRACKS CORR ODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 1998100200324 19981002 00324 EU 1998 10 2 98ZZZM704 1 19980906 A 5347 S53570203200 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN MID OUTB CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LE FT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT C ARGO TRACKS CORRODED. REMOVED AND REPLACED CORRODED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200325 19981002 00325 EU 1998 10 2 SIMA982473 1 19980903 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AM 447 SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AROUND NUT CLIP ON FLOORBEAM 36. INSTALLED SPLICE AND NEW SECTION OF FL OORBEAM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200326 19981002 00326 EU 1998 10 2 SIMA982471 1 19980904 A 5347 725370209 SEAT TRACK SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 256AE 340B256 ABI - SEAT TRACKS AT BL 18.3L AND BL 0 ARE CORRODED FROM FUSELAGE STATION 546 TO 686. SPLICE REPAIRED SEAT TRACKS. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998100200327 19981002 00327 EU 1998 10 2 SIMA982462 1 19980903 A 5347 S53375001226 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AM 447 SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT AFT INBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200328 19981002 00328 EU 1998 10 2 SIMA982431 1 19980831 A 5311 S536R00521R0100 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-1 INSPECTION, FOUND FRAME 36 CORRODED AT FLOOR LEVEL. REPAIRED FRAME. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100200333 19981002 00333 NE 1998 10 2 98ZZZX3606 1 19980827 A 6710 7690001880106 AMPLIFIER SKRSKY S76 S76A 8143006 NE DROOP COMP ERRATIC A HEEA O OTHER O OTHER AP APPROACH 1 SW 03 706AE 580 760275 ON APPROACH FOR LANDING, NR 1 ENGINE STARTED TO YAW. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 DCA AMPLIFIER INOPERATIVE AND THE NR 2 DCA AMPLIFIER ERRATIC. REPLACED BOTH. REF: S76 IPC, CHAPTER 76-11-00, FIGURE 1-14, AND FIGU RE 1-16. 1 G 7 2 3U H1NE 1998100200334 19981002 00334 NE 1998 10 2 98ZZZX3607 1 19980827 A 6710 7690001880106 AMPLIFIER SKRSKY S76 S76A 8143006 NE DROOP COMP INOPERATIVE A HEEA O OTHER O OTHER AP APPROACH 1 SW 03 706AE 29 760275 ON APPROACH FOR LANDING, NR 1 ENGINE STARTED TO YAW. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 DCA AMPLIFIER INOPERATIVE AND THE NR 2 DCA AMPLIFIER ERRATIC. REPLACED BOTH. REF: S76 IPC, CHAPTER 76-11-00, FIGURE 1-14, AND FIGU RE 1-16. 1 G 7 2 3U H1NE 1998100200340 19981002 00340 WP 1998 10 2 VJ9800430 1 19980915 A 5321 1A380141 FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 CENTER PANEL UNDER NR 3 GALLEY AT FS 200.0 CORRODED BEYOND LIMIT. TREATED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-30-2 AND 53-01. 2 L 7 2 4F A6WE 1998100200341 19981002 00341 WP 1998 10 2 VJ9800431 1 19980917 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 SEAT TRACK FS 965.091, 889, 852, 794 AND 617 HAVE GOUGES AND SEAT TRACK AT FS 965 CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED NEW SEAT TRACK IAW DC9 SRM51-10-4, 51-10-3, 51-60-0 AND 53-05, FIG 1. 2 L 7 2 4F A6WE 1998100200342 19981002 00342 WP 1998 10 2 VJ9800432 1 19980918 A 5321 FLOOR DOUG DC9 DC932 3022066 WP RT COCKPIT CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 COCKPIT FLOOR PANEL, RT, HAS CORRSION BEYOND LIMIT ON HAT SECTIONS. REMOVED CORRODED SKIN AND HAT SECTIONS. FABRICATED AND INSTALLED NEW FLOOR PANEL SKIN AND HAT SECTIONS IAW DC9 SRM 51-30-2, 51-20-0, 51-10-4, 51-10-3, AND 53-05.. 2 L 7 2 4F A6WE 1998100200343 19981002 00343 WP 1998 10 2 VJ9800433 1 19980925 A 3233 39132445331 ACTUATOR DOUG DC9 DC932 3022066 WP NLG FAILED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 966VV 47168 NOSE GEAR WOULD NOT RETRACT. FERRIED AIRCRAFT FROM IAD TO MAIN MAINTENANCE BASE IN ATL FOR CONVENIENCE. REPLACED NLG A CTUATING CYLINDER IAW MM 32-32-6, PG 204 - 206. LEAK AND OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998100200344 19981002 00344 WP 1998 10 2 VJ9800434 1 19980928 A 3350 6011779 POWER SUPPLY DOUG DC9 DC932 3022066 WP LT NACELLE INOPERATIVE A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 909VJ 47322 IN EMERGENCY POSITION, LH NACELLE LIGHT WON'T WORK. REPLACED BATTERY POWER SUPPLY IAW MM 33-50. 2 L 7 2 4F A6WE 1998100200345 19981002 00345 EA 1998 10 2 COMA9860277 1 19980926 A 2750 BPSU CNDAIR CL600 CL6002B19 EA TE FLAPS OUT OF ADJUST A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 938CA 7046 FLAPS FAILED. ADJUSTED THE RIGHT BPSU RIGGING. 2 L 7 2 4F RT A21EA 1998100200346 19981002 00346 EA 1998 10 2 COMA9860278 1 19980927 A 3230 PIN CNDAIR CL600 CL6002B19 EA NLG NOT REMOVED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 941CA 7050 NLG DID NOT RETRACT. REMOVED DOWN LOCK SAFETY PIN FROM NLG. 2 L 7 2 4F RT A21EA 1998100200347 19981002 00347 EA 1998 10 2 COMA9860279 1 19980916 A 5330 601R31021 SKIN CNDAIR CL600 CL6002B19 EA BS 242.75 GOUGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 17205 7013 FOUND TWO GOUGES IN SKIN AT FUSELAGE AT FUSELAGE STATION 242.75. APPROXIMATELY 7.75 AFT OF NOSE GEAR DOORS. 2 L 7 2 4F RT A21EA 1998100200349 19981002 00349 EA 1998 10 2 COMA9860281 1 19980915 A 5320 6007522144 INTERCOSTAL CNDAIR CL600 CL6002B19 EA FUSELAGE CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 7013 FOUND NR 2 HYDRAULIC SUPPORT BEAM INTERCOSTAL CRACKED. REPLACED INTERCOSTAL. 2 L 7 2 4F RT A21EA 1998100200350 19981002 00350 EA 1998 10 2 COMA9860282 1 19980913 A 5751 HINGE CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 915CA 9629 7013 RIGHT AILERON HAS EXCESSIVE PLAY AT THE HINGE. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998100200351 19981002 00351 EA 1998 10 2 COMA9860283 1 19980921 A 2752 85201009 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 930CA 7147 7046 DURING C-CHECK, FOUND THE LEFT INBOARD FLAP, OUTBOARD ACTUATOR TO HAVE EXCESSIVE PLAY. REPLACED ACTUATOR. 2 L 7 2 4F RT A21EA 1998100200352 19981002 00352 EA 1998 10 2 COMA9860284 1 19980919 A 5320 601R3521017 FRAME CNDAIR CL600 CL6002B19 EA APU INLET DRWAY CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 7046 APU INLET DOOR FRAME IS CRACKED .060 ON FORWARD BOTTOM CORNER. REPLACED FRAME. 2 L 7 2 4F RT A21EA 1998100200353 19981002 00353 NE 1998 10 2 COMA9860285 2 19980920 A 7530 4060781G03 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE RT ENGINE LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 398CA 7046 RIGHT ENGINE B-SUMP REGULATOR VALVE LEAKING. REPLACED VALVE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100200354 19981002 00354 EA 1998 10 2 COMA9860286 1 19980919 A 7830 1217542 FLEX SHAFT CNDAIR CL600 CL6002B19 EA LT TR UNIT LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 938CA 9949 7046 LEFT THRUST REVERSER FLEXSHAFT LEAKING GREASE THROUGH BRADING. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998100200355 19981002 00355 EA 1998 10 2 COMA9860287 1 19980920 A 5210 6006153552 STRIKER CNDAIR CL600 CL6002B19 EA PAX DOOR DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 938CA 7046 PAX DOOR SEAL STRIKER AT FS 310.00 IS DAMAGED. REPAIRED IN ACCORDANCE WITH REO 601R-52-11-008. 2 L 7 2 4F RT A21EA 1998100200356 19981002 00356 NM 1998 10 2 SWAA982071 1 19980910 A 2780 RETRACT MECH BOEING 737 7375H4 138449D NM NR 4 LE SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 507SW 24184 AIR TURNBACK TO PHX, DUE TO NR 4 SLAT FAILED TO RETRACT AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING (LGPAGE 9954 6). REMOVED AND REPLACED FLAP/SLAT MODULE AND FULL EXT SENSOR AS REQ PER BOEING MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998100200357 19981002 00357 NM 1998 10 2 SWAA982072 1 19980910 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 837 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED STR 25L AT BS 837. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200358 19981002 00358 NM 1998 10 2 SWAA982073 1 19980910 A 5320 ANGLE BOEING 737 7373H4 1384600 NM E/E COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND LEFT FWD E1-2 RACK MOUNT CRACKED AT SCREW HOLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200359 19981002 00359 NM 1998 10 2 SWAA982074 1 19980910 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 927-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 927 TO 947, BL0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200360 19981002 00360 NM 1998 10 2 SWAA982075 1 19980910 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 433 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND SKIN CUTOUT FOR NR 2 LRR XMIT ANTENNA CRACKED AT AFT END OF ANTENNA AT BS 433. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200361 19981002 00361 NM 1998 10 2 SWAA982076 1 19980910 A 5320 ANGLE BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND BOTTOM WEB ANGLE CRACKED JUST FWD FROM O/B SIDE AILERON. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200362 19981002 00362 NM 1998 10 2 SWAA982077 1 19980910 A 5712 RIB BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND UPPER I/B, T/E PANEL RIB CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200363 19981002 00363 NM 1998 10 2 SWAA982078 1 19980910 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 250 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL FOR NLG VIEWER CRACKED AT FWD LT SIDE BELOW COCKPIT FLOOR AT BS 250 LBL5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200364 19981002 00364 NM 1998 10 2 SWAA982079 1 19980910 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CLIP NUT HOLES CORRODED AT BS 986-1006, LBL 14. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998100200365 19981002 00365 NM 1998 10 2 SWAA982080 1 19980910 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND ANGLE AT BS 270 CORRODED BENEATH NUT PLATES LBL 10 TO RBL 10. REPAIRED PER TI-A53-02 . 2 L 7 2 4F RT A16WE 1998100200366 19981002 00366 NM 1998 10 2 SWAA982081 1 19980910 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 295 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED BS 295, STR 12 ON INTERCOSTAL WL 244, LBL 55. REPAIRED PER TI-A53-02. 2 L 7 2 4F RT A16WE 1998100200367 19981002 00367 NM 1998 10 2 SWAA982082 1 19980911 A 2913 371380 PUMP BOEING 737 7373H4 1384600 NM A HYD SYST FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 310SW 22949 AIRCRAFT FLT HOU-TUL, DIVERTED INTO DAL DUE TO HYDRAULIC A SYSTEM ENGINE DRIVEN PUMP FAILED IN FLIGHT. REMOVED AND REP LACED ENG DRIVEN HYDRAULIC PUMP PER BOEING MM, LK CHECK AND FUNCTION CHECK GOOD. 2 L 7 2 4F RT A16WE 1998100200368 19981002 00368 NM 1998 10 2 SWAA982083 1 19980911 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND LOWER AIRSTAIR DOOR SILL, FRAME ATTACH BRACKET CRACKED AT BS 328. 2 L 7 2 4F RT A16WE 1998100200369 19981002 00369 NM 1998 10 2 SWAA982084 1 19980911 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHTS INOP AT EMERGENCY EXIT ROW. RECONNECTED WIRING SPLICE PER BOEING M M. 2 L 7 2 4F RT A16WE 1998100200370 19981002 00370 NM 1998 10 2 SWAA982085 1 19980911 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED BS 344 FLOORBEAM LBL 32 TO RBL 10, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200371 19981002 00371 NM 1998 10 2 SWAA982086 1 19980911 A 5320 CHANNEL BOEING 737 7373H4 1384600 NM BS 312-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FWD ENTRY DOOR THRESHOLD SUPPORT CHANNEL AT BS 312 TO 344, LBL 60, WL 208. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200372 19981002 00372 NM 1998 10 2 SWAA982087 1 19980911 A 5320 BEAM BOEING 737 7373H4 1384600 NM BS 940-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED CREASE BEAM (AFT ENTRY DOOR AREA) AT BS 940-986, LBL 45-50 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200373 19981002 00373 NM 1998 10 2 SWAA982088 1 19980911 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 306-346 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED TOP AND BOTTOM OF WEB AROUND FASTENER HOLES AT BS 306-346, LBL 55-60, WL 208 . REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200374 19981002 00374 NM 1998 10 2 SWAA982089 1 19980911 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 328-344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STIFFENER AT BS 328-344, LBL 55-60, WL 208 AROUND FASTENER HOLES. REMOVED A ND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200375 19981002 00375 NM 1998 10 2 SWAA982094 1 19980911 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 350-354 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED WEB AT BS 350- 354, WL 208 TO 223, LBL 63. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200376 19981002 00376 NM 1998 10 2 SWAA982090 1 19980911 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 993 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED AFT LT LAV FWD WALL SUPPORT AT BS 993, LBL 13.5- 40.5, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200377 19981002 00377 NM 1998 10 2 SWAA982091 1 19980911 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED WEB BS 1016, LBL 41, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200378 19981002 00378 NM 1998 10 2 SWAA982092 1 19980911 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM BS 306-615 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED TOP WEB DOUBLER FWD ENTRY DOOR SILL AT BS 306-315, WL 208, LBL 50-60. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200379 19981002 00379 NM 1998 10 2 SWAA982093 1 19980911 A 5512 SKIN BOEING 737 7373H4 1384600 NM HORIZ STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED RT HORIZONTAL STAB O/B END WHERE STAB TIP MOUNTS TO STAB. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200380 19981002 00380 NM 1998 10 2 SWAA982095 1 19980911 A 5551 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED RT HORIZONTAL STAB L/E HAS A DAMAGED RIB AT L/E BS 244.72. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200381 19981002 00381 NM 1998 10 2 SWAA982096 1 19980913 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED RON CHECK, FOUND 4 IN SKIN CRACK, RT SIDE ABOVE AND BETWEEN CABIN WINDOWS 12-13. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998100200382 19981002 00382 NM 1998 10 2 SWAA982097 1 19980913 A 3350 BATTERY PACK BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 510SW 24187 DURING SCHEDULED SERVICE CHECK, FOUND OVER WING RT SIDE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK BA SE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200383 19981002 00383 NM 1998 10 2 SWAA982098 1 19980913 A 3350 LIGHT BOEING 737 7375H4 138449D NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 515SW 25154 DURING SCHEDULED SERVICE CHECK, FOUND LT OVER WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK HOUSING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200384 19981002 00384 1998 10 2 SWAA982099 4 19980914 A 2312 CONNECTOR BOEING 737 7373H4 1384600 NM NR 1 COMM FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 366SW 26577 AIRCRAFT EN ROUTE FROM PHX TO SLC DIVERTED TO LAS DUE TO NR 1 COMM INTERMITTENT REC IN AIR-NO TRANS. IN AIR CLOSE TO ST A ONLY, ON GRND WORKS OK. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED COAX CONNECTOR PER BOEING MM. OP 'S CK GOOD. 2 L 7 2 4F RT A16WE 1998100200385 19981002 00385 NM 1998 10 2 SWAA982100 1 19980914 A 3260 189929 SENSOR BOEING 737 7373T5 NM RT MLG FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 692SW 23062 AIRCRAFT EN ROUTE FROM TPA TO ABQ DIVERTED DUE TO RIGHT LANDING GEAR RED LIGHT FLICKERS ON AND OFF CRUISE. THREE GREEN LIGHTS FOR LANDING. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RT MAIN LANDING GEAR UPLOCK SENSOR. GEAR SWUNG. OPS CHECK GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200386 19981002 00386 NM 1998 10 2 SWAA982101 1 19980915 A 3830 DUMP VALVE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE LAVATORY CONTAMINATED A SWAA E A ENGINE SHUTDOWN UNSCHED LANDING X C ENGINE FLAMEOUT F.O.D. CR CRUISE 1 SW 07 304SW 22944 AIRCRAFT EN ROUTE FROM MCI TO OKC DIVERTED DUE TO INFLIGHT SHUTDOWN NR 2 ENGINE FLAMEOUT AT CRUISE POWER SETTING AT FL 3 10, M.755 (ACTUAL STATION COS). AFTER LANDING INSPECTION REVEALED 3-4 ADDITIONAL DENTS IN L/E RT WING JUST OUTBOARD OF TURNOFF/LANDING LIGHT. SUSPECT FWD LAV STILL LEAKING IN FLIGHT. C/W FOD BORESCOPE INSP PER SAM 451. NO OUT OF LIMIT D EFECTS NOTED. C/W TEST NR 5 POWER ASSURANCE CHECK PER BOEING MM. NO FAULTS NOTED. COCKPIT VOICE RECORDER REMOVED FOR MAINT CONVENIENCE. FOUND DUMP VALVE UNABLE TO SEAL DO TO EXCESSIVE PAPER TOWELS IN LAV TANK. REMOVED DUMP VALVE CLEANE D AND REINSTALLED. REMOVED AND REPLACED FILL VALVE ASSY PER BOEING MM (P/N 16007-045). REPAIRED DENTS PER SRM. 2 L 7 2 4F 4 F RT A16WE E2GL 1998100200387 19981002 00387 NM 1998 10 2 SWAA982102 1 19980914 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY TRACK LIGHTING INOP 5 LIGHTS AT OVERWING EXIT ROW. RECONNECTED WIRING T O LIGHTS. OPS CHECK OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200388 19981002 00388 NM 1998 10 2 SWAA982103 1 19980914 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FLOORBEAM STIFFENER ANGLE CRACKED AT BS 328, RBL 32, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200389 19981002 00389 NM 1998 10 2 SWAA982104 1 19980914 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FWD END OF INTERCOSTAL AT BS 380 LBL 25, W156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200390 19981002 00390 NM 1998 10 2 SWAA982105 1 19980914 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED BULKHEAD WEB AT BS 178, RBL 5, LBL 5, WL 188. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200391 19981002 00391 NM 1998 10 2 SWAA982106 1 19980914 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4 L/T. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200392 19981002 00392 NM 1998 10 2 SWAA982107 1 19980914 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 535.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND WEB SUPPORT ANGLE CRACKED AT BS 535.5, RBL51, WL 175. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200393 19981002 00393 NM 1998 10 2 SWAA982108 1 19980915 A 3350 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY EXIT LIGHT ASSY IN COCKPIT WILL NOT COME ON WHEN EMERGENCY LIGHTS ARE ACTIVA TED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER BOEING MM. 2 L 7 2 4F A16WE 1998100200394 19981002 00394 NM 1998 10 2 SWAA982109 1 19980915 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN BENT AT AFT LOWER CORNER OF LOWER HINGE CUTOUT. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1998100200395 19981002 00395 NM 1998 10 2 SWAA982110 1 19980915 A 5730 SKIN BOEING 737 7372H4 138448C NM WS 169 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED C1 CHECK, FOUND RT WING TOP BS 169 CRACKED APPROX .5 INCH. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200396 19981002 00396 NM 1998 10 2 SWAA982111 1 19980915 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED BS 360 AT STR 11 ON INTERCOSTAL WL 254, LBL 60. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200397 19981002 00397 NM 1998 10 2 SWAA982112 1 19980915 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED SHEAR TIE BETWEEN STRINGER 14 AND 15 AT BS 360, WL 228, LBL 69. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998100200398 19981002 00398 NM 1998 10 2 SWAA982113 1 19980915 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 348.2 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED AT BS 348.2, WL 221, LBL 65. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200399 19981002 00399 NM 1998 10 2 SWAA982114 1 19980915 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FLOOR PANEL TIE STRAP CORRODED AT BS 772, RBL 21 LBL 21 WL 156. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200400 19981002 00400 NM 1998 10 2 SWAA982115 1 19980915 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND BULKHEAD CRACKED AT BS 178, WL 197.5-199.75, LBL 4.7; WL 199-200, LBL 6.7 AND WL 210-221 0.75 LBL 6.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200401 19981002 00401 NM 1998 10 2 SWAA982116 1 19980915 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND BULKHEAD CRACKED AT BS 178, WL 197.5-198, RBL 6.7; WL 210-210.5, RBL 6.7 AND WL 209-210, RBL 4.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200402 19981002 00402 NM 1998 10 2 SWAA982117 1 19980915 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 1121 GOUGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND GOUGE IN SHEAR TIE AT BS 1121, STR 2L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200403 19981002 00403 NM 1998 10 2 SWAA982118 1 19980915 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 727E, LBL 42, WL 166. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200404 19981002 00404 NM 1998 10 2 SWAA982119 1 19980915 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 1088 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED ANGLE ON INTERIOR OF RT TORQUE BOX AT BS 1088 JUST ABOVE CUTOUT FOR APU AIR INLET DUCT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200405 19981002 00405 NM 1998 10 2 SWAA982120 1 19980916 A 5530 STIFFENER BOEING 737 7373H4 1384600 NM VERT STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED STIFFENER ON RT VERTICAL FIN REAR SPAR AT FIN BS 119.0 IN TRAILING EDGE CAVITY. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200406 19981002 00406 NM 1998 10 2 SWAA982121 1 19980916 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR SUPPORT ANGLE AT BS 178, LBL 18 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200407 19981002 00407 NM 1998 10 2 SWAA982122 1 19980916 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED AT BS 178, WL 194-198, RBL 4.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200408 19981002 00408 NM 1998 10 2 SWAA982123 1 19980916 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 727 BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP BENT AT BS 727, STR 26 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200409 19981002 00409 NM 1998 10 2 SWAA982124 1 19980916 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 1143 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER 5 LT LOWER CHORD CRACKED AT BS 1143. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200410 19981002 00410 NM 1998 10 2 SWAA982125 1 19980916 A 5347 TIE DOWN BOEING 737 7373H4 1384600 NM BS 847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED CARGO TIE DOWN STANSIONS AT BS 847, LBL 31-59, WL 174. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200411 19981002 00411 NM 1998 10 2 SWAA982126 1 19980916 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 807 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 807, LBL 48, WL 172. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200412 19981002 00412 NM 1998 10 2 SWAA982127 1 19980916 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 947 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND SUPPORT ANGLE CRACKED AFT SIDE OF FRAME AT BS 947, STR 22 LT.; AND BS 947 AT STR 23 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200413 19981002 00413 NM 1998 10 2 SWAA982128 1 19980916 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR WEB AT BS 178, RBL 25-29, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200414 19981002 00414 NM 1998 10 2 SWAA982129 1 19980916 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED SUPPORT ANGLE AT BS 178, RBL 28 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200415 19981002 00415 NM 1998 10 2 SWAA982130 1 19980916 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 717 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND RT WHEEL WELL ATTACH ANGLE HAS ELONGATED FASTENER HOLES AT BS 717, RBL 20, WL 149. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200416 19981002 00416 NM 1998 10 2 SWAA982131 1 19980916 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STABILIZER STRAP CRACKED AT BS 312, LBL 12, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200417 19981002 00417 NM 1998 10 2 SWAA982132 1 19980916 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM BS 683 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DAMAGED AREA AT BS 683, BETWEEN STR 6R AND STR 7R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200418 19981002 00418 NM 1998 10 2 SWAA982133 1 19980916 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 380 - 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL ATTACH BRACKETS ARE CRACKED AT BS 380 AND BS 400, RBL 25, WL 154. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200419 19981002 00419 NM 1998 10 2 SWAA982134 1 19980916 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL ATTACH BRACKETS ARE CRACKED AT BS 420, RBL 25, WL 154. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200420 19981002 00420 NM 1998 10 2 SWAA982135 1 19980916 A 3020 DUCT BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 96SW 23055 AIR TURNBACK DUE TO ENGINE NR 2 OVERHEAT LIGHT ILLUMINATED ON CLIMB-OUT AT APPX 5000 FT MSL. LIGHT WENT OUT WHEN POWER WAS REDUCED. NO OTHER SUPPORTING INDICATIONS. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED ENGINE NOSE C OWL ANTI-ICE DUCT. OP'S CHECK GOOD PER MM. 2 L 7 2 4F 4 F A16WE E2EA 1998100200421 19981002 00421 NM 1998 10 2 SWAA982136 1 19980917 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 53SW 21593 DURING SCHEDULED C4 CHECK, FOUND INTERCOSTAL CRACKED AT DOOR UPLATCH BRACKET. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F 4 F A16WE E2EA 1998100200423 19981002 00423 NM 1998 10 2 SWAA982138 1 19980917 A 5730 SKIN BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND NR 2 SLAT AT INNER AUX TRACK AREA LOWER SKIN AROUND RIVET CRACKED. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998100200424 19981002 00424 NM 1998 10 2 SWAA982139 1 19980917 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED PRESSURE DECK (FLOORBEAM) AT BS 663, RBL 41.0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200425 19981002 00425 NM 1998 10 2 SWAA982156 1 19980917 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND BS 178 LT CHORD ANGLE CRACKED AT WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200426 19981002 00426 NM 1998 10 2 SWAA982140 1 19980917 A 5230 WEB BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED 1/2D CHECK, FOUND FWD CARGO DOOR WEB CRACKED AT AFT LOWER CORNER SIDE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200427 19981002 00427 NM 1998 10 2 SWAA982141 1 19980917 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 787-854 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED SILL WEB TIE STRAP AT BS 787-854, RBL 19, WL 157. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998100200428 19981002 00428 NM 1998 10 2 SWAA982142 1 19980917 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED CARGO BAY DOOR FRAME AT BS 847, RBL 23-27, WL 163. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998100200429 19981002 00429 NM 1998 10 2 SWAA982143 1 19980917 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 794-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED SILL WEB AT BS 794-847, RBL 19, WL 162. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200430 19981002 00430 NM 1998 10 2 SWAA982144 1 19980917 A 5320 FRAME BOEING 737 7373H4 1384600 NM EMER EXIT DRWAY DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DOOR FRAME COVERPLATE DENTED AND GOUGED AT BS 790-794, RBL 22-36, WL 160. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200431 19981002 00431 NM 1998 10 2 SWAA982145 1 19980917 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED ON CARGO FLOORBEAM AROUND NUTPLATE LOCATIONS AT BS 727-947, LBL 12.5, WL 159. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200432 19981002 00432 NM 1998 10 2 SWAA982146 1 19980917 A 5312 BULKHEAD ANGLE BOEING 737 7373H4 1384600 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 947, LBL 21, RBL 21, WL 180. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200433 19981002 00433 NM 1998 10 2 SWAA982147 1 19980917 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE AT BS 727-947, LBL 3, WL 159. REMOVED AND RELA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200434 19981002 00434 NM 1998 10 2 SWAA982148 1 19980917 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE AT BS 727-947, RBL 3, WL 159. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200435 19981002 00435 NM 1998 10 2 SWAA982149 1 19980917 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE AT BS 727-947, RBL 8, WL 159. REMOVED AND REPL ACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200436 19981002 00436 NM 1998 10 2 SWAA982150 1 19980917 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 327 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD GALLEY DOORWAY AFT LOWER SKIN CUTOUT AT BS 327, WL 210. RE PAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200437 19981002 00437 NM 1998 10 2 SWAA982151 1 19980917 A 5314 KEEL BEAM BOEING 737 7373H4 1384600 NM BS 720-727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CHAFING DAMAGED TO KEELBEAM AT BS 720-727 O/B FLANGE. REPAIRED PER TRAMCO EWO 98-0834 2 L 7 2 4F RT A16WE 1998100200438 19981002 00438 NM 1998 10 2 SWAA982152 1 19980917 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 328, RT STR 20. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200439 19981002 00439 NM 1998 10 2 SWAA982153 1 19980917 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 937 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 937, 3 ABOVE STR 19L, WL 199. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200440 19981002 00440 NM 1998 10 2 SWAA982154 1 19980917 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 847-867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND VERTICAL SUPPORT WEB CORRODED AT BS 847-867, RBL 18, WL 162. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200441 19981002 00441 NM 1998 10 2 SWAA982155 1 19980917 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 767-787 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND VERTICAL SUPPORT WEB CORRODED AT BS 767-787, RBL 21, WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200442 19981002 00442 NM 1998 10 2 SWAA982157 1 19980917 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 927, STR 26 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200443 19981002 00443 NM 1998 10 2 SWAA982158 1 19980917 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 767 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED FRAME AT BS 767, RBL 32, WL 159. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200444 19981002 00444 NM 1998 10 2 SWAA982159 1 19980917 A 5320 BRACKET BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND E1-3 RACK CRACKED AT L BRACKET FRONT AND CENTER. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200445 19981002 00445 NM 1998 10 2 SWAA982160 1 19980917 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 178-180 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED VERTICAL BEAM WEB AT BS 178-180, LBL 5.7, WL 188. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998100200446 19981002 00446 NM 1998 10 2 SWAA982161 1 19980917 A 5320 STIFFENER BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED VERTICAL STIFFENER AT BS 178, LBL 5.7, WL 185. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200447 19981002 00447 NM 1998 10 2 SWAA982162 1 19980918 A 2780 RETRACT MECH BOEING 737 7372H4 138448C NM NR 4 LE SLAT MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 059SW 21811 AIR TURNBACK DUE TO AFTER TAKEOFF WITH FLAPS 5 DEGREES, NR 4 SLAT VISUALLY NOT ALIGNED WITH OTHER SLATS. RETURNED TO DA L, MADE AN UNVENTFUL LANDING. LEFT FLAPS AT POSITION 5 DEGREES. REMOVED AND REPLACED SLAT ACTUATOR (NR4) OPS AND LK CH ECKS OK PER BOEING MM. 2 L 7 2 4F A16WE 1998100200448 19981002 00448 NM 1998 10 2 SWAA982163 1 19980918 A 2130 CHECK VALVE BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 093SW 22965 AIR TURNBACK DUE TO LEAVING TEN THOUSAND FEET (10,000') CABIN CLIMBED AT 1000' FT/MIN TO 9800' CABIN. MAIN OUTFLOW CLOS ED MANUAL A/C NO HELP. AIRCRAFT MADE AN UNVENTFUL LANDING TO TPA. RESECURE CHECK VALVE EXTERNAL AIR CONDITION CONNECT ION. PRESSURIZATION A/C AND OPS CK NORMAL PER BOEING MM. C/W CABIN PRESSURIZATION INSP PER BOEING MM. NO DEFECTS NOTE D. (LP36781) 2 L 7 2 4F A16WE 1998100200449 19981002 00449 NE 1998 10 2 SWAA982164 2 19980920 A 7510 DUCT BOEING 737 7372T4 1384492 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A SWAA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 SW 07 702SW 22054 AIR TURNBACK DUE TO NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF FROM BWI (NOTE ANY EPR SETTING ABOVE 1.75 CAUSE D THE LIGHT TO RE-ILLUMINATE). AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED 13TH STAGE FUEL HEAT DUCTING PER BOEING MM. RAN ENG AT HIGH POWER. NO FAULTS NOTED. PERFORMED INSP PER BOEING MM. NO DAMAGED NOTED. 2 L 7 2 4F 4 F A16WE E2EA 1998100200450 19981002 00450 1998 10 2 SWAA982165 2 19980920 A 7261 OIL SYST BOEING 737 7373Q8 1384670 NM NR 1 ENGINE REQD SERVICE A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 689SW 23387 DIVERSION DUE TO NR 1 ENGINE OIL QUANTITY IS LOW, NEEDS SERVICING. AIRCRAFT MADE AN UNEVENTFUL LANDING. RAN NR 1 ENG. INSPECTED FOR OIL LEAKS, NO LEAKS NOTED. (LP 187371) 2 L 7 2 4F RT A16WE 1998100200451 19981002 00451 NM 1998 10 2 SWAA982166 1 19980918 A 5320 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED INNER SUPPORT ANGLE UNDER WINDOW. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200452 19981002 00452 NM 1998 10 2 SWAA982167 1 19980918 A 5320 BOW TIE BOEING 737 7372H4 138448C NM BS 1156 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND LT BOW TIE WORN AT BS 1156. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200453 19981002 00453 NM 1998 10 2 SWAA982168 1 19980918 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED BETWEEN SKIN AND STRINGER AT BS 967, STR 25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200454 19981002 00454 NM 1998 10 2 SWAA982169 1 19980918 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DRWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT LOWER CORNER OF LOWER HINGE CUTOUT. REPAIRED PER TI-A53-056 . 2 L 7 2 4F A16WE 1998100200455 19981002 00455 NM 1998 10 2 SWAA982170 1 19980918 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED WITH PREVIOUS STOP DRILL AT LOWER CORNER OF LOWER HINGE CUTOUT SKIN AND DOUBLER CRACK 1.5 BEAR STRAP CRACK .5. REPAIRED PER SWA RA 1-253-1888. 2 L 7 2 4F A16WE 1998100200456 19981002 00456 NM 1998 10 2 SWAA982171 1 19980918 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 847-850 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED LOWER TIE STRAP AT BS 847-850, RBL 19, WL 162. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200457 19981002 00457 NM 1998 10 2 SWAA982172 1 19980918 A 5320 FRAME BOEING 737 7373H4 1384600 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED DOOR FRAME COVERPLATE AT BS 492-496, RBL 25-31, WL 158. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200458 19981002 00458 NM 1998 10 2 SWAA982173 1 19980918 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED AROUND NUTPLATE HOLE ON FRAME AT BS 500 RBL 25, WL 157. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200459 19981002 00459 NM 1998 10 2 SWAA982174 1 19980918 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FWD END OF T-ANGLE OF FAIRING SUPPORT IS WORN AT BS 727, RBL 69, WL 183. REMOVED AND RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200460 19981002 00460 NM 1998 10 2 SWAA982175 1 19980918 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED CARGO FLOORBEAM AROUND NUTPLATE LOCATIONS AT BS 727-947, LBL 8, WL 159. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200461 19981002 00461 NM 1998 10 2 SWAA982176 1 19980918 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND 2 DENTS IN FRAME AT BS 827, LBL 24.5 AND LBL 28.5, WL 156. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200462 19981002 00462 NM 1998 10 2 SWAA982177 1 19980918 A 5320 SHIM BOEING 737 7373H4 1384600 NM BS 794.3 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED AFT BAY DOOR ROLLER BLOCK SHIMS AT BS 794.3, RBL 50, WL 165. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200463 19981002 00463 NM 1998 10 2 SWAA982178 1 19980918 A 5313 CLIP BOEING 737 7373H4 1384600 NM BS 420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 420, STR 22 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200464 19981002 00464 NM 1998 10 2 SWAA982179 1 19980918 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND PREVIOUS BLEND OUT SKIN AT BS 500B+29, LBL 14, WL 304. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200465 19981002 00465 NM 1998 10 2 SWAA982180 1 19980919 A 5730 SKIN BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 313SW 23335 DURING SCHEDULED C2 CHECK, FOUND NR 3 CRACK ON UPPER SURFACE OF FIXED L/E NEAR OUTBD END OF NR 2 SLAT. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998100200466 19981002 00466 NM 1998 10 2 SWAA982181 1 19980919 A 5511 6573783 RIB BOEING 737 7373H4 1384600 NM HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 325SW 23689 DURING SCHEDULED C4 CHECK, FOUND LT HORIZ STAB DENTED ON RIB APPROX 3.5 FT FROM INBD ROOT. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998100200467 19981002 00467 NM 1998 10 2 SWAA982182 1 19980919 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP FROM ROW 4-6. RELAMPED TRACK LIGHTS AS PER BOEI NG MM. 2 L 7 2 4F RT A16WE 1998100200468 19981002 00468 NM 1998 10 2 SWAA982183 1 19980919 A 3350 SOCKET BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED SERVICE CHECK, FOUND ROW 18 C OVERHEAD EMERGENCY PATH LIGHT OUT OF SOCKET. REPLACED PATH LIGHT IN SOCK ET PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200469 19981002 00469 NM 1998 10 2 SWAA982184 1 19980919 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 526SW 26568 DURING SCHEDULED SERVICE CHECK, FOUND TWO AFT EMERGENCY FLOOR TRACK LIGHTS ARE INOP. RESECURED WIRES AND OP'S CK'D GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200470 19981002 00470 NM 1998 10 2 SWAA982185 1 19980921 A 5314 KEEL BEAM BOEING 737 7372H4 138448C NM RT MLG WW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND KEELBEAM AFT PANEL IN W/W CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200471 19981002 00471 NM 1998 10 2 SWAA982186 1 19980921 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND LT SIDE CHORD CRACKED AT BS 178, LBL 32, WL 207. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F A16WE 1998100200472 19981002 00472 NM 1998 10 2 SWAA982187 1 19980921 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 227 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED AT BS 227, STRINGER 16 RT MEASURES 3.0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200473 19981002 00473 NM 1998 10 2 SWAA982188 1 19980921 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STR 8 RT AND 9 RT AT BS 747. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200474 19981002 00474 NM 1998 10 2 SWAA982189 1 19980921 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727B CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STR 8 RT AND 9 RT AT BS 727B. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200475 19981002 00475 NM 1998 10 2 SWAA982190 1 19980921 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND LT FRAME DOUBLER CRACKED ON AFT SIDE AT BS 727, STR NR 14, WL 231.5. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998100200476 19981002 00476 NM 1998 10 2 SWAA982191 1 19980921 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND SIDE CHORD CRACKED AT BS 178, LBL 29, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200477 19981002 00477 NM 1998 10 2 SWAA982192 1 19980921 A 5510 TIP BOEING 737 7373H4 1384600 NM HORIZ STAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND LT HORIZ STAB TIP, L/E AROUND SCREW HOLE DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200478 19981002 00478 NM 1998 10 2 SWAA982193 1 19980922 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING WALKAROUND CHECK, FOUND 3 CRACK RT SIDE ABOVE CABIN WINDOW NR 8 JUST FWD OF PATCH. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200479 19981002 00479 NM 1998 10 2 SWAA982194 1 19980922 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 522 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 094SW 23053 DURING WALKAROUND CHECK, FOUND HFEC INDICATIONS OF CRACK AT BS 522. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200480 19981002 00480 NM 1998 10 2 SWAA982195 1 19980922 A 3241 CONNECTOR BOEING 737 7375H4 138449D NM RT ANTISKID LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 527SW 26569 AIR TURNBACK DUE TO ANTI-SKID INOP LIGHT CAME ON DURING CLIMB-OUT. AIRCRAFT MADE AN UNEVENTFUL LANDING. RE-PINNED CONN ECTOR AT RT INBOARD TRANSDUCER PER BOEING MM. OPS CHECK GOOD. (LP 187922) 2 L 7 2 4F RT A16WE 1998100200481 19981002 00481 NM 1998 10 2 UPS98227721 1 19980901 A 5754 RIB BOEING 727 72721C 138400M NM NR 6 LE SLAT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D CRACK AT NR 6 SLAT I/B TRACK O/B RIB. REPAIRED RIB IAW SRM 51-40-2. 2 L 7 3 4F A3WE 1998100200482 19981002 00482 NM 1998 10 2 UPS98227722 1 19980901 A 5755 CASTING BOEING 727 72721C 138400M NM NR 6 SPOILER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D ON FURTHER INVESTIGATION OF NR 6 SPOILER LINKAGE SUPPORT CASTING MIGRATED REWORK SLEEVE REMOVED AND CO RROSION FOUND IN REWORKED AREA. REPLACED SUPPORT CASTING IAW DRAWING NR 65-16216. 2 L 7 3 4F A3WE 1998100200483 19981002 00483 NM 1998 10 2 UPS98227723 1 19980901 A 5751 WEB BOEING 727 72721C 138400M NM LT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D LT OUTBD AILERON FIXED WEIGHT BAY, INBOARD WEB IS CRACKED. REPAIRED IAW SRM 51-30-02. 2 L 7 3 4F A3WE 1998100200484 19981002 00484 NM 1998 10 2 UPS98227724 1 19980901 A 5753 BRACKET BOEING 727 72721C 138400M NM LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D LT OUTBD FLAP OUTBD SUPPORT RAMP STAY ROD REAR SPAR ATTACH BRACKET SUSPECT CRACKED. REPLACED SUPPORT BRACKET IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998100200485 19981002 00485 NM 1998 10 2 UPS98227725 1 19980902 A 5320 BRACKET BOEING 727 72721C 138400M NM CARGO DOORWAY CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D FRAME BS 488 OUTER CHORD ATTACH BRACKET CRACKED AT MAIN CARGO SUPPORT FITTING (FWD SIDE OF FRAME). CA RRIED OUT REPAIR IAW SRM 53-10-4 FIG 11. 2 L 7 3 4F A3WE 1998100200486 19981002 00486 NM 1998 10 2 UPS98227728 1 19980903 A 5730 PANEL BOEING 727 72721C 138400M NM WS 180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D NR 1 FUEL TANK ACCESS PANEL CORRODED (FRONT SPAR) LT WING. REPLACED PANEL IAW 28-11-10. 2 L 7 3 4F A3WE 1998100200487 19981002 00487 NM 1998 10 2 UPS98227729 1 19980903 A 5730 PANEL BOEING 727 72721C 138400M NM WS 491 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D LT WING BOLT ON FUEL TANK ACCESS PANELS ARE CORRODED PANELS NR 15 - NR 19. REPLACED PANELS IAW 28-12- 11. 2 L 7 3 4F A3WE 1998100200488 19981002 00488 NM 1998 10 2 UPS98227730 1 19980911 A 5330 SKIN BOEING 727 72721C 138400M NM FUSELAGE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D WHILE REPLACEING BS 740 LT FITTING SEVERAL HOLES ON FUSELAGE SKIN COMMON TO FITTING FOUND DAMAGED. CA RRIED OUT SKIN SPLICE REPAIR IAW EO 98-27-002 ENGINEERING FILE NR 5330-2071. 2 L 7 3 4F A3WE 1998100200489 19981002 00489 NM 1998 10 2 UPS98227731 1 19980910 A 5531 RIB BOEING 727 72721C 138400M NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D TENSION TIE RIB ATTACH FITTINGS FWD AND AFT VERTICAL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINEERING FILE NR 727-55-0374. 2 L 7 3 4F A3WE 1998100200490 19981002 00490 NM 1998 10 2 UPS98227732 1 19980910 A 5531 RIB BOEING 727 72721C 138400M NM VERT STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE:D TENSION TIE RIB FWD AND AFT VERTICAL HOLES ARE PITTED. REPAIR CARRIED OUT IAW SRS EO 98-27-021 ENGINE ERING FILE NO 727-55-0374. 2 L 7 3 4F A3WE 1998100200491 19981002 00491 NM 1998 10 2 UPS98227737 1 19980924 A 3350 BATTERIES BOEING 727 72730C 1384009 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 919UP 19012 EMER EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES IN BOTH EMER EXIT LIGHT ASSY. OPS NORMAL. 2 L 7 3 4F A3WE 1998100200492 19981002 00492 NM 1998 10 2 UPS98627736 1 19980925 A 2612 FIRE LIGHT BOEING 767 76734AF 1385212 NM NR 2 ENGINE ILLUMINATED A IPXA K NONE N FALSE WARNING DE DESCENT 1 SO 01 312UP 27763 FIRE PROTECTION SYS FAIL LIGHT ILLUM. EICAS MSG FIRE/OVHT SYS DISPLAYED. LP1 MOMENTARILY ON AND OFF FOR ABOUT 30-40 SE CS, THEN ONLY LP2 OCCURRED AT TOP OF DESCENT. NR 2 ENG NR 2 LOOP PREVIOUSLY DEFERED. T/S NR 1 LOOP PER FIM 26-11-00, B ITE CHECK GOOD. INSPECTED LOOPS AND ENG DUCTING NO DEFECTS NOTED WORK PERFORMED BY NON ETOPS QUALIFIED MECH. DEF NR C1 59742. 2 L 7 2 4F RT A1NM 1998100200493 19981002 00493 EU 1998 10 2 QXEA9801363 1 19980927 A 2150 PACK FOKKER F28 F28MK4000 4990810 EU NR 2 MALFUNCTIONED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 498US 11181 BOI - CREW NOTED SMOKE SMELL AND VIBRATION. TURNED NR 2 PACK OFF, SMOKE AND VIBRATION STOPPED. MAINTENANCE PLACED NR 2 PACK ON MEL. 2 L 7 2 4F RT A20EU 1998100200494 19981002 00494 EU 1998 10 2 QXEA9801364 1 19980924 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 PDX - OVERHEAD EXIT LIGHT OUT. MAINTENANCE REMOVED AND REPLACED CIRCUIT BOARD. OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998100200495 19981002 00495 NM 1998 10 2 QXEA9801365 1 19980925 A 3350 MS25231316 BULB DHAV 10005511 DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 840PH 74 SEA- COCKPIT OVERHEAD EMERGENCY LIGHT DOES NOT TEST. RELAMPED LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SE RVICE. 2 H 7 2 4T RT A13NM 1998100200496 19981002 00496 NM 1998 10 2 QXEA9801366 1 19980924 A 5210 SCREW DHAV DHC8 DHC8102 2809003 NM PAX DOOR LOOSE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 816PH 54 SEA- MAIN CABIN DOOR IS DIFFICULT TO OPEN FROM THE INSIDE. IT TAKES A LARGE AMOUNT OF FORCE TO MOVE THE INTERIOR HANDLE INTO THE UP POSITION. INSPECTED THE MAIN CABIN DOOR AND FOUND A SCREW BACKING OUT OF THE AFT DOOR SUPPORT ROD. TIGHTE NED LOOSE SCREW. 2 H 7 2 4T RT A13NM 1998100200497 19981002 00497 WP 1998 10 2 MWEA98970 1 19980922 A 3350 1001191 LIGHT DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 209ME 47730 FORWARD ENTRANCE PORTABLE EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FOWARD ENTRY EMERGENCY FLASHLIGHT. 2 L 7 2 4F A6WE 1998100200498 19981002 00498 WP 1998 10 2 MWEA98971 1 19980922 A 2560 5917689105 COVER DOUG DC9 DC932 3022066 WP PAX DOOR DETACHED A MWEA K NONE O OTHER CR CRUISE 1 GL 31 302ME 47102 FORWARD ENTRY DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998100200499 19981002 00499 WP 1998 10 2 RRXA98431 1 19980114 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1220-1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND FRAME PANEL CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 1220 TO 1260, BL 52R AND WL -9 . REMOVED PANEL, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW DAC DWG 5750725 AND DC-8 SRM 52-2-0 FIGURE 2. 2 L 7 4 4F RT 4A25 1998100200500 19981002 00500 WP 1998 10 2 RRXA98432 1 19980106 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 300-320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND LOWER CARGO DOOR FRAME FITTING CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 300 TO 320, BETWEEN LONGERONS 32 RIGHT AND 34 RIGHT. REMOVED FITTING, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED NEW FIT TING IAW DC-8 SRM 53-2-0 FIGURE 1F. 2 L 7 4 4F RT 4A25 1998100200501 19981002 00501 WP 1998 10 2 RRXA98433 1 19980102 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 879 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 2674U 46062 DURING A MAINTENANCE VISIT, FOUND BATH TUB FITTING AND SPLICE DOUBLER CORRODED BEYOND LIMITS IAW DC-8 SRM, AT STA 879 AN D LONGERON 24 LEFT. REMOVED FITTING, TREATED AREA IAW DC-8 SRM 51-1-8. REINSTALLED FITTING AFTER RE-WORK, FABRICATED A ND INSTALLED NEW SPLICE DOUBLER IAW DC-8 SRM 53-2-0 FIGURE 8. 2 L 7 4 4F RT 4A25 1998100200502 19981002 00502 NM 1998 10 2 VNAA9809021 2 19980925 A 7320 3037603 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 457PS 63514 3048 DURING THE TAXI FOR TAKEOFF, THE CREW NOTED A LEFT ENGINE ELECTRONIC CONTROL UNIT (ECU) FAIL WARNING MESSAGE. THE AIRCR AFT RETURNED TO THE GATE. PSA MAINTENANCE WAS DISPATCHED FROM PIT WITH PARTS TO REPAIR THE AIRCRAFT. MAINTENANCE INSPE CTED AND REPLACED THE LEFT 1.8 SENSOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-21-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100200503 19981002 00503 NM 1998 10 2 RAAA98B2042 1 19980926 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998100200504 19981002 00504 NM 1998 10 2 RAAA98B2043 1 19980926 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 LT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998100200505 19981002 00505 NM 1998 10 2 98FDEA00594 1 19980925 A 7997 WIRE BOEING 727 72722 1384002 NM NR 1 OIL TEMP BROKEN A FDEA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 191FE 19084 ON CLIMBOUT AFTER T/O, OBSERVED NR1 OIL TEMP PEG OUT. IT DID COME TO YELLOW BAND. CYCLED CB WHEN RESET GAUGE PEG AGAIN . ALL OTHER IND NORM. EXECUTED PRECAUTION SHUTDOWN PER RED TAB LAND AND TAXI NORM. FOUND BROKEN WIRE AT CONNECTOR ON TEMP BULB. REPAIRED GROUND WIRE IN CANNON PLUG AND OPS CKS GOOD. 2 L 7 3 4F A3WE 1998100200506 19981002 00506 NM 1998 10 2 DL72W981971 1 19980924 A 5754 651622370 SPAR BOEING 727 727247 138408F NM LE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W BN363 20872 SPAR CRACKED AT ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998100200507 19981002 00507 NM 1998 10 2 DLM88981974 1 19980924 A 3260 TARGET NAS62032H DOUG MD88 MD88 3023688 NM LT MLG OUT OF POSITION A DALA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SO 27 908DL NONE 49539 AFTER GEAR RETRACTION LEFT MAIN GEAR DID NOT INDICATE UP AND LOCKED. FOUND LT MLG RETRACTED POSTION TARGET OUT OF POSIT ION REPOSITIONED AND INSTALLED HARDWARE CKS OK. REF MD 88 IPC 32-30-00-12A ITEM 445, 450 AND 470. 2 L 7 2 4F RT A6WE 1998100200508 19981002 00508 NM 1998 10 2 DL72S981976 1 19980924 A 5755 PANEL BOEING 727 727232 1384082 NM NR 1 SPOILER DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 477DA 20754 FOUND ON A1 LETTER CK, NR 1 SPOILER PANEL DELAMINATED. REPAIRED PER SRM 57-50-6. 2 L 7 3 4F A3WE 1998100200509 19981002 00509 NM 1998 10 2 DLM11981977 1 19980925 A 3350 LIGHT P20700030 DOUG MD11 MD11 3023602 NM CABIN INOPERATIVE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 803DE 48474 JUMPSEAT 2L FWD FLASHLIGHT RED LIGHT NOT FLASHING. REPLACED FLASHLIGHT AND BATTERY. INDICATOR OPS NORMAL. 2 L 7 3 4F RT A22WE 1998100200510 19981002 00510 NM 1998 10 2 DL72W981982 1 19980909 A 5753 652163362 RIB BOEING 727 727247 138408F NM RT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 I/B AFT RIB IS CRACKED AT AFT LWR CORNER. REPAIRED PER MM 57-52-0 FIG 808. 2 L 7 3 4F A3WE 1998100200511 19981002 00511 NM 1998 10 2 DL72W981983 1 19980813 A 5753 652163229 SPAR BOEING 727 727247 138408F NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 AFT SPAR RAIL CRACKED TWO PLACES 35 INCHES FROM I/B END OF FLAP. DAMAGE WAS REPAIRED PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998100200512 19981002 00512 NM 1998 10 2 DL72W981984 1 19980813 A 5753 652163229 SKIN BOEING 727 727247 138408F NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2817W 20873 CRACK IN COVE SKIN 31 INCHES FROM I/B END OF FLAP. DAMAGE REPAIRED PER MM 57-52-0 FIG 809. 2 L 7 3 4F A3WE 1998100200513 19981002 00513 NM 1998 10 2 DLM88981985 1 19980926 A 8011 38322211 STARTER 38322211 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE FAILED A DALA O OTHER Z SIGNIFICANT FAILURE REPORT TX TAXI/GRND HDL 1 SO 27 918DL P794 49583 725423 ON ENG START NR 2 ENG STARTER FAILED. PIECES DAMAGED THE CSD WIRE HARNESS AND PUNCTURED A 3 X 1 HOLE IN THE FWD LOWER C OWLING. REPLACED STARTER AND TEMP REPAIRED COWLING. 2 L 7 2 4F 4 F RT A6WE E9NE 1998100200514 19981002 00514 NM 1998 10 2 DL72S981987 1 19980925 A 5311 FRAME BOEING 727 727232 1384082 NM BS 761 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 A CRACK WAS FOUND IN THE FS 761 RT FRAME DURING ACCOMPLISHMENT OF S/B 727-53-0197. THE CRACK IS TYPICAL OF THAT SHOWN I N SUBJECT S/B AND IS DUE TO FATIGUE. REPAIRED PER ERA 332248-14AD. 2 L 7 3 4F A3WE 1998100200515 19981002 00515 NM 1998 10 2 DLM88981989 1 19980925 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 901DE 53378 A CRACK WAS FOUND ON THE STA 1418 FRAME AT L-2R. CRACK IS COVERED IN S/B 53-184. CRACK WAS DUE TO FATIGUE. REPAIRED P ER ERA 332255-14. 2 L 7 2 4F RT A6WE 1998100200516 19981002 00516 NM 1998 10 2 DL733981991 1 19980926 A 3397 WIRE BOEING 737 737347 1384647 NM CABIN DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 302WA 23182 EMERGENCY TRACK LIGHT WIRE AT SEAT ROW 25DEF FOUND DAMAGED. PERFORMED APPROVED REPAIR PER BOEING STANDARD WIRING MANUAL . SYSTEM OPERATES NORMAL. 2 L 7 2 4F RT A16WE 1998100200517 19981002 00517 NM 1998 10 2 DL72S981992 1 19980926 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 517DA 0474 21433 DURING L/O, FOUND FLOOR TRACK LIGHTS FROM SEAT 27-36 INOP. REPLACED EMERGENCY LIGHTS PWR SUPPLY DAL (P/N 337701962) (S/ N 0474) OFF, (S/N 1881) ON. 2 L 7 3 4F A3WE 1998100200518 19981002 00518 1998 10 2 DLM88981993 4 19980927 A 2330 SWITCH H200792 DOUG MD88 MD88 3023688 NM COCKPIT LOOSE A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 952DL 49883 EN ROUTE, THE FLT CREW REPORTED THEY PUSHED THE P A BUTTON ON THE OVERHEAD AND SPARKS CAME FROM THE SWITCH ASSY. CAPT R ECEIVED A SHOCK. MAINTENANCE FOUND THE SWITCH ASSY LOOSE IN THE PANEL. SYSTEM CHECKED NORMAL AFTER TIGHTENING THE SWIT CH ASSY. 2 L 7 2 4F RT A6WE 1998100200519 19981002 00519 NM 1998 10 2 DL72S981995 1 19980927 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 475DA 20752 LT OVERWING EXIT DOOR(S), EMERGENCY LIGHTS INOP. REPLACED LT OVERWING EXIT DOOR(S) BATTERY PACK, SYSTEM OPS. NORMAL PE R MM. 2 L 7 3 4F A3WE 1998100200520 19981002 00520 NM 1998 10 2 DL72S981998 1 19980925 A 5320 PIN BOEING 727 727232 1384082 NM LEFT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 BORE CORRODED LEFT AFT BTL PIN IS CORRODED. CLEANED CORROSION PER SRM 53-40-1 FIG 4 DAMAGE WITHIN LIMITS OK TO TREAT. T REATED BORE PER PS 900-2-4-1 NO O2. 2 L 7 3 4F A3WE 1998100200521 19981002 00521 NM 1998 10 2 SWAA981421 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND UPPER FLANGE OF FLOORBEAM CORRODED AT PANEL HOLES TOP AND BOTTOM AT BS 312 LBL 15 TO RBL 22. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200522 19981002 00522 NM 1998 10 2 SWAA981422 1 19980721 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294.5-312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED AT FLOOR PANEL HOLES LBL 11 AT BS 294.5 TO 312. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998100200523 19981002 00523 NM 1998 10 2 SWAA981423 1 19980721 A 5240 HINGE BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR HINGE CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200524 19981002 00524 NM 1998 10 2 SWAA981424 1 19980721 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM GALLEY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND FWD LAV FWD BULKHEAD COMPOSITE DAMAGED SEVERAL AREAS. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200525 19981002 00525 NM 1998 10 2 SWAA981425 1 19980721 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 590 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL AT BS 950 POS 25-40L CORRODED AND WORN SCREW HOLES; BS 950 POS 18L-20L AN D BS 947-967 POS 17L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200526 19981002 00526 NM 1998 10 2 SWAA981426 1 19980721 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED TOP OF SHEAR WEB AT BS 1016 RBL 526 WL 208. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998100200527 19981002 00527 NM 1998 10 2 SWAA981427 1 19980721 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORROSION AROUND NUT PLATE HOLE AT BS 986 FLOORBEAM UPPER CHORD LBL 22 WL 208 AND BS 986 .5 LBL 22 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200528 19981002 00528 NM 1998 10 2 SWAA981428 1 19980721 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 328-344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 328 TO 344 LBL 47 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200529 19981002 00529 NM 1998 10 2 SWAA981429 1 19980721 A 5330 SKIN BOEING 737 7373G7 1384595 NM APU DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND APU DOOR FWD HINGE CUTOUT CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200530 19981002 00530 NM 1998 10 2 SWAA981430 1 19980721 A 5320 FRAME BOEING 737 7373G7 1384595 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY SERVICE DOORWAY UPPER FWD STUB FRAME CRACKED AT NR 1 STOP FITTING. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200531 19981002 00531 NM 1998 10 2 SWAA981431 1 19980721 A 5315 FLOORBEAM BOEING 737 737317 138447P NM BS 794-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT RBL 13 BETWEEN BS 794 AND BS 847 AROUND MANY FASTENER LOCATION S. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200532 19981002 00532 NM 1998 10 2 SWAA981432 1 19980721 A 5414 SKIN BOEING 737 737317 138447P NM NR 2 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT RBL 13 BETWEEN BS 794 AND BS 847 AROUND MANY FASTENER LOCATION S. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200533 19981002 00533 NM 1998 10 2 SWAA981433 1 19980721 A 5313 STRINGER BOEING 737 737317 138447P NM BS 844 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 26R AT BS 844 CORRODED AROUND HI-LOK. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200534 19981002 00534 NM 1998 10 2 SWAA981434 1 19980721 A 5313 STRINGER BOEING 737 737317 138447P NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 27L CORRODED BETWEEN BS 500C + 500D. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200535 19981002 00535 NM 1998 10 2 SWAA981435 1 19980721 A 3350 BATTERY PACK BOEING 737 737317 138447P NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT HAND CENTER EMERGENCY LIGHTS BATTERY PACK WILL NOT CHARGE. REMOVED AND REPLAC ED BATTERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200536 19981002 00536 NM 1998 10 2 SWAA981436 1 19980721 A 5315 FLOORBEAM BOEING 737 737317 138447P NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D CHECK, FOUND CRACKED FLOORBEAM AT TIE DOWN BS 787 RBL 14. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200537 19981002 00537 NM 1998 10 2 SWAA981437 1 19980721 A 3350 LIGHT BOEING 737 737317 138447P NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 698SW 23176 DURING SCHEDULED 1/2 D CHECK, FOUND 7 ABC BULLNOSE EGRESS LIGHT LOOSE. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200538 19981002 00538 NM 1998 10 2 SWAA981438 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 9475 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D CHECK, FOUND CORROSION IN AND AROUND SCREW HOLES AT FLOORBEAM BS 947.5 RBL 3 TO NR 3 SEAT TRACK. REPAIRED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200539 19981002 00539 NM 1998 10 2 SWAA981439 1 19980721 A 3350 513330124 LIGHT BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D CHECK, FOUND EMERGENCY LIGHT LENSE OVER AFT ENTRY DOOR BROKEN. REMOVED AND REPLACED PER BOEING M M. 2 L 7 2 4F RT A16WE 1998100200540 19981002 00540 NM 1998 10 2 SWAA981440 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 827-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOORBEAM AT BS 827-847 RBL 14. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200541 19981002 00541 NM 1998 10 2 SWAA981441 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 837 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D CHECK, FOUND CORRODED FLOORBEAM AT BS 837 STR 25L LBL 22. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200542 19981002 00542 NM 1998 10 2 SWAA981442 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 844 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND HOLE IN FLOORBEAM AT BS 844 RBL 8 AND AT BS 844 RBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200543 19981002 00543 NM 1998 10 2 SWAA981443 1 19980721 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED WEB AFT OF DOOR CUTOUT AT BS 847 RBL 25. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998100200544 19981002 00544 NM 1998 10 2 SWAA981444 1 19980721 A 5320 ANGLE BOEING 737 7373H4 1384600 NM GALLEY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACKED ANGLE BELOW TORQUE BOX FWD I/B CORNER. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200545 19981002 00545 NM 1998 10 2 SWAA981445 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 747-772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED FLOORBEAM AT BS 772 RBL 12, BS 774 RBL 3 AND BS 747-767 RBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200546 19981002 00546 NM 1998 10 2 SWAA981446 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 792-827 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM EXFOLIATED BETWEEN AT BS 792 TO 827. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200547 19981002 00547 NM 1998 10 2 SWAA981448 1 19980721 A 5347 TIEDOWN BOEING 737 7373H4 1384600 NM CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWN AT BS 787 RBL 14, BS 792 TO 847 RBL 21 AND BS 792 RBL 14. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200548 19981002 00548 NM 1998 10 2 SWAA981449 1 19980721 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 794-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED SURFACE WEB FROM BS 794 TO 847 RBL 25. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998100200549 19981002 00549 NM 1998 10 2 SWAA981450 1 19980721 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 794-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED STRINGER 25L BS 787 TO 791. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200550 19981002 00550 NM 1998 10 2 SWAA981451 1 19980721 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND HOLE IN FLOORBEAM AT BS 907 RBL 8. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200551 19981002 00551 NM 1998 10 2 SWAA981452 1 19980721 A 5347 TIE DOWN BOEING 737 7373H4 1384600 NM BS 867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED HOLE IN CARGO TIE DOWN AT BS 867 RBL 14. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998100200552 19981002 00552 NM 1998 10 2 SWAA981453 1 19980721 A 5313 STRINGER BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED STRINGER 25L AT BS 850 LBL 23, BS 871, BS 864 AND STR 28L BS 503. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200553 19981002 00553 NM 1998 10 2 SWAA981454 1 19980721 A 5312 BULKHEAD PANEL BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND BULKHEAD PANEL AT BS 380 RT SIDE GOUGED AND CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200554 19981002 00554 NM 1998 10 2 SWAA981455 1 19980721 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 294-305 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND SUPPORT ANGLE ON STRINGER 11L CRACKED AT BS 294 TO 305. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200555 19981002 00555 NM 1998 10 2 SWAA981456 1 19980721 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2 D-CHECK, FOUND WEB UPPER ANGLE CRACKED AT BS 380 TO 400 BL 0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200556 19981002 00556 NM 1998 10 2 SWAA981457 1 19980721 A 2560 SLIDE BOEING 737 7375H4 138449D NM PAX DOOR DETACHED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED BC4 CHECK, FOUND SLIDE WAS PULLED OUT OF DOOR BY OPS AGENT. RESECURED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200557 19981002 00557 NM 1998 10 2 SWAA981458 1 19980721 A 5347 TIE DOWN BOEING 737 7373H4 1384600 NM BS 854 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 25175 DURING SCHEDULED 1/2 D-CHECK, FOUND CORRODED CARGO TIE DOWN AT BS 854 RBL 14. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200558 19981002 00558 NM 1998 10 2 SWAA981459 1 19980721 A 3350 BATTERY PACK BOEING 737 7373A4 1384585 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 677SW 23289 DURING SCHEDULED RON CHECK, FOUND FWD EMERGENCY EGRESS LIGHTS INOP. RESEATED FWD BATTERY PACK AND OPS CK OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200559 19981002 00559 NM 1998 10 2 SWAA981460 1 19980721 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 704SW 22056 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHT COULD NOT BE TURNED OFF WITH THE SWITCH IN THE AFT POSITION. THE ONLY POSITION THE LIGHTS COULD BE TURNED OFF WAS IN THE ARMED POSITION WITH OR WITHOUT GROUND POWER OR APU POWER ON THE A/C. PERFORMED OPS CK OF EMERGENCY LIGHTS SYS SEVERAL TIMES, OPS CK OK PER BOEING MM. 2 L 7 2 4F A16WE 1998100200560 19981002 00560 NM 1998 10 2 SWAA981461 1 19980721 A 5330 SKIN BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 632SW 27707 DURING SCHEDULED SERVICE CHECK, FOUND FWD GALLEY DOOR UPPER HINGE FRAME CUTOUT CASTING CRACKED. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200561 19981002 00561 NM 1998 10 2 SWAA981462 1 19980722 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 887 STR 9L, BS 847 STR 9L AND BS 827 STR 9L. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998100200562 19981002 00562 NM 1998 10 2 SWAA981463 1 19980722 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 940-949 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN IS GOUGED AND DENTED FROM BS 995 TO 1005 BETWEEN STRINGER 3L AND 4L AND BS 940 TO 949, 2 INCHES BELOW STR 13L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200563 19981002 00563 NM 1998 10 2 SWAA981464 1 19980722 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 757 LIGHTNING STRIKE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE FUSELAGE SKIN AT BS 757 AT STR 10R AND AT BS ON LOWER ROW OF FASTENERS OF STR 4R LAP. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200564 19981002 00564 NM 1998 10 2 SWAA981465 1 19980722 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 887/807/727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 887 STR 9R, BS 807 STR 9R AND BS 727E STR 9R. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998100200565 19981002 00565 NM 1998 10 2 SWAA981466 1 19980722 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 973 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 973 RBL 50 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200566 19981002 00566 NM 1998 10 2 SWAA981467 1 19980722 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 1016-1033 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AND HAVE ELONGATED FASTENER HOLES AT BS 1016 TO 1033 RBL 940 WL 210. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200567 19981002 00567 NM 1998 10 2 SWAA981468 1 19980722 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 904 LIGHTNING STRIKE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND LIGHTNING STRIKE ON FUSELAGE SKIN AT BS 904 STR 15L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200568 19981002 00568 NM 1998 10 2 SWAA981469 1 19980722 A 5720 BEAM BOEING 737 7373G7 1384595 NM WINGS CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED RT MAIN LANDING GEAR BEAM FITTING. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200569 19981002 00569 NM 1998 10 2 SWAA981470 1 19980721 A 2131 CONTROLLER BOEING 737 7373H4 1384600 NM CABIN MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 638SW 27711 AIR TURNBACK PRESSURIZATION FAIL IN AUTO. AC MADE AN UNEVENTFUL LANDING. PERFORMED BITE TEST ON BOTH LT AND RT PRESS C ONTROLLERS PER BOEING MM, SYSTEM OPS NORMAL. NO FAULTS NO LEAKS FOUND. 2 L 7 2 4F RT A16WE 1998100200570 19981002 00570 NM 1998 10 2 SWAA981471 1 19980724 A 7933 162BL802A TEMP GAUGE BOEING 737 7372H4 138448C NM NR 1 MALFUNCTIONED A SWAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SW 07 050SW 21447 INFLIGHT SHUTDOWN HIGH OIL TEMP ON NR 1 ENG. CHECKLIST ACCOMPLISHED TEMP WOULD NOT DECREASE. ENG SHUTDOWN LANDING MODE . AC MADE AN UNEVENTFUL LANDING. VERIFIED NR 1 OIL TEMP GAUGE ERRATIC. REMOVED AND REPLACED NR 1 OIL TEMP GAUGE AND N R 1 TEMP BULB PER BOEING MM RAN ENGINES AT T/O POWER, ALL SYSTEMS CHECKED GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998100200571 19981002 00571 NM 1998 10 2 SWAA981472 1 19980724 A 2700 FLIGHT CONTROLS BOEING 737 7373H4 1384600 NM WING/EMPENNAGE SHIMMY A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 312SW 23334 AIR RETURN, ON CLIMBOUT A/C STARTED TO SHAKE/SHIMMY AT 160-180 KTS. FLAPS DOWN. AT 210-250 KTS CLIMBING CONTINUE SHAKE /SHIMMY LEVEL FLIGHT (10K) 230-250 KTS NOT AS BAD DURING DESCENT. CLEAN 230-210 KTS, SHAKING NOT AS BAD AS LEVEL FLT. F LAPS 5 GEAR DOWN 170 KTS. PRONOUNCED SHAKE/SHIMMY (NOT FISHTAIL). INSPECTED ALL FLIGHT CONTROLS, LANDING GEAR DOORS AN D ENGINES RAN ENGINES AT TAKEOFF POWER. ISOLATED FOUND NO FAULTS ON INSPEC AND TEST FLIGHT REVEALED NO PROBLEMS PER BOE ING MM. 2 L 7 2 4F RT A16WE 1998100200572 19981002 00572 NM 1998 10 2 SWAA981473 1 19980727 A 2612 FIRE WARNING BOEING 737 7372H4 138448C NM APU ACTIVATED A SWAA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 07 053SW 21534 AIR RETURN DUE TO FALSE APU FIRE WARNING BOTTLE WAS FIRED. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED APU AREA AND NO EVIDENCE OF FIRE FOUND. DEFERRED DETECTION AND EXTINGUISHING SYSTEMS PER BOEING MM. 2 L 7 2 4F A16WE 1998100200573 19981002 00573 NM 1998 10 2 SWAA981474 1 19980723 A 3350 S417N50915 LIGHT BOEING 737 7375H4 138449D NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT NEAR SEAT 12C IS RIPPED OUT. ALL OTHER LIGHTS WORK NORMALLY. INSTALLED TRACK LIGHTING ASSY PER BOEING MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998100200574 19981002 00574 NM 1998 10 2 SWAA981475 1 19980723 A 5530 ANGLE BOEING 737 7372H4 138448C NM VERT STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED 1/4 D-CHECK, FOUND ANGLE CRACKED AT BS 1128 TOP HALF OF STAB LT SIDE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200575 19981002 00575 NM 1998 10 2 SWAA981477 1 19980723 A 5712 RIB BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C4 CHECK, FOUND CRACKED I/B AFT UPPER WING PANEL STUB RIB. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200576 19981002 00576 NM 1998 10 2 SWAA981478 1 19980723 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C4 CHECK, FOUND EMERGENCY EGRESS LIGHT AT FWD ENTRY DOORWAY BROKEN. REMOVED AND REPLACED EMERGENCY EXI T LIGHT AS PER BOEING MM, OPS CHECK OK. 2 L 7 2 4F A16WE 1998100200577 19981002 00577 NM 1998 10 2 SWAA981476 1 19980723 A 5320 GRILLE BOEING 737 7373H4 1384600 NM CARGO COMPT BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED C2 CHECK, FOUND FWD CARGO AFT BULKHEAD BLOWOUT GRILLE BROKEN. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200578 19981002 00578 NM 1998 10 2 SWAA981479 1 19980723 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 947 GOUGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED C2 CHECK, FOUND GOUGE IN FUSELAGE SKIN AT BS 947L, 1 FT BELOW DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200579 19981002 00579 NM 1998 10 2 SWAA981480 1 19980723 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 947 GOUGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 347SW 24374 DURING SCHEDULED C2 CHECK, FOUND GOUGE IN FUSELAGE SKIN AT BS 947L 1 FT BELOW DOOR CUTOUT AND AT BS 983L 2 FT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200580 19981002 00580 NM 1998 10 2 SWAA981481 1 19980723 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND RT OVERWING EMERGENCY LIGHT BATTERY PACK IS BAD. REMOVED AND REPLACED BATTERY PAC K PER BOEING MM, OPS CHECK GOOD. 2 L 7 2 4F A16WE 1998100200581 19981002 00581 NM 1998 10 2 SWAA981482 1 19980723 A 5320 SHEAR TIE BOEING 737 737301 1384611 NM BS 1006 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND CRACKED SHEAR TIE AT BS 1006 LBL 6 TO LBL 8 AFT BAY BETWEEN STR 27 RT AND 27 LT. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200582 19981002 00582 NM 1998 10 2 SWAA981483 1 19980723 A 5330 SKIN BOEING 737 737301 1384611 NM BS 1032 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND EXTERNAL FUSELAGE SKIN GOUGED AT BS 1032 STR 9L. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998100200583 19981002 00583 NM 1998 10 2 SWAA981484 1 19980723 A 5311 FRAME BOEING 737 737301 1384611 NM BS 1006 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND DAMAGE AT FASTENER HOLES ON BS 1006 FRAME BL 0 BETWEEN STR 27L TO 27R. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200584 19981002 00584 NM 1998 10 2 SWAA981485 1 19980723 A 5512 SKIN BOEING 737 737301 1384611 NM HORIZ STAB DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND DELAMINATED RT HORIZ STAB UPPER SURFACE O/B T/E PANEL. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998100200585 19981002 00585 NM 1998 10 2 SWAA981486 1 19980723 A 5320 CLIP BOEING 737 737301 1384611 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND FRAME WITH 2 CLIPS ELONGATED HOLES LBL 20 AND 26. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998100200586 19981002 00586 NM 1998 10 2 SWAA981487 1 19980723 A 5311 FRAME BOEING 737 7373G7 1384595 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 328 RBL 58 WL 184. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200587 19981002 00587 NM 1998 10 2 SWAA981488 1 19980723 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 330 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 330 BETWEEN STR 21R AND 22R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200588 19981002 00588 NM 1998 10 2 SWAA981489 1 19980723 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 312328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 312 TO 328 LBL 12 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200589 19981002 00589 NM 1998 10 2 SWAA981490 1 19980723 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 207-208 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 344 LBL 25 RBL 11 WL 207-208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200590 19981002 00590 NM 1998 10 2 SWAA981491 1 19980723 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 344-360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 344 TO 360 LBL 1 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200591 19981002 00591 NM 1998 10 2 SWAA981492 1 19980723 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM STIFFENER AT BS 294.5 RBL 4653 WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200592 19981002 00592 NM 1998 10 2 SWAA981493 1 19980723 A 5320 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FWD FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON LT SIDE. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998100200593 19981002 00593 NM 1998 10 2 SWAA981494 1 19980723 A 5320 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND AFT FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON LT SIDE. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998100200594 19981002 00594 NM 1998 10 2 SWAA981495 1 19980723 A 5320 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FWD FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON RT SIDE. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998100200595 19981002 00595 NM 1998 10 2 SWAA981496 1 19980723 A 5320 ANGLE BOEING 737 7373G7 1384595 NM FUSELAGE DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND AFT FUSELAGE TO VERTICAL FIN SKATE ANGLE HAS CHAFING DAMAGE ON RT SIDE. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998100200596 19981002 00596 NM 1998 10 2 SWAA981497 1 19980724 A 5320 CHANNEL BOEING 737 7372H4 138448C NM E/E COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED 1/4 D-CHECK, FOUND E1-1 RACK R/T U-CHANNEL CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200597 19981002 00597 NM 1998 10 2 SWAA981498 1 19980724 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 325 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 054SW 21535 DURING SCHEDULED 1/4 D-CHECK, FOUND E1-3 RACK HAS A CLIP CRACKED AT LOWER SUPPORT BRACKET AT BS 325 LBL 6. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200598 19981002 00598 NM 1998 10 2 SWAA981499 1 19980724 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS AND OVERHEAD LIGHT INOP. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200599 19981002 00599 1998 10 2 SWAA981500 4 19980724 A 2565 SLIDE BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING WALKAROUND CHECK, FOUND AFT ENTRY ESCAPE SLIDE GAUGE UNABLE TO READ. REMOVED AND REPLACED SLIDE PACK PER BOEING MM. PRESS READ NORMAL. 2 L 7 2 4F A16WE 1998100200600 19981002 00600 NM 1998 10 2 SWAA981501 1 19980724 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 653SW 27723 DURING SCHEDULED C4 CHECK, FOUND EXPOSED FLOOR TRACK LIGHT WIRING AT ROWS 19 AND 211. REMOVED AND REPLACED FLOOR TRACK COVERS AS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200601 19981002 00601 NM 1998 10 2 SWAA981502 1 19980724 A 5512 SKIN BOEING 737 7373G7 1384595 NM HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND DENTED RIGHT HORIZONTAL REMOVABLE L/E AT BS 124.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200602 19981002 00602 NM 1998 10 2 SWAA981503 1 19980724 A 7830 WEB BOEING 737 7372H4 138448C NM NR 1 ENGINE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C2 CHECK, FOUND CRACKED TR DOGHOUSE FRONT WEB AREA AT TOP. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200603 19981002 00603 NM 1998 10 2 SWAA981504 1 19980724 A 5330 SKIN BOEING 737 737301 1384611 NM WINGS GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED TRAN CHECK, FOUND L/E GAUGED AT NR 4 SLAT TAI CUTOUT. REPAIRED INTERNAL AND EXTERNAL SURFACES PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998100200604 19981002 00604 NM 1998 10 2 SWAA981505 1 19980725 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 064SW 22062 DURING WALKAROUND CHECK, FOUND EXIT LIGHT ABOVE FWD SERVICE DOOR LOOSE AND ILLUMINATES FREQUENTLY. REPOSITIONED LIGHT A SSY INTO LOCKS OF LIGHT ASSY HOUSING AS PER BOEING MM. 2 L 7 2 4F A16WE 1998100200605 19981002 00605 NM 1998 10 2 SWAA981506 1 19980725 A 5414 SKIN BOEING 737 7372H4 138448C NM NR 1 PYLON DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING WALKAROUND CHECK, FOUND DENTED NR 1 ENG PYLON, AFT I/B END OF APPROX SIZE 7 X 250 DEEP FLANGE BENT AND RIVET PULL ED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200606 19981002 00606 NM 1998 10 2 SWAA981507 1 19980725 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600SW 27694 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHT COVERS ON FLOOR (EGRESS) AT ROW 16 THRU 18 ARE OFF. TRACKS ARE TEMP ORARY INSTALLED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200607 19981002 00607 NM 1998 10 2 SWAA981508 1 19980725 A 5312 BULKHEAD WEB BOEING 737 7373G7 1384595 NM BS 178 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND DAMAGED AT BS 178 BULKHEAD WEB LBL 50 WL 200-201 AND 197-198. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200608 19981002 00608 NM 1998 10 2 SWAA981509 1 19980725 A 5312 BULKHEAD WEB BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED INDICATIONS AT BS 178 BULKHEAD WEB RBL 5.0 WL 197-198 AND 200-201 AND WL 198-198 .5 RBL 67. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200609 19981002 00609 NM 1998 10 2 SWAA981510 1 19980725 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 794--847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED THRESHOLD WEB AT BS 794-847 RBL 25 WL 157. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200610 19981002 00610 NM 1998 10 2 SWAA981512 1 19980725 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 9432 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND DENTED FUSELAGE SKIN AT BS 943, 2 INCHES BELOW STR 22R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200611 19981002 00611 NM 1998 10 2 SWAA981513 1 19980725 A 5320 CHORD BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACK ON RT SIDE CHORD AT BS 178 WL 207 AND LT SIDE CHORD AT BS 178 WL 207. REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200612 19981002 00612 NM 1998 10 2 SWAA981514 1 19980725 A 5320 PLATE BOEING 737 7373G7 1384595 NM BS 791 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACK ON ANCHORD PLATE AT BS 791 LBL 40 WL 167 AND LBL 48 WL 172. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998100200613 19981002 00613 NM 1998 10 2 SWAA981515 1 19980725 A 5320 STRAP BOEING 737 7373G7 1384595 NM BS 790-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED STRAP AT BS 790 TO 847 RBL 20 WL 157. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200614 19981002 00614 NM 1998 10 2 SWAA981516 1 19980726 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING SERVICE CHECK, FOUND FWD B EMERGENCY TRACK LIGHT OUT. REMOVED AND REPLACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F A16WE 1998100200615 19981002 00615 NM 1998 10 2 SWAA981517 1 19980726 A 5400 CHORD BOEING 737 7373H4 1384600 NM PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22942 DURING SCHEDULED BC1 CHECK, FOUND OUTBOARD PYLON CHORD CRACKED AT NAC BS 319. REPAIRED PER SWA RA NR 1-354-192. 2 L 7 2 4F RT A16WE 1998100200616 19981002 00616 NM 1998 10 2 SWAA981518 1 19980726 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED BC1 CHECK, FOUND BULLNOSE EMERG LIGHT NOT SECURE AT 21 ABC AND 7 ABC. RESECURED EMERG LIGHT ASSY PER B OEING MM. 2 L 7 2 4F RT A16WE 1998100200617 19981002 00617 NM 1998 10 2 SWAA981511 1 19980726 A 5754 ANGLE BOEING 737 7373H4 1384600 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED BC1 CHECK, FOUND NR 6 LE SLAT ACTUATOR DOOR FWD SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED PER BOE ING MM. 2 L 7 2 4F RT A16WE 1998100200618 19981002 00618 NM 1998 10 2 SWAA981519 1 19980726 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 328 & 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 25251 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AROUND CLIP NUT HOLE AT BS 328 RBL 49 FWD LEG AND BS 986 LBL 35 FWD LEG. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200619 19981002 00619 NM 1998 10 2 SWAA981522 1 19980726 A 2910 LINE BOEING 737 7375H4 138449D NM EMERG BRAKE CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 512SW 24189 DURING SERVICE CHECK, FOUND FWD EMERGENCY BRAKE HYD LINE CHAFED. REMOVED AND REPLACED FWD EMERGENCY BRAKE HYD LINE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998100200620 19981002 00620 NM 1998 10 2 SWAA981523 1 19980727 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 064SW 22062 DURING WALKAROUND CHECK, FOUND LT AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT P ER BOEING MM. 2 L 7 2 4F A16WE 1998100200621 19981002 00621 NM 1998 10 2 SWAA981524 1 19980727 A 5330 SKIN BOEING 737 7372T4 1384492 NM BS 722 & 792 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722SW 22698 DURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 722 AND BS 792 APPROX 21 INCH LENGTH ABOVE STR 17L. REPAIR ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200622 19981002 00622 NM 1998 10 2 SWAA981525 1 19980727 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 947-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2D CHECK, FOUND LT Z ANGLE CORRODED IN SEVERAL PLACES FROM BS 947 TO 1006. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200623 19981002 00623 NM 1998 10 2 SWAA981526 1 19980727 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 947-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2D CHECK, FOUND RT Z ANGLE CORRODED IN SEVERAL SPOTS FROM BS 947 TO 1006. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200624 19981002 00624 NM 1998 10 2 SWAA981527 1 19980727 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 26580 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED SCREW HOLE ON FLOORBEAM AT BS 986 JUST INSIDE DOOR. REPAIRED PER BOEING TI- A53-014. 2 L 7 2 4F RT A16WE 1998100200625 19981002 00625 NM 1998 10 2 SWAA981528 1 19980727 A 5320 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 369SW 23752 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FWD LOWER CORNER OF DOOR FRAME. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200626 19981002 00626 NM 1998 10 2 SWAA981529 1 19980727 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 767-797 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION ON RT TRANSITION ANGLE FROM BS 767 TO 797 RBL 21. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200627 19981002 00627 NM 1998 10 2 SWAA981530 1 19980727 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 847-867 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND DENTED INTERCOSTAL AT BS 847 TO 867 LBL 30 WL 163. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200628 19981002 00628 NM 1998 10 2 SWAA981531 1 19980727 A 5347 TRACK BOEING 737 7373G7 1384595 NM BS 851 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND GOUGED CARGO TRACK AT ANCHORD POINT AT BS 851 LBL 17 WL 116. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998100200629 19981002 00629 NM 1998 10 2 SWAA981532 1 19980727 A 5330 SKIN BOEING 737 7373G7 1384595 NM BS 854 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND DENTED AT BS 854 STR 21R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200630 19981002 00630 NM 1998 10 2 SWAA981533 1 19980727 A 5314 KEELBEAM BOEING 737 7373G7 1384595 NM BS 854 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND WORKING FASTENER DAMAGED BS 720 RBL 7 OF HORIZONTAL FLANGE ON KEEL BEAM. REPAIRED PER T RAMCO ER NR 980626. 2 L 7 2 4F RT A16WE 1998100200631 19981002 00631 NM 1998 10 2 SWAA981534 1 19980727 A 5320 CLIP BOEING 737 7373G7 1384595 NM BS 400 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND STRINGER CLIP DAMAGED AT BS 400 RBL 65 AND BS 500D STR 19 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200632 19981002 00632 NM 1998 10 2 SWAA981535 1 19980727 A 5320 BEAM BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED CREASE BEAM AT BS 178 WL 207 RBL 29. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200633 19981002 00633 NM 1998 10 2 SWAA981536 1 19980727 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 178 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND ACCESS HOLE AT BS 178 WL 198.7 LBL 21. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200634 19981002 00634 NM 1998 10 2 SWAA981537 1 19980727 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 2865 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 286.5 AND BS 1006 LBL 36. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200635 19981002 00635 NM 1998 10 2 SWAA981538 1 19980727 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 967-986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 967 AND 986.5 RBL 18. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200636 19981002 00636 NM 1998 10 2 SWAA981539 1 19980727 A 5320 WEB BOEING 737 7373G7 1384595 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FLOOR WEB AT BS 178 WL 207 LBL 25-29 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200637 19981002 00637 NM 1998 10 2 SWAA981540 1 19980727 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED BETWEEN BS 986.5 AND 1006 BL 0 AND BETWEEN BS 967 AND 986.5 LBL 17. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200638 19981002 00638 NM 1998 10 2 SWAA981541 1 19980727 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 1114-1124 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED APU AIR INLET OPENING UPPER STRINGER AT BS 1114 TO 1124 WL 252 RBL 12. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200639 19981002 00639 NM 1998 10 2 SWAA981542 1 19980727 A 5312 BULKHEAD WEB BOEING 737 7373G7 1384595 NM BS 178 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND ELONGATED FASTENER HOLE IN WEB AT BS 178 BULKHEAD WL 184 TO 240 RBL 1736. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200640 19981002 00640 NM 1998 10 2 SWAA981543 1 19980727 A 5320 FRAME BOEING 737 7373G7 1384595 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND AFT CARGO BAY FWD DOOR FRAME COVER WEB DAMAGED AT BS 794 WL 154. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200641 19981002 00641 NM 1998 10 2 SWAA981544 1 19980727 A 5313 STRINGER BOEING 737 7373G7 1384595 NM BS 1118 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND APU INLET AIR DUCT AT LOWER TORQUE BOX CORRODED AT BS 1118 RBL 19 WL 238 ON STRINGER. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200642 19981002 00642 NM 1998 10 2 SWAA981545 1 19980727 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 615-640 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED SHEAR TIE WEB AT BS 615 STR 15R AND BS 640 STR 15R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200643 19981002 00643 NM 1998 10 2 SWAA981546 1 19980727 A 5320 TIE CLIP BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED TIE CLIP AT BS 663 STR 10L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200644 19981002 00644 NM 1998 10 2 SWAA981549 1 19980727 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 986.5-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CORRODED TOP AND BOTTOM SURFACE BETWEEN BS 986.5 AND 1006 LBL 15. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200645 19981002 00645 NM 1998 10 2 SWAA981551 1 19980730 A 3397 WIRE BOEING 737 7372T4 1384492 NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 702SW 22054 DURING SCHEDULED C1 CHECK, FOUND FLOOR TRACK EGRESS LIGHT STRIP HAS EXPOSED WIRING 9D. REMOVED AND REPLACED TRACK COVER AS PER BOEING MM. 2 L 7 2 4F A16WE 1998100200646 19981002 00646 NM 1998 10 2 SWAA981552 1 19980729 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 328 LBL 47 WL 200-207 (AFT SIDE OF FLOORBEAM). REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200647 19981002 00647 NM 1998 10 2 SWAA981553 1 19980729 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND CLIP NUT HOLE AT BS 986 RBL 36 FWD LEG BS 986 RBL 35 AFT LEG AND BS 986 RBL 30 AFT LEG. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200648 19981002 00648 NM 1998 10 2 SWAA981554 1 19980729 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2 D-CHECK, FOUND CORROSION AROUND CLIP NUT HOLE AT BS 986 LBL AFT LEG BS 986 LBL 14 AFT LEG AND BS 10 16 RBL 6. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200649 19981002 00649 NM 1998 10 2 SWAA981555 1 19980729 A 5315 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT BS 294.5 LBL 12 RBL 15 AND RBL 44 WL 208. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200650 19981002 00650 NM 1998 10 2 SWAA981556 1 19980729 A 5320 SUPPORT BOEING 737 7373G7 1384595 NM BS 312-328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 312 TO 328 RBL 12 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200651 19981002 00651 NM 1998 10 2 SWAA981557 1 19980729 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 312-328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 312-328 RBL 35 WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200652 19981002 00652 NM 1998 10 2 SWAA981558 1 19980729 A 5320 ANGLE BOEING 737 7373G7 1384595 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND CRACKED ANGLE AT BS 328 RBL 35 WL 200-207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200653 19981002 00653 NM 1998 10 2 SWAA981559 1 19980729 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 727A-767 RBL 21. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200654 19981002 00654 NM 1998 10 2 SWAA981560 1 19980729 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1016 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND DAMAGED FLOOR WEB AT BS 1016 RBL 15. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200655 19981002 00655 NM 1998 10 2 SWAA981561 1 19980729 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED C4 CHECK, FOUND CRACKED AFT CARGO DOOR HOLD OPEN LATCH INTERCOSTAL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200656 19981002 00656 NM 1998 10 2 SWAA981562 1 19980729 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM AT BS 767 RBL 13. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200657 19981002 00657 NM 1998 10 2 SWAA981563 1 19980729 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 797 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND DAMAGED WEB FWD OF CARGO CUTOUT AT BS 797 RBL 25. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200658 19981002 00658 NM 1998 10 2 SWAA981564 1 19980729 A 5320 WEB BOEING 737 7373H4 1384600 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND DAMAGED WEB AFT OF DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200659 19981002 00659 NM 1998 10 2 SWAA981565 1 19980729 A 5311 FRAME BOEING 737 7373G7 1384595 NM FUSELAGE DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND DENTED FRAME AT BS 787 RBL 29 WL 160, BS 727B LBL 32 WL 158, BS 747 LBL 27 WL 156, BS 76 7 LBL 28 WL 157, BS 807 LBL 26 WL 157 AND BS 500 RBL 32 WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200660 19981002 00660 NM 1998 10 2 SWAA981566 1 19980729 A 5312 BULKHEAD PANEL BOEING 737 7373G7 1384595 NM BS 380 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND FWD RT STATIONARY BULKHEAD PANEL DENTED AT BS 380 RBL 14 WL 159. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998100200661 19981002 00661 NM 1998 10 2 SWAA981567 1 19980729 A 5320 INTERCOSTAL BOEING 737 7373G7 1384595 NM BS 227.8 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED D-CHECK, FOUND GOUGED INTERCOSTAL AT BS 227.8 LBL 22 WL 2655. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200662 19981002 00662 NM 1998 10 2 SWAA981568 1 19980730 A 5320 ANGLE BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED L ANGLE JUST BELOW STR 12R FWD OF FWD GALLEY DOOR. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200663 19981002 00663 NM 1998 10 2 SWAA981569 1 19980730 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING WALKAROUND CHECK, FOUND APPROX 3 INCH SKIN CRACK IN TOP SIDE OF FUSELAGE BETWEEN CABIN WINDOWS 10 AND 11. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200664 19981002 00664 NM 1998 10 2 SWAA981570 1 19980730 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 302SW 22941 DURING WALKAROUND CHECK, FOUND APPROX 3 INCH CRACK TOP SIDE OF FUSELAGE BETWEEN CABIN WINDOWS 10 AND 11 RIGHT SIDE. REP AIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200665 19981002 00665 NM 1998 10 2 SWAA981571 1 19980730 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 767-797 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 374SW 26582 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE FROM BS 767-797 RBL 21. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200666 19981002 00666 NM 1998 10 2 SWAA981572 1 19980730 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 354-360 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SPV CHECK, FOUND GOUGED SKIN AND DENTED AT BS 354-360, 3 INCHES BELOW STR 19 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200667 19981002 00667 NM 1998 10 2 SWAA981573 1 19980730 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SPV CHECK, FOUND FRAME SHEAR TIE DAMAGED AT BS 360, 2 INCHES BELOW STR 19 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998100200668 19981002 00668 NM 1998 10 2 SWAA981574 1 19980730 A 5320 SPLICE BOEING 737 7373H4 1384600 NM BS 360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SPV CHECK, FOUND CIRCUMFERENTIAL BUTT SPLICE DOUBLER DAMAGED AT BS 360, 2 INCHES BELOW STR 19 RT. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998100200669 19981002 00669 NM 1998 10 2 SWAA981575 1 19980730 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 360 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 385SW 26600 DURING SPV CHECK, FOUND SKIN GOUGED AND DENTED AT BS 360 TO 378 STR 19 RT, 5 INCHES BELOW STR 19 RT. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998100200670 19981002 00670 NM 1998 10 2 SWAA981576 1 19980730 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 702SW 22054 DURING SCHEDULED C1 CHECK, FOUND RIVET HEADS POPPER AND SKIN BULDGED 14 INCHES FWD OF EXTERNAL A/C ACCESS DOOR. REPAIRE D PER BOEING SRM. 2 L 7 2 4F A16WE 1998100200681 19981002 00681 NE 1998 10 2 98ZZZX3623 2 19980901 A 7261 865046V PUMP MTSBSI MU2 MU2B35 5780411 CE GARRTT TPE331 TPE3316252M 01514 NE ENGINE FAILED A DKBA O OTHER J WARNING INDICATION LD LANDING 1 SO 09 503AA 1328 633 AT LANDING PILOT NOTICED OIL PRESSURE LOW. DURING TAXI, PILOT SHUT ENGINE DOWN. MAINTENANCE FOUND ENGINE WOULD NOT TUR N BY PROP MOVEMENT. ENGINE WAS REMOVED AND SENT FOR TEARDOWN INSPECTION. THIS INSPECTION REVEALED THAT TORSION SHAFT H AD SEIZED DUE TO SCAVANGE PUMP FAILURE. 1 H 7 2 3T RT A10SW E2WE 1998100200687 19981002 00687 CE 1998 10 2 98ZZZX3629 1 19980823 A 3244 178K431 TIRE GOODYEARAERO LEAR 60 60LEAR 5170707 CE MLG FAILED A DELA O OTHER E VIBRATION/BUFFET LD LANDING 1 CE 03 899SC 43 81411524 60040 CREW NOTICED SLIGHT VIBRATION DURING TAKEOFF AND AGAIN DURING LANDING. NR 3 TIRE WAS FOUND INFLATED, BUT THE THREAD HAD SEPARATED FROM TIRE. 2 L 7 2 4F RT A10CE 1998100200704 19981002 00704 WP 1998 10 2 TC8A98064 1 19980927 A 3260 SWITCH DOUG DC8 DC862F 3021972 WP GEAR DOORS OUT OF ADJUST A TC8A O OTHER N FALSE WARNING CL CLIMB 1 GL 23 187SK 46022 TRIP NR 2565, AFTER GEAR RETRACTION, ALL LIGHTS INDICATED NORMAL EXCEPT DOORS NOT LATCHED LIGHT REMAINED ON. DURING UPL ATCH CHECK DOORS NOT LATCHED WARNING LIGHT WENT OUT. THEN LANDING GEAR WAS LOWERED, ALL LIGHT INDICATIONS NORMAL AND DO ORS NOT LATCHED LIGHT WAS OUT. ADJUSTED GEAR DOOR SWITCHES. OPS CHECKS NORMAL IAW MM 32-31-4. 2 L 7 4 4F 4A25 1998100200705 19981002 00705 NM 1998 10 2 VNAA9809022 1 19980925 A 2520 20603AC SEAT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN LOOSE A VNAA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 436JS 82151 3052 THE FLIGHT ATTENDANT REPORTED THAT THE ATTENDANT SEAT CAME OFF TRACK, DURING THE TAXI OUT FOR DEPARTURE. THE AIRCRAFT R ETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESECURED THE FLIGHT ATTENDANT SEAT, IN ACCORDANCE WITH DORNIER MAINTENA NCE MANUAL 25-2-03. OPERATIONAL CHECKS WERE COMPLETED AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100200706 19981002 00706 NM 1998 10 2 VNAA9809023 1 19980926 A 5270 870003 PSEU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E COMPT TRIPPED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 436JS 77306 20032 3052 A CARGO DOOR WARNING INDICATION ILLUMINATED, DURING THE TAXI FOR DEPARTURE. THE AIRCRAFT RETURNED TO THE GATE. MAINTEN ANCE INSPECTED AND RERACKED THE PROXY SWITCH ELECTRONIC UNIT (PSEU), IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-61 -12. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100200707 19981002 00707 NE 1998 10 2 DLM88982001 2 19980927 A 7321 FUEL CONTROL DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE MALFUNCTIONED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 27 937DL 8217 49810 725790 TAKEOFF REJECTED AT 80 KNOTS DUE TO EPR ROLLBACK ON NR 2 ENGINE. EPR WAS MOMENTARILY STABLE AT 1.86 EPR THEN ROLLED BAC K T0 1.5. REPLACED ENGINE FUEL PUMP AND CONTROL. 2 L 7 2 4F 4 F RT A6WE E9NE 1998100200708 19981002 00708 NM 1998 10 2 DL72L982003 1 19980922 A 5315 BAC150529222 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FLOORBEAM CAP CORRODED STA 344 LBL 40 TO 48. REPAIRED PER 272 SRM 53-10-8. 2 L 7 3 4F A3WE 1998100200709 19981002 00709 NM 1998 10 2 DL72S982004 1 19980723 A 5753 SKIN BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 DURING SHOP INSPECTION, THE AFT LOWER COVE SKIN WAS FOUND CRACKED IN THE CORNERS OF THE CUTOUT FOR I/B DRIVE ROD. THE C RACKS WERE ROUTED OUT AND A DOUBLER INSTALLED PER 727 MM 57-52-0 FIG 809. 2 L 7 3 4F A3WE 1998100200710 19981002 00710 NM 1998 10 2 DL72S982005 1 19980723 A 5753 ANGLE BOEING 727 727232 1384082 NM LT TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 30 INCHES FROM O/B END OF FLAP. THE CRACK WAS RE PAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998100200711 19981002 00711 NM 1998 10 2 DL72S982006 1 19980723 A 5753 ANGLE BOEING 727 727232 1384082 NM NR 2 TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 405DA 21149 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 32 INCHES FROM I/B END OF FLAP. THE ANGLE WAS RE PAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998100200712 19981002 00712 NM 1998 10 2 DL72S982007 1 19980810 A 5753 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 44 INCHES FROM O/B END. THE ANGLE WAS REPAIRED P ER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998100200713 19981002 00713 NM 1998 10 2 DL72S982008 1 19980810 A 5753 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 35 INCHES FROM THE I/B END. THE ANGLE WAS REPAIR ED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802. 2 L 7 3 4F A3WE 1998100200714 19981002 00714 NM 1998 10 2 DL72S982009 1 19980810 A 5753 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 37 INCHES FROM I/B END. THE ANGLE WAS REPAIRED P ER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998100200715 19981002 00715 NM 1998 10 2 DL72S982010 1 19980810 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM TR TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 411DA 21223 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 19 AND 23 INCHES FROM I/B END. THE ANGLE WAS REP AIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998100200716 19981002 00716 NM 1998 10 2 DL76S982011 1 19980928 A 2910 AE70577778 LINE BOEING 767 767332 1382001 NM GE CF680 CF680A2 NE NR 2 ENGINE WORN A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 126DL 24076 580172 RIGHT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO SOON AFTER TAKEOFF. COMPLETED POM PROCEDURES AND RETURNED FOR LANDING. P ER CREW COMMENT ENGINE HYD PUMP DID NOT RUN DRY. NO PRESSURE LOSS NOTED. ENGINE PUMP SHUT DOWN PRIOR TO PRESSURE LOSS. FOUND NR 2 ENGINE HYD PRESSURE LINE WORN THRU. REPLACED HYD LINE (P/N 291201624). SERVICED RIGHT HYD SYSTEM. ENGINE RUN LEAK CHECK OPN CHECK OK. 2 L 7 2 4F 4 F RT A1NM E13NE 1998100200717 19981002 00717 WP 1998 10 2 DLL10982013 1 19980929 A 2612 CONNECTOR LKHEED 1011 10113851 5265010 WP NR 3 ENGINE CORRODED A DALA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 27 721DA 193C1139 NR 3 ENG FIRE INDICATION IN FLIGHT, POM PROCEDURE COMPLIED WITH. BOTH BOTTLES FIRED, CIRCUIT WOULD NOT TEST. REPLACED UPPER GAS GENERATOR AND AFT GEARBOX LOOP CONNECTORS. 2 L 7 3 4F A23WE 1998100200718 19981002 00718 NM 1998 10 2 DL757982014 1 19980929 A 2781 FSEU BOEING 757 757232 1384965 NM LE SLATS FAILED A DALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 27 618DL 22908 DIVERSION, PILOT REPORT: L/E SLAT ASYM EICAS MSG ILLUMINATED ALONG WITH T/E ANNUNCIATOR AT FL 350. FOUND AND REPLACED NR 1 FSEU CAUSING FALSE SLAT LOSS MSG ALL WIRING FROM PIN C9, PER FIM OK EVEN WITH FAULT DISPLAYED. ALSO, RESET BOXES 2 AND 3. OPERATIONAL CHECK GOOD PER MM CHAPTER 27. 2 L 7 2 4F RT A2NM 1998100200719 19981002 00719 NM 1998 10 2 DL72S982015 1 19980929 A 5720 ANGLE BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 540DA 22386 REF TPA LETTER CHECK D-1, SUPPORT ANGLE CRACKED AT LWR FWD SIDE OF NR 8 SPOILER ACTUATOR SUPPORT FITTING. INSTALLED DOU BLER PER M/M 57-20-22. 2 L 7 3 4F A3WE 1998100200720 19981002 00720 NM 1998 10 2 98UAL900448 1 19980902 A 2150 213W31304 TORQUE TUBE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT RAM AIR DOOR SHEARED A UALA A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 WP 29 770UA 26925 MODERATE VIBRATIONS AT DOOR 2 RIGHT FROM FLOOR. AIRCRAFT RETURNED TO DEN. *S/D* FOUND RIGHT PACK RAM AIR DOOR TORQUE TUBE ASSEMBLY (213W3130-4) SHAFT SHEARED. REPLACED TORQUE TUBE ASSEMBLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998100200721 19981002 00721 NM 1998 10 2 98UAL900449 1 19980905 A 2150 213W31303 TORQUE TUBE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT RAM AIR DOOR SHEARED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 WP 29 770UA 1691 26925 APPROXIMATELY 30 MINUTES AFTER TAKEOFF, FLIGHT EXPERIENCED A LOUD NOISE AND VIBRATION. AIRCRAFT RETURNED TO MIA. *S/D* FOUND LEFT PACK RAM AIR DOOR TORQUE TUBE ASSEMBLY (213W3130-3) SHAFT SHEARED. REPLACED TORQUE TUBE ASSEMBLY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998100200722 19981002 00722 NM 1998 10 2 98UAL900462 1 19980918 A 3397 W1334L476222 WIRE BOEING 747 747123 1384873 NM PWA JT9 JT9D7A 52054 NE CABIN FAILED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 157UA 20106 CEILING EMERGENCY LIGHT INOP AT AFT LAV NR 118 AISLE. REPAIRED WIRE NR W1334-L4762-22 AT LIGHT ASSEMBLY, OP CK OK. 2 L 7 4 4F 4 F A20WE E20EA 1998100200723 19981002 00723 NM 1998 10 2 98UAL900464 1 19980919 A 2424 REGULATOR SUNDSTRAND 939D1502 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 7259U 21406 GOT AN OVER EXCITED ANNUNCIATOR LIGHT ON NR 1 SYSTEM. BUS BREAKER DID NOT TRIP. RESET BROUGHT GENERATORS BACK ON LINE FOR 5 MINUTES. AT TAKEOFF ANNUNCIATOR LIGHT CAME ON AGAIN. SYSTEM NR 1 BUS TIE TRIPPED SYSTEM 1 FOLLOWED BY LEFT PACK TRIP. TANK NR 1 AFT BOOST PUMP BREAKER TRIPPED AND TANK NR 2 FORWARD RIGHT BOOST PUMP BREAKER TRIPPED. *S/D* REPLACED NR 1 VOLTAGE REGULATOR, NO FURTHER PROBLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1998100200724 19981002 00724 WP 1998 10 2 98UAL900465 1 19980921 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1838U 46632 ALL EEL LIGHTS IN C-ZONE ARE INOP. REPLACED 3 BATTERY PACKS IN FORWARD C ZONE AND 3 BATTERY PACKS IN AFT C ZONE. CHECK S OK. 2 L 7 3 4F 4 F A22WE E23EA 1998100200725 19981002 00725 WP 1998 10 2 98UAL900466 1 19980921 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1838U 46632 EMERGENCY OVERHEAD AND EXIT LIGHTS ON DOORS 2L, 2R AND SEVERAL LT AND RT THROUGH LIGHTS IN B ZONE ARE INOP. REPLACED BA TTERY PACK AND BATTERY CONTROL BOX. CHECKS OK. 2 L 7 3 4F 4 F A22WE E23EA 1998100200726 19981002 00726 NM 1998 10 2 98UAL900467 1 19980922 A 2752 240863 DRIVE MOTOR VICKERS, INC BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE TE FLAPS LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7455U 21909 AFTER DEPARTURE LOST HYDRAULIC SYSTEM A PRESSURE. CONTINUED TO ORD AND WAS TOWED TO THE GATE. *S/D* REPLACED HYD FLAP DRIVE MOTOR AND NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMPS PRECAUTIONARY. ALSO, REPLACED CASE DRAIN AND PRESSURE FILT ERS PER MAINTENANCE MANUAL. LEAK CHECK OK. 2 L 7 3 4F 4 F A3WE E2EA 1998100200727 19981002 00727 NM 1998 10 2 98UAL900468 1 19980922 A 3610 AIR VALVE ALLIED SIGNA 32895625 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LEFT FAILED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 343UA 24247 LOSS OF PRESSURIZATION. *S/D* THE LEFT HAND PACK TRIPPED OFF, THEN RESET AND TRIPPED OFF AGAIN. THEN THE RIGHT HAND P ACK TRIPPED OFF AND WAS RESET. THE LEFT HAND FAN AIR VALVE FAILED AND WAS REPLACED. THE RIGHT HAND FAN AIR VALVE TEMPE RATURE SENSOR FAILED AND WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998100200728 19981002 00728 NM 1998 10 2 98UAL900469 1 19980923 A 3350 900542U1 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT WING EXIT DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7297U 21892 BOTH OVERWING EXIT LIGHTS ON LEFT INTERIOR SIDE ARE INOPERATIVE. *S/D* REPLACED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1998100200729 19981002 00729 NM 1998 10 2 98UAL900470 1 19980924 A 2910 271N6119 LINE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT HYD SYST FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 539UA 25223 LANDED UNDER AMBER ALERT DUE TO LOSS OF FLUID FROM THE LEFT HYDRAULIC SYSTEM. *S/D* LEFT HAND DOWNLOCK ACTUATOR LINE D AMAGED. LINE REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998100200730 19981002 00730 NM 1998 10 2 98FDEA00600 1 19980927 A 2910 2249409501 PIPE DOUG MD11 MD11F 3023600 NM NR 3 ENGINE CRACKED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 582FE 48420 DECREASE FLUID IN HYD RES NR 3 BOTH PUMPS SHUTDOWN. REMOVED AND REPLACED PUMP CASE DRAIN PIPE PER MM 29-11-20-4. LEAK CHECK, NONE FOUND. REL PER MEL. REPLACED BOTH ENG DRIVEN PUMPS, FILTERS AND BROKEN LINE. 2 L 7 3 4F RT A22WE 1998100200731 19981002 00731 NM 1998 10 2 98FDEA00601 1 19980914 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1070 MISDRILLED A FDEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 25 169FE 18866 UPPER LOBE FLOORBEAM BS 1070, RBL 625 HAS DOUBLE DRILL HOLE IN FLOORBEAM. CUT OUT AREA OF DAMAGE AND REPAIR PER AARD 53 -10-07. 2 L 7 3 4F A3WE 1998100200732 19981002 00732 NM 1998 10 2 98FDEA00602 1 19980916 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 UPPER LOBE HEAVY CORROSION ON UPPER SURFACE OF LWR FLANGE OF FLOORBEAM BS 1050, RBL 39. INSTALLED FLOORBEAM LWR CHORD R EPAIR PER SRM 53-10 8 PG 11-17. 2 L 7 3 4F A3WE 1998100200733 19981002 00733 NM 1998 10 2 98FDEA00603 1 19980925 A 5315 5633571 FLOORBEAM BOEING 727 72722 1384002 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 UPPER LOBE, BS 1050 HEAVY CORROSION ON LWR FWD LEG OF FLOORBEAM AT LBL 29. BLENDED OUT CORROSION IN AREA NOTED PER SRM 51-10-6. BLENDED AREA OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED DOUBLER ON FLOORBEAM PER AARD 53-10-07-2. 2 L 7 3 4F A3WE 1998100200734 19981002 00734 NM 1998 10 2 98FDEA00605 1 19980925 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 970 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CABIN FLOORBEAM CUT ACROSS TOP FLANGE AT STR 970, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-5310-29648. 2 L 7 3 4F A3WE 1998100200735 19981002 00735 NM 1998 10 2 98FDEA00606 1 19980925 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1050 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CABIN FLOORBEAM CUT ACROSS TOP FLANGE BS 1050, RBL 63. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7- 5310-29648. 2 L 7 3 4F A3WE 1998100200736 19981002 00736 NM 1998 10 2 98FDEA00607 1 19980925 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1130 DAMAGE A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 FLOORBEAM CUT ACROSS TOP FLANGE BS 1130, RBL 63. BLENDED OUT DAMAGE AND INSTALLED .080 STRAP OF 7075-T6 ALUM PER AARD 5 3-10-07-01 AND 7-5310-29698. 2 L 7 3 4F A3WE 1998100200737 19981002 00737 NM 1998 10 2 98FDEA00608 1 19980925 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1010 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CABIN FLOORBEAM HAS ONE DOUBLE DRILL HOLE BS 1010, RBL 63. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-10-07-02 FI G 3 AND EA 7-5310-29648. 2 L 7 3 4F A3WE 1998100200738 19981002 00738 NM 1998 10 2 98FDEA00609 1 19980925 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 990 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 UPPER LOBE FLOORBEAM HAS DOUBLER DRILL HOLE BS 990. CUT OUT DAMAGE, INSTALLED DOUBLER PER AARD 53-10-07-02 AND EA 7-531 0-29648. 2 L 7 3 4F A3WE 1998100200739 19981002 00739 NM 1998 10 2 98FDEA00610 1 19980925 A 5330 SKIN BOEING 727 72722 1384002 NM BS 360 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 CORROSION ON FUSELAGE SKIN 25 PERCENT LOBE OF MATERIAL BETWEEN STR 25R-26R, BS 360. CUT OUT CORROSION, INSTALLED DOUBLE R AND FILLER ON OUTSIDE OF SKIN EXTENDING 3 ROWS BELOW SKIN LAP PER EA 7-5330-29666. DATED 9/18/98 AND SRM 53-30-3. 2 L 7 3 4F A3WE 1998100200740 19981002 00740 NM 1998 10 2 98FDEA00611 1 19980925 A 5320 FRAME BOEING 727 72722 1384002 NM CARGO DOORWAY CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 AFT CARGO FWD DOOR PORTAL FRAME CRACKED AT LOWER FWD DOOR STOP, OUTBD LWR FAST. REMOVED AND REPLACED AFT CARGO FWD DOOR PORTAL FRAME PER SRM 51-10-1. 2 L 7 3 4F A3WE 1998100200741 19981002 00741 NM 1998 10 2 98FDEA00612 1 19980925 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 680 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 BS 680 CORROSION ON BOTTOM SIDE OF FLOORBEAM LWR FLANGE AT SEV AREAS. BLENDED OUT CORROSION PER EA 7-5310-29662 DATED 9 -14-98. INSTALLED .071 7075-T6 ANGLES ON FWD AND AFT FLANGES PER AARD 53-10-7-2 AND EA 7-5310-29662. 2 L 7 3 4F A3WE 1998100200742 19981002 00742 NM 1998 10 2 98FDEA00613 1 19980916 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 169FE 18866 AFT CARGO FLOORBEAM BS 1050, LWR CHORD HAS CORROSION FROM RBL 24- RBL 43. INSTALLED FLOORBEAM REPAIR LWR CHORD PER SRM 53-10-8 PG 11-17. 2 L 7 3 4F A3WE 1998100200743 19981002 00743 NM 1998 10 2 98FDEA00597 1 19980928 A 5314 65184071 KEEL BEAM BOEING 727 72722 1384002 NM BS 1040 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 CORROSION ON RT KEEL BEAM AT BS 1040, WL 138, AFT CARGO BAY. *S/D* REMOVED AND REPLACED RT KEEL BEAM AT BS 1040 TO BS 961 WL 138 PER FEDEX EA 7-5330-42225. 2 L 7 3 4F A3WE 1998100200744 19981002 00744 NM 1998 10 2 98FDEA00598 1 19980929 A 3260 LIBHT BOEING 727 7272D4 138407U NM RT MLG DOOR INOPERATIVE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 288FE 21850 98-238 ON INIT T/O, THE RT GEAR DOOR LIGHT REMAIN ILLUM. ACCOMPLISH RED TABS. LIGHT REMAIN ILLUMINATED, SUSP RIGHT GE AR DID NOT RETRACT. WITH GEAR DOWN ANTI-SKID INOP AND SYS 'A' QUANTITY 2.5 GAL. REMOVED ANTI-SKID CONTROL UNIT. REPLA CED STRUT DOOR SUPPORT PER 727 MM. REINSTALL ROUT RIGHT ELECT CONDUIT AND SAFTIED. OPS NORM. COMPLIED WITH ENG AUTH 7 -3210-40942. OK FOR SERV. 2 L 7 3 4F A3WE 1998100200745 19981002 00745 NM 1998 10 2 98FDEA00599 1 19980929 A 3260 H1010154 SWITCH BOEING 727 72722C 138400F NM NLG FAILED A FDEA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 25 113FE 19894 ON APPROACH WITH GEAR LEVER DOWN, NOSE GEAR IND UNSAFE. DURING GO-AROUND LIGHT WENT OUT AND GREEN NOSE GEAR DOWN CAME O N. REPLACED NOSE LAND GEAR POSITION SWITCH AND OPER CK GOOD PER MM 32-61-21. 2 L 7 3 4F A3WE 1998100600001 19981006 00001 NM 1998 10 6 TSAA9833529 1 19980801 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1998100600002 19981006 00002 NM 1998 10 6 TSAA9833530 1 19980731 A 3350 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 CENTER AISLE OVERHEAD FOLDING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1998100600003 19981006 00003 NM 1998 10 6 TSAA9833531 1 19980803 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 3 POSITION EMERGENCY PATH LIGHT ASSY BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100600004 19981006 00004 WP 1998 10 6 VJ9800423 1 19980901 A 5321 1A355701 FLOOR DOUG DC9 DC932 3022066 WP BS 161 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 E/E BAY FLIGHT COMPARTMENT FLOOR FS 161.0 CORRODED AND A PORTION IS MISSING. CLEANED CORROSION, 100 PERCENT MATERIAL LO SS AND CRACKED SKIN. FABBED REPAIR DOUBLER IAW DC-9 SRM 51-01, 53-01. DRILLED, DEBURRED AND COUTERSUNK IAW DC-9 SRM 53 -11-1. TREATED AND PRIMED IAW DC-9 SRM 51-10-3. INSTALLED REPAIR IAW SRM 51-30-2, INSTALLED FLOOR PANEL IAW 51-30-1. 2 L 7 2 4F A6WE 1998100600005 19981006 00005 WP 1998 10 6 VJ9800424 1 19980821 A 5330 1A3559335594 SKIN DOUG DC9 DC932 3022066 WP BS 110 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FWD FUSELAGE RT SIDE FS 110 HAS LIGHTENING STRIKE. BLENDED AREA IAW SRM 53-04 FIG 38 FOUND TO BE OUT OF LIMITS IAW SRM 53-04 FIG 38, 53-01 FIG 1. REMOVED OUT OF LIMITS AREA, FABBED REPAIR DOUBLER FROM .032 TITANIUM. DRILLED, COUNTERSUNK, DEBURRED, TREATED, AND PRIMED IAW DC-9 SRM 53-04 FIG 38, AIRTRAN RES 981324. INSTALLED REPAIR DOUBLER IAW SRM 53-04 FI G 38. 2 L 7 2 4F A6WE 1998100600006 19981006 00006 WP 1998 10 6 VJ9800425 1 19980821 A 5321 1A363101 FLOOR DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FLOORBOARD NR 34 HAS CORROSION AROUND EDGES, CHAFED MARKS ON HAT CHANNEL AND BROKEN AT FASTENER ON PREVIOUS REPAIR CRACK . BLENDED CHAFED AREAS AND REMOVED CORROSION IAW SRM 53-01 FIG 1 IN LIMITS. REMOVED PREVIOUS REPAIR AND FOUND TO BE CO RRODED BEYOND LIMITS IAW SRM 53-01 FIG 1. FABBED, DRILLED, DEBURRED, TREATED, AND PRIMED IAW SRM 53-05 FIG 1. INSTALLE D DOUBLER REPAIR AND FILLER IAW DC-9 SRM 53-05 FIG 1. 2 L 7 2 4F A6WE 1998100600007 19981006 00007 WP 1998 10 6 VJ9800426 1 19980821 A 5320 5956034557 BRACKET DOUG DC9 DC932 3022066 WP BS 484 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FWD PIT FS 484 LONG 27R-28R FRAME BRACKET CORRODED. REMOVED FRAME BRACKET IN FWD BS 484 BETWEEN STR 27R AND 28R IAW SRM 51-30-1. REMOVED CORROSION ON BRACKET ORIGINAL THICKNESS .130. REMOVED .033 IAW AERO CARP MICROMETER NR A-1729, FOUND TO BE OUT OF LIMITS IAW DC-9 SRM 53-01 FIG 1. LOCATED NEW BRACKET, DRILLED, DEBURRED IAW 51-10-4. INSTALLED IAW 51-30 -5. 2 L 7 2 4F A6WE 1998100600008 19981006 00008 EU 1998 10 6 SIMA982223 1 19980810 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 268AE 17491 340B268 ALB - FLT 4894 - OVERHEAD EMERGENCY LIGHTS AT PASSENGER DOOR AND FLIGHT ATTENDANT'S SEAT DO NOT ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998100600009 19981006 00009 SO 1998 10 6 C2XA98IA396 1 19980827 A 3350 F02A250V1A FUSE EMB 120 EMB120RT SO CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16719 120138 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THE FORWARD RIGHT FUSELAGE EMERGENCY LIGHT WAS INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE FUSE FOR THE AFFECTED LIGHT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900001 19981009 00001 WP 1998 10 9 TWAA9815801 1 19980925 A 5320 SUPPORT DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND CENTER FLOOR SUPPORT, STA 218 TO 237, WAS CORRODED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PER SRM 51-01. 2 L 7 2 4F A6WE 1998100900002 19981009 00002 WP 1998 10 9 TWAA9815802 1 19980928 A 5320 59144141 PAN DOUG DC9 DC931 3022065 WP FWD ACCY COMPT WORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND PAN IN FWD ACCESSORY COMPT WITH INTERIM REPAIR INSTALLED PER ARA 11869 AND ARA 11870. R EPLACED PAN AND REPAIRED PER ARA 15700, AND SRM 51-30-00 AND SRM 51-30-2. 2 L 7 2 4F A6WE 1998100900003 19981009 00003 WP 1998 10 9 TWAA9815901 1 19980925 A 3350 362624 LIGHT DOUG DC9 DC951 3022051 WP CABIN SHORTED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 416EA 47751 FWD SECTION OF FIRST CLASS FLOOR EGRESS LIGHTING INOPERATIVE. REPLACED SHORTED LIGHT STRIP. CHECK-C 12-17-97 STL. 2 L 7 2 4F RT A6WE 1998100900004 19981009 00004 WP 1998 10 9 TWAA9815902 1 19980930 A 5730 PANEL DOUG DC9 DC931 3022065 WP LT WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND PANEL ABOVE O/B END OF LT AILERON, 8 IN TO 17 IN FROM O/B END, WAS CORRODED AND DELAMINA TED. INSTALLED NEW CORE AND ALUM SKIN PER SRM 51-70-2 HOT BOND PROCEDURE PER SERVICEABLE TAG. 2 L 7 2 4F A6WE 1998100900005 19981009 00005 WP 1998 10 9 TWAA9815903 1 19980930 A 5347 SEAT TRACK DOUG DC9 DC931 3022065 WP BS 218-237 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND NR 4 CABIN CHAIR TRACK CORRODED AT STA 218 TO 237. CORRODED SECTION OF TRACK REMOVED AN D NEW SECTION INSTALLED WITH EXISTING HARDWARE. 2 L 7 2 4F A6WE 1998100900006 19981009 00006 WP 1998 10 9 VJ9800444 1 19980915 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 962 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 SKIN AT FS 962, L25R, GOUGED BEYOND LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT GOUGE, FABRICATED AND INSTALLED EXTERNAL A ND FINGER DOUBLERS IAW DC9 SRM 53-04, FIG 38, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998100900007 19981009 00007 WP 1998 10 9 VJ9800445 1 19980925 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 967 GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 GOUGE IN FUSELAGE SKIN AT FS 967, L21-22R, BEYOND LIMIT IAW DC9 SRM 53-04, FIG 8. BLENDED AREA, FABRICATED AND INSTALLE D DOUBLER REPAIR IAW DC9 SRM 51-10-3, 53-31-0 FIG 8 AND 53-04 FIG 38. 2 L 7 2 4F A6WE 1998100900008 19981009 00008 WP 1998 10 9 VJ9800447 1 19980930 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP L1 DOOR DISLODGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 913VV 47318 FWD ENTRY EMERGENCY DOOR SLIDE DISLODGED FROM CASING WHEN DOOR OPENED. SECURED SLIDE IAW MM 25-00. 2 L 7 2 4F A6WE 1998100900009 19981009 00009 WP 1998 10 9 VJ9800448 1 19980916 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-190 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FLOOR SUPPORT UNDER NUT PLATES AT FS 160 - 190, LBL 44, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. REMOVED, FABRIC ATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 51-30-5, 51-10-2, 51-10-4 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1998100900010 19981009 00010 NM 1998 10 9 9810136637 1 19980928 A 3231 ROD BOEING 747 747251B 1384892 NM RT MLG DOOR DISCONNECTED A NWAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 GL 01 637US 23548 DURING CLIMB, THE RED DOOR OPEN AND GEAR LIGHTS REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. RECYCLED LANDING GE AR AND LIGHTS REMAINED ILLUMINATED. AIRCRAFT DUMPED FUEL AND RETURNED TO HNL AND LANDED WITHOUT INCIDENT. RECONNECTED RIGHT WING LANDING GEAR DOOR SEQUENCE VALVE CONNECTING ROD, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1998100900011 19981009 00011 WP 1998 10 9 9810149606 1 19980925 A 3231 ROLLER DOUG DC9 DC932 3022066 WP LT MLG DOOR OUT OF ADJUST A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 606NW 47225 AFTER LANDING GEAR EXTENSION, THE LANDING GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. THE FLIGHT CREW FOLLOWED COM PROCE DURES, RECYCLED THE LANDING GEAR SYSTEM, AND LANDED AT DTW WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT LANDING GEAR DOOR LOCK ROLLER ASSEMBLY AND REPLACED THE LEFT AND RIGHT LANDING GEAR DOOR SKIDS. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998100900012 19981009 00012 WP 1998 10 9 9810159619 1 19980926 A 3231 CONTROL CABLE DOUG DC9 DC932 3022066 WP NLG DOOR BROKEN A NWAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 01 619NW 47518 AFTER TAKEOFF, THE FLIGHT CREW NOTICED A LOUD BANG AND STRONG FLUTTER FROM THE NOSE LANDING GEAR DOOR AREA. FLIGHT RETU RNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR STOP CABLE AND NOSE LANDING GEAR DO OR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998100900013 19981009 00013 SO 1998 10 9 COMA9810223 1 19980929 A 3230 PIN EMB 120 EMB120RT SO NLG NOT REMOVED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 254CA 120233 NLG WILL NOT RETRACT. REMOVED THE DOWN LOCK SAFETY PIN FROM NLG. 2 L 7 2 4T RT A31SO 1998100900014 19981009 00014 NM 1998 10 9 UPS98227777 1 19980910 A 5510 652791713 BALANCE PANEL BOEING 727 72721C 138400M NM LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE-D, CORROSION ON NR 5 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21. 2 L 7 3 4F A3WE 1998100900015 19981009 00015 NM 1998 10 9 UPS98227778 1 19980908 A 5510 652791714 BALANCE PANEL BOEING 727 72721C 138400M NM RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE-D, RT STAB, LIGHT SURFACE CORROSION ON NR 5 BALANCE PANEL. BALANCE PANEL REPLACED IAW MM 27-30-21. 2 L 7 3 4F A3WE 1998100900016 19981009 00016 NM 1998 10 9 UPS98227779 1 19980908 A 5510 65279164 BALANCE PANEL BOEING 727 72721C 138400M NM RT HORIZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE-D, RT STAB NR 4 BALANCE PANEL CRACKED. BALANCE PANEL REPLACED IAW MM 27-30-21. 2 L 7 3 4F A3WE 1998100900017 19981009 00017 NM 1998 10 9 UPS98227780 1 19980910 A 5510 65279153 BALANCE PANEL BOEING 727 72721C 138400M NM LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 934UP 19135 INSPECTION TYPE-D, CORROSION ON NR 3 BALANCE PANEL LT HORIZ STAB. BALANCE PANEL REPLACED IAW MM 27-30-21. 2 L 7 3 4F A3WE 1998100900018 19981009 00018 EU 1998 10 9 QXEA9801367 1 19980928 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 AFT FACING EXIT SIGN AT ROW 8 IS DIM. MAINTENANCE RELAMPED, OPERATIONAL TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998100900019 19981009 00019 EU 1998 10 9 QXEA9801368 1 19980928 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 487US 11238 FORWARD EMERGENCY EXIT SIGN HAS BULBS OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTS ARE NORMAL. 2 L 7 2 4F RT A20EU 1998100900020 19981009 00020 WP 1998 10 9 98FDEA00614 1 19980930 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1741 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 375FE 46613 REPAIR OF INTERNAL FUSELAGE AREA BS 1741 LONGERON 13L, FUSELAGE BELL FRAME CRACKED. REPAIRED PER SRM 53-30-00 FIG 5. 2 L 7 3 4F A22WE 1998100900021 19981009 00021 WP 1998 10 9 MWEA98980 1 19980928 A 3350 6011779 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 302ME 47102 THE LEFT ENGINE NACELLE LIGHT WILL NOT TEST WITH EMERGENCY LIGHTING. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998100900022 19981009 00022 1998 10 9 SCNA98112 4 19980927 A 2565 5WD230600203 SLIDE DOUG DC10 DC1015 3022118 WP CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 151SY 10697 48295 DURING A LINE MAINTENANCE CHECK, THE R3 DOOR SLIDE PRESS TO TEST LIGHT WAS CONTINUOUSLY ILLUMINATED. FOUND SLIDE PRESSU RE TO BE LOW AND REMOVED AND REPLACED THE EMERGENCY SLIDE IAW MM 256101. SLIDE PACK PRESSURE INDICATOR TESTS NORMAL. 2 L 7 3 4F A22WE 1998100900023 19981009 00023 WP 1998 10 9 RRXA98434 1 19980926 A 3310 900816001 BALLAST DOUG DC8 DC873F 302199F WP GLARESHIELD FAILED A RRXA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 15 105WP 46095 SMOKE IN COCKPIT COMING FROM F/O'S RIGHT CONSOLE AND SUITCASE. FOUND GLARESHIELD BALLAST BURNED RT SIDE BY F/O'S LEG. TRANSFERRED TO DMI NR 809410 IAW MEL CHAP 33-1 CAT DUE DATE 10/6/98 PLACARD INSTALLED. (CLOSED 09/27/98 KLAX) REMOVED AND REPLACED BALLAST ASSY. SYS OPS NORMAL PER MM33-11. THIS CLEARS DMI 809410. 2 L 7 4 4F RT 4A25 1998100900024 19981009 00024 NM 1998 10 9 VNAA9809024 1 19980927 A 5610 001A561A0000207 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT CRACKED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 429JS 50114 15933 3043 DURING CRUISE, THE RIGHT HAND SIDE WINDSCREEN OUTER AND CENTER PANE CRACKED. THE CREW FOLLOWED THE CHECKLIST PROCEDURES , AND CONTINUED TO CLT. A NORMAL LANDING WAS PERFORMED IN CLT WITHOUT ANY FURTHER PROBLEMS. OUTSTATION MAINTENANCE INS PECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO CAK, TO FACILITATE REPAIR. THE FERRY FLIGHT WAS CARRIED OUT WITH OUT ANY PROBLEMS. CAK MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND SIDE WINDSHIELD, IN ACCORDANCE WITH DORNIER MAI NTENANCE MANUAL 56-12-00. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100900025 19981009 00025 NM 1998 10 9 VNAA9809025 1 19980928 A 3610 4069B000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 434JS 44533 2732 3051 DURING TAXI PRIOR TO DEPARTURE, A CROSS BLEED FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAI NTENANCE INSPECTED AND REPLACED THE CROSS BLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERATIO NAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100900026 19981009 00026 NM 1998 10 9 VNAA9809026 1 19980929 A 7330 1060K SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE SWAPPED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 430JS 70518 7197 3044 A RIGHT HAND FUEL FEED TEMPERATURE WARNING INDICATION ILLUMINATED, DURING THE CLIMBOUT PHASE OF THE FLIGHT. THE AIRCRAF T RETURNED TO THE FIELD AND LANDED. MAINTENANCE INSPECTED AND SWAPPED THE FUEL FEED TEMPERATURE SENSORS FROM RIGHT TO L EFT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-31-06. OPERATIONAL AND LEAK CHECKS WERE CARRIED OUT, THEN A FUNC TIONAL VERIFICATION FLIGHT WAS CONDUCTED WITH SATISFACTORY RESULTS. THE AIRCRAFT WAS RELEASED FROM MAINTENANCE AFTER TH E VERIFICATION FLIGHT. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100900027 19981009 00027 WP 1998 10 9 TWAA9816001 1 19981002 A 3350 58222 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 922L 47108 EGRESS LIGHTING FLICKERED AND QUIT AFTER 30 MINUTES INTO FLIGHT, ROWS 20 AND BACK. REPLACED POWER SUPPLY FOR EGRESS LIG HTS ROW 20 AFT. CHECK-C 11-15-97 MCI. 2 L 7 2 4F A6WE 1998100900028 19981009 00028 WP 1998 10 9 TWAA9816002 1 19981003 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9406W 53126 FOUND EMERGENCY OVERWING LIGHTS INOP. REPLACED BATTERY PACK. CHECK-C 1-15-98 STL. 2 L 7 2 4F RT A6WE 1998100900029 19981009 00029 NM 1998 10 9 TWAA9816005 1 19981002 A 3397 WIRE BOEING 757 757231 1384950 NM CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 705TW 28479 FOUND EGRESS LIGHTS INOP AT FWD EMERGENCY EQUIPMENT CLOSET. REPAIRED BAD SPLICE AT THE EQUIP CLOSET. CHECK-C 8-8-98 LA X. 2 L 7 2 4F RT A2NM 1998100900030 19981009 00030 WP 1998 10 9 TWAA9816006 1 19980917 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 813 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT LONGERON 18R, STA 813. CORROSION WAS APPROX 0.008 DEEP AND 3 I N BY 3 IN. REMOVED CORROSION AND REPAIRED WITH ALUM 2024-T3, 0.032 IN PER SRM 53-01, PAGE 9 FIG 2. 2 L 7 2 4F A6WE 1998100900031 19981009 00031 NE 1998 10 9 TWAA9815502 2 19980924 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LEFT FAILED A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 922L 47108 2114 THE LT ENG FILTER CLOG LIGHT ILLUMINATED AND EGT INCREASED. RETARDED THROTTLE AND DIVERTED TO BNA. FOUND METAL IN MAIN OIL SCREEN. ENGINE WAS CHANGED. CHECK-C 11-15-97 MCI. *S/D* ANALYSIS OF MATERIAL IN OIL SCREEN FOUND EVIDENCE OF M- 50 BEARING MATERIAL. SUBMITTER STATES, NR 3 BEARING ASSEMBLY. 2 L 7 2 4F 4 F A6WE E2EA 1998100900032 19981009 00032 WP 1998 10 9 TWAA9816102 1 19981005 A 2170 39347101 DUCT DOUG DC9 DC934 302207E WP CABIN FAILED A TWAA B EMER. DESCENT O OTHER CR CRUISE 1 CE 05 936L 47711 COULD NOT MAINTAIN CABIN PRESSURIZATION AT ALTITUDE. DESCENDED TO 10,000 FT AND PRESSURIZATION NORMAL FOR REMAINDER OF FLIGHT. REPLACED THE LEFT WATER SEPARATOR DUCT. CHECK-C 6-17-98 STL. 2 L 7 2 4F RT A6WE 1998100900033 19981009 00033 WP 1998 10 9 TWAA9816103 1 19981005 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 658 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND CRACK AT BOTTOM FWD SIDE OF FORMER RING BELOW CABIN FLOOR STA 658 LT. REPAIRED PER SRM 53-03, FIG 16. INSTALLED DOUBLER WITH HI-LOKS AS REQUIRED. 2 L 7 2 4F A6WE 1998100900034 19981009 00034 NM 1998 10 9 SPAA980005 1 19980930 A 3350 6013711 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE RT OVERWING EXTERNAL EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. THE ASSOCIATED SYSTEM BATTE RY PACK WAS REMOVED AND REPLACED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY PER BMM 33-51-11. 2 L 7 2 4F A16WE 1998100900035 19981009 00035 NM 1998 10 9 SPAA9800006 1 19980930 A 3350 110049 POWER SUPPLY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SPAA K NONE L NO TEST IN INSP/MAINT 1 WP 28 703S 22529 DURING SCHEDULED CHECK, THE FORWARD SECTION EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE. THE ASSOCIATED SYSTEM POWER SUP PLY WAS REMOVED AND REPLACED. SUBSEQUENT SYSTEM CHECK WAS SATISFACTORY PER BMM 33-51-11. 2 L 7 2 4F A16WE 1998100900036 19981009 00036 1998 10 9 VJ9800508 4 19981004 A 2565 9560892 SLIDE DOUG DC9 DC932 3022066 WP TAIL CONE INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 914VV 47486 TAIL CONE EMERGENCY ESCAPE SLIDE GAUGE READS IN THE RED. REPLACED TAIL CONE EVACUATION SLIDE ASSEMBLY IAW MM 25-60. PE RFORMED REQUIRED INSPECTION. 2 L 7 2 4F A6WE 1998100900037 19981009 00037 1998 10 9 VJ9800509 4 19981004 A 3425 2589433901 MONITOR DOUG DC9 DC932 3022066 WP E & E COMPT INOPERATIVE A ZZDA O OTHER J WARNING INDICATION CL CLIMB 1 SO 15 925VV 47319 CAPTAIN'S ADI GETS INTERMITTENT GYRO FLAG. REPLACED SMART BOX, OPS CHECKS GOOD IAW MM 34-00. 2 L 7 2 4F A6WE 1998100900038 19981009 00038 NM 1998 10 9 VJ9800449 1 19980920 A 5313 STRINGER BOEING 737 7372P6 NM BS 727 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 RT STA 727 OUTER CHORD OF STR 18A, FASTENERS REMOVED PER WORK CARD HAVE CRACK INDICATIONS OUT OF HOLES PER HFEC INSP 2 E ACH. FASTENERS HOLES, FWD HOLE CRACK IS AT 2 O' CLOCK AND 7 O' CLOCK POS AFT HOLE CRACK AT 2 O' CLOCK AND 3 O' CLOCK PO S. REMOVED RT 727 CHORD, APPLIED FAYED SEAL IAW B737 SRM 51-20-4. INSTALLED 727 CHORD STR TIE AND SPLICES IAW SRM 51-3 0-2 AND SB 53-1088. FABRICATED REPAIR DOUBLER AND INSTALLED IAW BOEING MESSAGE ITEM NR 4 AND DWG NR 65C37277 AND RES 98 1562 AND 981583. 2 L 7 2 4F RT A16WE 1998100900039 19981009 00039 NM 1998 10 9 VJ9800450 1 19980901 A 5320 BRACKET BOEING 737 7372P6 NM BS 520 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FWD CARGO STA 520 FLOOR SUPPORT L-BRACKET HAS SURFACE CORROSION FROM 27L-27R. BLENDED CORROSION, FOUND TO BE OUT OF LIM ITS PER SRM 53-10-1. FABRICATED REPAIR, TREATED, PRIMED, AND INSTALLED REPAIR ANGLE WET WITH SEALANT IAW B 737 51-10-2, MM 51-21-31, SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900040 19981009 00040 NM 1998 10 9 VJ9800451 1 19980904 A 5320 STRAP BOEING 737 7372P6 NM BS 430 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FWD CARGO FLOOR BOARD STRAP AT STA 430 HAS SURFACE CORROSION. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR S TRAP, TREATED, PRIMED, AND INSTALLED REPAIR AND NUT PLATES IAW SRM 51-10-6, 51-30-2, AND 51-10-2. 2 L 7 2 4F RT A16WE 1998100900041 19981009 00041 NM 1998 10 9 VJ9800452 1 19980909 A 5753 SKIN BOEING 737 7372P6 NM RT TE FLAP DAMAGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 RT I/B TRAILING EDGE FLAP AFT FLAP FWD SKIN PIERCED AND CHIPPED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABR ICATED SKIN FOR LEADING EDGE AFT FLAP IAW 57-50-1 PG 43 AND EO NR 981458. INSTALLED FABRICATED LEADING EDGE IAW SRM 51- 30-2, 57-50-4, AND EO NR 981458. 2 L 7 2 4F RT A16WE 1998100900042 19981009 00042 NM 1998 10 9 VJ9800453 1 19980915 A 5730 SKIN BOEING 737 7372P6 NM LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 SPOT OF CORROSION TOP LT WING AFT NR 1 SLAT CENTER AREA. MECH REMOVED CORROSION OUT OF LIMITS IAW SRM 51-10-6 AND 57-30 -1 FIG 5. CUT OUT CORRODED SECTION, FABRICATED DOUBLER AND FILLER, DRILLED, DEBURRED, COUNTERSUNK, TREATED, PRIMED, AND INSTALLED IAW SRM 57-30-3. 2 L 7 2 4F RT A16WE 1998100900043 19981009 00043 NM 1998 10 9 VJ9800454 1 19980904 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 277 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION UNDER TWO NUT PLATES ON UNDERSIDE OF BS 277 FLOORBEAM UPPER CAP, AFT HORIZ FLANGE LBL 16 AND 23. REMOVED CORR OSION OUT OF LIMITS LBL 17 IAW SRM 53-10-9. FABBED FLOORBEAM REPAIR, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 53- 10-9 FIG 6, 51-10-2, MM 51-21-31, AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900044 19981009 00044 NM 1998 10 9 VJ9800455 1 19980903 A 5320 SUPPORT BOEING 737 7372P6 NM BS 277-294 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION ON LONGITUDINAL FLOOR SUPPORT IN FWD LAV DOOR WAY. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICAT ED REPAIR, ALODINED, AND PRIMED AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, MM 51-21-31, AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900045 19981009 00045 NM 1998 10 9 VJ9800456 1 19980901 A 5320 CHANNEL BOEING 737 7372P6 NM BS 283 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LOWER END OF FWD DOOR JAM CORRODED BS 283, LBL 11. CUT CORROSION SECTION U CHANNEL, FORMED REPAIR ANGLE 1 EACH, TREATED , PRIMED, AND INSTALLED IAW SRM 51-10-2, 51-40-3. 2 L 7 2 4F RT A16WE 1998100900046 19981009 00046 NM 1998 10 9 VJ9800457 1 19980830 A 5320 SUPPORT BOEING 737 7372P6 NM BS 294 -312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LONG FLOOR SUPPORT BETWEEN BS 294 AND 312 FLOORBEAMS CORRODED BEYOND LIMITS. REMOVED CORROSION OUT OF LIMITS IAW SRM 53 -10-1. FABRICATED FLOOR SUPPORT REPAIR, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, 51-30-2, AND M M 51-21-31. 2 L 7 2 4F RT A16WE 1998100900047 19981009 00047 NM 1998 10 9 VJ9800458 1 19980902 A 5320 SUPPORT BOEING 737 7372P6 NM BS 312-328 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LONG FLOOR SUPPORT CORRODED BETWEEN BS 312 AND 328 FLOORBEAMS, RBL 10. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT REPAIR, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, MM 51-21-31 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900048 19981009 00048 NM 1998 10 9 VJ9800459 1 19980829 A 5320 SUPPORT BOEING 737 7372P6 NM BS 320 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION AROUND NUT PLATE HOLE, UPPER AND LOWER SIDES OF LATERAL FLOOR SUPPORT FWD FLANGE BS 320, RBL 10 TO 30. REMOVE D CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, MM 51-21-31, AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900049 19981009 00049 NM 1998 10 9 VJ9800480 1 19980928 A 5320 SUPPORT BOEING 737 7372P6 NM BS 320 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION AROUND NUT PLATE HOLES ON UPPER AND LWR SIDES OF FWD FLANGE OF BS 320 LATERAL FLOOR SUPPORT, RBL 30-56. CLEAN ED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT, ALODINED, PRIMED, AND INSTALLED FLOOR SUPPORT IA W B737 51-40-3, 51-10-2, MM 51-21-31, SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900050 19981009 00050 NM 1998 10 9 VJ9800481 1 19980904 A 5320 SUPPORT BOEING 737 7372P6 NM BS 1009-1016 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION ON DIAGONAL FLOOR SUPPORT BETWEEN BS 986 AND 1016 FLOORBEAMS LBL 4-15. REMOVED CORROSION BEYOND LIMITS STA 10 09-1016 IAW SRM 53-10-1. FABRICATED REPAIR, TREATED, PRIMED, AND INSTALLED REPAIR IAW 51-40-4, 51-20-2, MM 51-21-31, AN D SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900051 19981009 00051 NM 1998 10 9 VJ9800483 1 19980907 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 1016 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION FOUND SCATTERED THOUGHOUT FWD HORIZONTAL STAB FLANGE OF BS 1016 FLOORBEAM UPPER CAP, LBL 37 RBL 37. REMOVED C ORROSION FROM BS 1016 FLOORBEAM UPPER CAP LBL 37, RBL 37, MAT BL 0 TO RBL 37 IS .002 WITHIN LIMITS IAW SRM 51-10-6 AND 5 3-10-1. TREATED AND PRIMED BL 0 RBL 37 IAW SRM SRM 51-10-2, MM 51-21-31. MAT LOSS LBL 12 .065 AND LBL 33 .045 OUT OF L IMITS IAW SRM 53-10-1. FABRICATED FLOORBEAM REPAIR FROM BAC 1490-2831-.080 IAW 53-10-9. DRILLED, DEBURRED, COUNTESUNK, AND INSTALLED REPAIRS IAW SRM 51-10-4, 53-10-9, 51-30-2. 2 L 7 2 4F RT A16WE 1998100900052 19981009 00052 NM 1998 10 9 VJ9800484 1 19980903 A 5320 SUPPORT BOEING 737 7372P6 NM BS 294.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LT FWD LAV; AFT BULKHEAD SUPPORT HAS CORRODED FASTENERS AND IS CORRODED AT FWD EDGE STA 294.5, LBL 29. REMOVED CORROSIO N IAW SRM 51-10-6. MAT LOSS .019 OUT OF LIMITS IAW SRM 53-10-1. FABRICATED NEW FLOOR SUPPORT REPAIR FROM BAC 1510-335, IAW SRM 51-40-3. ALODINED AND PRIMED IAW SRM 51-10-2, MM 51-21-31. INSTALLED NEW FLOOR SUPPORT REPAIR IAW SRM 51-30-2 . 2 L 7 2 4F RT A16WE 1998100900053 19981009 00053 NM 1998 10 9 VJ9800485 1 19980902 A 5320 PANEL BOEING 737 7372P6 NM LT LAVATORY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LT AFT VANITY LOWER ACCESS COVER PLATE CORRODED. REMOVED CORROSION FROM THE ACCESS PANEL, OUT OF LIMITS IAW SRM 51-10-1 PG 5. FABRICATED 1 COVER PLATE FROM 6061 T6-.050 IAW SRM 51-10 FIG 7, UPON REMOVAL OF ACCESS PANEL FOUND .75 INCH CRAC K IN MATING FLANGE. STOP DRILLED CRACK IAW SRM 51-10-1 PG 6B. FABRICATED REPAIR FOR MATING FLANGE FROM 2024 T3- .032 I AW SRM 51-10-1 PG 18A. INSTALLED NEW FLANGE REPAIR AND ACCESS PLATE IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900054 19981009 00054 NM 1998 10 9 VJ9800486 1 19980901 A 5320 DOUBLER BOEING 737 7372P6 NM E/E COMP DOORWAY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 E/E COMPARTMENT DOOR OPENING IS CORRODED AND HAS BROKEN RIVET AT AFT DOUBLER LT AFT CORNER, FWD OF STA 344 LBL 9.5. REM OVED CORROSION OUT OF LIMITS IAW SRM 51-10-2, 52-01 FIG 1. REMOVED CORRODED DOUBLER AND FABRICATED NEW DOUBLER IAW SRM 51-30-02. ALODINED, PRIMED, DRILLED, DEBURRED, AND INSTALLED DOUBLER IAW 737 51-10-02, 51-30-02, AND 51-20-05. 2 L 7 2 4F RT A16WE 1998100900055 19981009 00055 NM 1998 10 9 VJ9800487 1 19980905 A 5311 FRAME BOEING 737 7372P6 NM AFT GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 HEAVY CORROSION ALONG FWD EDGE OF FLOORING IN AFT GALLEY. REMOVED BOTTOM OF GALLEY FRAME AND HONEYCOMB PANEL. FABRICAT ED 7 NEW ANGLES AND BOTTOM PANEL. INSTALLED ANGLES, PANEL AND BOTTOM FRAME IAW SRM 51-30-2, 51-10-6, 51-20-2 AND 51-40- 10. 2 L 7 2 4F RT A16WE 1998100900056 19981009 00056 NM 1998 10 9 VJ9800488 1 19980904 A 5241 DOOR BOEING 737 7372P6 NM GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LWR EDGE OF O/B COMPARTMENT DOOR CORRODED ON G-2 GALLEY. REMOVED O/B COMPT DOOR CORROSION OUT OF LIMITS IAW SRM 51-40-1 0. FABRICATED NEW DOOR AND INSTALLED IAW SRM 51-40-10. 2 L 7 2 4F RT A16WE 1998100900057 19981009 00057 NM 1998 10 9 VJ9800489 1 19980909 A 5321 FLOOR BOEING 737 7372P6 NM GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 HEAVY CORROSION ALONG FWD EDGE OF G-2 GALLEY FLOOR. REMOVED CORROSION BEYOND LIMITS OF FLOOR AND LOWER I/B WALL IAW SRM 51-30-2. FABRICATED SECTION OF WALL AND GALLEY FLOOR IAW SRM 51-40-10 PG 4-5. INSTALLED REPAIR PARTS IAW SRM 51-30-0, 51-40-10, AND 51-30-2. 2 L 7 2 4F RT A16WE 1998100900058 19981009 00058 NM 1998 10 9 VJ9800490 1 19980914 A 2530 ICE COMPT BOEING 737 7372P6 NM NR 2 GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 INNER SKIN OF LWR O/B COMPARTMENT (ICE) DOOR LOOSE AND CRACKED AT LWR END, NR 2 GALLEY. REMOVED INNER SKIN FOUND ON DOO R OUT OF LIMITS IAW SRM 51-10-6. FABRICATED NEW DOOR AND U CHANNEL, INSTALLED DOOR IAW SRM 51-40-10, 51-30-2. 2 L 7 2 4F RT A16WE 1998100900059 19981009 00059 NM 1998 10 9 VJ9800491 1 19980915 A 5730 SKIN BOEING 737 7372P6 NM WS 329 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 TOP OF WING L/E SURFACE CORROSION THRU OUT. REMOVED CORROSION WS 329 OUT OF LIMITS IAW B737 57-30-1 AND 57-30-2. CUT O UT AND FABRICATED 2 DOUBLER AND 1 FILLER, DRILLED, DEBURRED, TREATED, AND PRIMED IAW B737 TSR NR B 737-75-010 AND SRM 57 030-3. INSTALLED REPAIRED PARTS IAW TSR NR B737-57-010 AND B737 SRM 57-30-3. 2 L 7 2 4F RT A16WE 1998100900060 19981009 00060 NM 1998 10 9 VJ9800492 1 19980831 A 5320 BRACKET BOEING 737 7372P6 NM WS 75 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LOWER FWD I/B OF LT I/B LANDING LIGHT BRACKET 1 HAS CORROSION AT WS 75. REMOVED SUPPORT PLATE DUE TO CORROSION OUT OF L IMITS IAW SRM 51-30-2, 57-10-1. FABRICATED REPAIR SUPPORT PLATE IAW SRM 51-20-1 AND INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900061 19981009 00061 NM 1998 10 9 VJ9800493 1 19980831 A 5312 BULKHEAD BOEING 737 7372P6 NM BS 294.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 DEEP GOUGE IN FWD SIDE OF BS 294.5 PRESS BULKHEAD AT TOP OF NLG UPLOCK/DOWNLOCK UPLOCK CYCLE, BETWEEN DOWNLOCK LINK ATTA CHED FITTINGS. CUT OUT GAUGE AREA IAW RES 981424. FABRICATED 2 DOUBLERS, TREATED, PRIMED, AND INSTALLED IAW SRM 51-10- 2, MM 51-21-51, AND SRM 51-30-2. BACK SEALED REPAIR IAW SRM 51-20-4. 2 L 7 2 4F RT A16WE 1998100900062 19981009 00062 NM 1998 10 9 VJ9800494 1 19980901 A 5320 ANGLE BOEING 737 7372P6 NM BS 297-334 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION UNDER NUT PLATES ON UNDERSIDE OF R-1 DOOR THRESHOLD SCUFF PLATE ATTACH ANGLE, BS 297 TO 334. REMOVED CORROSIO N OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR STRAP FORM 7075 T6 .100. ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-10-2, MM 51-20-11, AND SRM 51-40-3. 2 L 7 2 4F RT A16WE 1998100900063 19981009 00063 NM 1998 10 9 VJ9800495 1 19980904 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 294 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION SCATTERED THRU OUT UPPER CAP OF BS 294 FLOORBEAM LBL 40-RBL 53. REMOVED CORROSION OUT OF LIMITS LBL 40 AND ME CH REMOVED CORROSION OUT OF LIMITS LBL 20-RBL 26. FABRICATED REPAIR PARTS, DRILLED UP, DEBURRED, TREATED, AND PRIMED AL L REPAIR PARTS AND EXISTING FLOORBEAM IAW SRM 51-10-2, 53-10-9, MM 51-21-21. INSTALLED REPAIR PARTS IAW SRM 51-10-9 AND 51-30-2. 2 L 7 2 4F RT A16WE 1998100900064 19981009 00064 NM 1998 10 9 VJ9800496 1 19980903 A 5321 FLOOR BOEING 737 7372P6 NM BS 967-986 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION AROUND FLOOR PANEL FASTENER HOLES ON UNDERSIDE OF CUSP MEMBRANE AT R-2 THRESHOLD, BETWEEN BS 967 TO 986 FLOORB EAMS. CLEANED CORROSION MATERIAL LOSS BETWEEN STA 977.5 TO 982.5 OUT OF LIMITS IAW SRM 53-10-1. FABRICATED REPAIR DOUB LER, DRILLED, DEBURRED, TREATED, AND PRIMED IAW SRM 51-40-2. INSTALLED DOUBLER IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900065 19981009 00065 NM 1998 10 9 VJ9800497 1 19980828 A 5314 PANEL BOEING 737 7372P6 NM NR 1 PYLON CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CHAFED AREA IN ACCESS PANEL AFT UNDERSIDE AREA NR 1 ENGINE PYLON. BLENDED CHAFED AREA OUT OF LIMITS IAW SRM 54-10-1. F ABRICATED DOUBLER, DRILLED, DEBURRED, ALODINED, AND PRIMED IAW SRM 51-10-2. INSTALLED DOULER IAW SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900066 19981009 00066 NM 1998 10 9 VJ9800499 1 19980904 A 5315 FLOORBEAM BOEING 737 7372P6 1C84609 NM FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FLOORBEAM AT FS 344 LBL 45 - RBL 12 OUT OF LIMITS. REMOVED CORRODED SECTION OF FLOORBEAM, FABRICATED REPAIR FLOORBEAM F ROM BAC 1505-10067 AND 4 SPLICES FROM 1490-2738. DRILLED UP, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW SRM 53-10-9 F IG 5, 51010-2, 51-30-2 AND MM 51-20-11. 2 L 7 2 4F RT A16WE 1998100900067 19981009 00067 NM 1998 10 9 VJ9800500 1 19980903 A 5320 SUPPORT BOEING 737 7372P6 NM BS 213-328 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FLOOR SUPPORT AT FS 312 TO 328 LBL 12 IS CORRODED OUT OF LIMITS. REMOVED FLOOR SUPPORT AND FABRICATED REPAIR FROM BAC 1 505-100604-15.625 IAW SRM 51-30-2 AND 51-40-4. INSTALLED REPAIR IAW B737 SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900068 19981009 00068 NM 1998 10 9 VJ9800501 1 19980903 A 5320 SUPPORT BOEING 737 7372P6 NM BS 328-344 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FLOOR SUPPORT AT FS 328 TO 344 LB 12 IS CORRODED OUT OF LIMITS. REMOVED FLOOR SUPPORT AND FABRICATED REPAIR FROM BAC 15 05-100604-15.5 IAW SRM 51-30-2 AND SRM 51-40-4. TREATED, PRIMED, AND INSTALLED IAW SRM 51-10-2, 51-20-11, 51-30-2. 2 L 7 2 4F RT A16WE 1998100900069 19981009 00069 NM 1998 10 9 VJ9800502 1 19980903 A 5320 SUPPORT BOEING 737 7372P6 NM FS 328-344 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FLOOR SUPPORT AT FS 328 TO 344 RBL 12 CORRODED OUT OF LIMITS. REMOVED FLOOR SUPPORT AND FABRICATED PARTS IAW SRM 51-40- 4. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 51-10-2, MM 51-21-21 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900070 19981009 00070 NM 1998 10 9 VJ9800503 1 19980904 A 5347 1A365422 SEAT TRACK BOEING 737 7372P6 NM BS 344 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 SEAT TRACK AT FS 344 RBL 22 HAS CORROSION IN TRACK. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK AND FABRICATED SEAT TRACK IAW B737 SRM 53-10-1 AND SRM 53-10-5. TREATED, PRIMED, AND INSTALLED PARTS IAW SRM 51-10-2, MM 5 1-21-21 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900071 19981009 00071 NM 1998 10 9 VJ9800504 1 19980904 A 5320 SUPPORT BOEING 737 7372P6 NM BS 344-360 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FLOOR SUPPORT AT FS 344 TO RBL 12 CORRODED OUT OF LIMITS. REMOVED FLOOR SUPPORT, IAW B737 SRM 51-40-4. TREATED, PRIMED , AND INSTALLED IAW SRM 51-10-2, MM 51-21 AND SRM 51-30-2. 2 L 7 2 4F RT A16WE 1998100900072 19981009 00072 NM 1998 10 9 VJ9800505 1 19980928 A 5320 SUPPORT BOEING 737 7372P6 NM BS 294-312 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 LONGITUDINAL FLOOR SUPPORT CORRODED BETWEEN BS 294-312 FLOORBEAMS, RBL 11. REMOVED CORROSION OUT OF LIMITS IAW SRM 53-1 0-1. FABRICATED FLOOR SUPPORT, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-40-3, 51-10-2, MM 51-21-31, AND SRM 51 -30-2. 2 L 7 2 4F RT A16WE 1998100900073 19981009 00073 NM 1998 10 9 VJ9800506 1 19980917 A 5313 STRINGER BOEING 737 7372P6 NM BS 219 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 AT FUS STA 219L STR 27L CORRODED BEYOND LIMITS THE SRM LIMIT UNDER STR TIE CLIP. CUT OUT SECTION OF CORRODED STRINGER. FABRICATED REPAIR STRINGER, DRILLED UP, DEBURRED, TREATED, PRIMED, AND INSTALLED IAW SRM 53-10-3 FIG 1, 51-10-2 AND 51- 20-11. 2 L 7 2 4F RT A16WE 1998100900074 19981009 00074 NM 1998 10 9 VJ9800507 1 19980830 A 5347 SEAT TRACK BOEING 737 7372P6 NM BS 767 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CABIN INTERIOR LEFT SEAT TRACK IS CHIPPED AT SEAT ROW 19. REMOVED OUT OF LIMITS SECTION OF SEAT TRACK, DRILLED UP, DEBU RRED, TREATED, PRIMED, AND INSTALLED NEW SECTION IAW B737 53-10-5 FIG 1, 51-10-2, ANS 51-30-2. 2 L 7 2 4F RT A16WE 1998100900075 19981009 00075 NM 1998 10 9 VJ980460 1 19980828 A 5320 SUPPORT BOEING 737 7372P6 NM BS 320 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 CORROSION AROUND NUT PLATE HOLES ON UPPER AND LOWER SIDES OF FWD FLAGE OF BS 320 LATERAL FLOOR SUPPORT, RBL 30-56. CLEA NED CORROSION OUT OF LIMITS IAW SRM 53-10-1. FABRICATED FLOOR SUPPORT, ALODINED, PRIMED, AND INSTALLED FLOOR SUPPORT IA W 51-40-3, 51-10-2, MM 51-21-31, AND 51-30-2. 2 L 7 2 4F RT A16WE 1998100900076 19981009 00076 NM 1998 10 9 VJ98498 1 19980904 A 5315 FLOORBEAM BOEING 737 7372P6 NM BS 328 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 EICJW 21355 FLOORBEAM AT FS 328 HAS CORROSION AND FLOORBEAM OUT OF LIMITS FROM RBL 12 RBL 55. REMOVED SECTION OF FLOORBEAM AND FABR ICATED REPAIR SECTION IAW SRM 53-10-9 FIG 5. ALODINED, PRIMED, AND INSTALLED REPAIRS PARTS IAW SRM 51-10-2, MM 51-21-21 AND SRM 51-30-2 AND 53-10-9 FIG 5. 2 L 7 2 4F RT A16WE 1998100900077 19981009 00077 1998 10 9 VJ9800510 4 19981005 A 3422 25883024 DIRECTIONAL GYRO DOUG DC9 DC932 3022066 WP E & E COMPT UNSERVICEABLE A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 938VV 47442 NR 1 COMPASS SYSTEM FLAGS WOULD PERIODICALLY APPEAR WITH INSTRUMENT FAILURE LIGHT. SUBSEQUENTLY NR 2 COMPASS FLAGS APPE ARED. IN ADDITION EXPERIENCED BLEED THRU AND INTERMITTENT COMMUNICATION ON NR 1 AND NR 3 COMM. FLIGHT CREW ELECTED TO RETURN TO DEPARTING STATION. REPLACED F/O DIRECTIONAL GYRO, CLEANED CONNECTORS CAPTAINS INSTRUMENT AMPLIFIER AND COMPAS S INDICATOR, OPS CHECKED NORMAL IAW MM 34-00. REPLACED NR 3 COMM CONTROL PANEL AND NR 2 COMM RT, OPS CHECKED NORMAL IAW MM 23-00. 2 L 7 2 4F A6WE 1998100900078 19981009 00078 WP 1998 10 9 VJ9800511 1 19980910 A 5260 3917698504 SKIN DOUG DC9 DC932 3022066 WP VENTRAL STAIRS CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 AFT VENTRAL STAIRS HAD DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND CORRODED FITTING IAW DC9 SRM 51-30-5, 51-30-0, 51-10-4 AND MM 52-63-0, PG 501. 2 L 7 2 4F A6WE 1998100900079 19981009 00079 WP 1998 10 9 VJ9800512 1 19980917 A 5620 99115351 WINDOW PANEL DOUG DC9 DC932 3022066 WP FS 813 - 869 LIGHTNING STRIKE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 RT WINDOW PANE HAS LIGHTNING STRIKE OUT OF LIMIT AT FS 813 TO 869. REPLACED WINDOW PANEL IAW DC9 SRM 51-30-2, 51-10-4, 51-10-3 AND 53-05, FIG 111. 2 L 7 2 4F A6WE 1998100900080 19981009 00080 WP 1998 10 9 VJ9800513 1 19980920 A 5523 TAB DOUG DC9 DC932 3022066 WP RT ELEVATOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 RT ELEVATOR GEAR TAB HAS 1 INCH DIAMETER CORROSION SPOT. CUT OUT CORROSION, CLEANED AREA, FABRICATED AND INSTALLED DOUB LER IAW DC9 SRM 51-70-2. 2 L 7 2 4F A6WE 1998100900081 19981009 00081 WP 1998 10 9 VJ9800514 1 19980928 A 5530 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 VERTICAL SKIN ON LT AND RT UPPER AND LOWER BANANA FAIRING CHAFED. RT UPPER BANANA FAIRING SKIN CHAFED OUT OF LIMIT IAW DC9 SRM 55-01. REMOVED SKIN, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2 AND 55-01. 2 L 7 2 4F A6WE 1998100900082 19981009 00082 WP 1998 10 9 VJ9800515 1 19980916 A 5320 2652479 SUPPORT DOUG DC9 DC932 3022066 WP BS 187 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 SUB FLOOR AT FS 187, LBL22, CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED NEW SUB FLOOR AND FLOOR SUPPORT IAW DC9 SRM 51-10-2, 51-10-4, AND 51-10-3. 2 L 7 2 4F A6WE 1998100900083 19981009 00083 WP 1998 10 9 VJ9800516 1 19980917 A 5320 602576 SUPPORT DOUG DC9 DC932 3022066 WP BS 160-200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FLOORBEAM AT FS 160 TO 200, RBL 45, CORRODED BEYOND LIMIT ON TOP AND AROUND SCREW HOLES. REMOVED CORRODED SECTION, FABR ICATED AND INSTALLED NEW SECTION AT FLOOR SUPPORT IAW DC9 SRM 51-10-1, 51-10-3, 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1998100900084 19981009 00084 WP 1998 10 9 VJ9800517 1 19980917 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 A CRACK AT FASTENER HOLE FS 617, L1R, DETECTED BY HFEC INSPECTION. CUT OUT CRACK, FABRICATED AND INSTALLED REPAIR DOUBL ER IAW DC9 SRM 51-30-0, 51-10-3 AND SR 09530129. 2 L 7 2 4F A6WE 1998100900085 19981009 00085 WP 1998 10 9 VJ9800518 1 19980922 A 5320 602576 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FLOOR SUPPORT AT FS 160, RBL 0-45, CORRODED BEYOND LIMIT. FABRICATED AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10- 3, 51-30-2, 51-10-4, 51-10-2. 2 L 7 2 4F A6WE 1998100900086 19981009 00086 NM 1998 10 9 VJ9800381R1 1 19980911 A 3240 BRAKE BOEING 737 737214 138446R NM NR 3 FIRE A ZZDA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 15 460AT 20158 NR 3 BRAKE CAUGHT ON FIRE AFTER HIGH SPEED TAXI TEST WAS PERFORMED; TEST COMMENCED AT 100 KNOTS AND AT 80 KNTS LOST PRES SURE AND WENT TO STOP ON RIGHT BRAKES. ATC ALERTED FLIGHT CREW FIRE WAS EMINATING FROM THE RIGHT WHEEL WELL AREA. BROU GHT THE AIRCRAFT TO A STOP. INSPECTED AND REPAINTED ALL BURNED SURFACES. R & R THE LOWER RT MLG LOWER STRUT AND WHEEL WELL DOOR IAW 32-13-11. PERFORMED GEAR SWING IAW 32-32-00. REPLACED GROUND SPOILER INTERLOCK VALVE CABLE IAW 27-62-51. REPLACED THE RT MLG ELECTRICAL HARNESS IAW 32-11-121. REPLACED THE RT MLG SHIMMY DAMPER ASSY AND HYD HOSE IAW 32-11-8 1. REPLACED THE NR 3 AND NR 4 MLG BRAKES AND TIRES. REPLACED THE NR 4 MLG ANTI-SKID TRANSDUCER IAW 32-42-11. 2 L 7 2 4F A16WE 1998100900087 19981009 00087 WP 1998 10 9 VJ9800415R1 1 19980918 A 3260 UPLOCK LATCH DOUG DC9 DC932 3022066 WP LT MLG LACK OF LUBE A ZZDA K NONE O OTHER CL CLIMB 1 SO 15 918VV 47320 LT GEAR UNSAFE LIGHT ILLUMINATED AFTER T/O WITH GEAR HANDLE UP, WHEN GEAR HANDLE PUT BACK DOWN, GEAR DOOR LIGHT ILLUMINA TED. INSPECTED AND FOUND DOOR UPLOCK LATCH FROZEN. CLEANED AND LUBRICATED LATCH IAW MM 32-00. OPS CHECKED GOOD WITH G EAR SWING IAW 32-00. 2 L 7 2 4F A6WE 1998100900088 19981009 00088 NM 1998 10 9 K3HA980117 1 19981004 A 3350 0816300610 LIGHT BOEING 727 727225 1384077 NM CABIN DAMAGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHTING INOP AND TRACK TORN UP APPROXIMATELY 3 FEET IN LENGTH. INSTALLED NEW EMERGENCY PATH LIGHT SOCKE T ASSEMBLY (P/N 08169-01), INSTALLED 3 NEW RED LENSES (P/N 07912-3), INSTALLED BULB, INSTALLED NEW 3 FOOT SECTION OF T RACK. OPS CHECK OK. 2 L 7 3 4F A3WE 1998100900089 19981009 00089 WP 1998 10 9 CALA9801894 1 19980930 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND A .375 INCH CRACK IN FUSELAGE SKIN AT STA 1418, LONGERON 2R. REPAIRED IAW SRM 53-04, FIGURE 40. 2 L 7 2 4F A6WE 1998100900090 19981009 00090 WP 1998 10 9 CALA9801895 1 19981001 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND A 1 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. THE DOOR BEAM WAS REPLACED IAW WORK CARD 99-5240-1-0 002. 2 L 7 2 4F A6WE 1998100900091 19981009 00091 WP 1998 10 9 CALA9801896 1 19980924 A 5320 FITTING DOUG DC9 DC981 3022081 WP BS 1007 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14871 48022 INSPECTION FOUND LONGERON 30 END FITTING CORRODED IN AFT BAGGAGE BIN AT STA 1007. THE LONGERON END FITTING WAS REPLACED IAW ECRA 5314-01002. 2 L 7 2 4F A6WE 1998100900092 19981009 00092 NM 1998 10 9 CALA9801897 1 19980929 A 5330 SKIN BOEING 737 7373T0 1384582 NM COCKPIT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16310 23361 INSPECTION FOUND A .25 INCH CRACK IN L-1 COCKPIT WINDOW FRAME SKIN. A REPAIR WAS INSTALLED IAW ECRA 5330-02710. 2 L 7 2 4F RT A16WE 1998100900093 19981009 00093 NM 1998 10 9 CALA9801898 1 19980930 A 5320 INTERCOSTAL BOEING 727 727243 138408D NM BS 1050 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND INTERCOSTAL CORRODED AT BS 1050, STRINGER 28R. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10- 1, 51-30-2, AND 51-10-6. 2 L 7 3 4F RT A3WE 1998100900094 19981009 00094 NM 1998 10 9 CALA9801899 1 19980930 A 5330 SKIN BOEING 727 727243 138408D NM BS 1050 TORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A TEAR IN RT LOWER FUSELAGE SKIN AT STA 1050, STRINGER 28R. THE TORN AREA WAS CUT OUT AND A DOUBLER WA S INSTALLED IAW SRM 53-30-3 AND 51-10-1. 2 L 7 3 4F RT A3WE 1998100900095 19981009 00095 NM 1998 10 9 CALA9801900 1 19981001 A 5280 WEB BOEING 727 727232 1384082 NM RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND A 1 INCH CRACK IN RT MLG FLYING DOOR WEB FORWARD OF AFT HINGE FITTING. THE HINGE WEB WAS REMOVED IAW S RM 51-30-2. A NEW HINGE WEB WAS INSTALLED IAW SRM 52-80-1, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998100900096 19981009 00096 WP 1998 10 9 CALA9801901 1 19981001 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND BELTFRAME WEB CORRODED AT STA 1338 BETWEEN LONGERONS 25 AND 26. THE CORRODED AREA WAS CUT OUT, FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-01, FIGURE 4. 2 L 7 2 4F A6WE 1998100900097 19981009 00097 WP 1998 10 9 CALA9801902 1 19981001 A 3233 FITTING DOUG DC9 DC982 3022082 WP RT MLG ACTUATOR WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND RT MLG RETRACT ACTUATOR UPPER ATTACH COKE BOTTLE FITTING WORN. A NEW COKE BOTTLE FITTING AND BUSHINGS WERE INSTALLED IAW MM 57-40-02. 2 L 7 2 4F A6WE 1998100900098 19981009 00098 WP 1998 10 9 CALA9801903 1 19981002 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1322 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14814 49112 INSPECTION FOUND BELTFRAME CORRODED AT STA 1322 BETWEEN LONGERON 29L AND 29R. THE CORROSION WAS REMOVED, FILLER AND DOU BLERS INSTALLED IAW SRM 53-03, FIGURE 2A. 2 L 7 2 4F A6WE 1998100900099 19981009 00099 NM 1998 10 9 CALA9801904 1 19981004 A 5400 CHANNEL BOEING 737 7373T0 1384582 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17321 23372 INSPECTION FOUND A 10 INCH CRACK IN AFT CHANNEL INSIDE NR 1 PYLON ABOVE LOWER AFT FAIRING. A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-2. 2 L 7 2 4F RT A16WE 1998100900100 19981009 00100 NM 1998 10 9 CALA9801905 1 19981005 A 5720 BEAM BOEING 727 727243 138408D NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A .375 INCH CRACK IN LT WING J-BEAM ABOVE NR 7 SPOILER ACTUATOR. A REPAIR WAS INSTALLED IAW ECRA 5750- 02914. 2 L 7 3 4F RT A3WE 1998100900101 19981009 00101 NM 1998 10 9 CALA9801906 1 19981005 A 5523 SKIN BOEING 727 727243 138408D NM RT ELEVATOR TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DELAMINATED. THE RT ELEVATOR CONTROL TAB WAS REMOVED AND REPLACE D IAW MM 27-30-11. 2 L 7 3 4F RT A3WE 1998100900102 19981009 00102 NM 1998 10 9 CALA9801907 1 19981005 A 5753 652163571 SKIN BOEING 727 727243 138408D NM LT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND LT WING OUTBOARD AFT FLAP UPPER SURFACE DELAMINATED 9 TO 15 INCHES FROM OUTBOARD EDGE. THE LT OUTBOARD AFT FLAP ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-51-12, PAGE 401. 2 L 7 3 4F RT A3WE 1998100900103 19981009 00103 WP 1998 10 9 9810169851 1 19981001 A 5753 DOOR DOUG DC9 DC951 3022051 WP NR 8 SLAT BENT A NWAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 01 760NC 47708 DURING APPROACH, SLAT DISAGREEMENT LIGHT ILLUMINATED ON SLAT EXTENSION. CREW REQUESTED EMERGENCY EQUIPMENT ON STANDBY A S A PRECAUTION. AIRCRAFT WAS LANDED SAFELY USING FLAPS ONLY. MAINTENANCE FOUND NR 8 INBOARD SLAT TRACK DOOR BENT. ADJ USTED DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998100900104 19981009 00104 SO 1998 10 9 COMA9810224 1 19981004 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 264CA 14838 120256 EMERGENCY EXIT LIGHT INOP. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998100900105 19981009 00105 EA 1998 10 9 COMA9860289 1 19981001 A 2913 PV304448 PUMP CNDAIR CL600 CL6002B19 EA RT HYD SYST FAILED A COMA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 948CA 9340 3372 7079 RIGHT HAND HYDRAULIC PUMP FAILED. REPLACED THE RIGHT HAND ENGINE DRIVEN HYDRAULIC PUMP. 2 L 7 2 4F RT A21EA 1998100900106 19981009 00106 EA 1998 10 9 COMA9860290 1 19981003 A 2740 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STAB FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 946CA 8929 7072 CONFIG TRIM WARNING. REPLACED THE HORIZONTAL TRIM ACTUATOR. 2 L 7 2 4F RT A21EA 1998100900107 19981009 00107 EA 1998 10 9 COMA9860291 1 19981005 A 2613 WIRE CNDAIR CL600 CL6002B19 1900309 EA ENGINE OUT OF POSITION A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 912CA 7011 JET PIPE OVERHEAT FAIL WARNING. WIRING TERMINALS SHORTING TO ENGINE COWLING. INSULATED TERMINALS FROM COWLING. 2 L 7 2 4F RT A21EA 1998100900108 19981009 00108 NM 1998 10 9 UPS98227869 1 19981004 A 2611 SMOKE DETECTOR BOEING 727 72725C 138400H NM LAVATORY MALFUNCTIONED A IPXA K NONE O OTHER CR CRUISE 1 SO 01 947UP 19722 INSPECTION TYPE-N/A, SMOKE DETECTOR WENT OFF IN FLIGHT, NO SMOKE DETECTED. DEACTIVATED UNIT AND RESET RIGHT AFT LAV, RE PEAT WRITE UP 3. RIGHT AVE LAVATORY SMOKE DETECTOR INOP, DEFERRED PER MEL 26-17 M160233 ASSIGNED. 2 L 7 3 4F A3WE 1998100900109 19981009 00109 WP 1998 10 9 UPS98827860 1 19980922 A 5720 56412521 DOUBLER DOUG DC8 DC873F 302199F WP WS 307 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E LWR ACCESS PANEL DOUBLER CRACKED BETWEEN STA'S XFS 303 AND XFS 310.25. REMOVED, FABRICAT ED AND INSTALLED DOUBLER IAW DWG 5641252 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998100900110 19981009 00110 WP 1998 10 9 UPS98827861 1 19980922 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 6.225 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED AT AFT O/B FASTENER AT STA XOLDI 6.225. STOP DRILLED CRACK AND REPAI RED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998100900111 19981009 00111 WP 1998 10 9 UPS98827862 1 19980922 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 379.0 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 379.0. STOP DRILLED CRACKED AND REPAIRE D IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998100900112 19981009 00112 WP 1998 10 9 UPS98827863 1 19980922 A 5720 97532937 ANGLE DOUG DC8 DC873F 302199F WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E VERTICAL ANGLE CRACKED AT LWR END AT STA XS 250.089. REMOVED, FABRICATED AND INSTALLED A NGLE IAW DWG 9753293 AND SRM 51-3-0, 51-1-20D. 2 L 7 4 4F RT 4A25 1998100900113 19981009 00113 WP 1998 10 9 UPS98827864 1 19980927 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1740 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE-C, LONG 34L AT FS 1745 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED LONG 34L FROM FS 172 0 TO 1766 IAW SRM 53-5-1 FIG 7, 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998100900114 19981009 00114 WP 1998 10 9 UPS98827865 1 19980927 A 5320 5645332113 DOUBLER DOUG DC8 DC871F 302199D WP BS 920-940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE-C, FINGER DOUBLER BULGING AND POPPED FASTENER AT RBL 65 AT FS 920 TO 940. REMOVED, FABRICATED AND INSTA LLED FINGER DOUBLER IAW SRM 57-7-1 FIG 10, 51-1-9, 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998100900115 19981009 00115 WP 1998 10 9 UPS98827866 1 19980927 A 5320 5645332115 DOUBLER DOUG DC8 DC871F 302199D WP BS 940-960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE-C, FINGER DOUBLER BLOWN OUT AT RBL 65 AT FS 940 TO 960. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLE R IAW SRM 53-7-1 FIG 10, 51-1-9, 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998100900116 19981009 00116 WP 1998 10 9 UPS98827867 1 19980918 A 5320 3754041501 FITTING DOUG DC8 DC871F 302199D WP BS 270 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 748UP 45948 INSPECTION TYPE-C, NR 1 PIT AT STR 32L STA 270, DOOR OPEN STOP/FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998100900117 19981009 00117 EU 1998 10 9 QXEA9801371 1 19981002 A 2120 AIR DISTR FOKKER F28 F28MK4000 4990810 EU CABIN ODOR A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 09 481US 11230 DURING FLIGHT NOTICED AN EXHAUST SMELL IN THE COCKPIT AND CABIN FROM ROW 6. VISUALLY INSPECTED COCKPIT, CABIN, APU AREA AND CARGO AREAS. GROUND RAN BOTH ENGINES. ON DEFECTS NOTED. 2 L 7 2 4F RT A20EU 1998100900118 19981009 00118 EU 1998 10 9 QXEA9801372 1 19980930 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 481US 11230 EXIT SIGN ABOVE NR 2 GALLEY WILL NOT ILLUMINATE. RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900119 19981009 00119 EU 1998 10 9 QXEA9801373 1 19981001 A 3350 6008905 BATTERY PACK GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 481US 11230 RIGHT WING EVACUATION LIGHTS INOP. INSTALLED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900120 19981009 00120 EU 1998 10 9 QXEA9801374 1 19981002 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 483US 11233 EMERGENCY EXIT LIGHTS AT 8E INOP. RELAMPED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900121 19981009 00121 EU 1998 10 9 QXEA9801375 1 19981004 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 EMERGENCY EXIT LIGHTS AT 8E INOP. RELAMPED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900122 19981009 00122 EU 1998 10 9 QXEA9801376 1 19981003 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 EMERGENCY EXIT LIGHTS AT ROW 9 INOP. RELAMPED LIGHT ASSEMBLY, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900123 19981009 00123 EU 1998 10 9 QXEA9801377 1 19981001 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 488US 11240 UPPER EMERGENCY LIGHT AT GALLEY SERVICE INOP. RELAMPED LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900124 19981009 00124 EU 1998 10 9 QXEA9801378 1 19981002 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 EMERGENCY EXIT SIGN AFT SIDE OF ROW 8 (28 VOLT SIDE) INOP. RELAMPED 28 VOLT PORTION OF EMERGENCY EXIT SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900125 19981009 00125 EU 1998 10 9 QXEA9801379 1 19981003 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 498US 11181 OVERWING EXIT LIGHTS AT ROWS 8A AND 9A INOP. REMOVED AND REPLACED LAMPS AT ROWS 8A AND 9A, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900126 19981009 00126 NM 1998 10 9 QXEA9801380 1 19981003 A 3233 10700105 ACTUATOR DHAV DHC8 DHC8102 2809003 NM LT MLG MALFUNCTION A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 821PH 28419 7288 104 LEFT MAIN GEAR DOOR HANGS OPEN ABOUT 2 INCHES DURING FLIGHT. FERRIED AIRCRAFT FROM SEA TO PDX FOR REPAIRS. IN PDX REPL ACED UPLOCK ACTUATOR, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998100900127 19981009 00127 NM 1998 10 9 98FDEA00617 1 19981005 A 5320 65163175 CHORD BOEING 727 72725C 138400H NM BS 351.2 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 CORROSION (C-53-100-01,1) ON BS 351.2 FRAME BETWEEN STR 26 AND 27 LT. *S/D* REMOVED AND REPLACED BS 351.2 LOWER REINFO RCEMENT CHORD PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1998100900128 19981009 00128 NM 1998 10 9 98FDEA00618 1 19981005 A 5313 651844431 STRINGER BOEING 727 72722 1384002 NM BS 360-385 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 CORROSION (C53-224-03-1/2) ON UPPER SURFACE OF STR 26R, BS 380, RBL 16, WL 152. *S/D* REMOVED AND REPLACED CORRODED ST R BS 360-385, STR 26R, WL 152 PER FED-EX SRM 53-10-3. 2 L 7 3 4F A3WE 1998100900129 19981009 00129 NM 1998 10 9 98FDEA00619 1 19981005 A 5313 651844431 STRINGER BOEING 727 72722 1384002 NM BS 392 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 NR 0211 CORROSION (C53-224-03-1/2) TOP OF STR 26 FROM BS 381-400, LBL 29, WL 156 IN FWD E/E BAY. REMOVED AND REPLACED STR 26L FROM BS 384-413, LBL 29, WL 156 PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1998100900130 19981009 00130 WP 1998 10 9 98FDEA00620 1 19981005 A 5311 BELLFRAME DOUG DC10 DC1010 3022110 WP BS 1781 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 375FE 46613 UPPER INTERNAL FUSELAGE AREAE BS 1781, LONGERON 13L, FUSELAGE BELL FRAME CRACKED. REMOVED AND REPLACED DAMAGED AREA PER SRM 53-30-00 FIG 5. 2 L 7 3 4F A22WE 1998100900131 19981009 00131 WP 1998 10 9 98FDEA00621 1 19980908 A 5311 BELLFRAME DOUG DC10 DC1010 3022110 WP BS 1761 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 375FE 46613 UPPER INTERNAL FUSELAGE BS 1761, LONGERON 13L BELL FRAME CRACKED. 2 L 7 3 4F A22WE 1998100900132 19981009 00132 WP 1998 10 9 ABXA9800866 1 19981002 A 5610 5613217507 WINDOW TRIM DOUG DOUG DC8 DC863 302198A WP COCKPIT LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 820AX 46155 CAPTAIN'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. FOUND LOOSE WINDOW TRIM. RESECURED TRIM, WINDOW OPERATED F REELY. 2 L 7 4 4F 4A25 1998100900133 19981009 00133 WP 1998 10 9 ABXA9800867 1 19981001 A 5610 5613217507 WINDOW DOUG DOUG DC8 DC861 3021952 WP COCKPIT STUCK A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 843AX 46017 CAPTAIN'S SLIDING WINDOW (EMERG EXIT) DIFFICULT TO OPEN. WO ULD NOT OPEN FULLY. LUBRICATED MECHANISM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998100900134 19981009 00134 WP 1998 10 9 ABXA9800868 1 19981001 A 5610 591297733 WINDOW TRIM DOUG DOUG DC8 DC863 302198A WP COCKPIT LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 821AX 46116 CAPTAIN'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN. INSTALLED AND SECURED WINDOW TRIM ON AFT SECTION OF WINDOW, OPS C HECKED GOOD. 2 L 7 4 4F 4A25 1998100900135 19981009 00135 WP 1998 10 9 MWEA98981 1 19981001 A 3350 6011777 BATTERY PACK DOUG DC9 DC914 3022034 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 600ME 45725 THE LEFT NACELLE EMERGENCY LIGHT IS INOPERATIVE. MTC REMOVED AND REPLACED LEFT NACELLE LIGHT BATTERY PACK. 2 L 7 2 4F A6WE 1998100900136 19981009 00136 WP 1998 10 9 MWEA98982 1 19981004 A 5312 591013037 ANGLE DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FOUND CRACK ON AFT SIDE OF AFT PRESSURE BULKHEAD -37 ANGLE. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998100900137 19981009 00137 WP 1998 10 9 MWEA98983 1 19981004 A 5330 59259911 SKIN DOUG DC9 DC932 3022066 WP BS 945 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FOUND CORROSION AT AFT CARGO COMPARTMENT AT FS 945 BETWEEN LONGERON 27 AND 28 RIGHT. MTC REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998100900138 19981009 00138 WP 1998 10 9 MWEA98984 1 19981004 A 5330 592032339 SKIN DOUG DC9 DC932 3022066 WP BS 324-356 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 REPLACED TEMPORARY REPAIR WITH A PERMANENT SKIN REPAIR AT FUSELAGE STATION 324 TO 356 BETWEEN LONGERONS 21R AND 22R. MT C FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998100900139 19981009 00139 WP 1998 10 9 MWEA98985 1 19981003 A 2560 113317 COVER DOUG DC9 DC915 3022036 WP PAX DOOR LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 THE FORWARD ENTRANCE SLIDE COVER FELL OFF. MTC REINSTALLED FORWARD ENTRANCE SLIDE COVER. 2 L 7 2 4F A6WE 1998100900140 19981009 00140 NM 1998 10 9 SCNA98113 1 19980928 A 3397 WIRE BOEING 727 727259 138408J NM CABIN LOOSE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD POSTION OF THE EMERGENCY PATH LIGHTING WAS FOUND TO BE INOPERATIVE. REPAI RED WIRE IAW SWP 201013. OPERATIONALLY CHECKS GOOD IAW B727 MM 33501. 2 L 7 3 4F A3WE 1998100900141 19981009 00141 NM 1998 10 9 SCNA98114 1 19980930 A 3350 1102832 LIGHT BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REP LACED THE ASSOCIATED LIGHT ASSEMBLY, LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998100900142 19981009 00142 NM 1998 10 9 SCNA98115 1 19980930 A 3350 SIGN BOEING 727 727259 138408J NM L 4 DOOR INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE LOWER EMERGENCY EXIT SIGN AT THE L4 DOOR WAS FOUND TO BE INOPERATIVE. FOUND RIBBON TO LOWER L4 DOOR EMERGENCY EXIT SIGN CUT. REPAIRED RIBBON AND OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1998100900143 19981009 00143 NM 1998 10 9 SCNA98116 1 19980929 A 3350 110049 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECK, THE AFT CABIN EMERGENCY TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLAC ED THE POWER SUPPLY FOR THE AFT CABIN FLOOR TRACK LIGHTING, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998100900144 19981009 00144 WP 1998 10 9 ARWA981001 1 19980930 A 3030 PITOT HEAT DOUG DC8 DC862 3021970 WP FUSELAGE INOPERATIVE A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 8968U 46069 PITOT HEATER INOP, LIGHT ON ZERO INDICATING ON OAI 1 AND OA. RESET CIRCUIT BREAKER ON PITOT HEAT SYSTEM, HEATER INOP. L T OPS CHECKED NORMAL PER MM 30-32, OAT 1 AND OAT 2 IS FUNCTION OF OLEO SWITCH, OPERATION NORMAL. 2 L 7 4 4F 4A25 1998100900145 19981009 00145 WP 1998 10 9 ARWA981002 1 19980930 A 3030 MO102 DETECTOR UNIT DOUG DC8 DC862 3021970 WP PITOT HEAT INOPERATIVE A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 8968U 46069 RETURNED TO BLOCK, ACCESSED CURRENT DETECTOR UNIT LIGHT ILLUMINATED. REMOVED AND REPLACED CURRENT DETECTOR UNIT, OPS CH ECKED NORMAL IAW MM 30-30-00. 2 L 7 4 4F 4A25 1998100900146 19981009 00146 1998 10 9 ARWA981003 4 19981002 A 3444 RADIO ALT DOUG DC8 DC862 3021970 WP E/E COMPT INOPERATIVE A ARWA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SO 19 791AL 46150 CREW REMOVED AND REPLACED NR 2 RADIO ALT OFF FLAG IN/VIEW. REMOVED AND REPLACED NR 2 RADIO ALT, OPS NORMAL IAW 34-16-00 . 2 L 7 4 4F 4A25 1998100900147 19981009 00147 WP 1998 10 9 TC8A98065 1 19981003 A 2910 FITTING DOUG DC8 DC861F 3021953 WP HYD SYST FAILED A TC8A O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 23 184SK 45981 DURING DESCENT, LOSS OF HYDRAULIC FLUID. QUANTITY DROPPED DOWN TO AUX MARK. PERFORMED IMMEDIATE ACTION ITEMS THEN ABNO RMAL HYDRAULIC PROCEDURES. REPLACED NR 10 ELBOW FITTING ON NR 3 ENGINE HYDRAULIC BY-PASS PUMP. SYSTEM CHECKED ON ENGIN E RUN. CHECKED IAW 29-10-12. 2 L 7 4 4F 4A25 1998100900148 19981009 00148 WP 1998 10 9 TC8A98066 1 19981004 A 5280 SWITCH DOUG DC8 DC862F 3021972 WP PAX DOOR DIRTY A TC8A O OTHER N FALSE WARNING CL CLIMB 1 GL 23 187SK 46022 DOOR NOT LATCHED LIGHT ILLUMINATED AFTER RETRACTION. RECYCLED GEAR AND LIGHT EXTINGUISHED. CLEANED CORROSION FROM RIGH T HAND MLG DOOR WARNING SWITCH GROUND WIRE, OPS GOOD ON GROUND PER MM 32-60-0. 2 L 7 4 4F 4A25 1998100900156 19981009 00156 CE 1998 10 9 CA980325035 1 19980317 A 2121 M2620B BRUSHES DYNAMICAIR 50380116 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA BLOWER WORN W A H I UNSCHED LANDING DEACTIVATE SYST/CIRCUITS CABIN DEPRESSURIZATION B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 794 PCE41483 (CAN) ON DEPARTURE, SMOKE REPORTED COMING FROM THE EYELET. PILOT GANGBARED THE ELECTRICAL SYSTEM, CABIN DEPRESSURIZED A ND AIRCRAFT RETURNED TO DEPARTURE BASE. VENT BLOWER REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 1998100900176 19981009 00176 SW 1998 10 9 CA980406032 1 19980304 A 5313 206031314049 LONGERON BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820180B (CAN) ON INSPECTION, RIGHT LONGERON CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 1998100900177 19981009 00177 SW 1998 10 9 CA980406033 1 19980304 A 5320 206031301121 TUNNEL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL CROSSTUBE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17248 CAE820180B (CAN) AFT CROSSTUBE TUNNELS P/N 206-031-301-121 AND P/N 206-031-302-269 CRACKED IN NUMEROUS LOCATIONS. 1 G 7 1 3U 3 U H2SW E4CE 1998100900178 19981009 00178 SW 1998 10 9 CA980406034 1 19980304 A 5330 DOUBLER 206031100283 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL PUMP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820180B (CAN) ON REMOVAL OF FUEL CELL, FOUND BOOST PUMP ATTACH DOUBLER AND DRAIN ATTACH DOUBLER CRACKED AND HAD ENLARGED HOLES. 1 G 7 1 3U 3 U H2SW E4CE 1998100900179 19981009 00179 SW 1998 10 9 CA980406035 1 19980304 A 5330 206031119051 PANEL BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE820180B (CAN) CENTER CONSOLE LEFT HAND PANEL CRACKED ON FORWARD SIDE AND DELAMINATED ON AFT SIDE ADJACENT TO BLEED AIR HEATER DI STRIBUTION VALVES. 1 G 7 1 3U 3 U H2SW E4CE 1998100900185 19981009 00185 NM 1998 10 9 CA980416001 1 19980403 A 3231 400088002 BELLCRANK PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA RT MLG DOOR BROKEN W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 2678 L727748A (CAN) DURING TEST FLIGHT WHEN THE LANDING GEAR WAS BEING CYCLED, NOTED THE RT MLG WAS NOT FULLY RETRACTED. A/C RETURNED TO BLOCKS. RT MLG DOOR BELLCRANK WAS BROKEN. REPLACED. 1 M 7 2 3O 3 O RT A17WE 1E4 1998100900196 19981009 00196 SW 1998 10 9 CA980421028 1 19980408 A 5330 206531118 SKIN BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL FUSELAGE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA CAE895726 (CAN) THE MOUNTING FLANGE OF THE MAINTENANCE STEP HAS A CAVITY WHICH ALLOWS MOISTURE TO COLLECT AND FREEZE/EXPAND CAUSIN G A RUPTURE IN THE SKIN OF THE A/C AND DAMAGE TO THE HONEYCOMB BENEATH. 1 G 7 1 3U 3 U NC H2SW E1GL 1998100900197 19981009 00197 SW 1998 10 9 CA980430001 1 19980105 A 6210 206010200033 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3522 CAE823401 (CAN) PILOT REPORTED MR VIBRATION. ENGINEER FOUND ONE CHORDWISE CRACK FROM THE BLADE SPAR TO THE TRAILING EDGE AT APPRO X 90.5 INCHES FROM THE TIP. 1 G 7 1 3U 3 U H2SW E4CE 1998100900200 19981009 00200 SW 1998 10 9 CA980504001 1 19980405 A 6210 204011250001 BLADE BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 502 A11338 LEO07807 (CAN) BLADE CRACKED ON BOTH SKINS AT 77.25 INCHES FROM TIP T/E. CRACK IS 15 INCHES CHORDWISE FORWARD FROM TRAILING EDGE THEN INBOARD 9 INCHES TOP AND BOTTOM. 1 G 7 1 4U 4 U H1SW E17EA 1998100900201 19981009 00201 SW 1998 10 9 CA980504003 1 19980312 A 6210 212015501005 BLADE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA MAIN ROTOR DENTED W O OTHER C F.O.D. LD LANDING 1 CA 1688 CPPS61467 (CAN) PILOT LANDED TOO CLOSE TO A TREE. TREE STRIKE RESULTED IN DENTS TO BOTH BLADES NEAR THE TIPS. 1 G 7 1 4U 4 U H4SW E22EA 1998100900221 19981009 00221 SW 1998 10 9 CA980519006 1 19980508 A 2910 204076504001 VALVE RONSON 1U1025 BELL 204 204B 1181404 SW LYC T53 T5311B 41549 NE HYDRAULIC SYS BROKEN W C D ABORTED TAKEOFF RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 CA 10117 1202 (CAN) ON RUN-UP, UNABLE TO SWITCH HYDRAULICS TO MANUAL. HYDRAULIC BYPASS VALVE CANNON PLUG RECEPTACLE BROKEN OFF AT ITS BASE. INTERIOR CONNECTIONS BROKEN ALLOWING INTERMITTENT CONTACT. 1 G 7 1 4U 4 U H1SW E1EA 1998100900225 19981009 00225 SW 1998 10 9 CA980521001 1 19980521 A 6510 206040931009 DRIVE SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL T/R DRIVE FAILED W B EMER. DESCENT F FLT CONT AFFECTED CL CLIMB 1 CA 10000 VNMA08093 CAE823296 (CAN) ON CLIMBOUT AT LOW SPEED, SUDDEN UNCONTROLLABLE YAW TO THE RIGHT. AFTER SEVERAL 360 DEGREE TURNS, AIRCRAFT SETTLE D INTO TREES. NR 2 SECTION OF T/R DRIVESHAFT BONDED COUPLING FAILED. CTSB INVESTIGATING. 1 G 7 1 3U 3 U H2SW E4CE 1998100900240 19981009 00240 SW 1998 10 9 CA980602047 1 19980413 A 5302 DOUBLER 206031004003 BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL BS 183 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA AOKN0521 CAE831797 (CAN) CRACK IN DOUBLER FOR PITCH CHANGE OPENING AT BS 183.0, CRACK IS .750 INCHES LONG OF TOTAL DOUBLER WIDTH OF 1 INCH. 1 G 7 1 3U 3 U H2SW E4CE 1998100900241 19981009 00241 SW 1998 10 9 CA980602052 1 19980328 A 2910 MS219606L CONNECTOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL HYDRAULIC SYS CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA CAE821623 (CAN) HYDRAULIC CONNECTOR BODY CRACKED POSSIBLY FROM OVERTORQUE. 1 G 7 1 3U 3 U H2SW E4CE 1998100900244 19981009 00244 SO 1998 10 9 CA980602074 1 19980414 A 3240 06108700 FITTING CLEVELAND 30123 PIPER PA31 PA31350 7103110 SO LYC O540 LTIO540J2BD 41533 EA BRAKE SYS DAMAGED W K NONE K FLUID LOSS LD LANDING 1 CA L783961AC (CAN) DURING FINAL APPROACH, PILOT CHECKED BRAKES FOR PRESSURE AND RT BRAKE WAS SOFT AND AFTER A FEW PUMPS, NO BRAKES WE RE FELT. LOWER HOSE HAD COME OUT OF BRAKE ASSY. SUBMITTER STATED POSSIBLY HIT BY SOMETHING. REPLACED. 1 L 7 2 3O 3 O A20SO E14EA 1998100900247 19981009 00247 SW 1998 10 9 CA980603013 1 19980516 A 6520 1000351875 PIN 206011724003 BELL 206 206L 1181522 SW TAIL ROTOR MISINSTALLED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON REPLACEMENT OF THE T/R GEARBOX, THE T/R CROSSHEAD HAD EXCESSIVE ROTATIONAL MOVEMENT. THE PIN USED TO LOCATE TH E PITCH CHANGE ROD WITHIN THE OUTPUT SHAFT HAD NOT BEEN INSTALLED CORRECTLY THROUGH THE KEY WITHIN THE ROD. 1 G 7 1 3U H2SW 1998100900249 19981009 00249 CE 1998 10 9 CA980610018 1 19980602 A 2131 13035616 CONTROLLER CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE CABIN FAILED W B I EMER. DESCENT CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 CA 215 (CAN) ON TAKEOFF, CABIN RATE NEEDLE STAYED AT ZERO AND CABIN ALTITUDE STAYED AT GROUND LEVEL. DIFFERENTIAL INCREASED AT FL 220 AND DIFFERENTIAL REACHED 8.5 CABIN ALTITUDE BEGAN INCREASING TO 6,000 WHEN AIRCRAFT REACHED FL 370, STARTED DESCE NT AT 1,000 FPM. CABIN RATE NEEDLE STAYED AT ZERO DIFFERENTIAL AND BEGAN INCREASING AT FL 240, CABIN RATE WENT TO 3,000 FPM, CABIN ALTITUDE CLIMBED QUICKLY TO 13,000 AND STOPPED. CABIN RATE THEN WENT TO ZERO. AIRCRAFT LANDED AND CABIN CO NTROLLER FOUND UNSERVICEABLE. PART TC: 210. 1 L 7 2 4F 4 F A22CE E1NE 1998100900265 19981009 00265 WP 1998 10 9 CA980622024 1 19980609 A 7333 FFR104MK1 FLOW REG LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE NR 3 ENGINE FAILED W O OTHER O OTHER CL CLIMB 1 CA 14825 (CAN) DURING TAKEOFF THERE WAS FLUCTUATION OF NR 3 ENGINE PARAMETERS, WHEN THRUST POWER WAS RETARDED PARAMETERS STABILIZ ED. DURING CRUISE THE ENGINE PARAMETERS WERE NORMAL. POST-FLIGHT TROUBLESHOOTING LED TO REPLACEMENT OF THE NR 3 ENGINE FUEL FLOW REGULATOR. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1998100900280 19981009 00280 NM 1998 10 9 CA980623016 1 19980615 A 2120 82120354009 DIVERTER BOX DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CABIN CRACKED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 19782 123010 (CAN) JUST PRIOR TO DESCENT, CREW NOTED CABIN PRESSURE WARNING LIGHT ON. MAXIMUM FLOW ON BLEED FLOW CONTROL SELECTED WH ICH CONTROLLED THE CLIMBING CABIN AND RE-PRESSURIZED THE AIRCRAFT. CABIN RECIRC DIVERTER VALVE BOX FOUND CRACKED ALONG THE LOWER AFT CORNER. PART TC: 22,086. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900281 19981009 00281 NM 1998 10 9 CA980623017 1 19980623 A 5610 CSP424318 SCREW PPG 8SC0519009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE WINDSCREEN SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 16466 91260H7875 TM120796 (CAN) DURING COMPLETION OF TASK NR 5310/07B, FOUND SCREW HEAD SHEARED OFF IN UPPER FORWARD CORNER OF THE CAPTAIN'S WINDO W. THIS IS ONE OF THE SCREWS THAT HOLDS THE WINDOW TO THE FRAME. PART TC: 19,980. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900296 19981009 00296 CE 1998 10 9 CA980629012 1 19980623 A 7332 99120332 SWITCH CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT BOOST PRESS FAILED W O OTHER N FALSE WARNING DE DESCENT 1 CA 814 71711 (CAN) ON DESCENT, WHEN THE ENGINES WERE THROTTLED BACK, THE 'FUEL PRESS LOW RT' AND THE 'BOOST PUMP ON RT' ILLUMINATED. CREW SELECTED THE RIGHT BOOST SWITCH FROM 'NORM' TO 'ON' AND LANDED WITHOUT INCIDENT. ENGINE PARAMETERS OK. AFTER LAND ING , THE BOOST PUMP SWITCH RE-SELECTED BACK TO 'NORM'. WHEN THROTTLE ADVANCED FROM IDLE, THE 'FUEL PRESS LOW' AND 'BOO ST PUMP ON' LIGHTS ILLUMINATED AGAIN. PART TC: 965. 1 L 7 2 4F 4 F A22CE E1NE 1998100900299 19981009 00299 EA 1998 10 9 CA980629015 1 19980531 A 2750 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WING FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 6535 807287 (CAN) ON APPROACH, FLAPS FAILED AT 45 DEGREES. ON GROUND, FLAPS SET AT ZERO DEGREES WITH HYD SYSTEM ON, CIRCUIT BREAKE R PULLED AND FAULT CLEARED. PART TC: 5,682. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100900300 19981009 00300 EA 1998 10 9 CA980629016 1 19980531 A 2750 FLAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WING FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 6537 807287 (CAN) ON FINAL, FLAPS TO HALF-SPEED AND THEN FLAPS FAILED. AFTER FLAPS SET AND INDICATING 45 DEGREES, FOUND FLAP CONTRO L ELECTRONIC UNIT POTENTIOMETERS POSITION 5-8 OUT OF RIG. PART TC: 15,682. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100900301 19981009 00301 NM 1998 10 9 CA980629017 1 19980531 A 5280 DOOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE NLG SEIZED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P709689 (CAN) AFTER TAKEOFF, LANDING GEAR DISAGREE MESSAGE WITH AIRFRAME VIBRATION AND GEAR INDICATION. RECYCLED GEAR, INDICATI ON RE-APPEARED. HEAVY LANDING CARRIED OUT. RIGHT HAND NOSE GEAR DOOR STRUT ASSY MANUAL RELEASE SEIZED. REPLACED DOOR STRUT, RIGGED NOSE GEAR DOOR PER MAINT MANUAL, OK. PART TC: 14,775. 2 L 7 2 4F 4 F RT A1NM E3NE 1998100900302 19981009 00302 WP 1998 10 9 CA980629019 1 19980603 A 3231 CONTROL CABLE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE MLG DOOR STIFF W O OTHER J WARNING INDICATION LD LANDING 1 CA P657309D (CAN) ON LANDING ROLL, GEAR DOOR OPEN LIGHT ON, LT GEAR DOOR OPEN CONFIRMED BY TOWER. MAINTENANCE CHECK FOUND CABLE OF LT MAIN GEAR DOOR SEQUENCE STIFF AND TORQUE TUBE RIVET SHEARED. CABLE CLEANED AND LUBRICATED, REPLACED DOOR AND RIVET, FOLLOW-UP CABLE RIGGING CHECKED AND RETRACTION TEST CARRIED OUT. 2 L 7 2 4F 4 F A6WE E2EA 1998100900303 19981009 00303 NM 1998 10 9 CA980629020 1 19980601 A 3230 664700500A4B LGCU AIRBUS A319 A319114 NM GEAR DOORS FAILED W O OTHER J WARNING INDICATION LD LANDING 1 CA (CAN) UNSAFE LANDING INDICATION ON APPROACH, FOLLOWED BY FLT ATTENDANT CHIME RINGING CONSTANTLY, ECAM SHOWED GROUND PROX IMITY WARNING SYSTEM FAILED, STANDBY PITOT FAILURE, LANDING GEAR CONTROL AND INTERFACE NR 1 FAULT, ENGINE NR 1 FAULT. U NABLE TO EXTEND GEAR. GEAR EXTENDED AFTER WAITING FIVE MINUTES AND UNSAFE INDICATION DISAPPEARED. MAINTENANCE FOUND LA NDING GEAR CONTROL UNIT AT FAULT AND REPLACED UNIT. SYSTEM TEST CARRIED OUT NORMAL. 2 L 7 2 4F RT A28NM 1998100900304 19981009 00304 EA 1998 10 9 CA980629021 1 19980604 A 2170 COALESCER BAG CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE CABIN AIR COND CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 807157 (CAN) TOILET SMOKE LIGHT ON AFTER TAKEOFF. MESSAGE ON ENGINE INDICATING AND CREW ALERTING SYSTEM AND ALARM IN LAVATORY . LIGHT WENT OUT AFTER 3 MINUTES. REPLACED BOTH COALESCER BAGS, RAN PACKS WITH ENGINE BLEED AIR, NO SMOKE OR UNUSUAL O DORS IN CABIN, FAULT DID NOT RE-APPEAR. CHANGED SMOKE DETECTOR. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100900305 19981009 00305 NM 1998 10 9 CA980629022 1 19980605 A 2750 3A1260A TRANSDUCER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA P709649 (CAN) ON START, FLAPS WOULD NOT EXTEND FULLY TO 5 DEGREES. AIRCRAFT SYSTEM POWERED DOWN THEN POWERED UP AND FLAPS OPERA TED NORMAL. FLAP SLAT ELECTRONIC UNIT FAULT FLAP LEVER ROTARY VARIABLE DISPLACEMENT. TRANSDUCER REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998100900306 19981009 00306 NM 1998 10 9 CA980629023 1 19980614 A 3230 CONNECTOR AIRBUS A319 A319114 NM MLG LOOSE W O OTHER N FALSE WARNING AP APPROACH 1 CA (CAN) ON SELECTING LANDING GEAR DOWN, NO LIGHT ON LANDING GEAR PANEL. GEAR CYCLED, WHEEL PAGE ON ECAM INDICATED GEAR DO WN, AND NORMAL A/C LANDING COMPLETED. TIGHTENED LT PROXIMITY CONNECTOR, RESET LANDING GEAR CONTROL INTERFACE UNIT, GEAR TESTED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998100900307 19981009 00307 WP 1998 10 9 CA980629025 1 19980611 A 2421 729641 GENERATOR LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENGINE CRACKED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA 10224 (CAN) IDG LOW PRESSURE LIGHT ILLUMINATED IN-FLGHT, IDG DISCONNECTED. POST-FLIGHT INSPECTION FOUND THE CHARGE FILTER PRE SSURE HOUSING CRACKED. NR 3 ENGINE IDG AND OIL COOLER WERE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1998100900312 19981009 00312 NE 1998 10 9 CA980706005 2 19980604 A 8530 ROD DOUG DC4 C54GDC 3021534 WP PWA R2000 R20007M2 52023 NE ENGINE BROKEN W E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA 44 P104304 (CAN) ENGINE BEGAN SEVERE VIBRATION IN CRUISE AND WAS SHUT DOWN. POST- FLIGHT INSPECTION FOUND THE CONNECTION ROD AT NR 14 CYLINDER HAD BROKEN. THE ENGINE WAS REPLACED AND TEST FLOWN SERVICEABLE. 2 L 7 4 4R 4 R A762 5E5 1998100900313 19981009 00313 NE 1998 10 9 CA980706006 2 19980605 A 8530 153084 HEAD DOUG DC4 DC4 3021502 WP PWA R2000 R20007M2 52023 NE NR 14 CYLINDER SPLIT W E A ENGINE SHUTDOWN UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE TO TAKEOFF 1 CA 632 P197846 (CAN) NR 1 ENGINE DEVELOPED VIBRATION/SHAKING ON TAKEOFF. NR 1 ENGINE WAS SHUTDOWN. POST-FLIGHT INVESTIGATION FOUND TH E NR 14 CYLINDER HEAD SPLIT. THE CYLINDER WAS REPLACED. THE ENGINE GROUND RUN SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4R 4 R A762 5E5 1998100900315 19981009 00315 NM 1998 10 9 CA980706008 1 19980603 A 3246 314801 WHEEL BFGOODRICH DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 11720 325 0105 123030 (CAN) LOUD BANG HEARD DURING TOW. NR 1 WHEEL ASSY, OUTER RIM BROKEN OUT FOR 1/3 OF THE RIM CIRCUMFERENCE INTO THE BEAD AREA, ALLOWING THE TIRE TO SLIDE OVER AND DEFLATE. NDT CHECK AS PART OF TIRE REPLACEMENT. NO CRACK FINDINGS. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900328 19981009 00328 EU 1998 10 9 CA980706025 1 19980613 A 2133 90231570381 OUTFLOW VALVE AIRBUS 320 A320211 3930320 EU CABIN PRESSURE FAILED W B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CA (CAN) EXCESSIVE CABIN ALTITUDE NOTED AT FLT LEVEL 310. CABIN ALTITUDE CLIMB AT 550, INITIATED EMERGENCY DESCENT, CABIN CONTINUED TO CLIMB TO 1180, AFTER LEVEL OFF CABIN PRESSURE STABILIZED. MAINTENANCE REPLACED OUTFLOW VALVE AND OPERATION ALLY CHECKED IN AUTO AND MANUAL MODE, SERVICEABLE. 2 L 7 2 4F RT A28NM 1998100900329 19981009 00329 EA 1998 10 9 CA980706026 1 19980618 A 2170 75368937 COALESCER BAGS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT PACK FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA 7581 807201 (CAN) AT TAKEOFF, AIR CONDITIONING SMOKE AND FOG IN COCKPIT AND CABIN. BOTH COALESCER BAGS REPLACED, RIGHT HAND PACK CL EANED. PART TC: 6,718. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100900330 19981009 00330 WP 1998 10 9 CA980706027 1 19980616 A 2133 OUTFLOW VALVE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESSURE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA P653457D (CAN) ON CLIMB-OUT, AT 26,000 FEET, FLOW LIGHT ILLUMINATED, CABIN DIFFERENTIAL AT MAXIMUM 8 POUNDS PER SQUARE INCH. LEV ELED OFF AT 280 WITH CABIN ALTITUDE AT 4,000 ABOUT 1,400 BELOW SCHEDULE, NO STANDBY LIGHT ON. SELECTED MANUAL TO REGAIN SCHEDULE, WHEN AUTOMATIC SELECTED IT TRIED TO DESCEND AGAIN, LANDED IN MANUAL. MAINTENANCE CHANGED PRESSURIZATION CONT ROL PANEL OUTFLOW VALVE ACTUATOR AND MOTOR. SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998100900331 19981009 00331 NM 1998 10 9 CA980706028 1 19980616 A 2133 OUTFLOW VALVE BOEING 747 747233B NM PWA JT9 JT9D7 52054 NE CABIN PRESSURE FAILED W D RETURN TO BLOCK P NO WARNING INDICATION CL CLIMB 1 CA P685935 (CAN) ON CLIMB, THE LT OUTFLOW VALVE STICKING THROUGH 22,000 FEET, UNABLE TO MAINTAIN CABIN ALTITUDE, AIRCRAFT RETURNED. WITH MODE SELECTOR SWITCH IN MANUAL, PRESSURIZATION WAS FLUCTUATING THROUGH 10,000 FEET IN CLIMB, ABLE TO OPERATE BOTH OUTFLOW VALVES NORMALLY. CHANGED LT OUTFLOW VALVE ACTUATOR AND PRESSURE CONTROLLER, SYSTEM TESTED OK. 2 L 7 4 4F 4 F RT A20WE E20EA 1998100900333 19981009 00333 WP 1998 10 9 CA980706030 1 19980609 A 2530 OVEN SOCKET DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE POSITION 17 FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA P656927D (CAN) DURING APPROACH, AN ELECTRICAL BURNING SMELL WAS DETECTED COMING FROM THE GALLEY. THE GALLEY POWER WAS TURNED OFF , SMELL DISSIPATED AND A/C LANDED SAFELY. MAINTENANCE FOUND OVEN POSITION NR 17 SOCKET BURNT. OVEN POSITION NR 17 SOCK ET WAS REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1998100900335 19981009 00335 EA 1998 10 9 CA980707001 1 19980529 A 5720 85711428102 BRACKET DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE FLAP SHROUD BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 15853 PCE123113 (CAN) AT FLAP SECONDARY DRIVE SHAFT LUBE AND INSPECTION, THE INBOARD RIGHT WING FLAP SHROUD SUPPORT STRUT BRACKET WAS FO UND BROKEN. PART TC: 23,946. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900336 19981009 00336 NM 1998 10 9 CA980707002 1 19980531 A 2160 7787272 PACK VALVE UNITEDTECH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AC PACK STUCK W K NONE O OTHER IN INSP/MAINT 1 CA 15495 900484 120144 (CAN) AFTER START WHEN BLEEDS TURNED ON, THE DUCT TEMP STARTED TO RISE TOWARDS THE RED LINE. UNABLE TO CONTROL ON EITHE R AUTO OR MANUAL. INSPECTION FOUND THE PACK VALVE STUCK AT FULL HOT. PART TC: 21,313. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900337 19981009 00337 NE 1998 10 9 CA980707007 2 19980607 A 7532 311489101 VALVE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE MALFUNCTIONED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 1336 123146 (CAN) AFTER START WHEN NR 2 ENGINE BLEED WAS SELECTED ON, SMOKE WAS GENERATED IN THE CABIN. INSPECTION FOUND GROOVES IN THE P2.5/03 SWITCHING VALVE AND VALVE COVER. THE PARTS WERE REPLACED. THE ENGINE GROUND RUN SERVICEABLE AND THE AIR Q UALITY WAS RESTORED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900338 19981009 00338 NE 1998 10 9 CA980707008 2 19980609 A 7320 324485315 HMU DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE MALFUNCTIONED W O OTHER O OTHER TO TAKEOFF 1 CA 6294 717 123133 (CAN) NR 2 ENGINE HAD A TORQUE SURGE ON TAKEOFF. ENGINE WIRING HARNESS WAS INSPECTED AND FOUND A-C PIN OPEN AT P10. PI N CLEANED. ENGINE EEC REPLACED, WING ROOT CANNON PLUGS CLEANED. HYDRO MECHANICAL UNIT (HMU) AND FUEL PUMP REPLACED. EN GINE GROUND RUN SERVICEABLE. PART TC: 10,147. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900340 19981009 00340 EU 1998 10 9 CA980707016 1 19980604 A 3250 CONTROL UNIT MESSIER C20216332292 AIRBUS 320 A320211 3930320 EU NLG STEERING MALFUNCTIONED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 22328 382 (CAN) ON LANDING, AFTER ROLL OUT, NOSE WHEEL STEERING FAILED. MAINTENANCE REPLACED STEERING SERVO VALVE AND BRAKE/STEER ING CONTROL UNIT. VALVE DID NOT RECTIFY THE PROBLEM, HOWEVER, THE BRAKE/STEERING CONTROL UNIT CURED THE PROBLEM. PART TC: 8,276. 2 L 7 2 4F RT A28NM 1998100900341 19981009 00341 1998 10 9 CA980707017 4 19980604 A 3160 INDICATOR GE 8DJ175LXP2 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE COCKPIT MALFUNCTIONED W O OTHER J WARNING INDICATION IN INSP/MAINT 1 CA 55780 0353 455337 (CAN) DURING INSPECTION, FOUND 2 INDICATORS THAT DID NOT EXHIBIT HARD FAULTS UNTIL HEATED TO WORKING ENVIRONMENT TEMPERA TURE (20-25 DEGREES CELSIUS). FUTURE TESTS OF THESE UNITS WILL INCLUDE A TEST AT THE AFOREMENTIONED TEMP TO INSURE RELI ABILITY. 2 L 7 3 4F 4 F A22WE E23EA 1998100900342 19981009 00342 NE 1998 10 9 CA980707018 2 19980604 A 8520 ROD 1211245011 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 24077 20787 08977 455337 (CAN) DURING INSPECTION, ACTUATOR INSTALLED ON NR 1 ENGINE FOUND LEAKING. SHOP REPORT FOUND PISTON ROD AND HOUSING ATTA CH BUSHINGS WORN BEYOND LIMITS. COMPONENT OVERHAULED AND RETURNED TO STOCK SERVICEABLE. 2 L 7 3 4F 4 F A22WE E23EA 1998100900343 19981009 00343 NM 1998 10 9 CA980707019 1 19980608 A 8012 SWITCH 1G38616927 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 28961 28 1593 674240 (CAN) AIRCRAFT DIVERTED DUE NR 2 ENGINE START VALVE LIGHT ON AND PRESSURE DROPPED IN PNEUMATIC SYSTEM. REPLACED PRESSUR E SWITCH. PART TC: 19,943. 2 L 7 2 4F 4 F A16WE E2EA 1998100900344 19981009 00344 NM 1998 10 9 CA980707020 1 19980610 A 3233 ACTUATOR 654462514 BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE NLG FAILED W A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CA 44970 DA4607 709378 (CAN) AIR TURNBACK DUE NOSE GEAR WOULD NOT RELEASE WITH LANDING GEAR LEVER. NOSE GEAR LOCK AND ACTUATOR AND TRANSFER CY LINDER REPLACED. GEAR SWING CARRIED OUT AIRCRAFT SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1998100900345 19981009 00345 NM 1998 10 9 CA980707021 1 19980610 A 5280 6591700221 DOOR 6591700221 BOEING 737 737296 1384486 NM PWA JT8 JT8D9A 52048 NE NLG CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 674465 (CAN) NOSE LANDING GEAR DOOR WORN ON INNER SURFACE. NO MENTION OF CLEARANCE CHECK IN AMM. DOOR REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1998100900346 19981009 00346 NM 1998 10 9 CA980707022 1 19980610 A 5280 6591700221 DOOR 6591700221 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE NLG CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 708821 (CAN) NOSE LANDING GEAR WORN ON INNER SURFACE. NO MENTION OF CLEARANCE CHECK IN AMM. DOOR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998100900347 19981009 00347 NM 1998 10 9 CA980707024 1 19980622 A 2131 7638102 CONTROLLER HAMSTD 7638102 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE CABIN PRESSURE FAILED W I A CABIN DEPRESSURIZATION UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 33861 DA3388 674646 (CAN) AIRCRAFT DIVERTED AND UNSCHEDULED LANDING WHEN PRESSURIZATION SYSTEM WOULD NOT CONTROL CABIN PRESSURE BELOW 10,000 FEET, A/C IN CRUISE AT 25,000 FEET. A/C DESCENT AND DEPRESSURIZATION WAS INITIATED. REPLACED CABIN PRESSURE CONTROLL ER AND OUTFLOW VALVE. ALSO, REPLACED RT COALESCER BAG. A/C RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1998100900348 19981009 00348 1998 10 9 CA980707025 4 19980625 A 3417 HG480B13 COMPUTER COLLINS HG480B13 BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE COCKPIT FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 26245 P1091 709520 (CAN) TAKEOFF ABORTED AT 90 KNOTS DUE CAPT'S AIRSPEED INDICATOR INDICATING ZERO DURING TAKEOFF ROLL. AIR DATA COMPUTER REPLACED. A/C SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1998100900349 19981009 00349 EU 1998 10 9 CA980707026 1 19980625 A 3246 46X162030PR TIRE GOODYEARAERO C201951523 AIRBUS 320 A320211 3930320 EU MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 9956 925 U4011 (CAN) DURING INSPECTION, FOUND DAMAGE TO NR 1 MAIN WHEEL AFTER REPORT OF TIRE DEBRIS FOUND ON RUNWAY. DAMAGE TO TRAILIN G EDGE FLAP WAS INSPECTED. WHEEL AND TIRE ASSEMBLY REPLACED. PART: 3,676. 2 L 7 2 4F RT A28NM 1998100900350 19981009 00350 NM 1998 10 9 CA980707027 1 19980629 A 7830 ACCESSORY UNIT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE THRUST REVERSER INOPERATIVE W A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CA 0867 707369 (CAN) AIR TURN BACK. THRUST REVERSER LIGHT CAME ON AT ROTATION. ENGINE ACCESSORY UNIT REPLACED. THRUST REVERSER ISOLA TION VALVE FUNCTION CARRIED OUT. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1998100900351 19981009 00351 NM 1998 10 9 CA980707028 1 19980629 A 3610 HPSOV BOEING 767 767375 NM ENGINE FAILED W C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 CA (CAN) TAKEOFF ABORTED AT 70 KNOTS DUE MASTER CAUTION SOUNDED AND EICAS MESSAGE R-HPSOV AND R-BLEED LT. A/C OPERATED PE R MEL WITH R-HPSOV AND T/R LOCKED OUT. REPLACED HPSOV. A/C SERVICEABLE. 2 L 7 2 4F RT A1NM 1998100900355 19981009 00355 SW 1998 10 9 CA980707033 1 19980601 A 7714 206062627003 SHAFT 206062627003 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TACH GENERATOR SHEARED W K NONE O OTHER NR NOT REPORTED 1 CA 4946 CAE821617 (CAN) NR N2 INDICATION. N2 TACH GENERATOR SHAFT SHEARED. 1 G 7 1 3U 3 U H2SW E4CE 1998100900356 19981009 00356 SW 1998 10 9 CA980707034 1 19980519 A 6710 71851 LINEAR ACTUATOR 71851 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL DROOP COMP FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 193 2538 CAE801518BA (CAN) INTERMITTENT OPERATION OF ACTUATOR. WOULD NOT BEEP DOWN. TWO TERMINAL BASES LOOSE. MOTOR VERY ROUGH RUNNING. 1 G 7 1 3U 3 U H2SW E4CE 1998100900357 19981009 00357 SW 1998 10 9 CA980707036 1 19980605 A 2435 23032018 STARTER LUCAS BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 302 3014 CAE820289 (CAN) STARTER/GENERATOR OVERHEATING AND SMOKING ON SHUT DOWN. DRIVEN BY REVERSE CURRENT RELAY. LOAD METER, RCR AND CIR CUIT BREAKERS REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998100900358 19981009 00358 SW 1998 10 9 CA980707040 1 19980611 A 6320 206040360037 BEARING 206040002007 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R GEARBOX FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 14074 2479 NFJ50670 820669 (CAN) MAIN TRANSMISSION CHIP DETECTOR. METAL FLAKES BEYOND LIMITS ON LONG MAGNETIC CHIP DETECTOR AND OIL MONITOR PLUG. SUSPECT BEARING FAILURE. 1 G 7 1 3U 3 U H2SW E4CE 1998100900360 19981009 00360 SW 1998 10 9 CA980707044 1 19980622 A 2140 DUCT SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP COCKPIT HEAT LOOSE W A UNSCHED LANDING O OTHER CR CRUISE 1 CA P54202 (CAN) CREW NOTICED THE LEFT ESSENTIAL BUS WAS ABNORMALLY HOT, SHORTLY AFTER THE NR 1 AUDIO CIRCUIT BREAKER TRIPPED. AI RCRAFT RETURNED OK. INSPECTION REVEALED THAT THE HOT AIR DUCT IN THE LEFT ESSENTIAL BUS AREA HAD BECOME DISLODGED DIREC TING HOT AIR ONTO THE BUS. IN ADDITION, THE NR 1 AUDIO PANEL CIRCUIT BREAKER WAS FOUND CRACKED. 2 L 7 2 4T 4 T RT A8SW E4WE 1998100900365 19981009 00365 EA 1998 10 9 CA980908001 2 19980818 A 7240 30286Z6 CASE GAS GEN BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA DIFFUSER PIPE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4199 A0373 CPPS60646 (CAN) AFTER POWER SECTION FAILED, ENGINE WAS BORESCOPED AND INTERNAL DAMAGE WARRANTED ENGINE REMOVAL. SUBSEQUENTLY, THE GAS GENERATOR CASE WAS FOUND CRACKED. PART TC: 3,086. 1 G 7 1 4U 4 U H4SW E22EA 1998100900368 19981009 00368 NE 1998 10 9 CA980908035 2 19980815 A 7200 ENGINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 MAKING METAL W E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CA 10066 (CAN) AFTER PUSH BACK DURING START OF NR 2 ENGINE, THE OIL FILTER PRESSURE LIGHT CAME ON. INSPECTION FOUND METAL IN THE MAIN OIL FILTER. THE ENGINE WAS REMOVED FOR INVESTIGATION. 2 L 7 3 4F 4 F A23WE E12EU 1998100900369 19981009 00369 NE 1998 10 9 CA980909024 2 19980825 A 7260 GEARBOX BOEING 757 75723A 1384967 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE SEIZED W E A ENGINE SHUTDOWN UNSCHED LANDING J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 CA 30863 (CAN) DURING FLIGHT, THE NR 2 ENGINE OIL PRESSURE DROPPED. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED. POST-FL IGHT INSPECTION FOUND THE GEARBOX SEIZED. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998100900370 19981009 00370 CE 1998 10 9 CA980915021 1 19980908 A 2422 SPC10PW INVERTER BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE AC SYSTEM FAULTY W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 4967 669 GGMPS0025 (CAN) AFTER TAKEOFF, BOTH AC BUSSES WENT OFF THE LINE. COULD NOT BE RESET. BOTH ATTITUDE AND HEADING REFERENCE WERE LO ST. AS THEY WERE IN VMC CONDITIONS, RETURNED TO THE AIRPORT. INVESTIGATION REVEALED THE RIGHT HAND INVERTER WAS AT FAUL T. BUT A SINGLE LOSS SHOULD NOT BECOME A TOTAL A/C LOSS. RAYTHEON CONTACTED. SUBMITTER STATED APPARENTLY A MOD HAD BEE N MADE BY THE MANUFACTURER BUT WAS NOT MANDATORY. MOD INTRODUCED TO COVER S/N 804 AND AFTER. THE UNITS IN THE CASE WERE RECOMMENDED FOR REPLACEMENT WITH POST S/N 804 THAT HAVE BEEN UPGRADED. PART TC: 5,870. 2 L 7 2 4T 4 T RT A24CE E26NE 1998100900372 19981009 00372 EU 1998 10 9 CA980916030 1 19980825 A 2742 1110039AAA ACTUATOR MENASCO 1110039AAA FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU HORIZ STAB JAMMED W B EMER. DESCENT F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA MC375 9621 (CAN) HORIZONTAL STAB JAMMED ON APPROACH. BOTH STAB CAUTION LIGHTS COME ON ON THE HYDRAULIC FLIGHT CONTROL PANEL. ALTER NATE SYSTEM TRIED BUT NOT OPERATIONAL. EMERGENCY DECLARED AND PASSENGERS ASKED TO MOVE TO REAR OF AIRCRAFT. CFR CALLED OUT. UNEVENTFUL LANDING CARRIED OUT. UNABLE TO DUPLICATE SNAG ON GROUND. ACTUATOR REPLACED, HISTORY OF SNAGS. REPLA CED. OLD ACTUATOR SENT FOR REPAIR AND STRIP REPORT. 2 L 7 2 4F 4 F RT A20EU E2EU 1998100900377 19981009 00377 WP 1998 10 9 VJ9800460 1 19980818 A 5312 591886513 BULKHEAD SKIN DOUG DC9 DC932 3022066 WP BS 600 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 CORROSION ON BULKHEAD SKIN AT FS 600, 28L - 28R. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR IAW DC9 SRM 51-10-3, 51-20-0, 51-30-1 AND ROD SKETCH 98-09-04-010. 2 L 7 2 4F A6WE 1998100900378 19981009 00378 WP 1998 10 9 VJ9800461 1 19980829 A 5320 1A538371 CHANNEL DOUG DC9 DC932 3022066 WP AFT LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 LT AFT LAV BRACKET ASSY HARDWARE AND BRACKET FOR PULLEYS ON AFT PRESSURE BULKHEAD CORRODED. FABRICATED CHANNEL REPAIR F ROM EXTRUSSION S1324556 IAW DC9 SRM 53-01, FIG 1 AND 50-10-1. TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30- 3, 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998100900379 19981009 00379 WP 1998 10 9 VJ9800462 1 19980830 A 5320 39515129501N FITTING DOUG DC9 DC932 3022066 WP BS 600 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 LONGERON END FITTING AT FS 600 CORRODED BEYOND LIMIT. LOCATED, DRILLED AND DEBURRED NEW FITTING IAW DC9 SRM 51-10-4. 2 L 7 2 4F A6WE 1998100900380 19981009 00380 WP 1998 10 9 VJ9800463 1 19980831 A 5320 SKIN DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 SKIN AT FS 966, L30, CORRODED BEYOND LIMIT. CUT OUT CORRODED SKIN AREA IAW DC9 SRM 53-04, FIG 9. FABRICATED, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3 AND 53-04, FIG 9. 2 L 7 2 4F A6WE 1998100900381 19981009 00381 WP 1998 10 9 VJ9800464 1 19980831 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 998 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 GILL LINER ATTACHING BRACKETS ALONG BOTTOM OF BULKHEAD AT STA 998 CORRODED. FABRICATED, HEAT TREATED, DRILLED, ALODINED AND PRIMED NEW ATTACH ANGLES IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4 AND AIRTRAN RES 981417. 2 L 7 2 4F A6WE 1998100900382 19981009 00382 WP 1998 10 9 VJ9800465 1 19980831 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP CARGO DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FWD CARGO DOOR JAMB AFT WEB SUPPORT HAS FASTENER HOLE CRACKED TO EDGE OF WEB. FABRICATED REPAIR DOUBLER FROM 2024T3-.04 0 IAW DC9 SRM 53-01. FIG 2. DRILLED, DEBURRED, TRIMMED IAW DC9 SRM 51-30-2 AND AIRTRAN RES 981439. 2 L 7 2 4F A6WE 1998100900383 19981009 00383 WP 1998 10 9 VJ9800466 1 19980831 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 560-579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FLOOR BRACKET BY NUTPLATES AT FS 560 -579, L27 -28R, CORRODED. FABRICATED NEW PANEL INTERCOSTAL FLANGE FROM 7075-80,.05 0, IAW DC9 SRM 51-30-1, 53-11-1, FIG 10. HEAT TREATED AND FABRICATED NEW INTERCOSTAL FLANGE FROM 7075-0,.050, IAW DC9 S RM 53-11-2 AND AIRTRAN RES 981112, HEAT TREATED, TRIMMED TO FIT, DRILLED, DEBURRED, TREATED AND PRIMED AND INSTALLED INT ERCOSTAL FWD PIT IAW DC9 SRM 51-10-2A, 51-10-4, 51-10-3, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998100900384 19981009 00384 WP 1998 10 9 VJ9800467 1 19980831 A 5320 SPLICE DOUG DC9 DC932 3022066 WP BS 484-503 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FWD PIT FS 484-503, L30, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. REMOVED LONGERON IAW DC9 SRM 53-11-2, FIG 14, CUT, TRIMMED, DRILLED, INSTALLED NEW SECTION LONGERON AND SPLICES IAW DC9 SRM 51-30-3, 51-30-3. SPLICES MADE FROM 7075T 7351.. 2 L 7 2 4F A6WE 1998100900385 19981009 00385 WP 1998 10 9 VJ9800468 1 19980831 A 5321 5917243105N FLOOR DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 ACCESS PANEL AND COVER FWD CARGO FLOOR PANEL CORRODED BEYOND LIMIT IAW DC9 SRM 53-01. FABRICATED NEW COVER PLATE, LOCAT ED NEW ACCESS PANEL, INSTALLED IAW DC9 SRM 51-10-2. 2 L 7 2 4F A6WE 1998100900386 19981009 00386 WP 1998 10 9 VJ9800469 1 19980904 A 5210 3917863214 CHANNEL DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 LT LOWER CORNER AFT ENTRY DOOR CRACKED 1.875 INCHED IN LENGTH. REPLACED CRACKED CHANNEL AND REINSTALLED AFT ENTRY DOOR ATTENDANT SEAT IAW DC9 OHM 25-21-3, MM 25-23-2 AND DC9 SRM 51-30-1, 51-30-2, 51-30-4, 51-30-5 AND AIRTRAN RES 981367. 2 L 7 2 4F A6WE 1998100900387 19981009 00387 WP 1998 10 9 VJ9800470 1 19980908 A 5311 99196181N FRAME DOUG DC9 DC932 3022066 WP BS 178 CRACKED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 LT MLG WW FRAME CRACKED UPPER AFT END TRAPEZOID STA 718. REPLACED FRAME STA 718 IAW EO 12-5311-29-B1044. 2 L 7 2 4F A6WE 1998100900388 19981009 00388 WP 1998 10 9 VJ9800471 1 19980911 A 5320 5910130387N1 CHORD DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 TEE CHORD HAS TONG CUT OFF AND CORROSION AT STA 996, L30. REMOVED TEE CHORD AT FS 996, L23L-29R, DRILLED DEBURRED, ALOD INED, PRIMED AND INSTALLED NEW TEE CHORD IAW DC9 SRM 53-03, FIG 37A, SB 53-232. 2 L 7 2 4F A6WE 1998100900389 19981009 00389 WP 1998 10 9 VJ9800472 1 19980915 A 5320 591486529N TEE DOUG DC9 DC932 3022066 WP BS 600 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 TEE CAP, STA 600. 28L-28R, CORRODED. DRILLED. LOCATED, DEBURRED AND INSTALLED NEW TEE CAP IAW DC9 SRM 51-10-4, 51-30, 5 1-20 AND DC9 DWG 5010068. 2 L 7 2 4F A6WE 1998100900390 19981009 00390 WP 1998 10 9 VJ9800473 1 19980915 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 600 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 BULKHEAD SKIN AT STA 600, L28L-28R, CORRODED. FORMED FILLER AND DOUBLERS, TREATED, PRIMED AND INSTALLED REPAIRS IAW DC9 SRM 51-10-3, 51-20, 51-30 AND ROD SKETCH 98-09-04-010. 2 L 7 2 4F A6WE 1998100900391 19981009 00391 WP 1998 10 9 VJ9800474 1 19980915 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 522 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 933VV 47489 FWD PIT FRAME FS 522, L24L-30, CORRODED. FABRICATED REPAIR FLOOR SUPPORT 7075-0, .063, HEAT TREATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-10-4, 51-10-2A, 53-21-0, 51-3-2 AND RES 981418. 2 L 7 2 4F A6WE 1998100900392 19981009 00392 WP 1998 10 9 VJ9800475 1 19980910 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 966VV 47168 LAP SEAM AT FS 200, L26L, CORRODED. CUT OUT AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLER IAW DC9 SRM 53-04 , FIG 37. 2 L 7 2 4F A6WE 1998100900393 19981009 00393 WP 1998 10 9 VJ9800476 1 19980930 A 3241 421396 CONTROL BOX DOUG DC9 DC932 3022066 WP MLG MALFUNCTIONED A ZZDA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 15 912VV 47359 NO BRAKE PRESSURE INDICATION WHEN ANTI-SKID SELECTED ON, TAKING AIRCRAFT RUNWAY POSITION. MAINTENANCE INSPECTED ANTI-SK ID AND BRAKE SYSTEM AND TROUBLE SHOT PROBLEM TO ANTI-SKID CONTROL BOX. . 2 L 7 2 4F A6WE 1998100900394 19981009 00394 WP 1998 10 9 VJ9800477 1 19980930 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE LOOSE A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 923VV 47529 GALLEY SLIDE COVER LOOSE. RESECURED IAW MM 25-61 AND PERFORMED REQUIRED INSPECTION. 2 L 7 2 4F A6WE 1998100900395 19981009 00395 WP 1998 10 9 VJ9800478 1 19980912 A 5311 9919817502 FRAME DOUG DC9 DC932 3022066 WP BS 966 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 MAIN FRAME RT FS 966 CRACKED. REPLACED FRAME IAW AIRTRAN EO 12-5311-29-B1044 AND RES 981533. 2 L 7 2 4F A6WE 1998100900396 19981009 00396 WP 1998 10 9 VJ9800479 1 19980917 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 530 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 RT WING LOWER REAR SPAR XW 530 VERTICAL LEG CORRODED. FABRICATED, INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-30-1, 51-10-4 , 53-22-1, AND AIRTRAN RES 981582. 2 L 7 2 4F A6WE 1998100900397 19981009 00397 WP 1998 10 9 VJ9800482 1 19980923 A 5711 SPAR DOUG DC9 DC932 3022066 WP WS 525 MAGNETIZED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 REPAIR ON AFT SIDE REAR SPAR LWR CAP XRS 525 DETERMINED TO BE MAGNETIC WITHIN 5 FEET FLUX VALVE. FABRICATED AND INSTALL ED REPAIR DOUBLER IAW DC9 SRM 51-10-3, 51-10-4 AND AIRTRAN RES 981625. 2 L 7 2 4F A6WE 1998100900398 19981009 00398 NM 1998 10 9 K3HA980114 1 19980930 A 3350 S106S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 FORWARD EMERGENCY AREA LIGHT BATTERIES DISCHARGED. REPLACED DISCHARGED BATTERIES IAW MM 33-59-00. 2 L 7 3 4F A3WE 1998100900399 19981009 00399 NM 1998 10 9 K3HA980115 1 19981001 A 5230 52J374 DOOR BOEING 727 727225 1384077 NM CARGO COMPT NOT SEALED A K3HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 356PA 20626 PASSING FL245, IN CLIMB, CABIN RATE OF CLIMB BECAME UNCONTROLLABLE. DIFFERENTIAL PRESSURE WAS APPROX 6.6 PSI. WARNING HORN SOUNDED AT 9000 FT CABIN ALTITUDE UNABLE TO CONTROL CABIN RATE OF CLIMB EVEN WITH MANUAL CONTROLLER UNTIL PASSING 1 6,200 FT IN DESCENT. CABIN RATE OF CLIMB BECAME UNCONTROLLABLE. FOUND SUIT CASE STRAP CAUGHT IN FWD CARGO DOOR SEAL. R EMOVED STRAP AND CHECKED SEAL. CHECK LEFT AND RIGHT PACK HEAT EXCHANGERS FOR LEAKAGE. CHECKED PNEUMATIC DUCTS FOR LEAKA GE, NONE NOTED. REMOVED AND REPLACED LEFT PACK FAN COOL DOOR ACT IAW MM 21-56-71, MAKING BOTH PACKS OPERATIONAL FOR TAK EOFF. PERFORMED PRESS SYSTEM CHECK NORMAL, ENGINES SYSTEM CHECK NORMAL IAW MM 21-30-0. 2 L 7 3 4F A3WE 1998100900400 19981009 00400 NM 1998 10 9 K3HA980116 1 19981001 A 2130 28620 VALVE BOEING 727 727225 1384077 NM E/E COMPT FAILED A K3HA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 25 356PA 20626 UNABLE TO CONTROL PRESSURIZATION ABOVE AT 12,300 CABIN GOT UP TO 8500 WITH APPROXIMATELY 4 TO 5 DIFFERENTIAL PRESSURE WI TH EVERYTHING CLOSED. REPAIRED L-1 DOOR SEAL LOWER MIDDLE PER MM 52-00-1, 52-11-71. FOUND EQUIP COOL FLOW CONTROL VALV E DEFECTIVE PRESSURIZED WITH VALVE LOCKED CLOSED ABLE TO GAIN 8.0 DIFF. PSI REMOVED AND REPLACED EQUIPMENT COOL FLOW CO NTROL VALVE IAW MM 21-58-21. PRESSURIZATION CHECK NORMAL PER MM 21-30-0. 2 L 7 3 4F A3WE 1998100900401 19981009 00401 EU 1998 10 9 JBXA980052 1 19981001 A 2910 AS1005D060608 UNION FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 HYD SYST CRACKED A JBXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 104ML 11445 INFLIGHT, HYDRAULIC SYSTEM NR 1 QUANTITY DOWN TO 34 PERCENT. AIRCRAFT DIVERTED TO EWR. TROUBLE SHOOTING, FOUND NR 1 SY STEM LEAKING AT T-FITTING MLG HYDRAULIC TUNNEL. REMOVED AND REPLACED T-FITTING, SERVICED AND LEAKED CHECKED SYSTEM, AND PRESSURE TESTED FITTING ALL IAW F-100 AMM CHPS 12-21-01, 29-00-00. 2 L 7 2 4F 4 F RT 1998100900402 19981009 00402 WP 1998 10 9 CALA9801857 1 19980926 A 2761 1040T1005 ACTUATOR DOUG DC9 DC982 3022082 WP SPOILER BURNT A CALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 12811 49265 THE CO-PILOT OBSERVED SMOKE COMING FROM THE THROTTLE QUADRANT AFTER TAKEOFF FROM COS. THE ELECTRICAL FIRE/SMOKE OF UNKN OWN ORIGIN EMERGENCY LIST WAS INITIATED AND THE AIRCRAFT WAS RETURNED TO COS WHERE IT LANDED WITHOUT INCIDENT. MAINTENA NCE FOUND THE AUTO SPOILER ACTUATOR BURNT WITH CIRCUIT BREAKER POPPED. THE AUTO SPOILER ACTUATOR WAS REMOVED AND REPLAC ED IAW MM 27-62-05. IN ADDITION, THE SPOILER CONTROL BOX WAS REMOVED AND REPLACED IAW MM 27-62-07. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998100900403 19981009 00403 NE 1998 10 9 CALA9801858 2 19980925 A 7320 LINE BOEING 737 737217 1384464 NM PWA JT8 JT8D9 52048 NE NR 1 ENGINE LEAKING A CALA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 09 14233 19887 665956 THE NR 1 ENGINE THROTTLE WAS TWO KNOBS AHEAD OF NR 2 WITH CLIMB POWER SET OUT OF MSP. THE SPLIT INCREASED TO ABOUT 3 KN OBS DIFFERENCE AS CLIMB PROGRESSED. FUEL FLOW WAS ABOUT 2000 LBS HIGHER ON NR 1 FOR SAME ENGINE PARAMETERS AT ABOUT 31, 000 FT. THE NR 1 ENGINE BEGAN TO SPOOL DOWN. THE ENGINE WAS SHUTDOWN AND THE ENGINE FAILURE CHECKLIST WAS COMPLETED. T HE A/C WAS DIVERTED TO ORD WHERE IT LANDED W/O INCIDENT. MX RAN THE NR 1 ENGINE AND FOUND FUEL LEAKING FROM OIL COOLER TO P/D VALVE LINE AT P/D FITTING. ALL SEALS AND RETAINERS FOR P/D VALVE WERE REPLACED IAW MM 73-12-1. THE ENGINE WAS R UN AT HIGH POWER WITH OPERATION CHECKING GOOD AND NO LEAKS DETECTED. 2 L 7 2 4F 4 F A16WE E2EA 1998100900404 19981009 00404 NM 1998 10 9 CALA9801859 1 19980925 A 3230 651781914 ACTUATOR BOEING 737 737130 1384435 NM NLG INOPERATIVE A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 77204 29982 19021 THE GEAR HANDLE WAS PLACED IN THE OFF POSITION AFTER TAKEOFF AND THE NOSE GEAR CAME DOWN. THE GEAR HANDLE WAS PLACED UP AND THE NOSE GEAR RAISED. THE GEAR HANDLE WAS THEN PLACED TO OFF AND THE GEAR STAYED UP. THE FLIGHT WAS CONTINUED WIT HOUT FURTHER PROBLEM. MAINTENANCE REMOVED AND REPLACED THE NOSE GEAR LOCK ACTUATOR IAW MM 32-33-21. THE NOSE GEAR WAS CYCLED SEVERAL TIMES AND OPERATION CHECKED GOOD. 2 L 7 2 4F A16WE 1998100900405 19981009 00405 1998 10 9 QXEA9801369 4 19980930 A 2330 AJA4N176 CONTACTOR DHAV DHC8 DHC8202 2809007 NM FUSELAGE MALFUNCTION A QXEA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NM 09 352PH 494 PSC- AFTER ENG START AND EXTERNAL POWER WAS REMOVED, THE RT SIDE OF THE COCKPIT WENT DEAD. THE DC BUS LIGHT, NR 2 GEN L IGHT, AND BATTERY TEMP WARNING LIGHT ALL ILLUMINATED. NOTICED DARK SMOKE COMING FROM THE RT NACELLE IN LARGE AMOUNTS AN D INCREASING IN INTENSITY. DISCHARGED NR 2 ENG AFT FIRE BOTTLE AND NOTIFIED CFR. SHUT DOWN ENG'S AND DEPLAINED PASSENG ERS W/O INCIDENT. MX INSPECTED AND FOUND NO EVIDENCE OF FIRE. REPLACED 2431 -K2 CONTACTOR, NR 2 STARTER GENERATOR, NR 2 GENERATOR CONTROL UNIT, MAIN A/C BATTERY, NR 2 ENG AFT FIRE BOTTLE, AND NR 2 ENG AFT FIRE BOTTLE BLOW OUT DISK. ALL O PS CHECKS GOOD. A/C RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998100900406 19981009 00406 NM 1998 10 9 QXEA9801370 1 19980930 A 6120 311835404 TSEU DHAV DHC8 DHC8202 2809007 NM NR 2 ENGINE MALFUNCTION A QXEA K NONE J WARNING INDICATION TO TAKEOFF 1 NM 09 368PH 520 BOI- AFTER TAKEOFF, THE AUTOFEATHER ARM LIGHT ILLUMINATED. CHECKED AGAIN AFTER LANDING AND THE AUTOFEATHER WILL NOT ARM . REPLACED THE NR 2 TORQUE SIGINAL CONDITIONER (TSEU). OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998100900407 19981009 00407 NM 1998 10 9 98FDEA00615 1 19981002 A 2910 LINE BOEING 727 72725 1384006 NM A HYD SYST FAILED A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 155FE 18288 98-241 COMPLETE LOSS OF SYS A IN FLT PRESS AND QUAN ZERO UNTIL GEAR CRANK DOWN. PER CONVERSATION WITH CREW 0 QUAN. LO W PRESS LIGHTS CAME ON. CREW SHUT OFF PUMP WITH 1000 PSI SHOW ON GAGE. REMOVED AND REPLACED PRESS LINE, NR 1 AND 2 ENG CASE DRAIN FILTER MM 29-11-0. OPR TEST NORM. 2 L 7 3 4F A3WE 1998100900408 19981009 00408 NM 1998 10 9 98FDEA00616 1 19981002 A 3610 CLAMPS BOEING 727 727227 1384078 NM NR 3 ENGINE DISCONNECTED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 25 494FE 21532 98-242 - APPROX 6 INTO FLT AT FL 330, NR 3 ENG STRUT OVERHEAT LIGHT ILLUM. CONFIG WAS BOTH PKS ON NR 2 AND NR 3 ENG BLD S OPEN, ENG ANTI-ICE CLOSED. RAN RED TAB PROCEDURES. ENG EXTINGUISH WITH NR 3 BLD CLOSED AND 3 ENG RETARD TO 65 PERCEN T N1. RESTORE ENG. LIGHT REMAIN EXTINGUISH REMAINDER OF FLT. FOUND CLAMP DISCONNECT BETWEEN PRECOOLER AND BLD AIR DUC T TO FIRE WALL RECONNECT CLAMP AND RAN ENG PER JET RUN HDBK. NO LEAKS FND. SYS CK OK PER MM 26-14-1. 2 L 7 3 4F A3WE 1998100900409 19981009 00409 WP 1998 10 9 ABXA9800855 1 19980927 A 3260 INDICATION DOUG DC8 DC863 302198A WP LANDING GEAR MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 815AX 46097 WHEN PERFORMING LANDING GEAR UPLATCH CHECK, RED LANDING GEAR NOT LATCHED LIGHT ILLUMINATED. RECYCLED GEAR, SAME RESULT S. OPS CHECKED LANDING GEAR. CLEARANCE CHECKS ALL FELL WITHIN LIMITS. NO DEFECTS NOTED. 2 L 7 4 4F 4A25 1998100900410 19981009 00410 WP 1998 10 9 ABXA9800844 1 19980926 A 5230 4920987503 FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND CARGO DOOR NR 4 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05. 2 L 7 2 4F A6WE 1998100900411 19981009 00411 WP 1998 10 9 ABXA9800845 1 19980926 A 5230 4920987503 FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND CARGO DOOR NR 5 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05. 2 L 7 2 4F A6WE 1998100900412 19981009 00412 WP 1998 10 9 ABXA9800846 1 19980926 A 5230 4920987503 FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND CARGO DOOR NR 2 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05. 2 L 7 2 4F A6WE 1998100900413 19981009 00413 WP 1998 10 9 ABXA9800847 1 19980926 A 5230 4920987503 FITTING DOUG DOUG DC9 DC932F 3022067 WP CARGO DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND CARGO DOOR NR 6 SPOOL FITTING ASSY PITTED. REMOVED CORROSION IAW SRM 53-05. 2 L 7 2 4F A6WE 1998100900414 19981009 00414 WP 1998 10 9 ABXA9800848 1 19980926 A 5720 9919402505 TRAP PANEL DOUG DOUG DC9 DC932F 3022067 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND LEFT FORWARD UPPER HORIZONTAL TRAPEZOIDAL PANEL CRACKED PAST 4TH HOLE. REPAIRED HORIZONTAL TRAPEZ OIDAL PANEL IAW DC9 SRM 57-09. 2 L 7 2 4F A6WE 1998100900415 19981009 00415 WP 1998 10 9 ABXA9800849 1 19980926 A 5311 99582387 FRAME DOUG DOUG DC9 DC932F 3022067 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND FRAME CRACKED AT LONGERON 17 RIGHT FS 980. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998100900416 19981009 00416 WP 1998 10 9 ABXA9800850 1 19980926 A 5330 59114025 SKIN DOUG DOUG DC9 DC932F 3022067 WP BS 69.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND NOSE SKIN CRACKED AT FS 69.5 LONGERON 15 LEFT. REPAIRED IAW EA 53100074-003-3. 2 L 7 2 4F A6WE 1998100900417 19981009 00417 WP 1998 10 9 ABXA9800851 1 19980926 A 5312 995821225 BULKHEAD TEE DOUG DOUG DC9 DC932F 3022067 WP BS 756 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND CORROSION ON UPPER SURFACE OF THE FORWARD LEG OF THE TEE-ANGLE AT STATION 756 BL O.O. REPAIRED BU LKHEAD TEE-ANGLE IAW REA D953-24842-MR. 2 L 7 2 4F A6WE 1998100900418 19981009 00418 WP 1998 10 9 ABXA9800852 1 19980926 A 5753 5910042502 VANE DOUG DOUG DC9 DC932F 3022067 WP RT TE FLAP DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND RIGHT CENTER FIXED VANE DELAMINATED. REPLACED FIXED VANE IAW DC9 MM 27-51-14. 2 L 7 2 4F A6WE 1998100900419 19981009 00419 WP 1998 10 9 ABXA9800853 1 19980928 A 5730 59127351 PANEL DOUG DOUG DC9 DC932F 3022067 WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND LEFT WING UPPER OUTBOARD BONDED PANEL, FORWARD OF AILERON, DELAMINATED. REPLACED LEFT WING UPPER OUTBOARD BONDED PANEL IAW DC9 SRM 51-30-1, 51-30-2, AND 51-10-4. 2 L 7 2 4F A6WE 1998100900420 19981009 00420 WP 1998 10 9 ABXA9800854 1 19980928 A 5753 995760016 ANGLE DOUG DOUG DC9 DC932F 3022067 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND OUTBOARD ATTACH ANGLE FOR RIGHT FLAP OUTBOARD HINGE CRACKED. REPLACED OUTBOARD SUPPORT ANGLE AND FORMER IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998100900421 19981009 00421 NM 1998 10 9 DL76G982030 1 19981001 A 3350 BPS73 POWER SUPPLY BOEING 767 7673P6 1385105 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 155DL 25269 FOUND ON O/W II F/C AND B/C SEAT TRACK LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY OPS CKS OK. 2 L 7 2 4F RT A1NM 1998100900422 19981009 00422 NM 1998 10 9 DL72S982032 1 19981002 A 5522 657278420 SKIN BOEING 727 727232 1384082 NM RT EVATOR MISDRILLED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 485DA 20865 RT ELEVATOR, REAR SPAR MOD, OS HOLES: AD 96-06-05. DURING REAR SPAR MOD PER EO 4-70183-3AD, SEVERAL H OLES IN THE UPPER SKIN WERE OVERSIZED. REPAIR BONDED AN INTERNAL DOUBLER AND INSTALL OVERSIZED FASTENERS. 2 L 7 3 4F A3WE 1998100900423 19981009 00423 NM 1998 10 9 DL72S982033 1 19981002 A 5753 65192708 TRACK BOEING 727 727232 1384082 NM TE FLAP CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 INBD FLAP INBD TRACK TYP CORROSION AT MLG BEAM ATTACH HOLES AND FWD LUG: AD 90-07-05: TYPICAL CORROSION WAS FOUND TO TH E MLG BEAM ATTACH HOLES (WITHIN THE AD AREA) AND AT THE FWD ATTACH LUG. OVERSIZED CORRODED HOLES AND MACHINED LUG FACES . 2 L 7 3 4F A3WE 1998100900424 19981009 00424 NM 1998 10 9 DL757982034 1 19981002 A 2120 212N30763 DUCT BOEING 757 757232 1384965 NM BS 1300 CRACKED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 650DL 212N30762 24390 DESCENDING THROUGH 16K ON APPROACH, A BURNING SMELL NOTICED BEGINNING AT ROW 34RT. SMELL SPREAD THROUGHOUT CABIN AND WA S SIMILAR TO BURNING POPCORN. F/A'S CKD FLOOR AT ROW 34 AND REPORTED FLOOR WAS WARM. SMELL DISSIPATED ON LANDING AFTER A/C WAS DEPRESSURIZED. NO VISIBLE SMOKE NOTED. FOUND APU AIR DUCT AT STA 1300 IN AFT BAG BIN CRACKED. REPLACED DUCT . 2 L 7 2 4F RT A2NM 1998100900425 19981009 00425 NM 1998 10 9 DL76L982035 1 19980930 A 5400 SPAR WEB BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 181DN 25986 PYLON NR 1 ENGINE NACELLE STRUT, AFT UPPER SPAR WEB FS 222, LBL4, CRACK REPAIR. A .75 INCH LONG CRACK WAS FOUND EMANATI NG FROM THE AFT, OUTBD CORNER OF A CUTOUT IN THE AFT UPPER SPAR WEB OF THE NR 1 ENGINE NACELLE STRUT AT FS 222, LBL4. THE CRACK WAS ROUTED OUT AND A STEEL DOUBLER REPAIR WAS INSTALLED AROUND THE CORNER OF THE CUTOUT PER ER/A 365126-14, R EV B. 2 L 7 2 4F RT A1NM 1998100900426 19981009 00426 NM 1998 10 9 DL72K982036 1 19981002 A 5320 65872608 FITTING BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 RT I/B TENSION TIE BOLT FITTING CRACKED. REPLACED PER BAC DRAWING 65-17509. 2 L 7 3 4F A3WE 1998100900427 19981009 00427 NM 1998 10 9 DL72S982037 1 19981003 A 2913 PUMP AS19570C BOEING 727 727232 1384082 NM B HYD SYST FAILED A DALA O OTHER K FLUID LOSS DE DESCENT 1 SO 27 477DA 1480620 20754 ON DESCENT, HYD QUANTITY SYSTEM 'B' WENT TO .3 GALLONS AND SLOWLY CONTINUED DOWN. RAN SYSTEM 'B' FLUID LOSS INOP CHECKL IST. FOUND NR 2 'B' SYSTEM PUMP LEAKING. REPLACED SAME, SERVICED RESERVIOR. PUMP OPS NORMAL. 2 L 7 3 4F A3WE 1998100900428 19981009 00428 NM 1998 10 9 DL73E982039 1 19981003 A 2121 FAN 215201 BOEING 737 737247 138448D NM A/C BAY FAILED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 236WA 23184 GASPER FAN C/B FOUND OPEN, WHEN CLOSED IT RETRIPPED ACCOMPANIED BY A LOUD POP HEARD UNDER FLOOR IN MID CABIN AND STRONG ELECTRICAL SMELL. INSP GASPER FAN NO PROBLEMS. REPLACED FAN. 2 L 7 2 4F A16WE 1998100900429 19981009 00429 NM 1998 10 9 DL72K982040 1 19981002 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 479DA 20756 FOUND ON B2 LETTER CK, LT AFT ENTRY DOOR FRAME CRACKED BELOW THE UPPER STOP CASTING WL 273. REPAIRED PER SRM 53-10-9. N R CARD 87. FOUND ON B2 LETTER CK, RT AFT ENTRY DOOR FRAME CRACKED BELOW THE UPPER STOP CASTING WL 273. REPAIRED PER SR M 53-10-9. NR CARD 86. 2 L 7 3 4F A3WE 1998100900430 19981009 00430 WP 1998 10 9 DLL19982041 1 19981003 A 2170 COALESCER LKHEED 1011 10113853 5265020 WP CABIN CONTAMINATED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 762DA 193Y1210 OILY SMELL IN 1ST CLASS CABIN AND C/P SMELL SEEMED NEARLY DISAPPEARED WITH NR 2 PACK OFF. RAN ENGINES PER PFHB AND PACK S ISOLATED SMELL TO NR 1 PACK. REPLACED COALESCER. 2 L 7 3 4F A23WE 1998100900431 19981009 00431 NM 1998 10 9 DLM11982042 1 19981003 A 2611 SMOKE ALERT DOUG MD11 MD11 3023602 NM LAVATORY ACTIVATED A DALA O OTHER N FALSE WARNING CR CRUISE 1 SO 27 810DE 48565 LAV SMOKE ALERT APPEARED FOR 10 MINS, RT SIDE BUSINESS CLASS LAV AND LT SIDE BUSINESS CLASS LAV. RED ANNUN LIGHTS CAME ON FOR BOTH LAVS. LAV SMOKE DETECTORS CHECKED, NO FAULTS FOUND. 2 L 7 3 4F RT A22WE 1998100900432 19981009 00432 NM 1998 10 9 DL76L982043 1 19981003 A 2497 WIRE BOEING 767 767332 1382001 NM SEAT 2A/B SHORTED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 174DN 24802 PAX SPILLED DRINK ON ELECT MOTORSEAT 2A/B, SHORTED OUT. BESIDES SEATS 2A/B FOUND CHAFFED/SHORTED WIRES BETWEEN AIR LOUV ERS/FLOOR. CUT WIRES, ISOLATED WITH END CONNECTORS/TAPE. MADE PROTACTED INSP OF WIRES BUNDLES BEHIND AIR LOUVERS FOUND SATISFACTORY STORED WIRES BEHIND LOUVER/FIXED. RESET C/B, FOOTREST/CHECKED. FOUND NORMAL. FWD TO MCO FOR MAIN BASE R EPAIR OF WIRES BUNDLES. SEATS 2A/B INOP IN ELECT MODE. OK IN MANUAL MODE. 2 L 7 2 4F RT A1NM 1998100900433 19981009 00433 NM 1998 10 9 DLM88982044 1 19981004 A 2530 OVEN 50459 DOUG MD88 MD88 3023688 NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 969DL 0266 53172 FWD GALLEY OVEN OVERHEATED AND STARTED SMOKING, PULLED C/B AND DISCONNECTED GALLEY POWER, SMOKED STIPPED. REPLACED OVEN /OPS OK. 2 L 7 2 4F RT A6WE 1998100900434 19981009 00434 WP 1998 10 9 DLL19982045 1 19981004 A 4990 OIL SYST LKHEED 1011 10113853 5265020 WP APU LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 27 762DA 26836 193Y1210 AFTER T/O, HAD ODOR AS DESCRIBED IN PREVIOUS WRITE UP THIS. DISSIPATED UNTIL DESCENT INITATED, THEN WHOLE CABIN AND FLT DECK FILLED WITH A VAPOR SMOKE. FOUND APU INTERNAL OIL LEAK. 2 L 7 3 4F A23WE 1998100900435 19981009 00435 NM 1998 10 9 DL757982046 1 19981003 A 5210 LATCH ROLLER BOEING 757 757232 1384965 NM PAX DOOR OUT OF ADJUST A DALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 27 607DL 22814 LT AFT ENTRY DOOR EICAS LIGHT INFLIGHT WITH AN ENTRY DOOR LIGHT ON FINAL APPROACH THE DOOR OPENED. 37,000 FT WHEN LIGHT CAME ON. CREW MADE EMERG DESCENT. ADJUSTED LATCH ROLLER OVER CTR PER MM AND ADJUST ESCAPE SLIDE HEIGHT. CHECKS GOOD . 2 L 7 2 4F RT A2NM 1998100900436 19981009 00436 WP 1998 10 9 DLL19982048 1 19981004 A 2120 AIR DISTR LKHEED 1011 10113853 5265020 WP CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 759DA 193Y1176 A/C DIVERTED COS DUE TO ODOR SIMILAR TO SULPHUR SMELL AT SEATS 22 AND 23 DF. A/C LANDED OVERWEIGHT 38K. CONTRACT MAINT INSPECTED AREA AND PERFORMED OVERWEIGHT LANDING INSP PER MM 5-50-01. NO DISCREPANCIES NOTED. 2 L 7 3 4F A23WE 1998100900437 19981009 00437 NM 1998 10 9 DL72S982053 1 19980929 A 5753 652163361 RIB BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 INBOARD AFT CLOSE OUT RIB CRACKED AT LWR AFT CORNER. DAMAG REPAIRED PER MM 57-52-0 ON SHOP ORDER 582612. 2 L 7 3 4F A3WE 1998100900438 19981009 00438 SO 1998 10 9 SWIA971266 1 19980902 A 2752 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT TE FLAP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 1105G 120105 ON FLAP RETRACTION AFTER DEPARTURE INBOARD FLAPS DID NOT RETRACT AND ASYMMETRY LIGHT ON FLAP PANEL ILLUMINATED. RETURNE D TO PDX. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR IAW MM 27-50-7. OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100900439 19981009 00439 1998 10 9 SWIA971267 4 19980903 A 2215 6225734002 SERVO EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE AUTO PILOT JAMMED A SWIA O OTHER F FLT CONT AFFECTED DE DESCENT 1 NM 07 212SW 120276 RUDDER PEDALS LOCKED DURING APPROACH AND LANDING. WAS ABLE TO REGAIN CONTROL WITH TILLER ON THE RUN WAY. FOUND RUDDER SERVO JAMMED. REPLACED RUDDER SERVO. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100900440 19981009 00440 EA 1998 10 9 SWIA971268 1 19980903 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 403SW 7028 WHILE DESCENDING INTO TUC FLAPS FAIL MESSAGE CAME ON. COMPLIED WITH CHECKLIST AND LANDED IN TUC WITH 0 FLAPS. POWERED DOWN AIRCRAFT FLAPS SYSTEM AND RESET SYSTEM. CHECKS NORMAL. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100900441 19981009 00441 EA 1998 10 9 SWIA971269 1 19980904 A 2751 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 403SW 7028 FLAPS FAILS MESSAGE AT LEVEL OFF EN ROUTE SLC/BOI. RETURNED TO SLC. REPLACED LEFT FLAP BRAKE POSITION SENSOR. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100900442 19981009 00442 1998 10 9 SWIA971270 4 19980905 A 3425 6226190204 AHC EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LEFT FAILED A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 187SW 120037 AFTER TAKEOFF IN 30 DEGREE RIGHT TURN THE YAW, TCAS AND CAPTAIN, GYRO FAILED. THEN ON APPROACH BACK INTO SLC FLAPS RIGH T INBOARD FAILED. INSTALLED NEW AHC-85 ON CAPTAINS SIDE AND ORIENTATED. OPS CHECKS GOOD. CLEANED FLAPS, CANNON PLUGS AND INSPECTED FLAPS. CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100900443 19981009 00443 SO 1998 10 9 SWIA971271 1 19980907 A 7112 TQ SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 207SW 120266 AFTER TAKEOFF RIGHT TORQUE GAUGE OSCILLATED BETWEEN 40 PERCENT AND 100 PERCENT AND THEN FEATHERED INADVERTENTLY. RETURN ED TO FIELD, REMOVED AND REPLACED TORQUE SENSOR ON RIGHT ENGINE, IAW EMB MM 76-11-02. REMOVED AND REPLACED RIGHT ENGINE HMU IAW MM 73-21-00 AND RII 73-301-IAW. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100900444 19981009 00444 1998 10 9 SWIA971272 4 19980907 A 3425 DPU EMB 120 EMB120RT SO PWA 118 PW118A NE LT/RT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 250YV 120250 AFTER ROTATION CAPTAIN'S EFIS FAILED (BLANK SCREEN). RETURNED TO FIELD. REPLACED BOTH DPU'S. OP CHECKED GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100900445 19981009 00445 NM 1998 10 9 P5CA9801527 1 19980921 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1955-1963 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 850FT 19755 LEVEL 2 CORROSION FOUND IN BULK CARGO COMPARTMENT BS 1955-1963L BL 5-7 STR 51. REPLACED AND SPLICED STRINGER PER SRM 51 -10-01 PG 18 AND SRWS914578. 2 L 7 4 4F A20WE 1998100900446 19981009 00446 NM 1998 10 9 P5CA9801528 1 19980904 A 3260 65B4750650 LOGIC BOX BOEING 747 747122 1384872 NM LANDING GEAR MALFUNCTION A P5CA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 WP 23 852FT 19757 FOLLOWING T/O, RED GEAR LIGHT ON P2 WITH HORN. AIR TURN BACK. REPLACED LANDING GEAR LOGIC MODULE IAW MM 31-26-03, OPS CHECK OK. 2 L 7 4 4F A20WE 1998100900447 19981009 00447 WP 1998 10 9 CKSA98539 1 19980927 A 2120 AIR DISTR LKHEED 1011 1011385115 5265015 WP COCKPIT ODOR A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 GL 23 107CK 193N1182 A STRONG ELECTRICAL SMELL WAS NOTICED IN THE COCKPIT AT 10,000 FT. WHEN STARTING THE APU. RAN APU AND APPLIED ELECTRIC AL POWER AND OPERATED PACKS. CHECKED LOWER FESC AND MESC. NO DEFECTS NOTED. ALL ELECTRICAL LOAD INDICATORS NORMAL. N O ELECTRICAL ODOR NOTICED. OK FOR SERVICE. 2 L 7 3 4F A23WE 1998100900490 19981009 00490 EU 1998 10 9 UF6A980704 1 19980708 A 3350 P4010021 BATTERY PACK BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 858AW 2035 GRB - FLT 5734 - FLIGHT ATTENDANT 'B' FLASHLIGHT INOP. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. SYSTEM OPS CHECK ED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900491 19981009 00491 EU 1998 10 9 UF6A980703 1 19980704 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 11461 2034 ORD - UPON DAILY INSPECTION, FOUND EMERGENCY LIGHTS INOP AT SEAT ROW 6 AND 7. MAINTENANCE REMOVED AND REPLACED NR 3 POW ER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900492 19981009 00492 EU 1998 10 9 UF68980702 1 19980703 A 3350 OL3071BPEGPL BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 853AW 2022 RIGHT AFT EMERGENCY LIGHT ASSEMBLY BULB INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998100900493 19981009 00493 NM 1998 10 9 TAOA099804 1 19980905 A 3350 P2070001214 FLASHLIGHT BOEING 727 727254 138408L NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 913TS 20250 FLT 6050, FOUND ON L/S CHECK, EMERGENCY FLASH LIGHT AT L-1 DOOR INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT AT L-1 DOO R CHECKS OK. (M) 2 L 7 3 4F A3WE 1998100900494 19981009 00494 NM 1998 10 9 TAOA099805 1 19980906 A 2611 824PY SMOKE DETECTOR BOEING 727 727254 138408L NM LAVATORY FAILED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 916TS 20437 FLIGHT 6520 - DCA-LGA - FORWARD LAVATORY SMOKE DETECTOR GOES OFF CONTINOUSLY. REPLACED FORWARD LAVATORY SMOKE DETECTOR OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998100900495 19981009 00495 NM 1998 10 9 TAOA099806 1 19980908 A 2611 824PY SMOKE DETECTOR BOEING 727 727225 1384077 NM LAVATORY MALFUNCTIONED A TAOA K NONE O OTHER IN INSP/MAINT 1 EA 15 922TS 20415 FLT 6110 - LGA-BOS - AFT LAV SMOKE DETECTOR CAME ON IN FLIGHT. REPLACED AFT LAV SMOKE DETECTOR PER MM 25-60-01. (M) 2 L 7 3 4F A3WE 1998100900496 19981009 00496 NM 1998 10 9 TAOA099807 1 19980908 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 922TS 20415 FLT 6141 - BOS-LGA - AFT EXIT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK OPERATIONAL CHECK NORMAL. (M ) 2 L 7 3 4F A3WE 1998100900497 19981009 00497 EU 1998 10 9 SIMA982421 1 19980830 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 536AT 1076 536 ORD - FLT 4326 - FLOOR PROXIMITY LIGHTS DOES NOT ILLUMINATE AT THE FORWARD PART OF THE CABIN. REMOVED AND REPLACED BATT ERY PACK AT SEAT ROW 4B. (M) 2 H 7 2 4T RT A53EU 1998100900498 19981009 00498 EU 1998 10 9 SIMA982411 1 19980829 A 5311 S5367131120051 FRAME AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURNIG CPCP-1 INSPECTION, FOUND FRAME 37 CORRODED ON THE RIGHT SIDE AT FLOOR LEVEL. REPAIRED FRAME. AIRCRAFT RET URNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900499 19981009 00499 EU 1998 10 9 SIMA982401 1 19980828 A 5347 S53678001240 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT INBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. RE MOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900500 19981009 00500 EU 1998 10 9 98ZZZM705 1 19980828 A 5347 S53678001242 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT INBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. RE MOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900501 19981009 00501 EU 1998 10 9 98ZZZM706 1 19980828 A 5347 S53678001225 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT INBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. RE MOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900502 19981009 00502 EU 1998 10 9 SIMA982391 1 19980827 A 5347 S53375001200 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AT 293 DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT F LIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900503 19981009 00503 EU 1998 10 9 98ZZZM707 1 19980827 A 5347 S53678001201 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AT 293 DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT F LIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900504 19981009 00504 EU 1998 10 9 98ZZZM708 1 19980827 A 5347 S53678001246 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AT 293 DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT F LIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900505 19981009 00505 EU 1998 10 9 98ZZZM709 1 19980827 A 5347 S53678001210 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AT 293 DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT F LIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900506 19981009 00506 EU 1998 10 9 98ZZZM710 1 19980827 A 5347 S53678001212 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 293AT 293 DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT F LIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900507 19981009 00507 EU 1998 10 9 SIMA982382 1 19980826 A 5315 S5367240620801 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 36 WITH SEVERAL ELONGATED HOLES ADJACENT TO SERVICE DOOR, AND FLOORBEAMS 38 AND 40 WERE CORRODED. REPAIRED ALL FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900508 19981009 00508 EU 1998 10 9 98ZZZM711 1 19980826 A 5315 S5367240720201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 36 WITH SEVERAL ELONGATED HOLES ADJACENT TO SERVICE DOOR, AND FLOORBEAMS 38 AND 40 WERE CORRODED. REPAIRED ALL FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900509 19981009 00509 EU 1998 10 9 98ZZZM712 1 19980826 A 5315 S5367240921801 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 282AT 282 SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 36 WITH SEVERAL ELONGATED HOLES ADJACENT TO SERVICE DOOR, AND FLOORBEAMS 38 AND 40 WERE CORRODED. REPAIRED ALL FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900510 19981009 00510 EU 1998 10 9 SIMA982331 1 19980821 A 3350 3012001 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 399AT 674 399 DFW - FLT 3618 - WITH EMERGENCY LIGHT SWITCH DISARMED. FLOOR PROXIMITY LIGHTS ILLUMINATED. REMOVED AND REPLACED BATTER Y PACK. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998100900511 19981009 00511 EU 1998 10 9 SABA980042 1 19980825 A 5270 SENSOR BAG JETSTM JETSTM3201 1500217 EU PAX DOOR MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 957AE 957 CLT - FLT 5205 - AFTER DEPARTING, THE DOOR WARNING CAPTION LIGHT CAME ON. AIRCREW DID NOT DECLARE AN INFLIGHT EMERGENCY . AIRCRAFT RETURNED TO CHARLOTTE, WITH NO OTHER PROBLEMS. MAINTENANCE INSPECTED THE DOOR LOCKS AND MICROSWITCHES. DOO R ALIGNMENT MARKING CHECKED GOOD. DOOR WAS OPENED AND CLOSED SEVERAL TIMES. DOOR WAS DEFERRED TO MSL. (M) 2 L 7 2 4T RT A56EU 1998100900512 19981009 00512 NM 1998 10 9 MASA98176 1 19980911 A 6123 AUTOFEATHER DHAV DHC8 DHC8202 2809007 NM PROPELLER MALFUNCTIONED A MASA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SW 07 446YV 446 FLT 5338 - PSP-PHX - AUTOFEATHER WOULD NOT ARM ON TAKEOFF. AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND THE SYSTEM OPERATED NORMALLY. NO DISCREPANCIES WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998100900513 19981009 00513 NM 1998 10 9 MASA98178 1 19980914 A 3350 GE85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 447YV 447 DURING ROUTINE MAINTENANCE, FOUND FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH 'ON' ANNUNCIATOR LIGHT WOULD NOT ILLUMINATE. BULB WAS REMOVED AND REPLACED, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998100900514 19981009 00514 NM 1998 10 9 HNAA9891037 1 19980807 A 2150 78249016 ACM DHAV DHC8 DHC8102 2809003 NM FUSELAGE FAILED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 910HA 3286 880345 022 FLT 3019 - CRW-DCA - NOXIOUS FUMES COMING FROM AIR CONDITIONING SYSTEM DURING FLIGHT. REMOVED AND REPLACED ACM AND HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998100900515 19981009 00515 NM 1998 10 9 98ZZZM713 1 19980807 A 2150 7786832 HEAT EXCHANGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE FAILED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 07 910HA 3286 931110 022 FLT 3019 - CRW-DCA - NOXIOUS FUMES COMING FROM AIR CONDITIONING SYSTEM DURING FLIGHT. REMOVED AND REPLACED ACM AND HEAT EXCHANGER. OPS AND LEAK CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998100900516 19981009 00516 NM 1998 10 9 HNAA9881641 1 19980828 A 5610 NP15790110 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT CRACKED A HNAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 07 816MA 92081H7769 231 FLT 3032 - ORF-CLT - RIGHT FORWARD FLIGHT DECK WINDSHIELD CRACKED DURING CLIMB, RETURNED TO ORF. REMOVED AND REPLACED W INDSHIELD. (M) 2 H 7 2 4T RT A13NM 1998100900517 19981009 00517 NM 1998 10 9 HNAA9897540 1 19980827 A 3350 6013211 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 975HA 17191 SBY84 176 DURING PRE-FLIGHT INSPECTION FOR FLIGHT 3349 DCA - CRW RIGHT FORWARD EXTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACE D BATTERY PACK 3351-PS2. (M) 2 H 7 2 4T RT A13NM 1998100900518 19981009 00518 NM 1998 10 9 HNAA9893142 1 19980828 A 5520 85520147103 STOP DHAV DHC8 DHC8102 2809003 NM HORIZ STAB SEPARATED A HNAA K NONE F FLT CONT AFFECTED CR CRUISE 1 EA 07 931HA 26610 132 FLT 3264 - EWN-CLT, FULL NOSE DOWN ELEVATOR TRIM REQUIRED FOR STRAIGHT AND LEVEL FLIGHT. DISCOVERED RIGHT ELEVATOR TOP STOP BUMPER BROKEN OFF ALLOWING ELEVATOR TO STRIKE RUDDER DURING RON IN EWN. REMOVED AND REPLACED ELEVATOR BUMPER AND R EPAIRED ELEVATOR AND TRIM TAB. (M) 2 H 7 2 4T RT A13NM 1998100900519 19981009 00519 NM 1998 10 9 HNAA9892839 1 19980827 A 5311 85530184 FRAME DHAV DHC8 DHC8102 2809003 NM APU BAY CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 928HA 120 DURING AN APU CHANGE AT RON IN SBY, A CRACK WAS FOUND ON A FRAME AT THE 10 O'CLOCK POSITION. THE CRACK WAS REPAIRED IAW RD8-55-199. (M) 2 H 7 2 4T RT A13NM 1998100900520 19981009 00520 NM 1998 10 9 HNAA9893843 1 19980828 A 3350 6013211X BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 938HA 19112 SBY50 152 DURING ORIGINATING CHECK FOR FLIGHT 3287 FROM TLM TO MCO, TWO FORWARD RED ESCAPE PATH LIGHTS INOP. REMOVED AND REPLACED POWER SUPPLY 3352 PS2. (M) 2 H 7 2 4T RT A13NM 1998100900521 19981009 00521 NM 1998 10 9 HNAA9892044 1 19980902 A 3230 574205 VALVE DHAV DHC8 DHC8102 2809003 NM MLG FAILED A HNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 07 920HA 33868 276 084 FLT 3470 - CLT-CHA - UPON GEAR UP SELECTION AFTER TAKEOFF, 3 RED UNSAFE LIGHTS ILLUMINATED AND GEAR DID NOT MOVE. SELEC TED GEAR DOWN AND 3 GEAR DOWN/LOCKED LIGHTS ON. RETURNED TO CLT. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998100900522 19981009 00522 NM 1998 10 9 HNAA9891746 1 19980908 A 3241 39671 VALVE HYDROAIRE DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE LEAKING A HNAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 07 917HA 16336 410 75 CRW/CLT - FLT 3342 - DURING DESCENT, NR 1 HYDRAULIC ISOLATE AND ROLL SPOILER INBD HYDRAULIC CAUTION LIGHTS ILLUMINATED W ITH REDUCED NR 1 HYDRAULIC SYSTEM QUANTITY. PERFORMED ZERO FLAP LANDING WITH NO NORMAL WHEEL BRAKES. REMOVED AND REPLA CED NR 1 ANTI-SKID CONTROL VALVE. LEAK AND OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998100900523 19981009 00523 WP 1998 10 9 G60A028 1 19980908 A 2830 AV16B1926C VALVE DOUG DC10 DC1030F 3023504 WP LT WING FAILED A G6OA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 601GC J62893A 47921 WHILE RETURNING TO ANC, UPON COMPLETION OF THE FUEL DUMP PROCEDURES, THE LEFT FUEL DUMP VALVE INDICATED A FAILURE TO CLO SE. GROUND MAINTENANCE REMOVED AND REPLACED THE GATE VALVE SHUTOFF ASSY IAW MM 28-30-02. OPERATIONAL CHECK NORMAL. (M ) 2 L 7 3 4F RT A22WE 1998100900524 19981009 00524 NM 1998 10 9 USAASB98212 1 19980817 A 7921 749965 OIL COOLER BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 EA 19 255AU 15655 22797 BWI - FLT 2662 - UPON CLIMB-OUT FROM BWI, THE NR 1 ENGINE OIL TEMPERATURE WENT INTO THE YELLOW BAND AT FL 160. FLIGHT R ETURNED TO FIELD AT BWI AND LANDED WITHOUT FURTHER INCIDENT. TEMPERATURE REMAINED IN YELLOW BAND FOR 12 MINUTES THEN WE NT TO THE EDGE OF GREEN BAND ON APPROACH. MAINTENANFE REMOVED AND REPLACED THE NR 1 ENGINE OIL COOLER ASSY AND THE OIL FILTER. OLD OIL FILTER CHECKED GOOD. RAN ENGINE AT TAKEOFF POWER FOR 2 MINUTES AND AT CRUISE POWER FOR 15 MINUTES. OI L TEMPERATURE INDICATION CHECKS GOOD ALONG WITH LEAK CHECK. (M) 2 L 7 2 4F A16WE 1998100900525 19981009 00525 NE 1998 10 9 USAASB98221 2 19980824 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE RT WING OVERTEMP A USAA E A ENGINE SHUTDOWN UNSCHED LANDING M J Y OVER TEMP WARNING INDICATION ENGINE STOPPAGE CL CLIMB 1 EA 19 260AU 38744 22866 709085 PIT - FLT 1571 - ON CLIMB-OUT FROM BUF, THE NR 2 ENGINE HIGH OIL TEMPERATURE LIGHT ILLUMINATED FOLLOWED BY THE LOW OIL P RESSURE LIGHT. CAPTAIN SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO PIT. FLIGHT LANDED WITHOUT INC IDENT. TOTAL SINGLE ENGINE TIME WAS 30 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSY. OPERATIONAL CH ECK LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998100900526 19981009 00526 NM 1998 10 9 USAA980365 1 19980826 A 5315 146N508922 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 614AU 18837 27145 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES .5 INCH BY .5 INCH BY 85 INCHES STATION 164 0 LBL 30 AND LBL 55 FLOORBEAM. CORROSION TASK NR C53-251-03. REPAIRED 'T' CAP PER EA 62303 AND SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1998100900527 19981009 00527 NM 1998 10 9 USAA980373 1 19980728 A 5320 WEB BOEING 757 757225 1384959 NM BS 1660-1681 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 44236 22198 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH CORROSION AREA FROM STATION 1660-1681 AT RBL 10 WEB. CORROSION TASK NR C53-251-03. FABRICATED AND REPLACED TO ANGLE OF WEB PER SRM 51-60-51. (M) 2 L 7 2 4F RT A2NM 1998100900528 19981009 00528 NM 1998 10 9 USAA980362 1 19980731 A 5314 144N814047 KEEL BEAM BOEING 757 757225 1384959 NM BS 1030 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 44236 22198 CLT - DURING C-2 CHECK VISUAL INSPECTION, FOUND CORROSION KEEL BEAM SUPPORT STATION 1030 LOWER FRAME BS 1030. REMOVED A ND REPLACED SUPPORT WITH IDENTICAL PART. (M) 2 L 7 2 4F RT A2NM 1998100900529 19981009 00529 NM 1998 10 9 USAA980363 1 19980731 A 5314 144N814048 KEEL BEAM BOEING 757 757225 1384959 NM BS 910 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 603AU 44236 22198 CLT - DURING A C-2 CHECK VISUAL INSPECTION, FOUND CORROSION KEEL BEAM SUPPORT STATION 910. REMOVED AND REPLACED SUPPORT WITH IDENTICAL PART. (M) 2 L 7 2 4F RT A2NM 1998100900530 19981009 00530 NM 1998 10 9 USAA980364 1 19980826 A 5315 146N508922 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 614AU 18837 27145 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SCREW HOLES 1.25 INCH BY 1.125 INCH BY .025 INCH STATIO N 1640 RBL 45 FLOORBEAM. CORROSION TASK NR C53-251-03. REPAIRED 'T' CAP PER EA 62306 AND SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1998100900531 19981009 00531 NM 1998 10 9 USAA980372 1 19980826 A 5320 SUPPORT BOEING 757 7572B7 1384964 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 614AU 27145 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AFT SIDE OF BEARING SUPPORT HOUSING FOR BODY TORQUE TU BE L-4 DOOR. FABRICATED REPAIR STRAP FROM TITANIUM AND FILLER. INSTALLED REPAIR PIECES IAW EA 62336. (M) 2 L 7 2 4F RT A2NM 1998100900532 19981009 00532 NM 1998 10 9 USAASB98226 1 19980802 A 3350 20131ALP BATTERY BOEING 737 7374B7 1384702 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 438US 24560 GSO - FOUND EMERGENCY EXIT LIGHT AT ROW 11 LEFT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK (M1479). (M) 2 L 7 2 4F RT A16WE 1998100900533 19981009 00533 WP 1998 10 9 USAAD98151 1 19980824 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 IND - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 5 AND 10 WERE INOPERATIVE. MAINTENANCE REPLACED THE CEILING EMERGENCY L IGHTS BATTERIES. (M) 2 L 7 2 4F A6WE 1998100900534 19981009 00534 WP 1998 10 9 USAAD98148 1 19980821 A 3350 60030451LB SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 SYR - THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGNS, AFTSECTION OF THE FLOOR EMERGENCY LIGHTS, AND THE RIGHT NACE LLE EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE AFT FLOOR EMERGENCY LIGHTS AND THE RIG HT NACELLE EMERGENCY LIGHT. THE POWER SUPPLY WAS REPLACED FOR THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGNS. (M ) 2 L 7 2 4F A6WE 1998100900535 19981009 00535 WP 1998 10 9 98ZZZM714 1 19980821 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 SYR - THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGNS, AFTSECTION OF THE FLOOR EMERGENCY LIGHTS, AND THE RIGHT NACE LLE EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE AFT FLOOR EMERGENCY LIGHTS AND THE RIG HT NACELLE EMERGENCY LIGHT. THE POWER SUPPLY WAS REPLACED FOR THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGNS. (M ) 2 L 7 2 4F A6WE 1998100900536 19981009 00536 WP 1998 10 9 98ZZZM715 1 19980821 A 3350 20131ALP BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 978VJ 47371 SYR - THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGNS, AFTSECTION OF THE FLOOR EMERGENCY LIGHTS, AND THE RIGHT NACE LLE EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE AFT FLOOR EMERGENCY LIGHTS AND THE RIG HT NACELLE EMERGENCY LIGHT. THE POWER SUPPLY WAS REPLACED FOR THE LEFT AND RIGHT AFT OVERWING EMERGENCY EXIT SIGNS. (M ) 2 L 7 2 4F A6WE 1998100900537 19981009 00537 WP 1998 10 9 USAAD98150 1 19980822 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 820US 49119 IND - THE FORWARD CABIN CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F A6WE 1998100900538 19981009 00538 NM 1998 10 9 USAABB98092 1 19980820 A 3350 86210066 BATTERIES BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 LAX - FOUND EIGHT FLOOR LEVEL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998100900539 19981009 00539 NM 1998 10 9 USAABB98093 1 19980901 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 623AU 27244 PHL - FOUND LOW LEVEL EMERGENCY LIGHT INOPERATIVE AT ROW 4. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998100900540 19981009 00540 NM 1998 10 9 USAABB98091 1 19980815 A 3350 20121 BATTERY CHARGER BOEING 767 767201 1385125 NM CABIN INOPERATIVE A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 646US 23898 PHL - FOUND EMERGENCY FLOOR LIGHTING NEAR MID LAV AREA INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A1NM 1998100900541 19981009 00541 WP 1998 10 9 USAAD98152 1 19980828 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP PAX CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924VJ 48144 IND - ONE SET OF CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CEILING EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998100900542 19981009 00542 WP 1998 10 9 USAA980360 1 19980817 A 5320 1199671 PAN DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 87365 47336 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 2 INCH BY 10 INCH AREA OF CORROSION AT E/E COMPARTMENT DOOR PAN AND LT INTER COSTAL. DEFECTIVE PART REPLACED WITH INDENTICAL PART NR 1199671 AND 1095915. (M) 2 L 7 2 4F A6WE 1998100900543 19981009 00543 WP 1998 10 9 98ZZZM716 1 19980817 A 5320 1095915 INTERCOSTAL DOUG DC9 DC931 3022065 WP FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 997VJ 87365 47336 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 2 INCH BY 10 INCH AREA OF CORROSION AT E/E COMPARTMENT DOOR PAN AND LT INTER COSTAL. DEFECTIVE PART REPLACED WITH INDENTICAL PART NR 1199671 AND 1095915. (M) 2 L 7 2 4F A6WE 1998100900544 19981009 00544 WP 1998 10 9 USAA980336 1 19980817 A 5311 9911958521 FRAME DOUG DC9 DC981 3022081 WP BS 1463 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 819US 48099 PIT - DURING C-6 CHECK, FOUND CORROSION IN TWO AREAS, 1 FT BY 1 INCH AT STATION 1463 CANTED FRAME LOWER MEMBER, LEFT OF CENTER. BLENDED OUT CORROSION AND INSTALLED TWO STRAPS .80 THICK PER EA 50321. (M) 2 L 7 2 4F A6WE 1998100900545 19981009 00545 WP 1998 10 9 USAAD98149 1 19980821 A 3231 2917521 SPRING DOUG DC9 DC931 3022065 WP NLG WW DISCONNECTED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 928VJ 48131 HPN-PIT - FLT 1432 - AFTER TAKEOFF AND LANDING GEAR RETRACTION THERE WAS A LOUD NOISE AND VIBRATION. THE FLT CREW CYCLE D THE GEAR THREE TIMES BUT THE VIBRATION REMAINED. THE AIRCRAFT DIVERTED TO LGA AND LANDED WITHOUT INCIDENT. MAINTENAN CE FOUND THE RIGHT NOSE GEAR DOOR FOLLOWUP SPRING DISCONNECTED FROM THE FOLLOWUP SYSTEM. THE SPRING WAS REINSTALLED AND THE NOSE GEAR WAS SWUNG. (M) 2 L 7 2 4F A6WE 1998100900546 19981009 00546 WP 1998 10 9 USAA980382 1 19980901 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 718 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 934VJ 48114 PIT - DURING C-6 CHECK, FOND TWO 1 INCH CRACKS AT STATION 718 AT LONGERON 5R. ACCOMPLISHED LONGERON SPLICE PER SRM 53-0 2. (M) 2 L 7 2 4F A6WE 1998100900547 19981009 00547 WP 1998 10 9 USAAD98142 1 19980908 A 4990 GTCP8598D APU DOUG DC9 DC931 3022065 WP APU BAY LEAKING A USAA O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 935VJ 50079 48115 CLT - FLT 1604 - DURING APPROACH, THE CREW NOTICED THE SMELL OF OIL APPARENTLY COMING FROM THE AIR CONDITION SYSTEM. TH E SMELL BECAME MORE INTENSE AFTER LANDING. MAINTENANCE FOUND THE APU DROPPING OIL FROM THE INTERNAL CORE. THE APU WAS MEL'D AND SCHEDULED FOR REPLACEMENT. (M) 2 L 7 2 4F A6WE 1998100900548 19981009 00548 WP 1998 10 9 USAAD98144 1 19980815 A 5240 SEAL DOUG DC9 DC982 3022082 WP SERVICE DOOR LOOSE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 825US 49237 PHL - FLT 200 - AFTER TAKEOFF, THE CREW HEARD A LOUD BANGING SOUND AND THE FORWARD SERVICE DOOR FAILED TO SEAL. THE AIR CRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED PIECE OF RUBBER TRIM THAT WAS HANGING OUTS IDE FORWARD SERVICE DOOR. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED. (M) 2 L 7 2 4F A6WE 1998100900549 19981009 00549 NM 1998 10 9 USAASB98222 1 19980828 A 2612 6131508551 FIRE LOOP BOEING 737 737301 1384611 NM NR 1 ENGINE CHAFED A USAA O OTHER N FALSE WARNING CR CRUISE 1 EA 19 354US 23557 PHL - FLT 1888 - EN ROUTE FROM MBJ TO PHL, THE NR 1 ENGINE FIRE WARNING DETECTION FAULT LIGHT ON THE ENGINE/APU FIRE PAN EL ILLUMINATED. THE NR 1 ENGINE FIRE HANDLE FLASHED ON AND OFF DURING FIRE/OVERHEAT TEST WITH FAULT LIGHT ON. UPON LAN DING IN PHL, LIGHT EXTINGUISHED. MAINTENANCE FOUND THE NR 1 ENGINE A/B LOOP WIRING IN CORE SECTION CHAFED AND SHORTED A GAINST PRSOV DISCONNECT BRACKET. REMOVED AND REPLACED NR 1 ENGINE CORE HARNESS. ALSO, REPLACED CORE HARNESS CONNECTOR D3088 (P/N BCREF115091) FOR CONDITION. FIRE WARNING OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1998100900550 19981009 00550 NM 1998 10 9 USAA980347 1 19980908 A 5330 SKIN BOEING 737 737201 1384454 NM BS 765 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 253AU 42288 22795 TPA - DURING WALK AROUND VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK ON EXTERNAL SKIN STATION 765 STRINGE R 19 RT. INSTALLED DOUBLER OF .080 2024 T-3 PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998100900551 19981009 00551 NM 1998 10 9 USAA980346 1 19980826 A 5315 6545815569 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 384US 37806 22957 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION ON FLOORBEAM AT BS 344 LBL 09 U PPER CHORD. REMOVED DAMAGED AREA AND INSTALLED REPAIR PARTS AND ANGLES PER REPAIR DOCUMENT 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998100900552 19981009 00552 EU 1998 10 9 SIMA982533 1 19980910 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 901AE 340B401 ABI - FOUND SEAT TRACK 18.3L AT FS 297 CORRODED. PERFORMED SPLICE REPAIR ON SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998100900553 19981009 00553 EU 1998 10 9 98ZZZM717 1 19980910 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT AFT OUTBOARD AND INBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900554 19981009 00554 EU 1998 10 9 98ZZZM718 1 19980910 A 5347 S53678001244 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 426AT 426 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT AFT OUTBOARD AND INBOARD, AND THE LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900555 19981009 00555 EU 1998 10 9 SIMA982532 1 19980906 A 5315 S53672406208 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900556 19981009 00556 EU 1998 10 9 98ZZZM719 1 19980906 A 5315 S53672407252 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900557 19981009 00557 EU 1998 10 9 98ZZZM720 1 19980906 A 5315 S53672408254 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCRAF T RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900558 19981009 00558 EU 1998 10 9 SIMA982531 1 19980910 A 5320 S53678008216 ZEE MEMBER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 410AT 410 SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. REMOVED AND REPLACED ZEE MEMBER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900559 19981009 00559 EU 1998 10 9 SIMA982511 1 19980908 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS 36, 38, AND 39 . AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900560 19981009 00560 EU 1998 10 9 98ZZZM721 1 19980908 A 5315 S536724075201 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS 36, 38, AND 39 . AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900561 19981009 00561 EU 1998 10 9 98ZZZM722 1 19980908 A 5315 S53672408254 FLOORBEAM AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 SAW - DURING CPCP-8 INSPECTION, FOUND FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS 36, 38, AND 39 . AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900562 19981009 00562 EU 1998 10 9 SIMA982502 1 19980907 A 5320 S5367131828001 PLATE AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 SAW - DURING CPCP-8 INSPECTION, FOUND THE SERVICE DOOR SILL PLATE CORRODED. REMOVED AND REPLACED SILL PLATE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900563 19981009 00563 EU 1998 10 9 SIMA982501 1 19980907 A 5347 S53375001220 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 DURING CPCP-8 INSPECTION, FOUND LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, AND THE LEFT AND RIGHT FLIGHT A TTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900564 19981009 00564 EU 1998 10 9 98ZZZM723 1 19980907 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 DURING CPCP-8 INSPECTION, FOUND LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, AND THE LEFT AND RIGHT FLIGHT A TTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900565 19981009 00565 EU 1998 10 9 98ZZZM724 1 19980907 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 DURING CPCP-8 INSPECTION, FOUND LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, AND THE LEFT AND RIGHT FLIGHT A TTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900566 19981009 00566 EU 1998 10 9 98ZZZM725 1 19980907 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 DURING CPCP-8 INSPECTION, FOUND LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, AND THE LEFT AND RIGHT FLIGHT A TTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900567 19981009 00567 EU 1998 10 9 98ZZZM726 1 19980907 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 408AT 408 DURING CPCP-8 INSPECTION, FOUND LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, AND THE LEFT AND RIGHT FLIGHT A TTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900568 19981009 00568 EU 1998 10 9 VTZA98274 1 19980828 A 2150 174600000001 ACM JETAIR JETSTM JETSTM4101 1500501 EU RT PACK MALFUNCTIONED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 322UE 41058 FLT 6589 - IAD-BOS - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT PACK STUCK IN FULL HOT. AIRCRAFT LAN DED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ACM, OPS CHECK OK. AIRCR AFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998100900569 19981009 00569 1998 10 9 VTZA98273 4 19980827 A 3425 7003360948 AHARS JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING P NO WARNING INDICATION CR CRUISE 1 EA 27 318UE 41041 FLT 6625 - IAD-ILM - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT AHARS FAILED. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT AHARS, OPS CHECK OK. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998100900570 19981009 00570 EU 1998 10 9 VTZA98272 1 19980827 A 7722 6100144A INDICATOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 EA 27 491UE 911 FLT 6251 - IAD-ABE - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO RT EGT FAILED. AIRCRAFT WENT TO GATE WITH NO FU RTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED EGT GAUGE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETU RNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998100900571 19981009 00571 EU 1998 10 9 VTZA98269 1 19980825 A 3350 S34C12ST6S010 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 324UE 41017 FLT 6543 - EWR-IAD - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE EMERGENCY TRACK LIGHTING NOT ILLUMINATING. MAINTEN ANCE CONTROL WAS NOTIFIED. AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIG HTING TRACK STRIP AND RESECURED SEVERAL LOOSE CONNECTORS IAW APPLICABLE MAINTENANCE PROCEDURES. ALL CHECKS WERE ACCOMPL ISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998100900572 19981009 00572 EU 1998 10 9 VTZA98268 1 19980825 A 3350 PT2112 LIGHT JETAIR JETSTM JETSTM4101 1500501 EU CABIN INOPERATIVE A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 302UE 41013 FLT 6347 - RIC-IAD - DURING TAXI, EXPERIENCED A DISCREPANCY WITH THE EMERGENCY TRACK LIGHTING NOT ILLUMINATING. MAINTEN ANCE CONTROL WAS NOTIFIED. AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING TR ACK STRIP CONNECTOR IAW APPLICABLE MAINTENANCE PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAF T WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998100900573 19981009 00573 NE 1998 10 9 VTZA98266 2 19980822 A 7320 31059005 FCU JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 27 321UE 41045 FLT 6632 - ILM-IAD - DURING CRUISE, AIRCRAFT DIVERTED AND MADE AN UNSCHEDULED LANDING AT RIC, DUE TO RT ENGINE LOSS OF P OWER SLOWLY. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT ENGINE FCU AND FUEL PUMP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1998100900574 19981009 00574 NE 1998 10 9 98ZZZM727 2 19980822 A 7314 31057807 FUEL PUMP JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE RT ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 EA 27 321UE 41045 FLT 6632 - ILM-IAD - DURING CRUISE, AIRCRAFT DIVERTED AND MADE AN UNSCHEDULED LANDING AT RIC, DUE TO RT ENGINE LOSS OF P OWER SLOWLY. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT ENGINE FCU AND FUEL PUMP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1998100900575 19981009 00575 EU 1998 10 9 VTZA98265 1 19980821 A 3260 BULBS JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING P NO WARNING INDICATION AP APPROACH 1 EA 27 313UE 41026 FLT 6558 - IAD-CHO - DURING APPROACH, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NO RT MAIN LANDING GEARA INDICATION. A IRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LIGHT BULBS, OPS CHEC K OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998100900576 19981009 00576 NE 1998 10 9 UF6A980710 2 19980715 A 7532 7857194 VALVE BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE FAILED A UF6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 854AW 10029 900747 2028 124224 SBN - FLT 5764 - AFTER TAKEOFF, WHEN BLEEDS ARE SELECTED ON NR 1 ENGINE, TORQUE DROPPED TO 70 PERCEN, NL 92 PERCENT, NH 90 PERCENT. MAINTENANCE REMOVED AND REPLACED NR 1 HP BLEED VALVE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998100900578 19981009 00578 EU 1998 10 9 UF6A980712 1 19980716 A 7797 3035343 WIRE BAG ATP ATP EU NR 1 ENG EGT LOOSE A UF6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 856AW 2032 ORD - FLT 5712 - AFTER TAKEOFF DURING CLIMB, NR 1 ITT WENT TO 775 DEGREES CELSIUS. MAINTENANCE REPOSITIONED THERMOCOUPL E HARNESS FROM GROUND. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900579 19981009 00579 EU 1998 10 9 UF6A980708 1 19980713 A 7722 3035969 THERMOCOUPLE BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 855AW 2029 ORD - FLT 5729 - NR 2 ENGINE ITT REACHES 779 AT TAKEOFF. MAINTENANCE REMOVED AND REPLACED THERMOCOUPLE. SYSTEM OPS CHE CKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900580 19981009 00580 EU 1998 10 9 UF6A980705 1 19980710 A 3350 188 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 ORD - ON DAILY, FUOND ROW 12CD EMERGENCY LIGHT OUT. MAINTENANCE REPAIRED FAULTY WIRE TERMINAL END. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900581 19981009 00581 EU 1998 10 9 UF6A980706 1 19980711 A 3350 OL3071BPE BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FLT 5722 - OVERHEAD EMERGENCY LIGH TINOP IN AFT GALLEY. MAINTENANCE REMOVED AND REPLACED OVERHEAD EMERGENCY LIGHT BULB. (M) 2 L 7 2 4T RT A27NM 1998100900582 19981009 00582 EU 1998 10 9 UF6A980707 1 19980713 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 11040 16826 2034 SBN - EMERGENCY LIGHTS DO NOT ILLUMINATE AT ROWS 4, 5, 6, AND 7. MAINTENANCE REMOVED AND REPLACED NR 4 POWER SUPPLY. S YSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900583 19981009 00583 1998 10 9 UF6A980715 4 19980719 A 3442 071131900 TRANSCEIVER BAG ATP ATP EU RADOME FAILED A UF6A A UNSCHED LANDING L NO TEST CR CRUISE 1 GL 31 851AW 6830 3567 2020 ORD - FLT 5758 - RADAR PAINTS MULTI-COLOR CONCENTRIC CIRCLES IN ALL RANGES. RADAR DOES NOT TEST SATISFACTORY. MAINTENA NCE REMOVED AND REPLACED RADAR SENSOR. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900584 19981009 00584 EU 1998 10 9 UF6A980716 1 19980721 A 2751 750SUE68 SYMBOL GENERATOR BAG ATP ATP EU NR 2 POSITION FAILED A UF6A A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 854AW 6004 1021 2028 ORD - FLT 5712 - NR 2 PFD WENT BLANK. MAINTENANCE REPLACED THE NR 2 SYMBLOL GENERATOR. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900585 19981009 00585 EU 1998 10 9 UF6A980714 1 19980717 A 6120 7863368 PCU BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 5772 2036 ORD - FLT 5765 - NR 2 ENGINE WOULD NOT COME OUT OF FEATHER WHEN CONDITION LEVER WAS ADVANCED TO MINIMUM RPM. MAINTENANC E REMOVED AND REPLACED NR 2 PCU. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900586 19981009 00586 NE 1998 10 9 UF6A980713 2 19980717 A 7321 7919002002 EEC BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE MALFUNCTIONED A UF6A O OTHER O OTHER AP APPROACH 1 GL 31 854AW 9248 2028 124224 ORD - FLT 5749 - NR 1 TORQUE FLUCTUATES 25 PERCENT AT SETTINGS OF 15 PERCENT TO 40 PERCENT ON APPROACH. MAINTENANCE REM OVED AND REPLACED NR 1 EEC. PERFORMED OPS CHECK AND TEST FLIGHT. ALL SYSTEMS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998100900588 19981009 00588 EU 1998 10 9 UF6A980719 1 19980729 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 11038 16997 2034 ORD - UPON DAILY INSPECTION, DISCOVERED NR 4 EMERGENCY LIGHTING POWER SUPPLY INOP. MAINTENANCE REMOVED AND REPLACED NR 4 POWER SUPPLY UNIT. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900589 19981009 00589 EU 1998 10 9 UF6A980802 1 19980803 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - AFT EXTERNAL RIGHT EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900590 19981009 00590 EU 1998 10 9 UF6A980807 1 19980812 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 7166 16819 2032 ORD - EMERGENCY LIGHTS INOP AT 9-10 CD. MAINTENANCE REMOVED AND REPLACED NR 5 EMERGENCY BATTERY PACK. SYSTEM OPS CHECK ED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900591 19981009 00591 EU 1998 10 9 UF6A980805 1 19980811 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 SBN - EXTERNAL EMERGENCY LIGHT AFT RIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998100900592 19981009 00592 NE 1998 10 9 UF6A980806 2 19980811 A 7321 ECC BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE MALFUNCTIONED A UF6A O OTHER O OTHER TX TAXI/GRND HDL 1 GL 31 854AW 2028 ORD - FLT 5758 - AFTER LANDING, NR 1 ENGINE FEATHERED ON ITS OWN. MAINTENANCE INSPECTED ENTIRE SYSTEM AND RAN ENGINES. COULD NOT DUPLICATE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998100900593 19981009 00593 EU 1998 10 9 UF6A980812 1 19980825 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP ON LEFT SIDE. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHEC KED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900594 19981009 00594 EU 1998 10 9 UF6A980809 1 19980823 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 856AW 2032 SBN - OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP ON RIGHT SIDE. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998100900595 19981009 00595 EU 1998 10 9 UF6A980811 1 19980825 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 2028 SBN - EXTERNAL EMERGENCY LIGHT AT AFT PASSENGER DOOR IS INOP. MAINTENANCE REMOVED AND REPLACED BULB. SYSTEM OPS CHECKE D GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900596 19981009 00596 NE 1998 10 9 UF6A980803 2 19980805 A 7321 7919002002 EEC BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE FAILED A UF6A K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 854AW 9086 90010459 2028 124224 ORD - FLT 5712 - NR 1 ENGINE FEATHERED AFTER LANDING WITHOUT MOVEMENT OF CONDITION LEVER. MAINTENANCE REMOVED AND REPLA CED NR 1 EEC. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998100900597 19981009 00597 1998 10 9 UF6A980801 4 19980801 A 3425 DISPLAY BAG ATP ATP EU COCKPIT MALFUNCTIONED A UF6A A UNSCHED LANDING G MULTIPLE FAILURE TO TAKEOFF 1 GL 31 854AW 2028 ORD - FLT 5717 - BOTH NAVIGATION DISPLAYS FAILED IN FLIGHT. MAINTENANCE COMPLIED WITH RECONFIGURATION FUNCTIONAL CHECK. SYSTEMS OPS CHECKED GOOD. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1998100900598 19981009 00598 EU 1998 10 9 UF6A980701 1 19980702 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 6270 17368 2034 ORD - UPON DAILY INSPECTION, FOUND THAT A FEW EMERGENCY LIGHTS WERE INOP. MAINTENANCE REMOVED AND REPLACED NR 4 POWER S UPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998100900599 19981009 00599 NM 1998 10 9 USAA980359 1 19980816 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 341US 35161 23510 CLT - DURING CX-1 CHECK EDDY CURRENT INSPECTION, FOUND A 1.2 INCH CRACK BELLY SKIN RADIO RACK EXHAUST CUTOUT STATION 380 BETWEEN STRINGER 28L AND STRINGER 27R. INSTALLED DOUBLER .0012024T-3 PER SB AND EA 62242. (M) 2 L 7 2 4F RT A16WE 1998100900600 19981009 00600 SO 1998 10 9 98ZZZM728 1 19980121 A 2752 1159SCC2117 ACTUATOR GULSTM G1159 G1159B 3953535 SO LT WING BINDING A BUEA O OTHER O OTHER AP APPROACH 1 GL 23 36PN 42 FLAPS WOULD NOT DEPLOY IN FLIGHT, NORMAL OR EMERGENCY, UPON APPROACH TO TEB. RETURNED TO PTK AND LANDED. REPLACED LEFT WING INBOARD FLAP ACTUATOR P/N 1159SCC211-7, S/N 36-1174, WITH OVERHAULED UNIT P/N 1159SCC211-15, S/N 76-117. CHECKED FLAP SYSTEM RIGGING AND OPERATION. (M) 2 L 7 2 4F RT A12EA 1998100900601 19981009 00601 NM 1998 10 9 TSAA9833506 1 19980914 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 1998100900602 19981009 00602 NM 1998 10 9 TSAA9833507 1 19980916 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 1 EMERGENCY FLOOR LIGHTING BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900603 19981009 00603 EU 1998 10 9 SABA980043 1 19980907 A 5270 SENSOR BAG JETSTM JETSTM3201 1500217 EU PAX DOOR MALFUNCTIONED A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 957AE 957 FLT 5208 - MYR-RDU - THE MAIN CABIN DOOR CAPTION LIGHT ILLUMINATED. AIR CREW DIVERTED INTO ILM. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED AT ILM WITH NO OTHER PROBLEMS. DOOR WAS INSPECTED AND FOUND TO BE LOCKING. CAPTION LIGH T WAS DEFERRED TO MSL 090798-05C. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998100900604 19981009 00604 1998 10 9 HALA9800329 4 19980920 A 3416 INDICATOR DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A HALA K NONE O OTHER CR CRUISE 1 WP 13 122AA 46522 FLT 9 - HNL - TCAS INOP IN FLIGHT AT THE SAME TIME GPWS CMPT FAIL AND WINDSHEAR INOP LIGHTS ILLUMINATED. BOTH RADAR SCR EENS WENT BLANK WITH THESE WORDS APPEARING, RADIO ALT NR 1 AND NR 2 ON DESCENT WHEN NR 1 RADIO ALT WAS TURNED ON AND TES TED TCAS APPEARED TO WORK NORMALLY. REPLACED NR 2 RADIO ALTIMETER T/R. RERACKED NR 1 RADIO ALTIMETER T/R. GROUND CHEC K NORMAL. (M) 2 L 7 3 4F A22WE 1998100900605 19981009 00605 NM 1998 10 9 USAA980317 1 19980722 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 967-998 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 273AU 42036 22885 TPA - DURING A CX-6 CHECK VISUAL INSPECTION, FOUND 12 INCHES OF HEAVY CORROSION STRINGER 25L STATION 967 AND STATION 986 TO STATION 998. REPLACED SECTION OF STRINGER WITH JT NEW PART AND SPLICED PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1998100900606 19981009 00606 NM 1998 10 9 TSAA9833492 1 19980910 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LED'S BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1998100900607 19981009 00607 NM 1998 10 9 TSAA9833493 1 19980910 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LED'S BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1998100900608 19981009 00608 NM 1998 10 9 TSAA9833494 1 19980910 A 3350 86210066 BATTERY PACK BOEING 737 7372S2C 138448G NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 806AL 21927 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY DUE TO LED'S BEING INOP. OPS CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F A16WE 1998100900609 19981009 00609 NM 1998 10 9 TSAA9833495 1 19980910 A 3350 873100151 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT ASSY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900610 19981009 00610 NM 1998 10 9 TSAA9833496 1 19980910 A 3350 873100151 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT ASSY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900611 19981009 00611 NM 1998 10 9 TSAA9833497 1 19980913 A 3350 6013211 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY PACK FROM THE AFT DOOR EMERGENCY LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F A16WE 1998100900612 19981009 00612 NM 1998 10 9 TSAA9833498 1 19980913 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED THE BATTERY PACK IN THE NR 4 POSITION EMERGENCY PROXIMITY FLOOR LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900613 19981009 00613 NM 1998 10 9 TSAA9833499 1 19980913 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE (M) 2 L 7 2 4F RT A16WE 1998100900614 19981009 00614 NM 1998 10 9 TSAA9833500 1 19980913 A 3350 8731002151 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900615 19981009 00615 NM 1998 10 9 TSAA9833501 1 19980913 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900616 19981009 00616 NM 1998 10 9 TSAA9833502 1 19980913 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 1 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900617 19981009 00617 NM 1998 10 9 TSAA9833503 1 19980913 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 2 POSITION EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900618 19981009 00618 SO 1998 10 9 C2XA98IA358 1 19980908 A 2170 44E202A SEPARATOR EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA E ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SW 09 22727 120177 FLT 3684 - THE CREW REPORTED A LEFT ENGINE DUCT LEAK. THE CREW SHUT DOWN THE NR 1 ENGINE AND LANDED AT EFD WITHOUT INCI DENT. MAINTENANCE REMOVED AND REPLACED THE WATER SEPARATOR ON THE LEFT ENGINE BLEED LINE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900619 19981009 00619 SO 1998 10 9 C2XA98IA362 1 19980912 A 3230 12041127001 HARNESS EMB 120 EMB120RT SO NLG FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 15725 120173 IAH - FLT 3893 - THE CREW REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDE NT WHERE MAINTENANCE REMOVED AND REPLACED THE 'A' SYSTEM DOWNLOCK PROXIMITY SWITCH WIRING HARNESS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900620 19981009 00620 EU 1998 10 9 C2XA98IA395 1 19980921 A 3350 3013000 POWER SUPPLY AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING MAINTENANCE VISIT NR 23, THE LEFT EXIT SIGN AND I-3 EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTEN ANCE REMOVED AND REPLACED THE FORWARD POWER SUPPLY IAW ATR42-500 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900621 19981009 00621 SO 1998 10 9 C2XA98IA394 1 19980923 A 5320 12006429001 TEE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900622 19981009 00622 SO 1998 10 9 C2XA98IA393 1 19980923 A 5320 12022670002 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILL ED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1998100900623 19981009 00623 SO 1998 10 9 C2XA98IA392 1 19980923 A 5320 12025957001 ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE SUPPORT ATTACH ANGLE AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900624 19981009 00624 SO 1998 10 9 C2XA98IA391 1 19980923 A 5320 12022670001 SUPPORT EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE SUPPORT AT FRAME 13 WAS FOUND TO BE CRACKED. MAINTENANCE STOP DRILLE D THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900625 19981009 00625 SO 1998 10 9 C2XA98IA390 1 19980923 A 5320 12025957001 ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FRAME 13 LEFT VERTICLE SUPPORT ATTACH ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED ANGLES IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900626 19981009 00626 SO 1998 10 9 C2XA98IA389 1 19980923 A 5320 12004149002 TEE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT T-PROFILE WAS FOUND TO BE CORRODED AT FRAME 36. MAINTENANCE REMOVED AND REPLA CED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900627 19981009 00627 SO 1998 10 9 C2XA98IA388 1 19980923 A 5320 12005779001 TEE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 40 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900628 19981009 00628 SO 1998 10 9 C2XA98IA387 1 19980923 A 5320 1200615700Z BEAM EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED FROM FRAME 44 TO FRAME 47. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED SECTION OF CREASE BEAM IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900629 19981009 00629 SO 1998 10 9 C2XA98IA386 1 19980923 A 5320 12005206001 STRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT BUTT STRAP WAS FOUND TO BE CORRODED AT FRAME 43. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1998100900630 19981009 00630 SO 1998 10 9 C2XA98IA385 1 19980923 A 5320 12006429001 TEE EMB 120 EMB120RT SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT T-PROFILE AT FRAME 44 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE T-PROFILE IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900631 19981009 00631 SO 1998 10 9 C2XA98IA384 1 19980923 A 5320 12006159501 BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM WAS FOUND TO BE CORRODED FROM FRAME 38 TO FRAME 44. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900632 19981009 00632 SO 1998 10 9 C2XA98IA383 1 19980923 A 5320 12006158002 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE RIGHT BUTT STRAP WAS FOUND TO BE CORRODED FROM FRAME 33 TO FRAME 44. MAINTENANCE R EMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP IAW EMB120 SRM 41-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900633 19981009 00633 SO 1998 10 9 C2XA98IA382 1 19980923 A 5320 12031657001 BRACKET EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, THE LEFT WING TO FUSELAGE FAIRING 193 LOWER SUPPORT BRACKET WAS FOUND TO BE CRACEKED AT THE FORWARD END. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR IAW EMB-120 SRM 51-40-02, AND THE A IRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900634 19981009 00634 SO 1998 10 9 C2XA98IA381 1 19980923 A 5320 12006158001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLOORBEAM BUTT-STRAP CORRODED BETWEEN FRAME 42 AND 44. MAINTENANCE REM OVED THE DAMAGED SECTION AND REPLACED WITH NEW SECTION IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900635 19981009 00635 SO 1998 10 9 C2XA98IA380 1 19980923 A 5320 12004166001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT FLOORBEAM BUTT-STRAP CORRODED AFT OF FRAME 38. MAINTENANCE REMOVED THE DAM AGED SECTION AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1998100900636 19981009 00636 SO 1998 10 9 C2XA98IA379 1 19980923 A 5530 14531597601 ANGLE EMB 120 EMB120RT SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND VERTICAL STABILIZER LEFT SIDE DRAG ANGLE CRACKED. MAINTENANCE REMOVED THE DAMAGE D FORWARD SECTION AND REPLACED IT IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5530-01013. T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900637 19981009 00637 SO 1998 10 9 C2XA98IA377 1 19980923 A 5753 12040327001 RIB EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP CENTER RIB CRACKED. MAINTENANCE REMOVED AND REPLACED THE FLAP IAW EMB-120 MM 27-50-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900638 19981009 00638 SO 1998 10 9 C2XA98IA378 1 19980923 A 5410 12007891002 FRAME EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT AFT MAIN LANDING GEAR DOOR INBOARD FORWARD HINGE POINT, AFT NACELLE HALF FR AME CRACKED. MAINTENANCE REMOVED AND REPLACED THE HALF FRAME IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR R ETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900639 19981009 00639 SO 1998 10 9 C2XA98IA376 1 19980923 A 5720 12018064002 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE FLAP CENTER SKIN SUPPORT CRACKED ON UPPER SIDE. MAINTENANCE REMOVE D AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900640 19981009 00640 SO 1998 10 9 C2XA98IA374 1 19980923 A 5720 12017054014 ANGLE EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING RIB 8 TO STRINGER 11 SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND R EPLACED THE ANGLE IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900641 19981009 00641 SO 1998 10 9 C2XA98IA375 1 19980923 A 5720 12017054015 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING LOWER SKIN SUPPORT FORWARD OF ACCESS 522EB CUTOUT ON RIB 8 CRACKED. MA INTENANCE REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A31SO 1998100900642 19981009 00642 SO 1998 10 9 C2XA98IA373 1 19980923 A 5720 12017054007 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN SUPPORT AT RIB 8, SECOND FROM FORWARD, CRACKED. MAINTENANC E REMOVED AND REPLACED THE SKIN SUPPORT IAW EMB-120 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900643 19981009 00643 EU 1998 10 9 C2XA98IA363 1 19980923 A 5320 S53070210208 SPLICE AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUND STRINGER 17 RIGHT SPLICE AT FRAME 29 CORRODED. MAINTENANCE REMOVED AND REPLACED THE STRINGER SPLICE IAW ATR-42 SRM 51-25-02, -04. THE AIRCRAFT WAS APPROVED FOR RETURN SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900644 19981009 00644 EU 1998 10 9 C2XA98IA364 1 19980923 A 5313 S5307020300063 STRINGER AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUND STRINGER 18 RIGHT CORRODED BETWEEN FRAMES 27 AND 29. MAINTENANCE REMOVED THE DAM AGED SECTION OF THE STRINGER AND INSTALLED NEW ONE IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 H 7 2 4T RT A53EU 1998100900645 19981009 00645 EU 1998 10 9 C2XA98IA365 1 19980923 A 5313 S53671289210 STRINGER AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUND STRINGER 16 RIGHT CORRODED BETWEEN FRAMES 29 AND 31. MAINTENANCE REMOVED AND REP LACED THE DAMAGED SECTION OF STRINGER IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900646 19981009 00646 EU 1998 10 9 C2XA98IA366 1 19980923 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 36 FLOORBEAM CORRODED AROUND SEVERAL FASTENER HOLES. MAINTENANCE INSTALLED REPAIR DOUBLERS IN 5 LOCATIONS IAW CONTINENTAL EXPERSS ENGINEEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5310-01037. T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900647 19981009 00647 EU 1998 10 9 C2XA98IA367 1 19980923 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUND FRAME 38 FLOORBEAM CORRODED AROUND SEVERAL FASTENER HOLES. MAINTENANCE REMOVED T HE CORROSION AND INSTALLED ONE REPAIR DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC5 310-01037. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900648 19981009 00648 EU 1998 10 9 C2XA98IA368 1 19980923 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUND LEFT FLIGHT ATTENDANTS SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW ATR42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900649 19981009 00649 EU 1998 10 9 C2XA98IA369 1 19980923 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUDN RIGHT FLIGHT ATTENDANTS SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLACED TH E SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900650 19981009 00650 EU 1998 10 9 C2XA98IA370 1 19980923 A 5320 S5397130900060 SUPPORT AEROSP ATR42 ATR42500 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE BELLY FAIRING PANEL 193CL CENTER SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900651 19981009 00651 EU 1998 10 9 C2XA98IA371 1 19980923 A 5320 S5397130900160 SUPPORT AEROSP ATR42 ATR42500 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 33449 507 IAH - DURING C-CHECK INSPECTION, FOUDN RIGHT SIDE BELT FAIRING PANEL 194CR CENTER SUPPORT CRACKED. MAINTENANCE REMOVED AND REPLACED THE SUPPORT IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900652 19981009 00652 EU 1998 10 9 C2XA98IA372 1 19980922 A 2910 4019501 PUMP AEROSP ATR42 ATR42320 8680930 EU GREEN HYD SYSTEM FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 14815 104 IAH - FLT 3828 - THE CREW REPORTED THAT THE NOSE LANDING GEAR WAS SLOW TO RETRACT. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE GREEN SYSTEM A/C WILD HYDRAULIC PUMP, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900653 19981009 00653 EU 1998 10 9 C2XA98BT073 1 19980923 A 3230 F96GA0102 GEAR HANDLE AEROSP ATR42 ATR42320 8680930 EU COCKPIT MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 86842 286 FLT 3388 - ON APPROACH, REPORTED LANDING GEAR WOULD NOT EXTEND, USED EMERGENCY SYSTEM. MAINTENANCE DETERMINED FAULTY LA NDING GEAR SELECTOR HANDLE. REMOVED AND REPLACED UNIT. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998100900654 19981009 00654 SO 1998 10 9 C2XA98CL067 1 19980910 A 5753 12021937003 FLAP TRACK EMB 120 EMB120RT SO LT WING WORN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16731 120190 GSO - FLT 3352 - CREW REPORTED THAT AFTER TAKEOFF THEY RECEIVED A FLAP ASYMMETRY WARNING ON THE OUTBOARD AND NACELLES. A IRCRAFT RETURNED TO FIELD. THE AIRCRAFT WAS MAINTENANCE FERRIED TO CLE, AFTER INSPECTION THE LEFT OUTBOARD LOWER CHANNE L INBOARD ROLLER WAS FOUND TO BE FALLING OFF THE TRACK. THE LEFT LOWER CHANNEL ASSEMBLY WAS REMOVED AND REPLACED IAW EM B-120MM 57-52-02. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900655 19981009 00655 SO 1998 10 9 C2XA98CL068 1 19980922 A 2750 3082001007 ACTUATOR EMB 120 EMB120RT SO LT WING FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 16719 18653 0212 120138 CLE - FLT 3003 - CREW REPORTED THAT DURING CLIMB-OUT THEY RECEIVED A FLAP CONTROL FAULT. AIRCRAFT RETURNED TO FIELD WIT HOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT WING NACELLE FLAP ACTUATOR IAW EMB-120 MM 27-50-08, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998100900656 19981009 00656 SO 1998 10 9 C2XA98BT070 1 19980906 A 5311 14521805401 FRAME EMB 145 EMB145 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14938 145029 FOUND DAMAGE CAUSED BY RAMP HANDLER BAG CART AFT OF CARGO DOOR BETWEEN FRAMES 27 AND 28. REPLACED FRAME AND REPAIRED WI TH DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998100900657 19981009 00657 SO 1998 10 9 98ZZZM729 1 19980906 A 5311 14523057651 FRAME EMB 145 EMB145 SO FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14938 145029 FOUND DAMAGE CAUSED BY RAMP HANDLER BAG CART AFT OF CARGO DOOR BETWEEN FRAMES 27 AND 28. REPLACED FRAME AND REPAIRED WI TH DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998100900658 19981009 00658 SO 1998 10 9 C2XA98BT068 1 19980918 A 8000 1452274601 CUP ASSY EMB 145 EMB145 SO FUSELAGE CRACKED A C2XA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 09 15926 145005 FLT 4225 - CREW REPORTED AIR START CONNECTOR DAMAGED BY RAMP PERSON. MAINTENANCE REMOVED AND REPLACED AIRSTART CONNECTO R BOX. OPS AND PRESS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1998100900659 19981009 00659 EU 1998 10 9 C2XA98BT072 1 19980921 A 3350 E006478A50 SWITCH AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 69901 379 FLT 3519 - CREW REPORTED EMERGENCY EXIT LIGHTS WILL NOT EXTINGUISH USING TWO MINUTE LIGHT SWITCH. MAINTENANCE REPORTED, REMOVED AND REPLACED TWO MINUTE SWITCH, OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998100900660 19981009 00660 WP 1998 10 9 AALA981472 1 19980804 A 4990 O-RING DOUG DC9 DC982 3022082 WP APU FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 251AA 49270 LAX - FLT 1576 - AFTER TAKEOFF COCKPIT AND CABIN BEGAN FILLING WITH SMOKE. DECLARED EMERGENCY AND RETURNED TO LAX AND L ANDED OVERWEIGHT WITHOUT INCIDENT. APU CHIP DETECTOR LEAKING OIL TO APU INLET. SHUT DOWN APU AND ACCOMPLISHED PACK BURN OUT. REPLACED THE O-RING ON THE LEFT SIDE MAG CHIP DETECTOR OF THE APU. ACCOMPLISHED LEAK CHECK. ACCOMPLISHED OVERWE IGHT LANDING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900661 19981009 00661 WP 1998 10 9 AALA981656 1 19980906 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 297AA 49309 DFW - FLT 1715 - DURING PREFLIGHT CHECK EMERGENCY EXIT FLOOR PATH LIGHTING IN FORWARD COACH CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT FORWARD SECTION OF COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F A6WE 1998100900662 19981009 00662 WP 1998 10 9 AALA981655 1 19980905 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 249AA 49269 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT CEILING LIGHT AFT OF CABIN INOPERATIVE. CLEANED CONTACTS ON EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900663 19981009 00663 WP 1998 10 9 AALA981481 1 19980808 A 3220 5910448557 STRUT DOUG DC9 DC982 3022082 WP NLG UNDER INFLATED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 70404 49315 ORD - FLT 358 - AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT FURTHER INCIDEN T. MAINTENANCE FOUND NOSE GEAR STRUT UNDER INFLATED. SERVICED NOSE GEAR STRUT PER PROCEDURES. SYSTEM GROUND CHECKED N ORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900664 19981009 00664 WP 1998 10 9 AALA981566 1 19980816 A 3260 5920629513 PISTON DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 255AA CPI003 49287 DFW - FLT 1317 - AFTER TAKEOFF DFW NOSE GEAR WOULD NOT RETRACT. HAD NUMEROUS SPOILER AND FLAP WARNINGS IN FLIGHT. OUTF LOW VALVE CYCLED OPEN AND CLOSED SEVRAL TIMES. RECYCLED GEAR AND CIRCUIT BREAKER PER OPERATIONS MANUAL. RETURNED DFW A ND LANDED WITHOUT INCIDENT. REPLACED LOWER PISTON PER MM. RETURNED NOSE GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED NOR MAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900665 19981009 00665 WP 1998 10 9 AALA981603 1 19980901 A 3260 833703 SENSOR DOUG DC9 DC982 3022082 WP NLG MALFUNCTIONED A AALA K NONE J WARNING INDICATION AP APPROACH 1 SW 07 454AA 49559 DFW - FLT 2229 - DURING APPROACH DFW LANDING GEAR WARNING HORN CAME ON. INITIALLY HAD 3 GREEN LIGHTS THEN NOSE GEAR RED LIGHT ILLUMINATED. NOSE LANDING GEAR INDICATED UP POSITION. RECYCLED GEAR WITH SAME RESULTS, RAN QRH PROCEDURE WITH G EAR UP WITH NOSE GEAR INDICATING LIGHT STILL RED. GEAR LOWERED AND NOSE GEAR LIGHT REMAINED RED WITH NOSE LANDING GEAR INDICATING UP. LANDED DFW WITHOUT INCIDENT. REPLACED NOSE GEAR LOCK SENSOR AND ACCOMPLISHED REQUIRED CHECKS. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900666 19981009 00666 1998 10 9 RAIA980906 4 19980914 A 3442 7007700301 TRANSCEIVER JETAIR JETSTM JETSTM4101 1500501 EU NOSE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 562HK 4677 41078 FLT 7502 - STL - WEATHER RADAR CYCLES ON AND OFF IN FLIGHT. MAINTENANCE REPLACED WEATHER RADAR RECEIVER/TRANSMITTER. ( M) 2 L 7 2 4T RT A41NM 1998100900667 19981009 00667 WP 1998 10 9 AALA981461 1 19980801 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7506 49800 ORD - FLT 832 - AFTER TAKEOFF ORD, A STRONG HEAVY SMELL OF BURNING RUBBER AND ELECTRICAL WIRING WAS NOTED. DECLARED EME RGENCY, TURNED OFF RECIRCULATING FANS AND SMELL DISSIPATED AND SEEMED TO CLEAR. RETURNED TO ORD AND LANDED WITHOUT INCI DENT. FOUND PARTIAL INGESTION OF A BIRD INTO NR 2 ENGINE. PERFORMED BIRD STRIKE INSPECTION PER MM, NO DAMAGE FOUND AND NO EVIDENCE OF IT ENTERING THE CORE SECTION. PRECAUTIONARY REPLACED COALESCER BAGS AND RAN ENGINES. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900668 19981009 00668 EU 1998 10 9 RAIA980815 1 19980824 A 6120 1680640 MONOPOLE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 433AM 14859 885 FLT 7054 - STL - LEFT SRL CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED LEFT ENGINE PROPELLER GOVERNOR MONO POLE. (M) 2 L 7 2 4T RT A56EU 1998100900669 19981009 00669 EU 1998 10 9 SIMA982491 1 19980906 A 2611 FR3222 DETECTOR AEROSP ATR42 ATR42300 8680920 EU CARGO BAY FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 249AT 792 0249 JFK - FLT 4944 - FAINT SMELL OF BURNING WOOD/PINE TAR THAT SUBSIDED AND RETURNED PROMINENTLY DURING TAKEOFF/CLIMB-OUT, N O VISIBLE SMOKE. RETURNED TO FIELD. INSPECTED FORWARD CARGO COMPARTMENT WITH ENGINES RUNNING AND DETERMINED SMELL TO B E COMING FROM SMOKE DETECTOR. REMOVED AND REPLACED FORWARD CARGO SMOKE DETECTOR. OPERATIONAL CHECK SATISFACTORY AND NO FURTHER SMELL DETECTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900670 19981009 00670 EU 1998 10 9 SIMA982561 1 19980913 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 389AE 340B389 SPS - FLT 3748 - AVIONICS SMOKE LIGHT ILLUMINATED WITH CHIME THEN WENT OUT. ABORTED TAKEOFF AT 90-100 KT. NO SMOKE OR SMELL WAS NOTED. RERACKED WEU AND REU. AVIONICS SMOKE DETECTION SYSTEM FUNCTIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998100900671 19981009 00671 NM 1998 10 9 USAASB98231 1 19980904 A 2420 915F2124 GCU BOEING 737 7374B7 1384702 NM COCKPIT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 431US 24553 RIC - FLT 811 - AFTER LEVEL OFF AT APPROXIMATELY FL 280, THE FLIGHT ATTENDANTS REPORTED AN UNUSUAL ODOR IN THE CABIN. S HORTLY THEREAFTER, ODOR WAS NOTICED IN THE COCKPIT. CREW DECLARED AN EMERGENCY AND DIVERTED TO RIC. FLIGHT LANDED WITH OUT INCIDENT AND TAXIED TO THE GATE. AT THE GATE, THE NR 1 GCU CIRCUIT BREAKER WAS FOUND POPPED AND THE UNIT WAS VERY H OT AND SMELLED LIKE THE ODOR IN THE CABIN. MAINTENANCE REMOVED AND REPLCED THE NR 1 GCU AND FOUND A BURNED PIN ON CONNE CTOR D410. ALSO, FOND T2 PHASE WIRE BURNED THROUGH AT SPLICE IN UPPER FORWARD PYLON BETWEEN CONNECTORS D410 AND D512P. REPAIRED AND REPLACED BURNED WIRES AND PINS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998100900672 19981009 00672 NM 1998 10 9 USAASB98242 1 19980915 A 3350 20121 CHARGER BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD FIRST CLASS SEATS (ROWS 1 AND 2) AND ABOVE THE FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998100900673 19981009 00673 NM 1998 10 9 98ZZZM730 1 19980915 A 3350 20131ALP BATTERY BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 425US 23992 ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP AT THE FORWARD FIRST CLASS SEATS (ROWS 1 AND 2) AND ABOVE THE FORWARD SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK AND BATTERY CHARGER. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998100900674 19981009 00674 NM 1998 10 9 USAASB98240 1 19980913 A 3350 SWITCH BOEING 737 737201 1384454 NM CABIN MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 256AU 22798 CMH - FLT 2395 - DURING BOARDING, PILOT REPORTED THE FLOOR LEVEL EMERGENCY EXIT LIGHTS ILLUMINATED WHILE THE OVERHEAD EM ERGENCY LIGHTS REMAINED OFF. COCKPIT SWITCH WAS IN THE ARMED POSITION AND THE FLIGHT ATTENDANT SWITCH WAS IN THE NORMAL POSITION. MAINTENANCE ADJUSTED THE LEFT OVERWING EMERGENCY EXIT DOOR SWITCH. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998100900675 19981009 00675 NE 1998 10 9 TAOA099808 2 19980913 A 7261 7578678 FILTER BOEING 727 727227 1384078 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE CLOGGED A TAOA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 925TS 21244 649693 FLT 6120 - LGA-BOS - DURING TAKEOFF ROLL AND TAKEOFF POWER SET, ENGINE NR 3 LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMIN ATED. TAKEOFF ABORTED. LIGHT EXTINGUISHED AT IDLE THRUST. REPLACED MAIN ENGINE OIL FILTER. FOUND LARGE AMOUNT OF CAR BON DEPOSITS. RAN ENGINE, REMOVED FILTER AGAIN. MINOR SOOT FOUND. REPLACED FILTER AGAIN. RAN ENGINE. FILTER CLEAN. ASSIGNED W568026, RECHECK FILTER AFTER 50 FLT HOURS. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998100900676 19981009 00676 EU 1998 10 9 USAAF98074 1 19980910 A 7500 DUCT FOKKER F28 F28MK0100 4990807 EU NR 2 ENGINE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 888AU 11357 ORF - FLT 1041 - JUST AFTER TAKEOFF FROM ORF, CREW RECEIVED A NR 2 ENGINE FIRE WARNING INDICATION. EPR ON NR 2 ENGINE D ROPPED FROM TAKEOFF TO 1.5 EPR. CAPTAIN PULLED NR 2 THROTTLE BACK TO IDLE AND THE FIRE WARNING INDICATION EXTINGUISHED. FLIGHT RETURNED TO ORF AND LANDED WITHOUT FURTHER INCIDENT. THE CREW DID NOT ACTIVATE THE NR 2 ENGINE FIRE BOTTLE. M AINTENANCE FOUND A 12TH STAGE BLEED AIR DUCT FAILED ON THE NR 2 ENGINE. THEY REPLACED THE 12TH STAGE AIR OFFTAKE CARRIE R ASSEMBLY AND CLAMPS. (M) 2 L 7 2 4F RT 1998100900677 19981009 00677 EU 1998 10 9 USAAF98076 1 19980914 A 3040 D21518405 WINDOW FOKKER F28 F28MK0100 4990807 EU COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 888AU 11357 RIC FLT 469 - AT APPROXIMATELY 2000 FT AGL AFTER TAKEOFF FROM RIC, THE FLIGHT CREW NOTICED A BURNING SMELL COMING FROM T HE LEFT SLIDING WINDOW. THE CREW SHUT OFF THE WINDSHIELD HEAT AND THE BURNING SMELL SUBSIDED. THE CREW DECIDED TO RETU RN TO RIC FOR PRECAUTIONARY REASONS. THE FLIGHT LANDED RIC WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT SLI DING WINDOW. (M) 2 L 7 2 4F RT 1998100900678 19981009 00678 NM 1998 10 9 USAASB98238 1 19980911 A 2133 VALVE BOEING 737 7373B7 1384580 NM FUSELAGE CLOGGED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 531AU 24478 CLT - FLT 61 - CREW WAS UNABLE TO PRESSURIZE AIRCRAFT UPON CLIMB-OUT FROM CLT. FLIGHT RETURNED TO FIELD AT CLT AND LAND ED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND AN INSULATION BLANKET STUCK IN THE UPPER PRE SSURIZATION SAFETY RELIEF VALVE. REMOVED INSULATION AND SECURED. ACCOMPLISHED PRESSURIZATION CONTROL SYSTEM TEST. PRE SSURIZED AIRCRAFT ON GROUND TO 6.5 PSI WITH APU AND ONE PACK. ACCOMPLISHED HULL LEAK DOWN CHECK AND FOUND TO BE WITHIN LIMITS PER MM CHAPTER 21. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1998100900679 19981009 00679 WP 1998 10 9 HALA9800325 1 19980915 A 2131 26XN2160 PRESS CONTROLLER DOUG DC9 DC951 3022051 WP FUSELAGE FAILED A HALA G O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 WP 13 660HA 584 48122 ITO - FLT 102 - DEPLOYED CABIN OXYGEN MASK INFLIGHT. CABIN PRESSURE CONTROLLER IN FULL CLOSED POSITION. FERRIED A/C UN PRESSURIZED FROM ITO TO HNL, A/C MADE AN UNEVENTFUL LANDING IN HNL. REMOVED AND REPLACED BOTH ENG SEG SW AND PASSENGER OXYGEN REGUALTOR PER MM 21-31-9. (M) 2 L 7 2 4F RT A6WE 1998100900680 19981009 00680 WP 1998 10 9 AALA981597 1 19980831 A 5280 DOOR DOUG DC9 DC982 3022082 WP NLG OPEN A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 271AA 49293 ORD - FLT 1122 - AFTER TAKEOFF ORD EN ROUTE TO BOS WITH GEAR RETRACTED THERE WAS A LOUD VIBRATION NOISE COMING FROM THE NOSE GEAR AREA. AS SPEED INCREASED THE NOISE GOT LOUDER. AIR INTERRUPTED AND RETURNED TO ORD AND LANDED WITHOUT INCIDE NT. CLOSED NOSE GEAR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900681 19981009 00681 WP 1998 10 9 AALA981574 1 19980819 A 3260 VALVE DOUG DC9 DC982 3022082 WP NLG FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 286AA 49298 LAS - FLT 552 - EN ROUTE LAS-ORD, NOSE GEAR RED LIGHT REMAINED ON AFTER GEAR RETRACTION. RETURNED AND LANDED LAS WITHOU T INCIDENT. REPLACED SCHRADER VALVE AND PACKING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998100900682 19981009 00682 NM 1998 10 9 AALA981661 1 19980903 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1183 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - GOUGE AT INSIDE AIRSTAIR PUMP COMP CEILING RT SIDE THROUGH HORIZONTAL FLANGE OF WEB. TRIM WEB AND REPAIRED WITH S TAINLESS DOUBLER PER SRM 51-40-2. REPAIRED CHORD PER 51-40-4 AND ESO 11697 DATED 9/3/98. (M) 2 L 7 3 4F A3WE 1998100900683 19981009 00683 NM 1998 10 9 AALA981599 1 19980901 A 2910 233145 VALVE BOEING 767 767323 1385205 NM HYDRAULIC SYSTEM MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 363AA 24044 LHR - FLT 67 - AFTER TAKEOFF LHR EN ROUTE TO ORD WITH GEAR HANDLE UP, CENTER PRESSURE DROPPED TO 690 PSI. GEAR WOULD NO T RETRACT, GOT GEAR DOORS AND TAIL SKID LIGHTS. RETUREND AND LANDED LHR OVERWEIGHT AT 346,000 LBS. LANDED WITHOTU INCI DENT. FOUND HYDRAULC DRIVE GENERATOR SHUTOFF VALVE IN OPEN POSITION. POSITIONED AND LOCKED VALVE IN CLOSED POSITION PE R MM AND ACCOMPLISHED CENTER HYDRAULC SYSTEM CHECK PER MM. ACCOMPLISHED OVERWEIGHT LANDING INSPECTION. SYSTEM GROUND C HECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998100900684 19981009 00684 NM 1998 10 9 AALA981683 1 19980912 A 2610 358050 CONTROL UNIT BOEING 727 727223 1384074 NM E/E BAY MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 879AA 21391 MIA - FLT 941 - EN ROUTE MIA-SAP - CLIMBING OUT OF 25,000 FT THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. RAN CHECKLI ST AND LIGHT EXTINGUISHED AFTER CLOSING WING AND NR 2 ENGINE ANTI-ICE. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLA CED AFT BODY HEAT CONTROLLER, RAN ALL THREE ENGINES AT ALL POWER SETTINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998100900685 19981009 00685 NM 1998 10 9 EISA98218 1 19980915 A 3010 F61C0058M1 VALVE BOEING 727 727223 1384074 NM NR 3 ENGINE MALFUNCTIONED A EISA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 6839 3332 20192 ON DEPARTURE FROM EMA, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. PERFORMED CHECKLIST PER AFM VOLUME 1 LIGHT EXTINGU ISHED. CONTINUED FLIGHT TO BRU. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED AIR SHUTOFF VALVE IAW MM 75. (M) 2 L 7 3 4F A3WE 1998100900686 19981009 00686 WP 1998 10 9 EISA98216 1 19980910 A 2612 FIRE LOOP DOUG DC9 DC931 3022065 WP RT ENGINE FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 977ML 47329 RIGHT ENGINE LOOP 'A' FAILS TO TEST, LOOP 'B' CHECK OK. FOUND ON PREFLIGHT. GENERATED FROM PILOT REPORT. FOUND CONTAC TS ON CONNECTOR TO BE DIRTY. CLEANED AND RESEATED CONTACTS. CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998100900687 19981009 00687 WP 1998 10 9 98ZZZM731 1 19980721 A 3350 CHARGER LKHEED 1011 10113851 5265010 WP CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 187AT 193C1077 LAX - DURING P/F, FOUND EMERGENCY EXIT PATH LIGHTS INOP BETWEEN ROWS 35HJK-39HJK. REMOVED AND REPLACED BATTERY CHARGER. (M) 2 L 7 3 4F A23WE 1998100900688 19981009 00688 WP 1998 10 9 98ZZZM732 1 19980808 A 3350 BATTERY CHARGER LKHEED 1011 10113851 5265010 WP CABIN FAILED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 186AT 193C1074 DURING P/F, FOUND EMERGENCY EGRESS LIGHTING INOP 'C' ZONE, LEFT OF AIRCRAFT, LAST SEAT INOP. REPAIRED WIRING AT 'C' ZON E LIGHTING STRIP AND REPLACED FUSE AT DOOR 3R BATTERY CHARGER. (M) 2 L 7 3 4F A23WE 1998100900689 19981009 00689 NM 1998 10 9 98ZZZM733 1 19980322 A 2761 2690002910 SLAT ACTUATOR BOEING 727 727227 1384078 NM LE SLATS FAILED A AMTA D RETURN TO BLOCK K FLUID LOSS CL CLIMB 1 GL 11 772AT 22003 LAS - DURING CLIMB, NR 5 LEADING EDGE SLAT DID NOT INDICATE FULLY EXTENDED AFTER USING ALTERNATE FLAP SWITCH, BOTH POSIT ION. RETURNED TO LAS. 'A' SYSTEM HYDRAULIC LOSS. FOUND ACTUATOR END CAP SEPARATED FROM HOUSING AND SEIZED ON ACTUATOR SHAFT. REMOVED AND REPLACED NR 5 SLAT ACTUATOR. OPERATIONAL CHECKED COMPONENT SYSTEM FOR LEAKS AND FOUND OK. (M) 2 L 7 3 4F A3WE 1998100900690 19981009 00690 WP 1998 10 9 98ZZZM734 1 19980610 A 3230 LINK LKHEED 1011 10113851 5265010 WP RT MLG BROKEN A AMTA J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 185AT 193C1052 SFO - ON DEPARTURE, AFTER GEAR RETRACTION, INTRANSIT LIGHT RT GEAR DOOR ILLUMINATED. CYCLED GEARS SEVERAL TIMES, SAME R ESULT. DUMPED FUEL AND RETURNED TO SFO. REMOVED AND REPLACED RT GEAR LINK ASSY 'T' BAR STOP PER MM 32-33-00. OPS CHEC KED NORMAL (M). 2 L 7 3 4F A23WE 1998100900691 19981009 00691 NM 1998 10 9 F3LA98163 1 19980829 A 5330 SKIN BOEING 737 737201 1384454 NM BS 245 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 205AU 19421 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED A 3 INCH CRACK IN NOSE WHEEL WELL SKIN, BS 245.6 TO 248.6, WL 168.5. A .125 INCH CRACK AT RIVET, BS 244.1, W 165.5, AND A .125 INCH CRACK AT BS 243.1, WL 164.3. MAINTENANCE REPAIRED DAMAGED AREAS PER SRM 51-40-2. (M) 2 L 7 2 4F A16WE 1998100900692 19981009 00692 NM 1998 10 9 F3LA98164 1 19980831 A 3350 LIGHT BOEING 737 737301 1384611 NM CABIN INOPERATIVE A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 578US 23257 DEN - UPON ARRIVAL, FLIGHT CREW REPORTED FLOOR PROXIMITY LIGHTING AT ROW 7 INOPERATIVE. REPAIRED WIRING AND SYSTEM CHEC KED OK. (M) 2 L 7 2 4F RT A16WE 1998100900693 19981009 00693 NM 1998 10 9 F3LA98165 1 19980916 A 2121 GASPER FAN BOEING 737 737201 1384454 NM CABIN MALFUNCTIONED A F3LA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 NM 03 207AU 19423 PIH - EN ROUTE TO SEA, FLT CREW REPORTED A STRONG ELECTRICAL ODOR IN AFT PASSENGER CABIN. AIRCRAFT WAS DIVERTED TO POCA TELLO AND LANDED WITHOUT INCIDENT. MAINTENANCE DETECTED ODOR COMING FROM AIR VENTS WITH GASPER FAN 'ON'. INSPECTED AIR CONDITIONING DISTRIBUTION BAY FOR ABNORMALITIES AND PLACARDED SYSTEM PER MEL 21-24. UPON ARRIVAL IN DEN, MAINTENANCE R EPLACED GASPER FAN AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998100900694 19981009 00694 EU 1998 10 9 RAIA980816 1 19980828 A 7332 1103P0545 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE CONTAMINATED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 432AM 883 FLT 7426 - STL - LEFT FUEL PRESSURE CAPTION ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE CLEANED LEFT ENGINE FUEL LOW PRESS URE SWITCH. (M) 2 L 7 2 4T RT A56EU 1998100900695 19981009 00695 EU 1998 10 9 RAIA980905 1 19980907 A 7712 WARNING LIGHT BAG JETSTM JETSTM3201 1500217 EU COCKPIT ILLUMINATED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 429AM 879 FLT 7072 - JLN - RIGHT SRL CAPTION ILLUMINATED ON TAKEOFF ROLL. MIANTENANCE DEFERRED RIGHT SRL PER MEL 76-1 CATEGORY C. (M) 2 L 7 2 4T RT A56EU 1998100900696 19981009 00696 EU 1998 10 9 RAIA980817 1 19980822 A 5347 S536780001000 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 13148 283 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FLIGHT ATTENDANT SEAT TRACKS. MAINTENANCE REPLACED FLIGHT ATTENDANT SEAT TRACKS IAW ATR72 SRM. (M) 2 H 7 2 4T RT A53EU 1998100900697 19981009 00697 EU 1998 10 9 RAIA980819 1 19980822 A 5315 S53672408202 FLOORBEAM AEROSP ATR72 ATR72202 8680940 EU FUSELAGE FLOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 13148 283 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT FLOORBEAM 36 TOP CAP. MAINTENANCE REPAIRED FLOORBEAM 36 IAW ATR72 SR M. (M) 2 H 7 2 4T RT A53EU 1998100900698 19981009 00698 EU 1998 10 9 RAIA980818 1 19980822 A 5347 S536780001000 SEAT TRACK AEROSP ATR72 ATR72202 8680940 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 723TE 283 STL - DURING MAINTENANCE CHECK, FOUND CORROSION AT RIGHT INBOARD SEAT TRACK. MAINTENANCE REPAIRED RIGHT INBOARD SEAT TR ACK IAW ATR72 SRM. (M) 2 H 7 2 4T RT A53EU 1998100900699 19981009 00699 WP 1998 10 9 RAIA980903 2 19980906 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT MALFUNCTIONED A RAIA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CE 03 428AM 877 FLT 7508 - STL - RIGHT ENGINE EGT FLUCTUATES 100 DEGREES WITH SRL ON. MAINTENANCE DEFERRED RIGHT SRL 76-1 CAT C. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998100900700 19981009 00700 EU 1998 10 9 SIMA982601 1 19980917 A 5347 S53570203202 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AM 447 SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS COR RODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900701 19981009 00701 EU 1998 10 9 98ZZZM735 1 19980917 A 5347 S53678001224 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AM 447 SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS COR RODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900702 19981009 00702 EU 1998 10 9 98ZZZM736 1 19980917 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AM 447 SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS COR RODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900703 19981009 00703 EU 1998 10 9 98ZZZM737 1 19980917 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 447AM 447 SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT MIDDLE AND AFT OUTBOARD, AND LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS COR RODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900704 19981009 00704 EU 1998 10 9 SIMA982591 1 19980916 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 243AE 340B243 DFW - FLT 3516 - EMERGENCY LIGHT AT SEAT 9A DOES NOT ILLUMINATED. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. ( M) 2 L 7 2 4T RT A52EU 1998100900705 19981009 00705 EU 1998 10 9 SIMA982562 1 19980913 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 498AT 498 ABI - DURING CPCP-2 INSPECTION, FOUND THE RIGHT FLIGHT ATTENDANT SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998100900706 19981009 00706 EU 1998 10 9 SIMA982542 1 19980911 A 3350 ASNE006281A4A SWITCH AEROSP ATR42 ATR42300 8680920 EU COCKPIT BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AT 327 ORD - FLT 4135 - EMERGENCY LIGHT SWITCH BROKE OFF. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH. OPERATIONAL CHECK GOOD . (M) 2 H 7 2 4T RT A53EU 1998100900707 19981009 00707 EU 1998 10 9 SIMA982541 1 19980911 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 223AT 16475 223 FLT 4085 - EMERGENCY EXIT LIGHTS AT FRONT OF CABIN DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL C HECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998100900708 19981009 00708 EU 1998 10 9 SIMA982433 1 19980901 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 37AE 1604 037 GRR - FORWARD CABIN FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOO D. (M) 2 H 7 2 4T RT A53EU 1998100900709 19981009 00709 NM 1998 10 9 USAA980337 1 19980807 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 42187 22886 TPA - DURING CX-5 VISUAL INSPECTION, FOUND A 1 INCH CRACK IN ANGLE AT STATION 727 COMPRESSION CHORD RBL 25. INSTALLED D OUBLER PER TYPICAL REPAIR NR 53-10-03A PART 3. (M) 2 L 7 2 4F A16WE 1998100900710 19981009 00710 NM 1998 10 9 USAA980338 1 19980807 A 5210 65528732 SKIN BOEING 737 7372B7 1384560 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 42187 22886 TPA - DURING CX-5 CHECK EDDY CURRENT INSPECTION, FOUND A .5 INCH CRACK IN OUTER SKIN OF AFT ENTRY DOOR, LOWER AFT CORNER OF UPPER HINGE CUTOUT. ROUTED DAMAGE AND INSTALLED DOUBLER OF .071,2024-T3 PER SRM 52-10-01, 51-30-8 AND EA 62192. (M ) 2 L 7 2 4F A16WE 1998100900711 19981009 00711 NM 1998 10 9 USAA980383 1 19980904 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 263AU 40259 22869 TPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK UNDER WING TO BODY FAIRING FUSELAGE SKIN AFT OF STATION 727B AND STRINGER 18R .50 BELOW. INSTALLED DOUBLER .063 301 .5 H STAINLESS PER EA 62403 AND SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998100900712 19981009 00712 1998 10 9 USAAD98161 4 19980915 A 2565 13621229 SLIDE DOUG DC9 DC931 3022065 WP FUSELAGE FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 958VJ 47351 PIT - THE AFT ESCAPE SLIDE MECHANISM FAILED TO DEPLOY THE SLIDE DURING FUNCTIONAL TEST. MAINTENANCE REPLACED THE SLIDE ASSY. (M) 2 L 7 2 4F A6WE 1998100900713 19981009 00713 NM 1998 10 9 USAA980397 1 19980905 A 5330 SKIN BOEING 737 737201 1384454 NM BS 771-775 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 52253 21666 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND 3.75 INCH CRACK ON SKIN BETWEEN STATION 771 AND 775 2 INCH ABOVE STRINGER 17 L. FOUND 5.5 INCH CRACK ON SKIN BETWEEN STATION 760 AND 766 2 INCH ABOVE STRINGER 17L. VISUALLY DETECTED AND CONFIRMED BY EDDY CURRENT. INSTALLED ONE EXTERNAL DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998100900851 19981009 00851 NM 1998 10 9 TWAA9816201 1 19981007 A 3350 CONNECTOR BOEING 767 767205 1385121 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 651TW 23058 FOUND EGRESS LIGHT STRIP INOPERATIVE ON RT SIDE BY CABIN SEATS 19-8 TO 22-8. SECURED LOOSE LIGHT STRIP CONN AT SEAT 22- 8. CHECK-C 9-23-98 LAX. 2 L 7 2 4F RT A1NM 1998100900852 19981009 00852 SO 1998 10 9 LR7A9838 1 19981002 A 5320 WEB LKHEED 382 382G 526414U SO BS 617 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1473 4606 RT GEAR WELL AFT PRESSURE WEB AT STA 617 HAS CRACKS ON THREE RISERS. REPAIRED IN ACCORDANCE WITH ED NR EDF49-1. 2 H 7 4 4T A1SO 1998100900853 19981009 00853 SO 1998 10 9 RAAA98E9033 1 19981003 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 17 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998100900854 19981009 00854 NM 1998 10 9 CALA9801908 1 19981005 A 5320 ANGLE BOEING 727 727243 138408D NM R-2 DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND FLOOR SUPPORT ANGLE JUST INSIDE R-2 DOOR THRESHOLD AREA CORRODED AROUND SCREW HOLES. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2, PAGE 4. 2 L 7 3 4F RT A3WE 1998100900855 19981009 00855 NM 1998 10 9 CALA9801909 1 19981005 A 5754 RIB BOEING 727 727243 138408D NM NR 3 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND A 1.25 INCH CRACK AT AFT LOWER END OF NR 3 SLAT LEADING EDGE RIB AND A 1.25 INCH CRACK WAS FOUND AT FOR WARD LOWER END OUTBOARD OF ACTUATOR ROD MOUNT. THE CRACKS WERE STOP DRILLED IAW SRM 51-30-2, A DOUBLER WAS INSTALLED IA W SRM 57-50-3, PAGE 26 AND 51-30-2, PAGE 14. 2 L 7 3 4F RT A3WE 1998100900856 19981009 00856 NM 1998 10 9 CALA9801910 1 19981005 A 5313 STRINGER BOEING 727 727243 138408D NM BS 1000 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND STRINGER 29R CORRODED AT STA 1000. THE CORRODED AREA WAS CUT OUT AND REPAIR PARTS WERE INSTALLED IAW S RM 51-40-3, 51-10-2, AND SB 727-53-0179. 2 L 7 3 4F RT A3WE 1998100900857 19981009 00857 NM 1998 10 9 CALA9801911 1 19981005 A 5752 652173623 AILERON TAB BOEING 727 727224 1384076 NM LT AILERON DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND LT INBOARD AILERON TAB DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-31. 2 L 7 3 4F A3WE 1998100900858 19981009 00858 NM 1998 10 9 CALA9801912 1 19981005 A 5741 BOTTLE PIN BOEING 727 727224 1384076 NM BS 870 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WING TO FUSELAGE BOTTLE PIN, BUSHING, AND RETAINING BOLT CORRODED AT BS 870. THE BOTTLE PIN, BUSHIN G, AND RETAINING BOLT WERE REMOVED AND REPLACED IAW MM 57-41-1, PAGE 403 AND 57-41-11, PAGE 404. 2 L 7 3 4F A3WE 1998100900859 19981009 00859 WP 1998 10 9 CALA9801913 1 19981007 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND A 1.375 INCH CRACK IN FORWARD SERVICE DOOR NR 4 BEAM. THE NR 4 BEAM WAS REMOVED AND REPLACED IAW SRM 5 1-30-2. 2 L 7 2 4F A6WE 1998100900860 19981009 00860 NM 1998 10 9 UPS98227879 1 19981003 A 5310 WEB BOEING 727 72727C 138400J NM BS 1266 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 914UP 19246 INSPECTION TYPE-C, THE AFT STAIRWELL TORQUE BOX INBOARD VERTICAL WEB IS CRACKED JUST UNDER PREVIOUS REPAIR AT BS 1266 WL 192 RBL 21. REMOVED PREVIOUS REPAIR CUT OUT DAMAGED AREA PER SRM 53-10-1. FABRICATED REPAIR DOUBLER PER SRM 51-40-2. INSTALLED DOUBLER PER SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998100900861 19981009 00861 WP 1998 10 9 UPS98827870 1 19980915 A 5312 BULKHEAD BEAM DOUG DC8 DC871F 302199D WP AFT PRESS BLKHD CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, AFT FACE OF PRESSURE BULKHEAD STA 1766, 4TH HORIZONTAL BEAM HAS 2 CRACKS, 1 TOP AND 1 BOTTOM CENTER BEHIND CONTROL CABLES APPROX STA 36 (E824). VERIFIED CRACK IAW MIL STD 271F. STOP DRILLED CRACK AND FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-5 FIG 26. ALODINED AND PRIMED ANGLE IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 1-1-20D. 2 L 7 4 4F RT 4A25 1998100900862 19981009 00862 WP 1998 10 9 UPS98827871 1 19980914 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 712 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, CORROSION ON FRAME STA 712 AT SEAT TRACK BOLT HOLES RBL 26. REMOVED AND REPLACED BOLTS IAW DC8 SRM 51-3-0. REMOVED CORROSION, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FOUND WITHIN LIMITS IAW DC8 SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998100900863 19981009 00863 WP 1998 10 9 UPS98827872 1 19980918 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1190 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, FUSELAGE EXTERIOR SKIN CORRODED STA 1190 AND LONG 22R. REPAIRED AREA IAW DC8 SRM 53-2-1 FIG 7. REM OVED CORROSION PER DC8 SRM 51-1-8. BLEND OUT WAS BEYOND LIMITS PER DC8 SRM 53-2-0. TRIMMED OUT DAMAGE, FABBED FILLER A ND DOUBLER PER DC8 SRM 53-2-1 FIG 7 AND REO 05 451. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PER REO-05451 AN D DC8 S RM 53-2-1 FIG 7. 2 L 7 4 4F RT 4A25 1998100900864 19981009 00864 WP 1998 10 9 UPS98827873 1 19980915 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, CORROSION AROUND NUT PLATE ON TORQUE BOX RAMP ATTACH ANGLE AT FS 280, LONGERON 33L. REMOVED CORROSI ON ON GUIDE RAIL IAW DC8 SRM 51-1-8, OUT OF LIMITS. REMOVED RAIL, MAT ID 7075-0 .063 PO 265649 IAW REO-05501. FAB ANGL E DOUBLER IAW REO-05501. HEAT TREAT TO T-6 IAW DC8 SRM 51-1-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 1998100900865 19981009 00865 WP 1998 10 9 UPS98827874 1 19980914 A 5320 PRESSURE PANEL DOUG DC8 DC871F 302199D WP BS 889 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, STA 889 TO 900 XCW 10L SKIN HAS A GOUGE AND IS CORRODED, CENTERWING. BLENDED OUT GOUGE AND CORROSIO N IAW DC8 SRM 53-2-0. ORIG .063 IAW 53-7-2. REMAIN .043. FAB REPAIR DOUBLER IAW REO-05478 AND DRILLED IAW DC8 S RM 51 -1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21, 51-1-15. 2 L 7 4 4F RT 4A25 1998100900866 19981009 00866 WP 1998 10 9 UPS98827875 1 19980911 A 5720 BRACKET DOUG DC8 DC871F 302199D WP WS 223 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, RT WING LEADING EDGE NR 3 PNEU SHUT-OFF AFT ATTACH BRACKET AT XW223 CRACKED. REMOVED BROKEN BRACKET IAW DC8 SRM 51-3-0. MAT ID FOR NEW BRACKET 302 STAINLESS STEEL .063 IN ANNEALED CONDITION IAW DAC DWG NR 5802881 AND D C8 SRM 51-9-0. FAB NEW BRACKET IAW DAC DWG 5802881. INSTALLED NEW BRACKET IAW DC8 SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998100900867 19981009 00867 WP 1998 10 9 UPS98827876 1 19980917 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 795 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, RT SIDE CENTER WING, STA 795 AND XCW46R FITTING IS CRACKED. REMOVED FITTING CRACKED AT RT CENTER WI NG STA 759 AND XCW46R. RECEIVED NEW FITTING 3641125-507 PO 270648. DRILLED HOLES IAW DC8 SRM 51-1 -24. ALODINED AND P RIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998100900868 19981009 00868 WP 1998 10 9 UPS98827877 1 19980917 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1919 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, TAIL CONE FRAME STA 1919 RT SIDE OF LONGERON 36 CRACKED. REMOVED DAMAGED SECTION OF FRAME, FORMED F RAME SECTION IAW DAC DWG 5 704650. HEAT TREATED ANGLES, SPLICES, FORMED FRAME IAW TPS-1003 AND DC8 SRM 51-1-1. FAB FRA ME AND SPLICE ANGLES AND DRILLED IAW DC8 SRM 53-2 -9. DAC DWG 5704650 AND DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998100900869 19981009 00869 WP 1998 10 9 UPS98827878 1 19980914 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE-C2, STA 902 AND XCW64L, FUSELAGE FRAME FITTING AND FLOORBEAM IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS. INSTALLED NEW FITTING AND ALL PARTS IAW DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998100900870 19981009 00870 WP 1998 10 9 UPS98827880 1 19981007 A 3350 6012235 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 709UP 45914 INSPECTION TYPE-N/A, EMERGENCY LIGHTS DID NOT ILLUMINATE DURING PREFLIGHT TEST. REPLACED EMERGENCY LIGHTING BATTERY PAC K. 2 L 7 4 4F RT 4A25 1998100900871 19981009 00871 WP 1998 10 9 UPS98827881 1 19980925 A 5320 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 640 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, FS 640 BETWEEN LONG 26L AND 27L THE SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND INSTALLED SHEAR TI E AND SPLICE IAW SRM 53-2-0 FIG 2A AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998100900872 19981009 00872 WP 1998 10 9 UPS98827882 1 19980925 A 5320 3646688506 SHEAR TIE DOUG DC8 DC873F 302199F WP BS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, FS 660 FRAME AT LONG 22R IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW DWG 3646688 AND SRM 51-1- 20D. 2 L 7 4 4F RT 4A25 1998100900873 19981009 00873 WP 1998 10 9 UPS98827883 1 19980926 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 735 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E UPPER SURFACE HAS .25 INCH CRACK BY ATTACH SCREW AT STA XFS 735. CUT OUT DAMAGE AND REPA IRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998100900874 19981009 00874 WP 1998 10 9 UPS98827884 1 19980927 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 610. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998100900875 19981009 00875 WP 1998 10 9 UPS98827885 1 19980927 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 616.25. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998100900876 19981009 00876 WP 1998 10 9 UPS98827886 1 19980927 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 578.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING L/E RIB CRACKED ON UPPER ARM BY AFT FASTENER AT STA XFS 578.75. STOP DRILLED CRACK AND REPAI RED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998100900877 19981009 00877 WP 1998 10 9 UPS98827887 1 19980928 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 317.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, RT WING L/E TOP SKIN AT STA XFS 317.5 IS CRACKED AT THE FRONT SPAR. CUT OUT DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998100900878 19981009 00878 WP 1998 10 9 UPS98827888 1 19980928 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, RT WING L/E TOP SKIN AT STA XFS 610 IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998100900879 19981009 00879 EU 1998 10 9 QXEA9801427 1 19981006 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 498US 11181 EMERGENCY EXIT LIGHT AT ROW 8A INOP. REMOVED AND REPLACED LAMP AT ROW 8A, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998100900880 19981009 00880 NM 1998 10 9 98FDEA00622 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 UPPER LOBE FLOORBEAM BS 1130, LBL 65 FIG 8 HAVE IN UPPER FLANGE AND LIGHT CORROSION UNDER FLANGE. REMOVED AND REPLACED CORROSION ON FLOORBEAM WITH FREEZE PLUG SRM 51-10-7. TREATED AND PRIMED AREA PER MM 51-20-0. 2 L 7 3 4F RT A3WE 1998100900881 19981009 00881 NM 1998 10 9 98FDEA00623 1 19981006 A 5311 BELL FRAME BOEING 727 727233 138408A NM BS 600 CRUSHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 LWR FWD CARGO COMP BS 600 BELL FRAME CRUSHED IN SEVERAL AREAS BETWEEN STR 26L AND 23L. REPAIRED BELL FRAME AT BS 600 BE TWEEN STR 26L AND 23L PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998100900882 19981009 00882 NM 1998 10 9 98FDEA00624 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 CORROSION ON THE BOTTOM O/B SEAT TRACK BOLTS BS 1130, RBL 65 O/B. INSTALLED DOUBLER ON FWD SIDE OF FLOORBEAM BS 1130, R BL 30 TO RBL 70 PER EA 7-5310-29637A DATED 9-4-98. 2 L 7 3 4F RT A3WE 1998100900883 19981009 00883 NM 1998 10 9 98FDEA00625 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 CORROSION UNDER NUT PLATE ON FLOORBEAM BS 130, RBL 43. INSTALLED DOUBLER ON FWD SIDE OF FLOORBEAM BS 1130, RBL 38 TO RB L 70 PER EA 7-5310-29637A DATED 9/4/98. 2 L 7 3 4F RT A3WE 1998100900884 19981009 00884 NM 1998 10 9 98FDEA00626 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 CORROSION ON FWD FLANGE OF FLOORBEAM BS 1130, RBL 45. INSTALLED DOUBLER ON FWD SIDE OF FLOORBEAM BS 1130, RBL 38 TO RBL 70 PER EA 7-5310-29637A DATED 9-4-98. 2 L 7 3 4F RT A3WE 1998100900885 19981009 00885 NM 1998 10 9 98FDEA00627 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 HEAVY AREA OF CORROSION ON TOP OF FLOORBEAM BS 720A, RBL 4 AT NUT PLATE HOLE (2 PLACES). REMOVED CORROSION ON FLOORBEAM , INSTALLED FLOORBEAM REPAIR PER AARD 53-10-7-2 FIG 2 IAW EA 7-5310-29647. 2 L 7 3 4F RT A3WE 1998100900886 19981009 00886 NM 1998 10 9 98FDEA00628 1 19981006 A 5311 BELTFRAME BOEING 727 727233 138408A NM BS 520 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 BELTFRAME DAMAGED BS 520, RT SIDE 6 INCHES ABOVE FLOORBEAM. TRIMMED OUT DAMAGE. INSTALLED TYPICAL FORMED SECTION REPAI R PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998100900887 19981009 00887 NM 1998 10 9 98FDEA00629 1 19981006 A 5311 BELL FRAME BOEING 727 727233 138408A NM BS 580 CRUSHED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 LWR FWD CARGO COMP BS 580 BELL FRAME CRUSHED IN SEVERAL AREAS BETWEEN STR 26 AND 23 LEFT. REPAIRED BELL FRAME AT BS 580 BETWEEN STR 26L AND 23L PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998100900888 19981009 00888 NM 1998 10 9 98FDEA00630 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1030 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 BS 1030 BL 0, FLOORBEAM REPAIR NOT PER SRM ON I/B AIRCRAFT. REMOVED PREVIOUS REPAIR AND INSTALLED FLOORBEAM REPAIR PER SRM 53-10-8, FIG 3. 2 L 7 3 4F RT A3WE 1998100900889 19981009 00889 NM 1998 10 9 98FDEA00631 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 CORROSION ON FLOORBEAM BS 1130, LBL 35 AND LBL 42. REPAIRED IAW EA NR 7-5310-29637B. 2 L 7 3 4F RT A3WE 1998100900890 19981009 00890 NM 1998 10 9 98FDEA00632 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 BS 870 FLOORBEAM AT BL 0 TO RBL 25 CORROSION ON FLOORBEAM AND IN FASTENER HOLES. REMOVED CORROSION AND INSTALLED FREEZE PLUG PER EA 7-5310-2964. 2 L 7 3 4F RT A3WE 1998100900891 19981009 00891 NM 1998 10 9 98FDEA00633 1 19981006 A 5320 FITTING BOEING 727 727233 138408A NM BS 870 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 BS 870 FLOORBEAM FITTING AT CENTER EXPANSION TRACK BELOW FLOOR LWR FITTING HAS CORROSION BOTH SIDES. REMOVED AND REPLAC ED CORROSION PER EA 7-5310-29647 AND REINSTALLED EXPANSION TRACK. 2 L 7 3 4F RT A3WE 1998100900892 19981009 00892 NM 1998 10 9 98FDEA00634 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 950 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 ACCOMPLISH REPAIR TO BS 950D, BL 0 AS PER SRM 53-10-8 FIG 8 PG 44 REF AARD 51-20-1-05. INSTALLED FLOORBEAM REPAIR PER S RM 53-10-8 FIG 8 AND EA 7-5310-29647. 2 L 7 3 4F RT A3WE 1998100900893 19981009 00893 NM 1998 10 9 98FDEA00635 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 BS 950D RBL 25 TO LBL 25, 8 FLOORBOARD FASTENER HOLES CORRODED AT FLOORBEAM. REMOVED CORROSION AREA AT RBL 10, BS 950D OUT OF LIMITS. INSTALLED FLOORBEAM REPAIR PER AARD 53-10-07-2 IAW EA 7-5310-29647. 2 L 7 3 4F RT A3WE 1998100900894 19981009 00894 NM 1998 10 9 98FDEA00636 1 19981006 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 CORROSION BETWEEN FLOORBEAM AND SEAT TRACK BS 1050, RBL 25. REMOVED CORROSION AND CUT OUT DAMAGE. INSTALLED REPAIR DOU BLERS PER SRM 53-10-8. 2 L 7 3 4F RT A3WE 1998100900895 19981009 00895 WP 1998 10 9 98FDEA00637 1 19981006 A 5530 ANGLE DOUG DC10 DC1010F 3022111 WP VERT STAB CRACKED A FDEA O OTHER O OTHER IN INSP/MAINT 1 SO 25 050FE 47804 REPLACED UPPER VERTICAL STAB REAR SPAR BASE ANGLE (CRACKED). REPLACED AMC7279-1 BASE ANGLE WITH AMC727950, BASE ANGLE P ER EO 8-5630-7-4303B PT 2. 2 L 7 3 4F A22WE 1998100900896 19981009 00896 NM 1998 10 9 98UAL900471 1 19980926 A 2121 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LEFT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 589UA 28707 DIVERTED TO HNL WITH A LEFT RECIRCULATION FAN PROBLEM. 2 L 7 2 4F 4 F RT A2NM E17NE 1998100900897 19981009 00897 NM 1998 10 9 98UAL900472 1 19980926 A 3411 856AE18 PITOT PROBE HONEYWELL HG480B14 BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE FWD FUSELAGE MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 982UA R2875806 21640 ALTIMETER IS READING INCORRECTLY. *S/D* MAINTENANCE REPLACED PITOT/STATIC PROBE AND NR 1 AIR DATA COMPUTER. THE REMOV ED AIR DATA COMPUTER TESTED NORMAL IN THE SHOP. 2 L 7 2 4F 4 F A16WE E2EA 1998100900898 19981009 00898 EU 1998 10 9 98UAL900473 1 19980925 A 3350 BR964421 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ROW 6, 10 & 15 INOPERATIVE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 413UA 470 EMERGENCY ESCAPE PATH LIGHTS INOP AT SEATS 6C, 10C, AND 15C. *S/D* REPLACED LIGHT ASSY, OPS CK NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1998100900899 19981009 00899 NM 1998 10 9 98UAL900474 1 19980926 A 4990 OIL SYST BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU REQD SERVICE A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 363UA 8898 537 24532 922361 APU WENT OFF-LINE. *S/D* APU FAULT LIGHT CAME ON AND APU SHUT DOWN INFLIGHT. SERVICED APU WITH ONE QUART OF OIL, STAR TED AND RAN SEVERAL TIMES ABOUT 4 HOURS. GROUND CHECKS NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1998100900900 19981009 00900 NM 1998 10 9 98UAL900476 1 19980924 A 2781 H1010262 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 6 LE FLAP FAILED A UALA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 WP 29 7285U 21563 # 6 LEADING EDGE FLAP SHOWS AMBER LIGHT WHEN IN FULL UP POSITION ON SECOND OFFICERS PANEL AND ON FORWARD PANEL. RETURNE D TO ORD. SUPPLEMENTAL DATA UPDATE REPLACED #6 LE FLAP SWITCH. SYSTEM OPERATES NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1998100900901 19981009 00901 NE 1998 10 9 98UAL900477 2 19980927 A 7532 BLEED VALVE ALLIEDSIGNAL 32144462 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 2 FAILED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 343UA 24247 RIGHT HAND PACK BECAME INOPERATIVE. *S/D* RIGHT HAND PACK TRIPPED OFF AND COULD NOT BE RESET DUE TO NR 2 HIGH STAGE BL EED VALVE FAILING IN THE OPEN POSITION. REPLACED THE NR 2 HIGH STAGE BLEED VALVE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998100900902 19981009 00902 NM 1998 10 9 98UAL900479 1 19980814 A 3397 WIRE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CABIN FAILED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 178UA 24385 UPPER DECK WINDOW LIGHTS AT SEATS 12AB AND 14GH PREVIOUSLY DEFERRED INOP. ON TAXI TO INBOUND GATE CIRCUIT BREAKERS TRIP PED ON P180 AND P414 PANELS. FOUND SEVERAL BURNT AND OVERHEATED WIRES COMMON TO WIRE BUNDLE W7510. *S/D* FOUND EVIDEN CE OF ARCING ON AIR DISTRIBUTION DUCT AND SIDE WALL PANEL END CAP LIGHT ASSY UPPER EDGE (P/N 417U7572-1 ASSY 417U7514-1 DETAIL). REPAIRED FIBERGLASS WIRE/WOUND AIR DISTRIBUTION DUCT AND INSULATION. REMOVED DAMAGED WIRE SECTIONS AND SPLICE D IN NEW WIRE SECTIONS AND SECURED CLEARANCE BETWEEN SIDE WALL PANEL END CAP UPPER EDGE. TESTED ALL EFFECTED SYSTEMS. 2 L 7 4 4F 4 F RT A20WE E24NE 1998100900903 19981009 00903 WP 1998 10 9 98UAL900480 1 19980928 A 3397 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1837U 47969 EEL LIGHT STRIP OUT AT 1EF THROUGH DOOR 2R, 9AB THROUGH 16AB AND 30HJ THROUGH 38HJ. SPLICED NEW RIBBON BY BULKHEAD 1R, 2L AND REPLACED LEADER CABLE ASSY, CHECKS OK. 2 L 7 3 4F 4 F A22WE E23EA 1998100900904 19981009 00904 NM 1998 10 9 98UAL900481 1 19980930 A 2133 MOTOR NORDMICRO 90231570381 AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE OUTFLOW VALVE FAILED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 813UA 3571 858 PRESSURIZATION 2 FAILURE DISPLAYED ON UPPER ECAM. RESET CB PRESSURIZATION 1 THEN FAILED FOLLOWED BY ANOTHER NR 2 FAILUR E. MANUAL MODE OK. RETURNED TO LAX. *S/D* PROBLEM CAUSED BY THE OUTFLOW VALVE MOTOR. REPLACED OUTFLOW VALVE MOTOR 10HL-3 PER MM 21-31-51-000-003 AND PERFORMED OPERATIONAL CHECK. FAULT CLEARED AND SYSTEM OPERATES NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1998100900905 19981009 00905 NE 1998 10 9 98UAL900482 2 19980930 A 7261 GEAR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 OIL PUMP FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 29 451UA 865 DIVERTED TO ONT WITH NR 2 ENGINE SHUTDOWN DUE TO OIL PRESSURE INDICATION. *S/D* OIL PUMP DRIVE GEAR FAILED CAUSING LOSS OF OIL PRESSURE. GEAR FAILED FROM A MANUFACTURING DEFECT. CONSIDERED ISOLATED CASE. 2 L 7 2 4F 4 F RT A28NM E40NE 1998100900906 19981009 00906 NE 1998 10 9 98UAL900483 2 19980928 A 7530 THERMOSTAT VF1958 342B010000 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE ENGINE BLEED SYS MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION UK UNKNOWN 1 WP 29 440UA 1213 702 RETURNED WITH ENGINE BLEED VALVE PROBLEM. *S/D* BLEED VALVE PROBLEM TRACED TO THERMOSTAT. REPLACED THERMOSTAT AND SYS TEM OPERATED NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1998100900907 19981009 00907 WP 1998 10 9 ABXA9800856 1 19980828 A 2750 39176002 FITTING DOUG DOUG DC9 DC932 3022066 WP RT TE FLAP GOUGED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND A RIGHT FLAP MOVEABLE VANE PULLEY BRACKET ATTACH FITTING GOUGED AND RIVETS SHEA RED. REPLACED RIGHT FLAP PULLEY BRACKET ATTACH FITTING IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998100900908 19981009 00908 WP 1998 10 9 ABXA9800857 1 19980826 A 5720 591957191 DOOR DOUG DOUG DC9 DC932 3022066 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT WING INBOARD BUTE DOOR CRACKED AT INBOARD CAM ROLLER. REPLACED LEFT I NBOARD BUTE DOOR IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998100900909 19981009 00909 WP 1998 10 9 ABXA9800858 1 19980826 A 5720 591217257 ANGLE DOUG DOUG DC9 DC932 3022066 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE INBOARD ATTACH ANGLE FOR THE CENTER BUTE DOOR CRACKED AT RIGHT WING STATION 164 HINGE BRACKET. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTER 51-30-01. 2 L 7 2 4F A6WE 1998100900910 19981009 00910 WP 1998 10 9 ABXA9800859 1 19980903 A 5210 59141211 ANGLE DOUG DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ENTRY DOOR PAN CRACKED OUT IN LOWER FORWARD CORNER. REPAIRED CRACK IA W ABX REA D952-24779. 2 L 7 2 4F A6WE 1998100900911 19981009 00911 WP 1998 10 9 ABXA9800860 1 19980916 A 5320 991078873 WEB DOUG DOUG DC9 DC932 3022066 WP BS 200-218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CUSP WEB BETWEEN FS 200 AND 218 CORRODED. REPLACED CUSP WEB IAW DC9 S RM CHAPTERS 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998100900912 19981009 00912 WP 1998 10 9 ABXA9800861 1 19980906 A 5320 WEB DOUG DOUG DC9 DC932 3022066 WP BS 218-237 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CUSP WEB BETWEEN FS 218 AND 237 CORRODED. REPLACED CUSP WEB IAW DC9 S RM CHAPTERS 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998100900913 19981009 00913 WP 1998 10 9 ABXA9800862 1 19980916 A 5320 WEB DOUG DOUG DC9 DC932 3022066 WP BS 237-313 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CUSP WEB CORRODED BETWEEN FS 237 TO FS 313. REPLACED CUSP WEB IAW DC9 SRM CHAPTERS 61-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998100900914 19981009 00914 WP 1998 10 9 ABXA9800863 1 19980917 A 5730 59104611 SKIN DOUG DOUG DC9 DC932 3022066 WP WS 20 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE UPPER SURFACE OF THE CENTER WING TANK CORRODED AT REAR SPAR AT STATION XCW2 0. REPAIRED UPPER SKIN SURFACE IAW ABX REA D957-24799MR. 2 L 7 2 4F A6WE 1998100900915 19981009 00915 WP 1998 10 9 ABXA9800864 1 19980827 A 2550 592600657 DOOR DOUG DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE AFT LOWER CARGO COMPARTMENT BARRIER DOOR CORRODED. REPLACED AFT CARGO BARR IER DOOR IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998100900916 19981009 00916 WP 1998 10 9 ABXA9800865 1 19980903 A 5311 99577397 SHEAR TIE DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND SHEAR TIE DOUBLER ON FUSELAGE FRAME AT FS 945 CRACKED AT LONGERON 14 RIGHT. RE PLACED SHEAR TIE AT FS 945 BETWEEN LONGERON 14 RIGHT AND LONGERON 16 RIGHT IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998100900917 19981009 00917 WP 1998 10 9 MWEA98986 1 19981005 A 2560 113317 COVER DOUG DC9 DC914 3022034 WP PAX DOOR SLIDE FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 800ME 45842 THE PASSENGER DOOR SLIDE COVER FELL OFF. MTC REINSTALLED PASSENGER DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998100900918 19981009 00918 WP 1998 10 9 MWEA98987 1 19981006 A 5210 49559481N HOOK DOUG DC9 DC932 3022066 WP PAX DOOR FRACTURED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FOUND MAIN CABIN DOOR HOLD OPEN HOOK ENCLOSURE FRACTURED. MTC DRILLED NEW DOOR HOOK ENCLOSURE AND INSTALLED. 2 L 7 2 4F A6WE 1998100900919 19981009 00919 WP 1998 10 9 MWEA98988 1 19981006 A 5330 5911408125 SKIN DOUG DC9 DC932 3022066 WP BS 256 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FOUND A PREVIOUS REPAIR DOUBLER UNDER FORWARD UPPER ADF ANTENNA AT STATION 256. MTC REMOVED DOUBLER, CLEANED SKIN, FABR ICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998100900920 19981009 00920 WP 1998 10 9 MWEA98989 1 19981006 A 5330 5911408125 SKIN DOUG DC9 DC932 3022066 WP BS 300 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FOUND A PREVIOUS REPAIR DOUBLER UNDER AFT UPPER ADF ANTENNA AT STATION 300. MTC REMOVED DOUBLER, CLEANED SKIN, FABRICAT ED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998100900921 19981009 00921 WP 1998 10 9 MWEA98990 1 19981006 A 2520 39139291 CLOSEOUT PANEL DOUG DC9 DC932 3022066 WP OVERWING EXIT OUT OF POSITION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 401ME 47133 FOUND THE AFT LEFT OVERWING EMERGENCY EXIT INSIDE HANDLE BINDS UP WITH THE HANDLE RECEPTICAL TRIM SCREW AT FORWARD END O F HANDLE. MTC REPOSITIONED CLOSE OUT PANEL. 2 L 7 2 4F A6WE 1998100900922 19981009 00922 WP 1998 10 9 MWEA98991 1 19981006 A 5530 991188110 RIB DOUG DC9 DC982 3022082 WP STATION ZFS 4962 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CRACKED RIB ON VERTICAL STABILIZER LEADING EDGE AT STATION ZFS 49 62 RIGHT SIDE. MTC FABRICATED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 1998100900923 19981009 00923 WP 1998 10 9 MWEA98992 1 19981006 A 5530 991188210 RIB DOUG DC9 DC982 3022082 WP STATION ZFS 430 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CRACKED RIB ON LEADING EDGE VERTICAL STABILIZER AT STATION ZFS 43 0 RIGHT SIDE. MTC FABRICATED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 1998100900924 19981009 00924 WP 1998 10 9 MWEA98993 1 19981006 A 5531 991188410 RIB DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CRACKED RIB ON LEADING EDGE VERTICAL STABILIZER AT STATION ZFS 30 0 RIGHT SIDE. MTC FABRICATED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 1998100900925 19981009 00925 WP 1998 10 9 MWEA98994 1 19981006 A 5531 99118829 RIB DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CRACKED RIB ON LEADING EDGE OF VERTICAL STABILIZER AT STATION ZFS 430 LEFT SIDE. MTC FABRICATED AND INSTALLED NEW RIB. 2 L 7 2 4F A6WE 1998100900926 19981009 00926 WP 1998 10 9 MWEA98995 1 19981006 A 5531 99118819 RIB DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CRACKED RIB ON LEADING EDGE OF VERTICAL STABILIZER AT STATION ZFS 49 62 LEFT SIDE. MTC FABRICATED AND INSTALLED N EW RIB. 2 L 7 2 4F A6WE 1998100900927 19981009 00927 NM 1998 10 9 SCNA98117 1 19981006 A 3350 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE LOWER EMERGENCY EXIT SIGN AT THE LEFT FORWARD OVERWING DOOR WAS FOUND BROKEN. REMO VED AND REPLACED ASSOCIATED EMERGENCY LIGHT ASSEMBLY. ALL EMERGENCY LIGHTS CHECK GOOD. 2 L 7 3 4F RT A3WE 1998100900928 19981009 00928 NM 1998 10 9 SCNA98118 1 19981004 A 3350 1000677 LIGHT BOEING 727 7272J4 1384006 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 284SC 21438 DURING A LINE MAINTENANCE CHECK, THE R1 EMERGENCY LIGHTS WERE FOUND TO OPERATE AFTER THE POWER WAS PUT ON THE AIRCRAFT. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AT THE R1 DOOR. OPERATIONALLY CHECKS NORMAL IAW B727 MAINTENANCE MAN UAL CHAPTER 3350106. 2 L 7 3 4F RT A3WE 1998100900929 19981009 00929 NM 1998 10 9 SCNA98119 1 19981006 A 3350 LIGHT BOEING 727 727225 1384077 NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE AT ROW 12 THRU 16. REPA IRED WIRES ON THE FLOOR TRACK LIGHTING AT ROW 12. EMERGENCY FLOOR TRACK LIGHTING CHECKS NORMAL. 2 L 7 3 4F A3WE 1998100900930 19981009 00930 NM 1998 10 9 SCNA98120 1 19981003 A 3350 900835A BATTERY PACK BOEING 727 727282 138408T NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE LEFT NR 2 LEFT OVERWING EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMO VED AND REPLACED THE NR 2 LEFT OVERWING EXTERIOR EMERGENCY LIGHT BATTERY PACK. OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1998100900931 19981009 00931 WP 1998 10 9 DHL98802002 1 19980926 A 3230 37591261 BOLT DOUG DC8 DC873F 302199F WP RT MLG SHEARED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 802DH 46076 ON S/O PREFLIGHT, FOUND RT MAIN LANDING GEAR OVER CENTER ARM ATTACH FITTING SHEARED OFF AND MISSING. INSTALLED UNIVERSA L LINK BOLT PER DC-8 MM 32-11-1. 2 L 7 4 4F RT 4A25 1998100900932 19981009 00932 WP 1998 10 9 DHL98805003 1 19981004 A 5730 SKIN DOUG DC8 DC873F 302199F WP RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 SKIN CRACK ON RT WING 14 INBOARD OF NR 4 PYLON. REPAIRED PER DACO S/B 57-100. 2 L 7 4 4F RT 4A25 1998100900933 19981009 00933 NM 1998 10 9 DHL9870801C 1 19980903 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 480-620 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, MAIN CABIN SEAT TRACK 24L HAS CORROSION. REMOVED SEAT TRACK FROM STA 480 TO 620 AND INSTALLED NEW PER SRM 5 1-30-2. N/R 3142 2 L 7 3 4F A3WE 1998100900934 19981009 00934 NM 1998 10 9 DHL9870802C 1 19980903 A 5330 SKIN BOEING 727 72725 1384006 NM BS 259.5 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, CORROSION AT BONDED SKIN DOUBLER AT BS 259.5 BETWEEN STRINGERS 3R TO 5R. CUT OUT DAMAGED AREA FROM STR 3R T O 7R. INSTALLED DOUBLER PER S/B 53-084. FILLER 3 X 3, DOUBLER 8 X 12. N/R 3154 2 L 7 3 4F A3WE 1998100900935 19981009 00935 NM 1998 10 9 DHL9870803C 1 19980903 A 5330 SKIN BOEING 727 72725 1384006 NM BS 259.5 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, CORROSION AT BONDED DOUBLER AT BS 259.5 BETWEEN STR 7 AND 8 RT. CUT OUT DAMAGED AREA , INSTALLED DOUBLER RE PAIR PER S/B 53-0084. FILLER 3 X 20, 8 X 25 DOUBLER. N/R 3155. 2 L 7 3 4F A3WE 1998100900936 19981009 00936 NM 1998 10 9 DHL9870804C 1 19980903 A 5330 SKIN BOEING 727 72725 1384006 NM BS 259 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, CORROSION PRESENT BS 259 BONDED SKIN DOUBLER AT STR 9L. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA, INST ALLED FILLER 5 X 4 AND DOUBLER 9 X 6 PER SRM 51-20-4. N/R 3156 2 L 7 3 4F A3WE 1998100900937 19981009 00937 NM 1998 10 9 DHL9870805C 1 19980902 A 5320 SUPPORT BOEING 727 72725 1384006 NM BS 630 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, C-1 CARGO COMPT FLOOR PANEL SUPPORT BOARD UNDERSIDE IS CORRODED AT RBL 13 APPROX STA 630. REMOVED SEAT TRA CK FROM BS 600 TO 720 PER SRM 51-30-2. REPLACED SEAT TRACK PER SRM 51-30-2. N/R 4512 2 L 7 3 4F A3WE 1998100900938 19981009 00938 NM 1998 10 9 DHL9870806C 1 19980903 A 7110 COWL BOEING 727 72725 1384006 NM NR 2 ENGINE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, NR 2 ENGINE INTAKE COWL HAS SKIN AND ANGLE CRACKED AT LOWER LT SIDE STA 1148. INSTALLED SKIN REPAIR AND RE PLACED ANGLE PER SRM 54-10-3, 6 X 3.5, DOUBLER 12 X 6, ANGLE 12 X 1 X 1. N/R 4538 2 L 7 3 4F A3WE 1998100900939 19981009 00939 NM 1998 10 9 DHL9870807C 1 19980902 A 7110 COWL BOEING 727 72725 1384006 NM NR 3 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, NR 3 ENGINE UPPER COWLING EXTERIOR SKIN DENTED ON TOP. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 6 X 1 0 PER SRM 54-10-3. N/R 6289 2 L 7 3 4F A3WE 1998100900940 19981009 00940 NM 1998 10 9 DHL9870808C 1 19980902 A 7110 COWL BOEING 727 72725 1384006 NM NR 2 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, NR 2 ENGINE RT AFT COWLING SKIN SURFACE HAS SEVERAL DENTS AND SCRATCHES. INSTALLED REPAIR AT OIL CANNING DE NT PER SRM 54-10-3, 6 X 5. N/R 6306 2 L 7 3 4F A3WE 1998100900941 19981009 00941 NM 1998 10 9 DHL9870809C 1 19980902 A 7110 COWL BOEING 727 72725 1384006 NM NR 3 ENGINE CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, NR 3 ENGINE LOWER COWLING SKIN SURFACE HAS BULGE. CUT OUT DAMAGED AREA, INSTALLED SKIN REPAIR PER SRM 54-10 -3, DOUBLER 15 X 14. N/R 6325 2 L 7 3 4F A3WE 1998100900942 19981009 00942 NM 1998 10 9 DHL9870810C 1 19980902 A 5330 SKIN BOEING 727 72725 1384006 NM BS 420 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FUSE SKIN CRACKED AT BS 420, STR 25R AT FASTENER. CUT OUT DAMAGED AREA, INSTALLED EXTERNAL DOUBLER REPAIR A T FUSELAGE SKIN PER SRM 53-30-3, 11 X 10. N/R 3069 2 L 7 3 4F A3WE 1998100900943 19981009 00943 NM 1998 10 9 DHL9870811C 1 19980902 A 5330 SKIN BOEING 727 72725 1384006 NM BS 420 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FUSE SKIN CRACKED AT FASTENER BS 420 STR 25L. CUT OUT DAMAGED AREA, HFEC OF AREA, INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 7 X 9. N/R 3070 2 L 7 3 4F A3WE 1998100900944 19981009 00944 NM 1998 10 9 DHL9870812C 1 19980902 A 5315 FLOORBEAM BOEING 727 72725 1384006 NM BS 303 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FWD LAV AREA AT STA 303, RBL 48 HAS A CRACKED SUPPORT FLOOR. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51 -40-3, 8 X 2.5. N/R 3093 2 L 7 3 4F A3WE 1998100900945 19981009 00945 NM 1998 10 9 DHL9870813C 1 19980902 A 5320 WEB BOEING 727 72725 1384006 NM LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, LT MLG WW WEB CRACKED AT LOWER FWD I/B CORNER. STOP DRILLED CRACK, PERFORMED HFEC, INSTALLED WEB REPAIR DO UBLER PER SRM 51-40-2, 8 X 6. ALSO, FOUND ANGLE CRACKED. REPAIRED PER SRM 51-40-4, 7 X 7. N/R 3097 2 L 7 3 4F A3WE 1998100900946 19981009 00946 NM 1998 10 9 DHL9870814C 1 19980903 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 564 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, MAIN CABIN SEAT TRACK HAS AREA OF LIGHT CORROSION AT BS 564 48 L. REMOVED CABIN SEAT TRACK LBL 48 FROM ST A 500 TO 580. INSTALLED PER SRM 53-10-5. N/R 3135 2 L 7 3 4F A3WE 1998100900947 19981009 00947 NM 1998 10 9 DHL9870815C 1 19980903 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 600 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, MAIN CABIN SEAT TRACK HAS SPOTS OF CORROSION AT BS 600 48L. REMOVED AND REPLACED SEAT TRACK PER SRM 51-30-2 FROM BS 580 TO 620. N/R 3141 2 L 7 3 4F A3WE 1998100900948 19981009 00948 NM 1998 10 9 DHL9870816C 1 19980903 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 610 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, CABIN SEAT TRACK HAS CORROSION AT BS 610 48L. REMOVED AND REPLACED SEAT TRACK FROM BS 580 TO 620 PER SRM 5 3-10-5. N/R 3142 2 L 7 3 4F A3WE 1998100900949 19981009 00949 NM 1998 10 9 DHL9870817C 1 19980903 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 540 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, MAIN CABIN SEAT TRACK HAS SPOTS OF CORROSION FROM BS 510 TO BS 540 24L. REMOVED AND REPLACED SEAT TRACK FRO M 480- 620 PER SRM 51-30-2. N/R 3147 2 L 7 3 4F A3WE 1998100900950 19981009 00950 NM 1998 10 9 DHL9870818C 1 19980902 A 5320 WEB BOEING 727 72725 1384006 NM BS 1238 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, AFT AIRSTAIR RT TORQUE HAS CRACK AT LIGHTENING HOLE AT STA 1238. STOP DRILLED CRACK, INSTALLED DOUBLER REPA IR PER SRM 51-40-2, 6 X 8. N/R 3047 2 L 7 3 4F A3WE 1998100900951 19981009 00951 NM 1998 10 9 DHL9870819C 1 19980902 A 5330 SKIN BOEING 727 72725 1384006 NM FUSELAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, AFT AIRSTAIR EXT SKIN REPAIR AT APPROX 12 INCHES FWD RT ACCESS PANEL HAS PREVIOUS REPAIR. CUT OUT DAMAGED A REA, INSTALLED DOUBLER AND FILLET PER SRM 51-30-2, 2' X 16. N/R 3053 2 L 7 3 4F A3WE 1998100900952 19981009 00952 NM 1998 10 9 DHL9870820C 1 19980902 A 5330 SKIN BOEING 727 72725 1384006 NM BS 259 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, BUTT JOINT BS 259 AFT PANEL INDICATES OVER 10 PERCENT MATERIAL LOSS BETWEEN STRINGER 21R TO 23R. CUT OUT DA MAGED SECTION, INSTALLED REPAIR PER S/B 53-0084. N/R 3043 2 L 7 3 4F A3WE 1998100900953 19981009 00953 NM 1998 10 9 DHL9870821C 1 19980902 A 5711 SPAR BOEING 727 72725 1384006 NM WS 330 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, LEFT WING UPPER FRONT SPAR SKIN FOUND CORROSION AROUND LEADING EDGE ATTACHMENT SCREWS AT WS 330. REMOVED CO RROSION OUT OF LIMITS. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-30-4, 16.75 X 2. N/R 1641 2 L 7 3 4F A3WE 1998100900954 19981009 00954 NM 1998 10 9 DHL9870822C 1 19980903 A 5712 RIB BOEING 727 72725 1384006 NM WS 260 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT CHECK, RT WING HAS CRACK AT L/E RIB STA 260 FASTENER UPPER COVE AREA INSIDE. REMOVED ANGLE REPAIR, STOP DRILLED, HFE C INSPECTION, INSTALLED REPAIR PER SRM 51-40-3. N/R 2381 2 L 7 3 4F A3WE 1998100900955 19981009 00955 NM 1998 10 9 DHL9870823C 1 19980902 A 5330 SKIN BOEING 727 72725 1384006 NM BS 360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, BUTT JOINT BS 360 AFT PANEL INDICATED 10 PERCENT MATERIAL LOSS. CUT OUT CORRODED AREA AT BS 360 FROM STRING ER 10R AND INSTALLED REPAIR PER S/B 53-0084 23.5 X 7.75. N/R 3045 2 L 7 3 4F A3WE 1998100900956 19981009 00956 NM 1998 10 9 DHL9870824C 1 19980903 A 5712 RIB BOEING 727 72725 1384006 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, RT WING L/E RIB O/B SIDE SLAT STA 0.260 HAS SEVERAL CRACKS IN REPAIR ANGLE. REPLACED ANGLE 16 X 1 X 1 PER S RM 51-10-1. N/R 2386 2 L 7 3 4F A3WE 1998100900957 19981009 00957 NM 1998 10 9 DHL9870825C 1 19980831 A 5330 SKIN BOEING 727 72725 1384006 NM BS 1130 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FUSELAGE UPPER SKIN FROM BS 1130 TO BS 1183 STR 3L TO 4L IS BULGED AT ATTACH FASTENERS. CUT OUT DAMAGED ARE A 3 X 1.5. INSTALLED FLUSH REPAIR PER SRM 53-30-3, 12 X 8. N/R 3010 2 L 7 3 4F A3WE 1998100900958 19981009 00958 NM 1998 10 9 DHL9870826C 1 19980902 A 5320 TEAR STRAP BOEING 727 72725 1384006 NM BS 680 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, FUSELAGE SKIN TEAR STRAP AT STA 680 JUST ABOVE STR 4R TO JUST BELOW STR 2R HAS DELAMINATION INDICATIONS. CU T OUT DAMAGED SECTION OF TEAR STRAP AND REINSTALLED NEW SECTION PER SRM 53-30-1, 16' X 3. N/R 3068 2 L 7 3 4F A3WE 1998100900959 19981009 00959 NM 1998 10 9 DHL9870827C 1 19980903 A 5720 WEB BOEING 727 72725 1384006 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, RT WING LOWER L/E ANGLE TO WEB CRACKED 2 PLACES WBL 92.8. INSTALLED ANGLE REPAIR PER SRM 51-40-3, 25 X 2 X 2. N/R 2375 2 L 7 3 4F A3WE 1998100900960 19981009 00960 NM 1998 10 9 DHL9870828C 1 19980903 A 5720 ANGLE BOEING 727 72725 1384006 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, RT WING I/B L/E COVE WBL 92.8 ANGLE REPAIR JUST BELOW TOP SKIN CRACKED. REMOVED ANGLE AND REPLACED PER SRM 51-30-2, 16 X 6. N/R 2374 2 L 7 3 4F A3WE 1998100900961 19981009 00961 NM 1998 10 9 DHL9870829C 1 19980903 A 5720 ANGLE BOEING 727 72725 1384006 NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, L/W LE SLAT FRONT SPAR CAVITY UPPER WEB SUPPORT ANGLE IS CRACKED AT UPPER CORNER WS 344. REMOVED AND REPLA CED SUPPORT ANGLE PER SRM 51-10-1, 3 X 18. N/R 1696 2 L 7 3 4F A3WE 1998100900962 19981009 00962 NM 1998 10 9 DHL9870830C 1 19980903 A 5754 SLAT BOEING 727 72725 1384006 NM NR 4 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, LEFT WING NR 4 L/E SLAT HAS SMALL CRACK AT VERTICAL SUPPORT STRAP NEXT TO ACTUATOR LOWER END AND I/B SIDE. I NSTALLED ANGLE REPAIR PER SRM 51-40-3, 1 X 1 X 9.5. N/R 1694 2 L 7 3 4F A3WE 1998100900963 19981009 00963 NM 1998 10 9 DHL9870831C 1 19980901 A 5712 RIB BOEING 727 72725 1384006 NM WS 601.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, INSPECTED LOWER RIB CHORDS AT WS 601.5 PER S/B 57-0127. FOUND LOWER FLANGE OF RIB CRACKED AT STR 8. STOP DRILLED AND INSTALLED ANGLE REPAIR PER SRM 57-10-5, 22.5 X 2. N/R 1615 2 L 7 3 4F A3WE 1998100900964 19981009 00964 NM 1998 10 9 DHL9870832C 1 19980903 A 5347 SEAT TRACK BOEING 727 72725 1384006 NM BS 535 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, CENTER SEAT TRACK STA 535 TO 555 LT CORRODED AND WORN. REPLACED CENTER SEAT TRACK FROM 440 TO 560 PER SRM 51-30-2. N/R 5597 2 L 7 3 4F A3WE 1998100900965 19981009 00965 NM 1998 10 9 DHL9870833C 1 19980903 A 2761 659892433 ANGLE BOEING 727 72725 1384006 NM NR 2 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, VERTICAL ANGLE CRACKED AT NR 2 SPOILER I/B ACTUATOR SUPPORT CASTING LOWER MOUNT HOLE. REMOVED AND INSTALLED NEW VERTICAL ANGLE PER SRM 57-10-1. N/R 1653 2 L 7 3 4F A3WE 1998100900966 19981009 00966 NM 1998 10 9 DHL9870834C 1 19980902 A 2761 ANGLE BOEING 727 72725 1384006 NM WS 224 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, R/W WS 224 COVE PANEL ANGLE CRACKED BELOW NR 8 SPOILER ACTUATOR. REMOVED AND REPLACED ANGLE PER SRM 51-30-2 , 9 X 4. N/R 2356 2 L 7 3 4F A3WE 1998100900967 19981009 00967 NM 1998 10 9 DHL9870835C 1 19980902 A 2520 PANEL BOEING 727 72725 1384006 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, THREE LARGE CRACKS IN DITCHING PANELS ABOVE BS 1183 REINFORCEMENT DOUBLER RBL 26 TO 46. REMOVED DITCHING PA NELS, INSTALLED NEW WEBS PER SRM 51-30-2, 10 X 6. N/R 3036 2 L 7 3 4F A3WE 1998100900968 19981009 00968 NM 1998 10 9 DHL9870836C 1 19980908 A 5712 RIB BOEING 727 72725 1384006 NM WS 546 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, RT WING LOWER RIB ANGLE CRACKED AT 3RD FROM AFT STRINGER BOLT HOLE. STOP DRILLED CRACK, HFEC, REPLACED WING RIB PER S/B 57-0127. N/R 2455 2 L 7 3 4F A3WE 1998100900969 19981009 00969 NM 1998 10 9 DHL9870837C 1 19980908 A 5712 RIB BOEING 727 72725 1384006 NM WS 546 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, STA 546 RT WING RIB LOWER ANGLE CRACKED AT SECOND FROM FWD STR BOLT HOLE. STOP DRILLED CRACK, HFEC, REMOVED AND REPLACED RIB PER S/B 57-0127. N/R 2454 2 L 7 3 4F A3WE 1998100900970 19981009 00970 NM 1998 10 9 DHL9870838C 1 19980908 A 5312 BULKHEAD BOEING 727 72725 1384006 NM BS 1183 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 708DH 18275 AT C-CHECK, INSPECTED BEAM AT 1183 BULKHEAD, WL 250. REMOVED PREVIOUS REPAIR AT LT PRESS BEAM BL 45. INSPECTED PREVIOU S STOP DRILL, INSTALLED REPAIR KIT PER S/B 53-005 PART 3. N/R 3173 2 L 7 3 4F A3WE 1998100900971 19981009 00971 NE 1998 10 9 TC8A98067 2 19981007 A 7200 ENGINE DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 1 FAILED A TC8A E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 23 184SK 43582 2122 45981 643960 DFW-DAY. TRIP# 02617 DISCREP: #1 ENGINE LOSS OF POWER ON CLIMBOUT 240-330. ENGINE SURGING FROM CLIMB EPR TO 1.6 THEN 1.3 SHUTDOWN, ALL PARAMETERS NORMAL. FERRIED AIRCRAFT TO KMIA. CORR. ACTION: 10/28/98 REMO VED AND REPLACED #1 ENGINE IAW MIP CHAPT 2, P.77 THRU 80 AND PAGE 99,100, OPS CHECKS NORMAL. 2 L 7 4 4F 4 F 4A25 1E8 1998100900972 19981009 00972 WP 1998 10 9 CKSA98540 1 19981002 A 2120 AIR DISTR LKHEED 1011 1011385115 5265015 WP COCKPIT ODOR A CKSA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 107CK 193N1182 ELECTRICAL ODOR COMNG FROM FEDC AREA. ODOR DIMINISHED WHEN FLT STATION COURIER AND AFT CABIN TEMP CONTROLS WERE UNLATCH ED. INSPECTED FLIGHT DECK, FWD AND AFT FESC AND MESC, COCKPIT LIGHTING AND ECS SYSTEM FOR ELECTRICAL MALFUNCTIONS AND S ECURITY. NO DEFECTS NOTED AT THIS STATION IAW L-1011 GENERAL PRACTICES. 2 L 7 3 4F A23WE 1998101400001 19981014 00001 NM 1998 10 14 UPS98627705 1 19980924 A 2612 FIRE WARNING BOEING 767 76734AF 1385212 NM COCKPIT ILLUMINATED A IPXA O OTHER N FALSE WARNING LD LANDING 1 SO 01 317UP 27745 INSPECTION TYPE-N/A, FIRE WARNING LIGHT DISPLAYED ON LANDING AND TAXI IN. NO DISPLAY IN THE FIRE HANDLE OR EICAS DISPLA Y. PERFORMED ENG/APU/CARGO FIRE BOTTLE BITE TEST PROCEDURE PER BIT MANUAL 26-2 LIGHT EXT. NO DEFECTS NOTED. 2 L 7 2 4F RT A1NM 1998101400002 19981014 00002 EU 1998 10 14 98ZZZM693 1 19980129 A 5741 BOLT BAG BAE146 BAE146200A 1500266 EU FR 29 LT WRONG PART A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 156TR E2156 LEFT FRAME 29 WING TO FUSELAGE LUG ATTACH BOLT DIFFERENT TYPE FASTENER INSTALLED AND DOES NOT HAVE ANY MARKINGS ON HEAD OF BOLT. REPORTED DETAILS TO BAE RDO, THE OVERSIZE BOLT FOUND AT FR 29 LEFT HYLT STRINGER NR 12 POSITION WAS INSTALLED AT BUILD. (M) 2 H 7 4 4F RT A49EU 1998101400003 19981014 00003 EU 1998 10 14 C2XA98BT056 1 19980806 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU FUSELAGE INOPERATIVE A C2XA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 09 14834 193 UPPER EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY AT 3WL. (M) 2 H 7 2 4T RT A53EU 1998101400004 19981014 00004 EU 1998 10 14 C2XA98BT057 1 19980807 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42300 8680920 EU FUSELAGE INOPERATIVE A C2XA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 09 16824 166 DURNG 2A INSPECTION IN BTV, FOUND EMERGENCY POWER SUPPLY UNIT AT 10WL INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY IN 10WL. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998101400005 19981014 00005 EA 1998 10 14 JBXA980051 1 19980928 A 5270 WARNING LIGHT CNDAIR CL600 CL6002B19 EA COCKPIT ILLUMINATED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 574ML 7242 PASSENGER DOOR LIGHT ILLUMINATED AT 4,000 FEET. OPS CHECKED DOOR ON GROUND AT CHS IAW MM REF NR 52-11-00. DOOR OPS CHE CKED GOOD. NO KNOWN DISCREPANCY FOUND. (X) 2 L 7 2 4F RT A21EA 1998101400006 19981014 00006 NM 1998 10 14 DL72L981973 1 19980923 A 2520 TRIM BOEING 727 727232 1384082 NM PAX DOOR OUT OF POSITION A DALA K NONE O OTHER CL CLIMB 1 SO 27 506DA 21308 A/C UNABLE TO PRESSURIZE. FOUND A PIECE OF INTERIOR TRIM BETWEEN DOOR SEAL AND A/C FRAME. REPOSITIONED TRIM, ALL OPS N ORMAL. 2 L 7 3 4F A3WE 1998101400007 19981014 00007 NM 1998 10 14 DL72L981978 1 19980922 A 5240 65569923 FITTING BOEING 727 727232 1384082 NM LT SERVICE DOOR WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 508DA 21310 FITTING WORN ON LT AFT SERVICE DOOR AFT LOWER EDGE OF DOOR. C/W MM 52-14-0 FIG 805. 2 L 7 3 4F A3WE 1998101400008 19981014 00008 1998 10 14 DLM90981980 4 19980925 A 2565 100504201 SLIDE DOUG MD90 MD9030 3023690 NM GALLEY DOOR DEPLOYED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 915DN 53395 R1 DOOR SLIDE ACCIDENTLY DROPPED OUT OF DOOR CRADLE AND DEPLOYED. REPLACED DOOR SLIDE PER M/M. 2 L 7 2 4F RT A6WE 1998101400009 19981014 00009 NM 1998 10 14 DL73E981988 1 19980921 A 5311 90526911 FRAME BOEING 737 737247 138448D NM BS 767 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 237WA 23185 A CRACK WAS FOUND DURING ACCOMPLISHMENT OF DAL EO 3-60725-3 AND WAS NOT TYPICAL. THE CRACK WAS IN THE WEB OF THE FRAME. REPAIRED PER ERA 332245-14. 2 L 7 2 4F A16WE 1998101400010 19981014 00010 NM 1998 10 14 DL72W981996 1 19980927 A 7312 HEAT VALVE 320115 BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A DALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 294WA 25504 22112 687345 NR 3 ENGINE OIL TEMPERATURE ROSE TO YELLOW BAND RANGE. FOLLOWED POM PROCEDURES FOR HIGH OIL TEMPERATURE. SHUTDOWN NR 3 ENGINE ACCORDING TO CHECKLIST PROCEDURES. REPLACED NR 3 ENGINE FUEL HEAT VALVE. LEAK AND FUNCTION CHECKS OK. INSPECT ED ENGINE FOR OIL TEMP CONDITION AND WINDMILL CONDITION. ALL OPERATIONS CHECKS OK PER MAINTENANCE MANUAL. 2 L 7 3 4F 4 F A3WE E2EA 1998101400011 19981014 00011 1998 10 14 98UAL900461 4 19980919 A 2565 SLIDE BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE RT WING DEPARTED A UALA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 WP 29 667UA 29239 RIGHT WING SLIDE DEPARTED ON TAKEOFF. 2 L 7 2 4F 4 F RT A1NM E24NE 1998101400013 19981014 00013 NM 1998 10 14 VNAA9809016 1 19980920 A 3610 4069B000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 429JS 42365 3043 A CROSS BLEED FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MA INTENANCE INSPECTED AND REPLACED THE CROSSBLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERATIO NAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101400014 19981014 00014 WP 1998 10 14 VJ9800411 1 19980921 A 3260 5910161118 INDICATION DOUG DC9 DC932 3022066 WP MLG DOOR MALFUNCTIONED A ZZDA O OTHER N FALSE WARNING CR CRUISE 1 SO 15 918VV 47320 GEAR DOOR OPEN LIGHT ON WITH LANDING GEAR INDICATING DOWN AND LOCKED. 2 L 7 2 4F A6WE 1998101400015 19981014 00015 WP 1998 10 14 VJ9800415 1 19980918 A 3260 5910161118 UNSAFE LIGHT DOUG DC9 DC932 3022066 WP MLG DOOR ILLUMINATED A ZZDA K NONE N FALSE WARNING CL CLIMB 1 SO 15 918VV 47320 LT GEAR UNSAFE LIGHT ILLUMINATED AFTER T/O WITH GEAR HANDLE UP, WHEN GEAR HANDLE PUT BACK DOWN, GEAR DOOR LIGHT ILLUMINA TED. 2 L 7 2 4F A6WE 1998101400016 19981014 00016 1998 10 14 VJ9800416 4 19980920 A 2565 1362122DME SLIDE DOUG DC9 DC932 3022066 WP TAIL CONE CONTAMINATED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 967VV 47170 TAIL CONE EVAC SLIDE ASSY SATURATED WITH FOREIGN MATERIALS. REMOVED AND REPLACED TAIL CONE SLIDE ASSY. 2 L 7 2 4F A6WE 1998101400017 19981014 00017 NM 1998 10 14 98UAL900458 1 19980915 A 3350 LIGHT BOEING 747 747238B 1384828 NM PWA JT9 JT9D7J 52054 NE CABIN INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 159UA 21140 CROSS AISLE EEL STRIP AT FORWARD GALLEY INOP. REPLACED EMERGENCY LIGHT STRIP AND RESECURED IN PLACE. OPERATIONAL CHECK GOOD. 2 L 7 4 4F 4 F A20WE E20EA 1998101400018 19981014 00018 NM 1998 10 14 98UAL900459 1 19980911 A 3150 EICAS HONEYWELL 3163HNP00304 BOEING 777 777222 1385219 NM PWA 4090 PW4090 NE LT COCKPIT MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 792UA 26934 EN ROUTE CDG TO IAD, LOWER EICAS DISPLAY BLINKING AND INDICATED ALTITUDE ON CAPTAIN'S PFD (PRIMARY FLIGHT DISPLAY) DROPS ALONG WITH CABIN ALTITUDE. FLIGHT DIVERTED TO LHR. AFTER INVESTIGATION OF THE CORE PROCESSING MODULE/GRAPHICS GENERAT OR BY BOTH BOEING AND HONEYWELL, RESULTS SHOW THAT THE UNIT HAD NUMEROUS POWER RESETS. BOEING AND HONEYWELL ARE REVISIN G THE AIMS CORE SOFTWARE TO PROVIDE FUTURE PROTECTION AGAINST THIS TYPE OF FAILURE. WITH THE NEW SOFTWARE, THIS TYPE OF FAILURE WOULD CAUSE THE CPM/GG TO SHUT DOWN AND PREVENT ERRONEOUS FLIGHT DECK EFFECTS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998101400019 19981014 00019 NM 1998 10 14 UPS98427691 1 19980920 A 3350 BATTERY PACK BOEING 747 747212B 1384886 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 520UP 21943 INSPECTION TYPE-N/A, TWO AFT EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACKS, OPS CHECK GOOD. 2 L 7 4 4F A20WE 1998101400020 19981014 00020 NM 1998 10 14 P5CA9801477 1 19980918 A 5330 SKIN BOEING 747 747283B 1384867 NM BS 680 DENTED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 FUSELAGE DENTED AFT OF FORWARD CARGO DOOR STATION 680. FABRICATED DOUBLER AND INSTALLED PER SRM 53-30-03. 2 L 7 4 4F A20WE 1998101600035 19981016 00035 NM 1998 10 16 P2EA98160 1 19980819 A 3260 WARNING SYSTEM BOEING 737 737247 138448D NM MLG ACTIVATED A P2EA O OTHER N FALSE WARNING CR CRUISE 1 CE 05 912MP 19607 FLT 8189 - MCI - NO EMERGENCY DECLARED LANDING UNEVENTFUL. NOSE GEAR RED LIGHT WAS ILLUMINATED IN FLIGHT. GEAR EXTENSI ON NORMAL. UNABLE TO BURN FUEL OUT OF CENT TANK WITH LEFT BOOST PUMPS ON. (M) 2 L 7 2 4F A16WE 1998101600036 19981016 00036 NM 1998 10 16 98ZZZX3701 1 19980819 A 2822 CHECK VALVE BOEING 737 737247 138448D NM LT BOOST PUMP WRONG PART A P2EA O OTHER N FALSE WARNING NR NOT REPORTED 1 CE 05 912MP 19607 MCI - FLT 8189 - NOSE GEAR RED LIGHT WAS ILLUMINATED IN-FLIGHT. GEAR EXTENSION NORMAL. FOUND UPLOCK TARGET MISSING. I NSTALLED TARGET AND ADJUSTED SENSOR, PERFORMED GEAR SWING, OPS CHECK NORMAL PER MM 32-61-41. UNABLE TO BURN FUEL OUT OF CENTER TANK WITH LEFT BOOST PUMPS ON. FOUND WRONG P/N INSTALLED IN LEFT CENTER BOOST PUMP CHECK VALVE. INSTALLED CORR ECT BOOST PUMP CHECK VALVE PER MM 28-22-71. REF: OPERATOR CONTROL NR P2EA98160. 2 L 7 2 4F A16WE 1998101600037 19981016 00037 NE 1998 10 16 SABA290041 3 19980813 A 6111 BLADE DHAV DHC8 DHC8102 2809003 NM HAMSTD 14SF 14SF23 NE RT PROPELLER BIRD STRIKE A SABA O OTHER O OTHER DE DESCENT 1 SO 33 817PH 56 GNV/CLT - FLT 5061 - UPON ARRIVAL INTO THE CHARLOTTE AREA, PILOT REPORTED HE TOOK A SMALL BIRD STRIKE ON THE RIGHT PROPE LLER. NO IN-FLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED AT CHARLOTTE WITH NO OTHER PROBLEMS. MAINTENANCE COMPLETED A BIRD STRIKE INSPECTION. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 6 C P7NE 1998101600038 19981016 00038 NM 1998 10 16 98ZZZX3702 1 19980710 A 5310 STRUCTURE BOEING 727 727223 1384074 NM BS 178-209 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 867AA 21372 TUL - AIRCRAFT SUSTAINED DAMAGE TO RADOME AND WRINKLES TO LT FUSELAGE. STA 178 TO STA 208, STR 17L TO STR 24L. SUSPECT AFT AIRSTAIR OUT OF RIG. REPAIRED RADOME, FUSELAGE DAMAGE. REPAIRED PER SRM 53-30-3. RIGGED AND ADJUSTED VENTRICAL S TAIR PER MM. ALL WORK ACCOMPLISHED ON W.O. NR 320 DATED 7-1-98. TULSA BOW 320-71-98. REF: OPERATOR CONTROL NR AALA98 1360. 2 L 7 3 4F A3WE 1998101600039 19981016 00039 WP 1998 10 16 G6OA024 1 19980701 A 3620 DC26F18325 CONNECTOR DOUG DC10 DC1030 3023501 WP NR 2 ENGINE LOOSE A G6OA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 605GC 47925 THE FLIGHT CREW REPORTED THE NR 2 ENGINE PNEUMATIC MANIFOLD FAILURE LIGHT ILLUMINATED. ACCOMPLISHED EMERGENCY PROCEDURE S PER AOM VOL 1. GROUND MAINTENANCE TROUBLESHOT THE SYSTEM. PERFORMED MANIFOLD DETECTION TEST PER MM 36-23-00. TESTED WITH NO FAULTS FOUND. FOUND DETECTION CONTROLLER CANNON PLUG LOOSE. CLEANED AND SECURED CANNON PLUG. (X) 2 L 7 3 4F A22WE 1998101600040 19981016 00040 NM 1998 10 16 98ZZZX3703 1 19980828 A 3010 320115 VALVE BOEING 727 72751C 1384015 NM NR 2 ENGINE LEAK A RYNA A E UNSCHED LANDING ENGINE SHUTDOWN N Y FALSE WARNING ENGINE STOPPAGE CL CLIMB 1 CE 07 436EX 19289 PHX/LAX - FLT 643 - ENGINE FIRE INDICATION ON CLIMB-OUT NR 2 ENGINE. SHUT DOWN NR 2 ENGINE, RETURNED TO PHX. 2 L 7 3 4F A3WE 1998101600041 19981016 00041 EU 1998 10 16 98ZZZX3704 2 19980819 A 7320 EU30764A T1 CANISTER GULSTM G1159 G1159 3953505 SO RROYCE SPEY SPEY5118 54523 EU LT ENGINE CRACKED A KKYA K NONE O OTHER IN INSP/MAINT 1 NE 03 220JR 50 8649 DURING A ROUTINE INSPECTION, A CRACK WAS FOUND AT THE BASE OF THE CAPILLARY TUBE MOUNT BOSS ON THE T1 CANISTER OF THE LE FT HAND ENGINE. THE CRACKED PART WAS REMOVED AND A SERVICEABLE UNIT WAS INSTALLED IAW ROLLS ROYCE MAINTENANCE MANUAL, C HAPTER 75. THERE HAD BEEN NO REPORTED OPERATIONAL PROBLEMS AS A RESULT OF THIS FAILURE. AIRCRAFT WAS RETURNED TO SERVI CE. 2 L 7 2 4F 4 F RT A12EA E2EU 1998101600042 19981016 00042 WP 1998 10 16 AALA981462 1 19980802 A 2613 4TL1413D SENSORS DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT MALFUNCTIONED A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 423AA 49335 DFW - FLT T0071 - SHORTLY AFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. APU WAS NOT RUNNING. DUR ING PERFORMANCE OF CHECK LIST, THE LIGHT EXTINGUISHED. REPLACED LEFT AND RIGHT HIGH TEMPERATURE SENSORS IN TAIL. RAN E NGINES AT POWER FOR 5 MINUTES. NO LIGHT NOTED. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998101600043 19981016 00043 WP 1998 10 16 AALA981466 1 19980730 A 2150 SEAL DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT LOOSE A AALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 SW 07 423AA 49335 DFW - FLT T1969 - SHORTLY AFTER TAKEOFF, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. APU WAS RUNNING DUE TO LE FT GENERATOR INOPERATIVE. LIGHT EVENTUALLY EXTINGUISHED AFTER FOUR TO FIVE MINUTES. RETURNED DFW AND LANDED OVERWEIGHT AND WITHOUT INCIDENT. RE-SEATED LEFT HEAT EXCHANGER SEAL, RAN ENGINES AT TAKEOFF POWER WITH AND WITHOUT APU AIR. NO L EAKS NOTED, NO TEMPERATURE WARNING. PERFORMED OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998101600045 19981016 00045 WP 1998 10 16 VJ9800519 1 19981007 A 2560 11331 COVER DOUG DC9 DC932 3022066 WP R1 DOOR SLIDE LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 939VV 47089 GALLEY DOOR SLIDE COVER NEEDS TO BE REATTACHED. INSTALLLED SLIDE COVER IAW MM 25-62. PERFORMED REQUIRED INSPECTION. 2 L 7 2 4F A6WE 1998101600046 19981016 00046 WP 1998 10 16 VJ9800520 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 206.25-229 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 DENT .O45 INCHES IN DEPTH AT FS 206.25, L21 AND 22R, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. COLD WORKED AREA, FABRICAT ED, INSTALLED REPAIR IAW DC9 SRM 53-04, FIG 38 VIEW P, 51-10-3 AND MM 21-00. 2 L 7 2 4F A6WE 1998101600047 19981016 00047 WP 1998 10 16 VJ9800521 1 19981001 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 237-313 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 NR 46 FLOORBOARD AT FS 237-313, RBL 22-44, CORRODED BEYOND LIMIT IAW DC9 SRM 53-20-1, PG 201. FABRICATED AND INSTALLED NEW FLOORBOARD IAW DC9 SRM 53-20-1, PG 201, 53-01, FIG 1, 51-10-3 AND 53-20-0, FIG 3. 2 L 7 2 4F A6WE 1998101600048 19981016 00048 WP 1998 10 16 VJ9800522 1 19981008 A 3510 11442321 MASK DOUG DC9 DC932 3022066 WP RT COCKPIT BROKEN A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 931VV 47674 FIRST OFFICER'S OXYGEN MASK BROKEN. REPLACED FO OXYGEN MASK; OPS CHECKED GOOD IAW MM 35-10. 2 L 7 2 4F A6WE 1998101600049 19981016 00049 EU 1998 10 16 MALA976203 1 19981001 A 7603 FLIGHT IDLE SAAB SF340 340B 7860101 EU ENGINE OUT OF ADJUST A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 421XJ 421 FLIGHT IDLE STOP LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO DTW. MAINTENANCE INSPECTED SYSTEM FOUND FLIGHT IDLE STOP OVERRIDE BINDING SLIGHTLY OPEN, PULLED, CLEANED AND RESET SYSTEM. ALL CHECKS GOOD AT THIS TIME. 2 L 7 2 4T RT A52EU 1998101600050 19981016 00050 EU 1998 10 16 MALA976204 1 19981003 A 3350 7239410802 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 436XJ 436 DURING INSPECTION FLOOR PROXIMITY LIGHTING BETWEEN SEATS 2A AND 3A INOP. MAINTENANCE REPLACED LIGHTING STRIP FOR FLOOR PROXIMITY LIGHTING BETWEEN SEATS 2A AND 3A. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998101600051 19981016 00051 1998 10 16 MALA976205 4 19981004 A 3420 IRS SYST BAC 146 AVRO146RJ85A 1500097 EU E/E COMPT TRIPPED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 505XJ E2313 WHEN FLAPS WERE RETRACTED AFTER TAKE OFF FTC AND EL TRIM ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE CYCLED AVI ONICS MASTER SWITCHES, ALIGNED IRS SYSTEM AND TESTED EL TRIM SYSTEM AND FLAPS, ALL SYSTEMS CHECK OK. 2 H 7 4 4F RT A49EU 1998101600052 19981016 00052 EU 1998 10 16 MALA976206 1 19981002 A 5610 8103731 WINDSHEILD SAAB SF340 SF340A 7850100 EU LT COCKPIT DELAMINATION A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 112XJ 340A112 ON DEPARTURE FROM DTW CREW HEARD CRACKLING AND SAW LEFT FRONT WINDSHIELD DELAMINATION GROWING. AIRCRAFT RETURNED TO DTW . MAINTENANCE REPLACED CAPTAIN'S WINDSHIELD IAW SAABMM WINDSHIELD HEAT CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998101600053 19981016 00053 EU 1998 10 16 MALA976207 1 19981002 A 2435 23080031 STARTER GEN SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 991XJ 091 AFTER GEAR RETRACTION BOTH LEFT EFIS TUBES WENT BLACK, AFTER HYDRAULIC PUMP STOPPED RUNNING AND BOTH LEFT TUBES CAME BAC K. FIVE MINUTES INTO FLIGHT EFIS TUBES WENT BLACK AGAIN, FOLLOWED QRH, SHUTDOWN LEFT GENERATOR. AIRCRAFT RETURNED TO D TW. MAINTENANCE REPLACED LEFT STARTER/DC GEN. RAN AIRCRAFT, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998101600054 19981016 00054 NM 1998 10 16 CALA9801914 1 19981007 A 2910 65445101708 LINE BOEING 737 7372C0 1384488 NM NR 2 ENGINE CHAFED A CALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14241 20070 THE 'A' HYDRAULIC SYSTEM WAS LOST WHILE EN ROUTE TO EWR. THE GEAR AND FLAPS WERE LOWERED MANUALLY AND THE AIRCRAFT LAND ED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 ENGINE HYDRAULIC PRESSURE LINE IN WING ROOT CHAFED ON CLAMP. THE HY DRAULIC LINE WAS REMOVED AND REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED. THE ENGINE WAS RUN AND ALL FLIGHT CONTROLS W ERE CYCLED WITH OPERATION CHECKING GOOD AND NO LEAKS NOTED. 2 L 7 2 4F A16WE 1998101600055 19981016 00055 WP 1998 10 16 CALA9801916 1 19981007 A 2530 8101280000B OVEN DOUG DC9 DC982 3022082 WP GALLEY FAILED A CALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 938AS 49365 AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE FORWARD CABIN AREA WHILE EN ROUTE TO ATL. NO VISIBLE SMIKE WAS PRESENT. T HE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD GALLEY NR 2 OVEN HAD A BURNED MOTOR. THE OVE N WAS PLACARDED INOPERATIVE. 2 L 7 2 4F A6WE 1998101600056 19981016 00056 NM 1998 10 16 CALA9801917 1 19981007 A 5753 652130174 SKIN BOEING 727 727243 138408D NM RT TE FOREFLAP BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND RT INBOARD FOREFLAP BENT AT O/B TRAILING EDGE. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1. 2 L 7 3 4F RT A3WE 1998101600057 19981016 00057 NM 1998 10 16 CALA9801918 1 19981007 A 5752 652172641 TAB BOEING 727 727243 138408D NM LT AILERON BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND LT OUTBOARD AILERON TAB INBOARD END BENT. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41, PA GE 401-403. 2 L 7 3 4F RT A3WE 1998101600058 19981016 00058 NM 1998 10 16 CALA9801919 1 19981008 A 5755 6517348108A SKIN BOEING 727 727243 138408D NM NR 8 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND THE RT WING NR 8 SPOILER DELAMINATED. THE SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1, PAGE 401-40 4. 2 L 7 3 4F RT A3WE 1998101600059 19981016 00059 NM 1998 10 16 CALA9801920 1 19981007 A 5751 652172519 SKIN BOEING 727 727243 138408D NM LT AILERON DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 579PE 21662 INSPECTION FOUND THE LT OUTBOARD AILERON TRAILING EDGE DELAMINATED SIX INCHES FROM OUTBOARD END. THE PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998101600060 19981016 00060 NM 1998 10 16 CALA9801921 1 19981007 A 3350 BACC45FT1212S CONNECTOR AEROFLITE BOEING 727 727232 1384082 NM CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14788 20642 INSPECTION FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG SHORTED AT POWER SUPPL Y. THE PLUG WAS REPLACED AND EXIT LIGHT OPERATION WAS RESTORED. 2 L 7 3 4F A3WE 1998101600061 19981016 00061 NM 1998 10 16 CALA9801922 1 19981007 A 5753 FAIRING BOEING 727 727224 1384076 NM NR 5 FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .25 INCH CRACK AT BOLT HOLE OF NR 5 FLAP TRACK CENTER FAIRING. A REPAIR WAS INSTALLED IAW SRM 51-40- 2, 51-10-2, 51-40-2, 51-30-2, AND MM 51-20-11. 2 L 7 3 4F A3WE 1998101600062 19981016 00062 NM 1998 10 16 CALA9801923 1 19981008 A 5753 FAIRING BOEING 727 727224 1384076 NM WS 124 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND A .25 INCH CRACK IN LT WING NR 4 FLAP TRACK FAIRING AT WS 124. A DOUBLER WAS INSTALLED IAW SRM 51-40-2 , 51-10-2, MM 51-20-11. 2 L 7 3 4F A3WE 1998101600063 19981016 00063 NM 1998 10 16 CALA9801924 1 19981008 A 5230 SKIN BOEING 757 757224 1384958 NM CARGO DOOR DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58101 27291 INSPECTION FOUND A DENT IN AFT CARGO DOOR EXTERNAL SKIN AT LOWER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 52-30-01 , PAGE 209. 2 L 7 2 4F RT A2NM 1998101600064 19981016 00064 WP 1998 10 16 CALA9801925 1 19981008 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 275 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 275 BETWEEN LONGERON 17L TO 18L. A REPAIR WAS INSTALLED IAW ECRA 5330-0244 5. 2 L 7 2 4F A6WE 1998101600065 19981016 00065 WP 1998 10 16 UPS98827889 1 19980926 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C LT WING L/E SKIN UPPER SURFACE CRACKED BY 2EA FASTENERS AT STA XFS 610.000. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998101600066 19981016 00066 WP 1998 10 16 UPS98827890 1 19980927 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE:C LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER AT STA XFS 597.5. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998101600067 19981016 00067 WP 1998 10 16 UPS98827891 1 19980910 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 FS 1690 LONG 28L AND 32L END FITTINGS ARE CORRODED. REMOVED AND REPLACED FITTING L32L. REMOVED CORR OSION FROM L28L IAW D C8 SRM 51-1-8. ALODINED AND PRIMED. 2 L 7 4 4F RT 4A25 1998101600068 19981016 00068 WP 1998 10 16 UPS98827892 1 19980910 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1766 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 AFT FACE OF PRESSURE BULKHEAD STA 1766 1ST HORIZONTAL BEAM LT OF C ENTER BEAM FITTING HAS CORR. REMO VED DAMAGED FITTING DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998101600069 19981016 00069 WP 1998 10 16 UPS98827893 1 19980910 A 5320 BEAM DOUG DC8 DC871F 302199D WP BS 1600 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 IN AFT ACC COMP FLOORBEAM TO FUSELAGE FITTING LOWER ANGLE AFT SIDE AT FUSELAGE STA 1600 AND -X57 IS CRACKED AND CORRODED. REMOVED CORRODED FITTING AT STA 1600, RECIEVED NEW FITTING P/N 37510 62-506U AWR 50003. DRILLED AND DEBURRED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998101600070 19981016 00070 WP 1998 10 16 UPS98827894 1 19980928 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 590-582 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 RT WING LEADING EDGE LWR SURFACE BULGED XFS 590-582/FWD OF FWD SPAR. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FABBED INNER DOUBLER IAW DC8 ADDENDIUM 5720-4087-B. FABRICATED OUTER DOUBLER IAW DAC DWG 56 41225. INSTALLED DOUBLER IAW DC8 SRM 1-1-21. 2 L 7 4 4F RT 4A25 1998101600071 19981016 00071 NM 1998 10 16 98FDEA00638 1 19981007 A 7931 1163P182 SWITCH BOEING 727 727225 1384077 NM NR 1 ENG OIL FAILED A FDEA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 25 465FE 21289 98-243 AT CRUISE, FL 330, NR 1 OIL FILTER BYPASS LIGHT CAME ON WHEN THROTTLE WAS RETARD TO IDLE, LIGHT WENT OUT FOR APP ROX 2 MIN, THEN CAME BACK ON AND REMAINED ON. ENG WAS SHUT DOWN IN ACCORD WITH RED TAB. OIL TEMP AND PRESS & QUAN NORM . REMOVED AND REPLACED LOW OIL PRESS SWITCH AND RAN. OPER AND LEAK CK ON NR 1 ENG PER MM 79-33-0, AND JET RUN HANDBOOK . OPER CK GOOD. LEAK CK GOOD. 2 L 7 3 4F A3WE 1998101600072 19981016 00072 NM 1998 10 16 98FDEA00639 1 19981007 A 2613 LOOP BOEING 727 727225 1384077 NM NR 2 OUT OF POSITION A FDEA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING UK UNKNOWN 1 SO 25 464FE 21288 98-244 WITH RT PACK ON, RT NR 2 BLD OPEN, LT PK OFF AND ALL OTHER BLDS CLOSED. THE LWR AFT BODY O/H LIGHT CAME ON PER RED TABS. LIGHT WENT OUT WHEN NR 1 ENG BLD AND LT PK WERE OPEN/TURN ON RESPECTIVELY. FOUND LOOP PUSH DOWN CLOSE TO RT DUCT WORK. REPOSITION LOOP AND ATTACH POINT. OPER RT PK WITH DESCRIBE BLD SET AS ABOVE. OPER CK NORM. NO LEAKS DETEC T. 2 L 7 3 4F A3WE 1998101600073 19981016 00073 NM 1998 10 16 98FDEA00640 1 19981007 A 5320 651758863 BEAM BOEING 727 72722 1384002 NM BS 264 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 WHILE WORKING NR 424, FOUND CORROSION ON 25 G-BEAM AT BS 264, WL 208, RBL 8 TO BE OUT OF LIMITS. *S/D* REMOVED AND REP LACED 25 G-BEAM, BS 264, WL 208, LBL 18 TO RBL 26 IAW FED-EX DRAWING 65-17593 AND FED-EX SRM 51-30-2. 2 L 7 3 4F A3WE 1998101600074 19981016 00074 WP 1998 10 16 ABXA9800876 1 19981006 A 3260 LIGHT DOUG DC9 DC932 3022066 WP RT MLG MALFUNCTIONED A ABXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 980AX 47176 DURING LANDING GEAR RETRACTION, THE RIGHT GEAR UNSAFE (RED) LIGHT REMAINED ILLUMINATED. RECYCLED GEAR. NO CHANGE. GRE EN LIGHT REMAINED OUT. WITH GEAR DOWN, LIGHTS WERE NORMAL. REPAIRED SHORTED WIRE AT TERMINAL STRIP S3-66. 2 L 7 2 4F A6WE 1998101600075 19981016 00075 NM 1998 10 16 DL73K982054 1 19981002 A 5330 SKIN BOEING 737 737232 1384475 NM BS 332 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 325DL 23097 FUSELAGE/SKIN ASSY/R1 DOOR CUTOUT/LOWER AFT CORNER: REPAIR FOR SKIN CRACK. A .5 TYPICAL CRACK WAS FOUND IN THE SKIN AN D BONDED DOUBLER AT THE LOWER AFT CORNER OF THE R1 (FWD GALLEY) DOOR CUTOUT. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN ALUMINUM DOUBLER AND TRIPLER PER ER/A 365772-14, REV B. 2 L 7 2 4F RT A16WE 1998101600076 19981016 00076 NM 1998 10 16 DL757982055 1 19981004 A 3350 LIGHT BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 643DL 23997 PASSENGER SEAT 1B EMERGENCY TRACK LIGHTING. REPAIRED DAMAGE TRACK LIGHTING AND SECURED SAME. 2 L 7 2 4F RT A2NM 1998101600077 19981016 00077 NM 1998 10 16 DL72S982056 1 19981005 A 5311 FRAME BOEING 727 727232 1384082 NM BS 761 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 WHILE PERFORMING INSPECTION PER SI 4-61904-12AD A CRACK WAS FOUND IN THE FS 761 RT FRAME ABOVE THE FIRST BOLT HOLE BELOW THE FLOOR LINE IN THE INBD FLANGE. REPAIRED PER ERA 332248-14AD. 2 L 7 3 4F A3WE 1998101600078 19981016 00078 NM 1998 10 16 DL76L982057 1 19981005 A 3350 BATTERY PACK 20131A BOEING 767 767332 1382001 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 181DN 28752 25986 EMERGENCY LIGHT AT CROSSOVER AISLE L1 L2 DOORS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A1NM 1998101600079 19981016 00079 NM 1998 10 16 DL72S982060 1 19980923 A 5320 SUPPORT BOEING 727 727232 1384082 NM NR 2 COWL WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 ITEM: NR 2 ENG FWD COWL SUPPORT RING IS WORN AT THE 9 O'CLOCK POS LOC ON FUSELAGE. REMOVED DAMAGED AREA. FABRICATED D OUBLER AND FILLER PER M/M 53-11-0 PG 801. OK TO INSTALL. INSTALLED REPAIR PER M/M 53-11-0 PG 801. 2 L 7 3 4F A3WE 1998101600080 19981016 00080 NM 1998 10 16 DL72S982061 1 19980824 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 CRACK AFT SPAR RAIL 19 FROM I/B END OF FLAP. REPAIRED ON SHOP ORDER 553647 PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998101600081 19981016 00081 NM 1998 10 16 DL72S982062 1 19980824 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 .5 INCH LONG CRACK IN COVE SKIN -31 FROM I/B END OF FLAP, REPAIRED ON SHOP ORDER 553647 PER MM5 7-52-0 FIG 809. 2 L 7 3 4F A3WE 1998101600082 19981016 00082 NM 1998 10 16 DL72S982063 1 19981006 A 5311 FRAME BOEING 727 727232 1384082 NM BS 784 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 A CRACK WAS FOUND IN THE FS 784 RT FRAME INBD FLANGE. THE CRACK PROPAGATES FROM THE FIRST FASTENER HOLE ABOVE THE FLOOR LINE. REPAIRED PER ERA 300891-14AD, REV A. 2 L 7 3 4F A3WE 1998101600083 19981016 00083 NM 1998 10 16 DL72W982064 1 19981006 A 5313 6518217103 STRINGER BOEING 727 727247 138408F NM BS 375 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 CORROSION DAMAGE FOUND THAT EXCEEDED ALLOWABLE LIMITS, ON THE S1L, AT BS 375. REPAIRED PER ERA 332246-14. 2 L 7 3 4F A3WE 1998101600084 19981016 00084 NM 1998 10 16 DL72S982065 1 19981006 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOPERATIVE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 516DA 21432 EMER TRACK LTS DAMAGED AT 26C. RELAMPED AND REPLACED LENS. ON TEST FOUND AFT FLOOR TRACK LTS INOP. FOUND AFT TRACK L IGHTING PWR SUPPLY BAD. REPLACED PWR SUPPLY. TEST GOOD. 2 L 7 3 4F A3WE 1998101600085 19981016 00085 NM 1998 10 16 DL72S982067 1 19980826 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 408DA 21152 DURING SHOP INSPECTION, THE AFT LOWER WAS FOUND CRACKED IN 2 PLACES, 32 AND 37 FROM IB END. THE ANGLE WAS REPAIRED PER 727MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998101600086 19981016 00086 NM 1998 10 16 DLM88982071 1 19981007 A 5311 59135951 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 999DN 53371 DURING RTN INSPECTION, MTC FOUND A CRACK AT L2R ON THE FS 1418 FRAME; IN TYPICAL LOCATION. REPAIRED PER ERA 332346-14. 2 L 7 2 4F RT A6WE 1998101600087 19981016 00087 NE 1998 10 16 DLL13982072 2 19981006 A 7320 FF REGULATOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 2 ENGINE OUT OF ADJUST A DALA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 790DL 39415 193A1143 NR 2 ENG LOW POWER ON TAKEOFF ROLL .491 EPR WITH LEVER FULL FORWARD TURNED NR 2 PACK OFF WITH NO INCREASE IN POWER. AB ORTED AT 80 KTS, ODM BRAKE TIME VERIFIED. ADJUSTED NR 2 FFR, RAN ENG PER PFHB TETS 13, OPS CK OK. 2 L 7 3 4F 4 F A23WE E12EU 1998101600088 19981016 00088 NM 1998 10 16 DL72W982073 1 19981007 A 5330 SKIN BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2813W 20869 FUSELAGE SKIN FS 720 S-28L-28R, REPAIR FOR SKIN CORROSION. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 720 BETWEEN STRI NGERS 28L AND 28R, DURING ROUTINE INSPECTIONS PER AD 91-09-09. THE CORRODED AREA OF SKIN WAS CUTOUT AN REPAIRED WITH A N EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG. 1. THE REPAIR WAS DOCUMENTED PER ER/A 365810-14AD, REV A. 2 L 7 3 4F A3WE 1998101600089 19981016 00089 NM 1998 10 16 DL72S982074 1 19981006 A 2782 BRACKET BOEING 727 727225 1384077 NM NR 1 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 WING NR 1 SLAT ACTUATOR SUPPORT BRACKET, REPAIR FOR CRACKED WEB AND DOUBLER. THE NR 1 SLAT OUTBD ACTUATOR SUPPORT BRACK ET WAS FOUND WITH THE WEB AND DOUBLER CRACKED. BOTH THE INBD AND OUTBD BRACKETS WERE MODIFIED PER BAC S/B 727-57-0130. THE REPAIR WAS DOCUMENTED PER ER/A 365812-14AD. 2 L 7 3 4F A3WE 1998101600090 19981016 00090 NM 1998 10 16 DL72S982075 1 19981002 A 5312 BULKHEAD BEAM BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 544DA 22493 FUSELAGE BULKHEAD FS 1183 LBL 18 VERTICAL BEAM, REPAIR FOR CRACK. A .75 INCH TYPICAL CRACK WAS FOUND IN RADIUS OF THE L BL 18 VERTICAL BEAM LOWER END ON THE FS 1183 BULKHEAD. THE CRACKED BEAM WAS REPAIRED PER BAC S/B 727-53-0202. THE REPA IR WAS DOCUMENTED PER ER/A 365782-14AD. 2 L 7 3 4F A3WE 1998101600091 19981016 00091 NM 1998 10 16 DL72S982076 1 19980915 A 5311 FRAME BOEING 727 727232 1384082 NM BS 930 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 AT HMV, FOUND FRAME CRACKED FS 930 BETWEEN STR 13R - 14R JUST ABOVE REPAIR. REMOVED DAMAGED PORTION OF FRAME. BEGAN DR ILLING FRAME REPAIR, DRILLED FRAME REPAIR. TREATED AND PAINTED PER PS 900-3-6 NR 3. OK TO INSTALL, BEGAN INSTALL. COM PLETED INSTALL OF FRAME REPAIR PER SRM 53-10-4. 2 L 7 3 4F A3WE 1998101600092 19981016 00092 NM 1998 10 16 DL72S982077 1 19980915 A 5754 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 AT HMV, FOUND RIB NR 5 AND RIB NR 15 CRACKED. ROUTED FRAME 5. REPAIRED DOUBLER AND FILLER AS PER M/M 57-54-0 FIG 814. OK TO INST REPAIR NR 5 RIB. INSTALLED REPAIR ON NR 5 RIB PER M/M 57-54-0 FIG 814. BEGAN MAKING DOUBLER. FINISHED ROU TING RIB NR 15. REPAIRED AND INSTALLED ANGLE PARTIALLY INSTALLED DOUBLER. FINISHED REPAIR PER M/M 57-40-0 FIG 814. 2 L 7 3 4F A3WE 1998101600093 19981016 00093 NM 1998 10 16 DL72W982078 1 19981005 A 5400 ANGLE 65312813 BOEING 727 727247 138408F NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 FOUND LT CHORD ANGLE ON NR 2 ENG SLOPING WEB WITH CORROSION BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH NEW CHORD ANGLE . 2 L 7 3 4F A3WE 1998101600094 19981016 00094 NM 1998 10 16 DL72W982079 1 19981007 A 5400 ANGLE 65312814 BOEING 727 727247 138408F NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 296WA 22533 WHILE PERFORMING HUSH-KIT MOD, FOUND RT CHORD ANGLE ON NR 2 ENG SLOPING WEB CORRODED BEYOND MFG SPECS. REPLACED RT CHOR D WITH NEW SCV CHORD. 2 L 7 3 4F A3WE 1998101600095 19981016 00095 NE 1998 10 16 DL76L982081 2 19981005 A 7230 BLADE BOEING 767 767332 1382001 NM PWA 4060 PW4060 52119 NE NR 1 ENGINE DAMAGED A DALA K NONE E VIBRATION/BUFFET AP APPROACH 1 SO 27 177DN 34513 25122 724169 ON APPROACH TO SFO, DEVELOPED HIGH LEFT ENGINE VIBRATIONS. ENGINE NOT SHUT DOWN. GROUND INSPECTION FOUND FAILURE OF ON E FIRST STAGE FAN BLADE AT THE MIDSPAN WHICH RESULTED IN DAMAGE TO SEVERAL OTHER FIRST STAGE BLADES. DAMAGE ALSO TO FAN EXIT GUIDE VANES. REMOVED AND REPLACED ALL N1 FAN BLADES AND SCHEDULED VANES FOR REPLACEMENT, BOROSCOPED ENGINE, RAN E NGINE. ENGINE CHECKS GOOD. 2 L 7 2 4F 4 F RT A1NM E24NE 1998101600096 19981016 00096 1998 10 16 SCNA98121 4 19981004 A 3442 MI585161 RT UNIT BOEING 727 7272J4 1384006 NM FWD FUSELAGE FAILED A SCNA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 285SC 2354 21676 DURING CLIMB, THE RADAR LOST PICTURE. PICTURE CAME BACK FIVE MINUTES PRIOR TO LANDING. DIVERTED AIRCRAFT TO IAH. REMO VED AND REPLACED THE RADAR RECEIVER/TRANSMITTER. RADAR SYSTEM OPERATIONALLY CHECKS GOOD IAW MM 340000. 2 L 7 3 4F RT A3WE 1998101600097 19981016 00097 EU 1998 10 16 HCMA0000207 1 19980607 A 6520 350A33215300 HINGE SNIAS 350 AS350BA 8680817 EU TAIL ROTOR DELAMINATED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 422B 772 2391 PART IS TORN BEYOND LIMITS AND THERE IS NO J-GAP. (X) 1 G 7 1 3U NC H9EU 1998101600098 19981016 00098 EU 1998 10 16 HCMA0000209 1 19980608 A 6520 350A33215300 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR DELAMINATED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 193BH 847 2894 RUBBER IS TORN BEYOND LIMITS AND THERE IS NO J-GAP. (X) 1 G 7 1 3U H9EU 1998101600099 19981016 00099 EU 1998 10 16 HCMA0000210 1 19980718 A 6420 350A33200405 BEARING SNIAS 350 AS350B2 8680813 EU T/R SPIDER ROUGH A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 196BH 930 MA0758 3036 BEARING WAS ROUGH, INSPECTED AND FOUND INNER RACE SPINNING. REPLACED. (X) 1 G 7 1 3U H9EU 1998101600100 19981016 00100 EU 1998 10 16 HCMA0000211 1 19980714 A 6510 7704411 SEAL SNIAS 350 AS350B2 8680813 EU T/R DRIVE LEAKING A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 196BH 908 3036 MAG SEAL LEAKS. (X) 1 G 7 1 3U H9EU 1998101600101 19981016 00101 EU 1998 10 16 HCMA0000212 1 19980729 A 8011 P600705 FLANGE SNIAS 350 AS350B2 8680813 EU STARTER WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 196BH 967 3036 BEARING SPINNING. (X) 1 G 7 1 3U H9EU 1998101600102 19981016 00102 NM 1998 10 16 TSAA9833479 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 1 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600103 19981016 00103 NM 1998 10 16 TSAA9833480 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 2 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600104 19981016 00104 NM 1998 10 16 TSAA9833481 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARAGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 3 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600105 19981016 00105 NM 1998 10 16 TSAA9833482 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 4 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600106 19981016 00106 NM 1998 10 16 TSAA9833483 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 5 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600107 19981016 00107 NM 1998 10 16 TSAA9833484 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED EMERGENCY PATH LIGHTING BATTERY PACK AT NR 6 POSITION. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600108 19981016 00108 NM 1998 10 16 TSAA9833485 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED AFT ENTRY EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600109 19981016 00109 NM 1998 10 16 TSAA9833486 1 19980903 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED RT OVERWING EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600110 19981016 00110 NM 1998 10 16 TSAA9833487 1 19980903 A 3350 8731002511 LIGHT BOEING 737 737209 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED RT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600111 19981016 00111 NM 1998 10 16 TSAA9833488 1 19980903 A 3350 8731002511 LIGHT BOEING 737 737209 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED AFT ENTRY EMERGENCY EXIT IDENTIFIER LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1998101600112 19981016 00112 EA 1998 10 16 VTZA98235 1 19980704 A 5210 H341425 HANDLE CNDAIR CL600 CL6002B19 EA PASSENGER DOOR LACK OF LUBE A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 625BR 7214 IAD/SAV - FLT 6735 - DURING CRUISE AT 2215 HOURS, EXPERIENCED A PASSENGER DOOR WARNING MESSAGE. AIRCRAFT RETURNED TO TH E IAD AND NOTIFIED MAINTENANCE CONTROL. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND LUBRICATED THE PASSENGER DOOR OU TER HANDLE. ALL REQUIRED CHECKS WERE ACCOMPLISHED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1998101600113 19981016 00113 WP 1998 10 16 AALA981537 1 19980816 A 3350 1032200 SWITCH DOUG DC9 DC983 3022083 WP COCKPIT FAILED A AALA O OTHER L NO TEST CR CRUISE 1 SW 07 598AA 53288 ORD - FLT T1881 - EN ROUTE DTW/ORD, EMERGENCY POWER SWITCH WAS INTERMITTENT. LANDED ORD WITHOUT INCIDENT. REPLACED EME RGENCY POWER SWITCH. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998101600114 19981016 00114 NM 1998 10 16 ASAA9840082 1 19980810 A 3350 LIGHT BOEING 737 737490 1384715 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 796AS 28891 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHT AT OVERHEAD BIN 19ABC WAS FOUND INOPERATIVE. CHECKED AND RELEASED P ER MEL 33-15B. ON 8-11-98 RELAMPED, NO HELP. TOOK A VOLTAGE READING AT D007104 AND D007106. VOLTAGE WAS ERRATIC. DID NOT FIND ANY VISIBLE DAMAGE TO WIRING. REQUIRES FURTHER TROUBLESHOOTING. REMAINS ON MEL. ON 8-12-98 FOUND GROUND WIR E DISCONNECTED ABOVE OVERHEAD BIN, RECONNECTED WIRE, NO HELP. PROBLEM GOT WORSE. NO VOLTAGE PRESENT AND NOW LIGHT AT 2 2ABC WAS INOPERATIVE. REQUIRES FURTHER TROUBLESHOOTING. REMAINS ON MEL. (X) 2 L 7 2 4F RT A16WE 1998101600115 19981016 00115 NM 1998 10 16 HNAA82836 1 19980807 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 828MA 13940 SB6122 333 DURING FLIGHT CREW ORIGINATING CHECK, FORWARD OVERHEAD EMERGENCY EXIT IDENTIFIER LIGHT INOPERATIVE. REMOVED AND REPLACE D BATTERY 3351 PS2, OPS CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998101600116 19981016 00116 NM 1998 10 16 GAIA9869 1 19980701 A 2120 AIR DISTR BOEING 727 727223 1384074 NM COCKPIT ODOR A GAIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 6838 20191 TOL - ON DEPARTURE, A STRONG ODOR OF BURNING RUBBER WAS BRIEFLY SMELLED IN THE COCKPIT. AIRCRAFT WAS RETURNED TO TOL AN D LANDED UNDER MAX LANDING WEIGHT WITHOUT FURTHER PROBLEMS. PERFORMED A THOROUGH INSPECTION OF LANDING GEAR AND GEAR WE LL. INSPECTED E/E BAY AND AFT STAIRWELL AREA. NO DEFECTS NOTED. AIRCRAFT SHOWED NO INDICATIONS OF DAMAGE OR OTHER ABN ORMALITIES. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998101600117 19981016 00117 SW 1998 10 16 HSYA817E 1 19980731 A 3213 48NBL2060YZP BEARING GULSTM 680 680FL 0141608 SW LT MLG LACK OF LUBE A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 113NA 1794149 BIL - DURING SCHEDULED MAINTENANCE INSPECTION, THE LEFT MAIN LANDING GEAR STRUT LOWER LEG WAS FOUND BINDING WITHIN THE P IVOT BEARINGS BETWEEN THE LOWER LEG AND UPPER BARREL. CONTAMINATION OF BEARINGS, DRY, NO LUBRICATION. LEFT STRUT ASSY WILL BE DISASSEMBLED, NON-DESTRUCTIVE TESTED AND INSPECTED, AND RE-ASSEMBLED USING SERVICEABLE PARTS. (X) 1 H 7 2 3O 2A4 1998101600118 19981016 00118 GL 1998 10 16 SIMA981653 2 19980614 A 7321 FADEC EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL COCKPIT OVERHEATED A SIMA O OTHER B N SMOKE/FUMES/ODORS/SPARKS FALSE WARNING IN INSP/MAINT 1 SW 21 603AE 145055 IND - FLT 4209 - RECEIVED SIMULTANEOUS EICAS (ENGINE INDICATING AND CREW ALERTING SYSTEM), MESSAGES, E1 CTL A FAIL, E2 C TL B FAIL. FLIGHT CREW NOTICED SLIGHT SMELL LIKE BURNING ELECTRICAL. RESET FADECS (FULL AUTHORITY DIGITAL ELECTRONIC C ONTROL SYSTEM ) FOR APPROXIMATELY 5 SECONDS THEN IT FAILED AGAIN. MAINTENANCE INSPECTED AND FOUND NO FAULT RECORDED ON MFD. RAN ENGINES FOR OPS CHECK OF ENGINES AND AIR CONDITIONING SYSTEM WITH NO SMELL NOTED. DID VISUAL CHECK OF AFT AVI ONICS COMPARTMENT WITH NO SIGNS OF ELECTRICAL DAMAGE. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T 4 F RT T00011AT TE6CH 1998101600119 19981016 00119 EU 1998 10 16 AALA981426 1 19980722 A 2910 NAS16128 O-RING FOKKER F28 F28MK0100 4990807 EU HYDRAULIC SYSTEM FAILED A AALA O OTHER J K WARNING INDICATION FLUID LOSS CR CRUISE 1 SW 07 1445B 11448 DFW - FLT T0455 - DURING CRUISE, NR 1 HYDRAULIC LOW LIGHT ILLUMINATED ON MFDU. CREW TURNED OFF NR 1 HYDRAULIC SYSTEM AN D FOLLOWED PROCEDURES FOR ALTERNATE FLAP AND GEAR EXTENSION. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT AND WAS TOWED TO THE GATE. MAINTENANCE FOUND O-RING IN SAMPLING VALVE LEAKING. REPLACED O-RING IN SAMPLING VALVE AND SERVICED NR 1 HYDRAULIC SYSTEM. SYSTEM GROUND AND LEAKED CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT 1998101600120 19981016 00120 CE 1998 10 16 98ZZZX3743 1 19980716 A 5753 35165050258 SKIN BEECH 1900 1900D 1154162 CE LT TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 140ZV 660 L0120 UE140 ICT - OVERNIGHT MAINTENANCE FOUND A 1 INCH CRACK ON LT OTBD FLAP 11 INCHES FROM TRAILING EDGE AND 29 INCHES FROM INBD ED GE ON BOTTOM SKIN. REPAIRED CRACK IAW AMWA TO 1900-27-00-0001. (X) 2 L 7 2 4T RT A24CE 1998101600121 19981016 00121 CE 1998 10 16 98ZZZX3744 1 19980718 A 5753 1016000143 SKIN BEECH 1900 1900D 1154162 CE LT TE FLAP CHAFED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 98YV 7639 734 UE98 ICT - OVERNIGHT MAINTENANCE FOUND A CHAFED SPOT ON THE DOVETAIL SKIN ON LT IBD FLAP. REPAIRED IAW ANWA TO 2900-27-00-00 01. (X) 2 L 7 2 4T RT A24CE 1998101600122 19981016 00122 SO 1998 10 16 C2XA98IA281 1 19980710 A 2770 14522144401 GUST LOCK EMB 145 EMB145LR SO FUSELAGE OUT OF RIG A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16951 145063 ICT - FLT 4154 - DURING PRE-FLIGHT INSPECTION, THE PILOT REPORTED THE GUST LOCK SYSTEM WAS BROKEN. MAINTENANCE INSPECTE D THE GUST LOCK SYSTEM AND FOUND IT TO BE OUT OF RIG. FURTHER EXAMINATION OF THE AIRCRAFT REVEALED SUBSEQUENT DAMAGE TO THE LEFT AND RIGHT ELEVATORS. MAINTENANCE RIGGED THE GUST LOCK SYSTEM, AND THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINT ENANCE REPAIRED THE DAMAGE TO THE ELEVATORS AND RETURNED THE AIRCRAFT TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 1998101600123 19981016 00123 SO 1998 10 16 C2XA98IA276 1 19980723 A 3231 22250100001 VALVE EMB 145 EMB145LR SO NLG FAILED A C2XA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 13949 145057 IAH - FLT 4175 - THE CREW REPORTED THE NOSE LANDING GEAR WOULD NOT EXTEND WHEN THE GEAR CONTROL LEVER WAS PLACED IN THE DOWN POSITION. THE CREW MANUALLY EXTENDED THE GEAR AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACE D THE LANDING GEAR DOOR SOLENOID VALVE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 1998101600124 19981016 00124 1998 10 16 GTIA9800101 4 19980820 A 2565 SLIDE DOUG DC9 DC982 3022082 WP CABIN DETACHED A GTIA K NONE O OTHER NR NOT REPORTED 1 GL 23 804RA 48048 MCO - FLT 501 - SLIDE PACK FELL OFF AFT ALLEY DOOR. REINSTALLED SLIDE PACK AS NECESSARY IAW MM 25-00-01. (X) 2 L 7 2 4F A6WE 1998101600125 19981016 00125 EA 1998 10 16 MASA98150 1 19980803 A 3350 1317 BULB DC10020004 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27172 7172 LIT/CLT - FLT 5773 - CREW REPORTED ROW 10 EMERGENCY FLOOD LIGHT INOPERABLE. MAINTENANCE ACTION WAS DEFERRED PER MEL 33- 51-1. AIRCRAFT RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. 2 L 7 2 4F RT A21EA 1998101600126 19981016 00126 EA 1998 10 16 MASA98170 1 19980906 A 3350 1317 BULB BM106002 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27172 7172 DURING ROUTINE MAINTENANCE, FOUND THE LEFT OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE BULB WAS REMOVED AND REPL ACED, OPS CHECK GOOD. (X) 2 L 7 2 4F RT A21EA 1998101600127 19981016 00127 EA 1998 10 16 MASA98171 1 19980906 A 3350 1317 BULB BM1006002 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27172 7172 DURING ROUTINE MAINTENANCE, FOUND THE RIGHT OVERWING EMERGENCY LIGHT WOULD NOT ILLUMINATE. THE BULB WAS REMOVED AND REP LACED. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A21EA 1998101600128 19981016 00128 EA 1998 10 16 MASA98155 1 19980813 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA E/E BAY MALFUNCTIONED A MASA L ABORTED APPROACH O OTHER AP APPROACH 1 SW 07 47202 7202 PHL/GHM - FLT 5760 - ON APPROACH TO BHM, THE LANDING GEAR WOULD NOT EXTEND. THE CREW MANUALLY EXTENDED THE GEAR. NO EM ERGENCY WAS DECLARED, HOWEVER, THE TRUCKS WERE DISPATCHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SEVERAL GEAR RETRACTIONS, BUT COULD NOT DUPLICATE THE PROBLEM. THEY REMOVED AND REPLACED THE PSEU AS A PRECAUTIONARY M EASURE THEN TEST FLEW THE AIRCRAFT. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998101600129 19981016 00129 EU 1998 10 16 SIMA982301 1 19980818 A 3230 HP84843062 VALVE SAAB SF340 340B 7860101 EU NLG WW FAILED A SIMA O OTHER O OTHER AP APPROACH 1 SW 21 350CF 1384 340B350 LAX - FLT 3313 - LANDING GEAR WOULD NOT EXTEND NORMALLY. CREW SUCCESSFULLY PERFORMED EMERGENCY GEAR EXTENSION PROCEDURE . AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDING GEAR CONTROL VALVE. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998101600130 19981016 00130 EA 1998 10 16 S9BA604Y 1 19980721 A 5512 C6TP10017 SKIN DHAV DHC6 DHC6300 2802606 EA HORIZONTAL STAB CRACKED A S9BA K NONE O OTHER IN INSP/MAINT 1 AL 05 288SA 32516 389 DURING EMMA INSPECTION NR 13, A CRACK WAS FOUND ON ELEVATOR CENTER HINGE BRACKET UPPER SUPPORT DOUBLER. REPLACED HORIZO NTAL STABILIZER, RIGGED CONTROLS, AND TEST FLIGHT SATISFACTORY IAW DHC-6-300 MM AND SEABORNE GMM. (X) 1 H 7 2 3T RT A9EA 1998101600131 19981016 00131 SW 1998 10 16 BXOA0000006 1 19980918 A 5320 206023100112 SUPPORT BELL 206 206L3 1182108 SW FUSELAGE CRACKED A BXOA K NONE O OTHER IN INSP/MAINT 1 EA 09 5000B 7371 51044 DURING 100 HOUR INSPECTION, RIGHT UPPER HORIZONTAL SUPPORT WAS FOUND CRACKED . (X) 1 G 7 1 3U H2SW 1998101600132 19981016 00132 SW 1998 10 16 BXOA0000070 1 19980916 A 5302 206033004143 INTERCOSTAL BELL 206 206L3 1182108 SW TAILBOOM ASSY CRACKED A A BXOA K NONE O OTHER IN INSP/MAINT 1 EA 09 3CW 3076 51420 51420 PILOT REQUESTED INSPECTION OF SUSPECTED CRACK IN TAIL BOOM AT LT UPPER SUPPORT FOR THE HORIZONTAL STABILIZER. UPON INSP ECTION, A LINE APPROXIMATELY .75 INCH LONG WAS FOUND AND DETERMINED TO BE A CRACK. WHILE PREPARING TO REMOVE LT UPPER S UPPORT, 2 CRACKS WERE FOUND BELOW THE LT LOWER SUPPORT. UPON REMOVAL OF HORIZONTAL STABILIZER, A CRACK 1.3 INCHES LONG STARTING .3 INCH AFT OF THE FWD UPPER CORNER OF LT TAIL BOOM CUT OUT, A CRACK 1.6 INCHES LONG STARTING .3 INCH FROM THE FWD LOWER CORNER OF LT TAIL BOOM CUT OUT, BOTH IN THE UPPER SKIN AND A CRACK 2.5 INCHES LONG STARTING .5 INCH FROM THE F WD LOWER CORNER OF THE LT TAILBOOM CUT OUT IN THE LOWER SKIN WAS FOUND. PART CYCLES, 3,179. (X) 1 G 7 1 3U H2SW 1998101600133 19981016 00133 GL 1998 10 16 98ZZZX3706 2 19980914 A 7240 6870992K COMBUSTION CASE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL ENGINE CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC S754 835391 DURING DAILY INSPECTION, ARM PIT AREA OF COMBUSTION CASE FOUND CRACKED, APPROXIMATELY 2.50 INCHES LONG. PILOTS NOTED AP PROXIMATELY 20 DEGREES TOT INCREASE ON THAT ENGINE ON PRIOR FLIGHT. REPLACED PART. 1 G 7 2 3U 3 U H3EU E4CE 1998101600134 19981016 00134 NE 1998 10 16 98ZZZX3707 2 19980520 A 7250 311450201 SHIELD DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE ENGINE CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 320 90000012 PCE206068 SHIELD CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 1,477. 1 G 7 2 3U 3 U NC H19NM E42NE 1998101600135 19981016 00135 NM 1998 10 16 98ZZZX3708 1 19980615 A 6720 900R2442012103 FAN ASSY DOUG MD900 MD900 3027375 NM NOTAR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 361 0033480917 90000012 BUBBLE IN SPAR AREA. REPLACED FAN ASSY WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600136 19981016 00136 NM 1998 10 16 98ZZZX3709 1 19980615 A 6720 900R2442012103 FAN ASSY DOUG MD900 MD900 3027375 NM NOTAR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 361 0033480967 90000012 BUBBLE IN SPAR AREA. REPLACED FAN ASSY WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600137 19981016 00137 NE 1998 10 16 98ZZZX3710 2 19980330 A 7230 430150601 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 5194C 522 1952 7169 LE45514EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1998101600138 19981016 00138 NE 1998 10 16 98ZZZX3711 2 19980330 A 7250 414144001 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 522 62556 7169 LE45514EF BEARING HAS EXCESSIVE PITTING. REPLACED WTIH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1998101600139 19981016 00139 NE 1998 10 16 98ZZZX3712 2 19980526 A 7230 430150601 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 90260 1826 7140 LE45511EFA REJECTED NEW OUT-OF-BOX. LEAKING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1998101600140 19981016 00140 NE 1998 10 16 98ZZZX3713 2 19980515 A 7230 430150601 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 118LF 384 1954 7137 LE45357EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH UNIT UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600141 19981016 00141 NE 1998 10 16 98ZZZX3714 2 19980515 A 7250 414144001 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 118LF 384 4792 7137 LE45357EA BEARING HAS EXCESSIVE PITTING. REPLACING WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600142 19981016 00142 NE 1998 10 16 98ZZZX3715 2 19980815 A 7260 230093303 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE ROUGH A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 118LF 384 7137 LE45357EA BEARING ROUGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600143 19981016 00143 NE 1998 10 16 98ZZZX3716 2 19980512 A 7250 411109008 NOZZLE ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY A003HXL 7127 LE45305E UNABLE TO GET CORRECT FLOW WHICH RESULTED IN ENGINE LOW POWER WITH HIGH EGT. -08 WEFA NEEDS TO BE BETWEEN 3.592 AND 3.6 00. WEFA FOR DISCREPANT UNIT IS 3.692 WHICH IS TOO HIGH FOR FLEET. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600144 19981016 00144 NE 1998 10 16 98ZZZX3717 2 19980512 A 7210 430101801 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ACCESSORY DOOR CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 697 7127 LE45305E BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600145 19981016 00145 NE 1998 10 16 98ZZZX3718 2 19980512 A 7261 416184001 TUBE ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE PT SCAVENGE LEAKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 697 7127 LE453053 TUBE ASSY LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600147 19981016 00147 NE 1998 10 16 98ZZZX3720 2 19980512 A 7230 410100712 SHAFT BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 697 90M110 7127 LE45305E SHAFT HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 1,661.3. 1 G 7 2 3U 3 U H13EU E5NE 1998101600150 19981016 00150 NE 1998 10 16 98ZZZX3723 2 19980305 A 7230 430150601 SEAL BOLKMS 117 BK117A1 5626010 EU LYC LTS101 LTS101650B1 41560 NE ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 128HH 257 1592 7036 LE45254EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600151 19981016 00151 NE 1998 10 16 98ZZZX3724 2 19980729 A 7220 311800501 SCREEN DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE AIR INLET WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 694 90000012 PCE206018 SCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1998101600152 19981016 00152 NM 1998 10 16 98ZZZX3725 1 19980818 A 2421 311697802 HARNESS DOUG MD900 MD900 3027375 NM ALTERNATOR FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1810 AA3689 90000012 PIN TO PMA (STATOR) IS EXCESSIVELY BURNED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600153 19981016 00153 NM 1998 10 16 98ZZZX3726 1 19980818 A 2421 3038628 STATOR DOUG MD900 MD900 3027375 NM ALTERNATOR FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1810 0082 90000012 PIN 'A' IS EXCESSIVELY BURNED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600155 19981016 00155 NM 1998 10 16 98ZZZX3728 1 19980615 A 6720 900R2442012103 FAN ASSY DOUG MD900 MD900 3027375 NM NOTAR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 361 0033480920 90000012 BUBBLE IN SPAR AREA. REPLACED WITH NEW FAN ASSY UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600157 19981016 00157 NE 1998 10 16 98ZZZX3730 2 19980330 A 7230 430151801 BEARING BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 522 960633100559 7169 LE45514EF EXCESSIVE ROLLER WEAR. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1998101600159 19981016 00159 NM 1998 10 16 98ZZZX3732 1 19980528 A 6321 900D3403502101 CALIPER DOUG MD900 MD900 3027375 NM ROTOR BRAKE STUCK A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 325 0020 90000012 AFT PISTON WILL NOT RETRACT. UNIT INSTALLED WHILE AC WAS IN MESA FOR WORK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600160 19981016 00160 NM 1998 10 16 98ZZZX3733 1 19980518 A 7160 900CF330001101 ACTUATOR DOUG MD900 MD900 3027375 NM INLET DOOR INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 170 46 90000012 UNIT INOPERATIVE. DOOR WILL NOT OPEN. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600161 19981016 00161 NM 1998 10 16 98ZZZX3734 1 19980508 A 7160 900CF330001101 ACTUATOR DOUG MD900 MD900 3027375 NM INLET DOOR INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 286 39 90000012 UNIT INOPERATIVE. MOTOR FAILED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600162 19981016 00162 NM 1998 10 16 98ZZZX3735 1 19980901 A 6710 900C2010214101 PITCH LINK DOUG MD900 MD900 3027375 NM MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 555 90000012 PITCH LINK ASSY WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600163 19981016 00163 NM 1998 10 16 98ZZZX3736 1 19980523 A 6220 900R310101107 BEARING DOUG MD900 MD900 3027375 NM MAIN ROTOR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1257 0206040635 90000012 BEARING DEBONDED FROM ELASTOMERS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600164 19981016 00164 NM 1998 10 16 98ZZZX3737 1 19980627 A 6220 BEARING DOUG MD900 MD900 3027375 NM MAIN ROTOR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1103 0206040623 90000012 BEARING DEBONDED FROM ELASTOMERS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998101600165 19981016 00165 NE 1998 10 16 98ZZZX3738 2 19980729 A 7220 311659901 SCREEN DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE INTAKE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1893 90000012 PCE206018 AIR INLET SCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTING. REPLACED WITH NEW UNIT, CORRECTED PR OBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1998101600166 19981016 00166 NE 1998 10 16 98ZZZX3739 2 19980512 A 7250 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 697 03912066 7127 LE45305E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600167 19981016 00167 NE 1998 10 16 98ZZZX3740 2 19980512 A 7230 430151801 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE CORRODED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 697 960633101015 7127 LE45305E BEARING HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600168 19981016 00168 NE 1998 10 16 98ZZZX3741 2 19980512 A 7230 430150601 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 697 1716 7127 LE45305E SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1998101600169 19981016 00169 NE 1998 10 16 98ZZZX3742 2 19980729 A 7220 311800501 SCREEN DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE AIR INLET WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 694 90000012 PCE206042 AIR INLET SCREEN WORN BEYOND SERVICEABLE LIMITS. WIRE MESH IS LOOSE AND FRETTI NG. REPLACED WITH NEW UNIT, CORRECTED P ROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1998101600170 19981016 00170 WP 1998 10 16 TWAA9816301 1 19981009 A 2782 39200485511 ACTUATOR DOUG DC9 DC932 3022066 WP RT LE SLAT WORN A TWAA H DEACTIVATE SYST/CIRCUITS F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 CE 05 932L 47669 THE RT WING LE SLATS EXTENDED ONLY HALF WAY. LT WING SLATS EXTENDED NORMALLY. ACFT HAD PRONOUNCED ROLL TENDENCY. LAND ED WITH SLATS RETRACTED. REPLACED BOTH RT WING SLAT ACTUATORS. CHECK-C 4-24-98 STL. 2 L 7 2 4F A6WE 1998101600172 19981016 00172 NM 1998 10 16 TWAA9816303 1 19981009 A 3350 S417N50911 LIGHT BOEING 767 767330 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 691LF 25137 DURING MAINT, FOUND TWO EGRESS LIGHTS INOPERATIVE ON RT SIDE OF FIRST CLASS, ROW 1. REPLACED LIGHT ASSEMBLY. CHECK-C 8 -13-98 LAX. 2 L 7 2 4F RT A1NM 1998101600173 19981016 00173 WP 1998 10 16 TWAA9816307 1 19981011 A 2510 G03667507 HOUSING DOUG DC9 DC982 3022082 WP RT COCKPIT DEFORMED A TWAA K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 05 953U 49267 FIRST OFFICER RT RUDDER PEDAL SEEMED TO BIND ON RUDDER PEDAL HOUSING. REPLACED FIRST OFF RUDDER PEDAL HOUSING. CHECK-C 3-25-98 MCI. 2 L 7 2 4F A6WE 1998101600174 19981016 00174 WP 1998 10 16 TWAA9816308 1 19981009 A 2410 696233B CSD DOUG DC9 DC982 3022082 WP LT ENGINE WORN A TWAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 05 954U 49426 FLIGHT LEFT STL WITH LT GENERATOR PLACARDED INOPERATIVE PER MEL. IN FLIGHT THE APU GENERATOR WENT OFF LINE AND AC CROSS TIE LOCKOUT LIGHT CAME ON. UNABLE TO RESET. MADE UNSCHEDULED LANDING AT MCI. REPLACED THE LT ENG CSD. PLACARDED THE APU GENERATOR INOPERATIVE PER MEL. CHECK-C 8-2-98 STL. *S/D* RESTORED THE APU BY REPLACING THE FUEL CONTROL, (P/N 360 8000-10), AND THE GENERATOR, (P/N 976J252-8). 2 L 7 2 4F A6WE 1998101600175 19981016 00175 WP 1998 10 16 TWAA9816309 1 19981011 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951U 49245 DURING MAINT CHECK, FOUND EMERGENCY CEILING LIGHT INOPERATIVE AT CABIN ROWS 9 AND 11. REPLACED BATTERY PACK. CHECK-C 7 -28-98 MCI. 2 L 7 2 4F A6WE 1998101600176 19981016 00176 WP 1998 10 16 TWAA9816310 1 19981011 A 3350 408822101 BATTERY PACK DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951U 49245 DURING MAINT CHECK, FOUND EMERGENCY CEILING LIGHT INOP AT AFT LAVS. REPLACED BATTERY PACK. CHECK-C 7-28-98 MCI. 2 L 7 2 4F A6WE 1998101600177 19981016 00177 WP 1998 10 16 TWAA9816311 1 19981007 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 996 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND STA 996 FORMER RING FOOT CRACKED ABOVE AND BELOW LONGERON 19L. REMOVED AND REPLACED FOR MER RING FOOT SECTION WITH NEW SECTION PART A5910163-79 PER SRM 51-31-0, AND TWA STANDARD PROCEDURES. 2 L 7 2 4F A6WE 1998101600178 19981016 00178 WP 1998 10 16 TWAA9816312 1 19981001 A 5312 BUKLHEAD WEB DOUG DC9 DC931 3022065 WP BS 965.091 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND AT RT FUSELAGE BULKHEAD WEB AT STA 965.091, PYLON FROM SPAR LOWER CAP, HIGH FREQ EDDY CU RRENT INDICATED CRACK IN LOWER OTBD BOLT HOLE. REAMED HOLE SIZE TO .02807 AND ELIMINATED. 2 L 7 2 4F A6WE 1998101600179 19981016 00179 WP 1998 10 16 TWAA9816313 1 19981007 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND LT LAV STA 980 LONGERON 14L WITH 2 IN CRACK IN FORMER FOOT. REPLACED CRACKED FORMER WIT H DAC P/N J060119-17 FORMER PER MO72J14 PHASE G, AND ARA 15706. 2 L 7 2 4F A6WE 1998101600180 19981016 00180 WP 1998 10 16 TWAA9816314 1 19981007 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 980 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND RT LAV STA 980 LONGERON 14R WITH 2 IN CRACK IN FORMER FOOT. REPAIRED PER MO72J14H, DRAW ING J060119, AND ARA 15706. 2 L 7 2 4F A6WE 1998101600181 19981016 00181 NM 1998 10 16 CKSA98543 1 19981008 A 5347 65B112441 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 460 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LBL75 AND RBL75 SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS IAW BOEING ENG DRWING. FOUND DURING C AND D CHE CK AND CPCP. WORK ORDER NUMBER MO280, NON-ROUTINE TASK NUMBER 65B20459-518-IO1. CPC WORK CARD NUMBER C53-210-0103. 2 L 7 4 4F RT A20WE 1998101600182 19981016 00182 NM 1998 10 16 CKSA98544 1 19981008 A 5210 GATE BOEING 747 7472B4B 138481B NM BS 440-480 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 L1 DOOR LOWER GATE CORRODED, ZONE 831, STA440-480, WL200, LBL110, LOCAL CORROSION. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-09-01. 2 L 7 4 4F RT A20WE 1998101600183 19981016 00183 NM 1998 10 16 CKSA98545 1 19981008 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 540-600 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK CORRODED AT SEC 41 UPPER DECK (200), STA 540 TO STA600, WL308, RBL46. REMOVED AND REPLACED IAW 747SRM 53-10- 05, ALTERNATIVE I, PG 2A (BAC1520-1566 M/C NR 13-7856-6800 605-CO2). FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WO RK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-02. 2 L 7 4 4F RT A20WE 1998101600184 19981016 00184 NM 1998 10 16 CKSA98546 1 19981008 A 5347 65B061364 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 581 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK AT SEC 41 UPPER DECK, ZONE 200 STA581, W/308, RBL65 CORRODED. REPAIRED IAW SUPP SHEET CKF-A-050 SHEET NR 1 A ND NR 2. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-02. 2 L 7 4 4F RT A20WE 1998101600185 19981016 00185 NM 1998 10 16 CKSA98547 1 19981008 A 5347 65B0655617 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 640-720 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK AT SEC 41, UPPER DECK ZONE 200, STA 540 TO 600, WL308, RBL46 CORRODED. REF TASK CARD NR ASA CKF-A-042 ITEM 1 AND 2. REPAIRED PER SUPPLEMENTAL SHEET NR 1. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT . WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-01. 2 L 7 4 4F RT A20WE 1998101600186 19981016 00186 NM 1998 10 16 CKSA98548 1 19981008 A 5320 65B0432464 SHEAR TIE BOEING 747 7472B4B 138481B NM BS 1740 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SHEAR TIE AT ZONE 100, STA 1740, STR 47L-48L CORRODED. REPAIRED IAW DWG 65B04324 SH 6, SUPP SHEETS 1 AND 2. FOUND DURI NG ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53 -110-01-03. 2 L 7 4 4F RT A20WE 1998101600187 19981016 00187 NM 1998 10 16 CKSA98549 1 19981008 A 5313 65B071114 STRINGER BOEING 747 7472B4B 138481B NM BS 1760 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 STRINGER AT STA 1760, STR 44R CORRODED BEYOND LIMITS. REPAIRED IAW SRM 51-30-02 AND DWG 65B04143 SHT 5. CORROSION APPR OX 8 LONG BY 1 WIDE BY .030 DEEP. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER. 2 L 7 4 4F RT A20WE 1998101600188 19981016 00188 NM 1998 10 16 CKSA98550 1 19981008 A 5240 65B0989125 GATE BOEING 747 7472B4B 138481B NM L5 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 DOOR L5 LWR GATE ASSY CORRODED BEYOND SRM LIMITS. REPAIRED IAW DWG 65B09891-47. FOUND DURING ACCOMPLISHMENT OF C, D CHE CK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-200-01-04. 2 L 7 4 4F RT A20WE 1998101600189 19981016 00189 NM 1998 10 16 CKSA98551 1 19981008 A 5320 65B04348167 WEB BOEING 747 7472B4B 138481B NM BS 2220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 65B04348-167 WEB CORRODED AT INBD END APPROX AREA .60 BY .40, STA2220, RBL50, WL160. REPAIRED IAW DWG 65B04348 SH 9, SU PP SHEET NR 1. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORR OSION TASK CARD NUMBER C53-125-01-02. 2 L 7 4 4F RT A20WE 1998101600190 19981016 00190 NM 1998 10 16 CKSA98552 1 19981008 A 5240 65B05091896 HINGE WEB BOEING 747 7472B4B 138481B NM NR 5 RT DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 INTERNAL DOOR NR 5 RT HINGE WEB CORRODED. REPLACED IAW ENG DWG 65B05091 SHEET 2 REV E ZONE A5 AND SHEET 10 VIEW 2A5-3 Z NB13. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TAS K CARD NUMBER C53-200-01-04. 2 L 7 4 4F RT A20WE 1998101600191 19981016 00191 NM 1998 10 16 CKSA98553 1 19981008 A 5230 65B176771 FITTING BOEING 747 7472B4B 138481B NM CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 REF CKF-AMD-026, TKR 1394706 AND 1394707, MM52-32-01 AND SB 747-52-2186. TWO MAIN DECK CARGO DOOR LATCH FITTINGS CORROD ED. REPLACED IAW APPLICABLE ENG DWG AND SB REQUIREMENTS (REF SB'S 747-52-2186 AND 52-2142). FOUND DURING ACCOMPLISHMEN T OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-200-01-04. 2 L 7 4 4F RT A20WE 1998101600192 19981016 00192 NM 1998 10 16 CKSA98554 1 19981008 A 5313 65B0448313 STRINGER BOEING 747 7472B4B 138481B NM BS 1950-1960 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 STA 1950-1960 STRINGER 51R HAS 8.5 AREA OF CORROSION. REPAIRED IAW ASA CKF-AMO-047 AND ASA- AMD-057. FOUND DURING ACCO MPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-125-01 -02. 2 L 7 4 4F RT A20WE 1998101600193 19981016 00193 NM 1998 10 16 CKSA98555 1 19981008 A 5330 65B041522 SKIN BOEING 747 7472B4B 138481B NM BS 2160-2180 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 FOUND WIDESPREAD CORROSION ON SKIN FROM STA 2160-STA 2180 AND STR47-STR51. REPAIRED IAW BOEING ENG DWG ASA-CKF-AMD-082 SK020/RD622 SHEETS 1 THROUGH 4. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER N UMBER MO280, CORROSION TASK CARD NUMBER C53-125-01-02. 2 L 7 4 4F RT A20WE 1998101600194 19981016 00194 NM 1998 10 16 CKSA98556 1 19981008 A 5230 65B0472815 FRAME BOEING 747 7472B4B 138481B NM CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 ZONE 140 AFT CARGO DOOR T-FRAME INTERIOR DOOR SRTUCTURE CORRODED BEYOND LIMITS. REPAIRED IAW ASA-CKF-AMD-055 SHEET 5. F OUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD N UMBER C53-110-01-03. 2 L 7 4 4F RT A20WE 1998101600195 19981016 00195 NM 1998 10 16 CKSA98557 1 19981008 A 5310 STRUCTURE BOEING 747 7472B4B 138481B NM BS 2180-2200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 AT AND AROUND LT DUMP VALVE, FOUND WIDESPREAD LEVEL 2 CORROSION AFFECTING SKIN, STRINGER, SHEAR TIE, FRAME, RIB, DOUBLER , LOCATED AT ZONE 100, STA 2180-2200, STR44L, WL130, LBL40. REPAIR IAW BOEING DOC CKF-AMD-121, CKF-AMD-152. FOUND DURI NG ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53 -125-01-02. 2 L 7 4 4F RT A20WE 1998101600196 19981016 00196 NM 1998 10 16 CKSA98558 1 19981008 A 5315 CKFAMD0601 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1740 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 FLOORBEAM UPPER CAP CORRODED AT ZONE 260, STA 1740, WL199, LBL37. AREA APPROX 21 SQ INCHES. REPAIRED IAW BOEING AMMEND MENT CKF-AMD-034 SUPP SHEET. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMB ER MO280, CORROSION TASK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600197 19981016 00197 NM 1998 10 16 CKSA98559 1 19981008 A 5230 65B178951 CHORD BOEING 747 7472B4B 138481B NM CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 MAIN DECK CARGO DOOR UPPER CHORD CORRODED. EXTENDS UNDER HINGE. REPAIRED IAW CKF-AMD-094 SHEET 1, BAC5300, BAC5004-2. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-200-01-04. 2 L 7 4 4F RT A20WE 1998101600198 19981016 00198 NM 1998 10 16 CKSA98560 1 19981008 A 5315 0161672316 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1700 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 FLOORBEAM UPPER CAP HAS AREA OF CORROSION APPROX 1.5 BY 2, ZONE 140, STA1700, WL200, LBL40. REPAIRED IAW CKF-AMD-063 SU PP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSI ON TASK CARD NUMBER C53-210-01-03. 2 L 7 4 4F RT A20WE 1998101600199 19981016 00199 NM 1998 10 16 CKSA98561 1 19981008 A 5347 CKFAMD0661 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 2240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK CORRODED BEYOND SRM LIMITS, STA2240, RBL75, WL199, 1.5 SQ AREA. REPAIRED PER CKF-AMD-066 SHEET 1. FOUND DUR ING ACCOMPLISHMENT OF C, D CHECK, CPCP WORK CARD ACCOMPLISHMENT. WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C5 3-210-01-04. 2 L 7 4 4F RT A20WE 1998101600200 19981016 00200 NM 1998 10 16 K3HA980118 1 19981005 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 AFT AIRSTAIR LOWER EMERGENCY LIGHT INOP. REMOVED AND REPLACED LOWER AIRSTAIR LIGHT ASSEMBLY AND BATTERIES, OPS CHECK OK PER MM 33-50-0. LIGHT ASSEMBLY P/N 11-0283-3 S/N K3332, BATTERY P/N S106, S/N 192193. 2 L 7 3 4F A3WE 1998101600201 19981016 00201 NM 1998 10 16 K3HA980119 1 19981006 A 3350 11036825 SIGN BOEING 727 727225 1384077 NM FWD GALLEY INOPERATIVE A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY EXIT SIGN IN FORWARD GALLEY ILLEGIBLE. REPLACED SIGN COVER WITH SERVICEABLE UNIT GOOD PER MM 33-50-00. 2 L 7 3 4F A3WE 1998101600202 19981016 00202 WP 1998 10 16 CALA9801926 1 19981008 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 275 & 332 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND LT FUSELAGE SKIN DENTED AT STA 332 BETWEEN LONGERON 23L AND 22L AND A STA 275 BETWEEN LONGERON 23L AND 22L AND STA 313 BETWEEN LONGERON 24L AND 23L. THE DENTS WERE REPAIRED IAW SRM 53-04, FIGURE 38, SHEET 18. 2 L 7 2 4F A6WE 1998101600203 19981016 00203 WP 1998 10 16 CALA9801927 1 19981008 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR JAMB PAN CORRODED. THE CORRODED SECTION OF PAN WAS REMOVED AND A NEW SE CTION WAS INSTALLED IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 1998101600204 19981016 00204 NM 1998 10 16 CALA9801928 1 19981009 A 5753 FITTING BOEING 727 727224 1384076 NM RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT WING NR 6 AND NR 8 FLAP TRACK ATTACH FITTINGS CORRODED. THE CORROSION WAS REMOVED AND THE FITTINGS WERE REPAIRED IAW ECRA 5740-01277. 2 L 7 3 4F A3WE 1998101600205 19981016 00205 NM 1998 10 16 CALA9801929 1 19981009 A 5753 FITTING BOEING 727 727224 1384076 NM RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND THE NR 2 AND NR 3 FLAP TRACK FORWARD MOUNT FITTINGS CORRODED. THE FLAP TRACK FITTINGS WERE REPAIRED IA W ECRA 5740-01277. 2 L 7 3 4F A3WE 1998101600206 19981016 00206 NM 1998 10 16 CALA9801930 1 19981009 A 5730 SKIN BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND THE LT WING UPPER TRAILING EDGE SKIN AT CUTOUT FOR NR 4 SPOILER SECOND FROM O/B HINGE AND SECOND FROM I /B HINGE CRACKED. BOTH CRACKS WERE 5/16 LONG. THE FASTENERS WERE REMOVED IAW SRM 51-30-2. THE CRACKS WERE STOP DRILLED AND DOUBLER REPAIRS WERE INSTALLED IAW SRM 57-30-4, FIGURE 10. 2 L 7 3 4F A3WE 1998101600207 19981016 00207 NM 1998 10 16 CALA9801931 1 19981009 A 5741 651597514 FITTING BOEING 727 727224 1384076 NM BS 870 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 RIGHT WING TO FUSELAGE AT BS 870 FACE AND BORE HAVE CORROSION. ACCOMPLISHED REPAIR BY OVERSIZE HOLE TO REMOVE CORROSION PER ECRA 5310-63775. 2 L 7 3 4F A3WE 1998101600208 19981016 00208 NM 1998 10 16 CALA9801932 1 19981009 A 5755 651734866 SKIN BOEING 727 727224 1384076 NM NR 8 SPOILER WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 25803 20666 RT WING NR 8 SPOILER CENTER CHAFE PAD WORN AND TE WORN/MISSING. DENTS OUT OF LIMITS PER SRM 57-50-1 FIG 5. REMOVED SPO ILER PANEL AND SENT OUT FOR REPAIR PER MM 27-62-1. 2 L 7 3 4F A3WE 1998101600209 19981016 00209 NM 1998 10 16 CALA9801933 1 19981009 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 FLOORBEAM TOP HAS SURFACE CORROSION FS 1130 RBL 12-12. REMOVED FASTENERS. CUT OUT ANGLE DAMAGE. FABRICATED NEW ANGLE, SPLICES. FABRICATED NEW FLOORBEAM TREATED AND INSTALLED PER SRM 51-10-2 AND 51-40-3. 2 L 7 3 4F A3WE 1998101600210 19981016 00210 WP 1998 10 16 CALA9801934 1 19981009 A 3350 08164120 LIGHT DOUG DC9 DC932 3022066 WP CABIN CRACKED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 43537 47112 FWD AISLE PATH LIGHTING COVER IN FIRST CLASS NEEDS TO BE RE-SECURED. REPLACED FWD SECTION OF BASE AND END CAP ASSY. 2 L 7 2 4F A6WE 1998101600211 19981016 00211 NM 1998 10 16 CALA9801935 1 19981009 A 5730 PANEL BOEING 727 727224 1384076 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 RT WING 35 FLAP TRACK AFT INBD PANEL LEADING EDGE OF PANEL IS BENT AND TORN. BLEND OUT TORN AREA PER SRM 53-10 FIG 1 MA T LOSS .001. 2 L 7 3 4F A3WE 1998101600212 19981016 00212 NM 1998 10 16 CALA9801936 1 19981009 A 5753 ANGLE BOEING 727 727224 1384076 NM NR 5 FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 RT WING NR 5 FLAP FWD INBOARD FAIRING BRACKET CRACKED IN RADIUS .25 INCH LONG. FABRICATED ANGLE FROM 7075 T6 .063. LOCA TED, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED PER SRM 51-40-3. 2 L 7 3 4F A3WE 1998101600213 19981016 00213 NM 1998 10 16 CALA9801937 1 19981009 A 5753 FAIRING BOEING 727 727224 1384076 NM NR 4 FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 NR 4 FLAP TRACK FAIRING AFT INBOARD ANGLE IS CRACKED .5 LONG. STOP DRILLED CRACK ON NR 4 FLAP TRACK FAIRING. FABRICATE D REPAIR FROM 7075 T6 .050. LOCATED, DRILLED, DEBURRED, ALODINED, PRIMED PER SRM 51-40-3, 51-10-2, MM 51-20-12 AND INST ALLED PER SRM 51-30-2. 2 L 7 3 4F A3WE 1998101600214 19981016 00214 NM 1998 10 16 CALA9801938 1 19981011 A 3211 HOUSING BOEING 727 727224 1384076 NM LT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 LEFT SIDE AFT TRUNNION BEARING HOUSING IS PITTED. REMOVED AND REPLACED LT AFT BEARING HOUSING PER MM 32-11-0. 2 L 7 3 4F A3WE 1998101600215 19981016 00215 WP 1998 10 16 CALA9801939 1 19981011 A 5350 LATCH DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 TAIL COMPARTMENT TAILCONE OUT OF RIG. OUTSIDE HANDLE PULL LOW, DELTA TRIANGLE NOT 90 DEGREES, CATCHES ON RIGHT SIDE LAT CHES. ADJUSTED LATCH LEVER CABLES AND ADJUSTED LOWER RIGHT LATCH LEVER. PERFORMED ADJUSTMENT TEST PER MM 53-53-00. 2 L 7 2 4F A6WE 1998101600216 19981016 00216 NM 1998 10 16 CALA9801940 1 19981011 A 2530 8103010000 OVEN BOEING 737 7373T0 1384582 NM GALLEY FAILED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 77303 23354 AFT GALLEY CENTER OVEN SMOKED. REPLACED CENTER OVEN. 2 L 7 2 4F RT A16WE 1998101600217 19981016 00217 WP 1998 10 16 CALA9801941 1 19981011 A 4990 38102621 APU DOUG DC10 DC1030 3023501 WP AFT FUSELAGE LEAKING A CALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 13067 34060 1761 47866 OIL SMELL IN COCKPIT. APU INTERNAL OIL LEAK CONFIRMED. CLEANED AIRCRAFT PACKS. PLACARD APU PER MEL. 2 L 7 3 4F A22WE 1998101600218 19981016 00218 WP 1998 10 16 CALA9801942 1 19981012 A 5320 5936037501 BEAM DOUG DC9 DC982 3022082 WP BS 1193 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 CORROSION ON I-BEAM BTWN STA 1193 AND 1212 AT L-29RT. REMOVED AND REPLACED I-BEAM PER SRM 51-30-2. 2 L 7 2 4F A6WE 1998101600219 19981016 00219 EA 1998 10 16 COMA9860292 1 19981007 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA K NONE O OTHER AP APPROACH 1 SO 01 912CA 4442 800 7011 FLAPS FAILED AT 8 DEGREES. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1998101600220 19981016 00220 SO 1998 10 16 COMA9810226 1 19981005 A 3350 10130115 SIGN EMB 120 EMB120RT SO CABIN BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 168CA 120168 EXIT SIGN ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998101600221 19981016 00221 1998 10 16 COMA9810227 2 19981005 A 7200 ENGINE EMB 120 EMB120RT SO RIGHT MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 266CA 120258 RIGHT HAND ENGINE NP WAS 104 PERCENT AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. GROUND RUNS AND FLIGHT CHECK WERE SATISFACTORY. 2 L 7 2 4T RT A31SO 1998101600222 19981016 00222 SO 1998 10 16 COMA9810228 1 19981006 A 5246 DOOR EMB 120 EMB120RT SO FUEL SERVICE NOT LATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 256CA 120245 SERVICE DOOR WARNING DURING TAKEOFF. SECURED LATCHES ON SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998101600223 19981016 00223 SO 1998 10 16 COMA9810229 1 19981007 A 2897 1C717 WIRE HARNESS EMB 120 EMB120RT SO RT BOOST PUMP OUT OF POSITION A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 DURING 2C INSPECTION, TASK 5720-622-01I, REVEALED THE WIRE HARNESS FOR THE RIGHT WING FORWARD FUEL BOOST PUMP TO BE CHAF FING ON THE METAL BRAIDED FUEL LINE. PUMP WIRE INSULATION WAS NOT DAMAGED ONLY WIRE HARNESS PROTECTIVE COVERING. REMOV ED PUMP AND HARNESS AND INSTALLED SERVICEABLE PUMP MAKING SURE THE WIRE HARNESS WAS CLEAR OF ALL STRUCTURE AND FUEL LINE S. 2 L 7 2 4T RT A31SO 1998101600224 19981016 00224 SO 1998 10 16 COMA9810230 1 19981008 A 5320 12046963001 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT FORWARD BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEABLE BUTTSTRAP USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998101600225 19981016 00225 SO 1998 10 16 COMA9810231 1 19981008 A 5320 12027929001 BUTTSTRAP EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 DURING 2C INSPECTION TASK 151-01Z REVEALED LEFT NR 5 BUTTSTRAP TO BE CORRODED. REMOVED BUTTSTRAP AND INSTALLED SERVICEA BLE BUTTSTRAP USING EMB 120 STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998101600226 19981016 00226 SO 1998 10 16 COMA9810232 1 19981008 A 5320 12005803001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 DURING 2C INSPECTION TASK 5310-131-01I REVEALED RIGHT NR 1 SILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998101600227 19981016 00227 SO 1998 10 16 COMA9810233 1 19981008 A 5320 12005802001 SILL EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT NR 1 STILL TO BE CORRODED. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998101600228 19981016 00228 SO 1998 10 16 COMA9810235 1 19981008 A 5320 12006962001 CROSSBEAM EMB 120 EMB120RT SO CABIN CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 DURING 2C INSPECTION, TASK 5310-131-01I REVEALED LEFT CENTER CROSSBEAM TO BE CORRODED AT FRAME 16. REMOVED AND REPLACED CROSSBEAM USING EMB 120 SRM STANDARD PRACTICES. 2 L 7 2 4T RT A31SO 1998101600229 19981016 00229 SO 1998 10 16 COMA9810236 1 19981006 A 5320 12007089003 BUTTPLATE EMB 120 EMB120RT SO FUSELAGE CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 247CA 120225 DURING 2C INSPECTION TASK 5310-131-O1I REVEALED CENTER BUTTPLATE TO HAVE SPOTS OF CORROSION THAT WERE BEYOND LIMITS. RE MOVED CENTER BUTTPLATE AND INSTALLED SERVICEABLE BUTTPLATE USING EMB120 SRM STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1. 2 L 7 2 4T RT A31SO 1998101600230 19981016 00230 NE 1998 10 16 SWAA982196 2 19980924 A 7200 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 1 FOD A SWAA E C ENGINE SHUTDOWN ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SW 07 607SW 27927 ABORTED TO TAKEOFF DUE TO AS POWER WAS APPLIED DURING TAKEOFF ROLL, A LARGE BANG TYPE NOISE WAS HEARD, SUSPECTED FOD. T HE AIRCRAFT WAS STOPPED AND RETURNED TO THE GATE. MAXIMUM SPEED REACHED ON TAKEOFF ROLL APPROX 15 MPH. ALL ENGINE INST RUMENT WERE NORMAL WITH INDICATIONS. PERFORMED ENG INSP PER BOEING MM. NO DAMAGE NOTED. SUSPECT FOD INGESTION NR 1 (S TYROFOAM) NR 1 ENG ON 10 CYCLE FLYBACK FOR BOROSCOPE INSP. BOROSCOPE INSPECTION PER BOEING MM. NO DEFECTS NOTED PER S AM 451. OK TO CONTINUE.(LP215646) 2 L 7 2 4F 4 F RT A16WE E2GL 1998101600231 19981016 00231 NM 1998 10 16 SWAA982197 1 19980927 A 5270 TARGET BOEING 737 7373H4 1384600 NM CARGO DOOR OUT OF ADJUST A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 394SW 27380 AIR TURNBACK DUE TO FWD CARGO LIGHT ILLUMINATED ON ROTATION. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND TARGET OUT OF ADJUSTMENT, RE-ALIGNED TARGET PER BOEING MM. OPS CHECK OK. (LP 87022) 2 L 7 2 4F RT A16WE 1998101600232 19981016 00232 NM 1998 10 16 SWAA982198 1 19980925 A 5610 WINDOW BOEING 737 7372H4 138448C NM LT COCKPIT LIGHTNING STRIKE A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 090SW 22905 AIR TURNBACK DUE TO ACFT SUSTAINED A LIGHTNING STRIKE TO CAPTS SIDE WINDOW ARE ON CLIMB-OUT OF SLC. AVIONICS AND FLIGHT INSTRUMENTS APPEAR NORMAL. AIRCRAFT MADE AN UNEVENTFUL LANDING. PERFORM LIGHTNING STRIKE INSPECTION PER BOEING MM. 2 L 7 2 4F A16WE 1998101600233 19981016 00233 NM 1998 10 16 SWAA982199 1 19980923 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND FWD EGRESS FLOOR TRACK HAS ONE RED LIGHT INOP. REPLACED LIGHT ASSY PER BOEING MM. 2 L 7 2 4F A16WE 1998101600234 19981016 00234 NM 1998 10 16 SWAA982200 1 19980923 A 5320 STANCHION BOEING 737 7372H4 138448C NM BS 298 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND LT FWD STANCHION HAS HFEC INDICATION OF A CRACK AT BS 298, LBL 25 INDB FASTENER 2ND F ROM BOTTOM. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998101600235 19981016 00235 NM 1998 10 16 SWAA982201 1 19980923 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 931 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C2 CHECK, FOUND FUSE SKIN CRACKED AT BS 931, STR 21R, CONFIRMED BY EDDY CURRENT. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1998101600236 19981016 00236 NM 1998 10 16 SWAA982202 1 19980923 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379SW 26586 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHT INOP ROW 20. RELAMPED OPS GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600237 19981016 00237 NM 1998 10 16 SWAA982203 1 19980923 A 5330 SKIN BOEING 737 7373H4 1384600 NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND AFT CARGO BAY, FLOORBEAM STRAP CORRODED AT BS 859, RBL 20, LBL 20, WL 156. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600238 19981016 00238 NM 1998 10 16 SWAA982204 1 19980923 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 379 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 379, 4 BELOW STR 17 RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600239 19981016 00239 NM 1998 10 16 SWAA982205 1 19980923 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 569 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND RT SKATE ANGLE CRACKED AT BS 569, RBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600240 19981016 00240 NM 1998 10 16 SWAA982206 1 19980923 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND GOUGE SKIN AT BS 500+18, 1 BELOW STR 22 RT. REPAIR PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600241 19981016 00241 NM 1998 10 16 SWAA982207 1 19980923 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 206 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT SHEAR TIE BS 206, WL 173, 5 BELOW STR 24L. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998101600242 19981016 00242 NM 1998 10 16 SWAA982208 1 19980923 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 569 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND LT SKATE ANGLE CRACKED AT BS 569, LBL 48, WL 173. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600243 19981016 00243 NM 1998 10 16 SWAA982209 1 19980923 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 535.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED WEB SUPPORT ANGLE AT BS 535.5, LBL 51, WL 175. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600244 19981016 00244 NM 1998 10 16 SWAA982210 1 19980923 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 384 & 387 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND TWO DENTED SKIN AT BS 384, 5.6 ABOVE STR 21 RT AND BS 387 1 ABOVE STR 21 RT. REPAIRED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600245 19981016 00245 NM 1998 10 16 SWAA982211 1 19980923 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 377 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 377, STR 22 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600246 19981016 00246 NM 1998 10 16 SWAA982212 1 19980923 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 914 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND SKIN CREASED AT BS 914, 4 ABOVE STR 25 RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600247 19981016 00247 NM 1998 10 16 SWAA982213 1 19980924 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500A+9.5 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND GOUGED SKIN AT BS 500A+9.5, 3 BELOW STR 22L, WL 170. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998101600248 19981016 00248 NM 1998 10 16 SWAA982214 1 19980924 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 500D CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 500 D STR 19 LT AND RT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600249 19981016 00249 NM 1998 10 16 SWAA982215 1 19980924 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1136 BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND OUTER SKIN BENT AT BS 1136, WL 240 LT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600250 19981016 00250 NM 1998 10 16 SWAA982216 1 19980924 A 5320 FRAME BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND AFT GALLEY DOOR FRAME 4 Z-ANGLES CORRODED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600251 19981016 00251 NM 1998 10 16 SWAA982222 1 19980924 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827/867/907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 LT, 8LT AT BS 907, BS 867 A ND BS 827. REPAIRED PER BOEING TI-6553-072. 2 L 7 2 4F RT A16WE 1998101600252 19981016 00252 NM 1998 10 16 SWAA982217 1 19980924 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 480/500/747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 LT, 8LT AT BS 747, BS 500A, AND 480. REPAIRED PER BOEING TI-653-072. 2 L 7 2 4F RT A16WE 1998101600253 19981016 00253 NM 1998 10 16 SWAA982218 1 19980924 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400/440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 LT, 8LT AT BS440, AND BS 40 0. REPAIRED PER BOEING TI-653-072. 2 L 7 2 4F RT A16WE 1998101600254 19981016 00254 NM 1998 10 16 SWAA982219 1 19980924 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 480/727/867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 RT, 8 RT AT BS 867, BS 727D AND BS 480. REPAIRED PER BOEING TI-630-072. 2 L 7 2 4F RT A16WE 1998101600255 19981016 00255 NM 1998 10 16 SWAA982220 1 19980924 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT HAT RACK ATTACH BRACKET BETWEEN STRINGERS 9 RT, 8 RT AT BS 440. REPAIR ED PER BOEING TI-630-072. 2 L 7 2 4F RT A16WE 1998101600256 19981016 00256 NM 1998 10 16 SWAA982221 1 19980924 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR WEB AT BS 1016, RBL 14, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600257 19981016 00257 NM 1998 10 16 SWAA982223 1 19980924 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CRACKED AT FLOORBOARD FASTENER HOLE AT BS 947 LBL 53, WL 208. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998101600258 19981016 00258 NM 1998 10 16 SWAA982224 1 19980924 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 943 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND SHEAR WEB UPPER ATTACH L-ANGLE CRACKED AT BS 943, WL 208, BL0. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600259 19981016 00259 NM 1998 10 16 SWAA982225 1 19980924 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 270 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED AT BS 270 Z-CHORD FROM LBL 11, RBL 11M WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600260 19981016 00260 NM 1998 10 16 SWAA982226 1 19980924 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CORRODED AT BS 986.5 FLOORBEAM FASTENER HOLES LBL 5, 35.5 RBL 4.5, 31, 39, WL 208 AND 20 7. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600261 19981016 00261 NM 1998 10 16 SWAA982227 1 19980923 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED AT BS 986.5 FLOORBEAM FASTENER HOLES LBL 5, 35.5 RBL 4.5, 31, 39, WL 208 AND 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600262 19981016 00262 NM 1998 10 16 SWAA982228 1 19980923 A 5320 STANDOFF BOEING 737 7373H4 1384600 NM BS 987 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND BROKEN STANDOFF ON LWR FLANGE AT BS 987 FLOORBEAM LBL 8, WL 200. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600263 19981016 00263 NM 1998 10 16 SWAA982229 1 19980923 A 5320 CREASE BEAM BOEING 737 7373H4 1384600 NM BS 947-987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED CREASE BEAM WEB AT BS 947-987 WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600264 19981016 00264 NM 1998 10 16 SWAA982230 1 19980923 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT FASTENER HOLES BS 727 TO 773, RBL 3, WL 160. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600265 19981016 00265 NM 1998 10 16 SWAA982231 1 19980924 A 3350 LIGHT BOEING 737 7373Q8 1384670 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 687SW 23388 DURING SCHEDULED SERVICE CHECK, FOUND OVER HEAD EMERGENCY LIGHT INOP, RT SIDE 4E. RELAMPED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600266 19981016 00266 NM 1998 10 16 SWAA982232 1 19980925 A 3350 BATTERY PACK BOEING 737 7373T0 1384582 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED SERVICE CHECK, FOUND FWD EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED FWD BATTERY PACK AND BASE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600267 19981016 00267 NM 1998 10 16 SWAA982233 1 19980925 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM 2 L 7 2 4F RT A16WE 1998101600268 19981016 00268 NM 1998 10 16 SWAA982234 1 19980925 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT CRACKED AT BS 540, RBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM 2 L 7 2 4F RT A16WE 1998101600269 19981016 00269 NM 1998 10 16 SWAA982235 1 19980925 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 300-328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND NUMEROUS UPPER SURFACE CORRODED AT I/B SIDE THRESHOLD ANGLE SUPPORT AT BS 300-328, RBL 5 6.5-59, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600270 19981016 00270 NM 1998 10 16 SWAA982236 1 19980926 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C1 CHECK, FOUND R-1 DOOR LOWER EMERGENCY EXIT SIGN IS UNSECURED. REMOVED AND REPLACED LIGHT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600271 19981016 00271 NM 1998 10 16 SWAA982237 1 19980925 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED STRAP AT BS 1016, LBL 3, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600272 19981016 00272 NM 1998 10 16 SWAA982238 1 19980925 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 1015 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED INTERCOSTAL AT BS 1015, LBL 37, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600273 19981016 00273 NM 1998 10 16 SWAA982239 1 19980925 A 5320 MOUNT BOEING 737 7373H4 1384600 NM BS 1012 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED AFT LAV MOUNT AT BS 1012, LBL 38, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600274 19981016 00274 NM 1998 10 16 SWAA982240 1 19980925 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AT BS 986, LBL 14, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600275 19981016 00275 NM 1998 10 16 SWAA982241 1 19980925 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL WEB CRACKED AT FASTENER LOCATION BS 312, RBL 1.5, WL 208. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998101600276 19981016 00276 NM 1998 10 16 SWAA982242 1 19980925 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 314.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL STRAP CRACKED AT BS 314.5, RBL 33, WL 200. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600277 19981016 00277 NM 1998 10 16 SWAA982243 1 19980925 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FLOORBEAM AROUND FASTENER LOCATIONS AT BS 328, WL 208, RBL 11. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600278 19981016 00278 NM 1998 10 16 SWAA982244 1 19980925 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND DAMAGED AT NUTPLATE LOCATIONS BS 312, RBL 1-12, WL 208 ON FLOORBEAM UPPER CHORD. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600279 19981016 00279 NM 1998 10 16 SWAA982245 1 19980925 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND LONGITUDINAL STRAP CRACKED AT WL 200, LBL 10 BS 312. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600280 19981016 00280 NM 1998 10 16 SWAA982246 1 19980925 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 326.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL WEB CRACKED AT BS 326.5, LBL 45, WL 208. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998101600281 19981016 00281 NM 1998 10 16 SWAA982247 1 19980925 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 344 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FLOORBEAM DAMAGED AT NUTPLATE BS 344, WL 208, LBL 28-48. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998101600282 19981016 00282 NM 1998 10 16 SWAA982248 1 19980925 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FLOORBEAM DAMAGED AT NUTPLATE BS 360, WL 208, RBL 52. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998101600283 19981016 00283 NM 1998 10 16 SWAA982249 1 19980925 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 994 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED OUTBOARD CHORD ANGLE ON THRESHOLD AT BS 994, RBL 51, WL 208. 2 L 7 2 4F RT A16WE 1998101600284 19981016 00284 NM 1998 10 16 SWAA982250 1 19980925 A 5330 SKIN BOEING 737 7373H4 1384600 NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FWD GALLEY SERVICE DOORWAY CRACKED AT SKIN CUTOUT LOWER AFT CORNER. REMOVED AND REPLACE D PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600285 19981016 00285 NM 1998 10 16 SWAA982251 1 19980925 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 380-400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CRACKED AT BS 380-400, WL 208, BL 0. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600286 19981016 00286 NM 1998 10 16 SWAA982252 1 19980925 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540, RBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600287 19981016 00287 NM 1998 10 16 SWAA982253 1 19980925 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FLOOR SUPPORT AT BS 540, LBL 1, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600288 19981016 00288 NM 1998 10 16 SWAA982254 1 19980925 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND OF BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 6.7, WL 212. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600289 19981016 00289 NM 1998 10 16 SWAA982255 1 19980925 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD SIDE CHORD RT SIDE CRACKED AT WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600290 19981016 00290 NM 1998 10 16 SWAA982256 1 19980925 A 5312 BULKHEAD WEB BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT LBL .5, RBL .5, WL 187. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600291 19981016 00291 NM 1998 10 16 SWAA982257 1 19980925 A 5312 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD SIDE CHORD LT SIDE CRACKED AT WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600292 19981016 00292 NM 1998 10 16 SWAA982258 1 19980926 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 180 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FLOOR WEB BS 180, WL 207, RBL 27 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998101600293 19981016 00293 NM 1998 10 16 SWAA982259 1 19980926 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 486 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FWD CARGO BAY AFT DOOR FRAME COVER PLATE WEB DAMAGED AT BS 486, WL 158, RBL 26. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600294 19981016 00294 NM 1998 10 16 SWAA982260 1 19980926 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 344 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FWD CARGO BAY AFT DOOR FRAME COVER PLATE WEB DAMAGED AT BS 344, RBL 26, WL 158. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600295 19981016 00295 NM 1998 10 16 SWAA982261 1 19980926 A 5320 BRACKET BOEING 737 7373H4 1384600 NM LANDING GEAR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND LT STABILIZER LINK LOWER PANEL L BRACKET CORRODED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600296 19981016 00296 NM 1998 10 16 SWAA982262 1 19980926 A 5320 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 312 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FLOORBEAM AT BS 312 DAMAGED FASTENER HOLES ON VERTICAL WEB FROM LBL 16 TO RBL 8, WL 207. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600297 19981016 00297 NM 1998 10 16 SWAA982263 1 19980926 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 296 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FWD SERVICE DOOR FLOOR WEB AT BS 296, RBL 56, WL 208.5. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600298 19981016 00298 NM 1998 10 16 SWAA982264 1 19980926 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 1006 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED WEB AT BS 1006, LBL 39, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600299 19981016 00299 NM 1998 10 16 SWAA982265 1 19980926 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1010-1013 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND TWO GOUGES ON FUSELAGE SKIN AT BS 1010 AND 1013, 2 BELOW STR 11R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600300 19981016 00300 NM 1998 10 16 SWAA982266 1 19980926 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 794 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED AFT CARGO DOOR CUTOUT FWD FRAME AT BS 794, RBL 42 TO 47, WL 167 TO 171 AROUN D LATCH FITTING. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600301 19981016 00301 NM 1998 10 16 SWAA982267 1 19980926 A 5320 DOUBLER BOEING 737 7373H4 1384600 NM CARGO DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FWD UPPER CORNER OF AFT CARGO DOOR CUTOUT BS 798, RBL 70, WL 195. REMOVED A ND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600302 19981016 00302 NM 1998 10 16 SWAA982269 1 19980926 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FASTENERS ON FLOORBEAM SUPPORT STRAP AT BS 860, WL 160, RBL 20 TO LBL 20. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600303 19981016 00303 NM 1998 10 16 SWAA982270 1 19980926 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED CARGO FLOORBEAM AT FASTENER HOLES BS 727 TO 773, RBL 8, WL 160. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600304 19981016 00304 NM 1998 10 16 SWAA982271 1 19980926 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 727-773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED CARGO FLOORBEAM AT FASTENER HOLES BS 727 TO 773, LBL 12, WL 10. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600305 19981016 00305 NM 1998 10 16 SWAA982272 1 19980926 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED ON SHEAR TIE UNDER FRAME TO KEEL BEAM CLIP AT BS 767, RBL 8, WL 150. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600306 19981016 00306 NM 1998 10 16 SWAA982273 1 19980926 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED ON SHEAR TIE BS 727E, LBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600307 19981016 00307 NM 1998 10 16 SWAA982274 1 19980926 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 7270 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND MISDRILLED HOLE ON FLOORBEAM AT BS 7270+5, LBL 17, WL 160. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600308 19981016 00308 NM 1998 10 16 SWAA982268 1 19980926 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 867-877 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND COMBINED TWO PREVIOUS SKIN REPAIRS INTO ONE REPAIR AT BS 867-877, STR 18R-20R. REPA IRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600309 19981016 00309 NM 1998 10 16 SWAA982275 1 19980926 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 950 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 950, RBL 26 TO 44, WL 208. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998101600310 19981016 00310 NM 1998 10 16 SWAA982276 1 19980926 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 950 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 950, RBL 46 TO 52, WL 208. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998101600311 19981016 00311 NM 1998 10 16 SWAA982277 1 19980926 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 967 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 967, RBL 5-41.5, WL 208. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998101600312 19981016 00312 NM 1998 10 16 SWAA982278 1 19980926 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOORBEAM AT BS 987, RBL 1-40, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600313 19981016 00313 NM 1998 10 16 SWAA982279 1 19980927 A 3350 SOCKET BOEING 737 7373H4 1384600 NM CABIN UNPLUGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 651SW 27721 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 14-18 INOPERATIVES. FOUND SOCKET ASSY UNPLUGED AT ROW 14, RESECURED PLUG PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600314 19981016 00314 NM 1998 10 16 SWAA982280 1 19980925 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 397 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND DENTED FUSELAGE SKIN AT BS 397, 2 BELOW STRINGER 15L. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998101600315 19981016 00315 NM 1998 10 16 SWAA982281 1 19980927 A 5230 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO PIT DOOR INTERCOSTAL CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600316 19981016 00316 NM 1998 10 16 SWAA982282 1 19980926 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM RBL39, BS 294.5. RREPAIRED PER TI-A53-014. 2 L 7 2 4F RT A16WE 1998101600317 19981016 00317 NM 1998 10 16 SWAA982283 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND ANGLE CRACKED O/B OF RT RAM AIR INLET BS 540. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600318 19981016 00318 NM 1998 10 16 SWAA982284 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE CORRODED AT BS 500A TO 500D. REMOVED AND REPLACED PER BOEING SRM . REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600319 19981016 00319 NM 1998 10 16 SWAA982285 1 19980926 A 5320 CLIP BOEING 737 7373Y0 1384671 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CLIP CRACKED AT BS 400, STR 28L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600320 19981016 00320 NM 1998 10 16 SWAA982286 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 767-797 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 767-797. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600321 19981016 00321 NM 1998 10 16 SWAA982287 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 847-867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 847-867. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600322 19981016 00322 NM 1998 10 16 SWAA982288 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 867-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED RT TRANSITION ANGLE AT BS 867-947. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600323 19981016 00323 NM 1998 10 16 SWAA982289 1 19980926 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM BS 967-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 967-986.5 LBL 17. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600324 19981016 00324 NM 1998 10 16 SWAA982290 1 19980926 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM BS 967-986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 967-986.5 RBL 18. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600325 19981016 00325 NM 1998 10 16 SWAA982291 1 19980927 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM BS 962 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT BS 962 RBL 13. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600326 19981016 00326 NM 1998 10 16 SWAA982292 1 19980926 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE AT BS 986.5, RBL 28 FWD FLANGE. REPAIRED PER TI-A53 -014. 2 L 7 2 4F RT A16WE 1998101600327 19981016 00327 NM 1998 10 16 SWAA982293 1 19980926 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE AT BS 986.5, RBL 15 FWD FLANGE. REPAIRED PER TI-A53 -014. 2 L 7 2 4F RT A16WE 1998101600328 19981016 00328 NM 1998 10 16 SWAA982294 1 19980926 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE AT BS 986.5, LBL 7 FWD FLANGE. REPAIRED PER TI-A53- 014. 2 L 7 2 4F RT A16WE 1998101600329 19981016 00329 NM 1998 10 16 SWAA982295 1 19980926 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE AT BS 986.5, RBL 43 FWD FLANGE. REPAIRED PER TI-A53 -014. 2 L 7 2 4F RT A16WE 1998101600330 19981016 00330 NM 1998 10 16 SWAA982296 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 927-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND UPPER WEB ANGLE CRACKED AT BS 927-947 BL0. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600331 19981016 00331 NM 1998 10 16 SWAA982297 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM E & E COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND LT E1-2 RACK SUPPORT ANGLE CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600332 19981016 00332 NM 1998 10 16 SWAA982298 1 19980926 A 5320 STRAP BOEING 737 7373Y0 1384671 NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND STABILIZER STRAP CRACKED AT BS 312, LBL 12. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600333 19981016 00333 NM 1998 10 16 SWAA982299 1 19980926 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 727-767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED TRANSITION ANGLE RT AT BS 727D-767. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600334 19981016 00334 NM 1998 10 16 SWAA982300 1 19980927 A 5312 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD AT RBL 5, WL 199, FWD SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600335 19981016 00335 NM 1998 10 16 SWAA982301 1 19980927 A 5312 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD AT RBL 5, WL 202, FWD SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600336 19981016 00336 NM 1998 10 16 SWAA982302 1 19980927 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL AFT SIDE OF BULKHEAD WL 195, LBL 26. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998101600337 19981016 00337 NM 1998 10 16 SWAA982303 1 19980927 A 5315 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED BULKHEAD AT LBL 5, WL 199, FWD SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600338 19981016 00338 NM 1998 10 16 SWAA982304 1 19980927 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 986 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE AT BS 986.5, RBL 8 FWD FLANGE. REPAIRED PER TI-A53- 014. 2 L 7 2 4F RT A16WE 1998101600339 19981016 00339 NM 1998 10 16 SWAA982305 1 19980928 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM RBL 28 BS 328. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600340 19981016 00340 NM 1998 10 16 SWAA982306 1 19980928 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM RBL 35 BS 328. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600341 19981016 00341 NM 1998 10 16 SWAA982307 1 19980928 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 813 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED NUT PLATES ACROSS FLOORBEAM AT BS 813. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600342 19981016 00342 NM 1998 10 16 SWAA982308 1 19980928 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 754 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM NUT PLATES AND BEAM SURFACE AT BS 754. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600343 19981016 00343 NM 1998 10 16 SWAA982309 1 19980928 A 5320 FRAME BOEING 737 7373Y0 1384671 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND WEB DAMAGED FWD OF DOOR FRAME AND STR 20R. REPAIRED PER TI-A53-039. 2 L 7 2 4F RT A16WE 1998101600344 19981016 00344 NM 1998 10 16 SWAA982311 1 19980928 A 5320 FRAME BOEING 737 7373Y0 1384671 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND FRAME CRACKED FWD DOOR FRAME CUTOUT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600345 19981016 00345 NM 1998 10 16 SWAA982312 1 19980928 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM CLIP NUT HOLE AT BS 1016, LBL 7. REPAIRED PER TI-A53-014. 2 L 7 2 4F RT A16WE 1998101600346 19981016 00346 NM 1998 10 16 SWAA982313 1 19980928 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM AFT GALLEY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT LBL 9 CLIP NUT HOLE. REPAIRED PER TE-A53-014. 2 L 7 2 4F RT A16WE 1998101600347 19981016 00347 NM 1998 10 16 SWAA982314 1 19980928 A 5330 SKIN BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND HFEC INDICATION OF 1.0 CRACKED SKIN AT BS 178, LBL 7, WL 213. REPAIRED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998101600348 19981016 00348 NM 1998 10 16 SWAA982315 1 19980928 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 311SW 23333 DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED ABOVE LT WING ILLUMINATION LIGHT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600349 19981016 00349 NM 1998 10 16 SWAA982316 1 19980929 A 2797 WIRE BOEING 737 7373H4 1384600 NM NR 1 LE FLAP BROKEN A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 309SW 22948 AIR TURNBACK DUE TO NR 1 KREUGER FLAP TRANSIT LIGHT LE FLAPS TRANSIT LIGHT ON WHEN FLAPS SELECTED UP RE-CYCLED, NO HELP. ALL INDICATIONS OK WHEN SELECTED DOWN. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND GROUND WIRE TO NR 1 KREUGER FLAP B ROKEN. INSTALLED NEW GROUND TERMINAL END PER BOEING MM. NO DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1998101600350 19981016 00350 NM 1998 10 16 SWAA982310 1 19980929 A 5270 GROUND STUD BOEING 737 7373H4 1384600 NM CARGO DOOR LOOSE A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 652SW 27722 AIR TURNBACK DUE TO FWD CARGO DOOR LIGHT CAME ON AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND DOOR SWITCH GROUND STUD LOOSE, MOVED GROUND TERMINAL FROM GROUND STUD NR GD00200A TO NR GD01008D. OPS CHECK GOOD AS PER BOEING MM. (LP 185388) 2 L 7 2 4F RT A16WE 1998101600351 19981016 00351 NM 1998 10 16 SWAA982317 1 19980929 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 860-887 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND SKIN WEAR COMMON TO DORSAL FIN AT BS 860-887, WL 306.5. ACCOMPLISHED REPAIR PER ACO NR 6738-55. 2 L 7 2 4F RT A16WE 1998101600352 19981016 00352 NM 1998 10 16 SWAA982318 1 19980929 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 535 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND CHAFING DAMAGE ON WEB AT BS 535, BL 53, WL 175. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600353 19981016 00353 NM 1998 10 16 SWAA982319 1 19980929 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 787-794 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLE ON INTERCOSTAL AT BS 787-794.3, RBL 24, WL 155. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998101600354 19981016 00354 NM 1998 10 16 SWAA982320 1 19980929 A 5343 FITTING BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FOUND ON RT MLG BEAM I/B ATTACH FITTING AROUND BUSHING FACES. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600355 19981016 00355 NM 1998 10 16 SWAA982321 1 19980929 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 767-867 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLES ON STRAP AT BS 767-867, RBL 24. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998101600356 19981016 00356 NM 1998 10 16 SWAA982322 1 19980929 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 840-867 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLES ON SHIM STRAP AT BS 840-867, RBL 24 . REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600357 19981016 00357 NM 1998 10 16 SWAA982323 1 19980929 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM BL0, BS 312. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600358 19981016 00358 NM 1998 10 16 SWAA982324 1 19980929 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM RBL 8, BS 312. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600359 19981016 00359 NM 1998 10 16 SWAA982325 1 19980929 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 38920 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM RBL 11, BS 312. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600360 19981016 00360 NM 1998 10 16 SWAA982326 1 19980929 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM RBL 21, BS 312. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600361 19981016 00361 NM 1998 10 16 SWAA982327 1 19980929 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM LBL 7, BS 312. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600362 19981016 00362 NM 1998 10 16 SWAA982328 1 19980929 A 5330 SKIN BOEING 737 7373Y0 1384671 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 38920 DURING SCHEDULED 1/2D CHECK, FOUND OUTER SKIN CRACKED AT LOWER HINGE CUTOUT EXTENDED ALONG UPPER SKIN OVERLAP. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600363 19981016 00363 NM 1998 10 16 SWAA982329 1 19980929 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 772 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UNDERNEATH STRAP AT BS 772, RBL 12. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998101600364 19981016 00364 NM 1998 10 16 SWAA982330 1 19980929 A 5320 STRAP BOEING 737 7373Y0 1384671 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED STABILIZER STRAP AT BS 344, LBL 48. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600365 19981016 00365 NM 1998 10 16 SWAA982331 1 19980929 A 5320 STANCHION BOEING 737 7373Y0 1384671 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND E-1 RACK RT FWD STANCHION CRACKED AT BS 294.5 UPPER BULKHEAD ATTACH ANGLE INBD FASTNE R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600366 19981016 00366 NM 1998 10 16 SWAA982332 1 19980929 A 5320 WEB BOEING 737 7373Y0 1384671 NM BS 795 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND WEB FWD DOOR OPENING DAMAGED AT BS 795, RBL 30. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600367 19981016 00367 NM 1998 10 16 SWAA982333 1 19980929 A 5320 WEB BOEING 737 7373Y0 1384671 NM BS 994-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED WEB BETWEEN BS 994 - 1016, LBL 38. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600368 19981016 00368 NM 1998 10 16 SWAA982334 1 19980929 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM BS 1006-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED INTERCOSTAL AT LBL 37.21, BS 1006-1016 ON UPPER AND LWR SURFACES. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600369 19981016 00369 NM 1998 10 16 SWAA982335 1 19980930 A 5320 CLIP BOEING 737 7373Y0 1384671 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND TIE CLIP CRACKED AT FASTENER BS 663. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600370 19981016 00370 NM 1998 10 16 SWAA982336 1 19980930 A 5311 FRAME BOEING 737 7373Y0 1384671 NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND FRAME AT BS 294.5 CRACKED AT FLOOR LEVEL (FWD OF FWD SERVICE DOOR). REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998101600371 19981016 00371 NM 1998 10 16 SWAA982337 1 19980930 A 5320 FRAME BOEING 737 7373Y0 1384671 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND DOOR FRAME CRACKED ALONG FWD EDGE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600372 19981016 00372 NM 1998 10 16 SWAA982338 1 19980930 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 490 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE CORRODED AT BS 490 TO 500A. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600373 19981016 00373 NM 1998 10 16 SWAA982339 1 19980930 A 5320 HOUSING BOEING 737 7373Y0 1384671 NM BS 382 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND DRAIN PLUG HOUSING CRACKED AT BS 382 BETWEEN STR 28R AND STR 27R. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600374 19981016 00374 NM 1998 10 16 SWAA982340 1 19980930 A 5320 CLIP BOEING 737 7373Y0 1384671 NM CARGO COMPT DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE ATTACH CLIP DAMAGED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600375 19981016 00375 NM 1998 10 16 SWAA982341 1 19980930 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 294 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND EVIDENCE OF CRACKED ANGLE AT FLOOR WEB ANGLE BS 294 FWD DOOR STUB FRAME. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600376 19981016 00376 NM 1998 10 16 SWAA982342 1 19980930 A 5320 WEB BOEING 737 7373Y0 1384671 NM BS 665 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND LT MLG W/W CEILING WEB CRACKED AT BS 665, LBL 31.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600377 19981016 00377 NM 1998 10 16 SWAA982343 1 19980930 A 5312 BULKHEAD SKIN BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED 178 BULKHEAD SKIN AT BS 178, RBL 1, WL 188 AFT SIDE. REMOVED AND REPLACED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600378 19981016 00378 NM 1998 10 16 SWAA982344 1 19980930 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 301 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND L ANGLE CRACKED AT BS 301, LBL 56, WL 257. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600379 19981016 00379 NM 1998 10 16 SWAA982345 1 19980930 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4RT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600380 19981016 00380 NM 1998 10 16 SWAA982346 1 19980930 A 5320 COLLAR BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND FASTENER COLLAR CRACKED AT RT I/B FWD SIDE OF FRAME SPLICE AT BS 727 STRINGER NR 13 WL 2 37. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600381 19981016 00381 NM 1998 10 16 SWAA982347 1 19980930 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND INBOARD FRAME CHORD CRACKED AT BS 616, LBL 64, WL 201. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600382 19981016 00382 NM 1998 10 16 SWAA982348 1 19980930 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED AT BS 663, STR 10 LT AND RT. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998101600383 19981016 00383 NM 1998 10 16 SWAA982349 1 19980930 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 359 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 359, STR 14 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600384 19981016 00384 NM 1998 10 16 SWAA982350 1 19980930 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 294-298 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL CRACKED AT BS 294-298, STR 16 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600385 19981016 00385 NM 1998 10 16 SWAA982351 1 19980930 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 293 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 293, STR 11 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600386 19981016 00386 NM 1998 10 16 SWAA982352 1 19980930 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 863 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 341SW 24091 DURING SCHEDULED D CHECK, FOUND GOUGED SKIN AT BS 863, STR 1. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600387 19981016 00387 NM 1998 10 16 SWAA982353 1 19981001 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED RON CHECK, FOUND 4 IN SKIN CRACKED AT RT SIDE ABOVE CABIN WINDOWS 11 AND 12 BS STA 500C STR 10R. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600388 19981016 00388 NM 1998 10 16 SWAA982354 1 19981001 A 5320 BRACKET BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED C1 CHECK, FOUND CARGO DOOR UPLATCH BRACKET INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998101600389 19981016 00389 NM 1998 10 16 SWAA982355 1 19981001 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED RON CHECK, FOUND ONE EGRESS LIGHT AT ROW 5 INOPERATIVE. REPLACED BULB PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600390 19981016 00390 NM 1998 10 16 SWAA982356 1 19981001 A 3350 LAMP BOEING 737 7373H4 1384600 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 356SW 25251 DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT FLOOR LEVEL LIGHT AT RT OVERWING EXIT BROKEN. REMOVED AND REPLACED LAM P ASSEMBLY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600391 19981016 00391 NM 1998 10 16 SWAA982357 1 19981001 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FWD CARGO PIT FLOOR SUPPORT STRAP AT BS 500+4, LBL 13, LBL 15.5, WL 156.5. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600392 19981016 00392 NM 1998 10 16 SWAA982358 1 19981001 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM PAX DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FWD ENTRY Z ANGLE. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600393 19981016 00393 NM 1998 10 16 SWAA982359 1 19981001 A 5320 WEB BOEING 737 7373Y0 1384671 NM BS 326 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT LBL 44.5 BS 326. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600394 19981016 00394 NM 1998 10 16 SWAA982360 1 19981001 A 5320 WEB BOEING 737 7373Y0 1384671 NM BS 326 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND WEB CRACKED AT RBL 31, BS 326. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600395 19981016 00395 NM 1998 10 16 SWAA982362 1 19981001 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL ATTACH ANGLE CRACKED AT FLOORBEAM WEB AT BS 520 BL 0. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600396 19981016 00396 NM 1998 10 16 SWAA982363 1 19981001 A 5312 BULKHEAD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AFT SIDE OF BLKHD WL 195, RBL 26. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998101600397 19981016 00397 NM 1998 10 16 SWAA982364 1 19981001 A 5311 FRAME BOEING 737 7373Y0 1384671 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND UPPER FWD CORNER STUB FRAME CRACKED IN RADIUS. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600398 19981016 00398 NM 1998 10 16 SWAA982365 1 19981001 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 333 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND SUPPORT ANGLE BELOW LT CREAST BEAM CRACKED AT BS 333, LBL 60. REMOVED AND REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600399 19981016 00399 NM 1998 10 16 SWAA982367 1 19981002 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 BULGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED C4 CHECK, FOUND SKIN BULGED AT BS 727, STR 28R. REPAIRED PER SWA RA NR 1-253-1895. 2 L 7 2 4F A16WE 1998101600400 19981016 00400 NM 1998 10 16 SWAA982368 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED UNDER STRAP AT LBL 4.7, WL 201. REMOVED AND REPLACED PER TRAMCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600401 19981016 00401 NM 1998 10 16 SWAA982369 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 198.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600402 19981016 00402 NM 1998 10 16 SWAA982370 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 201. REMOVED AND REPLACED PER TR AMCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600403 19981016 00403 NM 1998 10 16 SWAA982371 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 02, WL 207. REMOVED AND REPLACED PER TRA MCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600404 19981016 00404 NM 1998 10 16 SWAA982372 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 4.7, WL 212.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600405 19981016 00405 NM 1998 10 16 SWAA982373 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT RBL 6.7, WL 212.5. REMOVED AND REPLACED PER TRAMCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600406 19981016 00406 NM 1998 10 16 SWAA982374 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 4.7, WL 200. REMOVED AND REPLACED PER TR AMCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600407 19981016 00407 NM 1998 10 16 SWAA982375 1 19981002 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 26596 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD WEB CRACKED UNDER STRAP AT LBL 5.7, WL 201. REMOVED AND REPLACED PER TR AMCO ER 98-0891. 2 L 7 2 4F RT A16WE 1998101600408 19981016 00408 NM 1998 10 16 SWAA982376 1 19981002 A 5320 MOUNT BOEING 737 7373Y0 1384671 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED O/B LAV WALL MOUNT LBL 54 AT BS 312. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600409 19981016 00409 NM 1998 10 16 SWAA982377 1 19981002 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL AT BS 540, BL 0, RBL 24.75. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600410 19981016 00410 NM 1998 10 16 SWAA982378 1 19981002 A 5314 KEEL BEAM BOEING 737 7373Y0 1384671 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED KEEL BEAM LT SIDE AT BS 500D, LBL 7. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600411 19981016 00411 NM 1998 10 16 SWAA982379 1 19981002 A 5320 INTERCOSTAL BOEING 737 7373Y0 1384671 NM BS 390 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED INTERCOSTAL AT BS 390, BL 0. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600412 19981016 00412 NM 1998 10 16 SWAA982380 1 19981002 A 5312 BLKHD BRACKET BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND 1016 PRESS BULKHEAD FWD SIDE CENTERLINE AFT CLOSET TOP RT SUPPORT BRACKET CRACKED. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600413 19981016 00413 NM 1998 10 16 SWAA982381 1 19981002 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 288 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED AT BS 288 ON FUSELAGE ANGLE BELOW STR 12R. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998101600414 19981016 00414 NM 1998 10 16 SWAA982382 1 19981002 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 288 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED AT BS 288 ON FUSELAGE ANGLE ABOVE STR 11R. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998101600415 19981016 00415 NM 1998 10 16 SWAA982383 1 19981002 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 288 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED AT BS 288 ON FUSELAGE ANGLE BELOW STR 11R. REMOVED AND REPLACED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998101600416 19981016 00416 NM 1998 10 16 SWAA982384 1 19981003 A 5315 FLOORBEAM BOEING 737 7373Y0 1384671 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT BS 344, LBL 27.5. REPAIRED PER SWA RA 1-353-1891. 2 L 7 2 4F RT A16WE 1998101600417 19981016 00417 NM 1998 10 16 SWAA982385 1 19981003 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 306 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND ANGLE CRACKED AT STR 10L, BS 306. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600418 19981016 00418 NM 1998 10 16 SWAA982386 1 19981003 A 5320 WEB BOEING 737 7375H4 138449D NM CARGO DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED DOORWAY LOWER WEB. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600419 19981016 00419 NM 1998 10 16 SWAA982387 1 19981003 A 5320 DOME NUTS BOEING 737 7375H4 138449D NM CARGO COMPT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED 3 DOME NUTS AT BS 468, BL 0 FUSELAGE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600420 19981016 00420 NM 1998 10 16 SWAA982388 1 19981003 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 775-857 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED TIE STRAP AT BS 775-857, WL 156, RBL 19. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600421 19981016 00421 NM 1998 10 16 SWAA982389 1 19981003 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR TO BULKHEAD SUPPORT ANGLE AT BS 947.5 RBL 20, LBL 20. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600422 19981016 00422 NM 1998 10 16 SWAA982390 1 19981003 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 180 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND FLOOR WEB AT BS 180, WL 207, RBL 27 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600423 19981016 00423 NM 1998 10 16 SWAA982391 1 19981003 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL AT BS 500 TO 500A, LBL 25, WL 158 CRACKED AT FASTENER HOLE. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600424 19981016 00424 NM 1998 10 16 SWAA982392 1 19981003 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND INTERCOSTAL AT BS 727A TO 727B, RBL 25, WL 158 CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600425 19981016 00425 NM 1998 10 16 SWAA982393 1 19981003 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 771 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, RBL 3, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600426 19981016 00426 NM 1998 10 16 SWAA982394 1 19981003 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 771 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, LBL 8.10, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600427 19981016 00427 NM 1998 10 16 SWAA982395 1 19981003 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 304 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 304 BETWEEN STR 27-28 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600428 19981016 00428 NM 1998 10 16 SWAA982396 1 19981003 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 358 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND DENTED SKIN AT BS 358 ABOVE STR 22R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600429 19981016 00429 NM 1998 10 16 SWAA982397 1 19981003 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 794 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND STRINGER CLIP AND L ANGLE AT BS 794, WL 155, STR 26R HAS ELONGATED HOLES. REMOVED AN D REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600430 19981016 00430 NM 1998 10 16 SWAA982398 1 19981003 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 795 BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND WEB SUPPORT ANGLE BENTED AND SEVERAL TOOLING MARKS AT BS 795, WL 158, RBL 24. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600431 19981016 00431 NM 1998 10 16 SWAA982399 1 19981003 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 794 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND ELONGATED HOLES IN L-ANGLE AT BS 794, RBL 24, WL 155. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600432 19981016 00432 NM 1998 10 16 SWAA982400 1 19981003 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 963 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STR 22 RT, AT BS 963. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600433 19981016 00433 NM 1998 10 16 SWAA982401 1 19981003 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 847-867 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED HOLES IN INTERCOSTAL AT BS 847-867, RBL 24, WL 155. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600434 19981016 00434 NM 1998 10 16 SWAA982402 1 19981004 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 056SW 21721 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHTS AT FWD ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F A16WE 1998101600435 19981016 00435 NM 1998 10 16 SWAA982403 1 19981004 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY LIGHTS INOPERATIVES IN CABIN. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998101600436 19981016 00436 NM 1998 10 16 SWAA982404 1 19981004 A 3350 LIGHT BOEING 737 7373H4 1384600 NM COCKPIT INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 352SW 24888 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BULB PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600437 19981016 00437 NM 1998 10 16 SWAA982405 1 19981004 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 637SW 27710 DURING SCHEDULED SERVICE CHECK, FOUND EGRESS LIGHT C ROW 7 INOPERATIVE AND MISSING LENS. REMOVED AND REPLACED PER BOEIN G MM. 2 L 7 2 4F RT A16WE 1998101600438 19981016 00438 NM 1998 10 16 SWAA982406 1 19981004 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 637SW 27710 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT AFT OF L2 DOOR INOPERATIVE. REMOVED AND REPLACED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600439 19981016 00439 NM 1998 10 16 SWAA982407 1 19981004 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 807-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND LEFT TRANSITION ANGLE CORRODED AT BS 807-947. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600440 19981016 00440 NM 1998 10 16 SWAA982408 1 19981004 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 867-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND LEFT TRANSITION ANGLE CORRODED AT BS 867-947. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600441 19981016 00441 NM 1998 10 16 SWAA982409 1 19981004 A 5312 BULKHEAD SUPPORT BOEING 737 7373Y0 1384671 NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AT AFT BULK HEAD PANEL SUPPORT ANGLE AT BS 500D. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998101600442 19981016 00442 NM 1998 10 16 SWAA982410 1 19981004 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 727-747 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED TRANSITION ANGLE LT AT BS 727D-747. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600443 19981016 00443 NM 1998 10 16 SWAA982411 1 19981004 A 5320 ANGLE BOEING 737 7373Y0 1384671 NM BS 747-807 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED TRANSITION ANGLE LT AT BS 747-807. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600444 19981016 00444 NM 1998 10 16 SWAA982412 1 19981004 A 5320 ANGLE BOEING 737 7375H4 138449D NM BS 460-520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED TRANSITION ANGLE LT AT BS 460 TO 520, LBL 24. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600445 19981016 00445 NM 1998 10 16 SWAA982413 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 867 BETWEEN STR 8 AND 9 RT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600446 19981016 00446 NM 1998 10 16 SWAA982414 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 867 BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600447 19981016 00447 NM 1998 10 16 SWAA982415 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 907 BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600448 19981016 00448 NM 1998 10 16 SWAA982416 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 500A BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600449 19981016 00449 NM 1998 10 16 SWAA982417 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 480 BETWEEN STR 8 AND 9 LT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600450 19981016 00450 NM 1998 10 16 SWAA982418 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 400 BETWEEN STR 8 & 9 LT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600451 19981016 00451 NM 1998 10 16 SWAA982419 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 380 BETWEEN STR 8 & 9 LT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600452 19981016 00452 NM 1998 10 16 SWAA982420 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 400 BETWEEN STR 8 & 9 RT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600453 19981016 00453 NM 1998 10 16 SWAA982421 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 440 BETWEEN STR 8 & 9 RT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600454 19981016 00454 NM 1998 10 16 SWAA982422 1 19981005 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 480 BETWEEN STR 8 & 9 RT. REPAIRED PER TRAMCO ER NR 98-0896. 2 L 7 2 4F RT A16WE 1998101600455 19981016 00455 NM 1998 10 16 SWAA982423 1 19981005 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 962 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C2 CHECK, FOUND CRACKED FUSELAGE SKIN AT 962, STR 21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998101600456 19981016 00456 NM 1998 10 16 SWAA982424 1 19981005 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN DOUBLER TOP CENTER AT 178 BULKHEAD BENT & CRACKED. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1998101600457 19981016 00457 NM 1998 10 16 SWAA982425 1 19981005 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 647SW 28332 DURING SCHEDULED RON CHECK, FOUND LT FUSELAGE BEHIND LT WING HAS A LARGE HOLE, FROM BEING STRUCK BY BAGGAGE CART. REPAI RED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600458 19981016 00458 NM 1998 10 16 SWAA982426 1 19981005 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 523SW 26565 DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR LIGHTING WIRING EXPOSED AT EMERGENCY EXIT ROW ON CAPTAINS SIDE. CONNECTE D LOOSE WIRES PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600459 19981016 00459 NM 1998 10 16 SWAA982427 1 19981005 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR INTERIOR EMERGENCY EXIT LIGHT ASSY BROKEN OFF. REMOVED AND REPLA CED ASSY PER BOEING MM. 2 L 7 2 4F A16WE 1998101600460 19981016 00460 NM 1998 10 16 SWAA982429 1 19981005 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 927-947 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SPECIAL VISIT TO DALFORD, REMOVED INTERCOSTAL BETWEEN BS 927-947 STRINGER 14L TO FOM TASK NR 014N. REMOVED AND R EPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998101600461 19981016 00461 NM 1998 10 16 SWAA982430 1 19981005 A 3350 6013211 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SPECIAL VISIT TO DALFORD, REMOVED ALL EMERGENCY LIGHTS AND BATTEY PACKS TO FOM. REMOVED AND REPLACED EMERGENCY B ATTERY PACKS, ONE FOUND BAD. REPLACED PER BOEING MM. 2 L 7 2 4F A16WE 1998101600462 19981016 00462 NM 1998 10 16 SWAA982431 1 19981005 A 5400 ANGLE BOEING 737 7373H4 1384600 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E LWR SIDE ANGLE SUPPORT CRACKED JUST FWD OF TAILCONE FITTING. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600463 19981016 00463 NM 1998 10 16 SWAA982433 1 19981005 A 5400 ANGLE BOEING 737 7373H4 1384600 NM NR 1 PYLON CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E L- ANGLE AND STIFFENER ARE CHAFFED AT LWR SIDE OF FLAP CUTOUT. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600464 19981016 00464 NM 1998 10 16 SWAA982434 1 19981005 A 5400 BRACKET BOEING 737 7373H4 1384600 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E L BRACKET SUPPORT CRACKED AT UPPER OF FLAP CUTOUT ON AFT PANEL SUPPOR T. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600465 19981016 00465 NM 1998 10 16 SWAA982435 1 19981005 A 5400 BRACKET BOEING 737 7373H4 1384600 NM NR 1 PYLON GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND NR 1 PYLON SPRING DOOR AND MOUNT BRACKET IS GOUGED. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998101600466 19981016 00466 NM 1998 10 16 SWAA982436 1 19981005 A 5320 WEB BOEING 737 7373Y0 1384671 NM BS 294 WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND WEB HAS TWO WORN AREAS AT BS 294 BELOW STR 13L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600467 19981016 00467 NM 1998 10 16 SWAA982437 1 19981005 A 5313 STRINGER BOEING 737 7373Y0 1384671 NM BS 358 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND WEB ON STRINGER 16L CRACKED AT BS 358 LBL 63. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600468 19981016 00468 NM 1998 10 16 SWAA982438 1 19981005 A 5312 BULKHEAD CHORD BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND LT SIDE BULKHEAD CHORD CRACKED AT BS 178, LBL 32, WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600469 19981016 00469 NM 1998 10 16 SWAA982439 1 19981005 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED BC1 CHECK, FOUND FLOOR PATH EMERGENCY LIGHT STRIPS HAVE GAPS AND ARE TAPED. INSTALLED NEW FLOOR PATH E MERGENCY LIGHT STRIPS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600470 19981016 00470 NM 1998 10 16 SWAA982440 1 19981006 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 927 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING SCHEDULED A1 CHECK, FOUND CRACKED FUSELAGE SKIN JUST FWD AND OUTBOARD OF AFT WATER SERVICE PANEL AT BS 927 STR 20 L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998101600472 19981016 00472 NM 1998 10 16 SWAA982442 1 19981006 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 771 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, RBL 8.10, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600473 19981016 00473 NM 1998 10 16 SWAA982443 1 19981006 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 771 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 771, LBL 3, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600474 19981016 00474 NM 1998 10 16 SWAA982444 1 19981006 A 5320 FRAME BOEING 737 7373H4 1384600 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME COVERPLATE AT BS 847, RBL 30 DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600475 19981016 00475 NM 1998 10 16 SWAA982445 1 19981006 A 5320 COVERPLATE BOEING 737 7373H4 1384600 NM BS 794.5 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND AFT CARGO DOOR FRAME COVERPLATE AT BS 794.5, RBL 30 DAMAGED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600476 19981016 00476 NM 1998 10 16 SWAA982432 1 19981006 A 5754 SKIN BOEING 737 7373H4 1384600 NM NR 6 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED NR 6 SLAT LWR SKIN AT CENTER AUX TRACK. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600477 19981016 00477 NM 1998 10 16 SWAA982446 1 19981006 A 5320 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FWD SERVICE DOOR FWD LWR STUB FRAME AT BS 296, RBL 60, WL 209. REPAIRED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998101600478 19981016 00478 NM 1998 10 16 SWAA982447 1 19981006 A 5330 SKIN BOEING 737 7373H4 1384600 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED LWR FWD HINGE CUT OUT ON FSD. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600479 19981016 00479 NM 1998 10 16 SWAA982448 1 19981006 A 5400 CLIP BOEING 737 7373H4 1384600 NM NR 1 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND L-CLIP CRACKED, SUPPORT BRACKET TOP OF NR 1 PYLON. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998101600480 19981016 00480 NM 1998 10 16 SWAA982449 1 19981006 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED FRAME AT BS 907, RBL 2, WL 303. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600481 19981016 00481 NM 1998 10 16 SWAA982450 1 19981006 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER 16 RT AT BS 500C +4.0. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600482 19981016 00482 NM 1998 10 16 SWAA982451 1 19981006 A 5320 CLIP BOEING 737 7373H4 1384600 NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D CHECK, FOUND CRACKED STRINGER CLIP AT BS 277, STR 15R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600483 19981016 00483 NM 1998 10 16 SWAA982452 1 19981006 A 5321 FLOORBOARD BOEING 737 7373H4 1384600 NM BS 1040-1064 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FLOORBOARD PLATAFORM IN TAIL COMPARTMENT LOCATED BETWEEN BS 1040 AND BS 1064. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600484 19981016 00484 NM 1998 10 16 SWAA982454 1 19981006 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 767 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED SHEAR TIE AT BS 767 BETWEEN STR 21L AND 22L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600485 19981016 00485 NM 1998 10 16 SWAA982455 1 19981006 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED SHEAR TIE AT BS 727D BETWEEN STR 21L AND 22L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600486 19981016 00486 NM 1998 10 16 SWAA982456 1 19981006 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 795 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND L-ANGLE HAS ELONGATED HOLES AT BS 795, WL 155, RBL 20. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600487 19981016 00487 NM 1998 10 16 SWAA982457 1 19981006 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 877 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND INTERCOSTAL CRACKED AT BS 877, STR 25 RT WL 155. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600488 19981016 00488 NM 1998 10 16 SWAA982458 1 19981006 A 5320 FRAME BOEING 737 7373Y0 1384671 NM CARGO DOORWAY DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND WEB DAMAGED AT BODY FRAME COMMON TO L/E OF AFT B/B DOOR CUTOUT AT BS 793. REMOVED AN D REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600489 19981016 00489 NM 1998 10 16 SWAA982459 1 19981006 A 5400 ANGLE BOEING 737 7373Y0 1384671 NM NR 2 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND ATTACH ANGLE CRACKED AT UPPER SHELF PANEL NR 2 PYLON OTBD EDGE INBD OF NR 6 SPOILER. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600490 19981016 00490 NM 1998 10 16 SWAA982460 1 19981006 A 5320 ANGLE BOEING 737 7375H4 138449D NM GALLEY DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED RT Z ANGLE AT AFT SERVICE DOOR CUTOUT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998101600491 19981016 00491 NM 1998 10 16 SWAA982461 1 19981006 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 704SW 27838 DURING SCHEDULED SERVICE CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LWR LIGHT INOPERATIVE. FOUND C/P DD10748 MIS-PINN ED, CORRECTED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998101600492 19981016 00492 NM 1998 10 16 UPS98227899 1 19981010 A 3520 OXYGEN MASK BOEING 727 72725C 138400H NM CABIN FAILED TEST A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 EMERGENCY 02 MASKS DEPLOYMENT FAILED DROP TEST AT THE FOLLOWING STATIONS 5RT, 6LT, 9RT, 10LT, 11RT, 12LT, 16RT, 17RT, 18 LT, 18RT, 19RT AND AFT LAV. ADJUSTED MASKS AND RECOILED, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998101600493 19981016 00493 NM 1998 10 16 UPS98227900 1 19981010 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EEL RT SIDE AFT DOOR INOP. REPLACED BATT PACK P/N ON 96-2-1033. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998101600494 19981016 00494 NM 1998 10 16 UPS98227901 1 19981010 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 EEL OVER GALLEY DOOR INOP. REPLACED BATT PACK, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998101600495 19981016 00495 EU 1998 10 16 QXEA9801396 1 19980909 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 17565 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1998101600496 19981016 00496 EU 1998 10 16 QXEA9801397 1 19980909 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 17565 AND STRINGER 53A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1998101600497 19981016 00497 EU 1998 10 16 QXEA9801398 1 19980909 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED CLIP AT FRAME 17565 AND STRINGER 51. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 3. 2 L 7 2 4F RT A20EU 1998101600498 19981016 00498 EU 1998 10 16 QXEA9801399 1 19980921 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CHAFE DAMAGE ON FRAME 18075 AND STRINGER 18. REPAIRED IAW HORIZON AIR EA 4-53-557. 2 L 7 2 4F RT A20EU 1998101600499 19981016 00499 EU 1998 10 16 QXEA9801400 1 19980923 A 5210 HINGE FOKKER F28 F28MK4000 4990810 EU PAX DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - MAIN CABIN DOOR HINGE HAS EXCESSIVE PLAY (.032). REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998101600500 19981016 00500 EU 1998 10 16 QXEA9801401 1 19980912 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED FRAME CLIP AT FRAME 6305 AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998101600501 19981016 00501 EU 1998 10 16 QXEA9801402 1 19980913 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED FRAME CLIP AT FRAME 6805 AND STRINGER 16. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998101600502 19981016 00502 EU 1998 10 16 QXEA9801403 1 19980913 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - CRACKED FRAME CLIP AT FRAME 5805 AND STRINGER 18. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4. 2 L 7 2 4F RT A20EU 1998101600503 19981016 00503 EU 1998 10 16 QXEA9801404 1 19980916 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU CABIN GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - LEFT SIDE INBOARD SEAT TRACK FLANGE INBOARD SIDE TWO SMALL GOUGED AREAS. REPAIRED IAW FOKKER SRM 53-02-15, FIGURE 1, AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998101600504 19981016 00504 EU 1998 10 16 QXEA9801405 1 19980917 A 5210 FITTING FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - AFT MAIN CABIN DOOR ATTACH FITTING CASTING SHOWS SIGNS OF CORROSION ON UPPER END INSIDE MAIN CABIN DOOR SKIN AFT T OP CORNER. REPAIRED IAW FOKKER SRM 51-30-02 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998101600505 19981016 00505 EU 1998 10 16 QXEA9801406 1 19980912 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12045 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - FRAME 12405 HAS A CRACKED CLIP AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998101600506 19981016 00506 EU 1998 10 16 QXEA9801407 1 19980912 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - FRAME 12875 HAS A CRACKED CLIP AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998101600507 19981016 00507 EU 1998 10 16 QXEA9801408 1 19980912 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER 44 BETWEEN FRAME 12875 AND 13345 HAS CORROSION THROUGH AND AROUND HOLE TO SECURE INSULATION. REPAIRED IA W FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1998101600508 19981016 00508 EU 1998 10 16 QXEA9801409 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - LOWER ATTACH CLIP ON LEFT FRAME 11405 IS CRACKED AT WING BOX. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1998101600509 19981016 00509 EU 1998 10 16 QXEA9801410 1 19980912 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 11405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - LOWER ATTACH CLIP ON RIGHT FRAME 11405 IS CRACKED AT WING BOX. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998101600510 19981016 00510 EU 1998 10 16 QXEA9801411 1 19980917 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE ARE AREAS WITH CORROSION ON FRAME 9305 BETWEEN STRINGERS 46 AND 48. REPAIRED IAW HORIZON AIR EA 4-53-554. 2 L 7 2 4F RT A20EU 1998101600511 19981016 00511 EU 1998 10 16 QXEA9801412 1 19980910 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER 41 IS CRACKED AND CORRODED AS IT PASSES OVER FRAME 8805. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1, SEC TION A-A. 2 L 7 2 4F RT A20EU 1998101600512 19981016 00512 EU 1998 10 16 QXEA9801413 1 19980924 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 7805-8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - STRINGER 37 IS CRACKED AND CORRODED IN TWO PLACES BETWEEN FRAME 7805 AND 8305. REPAIRED IAW FOKKER SRM 53-02-05, PAGE 3, FIGURE 1. 2 L 7 2 4F RT A20EU 1998101600513 19981016 00513 EU 1998 10 16 QXEA9801414 1 19980923 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE IS CORROSION ALONG STRINGER 40 BETWEEN FRAME 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, FIGUR E 1. 2 L 7 2 4F RT A20EU 1998101600514 19981016 00514 EU 1998 10 16 QXEA9801415 1 19980923 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE IS CORROSION ALONG STRINGER 41 BETWEEN FRAME 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, FIGUR E 1. 2 L 7 2 4F RT A20EU 1998101600515 19981016 00515 EU 1998 10 16 QXEA9801416 1 19980923 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE IS CORROSION ALONG STRINGER 42 BETWEEN FRAME 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06, PAGE 3, FIGUR E 1 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998101600516 19981016 00516 EU 1998 10 16 QXEA9801417 1 19980923 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE IS CORROSION ALONG STRINGER 44 BETWEEN FRAME 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1, SEC TION E-E. 2 L 7 2 4F RT A20EU 1998101600517 19981016 00517 EU 1998 10 16 QXEA9801418 1 19980924 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE IS CORROSION ALONG STRINGER 45 BETWEEN FRAME 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06, FIGURE 1, SEC TION E-E. 2 L 7 2 4F RT A20EU 1998101600518 19981016 00518 EU 1998 10 16 QXEA9801419 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE IS A CRACK AROUND TOP RIVET HOLE OF CLIP JUST AFT OF FRAME 5805, BETWEEN STRINGERS 18 AND 19. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998101600519 19981016 00519 EU 1998 10 16 QXEA9801420 1 19980908 A 5230 WEB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - REAR CARGO DOOR BAY NR 3 AND NR 4 HAS CORROSION ON SIDE OF LOWER WEB AND TOP OF UPPER WEB. REPAIRED IAW FOKKER SR M 52-01-01. 2 L 7 2 4F RT A20EU 1998101600520 19981016 00520 EU 1998 10 16 QXEA9801421 1 19980908 A 5230 WEB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - REAR CARGO DOOR BAY NR 8 HAS CORROSION ON TOP OF UPPER WEB AND AROUND LIGHTENING HOLE AT LOWER WEB. REPAIRED IAW FOKKER SRM 52-01-01. 2 L 7 2 4F RT A20EU 1998101600521 19981016 00521 EU 1998 10 16 QXEA9801422 1 19980920 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 9305 MISDRILLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - ON FRAME 9305A ABOVE STRINGER 74 FOUND .25 INCH HOLE UNDER FLOOR SUPPORT BRACKET. REPAIRED IAW HORIZON AIR EA 4-5 3-552. 2 L 7 2 4F RT A20EU 1998101600522 19981016 00522 EU 1998 10 16 QXEA9801423 1 19980930 A 5230 HINGE FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - REAR CARGO DOOR HINGE IS DENTED APPROXIMATELY .030 DEEP AND 1 LONG. REPAIRED IAW EO 4-52-07B. 2 L 7 2 4F RT A20EU 1998101600523 19981016 00523 EU 1998 10 16 QXEA9801424 1 19980923 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - REAR CARGO BAY DOOR BOTTOM AFT CORNER IS DEEPLY DENTED. REPAIRED IAW EO 4-52-07B. 2 L 7 2 4F RT A20EU 1998101600524 19981016 00524 EU 1998 10 16 QXEA9801425 1 19980911 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FRAME 6805 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 PDX - THERE IS A DENT FORWARD OF FRAME 6805 STRINGER 16 5 LONG AND 4 WIDE IN THE LEFT FUSELAGE. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-04. 2 L 7 2 4F RT A20EU 1998101600526 19981016 00526 NM 1998 10 16 QXEA9801428 1 19981005 A 2611 3023143 DETECTOR KIDDE DHAV DHC8 DHC8102 2809003 NM CARGO COMPT MALFUNCTIONED A QXEA K NONE N FALSE WARNING CR CRUISE 1 NM 09 840PH 13107 74 PDX - EN ROUTE, INTERMITTENT ILLUMINATION OF CARGO SMOKE CAUTION LIGHT. REMOVED & REPLACED CARGO SMOKE DETECTOR. OPERA TIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998101600527 19981016 00527 EU 1998 10 16 QXEA9801429 1 19981007 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 GEG - EXIT SIGN AT ROW 8 INOPERATIVE. RELAMPED LIGHT AT ROW 8. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600528 19981016 00528 EU 1998 10 16 QXEA9801430 1 19981006 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 478US 11227 PDX - OVERHEAD EMERGENCY LIGHT AT ROW 8 HAS SEVERAL BULBS OUT. REPLACED OVERHEAD EMERGENCY LIGHTS. OPERATIONAL CHECK G OOD. 2 L 7 2 4F RT A20EU 1998101600529 19981016 00529 EU 1998 10 16 QXEA9801431 1 19981006 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 PDX - LEFT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT AFT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECK GOO D. 2 L 7 2 4F RT A20EU 1998101600530 19981016 00530 NM 1998 10 16 QXEA9801432 1 19981006 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 358PH 506 FORWARD ESCAPE PATH EMERGENCY LIGHT INOP. APPLIED A SPLICE TO CONNECTOR 3352-J3 AS AN INTERM REPAIR AND PLACED OM MRSI. 2 H 7 2 4T RT A13NM 1998101600531 19981016 00531 NM 1998 10 16 98FDEA00642 1 19981009 A 5311 BELLFRAME BOEING 727 727233 138408A NM BS 560 BENT A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 1755 UPR LOBE BENT BELLFRAME AT BS 560, RBL 65 5 APPROX ABOVE FLOORBEAM. CUT OUT DAMAGE AREA FAB DOUBLER, ALODINED, PRIMED & INSTALLED DOUBLER PER SRM 51-40-3. 2 L 7 3 4F RT A3WE 1998101600532 19981016 00532 NM 1998 10 16 98FDEA00643 1 19981008 A 5347 SEAT TRACK BOEING 727 727233 138408A NM BS 1050 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 NR 975 CORROSION ON SEAT TRACK & FLOORBEAM AT BS 1050 AT LBL 25 FROM C/L. SEAT/TRACK CORROSION REMOVED & NOW OUT OF LIM ITS. INSTALL FLOORBEAM UPPER CHORD BY ACCORD WITH SRM 53-10-8 FIG 1 & EA 7-5310-29647 DATED 9/30/98. 2 L 7 3 4F RT A3WE 1998101600533 19981016 00533 NM 1998 10 16 98FDEA00644 1 19981008 A 5313 651838727 STRINGER BOEING 727 72722 1384002 NM BS 1080 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 UPON REMOVAL OF LT KEEL BEAM ON NR 0190, FOUND CORROSION IN STR AT BS 1080, LBL 8, WL 138, STR 29L. *S/D* REPAIRED STR 29L, BS 1082-1098, LBL 8, WL 138 PER FED-EX SRM 53-10-3. 2 L 7 3 4F A3WE 1998101600534 19981016 00534 NM 1998 10 16 98FDEA00645 1 19981009 A 2720 POWER UNIT BOEING 727 727277 138408S NM LOWER RUDDER LEAKS A FDEA H DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 25 243FE 21480 98-245 AT FLT LVL 200, ON CLIMB-OUT 'A' SYS QUAN WAS 0.6 GAL GOOD PRESS. ON DESCENT QUANTITY DECREASE TOWARD 0 PRESS E RRATIC. MAN EXTEND GEAR AND FLAP A FLUID SHUTOFF SWITCH CLOSE AT 0835Z. FOUND LEAK LWR RUDDER PWR UNIT AT BASE RUDDER LOAD LIMIT VALVE MT PAD. REMOVED AND REPLACED PAD,VALVE PER MM 27-20-142 PG 401. SERV HYD SYS & OPER ALL SYS TO PURGE OUT AIR. OK FOR SERV. 2 L 7 3 4F RT A3WE 1998101600535 19981016 00535 1998 10 16 98FDEA00646 4 19981009 A 3417 HG480B13 ADC BOEING 727 727247 138408F NM E & E COMP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 235FE 21329 98-246 ON CLIMB-OUT, LOST CAPT AIRSPEED CAPT ALT, GPWS, ALT ALERTER, TRANSPONDER NR 1, & MODE C IN BOTH TRANSPONDER & AU TOPILOT. REMOVED AND REPLACED DADC PER BOEING 727 MM CHAPTER 34-12-11. OPER CKS NORM. AUTOPILOT DOWNGRADED TO CK CAT 2 STATUS. A/C DOWNGRADED TO NOT CAT 2 STATUS. 2 L 7 3 4F A3WE 1998101600536 19981016 00536 NE 1998 10 16 MWEA98996 2 19981006 A 7200 ENGINE DOUG DC9 DC914 3022034 WP PWA JT8 JT8D7B 52053 NE RIGHT FAILED A MWEA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 GL 31 500ME 45711 JUST AFTER TAKEOFF, RIGHT ENGINE FAILED AND STOPED SUDDENLY. PERFORMED QRH PROCEDURES, RETURNED TO GRR. REMOVED AND RE PLACED RIGHT ENGINE. 2 L 7 2 4F 4 F A6WE E2EA 1998101600537 19981016 00537 WP 1998 10 16 MWEA98997 1 19981005 A 3350 601179 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 FOUND RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998101600538 19981016 00538 WP 1998 10 16 MWEA98998 1 19981005 A 3350 6011775 BATTERY PACK DOUG DC9 DC932 3022066 WP LT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 FOUND LEFT NACELLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998101600539 19981016 00539 WP 1998 10 16 MWEA98999 1 19981007 A 3230 PINS DOUG DC9 DC932 3022066 WP LANDING GEAR NOT REMOVED A MWEA A UNSCHED LANDING J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 GL 31 204ME 47680 AFTER TAKEOFF FROM MKE AND LANDING GEAR HANDLE WAS RAISED TO THE UP POS. LANDING GEAR WOULD'NT COME UP. RETURNED TO MK E. MAINTENANCE REMOVED LANDING GEAR LOCKDOWN PINS. 2 L 7 2 4F A6WE 1998101600540 19981016 00540 WP 1998 10 16 MWEA981000 1 19981007 A 3350 6030431 BATTERY PACK DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A MWEA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 302ME 47102 DURING RECEIVING CHECK LIST, OVERHEAD COCKPIT EMERG LIGHTS DID NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE FWD EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1998101600541 19981016 00541 NM 1998 10 16 DL72S982083 1 19981008 A 5530 TAB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 59R FLANGE TAB AT FIN STA 133.8 CRACKED, HORIZONTALLY THROUGH ATTACH BOLT. REF NRC515 MV2. REPAIRED PER MM 55-30-0 FIG 803. 2 L 7 3 4F A3WE 1998101600542 19981016 00542 NM 1998 10 16 DL72S982085 1 19981008 A 5711 651620261 SPAR BOEING 727 727232 1384082 NM CTR WING DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 DURING INSPECTION OF THE CTR WING REAR SPAR AND REPAIR MANY FASTENER LOCATIONS IN THE SPAR PANEL WERE OVERSIZED DUE TO T OOLING DAMAGE. REPAIRED PER ERA 332359-14AD. 2 L 7 3 4F A3WE 1998101600543 19981016 00543 NM 1998 10 16 DL73S982086 1 19981008 A 5311 FRAME BOEING 737 737232 1384475 NM BS 440 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 STA 440 FRAME WEB FOUND CRACKED AT A TOOLING HOLE BETWEEN S13R - 14R. REPAIRED PER ERA 332298-14. 2 L 7 2 4F RT A16WE 1998101600544 19981016 00544 NM 1998 10 16 DL73S982087 1 19981008 A 5311 FRAME BOEING 737 737232 1384475 NM BS 420 - 787 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 DURING MODIFICATION OF THE FUSELAGE FRAMES SEVERAL WERE DAMAGED. THE DAMAGE REQUIRED TRIMMING OFF/OUT THE TOOLING DAMAG E. REPAIRED PER ERA 332294-14. 2 L 7 2 4F RT A16WE 1998101600545 19981016 00545 NM 1998 10 16 DL73S982088 1 19981008 A 5311 FRAME BOEING 737 737232 1384475 NM BS 907 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 CRACK FOUND IN THE FAIL/SAFE CHORD OF THE STA 907 FRAME AT APPROX S13R. REPAIRED PER ERA 332297-14. 2 L 7 2 4F RT A16WE 1998101600546 19981016 00546 NM 1998 10 16 DL73S982089 1 19981008 A 5330 SKIN BOEING 737 737232 1384475 NM CARGO DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 C2 DOOR CUTOUT WAS WITH AN EXISTING REPAIR ALONG THE FWD EDGE. UPON REMOVAL OF THE REPAIR ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332286-14. 2 L 7 2 4F RT A16WE 1998101600547 19981016 00547 NM 1998 10 16 DL73S982090 1 19981008 A 5343 65499533 FITTING BOEING 737 737232 1384475 NM BS 685 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 332DL 23104 THE LT MLG SIDE STRUT SUPPORT FITTING AT BS 685 WAS DAMAGED BY TOOL MARKS. REPAIRED PER ERA 332329-14. 2 L 7 2 4F RT A16WE 1998101600548 19981016 00548 NM 1998 10 16 DLM88982091 1 19981008 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 999DN 53371 FUSELAGE SKIN CUTOUT TO REMOVE DENT AT FS 237 AND 243, BETWEEN L18L AND L20L. REPAIRED PER ERA 332349-14. 2 L 7 2 4F RT A6WE 1998101600549 19981016 00549 NM 1998 10 16 DL72S982092 1 19981008 A 5532 65174633 SKIN BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 LT SIDE OF THE VERT STAB SKIN IS CRACKED AT THE INTERSECTIONOF S10 AND FUSE CREASE LINE. REPAIR PER ERA 332292-14. 2 L 7 3 4F A3WE 1998101600550 19981016 00550 NM 1998 10 16 DL72S982093 1 19981008 A 5320 FITTING BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 CRACKING WAS DETECTED IN FOUR OF EIGHT HOLES ON S18A, LT SIDE. HOLES WERE OVERSIZED THROUGH THE SKIN, STRINGER AND FITT ING. REPAIRED PER ERA 332264-14. 2 L 7 3 4F A3WE 1998101600551 19981016 00551 NM 1998 10 16 DL72S982094 1 19981008 A 5330 SKIN BOEING 727 727232 1384082 NM BS 294 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 FUSE SKIN HAD A TIME LIMITED REPAIR REMOVED AT FS294, S15R; AND ADDITIONAL DAMAGE WAS FOUND. REPAIRED PER ERA 332347-14 . 2 L 7 3 4F A3WE 1998101600552 19981016 00552 WP 1998 10 16 DLL19982095 1 19981008 A 3350 RPS1 BATTERY PACK LKHEED 1011 10113853 5265020 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 763DL 193Y1197 ON A/C LAYOVER CHECK, FOUND F/C TRACK LIGHT INOP. LIGHT BATTERY PACK BAD. REPLACED PACK LOCATED IN FWD BAG BIN, P/N 33 7701962 S/N 0417. 2 L 7 3 4F A23WE 1998101600553 19981016 00553 NM 1998 10 16 DLM11982096 1 19981008 A 3840 8378M11 COMPRESSOR 8378M11 DOUG MD11 MD11 3023602 NM NR 1 WATER SYST SEIZED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 805DE 002332 48476 AIRCRAFT DIVERTED INTO SNN WITH SMELL OF BURNING IN CABIN. IRISH AUTHORITIES REMOVED FDR AND CVR FOR ELAVUATION. AIRCR AF STILL IN SNN 100998 UNDER INVESTIGATION. NR 1 WATER SYS AIR COMP FAILED, BURNED WIRING TO COMPRESSOR. 2 L 7 3 4F RT A22WE 1998101600554 19981016 00554 NM 1998 10 16 DL757982100 1 19981009 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1640 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 MID VISIT, FLOORBEAM AT STA 1640 LBL 0 TO LBL 58 CORRODED, REPAIRED. 2 L 7 2 4F RT A2NM 1998101600555 19981016 00555 NM 1998 10 16 DL757982101 1 19981009 A 5320 BEAM BOEING 757 757232 1384965 NM BS 660 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 MID VISIT, CREASE BEAM CORRODED AT STATION 660 LBL63, REPAIRED. 2 L 7 2 4F RT A2NM 1998101600556 19981016 00556 NM 1998 10 16 DL757982102 1 19981009 A 5320 BEAM BOEING 757 757232 1384965 NM BS 680-785 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 MID VISIT, CORROSION ON CREASE BEAM AT R2 DOORWAY, STA 680 TO 785 RBL65. 2 L 7 2 4F RT A2NM 1998101600557 19981016 00557 NM 1998 10 16 DL757982103 1 19981009 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 345-379 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 MID VISIT, FLOORBEAM CORRODED AT STA 345 TO 379 BL 0, REPAIRED. 2 L 7 2 4F RT A2NM 1998101600558 19981016 00558 NM 1998 10 16 DL757982104 1 19981009 A 5321 FLOOR PANEL BOEING 757 757232 1384965 NM CARGO COMPT CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 683DA 27103 MID VISIT, CORROSION ON FIXED FLOOR PANEL RT STA 760 TO 800, REPAIRED. 2 L 7 2 4F RT A2NM 1998101600559 19981016 00559 NM 1998 10 16 DL72W982105 1 19981006 A 5753 652163230 ANGLE BOEING 727 727247 138408F NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 DURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT ANGLE WAS FOUND CRACKED 33 FROM THE IB END OF FLAP. THE ANGLE WAS REPAIR ED PER 727 MM 57-52-0,FIG. 802 BY INSTALLING A DOUBLER AND STOP DRILLING THE CRACK. 2 L 7 3 4F A3WE 1998101600560 19981016 00560 NM 1998 10 16 DL72L982106 1 19981009 A 5730 SKIN BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 CRACK AT NR 3 SLAT OB GUIDE CUT OUT AFT END. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998101600561 19981016 00561 NM 1998 10 16 DL72L982107 1 19981009 A 5720 STIFFENER BOEING 727 727232 1384082 NM LT WING SPAR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 SPAR STIFFENER CRACKED NR 3 SLAT IB TRACK. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998101600562 19981016 00562 NM 1998 10 16 DL72L982108 1 19981009 A 5730 SKIN BOEING 727 727232 1384082 NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 513DA 21315 CRACK AT NR 4 SLAT IB GUIDE CUTOUT AFT END. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998101600563 19981016 00563 NM 1998 10 16 DL767982109 1 19981010 A 2530 828450407 OVEN BOEING 767 767232 1385132 NM GALLEY CONTAMINATED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 110DL 22222 SHORTLY AFTER TAKEOFF, SMOKE OBSERVED FROM AFT GALLEY OVENS. COULD NOT DETERMINE SOURCE OF SMOKE, FOOD OR ELECTRICAL. F OUND BURNT SUBSTANCE IN CORNER OF LOWER LEFT OVEN IN AFT GALLEY. REPLACED OVEN ASSEMBLY AND NEW OVEN, OPS NORMAL. 2 L 7 2 4F RT A1NM 1998101600564 19981016 00564 NM 1998 10 16 DL72W982110 1 19981011 A 3260 LIGHT BOEING 727 727247 138408F NM NLG WARN ILLUMINATED A DALA K NONE O OTHER AP APPROACH 1 SO 27 2809W 20581 AFTER GEAR EXTENSION THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WITH NO GREEN NOSE GEAR LIGHT. POM PROCEDURES COMPLIED WITH AND A SAFE INDICATION OBTAINED AFTER MANUAL EXTENSION PROCEDURES ACCOMPLISHED. 2 L 7 3 4F A3WE 1998101600565 19981016 00565 WP 1998 10 16 SCNA98122 1 19981008 A 2530 WALL DOUG DC10 DC1015 3022118 WP GALLEY DELAMINATED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A MAINTENANCE CHECK, THE CENTER WALL BETWEEN THE P LIFT AND C LIFT WAS FOUND TO BE DELAMINATED. REMOVED AND REPL ACED THE DAMAGED SECTION OF HONEYCOMB. FABRICATED AND INSTALLED A DOUBLER IAW MDC-10 SRM 517100. 2 L 7 3 4F A22WE 1998101600566 19981016 00566 WP 1998 10 16 SCNA98123 1 19981007 A 5320 INTERCOSTAL DOUG DC10 DC1015 3022118 WP GALLEY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 151SY 48295 DURING A MAINTENANCE CHECK AN INTERCOSTAL THAT RUNS OUTBOARD TO THE RIGHT OF THE P LIFT WAS FOUND CORRODED. REMOVED COR RODED INTERCOSTAL AND FABRICATED A NEW SECTION OF INTERCOSTAL. TREATED AND PRIMED AND INSTALLED IAW SRM 537000. 2 L 7 3 4F A22WE 1998101600567 19981016 00567 NM 1998 10 16 SCNA98124 1 19981008 A 3350 LIGHT BOEING 727 727259 138408J NM CABIN INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE L1 DOOR EMERGENCY SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. CLEANED LAMP CONTACTS A ND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998101600568 19981016 00568 NM 1998 10 16 SCNA98125 1 19981008 A 3350 900835A BATTERY PACK BOEING 727 727259 138408J NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACE D THE BATTERY PACK AT M955. ALL EMERGENCY LIGHTS CHECK GOOD. 2 L 7 3 4F A3WE 1998101600569 19981016 00569 NM 1998 10 16 SCNA98126 1 19981009 A 2150 39854011 VALVE BOEING 727 727225 1384077 NM LEFT PACK FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 282SC 3368 22558 DURING CLIMB-OUT, THE PRESSURIZATION AUTO FAIL AND STANDBY LIGHT CAME ON AND THE RIGHT PACK OVERHEATED TO ABOUT 150 DEGR EES OR MORE BUT PACK DID NOT TRIP OFF. RETURNED TO MSP. PERFORMED A FUNCTIONAL CHECK OF THE PRESSURIZATION SYSTEM IAW MM 21310 WITH NO DEFECTS NOTED. FOUND THE LEFT PACK VALVE BAD CAUSING PACK VALVE CIRCUIT BREAKER TO POP. REMOVED AND R EPLACED THE LEFT PACK VALVE AND OPERATIONALLY CHECKS GOOD IAW 21110. ALSO, REMOVED AND REPLACED THE RIGHT PACK FAN IAW B727 MM CHAPTER 215800, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998101600570 19981016 00570 NM 1998 10 16 DHL98721002 1 19981008 A 7997 WIRE BOEING 727 727228 1384083 NM NR 2 ENGINE CHAFED A DHLA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 721DH 19545 NR 2 ENGINE OIL TEMP FLUCTUATED. FOUND CHAFFED WIRE ON OIL TEMP BULB. REPAIRED PER M/M 79-33. 2 L 7 3 4F RT A3WE 1998101600571 19981016 00571 NM 1998 10 16 DHL98721003 1 19981008 A 5230 DEPRESSOR BOEING 727 727228 NM CARGO DOOR OUT OF ADJUST A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 721DH 19545 LOUD SQUEAL EMITTED FROM CARGO DOOR AREA. ADJUSTED FWD DOOR CUT OUT SEAL DEPRESSOR PER MM 52-31-0. PRESSURIZED TO 8.6 PSI. OPS CHECK OK. 2 L 7 3 4F A3WE 1998101600572 19981016 00572 WP 1998 10 16 DHL98806001 1 19981005 A 2131 A2920710021 CONTROLLER DOUG DC8 DC873F 302199F WP CABIN MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 806DH 46002 AIRCRAFT FAILED TO PRESSURIZE AFTER TAKEOFF FROM SUVA IN AUTOMATIC AND MANUAL. FLOWS MAX ONLY 5 PSI. REMOVED AND REPLA CED CABIN PRESSURIZATION CONTROLLER PER MM 21-51-0. 2 L 7 4 4F RT 4A25 1998101600573 19981016 00573 SO 1998 10 16 SWIA971273 1 19981001 A 2751 FCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING DE DESCENT 1 NM 07 299SW 120329 NACELLE FLAP ASYMMETRY INDICATION, NO ADVERSE ROLL TENDENCY NOTED. THIS OCCURED ON APPROACH TO IMPERIAL, RETURNED TO PS P. FOUND FCU LOOSE IN MOUNT, CYCLED FLAPS NUMEROUS TIMES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600574 19981016 00574 SO 1998 10 16 SWIA971274 1 19981003 A 3260 PROX SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 195SW 120127 LEFT MAIN 'A' SYSTEM GREEN LIGHT STAYED ON AFTER GEAR RETRACTION. RECYCLED 3 TIMES, RED TRANSIT LIGHTS DID NOT ILLUMINA TE WHEN GEAR WAS PUT BACK DOWN, GREEN LIGHT WENT OUT IN BUMPS AT ABOUT 16,000 FT. RETURNED TO SLC, REPLACED BAD LEFT GE AR PROXIMITY SENSOR IN 'A' SYSTEM. SWUNG GEAR AND ALL SYSTEMS OPS AND READS NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600575 19981016 00575 EA 1998 10 16 SWIA971275 1 19981004 A 3230 UPLOCK ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 405SW 7029 GEAR DISAGREE ON TAKEOFF RETRACTION. RETURNED TO SLC. REMOVED AND REPLACED UPLOCK ACTUATOR IAW MM 32-33-01 AND 32-33-0 5. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED NLG RETRACTION ACTUATOR. 2 L 7 2 4F 4 F RT A21EA E15NE 1998101600576 19981016 00576 SO 1998 10 16 SWIA971276 1 19981006 A 2150 CONNECTORS EMB 120 EMB120RT SO PWA 118 PW118 NE PACK VALVES DIRTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 128AM 120109 BOTH PACKS BLOW VERY HOT AIR IN ALL MODES. RETURNED TO FIELD. CLEANED CONNECTORS ON PACK VALVES RAN BOTH PACKS. CHECK S GOOD ON GROUND 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600577 19981016 00577 WP 1998 10 16 RRXA98438 1 19981001 A 2150 CLAMP DOUG DC8 DC871 302199A WP RT ACM LOOSE A RRXA O OTHER J WARNING INDICATION CR CRUISE 1 WP 15 811AL 46099 RAPID DECOMPRESSION AT FL350, UNABLE TO HOLD CABIN ALT. FOUND DUCT CLAMP LOOSE ON RT ACM. SECURED SAME. PRESSURE CHEC K GOOD ON GROUND IAW M/M CHAPT 21. 2 L 7 4 4F 4A25 1998101600578 19981016 00578 WP 1998 10 16 RRXA98439 1 19981008 A 7722 CA11603 HARNESS DOUG DC8 DC873F 302199F WP NR 2 ENGINE EGT WORN A RRXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 795FT 46103 NR 2 ENG EGT GAUGE VERY ERRATIC BOTH THE DIGITAL AND ANILOG AT THE SAME TIME SECURED ENG NR 2 PER QRH. REMOVED AND REPL ACED LT AND RT EGT HARNESS ON NR 2 ENG EGT IND NORMAL. OPS CK GOOD ON GRD RUN. 2 L 7 4 4F RT 4A25 1998101600579 19981016 00579 WP 1998 10 16 RRXA98440 1 19981008 A 3230 PIN DOUG DC8 DC863 302198A WP LT MLG SHEARED A RRXA A UNSCHED LANDING J E WARNING INDICATION VIBRATION/BUFFET CL CLIMB 1 WP 15 950R 45903 LEFT MAIN GEAR WOULD NOT RETRACT. MAINTENANCE FOUND PIN ATTACHING RETRACT CYLINDER TO GEAR WAS SHEARED OFF. 2 L 7 4 4F 4A25 1998101600580 19981016 00580 NM 1998 10 16 VNAA9809027 1 19980930 A 2510 2A510002 SPRING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT LOOSE A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 434JS 3051 THE AIRCRAFT RETURNED TO THE GATE, DUE TO THE FIRST OFFICERS SEAT VERTICAL ADJUSTMENT FUNCTION BEING INOPERATIVE. MAINT ENANCE INSPECTED AND RE-SECURED THE VERTICAL ADJUSTMENT HELPER SPRING, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 25- 21-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101600581 19981016 00581 NM 1998 10 16 VNAA9810001 1 19981004 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 424JS 78269 3033 DURING TAXI, THE LEFT PROPELLER WHEN SELECTED, WOULD NOT COME OUT OF FEATHER. THE CREW ATTEMPTED A SECOND TIME TO UNFEA THER THE PROPELLER. THE PROPELLER UNFEATHERED, BUT WITH AN RPM AND TORQUE SURGE. THE TORQUE SURGE WAS LARGE ENOUGH TO OVER TORQUE THE PROPELLER AND ENGINE. MAINTENANCE INSPECTED AND REPLACED THE LEFT PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. MAINTENANCE ALSO COMPLETED AN OVERTORQUE INSPECTION ON THE PROPELLER AND ENG INE, IN ACCORDANCE WITH DORNIER MANUAL 05-57-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SE RVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101600582 19981016 00582 NM 1998 10 16 VNAA9810003 1 19981005 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 441JS 66229 57751 3059 THE LEFT PROPELLER FAILED TO UNFEATHER WHEN SELECTED, DURING THE PUSHBACK FOR DEPARTURE. THE AIRCRAFT WAS RETURNED TO T HE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MAN UAL 61-21-06. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101600583 19981016 00583 1998 10 16 VNAA9810004 4 19981006 A 3425 HG2010AC02 AHRU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE EQUIPMENT RACK FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 436JS 86609 41774 3052 A NUMBER TWO ATTITUDE/HEADING FAIL WARNING MESSAGE ILLUMINATED, DURING THE CLIMB-OUT PHASE OF THE FLIGHT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED, WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPLACED THE NUMBER TWO ATTIT UDE AND HEADING REFERENCE UNIT (AHRU), IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-21-20. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101600584 19981016 00584 NM 1998 10 16 VNAA9810006 1 19981007 A 3030 0851GW PITOT HEAT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT FUSELAGE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 426JS 15335 3038 A NUMBER ONE PITOT HEAT FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO TH E GATE. MAINTENANCE INSPECTED AND REPLACED THE NUMBER ONE PITOT PROBE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34 -11-04. OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101600585 19981016 00585 NM 1998 10 16 CKSA98541 1 19981004 A 2612 FIRE LIGHT BOEING 747 747146 NM PWA JT9 JT9D7J 52054 NE NR 2 ENGINE ILLUMINATED A CKSA K NONE N FALSE WARNING CR CRUISE 1 GL 23 702CK 20332 689460 NR 2 ENGINE 'B' LOOP FIRE DETECTION LIGHT ILLUMINATED, INDICATOR WENT OFF SCALE HIGH AND ERRATIC. INSPECTED LOOPS SYSTE M. OPS CHECK GOOD (TEST) IAW B747 M/M 26-11-00. 2 L 7 4 4F 4 F A20WE E20EA 1998101600586 19981016 00586 WP 1998 10 16 CKSA98542 1 19980929 A 2120 AIR DISTR DOUG DC8 DC863F 302198F WP COCKPIT ODOR A CKSA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 811CK 46147 DURING CLIMB-OUT, EXPERIENCED BAD SMELL IN THE COCKPIT. RAN NASI SYSTEM THROUGH ALL SETTINGS AND VISUALLY CHECKED INSTA LLATION OF SYSTEM. NO DEFECTS NOTED. 2 L 7 4 4F 4A25 1998101600587 19981016 00587 WP 1998 10 16 TWAA9816401 1 19981012 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9615W 53562 DURING MAINT CHECK, FOUND THREE EGRESS LIGHTS INOPERATIVE BETWEEN CABIN ROWS 3 AND 5. REPLACED ALL THREE BULBS. 2 L 7 2 4F RT A6WE 1998101600588 19981016 00588 WP 1998 10 16 TWAA9816402 1 19981012 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9615W 53562 DURING MAINT CHECK, FOUND RED EGRESS LIGHT INOPERATIVE AT CABIN ROW 22. REPLACED MODULES, (P/N 0105606-002, 0105606-004 ). 2 L 7 2 4F RT A6WE 1998101600589 19981016 00589 WP 1998 10 16 VJ9800523 1 19980917 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 737 & BS 639 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 HFEC INSPECTION DETECTED A CRACK ON RT SIDE LONGERON AT FS 639 AND AT RT SIDE LONGERON 1 AT FASTENER HOLE. CUT OUT CRAC KED AREA, APPROXIMATELY 10 INCHES IN DIAMETER AND CONFIRMED CRACK CONTAINED PER HFEC INSPECTION. CUT OUT CRACK, APPROXI MATELY.875 INCHES. FABRICATED AND INSTALLED INTERNAL AND EXTERNAL DOUBLERS IAW DC9 SRM 51-10-3, 51-30-2, 51-30-5, 53-04 FIG 40, AND DRG NR SRO 09530125. 2 L 7 2 4F A6WE 1998101600590 19981016 00590 WP 1998 10 16 VJ9800524 1 19981007 A 5321 FLOOR PANEL DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FWD ENTRY WAY FLOOR PANEL, NR 4691, CORRODED BEYOND LIMIT IAW DC9 SRM 53-01, FIG 1. REMOVED HAT SECTIONS, FABRICATED AN D INSTALLED NEW SKIN, REINSTALLED HAT SECTIONS IAW DC9 SRM 51-20-0, 51-10-3, 51-30-2, 53-20-0 FIG 2A, 51-10-2 AND 51-10- 4. 2 L 7 2 4F A6WE 1998101600591 19981016 00591 NM 1998 10 16 CKSA98562 1 19981008 A 5315 0160672315 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 AFTER REMOVAL OF CORROSION ON FLOORBEAM UPPER CAP REMAINING MATERIAL BEYOND SRM LIMITS. LOCATION STA 1680, WL 200, LBL 40. REPAIRED IAW CKF-AMD-038 SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDE R NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-03. 2 L 7 4 4F RT A20WE 1998101600592 19981016 00592 NM 1998 10 16 CKSA98563 1 19981008 A 5240 65B0489126 GATE BOEING 747 7472B4B 138481B NM R5 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 R5 DOOR UPPER GATE FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW CKF-AMD-073. FOUND DURING ACCOMPLISHMENT OF C D AND CPC P AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600593 19981016 00593 NM 1998 10 16 CKSA98564 1 19981008 A 5347 69B042573 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1710 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK AT STA 1700-1710, RBL 33, WL 199, ZONE 200 FOUND TO BE BEYOND SRM LIMITS. AREA OF APPROX 1.5 GROUND PAST LIM ITS. REPAIRED IAW CKF-AMD-030, CKF-AMD-074 SUPP SHEET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-03. 2 L 7 4 4F RT A20WE 1998101600594 19981016 00594 NM 1998 10 16 CKSA98565 1 19981008 A 5240 016US47413 GATE BOEING 747 7472B4B 138481B NM L4 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 L4 LOWER GATE FOUND BEYOND SRM LIMITS AFTER GRIND OUT. REPAIRED IAW SRM 51-30-02, ADJUSTED PER MM 52-11-01. FOUND DURI NG ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210 -09-04. 2 L 7 4 4F RT A20WE 1998101600595 19981016 00595 NM 1998 10 16 CKSA98566 1 19981008 A 5240 016US4751 GATE BOEING 747 7472B4B 138481B NM R4 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 R4 DOOR UPPER AND LOWER GATE FOUND BEYOND SRM LIMITS AFTER GRIND OUT. REPAIRED IAW SRM 51-30-02, ADJUSTED PER MM 52-11- 01. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-09-04. 2 L 7 4 4F RT A20WE 1998101600596 19981016 00596 NM 1998 10 16 CKSA98567 1 19981008 A 5347 69B042573 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1945-1970 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK AT STA 1945 TO 1970, WL 200, LBL 11.33 FOUND BEYOND SRM LIMITS AFTER GRIND OUT. REPAIRED IAW CKF-AMD-083 SUP P SHEET 2 THROUGH 7. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CO RROSION TASK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600597 19981016 00597 NM 1998 10 16 CKSA98568 1 19981008 A 5330 SKIN BOEING 747 7472B4B 138481B NM BS 1960-1972 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 STA 1960, STR 49R, 5 AREA ABOVE AND BELOW SKIN BUTT JOINT, SKIN IS BULGING AROUND FASTENERS. DISASSEMBLED FOR INSPECTIO N IAW BOEING CPM D6-41910 SEC 53-30-47 PART III. REPAIRED IAW CKF-AMD-095 SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-100-01-06. 2 L 7 4 4F RT A20WE 1998101600598 19981016 00598 NM 1998 10 16 CKSA98569 1 19981008 A 5230 SKIN BOEING 747 7472B4B 138481B NM CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 AFT CARGO DOOR SKIN AT STA 1832 FOUND TO BE BEYOND SRM LIMITS AFTER GRINDING OUT CORROSION. REPAIRED IAW CKF-AMD-086 SU PP SHEET 1. 2 L 7 4 4F RT A20WE 1998101600599 19981016 00599 NM 1998 10 16 CKSA98570 1 19981008 A 5315 65B3809345 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 FLOORBEAM UPPER CAP IN ZONE 200, STA 1780, WL 199, LBL 23 FOUND 1.5 SQUARE AREA OF CORROSION BEYOND SRM LIMITS. ALSO AT LBL 35 FOUND 1.5 X 2 AREA OF CORROSION BEYOND SRM LIMITS. REPAIRED IAW CKF-AMD-087 SUPP SHEETS 1-3. FOUND DURING ACCO MPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600600 19981016 00600 NM 1998 10 16 CKSA98571 1 19981008 A 5320 69B044801 ANGLE BOEING 747 7472B4B 138481B NM BS 1770 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SPLICE ANGLE HAS .7 X .6 AREA OF CORROSION AT STA 1770, LBL 11, WL 199. FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW CK F-AMD-088. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TA SK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600601 19981016 00601 NM 1998 10 16 CKSA98572 1 19981008 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1820 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK AT AFT MAIN DECK, STA 1820, WL 199, LBL 39 BEYOND SRM LIMITS. REPAIRED IAW CKF-AMD-101, CKF-AMD-113. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, JOB/TASK NUMBER 7DI1402. 2 L 7 4 4F RT A20WE 1998101600602 19981016 00602 NM 1998 10 16 CKSA98573 1 19981008 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1900-1910 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK AT AFT MAIN DECK, STA 1900 TO 1910, RBL 33, WL 199 CORRODED AREA .8 X .7 BEYOND SRM LIMITS. REPAIRED IAW CKF -AMD-103 SUPP SHEET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600603 19981016 00603 NM 1998 10 16 CKSA98574 1 19981008 A 5347 65B382733 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1900 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK AT AFT MAIN DECK ZONE 200, STA 1900, WL 199, RBL 11, AREA APPROX 1 X .8 CORRODED BEYOND SRM LIMITS. REPAIRED IAW CKF-AMD-104 SUPPLEMENTAL SHEET 1 & 2, ITEMS 1 THRU 3. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHIT A (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600604 19981016 00604 NM 1998 10 16 CKSA98575 1 19981008 A 5347 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1580 GOUGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 AT AFT MAIN DECK ZONE 200, STA 1580, LBL 33, WL 199 FOUND HAT SECTION OF SEAT TRACK HAS NUMEROUS AMOUNTS OF GOUGES ENCOM PASSING A 4.5 LENGTH X .4 WIDTH. REPAIRED IAW CKF-AMD-115 SUPP SHEET 2, CKF-AMD-145. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-03. 2 L 7 4 4F RT A20WE 1998101600605 19981016 00605 NM 1998 10 16 CKSA98576 1 19981008 A 5347 65B382711 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1970 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SEAT TRACK LOCATED AT AFT MAIN DECK ZONE 200, STA 1950 TO 2085, LBL 11, WL 199 HAS AREA OF CORROSION 1.5 X .9. REPAIRED IAW CKF-AMD-120- SUPP SHEETS 3, 4, 5, 6, 7. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WOR K ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-04. 2 L 7 4 4F RT A20WE 1998101600606 19981016 00606 NM 1998 10 16 CKSA98577 1 19981008 A 5313 65B041339 STRINGER BOEING 747 7472B4B 138481B NM BS 1508 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 STRINGER NR 65B04133-9 LOCATED AT LOWER CARGO AREA ZONE 100, STA 1660, STRINGER 47L HAD AREA 6 SQUARE OF CORROSION. REP AIRED IAW SRM 51-10-01, CKF-AMD-147, CKF-AMD-150 SUPP SHEETS 1, 1A, 2, 3, CKF-AMD-152. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-125-01-02. 2 L 7 4 4F RT A20WE 1998101600607 19981016 00607 NM 1998 10 16 CKSA98578 1 19981008 A 5320 65B07992255 STIFFENER BOEING 747 7472B4B 138481B NM BS 1245 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 DURING INSPECTION OF STA 1238 TO 1265 CANTED BULKHEAD FOUND AREAS OF CORROSION 3 X 1, 5 X 2 ON 65B07992-255 STIFFENER. R EPAIRED IAW CKF-CF-003, CKF-CF-009 SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-02-01. 2 L 7 4 4F RT A20WE 1998101600608 19981016 00608 NM 1998 10 16 CKSA98579 1 19981008 A 5315 65B1336316 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1331-1340 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 THE I/B SIDE OF FLOORBEAM WEB AT STA 1270 TO 1300, RBL 33, WL 189 CORRODED BEYOND SRM LIMITS. REPAIRED IAW CKF-CA-007 S UPP SHEET 1, SRM 53-10-07 PG 7, CKF-CA-019, CKF-CA-015 SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOE ING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-06. 2 L 7 4 4F RT A20WE 1998101600609 19981016 00609 NM 1998 10 16 CKSA98580 1 19981008 A 5210 65B250401 GATE BOEING 747 7472B4B 138481B NM PAX DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 UPPER AND LOWER GATE ASSY ON L3 DOOR CORRODED. BLEND-OUT BEYOND SRM LIMITS. REPAIRED IAW CKF-CA-003 ITEM 1, MM 747-52- 11. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-09. 2 L 7 4 4F RT A20WE 1998101600610 19981016 00610 NM 1998 10 16 CKSA98581 1 19981008 A 5330 65B154107 SKIN BOEING 747 7472B4B 138481B NM BS 1272 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SKIN PANEL ASSY AT C AFT, ZONE 200, STA 1272, WL 212, LBL 124 HAS CORROSION. BLEND OUT BEYOND SRM LIMITS. REPAIRED IAW CKF-CA-008. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-01-03. 2 L 7 4 4F RT A20WE 1998101600611 19981016 00611 NM 1998 10 16 CKSA98582 1 19981008 A 5210 STRAP BOEING 747 7472B4B 138481B NM 3R DOORWAY CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LWR FWD CORNER OF DOOR CUTOUT AT DOOR NR 3 RT, ZONE 250, STA 1319, WL 200 TO 208, RBL 126 CORRODED. BLEND OUT BEYOND SR M LIMITS. REPAIRED IAW ASA CKF-CA-020 SUPP SHEETS 1 & 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-200-01-03. 2 L 7 4 4F RT A20WE 1998101600612 19981016 00612 NM 1998 10 16 CKSA98583 1 19981008 A 5210 65B0988917 GATE BOEING 747 7472B4B 138481B NM PAX DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 R2 DOOR UPPER GATE CORRODED. BLEND OUT BEYOND SRM LIMITS. REPAIRED IAW CKF-B-011. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-210-09. 2 L 7 4 4F RT A20WE 1998101600613 19981016 00613 NM 1998 10 16 CKSA98584 1 19981008 A 5210 65B0988917 GATE BOEING 747 7472B4B 138481B NM PAX DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 L2 DOOR UPPER GATE ASSY CORRODED. BLEND OUT BEYOND SRM LIMITS. REPAIRED IAW CKF-B-010. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-200-01-02. 2 L 7 4 4F RT A20WE 1998101600614 19981016 00614 NM 1998 10 16 CKSA98585 1 19981008 A 5313 65B10097103 LONGERON BOEING 747 7472B4B 138481B NM BS 1322 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 FWD LONGERON CHORD AT LT W/W ZONE 100, STA 1322, LBL 126, WL 158 CORRODED. REPAIRED IAW CKF-EXB-080 SUPP SHEET 2, BOEIN G SB 747-53-2240. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORRO SION TASK CARD NUMBER C53-100-01-07. 2 L 7 4 4F RT A20WE 1998101600615 19981016 00615 NM 1998 10 16 CKSA98586 1 19981008 A 5320 65B06755601 SPLICE BOEING 747 7472B4B 138481B NM BS 1480-1540 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SPLICE PLATE LOCATED ON LWR BODY FAIRING SUPPORT STRUCTURE, ZONE 140, STA 1480 TO 1540, WL 90, BL 0 CORRODED. BLEND OUT BEYOND SRM LIMITS IAW 53-50-01. REPLACED PER REQMNTS OF 65B06755-1, CKF-EXB-068. FOUND DURING ACCOMPLISHMENT OF C D A ND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-190-01-02. 2 L 7 4 4F RT A20WE 1998101600616 19981016 00616 NM 1998 10 16 CKSA98587 1 19981008 A 5330 65B02696165 SKIN BOEING 747 7472B4B 138481B NM BS 2436 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SKIN LOCATED AT LT HORIZ STAB, ZONE 200, STA 2436, 15-21 LT, WL 265 CORRODED. BLEND OUT BEYOND SRM LIMITS. REPAIRED IA W SRM 53-30-03 FIG 41, DETAIL I AND CKF-EXB-069, SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WI CHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-310-01-01. 2 L 7 4 4F RT A20WE 1998101600617 19981016 00617 NM 1998 10 16 CKSA98588 1 19981008 A 5330 65B041181 SKIN BOEING 747 7472B4B 138481B NM BS 830 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SKIN PANEL LOCATED AT STA 830, WL 90, LBL 13 CORRODED. BLEND OUT BEYOND SRM LIMITS PER SRM 53-30-03 FIG 2. REPAIRED IA W CKF-EXB-089 SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO 280, CORROSION TASK CARD NUMBER C53-100-01-03. 2 L 7 4 4F RT A20WE 1998101600618 19981016 00618 NM 1998 10 16 CKSA98589 1 19981008 A 5330 65B041522 SKIN BOEING 747 7472B4B 138481B NM BS 2180 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LOWER LOBE SKIN BETWEEN STA 2140 AND 2190, STRINGERS 46R TO 46L, WL 125 HAS WIDESPREAD AREA OF CORROSION. BLEND OUT BEY OND SRM LIMITS. REPAIRED IAW CKF-EXB-020 AND BOEING SB 747-53-2156. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOE ING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-125-01-02. 2 L 7 4 4F RT A20WE 1998101600619 19981016 00619 NM 1998 10 16 CKSA98590 1 19981008 A 5313 65B10097103 LONGERON BOEING 747 7472B4B 138481B NM BS 1220 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LONGERON CHORD FWD END AT STA 1220 TO 1238 CORRODED. AFTER CORROSION REMOVED, NDI SHOWED 10 INCH CRACK DUE TO INTERGRAN ULAR CORROSION. REPAIRED IAW ASA CKF-EXB-080 SUPP SHEETS 1 & 2. 2 L 7 4 4F RT A20WE 1998101600620 19981016 00620 NM 1998 10 16 CKSA98591 1 19981008 A 5753 65B0207011 PANEL BOEING 747 7472B4B 138481B NM LT TE FLAP DELAMINATED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LT I/B FLAP PANEL DELAMINATED AND CORRODED. REPAIRED IAW ASA CKF-EXW-021, SRM 51-40-06, D6-500. FOUND DURING ACCOMPLIS HMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C57-560-01-01. 2 L 7 4 4F RT A20WE 1998101600621 19981016 00621 NM 1998 10 16 CKSA98592 1 19981008 A 5753 SPAR BOEING 747 7472B4B 138481B NM LT TE MIDFLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LT I/B MIDFLAP REAR SPAR LWR CHORD STA 136 HAD 10 X 2 AREA OF CORROSION ON LWR SFC. BLEND OUT BEYOND SRM LIMITS. REPAI RED IAW ASA CKF-EXW-050 SUPP SHEET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C57-560-01-01. 2 L 7 4 4F RT A20WE 1998101600622 19981016 00622 NM 1998 10 16 CKSA98593 1 19981008 A 5753 65B02025 SKIN BOEING 747 7472B4B 138481B NM LT TE MIDFLAP DELAMINATED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LT I/B MIDFLAP SKIN HAD 4 X 10 AREA OF DELAMINATION AND .30 HOLE. REPAIRED IAW CKF-EXW-051 SUPP SHEETS 2, 3, 4. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C57 -560-01-01. 2 L 7 4 4F RT A20WE 1998101600623 19981016 00623 NM 1998 10 16 CKSA98594 1 19981008 A 5753 65B02029 SPAR BOEING 747 7472B4B 138481B NM LT TE MIDFLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LT I/B MIDFLAP REAR SPAR WEB CORRODED. BLEND OUT BEYOND SRM LIMITS. REPAIRED IAW ASA CKF-EXW-052 SUPP SHEETS 2, 3, 4. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUM BER C57-560-01-01. 2 L 7 4 4F RT A20WE 1998101600624 19981016 00624 NM 1998 10 16 CKSA98595 1 19981008 A 5753 63B1307111 BEARING PLATE BOEING 747 7472B4B 138481B NM NR 4 TE FLAP TRK CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 NR 4 FLAP TRACK BEARING PLATE AND BUSHING HOLE CORROSION EXCEEDS LIMITS. REPAIRED IAW OHM 57-52-70 REPAIR 6.1 PARA 4, S B 747-57-2207. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSIO N TASK CARD NUMBER C57-560-03-01. 2 L 7 4 4F RT A20WE 1998101600625 19981016 00625 NM 1998 10 16 CKSA98596 1 19981008 A 5730 SKIN BOEING 747 7472B4B 138481B NM WS 1120 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 AT TOP SIDE OF RT WING STA 1120, WL 185, RBL 125, 3 AREAS OF CORROSION. AREA 1, .5 X 6, AREA 2, 3 X .9, AREA 3, .70 X 1 .30. REPAIRED IAW CKF-EXW-072 SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WOR K ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-190-01-02. 2 L 7 4 4F RT A20WE 1998101600626 19981016 00626 NM 1998 10 16 CKSA98597 1 19981008 A 5753 65B3901632 PANEL BOEING 747 7472B4B 138481B NM RT TE FOREFLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 RIGHT HAND I/B FOREFLAP, LWR SURFACE I/B FWD PANEL HAD CORROSION. FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW ENG DWG 65B39011. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TAS K CARD NUMBER C57-560-01-02. 2 L 7 4 4F RT A20WE 1998101600627 19981016 00627 NM 1998 10 16 CKSA98598 1 19981008 A 5751 610R9A SKIN BOEING 747 7472B4B 138481B NM LT AILERON CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 LT AILERON T/E GROUND STRAP DISBONDED AND CORRODED AT STATIC DISCHARGERS. REPAIRED IAW CKF-EXW-088 SUPP SHEET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C5 7-560-01-01. 2 L 7 4 4F RT A20WE 1998101600628 19981016 00628 1998 10 16 CKSA98599 4 19981008 A 2360 610B9A GROUND STRAP BOEING 747 7472B4B 138481B NM RT AILERON DISBONDED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 RT AILERON O/B GROUND STRAPS AT T/E CORRODED AND DISBONDED AT STATIC DISCHARGERS. REPAIRED IAW ASA CKF-EXW-090 SUPP SHE ET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CA RD NUMBER C57-560-01-02. 2 L 7 4 4F RT A20WE 1998101600629 19981016 00629 NM 1998 10 16 CKSA98600 1 19981008 A 5320 65B01742 SHEAR TIE BOEING 747 7472B4B 138481B NM BS 980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SHEAR TIE AT ZONE 120, STA 980, STR 47L, WL 95, LBL 0, HAD AREA OF CORROSION APPROX 3 X 4. ALSO STR 47R AT SAME LOCATIO N HAD AREA OF CORROSION APPROX 2 X 6. REPAIRED IAW SRM 747-51-10-01 AND ASA CKF KI-022. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-125-01-01. 2 L 7 4 4F RT A20WE 1998101600630 19981016 00630 NM 1998 10 16 CKSA98601 1 19981008 A 5320 65B0675621 SPLICE BOEING 747 7472B4B 138481B NM BS 960 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 ON WING TO BODY FAIRING SUPPORT STRUCTURE, STA 960, WL 95 TO 98, RBL 1-RBL 22 SPLICE WEBS FOUND AREA 3 X 22 CORRODED. B LEND OUT BEYOND SRM LIMITS. REPAIRED IAW ASA CKF-K1-031 SUPP SHEET 1. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT B OEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-190-01-02. 2 L 7 4 4F RT A20WE 1998101600631 19981016 00631 NM 1998 10 16 CKSA98602 1 19981008 A 5230 65B096389 SKIN BOEING 747 7472B4B 138481B NM CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 FWD CARGO DOOR AT ZONE 120, STA 592, INTERIOR DOOR SKIN/WEB HAD AREA 1 X 3 OF CORROSION. FOUND TO BE OUT OF LIMITS. RE PAIRED IAW ASA CKF-K1-026 SUPP SHEETS 3 & 4. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WOR K ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-110-01-02. 2 L 7 4 4F RT A20WE 1998101600632 19981016 00632 NM 1998 10 16 CKSA98603 1 19981008 A 5330 65B072012 SKIN BOEING 747 7472B4B 138481B NM BS 550 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 SKIN PANEL AT STA 550, LBL 15-18, WL 95 HAD AREA 3.5 X 6 CORRODED. REPAIRED IAW ASA CKF-KI-51 SUPP SHEET 2. FOUND DURI NG ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C53-125 -01-01. 2 L 7 4 4F RT A20WE 1998101600633 19981016 00633 NM 1998 10 16 CKSA98604 1 19981008 A 5313 65B0410722 STRINGER BOEING 747 7472B4B 138481B NM BS 550 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 STRINGER NEAR FWD LAV SVC PANEL ZONE 120, STA 550, STR 46L, WL 95, LBL 15 HAD AREA 7 X 2 CORRODED. REPAIRED IAW ASA CKF -K1-051 SUPP SHEETS 1 & 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO2 80, CORROSION TASK CARD NUMBER C53-125-01-01. 2 L 7 4 4F RT A20WE 1998101600634 19981016 00634 NM 1998 10 16 CKSA98605 1 19981008 A 5400 65B903772 STIFFENER BOEING 747 7472B4B 138481B NM NR 1 PYLON CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 712CK 21098 NR 2 STIFFENER IN RT NR 1 PYLON HAS NUMEROUS AREAS OF CORROSION. NDT VERIFIED OUT OF LIMITS. REPAIRED IAW ASA CKF-PYL- 017, CKF-PYL-029 & CKF-PYL-031 INCL ALL SUPP SHEETS. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIA B). WORK ORDER NUMBER MO280, ASA TASK CARD NUMBER CKF-PYL-003. 2 L 7 4 4F RT A20WE 1998101600635 19981016 00635 NM 1998 10 16 K3HA980120 1 19981007 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 FORWARD CABIN AREA EMERGENCY LIGHT INOP. REMOVED AND REPLACED FORWARD CABIN EMERGENCY AREA LIGHT AND BATTERIES IAW 33-5 0-81, OPS CHECK GOOD. EMERGENCY AREA LIGHT (P/N 11-0283-3), (S/N 23021). 2 L 7 3 4F A3WE 1998101600636 19981016 00636 NM 1998 10 16 K3HA980121 1 19981011 A 3411 BACH30BC060150 STATIC LINE BOEING 727 727225 1384077 NM LEFT INOPERATIVE A K3HA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 25 8883Z 21580 CAPTAINS ALTIMETER AND AIRSPEED INDICATION IS IN ERROR. BOTH READ LOW AND ERROR DIFFERENTIAL INCREASES WITH AIRCRAFT AL TITUDE. PERFORMED STATIC CHECK. LEAK INTERMITTANT ON CAPTAINS SIDE. CHECKED ALL LINES, CARGO AND LOWER-43. REMOVED A ND REPLACED STATIC LINES TO CAPTAINS ALTIMETER AND CAPTAINS IVISI PER MM 34-11-0. PERFORMED PITOT STATIC LEAK CHECK OF BOTH CAPTAINS AND FIRST OFFICERS SYSTEM PER MM 34-11-0 TO 25,000 FT ALL READINGS CHECKED OK. REMOVED TAPES AFTER CHECK. LEAK AND OPS CHECK OK. 2 L 7 3 4F A3WE 1998101600637 19981016 00637 WP 1998 10 16 IXXA9800076 1 19980925 A 2612 898475 FIRE LOOP DOUG DC8 DC871F 302199D WP NR 1 ENGINE DEFECTIVE A IXXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 GL 23 825BX 253 45978 EN ROUTE, THE NUMBER ONE ENGINE FIRE WARNING SOUNDED WITH THE MASTER FIRE WARNING LIGHT ILLUMINATED. THE FLIGHT CREW SE CURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND DISCHARGED ONE FIRE BOTTLE. THE FIRE WARNING LIGHT EXTINGUSHED FOLLOW ING FIRE BOTTLE DISCHARGE. THE FLIGHT CONTINUED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE AND FOUND NO EVIDENCE OF A FIRE. THE FIRE WARNING LOOPS AND ASSOCIATED WIRING WERE INSPECTED LOCATING A DEFECTIVE FIRE WAR NING LOOP, AND WAS REPLACED. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MAN UAL. 2 L 7 4 4F RT 4A25 1998101600638 19981016 00638 WP 1998 10 16 IXXA9800077 1 19980925 A 3260 CONNECTOR DOUG DC8 DC871F 302199D WP LT MLG DOOR CORRODED A IXXA K NONE N FALSE WARNING DE DESCENT 1 GL 23 822BX 2111 45813 DURING CLIMBOUT FROM A MISSED APPROACH, THE CREW RETRACTED THE LANDING GEAR, THE LANDING GEAR DOOR WARNING REMAINED ILLU MINATED. THE CREW CYCLED THE GEAR WITH THE DOOR WARNING INDICATION REMAINING THE SAME. MAINTENANCE INSPECTED THE LANDI NG GEAR DOOR SWITCHES WHICH REVEALED THE LEFT MAIN GEAR DOOR SWITCH CANNON PLUG CORRODED. MAINTENANCE CLEANED THE DOOR SWITCH AND THE CANNON PLUG. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL TEST. 2 L 7 4 4F RT 4A25 1998101600639 19981016 00639 WP 1998 10 16 IXXA9800078 1 19981008 A 5330 561386259 PLATING DOUG DC8 DC871F 302199D WP BS 21-30 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 824BX 559 45946 DURING ROUTINE PREFLIGHT INSPECTION, FOUND THE FUSELAGE EXTERNAL PLATING WITH CORROSION BULGE, TWO MISSING RIVET HEADS A ND THREE CRACKS MIGRATING FROM ONE MISSING RIVET HEADS BETWEEN FUSELAGE STATION -21.0 TO 30.0 BETWEEN LONGERON 31 RIGHT AND 35 LEFT. THE AIRCRAFT VISITED HEAVY MAINTENANCE FOR REPAIRS. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION A ND INSTALLATION AN INTERNAL FILLER, TWO INTERNAL SPLICE DOUBLERS, AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH DOUGLA S FAX FILE NUMBER 98-10-08-009 AND DOUGLAS STRUCTUAL REPAIR MANUAL. 2 L 7 4 4F RT 4A25 1998101600640 19981016 00640 WP 1998 10 16 IXXA9800079 1 19981012 A 3231 RETRACT MECH DOUG DC8 DC862 3021970 WP NLG DOOR LACK OF LUBE A IXXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 23 728PL 45918 AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW NOTICED A NOSE GEAR DOOR HAD FALLEN OPEN CAUSING A L OUD NOISE AND SLIGHT VIBRATION FROM THE NOSE WHEEL WELL AREA. THE CREW CYCLED THE GEAR, THE VIBRATION CONDITION WAS STI LL PRESENT. THE AIRCRAFT RETURNED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE LEFT FORWARD NOSE GEAR DOOR WAS OPEN. MAINTENANCE LUBRICATED THE FORWARD DOOR TELESCOPING ROD LINKAGE ASSEMBLY AND SECURED THE DOOR. 2 L 7 4 4F 4A25 1998101600641 19981016 00641 WP 1998 10 16 IXXA9800080 1 19981012 A 3244 9550328 TIRES DOUG DC8 DC862 3021970 WP NLG WORN A IXXA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 GL 23 728PL 447 45918 AFTER TAKEOFF, WHEN THE LANDING GEAR WAS RETRACTED, THE FLIGHT CREW HEARD AND FELT A VIBRATION THROUGH THE COCKPIT FLOO R. THE AIRCRAFT RETURNED TO RMS FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT WHICH REVEALED THE NOSE TIRES OUT OF ROUND. MAINTENANCE PERFORMED A SUCCESSFUL NOSE GEAR SWING IN ACCORDANCE WITH THE MAINTENANCE MANUAL. 2 L 7 4 4F 4A25 1998101600642 19981016 00642 NM 1998 10 16 AWXA9800209 1 19981003 A 5313 STRINGER BOEING 737 737277 1384570 NM BS 540 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 184AW 22651 CRACK AT LT STR 14 STA 540 IN SKIN. REPAIRED PER SRM 53-30-03 FIG 9. 2 L 7 2 4F RT A16WE 1998101600643 19981016 00643 NE 1998 10 16 AWXA9800210 2 19981008 A 7530 ETPU10002C TPU BOEING 757 7572S7 1384962 NM RROYCE RB211 RB211535E4 54555 NE NR 2 ENGINE FAILED A AWXA A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 WP 28 906AW 22661 10969 23568 ENGINE SHUTDOWN, NUMBER 2 ENGINE FLAMED OUT DURING DESCENT. EICAS MESSAGE APPEARED NR 2 ENGINE LOW PRESSURE PUMP. FOM PROCEDURE COMPLIED WITH. PRECAUTIONARY INSPECTIONS COMPLIED WITH. BITE TEST ON TPU SHOWED FAULT CODES B3, B5, B6, B9 & B20. REMOVED AND REPLACED TPU. REMOVED AND REPLACED THE DFDU DISC. INSPECTED WIRE HARNESS FROM TPU TO TFU FOR SECUR ITY AND ANY CHAFING. NO DEFECTS NOTED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998101600644 19981016 00644 EU 1998 10 16 AWXA9800211 1 19981009 A 7921 500260011 OIL COOLER AIRBUS 320 A320231 3930325 EU NR 1 ENGINE CRACKED A AWXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 644AW 18960 23128 317 NR 1 ENGINE OIL PRESSURE DROPPED AFTER TAKEOFF. ENGINE WAS SHUTDOWN, OIL QUANTITY DROPPED TO ZERO. LEAK FOUND AT LOWER SECTION OF NR 1 ENGINE AIR/OIL COOLER. REPLACED AIR/OIL COOLER AND SERVICED OIL TANK. 2 L 7 2 4F RT A28NM 1998101600645 19981016 00645 EU 1998 10 16 PNSA980901 1 19980903 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A PNSA O OTHER N FALSE WARNING DE DESCENT 1 AL 03 685PA 212 LAV SMOKE DETECT LIGHT ILLUMINATED IN FLIGHT. FLIGHT CREW INVESTIGATED AND DID NOT SMELL SMOKE. AIRCRAFT LANDED UNEVEN TFULLY. MAINTENANCE INVESTIGATED AND COULD NOT DETERMINE SOURCE. IT WAS NOTICED THAT THE LAV OVERHEAD LIGHT FLICKERED INTERMITTANTLY WHEN THE LAV DOOR WAS CLOSED. HOWEVER, THE LIGHT DID NOT EMIT SMOKE. LAMP WAS REPLACED ANYWAY AND NO FU RTHER PROBLEMS NOTED WITH SYSTEM. SYSTEM TESTS WERE NORMAL. 2 L 7 2 4T RT A52EU 1998101600646 19981016 00646 SO 1998 10 16 PNSA980902 1 19980919 A 2410 78614 PULLEY PIPER PA31 PA31350 7103110 SO RT ALTERNATOR WORN A PNSA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 03 15PR 318052011 RT ALTERNATOR LIGHT CAME ON WHILE CRUISING IN PRECIP. RETURNED TO BASE. REPLACED ALTERNATOR PULLEY DUE TO WEAR. 1 L 7 2 3O A20SO 1998101600647 19981016 00647 1998 10 16 PNSA980904 4 19980908 A 3416 EA801 ENCODING ALT CESSNA 441 441 2076020 CE COCKPIT MALFUNCTIONED A PNSA A UNSCHED LANDING O OTHER CL CLIMB 1 AL 03 544AL 2964 4410120 ENCODER REPORTED AS INACCURATE. AIRCRAFT RETURNED TO BASE. NO FAULT FOUND. NO FURTHER PROBLEMS NOTED. 1 L 7 2 3T RT A28CE 1998101600648 19981016 00648 1998 10 16 PNSA980905 2 19980902 A 8550 BREATHER GULSTM G44 G44 3951502 SO ENG OIL SYST CHAFED A PNSA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 AL 03 17481 1360 OIL FILM DEVELOPED ON WINDSHIELD SHORTLY AFTER TAKEOFF. RETURNED TO BASE. FOUND CHAFED BREATHER. REPLACED TUBING. 1 H 7 2 3I O A734 1998101600649 19981016 00649 SW 1998 10 16 PNSA980906 1 19980903 A 2910 2781032776 LINE SWRNGN SA227 SA227AC 8780603 SW RT ENGINE SPLIT A PNSA K NONE K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 AL 03 640PA AC759B ON PREFLIGHT FOR NEXT LEG, FOUND HYDRAULIC FLUID LEAKING FROM RT ENGINE. FOUND SPLIT HYDRAULIC LINE IN RT NACELLE. REP LACED LINE. 2 L 7 2 4T RT A8SW 1998101600650 19981016 00650 WP 1998 10 16 CALA9801943 1 19981013 A 3520 CCC778202 LATCH DOUG DC9 DC982 3022082 WP CABIN LACK OF LUBE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 OXYGEN COMPARTMENT 30 RT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00. 2 L 7 2 4F A6WE 1998101600651 19981016 00651 WP 1998 10 16 CALA9801944 1 19981013 A 3520 CCC778202 LATCH DOUG DC9 DC982 3022082 WP CABIN LACK OF LUBE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 OXYGEN COMPARTMENT 23 RT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00. 2 L 7 2 4F A6WE 1998101600652 19981016 00652 WP 1998 10 16 CALA9801945 1 19981013 A 3520 CCC77820 LATCH DOUG DC9 DC982 3022082 WP CABIN LACK OF LUBE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 OXYGEN COMPARTMENT 26LT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00. 2 L 7 2 4F A6WE 1998101600653 19981016 00653 WP 1998 10 16 CALA9801946 1 19981013 A 3520 CCC77820 LATCH DOUG DC9 DC982 3022082 WP CABIN LACK OF LUBE A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 OXYGEN COMPARTMENT 7RT DID NOT OPEN ON TEST. LUBRICATED LATCH PER MM 35-20-00. 2 L 7 2 4F A6WE 1998101600654 19981016 00654 NM 1998 10 16 CALA9801947 1 19981012 A 5753 FAIRING BOEING 727 727224 1384076 NM NR 6 FLAP TRACK CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 NR 6 FLAP TRACK MID FAIRING IS CRACKED .5 INCH LONG AT SKIN AFT EDGE. STOP DRILLED CRACK, HFEC INSP, FABRICATED TYPICAL REPAIR, DRILLED, DEBURRED, COUNTERSUNK, INSTALLED REPAIR. REMOVED AN INSTALLED TRACK GUIDE, TREATED, PRIMED PER SRM 51 -10-1, 51-40-2, 51-30-2, 51-10-2, AND NDT MANUAL 51-00-00. 2 L 7 3 4F A3WE 1998101600655 19981016 00655 NM 1998 10 16 CALA9801948 1 19981012 A 5330 SKIN BOEING 737 7373T0 1384582 NM BS 211-235 PITTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14334 23572 FOUND EVIDENCE OF LIGHTNING STRIKE JUST BELOW CAPTAINS SLIDING WINDOW. BURNISHED DAMAGE PER SRM 53-00-01. ISSUED DIP F OR PERMANENT REPAIR. 2 L 7 2 4F RT A16WE 1998101600657 19981016 00657 NM 1998 10 16 9810186730 1 19980812 A 5754 WEB BOEING 747 7472J9F 1384806 NM NR 12 LE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING M-CHECK, FOUND CRACKS IN THE CLOSURE PANEL/WEB OF THE NR 12 KRUEGER FLAP. REPAIRED PER EA 67-158217. 2 L 7 4 4F RT A20WE 1998101600658 19981016 00658 NM 1998 10 16 9810196638 1 19980922 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 1299-1317 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 638US 23549 DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE UPPER CHORD OF THE LONGITUDINAL FLOOR BEAMS FROM FS 1299-1317, RBL 11 AND 33. REPAIRED PER EA 66-158693. 2 L 7 4 4F A20WE 1998101600659 19981016 00659 WP 1998 10 16 9810201160 1 19980924 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 459 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 160US 46769 DURING M-CHECK, FOUND CRACK ON LOWER NOSE FUSELAGE FRAME AT FS 459. REPAIRED PER EA 11-157988. 2 L 7 3 4F A22WE 1998101600660 19981016 00660 WP 1998 10 16 9810211160 1 19980921 A 5315 FLOORBEAM DOUG DC10 DC1040 3023508 WP BS 1821 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 160US 46769 DURING M-CHECK, FOUND CRACK AT THE AFT CARGO FLOORBEAM UPPER CHORD UNDER THE LEFT SEAT TRACK AT FS 1821. REPAIRED PER E A 11-161103. 2 L 7 3 4F A22WE 1998101600661 19981016 00661 WP 1998 10 16 9810221160 1 19980917 A 5313 LONGERON DOUG DC10 DC1040 3023508 WP BS 1159-1179 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 160US 46769 DURING M-CHECK, FOUND CORROSION ON LONGERON INBOARD FLANGE UPPER SIDE AT FS 1159-1179, LONGERON 27L. REPAIRED PER EA 11 -160045. 2 L 7 3 4F A22WE 1998101600662 19981016 00662 WP 1998 10 16 9810239998 1 19980812 A 5314 KEEL BEAM DOUG DC9 DC931 3022065 WP BS 630 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8934E 47143 DURING M-CHECK, FOUND CORROSION ON THE FORWARD SECTION OF THE KEEL BEAM WEB AND GOUGED OVER LONGERON 30 AT FS 630. REPA IRED PER EA 99-159284. 2 L 7 2 4F A6WE 1998101600663 19981016 00663 EA 1998 10 16 COMA9860293 1 19981003 A 2750 601R93106403 FLEX SHAFT CNDAIR CL600 CL6002B19 EA RT WING SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 RIGHT OUTBOARD FLAP NR 4 FLEX SHAFT HAS STRAND SEPARATION. REPLACED FLEX SHAFT. 2 L 7 2 4F RT A21EA 1998101600664 19981016 00664 EA 1998 10 16 COMA9860294 1 19981003 A 2750 601R93106209 FLEX SHAFT CNDAIR CL600 CL6002B19 EA LT WING WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 LEFT INBOARD FLAP NR 2 FLEX DRIVE HEX DRIVE IS WORN. REPLACED FLEX DRIVE. 2 L 7 2 4F RT A21EA 1998101600665 19981016 00665 EA 1998 10 16 COMA9860295 1 19981003 A 5753 601R145011 SKIN CNDAIR CL600 CL6002B19 EA LT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7156 7091 LEFT OUTBOARD FLAP, OUTBOARD B.U.T.E. DOOR ROLLER CONTRACT SURFACE ON VANE IS WORN FLUSH WITH FLAP CONTOUR, CAUSING LEAD ING EDGE TO CONTACT AIRCRAFT. REPLACED LEFT OUTBOARD FLAP. 2 L 7 2 4F RT A21EA 1998101600666 19981016 00666 EA 1998 10 16 COMA9860296 1 19981005 A 5320 601R3520521 ANGLE CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 951CA 7091 CARGO DOOR STEP PLATE ANGLE BROKEN. REPLACED ANGLE. 2 L 7 2 4F RT A21EA 1998101600667 19981016 00667 EU 1998 10 16 QXEA9801433 1 19981007 A 2170 39862611 COALESCER BAG FOKKER F28 F28MK4000 4990810 EU COCKPIT CONTAMINATED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 486US 2500 2030 11237 COCKPIT PACK SMELLS WHEN HEAT IS DEMANDED. REPLACED WATER SOCK IAW MM 21-70-00, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600668 19981016 00668 EU 1998 10 16 QXEA9801434 1 19981008 A 2530 6008905 RECEPTICAL FOKKER F28 F28MK4000 4990810 EU GALLEY SHORTED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 494US 2897 482 11167 NR 2 WARMER IN GALLEY SMELLS OF HOT ELECTRICAL WIRE. FOUND JUG RECEPTICAL ARCING, POOR PIN TENSION. REPLACED RECEPTICA L, INSTALLED JUG. OPERATION CHECK GOOD. NO SMELLS NOTED. 2 L 7 2 4F RT A20EU 1998101600669 19981016 00669 EU 1998 10 16 QXEA9801436 1 19981009 A 3310 561408B2L2 BALLAST FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 486US 11237 ACRID SMELL OF BALLAST IN CAPTAINS SIDE OF FLIGHT DECK. REPLACED BALLAST TRANSFORMER, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600670 19981016 00670 EU 1998 10 16 QXEA9801437 1 19981008 A 3350 4500606 LIGHT FOKKER F28 F28MK4000 4990810 EU CABIN INOPERATIVE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 490US 3324 437 11152 BOTH CABIN OVERHEAD EXIT SIGNS AT ROW 8 INOP. REPLACED BOTH SIGNS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600671 19981016 00671 EU 1998 10 16 QXEA9801438 1 19981009 A 3350 MGG1055 LAMP GRIMES 5515900004 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 475AU 11222 EXIT (EMERGENCY) LIGHT AT SEAT 8A INOP. RELAMPED, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600672 19981016 00672 EU 1998 10 16 QXEA9801439 1 19981010 A 3350 MGG1055 LAMP GRIMES 5515900004 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 476US 11224 EXIT SIGN 8A INOP. RELAMPED EXIT SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600673 19981016 00673 EU 1998 10 16 QXEA9801440 1 19981010 A 3350 MGG1055 LAMP GRIMES 5515900004 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 477AU 11226 EMERGENCY EXIT SIGN FORWARD SIDE ROW 8 INOP. RELAMPED EMERGENCY EXIT SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600674 19981016 00674 EU 1998 10 16 QXEA9801441 1 19981010 A 3350 MGG1055 LAMP GRIMES 5515900004 FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 487US 11238 EMERGENCY EXIT SIGN AFT SIDE OF ROW 8 INOP. RELAMPED EMERGENCY EXIT SIGN, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600675 19981016 00675 EU 1998 10 16 QXEA9801442 1 19981009 A 3350 6008905 BATTERY FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 499US 3228 1681 11182 EXTERIOR WING ROUTE TRAILING EDGE EMERGENCY LIGHTS INOP. REPLACED NR 8 POSITION BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600676 19981016 00676 EU 1998 10 16 QXEA9801443 1 19981009 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR INOPERATIVE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 494US 11167 MAIN CABIN DOOR HANDLE INOP. PERFORMED FUNCTIONAL TEST OF INBOARD AND OUTBOARD DOOR CONTROL SYSTEM. NO FAULTS FOUND. 2 L 7 2 4F RT A20EU 1998101600677 19981016 00677 EU 1998 10 16 QXEA981435 1 19981010 A 3310 561408B2L2 BALLAST FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 477AU 11226 ACRID SMELL IN COCKPIT. REPLACED BALLAST AND ALL ASSOCIATED LIGHTS, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1998101600678 19981016 00678 NM 1998 10 16 98FDEA00648 1 19981012 A 3040 SEAL DOUG MD11 MD11 3023602 NM WINDSHIELD WIPER OUT OF POSITION A FDEA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 25 584FE 48436 AFTER T/O, HIGH PITCH NOISE FROM UNDER COCKPIT. THE CABIN OUTFLOW WAS CLOSED AND AVIONIC FAN OVERRIDE CAME ON. A/C WOU LDN'T PRESS AND CLIMB STOP AT 10,000 FT, DUMP FUEL AND RETURNED. T/S FOUND WINDSHIELD WIPER MTR ASSY PANEL SEAL OUT OF POSITION. REPOSITIONED SEAL, CKS OK. 2 L 7 3 4F RT A22WE 1998101600679 19981016 00679 NM 1998 10 16 98FDEA00649 1 19981013 A 5320 651592220 CHORD BOEING 727 72722 1384002 NM BS 380 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 WHILE WORKING NR 0213 FOUND CORROSION ON FAIL-SAFE CHORD, BS 380 BETWEEN STR 25 TO 26 RT. *S/D* REPAIRED FAIL-SAFE CHO RD BS 380 BETWEEN STR 25-26 RT IAW FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1998101600680 19981016 00680 NM 1998 10 16 98FDEA00650 1 19981013 A 5320 651838712 DOUBLER BOEING 727 72722 1384002 NM BS 961-990 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 WHILE WORKING NR0186, FOUND INTERNAL DOUBLER AT BS 961 TO 990, STR 28 TO 29 RT TO BE CORRODED AND OUT OF LIMITS PER SRM. 2 L 7 3 4F A3WE 1998101600681 19981016 00681 NM 1998 10 16 98FDEA00596 1 19980928 A 5320 651627910 BEAM BOEING 727 72722 1384002 NM BS 810-798 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 CORROSION UNDER NUT PLATE ON FLANGE OF LONGITUDINAL BEAM BS 798, LBL 25, WL 208. *S/D* REMOVED AND REPLACED LONGITUDIN AL BS 798, LBL 25, WL 208 PER FED-EX SRM 51-30-2, BOEING DWG 65-16279. 2 L 7 3 4F A3WE 1998101600682 19981016 00682 NM 1998 10 16 98FDEA00641 1 19981006 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM CARGO COMPT CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CORROSION MAIN CARGO FLOORBEAM BS 620 AT LBL 45.5 AND 2 HOLES CORRODED BETWEEN LBL 45.5 AND LBL 24.75 FWD SIDE OF FLOORB EAM UPPER CHORD. NOTE: 2 HOLES BETWEEN LBL 24.5 AND LBL 45.5 ARE NOT MAJOR REPAIRS. REPAIR CORROSION DAMAGE AT LBL 45. 5 BS 620 PER AARD 53-10-07-2 FIG 1 AND REMOVED CORROSION ON 2 HOLES BETWEEN LBL 45.5 AND LBL 24.75 PER 51-10-6. ALODINE D AND PRIMED PER MM 51-20-0. 2 L 7 3 4F A3WE 1998101600683 19981016 00683 WP 1998 10 16 ABXA9800889 1 19981009 A 5610 59124151 WINDOW DOUG DC8 DC861 3021952 WP COCKPIT LACK OF LUBE A ABXA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 849AX 45891 CAPTAIN'S SLIDING WINDOW (EMERG EXIT) VERY DIFFICULT TO OPEN. CLEANED AND LUBRICATED MECHANISM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998101600684 19981016 00684 WP 1998 10 16 ABXA9800890 1 19981008 A 5610 AN25341665 PIN DOUG DC8 DC861 3021952 WP SLIDING WINDOW MISSING A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 FIRST OFFICER'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN. FOUND PIN MISSING. REPLACED PIN, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998101600685 19981016 00685 NM 1998 10 16 VNAA9810008 1 19981008 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE BIRD STRIKE A VNAA K NONE O OTHER DE DESCENT 1 GL 07 457PS 3048 DURING THE DESCENT, THE AIRCRAFT WAS STRUCK BY A BIRD ON THE FUSELAGE, BELOW THE LEFT HAND FORWARD WINDSCREEN. THE AIRC RAFT CONTINUED THE DESCENT INTO PIT AND LANDED NORMALLY. MAINTENANCE CLEANED AND INSPECTED THE FORWARD FUSELAGE, IN ACC ORDANCE WITH DORNIER MAINTENANCE MANUAL 05-57-07. NO DAMAGE WAS FOUND. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101600686 19981016 00686 NM 1998 10 16 VNAA9810009 1 19981010 A 6120 DOLN511F07SND01 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE DIRTY A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 431JS 3028 THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND CLEANED THE RIGHT HAND PROPELLER OVERSPEED GOVERNOR CANNON PLUG, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-01-03. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101600687 19981016 00687 NM 1998 10 16 USAASB98241 1 19980913 A 5270 189929 SENSOR BOEING 737 737201 1384454 NM FUSELAGE OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 226US 21815 ATL - FLT 496 - AFTER TAKEOFF AT APPROXIMATELY 500 FT, THE FORWARD CARGO DOOR WARNING LIGHT ILLUMINATED. FLIGHT RETURNE D TO FIELD AT ATL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD CARGO DOOR SENSOR OUT OF ADJUSTMENT. ADJUSTED SENSOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998101600688 19981016 00688 NM 1998 10 16 USAA980339 1 19980807 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 950 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 42187 22886 TPA - DURING CX-5 CHECK EDDY CURRENT, FOUND A .125 INCH CRACK IN OUTER SKIN AT LOWER CORNER OF AFT ENTRY DOOR, LOWER HIN GE CUTOUT STATION 950.5 2.5 INCHES BELOW STRINGER 14L. ROUTED OUT CRACK AND REFINISHED AREA PER SRM 53-00-1 PAGE 102. ( M) 2 L 7 2 4F A16WE 1998101600689 19981016 00689 NM 1998 10 16 USAA980343 1 19980808 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 951 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 275AU 41811 22887 TPA - DURING A CX-3 CHECK EDDY CURRENT, FOUND A .300 INCH CRACK AFT SERV DOOR LOWER HINGE CUTOUT OUTER SKIN STATION 951, STRINGER 14R. INSTALLED FILLER .050 2024 T-3, ALSO DOUBLER .063 2024 T-3 AND TRIPLER .063 301.5 HARD S/S PER SRM 53-30 -3 PAGE 121. (M) 2 L 7 2 4F A16WE 1998101600690 19981016 00690 1998 10 16 AALA981478 4 19980806 A 2565 D29982125 SLIDE DOUG DC9 DC982 3022082 WP CABIN DEFECTIVE A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 471AA A3745 49601 ORD - DURING OVERNIGHT CHECK, ENTRY DOOR SLIDE HAD LOW PRESSURE. REPLACED ENTRY DOOR SLIDE. SYSTEM GROUND CHECKED NORM AL OPERATION. (M) 2 L 7 2 4F A6WE 1998101600691 19981016 00691 NM 1998 10 16 USAASB98207 1 19980811 A 2120 AIR DISTR BOEING 737 737301 1384611 NM COCKPIT ODOR A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 EA 19 575US 23740 CLT - FLT 1267 - ON TAKEOFF FROM LGA, CREW NOTICED A STRONG SMELL OF RUBBER BURNING IN THE COCKPIT AND THE CABIN. THERE WERE NO SIGNS OF SMOKE SMELL AND THE APU WAS OFF AT THE TIME. SMELL DISSIPATED ON CLIMB-OUT. FLIGHT CONTINUED ONTO CL T AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RAN BOTH PACKS ON THE GROUND AND CHECKED AIRCRAFT FOR POSSIBLE RUBBE R SMELL. COULD NOT DUPLICATE SMELL. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1998101600692 19981016 00692 EU 1998 10 16 USAAF98075 1 19980913 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 853US 11281 CLT - FLT 501 - ON APPROACH TO CLT, AT 2000 FT WHEN LANDING GEAR WAS SELECTED DOWN, THE RIGHT GEAR GREEN LAMP DID NOT IL LUMINATE. CREW PERFORMED A GO ARUOND PROCEDURE AND RECYCLED THE LANDING GEAR. IT WAS NOT REPORTED IF THE RECYCLE CORRE CTED THE SITUATION, BUT THE FLIGHT LANDED CLT WITHOUT FURTHER INCIDENT. MAINTENANCE RELAMPED THE 'RIGHT' GEAR INDICATIO N MODULE. OPERATION CHECK WAS NORMAL. (M) 2 L 7 2 4F RT 1998101600693 19981016 00693 NE 1998 10 16 UF6A980804 1 19980808 A 2700 CONTROLS BAG ATP ATP EU PWA PW120 PW126A NE COCKPIT VIBRATION A UF6A A UNSCHED LANDING E VIBRATION/BUFFET TO TAKEOFF 1 GL 31 857AW 2034 124223 ORD - FLT 5727 - HIGH PITCH HUM HEARD IN COCKPIT AFTER TAKEOFF WITH VIBRATION FELT IN FLIGHT CONTROLS, POWER LEVERS, TIL LER, AND FLOOR. MAINTENANCE PERFORMED OPS CHECK OF ENTIRE SYSTEM WITH NO DEFECTS NOTED. TEST FLIGHT WAS PERFORMED AND FOUND SATISFACTORY. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998101600694 19981016 00694 WP 1998 10 16 GAIA9882 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 342 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 342 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600695 19981016 00695 WP 1998 10 16 98ZZZM738 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 395 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 395 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600696 19981016 00696 WP 1998 10 16 98ZZZM739 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 408 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 408 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600697 19981016 00697 WP 1998 10 16 98ZZZM740 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 514 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 514 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600698 19981016 00698 WP 1998 10 16 98ZZZM741 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 609 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 609 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600699 19981016 00699 WP 1998 10 16 98ZZZM742 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 699 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 699 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600700 19981016 00700 WP 1998 10 16 98ZZZM743 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 737 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 737 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600701 19981016 00701 WP 1998 10 16 98ZZZM744 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 758 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 758 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600702 19981016 00702 WP 1998 10 16 98ZZZM745 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 427 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 427 LBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600703 19981016 00703 WP 1998 10 16 98ZZZM746 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 237 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 237 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600704 19981016 00704 WP 1998 10 16 98ZZZM747 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 256 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 256 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600705 19981016 00705 WP 1998 10 16 98ZZZM748 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 503 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 503 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600706 19981016 00706 WP 1998 10 16 98ZZZM749 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 514 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 514 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600707 19981016 00707 WP 1998 10 16 98ZZZM750 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 604 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 604 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600708 19981016 00708 WP 1998 10 16 98ZZZM751 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 680 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 680 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600709 19981016 00709 WP 1998 10 16 98ZZZM752 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 699 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 699 LBL 22 . ( M) 2 L 7 2 4F A6WE 1998101600710 19981016 00710 WP 1998 10 16 98ZZZM753 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 525 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 525 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600711 19981016 00711 WP 1998 10 16 98ZZZM754 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 544 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 544 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600712 19981016 00712 WP 1998 10 16 98ZZZM755 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 566 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 566 LBL 22. ( M) 2 L 7 2 4F A6WE 1998101600713 19981016 00713 WP 1998 10 16 98ZZZM756 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 237 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 237 RBL 22. ( M) 2 L 7 2 4F A6WE 1998101600714 19981016 00714 WP 1998 10 16 98ZZZM757 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 256 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 256 RBL 22. ( M) 2 L 7 2 4F A6WE 1998101600715 19981016 00715 WP 1998 10 16 98ZZZM758 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 332 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 332 RBL 22. ( M) 2 L 7 2 4F A6WE 1998101600716 19981016 00716 WP 1998 10 16 98ZZZM759 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 566 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 566 RBL 22. ( M) 2 L 7 2 4F A6WE 1998101600717 19981016 00717 WP 1998 10 16 98ZZZM760 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 604 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 604 RBL 22. ( M) 2 L 7 2 4F A6WE 1998101600718 19981016 00718 WP 1998 10 16 98ZZZM761 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 680 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 680 RBL 22. ( M) 2 L 7 2 4F A6WE 1998101600719 19981016 00719 WP 1998 10 16 98ZZZM762 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 699 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 699 RBL 22. ( M) 2 L 7 2 4F A6WE 1998101600720 19981016 00720 WP 1998 10 16 98ZZZM763 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 237 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 237 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600721 19981016 00721 WP 1998 10 16 98ZZZM764 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 256 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 256 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600722 19981016 00722 WP 1998 10 16 98ZZZM765 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 503 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 503 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600723 19981016 00723 WP 1998 10 16 98ZZZM766 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 525 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 525 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600724 19981016 00724 WP 1998 10 16 98ZZZM767 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 661 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 661 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600725 19981016 00725 WP 1998 10 16 98ZZZM768 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 680 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 680 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600726 19981016 00726 WP 1998 10 16 98ZZZM769 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 699 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 699 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600727 19981016 00727 WP 1998 10 16 98ZZZM770 1 19980826 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP BS 718 MISREPAIRED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS AND WORN AREAS ON THE FLOOR SEAT TRACKS AT STATION BS 718 RBL 44.5. (M) 2 L 7 2 4F A6WE 1998101600728 19981016 00728 NM 1998 10 16 TAOA099803 1 19980904 A 2910 65178218 MODULAR UNIT BOEING 727 727254 138408L NM FUSELAGE LEAKING A TAOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 15 913TS 1416A 20250 LGA-DCA - FLT 6451 - 'A' HYDRAULIC SYSTEM FAILURE IN FIGHT AFTER FLAP RETRACTION. FOUND 'A' SYSTEM MODULAR UNIT LEAKING DUE TO CRACKED FITTING REPLACED MODULE. REPLACED 1 AND 2 HYDRAULIC PUMPS, CASE DRAIN RETURN AND PRESSURE FILTERS. SER VICED HYDRAULIC SYSTEM 'A' ALL SYSTEMS CHECKED NORMAL IAW MM CHAPTERS 29-11-0 THROUGH 29-11-102. (M) 2 L 7 3 4F A3WE 1998101600729 19981016 00729 NM 1998 10 16 USAASB98213 1 19980818 A 2170 V1211 WATER SEPARATOR BOEING 737 7372B7 1384560 NM A/C BAY CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 266AU 22878 CLT - FLT 1806 - EN ROUTE FROM BNA TO PHL, 60 MILES SOUTHWEST OF CRW, F/A TOLD CAPTAIN THAT A STRONG ELECTRICAL SMELL WA S NOTED IN THE CABIN AROUND SEAT ROW 4A. CAPT DECIDED TO DIVERT TO CLT AND DECLARE AN EMERGENCY. CAPTAIN DID NOT DIVER T TO CRW OR ROA DUE TO A THRUST REVERSER ON MEL AND A LONGER RUNWAY NEEDED. FLT LANDED WITHOUT FURTHER INCIDENT. PASSE NGERS DEPLANED AT THE GATE. MX FOUND THE LEFT AIR CONDITIONING PACK TRIPPING ON THE GROUND. OPENED CEILING PANELS, CAR GO BINS AND E/E BAYS. OPERATED ALL CABIN LIGHTS AND EQUIPMENT. COULD NOT DUPLICATE SMELL OR PACK TRIP. REPLACED LEFT PACK WATER SEPARATOR BAG. OPERATED PACKS. AGAIN, NO SMELL OR PACK TRIP NOTED DURING GROUND OPERATIONS. (M) 2 L 7 2 4F A16WE 1998101600730 19981016 00730 WP 1998 10 16 USAAD98154 1 19980831 A 2420 692233B CSD DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 825US 49237 PHL-TPA - FLT 433 - EN ROUTE THE RIGHT ENGINE DRIVEN GENERATOR BECAME INOPERATIVE. THE FLIGHT CREW STARTED THE APU TO U SE THE APU GENERATOR. ABOUT 20 MINUTES LATER THE APU HIGH OIL TEMP LIGHT ILLUMINATED. THE APU WAS SHUTDOWN AND THE FLI GHT DIVERTED TO ORF. MAINTENANCE REPLACED THE RIGHT ENGINE CSD AND GENERATOR. THE APU WAS RUN FOR AN EXTENDED TIME BUT THEY WERE UNABLE TO DUPLICATE THE HIGH OIL TEMP LIGHT. (M) 2 L 7 2 4F A6WE 1998101600731 19981016 00731 WP 1998 10 16 98ZZZM771 1 19980831 A 2420 976J2526 GENERATOR DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 825US 49237 PHL-TPA - FLT 433 - EN ROUTE THE RIGHT ENGINE DRIVEN GENERATOR BECAME INOPERATIVE. THE FLIGHT CREW STARTED THE APU TO U SE THE APU GENERATOR. ABOUT 20 MINUTES LATER THE APU HIGH OIL TEMP LIGHT ILLUMINATED. THE APU WAS SHUTDOWN AND THE FLI GHT DIVERTED TO ORF. MAINTENANCE REPLACED THE RIGHT ENGINE CSD AND GENERATOR. THE APU WAS RUN FOR AN EXTENDED TIME BUT THEY WERE UNABLE TO DUPLICATE THE HIGH OIL TEMP LIGHT. (M) 2 L 7 2 4F A6WE 1998101600732 19981016 00732 WP 1998 10 16 USAAD98153 1 19980829 A 2150 RT PACK DOUG DC9 DC981 3022081 WP A/C BAY FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 802US 48036 CLT-IND - FLT 1128 - AFTER TAKEOFF, THE LEFT AIR CONDITIONING PACK QUIT OPERATING AND THE AIRCRAFT WOULD NOT PRESSURIZE. THE RIGHT AIR CONDITIONING PACK WAS ON MEL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENA NCE RAN THE LEFT AIR CONDITIONING PACK AND PRESSURIZED THE AIRCRAFT. ALL CHECKED NORMAL. THE RIGHT PACK WAS REPAIRED A ND THE MEL REMOVED. (M) 2 L 7 2 4F A6WE 1998101600733 19981016 00733 1998 10 16 MASA98159 4 19980823 A 3445 TCAS BEECH 1900 1900D 1154162 CE E/E BAY MALFUNCTIONED A MASA G O2 MASK DEPLOYED G MULTIPLE FAILURE AP APPROACH 1 SW 07 161YV UE161 FLT 5998 - MBS-PIT - APPROXIMATELY 15 MILES FROM PIT, THE TCAS DISPLAY SCREEN BLANKED OUT, THEN RESET. THE CREW SMELLED A FAINT ELECTRICAL ODOR. CREW DONNED OXYGEN MASKS AND GOGGLES AS A PRECAUTION AND AN EMERGENCY WAS DECLARED. THE AIRC RAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION WAS DEFERRED PER MEL 34-15. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998101600734 19981016 00734 CE 1998 10 16 S2YA98021 1 19980811 A 2497 WIRE BEECH 1900 1900D 1154162 CE LT WING CHAFED A S2YA K NONE O OTHER IN INSP/MAINT 1 GL 13 85SK UE85 A FLT CREW HAD WRITTEN UP THE LT AC BUS AS FAILING INFLIGHT. MAINTENANCE INSPECTED THE A/C AND FOUND FOUR WIRES CHAFFIN G IN THE LT FORWARD LEADING EDGE WING ROOT WS 29.06. THE WIRES WERE CHAFFING ON A GUIDE PLATE THAT ROUTES THE WIRES THR OUGH PART OF THE LEADING EDGE. IT WAS THOUGHT THAT THE WIRE INSULATION HAD BEEN CUT ON THE EDGE OF THE GUIDE PLATE DURI NG INSTALLATION AT THE FACTORY. THE WIRE NR'S ARE P24A10, P250E8, P150A10, AND P250A8. THESE WIRES ARE USED FOR INVERT ER AND AVIONICS POWER. NEW SECTIONS OF WIRE WERE INSTALLED, AND AFTER SATISFACTORY OPERATIONAL CHECK, THE A/C WAS RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998101600735 19981016 00735 NM 1998 10 16 TWRA9851 1 19980829 A 2830 65B821062 SWITCH BOEING 747 747124 1384874 NM LOAD LIMITER BROKEN A TWRA J A DUMP FUEL UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 15 602FF 700018 19734 AFTER TAKEOFF ROTATION F/O'S CONTROL WHEEL FORCE BECAME VERY HEAVY AND REQUIRED THE CAPTAIN TO TAKE OVER CONTROL F/O'S C ONTROL WHEEL HAS 1.5 INCHES OF LOST MOTION. IN ROLL AND PITCH FORCE IS ABOVE NORMAL BOTH A/P FUNCTIONS NORMAL. COMPLET ED JAMMED AND RESTRICTED FLIGHT CONTROL CHECKLIST 2.131 2 VOL 1. FOUND BROKEN SPRING ON F/O LOAD LIMITER UNIT. REMOVED AND REPLACED LOAD LIMITER ASSY MM REF 27-11-05. RIGGED F/O AS REQUIRED. GROUND OPS NORMAL ALL INDICATION NORMAL MM 27 -11-05. (M) 2 L 7 4 4F A20WE 1998101600736 19981016 00736 NM 1998 10 16 USVA99801 1 19980920 A 2612 894093 FIRE LOOP BOEING 737 737291 138448W NM NR 1 ENGINE FAILED A USVA E A F ENGINE SHUTDOWN UNSCHED LANDING ACTIVATE FIRE EXT. J WARNING INDICATION CL CLIMB 1 SO 11 7375F 20363 DURING CLIMB-OUT OF PIE NR 1 ENGINE FIRE WARNING SYSTEM ACTIVATED. EMERGENCY PROCEDURE FOLLOWED. RETURNED TO PIE AIRCR AFT LANDED WITHOUT INCIDENT. OVERWEIGHT LANDING SINK RATE LOW. FOUND NR 1 ENGINE FIRE DETECTION LOOP SHORTED. REPLACE D FIRE DETECTION LOOP, INSPECTED ENGINE, REPLACED FIRE EXTINGUISHER CONTAINERS AND COMPLIED WITH OVERWEIGHT LANDING INSP ECTION IAW BOEING MM 5-51-291. LOW TO MODERATE SINK RATE, PHASE 1 STEP 2A. (M) 2 L 7 2 4F A16WE 1998101600737 19981016 00737 SO 1998 10 16 98ZZZM772 1 19980330 A 2134 210013618 TRANSDUCER GULSTM G1159 G1159B 3953535 SO E/E BAY MALFUNCTIONED A BUEA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 23 36PN 42 LOST CABIN PRESSURIZATION CONTROL AT 37,000 FT, WENT TO MANUAL AND COULD NOT CONTROL. MADE EMERGENCY DESCENT TO 10,000 FT. REPLACED PRESSURIZATION SYSTEM TRANSDUCER, S/N 94-630, WITH REPAIRED UNIT P/N 2100136-1-10, S/N 12-946. PERFORMED CABIN PRESSURIZATION CONTROL. OPS CHECK. (M) 2 L 7 2 4F RT A12EA 1998101600738 19981016 00738 NM 1998 10 16 USAASB98232 1 19980905 A 2410 735511A CSD BOEING 737 737301 1384611 NM NR 1 FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 591US 32744 23936 MCI - FLT 128 - AIRCRAFT DEPARTED DEN WITH THE APU ON MEL. EN ROUTE TO PHL, THE NR 1 ENGINE GENERATOR FAILED IN FLIGHT. WITH ONLY ONE ELECTRICAL POWER SOURCE REMAINING, FLIGHT DIVERTED TO MCI AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGE NCY WAS DECLARED. MAINTENANCE FOUND METAL ON THE NR 1 CSD CHIP DETECTOR. REMOVED AND REPLACED THE CSD, OIL COOLER AND FILTERS PER MM 24-11-11. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998101600739 19981016 00739 EU 1998 10 16 USAA980390 1 19980905 A 5320 A82737403 FITTING FOKKER F28 F28MK0100 4990807 EU FUSELAGE BENT A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 862US 19993 11300 PIT - DURING UNSCHEDULED MAINTENANCE, FOUND SHEARED BOLTS IN ACTUATOR ATTACK BRACKET AND 2 INCH CRACKED BULKHEAD IN RT W HEEL WELL AT ACTUATOR ATTACH FITTING ON BULKHEAD. FITTING WAS BENT. MAINTENANCE FERRY FLIGHT FROM CLT-PIT. INSTALLED DOUBLER ON BULKHEAD AND STACKED SPLICE DOUBLERS ON SUPPORT ANGLE PER EA NR 50473 AND EA NR 50457. (M) 2 L 7 2 4F RT 1998101600740 19981016 00740 WP 1998 10 16 GAIA9884 1 19980826 A 5320 591016373 ANGLE DOUG DC9 DC915F 3022037 WP BS 817 MISDRILLED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING INSPECTION FOR AD 96-16-04 SEVERA MISMATCHED DRILLED HOLES WERE FOUND ON THE APB ANGLE AT FUSELAGE STATION 817 FR OM L6L TO L17L LT AND FROM L6R TO L17R RT. THE HOLES WERE PLUGGED IAW KITTY HAWK EA D9-53-065. THE AIRCRAFT WAS RETURN ED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998101600741 19981016 00741 WP 1998 10 16 GAIA9883 1 19980826 A 5312 5910130 BULKHEAD TEE DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 53348 47062 DURING INSPECTION FOR AD 96-10-04 A .25O INCH CRACK WAS FOUND ON THE UPSTANDING LEG OF THE ABP TEE ADJACENT TO RT BULKHE AD STIFFENER AT Z-24 AND LONGERON 15R. THE TEE WAS REPLACED IAW DC-9 SERVICE BULLETIN A53-232. THE AIRCRAFT WAS RETURN ED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998101600742 19981016 00742 WP 1998 10 16 USAA980394 1 19980910 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 44601 49119 PIT - DURING C-1 CHECK, FOUND TWO CRACKS 2 INCHES LONG AT STATION 1437, LONGERON 2-3 AND 3-4 RIGHT. INSTALLED DOUBLERS PER SRM 53-04 FIG 27. (M) 2 L 7 2 4F A6WE 1998101600743 19981016 00743 WP 1998 10 16 GAIA9886 1 19980826 A 5330 5911403 SKIN DOUG DC9 DC915F 3022037 WP BS 69 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 47062 DURING INSPECTION FOR AD 96-11-11 CRACKS WERE FOUND ON THE FUSELAGE NOSE SKIN AT STATION 69. THE SKIN WAS REPAIRED IAW DOUGLAS DC-9 SB 53-262. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998101600744 19981016 00744 WP 1998 10 16 GAIA9885 1 19980826 A 5320 39140252 FITTING DOUG DC9 DC915F 3022037 WP FUSELAGE CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 564PC 53348 47062 DURING INSPECTION FOR AD 96-10-11 SB 52-89 CRACKS WERE FOUND ON THE AFT LOWER CARGO DOOR SUPPORT FITTINGS. THE FITTINGS WERE REPLACED IAW THE DC-9 SRM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998101600745 19981016 00745 NM 1998 10 16 GAIA9888 1 19980911 A 5320 ANGLE BOEING 727 727223 1384074 NM CABIN CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6806 19481 THE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A TRANSITION 'B' CHECK. FORWARD LAVATORY 'T' ANGLE IS COR RODED AT FOWARD CENTER. REPLACED 'T' ANGLE IAW B727 SRM 51-10-1 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998101600746 19981016 00746 WP 1998 10 16 GAIA9887 1 19980901 A 3297 WIRE CVAC 240 240D 2422660 WP COCKPIT LOOSE A GAIA O OTHER N FALSE WARNING LD LANDING 1 SW 07 94279 101 KHA - FLT 524 - MEM-IND. ON APPROACH TO IND AFTER SELECTING GEAR DOWN, THE DOWN AND LOCKED LIGHTS FAILED TO ILLUMINATE. THE LANDING GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND THE LANDING GEAR WARNING HORN WAS SOUNDING. AN EMERGENCY WAS DECLARED. THE CREW FOLLOWED EMERGENCY GEAR EXTENTION PROCEDURES AND A FLYBY WAS MADE PAST THE TOWER. AN UNEVENTFUL LA NDING WAS MADE. INVESTIGATION FOUND A LOOSE WIRE ON THE LANDING GEAR LEVER MICROSWITCH IN THE CENTER CONSOLE. THE WIRE WAS RECONNECTED AND THE SYSTEM CHECKED OK PER THE CV MAINTENANCE. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4R RT A793 1998101600747 19981016 00747 EU 1998 10 16 VTZA98249 1 19980805 A 2910 1379305A155 LINE BAG JETSTM JETSTM3201 1500217 EU LT MLG CRACKED A VTZA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 27 494UE 810 FLT 6496 - IAD-MDT - DURING CLIMB, EXPERIENCED A LOSS OF HYD PRESS ON BOTH PUMPS, WHEN GEAR RETRACTED. FLT CREW CONTACT ED DISPATCH AND RETURNED TO IAD, WHERE AN EMERGENCY WAS DECLARED DUE TO NO HYDRAULIC PRESSURE. FLT CREW HAD TO MANUALLY PUMP GEAR DOWN AND MADE AN UNEVENTFUL LANDING AT IAD. AIRCRAFT WAS STOPPED ON TAXI WAY WHERE IT WAS MET BY MX AND RAMP PERSONNEL. LANDING GEAR WAS PINNED, PAX'S DEPLANED. A/C WAS TOWED TO HANGAR FOR REPAIR. THE LT MAIN LANDING GEAR RET RACT JACK PRESSURE LINE HAD CRACKED, CAUSING LOSS OF FLUID. PRESSURE LINE WAS REPLACED, ALL REQUIRED CHECKS WERE ACCOMP LISHED AND THE A/C WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A56EU 1998101600748 19981016 00748 EU 1998 10 16 SIMA982422 1 19980830 A 3310 1021S22511 LIGHT SAAB SF340 340B 7860101 EU COCKPIT INOPERATIVE A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 375AE 565 340B375 DFW - FLT 3706 - WHEN THE FIRST OFFICERS FLOOD LIGHT IS TURNED ON, THERE IS SMOKE COMING FROM THE LIGHT. REMOVED AND RE PLACED RIGHT FLOOD LIGHT ASSY. (M) 2 L 7 2 4T RT A52EU 1998101600749 19981016 00749 EU 1998 10 16 SIMA982413 1 19980829 A 3350 1317 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 297AE 340B297 DFW - FLT 5040 - EMERGENCY LIGHT OVER SEAT 4B DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998101600750 19981016 00750 NM 1998 10 16 98ZZZM773 1 19980708 A 3350 BATTERY PACK BOEING 727 727290 138408W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 774AT 2814 21510 IND - DURING P/F FOUND EMERGENCY FLOOR PATH LIGHTING INOP. REPLACED BATTERY PACK IAW MM 33-50-0, OPS CHECKED NORMAL. ( M) 2 L 7 3 4F A3WE 1998101600751 19981016 00751 NM 1998 10 16 EISA98214 1 19980909 A 2611 302842 SMOKE DETECTOR BOEING 727 72725 1384006 NM CARGO BAY MALFUNCTIONED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 300NE 0032 18974 NR 4 SMOKE DETECTOR WILL NOT TEST, ON PREFLIGHT, GENERATED BY PILOT REPORT. REMOVED AND REPLACED NR 4 SMOKE DETECTOR PO WER SUPPLY. OPS CHECK NORMAL PER MM CHAPTER 26. (M) 2 L 7 3 4F A3WE 1998101600752 19981016 00752 NM 1998 10 16 EISA98217 1 19980911 A 3350 1000679 LIGHT BOEING 727 727231 1384079 NM CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 74318 4986 20051 ON POSTFLIGHT, CABIN DOOR EMERGENCY EXIT LIGHT INOPERATIVE. GENERATED FROM MAINTENANCE REPORT. REPLACED CABIN DOOR EME RGENCY EXIT LIGHT IAW MM CHAPTER 33. (M) 2 L 7 3 4F A3WE 1998101600753 19981016 00753 NM 1998 10 16 AALA981660 1 19980828 A 5330 SKIN BOEING 727 727227 1384078 NM BS 380 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 716AA 20608 TUL - DEEP GOUGE IN SKIN STATION 380 STRINGER 6L AND 5 TO STRINGER 7L AND 5 AREA ALSO DENTED WHERE GOUGE IS AT. BLENDED GOUGE AND FABRICATED DOUBLER REPAIR, NO CUTOUT REQUIRED PER AARD 53-30-3. (M) 2 L 7 3 4F A3WE 1998101600754 19981016 00754 NM 1998 10 16 AALA981650 1 19980814 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - AFT CARGO DOOR LOWER CUTOUT CHORD ANGLE CORRODED AT STATION 950E. REMOVED CORROSION, INSTALLED DOUBLER IAW ESO 11 697, 8/13/98 AND SRM 51-40-4 PAGE 1 AND 2. (M) 2 L 7 3 4F A3WE 1998101600755 19981016 00755 NM 1998 10 16 AALA981649 1 19980904 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON FORWARD SIDE OF 580 FRAME OUTBOARD OF STRINGER 26L. INSTALLED NEW SHEAR TIE. (M) 2 L 7 3 4F A3WE 1998101600756 19981016 00756 NM 1998 10 16 AALA981648 1 19980904 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION 42 INCHES RBL STATION 344, FLOORBEAM LOWER SURFACE. INSTALLED REPAIR AT STATION 344, RBL 12 PER E SO 11697, DATED 8/12/98. (M) 2 L 7 3 4F A3WE 1998101600757 19981016 00757 NM 1998 10 16 AALA981647 1 19980904 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON SHEAR TIE STATION 720L BETWEEN 26R AND 27R. INSTALLED NEW SHEAR TIE. (M) 2 L 7 3 4F A3WE 1998101600758 19981016 00758 NM 1998 10 16 AALA981652 1 19980904 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION IN STRINGER 23R STATION 1148. REMOVED STRINGER 23R FROM 1141-1155 SPLICE IN NEW SECTION AS PER SR M 53-10-3 FIG 1 SHEET 1 PAGE 3. (M) 2 L 7 3 4F A3WE 1998101600759 19981016 00759 NM 1998 10 16 AALA981651 1 19980904 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1010-1015 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON FUSELAGE SKIN UPPER SURFACE OUTBOARD OF STRINGER 28L STATION 1010-1015 AND BELOW STRINGER 28L, STATION 1010-1015. REMOVED DAMAGED SKIN, INSTALLED REPAIR PER SRM 53-30-3 PAGE 148 FIG 3A. (M) 2 L 7 3 4F A3WE 1998101600760 19981016 00760 NM 1998 10 16 AALA981631 1 19980903 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1098 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CRACK COMING FROM FASTENER 12 INCHES FORWARD OF STATION 1110 AT NR 2 ENGINE INTAKE DOG HOUSE STRINGER NR 1. CUT OUT DAMAGE SKIN PER SRM 53-30-3 PAGE 12 AND INSTALLED DOUBLER PER BOEING S/B 727-53AD204. (M) 2 L 7 3 4F A3WE 1998101600761 19981016 00761 NM 1998 10 16 AALA981632 1 19980903 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1010-1015 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON FUSELAGE BELLY SKIN UPPER SURFACE OUTBOARD OF STRINGER 28 LT STATION 1010-1015, EXTENDING BELOW STRINGER 28 LT. REMOVED DAMAGED SKIN, INSTALLED FUSELAGE SKIN EXTERNAL REPAIR PER SRM 53-30-3 PAGE 14 FIG 3A, 8 INCHES BY 10 INCHES 7075 T-6 .080. (M) 2 L 7 3 4F A3WE 1998101600762 19981016 00762 NM 1998 10 16 AALA981633 1 19980903 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION EMITTING FROM UNDER ICE LIGHT HOUSING, FUSELAGE SKIN CUTOUT. FABRICATED DOUBLER, FILLER DRILLED H OLES, COUNTERSANK HOLES, ALODINED, PRIMED, APPLIED SEALANT AND INSTALLED DOUBLER FILLER AND ICE LIGHT PER SRM 53-30-3 FI G 22 PAGE 137. (M) 2 L 7 3 4F A3WE 1998101600763 19981016 00763 NM 1998 10 16 AALA981634 1 19980903 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680-686 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON SKIN UNDER LEVELING COMPOUND STATION 680-686, STRINGER 26L. REMOVED DAMAGED AREA 1 INCH BY 1 I NCH AND INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998101600764 19981016 00764 NM 1998 10 16 AALA981635 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CRACK ON FRAME AT FS 930 AND STRINGER 14R. INSTALLED DOUBLER AT FS 930 AND STRINGER 14R PER SRM 53-10-2 PAG E 28 E, F, AND G. (M) 2 L 7 3 4F A3WE 1998101600765 19981016 00765 NM 1998 10 16 AALA981645 1 19980908 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1010-1020 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION IN STRINGER 28LT STATION 1010-1020, CORROSION OUTBOARD STRINGER 28 LT, STATION 1010-1015. REMOVED DAMAGED STRINGER. INSTALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 4B DETAIL 1, 12 INCHES IN LENGTH. (M) 2 L 7 3 4F A3WE 1998101600766 19981016 00766 NM 1998 10 16 AALA981644 1 19980903 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND STRINGER 15L CRACK JUST FORWARD OF ICE LIGHT HOUSING. REMOVED CRACK AREA OF STRINGER, REPAIRED PER SRM 53-1 0-3 FIG 5. (M) 2 L 7 3 4F A3WE 1998101600767 19981016 00767 NM 1998 10 16 AALA981643 1 19980903 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND STRINGER 15L CRACKED JUST AFT OF ICE LIGHT. REMOVED CRACK AREA OF STRINGER AND REPAIRED PER SRM 53-10-3 FIG 5. (M) 2 L 7 3 4F A3WE 1998101600768 19981016 00768 NM 1998 10 16 AALA981642 1 19980903 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION 18 INCHES RBL AT STATION 344 BELOW BEAM. REPAIRED TOP OF FLOORBEAM LOWER SIDE BY INSTALLING STRAP PER AAR 53-10-7-2 PAGE 1-3. (M) 2 L 7 3 4F A3WE 1998101600769 19981016 00769 NM 1998 10 16 AALA981641 1 19980903 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON FLOORBEAM OF FS 380 AND RBL 47 INCHES. INSTALLED REPAIR STRAP PER SRM 53-10-07-2 FIG 1 ON FORW ARD SIDE OF FLOORBEAM. (M) 2 L 7 3 4F A3WE 1998101600770 19981016 00770 NM 1998 10 16 AALA981640 1 19980903 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON TOP CHORD OF FLOORBEAM FS 344 RBL 20 TO LBL 40. REPAIRED DAMAGED AREA OF TOP CHORD FLOORBEAM W ITH SPLICE AND REPAIR ANGLES PER SRM 53-10-8 PAGE 49-53. (M) 2 L 7 3 4F A3WE 1998101600771 19981016 00771 NM 1998 10 16 AALA981638 1 19980903 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CRACK ON RIGHT SIDE OF VERTICLE STIFFENER STATION 1183, RBL 38 WL 239 (INBOARD SIDE OF STIFFENER). INSTALLE D REPAIR DOUBLER PER BOEING S/B 727-53-0192 AND DRAWING 65C34406. (M) 2 L 7 3 4F A3WE 1998101600772 19981016 00772 NM 1998 10 16 AALA981637 1 19980903 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 1183 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CRACK IN VERTICLE STIFFENER FS 1183, RBL 38 WL 239 OUTBOARD SIDE OF STIFFENER. INSTALLED REPAIR DOUBLER PER BOEING S/B 727-53-0192 AND BOEING DRAWING NR 65C34406. (M) 2 L 7 3 4F A3WE 1998101600773 19981016 00773 NM 1998 10 16 AALA981630 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND FUSELAGE FRAME DENTED ABOVE STRINGER 23L, FS 500. INSTALLED BELL FRAME DOUBELR REPAIR PER SRM 51-40-3 PAGE 1 USING 7075T6, .071 THICK 11 INCHES LONG, .375 INCH FASTENER AND 24MS204700 RIVETS, 2 ROWS ON BOTTOM AND ONE ON TOP, 3 RIVETS EACH END. (M) 2 L 7 3 4F A3WE 1998101600774 19981016 00774 NM 1998 10 16 AALA981629 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 804 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CRACK STATION 804.95 STRINGER 14R. REMOVED AND REPLACED CRACKED BELL FRAME REINFORCEMENT ANGLE STATION 804. 95, STRINGER 14R PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1998101600775 19981016 00775 NM 1998 10 16 AALA981628 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND BELL FRAME HEAVY DAMAGE, OVERSIZE FIG 8 HOLE, RIVET TO SMALL, TAILS BENT HOLE GROUND THROUGH BELL FRAME. CU T OUT DAMAGED SECTION ANGLE, INSTALLED ANGLE REPAIR SRM 51-40-3. INSTALLED DOUBLER SRM 51-40-2 AND REPLACED BAD FASTENE RS. (M) 2 L 7 3 4F A3WE 1998101600776 19981016 00776 NM 1998 10 16 AALA981627 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1010 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND BELL FRAME DENTED STATION 1010, BETWEEN STRINGER 26 LT AND 25 LT. INSTALLED BELL FRAME DOUBLER AT STATION 1 010, BETWEEN STRINGER 26 LT AND 26 RT PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998101600777 19981016 00777 NM 1998 10 16 AALA981626 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND BELL FRAME DENTED. FABRICATED DOUBLER, DRILLED HOLES, TREATED AND PRIMED PER SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1998101600778 19981016 00778 NM 1998 10 16 AALA981625 1 19980903 A 5320 WEB BOEING 727 727223 1384074 NM CENTER TANK CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND 1.5 INCH CRACK IN WEB BETWEEN 2ND AND 3RD BAY CENTER TANK LBL 13.19 3 INCHES DOWN FROM TOP OF TANK. INSTALL ED DOUBLER PER SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998101600779 19981016 00779 NM 1998 10 16 AALA981624 1 19980903 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND CORROSION ON SHEAR TIE STATION 950B BETWEEN STRINGER 28RT AND 29 RT. REMOVED DAMAGED SHEAR TIE AND REPAIRED PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998101600780 19981016 00780 NM 1998 10 16 AALA981623 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FRAME STATION 700 DENTED ABOVE STRINGER 24R. REMOVED DAMAGE, REPAIRED DOUBLER SRM 51-40-3, FIG 1 SHEET 3 7075-T6, .063 INCH, 10 INCH DOUBLER, .375 AND .25 FASTENERS 20 EACH MS204700 RIVETS 2 ROWS ON SIDE, 1 ROW ON TOP. (M) 2 L 7 3 4F A3WE 1998101600781 19981016 00781 NM 1998 10 16 TWAA9816501 1 19981013 A 3350 S106CD BATTERY PACK BOEING 727 727231 1384079 NM GALLEY DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54351 21983 DURING MAINT CHECK, FOUND FWD GALLEY EMERGENCY LIGHT WAS DIM. REPLACED BATTERY PACK. CHECK-C 10-31-97 JFK. 2 L 7 3 4F A3WE 1998101600782 19981016 00782 WP 1998 10 16 TWAA9816502 1 19981012 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 958 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 958, LBL 50 IN, WAS CRACKED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 3 ROWS OF RIVETS ON 0.040 DOUBLER. 2 L 7 2 4F A6WE 1998101600783 19981016 00783 WP 1998 10 16 TWAA9816503 1 19981012 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 947 PUNCTURED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND MEMBRANE BELOW FLOOR AT STA 947, RBL 50 IN, WAS PUNCTURED. REPAIRED PER SRM 53-01, FIG 2. APPLIED 2 ROWS OF RIVETS ON 0.040 DOUBLER. 2 L 7 2 4F A6WE 1998101600784 19981016 00784 WP 1998 10 16 TWAA9816504 1 19981007 A 5312 BULKHEAD DOUG DC9 DC951 3022051 WP BS 1168 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 411EA 47732 DURING CHECK-C MAINT, FOUND AFT CARGO BIN WITH CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, STA 1168, LBL 1 IN. INSTAL LED NEW T PART NR 5910130-65, AND NEW GUSSET PER SRM 53-13-3, FIG 8 PAGE 19 AND 20. 2 L 7 2 4F RT A6WE 1998101600785 19981016 00785 WP 1998 10 16 VJ9800525 1 19980928 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 218-351 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 FWD CARGO FLOOR PANEL AT FS 218 TO 351 WAS FOUND WITH CORROSION AROUND EDGES. REMOVED PANEL, FABRICATED AND INSTALLED N EW PANEL IAW DC-9 SRM 51-10-3, 53-21-0 AND 53-01 PG 6. 2 L 7 2 4F A6WE 1998101600786 19981016 00786 WP 1998 10 16 VJ9800526 1 19980928 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 218-332. CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 FS 218 TO 332 THE LT FWD FLOOR PANEL AND TIE DOWN TRACK WAS FOUND WITH CORROSION. REMOVED FLOOR PANEL AND TIE DOWN TRAC K IAW DC-9 SRM 53-21-0 FIG 8, 51-10-3 AND RES 981748. 2 L 7 2 4F A6WE 1998101600787 19981016 00787 WP 1998 10 16 VJ9800527 1 19980928 A 5320 29559781200 SUPPORT DOUG DC9 DC932 3022066 WP BS 765-851 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 AFT CARGO COMPARTMENT FLOOR TRACK WAS FOUND WITH CORROSION ON THE INNER AND OUTER SURFACES AT FS 756 TO 851 LT. FABRICA TED AND INSTALLED NEW REPAIR MEMBER IAW SRM 51-10-3 AND 53-21-0 FIG 10. 2 L 7 2 4F A6WE 1998101600788 19981016 00788 WP 1998 10 16 VJ9800528 1 19980928 A 5330 SKIN DOUG DC9 DC932 3022066 WP GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 LEFT HAND AFT GALLEY PAN WAS FOUND WITH CORROSION ON THE I/B EDGE. REMOVED CORRODED SKIN. FABRICATED AND INSTALLED NEW SKIN IAW DC-9 SRM 51-30-2, 51-10-4, 51-10-3 AND RES 981704. 2 L 7 2 4F A6WE 1998101600789 19981016 00789 WP 1998 10 16 VJ9800529 1 19980930 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 FLOOR SUPPORT STRUCTURE AT FS 996 APPROX 31 LT OF THE CENTER LINE WAS FOUND WITH CORROSION AROUND FASTENER HOLE. REMOVE D THE UPPER L FLOORBEAM ANGLE IAW DC-9 SRM 53-01 FIG 1, 51-10-3, 51-30-2, 51-10-1. 2 L 7 2 4F A6WE 1998101600790 19981016 00790 WP 1998 10 16 VJ9800530 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 447 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 CREASED OUT OF LIMITS DENT WAS FOUND AT FS 447 L26 & 27 L 1 1.5 X .068 IAW DC-9 SRM 53-04 FIG 38. FABRICATED AND INSTAL LED REPAIR IAW SRM 53-04 FIG 38, 51-10-3 AND DAC NTSPM PART 8. 2 L 7 2 4F A6WE 1998101600791 19981016 00791 WP 1998 10 16 VJ9800531 1 19981001 A 5320 3924809503 FITTING DOUG DC9 DC932 3022066 WP BS 600 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 FOUND FWD CARGO COMPARTMENT L29L AT FS 600 WAS FOUND WITH CORROSION. FOUND END FITTING AT FS 600 L29R AND L30 CORRODED AROUND THE HARDWARE. REMOVED AND REPLACED THE FITTINGS IAW DC-9 SRM 51-10-3, 51-10-4, 51-30-5, 53-01 FIG 4, FIG-1, AND DWG 5910068. 2 L 7 2 4F A6WE 1998101600792 19981016 00792 WP 1998 10 16 VJ9800532 1 19981005 A 5347 674560674382201 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 DURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FOUND SEAT TRACK AT FS 200 RBL 44 WAS FOUND WITH CORROSION. REMO VED CORRODED SECTION OF SEAT TRACK. FABRICATED AND INSTALLED A NEW SECTION OF SEAT TRACK AND SPLICES IAW DC-9 SRM 51-30 -1, 51-30-2, AND 53-05 FIG 4F. 2 L 7 2 4F A6WE 1998101600793 19981016 00793 WP 1998 10 16 VJ9800533 1 19980928 A 3233 39208025505 ACTUATOR DOUG DC9 DC932 3022066 WP RT MLG CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 RT MLG RETRACT ACTUATOR AND CORRODED AND SUPPORT BUSHING TRUNNION IS WORN AND CORRODED. REMOVED AND REPLACED RT MLG RET RACT ACTUATOR AND BUSHINGS TRUNNION IAW DC9 32-32-2 AND 57-40-2. 2 L 7 2 4F A6WE 1998101600794 19981016 00794 WP 1998 10 16 CALA9801950 1 19981013 A 5320 5936038501 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 809NY 49263 MBB DOOR JAMB BEAM CORRODED. REMOVED AND REPLACED BEAM PER SRM 51-30-02 AND 51-30-05. 2 L 7 2 4F A6WE 1998101600795 19981016 00795 NM 1998 10 16 CALA9801951 1 19981014 A 5343 FITTING BOEING 727 727224 1384076 NM NLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 NLG TRUNNION CORRODED AND PITTED IN BORES LT AND RT. REMOVED CORROSION AND PITTING, FABRICATED AND INSTALLED NEW BUSHIN GS PER SRM 53-40-1. 2 L 7 3 4F A3WE 1998101600796 19981016 00796 NM 1998 10 16 CALA9801952 1 19981014 A 5720 66137224 FITTING BOEING 727 727224 1384076 NM RT WING WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 RIGHT WING FORWARD SIDE OF MLG BEAM WING T/E PANEL TO BEAM ATTACH LINK FITTING HAS ELONGATED BOLT HOLES. REMOVED AND RE PLACED FITTING PER SRM 51-30-1. 2 L 7 3 4F A3WE 1998101600797 19981016 00797 NM 1998 10 16 CALA9801953 1 19981014 A 5280 RIB BOEING 727 727224 1384076 NM RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 RIGHT MLG STRUT DOOR HAS INTERNAL RIB CRACKED .75 NR 2 RIB. STOP DRILLED CRACK, FABRICATED ANGLE DOUBLER, LOCATED, DRIL LED, DEBURRED, TREATED, PRIMED AND INSTALLED PER SRM 51-40-3, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998101600798 19981016 00798 NM 1998 10 16 CALA9801954 1 19981014 A 5280 RIB BOEING 727 727224 1384076 NM RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 RIGHT MLG STRUT DOOR INTERNAL RIB CRACKED 2.5 NR 4 RIB. REMOVED CRACKED SECTION, FABRICATED REPAIR, LOCATED, DRILLED, D EBURRED, ALODINED, PRIMED AND INSTALLED PER SRM 51-40-3, 51-20-2, 51-30-2 AND MM 51-20-12. 2 L 7 3 4F A3WE 1998101600799 19981016 00799 NM 1998 10 16 CALA9801955 1 19981014 A 5280 652814934 BEAM BOEING 727 727224 1384076 NM RT MLG DOOR MISDRILLED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 RIGHT MLG STRUT DOOR HAS 2 MISDRILLED HOLES IN MAIN BEAM. REMOVED FITTING, LOCATED, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED NEW FITTING PER SRM 51-10-2, 51-30-2, 51-30-3 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998101600800 19981016 00800 NM 1998 10 16 CALA9801956 1 19981014 A 5280 RIB BOEING 727 727224 1384076 NM RT MLG DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 RIGHT MLG STRUT DOOR HAS INTERNAL RIB NR 1 CRACKED .5 INCH. STOP DRILLED CRACK, FABRICATED ANGLE DOUBLER, LOCATED, DRIL LED, DEBURRED, TREATED, PRIMED AND INSTALLED PER SRM 51-40-3, 51-20-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998101600801 19981016 00801 WP 1998 10 16 CALA9801957 1 19981014 A 3397 WIRE DOUG DC10 DC1030 3023501 WP CABIN BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14063 47864 ROW 33 AND 34 L AND K EMERGENCY LIGHTS INOP. RESECURED BROKEN WIRE FOR EMERGENCY LIGHTS. 2 L 7 3 4F A22WE 1998101600802 19981016 00802 NM 1998 10 16 98UAL900441 1 19980906 A 2120 VALVE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E/E COMPT FAILED A UALA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 527UA 24995 AIRCRAFT RETURNED DUE TO A LOUD HUM AND VIBRATION IN THE FORWARD PASSENGER CABIN. *S/D* EQUIPMENT COOLING OVERBOARD EX HAUST VALVE FAILED CAUSING VIBRATION DURING CLIMB. SHOP FOUND DAMPER BROKEN. 2 L 7 2 4F 4 F RT A2NM E17NE 1998101600803 19981016 00803 NM 1998 10 16 98UAL900454 1 19980915 A 3150 CAUTION LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT ILLUMINATED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 316UA 23948 MASTER CAUTION LIGHT ILLUMINATED. *S/D* THERE IS NO RECORD NOTED IN THE AIRCRAFT HISTORY FOR THE MASTER CAUTION LIGHT ILLUMINATION. THE RECORD SHOWS THAT AN ABORTED TAKEOFF OCCURRED THEREFORE A HIGH ENERGY STOP CHECK WAS CONDUCTED WITH N O DAMAGE FOUND. IN ADDITION, THE NR 3 AND NR 4 TIRE ASSEMBLIES WERE REPLACED. 2 L 7 2 4F 4 F RT A16WE E2GL 1998101600804 19981016 00804 NM 1998 10 16 98UAL900484 1 19981005 A 2782 10605582 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 6 LE FLAP FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7258U 21405 NUMBER 6 LEADING EDGE FLAP WOULD NOT RETRACT FROM FULL-DOWN POSITION. NO CONTROL PROBLEMS REPORTED. RETURNED TO DEN. * S/D* REPLACED NR 6 LE FLAP ACTUATOR. SYSTEM OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998101600805 19981016 00805 EU 1998 10 16 98UAL900485 1 19980930 A 5210 MECHANISM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 2L OUT OF ADJUST A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 437UA 655 DOOR 2L WILL NOT SECURE PROPERLY. FERRIED AIRCRAFT TO ORD FOR REPAIR. *S/D* TROUBLESHOOTING REVEALED THAT DOOR WAS OU T OF RIG. ACCOMPLISHED RIG OF DOOR UPPER AND LOWER GUIDEARMS. DOOR OPERATION NORMAL. 2 L 7 2 4F 4 F RT A28NM E40NE 1998101600806 19981016 00806 NM 1998 10 16 98UAL900486 1 19980101 A 5753 SKIN AIRBUS A319 A319131 NM IAE V2527 V2527A5 NE TE FLAPS BIRD STRIKE A UALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 29 813UA 0858 AIRCRAFT EXPERIENCED 2 BIRD STRIKES. FLAPS STUCK IN THE NR 1 POSITION. RETURNED TO FIELD 5 KT ABOVE VFE, AMBER ALERT. OVERWEIGHT LANDING, NO FURTHER INCIDENT. *S/D* BIRD STRIKE CAUSED FLAPS REMAIN IN NR 1 POSITION. OVERSPEED OF 5 KTS IS ADDRESSED IN MM 05-51-13 AND TEMP REVISION 5-002. FLAPS WERE CHECKED PER THE MM WITH NO VISIBLE DAMAGE FOUND. NO FU RTHER ACTION IS REQUIRED. 2 L 7 2 4F 4 F RT A28NM E40NE 1998101600807 19981016 00807 EU 1998 10 16 98UAL900487 1 19981010 A 2530 GALLEY AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE AFT CABIN SMOKING A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 411UA 464 AIRCRAFT RETURNED TO GATE AFTER FLIGHT ATTENDANT NOTICED SMOKE FROM AFT GALLEY AREA. 2 L 7 2 4F 4 F RT A28NM E40NE 1998101600808 19981016 00808 NM 1998 10 16 98UAL900489 1 19981003 A 7711 EPR INDICATION BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT ENGINE LOW A UALA O OTHER O OTHER CR CRUISE 1 WP 29 612UA 21873 CREW REPORT, LEFT ENGINE EPR LOW ON TAKEOFF AND CLIMB. 2 L 7 2 4F 4 F RT A1NM E3NE 1998101600809 19981016 00809 NM 1998 10 16 98UAL900490 1 19981004 A 5610 WINDOW PPG 141T400422 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE RT COCKPIT CRACKED A UALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 774UA 94278H5468 26936 EN ROUTE SFO-DEN, CAPTAIN ADVISED DISPATCH OF ELECTRICAL SMELL AND LIGHT SMOKE COMING FROM LOWER LEFT HEATING UNIT ON WI NDOW R3. SUSPECT INNER GLASS PANE CRACKED/SHATTERED DUE FROM ARCING. WINDOW (141T4004-22) RETURNED TO VENDOR FOR EVALU ATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998101600810 19981016 00810 1998 10 16 98UAL900491 4 19981005 A 2565 2506500994001 DISARM LIGHT KORRY MFG CO 250650099400 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE DOOR 1L SLIDE MALFUNCTIONED A UALA K NONE O OTHER NR NOT REPORTED 1 WP 29 585UA 26709 DOOR 1 LEFT EMERGENCY ESCAPE SLIDE LIGHTS REMAIN ILLUMINATED IN THE ARMED AND DISARMED POSITION. *S/D* CYCLED DOOR ARM HANDLE SEVERAL TIMES AND FOUND LIGHT TO OPERATE NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1998101600811 19981016 00811 NM 1998 10 16 98UAL900492 1 19981005 A 3397 WIRE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN BROKEN A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7263U 21410 FORWARD ENTRY DOOR LOWER EMERGENCY EXIT SIGN INOP. REPLACED EEL CABLE, OPS CHECKS OK. 2 L 7 3 4F 4 F A3WE E2EA 1998101600812 19981016 00812 EU 1998 10 16 98UAL900493 1 19981004 A 2120 AIR DISTRIBUTION AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 433UA 589 BURNING SMELL FOLLOWED BY A WHC2 FAULT MESSAGE ON UPPER ECAM. *S/D* ACCOMPLISHED PACK OPERATIONAL TEST. ALL CHECKS GOOD , NO DISCREPANCIES FOUND, NO BURNING SMELL. NO FAULT MESSAGES DISPLAYED AFTER TEST. 2 L 7 2 4F 4 F RT A28NM E40NE 1998101600813 19981016 00813 NM 1998 10 16 98UAL900494 1 19980930 A 5320 65B0761020 SILL BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE BS 338 CRACKED A UALA K NONE O OTHER TO TAKEOFF 1 WP 29 171UA 24322 VERY LOUD WHISTLE OUT OF NR 3 COCKPIT WINDOW, RIGHT REAR WINDOW ON FO SIDE WAS NOTICED ON DEPT AND ARRIVAL WITH CAB DIFF PRESS AT 5.O. *S/D* DUE TO SQUEALING, THE WINDOW WAS REMOVED AND CORROSION DAMAGE WAS FOUND AT THE LOWER AFT CORNER S TA 338. THE DAMAGE WAS CONTAINED IN THE UPPER OUTBOARD FLANGE OF THE LOWER SILL. THE CORROSION REMOVAL RESULTED IN A 3 INCH SECTION OF THE FLANGE BEING TRIMMED OFF REVEALING A 3 INCH LONG CRACK. THE SILL WAS REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 1998101600814 19981016 00814 NE 1998 10 16 SWIA971278 2 19981008 A 7261 OIL SYST EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE REQD SERVICE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 130G 120130 OIL PRESSURE 1 WARNING AT V1 AND INTERMITTENT PRESSURE DROPS DURING CLIMBOUT. RETURNED TO AIRPORT. VISUALLY INSPECTED LEFT ENGINE AND NO OIL LEAKS EVIDENT. INSPECTED FILTER BY PASS AND CHIP DETECTOR LIGHTS, CHECKS NORMAL. SERVICED ENGIN E WITH 2 QUARTS EXXON 2380 TURBINE OIL. PERFORMED GROUND RUN AND ALL PARAMETERS NORMAL. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600815 19981016 00815 SO 1998 10 16 SWIA971279 1 19981008 A 3231 RETRACT MECH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NLG DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 291SW 120318 NOSE GEAR DOOR DID NOT CLOSE AFTER GEAR RETRACTION. RETURNED FOR LANDING. SECURED NOSE DOORS, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600816 19981016 00816 SO 1998 10 16 SWIA971280 1 19981008 A 3610 PRESS REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE LOOSE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 568SW 120343 RIGHT ENGINE DUCT LEAK LIGHT ILLUMINATED AFTER TAKEOFF. RETURNED TO FAT. SECURED COLLECTOR CAN ON RIGHT PRESSURE REGUL ATOR. OPS AND LEAKS GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600817 19981016 00817 SO 1998 10 16 SWIA971281 1 19981008 A 3610 PRESS REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE INOPERATIVE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 568SW 120343 LEFT AND RIGHT ENGINES DUCT LEAK LIGHT ILLUMINATE AFTER TAKEOFF. LEFT ILLUMINATED AND EXTINGUISHED BUT THE RIGHT ENGINE DID NOT. CHECKED, INSPECTED AND REINSTALLED RIGHT PRESSURE REGULATOR. OPS AND LEAKS CHECKS GOOD ON GROUND. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600818 19981016 00818 EA 1998 10 16 SWIA971282 1 19981008 A 3244 5010571 TIRE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT MLG FAILED A SWIA A UNSCHED LANDING O OTHER TO TAKEOFF 1 NM 07 411SW 7067 RIGHT MAIN TIRE BLEW RIGHT AT ROTATION ON TAKEOFF NR 3 MAIN. RETURNED TO SLC. REPLACED NR 3 AND NR 4 MAIN WHEEL ASSEMB LIES. 2 L 7 2 4F 4 F RT A21EA E15NE 1998101600819 19981016 00819 SO 1998 10 16 SWIA971283 1 19981009 A 2131 CONTROLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 AUTO CABIN PRESSURIZATION SYSTEM FAILED. RETURNED TO EKO. REPLACED CABIN PRESS CONTROL, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600820 19981016 00820 NE 1998 10 16 SWIA971284 2 19981009 A 7321 EEC CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE DIRTY A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 227SW 120304 RIGHT EEC CAUSES TORQUE INDICATION TO FLUCTUATE. RETURNED TO SFO. COMPLETED ENGINE RUN OF RIGHT ENGINE UP TO 100 PERCE NT TQ. NO TQ FLUCTUATIONS NOTED. ALL ENGINES INDICATIONS NORMAL WITH EEC IN MANUAL. CLEANED AND OHMED DIRTY CANNON PL UGS. RAN ENGINE IAW MM 72-00-00. OPS CHECKS GOOD WITH NO TORQUE FLUCTUATION. 2 L 7 2 4T 4 T RT A31SO E20NE 1998101600821 19981016 00821 NE 1998 10 16 VNAA9810010 2 19981011 A 7200 ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT BIRD STRIKE A VNAA K NONE C F.O.D. DE DESCENT 1 GL 07 427JS 25165 24485 3039 DURING THE DESCENT, A BIRD WAS INGESTED IN THE RT ENGINE. MAINTENANCE INSPECTED THE RT ENGINE AND PROPELLER FOR DAMAGE AND FOUND EVIDENCE OF BIRD REMAINS. THE PROPELLER WAS FOUND TO BE SERVICABLE. MAINTENANCE PERFORMED A POWER RUN ON THE ENGINE AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO DAY. MAINTENANCE IN DAY PERFORMED AN INSPECTION AND REPLACEMENT OF THE IGNITORS, AN INSPECTION OF THE LOW PRESSURE TURBINE BLADES, AND P2.5 SWITCHING VALVE, IN ACCORDANCE WITH DORNIER MM 74-21-02. 75-31-05, AND 72-30-03. THE RIGHT HAND FUEL NOZZELS WERE ALSO INSPECTED AND REPLACED IN ACCORDANCE WITH DO RNIER MM 73-11-11. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998101700001 19981017 00001 WP 1998 10 17 VJ9800446 1 19980930 A 3350 41B004AD073 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 917VV 47323 EMERGENCY LIGHT AT MAIN CABIN PASSENGER DOOR INOP. REPLACED BATTERIES, OPS CHECKED NORMAL. 2 L 7 2 4F A6WE 1998101700002 19981017 00002 NM 1998 10 17 TWAA9816003 1 19981001 A 3397 WIRE BOEING 767 7673Y0 NM CABIN BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 FOUND EGRESS LIGHTS INOP ON RT SIDE OF FIRST CLASS. REPAIRED BROKEN WIRES AT RT SIDE OF FIRST CLASS. CHECK-C 8-26-98 L AX. 2 L 7 2 4F RT A1NM 1998101700003 19981017 00003 NM 1998 10 17 TWAA9816004 1 19981001 A 3350 20121 BATTERY CHARGER BOEING 767 7673Y0 NM CABIN INOPERATIVE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 FOUND EMERGENCY LIGHTS INOP AT FWD RT CABIN DOOR AND AFT RT DOOR. REPLACED FWD BATTERY CHARGER. CHECK-C 8-26-98 LAX. 2 L 7 2 4F RT A1NM 1998101700004 19981017 00004 WP 1998 10 17 TWAA9816101 1 19981004 A 2520 5642845515 HOUSING DOUG DC9 DC981 3022081 WP LT COCKPIT WORN A TWAA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CE 05 921TW 49101 RETURNED FROM TAXI BECAUSE LEFT RUDDER PEDAL JAMMED. FOUND RUDDER PEDAL CAUGHT ON CAPTAIN'S RUDDER PEDAL ENCLOSURE. RE PLACED RUDDER PEDAL FIBERGLASS HOUSING ON CAPTAIN'S SIDE. CHECK-C 4-19-98 STL. 2 L 7 2 4F A6WE 1998101700005 19981017 00005 WP 1998 10 17 ARWA981007 1 19980909 A 5320 STRAP LKHEED 1011 10113851 5265010 WP BS 839/859/879 LOOSE A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 INVESTIGATE BULGE AT FS 846 TO 865 STR 30 ZONE 130. AREA ABOUT BULGE DE-RIVITED, SECTION OF FAIL-SAFE STRAP REMOVED. R EMOVED CORROSION STR 30 CUT AT FS 839, FS 859 AND FS 879. FRAME CUT AT FS 869 BETWEEN STR 29 AND 31, REPAIR LAID OUT, A LL NEW HOLES DRILLED, STRINGER SPLICE, DOUBLERS REMOVED. COUNTERSINK PRIMED AND PAINTED. REPAIR ACCOMPLISHED PER BWIA DRG BW-L15-53 A/4501. REF CON 110198 8110-3 ISSUED LISTED ON 337 REF W/O JWM 24000 CCF 5007 LOG PAGE 10466. 2 L 7 3 4F RT A23WE 1998101700006 19981017 00006 WP 1998 10 17 ARWA981008 1 19980909 A 5330 SKIN LKHEED 1011 10113851 5265010 WP MLG T BOX CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 EVIDENCE OF CORROSION BLEND OUT ON LWR SKIN OF MLG T/BOX PLEASE ASSESS DAMAGE A7 = IWI 360. REPAIR CARRIED OUT AND ADHE SIVE CURING AREA SAND AND IS OK FOR INSPECTION. REPAIR CARRIED OUT IAW SRM 51-25-00 AND BWIA APPROVED DRAWING NR BW-45 -57A/4502 CON 104/98 W/O JWN 24000 CCF 4099 LOG PAGE 10467. 2 L 7 3 4F RT A23WE 1998101700007 19981017 00007 WP 1998 10 17 ARWA981009 1 19980909 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 569-589 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 TWO FASTENERS PULLED IN AREA OF BULGE AND FUSE SKIN. BULGE AND FUSE SKIN CRACKED AT FS 569 TO 589 BETWEEN STR 34 AND 35 . BOOT STRAP REMOVED AND FAIL-SAFE STRAP LIFTED FOR ASSESSMENT. DRILLED DOUBLERS, REAM CUT TO SIZE, PRIMED AND PAINTED . REPAIR ACCOMPLISHED AS PER APPROVED BWIA DRAWING BW-L15-53-A/4500 REF CON 109/98 8110-3 ISSUED LISTED ON FAA 337 REF W/O JWM 24000 CCF 5012 LOG PAGE 10466. 2 L 7 3 4F RT A23WE 1998101700008 19981017 00008 WP 1998 10 17 ARWA981010 1 19980909 A 5330 SKIN LKHEED 1011 10113851 5265010 WP FUSELAGE CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 EVIDENCE OF CORROSION PRESENT FUSE SKIN FS ZONE 130 932-952 STR 26 TO 29. RIVETS REMOVED TO FACILITATE CORROSION CLEAN UP, .020 BONDED STRAP. CUT OUT ON INNER SURFACE OF SKIN TO ACCESS CORROSION, STRINGER SECTION CUT OUT TO ACCESS CORROSI ON FRAME BETWEEN STR 30 AND STR 28. REMOVED TO ACCESS CORROSION, DOUBLERS DRILLED AND REMOVED TO FINALIZE AND SENT TO P RIME AND PAINT. INSTALLED REPAIR DOUBLERS. CORROSION REPAIR DONE IAW BW DRG NR BW -L15-53-A/4503 FOR AREA BETWEEN STR 27 AND STR 28 8110-3 ISSUE 8/26/98 LISTED ON 337 REF CON 112198 W/O JWM 24000 CCF 5071 LOG PAGE 10466. 2 L 7 3 4F RT A23WE 1998101700009 19981017 00009 WP 1998 10 17 ARWA981011 1 19980909 A 5532 SKIN LKHEED 1011 10113851 5265010 WP VERT STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 CORROSION ON VERTICAL STAB AROUND AFT STATIC DISCHARGE BASE. REPAIR DONE IAW SRM 55-35-00. USING MAT (P/N 2024T3 050) (B/N 98/005851/5851) RIVETS NAS 1738E4-2 (B/N 95/040160/0160) CONS 118/98. DRAWING BW-L-15-55-A/4509. W/O JWM 24000 CC F 3139 MIN REPAIR. 2 L 7 3 4F RT A23WE 1998101700010 19981017 00010 WP 1998 10 17 ARWA981012 1 19980909 A 5320 STRAP LKHEED 1011 10113851 5265010 WP BS 1555 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 SEVERAL PULLED RIVETS ON FAIL-SAFE STRAP AT APPROX FS 1555 BETWEEN STR 41 AND 42. FAIL-SAFE STRAP REMOVED AS PER SRM 51 -40-01. CORROSION REMOVED AREA TREATED AND PAINTED PER SRM 51-21-01/02 AND REPAIR CARRIED OUT AS PER BWIA DRW NR BW-L15 -53-A/4507 W/O JWM 24000 CCF 6118 CONT NR 115/98 L/P 10467. 2 L 7 3 4F RT A23WE 1998101700011 19981017 00011 WP 1998 10 17 ARWA981013 1 19980909 A 5320 STRAP LKHEED 1011 10113851 5265010 WP BS 1595 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 CORROSION OBSERVED AROUND FAIL-SAFE STRAP AT APPROX FS 1595 BETWEEN STR 42 AND STR 44. CORROSION REPAIR CARRIED OUT IAW DRG BW-L15-53A/4506 AND CONCESSION NR 116/98 W/O JWM 24000 CCF 6119 LOG PAGE 10468 LISTED 337 8110-3 ISSUED. 2 L 7 3 4F RT A23WE 1998101700012 19981017 00012 WP 1998 10 17 ARWA981014 1 19980909 A 5330 SKIN LKHEED 1011 10113851 5265010 WP BS 865-883 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 CORROSION ON FUSELAGE SKIN AT FS 865 TO 883 STR 27 AND 28. REPAIR CARRIED OUT AS PER DRG NR BW -L15-53A/4508 REF CONCES SION 117/98 8130-3. ISSUED ON FAA 337 W/O JWM 24000 CCF 5160 L/D 10467. 2 L 7 3 4F RT A23WE 1998101700013 19981017 00013 WP 1998 10 17 ARWA981015 1 19980909 A 5350 FAIRING LKHEED 1011 10113851 5265010 WP LT HORIZ STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 306GB 1138 CORROSION ON AFTER BODY FAIRING ABOVE LT UPPER HORIZ STAB AIRGATE FAIRING. CORROSION REMOVED, BLEND OUT ACCOMPLISHED PE R BWIA BW-L15-53-A/4505, AREA TREATED IAW SRM 51-21-01/02, AREA PRIMED AND PAINTED. CONCESSION 113/98 W/O 24000 CCF 315 6 L/P 10465. 8110-3 ISSUED. LISTED ON FAA 337. 2 L 7 3 4F RT A23WE 1998101700019 19981017 00019 NM 1998 10 17 CALA9801860 1 19980924 A 2520 6176265001 MONITOR BOEING 737 737724 NM CABIN INOPERATIVE A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 24706 1037 28767 THE FLIGHT ATTENDANT OBSERVED SMOKE AT ROW 21 A-C WHILE EN ROUTE TO IAH. THE VIDEO SCREEN AT ROW 21 WAS ERRATIC. THE V IDEO SYSTEM WAS TURNED OFF AND VIDEO CIRCUIT BREAKERS WERE PULLED. THE SMOKE CEASED AND THE AIRCRAFT LANDED AT IAH WITH OUT INCIDENT. MAINTENANCE FOUND THE VIDEO MONITOR AT ROW 21ABC FAILED. THE VIDEO MONITOR WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. A FUNCTIONAL CHECK OF THE SONY PAVES SYSTEM WAS PERFORMED AND NO DISCREPANCIES WERE FOUND. 2 L 7 2 4F RT A16WE 1998101700020 19981017 00020 NE 1998 10 17 DL73K982051 2 19981003 A 7321 37820115 FUEL CONTROL 7436025 BOEING 737 737232 1384475 NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SO 27 301DL 23073 709164 NR 1 ENGINE COMPRESSOR STALLS AT FL370. AC YAWED LT EACH TIME AND N1 AND F/FLOW GAUGES FLUXED. N1 GAUGE WOULD SPIKE 5P C DROP. 5 SPIKES AT 1 SECOND INTERVALS. FLT DIVERSION TO MCO. INSP ENG COMPRESSOR AND EXH WITH BOROSCOPE. NO TROUBLE FOUND. CKED PS3 FILTER AND ALL ASSOC BLEED CONTROL LINES. REPLACED FUEL PUMP AND FUEL CONTROL PER MM. OPN AND LEAK C K OK PER PFHB. SNAP ACCEL/DECELL OK. BLEED SHIFT OK. 2 L 7 2 4F 4 F RT A16WE E2EA 1998101700021 19981017 00021 NM 1998 10 17 DL757982052 1 19981004 A 5414 SKIN BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 NACELLE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 635DL 23762 716401 NR 2 NACELLE STRUT SKINS, IB AND OB WERE FOUND CRACKED BEYOND PREV STOP DRILLS, ON REPETITIVE INSP BOTH WERE REPAIRED ON SRM 54-51-01-2-203 MIF ERA 259383-14. LOCATION IS NAC STA 107.7 REPAIR IS CLASSIFIED MAJOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1998102300062 19981023 00062 CE 1998 10 23 98ZZZX3806 1 19980904 A 3211 08410111 PIVOT PIN CESSNA 402 402B 207590P CE TRUNNION LOOSE A A HBCA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 11 7886Q 402B0214 THE PILOT STATED HE HEARD A FUNNY NOISE WHEN LANDING GEAR WAS RETRACTED. WHEN LANDING GEAR WAS EXTENDED TO LAND, DID NO T GET A SAFE INDICATION ON LT MAIN GEAR. UPON LANDING, ACFT SETTLED ON ITS GEAR, ROLLED SEVERAL FEET AND THE LT GEAR CA ME OFF OF THE ACFT. THE ROLL PIN (NAS561P4-28) THAT RETAINS THE UPPER TRUNNION PIVOT PIN (0841011-1) IN PLACE HAD SHEAR ED ALLOWING THE PIVOT PIN TO MOVE FORWARD WHICH ALLOWED THE GEAR TO COME OFF OF THE ACFT. 1 L 7 2 3O A7CE 1998102300064 19981023 00064 NM 1998 10 23 98ZZZX3808 1 19980916 A 3213 400054002 FITTING PIPER PA60 PA60600 7106001 NM MLG LOOSE A P DKBA K NONE O OTHER IN INSP/MAINT 1 SO 09 699RF 7172 600169074 COLLAR WORK LOOSE OR BREAKS. THIS LETS TIRE ROTATE AND GROUND CONTROL OF AIRCRAFT IS LOST. SUBMITTER STATED THIS PROBL EM IS THE THIRD IN 3 YEARS. ONE SUCH BREAK CAUSED DAMAGE TO AIRCRAFT. WHEN IT WENT OUT OF CONTROL ON LANDING ROLL-OUT. 1 M 7 2 3O RT A17WE 1998102300071 19981023 00071 WP 1998 10 23 TWAA9816601 1 19981014 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP ROW 29 DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 959U 49704 EGRESS LIGHTS IN FLOOR AFT OF ROW 29 CAME ON IN FLIGHT AND REMAINED ON. REPLACED BATTERIES IN POWER SUPPLY. CHECK-C 10 -1-98 STL. 2 L 7 2 4F A6WE 1998102300072 19981023 00072 WP 1998 10 23 TWAA9816602 1 19981014 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP GALLEY FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951TW 53470 DURING MAINT FOUND EGRESS LIGHT BY FIRST CLASS GALLEY WAS INOPERATIVE AND LENS CRACKED. REPLACED BULB (P/N 7732) AND LE NS (P/N 0105607-301). CHECK-C 6-14-98 STL. 2 L 7 2 4F RT A6WE 1998102300073 19981023 00073 WP 1998 10 23 TWAA9816603 1 19981014 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951TW 53470 DURING MAINT CHECK, FOUND EGRESS LIGHT BY ROW 7 INOPERATIVE. REPLACED LAMP. CHECK-C 6-14-98 STL. 2 L 7 2 4F RT A6WE 1998102300074 19981023 00074 WP 1998 10 23 TWAA9816604 1 19981014 A 3350 BULB DOUG DC9 DC983 3022083 WP CABIN CEILING FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951TW 53470 DURING MAINT CHECK, FOUND EMERGENCY LIGHT IN LEFT SIDE OF CEILING INOPERATIVE. REPLACED BULB. CHECK-C 6-14-98 STL. 2 L 7 2 4F RT A6WE 1998102300075 19981023 00075 WP 1998 10 23 TWAA9816605 1 19981014 A 3350 014597101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 951TW 53470 DURING MAINT CHECK, FOUND EMERGENCY LIGHT IN FRONT OF FIRST CLASS LAV WAS DIM. REPLACED BULB, (P/N 7732) AND BATTERY (P /N 014597-101). CHECK-C 6-14-98 STL. 2 L 7 2 4F RT A6WE 1998102300076 19981023 00076 NM 1998 10 23 TWAA9816606 1 19981007 A 5347 C0329524 SEAT TRACK BOEING 727 727231 1384079 NM BS 1010-1134 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54349 21968 DURING CHECK-C, MAINT FOUND NR 3 FLOOR TRACK CORRODED AT STA 1010 TO 1134, LBL 25. INSTALLED NEW TRACK FROM EXISTING CU T AT STA 1010 AFT TO 1134, WITH NEW TRACK MACHINED TO MATCH OLD PER SRM 53-10-5, DETAIL ON TRACK. PAINTED AND INSTALLED PER SRM 51-20-0. 2 L 7 3 4F A3WE 1998102300077 19981023 00077 NM 1998 10 23 TWAA9816607 1 19981009 A 5347 SEAT TRACK BOEING 727 727231 1384079 NM BS 1066-1134 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54349 21968 DURING CHECK-C, MAINT FOUND NR 1 FLOOR TRACK CORRODED AT STA 1066 TO 1134, LBL 5. INSTALLED NEW TRACK USING (P/N C03295 -24). INSTALLED PER SRM 53-10-5 FIG 7 PAGE 18. 2 L 7 3 4F A3WE 1998102300078 19981023 00078 NM 1998 10 23 TWAA9816608 1 19981008 A 5347 SEAT TRACK BOEING 727 727231 1384079 NM BS 1030-1134 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54349 21968 DURING CHECK-C, MAINT FOUND NR 2 FLOOR TRACK CORRODED AT STA 1030 TO 1134, LBL 4. INSTALLED NEW TRACK USING (P/N C03295 -24) AND INSTALLED TRACK PER SRM 53-10-5 FIG 7 PAGE 18. 2 L 7 3 4F A3WE 1998102300079 19981023 00079 NM 1998 10 23 TWAA9816609 1 19981007 A 5315 FLOORBEAM BOEING 727 727231 1384079 NM BS 1070 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 54349 21968 DURING CHECK-C, MAINT FOUND FLOORBEAM CAP CORRODED AT STA 1070, LBL 54. REPLACED FLOORBEAM CAP USING (P/N 10136-3005) A ND TWA DRAWING C03050. 2 L 7 3 4F A3WE 1998102300080 19981023 00080 WP 1998 10 23 CALA9801958 1 19981014 A 5320 59145581 DOUBLER DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 809NY 49263 CORROSION IN AFT BAG BIN AT STA 1309 JUST ABOVE LONGERON 23 LEFT SIDE. REMOVED AND REPLACED DOUBLER PER 51-30-02. 2 L 7 2 4F A6WE 1998102300081 19981023 00081 NM 1998 10 23 CALA9801959 1 19981015 A 3397 BR964411 WIRE BOEING 727 727227 1384078 NM ROW 10ABC BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 73751 21247 EMERGENCY AISLE PATH LIGHTING INOP AT ROW 10 ABC. FOUND BROKEN WIRE AT LIGHT ASSEMBLY. REMOVED AND REPLACED LIGHT ASSE MBLY PER MM 33-50-01. 2 L 7 3 4F A3WE 1998102300082 19981023 00082 WP 1998 10 23 CALA9801960 1 19981014 A 5320 5936663507 SUPPORT DOUG DC9 DC982 3022082 WP BS 604 BROKEN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16807 49261 MBB LT TIEDOWN RAIL CENTER FLOOR SUPPORT FLANGE MOUNTING EAR BROKEN AT STA 604. INSTALLED REPAIR PER EC/RA 5320-01533. 2 L 7 2 4F A6WE 1998102300083 19981023 00083 NM 1998 10 23 CALA9801961 1 19980919 A 3350 BATTERY BOEING 727 727224 1384076 NM GALLEY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 79750 22452 AFT GALLEY OVERHEAD EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY. 2 L 7 3 4F A3WE 1998102300084 19981023 00084 WP 1998 10 23 CALA9801962 1 19980924 A 3350 BATTERY DOUG DC9 DC932 3022066 WP AFT BAGGAGE DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12507 47788 LEFT EXTERIOR EMERGENCY LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS TURNED ON. REMOVED AND REPLACED AFT BATTERY PAC K IN AFT BAG BIN OVERHEAD PER MM 33-53-0. 2 L 7 2 4F A6WE 1998102300085 19981023 00085 WP 1998 10 23 CALA9801963 1 19980925 A 3350 BATTERY DOUG DC9 DC982 3022082 WP TAIL CONE DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93875 49125 TAIL CONE CEILING EMERGENCY LIGHTS FOUND INOP. REPLACED BATTERY PACK PER MM 33-53-00. 2 L 7 2 4F A6WE 1998102300086 19981023 00086 EA 1998 10 23 COMA9860303 1 19981013 A 2750 860D1118 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER N FALSE WARNING LD LANDING 1 SO 01 946CA 7072 FLAPS FAIL MESSAGE PRESENT DURING LANDING. REPLACED RIGHT HAND BPSU AND FECU. 2 L 7 2 4F RT A21EA 1998102300087 19981023 00087 EA 1998 10 23 COMA9860302 1 19981013 A 3241 17300124 HARNESS CNDAIR CL600 CL6002B19 EA RT MLG FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 959CA 7116 OUTBOARD ANTI-SKID MESSAGE APPEARED DURING TAKEOFF. TAKEOFF ABORTED. REPLACED RIGHT MAIN LANDING GEAR HARNESS OUTBOARD SIDE. 2 L 7 2 4F RT A21EA 1998102300088 19981023 00088 EA 1998 10 23 COMA9860301 1 19981013 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA RT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 716CA 7250 FLAP FAIL MESSAGE ON LANDING. REPLACED LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1998102300089 19981023 00089 EA 1998 10 23 COMA9860300 1 19981013 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA K NONE N FALSE WARNING LD LANDING 1 SO 01 946CA 7072 FLAPS FAIL MESSAGE DURING LANDING. PERFORMED VISUAL INSPECTION OF FLAPS. PERFORMED SELF TEST, CYCLED FLAPS. COULD NOT DUPLICATE. 2 L 7 2 4F RT A21EA 1998102300090 19981023 00090 EA 1998 10 23 COMA9860299 1 19981014 A 2613 356024310 OVERHEAT LOOP CNDAIR CL600 CL6002B19 EA RT PYLON MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 916CA 7014 RIGHT 14TH STAGE DUCT MESSAGE DURING FLIGHT. REPLACED THE RIGHT 14TH STAGE DUCT LOOP. 2 L 7 2 4F RT A21EA 1998102300091 19981023 00091 EA 1998 10 23 COMA9860298 1 19981010 A 3250 7300233 HARNESS CNDAIR CL600 CL6002B19 EA NLG STEERING DEFECTIVE A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 927CA 7031 STEERING SYSTEM FAILED DURING TAKEOFF. REPLACED THE STEER-BY-WIRE HARNESS. 2 L 7 2 4F RT A21EA 1998102300092 19981023 00092 EA 1998 10 23 COMA9860297 1 19981009 A 2750 860D10018 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A COMA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 946CA 7799 7072 FLAP FAIL MESSAGE DURING CRUISE FLIGHT. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1998102300093 19981023 00093 NM 1998 10 23 UPS98227907 1 19981015 A 3350 1000679 LIGHT BOEING 727 72725C 138400H NM COCKPIT INOPERATIVE A IPXA K NONE L NO TEST NR NOT REPORTED 1 SO 01 931UP 19858 INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT IN COCKPIT INTERMITTENTLY FLASHES ON AND OFF WITH SWITCH IN ARM POSITION. REM OVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CK NORMAL. 2 L 7 3 4F A3WE 1998102300094 19981023 00094 WP 1998 10 23 UPS98827908 1 19980925 A 5530 ANGLE DOUG DC8 DC873F 302199F WP VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, RT VERT STAB TO EMPENNAGE DRAG ANGLE CRACKED AND CORRODED IN HORIZONTAL LEG LOC APROX 11-14 AFT OF VE RT STAB FRONT SPAR. REPAIRED IAW SRM 53-2-5. 2 L 7 4 4F RT 4A25 1998102300095 19981023 00095 WP 1998 10 23 UPS98827909 1 19980927 A 5230 FRAME DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, THE D-PIT DOOR FRAME IS CRACKED IN 3 PLACES AT THE AFT UPPER CORNER. REPAIRED IAW SRM 52-4-1 AND 52- 2-0. 2 L 7 4 4F RT 4A25 1998102300096 19981023 00096 NE 1998 10 23 QXEA9801447 2 19980907 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 1 MALFUNCTION A QXEA E ENGINE SHUTDOWN J WARNING INDICATION UK UNKNOWN 1 NM 09 821PH 24509 3584 104 PCE120179 NR 1 ENGINE INDICATED OIL PRESSURE WAS BELOW 40 PSI. PERFORMED INFLIGHT SHUTDOWN OF NR 1 ENGINE. AIRCRAFT LANDED WITHO UT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. TEARDOWN RESUL TS OF ENGINE SHOW A FAILURE OF AN LP BLADE DUE TO A FRACTURE JUST ABOVE THE ROOT, WHICH CAUSED THE BALDE TO TRAVEL THROU GH THE GAS PATH. AN OUT OF BALANCE CONDITION RESULTED CAUSING ADDITIONAL ENGINE COMPONENT FAILURES. 2 H 7 2 4T 4 T RT A13NM E20NE 1998102300097 19981023 00097 NM 1998 10 23 98FDEA00595 1 19980928 A 5314 65184072 KEEL BEAM BOEING 727 72722 1384002 NM BS 1030 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 168FE 18865 CORROSION ON LT KEEL BEAM AT BS 1030, WL 138, LBL 12 IN THE AFT CARGO BAY. *S/D* REMOVED AND REPLACED LT KEEL BEAM AT BS 961-1087, WL 138, LBL 8 PER FEDEX. 2 L 7 3 4F A3WE 1998102300098 19981023 00098 WP 1998 10 23 ABXA9800869 1 19980917 A 5320 591000550 ANGLE DOUG DOUG DC9 DC932 3022066 WP RT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT WHEEL WELL SLANT PRESSURE PANEL LOWER ATTACH ANGLE CORRODED. REPLACE D ATTACH ANGLE IAW DC9 SRM. 2 L 7 2 4F A6WE 1998102300099 19981023 00099 WP 1998 10 23 ABXA9800870 1 19980917 A 5320 591000549 ANGLE DOUG DOUG DC9 DC932 3022066 WP LT MLG WW CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT WHEEL WELL SLANT PRESSURE PANEL LOWER ATTACH ANGLE CORRODED. REPLACED ATTACH ANGLE IAW DC9 SRM. 2 L 7 2 4F A6WE 1998102300100 19981023 00100 WP 1998 10 23 ABXA9800871 1 19980827 A 5347 52455978T TRACK DOUG DOUG DC9 DC932 3022066 WP BS 370 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLOOR TRACK IN THE FORWARD LOWER CARGO COMPARTMENT CORRODED AT FS 370 . REPLACED FLOOR TRACK AT FS 370 IAW DC9 SRM. 2 L 7 2 4F A6WE 1998102300101 19981023 00101 WP 1998 10 23 ABXA9800872 1 19980828 A 5347 5956039501 TRACK DOUG DC9 DC932 3022066 WP BS 756-855 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT FLOOR TRACK IN THE AFT LOWER CARGO COMPARTMENT CORRODED FROM FS 756 TO FS 855. REPLACED FLOOR TRACK FROM FS 756 TO 855 IAW DC9 SRM. 2 L 7 2 4F A6WE 1998102300102 19981023 00102 WP 1998 10 23 ABXA9800873 1 19980828 A 5347 5956039505 TRACK DOUG DC9 DC932 3022066 WP BS 889 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLOOR TRACK IN THE AFT LOWER CARGO COMPARTMENT CORRODED AT FS 889. R EPLACED FLOOR TRACK AT FS 889 IAW DC9 SRM. 2 L 7 2 4F A6WE 1998102300103 19981023 00103 WP 1998 10 23 ABXA9800874 1 19980903 A 5313 27779224 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 RIGHT CRACKED AT FS 945 ON UPPER AND LOWER FLANGE. REPLACED LONGER ON 17 RIGHT FROM FS 937 TO 996 IAW DC9 SRM. 2 L 7 2 4F A6WE 1998102300104 19981023 00104 WP 1998 10 23 ABXA9800875 1 19980902 A 5313 27779224 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT FS 945 ON THE LOWER FLANGE. REPLACED LONGERON SECT ION 17 LEFT AT FS 945 IAW DC9 SRM DRAWING K05864. 2 L 7 2 4F A6WE 1998102300105 19981023 00105 WP 1998 10 23 ABXA9800877 1 19980917 A 5312 595606543 BULKHEAD DOUG DOUG DC9 DC932 3022066 WP BS 699 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT CANTED BULKHEAD AT FS 699 CORRODED BETWEEN RBL 22 AND RBL 44. FABRIC ATED NEW PANEL IAW DOUGLAS DRAWING NR 5956065 AND ABX REA D924-24804. 2 L 7 2 4F A6WE 1998102300106 19981023 00106 WP 1998 10 23 ABXA9800878 1 19980917 A 5312 595606541 BULKHEAD DOUG DOUG DC9 DC932 3022066 WP BS 699 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT CANTED BULKHEAD AT FS 699 CORRODED BETWEEN LBL 22 AND LBL 54. FABRICA TED NEW PANEL IAW DOUGLAS DRAWING NR 5956065 AND ABX REA D924-24804. 2 L 7 2 4F A6WE 1998102300107 19981023 00107 WP 1998 10 23 ABXA9800879 1 19980909 A 5755 5910055516 SKIN DOUG DOUG DC9 DC932 3022066 WP RT SPOILER DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT OUTBOARD SPOILER UPPER SURFACE DELAMINATED. REPLACED THE RIGHT OUTBO ARD SPOILER PANEL IAW DC9 MM CHAPTER 27-61-01. 2 L 7 2 4F A6WE 1998102300108 19981023 00108 WP 1998 10 23 ABXA9800880 1 19980911 A 5400 SRO954000213 ANGLE DOUG DOUG DC9 DC932 3022066 WP LT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND A CRACK IN THE NR 1 ENGINE PYLON UPPER ATTACH ANGLE AT FS 980. REPAIRED CRACK IAW DC9 SRM CHAPTER 53-04. 2 L 7 2 4F A6WE 1998102300109 19981023 00109 WP 1998 10 23 ABXA9800881 1 19980831 A 5320 3916209501 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND VERTICAL SUPPORT BRACKET UNDER SEAT TRACK AT FS 680 AND LBL 44 CRACKED. REPLAC ED SUPPORT BRACKET IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998102300110 19981023 00110 WP 1998 10 23 ABXA9800882 1 19980902 A 5320 991968917 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND VERTICAL ATTACH FITTING CRACKED AT FS 617 UNDER SEAT TRACK AT LBL 44. REPLACED ATTACH FITTING IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998102300111 19981023 00111 WP 1998 10 23 ABXA9800883 1 19980903 A 5320 3916212501 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 617 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND VERTICAL ATTACH FITTING CRACKED AT FS 617 UNDER SEAT TRACK AT LBL 22. REPLACED ATTACH FITTING IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998102300112 19981023 00112 WP 1998 10 23 ABXA9800884 1 19980902 A 7620 4913804AS58904 CONTROL CABLE DOUG DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE NR 2 ENGINE CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND NR 2 ENGINE FUEL SHUT-OFF CABLE NR 57 HEAVILY CORRODED BETWEEN STATION 658 AND 699. REPLACED NR 2 ENGINE FUEL SHUT-OFF CABLE IAW DC9 MM CHAPTER 76-12-00. 2 L 7 2 4F 4 F A6WE E2EA 1998102300113 19981023 00113 WP 1998 10 23 ABXA9800885 1 19980831 A 5320 591034716 ANGLE DOUG DOUG DC9 DC932 3022066 WP BS 917 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND INTERCOSTAL LOWER SUPPORT ANGLE CORRODED AT FS 917 AND RBL 22. REPLACED ANGLE IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998102300114 19981023 00114 WP 1998 10 23 ABXA9800886 1 19980901 A 5753 99576003 RIB DOUG DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND RIB CRACKED INSIDE LEFT FLAP AT OUTBOARD FLAP HINGE. REPLACED RIB INSIDE LT FL AP IAW DC9 SRM CHAPTERS 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998102300115 19981023 00115 WP 1998 10 23 ABXA9800887 1 19980831 A 5753 995760020N ANGLE DOUG DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLAP OUTBOARD HINGE FITTING, INBOARD ATTACH ANGLE CRACKED. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998102300116 19981023 00116 WP 1998 10 23 ABAX9800888 1 19980831 A 5753 995760016N ANGLE DOUG DOUG DC9 DC932 3022066 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLAP OUTBOARD HINGE FITTING, OUTBOARD ATTACH ANGLE CRACKED. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998102300117 19981023 00117 WP 1998 10 23 ABXA9800891 1 19981012 A 5320 49176501N END CAP DOUG DOUG DC9 DC931 3022065 WP BS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND LONGERON 22R END CAP CORRODED AT STATION 996. REPLACED END CAP IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998102300118 19981023 00118 WP 1998 10 23 ABXA9800892 1 19981012 A 5312 99155613 BULKHEAD DOUG DOUG DC9 DC931 3022065 WP BS 996 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND FALSE BULKHEAD, STATION 996 EXFOLIATED JUST ABOVE LONGERON 30. REPAIRED BULKHEAD IAW ABX REA D953 -25069. 2 L 7 2 4F A6WE 1998102300119 19981023 00119 WP 1998 10 23 ABXA9800893 1 19981012 A 5313 59114277 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND LONGERON 16L AT STATION 965 CRACKED. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998102300120 19981023 00120 WP 1998 10 23 ABXA9800894 1 19981012 A 5315 991224359 FLOORBEAM DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND FLOORBEAM AT STATION 996 CRACKED JUST BELOW LONGERON 18R. REPAIRED FLOORBEAM IAW DC9 SRM 51-30-5, 51-30-1 AND ABX SSRM DRAWING K05019. 2 L 7 2 4F A6WE 1998102300121 19981023 00121 WP 1998 10 23 ABXA9800895 1 19981012 A 5320 99236693 MEMBRANE DOUG DOUG DC9 DC931 3022065 WP BS 180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND SUBFLOOR MEMBRANE CRACKED AT STATION 180 AND RBL 20. REPAIRED SUBFLOOR IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998102300122 19981023 00122 WP 1998 10 23 ABXA9800896 1 19981012 A 5320 4912385501N BULKHEAD FITTING DOUG DOUG DC9 DC931 3022065 WP BS 69 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND NOSE LANDING GEAR LEFT TUNNEL VERTICAL BULKHEAD FORWARD UPPER INBOARD FITTING AT STATION 69 CRACKE D. REPLACED FITTING IAW DC9 SRM 51-30-2 AND 51-30-1. 2 L 7 2 4F A6WE 1998102300123 19981023 00123 WP 1998 10 23 ABXA9800897 1 19981012 A 5753 995760020N ANGLE DOUG DOUG DC9 DC931 3022065 WP RT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND RIGHT FLAP OUTBOARD HINGE ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-31-1 AND 51-31-2. 2 L 7 2 4F A6WE 1998102300124 19981023 00124 WP 1998 10 23 ABXA9800898 1 19981012 A 5311 99196181N FRAME DOUG DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND LEFT WHEEL WELL MAIN FRAME STATION 718 CRACKED, EXTENDING INTO THE WEB. REPLACED FRAME IAW DC9 SR M 51-30. 2 L 7 2 4F A6WE 1998102300125 19981023 00125 WP 1998 10 23 ABXA9800899 1 19981012 A 5755 3923758504 FITTING DOUG DOUG DC9 DC931 3022065 WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND RIGHT OUTBOARD SPOILER TORSION BAR SUPPORT INBOARD FITTING CRACKED. REPAIRED IAW DC9 SRM 51-30-3 AND 51-30-5. 2 L 7 2 4F A6WE 1998102300126 19981023 00126 WP 1998 10 23 ABXA9800900 1 19981012 A 5755 3923255504N FITTING DOUG DOUG DC9 DC931 3022065 WP RT SPOILER CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND RIGHT INBOARD SPOILER TORSION BAR OUTBOARD SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-3 AND 51-30-5. 2 L 7 2 4F A6WE 1998102300127 19981023 00127 WP 1998 10 23 ABXA9800901 1 19981012 A 5210 3917853503 FRAME DOUG DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C CHECK, FOUND AFT ENTRY DOOR LOWER LEFT FRAME CRACKED IN LOWER POCKET. REPLACED FRAME IAW DC9 SRM 51-30-2, 51-3 0-1, AND 51-30-5. 2 L 7 2 4F A6WE 1998102300128 19981023 00128 WP 1998 10 23 ABXA9800905 1 19980902 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND LONGERON 16 LEFT LOWER FLANGE CRACKED AT FS 965. REPLACED LONGERON 16 LEFT AT FS 965 IAW DC9 SRM DRAWING K05864. 2 L 7 2 4F A6WE 1998102300129 19981023 00129 NM 1998 10 23 SPAA9800007 1 19981007 A 5312 BULKHEAD WEB BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING COMPLIANCE WITH AD 84-20-03, CORROSION WAS FOUND ON THE AFT PRESSURE BULKHEAD WEB, CHORDS, ANGLES AND FITTINGS AT BS 1016. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH AN ALTERNATE METHOD THAT WAS APPROVED BY BOEING ENGINEERING. FAA FORM 8110-3 AND ACCOMPANYING DATA ON FILE. 2 L 7 2 4F A16WE 1998102300130 19981023 00130 WP 1998 10 23 VJ9800411R1 1 19980921 A 3230 59101695514 UPLOCK LATCH DOUG DC9 DC932 3022066 WP LT MLG INOPERATIVE A ZZDA K NONE J WARNING INDICATION CR CRUISE 1 SO 15 918VV 47320 GEAR DOOR OPEN LIGHT ON WITH LANDING GEAR INDICATING DOWN AND LOCKED. REMOVED AND REPLACED THE LT MLG UPLOCK LATCH ASSY IAW D MM 32-31-4. 2 L 7 2 4F A6WE 1998102300131 19981023 00131 WP 1998 10 23 VJ9800534 1 19981015 A 3350 AD4002P603043 BATTERY DOUG DC9 DC932 3022066 WP ROW 18-21 DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 914VV 47486 EMERGENCY LIGHTS INOP ON ROWS 18, 19, 21. NICAD BATTERY PACKS DO NOT OPERATE LIGHTS WHILE IN EMERGENCY POSITION. REMOV ED AND REPLACED BATTERIES TO BATTERY CHARGER AT STA 634 POSITION B5-26 IAW 33-50. REPLACED THE POWER SUPPLY (P/N 60-030 4-31). 2 L 7 2 4F A6WE 1998102300132 19981023 00132 WP 1998 10 23 VJ9800535 1 19981014 A 2150 DUCT DOUG DC9 DC932 3022066 WP LT ACM LOOSE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 939VV 47089 AT FL 350 CABIN PRESSURE STARTED CLIMBING AT 2,000 FT PER MIN AND CABIN REACHED 12,000 FT, NO CONTROL AUTO OR MANUAL. D ESCENDED TO 10,000 FT CABIN CAME DOWN TO 9000 FT. ALL CABIN MASK DEPLOYED. FOUND LT WATER SEPARATOR DUCT OFF AND RT TU RBINE INLET ON ACM CLAMP LOOSE. RESECURED BOTH ITEMS AND SYSTEM OPS CHECKED GOOD PER MM 21-00. STOWED ALL CABIN O2 MAS KS PER MM 35-00. 2 L 7 2 4F A6WE 1998102300133 19981023 00133 NM 1998 10 23 CALA9801964 1 19981016 A 3350 RPS1B POWER SUPPLY RADIANT BOEING 737 7373T0 1384582 NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17309 23360 AFT 4 SEATS AND AFT 3 LOWER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY POWER SUPPLY IN AFT CEILING, STA 9 20 PER MM 33-51-51. 2 L 7 2 4F RT A16WE 1998102300134 19981023 00134 WP 1998 10 23 9810249614 1 19981012 A 2810 DRAIN DOUG DC9 DC932 3022066 WP RT FUEL SYST CONTAMINATED A NWAA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 GL 01 614NW 47128 DURING CRUISE FLIGHT, FUEL BEGAN VENTING FROM RIGHT WING WITH LEFT FUEL QUANTITY GAUGE INOPERATIVE. CREW DECLARED A YEL LOW EMERGENCY AND FLIGHT WAS DIVERTED TO MKE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED DEBRIS FROM INBOAR D FLOAT DRAIN VALVE, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998102300135 19981023 00135 WP 1998 10 23 98FDEA00651 1 19981015 A 5311 BELLFRAME DOUG DC10 DC1010F 3022111 WP BS 1781 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 053FE 47807 NR 304 CENTER CARGO COMP SUMP DRAIN AREA AT BS 1781, LONGERON 50L THROUGH 50R BELLFRAME HAS INTERGRANULAR CORROSION. RE MOVED J CAP AT BS 1781. FAB NEW SECTION OF J CAP PER SRM 53-30-00. INSTALLED J CAP AND REPAIR SPLICES PER SRM 53-30-00 . 2 L 7 3 4F A22WE 1998102300136 19981023 00136 WP 1998 10 23 ABXA9800914 1 19981014 A 2120 QS100M128H CLAMP DOUG DOUG DC8 DC862 3021970 WP RT EXCHANGER LOOSE A ABXA B EMER. DESCENT O OTHER DE DESCENT 1 GL 23 802AX 46134 AT FL 220, A LOUD BANG OCCURRED AND CABIN PRESSURE BEGAN TO INCREASE 500 FT PER MIN. INITIATED EMERGENCY DESCENT INTO B FI. FOUND RIGHT HEAT EXCHANGER DUCT CLAMP NOT SECURED. RESECURED CLAMP, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998102300137 19981023 00137 WP 1998 10 23 ABXA9800915 1 19981015 A 3244 4455X16518 TIRE THOMPSON DOUG DC8 DC861 3021952 WP LT MLG FAILED A ABXA O OTHER J WARNING INDICATION CL CLIMB 1 GL 23 850AX 45894 AFTER TAKEOFF AND DURING LANDING GEAR UPLATCH CHECK, LEFT GEAR INDICATED UNSAFE. RECYCLED GEAR, SAME RESULTS. FOUND LE FT TIRE RETREAD DISBONDED AND INTERFERRING WITH DOOR UPLATCH SYSTEM. REPLACED WHEEL/TIRE ASSY, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998102300138 19981023 00138 NM 1998 10 23 DHL98712008 1 19981013 A 3297 WIRE BOEING 727 72729 1384007 NM NLG BROKEN A DHLA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 01 712DH 19401 NOSE GEAR DOWN AND LOCK LIGHT GREEN WILL NOT ILLUMINATE UPON GEAR EXTENSION. LIGHT TESTED NORMAL. SPLICED TWO OPEN WIR ES IN NOSE WHEEL WELL, ONE ON LOCK SWITCH AND ONE ON POSITION SWITCH. 2 L 7 3 4F A3WE 1998102300139 19981023 00139 NM 1998 10 23 ASAA9840079 1 19980721 A 5210 DOOR BOEING 737 737490 1384715 NM LT DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 SFO - FLT 291 - PRIOR TO FLIGHT, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO CLOSE. LUBRICATED DOOR AND DOOR OPERATED NO RMALLY. (X) 2 L 7 2 4F RT A16WE 1998102300140 19981023 00140 EU 1998 10 23 98ZZZX3815 1 19980919 A 2131 10246429 CONTROLLER BRAERO DH125 HS125700A 4230170 EU CABIN FAILED A KKYA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED O OTHER CL CLIMB 1 NE 03 270KA 4721 NA0307 ON A DEAD HEAD LEG FRM OXC TO RAP WHILE CLIMBING THROUGH 31,000 FEET, THE CABIN ALTITUDE STARTED TO CLIMB AND COULD NOT BE CONTROLLED WITH THE PRESSURIZATION CONTROLLER. A DESCENT WAS INITIATED AND THE FLIGHT DECK HEAT WAS TURNED ON, THE C ABIN ACCENT WAS LIMITED TO 13,000 FEET. THE PASSENGER MASKS DEPLOYED NORMALLY. THE FLIGHT DIVERTED TO BUF AND LANDED W ITHOUT INCIDENT. THE CABIN PRESSURIZATION CONTROLLER WAS CHANGED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4F A3EU 1998102300141 19981023 00141 NM 1998 10 23 USAASB98236 1 19980910 A 2910 HYDRAULIC SYSTEM BOEING 737 737201 1384454 NM 'A' SYSTEM REQ'D SERVICE A USAA O OTHER J WARNING INDICATION DE DESCENT 1 EA 19 262AU 22868 MCO - FLT 2299 - APPROXIMATELY 20 MINUTES OUT FROM MCO, THE 'A' SYSTEM HYDRAULIC PUMP LOW PRESSURE LIGHT AND THE 'A' SYS TEM FLIGHT CONTROL LOW PRESSURE LIGHT ILLUMINATED WITH ZERO QUANTITY ON GAUGE. FLIGHT LANDED WITHOUT INCIDENT AT MCO AN D TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE SERVICED HYDRAULICS, PRESSURIZED AIRCRAFT WITH BOTH ENGINES RUNNI NG AND ACTUATED ALL HYDRAULIC SYSTEMS. NO LEAKS NOTED. (M) 2 L 7 2 4F A16WE 1998102300142 19981023 00142 EU 1998 10 23 98ZZZX3816 1 19980928 A 3260 WARNING HORN BAG BAE146 BAE146200A 1500266 EU COCKPIT MALFUNCTIONED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 608AW E2049 DEN - FLT 439 - ON TAKEOFF, LANDING GEAR HORN SOUNDED ON RETRACTION. AFTER RECEIVING CLE, RT MLG SHOWED UNLOCKED, GEAR EXTENDED NORMALLY, AND DOWN INDICATION WAS NORMAL. INSPECTED, SWUNG GEAR, COULD NOT DUPLICATE. REPLACED PCB GJ21 AND G J23 AS A PRECAUTION. OPS CHECKED GOOD. 2 H 7 4 4F RT A49EU 1998102300143 19981023 00143 NE 1998 10 23 WRLA98091 2 19980922 A 7412 EXCITER BOX DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE FAILED A WRLA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 117WA 48318 DURING TAXI FOR TAKEOFF, FLIGHT CREW WAS UNABLE TO START NR 1 ENGINE ON B-IGNITION. FLIGHT CREW ELECTED TO RETURN TO GA TE FOR MAINTENANCE. AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 1 ENGINE B-IGNITION EXCITER BOX. THIS DID NOT CORRECT MALFUNCTION. DEFERRED MALFUNCTION PER MEL 74-1. AIRCRAFT RETURNED TO SE RIVCE. WILL PROVIDE FOLLOW-UP REPORT WHEN CORRECTIVE ACTION IS ACCOMPLISHED. (X) 2 L 7 3 4F 4 F A22WE E23EA 1998102300144 19981023 00144 NM 1998 10 23 P2EA98175 1 19980929 A 5270 DOOR WARNING BOEING 737 737205 NM CARGO DOOR MALFUNCTIONED A P2EA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 05 412CE 20412 MCI - FLT 301 - AIR RETURN, NO EMERGENCY DECLARED, LANDING UNEVENTFUL. AFT CARGO DOOR LIGHT CAME ON AFTER TAKEOFF, AIRC RAFT WAS NOT PRESSURIZING. RETURNED TO MCI. CHECKED AFT CARGO DOOR PROXIMITY SWITCH AND TARGET. NO DEFECTS FOUND, AFT CARGO DOOR WARNING LIGHTS OPS CHECK NORMAL. CHECKED PRESSURIZATION CONTROL SYSTEM PER MM 21-31-0, OPS CHECK NORMAL. P RESSURIZED AIRCRAFT ON GROUND, AIRCRAFT PRESSURIZES NORMAL. (X) 2 L 7 2 4F A16WE 1998102300145 19981023 00145 NM 1998 10 23 EIAA980242 1 19980901 A 5711 SPAR BOEING 747 747SR46 NM LT WING CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 55842 20784 HKG - DURING C2 CHECK, RT WING L/E FRONT SPAR WEB FITTING AT WS 1483 HAS CORROSION. NRC 5456. REPLACED PER SRM 51-10-0 1. (X) 2 L 7 4 4F A20WE 1998102300146 19981023 00146 NM 1998 10 23 EISA98223 1 19980923 A 5210 DOOR BOEING 727 7272A7 138407K NM CREW ENTRY DOOR LEAKING A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 310NE 20241 UNABLE TO PRESSURIZE DUE TO LEAK IN CREW FORWARD ENTRY DOOR. NO WARNING LIGHTS. AIR TURN BACK TO IND. FOUND L-1 DOOR NOT PROPERLY CLOSED. OPENED AND CLOSED DOOR. PRESSURIZED ON GROUND, OK FOR SERVICE. TT: 69,782:12 HOURS. TC: 46,77 1. (X) 2 L 7 3 4F A3WE 1998102300147 19981023 00147 NM 1998 10 23 EIAA980241 1 19980901 A 5312 BULKHEAD FITTING BOEING 747 747SR46 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 55842 20784 HKG - DURING C2 CHECK DURING ACCOMPLISHMENT OF EO 53-747-513-98, REV A, AT 8 EACH LOCATIONS, CRACKS WERE FOUND AT FASTEN ER HOLES ON THE 1480 BULKHEAD NRC 5971-5972-5973-5974-5994-5995-5996-6154-6184-6171. ALL CRACKED FASTENER HOLES REPAIR ED BY OVERSIZE REAMING AND BUSHING INSTALLATION ON THE 1480 BULKHEAD FITTING PER RS R-53-43-33847 AND 8110-3 AND ECRA 47 7-51-41-1 DATED 8-31-98. (X) 2 L 7 4 4F A20WE 1998102300148 19981023 00148 SW 1998 10 23 98ZZZX3817 1 19980925 A 6240 AG44AF TACH GENERATOR SWRNGN SA227 SA227AC 8780603 SW LT ENGINE FAILED A EQGA O OTHER O OTHER CR CRUISE 1 SW 19 702M 4062 AC702 HOT/HRO - FLT 1215 - AIRRAFT WAS RELEASED FOR TAKEOFF FORM HOT TO HRO. WHILE EN ROUTE TO HRO, THE LT RPM GAUGE SLOWLY D ROPPED TO ZERO WITH NO APPARENT DROP IN ACTUAL ENGINE RPM. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL WHO INSTRUCTED THEM TO RETURN TO HOT IN ORDER FOR MAINTENANCE TO BE PERFORMED. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE TACH GENERATOR HAD FAILED. THE TACH GENERATOR WAS REPLACED WITH A SERVICEABLE UNIT AND OPERATIONAL CHECK GOOD. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. 2 L 7 2 4T RT A8SW 1998102300149 19981023 00149 SW 1998 10 23 98ZZZX3818 1 19980924 A 2150 BELT SWRNGN SA227 SA227AC 8780603 SW COMPRESSOR BROKEN A EQGA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 19 702M AC702 HOT/HRO - FLT 1217 - AIRCRAFT WAS RELEASED FOR TAKEOFF FROM HOT TO HRO. WHILE IN CLIMB TO HRO, THE CREW HEARD A LOUD BA NG FROM THE FRONT OF THE AIRCRAFT. THERE WERE NO INDICATIONS OF ANY PROBLEMS AND ALL SYSTEMS CHECKED GOOD. THE FLIGHT CREW CONTACTED MAINTENANCE CONTROL WHO INSTRUCTED THEM TO RETURN TO HOT IN ORDER FOR MAINTENANCE TO INSPECT THE AIRCRAFT . MAINTENANCE INSPECTED THE ACFT AND FOUND THE SUPPLEMENTAL AC COMPRESSOR BELT HAD BROKEN. THE SUPPLEMENTAL AC WAS MEL 'D. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (X) 2 L 7 2 4T RT A8SW 1998102300150 19981023 00150 EU 1998 10 23 VTZA98248 1 19980729 A 2910 HYDRAULIC SYS BAG JETSTM JETSTM3201 1500217 EU MAIN FLUCTUATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 486UE 905 IAD/SYR - FLT 6379 - DURING CLIMB AT 1740 HOURS ON 7-29-98, MAKE AN UNSCHEDULED LANDING DUE TO BOTH HYDRAULIC PSI FLUCTU ATED PLUS OR MINUS 200 PSI. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SERVICED AND BLED HYDRAULIC SYSTEM, OPS CHECK OK. AIRCRAFT RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1998102300151 19981023 00151 EA 1998 10 23 98ZZZX3819 1 19980921 A 5511 C6TP10017 RIB DHAV DHC6 DHC6300 2802606 EA HORIZONTAL STAB DAMAGED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 710PV 70141 751 HNL - RIGHT STABILZER OUTBOARD RIB AT STA 113.25 HAS NUMEROUS RIVETS PULLED OR MISSING ON UPPER SKIN. RIVET HOLES OVERS IZED AND ELONGATED. REPAIRED BY REPLACING WITH OVERSIZED RIVETS IAW DEHAVILLAND REPAIR DRAWING RD6-55-133. 1 H 7 2 3T RT A9EA 1998102300152 19981023 00152 CE 1998 10 23 98ZZZX3820 1 19980927 A 3260 INDICATOR BEECH 1900 1900C 1154161 CE COCKPIT MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 86UE UC86 MIA/TPA - FLT 9325 - PILOT REPORT: GEAR HANDLE 'RED' INTRANSIT LIGHTS ILLUMINATED IN-FLIGHT. INSPECTED GEAR WARNING SY STEM, PERFORMED GEAR EXTENSION AND RETRACTION OPERATIONAL CHECKS ON JACKS. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A24CE 1998102300153 19981023 00153 CE 1998 10 23 98ZZZX3821 1 19980920 A 3260 INDICATOR BEECH 1900 1900C 1154161 CE COCKPIT MALFUNCTIONED A GUUA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 11ZR UB11 RSW/TPQ - FLT 9136 - LANDING GEAR HANDLE ILLUMINATED IN-FLIGHT. GEAR HORN ALSO SOUNDED. GEAR HANDLE WAS IN UP POSITION , COULD NOT SILENCE HORN. PERFORMED LANDING GEAR RETRACTION, CHECKED ALL WIRES, SWITCHES, AND PC BOARDS. COULD NOT DUP LICATE. 2 L 7 2 4T RT A24CE 1998102300154 19981023 00154 CE 1998 10 23 98ZZZX3822 1 19980922 A 5210 11451403013 CABLE BEECH 1900 1900C 1154161 CE PAX DOOR BROKEN A GUUA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 19 198GA UB5 MIA/MCO - FLT 9380 - FORWARD CABIN DOOR WILL NOT OPEN WHEN HANDLE IS ROTATED. REMOVED AND REPLACED BROKEN DOOR CABLE. 2 L 7 2 4T RT A24CE 1998102300155 19981023 00155 CE 1998 10 23 98ZZZX3823 1 19980911 A 7500 1145500881 DUCT BEECH 1900 1900C 1154161 CE RT NACELLE LEAKING A GUUA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 19 126UE UC126 TPA/FLL - FLT 9175 - WHEN RIGHT BLEED AIR IS PLACED IN ON POSITION, RUBBER BURNING SMELL IS DETECTED THROUGHOUT CABIN. R EMOVED EXCESSIVE AMOUNTS OF SEALANT FROM RIGHT BLEED AIR PLUMBING. TEST FLIGHT ACCOMPLISHED SATISFACTORY. 2 L 7 2 4T RT A24CE 1998102300156 19981023 00156 CE 1998 10 23 98ZZZX3824 1 19980921 A 5270 INDICATOR BEECH 1900 1900C 1154161 CE COCKPIT MALFUNCTIONED A GUUA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 19 138GL UC138 MCO/EYW - FORWARD CABIN DOOR ANNUNCIATOR ILLUMINATED IN-FLIGHT. CAPTAIN PERFORMED EMERGENCY DIVERSION INTO RSW. SUBMITT ER STATED DETERMINED TO BE AN INDICATION PROBLEM, DEFERRED. 2 L 7 2 4T RT A24CE 1998102300157 19981023 00157 NE 1998 10 23 USAAD98171 2 19981002 A 7200 ENGINE DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217 52053 NE LT NACELLE FAILED A USAA A UNSCHED LANDING E Y VIBRATION/BUFFET ENGINE STOPPAGE CR CRUISE 1 EA 19 820US 49119 696428 ATL/PIT - FLT 592 - EN ROUTE, LT ENGINE BEGAN TO VIBRATE SEVERELY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT CONTINUED TO THE DISTINATION AND LANDED WITHOUT INCIDENT. 12 MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE LEFT ENGINE. ( X) 2 L 7 2 4F 4 F A6WE E9NE 1998102300158 19981023 00158 NE 1998 10 23 USAABB98100 2 19980927 A 7261 OIL SYSTEM BOEING 757 7572B7 1384964 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE LEAK A USAA O OTHER B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C CL CLIMB 1 EA 19 616AU 27147 30917 PHL - FLT 430 - FLIGHT ATTENDANTS NOTED HYDRAULIC SMELL IN MID CABIN AFTER TAKEOFF. MAINTENANCE FOUND THE SMELL WAS COM ING FROM THE RIGHT ENGINE BLEED AND THAT OIL WAS LEAKING FROM THE NR 1 BEARING AREA ON THE RIGHT ENGINE. THE ENGINE IS PROGRAMMED TO BE CHANGED. ENGINE TEAR DOWN FOUND THE CAUSE OF THE SMALL TO BE AN OIL LEAK IN THE INTERMEDIATE CASE OF T HE ENGINE. ON INSTALLATION, TOO MUCH ANTI-GALLING COMPOUND WAS USED CAUSING THE LEAK. (M) 2 L 7 2 4F 4 F RT A2NM E12EU 1998102300159 19981023 00159 NM 1998 10 23 P2EA98172 1 19980922 A 2150 20405010 ACM BOEING 737 737222 1384473 NM RT PACK FAILED A P2EA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 208AU 252603 19547 ATL - FLT 406 - RIGHT PACK PUTS SMOKE IN THE CABIN. RIGHT PACK DEFERRED PER MEL 21-1, CI NR M208057 ASSIGNED PER MAINTE NANCE CONTROLLER. PERFORMED SPECIAL PROCEDURES 21-1 AND 21-2. PLACARDS INSTALLED. REPLACED RT AIR CYCLE MACHINE PER M M 21-51-11, M208057 CLEARED. (M) 2 L 7 2 4F A16WE 1998102300160 19981023 00160 NM 1998 10 23 P2EA98171 1 19980921 A 2750 CIRCUIT BREAKER BOEING 737 737222 1384473 NM COCKPIT TRIPPED A P2EA B EMER. DESCENT J WARNING INDICATION NR NOT REPORTED 1 CE 05 209US 19548 DEN - FLT 305 - EMERGENCY DECLARED, FLAPS UP LANDING UNEVENTFUL. FLAP GAUGE INDICATED SPLIT FLAPS LOCKED OUT. UPON INS PECTION, FOUND BOTH TRAILING EDGE CIRCUIT BREAKERS TRIPPED. RESET BREAKERS, SYSTEM OPS NORMAL THROUGH FULL RANGE. REF MM 27-58-0A. (X) 2 L 7 2 4F A16WE 1998102300161 19981023 00161 NE 1998 10 23 PLGA980908A 3 19980908 A 6110 660710924 SLIDER BLOCK SAAB SF340 SF340A 7850100 EU ROTOL R389 R3894123F25 NE PROPELLER DAMAGED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 741BA 340A090 DGR487287 ALB - PROPELLER WAS REMOVED TO EVALUATE EXCESSIVE RADIAL PLAY. UPON INSPECTION, THE FOLLOWING WAS FOUND: SLIDER BLOCK HAD BECOME DETACHED FROM CROSSHEAD CAUSING CROSSHEAD TO ROTATE APPROXIMATELY 45 DEGREES. THE CROSSHEAD WAS DAMAGED BY O PERATING PIN OF PROPELLER BLADES. (X) 2 L 7 2 4T RT A52EU 6 C P30NE 1998102300162 19981023 00162 NM 1998 10 23 USAASB98239 1 19980913 A 3320 UNKNOWN BOEING 737 7373B7 1384580 NM CABIN ODOR A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 389US 23311 LGA - FLT 1157 - EN ROUTE FROM BUF TO LGA, THE FLIGHT ATTENDANT IN THE AFT GALLEY REPORTED A BURNING ODOR, BUT COULD NOT IDENTIFY ORIGIN. ODOR DISSIPATED WHEN LIGHTS TURNED OFF AND CIRCUIT BREAKERS WERE PULLED. FLIGHT CONTINUED AND LANDED AT LGA WITHOUT FURTHER INCIDENT. MAINTENANCE TURNED ON ALL EQUIPMENT IN AFT GALLEY AND RESET CIRCUIT BREAKERS. CHECKE D INSIDE CEILING PANELS AND BEHIND CIRCUIT BREAKER AND SWITCH PANELS. INSPECTED WIRING AND COULD NOT FIND ANY EVIDENCE OF BURNING OR ODOR. AIRCRAFT OK FOR SERVICE. (X) 2 L 7 2 4F RT A16WE 1998102300163 19981023 00163 WP 1998 10 23 AALA981598 1 19980831 A 3230 BYPASS HANDLE DOUG DC9 DC983 3022083 WP COCKPIT NOT CLOSED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 588AA 53251 YUL - FLT T2037 - AFTER TAKEOFF YUL EN ROUTE ORD, LANDING GEAR WOULD NOT RETRACT WITH GEAR HANDLE IN UP POSITION. RETUR NED AND LANDED YUL WITHOUT INCIDENT. STOWED GEAR DOOR BYPASS HANDLE IN FULL CLOSED LOCKED POSITION. SYSTEM GROUND CHEC KED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A6WE 1998102300164 19981023 00164 NE 1998 10 23 UF6A980709 2 19980710 A 7200 ENGINE BAG ATP ATP EU PWA PW120 PW126A NE LT NACELLE MALFUNCTIONED A UF6A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 854AW 2028 124224 SBN - FLT 5751 - ON CLIMB-OUT, LT NR 1 ENGINE TORQUE ROLLED BACK TO 40 PERCENT. NH AND NL WERE UP IN THE 115 PERCENT RA NGE. MAINTENANCE PERFORMED RESISTANCE CHECK OF NP, NH, NL, AND TQ SENSORS. DOWNLOADED EEC, BORESCOPED OP AND HP TURBIN ES. CHECKED REDUCTION GEARBOX AND TURBOMACHINE FILTERS FOR CONTAMINATION. PERFORMED POWER ASSURANCE RUN AND DATA DOWNL OAD OF FDR. ALL PARAMETERS WERE FOUND WITHIN LIMITS. NO DEFECTS NOTED. ENGINE TT: 11,244. (X) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998102300165 19981023 00165 NE 1998 10 23 RAIA981002 2 19981002 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT NACELLE FAILED A RAIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 03 570HK 5813 41089 PHL- FLT 7770 - LEFT ENGINE POWER SURGE DOWN TO 50 PERCENT LOSS. MAINTENANCE REPLACED LT ENGINE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1998102300166 19981023 00166 WP 1998 10 23 ASAA9880182 1 19980919 A 3350 0105606003 LIGHT GULTON DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE FOWARD 6 SETS OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE. REPLACED BROK EN LAMP MODULE AND OPERATED NORMALLY. (X) 2 L 7 2 4F RT A6WE 1998102300167 19981023 00167 EU 1998 10 23 RAIA981003 1 19981003 A 3297 WIRE AEROSP ATR72 ATR72202 8680940 EU ACM BAY FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 722TE 220 SGF - FLT 7012 - LANDING GEAR WOULD NOT COME DOWN. USED EMERGENCY EXTENSION. GEAR CAME DOWN. MAINTENANCE REPAIRED BRO KEN WIRE IN ACM BAY GOING TO LANDING GEAR CONTROL VALVE. (X) 2 H 7 2 4T RT A53EU 1998102300168 19981023 00168 EU 1998 10 23 RAIA980910 1 19980922 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 565HK 450 41082 DCA - FLT 7738 - POD SMOKE LIGHT CAME ON AFTER TAKEOFF. MAINTENANCE REPLACED SMOKE DETECTOR. (X) 2 L 7 2 4T RT A41NM 1998102300169 19981023 00169 EU 1998 10 23 RAIA980912 1 19980924 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 555HK 4908 41072 BHM - FLT 7453 - POD SMOKE LIGHT CAME ON AT 10,000 FEET ON DESCENT, LIGHT WENT OUT AT 5,000 FEET. MAINTENANCE REPLACED SMOKE DETECTOR IN POD BAGGAGE COMPARTMENT. (X) 2 L 7 2 4T RT A41NM 1998102300170 19981023 00170 EU 1998 10 23 USAASB98237 2 19980911 A 7250 BEARING BOEING 737 7373B7 1384580 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 ENGINE FAILED A USAA A UNSCHED LANDING R M E PARTIAL RPM/PWR LOSS OVER TEMP VIBRATION/BUFFET CR CRUISE 1 EA 19 514AU 36108 1072 23700 721341 CLT - FLT 1782 - CAPTAIN REPORTED THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALLS AT FL 370, REPEATED AT FL 350, THEN A SU STAINED SURGING AT FL 310. CREW ELECTED TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DE CLARED. DURING TAXI-IN, THE NR 1 ENGINE SUSTAINED A VIBRATION AND AN UNCONTROLLABLE EGT (733 AND CLIMBING). THE NR 1 E NGINE WAS SHUT DOWN AT THIS TIME. AIRCRAFT PROCEEDED TO TAXI TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EN GINE ASSEMBLY PER JOB CARD. ENGINE RUN, OPERATIONAL CHECK AND LEAK CHECK GOOD. FOLLOW-UP REVEALED NR 4 BEARING FAILED PER OPERATOR P/P ENGINEER. (X) 2 L 7 2 4F 4 F RT A16WE E21EU 1998102300171 19981023 00171 NM 1998 10 23 WRLA98092 1 19981002 A 5751 ARC72137 BALANCE WEIGHT DOUG MD11 MD11 3023602 NM AILERON CORRODED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 271WA 48518 DURING C-CHECK, RIGHT-HAND, OUTBOARD AILERON WAS IDENTIFIED AS HAVING CORROSION ON BALANCE WEIGHTS. MAINTENANCE PERSONN EL REMOVED CORROSION ON NR 3 AND NR 4 WEIGHTS PER SRM 51-82-00. NR 2 WEIGHT BEYOND SRM LIMITS. REPLACED WEIGHT WITH NE W PART. (X) 2 L 7 3 4F RT A22WE 1998102300172 19981023 00172 NM 1998 10 23 WRLA98093 1 19981002 A 5532 AGA7738505 PANEL DOUG MD11 MD11 3023602 NM VERTICAL STAB CHAFED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 271WA 48518 DURING C-CHECK, LOWER VERTICAL STABILIZER FIRE SEAL PANEL WAS FOUND CHAFED AND WORN THOUGH THE OUTER EDGE. MAINTENANCE PERSONNEL REPAIRED VIA WELDING PER DOUGLAS PROCESS SPECIFICATION. (X) 2 L 7 3 4F RT A22WE 1998102300173 19981023 00173 NM 1998 10 23 WRLA98094 1 19981002 A 5320 6012193 STANCHION DOUG MD11 MD11 3023602 NM CARGO BAY CRACKED A WRLA K NONE O OTHER IN INSP/MAINT 1 EA 27 271WA 48518 DURING C-CHECK, FORWARD BAGGAGE COMPARTMENT AFT BULKHEAD CENTER PANEL, LOWER ATTACH ANGLE WAS CRACKED/BROKEN. MAINTENAN CE PERSONNEL REPLACED T-EXTRUSION (STANCHION) PER SRM 53-40-0, PAGE 4, FIG 6. (X) 2 L 7 3 4F RT A22WE 1998102300174 19981023 00174 NM 1998 10 23 USAA980407 1 19980914 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 41361 22892 TPA - DURING CX-2 CHECK VISUAL VERIFIED BY EDDY CURRENT INSPECTION, FOUND A .75 INCH CRACK STA 312 BETWEEN STR 14L AND S TR 13L SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1998102300175 19981023 00175 NM 1998 10 23 USAA980404 1 19980912 A 5330 SKIN BOEING 737 737201 1384454 NM BS 368 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 21817 CLT - DURING RON CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK OUT OF FORWARD EDGE OF EQUIPMENT COOLING DUCT CUT OUT S TA 368 ON SKIN. INSTALLED DOUBLER PER TR 53-30-04 DRAWING 65C33930. (X) 2 L 7 2 4F A16WE 1998102300176 19981023 00176 NM 1998 10 23 USAA980401 1 19980911 A 5320 INTERCOSTAL BOEING 737 737201 1384454 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 42850 22758 CLT - DURING THROUGH-FLIGHT CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK BS 1016 WL 208 LBL 12 AND LBL 24 INTERCOSTAL S. REMOVED DAMAGED SECTIONS AND INSTALLED FABRICATED REPAIR PARTS PER SRM 51-40-2 FIG 1. (X) 2 L 7 2 4F A16WE 1998102300177 19981023 00177 NM 1998 10 23 USAA980399 1 19980911 A 5320 6546568515 WEB BOEING 737 737201 1384454 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 42850 22758 CLT- DURING THROUGH-FLIGHT VISUAL INSPECTION, FOUND A 11.2 INCH CRACK ADJACENT TO STR 7L AND THROUGH Y-CHORD STA 1016 AF T PRESSURE BULKHEAD WEB. REMOVED CRACKED WEB AND INSTALLED NEW REPLACMENT WEB PER EA 62364 AND EA62317. REF: OPER CO NTROL NR 98ZZZX3825. (X) 2 L 7 2 4F A16WE 1998102300178 19981023 00178 NM 1998 10 23 98ZZZX3825 1 19980911 A 5320 6546568541 WEB BOEING 737 737201 1384454 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 42850 22758 CLT- DURING THROUGH-FLIGHT VISUAL INSPECTION, FOUND A 11.2 INCH CRACK ADJACENT TO STR 7L AND THROUGH Y-CHORD STA 1016 AF T PRESSURE BULKHEAD WEB. REMOVED CRACKED WEB AND INSTALLED NEW REPLACMENT WEB PER EA 62364 AND EA62317. REF: OPER CON TROL NR USAA980399. 2 L 7 2 4F A16WE 1998102300179 19981023 00179 NM 1998 10 23 USAA980384 1 19980908 A 5330 SKIN BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 232US 48786 22018 TPA - DURING CX-5 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .50 INCH CRACK IN EXTERNAL SKIN STA 380 BL 3.01. IN STALLED DOUBLER OF .100 INCH 2024 T-3 PER TR 53-30-04 SB 737-53-1117. (X) 2 L 7 2 4F A16WE 1998102300180 19981023 00180 NM 1998 10 23 USAA980408 1 19980914 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 947 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 280AU 41361 22892 TPA - DURING CX-2 CHECK VISUAL AND VERIFIED BY EDDY CURRENT INSPECTION, FOUND A .8750 INCH CRACK STA 947 BETWEEN STR 15R AND STR 16R SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1998102300181 19981023 00181 NM 1998 10 23 USAA980406 1 19980917 A 5330 SKIN BOEING 737 737201 1384454 NM BS 491 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 241US 44966 22443 TPA - DURING CX-4 CHECK VISUAL VERIFIED BY EDDY CURRENT INSPECTION, FOUND A 1.1250 INCH CRACK IN L/E SKIN RT WING AT WS 491. INSTALLED DOUBLER OF 204 T-3 .040 INCH PER SRM 57-30-4 FIG 1. (X) 2 L 7 2 4F A16WE 1998102300182 19981023 00182 NE 1998 10 23 USAASB98251 2 19980924 A 7510 655812310 DUCT BOEING 737 7372B7 1384560 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 266AU 22878 BWI - FLT 2679 - ON CLIMB-OUT PASSING 13,000 FEET, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ACCOMPLISHED CHECK LIST AND WHEN THRUST LEVER WAS PULLED BACK ON NR 1 ENGINE, LIGHT EXTINGUISHED. CREW DECIDED TO RETURN TO FIELD AT BWI. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 1 ENGINE NOSE COWL ANTI-I CE DUCT HAD BLOWN. REPLACED DUCT. RAN ENGINE. OPS CHECK AND LEAK CHECK GOOD. NO FAULTS NOTED. (X) 2 L 7 2 4F 4 F A16WE E2EA 1998102300183 19981023 00183 NM 1998 10 23 USAASB98249 1 19980920 A 3260 189929 SWITCH BOEING 737 7372B7 1384560 NM RT MLG WW FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 271AU 22883 CLT - FLT 273 - AFTER TAKEOFF FROM PHL, CREW RECEIVED A RT MAIN GEAR GREEN LIGHT WHICH WOULD NOT EXTINGUISH AFTER RECYCL ING THE GEAR. CREW DECIDED TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAIN TENANCE REMOVED AND REPLACED THE RT MLG PROXIMITY SENSOR AND ITS ASSOCIATED CONNECTOR D4574P (P/N BACC45FT18A14P) IN THE RT WHEELWELL. CYCLED GEAR SEVERAL TIMES. SYSTEM OPS CHECK AND INDICATION CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998102300184 19981023 00184 NM 1998 10 23 USAASB98243 1 19980916 A 8012 2730426 VALVE BOEING 737 7372B7 1384560 NM NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 287AU 16066 23134 TPA - FLT 2636 - AFTER TAKEOFF AT 2,000 FEET AND CLIMBING, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW PER FORMED CHECK LIST PROCEDURES AND LIGHT REMAINED ON. CREW SHUT DOWN THE NR 1 ENGINE AT 5,000 FEET, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT TPA. LIGHT EXTINGUISHED ON BASE LEG. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. TOTAL SINGLE ENGINE TIME WAS 10 MINUTES. ALL ENGINE INDICATIONS WERE NORMAL ON TAKEOFF AND BEORE ENGINE SHUTDOWN. MAI NTENANCE TROUBLESHOT TO A FAULTY START VALVE. REPLACED NR 1 ENGINE START VALVE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (X) 2 L 7 2 4F A16WE 1998102300185 19981023 00185 NM 1998 10 23 USAA980415 1 19980916 A 5330 SKIN BOEING 737 737201 1384454 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 224US 52320 21666 CLT - DURING RON CHECK VISUAL WITH EDDY CURRENT INSPECTION, VERIFIED A 2 INCH CRACK ON SKIN STA 787 BETWEEN STR 22L AND STR 23L. INSTALLED NEW FILLER AND DOUBLER PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1998102300186 19981023 00186 NM 1998 10 23 USAA980403 1 19980912 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 50655 21817 CLT - DURING RON CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND APPROXIMATELY .75 INCH CRACK FUSELAGE SKIN STA 727A JUST ABOVE STR 16R. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-30-3. (X) 2 L 7 2 4F A16WE 1998102300187 19981023 00187 NM 1998 10 23 USAA980398 1 19980912 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 235US 47060 22275 CLT - DURING CHECK VISUAL INSPECTION, FOUND A 2 INCH SKIN CRACK 1 INCH ABOVE STR 16L 1 INCH TO 3 INCHES FORWARD OF STA 7 27B ON SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6 PAGE 2B, 2C, 2D, AND 2E. (X) 2 L 7 2 4F A16WE 1998102300188 19981023 00188 WP 1998 10 23 USAA980414 1 19980921 A 5313 S1242886 LONGERON DOUG DC9 DC982 3022082 WP BS 1289-1322 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 821US 43019 49138 PIT - DURING C-6 CHECK, FOUND 1 INCH BY 3 INCH AND 1 INCH BY 4 INCH AREAS OF CORROSION AT LONGERON 29L BETWEEN STA 1289 TO STA 1322. SPLICED IN A NEW SECTION LONGERON PER SRM 53-02 FIG 18. (X) 2 L 7 2 4F A6WE 1998102300241 19981023 00241 WP 1998 10 23 TWAA9816701 1 19981014 A 3350 3350 BULB DOUG DC9 DC983 3022083 WP ROW 16 FAILED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9406W 53126 EGRESS LIGHTS WERE REPORTED INOPERATIVE AT CABIN ROWS 1, 3, 10 AND 16. CORRECTIONS WERE DEFERRED PER MEL. ON LAYOVER R ESEATED BULBS AT ROWS 1, 3 AND 10. REPLACED BULB AT ROW 16. CHECK-C 1-15-98 STL. 2 L 7 2 4F RT A6WE 1998102300242 19981023 00242 NM 1998 10 23 TWAA9816702 1 19981016 A 3350 58225 CONNECTOR BOEING 727 727231 1384079 NM SEAT ROW 18 LOOSE A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 54354 21986 EGRESS LIGHTS WERE ILLUMINATED BY THE OVERWING EXITS WITH THE SWITCH IN THE ARMED POSITION. RESEATED CONNECTOR ON THE P OWER SUPPLY ABOVE SEAT ROW 18 ON LEFT SIDE. CHECK-C 5-21-98 MCI. 2 L 7 3 4F A3WE 1998102300243 19981023 00243 WP 1998 10 23 TWAA9816703 1 19981017 A 3350 58541 LIGHT DOUG DC9 DC982 3022082 WP CABIN FWD INOP A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 958U 49703 EGRESS LIGHT STRIPS IN FRONT OF CABIN INOPERATIVE. REPLACED THE TWO FRONT CABIN LIGHT STRIPS. CHECK-C 9-17-98 STL. 2 L 7 2 4F A6WE 1998102300244 19981023 00244 NM 1998 10 23 VJ9800536 1 19980929 A 5312 BULKHEAD ANGLE BOEING 737 737284 138448R NM BS 664 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 ATTACH ANGLE VERTICAL LEG ON SHEAR BEAM AT BS 664, S18R CRACKED BETWEEN THREE FASTENERS AND SHEAR BEAM AT BS 664, S18AL CRACKED IN RADIUS AT BULKHEAD ATTACH POINT. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW B737 SB 53-1066, REPAIR KI T 65C29228-29. REMOVED AND INSTALLED NEW L ANGLE IAW B737 SB 53-1066, REPAIR KIT 65C29228-30 AND SRM 51-10-01. 2 L 7 2 4F A16WE 1998102300245 19981023 00245 NM 1998 10 23 VJ9800537 1 19981006 A 5753 BUSHING BOEING 737 737284 138448R NM LT TE FLAP CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 LT WING O/B FLAP I/B TRACK PITTED WITH CORROSION ON AFT SPAR MOUNT SURFACE AND I/B BOLT HOLE. REMOVED CORROSION, FABRIC ATED AND INSTALLED NEW BUSHINGS AND SHIM IAW B737 SRM 51-10-6, MM 20-10-71 AND AIRTRAN EO 981765. 2 L 7 2 4F A16WE 1998102300246 19981023 00246 WP 1998 10 23 VJ9800538 1 19980919 A 5320 59137002 FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 AFT CABIN FLOORBEAM AT FS 996 RIGHT SIDE FITTING CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-5, 51-10-4, 51-10-3 AND 5 3-01 FIG 1. 2 L 7 2 4F A6WE 1998102300247 19981023 00247 WP 1998 10 23 VJ9800539 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 436 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 A DENT, 2 INCHES BY .016 AT FS 436, L27 AND 28R OUT OF LIMIT IAW DC9 SRM 53-04 FIG 38. CUT OUT DENTED AREA, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 53-01 FIG 4, 51-10-3, 51-30-2 AND RES 191736. 2 L 7 2 4F A6WE 1998102300248 19981023 00248 WP 1998 10 23 VJ9800540 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 351-362 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 A DENT, 11 INCHES BY 2.625 TIMES .084 WITH A DEPTH OF .098, FOUND AT FS 351 TO 362 L19 AND 20R. REMOVED AND FORMED NEW SKIN AND SPLICE. DRILLED, COUNTERSUNK, TREATED AND PRIMED. INSTALLED NEW SKIN AND SPLICE IAW DC9 SRM 51-30, 51-10-4, 5 1-10-3, RES 191745 AND DOUGLAS SB 380991. 2 L 7 2 4F A6WE 1998102300249 19981023 00249 WP 1998 10 23 VJ9800541 1 19980930 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 FLOOR SUPPORT STRUCTURE LEFT OF CENTER LINE CORRODED BEYOND LIMIT IAW DC9 SRM 53-01 FIG 1 AT FS 965, LBL 30. CUT OUT CO RRODED SECTION OF FLOORBEAM, FABRICATED AND INSTALLED NEW SECTION IAW DC9 SRM 53-05 FIG 20A. 2 L 7 2 4F A6WE 1998102300250 19981023 00250 NM 1998 10 23 K3HA980122 1 19980916 A 3350 252001 SWITCH BOEING 727 727225 1384077 NM COCKPIT INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 OVERHEAD EMERGENCY EXIT LIGHT AT AFT GALLEY COMES ON THEN OFF IN ABOUT 10 SECONDS, WHEN TURNED ON AT COCKPIT SWITCH. CH ECKED EMERGENCY LIGHTING SYSTEM, CHECK OK IAW 33-50-01. FOUND BASE LOOSE ON SWITCH, FUSE NO GOOD REPLACED FUSE. 2 L 7 3 4F A3WE 1998102300251 19981023 00251 NM 1998 10 23 K3HA980123 1 19980916 A 3350 252001 SWITCH FUSE BOEING 727 727225 1384077 NM COCKPIT INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 356PA 20626 WITH POWER REMOVED FROM A/C EMERGENCY LIGHT AT ROW 10 AND FRONT ENTRY LIGHT REMAIN ILLUMINATED. FOUND BASE LOOSE ON SWI TCH CIRCUIT FUSE, NO GOOD. REPLACED FUSE SYSTEM, CHECK OK IAW 33-50-01. 2 L 7 3 4F A3WE 1998102300252 19981023 00252 NM 1998 10 23 K3HA980124 1 19980919 A 3350 079123 LENSE BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 353PA 20622 EMERGENCY EXIT LIGHTS FLOOR TRACKS MISSING RED COVERS 2 LIGHTS, CENTER AISLE, NEAR L1. INSTALLED MISSING RED COVER ON 2 LIGHTS ON TRACK BY CENTER AISLE. OPS CHECKS GOOD IAW MM 33-50. 2 L 7 3 4F A3WE 1998102300253 19981023 00253 NM 1998 10 23 K3HA980125 1 19980920 A 3350 10085 POWER SUPPLY BOEING 727 727225 1384077 NM CABIN INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 CHECK FLOOR EMERGENCY LIGHTS. REMOVED AND REPLACED CEILING RAFT COMPARTMENT POWER SUPPLY CHARGING UNIT AND BATTERY PACK (P/N 2013-1A S/N 49492) OPS CHECK OK REF MM 33-50-01. 2 L 7 3 4F A3WE 1998102300254 19981023 00254 NM 1998 10 23 K3HA980126 1 19981015 A 3350 079120 LENS BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 8880Z 21453 FORWARD LEFT HAND EMERGENCY PATH LIGHT MISSING LENS COVER. REINSTALLED LENS COVER REF 33-50-01. TEST 23-11-0 OPS CHECK OK. 2 L 7 3 4F A3WE 1998102300255 19981023 00255 NM 1998 10 23 K3HA980127 1 19981014 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 AFT EMERGENCY AREA LIGHT INOP. REMOVED AND REPLACED AFT EMERGENCY AREA LIGHT BATTERIES. TEST 26-11-0, OPS CHECK OK. 2 L 7 3 4F A3WE 1998102300256 19981023 00256 NM 1998 10 23 K3HA980128 1 19981014 A 3350 S106S106 BATTERIES BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 FORWARD EMERGENCY AREA LIGHT INOP. REMOVED AND REPLACED FORWARD EMERGENCY AREA LIGHT BATTERIES. TEST 26-11-0, OPS CHEC K OK. 2 L 7 3 4F A3WE 1998102300257 19981023 00257 NM 1998 10 23 K3HA980129 1 19981015 A 3350 3071BPFGPL BULB BOEING 727 727225 1384077 NM ROW 29DEF FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 WHITE EMERGENCY PATH LIGHT INOP AT ROW 29DEF. RELAMPED LIGHTS, OPS CHECK GOOD PER MM 33-59-00. 2 L 7 3 4F A3WE 1998102300258 19981023 00258 NM 1998 10 23 K3HA980130 1 19981015 A 3350 09102008 END CAP BOEING 727 727225 1384077 NM CABIN MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 END CAP MISSING AFT EMERGENCY PATH TRACK. INSTALLED END CAP ON EMERGENCY PATH LIGHT TRACK PER MM 33-59-00. 2 L 7 3 4F A3WE 1998102300259 19981023 00259 NM 1998 10 23 AWXA9800212 1 19981009 A 3350 NLN7434A BATTERY PACK BOEING 737 737112 1384412 NM ROW 5-13 DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 708AW 19771 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS FROM ROW 5 TO ROW 13 NOT ILLUMINATING. REMOVED AND REPLACED BA TTERY PACK AT ROW 10 LT SIDE, OPS NORMAL. 2 L 7 2 4F A16WE 1998102300260 19981023 00260 1998 10 23 AWXA9800213 2 19980831 A 7200 ENGINE BOEING 737 737277 1384570 NM NR 2 FAILED A AWXA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 WP 28 181AW 42213 5002 22648 NR 2 ENGINE LOST OIL PRESS AND NR 2 LOW OIL PRESS LIGHT ILLUMINATED. OIL TEMP ROSE TO 135 DEGREES. SHUT NR 2 ENG DOWN WHEN PRESS REACHED 20 PSI, WINDMILLED APPROXIMATELY 18 MINUTES. AIR RETURN, RNR NR 2 ENGINE IAW TASK CARDS F5M71002 F5M 76001 R5M71002 R5M71002 F5M78002 R5M71003. 2 L 7 2 4F RT A16WE 1998102300261 19981023 00261 EU 1998 10 23 PNSA981001 1 19981016 A 7931 OIL PRESSURE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE ERRATIC A PNSA E A ENGINE SHUTDOWN UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CR CRUISE 1 AL 03 675PA 206 785163 DURING CRUISE, OIL PRESSURE FOR LT ENGINE BECAME ERRATIC. SECURED LT ENGINE. DIVERTED TO AKN. UNEVENTFUL LANDING WAS MADE. 2 L 7 2 4T 4 T RT A52EU E8NE 1998102300262 19981023 00262 SO 1998 10 23 RAAA98E9034 1 19981017 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 13 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 PAX ROW 13 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998102300263 19981023 00263 WP 1998 10 23 UPS98827916 1 19980925 A 5330 SKIN DOUG DC8 DC873F 302199F WP CARGO DOORWAY GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, THE FUSELAGE SKIN AT THE AFT LWR CORNER OF THE C-PIT DOOR IS GOUGED. REPAIRED IAW UPS EO DC8-5330-10 808-A. 2 L 7 4 4F RT 4A25 1998102300264 19981023 00264 WP 1998 10 23 UPS98827917 1 19981001 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1616 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, CORROSION BLEND OUT AT FS 1616 BETWEEN L33 TO 32R ON INTERNAL DOUBLER OUT OF LIMITS. REPAIRED IAW DH C SK 818-913 AND SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998102300265 19981023 00265 WP 1998 10 23 UPS98827918 1 19980926 A 5753 5769857613 PAN DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, LT WING O/B SLOT O/B PAN CRACKED. REMOVED AND REPLACED SLOT PAN IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998102300266 19981023 00266 WP 1998 10 23 UPS98827919 1 19981001 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1637 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, CORROSION BLEND OUT AT FS 1637 BETWEEN L32 TO 33R INTERNAL DOUBLER OUT OF LIMITS. REPAIRED IAW DHC S K-818-916. 2 L 7 4 4F RT 4A25 1998102300267 19981023 00267 WP 1998 10 23 UPS98827920 1 19980926 A 5320 36471171N FITTING DOUG DC8 DC873F 302199F WP BS 960 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, 960 FITTING CRACKED ABOVE LONG 24R RT W/W. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D AND 53-2-0 . 2 L 7 4 4F RT 4A25 1998102300268 19981023 00268 WP 1998 10 23 UPS98827921 1 19981001 A 5311 37558411 FRAME DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 818UP 46108 INSPECTION TYPE-C, FS 1220 FRAME AND ANGLE CORRODED 33R TO 35R C-3 DOOR BATHTUB AREA. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK-818-903. 2 L 7 4 4F RT 4A25 1998102300269 19981023 00269 WP 1998 10 23 UPS98827922 1 19981011 A 5330 SKIN DOUG DC8 DC873F 302199F WP CARGO DOORWAY CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 866UP 45966 INSPECTION TYPE-N/A, FOUND HI-LOK PULLED THROUGH SKIN AT LOWER BELLY NEAR PIT 33 DOOR. ALSO, FOUND 12 X 20 AREA OF CORR ISION IN AREA AS ABOVE. REPAIRED AREA BY REMOVING AND REPLACING SKIN PER EO DC8-5330-10798-A. 2 L 7 4 4F RT 4A25 1998102300270 19981023 00270 EU 1998 10 23 QXEA9801483 1 19981014 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 478US 11227 EMERGENCY EXIT LIGHT OUT ON RIGHT FORWARD WINDOW EXIT. MAINTENANCE RELAMPED, OPERATIONAL TEST IS SATISFACTORY. 2 L 7 2 4F RT A20EU 1998102300271 19981023 00271 EU 1998 10 23 QXEA9801484 1 19981008 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9A FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 EMERGENCY EXIT LIGHT AT ROW 9A IS INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TEST IS SATISFACTORY. 2 L 7 2 4F RT A20EU 1998102300272 19981023 00272 NM 1998 10 23 QXEA9801485 1 19981013 A 3350 6104781 POWER SUPPLY DHAV DHAV DHC8 DHC8102 2809003 NM CABIN INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 825PH 7013 213 EMERGENCY LIGHT AT ROW 4 INOPERATIVE. ONE OUTSIDE EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED PS4 BATTERY PACK A ND CHARGING UNIT. OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998102300273 19981023 00273 EU 1998 10 23 QXEA9801486 1 19981016 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 479AU 11228 EMERGENCY EXIT LIGHT OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST IS SATISFACTORY. 2 L 7 2 4F RT A20EU 1998102300274 19981023 00274 NM 1998 10 23 QXEA9801487 1 19981014 A 3350 CONNECTOR DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 360PH 515 EMERGENCY FLOOR LIGHT SECTION INOPERATIVE. REPAIRED CONNECTOR TO FLOOR LIGHTING. TESTED EMERGENCY ESCAPE PATH LIGHT SY STEM. ALL LIGHTS CHECK GOOD. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998102300275 19981023 00275 NM 1998 10 23 QXEA9801489 1 19981015 A 5210 SNUBBER DHAV DHC8 DHC8102 2809003 NM PAX DOOR INOP A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 826PH 214 MAIN CABIN DOOR HARD TO OPEN. REMOVED AND REPLACED MAIN CABIN DOOR GAS STRUT SNUBBER. OPERATIONAL CHECK NORMAL. 2 H 7 2 4T RT A13NM 1998102300276 19981023 00276 EU 1998 10 23 QXEA9801490 1 19981016 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU EXIT FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 488US 11240 FORWARD CABIN EXIT SIGN INOPERATIVE. MAINTENANCE RELAMPED EXIT SIGN. OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998102300277 19981023 00277 EU 1998 10 23 QXEA9801491 1 19981015 A 3350 5515800106 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 491US 11156 EXIT LIGHT AT COCKPIT THRESHOLD IS BOTH DIM AND INTERMITTENT. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LAMP ASSE MBLY. OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998102300278 19981023 00278 EU 1998 10 23 QXEA9801492 1 19981014 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 11167 THE LIGHT ABOVE THE EMERGENCY EVACUATION SLIDE IS INOPERATIVE. MAINTENANCE RELAMPED EXIT SIGN. OPERATIONAL TESTS NORMA L. 2 L 7 2 4F RT A20EU 1998102300279 19981023 00279 EU 1998 10 23 QXEA9801493 1 19981014 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT DOOR INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 11167 LIGHTS DIM IN EXIT SIGN ABOVE COCKPIT DOOR. MAINTENANCE REMOVED AND REPLACED EXIT SIGN. OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998102300280 19981023 00280 EU 1998 10 23 QXEA9801494 1 19981014 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU FWD EXIT INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 11167 LIGHTS DIM IN FORWARD EXIT SIGN IN PASSANGER CABIN CEILING NEXT TO CLOSET. MAINTENANCE REMOVED AND REPLACED EXIT SIGN. OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998102300281 19981023 00281 EU 1998 10 23 98FDEA00652 1 19981016 A 3260 SWITCH AIRBUS 310 A310203 EU NLG INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 403FE 230 NR 2 REG FAULT LIGHT ILLUM DURING CLIMB ON PRESS PG. THE V/S WAS THE SAME AS A/C RATE OF CLIMB. A/C DIDN'T PRESS. RET URN TO LAS. REMOVED AND REPLACED PROS ELECT UNIT PER 32-31-71. CHECKED WIRING FROM PROX BOX TO COCKPIT AND FROM PROX B OX TO GROUND, DUE TO RESIST TO GROUND READINGS. REMOVED AND REPLACED NOSE GEAR SHOCK ABS PRO SWITCH 82GB AND 55GB. ALL SYS OPS CHECK NORM ON GROUND PER AMM 32-61-00. MAINT CHECK FLT OF SYS ALSO SUCCESSFUL. 2 L 7 2 4F RT A35EU 1998102300282 19981023 00282 1998 10 23 98FDEA00653 4 19981017 A 3160 253CA01F102Y1 CONTACTOR AIRBUS 310 A310222 3930315 EU COCKPIT FAILED A FDEA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 SO 25 421FE 342 DURING T/O ROLL, JUST TO V1 CAPT PFD, ND WENT BLANK AS WELL AS THE ALT, HSI, GPWS WARN AC BUS OFF LIGHT BLINK AC EMER ON INVER LIGHT BLINK. WARNING HORN CAME ON WITH BLINK LIGHTS ONLY ECAM WAS FWS CRT AMBER CAUTION FAA SHOW 700 FT NO FLAP IND DURING LAND. REMOVED AND REPLACED RELAY 25XC, 6XE CONTACTORS 11XC, 12XC AND 1XC CB. RESTORED POWER, ALL OPS CKS NO RM. 2 L 7 2 4F RT A35EU 1998102300283 19981023 00283 NM 1998 10 23 98FDEA00654 1 19981019 A 5330 6518420277 SKIN BOEING 727 72725C 138400H NM BS 340-342 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR 273 BULGING SKIN AT BS 340-342, RBL 18, WL 148. ** S/D ** REPAIRED SKIN AT BS 338, RBL 21, WL 148 IAW FEDEX SRM 53 -30-03. 2 L 7 3 4F A3WE 1998102300284 19981023 00284 NM 1998 10 23 98FDEA00655 1 19981017 A 2797 WIRE BOEING 727 7272S2F 1384O81 NM TE FLAPS BROKEN A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 205FE 22927 ASYMMETRY I/B FLAP IND ON DEPARTURE WITH I/B FLAP AT 5 DEG. INSTALLED NEW IND, NO HELP. REINSTALLED ORIG FLAP IND. RE MOVED AND REPLACED RT I/B TRANSMITTER REF MM 27-52-2, NO HELP KH 193173 ORIG. REINSTALLED JHS 12168, CHECK WIRING FROM LT AND RT I/B FLAP POS TRANSMITTER TO I/B FLAP POS IND, ALL WIRING CHECK GOOD PER 727 WDM 27-52-01 GH 81251. FOUND GROU ND WIRE 014-20 BROKEN AT STUD GD90 REPAIR. 2 L 7 3 4F A3WE 1998102300285 19981023 00285 EU 1998 10 23 98FDEA00656 1 19981018 A 3230 DAMPER AIRBUS 310 A310203 EU LT MLG INOP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 408FE 257 T/O MEM COULD NOT RAISE GEAR HANDLE. TRIED BOTH POSITION DET SYSTEM 1 AND 2. RECYCLE HANDLE DOWN AND RETRIED. STILL NO T ABLE TO RETRACT. RETURNED TO MEM. REMOVED AND REPLACED LEFT MAIN LANDING GEAR PITCH DAMPER. PERFORMED GEAR SWING, O PS CHECK OK. 2 L 7 2 4F RT A35EU 1998102300286 19981023 00286 WP 1998 10 23 MWEA981001 1 19981018 A 5320 99365037 SPLICE DOUG DC9 DC982 3022082 WP BS 1117 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CORROSION ON PREVIOUS REPAIR AT FS 1117 LONGERON 2 AND 3R. MTC REMOVED CORROSION FABRICATED AND INSTALLED NEW SPL ICE. 2 L 7 2 4F A6WE 1998102300287 19981023 00287 WP 1998 10 23 MWEA981002 1 19981010 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE DETACHED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 209ME 47730 THE FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF. MTC REINSTALLED DOOR SLIDE COVER. 2 L 7 2 4F A6WE 1998102300288 19981023 00288 WP 1998 10 23 MWEA981003 1 19981010 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP PAX DOOR SLIDE DETACHED A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 209ME 47730 THE FORWARD ENTRANCE DOOR SLIDE COVER FELL OFF. MTC REINSTALLED SLIDE COVER. 2 L 7 2 4F A6WE 1998102300289 19981023 00289 WP 1998 10 23 MWEA981004 1 19981011 A 3260 0080004003 PROXIMITY SWITCH DOUG DC9 DC932 3022066 WP LT MLG FAILED A MWEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 203ME 47673 LEFT UNSAFE RED GEAR LIGHT REMAINS ON WITH GEAR HANDLE IN UP POSITION. MTC REMOVED AND REPLACED LEFT MLG UP LIMIT SWITC H AND PROXIMITY SWITCH CONTROL BOX. 2 L 7 2 4F A6WE 1998102300290 19981023 00290 1998 10 23 MWEA981005 4 19981009 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 THE GALLEY EMERGENCY SLIDE FORWARD FOUND WITH LESS THAN 500 PSI. MTC REMOVED AND REPLACED GALLEY DOOR EMERGENCY SLIDE. 2 L 7 2 4F A6WE 1998102300291 19981023 00291 NM 1998 10 23 DL72S982112 1 19981001 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 CORROSION FOUND AT FWD ATTACH LUG FACES AND BORE AND TO MLG BEAM ATTACH HOLES. BUSH LUG HOLES AND INSTALLED SPLICE PLAT E REPAIR FOR MLG BEAM ATTACH HOLES. 2 L 7 3 4F A3WE 1998102300292 19981023 00292 NM 1998 10 23 DL72S982113 1 19980928 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 TYPICAL CORROSION FOUND IN MLG BEAM ATTACH HOLES. REPAIRED SIMILAR TO SB 727-57-0178 EXCEPT TO OS HOLES, .838 MAX DIAME TER TO REMOVE ALL CORROSION. 2 L 7 3 4F A3WE 1998102300293 19981023 00293 NM 1998 10 23 DL72S982114 1 19980928 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 401DA 21145 BUSH FWD ATTACH LUG AND REPAIR MLG BEAM ATTACH HOLES PER SB 727-57-0178, EXCEPT INCREASE HOLE DIA TO .847. 2 L 7 3 4F A3WE 1998102300294 19981023 00294 NM 1998 10 23 DLM88982116 1 19981012 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 398 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 999DN 53371 FUSELAGE SKIN FOUND WITH DAMAGE THAT WAS BLENDED OUT AT THE CURRENT VISIT. BLEND WAS TOO DEEP REQUIRING SKIN CUTOUT. R EPAIRED PER ERA 332358-14. 2 L 7 2 4F RT A6WE 1998102300295 19981023 00295 NM 1998 10 23 DLM88982117 1 19981012 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 1323 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 999DN 53371 FUSELAGE SKIN JUST AFT OF THE LAV SERVICE PANEL WAS FOUND WITH A GOUGE. REPAIRED PER ERA 332361-14. 2 L 7 2 4F RT A6WE 1998102300296 19981023 00296 NM 1998 10 23 DL72W982118 1 19981012 A 5313 651821744 STRINGER BOEING 727 727247 138408F NM BS 371 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 CORROSION WAS FOUND ON THE I/B FLANGE OF S3R AT FS 371 REQUIRING A SECTION OF STRINGER TO BE CUT OUT. REPAIRED PER ERA 332244-14. 2 L 7 3 4F A3WE 1998102300297 19981023 00297 NM 1998 10 23 DL72W982119 1 19981012 A 5330 65545655 SKIN BOEING 727 727247 138408F NM BS 687 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 A FAILED FASTENER WAS FOUND IN THE UPPER ROW OF THE S26R SKIN LAP JOINT AT BS 684. CRACKS WERE FOUND EMANATING FROM THI S FASTENER HOLE IN THE OUTER SKIN ONLY. THE CRACKS WERE .125 AND .0937 LONG. REPAIRED PER ERA 332342-14. 2 L 7 3 4F A3WE 1998102300298 19981023 00298 NM 1998 10 23 DLM88982125 1 19981009 A 5330 5920323553 SKIN DOUG MD88 MD88 3023688 NM BS 390 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 924DL 49711 THE FUSELAGE SKIN JUST ABOVE THE C1 DOOR CUTOUT WAS GOUGED BY GROUND EQUIPMENT. THE GOUGE WAS TO THE SKIN ONLY AND WAS CUT OUT. THE CUT OUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 365804-14, REV A. 2 L 7 2 4F RT A6WE 1998102300299 19981023 00299 NM 1998 10 23 DL73E982127 1 19981012 A 5330 6545800219 SKIN BOEING 737 7372S3 NM L1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 THE UPPER HINGE CUTOUT OF THE L1 DOOR OPENING WAS FOUND WITH A TYPICAL CRACK IN THE SKIN AND BONDED DOUBLER. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER PER THE B737 SRM 53-30-3 FIG 21. THE REPAIR WAS DOCUMENTED P ER ER/A 365839-14, REV A. 2 L 7 2 4F RT A16WE 1998102300300 19981023 00300 NM 1998 10 23 DL73E982128 1 19981012 A 5315 6545410555 FLOORBEAM BOEING 737 7372S3 NM BS 725 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 THE UPPER CAP OF THE RBL 24.82 OVERWING PASSENGER FLOORBEAM WAS FOUND WITH A .5 INCH CRACK EMANATING FROM A CUTOUT FOR A SEAT TRACK ATTACH POINT. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER AND TRIPLER PER ER/A 365847-14, REV B. 2 L 7 2 4F RT A16WE 1998102300301 19981023 00301 NM 1998 10 23 DL72S982129 1 19981012 A 2782 BRACKET BOEING 727 727225 1384077 NM LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8891Z 21860 THE O/B ACTUATOR SUPPORT BRACKETS ON THE NR 2 AND NR 7 SLATS WERE FOUND WITH TYPICAL CRACKS IN THE WEB AND DOUBLER ASSY. THE I/B AND O/B ACTUATOR SUPPORT BRACKETS WERE REPAIRED/ MODIFIED PER THE REQUIREMENTS OF BAC S/B 727-57-0130, REV 2. THE REPAIRS WERE DOCUMENTED PER ER/A 365851-14AD. 2 L 7 3 4F A3WE 1998102300302 19981023 00302 NM 1998 10 23 DLM88982131 1 19981009 A 5330 5911401179 SKIN DOUG MD88 MD88 3023688 NM FS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 924DL 49711 THE FUSELAGE SKIN AT FS 218 BETWEEN STRINGERS 18L AND 20L WAS FOUND DENTED/DEFORMED. THE DAMAGED AREA OF SKIN WAS CUTOU T OVER A 13.5 X 3.75 AREA. THE SKIN CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 365809-14, REV A. 2 L 7 2 4F RT A6WE 1998102300303 19981023 00303 NM 1998 10 23 DL73E982133 1 19981013 A 3350 POWER SUPPLY RPS1B BOEING 737 737247 138448D NM FLT CREW INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 378DL 3811 23605 ON LAYOVER CHECK, FOUND F/C EMERGENCY LIGHTS- TRACK LIGHTING INOP. REPLACED POWER SUPPLY. 2 L 7 2 4F A16WE 1998102300304 19981023 00304 NM 1998 10 23 DL76L982134 1 19981013 A 3300 POWER SUPPLY 20131A BOEING 767 767332 1382001 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 198DN 59986 28455 FOUND ON LAYOVER INSPECTION, EMERGENCY LIGHTS SEAT ROWS 35 TO 45 ARE INOP, LEFT AND RIGHT SIDE OF AIRCRAFT. FOUND POWER SUPPLY PACK INOP. REPLACED POWER SUPPLY STATION 1356 LEFT SIDE, LIGHTS WORK OK. (S/N 59986) OFF, (S/N 9355) ON, (P/N 337101963). 2 L 7 2 4F RT A1NM 1998102300305 19981023 00305 NM 1998 10 23 DL72S982135 1 19980918 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 LWR AFT SPAR RAIL CRACKED TWO PLACES AT I/B DRIVE ROD CUTOUT. REPAIRED PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998102300306 19981023 00306 NM 1998 10 23 DL72S982136 1 19981013 A 5330 6554583125 SKIN BOEING 727 727232 1384082 NM BS 1140 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 476DA 20753 THE FUSELAGE SKIN AT STRINGER 22L BETWEEN FS 1110 AND 1166 WAS TORN AND GOUGED DUE TO CONTACT WITH GROUND EQUIPMENT. TH E DAMAGE WAS REMOVED FROM THE SKIN WITH TWO CUTOUTS MEASURING 4 X 28.25 AND 3.25 X 16.5. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER. INSTALLED PER ER/A 365850-14, REV A. A NEW SECTION OF STRINGER WAS SPLICED IN PER THE B727 SRM. 2 L 7 3 4F A3WE 1998102300307 19981023 00307 NM 1998 10 23 DL73K982137 1 19981013 A 5312 6516300205 BULKHEAD WEB BOEING 737 737232 1384475 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 311DL 23083 THE FS 178 BULKHEAD WEB WAS FOUND WITH A CRACK AT LBL 5.7, WL 212. THE WEB HAD A PREVIOUS REPAIR IN THE AREA FOR 3 OTHE R CRACKS WHICH WERE CUTUOUT OF THE WEB. THE EXISTING REPAIR DOUBLER WAS REMOVED, THE NEW CRACK CUTOUT, THE WEB INSPEC TED FURTHER AND A NEW ALUMINUM REPAIR DOUBLER WAS INSTALLED TO REPAIR ALL OF THE CUTOUT LOCATIONS. THE REPAIR WAS ACCOM PLISHED PER ER/A 365817-14, REV B. 2 L 7 2 4F RT A16WE 1998102300308 19981023 00308 NM 1998 10 23 DL72W982138 1 19981014 A 5320 FRAME BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 CRACK WAS FOUND IN THE AFT ENTRY DOORWAY LT FRAME AT WL 276.6. THE CRACK WAS 4.5 INCH LENGTH AND TYPICAL OF THAT FOUND IN SB 727-53-0055 REV 9. REPAIRED PER ERA 332362-14AD. 2 L 7 3 4F A3WE 1998102300309 19981023 00309 NM 1998 10 23 DL72S982139 1 19981014 A 5330 SKIN BOEING 727 727232 1384082 NM BS 295 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 FUSELAGE SKIN WAS FOUND WITH A TIME LIMITED EXT REPAIR DOUBLER FOR A CRACK IN THE SKIN AT FS 294.5, BELOW S15R. THE TIM E LIMITED REPAIR WAS REMOVED AND ADDITIONAL DAMAGE FOUND. REPAIRED PER ERA 332347-14. 2 L 7 3 4F A3WE 1998102300310 19981023 00310 NM 1998 10 23 DL72L982142 1 19981014 A 2782 SUPPORT BOEING 727 727232 1384082 NM NR 7 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 506DA 21308 THE DOUBLERS FOR THE NR 7 SLAT ACTUATOR SUPPORT STRUCTURE WERE FOUND WITH THE TYPICAL CRACKS PER BAC S/B 727-57-0130, RE V 2. THE CRACKED DOUBLERS WERE REPAIRED/MODIFIED PER THE REQUIREMENTS OF THE S/B. THE REPAIR WAS DOCUMENTED PE R ER/A 365879-14AD. 2 L 7 3 4F A3WE 1998102300311 19981023 00311 NM 1998 10 23 DL72S982143 1 19980929 A 5713 STRNGER BOEING 727 727232 1384082 NM BS 629 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 TAB CRACKED AT WING STRINGER TO FRAME ATTACHMENT STA 629 AT 4TH FROM FWD SIDE AND 2ND FROM FWD SIDE. REPAIRED PER MM 57 -13-0 FIG 804 NRC 521 AND NRC 520. 2 L 7 3 4F A3WE 1998102300312 19981023 00312 NE 1998 10 23 DLM88982145 2 19981015 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA A UNSCHED LANDING T J ENGINE CASE PENETRATION WARNING INDICATION TO TAKEOFF 1 SO 27 902DE 23284 53379 725530 NR 2 ENG FAILED AFTER T/O. RETURNED TO LAND. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1998102300313 19981023 00313 NM 1998 10 23 DLM88982147 1 19981015 A 5320 PAN DOUG MD88 MD88 3023688 NM CARGO DOORWAY CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 926DL 49713 THE FWD CARGO DOOR OPENING WAS FOUND WITH EXTENSIVE CORROSION ON THE LWR JAMB PAN REQUIRING A SPLICE OF THE PAN. REPAIR ED PER ERA 365892-14. 2 L 7 2 4F RT A6WE 1998102300314 19981023 00314 WP 1998 10 23 DLL14982148 1 19981016 A 3350 RPS1B BATTERY PACK LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 193C1244 FIRST CLASS EMERGENCY LIGHTS INOP. MTC REPLACED BATT PACK AND RACK. OPN NORMAL NOW. 2 L 7 3 4F A23WE 1998102300315 19981023 00315 NM 1998 10 23 DL72S982149 1 19981016 A 5711 FRAME BOEING 727 727232 1384082 NM BS 760 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 CRACK WAS FOUND IN THE VERT FLANGE OF THE WING TO FUSE UPPER ATTACH CHORD, LWR FRAME HOLE RBL 70.85, FS 760. REPAIRED P ER ERA 332283-14AD. 2 L 7 3 4F A3WE 1998102300316 19981023 00316 NM 1998 10 23 DL72S982150 1 19981016 A 5713 65185933 STRINGER BOEING 727 727232 1384082 NM WS 304 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 RT WING UPPER SURFACE S18 AT WS 304 WAS FOUND CRACKED, REQUIRING A 2.5 INCH CUTOUT. REPAIRED PER ERA 332341-14. 2 L 7 3 4F A3WE 1998102300317 19981023 00317 NM 1998 10 23 DL72S982151 1 19981016 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 950 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 FUSE STR 29R WAS FOUND CRACKED AT FS 950E. REPAIRED PER ERA 332275-14. 2 L 7 3 4F A3WE 1998102300318 19981023 00318 NM 1998 10 23 DL72S982153 1 19981016 A 5312 6516350 BLKHD STIFFENER BOEING 727 727232 1384082 NM BS 1183 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 THE FS 1183 BULKHEAD VERTICAL STIFFENER AT RBL 36.83 WAS FOUND WITH TYPICAL CRACKING AT WL 240. THE CRACKED STIFFENER W AS REPAIRED PER BAC S/B 727-53-0192 AND DOCUMENTED PER ER/A 365894-14. 2 L 7 3 4F A3WE 1998102300319 19981023 00319 NM 1998 10 23 DL72S982154 1 19981016 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 S18 TAB ON THE RT WING VENT BOX AT WS 171.5 WAS FOUND CRACKED. ADDITIONAL DAMAGE INCURRED WHILE INSTALLING THE SRM REPA IR. REPAIRED PER ERA 332288-14. 2 L 7 3 4F A3WE 1998102300320 19981023 00320 NM 1998 10 23 DL72K982155 1 19981016 A 5320 WEB BOEING 727 727232 1384082 NM BS 1290 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 RT TORQUE BOX VERT WEB CRACKED AT LIGHTENING HOLES STA 1290 AND 1235 RT. REPAIRED PER MM 53-11-0 PG 832. 2 L 7 3 4F A3WE 1998102300321 19981023 00321 NM 1998 10 23 DL72K982156 1 19981016 A 5330 SKIN BOEING 727 727232 1384082 NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 413DA 21233 A .5 INCH CRACK FUSELAGE SKIN AT L-4 WINDOW I/B FWD ATTACH SCREW. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1998102300322 19981023 00322 NM 1998 10 23 DL72S982157 1 19981016 A 3350 BATTERY S106 BOEING 727 727232 1384082 NM SEAT ROW 25 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 21223 SEAT ROW 25 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY, OPS NOW OK. 2 L 7 3 4F A3WE 1998102300323 19981023 00323 NM 1998 10 23 DL757982158 1 19981016 A 3397 WIRE BOEING 757 757232 1384965 NM SEAT 38 BROKEN A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 652DL 24392 ON L/O, FOUND EMERGENCY TRACK LIGHTING INOP FROM SEAT 38 AFT. RECONNECTED CABLE AT 38, CKS OK. 2 L 7 2 4F RT A2NM 1998102300324 19981023 00324 NM 1998 10 23 DL72S982162 1 19981018 A 3350 1000677 BATTERY BOEING 727 727232 1384082 NM ENTRY DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 401DA 21145 RT FWD ENTRY DOOR OVERHEAD EMEGENCY LIGHT WILL NOT TEST. REPLACED BATTERIES AND RACK NOW CKS NORMAL. 2 L 7 3 4F A3WE 1998102300325 19981023 00325 NM 1998 10 23 P5CA9801537 1 19981010 A 5321 FLOOR BOEING 747 747122 1384872 NM BS 500 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FLOOR PANEL STATION 500 TO 580 RBL 20 FOUND DELAMINATED. REMOVED AND REPAIRED PER SRM 51-10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998102300326 19981023 00326 NM 1998 10 23 P5CA9801538 1 19981016 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 200 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK PIT STA 2000 STR 22 SUPPORT ANGLE CRACKED. REMOVED AND REPAIRED PER SRM 51-10-01, 51-30-02 AND 51-40-04. 2 L 7 4 4F A20WE 1998102300327 19981023 00327 NM 1998 10 23 P5CA9801539 1 19981016 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK PIT STA 1970/1980 BL 22R ATTACH ANGLE HAS CRACK. REMOVED AND REPLACED PER SRM 51-10-01 AND SRM 51-30-03. 2 L 7 4 4F A20WE 1998102300328 19981023 00328 NM 1998 10 23 P5CA9801540 1 19981016 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 2020 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO COMPARTMENT STA 1960 BLR 34 TO STA 2020 BLR 34 FLOOR PANEL SUPPORT CRACKED. REMOVED AND REPLACED PER SRM 51- 30-01. 2 L 7 4 4F A20WE 1998102300329 19981023 00329 NM 1998 10 23 P5CA9801541 1 19981015 A 5311 FRAME BOEING 747 747122 1384872 NM BS 2060 GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 UPPER DECK FRAME AT BS 2060 STR 16L FOUND GOUGE. REPAIRED PER SRM 53-10-04. 2 L 7 4 4F A20WE 1998102300330 19981023 00330 NM 1998 10 23 P5CA9801542 1 19981015 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 2000 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO PIT AT STA 2000L FLOOR PANEL SUPPORT CRACKED AT TIEDOWN AREA. REMOVED AND REPLACED PER SRM 51-30-02. 2 L 7 4 4F A20WE 1998102300331 19981023 00331 NM 1998 10 23 P5CA9801543 1 19981015 A 5320 CHANNEL BOEING 747 747122 1384872 NM BS 2060 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO AREA STA 2060L SUPPORT CHANNEL HAS CRACK AT LT SIDE. REMOVED AND REPLACED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998102300332 19981023 00332 NM 1998 10 23 P5CA9801544 1 19981015 A 5313 STRINGER BOEING 747 747122 1384872 NM BS 1820 PUNCTURED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 UPPER DECK AT STA 1820R STR 15R FLANGE PUNCTURED. REPAIRED PER SRM 53-10-04, 51-30-02. 2 L 7 4 4F A20WE 1998102300333 19981023 00333 NM 1998 10 23 P5CA9801545 1 19981015 A 5320 CHANNEL BOEING 747 747122 1384872 NM BS 1940-2060 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO COMPARTMENT STA 1940 TO STA 2060R SEVERAL HAT CHANNELS CRACKED. REMOVED AND REPAIRED HAT CHANNEL PER SRM 51- 10-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998102300334 19981023 00334 NM 1998 10 23 P5CA9801546 1 19981007 A 5320 SUPPORT BOEING 747 747122 1384872 NM BS 2080 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO PIT STA 2080R FLOOR PANEL SUPPORT FOUND CRACKED. REPAIRED PER SRM 51-40-03. 2 L 7 4 4F A20WE 1998102300335 19981023 00335 NM 1998 10 23 P5CA9801547 1 19981007 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1960 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO COMPARTMENT AT STATION 1960 BL 50R ANGLE FOUND CRACKED. REPAIRED PER SRM 51-10-01, 53-10-03 AND 51-30-02. 2 L 7 4 4F A20WE 1998102300337 19981023 00337 NM 1998 10 23 P5CA9801549 1 19981017 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1940 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO STA 1940 BL 22L ATTACH ANGLE FOUND CRACKED. REPAIRED PER SRM 51-01-01, 51-30-02 AND 51-40-04. 2 L 7 4 4F A20WE 1998102300338 19981023 00338 NM 1998 10 23 P5CA9801550 1 19981017 A 5321 FLOOR BOEING 747 747122 1384872 NM BS 720 DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 REPLACED UPPER DECK FLOOR PANELS AT BS 720R DUE DELAMINATION. REMOVED AND REPLACED PER SRM 53-22-01, 51-10-01 AND 51-30 -02. 2 L 7 4 4F A20WE 1998102300339 19981023 00339 NM 1998 10 23 P5CA9801551 1 19981017 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 2000 & 2100 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO COMPARTMENT AT STA 2000/2100L ATTACH ANGLES FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-10-01 AND 51-30-0 2. 2 L 7 4 4F A20WE 1998102300340 19981023 00340 NM 1998 10 23 P5CA9801552 1 19981017 A 5320 ANGLE BOEING 747 747122 1384872 NM BS 1960-1980 CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 BULK CARGO PIT AT STATION 1960 TO 1980 BL 22L ATTACH ANGLE FOUND CRACKED. REMOVED AND REPLACED PER SRM 51-10-01 AND 51- 30-02. 2 L 7 4 4F A20WE 1998102300341 19981023 00341 NM 1998 10 23 P5CA9801553 1 19981017 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 570 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 FWD CARGO COMPARTMENT AT STATION 570 RBL 30 TO 35 FOUND BROKEN INTERCOSTAL. REMOVED AND REPLACED PER SRM 51-10-01 AND S RM 51-30-02. 2 L 7 4 4F A20WE 1998102300342 19981023 00342 NM 1998 10 23 P5CA9801554 1 19981017 A 5320 INTERCOSTAL BOEING 747 747122 1384872 NM BS 1720-1740 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 AFT CARGO BULK PIT BS 1720L TO BS 1740L SPACING RIB DAMAGED. REPAIRED PER SRM 51-10-01. 2 L 7 4 4F A20WE 1998102300343 19981023 00343 NM 1998 10 23 P5CA9801555 1 19981017 A 5730 PANEL BOEING 747 747122 1384872 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEFT WING PANEL FWD OF LEFT FLYING PANEL HAS CRACK. REPAIRED PER SRM 51-40-09 AND 51-24-11. 2 L 7 4 4F A20WE 1998102300344 19981023 00344 NM 1998 10 23 P5CA9801556 1 19981017 A 5347 BAC152015167 SEAT TRACK BOEING 747 747122 1384872 NM BS 520-740 CORROSION A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK BS 520L TO 740L. REPLACED SEAT TRACK FROM BS 520L TO 740L FOR CONVIENENCE PE R SRM 53-10-21 PG 45. 2 L 7 4 4F A20WE 1998102300345 19981023 00345 NM 1998 10 23 P5CA9801557 1 19981017 A 5347 BAC152015167 SEAT TRACK BOEING 747 747122 1384872 NM BS 520-720 CORRODED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 LEVEL 1 CORROSION ON UPPER DECK SEAT TRACK AT BS 520R TO 720R. REPLACED FOR CONVIENENCE PER SRM 52-10-21 PG 45. 2 L 7 4 4F A20WE 1998102300346 19981023 00346 WP 1998 10 23 ARWA981019 1 19981019 A 2782 72002C ACTUATOR LKHEED 1011 10113851 5265010 WP NR 6 LE SLAT INOP A ARWA O OTHER F J FLT CONT AFFECTED WARNING INDICATION TO TAKEOFF 1 SO 19 307GB 193U1131 L/E TRANS LIGHT ON, AFTER SLAT/FLAP RETRACTION. FLAPS RECYCLED, LIGHT REMAINED ON, AIRFRAME VIBRATES SLIGHTLY WITH FLAP S RETRACTED. SLAT DEGREE IND SHOWS 1-2 DEGREE EXTENSION WITH SLAT UP. AFTER LANDING L/E TRANS LIGHT EXTINGUISHED WHEN FLAPS RETRACTED. REMOVED AND REPLACED RT WING NR 6 SLAT ACTUATOR, OPS CHECK IAW M/M 27-81-21 NORMAL. 2 L 7 3 4F RT A23WE 1998102300347 19981023 00347 NM 1998 10 23 USAA980400 1 19980918 A 5320 WEB BOEING 737 737201 1384454 NM BS 1016 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 252AU 42850 22758 CLT - DURING THROUGH-FLIGHT VISUAL INSPECTION, FOUND A .50 INCH CRACK BS 1016 WEB AT STR 15L. REMOVED DAMAGE AND INSTAL LED FABRICATED REPAIR PART PER SRM 53-10-4 FIG 3. (X) 2 L 7 2 4F A16WE 1998102300361 19981023 00361 SW 1998 10 23 98ZZZX3849 1 19980815 A 2910 70010F0004154 HOSE BELL 206 206B3 1181506 SW HYDRAULIC SYSTEM RUPTURED A A EHAA O OTHER K F FLUID LOSS FLT CONT AFFECTED NR NOT REPORTED 1 AL 03 70DB 1730 AIRCRAFT LOST HYDRAULIC POWER TO FLIGHT CONTROLS DUE TO RUPTURED RT CYCLIC SERVO FLEX LINE. LINE SUPPLIES HYDRAULIC FLU ID TO AFT END OF SERVO. IMPROPER ASSY OF FITTING TO HOSE IS SUSPECTED. 1 G 7 1 3U H2SW 1998102300362 19981023 00362 EA 1998 10 23 CHI3212 1 19980923 A 6710 234HS5603 ACTUATOR BOEING 234 234 1385049 EA CYCLIC MALFUNCTIONED B A CHIR A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 NM 09 239CH 6621 146 0058TASV MJ006 PILOT ATTEMPTED TO APPLY SLIGHT AMOUNT OF AFT CYCLIC TO SLOW HELICOPTER AND EXTERNAL LOAD. THE CYCLIC WOULD NOT MOVE AF T OR FORWARD. NO SIGN OF ANYTHING BLOCKING THE CYCLIC MOTION, STILL HAD COLLECTIVE YAW AND ROLL CONTROLS, NO FORE AND A FT CONTROL. PILOT LOWERED COLLECTIVE FOR DESCENT TO A LANDING ON A ROAD IN EVENT CYCLIC CONTROL COULD NOT BE REGAINED. THE CYCLIC FREED AND A LANDING WAS MADE USING MINIMAL CONTROL INPUTS. POST-INSPECTION FOUND PITCH LOWER BOOST ACTUATOR OUTPUT TRUNNION WITH BINDING ROTATIONAL MOTION. (X) 2 G 7 2 4U H9EA 1998102300363 19981023 00363 NM 1998 10 23 98ZZZX3850 1 19980729 A 7160 311800401 SCREEN DOUG MD900 MD900 3027375 NM AIR INLET WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 694 90000012 SCREEN WORN BEYOND SERVICE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998102300364 19981023 00364 EU 1998 10 23 98ZZZX3851 1 19980916 A 7714 614764021 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 758 469 2917 INDICATOR UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998102300378 19981023 00378 CE 1998 10 23 98ZZZX3865 1 19980831 A 3230 08421043 BELLCRANK CESSNA 310 310R 2074245 CE NLG BROKE A A EHBA O OTHER O OTHER DE DESCENT 1 EA 17 49390 7497 310R0120 BELLCRANK BROKE AS THE GEAR WAS BEING RETRACTED IN-FLIGHT CAUSING THE NOSE LANDING GEAR TO GET STUCK IN THE UP POSITION. PILOT WAS UNABLE TO GET NOSE GEAR DOWN AND LANDED ON MAINS ONLY. 1 L 7 2 3O 3A10 1998102300384 19981023 00384 CE 1998 10 23 98ZZZX3871 1 19980910 A 3230 HMX5FG ROD END BEECH 58 58 1152740 CE NLG CRACKED A A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 2064V TH1004 GOING INTO MDW, NOSE GEAR NOT SHOWING DOWN AND LOCK. CYCLED GEAR, STILL NO DOWN AND LOCK INDICATION. AIRCRAFT LANDED, NOSE GEAR COLLAPSED. FOUND ROD END ON RETRACT ROD SPLIT OPEN AT GREASE FITTING SEPARATING ROD END FROM NOSE GEAR. 1 L 7 2 3O 3A16 1998102300388 19981023 00388 CE 1998 10 23 98ZZZX3875 1 19980922 A 3230 HMX5FG ROD END BEECH 58 58 1152740 CE NLG SPLIT A A BSYA O OTHER O OTHER LD LANDING 1 GL 07 58WA TH201 NOSE GEAR COLLAPSED LANDING AT BWI. FOUND ROD END ON RETRACT ROD SPLIT OPEN AT GREASE FITTING SEPARATING ROD END FROM N OSE GEAR. 1 L 7 2 3O 3A16 1998102300405 19981023 00405 WP 1998 10 23 TWAA9816405 1 19981016 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 897 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND LIGHT CORROSION ON THE FORMER CAP AT STA 897, LONGERON 27L TO 29L. REPLACED FORMER CAP PER STANDARD PROCESSES MANUAL 6-70-1. 2 L 7 2 4F A6WE 1998102300406 19981023 00406 WP 1998 10 23 TWAA9816801 1 19981019 A 3220 DEFLECTOR DOUG DC9 DC982 3022082 WP NLG OUT OF POSITION A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 925TW 49357 NOSE GEAR FAILED TO RETRACT ON TAKEOFF. RECYCLED GEAR ONCE NO HELP. RETURNED TO STL. FOUND SOME HARDWARE MISSING FROM THE NLG SPRAY DEFLECTOR, ALLOWING THE DEFLECTOR TO ROTATE. REPLACED A NUT, MFG AN320-8, BOLT, NAS 6208-11D, WASHER, NA S1106-28D, AND PIN, MS24665-302. CHECK-C 8-24-98 STL. 2 L 7 2 4F A6WE 1998102300407 19981023 00407 WP 1998 10 23 TWAA9816802 1 19981016 A 3350 7732 LAMP DOUG DC9 DC983 3022083 WP SEAT 23D FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9406W 53126 DURING MAINT, FOUND EGRESS LIGHTS INOPERATIVE AT CABIN SEAT 23D AND 30D. REPLACED LAMPS. CHECK-C 1-15-98 STL. 2 L 7 2 4F RT A6WE 1998102300408 19981023 00408 WP 1998 10 23 TWAA9816803 1 19981017 A 2170 1794609 COALESCER DOUG DC9 DC982 3022082 WP LT & RT PACK DIRTY A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CE 05 920TW 49369 AFTER TAKEOFF THERE WAS NOTICEABLE BURNING ODOR WHEN RT PACK WAS TURNED ON. REPLACED LT AND RT WATER SEPARATORS ACCOUNT DIRTY. ALSO, REPLACED APU PRECAUTIONARY, MFG 381276-1, DUE TO DRIED OIL IN INLET SCREEN. CHECK-C 6-18-98 STL. 2 L 7 2 4F A6WE 1998102300409 19981023 00409 WP 1998 10 23 TWAA9816804 1 19981016 A 5755 ANGLE DOUG DC9 DC931 3022065 WP RT SPOILER CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND RT WING OTBD SPOILER, OTBD DOWN STOP ANGLE WAS CRACKED ON THE INBD SIDE. INSTALLED NEW TEE ANGLE, MFG 5918134-1, PER SRM 51-01, PG 1 ITEM C. INSTALLED RIVETS PER SRM 51-30-02. INSTALLED FASTENERS PER SRM 5 1-30-0. 2 L 7 2 4F A6WE 1998102300410 19981023 00410 NM 1998 10 23 VJ9800543 1 19980930 A 5313 654769326 STRINGER BOEING 737 737284 138448R NM BS 727-840 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 RT BELLY SKIN HAS CORROSION BULGE BETWEEN FASTENERS AT BS 741, S28R. REMOVED AND REPLACED STRINGER S27R FROM BS 727-840 IAW B737 SRM 51-30-2, 51-10-1. 2 L 7 2 4F A16WE 1998102300411 19981023 00411 NM 1998 10 23 VJ9800544 1 19980930 A 5280 65522045 HINGE BOEING 737 737284 138448R NM LT MLG DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 TOP SIDE LT MLG DOOR HINGE CASTING CORRODED. REMOVED AND INSTALLED NEW CASTING, TRIMMED SKIN 2 INCHES, FABRICATED AND I NSTALLED FILLERS AND DOUBLERS IAW B737 SRM 51-30-2, 51-40-4, MM 32-13-11. 2 L 7 2 4F A16WE 1998102300412 19981023 00412 WP 1998 10 23 VJ9800545 1 19980916 A 5210 5918758503 HINGE DOUG DC9 DC932 3022066 WP PAX DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FWD PSGR DOOR UPPER HINGE CORRODED AND COATING MISSING. REPLACED UPPER DOOR HINGE IAW DC9 SRM 51-30-2, OHM 52-11-1 AND MM 52-71-0. 2 L 7 2 4F A6WE 1998102300413 19981023 00413 WP 1998 10 23 VJ9800546 1 19981006 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 680 CRACKED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 HFEC INSPECTION CONFIRMED FASTENER HOLE CRACK IN SKIN AT FS 680 RT SIDE AND FS 718 RT SIDE. CUT OUT CRACKED AREA, FABRI CATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW DC9 SRM 51-10-3, DC9 DWG SRO9530129 AND SRM 53-04, FIG 40. 2 L 7 2 4F A6WE 1998102300414 19981023 00414 EU 1998 10 23 MALA976214 1 19981010 A 2750 676801007 CONTROL UNIT BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 515XJ E2333 DURING FLIGHT WHEN FLAPS SELECTED TO 18 DEGREES, THE FLAP INOP AND FLAP FAULT LIGHTS ILLUMINATED. AIRCRAFT RETURNED TO DTW AND A NO FLAP LANDING MADE. MAINTENANCE RESET TORQUE LIMITER, REINSTATED NORMAL CONTROL. REPLACED FLAP CONTROL UNI T IAW AVRO AMM 27-50-17, 27-50-00. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998102300415 19981023 00415 NM 1998 10 23 MALA976215 1 19981014 A 5347 85320490133 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 848MA 346 DURING SEAT INSPECTION FOR AIRCRAFT TURN BACK, THE LEFT INBOARD SEAT RAIL FWD OF STA X255:0 HAS CORROSION. MAINTENANCE SPLICED NEW SECTION OF SEAT RAIL AND REPLACED SEAT RAIL IAW DEHAVILLAND RD8-53-1932. 2 H 7 2 4T RT A13NM 1998102300416 19981023 00416 NM 1998 10 23 MALA976216 1 19981014 A 2910 DSC252A40230 LINE DHAV DHC8 DHC8102 2809003 NM RT MLG BRAKE BROKEN A MALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 15 831MA 339 DURING DESCENT BOTH HYDRAULIC QUANTITIES WENT TO ZERO, PRESSURES REMAINED NORMAL. GEAR EXTENDED NORMALLY BUT PRESSURE O N NR 2 DROPPED TO ZERO, BUT RECOVERED TO 3000. DURING SHUT DOWN WHEN ENGINES WERE BROUGHT TO IDLE BOTH PRESSURES WENT T O ZERO. MAINTENANCE FOUND RIGHT INBOARD BRAKE LINE TO BE BROKEN AT THE LOWER FITTING. REMOVED AND INSTALLED A SERVICAB LE LINE. LEAK CHECK GOOD, SERVICED BOTH HYDRAULIC SYSTEMS. OPS CHECK GOOD. 2 H 7 2 4T RT A13NM 1998102300417 19981023 00417 EU 1998 10 23 MALA976217 1 19981016 A 3230 HP848430721 VALVE SAAB SF340 340B 7860101 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION DE DESCENT 1 GL 15 435XJ 435 LANDING GEAR WOULD NOT EXTEND NORMALLY FOLLOWED THE QRH. GEAR DID NOT EXTEND UNTIL THE EMERGENCY LANDING GEAR HANDLE WA S PULLED. THE FI OVERRIDE KNOB HAD TO BE PULLED, OBTAINED THREE GREEN DOWN AND LOCKED INDICATIONS. MAINTENANCE REPLACE D THE LANDING CONTROL VALVE AND RELAY 15GA. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998102300418 19981023 00418 EU 1998 10 23 MALA976218 1 19981015 A 3320 65111 BALLAST SAAB SF340 340B 7860101 EU LAVATORY FAILED A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 15 417XJ 340B417 CREW REPORTED AN ELECTRICAL SMELL (BURNT) IN THE LAV, THEY INVESTIGATED AND FOUND LIGHT BALLAST ARCING. CREW SHUT OFF L IGHTS IN LAV AND PROBLEM STOPPED. MAINTENACE DISCONNECTED POWER PLUG FOR BATHROOM BALLAST, REPLACED BALLAST AND RELAMPE D LAV LIGHTS IAW AMM 33-21-10. 2 L 7 2 4T RT A52EU 1998102300419 19981023 00419 1998 10 23 MALA976219 4 19981018 A 3414 6225353011 ASI SAAB SF340 340B 7860101 EU LT COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 233CH 233 CAPTAIN'S AIRSPEED INDICATOR FROZE UP AFTER TAKEOFF, STUCK UNTIL AFTER LANDING. RETURNED TO MSP. MAINTENANCE REPLACED THE LEFT ASI. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998102300420 19981023 00420 EU 1998 10 23 MALA976220 1 19981013 A 2421 31342003 GENERATOR SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA O OTHER J WARNING INDICATION CR CRUISE 1 GL 15 48XJ 048 LEFT AC GEN CAUTION LIGHT ILLUMINATED IN FLIGHT. PERFORMED QRH, NO RESET. AFTER LANDING MAINTENANCE REPLACED LEFT AC G EN THAT SEIZED AND SEPERATED AT BASE. INSTALLED SERVICEABLE AC GEN IAW SF340 MM 24-21-05, OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 1998102300421 19981023 00421 EU 1998 10 23 MALA976221 1 19981018 A 7603 C821466 CONTROL CABLE SAAB SF340 340B 7860101 EU LT ENGINE SEIZED A MALA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 GL 15 434XJ 434 LEFT POWER LEVER WAS STUCK AT 60 PERCENT TORQUE IN FLIGHT. CREW WAS UNABLE TO RETARD THROTTLE. LEFT ENGINE WAS SHUT DO WN AND SECURED IN COMPLIANCE WITH THE QRH:ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CABLE ASSEMBL Y POWER CONTROL FROM PCU TO HMU IAW SAAB AMM 76-10-00. GROUND RUN AND OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998102300422 19981023 00422 WP 1998 10 23 CALA9801965 1 19981017 A 3260 SWITCH DOUG DC9 DC982 3022082 WP LANDING GEAR MALFUNCTIONED A CALA O OTHER N FALSE WARNING CL CLIMB 1 SW 09 83872 49120 THE RED GEAR UNSAFE LIGHTS REMAINED ILLUMINATED AFTER TAKEOFF FROM SAT. THE GEAR WAS CYCLED AND THREE GREEN WERE RECEIV ED, BUT WARNING LIGHTS RETURNED TO RED AGAIN ON RAISING GEAR. THE FLIGHT WAS CONTINUED TO IAH AND WHEN GEAR WAS EXTENDE D ON APPROACH THREE GREEN GEAR SAFE LIGHTS ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE S1-89 SWITCH IAW MM 32-60- 1. GEAR OPERATION AND INDICATIONS CHECKED GOOD. 2 L 7 2 4F A6WE 1998102300423 19981023 00423 WP 1998 10 23 CALA9801966 1 19981016 A 5240 BEAM DOUG DC9 DC982 3022082 WP SERVICE DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 809NY 49263 INSPECTION FOUND A CRACK IN FORWARD SERVICE DOOR LOWER BEAM. THE LOWER BEAM WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998102300424 19981023 00424 WP 1998 10 23 CALA9801967 1 19981019 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1231 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 809NY 49263 INSPECTION FOUND LONGERON 24L CORRODED IN AFT CARGO COMPARTMENT AT STA 1231. REPAIRED IAW SRM 53-02, FIGURE 18. 2 L 7 2 4F A6WE 1998102300425 19981023 00425 WP 1998 10 23 CALA9801968 1 19981019 A 5350 CABLE DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJ A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 809NY 49263 THE AFT ENTRY DOOR TAILCONE RELEASE PULLED HIGH AT 25 POUNDS. THE CABLE AND CONDUIT WERE REPLACED AND AN ADJUSTMENT/TES T WAS PERFORMED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998102300426 19981023 00426 NM 1998 10 23 CALA9801969 1 19981017 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59302 23353 INSPECTION FOUND FLOORBEAM CORRODED AT NUTPLATES LOCATED IN E/E COMPARTMENT AT STA 312, RBL 3.5 TO 17. THE FLOORBEAM WA S REMOVED AND REPLACED IAW SRM 51-70-12, FIGURE 1. 2 L 7 2 4F RT A16WE 1998102300427 19981023 00427 NM 1998 10 23 CALA9801970 1 19981017 A 5523 657279974 SKIN BOEING 727 727224 1384076 NM RT ELEVATOR TAB DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT ELEVATOR CONTROL TAB TRAILING EDGE DELAMINATED. THE CONTROL TAB WAS REMOVED AND REPLACED IAW MM 27- 30-11. 2 L 7 3 4F A3WE 1998102300428 19981023 00428 NM 1998 10 23 CALA9801971 1 19981017 A 5752 652172648 TAB BOEING 727 727224 1384076 NM RT AILERON BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT WING OUTBOARD AILERON TAB BENT AT INBOARD TRAILING EDGE. THE AILERON TAB WAS REMOVED AND REPLACED I AW MM 27-10-41. 2 L 7 3 4F A3WE 1998102300429 19981023 00429 NM 1998 10 23 CALA9801972 1 19981017 A 5751 652176657 SKIN BOEING 727 727224 1384076 NM LT AILERON BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND LT OUTBOARD AILERON INBOARD END UPPER AND LOWER SKIN BENT. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-20-13. 2 L 7 3 4F A3WE 1998102300430 19981023 00430 NM 1998 10 23 CALA9801973 1 19981017 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 380-400 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT SEAT TRACK CORRODED AT FS 380-400. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-2,51-10-1, AND 51-10-2. 2 L 7 3 4F A3WE 1998102300431 19981023 00431 NM 1998 10 23 CALA9801974 1 19981017 A 5552 BRACKET BOEING 727 727224 1384076 NM LT ELEVATOR TAB WORN A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND LOOSE BOLTS AND WORN BOLT HOLES IN LT ELEVATOR TAB NR 1,3, AND 4 SUPPORT BRACKETS. THE TAB SUPPORT BRA CKETS WERE REMOVED AND REPLACED IAW MM 27-30-11. 2 L 7 3 4F A3WE 1998102300432 19981023 00432 WP 1998 10 23 9810259998 1 19980915 A 5320 ANGLE DOUG DC9 DC931 3022065 WP WING/FUSELAGE CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8934E 47143 DURING M CHECK, WING TO FUSELAGE ATTACH ANGLE WAS FOUND TO HAVE A 1.25 CRACK. REPAIRED PER EA 99-159285. 2 L 7 2 4F A6WE 1998102300433 19981023 00433 NE 1998 10 23 9810269750 2 19981016 A 7314 378200 FUEL PUMP DOUG DC9 DC941 302207N WP PWA JT8 JT8D11 52044 NE RT ENGINE FAILED A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 GL 01 750NW 35615 1572 47114 676209 DURING CRUISE AT 31,000 FEET, THE LEFT ENGINE EXPERIENCED A FLAMEOUT. ATTEMPTS TO RESTART ENGINE WERE UNSUCCESSFUL. CR EW PERFORMED ENGINE SHUTDOWN COM PROCEDURES. AIRCRAFT DIVERTED TO SDF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE FUEL PUMP AND FUEL CONTROL. ENGINE OPERATIONAL CHECK WAS OK AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A6WE E2EA 1998102300434 19981023 00434 WP 1998 10 23 9810271144 1 19981013 A 2910 LINE DOUG DC10 DC1040 3023508 WP LT MLG BRAKE FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 144JC 46753 ON DEPARTURE FROM HNL, LOST ALL HYDRAULIC FLUID IN NR 3 SYSTEM. FOLLOWED COM PROCEDURE AND RETURNED TO HNL. FLIGHT LAN DED WITHOUT INCIDENT. MAINTENANCE FOUND NR 4 BRAKE LINE CHAFED THROUGH. REPLACED BRAKE LINE AND SERVICED SYSTEM. OPER ATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998102300435 19981023 00435 NM 1998 10 23 UPS98227943 1 19981007 A 5400 WEB BOEING 727 727108C 1384039 NM BS 1376 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C WEB OVER NR 2 ENGINE CRACKED AT BS 1376 RT. NEW WEB FABRICATED AND INSTALLLED IAW DRAWING 65-17555. 2 L 7 3 4F A3WE 1998102300436 19981023 00436 NM 1998 10 23 UPS98227944 1 19980710 A 2760 65237993 QUADRANT BOEING 727 727108C 1384039 NM SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C NR 1 SPOILER QUADRANT IS CRACKED AT CABLE GUARD. NR 11 SPOILER QUADRANT REPLACED IAW 27-61-81 MM. 2 L 7 3 4F A3WE 1998102300437 19981023 00437 NM 1998 10 23 UPS98227945 1 19981005 A 5330 SKIN BOEING 727 727108C 1384039 NM BS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 380 S20R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 1. 2 L 7 3 4F A3WE 1998102300438 19981023 00438 NM 1998 10 23 UPS98227946 1 19981006 A 5755 SUPPORT BOEING 727 727108C 1384039 NM NR 5 SPOILER CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C SUPPORT CHANNEL FOR NR 5 SPOILER PANEL INB DOWNSTOP CASTING CRACKED. NR 5 SPOILER CHANNEL REPLACED IA W SRM 51-30-02. 2 L 7 3 4F A3WE 1998102300439 19981023 00439 NM 1998 10 23 UPS98227947 1 19981007 A 5347 SEAT TRACK BOEING 727 727108C 1384039 NM BS 870 BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C SEAT TRACK FLANGE BROKEN AT BS 870 RBL 24.75. SEAT TRACK SECTION REPLACED IAW SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 1998102300440 19981023 00440 NM 1998 10 23 UPS98227948 1 19981006 A 5512 PANEL BOEING 727 727108C 1384039 NM LT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C CORROSION ON LT HORIZ STAB LE PANEL NR 9103 INBD END. CUT OUT DAMAGED AREA IAW SRM 55-10-3 (FIG 2). C ARRIED OUT REPAIR IAW SRM 55-10-3 (FIG 2). 2 L 7 3 4F A3WE 1998102300441 19981023 00441 NM 1998 10 23 UPS98227949 1 19981016 A 3520 OXY MASK BOEING 727 72725C 138400H NM ROW 4ABC DEPLOYED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 951UP 19850 ROW 4ABC O2 CANISTER AND MASK DEPLOYED AND O2 GENERATOR USED. REMOVED AND REPLACED O2 GENERATOR AND REPLACED MASKS CKS OK IAW MM 35-00-00. 2 L 7 3 4F A3WE 1998102300442 19981023 00442 WP 1998 10 23 UPS98827924 1 19980922 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 902 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 FLOORBEAM, STA 902 CRACKED AT RT O/B FLANGE. ROUTED OUT DAMAGE, FABBED FILLER AND SHIM IAW REO-05489 REV A FABBED. REPAIR STRAP ON UPS N/R 809637, DRILLED AND INSTALLED IT, FILLER AND SHIM IAW DC8 SRM 51-1-20D, 51-1-24 AND REO 05489 REV A. 2 L 7 4 4F RT 4A25 1998102300443 19981023 00443 WP 1998 10 23 UPS98827925 1 19980910 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 110 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 FWD CARGO COMPARTMENT LONG 27 RT CORRODED AT STA 110. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED AND INSTALLED REPAIR IAW DWG DC08-53-0229. 2 L 7 4 4F RT 4A25 1998102300444 19981023 00444 WP 1998 10 23 UPS98827926 1 19980914 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 FWD PIT X-SLIDE DOOR TORQUE BOX Z FITTING CRACKED AT FS280 LONGERON 32R. REMOVED AND REPLACED Z FITT ING (BANANA FITTING) PT NR 3755827-501, REMOVED AND REPLACED FITTINGS PART NR 3754914-501 AND 3754914-501N. REMOVED AND REINSTALLED LONGERON END TIES 30R AND 32R. REMOVED LONGERON SECTION FS 250-280 L32R. INSTALL SPLICE AT FS 250 32R REI NSTALL LONG SECTION FS 250-280 L32R. 2 L 7 4 4F RT 4A25 1998102300445 19981023 00445 WP 1998 10 23 UPS98827927 1 19980914 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 AFT LOWER CARGO PIT STA 1220 BELOW CUSP AT LONG 21R FITTING CRACKED. BLEND OUT CRACK IAW DC8 SRM 51- 1-8. OUT OF LIMITS, PERFORMED HFEC IAW MIL-STD-271R TO VERIFY CRACK. REMOVED OLD FITTING. REMOVED AND REPLACED NEW FI TTING FROM BORING P/N 375496-502N, DRILLED HOLES IN NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1 -21, 51-1-20D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998102300446 19981023 00446 WP 1998 10 23 UPS98827928 1 19980915 A 5320 3755847 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 AFT PIT AFT SIDE OF TORQUE BOX BOTTOM AFT CORNER OF CARGO DOOR FRAME, TORQUE BOX FITTING CRACKED AT 2 PLACES (BANANA FTGS). REMOVED AND REPLACED FITTINGS, STA 1220 AND 1228 IAW DC8 SRM 51-1-20 D, 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1998102300447 19981023 00447 WP 1998 10 23 UPS98827929 1 19980907 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 711 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 RT WING L/E CORRODED AT XRS 711 FAST HOLES. CUT OUT CORROSION, FABBED REPAIR DOUBLER IAW DC8 SRM 57- 2-1 ALODINED AND PRIMED REPAIR IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 51 -1-20D, 51-1-21 AND 51-1-21A. 2 L 7 4 4F RT 4A25 1998102300448 19981023 00448 WP 1998 10 23 UPS98827930 1 19980923 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 680-702 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 INTERCOSTAL, FS 680-702 CORRODED RBL 20. REMOVED CORRODED WEB FABBED AND INSTALLED IAW DAC DWG 57732 75, DC8 SRM 51-1-21, 51-1-8. 2 L 7 4 4F RT 4A25 1998102300449 19981023 00449 WP 1998 10 23 UPS98827932 1 19980914 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 CORROSION AROUND NUTPLATE HOLES INSIDE X-SLIDE DOOR TORQUE BOX FS 280 LONGERON 31-32R. REMOVED CORRO SION IAW DC8 SRM 51-1-8. FOUND FITTING TO BE OUT OF LIMITS. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1 -21. 2 L 7 4 4F RT 4A25 1998102300450 19981023 00450 WP 1998 10 23 UPS98827933 1 19980914 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 STA 902 X.64 FLOORBEAM CORRODED. REMOVED 2 CORRODED ANGLES, DRILLED AND INSTALLED REPLACEMENT ANGLES IAW REO 05483, DC8 SRM 51-1-20D, 51-1-8. 2 L 7 4 4F RT 4A25 1998102300451 19981023 00451 WP 1998 10 23 UPS98827934 1 19980914 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 980 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 WW PRESS PNL AREA, STA 980 AND XCW 64L FITTING IS CRACKED. REMOVED CRACKED FITTING, FITTING PN NR 46 47365-1, FABBED ON NR 50004 LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51- 1-17. ALODINED AND PRIMED FITTING MATING SURFACES IAW DC8 SRM 51-1-8. 2 L 7 4 4F RT 4A25 1998102300452 19981023 00452 WP 1998 10 23 UPS98827935 1 19980909 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1580 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 BOTTOM OF FRAME AT STA 1580 LT IS BENT AND CRACKED. REMOVED EXISTING SHEAR TIE, AND FABRICATED NEW I AW REO 05454, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW REO-05454. 2 L 7 4 4F RT 4A25 1998102300453 19981023 00453 WP 1998 10 23 UPS98827936 1 19980917 A 5320 5706319501 EXTRUSION DOUG DC8 DC871F 302199D WP TAIL CONE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 TAIL CONE, L36 EXTRUSION CORRODED, STA 1890-1940. REMOVED AND REPLACED EXTRUSION IAW DC8 SRM 51-1-24 . 2 L 7 4 4F RT 4A25 1998102300454 19981023 00454 WP 1998 10 23 UPS98827937 1 19980922 A 5330 SKIN DOUG DC8 DC871F 302199D WP TAIL CONE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 TAILCONE LT LOWER SKIN CORRODED. REMOVED SKIN, FABBED NEW SKIN IAW DAC DWG 5764650. INSTALLED SKIN IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998102300455 19981023 00455 WP 1998 10 23 UPS98827938 1 19980921 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1971 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 TAILCONE FRAME, STA 1971 CORR, BLO TO RBL 6. REMOVED FRAME SECTION, FABBED NEW SECTION, AND SPLICES IAW DC8 SRM 5 3-2-0 AND DAC DWG 5704650. INSTALLED REPAIR IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998102300456 19981023 00456 WP 1998 10 23 UPS98827939 1 19980917 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1933 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 CRACKED TAIL CONE FRAME, STA 1933 RIGHT OF L36. REMOVED DAMAGE, FABBED REPAIR FRAME AND SPLICES IAW DC8S RM 53-2-0 FI G 2, 51-3-2. INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2, 51-1-20D AND 51-1-8. 2 L 7 4 4F RT 4A25 1998102300457 19981023 00457 WP 1998 10 23 UPS98827940 1 19980914 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1920 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 LT FRAME IN TAILCONE CRACKED AT CROSS STIFFENER FS 1920. STOP DRILLED FRAME, FABBED DOUBLER IAW DC8 SRM 53-2-0. INSTALLED DOUBLER IAW DC8 SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998102300458 19981023 00458 WP 1998 10 23 UPS98827941 1 19980917 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1912-1950 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 TAILCONE RT SKIN CORRODED, L33R TO L36 FS 1912-1950. REMOVED SKIN, FABBED AND INSTALLED NEW ONE IAW DAC DWG 5644500 AND DC8 SRM 51-1-8, 51-1-21. 2 L 7 4 4F RT 4A25 1998102300459 19981023 00459 WP 1998 10 23 ABXA9800916 1 19981019 A 5250 AR25291GR41 LATCH DOUG DOUG DC9 DC931 3022065 WP COCKPIT DOOR LOOSE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 938AX 47009 COCKPIT DOOR WAS JAMMED. SECURED HARDWARE ON DOOR LATCH ASSY. 2 L 7 2 4F A6WE 1998102300460 19981023 00460 NM 1998 10 23 VNAA9810014 1 19981015 A 6120 APS3D10001000A SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 442JS 73403 3060 A LEFT HAND PROPELLER LOW OIL PRESSURE WARNING MESSAGE ILLUMINATED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETU RNED TO THE GATE. PSA MAINTENANCE WAS DISPATCHED FROM PIT TO REPAIR THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED T HE LEFT HAND PROPELLER OIL PRESSURE SWITCH, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-12. OPERATIONAL CHECKS AND LEAK WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998102300461 19981023 00461 NM 1998 10 23 VNAA9810011 1 19981016 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FWD FUSELAGE BIRD STRIKE A VNAA K NONE C F.O.D. AP APPROACH 1 GL 07 459PS 3070 DURING THE APPROACH INTO PIT, THE AIRCRAFT WAS STRUCK BY A BIRD ON THE FUSELAGE BELOW THE LEFT HAND FRONT WINDSCREEN. T HE AIRCRAFT CONTINUED THE APPROACH TO PIT AND PERFORMED A NORMAL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT FOR DAMAGE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-57-07. NO DAMAGE WAS NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998102300462 19981023 00462 NM 1998 10 23 VNAA9810012 1 19981017 A 3240 3900001101 ACCUMULATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARKING BRAKE REQD SERVICE A VNAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 07 439JS 74254 3057 DURING THE CLIMB FROM GSP, THE CREW RECEIVED AN EMERGENCY PARK BRAKE ACCUMULATOR PRESSURE LOW WARNING MESSAGE. THE CREW COMPLIED WITH THE CHECKLIST, AND RETURNED TO GSP AND LANDED WITHOUT ANY FURTHER PROBLEMS. OUTSTATION MAINTENANCE INSPE CTED AND SERVICED THE EMERGENCY PARK BRAKE ACCUMULATOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-12-10. OPERATI ONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998102300463 19981023 00463 1998 10 23 VNAA9810013 4 19981018 A 3418 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E/E COMPT LOOSE A VNAA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 07 440JS 3058 DURING THE TAXI PRIOR TO TAKEOFF, A STICK PUSHER FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED, CLEANED, AND RESEATED THE 17VE CANNON PLUGS, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 31-12- 13. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998102300465 19981023 00465 NE 1998 10 23 TWAA9816901 2 19981019 A 7314 3782017 FUEL PUMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9 52048 NE LT ENGINE FAILED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CL CLIMB 1 CE 05 932L 47669 3952 NR 2 ENGINE HAD NO RESPONSE TO THROTTLE MOVEMENT. RETURNED TO BDL. ENGINE WAS SHUT DOWN ON APPROACH. REPLACED FUEL PU MP DUE TO HIGH STAGE FAILURE. CHECK-C 4-24-98 STL. 2 L 7 2 4F 4 F A6WE E2EA 1998102300466 19981023 00466 NM 1998 10 23 RAAA98B1091 1 19981020 A 3530 4566M37B042NM PBE BOEING 727 72722C 138400F NM COCKPIT VACUUM LOST A RAAA K NONE O OTHER CR CRUISE 1 AL 03 831RV 19093 FLIGHT CREW REPORTED COCKPIT PBE INDICATOR PROTRUDES IN FLIGHT. CHANGED PBE DUE POUCH VACUUM LOST. 2 L 7 3 4F A3WE 1998102300467 19981023 00467 EU 1998 10 23 QXEA9801448 1 19980930 A 5230 SILL FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 LOWER FORWARD REAR CARGO DOOR SILL IS DENTED AND BENT ALONG 8 OF FORWARD EDGE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998102300468 19981023 00468 EU 1998 10 23 QXEA9801449 1 19980914 A 5320 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO COMPT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 REAR CARGO BAY FLOOR FRAME 13815B HAS A CRACKED CASTELLATION BETWEEN STRINGERS 73 AND 72. REPAIRED IAW FOKKER SRM 53-02 -13 PAGE 5 FIGURE 3. 2 L 7 2 4F RT A20EU 1998102300469 19981023 00469 EU 1998 10 23 QXEA9801450 1 19980921 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 CENTER CARGO DOOR APERTURE CRACKED UNDER DOOR BRACKET. REPAIRED IAW FOKKER SRM 53-02-16 FIGURE 1 PAGE 3. 2 L 7 2 4F RT A20EU 1998102300470 19981023 00470 EU 1998 10 23 QXEA9801451 1 19980923 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME ON FORWARD END OF AFT CARGO DOOR IS CRACKED AND TORN. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998102300471 19981023 00471 EU 1998 10 23 QXEA9801452 1 19980923 A 5230 RIB FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 RIB ALONG FORWARD END OF AFT CARGO DOOR IS CRACKED. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998102300472 19981023 00472 EU 1998 10 23 QXEA9801453 1 19980930 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 AFT CARGO DOOR AFT JAMB, APPROXIMATELY 8.5 UP FROM LOWER CORNER SHARP DENT APPROXIMATELY .050 DEEP. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998102300473 19981023 00473 EU 1998 10 23 QXEA9801454 1 19980929 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 AFT CARGO DOOR, AFT JAMB APPROXIMATELY 17 INCHES DOWN FROM TOP OF DOORWAY THERE IS A DEEP DENT APPROXIMATELY .145 INCH D EEP. REPLACED DOOR JAMB. 2 L 7 2 4F RT A20EU 1998102300474 19981023 00474 EU 1998 10 23 QXEA9801455 1 19981005 A 5753 FAIRING FOKKER F28 F28MK4000 4990810 EU TE FLAP WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 VERTICAL TRACK ON FLAP FAIRING PANEL 92N HAS DEEP WEAR. REPAIRED IAW FOKKER MM 27-50-6, PAGE 802 AND HORIZON AIR EA 4-5 7-101. 2 L 7 2 4F RT A20EU 1998102300475 19981023 00475 EU 1998 10 23 QXEA9801456 1 19980920 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 3870-4175 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 STRINGER NUMBER 68 IS CRACKED BETWEEN FRAME 3870 AND 4175. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 8 PARAGRAPH 3C. 2 L 7 2 4F RT A20EU 1998102300476 19981023 00476 EU 1998 10 23 QXEA9801457 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15203 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME 15205 HAS A CRACKED CLIP AT STRINGER 50. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300477 19981023 00477 EU 1998 10 23 QXEA9801458 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME 14755 HAS A CRACKED CLIP AT STRINGER 26. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300478 19981023 00478 EU 1998 10 23 QXEA9801459 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME 14755 HAS A CRACKED CLIP AT STRINGER 49. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300479 19981023 00479 EU 1998 10 23 QXEA9801460 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME 13815A HAS A CRACKED CLIP AT STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300480 19981023 00480 EU 1998 10 23 QXEA9801461 1 19980929 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS CORROSION ALONG STRINGER 39 BETWEEN FRAMES 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06 PAGE 3 FIGURE 1. 2 L 7 2 4F RT A20EU 1998102300481 19981023 00481 EU 1998 10 23 QXEA9801462 1 19980923 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS CORROSION ALONG STRINGER 38 BETWEEN FRAMES 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06 PAGE 3 AND SRM 51-3 1-01. 2 L 7 2 4F RT A20EU 1998102300482 19981023 00482 EU 1998 10 23 QXEA9801463 1 19980925 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS CORROSION ALONG STRINGER 36 BETWEEN FRAMES 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-02-06 FIGURE 1 SECTION E- E. 2 L 7 2 4F RT A20EU 1998102300483 19981023 00483 EU 1998 10 23 QXEA9801464 1 19980925 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME 4900-5305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS CORROSION ALONG STRINGER 34 BETWEEN FRAMES 4900 AND 5305. REPAIRED IAW FOKKER SRM 53-03-06 PAGE 3 FIGURE 2. 2 L 7 2 4F RT A20EU 1998102300484 19981023 00484 EU 1998 10 23 QXEA9801465 1 19980922 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FLOOR STRUCTURE SUPPORT FOR NR 1 GALLEY IS CRACKED AND BROKEN OFF AT END OF SUPPORT ON 4TH SUPPORT INBOARD FROM CENTERLI NE STATION BL 0. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998102300485 19981023 00485 EU 1998 10 23 QXEA9801466 1 19980922 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FLOOR STRUCTURE SUPPORT UNDER NR 1 GALLEY IS MISSING A NUT PLATE AND IS CRUSHED DOWN AT END ON 5TH SUPPORT INBOARD FROM CENTERLINE STATION BL 0. REPAIRED IAW HORIZON AIR EA 4-53-560. 2 L 7 2 4F RT A20EU 1998102300486 19981023 00486 EU 1998 10 23 QXEA9801467 1 19980922 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU CABIN DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FLOOR STRUCTURE SUPPORT UNDER NR 1 GALLEY IS CRACKED AT END OF SUPPORT AND END NUT PLATE IS LOOSE AND FALLING OFF. REPA IRED IAW HORIZON AIR EA 4-53-560. 2 L 7 2 4F RT A20EU 1998102300487 19981023 00487 EU 1998 10 23 QXEA9801468 1 19980922 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU CABIN CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FLOOR STRUCTURE SUPPORT UNDER NR 1 GALLEY IS CRACKED ON 3RD SUPPORT FROM CENTERLINE STATION BL 0. REPAIRED IAW HORIZON EA 4-53-560. 2 L 7 2 4F RT A20EU 1998102300488 19981023 00488 EU 1998 10 23 QXEA9801469 1 19980911 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS A CRACK ON LOWER EDGE OF CLIP AT FRAME 7305A BETWEEN STRINGERS 39 AND 40. REPAIRED IAW FOKKER SRM 53-02-13 PAG E 4. 2 L 7 2 4F RT A20EU 1998102300489 19981023 00489 EU 1998 10 23 QXEA9801470 1 19980911 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS A CRACK ON LOWER EDGE OF CLIP AT FRAME 7305A BETWEEN STRINGERS 40 AND 41. REPAIRED IAW FOKKER SRM 53-02-13 PAG E 4. 2 L 7 2 4F RT A20EU 1998102300490 19981023 00490 EU 1998 10 23 QXEA9801471 1 19980917 A 5210 BUMPER FOKKER F28 F28MK4000 4990810 EU PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 MAIN CABIN DOOR BUMPER AREA HAS CRACKS VISIBLE FROM INSIDE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998102300491 19981023 00491 EU 1998 10 23 QXEA9801472 1 19980913 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS A CRACK IN CLIP AT FRAME 6305 BETWEEN STRINGERS 29 AND 30. REPAIRED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 1998102300492 19981023 00492 EU 1998 10 23 QXEA9801473 1 19981007 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 3820&3870 MISDRILLED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BOX FRAME 3820/3870 HAS MISDRILLED HOLE IN INBOARD AFT FLANGE OF TORQUE BOX. REPAIRED IAW FOKKER SRM 51-31-04. 2 L 7 2 4F RT A20EU 1998102300493 19981023 00493 EU 1998 10 23 QXEA9801474 1 19980921 A 5510 STIFFENER FOKKER F28 F28MK4000 4990810 EU LT HORIZ STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 LEFT-HAND SIDE HORIZONTAL STAB FRONT SIDE OF AFT SPAR STIFFENER IS CRACKED INBOARD OF RIB 1265. REPAIRED IAW FOKKER SRM 55-01-01 PAGE 6 PARAGRAPH 5B. 2 L 7 2 4F RT A20EU 1998102300494 19981023 00494 EU 1998 10 23 QXEA9801475 1 19980930 A 5320 FRAME FOKKER F28 F28MK4000 4990810 EU SERV DOORWAY MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 491US 11156 WEB OF FRAME 3870 NEXT TO SERVICE/EMERGENCY DOOR HAS 3 SETS OF BELOW MINIMUM PITCH RIVET HOLES. REPAIRED IAW HORIZON AI R EA 4-53-568. 2 L 7 2 4F RT A20EU 1998102300495 19981023 00495 EU 1998 10 23 QXEA9801476 1 19981004 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WS 7900-8056 DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS A LARGE AREA OF DELAMINATION ON TOP SURFACE OF RIGHT-HAND WING NEAR TRAILING EDGE BETWEEN STATION 7900 AND 8056 . REPAIRED IAW FOKKER SRM 51-70-00 PARAGRAPH 7B (9-10). 2 L 7 2 4F RT A20EU 1998102300496 19981023 00496 EU 1998 10 23 QXEA9801477 1 19981004 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 RIGHT-HAND WING OUTBOARD FLAP BOTTOM SKIN, HAS 2 CREASES AND 1 DENT NEAR TRAILING EDGE AT STATION 8000. REPAIRED IAW FO KKER SRM 51-70-00 PAGE 3, B. 2 L 7 2 4F RT A20EU 1998102300497 19981023 00497 EU 1998 10 23 QXEA9801478 1 19981004 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP VANE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 RIGHT-HAND INBOARD FLAP VANE HAS IMPACT DAMAGE ON TRAILING EDGE LOWER SKIN. REPAIRED IAW FOKKER SRM 51-70-0 METHOD 1 PA RAGRAPH 7C PAGES 12, 13. 2 L 7 2 4F RT A20EU 1998102300498 19981023 00498 EU 1998 10 23 QXEA9801479 1 19981001 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU RT TE FLAP VANE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 RIGHT-HAND INBOARD FLAP VANE HAS DEEP CHAFE APPROXIMATELY 6 TO 8 INCH LENGTH AND .010 TO .020 DEEP. REPAIRED IAW FOKKER SRM 51-31-05 FIGURE 8 PAGE 16-17. 2 L 7 2 4F RT A20EU 1998102300499 19981023 00499 EU 1998 10 23 QXEA9801480 1 19981001 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU RT WING DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 RIGHT-HAND WING NOSE AT STATION 1700 HAS A DEEP DENT MEASURED AT 0.87. REPAIRED IAW FOKKER SRM 51-70-10 PARAGRAPH 3. 2 L 7 2 4F RT A20EU 1998102300500 19981023 00500 EU 1998 10 23 QXEA9801481 1 19980930 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 DENT IN SKIN 1 INCH FORWARD OF DOOR PANEL 95A. REPAIRED IAW FOKKER SRM 53-02-17 PAGE 3. 2 L 7 2 4F RT A20EU 1998102300501 19981023 00501 EU 1998 10 23 QXEA9801495 1 19981012 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BACK UP ANGLE AT THE BASE OF THE VERTICAL STABILIZER LEADING EDGE HAS A SMALL CRACK. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998102300502 19981023 00502 EU 1998 10 23 QXEA9801496 1 19981009 A 2760 BEARING FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 LEFT-HAND SPEED BRAKE LEVER ASSEMBLY LOWER BEARING IS WORN. REPAIRED IAW HORIZON AIR EA 4-55-93. 2 L 7 2 4F RT A20EU 1998102300503 19981023 00503 EU 1998 10 23 QXEA9801497 1 19981009 A 5755 BEARING FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BEARING LOOSE IN FITTING FOR SPEED BRAKE LEVER ATTACHMENT AT LEFT -HAND LOWER POSITION. REPAIRED IAW FOKKER SRM PAGE 21 5, E3 FIGURE 9. 2 L 7 2 4F RT A20EU 1998102300504 19981023 00504 EU 1998 10 23 QXEA9801498 1 19981009 A 5755 BEARING FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BEARING LOOSE IN FITTING FOR SPEED BRAKE LEVER ATTACHMENT AT LEFT-HAND UPPER POSITION. REPAIRED IAW FOKKER SRM PAGE 215 , E3 FIGURE 9. 2 L 7 2 4F RT A20EU 1998102300505 19981023 00505 EU 1998 10 23 QXEA9801499 1 19981012 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BETWEEN FRAMES 19976 AND 20075 BETWEEN STRINGERS 36 AND 37 CRACKS ARE NOTED ALONG RIVET LINE FOR VERTICAL STABILIZER CON NECTION ANGLES. REPAIRED IAW HORIZON AIR EA 4-59-567. 2 L 7 2 4F RT A20EU 1998102300506 19981023 00506 EU 1998 10 23 QXEA9801500 1 19981012 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 BETWEEN FRAMES 19976 AND 20075 BETWEEN STRINGERS 38 AND 39 CRACKS ARE NOTED ALONG RIVET LINE FOR VERTICAL STABILIZER CON NECTION ANGLE. REPAIRED IAW HORIZON AIR EA 4-53-567. 2 L 7 2 4F RT A20EU 1998102300507 19981023 00507 EU 1998 10 23 QXEA9801501 1 19981003 A 5320 WEB FOKKER F28 F28MK4000 4990810 EU LEFT SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 LEFT-HAND TENSION MEMBER BOTTOM INBOARD WEB HAS DEEP SCRATCHES IN 3 PLACES. REPAIRED IAW HORIZON AIR EA 4-53-556. 2 L 7 2 4F RT A20EU 1998102300508 19981023 00508 EU 1998 10 23 QXEA9801502 1 19981001 A 2760 FITTING FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 SPEED BRAKE LEFT-HAND LEVER ASSEMBLY LOWER BUSHING HOLE FOR STRAIGHT PUSHROD IS ENLARGED AND OUT OF ROUND. REPAIRED IAW HORIZON AIR EA 4-55-86. 2 L 7 2 4F RT A20EU 1998102300509 19981023 00509 EU 1998 10 23 QXEA9801503 1 19981001 A 5755 FITTING FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 SPEED BRAKE LEFT-HAND LEVER UPPER BUSHING HOLE FOR STRAIGHT PUSHROD IS ENLARGED AND OUT OF ROUND. REPAIRED IAW HORIZON AIR EA 4-55-86. 2 L 7 2 4F RT A20EU 1998102300510 19981023 00510 EU 1998 10 23 QXEA9801504 1 19981001 A 2760 LEVER FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 SPEED BRAKE RIGHT-HAND LEVER ASSEMBLY ON AFT END OF UPPER SURFACE OF LOWER EAR ADJACENT TO STRAIGHT PUSHROD BOLT HOLE CH AFED. REPAIRED IAW HORIZON AIR EA 4-55-86. 2 L 7 2 4F RT A20EU 1998102300511 19981023 00511 EU 1998 10 23 QXEA9801505 1 19980926 A 5755 FITTING FOKKER F28 F28MK4000 4990810 EU SPEED BRAKE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 SPEED BRAKE CROSSHEAD ASSEMBLY DAMAGE TO RIGHT-HAND PUSHROD BOLT HOLE AREA, LOWER EAR OF CROSSHEAD. REPAIRED IAW HORIZO N AIR EA 4-55-85. 2 L 7 2 4F RT A20EU 1998102300512 19981023 00512 EU 1998 10 23 QXEA9801506 1 19981001 A 2760 FITTING FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 SPEED BRAKE LEFT-HAND LEVER ASSEMBLY VARIOUS DAMAGE EXISTS ON AFT END UPPER AND LOWER EARS ADJACENT TO STRAIGHT PUSHROD BOLT HOLE. REPAIRED IAW HORIZON AIR EA 4-55-86. 2 L 7 2 4F RT A20EU 1998102300513 19981023 00513 EU 1998 10 23 QXEA9801507 1 19981012 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FRAME19833-19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 CRACKS EXTENDING FROM RIVETS THROUGH FUSELAGE AT VERTICAL STABILIZER CONNECTING ANGLE BETWEEN FRAMES 19833 AND 19976 ON LEFT-HAND OUTBOARD OF STRINGER 36. REPAIRED IAW HORIZON AIR EA 4-53-567. 2 L 7 2 4F RT A20EU 1998102300514 19981023 00514 EU 1998 10 23 QXEA9801508 1 19981012 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME19832-19976 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 CRACK EXTENDING FROM RIVET AFT OF PREVIOUS REPAIR RIGHT-HAND OUTBOARD OF STRINGER 39 BETWEEN FRAME 19832 AND 19976 AT VE RTICAL STABILIZER CONNECTING ANGLE. REPAIRED IAW HORIZON AIR EA 4-53-567. 2 L 7 2 4F RT A20EU 1998102300515 19981023 00515 EU 1998 10 23 QXEA9801509 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 TWO WORKING RIVETS AND POSSIBLE CRACK IN RADIUS OF CLIP AT FRAME 16-2 AND STRINGER 43. REPAIRED IAW FOKKER SRM 53-10-5 PAGE 603 AND SRM 51-31-01 AND 53-10-05 PAGE 601. 2 L 7 2 4F RT A20EU 1998102300516 19981023 00516 EU 1998 10 23 QXEA9801510 1 19981012 A 5755 BUSHING FOKKER F28 F28MK4000 4990810 EU RT SPEED BRAKE WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 RIGHT-HAND SPEED BRAKE A FRAME PUSHROD FORWARD BUSHINGS WORN. REPAIRED IAW FOKKER SRM 27-61-05 PAGE 402 PARAGRAPH 3 AND HORIZON AIR EA 4-55-96. 2 L 7 2 4F RT A20EU 1998102300517 19981023 00517 EU 1998 10 23 QXEA9801511 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 6305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 THERE IS A CRACK IN CLIP AT FRAME 6305 BETWEEN STRINGER 43 AND 44. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300518 19981023 00518 EU 1998 10 23 QXEA9801512 1 19981001 A 5320 JAMB FOKKER F28 F28MK4000 4990810 EU LT EMER EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 LEFT-HAND FORWARD OVERWING EMERGENCY EXIT DOOR APERTURE HAS A TWO INCH CRACK IN THE SKIN AT THE LOWER FORWARD CORNER. R EPAIRED IAW HORIZON AIR EA 4-53-550. 2 L 7 2 4F RT A20EU 1998102300519 19981023 00519 EU 1998 10 23 QXEA9801513 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME 12405 HAS A CRACKED CLIP AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300520 19981023 00520 EU 1998 10 23 QXEA9801514 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME 12875 HAS A CRACKED CLIP AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300521 19981023 00521 EU 1998 10 23 QXEA9801515 1 19980910 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 FRAME 13815 HAS A CRACKED CLIP AT STRINGER 19. REPAIRED IAW FOKKER SRM 51-31-01 AND 53-02-13 PAGE 4. 2 L 7 2 4F RT A20EU 1998102300522 19981023 00522 EU 1998 10 23 QXEA9801516 1 19980920 A 5321 FLOOR FOKKER F28 F28MK4000 4990810 EU COCKPIT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 COCKPIT FLOOR HAS DENT WITH CRACK 4 INCHES LONG TWO INCHES OFF OF CAPTAINS CONTROL COLUMN BASE COVER. REPAIRED IAW FOKK ER SRM 53-02-01 PAGE 11 FIGURE 9 AND 51-31-01. 2 L 7 2 4F RT A20EU 1998102300523 19981023 00523 EU 1998 10 23 QXEA9801517 1 19980615 A 5320 FRAME FOKKER F28 F28MK4000 4990810 EU LT D WINDOW CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 491US 11156 LEFT-HAND D WINDOW FRAME HAS A CRACK THROUGH THE TOP NR 3 HOLE APPROXIMATELY 1 INCH LONG. REPAIRED IAW FOKKER SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1998102300524 19981023 00524 NM 1998 10 23 98FDEA00657 1 19981020 A 5230 65561261 FRAME BOEING 727 727227 1384078 NM CARGO DOOR MISDRILLED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 161 UPON REMOVAL OF #2 CARGO DOOR SEAL RETAINER, FOUND MISDRILLED HOLE IN FRAME AT BS 990, STR 26 R/H. ** S/D ** INSTALLED FASTENERS IN OPEN HOLES AS PER FEDEX SRM 51-30-02. 2 L 7 3 4F A3WE 1998102300525 19981023 00525 NM 1998 10 23 98FDEA00658 1 19981020 A 5320 651627910 BEAM BOEING 727 727227 1384078 NM BS 760-850 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 212 WHILE WORKING NR 199 FOUND CORROSION ON LONGITUDINAL BEAM BS 760 TO 850, LBL 25, WL 205. *S/D* REMOVED AND REP LACED LONG BEAM BS 760 TO 850, LBL 25, WL 208 PER FEDEX SRM 51-30-2 AND BOEING DWG 65-16279. 2 L 7 3 4F A3WE 1998102300526 19981023 00526 NM 1998 10 23 98FDEA00659 1 19981020 A 5314 65564413 KEEL BEAM BOEING 727 727227 1384078 NM BS 950-967 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 152 CORROSION ON OUTBOARD FLANGE OF L/H KEEL BEAM BS 950F+17. ** S/D ** REPAIRED L/H KEEL BEAM PER FEDEX SR 27-5 3-023 & FEDEX SRM 53-10-4 AT BS 950F+17. 2 L 7 3 4F A3WE 1998102300527 19981023 00527 NM 1998 10 23 98FDEA00660 1 19981021 A 3260 BULB BOEING 727 72727C 138400J NM RT MLG FAILED A FDEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 25 145FE 19109 ON APPROACH, WHEN GEAR HANDLE PUT DOWN BOTH LIGHTS IN RIGHT MAIN GEAR IND BURN OUT. DID GO-AROUND AND REPLACED BOTH BUL BS, WORKED OK. CHECKED MAIN GEAR IND LIGHTS, CHECKS OK. 2 L 7 3 4F A3WE 1998102300528 19981023 00528 NM 1998 10 23 98FDEA00661 1 19981021 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 540 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 UPPER LOBE CABIN, CORROSION ON UPPER AND LOWER SIDE OF FWD TOP FLOORBEAM FLANGE AT BS 540 RBL 10, 5 INCHES FROM CENTER O F A/C. REMOVED CORROSION PER SRM 51-10-6, BEYOND LIMITS. INSTALLED DOUBLER, ACCOMP PER AARD 53-10-01-1 FIG 2. 2 L 7 3 4F A3WE 1998102300529 19981023 00529 NM 1998 10 23 98FDEA00662 1 19981021 A 5313 STRINGER BOEING 727 72722 1384002 NM BS 480 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 STR 25R, BS 480 CRACKED AT BRACKET ATTACHMENT. REPAIRED STR 25R AT BS 480 PER SRM 53-10-3. 2 L 7 3 4F A3WE 1998102300530 19981023 00530 NM 1998 10 23 98FDEA00663 1 19981020 A 5311 FRAME BOEING 727 72722 1384002 NM BS 480 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 CRACK IN FRAME WEB BS 480, BELOW STR 26R. REPAIRED CRACK IN FRAME WEB BY STOP DRILL AND INSTALL OF DOUBLER PER SRM 53-1 0-4. 2 L 7 3 4F A3WE 1998102300531 19981023 00531 NM 1998 10 23 98FDEA00664 1 19981020 A 5315 FLOORBEAM BOEING 727 727233 138408A NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 219FE 21102 CORROSION ON TOP FLANGE AND BOTTOM OF TOP FLANGE ON FLOORBEAM BS 1110, LBL 65. REPAIRED FLOORBEAM AT BS 1110, LBL 65 PE R SRM 53-10-8 AND EA 7-5310-29647. 2 L 7 3 4F RT A3WE 1998102300532 19981023 00532 NM 1998 10 23 98UAL900495 1 19981009 A 2133 OUTFLOW VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE CABIN FAILED A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 777UA 26916 AFTER DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO FIELD. *S/D* AIRCRAFT WAS OPERATING WITH AFT OUT FLOW VALVE AT SEVEN PERCENT OPEN POSITION PER THE MEL DUE TO FAULTY LEFT HAND DC MOTOR. SUSPECT WHILE ACCOMPLISHING FOR WARD OUTFLOW VALVE MAINTENANCE MESSAGES CHECK AND ASSOCIATED ACTIVITIES, THE AFT OUTFLOW VALVE WAS SELECTED TO FULL OPEN POSITION. WHEN AFT OUTFLOW VALVE CIRCUIT BREAKERS WERE ONCE AGAIN PULLED PRIOR TO DISPATCH, THE AFT OUTFLOW VALVE REMA INED IN THE OPEN POSITION INHIBITING FULL PRESSURIZATION OF THE AIRCRAFT. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998102300533 19981023 00533 NM 1998 10 23 98UAL900496 1 19981010 A 3350 BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE AFT AIRSTAIR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7266U 21413 AFT AIRSTAIR AND OVERWING EMERGENCY EXIT LIGHTS AT 17F DID NOT ILLUMINATE WHEN USED. REPLACED BATTERIES IN LIGHT UNIT. 2 L 7 3 4F 4 F A3WE E2EA 1998102300534 19981023 00534 NM 1998 10 23 98UAL900497 1 19981010 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FIRE A UALA O OTHER A FLAME/FIRE CR CRUISE 1 WP 29 661UA 27158 CREW REPORTED FIRE IN FWD OVEN. FIRE CONTAINED WITHIN OVEN AND OVEN SECURED. 2 L 7 2 4F 4 F RT A1NM E24NE 1998102300535 19981023 00535 1998 10 23 98UAL900498 4 19981012 A 2565 7A14691 TUBE BF GOODRICH 7A14701 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE/RAFT TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 185UA 61495 G073 25395 SLIDE/RAFT FAILED PROOF TEST DURING UNIT OVERHAUL IN HOME SHOP, CAUSING A 6 FOOT TEAR IN THE TOP TUBE CENTER CROSSOVER T UBE. CAUSE COULD NOT BE DETERMINED. SENT UNIT TO VENDOR FOR EVALUATION AND REPAIR. 2 L 7 4 4F 4 F RT A20WE E24NE 1998102300536 19981023 00536 NM 1998 10 23 98UAL900499 1 19981009 A 2910 50604 SHUTTLE VALVE BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE A HYD SYST FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 983UA 21641 LOST SYSTEM A HYDRAULIC PRESSURE AND HYDRAULIC FLUID. *S/D* REPLACED SHUTTLE VALVE ON FWD BULKHEAD OF LT WHEEL WELL. L EAK CHECKS GOOD. MAINTENANCE TECHNICIAN STATES THAT A PLUG IN THE CAPPED OFF PORT FAILED. 2 L 7 2 4F 4 F A16WE E2EA 1998102300537 19981023 00537 NM 1998 10 23 98UAL900501 1 19981015 A 2120 AIR DIST BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE COCKPIT ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 WP 29 7271U 21418 DURING DESCENT, ELECTRICAL BURNING SMELL NOTICED IN COCKPIT INTERMITTENTLY. *S/D* MAINTENANCE INSPECTED COCKPIT, FORWA RD ACCESSORY COMPARTMENT, E & E COMPARTMENT AND FOUND NO EVIDENCE OR ODOR OF BURNED WIRING OR EQUIPMENT. NO FURTHER PRO BLEMS REPORTED. 2 L 7 3 4F 4 F A3WE E2EA 1998102300538 19981023 00538 NM 1998 10 23 98UAL900502 1 19981014 A 2760 CONTROL MECH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SPEED BRAKES MALFUNCTIONED A A UALA O OTHER F FLT CONT AFFECTED DE DESCENT 1 WP 29 7455U 21909 WHEN THE SPEED BRAKE IS DEPLOYED, AIRCRAFT BANKS TO THE LEFT EXCESSIVELY. AILERON TRIM SET AT 0. WHEN THE B-SYSTEM IS OFF, THE AIRCRAFT DOES NOT ROLL. 2 L 7 3 4F 4 F A3WE E2EA 1998102300539 19981023 00539 WP 1998 10 23 ABXA9800902 1 19981012 A 5210 4917860501 FITTING DOUG DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND AFT ENTRY DOOR UPPER BAYONET SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-1. 2 L 7 2 4F A6WE 1998102300540 19981023 00540 WP 1998 10 23 ABXA9800904 1 19980910 A 5523 5910414501 TAB DOUG DOUG DC9 DC932 3022066 WP LT ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 903AX 47427 WHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ELEVATOR GEAR TAB CRACKED. REPLACED LEFT ELEVATOR GEAR TAB IAW DC-9 S UPPLEMENTAL MAINTENANCE MANUAL CHAPTER 27-30-4. 2 L 7 2 4F A6WE 1998102300541 19981023 00541 WP 1998 10 23 ABXA9800903 1 19980915 A 5753 59225352 SLAT DOUG DOUG DC9 DC932F 3022067 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 909AX 47148 DURING C-CHECK, FOUND FITTING CRACKED AT PIVOT POINT ON RT/OUTBOARD SLAT ASSY. REPAIRED UNIT IAW DC-9 SRM. 2 L 7 2 4F A6WE 1998102300542 19981023 00542 WP 1998 10 23 ABXA9800906 1 19981012 A 5210 3917854503 FITTING DOUG DOUG DC9 DC931 3022065 WP PAX DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND VENTRAL DOOR RIGHT LOWER CORNER FITTING CRACKED. REPLACED FITTING IAW DC-9 SRM 51-30-2, 51-30-5 A ND 51-30-1. 2 L 7 2 4F A6WE 1998102300543 19981023 00543 WP 1998 10 23 ABXA9800907 1 19981012 A 2740 59109625 JACKSCREW DOUG DOUG DC9 DC931 3022065 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND HORIZONTAL STABILIZER JACK SCREW THREADS CORRODED AND PITTED. REPLACED JACK SCREW AND NUT ASSEMBL Y IAW DC-9 SMM 27-40-1. 2 L 7 2 4F A6WE 1998102300544 19981023 00544 WP 1998 10 23 ABXA9800908 1 19981012 A 5320 99578994 INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP BS 37 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND INTERCOSTAL CRACKED AFT SIDE OF STATION 37 BULKHEAD RBL 12. REPLACED INTERCOSTAL IAW DC-9 SRM 51- 30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998102300545 19981023 00545 WP 1998 10 23 ABXA9800909 1 19981012 A 5320 5917497501 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND JACK PAD FITTING CRACKED AT LONGERON 30 STATION 996. REPLACED FITTING IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998102300546 19981023 00546 WP 1998 10 23 ABXA9800910 1 19981012 A 5320 491558131 STIFFENER DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND VERTICAL STIFFENER CORRODED FORWARD SIDE OF WEB STATION 996 AT LONGERON 29L. REPLACED STIFFENER I AW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998102300547 19981023 00547 WP 1998 10 23 ABXA9800911 1 19981012 A 5320 99577305 INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND INTERCOSTAL AT LBL 50 STATION 718 CRACKED. REPLACED INTERCOSTAL IAW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998102300548 19981023 00548 WP 1998 10 23 ABXA9800912 1 19981012 A 5330 59114034 SKIN DOUG DOUG DC9 DC931 3022065 WP BS 76 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, EDDY CURRENT INSPECTION INDICATED TOP FUSELAGE SKIN CRACKED 18 RIGHT OF CENTER SPLICE, STATION 76. REPA IRED IAW DC-9 ABX EA 53100075-003-2. 2 L 7 2 4F A6WE 1998102300549 19981023 00549 WP 1998 10 23 ABXA9800913 1 19981012 A 5320 491558132 STIFFENER DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 946AX 47003 DURING C-CHECK, FOUND VERTICAL STIFFENER CORRODED FORWARD SIDE OF WEB STATION 996 AT LONGERON 29R. REPLACED STIFFENER I AW DC-9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998102300550 19981023 00550 NM 1998 10 23 MWEA981007 1 19981017 A 5712 99375875 RIB DOUG MD88 MD88 3023688 NM WS 256.75 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 601ME 49762 FOUND CRACK ON LEFT WING LEADING EDGE SECOND RIB OUTBOARD OF NUMBER 1 SLAT TRACK AT STATION 256.75. MTC FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F RT A6WE 1998102300551 19981023 00551 NM 1998 10 23 SCNA98717 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1030-1050 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT ANGLE BETWEEN STATIONS 1030 AND 1050 RBL 24 IN CABIN FL OOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 2155841701 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 5 13002. 2 L 7 3 4F A3WE 1998102300552 19981023 00552 NM 1998 10 23 SCNA98718 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1030-1050 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK SUPPORT ANGLE BETWEEN STATIONS 1030 AND 1050 RBL 44 IN CA BIN FLOOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511006. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 44871, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B 727 513001. 2 L 7 3 4F A3WE 1998102300553 19981023 00553 NM 1998 10 23 SCNA98719 1 19981003 A 5322 ANGLE BOEING 727 7272A1 138407F NM BS 1050-1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK SUPPORT ANGLE BETWEEN STATIONS 1050 AND 1070 RBL 20 IN CA BIN FLOOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED NEW PART FROM 215584171, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513001. 2 L 7 3 4F A3WE 1998102300554 19981023 00554 NM 1998 10 23 SCNA98721 1 19981003 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK AT STATION 1070 RBL 24 IN CABIN FLOOR STRUCTURE. CORROSIO N FOUND TO BE OUT OF LIMITS IAW SRM B727 531001. REMOVED SEAT TRACK IAW SRM B727 513002. FABRICATED NEW SEAT TRACK IAW SRM B727 531003. TREATED AND PRIMED IAW SRM B727 511006. INSTALLED IAW SRM B727 513001. 2 L 7 3 4F A3WE 1998102300555 19981023 00555 NM 1998 10 23 SCNA98722 1 19981003 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 1050-1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK BETWEEN STATIONS 1050 AND 1070 RBL 46 IN CABIN FLOOR STRUC TURE. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM B727 531001. REMOVED SEAT TRACK IAW SRM B727 513002. FABRICATED NEW SEAT TRACK IAW SRM B727 531003. TREATED AND PRIMED IAW SRM B727 511006. INSTALLED IAW SRM B727 513001. 2 L 7 3 4F A3WE 1998102300556 19981023 00556 NM 1998 10 23 SCNA98723 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON CABIN FLOOR SUPPORT ANGLE AT STATION 1070 RBL 30. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511006. CORROSION FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. FABRICATED NEW PART F ROM 44871, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM 513001. 2 L 7 3 4F A3WE 1998102300557 19981023 00557 NM 1998 10 23 SCNA98724 1 19981003 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND AT STATION 1110 ON T-CAP OF FLOORBEAM AT BL 0. CORROSION WAS TO BE OUT OF LIMITS IAW B727 SRM 511001. CUT OUT DAMAGED AREA IAW B727 SRM 531008. FABRICATED UPPER CHORD FROM BAC 1505100617. F ABRICATED NEW SUPPORT ANGLES FROM BAC 14902785. FABRICATED SUPPORT ANGLES FROM BAC 14902831. FABRICATED REINFORCEMENT STRAP FROM 7075 T6 .080. FABRICATED REINFORCEMENT STRAP FROM 7075 T6 .051. TREATED AND PRIMED IAW B727 SRM 511001 MM 5 12002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998102300558 19981023 00558 NM 1998 10 23 SCNA98725 1 19981003 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND AROUND A .25 DIA HOLE IN T-CAP OF FLOORBEAM AT STATION 1110 RBL 15. COR ROSION WAS TO BE OUT OF LIMITS IAW B727 SRM 511001. CUT OUT DAMAGED AREA IAW B727 SRM 531008. FABRICATED UPPER CHORD F ROM BAC 1505100617. FABRICATED NEW SUPPORT ANGLES FROM BAC 14902785. FABRICATED SUPPORT ANGLES FROM BAC 14902831. FAB RICATED REINFORCEMENT STRAP FROM 7075 T6 .080. FABRICATED REINFORCEMENT STRAP FROM 7075 T6 .051. TREATED AND PRIMED I AW B727 SRM 511001 MM 512002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998102300559 19981023 00559 NM 1998 10 23 SCNA98726 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1090-1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND BETWEEN STATIONS 1090 AND 1110 LBL 15 ON CABIN FLOOR SUPPORT ANGLE. REM OVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT LIMITS IAW B727 SRM 531001. FABRICATE D PART FROM 44871, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002. 2 L 7 3 4F A3WE 1998102300560 19981023 00560 NM 1998 10 23 SCNA98727 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1090-1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND BETWEEN STATIONS 1090 AND 1110 RBL 5 ON CABIN FLOOR SUPPORT ANGLE. REMO VED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT LIMITS IAW B727 SRM 531001. FABRICATED PART FROM 44871, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002. 2 L 7 3 4F A3WE 1998102300561 19981023 00561 NM 1998 10 23 SCNA98728 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1130-1140 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND BETWEEN STATIONS 1130 AND 1140 RBL 15 ON CABIN FLOOR SUPPORT ANGLE. REM OVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION FOUND TO BE OUT LIMITS IAW B727 SRM 531001. FABRICATE D PART FROM 215584171, 7075 T6511. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B727 513002. 2 L 7 3 4F A3WE 1998102300562 19981023 00562 NM 1998 10 23 SCNA98730 1 19981003 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 1050 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON UPPER FLOORBEAM STATION 1050 RBL 33. CORROSION OUT OF LIMITS IAW SRM B727 53-10-1. CUT OUT DAMAGED AREA IAW SRM B727 531008. REPAIRED UPPER CHORD FROM BAC 1505100617. REPAIRED SUPPORT A NGLES FROM BAC 14902785. REPAIRED SUPPORT ANGLE FROM BAC 14902831 AND 14902831. FABRICATED NEW STRAPS FROM 7075 T6 .08 0 AND .051. TREATED PRIMED IAW SRM B727 511001. INSTALLED IAW SRM B727 513002. 2 L 7 3 4F A3WE 1998102300563 19981023 00563 NM 1998 10 23 SCNA98716 1 19981003 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 1030-1050 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON SEAT TRACK BETWEEN STATIONS 1030 AND 1050 RBL 56 IN CABIN FLOOR STRUC TURE. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM B727 531001. REMOVED SEAT TRACK IAW SRM B727 513002. FABRICATED NEW SEAT TRACK IAW SRM B727 531003. TREATED AND PRIMED IAW SRM B727 511006. INSTALLED SEAT TRACK IAW SRM B727 513001. 2 L 7 3 4F A3WE 1998102300564 19981023 00564 NM 1998 10 23 SCNA98720 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1050-1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT ANGLE BETWEEN STATIONS 1050 AND 1070 LBL 27 ON CABIN FL OOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW B 727 SRM 531001. FABRICATED PART FROM 215584171, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B7 27513002. 2 L 7 3 4F A3WE 1998102300565 19981023 00565 NM 1998 10 23 SCNA98729 1 19981003 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1130-1140 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 286SC 21601 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT ANGLE BETWEEN STATIONS 1130 AND 1140 LBL 10 ON CABIN FL OOR STRUCTURE. REMOVED CORROSION FROM SUPPORT ANGLE IAW B727 SRM 511001. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW B 727 SRM 531001. FABRICATED PART FROM 215584171, 7075 T6. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW SRM B7 27 513002. 2 L 7 3 4F A3WE 1998102300566 19981023 00566 1998 10 23 SCNA98127 2 19981016 A 7200 ENGINE DOUG DC10 DC1015 3022118 WP NR 3 FAILED A SCNA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 15 153SY 29698 1090 48276 DURING THE TAKEOFF ROLL, A LOUD BANG WAS HEARD ACCOMPANIED BY HEAVY VIBRATION OF UNKNOWN ORIGIN. TAKEOFF WAS ABORTED AT 125 KNOTS. DURING A BORESCOPE INSPECTION OF THE NUMBER THREE ENGINE METAL WAS FOUND IN THE TAILPIPE. 2 L 7 3 4F A22WE 1998102300567 19981023 00567 NM 1998 10 23 VNAA9810016 1 19981016 A 3234 7178011 SELECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FLIGHT DECK FAILED A VNAA O OTHER J WARNING INDICATION AP APPROACH 1 GL 07 433JS 3047 THE LANDING GEAR FAILED TO EXTEND WHEN SELECTED, DURING THE APPROACH. THE CREW FOLLOWED THE CHECK LIST AND MANUALLY PUM PED THE LANDING GEAR DOWN. A NORMAL LANDING WAS PERFORMED WITHOUT FURTHER INCIDENT. OUTSTATION MAINTENANCE INSPECTED A ND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FERRY WAS COMPLETED WITHOUT ANY PROBLEMS. PIT MAINT ENANCE INSPECTED AND REPLACED THE LANDING GEAR SELECTOR HANDLE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-31-01. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998102300568 19981023 00568 NM 1998 10 23 VNAA9810017 1 19981017 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE CABIN DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 459PS 77610 846 3070 DURING THE PREFLIGHT INSPECTION, A SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS NOTED TO BE INOPERATIVE. MAINTENANCE I NSPECTED AND REPLACED THE 4LK EMERGENCY BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-52-01. OPERATION AL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998102300569 19981023 00569 WP 1998 10 23 TC8A98068 1 19981020 A 2420 TERMINAL DOUG DC8 DC8F54 3021926 WP NR 1&3 GENERATOR DAMAGED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 802CK 45679 TRIP NR 02692, DURING TAXI, NR 1 AND NR 3 GENERATOR UNPARALLELED, VOLTS AND FREQS OK. AIRCRAFT FERRIED TO KYIP. TROUBL ESHOT SYSTEM, REPLACED TERMINALS AT WIRE NR X56024 (NR 3 GCR). SYSTEM OPS GOOD IAW DMM 24-10-0. 2 L 7 4 4F 4A25 1998102300570 19981023 00570 NM 1998 10 23 AALA981622 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FUSELAGE BELL FRAME DENTED ABOVE STRINGER 24L AT FS 600. INSTALLED BELL FRAME DOUBLER PER SRM 51-40-3 PAGE 1 USIN G 7075-T6, .071 INCH THICK, 7 INCHES LONG, .375 INCH AND .25 INCH FASTENERS AND 20 MS 20470D RIVETS, TWO ROWS ON BOTTOM AND ONE RAN ON TOP, THREE RIVETS EACH END. (M) 2 L 7 3 4F A3WE 1998102300571 19981023 00571 NM 1998 10 23 AALA981621 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - BELL FRAME DENTED ABOVE STRINGER 24R AT FS 700. INSTALLED DOUBLER REPAIR PER SRM 51-40-3 FIG 1 SHEET 3 USING 7075 T6, .063 INCH, 10 INCH DOUBLER, .375 FASTENERS AND .25 INCH FASTENER, 20 MS2047AA RIVETS, TWO ROWS ON TOP SIDE AND ONE ROW ON TOP. 2 L 7 3 4F A3WE 1998102300572 19981023 00572 NM 1998 10 23 AALA981620 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FUSELAGE BELL FRAME DENTED ABOVE STRINGER 23-24R AT FS 680. INSTALLED REPAIR DOUBLER PER SRM 51-4-3 FIG 1 PAGE 3 USING 7075-T6, .063 INCH THICK, 8 INCH DOUBLER, 21 MS20470D06 RIVETS TWO ROWS PAST DAMAGE AND ONE ROW ON TOP WITH 3 RIVE TS AT EACH END. (M) 2 L 7 3 4F A3WE 1998102300573 19981023 00573 NM 1998 10 23 AALA981619 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 580 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FRAME 580 BENT STRINGER 23L-25L. REMOVED DAMAGE, MADE DOUBLER AND INSTALLED PER SRM 51-40-3 PAGE 3 FIG 1 DOUBLER IS .5 INCH LONG. 7075-T6, .063 T, .375 AND .25 MS2407DD RIVETS, 31 TOTAL, 4.25 INCHES AT TWO ROWS AND ONE ROW ON TOP. ( M) 2 L 7 3 4F A3WE 1998102300574 19981023 00574 NM 1998 10 23 AALA981618 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - DENT IN FRAME ABOVE STRINGER 24R AT FS 660. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER 51-40-3 FIG 1 PAGE 3, 8 INCH DOUBLER OF .063 INCH 7075-T6, 20.375 MS2047DD RIVETS, THREE ROWS. (M) 2 L 7 3 4F A3WE 1998102300575 19981023 00575 NM 1998 10 23 AALA981617 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND DENT IN FRAME AT FS 600 ABOVE STRINGER 23R. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER 51-40-3 FIG 1 PA GE 3, 8 INCH DOUBLER OF .063 INCH 7075-T6, 20.375 INCH RIVETS MS2047DD, THREE ROWS. (M) 2 L 7 3 4F A3WE 1998102300576 19981023 00576 NM 1998 10 23 AALA981616 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FRAME AT STATION 520 DENTED ABOVE STRINGER 23R. INSTALLED FRAME REPAIR PER SRM 51-40-3. REMOVED DAMAGE AREA, INS TALLED 13 INCH DOUBLER OF .073 7075-T6 WITH THIRTY FOUR .375 D-RIVETS AND FOUR .25 INCH D-RIVETS, TWO .375 INCH SCREWS A ND SIX .375 INCH BOLTS. (M) 2 L 7 3 4F A3WE 1998102300577 19981023 00577 NM 1998 10 23 AALA981615 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - BELL FRAME DENTED AT STRINGER 26 LT AND 5 INCH ABOVE STRINGER 26 LT. INSTALLED DOUBLER .080 7075-T6 OVER DAMAGE A REA PER SRM 51-40-3. BELL FRAME DOUBLER 13.5 INCH IN LENGTH. (M) 2 L 7 3 4F A3WE 1998102300578 19981023 00578 NM 1998 10 23 AALA981614 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - BELL FRAME DENTED. SRM 51-40-3, TREATED AND PRIMED SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1998102300579 19981023 00579 NM 1998 10 23 AALA981613 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - BELL FRAME DENTED STATION 1110, ABOVE STRINGER 26 RT. INSTALLED .080 7075-T6 DOUBLER OVER 1 INCH CUTOUT, TWO ROWS ON SIDE, ONE ROW ON TOP FLANGE DOUBLER 7.5 INCH BY 2.5 INCH. .375 AND .25 470DD RIVETS PER SRM 51-40-3 PAGE 1-4. (M) 2 L 7 3 4F A3WE 1998102300580 19981023 00580 NM 1998 10 23 AALA981612 1 19980903 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - FOUND FORWARD CARGO FRAME 720A DENTED ABOVE STRINGER 24R. REMOVED DAMAGED SECTION, INSTALLED DOUBLER 8 INCH OF 70 75-T6 .063 INCH, TWENTY MS2047DD FASTENERS, THREE ROWS OF FASTENERS, THREE PAST DAMAGE EACH SIDE PER SRM 51-40-3 FIG 1 P AGE 3. (M) 2 L 7 3 4F A3WE 1998102300581 19981023 00581 NM 1998 10 23 AALA981611 1 19980814 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - AFT CARGO DOOR LOWR CUTOUT CHORD ANGLE CORRODED AT STATION 990. REMOVED CORROSION, INSTALLED DOUBLER IAW ESO 1169 7, 2/13/98 AND SRM 51-40-4 PAGE 1 AND 2. (M) 2 L 7 3 4F A3WE 1998102300582 19981023 00582 NM 1998 10 23 AALA981610 1 19980903 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 540 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - SHEAR TIE CRACKED AT STATION 540 BETWEEN STRINGER 17L AND 16L. REMOVED AND REPLACED SHEAR TIE AT FS 540 BETWEEN S TRINGER 17L AND 16L PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998102300583 19981023 00583 NM 1998 10 23 AALA981636 1 19980903 A 5720 ANGLE BOEING 727 727223 1384074 NM WS 442 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 889AA 21527 TUL - THREE INCH CORROSION SPOT LOWER CHORD BOTTOM SIDE SURFACE AT NR 8 FLAP TRACK ATTACH AREA REAR SPAR. REMOVED CORRO SION, ALODINED AND PRIMED. INSTALLED 2024 T-3 .071 THICK DOUBLER USING EXISTING PATTERN, THREE ROWS HIGH LOCKS .375 ARO UND BLEND AREA, REF ESO 11697, DATED 8/10/98. (M) 2 L 7 3 4F A3WE 1998102300584 19981023 00584 NM 1998 10 23 AALA981694 1 19980911 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - FUSELAGE SKIN DENTED AND PUNCTURED AT STRINGER 26L STATION 720. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998102300585 19981023 00585 NM 1998 10 23 AALA981693 1 19980911 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 887AA 21526 TUL - LEFT FUSELAGE LOWER FAIRING ATTACH RIB FRAME AT STATION 720 DAMAGED. INSTALLED NEW RIB/FRAME. (M) 2 L 7 3 4F A3WE 1998102300586 19981023 00586 NM 1998 10 23 AALA981690 1 19980914 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - ONE CRACK AT ACCESS PANEL CUT OUT RT SIDE OF VERTICLE BELOW FLAG. INSTALLED FLUSH DOUBLER REPAIR PER SRM CH 54-10 -3 PAGE 18, FIG 4 SHT 5. (M) 2 L 7 3 4F A3WE 1998102300587 19981023 00587 NM 1998 10 23 AALA981691 1 19980914 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 846AA 20987 TUL - THREE CRACKS AT ACCESS PANEL CUT OUT LEFT SIDE OF VERTICLE, BELOW FLAG. INSTALLED THREE DOUBLERS PER SRM CHAPTER 54-10-3 PAGE 18, FIG 4, SHEET 5. (M) 2 L 7 3 4F A3WE 1998102300588 19981023 00588 WP 1998 10 23 AALA981697 1 19980910 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 443AA 49469 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOD LIGHT IN TAIL CONE COMPARTMENT INOPERATIVE. REPLACED EMERGENCY FLOO D LIGHT ASSEMBLY IN TAIL CONE COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998102300589 19981023 00589 NM 1998 10 23 AALA981595 1 19980830 A 3350 02019242004 LIGHT BOEING 767 767223 1385123 NM EMERG EXIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 316AA 22318 SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT FIXTURE RIGHT SIDE OF BUSINESS CLASS GALLEY MISSING. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY FOR RIGHT SIDE OF BUSINESS CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998102300590 19981023 00590 NM 1998 10 23 AALA981340 1 19980707 A 3350 LIGHT BOEING 757 757223 1384957 NM MID GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 690AA 25696 DFW - DURING OVERNIGHT CHECK, MID GALLEY EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT MID GALLEY EME RGENCY EXIT FLOOR. SYSTEM GROUD CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998102300591 19981023 00591 EU 1998 10 23 98ZZZM774 1 19980908 A 5620 137959C3 WINDOW BAG JETSTM JETSTM3101 1500215 EU BS 187 CRACKED A CHQA A UNSCHED LANDING O OTHER TO TAKEOFF 1 GL 11 845JS 769 AIRCRAFT RETURNED TO FIELD DUE TO OUTER CABIN PANE AT SEAT 2A CRACKED AFTER TAKEOFF. THE OUTER PANE AND SEAL WERE REPLA CED. (M) 2 L 7 2 4T RT A21EU 1998102300592 19981023 00592 NE 1998 10 23 98ZZZM775 2 19980829 A 7261 M061 PUMP LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 ENGINE FAILED A AMTA E D ENGINE SHUTDOWN RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION CL CLIMB 1 GL 11 192AT 193C1057 010353 FLT 709 - LAX - ON CLIMB-OUT, NR 3 ENGINE OIL QTY DROPPED TO ZERO (RAPIDLY) FOLLOWED BY NR 3 OIL PRESSURE ALSO READING Z ERO. ENGINE WAS SHUT DOWN AND AIR TURN BACK. NR 3 ENGINE OIL PUMP WAS REPLACED AND OPS CHECKED FOR LEAKS AND FOUND OK. (M) 2 L 7 3 4F 4 F A23WE E12EU 1998102300593 19981023 00593 WP 1998 10 23 AALA981677 1 19980908 A 2780 V3601 SWITCH DOUG DC9 DC983 3022083 WP COCKPIT FAILED A AALA J DUMP FUEL F FLT CONT AFFECTED AP APPROACH 1 SW 07 565AA 49347 ORD - FLT 1224 - EN ROUTE SAN-ORD - ON APPROACH SLAT DISAGREE LIGHT ILLUMINATED WHEN FLAPS EXTENDED TO 15 DEGREES. CREW DECLARED AN EMERGENCY. LIGHT EXTINGUISHED AFTER APPROX 30 MINUTES. LANDED ORD WITHOUT INCIDENT. REPLACED FLAPS/SLAT HANDLE SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998102300594 19981023 00594 WP 1998 10 23 AALA981659 1 19980906 A 3610 SEAL DOUG DC9 DC982 3022082 WP TAIL COMP LOOSE A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 423AA 49335 DFW - FLT 1501 - ON TAKEOFF DFW, TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE. WHEN SUPPLY HIGH PRESSURE BLEED OFF WAS SELECTED LIGHT EXTINGUISHED IMMEDIATELY. AIR INTERRUPTED AND RETURNED TO DFW AND LANDED OV ERWEIGHT WITHOUT INCIDENT. REPOSITIONED SECONDARY HEAT EXCHANGER EXHAUST SEAL. ACCOMPLISHED LEAK TEST WITH NO DISCREPA NCY NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998102300595 19981023 00595 WP 1998 10 23 AALA981608 1 19980903 A 3230 59370365501 CYLINDER DOUG DC9 DC982 3022082 WP RT MLG FAILED A AALA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 07 276AA 49273 DFW - FLT 1442 - AFTER TAKEOFF ELP EN ROUTE DFW, RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED. AIRCRAF T YAWED INDICATING GEAR OR DOORS STILL EXTENDED. PERFORMED QRH PROCEDURE AND RIGHT MAIN LANDING GEAR RETRACTED AND LIGH T EXTINGUISHED. LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR RETRACT CYLINDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998102300596 19981023 00596 WP 1998 10 23 AALA981607 1 19980903 A 3260 833605A PROX SWITCH DOUG DC9 DC982 3022082 WP E/E BAY FAILED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 437AA 49455 DTW - FLT 1220 - AFTER TAKEOFF ORD EN ROUTE ROC, THE AURAL WARNING FOR LANDING GEAR COULD NOT BE SILENCED. RETURNED AND LANDED ORD WITHOUT INCIDENT. REPLACED R2-295, PROXIMITY SWITCH UNIT. PRECAUTIONARY REPLACED AURAL WARNING UNIT. THRO TTLE SWITCHES NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998102300597 19981023 00597 WP 1998 10 23 ASAA9880158 1 19980824 A 5610 PIN DOUG DC9 DC983 3022083 WP COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 962AS 53076 SEA - AFTER ARRIVAL OF FLT 92, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. REPOSITIONED WIND OW LINKAGE PIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998102300598 19981023 00598 WP 1998 10 23 ASAA9880147 1 19980812 A 5210 HOOK DOUG DC9 DC983 3022083 WP PAX DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR HOOK WAS FOUND TO BE BENT AND WOULD NOT RETRACT FROM THE LOCKED POSITION. R EPLACED HOOK ASSY, BURNISHED MINOR GOUGE, AND ADJUSTED HOLD OPEN HOOK. DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998102300599 19981023 00599 WP 1998 10 23 ASAA9880148 1 19980814 A 5610 WINDOW DOUG DC9 DC982 3022082 WP COCKPIT LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 SEA - AFTER ARRIVAL OF FLT 721 - CREW REPORTED THE FLIGHT COMPARTMENT LT SLIDING WINDOW WOULD NOT OPEN. LUBRICATED THE WINDOW OPERATING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998102300600 19981023 00600 WP 1998 10 23 ASAA9880164 1 19980828 A 5610 PIN DOUG DC9 DC982 3022082 WP COCKPIT OUT OF POSITION A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 954AS 49387 ANC - PRIOR TO DEPARTURE OF FLT 196, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WAS STUCK OPEN. REPOSITIONE D WINDOW HINGE PIN IN CLEVIS AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998102300601 19981023 00601 WP 1998 10 23 ASAA9880167 1 19980831 A 5210 HINGE DOUG DC9 DC982 3022082 WP PAX DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 937AS 49364 PDX - DURING MAINTENANCE CHECK, THE L1 DOOR HOLD OPEN HOOK WOULD NOT ENGAGE. REMOVED TWO SHIMS FROM THE HINGE FRAME STO PPER AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998102300602 19981023 00602 1998 10 23 ASAA9880168 4 19980831 A 2565 D29982121 SLIDE DOUG DC9 DC983 3022083 WP PAX DOOR FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 2112 53451 OAK - DURING 15K CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOO R EMERGENCY EVACUATION SLIDE ASSY. (M) 2 L 7 2 4F RT A6WE 1998102300603 19981023 00603 1998 10 23 ASAA9880170 4 19980904 A 2565 D37013109 BOTTLE DOUG DC9 DC983 3022083 WP SLIDE DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 1177 53079 SEA - PRIOR TO DEPARTURE OF FLT 376, CREW REPORTED THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSY. (M) 2 L 7 2 4F RT A6WE 1998102300604 19981023 00604 1998 10 23 ASAA9880169 4 19980903 A 2565 D37013115 BOTTLE DOUG DC9 DC982 3022082 WP SLIDE DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 941AS 2369 49925 LAX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSY. (M) 2 L 7 2 4F A6WE 1998102300605 19981023 00605 1998 10 23 ASAA9880171 4 19980908 A 2565 D37013121 BOTTLE DOUG DC9 DC982 3022082 WP SLIDE DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 937AS 2589 49364 PDX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACE D THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSY. (M) 2 L 7 2 4F A6WE 1998102300606 19981023 00606 WP 1998 10 23 ASAA9880141 1 19980803 A 5610 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 963AS 53077 SEA - AFTER ARRIVAL OF FLT 99, CREW REPORTED THE FLIGHT COMPARTMENT RT SLIDING WINDOW WOULD NOT OPEN. ADJUSTED WINDOW T O TRACKS AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998102300607 19981023 00607 WP 1998 10 23 ASAA9880137 1 19980728 A 5210 SPRING DOUG DC9 DC982 3022082 WP PAX DOOR DISCONNECTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 PDX - DURING MAINTENANCE CHECK, THE L2 DOOR WOULD NOT LATCH OPEN. RECONNECTED SPRING TO HOLD OPEN MECHANISM AND OPERATE D NORMALLY. (M) 2 L 7 2 4F A6WE 1998102300608 19981023 00608 WP 1998 10 23 ASAA9880143 1 19980807 A 5610 WINDOW DOUG DC9 DC983 3022083 WP COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 963AS 53077 PDX - AFTER ARRIVAL OF FLT 727, CREW REPORTED FIRST OFFICERS WINDOW WOULD NOT OPEN. ADJUSTED UPPER FORWARD GUIDE PIN AN D OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998102300609 19981023 00609 NM 1998 10 23 EISA98219 1 19980909 A 2410 NUT BOEING 727 727223 1384074 NM GENERATOR LOOSE A EISA C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 6815 19490 REJECTED TAKEOFF AT TMP NR 3 GENERATOR TRIPPED OFF LINE ON POWER UP FOR TAKEOFF, CSD LOW OIL LIGHT CAME ON. GENERATED F ROM PILOT REPORT. FOUND B-NUT LOOSE ON COOLER, RETORQUED AND SERVICED CSD. LEAK CHECKED OK. (M) 2 L 7 3 4F A3WE 1998102300610 19981023 00610 NM 1998 10 23 NOCA1998 1 19980914 A 5270 TARGET BOEING 757 75728A 1384976 NM PAX DOOR OUT OF ADJUST A NOCA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 750NA 26277 FLT 81 - ADW - ABORTED TAKEOFF AT 100 KNOTS DUE TO EICAS WARNING OF THE R-4 ENTRY DOOR OPEN. RETURNED TO THE GATE WITHO UT INCIDENT. INSPECTION OF THE R-4 WAS VERIFIED CLOSED AND LOCKED AND THE DOOR HANDLE FOUND IN THE PROPER POSITION HIGH ENERGY STOP HEAT DAMAGE CHECK ACCOMPLISHED. NO HEAT DAMAGE FOUND. DOOR PROXIMITY TARGET ADJUSTED AND OPERATIONALLY CH ECKED GOOD. (M) 2 L 7 2 4F RT A2NM 1998102300611 19981023 00611 CE 1998 10 23 MASA98180 1 19980917 A 5260 1294000371 SEAL BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR LOOSE A MASA A B UNSCHED LANDING EMER. DESCENT O OTHER CL CLIMB 1 SW 07 68ZV UE68 FLT 5329 - FLL-TPA - DURING CLIMB-OUT, THE CREW HEARD A LOUD NOISE COMING FROM THE CABIN. THEY DETERMINED THAT THE AIRS TAIR DOOR SEAL HAD POPPED OUT OF ITS SEAT. THE AIRCRAFT EXPERIENCED A SLIGHT DEPRESSURIZATION, BUT THE OXYGEN MASKS WER E NOT DEPLOYED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REINSTALLED THE DOOR SEAL, OPS CH ECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998102300612 19981023 00612 NM 1998 10 23 MASA98179 1 19980905 A 2910 AE99149E CONNECTOR DHAV DHC8 DHC8202 2809007 NM MANIFOLD FAILED A MASA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 446YV 446 FLT 4446 - MTJ-PHX - DURING CLIMB-OUT FROM MTJ, THE MASTER CAUTION ILLUMINATED, AND THE CAUTION PANEL INDICATED NR 2 ENG INE HYDRAULICS. CREW DECLARED AN EMERGENCY AND DIVERTED TO GTJ. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLE SHOT AND REMOVED AND REPLACED AND FITTING ON THE RETURN FILTER MANIFOLD. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A13NM 1998102300613 19981023 00613 CE 1998 10 23 98ZZZM776 1 19980915 A 2150 7756355 ACM BEECH 1900 1900D 1154162 CE FUSELAGE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 842CA UE41 AIRCRAFT WILL NOT COOL. REPLACED AIR CYCLE MACHINE AND HEAT EXCHANGER. (M) 2 L 7 2 4T RT A24CE 1998102300614 19981023 00614 CE 1998 10 23 98ZZZM777 1 19980910 A 3230 1013880083 SERVICING VALVE BEECH 1900 1900D 1154162 CE LT WING FAILED A JJBA A UNSCHED LANDING L NO TEST CL CLIMB 1 EA 01 860CA 1854 UE134 LANDING GEAR FAILED TO RETRACT ON TAKEOFF. CIRCUIT BREAKER OPENED. SERVICING VALVE FOUND TO BE DEFECTIVE. REPLACED DE FECTIVE SERVICING VALVE IAW CHAP 32 RAYTHEON MM. OPS CHECK SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1998102300615 19981023 00615 EU 1998 10 23 SABA980045 1 19980911 A 3260 BULB BAG JETSTM JETSTM3201 1500217 EU COCKPIT LT MLG FAILED A SABA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 33 943AE 943 FLT 5137 - CLT-RWI - ON APPROACH FOR LANDING, LANDING GEAR WAS EXTENDED. A UNSAFE GEAR ON THE LEFT MAIN WAS INDICATED. AIR CREW DECLARED A INFLIGHT EMERGENCY. AIRCRAFT DID A FLYBY. TOWER TOLD THE AIRCREW THAT THREE GEAR WAS EXTENDED. A IRCRAFT LANDED AT RWI WITH NO OTHER PROBLEMS. MAINTENANCE FOUND A BAD BULB IN THE LEFT GEAR POSITION. REMOVED AND REPL ACED BULB, SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A56EU 1998102300616 19981023 00616 EU 1998 10 23 SABA980044 1 19980909 A 3230 7445B BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU HYDRAULIC SYSTEM FAILED A SABA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 33 952AE 952 FLT 5202 - CLT-LYH - AFTER TAKEOFF AND CLIMB-OUT, AIRCREW REPORTED A CONSTANT GEAR WARNING HORN. AIRCRAFT RETURNED TO C LT. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED AT CLT WITH NO OTHER PROBLEMS. MAINTENANCE FOUND THE BYPASS P IN POPPED. RESET PIN, PIN POPPED AGAIN. REMOVED AND REPLACED VALVE. BLEED HYD SYSTEM. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A56EU 1998102300617 19981023 00617 WP 1998 10 23 HALA9800326 1 19980917 A 2620 892857 CLAMP DOUG DC9 DC951 3022051 WP NR 2 ACM DUCT LOOSE A HALA F D ACTIVATE FIRE EXT. RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 13 673MC 95199CR 47726 KOA - FLT 317 - FIRE PROTECTION AGENT LOW LIGHT ON. FOUND LOWER FIRE BOTTLE THERMO DISCHARGED ONLY. REPLACED ACM PNEU DUCT, CLAMP LOOSE, RETORQUED AND SAFETIED. LEAK CHECK OK, LOW LIGHT CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998102300618 19981023 00618 NM 1998 10 23 TSAA9833509 1 19980918 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM FD ENTRY INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED EMERGENCY EXIT LIGHT AT FORWARD ENTRY DOOR DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F A16WE 1998102300619 19981023 00619 NM 1998 10 23 TSAA9833510 1 19980918 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM NR 2 POS DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 2 POSITION PROXIMITY FLOOR LIGHT BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998102300620 19981023 00620 NM 1998 10 23 TSAA9833511 1 19980921 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM NR 2 POS DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 2 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO BEING INOP. REPLACED BATTERY PACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998102300621 19981023 00621 EA 1998 10 23 98ZZZM778 1 19980921 A 5511 C6TP10017 RIB DHAV DHC6 DHC6300 2802606 EA HORIZ STAB DAMAGED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 710PV 70141 751 HNL - RIGHT STABILIZER OUTBOARD RIB AT STATION 113.25 HAS NUMEROUS RIVETS PULLED OR MISSING ON UPPER SKIN. RIVET HOLES OVERSIZED AND ELONGATED. (M) 1 H 7 2 3T RT A9EA 1998102300622 19981023 00622 EU 1998 10 23 RAIA980908 1 19980916 A 3234 1005383Y00 VALVE AEROSP ATR42 ATR42300 8680920 EU HYD BAY FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 426TE 21953 228 FLT 7408 - STL - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE. (M) 2 H 7 2 4T RT A53EU 1998102300623 19981023 00623 WP 1998 10 23 RAIA980907 2 19980914 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT MALFUNCTIONED A RAIA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS DE DESCENT 1 CE 03 427AM 876 FLT 7471 - ALO - ON DESCENT, RIGHT ENGINE TORQUE DROPPED TO 20 PERCENT AND EGT GAVE ERRONEOUS READINGS. CREW PERFORMED ENGINE SHUT DOWN. MAINTENANCE GROUND RAN, DEFERRED RIGHT TTL PER MEL 76-2 CAT C. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998102300624 19981023 00624 1998 10 23 SIMA982513 4 19980908 A 3460 6227236012 MFD SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 350CF 123 340B350 LAX - FLT 3281 - CREW REPORTED SMOKE ODOR IN THE COCKPIT. REMOVED AND REPLACED MULTI-FUNCTION DISPLAY UNIT. OPERATIONA L CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998102300625 19981023 00625 EU 1998 10 23 SIMA982631 1 19980920 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A SIMA K NONE N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 298AE A4272 340B298 DFW - FLT 3563 - LAV SMOKE WARNING LIGHT CAME ON PRIOR TO DEPARTING GATE AND WILL NOT GO OUT. REMOVED AND REPLACED LAV SMOKE DETECTOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998102300626 19981023 00626 EU 1998 10 23 SIMA982671 1 19980924 A 2611 721121000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA F D ACTIVATE FIRE EXT. RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SW 21 306AE A3216 340B306 LAS - FLT 3242 - CARGO SMOKE ANNUNCIATOR ON CWP ILLUMINATED. ACTIVATED FIRE EXTINGUISHER. RETURNED TO BLOCK. NO EVIDE NCE OF SMOKE. REMOVED AND REPLACED NR 1 CARGO SMOKE DETECTOR AND NR 1 CARGO FIRE EXTINGUISHER. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A52EU 1998102300627 19981023 00627 NM 1998 10 23 USAA980405 1 19980908 A 5315 BAC1518338 FLOORBEAM BOEING 757 7572B7 1384964 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 616AU 19014 27147 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION AT SCREW HOLES TOP OF T-CAP STATION 1640 LBL 64 TO RBL 64 FLOO RBEAM. REMOVED CORRODED T-CAP AND INSTALLED REPLACEMENT T-CAP AND REPAIR ANGLES PER TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1998102300628 19981023 00628 NM 1998 10 23 USAA980402 1 19980915 A 5330 143N36501 SKIN BOEING 757 757225 1384959 NM STATION 632 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 44730 22193 CLT - DURING A C-3 CHECK VISUAL INSPECTION, FOUND A LIGHTNING STRIKE AT EXISTING REPAIR STATION 632 STRINGER 19R ON SKIN . INSTALLED REPAIR DOUBLER PER EA 62360 AND SRM 53-00-01 FIG 203. (M) 2 L 7 2 4F RT A2NM 1998102300629 19981023 00629 NM 1998 10 23 USAA980380 1 19980915 A 5311 146N100719 FRAME BOEING 757 757225 1384959 NM BS 1320 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 44730 22193 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH CORRODED AREA BS 1320 LBBL 12 ON FRAME INST BODY. CO RROSION TASK NR C 53-155-02. BURNISHED AFFECTED AREA PER SRM 53-00-07 AND 51-10-00. (M) 2 L 7 2 4F RT A2NM 1998102300630 19981023 00630 1998 10 23 USAABB98099 4 19980905 A 2565 416T20231 HINGE BOEING 767 767201 1385125 NM SLIDE DOOR BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 645US 23897 PIT - ON WALK AROUND, MECHANIC FOUND RIGHT OVERWING SLIDE DOOR NOT FAIRED. MAINTENANCE REPLACED TWO BROKEN HINGES ON SL IDE DOOR. (M) 2 L 7 2 4F RT A1NM 1998102300631 19981023 00631 NM 1998 10 23 USAABB98094 1 19980903 A 2130 VALVE BOEING 767 767201 1385125 NM RT PACK MISINSTALLED A USAA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 EA 19 649US 23901 PHL - FLT 782 - AFTER TAKEFF FROM PIT, CREW COULD NOT GET THE RIGHT PACK ON LINE. FLIGHT DIVERTED TO PHL AND LANDED WIT H NO FURTHER INCIDENT. MAINTENANCE FOUND THAT PER AN MEL, THE PRESSURE REGULATING SHUTOFF VALVE HAD INCORRECTLY BEEN WI RED SHUT. THE VALVE WAS RESTORED TO NORMAL OPERATING CONDITION AND THE HIGH STAGE BLEED VALVE WIRED SHUT. FLIGHT CONTI NUED TO FRA. (M) 2 L 7 2 4F RT A1NM 1998102300632 19981023 00632 NM 1998 10 23 USAASB98244 1 19980916 A 3350 20131ALP BATTERY BOEING 737 737301 1384611 NM FWD ENTRY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 341US 23510 RDU - PILOT REPORTED THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT FOR THE FORWARD MAIN ENTRY DOOR IS INOP. MAINTENANCE REM OVED AND REPLACED THE BATTERY SUPPLY AND THE REFLECTOR ASSY FOR THE MAIN ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT ASSY. ( M) 2 L 7 2 4F RT A16WE 1998102300633 19981023 00633 NM 1998 10 23 98ZZZM779 1 19980916 A 3350 3114981 REFLECTOR BOEING 737 737301 1384611 NM FWD ENTRY INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 341US 23510 RDU - PILOT REPORTED THE EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT FOR THE FORWARD MAIN ENTRY DOOR IS INOP. MAINTENANCE REM OVED AND REPLACED THE BATTERY SUPPLY AND THE REFLECTOR ASSY FOR THE MAIN ENTRY DOOR EXTERIOR ESCAPE SLIDE LIGHT ASSY. ( M) 2 L 7 2 4F RT A16WE 1998102300634 19981023 00634 NM 1998 10 23 USAASB98254 1 19980927 A 3350 500000043 BATTERY CHARGER BOEING 737 737201 1384454 NM EMERG EXIT INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 260AU 22866 PHL - MAINTENANCE FOUND THE OVERWING EMERGENCY LIGHTS AND THE CENTER AISLE EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOV ED AND REPLACED THE BATTERY CHARGER ASSY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998102300635 19981023 00635 NM 1998 10 23 USAASB98250 1 19980922 A 3350 6104789 BATTERY PACK BOEING 737 737201 1384454 NM AFT ENTRY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 237US 22353 CMH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT THE AFT SERVICE DOORS DIM. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK AT M572. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998102300636 19981023 00636 NM 1998 10 23 USAASB98248 1 19980920 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 586US 23931 ROC - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS HAD FAILED AFTER 30 SECONDS OF OPERATION. MAINTENANCE REMOVED AND REPL ACED DISCHARGED BATTERY PACKS IN POWER SUPPLIES M1133 AND M1137. OPERATIONAL CHECK. (M) 2 L 7 2 4F RT A16WE 1998102300637 19981023 00637 NM 1998 10 23 USAASB98247 1 19980919 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM FWD ENTRY INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 245US 22751 DCA - PILOT REPORTED THAT UPON SHUTDOWN OF ALL POWER, EXCEPT GROUND SERVICE, LEAVES TWO EMERGENCY EXIT LIGHTS ON WHEN BA TTERY SWITCH IS TURNED OFF. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR EMERGNCY EXIT LIGHT ASSEMBLY. ALL CABIN EMERGENCY LIGHTS OPS CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998102300638 19981023 00638 NM 1998 10 23 USAASB98246 1 19980919 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM PAX ENTRY INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 BWI - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT OVER THE MAIN ENTRY DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE EM ERGENCY EXIT LIGHT ASSY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998102300639 19981023 00639 NM 1998 10 23 TSAA9833513 1 19980924 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM NR 2 POS DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 2 POSITION EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECKED OK. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998102300640 19981023 00640 NM 1998 10 23 TSAA9833512 1 19980922 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM NR 6 POS DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998102300641 19981023 00641 NM 1998 10 23 98ZZZM780 2 19980828 A 7510 320115 ANTI-ICE VALVE BOEING 727 72751C 1384015 NM NR 2 ENGINE LEAKING A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 436EX 19289 FLT 643 - PHX-LAX - ENGINE FIRE INDICATION ON CLIMB-OUT NR 2 ENGINE. SHUT DOWN NR 2 ENGINE, RETURNED TO PHX. REPAIRED LEAKS AT 8TH STAGE BLEED DUCT AT SECOND CONNECTION AFT OF FIRE WALL AND ENGINE ANTI-ICE VALVE AT 12 O'CLOCK POSITION. ( M) 2 L 7 3 4F A3WE 1998102300642 19981023 00642 NM 1998 10 23 98ZZZM781 1 19980904 A 5347 50044503 LOCK BOEING 727 727222 1384073 NM CARGO BAY BROKEN A RYNA O OTHER O OTHER CR CRUISE 1 CE 07 7643U 20037 CREW REPORTS POSSIBLE CARGO SHIFT. INSPECTED UPPER CARGO DECK, FOUND 3 LOCKS IN EACH POSITION SHEARED OFF AFT OF NR 4 T HROUGH NR 10 POSITIONS. FOUND 2 SECTIONS OF ROLLER TRAYS THAT CAME UP. INSTALLED ORIGINAL CONTAINER. FOUND BASE TO BE SEVERELY WARPED. AIRCRAFT WAS FERRIED TO DAY FOR REPAIR. REMOVED AND REPLACED 19 PALLET LOCKS FROM POSITIONS NR 4 THR OUGH NR 12, REPLACED 2 ROLLER TRAYS. (M) 2 L 7 3 4F A3WE 1998102300643 19981023 00643 NM 1998 10 23 98ZZZM782 1 19980904 A 5753 BOLT BOEING 727 72731 1384010 NM TE FLAP LOOSE A RYNA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 CE 07 210NE 18903 FLT 206 - AFTER TAKEOFF FROM GSO, AIRCRAFT HAS A VERY STRONG VIBRATION ANYTIME IT IS TURNED TO THE RIGHT. VIBRATION CEA SED WHEN THE AIRCRAFT WAS ROLLED TO THE LEFT, RETURNED TO GSO. TROUBLESHOT AND FOUND LEFT AND RIGHT INBOARD FLAP CARRIA GE BOLTS LOOSE, RETORQUED AND ADJUSTED FLAP DROOP AND CLEARANCES. (M) 2 L 7 3 4F A3WE 1998102300644 19981023 00644 NM 1998 10 23 P2EA98170 1 19980919 A 8012 A910062 SWITCH BOEING 737 737297 1384480 NM COCKPIT FAILED A P2EA E ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE NR NOT REPORTED 1 CE 05 5WM 22629 MSP - FLT 416 - EMERGENCY DECLARED, NR 1 ENGINE INFLIGHT SHUTDOWN, LANDING UNEVENTFUL. NR 1 START VALVE OPEN LIGHT ILLU MINATED IN FLIGHT ON CLIMB-OUT. NR 1 ENGINE SHUTDOWN IAW QRH. CVR C/B PULLED AT 1724Z. FOUND VOLTAGE FROM START SWITC H TO C/P ON START VALVE PIN 2. DISCONNECTED AND STOWED C/P. START VALVE REMAINS ON MEL 80-3, CI NR M005114. (M) 2 L 7 2 4F A16WE 1998102300645 19981023 00645 NM 1998 10 23 EISA98228 1 19980810 A 5313 STRINGER BOEING 727 7272A7 138407K NM BS 1175 MISSING A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK CPCP CARD 53-113-01, A 5 INCH SECTION OF STRINGER 30 WAS MISSING FROM FLOOR AFT CARGO P IT BS 1175. REMOVED DAMAGED STRINGER AND FABRICATED NEW STRINGER PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998102300646 19981023 00646 NM 1998 10 23 EISA98227 1 19980810 A 5311 FRAME BOEING 727 7272A7 138407K NM BS 540 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND FUSELAGE FRAME CRACKS AT STATION 540 WL 214. REMOVED DAMAGE AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998102300647 19981023 00647 NM 1998 10 23 EISA98226 1 19980810 A 5311 FRAME BOEING 727 7272A7 138407K NM BS 560 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND FUSELAGE FRAME CRACKS AT STATION 560 WL 214. REMOVED DAMAGE AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998102300648 19981023 00648 NM 1998 10 23 EISA98225 1 19980810 A 5347 SEAT TRACK BOEING 727 7272A7 138407K NM BS 1050 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK AT STATION 1050 LBL 25. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1998102300649 19981023 00649 NM 1998 10 23 ASAA9840088 1 19980824 A 3350 SIGN BOEING 737 7374Q8 NM LT AFT DOOR MISSING A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 779AS 25111 ANC - FLT 94 - THE LEFT AFT DOOR LOWER 'EXIT' SIGN WAS FOUND TO BE MISSING. REPLACED 'EXIT' SIGN. (M) 2 L 7 2 4F RT A16WE 1998102300650 19981023 00650 NM 1998 10 23 ASAA9810102 1 19980915 A 3350 6104781 BATTERY BOEING 737 7372Q8C 138448S NM ROW 12 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 12. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998102300651 19981023 00651 NM 1998 10 23 ASAA9810100 1 19980907 A 3350 8821004 BATTERY PACK BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - PRIOR TO FLT 124 - THE EMERGENCY EXIT FLOOR TRACK LIGHTS ILLUMINATED. REPLACED BATTERY PACK AND LIGHTS OPERATED N ORMALLY. (M) 2 L 7 2 4F A16WE 1998102300652 19981023 00652 NM 1998 10 23 ASAA9810099 1 19980902 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM SMOKE BARRIER DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIG HT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998102300653 19981023 00653 NM 1998 10 23 ASAA9810098 1 19980901 A 3350 6005401 BATTERY BOEING 737 7372X6C 1384552 NM R1 DOOR DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGH TS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998102300654 19981023 00654 NM 1998 10 23 ASAA9810090 1 19980826 A 3350 86210144 BATTERY BOEING 737 737290C 138448V NM SMOKE BARRIER DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED N ORMALLY. (M) 2 L 7 2 4F A16WE 1998102300655 19981023 00655 NM 1998 10 23 AALA981654 1 19980904 A 3350 1000679 LIGHT BOEING 767 767223 1385123 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 325AA 15047 22326 ORD - FLT 95 - ON AIRCRAFT SHUTDOWN AT ORD GATE, COCKPIT DOOR EMERGENCY EXIT LIGHT WOULD NOT EXTINGUISH. REPLACED COCKP IT DOOR EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998102300656 19981023 00656 NM 1998 10 23 AALA981657 1 19980907 A 3397 WIRE BOEING 767 767323 1385205 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 357AA 24038 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHT AT 24H INOPERATIVE. REPAIRED CONNECTOR WIRE AT SEAT 24H. SYSTE M GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998102300657 19981023 00657 NM 1998 10 23 AALA981658 1 19980903 A 3350 427303 TRANSFORMER BOEING 767 767223 1385123 NM E/E BAY FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 307AA 0267 22313 ORD - FLT 185 - DURING CRUISE, RED EQUIPMENT ACCESS ON OVERHEAD PANEL ILLUMINATED WITH ASSOCIATED EICAS MESSAGE. SOUND OF ELECTRICAL ARCING WAS NOTED BY CREW. LIGHT ALSO ILLUMINATED NOSE UNSAFE GEAR LIGHT. LANDED ORD WITHOUT INCIDENT. R EPLACED LEFT UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998102300658 19981023 00658 NM 1998 10 23 AALA981591 1 19980830 A 3232 AAP26551 ACTUATOR BOEING 727 727223 1384074 NM LT MLG DOOR MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 873AA 21385 IAH - FLT 2078 - AFTER TAKEOFF AND GEAR RETRACTION, EN ROUTE TO DFW, LEFT MAIN GEAR INDICATION WAS RED WITH ASSOCIATED G EAR DOOR WARNING LIGHT ILLUMINATED. LANDING GEAR HANDLE RETURNED TO OFF POSITION LIGHTS REMAINED ON. ADDITIONALLY LEFT GEAR GREEN LIGHT ILLUMINATED. AT GEAR DOWN, ALL INDICATION PLUS VISUAL INSPECTION SHOWED 3 DOWN AND GREEN LIGHTS, NO R ED LIGHTS. RETURNED AND LANDED IAH WITHOUT INCIDENT. SECURED A 12 INCH SEAL HANGING DOWN FROM LEFT GEAR WING DOOR END PLATE. DID MX FERRY TO DFW FOR PERMANENT REPAIRS. EN ROUTE DFW GRIPE REPEATED. LANDED DFW WITHOUT INCIDENT. REPLACED LEFT MLG DOOR ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300659 19981023 00659 EU 1998 10 23 AALA981699 1 19980915 A 3231 A11345403 STOP FOKKER F28 F28MK0100 4990807 EU LT MLG LOOSE A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 1460A 11480 DFW - FLT 1423 - DURING CRUISE, LEFT MAIN LANDING GEAR ILLUMINATED ON MFDU WITH NO AIR NOISE OR CONTROL PROBLEM NOTED AT LEVEL FLIGHT. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND LEFT MAIN GEAR DOOR STOP LOOSE AND EXTE NDED PREVENTING THE LEFT GEAR DOOR FROM CLOSING. RESECURED LEFT MAIN GEAR DOOR STOP LOCKING ASSY. AIRCRAFT WAS JACKED AND A GEAR SWING ACCOMPLISHED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998102300660 19981023 00660 WP 1998 10 23 AALA981701 1 19980917 A 3350 0200333001 LIGHT DOUG DC9 DC982 3022082 WP AFT STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 575AM 53152 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIR EMERGENCY EXIT L IGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998102300661 19981023 00661 NM 1998 10 23 AALA981703 1 19980917 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 515 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1760A 48550 TUL - FOUND CORROSION AROUND FLOORBOARD SCREW HOLES INBOARD OF NR 3 SEAT TRACK. REPAIRED NR 3 SEAT TRACK PER ESO 41000, DATED 9/16/98. (M) 2 L 7 3 4F RT A22WE 1998102300662 19981023 00662 NM 1998 10 23 AALA981702 1 19980719 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 449 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1760A 48550 TUL - FOUND CORROSION ON NR 2 SEAT TRACK STATION 470-499. ACCOMPLISHED REPAIR PER SRM VOL 1, 53-70-00 FIG 4 AND ESO 410 00, DATED 9-16-98. (M) 2 L 7 3 4F RT A22WE 1998102300663 19981023 00663 NM 1998 10 23 AALA981692 1 19980914 A 2752 FITTING DOUG MD11 MD11 3023602 NM WS 838 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1760A 48550 TUL - FOUND OUTBOARD FLAP RT WING, OUTBOARD HINGE ACTUATOR FORWARD ATTACH BOLT POINT IS EMITTING RUST. REMOVED BOLT AND ACTUATOR AND REMOVED ACTUATOR ATTACH BOLT. REMOVED CORROSION AND REPAIRED HOLE PER ESO NR 41000 DATED 9-10-98. REINST ALLED, OPS AND LEAK CHECKED ACTUATOR ASSY. (M) 2 L 7 3 4F RT A22WE 1998102300664 19981023 00664 NM 1998 10 23 AALA984189 1 19980921 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 377AN 25446 AFW - FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE. FABRICATED REPAIR STRAPS FROM .063-7-75-T6. INS TALLED REPAIR STRAPS, WET WITH BMS5-95. SEALANT USE BACB30NW6, FASTENERS OR EQUIVALENT. (M) 2 L 7 2 4F RT A1NM 1998102300665 19981023 00665 NM 1998 10 23 AALA984188 1 19980921 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 377AN 25446 AFW - FLOORBEAM AT STATION 347, RBL 11 HAD CORROSION BLENDED ON TOP SURFACE. FLOORBEAM AT STATION 347, RBL NR 11 HAD CO RROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. (M) 2 L 7 2 4F RT A1NM 1998102300666 19981023 00666 NM 1998 10 23 AALA984187 1 19980921 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 377AN 25446 AFW - FLOORBEAM AT STATION RBL 78 AND 75 HAD CORROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. FABRICATED EXTENDED RE PAIR STRAP FROM .063-7075-T6. INSTALL REPAIR STRAP WET WITH BMS 5-95 USE BACB3DW6 FASTENERS OR EQUIVALENT. (M) 2 L 7 2 4F RT A1NM 1998102300667 19981023 00667 WP 1998 10 23 AALA981675 1 19980904 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 1155-1212 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - FORWARD, AFT AND CENTER SECTIONS OF AFT CARGO DOOR BEAM CORRODED. REPAIRED DOOR BEAM AND INSTALLED DOUBLER IAW 53 -10-00-03. (M) 2 L 7 2 4F A6WE 1998102300668 19981023 00668 WP 1998 10 23 AALA981674 1 19980903 A 5530 PLATE DOUG DC9 DC982 3022082 WP VERTICAL STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - RIGHT OUTBOARD VERTICAL STAB LUG BORE CORRODED AND BLENDED OUT OF LIMITS. LUG REPAIRED IAW 55-30-00-4 AND ESO 805 59, DATED 9-1-98. (M) 2 L 7 2 4F A6WE 1998102300669 19981023 00669 WP 1998 10 23 AALA981673 1 19980903 A 5530 LUG DOUG DC9 DC982 3022082 WP VERTICAL STAB GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - LEFT OUTBOARD VERTICAL STAB LUG FRACE GOUGED AND CORRODED. REPLACED DAMAGED LUG PLATE WITH NEW PLATE FROM STOCK A ND WORKED PER AARD 55-30-00-4. (M) 2 L 7 2 4F A6WE 1998102300670 19981023 00670 WP 1998 10 23 AALA981672 1 19980903 A 5530 PLATE DOUG DC9 DC982 3022082 WP VERTICAL STAB GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - FOUND VERT STAB INBOARD LUG GOUGED AND SCORED LEFT SIDE. REWORKED AND BUSHED LUGS PER AARD 55-30-00-4. (M) 2 L 7 2 4F A6WE 1998102300671 19981023 00671 WP 1998 10 23 AALA981671 1 19980903 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 506 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - FOUND CORROSION ON CUSP AROUND BRACKET. INSTALLED DOUBLER IAW AARD 53-00-01. (M) 2 L 7 2 4F A6WE 1998102300672 19981023 00672 WP 1998 10 23 AALA981670 1 19980903 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 630-637 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - FOUND CORROSION ON CUSP 630-637. INSTALLED DOUBLER IAW AARD 53-00-00-02. (M) 2 L 7 2 4F A6WE 1998102300673 19981023 00673 WP 1998 10 23 AALA981669 1 19980908 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 642-653 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - CUSP MEMBRANE CORRODED FS 642-653 AND 660-670. INSTALLED DOUBLERS IAW 53-00-00-02. (M) 2 L 7 2 4F A6WE 1998102300674 19981023 00674 WP 1998 10 23 98ZZZM783 1 19980908 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 660-670 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - CUSP MEMBRANE CORRODED FS 642-653 AND 660-670. INSTALLED DOUBLERS IAW 53-00-00-02. (M) 2 L 7 2 4F A6WE 1998102300675 19981023 00675 WP 1998 10 23 AALA981668 1 19980903 A 5320 WEB DOUG DC9 DC982 3022082 WP FUSELAGE CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - CUSP CRACKED AT DRAIN LINE UNDER G-1 GALLEY DRAIN PAN. REMOVED DAMAGED AREA, INSTALLED DOUBLER IAW AARD 53-00-00- 02. (M) 2 L 7 2 4F A6WE 1998102300676 19981023 00676 WP 1998 10 23 AALA981667 1 19980903 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP BS 1338 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 431AA 49343 TUL - VERTICAL STIFFENER CORRODED, OUT OF LIMITS. INSTALLED DOUBLER IAW AARD 53-10-00-15 PAGE 1. (M) 2 L 7 2 4F A6WE 1998102300677 19981023 00677 WP 1998 10 23 AALA981666 1 19980906 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 598-712 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 589AA 53252 TUL - CUSP MEMBRANE CORRODED RT SIDE. REMOVED CUSP INSTALLED NEW SECTION IAW 51-10, FS 598-712. (M) 2 L 7 2 4F RT A6WE 1998102300678 19981023 00678 WP 1998 10 23 AALA981665 1 19980906 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 484-503 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 589AA 53252 TUL - FOUND CORROSION ON CUSP RIGHT SIDE. INSTALLED DOUBLER IAW AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 1998102300679 19981023 00679 WP 1998 10 23 AALA981664 1 19980904 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 826-845 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 589AA 53252 TUL - HOLE AND CORROSION IN AND ON CUSP BETWEEN STATION 826 AND 845. REPAIRED IAW AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 1998102300680 19981023 00680 WP 1998 10 23 AALA981663 1 19980906 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1022 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 589AA 53252 TUL - FASTENER HOLE IN ORIGINAL CUSP CRACKED. REPAIR IAW AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 1998102300681 19981023 00681 WP 1998 10 23 AALA981662 1 19980904 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 772-776 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 589AA 53252 TUL - FOUND CORROSION ON CUSP STATION 772 AND 776. REPAIRED IAW AARD 53-00-00-02. (M) 2 L 7 2 4F RT A6WE 1998102300682 19981023 00682 WP 1998 10 23 AALA981609 1 19980831 A 5320 CUSP DOUG DC9 DC982 3022082 WP BS 560 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7531A 49923 TUL - FOUND CORROSION CUSP AT FUSELAGE ATTACH ANGLE FS 560, RT FLOOR SIDE. INSTALLED DOUBLER AT STATION 552 TO STATION 560 PER SRM 53-05. (M) 2 L 7 2 4F A6WE 1998102300683 19981023 00683 NM 1998 10 23 AALA981686 1 19980909 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 874AA AA26 21386 DFW - DURING OVERNIGHT MAINTENANCE, AFT AIR STAIRS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIR EMERGENCY E XIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300684 19981023 00684 NM 1998 10 23 AALA981687 1 19980909 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 874AA 21386 DFW - DURING OVERNIGHT MAINTENANCE, MAIN CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED MAIN CABIN OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300685 19981023 00685 NM 1998 10 23 AALA981676 1 19980908 A 3350 LIGHT BOEING 727 727223 1384074 NM ROW 29-30 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 880AA 21519 ORD - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTING AT ROWS 29 AND 30 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300686 19981023 00686 NM 1998 10 23 AALA981682 1 19980911 A 3350 LIGHT BOEING 727 727227 1384078 NM AFT DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 723AA 20731 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT AFT DOOR MARKER INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300687 19981023 00687 NM 1998 10 23 AALA981534 1 19980816 A 3350 1001141 LIGHT BOEING 727 727227 1384078 NM VENTRAL STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 720AA 2448 20613 DFW - DURING OVERNIGHT MAINTENANCE, VENTRAL STAIR EMERGENCY EXIT LIGHTING INOPERATIVE. REPLACED VENTRAL STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300688 19981023 00688 NM 1998 10 23 AALA981577 1 19980823 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AIR STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 899AA 3404 22015 DFW - DURING OVERNIGHT MAINTENANCE, AIR STAIRS OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AIR STAIRS OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300689 19981023 00689 NM 1998 10 23 AALA981576 1 19980821 A 3397 WIRE BOEING 727 727223 1384074 NM SEAT 3E-21 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 710AA 22467 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS AND COACH, SEATS 3E THROUGH 21 INO PERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP WIRING AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 3 4F A3WE 1998102300690 19981023 00690 NM 1998 10 23 AALA981570 1 19980819 A 3350 LIGHT BOEING 727 727223 1384074 NM R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 844AA 20985 DFW - DURING OVERNIGHT MAINTENANCE, R1 DOOR SLIDE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED R1 DOOR SLIDE EMERGENCY EX IT LIGHT ASSEMBLY SOCKET. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300691 19981023 00691 NM 1998 10 23 AALA981471 1 19980819 A 3350 1000679 LIGHT BOEING 727 727227 1384078 NM AFT GALLEY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 717AA 20610 DFW - DURING OVERNIGHT MAINTENANCE, THE AFT GALLEY SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED AFT GALLEY SERVIC E DOOR EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300692 19981023 00692 NM 1998 10 23 AALA981590 1 19980830 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT ENTRY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 708AA 8372 22465 DFW - DURING OVERNIGHT CHECK, AFT ENTRY EMERGENCY LIGHT INOPERATIVE. REPLACED AFT ENTRY EMERGENCY LIGHT ASSEMLBY. SYST EM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300693 19981023 00693 NM 1998 10 23 AALA981335 1 19980705 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM R1 DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 870AA 21382 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT R1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT R1 DO OR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300694 19981023 00694 NM 1998 10 23 AALA981455 1 19980802 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 871AA 21383 DFW - DURING OVERNIGHT MAINTENANCE, AFT STAIR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR OVERHEAD EM ERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300695 19981023 00695 NM 1998 10 23 AALA981454 1 19980802 A 3350 3005931 LIGHT BOEING 727 727223 1384074 NM CARGO BAY INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6822 19700 DFW - DURING OVERNIGHT CHECK, RIGHT AFT EXTERIOR CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED RIGHT AFT EXTERI OR CARGO DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300696 19981023 00696 NM 1998 10 23 AALA981432 1 19980723 A 3350 CONNECTOR BOEING 727 727223 1384074 NM ROW 10D-15D LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 862AA 21089 MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR PATH LIGHTING AT PAX SEAT ROWS 10D THROUGH 15D INOPERATIVE. RESEATED LOOS E EMERGENCY FLOOR PATH LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998102300697 19981023 00697 EU 1998 10 23 AALA981433 1 19980725 A 3350 2LA00535820 LIGHT FOKKER F28 F28MK0100 4990807 EU RT OVERWING INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1439A 11434 ORD - DURING OVERNIGHT MAINTENANCE, RIGHT OVERWING UPPER EMERGENCY LIGHTS INOPERATIVE. REPLACED RIGHT OVERWING UPPER EM ERGENCY LIGHT ASSEMBLIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998102300698 19981023 00698 EU 1998 10 23 AALA981685 1 19980913 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1423A 11406 DFW - DURING OVERNIGHT CHECK, CABIN EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998102300699 19981023 00699 EU 1998 10 23 AALA981529 1 19980812 A 3350 CONNECTOR FOKKER F28 F28MK0100 4990807 EU CABIN 1ST CLASS FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1413A 11376 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING WOULD NOT ILLUMINATE. REPLACED EMERG ENCY EXIT FLOOR PATH LIGHTING CONNECTOR AT FIRST CLASS LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998102300700 19981023 00700 NM 1998 10 23 USAABB98097 1 19980911 A 5101 STRUCTURE BOEING 767 767201 1385125 NM AIRFRAME LIGHTNING STRIKE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 649US 23901 AMS - FLT 43 - FLIGHT RETURNED TO AMS AFTER TAKEOFF DUE TO LIGHTING STRIKE. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUN D MINOR DAMAGE. THE AIRCRAFT WAS RELEASED FOR FLIGHT. (M) 2 L 7 2 4F RT A1NM 1998102300701 19981023 00701 EU 1998 10 23 AALA981369 1 19980712 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU ROW 8 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1411G 11369 MFE - FLT 1662 - WHILE AT MFE EMERGENCY ESCAPE PATH FLOOR LIGHTING IN FIRST CLASS BACK TO ROW 8 INOPERATIVE. REPAIRED E MERGENCY ESCAPE PATH FLOOR LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998102300702 19981023 00702 NM 1998 10 23 TSAA9833505 1 19980914 A 3350 87310051 LIGHT ASSY BOEING 737 737230 NM NR 5 POS INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED NR 5 POSITION EMERGENCY FLOOR LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998102300703 19981023 00703 WP 1998 10 23 98ZZZM784 1 19980817 A 2780 BRAKE LKHEED 1011 10113851 5265010 WP SLAT ASSYMETRY MALFUNCTIONED A AMTA O OTHER F J FLT CONT AFFECTED WARNING INDICATION DE DESCENT 1 GL 11 193AT 193C1017 UPON LOWER FLAPS TO 4 DEGREES, DURING DESCENT, SLATS STOPPED AT APPROX 15 DEGREES WITH FLAPS/SLATS BRAKE LIGHT ILLUMINAT ED. PERFORMED EMERGENCY PROCEDURES PER AOM. FOUND SLAT ASSYMETRY BRAKE TRIPPED, AND UPPER SCREW JACKS FOUND DRY. BRAK E ASSY RESET AND SCREW JACK LUBRICATED. (M) 2 L 7 3 4F A23WE 1998102300704 19981023 00704 WP 1998 10 23 EISA98215 1 19980909 A 2130 980871173T1111 SWITCH DOUG DC9 DC931 3022065 WP RT PACK INOPERATIVE A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 977ML 8310 47329 RIGHT SIDE A/C PACK SHUT DOWN AT 35,000 FT, CABIN PRESSURE WARNING LIGHT CAME ON, PRESSURE ALTITUDE INDICATED 7000 FT IN THE CABIN. RETURNED TO EL PASO. GENERATED FROM PILOT REPORT. DETERMINED 2 SWITCHES BAD ON A/C SYSTEM REMOVED AND REP LACED 190 DEGREES SWITCH AND COMPRESSOR DISCHARGE SWITCH IAW MM 21-00. (M) 2 L 7 2 4F A6WE 1998102300705 19981023 00705 WP 1998 10 23 98ZZZM785 1 19980909 A 2130 1173T191 SWITCH DOUG DC9 DC931 3022065 WP RT PACK INOPERATIVE A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 977ML 750 47329 RIGHT SIDE A/C PACK SHUT DOWN AT 35,000 FT, CABIN PRESSURE WARNING LIGHT CAME ON, PRESSURE ALTITUDE INDICATED 7000 FT IN THE CABIN. RETURNED TO EL PASO. GENERATED FROM PILOT REPORT. DETERMINED 2 SWITCHES BAD ON A/C SYSTEM REMOVED AND REP LACED 190 DEGREES SWITCH AND COMPRESSOR DISCHARGE SWITCH IAW MM 21-00. (M) 2 L 7 2 4F A6WE 1998102300706 19981023 00706 NM 1998 10 23 F3LA98162 1 19980830 A 2750 CONTROL CABLE BOEING 737 737201 1384454 NM TE FLAP FAILED A F3LA O OTHER J WARNING INDICATION DE DESCENT 1 NM 03 212US 20212 DEN - DURING DESCENT, FLIGHT CREW REPORTED TRAILING EDGE FLAPS STUCK. LEFT FLAP UP, RIGHT FLAP AT 1 DEGREE. LEADING ED GE DEVICES FULL EXTEND. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP ASYMME TRY FAC-4 CABLE. ADJUSTED AND TESTED CABLE PER MM 27-51-301A AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1998102300707 19981023 00707 SO 1998 10 23 C2XA98IA360 1 19980908 A 3397 W502005720N WIRE EMB 120 EMB120RT SO FUSELAGE LT AFT BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 51726 120174 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT REAR EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. MAINT ENANCE REPAIRED A BROKEN WIRE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998102300708 19981023 00708 SO 1998 10 23 C2XA98BT067 1 19980915 A 2810 2810051102 VALVE EMB 145 EMB145 SO RT WING LEAKING A C2XA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 09 14939 0862 145030 BDL-CLE - FLT 4035 - EN ROUTE REPORTED LOSING 600 LBS OF FUEL IN 30 MINUTES. FLIGHT DIVERTED INTO BUF. MAINTENANCE DIS PATCHED AND FOUND A LEAKING FUEL VENT VALVE ON RT SIDE. REMOVED AND REPLACED UNIT AND RETURNED A/C TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998102300709 19981023 00709 SO 1998 10 23 C2XA98BT069 1 19980917 A 3350 7287103501 CONTROL MOD EMB 145 EMB145 SO COCKPIT INOPERATIVE A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12934 145019 BURNING SMELL IN FORWARD HALF OF CABIN WHENEVER LIGHTS ARE ON. EMERGENCY LIGHTS ARE ON WHEN COCKPIT SWITCH IS IN ARMED POSITION. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT CONTROL MODULE, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1998102300710 19981023 00710 EU 1998 10 23 98ZZZM786 1 19980903 A 7712 31024766 SIGNAL COND BAG JETSTM JETSTM3101 1500215 EU RT WING FAILED A CHQA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 11 844JS 13097192 760 AIRCRAFT RETURNED TO FIELD, DUE TO ERRATIC TORQUE AND EGT FLUCTUATION ON LEFT ENGINE. THE BRIDGES WERE SWAPPED ON THE T ORQUE SIGNAL AND CONDITIONER. THE SIGNAL CONDITIONER WAS ADJUSTED. A FUNCTIONAL CHECK OF THE SYSTEM WAS PERFORMED WITH ALL INDICATIONS NORMAL. THE TORQUE SIGNAL CONDITIONER WAS REPLACED AFTER ARRIVING AT MAINTENANCE BASE. THE NEW UNIT W AS ADJUSTED. A FUNCTIONAL CHECK WAS PERFORMED WITH ALL INDICATIONS NORMAL. (M) 2 L 7 2 4T RT A21EU 1998102300711 19981023 00711 NM 1998 10 23 ASAA9810101 1 19980913 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM ROW 14 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ILLUMINATED AT ROW 14. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998102300712 19981023 00712 NM 1998 10 23 98ZZZM787 1 19980913 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM ROW 14 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS REMAINED ILLUMINATED AT ROW 14. REPLACED RECEIVER AND BATTERY PACK, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998102300713 19981023 00713 CE 1998 10 23 MASA98175 1 19980912 A 6123 MS250851 SWITCH BEECH 1900 1900D 1154162 CE COCKPIT OUT OF ADJUST A MASA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 07 126YV UE126 FLT 5331 - RDG-PHL - THE LEFT AUTOFEATHER WOULD NOT ARM ON TAKEOFF, AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE ADJUSTED THE PEDESTAL SWITCHES, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998102300714 19981023 00714 WP 1998 10 23 ASAA9880160 1 19980825 A 5210 INTERLOCK DOUG DC9 DC982 3022082 WP PAX DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 957AS 49126 OAK - PRIOR TO DEPARTURE OF FLT 9001, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE PROPERLY. ADJUSTED THE FORWARD ENTRY ST AIR DOOR INTERLOCK ARM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998102300715 19981023 00715 EA 1998 10 23 MASA98181 1 19980926 A 3350 GE1317 BULB CNDAIR CL600 CL6002B19 EA RT WING FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27185 7185 WHILE PERFORMING ROUTINE MAINTENANCE, FOUND RIGHT AFT WING EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A21EA 1998102300716 19981023 00716 CE 1998 10 23 98ZZZM788 1 19980922 A 3260 H111541 SWITCH BEECH 1900 1900D 1154162 CE LT MLG FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 858CA UE72 AUTOFEATHER OFF ANNUNCIATOR STAYS ON INFLIGHT. LEFT MAIN LANDING GEAR UPLOCK SWITCH FAILED. REPLACED LEFT MAIN LANDING GEAR UPLOCK SWITCH, RETRACTION CHECK SAT IAW CHAPTER 32. (M) 2 L 7 2 4T RT A24CE 1998102300717 19981023 00717 WP 1998 10 23 HALA9800333 1 19980924 A 8012 3927965 VALVE DOUG DC9 DC951 3022051 WP NR 1 ENGINE FAILED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 601AP P2546C 47658 FLT 147 - KOA - NR 1 START VALVE WILL NOT OPEN, NO LIGHT NO PRESSURE DROP NO ENGINE ROTATION. REMOVED AND REPLACED LEFT ENGINE START VALVE. SECURITY CONDITION CHECK, GOOD, GROUND RUN, OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998102300718 19981023 00718 WP 1998 10 23 HALA9800332 1 19980923 A 2911 30591031 ACCUMULATOR DOUG DC9 DC951 3022051 WP HYDRAULIC SYSTEM MALFUNCTIONED A HALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 672MC 74Y8182LA 47661 FLT 167 - HNL - WITH AUX HYD PUJP OFF AND SELECTING RIGHT ENGINE HYD SYSTEM PRESSURE DROPS RAPIDLY TO BELOW 1500 PSI, TH EN SLOWLY CONTINUES DOWN. INSPECTED RIGHT HYD SYSTEM ACCUMULATOR OPS AND LEAK CHECK GOOD. FOUND RIGHT HYD SYSTEM ACCUM ULATOR CORRODED. (M) 2 L 7 2 4F RT A6WE 1998102300719 19981023 00719 NM 1998 10 23 EISA98222 1 19980920 A 3610 VALVE BOEING 727 727223 1384074 NM MLG WW OUT OF POSITION A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6839 20192 NR 3 STRUT OVERHEAT LIGHT ILLUMINATED AFTER APPLYING CLIMB POWER. AIR TURN TACK TO CHP. GENERATED FROM PILOT REPORT. R EPOSITIONED AND TIGHTENED MODULAR VALVE AND CORRESPONDING BULKHEAD CONNECTIONS. OPS CHECK GOOD IAW MM 36. (M) 2 L 7 3 4F A3WE 1998102300720 19981023 00720 WP 1998 10 23 EISA98224 1 19980923 A 3350 20131A BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 950VJ 19518 47564 FORWARD EMERGENCY LIGHTS DIM. FOUND ON POST FLIGHT BY MECHANIC. REMOVED AND REPLACED BATTERY PACK IAW 33-53-0, OPS CHE CK GOOD. (M) 2 L 7 2 4F A6WE 1998102300721 19981023 00721 WP 1998 10 23 EIAA980263 1 19980905 A 5711 SPAR DOUG DC9 DC932F 3022067 WP WS 270 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LEFT WING REAR SPAR UPPER CHORD HORIZONTAL LEG HAS CORROSION AT WS 270. REPAIRED PER SABER TECH D C9-57-138 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1998102300722 19981023 00722 WP 1998 10 23 EIAA980262 1 19980905 A 5315 FLOORBEAM DOUG DC9 DC932F 3022067 WP BS 945 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, BS 945 FLOORBEAM HAS CORROSION AT RBL 48. NRC Y036. REPAIRED PER SABER TECH DC9-53-189 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1998102300723 19981023 00723 WP 1998 10 23 EIAA980261 1 19980905 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 980 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, BS 980 FRAME CRACKED AT LONGERON 17R. NRC 7013. REPAIRED PER SRM 53-05 FIG 32 AND 51-30-02. (M) 2 L 7 2 4F A6WE 1998102300724 19981023 00724 WP 1998 10 23 EIAA980260 1 19980905 A 5210 PAN DOUG DC9 DC932F 3022067 WP CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LOWR AFT CARGO DOOR OUTER PAN HAS MULTIPLE CRACKS AT FORWARD NR 1 STOP. REPLACED DOOR PAN PER SRM 51-10-02. (M) 2 L 7 2 4F A6WE 1998102300725 19981023 00725 WP 1998 10 23 EIAA980259 1 19980905 A 5320 BEAM DOUG DC9 DC932F 3022067 WP BS 50 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LEFT NOSE GEAR SUPPORT BEAM AT FS 50 WAS FOUND CRACKED. NRC E043, E042. REPAIRED BEAM PER SRM 53 -15 FIG 110. (M) 2 L 7 2 4F A6WE 1998102300726 19981023 00726 WP 1998 10 23 AALA981593 1 19980829 A 2120 AIR DIST DOUG DC9 DC982 3022082 WP CABIN SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 470AA 49600 DFW - FLT 1955 - EN ROUTE DFW-SFO, APPROACHING 10,000 FT, CREW NOTED SMOKE ODOR IN COCKPIT, FOLLOWED BY FLIGHT ATTENDANT REPORT OF SMOKE IN CABIN. FAINT VISUAL OF SMOKE IN COCKPIT. STRONG ODOR IN CABIN. RETURNED TO DFW AND LANDED WITHOUT INCIDENT. RAN ENGINES, OPERATED PACKS, INSPECTED ACMS, RECIRCULATING FAN AND ELECTRICAL COMPONENTS IN AIR CONDITIONING . UNABLE TO DUPLICATE OR FIND ANY DISCREPANCIES. AIRCRAFT RETURN TO SERVICE DEPENDENT ON FUNCTIONAL CHECK FLIGHT FINDI NGS. PERFORMED FUNCTIONAL CHECK FLIGHT, WITH NO SMOKE NOTED. (M) 2 L 7 2 4F A6WE 1998102300727 19981023 00727 WP 1998 10 23 EIAA980258 1 19980905 A 5210 PAN DOUG DC9 DC932F 3022067 WP L1 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, L1 DOOR FORWARD PAN AT HINGE CUTOUT CRACKED, NR 1, NR 2, NR 5 AND NR 6 BEAM FORWARD ENDS CRACKED. REPLACED CRACKED PAN, REPAIRED BEAMS PER SRM 52-05 FIG 25, 18 AND 31. (M) 2 L 7 2 4F A6WE 1998102300728 19981023 00728 WP 1998 10 23 EIAA980256 1 19980905 A 5320 991855374 WEB DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, BS 965 RIGHT BULKHEAD FORWARD FACE IS CRACKED AT FASTENER HOLE. NRC Y053. REPAIRED PER SRM 51-10 -03 AND SABER TECH EA DC9-53-191 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1998102300729 19981023 00729 WP 1998 10 23 EIAA980255 1 19980905 A 5320 WEB DOUG DC9 DC932F 3022067 WP BS 737-775 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, WEB CUSP HAS CORROSION AT FS 737-775 LEFT SIDE. NRC W0304. REPLACED CUSP WEB PER SRM 51-10-02, 5 3-11-03. (M) 2 L 7 2 4F A6WE 1998102300730 19981023 00730 WP 1998 10 23 EIAA980254 1 19980905 A 5320 SUPPORT DOUG DC9 DC932F 3022067 WP BS 218 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, VERTICAL SUPPORT HAS HEAVY CORROSION AT BS 218 AT LBL 20. NRC G041. REPAIRED SUPPORT PER SRM 53- 01 FIG 2. (M) 2 L 7 2 4F A6WE 1998102300731 19981023 00731 WP 1998 10 23 EIAA980253 1 19980905 A 5753 SKIN DOUG DC9 DC932F 3022067 WP TE FLAP GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LEFT WING FLAP LEADING EDTE AT XRS 167.5, A GAUGE WAS FOUND IN THE LEADING EDGE SKIN. NRC A071. R EPAIRED PER SABER TECH EA DC9-57-177 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1998102300732 19981023 00732 WP 1998 10 23 EIAA980252 1 19980905 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 639 MISDRILLED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, BS 639 FRAME HAS HOLE DRILLED PARTIALLY THROUGH AT LONGERON 10L. NRC W275. REMOVED DAMAGED AREA AND INSTALLED REPAIR STRAP AND REPAIR PER SRM 51-10-02 AND SABER TECH EA DC9-53-187 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1998102300733 19981023 00733 WP 1998 10 23 EIAA980251 1 19980905 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, LONGERON 17R CRACKED AT BS 965. REPLACED DAMAGED SECTION PER SRM 53-11-3 FIG 4. (M) 2 L 7 2 4F A6WE 1998102300734 19981023 00734 WP 1998 10 23 EIAA980250 1 19980905 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LONGERON 16L CRACKED AT BS 965. NRC Y014. REPLACED DAMAGED SECTION AND INSTALLED SPLICE PER SRM 53-11-3 FIG 4 AND 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1998102900001 19981029 00001 NM 1998 10 29 CALA9801915 1 19981001 A 3350 10617844 BATTERY BOEING 727 727243 138408D NM CARGO DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17402 21265 INSPECTION FOUND RT AFT CARGO DOOR EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REPLACED AND LIGHT WAS RELAMP ED. 2 L 7 3 4F RT A3WE 1998102900002 19981029 00002 WP 1998 10 29 ARWA981016 1 19981008 A 2421 IDG LKHEED 1011 10113851 5265010 WP NR 2 ENGINE FAILED A ARWA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 SO 19 306GB 1138 AIRCRAFT ARRIVED MIAMI WITH NR 2 IDG DISCONNECTED DUE TO THE FACT THAT WHEN NR 2 GENERATOR IS CONNECTED AND NR 1 AND NR 3 GENERATORS BUS TRIPS. REPLACED LOAD CONTROLLER AND GEN BREAKER, STILL HAD PROBLEM, NEEDED AND IDG. PLACED ITEM ON DM I. 2 L 7 3 4F RT A23WE 1998102900003 19981029 00003 WP 1998 10 29 TWAA9816304 1 19981009 A 3350 60030451 POWER SUPPLY DOUG DC9 DC982 3022082 WP SEAT 8 DEF INOPERATIVE A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 940AS 49825 MID CABIN EGRESS LIGHTS WERE ON MOST OF THE FLIGHT REGARDLESS OF SWITCH POSITION. REPLACED BATTERY POWER SUPPLY AT SEAT 8DEF. CHECK-C 6-28-98 MCI. 2 L 7 2 4F A6WE 1998102900004 19981029 00004 NE 1998 10 29 TWAA9816305 2 19981010 A 7261 447245 BEARING DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE GEARBOX DRIVE WORN A TWAA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 CE 05 927TW 49358 1442 DURING CLIMB AT APPROX 3000 FT, THE RT ENG SHUT ITSELF DOWN. FLT RETURNED TO OKC. REPLACED THE ENGINE. CHECK-C 12-10- 97 MCI. UPON ENGINE TEAR DOWN FOUND THE UPPER GEARBOX DRIVE SUPPORT BEARING HAD FAILED, WHICH CAUSED THE N2 DRIVE SHAFT TO SHEAR WITH SUBSEQUENT ENGINE SPOOL DOWN. 2 L 7 2 4F 4 F A6WE E9NE 1998102900005 19981029 00005 WP 1998 10 29 TWAA9816306 1 19981010 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 6-11 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 940AS 49825 DURING MAINT CHECK, EGRESS LIGHTS AT APPROX CABIN ROW 6 THROUGH 11 STAYED ON WHEN THE SWITCH WAS OFF. REPLACED BATTERY PACK. CHECK-C 6-28-98 MCI. 2 L 7 2 4F A6WE 1998102900006 19981029 00006 EA 1998 10 29 JBXA980053 1 19981010 A 5101 STRUCTURE CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE AIRFRAME BIRD STRIKE A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 SO 05 570ML 7206 TAKEOFF ABORTED AT 80 KTS. DUE TO POSSIBLE BIRD STRIKE. INVESTIGATED POSSIBLE BIRD STRIKE IAW 05-51-25. NO DAMAGE NOT ED AT THIS TIME. 2 L 7 2 4F 4 F RT A21EA E15NE 1998102900007 19981029 00007 NM 1998 10 29 SWAA982361 1 19981001 A 5754 SKIN BOEING 737 7373Y0 1384671 NM NR 3 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED EXTENDING FROM FASTENER HOLES ON NR 3 SLAT LOWER SKIN. REMOVED AND REPLACED PER BOEING DRAWING 65C30133. 2 L 7 2 4F RT A16WE 1998102900008 19981029 00008 NM 1998 10 29 UPS98427898 1 19981010 A 2611 SMOKE DETECTOR BOEING 747 747121 1384871 NM CARGO COMPT MALFUNCTIONED A IPXA A B UNSCHED LANDING EMER. DESCENT N FALSE WARNING CR CRUISE 1 SO 01 691UP 19641 LT MAIN DECK CARGO SMOKE DETECT WARNING ON. VISUAL INSPECTED MAIN CARGO DECK AND NOTICED PRESENCE OF FUMES NEAR 14R PAL LET POSITION. DECLARED EMERGENCY AND DIVERTED TO COLD BAY (CDB) EMERGENCY CHECK LIST PERFORMED IAW AOM. INSPECTED AREA AROUND SUSPECTED FUMES FOR DAMAGE OR REMAINING FUMES. NO DEFECTS NOTED. SUSPECT SMOKE DETECTOR 4B ERRONEOUS. DEFERRE D 4B SMOKE DETECTOR PER MEL. 2 L 7 4 4F A20WE 1998102900009 19981029 00009 EU 1998 10 29 98FDEA00647 1 19981010 A 3260 PROX COMPUTER AIRBUS 310 A310203 EU E & E COMPT INOPERATIVE A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 403FE 230 98-247 AFT T/O KRIC, NR 1 ATS SWITCH DROP OFF & WOULD NOT RESET. PROBE HEAT LIGHT FAILED. NR 2 PRESS SYS INOP. NR 2 P RESS DRS WON'T CLOSE. NO CHG DUR FINAL APPROACH INTO RIC. PERFORM BITE CK ON GRND PROX BOX COMPUTER. NO FAULT CODE PR ESENT, RESET. ALL SYS RESET. CK NORM. OK FOR SERV. 2 L 7 2 4F RT A35EU 1998102900010 19981029 00010 1998 10 29 98UAL900488 4 19981002 A 2310 8220330001 HF TRANSCEIVER BOEING 777 777222 1385219 NM NR 2 POSITION FAILED A UALA K NONE O OTHER CR CRUISE 1 WP 29 794UA 4482 26936 EN ROUTE, LOST HIGH FREQUENCY RADIO NR 2. *S/D* THE DRIVERS IN THE TRANSCEIVER FAILED. FAILURE PREVENTED THE TRANSCEI VER FROM TUNING PROPERLY. THE FAILURE IS ATTRIBUTED TO NORMAL COMPONENT FAILURE. NEED FOR ADDITIONAL CORRECTIVE ACTION IS NOT INDICATED AT THIS TIME. 2 L 7 2 4F RT T0001SE 1998102900011 19981029 00011 1998 10 29 SWIA971277 4 19980808 A 3454 RMI EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 FAILED A SWIA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 205SW 120260 AFTER TAKEOFF STARTED SMELLING A STRONG ODOR AND SMOKE COMING FROM AIR CONDITIONING. NOTICED SMOKE ALSO COMING FROM BEH IND PANEL AND RMI CIRCUIT BREAKER POPPED. INSTALLED SERVICEABLE NR 2 RMI. RAN FOR 15 MINUTES. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000001 19981030 00001 NM 1998 10 30 TWAA9817001 1 19981019 A 3350 LIGHT BOEING 767 7673Q8 NM ROW 16-18 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 EGRESS FLOOR LIGHTS WERE FOUND INOPERATIVE LEFT SIDE OF ACFT, ROW 16 TO 18. SECURED LIGHT AT START OF STRIP AND ALL WOR KED. CHECK-C 9-18-98 LAX. 2 L 7 2 4F RT A1NM 1998103000002 19981030 00002 NM 1998 10 30 TWAA9817002 1 19981019 A 3350 3015545 BULB BOEING 767 7673Q8 NM EXTERIOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 634TW 28132 FOUND EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE AFT OF RT WING FLAP AND AT THE NR 2 DOOR ON LT SIDE OF ACFT. RELAMPED B OTH LIGHTS. CHECK-C 9-18-98 LAX. 2 L 7 2 4F RT A1NM 1998103000003 19981030 00003 WP 1998 10 30 VJ9800547 1 19980917 A 5330 99115311 PANEL DOUG DC9 DC932 3022066 WP BS 465-484 LIGHTNING STRIKE A ZZDA K NONE C F.O.D. IN INSP/MAINT 1 SO 15 911VV 47285 LIGHTNING STRIKE LT WINDOW PANEL AT 465 TO 484. REMOVED PANEL, CUT OUT SECTION, FABRICATED DOUBLERS AND FILLERS PLUS TW O INTERNAL DOUBLERS. INSTALLED REPAIR PARTS AND WINDOW PANEL IAW DC9 SRM 53-04 FIG 34. 2 L 7 2 4F A6WE 1998103000004 19981030 00004 WP 1998 10 30 VJ9800548 1 19980916 A 5312 BULKHEAD DOUBLER DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 UPPER RT DOUBLER AT BULKHEAD WEB FS 996 CORRODED. REMOVED CORRODED DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER IAW DC 9 SRM 51-10-3, 51-10-2 AND 53-02 FIG 2. 2 L 7 2 4F A6WE 1998103000005 19981030 00005 WP 1998 10 30 VJ9800549 1 19980912 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 579 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 FUSELAGE SKIN AT FS 579, L30, CORRODED. CUT OUT SECTION OF SKIN, FABRICATED AND INSTALLED EXTERNAL DOUBLER AND FINGER D OUBLERS IAW DC9 SRM 53-04 FIG 12B, 51-10-3, 51-30-1. 2 L 7 2 4F A6WE 1998103000006 19981030 00006 WP 1998 10 30 VJ9800550 1 19980911 A 5320 3678583503 Z SECTION DOUG DC9 DC932 3022066 WP BS 945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 AFT CABIN CENTER Z SECTION AT FS 945, RBL 2-20 AND LBL 2-20, CORRODED FROM BULKHEAD TO BULKHEAD. CORROSION OUT OF LIMIT IAW DC9 SRM 53-01, FIG 1. BROKE CABLE TENSION ON RUNS 129 AND 130 AND REMOVED CABLE BRACKETS. FABRICATED AND INSTALLE D Z SECTION REPAIRS IAW DC9 SRM 53-01, FIG 2. REINSTALLED PULLEY BRACKETS, RETENSIONED CABLE RUNS AND ACCOMPLISHED ADJU STMENT AND TEST IAW DC9 MM 27-40-0. 2 L 7 2 4F A6WE 1998103000007 19981030 00007 WP 1998 10 30 VJ9800551 1 19980911 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 AFT RT LAV FLOORBEAM AT FS 996 CORRODED FROM FUSELAGE TO LAV ENTRANCE. REMOVED RT CABLE RUN AND RT O/B PULLEY TOWER. C UT OUT CORRODED SECTION, TREATED AREA, FABRICATED AND INSTALLED FLOORBEAM SPLICE, FLOORBEAM WEB, ATTACH ANGLE, ANGLES AN D ATTACH ANGLE BRACKET IAW DC9 SRM 53-05, FIG 108. REINSTALLED CABLE RUN AND PULLEY BRACKET. RIG AND OPS CHECKED GOOD IAW DC9 MM 27-20-0. 2 L 7 2 4F A6WE 1998103000008 19981030 00008 WP 1998 10 30 VJ9800552 1 19980910 A 5313 5920319504 LONGERON DOUG DC9 DC932 3022066 WP BS 579 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 FORWARD PIT UNDER AUX TANK AT FS 579, L30, CORRODED. REPLACED L30 AT FS 579 IAW DC9 SRM 53-02 FIG 14. 2 L 7 2 4F A6WE 1998103000009 19981030 00009 WP 1998 10 30 VJ9800553 1 19980910 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 900 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 AFT GALLEY FLOOR PANEL CORRODED. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED NEW HAT SECTIONS AND FLOOR PANEL IAW DC9 SRM 51-20-0, 51-30-2, 53-21-0, FIG 4 AND 51-10-3. 2 L 7 2 4F A6WE 1998103000010 19981030 00010 WP 1998 10 30 VJ9800554 1 19980910 A 5260 3917698504 SKIN DOUG DC9 DC932 3022066 WP VENTRAL STAIRS DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 THE AFT VENTRAL STAIRS CONTAINED 27 DENTS TOO CLOSE TOGETHER IAW DC9 SRM 51-50-1, FIG 1-2A. REPLACED LOWER SKIN AND COR RODED FITTING IAW DC9 SRM 51-30-5, 51-30-0, 51-10-4 AND MM 52-63-0 PG 501. 2 L 7 2 4F A6WE 1998103000011 19981030 00011 WP 1998 10 30 VJ9800555 1 19980909 A 5347 S295597812000 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 917-996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 911VV 47285 FOUND CORROSION AROUND FASTENER HOLES ON SEAT TRACK AT FS 917 TO 996 LT. REPLACED SEAT TRACK IAW DC9 SRM 53-01 FIG 1, 5 1-10-4, 51-30-1 AND 51-10-3. 2 L 7 2 4F A6WE 1998103000012 19981030 00012 WP 1998 10 30 VJ9800557 1 19980914 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 914 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 A CRACK INDICATION AT COUNTER SUNK HOLE FOUND AT FS 194, L22L. CUT OUT CRACKED SECTION OF SKIN, FABRICATED AND INSTALLE D REPAIR DOUBLER AND FILLER IAW DC9 MM 51-00-0, SB 53-251 AND EO 12-5310-29-B1078. 2 L 7 2 4F A6WE 1998103000013 19981030 00013 WP 1998 10 30 VJ9800558 1 19980915 A 5320 591000644 ANGLE DOUG DC9 DC932 3022066 WP FS 598 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 A .75 INCH CRACK FOUND IN STIFFENER AT FS 598 RT SIDE OF FUSELAGE AT FORWARD SECTION OF WING TO FUSELAGE FILLET INTERIOR . REMOVED FILLET AND SKATE ANGLE. FABRICATED AND INSTALLED REPAIR FILLET, INSTALLED NEW SKATE ANGLE IAW DC9 SRM 51-30- 2, 51-10-2, 51-10-4, 51-10-2A, 51-30-5 AND RES 981686. 2 L 7 2 4F A6WE 1998103000014 19981030 00014 NM 1998 10 30 RAAA98B1092 1 19981020 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 7 & 17 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 7 AND 17 FLOOR PROXIMITY EGRESS LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 3 4F A3WE 1998103000015 19981030 00015 NM 1998 10 30 CALA9801975 1 19981017 A 3830 SERVICE PANEL BOEING 727 727224 1384076 NM RT LAVATORY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND RT FORWARD LAV SERVICE PANEL CORRODED AND DRAIN HANDLE WAS BROKEN. THE PANEL WAS REMOVED AND A NEW PAN EL WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2. 2 L 7 3 4F A3WE 1998103000016 19981030 00016 NM 1998 10 30 CALA9801976 1 19981019 A 5720 ANGLE BOEING 727 727224 1384076 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79748 22450 INSPECTION FOUND A .625 INCH CRACK IN LT WING AFT FALSE SPAR LOWER CHORD ANGLE AT BOLT HOLE (FWD OF NR 7 SPOILER ACTUATO R CASTING, WBL 135). THE ANGLE WAS CUT OUT AND A NEW ANGLE, SPLICE AND STRAPS WERE INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998103000017 19981030 00017 NM 1998 10 30 CALA9801977 1 19981018 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND FLOORBEAM T CAP CORRODED AT STA 986.5, WL 208, BBL 0 TO RBL 15. THE T CAP WAS REPLACED IAW SRM 53-00-5 1. 2 L 7 2 4F RT A16WE 1998103000018 19981030 00018 NM 1998 10 30 CALA9801978 1 19981019 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT FASTENER HOLE, STA 1016, WL 208, LBL 5 TO LBL 38. THE FLOORBEAM WAS R EPAIRED IAW ECRA 5310-03450. 2 L 7 2 4F RT A16WE 1998103000019 19981030 00019 NM 1998 10 30 CALA9801979 1 19981019 A 5744 FITTING BOEING 727 727224 1384076 NM NR 4 FLAP TRACK CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69735 20664 INSPECTION FOUND NR 4 FLAP TRACK ATTACH FITTING CORRODED. THE ATTACH FITTING WAS REMOVED AND REPLACED IAW ECRA 5740-018 62 AND MM 32-11-51. 2 L 7 3 4F A3WE 1998103000020 19981030 00020 WP 1998 10 30 CALA9801980 1 19981020 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 237 SCRATCHED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND LT FUSELAGE SKIN SCRATCHED AT STA 237, LONGERON 17L. THE EXISTING DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5 AND ECRA 5330-02445. 2 L 7 2 4F A6WE 1998103000021 19981030 00021 NM 1998 10 30 CALA9801981 1 19981021 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 312-328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12319 23370 INSPECTION FOUND CORROSION ON FLOORBEAM NUT PLATES AND ON DOUBLER AT STA 312 TO 328. THE CORROSION WAS REMOVED AND A RE PAIR WAS INSTALLED IAW SRM 51-70-12. 2 L 7 2 4F RT A16WE 1998103000022 19981030 00022 NM 1998 10 30 CALA9801982 1 19981021 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1006 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 61304 23355 INSPECTION FOUND LT AFT LAV FLOORBEAM CORRODED AT STA 1006, LBL 16 TO LBL 28. REPAIRED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1998103000023 19981030 00023 NM 1998 10 30 CALA9801983 1 19981021 A 5400 CHANNEL BOEING 727 727224 1384076 NM NR 1 PYLON CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 79746 22449 INSPECTION FOUND A 1 INCH CRACK IN NR 1 ENGINE LOWER PYLON PANEL NR 5107 AND A SMALL SECTION MISSING ON THE TRAILING END INNER FRAME U CHANNEL. THE U CHANNEL ON LOWER PYLON PANEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 AND MM 51-20-0. 2 L 7 3 4F A3WE 1998103000024 19981030 00024 WP 1998 10 30 9810289922 1 19981017 A 2120 AIR DIST DOUG DC9 DC932 3022066 WP FLIGHT DECK ODOR A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 945N 47664 DURING CLIMBOUT AT FL29O, BOTH PILOTS AND A FLIGHT ATTENDANT REPORTED AN ELECTRICAL ODOR IN THE FLIGHT DECK. FLIGHT DIV ERTED TO DFW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL WIRING AND COMPONENTS, BOTH FORWARD AND MAIN ELECTR ICAL COMPARTMENTS AND OPERATED BOTH ENGINES ON THE GROUND. NO TROUBLE FOUND. 2 L 7 2 4F A6WE 1998103000025 19981030 00025 NM 1998 10 30 9810296635 1 19980922 A 5400 CHANNEL BOEING 747 747227B 1384888 NM NR 4 PYLON CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 635US 21682 DURING PERIODIC CHECK, FOUND CRACK IN STIFFENER FLANGE ON NR 4 PYLON BL 0, FS 157. REPAIRED PER EA 66-160980, REV A. 2 L 7 4 4F A20WE 1998103000026 19981030 00026 EA 1998 10 30 COMA9860304 1 19981010 A 2750 601R93106505 FLEXSHAFT CNDAIR CL600 CL6002B19 EA NR 5 TE FLAP CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 NR 5 FLAP FLEXSHAFT IN LEFT WING IS HEAVILY CORRODED. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998103000027 19981030 00027 EA 1998 10 30 COMA9860305 1 19981011 A 2710 601R130001 CONTROL SYS CNDAIR CL600 CL6002B19 EA LT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 12600 7022 LEFT AILERON BACKLASH IS OUT OF TOLERANCE. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998103000028 19981030 00028 EA 1998 10 30 COMA9860306 1 19981012 A 2710 601R130002 CONTROL SYS CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 920CA 7022 FOUND RIGHT AILERON BACKLASH TOLERANCE OUT OF LIMITS ON BOTH SYSTEMS. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998103000029 19981030 00029 EA 1998 10 30 COMA9860307 1 19981014 A 2150 78279015 ACM CNDAIR CL600 CL6002B19 EA LEFT FAILED A COMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 964CA 5602 5602 7129 STRONG ODOR COMING FROM PACK SYS. REPLACED LEFT ACM AND LEFT ACM WATER SEPARATOR COALESCER BAG. 2 L 7 2 4F RT A21EA 1998103000030 19981030 00030 EA 1998 10 30 COMA9860308 1 19981016 A 5230 HANDLE CNDAIR CL600 CL6002B19 EA CARGO DOOR NOT LATCHED A COMA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 01 940CA 7048 CARGO DOOR WARNING IN FLIGHT. FOUND CARGO DOOR HANDLE NOT LATCHED. 2 L 7 2 4F RT A21EA 1998103000031 19981030 00031 EA 1998 10 30 COMA9860309 1 19981019 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 719CA 2479 7253 FLAPS FAILED IN FLIGHT AT ZERO DEGREES. REPLACED LEFT BPSU. 2 L 7 2 4F RT A21EA 1998103000032 19981030 00032 NM 1998 10 30 UPS98227950 1 19981007 A 5330 SKIN BOEING 727 727108C 1384039 NM BS 1850 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 1850 ABOVE NR 2 ENGINE RT COWL AFT HINGE POINT. SKIN REPAIRED AT BS 1850 RT PER SRM 54-30-2 FIG 4. 2 L 7 3 4F A3WE 1998103000033 19981030 00033 NM 1998 10 30 UPS98227951 1 19981007 A 5330 SKIN BOEING 727 727108C 1384039 NM BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, LIGHT SURFACE CORROSION ON SKIN BS 1180 BETWEEN S6L AND S7L. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1. REPAIRED IAW SRM 53-30-3 FIG 9. 2 L 7 3 4F A3WE 1998103000034 19981030 00034 NM 1998 10 30 UPS98227952 1 19981005 A 5330 SKIN BOEING 727 727108C 1384039 NM BS 380 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 380 S20R. REPAIR CARRIED OUT IAW SRM 53-30-3. 2 L 7 3 4F A3WE 1998103000035 19981030 00035 NM 1998 10 30 98FDEA00665 1 19981021 A 2710 DISAGREE LIGHT DOUG MD11 MD11F 3023600 NM AILERON MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 609FE 48549 98-254 - DURING FLAP RETRACTION, REVD LEVEL 2 AILERON DISAGREE ALERT. PERF AILERON DEFLECTION ADJUST TEST IAW 27-16-00- 5. TOOK AILERON POS MEAS NEUTRAL, FULL THROW AND DEFLECT POS. COMPARED SENSOR READOUT DURING TEST, ALL WITHIN LIMITS. OPS CK SEVERAL TIMES. NO ALERT APPEAR, CLEAR DMI. 2 L 7 3 4F RT A22WE 1998103000036 19981030 00036 NM 1998 10 30 98FDEA00666 1 19981021 A 2700 MIXER CABLE DOUG MD11 MD11F 3023600 NM WING FOD A A FDEA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 SO 25 581FE 48419 ON T/O LEG A/C REQ ALMOST FULL LT AILERON AND RUDDER TO HOLD HEAD. RETURNED TO AIRPORT. FOUND LATERAL CONT MIXER CABLE JAM WITH FOD CAUSING RT WING SPOILERS TO REMAIN IN UP POSITION. REMOVED FOD AND INSP MIXER AND FOUND NO DAMAGE. SPOIL ER RETRACT WHEN FOD REMOVED. RTS ON FCC 1 AND 2 PASS. VISUAL OPS CK ON ALL FLT CONTROL OK PER MXM AILERON 27-10-00-5, SPOILER 27-60-00-5, FLAPS 27-50-00-5 SLATS 27-80-00-5, ELEV 27-30-00-5, RUD 27-20-00-5. 2 L 7 3 4F RT A22WE 1998103000037 19981030 00037 NM 1998 10 30 98FDEA00667 1 19981022 A 3260 PROX UNIT BOEING 727 72722C 138400F NM RT MLG INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 112FE 19890 98-25 - WHEN GEAR HANDLE RAISED, RT MAIN GEAR IND DOWN (GREEN LIGHT) AND RED TRANSIT LIGHT WAS ILLUM. RECYCLED GEAR IN ACCORD WITH EMER PROC, NO HELP. RETURN TO GFK. AFTER RAISING GEAR AND PUT HANDLE TO OFF POS RED LIGHT OUT AND RIGHT MA IN GREEN LIGHT ILLUM. REMOVED AND REPLACED LANDING GEAR UNIT AS PER MM 32-09-111. REMOVED AND REPLACED RT MAIN DOWN LO CK SWITCH NR S98 AND UPLOCK NR 97 AND LT MAIN GEAR DOWN LOCK SWITCH NR 100 AND UPLOCK SWITCH NR 99 AS PER MM 32-61-21. O PER CK NORM. AC OK FOR SERV. 2 L 7 3 4F A3WE 1998103000038 19981030 00038 WP 1998 10 30 MWEA981008 1 19981021 A 5311 59114481 FRAME DOUG DC9 DC982 3022082 WP BS 1287 CUT A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CUT IN FRAME AT FS 1287 AT LONGERON 5R. MTC FABRICATED AND INSTALLED NEW FRAME. 2 L 7 2 4F A6WE 1998103000039 19981030 00039 WP 1998 10 30 MWEA981009 1 19981021 A 5313 5911429159 LONGERON DOUG DC9 DC982 3022082 WP BS 1338-1418 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CORROSION ON LONGERON 24L AT FS 1338 TO 1418. MTC FABRICATED AND INSTALLED NEW LONGERON. 2 L 7 2 4F A6WE 1998103000040 19981030 00040 WP 1998 10 30 MWEA981010 1 19981021 A 5522 9918480 SKIN DOUG DC9 DC982 3022082 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CORROSION ON LEFT ELEVATOR LOWER SKIN OUTBOARD AFT CORNER BETWEEN SKIN AND DOUBLER. MTC FABRICATED AND INSTALLED NEW DOUBLER. 2 L 7 2 4F A6WE 1998103000041 19981030 00041 WP 1998 10 30 MWEA981011 1 19981021 A 5522 9918480 SKIN DOUG DC9 DC982 3022082 WP LT ELEVATOR CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND LEFT ELEVATOR UPPER AND LOWER SKINS AT TRAILING EDGE OF OUTBOARD CORNER AT STATIC WICK DOUBLER LOCATION WITH BLEND OUTS BEYOND LIMITS. MTC FABRICATED AND INSTALLED DOUBLERS. 2 L 7 2 4F A6WE 1998103000042 19981030 00042 WP 1998 10 30 MWEA981012 1 19981020 A 3350 60030431 BATTERY PACK DOUG DC9 DC915 3022036 WP RT OVERWING DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 900ME 45841 FOUND RIGHT OVERWING EMERGENCY EXIT DOOR LIGHT INOPERATIVE. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998103000043 19981030 00043 WP 1998 10 30 MWEA981013 1 19981020 A 3350 6011777 BATTERY PACK DOUG DC9 DC932 3022066 WP RT NACELLE DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 501ME 47132 FOUND THE RIGHT NACELLE EMERGENCY LIGHT INOPERATIVE. MTC REMOVED AND REPLACED BATTERY PACK. 2 L 7 2 4F A6WE 1998103000044 19981030 00044 WP 1998 10 30 MWEA981014 1 19981019 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 209ME 47730 UPON LANDING FORWARD PASSENGER EMERGENCY SLIDE CAME LOOSE. MTC REINSTALLED FORWARD PASSENGER EMERGENCY SLIDE. 2 L 7 2 4F A6WE 1998103000045 19981030 00045 WP 1998 10 30 ARWA981060 1 19981020 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 175 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 CORROSION ON RIGHT WING TOP AT STATION XFS 175.0. CUT OUT AREA OF CORROSION, FABRICATED DOUBLER, FILLER AND INSTALLED I AW EO SEMAN NR 1028, WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1695. 2 L 7 4 4F 4A25 1998103000054 19981030 00054 SO 1998 10 30 98ZZZX3932 1 19980901 A 7603 555441 CONTROL CABLE PIPER PA34 PA34200 7103405 SO THROTTLE FAILED A BKAA O OTHER O OTHER NR NOT REPORTED 1 SO 13 55443 347350216 DURING FLIGHT, PILOT LOST THE ABILITY TO CONTROL RIGHT ENGINE THROTTLE. THROTTLE CABLE WAS INTERNALLY BROKEN, INNER CAB LE HAD CHAFED ON OUTER HOUSING AT ENGINE END OF CABLE. 1 L 7 2 3O A7SO 1998103000055 19981030 00055 CE 1998 10 30 98ZZZX3933 1 19980903 A 3231 57420057 BELLCRANK CESSNA 402 402C 207590R CE NLG CRACKED A GNXA K NONE O OTHER IN INSP/MAINT 1 SW 01 38CJ 614 402C0023 UPON INSPECTION OF LANDING GEAR SYSTEM, THE NOSE GEAR DOOR BELLCRANK WAS FOUND CRACKED AT LEFT DOOR EAR. THE NOSE GEAR D OORS WERE IMPROPERLY RIGGED CAUSING EXCESIVE STRESS ON BELLCRANK. 1 L 7 2 3O A7CE 1998103000061 19981030 00061 SO 1998 10 30 98ZZZX3939 2 19980821 A 8530 MS9072512 BOLTS BEECH 55 E55 1152732 CE CONT O520 IO520C 17032 SO CYLINDER HEAD CRACKED A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4079S 85 TE1037 299007R FOUND ROCKER COVERS ON NR 2, NR 4, AND NR 6 CYLINDERS CRACKED BY ROCKER SHAFT RETENSION BOLTS. BOLTS WERE ONLY STARTED BY HAND AND COVERS WERE INSTALLED. NR 2, NR 6, AND NR 4 CYLINDER COVERS WERE UNDER TENSION WHEN REMOVED. 1 L 7 2 3O 3 O 3A16 E5CE 1998103000076 19981030 00076 WP 1998 10 30 TWAA9817101 1 19981022 A 3350 408822101 BATTERIES DOUG DC9 DC982 3022082 WP FWD CABIN DISCHARGED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 919TW 49368 OVERHEAD EMERGENCY EXIT LIGHTS AND COCKPIT EMERGENCY LIGHTS WERE REPORTED INOPERATIVE. REPLACED BATTERIES IN FWD POWER SUPPLY. CHECK-C 8-27-98 STL. 2 L 7 2 4F A6WE 1998103000077 19981030 00077 WP 1998 10 30 TWAA9817102 1 19981022 A 3350 CIRCUIT BREAKER DOUG DC9 DC951 3022051 WP CABIN TRIPPED A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 412EA 47733 THE EMERGENCY EGRESS LIGHTS WERE FOUND ILLUMINATED. RESET THE RT TRANSFORMER RECTIFIER NR 1 AND 2 CIRCUIT BREAKERS. CH ECK-C 10-3-98 STL. 2 L 7 2 4F RT A6WE 1998103000078 19981030 00078 WP 1998 10 30 TWAA9817103 1 19981010 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 794 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 414EA 47746 FOUND .25 INCH CRACK INDICATION AT LONGERON 2R, STA 794. REMOVED AND REPLACED CRACKED LONGERON SECTION PER SRM 53-02. C HECK-C 6-9-98 STL. 2 L 7 2 4F RT A6WE 1998103000079 19981030 00079 SO 1998 10 30 LR7A9839 1 19981023 A 5313 3724461R LONGERON LKHEED 382 382G 526414U SO BS 858 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1669 4606 DUE TO CRACKED SLOPING LONGERON DOUBLER RT FS 858. ONE TIME FERRY UNPRESSURIZED FERRY AUTHORIZED IAW COTNEY EDF 60-1. 2 H 7 4 4T A1SO 1998103000080 19981030 00080 EA 1998 10 30 JBXA9800054 1 19981024 A 2750 855101009 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE LEFT FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 576ML 7257 FLAPS FAIL MESSAGE, AIR RETURN TO RDU. REPLACED LEFT BPSU IAW CRJ AMM 27-51-10. OPERATIONAL CHECK OF FLAPS OK. 2 L 7 2 4F 4 F RT A21EA E15NE 1998103000082 19981030 00082 EU 1998 10 30 QXEA9801523 1 19981022 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 5 &10 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 BOI - CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 5 AND 10. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998103000083 19981030 00083 EU 1998 10 30 QXEA9801524 1 19981022 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 &14 FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 498US 11181 BOI - CEILING EMERGENCY LIGHTS INOPERATIVE AT ROWS 8 AND 14. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998103000084 19981030 00084 NM 1998 10 30 98FDEA00668 1 19981021 A 3610 CLAMP BOEING 727 727227 1384078 NM NR 3 ENGINE LEAKING A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION UK UNKNOWN 1 SO 25 494FE 21532 NR 3 ENG STRUT OVERHEAT LIGHT CAME ON WITH RT PK AND NR 3 BLD ON. PER CK LIST TURN NR 3 BLD OFF LIGHT WENT OUT. AFTER THROTTLE UP LIGHT DID NOT COME BACK ON. FOUND ONE OF THE NR 3 ENG BLD VALVE CLAMP LEAK. REMOVED AND REPLACED NR 3 ENG BLD VALVE CLAMP. RAN NR 3 ENG PER JET RUN HANDBOOK. NO LEAK FOUND. 2 L 7 3 4F A3WE 1998103000085 19981030 00085 NE 1998 10 30 98FDEA00670 2 19981023 A 7321 FUEL CONTROL BOEING 727 72725 1384006 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE MALFUNCTIONED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK X ENGINE FLAMEOUT TO TAKEOFF 1 SO 25 503FE 18273 WHILE MAKING FINAL PWR SETTING DURING T/O CSTD PWR, THE NR 3 ENGINE SEIZED. NO UNUSUAL ENGINE READINGS NOTED DURING ACC ELERATED. INDY- IN WORK TO REMOVED AND REPLACED FUEL PUMP NOT A CONFIRMED FIX AS YET. *S/D* REMOVED AND REPLACED FUEL PUMP AND FUEL CONTROL IAW 73-11-1 SEE JOB PROG FORM. RAN NR 3 ENG PER JRH CHPT 6, OPS AND LEAK CK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1998103000086 19981030 00086 NM 1998 10 30 98FDEA00669 1 19981023 A 3260 ACCESSORY UNIT BOEING 727 72722C 138400F NM RT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 112FE 19890 98-258 - AFTER GEAR HANDLE RAISED UP RIGHT MAIN GEAR INDICATED DOWN AND LOCKED. REMOVED AND REPLACED LAND GEAR ANNUNCIA TOR PANEL DUE TO POSS OF PWR MM 33-10-00. REMOVED AND REPLACED LANDING GEAR ACCY UNIT. CYCLED GEAR SEVERAL TIMES AND A LL IND OPERATE NORM. A/C OK FOR SERVICE. 2 L 7 3 4F A3WE 1998103000087 19981030 00087 WP 1998 10 30 ABXA9800917 1 19981019 A 7830 5958782503 LINK DOUG DOUG DC9 DC931 3022065 WP NR 2 ENG TR UNIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 WHILE COMPLYING WITH AD 75-14-06, FOUND UPPER LEFT THRUST REVERSER DRIVER LINK CRACKED ON NR 2 ENGINE. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-05. 2 L 7 2 4F A6WE 1998103000088 19981030 00088 WP 1998 10 30 ABXA9800918 1 19981019 A 7830 5958782503 LINK DOUG DOUG DC9 DC931 3022065 WP NR 2 ENG TR UNIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 924AX 47403 WHILE COMPLYING WITH AD 75-14-06, FOUND LOWER LEFT THRUST REVERSER DRIVER LINK CRACKED ON NR 2 ENGINE. REPLACED THRUST REVERSER DRIVER LINK IAW DC9 MM 78-31-05. 2 L 7 2 4F A6WE 1998103000089 19981030 00089 WP 1998 10 30 ABXA9800919 1 19981019 A 5320 991050313 WEB DOUG DOUG DC9 DC941 302207N WP BS 1013 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 DURING C-CHECK, FOUND CUSP WEB CRACKED AT STATION 1013 RIGHT. REPLACED SECTION OF CUSP WEB IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998103000090 19981030 00090 WP 1998 10 30 ABXA9800920 1 19981019 A 5230 5910141ABX PAN DOUG DOUG DC9 DC941 302207N WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 DURING C-CHECK, FOUND FORWARD LOWER CARGO DOOR PAN CRACKED. REPLACED CARGO DOOR. 2 L 7 2 4F A6WE 1998103000091 19981030 00091 WP 1998 10 30 ABXA9800921 1 19981019 A 5320 99105035 WEB DOUG DOUG DC9 DC941 302207N WP BS 1036 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 DURING C-CHECK, FOUND CUSP WEB STATION 1036 LEFT CRACKED. REPAIRED CUSP WEB IAW ABX REA D953-25107MR. 2 L 7 2 4F A6WE 1998103000092 19981030 00092 WP 1998 10 30 ABXA9800922 1 19981019 A 5320 592266129 ANGLE DOUG DOUG DC9 DC941 302207N WP AFT FUEL TANK CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 DURING C-CHECK, FOUND ANGLE IN AFT FUEL TANK CRACKED. REPAIRED IAW ABX REA D953-25121MR. 2 L 7 2 4F A6WE 1998103000093 19981030 00093 WP 1998 10 30 ABXA9800923 1 19981019 A 5280 591078398 FITTING DOUG DOUG DC9 DC941 302207N WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 951AX 47616 DURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR DOOR ACTUATOR ATTACH FITTING CRACKED. REPLACED RIGHT MAIN LANDING GEAR DO OR. 2 L 7 2 4F A6WE 1998103000094 19981030 00094 WP 1998 10 30 ABXA9800924 1 19980512 A 5400 57695255 RIB DOUG DOUG DC8 DC863F 302198F WP NR 4 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 826AX 46061 NR 4 PYLON UPPER RIB HAD CRACK AT END. REPAIRED IAW DC8 SRM. 2 L 7 4 4F 4A25 1998103000095 19981030 00095 WP 1998 10 30 ABXA9800925 1 19981021 A 5610 5613217507 WINDOW DOUG DOUG DC8 DC863 302198A WP LT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 821AX 46116 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. LUBRICATED WINDOW TRACK. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998103000096 19981030 00096 WP 1998 10 30 ABXA9800926 1 19981021 A 5610 5613217508 WINDOW DOUG DOUG DC8 DC863 302198A WP RT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 821AX 46116 FIRST OFFICER'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. LUBRICATED WINDOW TRACKS. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998103000097 19981030 00097 NM 1998 10 30 DL76G982163 1 19981013 A 5754 114T410337A SKIN BOEING 767 7673P6 1385105 NM NR 3 & 5 TE FLAP DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 1501P 24983 WING NR 3 AND NR 5 SLATS, TRAILING EDGE WEDGES, DELAMINATION REPAIR. THE UPPER SKIN OF THE TRAILING EDGE WEDGES ON THE NR 3 AND NR 5, SLATS WERE FOUND WITH A 2 BY 4 AREA OF DELAMINATION ON EACHWEDGE. THE DISBONDED AREAS WERE TRIMMED AWAY AND REPAIRED PER B767 SRM 57-43-02. THE REPAIRS WERE DOCUMENTED PER ER/A 365861-14AD. 2 L 7 2 4F RT A1NM 1998103000098 19981030 00098 NM 1998 10 30 DL76L982164 1 19981019 A 2530 ELECT OUTLET BOEING 767 767332 1382001 NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 177DN 25122 FIRST CLASS GALLEY, UTILITY OUTLET C/B POPPED. SWITCH ARCED AND SMOKED. ENTIRE UNIT BECAME EXTREMELY HOT. PULLED FORW ARD GALLEY C/B. UNIT COOLED. 2 L 7 2 4F RT A1NM 1998103000099 19981030 00099 NM 1998 10 30 DL72W982165 1 19981019 A 5320 WEB BOEING 727 727247 138408F NM BS 300 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 CORROSION WAS FOUND ON THE UPPER HORIZ PRESSURE WEB DOUBLER OF THE NLG W/W FWD OF BS 315. THE DAMAGE NECESSITATED A NEW SECTION BE SPLICED IN. REPAIRED PER ERA 332271-14. 2 L 7 3 4F A3WE 1998103000101 19981030 00101 NM 1998 10 30 DL72S982170 1 19981020 A 5320 WEB BOEING 727 727232 1384082 NM BS 1240 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 541DA 22387 REF SHIP 541 TPA LTR CHK D1, FOUND 1 IN CRACK AT LIGHTNING HOLE STA 1240 RT VERTICAL WEB TORQUE BOX AREA. REPAIRED PER MM 53-11-10. 2 L 7 3 4F A3WE 1998103000102 19981030 00102 NM 1998 10 30 DLM88982171 1 19981021 A 2530 OVEN DOUG MD88 MD88 3023688 NM GALLEY DIRTY A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 934DL 49721 AFT GALLEY OVENS HAD LIGHT SMOKE AND BURNING ODOR. TURNED OFF ALL OVENS. SMOKE AND ODOR WENT AWAY, DID NOT SMELL LIKE BURNING FOOD. FOUND TAPE ON OVEN INSERTS. REMOVED INSERTS AND CHECKED OVENS, NO SMOKE NOTED. OPS NML. 2 L 7 2 4F RT A6WE 1998103000103 19981030 00103 NM 1998 10 30 DL72W982173 1 19981021 A 2782 SUPPORT BOEING 727 727247 138408F NM NR 1 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 294WA 22112 NR 1 LE FLAP ACT SUPPORT BOX CRACKED AT UPPER IB CORNER. REPAIRED PER MM 57-21-21. 2 L 7 3 4F A3WE 1998103000104 19981030 00104 NM 1998 10 30 DL72S982174 1 19981011 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 1 INCH HOLE WITH CRACKS AT LT ELEVATOR UPPER SKIN AT INBD END. REPAIRED PER 727 SRM 55-20-3 FIG 4. 2 L 7 3 4F A3WE 1998103000105 19981030 00105 WP 1998 10 30 DLL17982176 1 19981021 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113853 5265020 WP DOOR 2L DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 767DA 61439 193H1209 2L OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1998103000106 19981030 00106 NM 1998 10 30 DL757982177 1 19981021 A 3350 SIGN BR9279108 BOEING 757 757232 1384965 NM DOOR 4L LOOSE A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 675DL 25980 LIGHTED SIGN FOR EMERGENCY PATH LIGHTING AT 4L DOOR HANGING OFF WALL BY ITS WIRING. REPLACED LIGHTED SIGN ASSY, OPN NOR MAL. 2 L 7 2 4F RT A2NM 1998103000107 19981030 00107 NM 1998 10 30 DL757982178 1 19981022 A 3350 LIGHT BR9279108 BOEING 757 757232 1384965 NM JUMPSEAT 2R DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 651DL 24391 JUMP SEAT 2R AFT EMERGENCY TRACK LIGHTING FLOOR LIGHT DAMAGED. REPLACED LIGHT ASSY. 2 L 7 2 4F RT A2NM 1998103000108 19981030 00108 NM 1998 10 30 DL72S982180 1 19981021 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1080 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 FUSELAGE SKIN FS 1070-109, STRG 28R, SKIN CORROSION CUTOUT REPAIR. THE FUSELAGE SKIN WAS FOUND CORRODED IN TWO AREAS NE AR S-28R BETWEEN FS 1070 AND 1091. THE CORRODED AREAS WERE CUTOUT WITH A 14.25 BY 3.25 CUTUOUT AND A .75 BY 1.5 CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER, INSTALLED PER B727 SRM 53-30-3, FIG 3 AND DOCUMEN TED PER ER/A 365930-14. 2 L 7 3 4F A3WE 1998103000109 19981030 00109 NM 1998 10 30 DL72W982181 1 19981021 A 3350 LIGHT S106 BOEING 727 727247 138408F NM COCKPIT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2809W 20581 COCKPIT OVERHEAD EMERGENCY LIGHT PACK INOP ON TEST. REPLACED BATTERIES, CKS OK. 2 L 7 3 4F A3WE 1998103000110 19981030 00110 NM 1998 10 30 DL72S982182 1 19981022 A 5743 6562335 SUPPORT BOEING 727 727232 1384082 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 WING LT MLG SUPPORT BEAM, OUTBD LUG AND LOWER SURFACE, REPAIR FOR O/S HOLE BORES. THE OUTBD LUG BORE ON THE LT MLG SUPP ORT BEAM WAS OVERSIZED AND SPOT FACED TO REMOVE CORROSION. SEVERAL OF THE LOWER SURFACE PANEL ATTACH HOLES WERE ALSO OV ERSIZED TO REMOVE CORROSION. THE OVERSIZE REPAIR BUSHING WAS INSTALLED IN THE OVERSIZED LUG LOCATIONS AND REPAIR BUS HINGS OR OVERSIZE FASTENERS WERE INSTALLED IN THE LOWER SURFACE PANEL HOLES. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365 915-14. 2 L 7 3 4F A3WE 1998103000111 19981030 00111 NM 1998 10 30 DL73K982183 1 19981018 A 5343 6546922 FITTING BOEING 737 737232 1384475 NM LT & RT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 318DL 23090 FUSELAGE, RT AND LT MLG SIDE STRUT SUPPORT FITTING, BS 685, REPAIR FOR O/S HOLE BORES. THE LT AND RT MLG SIDE STRUT SUP PORT FITTINGS WERE FOUND WITH CORROSION IN THE LOWER HOLE BORES OF THE FITTINGS. THE HOLES WERE OVERSIZED TO REMOVE THE CORROSION AND LARGER DIA BUSHINGS WERE INSTALLED. THE REPAIRS WERE ACCOMPLISHED PER ER/A 365903-14, REV A. 2 L 7 2 4F RT A16WE 1998103000112 19981030 00112 NM 1998 10 30 DL76S982184 1 19981020 A 5330 146T324112 SKIN BOEING 767 767332 1382001 NM BS 1439 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 122DL 23436 FUSELAGE SKIN, FS 1439 STRG 36L-39L : GROUND DAMAGE REPAIR. THE FUSELAGE SKIN AT FS 1439 BETWEEN STRINGERS 36L AND 39L WAS DENTED OR TORN DUE TO CONTACT WITH GROUND EQUIPMENT. THE DAMAGED SKIN WAS CUTOUT OVER A 17 BY 7 AREA. THE CUTOU T WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 365913-14, REV A. 2 L 7 2 4F RT A1NM 1998103000113 19981030 00113 NM 1998 10 30 DL73K982186 1 19981020 A 5330 SKIN BOEING 737 737232 1384475 NM BS 520 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 302DL 23047 FUSELAGE SKIN, FS 520, S-16L SKIN CRACK REPAIR. THE FUSELAGE SKIN WAS FOUND WITH A CRACK ABOVE STRINGER 16L AT FS 520. THE CRACK WAS CUTOUT AND REPAIRED WITH AN EXTERNAL DOUBLER PER B737 SRM 53-30-3, FIG 1. THE REPAIR WAS DOCUMENTED PER ER/A 365917-14. THE REPAIR EXTENDS UNDER A FAIRING WHICH IS CONSIDERED AN SSI AREA SO THE REPAIR WILL BE HAVE A DA MAGE TOLERANCE ANALYSIS PERFORMED WITHIN 12 MONTHS PER THE REQUIREMENTS OF AD 98-11-03. 2 L 7 2 4F RT A16WE 1998103000114 19981030 00114 NM 1998 10 30 DL757982187 1 19981022 A 2751 TRANSMITTER 18196917 BOEING 757 757232 1384965 NM TE FLAPS FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 603DL 78 22810 T/E FLAP ASSY LIGHT CAME ON AFTER T/O WHEN RAISING FLAPS FROM 10-15 DEG. FLAP NEEDLES SPLIT AND STOPPED. REPLACED T/E FLAP TRANSMITTER. 2 L 7 2 4F RT A2NM 1998103000115 19981030 00115 NM 1998 10 30 DLM88982188 1 19981022 A 2133 CONTROL WHEEL DOUG MD88 MD88 3023688 NM OUT FLOW VALVE JAMMED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 959DL 49978 UNABLE TO PRESSURIZE AIRCRAFT WHILE CLIMBING THROUGH 3000 TO 4000 FT AGL. AUTO 1 AND AUTO 2 FAIL LIGHTS CAME ON AND UNA BLE TO CLOSE OUTFLOW VALVE MANUALLY WITH CONTROL WHEEL PAST THE 20 DEG MARK ON THE FLAP SCALE. FOUND SCREW JAMMING CONT ROL WHEEL IN PEDESTAL. REMOVED SCREW. 2 L 7 2 4F RT A6WE 1998103000116 19981030 00116 NM 1998 10 30 DL72S982189 1 19981022 A 5320 WEB BOEING 727 727232 1384082 NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 REF SHIP 525 TPA LTR CHK A2 .5 INCH CRACK AT RT TORQUE BOX VERT, WEB STA 1233. REPAIRED PER MM 53-11-0 PG 832. 2 L 7 3 4F A3WE 1998103000117 19981030 00117 WP 1998 10 30 ARWA981061 1 19981022 A 5270 WIRE LKHEED 1011 10113851 5265010 WP CARGO DOOR FAILED A ARWA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 308GB 1133 CABIN CARGO DOOR LIGHT ON F/E PANEL ILLUMINATED WHEN DOOR IS CLOSED REPAIRING WIRING AT 5272TBY2 PER MARSHALL WIRING DIA GRAM. OPS NORMAL IAW 52-72-01. 2 L 7 3 4F A23WE 1998103000118 19981030 00118 WP 1998 10 30 ARWA981062 1 19981022 A 3610 CLAMP LKHEED 1011 10113851 5265010 WP AFT FUSELAGE LOOSE A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 308GB 1133 RETURNED TO BLOCKS DUE PNEUMATIC LEAK, AFTER ENGINE START NR 8R CABIN SMOKE DETECTOR ILLUMINATED. UPON VISUAL INSPECTIO N HOT AIR WAS FOUND COMING THROUGH A HOLE IN THE AFT CABIN. FOUND LOOSE CLAMP AT AFT FUSELAGE DUCT COUPLING, RETORQUED CLAMP, OPS NORMAL, NO LEAKS NOTED AS PER M/M 20-20-00 PG 64-08. 2 L 7 3 4F RT A23WE 1998103000119 19981030 00119 WP 1998 10 30 CKSA98606 1 19981013 A 5220 STOP DOUG DC8 DC862 3021970 WP LT AFT EMER EXIT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 LT AFT EMERGENCY WINDOW STOP LWR PART EXTERNAL SKIN SHOWS LEVEL 2 CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REMOVED AND REPLACED STOP IAW SRM 51-3-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA P ERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 36537, CPCP TASK CARD NUMBER 5690-0559. 2 L 7 4 4F 4A25 1998103000120 19981030 00120 WP 1998 10 30 CKSA98607 1 19981013 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 761 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 107R-0551 FOUND RT WING L/E CORRODED AT ZONE 7R, STA XW 761. REMOVED COR ROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW 57-2-0. REPAIRED AFFECTED AREA IAW SRM 57-2-1. FOUND DURING D CH ECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBE R 36727, CPCP TASK CARD NUMBER 107R-0551. 2 L 7 4 4F 4A25 1998103000121 19981030 00121 WP 1998 10 30 CKSA98608 1 19981013 A 5347 SEAT TRACK DOUG DC8 DC862 3021970 WP FLIGHT COMPT CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 4640-0551, FOUND SEAT TRACK CORRODED AT FLT COMPARTMENT MID AREA. REMOVE D CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-3. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-3-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTI NE TASK CARD NUMBER 37041, CPCP TASK CARD NUMBER 4640-0551. 2 L 7 4 4F 4A25 1998103000122 19981030 00122 WP 1998 10 30 CKSA98609 1 19981013 A 5312 BLKHD DOUBLER DOUG DC8 DC862 3021970 WP BS 1200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 559R-0551, FOUND AFT BAGGAGE COMPT BULKHEAD DOUBLER CORRODED LOCATION STA 1200, LONGERON 23R TO LONGERON 24R, CORROSION FOUND TO BE LOCAL. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. INSTALLED DOUBLER ANGLE IAW SRM 53-2-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLIS HMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 37023, CPCP TASK CARD NUMBER 559R-0 551. 2 L 7 4 4F 4A25 1998103000123 19981030 00123 WP 1998 10 30 CKSA98610 1 19981013 A 5312 BLKHD DOUBLER DOUG DC8 DC862 3021970 WP BS 1218 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD 559R-0551, FOUND AFT BAGGAGE COMPARTMENT BULKHEAD DOUBLER CORRODED, FS 1218 BETW EEN LONGERON 24R AND 25R. REMOVED CORROSION IAW SRM 51-1-8, FOUND OUT OF LIMITS IAW SRM 53-2-0. INSTALLED NEW ANGLE I AW SRM 51-3-0, 51-1-21. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER N UMBER 818-166, NON ROUTINE TASK CARD NUMBER 37122, CPCP TASK CARD NUMBER 559R-0551. 2 L 7 4 4F 4A25 1998103000124 19981030 00124 WP 1998 10 30 CKSA98611 1 19981013 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 872 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 RT MLG W/W LONGERON 24 FITTING CRACKED 3.5 FROM STA 872 THROUGH STA 877. INSPECTED W/EDDY CURRENT METHOD, FOUND CRACK T O BE 5 .5 LONG IAW DP54751 ITEM 4-7 FIG 51, RECORDED ON M-40 38223. REPAIRED LONGERON FITTING IAW SRM 53-2-2. FOUND DU RING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK C ARD NUMBER 37626. 2 L 7 4 4F 4A25 1998103000125 19981030 00125 WP 1998 10 30 CKSA98612 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD 376L-1-0551, FOUND LT HORIZ STAB T/E PANEL UPPER AND LOWER PART SOWING LEVEL 2 C ORROSION BETWEEN STA XE29 TO STA XE73. REPLACED UPPER PANEL AT LT HORIZ STAB, STA XE25 TO STA XE312 DUE TO OTHER ADJACE NT AREAS AFFECTED (REFER TO M-40'S 38152, 38153, 38154 AND 38155) IAW SRM 55-2-0. FOUND DURING D CHECK, ROUTINE CPCP TA SK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38156, CPCP TASK C ARD NUMBER 376L-0551. 2 L 7 4 4F 4A25 1998103000126 19981030 00126 WP 1998 10 30 CKSA98613 1 19981013 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 395 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 573R-0551, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED 2 AT STA 395.00 L ONGERON 21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMEN T AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 37870, CPCP TASK CARD NUMBER 573R-0551. 2 L 7 4 4F 4A25 1998103000127 19981030 00127 WP 1998 10 30 CKSA98614 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 376L-0551, FOUND LT HORIZ STAB PANEL UPPER AND LWR SURFACE SHOWS LEVEL 2 CORROSION BETWEEN STA XE 73 AND STA XE 149. REPLACED PANEL IAW SRM 55-2-0 (SEE M-40 NUMER 38156 FOR DETAILS). FOUND DU RING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK C ARD NUMBER 38155, CPCP TASK CARD NUMBER 376L-0551. 2 L 7 4 4F 4A25 1998103000128 19981030 00128 WP 1998 10 30 CKSA98615 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK CARD 376L-0551, FOUND L HORIZ STAB UPPER AND LWR SFC SKIN PANEL SHOWS LEVEL 2 CORROSI ON BETWEEN STA XE149 TO STA XE221. REPLACED PANEL IAW SRM 55-2-0 (REFER TO M-40 38156 FOR DETAILS). FOUND DURING D CHE CK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38154, CPCP TASK CARD NUMBER 376L-0551. 2 L 7 4 4F 4A25 1998103000129 19981030 00129 WP 1998 10 30 CKSA98616 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 376L-0551, FOUND LEVEL 2 CORROSION AT L HORIZ STAB UPPER AND LWR SFC SKIN PANEL BETWE EN STA XE221 AND XE272. REPLACED PANEL IAW SRM 55-2-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38153, CPCP TASK CARD NUMBER 376L-0551. 2 L 7 4 4F 4A25 1998103000130 19981030 00130 WP 1998 10 30 CKSA98617 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 376L-0551, FOUND L HORIZ STAB T/E UPPER AND LWR SFC SKIN PANELS SHOWS LEVEL 2 CORROSI ON BETWEEEN STA XE 272 AND XE 312. REPLACED PANEL IAW SRM 55-2-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPL ISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38152, CPCP TASK CARD NUMBER 376L -0551. 2 L 7 4 4F 4A25 1998103000131 19981030 00131 WP 1998 10 30 CKSA98618 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 376R-0551, FOUND R HORIZ STAB T/E UPPER AND LWR SFC SKIN PANELS SHOWS LEVEL 2 CORROSI ON BETWEEEN STA XE 147.906 AND XE 219.979. REPLACED PANEL IAW SRM 55-2-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38100, CPCP TASK CARD NUM BER 376R-0551. 2 L 7 4 4F 4A25 1998103000132 19981030 00132 WP 1998 10 30 CKSA98619 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 376R-0551, FOUND L HORIZ STAB T/E UPPER AND LWR SFC SKIN PANELS SHOWS LEVEL 2 CORROSI ON BETWEEEN STA XE 75.672 AND XE 147.906. REPLACED PANEL IAW SRM 55-2-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38099, CPCP TASK CARD NUMB ER 376R-0551. 2 L 7 4 4F 4A25 1998103000133 19981030 00133 WP 1998 10 30 CKSA98620 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 376R-0551, FOUND L HORIZ STAB T/E UPPER AND LWR SFC SKIN PANELS SHOWS LEVEL 2 CORROSI ON BETWEEEN STA XE 270 AND XE 312.500. REPLACED PANEL IAW SRM 55-2-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACC OMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38087, CPCP TASK CARD NUMBER 376R-0551. 2 L 7 4 4F 4A25 1998103000134 19981030 00134 WP 1998 10 30 CKSA98621 1 19981013 A 5512 SKIN DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 376R-0551, FOUND L HORIZ STAB T/E UPPER AND LWR SFC SKIN PANELS SHOWS LEVEL 2 CORROSI ON BETWEEEN STA XE 219.979 AND XE 270.979. REPLACED PANEL IAW SRM 55-2-0. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 38086, CPCP TASK CARD NUM BER 376R-0551. 2 L 7 4 4F 4A25 1998103000135 19981030 00135 1998 10 30 CKSA98622 4 19981013 A 2360 BASE DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 376R-0551, FOUND RT HORIZ STAB T/E STATIC DISCHARGER BASES (2 EACH) SHOW LEVEL 2 CORR OSION. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAW SRM 55-2-0. REMOVED AND REPLACED STATIC DISCHARGER B ASES IAW SRM 51-1-21. FOUND DURING D CHECK, ROUTINE CPCP TASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUM BER 818-166, NON ROUTINE TASK CARD NUMBER 38032, CPCP TASK CARD NUMBER 376R-0551. 2 L 7 4 4F 4A25 1998103000136 19981030 00136 WP 1998 10 30 CKSA98623 1 19981013 A 5320 BASE DOUG DC8 DC862 3021970 WP GALLEY CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 818CK 45961 DURING ACCOMPLISHMENT OF CPCP TASK 5670-0551, FOUND CREW GALLEY BASE SHOWS LEVEL 2 CORROSION. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. REPLACED BASE IAW SRM 51-3-0. FOUND DURING D CHECK, ROUTINE CPCP T ASK CARD ACCOMPLISHMENT AT SIMON (LIMA PERU). WORK ORDER NUMBER 818-166, NON ROUTINE TASK CARD NUMBER 26270, CPCP TASK CARD NUMBER 5670-0551. 2 L 7 4 4F 4A25 1998103000137 19981030 00137 WP 1998 10 30 TC8A98069 1 19981022 A 2424 51202011 VOLTAGE REG DOUG DC8 DC8F54 3021926 WP NR 2 FAILED A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 802CK 45679 TRIP# 02707. DISCREP: #2 GENERATOR SHOWS UNBALANCED LOAD. CORR. ACTION: TRANSFERRED TO DMI 8809 AS PER ME L 24-1 CAT C. PLACARD INSTALLED, SPECIAL PROCEDURES COMPLIED WITH. 10/27/98 REMOVED AND REPLACED VOLTAGE REGULATOR IAW 2 4-5-11, OPS CHECKS GOOD, CLEARS DMI 8809. 2 L 7 4 4F 4A25 1998103000138 19981030 00138 WP 1998 10 30 TC8A98070 1 19981022 A 3231 47749341 BRACKETS DOUG DC8 DC8F55 3021928 WP LT MLG BROKEN A TC8A A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 GL 23 182SK 45817 TRIP NR 02705, AFTER T/O, GEAR UNSAFE LIGHT REMAINED ON, GEAR RECYLED, LIGHT REMAINED ON. RETURNED TO KDAY. FOUND LT M LG I/B DOOR UPLATCH ROLLER BRACKETS BROKEN. REMOVED AND REPLACED SAME. OPERATED DOOR SEVERAL TIMES, NO DEFECTS NOTED O R INDICATION PROBLEMS NOTED IAW DC8 MM 32-6-3. 2 L 7 4 4F 4A25 1998103000139 19981030 00139 WP 1998 10 30 TC8A98071 1 19981023 A 5280 DOOR DOUG DC8 DC8F55 3021928 WP LT MLG BENT A TC8A A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 182SK 45817 TRIP NR 02716, AFTER TAKEOFF, LANDING GEAR UNSAFE LIGHT REMAINED ON. RECYLED GEAR 2 TIMES, LIGHT STILL ON. DURING UPLA TCH CHECK SLIGHT VIBRATION AS IF GEAR NOT LATCHED UP. PERFORMED CHECKLIST ITEMS AND RETURNED TO KDAY. FOUND FOWARD OUT BOARD CORNER OF LEFT MAIN GEAR DOOR SLIGHTLY BENT. STRAIGHTENED AND OPS CHECKED IAW 32-1-4, NO DEFECTS NOTED AT THIS TI ME. 2 L 7 4 4F 4A25 1998103000140 19981030 00140 WP 1998 10 30 TC8A98072 1 19981023 A 2612 FIRE LOOP DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE LOOSE A TC8A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 182SK 45817 642688 TRIP# 02716. DISCREP: ON CLIMB OUT, ENGINE FIRE #3 ENGINE. PERFORMED CHECK LIST AND RETURNED TO KDAY FOR LANDING. S ECURED LOOSE FIRE WARNING LOOP IN BOMB BAY AREA, OPS CHECKS NORMAL IAW MM 26-2-0. 2 L 7 4 4F 4 F 4A25 1E8 1998103000168 19981030 00168 WP 1998 10 30 VJ9800559 1 19980917 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-389 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 DENTS BETWEEN FS 313 - 362, L23R - L25R, WERE DETERMINED TO BE TOO CLOSE TOGETHER IAW DC9 SRM 53-04, FIG 38, CONDITION 1 B, NOTE 3. FABRICATED AND INSTALLED NEW SKIN FROM FS 229 - 389. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 5 1-30-1, 51-30-9, 51-20-0, 51-10-3, MM 25-52-3 AND RES 981616. 2 L 7 2 4F A6WE 1998103000169 19981030 00169 NM 1998 10 30 VJ9800560 1 19981024 A 3350 6013211 POWER SUPPLY BOEING 737 7372P6 NM EXTERIOR INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 EICJW 21355 LT AFT EXTERIOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY AND BATTERY PACK ASSY; OPS CHECKS NORMAL. 2 L 7 2 4F RT A16WE 1998103000170 19981030 00170 NM 1998 10 30 AWXA9800214 1 19981017 A 2841 GAUGE BOEING 737 737277 1384570 NM NR 2 FUEL SYST INOP A AWXA O OTHER N FALSE WARNING AP APPROACH 1 WP 28 188AW 22655 ON APPROACH, RIGHT FUEL QTY INDICATION WENT TO ZERO, AFTER LANDING GAUGE RETURNED TO 7200 LBS. VERIFIED NO FUEL LEAKS, C/W MEL PROCEDURES 28-06, NR 2 FUEL GAUGE INOP. RESET C/B, PERFORMED FUEL QTY TEST, OPS CHECK NORMAL. 2 L 7 2 4F RT A16WE 1998103000171 19981030 00171 SO 1998 10 30 RAAA98E4020 1 19981022 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 22 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 PAX ROW 22 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998103000172 19981030 00172 SO 1998 10 30 COMA9810239 1 19981019 A 3246 314461 WHEEL EMB 120 EMB120RT SO RT MLG FAILED A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 257CA 17043 1248 DURING TAXI OUT, PILOT OF ANOTHER AIRCRAFT REPORTED A PROBLEM WITH THE RIGHT MAIN INBOARD TIRE. REPLACED RIGHT INBOARD WHEEL ASSEMBLY. ALSO, REPLACED OUTBOARD WHEEL ASSEMBLY AS A PRECAUTIONARY MEASURE. 2 L 7 2 4T RT A31SO 1998103000173 19981030 00173 SO 1998 10 30 COMA9810240 1 19981020 A 2820 12008717 LINE EMB 120 EMB120RT SO RT MLG WW LEAKING A COMA E ENGINE SHUTDOWN K FLUID LOSS TX TAXI/GRND HDL 1 SO 01 241CA 1211 WHILE RUNNING NR 2 ENGINE, IT STARTED LEAKING FUEL. REPLACED RIGHT VENT VALVE MOTIVE FLOW LINE. 2 L 7 2 4T RT A31SO 1998103000174 19981030 00174 SO 1998 10 30 COMA9810241 1 19981022 A 3350 10130115 SIGN EMB 120 EMB120RT SO SEAT 5A BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 256CA 1245 CREW REPORTED EMERGENCY EXIT SIGN BROKEN. REPLACED EXIT SIGN AT SEAT 5A. 2 L 7 2 4T RT A31SO 1998103000175 19981030 00175 EA 1998 10 30 COMA9860310 1 19981017 A 2910 6017523881 TUBE CNDAIR CL600 CL6002B19 EA NR 1 ENGINE LEAKING A COMA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 721CA 7259 INFLIGHT GOT HYD NR 1, ZERO PRESSURE MESSAGE. CHECKED HYD GAGE, FOUND NO PRESS URE. FIFTEEN MINUTES ELAPSED FROM FIRST INDICATION TO ENGINE SHUTDOWN. REPLACED NR 1 ENGINE HYDRAULIC PRESSURE LINE FROM THE ENGINE TO NR 1 RESERVOIR. 2 L 7 2 4F RT A21EA 1998103000176 19981030 00176 EA 1998 10 30 COMA9860311 1 19981019 A 2750 RETRACT MECH CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 924CA 7026 WHEN FLAPS RETRACTED AFTER LANDING, 'FLAPS FAIL' ILLUMINATED WITH SELECTOR AT 20 DEGREES INDICATOR AT 30 DEGREES. PERFO RMED EO 27-045AD BY INSPECTION OF FLAPS AND RESET OF FLAP SYSTEM. TRANSFERRED TO DEFERRED PER GMM 4-3 CAT 1 AND AD 98-2 0-01. 2 L 7 2 4F RT A21EA 1998103000177 19981030 00177 EA 1998 10 30 COMA9860312 1 19981020 A 2751 WARNING SYS CNDAIR CL600 CL6002B19 EA TE FLAPS ACTIVATED A COMA O OTHER N FALSE WARNING UK UNKNOWN 1 SO 01 912CA 7011 FLAP FAIL MESSAGE ILLUMINATED IN FLIGHT. FLAPS REMAINED AT 'ZERO'. PERFORMED EO 27-045AD BY VISUALLY INSPECTING FLAPS AND PERFORMING OPS CHECK OF FLAP SYSTEM IAW AD-98-01 PARA (B) 123 (ABC BE) DEFERRED PER GMM 4-3 CAT 1 AND AD 98-20-01 PA RAGRAPH (B). 2 L 7 2 4F RT A21EA 1998103000178 19981030 00178 EA 1998 10 30 COMA9860313 1 19981018 A 3610 32895902 VALVE CNDAIR CL600 CL6002B19 EA LEFT STUCK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 LEFT 14TH STAGE DUCT VALVE FAILED IN OPEN POSITION. REPLACED VALVE. 2 L 7 2 4F RT A21EA 1998103000179 19981030 00179 EA 1998 10 30 COMA9860314 1 19981021 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 964CA 7129 CREW REPORTED AN OVERHEAD EXIT EMERGENCY LIGHT OUT. REPLACED BULB. 2 L 7 2 4F RT A21EA 1998103000180 19981030 00180 EA 1998 10 30 COMA9860315 1 19981018 A 5751 601R130001 SKIN CNDAIR CL600 CL6002B19 EA LT AILERON DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 LEFT AILERON, LOWER OUTER SKIN IS DAMAGED. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998103000181 19981030 00181 EA 1998 10 30 COMA9860316 1 19981018 A 2710 601R130002 CONTROLS CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 RIGHT AILERON FAILED BACKLASH CHECKS. REPLACED AILERON. 2 L 7 2 4F RT A21EA 1998103000182 19981030 00182 EA 1998 10 30 COMA9860317 1 19981018 A 7920 601631009 OIL LINE CNDAIR CL600 CL6002B19 EA LT ENGINE TWISTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 LEFT ENGINE OIL SUPPLY LINE AT OIL FILL TANK IS TWISTED. REPLACED LINE. 2 L 7 2 4F RT A21EA 1998103000183 19981030 00183 EA 1998 10 30 COMA9860318 1 19981014 A 4980 601R9720913 DUCT CNDAIR CL600 CL6002B19 EA APU COMPT CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 941CA 7050 APU EXHAUST SUPPORT DUCT CHAFED. REPLACED DUCT. 2 L 7 2 4F RT A21EA 1998103000184 19981030 00184 EA 1998 10 30 COMA9860319 1 19981018 A 5532 600211342 PANEL CNDAIR CL600 CL6002B19 EA VERT STAB CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 7163 RIGHT LOWER VISOR PANEL CRACKED. REPLACED PANEL. 2 L 7 2 4F RT A21EA 1998103000185 19981030 00185 EA 1998 10 30 COMA9860320 1 19981018 A 2750 601R93106107 FLEX DRIVE CNDAIR CL600 CL6002B19 EA LT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 7163 LEFT FLAP FLEX DRIVE NR 1 IS BAD. STRAIN SEPARATED. REPLACED DRIVE SHAFT. 2 L 7 2 4F RT A21EA 1998103000186 19981030 00186 EA 1998 10 30 COMA9860321 1 19981018 A 2750 601R93106107 FLEX DRIVE CNDAIR CL600 CL6002B19 EA RT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 7163 RIGHT FLAP FLEX DRIVE CABLE NR 1 IS BAD. STRAIN SEPARATED. REPLACED FLEX DRIVE CABLE. 2 L 7 2 4F RT A21EA 1998103000187 19981030 00187 EA 1998 10 30 COMA9860322 1 19981018 A 4980 1079900004 CLAMP CNDAIR CL600 CL6002B19 EA APU COMPT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 7163 APU SUPPORT DUCT CLAMP CHAFED AND CRACKED. REPLACED CLAMP. 2 L 7 2 4F RT A21EA 1998103000188 19981030 00188 EA 1998 10 30 COMA9860323 1 19981018 A 2612 26212000 FIRE LOOP CNDAIR CL600 CL6002B19 EA RIGHT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 981CA 7163 FOUND RIGHT EXHAUST NOZZLE SENSING ELEMENT TO HAVE A BROKEN TIP. REPLACED SENSING ELEMENT. 2 L 7 2 4F RT A21EA 1998103000189 19981030 00189 NE 1998 10 30 COMA9860324 2 19981021 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 1 VIBRATION A COMA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 SO 01 969CA 7141 807425 NR 1 ENGINE N1 FAN VIB PEAKED AT 4.0 DURING CRUISE IN ICING CONDITIONS. ALL INDICATIONS IS NORMAL RANGE UPON LANDING. I NSPECTED FAN INLET AND TURBINE, NO DAMAGE WAS NOTED. OPERATED LEFT ENGINE AT VARIOUS POWER SETTINGS FOR 25 MINUTES. LE FT ENGINE N1 VIBS WERE .6. SUBMITTER STATES: SUSPECT ICE ON SPINNER IN FLIGHT WAS THE CAUSE OF THE PROBLEM. 2 L 7 2 4F 4 F RT A21EA E15NE 1998103000190 19981030 00190 NM 1998 10 30 UPS98227975 1 19981025 A 3350 LIGHT BOEING 727 72725C 138400H NM SEAT 11 L INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, EEL AT SEAT 11L IS INOP. INSTALLED EMERGENCY EXIT LIGHT, OPS CK OK (P/N 87-1001-71) (S/N 1018) ON, (S/N 1041) OFF. 2 L 7 3 4F A3WE 1998103000191 19981030 00191 NM 1998 10 30 UPS98227977 1 19981023 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 2 & 4 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, ROW 2 AND 4 EMERGENCY LIGHT FAILED. REPLACED ROW 2 AND 4 BATT PACKS, OPS CHECK NORMAL. 2 L 7 3 4F A3WE 1998103000192 19981030 00192 NM 1998 10 30 UPS98227978 1 19981023 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 6 & 13 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, ROW 6 AND 13 EMERGENCY LIGHT FAILED. REMOVED AND REPLACED BATT PACK AS ABOVE, OPS NORMAL. 2 L 7 3 4F A3WE 1998103000193 19981030 00193 NM 1998 10 30 UPS98227979 1 19981023 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM ROW 18 DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, ROW 18 AND BOTH EEL INOP. REMOVED AND REPLACED BATT PACKS, OPS NORMAL. 2 L 7 3 4F A3WE 1998103000194 19981030 00194 NM 1998 10 30 UPS98227980 1 19981023 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM MAIN ENTRY DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, FWD MAIN ENTRY EEL INOP. REMOVED AND REPLACED EEL ASSY, OPS CHECK GOOD (P/N 96-3-1030-1). 2 L 7 3 4F A3WE 1998103000195 19981030 00195 WP 1998 10 30 UPS98827956 1 19981010 A 5320 56155309 STIFFENER DOUG DC8 DC871F 302199D WP BS 8 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, A/C COMPT FS 8 AT LONG 28R, THE VERTICAL STIFFENER IS CORRODED. REMOVED, FABRICATED AND REPLACED VER TICAL STIFFENER IAW DWG 5615530 AND SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998103000196 19981030 00196 WP 1998 10 30 UPS98827957 1 19981011 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, TR WING UPPER SKIN AT XRS 74 AND STR 12 HAS A STRESS CORROSION CRACK. CUT OUT DAMAGE AND REPAIRED IA W SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 1998103000197 19981030 00197 WP 1998 10 30 UPS98827958 1 19981011 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 258 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING L/E SKIN AT THE L/E XW 258 IS CRACKED AT A FASTENER HOLE. STOP DRILLED CRACK AND REPAIRED IA W SRM 57-2-1 FIG 2H. 2 L 7 4 4F RT 4A25 1998103000198 19981030 00198 WP 1998 10 30 UPS98827959 1 19981011 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 622.5&629.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING L/E UPPER SKIN XFS 622.5 AND 628.75 IS CRACKED. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57- 2-1 FIG 38. 2 L 7 4 4F RT 4A25 1998103000199 19981030 00199 WP 1998 10 30 UPS98827960 1 19981011 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 163.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING L/E LWR SKIN AT XFS 163.75 IS CRACKED JUST FWD OF THE REPAIR DOUBLER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2A. 2 L 7 4 4F RT 4A25 1998103000200 19981030 00200 WP 1998 10 30 UPS98827961 1 19981011 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 653.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING L/E RIB AT XFS 653.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998103000201 19981030 00201 WP 1998 10 30 UPS98827962 1 19981011 A 5720 97532938 ANGLE DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING L/E VERTICAL ANGE JUST I/B OF XS 250.089 AND AFT OF THE SLOT IS CRACKED AT THE LWR END. REMO VED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998103000202 19981030 00202 WP 1998 10 30 UPS98827963 1 19981011 A 5320 36469561N FITTING DOUG DC8 DC871F 302199D WP BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, FITTING LT W/W AT LONG 23L FS 960 HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 F IG 8. 2 L 7 4 4F RT 4A25 1998103000203 19981030 00203 WP 1998 10 30 UPS98827964 1 19981013 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 691.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, LT WING L/E RIB AT XFS 691.250 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998103000204 19981030 00204 WP 1998 10 30 UPS98827965 1 19981013 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 385.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, LT WING L/E RIB AT XFS 385.25 IS CRACKED 16 FWD OF THE T/E. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998103000205 19981030 00205 WP 1998 10 30 UPS98827966 1 19981013 A 5720 97532937 ANGLE DOUG DC8 DC871F 302199D WP LT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, LT WING L/E VERTICAL FWD ANGLE CRACKED AT O/B END OF THE I/B SLOT. REMOVED, FABRICATED AND REPLACED VERTICAL ANGLE IAW DWG 9753293 AND SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998103000206 19981030 00206 WP 1998 10 30 UPS98827967 1 19981013 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 250.09 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, LT WING L/E RIB AT XS 250.089 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW S RM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998103000207 19981030 00207 WP 1998 10 30 UPS98827968 1 19981013 A 5210 WEB DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, FWD ENTRY DOOR INNER SKIN AT THE BAYONET CUTOUT IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SR M 52-2-0. 2 L 7 4 4F RT 4A25 1998103000208 19981030 00208 WP 1998 10 30 UPS98827969 1 19981013 A 5320 3755827501 FITTING DOUG DC8 DC871F 302199D WP BS 270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C FS STA 270 AT LONG 33R TO 30R THE TORQUE BOX FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998103000209 19981030 00209 WP 1998 10 30 UPS98827970 1 19981013 A 5320 97555361 FITTING DOUG DC8 DC871F 302199D WP BS 1334 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, FS 1334 AT LONG 21R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998103000210 19981030 00210 WP 1998 10 30 UPS98827971 1 19981013 A 5320 9755584504 FITTING DOUG DC8 DC871F 302199D WP BS 1288 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, FS 1288 AT LONG 21R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-2OD AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998103000211 19981030 00211 WP 1998 10 30 UPS98827972 1 19981014 A 5320 37502571 FITTING DOUG DC8 DC871F 302199D WP BS 450 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, LONGERON 31L SPLICE FITTING CRACKED AT FS 450. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998103000212 19981030 00212 WP 1998 10 30 UPS98827973 1 19981014 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, FS 680, RBL 24, THE FLOORBEAM ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DW G 4645517 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998103000213 19981030 00213 WP 1998 10 30 UPS98827974 1 19981020 A 5320 561650947 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 640 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, CORROSION AT FS 640 AT LONG 36 AND 34R, LWR FWD BULKHEAD LWR T-CHORD SHEAR TIE IS BLOWN OUT WITH HEAV Y CORROSION. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5616509 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998103000214 19981030 00214 NM 1998 10 30 98FDEA00671 1 19981019 A 5314 65564913 KEEL BEAM BOEING 727 727227 1384078 NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 148 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM BS 950 B+F. *S/D* REPAIRED OUTBOARD FLANGE OF LT KEEL BEAM BS 950B +7 IAW FEDEX DRAWING NR SR27-53-023. 2 L 7 3 4F A3WE 1998103000215 19981030 00215 NM 1998 10 30 98FDEA00672 1 19981019 A 5314 65564413 KEEL BEAM BOEING 727 727227 1384078 NM BS 950-967 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 149 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM BS 950C+6 TO BS 950C+17. *S/D* INSTALLED REPAIR STRAP BS 950C+6 TO 950C+17 LT KEEL BEAM PER FEDEX SRD 27-53-023. 2 L 7 3 4F A3WE 1998103000216 19981030 00216 NM 1998 10 30 98FDEA00673 1 19981019 A 5314 65564413 KEEL BEAM BOEING 727 727227 1384078 NM BS 950-955 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 150 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM, BS 950 D+5. *S/D* REMOVED CORROSION FROM KEEL BEAM LT OUTBOARD FL ANGE BS 950D+5 MATERIAL LOSS WAS .040 DEEP X 1 X 4. FOUND AREA TO BE OUT OF LIMITS. REPAIRED IAW FEDEX SR 27-53-023. 2 L 7 3 4F A3WE 1998103000217 19981030 00217 NM 1998 10 30 98FDEA00674 1 19981019 A 5314 65564413 KEEL BEAM BOEING 727 727227 1384078 NM BS 950-955 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 495FE 21669 NR 151 CORROSION ON OUTBOARD FLANGE OF LT KEEL BEAM BS 950E+5 AND BS 950 E+11. *S/D* REMOVED CORROSION AND INSTALLED D OUBLER, STRAP, FILLER AT BS 930E TO 950E+15 STR 29 LT IAW FEDEX SR DRAWING 27-33-023. 2 L 7 3 4F A3WE 1998103000218 19981030 00218 WP 1998 10 30 MWEA981015 1 19981023 A 3350 60030451 BATTERY PACK DOUG DC9 DC932 3022066 WP EMERGENCY EXIT DISCHARGED A MWEA K NONE L NO TEST IN INSP/MAINT 1 GL 31 203ME 47673 FOUND LEFT AND RIGHT FORWARD WING OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MTC REMOVED AND REPLACED EMERGENCY BATTERY PACK. 2 L 7 2 4F A6WE 1998103000219 19981030 00219 NM 1998 10 30 DHL98742004 1 19981019 A 2780 RETRACT MECH BOEING 727 727225 1384077 NM NR 4 LE FLAP MALFUNCTIONED A DHLA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 742DH 21290 AFTER LIGHTNING STRIKE, NR 4 LED FLAP EXTENDED. PERFORMED LIGHTENING STRIKE INSPECTION, NO DEFECTS NOTED, OPS CHECK GO OD. NR 4 LED FLAP SWITCH OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998103000220 19981030 00220 NM 1998 10 30 VNAA9810019 1 19981021 A 5610 001A561A0000206 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT FLIGHTDECK CRACKED A VNAA O OTHER O OTHER CR CRUISE 1 GL 07 430JS 33862 3044 DURING FLIGHT, THE LEFT HAND SIDE WINDSCREEN WAS NOTED TO BE CRACKED BY THE CREW. THE FLIGHT CONTINUED TO DCA AND LANDE D WITHOUT FURTHER PROBLEMS. OUTSTATION MAINTENANCE INSPECTED THE LEFT SIDE WINDOW, IN ACCORDANCE WITH DORNIER MAINTENAN CE MANUAL 56-10-10. THE WINDOW WAS DETERMINED TO BE AIRWORTHY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. LATER ON THIS DATE, PSA MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND SIDE WINDSCREEN, IN ACCORDANCE WITH DORNIER MAINTENANCE MANU AL 56-12-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998103000221 19981030 00221 NM 1998 10 30 VNAA9810020 1 19981022 A 3412 0102JG1AG01 PROBE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE TAT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 425JS 38143 15239 3037 DURING THE TAXI PRIOR TO TAKEOFF, A TOTAL AIR TEMPERATURE PROBE FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE FOR REPAIR. MAINTENANCE INSPECTED AND REPLACED THE TOTAL AIR TEMPERATURE PROBE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 34-11-03. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998103000222 19981030 00222 WP 1998 10 30 TWAA9817201 1 19981024 A 3350 BATTERIES DOUG DC9 DC983 3022083 WP AIRSTAIRS DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 921TW 49101 THE AIR STAIR EMERGENCY LIGHTS WERE REPORTED DIM. RECHARGED LIGHT SYSTEM SEVERAL HOURS. CHECK-C 4-19-98 STL. 2 L 7 2 4F RT A6WE 1998103000223 19981030 00223 NM 1998 10 30 TWAA9817202 1 19981024 A 3040 TERMINAL BOEING 727 727231 1384079 NM NR 1 WINDOW FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 54351 21983 THE CAPTAIN'S NR 1 WINDOW HEAT WAS ARCING AT THE WINDOW TERMINAL BLOCK. CREW PULLED THE WINDOW HEAT CIRCUIT BREAKER. R EPAIRED TERMINAL BLOCK BY REPLACING WIRE TERMINAL AND HARDWARE. CHECK-C 01-31-97 JFK. 2 L 7 3 4F A3WE 1998103000224 19981030 00224 WP 1998 10 30 VJ9800561 1 19981027 A 3350 CONNECTOR DOUG DC9 DC932 3022066 WP ROW 10 FAILED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 935VV 47534 LIGHT FOR EMERGENCY FLOOR PATH LIGHTING INOP AT ROW 10. REPAIRED FAULTY CONTACT, SYSTEM OPS CHECKED GOOD IAW MM 33-50. 2 L 7 2 4F A6WE 1998103000225 19981030 00225 NM 1998 10 30 RAAA98B1093 1 19981026 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 12 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 PAX ROW 12 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998103000226 19981030 00226 WP 1998 10 30 9810309956 1 19981021 A 3260 PROX SENSOR DOUG DC9 DC931 3022065 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 923RW 47183 DURING APPROACH, NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR EXTENSION. CREW CYCLED GEAR WITH SAME RESULTS. G EAR WAS VISUALLY CONFIRMED DOWN AND LOCKED THROUGH PEEP HOLE. EMERGENCY EQUIPMENT WAS CALLED OUT ON STANDBY AS A PRECAU TION. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR PROXIMITY SENSOR BROKEN. REPLACED SENSOR, OPERATI ONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998103000227 19981030 00227 SO 1998 10 30 COMA9810242 1 19981026 A 2731 ATG120TR PROX SENSOR EMB 120 EMB120RT SO ELEVATOR TRIM FAILED A COMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SO 01 463CA 120267 TAKEOFF TRIM AURAL WARNING. REPLACED ELEVATOR TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1998103000228 19981030 00228 EA 1998 10 30 COMA9860325 1 19981026 A 5270 WARNING SYS CNDAIR CL600 CL6002B19 EA CARGO COMPT ACTIVATED A COMA K NONE N FALSE WARNING LD LANDING 1 SO 01 957CA 7109 CARGO UNSAFE MESSAGE. COULD NOT DUPLICATE, NO DEFECTS FOUND. 2 L 7 2 4F RT A21EA 1998103000229 19981030 00229 EA 1998 10 30 COMA9860326 1 19981026 A 5230 HANDLE CNDAIR CL600 CL6002B19 EA CARGO DOOR NOT LATCHED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 917CA 7017 CARGO DOOR WARNING AFTER TAKEOFF. LATCHED AND STOWED CARGO HANDLE. 2 L 7 2 4F RT A21EA 1998103000230 19981030 00230 EA 1998 10 30 COMA9860327 1 19981023 A 3397 WIRE CNDAIR CL600 CL6002B19 EA ROW 5 BROKEN A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 965CA 7131 SEVERAL EMERGENCY FLOOR LIGHTS ARE INOP. REPAIRED BROKEN WIRE AT ROW 5. 2 L 7 2 4F RT A21EA 1998103000231 19981030 00231 NE 1998 10 30 COMA9860328 2 19981025 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FLAMED OUT A COMA E A ENGINE SHUTDOWN UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 SO 01 967CA 7134 807419 LEFT ENGINE FLAMED OUT AND WOULD NOT RELIGHT. REPLACED LEFT ENGINE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998103000232 19981030 00232 NM 1998 10 30 UPS98227982 1 19981006 A 5330 SKIN BOEING 727 727108C 1384039 NM BS 1075 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1075 S18R AREA AT BS 1071 TO BS 1080 STR 18R TO STR 19R. REPAIRED PER SRS EO 98-30-001 ENGINEERING FILE NR 5330-2085. 2 L 7 3 4F A3WE 1998103000233 19981030 00233 NM 1998 10 30 UPS98227983 1 19981007 A 5320 FLANGE BOEING 727 727108C 1384039 NM BS 913-5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, SUSPECT CRACK O/B FLANGE RADIUS OF BS 913-5 BETWEEN STR 18A SILL AND W/WELL CEILING LT W/WELL. REPAI R CARRIED OUT IAW SRS EO B727-5310-1896. 2 L 7 3 4F A3WE 1998103000234 19981030 00234 NM 1998 10 30 UPS98227984 1 19981008 A 5320 FLANGE BOEING 727 727108C 1384039 NM BS 910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, SUSPECT CRACK O/B FLANGE RADIUS BS 910 RT BETWEEN STR 18A SILL AND W/WELL CEILING IN RT W/WELL. REPA IR CARRIED OUT IAW SRM ADDENDUM EO B 727-5310-1896. 2 L 7 3 4F A3WE 1998103000235 19981030 00235 NM 1998 10 30 UPS98227985 1 19981008 A 5311 FRAME BOEING 727 727108C 1384039 NM BS 848.95 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, DURING INSP OF FRAME 848.95 LT FOURTH FASTENER HOLE ABOVE FLOOR FOUND TO BE .3125 WITH MECHANICAL DAM AGE AFTER MAX OVERSIZE. FRAME 848.95 LT REPAIRED IAW APPENDIX C OF EO B727-5310-5474. 2 L 7 3 4F A3WE 1998103000236 19981030 00236 NM 1998 10 30 UPS98227986 1 19981009 A 5320 CHANNEL BOEING 727 727108C 1384039 NM BS 351-2 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, SUSPECT CRACK AT BS 351-2 LOCK ACTUATOR SUPPORT CHANNEL LT SIDE UPPER BOLT HOLE. REPLACED CHANNEL IA W DRAWING NR 69-19122. 2 L 7 3 4F A3WE 1998103000237 19981030 00237 NM 1998 10 30 UPS98227987 1 19981011 A 5720 FITTING BOEING 727 727108C 1384039 NM WS 224.5 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, CORROSION FOUND ON RT LANDING GEAR SUPPPORT FITTING ON WING REAR SPAR STA 224.5. FITTING REPLACED IA W DRAWING 65-84405. 2 L 7 3 4F A3WE 1998103000238 19981030 00238 NM 1998 10 30 UPS98227988 1 19981012 A 5520 BRACKET BOEING 727 727108C 1384039 NM RT ELEVATOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, RT ELEVATOR AT REAR SPAR AND ELEV STA 66.5 BRACKET CRACKED. REPLACED BRACKET IAW DRAWING NR 69-19144 AND DRAWING NR 65-25635. 2 L 7 3 4F A3WE 1998103000239 19981030 00239 NM 1998 10 30 UPS98227989 1 19981014 A 5311 FRAME BOEING 727 727108C 1384039 NM FRAME 760.95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, CRACK FOUND EMINATING FROM FASTENER HOLE ON FRAME 760.95 RT OVERSIZE HOLE. FRAME 760.95 RT REPAIRED IAW APPENDIX C OF EO B727-5310-5474. 2 L 7 3 4F A3WE 1998103000240 19981030 00240 EU 1998 10 30 QXEA9801525 1 19981024 A 2410 CSD FOKKER F28 F28MK4000 4990810 EU NR 1 MALFUNCTIONED A QXEA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 475AU 11222 NR 1 CSD WARNING LIGHT ILLUMINATED AFTER TAKEOFF, FOLLOWED BY STRONG ACRID SMELL IN AREA BEHIND FIRST OFFICER'S SEAT. C OMPLIED WITH EMERGENCY CHECK LIST AND RETURNED TO SMF. MAINTENANCE INSPECTED AREA BEHIND FIRST OFFICER'S SEAT, NO DEFEC TS NOTED. NO ACRID SMELL NOTED. PLACED NR 1 CSD ON MEL REF 24-1. LATER THAT DAY IN PDX QX MAINTENANCE RE-INSPECTED, N O DISCREPANCIES NOTED, CONTINUE MEL. 2 L 7 2 4F RT A20EU 1998103000241 19981030 00241 EU 1998 10 30 QXEA9801526 1 19981022 A 3350 5515900004 CIRCUIT BOARD GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 482US 11231 LIGHTS DIM IN EXIT LIGHT ON CEILING NEXT TO CLOSET. MAINTENANCE REPLACED THE FORWARD CABIN EXIT CIRCUIT BOARD, OPERATIO NAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998103000242 19981030 00242 EU 1998 10 30 QXEA9801527 1 19981025 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9A FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 493US 11161 EXIT SIGN AT ROW 9A INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998103000243 19981030 00243 EU 1998 10 30 QXEA9801528 1 19981023 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9E FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 478US 11227 EMERGENCY EXIT SIGN AT ROW 9E HAS A LIGHT OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998103000244 19981030 00244 EU 1998 10 30 QXEA9801529 1 19981023 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 481US 11230 LIGHT INSIDE LEFT FORWARD EMERGENCY EXIT HANDLE COVER INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998103000245 19981030 00245 EU 1998 10 30 QXEA9801530 1 19981025 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8E FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 483US 11233 EMERGENCY LIGHT AT ROW 8E INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998103000246 19981030 00246 EU 1998 10 30 QXEA9801531 1 19981024 A 3350 6008905 BATTERY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN DISCHARGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 MOST AFT (3 EACH) EVACUATION LIGHTS INOPERATIVE IN CABIN OVERHEAD. MAINTENANCE REMOVED AND REPLACED LEFT HAND EMERGENCY BATTERY PACK IN AFT LEFT HAND OVERHEAD BIN, OPERATIONAL TESTS NORMAL. 2 L 7 2 4F RT A20EU 1998103000247 19981030 00247 WP 1998 10 30 ABXA9800927 1 19981022 A 3260 0351881 SOCKET DOUG DC9 DC932 3022066 WP GEAR DOOR INOPERATIVE A ABXA O OTHER P NO WARNING INDICATION DE DESCENT 1 GL 23 986AX 47543 THE GEAR DOOR OPEN LIGHT DID NOT ILLUMINATE WHEN THE LANDING GEAR LEVER WAS PUT IN THE DOWN POSITION DURING APPROACH. R EPLACED THE GEAR DOOR OPEN LIGHT SOCKET. 2 L 7 2 4F A6WE 1998103000248 19981030 00248 WP 1998 10 30 MWEA981017 1 19981026 A 5347 500201 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1271 DOUBLE DRILLED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND NUMBER ONE SEAT TRACK WITH DOUBLE DRILLED HOLES AT NUT PLATE AT STATION 1271. MTC FABRICATED AND INSTALLED CHANNE L NUMBER ONE. 2 L 7 2 4F A6WE 1998103000249 19981030 00249 WP 1998 10 30 MWEA981018 1 19981025 A 2560 113317 SLIDE COVER DOUG DC9 DC932 3022066 WP PAX DOOR FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 209ME 47730 THE FORWARD EMERGENCY DOOR SLIDE COVER FELL OFF. MTC REINSTALLED THE SLIDE COVER. 2 L 7 2 4F A6WE 1998103000250 19981030 00250 WP 1998 10 30 MWEA981019 1 19981025 A 2560 5917689103 SLIDE COVER DOUG DC9 DC932 3022066 WP PAX DOOR FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 209ME 47730 FORWARD ENTRANCE DOOR EVACUATION SLIDE COVER FELL OFF. REINSTALLED FWD ENTRANCE DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998103000251 19981030 00251 NM 1998 10 30 DL72S982192 1 19981022 A 5743 65162905 FITTING BOEING 727 727232 1384082 NM WS 304 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 527DA 21587 THE REAR SPAR ATTACHMENT LUG OF THE LT MLG SUPPORT BEAM ATTACH FITTING WAS FOUND WITH CORROSION IN THE LUG HOLE BORE. T HE HOLE WAS OVERSIZED TO 1.882 DIA TO REMOVE THE CORROSION AND AN OVERSIZE BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMP LISHED PER ER/A 365909-14. 2 L 7 3 4F A3WE 1998103000252 19981030 00252 NM 1998 10 30 DL72S982193 1 19981021 A 5330 SKIN BOEING 727 727232 1384082 NM L1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 A 1 INCH CRACK WAS FOUND IN THE SKIN AT THE UPPER HINGE CUTOUT OF THE FWD ENTRY DOOR CUTOUT. AN EXISTING EXTERNAL DOUBL ER REPAIR WAS LOCATED MIDWAY BETWEEN THE UPPER HINGE CUTOUT ANDTHE LOWER HINGE CUTOUT. THE UPPER HINGE CRACK WAS REPAIR ED PER SRM 53-30-3, FIG 29 & 31 (BASED ON S/B REPAIR) AND THE EXISTING DOUBLER WAS REMOVED AND REPLACED WITH AN INTERNAL DOUBLER INSTALLED PER SRM 53-30-3 FIG 13. 2 L 7 3 4F A3WE 1998103000253 19981030 00253 NM 1998 10 30 DL757982194 1 19981023 A 5330 143N33401 SKIN BOEING 757 757232 1384965 NM FS 445 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 665DN 25013 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 445 BETWEEN STR 19L & 20L. THE DENTED AREA WAS CUT OUT WITH A 3.5 X 3.5. CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND FILLER TO EXTEND BEYOND THE S-19L LAP SPLICE. THE REPAIR WAS ACC OMPLISHED PER ER/A 235990-14, REV B. 2 L 7 2 4F RT A2NM 1998103000254 19981030 00254 NM 1998 10 30 DL757982195 1 19981022 A 3350 BPS73 POWER SUPPLY BOEING 757 757232 1384965 NM SEAT 3C INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 678DL 25983 ON CABIN MAINTENANCE VISIT 2525, FOUND FIRST CLASS SEAT EMERGENCY TRACK LIGHTING INOP. REPLACED POWER SUPPLY AND BATTER Y PACK. ALSO, REPAIRED SEAT LIGHT AT 3C. 2 L 7 2 4F RT A2NM 1998103000255 19981030 00255 WP 1998 10 30 DLL14982196 1 19981023 A 3350 POWER SUPPLY 5165741 LKHEED 1011 1011385115 5265015 WP EXTERIOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 740DA 37684 193C1244 NUMBER TWO RIGHT EXTERIOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY, CHECKS NORMAL PER MM. 2 L 7 3 4F A23WE 1998103000256 19981030 00256 NM 1998 10 30 DL72W982197 1 19980910 A 5753 652163233 ANGLE BOEING 727 727247 138408F NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 DURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED 32 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIR ED PER MM 57-52-0 FIG 802, BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998103000257 19981030 00257 WP 1998 10 30 DLL10982198 1 19981023 A 3350 516574 POWER SUPPLY LKHEED 1011 10113851 5265010 WP EXTERIOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 193C1180 R2 EXTERIOR EMERGENCY EVAC LIGHT DID NOT ILLUM WHEN TESTED. REPLACED POWER SUPPLY, NOW TEST OK. 2 L 7 3 4F A23WE 1998103000258 19981030 00258 NM 1998 10 30 DL72S982199 1 19981024 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM EMERGENCY EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA 14487 20746 RT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998103000259 19981030 00259 WP 1998 10 30 DLL19982201 1 19981024 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113853 5265020 WP CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 764DA 61465 193H1202 EMERGENCY LIGHT POWER SUPPLY BAD, CHARGE LIGHT FLASHING. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998103000260 19981030 00260 NM 1998 10 30 DLM88982202 1 19981024 A 3350 B5107 BATTERY PACK DOUG MD88 MD88 3023688 NM BS 1100 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 910DE 53419 ON LAYOVER, FOUND FLOOR TRACK LIGHTING ON RT SIDE FROM APPROX STA 1100 AFT WOULD NOT COME ON. REPLACED THE BATTERY PACK B5-107. LIGHTS TESTED NORMAL. 2 L 7 2 4F RT A6WE 1998103000261 19981030 00261 NM 1998 10 30 DL72S982206 1 19981016 A 5312 BULKHEAD WEB BOEING 727 727232 1384082 NM BS 870 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 420DA 21273 WEB AT STA 970 LOWER BULKHEAD WEB CRACKED RBL 10. REMOVED DAMAGED WEB AS PER SRM 51-40-2. FABRICATED REPAIR PARTS IAW SRM 53-10-9 FIG 4. OK TO INSTALL. STARTED INSTALLING REPAIR DOUBLER. COMPLETED REPAIR PER SRM 53-10-9 FIG 4. 2 L 7 3 4F A3WE 1998103000262 19981030 00262 NM 1998 10 30 DL72S982207 1 19981014 A 5522 ACCESS PANEL BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 TWO INCH CRACK IN NR 2 LT BALANCE BOARD ACCESS PANEL AT O/B EDGE (MARKED). INSTALLED REPAIR DOUBLER PER SRM 55-20-3 FIG 5. 2 L 7 3 4F A3WE 1998103000263 19981030 00263 NM 1998 10 30 DL72S982208 1 19981014 A 5522 PANEL BOEING 727 727232 1384082 NM RT HORIZ STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 A 1.25 INCH CRACK AT NR 1 RT BALANCE BOARD ACCESS PANEL O/B EDGE (MARKED). 2 L 7 3 4F A3WE 1998103000264 19981030 00264 NM 1998 10 30 DL72W982209 1 19980910 A 5754 ANGLE BOEING 727 727247 138408F NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 AT HMV, FOUND NR 5 SLAT ANGLES - ACTUATOR ATTACH POINT BOTH I/B AND O/B ANGLES CRACKED. STOP DRILLED CRACK PER M/M, FAB D REPAIR DOUBLERS, INSTALLED PER MM 57-54-00 FIG 809. 2 L 7 3 4F A3WE 1998103000265 19981030 00265 NM 1998 10 30 DL72W982210 1 19980910 A 5754 GUIDE BOEING 727 727247 138408F NM NR 5 LE SLAT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 AT HMV, FOUND GUIDE ON NR 5 SLAT TRAILING EDGE O/B OF ACTUATOR WORN. WEAR LIMITS OK, REPAIRED PER M/M 27-81-11. 2 L 7 3 4F A3WE 1998103000266 19981030 00266 NM 1998 10 30 DL72W982213 1 19980911 A 5713 STRINGER BOEING 727 727247 138408F NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 ON HMV, RT WING OUTER UPPER STRINGER 2 RIB AT WS 656.5 STR 12 IS CRACKD AT FASTENER HOLE. CUT OUT VENT STRINGER, DRILLE D UP REPAIR ANGLES RADUIS FILLERS CVR ASSY PER MM 57-13-00. INSTALLED REPAIR ANGLES. 2 L 7 3 4F A3WE 1998103000267 19981030 00267 NM 1998 10 30 DL72S982214 1 19981026 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 FOUND ON C-1 LETTER CK, NR 1 SLAT I/B ACTUATOR ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998103000268 19981030 00268 NM 1998 10 30 DL72S982215 1 19981026 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 496DA 21076 A .5 INCH VISIBLE CRACK AT AFT ENTRY DOOR CUTOUT LT FRAME FWD END APPROX 6 BELOW UPPER STOP CASTING. REPAIRED PER SRM 5 3-10-9 FIG 11. 2 L 7 3 4F A3WE 1998103000269 19981030 00269 NM 1998 10 30 DL72W982216 1 19980911 A 5713 STRINGER BOEING 727 727247 138408F NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 AT HMV, FOUND RT WING OUTER W/UPR STRINGER 2 RIB AT WS 656.5 STRINGER 13 IS CRACKED AT FASTENER HOLE. REPAIR INFO IS RE F ON OPN 8602AD ITEM 5. CUT OUT VENT STRINGER, DRILLED UP REPAIR ANGLES RADIUS FILLER COVER ASSY PER M/M 57-13-00. INS TALLED PER SAME. 2 L 7 3 4F A3WE 1998103000270 19981030 00270 NM 1998 10 30 SCNA98129 1 19981023 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT ABOVE THE R2 DOOR WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACE D THE BATTERY PACK. LIGHT OPERATIONALLY CHECKS GOOD REFERENCE MM 335071. 2 L 7 3 4F RT A3WE 1998103000271 19981030 00271 NM 1998 10 30 SCNA98130 1 19981022 A 3350 37067001 BATTERIES BOEING 727 7272A1 138407F NM AFT AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERIES FOR THE AFT AIRSTAIR EMERGENCY LIGHT. EMERGENCY LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998103000272 19981030 00272 SO 1998 10 30 SWIA971285 1 19981009 A 3233 2060500005 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE NLG MALFUNCTIONED A SWIA L ABORTED APPROACH F FLT CONT AFFECTED DE DESCENT 1 NM 07 156CA 120156 ON APPROACH HAD US DO A GO-AROUND. ON GO-AROUND, NOSE GEAR A AND B REMAINED ON, (NO GROUND LIGHTS). NOSE GEAR WOULD NO T COME UP. REPLACED NOSE GEAR ACTUATOR FOR TROUBLESHOOTING. ALSO, REPLACED BAD ROD-END ASSY. SWUNG GEAR SEVERAL TIMES . ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000273 19981030 00273 SO 1998 10 30 SWIA971286 1 19981003 A 3233 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 289UE 120191 RIGHT MAIN GEAR RED DISAGREEMENT LIGHT ON AFTER RETRACT. CYCLED GEAR TWICE. RETURNED TO PDX. REPLACED RIGHT MAIN GEAR ACTUATOR PER MM 32-30-00. LEAK CHECKS AND OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000274 19981030 00274 SO 1998 10 30 SWIA971287 1 19981012 A 3230 SEQUENCE VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 218SW 120287 LEFT MAIN GEAR WOULD NOT RETRACT AFTER TAKEOFF. CYCLED GEAR THREE TIMES WITH NO CHANGE. RETURNED TO SMX. INSPECTED LE FT GEAR DOORS SEQUENCE VALVES FOR RIGGING, FOUND GOOD. CLEANED HEAVY GRIME FROM SEQUENCE VALVE. SWUNG GEAR SIX TIMES A ND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000275 19981030 00275 SO 1998 10 30 SWIA971288 1 19981012 A 2130 PRESSURIZATION EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 195SW 120127 CREW REPORTED CABIN PRESSURIZATION DIFFICULT TO OPERATE IN AUTO OR MANUAL. RETURNED TO SLC. INSPECTED DOOR AND EMERGEN CY EXITS SEALS, FOUND GOOD. PRESSURIZED A/C ON GROUND IN AUTO AND MANUAL CONTROL (2000 TO 5 PSI). OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000276 19981030 00276 SO 1998 10 30 SWIA971289 1 19981015 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT TE FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 207SW 120266 UNABLE TO RETRACT FLAPS, DISAGREEMENT. RETURNED TO SLC. REMOVED AND REPLACED RIGHT WING INBOARD FLAP ACTUATOR, OPS CH ECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000277 19981030 00277 SO 1998 10 30 SWIA971290 1 19981015 A 2131 CONTROLLER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 AIRCRAFT WOULD NOT PRESSURIZE IN EITHER MANUAL OR AUTO. RETURNED TO SLC. REPLACED PRESSURIZATION CONTROL. PRESSURIZED AIRCRAFT, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000279 19981030 00279 SO 1998 10 30 SWIA971292 1 19981016 A 2450 CIRCUIT BREAKER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE E & E COMPT TRIPPED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 223SW 120291 ON TAKEOFF, FIRST OFFICERS EHSI AND NAV NUMBER TWO WENT INOPERATIVE. RETURNED TO LAX. NORMAL POWER RETURNED TO BOTH UN ITS AFTER LANDING. FOUND NUMBER TWO EMERGENCY BUS CIRCUIT BREAKER POPPED. RESET CIRCUIT BREAKER. RAN ENGINE AND ALL C HECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998103000280 19981030 00280 WP 1998 10 30 RRXA98443 1 19981020 A 2910 FITTING DOUG DC8 DC863F 302198F WP NR 2 ENGINE LOOSE A RRXA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 15 957R 46137 LOST HYDRAULIC FLUID UP TO EMERGENCY LEVEL DURING CLIMBOUT TO LEVEL 330. PERFORMED ABNORMAL HYDRAULIC CHECKLIST PER QRH . TIGHTENED B-NUT FITTING ON NR 2 ENG HYD PUMP. LEAK CHECKS GOOD, SERVICED HYDS. 2 L 7 4 4F 4A25 1998103000281 19981030 00281 WP 1998 10 30 RRXA98444 1 19981020 A 7722 65003003 EGT INDICATOR DOUG DC8 DC871F 302199D WP GE CFM CFM562 GL NR 4 FAILED A RRXA E J A ENGINE SHUTDOWN DUMP FUEL UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 15 8076U 45941 692350 AFTER V1, NR 4 EGT MOMENTARILY WENT TO 907 DEG. REDUCED N1 1 PERCENT TO MAINTAIN EGT BELOW LIMITS. ACCOMPLISHED IN FLT SHUTDOWN, DUMPED FUEL, RETURNED TO MMMX. WINDMILL TIME 25 MIN AND OIL PRESS 0 PSI. REMOVED AND REPLACED NR 4 EGT IND ICATOR AS REQUIRED. OPS CHECKS NORMAL. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998103000282 19981030 00282 WP 1998 10 30 RRXA98445 1 19981022 A 3260 SQUAT SWITCH DOUG DC8 DC871F 302199D WP NLG MALFUNCTIONED A RRXA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 WP 15 8087U 45977 NR 1 IN FLIGHT SHUTDOWN OF RT PACK DUE TO EXCESSIVE VIB AND NOISE. INSPECTED NOSE AND PAC SECTION OF ACFT. SUSPECT PAC K WAS RUNNING WHEN NR 4 ENG WAS ALSO MALFUNCTIONING, SYS LEAK AND OP CHECKS GOOD. TOP OF DESCENT NR 1 ENG WENT BELOW MI N FLIGHT IDLE TO 32 PERCENT N1. REPLACED 51-68 OLEO SWITCH, SYS OP CHECK GOOD ON ENGINE RUN BY MAINTENANCE TEAM. TOP O F DESCENT NR 4 ENG WENT BELOW MIN FLIGHT IDLE TO 30 PERCENT N1. REPLACED R2-44 RIGHT GROUND RELAY AND 51-69 NOSE OLEO S WITCH, SYS OP CHECK GOOD ON ENGINE RUN BY MAINTENANCE TEAM. 2 L 7 4 4F RT 4A25 1998103000283 19981030 00283 GL 1998 10 30 RRXA98446 2 19981021 A 7320 MEC DOUG DC8 DC871F 302199D WP GE CFM CFM562 GL NR 2 ENGINE OUT OF ADJUST A RRXA E A ENGINE SHUTDOWN UNSCHED LANDING M J OVER TEMP WARNING INDICATION TO TAKEOFF 1 WP 15 8076U 45941 692543 NR 2 ENG SLOW TO ACCELERATE TO IDLE DURING START, SLOW TO CUTBACK. FUEL FLOW AND EGT HIGHER THAN 1, 3 & 4. AFTER V1 EG T WENT TO 905 DEG, 908 MOMENTARLEY, REDUCED N1 BY 2 PERCENT TO MAINTAIN EGT BELOW LIMITS. ACCOMPLISHED IN FLT SHUTDOWN AND RETURNED TO MMMX. WINDMILLING TIME 21 MIN AND OIL PRESS 0 PSI. PERFORMED STATIC RIG CHECK ON THE VBV AND VSV RIGGI NG TO MEC TO ENGINE NR 2. ENGINE RUN OPS CHECKS OK IAW MM 73-21-10. 2 L 7 4 4F 4 F RT 4A25 E2GL 1998103000284 19981030 00284 WP 1998 10 30 EIAA980249 1 19980905 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 680 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, SEAT TRACK AT BS 680 HAS TAB WORN BEYOND LIMITS AT BL 12. REPLACED SECTION OF SEAT TRACK PER SRM 53-05 FIG 4B, 33 INCH SECTION REPLACED. (M) 2 L 7 2 4F A6WE 1998103000285 19981030 00285 WP 1998 10 30 EIAA980248 1 19980905 A 5210 INTERCOSTAL DOUG DC9 DC932F 3022067 WP PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURNG C-CHECK, L1 DOOR HANDLE PAN AND INTERCOSTAL FOUND CRACKED, NRC V044. REPLACED DOOR PAN AND INTERCOSTAL PER SRM 51-30-0. (M) 2 L 7 2 4F A6WE 1998103000286 19981030 00286 NM 1998 10 30 EIAA980247 1 19980901 A 5312 PRESSURE BLKHD BOEING 747 747SR46 NM BS 2360 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 HKG - DURING C2 CHECK, BS 2360 AFT PRESSURE BULKHEAD WEB CRACKED AT APU DUCT CUTOUT 12 O'CLOCK POSITION. REPAIRED WEB P ER RS R-53-83-33849, EO 53-747-970-90 REV A, AND 8110-3 AND ECRA N477-51-41-1. (M) 2 L 7 4 4F A20WE 1998103000287 19981030 00287 NM 1998 10 30 EIAA980246 1 19980901 A 5210 SKIN BOEING 747 747SR46 NM PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 HKG - DURING C2 CHECK, RIGHT NR 1 MAIN ENTRY DOOR SKIN AND INTERNAL DOUBLER CRACKED. REPAIRED DOOR SKIN AND DOUBLER PER RS R-52-11-33828 AND 8110-3 ECRA 477-51-41-1. (M) 2 L 7 4 4F A20WE 1998103000288 19981030 00288 NM 1998 10 30 EIAA980245 1 19980901 A 5330 SKIN BOEING 747 747SR46 NM WS 707 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 HKG - DURING C2 CHECK, RIGHT WING LOWER SKIN PANEL, AT WS 707 BOOST PUMP ACCESS CUTOUT HAS CORROSION. REPAIRED LOWER SK IN PER RS R-57-26-33796 AND 8110-3 AND ECRA 477-51-41-1. (M) 2 L 7 4 4F A20WE 1998103000289 19981030 00289 NM 1998 10 30 EIAA980244 1 19980901 A 5313 STRINGER BOEING 747 747SR46 NM BS 1960 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 HKG - DURING C2 CHECK, MAIN DECK BS 1960 STRINGER 12R HAS A CRACK AT END. REPAIRED PER RS R053061-33833 AND 8110-3 AND ECRA 477-51-41-1. (M) 2 L 7 4 4F A20WE 1998103000290 19981030 00290 NM 1998 10 30 EIAA980243 1 19980901 A 7830 RING BOEING 747 747SR46 NM NR 4 ENGINE CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 477EV 20784 HKG - DURING C2 CHECK, NR 4 ENGINE THRUST REVERSER, CASCADE VANE SUPPORT RING HAS CHAFE MARKS AT 4 O'CLOCK POSITION. RE PAIRED SUPPORT RING PER RS R-78-31-33806 AND 8110-3 AND ECRA 477-51-41-1. (M) 2 L 7 4 4F A20WE 1998103000291 19981030 00291 NM 1998 10 30 EISA98239 1 19980810 A 5311 FRAME BOEING 727 7272A7 138407K NM CABIN CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-ROUTINE INSPECTION CARD, FOUND FUSELAGE FRAME CRACKED AT STATION 570. REPAIRED FRAME PER SRM 53-20-2 DOUBLER INSTALLED. (M) 2 L 7 3 4F A3WE 1998103000292 19981030 00292 NM 1998 10 30 EISA98238 1 19980810 A 5320 FLANGE BOEING 727 7272A7 138407K NM NLG WW CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-ROUTINE CPCP INSPECTION CARD, FOUND CORROSION IN NOSE WHEEL WELL PANEL 3120. CORROSION WAS F OUND ON OUTBOARD FLANGE. REPLACED FLANGE PER SRM 53-10-2 DOUBLER INSTALLED. (M) 2 L 7 3 4F A3WE 1998103000293 19981030 00293 NM 1998 10 30 EISA98237 1 19980810 A 5347 SEAT TRACK BOEING 727 7272A7 138407K NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 344 TO 480 RBL 44. REMOVED AND REP LACED SEAT TRACK PER SRM 53-10-1. (M) 2 L 7 3 4F A3WE 1998103000294 19981030 00294 NM 1998 10 30 EISA98236 1 19980810 A 3211 FITTING BOEING 727 7272A7 138407K NM LT MLG CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK, WHILE DOING SCHEDULED GEAR CHANGE LEFT FORWARD TRUNNION FITTING CORRODED. REMOVED AND REPLACED FWD TRUNNION FITTING PER SRM 51-10-1 AND 51-30-2 AND MM 20-80-1. (M) 2 L 7 3 4F A3WE 1998103000295 19981030 00295 NM 1998 10 30 EISA98235 1 19980810 A 5347 SEAT TRACK BOEING 727 7272A7 138407K NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION CARD, FOUND CORROSION ON SEAT TRACK STATION 560 RBL 44. REMOVED AND REPLACED DAMAGED AREA OF SEAT RACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1998103000296 19981030 00296 NM 1998 10 30 EISA98234 1 19980810 A 5347 SEAT TRACK BOEING 727 7272A7 138407K NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 837 RBL 24. REMOVED AND REPL ACED DAMAGED AREA OF SEAT TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1998103000297 19981030 00297 NM 1998 10 30 EISA98233 1 19980810 A 5347 SEAT TRACK BOEING 727 7272A7 138407K NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 400 RBL 23. REMOVED SEAT TRA CK FABRICATED NEW ONE PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1998103000298 19981030 00298 NM 1998 10 30 EISA98232 1 19980810 A 5320 WEB BOEING 727 7272A7 138407K NM BS 870 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE CPCP INSPECTION, FOUND RIGHT WEB AT STATION 870 IN KEELBEAM CRACKED. REMOVED D AMAGED AREA FABRICATED DOUBLER AND INSTALLED PER SRM 53-10-2 FIGURE 4. (M) 2 L 7 3 4F A3WE 1998103000299 19981030 00299 NM 1998 10 30 EISA98231 1 19980810 A 5320 ANGLE BOEING 727 7272A7 138407K NM KEELBEAM CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE CPCP INSPECTION CARD, FOUND VERTICAL ATTACH ANGLE AT STATION 870 IN KEELBEAM CR ACKED. REMOVED AND REPLACED WITH NEW PART PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998103000300 19981030 00300 NM 1998 10 30 EISA98230 1 19980810 A 5347 SEAT TRACK BOEING 727 7272A7 138407K NM CABIN CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK ROUTINE INSPECTION CARD, FOUND CORROSION SEAT TRACK STATION 640 AND RBL 44. REMOVED AN D REPLACED SEAT TRACK PER SRM 53-10-5. (M) 2 L 7 3 4F A3WE 1998103000301 19981030 00301 NM 1998 10 30 EISA98229 1 19980810 A 5320 WEB BOEING 727 7272A7 138407K NM BS 870 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 310NE 20241 DURING ACCOMPLISHMENT OF C-CHECK CPCP CARD INSPECTION, A 4 INCH CRACK WAS FOUND AT STATION 870 BULKHEAD AT APPROX BL 10. REPAIRED AREA WITH DOUBLER PER EO 53-98-143-1 AND SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998103000302 19981030 00302 WP 1998 10 30 98ZZZM789 2 19980806 A 7320 8974575 VALVE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LT ENGINE FAILED A CHQA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 11 844JS 8308265708 760 AIRCRAFT ABORTED TAKEOFF DUE TO LEFT ENGINE TORQUE FLUCTUATION. THE SYSTEM WAS INSPECTED AND THE BYPASS VALVE WAS FOUND TO BE AT FAULT. THE VALVE WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDICATIONS NORMAL. (M ) 2 L 7 2 4T 4 T RT A21EU E4WE 1998103000303 19981030 00303 EU 1998 10 30 98ZZZM790 1 19980716 A 2160 218D4 UNIT CONTROL GRAVINER BAG JETSTM JETSTM3101 1500215 EU WS 36 FAILED A CHQA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 839JS 803 748 AIRCRAFT RETURNED TO FIELD DUE TO LEFT DUCT LIGHT ILLUMINATED. THE SYSTEM WAS TROUBLESHOT AND THE DC CONTROL UNIT WAS D ETERMINED TO HAVE FAILED. THE UNIT WAS REPLACED AND A FUNCTIONAL CHECK PERFORMED WITH ALL INDICATIONS NORMAL. (M) 2 L 7 2 4T RT A21EU 1998103000304 19981030 00304 EU 1998 10 30 98ZZZM791 1 19980722 A 2161 7252C000 VALVE BAG JETSTM JETSTM3101 1500215 EU BS 230 FAILED A CHQA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 11 844JS 7994242 760 AIRCRAFT RETURNED TO FIELD DUE TO LIGHT SMOKE REPORTED IN CABIN. THE SYSTEM WAS TROUBLESHOT AND THE RIGHT TEMP CONTROL VALVE WAS DETERMINED TO BE AT FAULT. THE UNIT WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH ALL INDI CATIONS NORMAL. (M) 2 L 7 2 4T RT A21EU 1998103000305 19981030 00305 1998 10 30 98ZZZM792 3 19980807 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3101 1500215 EU LT ENGINE FAILED A CHQA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 GL 11 838JS 0397 741 AIRCRAFT ABORTED TAKEOFF DUE TO LEFT BETA LIGHT ILLUMINATED AT 60 PERCENT TORQUE. THE SYSTEM WAS TROUBLESHOT AND THE BE TA SWITCH WAS DETERMINED TO BE AT FAULT. THE SWITCH WAS REPLACED AND A FUNCTIONAL CHECK OF THE SYSTEM PERFORMED WITH AL L INDICATIONS NORMAL. (M) 2 L 7 2 4T RT A21EU 1998103000306 19981030 00306 EU 1998 10 30 98ZZZM793 1 19980728 A 2611 72111211000 SMOKE DETECTOR BAG JETSTM JETSTM3101 1500215 EU BS 419 FAILED A CHQA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 11 853JS A1444 730 CARGO SMOKE DETECTOR ILLUMINATED DURING TAXI. THE PASSENGERS WERE EVACUATED FROM THE AIRCRAFT. FIRE DEPARTMENT INSPECT ED BAGGAGE AREA AND FOUND NO SIGN OF SMOKE OR SMELL. ALL BAGS WERE REMOVED FROM CARGO AREA. CREW OPS DEFERRED. WHEN A IRCRAFT ARRIVED IN PIT, MAINTENANCE REPLACED THE SMOKE DETECTOR. A FUNCTIONAL TEST OF THE SYSTEM WAS PERFORMED WITH ALL INDICATIONS NORMAL. (M) 2 L 7 2 4T RT A21EU 1998103000307 19981030 00307 WP 1998 10 30 AALA981698 1 19980916 A 2121 6054578 FAN DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 462AA 366409 49592 DFW - FLT 85 - DURING DESCENT INTO DFW, FLIGHT ATTENDANT NOTED A ELECTRICAL SMELL IN THE AFT COACH CABIN. AIRCRAFT LAND ED DFW WITHOUT INCIDENT. MAINTENANCE FOUND THE CABIN CONDITIONED AIR RECIRCULATION FAN OVERHEATING. REPLACED CABIN CON DITIONED AIR RECIRCULATION FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998103000308 19981030 00308 WP 1998 10 30 AALA981678 1 19980908 A 3260 833605A SENSOR DOUG DC9 DC982 3022082 WP E/E BAY FAILED A AALA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 07 488AA 49681 DFW - FLT 616 - AFTER TAKEOFF YYC, AFTER GEAR WAS RAISED THE LEFT RED GEAR LIGHT REMAINED ILLUMINATED, AMBER GEAR DOOR O PEN LIGHT EXTINGUISHED. NO UNUSUAL YAW OR VIBRATION. AIRCRAFT CONTINUED TO DFW AND LANDED WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR DOOR PROXIMITY SENSOR UNIT. ACCOMPLISHED REQUIRED TESTS. SYSTEM GROUND CHECKED NORMAL OPERATION . (M) 2 L 7 2 4F A6WE 1998103000309 19981030 00309 WP 1998 10 30 ASAA9880181 1 19980918 A 3350 LIGHT DOUG DC9 DC983 3022083 WP ROW 3 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - PRIOR TO DEPARTURE OF FLIGHT 712, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FORWARD OF ROW 3 WERE INOPERATIVE . RECONNECTED WIRING TO LAMP MODULE AT ROW 3 AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000310 19981030 00310 NM 1998 10 30 EISA98220 1 19980919 A 2750 ANNUNCIATOR BOEING 727 7272M7 138407S NM COCKPIT MALFUNCTIONED A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 721RW 21200 AFTER TAKEOFF NR 2 LEADING EDGE FLAP LIGHT ON THE F/E ANNUNCIATOR PANEL WAS NOT ILLUMINATED, ALONG WITH THE LEADING EDGE FLAP AMBER LIGHT ON THE PILOTS FO RWARD PANEL. AIR TURN BACK TO ATH. GENERATED FROM PILOT REPORT. CYCLED FLAP THROUG H RANGES. OPS CHECK OK. ALL LEADING EDGE FLAPS OPERATED NORMALLY IAW MM 27-00. (M) 2 L 7 3 4F A3WE 1998103000311 19981030 00311 NM 1998 10 30 P2EA98168 1 19980828 A 2510 SEAT BOEING 737 737297 1384480 NM CABIN CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - PASSENGER CABIN SEATS LEFT POSITIONS 4, 5, 8, 12, 13, 15 AND 17 WITH FORWARD TUBE CRACKED AT THE INBOARD END. REP AIRED SEAT ASSEMBLIES LEFT SIDE POSITIONS 4, 5, 8, 12, 13, 15 AND 17 IAW COOPESA EO-COO-3-25-464-98 DATED SEPT 10, 1998. REF COOPESA WORK ORDER NR L1-0909-2-199, NON-ROUTINE NR 474. (M) 2 L 7 2 4F A16WE 1998103000312 19981030 00312 NM 1998 10 30 P2EA98169 1 19980828 A 2510 SEAT BOEING 737 737297 1384480 NM CABIN CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 5WM 22629 SJO - PASSENGER CABIN SEATS RIGHT POSITIONS 3, 5, 6, 7, 8, 10, 11, 12, 13, 14, 15 AND 17 FORWARD TUBE CRACKED AT THE OUT BOARD END. REPAIRED SEAT ASSEMBLIES RIGHT SIDE POSITIONS 3, 5, 6, 7, 8, 10, 11, 12, 13, 14, 15 AND 17 IAW COOPESA EO-CO O-3-25-464-98 DATED SEPT 10, 1998. REF COOPESA WORK ORDER L1-0909-2-203, NON-ROUTINE NR 477. (M) 2 L 7 2 4F A16WE 1998103000313 19981030 00313 WP 1998 10 30 USAAD98172 1 19981005 A 2120 AIR DIST DOUG DC9 DC981 3022081 WP CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 826US 48026 PHL-GSP - FLT 273 - AFTER TAKEOFF THE FLIGHT ATTENDANTS NOTICED A BURNING SMELL THROUGH THE AIR CONDITIONING SYSTEM. TH E SMELL SUBSIDED A LITTLE THEN RETURNED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE C HECKED THE AIR CONDITIONING SYSTEM AND FOUND TO BE SERVICED PROPERLY. THE ENGINE INTAKES AND EXHAUSTS WERE CHECKED ALON G WITH THE FORWARD E/E COMPARTMENT AND BATTERIES. THE CARGO COMPARTMENTS WERE CHECKED FOR SPILLS. ALL CHECKED NORMAL A ND NO CAUSE FOUND FOR THE ODOR. (M) 2 L 7 2 4F A6WE 1998103000314 19981030 00314 NM 1998 10 30 USAA980391 1 19980917 A 5315 654681165 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 31662 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION STATION 1006 LBL 2 BEAM INST PASS FLOOR. CORROSION TASK NR C53-107-02. INSTALLED REPAIR ANGLES PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 1998103000315 19981030 00315 NM 1998 10 30 USAA980385 1 19980917 A 5315 65468101 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 31662 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 10 INCH AREA OF CORROSION STATION 967 LBL 5 TO R BL 5 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED REPAIR ANGLES PER SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 1998103000316 19981030 00316 NM 1998 10 30 USAA980386 1 19980917 A 5315 654581094 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 31662 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 72 INCH AREA OF CORROSION CLIPNUT HOLES STATION 312 LBL 36 TO RBL 36 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-5 1. (M) 2 L 7 2 4F RT A16WE 1998103000317 19981030 00317 NM 1998 10 30 USAA980387 1 19980917 A 5315 6545815108 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 31662 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH BY 50 INCH AREA OF CORROSION STATION 344 BLO TO LBL 5 0 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998103000318 19981030 00318 NM 1998 10 30 USAA980421 1 19980930 A 5320 CC1134366 CHANNEL BOEING 737 7373B7 1384580 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 360 STRINGER 4L V-CHANNEL. REPLACED WITH IDENTI CAL PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998103000319 19981030 00319 NM 1998 10 30 USAA980422 1 19980930 A 5320 65516989 SPLICE BOEING 737 7373B7 1384580 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND STRINGER SPLICE CRACKED AROUND 4 RIVET HOLES .125 INCH EACH STRINGER AT STATION 907 STRINGER 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-40-02. (M) 2 L 7 2 4F RT A16WE 1998103000320 19981030 00320 NM 1998 10 30 USAA980423 1 19980930 A 5315 654681144 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH AREA OF CORROSION BS 986.5 LBL 4, 11, 21 AND LOWER SURFACE LBL 36 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP UPPER CHORD PER SRM 53-00-51 AND EA 62431. (M) 2 L 7 2 4F RT A16WE 1998103000321 19981030 00321 NM 1998 10 30 USAA980424 1 19980930 A 5315 654681144 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1006 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 2 INCH CORRODED AREA STATION 1006 BEAM T-CAP RBL 10. CORROS ION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-58-53500-012. (M) 2 L 7 2 4F RT A16WE 1998103000322 19981030 00322 NM 1998 10 30 USAA980425 1 19980930 A 5315 654581299 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND SEVERAL CORRODED AREAS .5 INCH BY .5 INCH BY 26 INCH BS 328 LB 12 TQ RBL 14, WL 208.1 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER SRM 51-70-12. (M) 2 L 7 2 4F RT A16WE 1998103000323 19981030 00323 NM 1998 10 30 USAA980420 1 19980930 A 5313 STRINGER BOEING 737 7373B7 1384580 NM BS 500 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500D AND STRINGER 28L. INSTALLED DOUBLERS PER SRM 53-30-12. (M) 2 L 7 2 4F RT A16WE 1998103000324 19981030 00324 NM 1998 10 30 USAA980419 1 19980930 A 5313 BAC1498151 STRINGER BOEING 737 7373B7 1384580 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND THREE .5 INCH CRACKS FROM RIVET TO RIVET STRINGER 4L STATION 907. NEW S TRINGER SPLICE INSTALLED PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998103000325 19981030 00325 NM 1998 10 30 USAA980443 1 19980930 A 5315 654680438 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH CORRODED AREA BS 967 RBL 49 BEAM INST PAX FLOOR. COR ROSION TASK NR C53-107-02. INSTALLED NEW T-CAP PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1998103000326 19981030 00326 NM 1998 10 30 USAA980442 1 19980930 A 5320 65C3079912 WEB BOEING 737 7373B7 1384580 NM BS 721 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK SHEAR BEAM WEB 518A RIGHT BS 721. REPLACED WITH IDENTICA L PART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1998103000327 19981030 00327 NM 1998 10 30 USAA980441 1 19980930 A 5311 65465522 FRAME BOEING 737 7373B7 1384580 NM BS 827 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 2 INCH CORRODED AREA BS 827 BETWEEN STRINGER 28L AND STRINGE R 28R RBL 2 BOTTOM FRAME. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998103000328 19981030 00328 NM 1998 10 30 USAA980440 1 19980930 A 5320 6545808582 WEB BOEING 737 7373B7 1384580 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A CRACKED AREA .25 INCH FORWARD SERVICE DOOR OPENING LWR FWD CORNER BS 2 94 STRINGER 17R FLOOR LEVEL. INSTALLED DOUBLER PER SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1998103000329 19981030 00329 NM 1998 10 30 USAA980465 1 19980930 A 5315 654581094 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 312 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 393US 37228 23315 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION AROUND FASTENERS .5 INCH BY .5 INCH BY 37 INCH STAI TON 312 BETWEEN LBL 14 AND RBL 23 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. INSTALLED NEW T-SECTION WITH DO UBLER PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998103000330 19981030 00330 EU 1998 10 30 USAAF98078 1 19980915 A 3350 6104789 BATTERY PACK FOKKER F28 F28MK0100 4990807 EU CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 860US 11295 GSO - EMERGENCY EXIT SIGN AT ENTRY DOOR INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M) 2 L 7 2 4F RT 1998103000331 19981030 00331 EU 1998 10 30 USAAF98083 1 19980923 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 895US 11380 GSO - FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND PIN PUSHED BACK IN CONNECTOR P3858B. THE REPOSITIONED TH E PIN IN THE CONNECTOR. (M) 2 L 7 2 4F RT 1998103000332 19981030 00332 EU 1998 10 30 USAAF98080 1 19980923 A 3150 WARNING UNIT FOKKER F28 F28MK0100 4990807 EU COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 865US 11308 PHL - FLT 1620 - TEN MINUTES AFTER DEPARTURE FROM PHL, FLIGHT WARNING COMPUTER INOP MESSAGE APPEARED ON THE MULTI FUNCTI ON DISPLAY. CREW RECYCLED BREAKERS BUT FAULT MESSAGE REMAINED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCID ENT. MAINTENANCE TESTED FLIGHT WARNING SYSTEM. SYSTEM TESTED PROPERLY AND NO FAULT MESSAGES WERE PRESENT. FLIGHT REFU ELED AND DEPARTED PHL. (M) 2 L 7 2 4F RT 1998103000333 19981030 00333 NM 1998 10 30 USAA980429 1 19980915 A 5330 SKIN BOEING 757 757225 1384959 NM BS 1285 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 601AU 44734 22193 CLT - DURING C-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 6 INCH AREA OF CORROSION AT DOME NUT ON FUSELAGE SKIN BS 128 5 JUST OUTBOARD OF STRINGER 29L. CORROSION TASK NR C53-155-02. INSTALLED DOUBLER AND FILLER PER EA 62324. (M) 2 L 7 2 4F RT A2NM 1998103000334 19981030 00334 NM 1998 10 30 USAASB98256 1 19980926 A 3260 SENSOR BOEING 737 7374B7 1384702 NM RT MLG MALFUNCTIONED A USAA O OTHER O OTHER CL CLIMB 1 EA 19 783AU 25022 BWI - FLT 1435 - AFTER TAKEOFF FROM BWI, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRAC TION. CREW RECYCLED GEAR AND RECEIVED NORMAL GEAR INDICATION. GEAR EXTENSION FOR LANDING WAS NORMAL. MAINTENANCE INSP ECTED THE RIGHT MLG UPLOCK INDICATION COMPONENTS AND FOUND NO DISCREPANCIES. LUBRICATED RIGHT MLG. AIRCRAFT OK FOR SER VICE. FURTHERMORE, WITHIN THE NEXT TWO DAYS, THERE WERE THREE ADDITIONAL REPORTS OF THE RIGHT MLG UNSAFE LIGHT ILLUMINA TING AFTER GEAR RETRACTION. AFTER REPLACING THE M982 AND M986 CARDS AND THE S74 UPLOCK SENSOR AND CANNON PLUG D4536P WI TH NO HELP, MAINTENANCE REPLACED THE M981 CARD AND THE DOWNLOCK SENSOR. RECHECKED CLEARANCE ON UPLOCK SENSOR PER MM AND 2 L 7 2 4F RT A16WE 1998103000335 19981030 00335 NM 1998 10 30 USAASB98257 1 19980929 A 5730 1060031105 PANEL BOEING 737 737401 1384701 NM LT WING LEAKING A USAA A UNSCHED LANDING K W FLUID LOSS INADEQUATE Q C CL CLIMB 1 EA 19 411US 23880 PBI - FLT 1908 - FLT WAS DELAYED FOR 4 HOURS IN MIA FOR FUEL LEAK REPAIR. AFTER TAKEOFF FROM MIA, F/A NOTICED FUEL LEAK ING FROM LEFT WING AND SPRAYING OFF THE TRAILING EDGE. CAPT WAS NOTIFIED AND SENT F/O BACK TO ACCOMPLISH A VISUAL CHECK . FUEL LEAK WAS REPORTED TO BE SIGNIFICANT. FLT DIVERTED TO PBI WHICH WAS THE NEAREST AIRPORT. NO EMERGENCY WAS DECLA RED, BUT AS A PRECAUTION, THE TOWER HAD CALLED OUT THE CFR EQUIP. FLT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UN DER ITS OWN POWER. NO PASSENGERS WERE ABOARD DUE TO LATENESS OF FLT. MAINTENANCE REPLACED A DAMAGED NUT PLATE AND INST ALLED A NEW FUEL PANEL ON THE LEFT WING UPPER SURFACE. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998103000336 19981030 00336 NM 1998 10 30 USAA980388 1 19980917 A 5315 654581292 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 31662 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 14 INCH AREA OF CORROSION STATION 328 LBL 51 TO RBL 65 FLOORBEAM UPPER CHORD. CORROSION TASK NR C63-107-02. SPLICED IN NEW T-CAP SECTION PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1998103000337 19981030 00337 NM 1998 10 30 USAA980416 1 19980917 A 5320 65505611 HOUSING BOEING 737 7373B7 1384580 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 31662 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT INBOARD FLANGE OF UPPER HINGE HOUSING FOR FORWARD SE RVICE DOOR FRAME 294.5. INSTALLED DOUBLER PER TR 53-10-11. (M) 2 L 7 2 4F RT A16WE 1998103000338 19981030 00338 NM 1998 10 30 USAA980417 1 19980917 A 5330 65184201138 SKIN BOEING 737 7373B7 1384580 NM BS 189 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 31662 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A .5 INCH HOLE IN FORWARD FUSELAGE STATION 189, 2 FT FORWARD AND 1 FT DO WN FROM 1ST OFFICERS WINDOW ON SKIN. REPAIRED EXISTING INTERMI REPAIR TO PERMANENT REV A PER EA 58180A. (M) 2 L 7 2 4F RT A16WE 1998103000339 19981030 00339 NM 1998 10 30 USAA980418 1 19980917 A 5311 654659588 FRAME BOEING 737 7373B7 1384580 NM BS 727-747 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 534AU 24516 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH DENT STATION 747 AND STRINGER 24L, 727E AND STRINGER 25L AND 767 AND STRINGER 21L FRAME. INSTALLED REPAIR ANGLES STATION 727E, STATION 747 STRINGER 24L AND STATION 767 STRI NGER 21L PER EA 62398 AND SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998103000340 19981030 00340 WP 1998 10 30 ORJA98221 1 19981001 A 3350 41B994AD073 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 836RA 53046 IN RNO, OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED 'D' CELL NICAD BATTERIES IN CHARGER 35-27, OPS CHECK OF EMERGENCY LIGHT IS OK. (M) 2 L 7 2 4F RT A6WE 1998103000341 19981030 00341 WP 1998 10 30 ORJA98220 1 19981001 A 3350 60117799 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 880RA 53186 IN RNO, INTERIOR OVERWING EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERHEAD OVERWING EMERGENCY EXIT POWER SUPPL Y UNIT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998103000342 19981030 00342 WP 1998 10 30 ORJA98219 1 19980927 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 10-15 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 880RA 53186 AT RENO, EMERGENCY LIGHTS WERE INOPERABLE AT ROWS 10-15. REPLACED CHARGER AND BATTERIES AT FWD LEFT OVERWING EXIT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998103000343 19981030 00343 WP 1998 10 30 ORJA98218 1 19980921 A 3350 LIGHT DOUG DC9 DC983 3022083 WP SEAT 5A INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 AT SJC, SEAT MOUNTED ESCAPE LIGHT AT 5A WAS INOPERABLE. FOUND AND TIGHTENED LOOSE CONNECTION FOR SEAT MOUNTED EMERGENCY ESCAPE LIGHT. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 1998103000344 19981030 00344 WP 1998 10 30 ORJA98217 1 19980920 A 3350 6011779 POWER SUPPLY DOUG DC9 DC987 3022087 WP ROW 23-26 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY EXIT LIGHTS AT ROWS 23-26 CAME ON, COULD NOT EXTINGUISH. INSTALLED NEW BATTERY ASSEMBLY. OPS CHECK G OOD AT ROWS 23-26. (M) 2 L 7 2 4F RT A6WE 1998103000345 19981030 00345 NM 1998 10 30 ORJA98216 1 19980918 A 3241 60060852 CONTROL UNIT DOUG MD90 MD9030 3023690 NM MLG FAILED A ORJA O OTHER O OTHER NR NOT REPORTED 1 WP 11 901RA 53489 AT RENO, ANTI-SKID FAULT. REMOVED AND REPLACED BRAKE CONTROL UNIT IAW MM 32-00. MAINTENANCE TAXI TEST FOUND NO FAULTS OR DISCREPANCIES. SYSTEM OPS CHECK NORMAL AND OK FOR SERICE. REF ORJA98215. (M) 2 L 7 2 4F RT A6WE 1998103000346 19981030 00346 1998 10 30 GTIA9800106 4 19980917 A 2565 SLIDE DOUG DC9 DC982 3022082 WP PAX DOOR LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 804RA 48048 DTW - L-1 DOOR SLIDE PACK FELL OFF WHEN AIRCRAFT WAS AT GATE. RE-INSTALLED SLIDE PACK IAW MD80 MM 25-61-0. NO DEFECTS NOTED AT THIS TIME. (M) 2 L 7 2 4F A6WE 1998103000347 19981030 00347 WP 1998 10 30 GTIA9800107 1 19980924 A 3350 LIGHT DOUG DC9 DC941 302207N WP CABIN INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 MCO - FLT 127 - CABIN EMERGENCY FLOOR PATH LIGHTING HAS AN AREA OF LIGHT BULBS THAT DO NOT ILLUMINATE. REPAIRED AND REP LACED WIRING POWER FEED STRIP CONNECTION FOR CENTER SECTION OF FLOOR TRACK LIGHTING. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998103000348 19981030 00348 WP 1998 10 30 GTIA9800109 1 19981001 A 3350 SWITCH DOUG DC9 DC932 3022066 WP ROW 8-13 INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 MYR - OVERHEAD EMERGENCY LIGHTS ROWS 8 TO 13 AND 16 TO 21 INOPERATIVE WHEN SWITCH IN COCKPIT IS PLACED TO 'ON'. EMERGEN CY LIGHTS ARM AND CHARGE AND EMERGENCY LIGHTS CHARGING C/B'S PULLED. FOUND SWITCH ON OVERHEAD TO BE FAULTY. REMOVED AN D REPLACED EMERGENCY LIGHT SWITCH AND OPERATIONAL CHECKS GOOD. ALL IAW MM 33-53-0. (M) 2 L 7 2 4F A6WE 1998103000349 19981030 00349 NM 1998 10 30 EIAA980234 1 19980804 A 5730 SKIN BOEING 747 747132 1384882 NM WS 136483884 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 19898 MZJ - DURING C5 CHECK, LEFT WING LOWER SURFACE LEADING EDGE PANEL BULGING DUE TO CORROSION AT WS 1364. REPAIRED WING SK IN PER ECRA 479-57-107-2, WITH 8110-3. (M) 2 L 7 4 4F A20WE 1998103000350 19981030 00350 NM 1998 10 30 EIAA980233 1 19980730 A 2612 FIRE LOOP BOEING 747 747132 1384882 NM NR 4 ENGINE ACTIVATED A EIAA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 481EV 19896 SNN - ON LANDING FLARE AT SHANNON, NR 4 ENGINE HAD A FIRE WARNING. AFTER LANDING NR 4 ENGINE SHUTDOWN, FIRE WARNING LIG HT EXTINGUISHED. NO BOTTLE DISCHARGED. (M) 2 L 7 4 4F A20WE 1998103000351 19981030 00351 WP 1998 10 30 EIAA980264 1 19980918 A 2822 6550934 PUMP DOUG DC9 DC933F 302207A WP FUEL TANK FAILED A EIAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 944F 47194 SEA - AIR TURN BACK DUE TO CENTER TANK BOOST PUMP FAILURE. AFT CENTER BOOST PUMPS. QA AND QB POPPED AFTER TAKEOFF, RES ET AND POPPED AFTER THREE MINUTES. REMOVED AND REPLACED AFT CENTER BOOST PUMP. OPS AND LEAK CHECK GOOD PER MM 28-20-1. (M) 2 L 7 2 4F A6WE 1998103000352 19981030 00352 WP 1998 10 30 EIAA980203 1 19980515 A 5754 SLAT DOUG DC9 DC933F 302207A WP LT WING BENT A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 51746 47191 SIT - ON POST FLIGHT WALKAROUND, FOUND LEFT WING SLAT ASSEMBLY BENT WITH SLIP JOINT BETWEEN SEGMENT NR 1 AND NR 2 BENT A ND BUCKLED. (M) 2 L 7 2 4F A6WE 1998103000353 19981030 00353 NM 1998 10 30 EIAA9802206 1 19980616 A 2910 65B9017082 LINE BOEING 747 747273C 1384896 NM PYLON CHAFED A EIAA K NONE K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 09 471EV 20651 NGU - DURING CLIMB, LOST NR 3 HYDRAULIC SYSTEM, QUANTITY WENT OT ZERO AND PRESSURE WAS FLUCTUATING DOWN TO 2200 PSI. TU RNED SYSTEM OFF. DIVERTED TO JFK. REPLACED HYDRAULIC LINE UNDER GAP COVER IN PYLON AND LEAK CHECKED GOOD MM 29-11-00. (M) 2 L 7 4 4F A20WE 1998103000354 19981030 00354 NM 1998 10 30 EIAA980235 1 19980804 A 5730 SKIN BOEING 747 747132 1384882 NM WS 1297-1309 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 83884 19898 MZJ - DURING C5 CHECK, RIGHT WING LOWER SKIN UPPER SURFACE HAS CORROSION AT FSS 1297-1309. REPAIRED WING SKIN PER ECRA 479-57-108-2 REV A, WITH 8110-3. (M) 2 L 7 4 4F A20WE 1998103000355 19981030 00355 NM 1998 10 30 BJNA980901 1 19980919 A 3350 1000679 LIGHT BOEING 737 737214 138446R NM L2 DOOR INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 EMERGENCY EXIT LIGHT ABOVE L-2 DOOR INOP. REPLACED EMERGENCY LIGHT ASSY IAW BMM 33-51-101, GROUND CHECKS NORMAL. (M) 2 L 7 2 4F A16WE 1998103000356 19981030 00356 NM 1998 10 30 BJNA981001 1 19981006 A 3350 P4010020 BATTERY PACK BOEING 737 737214 138446R NM CABIN DISCHARGED A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 RIGHT FORWARD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY PACK ON RIGHT ENTRY DOOR PER BMM 33-51-71. (M) 2 L 7 2 4F A16WE 1998103000357 19981030 00357 WP 1998 10 30 USAA980413 1 19980918 A 5730 SKIN DOUG DC9 DC981 3022081 WP RT WING CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 46477 48026 PIT - DURING C-CHECK, FOUND 2.25 INCH CRACK ON SKIN AT RT WING LEADING EDGE BETWEEN NR 2 AND NR 3 SLAT PANELS UPPER. ST OP DRILLED CRACK AND INSTALLED DOUBLER PER MD-80 SRM 57-06B PAGE 11, FIG 4. (M) 2 L 7 2 4F A6WE 1998103000358 19981030 00358 WP 1998 10 30 USAA980412 1 19980918 A 5313 LONGERON DOUG DC9 DC981 3022081 WP BS 218-225 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 826US 46477 48026 PIT - DURING C-3 CHECK, FOUND CORROSION ON APPROX 7 INCHES OF LONGERON (1 INCH BY 7 INCH) AT LONGERON 25R STATION 218 TO STATION 225. REPLACED SECTION OF LONGERON (SPLICED IN A SECTION) PER SRM 53-02. (M) 2 L 7 2 4F A6WE 1998103000359 19981030 00359 WP 1998 10 30 USAA980411 1 19980918 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1132/BS 1143 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 933VJ 78361 47216 PIT - DURING RON, FOUND CRACKS RANGING FROM .125 INCH TO .75 INCH ON SKIN AT LT SIDE STATION 1132 BETWEEN LONGERONS 15L/ 16L. CRACKS AT 4 FASTENER HOLES RT SIDE STATION 1143 BETWEEN LONGERONS 12R/159 CRACKS AT 10 FASTENER HOLES. CLASSIFIED A MINOR REPAIR. CUT OUT CRACKED AREAS, INSTALLED FILLERS AND EXTERNAL DOUBLERS PER EA NR 50516. (M) 2 L 7 2 4F A6WE 1998103000360 19981030 00360 WP 1998 10 30 USAA980410 1 19980911 A 5330 591001125 SKIN DOUG DC9 DC982 3022082 WP BS 1429 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 820US 44616 49119 PIT - DURING C-1 CHECK, FOUND 2 INCH CRACK AT DOUBLER STATION 1429 BETWEEN LONGERON 2-3 RIGHT. CUT OUT CRACK SECTION, I NSTALLED DOUBLER PER EA 50498. (M) 2 L 7 2 4F A6WE 1998103000361 19981030 00361 WP 1998 10 30 USAA980409 1 19980913 A 5330 59101309 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 991VJ 75151 47310 PIT - DURING C-5 CHECK, FOUND 1 INCH CRACK AT RADIUS OF -9 DOUBLER UPPER LT CORNER OF VENTRAL DOOR OPENING. ROUTED OUT CRACK AND INSTALLED DOUBLER PER EA 50476. (M) 2 L 7 2 4F A6WE 1998103000362 19981030 00362 WP 1998 10 30 USAA980427 1 19980923 A 5313 LONGERON DOUG DC9 DC931 3022065 WP BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 927VJ 40699 48154 PIT - DURING C-6 CHECK, FOUND LONGEORN CRACKED ACROSS INTERSECTION .20 INCH AT STATION 639 LONGERON 4L. INSTALLED SPLIC E PER SRM 53-02 PAGES 48-53. (M) 2 L 7 2 4F A6WE 1998103000363 19981030 00363 NM 1998 10 30 USAASB98253 1 19980924 A 2613 6678 OVERHEAT LOOP BOEING 737 737401 1384701 NM NR 1 ENGINE FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 407US 23877 CLT - FLT 835 - DURING CLIMB-OUT FROM CLT, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED. AFTER ACCOMPLISHING APPROPRIATE CHECKLIST, LIGHT EXTINGUISHED. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS D ECLARED AND THE ENGINE WAS NOT SHUT DOWN IN FLIGHT. MAINTENANCE FOUND THE NR 1 ENGINE 'A' LOOP INDICATING A FLASE OVERH EAT. REPLACED NR 1 ENGINE CORE LOOP DETECTOR. RAN ENGINE AT POWER WITH NO FAULTS NOTED. SYSTEM OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4F RT A16WE 1998103000364 19981030 00364 NM 1998 10 30 USAASB98245 1 19980918 A 2150 ACM BOEING 737 737401 1384701 NM RT PACK OVERSERVICED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 406US 23876 DCA - FLT 1488 - CREW REPORTED A STRONG OIL TYPE ODOR IN CABIN AT FL280 WHEN USING THE RIGHT PACK. WHEN CREW TURNED OFF RIGHT PACK, ODOR DISSIPATED. FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE OVERSERVICED. DRAINED OIL AND SERVICED TO PROPER LEVEL. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998103000365 19981030 00365 WP 1998 10 30 USAAD98164 1 19980923 A 2913 AS66411LS666 PUMP DOUG DC9 DC981 3022081 WP LT ENGINE FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 807US 48039 PIT-MDT - FLT 710 - AFTER TAKEOFF THE PRESSURE WENT TO ZERO FOR THE LEFT ENGINE HYDRAULIC PUMP. FOR MAINTENANCE CONVENI ENCE THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAU LIC PUMP. (M) 2 L 7 2 4F A6WE 1998103000366 19981030 00366 WP 1998 10 30 USAAD98163 1 19980923 A 3260 833703 SENSOR DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 921VJ 48141 PIT-SDF - FLT 1805 - AFTER REACHING CRUISE ALTITUDE, THE LEFT MAIN GEAR RED UNSAFE ILLUMINATED. THE AIRCRAFT RETURNED T O THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GEAR UPLATCH SENSOR. SEVERAL GEAR RETRACTIONS W ERE COMPLETED AND ALL INDICATIONS WER NORMAL. (M) 2 L 7 2 4F A6WE 1998103000367 19981030 00367 EU 1998 10 30 UF6A980717 1 19980721 A 7722 3038413 PROBE BAG ATP ATP EU NR 2 ENGINE FAILED A UF6A C ABORTED TAKEOFF M OVER TEMP TO TAKEOFF 1 GL 31 855AW 2029 ORD - FLT 5752 - ON TAKEOFF, NR 2 ENGINE ITT EXCEEDED 765 DEGREES CELSIUS. MAINTENANCE REPLACED THERMOCOUPLES. OPS CHE CKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998103000368 19981030 00368 NE 1998 10 30 UF6A980814 2 19980829 A 7321 7919002002 EEC BAG ATP ATP EU PWA PW120 PW126A NE NR 1 ENGINE FAILED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 858AW 6897 90010462 2035 124242 ORD - FLT 5754 - NR 1 ENGINE CONTROL FROZEN ON TAKEOFF ROLL AND PROP FEATHERED. MAINTENANCE INSPECTED ENGINE CONTROL RI GGING, CHECKED CONTINUITY AND RESISTANCE OF NR 2 TORQUE SENSOR. ALL SYSTEMS OPS CHECKED GOOD. NR 1 EEC WAS REMOVED AND OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998103000369 19981030 00369 EU 1998 10 30 UF6A980813 1 19980829 A 7712 310823801 TORQUE SENSOR BAG ATP ATP EU NR 1 ENGINE FAILED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 858AW 11144 9W056 2035 ORD - FLT 5742 - NR 1 ENGINE CONTROL FROZEN ON TAKEOFF ROLL. MAINTENANCE REMOVED AND REPLACED NR 2 TORQUE SENSOR ON NR 1 ENGINE. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998103000370 19981030 00370 EU 1998 10 30 UF6A980902 1 19980904 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 2034 SBN - RIGHT REAR EXTERIOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. (M) 2 L 7 2 4T RT A27NM 1998103000371 19981030 00371 1998 10 30 UF6A980901 4 19980902 A 3417 301FAD22 COMPUTER BAG ATP ATP EU E/E BAY MALFUNCTIONED A UF6A A UNSCHED LANDING O OTHER CR CRUISE 1 GL 31 859AW 12818 1167 2036 ORD - FLT 5711 - NR 2 ADC FAILED IN FLIGHT. MAINTENANCE INSPECTED AND FOUND STATIC QUICK DISCONNECT LOOSE ON NR 2 ADC. RESECURED QUICK DISCONNECT. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998103000372 19981030 00372 EU 1998 10 30 UF6A980903 1 19980904 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 9533 17447 2034 ORD - FLT 5727 - NR 2 OVERHEAD EMERGENCY LIGHTS FAILED TO ILLUMINATE WHEN TESTED. MAINTENANCE REMOVED AND REPLACED NR 5 EMERGENCY POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998103000373 19981030 00373 EU 1998 10 30 UF6A980815 1 19980830 A 6120 7863368 PCU BAG ATP ATP EU NR 1 ENGINE MALFUNCTIONED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 858AW 528 C0184 2035 ORD - FLT 5756 - ON TAKEOFF, PROP NR 1 CWP ILLUMINATED ALONG WITH RED LOW PITCH. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE PCU. PERFORMED HIGH SPEED TAXI. ALL SYSTEMS OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998103000374 19981030 00374 EU 1998 10 30 UF6A980718 1 19980725 A 6120 783368 PCU BAG ATP ATP EU NR 2 ENGINE MALFUNCTIONED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 854AW 8096 2028 CWA - FLT 5720 - NR 2 PROP CWP ILLUMINATED ON TAKEOFF. MAINTENANCE REPLACED THE NR 2 PCU. OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998103000375 19981030 00375 NM 1998 10 30 TSAA9853514 1 19980930 A 5313 STRINGER BOEING 737 737230 NM BS 967 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND CORROSION ON STRINGER 25L AT BS 967, JUST AFT OF WATER SERVICE PANEL. REPAIRED STRINGER 25L P ER SRM 53-10-3. (M) 2 L 7 2 4F RT A16WE 1998103000376 19981030 00376 NM 1998 10 30 TSAA9857515 1 19980930 A 5730 SKIN BOEING 737 737230 NM WS 418 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND LOWER LEFT WING SURFACE AT RSS 418 CORRODED, INBOARD OF NR 1 TRACK. REPAIRED PER ECO 1684 R9. (M) 2 L 7 2 4F RT A16WE 1998103000377 19981030 00377 NM 1998 10 30 TSAA9855516 1 19980930 A 5511 SPAR BOEING 737 737230 NM HORIZ STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND LEFT STABILIZER TOP SIDE STABILIZER STATION 83.50 AFT SPAR HAS CORROSION, TWO PLACES. REPAIRE D PER ECO 1889. (M) 2 L 7 2 4F RT A16WE 1998103000378 19981030 00378 NM 1998 10 30 TSAA9853517 1 19980930 A 5312 PRESS BULKHEAD BOEING 737 737230 NM BS 727 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND LEFT WHEEL WELL AREA BS 727 PRESSURE BULKHEAD CRACK APPROX 2.5 INCH LONG, LOWER CHORD. REPLAC ED LOWER CHORD IAW ECO 1785. (M) 2 L 7 2 4F RT A16WE 1998103000379 19981030 00379 NM 1998 10 30 TSAA9871518 1 19980930 A 7120 MOUNT BOEING 737 737230 NM NR 2 ENGINE LOOSE A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND NR 2 ENGINE FORWARD MOUNT LOOSE. REMOVED AND REPLACED BEARING AND BUSHINGS PER OHM 71-23-01. REPLACED BOLTS AND BUSHINGS USING ECO 2908, AD 98-14-09 AND REFERENCE PER MM 54-41-11. (M) 2 L 7 2 4F RT A16WE 1998103000380 19981030 00380 NM 1998 10 30 TSAA9853519 1 19980930 A 5330 SKIN BOEING 737 737230 NM BS 1155 CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND UPPER FUSELAGE SKIN CRACK AT BS 1155, 10 INCHES LEFT OF BL 0. CRACK APPROXIMATELY 2 INCHES LO NG. VERIFIED PER HFEC. REPAIRED PER SRM 53-30-3. (M) 2 L 7 2 4F RT A16WE 1998103000381 19981030 00381 NM 1998 10 30 TSAA9853522 1 19980930 A 5330 SKIN BOEING 737 737230 NM BS 967 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND LAP JOINT BULGING DUE TO POSSIBLE CORROSION BS 967, STRINGER 25L, AFT OF POTABLE WATER SERVICE PANEL. CLEANED CORROSION ON LAP JOINT IAW SRM 51-10-6. REPAIRED IAW ECO 2497 R1, PER OPTION 11. (M) 2 L 7 2 4F RT A16WE 1998103000382 19981030 00382 NM 1998 10 30 TSAA9853523 1 19980930 A 5330 SKIN BOEING 737 737230 NM BS 947 CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 818AL 22117 DURING HEAVY CHECK, FOUND LAP JOINT BULGING AND SHOWING SIGNS OF CORROSION, BS 947, STRINGER 25L, FORWARD OF POTABLE WAT ER SERVICE PANEL. CLEANED CORROSION ON LAP JOINT IAW SRM 51-10-6. REPAIRED IAW ECO 2907 R1, PER OPTION 11. (M) 2 L 7 2 4F RT A16WE 1998103000383 19981030 00383 EU 1998 10 30 SIMA982741 1 19981001 A 3350 3013017 BATTERY PACK AEROSP ATR72 ATR72212A 8680902 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 548AT 0848 548 SGF - FLT 3560 - EVERY OTHER FLOOR PROXIMITY LIGHT, LOWER AFT EXIT, AND UPPER MIDDLE EXIT SIGN LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED AFT EMERGENCY BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998103000384 19981030 00384 EU 1998 10 30 SIMA982673 1 19980925 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 595-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 174AE 340B174 ABI - DURING MBV INSPECTION, FOUND 3 SEPARATE SECTIONS OF SEAT TRACK CORRODED. PERFORMED REMOVAL AND REPLACEMENT OF TWO SEAT TRACK, AND SPLICE REPAIR ON THE REMAINING ONE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998103000385 19981030 00385 EU 1998 10 30 SIMA982672 1 19980924 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 640-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 ABI - DURING MBV INSPECTION, FOUND 4 SEPARATE SECTIONS OF SEAT TRACK CORRODED. PERFORMED REMOVAL AND REPLACEMENT OF ONE SEAT TRACK, AND SPLICE REPAIRS ON THE REMAINING THREE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998103000386 19981030 00386 EU 1998 10 30 98ZZZM794 1 19980924 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 640-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 ABI - DURING MBV INSPECTION, FOUND 4 SEPARATE SECTIONS OF SEAT TRACK CORRODED. PERFORMED REMOVAL AND REPLACEMENT OF ONE SEAT TRACK, AND SPLICE REPAIRS ON THE REMAINING THREE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998103000387 19981030 00387 EU 1998 10 30 98ZZZM795 1 19980924 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 624-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 ABI - DURING MBV INSPECTION, FOUND 4 SEPARATE SECTIONS OF SEAT TRACK CORRODED. PERFORMED REMOVAL AND REPLACEMENT OF ONE SEAT TRACK, AND SPLICE REPAIRS ON THE REMAINING THREE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998103000388 19981030 00388 EU 1998 10 30 98ZZZM796 1 19980924 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-354 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 ABI - DURING MBV INSPECTION, FOUND 4 SEPARATE SECTIONS OF SEAT TRACK CORRODED. PERFORMED REMOVAL AND REPLACEMENT OF ONE SEAT TRACK, AND SPLICE REPAIRS ON THE REMAINING THREE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998103000389 19981030 00389 WP 1998 10 30 HALA9800334 1 19981001 A 3350 LIGHT DOUG DC9 DC951 3022051 WP CABIN INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 420EA 47689 FLT 128 - HNL - SEVERAL OF THE OVERHEAD EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED INOPERATIVE BULBS AND THE OPERATIONA L CHECK WAS OK. (M) 2 L 7 2 4F RT A6WE 1998103000390 19981030 00390 WP 1998 10 30 EISA98245 1 19981004 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP GALLEY DOOR DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 945VJ 47066 GALLEY DOOR EMERGENCY LIGHT ON SLIDE PACK INOP. GENERATED FROM MAINTENANCE REPORT. REMOVED AND REPLACED BATTERY PACK. (M) 2 L 7 2 4F A6WE 1998103000391 19981030 00391 NM 1998 10 30 EISA98244 1 19980930 A 2750 71001296 ACTUATOR BOEING 727 7272M7 138407S NM TE FLAP FAILED A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 721RW 527030 21200 AFTER TAKEOFF FROM ORB WHILE RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES NR 4 LEADING EDGE DEVICE FAILED TO RETRACT. A CCOMPLISHED APPROPRIATE CHECKLIST, CONTACTED EXPRESS ONE DISPATCH AND WAS DIRECTED TO CPH. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED ACTUATOR AND SWITCH ON NR 4 SLATS, OPS CHECK GOOD IAW MM 27. (M) 2 L 7 3 4F A3WE 1998103000392 19981030 00392 NM 1998 10 30 98ZZZM797 1 19980930 A 2781 40142 SWITCH BOEING 727 7272M7 138407S NM TE FLAP FAILED A A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 721RW 8613 21200 AFTER TAKEOFF FROM ORB WHILE RETRACTING FLAPS FROM 5 DEGREES TO 2 DEGREES NR 4 LEADING EDGE DEVICE FAILED TO RETRACT. A CCOMPLISHED APPROPRIATE CHECKLIST, CONTACTED EXPRESS ONE DISPATCH AND WAS DIRECTED TO CPH. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED ACTUATOR AND SWITCH ON NR 4 SLATS, OPS CHECK GOOD IAW MM 27. (M) 2 L 7 3 4F A3WE 1998103000393 19981030 00393 NM 1998 10 30 EISA98241 1 19980929 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM PAX DOOR INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 316NE 19475 DURING SERVICE CHECK, FOUND FORWARD ENTRY EMERGENCY LIGHT INOPERATIVE. GENERATED BY MAINTENANCE REPORT. REMOVED AND RE PLACED LIGHT IAW MM 33-00. (M) 2 L 7 3 4F A3WE 1998103000394 19981030 00394 1998 10 30 ASAA9880179 4 19980916 A 2565 SLIDE DOUG DC9 DC983 3022083 WP PAX DOOR MALFUNCTIONED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1998103000395 19981030 00395 WP 1998 10 30 ASAA9880177 1 19980916 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 943AS 53018 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000396 19981030 00396 WP 1998 10 30 ASAA9880176 1 19980913 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 974AS 53450 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000397 19981030 00397 1998 10 30 ASAA9880175 4 19980911 A 2565 SLIDE DOUG DC9 DC982 3022082 WP PAX DOOR MALFUNCTIONED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 OAK - DURING CK CHECK, THE L1 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998103000398 19981030 00398 WP 1998 10 30 ASAA9880173 1 19980910 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 979AS 53471 LAX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000399 19981030 00399 WP 1998 10 30 ASAA9880166 1 19980830 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000400 19981030 00400 WP 1998 10 30 ASAA9880165 1 19980829 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 941AS 49925 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON ARM INDICATOR LIGHT WAS FOUND INOPERATIVE. RE PLACED THE LIGHT ASSEMLBY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998103000401 19981030 00401 WP 1998 10 30 ASAA9880163 1 19980828 A 3350 LIGHT DOUG DC9 DC983 3022083 WP ROW 21-23 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 960AS 53074 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS FROM ROWS 21 TO 23 WERE FOUND INOPERATIVE. REPLACED BR OKEN LAMP MODULE AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000402 19981030 00402 NM 1998 10 30 ASAA9840095 1 19980929 A 3350 LIGHT BOEING 737 7374Q8 NM ROW 15-20 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROWS 15-20. REPAI RED WIRING AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998103000403 19981030 00403 NM 1998 10 30 ASAA9840091 1 19980904 A 3350 LIGHT BOEING 737 7374Q8 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 SEA - DURING MAINTENANCE CHECK, THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED LIGHT AS SEMBLIES AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998103000404 19981030 00404 NM 1998 10 30 ASAA9810103 1 19980918 A 3350 883200312 RECEIVER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING AIRCRAFT RECON, THE SEAT PALLET FLOOR TRACK LIGHTS AT 6-11 AND SEAT PALLET LIGHTS AT 8-4 WERE FOUND TO BE I NOPERATIVE. REPLACED RECEIVER ON 6-11 AND BATTERIES ON 6-11 AND 8-4, ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998103000405 19981030 00405 NM 1998 10 30 98ZZZM798 1 19980918 A 3350 6104781 BATTERY BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING AIRCRAFT RECON, THE SEAT PALLET FLOOR TRACK LIGHTS AT 6-11 AND SEAT PALLET LIGHTS AT 8-4 WERE FOUND TO BE I NOPERATIVE. REPLACED RECEIVER ON 6-11 AND BATTERIES ON 6-11 AND 8-4, ALL LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998103000406 19981030 00406 NM 1998 10 30 ASAA9810104 1 19980927 A 3350 BATTERY PACK BOEING 737 737210C 1384459 NM ROW 18-20 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS AT ROWS 18-20 REMAINED ILLUMINATED WITH THE LIGHT SWITC H OFF. REPLACED THE BATTERY PACK AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998103000407 19981030 00407 WP 1998 10 30 ASAA9880197 1 19981002 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000408 19981030 00408 WP 1998 10 30 ASAA9880196 1 19981001 A 3397 WIRE DOUG DC9 DC983 3022083 WP FWD CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 949AS 53022 SEA - PRIOR TO DEPARTURE OF FLIGHT 460, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000409 19981030 00409 WP 1998 10 30 ASAA9880195 1 19980928 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 LAX - PRIOR TO DEPARTURE OF FLT 465, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. RESEATED FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000410 19981030 00410 WP 1998 10 30 ASAA9880193 1 19980926 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000411 19981030 00411 WP 1998 10 30 ASAA9880191 1 19980924 A 3350 POWER SUPPLY DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000412 19981030 00412 WP 1998 10 30 ASAA9880190 1 19980924 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000413 19981030 00413 WP 1998 10 30 ASAA9880187 1 19980923 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 964AS 53078 SEA - AFTER ARRIVAL OF FLT 531 - CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE. R ECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000414 19981030 00414 WP 1998 10 30 ASAA9880186 1 19980923 A 3350 BATTERY DOUG DC9 DC982 3022082 WP ROW 9-10 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 LAX - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 10 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998103000415 19981030 00415 WP 1998 10 30 ASAA9880185 1 19980922 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 ANC - PRIOR TO DEPARTURE OF FLT 92, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIVE . RECONNECTED WIRING IN FLOOR TRACK LIGHTS IN THE FORWARD CABIN AND THEY OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998103000416 19981030 00416 WP 1998 10 30 ASAA9880184 1 19980921 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND DIM. REPLACED THE BATTERIES IN T HE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998103000417 19981030 00417 WP 1998 10 30 ASAA9880183 1 19980921 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998103000418 19981030 00418 EU 1998 10 30 VTZA98250 1 19980802 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY MALFUNCTIONED A VTZA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 315UE 41033 FLT 6218 - RDU-IAD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BAGGAGE SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SMOKE DETECTOR. OP S CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998103000419 19981030 00419 EU 1998 10 30 VTZA98241 1 19980719 A 5270 91SE16 SWITCHES JETAIR JETSTM JETSTM4101 1500501 EU POD CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 302UE 41013 FLT 6170 - IAD-EWR - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO POD DOOR WARNING LIGHT ILLUMINATED. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 08457, MEL 52-4. MAINTENANCE CLO SED DMI 08457 ON 7-20-98 BY CLEANING POD DOOR MICROSWITCHES, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998103000420 19981030 00420 EU 1998 10 30 VTZA98256 2 19980810 A 7320 1379293L407 LINE BAG JETSTM JETSTM3201 1500217 EU LT ENGINE BROKEN A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 472UE 823 FLT 6299 - IAD-ABE - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE BETA LIGHT ILLUMINATED AND OIL PSI DR OPPED TO 70 PSI. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LE FT ENGINE P-3 LINE AND OIL TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000421 19981030 00421 EU 1998 10 30 98ZZZM799 1 19980810 A 7931 41SG107 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 472UE 823 FLT 6299 - IAD-ABE - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE BETA LIGHT ILLUMINATED AND OIL PSI DR OPPED TO 70 PSI. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LE FT ENGINE P-3 LINE AND OIL TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000422 19981030 00422 EU 1998 10 30 98ZZZM800 1 19980810 A 7931 100G14 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 472UE 823 FLT 6299 - IAD-ABE - DURING CRUISE, MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE BETA LIGHT ILLUMINATED AND OIL PSI DR OPPED TO 70 PSI. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LE FT ENGINE P-3 LINE AND OIL TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000423 19981030 00423 EU 1998 10 30 VTZA98253 1 19980809 A 3260 ATG1066 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT MLG OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 495UE 818 FLT 6292 - IAD-ROA - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO LEFT INTERNIST WARNING LIGHT ILLUMINATED. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED UPLOCK SWITCH. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000424 19981030 00424 NE 1998 10 30 VTZA98251 2 19980807 A 7200 310349016 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT NACELLE FAILED A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 EA 27 329UE 41097 P75115 FLT 6194 - IAD-EWR - DURING CRUISE, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LEFT ENGINE OIL PS I WENT TO ZERO. CREW SHUT DOWN ENGINE. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECT ED AND REMOVED AND REPLACED LEFT ENGINE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1998103000425 19981030 00425 EU 1998 10 30 VTZA98252 1 19980808 A 3240 AC69594 MAXERET BAG JETSTM JETSTM3201 1500217 EU BRAKE SYSTEM FAILED A VTZA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 474UE 849 FLT 6427 - IAD-ROA - DURING TAXI, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LOSS OF BRAKE PSI. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED MAXERET, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000426 19981030 00426 NE 1998 10 30 VTZA9267 2 19980823 A 7261 3103971 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE ENGINE CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 329UE 41097 FLT 6190 - IAD-BDL - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL F ILTER AND FLUSHED RT ENGINE OIL SYSTEM AND CLEANED AND REINSTALLED CHIP DETECTOR. OPS CHECK OK. AIRCRAFT WS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1998103000427 19981030 00427 NE 1998 10 30 98ZZZM801 2 19980823 A 7261 30014361 FILTER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE ENGINE CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 329UE 41097 FLT 6190 - IAD-BDL - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE OIL CONTAMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED OIL F ILTER AND FLUSHED RT ENGINE OIL SYSTEM AND CLEANED AND REINSTALLED CHIP DETECTOR. OPS CHECK OK. AIRCRAFT WS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1998103000428 19981030 00428 EU 1998 10 30 SIMA982412 1 19980829 A 2420 31342001 GENERATOR SAAB SF340 340B 7860101 EU RT ENGINE FAILED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 21 338SB 22273 746 340B338 TXK - FLT 5008 - RIGHT AC GENERATOR AND INLET LIGHT ILLUMINATED. SHORTLY AFTER THE RIGHT ENGINE OIL PRESSURE WARNING LI GHT ILLUMINATED ON THE CWP. RIGHT PROP GEARBOX OIL PRESSURE WAS SEEN TO BE DECREASING WHILE THE OIL TEMP WAS INCREASING . OIL WAS SEEN STREAMING FROM THE FRONT OF THE COWLING. AS OIL PRESSURE WAS GOING THROUGH THE YELLOW ARC, ENGINE WAS S HUT DOWN. AIRCRAFT DIVERTED INTO TXK. CREW REPORTED LARGE PUDDLE OF OIL UNDER RIGHT ENGINE AFTER PARKING ON THE RAMP. FOUND THAT THE AC GENERATOR FAILURE PROBABLY DAMAGED THE MOUNT/GARLOCK SEAL AND RESULTED IN FLUID LOSS. REMOVED AND RE PLACED RIGHT ENGINE ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998103000429 19981030 00429 EA 1998 10 30 VTZA98258 1 19980812 A 2750 855D1007 BSPU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 622BR 7187 FLT 6633 - CRW-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS AMBER FLAP FAIL MESSAGE ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT BSPU AND RT OUTBOARD TELEFLEX CABLE FROM ACTUATOR TO BSPU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998103000430 19981030 00430 EA 1998 10 30 98ZZZM802 1 19980812 A 2750 601R93106505 CONTROL CABLE CNDAIR CL600 CL6002B19 1900309 EA TE FLAPS FAILED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 622BR 7187 FLT 6633 - CRW-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS AMBER FLAP FAIL MESSAGE ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT BSPU AND RT OUTBOARD TELEFLEX CABLE FROM ACTUATOR TO BSPU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998103000431 19981030 00431 EA 1998 10 30 VTZA98257 1 19980811 A 2750 860D10018 FECU CNDAIR CL600 CL6002B19 EA TE FLAPS FAILED A VTZA O OTHER F J FLT CONT AFFECTED WARNING INDICATION LD LANDING 1 EA 27 622BR 7187 FLT 6760 - BNA-IAD - DURING LANDING, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP WARNING LIGH T ILLUMINATED, FLAPS STUCK AT 0 DEGREES. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4F RT A21EA 1998103000432 19981030 00432 1998 10 30 VTZA98262 4 19980817 A 3442 6227337001 RADAR R/T BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING L NO TEST CR CRUISE 1 EA 27 477UE 890 FLT 6606 - IAD-ROC - DURING CRUISE, AIRCRAFT RETURNED TO GATE DUE TO WEATHER RADAR INOP. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RADAR R/T, OPS CHECK OK. AIRCRAFT WAS RELEASED AN D RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000433 19981030 00433 EU 1998 10 30 VTZA98261 1 19980816 A 3242 215221 BRAKE BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 477UE 890 FLT 6253 - IAD-ABE - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO ABNORMAL NOISE FROM BRAKES. AIRCRAFT RETURNED TO GAT E WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT MAIN BRAKE ASSY, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000434 19981030 00434 EU 1998 10 30 VTZA98280 1 19980901 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU POD FAILED A VTZA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 EA 27 323UE 41059 FLT 6206 - IAD-CMH - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO POD SMOKE WARNING LIGHT ILLUMINATED. A IRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SMOKE DETECTOR, OPS C HECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998103000435 19981030 00435 EU 1998 10 30 VTZA98279 1 19980831 A 3230 1379098D401 VALVE JETAIR JETSTM JETSTM4101 1500501 EU MLG TRIPPED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 EA 27 320UE 41043 FLT 6483 - IAD-CHS - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WOULD NOT RETRACT. AIRCRAFT RETUR NED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET EMERGENCY EXTENSION PIN. MAINTENANCE PERFORMED G EAR SWING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998103000436 19981030 00436 EU 1998 10 30 VTZA98278 1 19980831 A 3350 LIGHTS JETAIR JETSTM JETSTM4101 1500501 EU CABIN MALFUNCTIONED A VTZA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 27 324UE 41017 FLT 6483 - IAD-CHS - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO EMERGENCY EXIT LIGHTS ILLUMINATED DURING TAXI. MAINT ENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVI CE. (M) 2 L 7 2 4T RT A41NM 1998103000437 19981030 00437 WP 1998 10 30 VTZA98277 2 19980829 A 7200 310338024 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT NACELLE FAILED A VTZA E ENGINE SHUTDOWN X J ENGINE FLAMEOUT WARNING INDICATION AP APPROACH 1 EA 27 470UE 814 P66159 FLT 6376 - CRW-IAD - DURING APPROACH, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS RT ENGINE FAILED ON SHORT FINAL. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT ENGINE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998103000438 19981030 00438 EU 1998 10 30 VTZA98276 1 19980828 A 2910 1379305A95 HOSE BAG JETSTM JETSTM3201 1500217 EU HYDRAULIC SYSTEM LOOSE A VTZA O OTHER K FLUID LOSS LD LANDING 1 EA 27 474UE 849 FLT 6348 - IAD-GSO - DURING LANDING, MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH LT HYDRAULIC PRESSURE INTERMIT TENT. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND TIGHTENED DOWN LINE TO RADIUS ROD. OP S CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998103000439 19981030 00439 WP 1998 10 30 VTZA98275 2 19980828 A 7200 310338024 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT NACELLE BIRDSTRIKE A VTZA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 EA 27 495UE 818 P66020 FLT 6392 - IAD-ORF - DURING TAKEOFF, MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE HAD A BIRDSTRIKE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT ENGINE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998103000440 19981030 00440 NM 1998 10 30 ASAA9840087 1 19980816 A 5210 COLLAR BOEING 737 7374Q8 NM PAX DOOR LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 SEA - PRIOR TO FLT 179, THE R1 DOOR WAS FOUND TO BE STUCK OPEN. FOUND COLLAR LOOSE. REINSTALLED COLLAR AND DOOR OPERAT ED NORMAL. (M) 2 L 7 2 4F RT A16WE 1998103000441 19981030 00441 CE 1998 10 30 PLGA980830A 1 19980814 A 7500 7275031506 LINE CESSNA 340 340A 2076405 CE RT ENGINE CRACKED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 339BE 340A044 PVD - FLT 4541 - AFTER TAKEOFF, THE CREW NOTICED THE RIGHT ENGINE OVERTEMP WARNING ILLUMINATED. ITT WAS REPORTED 961 DE GREES FOR 2-3 SECONDS. POWER WAS REDUCED ON ENGINE AND AIRCRAFT RETURNED TO PVD WITHOUT INCIDENT. MAINTENANCE REPLACED HP BLEED LINE ON RIGHT ENGINE. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 3O 3A25 1998103000442 19981030 00442 EU 1998 10 30 AALA981852 1 19981003 A 5330 SKIN AIRBUS 300 A300B4605R 3930308 EU FUSELAGE DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 70054 461 TUL - FOUND WINDSHIELD NEAR FRAME AND HAS DENT, ABOVE CAPT WINDSHIELD. CUT OUT DAMAGE AREA INSTALLED DOUBLER REPAIR PER SRM 53-11-12-2. (M) 2 L 7 2 4F RT A35EU 1998103000443 19981030 00443 EU 1998 10 30 AALA981896 1 19981007 A 5720 ANGLE AIRBUS 300 A300B4605R 3930308 EU LT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 50051 459 TUL - FOUND LEFT WING ROOT ANGLE CRACKED. REPLACED LEFT PICK UP ANGLE PER ESO 3095, DATED 10-7-98. (M) 2 L 7 2 4F RT A35EU 1998103000444 19981030 00444 NM 1998 10 30 AALA984191 1 19980925 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 904 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 378AN 25447 AFW - FLOORBEAM AT STATION 904 LBL 33 HAD CORROSION BLENDED ON TOP SURFACE. BLEND OUT GOUGES, ENSURED THAT ALL DAMAGE H AS BEEN REMOVED. ROTO/FLAP PEEN BLENDED AREA PER SRM 51-20-06 ALODINE AND APPLY 2 COATS OF PRIMER FILL WITH BMS-5-95 RE F MRB 767-1703. (M) 2 L 7 2 4F RT A1NM 1998103000445 19981030 00445 NM 1998 10 30 AALA984194 1 19980925 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 378AN 25447 AFW - FLOORBEAM AT STATION 1480 HAS CORROSION. BLEND OUT ALL CORROSION, ALODINE ALL BARE SURFACES FINISH WITH 2 COATS O F PRIMED FILL BLENDED AREA WITH BMS PER MRB 767-1693. (M) 2 L 7 2 4F RT A1NM 1998103000446 19981030 00446 NM 1998 10 30 AALA984195 1 19980925 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 378AN 25447 AFW - FLOORBEAM AT STATION 347 AND APPROX RBL 50 HAD CORROSION BLENDED. FABRICATE REPAIR STRAPS, ALODINE ALL BARE ALUMI NUM SURFACES. FINISH BLENDS PER MRB 767-1695. (M) 2 L 7 2 4F RT A1NM 1998103000447 19981030 00447 NM 1998 10 30 AALA984196 1 19980925 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 378AN 25447 AFW - FLOORBEAM STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE. FABRICATE REPAIR STRAPS, ALODINE ALL BARE ALUMINUM FILL BLENDS WITH BMS. INSTALL REPAIR STRAP WET WITH SEALANT PER MRB 767-1701. (M) 2 L 7 2 4F RT A1NM 1998103000448 19981030 00448 NM 1998 10 30 AALA981835 1 19980930 A 5713 STRINGER DOUG MD11 MD11 3023602 NM WS 724 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1761R 48551 TUL - FOUND CRACK IN STRINGER NR 10 LEFT WING TOP STRINGER. REMOVED CRACKED STRINGER SECTION AND INSTALLED SPLICE DOUBL ERS AND NEW STRINGER SECTION PER SRM 57-20-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1998103000449 19981030 00449 WP 1998 10 30 TWAA9817301 1 19981026 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 208-217 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND CORROSION ON MEMBRANE AT STA 208 TO 217, LONGERON 18L. REPLACED MEMBRANE PER SRM 53-05 FIG 55 SHEET 2 AND FASTENER SUB PER SRM 51-60-0 AND ARA 15704. 2 L 7 2 4F A6WE 1998103000450 19981030 00450 WP 1998 10 30 TWAA9817302 1 19981026 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 680 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 988Z 47134 DURING OP 16 MAINT CHECK, FOUND CABIN FLOORBEAM SUPPORT ANGLE CRACKED AT STA 680 LBL 43 IN. INSTALLED NEW FITTING (P/N 3916209-501N), USING TENSION HEAD HI-LOKS AND LIKE FASTENERS. 2 L 7 2 4F A6WE 1998103000451 19981030 00451 CE 1998 10 30 NSVA9810281 1 19981027 A 7110 11891005041 LATCH BEECH 1900 1900C 1154161 CE PWA PT6 PT6A65B 52043 EA RT ENG COWL FAILED A NSVA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 550CJ UC50 97178 RIGHT SIDE COWLING CAME LOOSE IN FLIGHT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. COWLING REMAINED ATTACHED TO THE NACE LLE. MAINTENANCE VISUALLY INSPECTED RT COWLING AND FOUND INBOARD COWLING LATCH FAILED. MAINTENANCE REMOVED AND REPLACE D THE COWLING LATCH ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E4EA 1998103000452 19981030 00452 WP 1998 10 30 VJ9800562 1 19980929 A 5313 59114189914 LONGERON DOUG DC9 DC932 3022066 WP BS 655-756 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 LT WHEEL WELL IN KEEL BEAM AREA AT FS 718-737 CORRODED BEYOND LIMIT IAW DC9 SRM 53-01 FIG 1. REMOVED AND REPLACED LONGE RON IAW DC9 SRM 51-30-2, 51-30-5, 51-30-1 AND 51-30-3. KEEL BEAM DETERMINED TO BE WITHIN LIMIT IAW AIRTRAN RES 981746. 2 L 7 2 4F A6WE 1998103000453 19981030 00453 WP 1998 10 30 VJ9800563 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 AFT CARGO SKIN AT FS 937, L28R, CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED NEW DOUBLER IAW DC9 SRM 53-01 FIG 4, 51-30-2 AND AIRTRAN RES 981737. 2 L 7 2 4F A6WE 1998103000454 19981030 00454 WP 1998 10 30 VJ9800564 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 522 CREASED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 CREASE AT FS 522, L28R, APPROXIMATELY 3 BY 5 TIMES .070 INCHES OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT AREA, RE MOVED DOUBLER, FABRICATED AND INSTALLED REPAIR AND FINGER DOUBLER IAW DC9 SRM 51-10-2, 53-04, FIG 12, 51-30-2, 51-30-5. 51-10-4 AND AIRTRAN RES 981760. 2 L 7 2 4F A6WE 1998103000455 19981030 00455 WP 1998 10 30 VJ9800565 1 19981001 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 379 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 DENT 11.1 BY .063 INCHES AT FS 379, L28-29R, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. CUT OUT DENT, FABRICATED AND INSTA LLED DOUBLER AND FILLER IAW DC9 SRM 53-01 FIG 4 AND AIRTRAN RES 981775. 2 L 7 2 4F A6WE 1998103000456 19981030 00456 WP 1998 10 30 VJ9800566 1 19981008 A 5320 3915135505N FITTING DOUG DC9 DC932 3022066 WP BS 756 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 LONGERON END FITTING AT FS 756, L29L - LBL7, CORRODED. REPLACED FITTING IAW DC9 SRM 51-30-1, 51-30-5 AND 51-10-4. 2 L 7 2 4F A6WE 1998103000457 19981030 00457 WP 1998 10 30 VJ9800567 1 19981008 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 756 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 LONGERON END FITTING AT FS 756, LBL3 - L29L, CORRODED. REPLACED END FITTING IAW DC9 SRM 51-10-3, 51-10-4 AND 51-30-1. 2 L 7 2 4F A6WE 1998103000458 19981030 00458 WP 1998 10 30 VJ9800568 1 19981013 A 5320 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 965-980 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 INTERCOASTAL AFT LEG CRACKED 1.5 INCHES AT FASTENER HOLE FS 965 TO 980, BL O. REMOVED INTERCOASTAL, FABRICATED AND INST ALLED INTERCOASTAL IAW DC9 SRM 51-10-3, 51-30-5, 51-10-2A, 53-11-3, FIG 11 AND AIRTRAN RES 981792. 2 L 7 2 4F A6WE 1998103000459 19981030 00459 WP 1998 10 30 VJ9800569 1 19981013 A 5730 SKIN DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 LT AFT PANEL UNDER LOWER BANANA FAIRING GOUGED AND CHAFED. REMOVED SKIN, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-3, 55-31-0, 51-10-4, 51-30-2 AND RES 981773. 2 L 7 2 4F A6WE 1998103000460 19981030 00460 WP 1998 10 30 VJ9800570 1 19981015 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 980 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 FLOOR SUPPORT BEAM LEGS AND LOWER SIDE AT FS 980, RL27, CORRODED. REMOVED SUPPORT, INSTALLED NEW FLOOR SUPPORT BEAM, FA BRICATED AND INSTALLED 16 EACH DOUBLER REPAIRS IAW DC9 SRM 53-04 FIG 79, 51-10-3 AND 51-10-4. 2 L 7 2 4F A6WE 1998103000461 19981030 00461 EU 1998 10 30 JBXA980005 1 19981027 A 3242 5011809 BRAKE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU RT MLG FAILED A JBXA O OTHER M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 SO 05 103ML 11444 RDU RIGHT MAIN INBOARD BRAKE NR 3 TEMP OVER REDLINE. PERFORMED INSPECTION OF BRAKE OVERHEAT, NO DEFECTS NOTED AT THIS T IME. REMOVED AND REPLACED NR 3 BRAKE IAW AMM 32-41-01 OPS CHK AND LEAK CHK GOOD. REMOVED AND REPLACED NR 3 AND NR 4 MA IN WHEEL ASSY IAW AMM 32-41-01. 2 L 7 2 4F 4 F RT 1998103000462 19981030 00462 WP 1998 10 30 UPS98827991 1 19981016 A 5720 CHORD DOUG DC8 DC871F 302199D WP WS 10-26 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, RT WING I/B LEADING EDGE UPPER CHORD XFS 10.0 TO 26.25 HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998103000463 19981030 00463 WP 1998 10 30 UPS98827992 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 760 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LT WING L/E RIB AT XFS 760 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000464 19981030 00464 WP 1998 10 30 UPS98827993 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 791.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LT WING L/E RIB AT XFS 791.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000465 19981030 00465 WP 1998 10 30 UPS98827994 1 19981020 A 5320 4611067 FITTING DOUG DC8 DC871F 302199D WP BS 70 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FS 70 LONGERON 27R END FITTING CORROSION REMOVAL BEYOND SRM LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998103000466 19981030 00466 WP 1998 10 30 UPS98827995 1 19981015 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 622&628&635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LT WING L/E UPPER SKIN CRACKED 3 PLACES 2 FWD OF T/E XFS 628.75, 622.5 AND 635.0. REPAIRED IAW SRM 5 7-2-1. 2 L 7 4 4F RT 4A25 1998103000467 19981030 00467 WP 1998 10 30 UPS98827996 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LT WING L/E RIB AT XFS 635.0 IS CRACKED AT AFT LWR END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000468 19981030 00468 WP 1998 10 30 UPS98827997 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LT WING L/E RIB AT XFS 810.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000469 19981030 00469 WP 1998 10 30 UPS98827998 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 741 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, RT WING L/E RIB AT XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000470 19981030 00470 WP 1998 10 30 UPS98827999 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 778 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, RT WING L/E RIB AT 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000471 19981030 00471 WP 1998 10 30 UPS98828000 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 822.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, RT WING L/E RIB AT XFS822.5 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000472 19981030 00472 WP 1998 10 30 UPS98828001 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 484.895 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LT WING L/E RIB AT XS 484.895 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998103000473 19981030 00473 EU 1998 10 30 QXEA01536 1 19981026 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8A & 9E FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 479AU 11228 EMERGENCY EXIT LIGHTS AT ROWS 8A AND 9E ARE INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998103000474 19981030 00474 NM 1998 10 30 QXEA9801532 1 19981024 A 3350 P4010021 BATTERY DHAV P2070001201S DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 824PH 157 EMERGENCY FLASHLIGHT BELOW FLIGHT ATTENDANT SEAT NOT FLASHING. REPLACED BATTERY PACK FOR THE EMERGENCY FLASHLIGHT, OPER ATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998103000475 19981030 00475 NM 1998 10 30 QXEA9801533 1 19981026 A 2611 PU90461R2 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTION A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 366PH 510 LAVATORY SMOKE DETECTOR ACTIVATED IN-FLIGHT. NO EVIDENCE OF FIRE OR SMOKE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENA NCE INSPECTED THE AIRCRAFT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REPLACED LAVATORY SMOKE DETECTOR, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998103000476 19981030 00476 NM 1998 10 30 QXEA9801534 1 19981024 A 3350 P4010021 BATTERY DHAV P2070001201S DHAV DHC8 DHC8102 2809003 NM COCKPIT DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 815PH 50 EMERGENCY FLASHLIGHT NOT BLINKING. REPLACED BATTERY PACK, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998103000477 19981030 00477 NM 1998 10 30 QXEA9801535 1 19981026 A 2611 473054 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTIONED A QXEA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 NM 09 363PH 520 SMOKE WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO PDX AND MADE AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AI RCRAFT AND FOUND NO EVIDENCE OF SMOKE OR FIRE. REPLACED BOTH SMOKE DETECTORS IN THE CARGO COMPARTMENT, OPERATIONAL CHEC KS GOOD. 2 H 7 2 4T RT A13NM 1998103000478 19981030 00478 NM 1998 10 30 98FDEA00675 1 19981027 A 2613 CONNECTOR BOEING 727 727227 1384078 NM NR 3 STRUT DIRTY A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 494FE 21532 DURING CLIMB WITH ENG ANTI-ICE ON, ENG NR 3 STRUT OVERHEAT LIGHT ILLUM. ALL ITEM IN EMERGENCY CHECKLIST ACCOMP. LIGHT WENT OUT AND REMAINED OUT WHEN THRUST WAS RESTORED. REPEAT WRITEUP. CONNECTION TO STRUT OVERHEAT DETECTOR REMOVED. CL EANED AND REFITTED. CLAMP CONNECTION IN STRUT AREA RETIGHTENED AS REQUIRE. GROUND RUN CARRIED OUT. SYS FUNCTION CKS S ATISFACTORY. 2 L 7 3 4F A3WE 1998103000479 19981030 00479 NM 1998 10 30 98FDEA00676 1 19981027 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 790 UPPER LOBE, CORROSION ON FLOORBEAM TOP SIDE OF UPPER FLANGE BS 1130, RBL 45 - RBL 65. REMOVED CORROSION, TREATED AND PRIMED AREA, INSTALLED DOUBLER PER EA 7-5310-29681. 2 L 7 3 4F A3WE 1998103000480 19981030 00480 NM 1998 10 30 98FDEA00677 1 19981028 A 5320 CASTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 1066 HFEC IND 2 CRACKS EXTEND FROM NR 1 HOLE LT BS 870 SPLICE IN CASTING AT 11 O'CLOCK AND 7 O'CLOCK ROW 4. REPAIR A CCOMPLISHED PER EA 7-5310-29685. 2 L 7 3 4F A3WE 1998103000481 19981030 00481 NM 1998 10 30 98FDEA00678 1 19981028 A 5320 CASTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 1064 HFEC IND CRACK IN 1 FASTENER HOLE AT LT BS 870 CASTING 2ND HOLE FROM BOTTOM, 1ST ROW FASTENERS BETWEEN STR 10L A ND 11L. REPAIR ACCOMPLISHED PER EA NR 7-5310-29685. 2 L 7 3 4F A3WE 1998103000482 19981030 00482 NM 1998 10 30 98FDEA00679 1 19981028 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 620 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 924 CORROSION ON UPPER FLANGE OF FLOORBEAM 620 BL O TO LBL 25. CUT AND REMOVED DAMAGED PART OF FLOORBEAM AND INSTALL ED UPPER CHORD REPAIR PER SRM 53-10-8 FIG 3. 2 L 7 3 4F A3WE 1998103000483 19981030 00483 NM 1998 10 30 98FDEA00680 1 19981028 A 5320 CASTING BOEING 727 72722 1384002 NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 1034 HFEC IND CRACK AT BOTTOM FASTENER HOLE IN LT BS 870 CASTING, 2ND HOLE FROM BOTTOM, 1ST ROW FASTENERS BETWEEN STR 9L AND 10L. REPAIR ACCOMPLISHED PER EA 7-5310-29685. 2 L 7 3 4F A3WE 1998103000484 19981030 00484 NM 1998 10 30 98FDEA00681 1 19981027 A 5315 FLOORBEAM BOEING 727 72722 1384002 NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 187FE 19079 NR 136 UPPER LOBE BS 1130 HEAVY CORROSION UNDER UPPER AFT LIP OF FLOORBEAM AT RBL 55. REMOVED CORROSION, TREATED AND PR IMED AREA AND INSTALLED DOUBLER PER EA 7-5310-29681. 2 L 7 3 4F A3WE 1998103000485 19981030 00485 NM 1998 10 30 98UAL900475 1 19980926 A 2731 HARDWARE 69633915 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE RT ELEV TAB WORN A UALA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 WP 29 338UA 24242 AIRCRAFT VIBRATING DURING FLIGHT. *S/D* RIGHT HAND ELEVATOR BALANCE TAB INBOARD HINGE HARDWARE WAS WORN. REPLACED SAM E. 2 L 7 2 4F 4 F RT A16WE E2GL 1998103000486 19981030 00486 WP 1998 10 30 98UAL900503 1 19981017 A 2120 AIR DIST DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 WP 29 1849U 46939 ENTIRE AIRPLANE HAS ODOR WHILE ON GROUND AND IN FLIGHT. PASSENGERS COMPLAINED OF OILY ODOR. 2 L 7 3 4F 4 F A22WE E23EA 1998103000487 19981030 00487 NE 1998 10 30 98UAL900504 2 19981017 A 7530 6A3321 ARM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 2 ENGINE FAILED A UALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 WP 29 433UA 589 V10167 NR 2 ENG HAD MULTIPLE COMPRESSOR STALLS, AUTO IGNITION CAME ON. COMPRESSOR STALL OCCURRED AT TOP OF DESCENT. *S/D* ENGI NE DISASSEMBLY INVESTIGATION FOUND THE CAUSE WAS A FAILED HPC STAGE 3 LEVER ARM. THE MANUFACTURER WILL PUBLISH SERVICE BULLETIN 72-0334 IN JANUARY 1999 TO REPLACE THE VSV LEVER ARMS WITH AN IMPROVED DESIGN. UA WILL PROTOTYPE THE MODIFICAT ION WITH THE MANUFACTURER'S ASSISTANCE AND SUBSEQUENTLY MODIFY ALL ENGINES. 2 L 7 2 4F 4 F RT A28NM E40NE 1998103000488 19981030 00488 NM 1998 10 30 98UAL900505 1 19981018 A 7603 THROTTLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE BINDING A UALA E ENGINE SHUTDOWN O OTHER DE DESCENT 1 WP 29 7448U 21902 NR 3 ENGINE SHUT DOWN IN FLIGHT DUE TO BINDING THROTTLE. 2 L 7 3 4F 4 F A3WE E2EA 1998103000489 19981030 00489 NM 1998 10 30 98UAL900507 1 19981020 A 3260 INDICATION AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE LANDING GEAR MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 818UA 882 AFTER TAKEOFF, ECAM WARNING: GEAR NOT DOWN. RETURNED TO FIELD. *S/D* ACCOMPLISHED LGCIU1 AND LGCIU2 TEST. NO FAULTS FO UND. REPLACED EEC DUE TO EPR PROBLEMS. TESTED FMGC AND AFS SYSTEM, ALL OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1998103000490 19981030 00490 1998 10 30 98UAL900508 4 19981020 A 2565 D31516109 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE DOOR 1L MALFUNCTIONED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 449UA 851 DOOR 1L SLIDE DEPLOYED AFTER ARRIVAL AT GATE. *S/D* FLIGHT CREW ACCIDENTALLY DEPLOYED THE SLIDE UPON ARRIVAL. SLIDE WAS REPLACED PER MM 40-25-62-44. 2 L 7 2 4F 4 F RT A28NM E40NE 1998103000491 19981030 00491 NM 1998 10 30 98UAL900509 1 19981020 A 2910 6517840845 TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 6 LE SLAT LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 WP 29 7453U 21907 A-HYDRAULIC SYSTEM PRESSURE INDICATION ZERO. ENGINE 1 AND 2 PUMP LOW PRESSURE LIGHTS ON. LOST ALL A-SYSTEM HYDRAULICS DURING FLAP RETRACTION AFTER LANDING. *S/D* REPAIRED LEAKING HYD LINE AT NR 6 L/E SLAT ACTUATOR. OPS CK FOUND BOTH AC TUATOR ATTACH BRACKETS BROKEN AT UPPER MOUNT HOLES. 2 L 7 3 4F 4 F A3WE E2EA 1998103000492 19981030 00492 NM 1998 10 30 98UAL900510 1 19981020 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 FORWARD CABIN CEILING EMERGENCY LIGHT INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1998103000493 19981030 00493 NE 1998 10 30 98UAL900511 2 19981019 A 7200 ENGINE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 MALFUNCTIONED A UALA O OTHER O OTHER CL CLIMB 1 WP 29 7292U 21570 NR 2 ENGINE EGT LIMITED DURING CLIMB. REDUCED THRUST TO 205 EPR TO KEEP EGT WITHIN LIMITS. RETURNED TO DEN. 2 L 7 3 4F 4 F A3WE E2EA 1998103000494 19981030 00494 NM 1998 10 30 98UAL900512 1 19981021 A 3310 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT COCKPIT FAILED A UALA O OTHER O OTHER AP APPROACH 1 WP 29 7454U 21908 ON SHORT FINAL, FIRST OFFICER'S OVERHEAD MAP LIGHT POPPED AND SHOWERED THE FIRST OFFICER WITH SPARKS. 2 L 7 3 4F 4 F A3WE E2EA 1998103000495 19981030 00495 NM 1998 10 30 98UAL900513 1 19981022 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7288U 21566 FORWARD CABIN CEILING EMERGENCY LIGHT INOPERATIVE. 2 L 7 3 4F 4 F A3WE E2EA 1998103000496 19981030 00496 1998 10 30 98UAL900514 4 19981012 A 2564 TUBE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE SLIDE/RAFT TORN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 185UA 25395 SLIDE/RAFT FAILED PROOF TEST DURING OVERHAUL DUE TO A 6 FOOT TEAR IN THE TOP TUBE CENTER CROSSOVER TUBE. 2 L 7 4 4F 4 F RT A20WE E24NE 1998103000497 19981030 00497 NM 1998 10 30 DHL9871501C 1 19981004 A 5347 SEAT TRACK BOEING 727 727155C 138404Z NM BS 600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, SEAT TRACK TONGUES CRACKED AT BL 48 LEFT BS 600. INSTALLED REPAIR SPLICE PER SRM 53-10-5. N/R 5128 2 L 7 3 4F A3WE 1998103000498 19981030 00498 NM 1998 10 30 DHL9871502C 1 19981008 A 5320 SUPPORT BOEING 727 727155C 138404Z NM BS 279 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, CORROSION AT BS 279 BL 3R UNDER COCKPIT FLOOR. REMOVED CORRODED FLOOR SUPPORT ANGLE, REPLACED FLOOR SUPPORT ANGLE PER SRM 51-40-4. N/R 5142 2 L 7 3 4F A3WE 1998103000499 19981030 00499 NM 1998 10 30 DHL9871503C 1 19981001 A 7110 SKIN BOEING 727 727155C 138404Z NM NR 1 ENGINE COWL STRETCHED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, NR 1 ENGINE INTAKE COWL HAS SKIN STRETCHED BETWEEN FASTENERS AT LOWER T/E POSITION. CUT OUT DAMAGED AREA AN D INSTALLED DOUBLER REPAIR PER SRM 54-30-3, 10 X 3.5. N/R 6009 2 L 7 3 4F A3WE 1998103000500 19981030 00500 NM 1998 10 30 DHL9871504C 1 19981002 A 7110 SKIN BOEING 727 727155C 138404Z NM NR 1 ENGINE COWL OIL CANNING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, NR 1 ENGINE TOP COWL HAS SKIN OIL CANNING BETWEEN NR 10 AND 11 RIBS. INSTALLED REPAIR PER SRM 54-10-3, DOUB LER 8 X 8. N/R 6091 2 L 7 3 4F A3WE 1998103000501 19981030 00501 NM 1998 10 30 DHL9871505C 1 19980102 A 7110 GUSSET BOEING 727 727155C 138404Z NM NR 1 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, NR 1 ENGINE COWL FWD I/B U-BOLT CUTOUT IS GOUGED. REMOVED DAMAGED GUSSETT AND REPLACED PER SRM 51-10-1, 6 X 5. N/R 6097 2 L 7 3 4F A3WE 1998103000502 19981030 00502 NM 1998 10 30 DHL9871506C 1 19981002 A 7110 SKIN BOEING 727 727155C 138404Z NM NR 1 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, NR 1 ENGINE TOP COWL I/B SKIN EDGE IS WORN AND CRACKED JUST AFT OF NR 4 V-BOLT. CUT OUT DAMAGED AREA, INSTA LLED DOUBLER REPAIR PER SRM 51-30-2, 2.5 X 2. N/R 6102 2 L 7 3 4F A3WE 1998103000503 19981030 00503 NM 1998 10 30 DHL9871507C 1 19980102 A 5330 SKIN BOEING 727 727155C 138404Z NM NR 2 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, NR 2 ENGINE LT COWL OUTSIDE SKIN LOWER HALF HAS SEVERAL BURNED HOLES THROUGH SKIN. CUT OUT DAMAGED AREA, AL ODIZED AND PRIMED, INSTALLED REPAIRS PER SRM 54-10-3. DOUBLER 12 X 12. N/R 6133 2 L 7 3 4F A3WE 1998103000504 19981030 00504 NM 1998 10 30 DHL9871508C 1 19980930 A 5280 DOOR BOEING 727 727155C 138404Z NM LT MLG GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT CHECK, LEFT MAIN STRUT DOOR INNER SKIN SURFACE 3.5 INCHES AWAY FROM DOOR CONNECTING LINK HAS GOUGES IN METAL SURFACE. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 51-30-2, 8 X 5. N/R 7016 2 L 7 3 4F A3WE 1998103000505 19981030 00505 NM 1998 10 30 DHL9871509C 1 19981001 A 5720 ANGLE BOEING 727 727155C 138404Z NM LT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, LT WING I/B AND O/B ANGLE CRACKED BELOW NR 7 SPOILER ACTUATOR. REPLACED ANGLES PER SRM 51-30-2. N/R 1043 2 L 7 3 4F A3WE 1998103000506 19981030 00506 NM 1998 10 30 DHL9871510C 1 19980102 A 5753 6924650 CASTING BOEING 727 727155C 138404Z NM NR 1 JASCKSCREW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, NR 1 JACK SCREW FAIRING FORWARD MOUNT CASTING IS CRACKED. REPLACED CASTING PER SRM 51-30-2. N/R 1105 2 L 7 3 4F A3WE 1998103000507 19981030 00507 NM 1998 10 30 DHL9871511C 1 19981001 A 5720 STRIP BOEING 727 727155C 138404Z NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, RT WING O/B SUPPORT ANGLE FOR RT WING LOWER SURFACE PANEL 8506 IS LOOSE AND CORROGATED STRIP IS CRACKED AT FWD END OF SUPPORT. REMOVED AND REPLACED CORROGATED STRIP PER SRM 51-30-2. N/R 2014 2 L 7 3 4F A3WE 1998103000508 19981030 00508 NM 1998 10 30 DHL9871512C 1 19981002 A 5720 SUPPORT BOEING 727 727155C 138404Z NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, RT WING FIXED INTERIOR VERTICAL SUPPORT WEB AT WBL 92.8 IS CRACKED AT THE 11TH BOLT FROM THE BOTOM JUST FWD OF FRONT SPAR. HFEC, INSTALLED DOUBLER REPAIR PER SRM. N/R 2036 2 L 7 3 4F A3WE 1998103000509 19981030 00509 NM 1998 10 30 DHL9871513C 1 19981005 A 5712 RIB BOEING 727 727155C 138404Z NM WS 246 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, R/W LEADING EDGE INTERNAL STRUCTURE UPPER SURFACE RIB AT STA 246 HAS LOWER CHORD ANGLE CORRODED AT APPROX 8 FWD OF WING FRONT SPAR. REMOVED AND REINSTALLED LOWER CHORD ANGLE PER SRM 51-30-2, 23 INCHES LONG. N/R 2118 2 L 7 3 4F A3WE 1998103000510 19981030 00510 NM 1998 10 30 DHL9871514C 1 19981001 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 440-460 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, EXTERNAL SKIN BETWEEN STA 440 AND 460 STR 19L TO 18L HAS TWO GOUGES. CUT OUT DAMAGED AREA, NDT NO CRACKS NO TED. INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 24 X 9.0. N/R 3017 2 L 7 3 4F A3WE 1998103000511 19981030 00511 NM 1998 10 30 DHL9871515C 1 19981002 A 5210 RETAINER BOEING 727 727155C 138404Z NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, FWD ENTRY DOOR AFT EDGE LINER RETAINER CRACKED AT LOWER END. REMOVED AND REPLACED RETAINER PER SRM 51-30-2, 24 X 1 X 1. N/R 3093 2 L 7 3 4F A3WE 1998103000512 19981030 00512 NM 1998 10 30 DHL9871516C 1 19981003 A 5320 ANGLE BOEING 727 727155C 138404Z NM BS 870 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, APU CUTOUT HAS CRACKED VERTICAL ANGLE AT FWD END AT STA 870 BULKHEAD. VERIFIED END OF CRACK WITH NDT. FAB RICATED ANGLE REPAIR PER SRM 51-40-4, .25 X .25. N/R 3116 2 L 7 3 4F A3WE 1998103000513 19981030 00513 NM 1998 10 30 DHL9871517C 1 19981002 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 440 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT CHECK, CORROSION AT BUTT JOINT 440 BETWEEN STR 18 RT AND 19 RT. CUT OUT DAMAGED AREA 10.5 X 4.5 AND INSTALLED DOUBLE R REPAIR PER S/B 53-0084, 14.5 X 17. N/R 3132 2 L 7 3 4F A3WE 1998103000514 19981030 00514 NM 1998 10 30 DHL9871518C 1 19981006 A 5320 ANGLE BOEING 727 727155C 138404Z NM BS 1580 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, EMPENNAGE VERTICAL AFT SPAR APPROX BS 1580 APPROX WL 462 LEFT ANGLE BRACKET CRACKED. REMOVED AND REPLACED A NGLE BRACKET PER SRM 55-10-1. N/R 4057 2 L 7 3 4F A3WE 1998103000515 19981030 00515 NM 1998 10 30 DHL9871519C 1 19981006 A 5530 ANGLE BOEING 727 727155C 138404Z NM TAIL CONE BURNT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, AFT FACE OF TAIL CONE ATTACH HOUSING SUPPORT ANGLE IS BURNT AT CENTER TOP. REMOVED AND REPLACED Z ANGLE PER SRM 51-10-1, 24 INCHES LONG. N/R 4059 2 L 7 3 4F A3WE 1998103000516 19981030 00516 NM 1998 10 30 DHL9871520C 1 19981029 A 2782 ANGLE BOEING 727 727155C 138404Z NM NR 2 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, LEFT WING NR 2 SLAT ACTUATOR COVER DOOR BOTH ATTACH ANGLE I/B AND O/B ARE CRACKED AT FWD END. REMOVED AND REPLACED ATTACH ANGLES PER SRM 51-40-4, 11 INCHES LONG. N/R 1112 2 L 7 3 4F A3WE 1998103000517 19981030 00517 NM 1998 10 30 DHL9871521C 1 19980108 A 5720 STIFFENER BOEING 727 727155C 138404Z NM WS 92 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, LEFT WING VERTICAL STIFFENER CRACKED AT LOWER END ON FWD SPAR WEB. STOP DRILLED CRACK, HFEC, INSTALLED ANGL E REPAIR PER SRM 51-40-3, 1.125 X 1.125 X 6.5. N/R 1124 2 L 7 3 4F A3WE 1998103000518 19981030 00518 NM 1998 10 30 DHL9871522C 1 19981002 A 2782 FITTING BOEING 727 727155C 138404Z NM NR 3 SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, LEFT FRONT SPAR NR 3 SLAT ACTUATOR I/B SUPPORT FITTING IS CRACKED AT TOOLING HOLE. REMOVED AND REPLACED SU PPORT FITTING PER SRM 51-10-1. N/R 1113 2 L 7 3 4F A3WE 1998103000519 19981030 00519 NM 1998 10 30 DHL9871523C 1 19981013 A 5720 BRACKET BOEING 727 727155C 138404Z NM RT WING TIP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, RIGHT WING TIP FWD NAV LIGHT BRACKET CRACKED AT I/B UPPER CORNER. REMOVED AND REPLACED BRACKET PER SRM 57-2 0-1, 8 X 3.1. N/R 2123 2 L 7 3 4F A3WE 1998103000520 19981030 00520 NM 1998 10 30 DHL9871524C 1 19981005 A 5712 RIB BOEING 727 727155C 138404Z NM RT WING TIP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, RIGHT WING TIP CRACK AT FWD UPPER EDGE. REMOVED AND REPLACED FWD RIB PER SRM 51-30-2. N/R 2064 2 L 7 3 4F A3WE 1998103000521 19981030 00521 NM 1998 10 30 DHL9871525C 1 19981002 A 5712 RIB BOEING 727 727155C 138404Z NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, RIGHT WING FIXED L/E INTERIOR THE NR 6 SLAT I/B TRACK SUPPORT RIB AT FRONT SPAR IS CRACKED VERTICALLY AT THE ATTACH BOLTS. INSTALLED NEW ATTACH ANGLES AT RT LEADING EDGE I/B TRACK AT NR 6 SLAT PER SRM 57-20-1, 10 INCHES LONG. 2 L 7 3 4F A3WE 1998103000522 19981030 00522 NM 1998 10 30 DHL9871526C 1 19981002 A 2782 FITTING BOEING 727 727155C 138404Z NM NR 6 LE SLAT ACT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, RT WING LEADING EDGE THE NR 6 L/E FLAP ACTUATOR HINGE UPPER SUPPORT FITTING IS CRACKED AT O/B FLANGE ATTACH FASTENERS. REMOVED AND REPLACED FITTING PER SRM 51-30-2. N/R 2034 2 L 7 3 4F A3WE 1998103000523 19981030 00523 NM 1998 10 30 DHL9871527C 1 19981006 A 5330 SKIN BOEING 727 727155C 138404Z NM BS 690-710 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, CORROSION LAP JOINT STA 690 TO STA 710. REMOVED CORROSION, BEYOND LIMITS, ACCOMPLISHED HFEC INSP FOR FASTEN ER HOLES. NO CRACKS NOTED. LFEC OF LAP SEAM. CUT OUT DAMAGED AREA PER SRM, FROM STA 698 TO 710. INSTALLED REPAIR PE R SRM 53-30-3 AND S/B 53-0072, 19 X 5. N/R 3136 2 L 7 3 4F A3WE 1998103000524 19981030 00524 NM 1998 10 30 DHL9871528C 1 19981019 A 5320 WEB BOEING 727 727155C 138404Z NM BS 1263 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 715DH 19618 AT C-CHECK, VERTICAL WEB CRACKED AT BOTTOM LIGHTENING HOLES AT BS 1263 RT SIDE OF AFT AIRSTAIRS AREA. STOP DRILLED CRA CK, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 2 X 6. N/R 3185 2 L 7 3 4F A3WE 1998103000525 19981030 00525 1998 10 30 RRXA98447 4 19981024 A 3421 258733513 VERT GYRO DOUG DC8 DC871F 302199D WP NR 2 FAILED A RRXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 15 8091U 45995 F/O'S HORIZON SHOWS INTERMITTENT GYRO AND FLIGHT DIRECTOR FLAGS IN VIEW AND DIFFERS 5-20 DEG NOSE UP. REMOVED AND REPLA CED NR 2 VERTICAL GYRO, SYSTEM OPS CHECKS GOOD IAW DC-8 M/M. 2 L 7 4 4F RT 4A25 1998110300001 19981103 00001 WP 1998 11 3 ORJA98236 1 19980818 A 5320 MS20470AD5 SUPPORT DOUG DC9 DC982 3022082 WP BS 160 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON UPPER FLANGE OF STATION 160 LEFT TO RIGHT FLOOR SUPPORT UNDER EPC PANEL. REPAIRED IAW DC-9/MD-80 S RM 51-00-1, 51-01, 51-10-0, 51-10-1, 51-10-2, 51-10-3, 51-10-4, 51-10-2, 51-30-3 AND 53-01. (M) 2 L 7 2 4F A6WE 1998110300002 19981103 00002 WP 1998 11 3 ORJA98260 1 19980922 A 5320 7075T6080 BRACKET DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 SUPPORT ANGLE BETWEEN FIRST AND SECOND LIGHTENING HOLES CORRODED ON WEB FOR AFT PIT THRESHOLD FRAME. CORROSION IS LEVEL 2. REMOVED ANGLE, FABRICATED NEW AND INSTALLED ANGLE IAW DC9/80 SRM 51-30-2, 53-01, 51-10-2, 51-10-3. (M) 2 L 7 2 4F A6WE 1998110300003 19981103 00003 WP 1998 11 3 ORJA98256 1 19981008 A 3350 EM1267 BATTERY DOUG DC9 DC987 3022087 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAS VEGAS, RIGHT OVERWING EMERGENCY LIGHTS CAME ON DURING DESCENT AND WOULD NOT GO OUT. REPLACED RIGHT OVERWING EXIT EMERENCY LIGHTS BATTERIES WITH NEW. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998110300004 19981103 00004 1998 11 3 ORJA98254 4 19980525 A 2565 D29982107 SLIDE DOUG DC9 DC983 3022083 WP PAX DOOR FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 AT MHV, C-CHECK L-1 DOOR SLIDE FAILS LIGHT SYSTEM CHECK PER CARD. REMOVED AND REPLACED DEFECTIVE L-1 DOOR SLIDE PER MM 25-62-00. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998110300005 19981103 00005 WP 1998 11 3 ORJA98253 1 19981008 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP PAX DOOR INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 AT SJC, EMERGENCY EXIT LIGHT INOPERATIVE AT L-2 DOOR. REMOVED AND REPLACED LIGHT UNIT ASSEMBLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998110300006 19981103 00006 WP 1998 11 3 ORJA98251 1 19980822 A 5347 SR095301157003A SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1309 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON SEAT TRACK STATION 1309 LBL 44. CUT OUT DAMAGED SECTION OF SEAT TRACK AND SPLICED IN NEW SECTION I AW DC-9 SRM 53-05. (M) 2 L 7 2 4F A6WE 1998110300007 19981103 00007 WP 1998 11 3 ORJA98249 1 19980821 A 5320 5936663503 CLIP DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON SEVERAL AFT CARGO TRACK FLOORBOARD ATTACH POINTS UNDER NUT CLIPS, LEFT AND RIGHT SIDES, FUEL LENGTH OF TRACKS. REPLACED IAW MD80/DC9 SRM 51-10-3, 51-10-4, 53-04, 53-05 AND 53-05-01. (M) 2 L 7 2 4F A6WE 1998110300008 19981103 00008 WP 1998 11 3 ORJA98250 1 19980821 A 5320 SHEAR CLIP DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON FRAME 1287 BETWEEN STRINGER 28R AND 27L. CUT OUT BAD SECTION OF SHEAR CLIP AND FABRICATED AND INST ALLED NEW CLIP IAW DC-9 SRM 53-03 FIG 3. (M) 2 L 7 2 4F A6WE 1998110300009 19981103 00009 WP 1998 11 3 ORJA98245 1 19980821 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 160 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION FLOOR SUPPORT ANGLE FORWARD OF L-1 DOOR AREA FS FORWARD OF STATION 160 HAS CORROSION AT DOME NUT AREA AND INTERIOR SURFACE. REMOVED, FABRICATED, TREATED, PRIMED AND REINSTALLED NEW FLOOR SUPPORT ANGLE IAW DC-9 SRM 51-10-2 , 21-10-3, 51-10-4 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1998110300010 19981103 00010 WP 1998 11 3 ORJA98246 1 19980823 A 5347 S493191788 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1211-1309 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON SEAT TRACK, STATION 1211, 1231, 1271, 1309 LBL 22. REMOVED AND REPLACED SECTION FROM 1164 TO 1309 IAW DC9 SRM 53-05 FIG 4F. (M) 2 L 7 2 4F A6WE 1998110300011 19981103 00011 WP 1998 11 3 ORJA98248 1 19980820 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1211 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON STRINGER 29R AND FRAME 1211, AFT PIT AFT DOOR FRAME. BLENDED CORROSION IAW DC9 SRM 51-10-3 ON FRAM E WITH IN LIMITS IAW DC9 SRM 53-01. FABRICATED NEW STRINGER SUPPORT IAW DC9 SRM 51-10-2. TREATED AND PRIMED IAW DC9 SR M 51-10-3. INSTALLED IAW DC9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1998110300012 19981103 00012 WP 1998 11 3 ORJA98240 1 19980822 A 5320 SHEAR TIE DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON AFT PIT SHEAR TIE AT STATION 1155 BETWEEN STRINGER 29R AND 29L. FABRICATED NEW SHEAR TIE IAW SRM 5 1-10-1 AND REINSTALLED ALL PARTS IAW DC-9 AND 51-30-2, OPS CHECK GOOD IAW MD-80 MM 21-00-00. (M) 2 L 7 2 4F A6WE 1998110300013 19981103 00013 WP 1998 11 3 ORJA98241 1 19980820 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION FORE TO AFT CABIN FLOOR SUPPORT CORRODED STATION 160 TO 200, 18 INCHES INBOARD OF R-1 DOOR. REMOVED, FABRICATED AND REINSTALLED IAW DC-9 SRM 51-10-22, 51-30-2. (M) 2 L 7 2 4F A6WE 1998110300014 19981103 00014 WP 1998 11 3 ORJA98238 1 19980820 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION, LEFT TO RIGHT CABIN FLOOR SUPPORT CORRODED STATION 160 FROM CABIN C/B TO RIGHT. REMOVED, FABRICATED, AND REINSTALLED IAW DC9 51-10-2 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1998110300015 19981103 00015 WP 1998 11 3 ORJA98233 1 19980814 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 180 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON LEFT TO RIGHT CABIN FLOOR SUPPORT AT STATION 180 FROM C/L TO RIGHT SIDE. FABRICATED NEW FLOOR SUPP ORT IAW DC9 SRM 51-10-2. TREATED AND PRIMED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-3. (M) 2 L 7 2 4F A6WE 1998110300016 19981103 00016 WP 1998 11 3 ORJA98227 1 19980812 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 200 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION AT STATION 200 APPROX 12 INCHES LEFT OF CENTERLINE FORWARD TO AFT CABIN FLOOR. SUPPORT EXFOLIATED AT AFT END AND CORRODED AT UPPER EDGE HOLES. FABRICATED NEW EXTUSION IAW DC9 SRM 51-10-2. TREATED AND PRIMED IAW DC9 SRM 51-10-3. INSTALLED EXTRUSION IAW DC9 SRM 51-30-1 AND 51-30-5. (M) 2 L 7 2 4F A6WE 1998110300017 19981103 00017 WP 1998 11 3 ORJA98224 1 19980812 A 5320 ANGLE DOUG DC9 DC982 3022082 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION AND CRACK ON FLOOR EDGE TRIM ANGLE AT AFT LOWER CORNER OF R1 DOOR. REMOVED CORRODED ANGLE. FABRICATE D NEW ANGLE IAW DC 9 SRM 51-10-2. INSTALLED ANGLE IAW DC9 51-30-2. (M) 2 L 7 2 4F A6WE 1998110300018 19981103 00018 WP 1998 11 3 ORJA98223 1 19980812 A 5320 ANGLE DOUG DC9 DC982 3022082 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION AND CRACK ON FLOOR EDGE TRIM ANGLE, AT FORWARD LOWER CORNER ON R-1 DOOR. REMOVED CORROSION, FABRICATE D NEW ANGLE IAW DC-9 SRM 51-10-2, INSTALLED IAW DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1998110300019 19981103 00019 WP 1998 11 3 ORJA98222 1 19980812 A 5320 MS20470AD44 SUPPORT DOUG DC9 DC982 3022082 WP BS 196 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION FOUND AT STATION 196, APPROX 38 INCHES LEFT OF CENTERLINE LEFT TO RIGHT CABIN FLOOR SUPPORT EXFOLIATED UNDER FORWARD WALL OF CLOSET. REMOVED AND REPLACED SUPPORT IAW DC9 SRM 51-10-4 AND 51-30-2. (M) 2 L 7 2 4F A6WE 1998110300020 19981103 00020 WP 1998 11 3 ORJA98234 1 19980819 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 465 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON FORWARD PIT FRAME AT FS 465 FROM STA 28L TO 28R. REPAIRED DAMAGED FRAME IAW DC9 SRM 53-03 AND 51-3 0-2. (M) 2 L 7 2 4F A6WE 1998110300021 19981103 00021 WP 1998 11 3 ORJA98229 1 19980815 A 5320 46621 FASTENER DOUG DC9 DC982 3022082 WP BS 1098 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON SEVERAL HI-LOCK NUTS ON FRAME ATTACH POINTS STATION 1098, BETWEEN STRINGER 28L AND 28R. REMOVED AN D REPLACED CORRODED NUTS IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1998110300022 19981103 00022 WP 1998 11 3 ORJA98230 1 19980815 A 5320 46621 FASTENER DOUG DC9 DC982 3022082 WP BS 1117-1130 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON SEVERAL HI-LOCK NUTS ON STRINGER 29R BETWEEN STATION 1117 AND 1130. REMOVED CORRODED HI-LOCK NUTS ON STRINGER 29R, BETWEEN STATION 1117 AND 1130. INSTALLED SERVICEABLE NUTS AND WASHERS IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1998110300023 19981103 00023 WP 1998 11 3 ORJA98231 1 19980815 A 5320 48290 FASTENER DOUG DC9 DC982 3022082 WP BS 1007-1041 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON HI-LOCK NUTS ON STRINGERS 30 AND 29R BETWEEN STATION 1007-1041. REPLACED CORRODED NUTS AND WASHERS IAW DC9 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1998110300024 19981103 00024 WP 1998 11 3 ORJA98232 1 19980815 A 5311 MS21042L3 FRAME DOUG DC9 DC982 3022082 WP BS 1117 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON FRAME AND ATTACH NUTS STATION 1117 AT STRINGER 28L. REMOVED AND REPLACED CORRODED NUTS IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1998110300025 19981103 00025 WP 1998 11 3 ORJA98228 1 19980812 A 5320 MS2104263 INTERCOSTAL DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION, AFT PIT INTERCOSTAL BELOW DOOR FRAME SUPPORT WEB AND BETWEEN STATION 1174 AND 1183 HAS CORRODED MOUNT FASTENERS BETWEEN STRINGER 29R AND 26R. REPLACED HARDWARE ON HI-LOCKS IAW DC9 MD80 SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1998110300026 19981103 00026 WP 1998 11 3 ORJA98226 1 19980813 A 5320 MS20470AD55 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION IN SEVERAL PLACES, FORE TO AFT CABIN FLOOR SUPPORT STATION 160 TO 200, 1ST RT OF C/L. REMOVED AND REP LACED SUPPORT IAW 51-30-2 AND 51-10-02. (M) 2 L 7 2 4F A6WE 1998110300027 19981103 00027 WP 1998 11 3 ORJA98225 1 19980812 A 5320 STRAP DOUG DC9 DC982 3022082 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON STRAP BETWEEN FORWARD AND AFT GIRT BAR LOCK CASTINGS AT R1 DOOR. REMOVED CORRODED STRAP. FABRICAT ED NEW STRAP IAW DC9 SRM 51-10-2. INSTALLED IAW DC9 SRM 51-10-2. (M) 2 L 7 2 4F A6WE 1998110600001 19981106 00001 NM 1998 11 6 TWAA9817401 1 19981028 A 3350 90083 BATTERY BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54345 21632 FOUND DUAL EMERGENCY EXIT SIGN IN CEILING OPPOSITE AFT GALLEY WAS INOPERATIVE. REPLACED BATTERY PACK. CHECK-C 6-12-98 MCI. 2 L 7 3 4F A3WE 1998110600002 19981106 00002 NM 1998 11 6 VJ9800571 1 19981012 A 5330 SKIN BOEING 737 737284 138448R NM FS 727 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 FUSELAGE SKIN UNDER STRINGER 27R AT STA 727-727A CORRODED. REMOVED CORROSION IAW SRM 53-30-1, TRIMMED OUT SKIN AND FABR ICATED FILLER AND DOUBLER IAW B737 SRM 53-30-3. ALODINED, PRIMED AND INSTALLED REPAIR IAW B737 SRM 51-10-2, 51-20-11, 5 3-30-3 AND 51-30-2. 2 L 7 2 4F A16WE 1998110600003 19981106 00003 SO 1998 11 6 COMA9810243 1 19981028 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 18 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 120233 EMERGENCY EXIT SIGN, ROW 8 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998110600004 19981106 00004 SO 1998 11 6 COMA9810244 1 19981028 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 249CA 120230 EMERGENCY EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998110600005 19981106 00005 EA 1998 11 6 COMA9860329 1 19981028 A 5330 601R35005 SKIN CNDAIR CL600 CL6002B19 EA BS 599 DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 945CA 7069 DAMAGE FOUND BY CREW ON POST FLIGHT INSPECTION. DENT BELOW CARGO DOOR AREA AT FS 599.00 AND STRINGER 22L AND 23 DENT WA S .098 DEEP, WITH A GOUGE OF .015. DAMAGED AREA WAS REMOVED AND REPAIRED IN ACCORDANCE WITH CRJ SRM 53-00-31. 2 L 7 2 4F RT A21EA 1998110600006 19981106 00006 EA 1998 11 6 COMA9860330 1 19981028 A 3150 14034007 WARNING UNIT CNDAIR CL600 CL6002B19 EA RT INST PANEL LOOSE A COMA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SO 01 918CA 7018 CO-PILOTS MASTER WARNING UNIT FELL OUT DURING TAKE OFF. INSTALLED A SERVICABLE MASTER WARNING UNIT. 2 L 7 2 4F RT A21EA 1998110600007 19981106 00007 NM 1998 11 6 UPS98228008 1 19981009 A 7603 BRACKET BOEING 727 727108C 1384039 NM NR 3 ENGINE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C ENGINE NR 3 ENGINE CONTROLS DRUM INSTALLATION, SUPPORT BRACKET HAS SUSPECT CRACK. REPAIRED BRACKET, R EINSTALLED AS PER MM CHP 76-11-21. 2 L 7 3 4F A3WE 1998110600008 19981106 00008 NM 1998 11 6 UPS98228009 1 19981012 A 2760 SUPPORT ROD BOEING 727 727108C 1384039 NM NR 8 SPOILER SHEARED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C NR 8 SPOILER I/B HINGE SUPPORT ROD SHEARED. SUPPORT ROD REMOVED AND REPLACED IAW MM SRM 51-30-2. 2 L 7 3 4F A3WE 1998110600009 19981106 00009 NM 1998 11 6 UPS98228010 1 19981008 A 2710 CASTING BOEING 727 727108C 1384039 NM LT AILERON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C ON REMOVAL OF LT INB AILERON TURNAROUND PULLEY, PULLEY CASTING FOUND CORRODED AT LWR LUG. REPLACED LT I/B TURNAROUND CASTING IAW SRM 51-30-02 AND MM 20-10-20. 2 L 7 3 4F A3WE 1998110600010 19981106 00010 NM 1998 11 6 UPS98228011 1 19981013 A 5753 SUPPORT BOEING 727 727108C 1384039 NM RT TE FLAP CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C SUPPORT ASSY CORRODED FOR RT I/B FLAP I/B TRACK AT ATTACH HOLE FOR MLG FITTING BOLT. SUPPORT ASSY REP LACED IAW MM 32-11-51. 2 L 7 3 4F A3WE 1998110600011 19981106 00011 NM 1998 11 6 UPS98228013 1 19981023 A 3211 BEARING BOEING 727 727108C 1384039 NM RT MLG CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C FWD RT MLG TRUNNION BEARING (FWD) AND SUPPORT CORRODED. BEARING AND SUPPORT REPLACED IAW MM 32-11-51 AND 32-11-72. 2 L 7 3 4F A3WE 1998110600012 19981106 00012 NM 1998 11 6 UPS98228014 1 19981007 A 5330 SKIN BOEING 727 727108C 1384039 NM BS 1130 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE:C SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 1130 JUST ABOVE STR 4 R. REPAIR CARRIED OUT IAW SRM 53-30-3 FIG 5. 2 L 7 3 4F A3WE 1998110600013 19981106 00013 NM 1998 11 6 UPS98428002 1 19981028 A 3350 900835A BATTERY PACK BOEING 747 747* NM CREW SERV DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 521UP 1 INSPECTION TYPE:ASE BATTERY VERY LOW CHARGE NOTE: BATTERY FOR CREW SVCS DOOR EMERGENCY LIGHTS. REMOVED AND REPLACED BAT TERY. OPS GOOD PER MM 25-60-00. 2 L 7 4 4F RT A20WE 1998110600014 19981106 00014 NM 1998 11 6 UPS98628012 1 19981027 A 2612 M10427 LOGIC CARD BOEING 767 76734AF 1385212 NM LT COCKPIT FAILED A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 317UP 27745 FIRE LIGHT ON PILOTS CENTER PANEL ILLUMINATED. ALL OTHER INDICATIONS NORMAL. LIGHT EXTINGUSHED DURING DESCENT. FOUND CARD M10427 TO CAUSE FAULT, (AUTO FIRE/OVERHEAT LOGIC TEST CARD). REMOVED AND REPLACED CARD M10427, THIS CLEARED FAULT. PERFORMED SYSTEM TEST OF ENGINE APU, LOWER/MAIN CARGO AFOLTS PER MM26-10-01. SYSTEM OPS CKS GOOD WITH NO FAULTS. 2 L 7 2 4F RT A1NM 1998110600015 19981106 00015 NM 1998 11 6 UPS98628015 1 19981029 A 3350 BULB BOEING 767 76734AF 1385212 NM CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 308UP 27761 EMERGENCY LIGHT UNARMED LIGHT INOP. RELAMPED, OPS CHK GOOD. 2 L 7 2 4F RT A1NM 1998110600016 19981106 00016 WP 1998 11 6 UPS98828003 1 19981014 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 270-280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C FWD LOWER CARGO LONG 36 HAS A CRACK ON THE LOWER FLANGE BETWEEN F/S 270-280. REMOVED AND REPLACED SEC TION OF LONGERON IAW SRM 53-2-2. 2 L 7 4 4F RT 4A25 1998110600017 19981106 00017 WP 1998 11 6 UPS98828004 1 19981010 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 285-295 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C LONGERON 35L CORRODED F/S 285-295. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 53 -2-2. 2 L 7 4 4F RT 4A25 1998110600018 19981106 00018 WP 1998 11 6 UPS98828005 1 19981015 A 5320 3755822501N FITTING DOUG DC8 DC871F 302199D WP BS 270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C FWD LOWER CARGO BATHTUB FITTING CRACKED AT F/S 270 BETWEEN LONG 35L- 36. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998110600019 19981106 00019 WP 1998 11 6 UPS98828006 1 19981010 A 5320 57554431 DOUBLER DOUG DC8 DC871F 302199D WP FWD LAV SERVICE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C FWD EXTERNAL RT FUSELAGE CORROSION ON PANEL LAND AT DEACTIVATED LAVATORY SERVICE PANEL. REMOVED, FABR ICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, DWG 5755443, AND DHC SK-729-598. 2 L 7 4 4F RT 4A25 1998110600020 19981106 00020 WP 1998 11 6 UPS98828007 1 19981016 A 5320 3755822501N SHEAR TIE DOUG DC8 DC871F 302199D WP BS 280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C SHEAR TIE FITTING AT F/S 280 BETWEEN L-35L TO 36. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998110600021 19981106 00021 WP 1998 11 6 UPS98828016 1 19981013 A 5315 37549461 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C F/S 1160 AT THE RT CUSP, THE FLOORBEAM TO CUSP FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3754946. 2 L 7 4 4F RT 4A25 1998110600022 19981106 00022 WP 1998 11 6 UPS98828017 1 19981013 A 5347 57792231 CARGO TRACK DOUG DC8 DC871F 302199D WP BS 1330-1410 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE:C LOWER CARGO TRACK CORRODED F/S 1330-1410 L-34L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0 AND DWG 5779223. 2 L 7 4 4F RT 4A25 1998110600023 19981106 00023 WP 1998 11 6 ABXA9800928 1 19981027 A 3260 7000010101 SWITCH DOUG DC8 DC861 3021952 WP RT MLG MALFUNCTION A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 844AX 45848 DURING INITIAL GEAR REACTION, RIGHT GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, NO CHANGE. PERFORMED GEAR U PLATCH CHECK. LIGHT EXTINGUISHED AND REMAINED OUT. REPLACED RIGHT MAIN LANDING GEAR UPLATCH SWITCH. OPS CHECKED GOOD IAW DC8 SMM. 2 L 7 4 4F 4A25 1998110600024 19981106 00024 NM 1998 11 6 DHL98715004 1 19981029 A 3010 DUCT BOEING 727 727155C 138404Z NM NR 7 LE SLAT BROKEN A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 715DH 19618 NR 7 SLAT DID NOT RETRACT WITH FLAPS SELECTED TO UP. ABNORMAL ROLL INDICATION. FOUND WING ANTI-ICING TELESCOPING DUCT ON NR 7 SLAT BROKEN AND HANGING OUT. REMOVED DUCT AND INSTALLED BLANKING PLATES PER MEL. CLOSED ANTI-ICING SHUTOFF VAL VES IN STUB WINGS. 2 L 7 3 4F A3WE 1998110600025 19981106 00025 NM 1998 11 6 DHL98724003 1 19981028 A 2424 939D1502 GCU 90252435 BOEING 727 727228 NM NR 1 & NR 3 FAILED A DHLA A UNSCHED LANDING H J G ELECT. POWER LOSS-50 PC WARNING INDICATION MULTIPLE FAILURE CL CLIMB 1 SO 01 724DH MM2347M 19862 NR 3 GEN TRIPPED OFF LINE, RESET, TRIPPED AGAIN. NR 1 GEN ALSO TRIPPED OFF, WAS ABLE TO RESET AGAIN ON GROUND. MOMENTA RILY LOST ALL FUEL GAUGES, EACH GAUGE WENT BLANK ON S/O PANEL. REPLACED NR 1 AND NR 3 VRGC AND NR 1 AND NR 3 GCUS AND BUSS PROTECTION PANEL. GROUND RAN FOR 15 MIN CHECKED ALL SYSTEMS. OPS CHECKED NORMAL. 2 L 7 3 4F A3WE 1998110600026 19981106 00026 NM 1998 11 6 VNAA9810021 1 19981024 A 3260 OL3092 BULB DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FAILED A VNAA O OTHER P NO WARNING INDICATION AP APPROACH 1 GL 07 432JS 3045 WHEN LANDING GEAR WAS SELECTED DOWN DURING THE APPROACH INTO PIT, THE LEFT HAND MAIN LANDING GEAR GREEN LAMP FAILED TO I LLUMINATE. THE CREW BEGAN PROCEDURE TO REPLACE THE INOPERATIVE LAMP. WHEN THE INOPERATIVE LAMP WAS TOUCHED DURING THE REPLACMENT PROCEDURE, IT BEGAN TO ILLUMINATE. THE CREW SECURED THE INDICATOR AND LANDED NORMALLY. MAINTENANCE INSPECTE D AND REPLACED, THE INTERMITTENT LEFT MAIN GEAR GREEN INDICATOR LIGHT BULB, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUA L 31-14-00. OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998110600027 19981106 00027 NM 1998 11 6 AALA981834 1 19980930 A 5713 STRINGER DOUG MD11 MD11 3023602 NM WS 683-693 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1761R 48551 TUL - DURING C-CHECK, FOUND STRINGER NR 11 CRACKED ON OUTBOARD END INSIDE RIGHT WING AT STATION XORS 683-693. REMOVED C RACKED STRINGER SECTION AND INSTALLED SPLICE DOUBLERS AND NEW STRINGER SECTION PER SRM 57-20-00-00-0. (M) 2 L 7 3 4F RT A22WE 1998110600028 19981106 00028 NM 1998 11 6 AALA981838 1 19981001 A 5711 SPAR DOUG MD11 MD11 3023602 NM WS 781-828 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1761R 48551 TUL - DURING C-CHECK, FOUND CORROSION ON REAR SPAR UPPER CAP AFT TANG BETWEEN RIGHT WING STATION XORS 781-828. REMOVED CORROSION AND REPAIRED PER SRM 51-21-01 AND ESO 41000 DATED 10-1-98. (M) 2 L 7 3 4F RT A22WE 1998110600029 19981106 00029 EU 1998 11 6 AALA981713 1 19980921 A 5320 ANGLE AIRBUS 300 A300B4605R 3930308 EU BS 2612 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 80052 460 TUL - EFO252X CALLS FOR INSPECTION OF RT FUSE WING ROOT PICKUP ANGLE FOR CRACKS. A .75 INCH CRACK RADIATING OUT OF FAST ENER TO THE OUTBOARD EDGE OF THE FITTING WAS FOUND. REMOVED PICKUP ANGLE, HFEC ACCOMPLISHED. NO CRACKS FOUND, INSTALLE D NEW ANGLE PER ECO EO794. (M) 2 L 7 2 4F RT A35EU 1998110600030 19981106 00030 EU 1998 11 6 AALA981723 1 19980924 A 5730 SKIN AIRBUS 300 A300B4605R 3930308 EU RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14053 420 TUL - FOUND RIGHT WING LOWER SURFACE AFT AND OUTBOARD OF NR 2 ENGINE PYLON HAS CORROSION TWO AREAS. REMOVED CORROSION, INSTALLED INTERAL DOUBLER REPAIR PER ESO 30595, DATED 9-24-98. (M) 2 L 7 2 4F RT A35EU 1998110600031 19981106 00031 WP 1998 11 6 AALA981853 1 19981002 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 160 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 432AA 49350 TUL - LONGERON CRACKED IN BOTH HAT SECTIONS AT FS 160. REPAIRED IAW SRM 53-02, FIG 18. (M) 2 L 7 2 4F A6WE 1998110600032 19981106 00032 WP 1998 11 6 AALA981709 1 19980916 A 5347 TRACK DOUG DC9 DC983 3022083 WP BS 1212-1322 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 590AA 53253 TUL - FOUND CORROSION IN RT TIE DOWN TRACK AT FASTENERS THAT ATTACH TRACK TO FRAMES. REPLACED TIE DOWN TRACK. (M) 2 L 7 2 4F RT A6WE 1998110600033 19981106 00033 WP 1998 11 6 AALA981708 1 19980917 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 598-712 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 590AA 53253 TUL - FOUND CUSP SECTION FROM RT STATION 598 TO STATION 712 RT, REQUIRES REPLACEMENT DUE TO SEVERAL AREAS OF CORROSION T HAT WENT BEYOND LIMITS. REPLACED CUSP SECTION FROM STATION 598 TO STATION 712 PER AARD 53-20-00-16. (M) 2 L 7 2 4F RT A6WE 1998110600034 19981106 00034 WP 1998 11 6 AALA981826 1 19980929 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 1155-1161 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7547A 53029 TUL - FOUND CORROSION ON CUSP STATION 1155 TO 1161 ABOVE CARGO DOOR CUTOUT. INSTALLED DOUBLER PER AARD 53-00-00 AND CUT OUT DAMAGED AREA. (M) 2 L 7 2 4F A6WE 1998110600035 19981106 00035 WP 1998 11 6 AALA981895 1 19981008 A 2530 2510000405 OVEN DOUG DC9 DC982 3022082 WP GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 225AA BBCZLSM 49175 DFW - FLT 1356 - EN ROUTE DFW - CREW AND PASSENGERS NOTED BURNING SMELL AND SMOKE. NO SOURCE COULD BE DETECTED BY CREW. RETURNED DFW AND LANDED WITHOUT INCIDENT. FOUND FIRST CLASS GALLEY OVEN TO BE CAUSE OF REPORTED SMELL IN CABIN. REPL ACED FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600036 19981106 00036 1998 11 6 AALA981833 4 19980709 A 2565 D31021107 SLIDE AIRCRUISERS AIRBUS 300 A300B4605R 3930308 EU CABIN FAILED A A AALA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. A FLAME/FIRE CL CLIMB 1 SW 07 80057 03484 465 SJU - FLT 574 - AFTER TAKEOFF SJU EN ROUTE TO MIA, THE NR 1 ENGINE EXPERIENCED A FIRE. CREW DECLARED AN EMERGENCY AND S HUT ENGINE DOWN. AIRCRAFT AIR INTERRUPTED BACK TO SJU AND LANDED WITHOUT FURTHER INCIDENT. AFTER AIRCRAFT CAME TO A ST OP AN EMERGENCY EGRESS WAS EXECUTED. THE 3R DOOR SLIDE FAILED TO FUNCTION NORMALLY AND DID NOT SUCCESSFULLY DEPLOY. A LL PASSENGERS AND CREW MEMBERS SUCCESSFULLY USED ALTERNATE AREAS TO EXIT THE AIRCRAFT. AFTER NTSB INVESTIGATION THE 3R DOOR SLIDE WAS REPLACED. DOOR AND SLIDE WAS CHECKED FOR NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998110600037 19981106 00037 NM 1998 11 6 F3LA98168 1 19981025 A 5320 ANGLE BOEING 737 7373M8 1384615 NM BS 800 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION, REPORTED AFT CARGO PIT ANGLE CRACKED AT BS 800, ABOVE STRINGER 25-R. MAINTENANCE REMOV ED DAMAGED AREA, FABRICATED REPLACEMENT ANGLE PER DRAWING NR 69-43477, INSTALLED PER SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1998110600038 19981106 00038 NM 1998 11 6 F3LA98169 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 312 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION, REPORTED CORROSION ON FLOORBEAM AT BS 312, LBL 30 TO LBL 5. MAINTENANCE REMOVED DAMAGE D AREAS, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-51, SRM 51-40-2 AND SRM 53-10-5. (M) 2 L 7 2 4F RT A16WE 1998110600039 19981106 00039 NM 1998 11 6 F3LA98170 1 19981025 A 5320 ANGLE BOEING 737 7373M8 1384615 NM BS 727-807 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORRODED FASTENERS HOLES AT AFT CARGO PIT LEFT SIDE WALL TO FLOORBOARD ATTACH A NGLE FROM BS 727B TO 807. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-60-53, SRM 51-40-2, SRM 51-10-3 AND SRM 51-30-2. (M) 2 L 7 2 4F RT A16WE 1998110600040 19981106 00040 NM 1998 11 6 F3LA98167 1 19981011 A 2761 ACTUATOR BOEING 737 737201 1384454 NM SPOILER FAILED A F3LA O OTHER J WARNING INDICATION LD LANDING 1 NM 03 207AU 19423 DEN - UPON ARRIVAL, FLT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE DURING LANDING. MAINTENANCE REPLACED NR 5 G ROUND SPOILER OUTBOARD ACTUATOR, SERVICED HYDRAULIC SYSTEM. PERFORMED LEAK CHECK AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1998110600041 19981106 00041 NM 1998 11 6 MASA98184 1 19981005 A 2731 TRIM DHAV DHC8 DHC8202 2809007 NM ELEVATOR MALFUNCTIONED A MASA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 SW 07 436YV 436 FLT 5254 - DRO-PHX - AFTER DEPARTURE, CREW REPORTED UNABLE TO TRIM THE ELEVATOR AFTER REACHING FLIGHT ALTITUDE. THE CRE W ELECTED TO RETURN TO DRO, AND EMERGENCY EQUIPMENT WAS REQUESTED BY THE CAPTAIN. ATC DECLARED AN EMERGENCY. AIRCRAFT LANDED IN DRO WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE SYSTEM COMPONENTS, NO DEFECTS WERE NOTED. MAINTENANC E PERFORMED IN OPERATIONAL SYSTEM CHECK, BUT COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998110600042 19981106 00042 NM 1998 11 6 EISA98242 1 19981001 A 5270 SENSOR BOEING 727 727277 138408S NM CARGO DOOR MALFUNCTIONED A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 275WC 20549 CAUTION LIGHT ILLUMINATED ON F/E PANEL FOR MAIN CARGO DOOR DURING FLIGHT. AIR TURN BACK TO BSL. INSPECTED CARGO DOOR P ER PEMCO MM 52-32-23. FOUND ALL OPS INDICATORS NORMAL. (M) 2 L 7 3 4F RT A3WE 1998110600043 19981106 00043 NM 1998 11 6 EISA98240 1 19980920 A 7500 LINE BOEING 727 727223 1384074 NM MLG WW OUT OF POSITION A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6839 20192 NR 3 STRUT OVERHEAT LIGHT ILLUMINATED AFTER APPLYING CLIMB POWER. AIR TURNBACK TO CPH. GENERATED BY PILOT REPORT. REP OSITIONED BLEED AIR SHUT-OFF LINE. OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998110600044 19981106 00044 WP 1998 11 6 ORJA98194 1 19980727 A 2613 DETECTOR DOUG DC9 DC982 3022082 WP TAIL COMP MALFUNCTIONED A ORJA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 11 822RA 49932 RETURN TO RENO, TAIL COMPT TEMP HI LIGHT CAME ON FOR 2 MINUTES AFTER TAKEOFF. OPERATING WITH LEFT THROTTLE RETARDED FOR 2 MINUTES, LIGHT WENT OUT. RESTORED THROTTLE AND TURNED LT PACK OFF. LIGHT CAME ON, THEN WENT OUT. PERFORMED MAINTEN ANCE ENGINE RUN PER MM 36-10-00, MODE 1, WITH LT PACK DISCONNECT FOR 5 MINUTES. RECONNECTED LT PACK, RAN FOR 5 MINUTES AT HIGH POWER. DID NOT GET LIGHT AT ANYTIME. SUSPECT WHEN PILOT WANTED GROUND START CART HOOKED UP TO AUGMENT APU AIR TO COOL A/C THAT IT OVERTEMPED TAIL COMPARTMENT. (M) 2 L 7 2 4F A6WE 1998110600045 19981106 00045 WP 1998 11 6 AALA981825 1 19980928 A 3350 0200333001 SIGN DOUG DC9 DC982 3022082 WP TAIL CONE INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 440AA 49549 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT SIGN AT TAIL CONE EMERGENCY HANDLE INOPERATIVE. REPLACED EMERGENCY E XIT LIGHT SIGN AT TAIL CONE EMERGENCY HANDLE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600046 19981106 00046 WP 1998 11 6 AALA981824 1 19980929 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE S AFFECT SYSTEMS IN INSP/MAINT 1 SW 07 568AA 49349 DFW - EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT SECTION COACH INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STR IP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998110600047 19981106 00047 NM 1998 11 6 AALA981848 1 19981005 A 3350 0201922001 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385AM 27059 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT 11H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AT 11H. SYS TEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998110600048 19981106 00048 NM 1998 11 6 AALA981829 1 19980929 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 618AA 24526 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY SEAT MOUNTED EXIT PATH LIGHTING SYSTEM AT SEAT 19D INOPERATIVE. REPLACED EMERGENCY SEAT MOUNTED EXIT PATH LIGHT ASSEMBLY AT SEAT 19D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998110600049 19981106 00049 NM 1998 11 6 AALA981830 1 19980929 A 3350 1000679 LIGHT BOEING 767 767323 1385205 NM COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351AA 24032 DFW - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT IN COCKPIT. SYSTEM G ROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998110600050 19981106 00050 NM 1998 11 6 AALA981718 1 19980923 A 3350 SIGN BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 698AN 26980 DFW - DURING OVERNIGHT CHECK, RIGHT AFT OVERWING EMERGENCY EXIT MARKER INOPERATIVE. SECURED RIGHT AFT OVERWING EMERGENC Y EXIT MARKER CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998110600051 19981106 00051 NM 1998 11 6 AALA981855 1 19981006 A 3350 LIGHT BOEING 767 767323 1385205 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 377AN 25446 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 7H INOPERATIVE. SECURED EMERGENCY EXIT SEAT LIGHT CONN ECTOR AT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998110600052 19981106 00052 NM 1998 11 6 AALA981894 1 19981007 A 3350 1013271 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661AA 25295 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER DOOR AT 17D INOPERATIVE. REPLACED SIDEWALL LIGHT ASSEMBLY . SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998110600053 19981106 00053 WP 1998 11 6 AALA981851 1 19981006 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70524 49916 DTW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AFT OF FIRST CLASS GALLEY INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600054 19981106 00054 SO 1998 11 6 98ZZZM803 1 19981007 A 3250 1159SCL200031 STEERING UNIT GULSTM G1159 G1159A 3970109 SO NLG MALFUNCTIONED A KKYA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 NE 03 165G 414 WHILE TAXIING FOR DEPARTURE FROM OXC TO LGA, THE PIC COMMANDED A HARD RIGHT TURN. WHEN HE TRIED TO STRAIGHTEN OUT THE A IRCRAFT, THE NOSE WHEEL STEERING FELT STIFF AND WOULD NOT RESPOND. THE AIRCRAFT WAS RETURNED TO MAINTENANCE. THE NOSE WHEEL STEERING UNIT WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A12EA 1998110600055 19981106 00055 NE 1998 11 6 WRLA98095 2 19981002 A 7200 ENGINE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 2 ENGINE MALFUNCTIONED A WRLA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 27 117WA 48318 517238 DURING INITIAL CLIMB OUT, 800 FT AGL, NR 2 ENGINE BEGAN SURGING. FLT CREW RETARDED THROTTLE FROM 95 PERCENT N1 TO FLIGH T IDLE. SURGING DISCONTINUED. UPON REACHING ASSIGNED ALTITUDE, FLIGHT CREW ADVANCED THROTTLE TO 75 PERCENT N1, AND SUR GING RETURNED. THROTTLE REDUCED TO FLT IDLE. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE POINT FOR MX. NR 2 ENG WAS LE FT AT FLT IDLE, AND AIRCRAFT RETURNED TO DEPARTURE POINT, LANDING WITHOUT FURTHER INCIDENT. MX PERSONNEL INSPECTED ENG EXTERIOR WITH NO EVIDENCE OF DAMAGE. PERFORMED BORESCOPE WITH NO EVIDENCE OF DAMAGE. ENGINE TREND MONITORING INDICATED THAT N2 WAS BELOW TARGET. RERIGGED THE VARIABLE STATOR VANE SYSTEM AND PERFORMED GROUND RUNS. 2 L 7 3 4F 4 F A22WE E23EA 1998110600056 19981106 00056 NM 1998 11 6 USAABB98095 1 19980903 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 604AU 22199 LAX - FOUND L4 DOOR EMERGENCY EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE LGIHT ASSEMBLY. (M) 2 L 7 2 4F RT A2NM 1998110600057 19981106 00057 NM 1998 11 6 USAABB98096 1 19980903 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 628AU 27806 LAX - FOUND FLOOR LEVEL EMERGENCY LIGHT AT SEAT ROW 23 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M) 2 L 7 2 4F RT A2NM 1998110600058 19981106 00058 NM 1998 11 6 USAABB98098 1 19980913 A 3350 873100151REV9 LIGHT BOEING 757 7572B7 1384964 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 629AU 27807 LAX - FOUND EMERGENCY FLOOR LIGHT INOPERATIVE AT ROW 13. REPLACED LIGHT ASSEMBLY AT ROW 13. (M) 2 L 7 2 4F RT A2NM 1998110600059 19981106 00059 NM 1998 11 6 USAA980392 1 19980909 A 5330 654577467 SKIN BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 40428 22956 CLT - DURING RON VISUAL INSPECTION, FOUND A 2 INCH CRACK ON STRINGER 24L FROM 2-5 INCH FORWARD OF STATION 727E ON SKIN. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 1998110600060 19981106 00060 NM 1998 11 6 USAA980381 1 19980821 A 5330 SKIN BOEING 737 737301 1384611 NM BS 379 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 346US 33324 23515 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK IN SKIN E/E DUCT COOLING OUTLET STATION 379 LBL 30. I NSTALLED DOUBLER OF .100 INCH 2024-T3 PER EA 62079 AND BOEING SB 737-53-1117. (M) 2 L 7 2 4F RT A16WE 1998110600061 19981106 00061 NM 1998 11 6 USAASB98233 1 19980906 A 2931 ST107R TRANSMITTER BOEING 737 737301 1384611 NM HYDRAULIC SYSTEM INOPERATIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 354US 23557 CLT - FLT 1080 - AT FL370, THE 'B' SYSTEM HYDRAULIC PRESSURE GAUGE WENT OT 750 PSI. SHORTLY THEREAFTER, THE 'B' SYSTEM HYDRAULIC QUANTITY RESERVOIR STARTED TO DECREASE. CREW DECIDED TO DIVERT TO CLT DUE TO POSSIBLE HYDRAULIC FLUID LOSS. F LIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE 'B' SYSTEM HYDR AULIC PRESSURE TRANSMITTER AND INDICATOR. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998110600062 19981106 00062 NM 1998 11 6 98ZZZM804 1 19980906 A 3240 SRDL0C7E INDICATOR BOEING 737 737301 1384611 NM COCKPIT INOPERATIVE A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 354US 23557 CLT - FLT 1080 - AT FL370, THE 'B' SYSTEM HYDRAULIC PRESSURE GAUGE WENT TO 750 PSI. SHORTLY THEREAFTER, THE 'B' SYSTEM HYDRAULIC QUANTITY RESERVOIR STARTED TO DECREASE. CREW DECIDED TO DIVERT TO CLT DUE TO POSSIBLE HYDRAULIC FLUID LOSS. F LIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE 'B' SYSTEM HYDR AULIC PRESSURE TRANSMITTER AND INDICATOR. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998110600063 19981106 00063 WP 1998 11 6 USAAD98158 1 19980907 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 939VJ 48120 DTW - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 9 AND 13 WERE DIM. MAINTENANCE REPLACED THE BATTERIES FOR THE CEILING E MERGENCY LIGHTS BETWEEN ROWS 9 AND 13. (M) 2 L 7 2 4F A6WE 1998110600064 19981106 00064 WP 1998 11 6 USAAD98166 1 19980929 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 928VJ 48131 IND - THE COCKPIT EMERGENCY LIGHT WOULD NOT TURN OFF WHEN THE AIRCRAFT POWER WAS REMOVED FROM THE PLANE. MAINTENANCE RE PLACED THE COCKPIT EMERGENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998110600065 19981106 00065 WP 1998 11 6 USAAD98155 1 19980906 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 PHL - THE LOW LEVEL EMERGENCY LIGHT AT ROW 25D STAYED ON WITH THE COCKPIT SWITCH IN THE ARM POSITION. MAINTENANCE REPLA CED THE LOW LEVEL EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998110600066 19981106 00066 WP 1998 11 6 USAAD98168 1 19981001 A 2421 976J2526 GENERATOR DOUG DC9 DC982 3022082 WP LT ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 829US 29189 49429 MCO-PIT - FLT 843 - EN ROUTE THE LEFT ENGINE GENERATOR POWER DROPPED OFF LINE, AND THE APU WAS ON MEL. THE AIRCRAFT DIV ERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE GENERATOR. (M) 2 L 7 2 4F A6WE 1998110600067 19981106 00067 WP 1998 11 6 USAAD98160 1 19980909 A 3350 14597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816US 48096 PHL - THE CEILING EMERGENCY LIGHTS BETWEEN ROWS 17 AND 21 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE CEILING EMERGENCY LIGHTS BETWEEN ROW 17 AND 21. (M) 2 L 7 2 4F A6WE 1998110600068 19981106 00068 WP 1998 11 6 USAAD98159 1 19980907 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 974VJ 47130 PIT - THE EMERGENCY LIGHT MOUNTED ON THE FORWARD ENTRY DOOR WAS DIM. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGE NCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998110600069 19981106 00069 1998 11 6 USAAD98162 4 19980922 A 3421 5223908001 INDICATOR DOUG DC9 DC931 3022065 WP COCKPIT FAILED A USAA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 EA 19 974VJ 37294 47130 PIT - FLT 1572 - AFTER TAKEOFF, THE CAPTAINS FLIGHT DIRECTOR INDICATOR WINGS MOVED TO THE OFF POSITION. THE AIRCRAFT RE TURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 ADI. (M) 2 L 7 2 4F A6WE 1998110600070 19981106 00070 NM 1998 11 6 USAASB98234 1 19980909 A 3350 6013211 POWER SUPPLY BOEING 737 737201 1384454 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 257AU 22799 EWR - MAINTENANCE FOUND THE FORWARD ENTRY DOOR EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY . OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998110600071 19981106 00071 WP 1998 11 6 USAAD98170 1 19980902 A 2170 17946081 WATER SEPARATOR DOUG DC9 DC931 3022065 WP A/C BAY CONTAMINATED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 967VJ 47375 PIT-DTW - FLT 1275 - AFTER TAKEOFF BOTH LAVATORY SMOKE DETECTORS ACTIVATED AND THE FLIGHT ATTENDANTS NOTICED A CHEMICAL SMELL THROUGHOUT THE CABIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH AIR CONDITIONING PACK WATER SEPARATORS. (M) 2 L 7 2 4F A6WE 1998110600072 19981106 00072 WP 1998 11 6 USAAD98169 1 19981002 A 2130 MS252531 SWITCH DOUG DC9 DC931 3022065 WP COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 974VJ 47130 CLT-BNA - FLT 899 - AFTER TAKEOFF, THE CABIN PRESSURE CONTROL FAILED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WIT HOUT INCIDENT. MAINTENANCE REPLACED THE MANUAL, AUTO CONTROL SWITCH IN THE PEDESTAL. (M) 2 L 7 2 4F A6WE 1998110600073 19981106 00073 WP 1998 11 6 USAAD98165 1 19980926 A 5240 SEAL DOUG DC9 DC982 3022082 WP SERVICE DOOR MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 825US 49237 CLT-BDL - FLT 995 - AFTER TAKEOFF, THE AFT LEFT SERVICE DOOR DID NOT SEAL WELL. THE CAPTAIN RECEIVED A FLOW LIGHT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOT SECURED. THE DOOR WAS SECURED A ND CHECKED OK. (M) 2 L 7 2 4F A6WE 1998110600074 19981106 00074 SW 1998 11 6 98ZZZM805 1 19980810 A 3260 MS243314 SWITCH SWRNGN SA227 SA227AC 8780603 SW MLG INOPERATIVE A MEJA D RETURN TO BLOCK O OTHER CR CRUISE 1 SW 17 372PH AC532 DURING A FAA CHECK RID AT SAT, THE LEFT ENGINE WAS SHUT DOWN BUT WOULD NOT RE-START. THE CREW REQUESTED PRIORITY FROM A TC AND MADE A SINGLE ENGINE LANDING AT SAT WITHOUT FURTHER INCIDENT. MX CLEANED THE LEFT OUTBOARD SQUAT SWITCH AND OPER ATIONS CHECK OF AIRCRAFT ON GROUND WAS GOOD. A FUNCTIONAL CHECK FLIGHT WAS CONDUCTED TO VERIFY AIR START PROCEDURES, BU T WAS UNSATISFACTORY SINCE THE LEFT PROPELLER WOULD NOT UNFEATHER IN FLIGHT. MAINTENANCE FOUND THE LEFT OUTBOARD SQUAT WAS DEFECTIVE. THE SWITCH WAS REMOVED AND REPLACED WITH A NEW UNIT AND THE OPS CHECK WAS GOOD. MAINTENANCE ALSO VERIFI ED THE UNFEATHER PUMP PRESSURE WAS 145 PSI, BUT DISCOVERED THAT THE UNFEATHER PUMP SUPPLY LINE WAS LEAKING AT THE PUMP. 2 L 7 2 4T RT A8SW 1998110600075 19981106 00075 SW 1998 11 6 98ZZZM806 1 19980811 A 7714 2719157003 INDICATOR SWRNGN SA227 SA227AC 8780603 SW COCKPIT FAILED A MEJA C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 17 2691W 569A AC655 SJU-POS - DURING WET T/O, THE RT ENG PRODUCED 80 PERCENT TQ AND THE T/O WAS ABORTED. WHEN ENG WAS RAN DRY, IT PRODUCED CHARTED TQ AND THE CAWI SYSTEM WAS DEFERRED. ON THE ENSUING DRY TAKEOFF, THE RT ENG PRODUCED 74 PERCENT TQ AND T/O WAS ABORTED. MX ADJUSTED SCREW 'X', PERFORMED ENG GROUND RUNS, RUNS WERE SATISFACTORY, AND A/C WAS RETURNED TO SERVICE. IN FLT FROM SJU TO POS, DURING CLIMB, THE RT ENG TQ DROPPED TO 98 PERCENT AND STARTED BY-PASSING. THE A/C RETURNED TO SJU AND MX ADJUSTED SCREW 'X', PERFORMED ENG GROUND RUNS, RUNS WERE SATISFACTORY. A FCF WAS FLOWN BUT WAS UNSATISFACTORY. MX DRAINED THE WATER/METHANOL, SERVICED THE SYSTEM WITH A NEW WATER/METHANOL MIXTURE, AND PERFORMED AN OP CHECK 2 L 7 2 4T RT A8SW 1998110600076 19981106 00076 WP 1998 11 6 ARWA981031 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 140 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 140, REMOVED CORROSION SRM 51-1-8. FABRICATED BEAM AN D INSTALLED IAW EO JOSS AIR , CO NR 18R5371013 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5080A. (M) 2 L 7 4 4F 4A25 1998110600077 19981106 00077 WP 1998 11 6 ARWA981030 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 55 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM FLIGHT COMPARTMENT STATION 55, LBL 29 TO LBL 47, CUT OUT OF CORROSION. FABRICATED BE AM UPPER CHORD AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371001, WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 4420. (M) 2 L 7 4 4F 4A25 1998110600078 19981106 00078 WP 1998 11 6 ARWA981029 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 100 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM UPPER AFTER FLANGE MAIN CABIN STATION 100 RBL 34 CUT OUT AREA OF CORROSION FABRICATED ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371016, WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5078A. ( M) 2 L 7 4 4F 4A25 1998110600079 19981106 00079 WP 1998 11 6 ARWA981028 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 55 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM FLIGHT COMPARTMENT STATION 55, RBL 12 TO RBL 29 CUT OUT AREA OF CORROSION. FABRICATE D BEAM UPPER CHORD AND INSTALLED IAW EO JOSS AIR NR 18R5371004, WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 4419. (M) 2 L 7 4 4F 4A25 1998110600080 19981106 00080 WP 1998 11 6 ARWA981027 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 80 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 80. CUT OUT AREA OF CORROSION, FABRICATED ANGLE AND I NSTALLED IAW EO JOSSAIR, CO NR 18R5371002 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5077A. (M) 2 L 7 4 4F 4A25 1998110600081 19981106 00081 WP 1998 11 6 ARWA981026 1 19981020 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 204 CORRODED A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON UPPER SKIN LEFT WING STATION XW 204.125 STRINGER 13 REMOVED CORROSION BEYOND LIMITS. FABRICATE D FILLERS AND DOUBLER AND INSTALLED IAW DOUGLAS ROD SKETCH 98-08-04-008 WORK ACCOMPLISHED UNDER ARROW FORM JW3B CPCP CON TROL 1625. (M) 2 L 7 4 4F 4A25 1998110600082 19981106 00082 WP 1998 11 6 ARWA981025 1 19981020 A 5753 SKIN DOUG DC8 DC863F 302198F WP WS 169-213 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - IMPROPER PATCHES AND CORROSION ON UPPER SKIN LEFT OUTBOARD FLAP STATION XF 213 TO XF 169. REMOVED UPPER SKIN FABR ICATED NEW PANEL SKIN AND REPLACED IAW REPAIR INFORMATION JOSSAIR, CO NR 18R5751031 AND SRM 51-3-0 WORK ACCOMPLISHED UND ER ARROW AIR FORM M3A CONTROL 1649. (M) 2 L 7 4 4F 4A25 1998110600083 19981106 00083 WP 1998 11 6 ARWA981024 1 19981020 A 5320 WEB DOUG DC8 DC863F 302198F WP NLG WW CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON TAPERED DOUBLER NLG W/W RIGHT AT STATION 8, CUT OUT AREA OF CORROSION. FABRICATED FILLERS AND DOUBLER AND INSTALLED IAW EO JOSSAIR, CO NR 18R5361009 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 4318. ( M) 2 L 7 4 4F 4A25 1998110600084 19981106 00084 WP 1998 11 6 ARWA981023 1 19981020 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 178 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - NR 1 CRACK ON LEADING EDGE RIGHT WING STATION XFS 178 PERFORMED STOP DRILL AND FABRICATED DOUBLER AND INSTALLED IA W EO SEMAN NR 1014 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1363. (M) 2 L 7 4 4F 4A25 1998110600085 19981106 00085 WP 1998 11 6 ARWA981022 1 19981020 A 5753 SKIN DOUG DC8 DC863F 302198F WP WS 367 DENTED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - DENTS, DEFORMATION AND CORROSION ON RT OUTBOARD FLAP T/E LOWER SKIN STATION XRS 367 TO XRS 400. REMOVED LOWER SKI N, FABRICATED NEW SKIN REPLACED IAW REPAIR INFORMATION JOSSAIR, CO NR 18R5751030 AND SRM 51-3-0 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1699. (M) 2 L 7 4 4F 4A25 1998110600086 19981106 00086 WP 1998 11 6 ARWA981021 1 19981020 A 5730 SKIN DOUG DC8 DC863F 302198F WP RT WING CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON L/E UPPER SKIN RIGHT WING CUT OUT AREA OF CORROSION FABRICATED DOUBLER AND INSTALLED IAW EO JOS SAIR, CO NR 18R5781019 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 1703. (M) 2 L 7 4 4F 4A25 1998110600088 19981106 00088 WP 1998 11 6 USAAD98183 1 19981014 A 3260 SENSOR DOUG DC9 DC931 3022065 WP NLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 991VJ 47310 GSO-LGA - FLT 990 - UPON GEAR EXTENSION DURING APPROACH, THE GREEN NOSE LANDING GEAR LIGHT DID NOT ILLUMINATE, ALL NOSE GEAR UNSAFE LIGHTS WERE OUT. THE GEAR WAS RECYCLED AND ALL INDICATIONS WERE NORMAL. MAINTENANCE CHECKED THE NOSE GEAR INDICATING SYSTEM, AND PERFORMED A GEAR RETRACTION AND EXTENSION TEST, ALL WAS NORMAL. (M) 2 L 7 2 4F A6WE 1998110600089 19981106 00089 WP 1998 11 6 USAAD98181 1 19981012 A 7933 INDICATOR DOUG DC9 DC931 3022065 WP ENGINE OIL MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 960VJ 47505 PIT-BNA - FLT 1285 - AFTER TAKEOFF THE CAPT NOTICED THE RIGHT ENGINE OIL TEMP WAS IN THE YELLOW ARCH. POWER WAS REDUCED BUT THE TEMPERATURE CONTINUED TO CLIMB THROUGH THE RED ARCH AND OF SCALE. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT RE TURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THERE WAS 20 MINUTES SINGLE ENGINE TIME. MAINTENANCE FOUND WIRES E355 A18N AND E355B18N LOOSE AT THE GROUND S TUD. THE WIRES WERE TIGHTENED AND ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998110600090 19981106 00090 EU 1998 11 6 VTZA98292 1 19980913 A 2460 M5001383 RELAY BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 479UE 893 FLT 6283 - IAD-HPN - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO ELECTRICAL BURNING SMELL IN CABIN. AIRC RAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT ANCINARY BUS BAR RELA Y. MAINTENANCE GROUND RAN AIRCRAFT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998110600091 19981106 00091 EU 1998 11 6 VTZA98291 1 19980911 A 5210 RNF10034 HOSE JETAIR JETSTM JETSTM4101 1500501 EU PAX DOOR PINCHED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 326UE 41064 FLT 6627 - IAD-ORH - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NO PSI IN AUTO OR MANUAL MODE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPOSITIONED PASSENGER DOOR SEAL INFLATION HOSE. O PS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998110600092 19981106 00092 WP 1998 11 6 VTZA98290 2 19980909 A 7200 310338024 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT NACELLE MALFUNCTIONED A VTZA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 495UE 818 P66213 FLT 6480 - GSO-IAD - DURING CRUISE, AIRCRAFT DIVERTED TO RDU DUE TO RIGHT ENGINE LOW OIL PRESSURE. CREW SHUTDOWN RIGHT ENGINE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND IS IN THE PROCESS OF CHANGING THE RT ENGINE. MAINTENANCE COMPLETED THE REMOVAL AND REPLACEMENT OF RT ENGINE ON 9-11-98. MAINTENANCE GROUND RAN AIRCRAFT. O PS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998110600093 19981106 00093 NM 1998 11 6 WRLA98096 1 19981103 A 3246 4306001100 HUBCAP DOUG MD11 MD11 3023602 NM MLG WHEEL DAMAGED A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 271WA 48518 DURING TAKEOFF ROLL OF FLIGHT NR WO-826, FLIGHT CREW RECEIVED A 'TIRE FAILURE' INDICATION ON SYSTEMS DISPLAY. FLIGHT CR EW ELECTED TO DISCONTINUE TAKEOFF (MAX SPEED ATTAINED 90 KNOTS). TAKEOFF WAS DISCONTINUED, AND AIRCRAFT RETURNED TO GAT E WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL INSPECTED AND FOUND NR 9 WHEEL (CENTER LANDING GEAR) HAD BROKEN HUBCA P AND DAMAGED WHEEL SPEED AND TIRE PRESSURE TRANSDUCERS. SUSPECT THAT DRIVE FORK ON HUBCAP BECAME DISLODGED, DAMAGING A SSOCIATED COMPONENTS. REPLACEMENT PARTS WERE NOT AVAILABLE ON SITE. TIRE PRESSURE AND TEMPERATURE SYSTEMS WERE DEFERRE D PER MEL. A REPLACEMENT HUBCAP WAS INSTALLED. AFTER 170 MINUTE DELAY, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A22WE 1998110600094 19981106 00094 EU 1998 11 6 VTZA98282 1 19980904 A 2910 1379007D441 LINE BAG JETSTM JETSTM3201 1500217 EU LT WING CHAFFED A VTZA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 27 482UE 897 FLT 6548 - CLE-IAD - DURING LANDING, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS ALL HYDRAULIC PRES SURE DROPPED TO ZERO. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES IN LEFT LEADING EDGE OF WING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998110600095 19981106 00095 EU 1998 11 6 98ZZZM807 1 19980904 A 2910 1379007D499 LINE BAG JETSTM JETSTM3201 1500217 EU LT WING CHAFFED A VTZA O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 EA 27 482UE 897 FLT 6548 - CLE-IAD - DURING LANDING, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS ALL HYDRAULIC PRES SURE DROPPED TO ZERO. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES IN LEFT LEADING EDGE OF WING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998110600096 19981106 00096 1998 11 6 VTZA98297 4 19980921 A 3442 7007700301 WX RADAR JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING L NO TEST CR CRUISE 1 EA 27 316UE 41055 FLT 6289 - IAD-CMH - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO WEATHER RADAR FAILED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WEATHER RADAR SCREEN, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998110600097 19981106 00097 EU 1998 11 6 VTZA98281 1 19980904 A 2750 TY175603B CONTROL UNIT JETAIR JETSTM JETSTM4101 1500501 EU TE FLAP MALFUNCTIONED A A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 305UE 41019 FLT 6522 - IAD-RIC - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO FLAPS WOULD NOT RETRACT. AIRCRAFT RETURN ED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET EMERGENCY SELECT BUTTON ON CONTROL UNIT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998110600098 19981106 00098 EU 1998 11 6 VTZA98289 1 19980908 A 2913 PV3004426 PUMP JETAIR JETSTM JETSTM4101 1500501 EU HYDRAULIC SYSTEM FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 326UE 41064 FLT 6572 - IAD-SCE - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOSS OF ALL HYDRAULIC PRESSURE. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PUMP, OPS CHECK O K. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998110600099 19981106 00099 NM 1998 11 6 TWAA9817501 1 19981028 A 3397 58541 WIRE BOEING 757 757231 1384950 NM CABIN DAMAGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 715TW 28483 THE FORWARD CABIN 26 INCH LONG EGRESS LIGHT STRIP WAS FOUND INOPERATIVE WHILE ON THE GROUND. THE STRIP HAD TORN LOOSE. STL SECURED THE LIGHT STRIP AND DEFERRED CORRECTIONS TO THE LIGHT MALFUNCTION PER MEL. ON LAYOVER THE COVER, MFG 5778-1 , AND CABLE WERE REPLACED. -----CLOSED---- 2 L 7 2 4F RT A2NM 1998110600100 19981106 00100 NM 1998 11 6 VJ9800572 1 19981029 A 2560 412SA MEGAPHONE BOEING 737 7372L9 1384497 NM CABIN INOP A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 FORWARD MEGAPHONE INOP. REPLACED MEGAPHONE IAW MM 25-69-0. 2 L 7 2 4F RT A16WE 1998110600101 19981106 00101 WP 1998 11 6 VJ9800573 1 19980915 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FLOOR PANEL LOCATED BETWEEN #3 GALLEY AND FORWARD FLIGHT ATTENDAANT SEAT, FS 200.0, CORRODED. REMOVED CORROSION, FABRIC ATED AAND INSTALLED REPAIR FLOOR PANEL IAW DC9 SRM 51-10-3, 53-21-0, AND 51-30-1. 2 L 7 2 4F A6WE 1998110600102 19981106 00102 WP 1998 11 6 CALA9801984 1 19981021 A 3260 7000010101 SWITCH DOUG DC9 DC932 3022066 WP LT MLG DOOR INOP A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 33506 47765 THE GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR WAS EXTENDED FOR LANDING AT IAH. THE L/H AND R/H MLG DOORS WERE DAMAGED ON LANDING. MAINTENANCE REMOVED AND REPLACED THE L/H MLG DOOR SWITCH. BOTH L/H AND R/H MLG DOORS WERE REMOVED A ND REPLACED IAW MM 32-12-01. INDICATION AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998110600103 19981106 00103 NM 1998 11 6 CALA9801985 1 19981023 A 3231 273N404122 ACTUATOR BOEING 757 757224 1384958 NM LT MLG DOOR INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 09 14120 27562 A GEAR DISAGREE LIGHT ILLUMINATED AFTER GEAR RETRACTION LEAVING EWR. ALTERNATE GEAR EXTENSION WAS PERFORMED AND THREE GR EEN WERE INDICATED. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE L/H MLG DOO R LOCK RELEASE ACTUATOR AT FAULT. THE LOCK RELEASE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-35-06. A GEAR SWING WAS P ERFORMED AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A2NM 1998110600104 19981106 00104 WP 1998 11 6 CALA9801986 1 19981027 A 3350 EMBS1392 CHARGER ENGMAGNETICS DOUG DC10 DC1030 3023501 WP CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14075 46922 THE EMERGENCY LIGHTS WOULD NOT TEST ON PREDEPARTURE CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK AND CHA RGER AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 3 4F A22WE 1998110600105 19981106 00105 1998 11 6 CALA9801987 4 19981027 A 2565 100502119 SLIDE PICO DOUG DC9 DC982 3022082 WP AFT SERV DOOR FAILED A CALA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 16804 25749 49246 THE AFT GALLEY SERVICE DOOR SLIDE WAS INADVERTENTLY PULLED, BUT DID NOT DEPLOY. INSPECTION BY MAINTENANCE FOUND THE AFT GALLEY SERVICE DOOR SLIDE LANYARD PULLED AND PRESSURE AT ZERO. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-62-0. 2 L 7 2 4F A6WE 1998110600106 19981106 00106 NM 1998 11 6 CALA9801988 1 19981024 A 2612 FIRE WARNING BOEING 737 7373T0 1384582 NM APU ACTIVATED A CALA O OTHER N FALSE WARNING DE DESCENT 1 SW 09 14337 23575 WHEN THE APU WAS STARTED ON DESCENT INTO SAT, THE APU FIRE WARNING LIGHT AND BELL ACTIVATED. THERE WERE NO LIGHTS IN APU FIRE HANDLE OR FOR ENGINES AND NO OTHER ABNORMAL INDICATIONS WERE NOTED. THE APU RAN NORMALLY AND THE LIGHT AND BELL WE RE SILENCED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE APU AND FOUND NO FAULTS. A FIRE WARNING TES T WAS PERFORMED IAW MM 26-11-00 AND NO FAULTS WERE NOTED. THE APU WAS RUN FULLY LOADED FOR 20 MINUTES WITH NO TROUBLE FO UND. THE PROBLEM COULD NOT BE DUPLICATED. 2 L 7 2 4F RT A16WE 1998110600107 19981106 00107 NM 1998 11 6 CALA9801989 1 19981023 A 3231 661516623 CABLES BOEING 727 727224 1384076 NM NLG DOORS OUT OF ADJUST A CALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 09 32725 20655 A LOUD EXTERNAL RUMBLE WAS HEARD ACCOMPANIED BY FLASHING GEAR WARNING LIGHTS WHILE CRUISING AT FL 290. THE AIRCRAFT WAS DIVERTED TO BWI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOORS OUT OF RIG. THE NOSE GEAR DOORS WERE ADJUSTED IAW MM 32-22-1. 2 L 7 3 4F A3WE 1998110600108 19981106 00108 NM 1998 11 6 CALA9801990 1 19981029 A 3350 6104789 BATTERY PACK BOEING 737 7372C0 1384488 NM ROW 12 & 20 DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14245 20074 INSPECTION FOUND THE AISLE PATH EMERGENCY LIGHTING STRIP IS INOPERATIVE FORWARD OF ROW 12 AND AFT OF ROW 20. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A16WE 1998110600109 19981106 00109 NM 1998 11 6 CALA9801991 1 19981027 A 3397 WIRE BOEING 727 727232 1384082 NM L2 DOOR LOOSE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND THE L-2 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE IN HARNESS. THE WIRE WAS REPQIRED AND OPERATIONAL CHECKS WERE GOOD IAAW MM 33-60-01, PAGE 201. 2 L 7 3 4F A3WE 1998110600110 19981106 00110 NM 1998 11 6 CALA9801992 1 19981027 A 3350 TERMINAL BOEING 727 727232 1384082 NM L1 DOOR INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND L-1 OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPAIRED TERMINAL AT LIGHT SOCKET ASSEMBLY A ND OPERATIONAL CHECKS WERE GOOD AT MM 33-60-00, PAGE 201. 2 L 7 3 4F A3WE 1998110600111 19981106 00111 NM 1998 11 6 CALA9801993 1 19981027 A 5752 65273623 SKIN BOEING 727 727232 1384082 NM LT AILERON TAB DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND L/H INBOARD AILERON TAB DEBONDED AT UPPER SKIN AND TRAILING EDGE AREA. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-11. 2 L 7 3 4F A3WE 1998110600112 19981106 00112 NM 1998 11 6 CALA9801994 1 19981027 A 5330 SKIN BOEING 727 727232 1384082 NM BS 440 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1 CRACK IN FUSELAGE SKIN AT STA 440 ABOVE STRINGER 25R. THE CRACKED AREA WAS CUT OUT AND A DOUBLER RE PAIR WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3. 2 L 7 3 4F A3WE 1998110600113 19981106 00113 WP 1998 11 6 CALA9801995 1 19981027 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1212-1309 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND L/H INBOARD SEAT TRACK CORRODED AT STA 1212-1309. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW S RM 51-30-1. 2 L 7 2 4F A6WE 1998110600114 19981106 00114 NM 1998 11 6 CALA9801996 1 19981027 A 5320 SIDE WALL BOEING 727 727232 1384082 NM NLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND 1/4 CRACKS IN NLG WHEEL WELL TOP CENTER, TOP RIGHT, AND RIGHT SIDEWALL PANELS. THE CRACKED AREAS WERE R EMOVED AND FILLER AND DOUBLER REPAIRS WERE INSTALLED IAW SRM 51-40-2 AND 51-30-2, PAGE 4. 2 L 7 3 4F A3WE 1998110600115 19981106 00115 NM 1998 11 6 CALA9801997 1 19981027 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 656.5 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 7/16 CRACK AT R/H WING AFT VENT BOX STRINGER AFT MOUNT LEG, WS 656.50. THE CRACK WAS STOP DRILLED AND REPAIR ANGLES WERE INSTALLED IAW SRM 51-10-2, EA 5762-01050, AND MM 28-20-00. 2 L 7 3 4F A3WE 1998110600116 19981106 00116 NM 1998 11 6 CALA9801998 1 19981027 A 5542 SKIN BOEING 727 727232 1384082 NM RUDDER DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND L/H UPPER RUDDER SKIN DENTED FOUR INCHES FROM LEADING EDGE AND APPROXIMATELY TWENTY INCHES DOWN FROM RU DDER ACTUATOR PANEL. THE CRACKED AREA WAS CUT OUT IAW SRM 55-20-3, FIGURE 1. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, FI GURE 1 AND 51-10-2. 2 L 7 3 4F A3WE 1998110600117 19981106 00117 NM 1998 11 6 CALA9801999 1 19981027 A 5730 SKIN BOEING 727 727232 1384082 NM RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 3/16 CRACK IN R/H WING UPPER TRAILING EDGE OUTBOARD HINGE CUTOUT AT #11 SPOILER HINGE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 57-30-1, AND 57-30-4, PAGE 29. 2 L 7 3 4F A3WE 1998110600118 19981106 00118 NM 1998 11 6 CALA9802000 1 19981027 A 5720 ANGLE BOEING 727 727232 1384082 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND LOWER LEADING EDGE TO RIB SUPPORT ANGLE CRACKED AROUND EIGHT BOLT HEADS INSIDE L/H WING LEADING EDGE AT OUTBOARD SIDE OF RIB, FSS 121. THE RIB SUPPORT ANGLE WAS REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-2, PAGE 2, 51-10-1, AND 51-10-2, PAGE 1. 2 L 7 3 4F A3WE 1998110600119 19981106 00119 NM 1998 11 6 CALA9802001 1 19981027 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE FOREFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 5/16 CRACK IN L/H WING OUTBOARD FOREFLAP LEADING EDGE ABOVE #1 SEQUENCE CARRIAGE AREA. A REPAIR WAS I NSTALLED IAW SRM 57-50-4, PAGES 16 AND 17, FIGURE 7. 2 L 7 3 4F A3WE 1998110600120 19981106 00120 WP 1998 11 6 CALA9802002 1 19981023 A 5320 INTERCOSTAL DOUG DC9 DC982 3022082 WP BS 474 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND A 2.5 CRACK IN INTERCOSTAL AT #1 VHF ANTENNA, STA 474. A NEW INTERCOSTAL WAS INSTALLED IAW EA 5330-0182 3. 2 L 7 2 4F A6WE 1998110600121 19981106 00121 WP 1998 11 6 CALA9802003 1 19981023 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 221 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND L/H INBOARD SEAT TRACK CORRODED AT STA 221. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SE CTION WAS INSTALLED IAW SRM 53-05, FIGURE 4. 2 L 7 2 4F A6WE 1998110600122 19981106 00122 WP 1998 11 6 CALA9802004 1 19981027 A 2560 S168MA MEGAPHONE DOUG DC9 DC932 3022066 WP CABIN INOP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14534 47110 INSPECTION FOUND FORWARD MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REPLACED. 2 L 7 2 4F A6WE 1998110600123 19981106 00123 WP 1998 11 6 9810319311 1 19981027 A 3230 LINK DOUG DC9 DC982 3022082 WP RT MLG BROKEN A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 314RC 49110 AFTER TAKEOFF, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT, RIGHT MAIN GEAR DOOR OPEN LIGHT, AND AUTO SPOILER DO NOT USE LI GHT ALL REMAINED ILLUMINATED. THE FLIGHT CREW CYCLED THE LANDING GEAR, RETURNED TO MSP, AND LANDED WITHOUT INCIDENT. MAI NTENANCE REPLACED A BROKEN LINK ON THE RETRACT ACTUATOR OF THE RIGHT MAIN LANDING GEAR. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998110600124 19981106 00124 NM 1998 11 6 P5CA9801575 1 19981029 A 5400 ANGLE BOEING 747 747122 1384872 NM NR 4 PYLON CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 #4 PYLON AFT BULKHEAD FWD SIDE HAS AN ANGLE STOP DRILLED AND CRACK APPEARS TO BE GOING BEYOND STOP DRILL. REPAIRED PER S RM 51-14-01 AND 51-30-02. 2 L 7 4 4F A20WE 1998110600125 19981106 00125 NM 1998 11 6 P5CA9801576 1 19981028 A 5753 CANOE BOEING 747 747122 1384872 NM NR 7 FLAP TRACK DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 #7 FLAP TRACK CANOE HAS U SHAPED HOLE. REPAIRED DAMAGED AREA PER SRM 51-40-15. 2 L 7 4 4F A20WE 1998110600126 19981106 00126 NM 1998 11 6 P5CA9801577 1 19981028 A 5330 PANEL BOEING 747 747122 1384872 NM FUSELAGE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 PANEL # 334GB HAS SMALL DELAMINATION. FABRICATED AND BONDED NEW SKINS IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1998110600127 19981106 00127 NM 1998 11 6 P5CA9801578 1 19981028 A 5542 SKIN BOEING 747 747122 1384872 NM RUDDER GOUGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 RUDDER LOWER LEFT GOUGE IN SKIN MID POINT. REMOVED DAMAGED SKIN AND REPAIRED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998110600128 19981106 00128 NM 1998 11 6 P5CA9801579 1 19980923 A 3350 CONNECTOR BOEING 747 747132 1384882 NM COCKPIT LOOSE A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 856FT 19897 EMERGENCY LIGHTING DOES NOT WORK. CLEANED AND RESEATED CANNON PLUG ON EMERGENCY PANEL SYSTEM. OPS NORMAL PER MM 33-51-00 . 2 L 7 4 4F A20WE 1998110600129 19981106 00129 EU 1998 11 6 QXEA9801537 1 19981028 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 GEG - SECOND FORWARD FACING OVERHEAD EMERGENCY EXIT SIGN HAS ALL 28 VOLT BULBS BURNT OUT. MAINTENANCE RELAMPED, OPERATIO NAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998110600130 19981106 00130 EU 1998 11 6 QXEA9801538 1 19981028 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 475AU 11222 GEG - FORWARD EXIT SIGN HAS SEVERAL 28 VOLT BULBS OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998110600131 19981106 00131 EU 1998 11 6 QXEA9801539 1 19981028 A 3350 406 LIGHT GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 475AU 11222 GEG - EMERGENCY EXIT LIGHT AT ROW 8 IN OUT. MAINTENANCE REPLACED LIGHT ASSEMBLY, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998110600132 19981106 00132 EU 1998 11 6 QXEA9801540 1 19981027 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT DOOR INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 479AU 11228 GEG - EMERGENCY EXIT SIGN AT COCKPIT DOOR INOPERATIVE. MAINTENANCE REPLACED EMERGENCY EXIT SIGN, OPERATIONAL TEST NORMAL . 2 L 7 2 4F RT A20EU 1998110600133 19981106 00133 EU 1998 11 6 QXEA9801541 1 19981027 A 3350 6008905 BATTERY GRIMES FOKKER F28 F28MK4000 4990810 EU UNDERWING DISCHARGED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 488US 982 11240 PDX - BOTH AFT UNDERWING EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED BATTERY POWER SUPPLY, OPERATIONAL TEST N ORMAL. 2 L 7 2 4F RT A20EU 1998110600134 19981106 00134 NM 1998 11 6 98FDEA00682 1 19981028 A 2170 COALESCER BAG BOEING 727 72725 1384006 NM CABIN CONTAMINATED A FDEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 502FE 18271 98-261 ACRID, RANCID BURN SMELL FROM LH PACK. ISOLATE LH PK & ODOR SUBSIDED. 2 PKS REQ THIS A/C. ODOR BEGAN T/O ROLL. ODOR CEASE F/L 180. RET AT DES USING #1 BLD. R&R WATER SEP BAG, SEALS ON N1 TACH & FRONT ACCY DRIVE SUPPORT ON AML 010 41373. R&R BLD AIR HEAT EXCH, AIR SEP PER MM 36-11-57. OPER CK NORM. OK FOR SERVICE. 2 L 7 3 4F A3WE 1998110600135 19981106 00135 NM 1998 11 6 98FDEA00683 1 19981030 A 3020 132775 DUCT BOEING 727 7272S2F 1384O81 NM NR 3 ENGINE RUPTURED A FDEA O OTHER J WARNING INDICATION UK UNKNOWN 1 SO 25 207FE 22929 98-262 #3 ENG FIRE LIGHT CAME ON, #3 THROTTLE WAS RETARDED TO IDLE LIGHT WENT OUT. FOUND #3 COWL ANTIICE DUCT BROKEN. R&R DUCT RAN ENGINE FOR LEAK CHECK. NO LEAKS NOTED A/C IS OK FOR SERVICE. 2 L 7 3 4F A3WE 1998110600136 19981106 00136 NM 1998 11 6 98FDEA00583 1 19980917 A 5311 65163517 FRAME BOEING 727 72725C 138400H NM E & E DOORWAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 118FE 19300 NR 546 CORROSION (C53-100-010) ON E&E DOOR FRAME AT BS 423, RBL 4-LBL 4, WL 148. ** S/D ** R&R E & E DOOR FRAME AT BS 423, WL 148 PER FEDEX SRM 51-30-2 & FEDEX SRM 51-10-1. 2 L 7 3 4F A3WE 1998110600137 19981106 00137 NM 1998 11 6 DL72W982217 1 19980914 A 5400 S-DUCT BOEING 727 727247 138408F NM NR 2 ENGINE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2816W 20872 AT HMV FOUND SKIN - BENT/CRACKED INSIDE S-DUCT APPROX 4FT FROM L/E OF INLET AT 12 O-CLOCK POSITION. CORR: MANUFACTURED REPAIR DBLR AND FILLER PER SRM 54-10-3 P.63 INSTLD PER SAME. 2 L 7 3 4F A3WE 1998110600138 19981106 00138 NM 1998 11 6 DL72S982218 1 19980923 A 5753 652163261 ANGLE BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 DURING SHOP VISIT THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 21 AND 34 FR OM IB END OF FLAP. THE ANGLE WAS REPAIRED BY SPLICING IN A NE W SECTION OF ANGLEPER MM 57-52-0, FIG. 802. 2 L 7 3 4F A3WE 1998110600139 19981106 00139 NM 1998 11 6 DL72S982220 1 19981028 A 3397 WIRE 337701962 BOEING 727 727232 1384082 NM ROW 12 SHORTED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 411DA 2136 21223 FOUND ON MAINT PREFLIGHT ROWS 12-19 EMERGENCY TRACK LIGHTINGINOP REPLACED BLOWN FUSE ON FWD POWER SUPPLY AFTER REPAIRING BARE WIRES UNDER SEAT ROW 12 DEF LIGHT OPN NORMAL REPLACED FWD BATTERY PRECAUTIONARY. 2 L 7 3 4F A3WE 1998110600140 19981106 00140 NM 1998 11 6 DLM88982221 1 19981027 A 3350 41B004AD073 BATTERY DOUG MD88 MD88 3023688 NM ROW 28-30 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 901DL 49532 FOUND ON L/O EMERGENCY LIGHTS AT ROW 28-30 INOP - REPLACED BATTERY PACK BATTERIES. 2 L 7 2 4F RT A6WE 1998110600141 19981106 00141 NM 1998 11 6 DL73K982223 1 19981027 A 2710 ABSB4 CONTROL CABLE BOEING 737 737232 1384475 NM RT AILERON FRAYED A DALA D RETURN TO BLOCK F FLT CONT AFFECTED TX TAXI/GRND HDL 1 SO 27 311DL 23083 RT AILERON BINDING AT FULL RT TRAVEL. INSP FOUND AILERON CABLE SEGMENT ABSB-4 FRAYED. MANUFACTURED & INSTLD NEW CABLE SEGMENT ABSB-4 PER M/M. REPLD 2 EA AILERON BUS CABLE PULLEYS AT APPROX STA RBL 60. RIGGED AILERON BUS CABLES AND OPS C KD, ADJUSTED FIRST OFFICERS BODY CABLES AA AND AB AND OPS CK GOOD PER M/M. 2 L 7 2 4F RT A16WE 1998110600142 19981106 00142 NM 1998 11 6 DL72S982225 1 19981028 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 6 LE FLAP ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 545DA 22494 REF. SHIP 545 TPA LTR. CHECK C2 10/28/98, NO. 6 L/E FLAP ACTUATOR SUPPORT BOX FOUND CRACKED AT UPPER I/B ANGLE. REPA IRED PER MM 57-20-21 PG. 811 2 L 7 3 4F A3WE 1998110600143 19981106 00143 1998 11 6 DLL19982227 2 19981028 A 7314 FUEL PUMP LKHEED 1011 10113853 5265020 WP NR 2 ENGINE MALFUNCTIONED A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 763DL 22501 193Y1197 14783 WHILE CLIMBING THRU 30000 FT NOTICED NBR 2 ENG FUEL PRESS. LIGHT ILLUM. REF. POM MANUAL.INITIALLY LIGHT WAS INTERM.-AFTE R 1 MIN. WENT TO STEADY.F/O NOTICED N1 AND N3 UNWINDING-GEN. TRIPPED OFF.ACCOM-FUEL PRESS.ABNORMAL CKLIST. ENG SHUT DOWN AND FOLLOW UP CKLIST.OBSERVED N1,N2,N3 ROTATION UNTIL ON FINAL APPROACH. RAN TEST NBR 19 PER FIM CKS GOOD. RPLCD FUE L PUMP,FUEL FILTER,FUEL PRESS. SWITCH OPS CK AND LK CK GOOD.RAN ENG PER PFHB ALL INDICATIONS NORMAL. OK FOR SERVICE 2 L 7 3 4F A23WE 1998110600144 19981106 00144 NM 1998 11 6 DL73K982229 1 19981029 A 2761 O-RING 654456115 BOEING 737 737232 1384475 NM NR 3 SPOILER ACT FAILED A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 319DL 3068A 23091 LOSS OF HYD SYS A QTY IN FLT. REPL NO3 FLT SPOILER ACTUATOR. O-RING RUPTURED ON ACTUATOR. ALL LEAK AND OPN TEST NML. 2 L 7 2 4F RT A16WE 1998110600145 19981106 00145 NE 1998 11 6 SCNA98131 2 19981027 A 7230 COMPRESSOR BOEING 727 727225 1384077 NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE DAMAGED A SCNA K NONE C F.O.D. IN INSP/MAINT 1 GL 15 282SC 42164 3494 22558 DURING A LINE MAINTENANCE CHECK, SOFT BODY COMPRESSOR INGESTION WAS DETECTED ON THE NUMBER THREE ENGINE. REMOVED AND RE PLACED ENGINE. 2 L 7 3 4F 4 F A3WE E2EA 1998110600146 19981106 00146 NM 1998 11 6 DHL98701001 1 19981028 A 3040 DR18ES RELAY BOEING 727 72730C 1384009 NM LEFT STICKING A DHLA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 01 701DH 19011 L/H WINDOW OVER HEAT LIGHT CAME ON IN FLIGHT . TRIED TO RESET IAW AOM . REMOVED AND REPLACED R-36 RELAY. OPS CHECK GOO D 2 L 7 3 4F A3WE 1998110600147 19981106 00147 1998 11 6 ARWA981064 4 19981030 A 3421 25873351 VERT GYRO DOUG DC8 DC862 3021970 WP LEFT MALFUNCTIONED A ARWA O OTHER J WARNING INDICATION CR CRUISE 1 SO 19 1804 45896 CAPT'S ADI GYRO FAILS IN ALL TURNS INTERMITTENTLY IN LEVEL FLIGHT ALSO WINDSHEAR FAIL ILUMINATED AT THE SAME TIME. R/R #1 VERT. GYRO I.A.W. DC-8 M/M 34-25-1 OPS CHECK OF HORIZONTAL SYSTEM, GOOD ON GROUND I.A.W. DC-8 M/M 34-25-0. 2 L 7 4 4F 4A25 1998110600148 19981106 00148 NM 1998 11 6 VNAA9810022 1 19981028 A 7312 3045594 FUEL HEATER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA O OTHER J WARNING INDICATION DE DESCENT 1 GL 07 442JS 70828 3060 116127 DURING THE DESCENT TO PIT, A RIGHT HAND ENGINE LOW OIL PRESSURE WARNING MESSAGE ILLUMINATED. THE AIRCRAFT CONTINUED THE DESCENT AND LANDED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND ENGINE FUEL OIL HEATER, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-11-10. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998110600149 19981106 00149 WP 1998 11 6 TC8A98073 1 19981029 A 5270 LIGHT DOUG DC8 DC862F 3021972 WP CARGO DOOR ILLUMINATED A TC8A D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 GL 23 187SK 46022 TRIP# 02738. DISCREP: DURING TAXI, CARGO INDICATION LIGHT ILLUMINATED ON DOOR SYSTEM AFTER TEST. CORR. ACTION: R ECYCLED DOOR AND OPS CHECKED IAW 52-36-1. 2 L 7 4 4F 4A25 1998110600150 19981106 00150 NE 1998 11 6 TC8A98074 2 19981030 A 7230 COMPRESSOR DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 181SK 45910 669217 TRIP# 02747. DISCREP: #2 ENGINE COMPRESSOR STALLED ON TAKEOFF ROLL. CORR ACTION: CLEANED AND LUBED PRBC VALVE, PERFORM ED FLAG CHECK IAW 75-30-03. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST, NO DEFECTS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1998110600151 19981106 00151 NE 1998 11 6 TC8A98075 2 19981030 A 7532 563883 PRBC VALVE DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE FAILED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 181SK 45910 669217 NR 2 ENGINE COMPRESSOR STALL ON T/O ROLL AT APPROX 60 KTS. REPLACED PRBC VALVE IAW MM 75-30-1 DUE TO FOUND STUCK. INSP ECTED ENGINE, FOUND INTAKE/TAILPIPE CLEAN. BORESCOPED ENGINE IAW PW MM 72-00. RUN UP CHECK COMPLETED BY CREW. ENGINE OPERATION ALL NORMAL IAW DC8 MM 71-00. 2 L 7 4 4F 4 F 4A25 1E8 1998110600152 19981106 00152 NM 1998 11 6 SWAA982624 1 19981023 A 2910 65449913 VALVE BOEING 737 7373A4 1384585 NM A HYD SYST LEAKING A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 676SW 23288 AFTER T/O LAX, AFTER RAISING L/G BOTH SYS A HYD LOW PRESSURE LIGHTS ILLUMINATED FOR ABOUT 5-10 SEC. HYD FLUID SYS A FLU ID WENT BELOW REFILL MARK FROM FULL AND CONTINUED TO DECREASE TO 1/2. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL L ANDING. REMOVED AND REPLACED A SYSTEM ISOLATION VALVE ASSY. LEAK CHECK OPS, CHECK GOOD PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998110600153 19981106 00153 NM 1998 11 6 SWAA982625 1 19981025 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND BS 1016 CRACKED IN SKIN BELOW CIRCUMFERENTIAL STRAP AT STR 6L, 3 FASTENERS. REPAI RED PER SWA RA 1-253-1904. 2 L 7 2 4F A16WE 1998110600154 19981106 00154 NM 1998 11 6 SWAA982626 1 19981026 A 5320 BAC14902629 ANGLE BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 OUTER CHORD LT ANGLE CRACKED AT WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600155 19981106 00155 NM 1998 11 6 SWAA982627 1 19981026 A 5312 BAC15062612 BULKHEAD BOEING 737 7372H4 138448C NM AFT PRESS BLKHD CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND AFT PRESSURE BULKHEAD CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600156 19981106 00156 NM 1998 11 6 SWAA982628 1 19981025 A 5320 WEB BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND CRACK INDICATION USING EDDY CURRENT INSP OF APB WEB AT BS 1016 AT STRINGER 6L UNDER Y CHORD, 2 FASTENERS. REQUIRES CRACK VERIFICATION FWD SIDE OF APB PER SI - 10818-53. ACCOMPLISHED REPAIR PER SWA RA NR 1-253-1902. 2 L 7 2 4F A16WE 1998110600157 19981106 00157 NM 1998 11 6 SWAA982629 1 19981025 A 3397 WIRE BOEING 737 7372H4 138448C NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND EGRESS FLOOR TRACK LIGHT SYSTEM BACK 2 SEGMENTS INOP. THREE BROKEN WIRES AT AFT FLOO R TRACK TO SIDEWALK AREA. REPAIRED WIRING PER BOEING M/M. 2 L 7 2 4F A16WE 1998110600158 19981106 00158 NM 1998 11 6 SWAA982630 1 19981022 A 2910 6544510844 LINE BOEING 737 7372H4 138448C NM A HYD SYST RUPTURED A SWAA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 07 082SW 22731 LOST A SYSTEM HYDRAULIC QUANTITY INBOUND INTO STL. MADE AN UNEVENTFUL LANDING. AIRCRAFT TOWED TO GATE. FOUND PRESSURE LINE LEAKING JUST I/B OF NR 2 ENGINE. REPLACED HYD PRESSURE LINE. 2 L 7 2 4F A16WE 1998110600159 19981106 00159 NM 1998 11 6 SWAA982631 1 19981023 A 5330 65C27755 SKIN BOEING 737 7372H4 138448C NM AFT SERV DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SERV DOOR HINGE CUTOUT. REPAIRED PER SWA T1-A53-056. 2 L 7 2 4F A16WE 1998110600160 19981106 00160 NM 1998 11 6 SWAA982632 1 19981025 A 5730 6526701 SKIN BOEING 737 7372H4 138448C NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, RT WING L/E CUTOUT CRACKED AT NR 4 SLAT, O/B TRACK. REPAIRED SWA TI-257-008. 2 L 7 2 4F A16WE 1998110600161 19981106 00161 NM 1998 11 6 SWAA982633 1 19981027 A 3230 6552811115 MODULE BOEING 737 7372H4 138448C NM LANDING GEAR INOP A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 057SW 21722 LANDING GEAR LEVER WOULD NOT RAISE ON DEPARTURE. PULLED OVERRIDE TRIGGER, GEAR RAISED NORMALLY. THRUST REV ISOLATION V ALVE LIGHT ILLUMINATED AND CONFIG WARNING HORN SOUNDED WITH FLAPS TO ZERO. RETURNED TO DAL. REPLACED LANDING GEAR ELEC TRICAL MODULE AND OPS CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1998110600162 19981106 00162 NM 1998 11 6 SWAA982634 1 19981023 A 5330 65C35794 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AFT ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED PER SWA T1-A53-056 . 2 L 7 2 4F A16WE 1998110600163 19981106 00163 NM 1998 11 6 SWAA982635 1 19981024 A 3350 65C37192 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SCHEDULED CHECK, FOUND FWD CABIN TRACK EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998110600164 19981106 00164 NM 1998 11 6 SWAA982636 1 19981024 A 3350 20121 BATTERY BOEING 737 7373H4 1384600 NM PAX DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 616SW 27699 DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998110600165 19981106 00165 NM 1998 11 6 SWAA982637 1 19981023 A 5320 BAC1505100361 CHORD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND T CHORD CRACKED AT BS 178, LBL 5.7, WL 184. REPAIRED PER SWA T1-253-031. 2 L 7 2 4F A16WE 1998110600166 19981106 00166 NM 1998 11 6 SWAA982638 1 19981026 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, LBL 10, WL 134. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600167 19981106 00167 NM 1998 11 6 SWAA982639 1 19981023 A 5313 6545774 STRINGER BOEING 737 7372H4 138448C NM BS 967-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CORRODED FROM BS 967 TO 1006. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600168 19981106 00168 NM 1998 11 6 SWAA982640 1 19981023 A 5330 6518420 SKIN BOEING 737 7372H4 138448C NM BS 340 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER, BS 340. REPAIRED PE R BOEING SRM AND BOEING DRAWING 65C27257. 2 L 7 2 4F A16WE 1998110600169 19981106 00169 NM 1998 11 6 SWAA982641 1 19981023 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 330 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRANSITION CHECK, FOUND SHEAR TIE CORRODED BETWEEN STRINGERS 27 AND 28L, BS 330. REPLACED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600170 19981106 00170 NM 1998 11 6 SWAA982642 1 19981026 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKS AT BS 1016 BELOW CIRCUMFERENTIAL STRAP AT S6L. REPAIRED PER SWA RA 1-253-1904. 2 L 7 2 4F A16WE 1998110600171 19981106 00171 NM 1998 11 6 SWAA982643 1 19981026 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 OUTER CHORD LT ANGLE CRACKED AT WL 207. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600172 19981106 00172 NM 1998 11 6 SWAA982644 1 19981026 A 2450 11519320502 DISTR PANEL BOEING 737 7377H4 NM E/E BAY SHORTED A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 718SW 27852 JUST PRIOR TO ENGINE START AN ACRID ELECTRICAL SMELL ENTERED CABIN AT THE TIME THE DUS WENT BLANK AND SEVERAL SYSTEMS FE LL OFF LINE. FOUND P-91 WIRES TO BE BURNT. REMOVED AND REPLACED POWER DISTRIBUTION PANEL 91 PER M/M 24-21-21-4 OPERATI ONAL CHECK OF SYSTEM OK. 2 L 7 2 4F RT A16WE 1998110600173 19981106 00173 NM 1998 11 6 SWAA982645 1 19981027 A 3350 65C27093 LIGHT BOEING 737 7372T4 1384492 NM SERVICE DOOR LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING WALKAROUND CHECK, FOUND AFT SERVICE DOOR EMERGENCY EXIT LIGHT OPERATING INTERMITTENTLY. RESECURED LIGHT ASSEMBLY AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F A16WE 1998110600174 19981106 00174 NM 1998 11 6 SWAA982646 1 19981027 A 3350 6556633 BATTERY BOEING 737 7372T4 1384492 NM OVERWING DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND OVERWING CEILING EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1998110600175 19981106 00175 NM 1998 11 6 SWAA982647 1 19981027 A 5330 65C35768 SKIN BOEING 737 7372T4 1384492 NM BS 785 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 785, S17L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600176 19981106 00176 NM 1998 11 6 SWAA982648 1 19981027 A 5330 65C35768 SKIN BOEING 737 7372T4 1384492 NM BS 750 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED SERVICE CHECK, FOUND TWO FUSELAGE SKIN CRACKS AT BS 750. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600177 19981106 00177 NM 1998 11 6 SWAA982649 1 19981028 A 2782 256A2001 ACTUATOR BOEING 737 7372H4 138448C NM NR 6 LE SLAT INOP A A SWAA D RETURN TO BLOCK J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SW 07 095SW 23054 RETURNED TO HOU DUE TO THE INABILITY TO RETRACT NR 6 L/E SLAT. REPLACED NR 6 SLAT ACTUATOR PER BOEING M/M. 2 L 7 2 4F A16WE 1998110600178 19981106 00178 NM 1998 11 6 SWAA982650 1 19981027 A 5320 ANGLE BOEING 737 7372H4 138448C NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4 D-CHECK, FOUND ATTACH ANGLE CRACKED ON AFT CARGO DOOR FRAME UNDER COUNTER SPRINGS. INSTALLED DOUBL ER PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600179 19981106 00179 NM 1998 11 6 SWAA982651 1 19981028 A 3350 20131 BATTERY CHARGER BOEING 737 7372T4 1384492 NM APAX DOORWAY INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED C2 CHECK, FOUND AFT ENTRYWAY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BATTERY CHARGER HO USING. 2 L 7 2 4F A16WE 1998110600180 19981106 00180 NM 1998 11 6 SWAA982653 1 19981029 A 2612 655280915 FIRE LOOP BOEING 737 7372H4 138448C NM NR 2 ENGINE MALFUNCTIONED A SWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 07 082SW 22731 ON APPROACH, NR 2 ENGINE FIRE WARNING BELL AND HORN SOUNDED. PERFORMED ENGINE SHUTDOWN PROCEDURES AND ACTIVATED FIRE BO TTLES. MADE AN UNEVENTFUL LANDING. INSPECTED WITH NO EVIDENCE OF FIRE OR OVERHEAT CONDITION. REMOVED AND REPLACED LOW ER FIRE LOOP. REMOVED AND REPLACED ENGINE AND APU FIRE DETECTION UNITS, AND BOTH FIRE BOTTLES. CLEANED AND REINSTALLED ALL LOOP DISCONNECTS TO UPPER AND LOWER DETECTORS. ALL RESISTANCE CHECKED WITHIN M/M LIMITS. ENGINE RUN CHECKED NORMA L. 2 L 7 2 4F A16WE 1998110600181 19981106 00181 NM 1998 11 6 SWAA982654 1 19981029 A 2120 AIR DIST BOEING 737 7372H4 138448C NM CABIN ODOR A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 102SW 23108 FUEL SMELL IN CABIN WITH APU AIR ON. EXAMINED A/C PACK BAY, KEEL BEAM AREA AND A/C DISTRIBUTION BAY, NO FUEL LEAK NOTED . NO FUEL FOUND AT APU FUEL LINE SHROUD DRAIN. REMOVED AND REPLACED LT AND RT WATER SEPARATOR BAGS PER MM. RAN APU FO R 30 MINS, NO FUEL SMELL FOUND. OPS CHECK AND LEAK CHECK GOOD. 2 L 7 2 4F A16WE 1998110600182 19981106 00182 NM 1998 11 6 SWAA982655 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S4L PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600183 19981106 00183 NM 1998 11 6 SWAA982656 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 540-727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 540 TO 727 AT S4R PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600184 19981106 00184 NM 1998 11 6 SWAA982657 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 727-908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S4L PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600185 19981106 00185 NM 1998 11 6 SWAA982658 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S10R PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600186 19981106 00186 NM 1998 11 6 SWAA982659 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S14L PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600187 19981106 00187 NM 1998 11 6 SWAA982660 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 727-908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S1OR PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600188 19981106 00188 NM 1998 11 6 SWAA982661 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S4R PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600189 19981106 00189 NM 1998 11 6 SWAA982662 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 540-727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 540 TO 727 AT S4L PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600190 19981106 00190 NM 1998 11 6 SWAA982663 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 727-908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S4R PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600191 19981106 00191 NM 1998 11 6 SWAA982664 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 727-908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 727 TO 908 AT S10L PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600192 19981106 00192 NM 1998 11 6 SWAA982665 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S14R PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600193 19981106 00193 NM 1998 11 6 SWAA982666 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 360 TO 540 AT S10L PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600194 19981106 00194 NM 1998 11 6 SWAA982667 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 908-951 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S10L PER DALFORT XEA X2-53-223. 2 L 7 2 4F A16WE 1998110600195 19981106 00195 NM 1998 11 6 SWAA982668 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 908-951 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S14L PER DALFORT XEA X2-53-224 REV 1. 2 L 7 2 4F A16WE 1998110600196 19981106 00196 NM 1998 11 6 SWAA982669 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 908-951 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S10R PER DALFORT XEA X2-53-223. 2 L 7 2 4F A16WE 1998110600197 19981106 00197 NM 1998 11 6 SWAA982670 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 908-951 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 951 AT S14R PER DALFORT XEA X2-53-224. 2 L 7 2 4F A16WE 1998110600198 19981106 00198 NM 1998 11 6 SWAA982671 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 908-1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 1016 AT S4R PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600199 19981106 00199 NM 1998 11 6 SWAA982672 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 908-1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, REPAIRED FUSELAGE LAP SKIN AT BS 908 TO 1016 AT S4L PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600200 19981106 00200 NM 1998 11 6 SWAA982673 1 19981029 A 5330 6545765 SKIN BOEING 737 7372H4 138448C NM BS 290 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACK INDICATION AT BS 290, S4R. REPAIRED PER SWA ACO 6717-53 REV 5. 2 L 7 2 4F A16WE 1998110600201 19981106 00201 NM 1998 11 6 SWAA982674 1 19981025 A 2781 189915 SWITCH BOEING 737 7373H4 1384600 NM NR 2 LE FLAP FAILED A A SWAA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 SW 07 329SW 23693 NR 2 L/E FLAP REMAINED FULL EXTEND AFTER RETRACTION ON DEPARTURE. RETURNED TO BURBANK. REMOVED AND REPLACED NR 2 LEADI NG EDGE FLAP PROX SWITCH PER MM, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998110600202 19981106 00202 WP 1998 11 6 TWAA9817601 1 19981031 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOP A TWAA K NONE L NO TEST TX TAXI/GRND HDL 1 CE 05 920TW 49369 DURING TAXI TO GATE EMERGENCY EGRESS LIGHTS CAME ON. UNABLE TO EXTINGUISH WITH EMERGENCY LIGHT SWITCH. STAYED ON ABOUT 30 SECONDS THEN WENT OFF. REPLACED EGRESS POWER SUPPLY FOR FIRST CLASS SECTION. CHECK-C 6-18-98 STL. 2 L 7 2 4F A6WE 1998110600203 19981106 00203 EU 1998 11 6 AWXA9800216 1 19981101 A 2700 3945122502 ELAC AIRBUS 320 A320232 3930326 EU E & E COMPT MALFUNCTIONED A A AWXA O OTHER F FLT CONT AFFECTED LD LANDING 1 WP 28 639AW 19716 10821 471 DURING FLAP EXTENSION POS 1 TO POS 2 AND POS 2 TO POS 3 AIRCRAFT ROLLED SHARPLY L/R SHORT DURATION ROLL. REPLACED BOTH ELAC COMPUTERS PER 27-93 AND TESTED PER 27-93-00, OK FOR SERVICE. 2 L 7 2 4F RT A28NM 1998110600204 19981106 00204 SO 1998 11 6 RAAA98E4021 1 19981031 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 RT OVERWING EMERGENCY EXIT AND AFT RT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED LIGHT ASS EMBLIES DUE FAILED. 2 L 7 4 4T 4A22 1998110600205 19981106 00205 SO 1998 11 6 RAAA98E4022 1 19981031 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO ROW 15 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 PAX ROW 15 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998110600206 19981106 00206 WP 1998 11 6 CALA9802005 1 19981101 A 3350 AD4002P BATTERIES AEROQUALITY DOUG DC9 DC982 3022082 WP L & R OVERWING DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND BOTH AFT LT AND RT OVERWING EMERGENCY EXIT SIGNS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED IAW MM 33-53-00, PAGE 409. 2 L 7 2 4F A6WE 1998110600207 19981106 00207 WP 1998 11 6 CALA9802006 1 19981101 A 5320 59367091 FITTING DOUG DC9 DC982 3022082 WP BS 980 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND A .75 INCH CRACK IN LT WHEEL WELL FITTING AT FLAP ACTUATOR MOUNTS STA 980. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998110600208 19981106 00208 WP 1998 11 6 CALA9802007 1 19981101 A 5315 FLOORBEAM DOUG DC10 DC1030 3023501 WP BS 1275 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND A 1 INCH CRACK IN FLOORBEAM AT STA 1275, RBL 104. REPAIRED IAW ECRA 5316-01000. 2 L 7 3 4F A22WE 1998110600209 19981106 00209 WP 1998 11 6 CALA9802008 1 19981101 A 3350 EMSE299 BATTERY PACK ENGMAGNETICS DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12064 47862 THE EMERGENCY LIGHT SYSTEM IN A ZONE FAILED AFTER SIX MINUTES. THE BATTERY PACKS WERE REPLACED AND OPERATION CHECKED GO OD IAW MM 33-50-00. 2 L 7 3 4F A22WE 1998110600210 19981106 00210 WP 1998 11 6 CALA9802009 1 19981102 A 5280 DOOR DOUG DC10 DC1030 3023501 WP RT MLG CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND A 1.75 INCH CRACK AT AFT LOWER CORNER OF RT MLG WHEEL WELL DOOR. THE AREA WAS REINFORCED WITH A DOUBLE R IAW SRM 51-21-01 AND 51-35-02. 2 L 7 3 4F A22WE 1998110600211 19981106 00211 NM 1998 11 6 CALA9802010 1 19981102 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND TWO .25 INCH DIAMETER HOLES IN RT ELEVATOR UPPER SKIN JUST AFT OF NR 3 ATTACH HINGE. A DOUBLER REPAIR WAS INSTALLED IAW SRM 55-20-3, PAGE 9. 2 L 7 3 4F A3WE 1998110600212 19981106 00212 NM 1998 11 6 CALA9802011 1 19981102 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A .5 INCH CRACK IN INBOARD SUPPORT BRACKET AT LOWER END WHERE LT WING NR 1 L/E FLAP ACTUATOR IS MOUNTED . A NEW SUPPORT BRACKET WAS INSTALLED IAW SRM 51-30-2, PAGE 3. 2 L 7 3 4F A3WE 1998110600213 19981106 00213 SO 1998 11 6 COMA9810247 1 19981101 A 5246 DOOR EMB 120 EMB120RT SO FUEL SYST NOT LATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK W INADEQUATE Q C TO TAKEOFF 1 SO 01 255CA 120238 DOOR WARNING DURING TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR. 2 L 7 2 4T RT A31SO 1998110600214 19981106 00214 SO 1998 11 6 COMA9810246 1 19981028 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 259CA 120252 EXIT SIGN AT ROW 5 IS BROKEN. REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998110600215 19981106 00215 1998 11 6 COMA9810245 4 19981029 A 3418 25C1175A SENSOR EMB 120 EMB120RT SO COCKPIT BURNT A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 267CA 120259 LAVATORY SMOKE ALARM ACTIVATED SMOKE IN COCKPIT. REPLACED BURNT AOA VANE CURRENT SENSOR. 2 L 7 2 4T RT A31SO 1998110600216 19981106 00216 EA 1998 11 6 COMA9860331 1 19981029 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 712CA 7244 OVERBOARD COOL AND DOOR OUTER HANDLE MESSAGE ON EICAS. INSPECTED DOOR AND FOUND NO DEFECTS. DOOR WARNING AND LATCH MEC HANISM OPERATE NORMAL. 2 L 7 2 4F RT A21EA 1998110600217 19981106 00217 EA 1998 11 6 COMA9860332 1 19981025 A 5312 6013501251 BULKHEAD ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 940CA 7048 BULKHEAD ANGLES AT FS 621 ARE CRACKED. REPLACED ANGLES. 2 L 7 2 4F RT A21EA 1998110600218 19981106 00218 EA 1998 11 6 COMA9860333 1 19981029 A 3397 BF10039001 WIRE CNDAIR CL600 CL6002B19 1900309 EA CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 963CA 7127 CABIN OVERHEAD EMERGENCY EXIT SIGN IS INOPERABLE. REPAIRED WIRING AT EMERGENCY LIGHT. 2 L 7 2 4F RT A21EA 1998110600219 19981106 00219 NM 1998 11 6 SWAA982492 1 19981008 A 5320 DOUBLER BOEING 737 7372H4 138448C NM BS 502 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND BS 502 STRINGER 4L, THE .032 DOUBLER CRACKED AROUND A RIVET HEAD. REPAIRED PER AC O 6717-3 REV 5. 2 L 7 2 4F A16WE 1998110600220 19981106 00220 NM 1998 11 6 SWAA982493 1 19981008 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 379, 399, 419 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND SKIN DAMAGED BY A SPOT FACER AT 3 HOLES, BS 379, 399, 419 ABOVE STRINGER 14L SPOT FACE IS .3125 INCH DIAMETER. REPAIRED CARRIED OUT ABOVE STRINGER PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600221 19981106 00221 NM 1998 11 6 SWAA982494 1 19981008 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C1 CHECK, FOUND MOST AFT RED EGRESS FLOOR LIGHT INOPERATIVE AND END CAP MISSING. RELAMPED EGRESS LIGHT , OPS CHECK GOOD AND REINSTALLED END CAP PER BOEING MM. 2 L 7 2 4F A16WE 1998110600222 19981106 00222 NM 1998 11 6 SWAA982495 1 19981008 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 787 BETWEEN STR 22L AND 23L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600223 19981106 00223 NM 1998 11 6 SWAA982496 1 19981008 A 3350 STRIP BOEING 737 7373H4 1384600 NM CABIN UNREADABLE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 080SW 26596 DURING SCHEDULED BC2 CHECK, FOUND AFT LWR EMERGENCY FLASHLIGHT STRIP UNREADABLE. REMOVED AND REPLACED EMERGENCY STRIP P ER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600224 19981106 00224 NM 1998 11 6 SWAA982497 1 19981008 A 3350 STRIP BOEING 737 7373H4 1384600 NM CABIN UNREADABLE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 080SW 26596 DURING SCHEDULED BC2 CHECK, FOUND FWD O/B EMERGENCY FLASHLIGHT STRIPS UNREADABLE. REMOVED AND REPLACED EMERGENCY STRIPS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600225 19981106 00225 NM 1998 11 6 SWAA982498 1 19981008 A 3350 LIGHT BOEING 737 7375H4 138449D NM ROW 6 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 525SW 26567 DURING SCHEDULED A2 CHECK, FOUND EMERGENCY TRACK LIGHT INOP AT ROW 6. RESEATED TRACK LIGHT CONNECTOR PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600226 19981106 00226 NM 1998 11 6 SWAA982499 1 19981008 A 5320 ANGLE BOEING 737 7373H4 1384600 NM CARGO DOORWAY BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED SERVICE CHECK, FOUND FWD B/B DOOR UP LATCH SUPPORT ANGLE BROKEN. REMOVED AND REPLACED SUPPORT ANGLE PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600227 19981106 00227 NM 1998 11 6 SWAA982500 1 19981009 A 3397 WIRE BOEING 737 7372T4 1384492 NM ROW 8 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721SW 22697 DURING SCHEDULED RON CHECK, FOUND LOOSE WIRES IN THE EMERGENCY EXIT LIGHTS AT ROW 8 F/O SIDE ONE WHITE LIGHT WON'T ILLUM INATE. REPAIRED WIRING AT ROW 8 F/O SIDE PER BOEING MM. 2 L 7 2 4F A16WE 1998110600228 19981106 00228 NM 1998 11 6 SWAA982501 1 19981009 A 3350 LIGHT BOEING 737 7373H4 1384600 NM EMERG EXIT SEPARATED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 600SW 27694 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHTING (TRACK) SEPARATED AT EMERGENCY EXIT. RECONNECTED LIGHTING SEGMEN T PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600229 19981106 00229 NM 1998 11 6 SWAA982502 1 19981009 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN KICKED UP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 604SW 27955 DURING WALKAROUND CHECK, FOUND EMERGENCY TRACK LIGHTS KICKED UP AT MID CABIN. REINSTALLED TRACK, FOUND RED LIGHT OUT AT WING EXIT ROW AND PLACARDED PER MEL. RECONNECTED RED LAMP AT EMERGENCY EXIT ROW PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600230 19981106 00230 NM 1998 11 6 SWAA982503 1 19981009 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1008 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 14L AT BS 1008 HAS HOLE RUBBED (DAMAGED) IN STRINGER FLANGE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600231 19981106 00231 NM 1998 11 6 SWAA982504 1 19981009 A 3350 LIGHT BOEING 737 7373H4 1384600 NM ROW 12 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 611SW 27697 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY TRACK LIGHTING SECURED WITH TAPE AT ROW 12. REMOVED TAPE AND SECURED LIGHTIN G PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600232 19981106 00232 NM 1998 11 6 SWAA982505 1 19981009 A 3350 LIGHT BOEING 737 7373Y0 1384671 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND REMOVED EGRESS LIGHTING FOM. INSTALLED EGRESS LIGHTING PER BOEING MM, OPS CHECK OK. 2 L 7 2 4F RT A16WE 1998110600233 19981106 00233 NM 1998 11 6 SWAA982506 1 19981009 A 5312 BULKHEAD SKIN BOEING 737 7373Y0 1384671 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 664SW 23495 DURING SCHEDULED 1/2D CHECK, FOUND HFEC INDICATION AT A1 CRACKED 178 BULKHEAD SKIN AT BS 178, LBL 1, WL 188 AFT SIDE. R EPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600234 19981106 00234 NM 1998 11 6 SWAA982507 1 19981011 A 2913 887477 PUMP BOEING 737 7373H4 1384600 NM NR 1 LOW PRESS A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 324SW 23414 AIR TURNBACK DUE TO NR 1 (B) ELECTRIC HYD PUMP LOW PRESURE LIGHT ILLUMINATED. AIRCRAFT MADE AN UNEVENTFUL LANDING. REM OVED AND REPLACED B PUMP, OPS CHECK GOOD PER BOEING MM (LPG 267342). 2 L 7 2 4F RT A16WE 1998110600235 19981106 00235 NE 1998 11 6 SWAA982508 2 19981011 A 7314 8063208 PUMP BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE NR 2 ENGINE MALFUNCTIONED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 521SW 25320 AIR TURNBACK DUE TO CLIMBING THROUGH FL 330, NR 2 ENG ROLLED BACK TO 65 PERCENT N1 FOR 30 SECONDS. DESCENT WAS STARTED AND ENGINE RETURNED TO NORMAL OPERATION. PMC CYCLED OFF WITH NO CHANGE IN ENGINE OPERATION. REMOVED AND REPLACED NR 2 ENGINE MEC AND PUMP ASSY PER BOEING MM. LEAK CK GOOD. PERFORMED HIGH PWR RUN, PARAMETERS CK GOOD ON GROUND (LPG 75819) . 2 L 7 2 4F 4 F RT A16WE E2GL 1998110600236 19981106 00236 NM 1998 11 6 SWAA982509 1 19981010 A 3350 6104789 BATTERY PACK BOEING 737 7372H4 138448C NM L1 & L2 DOORS DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 061SW 21970 DURING SCHEDULED SERVICE CHECK, FOUND EXTERIOR EMERGENCY EXIT LIGHT AFT OF L1 AND R1 DOORS INOPERATIVE. REMOVED AND REP LACED BATTERY PACK AND POWER SUPPLY ASSY PER BOEING MM. 2 L 7 2 4F A16WE 1998110600237 19981106 00237 NM 1998 11 6 SWAA982510 1 19981010 A 3397 WIRE BOEING 737 7373G7 1384595 NM ROW 10-12 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHTS AR ROW 10-12 INOPERATIVE. REPAIRED WIRING AT ROW 10 FLOOR TRACK LIG HT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600238 19981106 00238 NM 1998 11 6 SWAA982511 1 19981011 A 3350 LIGHT BOEING 737 7372H4 138448C NM RT OVERWING DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED SERVICE CHECK, FOUND LIGHT ASSY DAMAGED RT OVERWING DOOR EXIT LIGHT. REMOVED AND REPLACED RT OVERWING EXIT LIGHT ASSY PER BOEING MM. 2 L 7 2 4F A16WE 1998110600239 19981106 00239 NM 1998 11 6 SWAA982512 1 19981011 A 5320 ANGLE BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED RON CHECK, FOUND 2 ANGLES CRACKED FWD OF NR 1 LT ELECT B PUMP STIFFENER RUNS FROM FWD END LT SIDE OF KE EL BEAM VENT TO BOTTOM OF AILERON PCU FITTING (CRACKED MIDDLE OF STRINGER). INSTALLED ANGLE AND FASTENER IN FUEL TANK B ULKHEAD PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600240 19981106 00240 NM 1998 11 6 SWAA982513 1 19981011 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722SW 22698 DURING WALKAROUND CHECK, FOUND WHITE FLOOR PROXIMITY EMERGENCY ESCAPE PATH LIGHT OUT. INSTALLED LIGHT ASSY 5DEF PER BOE ING MM. 2 L 7 2 4F A16WE 1998110600241 19981106 00241 NM 1998 11 6 SWAA982514 1 19981011 A 3397 WIRE BOEING 737 7373H4 1384600 NM ROW 12 BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636SW 27709 DURING WALKAROUND CHECK, FOUND EGRESS LIGHTING PULLED UP BY ROW 12, THREE LIGHTS INOPERATIVE. INSTALLED WIRE SPLICE AND SECURED LIGHTS TO FLOOR PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600242 19981106 00242 NM 1998 11 6 SWAA982515 1 19981011 A 5320 INTERCOSTAL BOEING 737 7373Q8 1384670 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C2 CHECK, FOUND INTERCOSTAL CRACKED AT BS 520. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600243 19981106 00243 NM 1998 11 6 SWAA982516 1 19981012 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 540 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 663SW 23256 DURING SCHEDULED C2 CHECK, FOUND PULLED RIVET AT SKIN NEAR CONDITIONED AIR DOOR AT BS 540 KEEL BEAM. MADE PERMANENET RE PAIR PER RA 1-353-1897. 2 L 7 2 4F RT A16WE 1998110600244 19981106 00244 NM 1998 11 6 SWAA982517 1 19981012 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312SW 23334 DURING WALKAROUND CHECK, FOUND EMERGENCY TRACK LIGHTS WOULD NOT TURN-OFF WITH BATTERY POWER IN OFF AND EMERGENCY LIGHTS SWITCHED TURN IN OFF POSITION. REMOVED AND REPLACED FWD AND AFT FLOOR TRACK LIGHTING BATTERY PACKS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600245 19981106 00245 NM 1998 11 6 SWAA982518 1 19981012 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM PAX DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310SW 22949 DURING SERVICE CHECK, FOUND ON FWD ENTRY DOOR, EMERGENCY LIGHT INOPERATIVE. RESEATED BATTERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600246 19981106 00246 NM 1998 11 6 SWAA982519 1 19981012 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 857 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 857, RBL 7.5 UPPER SURFACE. CUT OUT DAMAGED AREA AND INSTA LLED REPAIR PARTS PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600247 19981106 00247 NM 1998 11 6 SWAA982520 1 19981012 A 5320 FRAME BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME AT BS 727, LBL 65.25, WL 232 ADJACENT TO STR 14L. REPAIRED PER TRAMCO ER NR 98-0921A. 2 L 7 2 4F RT A16WE 1998110600248 19981106 00248 NM 1998 11 6 SWAA982521 1 19981012 A 2782 FITTING BOEING 737 7373H4 1384600 NM NR 5 LE SLAT ACT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D-CHECK, FOUND CORRODED NR 5 SLAT ACTUATOR FITTING, I/B RIB HAS A PITTING CORRODED IN ROD END ATTACH HO LE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600249 19981106 00249 NM 1998 11 6 SWAA982522 1 19981012 A 3350 P00000CPC1 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED SERVICE CHECK, PERFORM C1 TASK 2041, REPLACE EMERGENCY LIGHT BATTERY PACKS BY USING SERVICEABLE BATTERI ES. IF SERVICEABLE BATTERIES ARE NOT AVAILABLE ACCOMPLISH TEST AS OUTLINE ON TASK CARD 2041. REMOVED AND REPLACED NINE EMERGENCY LIGHT BATTERY PACKS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600250 19981106 00250 NM 1998 11 6 SWAA982523 1 19981012 A 5320 STRAP BOEING 737 7373A4 1384585 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED FLOORBEAM ATTACH STRAP AT BS 773. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600251 19981106 00251 NM 1998 11 6 SWAA982524 1 19981012 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 301 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND L-ANGLE CRACKED AT BS 301, STR 10L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600252 19981106 00252 NM 1998 11 6 SWAA982525 1 19981012 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 470 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND BS 470, STR 14L SKIN LAP DOUBLER REPAIR. INSTALLED REPAIR PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600253 19981106 00253 NM 1998 11 6 SWAA982526 1 19981013 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 604SW 27955 DURING SCHEDULED WALKAROUND CHECK, FOUND OVERWING EMERGENCY FLOOR TRACK LIGHTING HAS LOOSE WIRE. RELAMPED AND RECONNECT ED EMERGENCY FLOOR TRACK LIGHTS PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600254 19981106 00254 NM 1998 11 6 SWAA982528 1 19981013 A 3350 BULB BOEING 737 7373G7 1384595 NM ROW 16 DEF FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 671SW 23785 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT LENS COVER ON OVERHEAD AT 16 DEF WILL NOT SECURE. INSTALLED BULB AND LENS COVER PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600255 19981106 00255 NM 1998 11 6 SWAA982527 1 19981012 A 3397 WIRE BOEING 737 7375H4 138449D NM CABIN EXPOSED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 506SW 24183 DURING SCHEDULED SERVICE CHECK, FOUND CABIN CREW REPORTS EXIT TRACK LIGHTING WIRES EXPOSED BY OVERWING EXIT. REPAIRED W IRES TO EMERGENCY TRACK LIGHT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600256 19981106 00256 NM 1998 11 6 SWAA982529 1 19981013 A 3350 LENS BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603SW 27954 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTING HAS SEVERAL LENS MISSING AND LIGHTS INOP. INSTALLED LENS WHE RE NEEDED AND RELAMPED WHERE NEEDED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600257 19981106 00257 NM 1998 11 6 SWAA982530 1 19981013 A 5512 657378337 SKIN BOEING 737 7375H4 138449D NM LT HORIZ STAB DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED RON CHECK, FOUND DENTED LEADING EDGE OF LT HORIZONTAL STABILIZER (CENTER SEC) DENT CAUSE ELONGATION OF SOME RIVETS HOLES. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600258 19981106 00258 NM 1998 11 6 SWAA982531 1 19981013 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 908-1016 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, REPLACE RIGHT HAND FUSELAGE SKIN AT BS 908 TO 1016 STR 20 LT TO STR 25 RT. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600259 19981106 00259 NM 1998 11 6 SWAA982532 1 19981013 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 908-916 PILLOWED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND PILLOWING SKIN IN AREA OF A PREVIOUS REPAIR AT BS 908 TO 916, STR 24L-25L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600260 19981106 00260 NM 1998 11 6 SWAA982533 1 19981013 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 908-1006 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED LAV WEB SUPPORT AT BS 986 TO 1006, LBL 35, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600261 19981106 00261 NM 1998 11 6 SWAA982534 1 19981013 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 344-360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FASTENER HOLES IN INTERCOSTAL AT BS 344 TO 360, STR 25LT. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600262 19981106 00262 NM 1998 11 6 SWAA982535 1 19981013 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 285 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FAIL-SAFE CHORD HAS 2 GOUGES AT BS 285, RBL 16-17, WL 157. REMOVED AND REPLA CED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600263 19981106 00263 NM 1998 11 6 SWAA982536 1 19981013 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 266 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED STRINGER 26 LT AT A FASTENER HOLE BS 266. REMOVED AND REPLACED STRINGER DAMA GED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600264 19981106 00264 NM 1998 11 6 SWAA982537 1 19981013 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND PANEL NR 3578 DELAMINATED AND CRACK AFT OF STAINLESS STEEL RUB PLATE ON HUMP OF PANEL . REMOVED DAMAGED SKIN AFT OF RUBPLATE AND REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600265 19981106 00265 NM 1998 11 6 SWAA982538 1 19981013 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 294-359 DOUBLE DRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND ELONGATED AND DOUBLE HOLES IN STRINGER 27 RT AT BS 294 TO 359. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600266 19981106 00266 NM 1998 11 6 SWAA982539 1 19981013 A 5754 SKIN BOEING 737 7373A4 1384585 NM NR 4 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND NR 4 SLAT SKIN CRACKED AT ACTUATOR. REPAIRED CRACK PER TI-A57-015. 2 L 7 2 4F RT A16WE 1998110600267 19981106 00267 NM 1998 11 6 SWAA982540 1 19981014 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SPECIAL VISIT TO DLF, FOUND REPAIR SKIN LAP ON STRINGERS PER SWA ACO 6717-53 REV5. SKIN LAP ACCOMPLISHED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998110600268 19981106 00268 NM 1998 11 6 SWAA982541 1 19981014 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED WALKAROUND CHECK, FOUND 1X AFT EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT UPPER FLASHL IGHT BATTERY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600269 19981106 00269 NM 1998 11 6 SWAA982542 1 19981014 A 5320 ANGLE BOEING 737 7373H4 1384600 NM LT A/C BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 392SW 27379 DURING SCHEDULED C1 CHECK, FOUND INLET SUPPORT ANGLE CRACKED. REPAIRED PER SWA RA NR 1-A53-1876. 2 L 7 2 4F RT A16WE 1998110600270 19981106 00270 NM 1998 11 6 SWAA982543 1 19981014 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 324-326 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 324 TO 326, WL 208, LBL 11. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998110600271 19981106 00271 NM 1998 11 6 SWAA982544 1 19981014 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED FRAME UNDER FLOOR TO SIDEWALL SUPPORT AT BS 727D, RBL 19, WL 158. REMOVED AN D REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600272 19981106 00272 NM 1998 11 6 SWAA982545 1 19981014 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED SHEAR TIE AT BS 827, 1 ABOVE STRINGER 23 LT. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600273 19981106 00273 NM 1998 11 6 SWAA982546 1 19981014 A 5330 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND SKIN CRACKED AT LT FWD NOSE GEAR DOOR CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600274 19981106 00274 NM 1998 11 6 SWAA982549 1 19981014 A 5320 STANCHION BOEING 737 7373A4 1384585 NM E & E COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND THE E-1 RT AFT STANCHION HAS A 1 INCH CRACK AT O/B VERTICAL RADIUS JUST BELOW THE E-1 SHELF SUPPORT ANGLE. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600275 19981106 00275 NM 1998 11 6 SWAA982550 1 19981014 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 847-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED LT AND RT FLOORBEAM NUT PLATE HOLE FROM BS 847 TO 947. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600276 19981106 00276 NM 1998 11 6 SWAA982551 1 19981014 A 3350 BULB BOEING 737 7373T5 NM ROW 16 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT AT ROW 16 OVERHEAD BIN IS INOPERATIVE. RELAMPED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600277 19981106 00277 NM 1998 11 6 SWAA982547 1 19981014 A 3350 20121 BATTERY BASE BOEING 737 7373H4 1384600 NM LT OVERWING INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED SERVICE CHECK, FOUND LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PA CK BASE PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600278 19981106 00278 NM 1998 11 6 SWAA982548 1 19981014 A 3350 BULB BOEING 737 7373A4 1384585 NM CARGO COMPT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND FWD RT CARGO LIGHT INOPERATIVE. RELAMPED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600279 19981106 00279 NM 1998 11 6 SWAA982552 1 19981015 A 5320 ANGLE BOEING 737 7373A4 1384585 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND ANGLE CRACKED I/B FLAP UPPER SHELF PANEL I/B PANEL. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600280 19981106 00280 NM 1998 11 6 SWAA982553 1 19981015 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 807 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED RADIUS OF SHEAR TIE AT BS 807, RBL 1 TO LBL 1, WL 152. REPAIRED FRAME SHEAR TIE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600281 19981106 00281 NM 1998 11 6 SWAA982554 1 19981015 A 5320 SILL BOEING 737 7373H4 1384600 NM BS 440-492 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED FWD CARGO DOOR SILL WEB SUPPORTING STRUCTURE AT BS 440 TO 492.4, RBL 24, WL 155. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600282 19981106 00282 NM 1998 11 6 SWAA982555 1 19981015 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND AT BS 344 FLOORBEAM TENSION STRAP CRACKED AT FASTENER LBL 46, WL 200. REMOVED AND RE PLACED FLOORBEAM TENSION STRAP PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600283 19981106 00283 NM 1998 11 6 SWAA982556 1 19981015 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 987-1017 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND STRINGER 23RT AT BS 987 TO 1017 HAS ELONGATED HOLES. REMOVED AND REPLACED STRINGER P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600284 19981106 00284 NM 1998 11 6 SWAA982557 1 19981018 A 2120 AIR DIST BOEING 737 7373H4 1384600 NM CABIN ODOR A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 341SW 24091 GATE RETURN DUE TO STRONG ODOR IN CABIN DURING TAXI OUT FOR DEPARTURE. INSPECTED BOTH AIR COND SYSTEMS, ELECTRICAL SYST EMS, BOTH CARGO PITS, GALLEYS, LAVS AND ENGINES. FOUND NO SOURCE OF ODORS, NO DEFECTS NOTED ALL PER BOEING MM (LPG NR 2 56051). 2 L 7 2 4F RT A16WE 1998110600285 19981106 00285 NM 1998 11 6 SWAA982558 1 19981017 A 2781 SWITCH BOEING 737 7373H4 1384600 NM NR 5 LE SLAT MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 365SW 26575 AIR TURNBACK DUE TO NR 5 LE SLAT INDICATED NOT RETRACTED AFTER TAKEOFF. CHECK LIST COMPLETED, STILL INDICATION ON OVERH EAD AND FWD PANEL. AIRCRAFT MADE AN UNEVENTFUL LANDING IN RNO. REMOVED AND REPLACED NR 5 SLAT MID-EXTEND SWITCH PER BO EING MM. 2 L 7 2 4F RT A16WE 1998110600286 19981106 00286 NM 1998 11 6 SWAA982560 1 19981016 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 400-420 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED INTERCOSTAL AT BS 400 TO 420, RBL 20, WL 152. REMOVED AND REPLACED PER BOEIN G SRM. 2 L 7 2 4F RT A16WE 1998110600287 19981106 00287 NM 1998 11 6 SWAA982561 1 19981016 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 727-740 MISDRILLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND MISDRILLED NUT PLATE HOLE CAUSING A EIGHT BALL HOLE EFFECT AT BS 727 +13, RBL 6, WL 1 55 ON CARGO TRACK. REMOVED AND REPLACED A REPLACEMENT SECTION OF FLOOR SUPPORT CHANNEL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600288 19981106 00288 NM 1998 11 6 SWAA982559 1 19981016 A 5320 CUTOUT LIP BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 391SW 27378 DURING SCHEDULED C1 CHECK, FOUND GROUND PWR CUTOUT CRACKED AT AFT MIDDLE LIP THROUGH TO RIVET .125 INCH LONG. PERMANENT LY REPAIRED PER SWA RA NR 1-353-1899. 2 L 7 2 4F RT A16WE 1998110600289 19981106 00289 NM 1998 11 6 SWAA982562 1 19981016 A 3350 CONNECTOR BOEING 737 7373H4 1384600 NM FWD GALLEY FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 642SW 27715 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT ABOVE FWD GALLEY LIGHT INOPERATIVE. FOUND BAD GROUND. REMOVED AN D REPLACED GROUND CONNECTOR PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600290 19981106 00290 NM 1998 11 6 SWAA982564 1 19981016 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 660 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 309SW 22948 DURING SCHEDULED SPECIAL VISIT TO DLF, FOUND CENTER FLOORBEAM IN PAX CABIN CRACKED AT BS 660. REPAIRED PER SWA RA NR 1- 357-0579. 2 L 7 2 4F RT A16WE 1998110600291 19981106 00291 NM 1998 11 6 SWAA982565 1 19981017 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED BULGE, KEEL BEAM AREA, JUST RIGHT OF CABIN AIR SERVICE PORT. REMOVED CORROS ION AND REPAIRED SKIN PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600292 19981106 00292 NM 1998 11 6 SWAA982566 1 19981017 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND BS 178 CRACKED IN SKIN AT LBL 7 WL 234. CUT OUT DAMAGE IN SKIN, REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600293 19981106 00293 NM 1998 11 6 SWAA982567 1 19981017 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 940 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED EXTERNAL FUSELAGE SKIN AT BS 940, STR 25R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600294 19981106 00294 NM 1998 11 6 SWAA982568 1 19981017 A 5320 ANGLE BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 396SW 27690 DURING SCHEDULED C4 CHECK, FOUND FLOOR LT PACK INLET SUPPORT ANGLE CRACKED. REPAIRED SUPPORT ANGLE PER SWA RA NR 1-A53- 1876. 2 L 7 2 4F RT A16WE 1998110600295 19981106 00295 NM 1998 11 6 SWAA982569 1 19981017 A 3350 LIGHT BOEING 737 737301 1384611 NM ROW 18 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY TRACK LIGHT COVER LOOSE FROM ROW 18 THROUGH AFT. RESECURED TRACK LIGHT PER B OEING MM. 2 L 7 2 4F RT A16WE 1998110600296 19981106 00296 NM 1998 11 6 SWAA982570 1 19981017 A 3350 LIGHT BOEING 737 7375H4 138449D NM ROW 6, 20 &16 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS AT ROW 6, 10 AND 16 ARE INOPERATIVE. RELAMPED FLOOR TRACK LIGHTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600297 19981106 00297 NM 1998 11 6 SWAA982563 1 19981017 A 3350 LIGHT BOEING 737 7375H4 138449D NM BIN 5 RT NOT ALIGNED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 520SW 25319 DURING SCHEDULED C1 CHECK, FOUND OVERHEAD BIN (5RT) EMERGENCY LIGHT LENS NEEDS ALIGNED. EMERGENCY LIGHT SECURED PER BOE ING MM. 2 L 7 2 4F RT A16WE 1998110600298 19981106 00298 NM 1998 11 6 SWAA982571 1 19981018 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM OVERWING INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY OVERWING EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER BOEING MM. 2 L 7 2 4F A16WE 1998110600299 19981106 00299 NM 1998 11 6 SWAA982572 1 19981018 A 3350 BATTERY PACK BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 055SW 21593 DURING SCHEDULED SERVICE CHECK, FOUND CENTER CABIN EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK AND BASE UNIT PER BOEING MM. 2 L 7 2 4F A16WE 1998110600300 19981106 00300 NM 1998 11 6 SWAA982573 1 19981018 A 5240 GUSSET BOEING 737 7373A4 1384585 NM FWD SVC DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND HFEC INDICATION OF CRACKED AFT LWR GUSSET ON FWD SERVICE DOOR AT O/B FASTENER. REPAI RED FWD SERVICE DOOR PER BOEING DWG 69-69854. 2 L 7 2 4F RT A16WE 1998110600301 19981106 00301 NE 1998 11 6 SWAA982574 2 19981018 A 7200 ENGINE BOEING 737 7375H4 138449D NM GE CFM56 CFM563B1 13802 NE NR 1 BIRD STRIKE A SWAA A UNSCHED LANDING C F.O.D. CR CRUISE 1 SW 07 527SW 26569 AIR TURNBACK DUE TO BIRD STRIKE NR 1 ENGINE. AIRCRAFT MADE AN UNEVENTFUL LANDING. PERFORMED BORESCOPE OF ENG, NO DAMAG E NOTED. REMOVED AND REPLACED ALL FAN BLADES AS PER BOEING MM. NO VIBRATION NOTED ON ENG RUN, OK TO CONTINUE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998110600302 19981106 00302 NM 1998 11 6 SWAA982575 1 19981018 A 4950 APU BOEING 737 7372H4 138448C NM CABIN ODOR A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED RON CHECK, FOUND FUEL SMELL IN CABIN WITH APU AIR ON. CONT PER MEL 49-1. OK FOR GROUND USE ONLY. OK FOR ENGINE START. 2 L 7 2 4F A16WE 1998110600303 19981106 00303 NE 1998 11 6 SWAA982576 2 19981019 A 7510 MANIFOLD BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 083SW 22732 AIR TURNBACK DUE TO NR 1 ENG OVERHEAT LIGHT CAME ON DURING CLIMBOUT. LIGHT EXTINGUISHED WHEN THRUST LEVER REDUCED TO ID LE. REMOVED NR 1 ENG TO FACILITATE MAINTENANCE PER SAM 104A. REMOVED AND REPLACED FUEL HEAT MANIFOLD PER BOEING MM. R EINSTALLED NR 1 ENGINE, OPS CHECK AND LEAK CHECK GOOD PER BOEING MM. 2 L 7 2 4F 4 F A16WE E2EA 1998110600304 19981106 00304 NM 1998 11 6 SWAA982577 1 19981019 A 3350 LIGHT BOEING 737 7373A4 1384585 NM ROW 22 & 23 MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND LIGHT MODULE MISSING FROM EGRESS FLOOR TRACK BETWEEN SEATS 22 AND 23 DEF. REPLACED E GRESS FLOOR TRACK LIGHT MODULE. 2 L 7 2 4F RT A16WE 1998110600305 19981106 00305 NM 1998 11 6 SWAA982578 1 19981019 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED PRESSURE WEB AT BS 663, LBL 31, VERIFIED BY HEFC. PRESSURE WEB REPAIRED PER SWA RA NR 1-353-1901. 2 L 7 2 4F RT A16WE 1998110600306 19981106 00306 NM 1998 11 6 SWAA982579 1 19981019 A 3350 LIGHT BOEING 737 7373H4 1384600 NM ROW 23 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 337SW 23959 DURING SCHEDULED C3 CHECK, FOUND FLOOR PROX LIGHT BULB INOPERATIVE AT SEAT ROW 23 DEF. REMOVED AND REPLACED FLOOR PROX LAMP AT SEAT ROW ROW 23 DEF PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600307 19981106 00307 NM 1998 11 6 SWAA982580 1 19981019 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 827 MIS DRILLED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND WHILE WORKING (FUSE 164), EIGHT BALLED HOLE ON FRAME AT BS 827, LBL 23 UNDER FLOOR TO SIDE WALL SUPPORT IN ACB. REPAIRED PER ENGINEERING NR 98-0815 AND BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600308 19981106 00308 NM 1998 11 6 SWAA982581 1 19981019 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED 178 BULKHEAD, RBL 4, WL 211.75-212 TO 25. CUT OUT CRACKED AREA AND REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600309 19981106 00309 NM 1998 11 6 SWAA982582 1 19981019 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND PANEL NR 3578 HAS NUMEROUS ELONGATED FASTENERS HOLES. REMOVED AND REPLACED DAMAGED S KIN AND ELONGATED FASTENER HOLES PER TRAMCO ER 98-0855. 2 L 7 2 4F RT A16WE 1998110600310 19981106 00310 NM 1998 11 6 SWAA982583 1 19981019 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND PANEL NR 3678 HAS NUMEROUS ELONGATED FASTENERS HOLES. REMOVED AND REPLACED DAMAGED S KIN AND ELONGATED FASTENER HOLES PER TRAMCO ER 98-0855. 2 L 7 2 4F RT A16WE 1998110600311 19981106 00311 NM 1998 11 6 SWAA982584 1 19981019 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 867 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND MECHANICAL DAMAGED FRAME AT BS 867, STR 26R. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600312 19981106 00312 NM 1998 11 6 SWAA982585 1 19981019 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 966 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 966 BETWEEN STRINGER 23 AND 24R. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998110600313 19981106 00313 NM 1998 11 6 SWAA982586 1 19981019 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 259.5 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND REPLACED FUSELAGE SIDE SKIN AT BS 259.5 TO 360, BL 0, STR 24L. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998110600314 19981106 00314 NM 1998 11 6 SWAA982587 1 19981019 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 265-296 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 25RT AT BS 265 TO 296. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600315 19981106 00315 NM 1998 11 6 SWAA982588 1 19981019 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 348-356 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 26 RT AT BS 348 TO 356, CONTINUES ON TO SPLICE AT BS 357 TO 360. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600316 19981106 00316 NM 1998 11 6 SWAA982589 1 19981019 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 359 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER SPLICE 27 LT AT BS 359. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600317 19981106 00317 NM 1998 11 6 SWAA982590 1 19981019 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 324-331 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 25 RT AT BS 324 TO 331. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600318 19981106 00318 NM 1998 11 6 SWAA982591 1 19981019 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND WHILE WORKING (FUSE 354), CRACKED FAIL-SAFE CHORD AT STRINGER 25 LT, BS 344, WL 158. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600319 19981106 00319 NM 1998 11 6 SWAA982592 1 19981019 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 285 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 285, RBL 18 TO 20, WL 152. REMOVED AND REPLACED WEB PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998110600320 19981106 00320 NM 1998 11 6 SWAA982593 1 19981019 A 5320 654582939 CHORD BOEING 737 7373H4 1384600 NM BS 297-305 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED T-CHORD, RBL 16, AT BS 297 TO 305, WL 150. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600321 19981106 00321 NM 1998 11 6 SWAA982594 1 19981019 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 277 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 277, STR 27 LT, WL 165. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998110600322 19981106 00322 NM 1998 11 6 SWAA982595 1 19981019 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 363-421 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 26 RT AT BS 363 TO 421. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600323 19981106 00323 NM 1998 11 6 SWAA982596 1 19981019 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 285.62 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND STRINGER CLIP AT BS 285.62, STR 26L HAS MECHANICAL DAMAGE. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600324 19981106 00324 NM 1998 11 6 SWAA982597 1 19981019 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED FRAME AT BS 380 RBL 20 WL 152. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600325 19981106 00325 NM 1998 11 6 SWAA982598 1 19981019 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 324-331 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND FUSELAGE 367 CRACKED STRINGER 25 LT AT BS 324 TO 331. TRAMCO RESPONSIBILITY. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600326 19981106 00326 NM 1998 11 6 SWAA982599 1 19981019 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 350-356 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND LOWER HORIZONTAL WEB CRACKED AT APPROX NAC BS 350 TO 356. REMOVED AND REPLACED INTER COSTAL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600327 19981106 00327 NM 1998 11 6 SWAA982600 1 19981021 A 2612 D1098 CONNECTOR BOEING 737 7372H4 138448C NM NR 2 ENGINE SHORTED A SWAA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 082SW 22731 INFLIGHT SHUTDOWN DUE TO NR 2 FIRE BLINKED A FEW TIMES WITH BELL, THEN STAYED ON. ALL OTHER INDICATIONS NORMAL. CHECK LIST WAS ACCOMPLISHED, BOTH BOTTLES FIRED, LIGHT REMAINED ILLUMINATED FOR REST OF FLIGHT. NOTHING NOTED ON INSTRUMENTS OR VISUALLY. SUSPECT FALSE FIRE WARNING. AIRCRAFT MADE AN UNEVENTFUL LANDING. FOUND CONECTOR D1098 SHORT TO GROUND. R EMOVED AND REPLACED CONECTOR D1098 PER BOEING MM. REMOVED AND REPLACED 1 AND 2 FIRE BOTTLES PER BOEING MM. RAN ENG FOR 20 MINUTES, OP CK OK. 2 L 7 2 4F A16WE 1998110600328 19981106 00328 NM 1998 11 6 SWAA982601 1 19981022 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DAMAGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 635SW 27708 DURING SCHEDULED WALKAROUND CHECK, FOUND TRACK LIGHTING MISSING COVER. REPAIRED TRACK WIRING PER BOING MM AND REINSTALL ED LENS COVER. OPS CKS GOOD. 2 L 7 2 4F RT A16WE 1998110600329 19981106 00329 NM 1998 11 6 SWAA982602 1 19981020 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26L CORRODED BETWEEN BS 727A AND 727 B, RBL 15. REPLACED STRINGER SECTION P ER BOEING SRM. 2 L 7 2 4F A16WE 1998110600330 19981106 00330 NM 1998 11 6 SWAA982603 1 19981020 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 092SW 22964 DURING SCHEDULED 1/4D CHECK, FOUND GLIDE SLOPE ANT ATTACH PANEL CRACKED AT LOWER RT CORNER. STOPPED DRILLED CRACK AND R EPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600331 19981106 00331 NM 1998 11 6 SWAA982604 1 19981020 A 5330 SKIN BOEING 737 7375H4 138449D NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 508SW 24185 DURING SCHEDULED C1 CHECK, FOUND UPPER HINGE CUTOUT AT AIRFRAME SIDE HAS .250 INCH CRACK AT CORNER. REPAIRED PER SWA RA NR 1-353-1903. 2 L 7 2 4F RT A16WE 1998110600332 19981106 00332 NM 1998 11 6 SWAA982605 1 19981020 A 3350 LIGHT BOEING 737 7372H4 138448C NM EXTERIOR INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING WALKAROUND CHECK, FOUND LT WING EMERGENCY EXIT EXTERIOR LIGHT INOPERATIVE. RELAMPED EXIT LIGHT PER BOEING MM, OP S NORMAL. 2 L 7 2 4F A16WE 1998110600333 19981106 00333 NM 1998 11 6 SWAA982606 1 19981021 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 354 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND ANGLE CRACKED AT BS 354 STR 16L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600334 19981106 00334 NM 1998 11 6 SWAA982607 1 19981021 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND ANGLE CRACKED AT BS 348 STR 16L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600335 19981106 00335 NM 1998 11 6 SWAA982608 1 19981021 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED 1/4D CHECK, FOUND ATTACH ANGLE CRACKED AT BS 344 AFT OF FRAME COMMON TO DOOR STOP 2ND FROM BOTTOM. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998110600336 19981106 00336 NM 1998 11 6 SWAA982609 1 19981021 A 3350 BULB BOEING 737 7372H4 138448C NM EXTERIOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING WALKAROUND CHECK, FOUND LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EXIT LIGHT PER BOEING MM, OPS NORMAL. 2 L 7 2 4F A16WE 1998110600337 19981106 00337 NM 1998 11 6 SWAA982610 1 19981021 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 268-290 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 26 RT FROM BS 268 TO 290. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600338 19981106 00338 NM 1998 11 6 SWAA982611 1 19981021 A 5754 ANGLE BOEING 737 7373H4 1384600 NM LT LE FLAP CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND LT WING ANGLE CRACKED ON FIXED LEADING EDGE O/B END OF K-FLAP AT AIRLOAD RIB. REMOVE D AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600339 19981106 00339 NM 1998 11 6 SWAA982612 1 19981021 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 347 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 25L, AT BS 347, LBL 34. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600340 19981106 00340 NM 1998 11 6 SWAA982613 1 19981021 A 5330 SKIN BOEING 737 7373H4 1384600 NM LT WING GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND LT WING LEADING EDGE IS GOUGED IN SEVERAL AREAS ABOVE NR 1 K-FLAP BETWEEN 15 AND 32 I /B OF NR 1 PYLON. REPAIRED DAMAGED LEADING EDGE SKIN PER ER 98-0785. 2 L 7 2 4F RT A16WE 1998110600341 19981106 00341 NM 1998 11 6 SWAA982614 1 19981020 A 5320 PRESSURE DECK BOEING 737 7373H4 1384600 NM E/E BAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 678SW 23290 DURING SCHEDULED 1/4D CHECK, FOUND HEFC CRACKED INDIC ON PRESSURE DECK APPROX 2 AT AFT RT CORNER OF TOP LT PANEL. REPAI RED PER SWA TI-A53-001. 2 L 7 2 4F RT A16WE 1998110600342 19981106 00342 NM 1998 11 6 SWAA982615 1 19981020 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 267 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND SHEAR TIE WITH EIGHT BALLED HOLE ABOVE STR 24 AT BS 267. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998110600343 19981106 00343 NM 1998 11 6 SWAA982616 1 19981020 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 360 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER TIE AT BS 360, STR 25L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600344 19981106 00344 NM 1998 11 6 SWAA982617 1 19981020 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 360 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED SKIN AT BS 259.5 TO 360, BL 0 TO STR 24R. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998110600345 19981106 00345 NM 1998 11 6 SWAA982618 1 19981020 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED SHEAR TIE AT BS 344, RBL 17 TO 18, WL 153. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600346 19981106 00346 NM 1998 11 6 SWAA982619 1 19981020 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 363 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CORRODED STRINGER 27R AT BS 363. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600347 19981106 00347 NM 1998 11 6 SWAA982620 1 19981020 A 5320 SUPPORT BOEING 737 7373H4 1384600 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND CRACKED SUPPORT STRUCTURE AT BS 540, RBL 70.5, JUST ABOVE FWD O/B CORNER OF RT A/C BA Y DOOR. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998110600348 19981106 00348 NM 1998 11 6 SWAA982621 1 19981021 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 303 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND DAMAGED TO INTERIOR SKIN AT BS 303 WL 305 LBL 11. REMOVED AND REPLACED PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998110600349 19981106 00349 NM 1998 11 6 SWAA982622 1 19981021 A 5512 SKIN BOEING 737 7373H4 1384600 NM LT HORIZ STAB DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRAN CHECK, FOUND LT HORIZONTAL STAB L/E SKIN IS DAMAGED AT UPPER SURFACE FASTENER L/E BS 98.66. REMOV ED DAMAGE FROM HORIZONTAL STAB. REPAIRED L/E SKIN PER ER 98-0863. 2 L 7 2 4F RT A16WE 1998110600350 19981106 00350 NM 1998 11 6 SWAA982623 1 19981021 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 610SW 27696 DURING SCHEDULED C1 CHECK, PERFORM TASK 2041 REPLACE EMERGENCY LIGHT BATTERY PACKS BY USING SERVICEABLE BATTERIES. PERF ORMED TASK EMERGENCY LIGHT FUNCTIONAL TEST, LIGHTS MEET THE REQUIREMENTS PER BOEING MM. 2 L 7 2 4F RT A16WE 1998110600351 19981106 00351 NM 1998 11 6 UPS98228033 1 19981007 A 5330 SKIN BOEING 727 727108C 1384039 NM BS 310 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 310 BETWEEN STR 9L AND S8L. REPAIR CARRIED OUT IAW SRS EO 98-30-003 AND 98-30-003 REVISION 1, REFERENCE UPS ENGINEERING FILE NUMBER 5330-2084. 2 L 7 3 4F A3WE 1998110600352 19981106 00352 NM 1998 11 6 UPS98228034 1 19981008 A 5311 FRAME BOEING 727 727108C 1384039 NM BS 910 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, SUSPECT CRACK OUTBOARD FLANGE RADIUS BS 910 LT BETWEEN STRINGER 18A SILL AND WHEEL WELL CEILING LT WH EEL WELL. REPAIR CARRIED OUT IAW SRM ADDENDUM EO B727-5310-1896. 2 L 7 3 4F A3WE 1998110600353 19981106 00353 NM 1998 11 6 UPS98228035 1 19981008 A 5320 65163301 FITTING BOEING 727 727108C 1384039 NM BS 870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, CORROSION ON 870 FRAME RT AT FLOORBEAM ATTACH RBL 62.5. FITTING REPLACED IAW EO B727-5310-3056. 2 L 7 3 4F A3WE 1998110600354 19981106 00354 NM 1998 11 6 UPS98228036 1 19981006 A 5313 STRINGER BOEING 727 727108C 1384039 NM BS 850-870 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, CORROSION ON LOWER FLANGE OF STRINGER 18A LEFT HAND BETWEEN BS 870 AND 850. REPAIR CARRIED OUT IAW S RS EO 98-30-004, REF UPS ENGINEERING FILE NUMBER 727-53-2086. 2 L 7 3 4F A3WE 1998110600355 19981106 00355 NM 1998 11 6 UPS98228045 1 19981031 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, AISLE EEL INOP AT ROWS 13, 14, 15, 18 AND 6 ABC. ALSO, AFT ENTRY DOOR. REMOVED AND REPLACED BATT PACKS AS ABOVE, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998110600356 19981106 00356 NM 1998 11 6 UPS98228046 1 19981101 A 5320 BRACKET BOEING 727 7271A7C 13840X2 NM FUSELAGE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 935UP 20143 INSPECTION TYPE-N/A, OPENING TO RIGHT OF TAIL SKID FOWARD CROSS MEMBER CRACKED JUST BELOW MANUAL PUMP. REPAIRED BRACKET PER SRM 51-10-02. 2 L 7 3 4F A3WE 1998110600357 19981106 00357 WP 1998 11 6 UPS98828026 1 19981011 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 691 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING L/E RIB AT STA 691.25 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998110600358 19981106 00358 WP 1998 11 6 UPS98828027 1 19981014 A 5720 56412521 DOUBLER DOUG DC8 DC871F 302199D WP LT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, LT WING L/E INNER DOUBLER AROUND SMALL LWR SWING DOWN PANEL UNDER I/B FIRE BOTTLE CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5641252. 2 L 7 4 4F RT 4A25 1998110600359 19981106 00359 WP 1998 11 6 UPS98828028 1 19981016 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 70 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING UPPER SKIN STA XRS 70 AT STRINGER 16 HAS A STRESS CORROSION CRACK. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998110600360 19981106 00360 WP 1998 11 6 UPS98828029 1 19981014 A 5320 36169481 FITTING DOUG DC8 DC871F 302199D WP BS 700 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, CRACKED FITTING FS 700 AT UPPER CUSP IN MAIN CABIN LT. REMOVED AND REPLACED FITTING IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998110600361 19981106 00361 WP 1998 11 6 UPS98828030 1 19981013 A 5240 SKIN DOUG DC8 DC871F 302199D WP SERVICE DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, AFT SERVICE DOOR NR 17 FWD LWR CORNER CRACK ON INNER SKIN FROM EDGE TO FASTENER .625 INCH LONG. REPA IRED IAW UPS EO DC8-5330-10839-A. 2 L 7 4 4F RT 4A25 1998110600362 19981106 00362 WP 1998 11 6 UPS98828031 1 19981011 A 5751 5705334202 SKIN DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, THE RT I/B AILERON UPPER L/E SKIN AT THE ACTUATOR IS CRACKED AT ONE SCREW HOLE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-1-21 AND DWG 5705334. 2 L 7 4 4F RT 4A25 1998110600363 19981106 00363 WP 1998 11 6 UPS98828032 1 19981011 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING L/E SKIN INTERNAL DOUBLER AT THE NR 3 PYLON CUTOUT IS CRACKED AT THE OPENING. REPAIRED IAW S RM 57-2-1. 2 L 7 4 4F RT 4A25 1998110600364 19981106 00364 WP 1998 11 6 UPS98828037 1 19981014 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, STA 680 LWR PRESS WEB AT LBL 29 IS CRACKED. REPAIRED AREA IAW SRM 53-2-5. 2 L 7 4 4F RT 4A25 1998110600365 19981106 00365 WP 1998 11 6 UPS98828038 1 19981013 A 5320 9755536501N FITTING DOUG DC8 DC871F 302199D WP BS 1280 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, STA 1280 AT STR 21L, THE FRAME TO CUSP LWR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9755536 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998110600366 19981106 00366 WP 1998 11 6 UPS98828039 1 19981013 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 290 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, STA 290 AT STR 35L O/B LEG IS CRACKED. REPAIRED AREA IAW SRM 53-2-2 FIG 10. 2 L 7 4 4F RT 4A25 1998110600367 19981106 00367 WP 1998 11 6 UPS98828041 1 19981018 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 428 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, RT WING LWR SKIN AT STA XRS 428 AND BETWEEN STR 62 TO 64 IS CRACKED. REPAIRED AREA IAW DHC SK 729-23 7. 2 L 7 4 4F RT 4A25 1998110600368 19981106 00368 WP 1998 11 6 UPS98828042 1 19981013 A 5320 97540242 FITTING DOUG DC8 DC871F 302199D WP BS 1220 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, STA 1220 RT SIDE, THE FLOORBEAM SUPPORT FITTING HAS A 5 INCH CRACK. REMOVED AND REPLACED FITTING IAW DWG 9754024 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998110600369 19981106 00369 WP 1998 11 6 UPS98828043 1 19981013 A 5320 9755584508 FITTING DOUG DC8 DC871F 302199D WP BS 1396 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, STA 1396 AT STR 21L, THE FRAME TIE FITTING HAS A 9 INCH CRACK. REMOVED, FABRICATED AND REPLACED FITT ING IAW DWG 9755584. 2 L 7 4 4F RT 4A25 1998110600370 19981106 00370 WP 1998 11 6 UPS98828048 1 19981101 A 5320 FITTING DOUG DC8 DC873F 302199F WP FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 DURING AS/E INSP NOTED SUSPECTED CORROSION ABOVE MLG I/B TORQUE TUBE RT SIDE. UPON FURTHER INSP FOUND CORRISION AT MATI NG SURFACE OF 3 ATTACH FITTINGS OF I/B LONG 24 ABOVE MLG. RELEASED FOR FERRY FLIGHT TO SAT FOR REPAIR. 2 L 7 4 4F RT 4A25 1998110600371 19981106 00371 1998 11 6 UPS98828050 4 19981102 A 2565 CONTAINER DOUG DC8 DC873F 302199F WP ESCAPE SLIDE DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 840UP 46140 INSPECTION TYPE-N/A, ESCAPE SLIDE KEEPS FALLING OUT OF ITS CONTAINER. INSTALLED NEW CONTAINER AS REQUIRED, ESCAPE AND G RIP BAR OPS NORMAL. 2 L 7 4 4F RT 4A25 1998110600372 19981106 00372 EU 1998 11 6 QXEA9800530 1 19980414 A 2150 2046002 PACK FOKKER F28 F28MK4000 4990810 EU CABIN SMOKING A QXEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 NM 09 482US 4325 11231 FLIGHT ATTENDANT REPORTED SMOKE AND HAZY CONDITIONS IN CABIN AND LAV SMOKE DETECTOR ACTIVATED. TURNED BOTH PACKS OFF AN D RETURNED TO GEG. MAINTENANCE ISOLATED PROBLEM TO CABIN PACK. DEFERRED PER MEL 21-1. AIRCRAFT RELEASED FOR TEST FLIG HT, TEST FLIGHT SATISFACTORY. ON 980416 CLEARED MEL BY REMOVING AND REPLACING THE CABIN REFRIGERATION UNIT. GROUND RAN AIRCRAFT AT HIGH POWER, CABIN PACK FULL HOT THEN FULL COLD, 10 MINUTS ON EACH SETTING. NO SMOKE NOTED. 2 L 7 2 4F RT A20EU 1998110600373 19981106 00373 EU 1998 11 6 QXEA9801542 1 19981029 A 3350 1312 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 13 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 490US 11152 FIVE VOLT CEILING EMERGENCY EXIT LIGHTS OUT AT ROW 13. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998110600374 19981106 00374 EU 1998 11 6 QXEA9801543 1 19981101 A 3397 WIRE GRIMES FOKKER F28 F28MK4000 4990810 EU SEAT 4B BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 EMERGENCY EXIT LIGHT AT SEAT 4B BASE IS INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT BASE OF SEAT. OPERATIONAL CHE CK IS NORMAL. 2 L 7 2 4F RT A20EU 1998110600375 19981106 00375 EU 1998 11 6 QXEA9801544 1 19981101 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU SEAT 8E FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 493US 11161 EMERGENCY OVERWING EXIT LIGHT AT SEAT 8E IS VERY DIM. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998110600376 19981106 00376 EU 1998 11 6 QXEA9801545 1 19981029 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 LEFT FORWARD EMERGENCY EXIT 28 VOLT LIGHT IS BURNT OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998110600377 19981106 00377 EU 1998 11 6 QXEA9801546 1 19981031 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 499US 11182 EMERGENCY EXIT SIGN AT ROW 8 IS OUT. MAINTENANCE RELAMPED, OPERATIONAL TEST NORMAL. 2 L 7 2 4F RT A20EU 1998110600378 19981106 00378 WP 1998 11 6 ABXA9800929 1 19981029 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816AX 46093 DURING PRE-DEPARTURE CHECK, FOUND THE EMERGENCY DISARM LIGHT NOT ON IN THE DISARM MODE. REPLACED THE EMERGENCY BATTERY LIGHT RACK. 2 L 7 4 4F 4A25 1998110600379 19981106 00379 WP 1998 11 6 ABXA9800930 1 19981028 A 3260 45973405505 UPLATCH MECH DOUG DC8 DC861 3021952 WP RT MLG LACK OF LUBE A ABXA O OTHER N FALSE WARNING TO TAKEOFF 1 GL 23 844AX 45848 AFTER TAKEOFF WITH GEAR HANDLE UP, THE LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED, ALONG WITH THE RIGHT GEAR DOOR LA TCH LIGHT. RECYCLED LANDING GEAR, NO HELP. CLEANED AND LUBRICATED RIGHT MAIN LANDING GEAR UPLATCH MECHANISM. 2 L 7 4 4F 4A25 1998110600380 19981106 00380 WP 1998 11 6 MWEA981020 1 19981031 A 5511 5918000516 SPAR DOUG DC9 DC915 3022036 WP RT HORIZ STAB CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FOUND RIGHT HORIZONTAL STAB REAR SPAR FORWARD FACE CRACKED AT THE OUTBOARD END. MTC REMOVED DAMAGED AREA, FABRICATED RE PAIR WEB DOUBLERS, ANGLES AND FILLERS. 2 L 7 2 4F A6WE 1998110600381 19981106 00381 WP 1998 11 6 MWEA981021 1 19980907 A 5313 76378133 LONGERON DOUG DC9 DC915 3022036 WP BS 544 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN STATION 544 LONGERON L7L IS CRACKED. MTC REMOVED CRACKED LONGERON SECTION AND TWO SPLICES. 2 L 7 2 4F A6WE 1998110600382 19981106 00382 WP 1998 11 6 MWEA981022 1 19981031 A 5320 4912798501N END CAP DOUG DC9 DC915 3022036 WP BS 759 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LOWER AFT CARGO COMPARTMENT RT L22R END CAP AT STA 759 HAS CORROSION. MTC REMOVED CORROSION AND INSTALLED NEW END CAP. 2 L 7 2 4F A6WE 1998110600383 19981106 00383 WP 1998 11 6 MWEA981023 1 19980907 A 5315 232999 FLOORBEAM DOUG DC9 DC915 3022036 WP BS 817 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN STATION 817 XT18 FLOORBEAM SCREW HOLES ELONGATED AND HAVE CORROSION. MTC CUT OUT DAMAGED AND CORRODED AREAS AND FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 1998110600384 19981106 00384 WP 1998 11 6 MWEA981024 1 19980915 A 5330 59114241 SKIN DOUG DC9 DC915 3022036 WP BS 460 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 PLATING UNDER LONGERON 22R AT STATION 760 CORRODED. MTC REMOVED CORROSION, FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998110600385 19981106 00385 WP 1998 11 6 MWEA981025 1 19980912 A 5320 9915545507 CUSP DOUG DC9 DC915 3022036 WP BS 332-351 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN STATION 332 351 RIGHT CUSP MEMBRANE AT LONG 18R CORRODED BULGING AND CRACKED. MTC REMOVED CORROSION, FABRICA TED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998110600386 19981106 00386 WP 1998 11 6 MWEA981026 1 19981031 A 5320 4912798501 CAP DOUG DC9 DC915 3022036 WP BS 759 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LOWER AFT CARGO COMPARTMENT RIGHT L22R END CAP AT STATION 759 HAS CORROSION. MTC REMOVED CORROSION AND INSTALLED NEW EN D CAP. 2 L 7 2 4F A6WE 1998110600387 19981106 00387 WP 1998 11 6 MWEA981027 1 19981028 A 5330 99234883 SKIN DOUG DC9 DC932 3022066 WP BS 579 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 FOUND CORROSION ON INTERIOR SKIN AT FS 579 BETWEEN LONGERON 29R AND 30R. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998110600388 19981106 00388 WP 1998 11 6 MWEA981028 1 19981028 A 5330 5911412191 SKIN DOUG DC9 DC932 3022066 WP BS 565 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 202ME 47672 PREVIOUS REPAIR ON FORWARD CARGO BELLY SKIN AT STATION 565 DOES NOT MEET SRM REQUIREMENTS. MTC FABRICATED AND INSTALLED SKIN SPLICE REPAIR. 2 L 7 2 4F A6WE 1998110600389 19981106 00389 WP 1998 11 6 ARWA981101 1 19981102 A 2923 57155A PUMP DOUG DC8 DC863F 302198F WP AUX HYD SYST INOP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 AFTER LOADING WHILE CLOSING MAIN CARGO DOOR, AUXILIARY PUMP (HYD) BLEW CURRENT LIMITERS SEVERAL TIMES. REMOVED AND REPL ACED AUX PUMP IAW DC-8 M/M 29-20-2. NO PRESS PRODUCED, SWAPPED REV PUMP AND AUX PUMP IAW DC-8 M/M 29-20-2, OPS CHECK GO OD. 2 L 7 4 4F 4A25 1998110600390 19981106 00390 EA 1998 11 6 VTZA98287 1 19980908 A 5270 864202 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 627BR 7233 FLT 6771 - IAD-GSP - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATE D. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED ADJUSTED PASSENGER DOOR PROXIMITY SENSOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998110600391 19981106 00391 EA 1998 11 6 VTZA98283 1 19980905 A 3620 SWITCH CNDAIR CL600 CL6002B19 EA RT ENGINE LOOSE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 625BR 7214 FLT 6715 - IAD-ATL - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGNE 10TH STAGE SOV WOULD NOT OPEN. A IRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESECURED LOOSE CONNECTOR ON LIGHT SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998110600392 19981106 00392 EU 1998 11 6 VTZA98294 1 19980918 A 3260 14176003423 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 315UE 41033 FLT 6435 - IAD-RDU - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WARNING STAYED ON FOR 10 SECONDS A FTER TAKEOFF. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED RT POWER LEVER MI CROSWITCH AND PERFORMED FUNCTION CHECK. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998110600393 19981106 00393 EU 1998 11 6 VTZA9300 1 19980924 A 7930 1241013 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU ENGINE OIL MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 471UE 821 FLT 6540 - IAD-BDL - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT OIL PRESSURE FLUCTUATION HIGH OFF SCA LE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT OIL PRESSURE TRANSDUCER. MAINTENANCE GROUND RAN AIRCRAFT, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998110600394 19981106 00394 1998 11 6 VTZA98301 4 19980927 A 3442 7007700301 TRANSCEIVER JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 327UE 41080 FLT 6454 - IAD-DTW - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO WEATHER RADAR WOULD NOT REMAIN ON A SELE CTED RANGE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED WEATHER RADAR SCREEN, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1998110600395 19981106 00395 EU 1998 11 6 VTZA98296 1 19980920 A 3240 S214161K INDICATOR BAG JETSTM JETSTM3201 1500217 EU RT BRAKE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 490UE 909 FLT 6282 - IAD-HPN - DURING CRUISE, AIRCRAFT DIVERTED TO JFK DUE TO RIGHT BRAKE PSI WENT TO ZERO. AFTER LANDING BRAKE P RESSURE WAS NORMAL. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 51048, MEL 32 -1, ON GAUGE. MAINTENANCE CLOSED DMI 51-48 ON 9-22-98 BY REMOVING AND REPLACING BRAKE INDICATOR AND TRANSMITTER. OPS C HECK OK, AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998110600396 19981106 00396 EU 1998 11 6 98ZZZM808 1 19980920 A 3240 S1226142 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU RT BRAKE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 490UE 909 FLT 6282 - IAD-HPN - DURING CRUISE, AIRCRAFT DIVERTED TO JFK DUE TO RIGHT BRAKE PSI WENT TO ZERO. AFTER LANDING BRAKE P RESSURE WAS NORMAL. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 51048, MEL 32 -1, ON GAUGE. MAINTENANCE CLOSED DMI 51-48 ON 9-22-98 BY REMOVING AND REPLACING BRAKE INDICATOR AND TRANSMITTER. OPS C HECK OK, AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998110600397 19981106 00397 NM 1998 11 6 TSAA9833539 1 19981002 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998110600398 19981106 00398 NM 1998 11 6 TSAA9833538 1 19981002 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 6 EMERGENCY GROUND PROXIMITY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1998110600399 19981106 00399 NM 1998 11 6 TSAA9833537 1 19981002 A 3350 86210066 BATTERY PACK BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED NR 5 EMERGENCY GROUND PROXIMITY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4U RT A16WE 1998110600400 19981106 00400 NM 1998 11 6 TSAA9833536 1 19981002 A 3350 8731002511 LIGHT BOEING 737 737209 NM AFT ENTRY INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED AFT ENTRY EMERGENCY EXIT IDENTIFIER LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998110600401 19981106 00401 NM 1998 11 6 TSAA9833535 1 19981002 A 3350 1000679 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED THE INTERIOR OVERWING EMERGENCY LIGHT BATTERY DUE TO LOW VOLTAGE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1998110600402 19981106 00402 NM 1998 11 6 TSAA9833553 1 19981011 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 3 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1998110600403 19981106 00403 NM 1998 11 6 TSAA9833552 1 19981011 A 3350 8731002511 LIGHT BOEING 737 737230 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998110600404 19981106 00404 NM 1998 11 6 TSAA9833551 1 19981011 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 1 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998110600405 19981106 00405 NM 1998 11 6 SABA980047 1 19980923 A 3240 82970010217 LINE DHAV DHC8 DHC8102 2809003 NM LT MLG WW CRACKED A SABA O OTHER K FLUID LOSS LD LANDING 1 SO 33 883CC 162 FLT 5010 - SOP-CLT - PILOT LOST NR 1 HYD PRESSURE. PRESSURE WAS A SLOW BLEED DOWN. ON APPROACH FOR LANDING THE PILOT W AS LOOKING FOR POSSIBLE NO BRAKES. NO INFLIGHT EMERGENCY WAS DECLARED. AFTER LANDING AT CLT, THE AIRCRAFT LOST BRAKES AT TAXI WAY C-11. PASSENGERS TRANSPORTED BY BUS TO GATE. AIRCRAFT TOWED AWAY. MAINTENANCE FOUND HYD LINE BETWEEN NR 1 AND NR 2 BRAKE VALVES, IN THE LEFT WHEEL WELL LEAKING. REMOVED AND REPLACED HYD LINE. SERVICED, BLEED AND OPS CHECKED SYSTEM. SYSTEM CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE, P/N 82970010-217. (M) 2 H 7 2 4T RT A13NM 1998110600406 19981106 00406 1998 11 6 SABA980048 4 19980928 A 3442 WX RADAR DHAV DHC8 DHC8102 2809003 NM COCKPIT MALFUNCTIONED A SABA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 33 817PH 56 CLT - FLT 5069 - RADAR DOES NOT FUNCTION PROPERLY. WILL NOT PAINT WX. AIRCRAFT RETURNED CLT. NO INFLIGHT EMERGENCY DE CLARED. AIRCRAFT LANDED CLT NO OTHER DISCREPANCIES REPORTED. PERFORMED FUNCTIONAL CHECK OF WX RADAR SYSTEM. OPS CHECK ED GOOD IAW DHC-8 MM ATA 34-41. (M) 2 H 7 2 4T RT A13NM 1998110600407 19981106 00407 NM 1998 11 6 SABA980049 1 19981003 A 7921 28E996 OIL COOLER DHAV DHC8 DHC8102 2809003 NM RT ENGINE CRACKED A SABA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 SO 33 818PH 12880820 58 GNV - FLT 5069 - RIGHT ENGINE OIL PRESSURE BELOW 55 PSI FEATHERED PROP AND OIL PRESSURE HELD AT 40 PSI 10 MIN LATER IT F ELL TO 30 PSI INFLIGHT SHUTDOWN OF RIGHT ENGINE. INFLIGHT EMERGENCY DECLARED. AIRCRAFT LANDED NO INCIDENTS. FOUND ENG INE OIL COOLER LEAKING. REPLACED OIL COOLER IAW DHC-8 MM ATA 72-10. OPERATIONAL LEAK CHECKED OK. (M) 2 H 7 2 4T RT A13NM 1998110600408 19981106 00408 NM 1998 11 6 AALA981822 1 19980927 A 3350 8330244022 LIGHT BOEING 767 767223 1385123 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 317AA 406 22319 SFO - EMERGENCY SEAT LIGHT AT SEAT 30 H/J INOPERATIVE. REPLACED SEAT 30H/J. SYSTEM GROUND CHECKED NORMAL OPERATION. ( M) 2 L 7 2 4F RT A1NM 1998110600409 19981106 00409 NM 1998 11 6 AALA981712 1 19980921 A 2612 233N62037 CONTROL PANEL BOEING 767 767223 1385123 NM E/E BAY FAILED A AALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 325AA 22326 DTW - FLT 24 - EN ROUTE ORD-BHX, AFT CARTO FIRE LIGHT ILLUMINATED. NO FIRE, AIR INTERRUPTED AND LANDED DTW WITHOUT INCI DENT. REPLACED APU/CARGO FIRE CONTROL PANEL. ACCOMPLISHED TEST OF SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M ) 2 L 7 2 4F RT A1NM 1998110600410 19981106 00410 WP 1998 11 6 AALA981832 1 19980928 A 3350 1003695 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 298AA 49310 ORD - FLT DURING OVERNIGHT CHECK, LEFT EXTERNAL OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LEFT EXTERNAL OVERWING EM ERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600411 19981106 00411 WP 1998 11 6 AALA981725 1 19980926 A 3350 LIGHT DOUG DC9 DC982 3022082 WP COCKPIT INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 426AA 49338 DFW - DURING OVERNIGHT CHECK, EMERGENCY LIGHT IN COCKPIT INOPERATIVE. SECURED GROUND ON EMERGENCY LIGHT IN COCKPIT. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600412 19981106 00412 WP 1998 11 6 AALA981717 1 19980923 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 478AA 49653 TUS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM ROW 7 THROUGH 17 INOPERATIVE. REPLACED EMER GENCY EXIT FLOOR PATH LIGHT STRIP FROM ROW 7 THROUGH 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600413 19981106 00413 WP 1998 11 6 AALA981715 1 19980922 A 3350 0200333001 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 438AA 49456 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT ABOVE AFT STAIR DOOR INOPERATIVE. RECONNECTED QUICK DISCONNECT ON EM ERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998110600414 19981106 00414 1998 11 6 AALA981837 4 19980929 A 2565 D31021107 SLIDE AIRCRUISERS AIRBUS 300 A300B4605R 3930308 EU PAX DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 25071 O238 514 JFK - DURING OVERNIGHT MAINTENANCE, CHECK OF L3 DOOR SLIDE DEPLOYMENT WAS UNSUCCESSFUL. REPLACED L3 DOOR SLIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998110600415 19981106 00415 WP 1998 11 6 AALA981716 1 19980922 A 3610 12J82350 CLAMP DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 417AA 49328 ORD - FLT 785 - EN ROUTE ORD - AUS CLIMBING THROUGH 500 FEET, THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH RIGHT PACK TURNED OFF. AIR INTERRUPTED AND RETURNED TO ORD. LANDED WITHOUT INCIDENT. FLIGHT ATTENDANT REPORTED THAT A PASSENGER NOTED A BURNING SMELL IN THE CABIN. SEEMED TO DISSIPATE WHEN THE RIGHT PACK WAS LEF T OFF. REPLACED RIGHT AUGMENTATION VALVE INBOARD CLAMP PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600416 19981106 00416 WP 1998 11 6 AALA981726 1 19980926 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY CONTAMINATED A AALA K NONE B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 16545 53027 BNA - FLT 1133 - DURING INITIAL CLIMB-OUT FROM LGA, LEAVING 500 FT, CREW NOTED STRONG FUMES/ODOR IN COCKPIT AND FORWARD CABIN. ACCOMPLISHED AIR CONDITIONING SMOKE/FUMES EMERGENCY CHECKLIST. TURNED LEFT AIR CONDITIONING SUPPLY SWITCH OFF. PULLED RECIRCULATING FAN CONTROL CIRCUIT BREAKER (J-7). CONTINUED ON AND LANDED BNA WITHOUT INCIDENT. REPLACED BOTH C OALESCER BAGS IN AIR CONDITIONING SYSTEM. ACCOMPLISHED PACK BURN OUT PROCEDURES PER MM. NO FUMES OR ODOR NOTED AFTER B AGS WERE CHANGED. NO RESIDUE IN COALESCER BAGS. RESET CIRCUIT BREAKER J-7 FOR RECIRCULATING FAN CONTROL. SYSTEM GROUN D CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600417 19981106 00417 WP 1998 11 6 AALA981819 1 19980924 A 7830 LINE DOUG DC9 DC982 3022082 WP THRUST REVERSER LOOSE A AALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 461AA 49566 DFW - FLT 739 - EN ROUTE LGA-DFW - RIGHT HYDRAULIC SYSTEM QUANTITY LOST ALL FLUID INDICATION WITH ASSOCIATED ZERO HYDRAU LIC PRESSURE ON RIGHT SIDE. LANDED DFW WITH LANDING GEAR DOORS OPEN. DOORS MADE CONTACT WITH RUNWAY. REPLACED RIGHT L ANDING PAD ON DOOR. TIGHTENED RIGHT THRUST REVERSER HYDRAULIC PRESSURE LINE AT ENGINE PYLON. SYSTEM GROUND CHECKED NOR MAL OPERATION. (M) 2 L 7 2 4F A6WE 1998110600418 19981106 00418 WP 1998 11 6 AALA981839 1 19981003 A 3150 CONNECTOR DOUG DC9 DC983 3022083 WP TAIL COMPARTMENT LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 570AA 49352 ORD - DURING OVERNIGHT MAINTENANCE, WARNING LIGHT ON OVERHEAD PANEL IN COCKPIT FAILED TO ILLUMINATE DURING TAIL CONE JET TISION CHECK. RESEATED CONNECTORS ON TAIL CONE SWITCHES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998110600419 19981106 00419 WP 1998 11 6 AALA981854 1 19981005 A 2170 WATER SEPARATOR DOUG DC9 DC983 3022083 WP A/C BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 562AA 49344 DFW - FLT 1737 - AFTER TAKEOFF DFW AT APPROXIMATELY 5000 FT, AN ACRID SMELL WAS DETECTED IN COCKPIT AND FIRST CLASS. CH ECKING CIRCUIT BREAKERS A HAZE WAS NOTICED IN AIR. AIRCRAFT AIR INTERRUPTED AND RETURNED TO DFW AND LANDED WITHOUT INCI DENT. INSPECTED AIRCRAFT FOR SOURCE OF SMELL, CHECKED ALL CIRCUIT BREAKERS FOR ARCING, CHECKED BALLASTS IN CABIN, CHECK ED OVENS FOR BURNING SMELL, RAN BOTH PACKS WITH APU AND ENGINES AT VARIOUS POWER SETTINGS. NO DISCREPANCIES NOTED, CHAN GED WATER SEPARATOR BAGS, ALL SYSTEM OPERATIONS CHECK SATISFACTORY, AIRCRAFT OK FOR SERVICE AT THIS TIME. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998110600420 19981106 00420 SO 1998 11 6 C2XA98CL063 1 19980812 A 7540 1103P273 SWITCH EMB 120 EMB120RT SO LT ENGINE LEAKING A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 16731 120190 CLE - FLT 4399 - CREW REPORTED THAT AFTER TAKEOFF THE LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED SEVERAL COMPONENTS INCLUDING THE ALARM LIGHT CONTROLLER, HP BLEED VALVE, AND SHUTOFF VALVE. THE AIRCRAFT FAIL ED TEST FLIGHT, THE DE-ICE PRESS SWITCH WAS REMOVED AND REPLACED IAW EMB-120 MM 36-10-00, OPERATIONAL AND LEAK CHECKS WE RE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600421 19981106 00421 WP 1998 11 6 USAAD98177 1 19981010 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP FUSELAGE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 971VJ 47051 IND - THE TAILCONE SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT BATTERY AND THE BULBS. (M) 2 L 7 2 4F A6WE 1998110600422 19981106 00422 WP 1998 11 6 USAAD98184 1 19981010 A 3350 9721055 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 818US 48098 PHL - THE FORWARD LOW LEVEL EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE FORWARD LOW LEVEL EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998110600423 19981106 00423 NM 1998 11 6 USAASB98270 1 19981013 A 3350 900835A BATTERY PACK BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 263AU 22869 CLT - FLT 765 - DURING CRUISE, PILOT REPORTED THE EMERGENCY FLOOR TRACK LIGHTING ILLUMINATED WITH THE SWITCH IN THE ARME D POSITION. MAINTENANCE REMOVED AND REPLACED THE FORWARD AND AFT OVERHEAD BATTERY PACKS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998110600424 19981106 00424 NM 1998 11 6 USAASB98271 1 19981014 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 BWI - MAINTENANCE FOUND THE AFT OVERHEAD CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTER Y PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998110600425 19981106 00425 NM 1998 11 6 USAASB98269 1 19981013 A 3350 081691 SOCKET BOEING 737 7373B7 1384580 NM ROW 22 FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 510AU 23385 PIT - MAINTENANCE FOUND THE EMERGENCY FLOOR TRACK LIGHTING AT SEAT ROW 22 INOP. MAINTENANCE REMOVED AND REPLACED THE LI GHT SOCKET AT SEAT ROW 22 FLOOR TRACK LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998110600426 19981106 00426 NM 1998 11 6 USAASB98268 1 19981011 A 3397 WIRE BOEING 737 7373B7 1384580 NM ROW 18 BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 507AU 23382 BWI - MAINTENANCE FOUND THE EMERGENCY EXIT FLOOR TRACK LIGHTS INOP FROM SEAT ROW 18 TO THE REAR OF THE AIRCRAFT. MAINTE NANCE REPAIRED BROKEN WIRE AT SEAT ROW 18 FLOOR TRACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998110600427 19981106 00427 WP 1998 11 6 USAAD98173 1 19980929 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 922VJ 48142 DTW - THE AFT OVERHEAD EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998110600428 19981106 00428 WP 1998 11 6 USAAD98175 1 19981007 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 965VJ 47374 IND - THE SERVICE DOOR SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE SERVICE DOOR SLIDE EMERGENCY LIG HT BATTERY. (M) 2 L 7 2 4F A6WE 1998110600429 19981106 00429 EU 1998 11 6 UF6A981001 1 19981001 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 6996 16357 2021 SBN - FLT 5757 - OVERWING EMERGENCY EXIT SIGNS AND FLOOR STRIP (ROW 6) LIGHTS DO NOT TEST. MAINTENANCE REMOVED AND REPL ACED NR 3 POWER SUPPLY. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998110600430 19981106 00430 EU 1998 11 6 UF6A980906 1 19980917 A 3350 P4010021 BATTERY BAG ATP ATP EU CABIN DISCHARGED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 857AW 2034 ORD - FLT 5743 - LED NOT BLINKING ON FLIGHT ATTENDANTS 'B' FLASHLIGHT. MAINTENANCE REMOVED AND REPLACED THE BATTERY. S YSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T RT A27NM 1998110600431 19981106 00431 EU 1998 11 6 UF6A980909 1 19980920 A 3350 1317 BULB BAG ATP ATP EU BS 198 FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FLT 5729 - OVERHEAD CABIN EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED BULB. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1998110600432 19981106 00432 EU 1998 11 6 UF6A980810 1 19980823 A 3350 6013211 POWER SUPPLY BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 852AW 2021 ORD - UPON DAILY INSPECTION, FOUND NR 7 BATTERY PACK FOR EMERGENCY EXIT LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED N R 7 EMERGENCY LIGHT POWER SUPPLY. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1998110600433 19981106 00433 EU 1998 11 6 SIMA982858 1 19981012 A 5320 S5367121729402 WEB AEROSP ATR72 ATR72212 EU BS 36-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 ABI - SEAT TRACK, FLOOR SUPPORT WEBS AND ENTRY FLOORBEAMS ARE CORRODED BETWEEN FRAMES 36 AND 39. REMOVED AND REPLACED S EAT TRACK, WEBS AND FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600434 19981106 00434 EU 1998 11 6 98ZZZM809 1 19981012 A 5347 EPN5300013019 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 36-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 ABI - SEAT TRACK, FLOOR SUPPORT WEBS AND ENTRY FLOORBEAMS ARE CORRODED BETWEEN FRAMES 36 AND 39. REMOVED AND REPLACED S EAT TRACK, WEBS AND FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600435 19981106 00435 EU 1998 11 6 98ZZZM810 1 19981012 A 5315 S5367240620802 FLOORBEAM AEROSP ATR72 ATR72212 EU BS 36-39 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 ABI - SEAT TRACK, FLOOR SUPPORT WEBS AND ENTRY FLOORBEAMS ARE CORRODED BETWEEN FRAMES 36 AND 39. REMOVED AND REPLACED S EAT TRACK, WEBS AND FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600436 19981106 00436 EU 1998 11 6 SIMA982857 1 19981012 A 5347 S5367800121002 SEAT TRACK AEROSP ATR72 ATR72212 EU BS 23-29 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 ABI - SEAT TRACK BETWEEN FRAMES 29 AND 35, AND BETWEEN FRAMES 23 TO 29 ARE CORRODED. REMOVED AND REPLACED SEAT TRACKS. (M) 2 H 7 2 4T RT A53EU 1998110600437 19981106 00437 EU 1998 11 6 SIMA982854 1 19981012 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU SEAT 6-7-10 INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 313AE 18534 340B313 OKC - FLT 5060 - FOUND EMERGENCY EXIT FLOOR PROXIMITY LIGHTS AT SEATS 6, 7 AND 10, AND OVERHEAD LIGHTS AT SEAT 7 AND 8 D O NOT ILLUMINATE. REMOVED AND REPLACED AFT EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998110600438 19981106 00438 EU 1998 11 6 SIMA982851 1 19981012 A 3350 1317 BULB SAAB SF340 340B 7860101 EU SEAT 8A FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 280AE 340B280 DFW - FLT 5166 - FOUND EMERGENCY LIGHT AT SEAT 8A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GO OD. (M) 2 L 7 2 4T RT A52EU 1998110600439 19981106 00439 EU 1998 11 6 SIMA98281 1 19981008 A 3350 3011210 BULB AEROSP ATR72 ATR72212 EU PAX DOOR FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 407AT 407 MIA - FLT 5700 - FOUND EMERGENCY LIGHT AT PAX DOOR STATION DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998110600440 19981106 00440 EU 1998 11 6 SIMA982692 1 19980926 A 3350 6839 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 394AE 340B394 DFW - FLT 3558 - FOUND EMERGENCY ARM LIGHT ON FLIGHT ATTENDANT CONTROL PANEL DOES NOT ILLUMINATE. REMOVED AND REPLACED ARM LIGHT BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998110600441 19981106 00441 EU 1998 11 6 SIMA982664 1 19980923 A 3350 AB3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 233RM 13061 235 ORD - FLT 4194 - FOUND FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998110600442 19981106 00442 SO 1998 11 6 SIMA982572 1 19980914 A 2611 W1911817 WIRE EMB 145 EMB145LR SO CARGO BAY LOOSE A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 602AE 145048 MKE - FLT 4300 - CARGO SMOKE INDICATION ILLUMINATED ON APPROACH. ACTIVATED FIRE EXTINGUISHERS. VERIFIED EVENT AS A FAL SE WARNING. REMOVED AND REPLACED BOTH HIGH AND LOW PRESSURE FIRE EXTINGUISHERS. PULLED BAGGAGE SMOKE DETECTOR CIRCUIT BREAKER AND COLLZRED PER EMBRAER LETTER REF SST 1639/98. ITEM IS DEFERRED. FOUND WIRE GOING TO PIN 7 WAS HELF IN BY ON LY TWO STRANDS. REPAIRED WIRE WITH SPARE CONNECTOR AT PIN 15. OPERATIONAL CHECK GOOD. MEL CLEARED. (M) 2 L 7 2 4T RT T00011AT 1998110600443 19981106 00443 EU 1998 11 6 REXA98112 1 19981002 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A REXA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 360PX A1605 340B220 CARGO SMOKE DETECTOR ILLUMINATED AFTER TAKEOFF. MEGOHMED ALL ASSOCIATED WIRING AND COMPONENT CONNECTORS, REMOVED AND RE PLACED WEU, REMOVED AND REPLACED CARGO SMOKE DETECTOR. (M) 2 L 7 2 4T RT A52EU 1998110600444 19981106 00444 EU 1998 11 6 REXA98111 1 19980930 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 360PX 340B220 CARGO SMOKE LIGHT CAME ON IN FLIGHT. CARGO SMOKE DETECTION SYSTEM OPS CHECKED IAW AMM 26-13-00. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998110600445 19981106 00445 EU 1998 11 6 REXA98109 1 19980922 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A REXA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 360PX 340B220 CARGO SMOKE LIGHT COMES ON INTERMITTENTLY. REMOVED AND REPLACED AFT OVERHEAD CARGO SMOKE DETECTOR. (M) 2 L 7 2 4T RT A52EU 1998110600446 19981106 00446 SW 1998 11 6 98ZZZM811 1 19981003 A 6120 31030952 SENSOR ORIFICE SWRNGN SA227 SA227AC 8780603 SW LT ENGINE FAILED A MEJA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 17 358AE AC688 WHILE EN ROUTE FROM JAN TO CVG, THE LEFT ENGINE INDICATED LOW OIL PRESSURE AND THE OIL PRESSURE LIGHT CAME ON. THE PILO T DECLARED AN EMERGENCY AND SHUT DOWN THE LEFT ENGINE. THE AIRCRAFT DIVERTED TO BWG AND LANDED SINGLE ENGINE WITHOUT AN Y FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE NEGATIVE TORQUE SENSOR ORIFICE ASSEMBLY. LEAK CHE CK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998110600447 19981106 00447 SW 1998 11 6 98ZZZM812 1 19981005 A 3230 2752019011A HOOK SWRNGN SA227 SA227AC 8780603 SW NLG INOPERATIVE A MEJA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 17 438MA AC721B AFTER TAKEOFF FROM OPF, THE NOSE GEAR WOULD NOT RETRACT AND WAS BANGING AGAINST THE STOPS. THE CREW RECYCLED THE GEAR A FEW TIMES AND THE NOSE GEAR STILL WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO OPF WITHOUT FURTHER INCIDENT. MAINTENAN CE REMOVED AND REPLACED THE HOOK ASSEMBLY AND A BUSHING WITH NEW PARTS. GEAR SWING SATISFACTORY AND AIRCRAFT WAS RETURN ED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998110600448 19981106 00448 1998 11 6 DKAA98017 4 19981012 A 3414 INDICATOR AMD FALC20 FALCON20C5 2730107 EU COCKPIT INOPERATIVE A DKAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 23 810RA 81 REJECTED TAKEOFF, NR 1 AIRSPEED INDICATOR INOPERATIVE. REPAIRED BROKEN LINE AT NR 1 PITOT MAST. SYSTEM CHECKS GOOD IAW PART 43 APPENDIX 'E' PARAGRAPH 'A'. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A7EU 1998110600449 19981106 00449 EU 1998 11 6 DKAA98016 1 19981010 A 3230 CONNECTOR AMD FALC20 FALCOND 2720304 EU MLG DIRTY A DKAA O OTHER O OTHER AP APPROACH 1 GL 23 226R 226 SELECTED GEAR DOWN, DOORS OPENED BUT GEAR DID NOT EXTEND. WITH AIRCRAFT ON JACKS, CLEANED, INSPECTED AND OHMED LANDING GEAR DOOR DOWNLOCK CANNON PLUGS. EXTENDED AND RETRACTED LANDING GEAR 10 CYCLES. OPERATIONAL CHECKS GOOD. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F A7EU 1998110600450 19981106 00450 WP 1998 11 6 USAAD98176 1 19981007 A 3260 0080004003 CONTROL BOX DOUG DC9 DC931 3022065 WP E/E BAY FAILED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 918VJ 22345 48138 PIT - FLT 7900 - DURING MAINTENANCE TEST HOP THE NOSE LANDING GEAR GREEN LIGHT WOULD NOT ILLUMINATED DURING FLIGHT WITH ANY GEAR EXTENSION METHOD, NORMAL OR NON NORMAL. THE NOSE GEAR WAS VERIFIED DOWN AND LOCKED USING THE NOSE GEAR VIEWPOR T. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SENSOR CONTROL BOX. (M) 2 L 7 2 4F A6WE 1998110600451 19981106 00451 1998 11 6 USAAD98178 4 19981010 A 2297 WIRE DOUG DC9 DC931 3022065 WP YAW DAMPER BROKEN A A USAA A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 EA 19 991VJ 47310 IAD-BOS - FLT 1682 - DURING CRUISE, THE FELT AN UNCOMMANDED YAW FROM THE RUDDER. THE PROBLEM CONTINUED AFTER COMPLETING THE ABNORMAL PROCEDURES FOR AN UNCOMMANDED YAW. THE AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE WIRE TO PIN 'V' OF THE YAW DAMPER ACTUATOR BROKEN THREE FEET FROM THE ACTUATOR. THE BREAK WOULD INTERMITTENT LY MAKE CONTACT CAUSING FALSE ACTUATION OF THE ACTUATOR. (M) 2 L 7 2 4F A6WE 1998110600452 19981106 00452 EU 1998 11 6 USAAF98071 1 19980820 A 3150 WARNING SYSTEM FOKKER F28 F28MK0100 4990807 EU CABIN PRESS ACTIVATED A USAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 886US 11346 PIT - FLT 274 - EN ROUTE LGA-SDF, CREW RECEIVED THREE CHIME WARNING FROM THE MFDU AND NOTED THAT THE CABIN ALTITUDE WAS CLIMBING THROUGH 10,000 FT. CREW PERFORMED AN EMERGENCY DESCENT. THE FLIGHT DIVERTED TO PIT AND LANDED WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4F RT 1998110600453 19981106 00453 EU 1998 11 6 USAA980479 1 19980929 A 5320 591015793N DOOR PAN FOKKER F28 F28MK0100 4990807 EU CARGO BAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND .5 INCH CRACK AFT CARGO DOOR PAN AT PAN AFT EDGE BELOW LATCH CAM ARM. INSTALLED DOUBLER PE R SRM 52-05 FIG 35A. (M) 2 L 7 2 4F RT 1998110600454 19981106 00454 EU 1998 11 6 USAA980478 1 19980929 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3870-4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q-1 CHECK, FOUND 29.125 INCH LONG 740MM CORRODED T-CAP BEYOND LIMITS AT T-CAP AT BL 1127R STATION 3870-4610 . REPLACED T-CAP PER SRM CHAPTER 51. (M) 2 L 7 2 4F RT 1998110600455 19981106 00455 EU 1998 11 6 USAA980477 1 19980929 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3870-4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q-1 CHECK, FOUND 38.625 INCH 980 MM CORRODED BEAM CORRODED BEYOND LIMITS MED FLOOR THRESHOLD SUPPORT AT STA TION 3870-4850. REPLACED SUPPORT PER SRM CHAPTER 51. (M) 2 L 7 2 4F RT 1998110600456 19981106 00456 EU 1998 11 6 USAA980476 1 19980929 A 5320 1155011 BEAM FOKKER F28 F28MK0100 4990807 EU BS 5600-6600 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q-1 CHECK, FOUND HEAVY CORROSION ON BEAM 24 INCHES LONG AT VALET AREA BL 475 AT STATION 5600-6600. REMOVED AND REPLACED PER SRM 51-70-06. (M) 2 L 7 2 4F RT 1998110600457 19981106 00457 EU 1998 11 6 USAA980475 1 19980929 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3870-4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q-1 CHECK, FOUND CORRODED MATERIAL 29.125 INCH 740MM AT BL 1127L STATION 3870-4610 T-CAP CORRODED BEYOND LI MIT. REPLACED T-CAP PER SRM CHAPTER 51. (M) 2 L 7 2 4F RT 1998110600458 19981106 00458 EU 1998 11 6 USAA980474 1 19980929 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU BS 24011/24611 DISBONDED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q-1 CHECK, FOUND DISBONDING 1.5 INCH BY 1.5 INCH AT SEAT AND 16 INCH BY 4.5 INCH STRINGER AT STATION 24011 AND 24611 WITHIN STRINGERS 21A AND 23 ON SKIN. FILLED CAVITY WITH SEALANT AND APPLIED RIVETS TO DISBOND AREA, PER EA NR 29417E. (M) 2 L 7 2 4F RT 1998110600459 19981106 00459 EU 1998 11 6 USAAF98082 1 19981004 A 2530 500387D3 COFFEE MAKER FOKKER F28 F28MK0100 4990807 EU GALLEY OVERHEATED A USAA G O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 19 889US 11358 BWI - FLT 1192 - EN ROUTE TO BWI AT FL230, SMOKE SMELL ENTERED THE COCKPIT. CREW STATED THAT SMOKE WAS NOT VISIBLE AND FLIGHT ATTENDANTS ALSO SMELLED SMOKE AND COULD SEE IT COMING FROM ABOVE COFFEE MAKERS. THE FLIGHT CREW PULLED THE COFFE E MAKER CIRCUIT BREAKERS AND THE SMOKE DISSIPATED. CREW DECLARED AND EMERGENCY AND FLIGHT LANDED BWI WITHOUT FURTHER IN CIDENT. MAINTENANCE CONFIRMED THAT THE NR 3 COFFEE MAKER CIRCUIT BOARD SHOWED EVIDENCE OF OVERHEATING. THEY REPLACED T HE COFFEE MAKER. (M) 2 L 7 2 4F RT 1998110600460 19981106 00460 EU 1998 11 6 USAAF98079 1 19980921 A 5230 D28645003 SEAL FOKKER F28 F28MK0100 4990807 EU CARGO DOOR DETERIORATED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 852US 11280 RIC - FLT 938 - AFTER TAKEOFF FROM RIC, 'MID CARGO DOOR' WARNING ILLUMINATED AND THE AIRCRAFT WOULD NOT PRESSURIZE. CRE W BURNED OFF EXCESS FUEL TO AVOID AN OVERWEIGHT LANDING. FLIGHT RETURNED TO RIC AND LANDED WITHOUT FURTHER INCIDENT. M AINTENANCE REPLACED THE MID CARGO DOOR VENT FLAP SEAL. (M) 2 L 7 2 4F RT 1998110600461 19981106 00461 EU 1998 11 6 USAAF98077 1 19980917 A 2131 21185265 CONTROLLER FOKKER F28 F28MK0100 4990807 EU E/E BAY INOPERATIVE A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 864US 11306 ILM - FLT 1690 - AFTER TAKEOFF FROM ILM, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO ILM AND LANDED WITHOUT F URTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 AUTOMATIC PRESSURIZATION CONTROLLER. (M) 2 L 7 2 4F RT 1998110600462 19981106 00462 EU 1998 11 6 USAAF98085 1 19981009 A 3230 VALVE FOKKER F28 F28MK0100 4990807 EU MLG OUT OF ADJUST A USAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 EA 19 895US 11380 BNA - FLT 1105 - ON APPROACH TO BNA WHEN LANDING GEAR HANDLE WAS SELECTED TO 'DOWN', GEAR HESITATED AND THEN SLOWLY EXTE NDED. THE GREEN NOSE GEAR DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. CREW ABORTED APPROACH AND RECYCLED THE LANDING GEAR HANDLE. ALL THREE LANDING GEAR EXTENDED NORMALLY. FLIGHT LANDED BNA WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS MAINTENANCE FERRIED TO A MAINTENANCE FACILITY IN CLT. MAINTENANCE ADJUSTED THE LANDING GEAR SEQUENCE VALVE. SYSTEM OPE RATED NORMALLY. (M) 2 L 7 2 4F RT 1998110600463 19981106 00463 NM 1998 11 6 USAASB98259 1 19981001 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 338US 23234 IAH - MAINTENANCE FOUND THE AFT CENTER EMERGENCY EXIT AISLE LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY P ACK IN THE AFT CABIN. (M) 2 L 7 2 4F RT A16WE 1998110600464 19981106 00464 NM 1998 11 6 TAOA099810 1 19980911 A 3350 37067001 BATTERY PACK BOEING 727 727254 138408L NM CABIN DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 914TS 20251 FLT 6030 - LGA-BOS - LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, TEST OK. (M) 2 L 7 3 4F A3WE 1998110600465 19981106 00465 NM 1998 11 6 TAOA109803 1 19981013 A 2611 824PY SMOKE DETECTOR BOEING 727 727225 1384077 NM LAVATORY MALFUNCTIONED A TAOA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 922TS TS970 20415 FLT 6531 - LGA-DCA - AFT LAVATORY SMOKE ALARM SOUNDED IN FLIGHT, NO EVIDENCE OF SMOKE HEAT OR FUMES. REPLACED AFT LAVAT ORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998110600466 19981106 00466 NM 1998 11 6 TAOA109802 1 19981011 A 3350 1000679 LIGHT BOEING 727 727254 138408L NM CABIN INOPERATIVE A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 914TS 6729 20251 FLT 6540 - DCA-LGA - LEFT OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED LIGHT ASSEMBLY OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998110600467 19981106 00467 1998 11 6 TAOA109801 4 19981010 A 3421 7057V4 INDICATOR SFENA BOEING 727 727227 1384078 NM COCKPIT MALFUNCTIONED A TAOA A UNSCHED LANDING I FLT. ATTITUDE INST. CR CRUISE 1 EA 15 926TS 19019 20774 FLT 6400 - DCA-LGA - STANDBY HORIZON INDICATOR FAILED IN FLIGHT. AIRCRAFT RETURNED TO DCA. REPLACED STANDBY HORIZON IN DICATOR, OPERATIONAL CHECKS NORMAL PER MM 34-25-0. (M) 2 L 7 3 4F A3WE 1998110600468 19981106 00468 EU 1998 11 6 SIMA982743 1 19981001 A 5347 S53678001248 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AM 448 SAW - DURING CPCP-8 INSPECTION, FOUND THE ELFT AFT INBOARD AND OUTBOARD, AND THE LEFT FORWARD OUTBOARD SEAT TRACKS CORRO DED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600469 19981106 00469 EU 1998 11 6 98ZZZM813 1 19981001 A 5347 S53678001246 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AM 448 SAW - DURING CPCP-8 INSPECTION, FOUND THE ELFT AFT INBOARD AND OUTBOARD, AND THE LEFT FORWARD OUTBOARD SEAT TRACKS CORRO DED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600470 19981106 00470 EU 1998 11 6 98ZZZM814 1 19981001 A 5347 S5337500121002 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AM 448 SAW - DURING CPCP-8 INSPECTION, FOUND THE ELFT AFT INBOARD AND OUTBOARD, AND THE LEFT FORWARD OUTBOARD SEAT TRACKS CORRO DED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600471 19981106 00471 EU 1998 11 6 SIMA982744 1 19981001 A 5315 S536724062802 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 448AM 448 SAW - DURING CPCP-8 INSPECTION, FOUND THE RIGHT AND LEFT SIDE OF FLOORBEAM 36 CORRODED. REMOVED AND REPLACED FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600472 19981106 00472 NM 1998 11 6 98ZZZM815 1 19981001 A 3230 1U1085 SEQUENCE VALVE BOEING 727 72722C 138400F NM RT MLG BROKEN A RYNA O OTHER O OTHER TO TAKEOFF 1 CE 07 429EX 19100 FLT 641 - SFO-SEA - LOSS 'A' SYSTEM HYDRAULIC ON TAKEOFF, FOLLOWED RYAN PROCEDURES AS PER REF E-16 RYAN FLT HANDBOOK. R EMOVED AND REPLACED RIGHT MAIN GEAR LOCK OPERATED SEQUENCE VALVE. (M) 2 L 7 3 4F A3WE 1998110600473 19981106 00473 NM 1998 11 6 P2EA98177 1 19981009 A 7120 BACB30LE8U21 BOLT BOEING 737 737281 138448P NM NR 2 ENGINE MISMANUFACTURED A A P2EA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 219US 752 20414 MCI - DURING ACCOMPLISHMENT OF AD 98-14-09, (S/B 737-54-1004), A DEFECT (POSSIBLE FRACTURE) WAS FOUND DURING ULTRASONIC INSPECTION OF THE NR 2 ENGINE FORWRD MOUNT, INBOARD ATTACH BOLT. REPLACED NR 2 ENGINE FORWARD MOUNT INBOARD ATTACH BOLT PER BOEING S/B 737-54-1004. (M) 2 L 7 2 4F A16WE 1998110600474 19981106 00474 NM 1998 11 6 P2EA98176 1 19981009 A 3260 SENSOR BOEING 737 737222 1384473 NM RT MLG CONTAMINATED A P2EA O OTHER N FALSE WARNING CL CLIMB 1 CE 05 209US 19548 MSP - FLT 614 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. RIGHT GEAR RED LIGHT STAYS ON WHEN GEAR RETRACTED UNTIL PRES SURE RELIEVED. LEVER MOVED TO OFF POSITION. FOUND UPLOCK SENSOR VERY DIRTY, CLEANED SENSOR. PERFORMED SENSOR RESISTAN CE TEST PER MM 32-61-0, OPS CHECK OK. PERFORMED UPLOCK SENSOR TEST PER MM 32-61-21, OPS CHECK NORMAL, NO OTHER DAMAGE F OUND. (M) 2 L 7 2 4F A16WE 1998110600475 19981106 00475 SO 1998 11 6 C2XA98IA400 1 19981002 A 3350 12021299001 SOCKET EMB 120 EMB120RT SO EXTERIOR DIRTY A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15730 120187 IAH - DURING PREFLIGHT INSPECTION, THE FORWARD LEFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE C LEANED THE LIGHT SOCKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600476 19981106 00476 EU 1998 11 6 C2XA98IA413 1 19981013 A 2910 GA63192 LINE AEROSP ATR42 ATR42320 8680930 EU HYDRAULIC SYSTEM BROKEN A C2XA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 09 18814 103 FLT 3829 - BPT-IAH, THE CREW REPORTED THE RIGHT MLG SHOWED AN UNSAFE INDICATION UPON RETRACTION. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BROKEN HYDRAULIC LINE UNDER PANEL 194CR. M AINTENANCE REMOVED AND REPLACED THE AFFECTED LINE AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600477 19981106 00477 EU 1998 11 6 C2XA98IA414 1 19981007 A 3350 167006 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14825 170 IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY AISLE PATH LIGHT WAS FOUND TO HAVE TWO INOPERATIVE BULBS. MAINTENANC E REMOVED AND REPLACED THE AFFECTED BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600478 19981106 00478 SO 1998 11 6 C2XA98IA415 1 19981009 A 3260 922FS2AGN2735 SWITCH EMB 120 EMB120RT SO NLG FAILED A C2XA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 09 15713 120114 FLT 3722 - EFD-IAH - DURING FLT, THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT ON THE INITIAL TRY. THE AIRC RAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NOSE LANDING GEAR DOWNLOCK SY STEM A PROX SWITCH TO BE DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PROX SWITCH IAW EMB120MM 32-60-01, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600479 19981106 00479 EU 1998 11 6 C2XA98IA416 1 19981012 A 5320 S5337129300200 CHANNEL AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTION, THE FORWARD CARGO DOOR THRESHOLD U-CHANNEL WAS FOUND TO BE CORRODED. MAINTENANCE REMOV ED AND REPLACED THE U-CHANNEL IAW ATR 42 SRM 51-25-01 AND 51-25-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600480 19981106 00480 EU 1998 11 6 C2XA98IA417 1 19981012 A 5320 S2541004020200 THRESHOLD AEROSP ATR42 ATR42320 8680930 EU LAVATORY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTION, THE LAV DOOR THRESHOLD WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600481 19981106 00481 EU 1998 11 6 C2XA98IA418 1 19981012 A 5313 S5367130029202 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 35-37 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTION, STRINGER 15 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 35 AND 37. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR42-320 SRM 51-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600482 19981106 00482 EU 1998 11 6 C2XA98IA419 1 19981012 A 5313 S5367130001802 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 35-36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTION, STRINGER 16 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 35 AND 36. MAINTENANCE REMOV ED AND REPLACED THE AFFECTED SECTION OF STRINGER IAW ATR 42-320 SRM 51-00-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600483 19981106 00483 EU 1998 11 6 C2XA98IA420 1 19981012 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTION, THE CABIN AISLE PATH LIGHT WAS FOUND TO HAVE DIM BULBS. MAINTENANCE CHARGED THE EMERGE NC LIGHT BATTERIES, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600484 19981106 00484 EU 1998 11 6 C2XA98IA421 1 19981012 A 5753 S5751000502100 FLAP AEROSP ATR42 ATR42320 8680930 EU RT WING DELAMINATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - DURIGN C-CHECK INSPECTION, THE RIGHT INBOARD FLAP UPPER SURFACE WAS FOUND TO BE HAVE A 2 SQ INCH DELAMINATED AREA. MAINTENANCE REPAIRED THE AFFECTED FLAP IAW CONTINENTAL EXPRESS ENGINEERING CHANGE REPAIR AUTHORIZATION EC5750-01122, A ND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600485 19981106 00485 EU 1998 11 6 C2XA98IA422 1 19981012 A 3350 C341516 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTION, THE AFT EMERGENCY GROUND ILLUMINATION LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE FOR THE AFFECTED LIGHTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 1998110600486 19981106 00486 EU 1998 11 6 C2XA98IA423 1 19981012 A 3350 33516000CF24 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE AFFECTED LIGHT AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600487 19981106 00487 EU 1998 11 6 C2XA98IA424 1 19981012 A 5320 S53671257226 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU BS 38-39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 18814 103 IAH - DURING C-CHECK INSPECTON, THE INTERCOSTAL BETWEEN FRAMES 38 AND 39 RIGHT WAS FOUND TO BE CORRODED. MAINTENANCE RE MOVED AND REPLACED THE INTERCOSTAL IAW ATR42-SRM 51-24-01, 51-21-28, AND 51-25-04, AND THE AIRCRAFT WAS APPROVED FOR RET URN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600488 19981106 00488 EU 1998 11 6 C2XA98IA405 1 19981006 A 3350 7012210 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING MAINTENANCE INSPECTION, SEVERAL BULBS WERE FOUND TO BE INOPERATIVE IN SEVERAL EMERGENCY EXIT SIGNS. MAINTE NANCE REMOVED AND REPLACED THE LIGHT BULBS AND OPERATIONAL CHECKED GOOD IAW ATR 42-320 JIC 33-50-00, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600489 19981106 00489 EU 1998 11 6 C2XA98IA404 1 19981006 A 3350 3011151 BULB AEROSP ATR42 ATR42320 8680930 EU PAX DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT IN THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT BULB AND OPERATIONAL CHECKED GOOD IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WAS APPRO VED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600490 19981106 00490 EU 1998 11 6 C2XA98IA403 1 19981006 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING MAINTENANCE INSPECTION, THE BATTERY IN EMERGENCY POWER SUPPLY 18WL WAS FOUND TO BE INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED BATTERY AND OPERATIONAL CHECKED GOOD IAW ATR42-320 JIC 33-51-21, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600491 19981106 00491 EU 1998 11 6 C2XA98IA402 1 19981006 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING MAINTENANCE INSPECTION, THE BATTERY IN EMERGENCY POWER SUPPLY 3WL WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERY AND OPERATIONAL CHECKED GOOD IAW ATR 42-320 JIC 33-51-21, AND THE AIRCRAFT WA S APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600492 19981106 00492 EU 1998 11 6 C2XA98IA401 1 19981007 A 3350 3013000 POWER SUPPLY AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING PREFLIGHT INSPECTION, THE FORWARD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REP LACED THE POWER SUPPLY FOR THE AFFECTED LIGHT AND OPERATIONAL CHECKED GOOD IAW ATR42-500 JIC 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998110600493 19981106 00493 SO 1998 11 6 C2XA98IA411 1 19981008 A 5280 12019412002 BRACKET EMB 120 EMB120RT SO RT MLG DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15713 120114 IAH - DURING C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FORWARD OUTBOARD DOOR ACTUATOR ATTACH BRACKET WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600494 19981106 00494 SO 1998 11 6 C2XA98IA410 1 19981008 A 5210 12026548001 BEARING EMB 120 EMB120RT SO PAX DOOR CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15713 120114 IAH - DURING C-CHECK INSPECTION, THE AFT OPENING/LOCKING BEARING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPL ACED THE AFFECTED BEARING IAW EMB120 MM CH 52-10-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600495 19981106 00495 SO 1998 11 6 C2XA98IA409 1 19981008 A 5713 12004367001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER 10 WAS FOUND TO BE CRACKED AT PANEL 522EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600496 19981106 00496 SO 1998 11 6 C2XA98IA408 1 19981008 A 5713 12004363001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15713 120114 IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER 8 WAS FOUND TO BE CRACKED AT PANEL 522EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND TH E AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600497 19981106 00497 SO 1998 11 6 C2XA98IA407 1 19981008 A 5713 12004367002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15713 120114 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 10 WS FOUND TO BE CRACKED AT PANEL 622EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600498 19981106 00498 SO 1998 11 6 C2XA98IA406 1 19981008 A 5713 12004363002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15713 120114 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING STRINGER 8 WAS FOUND TO BE CRACKED AT PANEL 622EB. MAINTENANCE REPAIRED THE DAMAGED SECTION OF STRINGER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5710-01010, AND T HE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600499 19981106 00499 EU 1998 11 6 UF6A980911 1 19980927 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU ROWS 1&2 CD INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 6924 19415 2032 SBN - PROXIMITY LIGHTING INOP ROW 1 AND 2 CD. MAINTENANCE REMOVED AND REPLACED NR 1 POWER SUPPLY. (M) 2 L 7 2 4T RT A27NM 1998110600501 19981106 00501 WP 1998 11 6 ARWA981058 1 19981020 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 980 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - TWO INCH CRACK RT MLG ON BATHTUB FITTING LONG 24R STATION 980. REMOVED FASTENERS, STOP DRILL CRACK .25 INCH MACHI NED ANGLE DOUBLER AND FITTING REPAIR AS PER SRM 53-20 FIG 11. DRILLED NEW PARTS IAW SRM 51-3-2 AND INSTALLED REPAIR IN FUSELAGE FRAME FITTING 5615040-2 IAW SRM 53-2-0 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 2076. (M) 2 L 7 4 4F 4A25 1998110600502 19981106 00502 SO 1998 11 6 ASOA98078 1 19981007 A 3620 M1160140242 SENSOR EMB 120 EMB120RT SO LT WING MALFUNCTIONED A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 11 263AS 120157 FLT 7097 - ON CLIMB-OUT GTR-AEX, RECEIVED DUCT LEAK WARNING ON THE LEFT ENGINE. AFTER COMPLETING THE POH CHECKLIST, SHU T DOWN THE LEFT ENGINE, DECLARED AN EMERGENCY AND DIVERTED TO JAN WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCI DENT. ON THE GROUND, THE WARNING OCCURRED AGAIN WITH BOTH ENGINES SECURED. THE BLEED SYSTEM WAS DEFERRED FOR A FAULTY INDICATION AND THE AIRCRAFT WAS POSITIONED BACK TO ATL. ATL MAINTENANCE REMOVED AND REPLACED THE PNEUMATIC LEAK SENSOR INBOARD OF THE LEFT LEADING EDGE. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600503 19981106 00503 SO 1998 11 6 ASOA98077 1 19981004 A 2121 EVAC2322C2 COOLING FAN EMB 120 EMB120RT SO AIR COND BAY FAILED A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 267AS 20657 120198 SHORTLY AFTER TAKEOFF DFW-AEX, THE FLIGHT ATTENDANT ADVISED THAT THE SMOKE DETECTOR WAS GOING OFF AND SMOKE WAS VISIBLE THROUGH OUT THE CABIN. CREW DECLARED AN EMERGENCY, REQUESTED FIRE EQUIPMENT AND RETURNED TO DFW. LANDING WAS MADE SAFE LY AND WITHOUT FURTHER INCIDENT. AIRCRAFT WAS TAXIED CLEAR OF THE RUNWAY AND ENGINES SECURED. PASSENGERS WERE EVACUATE D AND AIRCRAFT POWERED DOWN. DFW MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK GROUND COOLING FAN. OPERATIONAL CHECK S WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1998110600504 19981106 00504 WP 1998 11 6 ARWA981057 1 19981020 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 240 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 . 5 INCH CRACK ON RIGHT WING L/E UPPER SKIN AT STATION WS 240, FABRICATED DOUBLER AND INSTALLED IAW EO JOSSAIR, CO NR 18 R5781019 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1702. (M) 2 L 7 4 4F 4A25 1998110600505 19981106 00505 WP 1998 11 6 ARWA981056 1 19981020 A 5753 SKIN DOUG DC8 DC863F 302198F WP WS 60 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION AND DENT ON LOWER SKIN FLAP (LEFT INBOARD FLAP) STATION XW 60 REPLACED PANEL IAW REPAIR INFORMATIO N JOSSAIR, CO NR 18R57510 AND SRM 51-30-0 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1433. (M) 2 L 7 4 4F 4A25 1998110600506 19981106 00506 WP 1998 11 6 ARWA981055 1 19981020 A 5753 SKIN DOUG DC8 DC863F 302198F WP WS 407 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND DENTS, DEFORMATION AND CORROSION ON RT OUTBOARD FLA T/E LOWER SKIN STARS 407.00 TO XRS 454. REMOVED LOWER S KIN FABRICATED NEW SKIN AND REPLACED IAW REPAIR INFORMATION JOSSAIR, CO NR 18R5751020 AND SRM 51-3-0 WORK ACCOMPLISHED U NDER ARROW AIR FORM M3A CONTROL 1700. (M) 2 L 7 4 4F 4A25 1998110600507 19981106 00507 WP 1998 11 6 HALA980340 1 19981011 A 3350 BATTERY DOUG DC9 DC951 3022051 WP ROWS 6-11 DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 661HA 47796 HNL - FLT 102 - (LOG PAGE NR A 154589) - OVERHEAD EMERGENCY LIGHTS ROWS 6-11 INOPERABLE. REPLACED BATTERY, OPS CHECK OK . (X) 2 L 7 2 4F RT A6WE 1998110600508 19981106 00508 EU 1998 11 6 98ZZZX3954 1 19980615 A 5541 RIB BAG BAE146 BAE146300A 1500267 EU RUDDER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 ATW - NR 1 (BOTTOM) RIB ON RUDDER IS CRACKED WITH A SMALL PIECE BROKEN OUT. REPLACED RIB PER REPAIR INSTRUCTIONS HC554H 9005. 2 H 7 4 4F RT A49EU 1998110600509 19981106 00509 EU 1998 11 6 98ZZZX3955 1 19980915 A 5312 BULKHEAD BAG BAE146 BAE146200A 1500266 EU BS 50 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - BULKHEAD AFT OF FRAME 50 (ABOVE AIRBRAKE ACTUATOR) IS CRACKED IN RT LOWER CORNER AND ABOUT 4 INCHES FROM LEFT CORN ER. ALSO, RIVETS LOOSE IN BOTH CORNERS. REPAIRED RT AND LT CORNER AREAS OF BULKHEAD JUST AFT OF FRAME 50 IAW BAE FAXES DJR/RJ0602-98, JIM/RJ0491-96 AND DJR/RJ0670-98. 2 H 7 4 4F RT A49EU 1998110600510 19981106 00510 EU 1998 11 6 98ZZZX3956 1 19980612 A 5330 SKIN BAG BAE146 BAE146300A 1500267 EU FUSELAGE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 ATW - RIGHT MLG DOOR FORWARD LOWER CORNER DAMAGE DUE REPAIR IN 2,000 FLIGHTS PER AVRO FAX JM/0642-97. SEE SRM FOR SKIN REPAIR CRITERIA CURRENT TCA 25066 DUE REPAIR BY 27566 TCA. SEE FAX JM/RJ0317-98 FOR 500 FLIGHT EXTENSION TO 27566 TCA. REPAIRED FORWARD LOWER CORNER AND BOTTOM SKIN DAMAGE PER BAE SRM 53-81-11 FIG 204 AND BAE FAX REF JM/RJ0450-98. 2 H 7 4 4F RT A49EU 1998110600511 19981106 00511 EU 1998 11 6 98ZZZX3957 1 19980608 A 5330 SKIN BAG BAE146 BAE146300A 1500267 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 ATW - REF W/C DATED 10-19-96, LT AFT FUSELAGE HAS DENT LOCATED 24 INCHES AFT OF LT PRESSURE BULKHEAD AND 6 INCHES BELOW 'N' NUMBERS. DENT IS 5 INCHES LONG BY MIN/D MAX - 1 INCHES/.078 INCH. REPAIRED DENT IAW BAE FAX DJR/RJO437-98. 2 H 7 4 4F RT A49EU 1998110600512 19981106 00512 EU 1998 11 6 98ZZZX3958 1 19980605 A 5230 CAGE BAG BAE146 BAE146300A 1500267 EU CARGO DOOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 ATW - FORWARD CARGO DOOR AFT LOWER SEAL CAGE IS DENTED AND CRACKED. REPLACED FORWARD CARGO DOOR AFT LOWER SEAL CAGE. 2 H 7 4 4F RT A49EU 1998110600513 19981106 00513 EU 1998 11 6 98ZZZX3959 1 19981004 A 5260 ACTUATOR BAG BAE146 BAE146200A 1500266 EU AFT AIRSTAIR LEAKING A A6WA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 31 609AW E2070 ATW - FLT 581 - YELLOW HYDRAULIC FLUID LOST, WITH ASSOCIATED FLUID AT REAR AIRSTAIR AND LAVATORY. FOUND AFT AIRSTAIR, F ORWARD ACTUATOR LEAKING, CLEANED, CAPPED OFF LINE AND DEFERRED AND PLACARDED, C/W OVERWEIGHT LANDING INSPECTION. 2 H 7 4 4F RT A49EU 1998110600514 19981106 00514 EU 1998 11 6 98ZZZX3960 1 19980902 A 2710 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU RT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - THE RIGHT MAIN AILERON CENTER SECTION OF CABLES ARE CORRODED AT THE LOWER PULLEY IN THE WING ROOT JUST AFT OF FRAM E NR 29. REMOVED AND REPLACED THE RIGHT AILERON CENTER SECTION MAIN AILERON CONTROL CABLES. GEN W/C FOR FUNCTIONAL TES T. 2 H 7 4 4F RT A49EU 1998110600515 19981106 00515 EU 1998 11 6 98ZZZX3961 1 19980911 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU BS 5-7 LIGHTNING STRIKE A A6WA K NONE C F.O.D. IN INSP/MAINT 1 GL 31 179US E2041 ATW - DURING LIGHTNING STRIKE INSPECTION, NOTED ONE MINOR SKIN PIT BETWEEN FRAMES 5 AND 7 APPROXIMATELY STR 19L. CLEANE D AND PREPPED AREA. DAMAGED MEASURED AT .007 INCH DEPTH. PER BAE FAX, INSTALLED A .1250 INCH RIVET SL4070-32, BAE FAX DJR/RJ06820-98. 2 H 7 4 4F RT A49EU 1998110600516 19981106 00516 EU 1998 11 6 98ZZZX3962 1 19980903 A 5210 SKIN BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - LEFT FORWARD PASSENGER DOOR HAS 2 EACH CRACKS IN THE HANDLE BOX AREA. REPLACED BOTH BOX ANGLES IAW FAX DJR/RJ0318 -97 AND BAE SRM. ANGLES MADE PER PS1. 2 H 7 4 4F RT A49EU 1998110600517 19981106 00517 EU 1998 11 6 98ZZZX3963 1 19980911 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU BS 405 LIGHTNING STRIKE A A6WA K NONE C F.O.D. IN INSP/MAINT 1 GL 31 179US E2041 ATW - DURING LIGHTNING STRIKE INSPECTION, NOTED ONE MINOR SKIN PIT BETWEEN FRAMES 4 AND 5, STR 19L. CLEANED AND PREPPED AREA. DAMAGE MEASURED AT .014 INCH DEPTH. PER BAE FAX, INSTALLED A .1250 INCH RIVET SL4070-32. BAE FAX DJR/RJ0682-98 . 2 H 7 4 4F RT A49EU 1998110600518 19981106 00518 EU 1998 11 6 98ZZZX3964 1 19980911 A 3230 BRACKET BAG BAE146 BAE146200A 1500266 EU MLG CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - REF EO E92/067/632 REV A, LEFT HINGE BRACKET MISSING BUSHING, HOLE OVER SIZE, CORROSION AROUND HOLE IAW ITEM 6 SEC T I. REMOVED LEFT HINGE BRACKET WRK 1032. INSTALLED SERVICEABLE LT HINGE BRACKET WITH REPLACEMENT HARDWARE AS REQUIRED . 2 H 7 4 4F RT A49EU 1998110600519 19981106 00519 EU 1998 11 6 98ZZZX3965 1 19980917 A 3222 DIAPHRAGM BAG BAE146 BAE146200A 1500266 EU NLG CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - REF W/C 7030, NLG DIAPHRAGM AT ATTACHMENT POINT OF NLG RAM HAS BEEN FOUND CRACKED AT 6 O'CLOCK POSITION. CRACK EX TENDS DOWNWARD FROM AND INTO THE PIN HOLE .125 INCH. REPORTED TO AVRO/BAE RDO AND AWAITING FOR REPAIR ACTION. REPAIRED NLG DIAPHRAGM (LT) IAW AVRO FAX DJH/RJ0683-98 ISSUE 2. 2 H 7 4 4F RT A49EU 1998110600520 19981106 00520 EU 1998 11 6 98ZZZX3966 1 19980917 A 3233 BOLT BAG BAE146 BAE146200A 1500266 EU NLG ACTUATOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - NLG UPPER ACTUATOR MOUNT BOLT HEAD HAS CRACKED INDICATION. VERIFIED BY NDT 8-31-98 ID NR 042. REPLACED BOLT (INN ER) ONE-HALF DIAMETER AT NL9 UPPER ATTACH POINT FOR ACTUATOR IAW BAE 146 MM. REF W/C 7050 FOR RETRACTION TEST. 2 H 7 4 4F RT A49EU 1998110600521 19981106 00521 EU 1998 11 6 98ZZZX3967 1 19980902 A 2710 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - THE CENTER SECTION MAIN AILERON INTERCONNECT CABLES ARE CORRODED AT THE WING ROOT AREA. REMOVED AND REPLACED MAIN AILERON INTERCONNECT CENTER CABLES. GEN W/C FOR FUNCTIONAL TEST. 2 H 7 4 4F RT A49EU 1998110600522 19981106 00522 EU 1998 11 6 98ZZZX3968 1 19980904 A 5320 INTERCOSTAL BAG BAE146 BAE146200A 1500266 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - FORWARD VEST INTERCOSTALS, SILL PLATES NEED CLEANING AND SEALANT, INSPECTED FOR CORROSION. CLEANED AND INSPECTED. REMOVED MINOR CORROSION AND TREATED METAL, PRIMED, PAINTED, AND SEALED FORWARD VEST INTERCOSTALS AND SILL PLATES. 2 H 7 4 4F RT A49EU 1998110600523 19981106 00523 EU 1998 11 6 98ZZZX3969 1 19980915 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - AIRBRAKE ACTUATOR HAS CHAFED RIGHT FUSELAGE UPPER LONGERON APPROXIMATELY .030 INCH DEEP. REPAIRED RT FUSELAGE UPP ER LONGERON AT AIRBRAKE ACTUATOR IAW BAE FAX DJR/RJ0681-98, AVRO FAX DJR/RF0638-96, AND PRODUCTION DRAWING NR HC539H0229 . 2 H 7 4 4F RT A49EU 1998110600525 19981106 00525 EU 1998 11 6 98ZZZX3971 1 19980831 A 3520 VALVE BAG BAE146 BAE146200A 1500266 EU PASSENGER OXYGEN DEFECTIVE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - OXYGEN BOX 8RT. OXYGEN SHUT OFF WILL NOT STOP FLOW COMPLETELY. REMOVED AND REPLACED OXYGEN MASK AT 8RT. OPS AND LEAK CHECKS OK. 2 H 7 4 4F RT A49EU 1998110600526 19981106 00526 EU 1998 11 6 98ZZZX3972 1 19980914 A 5347 SEAT TRACK BAG BAE146 BAE146200A 1500266 EU BS 20 WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - SEAT TRACK RAIL, STA 252.33, FRAMES 20-20A, LT INBOARD CORRODED AND WORN BEYOND LIMITS. REPLACED FORWARD SECTION O F SEAT RAIL 87 INCHES TOTAL AND SPLICED PER SRM 53-00-32, PAGE 202. 2 H 7 4 4F RT A49EU 1998110600527 19981106 00527 EU 1998 11 6 USAA980428 1 19980929 A 5320 1154767 BEAM FOKKER F28 F28MK0100 4990807 EU BS 4610-6030 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND CORROSION FROM STA 4610 - STA 6030 BEAM BL 1127R, 1 INCH BY 3 INCH AREA. CORROSION ENTIRE LENGTH, DEEP AREA AT END OF SPLICE HAS .008 INCH METAL LEFT. (X) 2 L 7 2 4F RT 1998110600528 19981106 00528 EU 1998 11 6 USAA980493 1 19980929 A 2560 MOUNT FOKKER F28 F28MK0100 4990807 EU BS 4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND CORROSION AT GIRT BAR MOUNT BEYOND LIMITS, 1 INCH BY .50 INCH AT STA 4850 AFT SIDE MED. RE PAIRED PER SRM CHAPTER 51. (X) 2 L 7 2 4F RT 1998110600529 19981106 00529 EU 1998 11 6 USAA980492 1 19980929 A 5315 FLOOR BEAM FOKKER F28 F28MK0100 4990807 EU BS 3870-4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND .50 INCH BY 2 INCH FLOOR BEAM CORRODED AT STA 3870 - STA 4610, AT BL 600R. FABRICATED NEW PARTS FROM 2024-T-3, .032 INCH ANGLES AND STRIPS 204-T-3, .040 INCH DWG II A23622, A22271, D23695 AND D23699, FIG 09, FL OOR BEAM 600R. REPAIRED PER SRM 51-70 AND SRM 53-12-10 PAGE 0 DEC '94. (X) 2 L 7 2 4F RT 1998110600530 19981106 00530 NM 1998 11 6 USAABB98102 1 19981008 A 3350 20121 BATTERY CHARGER BOEING 767 7672B7 1385107 NM ROW 20 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - LOW LEVEL EMERGENCY LIGHT AT ROW 20 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (X) 2 L 7 2 4F RT A1NM 1998110600531 19981106 00531 NM 1998 11 6 USABB98104 1 19981010 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 33 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 625VJ 27246 LAX - FOUND FLOOR EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (X) 2 L 7 2 4F RT A2NM 1998110600532 19981106 00532 NM 1998 11 6 USAABB98103 1 19980924 A 3350 8731002511REV9 SIGN BOEING 757 757225 1384959 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 606AU 22202 LAX - FOUND L4 EXIT IDENTIFIER INOPERATIVE. MAINTENANCE REPLACED THE IDENTIFIER ASSEMBLY. (X) 2 L 7 2 4F RT A2NM 1998110600533 19981106 00533 WP 1998 11 6 USAAD98186 1 19981015 A 2420 976J2544 CONTROL PANEL DOUG DC9 DC931 3022065 WP E/E BAY FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 965VJ 47374 BWI/BOS - FLT 728 - AFTER DEPARTURE, THE LEFT ENGINE GENERATOR TRIPPED OFF-LINE. ATTEMPTS TO RESET WERE UNSUCCESSFUL. T HE APU WAS ON MEL LEAVING ONLY THE RIGHT ENGINE GENERATOR TO POWER THE AIRCRAFT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR CONTROL PANEL AND THE BUSS CONTROL PANEL. REF: OPER ATOR CONTROL NR 98ZZZX3973. (X) 2 L 7 2 4F A6WE 1998110600534 19981106 00534 WP 1998 11 6 98ZZZX3973 1 19981015 A 2450 914F5654 CONTROL PANEL DOUG DC9 DC931 3022065 WP E/E BAY FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 965VJ 47374 BWI/BOS - FLT 728 - AFTER DEPARTURE, THE LEFT ENGINE GENERATOR TRIPPED OFF-LINE. ATTEMPTS TO RESET WERE UNSUCCESSFUL. T HE APU WAS ON MEL LEAVING ONLY THE RIGHT ENGINE GENERATOR TO POWER THE AIRCRAFT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR CONTROL PANEL AND THE BUSS CONTROL PANEL. REF: OPER ATOR CONTROL NR USAAD98186. 2 L 7 2 4F A6WE 1998110600535 19981106 00535 WP 1998 11 6 USAAD98185 1 19981006 A 3350 6011777LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CARGO BAY INOPERABLE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 958VJ 47351 DAY - THE RIGHT NACELLE EMERGENCY LIGHT WAS INOPERABLE. MAINTENANCE REPLACED THE RIGHT NACELLE EMERGENCY LIGHT POWER SU PPLY. (X) 2 L 7 2 4F A6WE 1998110600536 19981106 00536 WP 1998 11 6 USAAD98174 1 19981006 A 3350 41B030CF00101 BATTERY DOUG DC9 DC931 3022065 WP CARGO BAY DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 958VJ 47351 PIT - THE LEFT AND RIGHT NACELLE EMERGENCY LIGHTS WERE INOPERABLE. MAINTENANCE REPLACED THE NACELLE LIGHT EMERGENCY LIG HT BATTERY PACKS. (X) 2 L 7 2 4F A6WE 1998110600537 19981106 00537 EU 1998 11 6 98ZZZX3974 1 19980904 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU BS 3 AND 19 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 179US E2041 ATW - FRAME 29 TOP LANDING GEAR LONGERONS CRACKED NR 3 AND NR 19 OUTBOARD OF BOTH OUTBOARD SEAT TRACK RAILS. REPAIRED A T FRAME 19, FLOOR BEAMS NR 3 AND NR 19 AT FORWARD OUTBOARD POSITIONS IAW BAE REPAIR DRAWING NR HC536H9211 AND BAE FAX NR DJR/RJ0207-97. (X) 2 H 7 4 4F RT A49EU 1998110600538 19981106 00538 EU 1998 11 6 98ZZZX3975 1 19980903 A 5320 DOOR SILL BAG BAE146 BAE146200A 1500266 EU FUSELAGE CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 179US E2041 ATW - SURFACE CORROSION ON AFT PASSENGER DOOR SILL PLATE. CLEANED CORROSION, TREATED, PRIMED, PAINTED AND SEALED DOOR S ILL. (X) 2 H 7 4 4F RT A49EU 1998110600539 19981106 00539 1998 11 6 98ZZZX3976 4 19980809 A 2565 D31050105 SLIDE BAG BAE146 BAE146300A 1500267 EU PASSENGER DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 614AW 3233 0310 E3132 MKE - FLT 621 - LEFT FORWARD PASSENGER DOOR EMERGENCY SLIDE HAS DROPPED DOWN IN ITS OWN CONTAINER. REMOVED AND REPLACED LEFT FORWARD PASSENGER SLIDE IAW MM BATTERY EFF CHECK DUE 3-5-99. COVER LATCH PULL OFF TEST C/W. S/N OFF 0310. S/N O N 0340. 2 H 7 4 4F RT A49EU 1998110600540 19981106 00540 EU 1998 11 6 98ZZZX3977 1 19980327 A 3520 4566M37B SEAL BAG BAE146 BAE146200A 1500266 EU CABIN BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US 1870 E9701130 E2042 DEN - FORWARD CABIN PBE SEAL IS BROKEN, POUCH IS SOFT. REPLACED PBE. 2 H 7 4 4F RT A49EU 1998110600541 19981106 00541 EU 1998 11 6 98ZZZX3978 1 19980403 A 3350 6035501 POWER SUPPLY BAG BAE146 BAE146200A 1500266 EU CABIN INOPERATIVE A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 179US 19587 152 E2041 DEN - THREE EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LEFT FORWARD POWER SUPPLY. 2 H 7 4 4F RT A49EU 1998110600543 19981106 00543 EU 1998 11 6 98ZZZX3980 1 19980924 A 2912 FILTER BAG BAE146 BAE146300A 1500267 EU HYDRAULIC SYSTEM LEAKING A A6WA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 31 615AW E3141 ORD - FLT 502 - F/S REPORTS STRONG TOXIC SMELL IN CABIN. MAINTENANCE FOUND O-RING FOR YELLOW HYDRAULIC SYSTEM HP FILTER BLOWN OUT. REMOVED AND REPLACED YELLOW HP FILTER O-RINGS. NO LEAKS NOTED. 2 H 7 4 4F RT A49EU 1998110600544 19981106 00544 1998 11 6 98ZZZX3981 4 19980616 A 2565 D31050103 SLIDE BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR DAMAGED A A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 183US 3568 0168 E2043 PACKBOARD BENT CAUSING SLIDE COVER NOT TO RELEASE, RIGHT AFT POSITION. REMOVED AND REPLACED SLIDE. 2 H 7 4 4F RT A49EU 1998110600546 19981106 00546 EU 1998 11 6 98ZZZX3983 1 19980429 A 3260 SWITCH BAG BAE146 BAE146200A 1500266 EU MLG CONTAMINATED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 290UE E2080 MYR - FLT 690 - UPON GEAR RETRACTION, LANDING GEAR DID NOT RETRACT. CLEANED SQUAT SWITCHES. 2 H 7 4 4F RT A49EU 1998110600547 19981106 00547 EU 1998 11 6 98ZZZX3984 1 19980320 A 5210 ROD BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 ATW - FORWARD PASSENGER DOOR DROPS BELOW DOOR FRAME WHEN OPENED AND DOES NOT DROP AND LATCH PROPERLY WHEN CLOSED. REPLA CED BROKEN LOWER ROD END ON THE CONTROL SHAFT ASSY TO TORQUE SHAFT CONTROL ROD. REPLACED LOWER HINGE COVER. NOTE: REM OVED AND REPLACED EVACUATION SLIDE TO FACILITATE MAINTEANCE. DOOR OPERATION CHECKED NORMAL. 2 H 7 4 4F RT A49EU 1998110600548 19981106 00548 EU 1998 11 6 98ZZZX3985 1 19980701 A 2120 AIR DIST BAG BAE146 BAE146200A 1500266 EU CABIN ODOR A A6WA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 GL 31 181US E2042 DEN - FLT 699 - SMOKEY HAZE WITH OIL SMELL IN FORWARD GALLEY AND CABIN. PERFORMED PACK BURN OUT. RAN ALL ENGINES AND A PU. NO FURTHER SMELL NOTED. 2 H 7 4 4F RT A49EU 1998110600549 19981106 00549 1998 11 6 98ZZZX3986 4 19980924 A 2565 D31050105 SLIDE BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 181US 4253 43 0359 E2042 ATW - SLIDE FOUND DEFECTIVE. REMOVED AND REPLACED SLIDE, CHECKS GOOD. 2 H 7 4 4F RT A49EU 1998110600550 19981106 00550 NE 1998 11 6 98ZZZX3987 1 19980827 A 2820 VALVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUEL SYSTEM MISINSTALLED A A6WA K NONE L W NO TEST INADEQUATE Q C IN INSP/MAINT 1 GL 31 179US E2041 ATW - CROSS FEED VALVE (FUEL) FAILED THE TEST. REF: MM 28-22-44 PG 203, 3-15-95. 1.E STEPS 6 AND 7. FOUND ACT ELECTR ICAL CONNECTORS P1 AND P2 SWAPPED. RETURNED PLUGS TO CORRECT POSITION TO NO AVAIL. TRIED NEW ACT HTE1451/1. ALSO, TO NO AVAIL. FOUND WIRE TERMINAL END NOT INSTALLED AT TERMINAL BLOCK 242-08-00 C4B RT ELECT DISCONNECT FUSE/WING T/EDGE. R EINSTALLED AND OPS CHECKED. 2 H 7 4 4F 4 F RT A49EU E6NE 1998110600551 19981106 00551 1998 11 6 98ZZZX3988 4 19980826 A 2565 D31050103 SLIDE BAG BAE146 BAE146200A 1500266 EU PASSENGER DOOR MALFUNCTIONED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 179US 4287 0171 E2041 ATW - FUNCTION CHECKED SLIDE (DEPLOY) AND THEN REMOVED FOR DETAILED INSPECTION. REF CHECKLIST. REPORT TASK ON STEP 543 IN COMPUTER. C/W DEPLOYMENT TEST IAW BAE 146 M. GEN W/C INST SERVICE SLIDE. REF W/C 892, SLIDE DEPLOYED TWISTED. RE MOVED AND REPLACED W/O BY7756, REPORTED MX 8/26. 2 H 7 4 4F RT A49EU 1998110600552 19981106 00552 EU 1998 11 6 98ZZZX3989 1 19980826 A 7620 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - NR 2 ENGINE FUEL SHUT-OFF CABLES AT THE WING ROOT PULLEYS FORWARD OF FRAME NR 26 ARE CORRODED. REMOVED AND REPLAC ED NR 2 ENGINE FUEL SHUT-OFF CABLES IAW BAE MM. C/W OPS TEST OF THE NR 2 SHUT-OFF VALVE, OPS CHECKED GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 1998110600553 19981106 00553 EU 1998 11 6 98ZZZX3990 1 19980907 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU BS 20 GOUGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 179US E2041 ATW - PER FAX DS/W/TJ/28015/97 AND DJR/RJ0912-96. SEVERAL GOUGES TO DENTS AFT OF FRAME 20 AND ABOVE LAP SEAM AT STR 19 MUST BE REPAIRED BY TCA OF 22593 TCA TO CORRESPOND WITH DUE TIME OF C-CHECK CURRENTLY SCHEDULED FOR 5-31-98. REPAIRED I AW BAE FAX REF NR DJH/RJ0569/98 AND DRAWING HC536H9251. 2 H 7 4 4F RT A49EU 1998110600554 19981106 00554 EU 1998 11 6 98ZZZX3991 1 19980602 A 5320 INTERCOSTAL BAG BAE146 BAE146300A 1500267 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 ATW - AFT VESTIBULE FLOOR SUPPORT STRUCTURE, FIRST INTERCOSTAL INBOARD OF AIRSTAIR RAILS, LT SIDE HAS A RIVET WITH CORRO SION AROUND IT. DRILLED OUT RIVET, REMOVED MINOR SURFACE CORROSION, USED PROTECTIVE TREATMENT ON BARE SURFACE, PRINTED AND COVERED SURFACE WITH PRC. INSTALLED NEW RIVET. 2 H 7 4 4F RT A49EU 1998110600555 19981106 00555 EU 1998 11 6 98ZZZX3992 1 19980615 A 5320 ANGLE BAG BAE146 BAE146300A 1500267 EU CARGO BAY MISSING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 ATW - FORWARD CARGO BAY: CENTER FORWARD CARGO FLOOR SUPPORT ANGLE AT FRAME 19D, SECTION MISSING. REPLACED FORWARD CARG O BAY CENTER FLOOR SUPPORT ANGLE AT FRAME 19D. 2 H 7 4 4F RT A49EU 1998110600556 19981106 00556 NM 1998 11 6 USAASB98267 1 19981011 A 3397 WIRE BOEING 737 737301 1384611 NM ROW 11 LOOSE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 350US 23553 LGA - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS AT SEAT ROW 11, LEFT HAND SIDE, INOPERABLE. MAINTENANCE ACCOMPLISHED AN INTERIM REPAIR PER ENGINEERING AUTHORIZATION NR 62698 WHICH INSTALLS A JUMPER WIRE FROM THE LIGHT ASSEMBLY ON SEAT RO W 9. A SPLICE WAS INSTALLED BETWEEN THE RED WIRES OF PIN NR 1 OF BOTH D9009P (SEAT ROW 9 LT LIGHT ASSY) AND D9010P (SEA T ROW 11 LT LIGHT ASSY). OPERATIONAL CHECK GOOD. AIRCRAFT IS TO RETURN TO ORIGINAL CONFIGURATION NO LATER THAN THE NEX T AVAILABLE CX MAINTENANCE CHECK. (X) 2 L 7 2 4F RT A16WE 1998110600557 19981106 00557 NE 1998 11 6 USAAD98179 2 19981011 A 7261 ACC336F1665 FILTER DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE GEARBOX CLOGGED A USAA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 19 800US 48034 708452 BOS/CLT - FLT 1638 - DURING CRUISE, THE LEFT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. ENGINE THRUST WAS REDUCED, BUT T HE LIGHT REMAINED ON. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT LANDED WITHOUT INCIDENT. THERE WAS 20 MINUTES SINGLE EN GINE TIME. MAINTENANCE REPLACED THE LEFT ENGINE OIL FILTER. (X) 2 L 7 2 4F 4 F A6WE E9NE 1998110600558 19981106 00558 NM 1998 11 6 USAA980473 1 19981009 A 5330 SKIN BOEING 737 7374B7 1384702 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 432US 25747 24554 CLT - DURING RON CHECK VISUAL INSPECTION FOUND A 1.50 INCH CRACK IN SKIN 2 INCHES AFT OF STA 727D RT SIDE 1 INCH BELOW S TR 23. INSTALLED DOUBLER PER TR 53-30-06. (X) 2 L 7 2 4F RT A16WE 1998110600559 19981106 00559 NM 1998 11 6 USAASB98265 1 19981009 A 2120 470044 FILTER BOEING 737 7374B7 1384702 NM A/C BAY DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 430US 24552 PHL - FLT 403 - ON CLIMB-OUT FROM PHL, THE FLIGHT CREW WAS ADVISED BY THE FLIGHT ATTENDANT THAT PASSENGERS IN ROWS 7 THR OUGH 11 REPORTED A BURNING SMELL OF RUBBER. SMELL WAS CONFIRMED AND THE CAPTAIN ELECTED TO RETURN TO FIELD AT PHL AND D ECLARE AN EMERGENCY. THE FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. NO EVACUATION WAS ACCOMPLISHED. MAINTENANCE PERFORMED A CHECK OF ALL ELECTRICAL COMPONENTS, LIGHTS, BALLAST'S WIRES, ETC. ALL CHECK GOOD . COULD NOT DUPLICATE SMELL. REMOVED AND REPLACED THE LEFT AND RIGHT RECIRCULATION FAN FILTERS. OPS CHECK GOOD. (X) 2 L 7 2 4F RT A16WE 1998110600560 19981106 00560 NM 1998 11 6 USAABB98106 1 19981011 A 3397 WIRE BOEING 767 7672B7 1385107 NM ROWS 13 AND 14 BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE THROUGHOUT THE CABIN. MAINTENANCE REPAIRED SYSTEM WIRING AT ROWS 13 A ND 14. (X) 2 L 7 2 4F RT A1NM 1998110600561 19981106 00561 NM 1998 11 6 USAABB98105 1 19981008 A 3350 20121 BATTERY CHARGER BOEING 767 7672B7 1385107 NM ROW 20 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - FOUND BATTERY CHARGER INOPERATIVE AT ROW 20. MAINTENANCE REPLACED THE BATTERY CHARGER. (X) 2 L 7 2 4F RT A1NM 1998110600562 19981106 00562 EU 1998 11 6 USAA980487 1 19980929 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3870-4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND CORROSION BEYOND LIMITS AFTER REMOVAL ON BEAM (3 INCHES BY .50 INCH AREA), AT BL 600R AT ST A 3870 - STA 4610. REPAIRED PER SRM 53-12-10, FIG 09. (X) 2 L 7 2 4F RT 1998110600563 19981106 00563 EU 1998 11 6 USAA980489 1 19980929 A 5320 1718730 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3870 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND BL ZERO CORRODED THROUGH AT STA 3870, 1 INCH BY .50 INCH AREA, T-CAP (BEAM). REPAIRED PER SRMS 51-70-06. (X) 2 L 7 2 4F RT 1998110600564 19981106 00564 EU 1998 11 6 USAA980488 1 19980929 A 5320 1154834 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3820 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND BEAM CORRODED THROUGH AT STA 3820 (1 INCH BY 1 INCH AREA) AT BL 1127R. REPAIRED PER SRM CH APTER 51. (X) 2 L 7 2 4F RT 1998110600565 19981106 00565 EU 1998 11 6 USAA980491 1 19980929 A 5320 1154340 MOUNT FOKKER F28 F28MK0100 4990807 EU BS 4850-5305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND GALLEY 2 INBOARD MOUNT EXCESSIVLEY CORRODED, .50 INCH BY .25 INCH AREA AT STA 4850 - STA 53 05. REPAIRED PER SRM 51-70-00. (X) 2 L 7 2 4F RT 1998110600566 19981106 00566 EU 1998 11 6 USAA980490 1 19980929 A 5347 D35424001 RAIL FOKKER F28 F28MK0100 4990807 EU BS 18921-22236 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 894US 15816 11379 PIT - DURING Q1 CHECK, FOUND LIGHT CORROSION (.50 INCH BY 12 INCH AREA) FORWARD SECTION OF CARGO RT TIE DOWN RAIL AFT. S ECTION NEEDS REPLACED AT STA 18921 TO STA 22236. CORROSION TREATED FROM STA 18921 TO STA 22236 AND REPLACED FRAMES 2223 6 TO 22706. REPLACED FRAME P/N D35424-001 AT STA 22236 TO STA 222706 PER SRM'S 51-20-01, 51-22-01, 51-23-01, 51-24-01, 51-40-02, PAGE 14, AND 51-41-01. (X) 2 L 7 2 4F RT 1998110600567 19981106 00567 WP 1998 11 6 TWAA9817701 1 19981102 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 22 DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 956U 49701 EMERGENCY EGRESS LIGHTS AFT OF ROW 22 CAME ON AND OFF DURING FLIGHT. REPLACED BATTERY PACK AT AFT ROW. CHECK-C 10-19-9 8 MCI. 2 L 7 2 4F A6WE 1998110600568 19981106 00568 WP 1998 11 6 TWAA9817702 1 19981102 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP NR 4 DIRTY A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 956U 49701 THE ESCAPE PATH LIGHTING CAME ON IN FLIGHT. CREW CYCLED THE EMERGENCY LIGHT SWITCH AND LIGHTS WENT OUT. MAINTENANCE CL EANED THE CONTACTS ON THE NR 4 EGRESS LIGHT BATTERY PACK. CHECK-C 10-19-98 MCI. 2 L 7 2 4F A6WE 1998110600569 19981106 00569 WP 1998 11 6 TWAA9817703 1 19981102 A 5313 LONGERON DOUG DC9 DC951 3022051 WP BS 851 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 417EA 47753 WHILE ACCOMPLISHING MC8ADAM CHECK, FOUND ONE INCH CRACK IN HAT SECTION OF LONGERON 2L AT STA 851. REPAIRED LONGERON 2L AT STA 851 PER SRM 53-02, FIG 18. CHECK-C 7-26-98 STL. 2 L 7 2 4F RT A6WE 1998110600570 19981106 00570 WP 1998 11 6 VJ9800574 1 19980916 A 5320 MOUNT DOUG DC9 DC932 3022066 WP BS 160 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FORWARD AIRLOCK ROD MOUNT PAD CORRODED AT FS 160, RBL 10. REMOVED PAD, FABRICATED AND INSTALLED ROD MOUNT PAD IAW DC9 S RM 51-10-3 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1998110600571 19981106 00571 WP 1998 11 6 VJ9800575 1 19980916 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 163 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 936VV 47397 FLIGHT ATTENDANT SEAT FLOOR MOUNT AT FS 163, LBL 16, CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PARTS IAW DC9 SRM 53-01 PG 10 AND 6 AND 51-10-3. 2 L 7 2 4F A6WE 1998110600572 19981106 00572 WP 1998 11 6 VJ9800576 1 19981103 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP ROW 24 INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 903VJ 47261 LT OVERHEAD EMERGENCY LIGHT AT ROW 24 INOP. REPLACED BATTERY POWER SUPPLY IAW MM 33-51. 2 L 7 2 4F A6WE 1998110600573 19981106 00573 EA 1998 11 6 JBXA9800056 1 19981103 A 5270 WARNING CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE RT EMER EXIT ACTIVATED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 577ML 7269 RIGHT OVERWING EMERGENCY DOOR CAUTION CAME ON AT 14,000 FT. PRESSURIZATION AND DOOR INTERNALLY INDICATIONS ALL NORMAL. AIR RETURN TO RDU. INSPECTED AND CHECKED RIGHT OVERWING EXIT DOOR, STOWED PROPERLY. ASSIGNED ITEM TO DMI PER MEL 52-7 0-3 2 L 7 2 4F 4 F RT A21EA E15NE 1998110600574 19981106 00574 1998 11 6 PNSA981002 2 19981018 A 7414 103493101 MAGNETO PIPER PA32 PA32301 7103207 SO RIGHT MALFUNCTIONED A PNSA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 AL 03 4327P 6907 328406002 RT MAGNETO HAD EXCESSIVE RPM DROP DURING ENGINE RUN UP PRIOR TO TAKEOFF. RETURNED TO GATE. REPLACED MAGNETO, OPERATION AL CHECK OK. 1 L 7 1 3O A3SO 1998110600575 19981106 00575 EU 1998 11 6 PNSA981003 1 19981007 A 5347 7253725 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294-319 CORRODED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 675PA 4000 206 DURING A 4000 HOUR INSPECTION, HEAVY CORROSION FOUND ON SEAT TRACK FLOOR FLANGES AT BL 0 AND BL 18, FROM STATION 294 TO 319. SPLICED IN NEW SEAT TRACKS PER SAAB SRM 53-70-60. 2 L 7 2 4T RT A52EU 1998110600576 19981106 00576 NM 1998 11 6 RAAA98B2044 1 19981103 A 5743 6519297 TRUNNION BOEING 727 72722C 138400F NM WS 224.5 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED LEFT MAIN LANDING GEAR CHANGE CPCP TASK C32-135-01 VISUAL AND HFEC INSPECTION FOUND WS 224.5 AFT REAR S PAR LANDING GEAR TRUNNION SUPPORT CORRODED IN AND AROUND BEARING RETAINER BUSHINGS AND FLANGE SURFACES. CHANGED AFT REA R SPAR LANDING GEAR TRUNNION SUPPORT PER S/B 727-57-132 AND SRM 51-10-1. M-54 NR 2. 2 L 7 3 4F A3WE 1998110600577 19981106 00577 NM 1998 11 6 RAAA98B2045 1 19981103 A 5743 6519297 TRUNNION BOEING 727 72722C 138400F NM WS 224.5 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 832RV 19098 DURING SCHEDULED RIGHT MAIN LANDING GEAR CHANGE CPCP TASK C32-135-01 VISUAL AND HFEC INSPECTION FOUND WS 224.5 AFT REAR SPAR LANDING GEAR TRUNNION SUPPORT CORRODED IN AND AROUND BEARING RETAINER BUSHINGS AND FLANGE SURFACES. CHANGED AFT RE AR SPAR LANDING GEAR TRUNNION SUPPORT PER S/B 727-57-132 AND SRM 51-10-1. M-54 NR 1. 2 L 7 3 4F A3WE 1998110600578 19981106 00578 NM 1998 11 6 CALA9802012 1 19981102 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1080-1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND SEAT TRACK CORRODED IN RT AFT GALLEY AREA AT STA 1080-1110, RBL 48. THE SEAT TRACK WAS REMOVED AND REP LACED IAW SRM 51-10-5, PAGE 1 AND 51-30-02 PAGE 4. 2 L 7 3 4F A3WE 1998110600579 19981106 00579 NM 1998 11 6 CALA9802013 1 19981102 A 5240 FITTING BOEING 727 727232 1384082 NM R2 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.5 INCH CRACK IN R-2 DOOR UPPER HINGE FITTING. THE UPPER HINGE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 3 4F A3WE 1998110600580 19981106 00580 WP 1998 11 6 CALA9802014 1 19981102 A 5320 SUPPORT DOUG DC9 DC981 3022081 WP BS 636 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND FLOOR SUPPORT CORRODED IN MAIN BAGGAGE BIN AT STA 636, LT SIDE. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-50-0. 2 L 7 2 4F A6WE 1998110600581 19981106 00581 NM 1998 11 6 CALA9802015 1 19981102 A 5720 CHORD BOEING 727 727232 1384082 NM WS 135.2 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A 2 INCH CRACK IN LT WING AFT FALSE SPAR LOWER CHORD AT WBL 135.2. THE CRACKED AREA WAS CUT OUT AND SP LICE ANGLE AND STRAPS WERE INSTALLED IAW SRM 51-30-2, 51-10-2, ECRA 5740-01866. 2 L 7 3 4F A3WE 1998110600582 19981106 00582 NM 1998 11 6 CALA9802016 1 19981102 A 5230 ANGLE BOEING 727 727232 1384082 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A 1 INCH CRACK IN C-3 DOOR T-ANGLE AT LOWER AFT DOOR STOP AREA. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-101. 2 L 7 3 4F A3WE 1998110600583 19981106 00583 NM 1998 11 6 CALA9802017 1 19981102 A 5311 FRAME BOEING 727 727232 1384082 NM BS 344 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A .5 INCH CRACK IN FLOOR LEVEL RIB AT RT SIDE OF STA 344. A STRAP WAS INSTALLED IAW SRM 51-10-2 AND 53 -10-8 FIGURE 6. 2 L 7 3 4F A3WE 1998110600584 19981106 00584 NM 1998 11 6 CALA9802018 1 19981102 A 5521 SPAR BOEING 727 727232 1384082 NM LT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND A .5 INCH CRACK IN LT ELEVATOR REAR SPAR. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-30-1, PAG E 401 AND 402. RIG AND OPERATIONAL CHECK WAS ACCOMPLISHED IAW MM 27-30-81 PAGE 507. 2 L 7 3 4F A3WE 1998110600585 19981106 00585 NM 1998 11 6 CALA9802019 1 19981103 A 5720 STIFFENER BOEING 727 727232 1384082 NM WS 244 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND RT WING FRONT SPAR VERTICAL STIFFENER CORRODED AT STA 244. THE STIFFENER WAS REPLACED IAW SRM 51-10-1 PAGE 4 AND 6A, SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998110600586 19981106 00586 NM 1998 11 6 CALA9802020 1 19981103 A 5320 WEB BOEING 727 727232 1384082 NM BS 1130-1148 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND CORROSION UNDER ANCHOR NUTS ON BOTTOM OF FLOOR WEB AT TWO DOUBLERS BETWEEN BS 1130 AND 1148, RBL 24 TO 42. THE WEB SECTION WAS REMOVED AND A NEW WEB SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-2 PAGE 4 AND 51-30-20 PAG E 1. 2 L 7 3 4F A3WE 1998110600587 19981106 00587 NM 1998 11 6 CALA9802021 1 19981103 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND FLOORBEAM CORRODED AT BS 1070, BL 0 TO RBL 52. THE CORRODED AREA WAS CUT OUT, A FLOORBEAM REPAIR WAS I NSTALLED IAW SRM 53-10-8 PAGE 13. 2 L 7 3 4F A3WE 1998110600588 19981106 00588 NE 1998 11 6 9810326601 2 19981028 A 7200 ENGINE BOEING 747 747151 1384891 NM PWA JT9 JT9D7A 52054 NE NR 4 FLAMED OUT A NWAA A E UNSCHED LANDING ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 GL 01 601US 19778 662490 DURING CRUISE AT FL390, THE NR 4 ENGINE FLAMED OUT. THE AIRCRAFT DESCENDED TO FL330 AND THE ENGINE WAS RESTARTED PER CO M. THE AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE PER FIM, WITH NO DISCREP ANCIES NOTED. THE ENGINE FUEL FILTER WAS REPLACED AND THE SUBSEQUENT ENGINE RUN WAS NORMAL. 2 L 7 4 4F 4 F A20WE E20EA 1998110600589 19981106 00589 EA 1998 11 6 COMA9860334 1 19981102 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 710CA 7241 CABIN DOOR WARNING AT 21,000 FT. ADJUSTED DOOR LATCH MECHANISM LINKAGE. 2 L 7 2 4F RT A21EA 1998110600590 19981106 00590 WP 1998 11 6 UPS98828051 1 19981012 A 5720 56422052 FITTING DOUG DC8 DC871F 302199D WP WS 98 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 729UP 46029 INSPECTION TYPE-C, THE RT LWR AUX SPAR TO REAR SPAR STA 98 TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED RE PLACEMENT FITTING IAW DHC SK- 729-846 AND SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998110600591 19981106 00591 WP 1998 11 6 UPS98828052 1 19981102 A 3350 6012235 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-N/A, EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY BATTERY PACK. 2 L 7 4 4F RT 4A25 1998110600592 19981106 00592 WP 1998 11 6 UPS98828054 1 19981020 A 5320 47516251 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, CRACKED FRAME FITTING AT LONG 11L FS 680. REMOVED AND REPLACED FITTING IAW SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1998110600593 19981106 00593 WP 1998 11 6 UPS98828055 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 335.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 335.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW S RM 57-2-0. 2 L 7 4 4F RT 4A25 1998110600594 19981106 00594 WP 1998 11 6 UPS98828056 1 19981016 A 5720 TRIPLER DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING L/E INTERNAL TRIPLER ABOVE THE NR 3 PYLON AT THE L/E OF THE PYLON CUT OUT IS CRACKED. REPA IRED L/E SKIN IAW EO DC8-5720-4087. 2 L 7 4 4F RT 4A25 1998110600595 19981106 00595 WP 1998 11 6 UPS98828057 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 566.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING L/E RIB AT XFS 566.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998110600596 19981106 00596 WP 1998 11 6 UPS98828058 1 19981019 A 5720 975329424 ANGLE DOUG DC8 DC871F 302199D WP WS 256 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING L/E RIB AT XW 256, ABOVE THE NR 3 PYLON, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABR ICATED AND REPLACED CLIP IAW DWG 9753294 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998110600597 19981106 00597 WP 1998 11 6 UPS98828059 1 19981019 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 250 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING L/E RIB AT XS 250.089 IS CRACKED 6 INCHES FWD OF THE SPAR. STOP DRILLED AND REPAIRED RIB I AW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998110600598 19981106 00598 WP 1998 11 6 UPS98828060 1 19981020 A 5720 576960039 DOUBLER DOUG DC8 DC871F 302199D WP WS 570 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING L/E LWR SKIN AT XFS 570.75, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FA BRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1998110600599 19981106 00599 WP 1998 11 6 UPS98828061 1 19981019 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 372.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING L/E RIB AT XFS 372.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW S RM 57-2-0. 2 L 7 4 4F RT 4A25 1998110600600 19981106 00600 WP 1998 11 6 UPS98828062 1 19981019 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 360.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING LWR L/E RIB AT XFS 360.25 IS CRACKED BEYOND THE DOUBLER. REPAIRED RIB IAW SRM 57-2-0 FIG 2 . 2 L 7 4 4F RT 4A25 1998110600601 19981106 00601 WP 1998 11 6 UPS98828063 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 585 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 585.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED L/E RIB IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998110600602 19981106 00602 WP 1998 11 6 UPS98828064 1 19981019 A 5320 47504191 FITTING DOUG DC8 DC871F 302199D WP BS 1160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 INTERCOSTAL END FITTING CRACKED AT FS 1160, LONG 18R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 1998110600603 19981106 00603 WP 1998 11 6 UPS98828065 1 19981019 A 5320 3779659501N FITTNG DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 5L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED LONG END FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998110600604 19981106 00604 WP 1998 11 6 UPS98828066 1 19981019 A 5320 3779659501N FITTNG DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 8L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998110600605 19981106 00605 WP 1998 11 6 UPS98828067 1 19981019 A 5320 3779659501N FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 7L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998110600606 19981106 00606 WP 1998 11 6 UPS98828068 1 19981019 A 5320 3779659501N FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 4R END FITTING AT FS 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21 A ND 51-3-0. 2 L 7 4 4F RT 4A25 1998110600607 19981106 00607 WP 1998 11 6 UPS98828069 1 19981019 A 5320 3779659501N FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 3R END FITTING AT FS 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 1998110600608 19981106 00608 WP 1998 11 6 UPS98828070 1 19981019 A 5320 3779659501N FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 7R END FITTING AT FS 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 1998110600609 19981106 00609 WP 1998 11 6 UPS98828071 1 19981020 A 5320 531385635 GUSSET DOUG DC8 DC871F 302199D WP FUSELAGE BROKEN A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 FRAME GUSSET AT UPPER AFT CORNER OF F/O'S EYEBROW WINDOW IS BROKEN. REMOVED, FABRICATED AND REPLAC ED GUSSET IAW DWG 5313856 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998110600610 19981106 00610 WP 1998 11 6 UPS98828072 1 19981019 A 5320 3779659501N FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 8R END FITTING IS CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 5-1-20D, 51-1-21 AN D 51-3-0. 2 L 7 4 4F RT 4A25 1998110600611 19981106 00611 WP 1998 11 6 UPS98828073 1 19981019 A 5320 3779659501 FITTING DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LONG 6L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51- 3-0. 2 L 7 4 4F RT 4A25 1998110600612 19981106 00612 WP 1998 11 6 UPS98828074 1 19981015 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 6 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LT WING UPPER SKIN CRACKED AT FUEL PROBE AT XRS 6 AND STR 8. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998110600613 19981106 00613 WP 1998 11 6 UPS98828075 1 19981020 A 5320 36431121 ANGLE DOUG DC8 DC871F 302199D WP BS 798 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LWR FLOORBEAM WEB ATTACH ANGLE CRACKED AT FS 798 AND LBL 49. REMOVED AND REPLACED ANGLE IAW SRM 51 -1-20D. 2 L 7 4 4F RT 4A25 1998110600614 19981106 00614 WP 1998 11 6 UPS98828076 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 797.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 797.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW SR M 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998110600615 19981106 00615 WP 1998 11 6 UPS98828077 1 19981020 A 5320 3755822505 FITTING DOUG DC8 DC871F 302199D WP BS 320 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 BULGING CORROSION ON BATHTUB FITTING FWD SIDE FS 320 BETWEEN LONG 32L AND 33L. REMOVED AND REPLACE D FITTING IAW SRM 53-2-0, 51-1-20D. 2 L 7 4 4F RT 4A25 1998110600616 19981106 00616 WP 1998 11 6 UPS98828078 1 19981020 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 304 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 304.0 IS CRACKED AT THE FWD PNEU DUCT SUPPORT FITTING. STOP DRILLED CRACK A ND REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998110600617 19981106 00617 WP 1998 11 6 98FDEA00684 1 19981101 A 3234 HANDLE DOUG DC10 DC1010F 3022111 WP LANDING GEAR DIRTY A FDEA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 25 385FE 46619 LANDING GEAR DID NOT COME DOWN WITH THE HANDLE DOWN. WENT AROUND THEN GEAR CAME DOWN (FROM HANDLE DOWN TO GEAR DOWN WAS 3 MIN). PERF A/C GEAR SWING RETRACT AND EXTENSION CKS, GEAR OPS CK OK. A/C GEAR EXTENSION TIME FROM HAND DOWN TO 3 GR EEN DOWN AND LOCK 19.85 SEC. CLEAN GEAR HANDLE SLIDE TO PREVENT HANDLE STICK, CAUSING GEAR LIGHT TO STAY RED. GEAR HAN DLE OPS CK OK. 2 L 7 3 4F A22WE 1998110600618 19981106 00618 NM 1998 11 6 98UAL900370 1 19980803 A 2822 BOOST PUMP BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE NR 1 FUEL TANK MALFUNCTIONED A A UALA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 WP 29 917UA 25384 724640 NR 1 ENGINE SHUT DOWN. *S/D* REPLACED FUEL SHUTOFF VALVE GATE, ACTUATOR, FORWARD AND AFT FUEL BOOST PUMPS FOR THE NUMB ER ONE TANK. FOUND BOTH BOOST PUMPS NOT SUPPLING FUEL AT REQUIRED PRESSURE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998110600619 19981106 00619 NM 1998 11 6 98UAL900506 1 19981019 A 2420 WIRE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT GENERATOR BROKEN A UALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 WP 29 516UA 24860 RETURNED TO ORD DUE TO ELECTRICAL PROBLEMS. *S/D* W2018-0002-06 WAS FOUND BROKEN AT LEFT GENERATOR CIRCUIT BREAKER C90 1 PHASE B. LOSS OF PHASE B AT L GEN CB CAUSED PARTIAL ELECTRICAL FAILURE. THE BROKEN WIRE TERMINAL WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998110600620 19981106 00620 NM 1998 11 6 98UAL900515 1 19981024 A 3230 RETRACT MECH BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT MLG MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 655UA 25393 LEFT MAIN LANDING GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO SFO. 2 L 7 2 4F 4 F RT A1NM E24NE 1998110600621 19981106 00621 WP 1998 11 6 98UAL900516 1 19981027 A 3350 LIGHT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE CABIN INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 1856U 46975 EEL PATH LIGHTING INOP ON ENTIRE RIGHT SIDE OF ZONE A CABIN. FLEXIBLE EEL LAMP BENEATH AND JUST FORWARD OF VIDEO SYSTEM CABINET INOP. FOUND FEEDER DAMAGED. SPLICED IN NEW SECTION OF FEEDER AND SECURED WITH TAPE. REPLACED ENTIRE EEL LAMP ASSEMBLY WITH ATTACHED FEEDER SEGMENT AND SECURED WITH TAPE. ALL OP CHECKS GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1998110600622 19981106 00622 EU 1998 11 6 98UAL900517 1 19981028 A 3350 LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE SEAT 3B INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 421UA 500 EMERGENCY LIGHTS INOP AT SEAT 3B. 2 L 7 2 4F 4 F RT A28NM E40NE 1998110600623 19981106 00623 NM 1998 11 6 98UAL900518 1 19981028 A 2824 VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE SURGE TANK FAILED A UALA O OTHER J WARNING INDICATION CR CRUISE 1 WP 29 611UA 21872 FUEL CONFIG LIGHT ON WITH 1200 NR UNCOMMANDED TRANSFER TO CENTER TANK. SEVERAL LEAKS WERE FOUND FROM THE LEFT MAIN TANK INTO THE CENTER TANK. A LEAKING SCAVANGE LINE B NUT WAS CORRECTED BY REPLACING THE O-RING. A LEAKING SEAL AROUND THE SURGE TANK, DRAIN LINE WHERE IT ENTERS INTO THE CENTER TANKS, WAS REPAIRED BY RESEALING THE AREA, AND LASTLY THE SURGE T ANK DRAIN VALVE AND VACUUM VALVES WERE REPLACED. AFTER ALL ABOVE ACTIONS, THE LEAK WAS CORRECTED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998110600624 19981106 00624 WP 1998 11 6 ABXA9800931 1 19981030 A 3260 H146 SWITCH DOUG DC9 DC932 3022066 WP RT NLG DEFECTIVE A ABXA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 GL 23 902AX 47426 WHEN LANDING GEAR WAS EXTENDED, GEAR DOOR OPEN LIGHT WOULD NOT EXTINGUISH. RECYCLED GEAR, LIGHT WOULD NOT GO OUT WITH G EAR IN THE UP POSTION. PERFORMED ABNORMAL PROCEDURE. LANDING WAS UNEVENTFUL. REPLACED RIGHT INBOARD GEAR DOWN SWITCH. 2 L 7 2 4F A6WE 1998110600625 19981106 00625 WP 1998 11 6 ABXA9800932 1 19981030 A 3350 5768458303 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DEPLETED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816AX 46093 ON PRE-DEPARTURE CHECK, FOUND EMERGENCY LIGHT SYSTEM INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY RACK. 2 L 7 4 4F 4A25 1998110600626 19981106 00626 WP 1998 11 6 RRXA98450 1 19981103 A 5311 5642861503 FRAME DOUG DC8 DC862 3021970 WP BS 834 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND A HOLE IN RADIUS OF FRAME STA 834 AT LONGERON 11R. REMOVED TIE PLATE, INSTALLED FASTE NER IN HOLE, REINSTALLED TIE PLATE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R78, AREA TREATED IAW DC-8 SRM 51- 1-8. 2 L 7 4 4F 4A25 1998110600627 19981106 00627 WP 1998 11 6 RRXA98451 1 19981103 A 5311 5750117501 FRAME DOUG DC8 DC862 3021970 WP FRAME 780 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 780 MISDRILLED HOLES BETWEEN LONGERONS 18, 19, 20 RIGHT. FABRICATED AND INSTALLED GUSSETS AND SPLICES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R105, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600628 19981106 00628 WP 1998 11 6 RRXA98452 1 19981103 A 5311 5640229521 FRAME DOUG DC8 DC862 3021970 WP FRAME 1240 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND HOLE IN RADIUS OF FRAME 1240 BETWEEN LONGERONS 11 AND 12 RIGHT. PLUGGED HOLE IN FRAME I AW FAA APPROVED DER COTNEY ENGINEERING RFTS 98-351 DATED 7-22-98. 2 L 7 4 4F 4A25 1998110600629 19981106 00629 WP 1998 11 6 CKSA98624 1 19981010 A 2130 NASI SYST DOUG DC8 DC861 3021952 WP NR 3 ENGINE ODOR A CKSA K NONE O OTHER TX TAXI/GRND HDL 1 GL 23 817CK 45887 RIGHT NASI SYSTEM HAS BURNT SMELL WHEN TURNED ON. SUSPECT NR 3 ENGINE. ACCOMPLISHED NR 3 AND NR 4 ENGINE RUN. NO SMEL L NOTED ON GROUND AS PER DC-8 MM NAS 21-00-00. 2 L 7 4 4F 4A25 1998110600630 19981106 00630 NE 1998 11 6 CKSA98625 2 19981025 A 7200 ENGINE BOEING 747 747269B NM PWA JT9 JT9D7J 52054 NE NR 1 FLAMED OUT A CKSA O OTHER X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 GL 23 708CK 21543 689468 NR 1 ENGINE FLAMED OUT AT 39,000 FT. ATTEMPTED RELIGHT, EGT WAS GOING TO EXCEED START LIMITS. SHUTDOWN, DESCENDED TO 3 1,000 FT ATTEMPTED RELIGHT. STARTED AND RAN NORMALLY. SUMPED FUEL TANKS, OPS CHECK NR 1 ENGINE FUEL PUMP FP-12 AND FP- 3 ALL IN LIMITS. PERFORMED WINDMILLING INSPECTION, NO DISCREPANCIES. PERFORMED ENGINE RUN UP, ALL PARAMETERS NORMAL. 2 L 7 4 4F 4 F RT A20WE E20EA 1998110600631 19981106 00631 NE 1998 11 6 TC8A98076 2 19981030 A 7230 BLADE DOUG DC8 DC8F54 3021926 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE DENTED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 802CK 45679 642684 COMPRESSOR STALL NR 3 ENGINE DURING TAKEOFF ROLL, APPROXIMATELY 60 KNOTS, ANTI-ICE OFF. INSPECTED COMPRESSOR AND TURBIN E IAW PW 72-0, PG 118, NO DEFECTS NOTED. INSPECTED INLET, FOUND 1 BLADE DENTED, BLENDED AND INSPECTED IAW PG 602/604. 2 L 7 4 4F 4 F 4A25 1E8 1998110600637 19981106 00637 NE 1998 11 6 98ZZZX3998 1 19981001 A 7712 7645001078119 TRANSMITTER SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL NR 2 ENGINE FAILED A HEEA A UNSCHED LANDING O OTHER TO TAKEOFF 1 SW 03 5426U 760167 CAE8905085 ON TAKEOFF, NR 2 ENGINE TORQUE DROPPED WITH A CONTINUING RISE IN ENGINE TEMPERATURE. PILOT RETARDED NR 2 ENGINE AND MAD E AN UNEVENTFUL LANDING. MAINTENANCE FOUND DEFECTIVE NR 2 ENGINE TORQUE TRANSMITTER. REF: ALLISON C-30 IPC, CHAPTER 7 3-32-00, FIG 1-18. 1 G 7 2 3U 3 U H1NE E1GL 1998110600645 19981106 00645 EA 1998 11 6 98ZZZX4007 2 19980626 A 8530 SL10456597Z VALVE GULSTM 680 680FL 0141608 SW LYC O540 IGSO540B1A 41532 EA LT ENGINE FAILED A HSYA O OTHER R J K PARTIAL RPM/PWR LOSS WARNING INDICATION FLUID LOSS CR CRUISE 1 NM 05 680AC 39 1603115 BIL - PILOT REPORTED A LOSS OF MANIFOLD PRESSURE ON THE LT ENGINE IN CRUISE AND OIL LEAKING FROM LT ENGINE AFTER SHUT DO WN IN BILLINGS. AIRCRAFT LANDED WITHOUT INCIDENT, NO EMERGENCY DECLARED. LEFT ENGINE, NR 2 CYLINDER EXHAUST VALVE FAIL ED, DAMAGE CAUSED TO CYLINDER, PISTON AND CYLINDER SUBASSEMBLIES. ALL DAMAGED COMPONENTS WILL BE REPLACED WITH SERVICEA BLE COMPONENTS AND OPERATIONALLY CHECKED. 1 H 7 2 3O 3 O 2A4 1E7 1998110600646 19981106 00646 EA 1998 11 6 98ZZZX4008 2 19980610 A 8530 5015 CYLINDER GULSTM 680 680FL 0141608 SW LYC O540 IGSO540B1A 41532 EA NR 2 ENGINE CRACKED A HSYA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 NM 05 4704E 1047 144176 FCA - FLT 5032 - PILOT OBSERVED NR 2 TURBO QUIT ON APPROACH, ENGINE MADE KNOCKING SOUND, AND PILOT SHUT DOWN NR 2 ENGINE . NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. NR 2 ENGINE, NR 3 CYLINDER PARTED WITH BROKEN CYLINDER STU DS. ENGINE WILL BE REPLACED WITH SERVICEABLE ENGINE. TEAR-DOWN AND EVALUATION TO BE PERFORMED ON FAILED ENGINE. ENGIN E TSO: 1,046.7 HOURS. 1 H 7 2 3O 3 O 2A4 1E7 1998110600647 19981106 00647 SW 1998 11 6 98ZZZX4009 1 19980731 A 3213 48NBC2060YZP BEARING GULSTM 680 680FL 0141608 SW LT MLG LACK OF LUBE A HSYA K NONE O OTHER IN INSP/MAINT 1 NM 05 113NA 1794149 BIL - DURING SCHEDULED MAINTENANCE INSPECTION, THE LEFT MAIN LANDING GEAR STRUT LOWER LEG WAS FOUND BINDING WITHIN THE P IVOT BEARINGS BETWEEN THE LOWER LEG AND UPPER BARREL. CONTAMINATION OF BEARINGS, DRY, NO LUBRICATION. LEFT STRUT ASSY WILL BE DISASSEMBLED, NON-DESTRUCTIVELY, TESTED AND INSPECTED, AND RE-ASSEMBLED USING SERVICEABLE PARTS. 1 H 7 2 3O 2A4 1998110600670 19981106 00670 NM 1998 11 6 K3HA980131 1 19981026 A 3350 079123 LENS BOEING 727 727225 1384077 NM ROW 1 ABC MISSING A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 361KP 20627 RED EMERGENCY PATH LIGHT LENS MISSING AT ROW 1ABC. INSTALLED LENS PER MM 33-50, OPS CHECK OK. 2 L 7 3 4F A3WE 1998110600671 19981106 00671 NM 1998 11 6 K3HA980132 1 19981028 A 3350 BULB BOEING 727 727225 1384077 NM ROW 19 ABC FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHT BULB OUT OF SOCKET AT ROW 19ABC. REPLACED BULB INTO SOCKET TESTED MM 33-50-0. 2 L 7 3 4F A3WE 1998110600672 19981106 00672 NM 1998 11 6 AWXA9800217 1 19981030 A 2170 COALESCER BAG BOEING 737 73733A 1384673 NM CABIN DIRTY A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 28 172AW 23631 A/C TOOK A DELAY FOR A REPORT OF ELECTRICAL SMELL AND SMOKE IN THE AFT CABIN AREA AROUND ROW 20. PHX TECH SUPPORT LOWER ED CEILING AND PSU'S FROM ROW 18 AFT, INSPECTED ALL AREAS ON PSU, CEILING, GALLEY'S AND LAV'S. LOWERED CEILING AND PSU' S ROW 18 AFT, CHECKED ALL PSU'S, CEILING AFT GALLEY AND LAV LIGHTING AND ELECTRICAL COMPONENTS AND NO DEFECTS NOTED. RA N RT PAX ON MAX HOT, FOUND HOT SMELL. TROUBLESHOT TO DIRTY SEPARATOR BAG. REMOVED AND REPLACED PER CARD S2C21004, RAN PAC OPS CK GOOD. 2 L 7 2 4F RT A16WE 1998110600673 19981106 00673 NM 1998 11 6 AWXA9800218 1 19981029 A 3350 LIGHT BOEING 737 7372A6 138448B NM DOOR R2 INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 145AW 30509 20194 EMERGENCY EXIT LT ABOVE DOOR R2 INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY IAW BMM 2560, OPS TEST GOOD. 2 L 7 2 4F A16WE 1998110600674 19981106 00674 NM 1998 11 6 CALA9802022 1 19981103 A 5347 SEAT TRACK BOEING 727 727232 1384082 NM BS 1090-1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND SEAT TRACK CORRODED IN RT AFT GALLEY AREA AT STA 1090 TO 1110, RBL 20. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-10-5 AND 51-30-2. 2 L 7 3 4F A3WE 1998110600675 19981106 00675 NM 1998 11 6 CALA9802023 1 19981103 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1130-1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND RT AFT LAV DOOR ENDWALL ANGLE AND HAT BRACKET CORRODED AT STA 1130 TO 1183, RBL 20. A REPAIR WAS INSTA LLED IAW SRM 51-40-2 AND 51-30-2. 2 L 7 3 4F A3WE 1998110600676 19981106 00676 NM 1998 11 6 CALA9802024 1 19981103 A 5310 STRUCTURE BOEING 727 727232 1384082 NM RT AFT LAV CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND RT AFT LAV SUBFLOOR CORRODED. THE CORRODED AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2 PAGE 4, 51-10-6 PAGE 2 AND 51-10-2 PAGE 1. 2 L 7 3 4F A3WE 1998110600677 19981106 00677 NM 1998 11 6 CALA9802025 1 19981103 A 5320 CHANNEL BOEING 727 727232 1384082 NM BS 1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND RT AFT LAV FORWARD HAT CHANNEL FOR WALL CORRODED AT STA 1140, RBL 20 TO WALL. THE HAT CHANNEL WAS REMO VED AND REPLACED IAW SRM 51-30-2 PAGE 4. 2 L 7 3 4F A3WE 1998110600678 19981106 00678 NM 1998 11 6 CALA9802026 1 19981103 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 320 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND FLOORBEAM CORRODED AT STA 320, LBL 20 TO 48. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT IAW SRM 53- 10-8. REPAIR ANGLES WERE INSTALLED IAW SRM 53-10-8 AND 51-10-2 PAGE 12. 2 L 7 3 4F A3WE 1998110600679 19981106 00679 NM 1998 11 6 CALA9802027 1 19981103 A 5411 FRAME BOEING 727 727232 1384082 NM FRAME 1303 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND THREE .75 INCH CRACKS IN VERTICAL FIN FRAME ON TOP OF S-DUCT AT FRAME 1303. A REPAIR WAS INSTALLED IAW SRM 51-40-2 PAGE 1 AND 51-30-2 PAGE 4. 2 L 7 3 4F A3WE 1998110600680 19981106 00680 NM 1998 11 6 CALA9802028 1 19981103 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 1 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A .5 INCH CRACK IN O/B LOWER END OF SUPPORT BRACKET WHERE LT WING NR 1 L/E FLAP ACTUATOR MOUNTS INSIDE LEADING EDGE. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2 AND 51-20-2 FIGURE 7. 2 L 7 3 4F A3WE 1998110600681 19981106 00681 NM 1998 11 6 CALA9802029 1 19981103 A 5712 RIB BOEING 727 727232 1384082 NM LT WING-TIP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 2.5 INCH CRACK IN LT WING TIP RIB INSIDE OVAL ACCESS CUTOUT 8111. A REPAIR WAS ACCOMPLISHED IAW SRM 51-40-3, PAGE 3. 2 L 7 3 4F A3WE 1998110600682 19981106 00682 NM 1998 11 6 CALA9802030 1 19981103 A 5753 PLATE BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.25 INCH CRACK IN PLATE INSIDE LT I/B MIDFLAP AT I/B CARRIAGE SPINDLE CUTOUT ACCESS THROUGH PANEL 84 43. THE PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 57-50-4 FIGURE 4. 2 L 7 3 4F A3WE 1998110600683 19981106 00683 NM 1998 11 6 CALA9802031 1 19981103 A 5754 CHORD BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A .3125 INCH CRACK IN LOWER CHORD OF LT WING NR 2 SLAT AT CUTOUT BELOW TELESCOPING ANTI-ICE TUBE. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-40-4 PAGE 11 AND 51-10-1 PAGE 6B. 2 L 7 3 4F A3WE 1998110600684 19981106 00684 NM 1998 11 6 CALA9802032 1 19981104 A 5320 SHEAR TIE BOEING 727 727232 1384082 NM BS 720 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND FRAME TO SKIN SHEAR TIE CORRODED AT STA 720C, STRINGER 28R TO 28L. A REPAIR WAS INSTALLED IAW SRM 53-1 0-4 PAGE 52. 2 L 7 3 4F A3WE 1998110600685 19981106 00685 NM 1998 11 6 CALA9802033 1 19981104 A 5753 RIB BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A .5 INCH CRACK IN LT O/B MIDFLAP I/B MOST RIB. THE CRACK WAS STOP DRILLED AND A REINFORCING ANGLE WAS INSTALLED IAW SRM 51-40-3 AND 51-10-2. 2 L 7 3 4F A3WE 1998110600686 19981106 00686 NM 1998 11 6 CALA9802034 1 19981104 A 5320 STIFFENER BOEING 727 727232 1384082 NM BS 300 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND STIFFENER IN NOSE WHEEL WELL AT FS 300, RBL 12 TO LBL 12 CORRODED. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-10-1. 2 L 7 3 4F A3WE 1998110600687 19981106 00687 WP 1998 11 6 ABXA9800942 1 19981103 A 3234 HANDLE DOUG DC8 DC862 3021970 WP LANDING GEAR LACK OF LUBE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 801AX 46077 ON APPROACH, WHEN GEAR EXTENDED HAD UNSAFE LIGHT AND NO GREEN DOWN INDICATION. RECYCLED GEAR, ALL INDICATIONS NORMAL. F OUND GEAR HANDLE STIFF. LUBRICATED HANDLE AND DOWNLOCK, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998110600688 19981106 00688 WP 1998 11 6 MWEA981029 1 19981103 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP BS 69 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND TWO CORROSION BLENDOUTS OUT OF LIMITS ON FORWARD SIDE OF STATION 69T. MTC FABRICATED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998110600690 19981106 00690 NM 1998 11 6 SCNA98134 1 19981031 A 7931 42D107A1 SWITCH BOEING 727 727227 1384078 NM NR 1 ENGINE FAILED A SCNA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 GL 15 275AF 9323 22092 DURING CLIMBOUT, THE NUMBER ONE ENGINE OIL PRESSURE LOW LIGHT ON FILTER BYPASS INDICATOR. RETURNED AIRCRAFT TO LAS. RE MOVED AND REPLACED BYPASS DIFFERENTIAL PRESSURE SWITCH REF MM 793300. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998110600691 19981106 00691 EA 1998 11 6 SWIA971293 2 19981020 A 7530 CONTROL UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT BLEED AIR MALFUNCTIONED A SWIA E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 NM 07 403SW 7028 THE L 14TH DUCT WARNING MESSAGE ON IN FLIGHT. LEFT ENGINE PRECAUTIONARY SHUT DOWN ACCOMPLISHED. REMOVED AND REPLACED L EFT BLEED AIR CONTROL UNIT, IAW CRJ MM 36-21-10. 2 L 7 2 4F 4 F RT A21EA E15NE 1998110600692 19981106 00692 1998 11 6 SWIA971294 4 19981021 A 3414 39948E2903 IAS INDICATOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT COCKPIT LEAKING A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 156CA 120156 ON TAKEOFF, FO'S AIRSPEED, ALTIMETER AND VSI VERY ERRATIC. ALTIMETER AS MUCH AS 1,500 FEET BEHIND CAPTAINS. AIRSPEED I NDICATOR 0 KNOTS MOST OF THE TIME. RETURNED TO SEA. COPILOTS IAS INDICATOR HAS A STATIC LEAK. REMOVED AND REPLACED CO PILOTS IAS INDICATOR IAW MM 34-12-01. TESTED IAW MM 34-11-00. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998110600693 19981106 00693 SO 1998 11 6 SWIA971295 1 19981023 A 5270 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE FUEL DOOR OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 203SW 120240 SERVICE DOOR LIGHT CAME ON IN FLIGHT. RETURNED TO FIELD. ADJUSTED FUEL DOOR MICRO-SWITCHES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998110600694 19981106 00694 SO 1998 11 6 SWIA971296 1 19981028 A 3010 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT WING FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 LEADING EDGE DEICE OUTBOARD LEFT AND RIGHT FAILED BOTH TIMERS IN HEAVY AND LIGHT CYCLES AFTER APPROX 6-8 SECONDS. RETUR NED TO FIELD. REPLACED OUTBOARD BOOT DEICE EJECTOR VALVE. GROUND RAN 15 MINUTES, CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998110600696 19981106 00696 SO 1998 11 6 SWIA971298 1 19981101 A 7920 LINE EMB 120 EMB120RT SO PWA 118 PW118 NE OIL COOLER FAILED A SWIA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 NM 07 162CA 120150 RIGHT ENGINE LOST OIL PRESSURE ON DESCENT. PRESSURE DROPPED BELOW 40 PSI AND ENGINE HAD TO BE SHUT DOWN. REPLACED OIL COOLER CROSS FLOW LINE. RAN ENGINE, LEAK AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998110600697 19981106 00697 SO 1998 11 6 SWIA971299 1 19981101 A 3010 DEICE BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT WING FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 ON CLIMB, OUTBOARD WING BOOTS FAILED BOTH TIMERS, BOTH CYCLES. RETURNED TO FIELD. REMOVED AND REPLACED OUTBOARD WING D EICE BOOT IAW MM. 2 L 7 2 4T 4 T RT A31SO E20NE 1998110600698 19981106 00698 SO 1998 11 6 SWIA971300 1 19981031 A 3010 DEICE BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT HORIZ STAB FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 308SW 120326 ON CLIMB, LEFT OUTBOARD STABLIZER DEICE BOOT FAILED, BOTH TIMERS. RETURNED TO FIELD. RAN BOTH ENGINES BUT COULD NOT DU PLICATE ON GROUND ON ALL SETTINGS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998110600699 19981106 00699 WP 1998 11 6 RRXA98467 1 19981104 A 5311 5640222523 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1100 WITH MISDRILLED HOLES AT LONGERONS 8 RIGHT AND BETWEEN LONGERONS 12 AND 13 RI GHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAPS AND FILLER IAW FAA APPROVED ACMI SKETCH SK98374 AND DC-8 SRM 51-1-21 , AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600700 19981106 00700 WP 1998 11 6 RRXA98468 1 19981104 A 5311 5642856507 FRAME DOUG DC8 DC862 3021970 WP FRAME 717 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 717 WITH MISDRILLED HOLES AT LONGERONS 9 AND 10 LEFT. ALSO LONGERON 11 LEFT INTER COSTAL MISDRILLED IN THE RADIUS. REMOVED CLIPS AND LOOSENED STRAPS, PLUGGED MISDRILLED HOLES IAW DC-8 SRM 51-1-21, FABR ICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA APPROVED ACMI SKETCH SK98260, HEAT TREATED IAW DC-8 SRM 51-1-1, ARE A TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600701 19981106 00701 WP 1998 11 6 RRXA98469 1 19981104 A 5311 5750180511 FRAME DOUG DC8 DC862 3021970 WP FRAME 1040 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1040 WITH HOLE IN RADIUS BETWEEN LONGERONS 10 AND 11 RIGHT. FABRICATED AND INSTA LLED REPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R73, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600702 19981106 00702 WP 1998 11 6 RRXA98470 1 19981104 A 5311 5750180511 FRAME DOUG DC8 DC862 3021970 WP FRAME 1040 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1040 WITH MISDRILLED HOLES AT LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED R EPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R73 AND DC-8 SRM 51-1-21, AREA TREATED IAW DC- 8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600703 19981106 00703 WP 1998 11 6 RRXA98471 1 19981104 A 5311 5755074507 FRAME DOUG DC8 DC862 3021970 WP FRAME 1220 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1220 WITH MISDRILLED HOLES IN RADIUS BETWEEN LONGERONS 7 AND 11 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R72, AREA TREATED IAW DC-8 SRM 5 1-1-8. 2 L 7 4 4F 4A25 1998110600704 19981106 00704 WP 1998 11 6 RRXA98472 1 19981104 A 5311 5640230515 FRAME DOUG DC8 DC862 3021970 WP FRAME 1260 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1260 WITH MISDRILLED HOLES IN RADIUS AT LONGERONS 8, 9, 11 AND 13 RIGHT. FABRICAT ED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R71, HEAT TREATED ANGLE IAW DC-8 SRM 51-1-1, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600705 19981106 00705 WP 1998 11 6 RRXA98473 1 19981104 A 5311 5612148501 FRAME DOUG DC8 DC862 3021970 WP FRAME 1586 CHAFED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1586 CHAFED AND DRILL MARKS AT LONGERON 27 TO 31 LEFT. REMOVED FASTENERS AND BLEN DED FRAME, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R61. 2 L 7 4 4F 4A25 1998110600706 19981106 00706 WP 1998 11 6 RRXA98474 1 19981104 A 5311 5640219517 FRAME DOUG DC8 DC862 3021970 WP FRAME 1000 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1000 WITH MISDRILLED HOLES AND GOUGES BETWEEN LONGERONS 7 AND 11 RIGHT. FABRICATE D AND INSTALLED REPAIR ANGLES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R82. 2 L 7 4 4F 4A25 1998110600707 19981106 00707 WP 1998 11 6 RRXA98475 1 19981104 A 5311 5779772515 FRAME DOUG DC8 DC862 3021970 WP FRAME 1020 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1020 WITH MISDRILLED HOLES BETWEEN LONGERONS 7 AND 9 RIGHT. FABRICATED AND INSTA LLED REPAIR STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R81, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600708 19981106 00708 WP 1998 11 6 RRXA98476 1 19981104 A 5311 5640224513 FRAME DOUG DC8 DC862 3021970 WP FRAME 1140 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1140 WITH MISDRILLED HOLE IN RADIUS AT LONGERONS 16 AND 19 RIGHT. FABRICATED AND INSTALLED STRAP AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R07, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600709 19981106 00709 WP 1998 11 6 RRXA98477 1 19981104 A 5311 5640234503 FRAME DOUG DC8 DC862 3021970 WP FRAME 1340 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1340 WITH MISDRILLED HOLES BETWEEN LONGERONS 6 AND 9 RIGHT. FABRICATED AND INSTAL LED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R84, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998110600710 19981106 00710 WP 1998 11 6 RRXA98478 1 19981104 A 5311 5640242507 FRAME DOUG DC8 DC862 3021970 WP FRAME 1500 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1500 WITH MISDRILLED HOLES AT LOWER AFT DOOR FRAME. FABRICATED AND INSTALLED REPA IR ANGLE AND CLIP, INSTALLED NEW CUSP WEB AND FITTING IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R99 AND RFTS 98 -420. 2 L 7 4 4F 4A25 1998110600711 19981106 00711 WP 1998 11 6 RRXA98479 1 19981104 A 5311 5640243527 FRAME DOUG DC8 DC862 3021970 WP FRAME 1520 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1520 WITH MISDRILLED HOLES AT LONGERONS 8 AND 9 RIGHT. FABRICATED AND INSTALLED R EPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R83. 2 L 7 4 4F 4A25 1998110600712 19981106 00712 WP 1998 11 6 ARWA981102 1 19981104 A 3230 PIN DOUG DC8 DC863F 302198F WP RT MLG BROKE A ARWA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 19 661AV 45969 AIR TURNBACK, RIGHT MLG RETRACT CYLINDER PIN BROKEN OFF. GEAR WOULD NOT RETRACT. DUMPED 40,000 LBS OF FUEL. AIRCRAFT WILL BE FERRY TO MIAMI, GEAR DOWN FOR MAINTENANCE PURPOSES. 2 L 7 4 4F 4A25 1998110600713 19981106 00713 NM 1998 11 6 VNAA9810023 1 19981028 A 7603 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 425JS 3037 DURING THE TAKEOFF, THE LEFT HAND ENGINE POWER CONTROL LEVER WOULD NOT ADVANCE ABOVE FLIGHT IDLE, WHEN SELECTED BY THE C REW. THE AIRCRAFT ABORTED THE TAKEOFF, AND RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED, CLEANED AND LUBRICA TED, THE LEFT HAND POWER LEVER CONTROL TRIGGER LOCK. OPERATIONAL CHECKS WERE COMPLETED, IN ACCORDANCE WITH DORNIER MAIN TENANCE MANUAL 76-11-10. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998110600714 19981106 00714 WP 1998 11 6 CKSA98626 1 19981103 A 5347 SEAT TRACK DOUG DC8 DC861 3021952 WP BS 1680-1750 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 5600-0551, FOUND SEAT TRACK AT FS 1680 TO 1750 CORRODED. REMOVED CORROSI ON, FOUND TO BE OUT OF LIMITS PER DC-8 SRM 53-2-3. REPAIRED IAW ZANTOP DRAWING 86302. FOUND AT OSC MAINTENANCE FACILIT Y DURING ACCOMPLISHMENT OF B-CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-302. NON ROUTINE TASK CARD NUMBER 44479. 2 L 7 4 4F 4A25 1998110600715 19981106 00715 WP 1998 11 6 CKSA98627 1 19981103 A 5347 SEAT TRACK DOUG DC8 DC861 3021952 WP BS 1680-1750 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 5600-0551, FOUND SEAT TRACK AT FS 1680 TO 1750 CORRODED. REMOVED CORROSI ON, FOUND TO BE OUT OF LIMITS PER DC-8 SRM 53-2-3. REPAIRED IAW ZANTOP DRAWING 86302. FOUND AT OSC MAINTENANCE FACILIT Y DURING ACCOMPLISHMENT OF B-CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-302. NON ROUTINE TASK CARD NUMBER 44480. 2 L 7 4 4F 4A25 1998110600716 19981106 00716 WP 1998 11 6 CKSA98628 1 19981103 A 5347 SEAT TRACK DOUG DC8 DC861 3021952 WP BS 1680-1766 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 5600-0551, FOUND SEAT TRACK AT FS 1680 TO 1766, RBL 24 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS PER DC-8 SRM 53-2-3. REPAIRED IAW ZANTOP DRAWING 86302. FOUND AT OSC MAINTENANCE FACILITY DURING ACCOMPLISHMENT OF B-CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-302. NON ROUTINE TASK CARD NUMBER 44481. 2 L 7 4 4F 4A25 1998110600717 19981106 00717 WP 1998 11 6 CKSA98629 1 19981103 A 5347 SEAT TRACK DOUG DC8 DC861 3021952 WP BS 1754 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 DURING ACCOMPLISHMENT OF CPCP TASK CARD NUMBER 5600-0551, FOUND SEAT TRACK SPLICE AT FS 1754 CORRODED. REMOVED CORROSIO N, FOUND TO BE OUT OF LIMITS PER B727 SRM 53-10-01. REPAIRED IAW ZANTOP DRAWING 86302. FOUND AT OSC MAINTENANCE FACILI TY DURING ACCOMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-302. NON ROUTINE TASK CARD NUMBER 44484. 2 L 7 4 4F 4A25 1998110600718 19981106 00718 WP 1998 11 6 CKSA98630 1 19981103 A 5320 WEB DOUG DC8 DC861 3021952 WP BS 8-99 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 COCKPIT FLOOR WEB AND FINGER DOUBLERS CORRODED AT STA -99 TO STA -8, LBL 97. REMOVED CORROSION IAW SRM 53-2-0 FIG 1F. F ABRICATED AND INSTALLED REPAIR PARTS IAW AIA EA D8-53-040 AND EDR D8-06232. FOUND AT OSC MAINTENANCE FACILITY DURING AC COMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-303. NON ROUTINE TASK CARD N UMBER 44492. 2 L 7 4 4F 4A25 1998110600719 19981106 00719 WP 1998 11 6 CKSA98631 1 19981103 A 5313 STRINGER DOUG DC8 DC861 3021952 WP FUSELAGE CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 STRINGER 21R AT RT SUB FLOOR BELOW FLT ENGR TABLE AFT BASE, APPROX 3 AREA OF CORROSION. REMOVED CORROSION IAW SRM 51-1- 8, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-2-1. FOUND AT OSC MAINTENANCE FACILITY DURING ACCOMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-303. CPCP TASK CARD NUMBER 4660-0551. NON ROUTINE TASK CARD NUMBER 44495. 2 L 7 4 4F 4A25 1998110600720 19981106 00720 WP 1998 11 6 CKSA98632 1 19981103 A 5313 STRINGER DOUG DC8 DC861 3021952 WP BS 1640-1650 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 AFT ACC COMPT STRINGER AT FS 1640 TO 1650, BETWEEN S-20R AND S-22R HAS SMALL AREA OF CORROSION. REMOVED CORROSION IAW S RM 51-1-8. FOUND TO BE OUT OF LIMITS IAW 53-2-0 FIG 1F. REPAIRED IAW SRM 51-1-4 AND AIA EDR D8-06233, SRM 53-2-2 FIG 1 0. FOUND AT OSC MAINTENANCE FACILITY DURING ACCOMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-302. CPCP TASK CARD NUMBER 5600-0551. NON ROUTINE TASK CARD NUMBER 44601. 2 L 7 4 4F 4A25 1998110600721 19981106 00721 WP 1998 11 6 CKSA98633 1 19981103 A 5311 FRAME DOUG DC8 DC861 3021952 WP BS 1746 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 CORROSION FOUND ON FRAME AT FS 1746.621 FROM STRINGER 34R TO STRINGER 34L. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW 53-2-0. REPAIRED IAW SRM 53-2-0 FIG 2. FOUND AT OSC MAINTENANCE FACILITY DURING ACCOMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817-302. CPCP TASK CARD NUMBER 5600-0551. NON ROUTINE TASK CARD NUMBER 44605. 2 L 7 4 4F 4A25 1998110600722 19981106 00722 WP 1998 11 6 CKSA98634 1 19981103 A 5320 WEB DOUG DC8 DC861 3021952 WP BS 67 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 817CK 45887 AT FS -67 LT APPROX S-21L CORROSION ON STIFFENER WEB. REMOVED CORROSION, REPAIRED IAW SRM 53-2-0 FIG 1D. FOUND AT OSC MAINTENANCE FACILITY DURING ACCOMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDER NUMBER 817 -303. CPCP TASK CARD NUMBER 4660-0551. NON ROUTINE TASK CARD NUMBER 44698. 2 L 7 4 4F 4A25 1998110600723 19981106 00723 WP 1998 11 6 CKSA98635 1 19981102 A 5313 STRINGER DOUG DC8 DC8F55 3021928 WP BS 1480 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161M 45762 CORROSION FOUND AT STA 1480 APPROX 4 AREA STRINGER 33R. REMOVED CORROSION IAW SRM 53-1-0. REMOVED DAMAGED AREA AND REP AIRED IAW SRM 53-2-1 FIG 7. FOUND AT OSC MAINTENANCE FACILITY DURING ACCOMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-05 51 CPCP TASK CARDS. WORK ORDER NUMBER 61M-350. CPCP TASK CARD NUMBER 5600-0551. NON ROUTINE TASK CARD NUMBER 44704. 2 L 7 4 4F 4A25 1998110600724 19981106 00724 WP 1998 11 6 CKSA98636 1 19981102 A 5330 SKIN DOUG DC8 DC8F55 3021928 WP BS 1320 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 6161M 45762 FOUND AT STATION 1320, STRINGER 35R AN AREA OF BULGING SKIN. REMOVED CORROSION IAW SRM 51-1-8. FOUND TO BE OUT OF LIMI TS IAW SRM 53-2-0. INSTALLED CLASS II REPAIR IAW DC-8 SRM 53-2-1. THIS REPAIR HAS BEEN PUT ON REPETATIVE INSPECTION. F OUND AT OSC MAINTENANCE FACILITY DURING ACCOMPLISHMENT OF B CHECK AND 60 MONTH AND 5600-0551 CPCP TASK CARDS. WORK ORDE R NUMBER 61M-364. CPCP TASK CARD NUMBER 5600-0551. NON ROUTINE TASK CARD NUMBER 44706. 2 L 7 4 4F 4A25 1998111000001 19981110 00001 WP 1998 11 10 ARWA981018 1 19981016 A 2781 COMPARATOR LKHEED 1011 10113851 5265010 WP LT FLAPS DIRTY A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 307GB 193U1131 AIR TURNBACK, LE TRANS LIGHT ON AFTER SLAT RETRACTION. FLAPS RECYCLED, LE TRANS LIGHT REMAINED ON. LIGHT WENT OUT WHEN FLAPS WERE RETRACTED AFTER LANDING. CLEANED AND RESEATED THE SLAT ASYMMETRY COMPARATOR. ALSO, CHECKED BOTH SLAT ASYMM ETRY BRAKE TRANSDUCER SW AND VALVE FOUND TO BE NORMAL. OPS CHECK NORMAL IAW M/M 27-81-36. FALSE INDICATION. 2 L 7 3 4F RT A23WE 1998111000002 19981110 00002 WP 1998 11 10 VJ9800542 1 19981016 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP LI DOOR DISLODGED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 917VV 47323 FWD CABIN MAIN PASSENGER DOOR SLIDE COVER DISLODGED WHEN OPENED AT JET BRIDGE. REINSTALLED AND PERFORMED REQUIRED INSPE CTION. 2 L 7 2 4F A6WE 1998111000003 19981110 00003 WP 1998 11 10 UPS98827931 1 19980915 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 160 GOUGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 798UP 45898 INSPECTION TYPE:C2 FWD LWR CARGO STA 160 RBL 50 FLOORBEAM HAS GOUGE AROUND THE HI-LOK REPAIRED IAW REO5465. 2 L 7 4 4F RT 4A25 1998111100001 19981111 00001 NM 1998 11 11 DHL98742003 1 19980519 A 2840 1061803173 SOCKET BOEING 727 727225 1384077 NM COCKPIT INOPERATIVE A DHLA A G UNSCHED LANDING O2 MASK DEPLOYED B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 742DH 21290 IN CRUISE, NR 1 TANK FORWARD FUEL BOOST PUMP LOW PRESSURE LIGHT SOCKET EMITTED SMOKE. DEFERRED PER MEL 28-6. LIGHT SOC KET WIRES CAPPED AND STOWED. 2 L 7 3 4F A3WE 1998111100002 19981111 00002 NE 1998 11 11 COMA9810237 2 19981015 A 7321 789415008 EEC EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A COMA D RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 164D 17928 1164 LEFT ENGINE EEC FAILED ON TAKEOFF. REPLACED LEFT ENGINE EEC. 2 L 7 2 4T 4 T RT A31SO E20NE 1998111100003 19981111 00003 SO 1998 11 11 COMA9810238 1 19981019 A 3230 PIN EMB 120 EMB120RT SO NLG NOT REMOVED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 247CA 1225 NOSE LANDING GEAR WOULD NOT RETRACT. REMOVED NLG PIN. GEAR SWINGS GOOD. 2 L 7 2 4T RT A31SO 1998111100004 19981111 00004 WP 1998 11 11 VJ9800556 1 19981021 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 966VV 47168 COCKPIT ENTRANCE EMERGENCY EXIT LIGHT INOP. REPLACED POWER PACK BATTERIES, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998111100006 19981111 00006 NM 1998 11 11 UPS98227981 1 19981007 A 5347 SEAT TRACK BOEING 727 727108C 1384039 NM BS 344 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 936UP 19503 INSPECTION TYPE-C, WHILE INSPECTION UNDER FWD LAV LOWER FLANGE OF SEAT TRACK AT BS 34.4 RBL 24.75 FOUND CORRODED SECTION OF SEAT TRACK. REPLACED BS 344 TO 400 RBL 24.75 TRACK FABRICATED FROM EXTRUSION BAC1520-1432 IAW SRM 53-10-5 FIG 1. 2 L 7 3 4F A3WE 1998111100007 19981111 00007 NM 1998 11 11 P5CA9801558 1 19981022 A 3230 65B0154019 ACTUATOR BOEING 747 747283B 1384867 NM LT MLG FAILED A P5CA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 23 921FT 21575 LEFT BODY GEAR DID NOT RETRACT. RED GEAR LIGHT AND RED DOOR LIGHT IN UP, NO GEAR GREEN LIGHT. GEAR HANDLE OFF, BODY GE AR THEN SHOWED DOWN AND LOCKED WITH DOOR OPEN. REMOVED AND REPLACED LT BODY GEAR LOCK ACTUATOR, PERFORMED EXTENSION AND RETRACTION OF BODY GEAR PER MM 32-33-15. 2 L 7 4 4F A20WE 1998111100008 19981111 00008 EA 1998 11 11 VTZA98255 1 19980809 A 5240 DOOR CNDAIR CL600 CL6002B19 EA FUSELAGE OPEN A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 620BR 7179 FLT 6749 - IAD-GSO - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO HOWLING NOISE AT 250K. AIRCRAFT RETURNE D TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND EXTERNAL POWER DOOR OPEN AND CLOSED DOOR. NO DAMAG E TO DOOR OR AIRFRAME. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998111300258 19981113 00258 SO 1998 11 13 98ZZZX4045 2 19980820 A 8520 CONNECTING ROD CESSNA 206 U206F 2073333 CE CONT O550 IO550* SO NR 2 PISTON BROKE A S SVVA O OTHER O OTHER NR NOT REPORTED 1 AL 05 50159 1663 U20601907 284677R NR 2 CONNECTING ROD BROKE AND BROKE THE CRANKCASE AND BROKE BOTH OF THE MAGS OFF THE ENGINE. 1 H 7 1 3O 3 O A4CE E3SO 1998111300274 19981113 00274 SW 1998 11 13 98ZZZX4061 1 19981023 A 2910 70060T00Y310 HOSE BELL 214 214ST 1182106 SW SERVO LOOSE A HEEA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 59805 28141 EXPERIENCED NR 2 HYDRAULIC SYSTEM PRESSURE DROP AND ILLUMINATION OF CAUTION LIGHT IN-FLIGHT. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HOSE LOOSE AT SERVO FITTING, TIGHTENED SAME. REF: 214ST IPC, CHAPTER 29-99-00, FIGURE 29-5, ITEM 23. 2 G 7 2 4U H10SW 1998111300449 19981113 00449 NM 1998 11 13 TWAA9817801 1 19981016 A 5730 SKIN BOEING 767 767231 1385131 NM WS 859-883 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 859 TO 883, LBL 74 IN TO 97 IN. REMOVED COR ROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT OF HOLES PER 51-00-03, PART 6, FOUND NO CRACKS. REPAIRED PER ARA 1 1596. 2 L 7 2 4F RT A1NM 1998111300450 19981113 00450 NM 1998 11 13 TWAA9817802 1 19981016 A 5730 SKIN BOEING 767 767231 1385131 NM WS 933-65 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING SKIN AT FASTENERS STA 933 TO 965, LBL 74 IN TO 97 IN. REMOVED COR ROSION PER SRM 51-10-00. NDT EDDY CURRENT PER 51-00-03 PART 5, FOUND NO CRACKS. SPOT FACED AND BLENDED AS NEEDED PER M CI 98-0185RE. REPAIRED PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300451 19981113 00451 NM 1998 11 13 TWAA9817803 1 19981016 A 5730 SKIN BOEING 767 767231 1385131 NM WS 911-933 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION AT TOP WING SKIN AT FASTENERS STA 911 TO 933, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS WERE FOUND. REMOVED CORROSION PER SRM 51-10-00. SPOT FACED AN D BLENDED AS NEEDED PER TWA MCI-98-0185RE. REPAIRED PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300452 19981113 00452 NM 1998 11 13 TWAA9817804 1 19981016 A 5730 SKIN BOEING 767 767231 1385131 NM WS 883-911 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON TOP WING AT FASTENERS STA 883 TO 911, LBL 74 IN TO 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED CORROSION PER SRM 51-10-11. REPAIRED PER ARA 1159 6. 2 L 7 2 4F RT A1NM 1998111300453 19981113 00453 NM 1998 11 13 TWAA9817805 1 19981016 A 5730 SKIN BOEING 767 767231 1385131 NM CENTER WING CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION, STA 860 BELOW EMERGENCY EXIT ON LT SIDE. REMOVED CORROSION PER SRM 51-10-00. NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6, AND NO CRACKS FOUND. R EPAIRED PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300454 19981113 00454 NM 1998 11 13 TWAA9817806 1 19981016 A 5330 SKIN BOEING 767 767231 1385131 NM BS 830-852 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SKIN, STA 830 TO 852, LBL 74 IN TO LBL 97 IN. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03 PART 6 AND NO CRACKS FOUND. REPAIRED PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300455 19981113 00455 NM 1998 11 13 VJ9800578 1 19981101 A 2910 HYD SYST BOEING 737 7372P6 NM NLG STEERING LOST A A ZZDA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 15 EICJW 21355 DURING CLIMBOUT, LOSS OF HYDRAULIC QUANTITY INDICATED. FLIGHT CREW RETURNED TO ATL MAINTENANCE BASE. ON LANDING LOST N OSE STEERING CAPABILITY AND AIRCRAFT DEPARTED RUNWAY RESULTING IN EXTENSIVE DAMAGE TO THE AIRCRAFT. PASSENGERS AND CREW SAFELY EVACUATED AIRCRAFT. 2 L 7 2 4F RT A16WE 1998111300456 19981113 00456 WP 1998 11 13 VJ9800579 1 19981104 A 2560 113317 COVER DOUG DC9 DC932 3022066 WP L1 DOOR SLIDE DISLODGED A ZZDA O OTHER O OTHER TX TAXI/GRND HDL 1 SO 15 910VJ 47277 FWD PASSENGER DOOR ESCAPE SLIDE COVER DISLODGED WHEN DOOR OPENED. REINSTALLED AND PERFORMED REQUIRED INSPECTION. 2 L 7 2 4F A6WE 1998111300457 19981113 00457 WP 1998 11 13 VJ9800580 1 19980929 A 5320 ANGLE DOUG DC9 DC932 3022066 WP PAX DOORWAY CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 AFT ENTRANCE DOOR LT SIDE WALL SUPPORT ANGLE CRACKED AND CORRODED. FABRICATED AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30 -2, 51-30-4, 52-11-0, FIG 2, 51-20-2A AND AIRTRAN RES 981705. 2 L 7 2 4F A6WE 1998111300458 19981113 00458 WP 1998 11 13 VJ9800581 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 410.5 & 412.5 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 DENT 1.5 INCHES BY .037 D/X=41 AT FS 410.5, L28-29R, AND FS 412.5, L28-29R, OF 1 INCH BY .018 D/X=56 OUT OF LIMIT IAW SR M 53-04, FIG 10. CUT OUT DENT, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC9 SRM 51-10-4, 53-01 FIG 4, 51-10-3, 51-30-2 AND -5 PLUS AIRTRAN RES 981762. 2 L 7 2 4F A6WE 1998111300459 19981113 00459 WP 1998 11 13 VJ9800582 1 19980930 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 116.5 CRACKED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 DENT 1.5 INCHES BY .038 D/X=35 OUT LIMIT IAW DC9 SRM 53-04 FIG 38, SHEET 10, CONDITION 1B3. CUT OUT DENT, FABRICATED AN D INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 38, 51-10-4, 51-30-2 AND AIRTRAN RES 981774. REINSTALLED ALL COMPONEN TS REMOVED FOR ACCESS AND OPS CHECKED GOOD IAW DC9 MM. 2 L 7 2 4F A6WE 1998111300460 19981113 00460 WP 1998 11 13 VJ9800583 1 19980930 A 5310 59114181N54N STRUCTURE DOUG DC9 DC932 3022066 WP BS 680-756 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 RT KEEL AREA AT FS 680 TO 756 CORRODED. Z ANGLE, L29R, LONGERON AND FITTING CORRODED BEYOND LIMIT. INSTALLED NEW PARTS IAW DC9 SRM 51-30-3, 51-10-4, 51-30-1, 51-30-2, 51-30-5 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1998111300461 19981113 00461 NM 1998 11 13 VJ9800577 1 19981104 A 2560 4125A MEGAPHONE BOEING 737 7372L9 1384497 NM CABIN INOPERATIVE A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 737Q 21279 FWD MEGAPHONE INOPERATIVE. REPLACED THE FWD MEGAPHONE IAW MM 25-69-0. 2 L 7 2 4F RT A16WE 1998111300462 19981113 00462 EU 1998 11 13 MALA976222 1 19981026 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO COMPT FAILED A MALA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 112XJ 340A112 ON SHUTDOWN, WHILE PASSENGER'S WERE DEPLANING THE CARGO SMOKE AND ASSOCIATED MASTER WARNING LIGHTS ILLUMINATED. WARNING CAME ON AND OFF ABOUT 4 TIMES WITHIN 10 MINUTES. RECYCLED POWER AND WARNING'S APPEARED ONCE. MAINTENANCE INSPECTED AN D REMOVED CARGO SMOKE DETECTOR. CARGO SMOKE DETECTOR TESTS GOOD, OPS CHECK GOOD. VERIFIED NO SMOKE PRESENT IN AIRCRAFT . 2 L 7 2 4T RT A52EU 1998111300463 19981113 00463 EU 1998 11 13 MALA976223 1 19981029 A 3230 L38710SA SWIVEL SAAB SF340 SF340A 7850100 EU RT MLG SHEARED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 114XJ 340A114 AFTER DEPARTURE WITH GEAR SELECTED UP THE HYDRAULIC CAUTION LIGHT ILLUMINATED. THE HYD PUMP WAS SELECTED OFF AND NOTED HYD QUANTITY AND MAIN PRESSURE AT ZERO, BUT EMERGENCY PRESSURE NORMAL. QRH PERFORMED AND A SUCCESSFUL GEAR FREE FALL PE RFORMED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE RIGHT DOWNLOCK SWIVEL, RT AND LT SEPARATION BOLTS. A/C GE AR SWUNG, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998111300464 19981113 00464 SO 1998 11 13 COMA9810248 1 19981103 A 5240 LATCH EMB 120 EMB120RT SO SERVICE DOOR NOT SECURED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 256CA 120245 DOOR WARNING DURING TAKEOFF. FUEL SERVICE DOOR NOT CLOSED. SECURED SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998111300465 19981113 00465 EA 1998 11 13 COMA9860335 1 19981103 A 3260 864807 PSEU CNDAIR CL600 CL6002B19 EA E & E COMPT MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 710CA 7241 CABIN DOOR WARNING DURING FLIGHT. COULD NOT DUPLCIATE DISCREPANCY. REPLACED THE PSEU FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1998111300466 19981113 00466 1998 11 13 COAM9860336 2 19981103 A 7532 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 EA AVIONCIS MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 11078 7014 ANTI-ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE DISCREPANCY. REPLACED BLEED CONTROL UNIT FOR TROUBLESHOOTING. 2 L 7 2 4F RT A21EA 1998111300467 19981113 00467 EU 1998 11 13 QXEA9801673 1 19981103 A 3350 5515800106 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU COCKPIT DOOR INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 480AU 11229 EXIT SIGN AT COCKPIT DOOR IS OUT. MAINTENANCE REPLACED THE SIGN ASSEMBLY, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998111300468 19981113 00468 EU 1998 11 13 QXEA9801674 1 19981102 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 9E FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 486US 11237 EXIT LIGHT AT ROW 9E IS INOPERATIVE. MAINTENANCE RELAMPED, OPERATIONAL TEST WAS NORMAL. 2 L 7 2 4F RT A20EU 1998111300469 19981113 00469 WP 1998 11 13 MWEA981030 1 19981104 A 5313 S2777922 LONGERON DOUG DC9 DC982 3022082 WP BS 389, 408 &427 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CABIN LONGERON 17L CRACKED AT LOWER FLANGE ATTACH POINT AT STATION 389 STATION 408 AND STATION 427. MTC FABRICATE D AND INSTALLED LONGERON SPLICE. 2 L 7 2 4F A6WE 1998111300470 19981113 00470 WP 1998 11 13 RRXA98480 1 19981104 A 5753 5769933501 VANE DOUG DC8 DC862 3021970 WP LT TE FLAP CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND LT O/B SLOT LEADING EDGE CRACKED IN TWO PLACES. ROUTED OUT CRACKS ON SLOT VANE AT STA X 0LD025.5 AND X0LD014.75, DRILLED AND COUNTERSANK NEW HOLES ON EACH SIDE OF CLEAN UP. INSTALLED NEW FASTENERS IAW FAA AP PROVED DER COTNEY ENGINEERING SKETCH E84-R104 AND DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998111300471 19981113 00471 WP 1998 11 13 RRXA98481 1 19981104 A 5753 5642900509 WEDGE DOUG DC8 DC862 3021970 WP RT TE FLAP CREASED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND RT INBOARD FLAP WEDGE AFT CENTER UPPER SKIN STA XCW26.75 CREASED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R58. 2 L 7 4 4F 4A25 1998111300472 19981113 00472 WP 1998 11 13 RRXA98482 1 19981104 A 5321 133171 FLOOR DOUG DC8 DC862 3021970 WP BS 1423 PUNCTURED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FLOOR PANEL AT STA 1423 BL 0 PUNCTURED. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA A PPROVED DER COTNEY ENGINEERING SKETCH SK98541 AND DC-8 SRM 51-1-21, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300473 19981113 00473 WP 1998 11 13 RRXA98483 1 19981104 A 5311 5640234503 FRAME DOUG DC8 DC862 3021970 WP FRAME 1340 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1340 WITH HOLE IN RADIUS BETWEEN LONGERONS 10 AND 11 RIGHT. FABRICATED AND INSTAL LED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R84, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300474 19981113 00474 WP 1998 11 13 RRXA98484 1 19981104 A 5311 5773257509 FRAME DOUG DC8 DC862 3021970 WP FRAME 1440 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1440 WITH MISDRILLED HOLES AT LONGERONS 5A-7 LEFT. FABRICATED AND INSTALLED REPAI R ANGLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R47. 2 L 7 4 4F 4A25 1998111300475 19981113 00475 WP 1998 11 13 RRXA98485 1 19981104 A 5311 5640229521 FRAME DOUG DC8 DC862 3021970 WP FRAME 1240 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1240 MISDRILLED BETWEEN LONGERONS 7 AND 9 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R46 AND DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998111300476 19981113 00476 WP 1998 11 13 RRXA98486 1 19981104 A 5311 5610084519 FRAME DOUG DC8 DC862 3021970 WP FRAME 450 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 450 MISDRILLED AT LONGERON 3 LEFT. REMOVED DAMAGED AREA, FABRICATED NEW RING AND BRACKET IAW ROSEMBALM DRAWING NR 44212, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED RING AND BRACKET IAW DC-8 SRM 51-1-20D AND 53-2-0. 2 L 7 4 4F 4A25 1998111300477 19981113 00477 WP 1998 11 13 RRXA98487 1 19981105 A 5311 97510983 FRAME DOUG DC8 DC862 3021970 WP FRAME 1400 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1400 WITH MISDRILLED HOLES AT LONGERONS 18, 20 AND 21 RIGHT. FABRICATED AND INSTA LLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R27. 2 L 7 4 4F 4A25 1998111300478 19981113 00478 WP 1998 11 13 RRXA98488 1 19981105 A 5311 5610088513 FRAME DOUG DC8 DC862 3021970 WP FRAME 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 280 WITH MISDRILLED HOLE BETWEEN LONGERONS 13-14 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R31, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300479 19981113 00479 WP 1998 11 13 RRXA98489 1 19981105 A 5311 5750717501 FRAME DOUG DC8 DC862 3021970 WP FRAME 781 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 781 WITH MISDRILLED HOLE BETWEEN LONGERONS 8 AND 9 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R106. 2 L 7 4 4F 4A25 1998111300480 19981113 00480 WP 1998 11 13 RRXA98490 1 19981105 A 5311 5640231503 FRAME DOUG DC8 DC862 3021970 WP FRAME 1280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1280 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR S TRAPS, GUSSET AND FILLER IAW FAA APPROVED ACMI SKETCH SK98383, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300481 19981113 00481 WP 1998 11 13 RRXA98491 1 19981105 A 5311 57544271 FRAME DOUG DC8 DC862 3021970 WP FRAME 580 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 580 WITH MISDRILLED HOLE AT LONGERON 9 LEFT. FABRICATED AND INSTALLED REPAIR ANGL ES, FILLER AND SHIM IAW FAA APPROVED ACMI SKETCH SK 98362, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300482 19981113 00482 WP 1998 11 13 RRXA98492 1 19981105 A 5311 97590021 FRAME DOUG DC8 DC862 3021970 WP FRAME 500 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 500 WITH MISDRILLED HOLE BETWEEN LONGERONS 16 AND 17 LEFT. FABRICATED AND INSTALL ED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R66, DC-8 SRM 53-2-0 AND 51-1-21. 2 L 7 4 4F 4A25 1998111300483 19981113 00483 WP 1998 11 13 RRXA98493 1 19981105 A 5311 5640232453 FRAME DOUG DC8 DC862 3021970 WP FRAME 1300 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1300 WITH MISDRILLED HOLE AT LONGERON 20 RIGHT. FABRICATED AND INSTALLED REPAIR I AW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R22, DC-8 SRM 53-2-0 AND 51-1-21. 2 L 7 4 4F 4A25 1998111300484 19981113 00484 WP 1998 11 13 RRXA98494 1 19981105 A 5311 5753352509 FRAME DOUG DC8 DC862 3021970 WP FRAME 1420 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1420 WITH MISDRILLED HOLE AT LONGERON 19 RIGHT. FABRICATED AND INSTALLED REPAIR A NGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R26, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51- 1-8. 2 L 7 4 4F 4A25 1998111300485 19981113 00485 WP 1998 11 13 RRXA98495 1 19981105 A 5311 5642861503 FRAME DOUG DC8 DC862 3021970 WP FRAME 834 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 834 WITH MISDRILLED HOLE AT LONGERON 15 RIGHT. FABRICATED AND INSTALLED REPAIR IA W FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R79. 2 L 7 4 4F 4A25 1998111300486 19981113 00486 WP 1998 11 13 RRXA98496 1 19981105 A 5311 5751961505 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLES AT LONGERONS 4, 5, 9, 10, 11 AND 13 RIGHT. FABRICATED AND I NSTALLED REPAIRS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R80, DC-8 SRM 51-1-21 AND AREAS TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300487 19981113 00487 WP 1998 11 13 RRXA98497 1 19981105 A 5321 35964 FLOOR DOUG DC8 DC862 3021970 WP BS 435-445 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FLOOR PANEL WITH CRACKS THROUGH BOLT HOLES AT FS 435 TO 445 LBL 60. FABRICATED AND INST ALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH SK98418, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300488 19981113 00488 WP 1998 11 13 RRXA98498 1 19981105 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 300 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FUSELAGE SKIN CRACKED AT FS 300 TO 320 BETWEEN LONGERONS 9 AND 10 LEFT. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E77-R04. 2 L 7 4 4F 4A25 1998111300489 19981113 00489 WP 1998 11 13 RRXA98499 1 19981105 A 5311 5640221517 FRAME DOUG DC8 DC862 3021970 WP FRAME 1080 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1080 WITH MISDRILLED HOLES AT LONGERONS 8 AND 10 LEFT. FABRICATED AND INSTALLED R EPAIR STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R38, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300490 19981113 00490 WP 1998 11 13 RRXA98500 1 19981105 A 5320 1648024 ANGLE DOUG DC8 DC862 3021970 WP BS 69 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND VERTICAL TO HORIZONTAL PRESSURE WEB ATTACH ANGLE CORRODED AT FS 69 RBL 12 TO 16. REMOVE D DAMAGED SECTION OF ATTACH ANGLE, FABRICATED AND INSTALLED NEW SECTION OF ATTACH ANGLE AND SPLICE REPAIR IAW FAA APPROV ED DER COTNEY ENGINEERING SKETCH E84-R102, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300491 19981113 00491 WP 1998 11 13 RRXA98501 1 19981105 A 5311 5640222523 FRAME DOUG DC8 DC862 3021970 WP FRAME 1100 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1100 WITH MISDRILLED HOLE AT LONGERON 14 LEFT. FABRICATED AND INSTALLED REPAIR DO UBLED IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R33, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300492 19981113 00492 WP 1998 11 13 RRXA98502 1 19981105 A 5311 5640233453 FRAME DOUG DC8 DC862 3021970 WP FRAME 1320 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 19 AND 20 RIGHT. REPAIRED FRAME IAW F AA APPROVED DER COTNEY ENGINEERING SKETCH E84-R23, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300493 19981113 00493 WP 1998 11 13 RRXA98503 1 19981105 A 5311 5750717501 FRAME DOUG DC8 DC862 3021970 WP FRAME 780 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT FOUND FRAME 780 WITH MISDRILLED HOLE AT LONGERON 11 RIGHT. FABRICATED AND INSTALLED REPAIR DOU BLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R49, HEAT TREATED IAW DC-8 SRM 51-1-1, INSTALLED IAW DC-8 SRM 51 -1-21 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300494 19981113 00494 WP 1998 11 13 RRXA98504 1 19981105 A 5311 5793172501 FRAME DOUG DC8 DC862 3021970 WP FRAME 940 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 940 WITH MISDRILLED HOLES BETWEEN LONGERONS 9 AND 12 RIGHT. FABRICATED AND INSTAL LED REPAIR ANGLES, SHIMS AND STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R86, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300495 19981113 00495 WP 1998 11 13 RRXA98505 1 19981105 A 5311 5750128501 FRAME DOUG DC8 DC862 3021970 WP FRAME 798 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 798 WITH MISDRILLED HOLE AT LONGERON 11 LEFT. FABRICATED AND INSTALLED REPAIR STR APS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R111, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300496 19981113 00496 WP 1998 11 13 RRXA98506 1 19981104 A 2913 55006 PUMP DOUG DC8 DC8F54 3021926 WP NR 2 HYD SYST FAILED A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 15 992CF 45884 HYD QUANTITY LOSS INFLIGHT. FOUND NR 2 ENG HYD PUMP INTERNAL SEALS ALLOWING FLUID TO FLOW INTO NR 2 ENG OIL SUPPLY. DR AINED, FLUSHED ENG OIL TANK 2 TIMES. REMOVED AND REPLACED OIL FILTER AND ENG HYD PUMP. PERFORMED LEAK CK OF ENG OIL AN D HYD SUPPLY, NONE NOTED. PERFORMED POWER RUN, OPS CK. HYD PUMP, NO DEFECTS NOTED. 2 L 7 4 4F 4A25 1998111300497 19981113 00497 WP 1998 11 13 RRXA98507 1 19981102 A 3231 LINKAGE DOUG DC8 DC862F 3021972 WP NLG DOORS LACK OF LUBE A RRXA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 WP 15 997CF 46154 VIBRATION FROM VICINITY OF NOSE WHEEL WELL ON GEAR RETRACTION. INSPECTED NOSE GEAR WHEEL WELL AREA, T/C COMPARTMENTS FO UND NO DEFECTS. LUBRICATED FWD NOSE GEAR DOORS LINKAGE. CYCLED SEVERAL TIMES, ALL OPS CKS GOOD IAW EWA MM CH 32-30. 2 L 7 4 4F 4A25 1998111300498 19981113 00498 WP 1998 11 13 RRXA98508 1 19981105 A 5311 5613466505 FRAME DOUG DC8 DC862 3021970 WP FRAME 640 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 640 WITH MISDRILLED HOLE ABOVE LONGERON 21 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R01, DC-8 SRM 51-1-20D AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300499 19981113 00499 WP 1998 11 13 RRXA98509 1 19981105 A 5311 5750128501 FRAME DOUG DC8 DC862 3021970 WP FRAME 798 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 798 WITH MISDRILLED HOLES AT LONGERONS 7, 8, 9, 10, 11, 14, 15 AND 21 RIGHT. FABR ICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R68, DC-8 SRM 51-1-20D AND TREATED AREA I AW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300500 19981113 00500 WP 1998 11 13 RRXA98510 1 19981105 A 5311 5640231503 FRAME DOUG DC8 DC862 3021970 WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1280 WITH MISDRILLED HOLES AT LONGERONS 10, 11 AND 12 RIGHT. FABRICATED AND INSTA LLED REPAIR ANGLE AND STRAPS IAW FAA APPROVED ACMI SKETCHES SK98381 AND SK98382, DC-8 SRM 51-1-21 AND AREA TREATED IAW D C-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300501 19981113 00501 WP 1998 11 13 RRXA98511 1 19981105 A 5311 5642859507 FRAME DOUG DC8 DC862 3021970 WP FRAME 822 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 822 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLE D REPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R76, DC-8 SRM 51-1-20, 53-2-0 AND AREA TREA TED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300502 19981113 00502 WP 1998 11 13 RRXA98512 1 19981105 A 5311 5750129501 FRAME DOUG DC8 DC862 3021970 WP FRAME 760 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 760 WITH MISDRILLED HOLE AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R48. 2 L 7 4 4F 4A25 1998111300503 19981113 00503 WP 1998 11 13 RRXA98513 1 19981105 A 5311 5750717501 FRAME DOUG DC8 DC862 3021970 WP FRAME 780 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 780 WITH MISDRILLED HOLE BETWEEN LONGERONS 9 AND 10 RIGHT. FABRICATED AND INSTALL ED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R49, DC-8 SRM 53-2-0 AND 51-1-1A. 2 L 7 4 4F 4A25 1998111300504 19981113 00504 WP 1998 11 13 RRXA98514 1 19981105 A 5315 2772345 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 1500 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1500 LEFT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND SHIM IAW FAA APPROVED ACMI SKETCH SK98464, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300505 19981113 00505 WP 1998 11 13 RRXA98515 1 19981105 A 5315 2772345 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 1480 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1480 LEFT CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAI R DOUBLER AND FILLER IAW FAA APPROVED ACMI SKETCH SK98463, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300506 19981113 00506 WP 1998 11 13 RRXA98516 1 19981105 A 5315 4613722 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 880 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 880 WITH MISDRILLED HOLES. REMOVED DAMAGED AREA, FABRICATED AND INSTALL ED REPAIR ANGLES, FILLER AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R54, DC-8 SRM 51-1-21, 51-1-20D AN D TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300507 19981113 00507 WP 1998 11 13 RRXA98517 1 19981105 A 5311 5640229521 FRAME DOUG DC8 DC862 3021970 WP FRAME 1240 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1240 WITH MISDRILLED HOLE AT LONGERON 8 LEFT. BLENDED AREA, FABRICATED AND INSTAL LED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R44, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SR M 51-1-8. 2 L 7 4 4F 4A25 1998111300508 19981113 00508 WP 1998 11 13 RRXA98518 1 19981105 A 5311 5753352509 FRAME DOUG DC8 DC862 3021970 WP FRAME 1420 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1420 WITH MISDRILLED HOLES AT LONGERONS 5, 7 AND 8 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R41. 2 L 7 4 4F 4A25 1998111300509 19981113 00509 WP 1998 11 13 RRXA98519 1 19981105 A 5311 5754002501 FRAME DOUG DC8 DC862 3021970 WP FRAME 560 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 560 WITH MISDRILLED HOLES AT LONGERONS 19 AND 20 RIGHT. PLUGGED MISDRILLED HOLES IAW DC-8 SRM 51-1-21, FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R45 AND T REATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300510 19981113 00510 WP 1998 11 13 RRXA98520 1 19981105 A 5311 57516521 FRAME DOUG DC8 DC862 3021970 WP FRAME 440 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 440 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 9 RIGHT. FABRICATED AND INSTALLE D REPAIR STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R36, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 5 1-1-8. 2 L 7 4 4F 4A25 1998111300511 19981113 00511 WP 1998 11 13 RRXA98521 1 19981105 A 5311 5640233505 FRAME DOUG DC8 DC862 3021970 WP FRAME 1320 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALL ED REPAIR ANGLE AND STRAP IAW FAA APPROVED ACMI SKETCH SK98385, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300512 19981113 00512 NM 1998 11 13 VNAA9811003 1 19981104 A 3412 0102561AGO1 TAT PROBE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 431JS 218 3028 A TOTAL AIR TEMPERATURE PROBE HEAT FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RET URNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE TOTAL AIR TEMPERATURE PROBE, IN ACCORDANCE WITH DORNIER MAINT ENANCE MANUAL 34-11-03. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998111300513 19981113 00513 WP 1998 11 13 TC8A98077 1 19981101 A 3260 SWITCH DOUG DC8 DC862F 3021972 WP RT MLG DIRTY A TC8A O OTHER N FALSE WARNING DE DESCENT 1 GL 23 187SK 46022 AFTER GEAR EXTENSION, NO GEAR DOWN INDICATION ON RIGHT MAIN GEAR, CYCLED GEAR, INDICATION OK. FOUND STANDING WATER IN C ONDUIT ABOVE RT MLG DOWNLOCK SWITCH. DRIED AND CLEANED CONNECTOR, RETIGHTENED CONDUIT AND INDICATION CHECKED GOOD ON TH E GROUND. 2 L 7 4 4F 4A25 1998111300514 19981113 00514 NM 1998 11 13 SWAA982676 1 19981030 A 5320 WEB BOEING 737 7372H4 138448C NM CARGO DOORWAY GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND WEB FWD OF DOOR CUTOUT GOUGED AND WORN. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300515 19981113 00515 NM 1998 11 13 SWAA982677 1 19981030 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN AT AFT ENTRY DOOR LWR HINGE CUTOUT. REPAIRED DOUBLERS PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998111300516 19981113 00516 NM 1998 11 13 SWAA982678 1 19981030 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND SKIN TORN AT EXTERNAL CONDITIONED AIR DOOR LOWER FUSELAGE. REPAIRED TEAR SKIN PER BO EING SRM. 2 L 7 2 4F A16WE 1998111300517 19981113 00517 NM 1998 11 13 SWAA982679 1 19981030 A 5330 SKIN BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED FUSELAGE SKIN AT AFT SVC DOOR LWR, HINGE CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300518 19981113 00518 NM 1998 11 13 SWAA982680 1 19981030 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 294.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND L-ANGLE CRACKED AT FLOOR LINE AND RT Z ANGLE AT BS 294.5. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F A16WE 1998111300519 19981113 00519 NM 1998 11 13 SWAA982681 1 19981030 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 312 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND STUB FRAME AT BS 312, STR 6L CRACKED IN RADIUS. REMOVED DAMAGED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300520 19981113 00520 NM 1998 11 13 SWAA982682 1 19981031 A 5320 FRAME BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND CRACKED WEB NOT PROPERLY REPAIRED AT LOWER FWD CORNER STUB FRAME. REPAIRED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1998111300521 19981113 00521 1998 11 13 SWAA982684 4 19981030 A 3442 36140710401 MOTOR BOEING 737 7372H4 138448C NM RADAR ANTENNA INOPERATIVE A SWAA A UNSCHED LANDING L NO TEST CR CRUISE 1 SW 07 056SW 21721 AIRCRAFT DIVERTED TO DAL DUE TO WX RADAR WOULD NOT PAINT WX OR GROUND RETURNS. WX RADAR INOPERATIVE. RED HALF MOON BAN D AT 5 MILE ARC. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED RADAR ANT MOTOR, OPS CHECK OK PER BOEING MM . 2 L 7 2 4F A16WE 1998111300522 19981113 00522 NM 1998 11 13 SWAA982683 1 19981031 A 5720 ANGLE BOEING 737 7372H4 138448C NM LT WING WORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND WORN SPOTS ON VERTICAL ANGLE JUST AFT OF LEFT GEAR CENTER DOOR FRAME. REMOVED AND RE PLACED ANGLE PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300523 19981113 00523 NM 1998 11 13 SWAA982685 1 19981030 A 3320 059393 BALLAST BOEING 737 7375H4 138449D NM ROW 11 FAILED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 502SW 24179 ON TAXI OUT, THE FLIGHT ATTENDANTS REPORTED A SMELL IN THE CABIN LIKE BURNING INSULATION (ELEC). CEILING LIGHT INOPERAT IVE-ROW 11. REMOVED AND REPLACED LIGHT BALLAST PER BOEING MM. OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998111300524 19981113 00524 NM 1998 11 13 SWAA982686 1 19981101 A 5320 WEB BOEING 737 7372H4 138448C NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND WEB AND WEB ATTACH CLIP CRACKED AT BS 277, STR 11L. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300525 19981113 00525 NM 1998 11 13 SWAA982687 1 19981030 A 3350 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 678AA 23290 DURING SCHEDULED SERVICE CHECK, FOUND ONE FLOOR TRACK LIGHT INOPERATIVE. RELAMPED PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111300526 19981113 00526 NM 1998 11 13 SWAA982688 1 19981030 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 927-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 7 FASTENER HOLES CRACKED STR 14L, AT BS 927-947. REPAIRED PE R XEA X2-53-224 REV 1. 2 L 7 2 4F A16WE 1998111300527 19981113 00527 NM 1998 11 13 SWAA982689 1 19981030 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 986-1006 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 3 FASTENER HOLES CRACKED STR 14L, AT BS 986-1006. INSTALLED REPAIRED DOUBLERS PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300528 19981113 00528 NM 1998 11 13 SWAA982690 1 19981030 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 908-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 15 FASTENER HOLES CRACKED STR 10L, AT BS 908-947. REMOVED AN D REPLACED DAMAGED FASTENER HOLES PER XEA X2-53-223. 2 L 7 2 4F A16WE 1998111300529 19981113 00529 NM 1998 11 13 SWAA982691 1 19981030 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 927-247 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 6 FASTENER HOLES CRACKED STR 14R, AT BS 927-947. REPAIRED PE R XEA X2-53-224. 2 L 7 2 4F A16WE 1998111300530 19981113 00530 NM 1998 11 13 SWAA982692 1 19981030 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 927-247 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND HFEC INDICATES 3 FASTENER HOLES CRACKED STR 10R, AT BS 927-947. REPAIRED PE R XEA X2-53-224. 2 L 7 2 4F A16WE 1998111300531 19981113 00531 NM 1998 11 13 SWAA982693 1 19981031 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND CRACKED 14L STRINGER SPLICE AT BS 908. REPLACED CRACKED STRINGER SPLICE PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300532 19981113 00532 NM 1998 11 13 SWAA982694 1 19981030 A 3350 BULB BOEING 737 7372T4 1384492 NM OVERWING EXIT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 722WN 22698 DURING WALKAROUND CHECK, FOUND OVERWING EXIT RED LIGHT (ONE INOPERATIVE). RELAMPED EMERGENCY EGRESS LIGHT PER BOEING MM . 2 L 7 2 4F A16WE 1998111300533 19981113 00533 NM 1998 11 13 SWAA982695 1 19981030 A 3397 WIRE BOEING 737 7373H4 1384600 NM ROW 19-23 LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 608SW 27928 DURING SCHEDULED C2 CHECK, FOUND CABIN FLOOR EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROW 18 THROUGH 23. REATTACHED WIRES INTO LIGHT RESEPTICAL PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111300534 19981113 00534 NM 1998 11 13 SWAA982696 1 19981031 A 3350 BATTERY CHARGER BOEING 737 7373H4 1384600 NM ROW 19 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING WALKAROUND CHECK, FOUND ALL EMERGENCY FLOOR TRACK LIGHTING AFT OF ROW 19 APPEAR INOPERATIVE. REPLACED BATTERY CH ARGER CONTROL HOUSING FOR AFT FLOOR TRACK LIGHTING PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111300535 19981113 00535 NM 1998 11 13 SWAA982697 1 19981030 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM BS 269 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRANSITION CHECK, FOUND CRACKED INTERCOSTAL AT BS 269, RBL 2, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300536 19981113 00536 NM 1998 11 13 SWAA982698 1 19981030 A 5350 FAIRING BOEING 737 7373H4 1384600 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRANSITION CHECK, WHILE WORKING DELAMINATION ON BODY FAIRING JUST FWD OF THE RT WHEEL WELL, FOUND RT WI NG ROOT FAIRING JUST FWD OF RT MLG WHEEL WELL HAS SEVERAL CRACKS BETWEEN FASTENER HOLES ON T/E. REPAIRED CRACKS BETWEEN FASTENER HOLES ON RT WING ROOT FAIRING JUST FWD OF RT MLG WHEEL WELL ON T/E PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300537 19981113 00537 NM 1998 11 13 SWAA982699 1 19981031 A 3350 BATTERY PACK BOEING 737 7373H4 1384600 NM LT & RT OVERWING DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED SERVICE CHECK, FOUND BOTH OVERWING EMERGENCY HATCH DOOR LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111300538 19981113 00538 NM 1998 11 13 SWAA982700 1 19981031 A 2450 912522C7C4001 RELAY BOEING 737 7375H4 138449D NM E & E COMPT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 515SW 25154 AIR TURNBACK AFTER CLIMBING THROUGH 24K FT CAS FAILED, SHORTLY AFTER LEVEL AT 33K BOTH TRANSPONDERS FAILED, 10 MIN LATER AUTO PRESS FAILED, LOW IDLE UPON DESCENT. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED R3 TRANSFER RELAY PER BOEING MM. OPS CHECK NORMAL. (LPG 71230) 2 L 7 2 4F RT A16WE 1998111300539 19981113 00539 NM 1998 11 13 SWAA982701 1 19981031 A 2410 CSD BOEING 737 7372T4 1384492 NM NR 1 REQD SERVICE A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SW 07 129SW 22340 TAKEOFF REJECTED AT 40KTS FOR NR 1 CSD LOW OIL PRESSURE LIGHT. RETURN TO GATE. SERVICED NR 1 CSD AND LEAK CHECKED PER BOEING MM. (LPG 40946) 2 L 7 2 4F A16WE 1998111300540 19981113 00540 NM 1998 11 13 SWAA982702 1 19981101 A 3397 WIRE BOEING 737 7372T4 1384492 NM OVERWING EXIT FAILED A SWAA K NONE B L SMOKE/FUMES/ODORS/SPARKS NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING WALKAROUND CHECK, FOUND FLOOR ESCAPE PATH LIGHTS CAME ON AND LIGHTS AT OVERWING EXIT POSITION STARTED SMOKING. F OUND BURNT WIRES AFTER GOING TO OFF POSITION WITH SWITCH. REMOVED AND REPLACED BULBS AT ROWS 12, 15, 21 PER BOEING MM. OPS CHECK GOOD. 2 L 7 2 4F A16WE 1998111300541 19981113 00541 NM 1998 11 13 SWAA982703 1 19981101 A 3350 110049 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING WALKAROUND CHECK, FOUND FWD FLOOR TRACK BATTERY BASE BAD. REMOVED AND REPLACED FWD FLOOR TRACK BATTERY BASE AND BATTERY. OPS CHECK GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998111300542 19981113 00542 NM 1998 11 13 SWAA982704 1 19981101 A 3350 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING WALKAROUND CHECK, FOUND FLOOR PROX EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS CAME ON AFTER CHANGING TO A/C GEN. POWER, WOULD NOT GO OUT. REPLACED FLOOR EMERGENCY PATCH LIGHT BATTERY PACK PER BOEING MM. 2 L 7 2 4F A16WE 1998111300543 19981113 00543 NM 1998 11 13 SWAA982705 1 19981101 A 5330 SKIN BOEING 737 7373H4 1384600 NM L-1 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 307SW 22947 DURING SCHEDULED A1 CHECK, FOUND L-1 DOOR FUSELAGE LOWER CUTOUT CRACKED APPROX 10. REPAIRED PER SWA RA 1-353-1910. 2 L 7 2 4F RT A16WE 1998111300544 19981113 00544 NM 1998 11 13 SWAA982706 1 19981101 A 5754 ROLLER BOEING 737 7372H4 138448C NM NR 5 LE SLAT LOOSE A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 096SW 23055 AIR TURNBACK DUE TO NR 5 L/E SLAT INTRANSIT INDICATION OCCURS INTERMITTENTLY OF FWD PANEL AND OVERHEAD LED PANEL WITH FL APS EXTENDED INFLIGHT. FOUND LOOSE ROLLER ON NR 5 SLAT INBOARD TRACK. REINSTALLED ROLLER PER BOEING MM. (LPG 243950) 2 L 7 2 4F A16WE 1998111300545 19981113 00545 NM 1998 11 13 SWAA982707 1 19981102 A 3397 WIRE BOEING 737 7372T4 1384492 NM EMERG EXIT BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING WALKAROUND CHECK, FOUND ON TAXI OUT WHEN THE F/A DIMMED, THE INTERIOR LIGHT, THE EMERGENCY EXIT STRIP LIGHTING SY STEM COMPLETELY ILLUMINATED ON THE FLOOR. REPAIRED BROKEN GROUND WIRE PER BOEING MM. 2 L 7 2 4F A16WE 1998111300546 19981113 00546 NM 1998 11 13 SWAA982708 1 19981101 A 2910 HYD LINE BOEING 737 7372T4 1384492 NM A HYD SYSTEM FAILED A SWAA K NONE K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 SW 07 722WN 22698 DURING FLIGHT A SYSTEM FAILED. REMOVED AND REPLACED HYD LINE LT W/W OPS AND LK CHECK OK PER BOEING MM.(LPG 223150) 2 L 7 2 4F A16WE 1998111300547 19981113 00547 NM 1998 11 13 SWAA982709 1 19981102 A 2820 61163 SHUTOFF VALVE BOEING 737 7373H4 1384600 NM NR 1 ENGINE FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 331SW 23695 NR 1 ENGINE FAILED TO START DURING PUSH BACK. RETURNS TO GATE. REMOVED AND REPLACED NR 1 ENGINE FUEL SHUTOFF VALVE PER BOEING MM. OPS CK AND LEAK CK NORMAL. (LPG 260123) 2 L 7 2 4F RT A16WE 1998111300548 19981113 00548 NM 1998 11 13 SWAA982710 1 19981102 A 3397 WIRE BOEING 737 7373H4 1384600 NM ROW 11-12 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 604SW 27955 DURING WALKAROUND CHECK, FOUND APPROX 4 EMERGENCY EXIT AISLE LIGHTS BETWEEN ROW 11 AND 12 ARE PULLED UP AND WIRES BROKEN . RECONNECTED WIRING TO LIGHT FIXTURES AND SECURED LIGHT LENSES, OPS CHECK GOOD. 2 L 7 2 4F RT A16WE 1998111300549 19981113 00549 NM 1998 11 13 SWAA982711 1 19981102 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 604SW 27955 DURING WALKAROUND CHECK, FOUND SMALL SECTION OF FLOOR TRACK LIGHTING MISSING MID CABIN AT EMERGENCY EXIT. REPLACED MISS ING SECTION OF FLOOR TRACK LIGHTING AND CHECKED WONDERFUL PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111300550 19981113 00550 NM 1998 11 13 SWAA982712 1 19981102 A 3350 110049 BATTERY CHARGER BOEING 737 7373H4 1384600 NM ROW 19-23 INOPERATIVE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR PATH LIGHTING INOPERATIVE IN ROWS 19 THROUGH 23. REMOVED AND REPLACED EM ERGENCY FLOOR PATH LIGHTING BATTERY CHARGER AND BATTERY PACK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111300551 19981113 00551 NM 1998 11 13 SWAA982713 1 19981102 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 675AA 23253 DURING WALKAROUND CHECK, FOUND EMERGENCY EXIT LIGHT SECOND WHITE FROM FWD LOOSE IN FLOOR TRACK. REMOVED AND REPLACED TR ACK ASSEMBLY, FWD 8 FEET OF CABIN PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111300552 19981113 00552 NM 1998 11 13 SWAA982714 1 19981102 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 967, 986,1006 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE VISIT CHECK, FOUND 3 SHEAR TIES AT BS 967-986.5 AND 1006, STR 4R HAVE MISDRILLED HOLES. REPAIR ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300553 19981113 00553 NM 1998 11 13 SWAA982715 1 19981102 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE VISIT CHECK, FOUND SHEAR TIE AT STR 14R, BS 400 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300554 19981113 00554 NM 1998 11 13 SWAA982716 1 19981102 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 480 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE VISIT CHECK, FOUND SHEAR TIE AT STR 14R, BS 480 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300555 19981113 00555 NM 1998 11 13 SWAA982717 1 19981102 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SERVICE VISIT CHECK, FOUND SHEAR TIE AT STR 14R, BS 360 CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300556 19981113 00556 NM 1998 11 13 SWAA982718 1 19981102 A 5320 PANEL BOEING 737 7372H4 138448C NM RT MLG WW PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND PANEL PUNCTURED AND SKYDROL SOAKED, BELOW HYD SERVICING PORT, RIGHT WHEEL WELL. REPA IRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300557 19981113 00557 NM 1998 11 13 SWAA982719 1 19981102 A 5320 WEB BOEING 737 7372H4 138448C NM BS 277 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND WEB CRACKED IN RADIUS AT STR 4L, BS 277. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300558 19981113 00558 NM 1998 11 13 SWAA982720 1 19981102 A 3350 STRIP BOEING 737 7372H4 138448C NM AFT GALLEY LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 086SW 22827 DURING SCHEDULED C3 CHECK, FOUND AFT END EGRESS FLOOR STRIP IS LOOSE. SECURED AFT END OF EGRESS FLOOR STRIP PER BOEING MM. 2 L 7 2 4F A16WE 1998111300559 19981113 00559 NM 1998 11 13 SWAA982721 1 19981102 A 5320 STRAP BOEING 737 7372H4 138448C NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 093SW 22965 DURING SCHEDULED A1 CHECK, FOUND AFT SVC DOOR LWR HINGE CUTOUT BEARSTRAP CRACKED AT LWR RADIUS OF CUTOUT. REPAIRED PER SWA RA 1-253-1912 2 L 7 2 4F A16WE 1998111300560 19981113 00560 NM 1998 11 13 SWAA982723 1 19981102 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 664 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND HFEC INDICATION OF A CRACKED IN BEADED PRESSURE WEB AT BS 664, RBL 32. REPAIRED PER SWA RA 1-353-1911. 2 L 7 2 4F RT A16WE 1998111300561 19981113 00561 NM 1998 11 13 SWAA982724 1 19981102 A 5320 PADS BOEING 737 7373A4 1384585 NM CARGO DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FWD CARGO DOOR STOP PADS HAVE LIGHT SURFACE CORRODED ALL AROUND CARGO DOOR CUTOUT IN FUSELAGE. 2 L 7 2 4F RT A16WE 1998111300562 19981113 00562 NM 1998 11 13 SWAA982725 1 19981102 A 5320 BRACKET BOEING 737 7373A4 1384585 NM BS 177 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND GLIDE SLOPE ANTENNA MOUNT BRACKET CRACKED, EXTENDING BEYOND STOP DRILL AT BS 177, RBL 6. REPAIRED CRACK PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300563 19981113 00563 NM 1998 11 13 SWAA982726 1 19981102 A 5320 WEB BOEING 737 7373A4 1384585 NM DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND DOORWAY LOWER WEB CORRODED ON NUT PLATES HOLES AND SCREWS DRILLED OFF. REMOVED AND R EPLACED DOORWAY WEB PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300564 19981113 00564 NM 1998 11 13 SWAA982727 1 19981102 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 727 LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND L SUPPORT ANGLE HAS LOOSE BOLTS AND MISSING WASHER AT BS 727+4, LBL 8 RT UNDER FLOOR BEAMS. REMOVED AND REPLACED FASTENERS PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300565 19981113 00565 NM 1998 11 13 SWAA982728 1 19981102 A 5320 FASTENERS BOEING 737 7373A4 1384585 NM FLOORBEAM SHEARED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND FASTENERS SHEARED AT FLOORBEAM TO FRAME AT BS 787, 794, 807 AND 827, RBL 8. REMOVED AND REPLACED FASTENERS PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300566 19981113 00566 NM 1998 11 13 SWAA982729 1 19981102 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED FLOORBEAM AT BS 773, RBL 3. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300567 19981113 00567 NM 1998 11 13 SWAA982730 1 19981102 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 773 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED FLOORBEAM AT BS 773, RBL 8. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300586 19981113 00586 EU 1998 11 13 CA980602035 1 19980425 A 6720 704A34130058 CONTROL CABLE SNIAS 350 AS350B1 8680811 EU TMECA ARRIEL ARRIEL1B 6OO30 NE PEDAL SEIZED W B A EMER. DESCENT UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 CA 290 (CAN) PILOT REPORTED RIGHT HAND PEDAL WOULD NOT GO BEYOND NEUTRAL POSITION AND LEFT PEDAL LIMITED TRAVEL. FLEXIBLE CABL E PARTLY SEIZED. 1 G 7 1 3U 3 U H9EU E19EU 1998111300587 19981113 00587 EU 1998 11 13 CA980602041 1 19980317 A 6220 704A3363315651 STOP ASSY SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR BLISTERED W K NONE O OTHER IN INSP/MAINT 1 CA 1239 347 (CAN) MAIN ROTOR STARFLEX SPHERICAL STOPS BLISTERED. S/N'S 4420, 4422, AND 4444 REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 1998111300589 19981113 00589 EU 1998 11 13 CA980706034 1 19980625 A 3213 10550012 CROSSTUBE 10550005 BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL SKID SHOE CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 443 CAE835656 (CAN) CORROSION BLISTER ON UNDERSIDE OF AFT LANDING GEAR CROSSTUBE. CORROSION DEPTH 0.75 TO 1.25 MM OVER A VISIBLE 30 S QUARE MM AREA. SUBMITTER SUGGESTED POSSIBLE INTERGRANULAR CORROSION. 1 G 7 2 3U 3 U H3EU E4CE 1998111300590 19981113 00590 EU 1998 11 13 CA980707035 1 19980522 A 6420 9681506552 O-RING SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R SHAFT CAP MISSING W K NONE K W FLUID LOSS INADEQUATE Q C IN INSP/MAINT 1 CA 946 (CAN) TAIL ROTOR OUTPUT SHAFT CAP PACKING 'O' RING MISSING FOLLOWING OVERHAUL. 1 G 7 1 3U 3 U H9EU E19EU 1998111300591 19981113 00591 EU 1998 11 13 CA980707037 1 19980607 A 5630 350902502 SLIDER ASSY SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE RT DOOR SEPARATED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA 347 (CAN) RIGHT HAND SLIDER WINDOW ASSY DEPARTED IN CRUISE. SLIDER RAILS IN GOOD CONDITION AND FIRMLY ATTACHED TO WINDOW. D OOR HAD BEEN REMOVED THE DAY BEFORE FOR SLINGING OPERATIONS. 1 G 7 1 3U 3 U H9EU E19EU 1998111300593 19981113 00593 EU 1998 11 13 CA980707041 1 19980614 A 2822 P94B12203C PUMP SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL BOOST LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 428 22723 347 (CAN) FUEL BOOST PUMP VIBRATES AND IS EXTREMELY NOISY. ON REMOVAL, FELT LIKE THE ARMATURE WAS LOOSE. 1 G 7 1 3U 3 U H9EU E19EU 1998111300596 19981113 00596 NM 1998 11 13 CA980804035 1 19980725 A 7120 8DK1763001 STRUT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE ENGINE MOUNT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 31970 120367 (CAN) A 300 DEGREE CRACK FOUND ON INSPECTION, TASK NR 5440/07F. STRUT WAS ORIGINAL INVENTORY AND HAD BEEN REWORKED TO P OST SB 8-71-17. COMPONENT SENT TO DEHAVILLAND FOR EVALUATION. PART TC: 36,346. 2 H 7 2 4T 4 T RT A13NM E20NE 1998111300599 19981113 00599 NM 1998 11 13 CA980810023 1 19980804 A 5714 NAS1465 BOLT 85710002005 DHAV DHC8 DHC8101 2809002 NM PWA 120 PW120A NE WS 42 & 43 CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 120830 (CAN) ON 40,000 CYCLES INSPECTION, LOCKBOLTS WERE FOUND FACTORY INSTALLED WITH STEEL WASHERS. 20 ON THE RIGHT SIDE AND 16 ON THE LEFT SIDE. GALVANIC CORROSION HAD STARTED TO DEVELOP. BRAD CONTACTED FOR REPAIR. LOCKBOLTS REMOVED AND WING BOX SKIN TREATED FOR CORROSION DAMAGE. NEW HI-LOCKS INSTALLED PER RD8-51-102. 2 H 7 2 4T 4 T RT A13NM E20NE 1998111300600 19981113 00600 SW 1998 11 13 CA980811003 1 19980729 A 3211 2735050001 BUSHING OAS55011 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT MLG BINDING W L ABORTED APPROACH O OTHER AP APPROACH 1 CA P54143 (CAN) LEFT MAIN GEAR FAILED TO EXTEND AFTER SEVERAL ATTEMPTS. GEAR MANUALLLY EXTENDED AND AIRCRAFT LANDED OK. INSPECT ION REVEALED THAT THE UPPER DRAG BRACE PIVOT BUSHINGS WERE PUSHED OUT TOWARDS THE UPPER DRAG BRACE BINDING THE BRACE AND PREVENTING IT FROM ROTATING FREELY. IT IS SUSPECTED THAT THESE BUSHINGS WERE PUSHED OUT FROM THE FORCE OF OVER GREASIN G THE PIVOT PIN. 2 L 7 2 4T 4 T RT A8SW E4WE 1998111300608 19981113 00608 EA 1998 11 13 CA980811012 1 19980805 A 2422 HARNESS DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA AC SYSTEM CHAFED W H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 CA PCE41522 (CAN) INTERMITTENT DOUBLE INVERTER FAILURE IN VFR FLIGHT. FOUND WIRE NUMBER X5B20, THE 115VAC FEED FROM THE INVERTER CO NTROL SWITCH TO THE THE AC FUSE PANEL CHAFED ON A CEILING PANEL SUPPORT STRINGER ON THE RIGHT HAND SIDE OF THE CABIN AT STA 1220.0. 1 H 7 2 3T 4 T RT A9EA E4EA 1998111300610 19981113 00610 NE 1998 11 13 CA980811014 2 19980715 A 7310 0301007710 LINE SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE FUEL SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 9132 (CAN) DURING INSPECTION, A FUEL LEAK WAS FOUND ON THE FUEL INJECTOR LINE AT THE FLAIRED AREA NEAR THE B-NUT. THE LINE W AS REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 1998111300612 19981113 00612 NE 1998 11 13 CA980814001 1 19980702 A 6210 7615009000051A SPAR 761500900051 SKRSKY S76 S76A 8143006 NE TMECA ARRIEL ARRIEL1S 60030 NE M/R BLADE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 13441 A08601414 3522TEC (CAN) ON 500-HOUR INSPECTION, CRACK IN THE ROOT END OF M/R BLADE. BLADE SCRAPPED. 1 G 7 2 3U 3 U H1NE E19EU 1998111300616 19981113 00616 CE 1998 11 13 CA980814005 1 19980806 A 5330 SKIN CESSNA 182 182G 2072716 CE FUSELAGE WRINKLED W O OTHER O OTHER LD LANDING 1 CA 1503 (CAN) ON LANDING OF FLOAT EQUIPPED AIRCRAFT HIT LARGE WAVE. ON RETURN TO DOCK, INVESTIGATON FOUND THE SIDE SKINS AND LO WER COWL WERE WRINKLED. FURTHER EXAMINATION FOUND THE FIREWALL AND BELLY SKINS WERE ALSO WRINKLED. NEW REINFORCED FIRE WALL AND TUNNEL INSTALLED. 1 H 7 1 3O NT 3A13 1998111300621 19981113 00621 NM 1998 11 13 CA980814011 1 19980721 A 2510 ACTUATOR BOEING 747 747433 NM PWA 4056 PW4056 NE SEAT 1K FAILED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA P724696 (CAN) 45 MINUTES PRIOR TO LANDING, THE FLIGHT DIRECTOR ADVISED THE CAPTAIN THAT SMOKE WAS EMANATING FROM SEAT 1K. FIRST OFFICER DISCONNECTED LUMBAR SUPPORT MOTOR AND SMOKE STOPPED. MOTOR REPLACED. 2 L 7 4 4F 4 F RT A20WE E24NE 1998111300622 19981113 00622 EU 1998 11 13 CA980814012 1 19980717 A 5350 RADOME AIRBUS A340 A340313 EU FUSELAGE BIRD STRIKE W O OTHER O OTHER CR CRUISE 1 CA (CAN) MUTIPLE BIRD STRIKES ON RADOME. MAINTENANCE INSPECTION OF RADOME CONFIRMED BIRD STRIKES, NO DAMAGE TO RADOME, ENG INES/VANES OR PITOT STATIC SYSTEM. 2 L 7 4 4F RT A197 1998111300623 19981113 00623 NM 1998 11 13 CA980814013 1 19980731 A 3244 TIRE BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE MLG FAILED W O OTHER O OTHER LD LANDING 1 CA P685968 (CAN) NR 8 TIRE BLOWN ON LANDING. REPLACED NR'S 7 AND 8 WHEELS, BRAKES AND AXLES. 2 L 7 4 4F 4 F A20WE E20EA 1998111300624 19981113 00624 NM 1998 11 13 CA980814014 1 19980730 A 2760 ROD BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE DRAG CONTROL OUT OF ADJUST W O OTHER J WARNING INDICATION TO TAKEOFF 1 CA P707550 (CAN) WHEN TAKEOFF POWER APPLIED, CONFIGURATION WARNING HORN CAME ON AND ENGINE INDICATING AND CREW ALERT SYSTEM MESSAGE SPOILERS ANNUNCIATED, LEVER IN FORWARD DOWN POSITION, TAKEOFF REJECTED. SPEED BRAKE CONTROL ROD ADJUSTED PER MM 27-62- 04. AUTO SPEED BRAKE TEST CARRIED OUT, SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1998111300625 19981113 00625 EA 1998 11 13 CA980818004 2 19980708 A 7530 311325201 VALVE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 ENGINE FAILED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 1446 PCE123138 (CAN) AFTER START, WHEN NR 2 ENGINE BLEED AIR SELECTED ON, THE CABIN FILLED WITH SMOKE. THE ENGINE WAS SHUTDOWN. INSPE CTION FOUND THE NR 2 ENGINE P2.5 SWITCHING VALVE COVER AND SLEEVE GROOVED. THE PARTS WERE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998111300626 19981113 00626 NM 1998 11 13 CA980818008 1 19980729 A 2530 65501961 COFFEE MAKER AIRCRFTPRDTS 3510001601 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE GALLEY MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 20168 0123 708821 (CAN) COFFEE MAKER FLASHED AND SMOKED, SMELL OF BURNING ENSUED. REPLACED COFFEE MAKER. PHASE LOSS DETECTOR CARD RESIST OR OVERLOADED AND BURNT. 2 L 7 2 4F 4 F A16WE E2EA 1998111300627 19981113 00627 1998 11 13 CA980818009 4 19980804 A 3418 861CAK SENSOR GULTON 861CAK BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE AOA DAMAGED W A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 CA 15481 4738 419013 687719 (CAN) STICK SHAKER ACTIVATION AT ROTATION. STICK SHAKER CONTINUED AFTER ROTATION. FOUND VANE BENT. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1998111300628 19981113 00628 WP 1998 11 13 CA980818010 1 19980731 A 5712 ARB23394 RIB ARB296115 DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE RT WING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 70438 517818 (CAN) ON WALK-AROUND, FOUND INSPECTION DOOR PANEL AT RIGHT HAND WING LOWER LEADING EDGE, LOWER SURFACE, OUTBOARD OF NR 3 PYLON AT DROOP LEADING EDGE WITH PULLED SCREWS AND WORN HOLES. FURTHER INSPECTION REVEALED RIB, ARB2339-4, ANGLE ARB30 13-13, SILL ARB1334-12, WEB ARB1334-4, CRACKED AND WORN. REPAIRED PER EVA98-D10-57-1259 AND DOUGLAS DWG. ARB 1334. PAR T TC: 11,099. 2 L 7 3 4F 4 F A22WE E23EA 1998111300629 19981113 00629 NM 1998 11 13 CA980818011 1 19980506 A 7603 NUT BOEING 727 72725 1384006 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE LOOSE W E ENGINE SHUTDOWN O OTHER DE DESCENT 1 CA 666036 (CAN) ON TOP OF DESCENT, CREW ATTEMPTED TO RETARD THE THRUST LEVERS TOWARDS FLIGHT IDLE. THE NR 2 ENGINE CONTROL WOULD NOT MOVE. THE ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE CROSS SHAFT RETAINING NUT HAD BACKED O FF AND RESTRICTED THE MOVEMENT OF THE FUEL CONTROL UNIT PUSH/PULL RODS. THE NUT WAS INSPECTED, REINSTALLED AND SECURED. THE ENGINE WAS RUN-UP SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998111300631 19981113 00631 GL 1998 11 13 CA980818015 2 19980703 A 7323 23006259 GOVERNOR 23006259 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TURBINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 2038 95AAD0001 CAE821010 (CAN) ROTOR RPM VARIES BETWEEN 95 TO 105 PERCENT. EXCESSIVE, SLOW OR NO RECOVERY UNDER DIFFERENT FLIGHT CONDITIONS. 1 G 7 1 3U 3 U H2SW E4CE 1998111300632 19981113 00632 EA 1998 11 13 CA980818016 1 19980707 A 6297 WIRE CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE MAIN ROTOR MISINSTALLED W K NONE L W NO TEST INADEQUATE Q C NR NOT REPORTED 1 CA 295035 (CAN) MAIN ROTOR BLADE B.I.M. TRANSDUCER TEST IN COCKPIT OK BUT ALL 5 M/R BLADE TRANSDUCERS DID NOT TEST. WIRES CROSSED AT TERMINAL STRIP 46. 2 G 7 2 4U 4 U H8EA 1E3 1998111300633 19981113 00633 SW 1998 11 13 CA980818017 1 19980712 A 7810 23031899 COLLECTOR BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL EXHAUST CRACKED W K NONE B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS IN INSP/MAINT 1 CA 2323 721 CAT70541 CAE860756 (CAN) ENGINE OIL CONSUMPTION WAS 1 LITRE PER HOUR AND SMOKE WAS COMING FROM THE EXHAUST STACK. INSPECTION FOUND THE 1ST STAGE NOZZLE AND EXHAUST COLLECTOR TO BE CRACKED BEYOND LIMITS. PART TC: 925. 1 G 7 1 3U 3 U H2SW E1GL 1998111300634 19981113 00634 EU 1998 11 13 CA980818018 1 19980713 A 6210 370 ABRASION STRIP 350A11001001 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R BLADE SEPARATED W A B UNSCHED LANDING EMER. DESCENT D INFLIGHT SEPARATION CR CRUISE 1 CA 9969 370 834 (CAN) LOWER ABRASION STRIP SEPARATING 11 CM FROM EDGE OF BLADE INBOARD 4 BY 5 CM TO TRAILING EDGE FROM JUST BEHIND STAIN LESS STEEL LEADING EDGE STRIP. 1 G 7 1 3U 3 U H9EU E19EU 1998111300635 19981113 00635 NE 1998 11 13 CA980818019 2 19980221 A 7230 0292152860 COVER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE COMPRESSOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 345 (CAN) COMPRESSOR COVER CRACKED IN AREA OF APERTURE AND PIECE BROKE AWAY. CENTRIFUGAL COMPRESSOR SCRAPPED DUE TO FOD. C RACK OCCURRED IN EXACT LOCATION AND SIZE AS INDICATED IN THE TURBOMECA ARRIEL 1 MAINTENANCE MANUAL, CHAPTER 72-30-10, FI GURE 605. 1 G 7 1 3U 3 U H9EU E19EU 1998111300636 19981113 00636 GL 1998 11 13 CA980818020 2 19980623 A 7210 6894171 GEAR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL GEARBOX BROKEN W K NONE J WARNING INDICATION DE DESCENT 1 CA 10722 9750 CAE8282558 (CAN) PILOT REPORTED CHIP LIGHT. INSPECITON FOUND PIECE OF GEAR TOOTH FROM THE FUEL CONTROL UNIT DRIVE TRAIN FOUND ON L OWER CHIP DETECTOR PLUG. 1 G 7 1 3U 3 U H2SW E4CE 1998111300637 19981113 00637 SW 1998 11 13 CA980818021 1 19980717 A 6730 206076031013 SERVO 206076031013 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FLIGHT CONTROL FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 7212 17 5415 CAE821623 (CAN) NEWLY INSTALLED HYDRAULIC SERVO CAUSING FEEDBACK IN CONTROLS. SERVO REPLACED AND FEEDBACK NIL. 1 G 7 1 3U 3 U H2SW E4CE 1998111300638 19981113 00638 GL 1998 11 13 CA980818022 2 19980629 A 7261 6853464 LINE BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL OIL SYSTEM BENT W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE830144 (CAN) NR 6 AND NR 7 SCAVENGE OIL LINE (P/N 6853464) REMOVED, FOUND BENT AND DENTED. LINE WAS ALSO INCORRECTLY INSTALLED ONTO NR 8 BEARING SCAVENGE OIL INLET FITTING. NR 8 BEARING SCAVENGE OIL LINE (P/N 6853463) REMOVED, FOUND BENT AND DEN TED. THE LINE WAS ALSO FOUND INCORRECTLY INSTALLED ONTO NR 6 AND NR 7 BEARING SCAVENGE OIL INLET FITTING. PART TC: 20 ,872. 1 G 7 1 3U 3 U H2SW E4CE 1998111300644 19981113 00644 NE 1998 11 13 CA980818032 2 19980512 A 7200 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE BAY MALFUNCTIONED W O OTHER E VIBRATION/BUFFET NR NOT REPORTED 1 CA 20219 14453 PCE120698 (CAN) UNUSUAL NOISE AND VIBRATION ON ENGINE START. THE ENGINE WAS REPLACED. INSPECTION FOUND THE ONLY COMPONENTS IN THE ACCESSORY GEARBOX DRIVE TRAIN WHICH SHOWED SIGNS OF SIGNIFICANT WEAR WERE THE OIL PUMP DRIVE BEVEL GEARS AND THE SPLINE S ON THE COUPLING SHAFT. SUBMITTER STATED THIS WEAR IS COMMON AND IS KNOWN TO CAUSE ENGINE VIBRATION. PART TC: 24,744 . 2 H 7 2 4T 4 T RT A13NM E20NE 1998111300655 19981113 00655 CE 1998 11 13 CA980825003 1 19980811 A 5311 5042002858 FRAME BEECH 100 100BEECH 1152916 CE PWA PT6 PT6A28 EA BS 207 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 17825 PCE41762 (CAN) FUSELAGE RIGHT FRAME AT STA 207 CRACKED THROUGH. CRACK RUNS FROM A STRINGER CUTOUT TO TWO DIFFERENT LIGHTING HOLE S. IN ADDITION, THERE ARE TWO SKIN CRACKS RADIATING FROM A SINGLE RIVET HOLE. THIS IS HOW THE CRACK WAS FOUND. REPAIRE D. PART TC: 24,227. 1 L 7 2 3T 4 T A14CE E4EA 1998111300663 19981113 00663 EU 1998 11 13 CA980825016 1 19980811 A 6520 350A33101120 COVER AEROSP 350A33020004 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R GEARBOX CRACKED W O OTHER E J VIBRATION/BUFFET WARNING INDICATION LD LANDING 1 CA 7657 2117 M660 4120 (CAN) AFTER LANDING, AS M/R RPM DECREASING THROUGH 300 RPM, UNUSUAL TAIL ROTOR VIBRATION FOLLOWED BY T/R CHIP LIGHT. T/ R GEARBOX CHANGED. OIL DRAINED FROM GEARBOX CONTAINED MINUTE AMOUNT OF FERROUS AND A LOT OF NON-FERROUS METAL PARTICLES . DISASSEMBLY REVEALED CRACK IN COVER ADJACENT TO ROLLER BEARING OUTER RACE AND THROUGH OIL GALLERY. 1 G 7 1 3U 3 U NC H9EU E19EU 1998111300664 19981113 00664 SW 1998 11 13 CA980825019 1 19980730 A 6710 4192102901 TRIM SWITCH ENSTRM 480 480TH28 SW ALLSN 250C 250C20 03013 GL CYCLIC FAILED W C ABORTED TAKEOFF F FLT CONT AFFECTED TO TAKEOFF 1 CA CAE845007 (CAN) TRIM SWITCH UNIT FAILED AS THE HELO WAS TAKING OFF, UNABLE TO TRIM FORWARD CYCLIC. 1 G 7 1 3O 3 U 0 H1CE E4CE 1998111300665 19981113 00665 NE 1998 11 13 CA980825020 2 19980814 A 8520 12081P4 STUD DHAV DHC2 DHC2MK1 2800102 EA PWA R985 R985AN14B 52008 NE NR 3 CYLINDER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA MM2018 (CAN) DURING INSPECTION, TWO CYLINDER HOLD-DOWN STUDS WERE FOUND BROKEN. ONE AT THE BASE OF NR 3 CYLINDER AND ONE AT TH E BASE OF NR 8 CYLINDER. 1 H 7 1 3R 3 R A806 5E1 1998111300668 19981113 00668 NM 1998 11 13 CA980827001 1 19980814 A 5620 655456011 WINDOW BOEING 727 72751C 1384015 NM PWA JT8 JT8D7B 52053 NE CABIN DAMAGED W K NONE D INFLIGHT SEPARATION NR NOT REPORTED 1 CA 654436 (CAN) AFTER ARRIVAL ON WALK-AROUND, FOUND NR 31 LEFT CABIN WINDOW DAMAGED, CENTER AREA OUTER PANE MISSING. REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1998111300671 19981113 00671 SW 1998 11 13 CA980827008 1 19980806 A 6210 212015501005 BLADE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA MAIN ROTOR DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 2699 60220 (CAN) ON DAILY INSPECTION, VOID FOUND IN NR 2 DOUBLER EXCEEDING LIMITS. BLADE REPLACED. 1 G 7 1 4U 4 U H4SW E22EA 1998111300672 19981113 00672 SW 1998 11 13 CA980827009 1 19980812 A 6210 212015501005 BLADE BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3421 60220 (CAN) ON DAILY INSPECTION, FOUND REPAIR PATCH MISSING FROM THE UNDERSIDE OF BLADE S/N A-833. DURING REMOVAL OF RESIDUAL ADHESIVE, A CRACK WAS FOUND IN THE SKIN AT 111.25 INCHES FROM TIP AND 6 INCHES FROM LEADING EDGE. THE 20 INCH LONG CRA CK ORIGINATES AT A NICK UNDER THE MISSING PATCH AND PASSES THROUGH AN ADJACENT PATCH PROGRESSING TOWARDS THE TRAILING ED GE. 1 G 7 1 4U 4 U H4SW E22EA 1998111300677 19981113 00677 NM 1998 11 13 CA980827015 1 19980806 A 2197 WIRE BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE AC BAY MISSING W A UNSCHED LANDING O OTHER TO TAKEOFF 1 CA P707529 (CAN) AIRCRAFT WAS UNABLE TO PRESSURIZE DURING CLIMB. FOUND GROUND WIRE MISSING ON PIN 11 OF D1872 COOLING CARD M867, W IRE W506-536-24 NOT CONNECTED TO P5552 CONNECTOR. WIRES INSTALLED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998111300679 19981113 00679 EU 1998 11 13 CA980827020 1 19980717 A 5350 RADOME AIRBUS A340 A340313 EU NOSE BIRD STRIKE W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) MULTIPLE BIRD STRIKES ON RADOME. MAINTENANCE CONFIRMED EVIDENCE OF MULTIPLE BIRD STRIKES ON RADOME. AIRCRAFT CHE CKED FOR OTHER DAMAGE AND NONE FOUND. AIRCRAFT DECLARED SERVICEABLE. 2 L 7 4 4F RT A197 1998111300680 19981113 00680 EU 1998 11 13 CA980827024 1 19980810 A 2530 TRAY AIRBUS 320 A320211 3930320 EU GALLEY CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) SMOKE OBSERVED IN GALLEY. SUBMITTER STATED PROBLEM CAUSED BY TAPE LEFT ON FOOD TRAY. TAPE REMOVED AND SMOKE/SMEL L DISAPPEARED. 2 L 7 2 4F RT A28NM 1998111300691 19981113 00691 NM 1998 11 13 CA980908014 1 19980811 A 7603 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE POWER LEVER FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 22392 120581 (CAN) DURING ENGINE CHANGE, FOUND LEFT CONDITION LEVER CABLE FRAYED WHERE IT PASSES OVER PULLEY, FORWARD OF THE ENGINE F IREWALL. CABLE ASSEMBLY REPLACED. PART TC: 23,209. 2 H 7 2 4T 4 T RT A13NM E20NE 1998111300706 19981113 00706 NE 1998 11 13 CA980908034 2 19980712 A 7320 LINE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE FRACTURED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 10491 (CAN) DURING CLIMBOUT, NR 2 ENGINE HAD A LOSS OF POWER. THE FUEL FLOW REGULATOR WAS REPLACED, BUT THE SNAG WAS NOT FIXED . FURTHER INSPECTION FOUND THE P1 LINE BROKEN AT THE PROBE. THE LINE WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE . 2 L 7 3 4F 4 F A23WE E12EU 1998111300707 19981113 00707 WP 1998 11 13 CA980908037 1 19980820 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE BS 901 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10284 (CAN) 3 INCH CRACK FOUND IN FUSELAGE OUTER SKIN TRIPLER AT R2 DOOR CUT-OUT LOWER CORNER. FS901 WL 206 REPAIRED PER SB 0 93-53-237 REV 4. 2 L 7 3 4F 4 F A23WE E12EU 1998111300708 19981113 00708 NE 1998 11 13 CA980908038 2 19980824 A 7314 PUMP LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NR 1 ENGINE FAILED W O OTHER O OTHER TO TAKEOFF 1 CA 10510 (CAN) NR 1 ENGINE COULD NOT OBTAIN TAKEOFF E.P.R. FUEL FLOW REGULATOR REPLACED AND CHECKED SERVICEABLE. THE FOLLOWING D AY THE SAME SNAG RECURRED. THE FUEL PUMP WAS REPLACED AND THE PROBLEM WAS FIXED. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 3 4F 4 F A23WE E12EU 1998111300709 19981113 00709 WP 1998 11 13 CA980908039 1 19980628 A 5350 1533890135 FAIRING LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE FUSELAGE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 10205 (CAN) ON TURNAROUND INSPECTION, FOUND HALF OF C-2 CARGO DOOR FAIRING MISSING. RIGHT STABILIZER LEADING EDGE BENT, POSSI BLY HIT BY FAIRING. LEADING EDGE REPLACED AND FAIRING INSTALLED. 2 L 7 3 4F 4 F A23WE E12EU 1998111300710 19981113 00710 WP 1998 11 13 CA980908040 1 19980819 A 5320 1518648101 FITTING LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE BS 1163 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10205 (CAN) DURING INSPECTION, FOUND SIDE FRAME FITTING AT FS 1163 LEFT SIDE CRACKED. FITTING TO BE REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1998111300711 19981113 00711 WP 1998 11 13 CA980908041 1 19980824 A 5210 AEH6333002 GEARBOX LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE PASSENGER DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 10205 (CAN) WHEN CLOSING REAR LEFT PASSENGER DOOR, LOUD NOISE WAS HEARD AND DOOR STOPPED MOVING. GEARBOX BROKEN, COUNTER-BALA NCE CASING UNRIVETED, AND FLEX DRIVE BOTH ENDS UNSWAGED. REPAIRED, PARTS REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1998111300719 19981113 00719 1998 11 13 CA980909007 4 19980827 A 3452 DM16013541 ANTENNA BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE ATC FAILED W D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CA 31425 (CAN) AIRCRAFT RETURNED TO RAMP DUE TO BOTH ATC TRANSPONDERS FAILED. UPPER ANTENNA REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998111300721 19981113 00721 NM 1998 11 13 CA980909009 1 19980818 A 2597 WIRE BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE GALLEY FAILED W O OTHER O OTHER CR CRUISE 1 CA P662912 (CAN) SMOKE IN NR 3 GALLEY. LIGHT ASSY WIRES FOR HOT CUP BURNT. REPAIRED. 2 L 7 4 4F 4 F A20WE E20EA 1998111300723 19981113 00723 EU 1998 11 13 CA980909011 1 19980818 A 2133 90231570381 OUTFLOW VALVE AIRBUS 320 A320211 3930320 EU CABIN PRESSURE FAILED W K NONE J WARNING INDICATION CR CRUISE 1 CA (CAN) RAPID DEPRESSURIZATION OCCURRED AT 37,000 FEET, OXYGEN MASKS DEPLOYED CABIN ABOVE 14,000 FEET, CABIN RATE OF CLIMB EXCEEDED 8,000 FEET, CONTROL REGAINED IN DESCENT, LEVELLED AT 16,000 FEET, FLIGHT CONTINUED TO DESTINATION. MAINTENANC E REPLACED OUTFLOW VALVE AND CABIN PRESSURE CONTROLLER P/N 9022-15702-9, AND OXYGEN GENERATORS. SYSTEM CHECKED SERVICEA BLE. 2 L 7 2 4F RT A28NM 1998111300725 19981113 00725 EA 1998 11 13 CA980909013 1 19980821 A 4920 APU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE APU BAY MALFUNCTIONED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 807365 (CAN) ON DEPARTURE CLIMB OUT, WHEN AIR CONDITIONING PACKS TURNED ON, SMOKE PRESENT IN CABIN AND FLIGHT DECK. PACKS TURN ED OFF AND SMOKE DISSIPATED. AUXILIARY POWER UNIT CHANGED. PACKS OPERATED NORMALLY. 2 L 7 2 4F 4 F RT A21EA E15NE 1998111300726 19981113 00726 EA 1998 11 13 CA980909014 2 19980822 A 7530 20035008067 CONTROL UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NR 1 ENGINE MALFUNCTIONED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA 807335 (CAN) NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO 14 STAGE DUCT AND AURAL MESSAGE. POST-FLIGHT INSPECTION FOUND NO DAMAGE TO THE LEFT HAND ENGINE PYLON DUCT. THE LEFT HAND BLEED CONTROLLER AND THE SENSING ELEMENT WERE REPLACED AND THE ENGINE WA S GROUND RUN SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998111300727 19981113 00727 1998 11 13 CA980909016 4 19980817 A 3417 40633513 ADC AIRBUS A319 A319114 NM E/E BAY INOPERATIVE W O OTHER J WARNING INDICATION AP APPROACH 1 CA (CAN) ON FINAL APPROACH, AIRCRAFT HAD A SUDDEN SHARP MOVEMENT WHEN FLAPS WERE SELECTED. AN AIRSPEED DIFFERENCE OF 10 TO 20 KNOTS BECAME APPARENT. THIS CONTINUED DOWN TO ROLL-OUT. CAPTAIN'S AIRSPEED SHOWED 70, 1ST OFFICER ZERO. NR 2 AIR D ATA AND INERTIAL REFERENCE UNIT INOPERATIVE. AIR DATA MODULE REPLACED AND SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998111300730 19981113 00730 WP 1998 11 13 CA980909023 1 19980823 A 2120 LS11088A1814 DUCT LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE AC BAY LOOSE W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 10510 (CAN) AFTER TAKEOFF, AIR CONDITIONING LEAK IN F.E.S.C. HEAVY LANDING CARRIED OUT. FOUND MOISTURE CONTROL MODULATING VA LVE DUCT ADRIFT. CLAMP INSTALLED. 2 L 7 3 4F 4 F A23WE E12EU 1998111300731 19981113 00731 NM 1998 11 13 CA980909025 1 19980722 A 2610 LOOP BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE RT ENGINE CHAFED W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 30734 (CAN) ON A CHECK EICAS MESSAGE, RIGHT ENGINE LOOP I, STATUS MESSAGE. LOOP WIRE CHAFED ON STARTER DUCT. LOOP REPAIRED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998111300738 19981113 00738 NM 1998 11 13 CA980915007 1 19980901 A 5230 85230448001 LINK ASSY 85230310001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CARGO DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 19419 120549 (CAN) CARGO DOOR WOULD NOT CLOSE. LINK ASSEMBLY FOUND BROKEN AT LOWER END. LINK ASSEMBLY REPLACED. CHECKED SERVICEABL E. PART TC: 21,951. 2 H 7 2 4T 4 T RT A13NM E20NE 1998111300739 19981113 00739 EU 1998 11 13 CA980915008 1 19980831 A 6220 350A31190703 STARFLEX AEROSP 355A31000106 SNIAS 350 AS350B2 8680813 EU ARM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 639 M936 (CAN) 2 CRACKS FOUND ON POS-FLIGHT INSPECTION. ONE CRACK DRESSED OUT PER MRR 62.20.00.772. SECOND CRACK WAS BEYOND LIM ITS PER MWC 62.20.00.601. PART TC: 1,409. 1 G 7 1 3U H9EU 1998111300741 19981113 00741 WP 1998 11 13 TWAA9817901 1 19981105 A 5330 SKIN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C, MAINT FOUND FUSELAGE SKIN CRACKED AT AFT HINGE CUTOUT FOR THE NOSE GEAR RT STRUT DOOR. INSTALLED DOUBLE R OF 0.063 7075T6 WITH AD-5 RIVETS. AREA PRIMED AND PAINTED. 2 L 7 2 4F A6WE 1998111300742 19981113 00742 WP 1998 11 13 TWAA9818001 1 19981106 A 5347 FLOOR TRACK DOUG DC9 DC983 3022083 WP BS 1193-1203 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9303K 49529 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR TRACK AT LBL 55, STA 1193 TO 1203. REPLACED TRACK WITH NEW USI NG MFG C0358-1. INSTALLED SAME FASTENERS AS ORIGINAL PER SPM 6-70-01 PG 3 AND 6-30-07 PG 1 AND 2. 2 L 7 2 4F RT A6WE 1998111300743 19981113 00743 WP 1998 11 13 TWAA9818002 1 19981103 A 5330 SKIN DOUG DC9 DC951 3022051 WP PAX DOORWAY CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 417EA 47753 MAINT FOUND, APPROX .25 INCH CRACK IN LOWER LEFT CORNER CUTOUT OF THE AFT ENTRY DOOR. STOP DRILLED AND SEALED CRACK PE R EMLR 68997 AND COMPLIED WITH EMLR 68995. CHECK-C 7-26-98 STL. 2 L 7 2 4F RT A6WE 1998111300744 19981113 00744 WP 1998 11 13 TWAA9818003 1 19981106 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 385-391 DENTED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9303K 49529 DURING OP 15 MAINT CHECK, FOUND SIX INCH BY 12 INCH BY 0.070 INCH DENT IN FUSELAGE SKIN AT STA 385 TO 391, LONGERON 29L TO 29R. REPAIRED PER ARA 15743. 2 L 7 2 4F RT A6WE 1998111300745 19981113 00745 WP 1998 11 13 TWAA9818004 1 19981106 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 409 WRINKLED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9303K 49529 DURING OP 15 MAINT CHECK, FOUND FUSELAGE SKIN WRINKLED AT STA 409, LONGERON 29R TO 30R. REPAIRED PER ARA 15743. 2 L 7 2 4F RT A6WE 1998111300746 19981113 00746 WP 1998 11 13 TWAA9818005 1 19981106 A 5347 FLOOR TRACK DOUG DC9 DC983 3022083 WP BS 1240-1244 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9303K 49529 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR TRACK AT LBL 55, STA 1240 TO 1244. REPLACED TRACK WITH NEW TRA CK MFG C03580-1. INSTALLED NEW FLOOR TRACK WITH SAME FASTENERS PER SPM 6-70-01 PAGE 3, AND 6-30-07, PG 1 AND 2. 2 L 7 2 4F RT A6WE 1998111300747 19981113 00747 NM 1998 11 13 TWAA9818006 1 19981019 A 5730 SKIN BOEING 767 767231 1385131 NM BS 846 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON CENTER FUEL TANK UPPER SKIN AT STA 846, RBL 79 TO 83. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. NO CRACKS FOUND USING HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PART 6. REPAIRED PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300748 19981113 00748 NM 1998 11 13 TWAA9818007 1 19981019 A 5730 SKIN BOEING 767 767231 1385131 NM BS 850-852 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION AT UPPER SKIN CENTER WING AT STA 850 TO 852.5, RBL 83.5 TO RBL 88.5, INTERGRAN ULAR CORROSION. SANDED CORROSION PER SRM 51-10-00, PAGE 16 PARA 6. ACCOMP HIGH FREQ EDDY CURRENT NDT PER 51-00-03, PAR T 6 AND NO CRACKS FOUND. REPAIRED PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300749 19981113 00749 NM 1998 11 13 TWAA9818008 1 19981026 A 5330 SKIN BOEING 767 767231 1385131 NM BS 830-852 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION AT UPPER SKIN STA 830 TO 852, RBL 74 TO RBL 97. REMOVED CORROSION PER S RM 51-10-00. NDT HIGH FREQ EDY CURRENT PER 51-10-03, PART 6 AND NO CRACKS FOUND. REPAIRED PER TWA ARA 11596. 2 L 7 2 4F RT A1NM 1998111300750 19981113 00750 NM 1998 11 13 TWAA9818009 1 19981026 A 5730 SKIN BOEING 767 767231 1385131 NM BS 860 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND HEAVY CORROSION ON UPPER SURFACE OF WING CENTER SECTION AT STA 860 BELOW EMERGENCY EXIT ON RT SIDE. CUT OUT CORRODED AREA PER SRM 51-10-00. ACCOMP NDT HIGH FREQ EDDY CURRENT PER 51-00-03, PART 6 AND NO CRAC KS FOUND. REMOVED CORROSION AND APPLIED REPAIR PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300751 19981113 00751 NM 1998 11 13 TWAA9818010 1 19981026 A 5730 SKIN BOEING 767 767231 1385131 NM BS 858-954 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND INTERGRANULAR CORROSION ON CENTER UPPER WING SKIN AT STA 954.5 TO 858, RBL 75 TO RBL 88. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 51-00-03, PART 6, AND NO CRACKS FOUND. REMOVED COR ROSION AND APPLIED REPAIR TO AREA PER ARA 11596. 2 L 7 2 4F RT A1NM 1998111300752 19981113 00752 NM 1998 11 13 TWAA9818011 1 19981026 A 5730 SKIN BOEING 767 767231 1385131 NM BS 853-853 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND BELOW UPPER CENTER WING SKIN SUPPORT BEAM WITH EXIFOLIATION CORROSION THRU BEAM. CORRO SION VISIBLE FROM STA 855 TO 853 RBL 75 TO RBL 86. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER TWA NDT MANUAL 5 1-10-03, PART 6 AND NO CRACKS FOUND. REPAIRED DAMAGED AREA PER ARA 11596A. 2 L 7 2 4F RT A1NM 1998111300753 19981113 00753 NM 1998 11 13 TWAA9818012 1 19981026 A 5730 SKIN BOEING 767 767231 1385131 NM BS 853-855 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, CENTER WING UPPER SKIN WAS CUT OUT FOR CORROSION TO SKIN STA 853 TO 855. RECTANGULAR SECT FRO NT 71 RBL TO 84 RBL AND REAR 69 RBL TO 86 RBL. ACCOMP HIGH FREQ EDDY CURRENT OF AREA AND HOLES PER 51-00-03 PART 6 OF T WA NDT MANUAL AND NO CRACKS FOUND. REPAIRED DAMAGED AREA PER ARA 11596A. 2 L 7 2 4F RT A1NM 1998111300754 19981113 00754 WP 1998 11 13 VJ9800584 1 19981106 A 2560 11331 COVER DOUG DC9 DC932 3022066 WP L1 DOOR DISLODGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 940VV 47523 FWD MAIN PASSENGER DOOR SLIDE COVER DISLODGED. REINSTALLED IAW MM 25-62-0 AND PERFORMED REQUIRED INSPECTION. 2 L 7 2 4F A6WE 1998111300755 19981113 00755 WP 1998 11 13 VJ9800585 1 19981001 A 5311 9919619503N FRAME DOUG DC9 DC932 3022066 WP FS 737 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 MAIN FRAME AT FS 737 LT CRACKED AT FWD SIDE I/B POCKET PT H TOWARD PT G. REPLACED FRAME IAW EO 12-5311-29-B1044, DC9 SR M 51-30-2, 51-30-5, 51-30-8. 2 L 7 2 4F A6WE 1998111300756 19981113 00756 WP 1998 11 13 VJ9800586 1 19981001 A 5210 991556531 BEAM DOUG DC9 DC932 3022066 WP PAX DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 LOWER BEAM AFT ENTRY DOOR SURFACE CORRODED AND CHAFE MARK 5 INCHES I/B OF LT LOWER CORNER. REPLACED BEAM IAW DC9 SRM 51 -30-01 AND DWG NR 9915565. 2 L 7 2 4F A6WE 1998111300757 19981113 00757 EU 1998 11 13 MALA976224 1 19981105 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU ROW 9A FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 98XJ 098 DURING INSPECTION, OVERHEAD EMERGENCY LIGHT 9A INOP. MAINTENANCE RELAMPED, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998111300758 19981113 00758 EU 1998 11 13 JBXA9800057 1 19981107 A 2130 566920 VALVE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU E & E COMPT FAILED A JBXA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 05 131ML 11323 COMPLETE LOSS OF CABIN PRESS. OPERATIONAL CHECK OF AVIONICS OUTLET VALVE BAD. REMOVED AND REPLACED AVIONICS OUTLET VAL VE IAW 21-26-08. 2 L 7 2 4F 4 F RT 1998111300759 19981113 00759 WP 1998 11 13 CALA9802035 1 19981104 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 200-204 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 INSPECTION FOUND CORROSION ON CUSP MEMBRANE AND AFT SIDE OF FRAME AT STA 200 TO 204 JUST AFT OF MAIN CABIN DOOR AFT LOWE R CORNER INSIDE LIGHTENING HOLE. A REPAIR WAS INSTALLED IAW ECRA 5310-03778. 2 L 7 2 4F A6WE 1998111300760 19981113 00760 NM 1998 11 13 CALA9802036 1 19981104 A 5755 65173481 SKIN BOEING 727 727232 1384082 NM NR 8 SPOILER DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND TOP SURFACE OF NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-81. 2 L 7 3 4F A3WE 1998111300761 19981113 00761 NM 1998 11 13 CALA9802037 1 19981104 A 3350 FUSE BOEING 727 727232 1384082 NM CABIN BLOWN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND LT AFT EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUSE AND OPERATION C HECKED GOOD IAW MM 33-51-00. 2 L 7 3 4F A3WE 1998111300762 19981113 00762 NM 1998 11 13 CALA9802038 1 19981104 A 5753 65216352 SKIN BOEING 727 727232 1384082 NM RT TE FLAP DELAMINATED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND RT WING O/B TE AFT FLAP O/B END UPPER SURFACE DELAMINATED AT SPAR. THE AFT FLAP WAS REMOVED AND REPLAC ED IAW MM 27-51-11. 2 L 7 3 4F A3WE 1998111300763 19981113 00763 NM 1998 11 13 CALA9802039 1 19981104 A 5510 69331746 SUPPORT BOEING 727 727232 1384082 NM RT HORIZ STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A .5 INCH CRACK IN RT HORIZONTAL STABILIZER TRAILING EDGE ELEVATOR AT STA 99.79 ATTACHING HINGE SUPPORT . THE ATTACHING HINGE SUPPORT WAS REPAIRED IAW SRM 55-10-4, PAGE 10-13 AND 51-30-2, PAGE 10. 2 L 7 3 4F A3WE 1998111300764 19981113 00764 NM 1998 11 13 CALA9802040 1 19981105 A 5530 STIFFENER BOEING 727 727232 1384082 NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.5 INCH CRACK IN STIFFENER INSIDE VERTICAL FIN ABOVE S DUCT AREA AT BS 1303-1323, BL 0. A NEW STIFF ENER WAS INSTALLED IAW SRM 51-10-1, PAGE 2 AND 51-30-2, PAGE 4. 2 L 7 3 4F A3WE 1998111300765 19981113 00765 WP 1998 11 13 CALA9802041 1 19981105 A 5720 DOUBLER DOUG DC10 DC1030 3023501 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND A 2.7 INCH CRACK AND DELAMINATION ON RT WING MLG SUPPORT DOUBLER. THE CRACKED AND DELAMINATED AREAS WE RE TRIMMED OUT AND REINFORCED WITH DOUBLER AND FILLER IAW SRM 53-45-01, FIGURE 1, 51-21-01, AND ECRA 5730-01595. 2 L 7 3 4F A22WE 1998111300766 19981113 00766 WP 1998 11 13 CALA9802042 1 19981105 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 515-535 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 515 TO 535, S28L. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUB LER AND FINGER DOUBLER IAW SRM 53-20-00, FIGURE 6, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998111300767 19981113 00767 WP 1998 11 13 CALA9802043 1 19981105 A 5347 SEAT TRACK DOUG DC9 DC981 3022081 WP LT COCKPIT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND CAPTAIN'S I/B AFT SEAT TRACK CORRODED. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-4. 2 L 7 2 4F A6WE 1998111300768 19981113 00768 WP 1998 11 13 CALA9802044 1 19981105 A 5350 HANDLE DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14889 49118 THE FORCE REQUIRED TO RELEASE TAIL CONE USING THE EXTERIOR, INTERIOR, AND AFT ENTRY DOOR HANDLES WAS OUT OF LIMITS. THE HANDLES WERE ADJUSTED AND TESTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998111300769 19981113 00769 WP 1998 11 13 CALA9802045 1 19981105 A 5330 SKIN DOUG DC10 DC1030 3023501 WP BS 1942 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND RT FUSELAGE SKIN DENTED AT STA 1942, STRINGERS 51-52. THE DENTED AREA WAS TRIMMED OUT AND REINFORCED W ITH INNER AND OUTER DOUBLERS IAW SRM 53-20-00, FIGURE 6, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998111300770 19981113 00770 WP 1998 11 13 CALA9802046 1 19981105 A 5347 SEAT TRACK DOUG DC10 DC1030 3023501 WP BS 1289 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND SEAT TRACK CORRODED AT STA 1289, RBL 107. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEC TION WAS INSTALLED IAW SRM 53-70-00, FIGURE 18 AND 51-21-01. 2 L 7 3 4F A22WE 1998111300771 19981113 00771 WP 1998 11 13 CALA9802047 1 19981105 A 3350 BR964411 LIGHT BRUCE DOUG DC10 DC1030 3023501 WP SEAT 21B,34K,36B INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND THE EMERGENCY EXIT LIGHT AT SEATS 21B, 34K, AND 36B INOPERATIVE. THE EMERGENCY LIGHT IN SEATS 21B, 34K , AND 36B WERE REPLACED IAW MM 33-50-00. 2 L 7 3 4F A22WE 1998111300772 19981113 00772 WP 1998 11 13 CALA9802048 1 19981106 A 5350 CHANNEL DOUG DC10 DC1030 3023501 WP RT MLG WW CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND A 1 INCH CRACK IN HORIZONTAL CHANNEL OF OUTBOARD AFT FAIRING AT RT MLG WHEEL WELL. THE CRACKED TEE WAS REMOVED AND A NEW TEE WAS INSTALLED IAW SRM 53-53-01, FIGURE 4, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998111300773 19981113 00773 WP 1998 11 13 CALA9802049 1 19981106 A 5753 SKIN DOUG DC10 DC1030 3023501 WP LT TE FLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12064 47862 INSPECTION FOUND THE LT OUTBOARD TRAILING EDGE FLAP INBOARD SKIN DENTED AT LOWER FLAP 29 INCHES FROM INBOARD END. THE D ENTED AREA WAS TRIMMED OUT AND REINFORCED WITH DOUBLER IAW SRM 57-10-00, FIGURE 7, 51-21-01, AND 51-31-01. 2 L 7 3 4F A22WE 1998111300774 19981113 00774 SO 1998 11 13 COMA9810249 1 19981108 A 3230 12038594001 BOX CONTROL EMB 120 EMB120RT SO LANDING GEAR MALFUNCTION A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 248CA 23879 120228 LANDING GEAR WILL NOT RETRACT. REPLACED LANDING GEAR CONTROL BOX. 2 L 7 2 4T RT A31SO 1998111300775 19981113 00775 SO 1998 11 13 COMA9810250 1 19981106 A 2752 343100101 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP LEAKING A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 01 243CA 120212 BLUE HYDRAULIC SYSTEM FAILED WHEN FLAPS SELECTED FOR LANDING. REPLACED THE LEFT HAND NACELLE FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1998111300776 19981113 00776 SO 1998 11 13 COMA9810251 1 19981105 A 7712 SEDLOC2R TORQUE IND EMB 120 EMB120RT SO RT ENGINE FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 241CA 120211 RIGHT HAND ENGINE TORQUE INDICATOR FAILED. REPLACED TORQUE INDICATOR. 2 L 7 2 4T RT A31SO 1998111300777 19981113 00777 SO 1998 11 13 COMA9810252 1 19981103 A 3010 38E966A PRESSURE REG EMB 120 EMB120RT SO LT WING LEAKING A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 268CA 19572 120262 LEFT HAND BLEED AIR DUCT LEAK WARNING. REPLACED THE LEFT HAND DEICE PRESSURE REGULATOR. 2 L 7 2 4T RT A31SO 1998111300778 19981113 00778 SO 1998 11 13 COMA9810253 1 19981104 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 LOOSE A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 256CA 120245 ROW 5 EXIT SIGN FELL OFF. REPLACED THE EXIT SIGN. 2 L 7 2 4T RT A31SO 1998111300779 19981113 00779 SO 1998 11 13 COMA9810254 1 19981104 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 22259 120152 ROW 1 AND ROW 4 EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998111300780 19981113 00780 SO 1998 11 13 COMA9810255 1 19981104 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 266CA 15421 120258 EMERGENCY LIGHTING IS WEAK. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998111300781 19981113 00781 EA 1998 11 13 COMA9860337 1 19981108 A 7830 TR UNIT CNDAIR CL600 CL6002B19 EA LT ENGINE MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 948CA 7079 LEFT THRUST REVERSER MESSAGE DURING TAKEOFF. DEFERRED LEFT HAND THRUST REVERSER. 2 L 7 2 4F RT A21EA 1998111300782 19981113 00782 EA 1998 11 13 COMA9860338 1 19981108 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA CABIN DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 912CA 7011 CABIN DOOR HANDLE POPPED OUT AFTER TAKEOFF. ADJUSTED DOOR HANDLE MECHANISM. 2 L 7 2 4F RT A21EA 1998111300783 19981113 00783 NE 1998 11 13 COMA9860339 2 19981106 A 7320 CONNECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ECU DIRTY A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 991CA 7216 807496 UNCOMMANDED ACCELERATION RIGHT HAND ENGINE DURING CRUISE FLIGHT. CLEANED WIRING CONNECTOR AT ENGINE ECU. 2 L 7 2 4F 4 F RT A21EA E15NE 1998111300784 19981113 00784 EA 1998 11 13 COMA9860340 1 19981106 A 2121 AEO8L4AA1 FAN CNDAIR CL600 CL6002B19 EA AVIONICS OVERHEATED A COMA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 982CA 7168 STRONG ELECTRICAL BURNING SMELL IN COCKPIT. REPLACED THE DISPLAY COOLING FANS. 2 L 7 2 4F RT A21EA 1998111300785 19981113 00785 EA 1998 11 13 COMA9860342 1 19981105 A 2121 FAN CNDAIR CL600 CL6002B19 EA CARGO COMPT FAILED A COMA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 977CA 7157 CARGO FAN FAIL MESSAGE. DEFERRED CARGO FAN. 2 L 7 2 4F RT A21EA 1998111300786 19981113 00786 EA 1998 11 13 COMA9860343 1 19981105 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO COMPT FAILED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 951CA 4524 7091 CARGO SMOKE WARNING. REPLACED SMOKE DETECTOR. 2 L 7 2 4F RT A21EA 1998111300787 19981113 00787 EA 1998 11 13 COMA9860344 1 19981105 A 5330 601R310211 SKIN CNDAIR CL600 CL6002B19 EA PAX DOORWAY DAMAGED A COMA K NONE O OTHER UK UNKNOWN 1 SO 01 967CA 7151 WHEN CREW PICKED UP AIRCRAFT AT THE GATE THEY NOTICED DAMAGE TO THE FUSELAGE CAUSED BY THE PASSENGER DOOR LATCHING PINS. REPAIRED AIRCRAFT IAW CANADAIR REO 601R-52-11-008 REPAIR A AND REO 601R 53-21-186. 2 L 7 2 4F RT A21EA 1998111300788 19981113 00788 EA 1998 11 13 COMA9860345 1 19981024 A 2750 601R93106503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP DAMAGED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 7168 DURING C-CHECK, FOUND NR 5 TE FLAP FLEXSHAFT BAD (RIGHT WING) THREADS ON ONE OF THE B-NUTS WERE STRIPPED. REPLACED FLEX SHAFT. 2 L 7 2 4F RT A21EA 1998111300789 19981113 00789 EA 1998 11 13 COMA9860346 1 19981024 A 2750 601R93106207 FLEXSHAFT CNDAIR CL600 CL6002B19 EA LT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 982CA 7168 LEFT SIDE TE FLAP NR 2 FLEXSHAFT FOUND UNSERVICEABLE DUE TO CORROSION. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998111300790 19981113 00790 WP 1998 11 13 UPS98828103 1 19981015 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 660 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FWD END OF LONGERON 36 AT FS 660 HAS PITTING CORROSION. REPAIRED IAW DHC SK-779-169. 2 L 7 4 4F RT 4A25 1998111300791 19981113 00791 WP 1998 11 13 UPS98828104 1 19981018 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FRAME CORRODED OUT OF LIMITS FS 1280 AT LONGERON 35R-36. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998111300792 19981113 00792 WP 1998 11 13 UPS98828105 1 19981031 A 5313 5750198502 LONGERON DOUG DC8 DC873F 302199F WP BS 879-980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-SP, TRANSFERED FROM LOG PAGE 709350 ITEM 1, CORROSION AT MATING FLANGE OF 3 ATTACH FITTINGS ON LONGERON 24 IN RT W/W AT STA 879, 902, AND 920. REMOVED AND REPLACED LONGERON 24 RT IAW DWG 5750198 AND SRM 51-1-20D AND SRM 51- 3-1. 2 L 7 4 4F RT 4A25 1998111300793 19981113 00793 WP 1998 11 13 UPS98828106 1 19981031 A 5320 36410042N FITTING DOUG DC8 DC873F 302199F WP BS 879.35 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 801UP 46101 INSPECTION TYPE-SP, FITTING AT FS 879.35 FOUND TO HAVE HEAVY CORROSION AROUND BOLT HOLES AND FLANGES BETWEEN LONGERON 24 AND CUSP RT W/W. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998111300794 19981113 00794 WP 1998 11 13 UPS98828107 1 19981021 A 5712 37048411 BULKHEAD FITTING DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, NR 3 MAIN TANK AT THE XRS 74 BULKHEAD STRINGER 51 AFT ATTACH FITTING IS CRACKED. REMOVED AND REPLACE D FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998111300795 19981113 00795 WP 1998 11 13 UPS98828108 1 19981103 A 5720 97532977 ANGLE DOUG DC8 DC871F 302199D WP NR 1 STUB WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, VERTICAL ATTACHMENT ANGLE ON THE I/B SIDE OF THE NR 1 STUB WING CRACKED IN RADIUS. REMOVED, FABRICAT ED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 9753297. 2 L 7 4 4F RT 4A25 1998111300796 19981113 00796 WP 1998 11 13 UPS98828109 1 19981019 A 5320 3779658501N FITTING DOUG DC8 DC871F 302199D WP BS 859 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LONGERON 10L END FITTING CRACKED FS 859. REMOVED AND REPLACED FITTING IAW SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998111300797 19981113 00797 WP 1998 11 13 UPS98828110 1 19981020 A 5320 37502711 SPLICE DOUG DC8 DC871F 302199D WP BS 640-660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FS 640 TO 660 STRINGER 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998111300798 19981113 00798 WP 1998 11 13 UPS98828111 1 19981019 A 5320 37797621 FITTING DOUG DC8 DC871F 302199D WP BS 680 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, LONGERON 9L END FITTING CRACKED FS 680. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SR M 51-1-21 AND DWG 3779762. 2 L 7 4 4F RT 4A25 1998111300799 19981113 00799 WP 1998 11 13 UPS98828112 1 19981101 A 5320 5751040 JAMB DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, DOOR JAMB AFT ENTRY DOOR AFT LOWER CORNER HAS 2 INCH CRACK. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998111300800 19981113 00800 WP 1998 11 13 UPS98828113 1 19981020 A 5320 36169452 FITTING DOUG DC8 DC871F 302199D WP BS 822 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, CRACKED FRAME CUSP FITTING AT FS 822 LT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW S RM 51-1-21 AND DWG 3616945. 2 L 7 4 4F RT 4A25 1998111300801 19981113 00801 WP 1998 11 13 UPS98828114 1 19981023 A 5320 37558242 FITTING DOUG DC8 DC871F 302199D WP BS 280 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FITTING AT FS 280 L-34R CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998111300802 19981113 00802 WP 1998 11 13 UPS98828115 1 19981020 A 5320 47504222N INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 857 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, CRACKED INTERCOSTAL FITTING AT LONGERON 19L FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998111300803 19981113 00803 WP 1998 11 13 UPS98828116 1 19981017 A 5320 4642581 FITTING DOUG DC8 DC871F 302199D WP BS 1392 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FS 1392 L-30R FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998111300804 19981113 00804 WP 1998 11 13 UPS98828117 1 19981026 A 5320 37558411 FITTING DOUG DC8 DC871F 302199D WP BS 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, BATHTUB FITTING IS CRACKED AT STA 1150 L-34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998111300805 19981113 00805 WP 1998 11 13 UPS98828118 1 19981021 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1746 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FRAME 1746 LOWER FLANGE CRACKED AND CORRODED AT L-35R. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1998111300806 19981113 00806 WP 1998 11 13 UPS98828119 1 19981027 A 5320 577384659 FITTING DOUG DC8 DC871F 302199D WP BS 1752 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, FITTING CORRODED FS 1752 BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1-21D. 2 L 7 4 4F RT 4A25 1998111300807 19981113 00807 WP 1998 11 13 UPS98828120 1 19981022 A 5312 RIB DOUG DC8 DC871F 302199D WP WS 385 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-D, CRACKED RIB AT XFS 385.25 LWR RIB LT L/E. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998111300808 19981113 00808 NM 1998 11 13 QXEA9801547 1 19981101 A 3222 881517 STRUT MESSIER 8800121 DHAV DHC8 DHC8102 2809003 NM NLG CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 829PH 27965 17384 DCL07486 304 PDX- DURING THE ACCOMPLISHMENT OF A SCHEDULED A CHECK, THE NOSE LANDING GEAR OUTER CYLINDER WAS FOUND CRACKED. THE CRAC K WAS ON THE AFT SIDE OF THE OUTER CYLINDER BEGINING AT THE TOP AND EXTENDING 5.5 INCHES VERTICALLY DOWN THE CYLINDER. R EPLACED THE NOSE GEAR ASSEMBLY. AIRCRAFT RETURNED TO SERVICE. REMOVED UNIT SENT TO ACCESSORY SHOP WHERE IT WAS CLEANED , AND THEN TORN DOWN. LOCAL FAA FSDO (NM09) WITNESSED THE TEARDOWN. NO ABNORMAL CONDITIONS WERE NOTED DURING TEARDOWN. OUTER CYLINDER FROM THE NOSE GEAR ASSEMBLY SENT TO AIRCRAFT MANUFACTURER (BOMBARDIER) IN TORONTO FOR FURTHER ANALYSIS. AWAITING RESULTS OF ANALYSIS AND TESTING. LANDING GEAR WAS SCRAPPED AND REMOVED FROM INVENTORY. 2 H 7 2 4T RT A13NM 1998111300809 19981113 00809 NM 1998 11 13 QXEA9801548 1 19981101 A 3350 P4010021 BATTERY DHAV P2070001201S DHAV DHC8 DHC8102 2809003 NM COCKPIT DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 821PH 104 COCKPIT EMERGENCY FLASHLIGHT IS NOT BLINKING. REPLACED BATTERY IN FLASHLIGHT, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998111300810 19981113 00810 EU 1998 11 13 QXEA01549 1 19981008 A 5753 TRACK FOKKER F28 F28MK4000 4990810 EU TE FLAP CANOE GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 FLAP CANOE PANEL 82DF VERTICAL GUIDE TRACK IS GROOVED. REPAIRED IAW FOKKER MM 27-50-6, B 2-3 AND HORIZON AIR EA 4-57-18 0. 2 L 7 2 4F RT A20EU 1998111300811 19981113 00811 EU 1998 11 13 QXEA01550 1 19981007 A 5753 TRACK FOKKER F28 F28MK4000 4990810 EU TE FLAP CANOE GROOVED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 FLAP CANOE PANEL 82CH VERTICAL GUIDE TRACK HAS A GROOVE WORN INTO TRACK. REPAIRED IAW FOKKER MM 27-50-06, PAGE 802, PAR AGRAPH B 2-3 AND HORIZON AIR EA 4-57-180. 2 L 7 2 4F RT A20EU 1998111300812 19981113 00812 EU 1998 11 13 QXEA01551 1 19981013 A 5540 STRINGER FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 STRINGER IS CRACKED AT THE NR 5 RIB INTERSECTION IN THE RUDDER. REPAIRED IAW FOKKER SRM 55-02-07, PAGE 5. 2 L 7 2 4F RT A20EU 1998111300813 19981113 00813 EU 1998 11 13 QXEA01552 1 19981016 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 HI-LOK LOOSE/SMOKING IN LEFT-HAND VERTICAL STAB CONNECTION ANGLE LOCATED 17 BACK FROM FORWARD END. REPAIRED IAW FOKKER SRM 51-31-02. 2 L 7 2 4F RT A20EU 1998111300814 19981113 00814 EU 1998 11 13 QXEA01553 1 19981017 A 5530 ANGLE FOKKER F28 F28MK4000 4990810 EU VERT STAB LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 HI-LOK LOOSE IN LEFT-HAND V STAB CONNECTION ANGLE 31 FORWARD OF AFT END OF CONNECTION ANGLE. REPAIRED IAW FOKKER SRM 51 -31-02. 2 L 7 2 4F RT A20EU 1998111300815 19981113 00815 EU 1998 11 13 QXEA01554 1 19981013 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 INSIDE THE RUDDER THE NR 5 RIB HAS 2 CRACKS PASSING THROUGH ATTACH CLIPS. REPAIRED IAW FOKKER SRM 51-31-05 AND SRM 51-3 1-01. 2 L 7 2 4F RT A20EU 1998111300816 19981113 00816 EU 1998 11 13 QXEA01555 1 19981015 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 FUSELAGE FRAME 17565 HAS A CRACK IN THE FRAME CLIP ADJACENT TO STRINGER 52. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 5 AND SRM 51-11-4 PAGE 2, PARAGRAPH E. 2 L 7 2 4F RT A20EU 1998111300817 19981113 00817 EU 1998 11 13 QXEA01556 1 19981016 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 FRAME 50-2 IS CRACKED TO UNKNOWN LENGTH BEHIND THE DIAGONAL BRACE MOUNT BRACKET AT STRINGER 56. REPAIRED IAW FOKKER SRM 51-10-9, PAGE 9, PARAGRAPH 4 AND SRM 53-26-04, PAGE 20, FIGURE 8, ITEM 235. 2 L 7 2 4F RT A20EU 1998111300818 19981113 00818 EU 1998 11 13 QXEA01557 1 19981015 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 OBLIQUE FRAME 50-2 HAS A CRACK THROUGH A CLIP THAT HAS PROGRESSED THROUGH THE STOP DRILL, NOT YET BEYOND STOP DRILL LIMI TS, LOCATED AT STRINGER 50. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998111300819 19981113 00819 EU 1998 11 13 QXEA01558 1 19981016 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 OBLIQUE FRAME 41-2 HAS A FRAME CLIP CRACKED BEYOND THE STOP DRILL REPAIR. REPAIRED IAW 53-02-13, PAGE 4, FIGURE 3 AND S RM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998111300820 19981113 00820 EU 1998 11 13 QXEA01559 1 19981016 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 OBLIQUE FRAME 50-2 HAS A CRACKED CLIP AT STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-10-05, PAGE 601. 2 L 7 2 4F RT A20EU 1998111300821 19981113 00821 EU 1998 11 13 QXEA01560 1 19981015 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 OBLIQUE FRAME 50-2 AT STRINGER 47 HAS CLIP CRACKED THROUGH A STOP DRILL HOLE. REPAIRED IAW FOKKER MM 53-10-05, PAGE 601 A. 2 L 7 2 4F RT A20EU 1998111300822 19981113 00822 EU 1998 11 13 QXEA01561 1 19981017 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 22293 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 VERTICAL FRAME 22293 HAS A 1 INCH CRACK AT STRINGER 53A. REPAIRED IAW HORIZON AIR EA 4-53-572. 2 L 7 2 4F RT A20EU 1998111300823 19981113 00823 EU 1998 11 13 QXEA01562 1 19981015 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 OBLIQUE FRAME 50-2 HAS A CLIP AT STRINGER 25 THAT IS CRACKED BEYOND LIMITS. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 3 AN D SRM 51-31-01 AND 51-31-02. 2 L 7 2 4F RT A20EU 1998111300824 19981113 00824 EU 1998 11 13 QXEA01563 1 19981030 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 MAIN CABIN DOOR FRICTION MECHANISM IS OUT OF ADJUSTMENT. REPAIRED IAW FOKKER MM 52-10-03, PAGE 583, PARAGRAPH C THROUGH F. 2 L 7 2 4F RT A20EU 1998111300825 19981113 00825 EU 1998 11 13 QXEA01564 1 19981030 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 MAIN CABIN DOOR WILL NOT OPEN FROM OUTSIDE. LOCK ROLLER DOES NOT PULL OUT OF DETENTE COMPLETELY. REPAIRED IAW FOKKER M M 52-10-4, PAGE 417, PARAGRAPH B, STEP 11 AND 12. 2 L 7 2 4F RT A20EU 1998111300826 19981113 00826 EU 1998 11 13 QXEA01565 1 19981029 A 5220 GLASS FOKKER F28 F28MK4000 4990810 EU EMERGENCY EXIT LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 GLASS COMING OUT OF EMERGENCY PUSH BUTTON, EXTERIOR ON SERVICE EMERGENCY DOOR. REPLACED BREAK GLASS PUSH BUTTON COVER F OR EXTERIOR SERVICE EMERGENCY DOOR. 2 L 7 2 4F RT A20EU 1998111300827 19981113 00827 EU 1998 11 13 QXEA01566 1 19981025 A 5220 MECHANISM FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 SERVICE EMERGENCY DOOR TOP MICROSWITCH ACTUATING ARM DOES NOT LINE UP WITH STRIKER PLATE ON DOOR. REALIGNED BRACKET AND ADJUSTED SWITCH. 2 L 7 2 4F RT A20EU 1998111300828 19981113 00828 EU 1998 11 13 QXEA01567 1 19981025 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 FRAME CLIP IS CRACKED AT FRAME 5305 AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1998111300829 19981113 00829 EU 1998 11 13 QXEA01568 1 19981025 A 5210 BRACKET FOKKER F28 F28MK4000 4990810 EU PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 MAIN CABIN DOOR AFT HOOK LATCH FORWARD SUPPORT BRACKET CRACKED AT TOP. REPAIRED IAW FOKKER MM 52-10-4, PAGE 501-502, PA RAGRAPH 2 A AND B. 2 L 7 2 4F RT A20EU 1998111300830 19981113 00830 EU 1998 11 13 QXEA01569 1 19981016 A 5210 COVER FOKKER F28 F28MK4000 4990810 EU PAX DOOR SNAGGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 THE FORWARD AND AFT SOUND PROOFING COVERS BECAME SNAGGED IN DOOR APERTURE DURING OPENING OF MAIN CABIN DOOR. REPAIRED C OMBING. 2 L 7 2 4F RT A20EU 1998111300831 19981113 00831 EU 1998 11 13 QXEA01570 1 19981013 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 THERE IS A CRACKED CASTELLATION AT FRAME 9305 AND STRINGER 28. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1998111300832 19981113 00832 EU 1998 11 13 QXEA01571 1 19981015 A 5210 HANDRAIL FOKKER F28 F28MK4000 4990810 EU PAX DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 FORWARD EXTENDING ROD FOR PASSENGER DOOR HANDRAILS HAS CHAFE DAMAGE. REPAIRED IAW HORIZON AIR EA 4-52-162 FOR STEPS 1 A ND 2 AND FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1998111300833 19981113 00833 EU 1998 11 13 QXEA01572 1 19981014 A 5210 BRACKET FOKKER F28 F28MK4000 4990810 EU PAX DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 MAIN CABIN DOOR HANDRAIL FORWARD INBOARD VERTICAL STANTION HAS CRACK IN BRACKET FOR QUICK RELEASE ROD. REPAIRED IAW FOK KER MM 52-10-01, PAGE 911, PARAGRAPH 4-C. 2 L 7 2 4F RT A20EU 1998111300834 19981113 00834 EU 1998 11 13 QXEA01573 1 19981013 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 16660 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 SMALL CRACK IN FRAME CLIP AT FRAME 16660 AND STRINGER 32. ALODINE AND PRIME IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1998111300835 19981113 00835 EU 1998 11 13 QXEA01574 1 19981015 A 5210 CABLE FOKKER F28 F28MK4000 4990810 EU PAX DOOR RUSTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 EXTERIOR MAIN CABIN DOOR RELEASE HANDLE CABLE APPEARS VERY DRY AND RUSTY WHERE IT ATTACHES TO HANDLE. REPAIRED IAW FOKK ER MM 20-30-09, PAGE 9. 2 L 7 2 4F RT A20EU 1998111300836 19981113 00836 EU 1998 11 13 QXEA01575 1 19981021 A 5210 HANDLE FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 MAIN CABIN DOOR EXTERIOR EMERGENCY RELEASE HANDLE DOES NOT LOCK IN EMERGENCY POSITION. REPAIRED IAW FOKKER SRM 52-10-05 , PAGE 402, PARAGRAPH B, 1 - 12. 2 L 7 2 4F RT A20EU 1998111300837 19981113 00837 EU 1998 11 13 QXEA01576 1 19981016 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 MAIN CABIN DOOR LATCHING SYSTEM STIFF. REPAIRED IAW FOKKER MM 52-10-01. 2 L 7 2 4F RT A20EU 1998111300838 19981113 00838 EU 1998 11 13 QXEA01577 1 19981005 A 5210 HANDLE FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 MAIN CABIN DOOR EMERGENCY RELEASE HANDLE OUTSIDE FUSELAGE HAD CORROSION AND RED PAINT IS WORN OFF. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 AND SRM 51-10-4 PAGE 8, PARAGRAPH 3 (1). 2 L 7 2 4F RT A20EU 1998111300839 19981113 00839 NM 1998 11 13 98FDEA00685 1 19981104 A 3232 731443 ACTUATOR BOEING 727 727227 1384078 NM RT MLG DOOR INOP A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 496FE 21670 ON DEPARTURE, GEAR RAISED NORMALLY IND LEVER TURN OFF, RED DOOR LIGHT ON FWD PNL AND RT GEAR DOOR, LT ON S/O'S PNL ILLUM . RAISED GEAR HANDLE TO UP AND RED DOOR LT. USING MANUAL LEVER-OPER RT GEAR DOOR NUMEROUS TIMES. DOOR LOCKED OK, NO H YD LEAK NOTE IND. REPLACED RT GEAR DOOR ACTUATOR PER MM 32-32-8, OPS AND LEAK CK OK. 2 L 7 3 4F A3WE 1998111300840 19981113 00840 NM 1998 11 13 98FDEA00686 1 19981105 A 3260 SENSOR BOEING 727 727225 1384077 NM RT MLG MALFUNCTIONED A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 463FE 22551 RT MAIN GEAR UNSAFE LIGHT DURING T/O. RETRACT GEAR AND GOT GOOD UP IND. LOWERED GEAR AND GOT RT MAIN UNSAFE. CK RT MA IN FOR GOOD DOWN IND WITH GEAR CRANK AND IT CK GOOD. FIVE MIN AFTER LANDING GOT UNSAFE RT MAIN IND AGAIN WHILE IN CHOCK S, IN ALL CASES WHEN RED UNSAFE LIGHT CAME. REMOVED AND REPLACED LANDING GEAR ASSY PER MM 32-09-121 AND RMG DOWNLOCK SE NSOR PER M/M 32-61-91. ALL CKS WERE NORM. 2 L 7 3 4F A3WE 1998111300841 19981113 00841 NM 1998 11 13 98FDEA00687 1 19981106 A 3010 DUCT BOEING 727 727225 1384077 NM FUSELAGE SEPARATED A FDEA H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CL CLIMB 1 SO 25 465FE 21289 ON DEPARTURE, THE LWR AFT BODY OVERHEAT LIGHT ILLUM. WHEN WING ANTI-ICE WAS TURNED OFF THE LIGHT WENT OUT. FOUND SURFA CE THERMAL ANTI-ICE CROSSOVER DUCT SEPARATED IN LT OVERHEAD STAIRWELL AREA. REASSEMBLED DUCT WORK, CK SATISFACTORY. 2 L 7 3 4F A3WE 1998111300842 19981113 00842 NM 1998 11 13 98FDEA00688 1 19981103 A 5311 651631220 FRAME BOEING 727 72725 1384006 NM BS 294.5 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 CORROSION (C53-224-03-1/2) ON FRAME BS 294.5, RBL 27, WL 173. *S/D* REMOVED AND REPLACED SPLICE PLATE AT BS 294.5, RBL 27, WL 173 PER FEDEX DRAWING NR 65-16312. 2 L 7 3 4F A3WE 1998111300843 19981113 00843 WP 1998 11 13 98FDEA00689 1 19981106 A 3260 SENSOR DOUG DC10 DC1010F 3022111 WP LT MLG DOOR OUT OF ADJUST A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 057FE 48264 LT MAIN GEAR IND UNSAFE UP BOTH PNLS, RED TABS COMPLETED, RETURN TO MEM. THREE GEAR PINS INSTALLED. ADJ TARGET LT MLG DOOR LATCH SENSOR PER MM 32-61-03, CYCLED GEAR NUMEROUS TIMES AND PERFORMED SUCCESSFUL EXTEND/RETRACT CK PER MM 32-10-00 . NO DEFECT NOTED, ALL GEAR IN LIGHT NORM. 2 L 7 3 4F A22WE 1998111300844 19981113 00844 NM 1998 11 13 98FDEA00690 1 19981106 A 5320 651891549 STIFFENER BOEING 727 72725 1384006 NM BS 311 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 BS 311, WL 178, LBL 36 BULGING AROUND FASTENERS ON FLOOR WEB. *S/D* REMOVED STIFFENER AT BS 312, LBL 15 TO LBL 45, WL 178 IAW DRAWING 65-18915. 2 L 7 3 4F A3WE 1998111300845 19981113 00845 WP 1998 11 13 ABXA9800963 1 19981106 A 3350 5700955503 BATTERY DOUG DC8 DC863F 302198F WP CABIN DISCHARGED A ABXA K NONE L NO TEST LD LANDING 1 GL 23 816AX 46093 EMERGENCY LIGHTS WOULD NOT DISARM. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC8 MM, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998111300846 19981113 00846 WP 1998 11 13 MWEA981031 1 19981030 A 5230 59101419 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FOUND CRACK ON FORWARD CARGO DOOR PAN FORWARD EDGE JUST BELOW FORWARD TORQUE TABLE. MTC FABRICATED AND INSTALLED DOUBLE R. 2 L 7 2 4F A6WE 1998111300847 19981113 00847 WP 1998 11 13 DHL9880401C 1 19980907 A 5350 FAIRING DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, R/W FAIRING PANEL EDGE IS DELAMINATED NR 262K. CLEANED AND REPAIRED PER SRM 51-1-19. N/R 730 2 L 7 4 4F RT 4A25 1998111300848 19981113 00848 WP 1998 11 13 DHL9880402C 1 19980904 A 5414 SKIN DOUG DC8 DC873F 302199F WP NR 4 PYLON CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, I/B SIDE FROM PYLON NR 4 STUB WING LEADING EDGE HAS 2 INCH CRACK PROGRESSING FROM PREVIOUS REPAIR. REMOVED , REPAIRED, FABRICATED NEW DOUBLER PER SRM 51-1-4. N/R 530 2 L 7 4 4F RT 4A25 1998111300849 19981113 00849 WP 1998 11 13 DHL9880403C 1 19980901 A 5730 PANEL DOUG DC8 DC873F 302199F WP CENTER WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT CHECK, LOWER FUSELAGE CENTER WING SECTION NR 161L PANEL 10 PERCENT DELAMINATED. REPAIRED PER SRM 51-1-21 AND REINST ALLED. N/R 0071 2 L 7 4 4F RT 4A25 1998111300850 19981113 00850 WP 1998 11 13 DHL9880404C 1 19980901 A 3230 BRACKET DOUG DC8 DC873F 302199F WP LT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LT MAIN LANDING GEAR WHEEL WELL FWD BULKHEAD PULLEY BRACKET CRACKED. REMOVED CRACKED BRACKET, FABRICATED NE W BRACKET PER SRM 51-1-4, 6 X 5. N/R 0087 2 L 7 4 4F RT 4A25 1998111300851 19981113 00851 WP 1998 11 13 DHL9880405C 1 19980903 A 5320 FRAME DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, FOUND CRACK LOCATED AT FRAME AFT SIDE LOWER POST MAIN CARGO DOOR AREA. STOP DRILLED CRACK, FABRICATED AND I NSTALLED DOUBLER PER SRM 53-2-0, 10 X 2. N/R 146 2 L 7 4 4F RT 4A25 1998111300852 19981113 00852 WP 1998 11 13 DHL9880406C 1 19980903 A 5320 SCUFF PLATE DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, MAIN CARGO DOOR SCUFF PLATE IS CRACKED AT I/B AFT CORNER. REMOVED SCUFF PLATE REPAIRED AND REINSTALLED PER SRM 51-3-0. N/R 241 2 L 7 4 4F RT 4A25 1998111300853 19981113 00853 WP 1998 11 13 DHL9880407C 1 19980902 A 5350 FAIRING DOUG DC8 DC873F 302199F WP LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING FAIRING PANEL NR 161V HAS DELAMINATION. REPAIRED DAMAGED PANEL AND REINSTALLED PER SRM 51-18 AND 51-1-21. N/R 250 2 L 7 4 4F RT 4A25 1998111300854 19981113 00854 WP 1998 11 13 DHL9880408C 1 19981003 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 347 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT WING LOWER SURFACE STA 347 HAS A CRACK. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FILLER PER DRAWING 18R5761025, 13 X 8. N/R 401 2 L 7 4 4F RT 4A25 1998111300855 19981113 00855 WP 1998 11 13 DHL9880409C 1 19980909 A 5350 FAIRING DOUG DC8 DC873F 302199F WP BS 680 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RIGHT WING, WING TO BODY FAIRING AT BS 680 SUPPORT STRUCTURE HAS METAL LINES CRACKED. REMOVED SUPPORT AND F ABRICATED AND INSTALLED PER MM 51-1-8. N/R 403 2 L 7 4 4F RT 4A25 1998111300856 19981113 00856 WP 1998 11 13 DHL9880410C 1 19980904 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 4 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, ENGINE NR 4 STRUCTURE FIXED LT SIDE PRIMARY COWL UPPER COWL UPPER AFT END CORNER IS CRACKED. REMOVED AND RE PLACED CHANNEL PER SRM 51-1-21, 5 X 1.5. N/R 505 2 L 7 4 4F RT 4A25 1998111300857 19981113 00857 WP 1998 11 13 DHL9880411C 1 19980912 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, NR 2 STRUCTURE FIXED LEFT SIDE COWL PRIMARY COWL UPPER AFT END CORNER CRACKED. REMOVED CRACKED CHANNEL AND FABRICATED AND INSTALLED NEW CHANNEL PER SRM 51-1-4, 5 X 1.5. N/R 506 2 L 7 4 4F RT 4A25 1998111300858 19981113 00858 WP 1998 11 13 DHL9880412C 1 19980906 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, NR 2 ENGINE LT DIFFUSER AREA AT 2 O'CLOCK POS COVER HOUSING IS CRACKED. INSTALLED NEW COVER PER SRM 51-3-0. N/R 579 2 L 7 4 4F RT 4A25 1998111300859 19981113 00859 WP 1998 11 13 DHL9880413C 1 19980906 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 2 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, NR 2 ENGINE RT FAN CASE LOWER AREA AT 6 O'CLOCK POS RT SIDE CERTICAL COVER CRACKED. REMOVED COVER, REPAIRE D AND REINSTALLED PER SRM 51-3-0. N/R 580 2 L 7 4 4F RT 4A25 1998111300860 19981113 00860 WP 1998 11 13 DHL9880414C 1 19980905 A 5523 SKIN DOUG DC8 DC873F 302199F WP LT ELEVATOR TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT ELEVATOR CONTROL TAB UPPER SURFACE I/B DELAMINATED AND DENTED. REMOVED AND REPLACED PER MM 27-30-3. N /R 607 2 L 7 4 4F RT 4A25 1998111300861 19981113 00861 WP 1998 11 13 DHL9880415C 1 19980905 A 5523 SKIN DOUG DC8 DC873F 302199F WP RT ELEVATOR TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT ELEVATOR CONTROL TAB UPPER AND LOWER L/E AND O/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED PER MM 27-30-0. N/R 608 2 L 7 4 4F RT 4A25 1998111300862 19981113 00862 WP 1998 11 13 DHL9880416C 1 19980906 A 5744 5751183505 FITTING DOUG DC8 DC873F 302199F WP WS 97 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT D-CHECK, LEFT WING I/B FLAP HINGE SUPPORT FITTING AT STA 97. FOUND 2 CRACKS IN FWD AND DRIVE LINK ATTACHING HOLES. REAMED HOLES .0312 OVERSIZE. HFEC, OUT OF LIMITS. REPLACED FITTING PER SRM 51-1-21. N/R 679 2 L 7 4 4F RT 4A25 1998111300863 19981113 00863 WP 1998 11 13 DHL9880417C 1 19980907 A 5350 FAIRING DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RIGHT WING FAIRING PANEL 162K2 DELAMINATED. REMOVED PANEL, REPAIRED AND REINSTALLED PER SRM 51-3-0. N/R 7 20 2 L 7 4 4F RT 4A25 1998111300864 19981113 00864 WP 1998 11 13 DHL9880418C 1 19981004 A 2810 VENT BOX DOUG DC8 DC873F 302199F WP NR 1 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, NR 1 ALT VENT BOX CRACKED. REMOVED AND REPAIRED BOX AND REINSTALLED PER MM 28-10-10. N/R 1073 2 L 7 4 4F RT 4A25 1998111300865 19981113 00865 WP 1998 11 13 DHL9880419C 1 19980928 A 5210 STRUCTURE DOUG DC8 DC873F 302199F WP PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, AFT PASSENGER DOOR FWD CORNER HAS A .625 INCH CRACK INSIDE CORNER. CUT OUT CRACKED AREA, FABRICATED FILLER AND ANGLE REPAIR AND INSTALLED PER DER NR 18R53210228, .5 X 3.5. N/R 1036 2 L 7 4 4F RT 4A25 1998111300866 19981113 00866 WP 1998 11 13 DHL9880420C 1 19980908 A 5230 SKIN DOUG DC8 DC873F 302199F WP C-3 DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, C-3 DOOR COVER SKIN BROKEN. STOP DRILLED AREA, FABRICATED REPAIR AND INSTALLED PER SRM 52-2-0, 4 X4. N/R 8 97 2 L 7 4 4F RT 4A25 1998111300867 19981113 00867 WP 1998 11 13 DHL9880421C 1 19980908 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WW FS 940 LBL 24 HAS A CRACK 4 INCHES LONG MIGRATING BELOW ANGLE. STOP DRILLED CRACK, FABRICATED REPAI R ANGLES PER SRM 53-2-2, ANGLES 6 X 18, 6 X 14. N/R 827 2 L 7 4 4F RT 4A25 1998111300868 19981113 00868 WP 1998 11 13 DHL9880422C 1 19980908 A 5320 FITTING DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT WHEEL WELL LONGERON 24 VERTICAL FITTING IS CRACKED. REMOVED CRACKED FITTING AND INSTALLED FITTING PER SR M 51-1-20D, 51-3-0. N/R 831 2 L 7 4 4F RT 4A25 1998111300869 19981113 00869 WP 1998 11 13 DHL9880423C 1 19980908 A 5320 5894264 FITTING DOUG DC8 DC873F 302199F WP RT MLG WW CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT WHEEL TRAPAZOIDAL FITTING CRACKED. FABRICATED TEMPLATE AND RELOCATED HOLES FROM OLD FITTING. INSTALLED PER S/B 53-61. N/R 832 2 L 7 4 4F RT 4A25 1998111300870 19981113 00870 WP 1998 11 13 DHL9880424C 1 19980908 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 940 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT WHEEL WELL LONGERON 24 VERTICAL FITTING AT STA 940 CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-8. N/R 833 2 L 7 4 4F RT 4A25 1998111300871 19981113 00871 WP 1998 11 13 DHL9880425C 1 19980908 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 22.750 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING UPPER T/E PANEL AT XW 0 TO XRS 22.750 AFT OF REAR SPAR HAS DENTS WITH DELAMINATION. REMOVED AND I NSTALLED NEW PANEL PER SRM 51-3-0. N/R 028 2 L 7 4 4F RT 4A25 1998111300872 19981113 00872 WP 1998 11 13 DHL9880426C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP LT WING DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING UPPER T/E PANEL XW 0-47.0 CENTER PANEL HAS DENTS WITH DELAMINATION. REMOVED AND REPAIRED PANEL A ND REINSTALLED PER SRM 51-1-8. N/R 029 2 L 7 4 4F RT 4A25 1998111300873 19981113 00873 WP 1998 11 13 DHL9880427C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 463-519 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LT WING UPPER T/E XRS 463 TO 519 PANEL HAS INTERM REPAIR. REMOVED, REPAIRED AND REINSTALLED PANEL PER SRM 5 1-1-21. N/R 030 2 L 7 4 4F RT 4A25 1998111300874 19981113 00874 WP 1998 11 13 DHL9880428C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 519 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING UPPER T/E AT XRS 519 INSERT PANEL HAS DELAMINATION. REMOVED, REPAIRED AND REPLACED PANEL PER SRM 51-1-21. N/R 0031 2 L 7 4 4F RT 4A25 1998111300875 19981113 00875 WP 1998 11 13 DHL9880429C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 693 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING LOWER T/E PANEL AT XRS 693 DELAMINATED. REMOVED AND REPAIRED PANEL, REINSTALLED PER SRM 51-1-8. N/R 0032 2 L 7 4 4F RT 4A25 1998111300876 19981113 00876 WP 1998 11 13 DHL9880430C 1 19980923 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 693-763 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING T/E HINGED PANEL STA XRS 693 TO 763 DELAMINATED. REMOVED AND REPAIRED DELAMINATED PANEL, REINSTAL LED PER SRM 51-1-3. N/R 033 2 L 7 4 4F RT 4A25 1998111300877 19981113 00877 WP 1998 11 13 DHL9880431C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 358-421 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LT WING LOWER T/E PANEL STA XRS 421 TO 358 PANEL HAS DELAMINATION. REMOVED, REPAIRED AND REINSTALLED PER SR M 51-1-8. N/R 034 2 L 7 4 4F RT 4A25 1998111300878 19981113 00878 WP 1998 11 13 DHL9880432C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 252 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING LOWER T/E PANEL STA XRS 252 I/B NR 2 ENGINE PYLON FAIRING HAS INTERM REPAIR. REMOVED DELAMINATED PANEL, REPAIRED AND REINSTALLED PER SRM 51-1-21. N/R 0035 2 L 7 4 4F RT 4A25 1998111300879 19981113 00879 WP 1998 11 13 DHL9880433C 1 19980901 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 428 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT WING STA XW 428 LOWER OUTER T/E PANEL DELAMINATED AT FWD I/B CORNER. REMOVED, REPAIRED AND REINSTALLED P ANEL PER SRM 51-1-21. N/R 038 2 L 7 4 4F RT 4A25 1998111300880 19981113 00880 WP 1998 11 13 DHL9880434C 1 19980831 A 5350 RADOME DOUG DC8 DC873F 302199F WP FWD FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RADOME HAS DELAMINATED AREAS PEELING AND SEVERAL NICKS. REMOVED AND REINSTALLED REPAIRED RADOME PER MM 53-5 0-1. N/R 0040 2 L 7 4 4F RT 4A25 1998111300881 19981113 00881 WP 1998 11 13 DHL9880435C 1 19980831 A 5330 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT CHECK, LOWER FUSELAGE CENTER WING SECTION NR 162F PANEL DELAMINATED. REMOVED AND REPLACED PER SRM 51-3-0. N/R 0041 2 L 7 4 4F RT 4A25 1998111300882 19981113 00882 WP 1998 11 13 DHL9880436C 1 19980831 A 5330 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LOWER FUSE AT CENTER WING SECTION ADF SENSE ANTENNA AND PANEL 162S DELAMINATED. REMOVED, REPAIRED AND REI NSTALLED PER SRM 51-1-21. N/R 042 2 L 7 4 4F RT 4A25 1998111300883 19981113 00883 WP 1998 11 13 DHL9880437C 1 19980831 A 5330 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LOWER FUSE CENTER WING SECTION NR 161G PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-3- 0. N/R 043 2 L 7 4 4F RT 4A25 1998111300884 19981113 00884 WP 1998 11 13 DHL9880438C 1 19980831 A 5753 VANE DOUG DC8 DC873F 302199F WP RT TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, I/B FLAP I/B NR 1 VANE I/B LOWER SURFACE DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER MM 27-51-14. N /R 0015 2 L 7 4 4F RT 4A25 1998111300885 19981113 00885 WP 1998 11 13 DHL9880439C 1 19980831 A 5753 VANE DOUG DC8 DC873F 302199F WP TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, O/B FLAP I/B VANE I/B LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM 27-51-14. N/R 0016 2 L 7 4 4F RT 4A25 1998111300886 19981113 00886 WP 1998 11 13 DHL9880440C 1 19980831 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, SPOILER NR 5 LOWER T/E SURFACE O/B END DELAMINATED. REMOVED AND REPLACED SPOILER PER MM 27-61-1. N/R 0017 2 L 7 4 4F RT 4A25 1998111300887 19981113 00887 WP 1998 11 13 DHL9880441C 1 19980831 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 2 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING LOWER NR 2 SPOILER HAS INTERM REPAIR. REMOVED AND REINSTALLED REPAIRED SPOILER PER MM 27-61-1. N /R 018 2 L 7 4 4F RT 4A25 1998111300888 19981113 00888 WP 1998 11 13 DHL9880442C 1 19980831 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, UPPER NR 5 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM 27-60-0. N/R 019 2 L 7 4 4F RT 4A25 1998111300889 19981113 00889 WP 1998 11 13 DHL9880443C 1 19980831 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 4 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, LEFT WING UPPER NR 4 SPOILER HAS DELAMINATION. REMOVED AND REPLACED REPAIRED SPOILER PER MM 27-61-1. N/R 0 20 2 L 7 4 4F RT 4A25 1998111300890 19981113 00890 WP 1998 11 13 DHL9880444C 1 19980831 A 5753 PANEL DOUG DC8 DC873F 302199F WP WS 418 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, STA 418 LOWER T/E PANEL DELAMINATED FWD END. REMOVED PANEL, REPAIRED AND REINSTALLED PER SRM 51-1-8. N/R 0 021 2 L 7 4 4F RT 4A25 1998111300891 19981113 00891 WP 1998 11 13 DHL9880445C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 130 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, STA XW 130 WING LOWER T/E PANEL FWD O/B EDGE IS DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PANEL PER SR M 51-1-21. N/R 022 2 L 7 4 4F RT 4A25 1998111300892 19981113 00892 WP 1998 11 13 DHL9880446C 1 19980831 A 5280 5648932 SKIN DOUG DC8 DC873F 302199F WP RT MLG DOOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT MLG OUTER DOOR I/B LOWER SURFACE IS DELAMINATED. REMOVED, REPAIRED AND REINSTALLED LANDING GEAR DOORS P ER SRM 51-3-0. N/R 023 2 L 7 4 4F RT 4A25 1998111300893 19981113 00893 WP 1998 11 13 DHL9880447C 1 19980831 A 5280 SKN DOUG DC8 DC873F 302199F WP RT MLG DOOR DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, RT MLG MIDDLE DOOR EXTERNAL SURFACE I/B END IS DELAMINATED. REMOVED AND REPLACED PANEL PER SRM 51-3-0. N/ R 024 2 L 7 4 4F RT 4A25 1998111300894 19981113 00894 WP 1998 11 13 DHL9880448C 1 19980831 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, WING I/B LOWER SURFACE FWD OF DRAG BRACE PANEL DELAMINATED. REMOVED DRAG BRACE PANEL, REPAIRED AND REINSTAL LED PER SRM 51-1-21. N/R 025 2 L 7 4 4F RT 4A25 1998111300895 19981113 00895 WP 1998 11 13 DHL9880449C 1 19980831 A 5752 SKIN DOUG DC8 DC873F 302199F WP RT AILERON TAB DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 804DH 46124 AT C-CHECK, I/B AILERON TRIM TAB LOWER SURFACE FWD O/B END DELAMINATED. REMOVED TAB, SENT FOR REPAIR AND REINSTALLED PE R MM 27-13-0. N/R 026 2 L 7 4 4F RT 4A25 1998111300896 19981113 00896 WP 1998 11 13 DHL98805004 1 19981107 A 7931 LINE DOUG DC8 DC873F 302199F WP NR 4 ENGINE CRACKED A DHLA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 805DH 46125 NR 4 ENGINE SHUT DOWN DUE TO LOW OIL QUANTITY AND OIL PRESSURE FLUCTUATIONS. REPLACED CRACKED LINE AT OIL PRESSURE TRAN SMITTER. 2 L 7 4 4F RT 4A25 1998111300897 19981113 00897 WP 1998 11 13 RRXA98522 1 19981106 A 5311 5773257509 FRAME DOUG DC8 DC862 3021970 WP FRAME 1440 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1440 WITH MISDRILLED HOLE AT LONGERON 12 RIGHT. FABRICATED AND INSTALLED REPAIR A NGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R35, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300898 19981113 00898 WP 1998 11 13 RRXA98523 1 19981106 A 5311 5615754515 FRAME DOUG DC8 DC862 3021970 WP FRAME 660 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT FOUND FRAME 660 WITH MISDRILLED HOLE AT LT CUSP. FABRICATED AND INSTALLED REPAIR IAW FAA APPRO VED DER COTNEY ENGINEERING SKETCH E84-R69. 2 L 7 4 4F 4A25 1998111300899 19981113 00899 WP 1998 11 13 RRXA98524 1 19981106 A 5512 5644310508 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND CORROSION ON LOWER SURFACE OF RT HORIZONTAL STABILIZER SKIN PANEL AT STA XE270 TO 310. R EMOVED CORROSION AND FOUND TO BE BEYOND LIMITS. FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENG INEERING SKETCH E84-R89 AND DC-8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998111300900 19981113 00900 WP 1998 11 13 RRXA98525 1 19981106 A 5311 5640232505 FRAME DOUG DC8 DC862 3021970 WP FRAME 1300 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1300 WITH MISDRILLED HOLES AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR STRAPS AND INTERCOSTAL CLIPS IAW FAA APPROVED ACMI SKETCH SK98384, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8 . 2 L 7 4 4F 4A25 1998111300901 19981113 00901 WP 1998 11 13 RRXA98526 1 19981106 A 5311 57533501 FRAME DOUG DC8 DC862 3021970 WP FRAME 1380 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1380 WITH MISDRILLED HOLE AT LONGERON 9 RIGHT. PLUGGED HOLE IN FRAME, FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED ACMI SKETCH SK98392, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300902 19981113 00902 WP 1998 11 13 RRXA98527 1 19981106 A 5311 5640230453 FRAME DOUG DC8 DC862 3021970 WP FRAME 1260 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1260 WITH MISDRILLED HOLE AT LONGERON 20 RIGHT. FABRICATED AND INSTALLED REPAIR A NGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R21, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300903 19981113 00903 WP 1998 11 13 RRXA98528 1 19981106 A 5311 5640221517 FRAME DOUG DC8 DC862 3021970 WP FRAME 1080 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1080 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALL ED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R97. HEAT TREATED ANGLE IAW DC-8 SRM 51-1-1 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300904 19981113 00904 WP 1998 11 13 RRXA98529 1 19981106 A 5311 5614160 FRAME DOUG DC8 DC862 3021970 WP FRAME 255 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 255 NICKED IN RADIUS BETWEEN LONGERONS 12 AND 13 RIGHT. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98364. HEAT TREATED IAW DC-8 SRM 51-1-1 AND AREA TREATED IAW DC-8 SRM 51-1 -8. 2 L 7 4 4F 4A25 1998111300905 19981113 00905 WP 1998 11 13 RRXA98530 1 19981106 A 5512 5641604328 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE185 OF RT HORIZONTAL STABILIZER. REMOVED PANE L, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R91, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300906 19981113 00906 WP 1998 11 13 RRXA98531 1 19981106 A 5311 5613466505 FRAME DOUG DC8 DC862 3021970 WP FRAME 640 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 640 WITH MISDRILLED HOLE AT LONGERON 12 RIGHT. FABRICATED AND INSTALLED REPAIR AN GLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R40, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51- 1-8. 2 L 7 4 4F 4A25 1998111300907 19981113 00907 WP 1998 11 13 RRXA98532 1 19981106 A 5311 5642500507 FRAME DOUG DC8 DC862 3021970 WP FRAME 700 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 700 WITH MISDRILLED HOLE BETWEEN LONGERONS 11 AND 12 LEFT. FABRICATED AND INSTALL ED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R65, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300908 19981113 00908 WP 1998 11 13 RRXA98533 1 19981106 A 5512 565174763057 SKIN DOUG DC8 DC862 3021970 WP HORIZ STABS CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE167 TO 221 OF LT HORIZONTAL STABILIZER. REMOV ED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R91, DC-8 SRM 51-1- 21 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300909 19981113 00909 WP 1998 11 13 RRXA98534 1 19981106 A 5512 56174763057 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE224 TO 260 OF LT HORIZONTAL STABILIZER. REMOV ED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R90, DC-8 SRM 51-1- 21 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300910 19981113 00910 WP 1998 11 13 RRXA98535 1 19981106 A 5512 565174766052 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE282 TO 291 OF LT HORIZONTAL STABILIZER. REMOV ED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R89, DC-8 SRM 51-1- 21 AND TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300911 19981113 00911 WP 1998 11 13 RRXA98536 1 19981106 A 5311 5755074509 FRAME DOUG DC8 DC862 3021970 WP FRAME 1180E MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1180 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED NEW INTE RCOSTAL CLIP AND REPAIR STRAPS IAW FAA APPROVED ACMI SKETCH SK98379, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1 -8. 2 L 7 4 4F 4A25 1998111300912 19981113 00912 WP 1998 11 13 RRXA98537 1 19981106 A 5311 5754232505 FRAME DOUG DC8 DC862 3021970 WP FRAME 1060 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1060 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALL ED REPAIR ANGLE, STRAPS AND SHIMS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R98, DC-8 SRM 51-1-21 AND AREA TREA TED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300913 19981113 00913 WP 1998 11 13 RRXA98538 1 19981106 A 5311 57533501 FRAME DOUG DC8 DC862 3021970 WP FRAME 1380 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1380 WITH MISDRILLED HOLE BETWEEN LONGERONS 11 AND 12 RIGHT. FABRICATED AND INSTA LLED REPAIR ANGLE, STRAPS AND FILLERS IAW FAA APPROVED ACMI SKETCH SK 98393, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300914 19981113 00914 WP 1998 11 13 RRXA98539 1 19981106 A 5311 5640235507 FRAME DOUG DC8 DC862 3021970 WP FRAME 1360 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1360 WITH MISDRILLED HOLES AT LONGERON 9 RIGHT. REMOVED GUSSET, REMOVED DAMAGED A REA, FABRICATED AND INSTALLED NEW SPLICE, STRAPS AND GUSSET IAW FAA APPROVED ACMI SKETCH SK98390, DC-8 SRM 51-1-21 AND A REA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300915 19981113 00915 WP 1998 11 13 RRXA98540 1 19981106 A 5311 5640233505 FRAME DOUG DC8 DC862 3021970 WP FRAME 1320 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 9 AND 10 LEFT. FABRICATED AND INSTALL ED REPAIR ANGLE AND SHIM IAW FAA APPROVED ACMI SKETCH SK98482, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300916 19981113 00916 WP 1998 11 13 RRXA98541 1 19981106 A 5311 5640223511 FRAME DOUG DC8 DC862 3021970 WP FRAME 1120 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 1120 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR A NGLE AND FILLER IAW FAA APPROVED ACMI SKETCH SK98376, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300917 19981113 00917 WP 1998 11 13 RRXA98542 1 19981106 A 5311 5615751517 FRAME DOUG DC8 DC862 3021970 WP FRAME 540 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 540 WITH DRILL DAMAGE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98484, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300918 19981113 00918 WP 1998 11 13 RRXA98543 1 19981106 A 5311 5615752515 FRAME DOUG DC8 DC862 3021970 WP FRAME 600 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 600 WITH MISDRILLED HOLE AT LT CUSP. REMOVED DAMAGED AREA, FABRICATED AND INSTALL ED REPAIR ANGLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R69, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300919 19981113 00919 WP 1998 11 13 RRXA98544 1 19981106 A 5311 5640720503 FRAME DOUG DC8 DC862 3021970 WP FRAME 880 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 880 WITH MISDRILLED HOLE AT LONGERON 3 LEFT. FABRICATED AND INSTALLED REPAIR ANGL E IAW FAA APPROVED ACMI SKETCH SK98300, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300920 19981113 00920 WP 1998 11 13 RRXA98545 1 19981106 A 5311 5751961505 FRAME DOUG DC8 DC862 3021970 WP FRAME 920 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 920 WITH MISDRILLED HOLE AT LONGERON 11 LEFT. PLUGGED HOLE, FABRICATED AND INSTAL LED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98302, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300921 19981113 00921 WP 1998 11 13 RRXA98546 1 19981106 A 5311 5640720503 FRAME DOUG DC8 DC862 3021970 WP FRAME 880 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 880 WITH MISDRILLED HOLE AT LONGERON 6 LEFT. FABRICATED AND INSTALLED REPAIR ANGL E IAW FAA APPROVED ACMI SKETCH SK98301, DC-8 SRM 51-1-1, 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300922 19981113 00922 WP 1998 11 13 RRXA98547 1 19981106 A 5311 5754002501 FRAME DOUG DC8 DC862 3021970 WP FRAME 560 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 560 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R93, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC -8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300923 19981113 00923 WP 1998 11 13 RRXA98548 1 19981106 A 5320 SCUFF PLATE DOUG DC8 DC862 3021970 WP CARGO DOORWAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND C-PIT DOOR THRESHOLD SCUFF PLATE BULGING AND SEVERAL PULLED FASTENERS. REMOVED DAMAGED SKIN AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R15, DC -8 SRM 51-1-20D, 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300924 19981113 00924 WP 1998 11 13 RRXA98549 1 19981106 A 5311 5640721503 FRAME DOUG DC8 DC862 3021970 WP FRAME 960 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND THE FACE OF FRAME 960 GOUGED AND MISDRILLED HOLE AT LONGERON 9 RIGHT. FABRICATED AND IN STALLED REPAIR ANGLE, STRAP AND FILLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R94, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300925 19981113 00925 WP 1998 11 13 RRXA98550 1 19981106 A 5311 5610088513 FRAME DOUG DC8 DC862 3021970 WP FRAME 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 280 WITH MISDRILLED HOLE AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED REPAIR DOU BLER, TIE CLIPS AND SHIMS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R31, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300926 19981113 00926 WP 1998 11 13 RRXA98551 1 19981107 A 5311 5793172501 FRAME DOUG DC8 DC862 3021970 WP FRAME 940 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 940 WITH MISDRILLED HOLE AT LONGERON 14 LEFT. FABRICATED AND INSTALLED REPAIR ANG LE AND STRAPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R109, DC-8 SRM 51-1-1, 51-1-20D AND AREA TREATED IAW DC -8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300927 19981113 00927 WP 1998 11 13 RRXA98552 1 19981107 A 5311 57511121 FRAME DOUG DC8 DC862 3021970 WP FRAME 540 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND 540 WITH MISDRILLED HOLE AT LT CUSP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REP AIR ANGLE, FILLER AND SHIM IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R67 AND DC-8 SRM 51-1-1A. 2 L 7 4 4F 4A25 1998111300928 19981113 00928 WP 1998 11 13 RRXA98553 1 19981107 A 5311 5750129501 FRAME DOUG DC8 DC862 3021970 WP FRAME 759 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 759 WITH MISDRILLED HOLE AT LONGERON 15 LEFT. FABRICATED AND INSTALLED REPAIR STR APS AND CLIPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R87, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED IAW DC-8 SR M 51-1-8. 2 L 7 4 4F 4A25 1998111300929 19981113 00929 WP 1998 11 13 RRXA98554 1 19981107 A 5311 5642859507 FRAME DOUG DC8 DC862 3021970 WP FRAME 822 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 822 WITH MISDRILLED HOLE AT LONGERON 3 LEFT. FABRICATED AND INSTALLED REPAIR ANGL E IAW FAA APPROVED ACMI SKETCH SK98298, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300930 19981113 00930 WP 1998 11 13 RRXA98555 1 19981107 A 5311 5613466505 FRAME DOUG DC8 DC862 3021970 WP FRAME 640 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 640 CRACKED BETWEEN LONGERONS 9 AND 10 RIGHT. FABRICATED AND INSTALLED REPAIR ANG LE AND FILLER IAW FAA APPROVED ACMI SKETCH SK98500, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300931 19981113 00931 WP 1998 11 13 RRXA98556 1 19981107 A 5311 5751961505 FRAME DOUG DC8 DC862 3021970 WP FRAME 920 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FRAME 920 WITH MISDRILLED HOLES AT LONGERON 16 LEFT. PLUGGED HOLES, FABRICATED AND INST ALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98242, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300932 19981113 00932 WP 1998 11 13 RRXA98557 1 19981107 A 5315 2640868 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 660 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING MAINTENANCE VISIT, FOUND FLOOR SUPPORT AT FS 660 WITH MISDRILLED HOLES IN THE UPPER FLANGE. REMOVED DAMAGED AREA , FABRICATED AND INSTALLED NEW T-CAP IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R51, DC-8 SRM 51-1-21 AND TREATE D AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998111300933 19981113 00933 NM 1998 11 13 VNAA9811005 1 19981103 A 6120 C33170232 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PCU LEAKING A VNAA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 GL 07 429JS 3043 OIL WAS NOTED TO BE COMING OUT OF THE RIGHT HAND ENGINE DRAIN, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED T O THE GATE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT O-RING SEALS, IN ACCORDANCE WITH D ORNIER MAINTENANCE MANUAL 61-21-10. LEAK AND OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998111300934 19981113 00934 NE 1998 11 13 TC8A98078 2 19981107 A 7532 PRBC DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 2 ENGINE DIRTY A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 181SK 45910 669217 ON T/O ROLL AT 110 KTS, NR 2 ENGINE COMPRESSOR STALLED, ABORTED TAKEOFF. CHECKED BRAKES PER GOM. CLEANED AND LUBED PRB C VALVE. PERFORMED FLAG CHECK IAW MM 75-30-3. PERFORMED VISUAL INSPECTION OF INTAKE EXHAUST, NO DEFECTS NOTED. 2 L 7 4 4F 4 F 4A25 1E8 1998111300935 19981113 00935 NM 1998 11 13 SWAA982731 1 19981103 A 5330 SKIN BOEING 737 7372H4 138448C NM AIRSTAIR DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND .5 INCH CRACKED FUSELAGE SKIN AT UPPER LEFT CORNER OF AIRSTAIR DOOR SKIN CUTOUT (VERI FIED WITH HFEC). INSTALLED DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300936 19981113 00936 NM 1998 11 13 SWAA982732 1 19981103 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 312, 328 &344 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM STABILIZER STRAP CHAFED FROM AIRSTAIRS AT BS 312, BS 328 AND BS 344, BL 0. REMOVED AND REPLACED FLOORBEAM STAB STRAP PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300937 19981113 00937 NM 1998 11 13 SWAA982733 1 19981103 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND FWD CARGO UPLATCH INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300938 19981113 00938 NM 1998 11 13 SWAA982734 1 19981103 A 5330 SKIN BOEING 737 7373H4 1384600 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 305SW 22945 DURING WALKAROUND CHECK, FOUND APPROX 4 INCHES SKIN CRACKED, LEFT SIDE BETWEEN CABIN WINDOWS 11 AND 12. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998111300939 19981113 00939 NM 1998 11 13 SWAA982735 1 19981103 A 5320 INTERCOSTAL BOEING 737 7375H4 138449D NM CARGO COMPT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 511SW 24188 DURING SCHEDULED BC3 CHECK, FOUND DOOR UPLOCK INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300940 19981113 00940 NM 1998 11 13 SWAA982736 1 19981103 A 5330 SKIN BOEING 737 7373T5 NM FUSELAGE DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 UNITED AIRLINES BAG CART WAS BLOWN INTO SIDE OF A/C DURING STORM IN THE MIDDLE OF THE NIGHT. A V-SHAPED TEAR APPROX 5 I NCHES BY 9 INCHES IN RT SIDE FUSELAGE APPROX 4 INCHES BEHIND AFT CARGO DOOR. REPAIRED DAMAGE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300941 19981113 00941 NM 1998 11 13 SWAA982737 1 19981103 A 5330 SKIN BOEING 737 7373T5 NM BS 887 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN DAMAGED AT BS 887, STR 21R. REPAIRED DAMAGE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300942 19981113 00942 NE 1998 11 13 SWAA982738 2 19981103 A 7200 ENGINE BOEING 737 7373H4 1384600 NM GE CFM56 CFM563B1 13802 NE NR 2 FOD A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK C F.O.D. TO TAKEOFF 1 SW 07 613SW 27931 ON TAKEOFF ROLL, PLASTIC BAG REPORTED INGESTED INTO NR 2 ENG. BEGAN ABORTED T/O AT 30 KTS INTO 20 KT HW. PERFORMED BIR D STRIKE INSPECTION PER BOEING MM. NO DAMAGED NOTED. INSPECTED NR 2 ENGINE FOR FOD, NONE FOUND AND NO DAMAGE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998111300943 19981113 00943 NM 1998 11 13 SWAA982739 1 19981104 A 2780 RETRACT MECH BOEING 737 7372H4 138448C NM NR 4 SLAT MALFUNCTIONED A A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 081SW 22730 AIR TURNBACK DUE TO NR 4 SLAT WOULD NOT RETRACT AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLAC ED NR 4 SLAT ACTUATOR, OPS CK AND LEAK CHECK GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998111300944 19981113 00944 NM 1998 11 13 SWAA982740 1 19981104 A 5240 HINGE BOEING 737 7372H4 138448C NM FUSELAGE BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND BROKEN HINGE ON EXTERNAL POWER RECEPTACLE DOOR. REMOVED AND REPLACED BROKEN HINGE PER B OEING SRM. 2 L 7 2 4F A16WE 1998111300945 19981113 00945 NM 1998 11 13 SWAA982741 1 19981104 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1051 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 1051 BETWEEN STR 20 AND 21 RT. CUT OUT DAMAGED AREA PER BOEING SRM AN D FABRICATED DOUBLER. 2 L 7 2 4F A16WE 1998111300946 19981113 00946 NM 1998 11 13 SWAA982742 1 19981104 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1137-1156 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND BLIND FASTENER IN SKIN DOUBLER AT BS 1137 TO 1156 STR 3L. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998111300947 19981113 00947 NM 1998 11 13 SWAA982743 1 19981104 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1137-1156 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND BLIND FASTENER IN SKIN DOUBLER AT BS 1137 TO 1156 STR 3R. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998111300948 19981113 00948 NM 1998 11 13 SWAA982744 1 19981104 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 771 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND BULGING SKIN AT BS 771, BL 0, WL 149. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300949 19981113 00949 NM 1998 11 13 SWAA982745 1 19981104 A 5320 FASTENER BOEING 737 7372H4 138448C NM FRAME CHORD MISINSTALLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND AT BS 639 RT, FASTENER GOING THROUGH I/B FRAME CHORD NOT INSTALLED AS PER BOEING SRM. R EMOVED AND REPLACED NEW FASTENER IN FRAME CHORD PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300950 19981113 00950 NM 1998 11 13 SWAA982746 1 19981104 A 5312 BULKHEAD STRIP BOEING 737 7372H4 138448C NM BS 1032 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED BULKHEAD SEAL RETAINING STRIP AT BS 1032, LBL 12, WL 209.5. REMOVED ADH REPLAC ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300951 19981113 00951 NM 1998 11 13 SWAA982747 1 19981104 A 5312 BULKHEAD STRIP BOEING 737 7372H4 138448C NM BS 1030 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED BULKHEAD SEAL RETAINING STRIP AT BS 1030, RBL 19, WL 209.5. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300952 19981113 00952 NM 1998 11 13 SWAA982748 1 19981104 A 5754 SKIN BOEING 737 7372H4 138448C NM NR 4 LE SLAT CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND FIXED L/E AT NR 4 SLAT O/B AUX TRACK, CUTOUT HAS A STOP DRILLED CRACK. REMOVED CRACK AR EA, FABRICATED DOUBLER AND FILLER PER SWA TR T1-251-008. 2 L 7 2 4F A16WE 1998111300953 19981113 00953 NM 1998 11 13 SWAA982749 1 19981104 A 5210 SKIN BOEING 737 7373A4 1384585 NM PAX DOOR BENT A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D-CHECK, FOUND FWD ENTRY DOOR SKIN BENT ON AFT EDGE ABOUT 5 INCHES FROM TOP. STRAIGHTEND DOOR SKIN PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300954 19981113 00954 NM 1998 11 13 SWAA982750 1 19981104 A 5320 BRACKET BOEING 737 7373A4 1384585 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D-CHECK, FOUND CORRODED SUPPORT BRACKET FOR ANTENNA BETWEEN BS 727D AND 727E, LBL 2. REMOVED AND RE PLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300955 19981113 00955 NM 1998 11 13 SWAA982751 1 19981104 A 3350 30043213 LIGHT BOEING 737 7372H4 138448C NM SERVICE DOOR INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 074SW 22674 DURING SCHEDULED SERVICED CHECK, FOUND EMERGENCY EXIT LIGHT BEHIND THE RIGHT SERVICE DOOR INOP. COULD NOT RELAMP. REMO VED AND REPLACED LIGHT ASSY PER BOEING MM. 2 L 7 2 4F A16WE 1998111300956 19981113 00956 NM 1998 11 13 SWAA982752 1 19981104 A 5320 ANGLE BOEING 737 7372H4 138448C NM SERVICE DOORWAY CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED THRESHOLD ATTACH ANGLE AT Z-ANGLE. REMOVED AND REPLACED Z-ANGLE PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300957 19981113 00957 NM 1998 11 13 SWAA982753 1 19981104 A 5751 ANGLE BOEING 737 7372H4 138448C NM AILERON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 085SW 22826 DURING SCHEDULED 1/4D CHECK, FOUND AILERON ACCESS PANEL 7104L SUPPORT ANGLE CRACKED IN TWO PLACES. REMOVED AND REPLACED ANGLE PER BOEING SRM. 2 L 7 2 4F A16WE 1998111300958 19981113 00958 NM 1998 11 13 SWAA982754 1 19981104 A 3350 BATTERY PACK BOEING 737 7372T4 1384492 NM PAX DOOR DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT FWD ENTRY DOOR. REMOVED AND REPLACED BATTERY PACK PER BOEING MM. 2 L 7 2 4F A16WE 1998111300959 19981113 00959 NM 1998 11 13 SWAA982755 1 19981104 A 5530 TIP BOEING 737 7373H4 1384600 NM VERT STAB CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 339SW 24090 DURING SCHEDULED D-CHECK, FOUND VERT FIN CENTER TIP FAIRING HAS WING CORRODED AT FASTENER HOLES AND FWD EDGE. REPAIRED L/E VERT STAB PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300960 19981113 00960 NM 1998 11 13 SWAA982756 1 19981104 A 5210 ANGLE BOEING 737 7373A4 1384585 NM PAX DOOR CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND ANGLE CRACKED ON UPPER AFT CORNER OF FWD ENTRY DOOR. REMOVED AND REPLACED ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300961 19981113 00961 NM 1998 11 13 SWAA982757 1 19981104 A 5314 KEEL BEAM BOEING 737 7373A4 1384585 NM FUSELAGE DELAMINATED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND KEEL BEAM ACCESS PANEL FWD OF WHEEL WELL IS DELAMINATED AND OIL SOAKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300962 19981113 00962 NM 1998 11 13 SWAA982758 1 19981104 A 5241 SKIN BOEING 737 7373A4 1384585 NM SERVICE DOOR DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND AFT GALLEY SVC DOOR SKIN BENT AT HINGE CUTOUT OF LOWER HINGE AREA. STRAIGHTENED SKIN PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998111300963 19981113 00963 WP 1998 11 13 ARWA981054 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1040 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON UPPER SKIN FUSELAGE EXTERIOR STATION 1040 LONGERON 1L, REMOVED CORROSION (BEYOND LIMITS) FABRIC ATED FILLER AND DOUBLER AND INSTALLED IAW EO SEMAN NR 1027 WORK ACCOMPLISHED UNDER ARROW ARI FORM JW3B CPCP CONTROL 5109 A. (M) 2 L 7 4 4F 4A25 1998111300964 19981113 00964 WP 1998 11 13 ARWA981053 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 640 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - BLEND OUT, FOUND BEYOND LIMITS ON FUSELAGE SKIN EXTERIOR STATION 640 LONG 35L TO LONG 32R FABRICATED DOUBLER AND I NSTALLED IAW EO SMAN NR 1008-1 AND SRM 51-1-20D WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5452. (M) 2 L 7 4 4F 4A25 1998111300965 19981113 00965 WP 1998 11 13 ARWA981052 1 19981020 A 5314 KEEL BEAM DOUG DC8 DC863F 302198F WP BS 920 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND 8 INCH CRACK ON KEEL BEAM TEE LT MLG WW STATION 920.00 CUT OUT DAMAGED AREA FABRICATED VERTICAL KEEL BEAM TE E, FILLER AND DOUBLER AND INSTALLED IAW EO SEMAN NR 1029 WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5511. (M) 2 L 7 4 4F 4A25 1998111300966 19981113 00966 WP 1998 11 13 ARWA981051 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 60 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION W60 RBL 25, CUT OUT AREA OF CORROSION FABRICATED FILLE R AND ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371015 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5085 A. (M) 2 L 7 4 4F 4A25 1998111300967 19981113 00967 WP 1998 11 13 ARWA981050 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 610 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON DOUBLER FINGER STATION 610 LONGERON 34L . REMOVED CORROSION (BEYOND LIMITS) CUT OUT AREA OF CO RROSION, FABRICATED DOUBLER AND INSTALLED IAW EO JOSSAIR, CO NR 18R5311018 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B C PCP CONTROL 5121A. (M) 2 L 7 4 4F 4A25 1998111300968 19981113 00968 WP 1998 11 13 ARWA981049 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1655 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND SKIN REPAIR IMPROPER FUSELAGE EXTERIOR STATION FS 1655 LONGER 21L. REMOVED IMPROPER REPAIR FABRICATED NEW O NE AND REPLACED IAW SRM 53-2-0 FIG 18 AND 51-1-20D WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5067A. (M) 2 L 7 4 4F 4A25 1998111300969 19981113 00969 WP 1998 11 13 ARWA981048 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 610 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FUSELAGE SKIN SPLICE DOUBLER FINGER STATION 610.00 LONGERON 34L. CUT OUT AREA OF CORROSION, FA BRICATED DOUBLER AND SHIM AND INSTALLED IAW EO JOSSAIR, CO NR 18R5311018. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B C PCP CONTROL 5074A. (M) 2 L 7 4 4F 4A25 1998111300970 19981113 00970 WP 1998 11 13 ARWA981047 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 1040 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM UPPER FORWARD FLANGE, MAIN CABIN STATION 1040 RBL 43.5 TO RBL 55. CUT OUT AREA OF CO RROSION, FABRICATED ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371030. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B C PCP CONTROL 5994. (M) 2 L 7 4 4F 4A25 1998111300971 19981113 00971 WP 1998 11 13 ARWA981046 1 19981020 A 5320 WEB DOUG DC8 DC863F 302198F WP BS 857 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON PATH RT MLG WW STATINO 857 THROUGH STATION 879. REMOVED CORROSION (BEYOND LIMITS). REMOVED PA TCH FABRICATED DOUBLER AND REPLACED IAW DOUGLAS ROD SKETCH 98-08-20-001 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5997. (M) 2 L 7 4 4F 4A25 1998111300972 19981113 00972 WP 1998 11 13 ARWA981045 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 35 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - IMPROPER REPAIR ON SKIN FUSELAGE EXTERNAL STATION 35, LONGERON 8L TO LONGERON 10L. REMOVED IMPROPER REPAIR FABRIC ATED DOUBLER AND REPLACED IAW SRM 53-2-0 FIG 15. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5071A. (M) 2 L 7 4 4F 4A25 1998111300973 19981113 00973 WP 1998 11 13 ARWA981044 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP FUSELAGE CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - NR 1 CRACK AND 3 INCH, 1.5 INCH RUPTURES AND INADEQUATE REPAIR CUT OUT DAMAGED AREA FABRICATED FILLERS, DOUBLER AN D TRIPLER AND INSTALLED IAW SRM 51-1-20D AND BOEING ROD SKETCH 98-08-18-005. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5679. (M) 2 L 7 4 4F 4A25 1998111300974 19981113 00974 WP 1998 11 13 ARWA981043 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 902 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FUSELAGE EXTERIOR SKIN STATION 902.125 LONGERON 13L TO 15L. REMOVED CORROSION (BEYOND LIMITS). FABRICATED DOUBELR AND INSTALLED IAW EO SEMAN NR 1024. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5117A . (M) 2 L 7 4 4F 4A25 1998111300975 19981113 00975 WP 1998 11 13 ARWA981042 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 55 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM CARGO COMPARTMENT STATION 55, RBL 12 TO RBL 12. REMVOED CORROSION, BEYOND LIMITS. F ABRICATED ANGLES TWO AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371031 WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CON TROL 4392. (M) 2 L 7 4 4F 4A25 1998111300976 19981113 00976 WP 1998 11 13 ARWA981041 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 1300 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 1300 RBL 17 CUT OUT AREA OF CORROSION. FABRICATED FIL LER AND ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371032. WORK ACCOMPLISHED UNDER ARROW AIR JW3B CPCP CONTROL 5990. (M) 2 L 7 4 4F 4A25 1998111300977 19981113 00977 WP 1998 11 13 ARWA981040 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 660-720 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON REPAIR FUSELAGE STATION 660 TO 720, LONG 34 LEFT TO LONG 34 RT. REMOVED OLD REPAIR FABRICATED DOUBLER AND TRIPLER AND INSTALLED IAW DOUGLAS ROD SKETCH 98-08-25-008. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5363. (M) 2 L 7 4 4F 4A25 1998111300978 19981113 00978 WP 1998 11 13 ARWA981039 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 879-902 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FUSELAGE EXTERIOR SKIN STATION 879 THROUGH 902 LONGERON 13R TO LONGERON 15R. REMOVED CORROSION (BEYOND LIMITS). FABRICATED DOUBELR IAW BOEING ACTION NR 378231 AND 379978. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW 3B CPCP CONTROL 5116A. (M) 2 L 7 4 4F 4A25 1998111300979 19981113 00979 WP 1998 11 13 ARWA981038 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 70 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 70, RBL 29. REMOVED CORROSION SRM 51-1-8. FABRICATED ANGLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371033. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5091A. (M) 2 L 7 4 4F 4A25 1998111300980 19981113 00980 WP 1998 11 13 ARWA981037 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 1364 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND REPAIR IMPROPER ON SKIN FUSELAGE EXTERIOR STATION 1364, LONGERON 23R. REMOVED IMPROPER REPAIR. FABRICATED DOUBLER AND FINGER DOUBLERS AND REPLACED IAW SRM 53-2-1 FIG 7. WORK ACCOMPLISHED UNDER ARROW FORM M3A CONTROL 5063A. ( M) 2 L 7 4 4F 4A25 1998111300981 19981113 00981 WP 1998 11 13 ARWA981036 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 175 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - INADEQUATE REPAIR ON FUSELAGE EXTERIOR SKIN STATION 175 LONGERON 28R TO LONGERON 29R. INADEQUATE DOUBLER AND FING ER DOUBLERS AND REPLACED IAW SRM 53-2-1 FIG 7. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5062A. (M) 2 L 7 4 4F 4A25 1998111300982 19981113 00982 WP 1998 11 13 ARWA981035 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 600 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM, UPPER AFT MAIN CARGO COMPARTMENT STATION 600 RBL 33 CUT OUT AREA OF CORROSION. FABR ICATED FILLER AND ANGLE AND INSTALLED IAW WITH EO JOSSAIR, CON NR 18R5371011. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW 3B CPCP CONTROL 5090A. (M) 2 L 7 4 4F 4A25 1998111300983 19981113 00983 WP 1998 11 13 ARWA981034 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 160 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM UPPER AFTR FLANGE STATION 160 RBL 25, CUT OUT AREA OF CORROSION. FABRICATED FILLERS AND ANGLES AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371017. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CONTROL 5081A. ( M) 2 L 7 4 4F 4A25 1998111300984 19981113 00984 WP 1998 11 13 ARWA981033 1 19981020 A 5315 FLOORBEAM DOUG DC8 DC863F 302198F WP BS 180 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON FLOORBEAM MAIN CARGO COMPARTMENT STATION 180, CUT OUT AREA OF CORROSION. FABRICATED FILLERS AN GLE AND INSTALLED IAW EO JOSSAIR, CO NR 18R5371014. WORK ACCOMPLISHED UNDER ARROW AIR FORM JW3B CPCP CONTROL 5082A. (M ) 2 L 7 4 4F 4A25 1998111300985 19981113 00985 WP 1998 11 13 ARWA981032 1 19981020 A 5330 SKIN DOUG DC8 DC863F 302198F WP BS 280 DAMAGED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND PATCH DETERIORATED ON FORWARD DOOR EXTERNAL FUSELAGE. FORWARD CARGO COMPARTMENT STATION 280. REMOVED PATCH AND FABRICATED DOUBLER AND REPLACED IAW SRM 53-2-0. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 5973. (M) 2 L 7 4 4F 4A25 1998111300986 19981113 00986 NM 1998 11 13 P2EA98174 1 19980924 A 7312 BACCF10HV16 CONNECTOR BOEING 737 737222 1384473 NM NR 1 ENGINE FAILED A P2EA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CE 05 208AU 19547 FLT 612 - MCI - EMERGENCY DECLARED, NR 1 ENGINE INFLIGHT SHUTDOWN, LANDING UNEVENTFUL. NR 1 FUEL HEAT VALVE CAME ON IN FLIGHT. NR 1 OIL TEMP EXCEEDED LIMTIS (TIME IN YELLOW BAND) SHUTDOWN NR 1 ENGINE, RETURNED TO MCI. FOUND WIRE BURNED A T 'B' PIN ON NR 1 FUEL HEAT VALVE CONNECTOR. REPLACED NR 1 FUEL HEAT CONNECTOR PER MM 20-24-20. REPLACED NR 1 FUEL HEA T VALVE, PRECAUTIONARY PER MM 73-14-11. DRAINED NR 1 ENGINE OIL. REPLACED OIL SCREEN ELEMENT, SERVICED OIL TO FULL. L EAK AND OPS CHECK OK. PERFORMED OIL TEMP INDICATOR ADJUST/TEST PER MM 79-34-11, CHECKS OK. REPLACED P5-2 FUEL PANEL PR ECAUTIONARY. PERFORMED EVALUATION FLIGHT. FUEL HEAT SYSTEM CYCLED IN FLIGHT. ALL INDICATIONS NORMAL. ALL OIL TEMP 2 L 7 2 4F A16WE 1998111300987 19981113 00987 NM 1998 11 13 P2EA98173 1 19980923 A 7312 CONNECTOR BOEING 737 737222 1384473 NM NR 1 ENGINE DAMAGED A P2EA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CE 05 208AU 19547 FLT 590 - MCI - EMERGENCY DECLARED, NR 1 ENGINE INFLIGHT SHUTDOWN. LANDING UNEVENTFUL. SHUTDOWN NR 1 ENGINE DUE TO HIG H OIL TEMP. FOUND LOOSE PIN IN FUEL HEAT VALVE CONNECTOR. RESET PIN, CLEANED CONNECTOR. VALVE OPS CHECKED OK. RAN EN GINE, CYCLED FUEL HEAT VALVE, VERIFIED OIL TEMP RISE, CYCLED VALVE TO OFF POSITION OIL TEMP NORMAL. (M) 2 L 7 2 4F A16WE 1998111300988 19981113 00988 NM 1998 11 13 NOCA2198 1 19981002 A 3610 32143067 VALVE BOEING 757 75723A 1384967 NM RT ENGINE INOPERATIVE A NOCA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 15 757NA 24567 SNN - ACCOMPLISHED HIGH ENERGY STOP INSPECTION. NO DISCREPANCIES NOTED. PERFORMED RIGHT ENGINE RUN UP. BLEED LIGHT CAM E ON AT 90 PERCENT. BLEED SWITCH POSITIONED TO OFF AND PLACARDED. ASSIGNED MEL IAW NAA DISPATCH DEVIATION GUIDE. REPL ACED RIGHT ENGINE PRSOV VALVE. LEAK CHECK AND OP CHECK OK. (M) 2 L 7 2 4F RT A2NM 1998111300989 19981113 00989 1998 11 13 NOCA2098 4 19980927 A 2562 EB2BW ELT BOEING 757 75723A 1384967 NM BS 400 INOPERATIVE A NOCA O OTHER N FALSE WARNING CR CRUISE 1 EA 15 757NA 24567 EMERGENCY LOCATOR TRANSMITTER SIGNAL INTERMITTENTLY TRANSMITTING DURING FLIGHT. SIGNAL CAN BE HEARD ON 121.5. REPLACED ELT TRANSMITTER. (M) 2 L 7 2 4F RT A2NM 1998111300990 19981113 00990 NM 1998 11 13 EISA98248 1 19981005 A 2611 302842 SMOKE DETECTOR BOEING 727 72731 1384010 NM CABIN FAILED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 240NE 26 18906 ON PREFLIGHT, NR 3 SMOKE DETECTOR IN CABIN WOULD NOT TEST. GENERATED FROM MAINTENANCE REPORT. REMOVED AND REPLACED NR 3 CABIN SMOKE DETECTOR. OPS CHECK NORMAL PER CHAPTER 26. (M) 2 L 7 3 4F A3WE 1998111300991 19981113 00991 NM 1998 11 13 EISA98247 1 19981006 A 2610 65249203 ACCESSORY UNIT BOEING 727 72731 1384010 NM CABIN MALFUNCTIONED A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 240NE R00130 18906 DURING FLIGHT, FIREBELL SOUNDS IN LIGHT/MODERATE PRECIPITATION ON VISIBLE MOISTURE. NO OTHER INDICATIONS OR LIGHTS. RE MOVED AND REPLACED FIRE ACCESSORY UNIT WITH SERVICEABLE UNIT. OPS CHECK GOOD PER MM 26-12-01. (M) 2 L 7 3 4F A3WE 1998111300992 19981113 00992 NM 1998 11 13 EISA98246 1 19981004 A 3350 1000677 LIGHT BOEING 727 7272M7 138407S NM CABIN INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 742RW 2416 21952 EMERGENCY LIGHT INOPERATIVE OVER MAIN ENTRY DOOR. GENERATED FROM MAINTENANCE REPORT. REPLACED EMERGENCY LIGHT ASSEMBLY . OPS CHECK GOOD IAW MM CHAPTER 33. (M) 2 L 7 3 4F A3WE 1998111300993 19981113 00993 EU 1998 11 13 COEA9802720 1 19980217 A 2612 D889N FIRE LOOP FOKKER F27 F27MK500 4990629 EU NR 2 ENGINE MALFUNCTIONED A COEA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 NM 13 720FE 10464 DURING TAXI INTO ONT, NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. NO SIGNS OF SMOKE OR FIRE WERE DETECTED. MAINTE NANCE INSPECTED AND TROUBLESHOT SYSTEM. FOUND THE FIRE WIRE SECTION AT INBOARD, LOWER FIREWALL SHORTED. REMOVED AND RE PLACED FIRE WIRE SEGMENT IAW RR MM 26-10-00. SYSTEM TESTS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T A817 1998111300994 19981113 00994 1998 11 13 98ZZZM816 4 19980923 A 2565 SLIDE BOEING 757 75723N 1384973 NM PAX DOOR MALFUNCTIONED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 516AT 27972 IND - WHILE PERFORMING TASK CARD 25-016-01, "SLIDE DEPLOYMENT FOR L-4 DOOR", THE DOOR ASSIST DID NOT OPEN THE DOOR IN 2- 6 SECONDS. HAD TO PUSH THE DOOR OPEN FOR SLIDE DEPLOYMENT. SUSPECTED SLIDE SHIFTED UNDER THE COVER CATCHING THE DOOR F RAME. A/C HAD P/C/W MOD SB 757-25-0175. THE SLIDE AND DOOR ASSIST BOTTLE WERE REPLACED AFTER INSPECTING THE COVER AND DOOR FRAME. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A2NM 1998111300995 19981113 00995 EU 1998 11 13 USAAF98072 1 19980830 A 5280 DOOR FOKKER F28 F28MK0100 4990807 EU RT MLG SEPARATED A USAA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 EA 19 862US 11300 HSV - FLT 721 - ON APPROACH TO HSV AFTER LANDING GEAR SELECTED DOWN, MLG DOOR UNSAFE' MESSAGE ILLUMINATED. CREW RECYCLE D GEAR. 10 SECONDS LATER THE MESSAGE APPEARED AGAIN. NO EMERGENCY WAS DECLARED AND FLIGHT LANDED WITHOUT FURTHER INCID ENT. MAINTENANCE FOUND THE RIGHT FORWARD MAIN LANDING GEAR INBOARD DOOR ACTUATOR HAD PULLED AWAY FROM THE KEEL BEAM. T HIS RESULTED IN STRUCTURAL DAMAGE TO THE KEEL BEAM. MAINTENANCE REPAIRED PER ENGINEERING AUTHORIZATION EA50457. ENGINE ERING ISSUED ENGINEERING ORDER 3298F064 TO CHECK THE TORQUE OF THE ACTUATOR HARDWARE ON THE REST OF THE F100 FLEET. (M) 2 L 7 2 4F RT 1998111300996 19981113 00996 NE 1998 11 13 ASAA9880139 2 19980729 A 7310 745608 FUEL SYSTEM DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RT ENGINE MALFUNCTIONED A ASAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 NM 01 957AS 31152 639 49126 PDX - FLT 648 - DURING CLIMB-OUT, CREW REPORTED THE RT ENGINE FLAMED OUT PASSING 25,000 FT. ACCOMPLISHED QRH PROCEDURE, ENGINE WOULD NOT RESTART. RETURNED TO PDX AND LANDED WITHOUT INCIDENT. INSPECTED RT ENGINE INLET AND EXHAUST, NO DEFE CT NOTED. MANUALLY ROTATED ENGINE, ROTATES FREELY. MOTORED ENGINE, ALL MOTORING PARAMETERS NORMAL. ACCOMPLISHED ENGIN E START, ALL START AND IDLE PARAMETERS NORMAL. DURING ENGINE RUN WITH FUEL HEAT SELECTED, FOUND ENGINE WOULD SHUTDOWN A FTER FUEL HEAT 60 SECOND TIME DELAY. REPLACED ENGINE FUEL CONTROL UNIT AND FILTER, FUEL PUMP, AND FUEL HEATER. ACCOMPL ISHED ENGINE RUN UP, ALL PARAMETERS AND OPERATIONS NORMAL. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998111300997 19981113 00997 NE 1998 11 13 98ZZZM817 2 19980729 A 7314 384300 FUEL PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RT ENGINE MALFUNCTIONED A ASAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 NM 01 957AS 20996 9158 49126 PDX - FLT 648 - DURING CLIMB-OUT, CREW REPORTED THE RT ENGINE FLAMED OUT PASSING 25,000 FT. ACCOMPLISHED QRH PROCEDURE, ENGINE WOULD NOT RESTART. RETURNED TO PDX AND LANDED WITHOUT INCIDENT. INSPECTED RT ENGINE INLET AND EXHAUST, NO DEFE CT NOTED. MANUALLY ROTATED ENGINE, ROTATES FREELY. MOTORED ENGINE, ALL MOTORING PARAMETERS NORMAL. ACCOMPLISHED ENGIN E START, ALL START AND IDLE PARAMETERS NORMAL. DURING ENGINE RUN WITH FUEL HEAT SELECTED, FOUND ENGINE WOULD SHUTDOWN A FTER FUEL HEAT 60 SECOND TIME DELAY. REPLACED ENGINE FUEL CONTROL UNIT AND FILTER, FUEL PUMP, AND FUEL HEATER. ACCOMPL ISHED ENGINE RUN UP, ALL PARAMETERS AND OPERATIONS NORMAL. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998111300998 19981113 00998 NE 1998 11 13 98ZZZM818 2 19980729 A 7321 76960612 FUEL CONTROL DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE RT ENGINE MALFUNCTIONED A ASAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 NM 01 957AS 31894 1102 49126 PDX - FLT 648 - DURING CLIMB-OUT, CREW REPORTED THE RT ENGINE FLAMED OUT PASSING 25,000 FT. ACCOMPLISHED QRH PROCEDURE, ENGINE WOULD NOT RESTART. RETURNED TO PDX AND LANDED WITHOUT INCIDENT. INSPECTED RT ENGINE INLET AND EXHAUST, NO DEFE CT NOTED. MANUALLY ROTATED ENGINE, ROTATES FREELY. MOTORED ENGINE, ALL MOTORING PARAMETERS NORMAL. ACCOMPLISHED ENGIN E START, ALL START AND IDLE PARAMETERS NORMAL. DURING ENGINE RUN WITH FUEL HEAT SELECTED, FOUND ENGINE WOULD SHUTDOWN A FTER FUEL HEAT 60 SECOND TIME DELAY. REPLACED ENGINE FUEL CONTROL UNIT AND FILTER, FUEL PUMP, AND FUEL HEATER. ACCOMPL ISHED ENGINE RUN UP, ALL PARAMETERS AND OPERATIONS NORMAL. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998111300999 19981113 00999 NE 1998 11 13 AALA981474 2 19980805 A 7314 6550934 FUEL PUMP NASH DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE CENTER TANK FAILED A AALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 255AA 1092A 49287 ORD - FLT 1949 - DURING CRUISE, EN ROUTE DTW-DFW, UNABLE TO TRANSFER FUEL FROM CENTER TANK. PHASE B PLUS C CIRCUIT BREA KER WILL NOT RESET ON FORWARD CENTER FUEL PUMP. AIR INTERRUPTED AND LANDED ORD WITHOUT INCIDENT. REPLACED FORWARD CENT ER FUEL PUMP AND HARNESS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998111301000 19981113 01000 EU 1998 11 13 VTZA98288 1 19980908 A 2121 1379208L414 DUCT BAG JETSTM JETSTM3201 1500217 EU ACM LOOSE A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 482UE 897 FLT 6568 - IAD-SCE - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CREW HEAD LOUD BANG AND WOULD NOT HOLD PR ESSURE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ACM DUCT AND RESECURED TO FLANGE, OPS CHECK OK. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998111301001 19981113 01001 1998 11 13 USAASB98162 4 19980629 A 2210 AFCS BOEING 737 7374B7 1384702 NM COCKPIT MALFUNCTIONED A USAA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 19 779AU 30707 24996 CLT - FLT 1903 - FLT WAS ON APPROACH, DESCENDING OUT OF 5,000 FT, WHEN THE AUTOPILOT BANKED THE A/C INTO A HARD LT TURN. CAPT TRIED TO DISENGAGE THE AUTOPILOT BUT IT WOULD NOT DISENGAGE. HE FIREWALLED THE ENGINES FOR APPROX 5 SECONDS FOR AN IMMEDIATE CLIMB AND WAS ABLE TO REGAIN CONTROL OF THE A/C. CAPT WAS ADVISED BY ATC TO AVOID TRAFFIC AND WAS SEQUENCE D BACK FOR LANDING. FLT LANDED W/O FURTHER INCIDENT. MX ACCOMP THE FOLLOWING, DFCS INFLIGHT FAULTS, GPWS INFLIGHT FAUL TS, DFCS CURRENT STATUS, DFCS GROUND FUNCTIONAL TESTS 36 AND 51, DFCS AILERON RIGGING TESTS, CHECK OF SHEAR RIVETS ON AU TOPILOT AILERON ACTUATORS, SELF TEST OF YAW DAMPER AND ELECTRICAL CHECK OF AUTOPILOT AILERON SERVO'S. ALL ABOVE ITEMS C 2 L 7 2 4F RT A16WE 1998111301002 19981113 01002 EU 1998 11 13 AALA981357 1 19980709 A 7930 SWITCH AIRBUS 300 A300B4605R 3930308 EU RT ENGINE FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 70072 515 LHR - FLT 109 - AFTER T/O, THE FWD INSTRUMENT PNL RT ENG OIL CLOG LAMP ILLUMINATED, FOLLOWED A SHORT TIME LATER BY THE E CAM PROCEDURE FOR OIL CLOG DIPICTED. RT THROTTLE RETARDED TO IDLE. AFTER 3 MINS WITH THE OIL CLOG LAMP BRIGHTLY LIT. T HE ENG WAS SHUT DOWN WITH THE RT FUEL SHUTOFF VALVE. A SINGLE ENG APPROACH WAS FLOWN AND A LANDING MADE AT 36,800 LBS. RT SIDE BRAKES INDICATED 700 DEGREES. THE RT 4 TIRES DEFLATED AFTER APPROX 30 MIN CREW WAS CLEARED TO DEPART. REPLACE D DIFF PRESS SW, ACCOMP NR 2 ENG POWER RUN. NO ABNORMAL IND'S. OK FOR SERV REF MX CHECK CARD AE059214. VISUAL INSPECT ION ACCOMP OF A/C WITH REF TO LANDING WT AND SINK RATE. ALL CHECKS OK. REPLACED ALL RT MLG WHEELS AND BRAKES. ALSO, 2 L 7 2 4F RT A35EU 1998111301003 19981113 01003 NE 1998 11 13 PLGA980902A 2 19980902 A 7200 6052T88601 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT79B 30030 NE LT NACELLE MAKING METAL A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 342BE 367395K 340A096 BOS - FLT 4383 - AFTER TAKEOFF, THE LEFT ENGINE CHIP DETECTOR WARNING ILLUMINATED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LARGE AMOUNTS OF METAL ON DETECTOR. LEFT ENGINE WAS REPLACED. AIRCRAFT WAS RETURN ED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998111301004 19981113 01004 NM 1998 11 13 USAASB98217 1 19980821 A 7932 39302001789 INDICATOR BOEING 737 737201 1384454 NM COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 235US 22275 TYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. AL L OTHER INDICATIONS WERE NORMAL. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINE WAS NEVER SHUT DOWN. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE REMOVED AND REPLAC ED THE NR 1 ENGINE OIL QTY INDICATOR. DRAINED OIL, REPLACED TRANSMITTER AND REFILLED OIL. CHECKED CALIBRATION AND CHEC KED FOR LEAKS. GROUND CHECKED OK. (M) 2 L 7 2 4F A16WE 1998111301005 19981113 01005 NM 1998 11 13 98ZZZM819 1 19980821 A 7932 39101201001 TRANSMITTER BOEING 737 737201 1384454 NM NR 1 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 235US 22275 TYS - FLT 1797 - AT 29,000 FT, THE NR 1 ENGINE OIL QTY SLOWLY DROPPED TO ONE GALLON AND EVENTUALLY TO A HALF GALLON. AL L OTHER INDICATIONS WERE NORMAL. FLIGHT DIVERTED TO TYS AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED AND THE NR 1 ENGINE WAS NEVER SHUT DOWN. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE REMOVED AND REPLAC ED THE NR 1 ENGINE OIL QTY INDICATOR. DRAINED OIL, REPLACED TRANSMITTER AND REFILLED OIL. CHECKED CALIBRATION AND CHEC KED FOR LEAKS. GROUND CHECKED OK. (M) 2 L 7 2 4F A16WE 1998111301006 19981113 01006 WP 1998 11 13 VTZA98246 1 19980723 A 7712 3104404 TORQUE BRIDGE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE FAILED A VTZA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 332UE 41100 FLT 6503 - LGA-IAD - DURING LANDING, EXPERIENCED A LT ENGINE TQ FLUCTUATION. A/C DECLARED AN EMERGENCY AND MADE AN UNEV ENTFUL LANDING AT IAD. MX CONTROL DISPATCHED. MX TO THE AIRCRAFT WHERE THE MX PERSONNEL FOUND A DISCREPANCY WITH THE L T ENGINE NR 1 TORQUE BRIDGE. MX PROGRAMMED THE IEC TO SELECT THE NR 2 TORQUE BRIDGE IAW SB TPE 331-76-7013 AND MM REF C HAP 71. ENGINE GROUND RUNS WERE COMPLETED SATISFACTORILY. DURING THE RUNS IT WAS NOTED THAT THE DELTA P/P BPX WAS CAUS ING AN ERROR MESSAGE TO THE IEC. MX REMOVED AND REPLACED THE DELTA P/P TRANSDUCER IAW CHP 76 OF THE MM. ALL GROUND ENG INE RUNS WERE COMPLETED AND WERE SATISFACTORY. A/C WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1998111301007 19981113 01007 WP 1998 11 13 98ZZZM820 2 19980723 A 7320 3105869 TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE FAILED A VTZA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 332UE 41100 FLT 6503 - LGA-IAD - DURING LANDING, EXPERIENCED A LT ENGINE TQ FLUCTUATION. A/C DECLARED AN EMERGENCY AND MADE AN UNEV ENTFUL LANDING AT IAD. MX CONTROL DISPATCHED. MX TO THE AIRCRAFT WHERE THE MX PERSONNEL FOUND A DISCREPANCY WITH THE L T ENGINE NR 1 TORQUE BRIDGE. MX PROGRAMMED THE IEC TO SELECT THE NR 2 TORQUE BRIDGE IAW SB TPE 331-76-7013 AND MM REF C HAP 71. ENGINE GROUND RUNS WERE COMPLETED SATISFACTORILY. DURING THE RUNS IT WAS NOTED THAT THE DELTA P/P BPX WAS CAUS ING AN ERROR MESSAGE TO THE IEC. MX REMOVED AND REPLACED THE DELTA P/P TRANSDUCER IAW CHP 76 OF THE MM. ALL GROUND ENG INE RUNS WERE COMPLETED AND WERE SATISFACTORY. A/C WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1998111301008 19981113 01008 WP 1998 11 13 VTZA98247 1 19980723 A 7712 3104404 TORQUE BRIDGES JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 307UE 41021 FLT 6205 - IAD-MHT - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE TORQUE FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SWAPPED TORQUE BRIDGES. OPS CHECK OK. AIRCRAFT W AS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1998111301009 19981113 01009 WP 1998 11 13 EIAA980238 1 19980827 A 3260 7000010101 SWITCH DOUG DC9 DC933F 302207A WP LT MLG FAILED A EIAA K NONE P NO WARNING INDICATION AP APPROACH 1 NM 09 933F 47191 OAK - UPON APPROACH INTO OAK, LEFT GEAR UNSAFE LIGHT DID NOT ILLUMINATE WHEN THROTTLES WERE RETARDED. UPON GEAR EXTENSI ON, LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE. PERFORMED LOW PASS FOR MAINTENANCE AND CONFIRMED GEAR WAS DOWN. NO HORN NOTED AT FL 40 AND HORN WAS SILENCED BY GEAR EXTENSION. FOUND BAD SWITCH AND CANNON PLUG. (M) 2 L 7 2 4F A6WE 1998111301010 19981113 01010 WP 1998 11 13 98ZZZM821 1 19980827 A 3260 DS0775070 CONNECTORS DOUG DC9 DC933F 302207A WP LT MLG FAULTY A EIAA K NONE P NO WARNING INDICATION AP APPROACH 1 NM 09 933F 47191 OAK - UPON APPROACH INTO OAK, LEFT GEAR UNSAFE LIGHT DID NOT ILLUMINATE WHEN THROTTLES WERE RETARDED. UPON GEAR EXTENSI ON, LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE. PERFORMED LOW PASS FOR MAINTENANCE AND CONFIRMED GEAR WAS DOWN. NO HORN NOTED AT FL 40 AND HORN WAS SILENCED BY GEAR EXTENSION. FOUND BAD SWITCH AND CANNON PLUG. (M) 2 L 7 2 4F A6WE 1998111301011 19981113 01011 EU 1998 11 13 USAASB98252 2 19980924 A 7200 ENGINE BOEING 737 7374B7 1384702 NM CFMINT CFM56 CFM563B2 13802 EU NR 1 FOD A USAA A UNSCHED LANDING C B E F.O.D. SMOKE/FUMES/ODORS/SPARKS VIBRATION/BUFFET CL CLIMB 1 EA 19 439US 24781 CLT - FLT 1579 - JUST AFTER TAKEOFF, THE NR 1 ENGINE INJESTED A MEDIUM SIZED BIRD. NO ADVERSE AFFECT WAS NOTICED IN ENG INE PARAMETERS BUT CREW DID NOTICE A DIFFERENT NOISE COMING FROM THAT ENGINE. A MOMENTARY SMELL IN CABIN WAS PRESENT AN D A VIBRATION WAS FELT AT CERTAIN POWER SETTINGS. FLIGHT RETURNED TO FIELD AT CLT AS A PRECAUTION AND LANDED WITHOUT FU RTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE ACCOMPLISHED BIRDSTRIKE INSPECTION AND BOROSCOPE INSPECTION PER MM 71-00-47. NO DEFECTS NOTED. CLEANED FAN, CORE INLET VANES AND OIL COOLER. AIRCRAFT OK FOR SERVICE (M) 2 L 7 2 4F 4 F RT A16WE E21EU 1998111301012 19981113 01012 WP 1998 11 13 EIAA980237 1 19980824 A 5230 SEAL DOUG DC9 DC933F 302207A WP CARGO DOOR FAILED A EIAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 09 944F 47194 SEA - DURING CLIMB, PASSING 4 PSI DIFFERENTIAL, A LOAD PULSATING HUM, VIBRATION AND AIR NOISE WAS HEARD FROM MAIN CABIN. PRESSURIZATION BECAME UNCONTROLLABLE. RETURNED TO SEA. REPLACED FORWARD UPPER CARGO DOOR PRESSURE SEAL PER MM 52-32- 01. PRESSURIZATION CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1998111301013 19981113 01013 WP 1998 11 13 RAIA980909 2 19980917 A 7320 8974575 BYPASS VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CE 03 422AM 1278 856 FLT 7397 - STL - LEFT ENGINE TORQUE DROPPED TO 40 PERCENT ON TAKEOFF ROLL. MAINTENANCE REPLACED LEFT FUEL BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998111301014 19981113 01014 NM 1998 11 13 CLCA9801 1 19981101 A 5754 114N300280A SKIN BOEING 757 75723APF 1384966 NM NR 6 LE FLAP DAMAGED A CLCA O OTHER D INFLIGHT SEPARATION AP APPROACH 1 SO 19 572CA A20299 24868 FLT 56 - BOG-MIA - UPON APPROACH, CREW LOGGED 'FLAPS MAKE LOUD GRINDING NOISE IN FLIGHT WHEN FLAPS MOVING FROM POSITION 0 TO 1.' UPON GROUND INSPECTION AT MAI, FOUND NR 6 INBOARD SLAT TRAILING EDGE WEDGE DAMAGED, PORTIONS OF MATERIAL MISSI NG. ALSO, FOUND MINOR DAMAGE TO UPPER WING COMPOSITE PANELS UNDER THE LOCATION OF THE T/E WEDGE. ACCOMPLISHED INSPECTI ON OF FUSELAGE EMPENAGE, VERT/HORIZONTAL STABILIZER INCLUDING FLIGHT CONTROL SURFACES, NO FURTHER DAMAGE FOUND. REPLACI NG NR 6 INBOARD SLAT WITH LOANER FROM BOEING. REMOVED SLAT WILL BE REPAIRED AT LOCAL COMPOSITE SHOP. (M) 2 L 7 2 4F RT A2NM 1998111301015 19981113 01015 NE 1998 11 13 EIAA980236 2 19980824 A 7261 SEAL BOEING 747 747SR46 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE FAILED A EIAA K NONE O OTHER TO TAKEOFF 1 NM 09 478EV 21033 HNL - AFTER TAKEOFF, NR 3 ENGINE OIL QTY DECREASED TO .5 GALLONS, OIL PRESSURE FLUCTUATED 40-45 PSI. REDUCED POWER AND OIL PRESSURE DROPPED TO 35 PSI WITH ASSOCIATED OIL PRESSURE LIGHT. SHUTDOWN ENGINE NR 3, WINDMILLED FOR APPROXIMATELY 3 2 MINUTES, OIL PRESSURE AT 12 PSI. PERFORMED ENGINE WINDMILL INSPECTION PER MM 72-00-00. CHECKED MAIN OIL FILTER AND C HIP DETECTORS PER MM 72-61-00 AND -05. REPLACED GENERATOR AND CSD GARLOCK SEALS PER MM 72-61-07 AND -08. REPLACED CSD TRANSFER TUBE PER MM 72-61-62. REPLACED CSD DRIVE SHAFT SEALS AND GENERATOR SEALS PER MM 72-61-16. RAN ENGINE, NO LEAK S FOUND. (M) 2 L 7 4 4F 4 F A20WE E20EA 1998111301016 19981113 01016 EU 1998 11 13 KDAA98012 1 19980916 A 3230 1500RC106P50 CONNECTOR AMD FALC20 FALCON20C5 2730107 EU LT MLG WW DAMAGED A DKAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 GL 23 980R 98 WHEN L/G WAS SELECTED TO DOWN, OBSERVED NO LIGHTS. L/G SELECTOR C/B WAS TRIPPED. AFTER RESETTING C/B GEAR WAS EXTENDED AND BACKED UP WITH NR 2 SYSTEM (PROCEDURE A) L/G SELECTOR C/B TRIPPED AGAIN (MEM). FOUND SHORTED CANNON PLUG AT 16G1. REPLACED CANNON PLUG WITH SERVICEABLE UNIT. OPERATIONAL CHECKS GOOD ON SEVERAL CYCLES IAW AMD MM 32-30. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A7EU 1998111301017 19981113 01017 NE 1998 11 13 AALA981689 2 19980913 A 7314 384300 PUMP DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217C 52053 NE NR 1 ENGINE FAILED A AALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 SW 07 469AA 8508 49599 RDU - FLT 1547 - EN ROUTE BOS-MCO - AT 35,000 FT LEFT INLET LOW FULE PRESSURE LIGHT ILLUMINATED. LEFT FUEL QTY DECREASE D NORMALLY. FIFTEEN MINUTES LATER LEFT ENGINE FLAMED OUT. RESTARTED ENGINE WITH X FEED OPEN. CREW DECLARED AN EMERGEN CY, AIR INTERRUPTED, AND LANDED RDU WITHOUT INCIDENT. REPLACED LEFT ENGINE FUEL PUMP AND FUE CONTROL. PERFORMED LEAK A ND TRIM CHECKS. REPLACED LEFT ENGINE FUEL PUMP AND FUEL CONTROL. PERFORMED LEAK AND TRIM CHECKS. REPLACED FORWARD AND AFT NR 1 FUEL TANK BOOST PUMPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998111301018 19981113 01018 NE 1998 11 13 98ZZZM822 2 19980730 A 8530 327627 VALVE DOUG DC6 DC6B 3021712 WP PWA R2800 R2800* 52026 NE NR 1 ENGINE BROKEN A TALA E ENGINE SHUTDOWN E Y J VIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 SO 19 841TA 44891 GVP7735 WHILE EN BOUND TO SANTO DOMINGO, NR 1 ENGINE BACKFIRED CONTINUOUSLY, ENGINE ANALYZER SHOWED R-8 S/S AT 1225. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. LANDING IN SANTO DOMINGO WITHOUT INCIDENT. REPLACED NR 8 CYLINDER IN NR 1 ENGINE. ENGI NE RUNUP CHECKED OK. (M) 2 L 7 4 4R 4 R 6A4 5E8 1998111301019 19981113 01019 NE 1998 11 13 SABA980046 2 19980917 A 7261 OIL SYSTEM DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT ENGINE REQ'D SERVICE A SABA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 33 820PH 063 FLT 5174 - AGS-CLT - AFTER TAKEOFF, PILOT REPORTED LOW OIL INDICATION ON THE LEFT ENGINE. AIRCRAFT RETURNED TO AGS AND MADE A SAFE LANDING. NO INFLIGHT EMERGENCY WAS DECLARED. MAINTENANCE SERVICED THE ENGINE WITH OIL. ENGINE RUN AND OPS CHECKED GOOD. A TEST FLIGHT WAS PERFORMED AND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1998111301020 19981113 01020 NE 1998 11 13 PLGA98031A 2 19980831 A 7260 DETECTOR SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE CONTAMINATED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 355BE 340B209 BOS - FLT 4275 - AFTER TAKEOFF, THE LEFT ENGINE CHIP DETECTOR WARNING ILLUMINATED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED DETECTOR AND GROUND RAN ENGINE PER GE CMM. ALL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998111301021 19981113 01021 NE 1998 11 13 USAASB98224 2 19980831 A 7321 9375M82P04 SENSOR BOEING 737 737301 1384611 NM GE CFM56 CFM56* 13802 NE NR 2 ENGINE FAILED A USAA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 EA 19 300AU 22493 23228 CHS - FLT 888 - AT FL370 WITH AUTOPILOT/AUTOTHROTTLES ON, THE NR 2 ENGINE POWER STARTED TO DECREASE WITH THROTTLES SPLIT TWO INCHES. TURNED AUTOTHROTTLE OFF AND POWER BECAME STABLE. TURNED AUTOTHROTTLES BACK ON AND POWER STARTED TO DECREA SE AGAIN. TURNED PMC OFF AND ENGINE STARTED TO WIND ALL THE WAY DOWN. TURNED PMC BACK ON AND MADE DECISION TO DIVERT T O CHS. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. NO ENGINE FLAMEOUT OCCURED. MAINTENANCE RI GGED THE NR 2 ENGINE FOR IDLE SPEED AND PART POWER TRIM IN ASSOCIATION WITH JOB CARD. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED NR 2 ENGINE T2 HYDROMECHANICAL SENSOR FOR INTERMITTENT OPERATION. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 1998111301022 19981113 01022 NE 1998 11 13 EISA98243 2 19980930 A 7412 103538754 IGNITER BOX BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE FAILED A EISA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 07 308AS 22002 NR 1 ENGINE FLAMED OUT IN FLIGHT. UNABLE TO RESTART. AIR TURN BACK TO BGY. REMOVED AND REPLACED IGNITOR BOX, FUEL CON TROL. FUEL PUMP, RAN ENGINE AND TRIMMED. CHECKS NORMAL. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998111301023 19981113 01023 NM 1998 11 13 98ZZZM823 1 19980930 A 4930 1436023 FUEL CONTROL BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE FAILED A EISA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 07 308AS 55501 22002 NR 1 ENGINE FLAMED OUT IN FLIGHT. UNABLE TO RESTART. AIR TURN BACK TO BGY. REMOVED AND REPLACED IGNITOR BOX, FUEL CON TROL. FUEL PUMP, RAN ENGINE AND TRIMMED. CHECKS NORMAL. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998111301024 19981113 01024 NM 1998 11 13 98ZZZM824 1 19980930 A 2822 384300 IGNITER BOX BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 1 ENGINE FAILED A EISA A UNSCHED LANDING X J ENGINE FLAMEOUT WARNING INDICATION CR CRUISE 1 SW 07 308AS 5823 22002 NR 1 ENGINE FLAMED OUT IN FLIGHT. UNABLE TO RESTART. AIR TURN BACK TO BGY. REMOVED AND REPLACED IGNITOR BOX, FUEL CON TROL. FUEL PUMP, RAN ENGINE AND TRIMMED. CHECKS NORMAL. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998111301025 19981113 01025 WP 1998 11 13 SABA980054 2 19981010 A 7320 39423091 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A SABA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 33 941AE 3431 P6432C 941 RDU - FLT 9142 - NTS TEST FLIGHT UNSUCCESSFUL COULD NOT RELIGHT NR 2 ENGINE. REMOVED AND REPLACED RT FUEL SHUTOFF VALVE IAW GARRETT MM ATA 73-00. GROUND RUNS OPS CHECKED GOOD. LEAK CHECKED GOOD. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998111301026 19981113 01026 NE 1998 11 13 SABA980052 2 19981008 A 7261 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 LACK OF LUBE A SABA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 SO 33 820PH 063 PGV - FLT 5212 - NR 1 ENGINE LOW PRESSURE WARNING LIGHTS DURING TAKEOFF ROLL. OIL PRESSURE FLUCTUATES LOW BETWEEN 45 AN D 55 PSI DURING NORMAL PRESSURE DURING STATIC RUNUP OIL PTY CHECKS NORMAL. INSPECTED NR 1 ENGINE AND FOUND OIL LEVEL LO W. SERVICED ENGINE OIL IAW DH-8 MMCH 12-10, RUN UP OPS CHECKS GOOD. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1998111301027 19981113 01027 NE 1998 11 13 PLGA980814A 2 19980830 A 7321 6071T20P16 DECU SAAB SF340 340B 7860101 EU GE CT7TP CT75A 30030 NE RT ENGINE MALFUNCTIONED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 362BE ECDT1574 340B291 BOS - FLT 4257 - AFTER TAKEOFF, THE RIGHT ENGINE ITT STARTED TO FLUCTUATE. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE DECU. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998111301028 19981113 01028 NM 1998 11 13 USAA980446 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 706 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 706 STRINGER 9L. REPAIRED PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998111301029 19981113 01029 NM 1998 11 13 USA980469 1 19980930 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH AT CLIP NUTS STATION 344 FLOORBEAM BL 0 LBL 4 2. CORROSION TASK NR C53-107-01. FABRICATED REPAIR PER TR 53-10-13 'T' CAP. (M) 2 L 7 2 4F A16WE 1998111301030 19981113 01030 NM 1998 11 13 USAA980445 1 19980930 A 5320 69353523 CLIP BOEING 737 7372B7 1384560 NM BS 500B CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK STATION 500B STRINGER 10L STRINGER TIE CLIP. REPAIRED PER SRM 51-10-1 AND EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998111301031 19981113 01031 NM 1998 11 13 USAA980444 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STRINGER TIE CLIP STATION 616 S 1. REPAIRED PER EO 539 3G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998111301032 19981113 01032 NM 1998 11 13 USAA980439 1 19980930 A 5320 654581945 ANGLE BOEING 737 7372B7 1384560 NM BS 259 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK IN RADIUS SUPPORT BRACKET FOR NLG AT BEAM VERT FLANGE STA TION 259 WL 192 ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1998111301033 19981113 01033 NM 1998 11 13 USAA980438 1 19980930 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 962 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK LOWER FORWARD CORNER LEFT AFT ENTRY DOOR CUTOUT S TATION 962 WL 208 SKIN. INSTALLED TRIPLER PER SRM 53-30-03 FIG 24. (M) 2 L 7 2 4F A16WE 1998111301034 19981113 01034 NM 1998 11 13 USAA980437 1 19980930 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 987 DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH LONG .875 INCH WIDE AND .09375 INCH DEEP DENT BETWEEN STATION 9 87.5 AND STATION 1006 STRINGER 17L SKIN. FABRICATED DOUBLER PER SRM 53-30-3 FIG 61. (M) 2 L 7 2 4F A16WE 1998111301035 19981113 01035 NM 1998 11 13 USAA980436 1 19980920 A 5330 SKIN BOEING 737 737201 1384454 NM BS 947 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 40679 22868 TPA - DURING CX-4 CHECK EDDY CURRENT, FOUND A .187 INCH CRACK UPPER HINGE CUTOUT AFT ENTRY DOOR SKIN STATION 947 STRINGE R 11L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 21A. (M) 2 L 7 2 4F A16WE 1998111301036 19981113 01036 NM 1998 11 13 USAA980434 1 19980920 A 5330 SKIN BOEING 737 737201 1384454 NM BS 947 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 233US 48082 22273 CLT - DURING PCI 1703 CHECK VISUAL AND HFEC, FOUND A .375 INCH LONG CRACK FUSELAGE STATION 947 RIGHT AFT SERV DOOR LOWER HINGE CUTOUT OF SKIN. INSTALLED DOUBLER PER EA62590. (M) 2 L 7 2 4F A16WE 1998111301037 19981113 01037 NM 1998 11 13 USAA980433 1 19980924 A 5240 6545871523 SKIN BOEING 737 737201 1384454 NM SERVICE DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 42998 22751 TPA - DURING CX-3 CHECK VISUAL, VERIFIED BY EDDY CURRENT INSPECTION, FOUND A .25 INCH CRACK IN FWD SERVICE DOOR EXTERIOR SKIN LOWER HINGE CUTOUT AFT UPPER CORNER. INSTALLED DOUBLER PER TR 52-40-03 A. (M) 2 L 7 2 4F A16WE 1998111301038 19981113 01038 NM 1998 11 13 USAA980483 1 19981011 A 5320 69353521 CLIP BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 40876 22866 CLT - DURING PCI 1227 VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 380 STRINGER 26L TIE CLIP. REMOVED AND REPLACED PER SRM 51-10-3. (M) 2 L 7 2 4F A16WE 1998111301039 19981113 01039 NM 1998 11 13 USAA980482 1 19981008 A 5210 65528732 SKIN BOEING 737 737201 1384454 NM PAX DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 43660 22755 TPA - DURING WALK AROUND VISUAL INSPECTION, FOUND A 1 INCH CRACK IN EXTERIOR SKIN AFT UPPER CORNER OF AFT ENTRY DOOR SKI N. INSTALLED DOUBLER PER SRM 52-00-03 FIG 5. (M) 2 L 7 2 4F A16WE 1998111301040 19981113 01040 NM 1998 11 13 USAA980495 1 19981009 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 388 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 288AU 38627 23135 LCQ - DURING PAINT VISUAL INSPECTION, FOUND A 2 INCH GOUGE STATION 388 BETWEEN STRINGER 19L AND 20L EXTERIOR SKIN. INST ALLED DOUBLER PER SRM 53-30-03 FIG 1. (M) 2 L 7 2 4F A16WE 1998111301041 19981113 01041 NM 1998 11 13 USAA980496 1 19981015 A 5330 SKIN BOEING 737 737201 1384454 NM BS727/747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 247US 43482 22754 CLT - DURING J2-W CHECK VISUAL INSPECTION, FOUND A 4.5 INCH CRACK BELOW STRINGER 17R BETWEEN STATION 727B AND STATION 74 7 FUSELAGE SKIN. INSTALLED DOUBLER AND FILLER PER EA 62685. (M) 2 L 7 2 4F A16WE 1998111301042 19981113 01042 NM 1998 11 13 USAA980480 1 19981004 A 5330 SKIN BOEING 737 737201 1384454 NM BS 787 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 251AU 43167 22757 TPA - DURING METROJET CONVERSION VISUAL INSPECTION VERIFIED WITH EDDY CURRENT, FOUND A 1.25 INCH CRACK STATION 787 STRIN GER 18L ON SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998111301043 19981113 01043 WP 1998 11 13 ORJA98239 1 19980822 A 5320 COVER PLATE DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON LEFT AND RIGHT COVER STRIPS AT CENTER FLOORBOARD STATION 160 TO 200. FABRICATED NEW STRIPS IAW DC9 SRM 51-10-2 TREATED AND PRIMED IAW DC0 SRM 51-10-3 AND INSTALLED IAW MD-80 MM 20-20-00. (M) 2 L 7 2 4F A6WE 1998111301044 19981113 01044 WP 1998 11 13 ORJA98247 1 19980823 A 5320 46190211 SUPPORT DOUG DC9 DC982 3022082 WP BS 1183-1338 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 3 CORROSION ON PNEUMATIC DUCT SUPPORT RODS IN AFT CARGO, LEFT SIDEWALL STATION 1183 TO 1338. REPLACED 5 JOINT ASS EMBLIES FROM STATION 1183 TO 1338 FOR PNEUMATIC DUCT IAW MD80 SRM 36-00-00. (M) 2 L 7 2 4F A6WE 1998111301045 19981113 01045 CE 1998 11 13 98ZZZM825 1 19981023 A 2822 1143890425 PUMP BEECH 1900 1900D 1154162 CE RT NACELLE LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 838CA 6069 B839 UE34 FUEL LEAK RIGHT ENGINE NACELLE. INSPECTION OF AIRCRAFT FOUND RIGHT ENGINE LOW PRESSURE FUEL BOOST PUMP LEAKING. REPLAC ED PUMP IAW MM CHAPTER 73-10-00. (M) 2 L 7 2 4T RT A24CE 1998111301046 19981113 01046 WP 1998 11 13 GTIA9800114 1 19981018 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 DTW - FOUND AFT SECTION EMERGENCY LIGHTS NOT WORKING. FOUND WIRES TO BE SHORTED IN SEVERAL PLACES. SPLICED IN NEW SPLI CES IAW DC-9 MM 20-50-1. (M) 2 L 7 2 4F A6WE 1998111301047 19981113 01047 WP 1998 11 13 GTIA9800117 1 19981015 A 2560 SLIDE DOUG DC9 DC931 3022065 WP CABIN LOOSE A GTIA K NONE O OTHER IN INSP/MAINT 1 GL 23 928ML 47326 MYR - FLT 381 - SLIDE PACK CAME LOOSE FROM GALLEY DOOR. REINSTALLED SLIDE PACK COVER AND SLIDE ON GALLEY DOOR RIGHT SID E OF AIRCRAFT. (M) 2 L 7 2 4F A6WE 1998111301048 19981113 01048 WP 1998 11 13 GTIA9800116 1 19981017 A 3350 BULB DOUG DC9 DC931 3022065 WP ROW 2 FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 DTW - OVERHEAD EMERGENCY LIGHT SYSTEM LEFT AND RIGHT LIGHTS INOPERATIVE AT ROW 2, LEFT AT ROW 4, AND RIGHT AT ROW 6. RE MOVED AND REPLACED LAMPS, OPERATIONAL CHECK NORMAL IAW DC-9 MM CHAPTER 33-53-0. (M) 2 L 7 2 4F A6WE 1998111301049 19981113 01049 NM 1998 11 13 F3LA98192 1 19981025 A 3350 BULB BOEING 737 7373M8 1384615 NM CABIN FAILED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED VARIOUS SECTIONS OF FLOOR PROXIMITY LIGHTING INOPERATIVE. MAINTENANCE REPLACED LAMPS AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1998111301050 19981113 01050 NM 1998 11 13 F3LA98191 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 986 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON UPPER CAP OF FLOORBEAM AT BS 986.5, RBL 40 TO LBL 40, MAIN CABIN F LOOR. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-60-51, SRM 51-40-2, SRM 51 -10-1 AND EA B737-53-068. (M) 2 L 7 2 4F RT A16WE 1998111301051 19981113 01051 NM 1998 11 13 F3LA98190 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 279-295 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON FLOOR SUPPORT BETWEEN BS 279 AND BS 295 AT RBL 31, MAIN CABIN FLOO R. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-02, SRM 51-10-01 AND EA B7 37-53-071. (M) 2 L 7 2 4F RT A16WE 1998111301052 19981113 01052 NM 1998 11 13 F3LA98189 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 277-295 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON FLOOR SUPPORT BETWEEN BS 277 AND BS 295 AT RBL 10.85, MAIN CABIN F LOOR. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-2 AND EA B737-53-071. ( M) 2 L 7 2 4F RT A16WE 1998111301053 19981113 01053 NM 1998 11 13 F3LA98188 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 320 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT BS 320, LBL 11.10, MAIN CABIN FLOOR. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-3, SRM 51-10-1 AND SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1998111301054 19981113 01054 NM 1998 11 13 F3LA98187 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 312-328 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT BS 312 TO 328 LBL 11.10, MAIN CABIN FLOOR. MAINT ENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-1, SRM 51-40-2 AND EA B737-53-071. (M) 2 L 7 2 4F RT A16WE 1998111301055 19981113 01055 NM 1998 11 13 F3LA98186 1 19981025 A 5320 INTERCOSTAL BOEING 737 7373M8 1384615 NM BS 946 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON INTERCOSTAL UPPER CAP, BS 946 TO BS 967 LBL 18, MAIN CABIN FLOOR. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-51, SRM 51-20-01 AND SRM 51-4 0-2. (M) 2 L 7 2 4F RT A16WE 1998111301056 19981113 01056 NM 1998 11 13 F3LA98184 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 950 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK, INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT BS 950, LBL 18 TO 50, MAIN CABIN FLOOR. MAINTEN ANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-60-51, SRM 51-30-1 AND SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1998111301057 19981113 01057 NM 1998 11 13 F3LA98183 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHEC, INSPECTION REPORTED CORROSION ON UPPER SURFACE OF FLOOR SUPPORT BS 947 TO BS 927. MAINTENANCE REMO VED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-1, SRM 51-40-2 AND EA B737-53-069. (M) 2 L 7 2 4F RT A16WE 1998111301058 19981113 01058 NM 1998 11 13 F3LA98182 1 19981025 A 5320 SUPPORT BOEING 737 7373M8 1384615 NM BS 948 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK, INSPECTION REPORTED FLOOR SUPPORT CORRODED ON UPPER CAP AT BS 948, LBL 18 TO 24. MAINTENANCE REMO VED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-60-51, SRM 51-40-2 AND EA B737-53-069. (M) 2 L 7 2 4F RT A16WE 1998111301059 19981113 01059 NM 1998 11 13 F3LA98181 1 19981025 A 5320 WEB BOEING 737 7373M8 1384615 NM BS 986 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CUSP WEB CRACKED AT STATION 986, LT INBOARD CORNER. MAINTENANCE REMOVED DAMAGE D AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-70-13, FIG 2 SRM 51-70-13, FIG 1 SRM 51-40-2 AND EA B737-53 -070. (M) 2 L 7 2 4F RT A16WE 1998111301060 19981113 01060 NM 1998 11 13 F3LA98180 1 19981026 A 5320 SUPPORT BOEING 737 7373M8 1384615 NM BS 947 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON FLOOR SUPPORT AT BS 947, RBL 17. MAINTENANCE REMOVED CORRODED ARE AS, FABRICATED REPLACEMENT PARTS AND REPAIRED PER EA 1489-EG0024 (B737-53-069), ARM 51-40-2 AND SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1998111301061 19981113 01061 NM 1998 11 13 F3LA98179 1 19981025 A 5320 INTERCOSTAL BOEING 737 7373M8 1384615 NM BS 946-968 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTEC CORROSION ON INTERCOSTAL UPPER CAP RBL 50, BS 946 TO BS 966, MAIN CABIN FLOOR. MAINTENANCE FABRICATED INTERCOSTAL PER DRAWING 65C33367 AND INSTALLED PER SRM 51-40-2 AND 51-20-01. (M) 2 L 7 2 4F RT A16WE 1998111301062 19981113 01062 NM 1998 11 13 F3LA98178 1 19981025 A 5315 FLOORBEAM BOEING 737 7373M8 1384615 NM BS 291 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON FLOORBEAM 291.5, LBL 20 TO RBL 40 (MAIN CABIN FLOOR). MAINTENANCE REMOVED CORROSION AND DAMAGED UPPER CHORD, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-10-51 AND 51-40-2. (M) 2 L 7 2 4F RT A16WE 1998111301063 19981113 01063 1998 11 13 98ZZZM826 4 19981020 A 3414 2719193027 INDICATOR SWRNGN SA227 SA227AC 8780603 SW COCKPIT INOPERATIVE A MEJA D RETURN TO BLOCK O OTHER CL CLIMB 1 SW 17 358AE 230628 AC688 AFTER TAKEOFF FROM LCH, THE LEFT AIRSPEED INDICATOR WAS INOPERATIVE. THE AIRCRAFT RETURNED TO LCH AND MAINTENANCE REMOV ED AND REPLACED THE LEFT AIRSPEED INDICATOR WITH A REPAIRED UNIT. MAINTENANCE PERFORMED A PITOT STATIC LEAK CHECK AND L EAK RATE WAS FOUND TO BE WITHIN LIMITS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998111301064 19981113 01064 NM 1998 11 13 TSAA9873556 1 19981023 A 7331 8TJ95GAB POWER SUPPLY BOEING 737 737282 13844AT NM FUEL FLOW FAILED A TSAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 13 824AL 23045 FLT 78 - LIH-HNL - ON TAKEOFF ROLL, APPROX 80 KTS, BOTH NR 1 AND NR 2 FUEL FLOW INDICATORS STARTED CYCLING BETWEEN 8,000 PPH DOWN TO 500 TO 1000 PH. ALL OTHER ENGINE PARAMETERS WERE NORMAL. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED A ND REPLACED FUEL FLOW POWER SUPPLY. GROUND CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998111301065 19981113 01065 NM 1998 11 13 TSAA9833554 1 19981022 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 1 AND NR 6 POSITION FLOOR EMERGENCY PROXIMITY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F RT A16WE 1998111301066 19981113 01066 NM 1998 11 13 TSAA9833555 1 19981022 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1998111301067 19981113 01067 NM 1998 11 13 F3LA98172 1 19981014 A 3397 WIRE BOEING 737 737201 1384454 NM ROW 17 LOOSE A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 207AU 19423 PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 17 INOPERATIVE. MAINTENANCE REPAIRED W IRING AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998111301068 19981113 01068 NM 1998 11 13 F3LA98171 1 19981013 A 8012 SOLENOID BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A F3LA A E UNSCHED LANDING ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 NM 03 217US 20215 FLT 658 - DEN - AIR TURN BACK, UPON CLIMB-OUT FROM DEN, FLIGHT CREW REPORTED NR 1 ENGINE START VALVE 'OPEN' LIGHT ILLUMI NATED. NR 1 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO DEN WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE START VALVE SOLENOID AND CHECKED OK. (M) 2 L 7 2 4F A16WE 1998111301069 19981113 01069 NM 1998 11 13 F3LA98177 1 19981026 A 5320 WEB BOEING 737 7373M8 1384615 NM BS 800 CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - FLT 303 - DURING C-CHECK INSPECTION, REPORTED CRACK IN DOOR FRAME WEB, BS 800 RT SIDE FORWARD OF AFT CARGO DOOR FR AME. MAINTENANCE FABRICATED AND INSTALLED NEW WEB PER SRM 51-30-1, SRM 51-10-2 AND SRM 51-40-2. (M) 2 L 7 2 4F RT A16WE 1998111301070 19981113 01070 NM 1998 11 13 F3LA98176 1 19981025 A 5753 SKIN BOEING 737 7373M8 1384615 NM TE FLAP CRACKED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED LT INBOARD MID FLAP, OUTBOARD LEADING EDGE, CRACKED NEXT TO WASTE GATE ACTIVATI ON ROD. MAINTENANCE REPAIRED CRACK (.25 INCH LONG) PER SRM 57-43-02 AND EA B737-57-034. (M) 2 L 7 2 4F RT A16WE 1998111301071 19981113 01071 NM 1998 11 13 F3LA98174 1 19981025 A 5320 BEAM BOEING 737 7373M8 1384615 NM BS 946 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON TRANSVERSE BEAM, BS 946 TO BS 986, AT R2 DOOR, MAIN CABIN FLOOR. M AINTENANCE FABRICATED REPLACEMENT TRANSVERSE BEAM AND REPAIRED PER SRM 53-60-15 AND SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1998111301072 19981113 01072 NM 1998 11 13 F3LA98173 1 19981012 A 2780 BOLT BOEING 737 73736Q 1384409 NM LE FLAP MISSING A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 307FL 28760 UPON ARRIVAL, FLIGHT CREW REPORTED NR 2 LEADING EDGE FLAP INDICATOR SHOWED FLAP IN EXTENDED MODE AT ALL SETTINGS. MAINT ENANCE INSTALLED MISSING BOLT AND NUT ASSY AT ATTACH FITTING FOR FLAP AND TAIL GATE ASSY AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1998111301073 19981113 01073 NM 1998 11 13 F3LA98175 1 19981025 A 5320 CLIP BOEING 737 7373M8 1384615 NM BS 986 CORRODED A F3LA K NONE O OTHER IN INSP/MAINT 1 NM 03 303FL 25039 PHX - DURING C-CHECK INSPECTION REPORTED CORROSION ON TIE CLIP AT BS 986, STRINGER 28L. MAINTENANCE FABRICATED NEW CLIP PER DRAWING 69-35364 AND INSTALLED PER SRM 53-00-53 AND 51-40-2. (M) 2 L 7 2 4F RT A16WE 1998111301074 19981113 01074 NM 1998 11 13 MZZA98220 1 19981008 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING HALF CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD AFT FLAP UPP ER SKIN EXISTING REPAIRED AT WBS 177. THE DAMAGED EXISTING REPAIR DOUBLER (5.125 INCH BY 3 INCH IN SIZE) WAS REMOVED AN D REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F RT A3WE 1998111301075 19981113 01075 NM 1998 11 13 MZZA98219 1 19981008 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS ON LEFT WING T/E INBOARD AFT FLAP LOWER S KIN WBL 205. THE DAMAGED SKIN 2.625 INCH DIAMETER WS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F RT A3WE 1998111301076 19981113 01076 NM 1998 11 13 MZZA98218 1 19981008 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD AFT FLAP L OWER SURFACE EXISTING REPAIRED DOUBLER AT WBL 105. THE DAMAGED EXISTING REPAIRED DOUBLER (14.3125 INCH BY 5 INCH IN SIZ E) WAS REMOVED AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F RT A3WE 1998111301077 19981113 01077 NM 1998 11 13 MZZA98215 1 19981006 A 5320 WEB BOEING 727 727277 138408S NM TORQUE BOX OIL CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RT SIDE AFT AIRSTAIR TORQUE BOX V ERTICAL WEB BETWEEN BS 1233 AND BS 1253. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1998111301078 19981113 01078 NM 1998 11 13 MZZA98214 1 19981006 A 5320 WEB BOEING 727 727277 138408S NM TORQUE BOX CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON RIGHT SIDE AFT AIRSTAIR TORQUE BO X VERTICAL WEB BETWEEN BS 1323 AND BS 1333. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEME NT STIFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1998111301079 19981113 01079 NM 1998 11 13 MZZA98212 1 19981006 A 5320 WEB BOEING 727 727277 138408S NM TORQUE BOX OIL CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX VERTICAL WEB BETWEEN BS 1323 AND BS 1333. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMEN T STIFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1998111301080 19981113 01080 NM 1998 11 13 MZZA98211 1 19981003 A 3350 S106 BATTERY BOEING 727 727277 138408S NM CABIN DISCHARGED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING HALF D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, PASSENGER CABIN EMERGENCY LIGHT BATTERIES WERE FOUND INOPE RATIVE. THE BATTERIES, P/N S106, WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL TEST FOUND SATISFACTORY. (M) 2 L 7 3 4F RT A3WE 1998111301081 19981113 01081 WP 1998 11 13 98ZZZM827 1 19980929 A 3246 3430020629 BEARING CVAC 340 34031 2422704 WP RT MLG DESTROYED A ERAA K NONE O OTHER LD LANDING 1 AL 03 569JA 287 9035005 69 RIGHT MLG OUTBOARD WHEEL ASSY DEPARTED AIRCRAFT ON LANDING ANC BOTH WHEEL BEARINGS HAD DISINTIGRATED. NO EVIDENCE OF HE AT DISTRESS. GREASE WAS FOUND IN BEARING CAVITY AND ON REMAINING ROLLERS. BEARINGS INSTALLED NEW TWO MONTHS EARLIER. S USPECT DAMAGED OR DEFECTIVE BEARING. 2 L 7 2 4R 6A6 1998111301082 19981113 01082 1998 11 13 NOCA2298 4 19981005 A 2565 SLIDE BOEING 757 75723A 1384967 NM PAX DOOR MALFUNCTIONED A NOCA K NONE O OTHER IN INSP/MAINT 1 EA 15 757NA 24567 ON CREW TRAINING OF EMERGENCY EVACUATION, THE R-3 DOOR EVACUATION SIDE DID NOT DEPLOY AUTOMATICALLY ON DOOR OPENING, IT HAD TO BE MANUALLY DEPLOYED. ESCAPE SLIDE PART NR D31041, S/N 0474 WAS SENT TO AIR CRUISERS FOR INSPECTION AND EVALUATI ON. INSPECTION REVEALED THAT ALL THE SLIDE SPECIFICATIONS AND PARAMETERS FOR AN AUTOMATIC DEPLOYMENT WERE FOUND TO BE N ORMAL. BASED ON AIRCRUISERS REPORT NO SPECIFIC DETERMINATION COULD BE MAD OF THE CAUSE FOR THE FAILURE TO AUTOMATICALLY DEPLOY. (M) 2 L 7 2 4F RT A2NM 1998111301083 19981113 01083 EU 1998 11 13 RAIA981006 1 19981009 A 5610 1379628C402 WINDSCREEN BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA B EMER. DESCENT O OTHER CR CRUISE 1 CE 03 340TE 12836 939 FLT 7479 - LEX - F/O'S FORWARD WINDSCREEN SHATTERED. MAINTENANCE REPLACED WINDSCREEN. (M) 2 L 7 2 4T RT A56EU 1998111301084 19981113 01084 EU 1998 11 13 SIMA982791 1 19981006 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 341SB 18315 340B341 LFT - 5032 - CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE. SWITCH WAS LEFT IN ARMED POSITION. REMOVED AND REPLACED EMERGEN CY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998111301085 19981113 01085 EU 1998 11 13 98ZZZM828 1 19981006 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 341SB 15490 340B341 LFT - 5032 - CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE. SWITCH WAS LEFT IN ARMED POSITION. REMOVED AND REPLACED EMERGEN CY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998111301086 19981113 01086 EU 1998 11 13 98ZZZM829 1 19981006 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 341SB 19174 340B341 LFT - 5032 - CABIN EMERGENCY LIGHTS DO NOT ILLUMINATE. SWITCH WAS LEFT IN ARMED POSITION. REMOVED AND REPLACED EMERGEN CY LIGHT POWER SUPPLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998111301087 19981113 01087 EU 1998 11 13 SIMA982802 1 19981007 A 3320 8SS00558800 TRANSFORMER AEROSP ATR72 ATR72212 EU SEAT 6CD FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 348AE 349 DFW - FLT 3625 - AIRCRAFT RETURNED TO DFW DUE TO ODOR OF SMOKE IN THE CABIN. EMEGENCY WAS DECLARED. AIRCRAFT LANDED SA FELY. REMOVED AND REPLACED SHORTED OUT TRANSFORMER AT SEAT 6CD PSU PANEL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1998111301088 19981113 01088 EU 1998 11 13 UF6A980907 1 19980917 A 3350 58786 CABLE ASSY BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 851AW 2020 ORD - FLT 5705 - AFT SECTION OF FLOOR PROXIMITY LIGHTING INOP. MAINTENANCE REPLACED CABLE ASSY. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1998111301089 19981113 01089 NM 1998 11 13 USAASB98262 1 19981007 A 3350 20121 CHARGER ASSY BOEING 737 737401 1384701 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 417US 23984 ALB - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR, FORWARD AND AFT EMERGENCY EVACUATION LIGHTS INOP ALONG WITH THE RIGHT A FT SERVICE DOOR SLIDE EVACUATION LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY FOR THE LEFT AFT ENT RY DOOR, FORWARD AND AFT EVACUATION LIGHTS AND SPLICED A BROKEN WIRE WHICH WAS FOUND IN THE OVERHEAD FOR THE RIGHT AFT S ERVICE DOOR SLIDE EVACUATION LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998111301090 19981113 01090 NM 1998 11 13 USAASB98261 1 19981007 A 3350 15AT17 SWITCH BOEING 737 7372B7 1384560 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 284AU 23131 ALB - MAINTENANCE FOUND THE EMERGENCY LIGHTS TESTING INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE S7 EMERGENCY LIGHT SWITCH AT THE P5 PANEL. OPERATIONAL CHECK GOOD PER MM 33-51-11. (M) 2 L 7 2 4F A16WE 1998111301091 19981113 01091 NM 1998 11 13 GAIA9890 1 19981008 A 3350 37067001 BATTERY PACK GRIMES BOEING 727 727251 138408H NM FS 289 DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 279US 1293 21158 EMERGENCY EXIT LIGHT IN COCKPIT DOES NOT ILLUMINATE. REMOVED AND REPLACED TWO BATTERIES. OPERATIONAL CHECK OK. AIRCRA FT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998111301092 19981113 01092 NM 1998 11 13 TSAA9833545 1 19980921 A 5320 INTERCOSTAL BOEING 737 7372M6C 1384708 NM BS 857 DENT A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 DENT NOTED AROUND RIVET AT BS 857 ALONG STRINGER 19R A/Y RATIO =.75/.048=15625. INSTALLED FABRICATED INTERCOSTAL AND RE PAIRED IAW SRM 53-30-3. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998111301093 19981113 01093 NM 1998 11 13 TSAA9833541 1 19981006 A 3350 6013211 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED FORWARD ENTRANCE EXIT IDENTIFIER BATTERY DUE TO LOW VOLTAGE. OPERATIONAL CHECK FOUND SATISFACTORY. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998111301094 19981113 01094 NM 1998 11 13 TSAA9833548 1 19980921 A 5511 SPAR BOEING 737 7372M6C 1384708 NM HORIZ STABILIZER CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 HORIZONTAL STAB UPPER RIGHT FRONT SPAR CHORD EXFOLIATED. REPAIRED PER ECO 2201R1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998111301095 19981113 01095 NM 1998 11 13 TSAA9833550 1 19980921 A 5531 SPAR BOEING 737 7372M6C 1384708 NM VERTICAL STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 VERTICAL STABILIZER REAR SPAR SKIN BULGING DUE TO CORROSION. REPAIR PER ECO 2509 R5. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT A16WE 1998111301096 19981113 01096 NM 1998 11 13 TSAA9833549 1 19980921 A 5531 SPAR BOEING 737 7372M6C 1384708 NM VERTICAL STAB CORRODED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 VERTICAL STABILIZER REAR SPAR SHOWS SIGNS OF EXFOLIATION. REPAIRED PER ECO 2509 R5. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998111301097 19981113 01097 NM 1998 11 13 TSAA9833526 1 19980930 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED FLOOR EMERGENCY LIGHT BATTERIES. SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998111301098 19981113 01098 NM 1998 11 13 TSAA9833527 1 19980930 A 3350 6013211 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED BATTERY PACK FROM THE AFT DOOR EMERGENCY SLIDE LIGHT. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998111301099 19981113 01099 NM 1998 11 13 MASA98186 1 19981009 A 3350 0201812003 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 5293 - PHX-YUM - PRIOR TO DEPARTURE, CREW NOTICED ONE OVERHEAD EMERGENCY LIGHT INOP. MAINTENANCE RESECURED LOOSE CO NNECTION, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998111301100 19981113 01100 WP 1998 11 13 HALA9800346 1 19981014 A 3350 P4010049 BATTERY DOUG DC9 DC951 3022051 WP ROW 6-10 DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 661HA 47796 HNL - FLT 106 - EMERGENCY LIGHTS OVERHEAD, INOP ROWS 6-10. REMOVED AND REPLACED BATTERY, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998111301101 19981113 01101 EU 1998 11 13 98ZZZM830 1 19980108 A 7120 YOKE BAG BAE146 BAE146200A 1500266 EU NR 4 PYLON CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 156TR E2156 NR 4 PYLON MOUNT YOKE HAS THE PYLON DRAIN LINE CHAFING ON ITS RIGHT SIDE TOP SURFACE. REMOVED NR 4 PYLON ENGINE FRONT M OUNT YOKE. INSPECTED AND FOUND CHAFEAGE TO BE WITHIN 146 SRM 54-50-41 LIMITS. BLENDED AREA AND REINSTALLED MOUNT YOKE IAW MM 71-10-11. (M) 2 H 7 4 4F RT A49EU 1998111301102 19981113 01102 EU 1998 11 13 98ZZZM831 1 19980911 A 3231 BRACKET BAG BAE146 BAE146200A 1500266 EU MLG DOOR DAMAGED A A6WA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 31 179US E2041 REF EO E92/067/632 REV A, RIGHT HINGE BRACKET HAS DEEP IMPACT DAMAGE AROUND BOLT HOLE AND CORROSION IAW ITEM 10 SECTION I. REMOVED RIGHT HINGE BRACKET WRK 1032. INSTALLED SERVICEABLE HINGE BRACKET WITH REPLACEMENT HARDWARE AS REQUIRED. ( M) 2 H 7 4 4F RT A49EU 1998111301103 19981113 01103 NM 1998 11 13 EISA98249 1 19981015 A 3350 LIGHT BOEING 727 7272A7 138407K NM COCKPIT INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 310NE 10033 20241 EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOPERATIVE. GENERATED FROM MAINTENANCE REPORT. REMOVED AND REPLACED EMERGENCY LIGHT, OPS CHECK GOOD PER MM 33-50. (M) 2 L 7 3 4F A3WE 1998111301104 19981113 01104 NM 1998 11 13 GAIA98106 1 19981023 A 5531 652298771 CHORD BOEING 727 727223 1384074 NM LT STAB CORROSION A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6834 20187 THE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. LEFT STABILIZER, UPPER TRAILING EDGE CHO RD HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGED T/E UPPER CHORD, PER 727 SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998111301105 19981113 01105 NM 1998 11 13 GAIA98105 1 19981023 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6834 20187 THE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. CORROSION ON FRAME STATION 1050, LBL 65, WL 208. REMOVED CORROSION AREA. INSTALLED DOUBLER IAW FVI DRAWING 53-98419-2. (M) 2 L 7 3 4F A3WE 1998111301106 19981113 01106 NM 1998 11 13 GAIA98104 1 19981023 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 950 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6834 20187 THE FOLLOWING ITEM WAS INITIAL LEVEL 2 CORROSION FOUND DURING A HEAVY C-CHECK. CORROSION ON SEAT TRACK RBL 45, STATION 950. REMOVED AND REPLACED DAMAGED SEAT RAIL SECTION IAW B 727 SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1998111301107 19981113 01107 NM 1998 11 13 GAIA9893 1 19981022 A 3260 SENSOR BOEING 727 727251 138408H NM RT MLG OUT OF ADJUST A GAIA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 264US 19983 TOL - ON TAKEOFF, RETRACTED LANDING GEAR. ONCE GEAR WAS RETRACTED, RIGHT MAIN LANDING GEAR LIGHT REMAINED ILLUMINATED. RECYCLED GEAR. RIGHT MAIN GEAR LIGHT REMAINED ON. ALL INDICATIONS ON FE PANEL OK. LIGHT EXTINGUISHED AT 17,000 FT. A LL INDICATIONS OK. INSPECTED AND FOUND RT MAIN GEAR UPLOCK SENSOR ACTUATOR OUT OF ADJUSTMENT. REPOSITIONED CLEANED AND INSPECTED SENSOR ACTUATOR. FUNCTIONALLY TESTED GOOD IAW B727 MM 32-61-81. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998111301108 19981113 01108 NM 1998 11 13 USAA980525 1 19981019 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STABILIZER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 429US 26761 24551 TPA - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK ELEV STATION 51-54 AT STAB STATION 67.54 HORIZONTAL ST ABILIZER SKIN. CUTOUT CRACK AND INSTALLED DOUBLER PER TR 55-10-07. (M) 2 L 7 2 4F RT A16WE 1998111301109 19981113 01109 WP 1998 11 13 USAA980526 1 19981007 A 5320 BEAM DOUG DC9 DC931 3022065 WP BS 980 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918VJ 48138 PIT - DURING Q-1 CHECK, FOUND CORROSION ON LAV FLOORBEAM, 6 AREAS, .375 INCH WIDE .035 INCH DEEP AT STATION 980 RT LAV A T HOLD DOWN HOLES. (M) 2 L 7 2 4F A6WE 1998111301110 19981113 01110 NM 1998 11 13 USAABB98107 1 19981017 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROWS 26/29 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 611AU 27123 PHL - AISLE EMERGENCY LIGHTS AT ROWS 26 AND 29 INOPERATIVE. MAINTENANCE REPLACED BOTH BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998111301111 19981113 01111 WP 1998 11 13 USAA980486 1 19981007 A 5320 FLANGE DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918VJ 48138 PIT - DURING Q-1 CHECK, FOUND .375 INCH CRACK AT LEFT DRAG ANGLE AT FOURTH RIVET FROM AFT END ON HORIZONTAL FLANGE. FAB RICATED SPLICE AND REPAIRED PER SRM 53-05 FIG 23A - 501 CONFIG. (M) 2 L 7 2 4F A6WE 1998111301112 19981113 01112 WP 1998 11 13 USAA980485 1 19981007 A 5320 591014119 PAN DOUG DC9 DC931 3022065 WP FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 918VJ 48138 PIT - DURING Q-1 CHECK, FOUND .25 INCH LONG CRACK AT FORWARD CARGO DOOR PAN RADIUS ADJACENT TO NR 5 DOOR STOP AT BLIND N UT HOLE. INSTALLED DOUBLER PER EA 50572. (M) 2 L 7 2 4F A6WE 1998111301113 19981113 01113 EU 1998 11 13 SIMA982947 1 19981022 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 ABI - CHAFED LEFT NACELLE OUTBOARD BEAM INNER SKIN PANEL AT NS 212. BLENDED CHAFE, PERFORMED EDDY CURRENT INSPECTION. F ABRICATED AND INSTALLED DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301114 19981113 01114 EU 1998 11 13 SIMA982946 1 19981021 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-329 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 ABI - SEAT TRACK 18.3L CORRODED FROM FS 297.0 TO FS 329.0. CUT OUT, FABRICATED AND INSTALLED 32 INCH EXTRUSION FOR REPA IR OF SEAT TRACK. (M) 2 L 7 2 4T RT A52EU 1998111301115 19981113 01115 EU 1998 11 13 SIMA982945 1 19981021 A 5414 AL7075T6 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 ABI - FOUND CHAFE ON THE LEFT INBOARD NACELLE FILLET FAIRING SEAL CONTRACT AREA. PERFORMED EDDY CURRENT INSPECTION, FAB RICATED AND INSTALLED DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301116 19981113 01116 EU 1998 11 13 SIMA982944 1 19981021 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 307-339 DENT A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 ABI - FOUND DENT ON THE RIGHT UPPER TAIL CONE SKIN AT FS 814 TO 817. CUT OUT DAMAGE, PERFORMED EDDY CURRENT INSPECTION. FABRICATED AND INSTALLED DOUBLER AND TRIPLER. AIRCRAFT RETURNED TO SERVICE (M) 2 L 7 2 4T RT A52EU 1998111301117 19981113 01117 EU 1998 11 13 SIMA982942 1 19981021 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 358 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 ABI - REPAIR OF DMI NR 254RM53024C, DENT IN RT FUSELAGE STATION 358.5 BETWEEN SL 1615/1616. CUT OUT DAMAGED AREA, PERFO RMED EDDY CURRENT INSPECTION. FABRICATED AND INSTALLED TWO EXTERNAL DOUBLERS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301118 19981113 01118 EU 1998 11 13 SIMA982941 1 19981021 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 ABI - DENT DISCOVERED ON LEFT FUSELAGE BETWEEN FRAME 339 AND 363, SL 1515 AND 1516. CUT OUT DAMAGED AREA, PERFORMED EDD Y CURRENT INSPECTION. FABRICATED AND INSTALLED TWO EXTERNAL DOUBLERS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301119 19981113 01119 EU 1998 11 13 SIMA982911 1 19981018 A 3350 6839 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 370AM 340B370 DFW - FLT 5302 - ARM LIGHT ON FLIGHT ATTENDANT PANEL DOES NOT ILLUMINATE. REMOVED AND REPLACED F/A PANEL ARM LIGHT BULB . OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998111301120 19981113 01120 EU 1998 11 13 SIMA982891 1 19981016 A 5320 7253721439 WEB SAAB SF340 340B 7860101 EU BS 287 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 191AE 340B191 ABI - WEB REINFORCEMENT AT FUSELAGE 287 CORRODED. REMOVED AND REPLACED WEB. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301121 19981113 01121 EU 1998 11 13 SIMA982882 1 19981015 A 5347 7253721459 TRACK SAAB SF340 340B 7860101 EU BS 230-265 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 191AE 340B191 ABI - GALLEY TRACK CORRODED. REMOVED AND REPLACED GALLEY TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301122 19981113 01122 EU 1998 11 13 SIMA982881 1 19981015 A 5323 7253710871 AIRSTAIR TRACK SAAB SF340 340B 7860101 EU BS 290 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 191AE 340B191 ABI - AIRSTAIR TRACK CORRODED. REMOVED AND REPLACED AIRSTAIR TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301123 19981113 01123 EU 1998 11 13 SIMA982853 1 19981012 A 3246 JAN982478 WHEEL SAAB SF340 340B 7860101 EU LT MLG FROZEN A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 332AE 340B332 ABI - SMOKE WAS SEEN COMING FROM THE LEFT MAIN LANDING GEAR ASSEMBLY WHILE THE AIRCRAFT WAS TAXIING TO THE GATE. FOUND THE NR 2 WHEEL BEARING HAD FROZE AND THE TIRE HAD BEEN DRAGGING, CAUSING THE SMOKE. NR 2 BRAKE WAS ALSO DAMAGED. REMOV ED AND REPLACED BOTH BRAKES AND BOTH WHEEL ASSEMBLIES ON THE LEFT GEAR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998111301124 19981113 01124 EU 1998 11 13 SIMA982852 1 19981012 A 3240 AIR124472 HOSE SAAB SF340 340B 7860101 EU LT BRAKE LEAKING A SIMA O OTHER K FLUID LOSS LD LANDING 1 SW 21 400BR 340B400 DFW - FLT 3652 - AFTER LANDING AT DFW, HYDRAULIC QUANTITY, BRAKE PRESSURE, AND ACCUMULATOR PRESSURE ALL WENT TO ZERO. D EPLANED PASSENGERS ON TAXIWAY. TOWED AIRCRAFT TO HANGAR. REMOVED AND REPLACED BRAKE LINE THAT ATTACHES TO THE LEFT OUT BOARD BRAKE DUE TO LEAKAGE. SERVICED HYDRAULIC SYSTEM. PERFORMED LEAK AND OPERATIONAL CHECKS. AIRCRAFT RETURNED TO SE RVICE. (M) 2 L 7 2 4T RT A52EU 1998111301125 19981113 01125 EU 1998 11 13 SIMA982543 1 19980911 A 3320 BA08006281 BALLAST SAAB SF340 340B 7860101 EU CABIN ODOR A SIMA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 21 283AE 340B283 ELECTRICAL/HOT PLASTIC SMELL BETWEEN ROWS 8-10. REMOVED AND REPLACED BALLASTS AT SEAT 8A AND 10. FUNCTIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998111301126 19981113 01126 NM 1998 11 13 P2EA98193 1 19981026 A 3241 9550604 VALVE BOEING 737 737222 1384473 NM LT MLG WW LEAKING A P2EA O OTHER K FLUID LOSS TX TAXI/GRND HDL 1 CE 05 209US MAR6748E 19548 MSP - FLT 614 - NO EMERGENCY DECLARED. LOST ALL HYDRAULIC FLUID WHILE TAXIING IN. REPLACED LEFT INBOARD ANTI-SKID CONT ROL VALVE, SERVICED HYDRAULIC RESERVOIR. OPS CHECK OK LEAK CHECK OK PER MM 32-42-31A. (M) 2 L 7 2 4F A16WE 1998111301127 19981113 01127 NM 1998 11 13 P2EA98191 1 19981009 A 5330 SKIN BOEING 737 737244 138448U NM BS 286-303 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 286 TO BS 303, BETWEEN STRINGER 4RT AND STRINGER 5 RT. REPAIRED FUSELAGE INTERNAL DOUBLER FROM BS 286 TO BS 303 PER SRM 53-30-3, FIG 17, DETAIL 1. (M) 2 L 7 2 4F A16WE 1998111301128 19981113 01128 NM 1998 11 13 P2EA98190 1 19981009 A 5330 SKIN BOEING 737 737244 138448U NM BS 344-360 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 344 TO BS 360, BETWEEN STRINGER 6 RT AND STRINGER 7 RT. REPAIRED FUSELAGE SKIN INTERNAL DOUBLER FROM BS 344 TO BS 360, BETWEEN STRINGER 6 RT AND STRINGER 7 RT PER SRM 53-30-3, FIG 17, DETAIL 1. (M) 2 L 7 2 4F A16WE 1998111301129 19981113 01129 NM 1998 11 13 P2EA98189 1 19981009 A 5330 SKIN BOEING 737 737244 138448U NM BS 328-338 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 328 TO BS 338, BETWEEN STRINGER 4 LT AND STRINGER 6 LT. REPAIRED INTERNAL DOUBLER FROM BS 328 TO BS 338, BETWEEN STRINGER 4 LT AND STRINGER 6 LT PER SRM 53-30-03, FIG 17 DETAIL 1. (M) 2 L 7 2 4F A16WE 1998111301130 19981113 01130 NM 1998 11 13 P2EA98188 1 19981004 A 5230 BEAM BOEING 737 737244 138448U NM CARGO DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - C1 DOOR BEAM NR 5 CRACKED, DEFECT SIZE=.500 INCH. REPAIRED C1 DOOR NR 5 BEAM, PER SRM 51-40-3, FIG 1. (M) 2 L 7 2 4F A16WE 1998111301131 19981113 01131 NM 1998 11 13 P2EA98187 1 19981003 A 5330 SKIN BOEING 737 737244 138448U NM BS 1104 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN WITH MISSING MATERIAL AT BS 1104, WL 223, RBL 23, DEFECT SIZE = .75 INCH. REPAIRED FUSELAGE SKIN BE TWEEN BS 1095 AND BS 1108, WL 217 TO WL 223, RBL 23 INCH PER SRM 53-30-03 FIG 3. (M) 2 L 7 2 4F A16WE 1998111301132 19981113 01132 NM 1998 11 13 P2EA98186 1 19981006 A 5311 FRAME BOEING 737 737244 138448U NM BS 927 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE FRAME CRACKED AT BS 927, STRINGER 2 RT, DEFECT SIZE, LENGTH=.500 INCH. REPAIRED FRAME SECTION BS 927, BE TWEEN STRINGER 2RT AND STRINGER 3 RT PER SRM 53-10-04 FIG 10. (M) 2 L 7 2 4F A16WE 1998111301133 19981113 01133 NM 1998 11 13 P2EA98185 1 19981020 A 5720 FITTING BOEING 737 737244 138448U NM WS 525 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING SPAR FITTING CRACKED AT FSS 525, DEFECT SIZE LENGTH=1 INCH. REPLACED FRONT SPAR FITTING PER SRM 51-10- 01 PAGES 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998111301134 19981113 01134 NM 1998 11 13 P2EA98184 1 19981003 A 5320 5097588 FITTING BOEING 737 737244 138448U NM PAX DOOR WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - L1 ENTRY DOOR LOWER STOP FITTING WORN. REPLACED STOP FITTING PER SRM 51-10-01 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998111301135 19981113 01135 NM 1998 11 13 P2EA98178 1 19981005 A 5313 STRINGER BOEING 737 737244 138448U NM BS 685 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - STRINGER 5 RT CRACKED AT BS 685, DEFECT SIZE .375 INCH LENGTH. FUSELAGE STRINGER 5 RT REPAIRED BETWEEN BS 679 TO BS 691 PER SRM 53-10-3, FIG 4. (M) 2 L 7 2 4F A16WE 1998111301136 19981113 01136 NM 1998 11 13 P2EA98180 1 19981003 A 5313 STRINGER BOEING 737 737244 138448U NM BS 920-933 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - STRINGER 25 LT CRACKED AT BS 927, DEFECT SIZE .375 INCH. REPAIRED FUSELAGE STRINGER SECTION BETWEEN BS 920 AND BS 933 PER SRM 53-10-03 FIG 1 SHEET 6. (M) 2 L 7 2 4F A16WE 1998111301137 19981113 01137 CE 1998 11 13 98ZZZM832 1 19980829 A 5711 1181000299 SPAR BEECH 1900 1900C 1154161 CE WING CORRODED A YADA K NONE O OTHER IN INSP/MAINT 1 AL 01 1563C 27935 UC20 FOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR IN TH E CABIN. CORROSION WAS FOUND ON THE FORWARD FACE OF THE SPAR CAP AND WAS DISTRIBUTED IN SMALL AREAS ACROSS THE SPAR, JU ST ABOVE THE EDGE OF THE SEALANT THAT IS USED TO SEAL THE SPAR RIVET FLANGE. DAMAGE WAS DETERMINED TO BE NEGLIGIBLE AFT ER CORROSION REMOVAL. 2 L 7 2 4T RT A24CE 1998111301138 19981113 01138 NM 1998 11 13 P2EA98182 1 19981004 A 5330 SKIN BOEING 737 737244 138448U NM BS 310-314 LIGHTNING STRIKE A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - LIGHTING STRIKE DETECTED IN FUSELAGE SKIN SECTION AT BS 312, STRINGER 3 LEFT, DEFECT SIZE .125 INCH LENGTH. REPAI RED FUSELAGE SKIN SECTION BETWEEN BS 310 AND BS 314 AT STRINGER 3 LEFT PER SRM 53-30-03, FIG 5. (M) 2 L 7 2 4F A16WE 1998111301139 19981113 01139 NM 1998 11 13 P2EA98183 1 19981017 A 5210 SKIN BOEING 737 737222 1384473 NM PAX DOOR DENT A P2EA K NONE O OTHER TX TAXI/GRND HDL 1 CE 05 209US 19548 ATL - FLT 612 - THE FOLLOWING OCCURED WHILE RAMP AGENT WAS CONNECTING TOW BAR TO PUSH TRACTOR. L1 DOOR SKIN DAMAGED BY JETWAY. INSTALLED DOUBLER ON L1 DOOR PER SRM 52-00-3, FIG 5. (M) 2 L 7 2 4F A16WE 1998111301140 19981113 01140 WP 1998 11 13 AALA981917 1 19981015 A 3397 A3060720201 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 413AA 49324 DFW - DURING OVERNIGHT MANTENANCE FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FIRST CLASS EMERGENCY EXIT LIG HT WIRE BETWEEN FIRST CLASS AND GALLEY FLOOR EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998111301141 19981113 01141 WP 1998 11 13 AALA981910 1 19981010 A 3350 59566781 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70504 49798 DFW - DURING OVERNIGHT CHECK, AFT LEFT SERVICE DOOR EMERGENCY EXIT SIDEWALL MARKER INOPERATIVE. REPLACED AFT LEFT SERVI CE DOOR EMERGENCY EXIT SIDEWALL MARKER LIGHT ASSEMBLY. GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998111301142 19981113 01142 WP 1998 11 13 AALA981911 1 19981012 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 210AA 49161 DURING OVERNIGHT MAINTENANCE, PORTABLE EMERGENCY LIGHT AT FORWARD FLIGHT ATTENDANT SEAT INOPERATIVE. REPLACED EMERGENCY PORTABLE LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998111301143 19981113 01143 WP 1998 11 13 AALA981898 1 19981010 A 3350 1001191 LIGHT GRIMES DOUG DC9 DC982 3022082 WP DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 575AM 2922 53152 DFW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR PORTABLE EMERGENCY LIGHT INOPERATIVE. REPLACED FORWARD ENTRY DOO R PORTABLE EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998111301149 19981113 01149 CE 1998 11 13 98ZZZX4070 1 19981005 A 2434 DOFF10300B ALTERNATOR ELECTROSYS CESSNA 210 210L 2073448 CE ENGINE FAILED A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 5489V 3 8081451 21060961 ALTERNATOR INSTALLED 10-1 AND REMOVED 10-2. ALTERNATOR HAD FIELD VOLTAGE, NO OUTPUT. 1 H 7 1 3O 3A21 1998111301151 19981113 01151 CE 1998 11 13 98ZZZX4072 1 19980910 A 3230 3582508714 ROD BEECH 58 58 1152740 CE NLG SEPARATED A BSYA O OTHER O OTHER AP APPROACH 1 GL 07 2064V 4262 TH1004 DURING APPROACH, THE NOSE RETRACT LANDING GEAR RT ROD ASSY ROD END PULLED APART FROM THE GEAR BRACKET. THE NOSE GEAR CO LLAPSED. THE CAUSE OF THE ROD END FAILURE IS UNKNOWN AT THIS TIME. 1 L 7 2 3O 3A16 1998111301155 19981113 01155 SO 1998 11 13 98ZZZX4076 2 19981001 A 7314 6467681A1 FUEL PUMP CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE OUT OF ADJUST A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 4372Y 481 A159804BR 21063977 293887R ENGINE CAME IN RUNNING ROUGH. FOUND FUEL PRESSURE HIGH. ADJUSTED PUMP AND RETURNED TO SERVICE. APPROXIMATELY 50 HOURS LATER, AIRCRAFT CAME IN WITH THE SAME CONDITION. THE THIRD TIME, PUMP WOULD NOT ADJUST AND PUMP WAS REJECTED. 1 H 7 1 3O 3 O 3A21 E8CE 1998111301156 19981113 01156 SO 1998 11 13 98ZZZX4077 2 19981001 A 7314 6467681A1 FUEL PUMP CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO ENGINE LEAKING A FPIA K NONE K FLUID LOSS NR NOT REPORTED 1 SO 15 4702C G149802BR3 21063591 293986R AFTER ENGINE INSTALLATION POST-RUN, THE FUEL PUMP LEAKED FORM DRAIN TUBE. RAN ENGINE SEVERAL MORE TIMES. THIS DID NOT REMEDY THE CONDITION. 1 H 7 1 3O 3 O 3A21 E8CE 1998111301157 19981113 01157 GL 1998 11 13 98ZZZX4078 3 19981001 A 6110 PROPELLER PIPER PA32 PA32RT300T 7103216 SO MCAULY D3A34 D3A34C404 GL FORWARD MISMANUFACTURED A FPIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 7660E 8 32RT7787001 768345 SUBMITTER STATED PROPELLER OVERHAULED, WOULD ONLY DEVELOP 2,650 RPM (2,850 REDLINE). 1 L 7 1 3O A3SO 5 C P47GL 1998111301167 19981113 01167 WP 1998 11 13 TWAA9818101 1 19981109 A 2150 39271411 VALVE DOUG DC9 DC931 3022065 WP LT AC SYST WORN A TWAA A B G UNSCHED LANDING EMER. DESCENT O2 MASK DEPLOYED J WARNING INDICATION CR CRUISE 1 CE 05 992Z 47095 CABIN PRESSURIZATION LOST AT FL260. PASSENGER OXYGEN MASKS DROPPED. DIVERTED TO MCI. REPLACED THE LEFT PRESSURE REGUL ATOR VALVE AND RT AIR CONDITIONING DUCT THAT HAD FAILED. DUCT MFG PART NBR 5953624-511. CHECK-C 9-4-98 STL. 2 L 7 2 4F A6WE 1998111301168 19981113 01168 NM 1998 11 13 TWAA9818102 1 19981110 A 3350 MS2465827E SWITCH BOEING 767 767231 1385131 NM COCKPIT WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 610TW 22573 THE EXTERIOR EMERGENCY LIGHT TEST SWITCH WAS FOUND INOPERATIVE. REPLACED SWITCH. CHECK-C 9-16-98 LAX. 2 L 7 2 4F RT A1NM 1998111301169 19981113 01169 NE 1998 11 13 VJ9800587 2 19981109 A 7314 7436025 FUEL PUMP DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A ZZDA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 SO 15 925VV 47319 674425 AFTER TAKEOFF AT 500 FEET ALTITUDE, NR 2 ENGINE FAILED, NO VIBRATION OR BANG EXPERIENCED. FOUND NR 2 ENGINE FUEL PUMP D RIVE SHAFT SHEARED. REPLACED FUEL PUMP IAW DC9 MM 73-10-1 AND FUEL CONTROL REPLACED IAW DC9 MM 73-20-1 AS PRECAUTIONARY MEASURE. OPS CHECKED NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1998111301170 19981113 01170 NM 1998 11 13 K3HA980133 1 19981105 A 3350 07912 LIGHT BOEING 727 727225 1384077 NM ROW 2 & 3 INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 BETWEEN ROWS 2 AND 3 EMERGENCY LIGHT NEEDS TO BE REPLACED. REINSTALLED LIGHT IN TRACK, OPS CHECK OK REF MM 33-50-01. 2 L 7 3 4F A3WE 1998111301171 19981113 01171 1998 11 13 IXXA9800081 4 19981101 A 3416 WIRE DOUG DC8 DC862 3021970 WP LT ALTIMETER LOOSE A IXXA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 21CX 45955 EN ROUTE, THE FLIGHT CREW DETECTED WHITE SMOKE EMITTING FROM UNDER THE CAPTAIN'S INSTRUMENT PANEL, ACCOMPANIED WITH AN O DOR, THEN DIMINISHED. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND CONTINUED TO KBWI FOR AN UNEVENTFUL LANDING. M AINTENANCE INSPECTED THE CAPTAIN'S INSTRUMENTS AND LIGHTING SYSTEMS WIRING LOCATING A LOOSE WIRE ON THE CAPTAIN'S ALTIME TER VIBRATOR, WHICH WAS SECURED. FURTHER INSPECTION REVEALED NO DISCREPANCIES. MAINTENANCE PERFORMED A SUCCUSSFUL INST RUMENTATION AND LIGHTING OPERATIONAL TEST ON EXTERNAL AND SHIP'S POWER AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1998111301172 19981113 01172 WP 1998 11 13 IXXA9800082 1 19981110 A 3260 DSO73S411 CONNECTOR DOUG DC8 DC871F 302199D WP LT MLG DOOR WET A IXXA K NONE N FALSE WARNING CL CLIMB 1 GL 23 826BX 2925 45998 AFTER TAKEOFF, THE LANDING GEAR WAS RETRACTED, THE GEAR DOOR WARNING LIGHT REMAINED ILLUMINATED. THE CREW CYCLED THE GE AR SEVERAL TIMES WITH THE WARNING INDICATION REMAINING THE SAME. THE CREW PERFORMED A SUCCESSFUL GEAR UPLATCH CHECK AND THE WARNING LIGHT EXTINGUSHED. WHEN THE GEAR HANDLE WAS PLACED BACK IN THE UP POSITION, THE WARNING LIGHT ILLUMINATED AGAIN. THE FLIGHT RETURNED TO DEN FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE GEAR DOOR WARNING SYSTEM, LOCAT ING MOISTURE IN THE LEFT MAIN GEAR DOOR UPLATCH SWITCH ELECTRICAL CONNECTOR. MAINTENANCE CLEANED THE SWITCH AND PERFORM ED A SUCCESSFUL OPERATIONAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL. 2 L 7 4 4F RT 4A25 1998111301173 19981113 01173 NM 1998 11 13 AWXA9800219 1 19981104 A 5210 STOP PINS BOEING 757 7572S7 1384962 NM PAX DOOR OUT OF ADJUST A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 904AW 23566 ON CLIMBOUT AT APPROX 8000 FT, EICAS MSG L AFT ENTRY DOOR AND OVERHEAD ENTRY DOOR LIGHT. FLIGHT ATTENDANT REPORTED DOOR HANDLE POPPED UP UNABLE TO CLOSE PRESSURIZATION NORMAL. ADJUSTED LEFT AFT ENTRY DOOR STOP PINS PER 757 MM 52-11 P 512 ITEM NR 4 PRESSURIZED CABIN, OPS CK GOOD. 2 L 7 2 4F RT A2NM 1998111301174 19981113 01174 NM 1998 11 13 AWXA9800220 1 19981105 A 3350 LIGHTS BOEING 757 7572G7 1384963 NM ROW 4-8-34 INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 910AW 24523 INTERIOR EMERGENCY LIGHTS ROWS 4 ABC, 8 ABC AND 34 AC INOP. DPI ISSUED MEL 33-51-1 COND 1C. BATTERIES CHARGERS CHARGED EMER BATTERIES NORMALLY IN FLIGHT. ALL EMER LIGHTS OP NORMAL. DPI CLEARED. 2 L 7 2 4F RT A2NM 1998111301175 19981113 01175 NM 1998 11 13 CALA9802050 1 19981109 A 5330 SKIN BOEING 757 757224 1384958 NM BS 625 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14102 27292 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 625 BETWEEN STRINGERS 16L AND 17L. REPAIRED IAW SRM 53-00-01, FIGURE 101. 2 L 7 2 4F RT A2NM 1998111301176 19981113 01176 NM 1998 11 13 CALA9802051 1 19981110 A 5754 CASTING BOEING 727 727232 1384082 NM NR 3 LE FLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1.62 INCH CRACK IN LT WING NR 3 LEADING EDGE FLAP MAIN CASTING AT O/B HINGE MOUNT AREA. THE NR 3 LEA DING EDGE FLAP WAS REMOVED AND REPLACED IAW MM 27-81-1. 2 L 7 3 4F A3WE 1998111301177 19981113 01177 NM 1998 11 13 CALA9802052 1 19981110 A 5330 SKIN BOEING 727 727232 1384082 NM BS 720 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN AT BS 720C, RBL 2 WITH A HOLE CHAFED THROUGH AT LBL 6. THE CRACKED AND CHAFED AREAS WERE CUT OUT. A REPAIR WAS INSTALLED IAW SRM 51-10-2 AND BOEING DRAWING 7275331041. 2 L 7 3 4F A3WE 1998111301178 19981113 01178 NM 1998 11 13 CALA9802053 1 19981110 A 5752 652172634 SKIN BOEING 727 727232 1384082 NM RT AILERON TAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND RT OUTBOARD AILERON TAB DENTED. THE RT OUTBOARD AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-0. 2 L 7 3 4F A3WE 1998111301179 19981113 01179 NM 1998 11 13 CALA9802054 1 19981106 A 3230 TORQUE LINK 6573761110 BOEING 737 7373T0 1384582 NM RT MLG BROKEN A CALA O OTHER E VIBRATION/BUFFET LD LANDING 1 SW 09 12318 1358 23369 A RT MLG TIRE BLEW OUT AFTER TOUCHDOWN. THERE WAS VIBRATION AND THE AIRCRAFT STOPPED ON THE RUNWAY. THERE WERE NO INDI CATIONS OF A PROBLEM PRIOR TO LANDING. MAINTENANCE FOUND THE RT TORQUE LINK BROKEN AND THE GEAR ROTATED 90 DEGREES. TH E RT MLG WAS REMOVED AND REPLACED DUE TO DAMAGE CAUSED ON LANDING. THE GEAR WAS CYCLED SEVERAL TIMES IAW MM 32-32-00 WI TH OPERATION AND INDICATIONS CHECKING GOOD. A MANUAL GEAR EXTENSION WAS ALSO PERFORMED IAW MM 32-34-00 AND OPERATION CH ECKED GOOD. A HARD LANDING AND HIGH DRAG/SIDE LOAD LANDING INSPECTION WAS PERFORMED ON THE NLG, LT MLG, AND RT MLG IAW MM 05-51-51, PAGES 201-206 AND ALL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1998111301180 19981113 01180 WP 1998 11 13 9810339860 1 19981109 A 3260 0080004003 CONTROL UNIT DOUG DC9 DC951 3022051 WP E/E COMPT INOP A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 769NC 36594 36594 47757 AFTER TAKEOFF, THE FLIGHT CREW PERFORMED A LANDING GEAR UPLATCH CHECK. THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED. LANDING GEAR WAS RECYCLED WITH A NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATION UPON LANDING GEAR RETRACTION . FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. LANDING GEAR INDICATION WAS NORMAL UPON LANDING. MAINTENANCE PE RFORMED A LANDING GEAR UPLATCH CHECK AND REPLACED THE LANDING GEAR CONTROL UNIT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998111301181 19981113 01181 SO 1998 11 13 COMA9810256 1 19981109 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 254CA 17290 120233 AFT SECTION OF EMERGENCY LIGHTING IS INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998111301182 19981113 01182 SO 1998 11 13 COMA9810257 1 19981107 A 3397 WIRE EMB 120 EMB120RT 3260202 SO ROW 5 LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 258CA 120247 EXIT SIGN AT ROW 5 IS INOPERABLE. CONNECTED WIRING, SIGN OPERATES NORMAL. 2 L 7 2 4T RT A31SO 1998111301183 19981113 01183 SO 1998 11 13 COMA9810258 1 19981106 A 2750 JO365 CONNECTOR EMB 120 EMB120RT SO TE FLAPS DEFECTIVE A COMA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 01 152CA 120152 FLAP CONTROL FAULT. REPLACED ACTUATOR WIRNG CONNECTOR JO 365. 2 L 7 2 4T RT A31SO 1998111301184 19981113 01184 SO 1998 11 13 COMA9810259 1 19981106 A 3150 UNIT EMB 120 EMB120RT SO AURAL WARNING FAILED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 264D 120256 AURAL WARNING UNIT FAILED. RESET AURAL WARNING UNIT, SYSTEM OPERATION NORMAL. 2 L 7 2 4T RT A31SO 1998111301185 19981113 01185 EA 1998 11 13 COMA9860347 1 19981107 A 5210 LATCH CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 966CA 7132 CABIN DOOR WARNING AT 21,000 FT. ADJUSTED DOOR LATCH MECHANISM. 2 L 7 2 4F RT A21EA 1998111301186 19981113 01186 NM 1998 11 13 UPS98228121 1 19981106 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM RT OVERWING DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER LIGHT AT RT AFT OVERWING EXIT INOP. REMOVED AND REPLACED BATTERY PACK, CKS OK (P/N 96-2-1033) . 2 L 7 3 4F A3WE 1998111301187 19981113 01187 NM 1998 11 13 UPS98228122 1 19981106 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER LIGHT AT FWD ENTRY DOOR BY COCKPIT DOOR INOP. REMOVED AND REPLACED BATT PACK, CHKS GOOD (P/N 96-2-1015). 2 L 7 3 4F A3WE 1998111301189 19981113 01189 NM 1998 11 13 UPS98228124 1 19981106 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM LT OVERWING DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER LIGHT AT CEILING LT OVER WING INOP. REMOVED AND REPLACED BATT PACK, CKS GOOD (P/N 96-2-1024). 2 L 7 3 4F A3WE 1998111301190 19981113 01190 NM 1998 11 13 UPS98228125 1 19981106 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER LIGHT AT CEILING AFT CENTER INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY, CKS OK (P/N 96-2-1 01). 2 L 7 3 4F A3WE 1998111301191 19981113 01191 NM 1998 11 13 UPS98228126 1 19981106 A 3350 BATTERY BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER LIGHT LEFT AFT INOP. REMOVED AND REPLACED BATTERY, CKS OK (P/N 96-2-1015). 2 L 7 3 4F A3WE 1998111301192 19981113 01192 NM 1998 11 13 UPS98228131 1 19981102 A 5312 BULKHEAD BOEING 727 72762C 138402C NM BS 178 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE-C, FWD PRESSURE BULKHEAD AND STIFFENERS FOUND DAMAGED BS 178 WL 200 RBL 5. REPAIRED IAW UPS EO B727-531 0-4290 USING REPAIR KIT 65C36289-1. 2 L 7 3 4F A3WE 1998111301193 19981113 01193 WP 1998 11 13 UPS98828128 1 19981018 A 5320 975492072 ANGLE DOUG DC8 DC871F 302199D WP BS 1230 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 FS 1230 LONG 36 TO L34L THE ATTACH ANGLE IS CRACKED AND GOUGED. REMOVED, FABRICATED AND REPLACED A NGLE IAW DWG 9754920 AND SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998111301194 19981113 01194 WP 1998 11 13 UPS98828129 1 19981015 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 690 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C3, LT WING LWR SKIN JUST O/B OF THE NR 1 PYLON AND FWD OF THE CENTER SPAR HAS HEAVY CORROSION. REMOVED CORROSION AND REPAIRED WING SKIN IAW DWG 5802630. 2 L 7 4 4F RT 4A25 1998111301195 19981113 01195 WP 1998 11 13 UPS98828130 1 19981021 A 5531 RIB DOUG DC8 DC871F 302199D WP VERT STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C3, VERTICAL STAB L/E RIB AT ZFS 223 IS CRACKED AT THE LT AFT END. STOPPED DRILLED CRACK AND REPAIRED R IB IAW SRM 55-2-0. 2 L 7 4 4F RT 4A25 1998111301196 19981113 01196 WP 1998 11 13 UPS98828132 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C3, RT WING L/E RIB AT XFS 660.0 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998111301197 19981113 01197 WP 1998 11 13 UPS98828133 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 622.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, RT WING L/E RIB AT XFS 622.5 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACKED AND REPAIRED RIB IA W SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998111301198 19981113 01198 WP 1998 11 13 UPS98828134 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, RT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG. 2 L 7 4 4F RT 4A25 1998111301199 19981113 01199 WP 1998 11 13 UPS98828135 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 616.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, LT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED RIB I AW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1998111301200 19981113 01200 NM 1998 11 13 UPS98227942 1 19981016 A 3350 1000679 LIGHT BOEING 727 72722C 138400F NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 941UP 19196 INSPECTION TYPE-N/A, EXIT LIGHT OVER FWD ENTRY DOOR INOP. REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CKD OK. 2 L 7 3 4F A3WE 1998111301201 19981113 01201 NM 1998 11 13 UPS98228136 1 19981102 A 5320 INTERCOSTAL BOEING 727 72762C 138402C NM BS 760 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE-C, INTERCOSTAL DAMAGED BS 760 LBL 45 LBL 62. REPAIR CARRIED OUT IAW SRM 51-20-1. 2 L 7 3 4F A3WE 1998111301202 19981113 01202 WP 1998 11 13 UPS98828137 1 19981104 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 433 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT THE SPAR AT XS 433 HAS INTERGRANULAR CORROSION AND IS CRACKED. REPAIRED IA W SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998111301203 19981113 01203 WP 1998 11 13 UPS98828138 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 778.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, RT WING L/E RIB AT XFS 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998111301204 19981113 01204 NM 1998 11 13 QXEA9801681 1 19981108 A 2120 AIR DIST DHAV DHC8 DHC8102 2809003 NM CABIN ODOR A QXEA O OTHER B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 816PH 54 SMELL OF JET FUEL IN THE CABIN AND COCKPIT AFTER TURNING ON NR 2 BLEED. TURNING OFF NR 2 BLEED GETS RID OF THE SMELL. M AINTENANCE PERFORMED AN INSPECTION OF THE BLEED AIR SYSTEM WITH NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. NO PAR TS REPLACED. 2 H 7 2 4T RT A13NM 1998111301205 19981113 01205 NM 1998 11 13 QXEA9801682 1 19981106 A 3350 61047811 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 357PH 599 504 TWO RED EMERGENCY TRACK LIGHT BULBS ARE BURNED OUT AT THE TYPE 2 EXIT. REPLACED THE PS2 BATTERY POWER SUPPLY. OPERATIO NAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998111301206 19981113 01206 NM 1998 11 13 QXEA9801680 1 19981024 A 3246 314353 WHEEL DHAV DHC8 DHC8102 2809003 NM RT MLG CRACKED A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 821PH 6339 316 104 NR 4 MAIN WHEEL BROKEN. THE OUTER RIM FAILED AT THE BEAD SEAT. THE CRACK RUNS APPROXIMATELY HALF OF THE WAY AROUND THE BEAD SEAT AREA. REPLACED THE NR 4 WHEEL ASSEMBLY. 2 H 7 2 4T RT A13NM 1998111301207 19981113 01207 1998 11 13 98FDEA00691 4 19981110 A 3442 622513 RT UNIT BOEING 727 7272S2F 1384O81 NM E & E COMPT INOP A FDEA A UNSCHED LANDING O OTHER UK UNKNOWN 1 SO 25 207FE 22929 RADAR NOT PAINTING WEATHER ACCURATELY ALL MODES AND RANGES. REMOVED AND REPLACED RADAR RECEIVER TRANSMITTER. OPER CKS GOOD PER MM 34-0. WEATHER RADAR OK FOR SERVICE. 2 L 7 3 4F A3WE 1998111301208 19981113 01208 WP 1998 11 13 98FDEA00692 1 19981110 A 2930 TEMP GAUGE DOUG DC10 DC1030F 3023504 WP NR 3 HYD SYST INOP A FDEA A UNSCHED LANDING P NO WARNING INDICATION CL CLIMB 1 SO 25 314FE 48312 NR 3 HYDRAULIC TEMP HAD SLOWLY INCREASED IN TEMP AFTER T/O. TEMP 108C, NO TEMP LIGHT, PRESS TO TEST WAS OK. REMOVED AN D REPLACED HYDRAULIC GAUGE AFTER TROUBLESHOOTING, RAN SYS, OK FOR SERVICE MM 29-33-01. 2 L 7 3 4F RT A22WE 1998111301209 19981113 01209 WP 1998 11 13 98FDEA00693 1 19980909 A 5310 STRUCTURE DOUG DC10 DC1010 3022110 WP L3 DOORWAY CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 375FE 46613 MAIN CABIN INTERIOR FUSELAGE BOX STRUCTURE ABOVE ENTRY DOOR L3, CORROSION ON TOP OF BOX STRUCTURE AND HARDWARE. *S/D* R EMOVED CORROSION AREA BLENDED WITHIN LIMITS PER SRM 53-00-01 FIG 1A PG 6A. ALODINED AND PRIMED. 2 L 7 3 4F A22WE 1998111301210 19981113 01210 NE 1998 11 13 98FDEA00694 2 19981110 A 7230 C1 DISK BOEING 727 72722C 138400F NM PWA JT8 JT8D7 52053 NE NR 1 ENGINE BIRD STRIKE A FDEA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 SO 25 112FE 19890 AFT V1 AND BEFORE ROTATION NR 1 ENG GAVE A LOUD BANG AND APPEARED TO COMPRESSOR STALL, FOLLOWED BY A SMELL COMING FROM T HE PACK A/C LEFT HAND. IN WORK AT THIS TIME TO REPLACE C1 DISK ASSY (BIRD INJESTION FOD). REMOVED AND REPLACED NR 1 EN G C1 DISK ASSY BREATHER AND VIB CK OK. BORESCOPE INSP GOOD 72-00-2610 AND 72-00-2607. 2 L 7 3 4F 4 F A3WE E2EA 1998111301211 19981113 01211 NM 1998 11 13 98FDEA00695 1 19981110 A 3230 656021132 ACCESSORY UNIT BOEING 727 727225 1384077 NM E & E COMPT INOP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 469FE 21581 AFT T/O, GEAR HANDLE WOULD NOT RAISE, GEAR LATCH FAILED TO RELEASE. PINS INSTALL. FOUND LAND ASSY UNIT BAD. REMOVED A ND REPLACED UNIT PER MM 32-09-121. PERFORMED FUNC TEST PER MM 32-09-122, ALL CK OK. REMOVED PLACARD AND INSTALLED ALIG N ON SIDE PANEL IN CORRECT PLACE. 2 L 7 3 4F A3WE 1998111301212 19981113 01212 NM 1998 11 13 98UAL900519 1 19981031 A 2120 LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E & E COMPT ILLUMINATED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 938UA 26671 EQUIPMENT COOLING EXHAUST OFF LIGHT ON STEADY IN BOTH NORMAL AND ALT POSITIONS. 2 L 7 2 4F 4 F RT A16WE E2GL 1998111301213 19981113 01213 NM 1998 11 13 98UAL900520 1 19981030 A 2613 896767 ELEMENT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE APU COMPT FAILED A UALA F ACTIVATE FIRE EXT. N FALSE WARNING NR NOT REPORTED 1 WP 29 352UA 24320 APU FIRE LIGHT CAME ON. NO EXTERIOR INDICATIONS. REPLACED APU TAIL PIPE OVER HEAT SENSING ELEMENT AND WIRE HARNESS FOR OVER HEAT ELEMENT, REF MM 26-15-14. TESTED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998111301214 19981113 01214 NE 1998 11 13 98UAL900521 2 19981029 A 7240 JA803794 COMBUSTOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE CRACKED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7279U 10964 21557 696607 NINE INCH CIRCUMFERENTIAL CRACK IN NR 5 COMBUSTION CHAMBER CAN OF NR 2 ENGINE. *S/D* SHOP INSPECTION OF THE NR 5 BURNER CAN REVEALED THE CRACK TO BE IN THE 2-3 LINER UNDER THE AIR SCOOP. CRACKING IN THIS AREA IS NOT UNCOMMON, ALTHOUGH AT 1 0,964 HOURS THE CRACKS ARE USUALLY LESS THAN 9 LONG. FURTHER INSPECTION OF THE CAN AND ENGINE REVEALED NO OTHER RELATED ABNORMALITIES. THE COMBUSTOR CAN ISOTOPE INSPECTION RESULTS WILL CONTINUE TO BE MONITORED CLOSELY. 2 L 7 3 4F 4 F A3WE E2EA 1998111301215 19981113 01215 NM 1998 11 13 98UAL900522 1 19981031 A 2781 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 LE SLAT MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7279U 21557 AFTER TAKEOFF, NR 4 LEADING EDGE SLAT GREEN LIGHT REMAINS ON WITH SLATS RETRACTED. RETURNED TO DEN. 2 L 7 3 4F 4 F A3WE E2EA 1998111301216 19981113 01216 NM 1998 11 13 98UAL900523 1 19981103 A 2750 RETRACT MECH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE TE FLAPS MALFUNCTIONED A A UALA O OTHER F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 519UA 24872 LANDED UNDER AMBER ALERT DUE TO A TRAILING EDGE FLAP DEPLOYMENT PROBLEM. 2 L 7 2 4F 4 F RT A2NM E17NE 1998111301218 19981113 01218 NM 1998 11 13 98UAL900525 1 19981106 A 3350 LIGHT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SEAT 10A INOP A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7270U 21417 EEL LIGHTING INOPERATIVE FROM SEAT 10A TO FIRST CLASS. 2 L 7 3 4F 4 F A3WE E2EA 1998111301219 19981113 01219 NM 1998 11 13 98UAL900526 1 19981104 A 2120 AIR DIST BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FLIGHT DECK ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 331UA 24192 HOT OIL SMELL WAS NOTED, ON THE FLIGHT DECK ONLY. AFTER THREE (3) MAINTENANCE OPERATIONAL CHECKS (ENGINES OPERATING) AN D DETAILED VISUAL INSPECTION OF THE APU/PNEUMATIC DUCTING, NO OIL LEAKS OR HOT OIL SMELLS WERE NOTED. NO FAULT FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 1998111301220 19981113 01220 1998 11 13 98UAL900527 4 19981105 A 2565 831A0S VALVE BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE SLIDE/RAFT LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 768UA 26919 DURING ROUTINE SHOP OVERHAUL OF A SLIDE/RAFT, THE TOP TUBE PRESSURE TEST VALVE BODY (P/N 831A0S), WAS FOUND TO BE LEAKIN G AT THE BASE OF THE VALVE BODY. 2 L 7 2 4F 4 F RT T0001SE E46NE 1998111301221 19981113 01221 WP 1998 11 13 ABXA9800933 1 19981103 A 5400 5765316 ANGLE DOUG DOUG DC8 DC861 3021952 WP NR 3 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 841AX 45908 NR 3 ENGINE PYLON SUPPORT ANGLE CRACKED AT AFT OUTBOARD END. REPAIRED PYLON RIB, LOWER SECTION IAW ABX REA-D854-24337MR . 2 L 7 4 4F 4A25 1998111301222 19981113 01222 WP 1998 11 13 ABXA9800934 1 19981102 A 5312 5910130287 BULKHEAD SKIN DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND THE AFT SIDE OF THE AFT PRESSURE BULKHEAD SKIN CRACKED AT THE RIGHT SIDE OF VENTRAL DOOR CUTOUT AP PROX 30 INCHES ABOVE FLOOR LINE. REPAIRED IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 1998111301223 19981113 01223 WP 1998 11 13 ABXA9800935 1 19981102 A 5400 591326313 ANGLE DOUG DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND NR 2 PYLON TO FUSELAGE ATTACH ANGLE CRACKED BENEATH THE PYLON LEADING EDGE. REPLACED ANGLE IAW DC 9 SRM 54-04. 2 L 7 2 4F A6WE 1998111301224 19981113 01224 WP 1998 11 13 ABXA9800936 1 19981102 A 5411 99582213 RIB DOUG DOUG DC9 DC932 3022066 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND FORWARD UPPER EDGE OF NR 1 PYLON RIB CRACKED INSIDE ACCESS PANEL AREA 8111. REPAIRED RIB IAW ABX DC9 SSRM DWG K05159. 2 L 7 2 4F A6WE 1998111301225 19981113 01225 WP 1998 11 13 ABXA9800937 1 19981102 A 5312 3917624517 BULKHEAD FITTING DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND THE VENTRAL DOOR LOWER, LEFT STOP SUPPORT FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-2 A ND 51-30-5. 2 L 7 2 4F A6WE 1998111301226 19981113 01226 WP 1998 11 13 ABXA9800938 1 19981102 A 5313 59114279 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND LONGERON 17R CRACKED AT PYLON BULKHEAD STATION 965. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998111301227 19981113 01227 WP 1998 11 13 ABXA9800940 1 19981102 A 5230 59101413 SKIN DOUG DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND THE FORWARD LOWER CARGO COMPARTMENT DOOR EXTERIOR SKIN CRACKED IN SEVERAL PLACES AT THE DOOR PAN A TTACH RIVETS. REPAIRED DOOR SKIN IAW ABX REA D952-25273. 2 L 7 2 4F A6WE 1998111301228 19981113 01228 WP 1998 11 13 ABXA9800941 1 19981102 A 5330 59134213 SKIN DOUG DOUG DC9 DC932 3022066 WP BS 100 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND FUSELAGE SKIN AT RIGHT AFT NOSE GEAR DOOR HINGE CUTOUT STATION 100 CRACKED. REPAIRED SKIN IAW DC9 SRM 53-05. 2 L 7 2 4F A6WE 1998111301229 19981113 01229 WP 1998 11 13 ABXA9800943 1 19980911 A 5320 37500252 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 900 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERCOSTAL TIE FITTING CRACKED AT STATION 900, LONGERON 21L. REPLACED FITTING IAW DWG 3750025 DC8 SRM 51-1-200. 2 L 7 4 4F 4A25 1998111301230 19981113 01230 WP 1998 11 13 ABXA9800944 1 19980911 A 5320 37558412 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT STATION 1200 BETWEEN LONGERON 34R TO 33R. REPLACED FITTING AT STATION 1200 BETWEEN LONGERON 34R TO 3 3R IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301231 19981113 01231 WP 1998 11 13 ABXA9800945 1 19980910 A 5313 575032229 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1348 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 34L CRACKED AT STATION 1348. REPLACED LONGERON 34L FROM STATION 1260 TO 1350 IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301232 19981113 01232 WP 1998 11 13 ABXA9800946 1 19980910 A 5320 37500252 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 900 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT STATION 900 LONGERON 20R. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3750025. 2 L 7 4 4F 4A25 1998111301233 19981113 01233 WP 1998 11 13 ABXA9800947 1 19980910 A 5320 3779874 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 834 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT LONGERON 20R, STATION 834. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3779874. 2 L 7 4 4F 4A25 1998111301234 19981113 01234 WP 1998 11 13 ABXA9800948 1 19980910 A 5712 57694662 RIB DOUG DOUG DC8 DC861 3021952 WP WS 622.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING LOWER LEADING EDGE RIB IS CRACKED FORWARD OF ACCESS PANEL AT STATION XFS622.5. REPAIRED IAW DC8 SRM 57-2-0. 2 L 7 4 4F 4A25 1998111301235 19981113 01235 WP 1998 11 13 ABXA9800949 1 19980910 A 5320 37558452 SHEAR TIE DOUG DOUG DC8 DC861 3021952 WP BS 1231 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 STATION 1231 BETWEEN STRINGER 34L TO 35L, SHEAR TIE FITTING IS CRACKED. REPLACED SHEAR TIE IAW DC8 51-1-20D. 2 L 7 4 4F 4A25 1998111301236 19981113 01236 WP 1998 11 13 ABXA9800950 1 19980910 A 5320 4641324501 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1690 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING AT STATION 1690, LONGERON 26L IS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998111301237 19981113 01237 WP 1998 11 13 ABXA9800951 1 19980910 A 5320 57533061 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 980-1000 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 END FITTING CRACKED AT STATION 980 TO 1000, STRINGER 23L. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301238 19981113 01238 WP 1998 11 13 ABXA9800952 1 19980910 A 5712 576946620 RIB DOUG DOUG DC8 DC861 3021952 WP WS 628.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END, STATION XFS 628.750. REPAIRED IAW DWG KO5056 AND DC8 SRM 5 7-2-0. 2 L 7 4 4F 4A25 1998111301239 19981113 01239 WP 1998 11 13 ABXA9800953 1 19980910 A 5712 576946622 RIB DOUG DOUG DC8 DC861 3021952 WP WS 635 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END, STATION XFS 635.000. REPAIRED IAW DWG KO5056 AND DC8 SRM 5 7-2-0. 2 L 7 4 4F 4A25 1998111301240 19981113 01240 WP 1998 11 13 ABXA9800954 1 19980910 A 5320 3755172501 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1170 & 1190 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 STATION 1170 AND 1190 AT LONGERON 33R TWO T-BOLT FITTINGS ARE CORRODED ON THE BOTTOM. REPLACED FITTINGS IAW DC8 SRM 51- 3-0 AND 51-1-20D. 2 L 7 4 4F 4A25 1998111301241 19981113 01241 WP 1998 11 13 ABXA9800955 1 19980910 A 5320 37558452N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1228 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT STATION 1228 BETWEEN LONGERONS 33L TO 34L. REPLACED FITTING IAW DC8 SRM 53-20 AND 51-1-20. 2 L 7 4 4F 4A25 1998111301242 19981113 01242 WP 1998 11 13 ABXA9800956 1 19980904 A 5320 37502571N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 600-620 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON SPLICE FITTING IS CRACKED AT STATION 600 TO 620 STRINGER 31L. REPLACED FITTING IAW DC8 DWG 3750257 AND SRM 51- 1-20D. 2 L 7 4 4F 4A25 1998111301243 19981113 01243 WP 1998 11 13 ABXA9800957 1 19980904 A 5320 37502571N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 440-460 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 31R SPLICE FITTING IS CRACKED AT STATION 440 TO 460. REPLACED FITTING IAW DC8 SRM 51-1-20D AND DWG 3750257. 2 L 7 4 4F 4A25 1998111301244 19981113 01244 WP 1998 11 13 ABXA9800958 1 19980904 A 5712 5769545 RIB DOUG DOUG DC8 DC861 3021952 WP WS 728.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT LEADING EDGE UPPER RIB IS CRACKED AT AFT END AT STATION XFS728.750. REPAIRED IAW DC8 DWG KO5056. 2 L 7 4 4F 4A25 1998111301245 19981113 01245 WP 1998 11 13 ABXA9800959 1 19980908 A 5730 5611340 SKIN DOUG DOUG DC8 DC861 3021952 WP WS 74 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING SKIN (TOP) AT STATION XRS 74.00 AND STRINGER 9 CRACKED. REPAIRED IAW DC8 SRM 57-2-1. 2 L 7 4 4F 4A25 1998111301246 19981113 01246 WP 1998 11 13 ABXA9800960 1 19980904 A 5712 5769545 RIB DOUG DOUG DC8 DC861 3021952 WP WS 733 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END AT STATIONS XFS 733.000. REPAIRED IAW DC8 DWG K05056. 2 L 7 4 4F 4A25 1998111301247 19981113 01247 WP 1998 11 13 ABXA9800961 1 19980904 A 5712 5769545 RIB DOUG DOUG DC8 DC861 3021952 WP WS 678.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING LEADING EDGE UPPER RIB IS CRACKED AT THE AFT END AT STATION XRS678.750. REPAIRED IAW DC9 SRM 57-20. 2 L 7 4 4F 4A25 1998111301248 19981113 01248 WP 1998 11 13 ABXA9800962 1 19980910 A 5320 3779874505 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 940 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT STATION 940 LONGERON 18L. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301249 19981113 01249 WP 1998 11 13 ABXA9800974 1 19981109 A 3260 UNSAFE LIGHT DOUG DC8 DC861 3021952 WP LANDING GEAR ILLUMINATED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 844AX 45848 ON GEAR RETRACTION, RED GEAR UNSAFE WARNING LIGHT ILLUMINATED. RECYCLED GEAR, UNSAFE LIGHT ILLUMINATED. PERFORMED SYST EM TEST IAW DC8 MM 32-60-00. ALL SYSTEMS CHECKED NORMAL. 2 L 7 4 4F 4A25 1998111301250 19981113 01250 WP 1998 11 13 ABXA9800975 1 19980921 A 5320 3779979506 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 857 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED FITTING AT LONGERON 13L, STATION 857. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301251 19981113 01251 WP 1998 11 13 ABXA9800976 1 19980921 A 5720 36433192 STIFFENER DOUG DOUG DC8 DC861 3021952 WP WS 98 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING TRAILING EDGE AT STATION XW98, VERTICAL STIFFENER IS CRACKED AT THE BOTTOM. REPAIRED IAW DC8 SRM 51-1-20D AN D 51-3-0. 2 L 7 4 4F 4A25 1998111301252 19981113 01252 WP 1998 11 13 ABXA9800977 1 19980920 A 5320 975494941 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 1120-1140 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 STATION 1120 TO 1140 AT STRINGER 33R, INTERCOSTAL HAS HEAVY CORROSION AND CRACKING. REPAIRED IAW DWG 9754949 AND DC8 SR M 51-1-20D, 51-3-0, AND 51-1-8. 2 L 7 4 4F 4A25 1998111301253 19981113 01253 WP 1998 11 13 ABXA9800978 1 19980918 A 5320 37501602 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT LONGERON 19L, STATION 680. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301254 19981113 01254 WP 1998 11 13 ABXA9800979 1 19980917 A 5320 47799401 SPLICE DOUG DOUG DC8 DC861 3021952 WP BS 610 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 BUTT SPLICE EXFOLIATED AT AFT END, STATION 610 AT LONGERON 31L. REPLACED SPLICE IAW DC8 SRM 51-1-20. 2 L 7 4 4F 4A25 1998111301255 19981113 01255 WP 1998 11 13 ABXA9800980 1 19980917 A 5320 5779915 DOUBLER DOUG DOUG DC8 DC861 3021952 WP BS 1350 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FINGER DOUBLER CORRODED BEYOND LIMITS AT STATION 1350, LONGERON 31L. REPLACED FINGER DOUBLER IAW DC8 SRM 53-4-1. 2 L 7 4 4F 4A25 1998111301256 19981113 01256 WP 1998 11 13 ABXA9800981 1 19980917 A 5320 3755822 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1200 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CORRODED AT STATION 1200, LONGERON 34R. REPLACED FITTING IAW DC8 SRM 53-2-0 AND 51-1-21D. 2 L 7 4 4F 4A25 1998111301257 19981113 01257 WP 1998 11 13 ABXA9800982 1 19980917 A 5320 570440823 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 1460-1480 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERCOSTAL AT STATION 1460 TO 1480 STRINGER 3L IS CRACKED. INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5704408 AND DC8 S RM 51-1-20D. 2 L 7 4 4F 4A25 1998111301258 19981113 01258 WP 1998 11 13 ABXA9800983 1 19980912 A 5320 3647390502 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED END FITTING AT STATION 680 LONGERON 14L. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3647390. 2 L 7 4 4F 4A25 1998111301259 19981113 01259 WP 1998 11 13 ABXA9800984 1 19980904 A 5320 37558451N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED FITTING AT LONGERON 35L, STATION 1200. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301260 19981113 01260 WP 1998 11 13 ABXA9800964 1 19980914 A 5311 56157453 FRAME DOUG DOUG DC8 DC861 3021952 WP BS 80 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 STATION 80 FRAME CRACKED AT LONGERON 6L AND 8L. REPAIRED IAW DC8 SRM 51-1-21 AND DRW K04888. 2 L 7 4 4F 4A25 1998111301261 19981113 01261 WP 1998 11 13 ABXA9800965 1 19980914 A 5320 3754220503 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 200-220 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 31L SPLICE FITTING CRACKED STATION 200 TO 220. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301262 19981113 01262 WP 1998 11 13 ABXA9800966 1 19980914 A 5320 3779874523 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 940 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT LONGERON 19L, STATION 940. REPAIRED IAW DWG 3779874 AND DC8 SR, 51-1-20D. 2 L 7 4 4F 4A25 1998111301263 19981113 01263 WP 1998 11 13 ABXA9800967 1 19980914 A 5320 47504221 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 857 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERCOSTAL FITTING CRACKED AT STATION 857 LONGERON 19R. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301264 19981113 01264 WP 1998 11 13 ABXA9800968 1 19980914 A 5320 3779874505 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 940 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT LONGERON 20L STATION 940. REPAIRED IAW DC8 SRM 51-1-11. 2 L 7 4 4F 4A25 1998111301265 19981113 01265 WP 1998 11 13 ABXA9800969 1 19980914 A 5320 3750330523 SPLICE DOUG DOUG DC8 DC861 3021952 WP BS 450 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FORWARD LOWER CARGO PRODUCTION SPLICE LONGERON 36 CRACKED AT AFT FASTENER HOLE, STATION 450. INSTALLED LONGERON SPLICE REPAIR IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301266 19981113 01266 WP 1998 11 13 ABXA9800970 1 19980914 A 5320 37558451N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1150 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING HAS HEAVY CORROSION AT STATION 1150, LONGERON 34L TO 35L. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301267 19981113 01267 WP 1998 11 13 ABXA9800971 1 19980907 A 5320 47504191 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1160-1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED FITTING INSIDE TORQUE BOX BETWEEN STATION 1180 TO 1160, LONGERON 19R. INSTALLED NEW FITTING AT STATION 1180, LO NGERON 19R IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301268 19981113 01268 WP 1998 11 13 ABXA9800972 1 19980908 A 5320 4750418 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 1155 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT STATION 1155, LONGERON 19R. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301269 19981113 01269 WP 1998 11 13 ABXA9800973 1 19980908 A 5320 564340218 STIFFENER DOUG DOUG DC8 DC861 3021952 WP BS 940 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WHEEL WELL OUTBOARD WEB STATION 940 VERTICAL STIFFENER CRACKED. REPAIRED IAW DC8 SRM 51-1-21. 2 L 7 4 4F 4A25 1998111301270 19981113 01270 WP 1998 11 13 ABXA9800996 1 19981110 A 5610 5613217517 WINDOW DOUG DC8 DC861 3021952 WP LT COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 851AX 45940 CAPTAIN'S SLIDING WINDOW (EMERG EXIT) WOULD NOT OPEN. ADJUSTED LOWER, AFT HOOK FITTING IAW DC8 MM 56-10-03. OPS CHECKE D GOOD. 2 L 7 4 4F 4A25 1998111301271 19981113 01271 WP 1998 11 13 ABXA9800985 1 19980908 A 5313 5250322 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1348 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 34L CRACKED AT STATION 1348. REPLACED LONGERON 34L FROM STATION 1260 TO 1350 IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301272 19981113 01272 WP 1998 11 13 ABXA9800986 1 19980907 A 5320 3779978 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1020 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT STATION 1020, LONGERON 20L. REPLACED FITTING AT STATION 1020, LONGERON 20L IAW DC8 SRM 5 1-1-20D. 2 L 7 4 4F 4A25 1998111301273 19981113 01273 WP 1998 11 13 ABXA9800987 1 19980909 A 5320 37558451N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1150 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 TORQUE BOX FITTING CRACKED AT LONGERON 35R, STATION 1150. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301274 19981113 01274 WP 1998 11 13 ABXA9800988 1 19980912 A 5320 37558412 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1230 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT STATION 1230 BETWEEN LONGERON 36-35L. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301275 19981113 01275 WP 1998 11 13 ABXA9800989 1 19980905 A 5320 37558401 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1220 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 DEEP PITTING CORROSION AT STATION 1220, LONGERON 33R. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301276 19981113 01276 WP 1998 11 13 ABXA9800990 1 19980911 A 5320 3779874506 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERCOSTAL TIE FITTING CRACKED AT STATION 960, LONGERON 18L. REPLACED FITTING IAW DWG 3779874 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301277 19981113 01277 WP 1998 11 13 ABXA9800991 1 19980909 A 5320 4641326N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1690 BROKEN A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 BROKEN END FITTING AT STATION 1690, LONGERON 23R. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301278 19981113 01278 WP 1998 11 13 ABXA9800992 1 19980905 A 5320 3755845N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1180 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED ON CROSS SLIDE DOOR AT LONGERON 35R, STATION 1180. INSTALLED NEW FITTING AT STATION 1180 LONGERON 35R I AW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301279 19981113 01279 WP 1998 11 13 ABXA9800993 1 19980809 A 5313 5750322 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1260-1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 STATION 1260 TO 1280 STRINGER 34R CRACKED ON BOTTOM INBOARD FLANGE. REPLACED LONGERON 34R FROM STATION 1260 TO 1350 IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301280 19981113 01280 WP 1998 11 13 ABXA9800994 1 19980809 A 5313 5750322 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1260-1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 STATION 1260 TO 1280 STRINGER 35L, BOTTOM OUTBOARD FLANGE CRACKED. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998111301281 19981113 01281 WP 1998 11 13 ABXA9800995 1 19981107 A 3350 5708458503 BATTERY PACK DOUG DC8 DC863 302198A WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 816AX 46093 EMERGENCY LIGHTS WOULD NOT DISARM. REPLACED THE EMERGENCY LIGHT BATTERY PACK. 2 L 7 4 4F 4A25 1998111301282 19981113 01282 WP 1998 11 13 MWEA981041 1 19981110 A 5315 9958185 FLOORBEAM DOUG DC9 DC915 3022036 WP BS 351 GOUGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FLOORBEAM AT FS 351 BUTT LINE 0 WAS FOUND GOUGED. REMOVED DAMAGE FABRICATED FILLERS AND REPAIR ANGLES INSTALLED REPAIR PIECES ON FLOORBEAM. 2 L 7 2 4F A6WE 1998111301283 19981113 01283 WP 1998 11 13 MWEA981042 1 19981110 A 5751 5910045 SKIN DOUG DC9 DC915 3022036 WP LT AILERON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT AILERON LOWER SKIN WAS FOUND CRACKED AROUND A PREVIOUS REPAIR. REMOVED OLD REPAIR AND DAMAGED SKIN FABRICATED FILL ERS AND DOUBLERS INSTALLED REPAIR SECTIONS OF SKIN. 2 L 7 2 4F A6WE 1998111301284 19981113 01284 WP 1998 11 13 MWEA981043 1 19981110 A 5347 5910152 SEAT TRACK DOUG DC9 DC915 3022036 WP BS 480-499 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT INBOARD SEAT TRACK AT FS 480 TO 499 HAS SEVERAL AREAS OF DAMAGE. REMOVED DAMAGED AREAS FABRICATED REPAIR FILLERS A ND STRAPS INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 1998111301285 19981113 01285 WP 1998 11 13 MWEA981044 1 19981110 A 5510 3912060 FITTING DOUG DC9 DC915 3022036 WP HORIZ STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 HORIZONTAL STAB PIVOT FITTING AT THE TOP OF THE VERTICAL STAB WAS FOUND CORRODED. REMOVED CORRODED FITTING AND INSTALLE D NEW FITTING. 2 L 7 2 4F A6WE 1998111301286 19981113 01286 WP 1998 11 13 MWEA981045 1 19981110 A 5720 5912437 DOUBLER DOUG DC9 DC915 3022036 WP LT WING CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT WING TOP TRUNNION FITTING DOUBLER WAS FOUND CRACKED. REMOVED CRACKED AREA AND INSTALLED AERODYNAMIC FILLER. 2 L 7 2 4F A6WE 1998111301287 19981113 01287 WP 1998 11 13 MWEA981046 1 19981110 A 5400 49198641 FITTING DOUG DC9 DC915 3022036 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 CRACKS FOUND LEFT PYLON REAR SPAR UPPER CAP ATTACH FITTING. REMOVED AND REPLACED CRACKED FITTING. 2 L 7 2 4F A6WE 1998111301288 19981113 01288 WP 1998 11 13 MWEA981047 1 19981110 A 5330 5911408507 SKIN DOUG DC9 DC915 3022036 WP BS 281 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT FUSELAGE SKIN HAS STATIC DISCHARGE BEYOND LIMITS. MTC FABRICATED AND INSTALLED REPAIR DOUBLER FINGER DOUBLER STRAP AND FILLER. 2 L 7 2 4F A6WE 1998111301289 19981113 01289 WP 1998 11 13 MWEA981048 1 19981110 A 5315 9958188 FLOORBEAM DOUG DC9 DC915 3022036 WP BS 804 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FLOORBEAM AT STATION 804 WAS FOUND CORRODED FROM BOTTLINE R14 TO R24. REMOVED DAMAGE SECTIONS, FABRICATED REPAIR ANGLES AND FILLERS, INSTALLED REPAIR ANGLES AND FILLERS ON BEAM. 2 L 7 2 4F A6WE 1998111301290 19981113 01290 WP 1998 11 13 MWEA981049 1 19981110 A 5313 2777922 LONGERON DOUG DC9 DC915 3022036 WP BS 806-817 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LONGERON 20 RIGHT WAS FOUND CORRODED FROM FS 806 TO 817. REMOVED DAMAGED SECTION OF LONGERON, OBTAINED SERVICEABLE REPL ACEMENT PART, INSTALLED SERVICEABLE SECTION OF LONGERON. 2 L 7 2 4F A6WE 1998111301291 19981113 01291 WP 1998 11 13 MWEA981050 1 19981110 A 5320 99581703 INTERCOSTAL DOUG DC9 DC915 3022036 WP BS 738 & 756 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 INTERCOSTAL BETWEEN FS 738 AND 756 AT BL 0 DAMAGED BETWEEN FLOORBEAMS. REMOVED DAMAGED INTERCOSTAL STA 758 TO 756, DRIL LED FASTENER HOLES IN NEW INTERCOSTAL AND INSTALLED. 2 L 7 2 4F A6WE 1998111301292 19981113 01292 WP 1998 11 13 DLL14982245 1 19981101 A 2120 AIR DIST LKHEED 1011 1011385115 5265015 WP CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 736DY 193C1227 ON DESCENT, PAX IN 42AB SMELLED SMOKE. UPON FURTHER INVESTIGATION BY FLT ATTEND, ELECTRICAL SMELLING SMOKE CONFIRMED AT 42AB AND BY DOORS 3L AND 3R. THE SMELL DISSIPATED ON DESCENT BUT STILL LINGERED. INSPECTED LIGHTS, NO PROBLEMS FOUND. 2 L 7 3 4F A23WE 1998111301293 19981113 01293 NM 1998 11 13 DL72S982252 1 19981031 A 2530 5374AD COFFEEMAKER BOEING 727 727232 1384082 NM AFT GALLEY FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 536DA 22049 INDICATION OF SMOKE OBSERVED BY FLT ATTEND IN AFT GALLEY AND AFT CABIN. REPLACED COFFEEMAKER AND CANNON PLUG. 2 L 7 3 4F A3WE 1998111301294 19981113 01294 NM 1998 11 13 DL72S982253 1 19981012 A 5753 652163261 SKIN BOEING 727 727232 1384082 NM LT TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 DURING SHOP INSP, THE COVE SKIN WAS FOUND CRACKED AT THE I/B AFT CORNER OF I/B AFT FLAP DRIVE ROD CUTOUT. THE SKIN WAS REPAIRED BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER PER MM 57-52-0, FIG 09. 2 L 7 3 4F A3WE 1998111301295 19981113 01295 NM 1998 11 13 DL72W982254 1 19981101 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM DOOR L2 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 292WA 22110 ON L/O, FOUND EMERGENCY EXIT LIGHT OVER DOOR L2 INOP. REPLACED BATTERY PACK, OPS CKS NORMAL. 2 L 7 3 4F A3WE 1998111301296 19981113 01296 NM 1998 11 13 DLM88982255 1 19981102 A 3297 WIRE MD88M DOUG MD88 MD88 3023688 NM LT MLG DAMAGED A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 915DL WHEELDL100 49546 AT GEAR EXTENTION LT MAIN INDICATED UNSAFE. FOLLOWED CHECK LIST PROCEDURES. LDG GEAR CYCLED ONCE, NO HELP. FOUND CON DUIT AND WIRING FOR MLG DOWN SENSE TORN DUE TO NR 2 TIRE FAILURE. REPLACED SAME. ALSO, REPLACED NR 1 AND NR 2 WHEEL/TI RE ASSEMBLIES. ALSO, FOUND DOWNLOCK BUNGEE SPRING AND RT SPRAY DEFLECTOR DAMAGED. REPLACED BOTH UNITS. NO DAMAGE TO O THER AREAS. OPS CHECKS NORMAL. 2 L 7 2 4F RT A6WE 1998111301297 19981113 01297 NM 1998 11 13 DLM88982257 1 19981103 A 2910 31914904 O-RING DOUG MD88 MD88 3023688 NM RT HYD SYST FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 997DL 53364 RIGHT HYDRAULIC QUANTITY DECREASED TO 4 QTS IN FLIGHT WITH AMBER WARNING LIGHT ON INDICATOR. PROCEDURES FOLLOWED AND S YSTEM TURNED OFF UNTIL PRIOR TO LANDING. AFTER LANDING RIGHT QUANTITY INDICATED 2 QTS WITH NORMAL PRESSURE. FOUND PRES SURE LINE TO RUDDER POWER PACK LEAKING AT UNION. REPLACED O-RING, SERVICED RT SYSTEM AND LEAK OPS CHECK OK. 2 L 7 2 4F RT A6WE 1998111301298 19981113 01298 NM 1998 11 13 DLM88982261 1 19981103 A 3350 CONNECTOR BR9279103 DOUG MD88 MD88 3023688 NM TAIL COMPT DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 912DL 49543 EMERGENCY LIGHTING ON WALL IN TAIL COMPARTMENT INOP. REMOVED LIGHT ASSY, FOUND WIRING PULLED FROM CONNECTORS. INSTALLE D NEW CONNECTORS AND REINSTALLED LIGHT ASSY, LIGHT OPS CKS NORMAL. 2 L 7 2 4F RT A6WE 1998111301299 19981113 01299 NM 1998 11 13 DL73K982264 1 19981102 A 5330 SKIN BOEING 737 737232 1384475 NM BS 740 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 THE FUSELAGE SKIN AT FS 740 WAS FOUND WITH A 1.25 INCH LONG CRACK BELOW STRINGER 18R. THE CRACK WAS REPAIRED PER THE B7 37-200 SRM 53-30-3 FIG 1. THE REPAIR DOUBLER EXTENDS UNDER THE WING TO BODY FAIRING, SO INFRINGES ON SSI F-41. THE REP AIR HAS BEEN DOCUMENTED PER ER/A 366006-14 AND REQUIRES A DTA WITHIN 12 MONTHS. 2 L 7 2 4F RT A16WE 1998111301300 19981113 01300 NM 1998 11 13 DL73K982266 1 19981031 A 5330 SKIN BOEING 737 737232 1384475 NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 313DL 23085 THE FUSELAGE SKIN AND DOUBLER WERE FOUND TO HAVE A 1.5 INCH TYPICAL CRACK AT THE LOWER AFT CORNER OF THE R1 DOOR CUTOUT. THE CRACK WAS REPAIRED PER THE B737-200 SRM 53-30-3 FIG 26, EXCEPT BLIND BOLTS WERE AUTHORIZED ON A TIME LIMITED BASIS . THE REPAIR WAS ACCOMPLISHED PER ER/A 365981-14, REV A. 2 L 7 2 4F RT A16WE 1998111301301 19981113 01301 WP 1998 11 13 DLL19982267 1 19981031 A 5330 1542249101 SKIN LKHEED 1011 10113853 5265020 WP BS 1745-1776 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 756DR 193Y1185 THE FUSELAGE SKIN WAS FOUND WITH THREE AREAS OF CORROSION BETWEEN FS 1745 AND 1776 BETWEEN S-31 AND 33. THE CORROSION R EMOVAL RESULTED IN THREE CUTOUTS SIZED 6 X 5, 5 X 4 AND 2 X 2. THE SKIN CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL A LUMINUM DOUBLER AND TRIPLER REPAIR PER ER/A 365961-14, REV A. 2 L 7 3 4F A23WE 1998111301302 19981113 01302 NM 1998 11 13 DL73K982268 1 19981103 A 5241 6545871523 HINGE BOEING 737 737232 1384475 NM R1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 THE LOWER GATE HINGE ON THE R1 DOOR WAS FOUND CRACKED. THE CRACKED HINGE WAS REMOVED AND REPLACED PER THE REQUIREMENTS OF BAC S/B 737-52A1124. THE REPAIR WAS DOCUMENTED PER ER/A 366007-14AD. 2 L 7 2 4F RT A16WE 1998111301303 19981113 01303 NM 1998 11 13 DLM88982270 1 19981104 A 2120 AIR DIST DOUG MD88 MD88 3023688 NM CABIN SMOKE A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 909DL 49540 FLIGHT ATTENDENTS REPORTED SMOKE ODOR IN REAR TO MID CABIN AREA DURING TAKEOFF AS A/C WAS PASSING 6000 FT IN CLIMB. POW ER SET AT CLIMB SETTING, NO ABNORMAL ENG READINGS. ODOR DISSIPATED AFTER POWER REDUCED TO IDLE TO LAND IN ATL. INSPECT ED APU AREA, NO ABNORMALITIES FOUND. PERFORMED DUCT BURN OUT. 2 L 7 2 4F RT A6WE 1998111301304 19981113 01304 NM 1998 11 13 DL72S982271 1 19981104 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 FOUND AT C1 LETTER CK, .5 INCH VISIBLE CRACK IN AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER STOP CASTING. REPAIRED PER SRM 53-10-9 FIG 11. 2 L 7 3 4F A3WE 1998111301305 19981113 01305 NM 1998 11 13 DL72S982272 1 19981104 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 913 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 FOUND ON C1 LETTER CK, STA 913 ANGLE CRACKED O/B END OF LT WHEEL WELL. REPAIRED PER MM 53-11-0. 2 L 7 3 4F A3WE 1998111301306 19981113 01306 NM 1998 11 13 DL72S982273 1 19981104 A 5754 RIB BOEING 727 727232 1384082 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 FOUND ON C1 LETTER CK, NR 4 SLAT L/E NOSE RIB I/B SIDE OF ACTUATOR CRACKED .5 INCH. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998111301307 19981113 01307 NM 1998 11 13 DL72S982275 1 19981105 A 5754 RIB BOEING 727 727225 1384077 NM NR 4 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FOUND ON A1 LETTER CK, 1 INCH CRACK L/E RIB O/B OF ACTUATOR ON NR 4 SLAT. REPAIRED PER MM 57-54-0 AND ERA 366036-14. 2 L 7 3 4F A3WE 1998111301308 19981113 01308 NM 1998 11 13 DL72S982276 1 19981105 A 5320 WEB BOEING 727 727225 1384077 NM BS 1223 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FOUND ON A1 LETTER CK, 1 INCH CRACK LT TORQUE BOX VERTICAL WEB FWD OF STA 1223. REPAIRED PER MM 53-11-0 AND ERA 366033- 14. 2 L 7 3 4F A3WE 1998111301309 19981113 01309 NM 1998 11 13 DL72S982277 1 19981105 A 5320 WEB BOEING 727 727225 1384077 NM BS 1283 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8882Z 21579 FOUND ON A1 LETTER CK, .5 INCH CRACK LT LOWER TORQUE BOX VERTICAL WEB STA 1283. REPAIRED PER MM 53-11-0 AND ERA 366033- 14. 2 L 7 3 4F A3WE 1998111301310 19981113 01310 NM 1998 11 13 DL767982222 1 19981026 A 2120 AIR DIST BOEING 767 767232 1385132 NM CABIN SMOKE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 113DA 22225 F/A REPORTED SMOKE IN AFT CABIN. UPON DISCONNECTING UTILITY BUSES ODOR/SMELL WENT AWAY. RESET UTILITY BUSES OPERATED A LL GALLEY EQUIPMENT, NO ODOR PRESENT. RAN PACK RECIRC FANS AND GASPER FANS, TURNED ON ALL LIGHTS AND VIDEO EQUIPMENT AN D NO TROUBLE FOUND. 2 L 7 2 4F RT A1NM 1998111301311 19981113 01311 NM 1998 11 13 DL72S982231 1 19981029 A 2930 MODULE 65178229 BOEING 727 727232 1384082 NM B HYD SYST LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 542DA 2274 22391 IN ROUTE, LOSS OF SYS -B- PRESS ENGAGED NR 2 -B- PUMP BOTH LOW PRESS LIGHTS ILLUMINATED. SYS -B- QTY READS ZERO, SYS -A- QTY READS 2 GAL. ACCOMPLISHED POM HYD SYS -B- LOSS PROCEDURE, NORM BRAKING USED FOR LANDING. UPON INSPECTION, FOUND - B- SYSTEM PRESSURE MODULE LEAKING. REPLACED -B- SYSTEM PRESSURE MODULE, LK CKS GOOD. 2 L 7 3 4F A3WE 1998111301312 19981113 01312 NM 1998 11 13 DL76L982232 1 19981004 A 3610 212T30087 INSULATION BOEING 767 767332 1382001 NM BS 1373 TORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 THE APU PNEUMATIC DUCT INSULATION WAS FOUND CHAFED THRU BETWEEN FS 1373 AND FS 1439 BY THE FIRE EXTINGISHER DISCHARGE LI NE, THE FIRE EXTINGUISHER DISCHARGE LINE INSULATION WAS FOUND DAMAGED. THE APU DUCT INSULATION (P/N 212T3008-7) AND FIR E EXTINGUISHER DISCHARGE LINE INSULATION (P/N R180FS) WAS REPLACED AND THE FIRE EXTINGUISHER DISCHARGE LINE WAS REPOSITI ONED TO PROVIDE CLEARANCE TO MINIMIZE CHAFING. 2 L 7 2 4F RT A1NM 1998111301313 19981113 01313 NM 1998 11 13 DL72K982236 1 19981029 A 2782 FITTING BOEING 727 727232 1384082 NM NR 7 SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 O/B SUPPORT FOR ACTUATOR FITTING LOBE CRACKED AT NR 7 SLAT. REPAIRED PER MM 57-42-0. 2 L 7 3 4F A3WE 1998111301314 19981113 01314 NM 1998 11 13 DL76G982239 1 19981030 A 3320 LIGHT 190611 BOEING 767 7673P6 1385105 NM MID GALLEY OVERHEATED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 154DL 25241 BURNING SMELL FROM AUX GALLEY AT R2 DOOR. PULLED AND COLLARED C/B FOR COUNTER LIGHTS. SUBMITTER SUSPECTS BALLAST, FWD TO MCO. 2 L 7 2 4F RT A1NM 1998111301315 19981113 01315 WP 1998 11 13 DLL10982240 1 19981030 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP 1L DOOR DISCHARGED A DALA K NONE L NO TEST CR CRUISE 1 SO 27 1734D 61464 193C1225 FWD EMER EXIT LIGHTS ILLUM TWICE DURING FLIGHT. FOUND BATTERY PACK AT 1L DOOR OPS INTERMITTENTLY. REPLACED SAME, OPS C K GOOD. 2 L 7 3 4F A23WE 1998111301316 19981113 01316 NM 1998 11 13 DL72S982241 1 19981031 A 2530 CONNECTOR 257005763 BOEING 727 727232 1384082 NM GALLY SHORTED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 536DA 22049 SMOKE IN AFT CABIN. FOUND THE CANNON PLUG FOR THE NR 3 COFFEEMAKER IN THE AFT GALLY SHORTED. PULLED AND COLLARD C/B, D ISCONNECTED CANNON PLUG FROM COFFEEMAKER. 2 L 7 3 4F A3WE 1998111301317 19981113 01317 NM 1998 11 13 DL72S982242 1 19981031 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 469DA WA7426 20746 RT WING INTERIOR EMERGENCY EXIT LIGHTS TEST OK BUT DO NOT OPERATE IN THE ARMED POSITION. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998111301318 19981113 01318 NM 1998 11 13 DL72S982244 1 19981101 A 2121 FAN 215201 BOEING 727 727232 1384082 NM AIR COND BAY FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 525DA AA7773 21585 BURNING SMELL COMING FORM GASPERS. PAX NOTICED SMELL WHICH QUICKLY DISSAPATED. AFTER ARRIVING AT GATE GASPER FAN CB WA S FOUND OPEN. ALSO, PAX REPORT SMOKE WAS VISIBLE AROUND AIR EYELETS AT ROWS 16, 17, 18 SMOKE HAD A PLASTIC SMELL. SMOK E STOPPED AND DISIPATED QUICKLY. NO FURTHER PROBLEMS AFTER T/O. REPLACED GASPER FAN. 2 L 7 3 4F A3WE 1998111301319 19981113 01319 NM 1998 11 13 DL72W982250 1 19981101 A 3350 900835A BATTERY BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2812W 20868 EMERGENCY LIGHT BATTERY PACK INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998111301320 19981113 01320 NM 1998 11 13 DL757982279 1 19981106 A 2781 ELECT UNIT 285T0012118 BOEING 757 757232 1384965 NM E/E COMPT FAILED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 677DL 763 25982 L/E SLAT DISAGREE LIGHT ILLUMINATED DURING FLAP RETRACTION ON DEPARTURE. FLAP IND STUCK BETWEEN 0 AND 1. PERFORMED POM PROCEDURE, NO HELP. RESET LT I/B ROTARY ACTUATOR OVERLOAD IND PIN AND REPLACED FLAP/SLAT ELECT UNIT. OP FLAPS/SLATS S EVERAL TIMES, OPS NORMAL. 2 L 7 2 4F RT A2NM 1998111301321 19981113 01321 NM 1998 11 13 DL72S982280 1 19981104 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 520DA 21471 DURING C-1 LETTER CHECK, .5 INCH VISIBLE CRACK IN AFT ENTRY DOOR CUTOUT LT FRAME AT SECOND FROM UPPER STOP CASTING. REP AIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1998111301322 19981113 01322 NM 1998 11 13 DL72S982282 1 19981106 A 5712 652163362 RIB BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 DURING SHOP INSPECTION, A REPAIR DOUBLER AT THE I/B AFT RIB WAS FOUND TO BE CRACKED. THE DOUBLER WAS REMOVED AND THE RI B WAS REPAIRED PER MM 57-52-0 FIG 808. 2 L 7 3 4F A3WE 1998111301323 19981113 01323 NM 1998 11 13 DL757982283 1 19981106 A 2530 OVEN 831620403 BOEING 757 757232 1384965 NM GALLEY FUMES A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 693DL 0194 29725 FWD CABIN ATTENDENTS REPORTED FUMES. REPLACED F/C OVEN. 2 L 7 2 4F RT A2NM 1998111301324 19981113 01324 NM 1998 11 13 DL73E982284 1 19981106 A 3230 LINE 000AE954D02 BOEING 737 737247 138448D NM NLG LEAKING A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 244WA 23518 AFTER TAKEOFF, THE NOSE GEAR INDICATED UNSAFE. BOTH RED AND GREEN LIGHT WITH THE GEAR HANDLE IN UP POSITION. FURTHER I NSPECTION REVEALED THE A SYSTEM HYD RAULIC DECREASING RAPIDLY TO ZERO. THE POM C/W AND LANDING MADE. ALL GEAR AND FLAP INDICATION WERE NORMAL. REPLACED PRESS LINE TO LOCK RETRACT ACTUATOR. 2 L 7 2 4F A16WE 1998111301325 19981113 01325 NM 1998 11 13 DL73K982285 1 19981106 A 2612 6937307139 MODULE BOEING 737 737232 1384475 NM COCKPIT FAILED A DALA A UNSCHED LANDING L NO TEST CR CRUISE 1 SO 27 311DL 23083 COCKPIT FIRE CONTROL PANEL SHORTED. POPPING NOISE COMING FROM PEDESTAL AREA. REMOVED AND REPLACED ENG/APU FIRE CONTROL MODULE. 2 L 7 2 4F RT A16WE 1998111301326 19981113 01326 NM 1998 11 13 DL72S982286 1 19981107 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CABIN WEAK A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 520DA 14374 21471 ON PREFLIGHT, CREW REPORTED AFT EMER EXIT LIGHT FLASHING. REPLACED BATT PACK, OPER OK. 2 L 7 3 4F A3WE 1998111301327 19981113 01327 NM 1998 11 13 DL72S982287 1 19981107 A 2530 COFFEEMAKER 5374E BOEING 727 727232 1384082 NM GALLEY FAILED A DALA K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 418DA 2050 21271 ELECTRICAL BURNING SMELL EMITTING FROM F/C GALLEY. REPLACED F/C COFFEEMAKER AND CANNON PLUG. 2 L 7 3 4F A3WE 1998111301328 19981113 01328 NM 1998 11 13 DL76G982288 1 19981107 A 3040 TERMINAL BOEING 767 7673P6 1385105 NM LT WINDOW LOOSE A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 152DL 24984 STRONG SMELL OF SMOKE, LOWER CORNER OF CAPTS FWD WIND SCREEN VERY HOT. TURNED OFF WINDOW HEAT AND SMELL WENT AWAY. FOU ND TERMINAL FOR LOWER CORNER LOOSE AND ARCING. CLEANED TERMINAL AND TIGHTENED SCREW. FOUND NO DAMAGE TO WINDOW AND NO FAULTS ON WINDOW HEAT CONTROLLER, ALL CHECKS NORMAL. 2 L 7 2 4F RT A1NM 1998111301329 19981113 01329 NM 1998 11 13 DL72S982290 1 19981107 A 5320 ANGLE BOEING 727 727232 1384082 NM BS 1263 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 521DA 21472 HORIZ TORQUE BOX ANGLE CRACKED STA 1263 BELOW FWD END OF ACTUATOR PAD. HORIZ GUSSET ANGLE CRACKED STA 1263 BELOW ACTUAT OR PAD. REPLACED ANGLE AND GUSSET PER SRM 53-10-10 FIG 1-3. 2 L 7 3 4F A3WE 1998111301330 19981113 01330 NM 1998 11 13 DLM11982294 1 19981108 A 2550 CONTROL UNIT 141VK1R214B DOUG MD11 MD11 3023602 NM CARGO COMPT FAILED A DALA H DEACTIVATE SYST/CIRCUITS A FLAME/FIRE IN INSP/MAINT 1 SO 27 811DE 48566 DURING TRIP CHECK, SMOKE AND FUMES SMELLED BY MTC AT SEAT 12A. FOUND SHORTED WIRE TO CARGO ROLLER IN FWD CARGO CAUSED F IRE IN CONTROLLER UNIT WHICH IGNITED MYLAR INSULATION BLANKET. REPLACED CONTROLLER UNIT, WIRING AND INSULATION BLANKET. 2 L 7 3 4F RT A22WE 1998111301331 19981113 01331 NM 1998 11 13 DL72S982298 1 19981108 A 3350 S106 BATTERY BOEING 727 727232 1384082 NM L2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 485DA 20865 EMERGENCY LIGHTS L2 DOOR DID NOT TEST ON LAYOVER. REPLACED BATTERIES, NOW TESTS NORMAL. 2 L 7 3 4F A3WE 1998111301332 19981113 01332 NM 1998 11 13 DL72S982299 1 19981108 A 3350 RPS1 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 408DA 21152 FIRST CLASS EMERGENCY LIGHTS INOP. REPLACED BATTERY PWR SUPPLY, NOW CKS GOOD. 2 L 7 3 4F A3WE 1998111301333 19981113 01333 NM 1998 11 13 DL76L982300 1 19981109 A 5411 311T311021 SPAR WEB BOEING 767 767332 1382001 NM NR 1 STRUT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 176DN 25061 TWO CRACKS WERE FOUND ON 8/20/97 EMANATING FROM A DRAIN HOLE ON THE NR 1 ENGINE STRUT FWD UPPER SPAR WEB AT NAC STA 158. THE CRACKS WERE TRIMMED OUT ON A TIME-LIMITED BASIS. AT 11/98 OVERHAUL, A PERMANENT DOUBLER REPAIR WAS INSTALLED. CR ACKS WERE DUE TO FATIGUE DAMAGE. REPAIRED PER ERA 362549-14. 2 L 7 2 4F RT A1NM 1998111301334 19981113 01334 NM 1998 11 13 DL72S982301 1 19981105 A 5753 65192709 FLAP TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 INBOARD FLAP INBOARD TRACK TYP CORROSION AT FWD LUG AND MLG BEAM ATTACH HOLES: AD 90-07-05. INSTALL OVERSIZED BUSHINGS IN FWD LUG HOLES, OVERSIZE MLG BEAM ATTACH HOLES AND PROCEED WITH SPLICE PLATE REPAIR PER BAC SB 727-57-0178. 2 L 7 3 4F A3WE 1998111301335 19981113 01335 NM 1998 11 13 DL73E982302 1 19981106 A 5330 SKIN BOEING 737 7372S3 NM BS 335 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 367DL 21774 THE FUSELAGE SKIN WAS FOUND WITH A 1.875 INCH CRACK BELOW THE L1 DOOR AT APPROX FS 335. THE CRACK IS TYPICAL OF BAC S/B 737-53-1083. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN INTERIM DOUBLER REPAIR PER THE S/B. THE REPAIR WILL BE R EPLACED WITH A PERMANENT REPAIR/MODIFICATION WITHIN 3000 HOURS PER THE S/B. THE REPAIR IS DOCUMENTED PERER/A 366027-14A D. 2 L 7 2 4F RT A16WE 1998111301336 19981113 01336 NM 1998 11 13 DL73E982303 1 19981104 A 5330 SKIN BOEING 737 7372S3 NM R2 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 369DL 21776 THE FUSELAGE SKIN, DOUBLER AND BEAR STRAP WERE FOUND WITH A 1 INCH TYPICAL CRACK IN THE LOWER FWD CORNER OF THE R2 DOOR CUTOUT. THE CRACK WAS REPAIRED PER B737 SRM 53-30-3, FIG 24 EXCEPT BLIND FASTENERS WERE AUTHORIZED ON A TIME-LIMITED BA SIS. THE REPAIR WAS DOCUMENTED PER ER/A 366018-14, REV B. 2 L 7 2 4F RT A16WE 1998111301337 19981113 01337 NM 1998 11 13 DL72K982304 1 19981105 A 5330 6554583161 SKIN BOEING 727 727232 1384082 NM BS 1166-1183 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 529DA 21703 THE FUSELAGE SKIN WAS FOUND DENTED JUST ABOVE STRINGER 21R BETWEEN FS 1166 AND 1183. THE DENT WAS CUT OUT 2 X 7.25, REP AIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366004-14, REV B. 2 L 7 3 4F A3WE 1998111301338 19981113 01338 NM 1998 11 13 DL72S982308 1 19981109 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM RT EXTERIOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z 13026 21858 RT EXTERIOR AND INTERIOR OVERWING EMER LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998111301339 19981113 01339 NM 1998 11 13 DL72S982309 1 19981109 A 3350 BATTERY PACK 900835A BOEING 727 727225 1384077 NM RT OVERWING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z WA7751 21858 RT OVERWING EMEG EXIT SIGN INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998111301340 19981113 01340 NM 1998 11 13 SCNA98135 1 19981106 A 3350 582214 BATTERY PACK BOEING 727 727259 138408J NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE. REM OVED AND REPLACED FORWARD EMERGENCY FLOOR TRACK LIGHTING POWER SUPPLY. FORWARD SECTION OF FLOOR TRACK LIGHTING OPERATIO NALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998111301341 19981113 01341 NM 1998 11 13 SCNA98136 1 19981104 A 3350 900835A BATTERY PACK BOEING 727 727259 138408J NM LT OVERWING DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND RE PLACED THE BATTERY AND BATTERY CHARGER PACK M955. LEFT AFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998111301342 19981113 01342 NM 1998 11 13 SCNA98137 1 19981108 A 3350 1000677 LIGHT BOEING 727 727227 1384078 NM L2 DOOR INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A LINE MAINTENANCE CHECK, THE L2 EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMER GENCY EXIT LIGHT ASSEMBLY. TESTED EMERGENCY LIGHT FOR PROPER OPERATION AND OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998111301343 19981113 01343 NM 1998 11 13 P5CA9801592 1 19981101 A 5210 DOOR BOEING 747 747123 1384873 NM L4 DOOR CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 L-4 DOOR LOWER AFT CORNER FOUND CRACK. REPAIRED DAMAGED SECTION PER SRM 52-10-02 AND 51-10-02. 2 L 7 4 4F A20WE 1998111301344 19981113 01344 NM 1998 11 13 P5CA9801593 1 19981110 A 5210 DOOR BOEING 747 747123 1384873 NM L5 DOOR NOT SEALED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DISCOVERED PRESSURIZATION LEAK AT L5 DOOR. REPAIRED PER MM 52-09-00. 2 L 7 4 4F A20WE 1998111301345 19981113 01345 NM 1998 11 13 P5CA9801594 1 19981110 A 2612 FIRE WARNING BOEING 747 747283B 1384867 NM CARGO COMPT ACTIVATED A P5CA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 23 921FT 21575 ON TAKEOFF ROLL, MAIN DECK CARGO FIRE WARNING 1 ILLUMINATED WITH BELL. ABORTED TAKEOFF AND EMERGENCY CHECKLIST CARRIED OUT IAW AOM VOL 1. ON TAXI IN, THE SAME WARNING CONTINUALLY CAME ON WITH NO SMOKE. NOTE: ACFT LOADED WITH LIVE CATTLE. FOUND 1A DETECTOR CAUSING SPURIOUS WARNING. DEACTIVATED AND TRANSFERED TO DMI PER MEL 26-11. 2 L 7 4 4F A20WE 1998111301346 19981113 01346 WP 1998 11 13 TC8A98079 1 19981111 A 2910 O-RING DOUG DC8 DC861F 3021953 WP NR 3 HYD PUMP BROKEN A TC8A O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 184SK 45981 HYDRAULIC LOSS TO STANDPIPE IN FLIGHT. PERFORMED CHECKLIST, OPERATED IN MANUAL REVERSION. FOUND HYDRAULIC LEAD NR 3 EN GINE, HYDRAULIC PUMP INLET. REMOVED AND REPLACED BROKEN O-RING IAW 20-13-0, OPS CHECK GOOD. 2 L 7 4 4F 4A25 1998111301347 19981113 01347 WP 1998 11 13 TC8A98080 1 19981111 A 2910 FITTING DOUG DC8 DC861F 3021953 WP NR 3 HYD PUMP LOOSE A TC8A O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 23 184SK 45981 SLOW HYDRAULIC FLUID DOWN TO STANDPIPE, MANUAL REVERSION LIGHT ON. ACCOMPLISHED ABNORMAL HYDRAULIC CHECKLIST. FOUND LO OSE FITTING PRESSURE SIDE OF NR 3 ENGINE HYDRAULIC PUMP. TIGHTENED FITTING, RAN ENGINE AND LEAK CHECK GOOD IAW 20-13-0. 2 L 7 4 4F 4A25 1998111800001 19981118 00001 WP 1998 11 18 EIAA980257 1 19980905 A 7110 COWL DOUG DC9 DC932F 3022067 WP NR 2 ENGINE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, NR 2 ENGINE NOSE COWL HAS LARGE CRACKS AT 4 O'CLOCK POSITION. NRC R040. REPAIRED PER SRM 54-04B FIG 1 AND SABER TECH EA DC9-54-013 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1998111800002 19981118 00002 NM 1998 11 18 VJ9800592 1 19981009 A 5414 SKIN BOEING 737 737284 138448R NM NR 1 NACELLE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 470AT 21501 NR 1 ENGINE I/B TAIL DOOR SKIN CORRODED. LOSS ON SKIN AT 3RD RIB FROM FWD PART OF COWL OUT OF LIMIT IAW B737 SRM 54-30- 1. CUT OUT AND FABRICATED REPAIR DOUBLER, DRILLED, DEBURRED AND INSTALLED IAW B737 SRM 54-10-3. TREATED ALL BLENDED AR EAS IAW B737 SRM 51-10-2. 2 L 7 2 4F A16WE 1998111800003 19981118 00003 NM 1998 11 18 DL733982132 1 19981013 A 3350 BATTERY 20131A BOEING 737 73735B NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 225DL 20874 25069 OVERWING EXIT IDENTIFIERS ONLY ILLUMINATE FOR 15 SECONDS. REPLACED BATTERY PACK, CHECKS GOOD. 2 L 7 2 4F RT A16WE 1998111800010 19981118 00010 NM 1998 11 18 SWAA982722 1 19981102 A 3350 LAMP BOEING 737 7373T0 1384582 NM CARGO COMPT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED SERVICE CHECK, FOUND FWD CARGO LIGHT INOPERATIVE. REMOVED AND REPLACED NEW LAMP PER BOEING MM. 2 L 7 2 4F RT A16WE 1998111800013 19981118 00013 WP 1998 11 18 ABXA9800939 1 19981102 A 5412 991556531 BULKHEAD FRAME DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 DURING C-CHECK, FOUND THE AFT PRESSURE BULKHEAD DOOR LOWER FRAME CORRODED. REPAIRED FRAME IAW DC9 SRM 51-30-2 AND 51-30 -5. 2 L 7 2 4F A6WE 1998111800014 19981118 00014 NM 1998 11 18 DLM88982292 1 19981108 A 4990 3812761 APU DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE AFT FUSELAGE LEAKING A DALA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 27 923DL 7046 P80367 49705 P80367 DISPATCH ADV A/C RETURNING TO YUL WITH SMOKE IN CABIN. CAPT REPORTED BURNING ODOR ONLY. GIRLS IN AFT CABIN REPORTED LA V SMOKE DETECTOR GOING OFF AND BURING ODOR. CAPT REPORTED HE WAS CLIMBING THRU 3,000 FT AND CLOUD COVER TURNED ON WING ANTI-ICE WHEN THEY NOTICED THE ODOR. HE CLIMBED TO 10,000 FT AND ODOR WAS GONE BUT DECIDED TO RETURN TO YUL. DURING DE SCENT GOING THRU CLOUD COVER AT 1,000 FT LEVEL TURNED ON ANTI-ICE AGAIN AND NOTICED BURNING SMELL. AFTER LANDING NO ODO R NOTICED. AIR CANADA MECHANIC FOUND APU OIL AT MIN AND COMPARTMENT SPRAYED WITH OIL. FTL CREW PLACARD APU INOP. 2 L 7 2 4F 4 F RT A6WE E9NE 1998111800015 19981118 00015 WP 1998 11 18 TWAA9817502 1 19981029 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 29 LOOSE A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 926TW 49356 THE EGRESS LIGHTS AT CABIN ROW 29 FORWARD KEPT COMING ON AND OFF. TIGHTENED CONNECTOR AT THE POWER SUPPLY. CHECK-C 10- 10-98 STL. ---CLOSED--- 2 L 7 2 4F A6WE 1998111800016 19981118 00016 WP 1998 11 18 TWAA9817503 1 19981029 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 24 DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 926TW 49356 THE FLOOR EGRESS LIGHTS AT ROW 29 FORWARD KEPT CYCLING ON AND OFF WITH SWITCH IN THE ARMED POSITION. REPLACED BATTERY P ACK AT ROW 24. CHECK-C 10-10-98 STL. ----CLOSED---- 2 L 7 2 4F A6WE 1998111800017 19981118 00017 NM 1998 11 18 P5CA9801571 1 19981027 A 5730 PANEL BOEING 747 747283B 1384867 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 TOP OF R/H WING L/E PANEL JUST I/B OF #4 ENG PREVIOUS REPAIR FOUND CRCKED. SANDED OFF PREVIOUS REPAIR CUT SKIN BACK TO A 6X6 INCH CUTOUT, CLEANED AREA APPLIED FIBERGLASS OVERLAYS IAW SRM 51-40-09. 2 L 7 4 4F A20WE 1998111800018 19981118 00018 NM 1998 11 18 P5CA9801572 1 19981030 A 5730 PANEL BOEING 747 747283B 1384867 NM RT WING DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 PANEL ON RT WING FWD OF FLYING HAS HOLE CENTER AFT. REPAIRED DAMAGE BY APPLYING FIBERGLASS FILLERS AND DOUBLERS AND COAT ING IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998111800019 19981118 00019 NM 1998 11 18 P5CA9801573 1 19981030 A 7110 COWL BOEING 747 747283B 1384867 NM NR 3 ENG DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 #3 NOSE COWL RING INNER SURFACE DAMAGED AT 11 OCLOCK POSITION. REPAIRED DAMAGED AREA IAW SRM 54-10-01. 2 L 7 4 4F A20WE 1998111800020 19981118 00020 NM 1998 11 18 P5CA9801574 1 19981030 A 7830 R RAIL BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 689185 #3 ENGINE R RAIL CRACKED LEFT SIDE AT 7 OCLOCK POSITION. WELDED, STRESS RELIEVED IAW PW MM 72-53-01. 2 L 7 4 4F 4 F A20WE E3NE 1998111800021 19981118 00021 NM 1998 11 18 SWAA982652 1 19981028 A 3350 1619 BULB BOEING 737 7373T0 1384582 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT RED ROW LIGHT INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998111800022 19981118 00022 NM 1998 11 18 P5CA9801580 1 19981101 A 7110 COWL BOEING 747 747283B 1384867 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 2 ENGINE I/B T/R COWL T/F INSIDE SKIN CRACKED LOWER TRAILING EDGE. REMOVED AND REPLACED WEB IAW SRM 51-10-01 AND 51- 30-02. 2 L 7 4 4F A20WE 1998111800023 19981118 00023 NM 1998 11 18 P5CA9801581 1 19981101 A 7110 COWL BOEING 747 747283B 1384867 NM NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 2 ENGINE O/B T/R COWL T/E INSIDE SKIN CRCKED AT LOWER TRAILING EDGE. REMOVED AND REPLACED WEB IAC SRM 51-10-01 AND 5 1-30-02. 2 L 7 4 4F A20WE 1998111800024 19981118 00024 NM 1998 11 18 P5CA9801582 1 19981101 A 7110 COWL BOEING 747 747283B 1384867 NM NR 3 ENGINE LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 NR 3 NOSE COWL SEVERAL RIVETS LOOSE AND NOT SEATED PROPERLY IN PREVIOUS REPAIR FWD RING AT 5 O'CLOCK POSITION. REMOVED PREVIOUS REPAIR, FABRICATED NEW DOUBLER, REPAIRED NOSE COWL IAW SRM 54-31-03 ROHR SRM. 2 L 7 4 4F A20WE 1998111800025 19981118 00025 NM 1998 11 18 P5CA9801583 1 19981101 A 5730 PANEL BOEING 747 747283B 1384867 NM RT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 TOP OF RT WING L/E PANEL I/B OF NR 3 ENG PYLON SURFACE CRACKED JUST BESIDE PREVIOUS REPAIR. REMOVED DAMAGED AREA AND RE PAIRED AREA IAW SRM 51-40-12. 2 L 7 4 4F A20WE 1998111800026 19981118 00026 NM 1998 11 18 P5CA9801584 1 19981101 A 5720 FITTING BOEING 747 747283B 1384867 NM LT WING CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEFT WING FLYING PANEL CRACKED FWD LEFT ATTACH FITTING. REMOVED AND REPLACED LT FLYING PANEL IAW SRM 51-10-01, RIG CHEC KED GOOD IAW MM 57-20-01. 2 L 7 4 4F A20WE 1998111800027 19981118 00027 NM 1998 11 18 P5CA9801585 1 19981101 A 5753 FAIRING BOEING 747 747283B 1384867 NM LT TE FLAP DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 LEFT WING O/B FLAP I/B FWD FAIRING HAS SEVERAL HOLES IN NOSE SECTION. POTTED HOLES, FABRICATED FIBERGLASS OVERLAYS AND BONDED THEM TO REPAIR AREA IAW SRM 51-40-15. 2 L 7 4 4F A20WE 1998111800028 19981118 00028 NM 1998 11 18 P5CA9801586 1 19981030 A 7830 RAIL BOEING 747 747283B 1384867 NM PWA JT9 JT9D70A 52054 NE NR 2 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 921FT 21575 689167 NR 2 ENGINE R-RAIL CRACK FOUND AT 6 O'CLOCK POSITION. WELDED AND STRESS RELIEVED IAW PW MM 72-53-01. 2 L 7 4 4F 4 F A20WE E3NE 1998112000001 19981120 00001 WP 1998 11 20 ARWA980812 1 19980826 A 3110 ANNUNCIATOR LKHEED 1011 1011385115 5265015 WP COCKPIT MALFUNCTIONED A ARWA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 19 308GB 193U1133 SJU - FLT 504 - GROUND TURN-BACK. FLIGHT CONTROL LIGHT ON PILOT'S ANNUNCIATOR PANEL NR 1 YAW SAS. RE-SEATED IA34 CARD IN ICCB BOARD. OPS CHECK NORMAL IAW MM 33-17-00. (X) 2 L 7 3 4F A23WE 1998112000002 19981120 00002 WP 1998 11 20 AALA981684 1 19980902 A 3610 5953625521 DUCT DOUG DC9 DC982 3022082 WP TAIL COMPARTMENT FAILED A AALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SW 07 423AA 49335 DFW - FLT T1501 - ON TAKEOFF DFW, TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. IMMEDIATELY, AIR INTERRUPTED AND RETURNED TO DFW AND LANDED WTIHOUT INCIDENT. REPLACED RIGHT HAND PACK DUCTS. ACCOMPLISHED POWER RUN CHECKS WITH NO DI SCREPANCY NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998112000003 19981120 00003 WP 1998 11 20 AALA981525 1 19980813 A 2612 59585701 DETECTOR DOUG DC9 DC982 3022082 WP NR 2 ENGINE FAILED A AALA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 07 7525A 49917 DFW - FLT T1056 - DURING CRUISE, NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. CREW ACCOMPLISHED THE FIRE DETECTOR LOOP L IGHT WITHOUT FIRE WARNING CHECK LIST. SECURED NR 2 ENGINE AND DISCHARGED FIRE BOTTLE. ENGINE SHUTDOWN WAS NORMAL, AND FIRE WARNING LIGHT EXTINGUISHED AFTER 2 MINUTES. AIRCRAFT LANDED DFW WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE A/B FIRE LOOP WOULD NOT TEST. REPLACED NR 2 A/B FIRE LOOP, FIRE BOTTLE EXTINGUISHER, AND ENGINE OIL FILTERS. RA N NR 2 ENGINE AT POWER WITH NO LEAKS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F A6WE 1998112000004 19981120 00004 NE 1998 11 20 98ZZZX4088 2 19980721 A 7532 32143042 VALVE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE NR 2 ENGINE LEAKING A AMTA K NONE O OTHER IN INSP/MAINT 1 GL 11 521AT 24368 MDW - DURING P/F, FOUND NR 2 ENGINE TRANSLATING COWL (11 O'CLOCK) WITH EVIDENCE OF HEAT DAMAGE. FURTHER INSPECTION REVE ALED THE HIGH PRESSURE (PNEUMATIC) SHUT-OFF VALVE WAS LEAKING. TRANSLATING COWL AND PNEUMATIC VALVE WERE REPLACED, OPER ATIONS CHECKED SYSTEM, AND OK FOR RETURN TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 1998112000014 19981120 00014 SO 1998 11 20 C2XA98IA302 1 19980818 A 3350 78241 POWER SUPPLY EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14950 145061 IAH - FLT 4191 - THE PILOT REPORTED THE FORWARD AISLE PATH LIGHTING AT THE GALLEY WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE INVERTER/POWER SUPPLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT T00011AT 1998112000016 19981120 00016 SO 1998 11 20 C2XAIA361 1 19980911 A 2120 UNKNOWN EMB 145 EMB145LR 3260212 SO COCKPIT SMOKE A C2XA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SW 09 14952 145067 IAH - FLT 4121 - DURING FLIGHT ON APPROACH TO IAH, CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT. THE AIRCRAFT LANDED A T IAH WITHOUT INCIDENT WHERE MAINTENANCE VERIFIED OPERATION OF AFFECTED SYSTEMS AND PERFORMED A VISUAL INSPECTION OF EQU IPMENT AND WIRING IN THE COCKPIT. NO DEFECTS WERE FOUND AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. NO FURTHE R INCIDENTS HAVE BEEN REPORTED TO-DATE. 2 L 7 2 4T RT T00011AT 1998112000017 19981120 00017 SO 1998 11 20 C2XA98BT071 1 19980911 A 3230 156221 SWITCH EMB 145 EMB145ER SO HYDRAULIC SYSTEM LEAKING A C2XA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SW 09 14943 145040 GSO - FLT 4071 - REPORTED 'NR 1 HYD LO QTY', 'NR 1 ENG HYD PUMP FAIL IN-FLIGHT', AND 'EMERG GEAR EXTENSION PROCEDURE C/W '. FOUND LT HYDRAULIC PRESSURE SUPPLY SWITCH LEAKING. REMOVED AND REPLACED SWITCH, REFILLED SYSTEM. OPS CHECKED PUMPS GOOD, LEAK CHECKED GOOD. ACFT TT: 1,371.8 HOURS. ACFT CYCLES: 1,117. (X) 2 L 7 2 4F RT T00011AT 1998112000018 19981120 00018 NM 1998 11 20 GAIA9889 1 19980915 A 3350 1060091103 BATTERY PACK GRIMES BOEING 727 72790C 1384030 NM BS 1183 DISCHARGED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 270AX 3221 19170 AFT AIRSTAIRS EMERGENCY EXIT LIGHTS DO NOT COME ON. (AIA NON-ROUTINE NR 35246). REMOVED BATTERY FROM AFT AIRSTAIRS EMER GENCY EXIT LIGHTS. SENT OUT FOR CHARGING. REINSTALLED CHARGED BATTERY. OPERATIONAL CHECK CARRIED OUT SATISFACTORY. AI RCRAFT WAS THEN RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1998112000019 19981120 00019 WP 1998 11 20 G6OA028 1 19980831 A 2830 VALVE DOUG DC10 DC1030F 3023504 WP FUEL SYSTEM FAILED A G6OA J DUMP FUEL J WARNING INDICATION AP APPROACH 1 EA 27 601GC 47929 WHILE RETURNING TO ANC, UPON COMPLETION OF FUEL DUMP PROCEDURES, THE LEFT HAND FUEL DUMP VALVE INDICATED A FAILURE TO CL OSE. (X) 2 L 7 3 4F RT A22WE 1998112000020 19981120 00020 EA 1998 11 20 JBXA980048 1 19980830 A 3411 856KV9 PITOT CNDAIR CL600 CL6002B19 EA FUSELAGE CONTAMINATED A JBXA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 05 573ML 7227 NO AIRSPEED ON TAKEOFF, TAKEOFF ABORTED AT 80 KNOTS. FOUND BUG STUCK ON PITOT HEAT NR 1 SYSTEM. CLEANED PITOT HEAD CAP TAIN'S SIDE. OPERATION CHECK AIRSPEED INDICATION CAPTAIN'S SIDE GOOD IAW 24-11-00. (X) 2 L 7 2 4F RT A21EA 1998112000021 19981120 00021 EA 1998 11 20 JBXA980049 1 19980901 A 3030 PITOT HEAT CNDAIR CL600 CL6002B19 EA PITOT MALFUNCTIONED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 570ML 7206 LEFT AND RIGHT PITOT HEAT FAILED AFTER TAKEOFF. CYCLED AIRCRAFT POWER. OPERATIONAL TEST OF PROBE HEATING SYSTEM GOOD I AW CL-65 AMM 30-31-15. (X) 2 L 7 2 4F RT A21EA 1998112000022 19981120 00022 EA 1998 11 20 MASA98173 1 19980909 A 5210 051940 SEAL CNDAIR CL600 CL6002B19 EA PASSENGER DOOR DIRTY A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 47202 601R319003 7202 CVG/PHL - FLT 5753 - CREW REPORTED CABIN DOOR WOULD NOT CLOSE. MAINTENANCE CLEANED AND LUBED DOOR SEAL, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998112000023 19981120 00023 EA 1998 11 20 MASA98177 1 19980913 A 2611 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY MALFUCNTIONED A MASA F B A ACTIVATE FIRE EXT. EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 37228 7228 BHM/PHL - FLT 5768 - AIRCRAFT WAS AT CRUISE ALTITUDE WHEN THE EICAS SYSTEM INDICATED SMOKE IN THE CARGO BAY. THE CREW D ECLARED AN EMERGENCY, DISCHARGED THE CARGO FIRE EXTINGUISHER BOTTLES AND DIVERTED TO RDU WHERE AIRCRAFT LANDED WITHOUT I NCIDENT. AIRCRAFT WAS SUBSEQUENTLY FERRIED TO BHM. MAINTENANCE TROUBLESHOT, NO DISCREPANCIES FOUND. CARGO BOTTLES WER E REMOVED AND REPLACED SINCE THEY WERE DISCHARGED DURING THE INCIDENT. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998112000024 19981120 00024 EU 1998 11 20 98ZZZX4099 1 19980909 A 6410 355A12004008 BLADE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR DELAMINATED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 102LN 20 6922 3065 BLADE DELAMINATED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998112000025 19981120 00025 EU 1998 11 20 98ZZZX4100 1 19981001 A 6240 614764021 INDICATOR SNIAS 350 AS350B2 8680813 EU COCKPIT STICKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 101LN 15 133 3038 INDICATOR NEEDLE STICKS. TAPPING INDICATOR WILL FREE NEEDLE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998112000026 19981120 00026 SO 1998 11 20 SIMA982662 1 19980923 A 3310 12315660401 LIGHT EMB 145 EMB145 SO COCKPIT INOPERATIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 611AE 145074 ORD - FLT 4115 - FIRST OFFICER'S MAP LIGHT SOCKET SHORTED OUT AND CAUSED SMOKE IN THE COCKPIT. MEL'D COCKPIT LIGHTING. REMOVED AND REPLACED MAP LIGHT ASSEMBLY AND RHEOSTAT. OPERATIONAL CHECK GOOD. CLEARED MEL. REF: OPER CONTROL NR 98Z ZZX4101. (X) 2 L 7 2 4F RT T00011AT 1998112000027 19981120 00027 SO 1998 11 20 98ZZZX4101 1 19980923 A 3310 12030182001 RHEOSTAT EMB 145 EMB145 SO COCKPIT INOPERATIVE A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 21 611AE 145074 ORD - FLT 4115 - FIRST OFFICER'S MAP LIGHT SOCKET SHORTED OUT AND CAUSED SMOKE IN THE COCKPIT. MEL'D COCKPIT LIGHTING. REMOVED AND REPLACED MAP LIGHT ASSEMBLY AND RHEOSTAT. OPERATIONAL CHECK GOOD. CLEARED MEL. REF: OPER CONTROL NR SIM A982662. 2 L 7 2 4F RT T00011AT 1998112000028 19981120 00028 EU 1998 11 20 SIMA982314 1 19980819 A 3350 66363 LIGHT SAAB SF340 340B 7860101 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 393AE 340B393 DFW - FLT 3557 - FLOOR PROXIMITY LIGHT AT SEAT 9A AND 10A DO NOT ILLUMINATE. REMOVED AND REPLACED LIGHT STRIP. OPERATI ONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998112000029 19981120 00029 SO 1998 11 20 SIMA982402 1 19980828 A 2611 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 SW 21 602AE 145048 DSM - FLT 4074 - UPON DESCENT, CARGO SMOKE WARNING ILLUMINATED. AS A PRECAUTION, CREW ACTIVATED CARGO FIRE EXTINGUISHER S. AIRCRAFT LANDED SAFELY, PASSENGERS DEPLANED NORMALLY. VERIFIED EVENT AS A FALSE WARNING, AS THERE WAS NO EVIDENCE O F SMOKE OR FIRE. OPENED MEL ON THE CARGO SMOKE INDICATION AND THE CARGO FIRE EXTINGUISHER SYSTEM. AIRCRAFT RETURNED TO SERVICE. NOTE: AWAITING FURTHER CORRECTIVE ACTION, TO BE FILED UPON COMPLETION. (X) 2 L 7 2 4T RT T00011AT 1998112000030 19981120 00030 EU 1998 11 20 SIMA982441 1 19980901 A 3240 AIR124472 HYDRAULIC LINE SAAB SF340 340B 7860101 EU RT BRAKE LEAKING A SIMA K NONE K FLUID LOSS IN INSP/MAINT 1 SW 21 320AE 340B320 DFW - FLT 3571 - LOST INBOARD BRAKE ACCUMULATOR PRESSURE. FOUND RT INBOARD BRAKE FLEX LINE LEAKING. REMOVED AND REPLAC ED BRAKE LINE. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998112000031 19981120 00031 EU 1998 11 20 SIMA982592 1 19980916 A 2611 SMOKE DETECTOR SAAB SF340 340B 7860101 EU E/E BAY FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 350CF 340B350 SBP - DURING PS-2 INSPECTION, THE AVIONICS SMOKE DETECTOR WOULD NOT TEST. FOUND BAD GROUND AT GROUNDING BLOCK 203VNGA. REMOVED BLOCK, CLEANED INSULATION MATERIAL FROM MOUNTING AREA AND REINSTALLED BLOCK. AVIONICS SMOKE DETECTOR TEST GOOD . (X) 2 L 7 2 4T RT A52EU 1998112000032 19981120 00032 EA 1998 11 20 VTZA98270 1 19980825 A 2750 860D10014 FECU CNDAIR CL600 CL6002B19 EA E/E BAY FAILED A VTZA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 627BR 7233 IND/IAD - FLT 6723 - DURING LANDING ON 8-25-98 AT 1150 HOURS, EXPERIENCED A FLAP FAIL MESSAGE ON THE MASTER CAUTION PANE L. AIRCRAFT DECLARED AN EMERGENCY AND LANDED AT IAD WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIR CRAFT WAS TAXIED TO HANGAR FOR TROUBLESHOOTING AND MAINTENANCE. MAINTENANCE FOUND THE FECU HAD FAILED. FECU WAS REMOVE D AND REPLACED AND ALL PERTINENT CHECKS ACCOMPLISHED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1998112000033 19981120 00033 EA 1998 11 20 VTZA98271 1 19980825 A 2750 601R931051 BPSU CNDAIR CL600 CL6002B19 EA TE FLAP FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 627BR 7233 IAD/RSW - FLT 6745 - ON 8-25-98 AT 1900 HOURS, EXPERIENCED A FLAP FAIL MESSAGE ON MASTER CAUTION PANEL. ACFT CONTACTED MAINT CONTROL AND DISPATCHED, DECISION TO RETURN TO IAD WAS MADE. UPON ARRIVAL AT IAD, ACFT DECLARED AN EMERGENCY AND L ANDED AT IAD WITH NO FURTHER INCIDENT. MAINT NOTIFIED AND ACFT WAS TAXIED TO HANGAR FOR T/S. (ACFT GROUNDED BY Q.A. UN TIL SOLID REPAIRS WERE MADE). MAINT FOUND BPSU HAD FAILED. BPSU WAS REMOVED AND REPLACED AND SYSTEM THOROUGHLY T/S WIT H ASSIST OF BOMBARDIER REP. ALL PERTINENT CHECKS WERE ACCOMPLISHED. ACFT WAS THEN RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1998112000034 19981120 00034 WP 1998 11 20 98ZZZX4102 1 19980825 A 2497 WIRE LKHEED 1011 1011385115 5265015 WP CABIN SHORTED A WRNA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 05 75AA 193U1201 AFTER ABOUT AN HOUR ON THE GROUND IN HNL, FOUND FORWARD A/C GROUND SERVICE BUS BREAKER TRIPPED AND THE NR 1 TRANSFORMER RECTIFIER BREAKER TRIPPED. SMOKE AND ARCING WERE SEEN IN LOWER GALLEY AREA AT LEFT CIRCUIT BREAKER PANEL. FOUND TWO WI RE BUNDLES BURNED. ONE FROM THE NR 1 FLIGHT STATION BUS EXTENSION, AND THE OTHER FROM THE NR 3 FLIGHT STATION BUS EXTEN SION. 2 L 7 3 4F A23WE 1998112000042 19981120 00042 NE 1998 11 20 98ZZZX4110 2 19980803 A 7240 414129001 ROTOR ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 1927 1176 SC17067 7017 LE45247EA ROTOR ASSY FAILED SB LT101-72-10-0153 (FAILED Q-ROTOR INSPECTION). EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT , CORRECTED PROBLEM. PART TC: 4,011.2. 1 G 7 2 3U 3 U H13EU E5NE 1998112000043 19981120 00043 NE 1998 11 20 98ZZZX4111 2 19980818 A 7240 414129001 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE POWER TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117BK 1317 SC46918 7229 LE45610EFA ROTOR ASSY FAILED SB LT101-72-10-0153 (FAILED Q-ROTOR INSPECTION). EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT , CORRECTED PROBLEM. PART TC: 1,730.6. 1 G 7 2 3U 3 U H13EU E5NE10 1998112000044 19981120 00044 NE 1998 11 20 98ZZZX4112 2 19980613 A 7240 414129001 ROTOR ASSY BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 3394 SC17171 7104 LE45320EA FAILED SB LT101-72-10-0153 (FAILED Q-ROTOR INSPECTION). EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TC: 9,744.4. 1 G 7 2 3U 3 U H13EU E5NE 1998112000045 19981120 00045 NE 1998 11 20 98ZZZX4113 2 19980908 A 7240 414129001 ROTOR ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 1397 1147 SC04032 7127 LE45382EA FAILED SB LT101-72-10-0153 (Q-ROTOR INSPECTION). EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLE M. PART TC: 3,518.5. 1 G 7 2 3U 3 U H13EU E5NE 1998112000047 19981120 00047 NE 1998 11 20 98ZZZX4115 2 19980720 A 7250 411105064 ROTOR ASSY BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE GAS PROD DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 2480 896 7173 LE45552EFA EXCESSIVE GP BLADE TIP RUBS CAUSED BY FAILURE (WARPAGE ) OF GP SHROUD P/N 4-111-007-20, TT: 1,282.2 HOURS. REPLACED W ITH REPAIRED UNIT, CORRECTED PROBLEM. PART TC: 3,445.4. 1 G 7 2 3U 3 U H13EU E5NE10 1998112000050 19981120 00050 WP 1998 11 20 TWAA9818201 1 19981107 A 5240 BEAM DOUG DC9 DC931 3022065 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 DURING CHECK-C MAINT, FOUND ON THE RT FWD SERVICE DOOR THE NR 5 BEAM HAD A CRACK AT THE AFT END OF THE BEAM CLIP AT I/B RIVET HOLE. REPLACED CLIP FASTENER PER SRM 51-30-5 AND SERVICE BULLETIN 52-125 R4. 2 L 7 2 4F A6WE 1998112000051 19981120 00051 NM 1998 11 20 TWAA9818202 1 19981029 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 580 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION AT STA 580 STRINGER 39L ON THE STRINGER. SPLICED STRINGER AT STA 577 TO 600 P ER SRM 53-00-03 PAGE 215, DETAIL III, FIG 207. 2 L 7 2 4F RT A1NM 1998112000052 19981120 00052 NM 1998 11 20 TWAA9818203 1 19981030 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 606-632 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND STRINGER 39L CORRODED AT STA 610 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEAN ED STA 606 TO 632. INSTALLED SPLICE BETWEEN STA 600 TO 637 PER SRM 53-00-03, PAGE 215 DETAIL 14, FIG 207 SHEET A. 2 L 7 2 4F RT A1NM 1998112000053 19981120 00053 NM 1998 11 20 TWAA9818204 1 19981030 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 610-632 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORRODED STRINGER 38R BETWEEN STA 610 TO 632. CUT OUT SECTION OF STRINGER FROM STA 600 TO 627. REMOVED CORROSION PER SRM 51-10-00 PAGE 16. INSTALLED CRACK REPAIR PER SRM 53-00-03 PAGE 219 FIG 203 SHEET 3. 2 L 7 2 4F RT A1NM 1998112000054 19981120 00054 NM 1998 11 20 TWAA9818205 1 19981030 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 616-632 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 39L BETWEEN STA 616 TO 632. REMOVED SECTION OF CORRODED STRINGER AND CLEANED STA 606 TO 632 PER SRM 51-10-00 PAGE 16. INSTALLED SPLICE BETWEEN STA 600 TO 632 PER SRM 53-00-03, PAGE 21 5 DETAIL III FIG 207 SHEET 9. 2 L 7 2 4F RT A1NM 1998112000055 19981120 00055 NM 1998 11 20 TWAA9818206 1 19981030 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 565 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON LOWER SIDE OF STRINGER 38R, STA 565. CUT OUT CORROSION PER SRM 51-10-03 PA GE 16. INSTALLED SECTION OF STRINGER AT 38R STA 565 PER SRM 53-00-03, FIG 202. 2 L 7 2 4F RT A1NM 1998112000056 19981120 00056 NM 1998 11 20 TWAA9818207 1 19981022 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 1085 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND FORWARD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SEC TION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1. 2 L 7 2 4F RT A1NM 1998112000057 19981120 00057 NM 1998 11 20 TWAA9818208 1 19981022 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PG 209 FIG 202. 2 L 7 2 4F RT A1NM 1998112000058 19981120 00058 NM 1998 11 20 TWAA9818209 1 19981022 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 1085 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND FWD END OF STRINGER 33R CRACKED AT FORMER TIE FITTING, STA 1085. SPLICED IN NEW SECTION OF STRINGER PER 767-200 SRM 53-00-03 PAGE 209 TO 216 AND 51-40-03 PAGE 1. 2 L 7 2 4F RT A1NM 1998112000059 19981120 00059 NM 1998 11 20 TWAA9818210 1 19981022 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND STRINGER 33L CRACKED AT STA 434. REPAIRED STRINGER PER SRM 53-00-03 PAGE 209 FIG 202. 2 L 7 2 4F RT A1NM 1998112000060 19981120 00060 WP 1998 11 20 TWAA9818211 1 19981110 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT, FOUND FORMER FOOT CRACKED AT STA 1087, BETWEEN STRINGER 1 AND 3R. REMOVED BROKEN FORMER FOOT AND MADE NEW ONE OUT OF 7075T6, AND INSTALLED WITH RIVETS AND PRIMED PER STANDARD PROCESES 6-70-01. 2 L 7 2 4F A6WE 1998112000061 19981120 00061 WP 1998 11 20 VJ9800588 1 19981111 A 3350 41D004AD0073 BATTERY PACK DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 901VJ 47275 EMERGENCY EXIT LIGHTS IN BUSINESS CLASS FAILED TO DISARM. REPLACED NICAD BATTERY, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998112000062 19981120 00062 NM 1998 11 20 K3HA980134 1 19981108 A 3350 079123 LIGHT BOEING 727 727225 1384077 NM CABIN INOP A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 NR 1 RED LIGHT INOP INTERMITTANT CONNECTION (E-PATH). REPLACED RED LIGHT, OPS CHECK OK REF MM33-50-01 (P/N 07912-3). 2 L 7 3 4F A3WE 1998112000063 19981120 00063 NM 1998 11 20 K3HA980135 1 19981108 A 3350 0816901 LIGHT BOEING 727 727225 1384077 NM ROW 4 & 18 INOP A K3HA K NONE O OTHER IN INSP/MAINT 1 EA 25 361KP 20627 EMERGENCY PATH LIGHT ROW 4 AND 18 INOP. REPLACED LIGHTS, OPS CHECK REF MM 33-50-01. LAMP (P/N 3071BPEGPL). REPLACED S PLICE WIRE SPACE. 2 L 7 3 4F A3WE 1998112000064 19981120 00064 WP 1998 11 20 UPS98828139 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 816.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 816.250 UPPER. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000065 19981120 00065 WP 1998 11 20 UPS98828140 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 810 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 810 UPPER. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000066 19981120 00066 WP 1998 11 20 UPS98828141 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 803.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, LT WING L/E RIB CRACKED XFS 803.750 UPPER. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000067 19981120 00067 WP 1998 11 20 UPS98828142 1 19981111 A 3350 BULB DOUG DC8 DC873F 302199F WP CABIN FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 806UP 46006 INSPECTION TYPE-N/A, EMERG EXIT DISARMED LIGHT INOP. RELAMPED, OPS CKS GOOD. 2 L 7 4 4F RT 4A25 1998112000068 19981120 00068 WP 1998 11 20 UPS98828143 1 19981104 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 485 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XW 485 IS CRACKED IN 3 PLACES. REPAIRED IAW SRM 57-2-1. 2 L 7 4 4F RT 4A25 1998112000069 19981120 00069 WP 1998 11 20 UPS98828144 1 19981104 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 210 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XFS 210 CRACKED. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000070 19981120 00070 WP 1998 11 20 UPS98828145 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 772.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, L/E RIB CRACKED XFS 772.5 LT WING. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000071 19981120 00071 WP 1998 11 20 UPS98828146 1 19981105 A 5312 RIB DOUG DC8 DC873F 302199F WP WS 785 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, L/E RIB CRACKED LT XFS785 UPPER RIB LT WING. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000072 19981120 00072 WP 1998 11 20 UPS98828147 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 835 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, LT WING L/E RIB CRACKED UPPER XFS 835. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000073 19981120 00073 WP 1998 11 20 ABXA9800997 1 19980915 A 5320 3779874505 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT STATION 960 AT LONGERON 13L. REPAIRED IAW DWG 3779874 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000074 19981120 00074 WP 1998 11 20 ABXA9800998 1 19980915 A 5320 3750160503 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED INSIDE INTERCOSTAL STATION 680 LONGERON 13R. REPAIRED IAW DWG 3750160 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000075 19981120 00075 WP 1998 11 20 ABXA9800999 1 19980914 A 5320 4750419502 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 702 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT STATION 702 LONGERON. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000076 19981120 00076 WP 1998 11 20 ABXA9801000 1 19980915 A 5712 576947120 RIB DOUG DOUG DC8 DC861 3021952 WP WS 766.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 RIGHT WING LEADING EDGE LOWER RIB CRACKED FORWARD OF ACCESS PANEL, STATION XFS 766.250. REPAIRED IAW SRM 57-3-1, 51-1-2 0D, 51-1-8 AND DWG 576947122. 2 L 7 4 4F 4A25 1998112000077 19981120 00077 WP 1998 11 20 ABXA9801001 1 19980915 A 5320 37798741 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 715 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT STATION 715, LONGERON 19L. INSTALLED FITTING AT STATION 715, LONGERON 19L IAW DC8 SRM 51-1-20D, 51-1 -8, 51-1-11 AND DWG 3779874. 2 L 7 4 4F 4A25 1998112000078 19981120 00078 WP 1998 11 20 ABXA9801002 1 19980915 A 5320 37558451N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1100 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED FITTING AT LONGERON 35L, STATION 1100. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000079 19981120 00079 WP 1998 11 20 ABXA9801003 1 19980915 A 5313 37585931 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1270-1350 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 36R STATION 1270 TO 1350 CRACKED UNDER SPLICE. INSTALLED REPAIR IAW DC8 SRM 51-1-20D, 51-1-8 AND DWG 5750322. 2 L 7 4 4F 4A25 1998112000080 19981120 00080 WP 1998 11 20 ABXA9801004 1 19980915 A 5320 47504382 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1000 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERCOSTAL FITTING CRACKED AT STATION 1000, LONGERON 20L. REPLACED FITTING IAW DC8 SRM 51-1-20D, 51-1-8 AND DWG 425043 8. 2 L 7 4 4F 4A25 1998112000081 19981120 00081 WP 1998 11 20 ABXA9801005 1 19981106 A 5313 591287046 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1021 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 DURING C-CHECK, FOUND CRACK IN LONGERON 17 RT, STATION 1021. REPLACED LONGERON SECTION IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998112000082 19981120 00082 WP 1998 11 20 ABXA9801006 1 19981109 A 5313 59114277 LONGERON DOUG DOUG DC9 DC941 302207N WP BS 1041 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 DURING C-CHECK, FOUND CRACK IN LONGERON 16 LT, STATION 1041. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998112000083 19981120 00083 WP 1998 11 20 ABXA9801017 1 19981111 A 3231 510361C LINK DOUG DOUG DC8 DC861 3021952 WP NLG DOOR WORN A ABXA O OTHER E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 GL 23 847AX 46031 ON GEAR RETRACTION EXPERIENCED VIBRATION FROM AREA UNDER THE COCKPIT. RECYCLED LANDING GEAR TWICE, NOISE CEASED AFTER S ECOND RECYCLED. REPLACED NOSE GEAR DOOR LEFT CRANK ASSEMBLY AND ADJUSTED IAW DC8 MM 32-22-1. 2 L 7 4 4F 4A25 1998112000084 19981120 00084 WP 1998 11 20 ABXA9801007 1 19980923 A 5320 3779874506 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FRAME TIE FITTING CRACK AT STATION 960, LONGERON 18R. REPLACED FRAME FITTING IAW DC8 SRM 51-1-20D AND DWG 3779874. 2 L 7 4 4F 4A25 1998112000085 19981120 00085 WP 1998 11 20 ABXA9801008 1 19980923 A 5320 3779874506 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 940 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FRAME TIE FITTING CRACKED AT STATION 940, LONGERON 20R. REPLACED FITTING IAW DC8 SRM 51-1-20D AND DWG 3779874. 2 L 7 4 4F 4A25 1998112000086 19981120 00086 WP 1998 11 20 ABXA9801009 1 19980923 A 5320 37558452N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1230 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED INBOARD FLANGE AT STATION 1230 BETWEEN LONGERON 36R AND 35R. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000087 19981120 00087 WP 1998 11 20 ABXA9801010 1 19980923 A 5320 37558451N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1220 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED INBOARD FLANGE AT STATION 1220 BETWEEN LONGERONS 34L AND 33L. REPLACED FITTING IAW DC8 SRM 53-2-0 AND 5 1-1-20D. 2 L 7 4 4F 4A25 1998112000088 19981120 00088 WP 1998 11 20 ABXA9801011 1 19980922 A 5320 3750025502 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 857 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING STATION 857, LONGERON 20L. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM. 2 L 7 4 4F 4A25 1998112000089 19981120 00089 WP 1998 11 20 ABXA9801012 1 19980922 A 5730 5611350 SKIN DOUG DOUG DC8 DC861 3021952 WP WS 66 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LEFT WING UPPER SURFACE AT REAR WING SPAR INBOARD OF NR 2 PYLON CORRODED OUT OF LIMITS AT XRS.66.0 AND REAR SPAR. FABRI CATED REPAIR DOUBLER AND INSTALLED IAW DC8 SRM 51-1-8, 51-1-26, 57-2-1 AND 51-1-20D. 2 L 7 4 4F 4A25 1998112000090 19981120 00090 WP 1998 11 20 ABXA9801013 1 19980922 A 5320 5779936 DOUBLER DOUG DOUG DC8 DC861 3021952 WP BS 1700 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERNAL DOUBLER UNDER LONGERON 17L AT STATION 1700 CORRODED. REPAIRED FINGER DOUBLER IAW DC8 SRM 51-1-21 AND 53-2-0. 2 L 7 4 4F 4A25 1998112000091 19981120 00091 WP 1998 11 20 ABXA9801014 1 19980922 A 5320 37741187 BRACKET DOUG DOUG DC8 DC861 3021952 WP BS 1750 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 ELEVATOR CABLE FEED THRU BRACKET IS CRACKED 2 PLACES AT STATION 1750, RBL 18. REPAIRED CABLE FEED THRU BRACKET IAW ABX REA D853-24177MR. 2 L 7 4 4F 4A25 1998112000092 19981120 00092 WP 1998 11 20 ABXA9801015 1 19980922 A 5320 37558401 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1150 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CORRODED OUT AT STATION 1150, LONGERON 32R. REPLACED FITTING IAW REA D853-24190MR AND DC8 SRM 51-1-21D. 2 L 7 4 4F 4A25 1998112000093 19981120 00093 WP 1998 11 20 ABXA9801016 1 19980923 A 5320 3779874505 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 940 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FRAME TIE FITTING CRACKED AT STATION 940, LONGERON 18R. REPLACED TIE FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000094 19981120 00094 WP 1998 11 20 MWEA981051 1 19981111 A 2560 113317 SLIDE DOUG DC9 DC932 3022066 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 215ME 47744 THE GALLEY DOOR SLIDE FELL OFF DOOR. MTC REINSTALLED SLIDE. 2 L 7 2 4F A6WE 1998112000095 19981120 00095 NM 1998 11 20 SCNA98731 1 19981028 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS AT STATION 1130, 30 INCHES TO THE RIGHT OF THE BUTTLINE SEAT TRACK IN MAIN CAB IN AREA. CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM B727 531001. FABRICATED NEW SEAT TRACK AND SPLICE FROM BAC152 0792 PER SRM B727 531005. TREATED AND PRIMED PER SRM 511002. INSTALLED PER SRM 513002. 2 L 7 3 4F A3WE 1998112000096 19981120 00096 NM 1998 11 20 SCNA98732 1 19981028 A 5320 SUPPORT BOEING 727 7272A1 138407F NM BS 1070 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON THE FLOOR SUPPORT AT STATION 1070 1.4 INCHES RIGHT OF THE BUTTLINE. C ORROSION WAS TO BE OUT OF LIMITS IAW B727 SRM 531001. REMOVED SUPPORT IAW SRM B727 513002. FABRICATED NEW SUPPORT ANGL E FORM BAC1518344 IAW B727 SRM 511001. TREATED AND PRIMED IAW B727 SRM 511002. INSTALLED SUPPORT IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998112000097 19981120 00097 NM 1998 11 20 SCNA98733 1 19981028 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1124 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON THE FLOOR SUPPORT ANGLE AT STATION 1124 LBL 16. CORROSION FOUND TO B E OUT OF LIMITS B727 SRM 531001. REMOVED SUPPORT ANGLE IAW B727 SRM 513002. FABRICATED NEW SUPPORT ANGLE FROM BAC15064 3 IAW B727 SRM 531001. TREATED AND PRIMED IAW B727 SRM 511002. INSTALLED SUPPORT IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998112000098 19981120 00098 NM 1998 11 20 SCNA98734 1 19981028 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 1120-1129 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON THE FLOOR SUPPORT ANGLE BETWEEN STATION 1120 AND 1129 LBL 12. CORROS ION WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. REMOVED SUPPORT ANGLE IAW B727 SRM 513002. FABRICATED NEW SUPPO RT ANGLE FROM BAC150643 IAW B727 SRM 531001. TREATED AND PRIMED IAW B727 SRM 511002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998112000099 19981120 00099 NM 1998 11 20 SCNA98735 1 19981028 A 5320 ANGLE BOEING 727 7272A1 138407F NM BS 328 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND IN PASSENGER CABIN FORWARD LAVATORY BS 328 WL 208 RBL 12. FLOOR SUPPORT BEAM HAS CORROSION PRESENT CAUSING THE SURFACE TO LIFT AND PEEL, APPROX 10 SQAURE INCHES. CORROSION WAS FOUND TO BE OU T OF LIMITS IAW B727 SRM 531005. REMOVED SUPPORT ANGLE IAW B727 SRM 513002. FABRICATED NEW SUPPORT ANGLE FROM BAC15091 00312 IAW B727 SRM 531002. TREATED AND PRIMED IAW B727 SRM 511006. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998112000100 19981120 00100 NM 1998 11 20 SCNA98736 1 19981027 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 380-440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND IN THE MAIN CABIN FLOOR FORWARD ENTRY AREA FS 380 TO 440 AT RBL 45.50 SE AT TRACK HAS PITTING CORROSION IN BOTTOM CHANNEL. CORROSION WAS FOUND TO BE OUT OF LIMITS PER B727 SRM 531001. REMOVED SEAT TRACK PER SRM 513002. FABRICATED NEW SEAT TRACK FROM BAC 1520792 PER SRM B727 531002. ALODINED AND PRIMED PER B7 27 SRM 511002. INSTALLED PER B727 SRM 513002. 2 L 7 3 4F A3WE 1998112000101 19981120 00101 NM 1998 11 20 SCNA98737 1 19981027 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 380-440 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND IN THE MAIN CABIN FLOOR FORWARD ENTRY AREA FS 380 TO 440 AT RBL 24.75 SE AT TRACK HAS PITTING CORROSION IN BOTTOM OF CHANNEL. CORROSION WAS FOUND TO BE OUT OF LIMITS PER B727 SRM 531001. REMO VED SEAT TRACK PER SRM 513002. FABRICATED NEW SEAT TRACK FROM BAC 1520792 PER SRM B727 531002. ALODINED AND PRIMED PER B727 SRM 511002. INSTALLED PER B727 SRM 513002. 2 L 7 3 4F A3WE 1998112000102 19981120 00102 NM 1998 11 20 SCNA98738 1 19981031 A 5311 FRAME BOEING 727 7272A1 138407F NM BS 420 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND IN THE MAIN CABIN FORWARD GALLEY FLOOR AREA STATION 420 AT BL 0 TOP OF F RAME. CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 531001. CUT OUT DAMAGED AREA AND FABRICATED REPAIR PARTS FROM BA C14902831 AND BAC14902787 7075 T6 PER B727 SRM 531008. ALODINED AND PRIMED. INSTALLED PER SRM 531008. 2 L 7 3 4F A3WE 1998112000103 19981120 00103 NM 1998 11 20 SCNA98739 1 19981028 A 5347 SEAT TRACK BOEING 727 7272A1 138407F NM BS 1110-1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND ON THE SEAT TRACK IN THE MAIN CABIN AREA STATION 1110 TO 1130, 34 INCHES LEFT OF BUTTLINE. REMOVED CORROSION IAW SRM 511006. CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 531001. FABRICAT ED NEW SEAT TRACK OUT OF 7075 T6511 IAW SRM 531005. ALODINED AND PRIMED IAW SRM 511002. INSTALLED IAW SRM 513002. 2 L 7 3 4F A3WE 1998112000104 19981120 00104 WP 1998 11 20 RRXA98558 1 19981104 A 3260 SWITCH DOUG DC8 DC862 3021970 WP NLG INOP A RRXA O OTHER N FALSE WARNING LD LANDING 1 WP 15 995CF 46024 ON APPROACH, NO GREEN NOSE LIGHT INDICATION, DOORS NOT LATCHED AND GEAR NOT LATCHED LIGHTS ARE ON, CYCLED THE GEAR SEVER AL TIMES, NO HELP. ACCOMPLISHED QRH PROCEDURES, PREFORMED EMERGENCY LANDING. PREFORMED T/S TO LANDING GEAR POSITION AN D WARNING SYS. FOUND NOSE GEAR DOWNLOCK LIMIT SWITCH INOP. REMOVED AND REPLACED SAME. PREFORMED TEST TO SYS OPS CHECK S GOOD IAW MM CH 32-60-0. 2 L 7 4 4F 4A25 1998112000105 19981120 00105 NE 1998 11 20 RRXA98559 2 19981107 A 7200 ENGINE DOUG DC8 DC871 302199A WP GE CFM56 CFM562C1 13802 NE NR 4 FAILED A RRXA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP CR CRUISE 1 WP 15 811AL 46099 692132 SHUT NR 4 DOWN AT 0535Z DUE SURGING AND HIGH EGT. RETARDED POWER LEVER AND AT 40 PERCENT N1 EGT READ 804DEG. ACFT FERR IED TO KGSO FOR ENGINE CHANGE. REMOVED AND REPLACED NR 4 ENGINE IAW EMERY ENG CHANGE CARD ME091. 2 L 7 4 4F 4 F 4A25 E2GL 1998112000106 19981120 00106 WP 1998 11 20 RRXA98560 1 19981110 A 2420 AIR DIST DOUG DC8 DC873F 302199F WP COCKPIT ODOR A RRXA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 15 870TV 46086 NR 1 AC LOADMETER FLUCTUATING IN FLIGHT WITH ACRID ODOR OF ELECTRICAL SMOKE. PLACED NR 1 GEN SWITCH OFF, ODOR DISSIPATE D AND QRH PROCEDURE COMPLETE. PERFORMED OPERATIONAL CK OF NR 1 GENERATOR SYSTEM, NR 1 GENERATOR OPS CKS GOOD UPON ENGIN E RUN UP. ALL PARAMETERS NORMAL. NO DEFECTS OR ODOR OF ELECTRICAL SMOKE NOTICED. 2 L 7 4 4F RT 4A25 1998112000107 19981120 00107 WP 1998 11 20 RRXA98561 1 19981110 A 3230 O-RING DOUG DC8 DC862 3021970 WP LT MLG LEAKING A RRXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 15 995CF 46024 LOSS OF HYDRAULIC QUANTITY AND HYDRAULIC PRESSURE. PERFORMED CHECK LISTS TO LOWER FLAPS. FOUND FITTING ON LT GEAR TRIM FITTING LEAKING. REMOVED FITTING, REPLACED O-RING, REINSTALLED FITTING, SERVICED HYD RES. PERFORMED GROUND RUN ON NR 2 AND NR 3 ENGINES, OPS CHECK HYD PUMPS AND LEAK CHECK BOGGIE TRIM FITTINGS, NO LEAKS NOTED. CYCLED FLAPS, SPOILERS, AI LERONS, RUDDER AND HORIZONTAL STAB SYSTEMS SERVERAL TIMES. 2 L 7 4 4F 4A25 1998112000108 19981120 00108 WP 1998 11 20 RRXA98562 1 19981110 A 5101 STRUCTURE DOUG DC8 DC871F 302199D WP AIR FRAME LIGHTNING STRIKE A RRXA O OTHER C F.O.D. AP APPROACH 1 WP 15 8177U 45983 ACFT HIT BY LIGHTNING, AN EMERGENCY DECLARED. ALL SYSTEMS AND NAVIGATION EQUIPMENT WORKED OK. PERFORMED SPECIAL INSPEC TION IAW EMERY CARD SP004 LIGHTNING STRIKE INSP, OK FOR SERVICE. 2 L 7 4 4F RT 4A25 1998112000109 19981120 00109 WP 1998 11 20 ARWA981103 1 19981112 A 2121 525116 ACTUATOR DOUG DC8 DC862 3021970 WP SELECTOR VLV NOT SECURED A ARWA O OTHER O OTHER CL CLIMB 1 SO 19 791AL 46150 UNABLE TO PRESSURIZE CABIN ALTITUDE REACHED 10,000 A/C ALTITUDE WAS 10,000 NO DOOR WARNING LIGHTS ILLUMINATED. T/S FOUN D REC FAN AIR SELECTOR VALVE ACTUATOR NOT SECURED. SECURED AIR SELECTOR VALVE ACTUATOR IAW M/M 21-21-5, OPS NORMAL ON R UN UP. 2 L 7 4 4F 4A25 1998112000110 19981120 00110 1998 11 20 VNAA9811006 4 19981107 A 3425 HG2010AC02 AHRS DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E & E COMPT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 427JS 74818 44996 3039 DURING THE TAXI FOR TAKEOFF, A NUMBER ONE ATTITUDE HEADING REFERENCE UNIT (AHRS) FAILURE WARNING MESSAGE ILLUMINATED. T HE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY WAS EXECUTED WITHOUT ANY PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE NUMBER ONE AHRS UNIT, IN ACCO RDANCE WITH DORNIER MAINTENANCE MANUAL 34-21-10. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112000111 19981120 00111 NM 1998 11 20 VNAA9811009 1 19981109 A 2424 2438 GCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 459PS 3070 A RIGHT HAND A/C GENERATOR FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND A/C GENERATOR CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAI NTENANCE MANUAL 24-21-02. OPERATIONAL CHECKS WERE COMPLETED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112000112 19981120 00112 NM 1998 11 20 VNAA9811010 1 19981110 A 5330 SKIN DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE BIRD STRIKE A VNAA K NONE C F.O.D. NR NOT REPORTED 1 GL 07 440JS 3058 WHILE INBOUND TO PIT, THE AIRCRAFT STRUCK A BIRD ON THE RIGHT HAND SIDE OF THE FUSELAGE. THE FLIGHT CONTINUED ON TO PIT , AND PERFORMED A NORMAL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05- 29-10. NO DAMAGE WAS NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112000114 19981120 00114 EU 1998 11 20 98ZZZX4119 1 19981013 A 3246 AHA1236 WHEEL ASSY DUNLOP STBROS SD3 SD360 8100606 EU RT MLG CRACKED A DATA O OTHER O OTHER LD LANDING 1 GL 13 124CA 210 52 SH3652 AFTER TOUCHDOWN, AIRCRAFT PULLED TO RIGHT AND VIBRATION NOTICED INDICATING RT MAIN TIRE FLAT. BROUGHT AIRCRAFT TO STOP ON RUNWAY AND SHUT DOWN. ON POST-FLIGHT EXAM, NOTICED RT MAIN WHEEL RIM CRACKED AND TIRE FLAT. THE RUNWAY WAS CLOSED, AND MECHANIC SENT IMMEDIATELY. RT MAIN WHEEL ASSY AND TIRE REMOVED AND REPLACED. OPS CHECK GOOD. 2 H 7 2 4T A41EU 1998112000453 19981120 00453 WP 1998 11 20 TWAA9818301 1 19981112 A 3350 2232 BULB DOUG DC9 DC983 3022083 WP LT/RT EXTERIOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9622A 53593 BOTH LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED BULBS. 2 L 7 2 4F RT A6WE 1998112000454 19981120 00454 NM 1998 11 20 TWAA9818302 1 19981026 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 561-562 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND STRINGER 39R WITH EXFOLIATION CORROSION AT STA 561 TO 562, ON TOP INBD LIP APPROX 1 IN L ONG. CORROSION REMOVED AND REPAIRED WITH J-ANGLE PER SRM 53-00-03, PAGE 218. 2 L 7 2 4F RT A1NM 1998112000455 19981120 00455 NM 1998 11 20 TWAA9818303 1 19981012 A 5310 STRUCTURE BOEING 767 767231 1385131 NM FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND FUSELAGE FORMER 434 STRINGER AND SPLICE CORRODED, STRINGER 39L. REPLACED S-39L AND SPLI CE PER SRM 53-00-03, PAGE 209. 2 L 7 2 4F RT A1NM 1998112000456 19981120 00456 NM 1998 11 20 TWAA9818304 1 19981005 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434-460 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39L WITH CORROSION AT STA 434 TO 460. REPLACED CORRODED STRINGER PER 53-00-3, FIG 202. 2 L 7 2 4F RT A1NM 1998112000457 19981120 00457 NM 1998 11 20 TWAA9818305 1 19981005 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434-460 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39R WITH CORROSION AT STA 434 TO 460. REPLACED CORRODED STRINGER AND SPLICE 7075-T6 WITH BAC15CC6KC HI-LOCS. 2 L 7 2 4F RT A1NM 1998112000458 19981120 00458 NM 1998 11 20 TWAA9818306 1 19981012 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 BROKEN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER SPLICE AND STRINGER BROKEN AT STA 434, STRINGER 34R. REPLACED DAMAGED PARTS PER SRM 53-00-03. 2 L 7 2 4F RT A1NM 1998112000459 19981120 00459 NM 1998 11 20 TWAA9818307 1 19981013 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 1395-1417 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND STRINGER 39L HAD CORROSION IN CHANNEL AT STA 1395 TO 1417. REMOVED CORROSION AND INSTAL LED DOUBLER PER SRM 53-00-03, FIG 202. 2 L 7 2 4F RT A1NM 1998112000460 19981120 00460 NM 1998 11 20 TWAA9818308 1 19981013 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 610-632 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND STRINGER 36L CORRODED AT STA 610 TO 632. SPLICED IN NEW 20 INCH SECTION AT STA 601 TO 6 21, PER SRM 53-00-03, PG 209 TO 215, FIG 202 SHEET 1 - 7. 2 L 7 2 4F RT A1NM 1998112000461 19981120 00461 NM 1998 11 20 TWAA9818309 1 19981014 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 34L AND STRINGER SPLICE AT STA 434. REMOVED DAMAGED PART OF STRIN GER AND STRINGER SPLICE AND INSTALLED REPAIR PER SRM 53-00-03, FIG 202. 2 L 7 2 4F RT A1NM 1998112000462 19981120 00462 NM 1998 11 20 TWAA9818310 1 19981014 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 615 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 38R AT STA 615. CUT OUT CORRODED SECTION AND REPAIRED STRINGER 38 R PER SRM 53-00-03, FIG 203. 2 L 7 2 4F RT A1NM 1998112000463 19981120 00463 NM 1998 11 20 TWAA9818311 1 19981106 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 610-632 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND FUSELAGE STRINGER 39R CORRODED BETWEEN STA 610 AND 632. REMOVED S39R AT STA 600 TO 622 AND INSTALLED NEW FABRICATED PART PER SRM 53-00-03. 2 L 7 2 4F RT A1NM 1998112000464 19981120 00464 NM 1998 11 20 TWAA9818312 1 19981021 A 5522 SKIN BOEING 767 767231 1385131 NM LT ELEVATOR GOUGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND LT ELEV HAD ONE INCH LONG GOUGE IN UPPER SURPACE, 29 IN OTBD FROM OTBD ACTUATOR, AND 15 IN AFT FROM THE LEADING EDGE. REMOVED DAMAGED AREA AND REPAIRED WITH 6 PLIES OF GRAPHITE OVERLAY PER SRM 55-20-01, PAR 3C, AND 51-10-17, PARA 2 SUBPARAGRAPH E, FIG 5 AND FIG 17. 2 L 7 2 4F RT A1NM 1998112000465 19981120 00465 WP 1998 11 20 VJ9800589 1 19980917 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 937-945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 AFT PIT RT FLOOR PANEL AT FS 937 - 945 CORRODED BEYOND LIMIT IAW SRM 53-01, FIG 1. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-3, 53-01, FIG 1, 51-10-2, AND 53-21-0, FIG 10. 2 L 7 2 4F A6WE 1998112000466 19981120 00466 WP 1998 11 20 VJ9800590 1 19980930 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 Z ANGLE FLOOR SUPPORT STRUCTURE AT FS 965, LBL1 - LBL22, CORRODED AND CRACKED ON O/B END. REMOVED Z ANGLE, FABRICATED A ND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-2, 51-10-4 AND 51-10-2. 2 L 7 2 4F A6WE 1998112000467 19981120 00467 WP 1998 11 20 VJ9800591 1 19981001 A 5321 FLOOR DOUG DC9 DC932 3022066 WP NR 62 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 924VV 47278 FLOORBOARD NR 62 CORRODED AROUND EDGES. REMOVED FLOOR PANEL AND HAT SECTION. FABRICATED AND INSTALLED NEW PANEL AND HA T SECTION IAW DC9 SRM 51-10-3, 51-30-1, 53-01, FIG 1, 51-10-4 AND MM 53-20-1. 2 L 7 2 4F A6WE 1998112000468 19981120 00468 EU 1998 11 20 MALA976225 1 19981108 A 3350 301 BULB BAC 146 AVRO146RJ85A 1500097 EU COCKPIT FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 515XJ E2333 DURING INSPECTION, CEILING COCKPIT EMERGENCY LIGHT INOP. MAINTENACE RELAMPED. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998112000469 19981120 00469 1998 11 20 MALA976226 4 19981108 A 3425 6226190113 AHRS SAAB SF340 340B 7860101 EU COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 9CJ 224 AVIONICS YELLOW FLAG ON EHSI APPEARED ONCE ON GROUND TAXING OUT, REST THEN THREE TIMES IN THE AIR, RESET TWICE, 3RD TIME WOULDN'T RESET, THEN SHUT OFF BY ITSELF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED NR 1 AHRS COMPUTER. OPS CHEC K GOOD IAW SF3 340 MM, CHAP 34. 2 L 7 2 4T RT A52EU 1998112000470 19981120 00470 EU 1998 11 20 MALA976227 1 19981110 A 3020 NH24668169 DUCT SAAB SF340 340B 7860101 EU RT ENGINE FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 411XJ 411 DURING FLIGHT, THE RIGHT INTAKE LIGHT ON DOESN'T EXTINGUISH WITH SWITCH ON. AIRCRAFT RETURNED DUE TO WEATHER. MAINTENA NCE REPLACED LOWER INLET DUCT IAW SF 340 AMM 71-60-05. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998112000471 19981120 00471 EU 1998 11 20 MALA976228 1 19981110 A 3060 660713245 TIMER SAAB SF340 340B 7860101 EU LT PROP DEICE FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 416XJ 416 AFTER TAKEOFF, THE LEFT PROP DE-ICE INTERMITTENT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED PROP DE-ICE TIMER. O PS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998112000472 19981120 00472 EU 1998 11 20 MALA976229 1 19981109 A 5230 SEAL SAAB SF340 340B 7860101 EU CARGO DOOR LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 416XJ 416 DURING CRUISE, PRESSURIZATION DID NOT WORK IN AUTO OR MANUAL MODE. RETURNED TO MSP DUE TO WEATHER. MAINTENANCE RESECUR ED DOOR SEAL AT THE TOP OF CARGO DOOR. 2 L 7 2 4T RT A52EU 1998112000473 19981120 00473 EU 1998 11 20 MALA976230 1 19981111 A 7930 4053T73P01 TEMP SENSOR SAAB SF340 340B 7860101 EU RT PROP FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 445XJ 445 AFTER TAKEOFF, THE RIGHT PROPELLER OIL TEMP INDICATION ABNORMALLY HIGH, FLUX BETWEEN RED LINE AND 155 DEGREES. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT PROP TEMP OIL DETECTOR. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 1998112000474 19981120 00474 WP 1998 11 20 9810359927 1 19981108 A 3231 ROLLER DOUG DC9 DC931 3022065 WP RT MLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 8920E 45835 RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETUR NED TO DTW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND RIGHT GEAR DOOR ROLLER OUT OF RIG. RIGGED DOOR ROLLER . OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998112000475 19981120 00475 WP 1998 11 20 9810349759 1 19980925 A 5311 FRAME DOUG DC9 DC941 302207N WP BS 329 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 759NW 47287 DURING M CHECK, THE LOWER SECTION OF FS 218, STR 25L FUSELAGE FRAME WAS FOUND CRACKED. REPAIRED PER EA 97-159355. MFG P ART NUMBER: 9911520-385. 2 L 7 2 4F A6WE 1998112000476 19981120 00476 SO 1998 11 20 COMA9810260 1 19981107 A 3150 80055711 WARN UNIT EMB 120 EMB120RT SO E & E COMPT FAILED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 264CA 1 120256 AURAL WARNING FAIL DURING TAXI. REPLACED AURAL WARNING UNIT. 2 L 7 2 4T RT A31SO 1998112000477 19981120 00477 EA 1998 11 20 COMA9860348 1 19981110 A 5101 STRUCTURE CNDAIR CL600 CL6002B19 EA AIRFRAME BIRD STRIKE A COMA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SO 01 981CA 7163 BIRD STRIKE COMPLIED WITH BIRD STRIKE INSPECTION, NO DAMAGE FOUND. 2 L 7 2 4F RT A21EA 1998112000478 19981120 00478 WP 1998 11 20 UPS98828148 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 628.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C LT WING L/E UPPER RIB CRACKED AT XFS 628.75. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000479 19981120 00479 WP 1998 11 20 UPS98828149 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 610 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C LT WING UPPER L/E RIB CRACKED XFS 610.00. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000480 19981120 00480 WP 1998 11 20 UPS98828150 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 728.75 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 728.750. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000481 19981120 00481 WP 1998 11 20 UPS98828151 1 19981105 A 5312 RIB DOUG DC8 DC873F 302199F WP WS 741.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 741.25. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000482 19981120 00482 WP 1998 11 20 UPS98828152 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 722.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 722.500. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000483 19981120 00483 WP 1998 11 20 UPS98828153 1 19981105 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 635 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE:C LT WING L/E RIB CRACKED XFS 635.00. REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112000484 19981120 00484 EU 1998 11 20 QXEA9801578 1 19981012 A 5220 SEAL FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CUT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SERVICE EMERGENCY EXIT DOOR SEAL HAS A CUT IN BOTTOM FORWARD CORNER. INJECTED SMALL QUANTITY OF PR1422 INTO CUT A ND SKINNED OVER EXTERIOR SO AS TO FUSE INNER AND OUTER PORTIONS OF SEAL. 2 L 7 2 4F RT A20EU 1998112000485 19981120 00485 EU 1998 11 20 QXEA9801579 1 19981011 A 5220 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SERVICE EMERGENCY DOOR HAS CHAFE DAMAGE THAT NEEDS TO BE TREATED AND PAINTED. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1998112000486 19981120 00486 EU 1998 11 20 QXEA9801580 1 19981017 A 5220 RIVETS FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SERVICE EMERGENCY DOOR COVER HAS LOOSE RIVETS ON AFT DOOR TRACK SEAT. REMOVED LOOSE RIVETS. INSTALLED NEW RIVETS . 2 L 7 2 4F RT A20EU 1998112000487 19981120 00487 EU 1998 11 20 QXEA9801581 1 19981026 A 5220 COVER FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SERVICE EMERGENCY DOOR FORWARD TRACK SEAL IS MISSING COVER ON RIVET ATTACH STRIP. REPAIRED IAW FOKKER SRM 51-31-0 5. 2 L 7 2 4F RT A20EU 1998112000488 19981120 00488 EU 1998 11 20 QXEA9801582 1 19981025 A 5220 SEAL FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - UPPER TRACK SEAL IS DETERIORATED ON SERVICE EMERGENCY EXIT COVER. REPLACED SEAL. 2 L 7 2 4F RT A20EU 1998112000489 19981120 00489 EU 1998 11 20 QXEA9801583 1 19981025 A 5220 COVER FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - GRASP HANDLE ATTACH HOLES ARE DETERIORATED ON SERVICE/EMERGENCY EXIT COVER. REPAIRED IAW FOKKER SRM 51-70-1, PAGE S 1-2. 2 L 7 2 4F RT A20EU 1998112000490 19981120 00490 EU 1998 11 20 QXEA9801584 1 19981025 A 5220 COVER FOKKER F28 F28MK4000 4990810 EU EMER EXIT COVER DETERIORATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SERVICE EMERGENCY EXIT DOOR COVER PLASTIC IS DETERIORATED AND CRACKING AT FORWARD UPPER CORNER. REPAIRED IAW FOKK ER SRM 51-70-1, PAGES 1-2. 2 L 7 2 4F RT A20EU 1998112000491 19981120 00491 EU 1998 11 20 QXEA9801585 1 19981017 A 5220 TRACKS FOKKER F28 F28MK4000 4990810 EU EMER EXIT DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - SERVICE EMERGENCY DOOR TRACKS ARE ALL BEAR METAL. TREATED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1998112000492 19981120 00492 EU 1998 11 20 QXEA9801586 1 19981016 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR OUT OF ADJUST A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - BELLVILLE WASHERS FOR FRICTION DISC ASSEMBLY FOR PASSENGER DOOR NEED ADJUSTMENT. ADJUSTED IAW FOKKER SRM 52-10-03 , PAGE 502C , PARAGRAPH D, 502-503 STEP 3 E AND F. 2 L 7 2 4F RT A20EU 1998112000493 19981120 00493 EU 1998 11 20 QXEA9801587 1 19981009 A 5210 JAMB NUT FOKKER F28 F28MK4000 4990810 EU PAX DOOR LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX - FORWARD EXTENDING ROD FOR PASSENGER DOOR HAND RAIL ADJUSTABLE ROD END SAFETY JAM NUT NOT SECURE. SECURED AND SAFE TIED JAMB NUT. 2 L 7 2 4F RT A20EU 1998112000494 19981120 00494 NM 1998 11 20 QXEA9801683 1 19981107 A 3350 82520977001 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN DAMAGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 357PH 504 PDX - ESCAPE PATH FLOOR LIGHTING ASSEMBLY IS DAMAGED (SECOND ASSEMBLY FROM THE FRONT). MAINTENANCE REPLACED THE DAMAGED SECTION OF FLOOR LIGHTING. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998112000495 19981120 00495 WP 1998 11 20 ABXA9801018 1 19980925 A 5320 3779874506N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CRACKED AT STATION 980, LONGERON 18R. REPLACED FITTING AT STATION 980, LONGERON 18R IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000496 19981120 00496 WP 1998 11 20 ABXA9801019 1 19980924 A 5720 564311719 ANGLE DOUG DOUG DC8 DC861 3021952 WP WS 3 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LEFT WING TRAILING EDGE CAVITY AT STATION XW 3.00, THE DRIVE LINK FITTING STIFFENER ANGLE IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000497 19981120 00497 WP 1998 11 20 ABXA9801020 1 19980924 A 5320 3750299503 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1040-1060 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 STATION 1040-1060, LONGERON 36L SPLICE FITTING IS CRACKED. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000498 19981120 00498 WP 1998 11 20 ABXA9801021 1 19980924 A 5320 3750026501 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT STATION 680, LONGERON 20L. INSTALLED NEW FITTING IAW DC8 SRM. 2 L 7 4 4F 4A25 1998112000499 19981120 00499 WP 1998 11 20 ABXA980122 1 19980924 A 5313 25972423 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1690-1766 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 26R CORRODED AND CRACKED AT STATION 1690-1766. REPAIRED IAW DC8 SRM 51-1-20 AND 53-1-0. 2 L 7 4 4F 4A25 1998112000500 19981120 00500 WP 1998 11 20 ABXA9801023 1 19980924 A 5320 37592221N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1260-1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON SPLICE FITTING AT STATION 1260-1280, LONGERON 34L IS CRACKED. REPLACED FITTING IAW DWG 3759222 AND DC8 SRM 51- 1-20D. 2 L 7 4 4F 4A25 1998112000501 19981120 00501 WP 1998 11 20 ABXA9801024 1 19980924 A 5320 3779978501 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1020 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED FITTING INSIDE INTERCOSTAL LONGERON 19R, STATION 1020. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000502 19981120 00502 WP 1998 11 20 ABXA9801025 1 19980924 A 5720 564311719 ANGLE DOUG DOUG DC8 DC861 3021952 WP WS 3 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LEFT WING AT STATION XW 3.00, THE DRIVE LINK STIFFENER ANGLE IS CRACKED. REPAIRED IAW DC8 SRM. 2 L 7 4 4F 4A25 1998112000503 19981120 00503 WP 1998 11 20 ABXA9801026 1 19980923 A 5320 3779874505N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 940 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FRAME TIE FITTING CRACKED AT STATION 940, LONGERON 19R. REPLACED FITTING IAW DC8 SRM 51-1-20D AND DWG 3779874. 2 L 7 4 4F 4A25 1998112000504 19981120 00504 WP 1998 11 20 ABXA9801027 1 19980923 A 5320 3779874505N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FRAME TIE FITTING CRACKED AT STATION 960, LONGERON 19R. REPLACED FITTING IAW DC8 SRM 51-1-20D AND DWG 3779874. 2 L 7 4 4F 4A25 1998112000505 19981120 00505 WP 1998 11 20 ABXA9801028 1 19981005 A 5313 97585055 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1050-1150 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 34L FROM FRAME STATION 1050 TO FRAME STATION 1150 HAS CORROSION BEYOND LIMITS. REPLACED LONGERON 34L FROM FRAM E STATION 1050 TO FRAME STATION 1270 IAW ABX REA D853-24189MR. 2 L 7 4 4F 4A25 1998112000506 19981120 00506 WP 1998 11 20 ABXA9801029 1 19980929 A 5330 5644130 SKIN DOUG DOUG DC8 DC861 3021952 WP BS 1690 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FUSELAGE SKIN CORRODED AND CRACKED AT STATION 1690, LONGERON 25R. REPAIRED IAW DC8 SRM 51-1-20D, 51-1-21, 53-2-1, AND A BX REA D853-24197. 2 L 7 4 4F 4A25 1998112000507 19981120 00507 WP 1998 11 20 ABXA9801030 1 19981005 A 5313 97585053 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1050-1270 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 34L FROM FRAME STATION 1050 TO FRAME STATION 1270 CORRODED BEYOND LIMITS. REPLACED LONGERON 34L IAW ABX REA D8 53-24189MR. 2 L 7 4 4F 4A25 1998112000508 19981120 00508 WP 1998 11 20 ABXA9801031 1 19980930 A 5320 37798742 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 822 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT STATION 822, LONGERON 19R. REPAIRED IAW DWG 3779874 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000509 19981120 00509 WP 1998 11 20 ABXA9801032 1 19980910 A 5320 564922738 DOUBLER DOUG DOUG DC8 DC861 3021952 WP BS 1690-1766 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FUSELAGE SKIN INTERNAL DOUBLER CORRODED BEYOND LIMITS AT LONGERON 10R, STATION 1690-1766. INSTALLED NEW DOUBLER IAW DC8 SRM 53-5-2 AND 51-1-21. 2 L 7 4 4F 4A25 1998112000510 19981120 00510 WP 1998 11 20 ABXA9801033 1 19980930 A 5320 1706317 SHEAR TIE DOUG DOUG DC8 DC861 3021952 WP BS 1000 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CORROSION ON SHEAR TIE AT STATION 1000 LONGERONS 34L-35L. REPAIRED IAW DC8 SRM 53-2-0 . 2 L 7 4 4F 4A25 1998112000511 19981120 00511 WP 1998 11 20 ABXA9801034 1 19981016 A 5210 36456593 FITTING DOUG DOUG DC8 DC861 3021952 WP L1 DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 L1 DOOR UPPER HINGE FITTING CRACKED. REPLACED DOOR HINGE IAW DC8 SRM 52-1-4. 2 L 7 4 4F 4A25 1998112000512 19981120 00512 WP 1998 11 20 ABXA9801035 1 19980925 A 5320 5646955503 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 960 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CUSP FRAME FITTING CORRODED OUT AT STATION 960, RIGHT SIDE. REPAIRED IAW DC8 SRM 51-21-2. 2 L 7 4 4F 4A25 1998112000513 19981120 00513 WP 1998 11 20 ABXA9801036 1 19980925 A 5320 4758514519N FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1228 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED FITTING AT LONGERON 32R, STATION 1228, AFT SIDE OF FRAME. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000514 19981120 00514 WP 1998 11 20 ABXA9801037 1 19981005 A 5330 5750322 SKIN DOUG DOUG DC8 DC861 3021952 WP BS 1080 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 BULGING AND POPPED FASTENERS ON TRIPLER AT STATION 1080, LONGERON 36R-34R. REPAIRED IAW DC8 SRM AND DWG 5750322, 51-1-2 0D. 2 L 7 4 4F 4A25 1998112000515 19981120 00515 WP 1998 11 20 ABXA9801038 1 19980901 A 5320 37558401 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 1230 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 FITTING CORRODED OUT AT STATION 1230, LONGERON 33R. REPAIRED IAW ABX REA D853-24191MR AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000516 19981120 00516 WP 1998 11 20 ABXA9801039 1 19980917 A 5400 5642301137 STIFFENER DOUG DOUG DC8 DC861 3021952 WP NR 4 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 NR 4 ENGINE LOWER AFT PYLON FAIRING INTERNAL STRUCTURE VERTICAL STIFFENER IS CRACKED AT TOP LEFT RIVET HOLE. REPAIRED I AW DC8 SRM 51-1-20D AND DWG 5643201. 2 L 7 4 4F 4A25 1998112000517 19981120 00517 WP 1998 11 20 ABXA9801040 1 19981005 A 5320 9758048 SHEAR TIE DOUG DOUG DC8 DC861 3021952 WP BS 1140 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 EXFOLIATED SHEAR TIE AT LONGERON 35L, STATION 1140. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 9758048. 2 L 7 4 4F 4A25 1998112000518 19981120 00518 WP 1998 11 20 ABXA9801041 1 19981005 A 5320 37584971N INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 1140 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERCOSTAL TO FRAME TIE-IN FITTING AT STATION 1140, LONGERON 36 IS CRACKED. REPAIRED IAW DC8 SRM 51-1-20D, 51-1-11, AN D 51-1-8. 2 L 7 4 4F 4A25 1998112000519 19981120 00519 WP 1998 11 20 ABXA9801042 1 19981001 A 5400 5765001 SUPPORT DOUG DOUG DC8 DC861 3021952 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 NR 1 PYLON OUTBOARD SIDE AT STATION AND YOP 230, SUPPORT CRACKED. REPAIRED IAW DWG 44088012-1 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000520 19981120 00520 WP 1998 11 20 ABXA9801043 1 19980929 A 5320 4750419504 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 798 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED INTERCOSTAL FITTING AT STATION 798 AND LONGERON 11R. REPAIRED IAW DC8 SRM 51-1-20D AND 51-1-11. 2 L 7 4 4F 4A25 1998112000521 19981120 00521 WP 1998 11 20 ABXA9801044 1 19980925 A 5313 975491331 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 260 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 LONGERON 35L, STATION 260 CRACKED. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1998112000522 19981120 00522 WP 1998 11 20 ABXA9801045 1 19981003 A 5320 3779782 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP BS 834 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 INTERCOSTAL CRACKED AT LONGERON 18R, STATION 834. REPLACED FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000523 19981120 00523 WP 1998 11 20 ABXA9801046 1 19981003 A 5320 975377623 WEB DOUG DOUG DC8 DC861 3021952 WP BS 1160-1220 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 NR 3 CARGO COMPARTMENT TORQUE BOX VERTICAL WEB IS CRACKED IN SEVERAL AREAS, LONGERON 26L AT STATION 1160-1220. REPAIRED IAW DC8 SRM 51-1-20D, 51-1-8, AND DWG 9753776. 2 L 7 4 4F 4A25 1998112000524 19981120 00524 WP 1998 11 20 ABXA9801047 1 19981002 A 5311 97558853 FRAME DOUG DOUG DC8 DC861 3021952 WP BS 1000 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 NR 3 CARGO COMPARTMENT FRAME STATION 1000, AFT SIDE UPPER FLANGE CORRODED AT STRINGER 34L TO 34R. REPAIRED IAW ABX REA D853-24204 AND DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998112000525 19981120 00525 WP 1998 11 20 ABXA9801048 1 19981002 A 5400 5765001 ANGLE DOUG DOUG DC8 DC861 3021952 WP NR 4 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED ANGLE ON NR 4 ENGINE PYLON, LOWER SIDE LEFT AFT OF PNEUMATIC DUCT OPENING. REPAIRED IAW ABX REA D854-24199 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000526 19981120 00526 WP 1998 11 20 ABXA9801049 1 19981005 A 5320 3750026501 FITTING DOUG DOUG DC8 DC861 3021952 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 844AX 45848 CRACKED FITTING INSIDE INTERCOSTAL STATION 680, LONGERON 19L. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998112000527 19981120 00527 NM 1998 11 20 SCNA98741 1 19981028 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 1110 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK, CORROSION WAS FOUND IN MAIN CABIN AREA, STATION 1110 O INCHES TO 20 INCHES LEFT OF BUTTLINE, FLOORBEAM 1110. REMOVED CORROSION IAW B727 SRM 511006. THE CORROSION WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 53100 1. TRIMMED DAMAGED UPPER CHORD IAW B727 SRM 531008. FABRICATED REPAIR FROM BAC 1505100617, BAC14902785, BAC 14902831, BAC15123396, BAC15123353 IAW SRM 531008. TREATED AND PRIMED B727 SRM IAW 511002. INSTALLED PER SRM 531008. 2 L 7 3 4F A3WE 1998112000528 19981120 00528 NM 1998 11 20 SCNA98742 1 19981028 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 1130 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK CORROSION WAS FOUND ON T-CAP OF FLOORBEAM AT STATION 1130 RBL 5 AFT CARGO PIT CEILING. CORRO SION WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 531001. REMOVED DAMAGED AREA IAW B727 SRM 513002. FABRICATED NEW PART FORM BAC14902831 IAW B727 SRM 531008. TREATED AND PRIMED IAW B727 SRM 511002. INSTALLED IAW B727 SRM 513002. 2 L 7 3 4F A3WE 1998112000529 19981120 00529 NM 1998 11 20 SCNA98740 1 19981028 A 5315 FLOORBEAM BOEING 727 7272A1 138407F NM BS 1030 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 287SC 21345 DURING A HEAVY MAINT CHECK CORROSION WAS FOUND IN MAIN CABIN AREA, FLOORBEAM AT 1030, BUTTLANE 0. REMOVED CORROSION IAW B727 SRM 511006. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. TRIMMED DAMAGED UPPER CHORD IAW SRM 53 1008. FABRICATED NEW PART FROM BAC1505100617, BAC14902785, BAC14902837 BAC 15123376 BAC151223353 IAW B727 SRM 531008. T REATED AND PRIMED IAW SRM B727 531002. INSTALLED IAW SRM B727 531008. 2 L 7 3 4F A3WE 1998112000530 19981120 00530 NM 1998 11 20 VNAA9811011 1 19981111 A 3250 2318000002 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING TRIPPED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 437JS 41235 11843 3055 A NOSE STEERING FAILURE WARNING OCCURRED, DURING THE TAXI PRIOR TO TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTAT ION MAINTENANCE INSPECTED AND RE-SEATED THE NOSE STEERING CONTROL UNIT. OPERATIONAL CHECKS WERE COMPLETED, IN ACCORDANC E WITH DORNIER MAINTENANCE MANUAL 32-51-06. THE OPERATIONAL CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RELEASED FRO M MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112000531 19981120 00531 WP 1998 11 20 TC8A98081 1 19981112 A 2421 GENERATOR DOUG DC8 DC862 3021970 WP NR 2 OUT OF ADJUST A TC8A D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 23 181SK 45910 NR 2 GENERATOR WILL NOT CARRY A NORMAL LOAD, NO VOLTS AND FREQS. ADJUSTED FREQS ON GENERATOR, ENGINE RUN CARRIED OUT, O PS CHECKS NORMAL IAW 24-20-1. 2 L 7 4 4F 4A25 1998112000532 19981120 00532 WP 1998 11 20 TWAA9818401 1 19981113 A 3397 0105606003 WIRE DOUG DC9 DC983 3022083 WP ROW 2 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9413T 53188 FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM THE FORWARD GALLEY TO CABIN ROW 2. FOUND WIRE PULLED OUT OF LIGHT MODULE. R EPLACED MODULE. CHECK-C 10-13-98 MCI. 2 L 7 2 4F RT A6WE 1998112000533 19981120 00533 NM 1998 11 20 TWAA9818402 1 19981006 A 5314 KEEL BEAM BOEING 767 767231 1385131 NM BS 933 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 603TW 22566 DURING CHECK-C MAINT, FOUND SURFACE CORROSION TO INTERGRANULAR CORROSION ON KEEL BEAM RT AND LT LOWER LEG, TOP AND BOTTO M OF I/B LEG FROM STA 933 THRU MAIN GEAR WHEEL WELL AREA. REMOVED CORROSION PER SRM 51-10-00 PG 1. TREATED WITH ALODIN E AND PRIMED. 2 L 7 2 4F RT A1NM 1998112000534 19981120 00534 NM 1998 11 20 TWAA9818403 1 19981002 A 5753 SKIN BOEING 757 757231 1384950 NM NR 5 TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 705TW 28479 DURING CHECK-C MAINT, FOUND RT I/B TRAILING EDGE FLAP I/B OF NR 5 FLAP CANOE, THE AFT FLAP LOWER SURFACE WAS DELAMINATED 3 IN BY 3 IN. REPAIRED PER 757 SRM 57-53-01 FIG 201, SHEET 5 TABLE 2. 2 L 7 2 4F RT A2NM 1998112000535 19981120 00535 NM 1998 11 20 TWAA9818404 1 19981103 A 5730 SKIN BOEING 757 7572Q8 1384972 NM LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 710TW 28169 DURING CHECK-C MAINT, FOUND LEFT WING LEADING EDGE. BULLNOSE CRACK 10 INCH LONG ON COMPOSITE PANEL LOCATED AFT OF AND B ETWEEN NR 3 AND 4 LEADING EDGE SLATS. INSTALLED 3 IN BY 10 IN HOT BOND REPAIR PER SRM 57-41-01 AND 51-70-07. 2 L 7 2 4F RT A2NM 1998112000536 19981120 00536 NM 1998 11 20 TWAA9818405 1 19981110 A 5754 SKIN BOEING 767 767231 1385131 NM NR 6 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 DURING CHECK-C MAINT, FOUND REPAIR AT NR 6 LEADING EDGE SLAT HAD DELAMINATED AT EDGE WHERE SEAL IS MISSING. INSTALLED A METAL TO METAL HOT BOND PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1998112000537 19981120 00537 NM 1998 11 20 TWAA9818406 1 19981110 A 5314 KEEL BEAM BOEING 767 767231 1385131 NM FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 DURING CHECK-C MAINT, ON KEEL BEAM FOUND INTERGRANULAR CORROSION ON TOP SIDE OF LT LOWER LEG ABOVE PANEL 149AL. REMOVED CORROSION AND APPLIED ALODINE AND PRIMED PER SRM 53-50-12. 2 L 7 2 4F RT A1NM 1998112000538 19981120 00538 NM 1998 11 20 TWAA9818407 1 19981110 A 5753 SKIN BOEING 767 767231 1385131 NM RT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 DURING CHECK-C MAINT, FOUND ON RT WING THE TRAILING EDGE FLAP TOP SIDE OF I/B TRAILING EDGE FLAP AT O/B END WAS DELAMINA TED APPROX 2 FT IN FROM O/B END. INSTALLED 9 IN BY 12 IN METAL HOT BONDED DOUBLER PER SRM 57-53-01 AND 57-70-10. 2 L 7 2 4F RT A1NM 1998112000539 19981120 00539 NM 1998 11 20 TWAA9818408 1 19981110 A 5314 KEEL BEAM BOEING 767 767231 1385131 NM FUSELAGE CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 607TW 22570 DURING CHECK-C MAINT, INSIDE THE KEEL BEAM ACCESS PANEL 149BL FOUND HEAVY CORROSION TOP SIDE OF LT BEAM IN 3 PLACES. RE MOVED CORROSION, ALODINED AND PRIMED PER SRM 53-50-12. 2 L 7 2 4F RT A1NM 1998112000540 19981120 00540 NM 1998 11 20 TWAA9818409 1 19981101 A 5754 SKIN BOEING 767 767205 1385121 NM NR 6 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT, O/B SIDE REPAIR DELAMINATED. REPLACED CORRODED HONEYCOMB AND INSTAL LED 12.5 IN BY 13 IN METAL OVERLAY PER SRM 51-70-10. 2 L 7 2 4F RT A1NM 1998112000541 19981120 00541 NM 1998 11 20 TWAA9818410 1 19981031 A 5754 SKIN BOEING 767 767205 1385121 NM NR 10 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, FOUND RT WING NR 10 LEADING EDGE SLAT TOP DELAMINATED O/B OF CENTER, AND I/B OF OLD PATCH, 2 IN WI DE BY 4 IN LONG. REMOVED PREVIOUS REPAIR AND ADDITIONAL DELAMINATED SKIN. REMOVED DAMAGED CORE. MADE 10 IN BY 25 IN C ORE AND SKIN METAL TO METAL HOT BOND REPAIR PER SRM 51-70-10 FIG 7. 2 L 7 2 4F RT A1NM 1998112000542 19981120 00542 NM 1998 11 20 TWAA9818411 1 19981030 A 5754 SKIN BOEING 767 767205 1385121 NM NR 6 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT I/B REPAIR HAD DELAMINATION. REMOVED DELAMINATED DOUBLER AND REPAIRE D DAMAGED CORE AND INSTALLED 10 BY 12 IN HOT BOND REPAIR PER 51-70-10. 2 L 7 2 4F RT A1NM 1998112000543 19981120 00543 NM 1998 11 20 TWAA9818412 1 19981030 A 5730 SKIN BOEING 767 767205 1385121 NM NR 6 LE SLAT DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 DURING CHECK-C MAINT, FOUND REPAIR COMING LOOSE ON THE LEADING EDGE OF LT WING, AFT OF OF NR 6 LEADING EDGE SLAT I/B SID E. REMOVED DELAMINATED REPAIR, REPLACED WITH 7 BY 7 IN HOT BONDED REPAIR PER SRM 51-70-07. 2 L 7 2 4F RT A1NM 1998112000544 19981120 00544 NM 1998 11 20 RAAA98B2046 1 19981103 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 AFT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998112000545 19981120 00545 WP 1998 11 20 CALA9802055 1 19981113 A 5280 ACA3810502 HINGES DOUG DC10 DC1030 3023501 WP RT NLG DOOR BROKEN A CALA O OTHER E VIBRATION/BUFFET DE DESCENT 1 SW 09 68065 87285 46590 A LOUD VIBRATION WAS OBSERVED WHILE ON DESCENT. THE VIBRATION SEEMED TO WEAKEN WHEN SLOWED TO 250 KNOTS. THE GEAR OPER ATED NORMAL UPON LANDING WITH LESS VIBRATION. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD NLG DOOR DUE TO BROKEN HI NGES. THE RT FORWARD NLG DOOR DRIVE LINK WAS REPLACED DUE TO A BROKEN ROD END AND HOUSING DAMAGE. THE LT AFT NLG DOOR STRUT BRACKET WAS REPLACED DUE TO DAMAGE. THE DOORS WERE RIGGED AND OPERATIONAL CHECKS WERE GOOD IAW MM 32-23-01. 2 L 7 3 4F A22WE 1998112000546 19981120 00546 WP 1998 11 20 CALA9802056 1 19981111 A 3397 WIRE DOUG DC9 DC982 3022082 WP ROW 26 BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 77827 49487 INSPECTION FOUND EMERGENCY SEAT MOUNTED LIGHTS INOPERATIVE AT ROW 14 TO 27. A BROKEN WIRE UNDER SEAT ROW 26 WAS REPAIRE D. 2 L 7 2 4F A6WE 1998112000547 19981120 00547 NM 1998 11 20 CALA9802057 1 19981111 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 986.5 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. REPAIRED IAW ECRA 5310-03450. 2 L 7 2 4F RT A16WE 1998112000548 19981120 00548 WP 1998 11 20 CALA9802058 1 19981112 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 285 DAMAGED A CALA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 92874 49122 THE FUSELAGE SKIN AT STA 285 BETWEEN LONGERON 23L AND 24L WAS BENT DUE TO IMPACT BY A TRUCK. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-04 FIGURE 38 SHEET 21. 2 L 7 2 4F A6WE 1998112000549 19981120 00549 WP 1998 11 20 CALA9802059 1 19981112 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 205 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND RIGHT CENTER SEAT TRACK CORRODED AT STA 205. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998112000550 19981120 00550 NM 1998 11 20 CALA9802060 1 19981113 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 242 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND COCKPIT FLOORBEAM CORRODED AT STA 242 FORWARD OF RT GEAR MANUAL EXTENSION. SUPPORT BRACKET AND FASTENE RS WERE REMOVED AND A NEW BRACKET AND ANGLE SUPPORTS WERE INSTALLED IAW SRM 53-10-8 PAGE 52 AND 51-10-2 FIGURE 4. 2 L 7 3 4F A3WE 1998112000551 19981120 00551 NM 1998 11 20 CALA9802061 1 19981113 A 5210 WEB BOEING 727 727232 1384082 NM L-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 4 INCH CRACK IN MAIN ENTRY L-1 DOOR WEB AT TOP AFT CORNER OF DOOR. THE CRACKED AREA WAS REMOVED. A MOUNT AND RIB WERE INSTALLED IAW SRM 51-10-1, 51-10-2 AND 51-30-2, PAGE 2-7. 2 L 7 3 4F A3WE 1998112000552 19981120 00552 NM 1998 11 20 CALA9802062 1 19981113 A 5720 CHORD BOEING 727 727232 1384082 NM WS 645-636 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND RT WING LOWER CHORD CORRODED AT WS 645 TO 636. THE CORROSION WAS REMOVED AND A DOUBLER REPAIR WAS INST ALLED IAW SRM 51-10-2, PAGE 14, 51-10-2, PAGE 4 AND 51-30-10 PAGE 1. 2 L 7 3 4F A3WE 1998112000553 19981120 00553 NM 1998 11 20 CALA9802063 1 19981113 A 5720 ANGLE BOEING 727 727232 1384082 NM WS 115 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 2 INCH CRACK IN SPAR ATTACH ANGLE OF RT WING LEADING EDGE RIB AT WS 115. THE CRACK WAS STOP DRILLED IAW SRM 51-40-3. AN ANGLE REPAIR WAS INSTALLED IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998112000554 19981120 00554 NM 1998 11 20 CALA9802064 1 19981113 A 5242 FRAME BOEING 727 727232 1384082 NM E & E DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND A 1 INCH CRACK IN E & E COMPARTMENT DOOR FRAME BEHIND RIGHT STOP FITTING. THE DOOR ASSEMBLY WAS REPLAC ED IAW MM 52-40-11. 2 L 7 3 4F A3WE 1998112000555 19981120 00555 NM 1998 11 20 CALA9802065 1 19981113 A 3350 P4010021 BATTERY DME BOEING 727 727232 1384082 NM CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND THE AFT FLIGHT ATTENDANT STATION LOWER FLASHLIGHT WEAK. THE FLASHLIGHT BATTERY WAS REPLACED IAW MM 25- 20-0. 2 L 7 3 4F A3WE 1998112000556 19981120 00556 SO 1998 11 20 COMA9810261 1 19981111 A 3350 SIGN EMB 120 EMB120RT SO ROW 8 BROKEN A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 263CA 1255 EMERGENCY EXIT SIGN AT ROW 8 BROKEN. REMOVED AND REPLACED EXIT SIGN ASSY. 2 L 7 2 4T RT A31SO 1998112000557 19981120 00557 SO 1998 11 20 COMA9810262 1 19981111 A 3350 SIGN EMB 120 EMB120RT SO ROW 8 FAILED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 463CA 1267 EMERGENCY EXIT SIGN AT ROW 8 BROKEN. REMOVED AND REPLACED EXIT SIGN. 2 L 7 2 4T RT A31SO 1998112000558 19981120 00558 SO 1998 11 20 COMA9810263 1 19981114 A 3350 1317 LAMP EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 159A 120159 ONE EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 1998112000559 19981120 00559 SO 1998 11 20 COMA9810264 1 19981113 A 6120 78249046 PCU EMB 120 EMB120RT SO RIGHT MALFUNCTION A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 246CA 18381 120223 RIGHT HAND NP VARIED BETWEEN 98 AND 102 PERCENT. REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A31SO 1998112000560 19981120 00560 SO 1998 11 20 COMA9810265 1 19981113 A 3260 922AA2YA6P2722 SENSOR EMB 120 EMB120RT SO LT MLG MALFUNCTION A COMA K NONE N FALSE WARNING CR CRUISE 1 SO 01 257CA 120248 LEFT HAND MLG A-SYSTEM POSITION INDICATION LIGHTS INDICATED DOWN WHEN GEAR WAS UP. REPLACED THE DOWNLOCK PROXIMITY SENS OR. 2 L 7 2 4T RT A31SO 1998112000561 19981120 00561 SO 1998 11 20 COMA9810266 1 19981111 A 3350 BULB EMB 120 EMB120RT SO ROW 5 FAILED A COMA K NONE L NO TEST UK UNKNOWN 1 SO 01 244CA 1217 EMERGENCY FLOOR LIGHT AT ROW 5 INOPERABLE. REMOVED AND REPLACED BULB. 2 L 7 2 4T RT A31SO 1998112000562 19981120 00562 SO 1998 11 20 COMA9810267 1 19981113 A 3260 922FS2A6N2735 SENSOR EMB 120 EMB120RT SO LT MLG FAILED A COMA O OTHER N FALSE WARNING DE DESCENT 1 SO 01 257CA 1248 LANDING GEAR HANDLE WOULD NOT GO TO THE DOWN POSITION WITHOUT USING OVERRIDE. REPLACED LEFT MAIN GEAR LOWER PROXIMITY S ENSOR. 2 L 7 2 4T RT A31SO 1998112000563 19981120 00563 SO 1998 11 20 COMA9810268 1 19981113 A 6120 78249012 PCU EMB 120 EMB120RT SO RT ENGINE FAILED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 246CA 15705 1223 AFTER TAKEOFF, NR 2 ENGINE NP VARIED FROM 98 TO 102.2 PERCENT. REPLACED PROPELLER CONTROL UNIT. 2 L 7 2 4T RT A31SO 1998112000564 19981120 00564 NM 1998 11 20 UPS98228161 1 19981103 A 5312 BULKHEAD BEAM BOEING 727 72762C 138402C NM BS 1183 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE-C, CRACK FOUND ON VERTICAL BEAM AT RIGHT BUTTOCK LINE 26.83 AT BS 1183 BULKHEAD CRACK ON VERTICAL BE AM AT RBL 26.85, BS 1183 BULKHEAD REPAIRED IAW APPENDIX D OF B727-5311-0631. 2 L 7 3 4F A3WE 1998112000565 19981120 00565 NM 1998 11 20 UPS98228162 1 19981102 A 5320 SUPPORT BOEING 727 72762C 138402C NM BS 780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE-C, CORROSION ON ANGLE SUPPORT FOR FRONT NET TIE DOWN BS 780 LBL 60.00. ANGLE SUPPORT REPLACED IAW SRM 5 1-30-2. 2 L 7 3 4F A3WE 1998112000566 19981120 00566 NM 1998 11 20 UPS98228166 1 19981103 A 5350 FRAME BOEING 727 72762C 138402C NM FUSELAGE CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE-C, FUSELAGE SLIDING FAIRING NR 3601 HAS CORRODED FRAME AT LOWER FWD CORNER. REPAIRED IAW SRM 53-10-4 AN D TYPICAL WEB REPAIRS IAW SRM 51-40-3. 2 L 7 3 4F A3WE 1998112000567 19981120 00567 NM 1998 11 20 UPS98228167 1 19981113 A 3350 BATTERY BOEING 727 727247 138408F NM COCKPIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 208UP 21701 INSPECTION TYPE-N/A, PREFLIGHT COCKPIT EMER EXIT LIGHT CAME OUT OF ASSEMBLY ABOVE DOOR. INSTALLED NEW BATTS AND REPLACE D ASSEMBLY, OPS CHECK OK. 2 L 7 3 4F A3WE 1998112000568 19981120 00568 WP 1998 11 20 UPS98828155 1 19981019 A 5720 36418402N FITTING DOUG DC8 DC871F 302199D WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C, 3 RT WING T/E, THE WING JACK POINT FITTING IS CRACKED AT THE UPPER END. REMOVED AND REPLACED THE WIN G JACK POINT FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1998112000569 19981120 00569 WP 1998 11 20 UPS98828156 1 19981020 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 1060 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C3, FS 1060, JUST BELOW LONG 21R THE FINGER DOUBLER IS CRACKED. REPAIRED FINGER DOUBLER IAW DHC SK 779- 268. 2 L 7 4 4F RT 4A25 1998112000570 19981120 00570 WP 1998 11 20 UPS98828157 1 19981022 A 5510 36538021 FITTING DOUG DC8 DC871F 302199D WP RT HORZ STAB CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C3, RT HORIZONTAL STAB O/B CENTER STA XFA 178 FRONT SPAR SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3653802 AND SRM 51-1-20D, 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1998112000571 19981120 00571 WP 1998 11 20 UPS98828158 1 19981029 A 5320 97537923 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 1120 - 1140 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C3, FS 1120 TO 1140 AT LONG 33L THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTA L IAW DWG 9753792 AND SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1998112000572 19981120 00572 WP 1998 11 20 UPS98828159 1 19981104 A 5720 576960036 DOUBLER DOUG DC8 DC871F 302199D WP WS 598.375 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE-C3, RT WING L/E LWR SKIN AT XFS 598.375 THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FAB RICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21. 2 L 7 4 4F RT 4A25 1998112000573 19981120 00573 NM 1998 11 20 98FDEA00696 1 19981114 A 2750 96010214 TRANSMITTER DOUG MD11 MD11F 3023600 NM LT TE FLAP INOP A FDEA A J UNSCHED LANDING DUMP FUEL N FALSE WARNING TO TAKEOFF 1 SO 25 616FE 48747 FLAP DISAGREE ALERT, LEFT FLAP SHOW 20 DEG, RT FLAP SHOW 25 DEG. ACCOMP FLAP 25 LAND AT PANC FLAP HANDLE REMAIN AT T/O. REMOVED AND REPLACED LT O/B FLAP POS TRANSMITTER AS PER MM 27-54-02-4 IND SAT AS PER ADJ TEST. 2 L 7 3 4F RT A22WE 1998112000574 19981120 00574 NM 1998 11 20 98FDEA00697 1 19981112 A 2781 INDICATION BOEING 727 7272S2F 1384O81 NM LE FLAPS MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 206FE 22928 REPEAT WRITEUP FLAPS RETRACT WITH LEAD EDGE FLAP LIGHT OUT THE LEAD EDGE FLAP AMBER LIGHT ILLUM. OPER FLAPS AND SLATS I N ALL POS. VISUAL INSP, THE MOVEMENT OF FLAPS AND SLATS, IT OPER NORM. CAN'T DUP ON GROUND, PERFORMED T/O WARN CK ALL SWITCHES OPER NORM. A/C OK TO CONT. 2 L 7 3 4F A3WE 1998112000575 19981120 00575 EU 1998 11 20 98FDEA00698 1 19981113 A 7830 SWITCN AIRBUS 310 A310222 3930315 EU NR 1 ENGINE LOOSE A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 419FE 345 NR 1 ENG REVERSER UNLOCK LIGHT AT T/O PWR. REJECTED T/O RETURN TO GATE. THRUST REVERSER NR 1 DEFER PER MEL 78-1 AND DE ACTIVATED IN FWD THRUST POS. T/S FOUND UNLOCK SWITCH LOOSE AT LT SIDE. ADJUSTED AND RESECURED UNLOCK SWITCH. REACTIVA TED PER MM 78-31-01. OPS CK NR 1 ENG T/REV USING APU AIR AND HOSE, FOUND T/REV OPER NORM AND ALL IND NORM. 2 L 7 2 4F RT A35EU 1998112000576 19981120 00576 NM 1998 11 20 98FDEA00699 1 19981114 A 3213 NAS4504U11 BOLT DOUG MD11 MD11F 3023600 NM LT MLG STRUT SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 DURING LT MLG SHOCK-STRUT LWR BEARING SEAL REPLACEMENT, ANTI-ROTATION BOLT (P/N NAS 4504 U11) FOUND SHEAR FROM CHAMBER ( ARG 7477-1) OF UPPER CYLINDER ASSY. *S/D* LT MLG CHAMBER ASSY REPLACED PER CMM 32-11-12. 2 L 7 3 4F RT A22WE 1998112000577 19981120 00577 NM 1998 11 20 98FDEA00700 1 19981116 A 5312 6516350344 BULKHEAD WEB BOEING 727 72725 1384006 NM BS 1183 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 WHILE WORKING NR 486 FOUND A CRACK IN 1183 BULKHEAD WEB AT RBL 12, WL 202. *S/D* REPAIRED BS 1183 BULKHEAD WEB PER SRM 53-10-9. 2 L 7 3 4F A3WE 1998112000578 19981120 00578 WP 1998 11 20 DHL98804003 1 19981110 A 3610 1944302 PRE COOLER DOUG DC8 DC873F 302199F WP NR 1 & 2 ENGINE MALFUNCTIONED A DHLA A J UNSCHED LANDING DUMP FUEL J M WARNING INDICATION OVER TEMP CR CRUISE 1 SO 01 804DH 53452 46124 LEFT MANIFOLD TEMP RUNNING 250 DEGREE WITH NO ANTI-ICE ON, WITH ENG ANTI-ICE ON NR 1 MANIFOLD AIR OVER TEMP LIGHT ILLUM INATED. TEMP WENT TO 280 DEGREES. REPLACED NR 1 AND NR 2 ENGINE PRECOOLERS. GROUND OPS CHECK NORMAL. 2 L 7 4 4F RT 4A25 1998112000580 19981120 00580 WP 1998 11 20 TC8A98082 1 19981115 A 2910 HYD FLUID DOUG DC8 DC862F 3021972 WP HYD SYST REQD SERVICE A TC8A D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 GL 23 183SK 45904 RETURNED TO THE RAMP DUE TO A DECREASE IN HYDRAULIC QUANTITY GAUGE. SERVICED HYDRAULIC SYSTEM. OPS RAN REVERSER PUMP, SPOILER PUMP, CHECKED AILERONS THEN CHECKED ALL AREAS OF W/W AND FLAP WELLS FOR LEAKS, NO LEAKS NOTED AT THIS TIME. 2 L 7 4 4F 4A25 1998112000628 19981120 00628 NM 1998 11 20 SWAA982759 1 19981105 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 373SW 26581 DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS PATH LIGHTS (RED) OUT AT MIDDLE CABIN AT EMERGENCY EXIT ROW. REPLACED L IGHT BULBS AND REINSTALLED LIGHT ASSY OPS, CKD OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000629 19981120 00629 NM 1998 11 20 SWAA982760 1 19981105 A 3350 6104781 BATTERY BOEING 737 7373H4 1384600 NM ROW 1-5 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 311SW 23333 DURING WALKAROUND CHECK, FOUND EGRESS LIGHTS ROWS 1 TO 5 INOPERATIVE. REMOVED AND REPLACED FWD EMERGENCY LIGHTS BATTERY ASSY PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000630 19981120 00630 NM 1998 11 20 SWAA982761 1 19981105 A 5320 ANGLE BOEING 737 7372H4 138448C NM LT MLG CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND LT MAIN LANDING GEAR STABILIZER BAR FAIRING L-ANGLES PITTED AND CORRODED AROUND BOLT HOL ES. REMOVED AND REPLACED L-ANGLES PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000631 19981120 00631 NM 1998 11 20 SWAA982762 1 19981105 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 1011 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED ANGLES AT BS 1011, RBL 42, WL 208.5. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000632 19981120 00632 NM 1998 11 20 SWAA982763 1 19981105 A 5320 WEB BOEING 737 7372H4 138448C NM BS 907-927 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND MISDRILLED HOLE IN WEB AT BS 907 TO 927, RBL 59-63, WL 208. REMOVED AND REPLACED PER BO EING SRM. 2 L 7 2 4F A16WE 1998112000633 19981120 00633 NM 1998 11 20 SWAA982764 1 19981105 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 500-520 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND 5 CHAFED AREAS ON INTERCOSTAL AT NUTCLIP LOCATIONS BS 500B-520, BL 0, WL 208. REMOVED A ND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000634 19981120 00634 NM 1998 11 20 SWAA982765 1 19981105 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP MECHANICAL DAMAGE AT BS 500 RT, STR 7R. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998112000635 19981120 00635 NM 1998 11 20 SWAA982766 1 19981105 A 5320 WEB BOEING 737 7372H4 138448C NM BS 328 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND ELONGATED HOLES FROM RBL 25 TO RBL 30, WL 207 AT BS 328. WHILE WORKING CUSTOMER CARD NR A617871. REPAIRED DAMAGED TO WEB BS 328 PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000636 19981120 00636 NM 1998 11 20 SWAA982767 1 19981105 A 5320 WEB BOEING 737 7372H4 138448C NM BS 328 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND ELONGATED HOLES AT RBL 14, LBL 12, LBL 22.5, WL 207 AT BS 328. REPAIRED DAMAGED WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000637 19981120 00637 NM 1998 11 20 SWAA982768 1 19981105 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 1138 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND SHEAR TIE BELOW STR 5A RT, BS 1138 CRACKED AT FASTENER HOLE. REMOVED AND REPLACED SHEAR TIE PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000638 19981120 00638 NM 1998 11 20 SWAA982769 1 19981105 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 1106-1154 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND SPLICE STRAP AT BS 1106-11 TO 4, STR 5AR CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000639 19981120 00639 NM 1998 11 20 SWAA982770 1 19981105 A 3350 SIGN BOEING 737 7373H4 1384600 NM SERVICE DOOR BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 646SW 28331 DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER BOEI NG MM. 2 L 7 2 4F RT A16WE 1998112000640 19981120 00640 NM 1998 11 20 SWAA982771 1 19981105 A 3350 LIGHT BOEING 737 7373A4 1384585 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED C3 CHECK, FOUND SEVERAL LIGHTS INOPERATIVE ON AFT END OF EMERGENCY LIGHTS STRIP. RELAMPED LIGHTS AT EN D OF STRAP PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000641 19981120 00641 NM 1998 11 20 SWAA982772 1 19981105 A 5320 WEB BOEING 737 7373A4 1384585 NM CARGO DOORWAY TORN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D CHECK, FOUND WEB TORN AT LOWER FWD CORNER OF DOOR CUTOUT. REMOVED AND REPLACED WEB PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998112000642 19981120 00642 NM 1998 11 20 SWAA982773 1 19981105 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/4D-CHECK, FOUND VERTICAL WEB CRACKED AT BS 947, LBL 18 NEXT TO STR 26L. REMOVED AND REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998112000643 19981120 00643 NM 1998 11 20 SWAA982774 1 19981105 A 3150 WARNING BOEING 737 7373H4 1384600 NM SPEED BRAKES ACTIVATED A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING CL CLIMB 1 SW 07 362SW 26573 AIRCRAFT ABORTED TAKEOFF. INFO ONLY TAKEOFF POWER ADVANCED AND T/O WARNING HORN SOUND. SPEED BRAKE HANDLE CYCLED AND WA RNING HORN DID NOT RETURN. ALL SYSTEMS CHECKED NORMAL. 2 L 7 2 4F RT A16WE 1998112000644 19981120 00644 NM 1998 11 20 SWAA982775 1 19981108 A 3411 O-RING BOEING 737 7373H4 1384600 NM LT PITOT SYS FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 602SW 27953 AIR TURNBACK DUE TO ALTIM AND AIRSPEED CAPTAIN SIDE ERRONEOUS AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMO VED AND REPLACED O-RING ON NR 1 AIR DATA PITOT LINE. OPS AND LEAK CK GOOD AS PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000645 19981120 00645 NM 1998 11 20 SWAA982776 1 19981107 A 7933 TEMP BULB BOEING 737 7372H4 138448C NM NR 2 ENGINE OIL MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 096SW 23055 AIRCRAFT DIVERTED DUE TO NR 2 ENGINE OIL TEMP 135 DEG FOR 15 MIN. SHUTDOWN NR 2 ENGINE. AIRCRAFT MADE AN UNEVENTFUL LA NDING. REPLACED NR 2 ENGINE OIL TEMP BULB. ENG RUN AT 92 PERCENT N2 AND OPS CK OK PER BOEING MM. 2 L 7 2 4F A16WE 1998112000646 19981120 00646 NM 1998 11 20 SWAA982777 1 19981106 A 5320 WEB BOEING 737 7372H4 138448C NM BS 992-1016 PUNCTURED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND WEB PUNCTURED AT BS 992 TO 1016, LBL 40 TO 45, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000647 19981120 00647 NM 1998 11 20 SWAA982778 1 19981106 A 5320 WEB BOEING 737 7372H4 138448C NM BS 907-927 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND WEB AT BS 907 TO 927, LBL 59 TO 63, WL 208 HAS MISDRILLED HOLE AT BS 920, LBL 59. REMOV ED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000648 19981120 00648 NM 1998 11 20 SWAA982779 1 19981106 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 920 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND L-ANGLE AT BS 920, LBL 59 TO 63, WL 207 HAS MISDRILLED HOLE AT BS 920, LBL 59, WL 207. R EMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000649 19981120 00649 NM 1998 11 20 SWAA982780 1 19981106 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 920 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND L-ANGLE AT BS 920, RBL 59 TO 63, WL 208 HAS MISDRILLED HOLE. REMOVED AND REPLACED PER B OEING SRM. 2 L 7 2 4F A16WE 1998112000650 19981120 00650 NM 1998 11 20 SWAA982781 1 19981106 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 986-999 CORRODED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND DRILL START AND CORRODED FLOOR SUPPORT ANGLE AT BS 986 TO 999, RBL 45, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000651 19981120 00651 NM 1998 11 20 SWAA982782 1 19981106 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 992-1010 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 992 TO 1010, LBL 40, WL 208. REMOVED AND REPLACED PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998112000652 19981120 00652 NM 1998 11 20 SWAA982783 1 19981106 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED UPPER T-CHORD OF 294 FLOORBEAM, AT WL 208. REMOVED AND REPLACED T-CHORD PER BO EING SRM. 2 L 7 2 4F A16WE 1998112000653 19981120 00653 NM 1998 11 20 SWAA982784 1 19981106 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 302 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 302, LBL 12, WL 208. REMOVED AND REPLACED FLOOR SUPPORT PE R BOEING SRM. 2 L 7 2 4F A16WE 1998112000654 19981120 00654 NM 1998 11 20 SWAA982785 1 19981106 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 500 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND DAMAGE FASTENER HEAD ON FWD CARGO PIT FRAME SPLICE AT BS 500A, STR 25R. REMOVED AND REP LACED FASTENER PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000655 19981120 00655 NM 1998 11 20 SWAA982786 1 19981106 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 420 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND MECHANICAL DAMAGE ON STRINGER CLIP (14L) AT BS 420. REMOVED AND REPLACED STRINGER CLIP PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000656 19981120 00656 NM 1998 11 20 SWAA982787 1 19981106 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 787 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CHAFING AROUND FASTENER HOLES IN FLOORBEAM AT BS 787, RBL 10 TO LBL 11, WL 208. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM AND INSTALLED REPAIR STRAP PER SWA TI-A53-014. 2 L 7 2 4F A16WE 1998112000657 19981120 00657 NM 1998 11 20 SWAA982788 1 19981106 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 727 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CHAFING AROUND FASTENER HOLES IN FLOORBEAM AT BS 727B, LBL 35 TO LBL 58, WL 208. REMOVE D AND REPLACED FLOORBEAM PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000658 19981120 00658 NM 1998 11 20 SWAA982789 1 19981106 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORROSION ON TOP FLANGE OF FLOORBEAM AT BS 947, RBL 44 TO RBL 53, WL 208. REMOVED AND R EPLACED FLOORBEAM PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000659 19981120 00659 NM 1998 11 20 SWAA982790 1 19981106 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 420 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORROSION ON TOP FLANGE OF FLOORBEAM AT NUTCLIP LOCATION AT BS 420, RBL 20, WL 208. REM OVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000660 19981120 00660 NM 1998 11 20 SWAA982791 1 19981106 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND AREAS OF BARE METAL AND CHAFING ON FLOORBEAM AT BS 344, LBL 57 TO RBL 57, WL 208.1. REM OVED AND REPLACED UPPER CHORD PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000661 19981120 00661 NM 1998 11 20 SWAA982792 1 19981106 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 380 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP AT BS 380, STR 2 RT HAS MECHANICAL DAMAGE. REMOVED AND REPLACED STRIN GER TIE CLIP PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000662 19981120 00662 NM 1998 11 20 SWAA982793 1 19981106 A 5320 CLIP BOEING 737 7372H4 138448C NM BS 440 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER TIE CLIP AT BS 440, STR 7 RT HAS MECHANICAL DAMAGE. REMOVED AND REPLACED STRIN GER TIE CLIP PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000663 19981120 00663 NM 1998 11 20 SWAA982794 1 19981106 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 409 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 409 BETWEEN STR 21R AND 22R. CUT OUT DAMAGED AREA, REMOVED AND REPLAC ED DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000664 19981120 00664 NM 1998 11 20 SWAA982795 1 19981106 A 5400 ANGLE BOEING 737 7373A4 1384585 NM NR 2 PYLON CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED RON CHECK, FOUND NR 2 ENG O/B PYLON AFT MOUNT AREA ABOVE ENG TAILPIPE L-ANGLE INSIDE AT TOP FASTENER IS CRACKED. REPAIRED ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000665 19981120 00665 NM 1998 11 20 SWAA982796 1 19981107 A 3350 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 721WN 22697 DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS LIGHTING FILLER TRACK WARPED AFT LOUNGE AREA RT SIDE. REPAIRED EGRESS L IGHTS, OPS CK GOOD PER BOEING MM. 2 L 7 2 4F A16WE 1998112000666 19981120 00666 NM 1998 11 20 SWAA982797 1 19981107 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 907 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 333SW 23697 DURING SCHEDULED C4 CHECK, FOUND DENTED FUSELAGE SKIN FWD OF BS 907 AND O/B OF STR 27L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000667 19981120 00667 NM 1998 11 20 SWAA982798 1 19981107 A 3350 LIGHT BOEING 737 7375H4 138449D NM ROW 8C INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED C1 CHECK, FOUND EMERGENCY FLOOR LIGHT ADJACENT TO SEAT 8C INOPERATIVE. RELAMPED EMERGENCY FLOOR LIGHT ADJACENT TO SEAT 8C PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000668 19981120 00668 NM 1998 11 20 SWAA982799 1 19981107 A 5315 FLOORBEAM BOEING 737 7375H4 138449D NM BS 314 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 521SW 25320 DURING SCHEDULED BC2 CHECK, FOUND FLOORBEAM WEB LOWER STRAP CRACKED AT BS 314, BL 0. REPAIRED STABILIZER STRAP PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998112000669 19981120 00669 NM 1998 11 20 SWAA982800 1 19981108 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 980 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 323SW 23344 DURING SCHEDULED RON CHECK, FOUND SKIN CRACKED APPROX 3 INCHES LENGTH AT BS 980, STR 21L. REPAIRED SKIN PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000670 19981120 00670 NM 1998 11 20 SWAA982801 1 19981108 A 3246 26066712 WHEEL BOEING 737 7373Q8 1384670 NM NR 1 & 2 MAIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 AFTER LANDING FOUND EVIDENCE LEFT MAIN LANDING GEAR DEPARTED RUNWAY INTO DIRT. PERFORMED INSP PER 05-51-51-2, NO DAMAGE FOUND ON A/C. REMOVED AND REPLACED NR 1 MAIN AND NR 2 MAIN WHEEL ASSY AS PER CAUTION. 2 L 7 2 4F RT A16WE 1998112000671 19981120 00671 NM 1998 11 20 SWAA982802 1 19981109 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 995-1004 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT NUT CLIP BS 995 TO 1004, LBL 14, WL 208. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000672 19981120 00672 NM 1998 11 20 SWAA982803 1 19981109 A 5320 TRACK BOEING 737 7372H4 138448C NM BS 993 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED HAT TRACK AT NUT CLIP BS 993, LBL 18 TO LBL 41, WL 208. REMOVED AND REPLACED H AT TRACK PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000673 19981120 00673 NM 1998 11 20 SWAA982812 1 19981109 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 987 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOORBEAM AT NUT CLIP BS 987, RBL 45, LBL 45, WL 208. REMOVED AND REPLACED TOP CHORD AND ANGLES PER TI-A53-055. 2 L 7 2 4F A16WE 1998112000674 19981120 00674 NM 1998 11 20 SWAA982804 1 19981109 A 5320 WEB BOEING 737 7372H4 138448C NM BS 986-1016 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED WEB AT BS 986 TO 1016M RBL 39 TO 46, WL 208. REMOVED AND REPLACED WEB PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998112000675 19981120 00675 NM 1998 11 20 SWAA982805 1 19981109 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED AT BS 328 FLOORBEAM UPPER T-CHORD, RBL 35, WL 208. REMOVED AND REPLACED UPPER CHORD AND ANGLES PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000676 19981120 00676 NM 1998 11 20 SWAA982806 1 19981109 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 500-520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED RIGHT HAND INTERCOSTAL AT BS 500B TO BS 520, STR 26R. REMOVED AND REPLACED INT ERCOSTAL PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000677 19981120 00677 NM 1998 11 20 SWAA982807 1 19981109 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED RIGHT HAND INTERCOSTAL AT BS 500A TO BS 500B, STR 26R. REMOVED AND REPLACED IN TERCOSTAL PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000678 19981120 00678 NM 1998 11 20 SWAA982808 1 19981109 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 277-294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CRACKED INTERCOSTAL AT BS 277 TO 294.5, BL 0, WL 208. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000679 19981120 00679 NM 1998 11 20 SWAA982809 1 19981109 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 1010 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT AT BS 1010, LBL 8, WL 208 AROUND NUT CLIP HOLES. REMOVED AND REP LACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000680 19981120 00680 NM 1998 11 20 SWAA982810 1 19981109 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 1010 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED TOP FLANGE OF FLOORBEAM AT BS 947, LBL 24 TO LBL 26 WL 208. 2 L 7 2 4F A16WE 1998112000681 19981120 00681 NM 1998 11 20 SWAA982811 1 19981109 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 767 CHAFING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CHAFING AROUND FASTENER HOLES IN FLOORBEAM AT BS 767, RBL 10 TO LBL 11, WL 208. CUT OUT DAMAGE AREA AND REPAIRED PARTS PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000682 19981120 00682 NM 1998 11 20 SWAA982813 1 19981109 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 500-520 BROKEN A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL BROKEN AT BS 500B TO 520, LBL 21, WL 156. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000683 19981120 00683 NM 1998 11 20 SWAA982814 1 19981109 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND SCREW HEAD DRILLED OFF ON LT T-ANGLE BETWEEN BS 727C AND BS 727D. REMOVED AND REPLAC ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000684 19981120 00684 NM 1998 11 20 SWAA982815 1 19981109 A 5330 SKIN BOEING 737 7373Y0 1384671 NM BS 887 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED A2 CHECK, FOUND SKIN CRACKED AT BS 887, STR 21R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000685 19981120 00685 NM 1998 11 20 SWAA982816 1 19981109 A 3350 LIGHT BOEING 737 7373H4 1384600 NM ROW 14 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 643SW 27716 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT ON LT OVERHEAD BIN AT ROW 14 IS INOPERATIVE. REPLACED EMERGENCY L IGHT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000686 19981120 00686 NM 1998 11 20 SWAA982818 1 19981110 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 837 DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 649SW 27719 AIRCRAFT DAMGE BY BAG CART, DENTED AND GAUGE AFT LEFT HAND FUSELAGE BS 837 AT LOWER SKIN LAP JOINT. WATER LINE STRINGER FLANGE BENT AFT CARGO HOLD FLOOR. OPENED CARGO PANEL, CUT OUT DAMAGE AREA, FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM. CLOSED CARGO PANEL AND RESTORED ORIGINAL FINISH. 2 L 7 2 4F RT A16WE 1998112000687 19981120 00687 NM 1998 11 20 SWAA982819 1 19981110 A 3350 1060091101 BATTERY PACK BOEING 737 7372H4 138448C NM COCKPIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 103SW 23109 DURING CHECK, FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER BOE ING MM. 2 L 7 2 4F A16WE 1998112000688 19981120 00688 1998 11 20 SWAA982820 4 19981110 A 3418 861CAS2 SENSOR BOEING 737 7373T5 NM LT STALL WARNING MALFUNCTIONED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 694SW 23061 AIR TURNBACK DUE TO STALL WARNING AT LIFTOFF. AIRSPEED NORMAL ON ALL INDICATIONS. WARNING QUIT AT TOUCHDOWN. AIRCRAFT MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED LT AOA SENSOR AND OPS CK GOOD PER BOEING MM. AIRCRAFT RECERTIFIED TO CAT IIIA STATUS. 2 L 7 2 4F RT A16WE 1998112000689 19981120 00689 NM 1998 11 20 SWAA982821 1 19981110 A 3350 BULB BOEING 737 7373H4 1384600 NM SERVICE DOOR MISSING A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 324SW 23414 DURING SCHEDULED C1 CHECK, FOUND CABIN FWD SERVICE DOOR LOWER EMERGENCY EXIT LIGHT BAR MISSING ONE LIGHT. RELAMPED FWD SERVICE DOOR LWR EMERGENCY EXIT LIGHT BAR PER MM. 2 L 7 2 4F RT A16WE 1998112000690 19981120 00690 NM 1998 11 20 SWAA982822 1 19981110 A 3350 BULB BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 105SW 23249 DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE ON BULLNOSE AT 14 LEFT. RELAMPED PER BOEING MM, OPS C HECK OK. 2 L 7 2 4F A16WE 1998112000691 19981120 00691 NM 1998 11 20 SWAA982823 1 19981110 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 400-420 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL DENTED AT BS 400 TO 420, LBL 21, WL 156. REMOVED AND REPLACED INTERCOSTAL P ER BOEING SRM. 2 L 7 2 4F A16WE 1998112000692 19981120 00692 NM 1998 11 20 SWAA982824 1 19981110 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 500-517 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 500+17, 2 ABOVE STR 18 RT. REPAIRED SKIN PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000693 19981120 00693 NM 1998 11 20 SWAA982825 1 19981110 A 3350 1060091101 BATTERY PACK BOEING 737 7372H4 138448C NM SERVICE DOOR MISSING A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 060SW 21812 DURING WALKAROUND CHECK, FOUND FWD SERVICE DOOR EMERGENCY LIGHTS BATTERY PACK ROBBED FOR A/C 103 COCKPIT POSITION. INST ALLED SERVICEABLE EMERGENCY LIGHT BATTERY PACK A ASSY PER BOEING MM. 2 L 7 2 4F A16WE 1998112000694 19981120 00694 NM 1998 11 20 SWAA982826 1 19981111 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 787-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND LIGHT CORROSION AROUND FASTENER ON FLOORBOARD SUPPORT FROM BS 787 TO BS 847 ABOVE STR 26R. REMOVED AND REPLACED FLOORBEAM AS PER SRM 26R. 2 L 7 2 4F RT A16WE 1998112000695 19981120 00695 NM 1998 11 20 SWAA982827 1 19981111 A 5320 ANGLE BOEING 737 7373A4 1384585 NM GALLEY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL UPPER L-ANGLE CRACKED IN TWO PLACES. REMOVED AND REPLACED UPPER L-ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000696 19981120 00696 NM 1998 11 20 SWAA982828 1 19981111 A 5320 INTERCOSTAL BOEING 737 7373A4 1384585 NM BS 328 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED ON AFT END AT BS 328, LBL 48. REMOVED AND REPLACED INTERCOSTAL P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000697 19981120 00697 NM 1998 11 20 SWAA982829 1 19981111 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND Z ANGLE ON FLOORBEAM CORRODED AT BS 344, LBL 59. REMOVED AND REPLACED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998112000698 19981120 00698 NM 1998 11 20 SWAA982830 1 19981111 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 380-400 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL L-ANGLE AT BS 380 TO 400, BL 0 CORRODED AND 4 CRACK. REMOVED AND REPLACE D L-ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000699 19981120 00699 NM 1998 11 20 SWAA982831 1 19981111 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 940-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM AT BS 940 TO 947, RBL 13. REMOVED AND REPLACED FLOORBEAM PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998112000700 19981120 00700 NM 1998 11 20 SWAA982832 1 19981111 A 5730 SKIN BOEING 737 7373H4 1384600 NM LT WING GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRANS CHECK, FOUND LT WING T/E LOWER WING SKIN JUST BELOW BEAM TO SPAR FITTING IS GOUGED AROUND FASTENE RS. REPAIRED LOWER WING SKIN BELOW BEAM TO SPAR FITTING PER TRAMCO ER 98-0940. 2 L 7 2 4F RT A16WE 1998112000701 19981120 00701 NM 1998 11 20 SWAA982833 1 19981111 A 3350 20131 BATTERY PACK BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 613SW 27931 DURING SCHEDULED SERVICE CHECK, FOUND FLOOR TRACK LIGHTING INOPERATIVE. REMOVED AND REPLACED CTR FLOOR TRACK LIGHTING BATTERY PACK AND POWER SUPPLY, OPS CHECK GOOD PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000702 19981120 00702 NM 1998 11 20 SWAA982835 1 19981111 A 3397 WIRE BOEING 737 7373H4 1384600 NM BS 907 FRAYED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661SW 23173 DURING SCHEDULED TRANSITION CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT BS 907 TO HAVE FRAYED WIRES ON BACK OF LIGHT. REPAIRED FRAYED WIRES ON OVERHEAD EMERGENCY EXIT LIGHT PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000703 19981120 00703 NM 1998 11 20 SWAA982836 1 19981111 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 344 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 371SW 26598 DURING SCHEDULED C2 CHECK, FOUND FLOORBEAM STRAP CRACKED JUST ABOVE AND O/B OF BATTERY IN E & E BAY OF BS 344. REPAIRED FLOORBEAM STRAP PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000704 19981120 00704 NM 1998 11 20 SWAA982837 1 19981111 A 5320 TIE STRAP BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR PANEL TIE STRAP AT BS 727+5, RBL 21, LBL 21, WL 156. REMOVED AND REPLACE D TIE STRAP PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000705 19981120 00705 NM 1998 11 20 SWAA982838 1 19981111 A 5320 TIE STRAP BOEING 737 7373H4 1384600 NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR PANEL TIE STRAP AT BS 727, RBL 21, LBL 21, WL 159. REMOVED AND REPLACED TIE STRAP PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000706 19981120 00706 NM 1998 11 20 SWAA982839 1 19981111 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 640 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND ANGLE, UPPER FASTENER HOLE IS ELONGATED AT BS 640, LBL 39, WL 166. REMOVED AND REPLACED DAMAGED AREA AND REPAIR ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000707 19981120 00707 NM 1998 11 20 SWAA982840 1 19981111 A 5320 BRACKET BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND APU SHROUD SUPPORT BRACKET IS CRACKED AT BS 727+2, BL 0, WL 163. REPAIRED APU SUPPORT B RACKET PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000708 19981120 00708 NM 1998 11 20 SWAA982841 1 19981111 A 5320 ANGLE BOEING 737 7372H4 138448C NM BS 993 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 933, BL 0, WL 208. REMOVED AND FABRICATED INTER COSTAL SUPPORT ANGLE PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000709 19981120 00709 NM 1998 11 20 SWAA982842 1 19981112 A 5511 RIB BOEING 737 7373H4 1384600 NM LT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB LEADING EDGE PANEL RIB CRACKED AT L/E BS 164.04. REMOVED AND REPLACE D RIB PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000710 19981120 00710 NM 1998 11 20 SWAA982843 1 19981112 A 5511 RIB BOEING 737 7373H4 1384600 NM LT HORIZ STAB CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND LT HORIZONTAL STAB LEADING EDGE PANEL RIB CRACKED AT L/E BS 170.34. REMOVED AND REPLACE D RIB PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000711 19981120 00711 NM 1998 11 20 SWAA982844 1 19981112 A 5330 SKIN BOEING 737 7373H4 1384600 NM L2 DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED C2 CHECK, FOUND .875 INCH CRACKED FUSELAGE SKIN AT LOWER HINGE CUTOUT OF L2 DOOR. REPAIRED PER SWA RA 1-353-1930 AND TI-353-070. 2 L 7 2 4F RT A16WE 1998112000712 19981120 00712 NM 1998 11 20 SWAA982845 1 19981112 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 503 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM KNICKED AT BS 503, RBL 9. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000713 19981120 00713 NM 1998 11 20 SWAA982846 1 19981112 A 5315 FLOORBEAM BOEING 737 7373Q8 1384670 NM BS 500 MISDRILLED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM ERRANT HOLE AT BS 500, LBL 13. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000714 19981120 00714 NM 1998 11 20 SWAA982847 1 19981112 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND BS 540, STR 21 SUPPORT ANGLE CRACKED. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000715 19981120 00715 NM 1998 11 20 SWAA982848 1 19981112 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND PRESSURE WEB CRACKED AT BS 663, LBL 33. REPAIRED WEB PER SWA RA 1-353-1924. 2 L 7 2 4F RT A16WE 1998112000716 19981120 00716 NM 1998 11 20 SWAA982849 1 19981112 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 847-867 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE CORRODED AT BS 847 TO 867. REMOVED AND REPLACED TRANSITION ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000717 19981120 00717 NM 1998 11 20 SWAA982850 1 19981112 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 867-887 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE CORRODED AT FASTENER HOLE BS 867 TO 887. EMOVED AND REPLACED TRA NSITION ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000718 19981120 00718 NM 1998 11 20 SWAA982851 1 19981112 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND PRESSURE WEB CRACKED AT BS 663, LBL 40. REPAIRED WEB PER SWA RA 1-353-1924. 2 L 7 2 4F RT A16WE 1998112000719 19981120 00719 NM 1998 11 20 SWAA982852 1 19981112 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED AFT FLOOR ANGLE AT BS 947. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000720 19981120 00720 NM 1998 11 20 SWAA982853 1 19981111 A 5320 FRAME BOEING 737 7373A4 1384585 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND FWD SERVICE DOOR FRAME CRACKED AT FWD LOWER CORNER AT BS 294.5, RBL 55. REPAIRED FRA ME PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000721 19981120 00721 NM 1998 11 20 SWAA982854 1 19981111 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 947.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 947.5, LBL 11. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000722 19981120 00722 NM 1998 11 20 SWAA982855 1 19981111 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 180 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND HORIZONTAL WEB CRACKED AT LIGHTENING HOLE AT BS 180, LBL 27, WL 207. REMOVED AND REP LACED HORIZONTAL WEB PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000723 19981120 00723 NM 1998 11 20 SWAA982856 1 19981111 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 887-907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE HAS CORRODED FASTENER HOLES FROM BS 887 TO 907. REMOVED AND REPL ACED TRANS ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000724 19981120 00724 NM 1998 11 20 SWAA982857 1 19981111 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 907-927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE HAS CORRODED FASTENER HOLES FROM BS 907 TO 927. REMOVED AND REPL ACED TRANS ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000725 19981120 00725 NM 1998 11 20 SWAA982858 1 19981111 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 927-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND RT TRANSITION ANGLE HAS CORRODED FASTENER HOLES FROM BS 927 TO 947. REMOVED AND REPL ACED TRANS ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000726 19981120 00726 NM 1998 11 20 SWAA982859 1 19981111 A 5320 INTERCOSTAL BOEING 737 7373A4 1384585 NM BS 305 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 305, STR 4L. REMOVED AND REPLACED INTERCOSTAL PER BOEING S RM. 2 L 7 2 4F RT A16WE 1998112000727 19981120 00727 NM 1998 11 20 SWAA982860 1 19981111 A 5320 BRACKET BOEING 737 7373A4 1384585 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO BIN, FWD BULKHEAD, WALL PANEL SUPPORT BRACKET CRACKED BS 727 CENTER LINE. 2 L 7 2 4F RT A16WE 1998112000728 19981120 00728 NM 1998 11 20 SWAA982861 1 19981111 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 787-847 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND LIGHT CORROSION AROUND FASTENER HOLES ON FLOORBEAM SUPPORT FROM BS 787 TO 847 ABOVE S TR 26R. REMOVED AND REPLACED FLOORBEAM PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000729 19981120 00729 NM 1998 11 20 SWAA982862 1 19981112 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 43. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000730 19981120 00730 NM 1998 11 20 SWAA982863 1 19981112 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 40. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000731 19981120 00731 NM 1998 11 20 SWAA982864 1 19981112 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 36. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000732 19981120 00732 NM 1998 11 20 SWAA982865 1 19981112 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 986.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORRODED FLOORBEAM UPPER FLANGE AT BS 986.5, RBL 32. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000733 19981120 00733 NM 1998 11 20 SWAA982866 1 19981112 A 5313 STRINGER BOEING 737 7373A4 1384585 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 16R TIE CLIP CRACKED AT BS 520. REMOVED AND REPLACED STRINGER PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998112000734 19981120 00734 NM 1998 11 20 SWAA982867 1 19981112 A 5313 STRINGER BOEING 737 7373A4 1384585 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 16L TIE CLIP CRACKED AT BS 520. REMOVED AND REPLACED STRINGER PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998112000735 19981120 00735 NM 1998 11 20 SWAA982868 1 19981112 A 5313 STRINGER BOEING 737 7373A4 1384585 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND STRINGER 10L TIE CLIP CRACKED AT BS 663. REMOVED AND REPLACED STRINGER PER BOEING SR M. 2 L 7 2 4F RT A16WE 1998112000736 19981120 00736 NM 1998 11 20 SWAA982869 1 19981112 A 5320 INTERCOSTAL BOEING 737 7373A4 1384585 NM BS 305 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL CRACKED AT BS 305, STR 54L. REMOVED AND REPLACED INTERCOSTAL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000737 19981120 00737 NM 1998 11 20 SWAA982870 1 19981112 A 5320 STRAP BOEING 737 7373A4 1384585 NM BS 305 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND STRAP CRACKED AT BS 305, STR 54L. REMOVED AND REPLACED STRAP PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000738 19981120 00738 NM 1998 11 20 SWAA982871 1 19981112 A 5320 ANGLE BOEING 737 7373A4 1384585 NM E & E COMP GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND LT UPPER ANGLE OVER E1-1 BENT AND GOUGED. REMOVED AND REPLACED ANGLE PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000739 19981120 00739 NM 1998 11 20 SWAA982872 1 19981112 A 5320 INTERCOSTAL BOEING 737 7373A4 1384585 NM BS 807-827 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND INTERCOSTAL ABOVE REAR BAGGAGE BIN DOOR CRACKED BETWEEN BS 807 TO 827. REMOVED AND R EPLACED INTERCOSTAL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000740 19981120 00740 NM 1998 11 20 SWAA982873 1 19981112 A 5330 SKIN BOEING 737 7372H4 138448C NM GALLEY DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND FWD GALLEY DOOR HINGE CUTOUT CRACKED ON THE FWD LWR CORNER. REPAIRED CUTOUT PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000741 19981120 00741 NM 1998 11 20 SWAA982874 1 19981111 A 5270 TARGET BOEING 737 7373H4 1384600 NM CARGO DOOR OUT OF ADJUST A SWAA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SW 07 339SW 24090 TAKEOFF ABORTED AT 75KTS INDICATED. TAKEOFF ABORTED DUE TO AFT CARGO LIGHT ILLUMINATED. OPC INDICATES 10.9 MILLION FT LBS/24 MINUTE BRAKE COOLING. ADJUSTED AFT CARGO DOOR TARGET AND OPS CKD OK PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000742 19981120 00742 NM 1998 11 20 SWAA982875 1 19981112 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED FLOOR SUPPORT LBL 12, WL 208, BS 294. REMOVED AND REPLACED FLOOR SUPPORT PER B OEING SRM. 2 L 7 2 4F A16WE 1998112000743 19981120 00743 NM 1998 11 20 SWAA982876 1 19981112 A 5320 INTERCOSTAL BOEING 737 7372H4 138448C NM BS 767-787 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND INTERCOSTAL AT BS 767 TO 787 CRACKED, RT STRINGER 25, WL 149. REMOVED AND REPLACED INTE RCOSTAL PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000744 19981120 00744 NM 1998 11 20 SWAA982877 1 19981112 A 5730 SKIN BOEING 737 7372H4 138448C NM RT WING CHAFED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND LEADING EDGE SKIN ABOVE NR 2 ENGINE PYLON IS CHAFED. REMOVED AND REPLACED SKIN PER BOEI NG SRM. 2 L 7 2 4F A16WE 1998112000745 19981120 00745 NM 1998 11 20 SWAA982878 1 19981112 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 489.5-499.5 MISREPAIRED A SWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND BLIND FASTENER IN SKIN REPAIR AT BS 489.5 TO BS 499.5, STR 7R. REMOVED EXISTING BLIND F ASTENER AND REPAIR CUT OUT DAMAGE PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000746 19981120 00746 NM 1998 11 20 SWAA982879 1 19981112 A 5320 DOUBLER BOEING 737 7372H4 138448C NM BS 332.1 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME DOUBLER AT BS 332.1, RBL 63, WL 216. REMOVED AND REPLACED FRAME DOUBLER P ER BOEING SRM. 2 L 7 2 4F A16WE 1998112000747 19981120 00747 NM 1998 11 20 SWAA982880 1 19981112 A 3350 LIGHT BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 399WN 27693 DURING WALKAROUND CHECK, FOUND FLOOR EMERGENCY TRACK LIGHTING IS COMING UP. REWIRED EMERGENCY TRACK LIGHTS PER BOEING M M. 2 L 7 2 4F RT A16WE 1998112000748 19981120 00748 NM 1998 11 20 SWAA982881 1 19981112 A 7722 WL202EED4 EGT IND BOEING 737 7373H4 1384600 NM NR 1 ENGINE INOPERATIVE A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 647SW 27717 EN ROUTE, AIRCRAFT DIVERT TO MDW DUE TO NR 1 EGT INOPERATIVE. AIRCRAFT MADE AN UNEVENFUL LANDING. REMOVED AND REPLACED NR 1 EGT INDICATOR PER BOEING MM. 2 L 7 2 4F RT A16WE 1998112000749 19981120 00749 NM 1998 11 20 SWAA982882 1 19981112 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 057SW 21722 DURING SERVICE CHECK, FOUND 4 INCH CRACKED FUSELAGE SKIN ON RT SIDE OF FUSELAGE (MARKED) 8 WINDOW BEHIND EMERGENCY EXIT. REPAIRED FUSELAGE SKIN PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000750 19981120 00750 NM 1998 11 20 SWAA982883 1 19981113 A 5320 ANGLE BOEING 737 7373A4 1384585 NM BS 636 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CRACKED FLOORBEAM ATTACH ANGLE AT BS 636, RBL 60. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000751 19981120 00751 NM 1998 11 20 SWAA982884 1 19981113 A 5320 INTERCOSTAL BOEING 737 7373A4 1384585 NM BS 294.5 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND CORROSION AROUND CLIP NUT HOLE ON INTERCOSTAL AT BS 294.5, LBL 11. INSTALLED NEW INT ERCOSTAL PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000752 19981120 00752 NM 1998 11 20 SWAA982885 1 19981113 A 5320 ANGLE BOEING 737 7373Q8 1384670 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND SUPPORT ANGLE CRACKED AT BS 540, STR 21. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000753 19981120 00753 NM 1998 11 20 SWAA982886 1 19981113 A 5320 FASTENER BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND HFEC CRACKED INDICATIONS COMING FROM HI-LOK AT WL 234, RBL 9 (FWD SIDE). REPAIRED PE R BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000754 19981120 00754 NM 1998 11 20 SWAA982887 1 19981113 A 5320 FASTENER BOEING 737 7373Q8 1384670 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND 2 HFEC CRACKED INDICATIONS COMING FROM HI-LOK AT WL 234, LBL 11 (FWD SIDE). REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000755 19981120 00755 NM 1998 11 20 SWAA982888 1 19981113 A 5320 STRAP BOEING 737 7373Q8 1384670 NM BS 860 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND CORROSION AROUND SCREW HOLES OF STRAP AT BS 860. REMOVED AND REPLACED STRAP PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998112000756 19981120 00756 NM 1998 11 20 SWAA982889 1 19981113 A 5320 STRAP BOEING 737 7373Q8 1384670 NM BS 770 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND CORRODED FLOORBEAM STRAP AT BS 770. REMOVED AND REPLACED STRAP PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112000757 19981120 00757 NM 1998 11 20 SWAA982890 1 19981113 A 5312 BULKHEAD ANGLE BOEING 737 7372H4 138448C NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED ON RT BULKHEAD SUPPORT ANGLE AT BS 520, RBL 26, WL 157. REPAIRED PER BOEING SR M. 2 L 7 2 4F A16WE 1998112000758 19981120 00758 NM 1998 11 20 SWAA982891 1 19981113 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 188 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 188, STR 14L. REMOVED AND REPLACED SKIN PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000759 19981120 00759 NM 1998 11 20 SWAA982892 1 19981113 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 341 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND GOUGES AND DRILL START ON STRINGER AT BS 341, 8R. REMOVED AND REPLACED STRINGER AND SPL ICE PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000760 19981120 00760 NM 1998 11 20 SWAA982893 1 19981113 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1051 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND DENTED SKIN AT BS 1051 BETWEEN STR 27R AND 37L. REPAIRED DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000761 19981120 00761 NM 1998 11 20 SWAA982894 1 19981113 A 5312 BULKHEAD ANGLE BOEING 737 7372H4 138448C NM BS 520 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CORRODED LT BULKHEAD SUPPORT ANGLE AT BS 520, LBL 26, WL 157. REMOVED AND REPLACED BULK HEAD SUPPORT ANGLE PER BOEING SRM. 2 L 7 2 4F A16WE 1998112000762 19981120 00762 NM 1998 11 20 SWAA982895 1 19981115 A 2910 BACH8B04NN0214T LINE BOEING 737 7372H4 138448C NM NLG UPLOCK ACT FAILED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 07 061SW 21970 AIR TURNBACK DUE TO NOSE GEAR SHOWED UNSAFE INDICATION AFTER TAKEOFF. ALL DOWN AND LOCKED INDICATIONS WERE NORMAL FOR L ANDING. NOSE GEAR WAS VISUALLY CONFIRMED NOT FULLY RETRACTED AFTER TAKEOFF. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSP ECTED, FOUND BROKEN HYD LINE TO NLG UPLOCK ACTUATOR. REPLACED 2 UPLOCK ACTUATOR FLEXIBLE HYD LINE PER BOEING MM. PERFO RMED FULL PRESSURE GEAR HANDLE UP LEAK AND OPS CHECK PER BOEING MM. LEAK CHECK GOOD. 2 L 7 2 4F A16WE 1998112000763 19981120 00763 WP 1998 11 20 RU3A98003 2 19980515 A 7530 BLEED VALVE BRAERO DH125 BAE125800A 1500285 EU GARRTT TFE731 TFE7315R 01518 WP LT ENGINE SATURATED A RU3A A UNSCHED LANDING B W SMOKE/FUMES/ODORS/SPARKS INADEQUATE Q C CL CLIMB 1 SW 21 95 258131 SMOKE AND STRONG FUMES IN CABIN AFTER TAKEOFF. RESIDUAL B/B GAS PATH CLEANER IN BLLED AIR SYSTEM. INVESTIGATION REVEAL ED THE LEFT ENGINE WAS WASHED ON 5/7-98. FOLLOW MM PROCEDURES FOR COMPRESSOR WASH. (M) 2 L 7 2 4F 4 F RT A3EU E6WE 1998112000764 19981120 00764 EU 1998 11 20 AALA981727 1 19980926 A 2150 22151621 DUCT FOKKER F28 F28MK0100 4990807 EU ACM BAY CRACKED A AALA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SW 07 1442E 11437 ORD - FLT 1361 - EN ROUTE EWR-ORD - WHILE NR 1 PACK WAS OFF, HAD PACK NR 2 FAULT. CREW REPORTED LOSS OF BOTH AIR CONDIT IONING PACKS. CAPTAIN DECLARED AN EMERGENCY AND AN EMERGENCY DESCENT WAS INITIATED TO 10,000. PACK 2 WAS PUT ON LINE A GAIN AT 10,000. WE CLIMB UP TO 20,000 FT TO FINISH THE FLIGHT AND THE NR 2 PACK WORKED FOR THE REMAINDER OF THE FLIGHT. LANDED ORD WITHOUT INCIDENT. REPLACED DUCT ASSEMBLY OPERATIONS AND LEAK CHECK OK. SYSTEM GROUND CHECKED NORMAL OPERA TION. (M) 2 L 7 2 4F RT 1998112000765 19981120 00765 EU 1998 11 20 AALA981820 1 19980924 A 5280 D11320426 DOOR FOKKER F28 F28MK0100 4990807 EU RT MLG CRACKED A AALA K NONE J WARNING INDICATION TO TAKEOFF 1 SW 07 1431B 11416 AUS - FLT 2549 - AFTER TAKEOFF RECEIVED CONSTANT MFDU ALERT SHOWING RIGHT MAIN LANDING GEAR DOOR WAS UNLATCHED. LANDING AUS WITHOUT INCIDENT. INSPECTED AND AUTHORIZED AIRCRAFT TO FERRY FROM AUS TO TUL FOR REPAIR TO RIGHT MAIN GEAR DOOR. R EPLACED RIGHT MLG DOOR PER MM. OPERATIONS CHECKED GOOD ON GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998112000766 19981120 00766 NM 1998 11 20 AALA981827 1 19980928 A 3260 106122629 SENSOR BOEING 727 727223 1384074 NM RT MLG MALFUNCTIONED A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 843AA 20984 ORD - FLT 1798 - EN ROUTE IAH-ORD, RIGHT MAIN GEAR RED LIGHT ILLUMINATED TWICE INTERMITTENTLY ON TAKEOFF ROLL. LANDED O RD WITHOUT INCIDENT. REPLACED DOWNLOCK SENSOR AT RIGHT POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112000767 19981120 00767 NM 1998 11 20 AALA981842 1 19981001 A 5510 CASTING BOEING 727 727223 1384074 NM HORIZ STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - HINGE MOUNT CASTING CRACKED AT LOWER REAR CHORD ATTACHMENT STATION 99.79 LEFT HORIZONTAL STAB. INSTALLED TRAILING EDGE RIB REPAIR PER SRM 55-10-4 PAGE 10. (M) 2 L 7 3 4F A3WE 1998112000768 19981120 00768 NM 1998 11 20 AALA981841 1 19981002 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 844AA 20985 TUL - DENT IN STATION 1050 BELTFRAME AT STRINGER 25L WITH .250 CRACK RUNNING PERPENDICULAR IN BOTTOM OF DENT, DENT LENGT H .75, WIDTH .50, DEPTH .040. CUTOUT 1 INCH BY 1 INCH OF UPPER FLANGE. INSTALLED DOUBLER PER 51-40-3 FIG 1. MATERIAL USED .0637075T6 FASTENERS USED .1875 AND .25 INCH HI-LOCKS, TWO ROWS FASTENERS ON VERTICAL, ONE ROW FASTENERS ON UPPER F LANGE, THREE FASTENERS PAST DAMAGE. (M) 2 L 7 3 4F A3WE 1998112000769 19981120 00769 NM 1998 11 20 AALA981889 1 19980916 A 5311 FRAME BOEING 727 727223 1384074 NM BS 970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION AT LOWER ANGLE OF STATION 970 BELT FRAME OUTBOARD OF STRINGER 29R (FWD SIDE). CUT OUT BAD SECTION OF BELTFRAME AND INSTALLED NEW SECTION OF FRAME AND REPAIRED WITH DOUBLER PER SRM 53-10-4 PAGE 4 FIG 1 SHEET 2. (M) 2 L 7 3 4F A3WE 1998112000770 19981120 00770 NM 1998 11 20 AALA981888 1 19981006 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - BELLFRAME HAS HOLE IN UPPER FLANGE. REMOVED DAMAGED MATERIAL AND FASTENER. DYE CHECKED FABRICATED AND DRILLED DO UBLER. ALODINED AND PRIMED AFFECTED AREA. INSTALLED DOUBLER PER SRM 53-10-4 FIG 1. (M) 2 L 7 3 4F A3WE 1998112000771 19981120 00771 NM 1998 11 20 AALA981887 1 19981006 A 5530 SUPPORT BOEING 727 727223 1384074 NM VERTICAL STAB CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - AFT CENTER TENSION TIE SUPPORT LUG ON TOP OF VERTICAL STABILIZER HAS WORN AREA OUTBOARD OF LEFT HOLE. REMOVED COR ROSION AND FLAP PEENED PER AARD 55-30-05-2 PAGE 1 AND 2 AND ESO 11697 DATED 8-28-98, TREATED AND PRIMED. (M) 2 L 7 3 4F A3WE 1998112000772 19981120 00772 NM 1998 11 20 AALA981886 1 19981006 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - BELL FRAME DENTED (ON TOP) STATION 500 BETWEEN STRINGER 23 RT AND 24 RT. CUT OUT DAMAGED AREA OF FRAME AND REPAIR ED PER SRM 51-40-3 IAW AARD 53-10-07-3. (M) 2 L 7 3 4F A3WE 1998112000773 19981120 00773 NM 1998 11 20 AALA981885 1 19981006 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - STUB FRAME CORRODED AT SKIN ATTACH ANGLE STATION 950E AND 6 FORWARD SIDE OUTBOARD OF STRINGER 29R. REMOVED AND RE PLACED STUB FRAME PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998112000774 19981120 00774 NM 1998 11 20 AALA981884 1 19981006 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - STATION 950F BELL FRAME DENT BETWEEN STRINGER 25 AND 26L. INSTALLED REPAIR PER SRM 51-40-3 FIG 1. 2 L 7 3 4F A3WE 1998112000775 19981120 00775 NM 1998 11 20 AALA981883 1 19981006 A 5320 SPLICE BOEING 727 727223 1384074 NM BS 1010 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - STRINGER 29R SPLICE RIGHT VERTICAL LEG CORRODED STATION 1010. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10- 3 FIG 1. (M) 2 L 7 3 4F A3WE 1998112000776 19981120 00776 NM 1998 11 20 AALA981882 1 19981006 A 5320 CLIP BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - STRINGER CLIP CORRODED OUTBOARD SIDE OF STRINGER 29R STATION 990 FORWARD SIDE. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1998112000777 19981120 00777 NM 1998 11 20 AALA981881 1 19981006 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1042-1047 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - BILGE SKIN CORRODED STATION 1042-1047 OUTBOARD SIDE OF STRINGER 29R. REPAIRED SKIN PER SRM 53-30-3. NO CUT OUT R EQUIRED PER SRM 53-30-03-3 AARD. (M) 2 L 7 3 4F A3WE 1998112000778 19981120 00778 NM 1998 11 20 AALA981880 1 19981006 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1040-1050 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - BILGE SKIN CORRODED STATION 1040-1050 OUTBOARD SIDE OF STRINGER 28R. REPAIRED SKIN PER SRM 53-30-3. NO CUT OUT R EQUIRED PER SRM 53-30-03-3 AARD. (M) 2 L 7 3 4F A3WE 1998112000779 19981120 00779 NM 1998 11 20 AALA981879 1 19981006 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND SKIN CORRODED BELOW BELTFRAME STATION 720C AND STRINGER 28L. INSTALLED DOUBLER TO REPAIR SKIN PER SRM 53-30 -3. CUT OUT CORRODED SKIN. (M) 2 L 7 3 4F A3WE 1998112000780 19981120 00780 NM 1998 11 20 AALA981878 1 19981006 A 5330 SKIN BOEING 727 727223 1384074 NM BS 950 CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - TWO HOLES WORN THROUGH FUSELAGE SKIN STATION 950B AND 14 INCH STRINGER 23L. REPAIRED PER SRM 53-30-3 FIG 3. INST ALLED DOUBLER. (M) 2 L 7 3 4F A3WE 1998112000781 19981120 00781 NM 1998 11 20 AALA981877 1 19980913 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORRODED SHEAR TIE FORWARD SIDE STATION 720C STRINGER 28-27 LT. REMOVED AND REPLACED WITH NEW SHEAR TIE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998112000782 19981120 00782 NM 1998 11 20 AALA981876 1 19981006 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - AFT FACE OF SHEAR TIE CORRODED STATION 1130 OUTBOARD OF STRINGER 29L. REMOVED AND REPLACED SHEAR TIE PER SRM 51-1 0-1. (M) 2 L 7 3 4F A3WE 1998112000783 19981120 00783 NM 1998 11 20 AALA981875 1 19981006 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND SHEAR TIE FORWARD FACE CORRODED STATION 1130 LEFT SIDE OF STRINGER 29L. REMOVED AND REPLACED SHEAR TIE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998112000784 19981120 00784 NM 1998 11 20 AALA981874 1 19980918 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION AT BELL FRAME SHEAR TIE STATION 1166 RIGHT OF STRINGER 30. INSTALLED SHEAR TIE. REPAIR PER SRM 5 3-10-4. (M) 2 L 7 3 4F A3WE 1998112000785 19981120 00785 NM 1998 11 20 AALA981873 1 19981006 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION ON SHEAR TIE STATION 1148 BETWEEN STRINGER 30 AND 29 RT. REMOVED AND REPLACED SHEAR TIE PER SRM 5 1-10-1. (M) 2 L 7 3 4F A3WE 1998112000786 19981120 00786 NM 1998 11 20 AALA981872 1 19981006 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION ON SHEAR TIE FORWARD 660 OUTBOARD STRINGER 27 RT. INSTALLED NEW SHEAR TIE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998112000787 19981120 00787 NM 1998 11 20 AALA981871 1 19981006 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION AFT SIDE BELTFRAME STATION 580 OUTBOARD STRINGER 27 LEFT, SHEAR TIE. INSTALLED NEW SHEAR TIE PER SRM 51-10-01. (M) 2 L 7 3 4F A3WE 1998112000788 19981120 00788 NM 1998 11 20 AALA981870 1 19980928 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - SHEAR TIE CORRODED ON AFT SIDE AT STATION 970 STRINGER 28-29R. REPLACED SHEAR TIE WITH NEW 51-10-1. (M) 2 L 7 3 4F A3WE 1998112000789 19981120 00789 NM 1998 11 20 AALA981869 1 19981006 A 5312 BULKHEAD BOEING 727 727223 1384074 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND 740 AFT BULKHEAD SKIN AND DOUBLER CORRODED. REMOVED CORROSION. REPLACED DOUBLER AND INSTALLED DOUBLER REPA IR PER SRM 51-40-2 PAGE 6B. (M) 2 L 7 3 4F A3WE 1998112000790 19981120 00790 NM 1998 11 20 AALA981868 1 19981006 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - BELL FRAME DENTED STATION 500 IN BETWEEN STRINGER 23 LEFT AND 22 LT. CUT OUT DAMAGED AREA AND INSTALLED .071 7075 -T6 DOUBLER IAW SRM 51-40-3 PER AARD 53-10-07-3. (M) 2 L 7 3 4F A3WE 1998112000791 19981120 00791 NM 1998 11 20 AALA981867 1 19981006 A 5311 FRAME BOEING 727 727223 1384074 NM BS 304 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FRAME CORRODED STATION 304 OUTBOARD OF RIGHT NOSE GEAR TRUNNION CASTING. REPLACED CORRODED FRAME PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998112000792 19981120 00792 NM 1998 11 20 AALA981866 1 19981006 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION OUTBOARD OF STRINGER 28 LEFT STATION 720F TO STATION 740. INSTALLED STRAP PER ESO 11697, DATED 9/ 2/98. (M) 2 L 7 3 4F A3WE 1998112000793 19981120 00793 NM 1998 11 20 AALA981865 1 19980803 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION IN STRINGER 27 RIGHT STATION 720F PLUS 5 INCHES. REMOVED CORROSION, INSTALLED REPAIR SPLICE PER S RM 53-10-3. (M) 2 L 7 3 4F A3WE 1998112000794 19981120 00794 NM 1998 11 20 AALA981864 1 19981006 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION OUTBOARD SIDE STRINGER 28 RT, STATION 720F. BLENDED CORRODED FROM AREA INSTALLED REPAIR STRAP PER ESO 11697 DATED 9-2-98. (M) 2 L 7 3 4F A3WE 1998112000795 19981120 00795 NM 1998 11 20 AALA9863 1 19981006 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND STRINGER 29R OUTBOARD LEG CORRODED STATION 950E TO 950E PLUS 5. REMOVED STRINGER 29R FROM STATION 950D PLUS 10 TO STATION 1005 AND INSTALLED NEW SECTION OF STRINGER AND REPAIR SPLICE PER AARD 53-10-03-1. (M) 2 L 7 3 4F A3WE 1998112000796 19981120 00796 NM 1998 11 20 AALA981862 1 19981006 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND STRINGER 15R CRACKED FORWARD OF ICE LIGHT STATION 720B PLUS 4. INSTALLED STRINGER REPAIR PER SRM 53-10-3. ( M) 2 L 7 3 4F A3WE 1998112000798 19981120 00798 NM 1998 11 20 AALA981860 1 19981006 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 344 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND STRINGER CRACKED AT BRACKET ATTACH HOLES STATION 344 STRINGER 5R. REPAIRED STRINGER 5 AT STATION 344 PER SR M 53-10-3 FIG 2, DETAIL 1. (M) 2 L 7 3 4F A3WE 1998112000799 19981120 00799 NM 1998 11 20 AALA981859 1 19981006 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FLOORBEAM TOP FLANGE CORRODED STATION 344, LBL 19. CUT OUT CORRODED AREA, INSTALLED DOUBLER AND FILLER AT STATION 344 FLOORBEAM LBL 19 PER SRM 53-10-8 PAGE 9C, 9D, AND 9E. (M) 2 L 7 3 4F A3WE 1998112000800 19981120 00800 NM 1998 11 20 AALA981858 1 19980910 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 312 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - TOP SURFACE OF FLOORBEAM CORRODED AT STATION 312 RBL 44 INCHES. CUT OUT CORROSION, TREATED AND PRIMED AREA. INST ALLED DOUBLER REPAIR PER SRM 53-10-8 PAGE 49-53. (M) 2 L 7 3 4F A3WE 1998112000801 19981120 00801 NM 1998 11 20 AALA981857 1 19981006 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND CORROSION ON UPPER FLOORBEAM FLANGE AT STATION 380 RBL 12 INCH OUTBOARD TO CREASE ANGLE. REPAIRED 380 FLOOR BEAM PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998112000802 19981120 00802 NM 1998 11 20 AALA981856 1 19981006 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND FLOORBEAM CORRODED STATION 380 RBL 48 - RBL 55. REPAIRED 380 FLOORBEAM PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998112000803 19981120 00803 NM 1998 11 20 AALA981919 1 19981014 A 5320 SUPPORT DOUG MD11 MD11 3023602 NM BS 1902 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - FOUND CORROSION ON GALLEY SUPPORT AND LUGS. REPLACED AFT GALLEY SUPPORT PER AARD 53-00-10 AND SRM 53-70-00. (M) 2 L 7 3 4F RT A22WE 1998112000804 19981120 00804 NM 1998 11 20 AALA981918 1 19981014 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1964 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - FOUND CORROSION ON SEAT TRACK NR 8 AT STATION 1964. CUT OUT CORRODED SECTION OF SEAT TRACK AND SPLICED IN NEW SEC TION IAW SRM 53-70-00-0. (M) 2 L 7 3 4F RT A22WE 1998112000805 19981120 00805 NM 1998 11 20 AALA981902 1 19981012 A 5713 STRINGER DOUG MD11 MD11 3023602 NM WS 737 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - RIGHT WING STRINGER NR 10 IS CRACKED AT THE OUTBOARD END. REMOVED CRACKED STRINGERS END AND SPLICED IN NEW SECTIO N PER SRM 57-20-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1998112000806 19981120 00806 NM 1998 11 20 AALA981901 1 19981011 A 5320 DOUG MD11 MD11 3023602 NM UNKNOWN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - FOUND CORROSION ON TOE OR 'T' ANGLE AROUND MOUNTING BOLT HOLES FOR LT AFT GALLEY SUPPORT. REMOVED AND REPLACED T- ANGLE PER 51-10-00-1 AARD. (M) 2 L 7 3 4F RT A22WE 1998112000807 19981120 00807 NM 1998 11 20 AALA981900 1 19981011 A 5320 ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - FOUND CORROSION ON FLOOR ANGLE INBOARD OF NR 6 SEAT TRACK. REMOVED AND REPLACED T-ANGLE PER AARD 51-10-00-1. (M) 2 L 7 3 4F RT A22WE 1998112000808 19981120 00808 NM 1998 11 20 AALA981899 1 19981013 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1964 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1758B 48527 TUL - FOUND CORROSION ON SEAT TRACK UNDER LAVATORY. REPLACED SECTION OF SEAT TRACK PER AARD 51-10-00-01 AND 53-70-00 OF THE SRM VOL 1. (M) 2 L 7 3 4F RT A22WE 1998112000809 19981120 00809 WP 1998 11 20 AALA981904 1 19981006 A 5320 STRAP DOUG DC9 DC982 3022082 WP BS 370-427 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 432AA 49350 TUL - FOUND FORWARD AND AFT CARGO DOOR CUTOUT STRUCTURE STRAPS GOUGED. REPLACED STRAPS IAW ESO 80559 10-6-98. (M) 2 L 7 2 4F A6WE 1998112000810 19981120 00810 WP 1998 11 20 AALA981905 1 19981005 A 5720 SLAT TRACK DOUG DC9 DC982 3022082 WP WS 136 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 423AA 49335 TUL - NR 4 SLAT TRACK CAN GOUGED FROM SLAT TRACK ON OUTBOARD SIDE. REPAIRED IAW AARD 57-20-00-6. (M) 2 L 7 2 4F A6WE 1998112000811 19981120 00811 WP 1998 11 20 AALA981907 1 19980929 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 674 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 432AA 49350 TUL - FOUND CORROSION ON DOOR BEAM LOWER FLANGE AT TAB FOR AFT DOOR STOP PAD. DOUBLER INSTALLED AS PER AARD 53-10-00-3 AREA PRIMED AND PAINTED PER SRM 51-10-03. (M) 2 L 7 2 4F A6WE 1998112000812 19981120 00812 WP 1998 11 20 AALA981908 1 19981002 A 5313 LONGERON DOUG DC9 DC982 3022082 WP BS 1418 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 432AA 49350 TUL - FOUND LONGERON R-2 CRACKED. REPAIRED IAW AARD 53-30-00-2. (M) 2 L 7 2 4F A6WE 1998112000813 19981120 00813 WP 1998 11 20 AALA981909 1 19980930 A 5347 TIEDOWN TRACK DOUG DC9 DC982 3022082 WP BS 427-465 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 432AA 49350 TUL - RIGHT TIE DOWN TRACK HAS CORROSION AROUND CENTER HOLE AND FLANGE HOLES. INSTALLED STRAP AT FS 446 PER AARD 53-20- 00-13 REV 8-21-98. BLENDED AND ALODINED PRIMED ALL WORKED AREAS. (M) 2 L 7 2 4F A6WE 1998112000814 19981120 00814 WP 1998 11 20 AALA981903 1 19981009 A 5347 TIEDOWN TRACK DOUG DC9 DC982 3022082 WP BS 1140-1193 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 510AM 49804 TUL - FOUND LEFT TIEDOWN TRACK PLATE EARS CORRODED OVER LINEAR DISTANCE OF 53 INCHES. SUBSEQUENT E58-4, 0104877 AND 010 4878 REQUIRED REMOVAL OF ENTIRE LEFT TIEDOWN TRACK IN AFT CARGO COMPT. REMOVED DAMAGED TIEDOWN AND REPLACED WITH NEW TR ACK. (M) 2 L 7 2 4F A6WE 1998112000815 19981120 00815 WP 1998 11 20 GTIA9800115 1 19981017 A 3350 BULB DOUG DC9 DC931 3022065 WP CABIN FAILED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 934ML 47526 EMERGENCY LIGHT SYSTEM IN VENTRAL STAIRWAY UPPER LEFT INOPERATIVE. REPLACED BULBS, STILL INOPERATIVE. REPLACED BULBS I AW DC-9 MM 33-50-1. CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1998112000816 19981120 00816 NM 1998 11 20 USAA980527 1 19981009 A 5330 SKIN BOEING 737 737301 1384611 NM BS 312 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 32573 23555 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK L-1 DOOR UPPER HINGE CUTOUT STATION 312 BETWEEN STRING ER 9L AND 10L EXTERIOR SKIN. INSTALLED DOUBLER PER EX 62655. (M) 2 L 7 2 4F RT A16WE 1998112000817 19981120 00817 NM 1998 11 20 USAA980528 1 19981009 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 352US 32573 23555 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK FS 380 BL 0 BETWEEN STRINGER 27L AND 27R EXTERIOR SKI N. INSTALLED DOUBLER PER EA 62680 AND SB 737-53-1117 REV 1. (M) 2 L 7 2 4F RT A16WE 1998112000818 19981120 00818 NM 1998 11 20 USAA980484 1 19981010 A 5330 SKIN BOEING 737 737301 1384611 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 586US 35892 23931 TPA - DURING CX-6 CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND A .125 INCH CRACK IN EXTERIOR SKIN STATION 380 BL 0. INSTALLED DOUBLER PER EA 62686 SB 737-53-1117 REV 2. (M) 2 L 7 2 4F RT A16WE 1998112000819 19981120 00819 NM 1998 11 20 USAA980481 1 19981013 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 508AU 36477 23383 TPA - DURING CX-5 CHECK VISUAL VERIFIED BY EDDY CURRENT, FOUND A 1.125 INCH CRACK IN EXTERIOR SKIN STATION 380 BL0 L .12 5 INCH . INSTALLED DOUBLER PER EA 62689, BOEING S/B 737-53-1117-1. (M) 2 L 7 2 4F RT A16WE 1998112000820 19981120 00820 NM 1998 11 20 USAASB98266 1 19981011 A 3241 CONTROL BOX BOEING 737 7373B7 1384580 NM MLG MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 375US 22954 MSY - FL 1106 - EN ROUTE FROM MSY TO LGA, THE ANTI-SKID LIGHT ILLUMINATED. WHEN DESCENDING INTO LGA, THE CREW RECYCLED THE GEAR TWICE TO SEE IF THE PROBLEM COULD BE RECTIFIED. THEY WERE UNSUCCESSFUL AND A DIVERSION WAS MADE TO PHL. FLIGH T LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFORMED ADJUSTMENT/TEST OF THE ANTI-SKID SYSTEM. C HECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 1998112000821 19981120 00821 NM 1998 11 20 USAA980497 1 19981015 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 951 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 524AU 35957 23859 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 951 WL 251.77 UPPER HINGE ARM CENTERLINE EXTER IOR SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-60-01 FIG 205. (M) 2 L 7 2 4F RT A16WE 1998112000822 19981120 00822 NM 1998 11 20 USAA980542 1 19981026 A 5313 STRINGER BOEING 737 7373B7 1384580 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STATION 616 STRINGER 3R STRINGER SHEAR TIE. REMOVED AND REPLACED STRINGER SHEAR TIE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998112000823 19981120 00823 NM 1998 11 20 USAA980541 1 19981026 A 5313 STRINGER BOEING 737 7373B7 1384580 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 3R STRINGER SHEAR TIE. REMOVED AN D REPLACED STRINGER SHEAR TIE PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998112000824 19981120 00824 NM 1998 11 20 USAA980533 1 19981026 A 5311 65544032 FRAME BOEING 737 7373B7 1384580 NM BS 1064 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37155 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A HOLE AT APU BLEED AIR DUCT CHAFFING FRAME FROM LIGHTENING BS 1064. IN STALLED FRAME REPAIR PER EA 62609B. (M) 2 L 7 2 4F RT A16WE 1998112000825 19981120 00825 NM 1998 11 20 USAA980532 1 19981026 A 5311 65C229101 FRAME BOEING 737 7373B7 1384580 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37155 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH CORROSION AREA STATION 500D BETWEEN STRINGER 26L AND STRINGER 27L ON FRAME, CORROSION TASK NR C53-208-01. INSTALLED SHEAR TIE DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1998112000826 19981120 00826 NM 1998 11 20 USAA980501 1 19981026 A 5347 SEAT TRACK BOEING 737 7373B7 1384580 NM BS 646 GOUGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH GOUGE STATION 646 LBL 25 ON SEAT TRACK. SPLICED IN NEW SEAT TRACK SECTION PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 1998112000827 19981120 00827 NM 1998 11 20 USAA980500 1 19981026 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 727 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AT STATION 727 PLUS 12 LBL 6.5 ON SKIN. CORR OSION TASK NR C53-208-01. INSTALLED DOUBLER AND TRIPLER PER EA 62603. (M) 2 L 7 2 4F RT A16WE 1998112000828 19981120 00828 NM 1998 11 20 USAA980499 1 19981026 A 5320 693535216 CLIP BOEING 737 7373B7 1384580 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .375 INCH CRACK STATION 616 STRINGER 8 L TIE CLIP. INSTALLED NEW TIE CL IP PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998112000829 19981120 00829 NM 1998 11 20 USAA980471 1 19981026 A 5311 6545808582 FRAME BOEING 737 7373B7 1384580 NM BS 300 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK AT LWR TERMINUS OF DOOR SURROUND FRAME BS 300 STRINGER 17R WL 209. INSTALLED FRAME REQUIRE PER SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F RT A16WE 1998112000830 19981120 00830 NM 1998 11 20 USAA980472 1 19981026 A 5311 6546547251 FRAME BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK OUTER CHORD STATION 727 STRINGER 14L. INSTALLED REPAI R FILLER, DOUBLER AND STRINGER CLIP PER EA 62614. (M) 2 L 7 2 4F RT A16WE 1998112000831 19981120 00831 NM 1998 11 20 USAA980498 1 19981026 A 5330 6545871523 SKIN BOEING 737 7373B7 1384580 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK FORWARD GALLEY DOOR UPPER HINGE AREA. INSTALLED DOUBLER PER EA 38966A SB 737-52-1096 REV 1. (M) 2 L 7 2 4F RT A16WE 1998112000832 19981120 00832 NE 1998 11 20 USAAD98187 2 19981018 A 7200 ENGINE DOUG DC9 DC981 3022081 WP PWA JT8 JT8D217 52053 NE RT NACELLE FAILED A USAA O OTHER X E J ENGINE FLAMEOUT VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 EA 19 803US 48035 BUF-PHL - FLT 1045 - UPON DESCENDING FROM CRUISE THE THROTTLES WERE RETARDED AND A SEVERE VIBRATION WAS FELT. THE RIGHT ENGINE VIBRATION METER WAS AT FULL SCALE. THE THROTTLES WERE MOVED TO IDLE AND THE VIBRATION SUBSIDED. REAPPLICATION OF POWER BROUGHT BACK THE VIBRATION. THE RIGHT THROTTLE WAS RETURNED TO IDLE AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. (M) 2 L 7 2 4F 4 F A6WE E9NE 1998112000833 19981120 00833 NE 1998 11 20 USAASB98274 2 19981018 A 7200 ENGINE BOEING 737 7373B7 1384580 NM PWA JT8 JT8D217 52053 NE NR 2 NACELLE FOD A USAA A UNSCHED LANDING C R B F.O.D. PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 397US 23319 CHS - FLT 175 - AFTER T/O AT APPROX 500 FT, CREW HEARD A LOUD NOISE AS IF A COMPRESSOR STALL OCCURRED ON THE NR 2 ENG. T HE NR 2 ENG INSTRUMENTS DROPPED OFF TO NEAR IDLE THEN GRADUALLY RECOVERED TO NORMAL. SMOKE WAS REPORTED IN THE CABIN, W HILE ONE PAX REPORTED A HYD SMELL AND ANOTHER BURNED TIRES. FLT RETURNED TO FIELD AT CHS AND LANDED W/O INCIDENT. ODOR IN CABIN DISSIPATED PRIOR TO TOUCHDOWN. NO EMERGENCY WAS DECLARED AND THE ENG WAS NOT SHUT DOWN IN FLT. UPON ARRIVAL AT THE GATE, MX DISCOVERED SIGNS OF A BIRD STRIKE. MX CLEANED BIRD REMAINS FROM THE NR 2 ENG AND THE RT WING LEADING ED GE, INBD OF ENG. NO DAMAGE NOTED TO WING LEADING EDGE. PROGRAMMED FOR NR 18 AND 19, FIRST STAGE FAN BLADE REPLACEMENT 2 L 7 2 4F 4 F RT A16WE E9NE 1998112000834 19981120 00834 NE 1998 11 20 TAOA109805 2 19981018 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D7B 52053 NE NR 1 NACELLE FAILED A TAOA C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 EA 15 923TS 20441 655383 ABORTED TAKEOFF ROLL AT APPROX 30 KNOTS DUE TO NR 1 ENGINE LOSS OF POWER. NR 1 ENGINE TURBINE FAILED WITH METAL IN THE TAIL PIPE. NR 1 ENGINE REPLACED. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998112000835 19981120 00835 NM 1998 11 20 TAOA109806 1 19981017 A 2751 18129932 INDICATOR BENDIX BOEING 727 727254 138408L NM COCKPIT MALFUNCTIONED A TAOA L ABORTED APPROACH F FLT CONT AFFECTED AP APPROACH 1 EA 15 912TS 0026AV 20438 FLT 6500 - DCA-LGA - ON APPROACH, UPON FLAP EXTENSION, INBOARD FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES. REPLACED INBOA RD FLAP POSITION INDICATOR. (M) 2 L 7 3 4F A3WE 1998112000836 19981120 00836 NM 1998 11 20 SABA980053 1 19981009 A 5280 BEARING DHAV DHC8 DHC8102 2809003 NM LT MLG DOOR LOOSE A SABA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 33 882CC 168 CLT-CVG - FLT 5085 - AFTER TAKEOFF FROM CLT, THE LEFT MAIN GEAR LIGHT ILLUMINATED. PILOT RETURNED TO CLT. NO INFLIGHT EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND A LOOSE BEARING IN THE LEFT FORWARD LANDING GEAR DOOR HINGE. REMOVED AND REPLACED THE BEARING. SYSTEM OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998112000837 19981120 00837 NE 1998 11 20 SABA980058 2 19981023 A 7200 310450001 ENGINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT NACELLE FAILED A SABA E ENGINE SHUTDOWN P NO WARNING INDICATION DE DESCENT 1 SO 33 817PH 120204 56 CLT-CVG - FLT 5033 - THE LEFT ENGINE HAD A UNCOMMANDED SHUT DOWN AT 9000 FT AND ON APPROACH TO CINCINNATI. THERE WAS NO UNUSUAL TEMPS OR PRESSURE READINGS PRIOR TO FAILURE. LEF TPROP DID NOT FEATHER. ALTERNATE FEATHER WAS USED. INFLIGHT EMERGENCY WAS DECLARED. EMERGENCY PROCEDURES WERE USED. FIRE AND SECURITY WERE CALLED OUT. AIRCRAFT LANDED AT CVG WI TH NO OTHER PROBLEMS. MAINTENANCE FROM CHARLOTTE FOUND METAL IN THE LEFT ENGINE OIL FILTER AND SYSTEM. ENGINE IS NOW B EING REMOVED AND REPLACED. AIRCRAFT NOT IN SERVICE AT THIS TIME. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1998112000838 19981120 00838 WP 1998 11 20 SABA980057 2 19981017 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT NACELLE MALFUNCTIONED A SABA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 33 962AE 962 CLT-LYH - FLT 5205 - DURING CLIMB-OUT, THE AIRCREW REPORTED THAT THE LEFT ENGINE WAS MAKING 97 PERCENT RPM AND 88 PERCEN T TORQUE. AIRCRAFT RETURNED TO CLT WITH NO OTHER PROBLEMS. NO INFLIGHT EMERGENCY WAS DECLARED. MAINTENANCE GROUND RUN THE AIRCRAFT WITH NO DEFECTS NOTED. BOTH ENGINES PRODUCED 100 PERCENT TORQUE. LEFT ENGINE RPM 100.5 PERCENT, RIGHT EN GINE 101 PERCENT RPM. LEFT ENGINE TEMP 630 DEGREES CELSIUS AND RIGHT ENGINE WAS 620 DEGREES CELSIUS, OAT WAS 25 DEGREES CELSIUS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998112000839 19981120 00839 NE 1998 11 20 SIMA983031 2 19981030 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT NACELLE FAILED A SIMA E ENGINE SHUTDOWN R B J PARTIAL RPM/PWR LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION DE DESCENT 1 SW 21 320AE 340B320 785212 SHV - FLT 5093 - ON DESCENT, THE RIGHT ENGINE CHIP LIGHT ILLUMINATED FOLLOWED BY SLIGHT SMOKE ODOR IN THE COCKPIT AND LO SS OF TORQUE. CREW SHUT DOWN THE ENGINE, DECLARED AN EMERGENCY AND LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE AS SEMBLY. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998112000840 19981120 00840 EU 1998 11 20 SIMA983006 1 19981027 A 2611 CONNECTOR SAAB SF340 340B 7860101 EU CARGO BAY LOOSE A SIMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 338SB 340B338 AEX - FLT 5092 - CARGO SMOKE WARNING LIGHT ILLUMINATED AND EXTINGUISHED. DISCHARGED ONE FIRE EXTINGUISHER AND DIVERTED INTO AEX. TIGHTENED LOOSE CANNON PLUG AT THE AFT/UPPER SMOKE DETECTOR AND DEFERRED THE FIRE EXTINGUISHER UNTIL AIRCRAFT RETURNED TO DALLAS. AT THAT TIME, THE SMOKE DETECTORS WERE CLEANED, THE FIRE EXTINGUISHER WAS REPLACED, THE MEL WAS CL EARED. THE SYSTEM WAS OPERATIONALLY CHECKED WITH NO FURTHER DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112000841 19981120 00841 EU 1998 11 20 SIMA983005 1 19981027 A 6120 78249052 PCU SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN R F PARTIAL RPM/PWR LOSS FLT CONT AFFECTED CL CLIMB 1 SW 21 256AE 910776 340B256 DFW - FLT 3793 - AFTER TAKEOFF, AT 7500 FEET AGL AND PROPS SET TO 1270 RPM, THE RIGHT ENGINE PROP RPM AND TORQUE STARTED TO FLUCTUATE. THE AIRCRAFT STARTED TO YAW AND THE PROP WOULD NOT RESPOND TO CONDITION LEVER MOVEMENT. THE ENGINE WAS SHUTDOWN. THE MAX PROP RPM OBSERVED WAS 1440. REMOVED AND REPLACED THE RIGHT PROPELLER CONTROL UNIT. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112000842 19981120 00842 EU 1998 11 20 SIMA983002 1 19981027 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 596-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 180AE 340B180 ABI - FOUND SEAT TRACK AT BL 0, 18.3L, AND 18.3R AT FS 596-686 CORRODED. CUT OUT 90 INCHES OF TRACK FOR 18.3R, FABRICAT ED AND INSTALLED AND EXTRUSION. REMOVED AND REPLACED SEAT TRACKS AT BL 0 AND BL 18.3L. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 1998112000843 19981120 00843 EU 1998 11 20 98ZZZM833 1 19981027 A 5347 7253720209 SEAT TRACK SAAB SF340 340B 7860101 EU BS 596-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 180AE 340B180 ABI - FOUND SEAT TRACK AT BL 0, 18.3L, AND 18.3R AT FS 596-686 CORRODED. CUT OUT 90 INCHES OF TRACK FOR 18.3R, FABRICAT ED AND INSTALLED AND EXTRUSION. REMOVED AND REPLACED SEAT TRACKS AT BL 0 AND BL 18.3L. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 1998112000844 19981120 00844 EU 1998 11 20 98ZZZM834 1 19981027 A 5320 46500043 EXTRUSION SAAB SF340 340B 7860101 EU BS 596-686 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 180AE 340B180 ABI - FOUND SEAT TRACK AT BL 0, 18.3L, AND 18.3R AT FS 596-686 CORRODED. CUT OUT 90 INCHES OF TRACK FOR 18.3R, FABRICAT ED AND INSTALLED AND EXTRUSION. REMOVED AND REPLACED SEAT TRACKS AT BL 0 AND BL 18.3L. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 1998112000845 19981120 00845 EU 1998 11 20 SIMA982991 1 19981026 A 3350 6013211 BATTERY PACK SAAB SF340 340B 7860101 EU ROW 6/7 DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 198AE 17476 340B198 MIA - FLT 5751 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROWS 6 AND 7 BC DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998112000846 19981120 00846 EU 1998 11 20 SIMA982963 1 19981023 A 3350 74331 BULB SAAB SF340 340B 7860101 EU SEAT 14A FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 231LN 340B231 DFW - FLT 5070 - EMERGENCY LIGHT ABOVE SEAT 14A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 1998112000847 19981120 00847 EU 1998 11 20 SIMA982962 1 19981023 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU LAVATORY MALFUNCTIONED A SIMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 21 306AE A3040 340B306 VCV - FLT 3242 - LAV SMOKE LIGHT ILLUMINATED. VERIFIED EVENT AS FALSE WARNING. REMOVED AND REPLACED SMOKE DETECTOR. O PERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998112000848 19981120 00848 EU 1998 11 20 SIMA982961 1 19981023 A 6120 78249055 PCU SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 392AE 960122 340B392 MAF - FLT 3814 - DURING AUTOCOARSEN CHECK, THE RIGHT PROPELLER FEATHERED UNCOMMANDED. UNABLE TO UNFEATHER. REMOVED AND REPLACED THE RIGHT PCU. LEAK AND OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4T RT A52EU 1998112000849 19981120 00849 GL 1998 11 20 SIMA982931 2 19981020 A 7200 ENGINE EMB 145 EMB145LR SO ALLSN AE300 AE3007A GL NR 2 NACELLE FAILED A SIMA O OTHER X ENGINE FLAMEOUT AP APPROACH 1 SW 21 603AE 145055 CAE311005 ORD - FLT 4318 - NR 2 ENGINE FLAMED OUT DUE TO LOW N1. RESTARTED ENGINE SUCCESSFULLY. REMOVED AND REPLACED NR 2 ENGINE . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 F RT T00011AT TE6CH 1998112000850 19981120 00850 EU 1998 11 20 RAIA981019 1 19981028 A 5347 S536780001000 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU COCKPIT CORROSION A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 STL - DURING MAINTENANCE, FOUND CORROSION AT LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. MAINTENANCE REPLACED SEAT TRA CK IAW ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 1998112000851 19981120 00851 NE 1998 11 20 RAIA981016 2 19981026 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT NACELLE FAILED A RAIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CE 03 570HK 7511 41089 75081 FLT 7660 - JFK - LEFT ENGINE TORQUE AND FUEL FLOW INDICATION ERRATIC. MAINTENANCE REPLACED LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1998112000852 19981120 00852 EU 1998 11 20 RAIA981015 1 19981024 A 3230 LINE BAG JETSTM JETSTM3201 1500217 EU MLG FAILED A RAIA B EMER. DESCENT K FLUID LOSS DE DESCENT 1 CE 03 341TE 950 FLT 7496 - STL - LANDING GEAR WILL NOT COME DOWN, HAND PUMPED GEAR DOWN OK. MAINTENANCE REPLACED BROKEN HYD LINE PER MM 29-10-00 PERFORMED SP-21. (M) 2 L 7 2 4T RT A56EU 1998112000853 19981120 00853 EU 1998 11 20 RAIA981020 1 19981028 A 3320 8ES00558800 POWER UNIT AEROSP ATR42 ATR42300 8680920 EU SEAT 4D FAILED A RAIA A UNSCHED LANDING A FLAME/FIRE CL CLIMB 1 CE 03 426TE 228 FLT 7129 - PIA - READING LIGHT POWER UNIT ASSY CAUGHT FIRE AT SEAT 4D. MAINTENANCE REPLACED READING LIGHT PANEL ASSY. ( M) 2 H 7 2 4T RT A53EU 1998112000854 19981120 00854 EU 1998 11 20 RAIA981027 1 19981028 A 5313 NTA44668 STRINGER AEROSP ATR42 ATR42300 8680920 EU BS 35-36 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 STL - FOUND CORROSION AT STRINGER 16 RIGHT AT FRAME 35 THROUGH 36. MAINTENANCE REPAIRED STRINGER 16 IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 1998112000855 19981120 00855 EU 1998 11 20 RAIA981028 1 19981028 A 5347 BAC15201560 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU COCKPIT CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 STL - RIGHT OUTBOARD SEAT TRACK IN COCKPIT IS CORRODED AT AFT END. MAINTENANCE REPAIRED SEAT TRACK IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 1998112000856 19981120 00856 EU 1998 11 20 RAIA981018 1 19981028 A 5240 7075T6063 SKIN AEROSP ATR42 ATR42300 8680920 EU SERVICE DOOR CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 SERVICE DOOR SKIN AT DOOR SILL HAS CORROSION. REPLACED SILL SKIN IAW ATR42 SRM 51-25-02 AND 51-25-04. (M) 2 H 7 2 4T RT A53EU 1998112000857 19981120 00857 EU 1998 11 20 RAIA981021 1 19981029 A 3000 3E18725 DE-ICE AMMETER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 431AM 15459 881 FLT 7325 - BMI - SMOKE IN COCKPIT, COMING FROM PROP HEAT PANEL. A/C DIVERTED TO SPI. MAINTENANCE REPLACED DE-ICE AMMET ER AND LEFT SKIRT PANEL. (M) 2 L 7 2 4T RT A56EU 1998112000858 19981120 00858 EU 1998 11 20 98ZZZM835 1 19981029 A 3310 13730386K411 SKIRT PANEL BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 03 431AM 15459 881 FLT 7325 - BMI - SMOKE IN COCKPIT, COMING FROM PROP HEAT PANEL. A/C DIVERTED TO SPI. MAINTENANCE REPLACED DE-ICE AMMET ER AND LEFT SKIRT PANEL. (M) 2 L 7 2 4T RT A56EU 1998112000859 19981120 00859 EU 1998 11 20 RAIA981026 1 19981028 A 5311 7075T6050 FRAME AEROSP ATR42 ATR42300 8680920 EU BS 30 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 STL - FOUND CORROSION AT FRAME 30 STRINGER 21 LEFT TO 19 RIGHT. MAINTENANCE REPAIRED FRAME 30 IAW ATR 42 SRM. (M) 2 H 7 2 4T RT A53EU 1998112000860 19981120 00860 EU 1998 11 20 RAIA981025 1 19981028 A 5311 7075T6050 FRAME AEROSP ATR42 ATR42300 8680920 EU BS 28 CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 STL - FOUND CORROSION AT FRAME 28 FROM STRINGER 21 LEFT TO 19 RIGHT. MAINTENANCE REPAIRED FRAME 28 IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 1998112000861 19981120 00861 EU 1998 11 20 RAIA981024 1 19981028 A 5313 NTA44658 STRINGER AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 STL - FOUND CORROSION AT STRINGER 15 AT AFT END OF PEDESTAL. MAINTENANCE REPAIRED STRINGER 15 IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 1998112000862 19981120 00862 EU 1998 11 20 RAIA981023 1 19981028 A 5315 BAC14902864 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A RAIA K NONE O OTHER IN INSP/MAINT 1 CE 03 423TE 22058 119 STL - FLOORBEAM NR 35 IS CORRODED ON TOP CAP AND BOTTOM OF TOP CAP. MAINTENANCE REPAIRED FLOORBEAM IAW ATR42 SRM. (M) 2 H 7 2 4T RT A53EU 1998112000863 19981120 00863 EU 1998 11 20 RAIA981022 1 19981029 A 7722 8972605 TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 422AM 4011 856 FLT 7334 - STL - DURING RUNUP FOR TAKEOFF, LEFT EGT GAUGE ERRATIC. MAINTENANCE REPLACED LEFT DELTA P/P BOX. (M) 2 L 7 2 4T RT A56EU 1998112000864 19981120 00864 EU 1998 11 20 RAIA981101 1 19981101 A 3010 13730897K FUSE JETAIR JETSTM JETSTM4101 1500501 EU ELEVATOR FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 553HK 41066 FLT 7723 - JFK - ELEVATOR HORN HEAT FAILED. MAINTENANCE REPLACED FUSE. (M) 2 L 7 2 4T RT A41NM 1998112000865 19981120 00865 EU 1998 11 20 RAIA981029 1 19981029 A 7712 MT938T11435S CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA B EMER. DESCENT Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CE 03 562HK 6450 41078 FLT 7663 - JFK - LEFT ENGINE SHUTDOWN IN FLIGHT. MAINTENANCE REPLACED LEFT ENGINE TORQUE RING CANNON PLUG. (M) 2 L 7 2 4T RT A41NM 1998112000866 19981120 00866 NM 1998 11 20 P2EA98210 1 19981005 A 5320 SPLICE BOEING 737 737244 138448U NM BS 663 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - INTERIOR FUSELAGE SPLICE CRACKED AT BS 663.75, STRINGER 6 LT, DEFECT SIZE LENGTH .25O INCH. REPLACED FUSELAGE SPL ICE FROM BS 657 TO BS 669, STRINGER 6 LEFT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998112000867 19981120 00867 NM 1998 11 20 P2EA98209 1 19981005 A 5320 SPLICE BOEING 737 737244 138448U NM BS 663 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - INTERIOR FUSELAGE SPLICE 5-7R CRACKED AT BS 663.75, DEFECT SIZE LENGTH .25 INCH. REPLACED FUSELAGE SPLICES FROM B S 657 AND BS 669, BETWEEN STRINGER 6 LT AND STRINGER 7 LT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998112000868 19981120 00868 NM 1998 11 20 P2EA98208 1 19981006 A 5330 SKIN BOEING 737 737244 138448U NM BS 946-956 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - AFT SERVICE DOORWAY, LOWER HINGE CUTOUT CRACKED AT FORWARD SECTION, DEFECT SIZE LENGTH .625 INCH. REPAIRED FUSELA GE SKIN SECTION FROM BS 946 TO BS 956, BETWEEN STRINGER 13 RT AND STRINGER 16 RT PER SRM 53-30-3 FIG 33. (M) 2 L 7 2 4F A16WE 1998112000869 19981120 00869 NM 1998 11 20 P2EA98206 1 19981005 A 5330 SKIN BOEING 737 737244 138448U NM BS 462-464 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN INTERNAL DOUBLER DISBONDED FROM BS 462 TO BS 464, BETWEEN STRINGER 13 LT AND STRINGER 14 LT. REPAIR ED FUSELAGE SKIN INTERNAL DOUBLER FROM BS 400 TO BS 500, BETWEEN STRINGER 10 LT AND STRINGER 14 LT PER BOEING SERVICE BU LLETIN 737-53-1048, REV 4 DATED SEPT 15, 1994, SEC 3 PART 3, FIG 3, DETAILS 2 AND DETAIL 3. (M) 2 L 7 2 4F A16WE 1998112000870 19981120 00870 NM 1998 11 20 P2EA98205 1 19981002 A 5320 DOOR FRAME BOEING 737 737244 138448U NM BS 500 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - C1 DOOR FRAME DENTED AT BS 500B, STRINGER 25 RT, DEFECT SIZE LENGTH 1 INCH WIDTH .135 INCH. REPAIRED C1 DOOR FRAM E AT BS 500B, BETWEEN STRINGER 22 RT AND STRINGER 25 RT PER SRM 51-40-3 FIG 1 PAGE 5. (M) 2 L 7 2 4F A16WE 1998112000871 19981120 00871 NM 1998 11 20 P2EA98204 1 19981005 A 5347 SEAT TRACK BOEING 737 737244 138448U NM BS 344-380 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PAX CABIN SEAT TRACK AND ANGLE CORRODED FROM BS 344 TO BS 380, LBL 46 INCHES AND LBL 63 INCHES. REPLACED SEAT TRA CK SECTION BETWEEN BS 344 AND BS 380, LBL 46 INCHES PER SRM 53-10-5 FIG 2, 51-10-1 PAGE 5, AND 51-30-2. (M) 2 L 7 2 4F A16WE 1998112000872 19981120 00872 NM 1998 11 20 98ZZZM836 1 19981005 A 5320 ANGLE BOEING 737 737244 138448U NM BS 344-380 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PAX CABIN SEAT TRACK AND ANGLE CORRODED FROM BS 344 TO BS 380, LBL 46 INCHES AND LBL 63 INCHES. REPLACED SEAT TRA CK SECTION BETWEEN BS 344 AND BS 380, LBL 46 INCHES PER SRM 53-10-5 FIG 2, 51-10-1 PAGE 5, AND 51-30-2. (M) 2 L 7 2 4F A16WE 1998112000873 19981120 00873 NM 1998 11 20 P2EA98203 1 19981006 A 5315 FLOORBEAM BOEING 737 737244 138448U NM BS 344 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PAX CABIN FLOORBEAM CORRODED AT BS 344, BETWEEN BL 0 TO LBL 55. REPLACED FLOORBEAM UPPER FLANGE AT BS 344 BETWEEN LBL 67 INCH TO RBL 41 INCH PER SRM 53-10-9 FIG 5, AND SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1998112000874 19981120 00874 NM 1998 11 20 P2EA98202 1 19981026 A 5330 SKIN BOEING 737 737244 138448U NM BS 967 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN SECTION CORRODED AT BS 967 BETWEEN STRINGER 26 LT AND STRINGER 26 RT. REPAIRED FUSELAGE SKIN SECTIO N FROM BS 962 TO BS 983, BETWEEN STRINGER 26 LT TO STRINGER 26 RT PER SRM 53-30-3 FIG 17. (M) 2 L 7 2 4F A16WE 1998112000875 19981120 00875 EU 1998 11 20 98ZZZM837 1 19980120 A 5330 SKIN AEROSP ATR72 ATR72212 EU FUSELAGE DENTED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT SIDE OF FUSELAGE DENTED BETWEEN FRAMES 18 AND 19 AT STRINGER 16R. REPAIRED SKIN IAW SRM 53-31-24 AND EO 72-53-0033. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000876 19981120 00876 EU 1998 11 20 98ZZZM838 1 19980120 A 5311 16S53671340200 FRAME AEROSP ATR72 ATR72212 EU BS 37 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FRAME 37 RIGHT TO BE CORRODED. FRAME 37 WAS REPAIRED IAW ATR 72 S RM 53-67-70 AND EO 72-53-0032. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000877 19981120 00877 EU 1998 11 20 98ZZZM839 1 19980120 A 5347 S53678001212 SEAT TRACK AEROSP ATR72 ATR72212 EU CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AFT CARGO SEAT TRACK CORRODED. RAI'D RIGHT AFT CARGO SEAT TRACK IAW ASA EO 72-53-0034. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000878 19981120 00878 EU 1998 11 20 98ZZZM840 1 19980120 A 5315 S53672408254 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FLOORBEAM 39 HAD HOLE AND CORROSION. BLENDED EDGE DAMAGE IAW SRM 51-10-00 AND HOLE IAW EO 72-53-003 SRM 53-00-00 FIG 429. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000879 19981120 00879 EU 1998 11 20 98ZZZM841 1 19980120 A 5320 S5367800821602 ZEE AEROSP ATR72 ATR72212 EU CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING 2C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT 'Z' MEMBER CORRODED. REPLACED 'Z' MEMBER IAW ATR72 SRM 51- 25-02. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000880 19981120 00880 EU 1998 11 20 98ZZZM842 1 19980120 A 5315 NTA44770 FLOORBEAM AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED FLOORBEAM 39 HAS A HOLE AND CORROSION. REPAIRED FLOORBEAM 39 IAW ATR 72 SRM 53-00-00 FIG 429 AND ASA EO 72-53-0031. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000881 19981120 00881 EU 1998 11 20 98ZZZM843 1 19980120 A 5347 S53678001228 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AFT F/A'S SEAT TRACK CORRODED. REPLACED RIGHT AFT F/A SEAT TRACK IAW ASA EO 72-53-0030. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000882 19981120 00882 EU 1998 11 20 98ZZZM844 1 19980120 A 5347 S53678001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED LEFT AFT F/A'S SEAT TRACK CORRODED. REPLACED LEFT AFT F/A SEAT T RACK IAW ASA EO 72-53-0030. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000883 19981120 00883 EU 1998 11 20 98ZZZM845 1 19980120 A 5347 S53678001245 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AIRCRAFT OUTBOARD SEAT TRACK CORRODED. REPLACED RIGHT AFT OUTBOARD SEAT TRACK IAW ASA EO 72-53-0034. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000884 19981120 00884 EU 1998 11 20 98ZZZM846 1 19980120 A 5347 S53375001210 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING 4C CHECK INSPECTION, MAINTENANCE REPORTED FORWARD LEFT OUTBOARD SEAT TRACK CORRODED. RAI'D SEAT TRACK IAW ATR72 SRM 51-25-04 AND ASA EO 72-53-0034. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000885 19981120 00885 EU 1998 11 20 98ZZZM847 1 19980107 A 5320 S5367240821401 BRACKET AEROSP ATR72 ATR72212 EU DOOR SILL CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 DURING C-CHECK INSPECTION, MAINTENANCE REPORTED SERVICE DOOR SILL PLATE ANGLE ATTACH BRACKETS CORRODED AT FRAME 39. MAN UFACTURED AND INSTALLED NEW FRAME CLEAT IAW ATR SRM 512401. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000886 19981120 00886 EU 1998 11 20 98ZZZM848 1 19980107 A 5313 S53671407228 STRINGER AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED AIRCRAFT RIGHT LOWER FUSELAGE STRINGER 18R IS CORRODED BETWEEN FRA ME 34-35. REPAIRED STRINGER IAW ATR 72 SRM 530000 FIG 428. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000887 19981120 00887 EU 1998 11 20 98ZZZM849 1 19980109 A 5311 S5367125722151 FRAME AEROSP ATR72 ATR72212 EU FUSELAGE CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT OUTER CHORD AT STRINGER 17, BETWEEN FRAMES 35-40 CORRODED. R AI CHORD IAW ATR SRM 512502. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000888 19981120 00888 EU 1998 11 20 98ZZZM850 1 19980109 A 5320 S5367800812602 SUPPORT AEROSP ATR72 ATR72212 EU CARGO BAY CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED AIRCRAFT CARGO 'Z' MEMBER CORRODED. INSTALLED NEW 'Z' MEMBER IAW ATR SRM 512503. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000889 19981120 00889 EU 1998 11 20 98ZZZM851 1 19980109 A 5347 S5367800121202 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LEFT F/A'S SEAT TRACK CORRODED. RAI LEFT F/A'S SEAT TRACK IAW EO 72-53-0027. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000890 19981120 00890 EU 1998 11 20 98ZZZM852 1 19980109 A 5347 S5367800122802 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT F/A'S SEAT TRACK CORRODED. RAI RT F/A'S SEAT TRACK IAW SRM 512504. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000891 19981120 00891 EU 1998 11 20 98ZZZM853 1 19980102 A 5347 S53678001245 SEAT TRACK AEROSP ATR72 ATR72212 EU CABIN CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT AIRCRAFT OUTBOARD SEAT TRACK AT FLOORBEAM 36R AND FRAME 33 C ORRODED. REPLACED SEAT TRACK BETWEEN FLOORBEAM AND FRAME 33 IAW ATR72 SRM 530027 AND EO 72-53-0029. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000892 19981120 00892 EU 1998 11 20 98ZZZM854 1 19980105 A 5730 S5241055200200 PANEL AEROSP ATR72 ATR72212 EU LT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED LEFT WING FEEDER TANK PANEL 522CT TO BE CORRODED. REPLACED PANEL 522CT IAW SRM 57000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000893 19981120 00893 EU 1998 11 20 98ZZZM855 1 19980103 A 5313 S533714202062 STRINGER AEROSP ATR72 ATR72212 EU BS 29/30 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED STRINGER 20 RT BETWEEN FRAMES 29 AND 30 AS CORRODED. REPAIRED STR INGER IAW SRM 530000 ATR 72. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000894 19981120 00894 EU 1998 11 20 98ZZZM856 1 19980105 A 5730 S5241055200200 PANEL AEROSP ATR72 ATR72212 EU RT WING CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 643AS 413 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED RIGHT WING FEEDER TANK PANEL 622CT CORRODED. REPLACED PANEL 622CT AS REQUIRED IAW SRM 570000. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000895 19981120 00895 EU 1998 11 20 98ZZZM857 1 19980120 A 5320 S5367800826901 SUPPORT AEROSP ATR72 ATR72212 EU BS 38-39 CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 641AS 387 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED FLOOR SUPPORT BETWEEN FRAMES 38 AND 39 CORRODED. FLOOR SUPPORT WA S REPLACED IAW SRM 512501. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112000896 19981120 00896 NM 1998 11 20 USAA980456 1 19980930 A 5320 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 LBL 24 FLOORBEAM. INSTALLED REPAIR ANGLE P ER EA 62449 SB 737-53-1120 REV 1 PART VI. (M) 2 L 7 2 4F A16WE 1998112000897 19981120 00897 NM 1998 11 20 USAA980455 1 19980930 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-4 CHECK HFEC INSPECTION, FOUND A 1.5 INCH CRACK BS 520 WL 208 RBL 24 FLOORBEAM. INSTALLED REPAIR ANGLES PER EA 62449 SB 737-53-1120 REV 1. (M) 2 L 7 2 4F A16WE 1998112000898 19981120 00898 NM 1998 11 20 USAA980454 1 19980930 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK HFEC INSPECTION, FOUND .25 INCH CRACK BS 520 RBL 45 FLOORBEAM 'T' CAP RADIUS. INSTALLED REPAIR A NGLES PER EA 62449 BOEING SB 737-53-1120 REV 1. (M) 2 L 7 2 4F A16WE 1998112000899 19981120 00899 NM 1998 11 20 USAA980453 1 19980930 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND CLIP NUT HOLES STATION 344 FLOORBEAM BL 0 TO LBBL 42. R EPAIRED 'T' CAP SPLICED DOUBLER PER SRM 53-10-13. (M) 2 L 7 2 4F A16WE 1998112000900 19981120 00900 NM 1998 11 20 USAA980452 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 10R STRINGER TIE CLIP. REPAIRED P ER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112000901 19981120 00901 NM 1998 11 20 USAA980451 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 8R STRINGER TIE CLIP. REPAIRED P ER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112000902 19981120 00902 NM 1998 11 20 USAA980450 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 7R STRINGER TIE CLIP. REPAIRED P ER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112000903 19981120 00903 NM 1998 11 20 USAA980449 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 2R STRINGER TIE CLIP. REPAIRED P ER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112000904 19981120 00904 NM 1998 11 20 USAA980448 1 19980930 A 5320 65353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727A STRINGER 2R, STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112000905 19981120 00905 NM 1998 11 20 USAA980447 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 747 STRINGER 7L STRINGER TIE CLIP. REPAIRED PE R EO 5939G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112000906 19981120 00906 NM 1998 11 20 P2EA98201 1 19981020 A 5711 SPAR BOEING 737 737244 138448U NM WS 475 WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING FRONT SPAR LOWER CHORD WORN AT WSL 475, DEFECT SIZE LENGTH 2.625 INCH, WIDTH .812 INCH DEPTH .055 INCH. REPAIRED FRONT SPAR LOWER CHORD AT WS 475 PER COOPESA EO C00-SJO-57-567-98 DATED OCT 15, 1998 AND BOEING FAX COO-SJO-9 8-0755RR DATED OCT 9, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1998112000907 19981120 00907 NM 1998 11 20 P2EA98200 1 19981005 A 5712 RIB BOEING 737 737244 138448U NM WS 135 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - LEFT WING NR 1 FUEL TANK RIB CRACKED AT WBL 135.5 IN AFT SECTION, BETWEEN REAR SPAR AND STRINGER 16. REPAIRED LEF T WING LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SB 737-57-1186 DATED APRIL 13, 1989 SECTIO N 3, PART 3, FIG 3. (M) 2 L 7 2 4F A16WE 1998112000908 19981120 00908 NM 1998 11 20 P2EA98199 1 19981013 A 5330 SKIN BOEING 737 737244 138448U NM BS 1020-1035 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PROVISIONAL FUSELAGE SKIN REPAIR FROM BS 1020 TO BS 1035, BETWEEN STRINGER 22 LT AND STRINGER 24 RT NOT COMPLIANT WITH THE SRM. REPAIRED FUSELAGE SKIN SECTION FROM BS 1020 TO BS 1035, BETWEEN STRINGER 2 LT AND STRINGER 24 LT PER SRM 53-30-3 FIG 16. (M) 2 L 7 2 4F A16WE 1998112000909 19981120 00909 NM 1998 11 20 P2EA98198 1 19981013 A 5330 SKIN BOEING 737 737244 138448U NM BS 1036-1051 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PROVISIONAL FUSELAGE SKIN REPAIR FROM BS 1036 TO BS 1051, BETWEEN STRINGERS 20 RT AND 23 RT NOT IN COMPLIANCE WITH SRM. REPAIRED FUSELAGE SKIN SECTION FROM BS 1035 TO BS 1054, BETWEEN STRINGER 19 RT AND 23 RT PER SRM 53-30-3 FIG 7. ( M) 2 L 7 2 4F A16WE 1998112000910 19981120 00910 NM 1998 11 20 98ZZZM858 1 19981015 A 5347 SEAT TRACK BOEING 737 737244 138448U NM BS 727-767 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PAX SEAT TRACK SECTION CORRODED FROM BS 727B TO BS 767, LBL 45 INCHES. REPLACED SEAT TRACK SECTION FROM BS 727B T O BS 767, LBL 45 INCHES, WL 208.1 PER SRM 51-10-1 PAGE 5, 51-30-2 AND 53-10-5 FIG 2. (M) 2 L 7 2 4F A16WE 1998112000911 19981120 00911 NM 1998 11 20 P2EA98196 1 19981015 A 5347 SEAT TRACK BOEING 737 737244 138448U NM BS 360-400 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PAX CABIN SEAT TRACK CORRODED FROM BS 360 TO BS 400, RBL 45 INCHES. REPLACED SEAT TRACK SECTION FROM BS 360 TO BS 400, RBL 45 INCHES, WL 208.1 PER SRM 51-10-1 PAGE 5, 51-30-2, AND 53-10-5 FIG 2. (M) 2 L 7 2 4F A16WE 1998112000912 19981120 00912 NM 1998 11 20 P2EA98195 1 19981015 A 5347 SEAT TRACK BOEING 737 737244 138448U NM BS 847-947 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PAX CABIN SEAT TRACK CORRODED FROM BS 847 TO BS 947, RBL 45 INCHES. REPLACED SEAT TRACK SECTION FROM BS 847 TO BS 947 RBL 45 INCHES PER SRM 51-10-1 PAGE 5, 51-30-2, AND 53-10-5 FIG 2. (M) 2 L 7 2 4F A16WE 1998112000913 19981120 00913 NM 1998 11 20 P2EA98194 1 19981005 A 5347 SEAT TRACK BOEING 737 737244 138448U NM BS 344-420 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PASSENGER CABIN SEAT TRACK CORRODED FROM BS 344 TO BS 420, LBL 25, WL 208.1. REPLACED SEAT TRACK SECTION FROM BS 344 TO BS 380, LBL 25 INCHES PER SRM 51-10-1 PAGE 5, 51-10-2, 53-10-5 FIG 2. (M) 2 L 7 2 4F A16WE 1998112000914 19981120 00914 NM 1998 11 20 P2EA98181 1 19981003 A 5313 STRINGER BOEING 737 737244 138448U NM BS 259-294 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - STRINGER 23RT CORRODED BETWEEN BS 259.5 TO BS 294.5, DEFECT SIZE 35 INCHES IN LENGTH. REPAIRED FUSELAGE STRINGER SECTION BETWEEN BS 259 AND BS 313 PER SRM 53-10-03 FIG 1 SHEET 7. (M) 2 L 7 2 4F A16WE 1998112000915 19981120 00915 NM 1998 11 20 P2EA98179 1 19981002 A 5330 SKIN BOEING 737 737244 138448U NM BS 815 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN SECTION CORRODED AT BS 815, STRINGER 20 LT. REPAIRED FUSELAGE LAP JOINT SKIN SECTION BETWEEN BS 809 AND BS 854, BETWEEN STRINGERS 19 LT AND 21 LT DUE TO CORROSION PER SRM 53-30-3 FIG 15. (M) 2 L 7 2 4F A16WE 1998112000916 19981120 00916 NM 1998 11 20 HNAA9894252 1 19980913 A 5347 85320490127 SEAT TRACKS DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 25129 163 DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPA IRED IAW EO8-53-98-817. (M) 2 H 7 2 4T RT A13NM 1998112000917 19981120 00917 NM 1998 11 20 HNAA9894249 1 19980913 A 5347 85320701117 SEAT TRACKS DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 163 DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPA IRED IAW EO8-53-98-917. (M) 2 H 7 2 4T RT A13NM 1998112000918 19981120 00918 NM 1998 11 20 HNAA9894250 1 19980913 A 5347 85320701123 SEAT TRACKS DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 25129 163 DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. SEAT TRACKS WERE REPAIRED IAW EO8-53-98-335. (M) 2 H 7 2 4T RT A13NM 1998112000919 19981120 00919 NM 1998 11 20 HNAA9894251 1 19980913 A 5347 85320490129 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 25129 163 DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPA IRED IAW E08-98-817. (M) 2 H 7 2 4T RT A13NM 1998112000920 19981120 00920 NM 1998 11 20 HNAA9894253 1 19980913 A 5347 85320490123 SEAT TRACK DHAV DHC8 DHC8102 2809003 NM CABIN CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 25129 163 DURING C-CHECK INSPECTION, THE SEAT TRACKS WERE FOUND CORRODED BEYOND THE DEHAVILLAND LIMITS. THE SEAT TRACKS WERE REPA IRED IAW EO8-98-817. (M) 2 H 7 2 4T RT A13NM 1998112000921 19981120 00921 NM 1998 11 20 HNAA9894254 1 19980913 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 942HA 25129 163 DURING C-CHECK INSPECTION, A DENT WAS BELOW THE ICE SHIELD ON STRINGER 235 WITH A MAX DEPTH OF .040 INCH, 1.6 INCH LONG AND .8 WIDE OUT OF THE LIMITS OF THE DEHAVILLAND SRM 53-00-16. THE DENT WAS PLACED ON A 250 HOUR REINSPECT FOR CRACKING IAW EO8-53-98-815. (M) 2 H 7 2 4T RT A13NM 1998112000922 19981120 00922 NM 1998 11 20 HNAA9891466 1 19981013 A 5210 85210368001 CABLE DHAV DHC8 DHC8102 2809003 NM PAX DOOR LOOSE A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 914HA 53 BWI - FLT 3249 - PAX DOOR WILL NOT OPEN. REMOVED AND REPLACED AIRSTAIR DOOR OUTER CABLE ASSY. (M) 2 H 7 2 4T RT A13NM 1998112000923 19981120 00923 NM 1998 11 20 HNAA9894365 1 19981006 A 3350 M533205 CIRCUIT BREAKER DHAV DHC8 DHC8102 2809003 NM COCKPIT TRIPPED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 943HA 167 HPN - FLT 3260 - AFT CEILING AISLE DOWN EMERGENCY LIGHT AND EMERGENCY EXIT SIGN AT ROW 4 INOP. RECYCLED CB L-1 (EMERGEN CY LIGHTS CONTROL). OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998112000924 19981120 00924 NM 1998 11 20 HNAA9894158 1 19980924 A 3231 54C546347 VALVE DHAV DHC8 DHC8102 2809003 NM NR 1 MLG DAMAGED A HNAA O OTHER J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 EA 07 941HA 676 161 AFTER GEAR RETRACTION, NR 2 ENGINE DRIVEN HYD PUMP CAUTION LIGHTS ILLUMINATED. SERVICED AND BLED NR 2 HYD SYSTEM. REMO VED AND REPLACED THREE LANDING GEAR DOOR SEQUENCER VALVE ON RON FOR FCD 8-32-94-351. NR 2 HYD SYSTEM WAS NOT BLED PROPE RLY. (M) 2 H 7 2 4T RT A13NM 1998112000925 19981120 00925 NM 1998 11 20 98ZZZM859 1 19980924 A 3231 54C546347 VALVE DHAV DHC8 DHC8102 2809003 NM NR 2 MLG DAMAGED A HNAA O OTHER J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 EA 07 941HA 124 161 AFTER GEAR RETRACTION, NR 2 ENGINE DRIVEN HYD PUMP CAUTION LIGHTS ILLUMINATED. SERVICED AND BLED NR 2 HYD SYSTEM. REMO VED AND REPLACED THREE LANDING GEAR DOOR SEQUENCER VALVE ON RON FOR FCD 8-32-94-351. NR 2 HYD SYSTEM WAS NOT BLED PROPE RLY. (M) 2 H 7 2 4T RT A13NM 1998112000926 19981120 00926 NM 1998 11 20 98ZZZM860 1 19980924 A 3231 54C546347 VALVE DHAV DHC8 DHC8102 2809003 NM NLG DAMAGED A HNAA O OTHER J W WARNING INDICATION INADEQUATE Q C CL CLIMB 1 EA 07 941HA 42 161 AFTER GEAR RETRACTION, NR 2 ENGINE DRIVEN HYD PUMP CAUTION LIGHTS ILLUMINATED. SERVICED AND BLED NR 2 HYD SYSTEM. REMO VED AND REPLACED THREE LANDING GEAR DOOR SEQUENCER VALVE ON RON FOR FCD 8-32-94-351. NR 2 HYD SYSTEM WAS NOT BLED PROPE RLY. (M) 2 H 7 2 4T RT A13NM 1998112000927 19981120 00927 NM 1998 11 20 HNAA9894159 1 19980923 A 3231 83231046001 ROD ASSY DHAV DHC8 DHC8102 2809003 NM LT MLG OUT OF ADJUST A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 941HA 25345 161 ON GER RETRACTION, LEFT FORWARD MAIN LANDING GEAR DOOR HANGS DOWN APPROX .5 INCH WITH GEAR UP AND LOCKED. NO ADVISORY L IGHT INDICATED. RIGGED AND ADJUSTED FORWARD DOOR. (M) 2 H 7 2 4T RT A13NM 1998112000928 19981120 00928 NM 1998 11 20 HNAA9894155 1 19980917 A 5230 85230310001 SKIN DHAV DHC8 DHC8102 2809003 NM CARGO DOOR DENTED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 941HA 25305 161 DURING RON MAINTENANCE A DENT WAS FOUND IN THE BAGGAGE DOOR 1 INCH AFT OF FRAME INCHES, 1.1 INCH IN LENGTH AND .8 INCH W IDE OUT OF THE LIMITS OF THE SRM. THE DENT WAS DEFERRED FOR REPAIR WITHIN 500 HOURS BY AN ENGINEERING DISPOSITION. (M) 2 H 7 2 4T RT A13NM 1998112000929 19981120 00929 NM 1998 11 20 HNAA9893156 1 19980915 A 5240 85410617005 DOOR DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE SEPARATED A HNAA K NONE D INFLIGHT SEPARATION NR NOT REPORTED 1 EA 07 931HA 26785 FI168 132 FLT 3293 - CHO-PIT - SPR ACCESS DOOR CAME OFF. REMOVED DOOR HINGES AND INSPECTED AREA, ENTERED ON CDC. ON SEPT 18, REI NSTALLED DOOR AND HINGES. CLEARED CDC ITEM. (M) 2 H 7 2 4T RT A13NM 1998112000930 19981120 00930 NM 1998 11 20 HNAA9891047 1 19980909 A 5260 4323 LOCK ASSY ADAMS DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 910HA 33896 022 FLT 3162 - GSO-DCA - COCKPIT DOOR DOES NOT OPEN, LATCH ASSY INTERMITTENTLY STICKS. INSPECTED DOOR LATCH ASSY AND STRIKE R PLATE FOR DEFECTS, NONE FOUND. COULD NOT DUPLICATE. (M) 2 H 7 2 4T RT A13NM 1998112000931 19981120 00931 NM 1998 11 20 HNAA9898148 1 19980910 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 981HA 11534 JAX085 378 FLT 3157 - ORF-PIT - DURING FLT, OVERHEAD CENTER AISLE EMERGENCY DOWNLIGHTS AND RT FORWARD EMERGENCY EXIT LIGHTS WERE IN OP. REMOVED AND REPLACED BATTERIES 3351 PS1 AND PS2. (M) 2 H 7 2 4T RT A13NM 1998112000932 19981120 00932 NM 1998 11 20 HNAA9892064 1 19981010 A 5730 85710024002 COVER DHAV DHC8 DHC8102 2809003 NM RT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 SBY - DURING C-CHECK INSPECTION, FOUND CORROSION ON THE RIGHT WING MIDDLE FUEL TANK LID THAT WAS MAINTENANCE MANUAL LIMI TS. REPAIRED IAW PIEDMONT AIRLINES E08-57-98-1033. (M) 2 H 7 2 4T RT A13NM 1998112000933 19981120 00933 NM 1998 11 20 HNAA9892063 1 19981010 A 5730 85710024002 COVER DHAV DHC8 DHC8102 2809003 NM RT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 SBY - DURING C-CHECK INSPECTION, THE RIGHT WING MIDDLE FUEL CELL COVER PLATE WAS FOUND TO BE CORRODED BEYOND MAINTENANCE MANUAL LIMITS. REPAIRED THE COVER IAW PIEDMONT AIRLINES E08-57-98-1033. (M) 2 H 7 2 4T RT A13NM 1998112000934 19981120 00934 NM 1998 11 20 HNAA9891062 1 19981004 A 5230 SKIN DHAV DHC8 DHC8102 2809003 NM CARGO DOOR DAMAGED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 910HA 34086 022 SBY - BAGGAGE DOOR SKIN FOUND DAMAGED ON TOP AFT CORNER IN TWO PLACES. REPAIRED IAW PIEDMONT AIRLINES E08-52-98-1025. ( M) 2 H 7 2 4T RT A13NM 1998112000935 19981120 00935 NM 1998 11 20 HNAA9892061 1 19981010 A 5730 85710023002 PLATE DHAV DHC8 DHC8102 2809003 NM RT WING CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 920HA 084 SBY - DURING C-CHECK INSPECTION, FOUND CORROSION PITS WERE FOUND IN THE FUEL CELL LID AND LADDER PLATE ON THE OUTBOARD E ND. REPAIRED IAW PIEDMONT AIRLINES E08-57-98-1033. (M) 2 H 7 2 4T RT A13NM 1998112000936 19981120 00936 NM 1998 11 20 HNAA9899565 1 19981021 A 3230 858601 PSEU DHAV DHC8 DHC8201 2809001 NM NLG FAILED A HNAA O OTHER O OTHER CL CLIMB 1 EA 07 995HA 4693 99 460 PNS - FLT 3054 - NOSE GEAR CYCLED ONCE ON CLIMB-OUT DOOR AND HANDLE LIGHTS ON. REMOVED AND REPLACED PSEU. OPS CHECK GO OD. (M) 2 H 7 2 4T RT A13NM 1998112000937 19981120 00937 NM 1998 11 20 GAIA9894 1 19981028 A 5312 BULKHEAD BOEING 727 727224 1384076 NM BS 950 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING HEAVY C-CHECK INSPECTION, FOUND A HOLE LOCATED AT FS 950, 10 INCHES ABOVE STRINGER 28 LEFT. THE HOLE WAS REPAIRE D USING BOEING TELEX AOC-OKO-98-0080TR. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000938 19981120 00938 NM 1998 11 20 GAIA9895 1 19981028 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 360 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING HEAVY C-CHECK INSPECTION, REVEALED TWO HOLES ELONGATED AT FS 360 STRINGER 19 LEFT. THE HOLES WHERE REAMED TO COR RECT THE OBLONG CONDITION. THE DAMAGE WAS REPAIRED IAW BOEING TELEX AOC-OKO-98-0087RR. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000939 19981120 00939 NM 1998 11 20 GAIA9896 1 19981028 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 870 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND A CRACK IN THE FLOORBEAM LOCATED AT BS 870 LBL 24.75. DURING REPAIR USING SRM REFERENCES MAINTENANCE MISSED DRILLED A HOLE IN WHICH REPAIR WAS OUTSIDE THE SCOPE OF THE SRM REPAIR. THE MISSED DR ILLED HOLE WAS REPAIRED USING FLIGHT VEHICLES INC REPAIR SKETCH NUMBER 53-98522-3. THE AIRCRAFT WAS THEN RETURNED TO SE RVICE. (M) 2 L 7 3 4F A3WE 1998112000940 19981120 00940 NM 1998 11 20 GAIA9897 1 19981028 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 740 CRACKED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND A CRACK IN THE FLOORBEAM LOCATED AT BS 740 RBL 35 UPPER CHORD. THE CRACK W AS REPAIRED USING FLIGHT VEHICLES INC REPAIR SKETCH NUMBER 53-98522-2. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000941 19981120 00941 NM 1998 11 20 GAIA9898 1 19981028 A 5720 FITTING BOEING 727 727224 1384076 NM WS 1135 DAMAGED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND TWO PILOT HOLES ELONGATED, LOCATED AT RT MLG WHEEL WELL AREA. THE HOLES WH ERE REPAIRED USING FLIGHT VEHICLES INC REPAIR SKETCH NUMBER 57-98515-2. THE AIRCRAFT WAS THEN RETURN TO SERVICE (M) 2 L 7 3 4F A3WE 1998112000942 19981120 00942 NM 1998 11 20 GAIA9899 1 19981022 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 950 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND CORROSION ALONG STRINGER 27 RIGHT AT BS 950. THE CORROSION WAS REMOVED AND REPAIRED IAW FLIGHT VEHICLES INC SKETCH NUMBER 53-98515-1. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000943 19981120 00943 NM 1998 11 20 GAIA98100 1 19981028 A 5230 SKIN BOEING 727 727224 1384076 NM CARGO DOOR SEPARATED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND THE AFT LOWER EDGE OUTER SKIN ALONG THE MAIN CARGO DOOR SEPARATING APPROX 8 INCH AT BS 645. THE DOOR WAS REPAIRED USING FLIGHT VEHICLES INC. REPAIR SKETCH NUMBER 5298522-1. THE AIRCRAFT WAS TH EN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000944 19981120 00944 NM 1998 11 20 GAIA98101 1 19981028 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1166 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND THE FRAME DENTED AT BS 1166 STRINGER 17, LEFT WATER LINE 211. THE FRAME WA S REPAIRED AT STRINGER 17, LEFT WATER LINE 211 USING FLIGHT VEHICLES INC. REPAIR SKETCH NUMBER 53-98515-4. THE AIRCRAF T WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000945 19981120 00945 NM 1998 11 20 GAIA98102 1 19981022 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1166 DENTED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND THE FRAME DENTED AT BS 1166 BETWEEN STRINGERS 15 RIGHT AND 16 RIGHT. THE F RAME WAS REPAIRED AT BS 1166 BETWEEN STRINGERS 14 RIGHT TO 16 RIGHT USING FLIGHT VEHICLES INC. REPAIR SKETCH NUMBER 53- 98515-5. THE AIRCRAFT WS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000946 19981120 00946 NM 1998 11 20 98ZZZM861 1 19981016 A 5210 65273421 SEAL BOEING 727 7272K5 NM PAX DOOR TORN A FX7A J A DUMP FUEL UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 369FA 21851 KLAS-KMDT - ON FAE FLIGHT NR 807, AIRCRAFT UNABLE TO PRESSURIZE, AT 20,000 FLT ALT CABIN WAS 10,000 FT. FUEL WAS DUMPED AND AIRCRAFT RETURNED TO KLAS. ON GROUND MAINTENANCE FOUND AFT ENTRY DOOR PRESSURE SEAL LOWER SIDE TORN. SEAL REPAIRE D IAW MM 51-30-1. ENGINE RUN WAS ACCOMPLISHED AND A/C PRESSURIZED NORMAL PER 21-31-00. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 3 4F RT A3WE 1998112000947 19981120 00947 NM 1998 11 20 98ZZZM862 1 19980829 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1130 CORRODED A FX7A K NONE O OTHER IN INSP/MAINT 1 SO 19 32719 20388 DURING C-CHECK INSPECTION, FOUND CORROSION ON STATION 1130 FLOORBEAM, CORROSION REMOVAL BLENDOUT WAS BEYOND SRM LIMITS. CORROSION WAS REPAIRED PER BOEING LETTER AND DRAWING HAE-TUS-98-0166TR AND SRM 53-10-8. AUTHORIZATION PER FAA FORM 811 0-3 DATED 8/27/98, FE WING NM-1220. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000948 19981120 00948 NM 1998 11 20 98ZZZM863 1 19980829 A 5330 SKIN BOEING 727 727224 1384076 NM FUSELAGE CORRODED A FX7A K NONE O OTHER IN INSP/MAINT 1 SO 19 32719 20388 DURING C-CHECK, FOUND LEVEL 2 CORROSION ON EXT FUSELAGE SKIN ABOVE R2 SERVICE DOOR UPPER HINGE AND BELOW R2 SERVICE DOOR BELOW LOWER HINGE. CORROSION WAS REPAIRED PER BOEING LETTER AND DRAWING HAE-TUS-98-014RR DATED 8/7/98 AND SRM 51-10-6, 53-30-1, 53-30-2, DRAWING HAE-TUS-98-0153RR DATED 8/10/98, SRM 51-10-6, 51-10-2 AND 51-30-2. AUTHORIZATION PER FAA 811 0-3, FE WING, NM-1220 DATED 8/21/98. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998112000949 19981120 00949 NM 1998 11 20 98ZZZM864 1 19981023 A 5210 6990299 HINGE COVER BOEING 727 7272K5 NM PAX DOOR DAMAGED A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 369FA 21851 FLT 907 - KMIA-KMLU - ON FAE FLT, SHORTLY AFTER TAKEOFF, A NOISE WAS EXPERIENCED ON OR AROUND THE FORWARD ENTRY DOOR, DU E TO THE PROXIMITY OF THE AIRPORT THE CAPTAIN DECIDED TO RETURN TO KMIA. NO EMERGENCY WAS DECLARED, OR FUEL DUMPED. ON GROUND MAINTENANCE, FOUND DOOR HINGE COVER DAMAGED. HINGE COVERED WAS REPLACED IAW MM 52-11-01. AIRCRAFT WAS PRESSURI ZED AND LEAK CHECK WAS PERFORMED AS PER MM 21-30-0. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F RT A3WE 1998112000950 19981120 00950 NM 1998 11 20 98ZZZM865 1 19981017 A 2120 656022924 DUCT BOEING 727 7272K5 NM RT A/C BAY CRACKED A FX7A A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 369FA 21851 FLT 807 - KLAS-KMDT, ON FAE FLIGHT, AIRCRAFT UNABLE TO MAINTAIN PRESET PRESSURIZATION, AT 20,000 FLT ALT CABIN WAS 10,00 0 FT. FUEL WAS DUMPED AND AIRCRAFT RETURNED TO KLAS. ON GROUND MAINTENANCE FOUND AN AIR LEAK ON THE RIGHT AIR CONDITIO NING BAY DUCT. MAINTENANCE DEFERRED THE RT AND LT AIR CONDITIONING PACKS IAW MEL 21-1-2 PER AUTHORIZATION NR M-415, CAT 'C'. BOTH PACKS CLOSED. AIRCRAFT RELEASED INTO SERVICE. MEL CLEARED ON LOG PAGE 2906 ON 10/17/98 BY REPLACING DUCT. (M) 2 L 7 3 4F RT A3WE 1998112000951 19981120 00951 EA 1998 11 20 98ZZZM866 1 19981024 A 2750 C6CW10831 ROD ASSEMBLY DHAV DHC6 DHC6300 2802606 EA WING ROOT GROOVED A ASWA K NONE O OTHER IN INSP/MAINT 1 WP 07 142SA 241 241 DURING AIRCRAFT SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND LEFT AND RIGHT WING ROOT TO INBOARD BELLCRANK FLAP ROD ASSEMBLIES HEAVILY GROOVED AND SCORED BY ROD GUIDE ROLLERS. THIS IS AN ONGOING CHRONIC PROBLEM ON THIS AIRCRAFT TYPE. GUIDE ROLLERS ARE MADE FROM A HARD MATERIAL THAT DAMAGED THE SOFTER RODS. THESE RODS ARE THE SUBJECT OF AD 80-03-08. M OD 6/1707 HAD PREVIOUSLY BEEN ACCOMPLISHED. (M) 1 H 7 2 3T RT A9EA 1998112000952 19981120 00952 WP 1998 11 20 AALA981915 1 19981009 A 2120 WATER SEPARATOR DOUG DC9 DC982 3022082 WP A/C BAY CONTAMINATED A A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 7522A 49899 MAF - FLT 839 - EN ROUTE DFW-SAN, APPROX 45 MINS INTO FLT, AFT CABIN F/A REPORTED STRONG SMELL OF SOMETHING BURNING IN A REA NEAR MID-CABIN. AS COCKPIT DOOR WAS OPENED THE SMELL OF HOT ELECTRICAL/HOT PLASTIC BECAME APPARENT ALONG WITH A LIG HT HAZE IN CABIN. INITIATED EMERGENCY DESCENT, PEFORMED CABIN/COCKPIT FIRE/SMOKE CHECKLIST SMOKE REMOVAL. EMERGENCY LA NDED AT MAF W/O INCIDENT. SOURCE OF SMELL COULD NOT BE DETERMINED BUT LINGERED IN A/C CABIN FOR ONE HOUR AFTER COMPLETE POWER DOWN. PERFORMED PACK BURN OUT PER MM. REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS, RAN BOTH PACKS FOR 2 HOUR S. NO SMELL NOTED, OPERATE ALL OVENS AND ALL LIGHTS WITH NO SMELL OR SMOKE NOTED. CHECKED E/E AND ALL CARGO PITS NO SM 2 L 7 2 4F A6WE 1998112000953 19981120 00953 NE 1998 11 20 ASOA98081 2 19981013 A 7200 ENGINE EMB 120 EMB120RT SO PWA 118 PW118 NE LT NACELLE MALFUNCTIONED A ASOA A E UNSCHED LANDING ENGINE SHUTDOWN J Y WARNING INDICATION ENGINE STOPPAGE CR CRUISE 1 SO 11 266AS 120188 115255 ATL-GPT - SHORTLY AFTER DESCENDING FROM FL 200 AND LEVELING OFF AT 14,000 FT, RECEIVED A TRIPLE CHIME AUDIO WARNING, ACC OMPANIED BY THE RED OIL PRESSURE WARNING ON THE MAP. THE LEFT ENGINE OIL PRESSURE GAUGE WAS INDICATING LESS THAN 20 PSI D. SHUT DOWN THE LEFT ENGINE AND DIVERTED INTO MOB, WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. THE EL ECTRIC FEATHER SWITCH WAS USED TO FEATHER THE PROPELLER, AS THE PROP WOULD NOT FEATHER USING THE CONDITION LEVER. AS MA INTENANCE REMOVED AND REPLACED THE LEFT ENGINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1998112000954 19981120 00954 WP 1998 11 20 ORJA98266 1 19980923 A 5320 DOUBLER DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 AT OKC LEVEL 2 CORROSION, INTERGRANULAR CORROSION ON BARE METAL DOUBLER BETWEEN VHF ANTENNA AND INTERNAL FRAME. REMOVED AND FABRICATED NEW DOUBLER ON LOWER VHF ANTENNA IAW DOUGLAS DC-9, SRM 51-10-2. LEAK CHECKED IAW MD80, MM 21-00-00, NO DEFECTS. (M) 2 L 7 2 4F A6WE 1998112000955 19981120 00955 WP 1998 11 20 ORJA98235 1 19980818 A 5320 41186 FASTENERS DOUG DC9 DC982 3022082 WP BS 1190 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON AFT PIT BELLY DRAW MOUNT FASTENERS ON EACH SIDE OF STRINGER 30, STATION 1190 ARE CORRODED. REMOVED AND REPLACED FASTENERS IAW DC-9 SRM 51-30-2. (M) 2 L 7 2 4F A6WE 1998112000956 19981120 00956 WP 1998 11 20 ORJA98237 1 19980820 A 2560 GIRT BAR DOUG DC9 DC982 3022082 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON R1 DOOR GIRT BAR LOCK ATTACH CASTINGS FORWARD AND AFT. FABRICATED BAR LOCK ATTACH FITTINGS FROM 70 75 T6 BAR STOCK, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1998112000957 19981120 00957 WP 1998 11 20 ORJA98242 1 19980820 A 5210 P19526 VALVE DOUG DC9 DC982 3022082 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION R-1 DOOR DRAIN CHECK VALVE CORRODED AND STUCK CLOSED. REMOVED AND REPLACED R-1 DOOR DRAIN CHECK VALVE IAW MD-80 MM 20-10-13. OPS CHECK GOOD, C/W ON JOB CARD 9740/8000-008. (M) 2 L 7 2 4F A6WE 1998112000958 19981120 00958 WP 1998 11 20 ORJA98243 1 19980820 A 2120 591511243 BOLT DOUG DC9 DC982 3022082 WP A/C COMPT CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON LEFT AIR CONDITION FORWARD BOLTS 4 EACH ON HEAT EXCHANGER CORRODED. REMOVED AND REPLACED CORRODED HARDWARE IAW DOUGLAS MD-80 CMM CHAPTER 21 SECTION 21-21-07. (M) 2 L 7 2 4F A6WE 1998112000959 19981120 00959 WP 1998 11 20 ORJA98244 1 19980820 A 5313 MS21042L3 STRINGER DOUG DC9 DC982 3022082 WP BS 1211-1250 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 823RA 49889 LEVEL 2 CORROSION ON STRINGER 29R HI-LOCK NUTS BETWEEN STATION 1211 AND 1250. REMOVED AND REPLACED NUTS IAW DC-9 SRM 51 -30-1. (M) 2 L 7 2 4F A6WE 1998112000960 19981120 00960 EU 1998 11 20 PLGA980923A 1 19980923 A 2430 51539007A GCU SAAB SF340 SF340A 7850100 EU RT DC GEN FAILED A PLGA A UNSCHED LANDING O OTHER CR CRUISE 1 NE 05 342BE 4507 340A096 BGR - FLT 4253 - IN FLIGHT, THE RIGHT DC GENERATOR FAILED. AIRCRAFT DIVERTED TO BGR AND LANDED WITHOUT INCIDENT. MAINT ENANCE REPLACED THE RIGHT GCU, SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998112000961 19981120 00961 1998 11 20 PLGA980922A 4 19980922 A 3442 6227337001 R/T UNIT SAAB SF340 SF340A 7850100 EU E/E BAY FAILED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 334BE 1786 340A158 BOS - FLT 4430 - AFTER TAKEOFF, THE RADAR FAILED. AIRCRAFT RETURNED TO BOS DUE TO WEATHER CONDITIONS. MAINTENANCE REPL ACED THE RADAR RECEIVER/TRANSMITTER UNIT. SYSTEM TESTED GOOD. (M) 2 L 7 2 4T RT A52EU 1998112000962 19981120 00962 EU 1998 11 20 PLGA980920A 1 19980920 A 3340 MS332075 BREAKER SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A PLGA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 05 751BA 340A157 ALB - FLT 4243 - DURING TAXI TO THE GATE, THE CREW REPORTED THE SMELL OF SMOKE IN THE COCKPIT. THE SMOKE WAS COMING FRO M THE RIGHT SIDE CIRCUIT BREAKER PANEL. AIRCRAFT CONTINUED TO GATE AND PASSENGERS DE-PLANED WITHOUT INCIDENT. MAINTENA NCE FOUND THE CIRCUIT BREAKER FOR THE LOGO LIGHTS BURNED. THE CONNECTOR TO LOGO LIGHT HAD SHORTED AND BREAKER FAILED TO OPEN. SHORT WAS REPAIRED AND BREAKER REPLACED. (M) 2 L 7 2 4T RT A52EU 1998112000963 19981120 00963 EU 1998 11 20 98ZZZM867 1 19980603 A 4930 216362037 MANIFOLD BAG BAE146 BAE146300A 1500267 EU NR 1 ENGINE LEAKING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW 1232P E3122 NR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29. 2 H 7 4 4F RT A49EU 1998112000964 19981120 00964 EU 1998 11 20 98ZZZM868 1 19980603 A 4930 216362038 MANIFOLD BAG BAE146 BAE146300A 1500267 EU NR 1 ENGINE LEAKING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW 405011 E3122 NR 1 ENGINE FUEL LEAK AT BOTH MANIFOLDS AT START. REPLACED LEFT AND RIGHT FUEL MANIFOLDS, REF WORK CARD NR 29. 2 H 7 4 4F RT A49EU 1998112000965 19981120 00965 WP 1998 11 20 HALA9800339 1 19981009 A 4950 SEAL DOUG DC9 DC951 3022051 WP APU FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 669HA 47654 FLT 168 - HNL - TAIL TEMP HIGH LIGHT CAME ON DURING CLIMB-OUT. AIRCRAFT MADE AN UNEVENTFUL LANDING IN HNL. REPLACED RT PACK PERRY SEALS, RE-TORQUED ACM CLAMPS, RE-TORQUED APU LOAD CONTROL CLAMP. OPS CHECK, LEAK CHECK OK FOR SERVICE. (M) 2 L 7 2 4F RT A6WE 1998112000966 19981120 00966 WP 1998 11 20 HALA9800337 1 19981009 A 7931 TRANSMITTER DOUG DC9 DC951 3022051 WP NR 1 ENG FAILED A HALA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 13 699HA 47763 FLT 182 - HNL - LEFT ENGINE OIL PRESSURE INDICATOR DROPPED TO ZERO. LOW PRESSURE LOW LIGHT REMAINED EXTINGUISHED. OTHE R INDICATIONS NORMAL. A/C ABORTED TAKEOFF AND RETURNED TO BLOCKS. REPLACED NR 1 ENGINE OIL PRESSURE INDICATOR, PRESSUR E TRANSMITTER. OIL PRESSURE XMITTER GROUND LUG. CHECKED WIRING FROM XMITTER TO IND. GROUND RUNUP AT IDLE AND TAKEOFF, CHECKED GOOD. (M) 2 L 7 2 4F RT A6WE 1998112000967 19981120 00967 NM 1998 11 20 TSAA9833524 1 19980930 A 3350 BATTERY BOEING 737 7372Y5 1384554 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 810AL 24031 REPLACED BATTERY IN POSITION 6 FLOOR PROXIMITY LIGHT ASSY DUE TO INOP. OPS CHECK OK. (M) 2 L 7 2 4U RT A16WE 1998112000968 19981120 00968 EA 1998 11 20 MASA98187 1 19981010 A 3397 59465 WIRE CNDAIR CL600 CL6002B19 EA ROW 1/2 FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27185 7185 DURING PERFORMANCE OF TASK CARD 013-33-900-001, MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH FLOOR LIGHT SEGMENT BETWEEN ROWS 1 AND 2 IN THE CENTER AISLE FLOOR FAILED TO ILLUMINATE. INVESTIGATION REVEALED A BROKEN TRANSITION CABLE. MAINTEN ANCE REPLACED THE CABLE, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A21EA 1998112000969 19981120 00969 NM 1998 11 20 TSAA9833544 1 19980921 A 5320 DOOR FRAME BOEING 737 7372M6C 1384708 NM FUSELAGE CRACKED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 805AL 21809 AFT CARGO DOOR FRAME CRACKED. REPLACED AFT CARGO DOOR IAW BOEING MM 52-31-0. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998112000970 19981120 00970 NM 1998 11 20 TSAA9832540 1 19981007 A 3230 651781914 LOCK ACTUATOR BOEING 737 737230 NM NLG FAILED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 823AL 23154 FLT 31 - HNL-ITO - NOSE GEAR WOULD NTO RETRACT AFTER TAKEOFF. RETURNED TO LANDING CONFIGURATION AND CONFIRMED ALL GEARS DOWN AND LOCKED. RETURNED TO HNL. NORMAL LANDING. REMOVED AND REPLACED NOSE GEAR LOCK ACTUATOR IAW MM 32-33-21. LEA K AND OPS CHECK COMPLIED WITH. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998112000971 19981120 00971 NE 1998 11 20 TSAA9871478 2 19980828 A 7200 ENGINE BOEING 737 73725A 1384481 NM PWA JT8 JT8D9A 52048 NE NR 2 NACELLE FAILED A TSAA A UNSCHED LANDING R E PARTIAL RPM/PWR LOSS VIBRATION/BUFFET CL CLIMB 1 WP 13 819AL 23791 ON TAKEOFF FROM HNL, A LOUD BANG FROM NR 2 ENGINE WAS HEARD FOLLOWED BY LOSS OF THRUST AND ENGINE VIBRATIONS. REDUCED P OWER AND MADE SINGLE ENGINE LANDING AT HNL. ENGINE WAS NOT SHUT DOWN. REMOVED AND REPLACED NR 2 ENGINE. FOUND CONTAIN ED TURBINE FAILURE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT A16WE E2EA 1998112000972 19981120 00972 NM 1998 11 20 TSAA9827534 1 19980930 A 5753 1060516222223 BUSHING BOEING 737 7372X6C 1384552 NM TE FLAP WORN A TSAA O OTHER O OTHER LD LANDING 1 WP 13 817AL 23292 ON LANDING, AIRCRAFT ROLLS TO THE LEFT 30 DEGREES WITH GEAR DOWN AND FLAPS 15. REPLACED NR 1 AND NR 2 FLAP JACKSCREW GI MBAL BUSHINGS. GROUND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998112000973 19981120 00973 NM 1998 11 20 TSAA9832533 1 19981003 A 3260 806002 PROXIMITY SWITCH BOEING 737 737230C 1384472 NM RT MLG MALFUNCTIONED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 820AL 22138 FLT 80 - HNL-KOA - RIGHT MAIN GEAR UNSAFE. RED LIGHT REMAINED ILLUMINATED AFTER GEAR UP. RETURNED TO HNL. PERFORMED L ANDING GEAR EXTENSION/RETRACTION TEST. NO DISCREPANCIES. MEASURED AND FOUND UPLOCK SENSOR GAP TO BE WITHIN TOLERANCES IN MM CHAPTER 32-61-21. REPLACED RT MLG UPLOCK PROXIMITY SWITCH AND MLG RED LIGHT PC CARD FOR T/S PURPOSES AND PRECAUTI ONARY REASONS. (M) 2 L 7 2 4F A16WE 1998112000974 19981120 00974 NM 1998 11 20 98ZZZM869 1 19981003 A 3260 655825029 LOGIC CARD BOEING 737 737230C 1384472 NM RT MLG MALFUNCTIONED A TSAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 820AL 22138 FLT 80 - HNL-KOA - RIGHT MAIN GEAR UNSAFE. RED LIGHT REMAINED ILLUMINATED AFTER GEAR UP. RETURNED TO HNL. PERFORMED L ANDING GEAR EXTENSION/RETRACTION TEST. NO DISCREPANCIES. MEASURED AND FOUND UPLOCK SENSOR GAP TO BE WITHIN TOLERANCES IN MM CHAPTER 32-61-21. REPLACED RT MLG UPLOCK PROXIMITY SWITCH AND MLG RED LIGHT PC CARD FOR T/S PURPOSES AND PRECAUTI ONARY REASONS. (M) 2 L 7 2 4F A16WE 1998112000975 19981120 00975 1998 11 20 UF6A980908 4 19980920 A 3444 9650576020 GPWS BAG ATP ATP EU E/E BAY FAILED A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 852AW 12964 2047 2021 ORD - FLT 5753 - ATTENTION GETTERS AND CHIRPERS ILLUMINATE AND SOUND WHEN POWER LEVERS ADVANCED FOR TAKEOFF. NO CWP'S. MAINTENANCE REMOVED AND REPLACED GPWS COMPUTER. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A27NM 1998112000976 19981120 00976 EU 1998 11 20 SIMA982745 1 19981001 A 3150 005WS00 WEU SAAB SF340 340B 7860101 EU E/E BAY MALFUNCTIONED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 263AE 1031 340B263 CLL - FLT 3794 - WHEN POWER WAS APPLIED FOR TAKEOFF, CONFIGURATION WARNING LIGHT ON CWP ILLUMINATED. CREW RESET WEU, PR OBLEM CONTINUED. AIRCRAFT RETURNED TO GATE. MAINTENANCE REMOVED AND REPLACED THE WEU. OPERATIONAL CHECK GOOD. AIRCRA FT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112000977 19981120 00977 NM 1998 11 20 PCAA9800782 1 19980906 A 3260 UNSAFE LIGHT DHAV DHC8 DHC8102 2809003 NM NLG ILLUMINATED A PCAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 13 822EX 187 DURING TAKEOFF AT ROTATION, RED NOSE GEAR UNSAFE LIGHT AND UNSAFE HANDLE LIGHTS ILLUMINATED, UNSAFE LIGHTS WENT OUT ONCE AIRBORNE. AIRCRAFT RETURNED TO FIELD IN MDT. MAINTENANCE TROUBLESHOT SYSTEM, CHECKED PSEU FOR FAULTS, NONE FOUND. IN SPECTED NLG PROXIMITY SWITCHES AND WIRING, NO DEFECTS FOUND. PERFORMED RETRACTION TEST, NO DEFECTS NOTED. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998112000978 19981120 00978 NM 1998 11 20 PCAA9800786 1 19980920 A 2432 20412 BATTERY DHAV DHC8 DHC8102 2809003 NM E/E BAY OVERTEMP A PCAA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION NR NOT REPORTED 1 EA 13 815EX 15134 321 DURING FLIGHT, THE MAIN BATTERY HOT LIGHT ILLUMINATED THE AIRCRAFT DIVERTED INTO MDT AND LANDED WITHOUT INCIDENT. MAINT ENANCE FOUND THE MAIN BATTERY AT FAULT. REMOVED AND REPLACED MAIN BATTERY IAW DHC PROCEDURES, OPERATIONAL AND TEMPERATU RE CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998112000979 19981120 00979 NM 1998 11 20 PCAA9800785 1 19980916 A 2611 3023143 SMOKE DETECTOR DHAV DHC8 DHC8102 2809003 NM CARGO BAY MALFUNCTIONED A PCAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 13 827EX 390 SMOKE WARNING LIGHT ILLUMINATED IN FLIGHT. NO SMOKE OR FIRE DETECTED. AIRCRAFT DIVERTED INTO UCA. INSPECTED CARGO BAY FOR EVIDENCE OF SMOKE/FIRE. NO DEFECTS NOTED. ELECTRICALLY DISABLED NR 1 AND NR 2 CARGO BAY SMOKE DETECTORS. AIRCRAF T DISPATCHED UNDER MEL RELIEF. SUBSEQUENTLY, MAINTENANCE REPLACED THE FORWARD AND AFT SMOKE DETECTORS. OPERATIONAL CHE CKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998112000980 19981120 00980 NM 1998 11 20 PCAA9800784 1 19980915 A 2432 20413 AUX BATTERY DHAV DHC8 DHC8102 2809003 NM E/E BAY MALFUNCTIONED A PCAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 13 806EX 263 AFTER TAKEOFF FROM PHL, THE AUXILLARY BATTERY TEMPERATURE WENT INTO THE CAUTION RANGE. THE BATTERY REMAINED HOT WITH TH E SWITCH IN THE OFF POSITION. INDICATION WAS IN THE MID SCALE AREA WITH NO ASSOCIATED HOT LIGHT. MAINTENANCE REMOVED A ND REPLACED THE AUXILLARY BATTERY IAW DHC PROCEDURES. VOLTAGE AND TEMPERATURE CHECKED GOOD. AIRCRAFT RETURNED TO SERVI CE. (M) 2 H 7 2 4T RT A13NM 1998112000981 19981120 00981 NM 1998 11 20 PCAA9800783 1 19980909 A 7931 TRANSMITTER DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE FAILED A PCAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 13 828EX 392 AFTER TAKEOFF FROM SYR, THE NR 2 ENGINE OIL PRESSURE INDICATED 100 PSI. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT I NCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, REPLACED WIRING FROM 9811-J29 TO OIL PRESSURE TRANSMITTER. REMOVED AND REPLAC ED NR 2 OIL PRESSURE TRANSMITTER, IAW DHC AND PWC PROCEDURES. RUN AND LEAK CHECK PROVED SATISFACTORY. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998112000982 19981120 00982 EU 1998 11 20 RAIA981011 1 19981016 A 7712 31024766 TSCU BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 426AM 15798 874 FLT 7436 - STL - RIGHT ENGINE TTL CAUSING FUEL TO BYPASS. MAINTENANCE RECALIBRATED TORQUE SIGNAL CONDITIONER. (M) 2 L 7 2 4T RT A56EU 1998112000983 19981120 00983 EU 1998 11 20 RAIA981010 1 19981018 A 2425 7004544712 SYMBOL GENERATOR AEROSP ATR72 ATR72202 8680940 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 721TE 14708 217 FLT 7011 - STL - CAPTAINS EFIS TUBES FAILED. MAINTENANCE REPLACED CAPTAINS SYMBOL GENERATOR. (M) 2 H 7 2 4T RT A53EU 1998112000984 19981120 00984 EU 1998 11 20 RAIA981004 1 19981002 A 7712 310703411 TORQUE RING BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CR CRUISE 1 CE 03 427AM 11902 876 FLT 7394 - STL - RIGHT ENGINE BYPASSING FUEL WITH TTL ON. MAINTENANCE REPLACED TORQUE RING IN GEAR BOX. (M) 2 L 7 2 4T RT A56EU 1998112000985 19981120 00985 WP 1998 11 20 RAIA981009 2 19981015 A 7320 31081961 P3 GASKET BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP LT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 423AM 858 66298 FLT 7395 - MWA - LEFT ENGINE TORQUE DROPPED TO 95 PERCENT ON TAKEOFF, TARGET WAS 100 PERCENT. MAINTENANCE REPLACED P-3 GASKET ON LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998112000986 19981120 00986 WP 1998 11 20 USAAD98180 1 19981011 A 5240 991158722 LATCH DOUG DC9 DC982 3022082 WP SERVICE DOOR LOOSE A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 815US 48095 BOS-CLT - FLT 1524 - ON ROTATION, THE ARICRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITH OUT INCIDENT. MAINTENANCE FOUND THE FORWARD 2 ACCESSORY HATCH LOCK ARMS UNSNAPPED. THE LOCKS WERE SECURED AND ALL CHEC KED NORMAL. (M) 2 L 7 2 4F A6WE 1998112000987 19981120 00987 EU 1998 11 20 UF6A980910 1 19980927 A 3150 CAWS BAG ATP ATP EU COCKPIT MALFUNCTIONED A UF6A C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 GL 31 852AW 2021 ORD - FLT 5759 - ATTENTION GETTER, BOTH AUDIBLE AND VISUAL, ILLUMINATED DURING TAKEOFF ROLL WITH POWER LEVERS ADVANCED. MAINTENANCE PERFORMED OPS CHECK OF GPWS SYSTEM AND PERFORMED ENGINE RUNS. NO DEFECTS NOTED. (M) 2 L 7 2 4T RT A27NM 1998112000988 19981120 00988 EU 1998 11 20 PIVA12211 1 19981022 A 2600 21562B SMOKE DETECTORS STBROS SD3 SD360 8100606 EU CARGO BAY MALFUNCTIONED A PIVA F A ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 13 711PM SH3715 AFT CARGO SMOKE DETECTOR WARNING CAME ON DURING CLIMB-OUT. OCCURED TWICE, ONCE OUT OF SAIPAN AND ONCE OUT OF GUAM. THE AIRCRAFT RETURNED TO FIELD BOTH TIMES. THERE WAS NO FIRE FIGHTER TIME. THE AIRCRAFT WAS FERRIED TO SIAPAN FROM GUAM A FTER THE SECOND OCCURENCE DUE TO FIRE EXTINGUISHERS DISCHARGED. (M) 2 H 7 2 4T A41EU 1998112000989 19981120 00989 NE 1998 11 20 MZZA98210 2 19981024 A 7200 ENGINE BOEING 727 727227 1384078 NM PWA JT8 JT8D17 52049 NE NR 3 NACELLE FAILED A MZZA O OTHER E VIBRATION/BUFFET DE DESCENT 1 WP 13 89427 21365 TKK - FLT 957 - NR 3 ENGINE WITH HEAVY VIBRATION. MAINTENANCE FOUND TURBINE BLADES MISSING IN EXHAUST SECTION. MAINTEN ANCE REMOVED AND REPLACED NR 3 ENGINE PER WORKCARD 07-7100-1-8001. OPS AND LEAK CHECK COMPLIED WITH, NO LEAKS NOTED. P OWER ASSURANCE RUN COMPLIED WITH PER WORKCARD 07-7100--1-7001. CHECK NORMAL AND RELEASED AIRCRAFT FOR SERVICE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998112000990 19981120 00990 WP 1998 11 20 HALA9800342 1 19981010 A 3260 PROXIMITY BOX DOUG DC10 DC1010 3022110 WP NLG FAILED A HALA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 153AA 46708 PDX - FLT 25 - NOSE GEAR UNSAFE LIGHT ILLUMINATED DURING CLIMB AT 20,000 FT VISUAL INSPECTION OF VIEWING PORT REVEALED N OTHING OBVIOUS. LIGHT EXTINGUISHED AT 26,000 FT AND DID NOT RE-ILLUMINATE. INSPECTED NLG PROX SWITCHES CONDITION AND S ECURITY CHECK OK. REPLACED PROXIMITY BOX, BITE CHECK OK. OK FOR SERVICE. (M) 2 L 7 3 4F A22WE 1998112001001 19981120 01001 NE 1998 11 20 98ZZZX4193 2 19980903 A 7200 ENGINE CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE RT NACELLE MALFUNCTIONED A ISYA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 25 84EA 6413 2914 5500484 PCE71369 PILOT REPORTED HOT OIL SMELL COMING FROM OVERHEAD VENTS DURING POSITIONING FLIGHT FOR MAINTENANCE. TROUBLESHOOTING SHOW ED SMELL COMING FROM RIGHT ENGINE. 1 L 7 2 4F 4 F A22CE E1NE 1998112001031 19981120 01031 WP 1998 11 20 TWAA9818501 1 19981111 A 5220 PAN DOUG DC9 DC931 3022065 WP EMER EXIT DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 DURING CHECK-C MAINT, FOUND LT FWD EMERGENCY EXIT DOOR WITH A ONE INCH CRACK IN AFT UPPER CORNER, AND 1 INCH CRACK IN LO WER AFT CORNER. REMOVED AND REPLACED PAN PER SRM 51-30. 2 L 7 2 4F A6WE 1998112001032 19981120 01032 WP 1998 11 20 TWAA9818502 1 19981111 A 5220 PAN DOUG DC9 DC931 3022065 WP EMER EXIT DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 DURING CHECK-C MAINT, FOUND RT FWD EMERGENCY EXIT DOOR WITH TWO 1 INCH PAN CRACKS IN DOOR CORNERS. REPLACED DOOR PAN PE R SRM 51-30 STANDARD PRACTICES ON SHOP TICKET 836533. 2 L 7 2 4F A6WE 1998112001033 19981120 01033 WP 1998 11 20 TWAA9818503 1 19981111 A 5220 PAN DOUG DC9 DC931 3022065 WP EMER EXIT DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 977Z 47249 DURING CHECK-C MAINT, THE LT AFT EMERGENCY EXIT DOOR HAD TWO 1 INCH CRACKS IN DOOR PAN IN BOTH CORNERS. REPAIRED PAN PE R DC9 SRM 51-00 STANDARD PROCEDURES. 2 L 7 2 4F A6WE 1998112001034 19981120 01034 1998 11 20 VJ9800593 2 19981116 A 7321 74B6025 FUEL CONTROL BOEING 737 7372T4 1384492 NM RT ENGINE FAILED A ZZDA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SO 15 467AT 22055 ON CLIMBOUT, LOST POWER ON NR 2 ENGINE. FLIGHT CREW SHUTDOWN ENGINE AND DIVERTED TO SAV. REPLACED DEFECTIVE FUEL CONTR OL. 2 L 7 2 4F A16WE 1998112001035 19981120 01035 WP 1998 11 20 VJ9800594 1 19981116 A 3241 284702 VALVE DOUG DC9 DC932 3022066 WP ANTI-SKID SYST FAILED A ZZDA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 15 933VV 47489 DURING INITIAL TAKEOFF ROLL AT APPROXIMATELY 40 KNOTS, FLIGHT CREW RECEIVED A MASTER CAUTION WARNING. FLIGHT CREW APPLI ED BRAKES WITH ANTISKID SYSTEM ON AND THERE WAS NO BRAKE PRESSURE. TURNED ANTISKID SYSTEM OFF AND BRAKE PRESSURE WAS AV AILABLE. AIRCRAFT STOPPED AND RETURNED TO GATE. REPLACED BRAKE VALVE IAW MM 32-42, OPS CHECKED OK. 2 L 7 2 4F A6WE 1998112001036 19981120 01036 WP 1998 11 20 VJ9800595 1 19981022 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 464-486 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 A NON-CONFORMING REPAIR FOUND AT FS 464 TO 486, LBL 4.5 AND RBL 4.5. REMOVED ANTENNA DOUBLER, STOP DRILLED CRACKS, FABR ICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 53-01 FIG 1, 53-04 FIG 3B, 51-10-3, 51-10-4, 51-30-2 AND DOUG LAS DRAWING SRO 9530005. 2 L 7 2 4F A6WE 1998112001037 19981120 01037 NM 1998 11 20 CALA9802066 1 19981114 A 5330 SKIN BOEING 747 747238B 1384828 NM BS 1997 DAMAGED A CALA K NONE C F.O.D. IN INSP/MAINT 1 SW 09 17025 20535 THE LOWER FUSELAGE BELLY SKIN WAS FOUND TO BE PUNCTURED BY GROUND EQUIPMENT AT STA 1997. THE PUNCTURED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 19, 53-10-3, FIGURE 1 AND 51-40-4, FIGURE 2. 2 L 7 4 4F A20WE 1998112001038 19981120 01038 NM 1998 11 20 CALA9802067 1 19981116 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 328 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND FLOORBEAM CORRODED AT BS 328, LBL 50 TO RBL 50. THE CORRODED AREA WAS REMOVED AND AN UPPER CHORD REPAI R SPLICE WAS INSTALLED IAW SRM 53-10-51. 2 L 7 2 4F RT A16WE 1998112001039 19981120 01039 NM 1998 11 20 CALA9802068 1 19981117 A 5330 SKIN BOEING 727 727232 1384082 NM BS 1191 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 59792 20646 INSPECTION FOUND LT FUSELAGE SKIN BULGED JUST BELOW AND AFT OF LAV SERVICE PANEL CUTOUT AREA AT BS 1191, S21L TO S22L. T HE AREA WAS REPAIRED IAW SRM 53-30-3 AND BOEING SERVICE BULLETIN 727-0550048. 2 L 7 3 4F A3WE 1998112001040 19981120 01040 NM 1998 11 20 CALA9802069 1 19981117 A 5754 65162241 SKIN BOEING 727 727232 1384082 NM NR 1 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND A 4 INCH CRACK IN SKIN AT AFT FACE OF LT WING NR 1 SLAT, INBOARD OF INBOARD TRACK AREA. THE NR 1 LE SL AT WAS REMOVED AND REPLACED IAW MM 27-81-11. 2 L 7 3 4F A3WE 1998112001041 19981120 01041 NM 1998 11 20 CALA9802070 1 19981117 A 5754 SKIN BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND TWO 1 INCH CRACKS AT SCREW HOLE TO RIVET HOLES OF NR 2 SLAT UPPER TRAILING EDGE WHERE I/B HOOK MOUNTS. THE FASTENERS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2, PAGE 3 AND 57-50-3, PAGES 27-28. 2 L 7 3 4F A3WE 1998112001042 19981120 01042 NM 1998 11 20 CALA9802071 1 19981117 A 5753 PLATE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND A 1 INCH CRACK IN PLATE AT RT INBOARD MIDFLAP ABOVE AFT END OF NR 5 SPINDLE. THE PLATE WAS REMOVED IAW SRM 51-30-2, PAGE 4. A NEW PLATE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2, PAGE 1. 2 L 7 3 4F A3WE 1998112001043 19981120 01043 EA 1998 11 20 COMA9860349 1 19981115 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 EA RT COCKPIT SHATTERED A COMA B EMER. DESCENT O OTHER CR CRUISE 1 SO 01 917CA 604 7017 CO-PILOTS SIDE WINDSHIELD SHATTERED. REPLACED WINDOW. 2 L 7 2 4F RT A21EA 1998112001044 19981120 01044 NM 1998 11 20 UPS98228169 1 19981104 A 5311 FRAME BOEING 727 72762C 138402C NM BS 825.95 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE-C DURING NDT INSPECTION, CRACK FOUND EMANATING FROM FOURTH FASTENER HOLE ABOVE FLOOR LINE AT BS 825.95 R T. REPAIRED IAW APPENDIX C OF EO B727-5310-5474. 2 L 7 3 4F A3WE 1998112001045 19981120 01045 NM 1998 11 20 UPS98228170 1 19981117 A 3350 1684 BULB BOEING 727 727185C 138406N NM CABIN FAILED A IPXA K NONE L NO TEST NR NOT REPORTED 1 SO 01 954UP 19827 INSPECTION TYPE-N/A, EMER EXIT LIGHTS UNARMED LIGHT DOES NOT PRESS TO TEST OR ILLUMINATE AT ALL. ARMED/UNARMED LIGHT RE LAMPED WITH A 1684 BULB AND OPS CHECKED SERVICEABLE. 2 L 7 3 4F A3WE 1998112001046 19981120 01046 EU 1998 11 20 QXEA9801686 1 19981113 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 486US 2447 11237 MAINTENANCE REPORTS FORWARD EMERGENCY POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED SAME, OPERATIONAL TEST SHOWS NORMA L FUNCTION. 2 L 7 2 4F RT A20EU 1998112001047 19981120 01047 NM 1998 11 20 QXEA9801687 1 19981113 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOP A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 357PH 2207 504 TWO RED EMERGENCY FLOOR LIGHTS IN THE FRONT OF THE CABIN ARE INOP. REPLACED BATTERY POWER SUPPLY, OPERATIONAL CHECKS GO OD. 2 H 7 2 4T RT A13NM 1998112001048 19981120 01048 WP 1998 11 20 ABXA9801060 1 19981112 A 5610 5613217508 WINDOW DOUG DC8 DC861 3021952 WP RT COCKPIT OUT OF ADJUST A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 848AX 46032 FIRST OFFICER'S WINDOW WOULD NOT OPEN. ADJUSTED LOWER AFT LINKAGE ROD IAW DC-8 MM 56-10-3, OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998112001049 19981120 01049 WP 1998 11 20 MWEA981067 1 19981116 A 5313 2777922 LONGERON DOUG DC9 DC915 3022036 WP BS 218 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LONGERON 29L AT FUSELAGE STATION 218 HAS ELONGATED HOLES. REMOVED DAMAGED SECTION OF LONGERON FABRICATED NEW SECTION OF LONGERON AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 1998112001050 19981120 01050 NM 1998 11 20 DL72S982315 1 19980930 A 5753 652163234 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP REPAIRED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED AT 2 PLACES APPROX 34 INCHES FROM I/B END OF FLAP. THE AN GLE WAS REPAIRED PER MM 57-52-00, FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER. 2 L 7 3 4F A3WE 1998112001051 19981120 01051 NM 1998 11 20 DL72S982316 1 19980930 A 5753 652163234 SKIN BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 DURING SHOP INSPECTION, THE COVE SKIN WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE SKIN WAS REPAIRED PER MM 57 -52-0, FIG 809 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998112001052 19981120 01052 WP 1998 11 20 DLL14982317 1 19981110 A 2430 LS1015825 CIRCUIT BREAKER LKHEED 1011 1011385115 5265015 WP COCKPIT SHORTED A DALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 SO 27 740DA 193C1244 NEAR TOP OF DESCENT, ELECTRICAL SPARKING AND ARCING BELOW DC STANDBY POWER CIRCUIT BREAKER. WHITE IN COLOR FOLLOWED BY ELECTRICAL SMELLING SMOKE AND RED GLOW OF HOT METAL/FIRE, BEHIND AND BELOW CIRCUIT BREAKER NUMBER 3F1. APPLIED HALON E XTINGUISHER TO GLOWING AREA AND GLOW WENT OUT. MULTIPLE SYSTEM FAILURES ENSUED. FOUND WIRE BUNDLE CLAMP SHORTED AGAINS T STANDBY DC POWER CIRCUIT BREAKER TERMINAL. ADDITIONAL SYSTEM FAILURES RELATED TO DC STANDBY RELAY. REPLACED CLAMP A ND BREAKER AND CHECKED ALL SYSTEMS INVOLVED. 2 L 7 3 4F A23WE 1998112001053 19981120 01053 NM 1998 11 20 DL72S982318 1 19980930 A 5753 652163234 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 407DA 21151 DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 18 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PE R MM 57-52-0 FIG 802 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A SPLICE DOUBLER. 2 L 7 3 4F A3WE 1998112001054 19981120 01054 NM 1998 11 20 DL72S982319 1 19980921 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 33 INCHES FROM O/B END OF FLAP. THE ANGLE WAS REPAIRED PE R MM 57-52-0 BY REPLACING A SECTION OF THE ANGLE AND INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998112001055 19981120 01055 NM 1998 11 20 DL72S982320 1 19980921 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM TR TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 DURING SHOP INSP, THE AFT CHORD ANGLE WAS FOUND CRACKED 33 INCHES FROM IB END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57 -52-0, FIG 809 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998112001056 19981120 01056 NM 1998 11 20 DL72S982321 1 19980921 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 409DA 21153 DURING SHOP INSPECTION, THE AFT CHORD ANGLE WAS FOUND CRACKED 34 INCHES FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1998112001057 19981120 01057 NM 1998 11 20 DL72S982322 1 19981110 A 5753 SKIN BOEING 727 727232 1384082 NM LT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 A .375 INCH CRACK AT NR 2 MIDFLAP LOWER SURFACE AT CUTOUT I/B OF NR 4 MIDFLAP FAIRING. REPAIRED PER M/M 57-52-0. 2 L 7 3 4F A3WE 1998112001058 19981120 01058 NM 1998 11 20 DL72S982323 1 19981110 A 5754 BRACKET BOEING 727 727232 1384082 NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 NR 6 L/E FLAP ACT ATTACH BRACKET CRACKED AT UPPER AND LWR ENDS. REPAIRED PER M/M 57-20-21 FIG 807. 2 L 7 3 4F A3WE 1998112001059 19981120 01059 NM 1998 11 20 DL72S982324 1 19981110 A 5720 ANGLE BOEING 727 727232 1384082 NM WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 494DA 21074 LWR CHORD ANGLE 1 INCH CRACK AT FWD END BELOW NR 8 SPOILER ACTUATOR. REPAIRED PER M/M 57-20-22 FIG 806. 2 L 7 3 4F A3WE 1998112001060 19981120 01060 WP 1998 11 20 DLL14982328 1 19981111 A 3350 POWER SUPPLY RPS1 LKHEED 1011 1011385115 5265015 WP CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1739D 1156 193C1237 EMERGENCY LIGHTS ON ALL THE TIME IN FIRST/BUSINESS. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998112001061 19981120 01061 NM 1998 11 20 DL72S982329 1 19981111 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 402DA 21146 FOUND AT LETTER CK B-2, AFT ENTRY DOOR CUTOUT LT FRAME HAS .3125 INCH VISIBLE CRACK 6 INCHES BELOW UPPER STOP CASTING. R EPAIRED PER SRM 53-10-8. 2 L 7 3 4F A3WE 1998112001062 19981120 01062 NM 1998 11 20 DLM88982332 1 19981111 A 2170 V1211 COALESCER BAGS DOUG MD88 MD88 3023688 NM CABIN DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 973DL 53241 ON INITIAL CLIMBOUT, A STRONG SMOKEY SMELL WAS NOTICED IN THE BACK OF THE A/C AND IN THE COCKPIT. SMELL STABILIZED AS C LIMB CONTINUED BUT DID NOT CLEAR UNTIL DESCENT BACK INTO ATLANTA. PERFORMED DUCT BURNOUT PER M/M AND REPLACED COALESCER BAGS. RAN BOTH ENGS TO T/O POWER WITH BOTH PACKS OPERATING. NO EVIDENCE OF SMOKE OR SMOKE SMELL. 2 L 7 2 4F RT A6WE 1998112001063 19981120 01063 NM 1998 11 20 DL76L982333 1 19981111 A 2120 AIR DIST BOEING 767 767332 1382001 NM CABIN ODOR A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 SO 27 172DN 24775 FLT ATTENDANT REPORTS, AN ODOR OF SMOKE ON LANDING IN AFT PART OF AIRCRAFT. CLEANED ALL OVENS IN AFT GALLEY, RAN OVENS FOR 45 MINUTES, OPERATED BOTH AIR CONDITIONING PACKS FOR 30 MINUTES AND COULD NOT DETECT SMOKE OR BURNT ODOR IN CABIN. 2 L 7 2 4F RT A1NM 1998112001064 19981120 01064 NM 1998 11 20 DL72W982334 1 19981106 A 5320 FRAME BOEING 727 727247 138408F NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 A .5 INCH VISIBLE CRACK AT AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER DOOR STOP. REPAIRED PER SRM 53-10-09. 2 L 7 3 4F A3WE 1998112001065 19981120 01065 NM 1998 11 20 DL72W982335 1 19981106 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 1050 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FOUND DURING MV2 CORROSION VISIT NRC 81, CORROSION ON FLOORBEAM STA 1050 AT RBL 33. REPAIRED PER M/M 53-20-11 FIG 804A RBL 33 TO RBL 19. 2 L 7 3 4F A3WE 1998112001066 19981120 01066 NM 1998 11 20 DL72E982336 1 19981112 A 5320 CHORD BOEING 727 727247 138408F NM BS 1342 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 FOUND ON F2 LETTER CK, 1 INCH CRACK IN STA 1342 CHORD ABOVE THE NUMBER 2 ENGINE S-DUCT. STOP DRILLED CRACK PER MM 53-11 -0. 2 L 7 3 4F A3WE 1998112001067 19981120 01067 NM 1998 11 20 DL72E982337 1 19981112 A 5754 ANGLE BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 831WA 21483 NR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER M/M 57-54-0 PG 816. 2 L 7 3 4F A3WE 1998112001068 19981120 01068 NM 1998 11 20 DL72W982338 1 19981113 A 3350 BATTERY PACK 900835A BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2820W T4265 21058 ON S/C, FOUND RT OVERWING EMER LIGHT INOP. FOUND BATT PACK INOP. REPLACED SAME. 2 L 7 3 4F A3WE 1998112001069 19981120 01069 NM 1998 11 20 DL72S982339 1 19981112 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 468DA 5666 20745 RIGHT AFT OVERWING EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998112001070 19981120 01070 NM 1998 11 20 DL72S982341 1 19981112 A 5754 STOP BOEING 727 727232 1384082 NM 6-7 & 8 LE SLAT LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 519DA 21470 DURING INSPECTION PER REQUIREMENTS OF AD 94-07-08, LOOSE SLAT STOP ATTACH BOLTS WERE FOUND LOOSE FOR THE NR 6, 7 & 8 SLA TS. EACH OF THESE SLAT LOCATIONS WERE MODIFIED PER THE REQUIREMENTS OF BAC S/B 727-57-171. THE MODIFICATION WAS DOCUME NTED PER ER/A 366092-14AD. 2 L 7 3 4F A3WE 1998112001071 19981120 01071 NM 1998 11 20 DLM88982342 1 19981113 A 4920 BEARING DOUG MD88 MD88 3023688 NM APU FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 905DL 7747 49536 000000 DURING CLIMBOUT, AFT LAV SMOKE DETECTOR SOUNDED AND SMOKE AND ODOR DETECTED BY FLT. ATTENDENTS. AIRCRAFT RETURNED TO YU L. CONTRACT MTC FOUND OIL LEAKING FROM APU INLET, SUBMITTER SUSPECTS BEARING FAILURE. MTC IN PROCESS OF CLEANING APU C OMPARTMENT CHANGING WATER SEPARATOR BAGS AND DUCT BURNOUT. 2 L 7 2 4F RT A6WE 1998112001072 19981120 01072 NM 1998 11 20 DL72W982343 1 19981111 A 5320 65562312 STRAP BOEING 727 727247 138408F NM R1 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 000000 THE R2 DOOR SURROUND BEAR STRAP WAS FOUND WITH A TYPICAL CRACK AT THE UPPER HINGE CUTOUT. THE CRACK WAS APPROX 2 INCHES LONG AND CONFINED TO THE BEAR STRAP ONLY. THE CRACK WAS REPAIRED WITH AN EXTERNAL DOUBLER PER BAC S/B 727-53-0136 & DOCUMENTED PER ER/A 366075-14. 2 L 7 3 4F A3WE 1998112001073 19981120 01073 NM 1998 11 20 DL767982344 1 19981111 A 5754 114T310021A WEDGE BOEING 767 767232 1385132 NM NR 6 LE SLAT DELAMINATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 106DA 22218 000000 THE UPPER SKIN OF THE TRAILING EDGE WEDGE ON THE NR 6 SLAT WAS FOUND WITH A 5 X 4 AREA OF DELAMINATION APPROXIMATELY 62 INCHES FROM THE O/B EDGE OF THE SLAT. THE DAMAGE WAS TRIMMED AWAY AND REPAIRED PER THE B767 SRM 51-70-10 AND DOCUMENTED PER ER/A 366072-14AD. 2 L 7 2 4F RT A1NM 1998112001074 19981120 01074 NM 1998 11 20 DLM88982345 1 19981113 A 2120 AIR DIST 4110001137 DOUG MD88 MD88 3023688 NM GALLEY SMOKE A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 910DL 49541 ON CLIMBOUT, THE FLT ATTENDANTS REPORTED SMOKE IN THE FWD GALLEY AND THE FLOOR WAS UNUSUALLY WARM. FOUND THE COFFEEMAKE R CIRCUIT BREAKERS HAD POPPED. FLIGHT RETURNED TO MLB. CONTRACT INSPECTED THE A/C FOR EVIDENCE OF OVERHEATING UND ER THE GALLEY FLOOR. FWD GALLEY INOPED FOR FLT TO ATL. OVERWEIGHT INSPECTION C/W PER M/M, NO TROUBLE FOUND. 2 L 7 2 4F RT A6WE 1998112001075 19981120 01075 NM 1998 11 20 DLM88982346 1 19981113 A 4930 38760354 SENSOR DOUG MD88 MD88 3023688 NM APU FAILED A DALA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 27 948DL 6493 49879 080143 AT V1, APU FLAMED OUT 122 KNOTS AND ELECTRICAL LOAD WAS PICKED UP BY RIGHT ENGINE ONLY. DID NOT ATTEMPT TO RESTART APU. RETURNED TO DFW. REPLACED PS SENSOR AND SET APU FOR VERIFICATION FLIGHT. 2 L 7 2 4F RT A6WE 1998112001076 19981120 01076 NM 1998 11 20 DL72W982347 1 19981022 A 5753 652163234 ANGLE BOEING 727 727247 138408F NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2815W 20871 080143 DURING SHOP INSP, THE LOWER AFT CHORD ANGLE WAS FOUND CRACKED 33 AND 36.5 INCHES FROM I/B END OF FLAP. THE ANGLE WAS RE PAIRED PER MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998112001077 19981120 01077 NM 1998 11 20 DL73S982349 1 19981113 A 3350 BATTERY PACK BPS73 BOEING 737 737232 1384475 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 323DL 5470 23095 THE 4 AFT EMERGENCY PATHWAY LIGHTS INOP. REPLACED BATTERY PACK. 2 L 7 2 4F RT A16WE 1998112001078 19981120 01078 NM 1998 11 20 DL72L982350 1 19981114 A 3350 LIGHT 1102833 BOEING 727 727232 1384082 NM ROW 13 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 507DA 10672 21309 L-1 AND FWD AISLE AREA EMERGENCY LIGHTS INOP. REPLACED BATTERIES IN THE L-1 DOOR POS AND REPLACED LIGHT ASSY FOR THE FW D AISLE EMERGENCY LIGHT. 2 L 7 3 4F A3WE 1998112001079 19981120 01079 NM 1998 11 20 DLM88982351 1 19981113 A 2120 AIR DIST DOUG MD88 MD88 3023688 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 910DL 49541 SMOKE SMELL IN FWD GALLEY/FWD CABIN AFTER TAKEOFF. NO VISIBLE SMOKE OR FIRE, DIVERT TO MCO. MTC INSPECTED A/C DUCTS, R ECIRC FAN AND FILTER. ALSO, REPLACED A/C WATER SEPARATOR COALESCER BAGS AND LEFT WATER SEPARATOR. CHECKED VALVE, RAN E NGS AT HI POWER OFF GATE WITH FLT CREW AND FOUND RT A/C SYS WITH SLIGHT OILY SMELL IN AIR FWD RT A/C SYS TO MCO. PLAC PER MEL. 2 L 7 2 4F RT A6WE 1998112001080 19981120 01080 NM 1998 11 20 DL72S982353 1 19981114 A 2560 MEGAPHONE MV10 BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 527DA 21587 MEGAPHONE INOP. REPLACED MEGAPHONE. 2 L 7 3 4F A3WE 1998112001081 19981120 01081 NM 1998 11 20 DL72S982354 1 19981114 A 3350 BATTERY BOEING 727 727232 1384082 NM GALLEY DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 482DA 20862 AFT GALLEY DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998112001082 19981120 01082 NM 1998 11 20 DL72S982355 1 19981114 A 3350 BATTERY PACK 900542 BOEING 727 727232 1384082 NM SERVICE DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 482DA T3993 20862 AFT SERVIVCE DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY RACK. 2 L 7 3 4F A3WE 1998112001083 19981120 01083 NM 1998 11 20 DL72K982356 1 19981114 A 3350 POWER SUPPLY RPS1 BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 491DA 1502 21060 FWD FLOOR EMERG LIGHTS INOP. REPLACED POWER SUPPLY. 2 L 7 3 4F A3WE 1998112001084 19981120 01084 NM 1998 11 20 DL72L982358 1 19981114 A 3350 BATTERY 37067001 BOEING 727 727232 1384082 NM AFT AIRSTAIR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 510DA 21312 AFT AIRSTAIR EMERGENCY LIGHTS FAILED TO TEST. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998112001085 19981120 01085 NM 1998 11 20 DL72S982360 1 19981114 A 3350 334701743 LIGHT BOEING 727 727232 1384082 NM L2 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 419DA 21272 L2 DOOR EMERG EXIT LIGHT INOP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1998112001086 19981120 01086 NM 1998 11 20 DL72S982362 1 19981115 A 3350 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 F/C EMERGENCY TRACK LIGHTS INOP. REPLACED BATTERY. 2 L 7 3 4F A3WE 1998112001087 19981120 01087 NM 1998 11 20 DL72S982363 1 19981103 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 4 LE SLAT DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 NR 4 SLAT, ANGLE CRACKED IN CORNER. DYE CHECKED PER PS 900-6-3. NO CRACK FOUND. BURNISHED AREA, TREATED AND PAINTED P ER PS 900-2 NR 5. 2 L 7 3 4F A3WE 1998112001088 19981120 01088 NM 1998 11 20 DL757982364 1 19981114 A 3350 BATTERY PACK BPS73 BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 602DL 2308 22809 EMERGENCY LIGHT IN FIRST CLASS (SIDES OF SEATS) DO NOT ILLUMINATE. REPLACED BATTERY MODULE BASE. 2 L 7 2 4F RT A2NM 1998112001089 19981120 01089 NM 1998 11 20 DLM88982365 1 19981116 A 7430 792055 SWITCH 792055 DOUG MD88 MD88 3023688 NM COCKPIT SHORTED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SO 27 925DL 49712 FLT CREW REPORTED SMOKE AND BURNING SMELL COMING FROM OVERHEAD CONTROL PANEL. IGNITION SWITCH STUCK IN A POSITION. MTC LOWERED PANEL TO FIND INDICATION OF EXCESSIVE HEAT IN AREA OF IGNITION SWITCH. REPORTED MINOR WIRE DAMAGE. MTC VERIFI ED SWITCH SHORTED AND OVERHEATED. REPLACED SWITCH. 2 L 7 2 4F RT A6WE 1998112001090 19981120 01090 NM 1998 11 20 DL72W982368 1 19981116 A 5754 ANGLE BOEING 727 727247 138408F NM NR 6 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 290WA 22108 FOUND ON D2 LETTER CK, NR 6 SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT THE I/B STOP PAD. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998112001091 19981120 01091 NM 1998 11 20 DL72S982369 1 19981103 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEV CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 SKIN CRACKED APPROX 1.5 ON LWR SURFACE OF RT ELEV FWD AND I/B OF TAB CONTROL ROD. DYE CHECKED AND STOP DRILLED CRACKS, FABRICATED REPAIR PART PER SRM 55-20-3 FIG 5. OK TO INSTALL. INSTALLED DOUBLER, FASTENERS AND DOUBLE WEIGH 63G PER SRM 55-20-3 FIG 5. 2 L 7 3 4F A3WE 1998112001092 19981120 01092 NM 1998 11 20 DL72W982373 1 19981116 A 3350 900835A BATTERY PACK BOEING 727 727247 138408F NM RT WING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2816W 20872 RT WING FWD EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998112001093 19981120 01093 NM 1998 11 20 DL72L982374 1 19981116 A 3350 BATTERY PACK 900835A BOEING 727 727232 1384082 NM CARGO DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 505DA T4159 21307 RIGHT AFT EMERGECY OVERWING LIGHTS ON AFT CARGO DOOR INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998112001094 19981120 01094 NM 1998 11 20 SCNA98138 1 19981110 A 3350 BULB BOEING 727 7272J4 1384006 NM RT OVERWING FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 285SC 21676 DURING A LINE MAINTENANCE CHECK, THE RIGHT FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. RELAMPED THE LIGHT ASSEM BLY, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998112001095 19981120 01095 NM 1998 11 20 SCNA98139 1 19981114 A 3350 37067001 BATTERY BOEING 727 7272A1 138407F NM AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS AT THE BOTTOM OF THE STAIRS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERIES. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1998112001096 19981120 01096 NM 1998 11 20 SCNA98140 1 19981114 A 3350 900835A BATTERY PACK BOEING 727 7272A1 138407F NM LT OVERWING DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 287SC 21345 DURING A LINE MAINTENANCE CHECK, THE LEFT OVERWING EXIT EXTERIOR EMERGENCY LIGHT NEAR THE TRAILING EDGE OF THE WING WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK FOR M954. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1998112001097 19981120 01097 SO 1998 11 20 SWIA971302 1 19981013 A 2133 2091G010800 OUTFLOW VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE CABIN FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 193SW 120088 CABIN DEPRESSURIZED WHILE CLIMBING OUT OF 13,000 FT AND WAS UNABLE TO CONTROL IT MANUALLY. RETURNED TO FIELD. SECURED OUTFLOW VALVES IN OPEN POSITION IAW MEL 21-30-01. REMOVED AND REPLACED ELECTRO-PNEUMATIC OUTFLOW VALVE. OPS CHECKS GOO D IAW 21-33-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112001098 19981120 01098 SO 1998 11 20 SWIA971303 1 19981014 A 3234 12038594501 CONTROL LEVER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR FAILED A SWIA L ABORTED APPROACH N FALSE WARNING LD LANDING 1 NM 07 203SW 120240 OBO GEAR INDICATION SYSTEM IS INOP. FLEW PAST TOWER TO CONFIRM GEAR DOWN AND LOCKED. MEL 32-60-1. REMOVED AND REPLACE D LANDING GEAR CONTROL LEVER IAW MM 32-31-00, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112001099 19981120 01099 SO 1998 11 20 SWIA971304 1 19981016 A 3020 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE DEICE DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 562SW 120336 RIGHT ENGINE INLET DEICE FAILED AGAIN IN FLIGHT. COULD NOT ESCAPE ICING CONDITIONS ALONG ROUTE AND DIVERTED BACK TO SFO . INSTALLED SERVICEABLE EJECTOR VALVE AND INSTALLED SERVICEABLE PRESSURE SWITCH AND PATCHED SMALL HOLE IN THROAT BOOT S YSTEM. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112001100 19981120 01100 SO 1998 11 20 SWIA971305 1 19981016 A 3020 BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE DEICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 220SW 120288 RIGHT ENGINE AIR INLET DEICE FAILED IN FLIGHT. RETURNED TO FIELD BECAUSE OF ICING IN AREA. REPLACED RIGHT ENGINE AIR I NLET DEICE BOOT PRESSURE SWITCH. OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112001101 19981120 01101 SO 1998 11 20 SWIA971306 1 19981017 A 3010 38E966A REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE WING DEICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 568SW 120343 WING DEICE BOOT OUTBOARD, INBOARD AND MIDDLE FAILED IN FLIGHT IN ICING CONDITIONS. RETURNED TO FAT. REMOVED AND REPLACE D 18 PSI REGULATOR. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112001103 19981120 01103 SO 1998 11 20 SWIA971308 1 19981019 A 3230 12038594001 CONTROL BOX EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LANDING GEAR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 196SW 120151 AFTER TAKEOFF, COULD NOT GET GEAR TO MOVE. TRIED TWO TIMES WITH NO MOVEMENT OF GEAR OBSERVED OR FELT. RETURNED TO JAC. REPLACED GEAR CONTROL BOX AND SWUNG GEAR IAW MM 32-00-00. GEAR OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112001104 19981120 01104 NM 1998 11 20 P5CA9801595 1 19981115 A 5330 SKIN BOEING 747 747122 1384872 NM BS 1960 PUNCTURE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 ON WALKAROUND, FOUND SKIN PUNCTURED 1 INCH HOLE AT ST 1960 FWD OF LOWER AFT CARGO DOOR SWITCH. REPAIRED PER SRM 53-30-0 3 PG 2J, TEMP REPAIR. PERMANENT REPAIR SCHEDULED NEXT C-CHECK PER COI ITEM 853-041. 2 L 7 4 4F A20WE 1998112001105 19981120 01105 NM 1998 11 20 P5CA9801596 1 19981115 A 3350 60B5003737 LIGHT BOEING 747 747132 1384882 NM UPPER DECK DOME INOP A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 856FT 19897 EMERGENCY LIGHT IN UPPER DECK DOME INOP. REPLACED EMERGENCY LIGHT ASSY AND CKECKED OK PER MM 35-51-00. 2 L 7 4 4F A20WE 1998112001106 19981120 01106 NM 1998 11 20 P5CA9801597 1 19981115 A 3350 60B5003733 LIGHT BOEING 747 747132 1384882 NM PAX DOOR INOP A P5CA K NONE L NO TEST IN INSP/MAINT 1 WP 23 856FT 19897 EMERGENCY EXIT LIGHT INOP AT DOOR SLIDE AREA. REPLACED EMERGENCY LIGHT MODULE AT UPPER DOOR OVERHEAD LOCATION. OPS CHE CK NORMAL PER MM 35-51-00. 2 L 7 4 4F A20WE 1998112001107 19981120 01107 NM 1998 11 20 VNAA9811014 1 19981115 A 2150 GB2001AA1 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT FAILED A VNAA D RETURN TO BLOCK M J OVER TEMP WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 424JS 3033 A LEFT HAND AIR CONDITIONING PACK OVERHEAT WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT R ETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED, AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND NACA DUCT CHECK VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 21-51-24. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED T O SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112001108 19981120 01108 1998 11 20 VNAA9811015 4 19981116 A 3418 STALL WARNING DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E & E COMPT TRIPPED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 442JS 3060 DURING TAXI, A STICK PUSHER WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND RESET THE STALL WARNING SYSTEM, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-33-00. OPERATIONAL CHECKS WERE COMPLET ED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112001109 19981120 01109 NE 1998 11 20 TC8A98083 2 19981116 A 7530 LINE DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE LOOSE A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 23 182SK 45817 642684 AT 90 KTS, NR 4 ENGINE COMPRESSOR STALLED, ABORTED TAKEOFF. FOUND LOOSE PNEUMATIC LINE AT INTERSTAGE BLEED VALVE. TIGH TENED LINE AND OPS CHECKED AT ALL POWER SETTINGS. FLAGGED BLEED VALVE SEVERAL TIMES, NO DEFECTS NOTED. ENGINE WAS RUN AT TAKEOFF POWER WITH SEVERAL THROTTLE BURSTS, NO PROBLEMS. 2 L 7 4 4F 4 F 4A25 1E8 1998112001128 19981120 01128 SW 1998 11 20 HEEA0016791 1 19981112 A 6330 407310203101 MOUNT BELL 407 407 1182206 SW M/R GEARBOX WORN E HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 612PH 53199 CORNER MAIN ROTOR GEARBOX MOUNT RUBBER WORN. PART TC: 2,870. 1 G 7 1 3U O H2SW 1998112001136 19981120 01136 NM 1998 11 20 HNAA9898479 1 19981113 A 5210 85210263101 GAS STRUT DHAV DHC8 DHC8102 2809003 NM PASSENGER DOOR FAILED A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 984HA 377 CLT - FLT 3212 - PASSENGER DOOR WILL NOT OPEN ALL THE WAY (HALF WAY). REPLACED AFT GAS STRUT ASSEMBLY. OPERATIONAL CHE CK GOOD. (M) 2 H 7 2 4T RT A13NM 1998112001137 19981120 01137 NM 1998 11 20 HNAA9893477 1 19981117 A 3350 6104791X BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 934HA PS097 139 FLO - FLT 3252 - EMERGENCY EXIT SIGN ABOVE PASSENGER DOOR WILL NOT ILLUMINATE. REPLACED EMERGENCY BATTERY BASE PS1 IN W ARDROBE CLOSET. (M) 2 H 7 2 4T RT A13NM 1998112001138 19981120 01138 NM 1998 11 20 HNAA9899478 1 19981117 A 2611 302313 CONNECTOR DHAV DHC8 DHC8102 2809003 NM NR 2 DETECTOR LOOSE A HNAA K NONE N FALSE WARNING NR NOT REPORTED 1 EA 07 994HA 459 TPA - FLT 3453 - SMOKE WARNING LIGHT ILLUMINATED TWICE IN FLIGHT AND WENT OUT. FOUND CANNON PLUG ONE-HALF TURN LOOSE ON FORWARD NR 2 SMOKE DETECTOR. INSPECTED PINS AND WIRING. RESECURED AND SAFETIED CANNON PLUG. INSPECTED NR 1 DETECTOR, NO DEFECTS NOTED. TESTED NR 1 AND NR 2 SMOKE DETECTORS. OPERATIONAL CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998112001139 19981120 01139 NM 1998 11 20 RAAA98B1094 1 19981117 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM RT OVERWING DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998112001140 19981120 01140 SO 1998 11 20 RAAA98E9035 1 19981117 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO CABIN INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT LT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT DUE FAILED. 2 L 7 4 4T 4A22 1998112001141 19981120 01141 NM 1998 11 20 CALA9802072 1 19981117 A 5754 ANGLE BOEING 727 727232 1384082 NM NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND A .375 INCH CRACK IN LT WING NR 2 SLAT LOWER CHORD ANGLE BELOW TELESCOPING ANTI-ICE DUCT AREA. THE CRA CK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, PAGE 16. 2 L 7 3 4F A3WE 1998112001142 19981120 01142 NM 1998 11 20 CALA9802073 1 19981117 A 2782 BRACKET BOEING 727 727232 1384082 NM NR 6 LE SLAT ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND TWO .5 INCH CRACKS IN NR 6 LE FLAP O/B ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACK ET WAS INSTALLED IAW SRM 51-20-1, FIGURE 18. 2 L 7 3 4F A3WE 1998112001143 19981120 01143 NM 1998 11 20 CALA9802074 1 19981117 A 5320 WEB BOEING 727 727232 1384082 NM CARGO COMPT PUNCTURED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND A PUNCTURE IN FORWARD CARGO AREA WEB JUST FORWARD OF UPPER AFT DOOR STOP. THE PUNCTURED AREA WAS ROUTE D OUT IAW SRM 51-10-1, PAGE 6B. A WEB REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-10-2, PAGE 4. 2 L 7 3 4F A3WE 1998112001144 19981120 01144 NM 1998 11 20 CALA9802075 1 19981117 A 5755 COVER BOEING 727 727232 1384082 NM NR 2 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND A .1875 AND .125 CRACK IN LT WING UPPER T/E HINGE COVER OF NR 2 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-30-2, PARAGRAPH 7. 2 L 7 3 4F A3WE 1998112001145 19981120 01145 NM 1998 11 20 CALA9802076 1 19981117 A 5720 COVER BOEING 727 727232 1384082 NM NR 3 SPOILER CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER T/E HINGE COVER OF NR 3 SPOILER HINGE. THE T/E HINGE COVER WAS REMOV ED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-20-1 AND 51-30-2, PARAGRAPH 7. 2 L 7 3 4F A3WE 1998112001146 19981120 01146 WP 1998 11 20 CALA9802077 1 19981117 A 2560 4953611501 ESCAPE LINE DOUG DC9 DC982 3022082 WP LT & RT OVERWING ROTTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND THE LT AND RT EMERGENCY OVERWING EXIT DOOR ESCAPE LINES DRY ROTTED AT HOOK ATTACH POINT. THE EMERGENCY ESCAPE LINES WERE REMOVED AND REPLACED IAW MM 25-61-00, PAGES 201A-204. 2 L 7 2 4F A6WE 1998112001147 19981120 01147 WP 1998 11 20 CALA9802078 1 19981117 A 5320 BULKHD STIFFENER DOUG DC9 DC982 3022082 WP BS 218 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 1.5 INCH CRACK IN E & E COMPARTMENT VERTICAL STIFFENER AT AFT BULKHEAD STA 218, FOUR INCHES ABOVE LON GERON 28L. THE CRACK WAS STOP DRILLED AND STACK DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, SHEET 4. 2 L 7 2 4F A6WE 1998112001148 19981120 01148 WP 1998 11 20 9810369985 1 19981113 A 3260 LAMP DOUG DC9 DC932 3022066 WP RT MLG FAILED A NWAA K NONE N FALSE WARNING AP APPROACH 1 GL 01 985US 47479 FLIGHT CREW NOTED THE RIGHT LANDING GEAR INDICATION (GREEN) DID NOT ILLUMINATE UPON LANDING GEAR EXTENSION. LANDING GEA R WAS RECYCLED WITH SIMILAR RESULTS. INDICATOR LAMP WAS REPLACED BY FLIGHT CREW. INDICATION CHECKED NORMAL AND AIRCRAF T LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPLACED ADDITIONAL INDICATOR LAMPS, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998112001149 19981120 01149 EU 1998 11 20 9810373238 1 19981114 A 3350 20131A BATTERY AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1338N 360 DURING TEST OF EMERGENCY PATH LIGHTING, FOUND LIGHTS INOPERATIVE IN FIRST CLASS AND THREE ROWS IN COACH. MAINTENANCE RE PLACED THE POWER SUPPLY UNIT AND BATTERY, OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1998112001150 19981120 01150 NM 1998 11 20 UPS98228172 1 19981117 A 3350 1864 BULB BOEING 727 727185C 138406N NM COCKPIT FAILED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 954UP 19827 INSPECTION TYPE-N/A, EMER EXIT LIGHTS UNARMED LIGHT DOES NOT PRESS TO TEST OR ILLUMINATE AT ALL. CHANGE BULB, NO HELP. ARMED/UNARMED LIGHT, RELAMPED WITH A 1864 BULB AND OPS CHECKED SERVICEABLE. 2 L 7 3 4F A3WE 1998112001151 19981120 01151 WP 1998 11 20 UPS98828174 1 19981117 A 3397 WIRE DOUG DC8 DC873F 302199F WP COCKPIT BROKEN A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 803UP 46073 INSPECTION TYPE-N/A, THE EMER LIGHT OVER THE COCKPIT DOOR WILL NOT COME ON WHEN TESTED. FOUND BROKEN WIRE AT BATT PACK BUSS TERMINAL NR 2. REPAIRED WIRE AND EMER LIGHTS, OPERATED NORMAL. 2 L 7 4 4F RT 4A25 1998112001152 19981120 01152 NM 1998 11 20 98FDEA00701 1 19981114 A 3213 NAS4504U11 BOLT DOUG MD11 MD11F 3023600 NM LT MLG STRUT SHEARED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 614FE 48528 DURING LT MLG SHOCK STRUT LWR BEARING SEAL REPLACEMENT, ANTI-ROTATION BOLT SHEARED FROM CHAMBER (ARG 7477-1) UPPER CYL ASSY. DAMAGED FOUND ON UPPER CHAMBER (NRG 6720-5) AND UPPER BEARING (ARG 7607-1). LEFT MLG CHAMBER ASSY REPLACED PER C MM 32-11-12. 2 L 7 3 4F RT A22WE 1998112001153 19981120 01153 EU 1998 11 20 98FDEA00702 1 19981117 A 5270 SWITCH AIRBUS 310 A310222 3930315 EU CARGO DOOR DIRTY A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 419FE 345 ON TAKEOFF, BULK CARGO DOOR SHOWED OPEN ON RIGHT AND LEFT ECAM OPEN. FOUND DOOR CLOSED. INSPECTED DOOR WARNING SWITCH, CONNECTOR WIRES OK. CLEANED WARNING SWITCH STRIKER DOOR, OPS AND IND CHECKED OK. 2 L 7 2 4F RT A35EU 1998112001154 19981120 01154 NM 1998 11 20 98FDEA00703 1 19981116 A 3610 CAP BOEING 727 727233 138408A NM NR 1 ENGINE LOOSE A FDEA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 222FE 20933 ALL POWER LEVERS AT IDLE, NR 1 ENG FIRE LIGHT ON, REMAINED OUT WITH NR 1 AT IDLE. INSPECTED ALL PNEUMATIC PLUMBING AND DUCTING, AIR LEAKAGE ON SURROUNDING SURFACES, TIGHTENED AND RESAFTIED CAP. CHECKS SATISFACTORILY. 2 L 7 3 4F RT A3WE 1998112001155 19981120 01155 NM 1998 11 20 98FDEA00704 1 19981118 A 2150 2040751 OIL SYST BOEING 727 727233 138408A NM ACM LEAKS A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 279FE 22346 AFT LEVEL OFF, NR 1 MAIN CARGO SMOKE LIGHT CAME ON. SMELL OF ENG FUMES. CARGO FIRE, SMOKE FUMES AND A/C SMOKE CKLST AC COMP. LIGHT EXTINGUISHED DURING DESCENT. REMOVED AND REPLACED WATER SEPARATOR BAGS, INSP PNEUMATIC DUCT AT AIR CLEANER FOR OIL. RAN ENG AND PACKS ALL OK. SUSP RT AIR CYCLE MACH HAS INTERNAL OIL LEAK. *S/D* REMOVED AND REPLACED RT AIR CYCLE MACHINE. 2 L 7 3 4F RT A3WE 1998112001156 19981120 01156 NM 1998 11 20 98FDEA00705 1 19981118 A 3260 SWITCH BOEING 727 7272S2F 1384O81 NM LANDING GEAR DIRTY A FDEA O OTHER N FALSE WARNING AP APPROACH 1 SO 25 206FE 22928 ON LANDING GEAR EXT THE LANDING GEAR DOOR LIGHT ON FWD PANEL IND 3 GRN AND 4 RED LIGHT. REMOVED DUST AND DEBRIS FROM LA NDING GEAR CNTRL LEVER POS IND SWITCH, CYCLE SEV TIMES. CK NORM GOOD PER MM 332-61-12 PG 401-403. OK FOR SERVICE. INS TALLED AND REMOVED LANDING GEAR PINS. 2 L 7 3 4F A3WE 1998112001157 19981120 01157 WP 1998 11 20 ABXA9801061 1 19981117 A 7931 31801040 TRANSMITTER DOUG DC8 DC861 3021952 WP PWA JT3D JT3D3B 52039 NE NR 3 ENGINE DEFECTIVE A ABXA E ENGINE SHUTDOWN N FALSE WARNING DE DESCENT 1 GL 23 843AX 51 46017 645508 NR 3 OIL PRESSURE FLUCTUATED 35 TO 37 PSI AFTER IDLE POWER SET DURING DESCENT. PRESSURE STEADIED ABOUT 37 PSI ON LEVEL OFF AT LOW ALTITUDE. WHEN PRESSURE DROPPED TO 35 TO 34 PSI, PRECAUTIONARY SHUT DOWN WAS ACCOMPLISHED . REPLACED NR 3 E NGINE OIL FILTER AS A PRECAUTION. NO FAULTS NOTED WITH FILTER IAW DC-8 MM. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITT ER IAW DC-8 MM. OIL PRESSURE CHECKED GOOD ON ENGINE RUN. 2 L 7 4 4F 4 F 4A25 1E8 1998112001158 19981120 01158 WP 1998 11 20 ABXA9801062 1 19981117 A 5610 5613217507 WINDOW DOUG DC8 DC863 302198A WP LT COCKPIT LACK OF LUBE A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 816AX 46093 CAPTAIN'S CLEARVIEW WINDOW (EMERG EXIT) WOULD NOT OPEN FULLY. CLEANED AND LUBRICATED CLEAR VIEW WINDOW MECHANISM. OPS CHECKED GOOD IAW DC-8 MM. 2 L 7 4 4F 4A25 1998112001159 19981120 01159 WP 1998 11 20 MWEA981078 1 19981117 A 5330 5920323131 SKIN DOUG DC9 DC915 3022036 WP BS 756 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FUSELAGE EXT SKIN DENTED AND GOUGED STATION 756 AND LONGERON 23R. TRIMMED OUT DAMAGED AREA OF SKIN, FABRICATED SKIN FIL LER AND DOUBLERS. 2 L 7 2 4F A6WE 1998112001160 19981120 01160 WP 1998 11 20 MWEA981079 1 19981117 A 5312 5910130394N1 BULKHEAD TEE DOUG DC9 DC915 3022036 WP AFT PRESS BULKHD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 AFT CARGO COMPT APB CORRODED, CRACKED, BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED TEE CHORD S ECTION. 2 L 7 2 4F A6WE 1998112001161 19981120 01161 WP 1998 11 20 MWEA981080 1 19981117 A 5312 5910163223 BLKHD DOUBLER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 AFT CARGO COMPARTMENT APB CORRODED, CRACKED, GOUGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED APB W EB DOUBLER AND TRIPLER AT RT STATION 817. 2 L 7 2 4F A6WE 1998112001162 19981120 01162 WP 1998 11 20 MWEA981081 1 19981117 A 5312 5910163229 BLKHD DOUBLER DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 AFT CARGO COMP AFT PRESSURE BULKHEAD IS CORRODED, CRACKED, BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED FINGER DOUBLER AT STATION 817 AFT PRESSURE BULKHEAD RADIUS 16. 2 L 7 2 4F A6WE 1998112001163 19981120 01163 WP 1998 11 20 MWEA981082 1 19981117 A 5312 5910163139N BULKHEAD ANGLE DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 AFT CARGO COMPT APB CORRODED, CRACKED BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED TEE FLOOR LE VEL SUPPORT ANGLE. 2 L 7 2 4F A6WE 1998112001164 19981120 01164 WP 1998 11 20 MWEA981083 1 19981117 A 5312 59101635 BULKHEAD SPLICE DOUG DC9 DC915 3022036 WP AFT PRESS BLKHD CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 AFT CARGO COMPARTMENT AFB CORRODED, CRACKED, BULGED RIVETS BROKEN BELOW RT LAV L19R TO L27R. REMOVED AND REPLACED EXIST ING FRAME REPAIR SPLICE RIGHT HAND STATION 817. 2 L 7 2 4F A6WE 1998112001165 19981120 01165 WP 1998 11 20 MWEA981084 1 19981117 A 5311 5910130394N1 FRAME DOUG DC9 DC915 3022036 WP BS 817 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 AFT PIT FRAME PITTED UNDER LONGERON END FITTING FS 817. MTC REMOVED CORROSION, FABRICATED AND INSTALLED NEW TEE CHORD S ECTION. 2 L 7 2 4F A6WE 1998112001166 19981120 01166 WP 1998 11 20 MWEA981085 1 19981117 A 5711 59113021 SPAR CAP DOUG DC9 DC915 3022036 WP WS 560 MISMANUFACTURED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 300ME 45718 FRONT SPAR SECTION MACHINED INCORRECT AT XS 560. MTC FABRICATED AND INSTALLED FILLERS AND DOUBLERS. 2 L 7 2 4F A6WE 1998112001167 19981120 01167 WP 1998 11 20 MWEA981086 1 19981117 A 5711 59113021 SPAR CAP DOUG DC9 DC915 3022036 WP WS 560 MISMANUFACTURED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 300ME 45718 FRONT SPAR SECTION MACHINED INCORRECTLY AT XS 560. FABBED FILLERS AND DOUBLER, ALODINED AND PRIMED. ALSO, INSTALLED DO ME, SEALED REPAIR FASTENERS. LEAK CHECK NOT REQ, REPAIR IN VENT BOX. 2 L 7 2 4F A6WE 1998112001168 19981120 01168 WP 1998 11 20 MWEA981087 1 19981117 A 5315 99115931 FLOORBEAM DOUG DC9 DC915 3022036 WP BS 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FLOORBEAM CORRODED STA 160 47 RBL BOTTOM SIDE. MTC REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 1998112001169 19981120 01169 1998 11 20 DHL98724004 4 19981113 A 3442 MI585161 RT UNIT BOEING 727 727228 NM RADAR SYST FAILED A DHLA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 724DH 19862 RADAR AT ABILIZATION WAS INOP, NOT PAINTING PROPERLY. REPLACED RADAR R/T. 2 L 7 3 4F A3WE 1998112001170 19981120 01170 WP 1998 11 20 RRXA98564 1 19981117 A 5311 561194311 FRAME DOUG DC8 DC863 302198A WP BS 70 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME FS 70 CAP CRACKED AT LONGERON 20 RIGHT AND DRILL DAMAGE AT LONGERON 13 TO 15 RIGHT . REMOVED DAMAGED AREAS, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05462. 2 L 7 4 4F 4A25 1998112001171 19981120 01171 WP 1998 11 20 RRXA98565 1 19981118 A 5720 988742721 ANGLE DOUG DC8 DC863 302198A WP WS 12 CHAFED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT FOUND ANGLE CHAFED EXCEEDING ALLOWABLE LIMITS ON LEFT WING INBOARD T/E STRUCTURE AT WING STA XW S-12. REPLACED ANGLE IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05479 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001172 19981120 01172 WP 1998 11 20 RRXA98566 1 19981118 A 5330 577993811 SKIN DOUG DC8 DC863 302198A WP BS 940 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND INTERNAL SKIN CRACKED AT FS 940 ABOVE LONGERON 24R. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05492 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001173 19981120 01173 WP 1998 11 20 RRXA98567 1 19981118 A 5311 5755076 FRAME DOUG DC8 DC863 302198A WP BS 1120 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 1120 WITH MISDRILLED HOLES BETWEEN LONGERONS 30 AND 33 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05506 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001174 19981120 01174 WP 1998 11 20 RRXA98568 1 19981118 A 5720 57547007 SPLICE DOUG DC8 DC863 302198A WP WS 257 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND SPLICE WITH DRILL DAMAGE ON LT WING L/E AT STA XW 257. REMOVED DAMAGED SPLICE, FABRICAT ED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05507 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001175 19981120 01175 WP 1998 11 20 RRXA98569 1 19981118 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND LONGERON 25 RIGHT AT FS 280 WITH MISDRILLED HOLES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05520 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001176 19981120 01176 WP 1998 11 20 RRXA98570 1 19981118 A 5311 575560 FRAME DOUG DC8 DC863 302198A WP BS 1140 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 1140 WITH MISDRILLED HOLES BETWEEN LONGERONS 31 AND 33 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05530 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001177 19981120 01177 WP 1998 11 20 RRXA98571 1 19981118 A 5315 5613301501 FLOORBEAM DOUG DC8 DC863 302198A WP BS 960 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FLOORBEAM UPPER FLANGE AT FS 960 WITH DRILL NICK AT 5.75 INCHES INBOARD OF LT CUSP. BLE NDED AND REPAIRED IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05539 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001178 19981120 01178 WP 1998 11 20 RRXA98572 1 19981118 A 5311 56428567 FRAME DOUG DC8 DC863 302198A WP BS 717 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 717 WITH MISDRILLED HOLE BETWEEN LONGERONS 20 AND 21 LEFT. FABRICATED AND I NSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05546 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001179 19981120 01179 WP 1998 11 20 RRXA98573 1 19981118 A 5311 564250019 FRAME DOUG DC8 DC863 302198A WP BS 700 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 700 WITH MISDRILLED HOLE BETWEEN LONGERONS 5 AND 6 LEFT. FABRICATED AND INS TALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05550 AND AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001180 19981120 01180 WP 1998 11 20 RRXA98574 1 19981118 A 5311 56456663 FRAME DOUG DC8 DC863 302198A WP BS 965 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 965 AT MLG DOOR JAMB CRACKED FROM FASTENER HOLE TO EDGE OF PART. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05553 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001181 19981120 01181 WP 1998 11 20 RRXA98575 1 19981118 A 5311 57519911 FRAME DOUG DC8 DC863 302198A WP BS 920 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 920 WITH MISDRILLED HOLES AT VERIOUS LOCATIONS. FABRICATED AND INSTALLED RE PAIRS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05555 AND TREATED AREAS IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001182 19981120 01182 WP 1998 11 20 RRXA98576 1 19981118 A 5711 5597832501 SPAR DOUG DC8 DC863 302198A WP WS 417 & 424 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND LT WING LOWER FRONT SPAR FORWARD FLANGE WITH MISDRILLED HOLES BETWEEN WS XFS 417 AND XFS 424. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05566 AND TREATED AREA IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112001183 19981120 01183 WP 1998 11 20 ARWA981104 1 19981118 A 7722 CONNECTOR DOUG DC8 DC862 3021970 WP NR 1 EGT LOOSE A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 19 802BN 45909 NR 1 EGT FLUCTUATING AT 300 DEGREES, ADVANCING THROTTLE ON T/O ROLL. ABORTED T/O AND RETURNED TO RAMP. TIGHTEN CANNO N PLUG ON EGT INDICATOR, OPS CHECKED NORMAL IAW M/M 77-20-00. 2 L 7 4 4F 4A25 1998112600001 19981126 00001 NM 1998 11 26 TWAA9818601 1 19981117 A 3350 CONNECTOR BOEING 767 7673Y0 NM ROW 2-5 LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 ON THE RT SIDE OF THE CABIN, THE EGRESS LIGHTS WERE INOPERATIVE FROM ROWS 2 TO 5. FOUND ELECTRICAL PLUGS DISCONNECTED. RECONNECTED PLUGS. CHECK-C 8-26-98 LAX. 2 L 7 2 4F RT A1NM 1998112600002 19981126 00002 WP 1998 11 26 TWAA9818602 1 19981113 A 5311 FORMER DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT, FOUND FORMER FOOT CRACKED AT STA 1087, STR 3L. REMOVED CRACKED FOOT AND INSTALLED NEW ONE PER SPE CIAL PROCESSES MANUAL 6-70-01, PAGE 2 ITEM 4. 2 L 7 2 4F A6WE 1998112600003 19981126 00003 WP 1998 11 26 TWAA9818603 1 19981113 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT, FOUND IN AFT FUSELAGE AT STA 1087, A 1.5 INCH CRACK AND SHEARED RIVETS BETWEEN LONGERON 2R AND 3R, O/B OF BATH TUB FITTING ON TIE ANGLE. REPLACED PART PER SPECIAL PROCESSES MANUAL 6-70-01, PAGE 2 FIG A. 2 L 7 2 4F A6WE 1998112600004 19981126 00004 WP 1998 11 26 TWAA9818604 1 19981113 A 5320 CASTING DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT, FOUND FORMER TIE CASTING CRACKED AT STA 1087, BETWEEN LONGERON 1R AND 2R. DRILLED AND INSTALLED N EW CASTING USING HLT 436 TENSION HI-LOKS PER SRM 51-60-0, PAGE 10 AND 51-30-5. 2 L 7 2 4F A6WE 1998112600005 19981126 00005 WP 1998 11 26 TWAA9818605 1 19981116 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 1097 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT, FOUND FUESLAGE TO TAIL ATTACH ANGLE CRACKED LT SIDE AT STA 1097. ONE CRACK 2 INCHES LONG IN RADIU S AND ONE CRACK FROM SCREW HOLE TO EDGE. CRACK WAS STOP DRILLED AND CRACK CONTAINMENT VERIFIED BY NDT. ANGLE WAS REPAI RED PER SRM 53-05, FIG 23. 2 L 7 2 4F A6WE 1998112600006 19981126 00006 WP 1998 11 26 VJ9800596 1 19981021 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1109-1116 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENTS AT FS 1109R AND 1116R, L22X.035X1, DX=29, .016 1/2 DX=32, CREASED AND OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. COL D WORKED DENT, PERFORMED HFEC TO VERIFY NO CRACKS, FABRICATED AND INSTALLED DOUBLERS IAW DC9 SRM 51-10-4, 53-01, FIG 2, 51-30-2. 2 L 7 2 4F A6WE 1998112600007 19981126 00007 WP 1998 11 26 VJ9800597 1 19981021 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 927-929 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENTS AT FS 927R AND 929R, L24, .053X2 DX=38, .029X2 DX=69, 0UT LIMIT IAW DC9 SRM 53-04, FIG 38. COLD WORKED DENTS, VER IFIED NO CRACKS BY HFEC, FABRICATED AND INSTALLED DOUBLER IAW DC9 SRM 53-04, FIG 38 AND 51-30-1. 2 L 7 2 4F A6WE 1998112600008 19981126 00008 WP 1998 11 26 VJ9800598 1 19981021 A 5330 PANEL DOUG DC9 DC932 3022066 WP BS 756-813 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 CORROSION ALONG I/B EDGE PANEL 2017 FROM CENTER OF BELLY AT WHEEL WELL FS 756 TO THUMB NAIL PANEL AT FS 813. CORROSION AT FS 813 OUT OF LIMIT. FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC9 SRM 51-10-3, 53-04, FIG 53 AND 53-01, FIG 3. 2 L 7 2 4F A6WE 1998112600009 19981126 00009 WP 1998 11 26 VJ9800599 1 19981021 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 250-260 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AT FS 256R, L17R .045X1 DX=22. ADDITIONAL DENTS AT FS 250, L18-17, FS 252. L17, FS 253, L17, FS 256, L16-17, FS 25 8, L16, FS 260, L17, LESS THAN 3 INCHES APART AND OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38. VERIFIED NO CRACKS BY HFEC. F ABRICATED AND INSTALLED REPAIR DOUBLERS IAW DC9 SRM 51-10-3, 53-04, FIG 38, AND RES 981792. 2 L 7 2 4F A6WE 1998112600010 19981126 00010 WP 1998 11 26 VJ9800600 1 19981021 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 207-210 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENTS AT FS 207R, L18-19, FS 210R, L19, AND FS 212R, L18, LESS THAN 3 INCHES APART AND OUT OF LIMIT IAW DC9 SRM 53-04, F IG 38, CONDITION 1 AND 2. DAMAGE REPAIRED IAW AIRTRAN RES 981791. HFEC INSPECTION ACCOMPLISHED AND NO CRACKS. REINSPE CT CRACKS ANNUALLY OR AT C-CHECK WHICHEVER CONFORMS TO MAINTENANCE PRACTICE PER DC9 SRM 53-04, FIG 38, SHEET 10. 2 L 7 2 4F A6WE 1998112600011 19981126 00011 WP 1998 11 26 VJ9800601 1 19981021 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 157-163 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENTS AT FS 157R, L18, FS 160R, L18-19, FS 161R, L19, FS 163R, L19. FOUND DENT AT FS 157R, L18 TO BE CONDITION 1B. CON FIRMIED NO CRACKS BY HFEC. REPETITIVELY INSPECT FOR CRACKS ANNUALLY OR AT C-CHECK PER DC9 SRM 53-04, FIG 38, SHEET 10. 2 L 7 2 4F A6WE 1998112600012 19981126 00012 WP 1998 11 26 VJ9800602 1 19981022 A 2760 5954283501 TORSION BAR DOUG DC9 DC932 3022066 WP RT SPOILER CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 RT O/B SPOILER TORSION BAR SERRATION AT STA XRS307 PITTED CORROSION BEYOND LIMIT. REMOVED TORSION BAR AND REPLACED WITH SERVICEABLE PARTS. INSTALLED TORSION BAR ASSY AND CHECK SYSTEM IAW DC9 MM 27-61-6, OPS CHECKED GOOD IAW MM 27-61-6. 2 L 7 2 4F A6WE 1998112600013 19981126 00013 WP 1998 11 26 VJ9800603 1 19981022 A 5330 9915570101 SKIN DOUG DC9 DC932 3022066 WP BS 1092 & 1097 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AND BULGE IN AFT ENTRY DOOR SKIN AT FS 1092 AND 1097. .033 X 1/14 AND .106 X 3, TOO CLOSE TO EACH OTHER AND ARE OUT OF LIMIT IAW DC9 SRM 51-50-1, FIG 12A. REMOVED AND INSTALLED NEW SKIN IAW DC9 SRM 51-10-4, 51-30-2, 51-30-1. 2 L 7 2 4F A6WE 1998112600014 19981126 00014 WP 1998 11 26 VJ9800604 1 19981022 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 960.5 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AT FS 960.5. L25R, .012 X 1 AND .026 X 1.1, TOTAL DEPTH .014 AND .028, DX=71 AND 39 RESPECTIVELY, OUT OF LIMIT PER DC9 SRM 53-04, FIG 38, CONDITION 1 B. COLD WORKED DENT, VERIFIED NO CRACKS BY HFEC. FABRICATED AND INSTALLED REPAIR DO UBLER, SPLICE AND SHEAR CLIP IAW DC9 SRM 53-04, FIG 38, 51-30-2, 53-03, FIG 3. 2 L 7 2 4F A6WE 1998112600015 19981126 00015 WP 1998 11 26 VJ9800605 1 19981022 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 953.5-968 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AT FS 953.5-968, L25-26R, .070 X .125, DEPTH .090 DX=35, 0UT LIMIT PER DC9 SRM 53-04, FIG 38, SHEET 10, CONDITION B . COLD WORKED DENTS, CONFIRMED NO CRACK BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 38 AND 53-04, FIG 3. 2 L 7 2 4F A6WE 1998112600016 19981126 00016 WP 1998 11 26 VJ9800607 1 19981022 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 171-172 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AT FS 171R-172R, L22-23, .009 X .0250 AND .009 X .0250, DEPTH .009, DX=28, CONDITION 1 B, TOO CLOSE TOGETHER PER DC 9 SRM 53-04, FIG 38, SHEET 10, NOTE 3. COLD WORKED DENTS, VERIFIED NO CRACK BY HFEC, FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC9 SRM 51-30-2, 53-04, FIG 38, 51-10-2, 51-30-1. 2 L 7 2 4F A6WE 1998112600017 19981126 00017 WP 1998 11 26 VJ9800608 1 19981028 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 1089 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 FRAME BLENDED OUT IN RADIOUS 45 INCHES FROM AFT STAIRS, LT SIDE, AT FS 1089. FABRICATED AND INSTALLED TWO L-ANGLES REPA IRS IAW DC9 SRM 51-30-2, 51-10-3 AND 53-01, PG 10. 2 L 7 2 4F A6WE 1998112600018 19981126 00018 WP 1998 11 26 VJ9800609 1 19981103 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 213.5 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AT FS 213.5L, L16-17, .023 X 1/2 DX=22, OUT OF LIMIT PER SRM 53-04, FIG 38, SHEET 10. COLD WORKED DENTS, VERIFIED NO CRACKS BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 51-04, FIG 38 AND 51-10-2. 2 L 7 2 4F A6WE 1998112600019 19981126 00019 WP 1998 11 26 VJ9800610 1 19981103 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 211-212 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AT FS 211L, L15, .055 X 3 DX=55, 212L, L15-16, .052 X 3 DX=58, 213L, L15-16, .016 X 1/4 DX=16, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38, SHEET 38. COLD WORKED DENTS. VERIFIED NO CRACKS BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER I AW DC9 SRM 51-10-3, 53-04, FIG 38, 51-20-0, AND 51-30-2. 2 L 7 2 4F A6WE 1998112600020 19981126 00020 WP 1998 11 26 VJ9800611 1 19981103 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 123-124 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 DENT AT FS 123L, L23-24. .035 X 1 DX=29, 124L, L23-24, .010 X .25 DX=25, OUT OF LIMIT IAW DC9 SRM 53-04, FIG 38, CONDITI ON 1B-3. NO FURTHER ACTION REQUIRED PER AIRTRAN RES 981872. 2 L 7 2 4F A6WE 1998112600021 19981126 00021 NM 1998 11 26 VJ9800612 1 19981118 A 2822 2580005 BOOST PUMP BOEING 737 737284 138448R NM LT WING MALFUNCTIONED A ZZDA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 15 470AT 21501 EN ROUTE, NR 2 TANK FUEL BOOST PUMP POPPED FWD AND AFT CIRCUIT BREAKER. FLIGHT CREW ELECTED TO DIVERT INTO MEM. SUMPED FUEL TANK AND NO WATER FOUND, REMOVED AND REPLACED FWD BOOST PUMP AT NR 2 TANK. LEAK CHECKED GOOD AND RAN ENGINES, FUE L SYSTEM CHECKED NORMAL. 2 L 7 2 4F A16WE 1998112600022 19981126 00022 WP 1998 11 26 VJ9800613 1 19981118 A 3350 60030431 POWER SUPPLY DOUG DC9 DC932 3022066 WP AIRSTAIR INOP A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 919VV 47260 EMERGENCY LIGHT AT AFT AIR STAIR ENTRY OUT. REPLACED POWER SUPPLY AND BATTERIES, OPS CHECKED GOOD IAW MM 33-00. 2 L 7 2 4F A6WE 1998112600023 19981126 00023 EU 1998 11 26 MALA976231 1 19981116 A 3260 CONNECTOR SAAB SF340 340B 7860101 EU LT MLG DNLOCK SW LOOSE A MALA O OTHER N FALSE WARNING AP APPROACH 1 GL 15 407XJ 340B407 WITH GEAR DOWN SELECTION, INTRANSIT LIGHT ILUMINATED WHILE HYDRAULIC PUMP RAN WITH 3000 PSI. PUMP WOULD THEN TURN OFF, IT OCILATED LIKE THIS 3 TIMES BEFORE THE NOSE AND RIGHT MAIN LIGHTS ILLUMINATED. THE INTRANSIT LIGHT WOULD THEN EXTINGU ISH. AFTER LANDING, THE GROUND OPS MODE DID NOT FUNCTION. MAINTENANCE FOUND CANNON PLUG OFF ON LEFT MAIN GEAR DOWN SWI TCH, RESECURED CANNON PLUG. DOWNLOCK INDICATION CHECKS GOOD. TEST FLIGHT REQUIRED, ALL CHECKS WERE NORMAL. 2 L 7 2 4T RT A52EU 1998112600024 19981126 00024 1998 11 26 MALA976232 4 19981108 A 3425 6226190113 AHRS SAAB SF340 340B 7860101 EU LT COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 233CH 233 IN FLIGHT THE LEFT AHRS FAILED. AIRCRAFT RTURNED TO MSP. MAINTENANCE REPLACED LEFT AHRS COMPUTER. NR 1 AHRS TESTS GOO D IAW SAAB MM. 2 L 7 2 4T RT A52EU 1998112600025 19981126 00025 EU 1998 11 26 MALA976233 1 19981113 A 5270 SWITCH SAAB SF340 SF340A 7850100 EU CARGO DOOR OUT OF ADJUST A MALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 15 119XJ 119 IN FLIGHT CARGO CAUTION LIGHT ILLUMINATED, UNABLE TO VERIFY CLOSED BECAUSE OF PRESSURIZATION DEFERRAL. AIRCRAFT RETURNE D TO DTW. MAINTENANCE READJUSTED CARGO DOOR MICRO SWITCH IAW SF3 AMM CHAP 52-70-00, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998112600026 19981126 00026 1998 11 26 MALA976234 4 19981113 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR MALFUNCTIONED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 503XJ E2310 MAIN PASSENGER DOOR SLIDE PARTIALLY DEPLOYED WHEN DOOR WAS OPENED. MAINTENANCE REPLACED FORWARD PASSENGER DOOR ESCAPE S LIDE REF RJ-85 AMM 25-60-11 401. OPS/SECURITY CHECK GOOD. 2 H 7 4 4F RT A49EU 1998112600027 19981126 00027 EU 1998 11 26 MALA976235 1 19981113 A 2160 VALVE SAAB SF340 340B 7860101 EU RIGHT STUCK A MALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 GL 15 450XJ 450 ON FLIGHT OUT OF MSP, AIRCRAFT INTERIOR TEMP BECOMES VERY HOT; IN AUTO MODE, NO TEMP CHANGE. WHEN SELECTED TO MANUAL MO DE, BECOMES EVEN HOTTER, WHEN SELECTING COLD THE DUCT OVERHEATS AND BLEED SHUTS DOWN. AIRCRAFT RETURNED TO MSP. MAINTE NANCE FOUND MAIN VALVE ON RIGHT SIDE STICKING, UNSTUCK VALVE AND RAN ENGINE. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998112600028 19981126 00028 1998 11 26 MALA976236 4 19981117 A 3416 6223975001 ALTIMETER SAAB SF340 340B 7860101 EU LT COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 410XJ 410 DURING FLIGHT THE CAPTAIN'S ALT SPINNING THROUGH ALTITUDES. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED NR 1 ALTIME TER. OPS CHECK GOOD IAW SF340 AMM CHAP 34. ALTIMETER TESTED TO 50K. 2 L 7 2 4T RT A52EU 1998112600029 19981126 00029 EU 1998 11 26 MALA976237 1 19981110 A 3210 LANDING GEAR SAAB SF340 SF340A 7850100 EU RT MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 89XJ 089 AFTER TAKEOFF, LANDING GEAR INTRANSIT LIGHT REMAINED ON. RECYCLED GEAR DOWN AND RIGHT MAIN GEAR HAD NEGATIVE DOWN INDIC ATION. LANDING AS PER QRH LANDING GEAR EMERGENCY PROCEDURE. MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR A SSEMBLY AND SEPARATION BOLTS IAW SAAB AMM CH 32. PERFORMED OPS CHECKS AND GEAR SWINGS AS REQUIRED. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998112600030 19981126 00030 NE 1998 11 26 K3HA980136 2 19981110 A 7200 ENGINE BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 2 FAILED A K3HA E ENGINE SHUTDOWN E VIBRATION/BUFFET DE DESCENT 1 EA 25 8880Z 21453 696477 ENGINE NR 2, ON DESCENT THROUGH 15,000 FT ENGINE STARTED TO VIBRATE, N1 AND N2 BEGAN FLUCTUATION, EGT STARTED UP THEN 65 0 DEGREE ENGINE WAS SHUT DOWN THEN WIND MILLED FOR 14 MINUTES WITH 5 PSI OIL PRESSURE. REMOVED AND REPLACED NR 2 ENGINE PER KIWI FORM M72A, AND B727 MM 71-00. 2 L 7 3 4F 4 F A3WE E2EA 1998112600031 19981126 00031 NM 1998 11 26 CALA9802079 1 19981118 A 5753 6521630209 SKIN BOEING 727 727232 1384082 NM LT TE FOREFLAP DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 27783 20638 INSPECTION FOUND LT I/B TE FOREFLAP DENTED AND A 1 X 1 AREA OF DEBONDING JUST OUTBOARD OF NR 3 FLAP TRACK AREA AT LOWER SURFACE. THE LT I/B TE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1. 2 L 7 3 4F A3WE 1998112600032 19981126 00032 NM 1998 11 26 CALA9802080 1 19981118 A 5347 SEAT TRACK BOEING 737 7373T0 1384582 NM BS 927 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 39343 23581 INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED AT STA 927, LBL 25. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INST ALLED IAW SRM 53-00-52. 2 L 7 2 4F RT A16WE 1998112600033 19981126 00033 WP 1998 11 26 CALA9802081 1 19981118 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-266 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED AT STA 200-266. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-05, F IGURE 4. 2 L 7 2 4F A6WE 1998112600034 19981126 00034 SO 1998 11 26 COMA9810269 1 19981118 A 3350 10130115 SIGN EMB 120 EMB120RT SO ROW 5 BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 463CA 120267 EXIT SIGN AT ROW 5 IS BROKEN. REPLACED SIGN. 2 L 7 2 4T RT A31SO 1998112600035 19981126 00035 SO 1998 11 26 COMA9810270 1 19981118 A 5240 LATCH EMB 120 EMB120RT SO SERVICE DOOR NOT SECURED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 247CA 120225 SERVICE DOOR WARNING DURING CLIMBOUT. AIRCRAFT RETURNED TO THE FIELD. CLOSED DOOR AND SECURED LATCH. 2 L 7 2 4T RT A31SO 1998112600036 19981126 00036 EA 1998 11 26 COMA9860350 1 19981116 A 5320 601R35031239 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 LEFT HAND AND RIGHT HAND CARGO FLOOR SUPPORT ANGLES AT FS 621, WL 73.5 ARE CRACKED. REPAIRED ANGLES PER REO 601R-53-61- 117. 2 L 7 2 4F RT A21EA 1998112600037 19981126 00037 EA 1998 11 26 COMA9860351 1 19981116 A 5753 601R1430342 SKIN CNDAIR CL600 CL6002B19 EA RT TE FLAP CHAFED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 954CA 7100 RIGHT HAND FLAP LEADING EDGE HAS CHAFE DAMAGE. REPLACED LEADING EDGE. 2 L 7 2 4F RT A21EA 1998112600038 19981126 00038 EA 1998 11 26 COMA9860352 1 19981115 A 5320 601R5361117 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 973CA 7146 CARGO FLOOR SUPPORT ANGLE RIGHT HAND SIDE AT FS 621 WL 73.5 IS CRACKED. REPAIRED SUPPORT ANGLE IAW REO 601R-53-61-117 R A. 2 L 7 2 4F RT A21EA 1998112600039 19981126 00039 EA 1998 11 26 COMA9860353 1 19981031 A 2750 601R93106105 FLEX SHAFT CNDAIR CL600 CL6002B19 EA LT TE FLAP SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 C-CHECK TASK 002-27-160-100, LEFT HAND FLAP, NR 1 FLEXSHAFT DRIVE IS UNSERVICEABLE DUE TO STRAND SEPARATION AND BROKEN H OUSING. REPLACED FLEXSHAFT ASSY. 2 L 7 2 4F RT A21EA 1998112600040 19981126 00040 EA 1998 11 26 COMA9860354 1 19981031 A 7830 32725706 ACTUATOR CNDAIR CL600 CL6002B19 EA LT ENG TR UNIT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 C-CHECK TASK 002-71-430-104, LEFT HAND THRUST REVERSER BALLSCREW ACTUATOR, 7 O'CLOCK POSITON, FORK END BROKEN. REPLACED ACTUATOR. 2 L 7 2 4F RT A21EA 1998112600041 19981126 00041 EA 1998 11 26 COMA9860355 1 19981031 A 7830 32725706 ACTUATOR CNDAIR CL600 CL6002B19 EA LT ENG TR UNIT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 C-CHECK TASK 002-71-430-104, LEFT HAND THRUST REVERSER BALL SCREW ACTUATOR, 5 O'CLOCK POSITION, FORK END BROKEN. REPLAC ED ACTUATOR. 2 L 7 2 4F RT A21EA 1998112600042 19981126 00042 EA 1998 11 26 COMA9860356 1 19981031 A 7830 32725706 ACTUATOR CNDAIR CL600 CL6002B19 EA RT ENG TR UNIT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 7092 C-CHECK TASK 002-78-440-101, RIGHT HAND THRUST REVERSER BALL SCREW ACTUATOR, 7 O'CLOCK POSITION, FORK END BROKEN. REPLA CED ACTUATOR. 2 L 7 2 4F RT A21EA 1998112600043 19981126 00043 EA 1998 11 26 COMA9860357 1 19981101 A 2432 100865 BATTERY CNDAIR CL600 CL6002B19 EA AVIONICS COMPT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 952CA 9934 3548 7092 EMERGENCY BATTERY IN FORWARD AVIONICS BAY IS CRACKED AT MOUNTING LUGS. REPLACED EMERGENCY BATTERY. 2 L 7 2 4F RT A21EA 1998112600044 19981126 00044 EA 1998 11 26 COMA9860358 1 19981117 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA EXTERIOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 982CA 7168 EXTERIOR EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1998112600045 19981126 00045 NM 1998 11 26 98FDEA00706 1 19981118 A 2612 894120 FIRE LOOP BOEING 727 727233 138408A NM NR 1 ENGINE FAILED A FDEA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 25 222FE 20933 NR 1 ENG FIRE LIGHT AND BELL ON, SHUT DOWN ENGINE LIGHT AND BELL OUT. REPLACED NR 1 LOWER FIRE DETECTION ELEMENT. 2 L 7 3 4F RT A3WE 1998112600046 19981126 00046 NM 1998 11 26 98FDEA00707 1 19981119 A 2611 SMOKE DETECTOR BOEING 727 72725 1384006 NM NR 2 FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 504FE 18274 PASSING FLIGHT LEVEL 270, NR 2 SMOKE DETECTOR WARNING LIGHT ON. REMOVED AND REPLACED NR 2 SMOKE DETECTOR AND SMOKE DETE CTOR CONTROL MODULE. 2 L 7 3 4F A3WE 1998112600047 19981126 00047 NM 1998 11 26 98FDEA00708 1 19981119 A 2612 FIRE WARNING BOEING 727 727233 138408A NM COCKPIT ACTIVATED A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 279FE 22346 FIRE WARNING LIGHT AND BELL ON. RAN ALL ENGINES TO TAKEOFF POWER, CND WARNING SYS, OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998112600048 19981126 00048 WP 1998 11 26 98FDEA00709 1 19981119 A 5312 AYB70151 BULKHEAD TEE DOUG DC10 DC1010F 3022111 WP BS 1156 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 054FE 47808 TEE CAP VERTICAL LEG BOTTOM ROW OF FASTENERS, DISCONTINUITY INDICATION LT SIDE. *S/D* REPAIRED 1156 BLKHD TEE CAP. 2 L 7 3 4F A22WE 1998112600049 19981126 00049 WP 1998 11 26 ABXA9801050 1 19981010 A 5311 99118603 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 1109 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE SHEAR TIE ON FRAME AT STATION 1109 CRACKED AT LEFT VERTICAL ATTACH ANGLE. R EPLACED FRAME IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998112600050 19981126 00050 WP 1998 11 26 ABXA9801051 1 19981012 A 5311 99118606 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 1109 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE SHEAR TIE ON FRAME AT STATION 1109 CRACKED AT THE RIGHT VERTICAL ATTACH ANG LE. REPLACED ANGLE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998112600051 19981126 00051 WP 1998 11 26 ABXA9801052 1 19981014 A 5320 591359612 ANGLE DOUG DOUG DC9 DC931 3022065 WP BS 1059 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND SHEAR TIE REPAIR DOUBLER CRACKED AT STATION 1059 BELOW LONGERON 15 RIGHT. REPL ACED ANGLE IAW DC9 SRM 53-03, AND DOUGLAS DWG 5913596. 2 L 7 2 4F A6WE 1998112600052 19981126 00052 WP 1998 11 26 ABXA9801053 1 19981015 A 5320 SB095301875 PANEL DOUG DOUG DC9 DC931 3022065 WP NLG WW CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE NOSE LANDING GEAR WHEEL WELL PRESSURE PANEL CRACKED AT STATION 83 NEAR RIGH T CUSP ANGLE. INSTALLED DOUBLER REPAIR IAW DC9 SB 53-187. 2 L 7 2 4F A6WE 1998112600053 19981126 00053 WP 1998 11 26 ABXA9801055 1 19981014 A 5312 9915558229N BULKHEAD CLIP DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD 4TH RADIAL STIFFENER LEFT ATTACH CLIP CRACKED. REPLA CED CLIP IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998112600054 19981126 00054 WP 1998 11 26 ABXA9801056 1 19981014 A 5320 99576935 JAMB DOUG DOUG DC9 DC931 3022065 WP BS 1059-1076 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE VENTRAL STAIR LEFT JAMB CORRODED ON OUTBOARD SIDE BETWEEN STATION 1059 AND 1076. REPLACED LEFT STAIR JAMB CHANNEL IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998112600055 19981126 00055 WP 1998 11 26 ABXA9801057 1 19981021 A 5320 3957174504 JAMB DOUG DOUG DC9 DC931 3022065 WP BS 1059-1076 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE VENTRAL STAIR RIGHT JAMB STRUCTURE CORRODED BETWEEN STATION 1059 AND 1076. REPLACED RIGHT JAMB FITTING IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998112600056 19981126 00056 WP 1998 11 26 ABXA9801058 1 19981012 A 5320 99115434 SUPPORT DOUG DOUG DC9 DC931 3022065 WP BS 541 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE RIGHT VERTICAL FLOORBEAM SUPPORT CRACKED AT STATION 541. REPLACED RIGHT FL OORBEAM STRUT IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998112600057 19981126 00057 WP 1998 11 26 ABXA9801059 1 19981115 A 2750 5751152503 DRIVE LINK DOUG DOUG DC8 DC863F 302198F WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 819AX 45927 WHILE COMPLYING WITH AD 88-10-7, FOUND CRACK INDICATION ON LEFT FLAP DRIVE LINK STATION 98 AT POINT J, OUTBOARD LUG. RE PLACED LINK IAW DC8 MM 27-51-4. 2 L 7 4 4F 4A25 1998112600058 19981126 00058 WP 1998 11 26 MWEA981088 1 19981118 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACKS ON LONGERON 16L AND 17L AT STATION 965. MTC SPLICED IN NEW SECTION OF LONGERON. 2 L 7 2 4F A6WE 1998112600059 19981126 00059 WP 1998 11 26 MWEA981089 1 19981118 A 5313 27779223 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND LONGERON 13L AT STATION 965 CRACKED. MTC SPLICED IN NEW SECTION OF LONGERON. 2 L 7 2 4F A6WE 1998112600060 19981126 00060 WP 1998 11 26 RRXA98577 1 19981119 A 5311 5642861501 FRAME DOUG DC8 DC863 302198A WP BS 834 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 834 WITH MISDRILLED HOLES AT VARIOUS LOCATIONS. FABRICATED AND INSTALLED RE PAIRS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05568, AREAS TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112600061 19981126 00061 WP 1998 11 26 RRXA98578 1 19981119 A 5230 K5230511 SKIN DOUG DC8 DC863 302198A WP CARGO DOOR MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND UPPER DECK MAIN CARGO DOOR LOWER INNER SKIN WITH MISDRILLED HOLES AT FS 211.97. FABRICA TED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05572, AREAS TREATED IAW DC-8 SRM 51- 1-8. 2 L 7 4 4F 4A25 1998112600062 19981126 00062 WP 1998 11 26 RRXA98579 1 19981119 A 5311 5754671505 FRAME DOUG DC8 DC863 302198A WP BS 260 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 260 WITH MISDRILLED HOLES BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. REMOVED D AMAGED AREAS AS REQUIRED, FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS AND SHIMS IAW FAA DER APPROVED TIMCO ENGINEERIN G SKETCH REO-05580, AREAS TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112600063 19981126 00063 WP 1998 11 26 RRXA98580 1 19981119 A 5320 97549483 WEB DOUG DC8 DC863 302198A WP BS 1180 & 1220 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND WEB AT FS 1180 AND FS 1220 BETWEEN LONGERONS 19 AND 21 RIGHT WITH MISDRILLED HOLES. FAB RICATED AND INSTALLED DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05582, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112600064 19981126 00064 WP 1998 11 26 RRXA98581 1 19981119 A 5313 564932649 LONGERON DOUG DC8 DC863 302198A WP BS 1734 CORROSION A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND LONGERON 8 LEFT WITH CORROSION AT FS 1734. REMOVED DAMAGED AREA, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05583. 2 L 7 4 4F 4A25 1998112600065 19981126 00065 WP 1998 11 26 RRXA98582 1 19981119 A 5712 97532973 RIB DOUG DC8 DC863 302198A WP WING MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND LT WING LEADING EDGE RIB WITH MISDRILLED HOLE AT WS XFS 540. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05589, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112600066 19981126 00066 WP 1998 11 26 RRXA98583 1 19981119 A 5311 5751008501 FRAME DOUG DC8 DC863 302198A WP BS 520 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME AT FS 520 WITH MISDRILLED HOLES BETWEEN LONGERONS 6 AND 9 RIGHT AND AT LONGERON 20 LEFT. FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS AND SHIMS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05591 , AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112600067 19981126 00067 WP 1998 11 26 RRXA98584 1 19981119 A 5522 565497033 SKIN DOUG DC8 DC863 302198A WP LT ELEVATOR DENTED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND LT ELEVATOR UPPER SKIN AT STA XE=200 DENTED BEYOND LIMITS. REMOVED DAMAGES AREA, FABRIC ATED AND INSTALLED REPAIR DOUBLERS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05594, AREA TREATED IAW DC-8 SRM 51 -1-8. 2 L 7 4 4F 4A25 1998112600068 19981126 00068 WP 1998 11 26 RRXA98585 1 19981119 A 5311 3614944514 FRAME DOUG DC8 DC863 302198A WP BS 380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME FS 380 WITH CORROSION IN FASTENER HOLE AT LONGERON 34 LEFT. REMOVED CORROSION, TR EATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR BUSHING AND STRAP IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05598. 2 L 7 4 4F 4A25 1998112600069 19981126 00069 WP 1998 11 26 RRXA98586 1 19981119 A 5330 5615378507 SKIN DOUG DC8 DC863 302198A WP BS 1395 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND SKIN GOUGED AT FS 1395 AT LONGERON 27 RIGHT. REMOVED DAMAGED AREA, FABRICATED AND INSTA LLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05604, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112600070 19981126 00070 WP 1998 11 26 RRXA98587 1 19981119 A 5313 5779917 LONGERON DOUG DC8 DC863 302198A WP FUSELAGE MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND LONGERONS AT FS 160 AND 180 WITH MISDRILLED HOLES IN LONGERONS 25, 26, 27 AND 28 LEFT. R EMOVED DAMAGED AREA, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW FAA DER APP ROVED TIMCO ENGINEERING SKETCH REO-05610. 2 L 7 4 4F 4A25 1998112600071 19981126 00071 WP 1998 11 26 RRXA98588 1 19981119 A 5311 5751991501 FRAME DOUG DC8 DC863 302198A WP BS 940 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAME FS 940 WITH MISDRILLED HOLES AT VERIOUS LOCATIONS. REMOVED DAMAGED AREAS, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW FAA DER APPROVED TIMCO SKETCH REO-05618 . 2 L 7 4 4F 4A25 1998112600072 19981126 00072 WP 1998 11 26 RRXA98589 1 19981119 A 5210 5615403 PAN DOUG DC8 DC863 302198A WP PAX DOOR CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND LEFT FORWARD ENTRY DOOR PAN CRACKED AT LOWER FORWARD CORNER. FABRICATED AND INSTALLED R EPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05648, AREA TREATED IAW DC-8 SRM 51-1-8. 2 L 7 4 4F 4A25 1998112600073 19981126 00073 WP 1998 11 26 RRXA98590 1 19981119 A 5311 97549199754921 FRAME DOUG DC8 DC863 302198A WP BS 1200 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FRAMS FS 1200 AND 1220 WITH MISDRILLED HOLES. REMOVED DAMAGED AREAS, TREATED AREAS IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-056 96. 2 L 7 4 4F 4A25 1998112600074 19981126 00074 WP 1998 11 26 RRXA98591 1 19981119 A 5320 56122987 WEB DOUG DC8 DC863 302198A WP BS 9-12 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FORWARD PRESSURE WEB WITH CORROSION BETWEEN STA 9 AND 12. REMOVED DAMAGED AREA, TREATED IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05707. 2 L 7 4 4F 4A25 1998112600075 19981126 00075 WP 1998 11 26 RRXA98592 1 19981119 A 5315 561214255 FLOORBEAM DOUG DC8 DC863 302198A WP BS 1700 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1700 WITH MISDRILLED HOLES IN UPPER HORIZONTAL FLANGE. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05744. 2 L 7 4 4F 4A25 1998112600076 19981126 00076 NM 1998 11 26 VNAA9811018 1 19981117 A 3243 AC69965 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE PARKING BRAKE FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 07 439JS 3057 WHILE EN ROUTE, AN EMERGENCY ACCUMULATOR LOW PRESSURE WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO PIT AND LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY PARKING BRAKE VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-43-02. OPERATION AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE . 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112600079 19981126 00079 CE 1998 11 26 98ZZZX4225 1 19981102 A 3231 55421029 TORQUE TUBE CESSNA 500 560CESSNA 2076750 CE NLG DOOR FAILED A IMJA K NONE O OTHER IN INSP/MAINT 1 EA 25 19MK 1339 5600395 ON PRE-FLIGHT, CREW FOUND NLG DOORS PARTIALLY OPEN. NO UNUSUAL INDICATION ON PREVIOUS LANDING. FOUND BROKEN WELD ON LE FT END OF TORQUE TUBE (THE END PIECE ACTS AS A HINGE FOR THE ASSY). IT APPEARS THIS WAS A MFG DEFECT. POOR WELD PENETR ATION WHERE BREAK OCCURRED. 2 L 7 2 4F RT A22CE 1998112600121 19981126 00121 CE 1998 11 26 98ZZZX4267 1 19981027 A 2410 ALTERNATOR ELECTROSYS ALT9422 BEECH 58 58 1152740 CE ALTERNATOR LOOSE A FPIA K NONE O OTHER IN INSP/MAINT 1 SO 15 329H 7111523 TH219 ALTERNATOR END BEARING RACE FOUND LOOSE IN ALTERNATOR HOUSING. TIME IN SERVICE: 24.7 HOURS. INSTALLED ON AIRCRAFT 9-1 9-98. REMOVED FROM AIRCRAFT 9-30-98. 1 L 7 2 3O 3A16 1998112600124 19981126 00124 NM 1998 11 26 HNAA9892057 1 19980916 A 3230 54C546347 VALVE DHAV DHC8 DHC8102 2809003 NM NLG FAILED A HNAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 EA 07 920HA 27493 89 084 CLT/HHH - FLT 3160 - LOST HYDRAULIC QUANTITY AND PRESSURE AFTER LANDING GEAR EXTENSION. DIVERTED TO SAV. REMOVED AND R EPLACED SOLENOID SEQUENCE VALVE FOR NOSE GEAR. SERVICED AND BLED NR 2 HYDRAULIC SYSTEM. OPS AND LEAK CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998112600127 19981126 00127 NM 1998 11 26 VJ9800614 1 19981027 A 5210 65554788 GATE BOEING 737 737222 1384473 NM L-2 DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 468AT 19074 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL. THE L-2 DOOR BOTTOM FRAME WAS FOUND WITH CORROSION. CORR OSION WAS OUT OF LIMITS IAW B737 SRM. REMOVED THE GATE AND INSTALLED IAW B737 SRM 51-30-2, 51-30-5 AND 52-00-2. 2 L 7 2 4F A16WE 1998112600128 19981126 00128 NM 1998 11 26 VJ9800615 1 19981029 A 5312 BULKHEAD BOEING 737 737222 1384473 NM BS 540 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 468AT 19074 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL. THE 540 BULKHEAD WAS FOUND WITH CORROSION AT THE BOTTOM S TRINGERS 26 AND 28R. REMOVED TWO EACH DOUBLERS, CUT OUT CORROSION. FABRICATED AND INSTALLED INNER DOUBLER AND TWO EACH DOUBLERS IAW B737 SRM 51-10-06, 51-10-2, MM 51-20-11 AND AIRTRAN RES 981859. 2 L 7 2 4F A16WE 1998112600129 19981126 00129 NM 1998 11 26 VJ9800616 1 19981029 A 5320 SHEAR TIE BOEING 737 737222 1384473 NM BS 285 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 468AT 19074 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND AT BS 285 LT SIDE BETWEEN W/W AND FUSEL AGE SKIN AT THE BOTTOM SKIN. MECHANICALLY REMOVED CORROSION. FUSELAGE SKIN AND BEAM WERE WITH-IN THE SRM LIMITS. THE SHEAR TIE WAS OUT LIMITS. CUT OUT CORRODED SECTION OF SHEAR TIE FABRICATED AND INSTALLED L ANGLE REPAIR IAW B737 SRM 53 -10-1, 51-10-2, 51-40-4 AND MM51-21-31. 2 L 7 2 4F A16WE 1998112600130 19981126 00130 EU 1998 11 26 MALA976238 1 19981114 A 3520 HOSE SAAB SF340 340B 7860101 EU SEAT 5D LOOSE A MALA A UNSCHED LANDING O OTHER CR CRUISE 1 GL 15 9CJ 224 DURING FLIGHT, O2 HOSE OVER SEAT 5D FELL OFF FROM ABOVE. AIRCRAFT RETURNED TO DTW. MAINTENANCE RESECURED PANEL AND HOS E ABOVE 5D, OVERHEAD PSU PANEL. SECURITY CHECK GOOD. 2 L 7 2 4T RT A52EU 1998112600131 19981126 00131 EU 1998 11 26 MALA976239 1 19981116 A 3610 5056T88P01 VALVE SAAB SF340 SF340A 7850100 EU LT BLEED AIR FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 DURING FLIGHT, LEFT AIR VALVE LIGHT ILLUMINATED. CREW PERFORMED ALL APPROPRIATE CHECKS, STILL INOP. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT ENGINE AIR BLEED SHUT OFF VALVE. ALL IAW GE MM, OPS CHECK GOOD ON THE GROUND. 2 L 7 2 4T RT A52EU 1998112600132 19981126 00132 EU 1998 11 26 MALA976240 1 19981117 A 3610 VALVE SAAB SF340 SF340A 7850100 EU LT ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 110XJ 340A110 DURING FLIGHT, LEFT AIR VALVE ILLUMINATED WHEN SWITCH TURNED ON, NO TORQUE DROP OR ITT RISE NOTED. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT ENGINE START BLEED AIR VALVE. OPS CHECK FOR 15 MINUTES GOOD. ALL IAW GE MM. 2 L 7 2 4T RT A52EU 1998112600133 19981126 00133 NE 1998 11 26 MALA976241 2 19981110 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RIGHT MALFUNCTIONED A MALA O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 15 418XJ 418 DURING FLIGHT, THE RIGHT ENGINE HAD A 5 SECOND ROO BACK AT 22,000 FEET, -28 DEGREES C, MINOR ICE. THE OTHER ENGINE INST RUMENTS REMAINED NORMAL. AIRCRAFT LANDING WITH NOTHING FURTHER. MAINTENANCE AFTER CONSULTATION WITH MX CONTROL AND FLI GHT CREW IT WAS DETERMINED THAT THE AIRCRAFT WAS IN ICING CONDITIONS, WITH NO DDT SHIFT, NO FURTHER ACTION REQUIRED PER GE MM 72-00-00 FAULT ISOLATION. TROUBLE NR 5 OK FOR RETURN TO SERVICE. 2 L 7 2 4T 4 T RT A52EU E8NE 1998112600134 19981126 00134 EU 1998 11 26 MALA976242 1 19981103 A 2612 472326 FIRE WIRE SAAB SF340 340B 7860101 EU LT ENGINE CHAFED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 441XJ 441 ON APPROACH TO MSP, THE LEFT FIRE DETECT FAIL CAUTION LIGHT CAME ON 4 TIMES, INTERMITTENTLY. AIRCRAFT LANDING WITHOUT I NCIDENT. MAINTENANCE INSPECTED AND FOUND AFT FIRE WIRE CHAFFED, FOUND ENGINE MOUNTS BAD. REPLACED ENGINE MOUNTS AND AF T FIRE WIRE. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998112600135 19981126 00135 EU 1998 11 26 MALA976243 1 19981029 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 417XJ 340B417 DURING C CK, 4 DENTS NOTED IN RT FUSELAGE SKIN AFT OF ICE SHIELD FROM FS 339.0 TO FS 363.0, BETWEEN SL 1615 AND SL 1617. DENTS FOUND TO BE WITHIN ALLOWABLE LIMITS IAW SAAB SRM 51-10-10 PAGE 15. A PERMANENT EXT DOUBLER REPAIR WAS ACCOMP'D. NDT EDDY CURRENT TEST REVEALED NO CRACKS TO FUSELAGE SKIN IN AREA. FAB'D EXT REPAIR DOUBLER FROM 2024-T3 ALUMINUM, 0. 050 THICK MEASURING 13.0 X 11.0. FAB'D EXT REPAIR TRIPLER FROM 2024-T3 ALUMINUM, 0.050 THICK MEASURING 11.25 X 7.5 AND INSTALLED IAW SAAB SRM 53-70-10 AND 51-40-21. FILLET SEALED REPAIR IAW SAAB SRM 51-20-50. APPLIED TOP COAT OF PAINT IA W SAAB AMM 21-30-00 WITH NO DEFECTS. ALL WORK ACCOMP'D IAW SAAB STRUCTURAL REPAIR MANUAL AND A/C MM. REF CELSIUS AEROT 2 L 7 2 4T RT A52EU 1998112600136 19981126 00136 EU 1998 11 26 MALA976244 1 19981111 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 356 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 421XJ 421 DURING C CK INSPECTION, DENT NOTED IN LT FUS SKIN AFT OF ICE SHIELD AT FS 356, BETWEEN SL 1515 AND SL 1516. DUE TO DEPT H OF DENT OUT OF ALLOWABLE LIMITS IAW SAAB SRM 51-10-00, AN EX DOUBLER AND TRIPLER REPAIR, CUT OUT DAMAGED AREA MEASURIN G 1.375 X 2.25. NDT EDDY CURRENT REVEALED NO CRACKS TO FUSELAGE SKIN IN CUT OUT AREA. FAB'D EXTERNAL REPAIR DOUBLER AN D TRIPLER FROM 2024-T3 ALUMINUM, .050 THICK, DOUBLER MEASURED 12.5 X 4.5, TRIPLER 11.0 X 4.25. REPAIR ACCOMP'D AND INST ALLED IAW SAAB SRM 53-70-10 AND 51-40-21. FILLET SEALED REPAIR IAW SAAB SRM 51-20-50. APPLIED TOP COAT OF PAINT IAW SA AB SRM 51-20-43. A PRESS LEAK CHECK WAS CONDUCTED IAW SAAB AMM 21-30-00 WITH NO DEFECTS NOTED. ALL WORK ACCOMP'D IAW S 2 L 7 2 4T RT A52EU 1998112600137 19981126 00137 EU 1998 11 26 MALA976245 1 19981118 A 3350 1317 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING INSPECTIO, EMERGENCY OVERHEAD LIGHTS INOP AT 2A, 6C/D AND 8C/D. MAINTENANCE RELAMPED. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998112600138 19981126 00138 NM 1998 11 26 K3HA980137 1 19981115 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM RT OVERWING DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 354PA 20624 AT POST FLIGHT, FOUND RIGHT FORWARD WING EMERGENCY LIGHT INOP. REMOVED AND REPLACED RIGHT BATTERY PACK REF MM 33-50-71, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998112600139 19981126 00139 NM 1998 11 26 K3HA980138 1 19981118 A 3397 WIRE BOEING 727 727225 1384077 NM ROW 31 BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 ROW 31 DEF EMERGENCY PATH LIGHTING WIRE BROKEN. REPAIRED BROKEN WIRE AT ROW 31 DEF EMERGENCY PATH LIGHT, OPS CHECK GOOD . 2 L 7 3 4F A3WE 1998112600140 19981126 00140 NM 1998 11 26 K3HA980139 1 19981118 A 3350 S106137067001 BATTERY BOEING 727 727225 1384077 NM R-1 DDOR DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8883Z 21580 R-1 DOOR EMERGENCY LIGHT ASSEMBLY INOP WITH SWITCH ON. REPLACED BATTERIES PER MM 33-50, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998112600141 19981126 00141 NM 1998 11 26 K3HA980140 1 19981120 A 3350 0816901 SOCKET BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 ON DAILY CHECK, ONE EACH EMERGENCY PATH LIGHT SOCKET NO GOOD. REPLACED EMERGENCY PATH LIGHT SOCKET PER MM 33-50. LIGHT OPS CHECK OK 2 L 7 3 4F A3WE 1998112600142 19981126 00142 1998 11 26 JBXA9800058 4 19981121 A 3418 COMPUTER CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE E & E COMPT TRIPPED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 573ML 7227 STALL FAIL MESSAGE ON EICAS. RESET STALL PROTECTION COMPUTER MEMORY IAW CL-65 MM 27-35-01. OPERATIONAL TEST OF STALL P ROTECTION COMPUTER CHECK GOOD, IAW CL-65 MM 27-35-01. 2 L 7 2 4F 4 F RT A21EA E15NE 1998112600143 19981126 00143 1998 11 26 AWXA9800221 4 19981115 A 2210 B397CAM0101B YAW DAMPER AIRBUS 320 A320231 3930325 EU NR 1 MALFUNCTIONED A AWXA O OTHER F FLT CONT AFFECTED UK UNKNOWN 1 WP 28 632AW 22612 4553 81 NR 1 YAW DAMPER FAULT. THE EVENT WAS PRECEEDED BY A RUDDER HARD OVER, SUSPECT THE RUDDER ACTUATOR. THE NOSE OF THE AIR CRAFT MOVED RAPIDLY 10 DEGREES. THE FLIGHT CREW WAS QUITE ALARMED. DPI / MEL 22-63-01 ISSUED.C: T/S PER TSM 22-63-00 R/R FAC 1 PER AMM 22-66-34. TEST OK PER 22-66-34 DPI/MEL CLEARED. 2 L 7 2 4F RT A28NM 1998112600144 19981126 00144 NM 1998 11 26 AWXA9800222 1 19981117 A 3350 417N52101 BATTERY PACK BOEING 757 757225 1384959 NM EXTERIOR DISCHARGED A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 915AW 22209 DURING ROUTINE MAINTENANCE CHECK, FOUND AFT LEFT EMERGENCY LIGHT EXTERIOR OUT. REMOVED AND REPLACED BATTERY PACK. OPS NORMAL. 2 L 7 2 4F RT A2NM 1998112600145 19981126 00145 SO 1998 11 26 RAAA98E4023 1 19981118 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO RT EMER EXIT FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 AFT RT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHT DUE FAILED. 2 L 7 4 4T 4A22 1998112600146 19981126 00146 SO 1998 11 26 RAAA98E9036 1 19981119 A 3350 1000553 LIGHT LKHEED 188 188C 5262604 SO LT&RT EMER EXIT FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 AFT LT AND AFT RT OVERWING EMERGENCY EXIT PULL DOWN EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED EMERGENCY LIGHTS DUE FAILED. 2 L 7 4 4T 4A22 1998112600147 19981126 00147 NM 1998 11 26 RAAA98B2047 1 19981119 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 12 DISCHARGED A RAAA K NONE L NO TEST CR CRUISE 1 AL 03 832RV 19098 CREW REPORTS NEED TO CHECK BATTERIES FOR PAX ROW 12 FLOOR PROXIMITY EGRESS LIGHT. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998112600148 19981126 00148 NM 1998 11 26 CALA9802082 1 19981117 A 3231 BEARING BOEING 727 727224 1384076 NM NLG DOOR WORN A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 93738 20666 THE NOSE GEAR DOORS OPEN LIGHT ON BOTH THE FORWARD AND SECOND OFFICER'S PANELS WERE ILLUMINATED AFTER GEAR RETRACTION DE PARTING BWI. THE WARNING LIGHTS WERE ACCOMPANIED BY RUMBLING AIR NOISE. THE GEAR WAS CYCLED WITH NO CHANGE. THE AIRCR AFT WAS DIVERTED TO EWR AND THE GEAR EXTENDED NORMALLY FOR LANDING. MAINTENANCE FOUND THAT THE NLG FORWARD DOORS HAD WO RN PARTS INCLUDING BEARING, BUSHINGS, SPACERS, 4H FITTING, AND BOLT. THE WORN PARTS WERE REPLACED. THE NOSE GEAR DOORS WERE ADJUSTED AND TESTED IAW MM 32-22-1, PAGE 501. A NOSE GEAR EXTENSION AND RETRACTION TEST WAS PERFORMED IAW MM 32-3 3-0, PAGE 501 AND OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1998112600149 19981126 00149 NM 1998 11 26 CALA9802083 1 19981120 A 3397 WIRE BOEING 757 757224 1384958 NM LT&RT EMER EXIT DAMAGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14118 27560 INSPECTION FOUND LT AND RT OVERWING EMERGENCY EXIT LIGHTS AT FLOOR LEVEL INOPERATIVE. DAMAGED WIRING WAS REPAIRED IAW E CRA 3350-01242 AND OPERATION OF THE LIGHTS CHECKED GOOD. 2 L 7 2 4F RT A2NM 1998112600150 19981126 00150 WP 1998 11 26 CALA9802084 1 19981120 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 196-218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND SEAT TRACK CORRODED AT STA 196-218. A NEW SECTION OF SEAT TRACK WAS INSTALLED IAW SRM 53-05. 2 L 7 2 4F A6WE 1998112600151 19981126 00151 WP 1998 11 26 9810389906 1 19981119 A 3260 SENSOR DOUG DC9 DC931 3022065 WP NLG BROKEN A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 956N 47252 DURING APPROACH INTO MEM, NOSE LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW DECLARED AN EMERGENCY A ND EXECUTED GO-AROUND PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE GEAR DOWNLOCK PROXIMITY SEN SOR BROKEN. REPLACED SENSOR. OPERATIONAL CHECK NORMAL ON GEAR SWING. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1998112600152 19981126 00152 NM 1998 11 26 UPS98228204 1 19981109 A 5542 SKIN BOEING 727 72762C 138402C NM RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C SURFACE CORROSION ON LOWER RUDDER SKIN PANEL LEFT SIDE BETWEEN FRONT SPAR AND REAR SPAR BY PCU ATTACH POINT. RUDDER REPLACED IAW MM 27-20-1. 2 L 7 3 4F A3WE 1998112600153 19981126 00153 NM 1998 11 26 UPS98228205 1 19981103 A 5542 SKIN BOEING 727 72762C 138402C NM RUDDER CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 912UP 19244 INSPECTION TYPE:C CORROSION ON LOWER RUDDER SKIN PANEL RT SIDE FRONT SPAR AREA BY PCU ATTACH POIN. RUDDER REMOVED IAW MM 27-20-11. 2 L 7 3 4F A3WE 1998112600154 19981126 00154 WP 1998 11 26 UPS98828175 1 19981117 A 3246 BEARING DOUG DC8 DC873F 302199F WP NR 6 MLG TIRE MISSING A IPXA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 01 851UP 46051 LEFT MAIN GEAR AFT INBD TIRE SMOKING, A/C ABORTED TAKEOFF AND RETURNED TO RAMP WITH NR 6 MAIN TIRE MISSING AXLE NUT AND OUTER BEARING. FOUND NR 6 WHEEL AND BRAKE ASS. DAMAGED AND AXLE THREADS N.G. REMOVED AND REPLACED LT BOGIE PER MM 32- 11-05 PN ON AND OFF 5759181-501 SN ON UP17253 SN OFF UP14318. 2 L 7 4 4F RT 4A25 1998112600155 19981126 00155 WP 1998 11 26 UPS98828197 1 19981021 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1140 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 779UP 45979 INSPECTION TYPE:C LONGERON 33L CORRODED AT F/S 1140. REPAIRED IAW SRM 53-2-2. 2 L 7 4 4F RT 4A25 1998112600156 19981126 00156 WP 1998 11 26 UPS98828208 1 19981020 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 1540-1560 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:D AFT ACCY COMPARTMENT/CORROSION ON LONGERON INNER SURFACE LONGERON 2 5L FS 1540-1560. REMOVED CORR IAW DC8 SRM 51-1-8. FOUND TO BE OUT OF LIMITS IAW DC8 S RM 53-2-0. REMOVED DAMAGED SECTION OF LONGERON DRILLED AND DEBURR ED LONG END SPLICES IAW DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SR M 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998112600157 19981126 00157 WP 1998 11 26 UPS98828209 1 19981019 A 5320 PAN DOUG DC8 DC871F 302199D WP SERVICE DOOR PUNCTURED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:D RIGHT AFT SERVICE DOOR JAMB PUNCTURE IN LOWER AFT PAN. REMOVED DAMAGED SECTION OF PAN FABRICATED NEW SECTION. FABRICATED SPLICE ANGLES ALODINED PRIMED AND INSTALLED NEW PARTS. 2 L 7 4 4F RT 4A25 1998112600158 19981126 00158 WP 1998 11 26 UPS98828210 1 19981022 A 5312 BULKHEAD DOUG DC8 DC871F 302199D WP BS 1766 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:D AT LONGERON 10L AT STA 1766 HAS A CRACK AT BULKHEAD. REMOVED STRAP FROM ACCESS. STOP DRILLED IAW DC8 SRM 53-7-5 FIG 9. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED STRAP IAW DC8 SRM 51-1-70D 2 L 7 4 4F RT 4A25 1998112600159 19981126 00159 WP 1998 11 26 UPS98828211 1 19981019 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE:D CORRODED ANGLE AT RT END OF FRAME STA 940 AT AFT UPPER CAP. REMOVED AND REPLACED ANGLE FRAME STA 940 AT UPPER CAP. 2 L 7 4 4F RT 4A25 1998112600160 19981126 00160 NM 1998 11 26 QXEA9801723 1 19981117 A 3350 1010951 LIGHT DHAV DHC8 DHC8102 2809003 NM LT UNDERWING BROKEN A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 829PH 512 SEA- LEFT UNDERWING CABIN EMERGENCY LIGHT BROKEN. MAINTENANCE REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCR AFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998112600161 19981126 00161 WP 1998 11 26 ABXA9801084 1 19981119 A 3260 H141003 SWITCH DOUG DC8 DC862 3021970 WP LT MLG WORN A ABXA D RETURN TO BLOCK N FALSE WARNING AP APPROACH 1 GL 23 801AX 46077 ON GEAR EXTENSION, DID NOT GET LEFT MAIN GEAR (GREEN) LIGHT. RED GEAR UNSAFE LIGHT DID NOT ILLUMINATE. RECYCLED GEAR A ND ACCOMPLISHED TOWER FLY-BY. LANDING WAS UNEVENTFUL. COULD NOT DUPLICATE DISCREPANCY. INSPECTED WIRING AND REPLACED MAIN GEAR DOWN SWITCH AS PRECAUTIONARY. SYSTEM OPS CHECKED GOOD IAW DC8 MM. 2 L 7 4 4F 4A25 1998112600162 19981126 00162 NE 1998 11 26 DHL98717003 2 19981117 A 7320 9148810 P & D VALVE BOEING 727 72723 1384004 NM PWA JT8 JT8D7 52053 NE NR 1 ENGINE FAILED A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 717DH 19389 AFTER TAKEOFF FROM MIA AT CLIMB, THRUST SETTING THE CREW NOTICED A VIBRATION AND NR 1 ENGINE EPR WAS FLUCTUATING BETWEE N 1.75 AND 1.5 FUEL FLOW AND N2 FLUCTUATING. WHEN THRUST REDUCED THE VIBRATION WAS MINIMAL. FLIGHT RETURNED TO MIA. R EMOVED AND REPLACED P AND D VALVE AND DRAINED MOISTURE TRAP. 2 L 7 3 4F 4 F A3WE E2EA 1998112600163 19981126 00163 NM 1998 11 26 SWAA982935 1 19981119 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING WALKAROUBD CHECK, FOUND FUSELAGE SKIN CRACK RT SIDE AFT ABOVE AFT WING BODY FAIRING. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600164 19981126 00164 NM 1998 11 26 SWAA982936 1 19981119 A 3350 6556633 LIGHT BOEING 737 7373H4 1384600 NM ROW 14 INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 636WN 27709 DURING SCHEDULED SC CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT AT ROW 14DEF INOP. REPAIRED PER M/M. 2 L 7 2 4F RT A16WE 1998112600165 19981126 00165 NM 1998 11 26 SWAA982937 1 19981120 A 3350 LAMP BOEING 737 7373H4 1384600 NM ROW 22 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 319SW 23340 DURING SCHEDULED SC CHECK, FOUND ROW 22 BULLNOSE EMERG LIGHT INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998112600166 19981126 00166 NM 1998 11 26 SWAA982938 1 19981120 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 372SW 26599 DURING SCHEDULED BC1 CHECK, FOUND SEVERAL FLOOR TRACK LIGHTS INOP. REATTACHED LOOSE WIRING AND OPS CHECKED PER BOEING M /M. 2 L 7 2 4F RT A16WE 1998112600167 19981126 00167 NM 1998 11 26 SWAA982939 1 19981119 A 3350 BATTERY BOEING 737 7373T5 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 667SW 23063 DURING PRE-FLIGHT CHECK, FOUND FWD I/B EMER FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998112600168 19981126 00168 NM 1998 11 26 SWAA982940 1 19981118 A 3350 LAMP BOEING 737 7373A4 1384585 NM ROW 18 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 18. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998112600169 19981126 00169 NM 1998 11 26 SWAA982941 1 19981122 A 2782 6546423251 ACTUATOR BOEING 737 7372H4 138448C NM NR 3 LE SLAT FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 07 063SW 22061 RETURNED TO DAL DUE TO NR 3 SLAT STUCK IN TRANSIT POSITION, VISUALLY CONTINUED PARTIALLY EXTENED IN FLAPS 1/5 POS. WITH T/E FLAPS AT POS 15 ALL LEADING EDGE SLATS WENT FULL EXTEND. REMOVED AND REPLACED NR 3 SLAT ACTUATOR PER M/M. LEAK CK OK. REMOVED AND REPLACED NR 3 SLAT PER M/M. OPS CK OK PER M/M, PN:65-46423-251 S/N OFF:BN62, PN:65-46423-269 S/N ON:B N297, PN:65-44651-16 S/N OFF:2579T, S/N ON:2103T. 2 L 7 2 4F A16WE 1998112600170 19981126 00170 NM 1998 11 26 SWAA982942 1 19981119 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 370-350 DAMAGE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 634SW 27937 SKIN TORN AT LAP AND BUTT JOINT FWD CARGO DOOR AND SLICED HOLE IN SKIN AT S19R FROM BS 370-350 DUE TO GROUND EQUIPMENT. REPAIRED PER TRAMCO EWO 98-1088. 2 L 7 2 4F RT A16WE 1998112600171 19981126 00171 NM 1998 11 26 SWAA982943 1 19981119 A 5330 SKIN BOEING 737 7373Q8 1384670 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4 D CHECK, FOUND A FUSELAGE SKIN CRACK EMANATING FROM A RIVET HOLE AT FWD UPPER CORNER OF AIRSTAIRS C UTOUT. REPAIRED PER SWA RA 1-353-1940. 2 L 7 2 4F RT A16WE 1998112600172 19981126 00172 NM 1998 11 26 SWAA982944 1 19981119 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2 D CHECK, FOUND 1 WEB CRACK AT BS 178, WL 188, LBL 1. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600173 19981126 00173 NM 1998 11 26 SWAA982945 1 19981119 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2 D CHECK, FOUND LEFT SIDE CHORD CRACKED AT BS 178, WL 207, LBL. 29. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600174 19981126 00174 NM 1998 11 26 SWAA982946 1 19981119 A 5312 BULKHEAD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKS AT WL 218, LBL 18-16. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600175 19981126 00175 NM 1998 11 26 SWAA982947 1 19981119 A 5312 BULKHEAD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2 D CHECK, FOUND BS 178 BULKHEAD CRACKS AT WL 213, LBL 6.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600176 19981126 00176 NM 1998 11 26 SWAA982948 1 19981119 A 3350 LAMP BOEING 737 7373A4 1384585 NM ROW 18 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 680AA 23505 DURING SCHEDULED C3 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROW 18. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998112600177 19981126 00177 NM 1998 11 26 SWAA982949 1 19981119 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 266 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CREASED AT BS 266, AT S4 TO 6L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600178 19981126 00178 NM 1998 11 26 SWAA982950 1 19981119 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM BS 328 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 328, RBL 14, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600179 19981126 00179 NM 1998 11 26 SWAA982951 1 19981119 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND I/B CHORD CRACKED AT BS 616, LBL 64.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600180 19981126 00180 NM 1998 11 26 SWAA982952 1 19981119 A 5320 BEAM BOEING 737 7373H4 1384600 NM BS 500-516 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND FLOOR SUPPORT BEAM CORRODED AT BS 500C+16. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600181 19981126 00181 NM 1998 11 26 SWAA982953 1 19981119 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 616 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND LOWER SIDE OF CREASE BEAM WEB CORRODED AT BS 616, LBL 67. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600182 19981126 00182 NM 1998 11 26 SWAA982954 1 19981119 A 5240 FRAME BOEING 737 7373H4 1384600 NM SERVICE DOOR CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND FWD SERVICE DOORWAY UPPER FWD FRAME CRACKED AT BS 296, RBL 48, WL 269. REPLACED PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998112600183 19981126 00183 NM 1998 11 26 SWAA982955 1 19981119 A 5312 BULKHEAD CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND SIDE CHORDS CRACKED IN RADIUS OF CHORD AT BS 178, LBL 29 AND RBL 29, WL 207. REPLACED P ER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600184 19981126 00184 NM 1998 11 26 SWAA982956 1 19981119 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 1006 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 1006, S20R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600185 19981126 00185 NM 1998 11 26 SWAA982957 1 19981122 A 5730 SKIN BOEING 737 7372H4 138448C NM LT WING DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 063SW 22061 NR 3 SLAT I/B AUX TRACK CUTOUT SKIN DAMAGED. REPAIRED PER SWA RA 1-257-0598. 2 L 7 2 4F A16WE 1998112600186 19981126 00186 NM 1998 11 26 SWAA982958 1 19981119 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 752-758 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 752 TO 758 BETWEEN S8-9L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600187 19981126 00187 NM 1998 11 26 SWAA982959 1 19981119 A 5730 SKIN BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND LT WING L/E BULLNOSE CRACKED AT LOWER EDGE OF NR 3 SLAT I/B STOP. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1998112600188 19981126 00188 NM 1998 11 26 SWAA982960 1 19981119 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND FRAME FAIL/SAFE CHORD CORRODED AT BS 907, RBL 31, WL 173. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600189 19981126 00189 NM 1998 11 26 SWAA982961 1 19981119 A 5320 CHORD BOEING 737 7372H4 138448C NM BS 185-188 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND LOWER CHORD DAMAGED AT BS 185 TO 188, AT S10L, WL 233. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600190 19981126 00190 NM 1998 11 26 SWAA982962 1 19981119 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, AT S4L. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600191 19981126 00191 NM 1998 11 26 SWAA982963 1 19981119 A 5320 SUPPORT BOEING 737 7372H4 138448C NM BS 540 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND FLOORBEAM SUPPORT DAMAGED AT BS 540. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600192 19981126 00192 NM 1998 11 26 SWAA982964 1 19981119 A 2710 DOUBLER BOEING 737 7372H4 138448C NM BS 678 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND CRACK IN AILERON QUADRANT DOUBLER AT BS 678, LBL AND RBL 25, WL 206. REPLACED PER BOEIN G SRM. 2 L 7 2 4F A16WE 1998112600193 19981126 00193 NM 1998 11 26 SWAA982965 1 19981119 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 400 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND CRACK IN FUSELAGE FRAME AT BS 400, 3 ABOVE S21L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600194 19981126 00194 NM 1998 11 26 SWAA982966 1 19981119 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, REPLACED FUSELAGE SKIN LAP REPAIR AT BS 727A+10. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600195 19981126 00195 NM 1998 11 26 SWAA982967 1 19981119 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND CRACK AT WL 218, LBL 11 TO 12, BS 178. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600196 19981126 00196 NM 1998 11 26 SWAA982968 1 19981119 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 500 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND FUSE FRAME DENTED AT BS 500, S23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600197 19981126 00197 NM 1998 11 26 SWAA982969 1 19981119 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 911 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D CHECK, FOUND FUSE SKIN DENTED AT BS 911, 2 BELOW S17R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998112600198 19981126 00198 NM 1998 11 26 SWAA982970 1 19981118 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 775 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED BC4 CHECK, FOUND A 2.5 FUSELAGE SKIN CRACK AT BS 775, S23. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600199 19981126 00199 NM 1998 11 26 SWAA982971 1 19981118 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND A 2.3 FLOOR BEAM CRACK AT BS 540, LBL 24. REPAIRED PER SWA ACO 3198-53 AND BOEING DR AWING 65C34688. 2 L 7 2 4F RT A16WE 1998112600200 19981126 00200 NM 1998 11 26 SWAA982972 1 19981118 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND A 2 INCH FLOORBEAM CRACK AT BS 540, RBL 45. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600201 19981126 00201 NM 1998 11 26 SWAA982973 1 19981118 A 5330 SKIN BOEING 737 737301 1384611 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK BELOW EMERGENCY ESCAPE LIGHT LT SIDE BEHIND AFT WING TO BODY FAIRING. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600202 19981126 00202 NM 1998 11 26 SWAA982974 1 19981118 A 3350 20131A BATTERY BOEING 737 737301 1384611 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998112600203 19981126 00203 NM 1998 11 26 SWAA982975 1 19981119 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM FUSELAGE CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 986.5, LBL 25, 40, 43, WL 208. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600204 19981126 00204 NM 1998 11 26 SWAA982976 1 19981118 A 5312 BULKHEAD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACK AT WL 197-201, LBL 4.7, WL 210-212, LBL 6.7, WL 200-201, RBL 4.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600205 19981126 00205 NM 1998 11 26 SWAA982977 1 19981118 A 2170 COALESCER BOEING 737 7372T4 1384492 NM LT ACM DIRTY A SWAA K NONE O OTHER CR CRUISE 1 SW 07 721WN 22697 DURING CRUISE, CREW DETECTED A STRONG UNIDENTIFIABLE SMELL IN COCKPIT AND CABIN. DESCENDED TO 24,000 AND ISOLATED LEFT PACK. ODOR DISSAPATED, CONTINUED PER MEL 21-1. REPLACED COALESOR BAG AND SERVICED AIR CYCLE MACHINE PER BOEING M/M. 2 L 7 2 4F A16WE 1998112600206 19981126 00206 NM 1998 11 26 SWAA982978 1 19981118 A 5247 SKIN BOEING 737 7373H4 1384600 NM APU DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D CHECK, FOUND APU DOOR SKIN DENTED 2 PLACES. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600207 19981126 00207 NM 1998 11 26 SWAA982979 1 19981118 A 5315 FLOORBEAM BOEING 737 7373H4 1384600 NM COCKPIT CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED RON, FOUND COCKPIT FLOORBEAM CORROSION. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998112600208 19981126 00208 1998 11 26 SWAA982980 4 19981119 A 2565 0250072 SLIDE BOEING 737 7372H4 138448C NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 059SW 21811 DURING SCHEDULED ANNUAL SAMPLE EMERGENCY ESCAPE SLIDE OPERATIONAL CHECK PROGRAM, SLIDE, S/N 2825, FAILED DEPLOYMENT CHE CK DUE TO A HOLE. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1998112600240 19981126 00240 EA 1998 11 26 98ZZZX4303 2 19981023 A 7230 GAS GENERATOR STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45 52043 EA RT ENGINE FAILED A DATA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 13 55AN 4653 SH3025 PCE84314 AIRCRAFT DEPARTED, ABOUT 5 MINUTES AFTER LEVELING OFF, RT ENGINE SPUN DOWN. LANDED BACK AT BASE WITH SINGLE ENGINE, WIT HOUT TRYING TO RESTART IT. NOTICED THE RIGHT TORQUE GAUGE DROPPED, BUT DISREGARDED IT BECAUSE ALL OTHER GAUGES WERE NOR MAL. MECHANIC DISPATCHED AND INSPECTED ALL LINKAGES AND CONNECTIONS OF ENGINE COMPONENTS. MAXIMUM POWER RUN DONE ON GR OUND - NORMAL. DRAINED FUEL OK. FLIGHT CHECK REVEALED PROPELLER TACH AND GG INDICATOR FLUCTUATED. CHANGED. OPS CHECK OK. 2 H 7 2 4T 4 T A41EU E4EA 1998112600241 19981126 00241 EA 1998 11 26 98ZZZX4304 2 19981026 A 7230 GAS GENERATOR STBROS SD3 SD330 8100602 EU PWA PT6 PT6A45R 52043 EA RT ENGINE FAILED A DATA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 GL 13 55AN 4654 SH3025 PCE84314 PILOT REPORTED RIGHT ENGINE SHUT DOWN IN-FLIGHT. THE PROPS AUTOFEATHERED AND THE ENGINE WOULD NOT RELIGHT. THE MECHANI CS REMOVED AND REPLACED THE RT FUEL PUMP AND FUEL CONTROL UNIT. THEY RIGGED THE ASSEMBLY. OPS CHECK GOOD. 2 H 7 2 4T 4 T A41EU E4EA 1998112600246 19981126 00246 WP 1998 11 26 98ZZZX4309 2 19981019 A 7230 30736383 FAN BLADE LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP RT ENGINE FAILED A VLLA O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 GL 05 108RB 097 74544 ON DESCENT INTO HWO, PILOTS FELT RT ENGINE VIBRATION. PILOTS REDUCED POWER AND LANDED HWO. FOUND FRONT FAN BLADE MID-S PAN DAMPENER MISSING FROM FAN BLADE. CYCLES: 3,766. 2 L 7 2 4F 4 F A10CE E6WE 1998112600270 19981126 00270 NM 1998 11 26 98ZZZX4333 1 19980901 A 3211 FITTING PIPER PA60 PA60600 7106001 NM WING CRACKED A DKBA K NONE O OTHER IN INSP/MAINT 1 SO 09 801MA 600433147 DURING AAIP INSPECTION, LEFT WING, LOWER SIDE, AT THE GEAR ATTACHMENT POINT, WAS FOUND WITH A CRACK. THIS CRACK IS BEYO ND THE ALLLOWABLE LIMITS AS SPECIFIED BY THE AEROSTAR SM AND SB 600-66. 1 M 7 2 3O RT A17WE 1998112600271 19981126 00271 NM 1998 11 26 98ZZZX4334 1 19980902 A 3211 FITTING PIPER PA60 PA60600 7106001 NM WING CRACKED A DKBA K NONE O OTHER IN INSP/MAINT 1 SO 09 876SM 600340124 DURING AAIP INSPECTION, LEFT WING, LOWER SIDE, AT THE GEAR ATTACHMENT POINT, WAS FOUND WITH A CRACK. THIS CRACK IS BEYO ND THE ALLLOWABLE LIMITS AS SPECIFIED BY THE AEROSTAR SM AND SB 600-66. 1 M 7 2 3O RT A17WE 1998112600287 19981126 00287 NE 1998 11 26 98ZZZX4350 2 19981029 A 7310 430137601 FUEL MANIFOLD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 2 ENGINE LEAKING A HEEA A UNSCHED LANDING K FLUID LOSS NR NOT REPORTED 1 SW 03 911RZ 1PJ01160 7092 LE45091AE DURING FLIGHT, MEDIC NOTICED FUEL DRIPPING ON THE SIDE WINDOW. AIRCRAFT WAS LANDED AT LAFAYETTE HELIPORT. FOUND NR 2 E NGINE MANIFOLD LEADING. REF: LTS-101-4-7 IPC, CHAPTER 73-10-00, FIGURE 3, ITEM 15D. 1 G 7 2 3U 3 U H13EU E5NE 1998112600296 19981126 00296 WP 1998 11 26 TWAA9818701 1 19981119 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 1081 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT, FOUND TAIL TO FUSELAGE ANGLE IN DORSAL FIN CRACKED FROM SCREW HOLE TO EDGE, ON RT SIDE AT STA 1081 . REMOVED CRACKED ANGLE AND REPLACED WITH NEW ANGLE (P/N SR09530162-4), PER SB 53-223 REV 2, AND ARA 15725. 2 L 7 2 4F A6WE 1998112600297 19981126 00297 NM 1998 11 26 HNAA9898080 1 19981119 A 3350 6104791X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 980HA 376 HVN - FLT 3091 - NUMEROUS INTERIOR/EXTERIOR EMERGENCY LIGHTS OUT. REPLACED ALL EMERGENCY BATTERY POWER SUPPLIES. OPS C HECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998112600298 19981126 00298 NM 1998 11 26 HNAA9899381 1 19981119 A 3350 6013211X POWER SUPPLY DHAV DHC8 DHC8201 2809001 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 993HA ORF57 457 MIA - FLT 3054 - NR 3 AND NR 4 FORWARD CABIN ESCAPE PATH RED LIGHTS INOPERATIVE. REPLACED BATTERY POWER SUPPLY AND POWE R SUPPLY BASE. OPERATIONAL CHECK GOOD. (X) 2 H 7 2 4T RT A13NM 1998112600299 19981126 00299 NM 1998 11 26 VJ9800617 1 19981031 A 5280 65494427 FITTING BOEING 737 737222 1384473 NM LT MLG DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 468AT 19074 LT MLG OUTER DOOR SUPPORT BEAM ATTACH FITTING, AFT SIDE OF REAR SPAR, HAS FRETTED CORROSION. REPLACED SUPPORT BEAM ATTA CH FITTING IAW B737 SRM 57-15-01. 2 L 7 2 4F A16WE 1998112600300 19981126 00300 WP 1998 11 26 VJ9800618 1 19981020 A 5720 5910042503 VANE DOUG DC9 DC932 3022066 WP LT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 LT WING CENTER FIXED VANE FLAP L/E CORRODED. REPLACED FIXED VANE IAW DC9 MM 27-51-3. FIT AND FAIRED, OPS CHECKED GOOD IAW DC9 MM 27-51-3. 2 L 7 2 4F A6WE 1998112600301 19981126 00301 WP 1998 11 26 VJ9800619 1 19981022 A 2760 39209445033923 MECHANISM DOUG DC9 DC932 3022066 WP WS 307 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 RT O/B SPOILER CAM ARM, TORSION ARM AND TORSION BAR AT XRS 307, SERRATION FOUND PITTED CORRODED. REPLACED TORSION BAR ( 3920944-503), CAM ARM ASSY ( 3923153-505) AND TORSION ARM (3920944-503) IAW DC9 MM 27-61-1 AND 27-61-6. 2 L 7 2 4F A6WE 1998112600302 19981126 00302 WP 1998 11 26 VJ9800620 1 19981022 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218-588 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 937VV 45774 FUSELAGE SKIN AT FS 218 TO 588R, L18-L27, DENTED. REPLACED SKIN IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2, MM 34-10-0 AND A IRTRAN RES 191790 WITH DER APPROVAL BY DM BURCH NR NM1034. 2 L 7 2 4F A6WE 1998112600303 19981126 00303 WP 1998 11 26 VJ9800621 1 19981119 A 4930 S9027E267 O-RIING DOUG DC9 DC932 3022066 WP APPU COMPT FAILED A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 921VV 47284 AFTER TAKEOFF FLIGHT CREW PERCEIVED THE ODOR OF FUMES IN COCKPIT AND ELECTED TO RETURN TO ATL MAINTENANCE BASE. INVESTI GATED BY MAINTENANCE AND FOUND FUEL SHROUD GOING TO APU TO NOT BE PROPERLY SEATED. REPLACED O-RING AND SEAL TO INSURE I NTEGRITY OF FUEL LINE SHROUD. AS PRECAUTIONARY MEASURE REPLACED COALESCER BAGS. 2 L 7 2 4F A6WE 1998112600304 19981126 00304 WP 1998 11 26 VJ9800622 1 19981122 A 3230 59104475009 RETRACT MECH DOUG DC9 DC932 3022066 WP NLG MALFUNCTIONED A ZZDA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 966VV 47168 NLG WOULD NOT RETRACT AFTER TAKEOFF. ALL GEAR INDICATIONS NORMAL WITH GEAR IN DOWN POSITION. CREW ELECTED TO RETURN TO DEPARTING STATION. INSPECTED GEAR FOR BROKEN, MISSING PARTS, AND LEAKS; NONE FOUND. PINNED GEAR AND FERRIED AIRCRAFT TO ATL MAINTENANCE BASE. PERFORMED FURTHER CHECKS BY JACKING AND RETRACTING GEAR AND NO DEFECTS NOTED; LUBRICATED GEAR AND ALL WITHING LIMIT IAW MM 32-20-0 AND 32-30-0. 2 L 7 2 4F A6WE 1998112600305 19981126 00305 WP 1998 11 26 CALA9802085 1 19981120 A 3350 EMBS13922 BATTERY PACK ENGMAGNETICS DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14075 46922 THE EMERGENCY LIGHTS WOULD NOT TEST DURING PREDEPARTURE CHECK. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK AN D CHARGER AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1998112600306 19981126 00306 WP 1998 11 26 CALA9802086 1 19981120 A 3350 EMSE299A BATTERY PACK AMIIND DOUG DC10 DC1030 3023501 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19072 46576 INSPECTION FOUND FIRST CLASS AREA EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD. 2 L 7 3 4F A22WE 1998112600307 19981126 00307 WP 1998 11 26 CALA9802087 1 19981121 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 226 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 226, LONGERON 17L. REPAIRED IAW SRM 53-04, FIGURE 47. 2 L 7 2 4F A6WE 1998112600308 19981126 00308 WP 1998 11 26 CALA9802088 1 19981121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 230 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND SEAT TRACK CORRODED AT STA 230. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1998112600309 19981126 00309 WP 1998 11 26 CALA9802089 1 19981121 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 200-240 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND RT CENTER SEAT TRACK CORRODED AT STA 200 TO 240. THE SEAT TRACK WAS REPLACED IAW SRM 53-05, FIGURE 4F. 2 L 7 2 4F A6WE 1998112600310 19981126 00310 WP 1998 11 26 CALA9802090 1 19981121 A 5312 BULKHEAD WEB DOUG DC9 DC982 3022082 WP BS 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND A 6 INCH CRACK IN WEB SECTION AT TAIL COMPARTMENT CANTED BULKHEAD STA 1463. THE WEB SECTION WAS REMOV ED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998112600311 19981126 00311 WP 1998 11 26 CALA9802091 1 19981121 A 5530 ANGLE DOUG DC9 DC982 3022082 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 69803 49229 INSPECTION FOUND A .625 INCH CRACK IN LT VERTICAL STABILIZER ANGLE 37.5 INCHES AFT OF STA 1089.5. REPAIRED IAW SRM 55-0 2, FIGURE 26. 2 L 7 2 4F A6WE 1998112600312 19981126 00312 EA 1998 11 26 COMA9860359 1 19981122 A 2910 6007522660 TUBING CNDAIR CL600 CL6002B19 EA NR 3 HYD SYST FAILED A COMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 01 991CA 4931 7216 AFTER FLT DEPT CAE, NR 3 HYDRAULIC QUANTITY READ ZERO. NOSE GEAR INDICATED DOWN, ONE MAIN INDICATED UP, THE OTHER MAIN INTRANSIT. CREW EXTENDED GEAR MANUALLY. FLT DECLARED AN EMERGENCY AND DIVERTED BACK TO CAE. FLT LANDED IN CAE WITHOUT FURTHER INCIDENT. INSTALLED NEW HYD TUBING (P/N 600-75226-60), (S/N 1307718), PERFORMED LEAK CHECK AFTER SWAGING. NO DISCREPANCIES NOTED. 2 L 7 2 4F RT A21EA 1998112600313 19981126 00313 EA 1998 11 26 COMA9860360 1 19981121 A 3030 7858062 HEAT CONTROLLER CNDAIR CL600 CL6002B19 EA NR 2 ADS MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 976CA 7151 TAT AND AOA HEAT CAUTION MESSAGE ON EICAS. REPLACED THE NR 2 ADS HEAT CONTROLLER. 2 L 7 2 4F RT A21EA 1998112600314 19981126 00314 NE 1998 11 26 COMA9860361 2 19981119 A 7321 6078T55P09 FUEL CONTROL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE RT ENGINE MALFUNCTION A COMA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 SO 01 971CA 4432 7145 807424 UNABLE TO REDUCE POWER BELOW 60 PERCENT N1. RIGHT HAND ENGINE (IFSD). REPLACED THE FUEL CONTROL. 2 L 7 2 4F 4 F RT A21EA E15NE 1998112600315 19981126 00315 EA 1998 11 26 COMA9860362 1 19981120 A 3350 LIGHT CNDAIR CL600 CL6002B19 EA ROW 2 & 5 CONTAMINATED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 977CA 7157 EMERGENCY FLOOR LIGHTING ROWS 2 AND 5 ARE INOPERABLE. REMOVED MOISTURE FROM FLOOR PATH LIGHT TRACK, SYSTEM TEST SATISFA CTORY. 2 L 7 2 4F RT A21EA 1998112600316 19981126 00316 NM 1998 11 26 UPS98228228 1 19981120 A 3350 LIGHT BOEING 727 72725C 138400H NM CABIN INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 947UP 19722 INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT ASSY, OPERATION CK GOOD (P/N 96-3-1010) (S/N 101 5) ON, (S/N 1004). 2 L 7 3 4F A3WE 1998112600317 19981126 00317 NE 1998 11 26 UPS98228229 2 19981120 A 7314 378200 FUEL PUMP BOEING 727 727247 138408F NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE FAILED A IPXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 207UP 21699 INSPECTION TYPE-N/A, CLIMBING OUT OF 700 FT AGL NR 1 ENGINE FAILED. CHECKLIST RUN ENGINE WAS IN RESTART ENVELOPE, RESTA RT ATTEMPT UNSUCCESSFUL OIL PRESS AND INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 FUEL CONTROL AND FUEL PUMP PER MM 7 3-21-1 AND 73-11-1, RUN CK GOOD. 2 L 7 3 4F 4 F A3WE E2EA 1998112600318 19981126 00318 WP 1998 11 26 UPS98828212 1 19981020 A 5320 INTERCOSTAL DOUG DC8 DC871F 302199D WP BS 970 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, INTERCOSTAL BETWEEN MLG DOORS FS 970 CRACKED, WORN AND LOOSE BRACKETS. REMOVED INTERCOSTAL, DRILLED NEW INTERCOSTAL TO FIT IAW DC8 SRM 51-1 -24. INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998112600319 19981126 00319 WP 1998 11 26 UPS98828213 1 19981022 A 5320 ANGLE DOUG DC8 DC871F 302199D WP CARGO COMPT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, CORROSION ON CUSP TO FRAME ANGLE, FWD OF FRAME 140 AT L21R. REMOVED CORRODED FITTING, LOCATED AND DR ILLED NEW FITTING IAW DC8 SR M 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998112600320 19981126 00320 WP 1998 11 26 UPS98828214 1 19981020 A 5320 FRAME DOUG DC8 DC871F 302199D WP BS 1700 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, FRAME CORRODED BETWEEN LONGERONS 35 LT TO 35 RT AT STA 1700. REMOVED CORROSION FOUND TO BE OUT OF LI MITS IAW DC8 SRM 51-1-8. FABRICATED NEW ANGLE, ALODINED, PRIMED AND INSTALLED ANGLE. 2 L 7 4 4F RT 4A25 1998112600321 19981126 00321 WP 1998 11 26 UPS98828215 1 19981022 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1717 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, AT LONGERON 11L STA 1717 CRACKED AT MAIN FRAME. REMOVED CRACKED SECTION FABRICATED NEW AND INSTALLED IAW DC8 SRM 53- 2-0, 51-1-20D, 51-1-8, 53-5-1. 2 L 7 4 4F RT 4A25 1998112600322 19981126 00322 WP 1998 11 26 UPS98828216 1 19981104 A 5400 FITTING DOUG DC8 DC871F 302199D WP NR 1 PYLON CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, NR 1 PYLON THROUGH PANEL 197B FIRST RT VERTICAL STIFFENER LWR ATTACH FITTING CORRODED. REMOVED OLD F ITTING, RCD NEW FITTING FROM MACHINE SHOP DRILLED HOLES AND INSTALLED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1998112600323 19981126 00323 WP 1998 11 26 UPS98828217 1 19981019 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 978 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, CORROSION AROUND FASTENERS AT TOP OF LT CORNER OF MLG WHEEL WELL WEB ATTACH PLATES, STA 978. FOUND F ITTING TO BE CRACKED. REMOVED AND REPLACED IAW DC8 SRM 51-1-24 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998112600324 19981126 00324 WP 1998 11 26 UPS98828218 1 19981020 A 5320 DOUBLER DOUG DC8 DC871F 302199D WP BS 1540-1560 CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, AFT ACC COMPARTMENT CORROSION O9N FINGER DOUBLER AT LONGERON 31L-32L FS 1540 TO 1560. FAB NEW SECTIO N OF FINGER DOUBLER IAW 53-4-1, FAB LONGERON SPLICE IAW REO-05809, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IA W DC8 SRM 51-1-21 AND 51-1-20D. 2 L 7 4 4F RT 4A25 1998112600325 19981126 00325 WP 1998 11 26 UPS98828220 1 19981021 A 5350 SKIN DOUG DC8 DC871F 302199D WP TAIL CONE CORROSION A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 744UP 45944 INSPECTION TYPE-D, REMOVED FWD SKIN ON RIGHT SIDE OF TAIL CONE DUE TO CORROSION. FAB NEW SKIN IAW DAC DWG 5644500, ALOD INED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1998112600326 19981126 00326 WP 1998 11 26 UPS98828221 1 19981106 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 672.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, RT WING L/E RIB AT FS 672.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1998112600327 19981126 00327 WP 1998 11 26 UPS98828222 1 19981104 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 55 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, LT FUSELAGE SKIN AT STA 55 AT STR 21R IS CRACKED AT THE DOUBLER. REPAIRED IAW DC8-5330-0793-I. 2 L 7 4 4F RT 4A25 1998112600328 19981126 00328 WP 1998 11 26 UPS98828223 1 19981106 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 950-1010 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, SEAT TRACK AT STA 950 TO 1010 RBL 44 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW DC8-5320-8309-C. 2 L 7 4 4F RT 4A25 1998112600329 19981126 00329 WP 1998 11 26 UPS98828225 1 19981116 A 5320 97540551 TRACK DOUG DC8 DC873F 302199F WP CARGO COMPT CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 894UP 46094 INSPECTION TYPE-C, A PIT CROSS SLIDE DOOR JAMB TORQUE BOX UPPER WEB TRACK BETWEEN STR 36 AND 32R IS CRACKED. REMOVED AN D REPLACED TRACK IAW SRM 51-3-0. 2 L 7 4 4F RT 4A25 1998112600330 19981126 00330 WP 1998 11 26 UPS98828226 1 19981121 A 5730 PANEL DOUG DC8 DC873F 302199F WP RT WING CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 810UP 46001 INSPECTION TYPE-N/A, RT WING LOWER ACCESS PANEL CRACKED AT O/B OF I/B SLOT CUTOUT. PANEL REPLACED. 2 L 7 4 4F RT 4A25 1998112600331 19981126 00331 EU 1998 11 26 QXEA9801688 1 19981029 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT TE FLAP DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 LEFT-HAND INBOARD FLAP UPPER INBOARD TRAILING EDGE HAS 2 DENTS AT APPROXIMATELY STATION 2000 AND 2600. REPAIRED IAW FOK KER SRM 51-10-04, PAGE 2, PARAGRAPH 7C. 2 L 7 2 4F RT A20EU 1998112600333 19981126 00333 EU 1998 11 26 QXEA9801690 1 19981110 A 5711 SPAR FOKKER F28 F28MK4000 4990810 EU WS 4700 DELAMINATED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 LEFT-HAND WING FRONT SPAR LOWER MOUNTING FLANGE FOR INBOARD END OF PANEL 61C AT STATION 4700 HAS ONE LAYER DELAMINATING. REPAIRED IAW FOKKER SRM 51-10-04, PARAGRAPH 4B (2). 2 L 7 2 4F RT A20EU 1998112600334 19981126 00334 EU 1998 11 26 QXEA9801691 1 19981104 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 19975-20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 FUSELAGE SKIN CRACKED AT FOUR RIVETS BETWEEN FRAMES 19976 AND 20075 AND STRINGERS 38 AND 39. REPAIRED IAW HORIZON AIR E A 4-53-585. 2 L 7 2 4F RT A20EU 1998112600335 19981126 00335 EU 1998 11 26 QXEA9801692 1 19981107 A 5755 LINK FOKKER F28 F28MK4000 4990810 EU LT SPEED BRAKE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 SPEED BRAKE LEFT-HAND SUPPORT LINK CHAFING ON COMPOSITE TAIL CONE AT UPPER AND LOWER ARMS. REPAIRED IAW HORIZON AIR EA 4-55-103. 2 L 7 2 4F RT A20EU 1998112600336 19981126 00336 EU 1998 11 26 QXEA9801693 1 19981029 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU BS 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 FRAME 17565 HAS CRACKED CLIP AT STRINGER 56. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601 A. 2 L 7 2 4F RT A20EU 1998112600337 19981126 00337 EU 1998 11 26 QXEA9801694 1 19981031 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 16-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 OBLIQUE FRAME 16-2 HAS CRACKED REPAIR ANGLE ON AFT SIDE BETWEEN STRINGER 33 AND V-SKIN CUTOUT. REPAIRED IAW FOKKER SRM 53-02-12, PAGE 4, FIGURE 3. 2 L 7 2 4F RT A20EU 1998112600338 19981126 00338 EU 1998 11 26 QXEA9801696 1 19981103 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 LEFT-HAND FUSELAGE SKIN HAS CHAFE DAMAGE AT PANEL 91BD. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600339 19981126 00339 EU 1998 11 26 QXEA9801697 1 19981103 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 RIGHT-HAND FUSELAGE AFT OF WING FAIRING AT PANEL 92BD HAS DAMAGE FROM 92BD RUBBING FUSELAGE SKIN. REPAIRED IAW FOKKER S RM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600340 19981126 00340 EU 1998 11 26 QXEA9801698 1 19981017 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACK IN A CLIP AT FRAME 5305 AT STRINGER 39. REPAIRED IAW FOKKER SRM 53-02-13, AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600341 19981126 00341 EU 1998 11 26 QXEA9801701 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACK IN A CLIP AT FRAME 7805 AT STRINGER 34. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600342 19981126 00342 EU 1998 11 26 QXEA9801702 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACK IN A CLIP AT FRAME 5805 AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600343 19981126 00343 EU 1998 11 26 QXEA9801703 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACK IN A CLIP AT FRAME 5805 AT STRINGER 41. REPAIRED IAW FOKKER SRM 53-02-13, AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600344 19981126 00344 EU 1998 11 26 QXEA9801704 1 19981019 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 FRAME CASTELLATION AT FRAME 10966, STRINGER 43 HAD A CRACK. REPAIRED IAW FOKKER SRM 51-31-01, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1998112600345 19981126 00345 EU 1998 11 26 QXEA9801705 1 19981019 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 FRAME CASTELLATION AT FRAME 10346 AT STRINGER 32 HAD A CRACK. REPAIRED IAW FOKKER SRM 51-31-01 PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1998112600346 19981126 00346 EU 1998 11 26 QXEA9801706 1 19981019 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 FRAME CASTELLATION AT FRAME 10346, STRINGER 44 HAS A CRACK. REPAIRED IAW FOKKER SRM 51-31-01 PARAGRAPH 7 PAGE 13-17. 2 L 7 2 4F RT A20EU 1998112600347 19981126 00347 EU 1998 11 26 QXEA9801707 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 3805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 CLIP REPAIR IS CRACKED AT FRAME 3805, STRINGER 30. REPAIRED IAW FOKKER SRM 53-02-13 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600348 19981126 00348 EU 1998 11 26 QXEA9801708 1 19981019 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 FRAME CASTELLATION CRACKED AT FRAME 5805, STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13 AND 51-31-01. 2 L 7 2 4F RT A20EU 1998112600349 19981126 00349 EU 1998 11 26 QXEA9801709 1 19981104 A 5220 DOOR FOKKER F28 F28MK4000 4990810 EU RT EMER EXIT CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 RIGHT-HAND FORWARD OVERWING EMERGENCY EXIT DOOR HAS A CRACK IN LOWER AFT AS SEEN THROUGH LIGHTENING HOLE. REPAIRED IAW HORIZON AIR EO 4-52-21 E. 2 L 7 2 4F RT A20EU 1998112600350 19981126 00350 EU 1998 11 26 QXEA9801710 1 19981016 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 14755 AND STRINGER 49. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998112600351 19981126 00351 EU 1998 11 26 QXEA9801711 1 19981016 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 13815A AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13 FIGURE 2. 2 L 7 2 4F RT A20EU 1998112600352 19981126 00352 EU 1998 11 26 QXEA9801712 1 19981016 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 13815A AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1998112600353 19981126 00353 EU 1998 11 26 QXEA9801713 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 13815A AND STRINGER 33. REPAIRED IAW FOKKER SRM 51-10-4, STEP 4 AND SRM 51-31-01, PARA GRAPH 7, PAGE 13-17. 2 L 7 2 4F RT A20EU 1998112600354 19981126 00354 EU 1998 11 26 QXEA9801714 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 13815 AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARA GRAPH 7. 2 L 7 2 4F RT A20EU 1998112600355 19981126 00355 EU 1998 11 26 QXEA9801715 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 12875 AND STRINGER 45. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARA GRAPH 7. 2 L 7 2 4F RT A20EU 1998112600356 19981126 00356 EU 1998 11 26 QXEA9801716 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 12875 AND STRINGER 44. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARA GRAPH 7, PAGES 13-17. 2 L 7 2 4F RT A20EU 1998112600357 19981126 00357 EU 1998 11 26 QXEA9801717 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 12875 AND STRINGER 42. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-01, PARA GRAPH 7. 2 L 7 2 4F RT A20EU 1998112600358 19981126 00358 EU 1998 11 26 QXEA9801718 1 19981019 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THERE IS A CRACKED CLIP AT FRAME 12405 AND STRINGER 43. REPAIRED IAW FOKKER SRM 51-10-04, STEP 4 AND SRM 51-31-07, PARA GRAPH 7. 2 L 7 2 4F RT A20EU 1998112600359 19981126 00359 EU 1998 11 26 QXEA9801719 1 19981030 A 5320 SIDEWALL FOKKER F28 F28MK4000 4990810 EU RT ACM COMPT DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 DENT IN SIDE WALL BY LOWER AFT ACM MOUNT, RIGHT-HAND ACM. REPAIRED IAW FOKKER SRM 53-02-01, FIGURE 9 PAGE 11 AND HORIZO N AIR EA 4-53-579. 2 L 7 2 4F RT A20EU 1998112600360 19981126 00360 EU 1998 11 26 QXEA9801720 1 19981027 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 AFT CARGO PIT FRAME 13815A STRINGER 72 CRACKED CLIP. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998112600361 19981126 00361 EU 1998 11 26 QXEA9801721 1 19981028 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 4900 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 484US 11234 THE FLOOR SUPPORT IS CRACKED AT CLIP LOCATED AT FRAME 4900 BETWEEN AND ABOVE STRINGERS 70 AND 71. REPAIRED IAW FOKKER S RM 51-31-05. 2 L 7 2 4F RT A20EU 1998112600362 19981126 00362 EU 1998 11 26 98FDEA00710 1 19981120 A 2430 MODULE AIRBUS 300 A300F4605R 3930327 EU NR 3 BATTERY FAILED A FDEA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 25 667FE 771 NR 3 BATTERY STRONG ODOR PRESENT, BATTERY INDICATED AMBER, THEN OFF. REMOVED AND REPLACED DIODE MODULES 64VD AND 65VD. 2 L 7 2 4F RT A35EU 1998112600363 19981126 00363 WP 1998 11 26 ABXA9801063 1 19981026 A 5320 59203311B FITTING DOUG DOUG DC9 DC931 3022065 WP BS 579-598 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 30 END FITTING CORRODED BETWEEN STATION 579 AND 598. REPLACED LONGERO N END FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998112600364 19981126 00364 WP 1998 11 26 ABXA9801064 1 19981024 A 5320 DO489822 WEB DOUG DOUG DC9 DC931 3022065 WP BS 601 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE RIGHT CUSP WEB CRACKED AT STATION 601. REPLACED RIGHT CUSP WEB BETWEEN STA TION 598 AND 646 IAW DC9 SRM 51-10-3B AND 51-30-2. 2 L 7 2 4F A6WE 1998112600365 19981126 00365 WP 1998 11 26 ABXA9801065 1 19981026 A 5313 SRO95J013715 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 579-585 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 30 CRACKED BETWEEN STATION 579 AND 585. REPLACED LONGERON SECTION IAW DC9 SRM CHAPTER 53-02. 2 L 7 2 4F A6WE 1998112600366 19981126 00366 WP 1998 11 26 ABXA9801066 1 19981022 A 5312 9915558236N BULKHEAD CLIP DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD 2ND RADIAL CRACKED AT END CLIP. REPLACED CLIP IAW DC 9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998112600367 19981126 00367 WP 1998 11 26 ABXA9801067 1 19981021 A 5720 99100105 DOUBLER DOUG DOUG DC9 DC931 3022065 WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT WING REAR SPAR DOUBLER CRACKED OUTBOARD OF TRAPEZOIDAL PANEL. REPAIRE D IAW ABX REA D957-25131MR. 2 L 7 2 4F A6WE 1998112600368 19981126 00368 WP 1998 11 26 ABXA9801068 1 19981020 A 5752 5710047502 TAB DOUG DOUG DC9 DC931 3022065 WP RT AILERON DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE RIGHT AILERON CONTROL TAB HAD INTERNAL WATER INTRUSION. REPLACED RIGHT AIL ERON CONTROL TAB IAW DC9 MM CHAPTER 27-10-2. 2 L 7 2 4F A6WE 1998112600369 19981126 00369 WP 1998 11 26 ABXA9801069 1 19981006 A 5730 59127351 PANEL DOUG DOUG DC9 DC931 3022065 WP LT WING DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT WING OUTBOARD TRAILING EDGE PANEL DELAMINATED. REPLACED PANEL IAW DC9 SRM. 2 L 7 2 4F A6WE 1998112600370 19981126 00370 WP 1998 11 26 ABXA9801070 1 19981021 A 5730 591216148 PANEL DOUG DOUG DC9 DC931 3022065 WP WS 101 DELAMINATED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND RIGHT WING LOWER INBOARD TRAILING EDGE PANEL AT XRS 101 DELAMINATED. REPLACED PANEL IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998112600371 19981126 00371 WP 1998 11 26 ABXA9801071 1 19981013 A 5720 99100105 DOUBLER DOUG DOUG DC9 DC931 3022065 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND RIGHT WING REAR SPAR DOUBLER CRACKED OUTBOARD OF TRAPEZOIDAL PANEL. REPAIRED I AW ABX REA D957-25132MR. 2 L 7 2 4F A6WE 1998112600372 19981126 00372 WP 1998 11 26 ABXA9801072 1 19981009 A 5313 591140617N LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 4 LEFT CRACKED AT STATION 160. REPLACED LONGERON 4L AT STATION 160 IA W DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998112600373 19981126 00373 WP 1998 11 26 ABXA9801073 1 19980816 A 5730 5611350 SKIN DOUG DOUG DC8 DC861 3021952 WP WS 310.25 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 FOUND CORROSION, LEFT WING EXTERIOR AT XFS 310.250. REPAIRED IAW ABX REA D857-17806MR. 2 L 7 4 4F 4A25 1998112600374 19981126 00374 WP 1998 11 26 ABXA9801074 1 19980816 A 5313 5750198 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 920 CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 FOUND CORROSION AND CRACK ON LONGERON 24 AT STATION 920 IN RIGHT WHEEL WELL. REPAIRED IAW DC8 SRM 53-2-2. 2 L 7 4 4F 4A25 1998112600375 19981126 00375 WP 1998 11 26 ABXA9801075 1 19980816 A 5730 56433215 SKIN DOUG DOUG DC8 DC861 3021952 WP LT WING CORROSION A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 DEEP CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN. REPAIRED IAW ABX REA D857-17828MR. 2 L 7 4 4F 4A25 1998112600376 19981126 00376 WP 1998 11 26 ABXA9801076 1 19980816 A 5330 57552713 SKIN DOUG DOUG DC8 DC861 3021952 WP BS 360-380 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 CORROSION FOUND UNDER SKIN AT STATION 360 TO 380, STRINGER 35L. REPAIRED IAW ABX REA D853-17894MR. 2 L 7 4 4F 4A25 1998112600377 19981126 00377 WP 1998 11 26 ABXA9801077 1 19980816 A 5320 36469561 STIFFENER DOUG DOUG DC8 DC861 3021952 WP BS 940 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 LEVEL 2 CORROSION ON STIFFENER AT LONGERON 24L, STATION 940, LEFT WHEEL WELL. REPAIRED IAW ABX REAS D853-17845 AND D853 -17844. 2 L 7 4 4F 4A25 1998112600378 19981126 00378 WP 1998 11 26 ABXA9801078 1 19980816 A 5720 5641251512 INTERCOSTAL DOUG DOUG DC8 DC861 3021952 WP WS 13.25 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 RIGHT WING LEADING EDGE CORROSION ON INTERCOSTAL AND INNER DOUBLER AT STATION XFS 13.250. REPAIRED IAW ABX REA D857-178 31. 2 L 7 4 4F 4A25 1998112600379 19981126 00379 WP 1998 11 26 ABXA9801079 1 19980818 A 5330 577331151 SKIN DOUG DOUG DC8 DC861 3021952 WP BS 1640-1660 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 CORROSION ON LOWER SKIN BETWEEN STATION 1640 TO 1660 LONGERON 22R-26R. REPAIRED IAW ABX REA D853-17876MR. 2 L 7 4 4F 4A25 1998112600380 19981126 00380 WP 1998 11 26 ABXA9801080 1 19980816 A 5330 9755584503 SKIN DOUG DOUG DC8 DC861 3021952 WP BS 1280-1300 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 LEVEL 2 CORROSION ON CUSP UPPER SKIN BETWEEN STATION 1280 TO 1300, LEFT SIDE. REPAIRED IAW ABX D853-17871MR. 2 L 7 4 4F 4A25 1998112600381 19981126 00381 WP 1998 11 26 ABXA9801081 1 19980515 A 5320 57549923 WEB DOUG DOUG DC8 DC861 3021952 WP BS 680 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 LEVEL 2 CORROSION ON LOWER WEB BETWEEN STRINGER 36L - 35L, STATION 680 LOWER SKIN. REPAIRED IAW ABX REA D853-17877. 2 L 7 4 4F 4A25 1998112600382 19981126 00382 WP 1998 11 26 ABXA9801082 1 19980816 A 5713 5643321102 STRINGER DOUG DOUG DC8 DC861 3021952 WP RT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 RIGHT REAR SPAR, ANGLE SUPPORT CORRODED UNDER TRAILING EDGE UPPER SKIN STRINGER. REPAIRED IAW ABX REA D857-17836. 2 L 7 4 4F 4A25 1998112600383 19981126 00383 WP 1998 11 26 ABXA9801083 1 19980816 A 5713 564332179 STRINGER DOUG DOUG DC8 DC861 3021952 WP WS 162-436 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 847AX 46031 LEVEL 2 CORROSION, ON LEFT WING STRINGERS, AFTER TRAILING EDGE SKIN REMOVAL STATION XRS 162 TO 436. REPAIRED IAW ABX RE A D857-17828MR. 2 L 7 4 4F 4A25 1998112600384 19981126 00384 WP 1998 11 26 MWEA981090 1 19981119 A 5101 STRUCTURE DOUG DC9 DC932 3022066 WP AIRFRAME BIRD STRIKE A MWEA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 31 204ME 47680 ON CLIMBOUT, AIRCRAFT TOOK MULTIPLE BIRD STRIKES AND RETURNED TO MKE. MKE MTC COMPLETED A BIRD STRIKE INSPECTION AND NO DAMAGE WAS FOUND. REMOVED TWO STRIKE MARKS. 2 L 7 2 4F A6WE 1998112600385 19981126 00385 1998 11 26 MWEA981091 4 19981117 A 3425 1RN1017622 WIRE DOUG DC9 DC982 3022082 WP COCKPIT MISPINNED A MWEA O OTHER O OTHER NR NOT REPORTED 1 GL 31 809ME 48071 MKE - FLT 5 - TRK2 AND NAV2 AMBER INDICATIONS CONTINUOUSLY APPEAR AT FIRST OFFICER'S PRIMARY FLIGHT DISPLAY AND NAV DISP LAY CONTACTED MTC CTL. AMENDED FLIGHT RELEASE AND RETURNED TO DEPARTURE AIRPORT. CAPPED AND STOWED WIRE. (X) 2 L 7 2 4F A6WE 1998112600386 19981126 00386 NM 1998 11 26 DL72S982375 1 19981116 A 3350 LIGHT 81 BOEING 727 727232 1384082 NM WING EMER EXIT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 522DA 21582 EMER AREA LIGHT AT WING EXITS IN CABIN INOP. FOUND THAT LAMP AT EXTERIOR WING EXIT SHORTING CIRCUIT. REPLACED LAMP AND BATTERY PACK AND RACK FUSES, OPERATION CHECK GOOD. 2 L 7 3 4F A3WE 1998112600387 19981126 00387 WP 1998 11 26 DLL19982379 1 19981117 A 2710 SERVO 38380007 LKHEED 1011 10113853 5265020 WP LT AILERON FAILED A DALA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 27 764DA 10 193H1202 DURING APPROACH HAD DIFFICULTY FLYING STRAIGHT WITHOUT UNUSUALLY SEVERE RT AILERON AND RUDDER INPUTS SPI SHOWED LT OUTBD AILERON STUCK AT 8 UNITS UP. MTC IN PROGRESS LT AILERON NO MOVEMENT. REPLACED LT O/B AILERON SERVO, OPS CHECKS NORMAL . 2 L 7 3 4F A23WE 1998112600388 19981126 00388 NM 1998 11 26 DLM11982381 1 19981114 A 2530 2676 CHILLER DOUG MD11 MD11 3023602 NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 802DE 48473 AFT GALLEY CHILLER OVERHEATED CAUSING STRONG ELECTRICAL SMELL. CHILLERS SHUTOFF AND SMELL WENT AWAY. C/B FOR CHILLER P ULLED AND COLLARD, REPLACED G8 GALLEY CHILLER. 2 L 7 3 4F RT A22WE 1998112600389 19981126 00389 NM 1998 11 26 DL72S982382 1 19981117 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 21074 LEFT OVERWING EMERG LIGHT MID INOP. REPLACED BATTERY PACK AND SWITCHING CHARGING UNIT, OPS OK. 2 L 7 3 4F A3WE 1998112600390 19981126 00390 NM 1998 11 26 DL72S982383 1 19981117 A 3350 POWER SUPPLY BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 21074 EMERG EXIT LIGHT SIGN OVERHEAD AISLE AT ROW 20 INOP ON TEST. REPLACED FUSES IN POWER SUPPLY, OPN CKS OK. 2 L 7 3 4F A3WE 1998112600391 19981126 00391 NM 1998 11 26 DL72K982384 1 19981117 A 2120 17805021 DUCT BOEING 727 727232 1384082 NM LT AC BAY FAILED A DALA B EMER. DESCENT O OTHER CL CLIMB 1 SO 27 481DA 20861 AIRCRAFT WOULD NOT PRESSURIZE AFTER T/O, CABIN ROC SHOWED 400 FT CLIMBS THROUGH ENTIRE CLIMB. C/W LOSS OF PRESSURIZATIO N CK LIST BUT COULD NOT STOP CLIMBING. CARGO HEAT OUTFLOW VLV CLOSED. REPLACED WATER SEPARATOR ASSY AND DAMAGED DUCT. PRESSURIZED A/C TO 6 PSI. SYSTEM CHECKS NORMAL. 2 L 7 3 4F A3WE 1998112600392 19981126 00392 NM 1998 11 26 DL757982385 1 19981117 A 3350 20131A BATTERY PACK BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 681DA 26957 FOUND ON L/O, EXTERIOR MID OVERWING EMER LIGHT AND AFT OVERWING EMER LIGHT AND CENTER AISLE LIGHTS INOP. REPLACED BATTE RY PACK AT M735, EMERGENCY LIGHTS CK GOOD. 2 L 7 2 4F RT A2NM 1998112600393 19981126 00393 NM 1998 11 26 DL73E982388 1 19981118 A 2751 INDICATION 2061141 BOEING 737 737247 138448D NM TE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 374DL 1302 23521 TRAILING EDGE FLAP STOPPED AT 2 DEG ON RETRACTION DUE TO SPLIT IN INDICATOR BETWEEN LEFT AND RIGHT NEEDLES. EXTENDED US ING ALT FLAPS SWITCH AND LANDED AS PER POM. REPLACED FLAP RELAY UNIT AND TRAILING EDGE FLAPS POSITION IND. CLEANED CAN NON PLUGS ON LT AND RT FLAP POSITION TRANSMITTERS, RAN FLAPS ALL CK OK. 2 L 7 2 4F A16WE 1998112600394 19981126 00394 NM 1998 11 26 DL72S982389 1 19981118 A 2782 ACTUATOR 269002917 BOEING 727 727232 1384082 NM NR 4 L/E SLAT FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 403DA 21147 A-SYS HYD FAILURE ON APPROACH. FOUND THE NR 4 L/E SLAT ACT FAILED. REPLACED SAME. 2 L 7 3 4F A3WE 1998112600395 19981126 00395 NM 1998 11 26 DL733982391 1 19981118 A 3350 POWER SUPPLY BPS73 BOEING 737 737347 1384647 NM ROW 18-27 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 312WA 5415 23598 ON INSPECTION, FOUND EMERGENCY PATH LIGHTS FROM ROWS 18 TO 27 INOP. REPLACED POWER SUPPLY AT BATTERY PACK M1136. ALL L IGHTS OPERATE NORMAL. 2 L 7 2 4F RT A16WE 1998112600396 19981126 00396 NM 1998 11 26 DL72S982392 1 19981118 A 3230 RETRACT MECH 651781915 BOEING 727 727225 1384077 NM RT MLG FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 8890Z DA1198 21859 UPON CLIMBOUT, RT MAIN GEAR REMAINED DOWN WITH GEAR HANDLE RAISED. CYCLED GEAR PER POM PROCEDURES. GEAR REMAINED DOWN. FLT RETURNED TO CVG. REPLACED UPLOCK ACTUATOR AND SEQUENCE VLV. DID RETRACTION AND EXTENT CHECK. ALSO, MANUAL EXTEN T CHECK PER M/M CHAP 32, OPS NORMAL. 2 L 7 3 4F A3WE 1998112600397 19981126 00397 WP 1998 11 26 DLL10982393 1 19981118 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP GALLEY INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 718DA 65489 193C1097 LWR GALLEY EMER LIGHT INOP. REPLACED PWR SUPPLY, OP CK NORMAL. 2 L 7 3 4F A23WE 1998112600398 19981126 00398 NM 1998 11 26 DL72E982394 1 19981118 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM OVERWING EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 LT CTR OVERWING EMER LIGHT INOP. REPLACED BULB AND BATT PACK, NO HELP. REPLACED CHARGING RACK, CKS OK. 2 L 7 3 4F A3WE 1998112600399 19981126 00399 NM 1998 11 26 DL72K982395 1 19981117 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR MISINSTALLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 414DA 21256 AT MV2, FOUND ON LT ELEVATOR SKIN GAPPED, I/B T/E SKIN HAS GAP BETWEEN UPPER AND LOWER SKIN. COMPLETED RESEALING AND RE PAIR PER SRM 55-20-0 PG 801. 2 L 7 3 4F A3WE 1998112600400 19981126 00400 NM 1998 11 26 DL72K982396 1 19981117 A 5522 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR SEPARATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 414DA 21256 AT MV2, FOUND LT ELEVATOR SKIN SEPARATED O/B OF TAB CUTOUT. COMPLETED RESEALING AND REPAIRED PER SRM 55-20-0 PG 801. 2 L 7 3 4F A3WE 1998112600401 19981126 00401 NM 1998 11 26 DL73E982397 1 19981119 A 2910 VALVE BOEING 737 737247 138448D NM HYD TANK WORN A DALA K NONE O OTHER DE DESCENT 1 SO 27 381DL 23608 ON INITIAL DESCENT THRU FL31, GOT LOW PRESSURE LIGHT ON A-HYD SYSTEM AND ELEV FEEL LIGHT. SYS-A HYD PRESSURE WAS ZERO A ND HYD QTY WAS LOW. FOLLOWED POM PROCEDURES. ON GROUND HYD QTY APPEARED NORMAL. SERVICED HEAD PRESSURE AND CHANGED FI LTERS AND CHECKED VALVE. 2 L 7 2 4F A16WE 1998112600402 19981126 00402 WP 1998 11 26 DLL17982398 1 19981119 A 3350 POWER PACK 5165741 LKHEED 1011 10113853 5265020 WP R2 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 766DA 56575 193H1207 OVERHEAD RT AND R2 ENTRY EMERGENCY LIGHTS INOP. REPLACED POWER PACK. 2 L 7 3 4F A23WE 1998112600403 19981126 00403 NE 1998 11 26 DLM88982399 2 19981120 A 7230 COMPRESSOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 ENGINE STALLED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 919DE 18806 53422 725812 AT ROTATION, THE NR 2 ENGINE HAD A SEVERE COMPRESSOR STALL. FLIGHT RETURNED TO AUS. THE NR 1 ENGINE WAS FIREWALLED WIT H FLASHING PARAMETERS. NR 2 ENGINE CHANGED. 2 L 7 2 4F 4 F RT A6WE E9NE 1998112600404 19981126 00404 NM 1998 11 26 DL72K982400 1 19981120 A 5522 SKIN BOEING 727 727232 1384082 NM RT ELEVATOR DEBONDED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 414DA 21256 RT ELEVATOR T/E DISBONDED I/B OF TAB. REPAIRED PER M/M 55-20-0 PAGE 801. 2 L 7 3 4F A3WE 1998112600405 19981126 00405 NM 1998 11 26 DL72S982401 1 19981120 A 5720 TIP GTIP BOEING 727 727232 1384082 NM RT WING DAMAGED A DALA O OTHER C F.O.D. LD LANDING 1 SO 27 497DA 21077 FLAP FAIRING RT WING TIP DAMAGED ON LANDING. FOUND ON INSP RT O/B AILERON AND TAB DAMAGED, NR 4 AFT FLAP AND FAIRING DA MAGED, RT WING TIP DAMAGED O/B EDGE. REPAIRED ALL. 2 L 7 3 4F A3WE 1998112600406 19981126 00406 NM 1998 11 26 DL76L982403 1 19981112 A 2620 212T300820 LINE BOEING 767 767332 1382001 NM CARGO COMPT OUT OF POSITION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 THE APU PNEUMATIC BLEED DUCT INSULATION AT FS 1361 IN THE L/SIDEWALL OF THE C-2 CARGO COMPARTMENT WAS FOUND CHAFED THROU GH BY THE FIRE EXTINGUISHER DISCHARGE LINE. THE (P/N R180FS), INSULATION ON THE FIRE EXTINGUISHER DISCHARGE LINE WAS AL SO CHAFED AND DRY AT THIS LOCATION. THE APU PNEUMATIC DUCT AND FIRE EXTINGUISHER DISCHARGE LINE INSULATION WAS REPLACED AND THE FIRE EXTINGUISHER DISCHARGE LINE WAS REPOSITIONED TO PROVIDE CLEARANCE. 2 L 7 2 4F RT A1NM 1998112600407 19981126 00407 NM 1998 11 26 DL72S982404 1 19981104 A 5753 652163262 ANGLE BOEING 727 727232 1384082 NM RT TE MIDFLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 DURING SHOP VISIT, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED 19 INCHES FROM I/B END. THE ANGLE WAS REPAIRED PER MM 57 -52-0, FIG 802 BY INSTALLING A DOUBLER. 2 L 7 3 4F A3WE 1998112600408 19981126 00408 NM 1998 11 26 DL757982405 1 19981120 A 3297 WIRE BOEING 757 757232 1384965 NM COCKPIT SHORTED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 629DL 22919 ON TAKEOFF, NUMEROUS INDICATING LIGHTS CAME ON, HOWERVER ALL SYSTEM WERE OPERATING NORMAL. STARTED APU AND CYCLED GEN C ONTROL SWITCHES, NO HELP. FOUND WIRE FROM RT GEAR SAFE LIGHT SHORTED TO GROUND AT GEAR HANDLE ROD END BOLT. REPAIRED W IRE AND PROVIDED CLEARANCE, ALL LIGHTS OPS NORMAL. 2 L 7 2 4F RT A2NM 1998112600409 19981126 00409 NM 1998 11 26 DLM88982407 1 19981119 A 2910 O-RING 31914912 DOUG MD88 MD88 3023688 NM RT HYD SYST FAILED A DALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 27 960DL 49979 RIGHT HYDRAULIC SYSTEM FAILURE. REPLACED O-RING ON RT PRESSURE LINE. 2 L 7 2 4F RT A6WE 1998112600410 19981126 00410 NM 1998 11 26 DL733982408 1 19981120 A 3230 SHIM BOEING 737 737347 1384647 NM NLG WORN A DALA O OTHER J WARNING INDICATION AP APPROACH 1 SO 27 303WA 23183 NOSE GEAR WOULD NOT EXTEND WITH NORMAL GEAR EXTENSION. MANUAL GEAR EXTENSION WAS REQUIRED TO GET A SAFE NOSE GEAR INDI CATION. FOUND SHIM MISSING ON OVER CTR LINKAGE. INSTALLED SAME, ALL OPS CKS OK. RETRACTION CK NORMAL. 2 L 7 2 4F RT A16WE 1998112600411 19981126 00411 NM 1998 11 26 DL76L982409 1 19981121 A 2120 AIR DIST BOEING 767 767332 1382001 NM MID GALLEY ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 189DN 25990 HEAVY HOT DUCT ELECTRICAL SMELL AFT OF MID GALLEY. PULLED AFT EQ EXHAUST FAN NR 1, NO HELP. INSPECTED ENTIRE AREA AFT OF MID GALLEY INCLUDING GALLEY OVENS AND COFFEEMAKERS. RAN BOTH PACKS AND ENTERTAINMENT SYSTEM, NO FAULTS FOUND, A/C DI SPATCHED. AS A PRECAUTION, CLEANED GALLEY VENT FAN SCREEN, REPLACED S75 THERMAL SWITCH AND V13 CARGO HEAT VALVE PER MSU SET UP. RAN ALL GALLEY AND CABIN SYSTEMS, NO PROBLEM NOTED. 2 L 7 2 4F RT A1NM 1998112600412 19981126 00412 NM 1998 11 26 DL72W982411 1 19981121 A 3350 BATTERY PACK 900835A BOEING 727 727247 138408F NM OVERWING EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 296WA 12958 22533 ON L/O, FOUND INTERNAL OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK, EMERGENCY LIGHTS NOW CHECK NORMAL PE R M/M. 2 L 7 3 4F A3WE 1998112600413 19981126 00413 NM 1998 11 26 DLM88982413 1 19981122 A 2530 OVEN DOUG MD88 MD88 3023688 NM GALLEY DIRTY A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 907DL 49538 THERE WAS A BURNING SMELL /RUBBERY SCENT/ IN 4-5 ROW ZONE AREA NEAR FWD LEADING EDGE OF WING. INSP CABIN AREA 4-5 ROW A REA FWD OF LEADING EDGE OF WING. CLEANED DEBRIS FROM OVENS AND CLEANED SAME. PERFORMED HI PWR RUN OF ENGINES, NO DEFEC TS NOTED. CHECKED CABIN LIGH BALLASTS IN SUSPECTED AREA. 2 L 7 2 4F RT A6WE 1998112600414 19981126 00414 NM 1998 11 26 DL73E982414 1 19981122 A 2751 INDICATOR 2061141 BOEING 737 737247 138448D NM TE FLAPS MALFUNCTIONED A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 374DL 1164 23521 ON CLIMBOUT, SPLIT FLAP AT 2 DEG. REPLACED FLAP INDICATOR, CKD ALL FLAP TRANSMISSIONS, ALL CK OK. LUBED FLAPS, RAN FLA PS SEVERAL TIMES, CKS OK. 2 L 7 2 4F A16WE 1998112600415 19981126 00415 WP 1998 11 26 DLL14982415 1 19981121 A 3350 BATTERY PACK 5165741 LKHEED 1011 1011385115 5265015 WP CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1739D 64385 193C1237 R3 DOOR EMERGENCY LIGHTS GO OFF AFTER ABOUT 1 MIN. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1998112600416 19981126 00416 NM 1998 11 26 DLM88982416 1 19981121 A 3397 WIRE DOUG MD88 MD88 3023688 NM ROW 31 LOOSE A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 920DL 49644 EMERGENCY PATH LIGHTING INOP FROM ROW 31 AFT. REPAIRED WIRES. 2 L 7 2 4F RT A6WE 1998112600417 19981126 00417 WP 1998 11 26 DLL19982417 1 19981122 A 3350 RPS1 POWER SUPPLY LKHEED 1011 10113853 5265020 WP ROW 34-40 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 768DL 193H1216 EMERGENCY TRACK LIGHTING WILL NOT TEST BETWEEN ROWS 34-40 RT SIDE ONLY. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998112600418 19981126 00418 NM 1998 11 26 SCNA98141 1 19981117 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE FORWARD AISLE BULLNOSE EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND RE PLACED THE BATTERY PACK M1088. ALL EMERGENCY LIGHTING CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998112600419 19981126 00419 WP 1998 11 26 ARWA981105 1 19981119 A 5230 FRAME DOUG DC8 DC862 3021970 WP NR 4 CARGO DOOR CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 2.5 INCH CRACK NR 4 PIT DOOR BOTTOM FRAME JUST ABOVE BUMPER. STOP DRILLED CRACK, INSTALLED DOUBLERS PER SRM 52 -2-0 UNDER WORK ORDER NR 1299. 2 L 7 4 4F 4A25 1998112600420 19981126 00420 WP 1998 11 26 ARWA981106 1 19981119 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1530 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 1.25 INCH CRACK IN LONGERON 28L END FITTING STA 1530. REPLACED FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 130 2. 2 L 7 4 4F 4A25 1998112600421 19981126 00421 WP 1998 11 26 ARWA981107 1 19981119 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 990 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 6 INCH CRACK IN LONGERON END CAP FITTING 22L STA 990. REPLACED FITTING PER SRM 51-1-20 UNDER WORK NR 1302. 2 L 7 4 4F 4A25 1998112600422 19981126 00422 WP 1998 11 26 ARWA981108 1 19981119 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 990 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, LONGERON 23R END CAP FITTING 5 INCH CRACK STA 990. REPLACED FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302. 2 L 7 4 4F 4A25 1998112600423 19981126 00423 WP 1998 11 26 ARWA981109 1 19981119 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 990 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, LONGERON 22R END CAP 6.5 INCH CRACK STA 990. REPLACED END CAP FITTING PER SRM 51-1-20 UNDER WORK ORDER NR 1302 . 2 L 7 4 4F 4A25 1998112600424 19981126 00424 WP 1998 11 26 ARWA981110 1 19981119 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1090 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 4.5 INCH CRACK IN LONGERON SPLICE FITTING 25R STA 1090. REPLACED LONGERON FITTING PER SRM 51-1-20 UNDER WORK O RDER NR 1302. 2 L 7 4 4F 4A25 1998112600425 19981126 00425 WP 1998 11 26 ARWA981111 1 19981119 A 5712 RIB DOUG DC8 DC862 3021970 WP WS 422 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 3.5 INCH CRACK IN RT WING L/E RIB STA XFS 422. STOP DRILLED CRACK, INSTALLED DOUBLER PER SRM 57-2-0 UNDER WORK ORDER NR 1299. 2 L 7 4 4F 4A25 1998112600426 19981126 00426 WP 1998 11 26 ARWA981112 1 19981119 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, LT HORIZONTAL STAB L/E CORROSION AT SCREW HOLES O/B END UPPER SURFACE. REMOVED CORROSION AND INSTALLED DOUBLER S PER EO NR 98-0924-02 ON 8110-3 DATED SEPT 24, 1998 UNDER WORK NR 1300. 2 L 7 4 4F 4A25 1998112600427 19981126 00427 WP 1998 11 26 ARWA981113 1 19981119 A 5512 SKIN DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, LT HORIZ STAB L/E I/B LITE CORROSION AT FASTENERS XFS 180. REMOVED CORROSION AND INSTALLED DOUBLERS PER EO NR 98-0924-02 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300. 2 L 7 4 4F 4A25 1998112600428 19981126 00428 WP 1998 11 26 ARWA981114 1 19981119 A 5330 SKIN DOUG DC8 DC862 3021970 WP BS 1320 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, FUSELAGE SKIN CORRODED AND SHEAR FOOT BULGED AFT SIDE FUSELAGE FRAME STA 1320 BETWEEN LONGERON 29L-31L. REMOVE D DAMAGED SKIN, FABRICATED DOUBLERS AND INSTALLED PER SRM 53-2-1 UNDER WORK ORDER NR 1302. 2 L 7 4 4F 4A25 1998112600429 19981126 00429 WP 1998 11 26 ARWA981115 1 19981119 A 5313 LONGERON DOUG DC8 DC862 3021970 WP FRAME 1060 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, CORROSION BLISTER/CRACK ON LONGERON 27R FUSELAGE FRAME 1060. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER DR AWING NR 98-012 ON 8110-3 DATED SEPT 04, 1998 UNDER WORK ORDER NR 1302. 2 L 7 4 4F 4A25 1998112600430 19981126 00430 WP 1998 11 26 ARWA981116 1 19981119 A 5400 ANGLE DOUG DC8 DC862 3021970 WP NR 3 PYLON CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 8 INCH CRACK IN RADIUS OF TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN310. STOP DRILLED CRACK, INSTAL LED DOUBLER PER EO NR 98-0926-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300. 2 L 7 4 4F 4A25 1998112600431 19981126 00431 WP 1998 11 26 ARWA981117 1 19981119 A 5400 ANGLE DOUG DC8 DC862 3021970 WP NR 3 PYLON CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 4.5 INCH CRACK TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN336. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER EO NR 98-0924-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300. 2 L 7 4 4F 4A25 1998112600432 19981126 00432 WP 1998 11 26 ARWA981118 1 19981119 A 5711 SPAR DOUG DC8 DC862 3021970 WP WS 857 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS 33 TO 35 RIGHT OF CENTER LINE AND 53 TO 54 STA 857 RT W/W. S TOP DRILLED AND INSTALLED DOUBLERS PER DRAWING NR 98-015 ON 8110-3, DATED SEPT 30, 1998 UNDER WORK ORDER NR 1300. 2 L 7 4 4F 4A25 1998112600433 19981126 00433 WP 1998 11 26 ARWA981119 1 19981119 A 5711 SPAR DOUG DC8 DC862 3021970 WP CENTER WING CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, CENTER WING REAR SPAR LOWER CAP CRACKED BETWEEN FASTENERS STA 857 LBL 37, 51, 61 LT W/W. STOP DRILLED CRACKS A ND INSTALLED DOUBLERS PER DRAWING NR 98-013 ON 8110-3 DATED SEPT 22, 1998 UNDER WORK ORDER NR 1300. 2 L 7 4 4F 4A25 1998112600434 19981126 00434 WP 1998 11 26 ARWA981120 1 19981119 A 5730 SKIN DOUG DC8 DC862 3021970 WP WS 74.86 CRACKED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, 1.75 INCH CRACK IN LEFT WING SKIN UPPER SURFACE AT STA 74.86. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 57-2 -1 UNDER WORK ORDER NR 1302. 2 L 7 4 4F 4A25 1998112600435 19981126 00435 WP 1998 11 26 ARWA981121 1 19981119 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 168-188 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, FINGER DOUBLER CORRODED AT CUSP LINE RT O/B OF F/E POSITION SUBFLOOR PRESSURE PANEL STA 168 TO 188. REMOVED DA MAGED SKIN AND INSTALLED DOUBLERS PER EO NR 98-0924 ON 8110-3 DATED SEPT 24, 1998 UNDER WORK ORDER NR 1302. 2 L 7 4 4F 4A25 1998112600436 19981126 00436 WP 1998 11 26 ARWA981122 1 19981119 A 5315 FLOORBEAM DOUG DC8 DC862 3021970 WP BS 1140 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, CORROSION BLISTERS ON FLOORBEAM TOP FWD EDGE AT NUT PLATES STA 1140 BETWEEN NR 2 AND NR 4 SEAT TRACKS. REMOVED ENTIRE UPPER SECTION AND INSTALLED DOUBLER PER EO NR 98-924-04 0N 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1302. 2 L 7 4 4F 4A25 1998112600437 19981126 00437 WP 1998 11 26 ARWA981123 1 19981119 A 5311 FRAME DOUG DC8 DC862 3021970 WP FRAME 1340 MISDRILLED A ARWA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, FRAME 1340 AT LT CUSP ABOVE FLOOR FITTING HAS DRILLED HOLE AT EDGE OF ANGLE. REMOVED DAMAGED AREA AND INSTALLE D DOUBLERS PER DRAWING NR 98-012 ON 8110-3 DATED SEPT 09, 1998 UNDER WORK ORDER NR 1392. 2 L 7 4 4F 4A25 1998112600438 19981126 00438 WP 1998 11 26 ARWA981124 1 19981119 A 5400 FASTENERS DOUG DC8 DC862 3021970 WP NR 1 & 2 PYLONS MISINSTALLED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, NR 1 AND NR 2 PYLON'S HAVE WRONG FASTENERS INSTALLED IN PLANKS. OPENED REPLACEMENT HOLES TO .260 DIA AND INSTA LLED PER EO DRAWING NR 98-014 ON 8110-3, DATED SEPT 28, 1998 UNDER WORK NR 1299. 2 L 7 4 4F 4A25 1998112600439 19981126 00439 WP 1998 11 26 ARWA981125 1 19981119 A 5751 SKIN DOUG DC8 DC862 3021970 WP LT AILERON CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 810BN 45905 C-CHECK, CORROSION FOUND BETWEEN LOWER SKIN AND RIBS ON LT I/B AILERON. REMOVED DAMAGED LOWER SKIN, FABRICATED REPAIR S KIN PER EO DRAWING NR 98-0924-3, ON 8110-3, DATED SEPT 25, 1998 UNDER WORK ORDER NR 1299. 2 L 7 4 4F 4A25 1998112600440 19981126 00440 NM 1998 11 26 VNAA9811019 1 19981118 A 5610 SPSDO328221A WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT BIRD STRIKE A VNAA K NONE C F.O.D. CL CLIMB 1 GL 07 436JS 35987 3052 SHORTLY AFTER TAKEOFF, THE AIRCRAFT TOOK A BIRD STRIKE ON THE LEFT HAND FORWARD WINDSHIELD. THE AIRCRAFT CONTINUED ON T O PIT AND PERFORMED A NORMAL LANDING. WHEN IN RANGE OF PIT, THE CREW REQUESTED MAINTENANCE. PIT MAINTENANCE INSPECTED THE AIRCRAFT FOR DAMAGE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-11-00. NO DAMAGE WAS NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112600441 19981126 00441 NM 1998 11 26 CKS98642 1 19981120 A 5313 65B04369133 STRINGER BOEING 747 7472B4B 138481B NM BS 2176-2180 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STRINGER 51R AT STA 2176 TO STA 2180 HAS AREA OF LEVEL 2 CORROSION. REPAIRED IAW SRM 53-30-03 FIG 1 AND CKF-AMD-053 SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING W ICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7DI1415, NON ROUTINE WORK CARD NR CKF-AMD-012, CPCP TASK CARD NR C 53-125-01-02. 2 L 7 4 4F RT A20WE 1998112600442 19981126 00442 NM 1998 11 26 CKSA89648 1 19981120 A 5315 65B380863 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 TOP SURFACE OF FLOORBEAM UPPER CAP AT STA 1720, WL 200, BL 0 TO LBL 108 HAS SEVERAL AREAS 1 INCH DIAMETER WITH EXFOLIATE D LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38134-6 ITEMS 2 AND 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTI NE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-2 10-01, CPCP TASK CARD NR C53-210-01-03. 2 L 7 4 4F RT A20WE 1998112600443 19981126 00443 NM 1998 11 26 CKSA98637 1 19981120 A 5315 CKFA0164 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 520 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 TOP CHORD OF FLOORBEAM AT UPPER DECK ZONE 230, STA 520, WL 307, LBL 27.99 TO LBL 46.65 HAS AREA 20 X 2 OF LEVEL 2 CORROS ION. REPAIRED IAW DRAWING 65B10936 SUPP SHEET 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHEC K, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7DI2102, NON R OUTINE WORK CARD NR CKF-A-016, CPCP TASK NR C53-210-01-01. 2 L 7 4 4F RT A20WE 1998112600444 19981126 00444 NM 1998 11 26 CKSA98638 1 19981120 A 5347 CKFA0191 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 520 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LEVEL 2 CORROSION FOUND ON SEAT TRACK AT ZONE 230, STA 520 TO 600, WL 307, LBL 27.99. REPAIRED IAW 747 SRM 53-10-05, AL TERNATIVE 1, PAGE 2A. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI2227, NON ROUTINE WORK CARD NR ASA CKF-A-019, CPCP TASK CARD C53-210-01 PART 1. 2 L 7 4 4F RT A20WE 1998112600445 19981126 00445 NM 1998 11 26 CKSA98639 1 19981120 A 5320 65B1093219 UPPER CHORD BOEING 747 7472B4B 138481B NM BS 440 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AT UPPER DECK ZONE 230, STA 440, RBL 46-49, WL 309, UPPER CHORD HAS AREA OF LEVEL 2 CORROSION 3.5 X 1.5. FOUND DURING A CCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WOR K ORDER NUMBER MO280, TASK CARD NR 7CI2227, NON ROUTINE WORK CARD NR CKF-A-028, CPCP TASK NR C53-210-03-01. 2 L 7 4 4F RT A20WE 1998112600446 19981126 00446 NM 1998 11 26 CKSA98640 1 19981120 A 5330 65B04201 SKIN BOEING 747 7472B4B 138481B NM BS 1484 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MACHINED SKIN AT STA 1484 BETWEEN STR 10 LT AND 11 LT HAS AREA OF EXFOLIATED CORROSION 2 INCH DIAMETER, APPROX .050 DEEP . REPAIRED IAW SRM 53-30-03 FIG 47. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHME NT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01-06, NON ROUTINE WORK C ARD NR CKF-AMD-003. 2 L 7 4 4F RT A20WE 1998112600447 19981126 00447 NM 1998 11 26 CKSA98641 1 19981120 A 5320 65B178951 CHORD BOEING 747 7472B4B 138481B NM CARGO DOORWAY CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 MAIN DECK CARGO DOOR UPPER CHORD CORRODED UNDER HINGES FULL LENGTH OF DOOR, INTERIOR WEB CORRODED BEYOND LIMITS (NOT CON NECTED TO DOOR). REPAIRED IAW MM 52-34-01 AND DWG 65B17895-1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI2601 , NON ROUTINE WORK CARD NR CKF-AMD-010, CPCP TASK NR C53-110-01. 2 L 7 4 4F RT A20WE 1998112600448 19981126 00448 NM 1998 11 26 CKSA98643 1 19981120 A 5330 65B044292 SKIN BOEING 747 7472B4B 138481B NM BS 2190-2200 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SKIN (ONLY) AT ZONE 100, STA 2200, BETWEEN STR 48 AND 49 HAS AREA OF LEVEL 2 CORROSION. REPAIRED IAW SRM 53-30-03 FIG 1 AND CKF-AMD-053 SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP T ASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7DI1415, NON ROUTINE WORK CARD NR CKF-AMD-012 , CPCP TASK CARD NR C53-125-01-02. 2 L 7 4 4F RT A20WE 1998112600449 19981126 00449 NM 1998 11 26 CKSA98644 1 19981120 A 5315 65B38089602 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1780 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 1780 WL 200 RBL 24 THE TOP SURFACE OF UPPER CAP HAS AREA 1.20 X 2.50 OF LEVEL 2 CORROSION. REPAIRED IAW SRM 51-10-0 1 FIG 18.01. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, NON ROUTINE WORK CARD NR CKF-AMD-014. 2 L 7 4 4F RT A20WE 1998112600451 19981126 00451 NM 1998 11 26 CKSA98646 1 19981120 A 5315 65380833 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1660 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 TOP SURFACE OF FLOORBEAM UPPER CAP AT STA 1660, WL 200, LBL 33-39 HAS AREA 6 X 2.5 WITH EXFOLIATED LEVEL 2 CORROSION. R EPAIRED IAW DWG 65B38083 SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, CPCP TASK CARD NR C53-210- 01-03. 2 L 7 4 4F RT A20WE 1998112600452 19981126 00452 NM 1998 11 26 CKSA98647 1 19981120 A 5315 65B3808744 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1740 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 TOP SURFACE OF FLOORBEAM UPPER CAP AT STA 1740, WL 200, LBL 8 TO LBL 38 HAS 4 AREAS 1-2 DIAMETER WITH EXFOLIATED LEVEL 2 CORROSION. REPAIRED IAW DWG 65B38087 SHT 4. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACC OMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, CPCP TASK CA RD NR C53-210-01-04. 2 L 7 4 4F RT A20WE 1998112600453 19981126 00453 NM 1998 11 26 CKSA98649 1 19981120 A 5347 69B042561 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SEAT TRACK AT ZONE 200, STA 1680 TO STA 1703, WL 200, HAS AREA 1.2 X 3 WITH LEVEL 2 PITTING CORROSION. REPAIRED IAW AME NDMENT CKF-AMD-109 SHT 2 AND DWG 65B38251 SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, CPCP TASK CARD NR C53-210-07. 2 L 7 4 4F RT A20WE 1998112600454 19981126 00454 NM 1998 11 26 CKSA98650 1 19981120 A 5347 65B382721 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1620 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SEAT TRACK AT ZONE 200, STA 1620, WL 200, LBL 11 HAS AREA 1 X 2.5 OF EXFOLIATED LEVEL 2 CORROSION. REPAIRED IAW DWG 65B 38253 SHT 1 AND ATTACHMENT SHEETS 1-3 AND ASA-CKF-AMD-023 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, CPCP TASK CARD NR C53-210-07-01. 2 L 7 4 4F RT A20WE 1998112600455 19981126 00455 NM 1998 11 26 CKSA98651 1 19981120 A 5320 65B003006 SHEAR TIE BOEING 747 7472B4B 138481B NM BS 1720 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SHEAR TIE AT ZONE 100, STA 1720, STR 51R TO STR 51L, WL 91 BL 0, HAS APPROX 6 SQ AREA OF LEVEL 2 CORROSION. REPAIRED IA W CKF-AMD-025 SUPP SHT 1, 2, 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7DI1415-1250, CPCP TASK CARD NR C53-12 5-07-01. 2 L 7 4 4F RT A20WE 1998112600456 19981126 00456 NM 1998 11 26 CKSA98652 1 19981120 A 5347 65B38961600 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 2100 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SEAT TRACK LOCATED AFT MAIN DECK, ZONE 200 STA 2100 WL 199.5 RBL 89 HAS AREA APPROX 24 OF LEVEL 2 CORROSION. REPAIRED I AW DWG 65B38251 SHT 2 AND ASA CKF-AMD-028 SUPP SHT 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, CPCP TASK CARD NR C53-210-07-01. 2 L 7 4 4F RT A20WE 1998112600457 19981126 00457 NM 1998 11 26 CKSA98653 1 19981120 A 5347 65B38961600 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1770-2110 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SEAT TRACK LOCATED AFT MAIN DECK, ZONE 200 STA 1770 TO STA 2110 WL 199.5 RBL 33.99 HAS AREA APPROX 24 OF LEVEL 2 CORROSI ON. REPAIRED IAW DWG 65B38251 SHT 2 AND ASA CKF-AMD-028 SUPP SHT 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, R OUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C 53-210-01, CPCP TASK CARD NR C53-210-07-01. 2 L 7 4 4F RT A20WE 1998112600458 19981126 00458 NM 1998 11 26 CKSA98654 1 19981120 A 5347 65B38961600 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1946-2280 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SEAT TRACK LOCATED AFT MAIN DECK, ZONE 200 STA 1946 TO STA 2280 WL 199.5 RBL 11.33 HAS AREA APPROX 24 OF LEVEL 2 CORROSI ON. REPAIRED IAW DWG 65B38251 SHT 2 AND ASA CKF-AMD-028 SUPP SHT 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, R OUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C 53-210-01, CPCP TASK CARD NR C53-210-07-01. 2 L 7 4 4F RT A20WE 1998112600459 19981126 00459 NM 1998 11 26 CKSA98655 1 19981120 A 5315 65B1776734 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1820 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 UPPER CAP OF FLOORBEAM LOCATED ZONE 200 STA 1820 WL 200 FROM LBL 11 TO RBL 25, HAS AREA OF EXFOLIATED CORROSION COVERING APPROX 40 PERCENT OF CAP. REPLACED IAW SRM 51-30-02 DWG 65B17767. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, RO UTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C5 3-210-01, CPCP TASK CARD NR C53-210-01-04. 2 L 7 4 4F RT A20WE 1998112600460 19981126 00460 NM 1998 11 26 CKSA98656 1 19981120 A 5347 65B382651 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1658 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 2110 WL 200 LBL 33, THE CROWN AREA OF THE 65B38265-1 SEAT TRACK HAS 2 CRACKS. ONE CRACK RUNS FROM AFT EDGE OF -1 SE AT TRACK FWD FOR .80 LONG. THE OTHER CRACK RUNS FROM AFT EDGE OF -1 SEAT TRACK FWD FOR 5 LONG. REPAIRED IAW ASA CKF-AM D-032 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CAR DS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, CPCP TASK CARD NR C53-210-07-01. 2 L 7 4 4F RT A20WE 1998112600461 19981126 00461 NM 1998 11 26 CKSA98657 1 19981120 A 5347 65B382734 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1780-1940 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 TOP SURFACE OF SEAT TRACK LOCATED ZONE 200 STA 1780 TO STA 1940 WL 200 RBL 11 HAS MOD TO SEVERE CORROSION. AREA OF CORR OSION APPROX 15 PERCENT. REPAIRED IAW DWG 65B38253 SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-C HECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C53-210-01, CPCP TASK CARD NR C53-210-07-01. 2 L 7 4 4F RT A20WE 1998112600462 19981126 00462 NM 1998 11 26 CKSA98658 1 19981120 A 5313 65B0415430 STRINGER BOEING 747 7472B4B 138481B NM BS 2064 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 UPPER FLANGE OF STRINGER LOCATED ZONE 100 STA 2064 STR 28R WL 185 HAS .5 AREA OF SEVERE CORROSION. REMOVED CORROSION IA W SRM 51-10-01, TREATED PER SRM 51-10-02 AND DWG 65B04154. REPAIRED IAW ASA CKF-AMD-088. FOUND DURING ACCOMPLISHMENT O F CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-AMD-037, CPCP TASK CARD NR C53-110-01-03. 2 L 7 4 4F RT A20WE 1998112600463 19981126 00463 NM 1998 11 26 CKSA98659 1 19981120 A 5330 65B044292 SKIN BOEING 747 7472B4B 138481B NM BS 2183-2187 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SKIN PANEL LOCATED BETWEEN STA 2183 AND 2187, STRINGER 44R AND 46R, HAS AN AREA OF APPROX 3 X 6 OF LEVEL 2 CORROSION. R EPAIRED IAW ASA CKF-AMD-053 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLIS HMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-AMD-012, CPCP TASK CARD NR C53-100-01-06. 2 L 7 4 4F RT A20WE 1998112600464 19981126 00464 NM 1998 11 26 CKSA98660 1 19981120 A 5330 65B041522 SKIN BOEING 747 7472B4B 138481B NM BS 1960 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SKIN PANEL LOCATED AT ZONE 100, STA 1960 STR 51R TO 51L WL 125 HAS AREA APPROX 4.0 SQ INCHES OF MODERATE CORROSION. REP AIRED IAW 747 SRM 53-30-03, FIG 47 DETAIL 1 AND ASA CKF-AMD-068 SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVE RSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK C ARD NR CKF-AMD-008, CPCP TASK CARD NR C53-100-01-06. 2 L 7 4 4F RT A20WE 1998112600465 19981126 00465 NM 1998 11 26 CKSA98661 1 19981120 A 5315 65B061617 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 2349 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FLOORBEAM UPPER CAP AT ZONE 200, STA 2349 WL 199 LBL 32 HAS AREA 1 X 1 OF SEVERE CORROSION. DEPTH OF CORROSION EXCEEDS 20 PERCENT OF MATERIAL. REMOVED AND REPLACED THE 65B06161-7 UPPER CAP IAW BOEING DWG 65B06161 SHTS PL & 2. FOUND DURIN G ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). W ORK ORDER NUMBER MO280, TASK CARD NR 65B16282-501-IO1, CPCP TASK CARD NR C53-210-01-04. 2 L 7 4 4F RT A20WE 1998112600466 19981126 00466 NM 1998 11 26 CKSA98662 1 19981120 A 5347 65B065486 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 1770 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 IN AFT CARGO AREA ZONE 100, STA 1770 RBL 24 WL 118 HAS AN AREA 0.4 X 0.6 OF EXFOLIATED CORROSION ON SEAT TRACK 65B06548- 6. REPAIRED IAW ASA CKF-AMD-096 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCO MPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-AMD-096, CPCP TASK CA RD NR C53-110-01-03. 2 L 7 4 4F RT A20WE 1998112600467 19981126 00467 NM 1998 11 26 CKSA98663 1 19981120 A 5315 65B381133 FRAME BOEING 747 7472B4B 138481B NM BS 2260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FLOORBEAM CAP LOCATED AT ZONE 200 AFT MAIN DECK, STA 2260, WL 199, RBL 44 HAS SCREW HOLE SHOWING CORROSION AREA OF 0.60 DIAMETER. REPAIRED IAW ASA CKF-AMD-115 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, A ND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 41168-3-1-001, CPC P TASK CARD NR C53-210-01-04. 2 L 7 4 4F RT A20WE 1998112600468 19981126 00468 NM 1998 11 26 CKSA98664 1 19981120 A 5347 65B382711 SEAT TRACK BOEING 747 7472B4B 138481B NM BS 2258 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 AT ZONE 200 AFT MAIN DECK, STATION 2258 WL 199 LBL 33, THE INBD FLANGE OF 65B38271-1 SEAT TRACK HAS 1 SQAURE AREA OF LEV EL 2 EXFOLIATED CORROSION. REPAIRED IAW 747 SRM 53-10-05 ALT 1 DETAIL 1 AND ASA CKF-AMD-121. FOUND DURING ACCOMPLISHME NT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUM BER MO280, TASK CARD NR C53-210-07-01, CPCP TASK CARD NR C53-210-07-01. 2 L 7 4 4F RT A20WE 1998112600469 19981126 00469 NM 1998 11 26 CKSA98665 1 19981120 A 5315 65B380853 FLOORBEAM BOEING 747 7472B4B 138481B NM BS 1700 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FLOORBEAM UPPER CAP 65B38085 AT AFT MAIN DECK ZONE 200, STA 1700 WL 199 LBL 18 TO LBL 23 HAS LEVEL 2 EXFOLIATED CORROSIO N ON AFT EDGE OF -3 CAP. REPAIRED IAW ASA CKF-AMD-127 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSIO N, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 016U6390-554-IO1, CPCP TASK CARD NR C53-210-01-03. 2 L 7 4 4F RT A20WE 1998112600470 19981126 00470 NM 1998 11 26 CKSA98666 1 19981120 A 5330 65B16079 SKIN BOEING 747 7472B4B 138481B NM BS 1090 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 UPPER WING SKIN PANEL AT STA 1090 WL 200 RBL 127, HAS AN AREA 2.0 X 2.0 OF LEVEL 2 CORROSION. REPAIRED IAW SRM 51-10-01 , FIG 18.01 PER D6-5000 AND ASA CKF-CF-009 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK , AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-CF-003, CPC P TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600471 19981126 00471 NM 1998 11 26 CKSA98667 1 19981120 A 5330 65B16079 SKIN BOEING 747 7472B4B 138481B NM BS 1125 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 UPPER WING SKIN PANEL AT STA 1125 WL 200 RBL 127 HAS AN AREA 6.0 X 2.0 OF LEVEL 2 CORROSION. AREA IS NEAR UPPER WING TO BODY. REPAIRED IAW SRM 51-10-01, FIG 18.01 PER D6-5000 AND ASA CKF-CF-010 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHME NT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUM BER MO280, TASK CARD NR 0204-7C11026, CPCP TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600472 19981126 00472 NM 1998 11 26 CKSA98668 1 19981120 A 5320 65B133759 WEB BOEING 747 7472B4B 138481B NM BS 1340 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 UPPER SURFACE OF PRESSURE DECK, WEB 65B13375-9 LOCATED STA 1340 TO 1350, WL 186, RBL 2-11, HAS 10 X 8 AREA OF LEVEL 2 CO RROSION. REPAIRED IAW ASA CKF-CA-017 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-CA-017. 2 L 7 4 4F RT A20WE 1998112600473 19981126 00473 NM 1998 11 26 CKSA98669 1 19981120 A 5320 FRAME BOEING 747 7472B4B 138481B NM 3R DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 INSIDE SKIN AFT NR 3 RT DOOR FRAME STA 139 WL 212 RBL 127 HAS 2 X 6 AREA OF EXFOLIATED CORROSION. REPAIRED IAW D6-41910 PART 1, 747 SRM 53-30-01 DETAIL 2 OF FIG 1, AND ASA AMD-CA-014 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVER SION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CA RD NR CKF-CA-007, CPCP TASK CARD NR C53-210-08-02. 2 L 7 4 4F RT A20WE 1998112600474 19981126 00474 NM 1998 11 26 CKSA98670 1 19981120 A 5330 65B026963 SKIN BOEING 747 7472B4B 138481B NM BS 2598 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SKIN PANEL ASSY AT SEC 48 RT FS, ZONE 310 STA 2598 STR 46R JUST ABOVE TAIL JACK PAD, HAS AREA 1.5 SQUARE OF LEVEL 2 CORR OSION. REPAIRED IAW SRM 51-10-01, 51-10-02, SRM 51-30-02, DWG 65B02701 SH 6. FOUND DURING ACCOMPLISHMENT OF CARGO CONV ERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 5027 C53-200-01, CPCP TASK CARD NR C53-200-01-05. 2 L 7 4 4F RT A20WE 1998112600475 19981126 00475 NM 1998 11 26 CKSA98671 1 19981120 A 5312 65B02634328 BULKHEAD RING BOEING 747 7472B4B 138481B NM AFT PRESS BLKHD CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 ZONE 310, PRESSURE BLKHD STA 2360 WL 185 BL 0 TO RBL 6, THE AFT FACE OF RING SEGMENT 65B02634-328 HAS 4 SQUARE INCH AREA OF LEVEL 2 CORROSION. REPAIRED IAW ASA CKF-6XB-065 SUPP SHT 2, 3, 4. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 0434 7CI 3117. 2 L 7 4 4F RT A20WE 1998112600476 19981126 00476 NM 1998 11 26 CKSA98672 1 19981120 A 5310 65B1149815 STRUCTURE BOEING 747 7472B4B 138481B NM BS 1322 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LAV LEAK CAUSED LEVEL 2 CORROSION TO BRACKETS, FITTINGS, WEBS, CLIPS, ANGLES AND FASTENERS IN AREA BETWEEN LANDING GEAR DOORS. ZONE 191, STA 1322 WL 96 LBL 5. REPAIRED IAW ASA CKF-EXB-136 SUPP SHT 2, SRM D6-13592, CHAPTER 51-30-02 AND ASA CKF-EXB-172. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS A T BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXB-067, CPCP TASK CARD NR C53-190-01-01. 2 L 7 4 4F RT A20WE 1998112600477 19981126 00477 NM 1998 11 26 CKSA98673 1 19981120 A 5310 65B140625 STRUCTURE BOEING 747 7472B4B 138481B NM BS 1480 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 KEEL BEAM AREA ZONE 129-204, STA 1267 TO STA 1480, BRACKETS, FITTINGS, FASTENERS, FRAMES AND WEBS HAVE SIGNS OF CORROSIO N. REPAIRED ALL IAW SRM 51-10-01, SRM 51-10-02 AND ASA AMD-CKF-EXB-136 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARG O CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI1328, CPCP TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600478 19981126 00478 NM 1998 11 26 CKSA98674 1 19981120 A 5330 65B02699108 SKIN BOEING 747 7472B4B 138481B NM BS 2360 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 SKIN PANEL ASSY AT ZONES 100-200 (EXT SKINS) STA 2360, STR 46L TO 46R, RBL 8 TO LBL 8, HAS APPROX 4 SQ INCH AREA OF LEVE L 2 CORROSION NEAR LAV SVC DOOR. REPAIRED IAW BOEING ASA CKF-EXB-069 SUPP SHT 6. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, T ASK CARD NR 5009 C53-100-01, CPCP TASK CARD NR C53-100-01-06. 2 L 7 4 4F RT A20WE 1998112600479 19981126 00479 NM 1998 11 26 CKSA98675 1 19981120 A 5350 69B018351 CHANNEL BOEING 747 7472B4B 138481B NM BS 840 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STA 840, WL 91, RBL 21, THE AFT I/B FLANGE OF THE 69B01835-1 BODY FAIRING CHANNEL HAS AN AREA APPROX 1.50 SQ INCH WITH M ODERATE CORROSION. REPAIRED IAW BOEING ASA CKF-EXB-239 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSI ON, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7DI2902, CPCP TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600480 19981126 00480 NM 1998 11 26 CKSA98676 1 19981120 A 5311 65B0670444 FRAME BOEING 747 7472B4B 138481B NM BS 920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FWD AND AFT SIDE OF THE 65B06740-44 FRAME ASSY AT STA 920, WL 92, BL 0 TO LBL 20 HAS AREA OF LEVEL 2 CORROSION COVERING APPROX 10 PERCENT OF SFC. REPAIRED IAW BOEING ASA CKF-EXB-239 SUPP SHT 2 ITEM 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO 280, TASK CARD NR 7DI2902, CPCP TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600481 19981126 00481 NM 1998 11 26 CKSA98677 1 19981120 A 5713 65B150323 LONGERON BOEING 747 7472B4B 138481B NM BS 1438 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LONGERON CHORD AT LWG ZONE 100, STA 1372 TO STA 1460, WL 152, LBL 127 (LT OVERWING) REPLACED FOR LEVEL 2 CORROSION. FOU ND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA ( KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXB-068, CPCP TASK CARD NR C53-190-01-01. 2 L 7 4 4F RT A20WE 1998112600482 19981126 00482 NM 1998 11 26 CKSA98678 1 19981120 A 5521 65B057506 SPAR BOEING 747 7472B4B 138481B NM RT ELEVATOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT ELEVATOR REAR OUTBD SPAR, ZONE 300, HAS 6 AREAS 6 TO 8 INCHES OF SEVERE CORROSION WITH EXFOLIATION. REMOVED AND REPL ACED SPAR IAW BOEING DWG ASA CKF-EXB-217 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CT3001, CPCP TAS K CARD NR C55-330-01-02. 2 L 7 4 4F RT A20WE 1998112600483 19981126 00483 NM 1998 11 26 CKSA98679 1 19981120 A 5320 65B152612 WEB BOEING 747 7472B4B 138481B NM BS 1372 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 OUTBOARD SIDE OF WEB ASSY LOCATED ZONE 100, STA 1372 TO STA 1416, WL 152, RBL 127 HAS NUMEROUS AREAS OF SEVERE CORROSION AND PITTING. REPAIRED IAW BOEING DOCUMENT ASA CKF-EXB-223 SUPP SHTS 6 AND 7. FOUND DURING ACCOMPLISHMENT OF CARGO CON VERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXB-123, CPCP TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600484 19981126 00484 NM 1998 11 26 CKSA98680 1 19981120 A 5311 65B150092 FRAME BOEING 747 7472B4B 138481B NM BS 1394-1480 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CHORD VERT FLANGE AT ZONE 100, STA 1394 TO STA 1480, WL 152, RBL 127 HAS AREA APPROX 18 INCHES OF EXFOLIATED CORROSION. REPAIRED IAW BOEING ASA CKF-EXB-223 SUPP SHTS 6 AND 7. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHEC K, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXB-194, C PCP TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600485 19981126 00485 NM 1998 11 26 CKSA98681 1 19981120 A 5313 65B1500410 LONGERON BOEING 747 7472B4B 138481B NM BS 1350 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LONGERON AT ZONE 100, STA 1350 TO STA 1468, WL 152, RBL133 CHANGED FOR CORROSION. AT HORIZ FLANGE (REMOVED PREVIOUS PER S/B) WEB HAS LOCALIZED EXFOLIATION CORROSION. REPLACED LONGERON AND WEB IAW BOEING ASA CKF-EXB-223 SUPP SHTS 6 AND 7. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHI TA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXB-023, CPCP TASK CARD NR C53-190-01-02. 2 L 7 4 4F RT A20WE 1998112600486 19981126 00486 NM 1998 11 26 CKSA98682 1 19981120 A 5520 65B0575315 CHORD BOEING 747 7472B4B 138481B NM LT ELEVATOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LT ELEVATOR, ZONE 330 OUTBD, STA 260 TO STA 279, 2 INCH AND 4 INCH AREA CORRODED BEYOND SRM LIMITS. REPLACED CHORD IAW BOEING DWG 65B05753 AND BAC5004-L-2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHME NT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR REF-EXB-035, CPCP TASK CARD NR C5 5-330-01-01. 2 L 7 4 4F RT A20WE 1998112600487 19981126 00487 NM 1998 11 26 CKSA98683 1 19981120 A 5720 65B0782669 CHORD BOEING 747 7472B4B 138481B NM WS 1185 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LOWER T-CHORD OF WEB AT ZONE 500, OLES 1185 LT WING, SEVERE EXFOLIATED CORROSION EXISTS AT NOTED LOCATION MEASURES 12.0 X 1.5. REPAIRED IAW BOEING ASA CKF-EXW-121 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHEC K, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7C15021 NR 706 , CPCP TASK CARD NR C57-510-01-01. 2 L 7 4 4F RT A20WE 1998112600488 19981126 00488 NM 1998 11 26 CKSA98684 1 19981120 A 5753 65B02077202 SKIN BOEING 747 7472B4B 138481B NM RT TE AFT FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT AFT I/B TRAILING EDGE FLAP UPPER SKIN ON O/B PANEL HAS 5 EXISTING PATCHES NOT DONE IAW SRM REQUIREMENTS. PEELING, CO RROSION AND SEPARATING WERE REPAIRED IAW BOEING ASA CKF-EXW-010 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVER SION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CA RD NR 7C16018, CPCP TASK CARD NR C57-560-01-01. 2 L 7 4 4F RT A20WE 1998112600489 19981126 00489 NM 1998 11 26 CKSA98685 1 19981120 A 5753 65B1721719 PLATE BOEING 747 7472B4B 138481B NM RT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT WING FLAP TRACK BEARING PLATES AT STA 353 WBL 584 AND 743 (NR 5, 6, 7) SHOW MODERATE CORROSION. REPLACED PLATES IAW BOEING DWG 65B07782 AND ASA CKF-EXW-072 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, A ND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI6404, CPCP TASK CARD NR C57-560-03-02. 2 L 7 4 4F RT A20WE 1998112600490 19981126 00490 NM 1998 11 26 CKSA98686 1 19981120 A 5753 65B1307112 PLATE BOEING 747 7472B4B 138481B NM RT TE FLAP RUSTED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT FLAP TRACK NR 5, ZONE 600, MOUNTING PLATE SEVERE RUST FOUND. REPAIRED IAW BOEING ASA CKF-EXV-071 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIA B). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXW-056, CPCP TASK CARD NR C57-560-01-02. 2 L 7 4 4F RT A20WE 1998112600491 19981126 00491 NM 1998 11 26 CKSA98687 1 19981120 A 5753 65B020319 TIE PLATE BOEING 747 7472B4B 138481B NM LT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LT I/B MIDFLAP ZONE 500, WBL 216 LT, AN AREA 5 X 1.5 INCH OF EXFOLIATED CORROSION EXISTS ON LWR I/B SFC. REPAIRED IAW B OEING ASA CKF-EXW-115 SUPP SHT 1 AND 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLIS HMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXW-050, CPCP TASK CARD NR C57-560-01-01. 2 L 7 4 4F RT A20WE 1998112600492 19981126 00492 NM 1998 11 26 CKSA98688 1 19981120 A 5753 CKFEXW0831 TRACK BOEING 747 7472B4B 138481B NM LT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 ZONE 500, NR 4 LT FLAP TRACK BUSHING FWD BOLT HOLES AND MOUNTING AREA CORRODED BEYOND LIMITS. REPAIRED IAW BOEING ASA C KF-EXW-083 SUPP SHT 2. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TAS K CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-6XW-07L, CPCP TASK CARD NR C57-560-01-01. 2 L 7 4 4F RT A20WE 1998112600493 19981126 00493 NM 1998 11 26 CKSA98689 1 19981120 A 5753 CKFEXW1081 TRACK BOEING 747 7472B4B 138481B NM LT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 ZONE 500, NR 1 LT FLAP TRACK BUSHING FWD BOLT HOLES AND MOUNTING AREA CORRODED BEYOND LIMITS. REPAIRED IAW BOEING ASA C KF-EXW-108 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TAS K CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXW-055, CPCP TASK CARD NR C57-560-01-01. 2 L 7 4 4F RT A20WE 1998112600494 19981126 00494 NM 1998 11 26 CKSA98690 1 19981120 A 5753 ASACKFEXW1171 TRACK BOEING 747 7472B4B 138481B NM RT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT WING FLAP TRACKS NR 6, 7, 8, ZONE 600, BUSHING MOUNT HOLES CORRODED. REWORKED BUSHING MOUNTS IAW BOEING ASA CKF-EXW- 117 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXW-051, 052, 054, CPCP TASK CARD NR C57-560-01-02 . 2 L 7 4 4F RT A20WE 1998112600495 19981126 00495 NM 1998 11 26 CKSA98691 1 19981120 A 5753 65B170681 TRACK BOEING 747 7472B4B 138481B NM RT TE FLAP PITTED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 FLAP TRACK NR 5 RT, ZONE 600, WING TO TRACK MATING SURFACE PITTED BEYOND LIMITS. REPAIRED IAW BOEING ASA CKF-EXW-130 SU PP SHT 1, OHM 57-52-70 REPAIR 6-1, S/B 747-57-2207 FIG 1; NOTES 5, 12, 13 AND OHM 57-52-70 REPAIR 1-1, PARA 1C & 1E. FO UND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR C57-560-01-02, CPCP TASK CARD NR C57-560-01-02. 2 L 7 4 4F RT A20WE 1998112600496 19981126 00496 NM 1998 11 26 CKSA98692 1 19981120 A 5753 WEB BOEING 747 7472B4B 138481B NM RT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT OUTBD T/E MIDFLAP NR 3 SPAR WEB AT CENTER OF FLAP HAS 2 AREA OF CORROSION BEYOND LIMITS. REPAIRED WEB IAW BOEING ASA CKF-EXW-135. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS A T BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXW-021, CPCP TASK CARD NR C57-560-01-02. 2 L 7 4 4F RT A20WE 1998112600497 19981126 00497 NM 1998 11 26 CKSA98693 1 19981120 A 5753 65B170621 PLATE BOEING 747 7472B4B 138481B NM RT TE FLAP CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT TRAILING EDGE FLAP TRACKS 1, 2, 3, SIDE LOAD SURFACES (UPPER INBD AND AFT OUTBD) CORRODED BEYOND LIMITS. REPAIRED IA W BOEING ASA CKF-EXW-132 SUPP SHT 1, 2, 3. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMP LISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR CKF-EXW-053 058 108, CPCP T ASK CARD NR C57-560-01-01. 2 L 7 4 4F RT A20WE 1998112600498 19981126 00498 NM 1998 11 26 CKSA98694 1 19981120 A 5313 65B0436656 STRINGER BOEING 747 7472B4B 138481B NM BS 887 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LOCATED AT STA 887 STR 44L WL 118 STRINGER HAS AN AREA OF CORROSION 1.20 X .80 BEYOND SRM LIMITS. REPAIRED IAW SRM 51-1 0-01 & CPM 20-40-00 AND BOEING ASA CKF-K1-029 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CH ECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI1014, CPC P TASK CARD NR C53-125-01-01. 2 L 7 4 4F RT A20WE 1998112600499 19981126 00499 NM 1998 11 26 CKSA98695 1 19981120 A 5313 65B041182 STRINGER BOEING 747 7472B4B 138481B NM BS 734-745 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STRINGER LOCATED AT STA 743 TO STA 745, STR 47L, WL 92 HAS AREA APPROX 6 LENGTH OF LEVEL 2 CORROSION. REPAIRED STRINGER IAW BOEING ASA CKF-K1-017. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPC P TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI1014, CPCP TASK CARD NR C53-125-01-01. 2 L 7 4 4F RT A20WE 1998112600500 19981126 00500 NM 1998 11 26 CKSA98696 1 19981120 A 5311 65B074112 FRAME BOEING 747 7472B4B 138481B NM BS 940 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 CHORD LOCATED AT K1 FWD CARGO, ZONE 100 STA 940 WL 118 LBL 6 TOP CAP HAS AREA .40 DIAMETER OF CORROSION. AREA IS ADJACE NT TO A NR 6 COUNTERSUNK RIVET. REPAIRED IAW BOEING ASA CKF-K1-028 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CO NVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TAS K CARD NR 7CI1014, CPCP TASK CARD NR C53-110-01-02. 2 L 7 4 4F RT A20WE 1998112600501 19981126 00501 NM 1998 11 26 CKSA98697 1 19981120 A 5313 65B041182 STRINGER BOEING 747 7472B4B 138481B NM BS 835-842 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LOCATED AT K1 FWD CARGO, ZONE 100 STA 835 TO STA 842 WL 91 LBL 5 THE I/B AND O/B FLANGES OF STRINGER HAS 3 AREAS OF SEVE RE CORROSION 7' X 1'. REPAIRED STRINGER IAW BOEING ASA CKF-K1-015 SUPP SHT 1. FOUND DURING ACCOMPLISHMENT OF CARGO CON VERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI1014, CPCP TASK CARD NR C53-125-01-01. 2 L 7 4 4F RT A20WE 1998112600502 19981126 00502 NM 1998 11 26 CKSA98698 1 19981120 A 5210 65B0988915 GATE BOEING 747 7472B4B 138481B NM L2 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LT DOOR NR 2 UPPER GATE ASSY HAS SEVERE CORROSION EXTENDING UNDER HINGE. REMOVED AND REPLACED UPPER GATE ASSY IAW BOEIN G ASA CKF-MEO-017 DWG 65B09889. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI8323, CPCP TASK CARD NR C53-210-09- 01. 2 L 7 4 4F RT A20WE 1998112600503 19981126 00503 NM 1998 11 26 CKSA98699 1 19981120 A 5220 65B135933 GATE BOEING 747 7472B4B 138481B NM L3 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 NR 3 LT DOOR LOWER GATE ASSY CORRODED ALONG LOWER EDGE (REF IPC 52-11-09-02, ITEM NR 65). REMOVED CORROSION IAW SRM 51- 10-01, FOUND TO BE BEYOND SRM LIMITS. REMOVED AND REPLACED LOWER GATE PER DWG 65B13593, BAC5004-2 AND -1, BAC5009. FOU ND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA ( KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI8333, CPCP TASK CARD NR C53-210-09-01. 2 L 7 4 4F RT A20WE 1998112600504 19981126 00504 NM 1998 11 26 CKSA98700 1 19981120 A 5220 65B0988915 GATE BOEING 747 7472B4B 138481B NM L4 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LT NR 4 DOOR UPPER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED UPPER GATE ASSY IAW BOEING ASA CKF-MED-018, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR 7CI8343, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600505 19981126 00505 NM 1998 11 26 CKSA98701 1 19981120 A 5220 65B0989125 GATE BOEING 747 7472B4B 138481B NM L5 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 LT NR 5 DOOR UPPER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED UPPER GATE ASSY IAW BOEING ASA CKF-MED-015. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR 7CI8353, CPCP TA SK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600506 19981126 00506 NM 1998 11 26 CKSA98702 1 19981120 A 5220 65B135916 GATE BOEING 747 7472B4B 138481B NM R1 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT NR 1 DOOR LOWER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED LOWER GATE ASSY IAW BOEING ASA CKF-MED-066, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR 7CI8413, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600507 19981126 00507 NM 1998 11 26 CKSA98703 1 19981120 A 5220 65B0989012 GATE BOEING 747 7472B4B 138481B NM R2 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT NR 2 DOOR LOWER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED LOWER GATE ASSY IAW BOEING ASA CKF-MED-007, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR 7CI8423, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600508 19981126 00508 NM 1998 11 26 CKSA98704 1 19981120 A 5220 65B135933 GATE BOEING 747 7472B4B 138481B NM R3 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT NR 3 DOOR LOWER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED LOWER GATE ASSY IAW BOEING ASA CKF-MED-008, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR 7CI8433, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600510 19981126 00510 NM 1998 11 26 CKSA98706 1 19981120 A 5220 65B0989126 GATE BOEING 747 7472B4B 138481B NM R5 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT NR 5 DOOR UPPER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED UPPER GATE ASSY IAW BOEING ASA CKF-MED-014, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR N/A, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600511 19981126 00511 NM 1998 11 26 CKSA98707 1 19981120 A 5220 65B0989218 GATE BOEING 747 7472B4B 138481B NM R5 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT NR 5 DOOR LOWER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED LOWER GATE ASSY IAW BOEING ASA CKF-MED-012, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR 7CI8453, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600512 19981126 00512 NM 1998 11 26 CKSA98708 1 19981120 A 5240 65B135892 GATE BOEING 747 7472B4B 138481B NM R1 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT NR 1 DOOR UPPER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED UPPER GATE ASSY IAW BOEING ASA CKF-MED-016, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR 7CI8413, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998112600513 19981126 00513 NM 1998 11 26 CKSA98709 1 19981120 A 5313 65B04107 STRINGER BOEING 747 7472B4B 138481B NM BS 680 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 STRINGER LOCATED AT K1 FWD CARGO, ZONE 100, STA 680 LBL 5 STRINGER 47L HAS HEAVY EXFOLIATED CORROSION IN BOTTOM OF STRIN GER (APPROX 2 LONG). REPAIRED IAW BOEING ASA CKF-K1-037. FOUND DURING ACCOMPLISHMENT OF CARGO CONVERSION, ROUTINE C-CH ECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, TASK CARD NR N/A, CPCP TA SK CARD NR C53-125-01-01. 2 L 7 4 4F RT A20WE 1998112600514 19981126 00514 WP 1998 11 26 98ZZZM870 1 19980714 A 2120 UNKNOWN DOUG DC8 DC8F54 3021926 WP CABIN ODOR A FXLA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SO 19 54FA 59952 45637 ON ARRIVAL GYE, REPORTED SMOKE ODOR FROM UNKNOWN SOURCE IN COCKPIT AND CABIN. ON GROUND, RAN ENGINES AND PRESSURIZED AI RCRAFT TO CHECK NASI PNEUMATIC FLOW CONTROL SYSTEM IAW STC ST466CH. NO SMOKE ODOR WAS NOTED IN AIRCRAFT. AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER REPORTS RECEIVED ON SUBSEQUENT FLIGHTS. (M) 2 L 7 4 4F 4A25 1998112600515 19981126 00515 NM 1998 11 26 USAA980432 1 19980924 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 42998 22751 TPA - DURING CX-3 CEHCK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK IN EXTERNAL SKIN RIGHT SIDE OF FUSELAGE AT STATION 727 A PLUS 8 INCHES AND STRINGER 18R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998112600516 19981126 00516 NM 1998 11 26 USAA980431 1 19980924 A 5330 SKIN BOEING 737 737201 1384454 NM BS 757 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 42998 22751 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN SKIN RIGHT SIDE FUSELAGE STATION 757 AND STRINGER 18 R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998112600517 19981126 00517 NM 1998 11 26 USAA980430 1 19980924 A 5330 SKIN BOEING 737 737201 1384454 NM BS 927 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 245US 42998 22751 TPA - DURING CX-6 CHECK VISUAL INSPECTION, FOUND A 3.5 INCH CRACK IN FUSELAGE SKIN RIGHT AFT FUSELAGE STATION 927 AND ST RINGER 22R. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1998112600518 19981126 00518 NM 1998 11 26 USAA980435 1 19980920 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 1016/1003 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 262AU 40679 22868 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND CORROSION 10 INCH BY 1 INCH STRINGER 27L FS 1016-1003. CUT OUT CORRODE D STRINGER AND REPLACED AND SPLICED NEW STRINGER PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1998112600519 19981126 00519 EU 1998 11 26 USAA980540 1 19981022 A 5320 1718730 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3845-3450 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 896US 15938 11391 PIT - DURING Q-1 CHECK, FOUND CORROSION AROUND SCREW HOLES 1 INCH AT T-CAP BL 11276 STATION 3845-3450. REPLACED T-CAP. (M) 2 L 7 2 4F RT 1998112600520 19981126 00520 EU 1998 11 26 USAA980539 1 19981022 A 5320 ANGLE FOKKER F28 F28MK0100 4990807 EU BS 14911 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 896US 15938 11391 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK WING ATTACH ANGLE LEFT SIDE AT STATION 14911 BETWEEN STRINGER 10 AND 12. LOC ALLY FABRICATED ANGLE JOB CARD NR J5-90-0900-029. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT 1998112600521 19981126 00521 EU 1998 11 26 USAA980538 1 19981022 A 5320 ANGLE FOKKER F28 F28MK0100 4990807 EU BS 14911 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 896US 15938 11391 PIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK WING ATTACH ANGLE RIGHT SIDE AT STATION 14911 BETWEEN STRINGER 66 AND 64. LO CALLY FABRICATED ANGLE JOB CARD NR J5-90-09-000-029. INSTALLED DOUBLER. (M) 2 L 7 2 4F RT 1998112600522 19981126 00522 EU 1998 11 26 USAA980537 1 19981022 A 5320 1718730 BEAM FOKKER F28 F28MK0100 4990807 EU BS 4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 896US 15938 11391 PIT - DURING Q-1 CHECK, FOUND CORROSION 4 INCHES, 100 PERCENT CORRODED THROUGH ON BEAM AT STATION 4850 BL NR 0. REPLACE D T-CAP. (M) 2 L 7 2 4F RT 1998112600523 19981126 00523 EU 1998 11 26 USAA980536 1 19981022 A 5320 1718730 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3845-3450 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 896US 15938 11391 PIT - DURING Q-1 CHECK, FOUND HEAVY CORROSION 8 INCHES BY WIDTH OF T-CAP 4 INCHES APPROX AT BL 1127L STATION 3845-3450. REPLACED T-CAP. (M) 2 L 7 2 4F RT 1998112600524 19981126 00524 EU 1998 11 26 USAA980535 1 19981022 A 5330 1154765 SKIN FOKKER F28 F28MK0100 4990807 EU BS 4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 896US 15938 11391 PIT - DURING Q-1 CHECK, FOUND CORROSION 1 INCH AROUND SCREW HOLES ON SKIN AT BL 600 STATION 4850. REPLACED BEAM. (M) 2 L 7 2 4F RT 1998112600525 19981126 00525 NM 1998 11 26 USAA980522 1 19981021 A 5315 6545808179 FLOORBEAM BOEING 737 737401 1384701 NM BS 294 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 27716 23876 CLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 52 INCH ACROSS FLOORBEAM EACH SCREW HOLE 1 INCH BY 2 INCH AREA OF CORR OSION STATION 294.5, LBL 7 RBL 45 FLOORBEAM UPPER CHORD. CORROSION TASK NR C 53-107-02. BURNISHED FLOORBEAM EXCEPT AT STATION LBL 7, REPAIRED DOUBLER ANGLES PER EA 62682 AND SRM 51-70-12. (M) 2 L 7 2 4F RT A16WE 1998112600526 19981126 00526 NM 1998 11 26 USAASB98273 1 19981018 A 3350 15AT17 SWITCH BOEING 737 7372B7 1384560 NM COCKPIT FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 280AU 22892 PIT - MAINTENANCE FOUND ALL EMERGENCY LIGHTS INOP THROUGHOUT THE AIRCRAFT. MAINTENANCE FOUND THE EMERGENCY LIGHT SWITCH IN THE COCKPIT BAD. REMOVED AND REPLACED SWITCH. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998112600527 19981126 00527 NM 1998 11 26 USAASB98275 1 19981019 A 3350 320562 CONNECTOR BOEING 737 737201 1384454 NM ROW 13 LOOSE A USAA O OTHER O OTHER CR CRUISE 1 EA 19 263AU 22869 TPA - PILOT REPORTED THAT THE EMERGENCY EXIT LIGHTS AND THE FLOOR EMERGENCY LIGHTS ILLUMINATED ON THEIR OWN DURING FLIGH T. MAINTENANCE FOUND A CONNECTOR AT SEAT ROW 13 LEFT, NO MAKING GOOD CONTACT. REMOVED AND REPLACED CONNECTOR. OPERATI ONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998112600528 19981126 00528 NM 1998 11 26 USAASB98272 1 19981015 A 3350 62AT223 SWITCH BOEING 737 737201 1384454 NM CABIN FAILED A USAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 EA 19 263AU 22869 PHL - FLT 1244 - AFTER PUSHBACK, EMERGENCY EXI TLIGHTS IN SEAT ROWS ILLUMINATED AND COULD ONLY BE EXTINGUISHED BY TURNIN G OFF THE EMERGENCY EXIT LIGHTS SWITCH IN COCKPIT. AIRCRAFT RETURNED TO GATE. MAINTENANCE TROUBLESHOT SYSTEM AND REPLA CED THE FLIGHT ATTENDANT AFT EMERGENCY EXIT SWITCH AND RESOLDERED BROKEN CONNECTION AT SEAT ROW 5 ABC. CHECKED WIRING A ND OPERATION OF COCKPIT SWITCH AND LEFT OVERWING EMERGENCY EXIT DOOR SWITCH S298. RESEATED THE OVERWING EXIT DOORS. GR OUND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998112600529 19981126 00529 NM 1998 11 26 USAA980521 1 19981021 A 5347 69403526 SEAT TRACK BOEING 737 737401 1384701 NM BS 328-336 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 27716 23876 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND CORROSION ON SEAT TRACK STATION 328 TO 336 RBL 22. CORROSION TASK NR C 53-107-02. INSTALLED NEW SEAT TRACK PER SRM 53-00-52. (M) 2 L 7 2 4F RT A16WE 1998112600530 19981126 00530 NM 1998 11 26 USAA980468 1 19980930 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 300-340 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AT LWR THRESHOLD SUPPORT ZEE AREA FWD SERVICE DOOR STATION 300 TO 340 ZEE ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-1. (M) 2 L 7 2 4F A16WE 1998112600531 19981126 00531 NM 1998 11 26 USAA980467 1 19980930 A 5311 FRAME BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A CRACK OUTBOARD FRAME CHORD BS 727 STRINGER 15L. INST ALLED DOUBLERS, FILLERS AND STRAPS PER EA 62502. (M) 2 L 7 2 4F A16WE 1998112600532 19981126 00532 NM 1998 11 26 C8GA1006981 1 19981006 A 2740 651948215 JACKSCREW BOEING 727 727214 138407R NM STAB TRIM FAILED A C8GA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 15 227JL 20875 FLT 312 - KPHL-TJSJ - AFTER TAKEOFF AT FL 180, THE AUTO PILOT DISENGAGED AND THE STABILIZER TRIM JAMMED AT 5 DEGREES NOS E UP. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO KPHL. THE STABILIZER TRIM BECAME OPERATIONAL ON APPROACH A T 700 FT AGL. THE AIRCRAFT LANDED WITHOUT INCIDENT. A STABILIZER SYSTEM INSPECTION WAS PERFORMED. NO DISCREPANCIES WE RE NOTED. THE JACKSCREW AND GEARBOX WERE CLEANED LUBED, AND AIRCRAFT RELEASED FOR A LOCAL ACCEPTANCE FLIGHT. DURING TH E ACCEPTANCE FLIGHT AT FL 180, THE STABILIZER TRIM JAMMED AGAIN. THE CREW DECLARED ANOTHER EMERGENCY AND RETURNED TO KP HL. THE A/C LANDED WITHOUT INCIDENT. (M) 2 L 7 3 4F A3WE 1998112600533 19981126 00533 NM 1998 11 26 TSAA9833532 1 19981001 A 3350 9221009 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED AFT SERVICE DOOR IDENTIFIER EMERGENCY LIGHT ASSY. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998112600534 19981126 00534 NM 1998 11 26 TSAA9833528 1 19981001 A 3350 1000679 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED THE AFT DOOR EMERGENCY LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998112600535 19981126 00535 NM 1998 11 26 TSAA9833558 1 19981107 A 3350 6013211 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPERATIONAL CHECK GOOD. AIRCR AFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998112600536 19981126 00536 NM 1998 11 26 TSAA9833557 1 19981107 A 3350 8731002511 LIGHT BOEING 737 7372M6C 1384708 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY LIGHT DUE TO BEING INOP. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F RT A16WE 1998112600537 19981126 00537 EU 1998 11 26 SIMA983061 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - LOWER EXTERNAL FUSELAGE SKIN IS CORRODED IN SEVERAL PLACES BETWEEN FS 590 AND 614 FROM CENTERLINE, TO APPROX 24 IN CHES OUTBOARD LEFT, STATION 604-608, WL CL-10. POLISHED OUT UP TO 50 PERCENT SKIN THICKNESS, BEAD BLASTED AREA. FABRIC ATED AND INSTALLED EXTERNAL DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600538 19981126 00538 EU 1998 11 26 SIMA983035 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 174AE 340B174 OKC - AFT EXTERNAL FUSELAGE BELLY SKIN IS CORRODED AROUND BUTT JOINT AT STATION 622. CUT OUT DAMAGE, FABRICATED AND INS TALLED FILLER FROM .040 AND DOUBLER FROM .063. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600539 19981126 00539 EU 1998 11 26 SIMA983034 1 19981102 A 5330 AL2024T3 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 174AE 340B174 OKC - LEFT SIDE OF EXTERNAL FUSELAGE SKIN IS CORRODED AT FS 413 WL 113.8. BEAD BLASTED SKIN, FABRICATED AND INSTALLED E XTERNAL DOUBLER AND TRIPLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600540 19981126 00540 EU 1998 11 26 SIMA9830616 1 19981102 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 ABI - LEFT NACELLE OUTBOARD UPPER SKIN CHAFING. CUT OUT DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION. NO INDICATION S OF CRACKS. FABRICATED AND INSTALLED REINFORCEMENT DOUBLER .025 INCH. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600542 19981126 00542 EU 1998 11 26 SIMA9830613 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 733 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 180AE 340B180 ABI - DURING MBV INSPECTION, AN AREA OF CORROSION FOUND BEYOND SRM LIMITS ON EXTERIOR FUSELAGE SKIN AT FS 733 ABOVE SL 1 504. CORROSION REMOVED, EDDY CURRENT INSPECTION DONE WITH NO INDICATION OF CRACKS. FABRICTED DOUBLER AND TRIPLER .032 THICH. ATTACHED TO FUSELAGE, AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600543 19981126 00543 EU 1998 11 26 SIMA9830612 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - EXTERNAL FUSELAGE BELLY SKIN IS CORRODED AT FS 668. CUT OUT CORRODED SKIN, FABRICATED AND INSTALLED DOUBLER. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600544 19981126 00544 EU 1998 11 26 SIMA9830611 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - EXTERNAL FUSELAGE BELLY SKIN IS CORRODED FROM FS 710 TO FS WL 65. CUT OUT CORRODED AREA. FABRICATED AND INSTALLE D FILLER AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600545 19981126 00545 EU 1998 11 26 SIMA9830610 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - LEFT SIDE OF EXTERNAL FUSELAGE SKIN IS CORRODED AT S 605, WL 76. PERFORMED DYE PENETRANT INSPECTION AND INSTALLED DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600546 19981126 00546 EU 1998 11 26 SIMA983069 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - EXTERNAL FUSELAGE SKIN IS CORRODED JUST FORWARD OF THE CARGO DOOR, FROM FS 575-FS 625 WL 63 - WL 67.5. CUT OUT TW O AREAS OF CORROSION. FABRICATED AND INSTALLED TWO DOUBLERS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600547 19981126 00547 EU 1998 11 26 SIMA983068 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - EXTERNAL FUSELAGE SKIN IS CORRODED AT FS 793 WL 90 TO 113. CUT OUT CORRODED SKIN, FABRICATED AND INSTALLED FILLER , EXTERNAL DOUBLER, AND TRIPLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600548 19981126 00548 EU 1998 11 26 SIMA983066 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - LARGE AREA OF CORROSION ON BELLY OF EMPENNAGE FROM FS 793 FS 803 CL TO 10 INCHES OUTBOARD LEFT, AFT TO HATCH ACCES S. CUT OUT CORROSION, FABRICATED AND INSTALLED FILLER AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600549 19981126 00549 EU 1998 11 26 SIMA983065 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - LEFT SIDE OF FUSELAGE SKIN HAS CORROSION AT FS 710-718 AND A SMALL DENT BELOW CARGO DOOR AT FS 718 WL 65. CUT OUT CORROSION AND DENT, FABRICATED AND INSTALLED FILLER AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600550 19981126 00550 EU 1998 11 26 SIMA983064 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - LEFT SIDE OF FUSELAGE EXTERNAL DOUBLER AND SKIN AROUND DOUBLER IS CORRODED AT STRINGER SL 1504, FS 464 AT CROWN EL FT. REMOVED DOUBLER, CUT OUT DAMAGE. FABRICATED AND INSTALLED FILLER AND NEW DOUBLER. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4T RT A52EU 1998112600551 19981126 00551 EU 1998 11 26 SIMA983063 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - RIVET HEADS SANDED FLAT ON EXTERNAL AFT FUSELAGE SKIN INBOARD OF LEFT HORIZONTAL STABILIZER. CORROSION AND A CREA SE ALSO EXIST Y790-Y793, WL 130-138. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER. AIRCRAFT RETUR NED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600552 19981126 00552 EU 1998 11 26 SIMA983062 1 19981102 A 5330 SKIN SAAB SF340 340B 7860101 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 177AE 340B177 OKC - EXTERNAL FUSELAGE SKIN IS CORRODED ON SL 1505 AND SL 1506 AT Y439 AND CROWN. BLENDED OUT PITS, FABRICATED AND INS TALLED DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998112600553 19981126 00553 EU 1998 11 26 SIMA983032 1 19981030 A 3350 3013000 BATTERY PACK AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 533AT 8458 533 DFW - FLT 3613 - FORWARD EMERGENCY LIGHTS DO NOT TEST CORRECTLY. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT POWER SUP PLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998112600554 19981126 00554 EU 1998 11 26 SIMA982746 1 19981001 A 5347 S53678001202 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 211 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AFT INBOARD AND FLIGHT ATTENDANT, THE RIGHT AFT INBOARD AND FLIGHT ATTEND ANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600555 19981126 00555 EU 1998 11 26 98ZZZM871 1 19981001 A 5347 S53678001210 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 211 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AFT INBOARD AND FLIGHT ATTENDANT, THE RIGHT AFT INBOARD AND FLIGHT ATTEND ANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600556 19981126 00556 EU 1998 11 26 98ZZZM872 1 19981001 A 5347 S53678001204 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 211 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AFT INBOARD AND FLIGHT ATTENDANT, THE RIGHT AFT INBOARD AND FLIGHT ATTEND ANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600557 19981126 00557 EU 1998 11 26 98ZZZM873 1 19981001 A 5347 S5337500121402 SEAT TRACKS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 211 SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT AFT INBOARD AND FLIGHT ATTENDANT, THE RIGHT AFT INBOARD AND FLIGHT ATTEND ANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600558 19981126 00558 EU 1998 11 26 SIMA982747 1 19981001 A 5330 S5367128920005 SKIN AEROSP ATR42 ATR42300 8680920 EU BS 31-32 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 211 SAW - DURING CPCP-1 INSPECTION, CLEARED DMI 213MQ53014D. DENT IN LEFT SIDE OF THE FUSELAGE BETWEEN FRAME 31 AND 32, AT STRINGER 16. REPAIRED DENT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600559 19981126 00559 EU 1998 11 26 SIMA982748 1 19981001 A 5320 S5367800920102 SUPPORT AEROSP ATR42 ATR42300 8680920 EU BS 36-38 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 211 SAW - DURING CPCP-1 INSPECTION, FOUND THE RIGHT FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 CORRODED. REMOVED AND REPLACED F LOOR SUPPORT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600560 19981126 00560 EU 1998 11 26 SIMA982761 1 19981001 A 5315 S5367240921802 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 213AT 211 SAW - DURING CPCP-1 INSPECTION, FOUND THE FLOORBEAM 40 CORRODED AROUND THE NUT PLATE CLIPS. REPAIRED FLOORBEAM. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600561 19981126 00561 EU 1998 11 26 SIMA982992 1 19981026 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 310DK 17785 310 GRR - FLT 4028 - SEVERAL EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK. OPERAT IONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998112600562 19981126 00562 EU 1998 11 26 SIMA983011 1 19981028 A 5315 S53672408202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 233RM 235 DURING CPCP1 INSPECTION, FOUND TOP OF FLOORBEAM 39 CORRODED. REPAIRED FLOORBEAM. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600563 19981126 00563 EU 1998 11 26 SIMA983012 1 19981028 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 233RM 235 SAW - DURING CPCP-1 INSPECTION, FOUND RIGHT OUTBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED SEAT TRACK. AIRCRAFT RE TURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600564 19981126 00564 EU 1998 11 26 SIMA983003 1 19981027 A 5330 SKIN AEROSP ATR72 ATR72212 EU BS 8-10 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 ABI - DAMAGE ON RIGHT LOWER FUSELAGE BETWEEN FRAMES 8 AND 10, AND BETWEEN STRINGER 20 AND BL 0. CUT OUT DAMAGE, PERFORM ED EDDY CURRENT INSPECTION. FABRICATED AND INSTALLED EXTERNAL DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600565 19981126 00565 EU 1998 11 26 SIMA983023 1 19981029 A 2150 22051201 ACM AEROSP ATR72 ATR72212 EU LT PACK SEIZED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 414WF 7257 0242 414 MIA - FLT 5804 - FOUL ODOR MIXED WITH POSSIBLE SMOKE IN THE CABIN/COCKPIT. SMELL ISOLATED TO THE LEFT ACM. REMOVED AND REPLACED AIR CYCLE MACHINE. (M) 2 H 7 2 4T RT A53EU 1998112600566 19981126 00566 EU 1998 11 26 SIMA983091 1 19981105 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN INOP A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 320AE 19200 340B320 DFW - FLT 3706 - OVERHEAD EMERGENCY LIGHTS AT SEATS 3A, 4BC, 5BC AND FLOOR PROXIMITY LIGHTS AT 4 BC AND 5 BC DO NOT ILLU MINATE. REMOVED AND REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998112600567 19981126 00567 EU 1998 11 26 SIMA983071 1 19981103 A 2910 S2918156104200 LINE AEROSP ATR72 ATR72212 EU HYD SYSTEM FAILED A SIMA O OTHER K FLUID LOSS DE DESCENT 1 SW 21 288AM 288 DFW - FLT 3690 - GREEN SYSTEM HYDRAULIC LOW LEVEL WARNING LIGHT CAME ON. PULLED EMERGENCY GEAR EXTENSION HANDLE. REMOV ED AND REPLACED BROKEN PIPE FROM THE GREEN ACCUMULATOR TO THE BRAKE MANIFOLD. RESERVICED HYDRAULIC SYSTEM AND PERFORMED LEAK CHECK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600568 19981126 00568 EU 1998 11 26 SIMA983081 1 19981104 A 5315 S536724080100 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600569 19981126 00569 EU 1998 11 26 98ZZZM874 1 19981104 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETU RNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600571 19981126 00571 EU 1998 11 26 98ZZZM875 1 19981105 A 3350 3012001 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AT 11120 420 DFW - FLT 3504 - SOME EMERGENCY FLOOR LIGHTS REMAIN ILLUMINATED. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1998112600572 19981126 00572 NE 1998 11 26 SIMA983112 2 19981107 A 7510 6068T56P01 VALVE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LT ENGINE FAILED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 21 298AE GRTB2692 340B298 785158 DFW - FLT 5089 - AT ABOUT 400 FT, THE CREW TURNED ON THE INLET ANTI-ICE PROTECTION, AND THE LEFT AIR VALVE WARNING LIGHT CAME ON. THEY CYCLED THE SWITCH A COUPLE OF TIMES BUT THE LIGHT DID NOT GO OUT. AT ABOUT 2000 FT, THE LEFT ENGINE STA RTED LOSING POWER. THE ENGINE WAS SHUTDOWN. REMOVED AND REPLACED THE LEFT AIR VALVE. INSPECTED THE ENGINE AND PERFORM ED RUNS WITH NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998112600573 19981126 00573 WP 1998 11 26 AALA981707 1 19980920 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 70404 49315 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT NEAR AFT CABIN DOOR INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEAR AFT CABIN DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998112600574 19981126 00574 EU 1998 11 26 C2XA98IA451 1 19981029 A 5320 S53070210208 SPLICE AEROSP ATR42 ATR42500 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16450 510 IAH - DURING C-CHECK INSPECTION, THE SPLICE AT STRINGER 16 RIGHT FRAME 29 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPLICE IAW ATR42-500 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600575 19981126 00575 EU 1998 11 26 C2XA98IA454 1 19981029 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19812 99 EFD - DURING MAINTENANCE INSPECTION, THE AISLE PATH EMERGENCY LIGHTING WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 AND NR 3 EMERGENCY LIGHT BATTERY PACKS IAW ATR42-320 MM 33-51-21, AND THE AIRCRAFT WAS APPROVED F OR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600576 19981126 00576 EU 1998 11 26 C2XA98IA452 1 19981029 A 5347 S53678001214 SEAT TRACK AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16450 510 IAH - DURING C-CHECK INSPECTION, THE LEFT FLIGHT ATTENDANTS SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AN D REPLACED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600577 19981126 00577 EU 1998 11 26 C2XA98IA450 1 19981029 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16450 510 IAH - DURING C-CHECK INSPECTION, THE RIGHT FLIGHT ATTENDANTS SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED SEAT TRACK AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998112600578 19981126 00578 WP 1998 11 26 AALA981587 1 19980825 A 2913 314195 PUMP VICKERS DOUG DC9 DC982 3022082 WP RT ENGINE FAILED A AALA K NONE J WARNING INDICATION CR CRUISE 1 SW 07 587AA BBDDNKW 53250 DFW - FLT 1564 - DURING CRUISE EN ROUTE NR 2 HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. EXTENDED LANDING GEAR USING EMERGENCY HANDLE. LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT ENGINE HYDRAULIC PUMP AND FILTERS. SYSTEM GROUND CHECKE D NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998112600579 19981126 00579 WP 1998 11 26 AALA981589 1 19980817 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 7537A 49991 TUL - AFT CARGO CORROSION ON FRAME AFT SIDE LOWER LIP FS 1287 FROM LG 29R, LG29L. INSTALLED DOUBLER PER 53-03. (M) 2 L 7 2 4F A6WE 1998112600580 19981126 00580 NM 1998 11 26 AALA981997 1 19981026 A 5320 ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1756 48491 TUL - T-ANGLE CORRODED UNDER NR 2 GALLEY MOUNT AT STATION 2007. REMOVED AND REPLACED T-ANGLE PER AARD 51-10-00-00-1. ( M) 2 L 7 3 4F RT A22WE 1998112600581 19981126 00581 EU 1998 11 26 AALA981714 1 19980921 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1437B 11427 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 15 INOPERATIVE. REPLACED EMERGENCY E XIT FLOOR PATH LIGHT STRIP AT SEAT ROW 15. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998112600582 19981126 00582 EU 1998 11 26 AALA981823 1 19980928 A 3397 WIRE FOKKER F28 F28MK0100 4990807 EU CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1413A 11376 DFW - EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS AND HALFWAY DOWN COACH INOPERATIVE. REPAIRED SHORTED WIRE IN EM ERGENCY EXIT FLOOR PATH LIGHT STRIPS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998112600583 19981126 00583 NM 1998 11 26 AALA981912 1 19981013 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN CORRODED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS FOR LAST SIX FEET OF TRACK INOPERATIVE. SPLICED NE W WIRE IN EMERGENCY EXIT FLOOR PATH LIGHT STRIP. (M) 2 L 7 3 4F A3WE 1998112600584 19981126 00584 NM 1998 11 26 AALA981710 1 19980921 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 896AA 22012 DFW - DURING OVERNIGHT MAINTENANCE, R2 DOOR EMERGENCY EXIT FLOOR PATH LIGHTING JUMPER WIRE BROKEN. REPLACED R2 DOOR EM ERGENCY EXIT FLOOR PATH LIGHT JUMPER WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600585 19981126 00585 NM 1998 11 26 AALA981711 1 19980901 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 896AA 22012 DFW - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT HAS ONE LIGHT INOPERATIVE. REPLACED EME RGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600586 19981126 00586 NM 1998 11 26 AALA981719 1 19980923 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 872AA 21384 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR P ATH LIGHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600587 19981126 00587 NM 1998 11 26 AALA981721 1 19980924 A 3350 CONNECTOR BOEING 727 727223 1384074 NM CABIN CONTAMINATED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 898AA 22014 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT CEILING LIGHT AT ROW 9 INOPERATIVE. CLEANED CONTACTS ON OVERHEAD EME RGENCY EXIT LIGHT AT ROW 9. SYSTEM GROUND CHECKED NROMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600588 19981126 00588 EU 1998 11 26 AALA981831 1 19980930 A 3350 P2010031301 LIGHT FOKKER F28 F28MK0100 4990807 EU CABIN DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1432A 11417 ORD - DURING OVERNIGHT MAINTENANCE, LEFT AFT OVERWING EMERGENCY EXIT LIGHT DAMAGED. REPLACED LEFT AFT OVERWING EMERGENC Y EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998112600589 19981126 00589 NM 1998 11 26 AALA981893 1 19981008 A 3350 1000677 LIGHT GRIMES BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 873AA 21385 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER AFT ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY OVER AFT ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600590 19981126 00590 NM 1998 11 26 AALA981892 1 19981008 A 3350 1000677 LIGHT BOEING 727 727223 1384074 NM PAX DOOR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 873AA 21385 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER FORWARD ENTRY DOOR INOPERATIVE. REPLACED EMERGENCY EXIT L IGHT ASSEMBLY OVER FORWARD ENTRY DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600592 19981126 00592 NM 1998 11 26 98ZZZM876 1 19981010 A 2421 20040 ALTERNATOR DORNER DO32 DO328100 2996000 NM ENGINE FAILED A EQGA O OTHER O OTHER CR CRUISE 1 SW 19 340LS 1079 3040 DEN - FLT 427 - APPROX HALFWAY EN ROUTE TO ASE FROM DEN, CREW RECEIVED A LT ALTERNATOR FAIL MESSAGE. CREW CONTACTED MX CONTROL AND ADVISED OF THE SITUATION. CREW REQUESTED TO CONTINUE TO ASE AND MX CONTROL CONCURRED. ON SHORT FINAL INTO ASE CREW NOTICED THAT THE LT ENGINE TORQUE HAD DROPPED TO ZERO. CREW MANUALLY FEATHERED PROPELLER AND LANDED IN ASE UNE VENTFULLY. MAINTENANCE INSPECTED THE AIRCRAFT AND DTERMINED THE LEFT ENGINE ALTERNATOR HAD FAILED AND IN DOING SO HAD C UT THE P3 AIR SUPPLY TUBE. MAINTENANCE REPLACED THE ALTERNATOR AND P3 AIR TUBE. MAINTENANCE ALSO INSPECTED ENGINE AREA TO VERIFY NO OTHER PROBLEMS EXISTED. MAINTENANCE PERFORMED NECESSARY OPERATIONAL CHECKS. ALL CHECKS WERE SATISFACTORY 2 H 7 2 4T RT A45NM 1998112600593 19981126 00593 NM 1998 11 26 ASAA9810105 1 19981004 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM BS 767 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING C-CHECK, THE AFT CARGO COMPARTMENT FLOORBEAM WAS FOUND TO BE CORRODED AT STATION 767, RBL 24-48. REPAIRED PER EA 5310-01610 AND BOEING TELEX ASA-SEA-98-0376RR. (M) 2 L 7 2 4F A16WE 1998112600594 19981126 00594 NM 1998 11 26 ASAA9810106 1 19981004 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM BS 1006 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING C-CHECK, THE CABIN FLOORBEAM WAS FOUND TO BE CORRODED AT STATION 1006, LBL 12. REPAIRED PER EA 5310-01612 AND BOEING TELEX ASA-SEA-98-0377RR. (M) 2 L 7 2 4F A16WE 1998112600595 19981126 00595 NM 1998 11 26 ASAA9810107 1 19981004 A 5315 FLOORBEAM BOEING 737 737290C 138448V NM BS 481 GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 740AS 22578 SEA - DURING C-CHECK, THE CABIN FLOOR TRACK WAS FOUND TO BE GOUGED AT STATION 481, LBL 43.5. REPAIRED PER EA 5310-01614 AND BOEING TELEX ASA-SEA-98-0378RR. (M) 2 L 7 2 4F A16WE 1998112600596 19981126 00596 NM 1998 11 26 ASAA9810112 1 19981021 A 5610 57176243 PIN BOEING 737 7372Q8C 138448S NM COCKPIT WINDOW CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 741AS 21959 ANC - FLT 147 - THE CAPTAINS SLIDING WINDOW WAS FOUND TO BE HARD TO CLOSE. INSPECTED AND FOUND THE GUIDE PIN CRACKED. R EPLACED THE CAPTAINS SLIDING WINDOW AND THE WINDOW OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998112600597 19981126 00597 WP 1998 11 26 USAAD98189 1 19981022 A 7830 NAS16124 O-RING DOUG DC9 DC981 3022081 WP CONTROL VALVE FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 806US 48038 CLT-TPA - FLT 1816 - DURING CRUISE THE LEFT HYDRAULIC QUANTITY LOW LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED TO SAV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED AN O-RING ON THE LEFT THRUST REVERSER CONTROL VALVE. (M) 2 L 7 2 4F A6WE 1998112600598 19981126 00598 WP 1998 11 26 USAAD98190 1 19981023 A 2120 UNKNOWN DOUG DC9 DC931 3022065 WP CABIN ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 922VJ 48142 GSO - FLT 990 - AFTER TAKEOFF, PASSENGERS NOTED A BURNING SMELL IN THE CABIN. FLIGHT RETURNED TO GSO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED FULL POWER RUN-UPS ON BOTH ENGINES AND COULD NOT DUPLICATE THE PROBLEM. THE A IRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F A6WE 1998112600599 19981126 00599 WP 1998 11 26 USAAD98192 1 19981029 A 3230 59516395001 CYLINDER DOUG DC9 DC931 3022065 WP NLG FAILED A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 934VJ 47769 48114 DCA-SYR - FLT 366 - DURING APPROACH WITH THE GEAR HANDLE DOWN THE GREEN NOSE GEAR LIGHT WOULD NOT ILLUMINATE. AFTER OPE RATING THE LANDING GEAR FREE FALL HANDLE THE NOSE GEAR EXTENDED. MAINTENANCE REPLACED THE NOSE GEAR BUNGEE CYLINDER AND LUBED THE NOSE GEAR. ACCOMPLISHED GEAR SWING AND GEAR FREE FALL, ALL CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1998112600600 19981126 00600 NM 1998 11 26 USAA980550 1 19981029 A 5320 SILL BOEING 737 7372B7 1384560 NM BS 300-306 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH AREA OF CORROSION BS 300-306 WL 208.10, RBBL 54 FORWA RD SERVICE DOOR INNER CHORD. CORROSION TASK NR C53-107-01. INSTALLED NEW 'Z' ANGLE PER SRM 51-10-1 AND SRM 51-30-2. ( M) 2 L 7 2 4F A16WE 1998112600601 19981126 00601 NM 1998 11 26 USAA980546 1 19981029 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 342 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .03125 INCH CRACK AT LOWER AFT CORNERS FORWARD ENTRY DOOR STATION 342 WL 208.1 SKIN FUSELAGE. CUT OUT CRACKED AREA FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER PER BOEING DRA WING 65C27257 AND EA 62845. (M) 2 L 7 2 4F A16WE 1998112600602 19981126 00602 NM 1998 11 26 USAA980545 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 7R TIE CLIP. INSTALLED NEW STRINGER T IE CLIP PER PCI 1093, EO 5393G227. (M) 2 L 7 2 4F A16WE 1998112600603 19981126 00603 NM 1998 11 26 USAA980544 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION FOUND A .25 INCH CRACK BS 727A STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PE R PCI 1093, EO 5393G227. (M) 2 L 7 2 4F A16WE 1998112600604 19981126 00604 NM 1998 11 26 USAA980543 1 19981029 A 5320 WEB BOEING 737 7372B7 1384560 NM BS 706-712 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-2 CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND A CRACK BL 0 BS 706, .6 INCH CRACK BS 708 .25 I NCH CRACK BS 709 .6 INCH CRACK BS 710 .2 INCH CRACK BS 712 .15 INCH CRACK ON WEB. INSTALLED DOUBELR PER EA 62724A. (M) 2 L 7 2 4F A16WE 1998112600605 19981126 00605 NM 1998 11 26 USAA980534 1 19981029 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 961 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-CHECK VISUAL INSPECTION, FOUND A .20 INCH CRACK LEFT AFT ENTRY DOORWAY FORWARD LOWER CORNER BS 961, 2 INC HES ABOVE STRINGER 17L OF SKIN. INSTALLED TRIPLER PER REPAIR DOCUMENT 53-30-3 FIG 24. (M) 2 L 7 2 4F A16WE 1998112600606 19981126 00606 NM 1998 11 26 USAA980524 1 19981029 A 5315 654681129 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 11 CORRODED AREAS BS 986.5 LBL 18 TO RBL 43 WL 208.1 OF FLOORBEAM. CORR OSION TASK NR C53-107-02. INSTALLED REPAIR T-CAP PER SRM 53-10-9 FIG 2. (M) 2 L 7 2 4F A16WE 1998112600607 19981126 00607 NM 1998 11 26 USAA980518 1 19981029 A 5313 6552928591 STRINGER BOEING 737 7372B7 1384560 NM BS 927 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 927 STRINGER 25L. REPAIRED AREA PER SRM 53-10- 1. (M) 2 L 7 2 4F A16WE 1998112600608 19981126 00608 NM 1998 11 26 USAA980516 1 19981029 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 807 STRINGER 9R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112600609 19981126 00609 NM 1998 11 26 USAA980515 1 19981029 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 2R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112600610 19981126 00610 NM 1998 11 26 USAA980513 1 19981029 A 5320 69374024 SILL BOEING 737 7372B7 1384560 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 294.5 WL 208.10 RBBL 53 FORWARD SERVICE ENTRY DOOR LOW ER SILL INBOARD CHORD DOUBLER ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M) 2 L 7 2 4F A16WE 1998112600611 19981126 00611 NM 1998 11 26 USAA980512 1 19981029 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE DENTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 1.5 INCH BY .062 INCH DENT 11 INCH AFT OF REAR ENTRY AND 18 INCH ABOVE LOWER DOOR SILL OF SKIN. INSTALLED DOUBLER PER SERM 53-30-3. (M) 2 L 7 2 4F A16WE 1998112600612 19981126 00612 NM 1998 11 26 USAA980510 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 597 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 597 STRINGER 9R. INSTALLED MODIFIED PART PAR EO 539 3G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998112600613 19981126 00613 NM 1998 11 26 USAA980508 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 5R TIE CLIP. INSTALLED MODIFIED PART P ER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998112600614 19981126 00614 NM 1998 11 26 P2EA98225 1 19981003 A 5210 65954791 FITTING BOEING 737 737244 138448U NM PAX DOOR WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FORWARD ENTRY DOOR AFT LOWER STOP FITTING WORN. FORWARD ENTRY DOOR LOWER AFT STOP FITTING REPLACED PER SRM 51-10- 1 PAGE 5, 51-30-2. (M) 2 L 7 2 4F A16WE 1998112600615 19981126 00615 NM 1998 11 26 PE2A98224 1 19981101 A 5230 10608211 SEAL BOEING 737 737247 138448D NM CARGO DOOR WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 MDW - FLT 815 - AIR RETURN, NO EMERGENCY DECLARED LANDING UNEVENTFUL. AIRCRAFT ON DEPARTURE FROM MDW WOULD NOT PRESSURI ZE IN AUTO, STANDBY, OR MANAUL. DEFERRED PER MEL 21-14-2, CI NR M912306. REF CI M912306. REPLACED LEAKING FLEX LINE A T 450 TEMP SENSOR PER MM 36-11-0 AND REPLACED BAD DOOR SEAL AT FORWARD CARGO DOOR PER MM 52-09-0. PRESSURIZED AIRCRAFT, LEAK CHECK AND OPS CHECK OK PER MM 21-00. (M) 2 L 7 2 4F A16WE 1998112600616 19981126 00616 NM 1998 11 26 P2EA98223 1 19981003 A 5330 SKIN BOEING 737 737244 138448U NM BS 178 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN MISSING MATERIAL AT BS 178, BETWEEN BL 0 TO RBL 6 INCH, WL 231. REPLACED FUSELAGE SKIN DOUBLER FROM BS 178 AND BS 188, FROM RBL 9 INCH TO LBL 9 INCH PER BOEING SERVICE BULLETIN 737-53-1059 REV 1 DATED MAY 17, 1990, SECT ION 3. (M) 2 L 7 2 4F A16WE 1998112600617 19981126 00617 NM 1998 11 26 P2EA98222 1 19981026 A 5210 FRAME BOEING 737 737244 138448U NM PAX DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FORWARD ENTRY DOOR LOWER AFT SECTION CRACKED, DEFECT SIZE LENGTH 1 INCH. REPAIRED FORWARD ENTRY DOOR LOWER AFT FR AME SECTION PER SRM 51-40-3 FIG 1 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998112600618 19981126 00618 NM 1998 11 26 P2EA98221 1 19981006 A 5315 FLOORBEAM BOEING 737 737244 138448U NM BS 947 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FLOORBEAM UPPER CHORD CORRODED AT BS 947, FROM RBL 45 INCHES TO RBL 53 INCHES. REPAIRED FLOORBEAM UPPER CHORD AT BS 947, FROM LBL 60 INCH TO RBL 60 INCH PER BOEING FAX COO-SJO-98-0764RR DATED OCT 12, 1998 AND COOPESA EO COO-3-53-569- 78 DATED OCT 15, 1998. DOCUMENTED ON FAA FORM 8110-3, (M) 2 L 7 2 4F A16WE 1998112600619 19981126 00619 NM 1998 11 26 P2EA98220 1 19981002 A 5320 BEAM BOEING 737 737244 138448U NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - VERTICAL BEAM CRACKED IN AFT CARGO COMPARTMENT AT BS 727, LBL 18 INCHES, WL 150. DEFECT SIZE LENGTH 1 INCH. REPA IRED FUSELAGE BULKHEAD VERTICAL BEAM SECTION AT BS 727, LBL 18, WL 150 PER SRM 51-40-4 FIG 2. (M) 2 L 7 2 4F A16WE 1998112600620 19981126 00620 NM 1998 11 26 P2EA98219 1 19981005 A 5712 RIB BOEING 737 737244 138448U NM WS 135 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING NR 3 FUEL TANK RIB CRACKED IN AFT SECTION BETWEEN REAR SPAR AND STRINGER 2, WBL 135.5 DEFECT SIZE, LENG TH 1 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5 BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SERVICE BULLET IN 737-57-1186 DATED APRIL 13, SECTION 3 PART 3, FIG 3. (M) 2 L 7 2 4F A16WE 1998112600621 19981126 00621 NM 1998 11 26 P2EA98218 1 19981005 A 5330 SKIN BOEING 737 737244 138448U NM BS 244-259 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN CORRODED AND DISBONDED FROM BS 244 TO BS 259, STRINGER 25LT, WL 154, LBL 19. REPAIRED FUSELAGE SKIN FROM BS 235.8 TO BS 259.5, BETWEEN STRINGER 24 LT AND STRINGER 26LT PER COOPESA EO COO-3-53-577-98 DATED OCT 19, 1998 A ND BOEING FAX COO-SJO-98-0782RR DATED OCT 19, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1998112600622 19981126 00622 NM 1998 11 26 P2EA98217 1 19981003 A 5330 SKIN BOEING 737 737244 138448U NM BS 203 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - HOLE FOUND IN FUSELAGE OUTER SKIN SECTION AT BS 203, RBL 7 INCH AND WL 153 INCH, DEFECT SIZE LENGTH .75 INCH WIDTH .437 INCH. REPAIRED FUSELAGE SKIN SECTION FROM BS 192.5 TO BS 203, BETWEEN BL 0 AND RBL 17 INCH, WL 153 PER SRM 53-30- 3 FIG 6. (M) 2 L 7 2 4F A16WE 1998112600623 19981126 00623 NM 1998 11 26 P2EA98216 1 19981002 A 5720 BEAM BOEING 737 737244 138448U NM WS 222 WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING TRUNNION SUPPORT BEAM WORN AT RSS 222. REPAIRED RIGHT WING MAIN LANDING GEAR BEAM UPPER FORWARD FLANGE SECTION PER BOEING FAX COO-SJO-98-0761RR DATED OCT 12, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1998112600624 19981126 00624 NM 1998 11 26 P2EA98215 1 19981002 A 5330 SKIN BOEING 737 737244 138448U NM BS 345-360 CANNED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN OIL CANNED FROM BS 345 TO BS 360, BETWEEN STRINGER 16 RT AND STRINGER 19 RT. REPAIRED FUSELAGE SKIN SECTION FROM BS 311 TO BS 360, BETWEEN STRINGER 15 RT AND STRINGER 19 RT PER COOPESA EO COO-3-53-570-98 DATED OCT 16, 1 998 AND BOEING FAX COO-SJO-98-0773RR DATED OCT 14, 1998. DOCUMENTED ON FAA FORM 8110-2. (M) 2 L 7 2 4F A16WE 1998112600625 19981126 00625 NM 1998 11 26 P2EA98214 1 19980930 A 5330 65C3674539 SKIN BOEING 737 737244 138448U NM BS 259-360 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN CORRODED FROM BS 259.5 TO BS 360, BETWEEN STRINGER 19 RT AND STRINGER 24 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 259.5 AND BS 360, BETWEEN STRINGER 19 RT AND STRINGER 24 RT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M ) 2 L 7 2 4F A16WE 1998112600626 19981126 00626 NM 1998 11 26 P2EA98213 1 19981003 A 5311 FRAME BOEING 737 737244 138448U NM BS 500 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FORWARD CARGO COMPARTMENT FRAME DENTED AT BS 500A, BETWEEN STRINGER 23 RT AND STRINGER 24 RT. REPAIRED FORWARD CA RGO COMPARTMENT FRAME, UPPER FLANGE AT BS 500A, BETWEEN STRINGER 23 RT AND STRINGER 24 RT PER SRM 51-40-3, FIG 1, PAGE 5 . (M) 2 L 7 2 4F A16WE 1998112600627 19981126 00627 NM 1998 11 26 P2EA98212 1 19981002 A 5230 SKIN BOEING 737 737244 138448U NM CARGO DOOR DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - C1 DOOR SKIN DENTED, SCRATCHES AND PROVISIONAL REPAIRS, DEFECT SIZE AVERAGE .200 INCH. REPLACED C1 DOOR SKIN PER SRM 52-30-2 FIG 3. (M) 2 L 7 2 4F A16WE 1998112600628 19981126 00628 NM 1998 11 26 P2EA98211 1 19981002 A 5720 STIFFENER BOEING 737 737244 138448U NM WS 155 WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING REAR STIFFENER WORN AT RSS 155. REPLACED RIGHT WING REAR SPAR STIFFENER AT RSS 155 PER SRM 51-10-1 PAG E 5, AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1998112600629 19981126 00629 NM 1998 11 26 NOCA2398 1 19981027 A 3350 767 LIGHT BOEING 757 75728A 1384976 NM R4 DOOR INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE AT DOOR R-4. FOUND INOPERATIVE DURING INSPECTION. RELAMPED EXTERIOR EMERGENC Y LIGHT AT DOOR R-4. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A2NM 1998112600630 19981126 00630 NM 1998 11 26 NOCA2498 1 19981027 A 3350 BP573 POWER SUPPLY BOEING 757 75728A 1384976 NM CABIN INOPERATIVE A NOCA K NONE L NO TEST IN INSP/MAINT 1 EA 15 750NA 26277 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK, TWO EACH IN AFT SECTION DEPLETED. REPLACED TWO EACH POWER SUPPLY BATTERY PAC KS. OPS CHECK OK. (M) 2 L 7 2 4F RT A2NM 1998112600631 19981126 00631 NM 1998 11 26 98ZZZM877 1 19981026 A 3350 38931002 CONNECTOR GRIMES BOEING 727 727225 1384077 NM ROW 18-23 CONTAMINATED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 806MA 22437 DURING PREFLIGHT, FOUND EMERGENCY EXIT FLOOR LIGHTS FROM 18 TO 23 INOP. CLEANED CANNON PLUG AND RECONNECTED BATTERY PAC K, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998112600632 19981126 00632 NM 1998 11 26 98ZZZM878 1 19981027 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM FUSELAGE DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 889MA 70220 21854 DURING PREFLIGHT, FOUND EXTERIOR EMERGENCY LIGHT, MOST AFT ON LEFT FAIRING INOPERATIVE. REPLACED BATTERY PACK IAW MM 33 -50-22. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1998112600633 19981126 00633 NM 1998 11 26 98ZZZM879 1 19981026 A 3350 58L214 BATTERY PACK BOEING 727 727225 1384077 NM ROW 21/17 DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 886MA 21855 DURING PREFLIGHT, FOUND BOTTOM EMERGENCY EXIT SIGN FOR DOOR, ROWS 21 AND 17 ON LEFT SIDE INOP. REPLACED BATTERY PACK, O PS CHECK OK PER MM 33-59-00. (M) 2 L 7 3 4F A3WE 1998112600634 19981126 00634 NM 1998 11 26 98ZZZM880 1 19981026 A 3350 900814 BATTERY BOEING 727 727225 1384077 NM EMERGENCY EXIT DISCHARGED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 806MA 22437 DURING PREFLIGHT, FOUND RIGHT FORWARD EMERGENCY EXIT OVERWING LIGHT IS FLICKERING. REMOVED AND REPLACED BATTERY PACK, O PS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998112600635 19981126 00635 NM 1998 11 26 98ZZZM881 1 19981026 A 3350 CONNECTOR BOEING 727 727225 1384077 NM ROW 19/21 CONTAMINATED A MYWA K NONE L NO TEST IN INSP/MAINT 1 SO 19 806MA 22437 DURING PREFLIGHT, FOUND EMERGENCY EXIT SIGNS (BOTTOM) FOR ROWS 19 AND 21 ON LEFT SIDE INOP. CLEANED CANNON PLUG AND REC ONNECTED BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 3 4F A3WE 1998112600636 19981126 00636 NM 1998 11 26 BJNA981003 1 19981024 A 5512 PANEL BOEING 737 737214 138446R NM HORIZONTAL STAB DELAMINATED A BJNA K NONE O OTHER IN INSP/MAINT 1 WP 11 457TM 20156 UPON (PHASE 9) INSPECTION DISCOVERED RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL DELAMINATING. REPAIRED HORIZ ONTAL 1E PANEL WORK ORDER 02-0001, AND 02-0002, JOB NR 10-1166, WORK PERFORMED BY EVERGREEN AIR CENTER. (M) 2 L 7 2 4F A16WE 1998112600637 19981126 00637 EA 1998 11 26 98ZZZM882 1 19981024 A 2750 C6CW10831 ROD ASSY DHAV DHC6 DHC6300 2802606 EA WING ROOT WORN A P ASWA K NONE O OTHER IN INSP/MAINT 1 WP 07 142SA 241 241 DURING AIRCRAFT SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND LEFT AND RIGHT WING ROOT TO INBOARD BELLCRANK FLAP ROD ASSEMBLIES HEAVILY GROOVED AND SCORED BY ROD GUIDE ROLLERS. THIS IS AN ONGOING CHRONIC PROBLEM ON THIS AIRCRAFT TYPE. GUIDE ROLLERS ARE MADE FROM A HARD MATERIAL THAT DAMAGES THE SOFTER RODS. THESE RODS ARE THE SUBJECT OF AD 80-03-08. M OD 6/1707 HAD PREVIOUSLY BEEN ACCOMPLISHED. (M) 1 H 7 2 3T RT A9EA 1998112600638 19981126 00638 CE 1998 11 26 98ZZZM883 1 19981009 A 2610 70522 HARNESS BEECH 1900 1900D 1154162 CE LT NACELLE LOOSE A AMWA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 CE 07 176YV UE176 FLT 5600 - RTF WHEN THE LT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. THE LEFT ENGINEWAS SHUT DOWN. EMERGENCY EQUIPMEN T WAS CALLED. AIRCRAFT LANDED WITHOUT INCIDENT. ICT MAINTENANCE THEN RETURNED THE AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998112600639 19981126 00639 NM 1998 11 26 BJNA981002 1 19981023 A 3320 1012623 LIGHT BOEING 737 737214 138446R NM SEAT 10C INOPERATIVE A BJNA K NONE L NO TEST IN INSP/MAINT 1 WP 11 457TM 20156 EMERGENCY LIGHT ON PASSENGER SEAT 10C IS BROKEN. REMOVED AND REPLACED EXIT SIGN LIGHT ASSY PER BMM 33-51-11. (M) 2 L 7 2 4F A16WE 1998112600640 19981126 00640 1998 11 26 98ZZZM884 4 19981008 A 3425 6229681001 EHSI BEECH 1900 1900D 1154162 CE INST PANEL FAILED A AMWA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 140ZV UE140 FLT 5633 - SGF-MCI - EN ROUTE, THE CREW REPORTED SMOKE IN THE COCKPIT AFTER THE CAPTAINS EHSI FAILED. EMERGENCY WAS DEC LARED. THE AIRCRAFT LANDED IN MCI WITHOUT INCIDENT. MCI MAINTENANCE REPLACED THE EHSI AND INSPECTED AIRCRAFT FOR DAMAG E. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER INCIDENT REPORTED. (M) 2 L 7 2 4T RT A24CE 1998112600641 19981126 00641 CE 1998 11 26 98ZZZM885 1 19981010 A 2610 MS21353341 SWITCH BEECH 1900 1900D 1154162 CE LT NACELLE MALFUNCTIONED A AMWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 176YV 1110 UE176 FLT 5665 - ICT-MCI - EN ROUTE, T-HANDLE AND FIRE LOOP ILLUMINATE INTERMITTENTLY. ICT MAINTENANCE FOUND AND REPAIRED CHA FFED WIRES UNDER THE LEFT FORWARD FLOORBOARD AND REPLACED THE LEFT FIRE LOOP TEST SWITCH. THE AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER INCIDENT AT THIS TIME. (M) 2 L 7 2 4T RT A24CE 1998112600642 19981126 00642 WP 1998 11 26 ORJA98262 1 19980922 A 3210 GUARD DOUG DC9 DC982 3022082 WP NLG CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 AT OKC, LEVEL 2 CORROSION, ON NLG TIRE SPLASH GUARD ASSY AND ATTACHING HARDWARE WERE CORRODED. REMOVED AND REPLACED HAR DWARE IAW DOUGLAS MD-80, MM CHAPTER 32, SECTION 32-20-01. REMOVED SURFACE CORROSION IW DC-9 SRM 51-10 3/.017 MAX MATERI AL LOSS WITHIN LIMITS IAW DC-9, SRM 53-01, FIG 1. TREATED AND PRIMED IAW DC-9 SRM 53-10-03. (M) 2 L 7 2 4F A6WE 1998112600643 19981126 00643 WP 1998 11 26 ORJA98263 1 19980922 A 5320 NUT PLATE DOUG DC9 DC982 3022082 WP FUSELAGE CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 AT OKC, LEVEL 2 CORROSION, CORRODED NUT PLATE ON FWD AREA OF FWD CARGO DOOR CUT OUT. REMOVED AND REPLACED NUT PLATE. R EPAIRED IAW DC9/MD80 SRM 51-30-2, 51-70-0 ARM 53-00. (M) 2 L 7 2 4F A6WE 1998112600644 19981126 00644 WP 1998 11 26 ORJA98264 1 19980823 A 5320 NUT DOUG DC9 DC982 3022082 WP BS 1212 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 AT OKC LEVEL 2 CORROSION, NUT RUSTY AT AFT INBOARD CORNER OF FRAME 1212 TO STRINGER 29R. REMOVED AND REPLACED RUSTY FAS TENTERS IAW DC9 SRM 51-30-1. (M) 2 L 7 2 4F A6WE 1998112600645 19981126 00645 WP 1998 11 26 ORJA98265 1 19980923 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 AT OKC LEVEL 2 CORROSION, ATTACH ANGLE CORRODED ON FORWARD SIDE OF FRAME 1174 INBOARD CORNER OF STRINGER 29R IN AFT PIT. REMOVED CORRODED ATTACH ANGLE, BLENDED CORROSION OUT OF LIMITS IAW MC-80, SRM 53-01. FABRICATED NEW ANGLE IAW MC80, S RM 51-10-2, TREATED AND PRIMED IAW MC80, SRM 51-10-3. INSTALLED ANGLE IAW MD80, SRM 51-30-5. (M) 2 L 7 2 4F A6WE 1998112600646 19981126 00646 NM 1998 11 26 USAA980466 1 19980930 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 887-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY 6 INCH AREA OF CORROSION LBL 54 STATION 887 TO STATION 1016. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART PER SRM 53-10-01. (M) 2 L 7 2 4F A16WE 1998112600647 19981126 00647 NM 1998 11 26 USAA980464 1 19980930 A 5315 6546568 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY .5 INCH BY 24 INCH AREA OF CORROSION CLIP NUT HOLES BS 1016 BETWEEN LBL 12 AND LBL 36 FLOORBEAM UPPER CHORD. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER SRM 53-10-9. (M ) 2 L 7 2 4F A16WE 1998112600648 19981126 00648 NM 1998 11 26 USAA980463 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 767 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112600649 19981126 00649 NM 1998 11 26 USAA980462 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727A STRINGER 6R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112600650 19981126 00650 NM 1998 11 26 USAA980461 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 747 STRINGER 7R STRINGER TIE CLIP. REPAIRED PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112600651 19981126 00651 NM 1998 11 26 USAA980460 1 19980930 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 663 BBL .07 UPPER CHORD LONGITUDINAL FLOORBEAM. INSTA LLED SPLICE ANGLES, STRAPS AND REINFORCED ANGLES PER EA 62511 AND BOEING S/B737-57-1210. (M) 2 L 7 2 4F A16WE 1998112600652 19981126 00652 NM 1998 11 26 USAA980459 1 19980930 A 5320 654581951 WEB BOEING 737 7372B7 1384560 NM BS 230 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2.5 INCH CRACK BS 230.5 WL 187 BL 0 RETRACT ACT FITTING SUPPORT WEB NL G. INSTALLED DOUBLER PER SRM 51-40-2 FIG 1, BOEING 737-200. (M) 2 L 7 2 4F A16WE 1998112600653 19981126 00653 NM 1998 11 26 USAA980458 1 19980930 A 5315 FLOORBEAM BOEING 737 7372B7 1384560 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND SEVERAL SCREW HOLES ON FLOORBEAM STATION 947.5. CORROS ION TASK NR C53-107-02. INSTALLED NEW T-CAP TO FLOORBEAM PER SRM 53-10-9. (M) 2 L 7 2 4F A16WE 1998112600654 19981126 00654 NM 1998 11 26 USAA980457 1 19980930 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 269AU 43227 22881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 4L STRINGER TIE CLIP. REPAIRED PE R EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998112600655 19981126 00655 CE 1998 11 26 98ZZZM886 1 19981024 A 2750 1015210161 ACTUATOR BEECH 1900 1900D 1154162 CE TE FLAP FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 858CA 10675 592D92 UE72 FLAPS STUCK AT 17 DEGREES. SECURED FLAPS TO UP POSITION. INSPECTION OF COMPONENTS FOUND LT INBD ACTUATOR FAILURE. REM OVED AND REPLACED LT INBD FLAP ACTUATOR IAW RAYTHEON MAINTENANCE MANUAL CHAPTER 27. (M) 2 L 7 2 4T RT A24CE 1998112600656 19981126 00656 CE 1998 11 26 98ZZZM887 1 19981024 A 2161 HYLZ51071 TEMP CONTROLLER BEECH 1900 1900D 1154162 CE CABIN FAILED A JJBA B EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 01 852CA 62163 752 UE55 DURING DESCENT AT APPROXIMATELY 14,000 FT, A SUDDEN AND STRONG BURNING SMELL WITH A HAZE OF SMOKE FILLED COCKPIT. INSPE CTION OF AIRCRAFT FOUND CIRCUIT CARD FAILURE IN CABIN TEMPERATURE CONTROLLER IN CABIN CEILING. UNIT WAS REPLACED AND SY STEM CHECKED SATISFACTORY IAW CHAPTER 21. (M) 2 L 7 2 4T RT A24CE 1998112600657 19981126 00657 NM 1998 11 26 USAASB98258 1 19981001 A 2120 65544741 SUPPLY DUCT BOEING 737 7372B7 1384560 NM AC BAY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 269AU 22881 LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS H EARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RET URNED TO FIELD AT LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A BLOWN RIGHT HOT AIR SUPPLY DUCT A ND BLOWN MIX CHAMBER DUCT. ALSO, REPLACED RIGHT PACK PRESSURE REGULATOR AND PACK CONTROL VALVE. ACCOMPLISHED ENGINE BL EED AIR COMPRESSION CONTROL SYSTEM TEST PER MM 21-11-0. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998112600658 19981126 00658 NM 1998 11 26 98ZZZM888 1 19981001 A 2120 65789473 MIX CHAMBER DUCT BOEING 737 7372B7 1384560 NM AC BAY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 269AU 22881 LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS H EARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RET URNED TO FIELD AT LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A BLOWN RIGHT HOT AIR SUPPLY DUCT A ND BLOWN MIX CHAMBER DUCT. ALSO, REPLACED RIGHT PACK PRESSURE REGULATOR AND PACK CONTROL VALVE. ACCOMPLISHED ENGINE BL EED AIR COMPRESSION CONTROL SYSTEM TEST PER MM 21-11-0. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998112600659 19981126 00659 NM 1998 11 26 98ZZZM889 1 19981001 A 2120 39268631 PRESS REGULATOR BOEING 737 7372B7 1384560 NM AC BAY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 269AU 22881 LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS H EARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RET URNED TO FIELD AT LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A BLOWN RIGHT HOT AIR SUPPLY DUCT A ND BLOWN MIX CHAMBER DUCT. ALSO, REPLACED RIGHT PACK PRESSURE REGULATOR AND PACK CONTROL VALVE. ACCOMPLISHED ENGINE BL EED AIR COMPRESSION CONTROL SYSTEM TEST PER MM 21-11-0. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998112600660 19981126 00660 NM 1998 11 26 98ZZZM890 1 19981001 A 2120 39606411 PACK CONTROL VLV BOEING 737 7372B7 1384560 NM AC BAY FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 269AU 22881 LGA - FLT 1599 - FOR TAKEOFF, FLIGHT WAS CONFIGURED FOR A BLEEDS OFF TAKEOFF. WHEN CREW RECONFIGURED, A LOUD BANG WAS H EARD. AFTER A MINUTE OR TWO, THE FLIGHT ATTENDANTS REPORTED SMOKE IN THE CABIN. AN EMERGENCY WAS DECLARED. FLIGHT RET URNED TO FIELD AT LGA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED A BLOWN RIGHT HOT AIR SUPPLY DUCT A ND BLOWN MIX CHAMBER DUCT. ALSO, REPLACED RIGHT PACK PRESSURE REGULATOR AND PACK CONTROL VALVE. ACCOMPLISHED ENGINE BL EED AIR COMPRESSION CONTROL SYSTEM TEST PER MM 21-11-0. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998112600661 19981126 00661 CE 1998 11 26 98ZZZM891 1 19981010 A 2610 1143200523 SWITCH BEECH 1900 1900D 1154162 CE LT NACELLE MALFUNCTIONED A AMWA D RETURN TO BLOCK J WARNING INDICATION CL CLIMB 1 CE 07 176YV 2113 1110 UE176 FLT 5633 - RETURNED TO THE FIELD IN MCI WHEN THE LEFT FIRE LOOP LIGHT CAME ON IN FLIGHT. MCI MAINTENANCE COULD NOT DUPL ICATE THE DISCREPANCY, BUT DID CHANGE THE T-HANDLE AND RETURNED THE AIRCRAFT TO SERVICE AFTER A TEST FLIGHT THAT PRODUCE D NO DISCREPANCY. (M) 2 L 7 2 4T RT A24CE 1998112600662 19981126 00662 CE 1998 11 26 98ZZZM892 1 19980403 A 5753 351650505259 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 242YV 3734 244R UE242 OVERNIGHT MAINTENANCE ICT, FOUND .5 INCH CRACK IN THE RT OUTBOARD FLAP TE 7 INCH FROM INBOARD END. REPAIRED FLAP IAW AM WA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600663 19981126 00663 CE 1998 11 26 98ZZZM893 1 19980330 A 5753 10116000144 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 139ZV 445 SC3429 UE139 DURING ACCEPTANCE INSPECTION ICT MAINTENANCE, FOUND THE OUTBOARD ATTACH POINT INBOARD ACCESS HOLE ON THE RT INBOARD FLAP HAD SMALL CRACK FROM IT. REPAIRED CRACK IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600664 19981126 00664 CE 1998 11 26 98ZZZM894 1 19980401 A 5753 10116000144 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 231YV 4242 695 UE231 OVERNIGHT MAINTENANCE IN ICT, FOUND A .5 INCH CRACK EXTENDING FROM A RIVET ON THE RT INBOARD FLAP DOVETAIL. REPAIRED IA W AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600665 19981126 00665 CE 1998 11 26 98ZZZM895 1 19980523 A 5753 10116000143 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 237YV 6546 405 UE237 ICT OVERNIGHT MAINTENANCE, FOUND LEFT INBOARD FLAP TOP SKIN CRACKED AT INBOARD ATTACH BRACKET. REPAIRED IAW AMWA TO 190 0-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600666 19981126 00666 CE 1998 11 26 98ZZZM896 1 19980328 A 5753 35165050259 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 176YV 1549 925 UE176 OVERNIGHT MAINTENANCE IN ICT FOUND A 1 INCH CRACK IN TOP SKIN .5 INCH FROM INBOARD AND 9.5 INCH FROM TE ON RHOB FLAP. R EPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600667 19981126 00667 CE 1998 11 26 98ZZZM897 1 19980409 A 5753 10116000143 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 233YV 4157 729 UE233 ICT OVERNIGHT MAINTENANCE FOUND A .5 INCH CRACK IN LEFT INBOARD FLAP BOTTOM SKIN 36 INCHES FROM INBOARD END AND 2 INCH A FT OF LE. REPAIRED IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600668 19981126 00668 CE 1998 11 26 98ZZZM898 1 19980406 A 5753 35165050259 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 163YV 6413 171 UE163 OVERNIGHT MAINTENANCE IN ICT, FOUND A SMALL CRACK ON THE RT OUTBOARD FLAP LOWER SKIN TE 10 INCH FROM INBOARD END. REPAI RED IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600669 19981126 00669 CE 1998 11 26 98ZZZM899 1 19980403 A 5753 35165050258 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 242YV 3079 754 UE242 OVERNIGHT MAINTENANCE IN ICT, FOUND TWO .5 INCH CRACKS IN BOTTOM SKIN EXTENDING FROM TWO ADJACENT RIVETS ON THE CENTER S PAR ON THE LEFT OUTBOARD FLAP. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600670 19981126 00670 CE 1998 11 26 98ZZZM900 1 19980328 A 5753 35165050258 SKIN BEECH 1900 1900D 1154162 CE TE FLAP CRACKED A AMWA K NONE O OTHER IN INSP/MAINT 1 CE 07 171ZV 5681 171 UE171 OVERNIGHT MAINTENANCE, FOUND .5 INCH CRACK IN LHOB FLAP 29.5 INCH FROM OUTBOARD EDGE AND 15 INCH FROM TRAILING EDGE ON B OTTOM SKIN. REPAIRED FLAP IAW AMWA TO 1900-27-00-0001. (M) 2 L 7 2 4T RT A24CE 1998112600671 19981126 00671 CE 1998 11 26 98ZZZM901 1 19981007 A 2610 70522 FIRE LOOP BEECH 1900 1900D 1154162 CE LT NACELLE LOOSE A AMWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 176YV UE176 FLIGHT 5609 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED. INTERMITTENTLY IN FLIGHT. MAINTENANCE FOUND LO OSE WIRE AT LOOP CONNECTOR. WIRE WAS RESOLDERED, PERFORMED GROUND RUN OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 1998112600672 19981126 00672 CE 1998 11 26 98ZZZM902 1 19981008 A 2610 24409015 FIRE LOOP BEECH 1900 1900D 1154162 CE LT NACELLE MALFUNCTIONED A AMWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 176YV UE176 FLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORW ARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 1998112600673 19981126 00673 CE 1998 11 26 98ZZZM903 1 19981008 A 2610 24412886 FIRE LOOP BEECH 1900 1900D 1154162 CE LT NACELLE MALFUNCTIONED A AMWA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 07 176YV UE176 FLT 5601 - REPORTED LT FIRE T-HANDLE AND FIRE LOOP WERE ILLUMINATED INTERMITTENTLY IN FLIGHT. MAINTENANCE REPLACED FORW ARD AND AFT FIRE LOOP DETECTORS, PERFORMED GROUND RUN OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 1998112600674 19981126 00674 CE 1998 11 26 98ZZZM904 1 19981010 A 3230 11438800013 POWER PACK VICKERS BEECH 1900 1900C 1154161 CE MLG INOPERATIVE A YADA O OTHER O OTHER NR NOT REPORTED 1 AL 01 31240 MX459368 UC28 PILOT REPORTE THE LANDING GEAR SYATED DOWN WHEN SELECTED UP AND THE LANDING GEAR RELAY CIRCUIT BREAKER POPPED. THE LAND ING GEAR CONTINUED TO SHOW THREE GREEN DOWN AND LOCKED LIGHTS. A NORMAL LANDING WAS PERFORMED. MAINTENANCE DETERMINED THE HYDRAULIC POWER PACK HAD FAILED AND REPLACED THE UNIT. ALL POST REPLACEMENT CHECKS WERE NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 2 4T RT A24CE 1998112600675 19981126 00675 NM 1998 11 26 AALA981828 1 19980927 A 3260 69553584 LINKAGE BOEING 727 727223 1384074 NM LT MLG MALFUNCTIONED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 712AA 22468 ORD - FLT 1171 - AFTER TAKEOFF TPA EN ROUTE ORD HAD TO USE THE LANDING GEAR LOCK OVERRIDE TO RAISE LANDING GEAR. LANDED ORD WITHOUT INCIDENT. REPLACED AIR/GROUND MECHANICAL LINKAGE IN LEFT GEAR WHEEL WELL. OPERATIONS NORMAL ON AIRCRAFT G EAR RETRACTION AND EXTENSION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600676 19981126 00676 NM 1998 11 26 AALA981724 1 19980926 A 2750 240863 MOTOR VICKERS BOEING 727 727223 1384074 NM TE FLAP MALFUNCTIONED A AALA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 849AA MX256864D 20990 ORD - FLT 1214 - EN ROUTE ORD-YYZ - LOST SYSTEM 'A' HYDRAULIC IN FLIGHT. RETURNED ORD, MANUALLY EXTENDED LANDING GEAR, ELECTRICALLY EXTENDED FLAPS AND LANDED WITHOUT INCIDENT. REPLACED OUTBOARD FLAP DRIVE MOTOR PER MM. REFILLED HYDRAULIC SYSTEMS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600677 19981126 00677 WP 1998 11 26 AALA981913 1 19981008 A 2150 18406032 HEAT EXCHANGERS GARRTT DOUG DC9 DC982 3022082 WP ACM BAY FAILED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 271AA 1094164 49293 DFW - FLT 1004 - DURING CLIMB-OUT DFW, SMOKE AND ACIDIC FUMES REPORTED IN CABIN. FIRST REPORTED IN MID CABIN. FUMES CA USED MILD BURNING SENSATION TO PASSENGERS EYES. AIR INTERRUPTED, RETURNED, AND LANDED DFW WITHOUT INCIDENT. REPLACED L EFT AND RIGHT ACMS HEAT EXCHANGERS AND PERFORMED PACK BURN, FUMES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998112600678 19981126 00678 EU 1998 11 26 AALA981916 1 19981014 A 2530 880301000 OVEN FOKKER F28 F28MK0100 4990807 EU GALLEY OVERHEATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 1459A 11479 YYZ- FLT 1012 - EN ROUTE YYZ-LGA, CLIMBING THROUGH 8,000 FT, BLUE THIN SMOKE ENTERED THE COCKPIT AND REMAINED FOR A FEW MINUTES WHILE SLOWLY DISSIPATING. ALL ELECTRICAL LOADS NORMAL. CREW SUSPECTED FIRST CLASS OVEN MAY BE SOURCE OF SMOKE. RETURNED YYZ AND LANDED WITHOUT INCIDENT. TROUBLESHOT AND DETERMINED THAT LEFT FIRST CLASS GALLEY OVEN SOURCE OF SMOK E DUE TO OVERHEATING BREAKFAST. RAN PACKS. GROUND CHECKED NORMAL OPERATION. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT 1998112600679 19981126 00679 WP 1998 11 26 TWAA9818801 1 19981122 A 2910 LINE DOUG DC9 DC983 3022083 WP RT HYD SYST LOOSE A TWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CE 05 9624T 53594 RT HYDRAULIC SYSTEM FAILED. LOST ALL FLUID. NEC TO MANUALLY EXTEND THE LANDING GEAR. FOUND LOOSE HYD LINE IN RT WHEEL WELL. TIGHTENED LINE. ALSO, REPLACED THE RT ENG HYD PUMP AND CASE DRAIN FILTER PRECAUTIONARY. 2 L 7 2 4F RT A6WE 1998112600680 19981126 00680 NM 1998 11 26 TWAA9818803 1 19981122 A 3350 POWER SUPPLY BOEING 727 727231 1384079 NM EMER EXIT INOP A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 54354 21986 EMERGENCY EXIT ROW LIGHTS FLICKERED ON AND OFF WHILE IN FLIGHT. RECHARGED EGRESS POWER SUPPLIES. CHECK-C 5-21-98 MCI. 2 L 7 3 4F A3WE 1998112600681 19981126 00681 NM 1998 11 26 TWAA9818804 1 19981122 A 3350 58225 BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE O OTHER CR CRUISE 1 CE 05 54354 21986 DURING CRUISE, THE ESCAPE PATH LIGHTS IN THE CENTER OF THE CABIN FLICKER ON-OFF. REPLACED BOTH BATTERY PACKS ABOVE THE EMERGENCY ESCAPE DOORS. 2 L 7 3 4F A3WE 1998112600683 19981126 00683 NM 1998 11 26 TWAA9818806 1 19981123 A 3350 1317 LAMP BOEING 767 7673Y0 NM ROW 25 & 41 FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 632TW 24953 FOUND OVERHEAD EMERGENCY LIGHTS INOPERATIVE OVER CABIN ROWS 25 RT SIDE AND 41 LT SIDE. RELAMPED, CHECK-C 8-26-98 LAX. 2 L 7 2 4F RT A1NM 1998112600684 19981126 00684 NM 1998 11 26 TWAA9818807 1 19981123 A 3350 S417N5092 COVER BOEING 767 7673Y0 NM ROW 4 & 5 MISSING A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 632TW 24953 FOUND FLOOR EGRESS LIGHT COVERS MISSING AT ROWS 4 AND 5 ON RT SIDE, AND ROW 5 ON LT SIDE. REPLACED COVERS. CHECK-C 8-2 6-98 LAX. 2 L 7 2 4F RT A1NM 1998112600685 19981126 00685 NM 1998 11 26 TWAA9818808 1 19981124 A 5754 SKIN BOEING 767 767205 1385121 NM NR 6 LE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 650TW 23057 FOUND 12 INCH BY 12 DELAMINATION ON UPPER SURFACE OF NR 6 L/E DEVICE, AT O/B END. INSTALLED METAL TO METAL HOT BOND REP AIR PER 767 SRM 51-70-10. CHECK-C 10-28-98 LAX. 2 L 7 2 4F RT A1NM 1998112600686 19981126 00686 NM 1998 11 26 HNAA9892483 1 19981123 A 3350 POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 924HA 105 CHO - FLT 3251 - FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED 3352-PS1 AND 3352-PS2 BATTERY POWER SUPPLIES AND BASE ASS EMBLIES. POWER SUPPLIES P/N OFF 61-0479-1X S/N SBY106 AND ORF61. POWER SUPPLY BASE P/N OFF NSN7 AND PS207. (M) 2 H 7 2 4T RT A13NM 1998112600687 19981126 00687 NM 1998 11 26 HNAA9898782 1 19981120 A 3244 31442 TIRE DHAV DHC8 DHC8201 2809001 NM NLG FAILED A HNAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 07 987HA 0045 425 MCO - FLT 3090 - LEFT NOSE TIRE DISINTEGRATED ON TAKEOFF AND DAMAGED LEFT NOSE GEAR DOOR, NOSE GEAR WIRE HARNESS AND DEN TED FUSELAGE AFT OF GEAR WELL. REPLACES BOTH NOSE WHEEL ASSEMBLIES AND REPAIRED AFFECTED ITEMS. (M) 2 H 7 2 4T RT A13NM 1998112600688 19981126 00688 WP 1998 11 26 VJ9800623 1 19981026 A 5280 65C335341 ANGLE DOUG DC9 DC932 3022066 WP NLG CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 RT NLG DOOR SEAL STRIKER ANGLE CORRODED FROM FWD TO AFT END. REPLACED ANGLE IAW DC9 SRM 51-10-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998112600689 19981126 00689 WP 1998 11 26 VJ9800624 1 19981030 A 2530 ANGLE DOUG DC9 DC932 3022066 WP NR 2 GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 NR 2 GALLEY ICE DRAWER CORRODED ON BEAM. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW DC9 SRM 51-30-1, 51-10-3, 51-1 0-2. 2 L 7 2 4F A6WE 1998112600690 19981126 00690 WP 1998 11 26 VJ9800625 1 19981031 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 509.5-531.7 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 RT WING LOWER SURFACE O/B TRAILING EDGE WING SKIN CORRODED AT XRS 509.5 - XRZ 531.7. REMOVED, FABRICATED AND INSTALLED NEW SKIN IAW DC9 SRM 51-20-0, 51-30-2, 57-31-3, 51-10-4, AND 51-30-9. 2 L 7 2 4F A6WE 1998112600691 19981126 00691 WP 1998 11 26 VJ9800626 1 19981102 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 160 - 219 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 FLOOR SUPPORT (60-2576) AT FS 200, T-CAP UPPER SURFACE AND FASTENER HOLES AT FS 160 TO 219 CORRODED. REMOVED, FABRICATE D AND INSTALLED NEW FLOOR SUPPORT IAW DC9 SRM 51-10-3, 51-30-2, 51-10-4, 51-10-3 53-01, FIG 1. 2 L 7 2 4F A6WE 1998112600692 19981126 00692 WP 1998 11 26 VJ9800627 1 19981102 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 160 - 200 CRACKED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 Z-ANGLE AT FS 160 TO 200 LT FOUND CRACKED AND MATERIAL MISSING. REMOVED, FABRICATED AND INSTALLED NEW Z-ANGLE IAW DC9 S RM 51-30-2, 51-30-8, 51-20-0, 51-10-4, 51-10-1. 2 L 7 2 4F A6WE 1998112600693 19981126 00693 WP 1998 11 26 VJ9800628 1 19981119 A 5730 CN19684 PANEL DOUG DC9 DC932 3022066 WP LT WING LEAKING A ZZDA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SO 15 949VV 47484 LT WING FUEL ACCESS PANEL LEAKING. FLIGHT CREW ELECTED TO RETURN TO ATL MAINTENANCE BASE. INSPECTED AIRCRAFT AND FOUND NO RESIDUAL FLUID BUT INSTALLED DOME NUT ON FUEL INSPECTION PLATE IAW MM 28-00. LEAK CHECKED GOOD. 2 L 7 2 4F A6WE 1998112600694 19981126 00694 WP 1998 11 26 VJ9800629 1 19981122 A 2612 W322824N FIRE LOOP DOUG DC9 DC932 3022066 WP NR 1 ENGINE MALFUNCTIONED A ZZDA E ENGINE SHUTDOWN N FALSE WARNING AP APPROACH 1 SO 15 933VV 47489 FIRE DETECTION LOOP LIGHT ILLUMINATED WITH FIRE HANDLE LIGHT FLICKERING ON NR 1 ENGINE. PERFORMED LOOP TEST PER AOM AND FLIGHT CREW ELECTED TO SECURE NR 1 ENGINE. DECLARED EMERGENCY LANDING BUT LANDING WAS NORMAL AND NO EVACUATION WAS PER FORMED. REPLACED FIRE BOTTLE AND SQUIBB, SPLICED WIRES ON LT PYLON LOOP PER MM 20-50, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998112600695 19981126 00695 EU 1998 11 26 MALA976246 1 19981121 A 3350 CIRCUIT BREAKER BAC 146 AVRO146RJ85A 1500097 EU COCKPIT TRIPPED A MALA O OTHER L NO TEST IN INSP/MAINT 1 GL 15 513XJ E2329 DURING INSPECTION, EMERGENCY LIGHTS INOP. MAINTENANCE FOUND CB CABIN EMERGENCY NR 2 AT F35 GRID LOCATION FLIGHT DECK PO PPED. RESET, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998112600696 19981126 00696 EU 1998 11 26 MALA976247 1 19981119 A 7603 CIRCUIT BREAKER SAAB SF340 SF340A 7850100 EU COCKPIT TRIPPED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 114XJ 340A114 DURING FLIGHT, THE FLIGHT IDLE STOP OPEN LIGHT ILLUMINATED AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO DTW. MAINTENANC E PULLED AND RESET CB. PERFORMED OPS CHECKS PER SAAB MM 76. TEST FLIGHT SATISFACTORY. 2 L 7 2 4T RT A52EU 1998112600697 19981126 00697 EU 1998 11 26 MALA976248 1 19981121 A 3020 SENSORS SAAB SF340 SF340A 7850100 EU LT INTAKE MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 79XJ 079 LEFT INTAKE INOP CAME ON DURING FLIGHT, SHUT SYSTEM OFF, RESELECTED ON AND LIGHT CAME BACK ON AFTER BETWEEN 15-80 SECOND S. SHUT SYSTEM OFF FOR SEVERAL MINUTES AND TRIED AGAIN, SAME THING HAPPENED. AIRCRAFT RETURNED TO DTW. MAINTENANCE SW APPED NORMAL AND OVERTEMP SENSORS TO SPARE SENSORS. GROUND RAN AIRCRAFT, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998112600698 19981126 00698 EU 1998 11 26 MALA976249 1 19981119 A 3610 HC361H0377006 DUCT BAC 146 AVRO146RJ85A 1500097 EU NR 4 ENGINE FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 501XJ E2208 NR 4 ENGINE FIRE WARNING ACTIVATED ON CLIMBOUT. NR 4 ENGINE SHUTDOWN AND RETURNED TO LEX. MAINTENANCE INSTALLED NEW DU CT BETWEEN 12 O'CLOCK POSITION. PERFORMED ENGINE RUNS AND VERIFIED NO FIRE WARNINGS. 2 H 7 4 4F RT A49EU 1998112600699 19981126 00699 SO 1998 11 26 LR7A9841 1 19981106 A 5744 34862712 FITTING LKHEED 382 382G 526414U SO WS 241 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 402LC 581 4698 DURING ROUTINE MAINT, THE LT OWS 241 FLAP TRACK ATTACH FITTING WAS DISCOVERED CRACKED. REMOVED AND REPLACED FITTING IAW SMP 583 51-10 PARA G, AND 57-10-04. 2 H 7 4 4T A1SO 1998112600700 19981126 00700 SO 1998 11 26 LR7A9842 1 19981112 A 5313 34258224R STRINGER LKHEED 382 382G 526414U SO BS 880 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1669 4606 INNER CAP (P/N 342582-24R) WAS DISCOVERED CRACKED DURING MAINTENANCE. CRACK WAS .15 INCH LENGTH AT WL 203 FS 880 RT BL 63R. REPAIRED PER MAINT PRODUCTION PERMIT L100-401-98-008 COTNEY DOC NR F68 REV 1R DATED 11/6/98. 2 H 7 4 4T A1SO 1998112600701 19981126 00701 SO 1998 11 26 LR7A9843 1 19981112 A 5320 3561984 FITTING LKHEED 382 382G 526414U SO BS 737 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1669 4606 RT FWD STA 737 (817E) END FITTING CORRODED BEYOND LIMITS. REPLACED END FITTING PER SMP 583 53-10-10. 2 H 7 4 4T A1SO 1998112600702 19981126 00702 SO 1998 11 26 LR7A9844 1 19981112 A 5320 3561824 FITTING LKHEED 382 382G 526414U SO BS 737 CORRODED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1669 4606 RT FWD STA 737 (817E) FITTING HAS STRESS CORROSION BEYOND LIMITS. REPLACED END FITTING PER SMP 583 53-50-4 AND SMP 52- 30. 2 H 7 4 4T A1SO 1998112600703 19981126 00703 SO 1998 11 26 LR7A9845 1 19981112 A 5320 3530428R FITTING LKHEED 382 382G 526414U SO BS 990 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1669 4606 FS 990 RT ATTACH FITTING CRACKED. REPLACED FITTING IAW SMP 583 53-50. 2 H 7 4 4T A1SO 1998112600704 19981126 00704 SO 1998 11 26 LR7A9846 1 19981112 A 5320 3530454 WEB LKHEED 382 382G 526414U SO BS 990 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 56648 1669 4606 FS 990 RT WEB CRACKED. REPLACED WEB IAW SMP583-53-50. 2 H 7 4 4T A1SO 1998112600705 19981126 00705 SO 1998 11 26 LR7A9847 1 19981112 A 5320 342593R FITTING LKHEED 382 382G 526414U SO BS 858 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1669 4606 FS 858 RT FITTING CRACKED. REPLACED FITTING PER SMP583-53-50. 2 H 7 4 4T A1SO 1998112600706 19981126 00706 SO 1998 11 26 LR7A9848 1 19981112 A 5320 3891553 FITTING LKHEED 382 382G 526414U SO BS 345 CRACKED A LR7A K NONE O OTHER IN INSP/MAINT 1 AL 03 401LC 1669 4606 FS 345E LT END FITTING CRACKED IN THE RADIUS 0.3 INCH LENGTH. REPAIRED PER MAINT PRODUCTION PERMIT L100-401-98-010 AND COTNEY COMPANY DOC NR F68 REV1R DATED 11/6/98. 2 H 7 4 4T A1SO 1998112600707 19981126 00707 NM 1998 11 26 CALA9802092 1 19981123 A 3260 655825029 CARD BOEING 737 7373T0 1384582 NM RT MLG MALFUNCTIONED A CALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 09 16339 23577 THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. THE LIGHT EXTINGUISHED DURING CHECKLIST PROCEDURES. WHEN THE LANDING GEAR HANDLE WAS MOVED TO OFF THE LIGHT CAME ON AGAIN. THE LIGHT EXTINGUISHED WHEN THE GE AR HANDLE WAS MOVED TO THE UP POSITION. THE FLIGHT WAS CONTINUED TO DEN WHERE IT LANDED WITHOUT FURTHER GEAR WARNING IN DICATION PROBLEMS. 2 L 7 2 4F RT A16WE 1998112600708 19981126 00708 NM 1998 11 26 CALA9802093 1 19981123 A 5720 STIFFENER BOEING 727 727243 138408D NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .75 INCH CRACK IN LT WING RIB STIFFENER AT LOWER END, WBL 92.0. AN ANGLE REPAIR WAS INSTALLED IAW SR M 51-40-3. 2 L 7 3 4F RT A3WE 1998112600709 19981126 00709 NM 1998 11 26 CALA9802094 1 19981123 A 5720 ANGLE BOEING 727 727243 138408D NM WS 121 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND CRACKS IN LOWER ANGLE AT O/B SIDE OF RIB AROUND SEVEN BOLT HEADS INSIDE LT WING LE AFT OF NR 3 LE FLAP I/B END, FS 121. THE ANGLE WAS REMOVED IAW SRM 51-30-2, PAGE 3 AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-10-2, PAGE 12 AND 51-30-2 PAGE 2. 2 L 7 3 4F RT A3WE 1998112600710 19981126 00710 WP 1998 11 26 CALA9802095 1 19981123 A 5350 CLIPS DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJMT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 THE FORCE REQUIRED TO PULL BOTH THE EXTERIOR AND INTERIOR TAIL CONE RELEASE HANDLES FROM CLIPS WAS LOW. THE EXTERIOR AN D INTERIOR HANDLE CLIPS WERE ADJUSTED IAW MM 53-53-00. 2 L 7 2 4F A6WE 1998112600711 19981126 00711 WP 1998 11 26 CALA9802096 1 19981123 A 5350 CABLES DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJMT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 THE FORCE REQUIRED TO RELEASE TAIL CONE USING EXTERIOR HANDLE WAS LOW. THE TAIL CONE CABLES WERE ADJUSTED IAW MM 53-53- 00. 2 L 7 2 4F A6WE 1998112600712 19981126 00712 NM 1998 11 26 CALA9802097 1 19981123 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 1070 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND AFT CARGO FLOORBEAM CORRODED AT STA 1070, RBL 12 TO 48. A REPAIR WAS INSTALLED IAW SRM 53-10-8. 2 L 7 3 4F RT A3WE 1998112600713 19981126 00713 WP 1998 11 26 CALA9802098 1 19981123 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 927 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND A .5 INCH CRACK IN RT CABIN FLOOR SUPPORT AT BELTFRAME STA 927. THE FLOOR SUPPORT WAS REMOVED, A NEW F LOOR SUPPORT WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998112600714 19981126 00714 WP 1998 11 26 CALA9802099 1 19981123 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND A 7 INCH CRACK IN WEB ON RT BELL FRAME IN TAIL COMPARTMENT AT STA 1437. A NEW WEB WAS INSTALLED IAW SR M 53-01. 2 L 7 2 4F A6WE 1998112600715 19981126 00715 WP 1998 11 26 CALA9802100 1 19981123 A 5311 FRAME DOUG DC9 DC981 3022081 WP BS 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16883 48073 INSPECTION FOUND A 7 INCH CRACK IN CANTED FRAME WEB AT STA 1463. THE WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 5 1-30-5. 2 L 7 2 4F A6WE 1998112600716 19981126 00716 WP 1998 11 26 CALA9802101 1 19981124 A 5320 STIFFENER DOUG DC9 DC982 3022082 WP AFT AIRSTAIR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16815 49113 INSPECTION FOUND A .75 INCH CRACK IN SUPPORT STIFFENER ON BOTH LEFT AND RIGHT SIDES OF TAIL COMPARTMENT AFT STAIR HINGE AREA. THE CRACKS WERE STOP DRILLED IAW ECRA 5320-01547. A DIP WAS ISSUED TO INSPECT THE AREAS EVERY FIVE DAYS AND TO P ERMANENTLY REPAIR WITHIN 30 DAYS. 2 L 7 2 4F A6WE 1998112600717 19981126 00717 NM 1998 11 26 CALA9802102 1 19981124 A 5330 SKIN BOEING 727 727243 138408D NM BS 1050 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND RT FUSELAGE SKIN CORRODED AT STA 1050, STRINGER 28R. THE CORRODED AREA WAS CUT OUT, A REPAIR DOUBLER A ND FILLER WERE INSTALLED IAW SRM 51-10-1, 51-10-2, 53-30-3, PAGE 14. 2 L 7 3 4F RT A3WE 1998112600718 19981126 00718 EA 1998 11 26 COMA9860363 1 19981122 A 2130 PRESSURE SYST CNDAIR CL600 CL6002B19 EA CABIN MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 986CA 7174 CABIN PRESSURE WAS FLUCTUATING AT 8,000 FT. COULD NOT DUPLICATE DISCREPANCY. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1998112600719 19981126 00719 NM 1998 11 26 98FDEA00711 1 19981121 A 2782 651781822 ACTUATOR BOEING 727 727232 1384082 NM NR 6 LE FLAP FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 499FE 21018 WHILE RETRACTING FLAPS AFTER T/O, NR 6 LED FAILED TO RETRACT. TRIED LOWERING FLAPS TO 2 DEG AND THEN RETRACTING BACK TO FULLY UP POSITION AND NR 6 LED STILL FAILED TO RETRACT. REMOVED AND REPLACED NR 6 SLAT ACT IAW MM 27-81-32, OPS CK NOR MAL. 2 L 7 3 4F A3WE 1998112600720 19981126 00720 NM 1998 11 26 98FDEA00712 1 19981121 A 5311 65207282 FRAME BOEING 727 72725 1384006 NM BS 1057 CORRDED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 WHILE WORKING NR 0189 FOUND CORROSION ON FRAME AT BS 1057, RBL 9 TO 12 WL 141 TO 138. *S/D* REPAIRED FRAME IAW FEDEX S RM 51-40-3. 2 L 7 3 4F A3WE 1998112600721 19981126 00721 NM 1998 11 26 98FDEA00713 1 19981121 A 5320 6516344 SHEAR TIE BOEING 727 72725 1384006 NM BS 1070 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 CORROSION (C53-113-02) ON SHEAR TIE AT BS 1070 RBL 9 WL 141. 2 L 7 3 4F A3WE 1998112600722 19981126 00722 WP 1998 11 26 ABXA9801085 1 19981120 A 5315 991224357 FLOORBEAM DOUG DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FLOORBEAM AT STATION 965 CORRODED FROM LBL 22 TO LBL 44. REPAIRED FLOORBEAM IAW ABX REA D953-2556 5MR. 2 L 7 2 4F A6WE 1998112600723 19981126 00723 WP 1998 11 26 ABXA9801086 1 19981120 A 5312 3917624517 BULKHEAD FITTING DOUG DOUG DC9 DC932 3022066 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND AFT PRESSURE BULKHEAD DOOR JAMB FITTING CRACKED JUST ABOVE DOOR WARNING SWITCH. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998112600724 19981126 00724 WP 1998 11 26 ABXA9801087 1 19981120 A 5315 3916209502 SUPPORT DOUG DOUG DC9 DC932 3022066 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FLOORBEAM SUPPORT CRACKED STATION 680 AND RBL 44. REPLACED SUPPORT FITTING IAW DC9 SRM 51-30-1 AN D 51-30-2. 2 L 7 2 4F A6WE 1998112600725 19981126 00725 WP 1998 11 26 ABXA9801088 1 19981120 A 5315 9915527505 FLOORBEAM DOUG DOUG DC9 DC932 3022066 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FLOORBEAM AT STATION 680 AND LBL 54 CRACKED. REPLACED FLOORBEAM IAW DC9 SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1998112600726 19981126 00726 WP 1998 11 26 ABXA9801089 1 19981120 A 5400 9958159102 ANGLE DOUG DOUG DC9 DC932 3022066 WP NR 2 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND VERTICAL ANGLE/BRACKET CRACKED ON OUTBOARD SIDE OF NR 2 PYLON, UNDER THROTTLE CONDUIT JAM NUT. RE PLACED BRACKET/ANGLE IAW DC9 SRM. 2 L 7 2 4F A6WE 1998112600727 19981126 00727 WP 1998 11 26 ABXA9801090 1 19981120 A 5320 99101515 WEB DOUG DOUG DC9 DC932 3022066 WP BS 658 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND RIGHT CUSP WEB CRACKED UNDER FLOOR TRACK AT RBL 54, STATION 658. REPAIRED IAW DC9 SRM 53-01. 2 L 7 2 4F A6WE 1998112600728 19981126 00728 WP 1998 11 26 ABXA9801091 1 19980806 A 5313 37585931 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1340 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 LONGERON 356 STATION 1340 IS CRACKED. REPAIRED IAW DC9 SRM 51-1-20D AND 51-3-2. 2 L 7 4 4F 4A25 1998112600729 19981126 00729 WP 1998 11 26 ABXA9801092 1 19980806 A 5320 5758011 SUPPORT DOUG DOUG DC8 DC861 3021952 WP BS 260 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 FORWARD LOWER CARGO FLOOR SUPPORT ANGLE CRACKED AT STATION 260, LONGERON 33L. REPAIRED IAW DC8 SRM 51-1-3 AND 51-1-8, 5 1-1-20, AND 51-1-21. 2 L 7 4 4F 4A25 1998112600730 19981126 00730 WP 1998 11 26 ABXA9801093 1 19980806 A 5753 5642970506 SKIN DOUG DOUG DC8 DC861 3021952 WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 LEFT WING OUTBOARD FLAP UPPER SURFACE BULGED JUST FORWARD OF PRIOR DOUBLER REPAIR OUTBOARD OF OUTBOARD HINGE FOLDING COV ER. REPAIRED IAW DC8 SRM 57-7-0, AND 57-2-1. 2 L 7 4 4F 4A25 1998112600731 19981126 00731 WP 1998 11 26 ABXA9801094 1 19980806 A 5730 57053272 PANEL DOUG DOUG DC8 DC861 3021952 WP RT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 RIGHT WING LOWER TRAILING EDGE PANEL 577B EXTERIOR SKIN CRACKED AND DISBONDED. REPAIRED IAW DC8 SRM 51-1-8 AND 57-3-0. 2 L 7 4 4F 4A25 1998112600732 19981126 00732 WP 1998 11 26 ABXA9801095 1 19980729 A 5313 3750151501 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 560 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 CORROSION ON LONGERON 36 AT STATION 560. REPAIRED IAW ABX REA D85323445MR. 2 L 7 4 4F 4A25 1998112600733 19981126 00733 WP 1998 11 26 ABXA9801096 1 19980727 A 5320 5614974 DOUBLER DOUG DOUG DC8 DC861 3021952 WP BS 140 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 FORWARD LOWER CARGO STATION 140 AT LONGERON 35R INTERNAL DOUBLER IS CRACKED. REPAIRED IAW ABX REA D853-23438MR. 2 L 7 4 4F 4A25 1998112600734 19981126 00734 WP 1998 11 26 ABXA9801097 1 19980729 A 5210 5613859 SKIN DOUG DOUG DC8 DC861 3021952 WP L1 DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 CRACK AT FORWARD PASSENGER DOOR CORNER. REPAIRED IAW ABX REA D853-23437MR, REV A. 2 L 7 4 4F 4A25 1998112600735 19981126 00735 WP 1998 11 26 ABXA9801098 1 19980729 A 5400 546230111 ANGLE DOUG DOUG DC8 DC861 3021952 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 RADIUS CRACK AT NR 1 PYLON ATTACH ANGLE. REPAIRED IAW ABX REA D854-23442MR. 2 L 7 4 4F 4A25 1998112600736 19981126 00736 WP 1998 11 26 ABXA9801099 1 19980729 A 5313 565192719 LONGERON DOUG DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 CORROSION AND CRACK ON LONGERON 2L. REPAIRED IAW ABX REA D853-23444MR. 2 L 7 4 4F 4A25 1998112600737 19981126 00737 WP 1998 11 26 ABXA9801100 1 19980729 A 5320 5614974 TEAR STRIP DOUG DOUG DC8 DC861 3021952 WP FUSELAGE CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 STATION 140 TEAR STRIP IS CRACKED. REPAIRED IAW ABX REA D853-23438MR. 2 L 7 4 4F 4A25 1998112600738 19981126 00738 WP 1998 11 26 ABXA9801101 1 19980806 A 5320 97549441 JAMB DOUG DOUG DC8 DC861 3021952 WP C3 DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 C3 DOOR JAMB CORRODED. REPAIRED IAW REA D853-23458MR. 2 L 7 4 4F 4A25 1998112600739 19981126 00739 WP 1998 11 26 ABXA9801102 1 19980806 A 5414 5765901 PANEL DOUG DOUG DC8 DC861 3021952 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 NR 1 PYLON ACCESS PANEL LAND DOUBLER HAS A CRACK FROM CAM LOK HOLE TO EDGE OF DOUBLER, LENGTH 44. REPAIRED IAW ABX REA D854-23467MR. 2 L 7 4 4F 4A25 1998112600740 19981126 00740 WP 1998 11 26 ABXA9801103 1 19980806 A 5320 37592221 SPLICE DOUG DOUG DC8 DC861 3021952 WP BS 1280 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 LONGERON SPLICE AT STATION 1280 LONGERON 34R IS CORRODED. REPAIRED IAW DC8 SRM 51-3-2 AND 51-1-20D. 2 L 7 4 4F 4A25 1998112600741 19981126 00741 WP 1998 11 26 ABXA9801104 1 19980806 A 5313 575032229 LONGERON DOUG DOUG DC8 DC861 3021952 WP BS 1280 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 LONGERON 3LL IS CRACKED AT STATION 1280 TO 1260. REPAIRED IAW DC8 SRM 51-3-0. 2 L 7 4 4F 4A25 1998112600742 19981126 00742 WP 1998 11 26 MWEA981107 1 19981112 A 5320 99115057 ANGLE DOUG DC9 DC915 3022036 WP BS 84 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 GSO - SECONDARY ATTACH ANGLES CRACKED IN RADIUS STATION 84. MAINTENANCE STOPPED DRILLED CRACKS, REMOVED AND REPLACED IN TERCOSTAL. FABRICATED AND INSTALLED ANGLES AND DOUBLERS. (M) 2 L 7 2 4F A6WE 1998112600743 19981126 00743 WP 1998 11 26 MWEA981108 1 19981111 A 5315 99115469 FLOORBEAM DOUG DC9 DC915 3022036 WP BS 817 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 300ME 45718 GSO - FLOORBEAM AT STATION 817 AT RBL 16 HAS 2 PLUGS THAT ARE PROTRUDING OUT OF WEB AND CLOSE TO REPAIR HOLES WHICH ARE EXISTING. FABRICATED AND INSTALLED STATION 817 FLOORBEAM WEB FILLER AND DOUBLER REPAIRS. (M) 2 L 7 2 4F A6WE 1998112600744 19981126 00744 WP 1998 11 26 MWEA981109 1 19981111 A 5315 991154613 FLOORBEAM DOUG DC9 DC915 3022036 WP BS 817 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 300ME 45718 GSO - NEW STATION 817 FLOORBEAM UPPER ANGLE BEAM CAP HAS NO ED ON THE LAST HOLE ON LEFT SIDE TOP LEG. FABRICATED AND IN STALLED STATION 817 FLOORBEAM REPAIR PARTS AND INSTALLED. (M) 2 L 7 2 4F A6WE 1998112600745 19981126 00745 WP 1998 11 26 MWEA981110 1 19981111 A 5315 991154613 FLOORBEAM DOUG DC9 DC915 3022036 WP BS 817 MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 300ME 45718 FLOORBEAM AT STA 817 AT RBL 16 HAS 2 PLUGS THAT ARE PROTRUDING OUT OF WEB AND TOO CLOSE TO REPAIR HOLES WHICH ARE EXISTI NG. DRILLED UP NEW EXTRUDED UPPER BEAM CAP AT STATION 817 FLOOR BEAM AND INSTALLED. 2 L 7 2 4F A6WE 1998112600746 19981126 00746 SO 1998 11 26 SWIA971309 1 19981110 A 3010 3D237606 DE-ICE BOOT EMB 120 EMB120RT SO PWA 118 PW118 NE LT & RT WING FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 161CA 120143 LEFT OUTBOARD AND RIGHT OUTBOARD WINGS DEICE BOOTS FAILED. RETURNED TO FAT. REPLACED OUTBOARD WING EJECTOR FLOW CONTRO L VALVE, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112600748 19981126 00748 SO 1998 11 26 SWIA971311 1 19981110 A 3010 38E966A REGULATOR EMB 120 EMB120RT SO PWA 118 PW118A NE LT & RT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 LEADING EDGE BOOTS FAIL IN ALL MODES OF OPERATION. RETURNED TO FAT. REPLACED LEFT AND RIGHT DEICE PRESS REGULATORS, OP S CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112600749 19981126 00749 SO 1998 11 26 SWIA971313 1 19981110 A 3260 SENSOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT MLG FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 567SW 120342 LEFT A GREEN LIGHT REMAINS ON AT ALL TIMES WHEN CYCLING LANDING GEAR, LEFT RED A DISAGREEMENT LIGHT STAYS OUT. RETURNED TO FIELD. REPLACED LEFT STRUT GREEN A LIGHT PROX SENSOR. SWUNG GEAR SEVERAL TIMES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112600750 19981126 00750 SO 1998 11 26 SWIA971314 1 19981109 A 2750 RETRACT MECH EMB 120 EMB120RT SO PWA 118 PW118A NE TE FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 268UE 120207 AFTER TAKEOFF, FLAPS SELECTED UP WITH RESULTING DISAGREEMENT QRH WAS CONSULTED. CYCLED FLAPS AND WERE UNABLE TO GET FLA PS UP OR DISAGREEMENT LIGHT TO EXTINGUISH. RETURNED TO ONT. OBSERVED OPERATION OF FLAPS THROUGH SEVERAL CYCLES, OPS CH ECKS GOOD. NO FAULTS FOUND AT THIS TIME. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112600751 19981126 00751 EA 1998 11 26 SWIA971315 1 19981115 A 2751 INDICATION CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 407SW 7034 FLAP FAIL MESSAGE COMES ON IN CRUISE WHILE LEVEL AT 35,000. FLAPS REMAINED AT 0, NO CONTROL PROBLEMS. RETURNED TO SLC. RESET CB1-F4 AND CB2-F4, IAW A/D 98-20-01 PAR B. FLAP SYSTEM RESET TO NORMAL AND NO EVIDENCE OF TWISTING, SKEWING OR ABNORMAL DEFORMATION. 2 L 7 2 4F 4 F RT A21EA E15NE 1998112600752 19981126 00752 NE 1998 11 26 SWIA971316 2 19981117 A 7321 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT EEC DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 290SW 120317 LEFT ENGINE TORQUE SURGED AFTER TAKEOFF TO 108 PERCENT, 111 PERCCENT, 109 PERCENT AND 115 PERCENT. LEFT EEC REVERTED TO MANUAL. RESET LEFT EEC AND MAINTAINED ABOUT 40 PERCENT TORQUE ON LEFT ENGINE. RIGHT ENGINE NORMAL. RETURNED TO AIRPO RT AND RAN ENGINE (LEFT) AT HIGH POWER WITH EEC OFF, MEL 73-21-1. CLEANED EEC SENSOR CONNECTORS AND OHMED SYSTEM. OPS NORMAL DURING GROUND RUN. 2 L 7 2 4T 4 T RT A31SO E20NE 1998112600753 19981126 00753 NM 1998 11 26 P5CA9801598 1 19981122 A 2150 PACK BOEING 747 747283B 1384867 NM NR 2 MALFUNCTIONED A P5CA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 23 921FT 21575 NR 2 PACK UNCONTROLLABLE IN AUTO AND MANUAL MODE. DUE TO INOP NR 3 PACK ON DMI, HAD TO RETURN TO HKG. INTERCHANGE NR 2 AND NR 3 PACK CONTROLLERS BYPASS VALVE AND TEMP SENSOR AND NR 3 PACK OPS NORMAL. 2 L 7 4 4F A20WE 1998112600754 19981126 00754 NM 1998 11 26 P5CA9801599 1 19981105 A 2910 LINE BOEING 747 747122 1384872 NM NR 4 PYLON LOOSE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 853FT 19753 NR 4 HYDRAULIC SYSTEM DROPPED BY 2 GALLONS DURING FIRST HOUR OF FLIGHT. DEPRESSURIZED SYSTEM AND LOSS STOPPED. FOUND H YD LINE IN PYLON AFT OF FIREWALL LOOSE. RESECURED AND TIGHTENED LINE. OPS AND LEAK CHECK GOOD PER MM 29-00-00 AND SERV ICED FULL PER MM 12-00-00. 2 L 7 4 4F A20WE 1998112600755 19981126 00755 WP 1998 11 26 ARWA981128 1 19981123 A 3260 CONNECTOR DOUG DC8 DC862 3021970 WP NLG LOOSE A ARWA O OTHER N FALSE WARNING LD LANDING 1 SO 19 8968U 46069 NOSE GEAR DOWN LIGHT DID NOT COME ON WHEN GEAR WAS EXTENDED. T/S FOUND DOWNLOCK SWITCH CANNON PLUG NOT SECURED. SECURE D CANNON PLUG ON DOWNLOCK SWITCH, OPS NORMAL WITH GEAR SWING IAW 32-60-00. 2 L 7 4 4F 4A25 1998120200001 19981202 00001 1998 12 2 SWIA971301 4 19981030 A 3418 STALL UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE E & E COMPT FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 411SW 7067 DURING CLIMBOUT, THE EICAS CAUTION MESSAGE STALL FAIL DISPLAYED. CONSULTED MAINTENANCE CONTROL, ADVISED RETURN TO SLC A FTER COMPLETING QRH. REMOVED AND REPLACED STALL PROTECTION UNIT, OPS CHECK GOOD ON GROUND. 2 L 7 2 4F 4 F RT A21EA E15NE 1998120400004 19981204 00004 NE 1998 12 4 CA980406029 2 19980115 A 7250 0292507640 COVER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TURBINE SECTION GOUGED W K NONE O OTHER IN INSP/MAINT 1 CA 258 (CAN) DURING REAR BEARING CLEANING, THE BEARING COVER WAS FOUND TO BE GOUGED IN AREA OF CONTACT WITH BEARING ATTACHMENT NUT. PART TC: 3,848. 1 G 7 1 3U 3 U H9EU E19EU 1998120400005 19981204 00005 NE 1998 12 4 CA980406030 2 19980306 A 7412 0301047920 SUPPORT SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 295 835 (CAN) IGNITOR BOX SUPPORT FOUND CRACKED ON DAILY INSPECTION. NO EXCESSIVE ENGINE VIBRATIONS WERE NOTED IN ENGINE. 1 G 7 1 3U 3 U H9EU E19EU 1998120400006 19981204 00006 GL 1998 12 4 CA980406031 2 19980211 A 7314 6899253 PUMP TRW BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1457 T3161 CAE822231 (CAN) ENGINE DRIVEN FUEL PUMP DRAIN SEAL LEAKING BEYOND LIMIT. PUMP ALSO MAKING LOUD SQUEALS DURING START-UP. 1 G 7 1 3U 3 U H2SW E4CE 1998120400007 19981204 00007 SW 1998 12 4 CA980406039 1 19980330 A 6120 8696475 SLEEVE 86913019 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HARTZL HCB3T HCB3TN5 GL PITCH CONTROL WORN W K NONE O OTHER IN INSP/MAINT 1 CA P146371 P54239 BV6078 (CAN) WHEN NR 1 ENGINE SHUT DOWN, THE NR 1 PROPELLER FEATHERED AND COULD NOT BE PUT ON THE START LOCKS. SLEEVE PIN WORN BEYOND LIMITS AND THE INTERNAL BUSHING WAS ALSO WORN. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C P15EA 1998120400008 19981204 00008 WP 1998 12 4 CA980406040 2 19980331 A 7230 31081642 BLADES SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP 1ST STAGE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1623 2035012224 P54239 (CAN) WHEN COMPLETING PERIODIC BORESCOPE INSPECTION, THE NR 1 ROTOR BLADES HAD EVIDENCE OF WEAR ON THE LEADING EDGES. F URTHER INVESTIGATION INDICATED BLADES WORN BEYOND LIMITS. ROTOR RETURNED TO GARRETT. 2 L 7 2 4T 4 T RT A8SW E4WE 1998120400009 19981204 00009 WP 1998 12 4 CA980406041 2 19980331 A 7230 31081642 BLADES SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP 1ST STAGE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1021 9032203800 P54174 (CAN) DURING PERIODIC BORESCOPE INSPECTION, THE NR 1 ROTOR BLADES SHOWED EVIDENCE OF WEAR ON THE LEADING EDGES. FURTHER INVESTIGATION SHOWED DAMAGE TO BLADES BEYOND LIMITS. ROTOR RETURNED TO GARRETT. 2 L 7 2 4T 4 T RT A8SW E4WE 1998120400010 19981204 00010 WP 1998 12 4 CA980406042 2 19980331 A 7230 31081642 BLADES SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP 1ST STAGE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 455 6032293759 P54259 (CAN) DURING PERIODIC BORESCOPE INSPECTION, THE NR 1 TURBINE BLADES SHOWED EVIDENCE OF LEADING EDGE WEAR. FURTHER INVES TIGATION INDICATED THAT THE DAMAGE WAS BEYOND LIMITS. 2 L 7 2 4T 4 T RT A8SW E4WE 1998120400011 19981204 00011 WP 1998 12 4 CA980406043 2 19980331 A 7230 31081642 BLADES SWRNGN SA226 SA226AT 8780405 SW GARRTT TPE331 TPE33110UA 01514 WP 1ST STAGE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 529 6032293796 P54098 (CAN) DURING PERIODIC BORESCOPE INSPECTION, THE NR 1 TURBINE BLADES WERE FOUND WORN ON THE LEADING EDGES. FURTHER INVES TIGATION REVEALED THAT THE NR 1 ROTOR BLADES WERE WORN BEYOND LIMITS. 2 L 7 2 4T 4 T RT A5SW E4WE 1998120400012 19981204 00012 WP 1998 12 4 CA980406044 2 19980331 A 7230 31081642 BLADES SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP 1ST STAGE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1221 2035012224 P54031 (CAN) DURING PERIODIC BORESCOPE INSPECTION, IT WAS FOUND THAT THE NR 1 TURBINE BLADES WERE WORN ON THE LEADING EDGES. F URTHER INVESTIGATION FOUND THAT THEY WERE WORN BEYOND LIMITS. 2 L 7 2 4T 4 T RT A8SW E4WE 1998120400013 19981204 00013 WP 1998 12 4 CA980406045 2 19980331 A 7230 31081642 BLADES SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP 1ST STAGE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 2018 7035011540 P54177 (CAN) DURING PERIODIC BORESCOPE INSPECTION, THE NR 1 TURBINE BLADES WERE FOUND WORN ON THE LEADING EDGES. FURTHER INVES TIGATION SHOWED THAT THEY WERE WORN BEYOND LIMITS. 2 L 7 2 4T 4 T RT A8SW E4WE 1998120400017 19981204 00017 WP 1998 12 4 CA980507006 1 19980506 A 7810 23030979 CLAMP 6879874 HUGHES 369 369HE 4470720 WP ALLSN 250C 250C18 03011 GL EXHAUST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 188 CAE801229B (CAN) EXHAUST COLLECTOR WELDED MARON CLAMP RING FOUND CRACKED. 1 G 7 1 3U 3 U H3WE E4CE 1998120400024 19981204 00024 WP 1998 12 4 CA980602026 1 19980525 A 7120 AUB7353501 NUT RETAINER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE NR 1 ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 52892 455794 (CAN) NR 1 ENGINE AFT ENGINE MOUNT, FORWARD NUT, NUT RETAINER ASSEMBLIES FOUND BROKEN. BOTH FORWARD LEFT AND RIGHT RETA INER PLATES WERE REPLACED ON THE AFT MOUNT. PART TC: 13,536. 2 L 7 3 4F 4 F A22WE E23EA 1998120400026 19981204 00026 NE 1998 12 4 CA980602036 2 19980302 A 7200 ENGINE 0292005060 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE BAY CONTAMINATED W D RETURN TO BLOCK J WARNING INDICATION NR NOT REPORTED 1 CA 946 (CAN) FOLLOWING START, THE ENGINE RPM WAS INCREASED TO 100 PERCENT WHEN ENGINE CHIP DETECT LIGHT CAME ON. METAL FOUND O N CHIP DETECTOR AND MODULES 02 AND 03 WERE REPLACED. 1 G 7 1 3U 3 U H9EU E19EU 1998120400028 19981204 00028 SW 1998 12 4 CA980602046 1 19980428 A 6230 20057564D BOLT 206010450113 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL SWASHPLATE MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE820758 (CAN) ATTEMPT TO INSTALL BOLT THROUGH SWASHPLATE DRIVE LINK LEVER ASSY FAILED DUE TO NEW BOLT BEING OVERSIZE WITH CADIUM PLATING REMOVED. BOLT ALSO EXHIBITS PITTING ON SHANK AND SEEMS TO BE MADE OF INFERIOR MATERIAL. 1 G 7 1 3U 3 U H2SW E4CE 1998120400029 19981204 00029 NE 1998 12 4 CA980602051 2 19980327 A 7230 0169448330 FCU SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1022 835 (CAN) FUEL LEAKING FROM THE FCU DRAIN WITH BOOST PUMP PRESSURE ON. ALSO, HIGH FUEL CONSUMPTION. 1 G 7 1 3U 3 U H9EU E19EU 1998120400030 19981204 00030 WP 1998 12 4 CA980602054 1 19980421 A 6710 NAS620458D BOLT HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA CAE832104 (CAN) BOLT RECEIVED WITH OBVIOUS DEFECTS. PIECES .001 INCH - .002 INCH THICK FLAKING OFF THE SHANK SURFACE. 1 G 7 1 3U 3 U H3WE E4CE 1998120400039 19981204 00039 EU 1998 12 4 CA980629026 1 19980609 A 7400 9550147560 SOLENOID SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE IGNITION DAMAGED W B A EMER. DESCENT UNSCHED LANDING X ENGINE FLAMEOUT CR CRUISE 1 CA 3710 1178 4103 505 (CAN) DURING CRUISE AT 1300 AGL WITH EXTERNAL SLUNG LOAD, THE ENGINE FLAMED OUT. LOAD RELEASED. INSPECTION REVEALED TH AT THE THREADS IN THE ENGINE IGNITION SOLENOID WERE FOUND STRIPPED AND A UNION P/N 0301020420 CAME OUT OF THE VALVE. TH E UNION WAS FOUND STILL ATTACHED TO THE FUEL LINE BY A B-NUT AND WAS PROPERLY LOCKWIRED AND THE O-RING INTACT. PART TC: 1,990. 1 G 7 1 3U 3 U NC H9EU E19EU 1998120400040 19981204 00040 GL 1998 12 4 CA980629027 2 19980621 A 7230 23039752 VANE 23038126 BELL 206 206L 1181522 SW ALLSN 250C 250C20 03013 GL STRUT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1319 CAC15277 CAE832421 (CAN) THE FRONT FRAME SUPPORT STRUT WAS FOUND CRACKED THE FULL LENGTH OF THE TRAILING EDGE AT APPROXIMATELY 10 O'CLOCK P OSITION. PART TC: 2,127. 1 G 7 1 3U 3 U H2SW E4CE 1998120400042 19981204 00042 WP 1998 12 4 CA980724019 1 19980625 A 6220 369D212543 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL MAIN ROTOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 711 CAE830901 (CAN) MAIN ROTOR HUB, EXCESSIVE UP AND DOWN PLAY ON MAST. 1 G 7 1 3U 3 U H3WE E4CE 1998120400043 19981204 00043 SW 1998 12 4 CA980804007 1 19980720 A 2400 ELECTRICAL SYS BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA DC SYSTEM FAILED W A E UNSCHED LANDING ENGINE SHUTDOWN G H J MULTIPLE FAILURE ELECT. POWER LOSS-50 PC WARNING INDICATION HO HOVERING 1 CA CPPS61401 (CAN) A LARGE AMOUNT OF STATIC ELECTRICITY WAS OCCURRING DURING SLINGING OPS ON LONG LINE. WHILE SLINGING A LOAD, THE S TARTER/GENERATOR FOR ONE ENGINE WENT OFF-LINE. PILOT RESET THE GENERATOR AND IT CAME BACK ON-LINE. A SECOND BUILD-UP O F STATIC FOLLOWED BY A DISCHARGE CAUSED A COMPLETE POWER FAILURE (NO BATTERY, NO GEN). PILOT COULD NOT RELEASE THE LOAD ELECTRICALLY AND FUEL BOOST PUMPS INOPERATIVE. UNCOMMANDED ENGINE POWER ROLLBACK, POSSIBLY CAUSED BY FUEL BOOST PUMPS INOPERATIVE. 1 G 7 1 4U 4 U H4SW E22EA 1998120400047 19981204 00047 SW 1998 12 4 CA980825017 1 19980710 A 3210 3011 STRAP 206325008 BELL 206 206L 1181522 SW SKID TUBE TORN W K NONE O OTHER IN INSP/MAINT 1 CA 3011 (CAN) STRAP DAMAGED, SADDLE CREEPS FORWARD ON SKID TUBE. 1 G 7 1 3U H2SW 1998120400048 19981204 00048 SW 1998 12 4 CA980825018 1 19980710 A 5610 206201045 WINDOW BELL 206 206L 1181522 SW COCKPIT LOOSE W K NONE O OTHER NR NOT REPORTED 1 CA (CAN) RUBBER MOUNTED WEDGE WINDOW COMES OFF SEAL AFTER A FEW HOURS FLYING. 1 G 7 1 3U H2SW 1998120400049 19981204 00049 EU 1998 12 4 CA980908033 1 19980821 A 3310 8ES00558800 POWER UNIT S92513063001 AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE ROW 3 FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 120619 881231 (CAN) DURING CLIMB, FLIGHT ATTENDANT NOTICED SMOKE FROM THE OVERHEAD BIN AT LOCATION 3CD. CREW DEACTIVATED LIGHT CIRCUI T AND AIRCRAFT RETURNED TO BLOCKS. POWER SUPPLY UNIT FOR READING LIGHT HAD FAILED. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1998120400050 19981204 00050 NM 1998 12 4 CA980908047 1 19980823 A 3246 83240011S101 WHEEL BFGOODRICH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG FAILED W K NONE O OTHER TX TAXI/GRND HDL 1 CA 17930 1344 PCE121242 (CAN) A 19 INCH PIECE OF WHEEL BEAD SEPARATED WHILE THE AIRCRAFT WAS TAXIING TO TERMINAL FOLLOWING LANDING. PART TC: 2 0,135. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400051 19981204 00051 NM 1998 12 4 CA980908048 1 19980831 A 3233 85411783001 BRACKET DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 120383 (CAN) MLG ACTUATOR BRACKET FOUND CRACKED AROUND THE SPIGOT. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400060 19981204 00060 WP 1998 12 4 CA980915024 1 19980906 A 3243 1551351101 CONTROL CABLE LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE BRAKE VALVE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 10491 (CAN) UNABLE TO RELEASE PARKING BRAKE, CREW HAD TO CYCLE BRAKES TO RELEASE PARKING BRAKE. DUAL POWER BRAKE VALVE CONTRO L CABLE FRAYED AT PULLEY UNDER PILOT'S SEAT. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1998120400061 19981204 00061 NM 1998 12 4 CA980916001 1 19980815 A 5210 85210180001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PAX DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 121165 (CAN) MAIN AIRSTAIR DOOR UNSUPPORTED DURING OPENING/CLOSING. DOOR SUPPORT CABLE FOUND OFF PULLEY AND BROKEN INSIDE FORW ARD WARDROBE. BROKEN CABLE FOUND LYING ACROSS RELAY PANEL, MELTED IN TWO FROM CONTACT WITH RELAYS. CABLE/PULLEY ASSEMB LY REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400063 19981204 00063 EU 1998 12 4 CA980916003 1 19980816 A 2120 UNKNOWN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 24978 LF05463A (CAN) DURING DESCENT, SMELL NOTICED IN THE CABIN. AIR SAMPLE TAKEN. APU NOT RUNNING. INSPECTED ALL ENGINE NR 1 AND NR 9 SEALS FOR OIL LEAKS. NO FAULTS FOUND, AIRCRAFT RETURNED TO SERVICE. PART TC: 28,053. 2 H 7 4 4F 4 F RT A49EU E6NE 1998120400064 19981204 00064 EU 1998 12 4 CA980916004 1 19980819 A 3520 K38667 OXYGEN MASK BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN WRONG PART W K NONE O OTHER IN INSP/MAINT 1 CA LR05628A (CAN) PART NUMBER K38667 DROP-OUT OXYGEN MASK ASSY [65 PSI SYSTEM] FOUND TO BE INSTALLED ON POST MOD 50043A - BAROMETRIC VALVE AUTOMATIC DROP-OUT [5-9 PSI SYSTEM] AIRCRAFT. BAE PC SHOWS P/N K38667 MASK ASSY WITH AIRCRAFT EFFECTIVITY SERIAL NUMBERS 001-999. MOD 50043A LOWERS PASSENGER OXYGEN SYSTEM PRESSURE FROM 65 PSI TO 5-9 PSI AND REQUIRES P/N K38669 MAS K ASSY. BAE IPC SHOWS P/N K38669 MASK WITH NO EFFECTIVITY CODE. SUBMITTER STATES THAT THIS PROBLEM WAS FOUND ON ALL FI VE OF THEIR OPERATOR'S FLEET. 2 H 7 4 4F 4 F RT A49EU E6NE 1998120400065 19981204 00065 NM 1998 12 4 CA980916005 1 19980817 A 2435 23088002A STARTER/GEN DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE FAILED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 3703 779 1284 120229 (CAN) DURING CLIMB-OUT, NR 2 AC POWER MONITOR GAVE ERRONEOUS READINGS AND WENT BLANK. NR 2 ENGINE INDICATIONS WERE REA DING ERRONEOUSLY (INDICATING HIGHER TORQUE, FUEL FLOW), ITT. AIRCRAFT RETURNED FOR NORMAL LANDING. NR 2 STARTER/GENERA TOR REPLACED. PART TC: 4,840. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400066 19981204 00066 NM 1998 12 4 CA980916006 1 19980821 A 3246 314354 WHEEL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 2289 377 2383 120229 (CAN) DURING WHEEL INSPECTION, EDDY CURRENT SHOWED SEVERAL CORROSION PITS IN AREA OF TIRE BEAD. WHEEL HALVES SCRAPPED. PART TC: 3,097. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400067 19981204 00067 EA 1998 12 4 CA980916007 1 19980802 A 2720 72740252001 TRANSMITTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RUDDER MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA 16838 123129 (CAN) RUDDER NOT INDICATING FULL LEFT TRAVEL. RUDDER POSITION SYNCRO TRANSMITTER LEVER (P/N 72740252-001) AND BRACKET ( P/N 72760297101) FOUND WORN. BRACKET AND LEVER REPLACED. PART TC: 25,770. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400068 19981204 00068 NM 1998 12 4 CA980916008 1 19980822 A 3320 BV033000220 LIGHT SOCKET BR63031021 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ROW 8 FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 4726 120152 (CAN) DURING INSPECTION OF CABIN, FLUORESCENT LIGHTING, FOUND ROW 8 LAMP NOT ILLUMINATED. INSPECTION FOUND LAMP SOCKET BURNED. LAMP SOCKET P/N BV03300-02-20 FOUND BURNED, SOCKET ON OTHER END OF TUBE P/N BV03302-02-23 NOT BURNED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400069 19981204 00069 NE 1998 12 4 CA980916009 2 19980825 A 7532 311325201 VALVE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE DAMAGED W K NONE B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA PCE123133 (CAN) AFTER START, WHEN NR 2 ENGINE BLEED AIR WAS SELECTED ON, SMOKE APPEARED IN THE CABIN. ENGINE AIR SWITCHING VALVE WAS FOUND GROOVED. THE VALVE WAS REPAIRED AND REINSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400070 19981204 00070 NE 1998 12 4 CA980916013 2 19980831 A 7260 BEARING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 ENGINE FAILED W E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA PCE123126 (CAN) NR 1 ENGINE EXPERIENCED POWER LOSS IN-FLIGHT. TORQUE DROPPED FROM 66 PERCENT TO 33 PERCENT. FUEL FLOW DROPPED FR OM 380 TO 280 PPH AND OIL PRESSURE DROPPED TO ZERO. NR 1 ENGINE WAS SHUT DOWN. INITIAL INVESTIGATION ON CAUSE OF POWER LOSS SHOWED A FAILURE OF NR 5 BEARING IN THE TURBO MACHINERY. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400071 19981204 00071 NE 1998 12 4 CA980916014 2 19980904 A 7310 7589141 FILTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE DIRTY W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 980 120648 (CAN) NR 2 ENGINE FUEL BYPASS CAUTION LIGHT ILLUMINATED ON CLIMB. AIRCRAFT RETURNED TO POINT OF DEPARTURE. NR 2 ENGINE FUEL FILTER REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400073 19981204 00073 NM 1998 12 4 CA980916017 1 19980811 A 3240 R30F4 PULLEY 65463934 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE RUDDER SEIZED W D RETURN TO BLOCK O OTHER TO TAKEOFF 1 CA 40716 18192 687733 (CAN) ON TAKEOFF ROLL, AIRCRAFT VEERED TO THE RIGHT WITH FULL RUDDER APPLIED. AIRCRAFT RETURNED TO GATE USING TILLER. F OUND PULLEY BEARING AT METERING VALVE CRANK SEIZED, LIMITING CENTERING ACTION OF METERING VALVE. PULLEY AND CRANK REPLA CED. PART TC: 17,270. 2 L 7 2 4F 4 F A16WE E2EA 1998120400074 19981204 00074 EU 1998 12 4 CA980916018 1 19980810 A 2822 ASNE0390DD03 CONNECTOR ASNE0390DD03 AIRBUS 320 A320211 3930320 EU FUEL SYSTEM FAILED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION IN INSP/MAINT 1 CA 21784 (CAN) DURING TROUBLESHOOTING FOR PUMP, CIRCUIT BREAKER TRIPPING, FOUND MALE AND FEMALE PORTIONS OF PLUG BURNED. SUBMITT ER SUSPECTED RESISTANCE IN PLUG TO BE CAUSE. REPLACED. PART TC: 7,989. 2 L 7 2 4F RT A28NM 1998120400075 19981204 00075 WP 1998 12 4 CA980916020 1 19980820 A 5730 NAS4605U12 PANEL SCREW 533T DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE LT WING WRONG PART W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 455367 (CAN) FUEL VENTING FROM LT WING INSPECTION PANEL IN-FLIGHT. STOPPED AT 34,000 POUNDS. INSPECTION PANEL SCREW TOO LONG, DAMAGED CAP NUTS. CAP NUTS REPLACED AND PROPER SCREW PER IPC INSTALLED. 2 L 7 3 4F 4 F A22WE E23EA 1998120400076 19981204 00076 NM 1998 12 4 CA980916021 1 19980824 A 7722 SEL0C19D INDICATOR SELOC19D BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE COCKPIT READS LOW W C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CA 30677 481BA 709520 (CAN) ABORTED TAKEOFF DUE TO EGT 650 DEGREES, ALSO, EPR NOT ACTIVATED, AIRCRAFT RETURNED TO RAMP. CLEANED WATER TRAP AN D PS4 LINE. ENGINE RUN AT TAKEOFF POWER. AIRCRAFT SERVICEABLE. REPLACED NR 1 EGT INDICATOR. 2 L 7 2 4F 4 F A16WE E2EA 1998120400077 19981204 00077 NM 1998 12 4 CA980916022 1 19980824 A 2610 D1098B CONNECTOR BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE NR 2 ENGINE CONTAMINATED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 709378 (CAN) INTERMITTENT FIRE WARNING ON NR 2 ENGINE. AIRCRAFT RETURNED AFTER SWITCHING OVERHEAT TO FIRE POSITION. LIGHT WEN T OUT. FOUND CONNECTOR CONTAMINATED WITH OIL. CLEANED AND AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F A16WE E2EA 1998120400078 19981204 00078 NM 1998 12 4 CA980916023 1 19980825 A 2410 728550 CSD BOEING 737 737296 1384486 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE MALFUNCTIONED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA P707313B (CAN) NR 1 ENGINE GENERATOR AND CONSTANT SPEED DRIVE (CSD) WENT FULL VOLTS AND FREQUENCY. THE GENERATOR WAS TURNED OFF. VIBRATION WAS NOTICED, SO THE CSD WAS DISCONNECTED. A SEAL ON THE GEARBOX WAS FOUND NICKED. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1998120400079 19981204 00079 EU 1998 12 4 CA980916024 1 19980825 A 5610 NP165113 WINDOW PPG NP165113 AIRBUS 320 A320211 3930320 EU CRACKED CRACKED W H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 CA 12446 54015 (CAN) EN ROUTE, CAPTAIN'S OUTER PANE, 31 WINDOW CRACKED. PULLED CIRCUIT BREAKER, AIRCRAFT RETURNED. INVESTIGATION SHOW ED SIGNS OF BIRD STRIKE IN UPPER CORNER OF WINDOW, WINDOW REPLACED. PART TC: 4,524. 2 L 7 2 4F RT A28NM 1998120400080 19981204 00080 WP 1998 12 4 CA980916025 1 19980826 A 5730 534AT PANEL DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE WING LEAKING W J A DUMP FUEL UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 75981 455367 (CAN) FUEL LEAKING FROM WING PANEL 534 DURING FLIGHT. PANELS 534AT, 531AT, 534BT,534CT, 535AT, AND 535BT REMOVED FOR R EPAIRS AND REINSTALLED. PART TC: 18,133. 2 L 7 3 4F 4 F A22WE E23EA 1998120400081 19981204 00081 WP 1998 12 4 CA980916026 1 19980906 A 2897 Q204M16 WIRE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE FUEL PANEL CHAFED W A UNSCHED LANDING G MULTIPLE FAILURE CL CLIMB 1 CA 517819 (CAN) AFTER TAKEOFF, THE GROUND REFUEL AND FUEL TANK FILL VALVE AND BATTERY BUS SENSING CIRCUIT BREAKERS TRIPPED. ALSO, BATTERY BUS OFF LIGHT CAME ON. BOTH CIRCUIT BREAKERS RESET AND TRIPPED AGAIN, AIRCRAFT RETURNED. FOUND WIRE CHAFED AT EXTERNAL REFUEL PANEL. REPAIRED. 2 L 7 3 4F 4 F A22WE E23EA 1998120400082 19981204 00082 NM 1998 12 4 CA980916027 1 19980908 A 2612 896767896768 FIRE LOOP KIDDE 896767 BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE APU BAY MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 10861160 688478 (CAN) SHORTLY AFTER TAKEOFF, APU FIRE WARNING LIGHT CAME ON AND BELL SOUNDED. APU SHUT DOWN. FIRE DRILL COMPLETED. FI RE LIGHT REMAINED ON AND FIRE BELL SOUNDED INTERMITTENTLY. AIRCRAFT RETURNED. REPLACED TAIL PIPE AND EXHAUST DUCT FIR E DETECTION LOOPS AS RESISTANCE WAS TOO LOW. 2 L 7 2 4F 4 F A16WE E2EA 1998120400083 19981204 00083 WP 1998 12 4 CA980916028 1 19980819 A 2612 355900575 FIRE LOOP CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL NR 2 ENGINE MALFUNCTIONED W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CA 501639 (CAN) DURING CRUISE, INTERMITTENT ZONE 2 WARNING LIGHT AND BELL (NR 2 ENG). LIGHT CONTROLLED BY REDUCING POWER. HOWEVE R, ON DESCENT, LIGHT AND BELL ILLUMINATED STEADY. ENGINE SHUTDOWN AND FIRE BOTTLES FIRED. BOTTLES AND SQUIBS REPLACED . RT ENG ZONE 2 FIRE LOOP REPLACED. 2 L 7 2 4R 4 T 6A6 E282 1998120400085 19981204 00085 EU 1998 12 4 CA980916031 1 19980918 A 2420 914F5696 GCU WESTINGHOUSE 976J2555 FOKKER F28 F28MK1000 4990808 EU NR 1 FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA YH1067 (CAN) ON APPROACH, COCKPIT FILLED WITH SMOKE AS THE NR 1 GCU WAS FAILING. ALSO, NR 1 GENERATOR TRIPPED OFF-LINE AT THI S TIME. THE CABIN REMAINED SMOKE FREE DURING DESCENT AND LANDING. INSPECTION REVEALED THAT NR 1 GCU SMOKED, GCU REPLAC ED, BUT ON GROUND RUN, THE GCU SMOKED AGAIN. NR 1 GENERATOR AND GCU REPLACED, AIRCRAFT SERVICEABLE. 2 L 7 2 4F RT A20EU 1998120400086 19981204 00086 EU 1998 12 4 CA980916033 1 19980906 A 4900 38075411 APU AIRESRCH 38075411 FOKKER F28 F28MK1000 4990808 EU TAIL SECTION FAILED W B A EMER. DESCENT UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 CA P37662 (CAN) SHORTLY AFTER TAKEOFF, THE LAVATORY SMOKE DETECTOR SOUNDED, EMERGENCY DECLARED. AIRCRAFT RETURNED AND OVERWEIGHT LANDING CARRIED OUT. HEAVY LANDING CHECK CARRIED OUT, ALL OK. REPLACED SMOKE DETECTOR. GROUND RUN SERVICEABLE. NEXT FLIGHT, SMOKE DETECTOR SOUNDED. AUXILIARY POWER UNIT AT FAULT. AIRCRAFT OPERATED UNDER MEL. APU TO BE REPLACED. 2 L 7 2 4F RT A20EU 1998120400087 19981204 00087 GL 1998 12 4 CA980916035 2 19980709 A 7250 6898735 NOZZLE HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL 1ST STAGE CRACKED W A UNSCHED LANDING J WARNING INDICATION HO HOVERING 1 CA 6313 795 CAT33907 CAE830901 (CAN) PILOT REPORTED TOT OF 813C FOR 6 SECONDS. INSPECTION FOUND THE TURBINE FIRST STAGE NOZZLE CRACKED AND ERODED ON 1 9 VANES. THE COMBUSTION LINER 980916051 WAS ALSO CRACKED. THE OVERTEMP IS NOT CONSIDERED THE SOURCE OF EITHER THE TURB INE OR COMBUSTION LINER DAMAGE. PART TC: 932. 1 G 7 1 3U 3 U H3WE E4CE 1998120400088 19981204 00088 EU 1998 12 4 CA980916036 1 19980709 A 6210 355A11002011 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 3898 78 6555 4432 (CAN) ON PRE-FLIGHT, VOID FOUND IN THE TIP OF THE BLADE. VOID IS 3 INCHES BY .25 INCH BY .25 INCH DEEP. 1 G 7 1 3U 3 U NC H9EU E19EU 1998120400089 19981204 00089 SW 1998 12 4 CA980916037 1 19980715 A 6410 206010777001 BLADE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 150 CAE820743 (CAN) TAIL ROTOR BLADE STATIC STOP BUMPER CUT THROUGH. THIS BLACK COLORED BUMPER IS MUCH THINNER THAN THE ORIGINAL ORAN GE/BROWN BELL MANUFACTURED BUMPER. 1 G 7 1 3U 3 U H2SW E4CE 1998120400090 19981204 00090 EU 1998 12 4 CA980916038 1 19980720 A 6220 704A33633156 SPHERICAL STOPS SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R HEAD BLISTERED W K NONE O OTHER IN INSP/MAINT 1 CA 748 4294 (CAN) MAIN ROTOR STARFLEX 3 SPHERICAL STOPS BLISTERED TO LIMITS. S/N 3403, S/N 4311, AND S/N 4419. 1 G 7 1 3U 3 U NC H9EU E19EU 1998120400091 19981204 00091 SW 1998 12 4 CA980916039 1 19980730 A 3411 206070547001 TUBE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL PITOT SYSTEM MELTED W K NONE O OTHER NR NOT REPORTED 1 CA CAE802078BA (CAN) AIRSPEED INDICATOR READING 30-40 KNOTS LOW IN CRUISE. TUBING FROM PITOT HEAD TO 'T' FITTING HAD A HOLE MELTED THR OUGH FROM PROXIMITY TO LANDING LIGHT. 1 G 7 1 3U 3 U H2SW E4CE 1998120400092 19981204 00092 EU 1998 12 4 CA980916040 1 19980523 A 6410 355A12004008 SPAR 355A12004008 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE T/R BLADE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 7031 451 (CAN) SUSPECT CRACKED SPAR. FLEXING OF BLADE PRODUCES SOUND OF CRACKED SPAR AND VISIBLE SPLINTERS SHOWING. SMALL CRACK S .3750 INCH LONG ON SIDES OF BLADES. 1 G 7 1 3U 3 U H9EU E19EU 1998120400093 19981204 00093 SW 1998 12 4 CA980916041 1 19980819 A 6730 212076004003 SERVO 212076004003 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA TAIL ROTOR WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 3432 479 CPPS61926 (CAN) SUBSEQUENT TO BELL ASB 212-98-103, TAIL SERVO INPUT LEVER FOUND TO BE UNAPPROVED PART AS DESCRIBED IN THE ASB. 1 G 7 1 4U 4 U H4SW E22EA 1998120400100 19981204 00100 NM 1998 12 4 CA980916053 1 19980730 A 5330 SKIN BOEING 737 737210C 1384459 NM PWA JT8 JT8D9A 52048 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 687721 (CAN) DURING PRESSURIZATION CHECK, A 4 INCH CRACK WAS DETECTED IN THE FUSELAGE SKIN AT R1 DOOR, FORWARD GALLEY, LOWER AF T CORNER. REPAIRED IAW SRM 53-30-3. 2 L 7 2 4F 4 F A16WE E2EA 1998120400101 19981204 00101 EU 1998 12 4 CA980916055 1 19980807 A 3244 TIRE BRAERO 748 HS7482B 1500248 EU MLG RUPTURED W O OTHER O OTHER TO TAKEOFF 1 CA (CAN) ON DEPARTURE, GROUND PERSONNEL REPORTED DEBRIS ON RUNWAY, AIRCRAFT MADE LOW PASS AND NR 2 POSITION TIRE APPEARED F LAT. AIRCRAFT LANDED AND NR 1 AND NR 2 WHEELS REPLACED. DIAMOND SHAPE SECTION OF RUBBER 18 BY 11 MISSING FROM TIRE. 2 L 7 2 3T A24EU 1998120400103 19981204 00103 WP 1998 12 4 CA980916062 1 19980908 A 3260 SENSOR LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE MLG LOOSE W J A DUMP FUEL UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CA 10491 (CAN) AFTER TAKEOFF AND GEAR SELECTED UP, DOOR INTRANSIT LIGHT REMAINED ON. FUEL DUMPED AND AIRCRAFT LANDED. RIGHT DOO R PROXIMITY SWITCH LOOSE, ADJUSTED AND TESTED SERVICEABLE. 2 L 7 3 4F 4 F A23WE E12EU 1998120400104 19981204 00104 NM 1998 12 4 CA980916063 1 19980907 A 3246 431276 BOLT BFGOODRICH 31428 BOEING 757 757236 NM RROYCE RB211 RB211535E4 54555 NE MLG SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 99 30864 (CAN) BOLT MISSING FROM NR 5 WHEEL ASSY. BOLT SHEARED AT THREADED PORTION. REST OF BOLT IN WHEEL. WHEEL REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1998120400105 19981204 00105 WP 1998 12 4 CA980916064 1 19980819 A 2160 VALVE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 3 PACK OVERHEATED W K NONE B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CA 10059 (CAN) ON FINAL APPROACH, NR 3 PACK FLOW CONTROL VALVE OVERHEAT LIGHT CAME ON. ON TOUCHDOWN, CABIN FILLED WITH SMOKE, PA CK WAS IN AUTOMODE. IN-FLIGHT FLOW BAR WAS CYCLING CONSTANTLY, BUT NO OVERHEAT OBSERVED. PACK FLOW CONTROL VALVE AND T URBINE BYPASS REPLACED AND OPERATIONAL CHECK OK. 2 L 7 3 4F 4 F A23WE E12EU 1998120400109 19981204 00109 SW 1998 12 4 CA980916068 1 19980901 A 6410 206310105101 BEARING 206016201131 BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL T/R BLADE LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 1687 CS5853 CAE895726 (CAN) ON DAILY INSPECTION, TAIL ROTOR BLADE OUTBOARD BEARING LOOSE AUXILIARY IN THE BLADE. PART TC: 1 G 7 1 3U 3 U NC H2SW E1GL 1998120400111 19981204 00111 SW 1998 12 4 CA980916070 1 19980902 A 6420 206011812005 TRUNNION 206011810153 BELL 206 206L 1181522 SW TAIL ROTOR BRINNELLED W K NONE O OTHER IN INSP/MAINT 1 CA 635 A006408 (CAN) DURING BLADE CHANGE, TRUNNION RACE BRINNELLED BEYOND LIMITS. 1 G 7 1 3U H2SW 1998120400112 19981204 00112 NE 1998 12 4 CA980916071 2 19980910 A 7311 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 11447 67 120324 (CAN) ON INSPECTION, OIL COOLER FOUND LEAKING. PART TC: 12,936. 2 H 7 2 4T 4 T RT A13NM E20NE 1998120400114 19981204 00114 SW 1998 12 4 CA980922004 1 19980912 A 6510 204040620003 DRIVESHAFT BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE TAIL ROTOR SHEARED W K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 CA LEO07256X (CAN) ON START-UP, ENGINEER NOTICED THAT TAIL ROTOR WAS NOT ACCELLERATING LIKE THE M/R. SECOND DRIVESHAFT AHEAD OF THE 42 DEGREES GEARBOX HAD SHEARED AT ABOUT MID-SPAN. 1 G 7 1 4U 4 U H1SW E17EA 1998120400115 19981204 00115 WP 1998 12 4 CA980922005 1 19980913 A 5244 369A20323 COVER 369A2032 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL STA 142 SEPARATED W O OTHER D INFLIGHT SEPARATION CR CRUISE 1 CA 8843 CAE832839 (CAN) IN CRUISE DURING A 40 MINUTE FLIGHT, PILOT FELT A THUMP IN PEDALS BUT NO BUZZ DEVELOPED. ON POST-FLIGHT INSPECTIO N, PILOT NOTICED BELLCRANK COVER MISSING AT STATION 142. THREE STUDS STILL IN PLACE. ONE TAIL ROTOR BLADE HAD A DENT BEYOND LIMITS. 1 G 7 1 3U 3 U H3WE E4CE 1998120400126 19981204 00126 SW 1998 12 4 CA980922022 1 19980416 A 6220 MS3569129 NUT 206010355009 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R HEAD CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10211 801799BA (CAN) PITCH CHANGE LINK ADJUSTER LOCKNUTS CRACKED ON MAGNETIC PARTICLE INSPECTION. SUBMITTER STATED THE VISUAL INSPECTI ON CALLED FOR IS NOT ADEQUATE FOR THE DEFECT FOUND HERE. 1 G 7 1 3U 3 U H2SW E4CE 1998120400132 19981204 00132 GL 1998 12 4 CA980928005 2 19980905 A 7321 DPVI25490923 FUEL CONTROL BENDIX SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL ENGINE FAULTY W E ENGINE SHUTDOWN J WARNING INDICATION IN INSP/MAINT 1 CA 334531 CAE890185S (CAN) ENGINE STARTED HOT AND DID NOT IMMEDIATELY SHUT DOWN WHEN THE THROTTLE WAS STOP COCKED. FUEL LEVER WAS STOP COCKE D AND 3-5 SECONDS LATER, THE ENGINE SHUT DOWN. THE FUEL CONTROL UNIT WAS FOUND FAULTY. 1 G 7 2 3U 3 U H1NE E1GL 1998120400135 19981204 00135 SO 1998 12 4 CA980928008 2 19980910 A 8530 CYLINDER CESSNA 402 402B 207590P CE CONT O520 TSIO520* 17040 SO NR 1 ENGINE FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 CA 20652871E (CAN) DURING CRUISE, THE NR 1 ENGINE BEGAN RUNNING ROUGH, AIRCRAFT RETURNED TO DEPARTURE POINT. POST-FLIGHT INSPECTION FOUND NO COMPRESSION ON NR 6 CYLINDER AND METAL WAS FOUND IN THE OIL FILTER. THE ENGINE WAS REPLACED AND THE AIRCRAFT WA S RETURNED TO SERVICE. 1 L 7 2 3O 3 O A7CE E8CE 1998120400136 19981204 00136 WP 1998 12 4 CA980928009 1 19980910 A 6123 O-RING CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13D 03004 GL ALLSN A6441 A6441FN606 GL NR 1 ENGINE DAMAGED W E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 501805 HC2425 (CAN) DURING CRUISE, THE NR 1 ENGINE EXPERIENCED AN RPM DROP, THE ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO POINT OF D EPARTURE. POST-FLIGHT INSPECTION FOUND A FEATHER RESERVOIR OIL TRANSFER O-RING PINCHED. THE O-RING WAS REPLACED AND TH E AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4R 4 T 6A6 E282 6 C P898 1998120400138 19981204 00138 EU 1998 12 4 CA980928011 1 19980916 A 3230 125753 SPRING DOWTY 2004270005 FOKKER F28 F28MK1000 4990808 EU UPLOCK BROKEN W O OTHER J WARNING INDICATION AP APPROACH 1 CA DRG325571 (CAN) ON APPROACH ON GEAR DOWN SELECTION, FIVE GREEN LIGHTS, BUT NO RT MLG DOOR DOOR LIGHT. GEAR CYCLED AND GOT SAME RE SULT, AIRCRAFT LANDED. FOUND RT GEAR DOOR UPLOCK SPRING BROKEN. REPLACED. 2 L 7 2 4F RT A20EU 1998120400140 19981204 00140 EU 1998 12 4 CA980928013 1 19980915 A 2910 112SS3568 PLUG HAWKER 9Q2277 BRAERO 748 HS7482A 4231001 EU HYD MANIFOLD CRACKED W A UNSCHED LANDING G K J MULTIPLE FAILURE FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) AFTER TAKEOFF, THE LANDING GEAR FAILED TO RETRACT WHEN SELECTED UP. AFTER THE UP SELECTION THE HYDRAULIC PRESSURE WAS SEEN TO FAIL. AIRCRAFT RETURNED TO BLOCKS. INVESTIGATION REVEALED THAT A MANIFOLD BLANKING PLUG HAD CRACKED UNDE R THE HEAD AND ALLOWED SYSTEM FLUID TO ESCAPE. NEW PLUG INSTALLED. 2 L 7 2 3T A24EU 1998120400141 19981204 00141 EU 1998 12 4 CA980928014 1 19980917 A 2910 24Q2395 LINE BRAERO 748 HS7482A 4231001 EU HYDRAULIC SYS CHAFED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 20290 (CAN) DURING FLIGHT, THE PORT HYDRAULIC FLOW LIGHT CAME ON FOLLOWED BY THE STANDBY LIGHT. EMERGENCY DECLARED AND A SAFE LANDING CARRIED OUT. PORT HYDRAULIC PUMP LINE CHAFED THROUGH ON THE EDGE OF THE GENERATOR BRUSH COVER ALLOWING A MASSI VE HYDRAULIC LEAK. REPLACED. PART TC: 21,649. 2 L 7 2 3T A24EU 1998120400143 19981204 00143 EU 1998 12 4 CA980928017 1 19980916 A 6420 60102RS1MT33CA BEARING 350A33200405 SNIAS 350 AS350B2 8680813 EU PITCH CHANGE FAILED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 6427 190 M166 (CAN) IN CRUISE, VIBRATION AND A GROWLING NOISE FELT IN THE HELO. ABNORMAL AXIAL PLAY IN THE TAIL ROTOR PITCH CHANGE BE ARING ASSY. BEARING ROUGH. AS350 IPC 65.20.30 FIG 1B ITEM 70 AND 65.20.10 FIG. 1 ITEM 30C. 1 G 7 1 3U H9EU 1998120400147 19981204 00147 NM 1998 12 4 CA980928021 1 19980827 A 2810 FUEL CAP AIRBUS A319 A319114 NM FUEL SYSTEM MISSING W O OTHER K FLUID LOSS CR CRUISE 1 CA (CAN) PASSENGER REPORTED THAT A FUEL CAP WAS FLAPPING. CAP REPLACED. 2 L 7 2 4F RT A28NM 1998120400148 19981204 00148 EU 1998 12 4 CA980928026 1 19980828 A 2722 810A000003 SERVO AIRBUS 320 A320211 3930320 EU RUDDER MALFUNCTIONED W O OTHER K E FLUID LOSS VIBRATION/BUFFET CL CLIMB 1 CA 19184 (CAN) VERY HIGH VIBRATION IN AFT CABIN ON CLIMB OUT FOR ABOUT 30 SECONDS. GREEN SYSTEM RUDDER SERVO REPLACED. PART TC: 8,813. 2 L 7 2 4F RT A28NM 1998120400149 19981204 00149 EU 1998 12 4 CA980928027 1 19980830 A 3240 VALVE AIRBUS 320 A320211 3930320 EU NR 4 WHEEL FAILED W O OTHER K FLUID LOSS LD LANDING 1 CA (CAN) ON LANDING AFTER MAIN LANDING GEAR TOUCHED DOWN, NR 4 WHEEL TIRE BLEW AND NR 3 DAMAGED. RT SIDE BRAKES LOCKED. A IRCRAFT TAXIED TO GATE. REPLACED NORMAL AND ALTERNATE SAFETY VALVE, NR 4 BRAKE CARRIER AND NR 3 AND NR 4 MAIN WHEELS, S YSTEM BLED OK. 2 L 7 2 4F RT A28NM 1998120400150 19981204 00150 EU 1998 12 4 CA980928028 1 19980826 A 4930 38832406 BOLT AIRBUS A340 A340313 EU FCU LOOSE W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) 1.5 HOURS AFTER LANDING, SMOKE WAS SEEN COMING FROM THE AUXILIARY POWER UNIT. THE APU WAS SELECTED OFF FROM THE C OCKPIT. INSPECTION FOUND FUEL IN THE APU OIL TANK AND EVIDENCE OF BURNING AT THE EXHAUST MUFFLER. FURTHER INSPECTION F OUND A FCU BOLT HAD BACKED OFF. THE FCU WAS REPLACED AND THE FILTERS WERE REPLACED. THE APU WAS GROUND RUN SERVICEABLE . 2 L 7 4 4F RT A197 1998120400158 19981204 00158 SW 1998 12 4 CA980930001 1 19980923 A 6220 212011112103 BEARING 205812001103 BELL 205 205A1 1181414 SW LYC T53 T5317A 41549 NE MAIN ROTOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 1538 ABG8989 LEO7664C (CAN) ON PURGING GREASE FROM MAIN ROTOR GRIPS, OUTGOING GREASE WAS BROWNISH IN COLOR. ON DISASSEMBLY, BEARING CAGE WEAR ING ON THE INNER RACE. BEARING REPLACED. 1 G 7 1 4U 4 U H1SW E17EA 1998120400159 19981204 00159 EU 1998 12 4 CA980930002 1 19980922 A 6420 350A33200403 SPIDER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 923 MA0528 4002 (CAN) ON PRE-FLIGHT, EXCESSIVE AXIAL PLAY BETWEEN STATIONARY AND ROTATING PARTS OF THE TAIL ROTOR SPIDER ASSY. ON DISAS SEMBLY OF THE SPIDER, 'GRAPHOIL' COATING THAT GOES BETWEEN THE INNER RACE OF THE BEARING AND THE ROTATING SPIDER WAS SOF T AND DEGRADED WHICH ALLOWED THE INNER RACE TO MOVE ON THE SHAFT. 1 G 7 1 3U 3 U H9EU E19EU 1998120400163 19981204 00163 SO 1998 12 4 CA980930007 1 19980612 A 2997 WIRE PIPER PA31 PA31350 7103110 SO HYD POWER PACK BROKEN W D RETURN TO BLOCK O OTHER CL CLIMB 1 CA (CAN) LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. WIRE FOUND BROKEN AT THE HYDRAULIC POWER PACK MICROSWITCH. 1 L 7 2 3O A20SO 1998120400172 19981204 00172 EA 1998 12 4 CA980930023 2 19980921 A 7414 4371 MAGNETO SLICK PARTEN P68 P68C 6780105 EU LYC O360 IO360A1B6 41514 EA LT MAG MALFUNCTIONED W O OTHER O OTHER NR NOT REPORTED 1 CA 521 85080008 L2370951A (CAN) LEFT HAND MAGNETO HAD ERRATIC MAG DROP. 1 H 7 2 3O 3 O A31EU 1E10 1998120400178 19981204 00178 NM 1998 12 4 TWAA9818901 1 19981122 A 3350 58225 BATTERY PACK BOEING 727 727231 1384079 NM EMER EXIT ROW DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 54354 21986 DURING CRUISE, EMERGENCY EXIT ROW LIGHTS AND FLOOR LIGHTS FLICKER ON-OFF. RECHARGED EGRESS POWER SUPPLIES. 2 L 7 3 4F A3WE 1998120400179 19981204 00179 WP 1998 12 4 TWAA9818903 1 19981122 A 3350 58222 POWER SUPPLY DOUG DC9 DC982 3022082 WP ROW 2-5 INOP A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 911TW 49182 DURING PREFLIGHT INSPECTION, FOUND EGRESS LIGHTS INOP BETWEEN ROWS 2 TO 15. REPLACED POWER SUPPLY. 2 L 7 2 4F A6WE 1998120400180 19981204 00180 WP 1998 12 4 TWAA9818904 1 19981123 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 2-15 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 922TW 48013 DURING PREFLIGHT, FOUND EGRESS LIGHTING INOP BETWEEN ROWS 2 TO 15. REPLACED NR 2 EGRESS BATTERY PACK. 2 L 7 2 4F A6WE 1998120400181 19981204 00181 WP 1998 12 4 TWAA9818905 1 19981124 A 2530 50226MFGNR OVEN DOUG DC9 DC982 3022082 WP GALLEY FAILED A TWAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CE 05 952U 49266 DURING DESCENT, SMOKE IN FIRST CLASS CABIN. REPLACED GALLEY OVEN. 2 L 7 2 4F A6WE 1998120400182 19981204 00182 WP 1998 12 4 TWAA9818906 1 19981124 A 3350 0105607001 LENSE DOUG DC9 DC983 3022083 WP ROW 3-29 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9413T 53188 PARKED AT THE GATE IT WAS NOTED THAT THE EMERGENCY EGRESS LIGHT SYSTEM TRACK COVER/LENSE WAS DAMAGED AT ROWS 3 AND 29. R EMOVED AND REPLACED LIGHT COVER/LENSE. 2 L 7 2 4F RT A6WE 1998120400183 19981204 00183 WP 1998 12 4 TWAA9819802 1 19981201 A 3350 LIGHT DOUG DC9 DC983 3022083 WP ROW 15 INOP A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 EIBWD 49575 TWO OF THE FORWARD RED EMERGENCY EGRESS FLOOR LIGHTS WERE INOPERATIVE AT THE FORWARD END, AND ONE LIGHT AT ROW 15 WAS IN OPERATIVE. RESEATED CONNECTORS AND BULBS AT FWD RED FLOOR EGRESS LIGHTS, AND RESEATED EGRESS LIGHT BULB AT ROW 15. CHE CK-C 2-6-98 MCI. 2 L 7 2 4F RT A6WE 1998120400184 19981204 00184 NM 1998 12 4 AWXA9800223 1 19981120 A 2120 AIR DISTRIBUTION BOEING 737 737277 1384570 NM COCKPIT ODOR A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 WP 28 189AW 22656 D-SMELLED RAW EXHAUST IN COCKPINT AND F/C CABIN ON FINAL. SHUT OFF NR 2 ON TAXI AND POWERED NR 1 TO 1.3 EPR, SMELLED EX HAUST AGAIN. RAN APU IN HIGH HEAT ON LEFT PACK NORMAL ODORS. GOOD HEAT INSIDE AND OUT OF A/C. CHECKED BOTH PACK ACM O IL AND TURBO FAN OIL OK INSPECTED INLETS AND EXHAUST OF ENGINE CHECK OK NO OIL. RAN ENGINES AND NO OIL SMELL IN CABIN. OK FOR SERVICE. 2 L 7 2 4F RT A16WE 1998120400185 19981204 00185 NM 1998 12 4 AWXA9800225 1 19981124 A 3350 2TC475 CIRCUIT BREAKER BOEING 757 7572G7 1384963 NM COCKPIT FAILED A AWXA K NONE O OTHER CL CLIMB 1 WP 28 910AW 24523 AFTER TAKEOFF INFLIGHT CREW REPORTED EMERGENCY EXIT LIGHTS ILLUMINATED. FLIGHT DECK SWITCH MOVED FROM ON TO OFF AND BAC K TO ARMED, LIGHTS REMAINED ILLUMINATED. REPLACED BATTERY PACKS M9001, M731, M735, M9002 AND M737 AND FOUND CHARGING CB TO BE FAULTY, REPLACED CB. OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A2NM 1998120400186 19981204 00186 EU 1998 12 4 AWXA9800226 1 19981126 A 2916 S43500272 MANIFOLD AIRBUS 320 A320231 3930325 EU YELLOW HYD SYST CRACKED A AWXA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 WP 28 643AW 18448 18448 315 LOST YELLOW HYDRAULIC QUANTITY AND SYSTEM LOST AFTER GEAR RETRACTION. REPLACED GROUND LEAKAGE MEASUREMENT MANIFOLD OF Y ELLOW HYD SYSTEM PER MM, OPS AND LEAK CK GOOD. 2 L 7 2 4F RT A28NM 1998120400187 19981204 00187 NM 1998 12 4 CALA9802103 1 19981124 A 2612 89931505 MODULE BOEING 737 7373T0 1384582 NM E & E COMPT INOP A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14337 31168 23575 THE FIRE WARNING LIGHT AND BELL ACTIVATED WHILE ON SHORT FINAL INTO EWR. THE WARNING WAS ON THE GLARESHIELD WITH NO IND ICATIONS IN T-HANDLE ON THROTTLE CONSOLE. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE O F FIRE. MAINTENANCE FOUND THE FIRE DETECTION MODULE AT FAULT. THE MODULE WAS REMOVED AND REPLACED. BITE CHECK WAS GOO D WITH NO OTHER DEFECTS NOTED. 2 L 7 2 4F RT A16WE 1998120400188 19981204 00188 NM 1998 12 4 CALA9802104 1 19981124 A 5754 CHORD BOEING 727 727243 138408D NM NR 3 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 2.25 INCH CRACK IN LT WING NR 3 SLAT AT LOWER CHORD BELOW OUTBOARD STOP PAD. THE CHORD WAS REMOVED A ND A NEW CHORD WAS INSTALLED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 1998120400189 19981204 00189 WP 1998 12 4 CALA9802105 1 19981124 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58545 47094 A DENT WAS FOUND IN RT FUSELAGE SKIN FOURTEEN INCHES FORWARD OF AFT BAG BIN DOOR. THE SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 12B. 2 L 7 2 4F A6WE 1998120400190 19981204 00190 WP 1998 12 4 CALA9802106 1 19981124 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58545 47094 A DENT WAS FOUND IN RT FUSELAGE SKIN AFT OF R-1 SERVICE DOOR. THE DENTED AREA WAS CUT OUT. A REPAIR DOUBLER WAS INSTAL LED IAW SRM 53-04, FIGURE 12A AND 12B AND SRM 51-10-3. 2 L 7 2 4F A6WE 1998120400191 19981204 00191 WP 1998 12 4 CALA9802107 1 19981124 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1098-1193 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND LT INBOARD SEAT TRACK CORRODED AT CLIP NUT, STA 1098-1193. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4F, PAGE 10Q. 2 L 7 2 4F A6WE 1998120400192 19981204 00192 WP 1998 12 4 CALA9802108 1 19981124 A 5315 FLOORBEAM DOUG DC9 DC982 3022082 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND CORROSION UNDER NUT PLATE ON FLOORBEAM AT STA 218 LBL 54, UNDER FORWARD LAV FLOOR PANEL. A REPAIR DOUB LER WAS INSTALLED IAW SRM 53-05, FIGURE 20A. 2 L 7 2 4F A6WE 1998120400193 19981204 00193 EA 1998 12 4 COMA9860364 1 19981124 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA ROW 10 FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 934CA 7042 OVERHEAD EMERGENCY LIGHT AT ROW 10 IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1998120400194 19981204 00194 NM 1998 12 4 QXEA9801752 1 19981123 A 2611 819 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM CARGO COMPT MALFUNCTIONED A QXEA K NONE N FALSE WARNING UK UNKNOWN 1 NM 09 366PH 39 520 SEA - SMOKE LIGHT CAME ON INTERMITTENTLY 4 TIMES. VISUALLY DETECTED NO SMOKE IN THE CARGO COMPARTMENT. MAINTENANCE PLA CED THE THE SMOKE DETECTOR ON MEL NR 226150. MEL CLEARED BY REPLACING THE NR 2 SMOKE DETECTOR. OPERATIONAL CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998120400195 19981204 00195 1998 12 4 QXEA9801753 4 19981123 A 3451 6224298001 HSI FOKKER F28 F28MK4000 4990810 EU NR 1 FAILED A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 488US 1062 11240 YYC - PILOT REPORTS NR 1 DME DISPLAY ON CAPTAINS HSI FAILED. NR 1 DME INFORMATION ON FIRST OFFICERS DME REPEATER REMAIN ED NORMAL. NR 1 DME XCVR CIRCUIT BREAKER POPED. ACRID SMELL NOTED IN COCKPIT. BOTH DME'S FAILED. MAINTENANCE CAPPED AND STOWED CANNON PLUGS FOR THE NR 1 HSI. AIRCRAFT FERRIED TO SEA. SEA MAINTENANCE REPLACED THE NR 1 HSI, UNABLE TO CO MPLETE OPERATIONAL TESTS DUE TO SEA-TAC DME INOPERATIVE. AIRCRAFT REMAINS CAT I. 2 L 7 2 4F RT A20EU 1998120400196 19981204 00196 EU 1998 12 4 98FDEA00714 1 19981125 A 7931 648804191 INDICATOR AIRBUS 310 A310222 3930315 EU NR 1 ENGINE FAILED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 421FE 342 98-0286, NR 1 ENG OIL INDICATORS DECREASED TO 0 AT FL350, BOTH ECAM AND ANALOG. REMOVED AND REPLACED ENGINE OIL QTY DUA L INDICATOR. 2 L 7 2 4F RT A35EU 1998120400197 19981204 00197 WP 1998 12 4 MWEA981111 1 19981123 A 2560 11320 LATCH DOUG DC9 DC932 3022066 WP GIRT BAR MALFUNCTIONED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 MKE - FLT 417 - THE GIRT BAR WOULD NOT FIT IN PLACE. MAINTENANCE REPLACED AFT GIRT BAR LATCH. (M) 2 L 7 2 4F A6WE 1998120400198 19981204 00198 NM 1998 12 4 DHL98702004 1 19981126 A 3020 652673826 DUCT BOEING 727 72730C 1384009 NM NR 3 ENGINE BLOWN A DHLA A E F J UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 01 702DH 19793 ENGINE FIRE WARNING ON NR 3 ENGINE ON CLIMB-OUT AT 4000 FT. FOUND NOSE COWL ANTI-ICE PIPE BLOWN. REPLACED PER MM 75-1 0-0. 2 L 7 3 4F A3WE 1998120400199 19981204 00199 WP 1998 12 4 ARWA981130 1 19981124 A 3231 CONTROL CABLE DOUG DC8 DC862 3021970 WP LT MLG DOOR BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 8968U 46069 LT MLG DOOR UPLOCK FOLLOW UP CABLE BROKEN. FABRICATED CABLE AS PER SAMPLE IAW DACO M/M 91-10-42. OPERATION CHECKED NOR MAL IAW M/M 32-12-1. 2 L 7 4 4F 4A25 1998120400200 19981204 00200 NM 1998 12 4 CKSA98710 1 19981124 A 2121 5007024620 FAN BOEING 727 72722C 138400F NM FUSELAGE BURNT A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 23 727CK 19195 SMELLED SMOKE COMING FROM THE GASPERS. REMOVED AND REPLACED GASPER FAN IAW 727 MM CH 21-50-36. OPS CHECK GOOD ON GROUN D. 2 L 7 3 4F A3WE 1998120400201 19981204 00201 NM 1998 12 4 TWAA9819001 1 19981125 A 3350 767 BULB BOEING 767 7673Q8 NM EXTERIOR FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 635TW 28207 FOUND TWO EMERGENCY LIGHTS INOPERATIVE AFT OF RT WING, ONE AFT OF LT WING, AND ONE AFT OF R1 DOOR. REPLACED BULBS IN E ACH. CHECK-C 10-07-98 LAX. 2 L 7 2 4F RT A1NM 1998120400202 19981204 00202 NM 1998 12 4 TWAA9819002 1 19981127 A 3397 WIRE BOEING 757 7572Q8 1384972 NM CABIN LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 704X 28163 FOUND FIRST CLASS FLOOR EGRESS LIGHT STRIP INOPERATIVE. FOUND STRIP UNPLUGGED. SECURED CABLE. CHECK-C 7-19-98 LAX. 2 L 7 2 4F RT A2NM 1998120400203 19981204 00203 WP 1998 12 4 TWAA9819003 1 19981127 A 3350 0105601003PA57 COVER DOUG DC9 DC983 3022083 WP CABIN MISSING A TWAA K NONE O OTHER NR NOT REPORTED 1 CE 05 9404V 53140 FOUND EGRESS LIGHT COVER MISSING. REPLACED COVER AND LAMP, (P/N 7732). CHECK-C 11-12-98 STL. 2 L 7 2 4F RT A6WE 1998120400204 19981204 00204 WP 1998 12 4 TWAA9819004 1 19981129 A 3350 41B030CF00101 BATTERY PACK DOUG DC9 DC983 3022083 WP EMER EXIT DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9401W 53137 FOUND OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK. CHECK-C 12-16-97. 2 L 7 2 4F RT A6WE 1998120400205 19981204 00205 WP 1998 12 4 TWAA9819005 1 19981129 A 3397 A054984 WIRE DOUG DC9 DC983 3022083 WP ROW 17 WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9413T 53188 FOUND EMERGENCY EGRESS LIGHT COVER STRIP MISSING AT CABIN ROW 17. REPLACED COVER (P/N 5778-1), AND LIGHT CABLE. CHECK -C 9-1-98 STL. 2 L 7 2 4F RT A6WE 1998120400206 19981204 00206 WP 1998 12 4 TWAA9819006 1 19981120 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 1097 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 985Z 47491 DURING CHECK-C MAINT, FOUND DORSAL FIN TO FUSELAGE ATTACH ANGLE CRACKED ON RT SIDE AT STA 1097, APPROX 1.5 INCH LONG IN RADIUS. CRACK WAS STOP DRILLED AND CRACK CONTAINMENT VERIFIED BY NDT. ANGLE WAS REPAIRED PER SRM 53-05, FIG 23. 2 L 7 2 4F A6WE 1998120400207 19981204 00207 WP 1998 12 4 TWAA9819007 1 19981124 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1130-1133 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 9303K 49529 DURING OP 15 MAINT CHECK, FOUND CORROSION REMOVAL MATERIAL LOSS AT LT O/B CHAIR TRACK LBL 51, STA 1130 TO 1133. REMOVED DAMAGED PART AND RE-INSTALLED NEW PART PER TWA STD PROCESS MANUAL 6-70-01, PG 3 ITEM B. 2 L 7 2 4F RT A6WE 1998120400208 19981204 00208 NM 1998 12 4 HNAA9893084 1 19981129 A 5210 STOP DHAV DHC8 DHC8102 2809003 NM PASSENGER DOOR OUT OF ADJUST A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 930HA 126 DCA - FLT 3159 - UNABLE TO OPEN PASSENGER DOOR FROM INSIDE. FOUND LOWER DOOR SKIN RUBBING. ADDED SHIMS AND ADJUSTED AL L DOOR STOPS. PRESSURIZED AIRCRAFT. OPERATIONAL AND LEAK CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998120400209 19981204 00209 NM 1998 12 4 HNAA9893685 1 19981129 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 1 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 936HA 145 ORF - NR 1 NACELLE EXHAUST FINGERNAIL IS CRACKED AT THE OUTBOARD FORWARD SIDE SKIN AND HAS SEVERAL LOOSE RIVETS AND MISS ING RIVETS AT THE TOP FORWARD SKIN. REPAIRED CRACKED SKIN AND REPLACED RIVETS. (M) 2 H 7 2 4T RT A13NM 1998120400210 19981204 00210 NM 1998 12 4 HNAA9893786 1 19981128 A 5411 FRAME DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 937HA 148 SBY - NR 2 NACELLE OUTBOARD MAIN OUTBOARD MAIN FRAME 'Z' MEMBER CRACKED AT UPPER END. STOP DRILLED CRACK AND INSTALLED RIVETS THROUGH 'Z' MEMBER, LANDING GEAR MAIN FRAME AND SKIN. (M) 2 H 7 2 4T RT A13NM 1998120400211 19981204 00211 1998 12 4 MALA976250 4 19981125 A 2565 D31050105 SLIDE BAC 146 AVRO146RJ85A 1500097 EU PAX DOOR DEPLOYED A MALA K NONE O OTHER NR NOT REPORTED 1 GL 15 502XJ E2307 MAIN CABIN DOOR EMERGENCY SLIDE PARTIALLY DEPLOYED. MAINTENANCE REPLACED FORWARD PASSENGER DOOR SLIDE. ALL CHECKS GOOD . 2 H 7 4 4F RT A49EU 1998120400212 19981204 00212 EU 1998 12 4 MALA976251 1 19981125 A 2611 CONNECTOR SAAB SF340 340B 7860101 EU CARGO COMPT LOOSE A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 9CJ 224 CARGO SMOKE DETECTOR DID NOT TEST. MAINTENANCE FOUND CONNECTOR PLUG LOOSE. INSTALLED PLUG AND TESTED SYSTEM, CHECKS GO OD. 2 L 7 2 4T RT A52EU 1998120400213 19981204 00213 EU 1998 12 4 MALA976252 1 19981125 A 3020 ND0075200 CONTROLLER SAAB SF340 340B 7860101 EU LT NACELLE INTERNAL FAULT A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 592MA 340B199 DURING FLIGHT, THE LEFT INTAKE ILLUMINATED AT 4 SECONDS AFTER ENGINE ANTI-ICE SWITCHED ON OR WHEN RESETTING LEFT INTAKE CIRCUIT BREAKER. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED LEFT THERMAL CONTROLLER, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998120400214 19981204 00214 EU 1998 12 4 MALA976253 1 19981125 A 3350 OL307115 BULB SAAB SF340 SF340A 7850100 EU CABIN FAILED A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 110XJ 340A110 DURING INSPECTION, EMERGENCY EXIT SIGN AT SEAT 1A INOP. MAINTENANCE RELAMPED, ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998120400215 19981204 00215 SO 1998 12 4 RAAA98E4024 1 19981123 A 3350 S102 BATTERY PACK GRIMES 1000553 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 AFT RT EMERGENCY EXIT PULL DOWN EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998120400216 19981204 00216 NM 1998 12 4 RAAA98B1095 1 19981128 A 5330 SKIN BOEING 727 72722C 138400F NM BS 542 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SCHEDULED B2 INSPECTION PER CARD B1 51001, FOUND BS 542 FUSELAGE SKIN CORRODED AROUND ANTENNA DOUBLER BLANK BETWE EN STR 28L AND 28R. REPAIRED PER SRM 53-30-3 FIG 1, M-54 NR 068. 2 L 7 3 4F A3WE 1998120400217 19981204 00217 NM 1998 12 4 RAAA98B1096 1 19981128 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT FWD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998120400218 19981204 00218 SO 1998 12 4 RAAA98E4025 1 19981125 A 3350 8621006 BATTERY PACK INTVLV 873100112 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 9744C 188C1140 PAX ROW 14 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998120400219 19981204 00219 SO 1998 12 4 RAAA98E9037 1 19981125 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998120400220 19981204 00220 WP 1998 12 4 CALA9802110 1 19981126 A 3260 833702 SENSOR DOUG DC9 DC982 3022082 WP NLG INOP A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 35888 49117 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION DEPARTING EWR. THE UNSAFE LIGHT WAS ACCOMPANI ED BY AIR NOISE INDICATIVE OF THE NOSE GEAR NOT BEING RETRACTED. THE GEAR WAS RECYCLED AND GEAR SAFE WAS INDICATED. TH E AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SENSOR AT FAULT. THE NOSE GEAR DOWNLOCK S ENSOR WAS REPLACED AND ADJUSTED IAW MM 32-60-05. IN ADDITION, A FULL NOSE STRUT SERVICE WAS PERFORMED IAW MM 32-21-02. A NOSE GEAR SWING WAS PERFORMED WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F A6WE 1998120400221 19981204 00221 NM 1998 12 4 CALA9802111 1 19981125 A 2782 BRACKET BOEING 727 727243 138408D NM NR 2 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 1 INCH CRACK IN I/B AND O/B BRACKETS AT LT WING NR 2 LE FLAP ACTUATOR MOUNT. THE BRACKETS WERE REMOV ED AND NEW BRACKETS WERE INSTALLED IAW SRM 51-30-2, FIGURE 1. 2 L 7 3 4F RT A3WE 1998120400222 19981204 00222 WP 1998 12 4 CALA9802112 1 19981125 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 503 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND TWO 1 INCH CRACKS IN FRAME AT LONGERON 6R AND A 1 INCH CRACK IN FRAME AT LONGERON 6L, STA 503. FRAME R EPAIRS WERE INSTALLED IAW SRM 53-03, FIGURE 32. 2 L 7 2 4F A6WE 1998120400223 19981204 00223 WP 1998 12 4 CALA9802113 1 19981125 A 5210 BEAM DOUG DC9 DC982 3022082 WP CABIN DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 1.25 INCH CRACK IN MAIN CABIN DOOR LOWER HORIZONTAL BEAM. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-0. 2 L 7 2 4F A6WE 1998120400224 19981204 00224 WP 1998 12 4 CALA9802114 1 19981128 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1079-1212 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND SECOND SEAT TRACK FROM OUTBOARD CORRODED AROUND ALL CAP NUTS AT STA 1079 TO 1212. THE SEAT TRACK WAS R EMOVED AND REPLACED IAW SRM 53-05. 2 L 7 2 4F A6WE 1998120400225 19981204 00225 WP 1998 12 4 CALA9802115 1 19981125 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 237-249 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 INSPECTION FOUND DENTS IN FUSELAGE SKIN FROM STA 237 TO 249 BETWEEN LONGERONS 16L AND 17L AND. ALSO, THE SKIN WAS BULGIN G AROUND FASTENERS AT STA 237 TO 269, LONGERONS 17L AND 18L. A FLUSH REPAIR WAS ACCOMPLISHED AT THE DENTED AREA IAW ECR A 5330-02445. THE LONGERONS WERE REPAIRED IAW SRM 53-02. 2 L 7 2 4F A6WE 1998120400226 19981204 00226 NM 1998 12 4 CALA9802116 1 19981125 A 3350 S106 BATTERIES AEROQUALITY BOEING 727 727224 1384076 NM R-1 DOOR DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 32725 20655 THE R-1 DOOR INTERIOR OVERHEAD LIGHT WOULD NOT TEST. THE BATTERIES WERE REPLACED IAW MM 33-50-101 AND OPERATION CHECKED GOOD. 2 L 7 3 4F A3WE 1998120400227 19981204 00227 WP 1998 12 4 CALA9802117 1 19981129 A 5532 PANEL DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58545 47094 INSPECTION FOUND A 4 INCH CRACK IN RT LOWER VERTICAL STABILIZER SLIDING PANEL. A REPAIR DOUBLER WAS INSTALLED IAW SRM 5 5-01 FIGURE 2, 51-10-2A, 51-10-4, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1998120400228 19981204 00228 WP 1998 12 4 CALA9802118 1 19981129 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 676 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 58545 47094 INSPECTION FOUND FUSELAGE SKIN CORRODED UNDER KEEL BEAM AREA AT BS 676, LONGERON 30. A PERMANENT REPAIR DOUBLER AND FIL LER WERE INSTALLED IAW ENGINEERING ORDER 07512 AND SRM 53-04, FIGURE 38, SHEET 3. 2 L 7 2 4F A6WE 1998120400229 19981204 00229 WP 1998 12 4 CALA9802119 1 19981129 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 712 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND TWO 1 INCH CRACKS IN BELTFRAME AT STA 712 LONGERON 6L AND TWO 1 INCH CRACKS WERE FOUND IN BELTFRAME AT STA 712 LONGERON 6R. THE BELTFRAME WAS REMOVED AND REPLACED FROM LONGERON 7L TO 7R IAW SRM 53-03, FIGURE 32. 2 L 7 2 4F A6WE 1998120400230 19981204 00230 WP 1998 12 4 CALA9802120 1 19981130 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 1117 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND LT OUTBOARD SEAT TRACK FORWARD OF AFT SERVICE DOOR AT STA 1117 CORRODED. THE SEAT TRACK WAS REMOVED AN D REPLACED IAW SRM 51-30-1. 2 L 7 2 4F A6WE 1998120400231 19981204 00231 SO 1998 12 4 COMA9810271 1 19981128 A 3150 WARNING EMB 120 EMB120RT SO FUEL SYST ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 269CA 120263 FUEL WARNING ON MAP DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T RT A31SO 1998120400232 19981204 00232 EA 1998 12 4 COMA9860365 1 19981121 A 2750 601R93106503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT WING CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7027 RIGHT WING NR 5 FLAP FLEXSHAFT IS HEAVILY CORRODED. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998120400233 19981204 00233 EA 1998 12 4 COMA9860366 1 19981122 A 2730 10231007 DAMPENER CNDAIR CL600 CL6002B19 EA RT ELEVATOR LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 2721 7027 RIGHT ELEVATOR OUTBOARD FLUTTER DAMPENER LEAKING OUT OF LIMITS. REPLACED DAMPENER. 2 L 7 2 4F RT A21EA 1998120400234 19981204 00234 EA 1998 12 4 COMA9860367 1 19981121 A 4950 320207221 VALVE CNDAIR CL600 CL6002B19 EA APU WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 7752 7027 APU AIR SUPPLY CHECK VALVE WORN AND FALLING OUT. REPLACED VALVE. 2 L 7 2 4F RT A21EA 1998120400235 19981204 00235 EA 1998 12 4 COMA9860368 1 19981121 A 2750 601R93016103 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT WING SEPERATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 10343 7027 RIGHT WING NR 1 FLEXSHAFT HAS STRAND SEPARATION. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998120400236 19981204 00236 EA 1998 12 4 COMA9860369 1 19981124 A 3610 979981 VALVE CNDAIR CL600 CL6002B19 EA RT ENGINE STUCK A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 926CA 6606 7027 RIGHT ENGINE 10TH STAGE ISOLATION VALVE STUCK PARITALLY OPEN. REPLACED VALVE. 2 L 7 2 4F RT A21EA 1998120400237 19981204 00237 NM 1998 12 4 QXEA9801754 1 19981128 A 3350 50309008 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 811PH 2496 457 23 LEFT FORWARD FUSELAGE EMERGENCY LIGHT INOP. REPLACED BATTERY FOR EMERGENCY LIGHTING, OPERATION CHECK GOOD. 2 H 7 2 4T RT A13NM 1998120400238 19981204 00238 NM 1998 12 4 QXEA9801755 1 19981126 A 3350 CONNECTOR DHAV DHC8 DHC8102 2809003 NM CABIN BROKEN A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 828PH 287 FORWARD END OF NR 3 AND NR 4 EMERGENCY TRACK LIGHTING INOP. FOUND BROKEN PLUG CONNECTOR 3352-J3. APPLIED INTERIM REPAI R, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998120400239 19981204 00239 WP 1998 12 4 98FDEA00715 1 19981119 A 3241 CONTROL DOUG DC10 DC1030F 3023504 WP LT MLG INOP A FDEA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 SO 25 321FE 47836 NR 5 BRAKE TEMP 150 DEG, LEFT GEAR DOWN. REMOVED AND REPLACED NR 5 BRAKE ASSY TEMP SENSOR AND ANTISKID CONTROL UNIT, PE RF BITE TEST. 2 L 7 3 4F RT A22WE 1998120400240 19981204 00240 1998 12 4 98FDEA00716 4 19981130 A 2297 WIRE DOUG MD11 MD11F 3023600 NM AUTO FLIGHT SYST CHAFED A FDEA D RETURN TO BLOCK G MULTIPLE FAILURE CL CLIMB 1 SO 25 614FE 48528 DEFECTIVE AUTO PILOT, AUTOTHROTTLES, FLIGHT DIR SYS, TAT PROBE HEAT, FLAPS ALERT, PRESS, AVIONICS FAN, TRANSPONDER, AUTO BRAKE. FOUND DEFECT CAUSE BY CHAFING AND SHORTING OF THREE WIRES. 2 L 7 3 4F RT A22WE 1998120400241 19981204 00241 NM 1998 12 4 98FDEA00717 1 19981125 A 2420 902F2832 BUS PANEL BOEING 727 72725 1384006 NM E & E COMPT FAILED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 503FE 18273 SMELLED FUMES IN COCKPIT. REPLACED CIRCUIT BREAKER, REMOVED AND REPLACED BUS PROTECTION PANEL, PERF OPER CKS PER MM 24- 20-0 AND ALL CKS GOOD. NO OTHER PROBLEMS. 2 L 7 3 4F A3WE 1998120400242 19981204 00242 EU 1998 12 4 98FDEA00718 1 19981128 A 3297 WIRE AIRBUS 300 A300F4605R 3930327 EU LANDING GEAR CUT A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 656FE 745 LANDING GEAR WOULD NOT RETRACT ON T/O. TRIED SYS 2 WITH NO EFFECT. SEV COCKPIT ITEM NOT WORK, SUSP RELAY SWITCH. REMO VED 400VU PNL ON CTR INSTRUMENT PNL AND FOUND NUM CUT WIRES ON CONN 1486VC. REPAIRED WIRES 3231-0118, 3248-0107, 3231-0 026, 3314-2264, 3314-2268 & 3248-0118 AT PLUG 1486VCA. REINSTALLED PNL AND OPS CKD GOOD. 2 L 7 2 4F RT A35EU 1998120400243 19981204 00243 NM 1998 12 4 DLM11982418 1 19981119 A 5330 SKIN DOUG MD11 MD11 3023602 NM BS 1850-1960 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 810DE 48565 THE FUSELAGE SKIN WAS PUNCTURED AND GOUGED BETWEEN FS 1850 AND 1960, BETWEEN STRINGERS 48L AND 48R DUE TO A TAIL STRIKE. THE DAMAGED SECTION OF SKIN WAS REMOVED BETWEEN THE EXISTING SKIN SPLICES AT 48L AND 48R AND A NEW SECTION OF SKIN WAS SPLICED IN WITH A NEW SPLICE AT FS 1950. THE REPAIR WAS ACCOMPLISHED PER ER/A 366102-14, REV B. 2 L 7 3 4F RT A22WE 1998120400244 19981204 00244 NM 1998 12 4 DL76S982419 1 19981119 A 5330 146T35622 SKIN BOEING 767 767332 1382001 NM BS 1109 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 126DL 24076 THE FUSELAGE SKIN SUFFERED A DEEP GOUGE AT FS 1109 AND S-19R FROM A DAMAGED SECTION OF ADJACENT FAIRING. THE DAMAGED AR EA OF SKIN WAS CUT OUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 366133-14, REV A. 2 L 7 2 4F RT A1NM 1998120400245 19981204 00245 NM 1998 12 4 DL73E982420 1 19981123 A 3350 RPS1 BATTERY PACK BOEING 737 7372S3 NM CABIN DISCHARGED A DALA K NONE L NO TEST CR CRUISE 1 SO 27 369DL 21776 ONE SECTION OF EMERGENCY LIGHTS REMAINED ON DURING FLT. REPLACED EMERG BATTERY PACK, OPS CK OK. 2 L 7 2 4F RT A16WE 1998120400246 19981204 00246 NM 1998 12 4 DL73K982421 1 19981119 A 5330 SKIN BOEING 737 737232 1384475 NM BS 747 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 303DL 23075 THE FUSELAGE SKIN WAS FOUND WITH A 2 INCH CRACK AT FS 747 JUST BELOW S-18R. THE CRACK WAS ROUTED OUT OF THE EXISTING SK IN AND AN EXISTING, ADJACENT SKIN REPAIR WAS REMOVED AND THE UNDERLYING EXISTING SKIN CUTOUT INSPECTED. BOTH AREAS WE RE INCORPORATED INTO A SINGLE EXTERNAL ALUMINUM DOUBLER REPAIR ACCOMPLISHED PER THE GUIDELINES OF B737 SRM 53-30-3. THE REPAIR AND FOLLOW-UP DTA REQUIREMENT WERE DOCUMENTED PER ERA. 2 L 7 2 4F RT A16WE 1998120400247 19981204 00247 NE 1998 12 4 DL76R982423 2 19981121 A 7200 ENGINE BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE NR 1 MALFUNCTIONED A DALA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 27 EICKE 17383 724492 26208 724492 ON TAXI OUT, BOTH ENGINES SPOOLED DOWN FROM IDLE POWER AND PILOTS MANUALLY SHUT DOWN BOTH ENGINES WHEN GENERATOR DISCONN ECTED AND RED OIL PRESSURE INDICATION CAME ON. INSPECTED FUEL FOR CONTAMINATION AND SENT FUEL SAMPLES TO LOCAL FUEL PRO VIDER FOR LAB TESTS, NO PROBLEMS NOTED. SUSPECTED ICING DUE TO EXTENDED TIME ON GROUND TIME (10 DAYS) EVEN THOUGH ENG INES WERE RUN DAILY. HANGARED AIRCRAFT FOR 20 HRS, RAN ENGINES, ALL SYSTEMS NORMAL. PERFORMED CHECK FLIGHT, ALL SYSTEM S NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1998120400248 19981204 00248 NE 1998 12 4 DL76R982424 2 19981121 A 7200 ENGINE BOEING 767 7673Y0 NM PWA 4060 PW4060 52119 NE NR 2 MALFUNCTIONED A DALA D RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TX TAXI/GRND HDL 1 SO 27 EICKE 13664 26208 724689 ON TAXI OUT, BOTH ENGINES SPOOLED DOWN FROM IDLE POWER AND PILOTS MANUALLY SHUT DOWN BOTH ENGINES WHEN THE GENERATORS DI SCONNECTED AND THE RED OIL WARING INDICATIONS CAME ON. INSPECTED FUEL FOR CONTAMINATION AND SENT FUEL SAMPLES TO LOCAL FUEL PROVIDER FOR LAB TESTS, NO PROBLEM NOTED. SUSPECT ICING DUE TO EXTENDED GROUND TIME (10 DAYS) EVEN THOUGH ENGINES WERE RUN DAILY. HANGARED AIRCRAFT FOR 20 HRS, RAN ENGINES, ALL SYSTEMS NORMAL. PERFORMED CHECK FLIGHT, ALL SYSTEMS NOR MAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1998120400249 19981204 00249 NM 1998 12 4 DL72S982426 1 19981123 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 FOUND AT D-2 LETTER CK, .5 INCH VISIBLE CRACK IN LT FRAME OF AFT ENTRY DOOR CUTOUT AT DATA PLATE. REPAIRED PER SRM 53-1 0-9. 2 L 7 3 4F A3WE 1998120400250 19981204 00250 NM 1998 12 4 DL72S982430 1 19981123 A 5522 657278419 SKIN BOEING 727 727232 1384082 NM LT ELEVATOR SEPARATED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 LT ELEV T/E SEPARATING I/B EDGE. LIGHTNING STRIKE LT ELEV O/B EDGE. REPAIRED PER MM 55-20-0 PG 801. 2 L 7 3 4F A3WE 1998120400251 19981204 00251 NM 1998 12 4 DL72S982433 1 19981124 A 3350 BATTERY PACK 276003 BOEING 727 727232 1384082 NM LT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 522DA VA5556 21582 EMERG LIGHT OVERWING FWD POSITION LT WING INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998120400252 19981204 00252 NM 1998 12 4 DL72W982434 1 19981120 A 5522 PANEL BOEING 727 727247 138408F NM LT ELEVATOR PUNCTURE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FOUND DURING MV2 CORROSION VISIT NRC 330, HOLE IN LT ELEVATOR BALANCE BOARD ACCESS PANEL NR 9119. REPAIRED PER SRM 55-2 0-3 FIG 1. 2 L 7 3 4F A3WE 1998120400253 19981204 00253 NM 1998 12 4 DL72W982435 1 19981106 A 5315 FLOORBEAM BOEING 727 727247 138408F NM BS 344 CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FOUND DURING MV2 CORROSION VISIT NRC 16, CORROSION ON FLOORBEAM STA 344 BETWEEN RBL 13 AND RB L 25. REPAIRED PER SRM 53-10-8 FIG 11. 2 L 7 3 4F A3WE 1998120400254 19981204 00254 NM 1998 12 4 DLM88982436 1 19981025 A 5311 5913595501 FRAME DOUG MD88 MD88 3023688 NM BS 1418 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DE 53410 FS 1418 FRAME CRACKED AT L2R. CRACK IS APPROX 2.0625 INCH LENGTH. REPAIRED PER ERA 332541-14. 2 L 7 2 4F RT A6WE 1998120400255 19981204 00255 NM 1998 12 4 DL72S982437 1 19981125 A 5512 SKIN BOEING 727 727232 1384082 NM LT HORIZ STAB DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 LWR SKIN OF THE LT HORIZONTAL STAB HAS A PRE-EXISTING EXTERNAL T/L REPAIR. NEED PERMANENT REPAIR INSTRUCTIONS. REPAIRE D PER ERA 332447-14. 2 L 7 3 4F A3WE 1998120400256 19981204 00256 NM 1998 12 4 DL72S982438 1 19981025 A 5320 694367013 SHEAR TIE BOEING 727 727232 1384082 NM BS 600 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 SHEAR TIES AT BS 580 AND 620, S14R WERE DAMAGED DUE TO REWORK OF THE SKIN LAP JOINT. REPAIRED PER ERA 332452-14. 2 L 7 3 4F A3WE 1998120400257 19981204 00257 NM 1998 12 4 DL72S982439 1 19981025 A 5311 651634234 FRAME BOEING 727 727232 1384082 NM BS 1030 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 LOWER LOBE FRAMES IN THE AFT B/B AT BS 1030 WERE FOUND DENTED BETWEEN S26R AND 27R. MISDRILLED HOLES WERE DONE DURING A CCOMPLISHMENT OF SRM REPAIR. REPAIRED PER ERA 332463-14AD. 2 L 7 3 4F A3WE 1998120400258 19981204 00258 NM 1998 12 4 DL72S982440 1 19981025 A 5330 655458614 SKIN BOEING 727 727232 1384082 NM BS 681 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 A SKIN BULGE AND TWO CRACKED FASTENER HOLES WERE DISCOVERED AT BS 681, 8 INCHES ABOVE STRINGER 14R. UPON FURTHER INSPEC TION CORROSION WAS FOUND ON THE I/B SIDE OF THE WINDOW BELT SKIN PANEL. REPAIRED PER ERA 332473-14. 2 L 7 3 4F A3WE 1998120400259 19981204 00259 NM 1998 12 4 DL72S982441 1 19981123 A 5330 SKIN BOEING 727 727232 1384082 NM BS 228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 483DA 20863 THE FUSELAGE WAS FOUND WITH TWO .5 INCH CRACKS EMANATING FROM LIGHTNING STRIKE MARKS OVER THE FS 228 FRAME JUST BELOW TH E STRINGER 19L SKIN LAP SPLICE. THE CRACKS WERE ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUB LER PER B727 SRM 53-30-3. THE REPAIR WAS DOCUMENTED PER ER/A 366158-14. 2 L 7 3 4F A3WE 1998120400260 19981204 00260 NM 1998 12 4 DLM11982443 1 19981125 A 3350 330701622 BATTERY PACK DOUG MD11 MD11 3023602 NM ROW 30-38 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 814DE 48769 EMERG PATH LIGHTS OUT ROW 30 TO 38 LT AND RT SIDE. REPLACED BATTERY CHARGER AND BATTERY PACK, CKS OK. 2 L 7 3 4F RT A22WE 1998120400261 19981204 00261 NM 1998 12 4 DL757982444 1 19981126 A 2913 PUMP 731966 BOEING 757 757232 1384965 NM RT HYD SYSTEM FAILED A DALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 SO 27 619DL MX417183 22909 RT ELECTRIC HYD PUMP EICAS OVERHEAT MSG IN ROUTE. REPLACED RT SYSTEM AC HYD PUMP, PRESSURE AND CASE DRAIN FILTERS. LE AK CHECK AND OPERATIONAL CK OK. 2 L 7 2 4F RT A2NM 1998120400262 19981204 00262 NM 1998 12 4 DL72W982445 1 19981126 A 2782 ACTUATOR 269002914 BOEING 727 727247 138408F NM NR 3 LE SLAT DAMAGED A DALA D RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 296WA DL401X 22533 NR 3 L/E SLAT ACTUATOR CASE FAILURE, RESULTING IN LOSS OF A-SYS HYD POWER. REPLACED ACTUATOR. 2 L 7 3 4F A3WE 1998120400263 19981204 00263 NM 1998 12 4 DLM90982446 1 19981126 A 7920 6A5082 TUBE DOUG MD900 MD900 3027375 NM IAE V2528 V2528D5 NE NR 2 ENGINE CRACKED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SO 27 915DN 53395 020015 LOST OIL QTY DURING T/O ROLL AT ABOUT 90 KTS. FIRST INDICATION ON OAP, LOOKED DOWN AND SAW OIL PRESSURE AT 75-80 PSI. P RESSURE STARTED COMING BACK UP THEN QTY DROPPED TO 0. FOUND OIL LINE TO SCAVENGE DIFFERENTIAL PRESSURE SWITCH LEAKING. REPLACED OIL LINE, LEAK CHECKS OK. 1 G 7 2 3U 4 F NC H19NM E40NE 1998120400264 19981204 00264 WP 1998 12 4 DLL10982447 1 19981126 A 2910 1549446105 HOSE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 2 ENGINE CHAFED A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 729DA 193C1180 010579 LOSS OF C HYDRAULIC QTY DURING DESCENT, QUARTER TANK REMAINING. ENG PUMP AND C2 ATM WOULD NOT PROVIDE PRESS. C3 ELEC P UMP PROVIDED PRESS ONCE ON GROUND. FOUND C-SYS EDP PRESS FLEX LINE AND RIGID LINE CHAFED. REPLACED FLEX LINE, STILL NE EDS RIGID LINE REPLACED (P/N 1549446-105) REF IPC 29-11-53 FIG 1 PG 0 ITEM 95. RENDERED C SYST EDP INOP PER MEL 29-11-0 7. EDP SHAFT IN MCO POUCH. L-17 C/B PULLED AND COLLARED NO HYD LKS W/ ALL SYS PRESSURIZED AND ENG RUNNING. 2 L 7 3 4F 4 F A23WE E12EU 1998120400265 19981204 00265 NM 1998 12 4 DL72S982449 1 19981127 A 3350 900542 BATTERY PACK BOEING 727 727232 1384082 NM OVERWING EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 494DA 21074 LEFT FWD AND MID OVERWING EMERG LIGHTS INOP. ALSO, AFT SERVICE DOOR EXIT SIGN INOP, FOUND ON L/O. REPAIRED WIRE AT AFT SERVICE DOOR EMERG EXIT SIGN. ALSO, REPLACED PACK. REPLACED PACK AT MID OVERWING EMERG RACK. REPLACED RACK AND PACK FOR FWD OVERWING EMERG LIGHT, ALL CKS GOOD. 2 L 7 3 4F A3WE 1998120400266 19981204 00266 NM 1998 12 4 DL72S982451 1 19981128 A 3350 FUSE 276005 BOEING 727 727225 1384077 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 FWD EMER FLOOR LIGHTS INOP. REPLACED FUSES NR 1 PWR SUPPLY, OPS CKS NORMAL. 2 L 7 3 4F A3WE 1998120400267 19981204 00267 NM 1998 12 4 DL72K982452 1 19981128 A 3350 900835A BATTERY PACK BOEING 727 727232 1384082 NM ROW 21 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 479DA 20756 EMERGENCY EXIT LIGHT SIGN WILL NOT ILLUM WHEN TESTED O/H ROW 21. REPLACED BATTERY PACK, CKS NORMAL. 2 L 7 3 4F A3WE 1998120400268 19981204 00268 NM 1998 12 4 DL72S982453 1 19981128 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM R 2 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8889Z T4185 21858 R2 DOOR EMER EXIT LIGHT INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998120400269 19981204 00269 NE 1998 12 4 DL72S982454 2 19981129 A 7261 FILTER BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 3 ENGINE CLOGGED A DALA O OTHER J WARNING INDICATION LD LANDING 1 SO 27 499DA 53151 21143 700444 NR 3 ENGINE OIL FILTER BYPASS ILLUMINATED IN FLIGHT. THE LIGHT EXTINGUISHED AT 45 TO 50 PERCENT N1 ALL ON SHORT FINAL. LIGHT RE-ILLUMINATED AT IDLE. PER T/S CHART REPLACED FILTER, PERFORMED BREATHER PRESS CK, CKS GOOD. REPLACED FILTER, OK FOR SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998120400270 19981204 00270 NM 1998 12 4 DL72S982455 1 19981129 A 2750 RETRACT MECH BOEING 727 727232 1384082 NM TE FLAPS LACK OF LUBE A DALA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED DE DESCENT 1 SO 27 411DA 21223 OUTBOARD FLAPS WOULD NOT EXTEND PAST 15 TO 20 DEGS. DIVERTED TO JFK. PERFORMED OPS CHECK, COULD NOT DUPLICATE. DUE PR EVIOUS ITEMS, SERVICED TRANS AND JACKSCREW GEARBOXES LUBED TRACKS AND JACKSCREW BALLNUTS ON OUTBOARD FLAPS. 2 L 7 3 4F A3WE 1998120400271 19981204 00271 NM 1998 12 4 DL72S982456 1 19981129 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM R1 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 515DA 21431 R-1 DOOR EMERG EXIT LIGHT INOP. REPLACED LIGHT ASSY, OPS CK NORMAL. 2 L 7 3 4F A3WE 1998120400272 19981204 00272 NM 1998 12 4 SCNA98142 1 19981124 A 3350 LIGHT BOEING 727 727282 138408T NM L1 DOOR INOP A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE L1 EMERGENCY SLIDE LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BUL B, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998120400273 19981204 00273 WP 1998 12 4 DHL98806002 1 19981127 A 3310 BA170 TRANSFORMER DOUG DC8 DC873F 302199F WP RT COCKPIT BURNED A DHLA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 01 806DH 46002 FIRST OFFICERS FLUORESCENT BULBS WENT BRIGHT, THEN OUT. HEAVY SMOKE EMITTED FROM RT SIDE PANEL. TURNED OFF LIGHTS THEN SMOKE DISIPATED. REPLACED TRANSFORMER BALLAST PER MM 33-10-0, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1998120400274 19981204 00274 NM 1998 12 4 VNAA9811021 1 19981121 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 424JS 74738 63487 3033 THE RIGHT HAND PROPELLER FAILED TO COME OUT OF THE FEATHER POSITION, WHEN SELECTED. DURING THE ATTEMPT TO GET THE PROPE LLER OUT OF FEATHER, THE RIGHT ENGINE WAS OVER TORQUED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND C OMPLIED WITH A OVER TORQUE INSPECTION OF THE RIGHT HAND ENGINE, IN ACCORDANCE WITH DORNIER MANTENANCE MANUAL 05-57-01. M AINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 6 1-21-06. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998120400275 19981204 00275 NM 1998 12 4 VNAA9811022 1 19981122 A 5610 001A561A0000207 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 461PS 64681 21566 3075 DURING THE TAXI FOR TAKEOFF, A RIGHT HAND WINDSCREEN HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO TH E GATE. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT HAND SIDE WINDSCREEN HEAT, IN ACCORDANCE WITH THE DORNIER MINIMUM EQUIPMENT LIST, AND RETURNED THE AIRCRAFT TO SERVICE. LATER THAT DAY, PIT MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND SIDE WINDSCREEN, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-12-00. OPERATIONAL CHECKS WERE COMPLETED, AND TH E DEFERRAL WAS REMOVED. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998120400276 19981204 00276 NM 1998 12 4 VNAA9811023 1 19981125 A 5610 001A561A0000207 WINDSHIELD DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RIGHT FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 427JS 68545 28087 3039 THE AIRCRAFT RETURNED TO THE GATE FOLLOWING A WINDSCREEN HEAT FAIL WARNING MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND SIDE WINDSCREEN, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-12-00. OPERATIONAL CHECKS WERE COMPLET ED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998120400277 19981204 00277 NE 1998 12 4 TC8A98084 2 19981126 A 7230 COMPRESSOR DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 182SK 45817 ON TAKEOFF, COMPRESSOR STALL, ABORTED TAKEOFF. SUSPECT NR 4 ENGINE. CONDUCTED ENGINE RUN ON NR 4 ENGINE AND BLEED AIR CHECK WITH OPERATING FLIGHT CREW, OPS CHECK GOOD IAW MM 75-00. PERFORMED FOD CHECK OF INLET AND EXHAUST, OK. FLAG CHEC K, NO FOD NOTED, FLAG CHECK GOOD IAW MM 76-00. 2 L 7 4 4F 4 F 4A25 1E8 1998120400339 19981204 00339 NM 1998 12 4 SWAA982981 1 19981121 A 3350 1000679 LIGHT BOEING 737 7372H4 138448C NM COCKPIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 60SW 21812 FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH. OK TO CONTINUE PER MEL 33-15. REMOVED AND REPLACED LIGHT ASSY, O PS CK OK PER M/M. 2 L 7 2 4F A16WE 1998120400340 19981204 00340 NE 1998 12 4 SWAA982982 2 19981117 A 7230 COMPRESSOR BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE DAMAGED A SWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 60SW 21812 RETURNED TO MDW DUE TO BIRD STRIKE TO NR 1 ENG. INSPECTED AND FOUND 2 SHINGLED FAN BLADES. REMOVED AND REPLACED C1 FAN ASSY AND PERFORMED ENG RUN, OPS CKS GOOD. 2 L 7 2 4F 4 F A16WE E2EA 1998120400341 19981204 00341 NM 1998 12 4 SWAA982983 1 19981121 A 3350 CONNECTOR BOEING 737 7373H4 1384600 NM ROW 15-18 DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 383SW 26589 DURING SCHEDULED SC, FOUND FLOOR TRACK LIGHTING INOP AT ROWS 15 TO 18. RECONNECTED LOOSE CONNECTOR AT ROW 18. 2 L 7 2 4F RT A16WE 1998120400342 19981204 00342 1998 12 4 SWAA982984 4 19981120 A 2565 SLIDE BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED ANNUAL SAMPLE ESCAPE SLIDE OPERATIONAL CHECK, SLIDE (S/N 18471679) FAILED TO DEPLOY SUCCESSFULLY. SLID E FELL ONTO ENTRYWAY FLOOR. SLIDE WAS THEN POSITIONED MANUALLY OUT OF THE ENTRYWAY AND PROPERLY INFLATED. REPLACED SLI DE ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1998120400343 19981204 00343 NM 1998 12 4 SWAA982985 1 19981120 A 3230 2732513 ROD BOEING 737 7373H4 1384600 NM LANDING GEAR BROKEN A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 330SW 23694 RETURNED TO PHX DUE TO AFTER TAKEOFF LANDING GEAR WOULD NOT RAISE. ALL COCKPIT INDICATIONS POINTED TO A AIR/GROUND SENS OR PROBLEM. FOUND GROUND SPOILER INTERLOCK CABLE LOWER ROD END BROKEN. REPLACED AND RIGGED CABLE AS REQUIRED PER M/M. CYCLED GEAR, OPS NORMAL. 2 L 7 2 4F RT A16WE 1998120400344 19981204 00344 NM 1998 12 4 SWAA982986 1 19981122 A 3260 655825029 CARD BOEING 737 7373Q8 1384670 NM E/E BAY FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 689SW 23387 RETURNED TO TPA DUE TO AFTER GEAR RETRACTION NOSE WHEEL RED AND GREEN LIGHTS REMAINED ON WITH HANDLE UP. WITH HANDLE OF F NOSE WHEEL WAS GREEN, MAIN GEAR WENT NORMALLY UP AND LOCKED. REMOVED AND REPLACED M983 CARD, JACKED NOSE OF AIRCRAFT, CYCLED NOSE GEAR SEVERAL TIMES AND OPS CHECKED GOOD PER M/M. 2 L 7 2 4F RT A16WE 1998120400345 19981204 00345 NE 1998 12 4 SWAA982987 2 19981120 A 7314 378200 FUEL PUMP BOEING 737 7372H4 138448C NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 51SW 21448 ON TAKEOFF ROLL, NR 1 ENGINE ROLLED BACK APPROX 10 PERCENT. NR 1 THROTTLE WAS PUSHED UP AND ALL INDICATIONS WERE NORMAL . ON CLIMBOUT, THE THROTTLES WERE SPLIT APPROXIMATE 3 AND INCREASED WITH CLIMB. AIRCRAFT RETURNED TO MCO WITH NO PROBL EMS. REMOVED AND REPLACED NR 1 ENG FUEL PUMP AND FUEL CONTROL PER M/M. LEAK AND OP'S CHECK GOOD. PERFORMED FIELD TRIM PER BOEING M/M. 2 L 7 2 4F 4 F A16WE E2EA 1998120400346 19981204 00346 NM 1998 12 4 SWAA982988 1 19981119 A 2782 654465116 ACTUATOR BOEING 737 7372T4 1384492 NM NR 4 LE SLAT FAILED A SWAA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 130SW 22699 AFTER TAKEOFF, NR 4 L/E SLAT WOULD NOT RETRACT. AIRCRAFT RETURNED TO SDF AND MADE AN UNEVENTFUL LANDING. REPLACED NR 4 L/E SLAT ACTUATOR PER BOEING M/M. 2 L 7 2 4F A16WE 1998120400347 19981204 00347 NM 1998 12 4 SWAA982989 1 19981123 A 5730 SKIN BOEING 737 7373Q8 1384670 NM RT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND RT WING FIXED L/E CRACKED AT NR 6 SLAT I/B AUX TRACK CUTOUT. REPAIRED PER BOEING SRM . 2 L 7 2 4F RT A16WE 1998120400348 19981204 00348 NM 1998 12 4 SWAA982990 1 19981123 A 3397 WIRE BOEING 737 7373A4 1384585 NM ROW 1-8 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 673AA 23251 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY TRACK LIGHTS INOP FROM ROWS 1 TO 8. REPLACED TRACK WIRE AND OP CHECKED PER B OEING M/M. 2 L 7 2 4F RT A16WE 1998120400349 19981204 00349 NM 1998 12 4 SWAA982991 1 19981123 A 3350 BULB BOEING 737 737301 1384611 NM PAX DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659SW 23229 DURING SCHEDULED SC CHECK, FOUND AFT ENTRY DOOR EMERGENCY LIGHT INOP. RELAMPED AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998120400350 19981204 00350 1998 12 4 SWAA982992 4 19981123 A 2565 22022900131 SLIDE BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 DURING SCHEDULED A1 CHECK, FOUND FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F A16WE 1998120400351 19981204 00351 NM 1998 12 4 SWAA982993 1 19981123 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 310 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 104SW 23110 DURING SCHEDULED C2 CHECK, FOUND A 1 INCH FUSELAGE SKIN CRACK AT BS 310 FWD OF FWD ENTRY DOOR GUIDE ARM. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1998120400352 19981204 00352 NM 1998 12 4 SWAA982994 1 19981120 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACKED ON RT SIDE AFT AND ABOVE WING. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400353 19981204 00353 NM 1998 12 4 SWAA982995 1 19981120 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 867 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 686SW 23175 DURING SCHEDULED SC CHECK, FOUND A 1 INCH FUSELAGE SKIN CRACK AT BS 867, AT S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400354 19981204 00354 NM 1998 12 4 SWAA982996 1 19981123 A 5320 CHANNEL BOEING 737 7372H4 138448C NM BS 283 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND CHANNEL GOUGED AT S14R AT BS 283, RBL 60, WL 230. REPAIRED PER TRAMCO EWO 98-1074. 2 L 7 2 4F A16WE 1998120400355 19981204 00355 NM 1998 12 4 SWAA982997 1 19981123 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT I/B CHORD, REINFORECEMENT ANGLE AND FRAME WEB AT BS 616, LBL 66, W L 207. REPAIRED PER BOEING DRAWING 65C31658 AND SWA ACO 581-53. 2 L 7 2 4F A16WE 1998120400356 19981204 00356 NM 1998 12 4 SWAA982998 1 19981123 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 767 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME DENTED AT BS 767, LBL 24, WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400357 19981204 00357 NM 1998 12 4 SWAA982999 1 19981123 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 787 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME DENTED 2 PLACES AT BS 787, RBL 26.5 AND 31, WL 158. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400358 19981204 00358 NM 1998 12 4 SWAA983000 1 19981123 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 496 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED AT BS 496, S22R AND S23R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400359 19981204 00359 NM 1998 12 4 SWAA983001 1 19981120 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 440, 480, 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 440, 480, 747 AND 827. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400360 19981204 00360 NM 1998 12 4 SWAA983002 1 19981123 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 348 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND A CRACK INDICATION IN FUSELAGE SKIN EMANATING FROM FASTENER HOLE AT BS 348 BELOW FWD ENTRY DOOR. REPAIRED SWA RA 1-353-193 AND BOEING DRAWING 65C27257. 2 L 7 2 4F RT A16WE 1998120400361 19981204 00361 NM 1998 12 4 SWAA983003 1 19981123 A 5330 SKIN BOEING 737 7373Q8 1384670 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND 2 ADJACENT CRACKS IN FUSELAGE SKIN AT AFT LOWER CORNER OF FWD SERV DOOR CUTOUT. REPA IRED BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400362 19981204 00362 NM 1998 12 4 SWAA983004 1 19981123 A 5320 WEB BOEING 737 7373Q8 1384670 NM BS 664 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT BS 664. REPAIRED PER SWA RA 1-353-1929. 2 L 7 2 4F RT A16WE 1998120400363 19981204 00363 NM 1998 12 4 SWAA983005 1 19981122 A 3397 WIRE BOEING 737 7373Q8 1384670 NM CABIN BROKEN A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 672SW 23406 DURING SCHEDULED 1/4D CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT OVERWING EXITS. REPAIRED BROKEN WIRE AND OP CHECKED PE R BOEING M/M. 2 L 7 2 4F RT A16WE 1998120400364 19981204 00364 NM 1998 12 4 SWAA983006 1 19981120 A 3350 P4010021 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 59SW 21811 DURING SCHEDULED A1 CHECK, FOUND AFT CABIN LOWER EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1998120400365 19981204 00365 NM 1998 12 4 SWAA983007 1 19981120 A 3250 STEERING BOEING 737 7373H4 1384600 NM NLG FROZEN A SWAA K NONE O OTHER LD LANDING 1 SW 07 687SW 23388 ON LANDING WHILE TRYING TO CLEAR RWY THE NWS TILLER WOULD NOT MOVE EITHER DIRECTION. AFTER APPLYING EXCESSIVE FORCE, WA S ABLE TO STEER A/C TO TUG FOR TOW IN. IT WAS EXTREMELY STIFF AND HAD A GRINDING FEEL. DUE TO WATER ACCUM ON NOSE GEAR STEERING FROZEN AT ALTITUDE, LUBRICATED NOSE GEAR PER M/M. TAXIED A/C, OP CK NORMAL. 2 L 7 2 4F RT A16WE 1998120400366 19981204 00366 NM 1998 12 4 SWAA983008 1 19981120 A 3230 27325 CONTROL CABLE BOEING 737 7372H4 138448C NM LANDING GEAR FAILED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 71SW 22358 AFTER TAKEOFF WITH GEAR HANDLE UP GET THREE RED LANDING GEAR LIGHTS AND HORN SOUNDS. LANDING GEAR DID RETRACT, BUT RED UNSAFE LIGHTS REMAINED ON AND HORN SOUNDS. REMOVED AND REPLACED GROUND INTERLOCK TELEFLEX CABLE PER MM, OPS CHECKS NORM AL. 2 L 7 2 4F A16WE 1998120400367 19981204 00367 1998 12 4 SWAA983009 4 19981120 A 2210 4030952 COUPLER BOEING 737 7372H4 138448C NM YAW DAMPER FAILED A SWAA K NONE F FLT CONT AFFECTED DE DESCENT 1 SW 07 95SW 23054 AT SPEEDS LESS THAN 210 KTS, AIRCRAFT YAWS BACK AND FORTH WITH YAW DAMPER ON. REMOVED AND REPLACED YAW DAMPER COUPLER, OPS CHECKED GOOD PER BOEING M/M. 2 L 7 2 4F A16WE 1998120400368 19981204 00368 NM 1998 12 4 SWAA983010 1 19981120 A 3240 BRAKES BOEING 737 7372T4 1384492 NM MLG MALFUNCTIONED A SWAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SW 07 722WN 22698 RETURNED TO GATE AFTER BEING CLEARED INTO POSITION FOR TAKEOFF DUE TO ABNORMAL FEEL IN BRAKES; RIGHT MAIN BRAKES FELT A S IF THEY WERE BRAKING. ONSET OF BRAKING AFTER PEDAL APPLICATION WAS UNEVEN. TAXIED ACFT WITH ANTISKID ON AND OFF. B RAKING WAS NORMAL WITH NO DEFECTS NOTED. ANTISKID CK'D GOOD BOEING M/M. 2 L 7 2 4F A16WE 1998120400369 19981204 00369 NM 1998 12 4 SWAA983011 1 19981122 A 3350 6573709 LIGHT BOEING 737 7372H4 138448C NM FLIGHT DECK INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 60SW 21812 FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT EXTINGUISH. OK TO CONTINUE PER MEL 33-15. REPLACED LIGHT ASSEMBLY PER BOEING M/M. 2 L 7 2 4F A16WE 1998120400370 19981204 00370 NM 1998 12 4 SWAA983012 1 19981124 A 3350 2013A BATTERY BOEING 737 7375H4 138449D NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 508SW 24185 DURING SCHEDULED RON CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS INOP MID CABIN AREA. REMOVED AND REPLACED BATTERY PACK P ER BOEING M/M. 2 L 7 2 4F RT A16WE 1998120400371 19981204 00371 NM 1998 12 4 SWAA983013 1 19981124 A 3350 P4010021 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 348SW 24375 DURING SCHEDULED SC CHECK, FOUND EMERGENCY FLASHLIGHT AT FWD GALLEY BATTERY LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998120400372 19981204 00372 NM 1998 12 4 SWAA983014 1 19981120 A 5320 CHANNEL BOEING 737 7373H4 1384600 NM BS 359 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 359, S14L. REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400373 19981204 00373 NM 1998 12 4 SWAA983015 1 19981120 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 380, ABOVE S16R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400374 19981204 00374 NM 1998 12 4 SWAA983016 1 19981120 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME CRACKED AT BS 360, ABOVE S15R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400375 19981204 00375 NM 1998 12 4 SWAA983017 1 19981120 A 5313 STRINGER BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND STRINGER 16L CRACKED AT BS 500B+2.5. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400376 19981204 00376 NM 1998 12 4 SWAA983018 1 19981120 A 5320 SHEAR TIE BOEING 737 7373H4 1384600 NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSE FRAME SHEAR TIES CRACKED AT BS 360, BETWEEN S13 AND 15L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400377 19981204 00377 NM 1998 12 4 SWAA983019 1 19981124 A 5320 POST BOEING 737 7373A4 1384585 NM L1 WINDOW CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2 D-CHECK, FOUND COCKPIT WINDOW POST CRACKED AT UPPER O/B CORNER OF L1 WINDOW APPROX .5 IN LENGTH. R EPAIRED PER SWA RA 1-A53-1156. 2 L 7 2 4F RT A16WE 1998120400378 19981204 00378 NM 1998 12 4 SWAA983020 1 19981124 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2 D-CHECK, FOUND CRACK IN BEADED PRESSURE WEB AT BS 663, RBL 40 MLG CEILING. REPAIRED PER SWA RA 1-3 53-1921. 2 L 7 2 4F RT A16WE 1998120400379 19981204 00379 NM 1998 12 4 SWAA983021 1 19981127 A 3350 BULB BOEING 737 7375H4 138449D NM EMER EXIT FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING PREFLIGHT CHECK, FOUND RED EMERGENCY EXIT FLOOR TRACK LIGHTS AT OVERWING EXIT INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998120400380 19981204 00380 NM 1998 12 4 SWAA983022 1 19981125 A 3350 BULB BOEING 737 7373H4 1384600 NM ROW 20 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 366SW 26577 DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT TRACK AT BULLNOSE ROW 20DEF INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998120400381 19981204 00381 NM 1998 12 4 SWAA983023 1 19981126 A 2131 7638101 CONTROLLER BOEING 737 7373Y0 1384671 NM NR 1 MALFUNCTIONED A SWAA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 699SW 23826 AT FL 350, PRESS MODE SELECTOR IN AUTO, THE ALTITUDE 'CABIN' WARNING HORN SOUNDED. EMERGENCY DECLARED. EMERGENCY DESCE NT ACCOMPLISHED. PASSENGER MASK DID NOT DROP. CABIN ALT INCREASED TO APPROX 12,500 FT, MAN PRESS OK. REPLACED CABIN P RESSURIZATION CONTROLLER, OPS CK OK PER M/M. 2 L 7 2 4F RT A16WE 1998120400382 19981204 00382 NM 1998 12 4 SWAA983024 1 19981129 A 5330 6545768 SKIN BOEING 737 7373H4 1384600 NM BS 770 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 312SW 23334 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED 2.5 INCHES AT S19R, BS 770. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400383 19981204 00383 NM 1998 12 4 SWAA983025 1 19981130 A 2120 AIR DIST BOEING 737 7372H4 138448C NM CABIN ODOR A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 086SW 22827 UPON TAKEOFF THRUST APPLICATION, SLIGHT ODOR WAS NOTICED SIMILAR TO HOT PACK. ODOR BECAME STRONGER AFTER TAKEOFF. VERY LIGHT SMOKE APPEARED IN CABIN. RAN BOTH ENGS, VERIFIED SMELL COMING FROM ENGINES DUE TO A CHEMICAL ENG WASH ON RON. S MOKE WAS FROM A/C SYSTEM COLD AIR. OK FOR SERVICE. 2 L 7 2 4F A16WE 1998120400384 19981204 00384 NM 1998 12 4 SWAA983026 1 19981130 A 3260 189929 SENSOR BOEING 737 7373G7 1384595 NM LT MLG FAILED A SWAA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 07 690SW 23783 WITH GEAR HANDLE UP, LEFT MAIN GEAR INDICATED UNSAFE (RED LIGHT). LEFT MAIN RED AND GREEN GEAR LIGHTS ILLUMINATED WITH GEAR HANDLE OFF. WITH GEAR EXTENDED ALL INDICATIONS SAFE AND OK HYD PRESS AND QTY NORMAL. REMOVED AND REPLACED LT MAIN GEAR UPLOCK SENSOR PER M/M, OPS AND ADJUSTED PER M/M. 2 L 7 2 4F RT A16WE 1998120400385 19981204 00385 NM 1998 12 4 SWAA983027 1 19981202 A 5320 WEB BOEING 737 7373A4 1384585 NM BS 664 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 679AA 23291 DURING SCHEDULED 1/2D CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 664, RBL 32. REPAIRED PER SWA RA 1-353-1911. 2 L 7 2 4F RT A16WE 1998120400386 19981204 00386 NM 1998 12 4 SWAA983028 1 19981130 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 328/360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 328 BELOW S20R AND BS 360, AT S20R. REPAIRED PER BOEING S RM. 2 L 7 2 4F A16WE 1998120400387 19981204 00387 NM 1998 12 4 SWAA983029 1 19981130 A 5220 SKIN BOEING 737 7372H4 138448C NM EMER EXIT DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND RT OVERWING EXIT HATCH DENTED ON LOWER EXT SKIN. RESKINNED DOOR PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400388 19981204 00388 NM 1998 12 4 SWAA983030 1 19981130 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 580.5 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CRACK IN S17R O/B CHORD, AT BS 580.5. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400389 19981204 00389 NM 1998 12 4 SWAA983031 1 19981130 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 807 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 807 AT LBL 28, WL 160. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400390 19981204 00390 NM 1998 12 4 SWAA983032 1 19981130 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 907 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, RBL 12. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400391 19981204 00391 NM 1998 12 4 SWAA983033 1 19981130 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 927 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L CORRODED AT BS 927, LBL 12. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400392 19981204 00392 NM 1998 12 4 SWAA983034 1 19981130 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 359 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND FACTORY STRINGER SPLICE CORRODED AT STRINGER 27L, BS 359, WL 147. REPLACED PER BOEING S RM. 2 L 7 2 4F A16WE 1998120400393 19981204 00393 NM 1998 12 4 SWAA983035 1 19981130 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 767 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER 20R CORRODED AT BS 767. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400394 19981204 00394 NM 1998 12 4 SWAA983036 1 19981130 A 5711 SPAR BOEING 737 7372H4 138448C NM LT WING CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND LEFT WING CENTER FUEL CELL UPPER REAR SPAR SEAL CUP CRACKED. REPAIRED PER TRAMCO EWO 98 -1085. 2 L 7 2 4F A16WE 1998120400395 19981204 00395 NM 1998 12 4 SWAA983037 1 19981130 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 559 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 559 AT RBL 66, WL 216. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400396 19981204 00396 NM 1998 12 4 SWAA983038 1 19981130 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 727 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TOP CHORD DAMAGED AT BS 727A, RBL 58, WL 208. REPLACED DAMAGED SECTION PER BO EING SRM. 2 L 7 2 4F A16WE 1998120400397 19981204 00397 NM 1998 12 4 SWAA983039 1 19981130 A 5320 BEAM BOEING 737 7372H4 138448C NM BS 616 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM CRACKED AT BS 616, LBL 65, WL 208. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400398 19981204 00398 NM 1998 12 4 SWAA983040 1 19981130 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 760 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER 16R FLANGE CRACKED BS 760. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998120400399 19981204 00399 NM 1998 12 4 SWAA983041 1 19981127 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 067SW 22356 DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN BULGE AT BS 727, S28R. REPAIRED PER BOEING SWA RA 1-253-1895. 2 L 7 2 4F A16WE 1998120400400 19981204 00400 NM 1998 12 4 SWAA983042 1 19981130 A 5330 6545768 SKIN BOEING 737 7372H4 138448C NM BS 801 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 091SW 22963 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 801, S23L. REPAIRED PER BOEING SWA RA 1-253-1895. 2 L 7 2 4F A16WE 1998120400401 19981204 00401 NM 1998 12 4 SWAA983043 1 19981130 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 807 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 807 AT LBL 31, WL 161. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400402 19981204 00402 NM 1998 12 4 SWAA983044 1 19981130 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 767 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME DENTED AT BS 767 AT RBL 27, WL 157. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400403 19981204 00403 NM 1998 12 4 SWAA983045 1 19981130 A 5330 SKIN BOEING 737 7373H4 1384600 NM R2 DOORWAY DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AFT OF R2 DOOR BELOW EMERG LIGHT. INSTALLED REPAIR DOUBLER PER BOE ING SRM. 2 L 7 2 4F RT A16WE 1998120400404 19981204 00404 NM 1998 12 4 SWAA983046 1 19981130 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 912 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 912, BELOW S16L. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400405 19981204 00405 NM 1998 12 4 SWAA983047 1 19981130 A 5230 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR DENTED CENTER OF DOOR 11 INCHES FROM TOP. INSTALLED REPAIR DOUBLER PER B OEING SRM. 2 L 7 2 4F RT A16WE 1998120400406 19981204 00406 NM 1998 12 4 SWAA983048 1 19981130 A 5230 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR DENTED 5 INCHES FROM AFT EDGE, 12 INCHES FROM TOP. INSTALLED REPAIR DOUB LER PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400407 19981204 00407 NM 1998 12 4 SWAA983049 1 19981130 A 5230 SKIN BOEING 737 7373H4 1384600 NM CARGO DOOR DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR DENTED 1 INCH FROM AFT EDGE, 12 INCHES FROM TOP. INSTALLED REPAIR DOUBLE R PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998120400408 19981204 00408 NM 1998 12 4 SWAA983050 1 19981130 A 5311 FRAME BOEING 737 7373H4 1384600 NM BS 907 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 343SW 24151 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907 AT LBL 2 FROM S1. REPAIRED PER TRAMCO EWO 98-1050. 2 L 7 2 4F RT A16WE 1998120400409 19981204 00409 NM 1998 12 4 SWAA983051 1 19981130 A 3397 WIRE BOEING 737 7373H4 1384600 NM CABIN DISCONNECTED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 358SW 26595 DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EXIT SIGN LIGHTS INOP. REPAIRED WIRE TO BATTERY PACK PER BOEI NG M/M. 2 L 7 2 4F RT A16WE 1998120400410 19981204 00410 1998 12 4 98ZZZX4422 4 19981022 A 3120 B1894522282A CLOCK SNIAS 350 AS350B2 8680813 EU COCKPIT MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 102LN 50 792559 3065 CLOCK'S SECOND HAND STICKS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1998120400411 19981204 00411 1998 12 4 98ZZZX4423 4 19981115 A 3160 900A3720002107 DISPLAY DOUG MD900 MD900 3027375 NM COCKPIT DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 499 008251007 90000012 SCREEN SEPARATED WHICH CAUSES LIGHT TO SHINE THROUGH. THE SEPARATION ALSO CAUSED THE FORMATION OF A SINGLE BUBBLE WHICH DISTORTS ONE OF THE ANNUNICATOR WARNING LIGHTS. AT TIMES, THE BUBBLE WOULD CAUSE THE ILLUSION OF FALSE WARNING LIGHT T HAT COULD CAUSE THE PILOT TO REACT TO A FALSE INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1998120400412 19981204 00412 EU 1998 12 4 HCMA0000214 1 19980928 A 6520 350A33215300 HINGE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR TORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 196BH 671 3036 HINGE IS TORN BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1998120400413 19981204 00413 EU 1998 12 4 HCMA0000215 1 19980930 A 6520 350A33215300 HINGE LAMINATE SNIAS 350 AS350B 8680801 EU TAILROTOR TORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 312B 857 2243 HINGE IS TORN BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1998120400414 19981204 00414 EU 1998 12 4 HCMA0000220 1 19981011 A 6520 350A33215300 HINGE LAMINATE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CRACKED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 193BH 655 2894 RUBBER IS CRACKED BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1998120400415 19981204 00415 EU 1998 12 4 HCMA0000222 1 19980928 A 6520 350A33215300 HINGE LAMINATE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR CUT A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 196BH 642 3036 HINGE IS WORN AND CUT BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1998120400416 19981204 00416 CE 1998 12 4 98ZZZX4424 1 19981107 A 2133 10138001313 VALVE BEECH 200 B200 1152922 CE CABIN PRESSURE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 220TB 411 2266 BB1057 VALVE, FLOW CONTROL HAS LOW OUTPUT. PROBLEM FOLLOWED UNIT WHILE SWAPPING FROM SIDE-TO-SIDE. REPLACED IWTH NEW UNIT, CO RRECTED PROBLEM. 1 L 7 2 4T A24CE 1998120400417 19981204 00417 EU 1998 12 4 98ZZZX4425 1 19981021 A 7170 0174126090 VALVE SNIAS 350 AS350B2 8680813 EU ENGINE DRAIN STICKING A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 102LN 49 515M 3065 VALVE STICKS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 173.5. 1 G 7 1 3U H9EU 1998120400418 19981204 00418 GL 1998 12 4 98ZZZX4426 2 19981027 A 7323 25246929 GOVERNOR SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 ENGINE FAILED A HEEA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 03 1547D 5869 1879 760077 CAE890607S DURING DEPARTURE, EXPERIENCED NR 2 ENGINE HIGH SIDE FAILURE. RETURNED TO MAINTENANCE. REPLACED NR 2 GOVERNOR. 1 G 7 2 3U 3 U H1NE E1GL 1998120400419 19981204 00419 NE 1998 12 4 98ZZZX4427 2 19981027 A 7200 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE NR 1 MALFUNCTIONED A HEEA O OTHER O OTHER AP APPROACH 1 SW 03 3911L 9089 109 33023 CPPS61439 ON FINAL, NR 1 ENGINE STALLED. RUN-ON LANDING ACCOMPLISHED. TROUBLESHOOTING IN PROGRESS. 1 G 7 2 4U 4 U H4SW E22EA 1998120400420 19981204 00420 NE 1998 12 4 98ZZZX4428 1 19981108 A 2422 P173 STATIC INVERTER SKRSKY S76 S76A 8143006 NE CARGO BAY FAILED A HEEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 03 15459 760222 WHILE IN CRUISE FLIGHT OUTBOUND, CREW DETECTED SMOKE ODOR ONLY. RETURNED TO BASE FOR MAINTENANCE. REF: STC SH8641SW, AIRLOG DRAWING NR S76-00-1001. 1 G 7 2 3U H1NE 1998120400421 19981204 00421 1998 12 4 98ZZZX4429 4 19981109 A 2312 MS3476W12105 CONNECTOR BELL 412 412 1182202 SW INSTRUMENT PANEL CHAFED A A HEEA O OTHER A FLAME/FIRE NR NOT REPORTED 1 SW 03 21498 36003 DURING BASE LEG, PILOT INSTRUMENT LIGHTS WENT OUT. WHEN CIRCUIT BREAKER WAS RESET, SPARKS WERE OBSERVED AT THE LOWER IN SIDE CORNER OF THE PILOTS WINDSHIELD NEAR CENTER POST. FOUND INSTRUMENT LIGHT WIRE CHAFED AGAINST THE FUEL QUANTITY IND ICATION CANNON PLUG. REF: 412 IPC, FIGURE 96-6-63. 1 G 7 2 4U H4SW 1998120400422 19981204 00422 NM 1998 12 4 K3HA0980145 1 19981126 A 3350 08163000603 LIGHT BOEING 727 727225 1384077 NM ROW 1 ABC BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH LIGHT TRACK FORWARD OF ROW 1ABC BROKEN AND CRACKED. REMOVED AND REPLACED TRACK ASSEMBLY PER MM 33-59-00. 2 L 7 3 4F A3WE 1998120400423 19981204 00423 NM 1998 12 4 K3HA980141 1 19981130 A 2133 OUT FLOW VALVE BOEING 727 727225 1384077 NM CABIN OBSTRUCTED A K3HA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 25 354PA 20624 UNABLE TO PRESSURIZE, DUMPED FUEL AND RETURNED FOR LANDING. TROUBLESHOT, FOUND INSULATION BLANKET OBSTRUCTING LEFT HAND OUT FLOW VALVE. REMOVED OBSTRUCTION AND CLEANED OUT FLOW VALVES PER MM 21-30-11. AIRCRAFT PRESSURIZED OK PER MM 21-30 -0. 2 L 7 3 4F A3WE 1998120400424 19981204 00424 NM 1998 12 4 K3HA980142 1 19981125 A 3350 S106S106 BATTERY BOEING 727 727225 1384077 NM AFT AIRSTAIR DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 353PA 20622 ON POST FLIGHT INSPECTION, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOP. REMOVED AND REPLACED TWO NICAD BATTERY ON AFT AIRST AIR EMERGENCY LIGHT. OPS CHECK GOOD PER 33-50-71. 2 L 7 3 4F A3WE 1998120400425 19981204 00425 NM 1998 12 4 K3HA980143 1 19981125 A 3350 3071BPEGPL LAMP BOEING 727 727225 1384077 NM FORWARD FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 FORWARD TWO RED LIGHT EMERGENCY PATH LIGHT INOP. REPLACED SOCKET ASSEMBLY (P/N 08169-01). RELAMPED TEST OK, REF MM 33- 50-01. 2 L 7 3 4F A3WE 1998120400426 19981204 00426 NM 1998 12 4 K3HA980144 1 19981125 A 3350 079173 LENS BOEING 727 727225 1384077 NM ROW 1 MISSING A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 MISSING EMERGENCY PATH LIGHT RED LENS AND LAMP SEAT 1ABC. INSTALLED RED LENS AND RELAMPED SEAT 1ABC AREA, TEST OK REF 3 3-50-01. 2 L 7 3 4F A3WE 1998120400427 19981204 00427 SO 1998 12 4 RAAA98E9038 1 19981130 A 3350 8621014 BATTERY PACK INTVLV 873100212 LKHEED 188 188C 5262604 SO CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 2007 RT FWD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1998120400428 19981204 00428 NM 1998 12 4 CALA9802121 1 19981130 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 1110 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 1110, RBL 44. THE CORRODED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IA W SRM 51-10-2 AND 53-10-8, PAGE 44. 2 L 7 3 4F RT A3WE 1998120400429 19981204 00429 NM 1998 12 4 CALA9802122 1 19981130 A 2782 BRACKET BOEING 727 727243 138408D NM NR 6 LE FLAP ACT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .5 INCH CRACK IN RT WING NR 6 LEADING EDGE FLAP ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-10-2 AND 51-30-7. 2 L 7 3 4F RT A3WE 1998120400430 19981204 00430 NM 1998 12 4 CALA9802123 1 19981130 A 5320 WEB BOEING 727 727243 138408D NM BS 378 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND WEB CORRODED WHERE R-1 FORWARD DRAIN LINE FITTING ATTACHES, FS 378. THE CORRODED AREA OF WEB WAS REMOV ED IAW SRM 51-40-2. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-2, PAGE 7 AND 51-10-2, PAGE 2. 2 L 7 3 4F RT A3WE 1998120400431 19981204 00431 NM 1998 12 4 CALA9802124 1 19981130 A 5320 SUPPORT BOEING 727 727243 138408D NM BS 420 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND CABIN FLOOR SUPPORT ANGLE CORRODED AT STA 420, RBL 62. THE FLOOR SUPPORT ANGLE WAS REMOVED AND REPLACE D IAW 53-30-2 AND 51-30-2. 2 L 7 3 4F RT A3WE 1998120400432 19981204 00432 NM 1998 12 4 CALA9802125 1 19981130 A 5321 FLOOR BOEING 727 727232 1384082 NM BS 1111-1183 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND CORROSION ON RT AFT LAV FLOOR PAN AT BS 1111 TO 1183. THE FLOOR PAN WAS REMOVED AND A NEW PAN WAS INST ALLED IAW SRM 51-30-2, 51-40-2 FIGURE 1, 51-10-2 AND MM 51-20-11. 2 L 7 3 4F A3WE 1998120400433 19981204 00433 NM 1998 12 4 9810412288 1 19980910 A 5314 KEEL BEAM BOEING 727 727251 138408H NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 288US 21376 DURING M-CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF LEFT KEEL BEAM AT FS 950 AND 970. REPAIRED PER EA 22-15996 AND EA 22-15999 (P/N 65-5644-1). 2 L 7 3 4F A3WE 1998120400434 19981204 00434 NM 1998 12 4 9810422710 1 19981005 A 5314 KEEL BEAM BOEING 727 727225 1384077 NM BS 950 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 820EA 22557 DURING H-CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF RIGHT KEEL BEAM AT FS 950, STR 29L - 29R. REPAIRED PER EA 27-1607 38. 2 L 7 3 4F A3WE 1998120400435 19981204 00435 NM 1998 12 4 9810436730 1 19980812 A 5754 WEB BOEING 747 7472J9F 1384806 NM NR 15 LE FLAP CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING M-CHECK, FOUND CRACK ON CENTER WEB TO FITTING ON RIGHT WING, NR 15 KRUEGER FLAP. REPAIRED PER EA 67-162311. 2 L 7 4 4F RT A20WE 1998120400436 19981204 00436 NM 1998 12 4 9810446730 1 19980817 A 5311 FRAME BOEING 747 7472J9F 1384806 NM BS 360 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 630US 21668 DURING M-CHECK, FOUND CRACK IN FRAME FLANGE AT STRINGER CUTOUT, UPPER DECK FS 360, STR 1R. REPAIRED PER EA 67-162325 (P /N 6DB1711-642). 2 L 7 4 4F RT A20WE 1998120400437 19981204 00437 WP 1998 12 4 9810459910 1 19981009 A 5312 BULKHEAD DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 960N 47256 DURING SURVEILLANCE INSPECTION, FOUND CRACK ON UPPER LEFT CORNER OF AFT PRESSURE BULKHEAD VENTRAL DOOR CUTOUT. REPAIRED PER EA 99-160501 (P/N 5910130-9). 2 L 7 2 4F A6WE 1998120400438 19981204 00438 WP 1998 12 4 9810469953 1 19981106 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 180 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 918RW 47158 DURING M-CHECK, FOUND CRACK AT FORWARD ENTRY DOOR JAMB LOWER DEPRESSOR ANGLES FS 180. REPAIRED PER EA 99-160834 (P/N 59 57094-1). 2 L 7 2 4F A6WE 1998120400439 19981204 00439 WP 1998 12 4 9810479916 1 19981016 A 5320 BEAM DOUG DC9 DC932 3022066 WP BS 756 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 949N 47566 DURING M-CHECK, FOUND CRACK IN VERTICAL SUPPORT BEAM AT FS 756, 24 INCHES TO THE LEFT A/C CENTERLINE. REPAIRED PER EA 9 9-159451 (P/N 9958212-7). 2 L 7 2 4F A6WE 1998120400440 19981204 00440 WP 1998 12 4 9810489942 1 19981012 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3991C 47175 DURING M-CHECK, FOUND CRACK IN SKIN FASTENER HOLE AT FS 110 BETWEEN LONGERONS 25R AND 26R. REPAIRED PER EA 99-160832. 2 L 7 2 4F A6WE 1998120400441 19981204 00441 WP 1998 12 4 9810499942 1 19980923 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 3991C 47175 DURING M-CHECK, FOUND CRACK ON FRAME WEB AT FS 1038, INBOARD OF LONGERON 14R, EMITTING FROM UNDER STIFFENER. REPAIRED P ER EA 99-162759. 2 L 7 2 4F A6WE 1998120400442 19981204 00442 WP 1998 12 4 9810509970 1 19980929 A 5711 SPAR CAP DOUG DC9 DC931 3022065 WP WS 353 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9334 47247 DURING M-CHECK, A CRACK WAS FOUND IN THE REAR SPAR LOWER CAP AT FS XRS 353. REPAIRED PER EA 99-159317 (P/N 5911301-502) . 2 L 7 2 4F A6WE 1998120400443 19981204 00443 SO 1998 12 4 COMA9810272 1 19981130 A 2752 3082001007 ACTUATOR EMB 120 EMB120RT SO LT TE FLAP MALFUNCTION A COMA K NONE O OTHER DE DESCENT 1 SO 01 152CA 13702 120152 FLAP CONTROL FAULT DURING APPROACH. REPLACED THE LEFT HAND NACELLE FLAP ACTUATOR. 2 L 7 2 4T RT A31SO 1998120400444 19981204 00444 EA 1998 12 4 COMA9860370 1 19981130 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 929CA 7035 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. INSPECTED AND FOUND NO DEFECTS WITH DOOR HANDLE. 2 L 7 2 4F RT A21EA 1998120400445 19981204 00445 EU 1998 12 4 QXEA9801756 1 19981127 A 3350 5515900004 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 478US 11227 EXIT SIGN ABOVE GALLEY HAS 6 28V LAMPS OUT. MAINTENANCE REMOVED AND REPLACED THE CIRCUIT BOARD ASSEMBLY, OPERATIONAL TE ST NORMAL. 2 L 7 2 4F RT A20EU 1998120400446 19981204 00446 EU 1998 12 4 QXEA9801757 1 19981124 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU CARGO COMPT INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 484US 7659 16 11234 RIGHT HAND FORWARD EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED SELF CONTAINED BATTERY POWER SUPPLY IN FO RWARD BELLY CARGO COMPARTMENT, OPERATIONAL TESTS WERE NORMAL. 2 L 7 2 4F RT A20EU 1998120400447 19981204 00447 EU 1998 12 4 QXEA9801758 1 19981128 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU SEAT 5B FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 EVACUATION LIGHT AT SEAT 5B INOPERATIVE. MAINTENANCE RESPLICED WIRES UNDER THE SEAT, OPERATIONAL TEST WAS NORMAL. 2 L 7 2 4F RT A20EU 1998120400448 19981204 00448 EU 1998 12 4 QXEA9801759 1 19981127 A 3350 6008905 POWER SUPPLY FOKKER F28 F28MK4000 4990810 EU ROW 2 & 4 INOP A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 498US 11181 EVACUATION LIGHTS AT ROWS 2 AND 4 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY, OPERATIONALLY TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998120400449 19981204 00449 NM 1998 12 4 98FDEA00719 1 19981201 A 5321 65189155 FLOOR BOEING 727 72725 1384006 NM BS 298 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 506FE 18277 NR 0444 CORROSION ON FLOOR PANEL CUTOUT UNDERSIDE AT BS 298, WL 178, LBL 31. *S/D* REMOVED WEB SECTION BS 294 TO 320, LBL 25 TO LBL 35. FABRICATED NEW WEB AND INSTALLED IAW FEDEX DRG 65-18915 AND FEDEX EA 7-5310-43158. 2 L 7 3 4F A3WE 1998120400450 19981204 00450 WP 1998 12 4 ABXA9801105 1 19981031 A 5712 576947025 RIB DOUG DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION FS 785. REPAIRED IAW DWG K05056. 2 L 7 4 4F 4A25 1998120400451 19981204 00451 WP 1998 12 4 ABXA9801106 1 19981031 A 5712 57694667 RIB DOUG DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS591.250. REPAIRED IAW SRM 51-1-20D. 2 L 7 4 4F 4A25 1998120400452 19981204 00452 WP 1998 12 4 ABXA9801107 1 19981104 A 5320 37741187 ANGLE DOUG DOUG DC8 DC863 302198A WP BS 1750 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 ELEVATOR UP CABLE FEED THROUGH BRACKET CRACKED AT RBL 24, STATION 1750. REPAIRED IAW ABX REA D853-24898MR. 2 L 7 4 4F 4A25 1998120400453 19981204 00453 WP 1998 12 4 ABXA9801108 1 19981116 A 5521 5910411515 SPAR DOUG DOUG DC9 DC941 302207N WP LT ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 WHILE COMPLYING WITH AD 79-19-02, FOUND LEFT ELEVATOR CRACKED IN FRONT SPAR AREA. REPLACED ELEVATOR IAW DC9 MM 27-30-02 AND 27-30-03. 2 L 7 2 4F A6WE 1998120400454 19981204 00454 WP 1998 12 4 ABXA9801109 1 19981104 A 5320 59197415 INTERCOSTAL DOUG DOUG DC9 DC931 3022065 WP BS 507 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND INTERCOSTAL CRACKED AT STATION 507 AT RBL 50. REPAIRED IAW ABX REA D938-25412. 2 L 7 2 4F A6WE 1998120400455 19981204 00455 WP 1998 12 4 ABXA9801110 1 19981104 A 5320 995823869 SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND FUSELAGE FRAME SHEAR TIE CRACKED AT STATION 980 LEFT, BEHIND LONGERON 17L. REP LACED SHEAR TIE IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998120400456 19981204 00456 WP 1998 12 4 ABXA9801111 1 19981024 A 5400 99155016 PYLON DOUG DOUG DC9 DC931 3022065 WP NR 2 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND NR 2 PYLON CRACKED INTERNALLY, JUST AFT OF THE AFT SPAR. REPAIRED CRACK IAW AB X REA D954-25253 AND ABX DWG K05159. 2 L 7 2 4F A6WE 1998120400457 19981204 00457 WP 1998 12 4 ABXA9801112 1 19981105 A 5730 9919470505 SKIN DOUG DOUG DC9 DC931 3022065 WP LT WING CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT WING OUTBOARD TRAILING EDGE SECTION HAD EXTENSIVE CORROSION ON INNER S URFACE OF UPPER SKIN AROUND FINGER DOUBLERS. REPLACED SKIN IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998120400458 19981204 00458 WP 1998 12 4 ABXA9801113 1 19981113 A 5320 995823870 SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND FRAME SHEAR TIE CRACKED AT STATION 980 AND LONGERON 17 RIGHT. REPLACED SHEAR T IE IAW DC9 SRM CHAPTER 53-03, FIGURE 32. 2 L 7 2 4F A6WE 1998120400459 19981204 00459 WP 1998 12 4 ABXA9801114 1 19981103 A 5313 27779225 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 & 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 17 LEFT CRACKED AT STATION 965 AND 980. REPLACED LONGERON SECTION IAW DC9 SUPPLEMENTAL SRM DWG K05864. 2 L 7 2 4F A6WE 1998120400460 19981204 00460 WP 1998 12 4 ABXA9801115 1 19981102 A 5313 27779226 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 & 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 17 RIGHT CRACKED AT STATION 965 AND 980. REPLACED LONGERON SECTION IA W DC9 SUPPLEMENTAL SRM DWG K05864. 2 L 7 2 4F A6WE 1998120400461 19981204 00461 WP 1998 12 4 ABXA9801116 1 19981030 A 5320 WEB DOUG DOUG DC9 DC931 3022065 WP BS 960 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE LEFT CUSP MEMBRANE CRACKED AT STATION 960. REPLACED CUSP WEB IAW DC9 SRM 5 1-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998120400462 19981204 00462 WP 1998 12 4 ABXA9801117 1 19981026 A 5313 591486529N LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 604 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND CORROSION ON THE PRESSURE PANEL LONGERON TEE CAP AT STATION 604, BETWEEN LONGER ONS 29 LEFT AND 29 RIGHT. REPLACED TEE CAP IAW DC9 SRM 51-30-1 AND 51-30-2. 2 L 7 2 4F A6WE 1998120400463 19981204 00463 WP 1998 12 4 ABXA9801118 1 19981026 A 5320 59203321 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 579-598 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND LONGERON 29 RIGHT END FITTING CORRODED AT STATION 579 TO 598. REPLACED LONGERO N END FITTING IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998120400464 19981204 00464 WP 1998 12 4 ABXA9801119 1 19980813 A 5320 97549453 JAMB DOUG DOUG DC8 DC861 3021952 WP C-3 DOOR CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 850AX 45894 DOOR JAMB WEB HAS CORROSION AT STATION X1.38 X 5.80 (C-3 DOOR). REPAIRED IAW ABX REA D853-24258MR. 2 L 7 4 4F 4A25 1998120400465 19981204 00465 WP 1998 12 4 ABXA9801135 1 19981129 A 3350 60030451 POWER SUPPLY DOUG DC9 DC941 302207N WP CABIN INOP A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 952AX 4843 47615 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY. 2 L 7 2 4F A6WE 1998120400466 19981204 00466 WP 1998 12 4 MWEA981113 1 19981125 A 2560 3552273501 LATCH DOUG DC9 DC915 3022036 WP GIRT BAR LACK OF LUBE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 300ME 45718 GIRT BAR LATCHES HARD TO OPERATE ON FORWARD ENTRY DOOR. CLEANED AND LUBRICATED FORWARD ENTRY DOOR ESCAPE SLIDE GIRT BAR LATCHES. 2 L 7 2 4F A6WE 1998120400467 19981204 00467 WP 1998 12 4 MWEA981114 1 19981129 A 2560 5956953503 COVER DOUG DC9 DC981 3022081 WP ESCAPE SLIDE LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 809ME 48071 LGA - FLT 5 - AFT GALLEY DOOR ESCAPE SLIDE COVER CAME LOOSE. RE-SECURED AFT GALLEY DOOR SLIDE COVER. (X) 2 L 7 2 4F A6WE 1998120400468 19981204 00468 WP 1998 12 4 MWEA981115 1 19981128 A 2560 5917689103 COVER DOUG DC9 DC932 3022066 WP ESCAPE SLIDE LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 212ME 47701 MKE - FLT 95 - GALLEY DOOR EVACUATION SLIDE COVER FELL OFF. RE-INSTALLED FORWARD GALLEY DOOR SLIDE COVER. (X) 2 L 7 2 4F A6WE 1998120400469 19981204 00469 NM 1998 12 4 VNAA9811024 1 19981126 A 3610 4069B000 VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE FUSELAGE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 436JS 82721 3052 DURING THE TAXI PRIOR TO TAKEOFF, A CROSS-BLEED FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE GATE. M AINTENANCE INSPECTED AND REPLACED THE CROSS-BLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-10. OPERAT IONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998120400470 19981204 00470 NM 1998 12 4 VNAA9811025 1 19981129 A 6120 D11992 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT ENGINE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 457PS 82345 61747 3048 THE RIGHT HAND PROPELLER FAILED TO COME OUT OF FEATHER WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE I NSPECTED AND REPLACED THE RIGHT HAND PROPELLER CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OP ERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998120400472 19981204 00472 SW 1998 12 4 98ZZZX4431 1 19981029 A 2910 70060T000Y310 LINE BELL 214 214ST 1182106 SW HYDRAULIC SYSTEM CHAFED A HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 6957Y 28139 AIRCRAFT DEPARTED, LOST NR 2 HYDRAULIC PRESSURE. AIRCRAFT RETURNED TO BASE. FOUND LINES, ITEMS 23 AND 24, CHAFED. NR 2 HYDRAULIC SYSTEM TO COLLECTIVE SERVO. REF: 214ST IBB, FIGURE 29.5, ITEMS 23 AND 24. 2 G 7 2 4U H10SW 1998120400473 19981204 00473 SW 1998 12 4 98ZZZX4432 1 19981029 A 2910 70060Y000Y310 LINE BELL 214 214ST 1182106 SW HYDRAULIC SYSTEM CHAFED A HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 6957Y 28139 AIRCRAFT DEPARTED, LOST NR 2 HYDRAULIC PRESSURE. AIRCRAFT RETURNED TO BASE. FOUND LINES, ITEMS 23 AND 24, CHAFED. NR 2 HYDRAULIC SYSTEM TO COLLECTIVE SERVO. REF: 214ST IBB, FIGURE 29.5, ITEMS 23 AND 24. 2 G 7 2 4U H10SW 1998120400485 19981204 00485 1998 12 4 DKAA98018 4 19981014 A 3414 42218152308 INDICATOR AMD FALC20 FALCON20C5 2730107 EU COCKPIT INOPERATIVE A DKAA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 23 810RA 560 81 NR 1 AIRSPEED INDICATOR INOPERATIVE. UPON V1 CALLOUT AIRSPEED DROPPED TO 105 KIAS AND FROZE. AT LEVEL CRUISE, 200 KNOT S IT INDICATES 160 KNOTS AND BLEED OFF TO 0 ON SHORT FINAL. REPLACED STATIC DEFECT CORRECTION MODULE IAW AMD MM 54-10. SYSTEM OPERATIONAL AND LEAK CHECKS GOOD PER FAR 43 APPENDIX E. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A7EU 1998120400486 19981204 00486 SW 1998 12 4 98ZZZM905 1 19981016 A 7603 POWER LEVER SWRNGN SA227 SA227AC 8780603 SW COCKPIT OUT OF RIG A EQGA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 19 704C 704 DFW - FLT 1253 - DURING SETTING OF T/O PWR, CREW EXPERIENCED MINOR RPM FLUX ON THE LT ENG, THRU RPM STABILIZED AT 99.5 P ERCENT. RT ENG OP NORMALLY. AT FIRST PWR REDUCTION ON CLIMB-OUT, CREW NOTICED LT PWR LEVER WAS PULLED BACK TO FLT IDLE GATE AND THE TQ WAS STILL 35 PERCENT. CREW ADVISED MX CONTROL AND SUGGESTED TURNING LT SRL OFF. CREW DID THIS WITH NO CHANGE TO LT TQ THOUGH EGT INCREASED 30 DEGREES CELSIUS. CREW DECIDED TO RETURN TO DFW AND SHUT DOWN ENG AND DECLARED AN EMERG. CREW EXECUTED PRE-PLANNED ENG SHUT DOWN CHECKLIST AND MADE AN UNEVENTFUL LANDING IN DFW. MX INSPECTED THE A/ C AND DETERMINED THE LT ENG PEDASTAL RIGGING WAS OFF. MX RE-RIGGED POWER LEVER HOUSING AND INTERNAL POWER LEVER CABLE A 2 L 7 2 4T RT A8SW 1998120400487 19981204 00487 NE 1998 12 4 98ZZZM906 2 19981017 A 7412 103243303 IGNITOR BOX LEAR 25 25 5170506 CE GE CJ610 CJ6106 30006 NE RT ENGINE FAILED A EXOA B EMER. DESCENT X J ENGINE FLAMEOUT WARNING INDICATION CL CLIMB 1 SO 17 20HJ 024 251066A RIGHT ENGINE FLAMED OUT AT FL 400, DESCENDED BELOW FL 250, ATTEMPTED RESTART 3 TIMES, SECURED ENGINE LANDED ILM. FOUND IGNITOR BOX. INOP, REPLACED IGNITOR BOX GROUND RUN/POWER RUN NORMAL. UNABLE TO DETERMINE CAUSE OF FLAME OUT AT THIS TI ME. 2 L 7 2 4J 4 J A10CE 1E16 1998120400488 19981204 00488 WP 1998 12 4 GTIA9800108 1 19980929 A 3350 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 ACY - FLT 348 - ON PREFLIGHT, FIVE OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. REMOVED AND REPLACED NICAD BATTERIES AND BULBS WHERE NEEDED IAW MM 33-40 AND OPERATIONAL CHECKS OK. (M) 2 L 7 2 4F A6WE 1998120400489 19981204 00489 NM 1998 12 4 P2EA98192 1 19981025 A 2612 655280915 FIRE DETECTOR BOEING 737 737297 1384480 NM E/E BAY FAILED A P2EA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J N WARNING INDICATION FALSE WARNING DE DESCENT 1 CE 05 5WM D00596 22629 FLT 404 - MCI - 15 MINS BEFORE LANDING, STARTED GETTING QUICK INTERMITTENT FLASHES ON THE NR 1 ENGINE FIRE WARNING SWITC H. STOPPED FOR 5 MINUTES, THEN STARTED AGAIN. CONTINUED TO LANDING. DECLARED EMERGENCY AND SHUT DOWN NR 1 ENGINE AFTE R LANDING. PULLED FIRE SWITCH AND FIRED LEFT EXTINGUISHER BOTTLE. TROUBLSHOT PER MM 26-11-0, CHECKED CONTINUITY OF FIR ELOOPS, OK. CHECK FOR RESISTANCE TO GROUND, OK. FOUND NR 1 FIRE TEST INOP. REPLACED FIRE DETECTOR UNIT PER MM 26-11-0 , OPS CHECK OK. REPLACED NR 1 FIRE BOTTLE PER MM 26-21-11, PAGES 401-404. (M) 2 L 7 2 4F A16WE 1998120400490 19981204 00490 CE 1998 12 4 RU3A9805 1 19981006 A 2610 FIRE LOOP RKWELL NA265 NA26580 7630108 CE RT ENGINE MALFUNCTIONED A RU3A O OTHER J WARNING INDICATION CR CRUISE 1 SW 21 58 38024 RIGHT ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT. ENGINE POWER LEVER WAS BROUGHT BACK TO IDLE AND LIGHT EXTINGUISHED. RET URN TO STATION WITHOUT FURTHER INCIDENT. (M) 2 L 7 2 4F A2WE 1998120400491 19981204 00491 EU 1998 12 4 SIMA982841 1 19981011 A 3234 D49412001 CONTROL HANDLE SAAB SF340 340B 7860101 EU COCKPIT MALFUNCTIONED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 232AE 3100690 340B232 DFW - FLT 3232 - UNSAFE GEAR INDICATION ON ALL THREE GEAR. RESET CIRCUIT BREAKERS, RECYCLED GEAR, ALL THREE STILL UNSAF E. BULBS TEST OK. INTRANSIT LIGHTS WORKS OK. PULLED EMERGENCY EXTENSION HANDLE, THEN GEAR INDICATED SAFE. REMOVED AN D REPLACED LANDING GEAR CONTROL HANDLE AND OPERATIONAL CHECKED WITH NO DEFECTS NOTED. INSTALLED NEW EXPLOSIVE BOLTS AND RESET EMERGENCY HANDLE. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998120400492 19981204 00492 EU 1998 12 4 SIMA982862 1 19981013 A 3230 HP848430621 CONTROL VALVE SAAB SF340 340B 7860101 EU NLG WW INOPERATIVE A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 232AE 1294 340B232 DFW - FLT 3932 - WHEN GEAR WAS SELECTED TO DOWN POSITION, THE INTRANSIT LIGHT ILLUMINATED, AND THE HYDRAULIC PUMP WAS OB SERVED TO BE RUNNING, BUT THE GEAR STILL SEEMED TO BE ON THE UPLOCKS. CIRCUIT BREAKERS WERE RESET PER QRH AND HANDLE PO SITION CYCLED, STILL NO GREEN LIGHT INDICATIONS. GEAR CAME DOWN WITH 3 GREEN LIGHTS WHEN EMERGENCY LANDING GEAR EXTENSI ON HANDLE WAS PULLED. NOSE WHEEL STEERING WAS ALSO INOPERATIVE AFTER LANDING. REMOVED AND REPLACED LANDING GEAR CONTRO L VALVE FOR BOTH LANDING GEAR PROBLEM AND STEERING PROBLEM. REMOVED AND REPLACED THE GEAR DOOR EXPLOSIVE BOLTS. SYSTEM S LEAK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998120400493 19981204 00493 WP 1998 12 4 USAAD98182 1 19981013 A 5230 DOOR DOUG DC9 DC931 3022065 WP CARGO BAY UNLATCHED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 978VJ 47371 TOL - CAK FLT 7002, AIRCRAFT FAILED TO PRESSURIZE ON LIFT OFF. A SEVERE BUFFETING OCCURRED ON CLIMB-OUT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD CARGO DOOR OPEN. NO DAMAGE WAS NOTED TO THE AIRCRAFT AND THE FORWARD CARGO DOOR WARNING SYSTEM WAS PLACED ON MEL. DURING THE OVERNIGHT MAINTENANCE VISIT, TH E DOOR WARNING SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998120400494 19981204 00494 WP 1998 12 4 SABA980050 2 19981008 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UHR WP RIGHT FAILED A SABA E ENGINE SHUTDOWN R J PARTIAL RPM/PWR LOSS WARNING INDICATION AP APPROACH 1 SO 33 941AE 941 P66337C RDU - FLT 5215 - RIGHT ENGINE LOST RPM AND OIL PRESSURE. SHUT THE ENGINE DOWN. CREW DECLARED EMERGENCY. AIRCRAFT LAND ED SAFELY NO INCIDENTS. REMOVED AND REPLACED RIGHT ENGINE IAW JE32 MM ATA 71-00-01. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1998120400495 19981204 00495 EU 1998 12 4 USAAF98084 1 19981008 A 2760 SENSOR FOKKER F28 F28MK0100 4990807 EU LIFTDUMPER OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 895US 11380 CLT - FLT 1856 - AFTER TAKEOFF FROM CLT, CREW RECEIVED SEVERAL LIFTDUMPER UNSAFE WARNINGS AND LIFTDUMPER FAULTS. NO EME RGENCY WAS DECLARED, HOWEVER, FLIGHT RETURNED TO CLT. FLIGHT LANDED CLT WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED RIGHT SIDE LIFTDUMPER INLOCK SENSOR NR 2 AND SECURED NR 4 SENSOR BRACKET. (M) 2 L 7 2 4F RT 1998120400496 19981204 00496 EU 1998 12 4 USAAF98086 1 19981009 A 2120 AIR DIST FOKKER F28 F28MK0100 4990807 EU COCKPIT ODOR A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 852US 11280 PIT - FLT 1809 - EN ROUTE TO CRW FROM PIT, FLIGHT CREW NOTICED AN ELECTRICAL SMELL IN THE COCKPIT. THERE WAS NO VISIBLE SMOKE. FLIGHT ATTENDANTS ALSO NOTICED THE SMELL IN THE CABIN. THE FLIGHT CREW INSTRUCTED THE FLIGHT ATTENDANTS TO SHU T OFF THE COFFEEMAKERS. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPENED ALL PANELS IN C OCKPIT, GALLEY AND ELECTRICAL BAYS. ALSO, CHECKED FORWARD AND AFT AVIONICS BAYS. RAN ENGINES. NO FAULTS NOTED. NO EL ECTRICAL SMELLS NOTED. (M) 2 L 7 2 4F RT 1998120400497 19981204 00497 EU 1998 12 4 C2XA98BT063 1 19980902 A 2730 CONNECTOR AEROSP ATR42 ATR42320 8680930 EU ELEVATOR LOOSE A C2XA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 09 14822 163 FLIGHT 3389 - ON TAKEOFF FROM EWR, PITCH DISCONNECTED ON TAKEOFF. MAINTENANCE RECONNECTED PITCH UNCOUPLING MECHANISM PE RFORMED FUNCTIONAL TEST AND RECONNECTED. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998120400498 19981204 00498 WP 1998 12 4 EISA98221 1 19980919 A 3520 OXYGEN PANEL DOUG DC9 DC931 3022065 WP COCKPIT MALFUNCTIONED A EISA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 950VJ 47564 DURING CRUISE FLIGHT, BLUE OXYGEN LIGHTS AT FLIGHT ATTENDANT JUMPSEAT ILLUMINATED. AFTER TESTING COCKPIT ANNUNCIATOR. T HE CABIN OXYGEN LIGHTS IN COCKPIT ILLUMINATED AIR TURN BACK TO ACY FOR MAINTENANCE. GENERATED FROM PILOT REPORT. PERFO RMED OPS CHECK IAW 35-20-0. LEAK CHECK GOOD, NO MALFUNCTION FOUND WITH SYSTEM. (M) 2 L 7 2 4F A6WE 1998120400499 19981204 00499 NM 1998 12 4 USAA980552 1 19981029 A 5313 STRINGER BOEING 737 7372B7 1384560 NM BS 907 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 6 INCH CORRODED AREA STATION 907, STRINGER 26L. CORROSION TASK NR C53 -208-01. INSTALLED NEW STRINGER AND STRINGER SPLICES PER SRM 53-10-3. (M) 2 L 7 2 4F A16WE 1998120400500 19981204 00500 NM 1998 12 4 USAA980554 1 19981029 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 1146 CREASED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CREASE APU DOOR AFT LATCH CUTOUT AT STATION 1146 ON SKIN. INST ALLED DOUBLER PER EA 62761. (M) 2 L 7 2 4F A16WE 1998120400501 19981204 00501 NM 1998 12 4 USAA980553 1 19981029 A 5330 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT ENTRY DOORWAY AT LOWER HINGE CUTOUT ON FUSELAGE SKIN . INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 34 AND TR 53-30-11. (M) 2 L 7 2 4F A16WE 1998120400502 19981204 00502 NM 1998 12 4 USAA980551 1 19981029 A 5320 ANGLE BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH STATION 727 WL 200 LBL 45 CHORD ANGLE. INSTALLED REPAIR ANGLE PER TR 53-10-03A. (M) 2 L 7 2 4F A16WE 1998120400503 19981204 00503 NM 1998 12 4 USAASB98290 1 19981030 A 2130 39606411 PACK VALVE BOEING 737 7372B7 1384560 NM A/C BAY MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 266AU 22878 PHL - FLT 1264 - AT APPROXIMATELY 400 FT, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED. CREW SWITCHED OVER TO STANDBY MODE AND COULD NOT CONTROL RATE OF CLIMB IN CABIN. CREW THEN TRIED MANUAL MODE AND AIRCRAFT STILL WOULD NOT PRESSURIZE . FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REP LACED THE E/E PRESSURE REGULATING VALVE AND THE RIGHT PACK FLOW CONTROL VALVE PER MM. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998120400504 19981204 00504 NM 1998 12 4 98ZZZM907 1 19981030 A 2130 327375 VALVE BOEING 737 7372B7 1384560 NM A/C BAY MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 266AU 22878 PHL - FLT 1264 - AT APPROXIMATELY 400 FT, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED. CREW SWITCHED OVER TO STANDBY MODE AND COULD NOT CONTROL RATE OF CLIMB IN CABIN. CREW THEN TRIED MANUAL MODE AND AIRCRAFT STILL WOULD NOT PRESSURIZE . FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REP LACED THE E/E PRESSURE REGULATING VALVE AND THE RIGHT PACK FLOW CONTROL VALVE PER MM. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998120400505 19981204 00505 WP 1998 12 4 USAAD98188 1 19981021 A 3260 BULB DOUG DC9 DC931 3022065 WP COCKPIT FAILED A USAA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 EA 19 963VJ 47508 BNA-PHL - FLT 1952 - DURING APPROACH, THE LANDING GEAR WAS LOWERED BUT THE CREW DID NOT GET A POSITIVE NOSE GEAR INDICAT ION. A GO-AROUND WAS INITIATED. THE CREW CHANGED THE LIGHT BULB AND RECYCLED THE GEAR AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. (M) 2 L 7 2 4F A6WE 1998120400506 19981204 00506 1998 12 4 USAASB98255 4 19980925 A 3442 20412170416 RADAR UNIT BOEING 737 737401 1384701 NM E/E BAY FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 405US 25947 23885 CLT - FLT 401 - EN ROUTE FROM LGA TO TPA, THE AIRCRAFT WEATHER RADAR BEGAN SPIKING IN VARIOUS QUADRANTS AT VARIOUS TIMES IN ALL RANGES BETWEEN 20-320 MILES. ADJUSTED GAIN FROM MINIMUM TO MAXIUM WITH NO IMPROVEMENT NOTED. RADAR GIVES UNREL IABLE PRESENTATION. FLIGHT DIVERTED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANC E REMOVED AND REPLACED THE WEATHER RADAR TRANSCEIVER. GROUND OPERATIONAL CHECK GOOD. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A16WE 1998120400507 19981204 00507 NM 1998 12 4 USAASB98161 1 19980627 A 2420 6130200003 HARNESS BOEING 737 737201 1384454 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 248US 22755 SAV - FLT 2238 - SHORTLY AFTER TAKEOFF, THE NR 2 ENGINE GENERATOR DROPPED OFF LINE. AFTER LEVELING OFF, THE CREW TRIED TO PUT THE GENERATOR BACK ON LINE BUT WAS NOT SUCCESSFUL. THE NR 1 ENGINE CSD WAS ALREADY ON MEL AND WITH THE APU BEING THE ONLY SOURCE OF POWER, THE CREW ELECTED TO RETURN TO FIELD AT SAV. FLIGHT LANDED WITHOUT INCIDENT AND NO EMERGENCY BEING DECLARED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE GENERATOR FEEDER WIRE HARNESS. GROUND OPERATIONAL CHE CK GOOD. CLEARED MEL ON THE NR 1 ENGINE CSD BY REPLACEMENT OF THE OIL COOLER ASSEMBLY AND THE CSD. OPERATIONAL CHECK G OOD. (M) 2 L 7 2 4F A16WE 1998120400508 19981204 00508 1998 12 4 USAASB98283 4 19981026 A 2210 4030952906 YAW DAMPER BOEING 737 737401 1384701 NM E/E BAY FAILED A USAA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 19 421US 34900 23988 CLT - FLT 1669 - ON TAKEOFF ROLL AT 110-120 KNOTS, THE AIRCRAFT PULLED HARD TO THE LEFT AND THE CREW HEARD A LOUD BANG. THE AIRCRAFT ROTATED AND THE CREW SUSPECTED A BLOWN TIRE. CHECKLIST WAS ACCOMPLISHED AND THE FLIGHT RETURNED TO FIELD AT CLT. NO EMERGENCY WAS DECLARED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE UNDER ITS OWN POWER. AT THE GATE, NO BLOWN TIRES WERE FOUND. MAINTENANCE FOUND THE YAW DAMPER COUPLER HAD FAILED. REPLACED SAME. BITE AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F RT A16WE 1998120400509 19981204 00509 NM 1998 12 4 GAIA9891 1 19981015 A 5753 FLAP BOEING 727 727223 1384074 NM WING LACK OF LUBE A GAIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SW 07 6821 19496 ON DEPARTURE FROM OAK, OUTBOARD FLAPS LOCKED AT 2 DEGREES, AND INBOARD FLAPS FUNCTIONED NORMALLY. DECLARED AN EMERGENCY AND RETURNED TO OAK AND LANDED WITHOUT ANY FURTHER PROBLEMS. CLEANED, LUBED, AND OPERATIONAL CHECKED THE FLAP SYSTEM T HROUGH SEVERAL CYCLES. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998120400510 19981204 00510 NM 1998 12 4 GAIA98103 1 19981028 A 5260 65262116711 RISER BOEING 727 727224 1384076 NM AIRSTAIR CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69740 20668 DURING ROUTINE HEAVY CHECK, INSPECTION FOUND CORROSION ALONG 6 OF THE AFT AIRSTAIR RISERS. FABRICATION OF PARTS WAS NEC ESSARY DO TO LENGTH IN LEAD TIME FROM BOEING. THE RISERS WHERE REPLACED WITH RISERS FABRICTED USING FLIGHT VEHICLES INC REPAIR SKETCH 52-98515-3. THEN AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998120400511 19981204 00511 NE 1998 12 4 VTZA98285 2 19980907 A 7532 VALVE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A1 30015 NE COMPRESSOR FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 621BR 7186 FLT 6700 - IAD-BNA - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO 10 TH STAGE BLEED AIR SHOWS PSI WITH VAL VE CLOSE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 1998120400512 19981204 00512 1998 12 4 USAABB98101 4 19981006 A 3454 VOR BOEING 767 7672B7 1385107 NM COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 651US 24764 PHL - FLT EN ROUTE PHL-MAD, THE AUTOTHROTTLES FAILED. CREW WAS ABLE TO RESET. SUBSEQUENTLY, THE CREW RECEIVED THE EICA S MESSAGE 'LT FMT FAIL', AT WHICH TIME THE CENTER AUTOPILOT DISENGAGED. CREW WAS ABLE TO REGAIN USE OF LEFT FMC, BUT DE CIDED TO RETURN TO PHL. EN ROUTE PHL, THE RIGHT ADF FAILED ONCE AND THE RIGHT VOR FAILED THREE TIMES (CREW WAS ABLE TO STORE AFTER EACH FAILURE). FLIGHT LANDED AT PHL WITH NO FURTHER PROBLEMS. MAINTENANCE PERFORMED THE FIM PROCEDURE FOR THE FMC, AND FOUND NO PROBLEMS. THE RIGHT VOR AND RIGHT ADF RECEIVERS WERE REPLACED AS A PRECAUTION. (M) 2 L 7 2 4F RT A1NM 1998120400513 19981204 00513 NE 1998 12 4 USAASB98260 2 19981006 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D9A 52048 NE RIGHT FAILED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 227AU 52613 21816 674156 CLT - FLT 423 - ON CLIMB-OUT FROM CLT AT 1,500 FEET, THE NR 2 ENGINE SUDDENLY DROPPED TO IDLE THRUST. ENGINE WAS UNRESP ONSIVE TO THROTTLE MOVEMENT. ENGINE TEMPERATURES AND PRESSURE WERE NORMAL. GENERATOR REMAINED ON LINE. FLIGHT RETURNE D TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. THE NR 2 ENGINE WAS NOT SHUT DOWN IN FLIGHT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FUEL CONTROL UNIT, FUEL PUMP AND T2 SENSOR WITH NO HELP. REM OVED AND REPLACED THE NR 2 ENGINE DUE TO PERFORMANCE PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998120400514 19981204 00514 NE 1998 12 4 USAASB98263 2 19981006 A 7200 ENGINE BOEING 737 7372Q9 138448M NM PWA JT8 JT8D9A 52048 NE RIGHT FOD A USAA E A ENGINE SHUTDOWN UNSCHED LANDING C F.O.D. CL CLIMB 1 EA 19 230AU 44707 21975 687799 PHL - FLT 886 - DURING CLIMB-OUT FROM PHL AT APPROXIMATELY 1,100 FT, THE CAPTAIN REPORTED SEEING A LARGE BIRD GO PAST TH E AIRCRAFT. THE BIRD STRUCK THE NR 2 ENGINE CAUSING DAMAGE. CAPTAIN SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY A ND RETURNED TO FIELD AT PHL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSY PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998120400515 19981204 00515 EU 1998 12 4 DKAA98015 1 19981006 A 2720 1250B TRIM SWITCH AMD FALC20 FALCON20C5 2730107 EU COCKPIT FAILED A DKAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 23 810RA 81 SMOKE FROM CAPTAINS TRIM SWITCH RIGHT AFTER START. TRIM WAS NEVER ACTIVATED BUT IT WAS AUDIBLY 'RUNNING AWAY'. REPLACE D CAPTAIN CONTROL TAILPLANE TRIM SWITCH AND ASSOCIATED WIRING. SYSTEM OPERATIONAL CHECKS GOOD IAW MM 27-40. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4F RT A7EU 1998120400516 19981204 00516 EU 1998 12 4 DKAA98011 1 19980812 A 3231 VTS443 GEAR DOOR LOCK AMD FALC20 FALCON 2720302 EU LT MLG FAILED A DKAA O OTHER O OTHER CL CLIMB 1 GL 23 227R 44 227 AIRCRAFT DEPARTED UNDER PART 91 FOR YIP. CREW SELECTED GEAR UP AND NOTED LEFT GEAR DOOR UNLOCKED LIGHT STAYED ILLUMINAT ED. CREW CYCLED GEAR, LEFT GEAR DOOR UNLOCKED LIGHT STAYED ON. CREW RESTRICTED AIRCRAFT SPPED TO VLO PER CHECKLIST. U PON ARRIVAL AT YIP, MAINTENANCE FOUND LEFT GEAR DOOR (P/N MY20-293-10-F1) HAD DEPARTED AIRCRAFT DUE TO FRACTURES AT FORW ARD HINGE ARM (P/N MY20293-10811-5) AND AFT HINGE ARM (P/N MY20293-10821). FORWARD GEAR DOOR LOCK WAS SENT TO VENDOR FO R EVALUATION TO DETERMINE IF INTERNAL MICROSWITCH SEQUENCING PROBLEM WAS PRESENT. (M) 2 L 7 2 4F A7EU 1998120400517 19981204 00517 NE 1998 12 4 ORJA98252 2 19981005 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 FAILED A ORJA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 11 875RA 53182 AT LAX - AIR TURN BACK, AFTER ENGINES SPOOLED AND AUTO THROTTLES ON AS POWER ADVANCED THE RIGHT ENGINE POPPED AND STARTE D VIBRATING AFTER CLEARING RUNWAY, TRIED TO PULL RIGHT ENGINE UP, BUT IT DID NOT RESPOND N1 STAYED T 20 PERCENT N2 AT 44 PERCENT RIGHT ENGINE WAS SHUT DOWN. REPAIRED AND REPLACED NR 2 ENGINE. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1998120400518 19981204 00518 1998 12 4 ORJA98257 4 19981012 A 3197 WIRE DOUG DC9 DC983 3022083 WP INST PANEL FAILED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 876RA 53183 AT RENO, NR 2 AGENT LOW LIGHT INOP AT APU FIRE CONTROL PANEL AFT LEFT FUSELAGE. REMOVED AND REPLACED BROKEN GROUND WIRE TERMINAL. SECURED TERMINAL. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998120400519 19981204 00519 WP 1998 12 4 ORJA98258 1 19980919 A 5320 PIC23933 FASTENER DOUG DC9 DC982 3022082 WP SCUFF PLATE CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 LEVEL 2 CORROSION IN FUSELAGE ZONE. FASTENERS RUSTY AND LOOSE IN R1 DOOR LOWER EXTERNAL SCUFF PLATE. REMOVED AND REPLA CED CORRODED FASTENERS IAW DC9-SRM 51-10-5B. (M) 2 L 7 2 4F A6WE 1998120400520 19981204 00520 WP 1998 12 4 ORJA98259 1 19980921 A 5320 PLATE DOUG DC9 DC982 3022082 WP BS 1174 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 FOUND CORROSION ON ANTENNA BLOCK OFF PLATE AND SEALANT MISSING IN SET SCREWS, APP STATION 1174, STRINGER 30 LEVEL 2 CORR OSION. FABRICATED AND INSTALLED REPAIR PER DC-9 SRM 53-04, PAGE 37, FIG 12B, SHEET 3. LEAK CHECK IAW, MD-80, MM 21-00- 00. NO DEFECTS. (M) 2 L 7 2 4F A6WE 1998120400521 19981204 00521 WP 1998 12 4 ORJA98261 1 19980922 A 5320 FASTENERS DOUG DC9 DC982 3022082 WP CARGO BAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 824RA 53017 AT OKC, LEVEL 2 CORROSION AT MID PIT DRAIN HOLE AT STATION 788 HAS HARDWARE CORROSION. REMOVED CORRODED FASTENERS AND R EPLACED WITH NEW FASTENERS AND REPLACED WITH NEW FASTENERS IAW DC/MD80, SRM 51-30-5. LEAK CHECK IAW MD80 21-00-00. NO DEFECTS. (M) 2 L 7 2 4F A6WE 1998120400522 19981204 00522 EU 1998 12 4 REXA98114 1 19981025 A 2610 89905202 CONTROL BOX SAAB SF340 SF340A 7850100 EU RT NACELLE INOPERATIVE A REXA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. J WARNING INDICATION TO TAKEOFF 1 SO 25 327PX 0230 340A059 AFTER TAKEOFF GOT RIGHT 'FIRE WARNING'. COMPLIED WITH CHECKLIST AND BLEW FIRE BOTTLES, AND SHUTDOWN ENGINE. REMOVED AN D REPLACED FIRE BOTTLES. REMOVED AND REPLACED RIGHT FIRE LOOP CONTROL BOX. (M) 2 L 7 2 4T RT A52EU 1998120400523 19981204 00523 NM 1998 12 4 P2EA98232 1 19981011 A 5330 SKIN BOEING 737 737244 138448U NM BS 901 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PROVISIONAL FUSELAGE SKIN REPAIR AT BS 901, BETWEEN STRINGER 24 LT AND STRINGER 26 LT PER COOPESA EO C00-3-53-591- 98 DATED OCT 27, 1998 AND BOEING FAX C00-SJO-98-0830RR DATED OCT 26, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1998120400524 19981204 00524 NM 1998 12 4 P2EA98231 1 19981011 A 5330 SKIN BOEING 737 737244 138448U NM BS 1016 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - PROVISIONAL FUSELAGE SKIN REPAIR AT BS 1016, BETWEEN STRINGER 12 LEFT AND STRINGER 15 LEFT. REPLACED FUSELAGE SKI N SECTION FROM BS 989 TO BS 1016, BETWEEN STRINGER 10 LEFT AND STRINGER 14 LT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. R EPAIRED FUSELAGE SKIN SECTION FROM BS 999 TO BS 1016, BETWEEN STRINGER 13 LEFT AND STRINGER 17 LEFT PER COOPESA EO COO-3 -53-585-98 DATED OCT 22, 1998. (M) 2 L 7 2 4F A16WE 1998120400525 19981204 00525 NM 1998 12 4 P2EA98230 1 19981006 A 5330 SKIN BOEING 737 737244 138448U NM BS 286-292 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FORWARD SERVICE DOOR (R1) UPPER HINGE CUTOUT CRACKED, DEFECT SIZE, CANNOT DETERMINE. REPAIRED FUSELAGE SKIN FROM BS 286.5 TO BS 292.5, BETWEEN STRINGER 9 RT AND STRINGER 13 RT. (M) 2 L 7 2 4F A16WE 1998120400526 19981204 00526 NM 1998 12 4 P2EA98229 1 19981005 A 5315 FLOORBEAM BOEING 737 737244 138448U NM BS 663-673 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FLOORBEAM CRACKED IN MULTIPLE PLACES FROM BS 663 AND BS 673, LBL 24 INCHES, AVERAGE DEFECT SIZE, LENGTH .312 INCH. REPAIRED FLOORBEAM UPPER CHORD FROM BS 660 AND BS 681, LBL 24.82. (M) 2 L 7 2 4F A16WE 1998120400527 19981204 00527 NM 1998 12 4 P2EA98228 1 19981011 A 5753 6546486505 SKIN BOEING 737 737244 138448U NM TE FLAP DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - UPPER SKIN DELAMINATED INBOARD MID FLAP TRAILING EDGE. REPLACED LEFT WING, INBOARD MID FLAP TRAILING EDGE UPPER S KIN. (M) 2 L 7 2 4F A16WE 1998120400528 19981204 00528 NM 1998 12 4 P2EA98226 1 19981003 A 5330 SKIN BOEING 737 737244 138448U NM BS 259-360 DISBONDED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FUSELAGE SKIN DISBONDED FROM BS 259 TO BS 360, STRINGER 24 RT. REPLACED FUSELAGE SKIN SECTION FROM BS 259 TO BS 3 60, BETWEEN STRINGER 24 RT AND BL 0 PER SRM 51-10-1 PAGE 5, SRM 51-30-2 PAGE 1. (M) 2 L 7 2 4F A16WE 1998120400529 19981204 00529 EU 1998 12 4 C2XA98BT079 1 19981030 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14834 193 LOWER RIGHT EMERGENCY SIGN INOP AT REAR OF THE CABIN. REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY PACK, OPS CHE CKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998120400530 19981204 00530 SO 1998 12 4 C2XA98IA449 1 19981027 A 5320 12015374002 ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENA NCE REPAIRED THE ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5530-01013. THE AIRCRAFT WAS R ETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400531 19981204 00531 SO 1998 12 4 C2XA98IA448 1 19981027 A 5320 12015374001 ANGLE EMB 120 EMB120RT SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICLE STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND CRACKED. MAINTENANCE REP AIRED THE ANGLE IAW CONTINENTAL EXPERSS ENGINEERING CHANGE/REPAIR EC5530-01013. THE AIRCRAFT WAS THEN APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400532 19981204 00532 SO 1998 12 4 C2XA98IA447 1 19981027 A 5522 12002458003 SKIN EMB 120 EMB120RT SO ELEVATOR DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT ELEVATOR WAS FOUND TO HAVE LIGHTENING STRIKE DAMAGE. MAINTENANCE REPAIRED THE AFFECTED AREAS OF THE ELEVATOR IAW EMB 120 SRM 55-20-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400533 19981204 00533 SO 1998 12 4 C2XA98IA446 1 19981027 A 5347 12026864007 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE AFFECTED PORTION OF SEAT TRACK IAW THE EMB120 SRM 53-01-05. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE . (M) 2 L 7 2 4T RT A31SO 1998120400534 19981204 00534 SO 1998 12 4 C2XA98IA445 1 19981027 A 5347 12026865609 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT AFT FLOOR SEAT TRACK WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLA CED THE AFFECTED PORTION OF SEAT TRACK IAW THE EMB120 SRM 53-01-05. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVIC E. (M) 2 L 7 2 4T RT A31SO 1998120400535 19981204 00535 SO 1998 12 4 C2XA98IA444 1 19981027 A 5320 12025957001 SUPPORT EMB 120 EMB120RT SO COCKPIT CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTIONS, THE SUPPORTS FOR THE COCKPIT ENTRY STEP WERE FOUND CRACKED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED SUPPORTS IAW THE EMB120 SRM. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400536 19981204 00536 SO 1998 12 4 C2XA98IA443 1 19981027 A 5320 1200779001 BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 5320 IAH - DURING C-CHECK INSPECTION, THE RIGHT CREASE BEAM FROM FRAME 38 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF CREASE BEAM AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. REFERENCE EMB120 SRM 51-40-02. (M) 2 L 7 2 4T RT A31SO 1998120400537 19981204 00537 SO 1998 12 4 C2XA98IA442 1 19981027 A 5320 12006257007 BEAM EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CEHCK INSPECTION, THE CREASE BEAM AT FRAME 44 TO FRAME 47 WAS FOUND CORRODED. MAINTENANCE REMOVED AND RE PLACED THE AFFECTED PORTION OF CREASE BEAM IAW THE EMB 120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400538 19981204 00538 SO 1998 12 4 C2XA98IA441 1 19981027 A 5320 12018811001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER BUTTSTRAP AT FRAME 38 TO 44 WAS FOUND CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400539 19981204 00539 SO 1998 12 4 C2XA98IA440 1 19981027 A 5320 12027929001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP AT FRAME 33 TO FRAME 44 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400540 19981204 00540 SO 1998 12 4 C2XA98IA439 1 19981027 A 5320 12027929001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE RIGHT CENTER FLOORBEAM BUTTSTRAP AT FRAME 33 TO FRAME 38 WAS FOUND CORRODED. MAINT ENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400541 19981204 00541 SO 1998 12 4 C2XA98IA438 1 19981027 A 5320 12027928001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT CENTER BUTTSTRAP AT FRAME 28 TO FRAME 33 WAS FOUND TO BE CORRODED. MAINTENANC E REMOVED AND REPLACED THE AFFECTED PORTION OF THE BUTTSTRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400542 19981204 00542 SO 1998 12 4 C2XA98IA437 1 19981027 A 5320 12027929001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE BUTTSTRAP AT FRAME 33 TO FRAME 38, WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-40-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400543 19981204 00543 SO 1998 12 4 C2XA98IA436 1 19981027 A 5347 12015995603 SEAT TRACK EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT FORWARD FLOOR SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF SEAT TRACK IAW THE EMB 120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4T RT A31SO 1998120400544 19981204 00544 SO 1998 12 4 C2XA98IA435 1 19981027 A 5320 12026671001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT SIDE BUTTSTRAP AT FRAME 13A WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED PORTION OF BUTTSTRAP IAW THE EMB120 SRM 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4T RT A31SO 1998120400545 19981204 00545 SO 1998 12 4 C2XA98IA434 1 19981027 A 5713 12004367001 STRINGER EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE LEFT WING STRINGER NR 10 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED THE AFFECTED PORTION OF STRINGER AND INSTALLED A SPLICE REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC571 0-01010. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400546 19981204 00546 SO 1998 12 4 C2XA98IA433 1 19981027 A 3221 2069600001 TRUNNION EMB 120 EMB120RT SO NLG CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15725 120173 IAH - DURING C-CHECK INSPECTION, THE NOSE LANDING GEAR LOWER TRUNNION WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE TRUNNION AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400547 19981204 00547 EU 1998 12 4 C2XA98BT077 1 19981025 A 3211 S5357840000351 FITTING AEROSP ATR42 ATR42320 8680930 EU RT MLG WW CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 86842 286 RIGHT MAIN GEAR HAS MAIN GEAR ACTUATOR BROKEN AT ATTACH POINT. REMOVED AND REPLACED MAIN GEAR ATTACH FITTING IAW ATR42 JIC 53-57-30, OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998120400548 19981204 00548 EU 1998 12 4 C2XA98BT075 1 19981024 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14834 193 LEFT AND RIGHT EMERGENCY EXIT SIGNS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK AT FUSELAGE POSITION 3WL, OP S CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1998120400549 19981204 00549 EU 1998 12 4 C2XA98BT074 1 19981027 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 21837 202 FORWARD EMERGENCY FLOOR TRACK LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IN EMERGENCY LIGHTING POWER SUPPLY. (M) 2 H 7 2 4T RT A53EU 1998120400550 19981204 00550 SO 1998 12 4 C2XA98IA430 1 19981023 A 3350 12021299001 LIGHT EMB 120 EMB120RT SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17720 120142 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MAINTENA NCE CLEANED THE LIGHT SOCKET AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE PROBLEM REPEATED ON PREFLIGHT INS PECTION FOR FLIGHT 3820, AND MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETUR N TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998120400551 19981204 00551 EU 1998 12 4 C2XA98IA431 1 19981021 A 3350 3013000 POWER SUPPLY AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY LIGHT POWER SUPPLY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE POWER SUPPLY IAW ATR42 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400552 19981204 00552 EU 1998 12 4 98ZZZM908 1 19980619 A 3520 LAYNARD BAG BAE146 BAE146300A 1500267 EU OXYGEN MASK WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 OXYGEN MASK AT 20 RT REBREATHER FEL HAS HOLES AND PIN STRING FRAYED, 11 LT. REBREATHER FELT HAS HOLES. REPLACED FELTS RT 20, 11 LT. REPLACED LANYARD 20 RT. CHECKS OK. (M) 2 H 7 4 4F RT A49EU 1998120400553 19981204 00553 WP 1998 12 4 USAAD98200 1 19981107 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 800US 48034 PHL - THE PASSENGER CABIN LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE CABIN LOW LEVEL EMERGEN CY LIGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998120400554 19981204 00554 EU 1998 12 4 USAAF98090 1 19981108 A 2760 233009 ACTUATOR FOKKER F28 F28MK0100 4990807 EU SPEED BRAKE LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 853US 11281 PHL - FLT 1809 - WHILE CLIMBING OUT FROM HPN AT 16000 FT, CREW RECEIVED A 'HYD SYS 1 LOW QTY, ALERT. CREW PERFORMED THE ABNORMAL PROCEDURE CHECKLIST. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO PHL. FLIGHT LANDED PHL WITHOUT FUR THER INCIDENT. MAINTENANCE REPLACED THE SPEED BRAKE ACTUATOR DUE TO HYDRAULIC LEAKAGE. (M) 2 L 7 2 4F RT 1998120400555 19981204 00555 NM 1998 12 4 USAASB98293 1 19981107 A 7722 WL202EED6 INDICATOR BOEING 737 7373B7 1384580 NM COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 520AU 34469 23706 BOS - FLT 258 - ON CLIMB-OUT FROM BOS, THE NR 1 ENGINE OVERHEATED. CAPTAIN ACCOMPLISHED HANDBOOK PROCEDURES, THROTTLED BACK THE NR 1 ENGINE TO IDLE AND DECLARED AN EMERGENCY. FLIGHT RETURNED TO FIELD AT BOS AND LANDED WITHOUT FURTHER INCI DENT. THE AIRCRAFT LANDED WITH THE NR 1 ENGINE AT IDLE. NO INFLIGHT ENGINE SHUTDOWN OCCURRED. MAINTENANCE PERFORMED R ESISTANCE TEST PER MM FOR THE EGT SYSTEM. NO DEFECTS NOTED. ACCOMPLISHED BOROSCOPE INSPECTION OF THE LOW PRESSURE TURB INE AND HIGH PRESSURE TURBINE ON THE NR 1 ENGINE. NO DEFECTS NOTED. RAN ENGINE UP TO POWER. NO DEFECTS NOTED. REPLAC ED NR 1 ENGINE EGT INDICATOR AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998120400556 19981204 00556 NM 1998 12 4 USAASB98288 1 19981027 A 2611 UNKNOWN BOEING 737 7373B7 1384580 NM LAVATORY SMOKE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 530AU 24412 PHL - FLT 1119 - SHORTLY AFTER TAKEOFF, FLIGHT ATTENDANT NOTIFIED CAPT THAT BOTH AFT LAVATORY SMOKE DETECTORS HAD GONE O FF AND THERE WAS BOTH AND ODOR AND VISIBLE SMOKE PRESENT. CAPTAIN IMMEDIATELY DECLARED AN EMERGENCY AND RETURNED TO FIE LD AT PHL. UPON TOUCHDOWN, SMOKE AND ODOR HAD SUBSIDED AND CAPTAIN DECIDED IT WAS SAFE ENOUGH TO TAXI TO THE GATE. PAS SENGERS DEPLANED BY NORMAL PROCEDURES WITHOUT INCIDENT. MAINTENANCE RAN ENGINES AT TAKEOFF POWER FOR SEVERAL MINUTES. N O SMOKE OR ODOR WAS NOTED IN CABIN. LAVATORY SMOKE DETECTORS OPERATED NORMALLY. REMOVED AND REPLACED AFT LAVATORY SMOK E DETECTOR BATTERIES (P/N EN22) AS PRECAUTIONARY. OPERATIONAL CHECK GOOD. COULD NOT DUPLICATE SMOKE OR ODOR. (M) 2 L 7 2 4F RT A16WE 1998120400557 19981204 00557 NM 1998 12 4 USAASB98278 1 19981021 A 3260 MS253831 SWITCH BOEING 737 737301 1384611 NM COCKPIT CONTAMINATED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 338US 23234 PIT - FLT 345 - DURING LANDING GEAR EXTENSION, GEAR CAME DOWN WITH 3 GREEN AND 3 RED LIGHTS. HYDRAULIC PRESSURE WAS NOR MAL. CREW RECYCLED GEAR AND RECEIVED 3 GREEN LIGHTS WITH RED LIGHTS EXTINGUISHED. FLIGHT LANDED WITHOUT FURTHER INCIDE NT. MAINTENANCE CLEANED THE LANDING GEAR HANDLE S78 MICROSWITCH, PINNED THE LANDING GEAR AND OPERATED THE GEAR HANDLE S EVERAL TIMES. OPERATIONAL CHECK GOOD. REMOVED GEAR PINS. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4F RT A16WE 1998120400558 19981204 00558 WP 1998 12 4 USAAD98195 1 19981102 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 PHL - THE LOW LEVEL EMERGENCY LIGHT AT ROWS 16 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1998120400559 19981204 00559 WP 1998 12 4 USAAD98193 1 19981030 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC981 3022081 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 809US 48041 PIT - THE EMERGENCY LIGHTS STAYED ON ALL THE TIME. MAINTENANCE REPLACED THE FORWARD ENTRY AND COCKPIT EMERGENCY LIGHT P OWER SUPPLY. (M) 2 L 7 2 4F A6WE 1998120400560 19981204 00560 WP 1998 12 4 USAAD98191 1 19981028 A 3350 60030451LM POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 946VJ 47026 DTW - THE GALLEY AREA EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE GALLEY AREA EMERGENCY LIGHT POWER SUP PLY. (M) 2 L 7 2 4F A6WE 1998120400561 19981204 00561 WP 1998 12 4 USAAD98199 1 19981031 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 PHL - THE EMERGENCY OVERHEAD, EXIT WINDOWS, AND LOW LEVEL LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY L IGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998120400562 19981204 00562 WP 1998 12 4 98ZZZM909 1 19981031 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 PHL - THE EMERGENCY OVERHEAD, EXIT WINDOWS, AND LOW LEVEL LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY L IGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998120400563 19981204 00563 WP 1998 12 4 98ZZZM910 1 19981031 A 3350 14597101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 PHL - THE EMERGENCY OVERHEAD, EXIT WINDOWS, AND LOW LEVEL LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY L IGHT BATTERIES. (M) 2 L 7 2 4F A6WE 1998120400564 19981204 00564 WP 1998 12 4 USAAD98194 1 19981031 A 3350 9721055 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 PHL - THE FOLLOWING EMERGENCY LIGHTS WERE INOPERATIVE, PASSENGER CABIN LOW LEVEL LIGHTS, OVERWING EXIT LIGHTS, AFT FUSEL AGE EMERGENCY LIGHTS, OVERWING EXIT IDENTIFIER LIGHTS. MAINTENANCE REPLACED THE BATTERIES FOR ALL THE INOPERATIVE EMERG ENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998120400565 19981204 00565 WP 1998 12 4 98ZZZM911 1 19981031 A 3350 14597101 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 PHL - THE FOLLOWING EMERGENCY LIGHTS WERE INOPERATIVE, PASSENGER CABIN LOW LEVEL LIGHTS, OVERWING EXIT LIGHTS, AFT FUSEL AGE EMERGENCY LIGHTS, OVERWING EXIT IDENTIFIER LIGHTS. MAINTENANCE REPLACED THE BATTERIES FOR ALL THE INOPERATIVE EMERG ENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998120400566 19981204 00566 WP 1998 12 4 98ZZZM912 1 19981031 A 3350 9721050 BATTERY DOUG DC9 DC981 3022081 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 801US 48037 PHL - THE FOLLOWING EMERGENCY LIGHTS WERE INOPERATIVE, PASSENGER CABIN LOW LEVEL LIGHTS, OVERWING EXIT LIGHTS, AFT FUSEL AGE EMERGENCY LIGHTS, OVERWING EXIT IDENTIFIER LIGHTS. MAINTENANCE REPLACED THE BATTERIES FOR ALL THE INOPERATIVE EMERG ENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998120400567 19981204 00567 NM 1998 12 4 USAASB98277 1 19981021 A 5210 6990299 SEAL BOEING 737 7373B7 1384580 NM PAX DOOR LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 517AU 23703 PHL - FLT 2054 - AFTER TAKEOFF, CREW REPORTED A LOUD AIR LEAK FROM THE FORWARD MAIN ENTRY DOOR. AT ABOUT FL200, CAPTAIN ELECTED TO RETURN TO FIELD AT PHL. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE FORWARD MAIN ENTRY DOOR LOWER HINGE SEAL DAMAGED. REPLACED LOWER HINGE SEAL AND RIGGED/ADJUSTED DOOR IN ASSOCIATION WIT H MM. OPERATIONAL CHECK GOOD. PRESSURIZED AIRCRAFT. PRESSURIZATION CHECK GOOD. NO LEAKS NOTED. (M) 2 L 7 2 4F RT A16WE 1998120400568 19981204 00568 NM 1998 12 4 USAASB98282 1 19981024 A 2910 1062030222 LINE BOEING 737 7373B7 1384580 NM LT MLG LEAKING A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 EA 19 519AU 23705 CLT - FLT 1655 - ON CLIMB-OUT FROM CLT AND RAISING LANDING GEAR, THE 'A' SYSTEM HYDRAULIC QTY GAUGE WENT TO ZERO AND THE 'A' SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. CREW ACCOMPLISHED CHECKLIST, DECLARED AN EMERGENCY AND RETURNED TO FIELD A T CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR UPLOCK ACTUATOR HYDRAULIC PRESSURE LINE LEAKING. REMOVED AND REPLACED SAME AND SERVICED HYDRAULIC RESERVOIR. LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998120400569 19981204 00569 NM 1998 12 4 USAASB98284 1 19981027 A 3260 BR20AXH5V3 RELAY BOEING 737 7373B7 1384580 NM E/E BAY FAILED A USAA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 EA 19 517AU 23703 CAE - FLT 1922 - ON APPROACH TO CAE, AS GEAR WAS EXTENDED, CREW RECEIVED THREE GREEN GEAR INDICATIONS AND A RED LIGHT FO R THE NOSE GEAR. CAPTAIN RECYCLED THE GEAR BUT THE RED LIGHT REMAINED ILLUMINATED. A TOWER FLYBY WAS ACCOMPLISHED. TO WER PERSONNEL CONFIRMED VISUALLY THAT THE GEAR APPEARED TO BE DOWN. ON SHORT FINAL, THE RED NOSE GEAR LIGHT EXTINGUISHE D AND THE AIRCRAFT LANDED WITH THREE GREEN GEAR INDICATIONS. NO EMERGENCY WAS DECLARED. AIRCRAFT TAXIED TO THE GATE ON ITS OWN POWER. MAINTENANCE REMOVED AND REPLACED THE R374 RELAY PER MM. GEAR OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998120400570 19981204 00570 NM 1998 12 4 USAASB98289 1 19981029 A 3230 651781914 LOCK ACTUATOR BOEING 737 737301 1384611 NM NLG FAILED A USAA O OTHER J WARNING INDICATION CL CLIMB 1 EA 19 563AU 35523 23551 CLT - FLT 984 - AFTER TAKEOFF WITH GEAR LEVER IN THE UP POSITION, THE RED NOSE GEAR WARNING LIGHT ILLUMINATED. GEAR APP EARED TO BE UP. WHEN GEAR LEVER WAS PLACED TO THE OFF POSITION, NOSE GEAR DROPPED TO THE EXTEND POSITION. FLIGHT LANDE D WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE LANDING GEAR LOCK ACTUATOR PER MM 32-33-21 AND AD JUSTED THE NOSE LANDING GEAR DOORS PER MM 32-33-61. LEAK CHECK AND OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998120400571 19981204 00571 NM 1998 12 4 ASAA9840093 1 19980924 A 5240 RELEASE ASSY BOEING 737 7374Q8 NM R1 DOOR FAILED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 764AS 25101 PDX - DURING MAINTENANCE CHECK, THE R1 DOOR HOLD OPEN LEVER ASSY WAS FOUND TO NOT HOLD THE DOOR IN THE OPEN POSITION, AN D WOULD NOT LOCK. REPLACED LEVER ASSEMBLY AND DOOR HOLD OPEN OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998120400572 19981204 00572 NM 1998 12 4 ASAA9810109 1 19981009 A 3397 WIRE BOEING 737 737290C 138448V NM ROW 20 BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - FLT 42 - PRIOR TO DEPARTURE, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 20 WAS FOUND INOPERATIVE. RELAMPED AND R EPAIRED BROKEN WIRING, LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998120400573 19981204 00573 1998 12 4 ASAA9840100 4 19981018 A 2565 SLIDE BOEING 737 7374Q8 NM CABIN DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 784AS 28199 YVR - DURING PREFLIGHT FOR FLIGHT 654, CREW REPORTED THAT THE R1, R2, AND L2 DOOR EVACUATION SLIDE MANUAL INFLATION HAND LES WERE MISSING. REPLACED THE R1, R2, AND L2 DOOR EVACUATION SLIDES. (M) 2 L 7 2 4F RT A16WE 1998120400574 19981204 00574 NM 1998 12 4 ASAA9840102 1 19981028 A 5210 CAM ROLLER BOEING 737 7374Q8 NM PAX DOOR CONTAMINATED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 782AS 25113 SEA - PRIOR TO FLT 75 - THE CREW REPORTED THAT THE L1 DOOR WAS DIFFICULT TO CLOSE. REMOVED LINER AND INSPECTED LINKAGE AND ROD ENDS, NO DEFECTS NOTED. FOUND CAM ROLLERS GUMMED UP, CLEANED SAME. LUBRICATED DOOR MECHANISM AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998120400575 19981204 00575 WP 1998 12 4 AALA981929 1 19981023 A 2910 792807781190 LINE DOUG DC10 DC1030 3023501 WP MLG LEAKING A AALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 SW 07 164AA 46950 DFW - FLT 5 - AFTER TAKEOFF, UNABLE TO RETRACT LANDING GEAR. AIRCRAFT RETURNED TO DFW AND LANDED WITHOUT INCIDENT. FOU ND TRIM CYLINDER FUSE IN BYPASS POSITION. RESET FUSE AND FOUND LEAK IN SUPPLY LINE. REPLACED SUPPLY LINE, SERVICED AND BLED SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1998120400576 19981204 00576 NM 1998 12 4 AALA981926 1 19981022 A 3230 NLG BOEING 727 727223 1384074 NM NLG LACK OF LUBE A AALA K NONE O OTHER AP APPROACH 1 SW 07 868AA 21373 DFW - FLT 1607 - DURING APPROACH DFW, NOSE LANDING GEAR HUNG UP MOMENTARILY BEFORE EXTENDING NORMALLY. FLIGHT LANDED DF W WITHOUT FURTHER INCIDENT. NOSE LANDING GEAR WAS INSPECTED, LUBRICATED, AND SWUNG SEVERAL TIMES WITH NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998120400577 19981204 00577 WP 1998 12 4 AALA982006 1 19981028 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 205AA 49155 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SERVICE DOOR INOPERATIVE. REPAIRED WIRE AT CONNECTOR FOR CH ARGER/BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998120400578 19981204 00578 WP 1998 12 4 AALA981925 1 19981021 A 2530 8803010000 OVEN DOUG DC9 DC982 3022082 WP NR 3 GALLEY MALFUNCTIONED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 417AA BBCZLSM 49328 DFW - FLT 1642 - AFTER TAKEOFF, CREW AND PASSENGERS NOTED BURNING SMELL AND SMOKE. AIRCRAFT RETURNED DFW AND LANDED OVE RWEIGHT WITHOUT INCIDENT. FOUND NR 3 GALLEY OVEN TO BE CAUSE OF REPORTED SMELL IN CABIN. REPLACED NR 3 GALLEY OVEN. A CCOMPLISHED OVERWEIGHT INSPECTION WITH NO IRREGULARITIES NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998120400579 19981204 00579 NM 1998 12 4 AALA981920 1 19981018 A 3350 CONNECTOR BOEING 767 767323 1385205 NM SEAT 28 A/B LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 353AA 24034 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 28A/B INOPERATIVE. RECONNECTED LOOSE EMERGENCY EXI T LIGHT PIN IN CONNECTOR AT PASSENGER SEAT 28A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998120400580 19981204 00580 NM 1998 12 4 AALA981927 1 19981022 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 699AN 27051 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR LIGHT INOPERATIVE AT COFFEE BAR. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT COFFEE BAR. SYSTEM GRUOND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998120400581 19981204 00581 NM 1998 12 4 AALA981704 1 19980918 A 3350 3020442 LIGHT GRIMES BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 645AA 24603 DFW - DURING OVERNIGHT MAINTENANCE, R2 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. RESEATED R2 DOOR EMERGENCY EXIT LIGHT ASS EMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998120400582 19981204 00582 WP 1998 12 4 AALA982002 1 19981026 A 2150 20497511 ACM GARRTT DOUG DC10 DC1030 3023501 WP NR 1 PACK MALFUNCTIONED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 137AA 62433 47847 DFW - FLT 5 - DURING LEVEL OFF FL310, FLIGHT ATTENDANT REPORTED SMOKE THROUGHOUT CABIN. FIRST OFFICER INVESTIGATED AND REPORTED IT SMELLED LIKE ELECTRICAL SMOKE. CREW ACCOMPLISHED CHECKLIST AND RETURNED AND LANDED DFW WITHOUT FURTHER INCI DENT. AIRCRAFT WAS TAKEN OUT OF SERVICE. TROUBLE SHOOTING FOUND NR 1 PACK AS SOURCE OF ODOR. REPLACED NUMBER ONE AIR CYCLE MACHINE AND AS A PRECAUTIONARY, REPLACED COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATION. AIRCRAFT WAS RE TURNED TO SERVICE AFTER SUCCESSFUL FUNCTIONAL CHECK FLIGHT. (M) 2 L 7 3 4F A22WE 1998120400583 19981204 00583 NM 1998 12 4 AALA981931 1 19981024 A 3397 WIRE BOEING 767 767223 1385123 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 312AA 22315 SFO - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY BIDIRECTIONAL EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPAIRED BROK EN WIRE AT FORWARD GALLEY BIDIRECTIONAL EMERGENCY FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998120400584 19981204 00584 NM 1998 12 4 AALA981930 1 19981023 A 2750 96010214 TRANSMITTER LITTON DOUG MD11 MD11 3023602 NM RT TE FLAP FAILED A AALA D RETURN TO BLOCK F FLT CONT AFFECTED CL CLIMB 1 SW 07 1758B 1038 48527 DFW - FLT 2248 - DURING CLIMB-OUT, FLAPS WERE FULLY RETRACTED AND THE RIGHT OUTBOARD FLAP INDICATED 6 DEGREES EXTENSION. AIRCRAFT AIR INTERRUPTED AND LANDED DFW WITHOUT FURTHER INCIDENT. FOUND RIGHT OUTBOARD FLAP TRANSMITTER FAULTY. REPL ACED RIGHT OUTBOARD FLAP TRANSMITTER AND ACCOMPLISHED SYSTEM ADJUSTMENT AND TEST. PERFORMED CAT III TEST, ALL SYSTEMS C HECK NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1998120400585 19981204 00585 WP 1998 12 4 AALA981998 1 19981026 A 5230 DOOR PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 449AA 49475 TUL - FOUND CORROSION AROUND HOLES IN FORWARD CARGO DOOR PAN. CUT OUT DAMAGED SECTION OF PAN. INSTALLED NEW SECTION OF LOWER CARGO DOOR PAN AND FORWARD AND AFT SPLICE DOUBLERS PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 1998120400586 19981204 00586 NM 1998 12 4 USAA980520 1 19981105 A 5315 141N51131 FLOORBEAM BOEING 757 757225 1384959 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 44869 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER 'T' CAP OF FLOORBEAM BS 377 LBL 50 TO RBL 7. CORR OSION TASK NR C53-117-01. BURNISHED AFFECTED AREA PER SRM 53-00-51 FIG 101. (M) 2 L 7 2 4F RT A2NM 1998120400587 19981204 00587 NM 1998 12 4 USAA980519 1 19981105 A 5315 141N51121 FLOORBEAM BOEING 757 757225 1384959 NM BS 365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 44869 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER 'T' CAP OF FLOORBEAM BS 365 RBL 60 TO LBL 60 WL 20 8. INSTALLED 'T' CAP PER EA 62705. (M) 2 L 7 2 4F RT A2NM 1998120400588 19981204 00588 NM 1998 12 4 USAA980514 1 19981105 A 5315 141N51111 FLOORBEAM BOEING 757 757225 1384959 NM BS 345 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 44869 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION ALONG UPPER 'T' CAP OF FLOORBEAM BS 345, LBL 60 TO RBL 60 WL 2 08. INSTALLED 'T' CAP ON FLOORBEAM PER TR 53-15-01. (M) 2 L 7 2 4F RT A2NM 1998120400589 19981204 00589 NM 1998 12 4 UIEA9809 1 19981109 A 2910 LINE BOEING 747 747230B 1384889 NM HYDRAULIC SYSTEM LEAKING A UIEA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS K FLUID LOSS CR CRUISE 1 EA 15 508MC 21644 FLT C1353 - ATL/ANC - DIVERTED TO JFK DUE NR 1 HYDRAULIC SYSTEM STARTED TO LOSE FLUID VERY SLOWLY IN FLIGHT. USED ABNOR MAL CHECKLIST PROCEDURE AND SYSTEM STILL LOST FLUID VERY SLOWLY. WITH ADP OFF AND EDP IN SUPPLY OFF, SYSTEM IS COMPLETE LY EMPTY. HAD TO EXTEND GEAR AND TE FLAP WITH ALT SYSTEMS. LANDING WAS UNEVENTFUL. FOUND NR 1 HYD SYSTEM RETURN LINE FROM PRESSURE BULKHEAD (TAIL COMPT), LEAKING (REF IPC 29-11-16, FIG 1, ITEM 423). REPAIRED LINE PER MM 20-11-05. SERVI CED NR 1 HYD SYSTEM AND PERFORMED LEAK CHECK AND BLED SYSTEM. NO LEAKS FOUND. SYSTEM OPERATION NOW NORMAL. (M) 2 L 7 4 4F A20WE 1998120400590 19981204 00590 EU 1998 12 4 SIMA983166 1 19981112 A 5320 S536780082201 CHORD AEROSP ATR42 ATR42300 8680920 EU BS 39-40 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT CHORD BETWEEN FRAMES 39 AND 40 CORRODED. REMOVED AND REPLACED THE CHORD. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400591 19981204 00591 EU 1998 12 4 SIMA983165 1 19981112 A 5313 S5367125722151 STRINGER AEROSP ATR42 ATR42300 8680920 EU BS 35-37 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND STRINGER 17 RIGHT BETWEEN FRAME 35 AND 37 CORRODED. REMOVED AND REPLACED STRINGER 17 RIGHT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400592 19981204 00592 EU 1998 12 4 SIMA983163 1 19981112 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND CORROSION ON THE RIGHT AFT INBOARD AND OUTBOARD, THE RIGHT AND LEFT FORWARD OUTBOAR D, THE RIGHT AND LEFT FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS. REMOVED AND REPLACED THE SEAT TRACKS. AIR CRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400593 19981204 00593 EU 1998 12 4 98ZZZM913 1 19981112 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND CORROSION ON THE RIGHT AFT INBOARD AND OUTBOARD, THE RIGHT AND LEFT FORWARD OUTBOAR D, THE RIGHT AND LEFT FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS. REMOVED AND REPLACED THE SEAT TRACKS. AIR CRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400594 19981204 00594 EU 1998 12 4 98ZZZM914 1 19981112 A 5347 S5367800125002 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND CORROSION ON THE RIGHT AFT INBOARD AND OUTBOARD, THE RIGHT AND LEFT FORWARD OUTBOAR D, THE RIGHT AND LEFT FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS. REMOVED AND REPLACED THE SEAT TRACKS. AIR CRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400595 19981204 00595 EU 1998 12 4 98ZZZM915 1 19981112 A 5347 S5337500121402 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND CORROSION ON THE RIGHT AFT INBOARD AND OUTBOARD, THE RIGHT AND LEFT FORWARD OUTBOAR D, THE RIGHT AND LEFT FLIGHT ATTENDANT AND THE LEFT AFT INBOARD SEAT TRACKS. REMOVED AND REPLACED THE SEAT TRACKS. AIR CRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400596 19981204 00596 EU 1998 12 4 SIMA983162 1 19981112 A 5315 S5367240720201 FLOORBEAMS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400597 19981204 00597 EU 1998 12 4 98ZZZM916 1 19981112 A 5315 S5367240820200 FLOORBEAMS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400598 19981204 00598 EU 1998 12 4 98ZZZM917 1 19981112 A 5315 S5367240620801 FLOORBEAMS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400599 19981204 00599 EU 1998 12 4 98ZZZM918 1 19981112 A 5315 S5367240921801 FLOORBEAMS AEROSP ATR42 ATR42300 8680920 EU FUSELAGE CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED. REMOVED AND REPLACED THE FLOORBEAMS. AIRCR AFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400600 19981204 00600 EU 1998 12 4 SIMA983161 1 19981112 A 5320 S53671217980800 DRAIN TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND THE PASSENGER DOOR SILL DRAIN TRACK BETWEEN FRAMES 36 AND 39 CORRODED. REMOVED AND REPLACED THE DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE (M) 2 H 7 2 4T RT A53EU 1998120400601 19981204 00601 EU 1998 12 4 SIMA983155 1 19981111 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 340B218 ABI - FOUND CORROSION ON LEFT FUSELAGE, AFT OF ICE SHIELD, AT FS 339. CUT OUT DAMAGED AREA AND PERFORMED EDDY CURRENT I NSPECTION WITH NO INDICATION OF CRACKS. FABRICATED AND INSTALLED TWO EXTERNAL DOUBLERS .050 THICK. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4T RT A52EU 1998120400602 19981204 00602 EU 1998 12 4 SIMA983151 1 19981111 A 2611 72111211000 SMOKE DETECTORS SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 21 317AE A2718 340B317 DFW - FLT 5193 - CARGO SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED NR 1 FIRE EXTINGUISHER. RETURNED TO FIELD. INSPECT ED CARGO BAY WITH NO EVIDENCE SMOKE FOR FIRE. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND NR 1 FIRE EXTINGUISHE R. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998120400603 19981204 00603 EU 1998 12 4 98ZZZM919 1 19981111 A 2611 72111211000 SMOKE DETECTORS SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA A F UNSCHED LANDING ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 21 317AE A2446 340B317 DFW - FLT 5193 - CARGO SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED NR 1 FIRE EXTINGUISHER. RETURNED TO FIELD. INSPECT ED CARGO BAY WITH NO EVIDENCE SMOKE FOR FIRE. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AND NR 1 FIRE EXTINGUISHE R. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998120400604 19981204 00604 EU 1998 12 4 SIMA983142 1 19981110 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-329 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 334AE 340B334 ABI - FOUND SEAT TRACK 18.3L WAS FOUND CORRODED AT FS 297-329. CUT OUT 32 INCH SECTION OF EXISTING SEAT TRACK. FABRICA TED AND INSTALLED A 32 INCH LONG EXTRUSION. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998120400605 19981204 00605 EU 1998 12 4 SIMA983141 1 19981110 A 3350 1317 BULB SAAB SF340 340B 7860101 EU SEAT 10C FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 264AE 340B264 SAW - FOUND EMERGENCY LIGHT ABOVE SEAT 10C DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M ) 2 L 7 2 4T RT A52EU 1998120400606 19981204 00606 EU 1998 12 4 SIMA983134 1 19981109 A 5320 S5367121729801 DRAIN TRACK AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND THE SERVICE DOOR DRAIN TRACK BETWEEN FRAME 36 AND 39 CORRODED. REMOVED AND REPLACE D THE DRAIN TRACK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400607 19981204 00607 EU 1998 12 4 SIMA983133 1 19981109 A 5320 S5367121729402 SILL AEROSP ATR42 ATR42320 8680930 EU PAX DOOR CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND THE PASSENGER DOOR SILL PLATE BETWEEN FRAME 36 AND 39 CORRODED. REMOVED AND REPLAC ED THE SILL PLATE. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400608 19981204 00608 EU 1998 12 4 SIMA983132 1 19981109 A 5320 S5367800821602 SUPPORT AEROSP ATR42 ATR42320 8680930 EU CARGO BAY CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT CARGO ZEE MEMBER CORRODED. REMOVED AND REPLACED THE ZEE MEMBER. AIR CRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400609 19981204 00609 EU 1998 12 4 SIMA983131 1 19981109 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TR ACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400610 19981204 00610 EU 1998 12 4 98ZZZM920 1 19981109 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TR ACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400611 19981204 00611 EU 1998 12 4 98ZZZM921 1 19981109 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT INBOARD AND OUTBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TR ACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998120400612 19981204 00612 EU 1998 12 4 SIMA983111 1 19981107 A 3350 BULB AEROSP ATR42 ATR42300 8680920 EU SEAT 4AB FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 11B28 045 ORD - FLT 9753 - FLOOR PROXIMITY LIGHT AT SEAT 4AB DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB AND BATTERY PACK. OP ERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998120400613 19981204 00613 EU 1998 12 4 98ZZZM922 1 19981107 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 424MQ 11B28 045 ORD - FLT 9753 - FLOOR PROXIMITY LIGHT AT SEAT 4AB DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB AND BATTERY PACK. OP ERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998120400614 19981204 00614 EU 1998 12 4 SIMA983093 1 19981105 A 3350 3071BPEGL BULB SAAB SF340 340B 7860101 EU SEAT 9BC FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343SB 340B343 LAX - FLT 3230 - EMERGENCY FLOOR PROXIMITY LIGHT AT SEAT 9BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATION AL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998120400615 19981204 00615 EU 1998 12 4 SIMA983072 1 19981103 A 3350 AD3127 BATTERY PACK AEROSP ATR42 ATR42300 8680920 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AT 17778 327 ORD - FLT 4394 - THREE FLOOR PROXIMITY LIGHT STRIPS DO NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK FOR THE POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998120400616 19981204 00616 EU 1998 12 4 SIMA983041 1 19981031 A 3350 6500006 LIGHT SAAB SF340 340B 7860101 EU SEAT 8A INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 210AE 340210 TPA - FLT 5824 - SMOKE IN THE CABIN AT OVERHEAD LIGHT 8A. FOUND BULB SHORTED TO SOCKET. REMOVED BULB, PULLED AND COLLA RED CIRCUIT BREAKER FOR OVERHEAD LIGHTS AND ISSUED MEL 33-02. BAD SOCKET INFORMATION BELOW. REMOVED AND REPLACED LIGHT ASSEMBLY ON 10 NOV. OPERATIONAL CHECK GOOD. MEL CLEARED. (M) 2 L 7 2 4T RT A52EU 1998120400617 19981204 00617 SO 1998 12 4 SIMA982803 1 19981007 A 2611 PU90431 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 603AE 05567 145055 ORD - FLT 2600 - FOUND BAGGAGE SMOKE WARNING LIGHT CAME ON. DISCHARGED BOTH FIRE BOTTLES. LANDED SAFELY. PERFORMED VI SUAL INSPECTION OF BAGGAGE COMPARTMENT WITH NO EVIDENCE OF SMOKE OR FIRE. REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS, AND BOTH FIRE BOTTLES. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1998120400618 19981204 00618 SO 1998 12 4 98ZZZM923 1 19981007 A 2611 PU90431 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 SW 21 603AE 05568 145055 ORD - FLT 2600 - FOUND BAGGAGE SMOKE WARNING LIGHT CAME ON. DISCHARGED BOTH FIRE BOTTLES. LANDED SAFELY. PERFORMED VI SUAL INSPECTION OF BAGGAGE COMPARTMENT WITH NO EVIDENCE OF SMOKE OR FIRE. REMOVED AND REPLACED BOTH BAGGAGE COMPARTMENT SMOKE DETECTORS, AND BOTH FIRE BOTTLES. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1998120400619 19981204 00619 1998 12 4 P2EA98243 4 19981108 A 3418 CONNECTOR BOEING 737 737297 1384480 NM COCKPIT DIRTY A P2EA H DEACTIVATE SYST/CIRCUITS N FALSE WARNING CR CRUISE 1 CE 05 5WM 22629 FLT 707 - MSP - NO EMERGENCY DECLARED LANDING UNEVENTFUL. AOA STICK SHAKER CAME ON IN FLIGHT AN ON GROUND, PULLED C/B S HAKING STOPPED, RETURNS WHEN C/B IN RESET. FOUND STICK SHAKER CONNECTOR DIRTY, CLEANED AND RECONNECTED, OPS CHECK OK PE R MM 27-32-0. (M) 2 L 7 2 4F A16WE 1998120400620 19981204 00620 NM 1998 12 4 P2EA98247 1 19981110 A 2612 1707C FIRE CONTROL BOX BOEING 737 737222 1384473 NM E/E BAY FAILED A P2EA B E A EMER. DESCENT ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 CE 05 603DJ 125 19955 MSP - FLT 418 - EMERGENCY DECLARED NR 2 ENGINE SHUTDOWN INFLIGHT, LANDING UNEVENTFUL. ON CLIMB-OUT, NR 2 ENGINE OVERHEA T LIGHT ILLUMINATED. CHECKLIST COMPLIED WITH. REPLACED FIRE CONTROL BOX (MODULE), ALSO INSPECTED OVERHEAT LOOP. RAN E NGINE WITH BLEEDS AND ANTI-ICE ON. COULD NOT GET OVERHEAT LIGHT TO COME ON (FAIL). OPS CHECK NORMAL. REPLACED BOTH (F WD AND AFT) ENGINE FIRE BOTTLES PER MM 26-21-11. (M) 2 L 7 2 4F A16WE 1998120400621 19981204 00621 NM 1998 12 4 MASA98201 1 19981112 A 3350 OL3071BPEGPL BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 DURING A ROUTINE LINE CHECK INSPECTION, MAINTENANCE PERSONNEL, FOUND THE FLIGHT ATTENDANTS OVERHEAD EMERGENCY EXIT SIGN WITH SEVERAL BURNED OUT BULBS. MAINTENANCE REPLACED THE BULBS, OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998120400622 19981204 00622 NM 1998 12 4 MASA98200 1 19981110 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 DURING ROUTINE LINE CHECK INSPECTION, FOUND THE FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH NORMAL LIGHT DID NOT ILLUMINATED . REPLACED BULB, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998120400623 19981204 00623 NM 1998 12 4 MASA98198 1 19981104 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 FLT 6322 - PHX-GJT - WHILE THE AIRCRAFT WAS WAITING ON THE RAMP PRIOR TO DEPARTURE, PHX MAINTENANCE NOTICED THAT THE F/A 'S EMERGENCY LIGHT SWITCH BACKLIGHTING WAS INOP. RELAMPED THE SWITCH, OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1998120400624 19981204 00624 NM 1998 12 4 MASA98197 1 19981104 A 3350 AML91LA85 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 454YV 454 FLT 6205 - PHX-FLG - DURING PREFLIGHT, THE CREW REPORTED THE FLIGHT ATTENDANTS EMERGENCY LIGHT SWITCH DID NOT HAVE ANY B ACKLIGHTING. MAINTENANCE RELAMPED THE SWITCH, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998120400625 19981204 00625 CE 1998 12 4 MASA98202 1 19981113 A 5270 V3101D8 SWITCH BEECH 1900 1900D 1154162 CE CARGO DOOR OUT OF ADJUST A MASA B A EMER. DESCENT UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SW 07 33YV UE33 FLT 54 - ABQ-CNM - IN FLIGHT, CREW RECEIVED A CARGO DOOR WARNING ANNUNC. CREW DECLARED AN EMERGENCY AND DIVERTED TO ROW PER THE CFM ROW MAINTENANCE ADJUSTED THE DOOR HANDLE MICROSWITCH, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998120400626 19981204 00626 CE 1998 12 4 MASA98196 1 19981103 A 2120 UNKNOWN BEECH 1900 1900D 1154162 CE CABIN SMOKE A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 104YV UE104 FLT 700 - FMN-ABQ - AFTER TAKEOFF, CREW REPORTED SMOKE IN THE COCKPIT AND CABIN. AIRCRAFT RETURNED TO THE FIELD. NO EM ERGENCY WAS DECLARED, THE MASKS WERE NOT DEPLOYED. MAINTENANCE T/S THE SYSTEM BUT WERE UNABLE TO DUPLICATE THE DISCREPA NCY. NO DISCREPANCIES WERE NOTED, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998120400627 19981204 00627 CE 1998 12 4 MASA98193 1 19981030 A 5260 MS166241075 RETAINING RING BEECH 1900 1900D 1154162 CE AIRSTAIR DOOR SHEARED A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 70ZV UE70 FLT 5342 - GON-PHL - UPON CLOSING, THE AIRSTAIR DOOR, THE OUTER DOOR HANDLE FELL OFF. MAINTENANCE REPLACED THE RETAININ G RING AND REINSTALLED THE DOOR HANDLE, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998120400628 19981204 00628 EA 1998 12 4 MASA98189 1 19981022 A 3350 1317 BULB BRUCE BC10020004 CNDAIR CL600 CL6002B19 EA ROW 2 FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 DCA\HSV - FLT 5792 - DURING POST WALK-AROUND, CAPTAIN FOUND THE CEILING EMERGENCY LIGHT AT ROW 2 WAS NOT ILLUMINATING. M AINTENANCE DEFERRED THE EMERGENCY LIGHT PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (X) 2 L 7 2 4F RT A21EA 1998120400629 19981204 00629 EA 1998 12 4 MASA98192 1 19981030 A 3350 1317 BULB BRUCE BM10006002 CNDAIR CL600 CL6002B19 EA EMERGENCY EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 37228 7228 DURING PREFLIGHT WALK-AROUND, CREW NOTICED THE RIGHT FORWARD EXTERIOR EMERGENCY LIGHT WAS NOT ILLUMINATING. MAINTENANCE DEFERRED THE LIGHT PER MEL 33-51-2. AIRCRAFT WAS RETURNED TO SERIVCE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (X) 2 L 7 2 4F RT A21EA 1998120400630 19981204 00630 WP 1998 12 4 GTIA9800120 1 19981101 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 ACY - FLT 19 - EMERGENCY AISLE LIGHTS INOPERATIVE. FOUND BROKEN WIRE ON FORWARD SECTION OF AISLE LIGHTS REPAIRED SAME, OPERATIONAL CHECK NORMAL IAW 33-53-0. (M) 2 L 7 2 4F A6WE 1998120400631 19981204 00631 WP 1998 12 4 GTIA9800119 1 19981022 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN LOOSE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 12536 47113 ACY - FLT 876A - LAST SIX EMERGENCY FLOOR TRACK LIGHTS INOPERATIVE. FOUND WIRE DISCONNECTED. RECONNECTED WIRE, OPERATI ONAL CHECK GOOD IAW 33-53-0. (M) 2 L 7 2 4F A6WE 1998120400632 19981204 00632 WP 1998 12 4 GTIA9800124 1 19981105 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 804RA 48048 DTW - MULTIPLE OVERHEAD EMERGENCY LIGHTS OUT. REPLACED EMERGENCY BATTERY POWER SUPPLY, OPERATIONAL CHECKED GOOD IAW MD- 80 MM 33-50. (M) 2 L 7 2 4F A6WE 1998120400633 19981204 00633 WP 1998 12 4 GTIA9800123 1 19981101 A 3397 WIRE DOUG DC9 DC941 302207N WP CABIN BROKEN A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 130NK 47604 ACY - FLT 19 - EMERGENCY AISLE LIGHTS INOPERATIVE. FOUND BROKEN WIRE ON FORWARD SECTION OF AISLE LIGHTS. REPAIRED SAME OPERATIONAL CHECKS NORMAL IAW 33-53-0. (M) 2 L 7 2 4F A6WE 1998120400634 19981204 00634 WP 1998 12 4 GTIA9800122 1 19981025 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 DTW - FLT 558 - DURING DAILY, FOUND AFT TAIL CONE EMERGENCY LIGHTS INOPERATIVE. FOUND BATTERY PACK AT R-27 IN AFT LAVAT ORY INOPERATIVE. REMOVED AND INSTALLED SERVICEABLE BATTERY PACK IAW MM 33-53-0. OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1998120400635 19981204 00635 WP 1998 12 4 GTIA9800125 1 19981106 A 3350 LIGHT DOUG DC9 DC931 3022065 WP OVERWING EXIT INOPERATIVE A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 928ML 47326 DTW - EMERGENCY FLOOR TRACK LIGHTING HAS AN INOPERATIVE BULB (RED AT OVERWING EXIT). REINSTALLED LOOSE BULB IN RECEPTAC LE. OPERATION CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1998120400636 19981204 00636 NM 1998 12 4 GAIA98110 1 19981105 A 3260 CONNECTOR BOEING 727 727224 1384076 NM LT MLG LOOSE A GAIA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 69740 20668 DURING APPROACH FROM KYIP TO KHUF, WHEN GEAR WAS SELECTED DOWN, THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED ON F IRST AND SECOND ATTEMPTS. IT INDICATED DOWN AND LOCKED ON THE THIRD ATTEMPT. AN UNEVENTFUL LANDING WAS MADE. MAINTENA NCE FOUND A LOOSE CONNECTOR ON THE DOWNLOCK SWITCH. THE CONNECTOR WAS TIGHTENED. AN OPERATIONAL CHECK OF THE GEAR WAS PERFORMED SATISFACTORY IAW B727 MM 32-60. THE AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998120400637 19981204 00637 NM 1998 12 4 GAIA98111 1 19981105 A 3350 GE307 BULB BOEING 727 727223 1384074 NM BS 289 FAILED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6809 19484 FORWARD ENTRY DOOR, OVERHEAD EMERGENCY EXIT LIGHT INOP WHEN EMERGENCY EXIT LIGHT SWITCH PLACED IN ON POSITION. REPLACED FORWARD ENTRY DOOR LIGHT BULB. OPERATIONAL CHECK PERFORMED OK. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998120400638 19981204 00638 NM 1998 12 4 GAIA98112 1 19981110 A 2612 FIRE LOOP BOEING 727 727251 138408H NM FUSELAGE MALFUNCTIONED A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 EN ROUTE FROM MCI TO PHX THE AIRCRAFT HAD THE FIRE WARNING BELL COME ON WITH OUT ANY WARNING LIGHT INDICATION AS TO WHIC H ENGINE OR ANY OTHER INDICATIONS. THE AIRCRAFT LANDED WITHOUT DIFFICULTIES. TESTED THE FIRE DETECTION SYSTEM AS PER B OEING MM CHAPTER 26. CLEANED CONNECTORS AT FIRE DETECTORS AND OPERATING POWER UNITS, CHECKED CIRCUIT BREAKERS AND WIRIN G FOR THE NR 1, NR 2 AND NR 3 ENGINE FIRE DETECTION SYSTEMS AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS RETURNED TO SER VICE. (M) 2 L 7 3 4F A3WE 1998120400639 19981204 00639 NM 1998 12 4 GAIA98114 1 19981111 A 2612 SWITCH BOEING 727 727251 138408H NM COCKPIT MALFUNCTIONED A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 EN ROUTE FROM TOL TO SLC, THE AIRCRAFT HAD THE FIRE WARNING BELL COME ON WITH ANY WARNING LIGHT INDICATION AS TO WHICH E NGINE OR ANY OTHER INDICATIONS. THE AIRCRAFT LANDED WITHOUT DIFFICULTIES. FOUND GLARESHIELD SWITCH STUCK. CLEANED FIR E TEST SWITCH. OPERATIONAL CHECK FOUND NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998120400640 19981204 00640 NM 1998 12 4 GAIA98116 1 19981113 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1110 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN, MAIN CABIN FLOORBEAM HAS SURFACE CORROSION ON TOP F LANGE, BS 1110, RBL 43. REMOVED CORROSION IAW B727 SRM. FABRICATED REPAIR PARTS IAW B727 SRM. FABRICATED REPAIRPARTS IAW B727 SRM 53-10-8 FIG 8. INSTALLED REPAIR IAW B727 SRM 53-10-8 FIG 8. (M) 2 L 7 3 4F A3WE 1998120400641 19981204 00641 NM 1998 12 4 GAIA98117 1 19981113 A 5315 65C33557 FLOORBEAM BOEING 727 727224 1384076 NM BS 1176 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOOR CHORD AND UPPER ANGLE HAS SURFACE CORROSION AT BS 1176.9, LBL 61 - LBL 66. REMOVED CORRSOSION AND REPAIRED DAMAGED CHORD IAW AMERICAN INTERNATIONAL AIRW AYS EDR. ENGINEERING DEVIATION REQUEST NR B2-06136, DATED 9/19/98. (M) 2 L 7 3 4F A3WE 1998120400642 19981204 00642 NM 1998 12 4 GAIA98118 1 19981113 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1148 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FUSELAGE CIRCUMFERENTIAL FRAME HAS SURF ACE CORROSION AT BS 1148, STRINGER 16R TO 12R. CLEANED CORROSION AND FOUND, OUT OF LIMITS. FABRICATED REPAIR PART IAW B727 51-40-03, FIG 1. INSTALLED REPAIR IAW B727 SRM 51-40-03 FIG 1. (M) 2 L 7 3 4F A3WE 1998120400643 19981204 00643 NM 1998 12 4 GAIA98119 1 19981113 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 1177 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOOR CHORD ANGLE HAS SURFACE CORROSION AT BS 1177, RBL 54 TO RBL 66. REMOVED CORRODED ANGLE IAW B727 SRM 51-30-2. REPLACED ANGLE IAW B727 SRM 51-10-1 AND 51 -30-2. (M) 2 L 7 3 4F A3WE 1998120400644 19981204 00644 NM 1998 12 4 GAIA98120 1 19981113 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1070 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSION FOUND DURNIG A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOORBEAM TOP SURFACE HAS CORROSION AT BS 1070, RBL 53. REMOVED CORROSION FROM UPPER SURFACE OF FLOORBEAM IAW B727 SRM 53-10-01. INSTALLED REPAIR PARTS IAW B 727 SRM 51-30-02 AND SRM 53-10-08. (M) 2 L 7 3 4F A3WE 1998120400645 19981204 00645 NM 1998 12 4 GAIA98121 1 19981113 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 1070 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSIO NFOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. MAIN CABIN FLOORBEAM HAS SURFACE CORROSION, TOP FL ANGE, AT BS 1070 RBL 48 AND 53. REMOVED CORROSION FROM UPPER SURFACE OF FLOORBEAM IAW B727 SRM 53-10-01. FABRICATED RE PAIR PARTS IAW BAC 727 SRM 53-10-8. INSTALLED REPAIR PARTS IAW B727 SRM 51-30-02 AND SRM 53-10-08. (M) 2 L 7 3 4F A3WE 1998120400646 19981204 00646 NM 1998 12 4 GAIA98122 1 19981113 A 5320 ANGLE BOEING 727 727224 1384076 NM BS 870 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. OUTER SIDE OF FLOORBEAM WEB, AFT ATTACH ANGLE IS C ORRODED, BS 870, RBL 45. REMOVED CORROSION AND REPAIRED TEE ANGLE AT BS 870, RBL 45. REMOVED CORROSION AND REPAIRED TE E ANGLE AT BS 870, IAW B727 SRM 51-40-04. INSTALLED ANGLE AND FASTENERS, IAW B727 SRM 51-30-02. (M) 2 L 7 3 4F A3WE 1998120400647 19981204 00647 NM 1998 12 4 GAIA98123 1 19981113 A 5311 FRAME BOEING 727 727224 1384076 NM BS 1160 CORRODED A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 69739 20667 LEVEL 2 CORROSION FOUND DURING A TRANSITION LIGHT 'C' PHASE IN PLAN. CABIN FRAME HAS CORROSION AT BS 1160, STRINGER 25L . REMOVED CORROSION AND DAMAGE. FABRICATED REPAIR ANGLE IAW B727 SRM 53-10-4, FIG 12. INSTALLED REPAIR IAW B727 SRM 5 3-10-04 FIG 12. (M) 2 L 7 3 4F A3WE 1998120400648 19981204 00648 NM 1998 12 4 GAIA98108 1 19981103 A 2720 591005017 SWITCH BOEING 727 727223 1384074 NM RUDDER LOOSE A GAIA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 SW 07 6834 20187 KHA - FLT 827 - ATL-TOL - IN CLIMB, THE FLIGHT CREW NOTICED THE 'A' SYSTEM HYDRAULIC QUANTITY WAS DROPPING. AN EMERGENC Y WAS DECLARED AND THE AIRCRAFT RETURNED TO ATL. AN UNEVENTFUL LANDING WAS MADE. INVESTIGATION REVEALED THAT THE LOWER RUDDER POWER PACK WAS LEAKING HYDRAULIC FLUID DUE TO A LOOSE PRESSURE SWITCH. THE SWITCH WAS RETORQUED AND LEAK CHECKE D. THE AIRCRAFT WAS RETURNED TO SERVICE (M) 2 L 7 3 4F A3WE 1998120400649 19981204 00649 NM 1998 12 4 AALA982008 1 19981201 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 360 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FLOORBEAM UPPER CAP WORN STATION 360, BL 0. REPAIRED STATION 360 FLOORBEAM UPPER CAP AT BL 0 PER SRM 53-10-8. (M ) 2 L 7 3 4F A3WE 1998120400650 19981204 00650 NM 1998 12 4 AALA982007 1 19981023 A 5347 SEAT TRACK DOUG MD11 MD11 3023602 NM BS 1385 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1756 48491 TUL - NR 2 SEAT TRACK CORRODED AT STATION 1385. REPAIRED PER SRM 53-70-00-0 VOL 1. (M) 2 L 7 3 4F RT A22WE 1998120400651 19981204 00651 NM 1998 12 4 AALA984211 1 19981016 A 5320 SPLICE BOEING 767 767223 1385123 NM BS 434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 335AA 22333 AFW - FORWARD CARGO COMPT STRINGER SPLICES AND STRINGERS HAVE CORROSION. TRIM BACK TO COMPLETELY REMOVE THE CORROSION O N THE AFFECTED STRINGER INSTALL THE STRINGER SPLICE REPAIR. (M) 2 L 7 2 4F RT A1NM 1998120400652 19981204 00652 NM 1998 12 4 AALA984207 1 19981016 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 335AA 22333 AFW - FLOORBEAM AT STATION 347 RBL 34 HAD LIGHT CORROSION BLENDED FROM THE UPPER AND LOWER SURFACE OF THE TOP CAP. REFE R TO FIG 1, COMPLETELY REMOVED CORROSION, ALODINE ALL BARE ALUMINUM SURFACES. FINISHED BLENDED AREA WITH TWO COATS OF P RIMER. FILL BLENDS WITH PROSEAL 870. (M) 2 L 7 2 4F RT A1NM 1998120400653 19981204 00653 NM 1998 12 4 AALA984206 1 19981015 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 335AA 22333 AFW - FOUND FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL ON UPPER SURFACE. FABRICATE REPAIR STRAP OUT OF 301.5 H STA INLESS STEEL, .050 THICK. ALODINE AND PRIME ALL BARE SURFACES. FILL BLENDS WITH BMS 5-92. INSTALL REPAIR STRAP WET WI TH BMS-95 SEALANT. (M) 2 L 7 2 4F RT A1NM 1998120400654 19981204 00654 NM 1998 12 4 AALA984204 1 19981009 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 379AA 25448 AFW - FLOORBEAM AT RBL 33 HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCH. BLEND OUT ALL CORROSION. DYE PENE TRANT INSPECT AND ROTO-PEEN REPAIRS AREA. ALODINE ALL BARE SURFACES. FINISH WITH 2 COATS OF BMS-10-11 PRIMER. FILL BL END WITH BMS5-95. (M) 2 L 7 2 4F RT A1NM 1998120400655 19981204 00655 NM 1998 12 4 AALA984203 1 19981009 A 5315 FLOORBEAM BOEING 767 767323 1385205 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 379AA 25448 AFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL ON UPPER SURFACE AS SHOWN ON SKETCHES. FABRICATED STRAP FROM 301. 5 HARD STAINLESS STEEL .050 INCH THICK APPLIED TWO COATS OF BMS-10-11 PRIMER TO THE STRAP AND FLOORBEAM. FILLED BLENDED AREA WITH BMS5-92. INSTALLED STRAP WET WITH BMS5-95 SEALANT PROSEAL OF 70 USING BAC B30NW6 HI-LOCKS. (M) 2 L 7 2 4F RT A1NM 1998120400656 19981204 00656 NM 1998 12 4 AALA984199 1 19981009 A 5311 FRAME BOEING 767 767223 1385123 NM BS 1087 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 316AA 22318 AFW - AFT CARGO FRAME J CAP AT STATION 1087 RBL 20 HAD CORROSION BLENDED BEYOND SRM LIMITS. REPAIR IAW MRB 767-1719. ( M) 2 L 7 2 4F RT A1NM 1998120400657 19981204 00657 EU 1998 12 4 AALA981928 1 19981023 A 5315 FLOORBEAM FOKKER F28 F28MK0100 4990807 EU BS 4610/4850 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1449D 11458 TUL - FLOORBEAM NR 5 HEAVY CORROSION. INSTALLED FLOORBEAM STRAP 53-12-10-1 PAGE NR 2 ITEM B. (M) 2 L 7 2 4F RT 1998120400658 19981204 00658 WP 1998 12 4 ZIAA98039 1 19981003 A 5330 2014T6AL SKIN DOUG DC8 DC8F54 3021926 WP BS 600 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 8041U 57385 45675 YIP - BELLY AT APPROXIMATELY FS 600, REINFORCING PLATE HAS SEVERAL POPPED RIVETS. REMOVED PLATE DUE TO CORROSION. REMO VED SKIN DAMAGE DUE TO CORROSION. REPAIRED SKIN IAW ZANTOP DRAWING SKA95008-1 REVISION A. SEALED EDGES WITH CS3204 B1/ 2. (M) 2 L 7 4 4F 4A25 1998120400659 19981204 00659 WP 1998 12 4 ZIAA98038 1 19980817 A 5730 8005191 PANEL LKHEED 188 188A 5262602 WP WS 88-91 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK UPPER SURFACE. THREE INCH LONG SUBSURFACE RP/UT CORROSION/CR ACK INDICATION IN PLANK 9 AT 8/9 JOINT, LWS 88-91. ROUTED OUT CRACKED AREA, WS 87 TO WS 90 PER SB620. INSTALLED REPAIR PER SB620 DRAWING 841880. (M) 2 L 7 4 4T RT 4A22 1998120400660 19981204 00660 WP 1998 12 4 ZIAA98037 1 19980817 A 5730 8339883 PANEL LKHEED 188 188A 5262602 WP WS 78-83 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK LOWER SURFACE, 5 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK I NDICATION IN PLANK 4 AT 3/4 PLANK JOINT, LWS 78-83. ROUTED OUT CRACKED AREA, LRWS 77.5 TO LWS 83.5, PER SB620. FABRICA TED AND INSTALLED REPAIR PER L-188 SRM 57-2-1 FIG 3, SHEET 25. (M) 2 L 7 4 4T RT 4A22 1998120400661 19981204 00661 WP 1998 12 4 ZIAA98036 1 19980817 A 5730 8233351 PANEL LKHEED 188 188A 5262602 WP WS 92-96 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK UPPER SURFACE, 4 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK I NDICATION IN PLANK 5 AT 4/5 PLANK JOINT, LWS 92-96. ROUTED OUT CRACKED AREA, LRWS93 TO LWS96, PER SB 620. FABRICATED A ND INSTALLED REPAIR PER L-188 SRM 57-2-1 FIG 3, SHEET 25. (M) 2 L 7 4 4T RT 4A22 1998120400662 19981204 00662 WP 1998 12 4 ZIAA98035 1 19980817 A 5730 8398011 PANEL LKHEED 188 188A 5262602 WP WS 103-105 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK LOWER SURFACE, 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK I NDICATION IN PLANK 1 AT 1/2 PLANK JOINT, LWS 103.5-105.5. ROUTED OUT CRACKED AREA, LRWS103 TO LWS106,PER SB620. FABRIC ATED AND INSTALLED REPAIR PER L-188 SRM 57-2-1 FIG 3, SHEET 25. (M) 2 L 7 4 4T RT 4A22 1998120400663 19981204 00663 WP 1998 12 4 ZIAA98034 1 19980815 A 5730 8233352 PANEL LKHEED 188 188A 5262602 WP WS 286-287 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 4 FUEL TANK UPPER SURFACE, 1 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 5 AT 4/5 PLANK JOINT, RWS 286-287. ROUTED OUT CRACKED AREA, RWS284 TO RWS286, PER SB620. FABRICATE D AND INSTALLED REPAIR PER L-188 SRM 57-2-1 PAGE 33. (M) 2 L 7 4 4T RT 4A22 1998120400664 19981204 00664 WP 1998 12 4 ZIAA98033 1 19980815 A 5730 8005501 PANEL LKHEED 188 188A 5262602 WP WS 37-49 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, CENTER DRY BAY LOWER SURFACE, 11.5 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATI ON IN PLANK 5 AT 5/6 PLANK JOINT, LWS 37.5-49. ROUTED OUT CRACKED AREA, LWS37 TO LWS49, PER SB620. FABRICATED AND INST ALLED REPAIR PER L-188 SRM 57-2-1, SHEET 25. (M) 2 L 7 4 4T RT 4A22 1998120400665 19981204 00665 WP 1998 12 4 ZIAA98032 1 19980818 A 5730 8398031 PANEL LKHEED 188 188A 5262602 WP WS 166-168 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING LOWER SURFACE DRY BAY, 2 INCH LONG SUBSRUFACE RP/UT CORROSION/CRACK INDICATI ON IN PLANK 3 AT 2/3 PLANK JOINT, LWS 166-168. ROUTED OUT CRACKED AREA, LWS164 TO LWS168, PER SB620. FABRICATED AND IN STALLED REPAIR PER SB620 DWG 841880. (M) 2 L 7 4 4T RT 4A22 1998120400666 19981204 00666 WP 1998 12 4 ZIAA98031 1 19980818 A 5730 8398121 PANEL LKHEED 188 188A 5262602 WP WS 172-179 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LT WING UPPER SURFACE-DRY BAY, 7 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 2 AT 2/3 PLANK JOINT, LWS 172-179. ROUTED OUT CRACKED AREA, LWS 176 TO LWS 180, PER SB 620. REPAIRED PER ZIA DRAWING F25-R07. (M) 2 L 7 4 4T RT 4A22 1998120400667 19981204 00667 WP 1998 12 4 ZIAA98030 1 19980818 A 5730 8005171 PANEL LKHEED 188 188A 5262602 WP WS 188-193 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 5 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICAT ION IN PLANK 7 AT 6/7 PLANK JOINT, LWS 188-193. ROUTED OUT CRACKED AREA, LWS 188.5 TO LWS197.5, PER SB 620. FABRICATED AND INSTALLED REPAIR PER SB620 DRAWING 841880. (M) 2 L 7 4 4T RT 4A22 1998120400668 19981204 00668 WP 1998 12 4 ZIAA98029 1 19980818 A 5730 8233311 PANEL LKHEED 188 188A 5262602 WP WS 181-183 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICAT ION IN PLANK 1 AT 1/2 PLANK JOINT, LWS 181-183. ROUTED OUT CRACKED AREA, LWS176.5 TO LWS180.5, PER SB620. REPAIRED PER ZIA DRAWING F25-R07. (M) 2 L 7 4 4T RT 4A22 1998120400669 19981204 00669 WP 1998 12 4 ZIAA98028 1 19980818 A 5730 8233311 PANEL LKHEED 188 188A 5262602 WP WS 196-198 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING UPPER SURFACE-DRY BAY. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICAT ION IN PLANK 1 AT 1/2 PLANK JOINT, LWS 196-198. ROUTED OUT CRACKED AREA, LWS194 TO LWS196.5, PER SB620. REPAIRED PER Z IA DRAWING F25-R07. (M) 2 L 7 4 4T RT 4A22 1998120400670 19981204 00670 WP 1998 12 4 ZIAA98027 1 19980818 A 5730 8339883 PANEL LKHEED 188 188A 5262602 WP WS 115-117 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK-LOWER SURFACE. 2 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 4 AT 3/4 PLANK JOINT, LWS 115-117. ROUTED OUT CRACKED AREA, LWS115 TO LWS119, PER SB620. REPAIRED PER ZIA DRAWING F25-R06. (M) 2 L 7 4 4T RT 4A22 1998120400671 19981204 00671 WP 1998 12 4 ZIAA98018 1 19980815 A 5730 800547 PANEL LKHEED 188 188A 5262602 WP WS 40-48 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, CENTER DRY BAY, LOWER SURFACE. 8 INCH LONG RP/UT CORROSION/CRACK INDICATION IN PLANK NR 2 AT 2/3 PLANK JOINT, RWS 40-48. ROUTED OUT CRACKED AREA, WS 39 TO WS 46 PER SB620. REPAIRED PER ZIA DRAWING F25-R0 8. (M) 2 L 7 4 4T RT 4A22 1998120400672 19981204 00672 WP 1998 12 4 ZIAA98017 1 19980815 A 5730 8233312 PANEL LKHEED 188 188A 5262602 WP WS 80-81 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RT WING NR WING NR 3 FUEL TANK UPPER SURFACE. 1 INCH LONG SUBSURFACE RP/UT CORROSION/ CRACK INDICATION IN PLANK 1 AT 1/2 PLANK JOINT, RWS 80-81. ROUTED OUT CRACKED AREA, WS 78.5 TO WS 80 PER SB620. REPAIR ED PER ZIA DRAWING F25-R02. SEALED REPAIR WITH CS3204 A1/2 AS REQUESTED. (M) 2 L 7 4 4T RT 4A22 1998120400673 19981204 00673 WP 1998 12 4 ZIAA98016 1 19980815 A 5730 8233362 PANEL LKHEED 188 188A 5262602 WP WS 227-230 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 4 FUEL TANK UPPER SURFACE. 3 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 6 AT 5/6 PLANK JOINT, RWS 227-230. ROUTED OUT CRACKED AREA, WS 227 TO WS 228.5 PER SB620. FABRICA TED AND INSTALLED REPAIR PER L-188 SRM 57-2-1 PAGE 33. SEALED REPAIR WITH CS3204 A1/2 AS REQUESTED. (M) 2 L 7 4 4T RT 4A22 1998120400674 19981204 00674 WP 1998 12 4 ZIAA98015 1 19980815 A 5730 8233362 PANEL LKHEED 188 188A 5262602 WP WS 142-145 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 3 FUEL TANK UPPER SURFACE. THREE INCH LONG SUBSURFACE RP/UT CORROSION/C RACK INDICATION IN PLANK 6 AT 5/6 PLANK JOINT, RWS 142-145. ROUTED OUT CRACKED AREA, WS 145 TO WS 141 PER SB620. FABRI CATED AND INSTALLED REPAIR PER L-188 SRM 57-2-1 FIG 3 SHEET 25. SEALED REPAIR WITH CS3204 A1/2 AS REQUESTED. (M) 2 L 7 4 4T RT 4A22 1998120400675 19981204 00675 WP 1998 12 4 ZIAA98014 1 19980815 A 5730 8233362 PANEL LKHEED 188 188A 5262602 WP WS 119-121 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 3 FUEL TANK UPPER SURFACE. 1.5 INCH LONG SUBSURFACE RPEC CORROSION/CRAC K INDICATION IN PLANK 6 AT 5/6 PLANK JOINT, RWS 119.5-121. ROUTED OUT CRACKED AREA, WS 119 TO WS 121 PER SB620. FABRIC ATED AND INSTALLED REPAIR PER L-188 SRM 57-2-1 FIG 3 SHEET 25. SEALED REPAIR WITH CS3204 A1/2 AS REQUESTED. (M) 2 L 7 4 4T RT 4A22 1998120400676 19981204 00676 WP 1998 12 4 ZIAA98013 1 19980815 A 5730 8233352 PANEL LKHEED 188 188A 5262602 WP WS 142-143 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 3 FUEL TANK UPPER SURFACE. ONE INCH LONG SUBSURFACE RP/UT CORROSION/CRA CK INDICATION IN PLANK 5 AT 4/5 PLANK JOINT, RWS 142-143. ROUTED OUT CRACKED AREA, WS 141 TO WS 144 PER SB620. FABRICA TED AND INSTALLED REPAIR PER L-188 SRM 57-2-1 FIG 3 (SHEET 25). SEALED REPAIR WITH CS3204 A1/2 AS REQUESTED. (M) 2 L 7 4 4T RT 4A22 1998120400677 19981204 00677 WP 1998 12 4 ZIAA98010 1 19980804 A 5730 8005162 PANEL LKHEED 188 188A 5262602 WP WS 200 CRACKED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 5512 46173 188A1017 YIP - RIGHT DRY BAY UPPER SURFACE CRACK AT WS 200 BETWEEN RISER 40-41 COMING FROM OUTBOARD SKATE ANGLE FASTENERS, ROUTED OUT CRACK. REPAIRED PER ZIA SKETCH NR F14-R01. (M) 2 L 7 4 4T RT 4A22 1998120400678 19981204 00678 WP 1998 12 4 ZIAA98012 1 19980815 A 5730 8005182 PANEL LKHEED 188 188A 5262602 WP WS 78 TO 102 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 3 FUEL TANK UPPER SURFACE. 23.5 INCH LONG SUBSURFACE AND SURFACE CORROS ION, RP/UT CORROSION/CRACK INDICATION IN PLANK 8 AT 7/8 JOINT, RWS 78.5-102. ROUTED OUT CRACKED AREA WS88 TO WS91 PER S B 620. ALL OTHER AREAS, WIDEN SPLICE GAP. REMOVED CORROSION CONFIRMED WITH DYE-CHECK. MATERIAL REMOVED NEGLIGIBLE PER SB 620. REPAIRED PER L-188 SRM 57-2-1 PAGE 33. SEALED REPAIR WITH CS3204 A1/2 AS REQUESTED. (M) 2 L 7 4 4T RT 4A22 1998120400679 19981204 00679 WP 1998 12 4 ZIAA98026 1 19980817 A 5730 8398121 PANEL LKHEED 188 188A 5262602 WP WS 77-80 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK UPPER SURFACE. THREE INCH LONG SUBSURFACE RP/UT CORROSION/CR ACK INDICATION IN PLANK 2 AT 2/3 PLANK JOINT, LWS 77-80. ROUTED OUT CRACKED AREA, LWS76 TO LWS80, PER SB620. FABRICATE D AND INSTALLED REPAIR PER L-188 SB678 DRAWING 842451. (M) 2 L 7 4 4T RT 4A22 1998120400680 19981204 00680 WP 1998 12 4 ZIAA98025 1 19980817 A 5730 8233351 PANEL LKHEED 188 188A 5262602 WP WS 147-148 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LT WING NR 2 FUEL TANK UPPER SURFACE. ONE INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 5 AT 4/5 PLANK JOINT, LWS 147.5-148.5. ROUTED OUT CRACKED AREA, LWS146 TO LWS149.5, PER SB620. REP AIRED PER ZIA DRAWING F25-R03. (M) 2 L 7 4 4T RT 4A22 1998120400681 19981204 00681 WP 1998 12 4 ZIAA98024 1 19980817 A 5730 8233351 PANEL LKHEED 188 188A 5262602 WP WS 138-144 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, LEFT WING NR 2 FUEL TANK UPPER SURFACE. 3.5 INCH LONG SUBSURFACE RP/UT CORROSION/CRAC K INDICATION IN PLANK 5 AT 4/5 PLANK JOINT, LWS 139.5-143. ROUTED OUT CRACKED AREA, LWS138 TO LWS144, PER SB620. REPAI RED PER ZIA DRAWING F25-RO3. (M) 2 L 7 4 4T RT 4A22 1998120400682 19981204 00682 WP 1998 12 4 ZIAA98023 1 19980815 A 5730 8233352 PANEL LKHEED 188 188A 5262602 WP WS 193-194 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 3 EXHAUST AREA. 1 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICATION IN PLANK 5 AT 4/5 PLANK JOINT, RWS 193-194. ROUTED OUT CRACKED AREA, RWS 190 TO RWS 192, PER SB 620. REPAIRED PER ZIA DRAWING F25-R05. (M) 2 L 7 4 4T RT 4A22 1998120400683 19981204 00683 WP 1998 12 4 ZIAA98022 1 19980815 A 5730 8398122 PANEL LKHEED 188 188A 5262602 WP WS 1860187 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, RIGHT WING NR 3 NACELLE UPPER SURFACE. 1 INCH LONG SUBSURFACE RP/UT CORROSION/CRACK I NDICATION IN PLANK 2 AT 2/3 PLANK JOINT, RWS 186-187. ROUTED OUT CRACKED AREA, RWS 185 TO RWS 188, PER SB 620. REPAIRE D PER ZIA DRAWING F25-R01. (M) 2 L 7 4 4T RT 4A22 1998120400684 19981204 00684 WP 1998 12 4 ZIAA98021 1 19980815 A 5730 8233351 PANEL LKHEED 188 188A 5262602 WP WS 199-202 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION,RIGHT WING NR 3 EXHAUST AREA. THREE INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICAT ION IN PLANK 5 AT 4/5 PLANK JOINT, RWS 199-202. ROUTED OUT CRACKED AREA, RWS 198 TO RWS 202, PER SB620. REPAIRED PER Z IA DRAWING F25-R05. (M) 2 L 7 4 4T RT 4A22 1998120400685 19981204 00685 WP 1998 12 4 ZIAA98020 1 19980815 A 5730 8005471 PANEL LKHEED 188 188A 5262602 WP WS 5-9 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, CENTE RDRY BAY, LOWER SURFACE. FOUR INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICA TION IN PLANK 2 AT 2/3 PLANK JOINT, LWS 5-9. ROUTED OUT CRACKED AREA, LWS 6 TO LWS 9 PER SB620. FABRICATED AND INSTALL ED REPAIR PER L-188 SRM 57-2-1 PAGE 33. (M) 2 L 7 4 4T RT 4A22 1998120400686 19981204 00686 WP 1998 12 4 ZIAA98019 1 19980815 A 5730 8005501 PANEL LKHEED 188 188A 5262602 WP WS 17-19 CRACKED C TM9B K NONE O OTHER IN INSP/MAINT 1 GL 23 346HA 50657 188A1043 YIP - PER AD 66-04-02 INSPECTION, CENTER DRY BAY, LOWER SURFACE. TWO INCH LONG SUBSURFACE RP/UT CORROSION/CRACK INDICAT ION IN PLANK 5 AT 5/6 PLANK JOINT, RWS 17-19. ROUTED OUT CRACKED AREA, WS 14 TO WS 21 PER SB620. REPAIRED PER ZIA DRAW ING F25-R04. (M) 2 L 7 4 4T RT 4A22 1998120400687 19981204 00687 SO 1998 12 4 ZIAA98011 1 19980914 A 5330 8001201 SKIN LKHEED 188 188C 5262604 SO BS 200-237 CORRODED A ZIAA K NONE O OTHER IN INSP/MAINT 1 GL 23 286F 62035 188C1146 YIP - POPPED RIVETS RIGHT SIDE, FORWARD OF BELLY DOOR CUTOUT. REMOVED CORRODED SECTION OF FUSELAGE SKIN AT RFS 200 TO 2 37.5. REPAIRED SKIN BY REPLACING SKIN FROM STATION 200 TO 237.5 AS PER L-188 SRM 53-2-1 PAGE 9 FIG 2 SHEET 2. (M) 2 L 7 4 4T 4A22 1998120400688 19981204 00688 NM 1998 12 4 USAA980509 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURIGN Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 8R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998120400689 19981204 00689 NM 1998 12 4 USAA980517 1 19981029 A 5320 693535214 CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 1R TIE CLIP. REMOVED AND REPLACED PER EO 5393G227 REV 'A'. (M) 2 L 7 2 4F A16WE 1998120400690 19981204 00690 WP 1998 12 4 TWAA9819101 1 19981201 A 3397 010560100 WIRE DOUG DC9 DC983 3022083 WP ROW 1 BROKEN A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 EIBWD 49575 FOUND COVER FOR EGRESS FLOOR LIGHTING BY SEAT 1D WAS BROKEN AND WIRE DAMAGED. REPAIRED WIRING, REPLACED A LAMP ASSY, (P /N 0105606-003) AND INSTALLED NEW TRACK COVER. CHECK-C 2-6-98 MCI. 2 L 7 2 4F RT A6WE 1998120400691 19981204 00691 WP 1998 12 4 TWAA9819102 1 19981129 A 5312 BULKHEAD TEE DOUG DC9 DC951 3022051 WP FUSELAGE CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 406EA 47686 EDDY CURRENT FOUND TWO CRACK INDICATIONS IN RADIUS OF BULKHEAD TEE BETWEEN LONGERON 8R AND 9R. REMOVED AND REPLACED SEC TION OF BULKHEAD TEE BETWEEN LONGERON 6R AND 11R PER SRM 53-03, FIG 37. CHECK-C 4-13-98 STL. 2 L 7 2 4F RT A6WE 1998120400692 19981204 00692 NM 1998 12 4 TWAA9819103 1 19981125 A 5753 SKIN BOEING 767 767231 1385131 NM LT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 609TW 22572 DURING CHECK-C MAINT, FOUND LT WING O/B FLAP, LOWER SURFACE AT I/B END, WITH DELAMINATION APPROX 12 IN BY 27 IN. APPLIE D 28 IN BY 16 IN HOT BOND REPAIR PER SRM 57-53-01 AND SRM 51-70-05. 2 L 7 2 4F RT A1NM 1998120400693 19981204 00693 1998 12 4 SPAA9800008 4 19981020 A 2565 116111DG SLIDE BOEING 737 7372T4 1384492 NM R-1 DOOR DID NOT INFLATE A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 R1 DOOR EMERGENCY ESCAPE SLIDE FAILED TO PROPERLY INFLATE DURING CREW TRAINING EXERCISE. THE EVACUATION SLIDE ASSEMBLY WAS ROUTED TO THE OVERHAUL VENDOR FOR EVALUATION. THE OVERHAUL VENDOR REPLACED THE REGULATOR VALVE ASSEMBLY, (P/N 3001- BN) AND INFLATION HOSE ASSEMBLY, (P/N 1271-1080K) TO CORRECT THE SLOW INFLATION AND LOW PRESSURE SITUATION. 2 L 7 2 4F A16WE 1998120400694 19981204 00694 WP 1998 12 4 VJ9800631 1 19981126 A 2170 1808491 COALESCER BAG DOUG DC9 DC932 3022066 WP CABIN DIRTY A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 930VV 47723 ON T/O, VAPOR WAS PRESENT IN CABIN AND AFT SMOKE DETECTOR ACTIVATED AS PRECAUTION. RETURN TO FORT LAUDERDALE. REMOVED AND REPLACED BOTH COALESCER BAGS, ADJUSTED SENSE LINE (APU) WIPE DUST, CLEAN OFF RESIDUE. RAN BOTH ENGINES AT HIGH POWE R AND NO SMOKE NOTED. ALL WORK IAW 21-00. 2 L 7 2 4F A6WE 1998120400695 19981204 00695 WP 1998 12 4 VJ9800632 1 19981129 A 2170 21D101 COALESCER BAG DOUG DC9 DC932 3022066 WP CABIN DIRTY A ZZDA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 15 930VV 47723 RESIDUAL SMOKE/OIL FROM APU MAINTENANCE SET OFF AFT LAV SMOKE DETECTORS SHORTLY AFTER T/O. SOUNDED FOR 30 SECONDS THEN WENT OUT. LANDING WEIGHT APROXIMATELY 100,000 LBS, NEEDS INSPECTION. REMOVED AND REPLACED COALESCER BAGS ON RT AND LT PACKS IAW 21-00, OPS CHECKED GOOD. NO SMELL OF OIL OR SMOKE. C/W OVERWEIGHT LANDING INSPECTION PER W/C 0022B SHEET A, NO DEFECTS NOTED AT THIS TIME. 2 L 7 2 4F A6WE 1998120400696 19981204 00696 WP 1998 12 4 VJ9800633 1 19981116 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 229-399 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING A SCHEDULED INSPECTION, THE FUSELAGE SKIN AT FS 229 TO 399 L18R TO 26R WAS REMOVED AND REPLACED DUE TO NUMEROUS D ENTS OUT OF LIMITS AND TWO LARGE EXISTING REPAIRS. 2 L 7 2 4F A6WE 1998120400697 19981204 00697 WP 1998 12 4 VJ9800634 1 19981120 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING SCHEDULED INSPECTION, THE FUSELAGE AT FS 965 L16R TO L17R WAS FOUND CRACKED. CUT OUT CRACK, FABRICATED AND INSTA LLED REPAIR FILLER AND DOUBLER IAW DC9 SRM 51-10-3, 51-20-1, 51-10-4, 53-04 FIGURE 17 AND AIRTRAN RES 981976. 2 L 7 2 4F A6WE 1998120400698 19981204 00698 WP 1998 12 4 VJ9800635 1 19981201 A 5320 PANEL DOUG DC9 DC932 3022066 WP BS 658-756 CORROSION A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING A SCHEDULED INSPECTION, LT W/W FWD OUTBOARD CORNER HAS CORROSION ON FWD SKIN FS 658 TO 756. REMOVED PRESSURE PAN EL, FORMED NEW PRESSURE PANEL AND SPLICES, DRILLED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-4, 51-10-3, 51-20 AND RES 989 54. 2 L 7 2 4F A6WE 1998120400699 19981204 00699 WP 1998 12 4 VJ9800636 1 19981114 A 5347 SEAT TRACKS DOUG DC9 DC932 3022066 WP CABIN CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 SCHEDULED INSPECTION, SEAT TRACKS WERE FOUND WITH CORROSION AND OUT OF LIMITS IN THE FOLLOWING LOCATIONS: LBL 22 BS 275 TO 589, LBL 44 BS 275 TO 589, RBL 22 BS 398 TO 550 AND FS 936 TO 996. REMOVED AND REPLACED SEAT TRACKS IAW DC9 SRM 53- 05 FIG 4F, 51-10-3 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1998120400700 19981204 00700 1998 12 4 JBXA9800059 4 19981201 A 3418 6005915615 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE STICK PUSHER MALFUNCTIONED A JBXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 05 573ML 7227 STALL FAIL MESSAGE ON EICAS ON TAKEOFF AFTER GEAR RETRACTION. REMOVED AND REPLACED STICK PUSHER ACTUATOR. OPERATIONAL TEST OF STALL PROTECTION SYSTEM GOOD. WORK PERFORMED IAW 27-35-15. 2 L 7 2 4F 4 F RT A21EA E15NE 1998120400701 19981204 00701 NM 1998 12 4 AWXA9800224 1 19981114 A 4990 PUMP BOEING 737 7373Y0 1384671 NM APU LOOSE A AWXA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 28 331AW 23747 CREW REPORTED WHITE VAPOR/SMOKE IN CABIN. RAN LEFT PACK AND FLT DECK FILLED WITH SMOKE, SO THE APU WAS SHUT DOWN. FOUN D LEAKING FROM SPLIT IN OIL PUMP. TIGHTENED SCREWS AND LEAK STOPPED. 2 L 7 2 4F RT A16WE 1998120400702 19981204 00702 NM 1998 12 4 AWXA9800227 1 19981127 A 3397 WIRE BOEING 757 757225 1384959 NM ROW 33 BROKEN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 907AW 22691 AFT CABIN SECTION SEAT ESCAPE PATH EMERGENCY LIGHTS INOP. REPAIRED WIRING AT SEAT 33ABC, REMOVED AND REPLACED F1 FUSE O N M9002 OPS CK GOOD. 2 L 7 2 4F RT A2NM 1998120400703 19981204 00703 EU 1998 12 4 AWXA9800228 1 19981129 A 3231 S4340131004 VALVE AIRBUS 320 A320232 3930326 EU RT MLG WW MALFUNCTIONED A AWXA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 28 647AW 762 LOUD NOISE BANGING TYPE HEARD AND FELT IN COCKPIT TO ROW 4 DURING FLIGHT. UNABLE TO IDENTIFY SOURCE OF NOISE, DIVERTED FLIGHT TO TPA. REMOVED AND REPLACED SAFETY VALVE 49GA PER MM 32-31-17. OPERATIONAL CHECK GOOD PER 32-31-00-710-005. 2 L 7 2 4F RT A28NM 1998120400704 19981204 00704 NM 1998 12 4 AWXA9800229 1 19981201 A 2782 500639R ACTUATOR BOEING 737 737297 1384480 NM RT LE SLAT MALFUNCTIONED A AWXA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 28 147AW 22630 CABIN FLOORBEAM STA 696 LBL 63 FLOORBEAM WEB IS CRACKED, MARKED NR 38. RESEARCHED, NOT A REPAIR IN THE SRM MAPPED AREA AND SENT TO ENGINEERING REF LOG 5082720. 2 L 7 2 4F A16WE 1998120400705 19981204 00705 WP 1998 12 4 9810511225 1 19981124 A 3350 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN SMOKING A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 01 225NW 46582 DURING CRUISE, NOTICED SMOKE IN OVERHEAD CEILING BETWEEN FIRST GALLEY AND COAT CLOSET. ALSO, SMOKE COMING FROM EMERGENC Y POWER SUPPLY. FLIGHT DIVERTED TO GEG AND LANDED WITHOUT INCIDENT. REPLACED BATTERY PACK AND POWER SUPPLY, OPERATIONA L CHECK OK. 2 L 7 3 4F A22WE 1998120400706 19981204 00706 WP 1998 12 4 9810521237 1 19981126 A 3350 POWER SUPPLY DOUG DC10 DC1030 3023501 WP CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 237NW 47884 DURING LINE CHECK, MID CABIN POWER SUPPLY FAILED. REPLACED MID CABIN BATTERY PACK AND POWER SUPPLY, OPERATIONAL CHECK O K. 2 L 7 3 4F A22WE 1998120400707 19981204 00707 WP 1998 12 4 9810531162 1 19981127 A 3350 BATTERY PACK DOUG DC10 DC1040 3023508 WP ROW 22-27 DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 162US 46771 DURING LINE CHECK, LEFT AND RIGHT AISLE ESCAPE PATH LIGHTS OUT FROM ROW 22 TO 27. REPLACED BATTERY PACK AND CHARGER, OP ERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1998120400708 19981204 00708 WP 1998 12 4 9810549611 1 19981126 A 3260 LIGHT DOUG DC9 DC932 3022066 WP LT MLG INOPERATIVE A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 611NA 47435 DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR DOWN AND LOCKED GREEN INDICATION LIGHT ILLUMINATED WITH THE LANDING GEAR IN THE RETRACTED POSITION. THE FLIGHT CREW REDUCED AIRSPEED AND RECYCLED THE LANDING GEAR. AFTER RECYCLING, THE NOSE LAND ING GEAR UNSAFE RED LIGHT ILLUMINATED WITH LANDING GEAR RETRACTED. THE LANDING GEAR WAS AGAIN RECYCLED WITH NORMAL INDI CATIONS. THE FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT LANDING GEAR G REEN LIGHT MODULE AND THE LANDING GEAR INDICATION PROCESSOR UNIT PRECAUTIONARY. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998120400709 19981204 00709 NM 1998 12 4 QXEA9801760 1 19981018 A 5510 85510006001 STRINGER DHAV DHAV DHC8 DHC8102 2809003 NM HORIZ STAB DISBONDED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 812PH 26 DURING NDT INSPECTION, ON LEFT (TOP AND BOTTOM) AND RIGHT (TOP AND BOTTOM) OF HORIZONTAL STABILIZER REQUIRED BY TASK 550 0/01, FOUND SEVERAL LOCATIONS OF STRINGER DISBONDED. REMOVED AND REPLACED HORIZONTAL STABILIZER. 2 H 7 2 4T RT A13NM 1998120400710 19981204 00710 WP 1998 12 4 ARWA981201 1 19981202 A 7930 42D491C SWITCH DOUG DC8 DC862 3021970 WP NR 1 ENGINE INOP A ARWA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 19 810BN 45905 PRECAUTIONARY SHUT DOWN DUE ENGINE OIL PRESSURE LIGHT FOR NR 1 ENGINE. FOLLOWED ABNORMAL CHECKLIST FOR ENGINE OIL PRESS . LIGHT ON, OIL PRESS 48 PSI, OIL TEMPERATURE MAX 105 DEGREE AFTER THROTTLE RETARD DURING CLIMB 80 PSI, OIL PRESS WHEN ENGINE WINDMILLING, 10 PSI. CHECKED OIL PRESS FILTER, OK. SERVICE ENGINE OIL, GROUND RUN SATISFACTORY; DIF PRESS SWITC H FOUND U/S, DISCONNECTED SWITCH AND TRANSFERRED TO DMI LOG NR 9441. REMOVED AND REPLACED DIF PRESS SWITCH PER MM 79-33 -0. OPS CHECKED NORMAL. 2 L 7 4 4F 4A25 1998120800001 19981208 00001 WP 1998 12 8 VJ9800606 1 19981022 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 945-966 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 25 937VV 45774 DENT AT FS 945-966, L22R, .021X1.5, DEPTH .026 DX=58, OUT LIMIT IAW DC9 SRM 53-04, FIG 38, SHEET 10. COLD WORKED AREA, VERFIED NO CRACK BY HFEC, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-04, FIG 38, 51-30-2 AND AIRTRAN RES 981 842. 2 L 7 2 4F A6WE 1998120800002 19981208 00002 WP 1998 12 8 ABXA9801054 1 19981015 A 5312 991556531 BULKHEAD CHANNEL DOUG DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 906AX 47072 WHILE COMPLYING WITH D-INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR HAD A CRACK ON BOTTOM CHANNEL. REPLACED LOWER C HANNEL IAW DC9 SRM CHAPTERS 51-10-2, 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998120800003 19981208 00003 NM 1998 12 8 DL76G982376 1 19981115 A 2421 IDG BOEING 767 7673P6 1385105 NM NR 1 ENGINE MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 154DL 533 25241 695339 NR 1 IDG DRIVE LIGHT EICAS MSG, NR 1 IDG DISCONNECTED. A/C RETURNED TO ATL FOR UNEVENTFUL OVERWEIGHT LANDING. REPLACED NR 1 IDG. SWAPPED TO A/C 172 TO MINIMIZE DELAY. 2 L 7 2 4F RT A1NM 1998120800004 19981208 00004 NM 1998 12 8 DLM88982410 1 19981121 A 4990 OIL SYST DOUG MD88 MD88 3023688 NM APU COMPT LEAK A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 905DL 7866 49536 P80224 AFTER T/O, THE RIGHT AFT LAVATORY SMOKE DETECTOR WENT OFF. FLIGHT ATTENDANT REPORTED BURNING SMELL. RETURNED TO JFK. A PU OIL LEAK. DUCT BURNOUT AND SOCK CHANGED. 2 L 7 2 4F RT A6WE 1998120800005 19981208 00005 WP 1998 12 8 TWAA9818802 1 19981122 A 3350 58222 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 7 DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 911TW 49182 FOUND EGRESS TRACK LIGHTING INOPERATIVE BETWEEN CABIN ROW 2 AND 15. REPLACED BATTERY PACK AND REPAIRED FEEDER STRIP AT ROW 7. CHECK-C 9-17-98 STL. 2 L 7 2 4F A6WE 1998120800006 19981208 00006 SO 1998 12 8 SWIA971312 1 19981110 A 2750 FCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 298SW 120328 AFTER TAKEOFF AND FLAP RETRACTION, FLAP DISAGREEMENT COULD NOT FIX. RETURNED TO SFO. REPLACED FCU, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998120800007 19981208 00007 NE 1998 12 8 ARWA981129 2 19981123 A 7200 ENGINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 FAILED A ARWA E ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SO 19 661AV 45969 SHUT DOWN NR 4 ENGINE AT 21:48 DUE TO LOSS OF OIL QUANTITY. WINDMILLING OIL PRESS, 2 TO 5 PSI. INSPECTED MAIN OIL FILT ER AND FOUND CONTAMINATED. PREPARED ENGINE FOR FERRY FLIGHT IAW GMM PAGE 6-3-1 TO 6-3-5, TO MIAMI FOR ENGINE CHANGE. 2 L 7 4 4F 4 F 4A25 1E8 1998120900001 19981209 00001 NM 1998 12 9 AALA984205 1 19981016 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 335AA 22333 AFW - FLOORBEAM AT STATION 287 HAS CORROSION REMOVAL ON UPPER SURFACE. REFER TO FIGURES 1, 2 AND 3, ALODINE ALL BARE AL UMINUM SURFACES, REFINISH THE BLENDED AREA WITH 2 COATS OF PRIMER, FILL BLENDS WITH PROSEAL 870. (M) 2 L 7 2 4F RT A1NM 1998121100037 19981211 00037 SO 1998 12 11 98ZZZX4480 1 19981106 A 3240 7096403 LINE PIPER PA42 PA42 7104202 SO COCKPIT LEAKING A TIMA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 175AA 6728 428001017 RIGHT BRAKE SOFT. FOUND THE STEEL BRAIDED LINE RUBBING ON STEEL HARD LINE AND WORE A HOLE IN STEEL LINE. SUBMITTER REC OMMENDED THE LINES UNDER INSTRUMENT PANEL BE CHECKED FOR CHAFING. 1 L 7 2 4T A23SO 1998121100044 19981211 00044 WP 1998 12 11 VJ9800637 1 19981102 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 220-237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING A SCHEDULED INSPECTION, THE FORWARD CABIN FLOORING SUPPORT STRUCTURE TEE CAP RUNNING DOWN THE CENTER LINE AT FS 2 37 WAS FOUND WITH CORROSION ON THE UPPER SURFACE AND AROUND FASTENER HOLES. REMOVED THE SUPPORT, FABRICATED AND INSTALL ED A NEW SUPPORT IAW DC9 SRM 51-10-3, 51-10-2, AND 51-10-4. 2 L 7 2 4F A6WE 1998121100045 19981211 00045 WP 1998 12 11 VJ9800638 1 19981104 A 5347 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 200 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING A SCHEDULE INSPECTION, THE RT O/B SEAT TRACK RBL 44 FS 200 WAS FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED SE CTION OF TRACK, FABRICATED AND INSTALLED REPAIR MEMBER IAW DC9 SRM 53-05 FIG 4F AND 51-10-3. 2 L 7 2 4F A6WE 1998121100046 19981211 00046 WP 1998 12 11 VJ9800639 1 19981110 A 5330 SKIN DOUG DC9 DC932 3022066 WP COCKPIT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING A SCHEDULED INSPECTION, THE COCKPIT FLOOR PANEL UNDER THE CO-PILOTS SEAT WAS FOUND CRACKED AND CORRODED AROUND TH E SCREW HOLES. REMOVED THE UPPER SKIN, FABRICATED AND INSTALLED A NEW SKIN IAW DC9 SRM 51-30-2 AND 53-21-0 FIG 2D. 2 L 7 2 4F A6WE 1998121100047 19981211 00047 NM 1998 12 11 CALA9802126 1 19981201 A 3230 273A14012 MANIFOLD BOEING 737 737724 NM NLG INOP A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 15710 28780 WHEN LANDING GEAR WAS EXTENDED THE NOSE GEAR DID NOT LOCK DOWN AND THE RED LIGHT ON FORWARD PANEL WAS ILLUMINATED. THE GEAR WAS CYCLED AND INDICATIONS WERE NORMAL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR LOC K VALVE MANIFOLD AT FAULT. THE NOSE GEAR LOCK VALVE MANIFOLD WAS REMOVED AND REPLACED IAW MM 32-33-01. LEAK AND OPERAT IONAL CHECKS WERE GOOD. 2 L 7 2 4F RT A16WE 1998121100048 19981211 00048 WP 1998 12 11 CALA9802127 1 19981201 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1136 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND TWO, 1 INCH CRACKS IN BELTFRAME AT STA 1136, LONGERON 6R. A NEW BELTFRAME SECTION WAS INSTALLED IAW SR M 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998121100049 19981211 00049 WP 1998 12 11 CALA9802128 1 19981201 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS232 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 THE JETWAY LEFT A GOUGE IN LT FUSELAGE SKIN AT STA 232, LONGERON 7L. REPAIRED IAW ECRA 5330-02742. 2 L 7 2 4F A6WE 1998121100050 19981211 00050 WP 1998 12 11 CALA9802129 1 19981202 A 5230 3913249502 FITTING DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO DOOR NR 1 HORIZONTAL BEAM FORWARD END FITTING. A NEW FITTING WAS INSTALLED IAW SRM 51-30-5. 2 L 7 2 4F A6WE 1998121100051 19981211 00051 WP 1998 12 11 CALA9802130 1 19981202 A 5210 BEAM DOUG DC9 DC982 3022082 WP PAX DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A .75 INCH CRACK IN MAIN CABIN DOOR NR 5 HORIZONTAL BEAM. A NEW NR 5 BEAM WAS INSTALLED IAW SRM 51-30- 2 AND 51-10-3. 2 L 7 2 4F A6WE 1998121100052 19981211 00052 WP 1998 12 11 CALA9802131 1 19981202 A 5350 CABLE DOUG DC9 DC982 3022082 WP TAIL CONE FRAYED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 10801 49127 THE TAIL CONE DID NOT COMPLETELY RELEASE FROM AIRCRAFT WHEN OPERATED FROM AFT VENTRAL DOOR. THE FRAYED CABLE WAS REPLAC ED AND RIGGED IAW MM 53-53-0. 2 L 7 2 4F A6WE 1998121100053 19981211 00053 NM 1998 12 11 CALA9802132 1 19981202 A 5321 FLOOR BOEING 727 727232 1384082 NM BS 1177-1171 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 45793 20647 INSPECTION FOUND CABIN FLOOR PAN CORRODED AT AFT ENTRY STA 1177 TO 1171, BL 0 TO LBL 18. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 53-10-2. 2 L 7 3 4F A3WE 1998121100054 19981211 00054 SO 1998 12 11 COMA9810273 1 19981127 A 5320 12022788003 WINDOW POST EMB 120 EMB120RT SO COCKPIT CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 FOUND CRACK ON POST BETWEEN PILOTS WINDSHIELD AND DV WINDOW. INSTALLED DOUBLER ON WINDOW POST IAW EMB EST-474/95 DATE 01NOV95. 2 L 7 2 4T RT A31SO 1998121100055 19981211 00055 SO 1998 12 11 COMA9810274 1 19981201 A 3260 922AA27AGP2722 SENSOR EMB 120 EMB120RT SO RT MLG MALFUNCTIONED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 247CA 120225 AFTER LANDING GEAR RETRACTED, RIGHT HAND MLG DOWN INDICATOR REMAINED ON. REPLACED DEFECTIVE DOWNLOCK PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1998121100056 19981211 00056 SO 1998 12 11 COMA9810275 1 19981128 A 2750 CONTROL EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 159A 120159 FLAP CONTROL FAULT DURING TAKEOFF. CANNOT DUPLICATE DISCREPANCY. C/W SERVICE BULLETIN 120-027-0067 FOR TROUBLESHOOTING . 2 L 7 2 4T RT A31SO 1998121100057 19981211 00057 EA 1998 12 11 COMA9860371 1 19981201 A 2752 853D10011 ACTUATOR CNDAIR CL600 CL6002B19 EA LT TE FLAP FAILED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 712CA 1125 7244 FLAPS FAILED AT 39 DEGREES. REPLACED LEFT HAND OUTBOARD FLAP ACTUATORS. 2 L 7 2 4F RT A21EA 1998121100058 19981211 00058 EA 1998 12 11 COMA9860372 1 19981202 A 3230 555405 VALVE CNDAIR CL600 CL6002B19 EA NLG FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 995CA 4 4 7229 NLG DOES NOT RETRACT. REPLACED THE NLG SELECTOR VALVE. 2 L 7 2 4F RT A21EA 1998121100059 19981211 00059 EA 1998 12 11 COMA9860373 1 19981202 A 3350 CONNECTOR CNDAIR CL600 CL6002B19 EA CABIN LOOSE A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946CA 7072 AFT SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. SECURED WIRING CONNECTOR BETWEEN LIGHT STRIPS. 2 L 7 2 4F RT A21EA 1998121100060 19981211 00060 NM 1998 12 11 QXEA9801762 1 19981130 A 2120 AIR DIST DHAV DHC8 DHC8202 2809007 NM CABIN SMOKE A QXEA K NONE B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 358PH 506 COLD BLACK SMOKE OR MIST CAME OUT OF THE FLOOR VENTS AT ROWS 2 AND 3 ON BOTH SIDES OF THE AIRCRAFT. MAINTENANCE INSPECT ED BELOW THE FLOOR PANELS IN THE SUSPECTED AREA AND FOUND NO DEFECTS. GROUND RAN ENGINES, WITH AIR CONDITIONING SYSTEM ON BOTH HOT AND COLD. NO DEFECTS NOTED. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998121100061 19981211 00061 NM 1998 12 11 QXEA9801763 1 19981109 A 3350 6104781 BATTERY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 362PH 11042 122 518 TWO RED EMERGENCY PATH FLOOR LIGHTS ARE INOP. MAINTENANCE REPLACED THE 3351 PS4 BATTERY PACK, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998121100062 19981211 00062 EU 1998 12 11 98FDEA00720 1 19981202 A 5610 WINDOW AIRBUS 300 A300F4605R 3930327 EU LT COCKPIT CRACKED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 664FE 768 CAPT L-1 WINDOW BEGAN ARCING PRIOR TO CRACKING SEVERELY ACROSS THE ENTIRE WINDOW. REMOVED AND REPLACED CAPT L-1 WIND AN D TEMP CONTROLLER, PER M/M REF 30-42-11-4, OPS CKD GOOD. 2 L 7 2 4F RT A35EU 1998121100063 19981211 00063 EU 1998 12 11 98FDEA00721 1 19981119 A 5270 CONTROL AIRBUS 300 A300F4605R 3930327 EU PAX DOOR MALFUNCTIONED A FDEA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 25 657FE 748 DURING CRUISE, ECAM 'RIGHT MAIN CABIN DOOR UNLOCKED'. DESCEND TO MEA OF 11,000 DIVERT TO ABQ. CABIN DOOR RT VISUALLY C KD CLOSED AND LOCKED. CATC CONTROL NR 44470, EXP 29NOV98, ASSIGN NEW CONTROL NR 44474, EXP 29NOV98. 2 L 7 2 4F RT A35EU 1998121100064 19981211 00064 WP 1998 12 11 ABXA9801120 1 19981114 A 5730 56434093 PLATE DOUG DOUG DC8 DC863 302198A WP LT WING CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING TRAILING EDGE SUPPORT STRUCTURE PLATE CRACKED, AFT OF NR 3 SPOILER ACTUATOR. REPAIRED IAW DC8 SRM 57-5-3 AND 57-2-0. 2 L 7 4 4F 4A25 1998121100065 19981211 00065 WP 1998 12 11 ABXA9801121 1 19981112 A 5313 37503421 LONGERON DOUG DOUG DC8 DC863 302198A WP BS 660 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 HEAVY CORROSION ON LONGERON 28R AT STATION 66O. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3750342. 2 L 7 4 4F 4A25 1998121100066 19981211 00066 WP 1998 12 11 ABXA9801122 1 19981109 A 5712 5769523 RIB DOUG DOUG DC8 DC863 302198A WP WS 520 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING LEADING EDGE RIB CRACKED AT STATION XS520.168. REPAIRED IAW DC8 51-1-21, 51-1-20D AND DWG 5769523. 2 L 7 4 4F 4A25 1998121100067 19981211 00067 WP 1998 12 11 ABXA9801123 1 19981111 A 5310 5612298 STRUCTURE DOUG DOUG DC8 DC863 302198A WP BS 50-60 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 COCKPIT SUBFLOOR STATION -60 TO -50, LBL 24-30, SHEARED RIVETS AND INTERNAL CORROSION. REPAIRED IAW ABX REA D853-24900 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998121100068 19981211 00068 WP 1998 12 11 ABXA9801124 1 19981111 A 5712 5769545 RIB DOUG DOUG DC8 DC863 302198A WP WS 520.168 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 RIGHT WING OUTBOARD STUB WING LEADING EDGE RIB CRACKED, 7 INCHES FORWARD OF FRONT SPAR AT STATION XS 520.168. REPAIRED IAW DC8 SRM. 2 L 7 4 4F 4A25 1998121100069 19981211 00069 WP 1998 12 11 ABXA9801125 1 19981110 A 5712 5769466 RIB DOUG DOUG DC8 DC863 302198A WP WS 610 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 RIGHT WING LEADING EDGE RIB AT STATION XFS 610 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056, DC8 SRM 51 -1-8 AND 51-1-20D. 2 L 7 4 4F 4A25 1998121100070 19981211 00070 WP 1998 12 11 ABXA9801126 1 19981110 A 5311 SR0853000861 FRAME DOUG DOUG DC8 DC863 302198A WP BS 1580 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 BELTFRAME CORRODED AT STATION 1580 BETWEEN LONGERON 36R AND 35R. REPAIRED IAW DC8 SRM 51-1-21 AND 53-2-0. 2 L 7 4 4F 4A25 1998121100071 19981211 00071 WP 1998 12 11 ABXA9801127 1 19981109 A 5320 3779874501 FITTING DOUG DOUG DC8 DC863 302198A WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 CRACKED INTERCOSTAL FITTING AT STATION 680 LONGERON 18L. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3179874. 2 L 7 4 4F 4A25 1998121100072 19981211 00072 WP 1998 12 11 ABXA9801128 1 19981102 A 5712 431092 RIB DOUG DOUG DC8 DC863 302198A WP WS 772.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING LEADING EDGE RIB CRACKED STATION SFX 772.500. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998121100073 19981211 00073 WP 1998 12 11 ABXA9801129 1 19981104 A 5320 3750257503N FITTING DOUG DOUG DC8 DC863 302198A WP BS 200-220 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LONGERON 31L SPLICE CRACKED STATION 200 TO 220. REPLACED SPLICE IAW DC8 SRM 53-1-0 AND 51-1-20D. 2 L 7 4 4F 4A25 1998121100074 19981211 00074 WP 1998 12 11 ABXA9801130 1 19981031 A 5320 47516402 FITTING DOUG DOUG DC8 DC863 302198A WP BS 822 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 863AX 46122 CRACKED INTERCOSTAL FITTING AT STATION 822, LONGERON 18A. REPAIRED IAW DWG 4751640 AND DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998121100075 19981211 00075 WP 1998 12 11 ABXA9801131 1 19981109 A 5320 37558451N FITTING DOUG DOUG DC8 DC863 302198A WP BS 1180 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 BATH TUB FITTING AT STATION 1180 BETWEEN LONGERON 35R AND 36R CORRODED. REPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998121100076 19981211 00076 WP 1998 12 11 ABXA9801132 1 19981109 A 5312 5750837 BULKHEAD BRACKET DOUG DOUG DC8 DC863 302198A WP BS 640 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 STATION 640 BULKHEAD TO FUSELAGE ATTACH BRACKET CRACKED BETWEEN LONGERON -26L AND -27L FORWARD ACCESSORY COMPARTMENT. R EPAIRED IAW DC8 SRM 53-2-0. 2 L 7 4 4F 4A25 1998121100077 19981211 00077 WP 1998 12 11 ABXA9801133 1 19981023 A 5320 37544731N SPLICE DOUG DOUG DC8 DC863 302198A WP BS 380-400 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LONGERON 31L SPLICE CRACKED BETWEEN STATION 400 AND 380. REPAIRED IAW DC8 SRM 51-1-20D. 2 L 7 4 4F 4A25 1998121100078 19981211 00078 WP 1998 12 11 ABXA9801134 1 19981108 A 5400 5754701 DOUBLER DOUG DOUG DC8 DC863 302198A WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING NR 1 PYLON STUB WING LOWER SURFACE REPAIR DOUBLER CRACKED BETWEEN 2 RIVETS. REPAIRED IAW DC8 SRM 51-1-26. 2 L 7 4 4F 4A25 1998121100079 19981211 00079 WP 1998 12 11 ABXA9801156 1 19981202 A 3350 41B004AD07G3 BATTERY DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 965AX 47498 EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1998121100080 19981211 00080 WP 1998 12 11 MWEA981116 1 19981201 A 3220 LANDING GEAR DOUG DC9 DC915 3022036 WP NLG BIRD STRIKE A MWEA A UNSCHED LANDING C F.O.D. TO TAKEOFF 1 GL 31 300ME 45718 PILOT REPORTED BIRD STRIKE DURING TAKEOFF POSSIBLE IN NOSE GEAR AREA. RETURNED TO RDU PERFORMED BIRD STRIKE INSPECTION IAW DC9MM 05-56-0. NO DAMAGE NOTED. 2 L 7 2 4F A6WE 1998121100081 19981211 00081 NM 1998 12 11 SCNA98143 1 19981201 A 3350 BULB BOEING 727 727225 1384077 NM ROW 20D FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY TRACK LIGHTING WAS FOUND TO HAVE ONE LIGHT OUT AT SEAT 20D. REPLACED EME RGENCY TRACK LIGHTING BULB AND LENS AT SEAT 20D, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998121100082 19981211 00082 SO 1998 12 11 SWIA971318 1 19981115 A 5230 SEAL EMB 120 EMB120RT SO PWA 118 PW118A NE CARGO DOOR FAILED A SWIA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 NM 07 289YV 120289 AT FLIGHT 200 LOST CABIN PRESSURE. NO CHANGE IN MANUAL MODE. PERFORMED RAPID DESCENT TO 8000 FEET TO CONTROL PRESSURE. REINSTALLED TOP SECTION OF CARGO DOOR SEAL, CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121100083 19981211 00083 SO 1998 12 11 SWIA971319 1 19981119 A 3231 VALVE EMB 120 EMB120RT SO PWA 118 PW118 NE LT MLG DOOR MALFUNCTIONED A SWIA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 NM 07 129AM 120119 AFTER GEAR RETRACTION, LEFT RED LIGHTS REMAINED ON. FELT VIBRATION COMING FROM LEFT MAIN GEAR. AFTER GEAR WAS SELECTED DOWN ALL INDICATIONS WERE NORMAL. RETURNED TO FIELD. REPLACED LEFT OUTBOARD DOOR SEQUENCE VALVE. OPS CHECKS IAW MM 3 2. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121100084 19981211 00084 SO 1998 12 11 SWIA971320 1 19981125 A 3020 BOOT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE LT ENG INLET FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 292UX 120292 LEFT ENGINE AIR INLET BOOT FAILED IN FLIGHT. RETURNED TO SEA. INSTALLED UNIVERSAL INLET IAW MM 30-20-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121100085 19981211 00085 SO 1998 12 11 SWIA971321 1 19981125 A 2910 LINE EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG DOOR FAILED A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 1117H 120117 UPON FLAP RETRACTION AFTER TAKEOFF, LOST ALL GREEN SYSTEM HYDRAULICS. PERFORMED QRH PROCEDURES FOLLOWING LOSS OF GREEN SYSTEM HYDRAULICS. RETURNED TO GATE. REMOVED AND REPLACED RIGHT FORWARD INBOARD GEAR DOOR HYDRAULIC HOSE, IAW MM 12-00 -00. OPS CHECKS GOOD. SERVICED GREEN HYDRAULIC SYSTEM IAW MM 12-13-01. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121100086 19981211 00086 NE 1998 12 11 SWIA971322 2 19981125 A 7261 OIL SYST EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE RT ENGINE REQD SERVICE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 292UX 120292 ON DEPARTURE, RIGHT OIL PRESSURE FLUCTUATED BETWEEN 50 AND 35 PSI CAUSING AN AURAL WARNING AND LIGHT. RETURNED TO FIELD . CREW SERVICED OIL. GROUND RAN ENGINE AT 100 PERCENT AND CRUISE POWER. ALL OIL SYSTEM INDICATION CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121100087 19981211 00087 EA 1998 12 11 SWIA971323 1 19981127 A 3010 SWITCH CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT WING ANTI-ICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 409SW 7056 WITH WING ANTI-ICE SELECTED ON ANTI-ICE DUCT MESSAGE CAME ON SHOWING LEFT WING RED, SAME IN BOTH NORMAL, STANDBY MODES. RETURNED TO SLC. REPLACED 3 THERMAL SWITCHES IN LEFT WING MID SECTION AND HEAT SHRINK INSTALLED ON LEFT WIRE ENDS. RA N AIRCRAFT AND TAXIED FOR 20 MINUTES. NO DISCREPANCIES NOTED. OPS CHECKS GOOD IN STANDBY AND ON POSITIONS. 2 L 7 2 4F 4 F RT A21EA E15NE 1998121100089 19981211 00089 NE 1998 12 11 SWIA971325 2 19981129 A 7200 ENGINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FAILED A SWIA A UNSCHED LANDING E J B VIBRATION/BUFFET WARNING INDICATION SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 07 406SW 7030 DURING TAKEOFF, LEFT ENGINE ITT WAS IN YELLOW RANGE. DURING CLIMB ITT HAD A 877 FT RED EXCURSION FOR ABOUT 2 SEC. ICIN G CONDITIONS WERE ENCOUNTERED AND ITT WENT RED 888 FT WITH N21 PERCENT HIGHER THAN RIGHT, FUEL FLOWS 90 LBS HIGHER. ABO UT 3 TO 4 SECONDS, LEFT ENGINE ROLLED VIBRATED AND ROLLED BACK WITH SMOKE IN THE CABIN. SEVERE DAMAGE, QRH PERFORMED. C /W ENGINE CHANGE PER RII 71-401. 2 L 7 2 4F 4 F RT A21EA E15NE 1998121100090 19981211 00090 1998 12 11 P5CA9801613 4 19981126 A 3442 MI592087 ANTENNA BOEING 747 747122 1384872 NM WEATHER RADAR MALFUNCTION A P5CA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 23 851FT 19756 RADAR SYSTEM TILT APPEARS TO POINT FULL DOWN IN SYSTEMS 1 AND 2, TESTS OK. AIRCRAFT RETURNED TO JFK. REMOVED AND REPLA CED WEATHER RADAR ANTENNA REF MM 34-43-03. OPERATIONS CHECK OK. REPLACED NR 1 R/T REF MM 34-43-02. OPS CHECK NORMAL. 2 L 7 4 4F A20WE 1998121100091 19981211 00091 WP 1998 12 11 CKSA98711 1 19981112 A 2130 FILTER DOUG DC8 DC862 3021970 WP FWD FUSELAGE DIRTY A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 818CK 45961 NASI SYSTEM PRODUCES BURNT ODOR IN CRUISE FLIGHT WITH BLEEDS IN LOW BOTH NASI'S ON. CLEANED NASI SYSTEM FILTERS AS PER DC-8 MM NASI MM 21-00-0. OPS CHECK GOOD ON GROUND. 2 L 7 4 4F 4A25 1998121100092 19981211 00092 NM 1998 12 11 SWAA983052 1 19981130 A 3350 BULB BOEING 737 7373H4 1384600 NM SERVICE DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED BC2 CHECK, FOUND 2 BURNED OUT BULBS AT EMERGENCY EXIT LIGHT AT FWD SERV DOOR. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121100093 19981211 00093 NM 1998 12 11 SWAA983053 1 19981201 A 5240 STRAP BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 386SW 26601 AFTER TAKEOFF LOUD BANGING NOISE HEARD BY CABIN CREW IN FWD SERVICE DOOR AREA. NOISE GOT LOUDER WITH INCREASED AIRSPEED . AIRCRAFT RETURNED TO PDX AND FOUND FWD SERVICE DOOR STRAP OUTSIDE A/C THROUGH HINGE. FOUND SIX INCHES OF SAFETY STRA P PROTRUDING FROM LOWER HINGE. NO DAMAGE NOTED AND SEAL OK. STOWED STRAP. 2 L 7 2 4F RT A16WE 1998121100094 19981211 00094 NM 1998 12 11 SWAA983054 1 19981201 A 5330 SKIN BOEING 737 7373G7 1384595 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 690SW 23783 DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD RT RADIUS OF AC GROUND CONNECTION CUTOUT. REPAIRED PER BO EING SRM. 2 L 7 2 4F RT A16WE 1998121100095 19981211 00095 NM 1998 12 11 SWAA983055 1 19981201 A 5312 BULKHEAD CHORD BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 677AA 23289 DURING SCHEDULED 1/2D CHECK, FOUND SIDE CHORD CRACKED AT BS 178 BULKHEAD, RBL 29. REPLACED CHORD PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121100096 19981211 00096 NM 1998 12 11 SWAA983056 1 19981201 A 3350 LAMP BOEING 737 7373H4 1384600 NM ROW 23 FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 344SW 24152 DURING SCHEDULED SC CHECK, FOUND A WHITE EMERGENCY FLOOR TRACK LIGHT INOP AT ROW 23DEF. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121100097 19981211 00097 NM 1998 12 11 SWAA983057 1 19981201 A 3350 LAMP BOEING 737 7373H4 1384600 NM SERVICE DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED BC2 CHECK, FOUND EMERGENCY EXIT LIGHT AT FWD SERVICE DOOR INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121100098 19981211 00098 CE 1998 12 11 98ZZZX4487 1 19981030 A 3230 S1232515 CIRCUIT BREAKER CESSNA 402 402B 207590P CE COCKPIT FAILED A FSEA O OTHER J WARNING INDICATION CL CLIMB 1 NE 05 567JS 402B1090 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT COME UP. REPLACED LANDING GEARA BREAKER, P/N S1235-515. OPS CHECK GOOD. 1 L 7 2 3O A7CE 1998121100111 19981211 00111 NE 1998 12 11 98ZZZX4501 2 19981111 A 8530 116731CP CYLINDER DOUG DC3 DC3C 3021457 WP PWA R1830 R183090D 52020 NE ENGINE FAILED A VLLA O OTHER O OTHER CL CLIMB 1 GL 05 36AP 11299 12 12807X 13439 BP432569 AFTER TAKEOFF ON CLIMB, LEFT ENGINE STARTED TO SHAKE. FOUND NR 14 CYLINDER WITH BROKEN EXHAUST VALVE. 2 L 7 2 4R 4 R A669 5E4 1998121100112 19981211 00112 SO 1998 12 11 98ZZZX4502 1 19981110 A 2140 A23D0475 REGULATOR JANITROL B4500 PIPER PA31 PA31350 7103110 SO HEATER PRESSURE LEAKING A FFSA K NONE K FLUID LOSS IN INSP/MAINT 1 AL 01 4112K 37 A98010072 318353006 FUEL LEAK ON INLET SIDE OF REGULATOR BODY. SUBMITTER STATED THIS WAS ONE OF THREE REGULATORS INSTALLED IN A TWO-WEEK PE RIOD THAT FAILED. MFG DATE 7-98. REMOVED 11-10-98. 1 L 7 2 3O A20SO 1998121100120 19981211 00120 CE 1998 12 11 98ZZZX4510 1 19981007 A 3230 583800901 MOTOR BEECH 58 58 1152740 CE MLG FAILED A BSYA O OTHER O OTHER AP APPROACH 1 GL 07 36673 TH1143 AIRCRAFT GOING INTO JACKSON (JAN) LANDING GEAR WOULD NOT COME DOWN. HAND CRANKED GEAR TO DOWN AND LOCK, LANDED, NO PROB LEMS. FOUND GEAR MOTOR INOPERATIVE, REMOVED AND REPLACED GEAR MOTOR. OPS CHECKED GOOD. 1 L 7 2 3O 3A16 1998121100127 19981211 00127 EA 1998 12 11 98ZZZX4517 2 19980910 A 8500 ENGINE PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA LEFT MALFUNCTIONED A WVBA O OTHER O OTHER AP APPROACH 1 AL 01 300ED 5350 1195 317852008 L789861A IN PREPARATION FOR LANDING, PILOT NOTICED LEFT ENGINE'S RPMS LAGGING THE RIGHT ENGINE. WITH ANY POWER REDUCTIONS, THE L EFT ENGINE'S RPMS LAGGED EVEN FURTHER. THERE WAS NO RESPONSE WHEN THE PROPELLER CONTROL LEVER WAS MOVED TO THE FULL FOR WARD POSITION (INCREASE RPM, DECREASE PITCH). ON FINAL APPROACH WHEN THE LEFT ENGINE THROTTLE WAS MOVED TO IDLE, PROPEL LER'S BLADES WENT TO THE FULL FEATHERED POSITION. SUBMITTER STATED CAUSE UNDETERMINED AT THIS TIME. 1 L 7 2 3O 3 O A20SO E14EA 1998121100140 19981211 00140 CE 1998 12 11 98ZZZX4530 1 19981101 A 5210 STCSA4184WE COMPRESSOR BEECH 58 58 1152740 CE DOOR SEAL MALFUNCTIONED A P A ZWSA K NONE O OTHER IN INSP/MAINT 1 GL 13 17979 TH832 INFLATABLE DOOR SEAL SYSTEM SQUAWKED AS INOPERABLE. REPLACED FUSE, STILL INOPERABLE. INVESTIGATION REVEALED SYSTEM RES ISTORS WERE GENERATING ENOUGH HEAT TO SCORCH AIRCRAFT INSULATION. WIRES LEADING TO AND FROM RESISTORS SHOW SIGNS OF HEA T DAMAGE, WIRE DEFORMED AND INSULATION MELTED. SUBMITTER STATED SYSTEM COMPRESSOR CASE DEFORMED SLIGHTLY, POSSIBLE BECA USE OF HEAT. 1 L 7 2 3O 3A16 1998121100152 19981211 00152 NM 1998 12 11 TWAA9818902 1 19981122 A 3350 58225 BATTERY PACK BOEING 727 727231 1384079 NM EMER EXIT DOOR DISCHARGED A TWAA K NONE L NO TEST CR CRUISE 1 CE 05 54354 21986 DURING CRUISE, THE ESCAPE PATH LIGHTS IN THE CENTER OF THE CABIN FLICKER ON-OFF. REPLACED BOTH BATTERY PACKS ABOVE THE EMERGENCY ESCAPE DOORS. 2 L 7 3 4F A3WE 1998121100153 19981211 00153 WP 1998 12 11 TWAA9819201 1 19981201 A 3340 8906K1269 SWITCH DOUG DC9 DC951 3022051 WP TAXI LIGHT LOOSE A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 409EA 47728 SPARKS CAME OUT OF THE NOSE TAXI LIGHT SWITCH. TURNED OFF SWITCH. CIRCUIT BREAKER POPPED. SYSTEM WAS PLACARDED INOPER ATIVE PER MEL. MAINTENANCE LATER TIGHTENED THE SWITCH. CHECK-C 9-16-98 MCI. 2 L 7 2 4F RT A6WE 1998121100154 19981211 00154 NM 1998 12 11 TWAA9819202 1 19981203 A 3350 BATTERY PACK BOEING 727 727231 1384079 NM OVERWING EXIT LOOSE A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 64346 21633 FOUND BOTH AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. RESEATED BOTH BATTERY PACKS. CHECK-C 9-11-98 MCI. 2 L 7 3 4F A3WE 1998121100155 19981211 00155 EU 1998 12 11 MALA976254 1 19981201 A 2622 BA510156SR3 FIRE BOTTLE SAAB SF340 SF340A 7850100 EU GALLEY DISCHARGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 76XJ 076 DURING INSPECTION CREW NOTED GALLEY FIRE EXTINGUISHER DISCHARGED. MAINTENANCE REPLACED FIRE EXTINGUISHER. 2 L 7 2 4T RT A52EU 1998121100156 19981211 00156 1998 12 11 MALA976255 4 19981202 A 3442 20412220435 RADAR BAC 146 AVRO146RJ85A 1500097 EU COCKPIT INOP A MALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 514XJ E2330 DURING PUSHBACK SMOKE CAME FROM CENTER PANEL AND RADAR BECAME INOPERATIVE. RETURNED TO GATE. MAINTENANCE REPLACED WEAT HER RADAR INDICATOR. OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1998121100157 19981211 00157 EU 1998 12 11 MALA976256 1 19981128 A 2150 4325C000002 TEMP CONTROL BAC 146 AVRO146RJ85A 1500097 EU FLIGHT DECK MALFUNCTIONED A MALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 15 508XJ E2317 ON TAXI OUT, REAR BAY HI TEMP WARNING LIGHT, LIGHT WENT OUT WHEN PACKS WERE SHUT OFF. RETURNED TO GATE. MAINTENANCE RE PLACED FLIGHT DECK TEMP CONTROL BOX. ITEM REMAINS DEFERRED. 2 H 7 4 4F RT A49EU 1998121100158 19981211 00158 WP 1998 12 11 CALA9802133 1 19981203 A 3350 60030431 POWER SUPPLY DOUG DC9 DC982 3022082 WP EMER EXIT INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13891 49102 INSPECTION FOUND THE LT AND RT INTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND RE PLACED. 2 L 7 2 4F A6WE 1998121100159 19981211 00159 NM 1998 12 11 CALA9802134 1 19981203 A 5230 FRAME BOEING 737 7373T0 1384582 NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 77303 23354 INSPECTION FOUND A 9 INCH CRACK IN FORWARD CARGO DOOR FRAME UNDER AFT LOCK ROLLER. THE DOOR FRAME WAS REMOVED AND REPLA CED IAW SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F RT A16WE 1998121100160 19981211 00160 WP 1998 12 11 CALA9802135 1 19981203 A 5311 BELTFRAME DOUG DC9 DC982 3022082 WP BS 1446 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND 1 INCH CRACKS BETWEEN ATTACH BOLTS IN BELTFRAME STA 1446 AT LONGERONS 2L, 3L, 4L, 2R, 3R, 4R, AND 5R. T HE BELTFRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998121100161 19981211 00161 WP 1998 12 11 9810559751 1 19981201 A 2150 ACM DOUG DC9 DC941 302207N WP TAIL SECTION INOPERATIVE A NWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 GL 01 751NW 47115 DURING CLIMB-OUT, THE FLIGHT CREW REPORTED AN AERIAL TYPE SMELL COMING FROM THE GALLEY AREA. FLIGHT CREW PERFORMED ON A IR CONDITIONING SMOKE PROCEDURE, DECLARED A YELLOW EMERGENCY, DIVERTED FLIGHT TO RST, AND LANDED WITHOUT INCIDENT. MAIN TENANCE PERFORMED AN EXTENSIVE INSPECTION OF THE AIRCRAFT AND REPLACED THE LEFT AIR CYCLE MACHINE AND COALESCER BAG. OP ERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121100162 19981211 00162 EU 1998 12 11 QXEA9801764 1 19981201 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 487US 11238 GEG - FORWARD EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED FAULTY CANNON PLUG, OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998121100163 19981211 00163 EU 1998 12 11 QXEA9801765 1 19981201 A 3397 WIRE FOKKER F28 F28MK4000 4990810 EU SEAT 5 SHORTED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 494US 11167 SEA - SEVERAL EMERGENCY EXIT LIGHTS ARE OUT. MAINTENANCE REPAIRED SHORTED WIRE AT SEAT 5, OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998121100164 19981211 00164 NM 1998 12 11 98FDEA00722 1 19981202 A 3230 LINE BOEING 727 727233 138408A NM MLG FAILED A FDEA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 284FE 22621 98-290 - RETRACT HAS 'A' SYS HYD QTY LOSS ACCOMPLISH BY ENG 1 AND 2, PUMP LOW PRESS LIGHT. RT MAIN GEAR FAIL TO RETRACT . REMOVED AND REPLACED RETURN LINE FROM RT GEAR ACT CK 'A' SYS HYD MOTOR CLOSE DRAIN FILTER FOR NR 1 AND NR 2 SYS PUMP. NO METAL FND. SYS OPS AND LEAK CK OK MM 29-11-00. 2 L 7 3 4F RT A3WE 1998121100165 19981211 00165 NM 1998 12 11 98FDEA00723 1 19981203 A 3150 512776 AURAL WARNING BOEING 727 72722 1384002 NM COCKPIT SOUNDED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 149FE 19087 98-291 FIRE WARN BELL SOUND AT ROTATION. NO LIGHTS. SYS AFT LAND WAS NORM. BELL SOUND UNTIL BELL CUTOUT SWITCH WAS PU SH. INSPECTION APU ENG AND CARGO. ALL OK TEST APU, ENGINES AND CARGO SMOKE SYS. REMOVED AND REPLACED AURAL WARNING BO X PER MM. FIRE SYS TEST OK. 2 L 7 3 4F A3WE 1998121100166 19981211 00166 WP 1998 12 11 ABXA9801157 1 19981104 A 5521 5910411515 SPAR DOUG DOUG DC9 DC941 302207N WP LT ELEVATOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 979AX 47492 LEFT ELEVATOR SPAR CRACKED IN 4 PLACES. REPAIRED UNIT IAW DC9 SRM. 2 L 7 2 4F A6WE 1998121100167 19981211 00167 WP 1998 12 11 ABXA9801158 1 19981029 A 5280 5910161118 SKIN DOUG DOUG DC9 DC932 3022066 WP RT MLG DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 985AX 47522 RIGHT MAIN LANDING GEAR DOOR HAD 2 CRACK ON LOWER SKIN SURFACE. REPAIRED UNIT IAW DC9 SRM. 2 L 7 2 4F A6WE 1998121100168 19981211 00168 NM 1998 12 11 VNAA9812003 1 19981202 A 3251 2318000002 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NLG STEERING FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 432JS 88393 3045 THE AIRCRAFT RETURNED TO THE GATE AFTER RECEIVING A NOSE STEERING FAIL WARNING INDICATION. MAINTENANCE INSPECTED AND RE PLACED THE NOSE STEERING CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-51-06. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998121100169 19981211 00169 WP 1998 12 11 TWAA9819301 1 19981204 A 2530 4110001143 COFFEEMAKER DOUG DC9 DC982 3022082 WP NR 3 GALLEY FAILED A TWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CE 05 914TW 49185 THE NUMBER 3 GALLEY COFFEEMAKER CAUSED SPARKS. CREW PULLED CIRCUIT BREAKER. MAINT REPLACED THE COFFEEMAKER. CHECK-C 2 -28-98 MCI. 2 L 7 2 4F A6WE 1998121100170 19981211 00170 NM 1998 12 11 TWAA9819302 1 19981204 A 3350 BATTERY PACK BOEING 767 7673Q8 NM ROW 28-40 DISCHARGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 635TW 28207 FOUND CABIN EGRESS EMERGENCY LIGHTS INOPERATIVE ON LEFT SIDE OF AIRCRAFT, ROWS 28 THROUGH 40. REPLACED BATTERY CHARGER, 2012-1, AND BATTERY PACK, 2013-1A. CHECK-C 10-07-98 LAX. 2 L 7 2 4F RT A1NM 1998121100171 19981211 00171 NM 1998 12 11 TWAA9819303 1 19981204 A 3230 1U1085 VALVE BOEING 727 727231 1384079 NM LANDING GEAR CRACKED A TWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 05 54352 21984 AFTER TAKEOFF, UPON GEAR RETRACTION, THE A HYDRAULIC SYSTEM PRESSURE AND QUANTITY DROPPED. RETURNED TO STL. REPLACED T HE RT LANDING GEAR HYDRAULIC SEQUENCE VALVE. CHECK-C 3-19-98 MCI. 2 L 7 3 4F A3WE 1998121100172 19981211 00172 WP 1998 12 11 TWAA9819304 1 19981206 A 3350 60030451LB BATTERY PACK DOUG DC9 DC941 302207N WP L1 DOOR DIRTY A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 933L 47617 EMERGENCY LIGHTS AT THE L1 CABIN DOOR STAYED ON WHEN POWER WAS REMOVED DURING LAYOVER. CLEANED AND SECURED CONNECTOR TO BATTERY PACK. CHECK-C 2-16-98 STL. 2 L 7 2 4F A6WE 1998121100173 19981211 00173 WP 1998 12 11 CALA9802136 1 19981204 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 180-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND FUSELAGE SKIN CORRODED AROUND MARKER BEACON ANTENNA AREA AT STA 180 TO 200. A DOUBLER WAS INSTALLED IA W ECRA 5330-02745. 2 L 7 2 4F A6WE 1998121100174 19981211 00174 WP 1998 12 11 CALA9802137 1 19981206 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1289 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND A 2 INCH CRACK ON FLOORBEAM STA 1289, AT NR 3 DOOR LOWER JAMB. THE CRACKED AREA OF FLOORBEAM WAS TRIMM ED OUT, A REPAIR WAS PERFORMED IAW ENGINEERING ORDER D10-53-86781 AND ECRA 5314-01003. 2 L 7 3 4F A22WE 1998121100175 19981211 00175 WP 1998 12 11 CALA9802138 1 19981206 A 5712 RIB DOUG DC10 DC1010 3022110 WP WS 455-506 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND A 1 INCH CRACK ON RIB OF FIXED LEADING EDGE RT WING BETWEEN STA XORS 455 AND 506. THE CRACKED AREA OF RIB WAS TRIMMED. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4 AND 51-31-01. 2 L 7 3 4F A22WE 1998121100176 19981211 00176 WP 1998 12 11 CALA9802139 1 19981206 A 5712 RIB DOUG DC10 DC1010 3022110 WP RT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND A 1 INCH CRACK ON RIB OF RT WING FIXED LEADING EDGE JUST IN FRONT OF L/E DEVICE NR 5. THE CRACKED AREA OF RIB WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH A DOUBLER IAW SRM 57-00-01, FIGURE 4, 51-21-01, AND 51-33-01. 2 L 7 3 4F A22WE 1998121100177 19981211 00177 WP 1998 12 11 CALA9802140 1 19981206 A 5350 FRAME DOUG DC10 DC1010 3022110 WP TAIL CONE CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND A 2 INCH CRACK IN TAIL CONE FRAME UNDER ACTUATOR LINK AREA. THE CRACKED AREA WAS TRIMMED OUT. THE ARE A WAS REINFORCED WITH FRAME AND SPLICE IAW SRM 53-30-00, FIGURE 3, 51-31-01 AND 51-21-01. 2 L 7 3 4F A22WE 1998121100178 19981211 00178 WP 1998 12 11 CALA9802141 1 19981206 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 791 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND GALLEY FLOOR SUPPORT CORRODED AT STA 791, RBL 50 TO 70. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998121100179 19981211 00179 WP 1998 12 11 CALA9802142 1 19981206 A 5311 FRAME DOUG DC9 DC982 3022082 WP BS 1463 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND A 6 INCH CRACK IN CANTED FRAME WEB AT STA 1463. THE CRACKED AREA WAS REMOVED AND A WEB AND SPLICE REPA IR WAS INSTALLED IAW SRM 53-01, FIGURE 2. 2 L 7 2 4F A6WE 1998121100180 19981211 00180 NM 1998 12 11 UPS98228276 1 19981205 A 3350 LIGHT BOEING 727 72725C 138400H NM RT WING INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, RT WING CENTER OVERWING ILLUMINATION EMERGENCY LIGHT IS NOT WORKING. REMOVED AND REPLACED THE CENT ER RIGHT HAND OVERWING EXTERNAL RECEIVER AND PLATE ASSY IAW BMM 33-50-101, OPS CK GOOD. 2 L 7 3 4F A3WE 1998121100181 19981211 00181 NM 1998 12 11 UPS98228277 1 19981205 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 946UP 19721 INSPECTION TYPE-N/A, AFT CABIN EMER LIGHT EXIT MARKER INOP. REMOVED AND REPLACED THE AFT CABIN EXIT MARKER BATTERY PACK IAW BMM 33-50-81, OPS CK GOOD. 2 L 7 3 4F A3WE 1998121100182 19981211 00182 NM 1998 12 11 UPS98428275 1 19981204 A 3310 CARD BOEING 747 747123 1384873 NM JT9D COCKPIT FAILED A IPXA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 01 675UP 20390 INSPECTION TYPE-N/A, BLOCK TURNBACK DUE TO BURNING ODOR IN COCKPIT. FOUND A16 CARD IN MASTER DIM AND TEST ELECTRONIC CA RD FILE FAULTED CAUSING ODOR IN FLIGHT COMPARTMENT. 2 L 7 4 4F A20WE 1998121100183 19981211 00183 NM 1998 12 11 UPS98628274 1 19981202 A 3350 BULB BOEING 767 76734AF 1385212 NM CABIN FAILED A IPXA K NONE L NO TEST UK UNKNOWN 1 SO 01 301UP 27239 INSPECTION TYPE-N/A, EMERGENCY EXIT UNARMED LIGHT HAS ONE BULB BURNED OUT. RELAMPED EMERGENCY EXIT LIGHT, OPS CHECK GOO D. 2 L 7 2 4F RT A1NM 1998121100184 19981211 00184 NM 1998 12 11 QXEA9801783 1 19981201 A 5210 MECHANISM DHAV DHC8 DHC8202 2809007 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 359PH 514 MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE LUBRICATED THE MAIN CABIN DOOR STAYS, OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998121100185 19981211 00185 NM 1998 12 11 QXEA9801784 1 19981128 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 825PH 512 MAIN CABIN DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBRICATED MAIN CABIN DOOR STOPS AND LINKAGE, OPERATIONAL CH ECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998121100186 19981211 00186 NM 1998 12 11 98FDEA00724 1 19981204 A 2750 MS9391130ZE4C DRIVE UNIT BOEING 727 727277 138408S NM LT TE FLAP FAILED A FDEA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 25 244FE 21647 TOTAL LOSS OF A SYS QUANT ON SHORT FINAL. REPLACED CASE DRAIN FILTERS PER MM 29-11-041, I/B FLAP DRIVE UNIT HYD MTR PER MM 27-51-062-4, A SYS HYD PRESS FILTER PER MM 29-11-062-3. ENGINE DRIVEN HYD PUMPS OPER NORM. 2 L 7 3 4F RT A3WE 1998121100187 19981211 00187 NM 1998 12 11 98FDEA00725 1 19981205 A 2910 SWITCH BOEING 727 727227 1384078 NM B HYD SYST MISWIRED A FDEA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 25 496FE 21670 98-293 AT FLT LVL 330 HAD KW SPIKE TO 40 KW ON ALL 3 GEN. AUTOPILOT DISCONN AND CAPT ADC FAILED MOMENTARILY. COCKPIT LIGHT DIMMED DURING FLUXES. REWIRED B SYS HYD SWITCH. RAN MOTOR WITH LOAD APLIED. GEN IND NORM. 2 L 7 3 4F A3WE 1998121100188 19981211 00188 1998 12 11 98FDEA00726 2 19981205 A 7261 PUMP BOEING 727 72722C 138400F NM NR 2 ENGINE FAILED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 107FE 19202 DURING CLIMBOUT, NR 2 LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON. OIL PRESS DROPPED TO ZERO, TEMP WAS OK. SHUTDOWN ENG PER RED TABS WITHIN 4 TO 5 MIN. *S/D* REMOVED AND REPLACED NR 2 ENG OIL PUMP. 2 L 7 3 4F A3WE 1998121100189 19981211 00189 NM 1998 12 11 98FDEA00727 1 19981204 A 5313 6554574107 STRINGER BOEING 727 7272S2F 1384O81 NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 217FE 22938 NR 206 CORROSION (C53-224-01) ON STR CLIP AND STR, BS 720D, STR 5 RT. *S/D* REMOVED CORRODED SECTION OF STR NR 5 RT FR OM BS 720C+10 TO 720D+8 IAW FEDEX SRM 53-10-3. REPLACED STR 5 R, BS 720C+10 TO 220D+8 PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1998121100190 19981211 00190 WP 1998 12 11 ABXA9801159 1 19981203 A 3260 7000010101 SWITCH DOUG DC9 DC931 3022065 WP LT MLG MALFUNCTION A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 947AX 47004 GEAR UPLATCH CHECK NOT SATISFACTORY, THE LEFT MAIN GEAR INDICATION REMAINED GREEN. RECYCLED GEAR DOWN, ALL 3 GEAR HAD N O UNSAFE LIGHT. RAISED GEAR, LEFT GEAR GREEN LIGHT STAYED ON, NO GEAR DOOR OPEN LIGHT. REPLACED LEFT MAIN GEAR DOWNLOC K SWITCH, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998121100191 19981211 00191 WP 1998 12 11 MWEA981117 1 19981202 A 5320 59174637 JAMB DOUG DC9 DC932 3022066 WP VENTRAL STAIR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACK IN VENTRAL STAIR DOOR JAMB RADIUS ON RIGHT SIDE JUST ABOVE TOP DOOR STRIKER PLATE. MTC INSTALLED SPLICE SEC TION OF DOOR JAMB. 2 L 7 2 4F A6WE 1998121100192 19981211 00192 WP 1998 12 11 MWEA981118 1 19981203 A 3350 60030931 BATTERY PACK DOUG DC9 DC932 3022066 WP COCKPIT DISCHARGED A MWEA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 215ME 47744 COCKPIT PEANUT LIGHTS FOR THE EVACUATION LIGHTS WILL NOT GO OUT WITH ALL SWITCHES AFT. MTC REPLACED THE EMERGENCY CEILI NG BATTERY PACK. 2 L 7 2 4F A6WE 1998121100193 19981211 00193 WP 1998 12 11 MWEA981119 1 19981202 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACKED LONGERON 16R AND 17R AT STATION 965. MTC FABRICATED AND INSTALLED LONGERON SECTION. 2 L 7 2 4F A6WE 1998121100194 19981211 00194 WP 1998 12 11 MWEA981120 1 19981202 A 5315 995823822 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 981 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND LIGHT CORROSION ON FLOORBEAM UNDER RIGHT LAV AT STATION 981. MTC REMOVED CORROSION FABRICATED AND INSTALLED REPAI R ANGLE. 2 L 7 2 4F A6WE 1998121100195 19981211 00195 WP 1998 12 11 MWEA981121 1 19981202 A 5320 9912243189 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACKED SHEAR TIE AT STATION 965 BETWEEN L16L AND L17L. MTC FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 1998121100196 19981211 00196 WP 1998 12 11 MWEA981122 1 19981202 A 5320 591016380 CLIP DOUG DC9 DC932 3022066 WP BS 996 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACKED SHEAR CLIP AT STATION 996 BETWEEN LONGERON 18R AND 19R. MTC FABRICATED AND INSTALLED REPAIR ANGLE. 2 L 7 2 4F A6WE 1998121100197 19981211 00197 WP 1998 12 11 MWEA981123 1 19981202 A 5320 9912243190 SHEAR TIE DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACKED SHEAR TIE AT STATION 965 BETWEEN L16R AND L17R. MTC FABRICATED AND INSTALLED NEW SHEAR TIE. 2 L 7 2 4F A6WE 1998121100198 19981211 00198 WP 1998 12 11 MWEA981124 1 19981202 A 5313 59114055 LONGERON DOUG DC9 DC932 3022066 WP BS 180 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACK IN LONGERON 4 RIGHT AT STATION 180. MTC FABRICATED AND INSTALLED NEW LONGERON SECTION. 2 L 7 2 4F A6WE 1998121100199 19981211 00199 WP 1998 12 11 MWEA981125 1 19981202 A 5313 591140617 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACK IN LONGERON 4 LEFT AT STATION 200. MTC FABRICATED AND INSTALLED NEW LONGERON SECTION. 2 L 7 2 4F A6WE 1998121100200 19981211 00200 WP 1998 12 11 MWEA981126 1 19981202 A 5313 591140613 LONGERON DOUG DC9 DC932 3022066 WP BS 200 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACK IN LONGERON 2 LEFT AT STATION 200. MTC FABRICATED AND INSTALLED NEW LONGERON SECTION. 2 L 7 2 4F A6WE 1998121100201 19981211 00201 WP 1998 12 11 MWEA981127 1 19981202 A 5330 5911408503 SKIN DOUG DC9 DC932 3022066 WP BS 537 NICKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND A NICK IN SKIN AT FUSELAGE STATION 537 LONGERON 3 RIGHT AND FUSELAGE STATION 500 LONGERON 3 RIGHT. MTC FABRICATED AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F A6WE 1998121100202 19981211 00202 WP 1998 12 11 MWEA981128 1 19981202 A 5320 991224649 ANGLE DOUG DC9 DC932 3022066 WP BS 1087 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 FOUND CRACKED SHEAR CLIP AT TOP OF FRAME ANGLE AT STATION 1087 INBOARD OF LONGERON 3 RIGHT. MTC FABRICATED AND INSTALLE D SHEAR CLIP. 2 L 7 2 4F A6WE 1998121100203 19981211 00203 WP 1998 12 11 MWEA981129 1 19981202 A 5330 59203231 SKIN DOUG DC9 DC932 3022066 WP BS 530 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 INSTALLED TEMPORARY CLASS THREE REPAIR TO FUSELAGE SKIN AT STATION 530 LONGERON 22 RIGHT TO 23 RIGHT. MTC FABRICATED AN D INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998121100204 19981211 00204 WP 1998 12 11 SCNA98147 1 19981204 A 2611 30231R17 SMOKE DETECTOR DOUG DC10 DC1015 3022118 WP CARGO COMPT NO TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 154SY 48259 DURING A LINE MAINTENANCE CHECK, THE NUMBER 4 CARGO SMOKE DETECTOR DID NOT TEST. REMOVED AND REPLACED THE SMOKE DETECTO R, OPERATIONALLY CHECKED GOOD. 2 L 7 3 4F A22WE 1998121100205 19981211 00205 NM 1998 12 11 SCNA98144 1 19981204 A 2824 6563 VALVE BOEING 727 7272A1 138407F NM NR 2 MALFUNCTIONED A SCNA A J UNSCHED LANDING DUMP FUEL O OTHER CL CLIMB 1 GL 15 285SC 22676 AT LEVEL OFF AT 31,000 FEET, NOTICED TANKS 1 AND 3 WERE DECREASING BETWEEN 9,000 AND 10,000 POUNDS EACH. TANKS 1 AND 3 CONTINUED TO DECREASE CREATING A FUEL LIMITATION PROBLEM WITH THE BOOST PUMP ON TANKS 1 AND 3 ON OR OFF. UNABLE TO STOP IMBALANCE SO ELECTED TO RETURN TO MSP. DUMPED FUEL FOR LANDING LIMITATIONS. FOUND NUMBER TWO FUEL MANIFOLD CROSSFEED VALVE INTERMITTENT. REMOVED AND REPLACED NUMBER TWO CROSSFEED VALVE PER 727 MAINTENANCE MANUAL 282211. OPERATIONALLY C HECKED GOOD. 2 L 7 3 4F A3WE 1998121100206 19981211 00206 NM 1998 12 11 SCNA98145 1 19981129 A 2530 COFFEEMAKER BOEING 727 7272J4 1384006 NM GALLEY FAILED A SCNA K NONE O OTHER NR NOT REPORTED 1 GL 15 284SC 21438 FORWARD GALLEY, WHEN BREW BUTTON FOR THE COFFEEMAKER WAS PUSHED THERE WAS ELECTRIC ARCING WHICH OCCURS ON CIRCUIT BREAKE R PANEL. TIGHTENED AND REPOSITIONED WIRE IN BACK OF CIRCUIT BREAKER PANEL. OPERATIONALLY CHECKED GOOD PER MAINTENANCE M ANUAL 25306. 2 L 7 3 4F RT A3WE 1998121100207 19981211 00207 NM 1998 12 11 SCNA98146 1 19981205 A 2131 OUTFLOW VALVE BOEING 727 7272J4 1384006 NM CABIN MALFUNCTIONED A SCNA G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 GL 15 290SC 20764 ON CLIMBOUT, PRESSURIZATION APPEARED TO BE WORKING NORMALLY. AT FL230 CABIN ALTITUDE WARNING HORN SOUNDED. CABIN ALTIT UDE INDICATED 13,000 FT. CABIN WAS CLIMBING AT 1000 FPM, O2 MASKS DROPPED IN THE PASSENGER CABIN. AUTO FAIL AND STANDB Y LIGHTS CAME ON. CREW O2 MASKS WERE PUT ON. PASSENGER O2 LIGHT WAS NOT ILLUMINATED. OUTFLOW VALVE INDICATED FULL CLO SED. STANDBY MODE WAS NOT CONTROLLING THE CABIN, WHEN THE CARGO OUTFLOW VALVE WAS CLOSED THE CABIN STOPPED CLIMBING AND STARTED A 2-300 FPM RATE OF DESCENT. CARGO OUTFLOW VALVE WAS CYCLED AND MADE RATE OF DESCENT INCREASE TO 600 FPM. AT 11,000 FT ON DESCENT INTO DESTINATION AUTO SELECTED AND SYSTEM APPEARED TO WORK NORMALLY. COULD NOT DUPLIATE ON GROUND. 2 L 7 3 4F RT A3WE 1998121100208 19981211 00208 SW 1998 12 11 DHL987DQ001 1 19981202 A 5610 206542011 WINDOW BELL 206 206L1 1182107 SW LT COCKPIT BROKEN A DHLA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 7DQ 45685 LOWER LEFT CHIN BUBBLE SUSTAINED BIRD STRIKE. REPLACED CHIN BUBBLE. 1 G 7 1 3U H2SW 1998121100209 19981211 00209 EA 1998 12 11 ASOA98079 1 19981011 A 5610 NP1393221 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT CRACKED A ASOA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 11 825AS 1966 7207 ATL/SWF - FLT 7810 - EN ROUTE AT 33,000 FEET, THE LT WINDOW BEGAN TO CRACK (FORWARD RT CORNER). CREW DECLARED AN EMERGE NCY AND DIVERTED INTO ROA WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. THE WINDOW CONTINUED TO CRACK DUR ING DESCENT DOWN REPLACED THE WINDOW. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. T AT: 1,965.5 HOURS. (X) 2 L 7 2 4F RT A21EA 1998121100210 19981211 00210 NM 1998 12 11 98ZZZX4542 1 19980617 A 3350 LIGHT BOEING 757 75723N 1384973 NM CABIN INOPERATIVE A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 MDW - DURING P/F, FOUND EMERGENCY FLOOR TRACK LIGHTING INOPERABLE FROM ROW 22 TO ROW 27. REPAIRED PUSHED BACK PIN ON PO WER PACK AND REPLACED FUSES ON TWO DIFFERENT PACKS. OPS CHECK NORMAL. 2 L 7 2 4F RT A2NM 1998121100211 19981211 00211 NE 1998 12 11 98ZZZX4543 2 19980803 A 7321 ESC10304C4 FUEL CONTROL BOEING 757 75723N 1384973 NM RROYCE RB211 RB211535C37 54555 NE RT ENGINE FAILED A AMTA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 11 517AT 27973 SCEL - REJECTED TAKEOFF DUE TO FAILURE OF RIGHT ENGINE TO DEVELOP TAKEOFF POWER INDICATED AT MAXIMUM THROTTLE 1.55 EPR A ND 80 PERCENT N1. REMOVED AND REPLACED RIGHT EEC, PERFORMED ENGINE RUN PER 71-00-00. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F RT A2NM E12EU 1998121100212 19981211 00212 NM 1998 12 11 98ZZZX4544 1 19980702 A 3350 BATTERY BOEING 727 7272Q6 138407V NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 782AT 21972 IND - RIGHT SIDE AFT OVERWING EXPRESS (ABOVE FLAP) LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY PACK. 2 L 7 3 4F RT A3WE 1998121100213 19981211 00213 NM 1998 12 11 ASAA9840094 1 19980924 A 3350 LIGHT BOEING 737 737490 1384715 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 799AS 29270 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-18. RECONNECTED LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1998121100214 19981211 00214 NM 1998 12 11 AALA981572 1 19980820 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 605AA 27056 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 9 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 9. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998121100215 19981211 00215 NM 1998 12 11 AALA981573 1 19980820 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 605AA 27056 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 18 AND AFT GETS PROGRESSIVELY DIMMER. R EPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT ROW 18. SYST EM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998121100216 19981211 00216 NM 1998 12 11 AALA981679 1 19980908 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 603AA 27054 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING BY OVERWING DOORS INOPERATIVE. REPLACED EMERGEN CY EXIT FLOOR PATH LIGHT STRIP BY OVERWING DOORS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 2 4F RT A2NM 1998121100217 19981211 00217 SO 1998 12 11 C2XA98IA412 1 19981007 A 3320 5108WW BULB EMB 145 EMB145LR SO AFT CABIN FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14953 145071 ATL - FLT 4207 - PILOT REPORTED SMOKE IN THE CABIN. THE CREW DIVERTED INTO ATL AND LANDED WITHOUT INCIDENT. MAINTENANC E FOUND TWO BULBS AT THE AFT CABIN AREA THAT WERE BURNED ON THE ENDS. THE AIRCRAFT WAS RELEASED UNDER MEL NR 33-20-00. THE MEL WAS CLEARED AT IAH, FLT 4207 WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULBS. NO FURTHER INCIDENTS H AVE BEEN REPORTED. (X) 2 L 7 2 4T RT T00011AT 1998121100218 19981211 00218 EU 1998 12 11 C2XA98IA399 1 19981001 A 3350 7008123 LIGHT AEROSP ATR42 ATR42500 EU SERVICE DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14445 503 IAH - DURING LINE CHECK INSPECTION, THE AFT SERVICE DOOR RT HAND EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANC E REMOVED AND REPLACED THE AFFECTED BULBS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1998121100219 19981211 00219 EU 1998 12 11 98ZZZX4545 1 19981001 A 3350 7012210 LIGHT AEROSP ATR42 ATR42500 EU ROWS 9 & 10 INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14445 503 IAH - DURING LINE CHECK INPSECTION, THE OVERHEAD EMERGENCY LIGHTS AT ROWS 9 AND 10 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULBS, AND THE AIRACRAFT WAS APPROVED FOR RETURN TO SERVICE. 2 H 7 2 4T RT A53EU 1998121100220 19981211 00220 EU 1998 12 11 C2XA98IA397 1 19981001 A 3350 OP1670 BULB AEROSP ATR42 ATR42500 EU CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14445 503 IAH - DURING LINE CHECK INSPECTION, THE EMERGENCY FLOOR LIGHTING WAS FOUND INOPERABLE AT SEATS 4AB, 6AB, 8AB, 9AB, 11AB, 12AB, AND 14A. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BULBS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVIC E. (X) 2 H 7 2 4T RT A53EU 1998121100222 19981211 00222 EU 1998 12 11 FJT98109221 1 19981028 A 3520 WK333001 MASK KIDDE K386384 BAG JETSTM JETSTM3201 1500217 EU CABIN FUSED A A FJTA O OTHER O OTHER NR NOT REPORTED 1 SO 03 922CX 10634 3833 922 BNA - AIRCRAFT WAS IN MAINT FOR A 4,000-HR INSPECTION. JETSTREAM MAINT TASK 35-20-00 REQUIRES PASSENGER OXYGEN MASKS BE DELPOYED, INSPECTED, CLEANED, AND REPACKED EVERY 4,000 HOURS. DURING INSPECTION, NOTICED AFTER DEPLOYING OXYGEN MASKS, A MAJORITY WERE FUSED TOGETHER. THEY HAD TO BE SEPARATED CAREFULLY BY HAND. THREE OF THE 23 MASKS WERE TORN WHILE ATT EMPTING TO SEPARATE THE MASKS. HISTORY: DATE CODES OF 3 TORN MASKS, 6/90, 9/90, AND 10/90. ACFT PLACED IN SERVICE 1/9 1. ACFT OPER BY AMR EAGLE FROM 1/91-4/96. ACFT STORED IN DESERT FROM 4/5/96 TO 5/23/97. ACFT BACK IN SERVICE 6/4/97. LAST INSP OF MASKS 5/9/95. APPROX 65 TO 75 PERCENT OF THE MASKS STICKING OR FUSED TOGETHER. PART TC: 13,093. (X) 2 L 7 2 4T RT A56EU 1998121100223 19981211 00223 CE 1998 12 11 98ZZZX4547 1 19981005 A 5210 MS3548941 SEAL CESSNA 500 550 2076604 CE PASSENGER DOOR FAILED A J7SA B A EMER. DESCENT UNSCHED LANDING O OTHER CR CRUISE 1 SW 21 551BC 5500242 AIRACRAFT LOST PRESSURIZATION DURING CRUISE AT FL 37 DUE TO A COLLAPSED CABIN DOOR SEAL. FLIGHT CREW EXECUTED THE EMERG ENCY DESCENT AT THE NEAREST AIRPORT - EL PASO, TEXAS 1 L 7 2 4F A22CE 1998121100224 19981211 00224 EA 1998 12 11 MASA98188 1 19981021 A 3350 AML1317 BULB 600522019 CNDAIR CL600 CL6002B19 EA FUSELAGE FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 RDU - DURING PRE-FLIGHT INSPECTION, PILOT REPORTED LT FORWARD EMERGENCY LIGHT BULB FAILED TO ILLUMINATE. MAINTENANCE AC TION DEFERRED PER MEL 33-51-2. (THE BULB WAS REMOVED AND REPLACED LATER ON THE SAME DAY IN BOS). AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998121100227 19981211 00227 EU 1998 12 11 SIMA982571 1 19980914 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 240DS 340B240 DFW - FLT 3662 - ROW 12 FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. OPENED MEL. REMOVED AND REPLACED BULB AT ROW 12. OP ERATIONAL CHECK GOOD. MEL CLEARED. (X) 2 L 7 2 4T RT A52EU 1998121100228 19981211 00228 EU 1998 12 11 SIMA982781 1 19981005 A 3350 3071BPEG BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 330AE 340B330 JFK - FLT 4940 - EMERGENCY FLOOR LIGHTING AT SEAT 9BC DOES NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT B ULB. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998121100229 19981211 00229 SO 1998 12 11 SIMA982831 1 19981010 A 2434 30086010 GENERATOR EMB 145 EMB145 SO RT ENGINE FAILED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 605RR 98020 145059 MKE - BILL OF WORK ISSUED TO CLEAR AN MEL ON THE NR 2 GENERATOR BEARING INDICATOR. FOUND GENERATOR WINDINGS HANGING OUT OF THE HOUSING, AND THE GENERATOR WAS HELD ONLY BY ITS WIRES. NO DAMAGE TO THE ENGINE OR COWLINGS WAS NOTED. REMOVED AND REPLACED GENERATOR. CLEARED MEL. (X) 2 L 7 2 4F RT T00011AT 1998121100230 19981211 00230 EU 1998 12 11 SIMA982856 1 19981012 A 3230 AIR130902 CONNECTOR SAAB SF340 340B 7860101 EU RT MLG BAY DISCONNECTED A SIMA O OTHER P NO WARNING INDICATION AP APPROACH 1 SW 21 903AE 340B282 DFW - FLT 3598 - RIGHT MAIN LANDING DOWN AND LOCKED LIGHT DID NOT ILLUMINATE. INTRANSIT LIGHT WORKED NORMAL. UNEVENTF UL LANDING. MAINTENANCE PINNED THE GEAR AND CREW TAXIED IN. INSTALLED RIGHT MAIN LANDING GEAR DOWNLOCK SWITCH CANNON P LUG. PERFORMED EXTENSION AND RETRACTION. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1998121100231 19981211 00231 EU 1998 12 11 SIMA982801 1 19981007 A 5220 7252210508 EXIT SAAB SF340 340B 7860101 EU RT ROW 8 MISADJUSTED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 904AE 340B314 DFW - FLT 3514 - RIGHT EMERGENCY EXIT AT ROW 8 FELL INTO THE AIRCRAFT JUST PRIOR TO PARKING. CREW REPORTED THE HANDLE WAS IN THE CLOSED POSITION. ADJUSTED THE DOOR LATCHING MECHANISM. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A52EU 1998121100232 19981211 00232 EA 1998 12 11 VTZA98298 1 19980924 A 3260 601R575111 UPLOCK CNDAIR CL600 CL6002B19 EA LT MLG OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 626BR 7225 IAD/SAV - FLT 6733 - DURING TAKEOFF AT 1,735 HOURS ON 9-24-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR DISAGREE MESSAGE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND ADJUSTED LT MLG UPLOCK TARGET AND PERFORMED GEAR SWING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998121100233 19981211 00233 EA 1998 12 11 VTZA98259 1 19980812 A 2780 T/E FLAP CNDAIR CL600 CL6002B19 EA WING FAILED A VTZA O OTHER J WARNING INDICATION LD LANDING 1 EA 27 626BR 7225 RDU/IAD - FLT 6741 - DURING LANDING AT 0650 HRS ON 8-12-98, ACFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAPS FAILED ON FINAL. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND NO DEFECTS AND COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998121100234 19981211 00234 EA 1998 12 11 VTZA98260 1 19980816 A 2752 852D100MD51 ACTUATOR CNDAIR CL600 CL6002B19 EA T/E FLAPS FAILED A VTZA B EMER. DESCENT J WARNING INDICATION LD LANDING 1 EA 27 629BR 7251 IAD/BNA - FLT 6700 - DURING LANDING AT 1,000 HRS ON 8-16-98, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHIC H WAS FLAP WARNING LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS, AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND REMOVED AND REPLACED LT OUTBOARD/INBOARD FLAP ACTUATOR. MAINTENANCE PERFORMED OPS CHECK, OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1998121100235 19981211 00235 NM 1998 12 11 W7NA9800003 1 19980917 A 2820 FUEL MANIFOLD BOEING 737 737247 138448D NM NR 1 ENGINE CHAFED A W7NA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 07 902WC 19613 ACY - RT FUEL MANIFOLD P/N 581033 FND WITH CHAFE THRU HOLE BETWEEN NR'S 2 AND 3 FUEL NOZZLE. CHAFE CAUSED BY BRACKET P/ N 487659 CRACKING AND PARTING NR 2 NOZZLE AND LOGGING ITSELF BTWN MANIFOLD AND CCOC FWD FLANGE. REMOVED AND REPLACED RT FUEL MANIFOLD IAW PWA JT8D MM 73-13-1. BRACKETS P/N 487659 AT NOZZLES 1,2,3,4,8, AND 9 CRACKED (NR 2 DEPARTED). REMOV ED AND REPLACED SIX BRACKETS, P/N 487659, LOCATIONS 1,2 3 4,8, AND 9 IAW PWA JT8D MM 73-13-1. RT DIFFUSER INNER DUCT CR ACKED AT NR 1 FUEL NOZZLE, CRACKED AND TORN AT NR 2 FUEL NOZZLE. REMOVED AND REPLACED RT AND LT DIFFUSER INNER DUCT P/N 794886 AND 794887 IAW PWA JT8D MM 72-00-38. PERFORMED ENGINE RUN-UP CHK IAW PWA JT8D MM 72-00 TESTS B, C, H. 2 L 7 2 4F A16WE 1998121100236 19981211 00236 WP 1998 12 11 WXOA98001 1 19981014 A 3320 MB10P1 CONNECTOR DOUG DC9 DC921 302205A WP ROWS 9-10 FAILED A WXOA K NONE O OTHER IN INSP/MAINT 1 WP 17 127NK 47361 FAT - DURING ACCOMPLISHMENT OF SCHEDULED AIRCRAFT MAINTENANCE, FOUND DAMAGED ELECTRICAL WIRING CONNECTOR AT PRODUCTION S PLICE FOR ROWS 9-10 (RT) CABIN INTERIOR OVERHEAD AND SIDEWALL LIGHTING. GROUND WIRE DISCOVERED LOOSE AT CONNECTOR CAUSI NG ELECTRICAL ARCING RESULTING IN THE DAMAGE TO CONNECTOR. REMOVED CONNECTOR AND REPAIRED WIRING. (X) 2 L 7 2 4F A6WE 1998121100237 19981211 00237 1998 12 11 W7NA9800002 4 19980918 A 2210 4030952906 YAW COUPLER HONEYWELL 4030952906 BOEING 737 7372Y5 1384554 NM RUDDER FAILED A A W7NA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 07 118RW 83011934 23040 EWR - FLT 1606 - DURING TAKEOFF ROLL AT 90 KNOTS, AIRCRAFT VEERED SIGNIFICANTLY TO THE LEFT TWICE. ABORTED TAKEOFF. I NSPECTED AND FOUND YAW DAMPENER FAILED HARD LEFT. REMOVED AND REPLACED YAW DAMPENER COUPLER PER MM 22-11-141. GROUND T ESTS SHOW OPS NORMAL. (X) 2 L 7 2 4U RT A16WE 1998121100238 19981211 00238 EA 1998 12 11 SABA9804 1 19980628 A 6123 8190026 SWITCH DHAV DHC6 DHC6300 2802606 EA AUTOFEATHER FAILED A S9BA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 05 251SA 524 KIA/KTN - ON FLIGHT, CREW REPORTED ON LOG PAGE 16304 'UNSCHEDULED AUTOFEATHER RIGHT SIDE ON TAKEOFF'. THE CREW RETURNED TO DOCK WITH NO FURTHER PROBLEM. REPLACED AUTOFEATHER PRESSURE SWITCH. OPS CHECK OK PER PSM 1-63-2 CHAPTER 61 ON LOG PAGE 16304 DATED 6-28-98. (X) 1 H 7 2 3T RT A9EA 1998121100249 19981211 00249 SO 1998 12 11 98ZZZX4560 1 19981110 A 2140 A23D0475 FUEL REGULATOR JANITROL B4050 PIPER PA31 PA31350 7103110 SO HEATER MALFUNCTIONED A P A FFSA K NONE K W FLUID LOSS INADEQUATE Q C IN INSP/MAINT 1 AL 01 4301C 16 3933220 318353001 REGULATOR LEAKING BETWEEN GASKETS. THIS WAS ONE OF THREE REGULATORS INSTALLED IN A TWO-WEEK PERIOD THAT FAILED. MFG DA TE: 7-98. REMOVED 11-4-98. 1 L 7 2 3O A20SO 1998121100250 19981211 00250 SO 1998 12 11 98ZZZX4561 1 19981110 A 2140 A23D0475 FUEL REGULATOR JANITROL B4050 PIPER PA31 PA31350 7103110 SO HEATER FAILED A P A FFSA K NONE K W FLUID LOSS INADEQUATE Q C IN INSP/MAINT 1 AL 01 4301C 3933220 318353001 FUEL REGULATOR WILL NOT OPEN TO ALLOW FUEL FLOW. PART MFG: 6-98. REMOVED. 1 L 7 2 3O A20SO 1998121100251 19981211 00251 SO 1998 12 11 98ZZZX4562 1 19981110 A 2140 A23D0475 FUEL REGULATOR JANITROL B4050 PIPER PA31 PA31350 7103110 SO HEATER MALFUNCTIONED A P A FFSA K NONE K W FLUID LOSS INADEQUATE Q C IN INSP/MAINT 1 AL 01 4301C 5 3933220 318353001 LEAKING FUEL FROM BODY (TOP). THIS WAS ONE OF THREE REGULATORS IN TWO-WEEK PERIOD THAT FAILED. MFG DATE: 8-98. REMOVE D 11-7-98. 1 L 7 2 3O A20SO 1998121100252 19981211 00252 CE 1998 12 11 98ZZZX4563 1 19981110 A 3222 5042000214 STRUT CESSNA 310 310P 2074238 CE NLG FAILED A EHBA O OTHER O OTHER LD LANDING 1 EA 17 5092P 310P0057 NOSE LANDING GEAR FAILED TO FULLY EXTEND ON TAKEOFF. NOSE GEAR WAS UNABLE TO PROPERLY STOW IN WHEELWELL AND GETTING STU CK IN THE UP POSITION. AIRCRAFT LANDED ON THE MAIN GEAR ONLY DAMAGING NOSE AND BOTH PROPELLERS. SUBMITTER STATED IN SP EAKING WITH CESSNA REP, A SUDDEN DROP IN OAT WILL CAUSE THIS CONDITION. 1 L 7 2 3O 3A10 1998121100323 19981211 00323 NM 1998 12 11 USAA980523 1 19981015 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 274US 42706 22886 PIT - FOUND RON, FOUND 3 INCH CRACK IN SKIN AT STATION 767 .5 INCH ABOVE STRINGER NR 20. INSTALLED DOUBLER PER SRM 53-3 0-03. (M) 2 L 7 2 4F A16WE 1998121100324 19981211 00324 WP 1998 12 11 USAA980531 1 19981017 A 5311 99118594 FRAME DOUG DC9 DC931 3022065 WP BS 1104 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 931VJ 78786 47188 PIT - DURING C-4 CHECK, FOUND .5 INCH TO .75 INCH CRACKS AT STATION 1104 AT FRAME LONGERON 13R. REPLACED FROM STA 1104 FROM 11R-22R FLOOR, FACTORY SPLICE PER SRM 53-03 FIG 30. (M) 2 L 7 2 4F A6WE 1998121100325 19981211 00325 WP 1998 12 11 USAA980530 1 19981017 A 5311 99118593 FRAME DOUG DC9 DC931 3022065 WP BS 1104 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 931VJ 78786 47188 PIT - DURING C-4 CHECK, FOUND .5 INCH CRACKS AT LONGERON 14L, STATION 1104 CANTED FRAME. REPLACED FRAME FROM 11L TO 22L FLOOR FACTORY SPLICE PER SRM 53-03 FIG 30. (M) 2 L 7 2 4F A6WE 1998121100326 19981211 00326 WP 1998 12 11 USAA980529 1 19981017 A 5311 9911859121 FRAME DOUG DC9 DC931 3022065 WP BS 1104 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 931VJ 78786 47188 PIT - DURING C-4 CHECK, FOUND .5 INCH CRACKS AT 3 LONGERONS AT STATION 1104 LONGERONS 3R, 4R, AND 6R. REPLACED FRAME AS SEMBLY PER SRM 53-03 FIG 30. (M) 2 L 7 2 4F A6WE 1998121100327 19981211 00327 WP 1998 12 11 USAAD98197 1 19981102 A 3230 59516395001 CYLINDER DOUG DC9 DC931 3022065 WP NLG WW MALFUNCTIONED A USAA O OTHER O OTHER AP APPROACH 1 EA 19 967VJ 74934 47375 BWI-BDL - FLT 1074 - THERE WAS A NOSE GEAR UNSAFE INDICATION WHEN THE LANDING GEAR WAS EXTENDED FOR LANDING. AFTER CYCL ING THE GEAR, ALL INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE NOSE LANDING GEAR BUNGEE CYLINDER. (M) 2 L 7 2 4F A6WE 1998121100328 19981211 00328 WP 1998 12 11 USAAD98198 1 19981103 A 2560 3753213143 LANYARD DOUG DC9 DC931 3022065 WP SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 955VJ 47593 LEX - THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LANYARD WAS BROKEN. MAINTENANCE REPLACED THE MAIN ENTRANCE DOOR EMERGENCY SLIDE LANYARD. (M) 2 L 7 2 4F A6WE 1998121100329 19981211 00329 NM 1998 12 11 USAASB98281 1 19981023 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 525AU 23860 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP IN THE MID AND AFT CABIN. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK AND TWO BATTERY CHARGER ASSEMBLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998121100330 19981211 00330 NM 1998 12 11 98ZZZM924 1 19981023 A 3350 20121 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 525AU 23860 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP IN THE MID AND AFT CABIN. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK AND TWO BATTERY CHARGER ASSEMBLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998121100331 19981211 00331 NM 1998 12 11 98ZZZM925 1 19981023 A 3350 110049 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 525AU 23860 PIT - MAINTENANCE FOUND THE EMERGENCY LIGHTS INOP IN THE MID AND AFT CABIN. MAINTENANCE REMOVED AND REPLACED A BATTERY PACK AND TWO BATTERY CHARGER ASSEMBLIES. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998121100332 19981211 00332 NM 1998 12 11 USAASB98286 1 19981029 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 ROC - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE FORWARD SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED TH E BATTERIES IN THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998121100333 19981211 00333 NM 1998 12 11 USAASB98279 1 19981022 A 3350 S106 BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 229US 21818 CLE - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN ABOVE THE AFT LEFT SERVICE DOOR DIM. MAINTENANCE REMOVED AND REPLACED T HE BATTERIES FOR THE EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998121100334 19981211 00334 NM 1998 12 11 USAA980502 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 807 STRINGER 9R TIE CLIP. INSTALLED MODIFIED P ART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998121100335 19981211 00335 NM 1998 12 11 USAA980511 1 19981029 A 5330 SKIN BOEING 737 7372B7 1384560 NM BS 767 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 767 STRINGER 19R OF SKIN. INSTALLED DOUBLER PE R SRM 53-30-3. (M) 2 L 7 2 4F A16WE 1998121100336 19981211 00336 NM 1998 12 11 USAA980507 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 685 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 685 STRINGER 4R TIE CLIP. INSTALLED MODIFIED PART P ER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998121100337 19981211 00337 NM 1998 12 11 USAA980506 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 747 STRINGER 9L TIE CLIP. INSTALLED MODIFIED PART P ER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998121100338 19981211 00338 NM 1998 12 11 USAA980505 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 639 STRINGER 4L TIE CLIP. INSTALLED MODIFIED PART P ER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998121100339 19981211 00339 NM 1998 12 11 USAA980504 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VIAUL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 2R TIE CLIP. INSTALLED MODIFIED PA RT PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998121100340 19981211 00340 NM 1998 12 11 USAA980503 1 19981029 A 5320 69353521 CLIP BOEING 737 7372B7 1384560 NM BS 616 CRACKED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 268AU 43959 22880 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 1R TIE CLIP. INSTALLED MODIFIED P ART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M) 2 L 7 2 4F A16WE 1998121100341 19981211 00341 NM 1998 12 11 TAOA109809 1 19981027 A 3350 900835A BATTERY BOEING 727 727227 1384078 NM FUSELAGE DISCHARGED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 927TS N2109 20837 FLT 6521 - LGA-DCA - RIGHT FORWARD OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1998121100342 19981211 00342 NM 1998 12 11 TAOA109810 1 19981027 A 3350 ML3071 BULB BOEING 727 727227 1384078 NM CABIN FAILED A TAOA K NONE L NO TEST IN INSP/MAINT 1 EA 15 927TS 20837 FLT 6521 - LGA-DCA - ESCAPE PATH LIGHTING AT 26A INOP. RELAMPED. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1998121100343 19981211 00343 WP 1998 12 11 GAIA98109 1 19981101 A 3234 4913801BS25124 CONTROL CABLE DOUG DC9 DC915F 3022037 WP RT MLG WW LOOSE A GAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 563PC 47055 KHA - FLT 1211 - YIP-MMLO - AFTER TAKEOFF FROM YIP THE FLIGHT CREW FOUND THE LANDING GEAR DID NOT RETRACT WITH THE GEAR HANDLE UP. THE CREW ELECTED TO RETURN TO YIP AND MADE AN UNEVENTFUL LANDING. INVESTIGATION FOUND THE LANDING GEAR BY-P ASS HANDLE CABLE OFF A PULLEY KEEPING THE LANDING GEAR CONTROL VALVE FROM FULLY RETURNING TO THE NORMAL POSITION. THE C ABLE WAS REINSTALLED ON THE PULLEY AND THE LANDING GEAR WAS OPS CHECKED SEVERAL TIME WITH NO DEFECTS NOTED. THE AIRCRAF T WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998121100344 19981211 00344 WP 1998 12 11 ASAA9880219 1 19981105 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1117 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OAK - DURING 15K CHECK, CORROSION WAS FOUND ON FLOOR WEB OUTBOARD OF FLOOR PANEL E-13 AT FS 1117. REPAIRED WITH DOUBLER IAW ASA EA 5320-01203. (M) 2 L 7 2 4F RT A6WE 1998121100345 19981211 00345 NM 1998 12 11 MZZA98225 1 19980926 A 5320 6519606254 CHANNEL BOEING 727 727224 1384076 NM LAVATORY CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON RT AFT LAVATORY INBOARD WALL PARTITION L OWER SUPPORT HAT CHANNEL. THE CORRODED HAT CHANNEL, P/N 65-19606-254 WAS REMOVED AND REPLACED WITH NEW HAT CHANNEL. (M ) 2 L 7 3 4F A3WE 1998121100346 19981211 00346 NM 1998 12 11 MZZA98224 1 19980923 A 5311 655414928 FRAME BOEING 727 727224 1384076 NM BS 300-356 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON R1 SERVICE DOOR LOWER SILL INBOARD CHORD (Z-CHANNEL) UPPER SURFACE BETWEEN BS 300 AND BS 356. THE CORRODED INBOARD CHORD WAS CORROSION CLEANUP AND REPAIRED PER B727 SRM 51-10-06 AND 51-40-01. (M) 2 L 7 3 4F A3WE 1998121100347 19981211 00347 NM 1998 12 11 MZZA98223 1 19981002 A 5315 FLOORBEAM BOEING 727 727224 1384076 NM BS 344 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DUIRNG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPER CHORD AF T FLANGE AT BS 344 RBBL 10. THE CORRODED UPPER CHORD AFT FLANGE 3 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 7. (M) 2 L 7 3 4F A3WE 1998121100348 19981211 00348 NM 1998 12 11 MZZA98222 1 19980928 A 5320 6518745421 DOUBLER BOEING 727 727224 1384076 NM RT MLG WW CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON RIGHT MAIN WHEEL WELL PRESSURE FLOOR REI NFORCEMENT DOUBLER AT BS 901 RBBL 39. THE DAMAGED REINFORCEMENT DOUBLER, P/N 65-18745-421 WAS REMOVED AND REPLACED WITH NEW REINFORCEMENT DOUBLER PER CMI EA 5310-01847. (M) 2 L 7 3 4F A3WE 1998121100349 19981211 00349 NM 1998 12 11 MZZA98244 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD AFT FLAP T/E UP PER SKIN AT WBL 105 AND WBL 118. THE DAMAGED SKIN 36 INCH BY 1.8 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100350 19981211 00350 NM 1998 12 11 MZZA98245 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP T/E UP PER SKIN AT WBL 83. THE DAMAGED SKIN 13 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100351 19981211 00351 NM 1998 12 11 MZZA98246 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP T/E UP PER SKIN AT WBL 122 AND BETWEEN WBL 129 AND WBL 184. THE DAMAGED SKIN 86.5 INCH BY 4 INCH IN SIZE WAS TRIMMED OUT AND R EPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100352 19981211 00352 NM 1998 12 11 MZZA98247 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASI, CORROSION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP NOSE UPPER SKIN AT WBL 123. THE CORRODED SKIN 1.5 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 57-50-4 FIGURE 2. (M) 2 L 7 3 4F A3WE 1998121100353 19981211 00353 NM 1998 12 11 MZZA98248 1 19980928 A 5755 6517348108A SKIN BOEING 727 727224 1384076 NM NR 7 SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 7 SPOILER T/E UPPER SKIN. THE DAM AGED SKIN 6 INCH BY 2.4 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100354 19981211 00354 NM 1998 12 11 MZZA98249 1 19981020 A 5753 652163491 SKIN BOEING 727 727224 1384076 NM LT TE FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD AFT FLAP LOWER SKIN AT WBL 92. THE DAMAGED SKIN 3 INCHES DIAMETER WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100355 19981211 00355 NM 1998 12 11 MZZA98231 1 19980928 A 5311 655614870 FRAME BOEING 727 727224 1384076 NM BS 1016-1105 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT AFT SERVICD DOOR LOWER SILL INBOARD CHORD AT RBBL 64 BETWEEN BS 1080, BS 1089 AND BS 1066. THE CORRODED DOOR LOWER SILL INBOARD CHORD (Z-CHANNEL) FROM BS 1016 TO BS 1105 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 1998121100356 19981211 00356 NM 1998 12 11 MZZA9825 1 19980923 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RIGHT WING T/E INBOARD AFT FLAP LOWER SKIN AT WBL 97. THE DAMAGED SKIN 12.5 INCH BY 3.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100357 19981211 00357 NM 1998 12 11 MZZA98252 1 19980924 A 5755 651734781 SKIN BOEING 727 727224 1384076 NM NR 11 SPOILER CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 11 SPOILER UPPER SKIN AT WBL 317 A ND WBL 327. THE DAMAGED SKIN 18 INCH BY 7 INCH AND 9 INCH DIAMETER WERE TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100358 19981211 00358 NM 1998 12 11 MZZA98253 1 19980925 A 5743 658216294 BEAM BOEING 727 727224 1384076 NM RT MLG CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON RT MLG SUPPORT BEAM LOWER SURFACE ATTACH TO INBOARD TRACK AT WBL 127. THE MLG SUPPORT BEAM WAS BLEND OUT REPAIRED PER CMI E/RA NR 5740-01864 DATED OCT 26, 1998 . (M) 2 L 7 3 4F A3WE 1998121100359 19981211 00359 NM 1998 12 11 MZZA98254 1 19980925 A 5754 SKIN BOEING 727 727224 1384076 NM RT LE FLAP DISBONDED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DISBONDED WAS FOUND ON RT WING T/E INBOARD FORE FLAP UPPER SKIN EXISTING FIBERGLASS REPAIR DOUBLER. THE DAMAGED SKIN 13 INCHES BY 1.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B7 27 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100360 19981211 00360 NM 1998 12 11 MZZA98255 1 19980927 A 5753 SPAR BOEING 727 727224 1384076 NM RT TE FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT WING T/E INBOARD MID FLAP R EAR SPAR LOWER CHORD AFT FLANGE AT WBL 87. THE CORRODED MID FLAP REAR SPAR LOWER CHORD AFT FLANGE 1.375 INCH BY 6.625 I NCH WAS TRIMMED OUT AND REPAIRED PER CMI EC/RA NR 5750-03061 DATED OCT 28, 1998. (M) 2 L 7 3 4F A3WE 1998121100361 19981211 00361 NM 1998 12 11 MZZA98256 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM RT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON RIGHT WING T/E INBOARD MID FLAP T/E U PPER SKIN AT WBL 80 AND WBL 90. THE DAMAGED SKIN 25.125 INCH BY 2.65 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100362 19981211 00362 NM 1998 12 11 MZZA98257 1 19980925 A 5320 STIFFENER BOEING 727 727224 1384076 NM BS 918 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT MAIN W/W INBOARD ALL STIFFENER AT B S 918. THE CORRODED STIFFENER 3 INCH LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1998121100363 19981211 00363 NM 1998 12 11 MZZA98258 1 19980925 A 5320 STIFFENER BOEING 727 727224 1384076 NM BS 933 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT MAIN W/W INBOARD WALL STIFFENER AT BS 933. THE CORRODED STIFFENER WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1998121100364 19981211 00364 NM 1998 12 11 MZZA98259 1 19980927 A 5753 SPLICE BOEING 727 727224 1384076 NM LT TE FLAP CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP L/E INTER IOR SPLICE PLATE AT WBL 122. THE CORRODED SPLICE PLATE WAS REMOVED AND REPLACED WITH NEW SPLICE PLATE MADE FROM 2024-T3 CLAD SHEET. (M) 2 L 7 3 4F A3WE 1998121100365 19981211 00365 EU 1998 12 11 C2XA98IA461 1 19981110 A 5315 S53672406208 FLOORBEAM AEROSP ATR42 ATR42500 EU BS 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM AT FRAME 36 CORRODED. MAINTENANCE REMOVED THE EXISTING CORROSION AND I NSTALLED REPAIR DOUBLERS WHERE REQUIRED IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC 5310-0 1037. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100366 19981211 00366 EU 1998 12 11 C2XA98IA463 1 19981110 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING C-CHECK INSPECTION, FOUND LEFT SIDE FLIGHT ATTENDANTS SEAT TRACK CORRODED. MAINTENANCE REMOVED THE EXISTIN G CORROSION AND INSTALLED A REPAIR DOUBLER IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC 534 0-01018. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100367 19981211 00367 EU 1998 12 11 C2XA98IA462 1 19981110 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42500 EU BS 38 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING C-CHECK INSPECTION, FOUND FLOORBEAM AT FRAME 38 CORRODED. MAINTENANCE REMOVED THE EXISTING CORROSION AND I NSTALLED REPAIR DOUBLERS WHERE REQUIRED IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION (ECRA) EC 5310-0 1037. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100368 19981211 00368 EU 1998 12 11 C2XA98IA464 1 19981110 A 5313 S5357140021500 STRINGER AEROSP ATR42 ATR42500 EU BS 27-29 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING C-CHECK INSPECTION, FOUND STRINGER 16 RIGHT CORRODED FROM FRAME 27 TO 29. MAINTENANCE REMOVED AND REPLACED THE STRINGER IAW ATR-42 SRM 51-21-42 AND 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 1998121100369 19981211 00369 SO 1998 12 11 C2XA98IA465 1 19981103 A 3350 GE1317 BULB EMB 145 EMB145LR SO FUSELAGE FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14952 145067 IAH - DURING PRE-FLIGHT INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULBS IN THE AFFECTED LIGHTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1998121100370 19981211 00370 SO 1998 12 11 C2XA98IA457 1 19981110 A 5730 12015668001 SKIN EMB 120 EMB120RT SO LT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12709 120101 IAH - DURING C-CHECK INSPECTION, FOUND LEFT WING INBOARD LOWER SKIN CRACKED ON INBOARD FORWARD SIDE OF ACCESS 521AB. MA INTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998121100371 19981211 00371 SO 1998 12 11 C2XA98IA458 1 19981110 A 5730 12015667002 SKIN EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12709 120101 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING INBOARD LOWER SKIN CRACKED ON INBOARD FORWARD CORNER OF ACCESS 622EB. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 57-20-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998121100372 19981211 00372 SO 1998 12 11 C2XA98IA459 1 19981110 A 5320 12015374002 ANGLE EMB 120 EMB120RT SO VERTICAL STAB CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12709 120101 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE VERTICAL STIFFENER STABILIZER DRAG ANGEL CRACKED ON FORWARD END. MAIN TENANCE REMOVED AND REPLACED THE DAMAGED SECTION OF THE DRAG ANGLE IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUT HORIZATION (ECRA) EC5530-01013. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998121100373 19981211 00373 SO 1998 12 11 C2XA98CL072 1 19981106 A 3350 F0035 FUSE EMB 120 EMB120RT SO ROW 9-11 FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 47722 120166 CLE - FLT 3351 - CREW REPORTED THE EMERGENCY ESCAPE FLOOR LIGHTS DO NOT WORK FROM ROW 9 TO ROW 11. MAINTENANCE INSPECTE D THE EMERGENCY LIGHTING SYSTEM THEN REMOVED AND REPLACED A FUSE AND ALSO REPAIRED A WIRE FOR PRECAUTIONARY REASON. THE EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECKS WERE SATISFACTORY IAW EMB120 MM 33-50-00. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998121100374 19981211 00374 CE 1998 12 11 C2XA98CL071 1 19981105 A 3060 3E24143 BRUSH BLOCK BEECH 1900 1900D 1154162 CE RT PROPELLER WORN A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 48544 UE183 CLE - FLT 3291 - CREW REPORTED THAT AFTER TAKEOFF THE RIGHT PROPELLER ANTI-ICE SYSTEM WAS INDICATING 24 AMPS. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE RIGHT PROPELLER ANTI-ICE SYSTEM THEN REMOVED AND REPLACED THE DE-ICE BRUSH BLOCK IAW B1900 MM 30-60-00, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1998121100375 19981211 00375 1998 12 11 C2XA98IA467 4 19981118 A 2562 4630150 ELT BEECH 1900 1900D 1154162 CE FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69548 UE193 IAH - DUIRNG LINE MAINTENANCE INSPECTION, THE ELT WAS FOUND TO BE TRANSMITTING INADVERTANTLY WHEN NO SELECTED. MAINTENA NCE INSPECTED THE AIRCRAFT AND FOUND THE ELT CASE TO BE DAMAGED. MAINTENANCE REMOVED AND REPLACED THE ELT IAW B1900 MM 25-60-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998121100376 19981211 00376 1998 12 11 C2XA98IA456 4 19981117 A 2562 4530150 ELT BEECH 1900 1900D 1154162 CE FUSELAGE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 69549 UE194 IAH - FLT 3910 - THE CREW REPORTED THAT THE ELT REMOTE SWITCH LIGHT WAS ILLUMINATED WITH THE SWITCH IN THE OFF POSITION BUT, THE ELT WAS NOT TRANSMITTING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE ELT CASE TO BE DAMAGED. MAINTENANC E REMOVED AND REPLACED THE ELT IAW B1900 MM 25-60-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1998121100377 19981211 00377 NM 1998 12 11 GAIA98115A 1 19981116 A 2612 1011B1 POWER SUPPLY BOEING 727 727251 138408H NM COCKPIT INOPERATIVE A GAIA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 279US 21158 EN ROUTE TO TOL TO PHX, THE AIRCRAFT HAD THE FIRE WARNING BELL CAME ON WITHOUT ANY WARNING LIGHT INDICATION AS TO WHICH ENGINE OR ANY OTHER INDICATIONS DURING CRUISE. THE AIRCRAFT LANDED WITHOUT ANY FURTHER DIFFICULTIES. REMOVED AND REPLA CED THE NR 1 FIRE WARNING POWER SUPPLY UNIT. OPERATIONALLY CHECKS NORMAL TO GROUND. THE AIRCRAFT IS RETURNED TO SERVIC E. (M) 2 L 7 3 4F A3WE 1998121100378 19981211 00378 NM 1998 12 11 GAIA98124 1 19981118 A 3230 PIN BOEING 727 727214 138407R NM NLG UNLOCKED A GAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 750US 21512 DURING SCHEDULED FLIGHT FROM MCI TO PHX THE AIRCRAFT WAS DIVERTED TO ELP. THE CREW WAS NOTIFIED THAT THE NOSE GEAR TORQ UE LINKS WERE NOT SECURED PROPERLY BY THE GROUND HANDLER VIA ARINC. THE FLT CREW WAS INFORMED BY PHX CONTROL THAT THEY WHERE UNABLE TO LAND THERE AND THAT THEY WOULD HAVE TO DIVERT TO ELP. THE CREW MADE A PRECAUTIONARY LANDING WITHOUT FUR THER INCIDENT. INSPECTED NLG TORQUE LINKS, LOCKING PIN. FOUND LOCKING TAB UNLOCKED. REMOVED PIN AND VISUALLY INSPECTE D TORQUE LINK ARMS AND BUSHINGS. NO DAMAGE NOTED. VERIFIED LOCKING FUNCTION OK. SECURED LOCKING PIN AND AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1998121100379 19981211 00379 WP 1998 12 11 HALA9800385 1 19981107 A 3260 SENSOR DOUG DC9 DC951 3022051 WP LT MLG MALFUNCTIONED A HALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 13 699HA 47763 HNL - FLT 385 - LEFT MAIN GEAR UNSAFE LIGHT (RED) CAME ON AND WENT OFF SEVERAL TIMES DURING FLIGHT WITH GEAR RETRACTED. REMOVED AND REPLACED GEAR-UP SENSOR. CONTINUITY TESTED UP AND DOWN LOCK CIRCUITS. NO DEFECTS NOTED. REPLACED 52-57 A ND 92-55 PROX SENSORS AS PRECAUTIONARY CHECK OK PER MM 32-60-0 CODE 10. (M) 2 L 7 2 4F RT A6WE 1998121100380 19981211 00380 WP 1998 12 11 HALA9800387 1 19981112 A 5730 PANEL DOUG DC9 DC951 3022051 WP RT WING LOOSE A HALA O OTHER K FLUID LOSS NR NOT REPORTED 1 WP 13 699HA 47763 KOA - FLT 388 - PASSENGER REPORTS FUEL LEAKING FROM ACCESS PANEL ON TOP OF RIGHT WING INFLIGHT. RESECURED FUEL TANK ACC ESS PANEL NR 2 OUTBOARD OF FORWARD EMERGENCY DOOR LEAK CHECK GOOD, SECURITY CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998121100381 19981211 00381 NM 1998 12 11 MZZA98241 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E OUTBOARD AFT FLAP UPPER SKIN AT INBOARD AFT CORNER. THE DAMAGED SKIN 3.5 INCH BY 3.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51 -40-6. (M) 2 L 7 3 4F A3WE 1998121100382 19981211 00382 NM 1998 12 11 MZZA98242 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E OUTBOARD AFT FLAP T/E U PPER SKIN AT WBL 348. THE DAMAGED SKIN 18 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M ) 2 L 7 3 4F A3WE 1998121100383 19981211 00383 NM 1998 12 11 MZZA98243 1 19980927 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E AFT FLAP LOWER SKIN AT WBL 232. THE DAMAGED SKIN 4 INCH 10.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100384 19981211 00384 NM 1998 12 11 MZZA98239 1 19980925 A 5754 SKIN BOEING 727 727224 1384076 NM LT LE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD FORE FLAP UPPER SKIN AT WBL 72. THE DAMAGED SKIN 7.125 INCH BY 5.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M ) 2 L 7 3 4F A3WE 1998121100385 19981211 00385 NM 1998 12 11 MZZA98238 1 19980925 A 5754 SKIN BOEING 727 727224 1384076 NM LT LE FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E OUTBOARD FORE FLAP T/E LOWER SKIN AT WBL 485. THE DAMAGED SKIN 2.5 INCH BY 2.5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100386 19981211 00386 NM 1998 12 11 MZZA98237 1 19980930 A 5542 SKIN BOEING 727 727224 1384076 NM RUDDER TAB DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON UPPER RUDDER CONTROL TAB LEFT SIDE L/ E SKIN. THE DAMAGED SKIN 2 INCH BY 12 INCH, 2 INCH BY 4 INCH , 1 INCH BY 5 INCH AND 1 INCH BY 5 INCH IN SIZE WERE TRIMM ED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1998121100387 19981211 00387 NM 1998 12 11 MZZA98236 1 19980930 A 5542 65624446 SKIN BOEING 727 727224 1384076 NM RUDDER TAB CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LOWER RUDDER TAB L/E NOSE SKIN AT RUDDER STATION 80. THE CORRODED NOSE SKIN, P/N 65-62444-5 WAS REMOVED AND REPLACED WITH NEW SKIN. (M) 2 L 7 3 4F A3WE 1998121100388 19981211 00388 NM 1998 12 11 MZZA98235 1 19980930 A 5311 FRAME BOEING 727 727224 1384076 NM BS 804 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1.5 INCH LONG CRACK WAS FOUND ON BS 804.5 FRAME OUTBOARD CHORD AT S-14R. THE CRACK END WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1998121100389 19981211 00389 NM 1998 12 11 MZZA98234 1 19980929 A 5321 FLOOR BOEING 727 727224 1384076 NM BS 1173 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FLOOR WEB AT BS 1173 RBBL 45. THE CORRO DED FLOOR WEB 1 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998121100390 19981211 00390 NM 1998 12 11 MZZA98233 1 19980929 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 380-420 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBBL 24 .75 BETWEEN BS 380 AND BS 420. THE CORRODED SEAT TRACK FROM BS 380 TO BS 420 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B727 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1998121100391 19981211 00391 NM 1998 12 11 MZZA98232 1 19980928 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1030-1070 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBBL 24 .75 BETWEEN BS 1035 AND BS 1067. THE CORRODED SEAT TRACK FROM BS 1030 TO BS 1070 WAS TRIMMED OUT AND INSTALLED REPLACEM ENT TRACK PER B727 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1998121100392 19981211 00392 NM 1998 12 11 MZZA98260 1 19980925 A 5754 651622292 WEB BOEING 727 727224 1384076 NM NR 6 LE FLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .625 INCH LONG CRACK WAS FOUND ON NR 6 SLAT INTERIOR FORWARD WE B AT SS 156. THE CRACK END WAS STOP DRILLED AND REPAIRED PER B727 SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998121100393 19981211 00393 EU 1998 12 11 RAIA981008 1 19981015 A 2150 12503903 EVAPORATOR BAG JETSTM JETSTM3201 1500217 EU A/C BAY FAILED A RAIA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CE 03 860AE 860 FLT 4721 - SFO - SMOKE IN CABIN COMING FROM AIR CONDITIONER VENT ABOVE AFT BAGGAGE. MAINTENANCE REPLACED EVAPORATER MOD ULE. (M) 2 L 7 2 4T RT A56EU 1998121100394 19981211 00394 NM 1998 12 11 PCAA9800791 1 19981025 A 2432 20412 BATTERY DHAV DHC8 DHC8102 2809003 NM E/E BAY OVERTEMP A PCAA A UNSCHED LANDING M OVER TEMP NR NOT REPORTED 1 EA 13 824EX 038211 387 EN ROUTE FROM PIT TO IPT, THE MAIN BATTERY HOT CAUTION LIGHT ILLUMINATED AND TEMPERATURE MONITOR ROSE TO 60 DEGREES CELS IUS. THE CREW DIVERTED INTO SCE, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM, FOUND BATTERY AT FAULT. REMOVED AND REPLACED MAIN BATTERY, OPERATION CHECK GOOD IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998121100395 19981211 00395 NM 1998 12 11 PCAA9800788 1 19981018 A 2431 68001008010 INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 13 816EX 203 329 EN ROUTE TO PIT, THE MAIN AND AUXILIARY BATTERY CAUTION LIGHTS ILLUMINATED. THE TEMPERATURE MONITOR WENT DEAD ASSOCIATE D WITH THE CIRCUIT BREAKER POPPING. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHO T SYSTEM, FOUND THE TEMPERATURE MONITOR AT FAULT. THE MONITOR WAS REMOVED AND REPLACED IAW DHC PROCEDURES. TESTED OK. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998121100396 19981211 00396 NM 1998 12 11 PCAA9800790 1 19981018 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM NR 2 ENGINE FAILED A PCAA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 EA 13 818EX 930140 235 NR 2 OIL TEMP PEAKED AT 120 DURING CLIMB. GOT AS LOW AS 114 DURING DESCENT. PRECAUTIONARY LANDING MADE AT BDL. LIMITA TION EXCEEDED BY 7 MINS AT 115 DEGREES WHILE COMING IN ON APPROACH. REMOVED AND REPLACED OIL COOLER ASSEMBLY. GROUND R AN ENGINE, TEMPERATURE HELD AT 80 DEGREES. SYSTEM OPERATIONAL AND LEAK CHECK GOOD IAW DHC PROCEDURES. ENGINE OIL SYSTE M INSPECTED PER PWM MANUAL FOR EXCEEDING LIMITS. NO DEFECTS FOUND. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998121100397 19981211 00397 NM 1998 12 11 PCAA9800787 1 19981014 A 7931 54273618010 INDICATOR DHAV DHC8 DHC8102 2809003 NM COCKPIT FAILED A PCAA A UNSCHED LANDING N FALSE WARNING NR NOT REPORTED 1 EA 13 815EX 129 321 EN ROUTE TO BOS FROM MDT, THE NR 1 ENGINE OIL TEMP WENT OFF SCALE. THE AIRCRAFT RETURNED TO MDT AND LANDED WITHOUT INCI DENT. MAINTENANCE TROUBLESHOT AND FOUND THE TEMP INDICATION AT FAULT. THE OIL TEMP INDICATOR AND BULB WERE REMOVED AND REPLACED. SYSTEM OPERATIONALLY CHECKED GOOD. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998121100398 19981211 00398 1998 12 11 HALA9800321 4 19980913 A 2330 PA SYSTEM DOUG DC10 DC1010 3022110 WP CABIN MALFUNCTIONED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 171AA 46906 SEA - FLT 23 - STATIC INTERFERENCE HEARD FROM OVERHEAD SPEAKER/HEADSET AT WHICH TIME THE NR 1 F/D, NR 1 FMA, AND NR 1 GP S WENT BLANK. AFTER STATIC STOPS, F/D, GPS RETURN TO NORMAL, FMA STAYS BLANK. WHEN MODE TEST SWITCH IS DEPRESSED, FMA RETURNS TO NORMAL. OCCURRED 3 TIMES ON FINAL. UNABLE TO DUPLICATE STATIC ON NR 1 OVERHEAD SPEAKER/HEADSET. OPS CHECK OK ON GROUND. OK FOR SERVICE. (M) 2 L 7 3 4F A22WE 1998121100399 19981211 00399 EU 1998 12 11 C2XA98IA460 1 19981110 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42500 EU CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17448 506 IAH - DURING C-CHECK INSPECTION, FOUND RIGHT SIDE FLIGHT ATTENDANTS SEAT TRACK CORRODED. MAINTENANCE REMOVED AND REPLAC ED THE SEAT TRACK IAW ATR-42 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100400 19981211 00400 EU 1998 12 11 C2XA98BT078 1 19981027 A 2611 FR3222 SMOKE DETECTOR AEROSP ATR72 ATR72212 EU CARGO BAY MALFUNCTIONED A C2XA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 SW 09 69902 385 UPON TAXIING IN TO GATE AREA, CREW REPORTED AFT SMOKE MASTER WARNING INDICATOR REPEATED. MAINTENANCE REMOVED AND REPLAC ED THE AUX AND AFT CARGO COMPARTMENT SMOKE DETECTORS. OPS AND FUNCTIONALLY CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1998121100401 19981211 00401 EU 1998 12 11 C2XA98IA425 1 19981014 A 3211 D58806 SPACER AEROSP ATR42 ATR42320 8680930 EU RT MLG MISSING A C2XA A UNSCHED LANDING W INADEQUATE Q C CL CLIMB 1 SW 09 18814 103 IAH - FLT 3780 - THE CREW REPORTED THE RIGHT MAIN LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED THE RIGHT MAIN LANDING GEAR AND INSTALLED THE AFT TRUNNION PIN SPACER, AND REINSTALLED THE LANDING GEAR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100402 19981211 00402 EU 1998 12 11 C2XA98IA428 1 19981020 A 2121 EVCTA325 FAN AEROSP ATR42 ATR42320 8680930 EU CABIN FROZEN A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 14821 160 HRL - DURING CLIMB-OUT ON FLIGHT 3968, THE CREW REPORTED A STRONG ODOR OF ELECTRICAL SMOKE IN THE COCKPIT AND CABIN. TH E AIRCRAFT RETURNED TO HRL AND LANDED WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE VENT FAN M OTOR TO BE FROZEN. MAINTENANCE PULLED AND COLLARD THE CIRCUIT BREAKER AND PLACED THE FAN ON MEL ATA 21-70-00 CONTROL NU MBER 107072, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100403 19981211 00403 EU 1998 12 11 C2XA98IA426 1 19981016 A 2121 011232500 FAN AEROSP ATR42 ATR42500 EU CABIN INOPERATIVE A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 09 19446 504 IAH - FLT 3934 - THE CREW REPORTED SMOKE IN THE CABIN, THE AIRCRAFT WAS DIVERTED TO VCT AND LANDED WITHOUT INCIDENT. MA INTENANCE REMOVED AND REPLACED THE RIGHT RECIRCULATION FAN IAW ATR-42 MM 21-22-21. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100404 19981211 00404 SO 1998 12 11 C2XA98IA427 1 19981018 A 3230 2050500101 PROX SWITCH EMB 120 EMB120RT SO LT MLG INOPERATIVE A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12703 120084 IAH - FLT 3896, THE CREW REPORTED THE LANDING GEAR WOULD NOT RETRACT, THE AIRCRAFT RETURNED TO LRD AND LANDED WITHOUT IN CIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR DOWN PROXIMITY SWITCH IAW EMB-120 MM 32-01-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1998121100405 19981211 00405 SO 1998 12 11 C2XA98CL070 1 19981030 A 2740 3621001007 CONTROL UNIT EMB 145 EMB145 SO E/E BAY FAILED A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 14942 1959 1049 145037 HPN - FLIGHT 4053 - CREW REPORTED THAT DURING BEFORE TAKEOFF CHECKS THE TAKEOFF CONFIGURATION WARNING SOUNDED FOR 'TRIM' . AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE HORIZONTAL STABILIZE R CONTROL UNIT IAW EMB-145 MM 27-40-01. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT T00011AT 1998121100406 19981211 00406 SO 1998 12 11 C2XA98CL069 1 19981028 A 2750 3075001017 CONTROL UNIT EMB 120 EMB120RT SO TE FLAPS FAILED A C2XA O OTHER O OTHER NR NOT REPORTED 1 SW 09 15732 11560 232 120195 CLE - FLT 3296 - CREW REPORTED THEY RECEIVED MULTIPLE FLAP CONTROL FAULTS IN THE AIR AND ON THE GROUND. MAINTENANCE INS PECTED THE FLAP SYSTEM AND FOUND A FAULTY FLAP CONTROL UNIT. THE CONTROL UNIT WAS REMOVED AND REPLACED IAW EMB-120 MM 2 7-50-06, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1998121100407 19981211 00407 EU 1998 12 11 C2XA98IA453 1 19981029 A 5313 S53070210208 STRINGER AEROSP ATR42 ATR42500 EU BS 28 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16450 510 IAH - DURING C-CHECK INSPECTION, FOUND STRINGER 16 RIGHT TO BE CORRODED AT FRAME 28. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED SECTION OF STRINGER, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121100408 19981211 00408 NM 1998 12 11 AALA982030 1 19981031 A 3350 CONNECTOR BOEING 757 757223 1384957 NM ROW 10D FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 695AN 26975 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE AT SEAT ROW 10D. REPAIRED SHORTED EMERGENC Y EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT ROW 10D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998121100409 19981211 00409 EU 1998 12 11 PLGA981030A 1 19981030 A 3230 D49412001 CONTROL BOX SAAB SF340 340B 7860101 EU MLG MALFUNCTIONED A PLGA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 NE 05 361BE 453 340B290 BOS - FLT 4432 - DURING APPROACH TO BOS, THE LANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. CREW FOLLOWED PROCEDURES A ND EXTENDED THE GEAR USING EMERGENCY PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GE AR CONTROL BOX. SYSTEM TESTED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998121100410 19981211 00410 EU 1998 12 11 USAA980576 1 19981111 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU BS 27526 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 881US 11333 PIT - DURING C-1 CHECK, FOUND TWO 1 INCH HOLES CHAFFED IN SKIN BETWEEN STATION 27526 AND OBLIQUE FRAME NR 16-2. INSTALL ED DOUBLER PER EA 50951. (M) 2 L 7 2 4F RT 1998121100411 19981211 00411 EU 1998 12 11 USAA980575 1 19981111 A 5313 LONGERON FOKKER F28 F28MK0100 4990807 EU BS 27526 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 881US 18369 11333 PIT - DURING C-1 CHECK, FOUND LONGERON CHAFED THROUGH .125 INCH BY .25 INCH AT LONGERON NR 50 CHAFED THROUGH AT STATION 27526. LONGERON DAMAGE CUT OUT, NEW PIECE SPLICED IN PER SRM 51-70-06 PAGE 206. (M) 2 L 7 2 4F RT 1998121100412 19981211 00412 NM 1998 12 11 USAASB98294 1 19981110 A 3350 1000679 LIGHT BOEING 737 7372B7 1384560 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 284AU 23131 ROC - DURING OVERNIGHT CHECK WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM. MAINTENANCE FOUND THE EME RGENCY EXIT SIGN OVER THE AFT RIGHT SERVICED DOOR WOULD NOT ILLUMINATE. MAINTENANCE CHECKED BATTERIES AND LAMPS. CHECK ED GOOD. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK NOW SATISFACTORY. (M) 2 L 7 2 4F A16WE 1998121100413 19981211 00413 NM 1998 12 11 USAA980567 1 19981105 A 5313 146N3110 STRINGER BOEING 757 757225 1384959 NM BS 1436-1456 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 44869 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND HEAVY CORROSION BETWEEN STATION 1436 AND 1456 STRINGER 28R. CORROSION T ASK NR C53-155-02. REPAIRED STRINGER PER SRM 51-40-02 REF EA 62729 AND SRM 51-40-03. (M) 2 L 7 2 4F RT A2NM 1998121100414 19981211 00414 NM 1998 12 11 USAA980569 1 19981105 A 5314 KEEL BEAM BOEING 757 757225 1384959 NM BS 1407 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 44869 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION FOUND A CORRODED KEEL BEAM 1 INCH BY 1 INCH STATION 1407 STRINGER 29R. REMOVED CORROSION AND INSTALLED FREEZE PLUG PER EA 62716A. (M) 2 L 7 2 4F RT A2NM 1998121100415 19981211 00415 NM 1998 12 11 USAA980568 1 19981105 A 5313 STRINGER BOEING 757 757225 1384959 NM BS 1482 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION BS 1482 STRINGER 27R. REMOVED CORR ODED AREA AND FABRICATED NEW STRINGER TIE FITTING PER SRM 51-10-00 PAR 9. (M) 2 L 7 2 4F RT A2NM 1998121100416 19981211 00416 WP 1998 12 11 ASAA9880200 1 19981003 A 5610 LOCK DOUG DC9 DC983 3022083 WP COCKPIT BINDING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 FAI - PRIOR TO DEPARTURE OF FLIGHT 80, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. FREED WINDOW UPPER LOCK MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121100417 19981211 00417 WP 1998 12 11 ASAA9880192 1 19980924 A 5241 DOOR HANDLE DOUG DC9 DC983 3022083 WP GALLEY DOOR MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 964AS 53078 SEA - AFTER ARRIVAL OF FLIGHT 545, CREW REPORTED THE L2 DOOR HANDLE WAS DIFFICULT TO OPERATE. ADJUSTED AND LUBRICATED T HE L2 DOOR HANDLE OPERATING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121100418 19981211 00418 WP 1998 12 11 ASAA9880189 1 19980924 A 5241 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP GALLEY DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 948AS 53021 SEA - DURING MAINTENANCE CEHCK, THE L2 DOOR WOULD NOT LATCH OPEN. ADJUSTED THE DOOR HOLD OPEN LATCH AND OPERATED NORMAL LY. (M) 2 L 7 2 4F RT A6WE 1998121100419 19981211 00419 WP 1998 12 11 ASAA9880188 1 19980923 A 5210 591473027 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP PAX DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 972AS 53448 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WOULD NOT LATCH OPEN. FOUND DOOR HOLD OPEN HOOK PIVOT LINK BENT. REPLACED LINK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121100420 19981211 00420 WP 1998 12 11 ASAA9880194 1 19980928 A 5610 GUIDE DOUG DC9 DC983 3022083 WP COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 975AS 53451 SEA - PRIOR TO DEPARTURE OF FLIGHT 198, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WAS BINDING. ADJUSTED WINDOW UPPER GUIDE MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121100421 19981211 00421 WP 1998 12 11 ASAA9880199 1 19981003 A 5610 LOCK MECH DOUG DC9 DC983 3022083 WP COCKPIT BINDING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 FAI - AFTER ARRIVAL OF FLIGHT 97, CREW REPORTED THE FLIGHT COMPARTMENT RIGHT SLIDING WINDOW WOULD NOT OPEN. LUBRICATED WINDOW UPPER LOCK MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121100422 19981211 00422 WP 1998 12 11 ASAA9880180 1 19980917 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP PAX DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 957AS 49126 SEA - AFTER ARRIVAL OF FLIGHT 435, CREW REPORTED THE L1 DOOR CATCHING AT SEAM. ADJUSTED L1 DOOR BAYONET AND LOCK MECHAN ISMS AND ADJUSTED DOOR HORIZONTAL POSITION AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998121100423 19981211 00423 WP 1998 12 11 ASAA9880178 1 19980916 A 5210 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP PAX DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 SEA - PRIOR TO DEPARTURE OF FLIGHT 288, CREW REPORTED THE L1 DOOR WOULD NOT LATCH OPEN. FOND DOOR HOLD OPEN HOOK BENT, STRAIGHTENED HOOK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121100424 19981211 00424 WP 1998 12 11 ASAA9880174 1 19980911 A 5210 HINGE DOUG DC9 DC982 3022082 WP PAX DOOR LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 955AS 48080 PDX - DURING MAINTENANCE CHECK, THE R1 DOOR HOLD OPEN HOOK WOULD NOT ENGAGE. TIGHTENED LOOSE BOLTS ON DOOR UPPER HINGE FITTING AND ADJUSTED HOLD OPEN HOOK AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998121100425 19981211 00425 NM 1998 12 11 AALA982031 1 19981106 A 3350 CONNECTOR BOEING 767 767323 1385205 NM SEAT 38HJ FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 386AA 27060 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXI TLIGHT AT PAX SEAT 38HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT CONNECTO R AT PAX SEAT 38HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998121100426 19981211 00426 NM 1998 12 11 AALA982032 1 19981107 A 3397 WIRE BOEING 757 757223 1384957 NM ROW 4 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 684AA 25341 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR PATH LIGHT INOPERATIVE FROM OVERWING EXIT ROWS TO PASSENGER SEAT ROW 4. REPAIRED BROKEN EMERGENCY FLOOR LIGHT WIRE AT SEAT ROW 4. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998121100427 19981211 00427 WP 1998 12 11 AALA982084 1 19981117 A 5320 BEAM DOUG DC9 DC982 3022082 WP BS 655 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 442AA 49468 TUL - FORWARD DOOR STOP HOLE ON DOOR BEAM BLENDED BEYOND LIMITS. INSTALLED DOUBLER PER AARD 53-10-00-3. (M) 2 L 7 2 4F A6WE 1998121100428 19981211 00428 WP 1998 12 11 AALA982072 1 19981112 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP BS 237 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 442AA 49468 TUL - FOUND CORROSION ON SEAT TRACK. INSTALLED PLUG REPAIR PER AARD 53-20-00-10. (M) 2 L 7 2 4F A6WE 1998121100429 19981211 00429 WP 1998 12 11 AALA982071 1 19981111 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 1155 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 442AA 49468 TUL - FOUND DEEP SURFACE CORROSION. REMOVED AND REPLACED FITTING. (M) 2 L 7 2 4F A6WE 1998121100430 19981211 00430 WP 1998 12 11 AALA982034 1 19981107 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY CONTAMINATED A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 7544A 53026 DFW - FLT 797 - DURING CLIMB-OUT, A HEAVY ODOR ACCOMPANIED BY BLUE COLORED SMOKE WAS OBSERVED IN THE CABIN. AIRCRAFT AI R INTERRUPTED AND RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE WATER SEPARATOR BAGS SATURATE D WITH DE-ICING FLUID. INSPECTED DUCTS FOR FLUID AND FOUND NO FLUID. REPLACED WATER SEPARATOR BAGS AND RAN APU AND ENG INES AT FULL POWER WITH PACKS ON. PACKS OPERATED NORMALLY AT ALL TEMPERATURE SETTINGS. SYSTEM GROUND CHECKED NORMAL OP ERATION. (M) 2 L 7 2 4F A6WE 1998121100431 19981211 00431 WP 1998 12 11 AALA982015 1 19981030 A 2530 2510000405 OVEN DOUG DC9 DC982 3022082 WP GALLEY DIRTY A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 475AA 49650 DFW - FLT 899 - AFTER TAKEOFF DFW, CREW AND PASSENGERS NOTED A SMOKE SMELL IN AFT CABIN. NO SOURCE COULD BE DETECTED BY CREW. RETURNED DFW AND LANDED WITHOUT INCIDENT. FOUND AFT GALLEY OVEN TO BE CAUSE OF REPORTED SMELL IN CABIN. REPLAC ED AFT GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100432 19981211 00432 NM 1998 12 11 AALA982013 1 19981210 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STRINGER 19R STATION 720D PLUS 13 INCHES THROUGH 720D PLUS 14 INCHES HAS DOUBLE DRILLED HOLE. INSTALLED STR INGER REPAIR PER SRM 53-10-3 PAGE 4E. (M) 2 L 7 3 4F A3WE 1998121100433 19981211 00433 NM 1998 12 11 AALA982012 1 19981201 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 520 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - DEEP GOUGE IN STRINGER 25 LEFT AT STATION 520. CUT OUT DAMAGED AREA OF STRINGER 25L AND INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998121100434 19981211 00434 NM 1998 12 11 ASAA9810118 1 19981115 A 3350 6104781 BATTERY GRIMES BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE FORWARD SEAT PALLET EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BA TTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998121100435 19981211 00435 NM 1998 12 11 ASAA9810117 1 19981109 A 3350 1060091102 LIGHT BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE INTERIOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND TO BE VERY DIM. REPLACED LIGHT ASS EMBLY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100436 19981211 00436 NM 1998 12 11 ASAA9810116 1 19981102 A 3350 1060091102 LIGHT BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE FLIGHT STATION OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY ILLUMINATED WHEN POWER WAS REM OVED FROM THE AIRCRAFT. REPLACED LIGHT ASSEMBLY AND SYSTEM OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100437 19981211 00437 NM 1998 12 11 ASAA9810115 1 19981031 A 3350 BATTERY PACK BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 1-11 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND RECEIVER , AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100438 19981211 00438 NM 1998 12 11 98ZZZM926 1 19981031 A 3350 RECEIVER BOEING 737 737298C 1384490 NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 ANC - DURING MAINTENANCE CHECK, FOUND PALLET 1-11 EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND RECEIVER , AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100439 19981211 00439 NM 1998 12 11 ASAA9810114 1 19981028 A 3350 1060091102 LIGHT GRIMES BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - DURING MAINTENANCE CHECK, THE R2 DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIG HT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998121100440 19981211 00440 NM 1998 12 11 ASAA9810113 1 19981026 A 3350 610478 BATTERY GRIMES BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR LIGHTS WOULD NOT WORK FROM FLIGHT DECK SWITCH. REPLACED RECEIV ER BATTERY AT ROW 3 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100441 19981211 00441 NM 1998 12 11 ASAA9810111 1 19981014 A 3350 883200312 TRANSMITTER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, THE FORWARD EMERGENCY EXIT LIGHT TRANSMITTER WAS FOUND TO BE INOPERATIVE. REPLACED TRAN SMITTER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998121100442 19981211 00442 NM 1998 12 11 ASAA9810110 1 19981013 A 3350 86210144 BATTERY BOEING 737 7372Q8C 138448S NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 741AS 21959 ANC - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIG HT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998121100443 19981211 00443 NM 1998 12 11 ASAA9810108 1 19981009 A 3350 LIGHT BOEING 737 737290C 138448V NM ROW 18 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 JNU - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT AT ROW 18 WS FOUND INOPERATIVE. REPLACED LAMP HOLD ER AND LENS. LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998121100444 19981211 00444 NM 1998 12 11 AALA982025 1 19981103 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 659AA 24617 DFW - DURING OVERNIGHT CHECK, FORWARD EMERGENCY EXIT FLOOR LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FORWARD EMERGENCY EXIT FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998121100445 19981211 00445 NM 1998 12 11 AALA982027 1 19981102 A 3397 WIRE BOEING 757 757223 1384957 NM ROW 6E FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 661AA 25295 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE BETWEEN SEAT ROWS 1E THROUGH 6E. REPAIRED S PLICE AT SEAT ROW 6E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1998121100446 19981211 00446 NM 1998 12 11 ASAA9840107 1 19981117 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 756AS 25097 PDX - DURING MAINTENANCE CHECK THE AFT EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRI NG/LIGHTS AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100447 19981211 00447 NM 1998 12 11 ASAA9840099 1 19981017 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA O OTHER L NO TEST TX TAXI/GRND HDL 1 NM 01 772AS 25105 SEA - PRIOR TO FLIGHT 412, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE DISCONNECTED AND EXPOSED IN THE MID CA BIN AREA. RECONNECTED WIRING TO LIGHT ASSEMBLIES AND REPLACED COVERS, LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100448 19981211 00448 NM 1998 12 11 ASAA9840097 1 19981015 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 PDX - DURING MAINTENANCE CHECK, THE AFT THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECT ED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100449 19981211 00449 NM 1998 12 11 ASAA9840096 1 19981004 A 3397 WIRE BOEING 737 7374Q8 138447Q NM ROW 14 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 JNU - PRIOR TO FLT 76 - FOUR EACH EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AN D LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998121100450 19981211 00450 NM 1998 12 11 ALAA981932 1 19981022 A 5330 SKIN BOEING 727 727223 1384074 NM BS 625 TORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6823 19701 TUL - FOUND 8 INCH DIAGONAL TEAR IN SKIN STATION 625 JUST ABOVE STRINGER 26R, THROUGH SKIN AND BEARSTRAP AT LAP SPLICE. REPAIRED WITH QUADRUPLER PER INTERIM REPAIR ESO 11697 DATED 10-21-98, REPAIRED 26R CUTOUT DAMAGE INSTALLED REPAIR SPLIC E PER 51-40-4. (M) 2 L 7 3 4F A3WE 1998121100451 19981211 00451 NM 1998 12 11 AALA981445 1 19980728 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 344 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 881AA 21520 TUL - FOUND STATION 344 STRINGER 5 RT BACKSIDE OF STRINGER CRACKED TWO PLACES UPPER AND LOWER. CUTOUT DAMAGED AREA. IN STALLED STRINGER REPAIR PER SRM 53-10-3 PAGE 3 THROUGH 4B. (M) 2 L 7 3 4F A3WE 1998121100452 19981211 00452 NM 1998 12 11 AALA984223 1 19981106 A 5230 SKIN BOEING 767 767223 1385123 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 336AA 22334 AFW - BULK CARGO DOOR HAD 5 SMALL AREAS OF CORROSION BLENDED BEYOND SRM LIMITS. REPAIRED IAW MRB 767-1739. (M) 2 L 7 2 4F RT A1NM 1998121100453 19981211 00453 WP 1998 12 11 AALA982068 1 19981111 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 269AA 49292 DFW - DURING MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN AFT CABIN INOPERATIVE. REPLACED EMERGENCY EXIT FL OOR PATH LIGHT STRIP IN AFT CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100454 19981211 00454 WP 1998 12 11 AALA982067 1 19981111 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 228AA 49178 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING AT FIRST CLASS GALLEY INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT STRIP FLAP CONNECTOR AT FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100455 19981211 00455 WP 1998 12 11 AALA982066 1 19981111 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 479AA 49654 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT FORWARD GALLEY INOPERATIVE. REPLACED JUMPER STRIP WIRE FOR EMERGENCY EXIT LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100456 19981211 00456 WP 1998 12 11 AALA982073 1 19981112 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 575AM 53152 DFW - DURING MAINTENANCE, EMERGENCY EXIT LIGHTS BETWEEN FIRST CLASS AND COACH CABIN WERE INOPERATIVE. REPLACED EMERGENC Y EXIT LIGHT JUMPER STRIP BETWEEN FIRST CLASS AND COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100457 19981211 00457 WP 1998 12 11 AALA982035 1 19981109 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 475AA 49650 DFW - DURING MAINTENANCE CHECK, AFT CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT CLASS EMERGENCY EXIT LIGHT STR IP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100458 19981211 00458 WP 1998 12 11 AALA982028 1 19981104 A 3350 L201011 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 568AA 49349 DTW - DURING OVERNIGHT MAINTENANCE, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REPLACED FORWARD ENTR Y DOOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A6WE 1998121100459 19981211 00459 NM 1998 12 11 AALA982017 1 19981031 A 2121 732591D FAN BOEING 767 767323 1385205 NM E/E BAY FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 362AA 805 24043 LHR - FLT 104 - DURING CRUISE, FLIGHT ATTENDANT NOTED A ELECTRICAL BURNING SMELL IN THE FORWARD CABIN AND AN UNUSUAL NOI SE FROM SEAT ROW 2HJ. AIRCRAFT LANDED LHR WITHOUT INCIDENT. MAINTENANCE FOUND THE EQUIPMENT COOLING FAN OVERHEATING. R EPLACED EQUIPMENT COOLING FAN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1998121100460 19981211 00460 WP 1998 12 11 AALA982081 1 19981115 A 2130 7124951 FLEX CONNECTOR DOUG DC9 DC982 3022082 WP ACM BAY TORN A AALA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 408AA 49319 DFW - FLT 1022 - EN ROUTE BUR-DFW, DURING CRUISE AT 24,000 FT, CABIN SUPPLY TEMPERATURE WENT FULL HOT. FLOW LIGHT ILLUM INATED, RIGHT SUPPLY PRESSURE WENT TO ZERO. CABIN PRESSURE BEGAN CLIMBING. AIRCRAFT IN DESCENT, CABIN CONTINUED CLIMBI NG AT 7,500 FT. CREW WENT MANUAL AND VERIFIED THE FLOW VALVE WAS CLOSED. CABIN CONTINUED TO CLIMB THROUGH 10,000 FT. C REW DROPPED THE MASKS AND LANDED DFW WITHOUT FURTHER INCIDENT. REPLACED WATER SEPARATOR INLET BOOT AND OXYGEN MASKS. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100461 19981211 00461 WP 1998 12 11 AALA982080 1 19981116 A 3233 39370335503 BUNGEE DOUG DC9 DC982 3022082 WP LT MLG MALFUNCTIONED A AALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SW 07 407AA CPT0612 49318 ORD - FLT 2240 - AFTER TAKEOFF DFW EN ROUTE ORD, LEFT GEAR RED LIGHT AND GEAR DOOR OPEN LIGHTS REMAINED ILLUMINATED WHEN GEAR RETRACTED. VIBRATION AND PERFORMANCE CONFIRMED THAT LEFT GEAR REMAINED EXTENDED. CYCLING GEAR PER OPERATION MANU AL DID NOT HELP. NORMAL GEAR DOWN INDICATIONS WITH GEAR EXTENDED. LANDED ORD WITHOUT INCIDENT. REPLACED LEFT MLG BUNG EE PER MM. OPERATIONS AND LEAK CHECKS GOOD. SYSTEM GROUND CHECED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1998121100462 19981211 00462 EU 1998 12 11 AALA982014 1 19981027 A 3260 880501 SENSOR ELDEC FOKKER F28 F28MK0100 4990807 EU LT MLG FAILED A AALA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 1452B 11464 IAH - FLT 1399 - DURING CRUISE, LEFT MAIN GEAR DOWN LOCK SWITCH MESSAGE WAS INTERMITTENT ON MFDU. AIRCRAFT LANDED IAH W ITHOUT FURTHER INCIDENT. FOUND NR 2 DOOR LOCK SENSOR FAULTY. REPLACED NR 2 DOOR LOCK SENSOR AND ACCOMPLISHED PROXIMITY CHECK. SWUNG GEAR SEVERAL TIMES WITH NORMAL OPERATION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1998121100463 19981211 00463 WP 1998 12 11 ASAA9880213 1 19981028 A 5210 4928806501 HOLD OPEN HOOK DOUG DC9 DC983 3022083 WP PAX DOOR BENT A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 974AS 53450 SEA - PRIOR TO DEPARTURE OF FLIGHT 318, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO OPEN AND HOLD OPEN LATCH WOULD NOT LI NE UP. REPLACED DOOR HOLD OPEN HOOK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121100464 19981211 00464 WP 1998 12 11 ZIAA98040 1 19981023 A 2612 FIRE LOOP LKHEED 188 188A 5262602 WP NR 4 ENGINE MALFUNCTIONED A ZIAA E F A ENGINE SHUTDOWN ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CR CRUISE 1 GL 23 5512 188A1017 MEM - SHUTDOWN NR 4 ENGINE DUE TO FIRE WARNING IN ZONES 2/3 AT 1811Z. FIRED BOTTLE AND LIGHTS WENT OUT. AT 1838Z FIRE WARNING IN ZONES 2/3, ENGINE NR 4 CAME ON AGAIN. FIRED SECOND BOTTLE AND WARNING REMAINED ON. DIVERTED TO MEM. REMOVE D AND REPLACED NR 3/4 BOTTLES AND SQUIBBS. PREPARED AIRCRAFT FOR THREE ENGINE FERRY. REMOVED AND REPLACED ZONE 2 LOOP AND CLEANED ZONE 3 CONNECTOR. OPERATIONAL CHECK GOOD IAW L-188 MM 26-1-0. (M) 2 L 7 4 4T RT 4A22 1998121100465 19981211 00465 NM 1998 12 11 AALA982050 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680-690 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION ON FUSELAGE SKIN OUTBOARD SIDE OF STRINGER 28R, STATION 680-690. INSTALLED EXTERNAL DOUBLER PER S RM 53-30-3 .063 2024 PLUS 3, 21 INCHES BY 11 INCHES. (M) 2 L 7 3 4F A3WE 1998121100466 19981211 00466 NM 1998 12 11 AALA982049 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION AROUND LEFT ICE LIGHT STATION 720B-720C BETWEEN STRINGER 16 LEFT AND 19 LEFT. PERFORMED FUSELAGE SKIN REPAIR AT LEFT WING SCANNING LIGHT CUTOUT PER SRM 53-30-3, ALODINED AND PRIMED PER MM 51-20-0. (M) 2 L 7 3 4F A3WE 1998121100467 19981211 00467 NM 1998 12 11 AALA982048 1 19981104 A 5311 FRAME BOEING 727 727223 1384074 NM BS 375 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION ON BELL FRAME AT STATION 375 RIGHT WL 209.1 JUST ABOVE FLOOR LEVEL. CUT OUT DAMAGE INSTALLED TYPI CAL FORMED SECTION. REPAIR PER SRM 51-40-3 FIG 1 SHEET 3, L-ANGLE DOUBLER 7075 T-6 .090, 1.375 INCH BY 2 INCH BY 8.75 I NCH, 29 HI-LOCKS TOTAL .1875 INCH DIAMETER. (M) 2 L 7 3 4F A3WE 1998121100468 19981211 00468 NM 1998 12 11 AALA982047 1 19981026 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - AFT SIDE OF SHEAR TIE IS CORRODED. REPLACED SHEAR TIE STRINGER 28L-29L, STATION 1166. (M) 2 L 7 3 4F A3WE 1998121100469 19981211 00469 NM 1998 12 11 AALA982046 1 19981104 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 600 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - BELLFRAME SHEAR TIE CRACKED AND DEFORMED STA 600 ABOVE STRINGER 16R. REPAIRED SHEAR TIE PER SRM 53-10-4 AND SKIN PER 53-30-3. (M) 2 L 7 3 4F A3WE 1998121100470 19981211 00470 NM 1998 12 11 AALA982045 1 19981104 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1050 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION FLOORBEAM STATION 1050 LB 10 TO LB 55. REMOVED CORROSION, CUTOUT, BEYOND LIMITS, AREA AND INSTAL LED REPAIR PER SRM 53-10-8 PAGE 9A AND 9B. (M) 2 L 7 3 4F A3WE 1998121100471 19981211 00471 NM 1998 12 11 AALA982044 1 19981104 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 FOUND CORROSION ON UNDERSIDE BS 1110 FLOORBEAM UPPER CHORD ADJ TO FASTENER COVERED BY GALLEY. INSTALLED FLOORBEAM REPAI R PER SRM 53-10-8 PAGE 9E. (M) 2 L 7 3 4F A3WE 1998121100472 19981211 00472 NM 1998 12 11 AALA982043 1 19981104 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND STRINGER 15R CRACKED FORWARD OF ICE LIGHT AT STATION 720B PLUS 4 INCHES. REPAIRED CRACKED STRINGER IAW SRM 53-10-3 PAGE 3-4B. (M) 2 L 7 3 4F A3WE 1998121100473 19981211 00473 NM 1998 12 11 AALA982042 1 19981104 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 344 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND STRINGER 5 RT CRACKED IN TWO PLACES UPPER FLANGES WHERE CLIP ATTACHES STATION 344. STOP DRILLED CRACKS AND INSTALLED DOUBLERS PER SRM 53-10-3 PAGE 4C-6. (M) 2 L 7 3 4F A3WE 1998121100474 19981211 00474 NM 1998 12 11 AALA982041 1 19981021 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CRACK AT END OF STRINGER LAST RIVIT. CUT OUT BAD SECTION OF STRINGER AND SPLICED IN NEW SECTION PER SRM 53- 10-3 FIG 5 ESO 11697. (M) 2 L 7 3 4F A3WE 1998121100475 19981211 00475 NM 1998 12 11 AALA982040 1 19981013 A 5320 WEB BOEING 727 727223 1384074 NM BS 351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND STATION 351 HAS CORROSION AROUND SEVERAL FASTENERS AT LOWER END OF WEB, FORWARD SIDE. REPAIRED WEB IAW ESO 11697 AND SRM 53-10-9. ENGINEER APPROVED ACCEPTABLE TO NT TRIM OUT BLEND AREA. (M) 2 L 7 3 4F A3WE 1998121100476 19981211 00476 NM 1998 12 11 AALA982039 1 19981104 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 687 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION INSIDE STRINGER CHANNEL BETWEEN RIVITS. INSTALLED STRINGER SPLICE SAME AS ORIGINAL MATERIAL PRODU CTION SPLICE EXCEPT EXTENDED THE SAME NR FASTENERS PAST DAMAGE PER ESO 11697 DATED 10/15/98. (M) 2 L 7 3 4F A3WE 1998121100477 19981211 00477 NM 1998 12 11 AALA982038 1 19981104 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION ON FLOORBEAM AT STATION 1070, BL 0 - LBL 22. REMOVED CORRODED UPPER PORTION OF FLOORBEAM AND INST ALLED FLOORBEAM REPAIR PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998121100478 19981211 00478 NM 1998 12 11 AALA982037 1 19981104 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION ON OUTSIDE OF STRINGER 29L STATION 950A TO 970. REMOVED CORROSION AND INSTALLED .071, 7075-T6 REP AIR STRAP PER ECO 11697 DATED 10-14-98. (M) 2 L 7 3 4F A3WE 1998121100479 19981211 00479 NE 1998 12 11 AALA982083 2 19981117 A 7250 840001 TURBINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 1 ENGINE FAILED A AALA A E J UNSCHED LANDING ENGINE SHUTDOWN DUMP FUEL R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 SW 07 722AA 20730 666101 MIA - FLT T1301 - EN ROUTE MIA/EWR AFTER TAKEOFF ABOUT 1,600 FEET LOST POWER, DUMPED FUEL, AND RETURNED AND LANDED MIA W ITHOUT FURTHER INCIDENT. REPLACED NR 1 ENGINE, PERFORMED ENGINE RUN-UP, AND LEAK CHECKED. SYSTEM GROUND CHECKED NORMAL OPERATION. SHOP FINDINGS: THE ENGINE (SN 666101) WAS SHUT DOWN DUE TO TURBINE FAILURE. CONFIRMED SOURCE OF FAILURE W AS CAUSED BY TWO FIRST STAGE TURBINE BLADES. THE TWO EACH BLADES EXPERIENCED INCREASED RATE OF CREEP AND SUBSEQUENT STR ESS RUPTURE ACROSS THE SPAN OF THE BLADE. (X) 2 L 7 3 4F 4 F A3WE E2EA 1998121100480 19981211 00480 NE 1998 12 11 AALA982076 2 19981114 A 7250 TURBINE BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE NR 2 ENGINE FAILED A AALA E A ENGINE SHUTDOWN UNSCHED LANDING J M WARNING INDICATION OVER TEMP CL CLIMB 1 SW 07 726AA 20733 MIA - FLT 1301 - AFTER TAKEOFF MIA, NR 2 ENGINE WAS SHUT DOWN BY CREW DUE TO HIGH ENGINE EXHAUST GAS TEMPERATURE AND VIB RATION. CREW DECLARED AN EMERGENCY, RETURNED AND LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED NR 2 ENGINE. SOURCE OF HIGH EGT WAS CAUSED BY FAILURE OF 1ST STAGE TURBINE BLADE DUE TO CREEP AND STRESS RUPTURE. BLADE EVALUATION INDICATES OVERTEMP AT THE BLADE 1/2 AND 3/4 SPAN. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998121100481 19981211 00481 EU 1998 12 11 PLGA981111A 1 19981111 A 2910 3268 VALVE SAAB SF340 SF340A 7850100 EU HYDRAULIC SYSTEM MALFUNCTIONED A PLGA O OTHER J WARNING INDICATION AP APPROACH 1 NE 05 340BE 314 340A062 LGA - FLT 4541 - DURING APPROACH, CREW NOTICED MAIN AND EMERGENCY HYDRAULIC PRESSURE STARTED TO DROP. LANDING GEAR WAS EXTENDED USING EMERGENCY PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DUMP VALVE ON MAIN AND EMERGE NCY ACCUMULATOR HAD FAILED. BOTH DUMP VALVES WERE REPLACED. SYSTEM CHECKED GOOD. EMERGENCY VALVE P/N 3268, S/N 315. ( M) 2 L 7 2 4T RT A52EU 1998121100482 19981211 00482 EU 1998 12 11 PLGA981011A 1 19981011 A 2910 AE7064585 LINE SAAB SF340 340B 7860101 EU NLG RUPTURED A PLGA L ABORTED APPROACH K FLUID LOSS AP APPROACH 1 NE 05 365BE 4Q91DOM 340B299 BOS - FLT 4482 - AFTER LANDING GEAR WAS SELECTED DOWN FOR LANDING AT BOS, THE HYDRAULIC QUANTITY INDICATOR WENT TO ZERO AND THE HYDRAULIC WARNING ILLUMINATED. THE AIRCRAFT LANDED WITH FLAPS UP WITHOUT INCIDENT. MAINTENANCE FOUND THE NOSE GEAR RETRACT ACTUATOR HYDRAULIC LINE RUPTURED. LINE WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998121100483 19981211 00483 EU 1998 12 11 PLGA981016A 1 19981016 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 SF340A 7850100 EU CARGO BAY CONTAMINATED A PLGA F ACTIVATE FIRE EXT. N FALSE WARNING DE DESCENT 1 NE 05 340BE A2529 340A062 BTV - FLT 4221 - DURING DESCENT INTO BTV, THE CARGO COMPARTMENT SMOKE WARNING LIGHT ILLUMINATED. THE CREW FOLLOWED PROC EDURES AND DISCHARGED THE FIRE EXTINGUISHER BOTTLE. THE WARNING LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO BTV AND LAND ED WITHOUT INCIDENT. MAINTENANCE FOUND NO INDICATION OF FIRE OR SMOKE IN CARGO AREA. BOTH SMOKE DETECTORS WAS REPLACED ALONG WITH EXTINGUISHER BOTTLE. AIRCRAFT RETURNED TO SERVICE. DETECTOR P/N 72-111211-000, S/N A4370/9137. (M) 2 L 7 2 4T RT A52EU 1998121100484 19981211 00484 1998 12 11 PLGA981007A 4 19981007 A 2340 INTERCOM SAAB SF340 SF340A 7850100 EU COCKPIT FAILED A PLGA A UNSCHED LANDING O OTHER CL CLIMB 1 NE 05 346BE 340A150 BOS - FLT 4232 - DURING TAKEOFF ROLL, THE COCKPIT INTERCOM SYSTEM FAILED WHICH CUT COMMUNICATION BETWEEN THE CREW AS 'V' SPEEDS WERE CALLED OUT. THE AIRCRAFT WAS ROTATED AT 150 KTS WHICH WAS 14 KTS ABOVE MAXIMUM TIRE SPEED. AIRCRAFT RETUR NED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED TIRES USING MANUFACTURE DATA AND FOUND TO BE GOOD FOR CON TINUED SERVICE. (M) 2 L 7 2 4T RT A52EU 1998121100485 19981211 00485 NM 1998 12 11 AALA984214 1 19981030 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 852-933 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 338AA 22335 AFW - FLOORBEAMS AT LT AND RT BL 11 HAVE CORROSION REMOVAL ON UPPER SURFACE STATION 933. ROTO PEEN BLENDED AREA, ALODIN E BEFORE PRIMER, APPLIED TWO COATS PRIMER. FILL BLENDS WITH BMS5-95. (M) 2 L 7 2 4F RT A1NM 1998121100486 19981211 00486 NM 1998 12 11 AALA984184 1 19981103 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 338AA 22335 AFW - FLOORBEAM AT STATINO 325 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINED AREA, FABRICATED STRAP FROM .050 301.5 HARD STAINLESS STEEL. ATTACHED STRAP USING BACB30NW6 HI-LOCKS. APPLIED TWO COATS PRIMER TO STRAP AND FLOORBEAM. (M) 2 L 7 2 4F RT A1NM 1998121100487 19981211 00487 NM 1998 12 11 AALA984222 1 19981109 A 5320 SUPPORT BOEING 767 767223 1385123 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 336AA 22334 AFW - VERY FORWARD VERTICAL LEG OF L-2 DOOR FLOOR SUPPORT TEE (SPLASH GUARD) AT STATION 1480, HAD CORROSION BLEND BEYOND SRM LIMITS. REFER TO ATTACHED FIGURE, BLEND OUT CORROSION, ALODINED AND APPLY TWO COATS OF PRIMER. (M) 2 L 7 2 4F RT A1NM 1998121100488 19981211 00488 NM 1998 12 11 AALA984221 1 19981109 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 336AA 22334 AFW - FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINE BLENDED AREA FABRICATE STRAP APPLY TWO C OATS PRIMER FILL BLENDED AREA INSTALL STRAP WET. (M) 2 L 7 2 4F RT A1NM 1998121100489 19981211 00489 NM 1998 12 11 AALA984220 1 19981109 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 336AA 22334 AFW - FLOORBEAM AT STATION 287 HAS CORROSION REMOVAL ON UPPER SURFACE. ALODINE BLENDED AREA FABRICATE STRAP APPLY TWO C OATS PRIMER. INSTALL STRAP WET WITH SEALANT. (M) 2 L 7 2 4F RT A1NM 1998121100490 19981211 00490 NM 1998 12 11 AALA984225 1 19981106 A 5730 SKIN BOEING 767 767223 1385123 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 336AA 22334 AFW - FOUND CENTER WING UPPER SKIN HAD CORROSION BLENDED BEYOND SRM LIMITS, AT STATION 955 RBL 71. REPAIRED IAW MRB 767 -1735. (M) 2 L 7 2 4F RT A1NM 1998121100491 19981211 00491 NM 1998 12 11 AALA982065 1 19981104 A 5530 STRAP BOEING 727 727223 1384074 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND CORROSION ON HORIZ STAB REAR UPPER SRM FAIL/SAFE STRAP RIGHT SIDE. REPAIRED PER ESO 11697, DATED 10/15/98. (M) 2 L 7 3 4F A3WE 1998121100492 19981211 00492 NM 1998 12 11 AALA982064 1 19981104 A 5512 SKIN BOEING 727 727223 1384074 NM HORIZ STABILIZER DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - DEEP LIGHTNING BURN ON HORIZ STAB (LT) REAR SPAR AND SKIN. BLENDED SPAR AND REPAIRED PER SRM 55-10-3. (M) 2 L 7 3 4F A3WE 1998121100493 19981211 00493 NM 1998 12 11 AALA982063 1 19981104 A 5511 SPAR BOEING 727 727223 1384074 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - HORIZ STABILIZER FRONT SPAR CENTER SECTION RIGHT UPPER 'A' FRAME MOUNT LUGS AND LOWER 'A' FRAME MOUNT LUGS CORRODE D. REPAIRED PER ESO 11697 DATED 10/15/98. (M) 2 L 7 3 4F A3WE 1998121100494 19981211 00494 NM 1998 12 11 AALA982062 1 19981104 A 5531 SPAR BOEING 727 727223 1384074 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - HORIZ STABILIZER FRONT SPAR CENTER SECTION LEFT UPPER AND LEFT LOWER 'A' FRAME ATTACH LUGS CORRODED. REPAIRED PER ESO 11697, DATED 10/15/98. (M) 2 L 7 3 4F A3WE 1998121100495 19981211 00495 NM 1998 12 11 AALA982060 1 19981104 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680-683 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND 28R STRINGER FORWARD OF STATION 690 FOUND TO BE CORRODED. FABRICATED NEW STRINGER SPLICE EXTENDED TO PICK U P SAME NUMBER OF FASTENERS PAST DAMAGE CUTOUT PER ESO 11697, DATED 10/21/98. (M) 2 L 7 3 4F A3WE 1998121100496 19981211 00496 NM 1998 12 11 AALA982059 1 19981104 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 686 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND STRINGER AFT OF VENT TOP OF TANK CRACKED AT STATION 686.50. INSTALLED REPAIR PER BOEING S/B 727-57-A155. ( M) 2 L 7 3 4F A3WE 1998121100497 19981211 00497 NM 1998 12 11 AALA982058 1 19981104 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 340-344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND STATION 340-344 RIGHT SKATE ANGLE HAS CORROSION, FOUND UNDER LEVELING COMPOUND WHICH WAS REMOVED TO ACCOMPLI SH WORK ON E58 NR 2736701. REMOVAL OF CORROSION WAS BEYOND LIMITS, INSTALLED 12.75 INCH LONG 'L' ANGLE REPAIR PER ESO 1 1697, DATED 14 OCT 98 OVER FLANGE OF CHORD AT STATION 377-350 RIGHT SIDE. (M) 2 L 7 3 4F A3WE 1998121100498 19981211 00498 NM 1998 12 11 AALA982057 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 834 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND LOWER WING SKIN CORRODED ABOVE RIGHT PRIMARY HEAT EXCHANGER STATION 834 RBL 30. REMOVED CORROSION, REMOVED NECESSARY FASTENERS, CLEANED, TREATED, PREPARED AREA AND INSTALLED DOUBLER PER SRM 57-30-3, SEALED AREA WITH 1422A/B. ( M) 2 L 7 3 4F A3WE 1998121100499 19981211 00499 NM 1998 12 11 AALA982056 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1148-1150 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND INNER SKIN CORRODED JUST ABOVE STRINGER 26R, STATION 1148-1150. INSTALLED DOUBLER REPAIR PER SRM 53-30-3. ( M) 2 L 7 3 4F A3WE 1998121100500 19981211 00500 NM 1998 12 11 AALA982055 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1083 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - DEEP GOUGE IN SKIN STRINGER 174. BLENDED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 4. (M) 2 L 7 3 4F A3WE 1998121100501 19981211 00501 NM 1998 12 11 AALA982054 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1082 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - BULGE IN SKIN AT STRINGER 18L. CUT OUT BULGED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 4. (M) 2 L 7 3 4F A3WE 1998121100502 19981211 00502 NM 1998 12 11 AALA982053 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1080 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - DENT IN SKIN STATION 1080 STRINGER 19L. CUTOUT DENTED AREA AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 4. (M) 2 L 7 3 4F A3WE 1998121100503 19981211 00503 NM 1998 12 11 AALA982052 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM BS 415 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND INNER SURFACE OF SKIN GOUGED STATION 415 BELOW STRINGER 9 LEFT. BLENDED GOUGE AND INSTALLED DOUBLER PER SRM 53-30-1 PAGES 1-8. (M) 2 L 7 3 4F A3WE 1998121100504 19981211 00504 NM 1998 12 11 AALA982051 1 19981104 A 5330 SKIN BOEING 727 727223 1384074 NM FUSELAGE GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - FOUND DEEP GOUGE IN FUSE SKIN AT AFT LOWER CORNER OF LEFT AFT GALLEY DOOR CUTOUT. BLENDED AREA AND INSTALLED DOUB LER PER 53-30-3 FIG 4. (M) 2 L 7 3 4F A3WE 1998121100505 19981211 00505 NM 1998 12 11 AALA982003 1 19981028 A 5240 SKIN BOEING 727 727227 1384078 NM SERVICE DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 730AA 20737 TUL - RIGHT AFT SERVICE DOOR FRAME SKIN HAS HEAVY CORROSION AT APPROX 56 INCHES ABOVE FLOOR LINE. REPAIRED WITH EXTERNA L FUSELAGE DOUBLER AND TRIPLER PER ESO 11697, DATED 10/20/98. (M) 2 L 7 3 4F A3WE 1998121100506 19981211 00506 NM 1998 12 11 AALA982004 1 19981028 A 5311 FRAME BOEING 727 727227 1384078 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 730AA 20737 TUL - LEFT SIDE BELTFRAME DENTED AND BULGED ON SIDES AT STATION 680 BETWEEN STRINGER 22L AND 23L. REMOVED DAMAGED AREA OF FRAME AT STATION 680 LEFT BETWEEN STRINGER 22L AND 23L AND INSTALLED DOUBLER PER SRM 51-40-3 PAGE 2. (M) 2 L 7 3 4F A3WE 1998121100507 19981211 00507 NM 1998 12 11 AALA982005 1 19981028 A 5311 FRAME BOEING 727 727227 1384078 NM BS 913 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 730AA 20737 TUL - FOUND CRACK IN RADIUS AT OUTER FLANGE OF LEFT STATION 913.5 FRAME. STOP DRILLED CRACK AND INSTALLED REPAIR PER SR M 53-10-2 FIG 3. (M) 2 L 7 3 4F A3WE 1998121100508 19981211 00508 NM 1998 12 11 AALA981933 1 19981016 A 5311 FRAME BOEING 727 727227 1384078 NM BS 560 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 717AA 20610 TUL - FOUND FS 560 FRAME WEB CRACKED AT NR 2 AND NR 3 DOOR STOP ATTACH HOLES. CUTOUT FRAME WEB FROM STRINGER 24R TO STR INGER 21R 20 INCH OVERALL, SPLICED REPLACEMENT WEB PER TYPICAL WEB REPAIR SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998121100509 19981211 00509 NM 1998 12 11 AALA981963 1 19980929 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - BELLFRAME DENTED TOP SIDE, RADIUS AND INTO WEB STATION 660 STRINGER 20L AREA. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 51-40-3 USING .050, 7075-T6 MATERIAL WITH .1875 BUTTON HEAD AND COUNTERSUNK 'D' RIVETS. (M) 2 L 7 3 4F A3WE 1998121100510 19981211 00510 NM 1998 12 11 AALA981964 1 19980929 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - BELLFRAME DENTED TOPSIDE, RADIUS AND INTO WEB STATION 660 STRINGER 22L AREA. REMOVED DAMAGED AREA AND INSTALLED R EPAIR PER SRM 51-40-3, USING .050 7075-T6 MATERIAL WITH .1875 BUTTON HEAD AND COUNTERSUNK 'D' RIVETS. (M) 2 L 7 3 4F A3WE 1998121100511 19981211 00511 NM 1998 12 11 AALA981965 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - BELLFRAME DENTED STATION 520 TOP SIDE INTO RADIUS, WEB STRINGER 22 AREA. REMOVED DAMAGED AREA AND INSTALLED REPAI R, SRM 51-40-3 .050 7075-T6, REPAIR MATERILA AND .1875 FLUSH AND PAN 'D' RIVETS. (M) 2 L 7 3 4F A3WE 1998121100512 19981211 00512 NM 1998 12 11 AALA981966 1 19981001 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - BELLFRAME DENTED TOPSIDE FORWARD RADIUS STATION 660 STRINGER 24R. REMOVED DAMAGE AREA AND INSTALLED REPAIR PER SR M 51-40-3 USING .050, 7075-T6 MATERIAL WITH .1875 BUTTON HEAD AND COUNTERSUNK 'D' RIVETS. (M) 2 L 7 3 4F A3WE 1998121100513 19981211 00513 NM 1998 12 11 AALA981943 1 19981015 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1050-1070 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND STATION 1050-1070 STRINGER 28R SKIN IS BULGING. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER FOR SKIN CUTOUT IAW SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1998121100514 19981211 00514 NM 1998 12 11 AALA981942 1 19981015 A 5330 SKIN BOEING 727 727223 1384074 NM BS 500-502 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND SKIN CORRODED UNDER LEVELING COMPOUND STATION 500-502, STRINGER 26-27L. REPAIRED AND INSTALLED DOUBLER AT S TATION 500-502, STRINGER 26L TO 27L PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998121100515 19981211 00515 NM 1998 12 11 AALA981941 1 19981015 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 640-721 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND CORROSION AROUND RIVETS STRINGER 28R, 640-660, 685-690, 710-721. REMOVED CORRODED STRINGER AND INSTALLED FI LLER AND SPLICE AT STATION 28R BETWEEN STATION 640 AND 721. (M) 2 L 7 3 4F A3WE 1998121100516 19981211 00516 NM 1998 12 11 AALA981940 1 19981015 A 5330 SKIN BOEING 727 727223 1384074 NM BS 690-700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND CORROSION ON SKIN AND AROUND FASTENERS STRINGER 27L, STATION 690-700. INSTALLED DOUBLER REPAIR PER SRM 53-3 0-5. INSTALLED INTERCOSTALS AND TRANSITION PANEL. (M) 2 L 7 3 4F A3WE 1998121100517 19981211 00517 NM 1998 12 11 AALA981939 1 19981013 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 702 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND CORROSION IN BOTTOM OF STRINGER AT NUT PLATE STATION 702. CUT OUT DAMAGED AREA OF STRINGER. INSTALLED REP AIR SPLICE AND FILLER IAW SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998121100518 19981211 00518 NM 1998 12 11 AALA981938 1 19981015 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1012 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND STATION 1012 STRINGER 29R HAS SKIN BULGING AROUND FASTENERS. INSTALLED NEW STRINGER SECTION AND SPLICE AS P ER SRM 53-10-3 FIG 1, STRINGER SECTION BAC 1498-147. INSTALLED STATION 1011-1021. TEN INCHES OF BAC1498-131 REPAIR MAT ERIAL INSTALLED WITH FIVE FASTENERS EACH SIDE OF DAMAGE. .1875 1ST OVER HI-LOCKS USED THROUGHOUT REPAIR. (M) 2 L 7 3 4F A3WE 1998121100519 19981211 00519 NM 1998 12 11 AALA981937 1 19981015 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 504-506 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND CORROSION ON BOTTOM OF STRINGER 27L STATION 504-506. CUT OUT CORRODED SECTION OF STRINGER. INSTALLED STRIN GER REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998121100520 19981211 00520 NM 1998 12 11 AALA981936 1 19981015 A 5330 SKIN BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - CORROSION ON INSIDE OF SKIN WHERE LEVELING COMPOUND REMOVED STATION 580, STRINGER 28L ABOUT 1.5 INCHES DIAMETER. C UT OUT CORROSION, INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998121100521 19981211 00521 NM 1998 12 11 AALA981935 1 19981015 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - BELLFRAME DENTED STATION 720A, STRINGER 25R. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3 FIG 1 WITH .187 5 AND .25 INCH HI-LOCKS FASTENERS PAST DAMAGE DOUBLER THICKNESS .067. (M) 2 L 7 3 4F A3WE 1998121100522 19981211 00522 NM 1998 12 11 AALA981934 1 19981015 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 303-312 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 706AA 22463 TUL - FOUND BELOW FORWARD ENTRY DOOR FLOORBOARD BETWEEN FLOORBEAM STATION 312 AND 303, LBL 48, SUPPORT ANGLE CRACKED. R EPLACED SUPPORT ANGLE. (M) 2 L 7 3 4F A3WE 1998121100523 19981211 00523 NM 1998 12 11 AALA984216 1 19981106 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 875 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 336AA 22334 AFW - FLOORBEAM RBL 11 AND STATION 875 HAD A WEAR MARK AND LIGHT CORROSION BLENDED BEYOND LIMITS. BLEND OUT CORROSION, ROTO-PEEN AREA. ALODINE AND APPLY TWO COATS OF PRIMER AND FILL WITH SEALANT. (M) 2 L 7 2 4F RT A1NM 1998121100524 19981211 00524 NM 1998 12 11 AALA984215 1 19981106 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 336AA 22334 AFW - FLOORBEAM AT STATION 325 HAS CORROSION REMOVAL ON UPPER AND LOWER SURFACE. ALODINE BLENDED AREA, FABRICATED STRAP . APPLY TWO COATS PRIMER, INSTALL STRAP WET WITH SEALANT. (M) 2 L 7 2 4F RT A1NM 1998121100525 19981211 00525 NM 1998 12 11 UIEA9808 1 19981030 A 5210 CAM BOEING 747 747230B 1384889 NM PAX DOOR BROKEN A UIEA I J A CABIN DEPRESSURIZATION DUMP FUEL UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 15 508MC 21644 FLT 1327 - ATB - ANC - AFTER TAEKOFF, DOOR OPEN L-1 LIGHT CAME ON. AIRCRAFT DEPRESSURIZATION CHECKLIST COMPLETED. ABOR TED FLIGHT, FUEL DUMP CHECKLIST COMPLETED. LANDING UNEVENTFUL. AFTER LANDING, MAINTENANCE FOUND UPPER AFT CRANK ROLLER CAM BROKEN ON L1 MAIN ENTRY DOOR. EO 4752A017 ISSUED FOR ONE TIME FLIGHT FROM ANC TO TPE. TPE MAINTENANCE REPLACED L1 MAIN ENTRY DOOR UPPER AFT CRANK ROLLER CAM ASSY. DOOR OPERATIONAL CHECKS PER MM 52-11-07 NORMAL. (M) 2 L 7 4 4F A20WE 1998121100526 19981211 00526 NE 1998 12 11 98ZZZM927 2 19980328 A 7510 POPPET VALVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 ENGINE FAILED A A6WA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 GL 31 606AW E2033 NR 4 ENGINE READS 7 PERCENT BELOW N1 REF AT 904 DEGREES TGT, ABORTED TAKEOFF AT LESS THAN 60 KTS, RETURNED TO GATE AT DE N. REPLACED FCU POPPET VALVE ASY. ENGINE STILL LOW ON POWER. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1998121100528 19981211 00528 EU 1998 12 11 USAAF98081 1 19980927 A 2761 D43812419 SENSOR FOKKER F28 F28MK0100 4990807 EU DRAG CONTROL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 893US 11373 BOS - FLT 2162 - 'LIFTDUMP UNSAFE' MESSAGE ILLUMINATED ON CLIMB-OUT FROM BOS. THE FLIGHT CONTROLS FELT HEAVY AND ASYMME TRIC. THE FLIGHT RETURNED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 AND 3 INLOCK SENSO RS AND RIGGED AS NECESSARY. (M) 2 L 7 2 4F RT 1998121100529 19981211 00529 EU 1998 12 11 98ZZZM929 1 19980927 A 2761 D43812405 SENSOR FOKKER F28 F28MK0100 4990807 EU DRAG CONTROL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 893US 11373 BOS - FLT 2162 - 'LIFTDUMP UNSAFE' MESSAGE ILLUMINATED ON CLIMB-OUT FROM BOS. THE FLIGHT CONTROLS FELT HEAVY AND ASYMME TRIC. THE FLIGHT RETURNED TO BOS AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 AND 3 INLOCK SENSO RS AND RIGGED AS NECESSARY. (M) 2 L 7 2 4F RT 1998121100530 19981211 00530 EU 1998 12 11 RAIA981005 1 19981008 A 7930 81071100010 TRANSMITTER AEROSP ATR42 ATR42300 8680920 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 425TE 15642 125 FLT 7148 - STL - LEFT ENGINE OIL PRESS FLUCTUATES. MAINTENANCE REPLACED OIL PRESS TRANSMITTER. (M) 2 H 7 2 4T RT A53EU 1998121100531 19981211 00531 EU 1998 12 11 RAIA981007 1 19981009 A 2150 1718D000 ACM JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A RAIA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 CE 03 554HK 674 41067 FLT 7743 - JFK - LEFT DUCT TEMP OVERHEAT LIGHT CAME ON IN FLIGHT. MAINTENANCE REPLACED LEFT AIR CYCLE MACHINE. (M) 2 L 7 2 4T RT A41NM 1998121100532 19981211 00532 EU 1998 12 11 RAIA981012 1 19981021 A 3040 ANN60 FUSE JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 557HK 41074 FLT 7720 - JFK - CAPTAINS WINDSHIELD HEAT FAILED ON OUTBOARD SIDE. MAINTENANCE REPLACED FUSE FOR W/S HEAT. (M) 2 L 7 2 4T RT A41NM 1998121100533 19981211 00533 EU 1998 12 11 RAIA981013 1 19981022 A 3260 AIR135864 UPLOCK SWITCH JETAIR JETSTM JETSTM4101 1500501 EU NLG FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 572HK 41091 FLT 7782 - JFK - NOSE LANDING GEAR LIGHT DID NOT GO OUT. MAINTENANCE REPLACED NOSE LANDING GEAR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A41NM 1998121100534 19981211 00534 NM 1998 12 11 USAA980549 1 19981019 A 5512 SKIN BOEING 737 7374B7 1384702 NM HORIZ STABILIZER CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 429US 26761 24551 TPA - DURING C-2 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK ELEVATOR STATION 81.54 AT STAB STATION 67.54 HORIZ STA B SKIN. CUTOUT CRACK AND INSTALLED DOUBLER PER TR 55-10-07. (M) 2 L 7 2 4F RT A16WE 1998121100535 19981211 00535 NM 1998 12 11 USAASB98291 1 19981031 A 2150 220517011 ACM BOEING 737 737401 1384701 NM RT AC BAY FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 407US 29904 23877 TPA - FLT 1425 - AFTER TAKEOFF FROM TPA, CREW COULD NOT GET THE AIRCRAFT TO PRESSURIZE. CREW WENT THROUGH ALL PROCEDURE S BUT AIRCRAFT FAILED TO PRESSURIZE. DIFFERENTIAL PRESSURE NEVER INCREASED BEYOND 1.5 SPI. OUTFLOW VALVE INDICATED FUL L CLOSED. FLIGHT RETURNED TO FIELD TO TPA AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ACM. OPERATIONAL CHECK GOOD. PRESSURIZED AIRCRAFT TO 3 PSI. PRESSURIZATION CHECK GOOD . (M) 2 L 7 2 4F RT A16WE 1998121100536 19981211 00536 NM 1998 12 11 USAA980555 1 19981021 A 5320 654585557 SILL BOEING 737 737401 1384701 NM BS 947/987 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND 2 AREAS OF CORROSION 2 INCHES BY 3 INCHES BETWEEN STATION 947 AND 987 RB L 65 SILL INST GALLEY DOOR. CORROSION TASK NR C53-107-02. REPLACED WITH IDENTICAL PART PER BOEING 737-400 SRM 51-40-00 AND 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998121100537 19981211 00537 NM 1998 12 11 USAA980556 1 19981021 A 5315 6546809126 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q2 CHECK, VISUAL INSPECTION FOUND SEVERAL 1 INCH BY 1 INCH CORRODED AREAS AT STATION 947.5 BETWEEN LBL 20 A ND RBL 20, WL 208. DEFECTIVE PART FLOORBEAM. CORROSION TASK NR C53-107-02. SPLICED IN REPAIR 'T' CAP PER T/R 53-60-02 . (M) 2 L 7 2 4F RT A16WE 1998121100538 19981211 00538 NM 1998 12 11 USAA980557 1 19981021 A 5315 65468102 FLOORBEAM BOEING 737 737401 1384701 NM BS 967 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q2 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH AREAS OF CORROSION STATION 967 BETWEEN LBL 20 AN D RBL 30 WL 208 FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER BOEING 737-400 SRM 53-30-51. (M) 2 L 7 2 4F RT A16WE 1998121100539 19981211 00539 NM 1998 12 11 USAA980558 1 19981021 A 5320 655287864 SILL BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL 2 INCH BY 2 INCH AREAS OF CORROSION BETWEEN STATION 947 AND 987 LBL 65 WL 208 SILL INST AFT ENTRY DOOR. CORROSION TASK NR C53-107-02. INSTALLED DOUBLER PER BOEING 737-400 SRM 51-40-0 0 AND 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998121100540 19981211 00540 NM 1998 12 11 USAA980559 1 19981021 A 5315 654681180 FLOORBEAM BOEING 737 737401 1384701 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND SEVERAL 1 INCH BY 1 INCH AREA OF CORROSION STATION 986.5 LBL 65 RBL 65 W L 208 FLOORBEAM INST. CORROSION TASK NC C53-107-02. SPLICED IN REPAIR 'T' CAP PER TR 53-60-01. (M) 2 L 7 2 4F RT A16WE 1998121100541 19981211 00541 NM 1998 12 11 USAA980560 1 19981021 A 5320 69353501 CLIP BOEING 737 737401 1384701 NM BS 927 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION STATION 927 STRINGER 21R TIE CLIP. CORROSION TASK NR C53-202-02. REPLACED WITH IDENTICAL PARTS PER BOEING 737-400 SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1998121100542 19981211 00542 NM 1998 12 11 USAA980561 1 19981021 A 5311 65465591 FRAME BOEING 737 737401 1384701 NM BS 927 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 1 INCH AREA OF CORROSION STATION 927 BETWEEN STRINGER 22R AN D 21R ON FRAME. CORROSION TASK NR C53-202-01. INSTALLED DOUBLER PER BOEING 737-400 SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1998121100543 19981211 00543 EU 1998 12 11 USAAF98087 1 19981027 A 2840 VS853707 SENSOR FOKKER F28 F28MK0100 4990807 EU CENTER CELL INOPERATIVE A USAA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 EA 19 864US 11306 PHL - FLT 320 - AFTER TAKEOFF FROM PHL, THE TOWER REPORTED THAT FUEL WAS VENTING FROM THE RIGHT WING. AN 'AUTO FUEL FEE D' FAULT ALSO ILLUMINATED. FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE CENTER FUEL TANK RIGHT FLOW SENSOR. (M) 2 L 7 2 4F RT 1998121100544 19981211 00544 NM 1998 12 11 HNAA9898987 1 19981205 A 3397 WIRE DHAV DHC8 DHC8201 2809001 NM CABIN BROKEN A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 989HA 427 EYW - FLT 3054 - SECOND AND THIRD RED FLOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED PS 3352-PS1 POWER SUPPLY AND REPAIRE D BROKEN WIRE AT LIGHT SOCKET. (M) 2 H 7 2 4T RT A13NM 1998121100545 19981211 00545 NM 1998 12 11 HNAA9892488 1 19981204 A 3040 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM COCKPIT ARCED A HNAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 07 924HA 105 PHL - FLT 3038 - CAPTAINS WINDSHIELD ARCS AT WINDSHIELD HEAT CONNECTIONS. OPERATED PER MEL 30-10. (M) 2 H 7 2 4T RT A13NM 1998121100546 19981211 00546 NM 1998 12 11 HNAA9892389 1 19981205 A 5310 STRUCTURE DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 923HA 099 CORROSION FOUND FUSELAGE FRAMES AT STA X222 BETWEEN STRINGERS 32S AND 32P (FRAME, STRINGER, SKIN AND SEAT RAIL SUPPORT), STA X215 BETWEEN STRINGERS 30S AND 31S (FRAME, SEAT RAIL SUPPORT AND TENSION FITTING), STA X467 BETWEEN STRINGERS 29S, 30S AND 31S RT SIDE, STA X487 BETWEEN STRINGERS 29S, 30S AND 31S RT SIDE, STA X445 BETWEEN STRINGERS 29S, 30S AND 31S, S TA X434 STRINGER 30S, STA X291 ON STRINGER 31S, STA X312 STRINGER 31, STA X270 STRINGER 28, STA X366 STRINGER 30, STA X3 66 BETWEEN STRINGERS 29S, 30S AND 31S, FASTENER BOTTOM RIGHT SIDE DATUM FRAME AND TENSION FITTING, SEAT RAIL TO FRAME AT TACH AREA AT FORWARD EMERGENCY EXIT RIGHT SIDE, TIE DOWN HOOKS IN BAG BAY. REPAIRED ALL ITEMS. 2 H 7 2 4T RT A13NM 1998121100547 19981211 00547 WP 1998 12 11 VJ9800640 1 19981124 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 454 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND A CRACK 12.5 IN LENGTH WAS FOUND AFTER REMOVAL OF DOUBLER AT FS 454 BL0. F ABRICATED AND INSTALLED PARTS IAW AIRTRAN EO NR 12-5210-29-B1054 REV A. 2 L 7 2 4F A6WE 1998121100548 19981211 00548 WP 1998 12 11 VJ9800641 1 19981202 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945 & 965 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION AT AERO CORP, FL. CRACKS WERE FOUND IN LONGERON 17L AT FS 945 ON THE LOWER FLANGE TO THE FRAME AND FS 965 AT THE FRAME ATTACH ANGLE. CUT OUT CRACKED SECTIONS OF THE LONGERON, FABRICATED AND REPAIRED MEMBER SECTIONS IAW DC9 SRM 53-02 FIG 18. LONGERON P/N 2777922-4 AND SPLICE P/N 7637813-3. 2 L 7 2 4F A6WE 1998121100549 19981211 00549 WP 1998 12 11 VJ9800642 1 19981202 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 DURING A SCHEDULED INSPECTION AT AERO CORP, FL, CRACKS WERE FOUND AT ATTACHED ANGLE IN THE LONGERON AREA L16L AND L13R A T FS 965. CUT OUT CRACKED SECTIONS OF LONGERON, FABRICATED AND REPAIR MEMBERS IAW DC9 SRM 53-02 FIG 18. LONGERON P/N 2 777922-4, SPLICE P/N 7637813-3 FOR LOCATION L16L. LONGERON P/N S277822-3, SPLICE P/N 7637813-3 FOR LOCATION L13R. 2 L 7 2 4F A6WE 1998121100550 19981211 00550 WP 1998 12 11 VJ9800643 1 19981204 A 5320 WEB DOUG DC9 DC932 3022066 WP BS 598 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION AT AERO CORP, FL, THE CUSP WEB AT FS 598 WAS FOUND CRACKED. CRACK WAS TERMINATED AT WEB AND LIGHTI NG HOLE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01 FIG 1 AND 2 AND 51-30-2. 2 L 7 2 4F A6WE 1998121100551 19981211 00551 WP 1998 12 11 VJ9800644 1 19981130 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION AT AERO CORP, FL. THE INTERNAL FUSELAGE OF THE INTERNAL SKIN AT FS 218 BETWEEN L30 AND L29R WAS FO UND WITH CORROSION AROUND THE BASE OF THE VERTICAL SUPPORT I BEAM IN THE E/E COMPARTMENT. REMOVED DOUBLER, FABRICATED A ND INSTALLED NEW DOUBLER IAW DC9 SRM 53-11-1, 51-10-4 AND 51-30-1. 2 L 7 2 4F A6WE 1998121100552 19981211 00552 SO 1998 12 11 PNSA981101 1 19981128 A 7714 574AW INDICATOR PIPER PA31 PA31350 7103110 SO RT PROP RPM FAILED A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 AL 03 27801 1465 317852157 ABORTED TAKEOFF DUE TO RT PROP RPM INDICATING LOW RPM. REPLACED INDICATOR, OPS CHECK OK. 1 L 7 2 3O A20SO 1998121100553 19981211 00553 WP 1998 12 11 PNSA981102 2 19981128 A 7320 FUEL CONTROL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP LT ENGINE OUT OF ADJUST A PNSA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 AL 03 41NE AC741B LEFT ENGINE DID NOT REACH TARGET TORQUE, ABORTED TAKE-OFF. ADJUSTED MAX POWER FUEL FLOW SUBSEQUENT OPS CHECK OF TORQU E OK, AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4T 4 T RT A8SW E4WE 1998121100554 19981211 00554 EU 1998 12 11 PNSA981103 1 19981110 A 3150 M835366022L RELAY SAAB SF340 340B 7860101 EU COCKPIT INOP A PNSA K NONE L NO TEST TX TAXI/GRND HDL 1 AL 03 675PA 206 PRIOR TO ENGINE START UPPER LAMP TEST DID NOT TEST PROPERLY. REPLACED CONTROL RELAY, OPS CHECK OK. 2 L 7 2 4T RT A52EU 1998121100555 19981211 00555 CE 1998 12 11 PNSA981105 1 19981110 A 7810 265401415 DUCT CESSNA 208 208B 2073701 CE PRIMARY EXHAUST DAMAGED A PNSA K NONE O OTHER IN INSP/MAINT 1 AL 03 750PA 9141 208B0628 DURING A SCHEDULED INSPECTION, THE PRIMARY EXHAUST DUCT WAS FOUND TO HAVE A 2.5 BY 6.O INCH HOLE IN THE CENTER OF THE OU TBOARD SURFACE OF THE DUCT. THIS AREA IS LOCATED BEHIND THE OIL COOLER AND IS NOT VISIBLE WITH THE COWLING INSTALLED NO DAMAGE TO THE SURROUNDING COWLING WAS FOUND. 1 H 7 1 3T A37CE 1998121100556 19981211 00556 WP 1998 12 11 CALA9802144 1 19981207 A 2497 780029700 WIRE DOUG DC9 DC982 3022082 WP E & E COMPT FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 INSPECTION FOUND APU POWER FEEDER CABLES BURNT AT 'T' STRIP S3-23 IN E/E COMPARTMENT, STA 207. ALL THREE PHASES (A,B, A ND C) OF APU POWER FEEDER CABLES WERE REPLACED. IN ADDITION, BOTH APU GEN RELAYS AND WIRES WERE REPLACED. OPERATIONAL CHECKS WERE GOOD. 2 L 7 2 4F A6WE 1998121100557 19981211 00557 NM 1998 12 11 CALA9802145 1 19981207 A 3350 276005 FUSE FUSEUNLIMIT BOEING 727 727232 1384082 NM ROW 20 FAILED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 15790 20644 INSPECTION FOUND AFT SECTION OF AISLE EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND PINS PULLED OUT OF CONNECT OR AT ROW 20 SEAT LIGHT PIGTAIL. THE CONNECTOR WAS REPINNED. ALSO, FOUND AFT POWER SUPPLY BASE F-2 FUSE BLOWN. THE FUS E WAS REMOVED AND REPLACED. OPERATION OF THE EMERGENCY AISLE PATH LIGHTING WAS RESTORED. 2 L 7 3 4F A3WE 1998121100558 19981211 00558 SO 1998 12 11 COMA9810276 1 19981206 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 248CA 14514 960 120228 TWO EMERGENCY LIGHTS ARE INOPERABLE FORWARD CABIN SECTION. REPLACED EMERGENCY LIGHT BATTERY. 2 L 7 2 4T RT A31SO 1998121100559 19981211 00559 SO 1998 12 11 COMA9810277 1 19981202 A 5246 12048166003 FASTENER EMB 120 EMB120RT SO FUEL DOOR BROKEN A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 247CA 120225 SERVICE DOOR WARNING DURING TAKEOFF. REPLACED BROKEN CAM LOCK FASTENER ON SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998121100560 19981211 00560 EA 1998 12 11 COMA9860374 1 19981204 A 5297 MC20C22 WIRE CNDAIR CL600 CL6002B19 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 966CA 7132 DOOR HANDLE CAUTION MESSAGE. REPAIRED BROKEN WIRE AT DOOR WIRE HARNESS. 2 L 7 2 4F RT A21EA 1998121100561 19981211 00561 EA 1998 12 11 COMA9860375 1 19981204 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA ROW 7 & 12 FAILED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 952CA 7092 EMERGENCY LIGHTS ARE INOPERABLE AT ROWS 7 AND 12. REPLACED LIGHT BULBS. 2 L 7 2 4F RT A21EA 1998121100562 19981211 00562 EA 1998 12 11 COMA9860376 1 19981206 A 3350 1317 LAMP CNDAIR CL600 CL6002B19 EA PAX DOOR FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 957CA 7109 EMERGENCY LIGHT BY MAIN CABIN DOOR IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4F RT A21EA 1998121100563 19981211 00563 EA 1998 12 11 COMA9860377 1 19981207 A 2421 GENERATOR CNDAIR CL600 CL6002B19 EA LEFT FAILED A COMA C ABORTED TAKEOFF H ELECT. POWER LOSS-50 PC TO TAKEOFF 1 SO 01 710CA 7241 LEFT GENERATOR FAILED DURING TAKEOFF. SERVICED THE LEFT HAND IDG OIL TO FULL. SYSTEM FUNCTION NORMAL. 2 L 7 2 4F RT A21EA 1998121100564 19981211 00564 NM 1998 12 11 98FDEA00728 1 19981208 A 3270 SWITCH BOEING 727 7272D4 138407U NM TAIL SKID LACK OF LUBE A FDEA O OTHER N FALSE WARNING CL CLIMB 1 SO 25 287FE 21849 98-295 - TAIL SKID LIGHT REMAIN ON AFT T/O, CYCLED THE LAND ONCE, LIGHT STILL ON. REMOVED AND REPLACED GEAR PINS. CLEA N AND LUBE TAIL SKID UP SWITCH. TAIL SKID IS FAIRED WITH FUSELAGE WHEN IN RETRACT POSITION. 2 L 7 3 4F A3WE 1998121100565 19981211 00565 WP 1998 12 11 98FDEA00729 1 19981205 A 3260 SENSOR DOUG DC10 DC1030F 3023504 WP LT MLG DOOR OUT OF ADJUST A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 305FE 47870 98-296 - AFT GEAR RETRACT, LMLG REMAIN ILLUM RED. RECYCLE GEAR 3 TIMES LIGHT REMAIN ON. DID REPOSITION OF STOP SENSOR IN LT MAIN LAND GEAR UP AND DOOR LATCH SENSOR. READJUST CLEARANCE AT TARGET AND PROXIMITY SENSOR AND THEN PERF OPER CK OF L/G SWING AS PER MM 32-34-03-2 AND 7-11-00-2, ALL FUNCTION IS GOOD. A/C OK FOR SVC. 2 L 7 3 4F RT A22WE 1998121100566 19981211 00566 EU 1998 12 11 98FDEA00730 1 19981208 A 3230 RETRACT MECH AIRBUS 310 A310203 EU LT MLG MALFUNCTIONED A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 423FE 281 98-297 - LAND GEAR WOULD NOT RETRACT AFT T/O RETURN TO MEM. FOUND LEFT GEAR TRUCK LEVEL CYLINDER CHARGE IND BUTTON POPP ED 285862. RESERVICED PITCH DAMPER PER A310 AMM 12-12-32. PERF NORM EXTENSION/RETRACTION PER A310 AMM 32-31-00 OPS CK NORM. 2 L 7 2 4F RT A35EU 1998121100567 19981211 00567 NM 1998 12 11 98FDEA00731 1 19981207 A 5320 65176639 SHEAR TIE BOEING 727 727247 138408F NM BS 580 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 380, LBL 4 RBL 4, WL 148. *S/D* REMOVED AND REPLACED SHEAR TIE BS 580 IAW FEDEX SRM 53-10-4, DWG 65-15932. 2 L 7 3 4F A3WE 1998121100568 19981211 00568 NM 1998 12 11 98FDEA00732 1 19981207 A 5313 BAC1498138 STRINGER BOEING 727 727247 138408F NM BS 380 DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 144 BS 380+12, STR 23 LT UPPER FLANGE OF STRINGER IS DENTED. *S/D* REPAIRED STR IAW FEDEX SRM 53-10-3, FEDEX EA 7-5 310-43152. 2 L 7 3 4F A3WE 1998121100569 19981211 00569 NM 1998 12 11 98FDEA00733 1 19981207 A 5311 655612950 FRAME BOEING 727 727247 138408F NM BS 950 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 163 CORROSION C53-113-01(2) AFT CARGO BAY STUB FRAME AT BS 950E+6 STR 29R. REMOVED AND REPLACED AFT CARGO BAY STUB F RAME IAW FEDEX SRM 51-30-2 AND FEDEX DWG 65-56129. 2 L 7 3 4F A3WE 1998121100570 19981211 00570 NM 1998 12 11 98FDEA00734 1 19981207 A 5315 BAC1518338 FLOORBEAM BOEING 727 727247 138408F NM BS 1110 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 187 CORROSION C53-224-04 ON FLOORBEAM UPPER CHORD BS 1110, LBL 11 TO RBL 43, WL 208. REMOVED DAMAGE, FABRICATED, LOC ATED, DRILLED ALODINED, PRIMED, PAINTED AND INSTALL FLOORBEAM SEGMENT AND REPAIR PARTS IAW FEDEX SRM 53-10-8, 51-30-2 AN D FEDEX MM 51-20-151. 2 L 7 3 4F A3WE 1998121100571 19981211 00571 NM 1998 12 11 98UAL900528 1 19981105 A 2612 22604700 FIRE LOOP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ENGINE MALFUNCTIONED A UALA F E A ACTIVATE FIRE EXT. ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 386UA 24661 FIRE WARNING INDICATION. REPLACED LOWER FAN LOOP AND FIREWALL LOOP. 2 L 7 2 4F 4 F RT A16WE E2GL 1998121100572 19981211 00572 NM 1998 12 11 98UAL900553 1 19981121 A 2612 MODULE 69782141 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE COCKPIT FAILED A UALA O OTHER P NO WARNING INDICATION NR NOT REPORTED 1 WP 29 341UA D01319 24245 FIRE WARNING BELL INOP. REPLACED AURAL WARNING MODULE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998121100573 19981211 00573 NM 1998 12 11 98UAL900555 1 19981116 A 2822 6072101 PUMP CRANEHYDROAI 6072101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 107UA 540 26900 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 2 RECOVERED FROM THE NR 2 MAIN FUEL TANK (AFT POSITION) OF ACFT 8407 W AS FOUND TO EXHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. TESTING OF THE PUMP BY THE VENDOR SHOWED THAT THE AXIAL THRUST-BALANCING MECHANISM FAILED. THE THRUST WASHER/BEARING IS SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998121100574 19981211 00574 NM 1998 12 11 98UAL900556 1 19981122 A 2530 COFFEEMAKER GRIMES 35200015 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY DEFECTIVE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 29 7455U 21909 MINOR SMOKE IN AFT GALLEY. SUBMITTER STATES, SUSPECTED CAUSE WAS EITHER A LIGHT BULB OR A COFFEE MAKER. SUBSEQUENT INS PECTION SHOWED THAT THE COFFEE MAKER WAS DEFECTIVE. THE COFFEE MAKER WAS REPLACED AND CHECKED FOR PROPER OPERATION. 2 L 7 3 4F 4 F A3WE E2EA 1998121100575 19981211 00575 NM 1998 12 11 98UAL900557 1 19981123 A 2822 6072101 PUMP CRANEHYDROAI 6072101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 2 DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 107UA 644 644 26900 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 2 RECOVERED FROM THE NR 2 MAIN FUEL TANK (FWD POSITION) OF ACFT 8407 W AS FOUND TO EXHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. TESTING OF THE PUMP BY THE VENDOR SHOWED THAT THE AXIAL THRUST-BALANCING MECHANISM FAILED. THE THRUST WASHER/BEARING IS SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998121100576 19981211 00576 NM 1998 12 11 98UAL900558 1 19981114 A 2822 6072101 PUMP CRANE HYDRO 6072101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CENTER WING DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 192UA 131 26881 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 1 RECOVERED FROM THE CENTER WING FUEL TANK OF ACFT 8192 WAS FOUND TO E XHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. THE THRUST WASHER/BEARING I S SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998121100577 19981211 00577 NM 1998 12 11 98UAL900559 1 19981105 A 2822 6072101 PUMP CRANE HYDRO 6072101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CENTER WING DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 196UA 130 28715 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 1 RECOVERED FROM THE CENTER WING FUEL TANK OF ACFT 8496 WAS FOUND TO E XHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. THE THRUST WASHER/BEARING I S SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998121100578 19981211 00578 NM 1998 12 11 98UAL900560 1 19981117 A 2822 6072101 PUMP CRANE HYDRO 6072101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CENTER WING DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 188UA 146 26877 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 1 RECOVERED FROM THE CENTER WING FUEL TANK OF ACFT 8188 WAS FOUND TO E XHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. THE THRUST WASHER/BEARING I S SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998121100579 19981211 00579 NM 1998 12 11 98UAL900561 1 19981115 A 2822 6072101 PUMP CRANE HYDRO 6072101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CENTER WING DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 172UA 144 24363 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 1 RECOVERED FROM THE CENTER WING FUEL TANK OF ACFT 8672 WAS FOUND TO E XHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. THE THRUST WASHER/BEARING I S SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998121100580 19981211 00580 NM 1998 12 11 98UAL900562 1 19981120 A 2822 6072101 PUMP CRANE HYDRO 6072101 BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE CENTER WING DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 180UA 25224 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 1 RECOVERED FROM THE CENTER WING FUEL TANK OF ACFT 8480 WAS FOUND TO E XHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. THE THRUST WASHER/BEARING I S SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F 4 F RT A20WE E24NE 1998121100581 19981211 00581 NM 1998 12 11 98UAL900563 1 19981101 A 2822 6072101 PUMP CRANE HYDRO 6072101 BOEING 747 747422 1384935 NM CENTER WING DAMAGED A UALA K NONE J WARNING INDICATION NR NOT REPORTED 1 WP 29 197UA 5784 26901 FUEL OVERRIDE/JETTISON PUMP PART NR 60-72101 DASH 1 RECOVERED FROM THE CENTER WING FUEL TANK OF ACFT 8497 WAS FOUND TO E XHIBIT EXCESSIVE IMPELLER END-PLAY AND GOUGING OF THE IMPELLER UNIT WITH THE INLET ADAPTER. THE THRUST WASHER/BEARING I S SUSPECTED TO HAVE BEEN MANUFACTURED INCORRECTLY. ROOT CAUSE OF FAILURE HAS NOT BEEN IDENTIFIED AS YET. 2 L 7 4 4F RT A20WE 1998121100582 19981211 00582 NM 1998 12 11 98UAL900569 1 19981128 A 3350 20131 BATTERY PACK BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE ROW 6 DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 377UA 24642 THE BATTERY FOR THE EEL ON THE LEFT SIDE IS INOP. EEL LIGHTS WERE LEFT ON THE LEFT SIDE OF THE AIRCRAFT, IN EFFECT DRAI NING THE BATTERY. THE BATTERY WAS REPLACED AT ROW 6 ON THE LEFT SIDE AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998121100584 19981211 00584 NM 1998 12 11 98UAL900571 1 19981126 A 2121 FAN 65772 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE E & E COMPT INOP A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 901UA 25001 EXHAUST COOLING FAN INOP. REPLACED THE EQUIPMENT RACK ELECTRIC COOLING BLOWER. 2 L 7 2 4F 4 F RT A16WE E2GL 1998121100585 19981211 00585 NM 1998 12 11 98UAL900572 1 19981125 A 3350 9F19948 LIGHT BOEING 747 747422 1384935 NM 4L DOOR INOPERATIVE A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 173UA 24380 DOOR 4L EMERGENCY SLIDE LIGHT COMES ON WHEN EMERGENCY LIGHT SWITCH IS ARMED. *S/D* REPLACED LIGHT ASSEMBLY 9F19948 AND W IRE W2086-003-20 FROM DX321 PLUG TO TB211 PER GNMM2-0-15-1 AND WD33-51-52. 2 L 7 4 4F RT A20WE 1998121100586 19981211 00586 WP 1998 12 11 98UAL900573 1 19981125 A 2910 LINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL FUSELAGE LEAKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 1834U 47966 ODOR IN CABIN AROUND DOOR 3 AREA ON TAKEOFF, CLIMB AND INTERMITTENTLY IN CRUISE. SMELLS LIKE HOT OIL. REPAIRED HYDRAUL IC LEAK NEAR APU INLET, BURNED OUT ALL 3 PACKS. REPLACED ALL 3 COALESCER BAGS. THERE HAVE BEEN NO REOCCURANCES. 2 L 7 3 4F 4 F A22WE E23EA 1998121100587 19981211 00587 WP 1998 12 11 98UAL900574 1 19981124 A 3350 BATTERY PACK DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN DISCHARGED A UALA K NONE L NO TEST NR NOT REPORTED 1 WP 29 1838U 46632 C ZONE EEL LIGHTS INOPERABLE ALONG BOTH AISLES. FOUND BATTERY PACKS DISCHARGED. REPLACED BATTERY PACKS AND CHECKS OKAY . 2 L 7 3 4F 4 F A22WE E23EA 1998121100588 19981211 00588 NM 1998 12 11 98UAL900575 1 19981128 A 2750 FSEU BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE TE FLAPS MALFUNCTIONED A UALA L ABORTED APPROACH F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 WP 29 619UA 21879 FLIGHT HAD EICAS ERROR/GROUND DISAGREEMENT LIGHT ILLUMINATE. EXECUTED GO-AROUND. FLAPS THEN LOCKED-OUT AT 22 DEGREES. E MERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT. *S/D* CAUSE: FAILURE PROTECTION SHUTDOWN OF T/E FLAPS WAS TRIGGER ED BY THE FLAP/SLAT ELECTRONIC UNIT (FSEU) SENSING A TRAILING EDGE FLAP DISAGREE CONDITION. MAINTENANCE CLEARED ALL EXI STING FAULTS ON THE FSEU, VERIFIED PROPER OPERATION OF T/E FLAP POSITION TRANSMITTERS AND FLAP ROTARY ACTUATORS PER MM. FINAL OPERATIONAL CHECKS PER MM FOUND ALL OK. 2 L 7 2 4F 4 F RT A1NM E3NE 1998121100589 19981211 00589 NM 1998 12 11 98UAL900576 1 19981129 A 3230 1C1322 ACTUATOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT MLG TRUCK FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 641UA 25091 LEFT MAIN GEAR WOULD NOT RECYCLE AFTER CLIMB-OUT. RECYCLED GEAR, LEFT MAIN WOULD NOT RECYCLE. DIVERTED LHR, OVERWEIGHT LANDING. CHECK VALVE IN TRUCK POSITION ACTUATOR PRESSURE LINE WAS MALFUNCTIONING, ALLOWING BYPASS AND PREVENTING UNLOC K ACTUATORS TO BUILD UP UNLOCK PRESSURE. REPLACED TRUCK POSITION ACTUATOR. 2 L 7 2 4F 4 F RT A1NM E24NE 1998121100590 19981211 00590 NM 1998 12 11 98UAL900577 1 19981129 A 2121 FAN ALLIED SIGNA 6066221 BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT AC SYST FAILED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 604UA 121185 21865 CREW ADVISED SMELLING SMOKE ODOR IN CABIN. DIVERTED TO DEN. *S/D* LEFT AIR CONDITIONING RECIRCULATION FAN WAS REPLACE D DUE TO SMELL LIKE SMOKE. SHOP FINDINGS CONFIRMED ROUGH AND DRY BEARINGS, BUT NO OTHER INTERNAL HEAT DAMAGE. PROBABLE CAUSE OF SMOKE ODOR IS BEARING OVERHEAT RESULTING IN SMOKING GREASE. 2 L 7 2 4F 4 F RT A1NM E3NE 1998121100591 19981211 00591 NM 1998 12 11 98UAL900578 1 19981127 A 2731 56024004 ACTUATOR BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE STAB TRIM FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 7259U 21406 STABILIZER WOULD NOT TRIM (ON PEDESTAL) AFT OF 4.5 UNITS ELECTRICALLY. RETURNED TO DEN. *S/D* REPLACED MAIN ELECTRIC ST AB TRIM ACTUATOR, SYSTEM OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1998121100592 19981211 00592 NM 1998 12 11 98UAL900579 1 19981128 A 3230 69499542 BUSHING BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE RT MLG DNLOCK MISSING A UALA L ABORTED APPROACH J E WARNING INDICATION VIBRATION/BUFFET LD LANDING 1 WP 29 7276U 21423 ON TOUCHDOWN, RIGHT MAIN LANDING GEAR WARNING LIGHT CAME ON. FELT VIBRATION ON RIGHT SIDE. INITIATED A GO-AROUND. *S/ D* FOUND RT MAIN LANDING GEAR DOWNLOCK SENSOR ACTUATOR MISSING BUSHING. REPLACED BUSHING AND PERFORMED DOWNLOCK SENSOR AND LANDING GEAR POSITION INDICATING AND WARNING SYSTEM TEST PER MAINTENANCE MANUAL. SWUNG GEAR NUMEROUS TIMES AND OPS CHECKS GOOD. ALSO, PERFORMED MANUAL GEAR EXTENSION. 2 L 7 3 4F 4 F A3WE E2EA 1998121100593 19981211 00593 WP 1998 12 11 98UAL900580 1 19981124 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL CABIN MISWIRED A UALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 29 1838U 46632 EEL LIGHTS INOP. NO POWER FROM OVERWING AND AFT CABIN BATTERY PACKS IN C ZONE. *S/D* FOUND WIRE L2712 K10 CONNECTED T O TERMINAL A1 OF R2-178. CONNECTED SAME WIRE TO R2-178 TERMINAL A3. 2 L 7 3 4F 4 F A22WE E23EA 1998121100594 19981211 00594 NM 1998 12 11 98UAL900581 1 19981129 A 4950 PNEUMATIC SYST BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE CABIN SMOKING A UALA H DEACTIVATE SYST/CIRCUITS B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 WP 29 529UA 25019 CREW REPORTED TWO AFT SMOKE DETECTORS SOUNDING INTERMITTENTLY. *S/D* MAINTENANCE DETERMINED THAT THE CAUSE OF SMOKE IN CABIN WAS A RESULT OF PNEUMATIC SYSTEM OIL CONTAMINATION FROM THE APU. THE SUSPECT APU WAS REPLACED IN ORD ON 12/3/98. PACK BURNOUT WAS ACCOMPLISHED TO EXPEL RESIDUAL OIL IN PNEUMATIC SYSTEM. APU HAS BEEN RETURNED TO SHOP FOR ANALYSIS. 2 L 7 2 4F 4 F RT A2NM E17NE 1998121100595 19981211 00595 WP 1998 12 11 MWEA981130 1 19981202 A 2560 113317 SLIDE DOUG DC9 DC915 3022036 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 300ME 45718 THE GALLEY DOOR SLIDE FELL OUT OF DOOR. MAINTENANCE REINSTALLED EMERGENCY ESCAPE SLIDE. 2 L 7 2 4F A6WE 1998121100596 19981211 00596 WP 1998 12 11 MWEA981131 1 19981205 A 2560 113317 SLIDE DOUG DC9 DC915 3022036 WP GALLEY DOOR LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 THE GALLEY DOOR SLIDE FELL OUT OF DOOR. MAINTENANCE REISNTALLED FORWARD GALLEY DOOR SLIDE. 2 L 7 2 4F A6WE 1998121100597 19981211 00597 WP 1998 12 11 MWEA981132 1 19980918 A 5330 5930461 SKIN DOUG DC9 DC915 3022036 WP FUSELAGE CHAFFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 BARE METAL CHAFFING LEFT FUSE EXTERIOR SKIN UNDER AFT WING TO FOS FAIRING STA FUSELAGE STATION. MAINTENANCE FABRICATED DOUBLER AND TRIPLE AND INSTALLED. 2 L 7 2 4F A6WE 1998121100598 19981211 00598 WP 1998 12 11 MWEA981133 1 19981207 A 5330 5911425 SKIN DOUG DC9 DC915 3022036 WP BS 710-718 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 EXTERNAL SKIN AT STATION 710 TO 718 BETWEEN LONGERON 29R AND 30 IS DAMAGED DUE TO EXCESSIVE CUT OUT. REMOVED ALL DAMAGE FABRICATED FILLER DOUBLER AND TRIPPLER. ALSO, INSTALLED REPAIR PARTS. 2 L 7 2 4F A6WE 1998121100599 19981211 00599 WP 1998 12 11 MWEA981134 1 19981207 A 5311 5911448 FRAME DOUG DC9 DC915 3022036 WP BS 218 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 FRAME AT STATION 218 LONGERON 25 LEFT AND 25 RIGHT WAS BLENDED BEYOND LIMITS. REMOVED DAMAGED SECTION OF FRAME AND INST ALLED REPAIR SECTION OF FRAME. 2 L 7 2 4F A6WE 1998121100600 19981211 00600 WP 1998 12 11 MWEA981135 1 19981207 A 5320 591924 DOUBLER DOUG DC9 DC915 3022036 WP FUSELAGE DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 LEFT MAIN STATIC PORT ADAPTER PLATE HAS CORRODED AND BROKEN SCREWS. REMOVED AND REPLACED STATIC PORT DOUBLER. 2 L 7 2 4F A6WE 1998121100601 19981211 00601 WP 1998 12 11 MWEA981136 1 19981207 A 5320 9910151 MEMBRANE DOUG DC9 DC915 3022036 WP BS 510 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 CUSP MEMBRANE CRACKED AT FS 510 LONGERON 18 RIGHT. REMOVED DAMAGED AREA FABRICATED AND INSTALLED FILLER AND DOUBLER. 2 L 7 2 4F A6WE 1998121100602 19981211 00602 WP 1998 12 11 MWEA981137 1 19981109 A 5320 591008561 CUSP DOUG DC9 DC915 3022036 WP BS 160 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 CUSP AT STATION 160 BELOW R1 DOOR FORWARD SIDE CUT OUT IS CORRODED. REPAIRED CUSP AT STATION 160 BELOW R1 DOOR IAW DAC DRAWING 5910085 AND 7060288 2 L 7 2 4F A6WE 1998121100603 19981211 00603 NM 1998 12 11 DL72K982461 1 19981117 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 414DA 21256 AT MV2 FOUND FLOORBEAM CORRODED FS 344 RBL 20-LBL65. REMOVED CORROSION PER SRM 53-10-8 FIG 11. REMOVED T-CAP, FAB'D RE PAIR, INSTALLED PER SAME. CONTINUED ON N/R 1043. 2 L 7 3 4F A3WE 1998121100604 19981211 00604 NM 1998 12 11 DL72K982462 1 19981117 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 344 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 414DA 21256 AT MV2, FOUND CONTINUATION OF N/R 610. INSTALLED CAP PER SRM 53-10-9-11. 2 L 7 3 4F A3WE 1998121100605 19981211 00605 WP 1998 12 11 DLL10982463 1 19981130 A 3350 BATTERY PACK 5165741 LKHEED 1011 10113851 5265010 WP L-4 DOOR DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 54078 193C1180 FOUND EXTERIOR EMERGENCY LIGHT AT 4L DOOR INOP. REPLACED BATTERY PACK. 2 L 7 3 4F A23WE 1998121100606 19981211 00606 NM 1998 12 11 DL72S982464 1 19981130 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 FOUND ON LETTER CK, C-2 - .5 INCH VISIBLE CRACK IN LT FRAME OF AFT ENTRY DOOR CUTOUT AT DATA PLATE. REPAIR PER SRM 53-1 0-9. 2 L 7 3 4F A3WE 1998121100607 19981211 00607 NM 1998 12 11 DL72S982465 1 19981130 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 FOUND AT LETTER CHECK C-2, .5 INCH VISIBLE CRACK IN RT FRAME OF AFT ENTRY DOOR CUTOUT AT 2ND FROM TOP STOP CASTING. REP AIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1998121100608 19981211 00608 NM 1998 12 11 DL72S982466 1 19981130 A 5240 SKIN BOEING 727 727232 1384082 NM R-1 DOOR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 497DA 21077 REF SHIP 497 TPA LTR CHK C2, TWO SMALL CRACKS UPPER AFT CORNER UPPER HINGE CUTOUT, R1 DOOR SKIN. REPAIRED PER MM 52-11- 01. 2 L 7 3 4F A3WE 1998121100609 19981211 00609 NM 1998 12 11 DL72L982470 1 19981127 A 5754 651622370 STOP BOEING 727 727232 1384082 NM NR 7 LE SLAT LOOSE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 505DA 21307 WING NR 7 SLAT, DOWNSTOP FITTING, REPAIR FOR LOOSE BOLT. THE NR 7 SLAT DOWNSTOP FITTINGS WERE FOUND WITH LOOSE BOLTS. D URING INSPECTIONS PER S/B 727-57-171. THE STOP FITTINGS FOR THE SLAT WERE MODIFIED PER THE REQUIREMENTS OF THE S/B. THE MODIFICATION OF THE NR 7 SLAT STOPS WAS DOCUMENTED PER ER/A 366172-14AD. 2 L 7 3 4F A3WE 1998121100610 19981211 00610 NM 1998 12 11 DL72W982473 1 19981126 A 5320 FITTING BOEING 727 727247 138408F NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FUSELAGE STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG ATTACH FITTING WAS INSPECTED PER BAC S/B727-53-0141 (LT SIDE). TWO FASTENER HOLES COMMON TO STRINGER 18-A WERE FOUND TO HAVE CRACK INDICATIONS. THE HOLES W ERE OVERSIZED TO REMOVE THE CRACK INDICATIONS, AND BUSHINGS AND OVERSIZE BOLTS WERE INSTALLED PER ER/A 366149-14. 2 L 7 3 4F A3WE 1998121100611 19981211 00611 NM 1998 12 11 DL72W982474 1 19981126 A 5320 65861135 FITTING BOEING 727 727247 138408F NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FUSELAGE RT STA 940 FITTING STRINGER 18-A, REPAIR FOR O/S HOLES. THE STATION 940 MLG FITTING AREA WAS INSPECTED PER BAC S/B 727-53-0141. CORROSION AND CRACK INDICATIONS WERE FOUND IN THE FITTING, STRINGER, AND SKIN. THE DAMAGED AREA OF SKIN WAS CUTOUT AND REPAIRED WITH A DOUBLER PER S/B 727-53-0172. THE STRINGER WAS SPLICED PER THE S/B, AND FITTING HOL ES WEREOVERSIZED AND BUSHED. THE REPAIR WAS ACCOMPLISHED PER ER/A 332512-14, REV A. 2 L 7 3 4F A3WE 1998121100612 19981211 00612 NM 1998 12 11 DL72W982475 1 19981126 A 5330 65545902 SKIN BOEING 727 727247 138408F NM BS 720 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2819W 21057 FUSELAGE SKIN FS 720A-720B, STRINGER 27R-28R. REPAIR FOR CORROSION CUTOUT. THE FUSLAGE SKIN WAS FOUND CORRODED BETWEEN FS 720A AND FS 720B BETWEEN STRINGERS 27R AND 28R. THE CORROSION WAS REMOVED WITH A 3 BY 3.75 CUTOUT AND A 7.5 BY 3 CU TOUT. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER PER ER/A 366104-14, REV A. 2 L 7 3 4F A3WE 1998121100613 19981211 00613 NM 1998 12 11 DL72S982479 1 19981201 A 3350 RPS1 PWR SUPPLY BOEING 727 727225 1384077 NM ROW 1-11 INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND ON L/O, EMERGENCY ESCAPE PATH LIGHTS INOP ROW 1 THROUGH 11. REPLACED POWER SUPPLY AND BATTERY. 2 L 7 3 4F A3WE 1998121100614 19981211 00614 NM 1998 12 11 DL72S982480 1 19981201 A 3350 20131A BATTERY BOEING 727 727225 1384077 NM ROW 1-11 DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 8890Z 21859 FOUND ON L/O, EMERGENCY ESCAPE PATH LIGHTS INOP ROWS 1-11. REPLACED PWR SUPPLY AND BATTERY. 2 L 7 3 4F A3WE 1998121100615 19981211 00615 NM 1998 12 11 DL72S982482 1 19981202 A 5530 STRINGER BOEING 727 727225 1384077 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 REF SHIP 538 TPA LTR CHK E-2 12-02-98, VERT FIN STRINGER 10L CRACKED STA 180.6. REPAIRED PER MM 55-30-0. 2 L 7 3 4F A3WE 1998121100616 19981211 00616 NM 1998 12 11 DL72S982483 1 19981202 A 5320 WEB BOEING 727 727225 1384077 NM BS 1233 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 REF SHIP 438 TPA LTR CHK E-2 12-02-98, .5 CRACK RT TORQUE BOX VERT WEB AT UPPER END STA 1233. REPAIRED PER MM 53-11-0 P G832. 2 L 7 3 4F A3WE 1998121100617 19981211 00617 NM 1998 12 11 DL72S982484 1 19981202 A 5320 WEB BOEING 727 727225 1384077 NM BS 1236 & 1228 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 8890Z 21859 REF SHIP 438 TPA LTR CHK E-2 12-02-98, TWO CRACKS AT LIGHTNING HOLES RT SIDE TORQUE BOX STA 1236 AND 1228. REPAIRED PE R MM 53-11-0 PG 828. 2 L 7 3 4F A3WE 1998121100618 19981211 00618 NM 1998 12 11 DL757982485 1 19981202 A 2530 811150417 COFFEEMAKER BOEING 757 757232 1384965 NM GALLEY FAILED A DALA K NONE M B OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 668DN 25141 MID GALLEY AT 2L DOOR AFT SEC COFFEEMAKER BEGAN SMOKING, MODERATE AMOUNT ACRID SMOKE-POWER SECURED. ALL C/B ASSOCIATED WITH GALLEY PULLED, SMOKE STOPPED IT TOOK 10 MIN FOR HEAT TO STOP COMING FROM TOP CORNER AREA, COOLED SLOWLY. NOTE AT O NE TIME BULKHEAD AFT OF GALLEY WAS WARM TO TOUCH. WATER STARTED LEAKING BAD. SECURED WATER VLV. FOUND WATER MAKER BUR NED UP. WATER DISCONNECT LEAKING. ELECT AND WATER DISCONNECTED ON NEW COFFEEMAKER. NEED WATER HOSE ASSY. 2 L 7 2 4F RT A2NM 1998121100619 19981211 00619 NM 1998 12 11 DL72S982487 1 19981201 A 5400 65312814 ANGLE BOEING 727 727232 1384082 NM NR 2 ENGINE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 517DA 21433 FOUND CORROSION ON HEAVYWEIGHT HUSH-KIT MOD ON RT NR 2 ENG AFT MOUNT SUPPORT CHORD ANGLE IN EXCEEDANCE OF MFG MINIMUM AL LOWABLE TOLERANCES. REPLACED RT CHORD ANGLE WITH NEW MFG PART. 2 L 7 3 4F A3WE 1998121100620 19981211 00620 NM 1998 12 11 DL757982488 1 19981202 A 2530 COFFEEMAKER 811150417 BOEING 757 757232 1384965 NM GALLEY FAILED A DALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 668DN 75 25141 SMOKE IN CABIN AT LT MID GALLEY FROM AFT COFFEEMAKER. C/B PULLED, SMOKE STOPPED. REPLACED COFFEEMAKER. 2 L 7 2 4F RT A2NM 1998121100621 19981211 00621 NM 1998 12 11 DL76G982491 1 19981203 A 3350 BPS73 PWR SUPPLY BOEING 767 7673P6 1385105 NM CABIN FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 153DL 24985 FOUND ON OW II CHECK, EMERGENCY SEAT LIGHTS INOP SEATS 13A/BTO 22 A/B. REPLACED POWER SUPPLY. EMERGENCY LIGHTS OPS CKS OK. 2 L 7 2 4F RT A1NM 1998121100622 19981211 00622 NM 1998 12 11 DL72S982494 1 19981201 A 5315 FLOORBEAM BOEING 727 727232 1384082 NM BS 1070 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 CORROSION FOUND ON FLOORBEAM STA 1070 AT LBL 55 SEAT TRACK ATTACH POINT (MARKED). REPAIRED PER SRM 53-20-11 FIG 804A. 2 L 7 3 4F A3WE 1998121100623 19981211 00623 WP 1998 12 11 DLL10982496 1 19981204 A 3350 POWER SUPPLY 516574 LKHEED 1011 10113851 5265010 WP GALLEY INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 1731D 69523 193C1200 DURING LAYOVER, EMERGENCY CEILING LIGHTS BY L2/R2 INOP. POWER SUPPLY DOES NOT CHARGE. REPLACED POWER SUPPLY. 2 L 7 3 4F A23WE 1998121100624 19981211 00624 NM 1998 12 11 DLM88982497 1 19981205 A 3350 BATTERY DOUG MD88 MD88 3023688 NM CABIN DISCHARGED A DALA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 27 957DL 49976 FLASHLIGHT AFT OF FLIGHT ATTENDANT, FWD LIGHT RED LIGHT DOES NOT BLINK. REPLACED BATTERY PER M/M. OPS CHECKS GOOD. 2 L 7 2 4F RT A6WE 1998121100625 19981211 00625 NM 1998 12 11 DL73K982498 1 19981205 A 2782 6546422300A ACTUATOR BOEING 737 737232 1384475 NM NR 5 LE SLAT FAILED A DALA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 27 329DL 23101 LEADING EDGE AMBER LIGHT ON SLAT NR 5. REPLACED NR 5 SLAT AND ACTUATOR. 2 L 7 2 4F RT A16WE 1998121100626 19981211 00626 1998 12 11 DL76G982503 4 19981206 A 3140 EICAS 6226088108 BOEING 767 7673P6 1385105 NM LEFT MALFUNCTIONED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 152DL 1341 24984 LEFT EICAS FAULT INDICATION, DIVERTED TO JFK. BITE CHECK SHOWED PROG PIN ERROR, TEST FAIL, LEFT COMP FAIL, CU CODE 0200 - 0080 DISCRETE 202 -210. REPLACED LEFT EICAS COMP AND PSEU. CHECKED FOR PUSHED BACK PINS, FOUND NONE. SYSTEM CHECKS OK. OVERWEIGHT LANDING INSPECTION PERFORMED PER 5-51-35-2. NO DAMAGE FOUND. 2 L 7 2 4F RT A1NM 1998121100627 19981211 00627 NM 1998 12 11 DL72L982505 1 19981130 A 5713 STRINGER BOEING 727 727232 1384082 NM WS 656.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 ITEM: OUTER WING UPPER STRINGER TO RIB WS 656.5 HAS A CRACK AT STRINGER 10 COMING FROM THE FASTENER HOLE. CRACK IS IN S TRINGER. REPAIR INTO REFERENCED ON 8502AD ITEM 5. CRACK ORIGINATES IN FASTENER HOLE AND PROPAGATES TO EDGE OF STRINGER . DRILLED REPAIR DOUBLERS AND RADIUS BLOCKS AND STRINGER 10 AT WS 656.5 PER MM 57-13-0 PG 801-805. OK TO INSTALL. INS TALLED REPAIR PER MM 57-13-0 PG 801-805. 2 L 7 3 4F A3WE 1998121100628 19981211 00628 NM 1998 12 11 DL72L982508 1 19981207 A 5720 STIFFENER BOEING 727 727232 1384082 NM RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 REF SHIP 512 TPA LTR CHK D-1 12-07-98, L/E SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK I/B STIFFENER. REPLACED PER MM 57-20-21. 2 L 7 3 4F A3WE 1998121100629 19981211 00629 NM 1998 12 11 DL72L982509 1 19981207 A 5712 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 512DA 21314 REF SHIP 512 TPA LTR CHK D-1 12-07-98, NR 5 L/E SLAT I/B ACTUATOR ATTACH RIB CRACKED. REPAIRED PER MM 57-54-0 AND ERA 3 66246-14. 2 L 7 3 4F A3WE 1998121100630 19981211 00630 WP 1998 12 11 ARWA981203 1 19981208 A 3411 PITOT SYST DOUG DC8 DC862 3021970 WP LEFT & RIGHT CONTAMINATED A ARWA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 19 8968U 46069 DURING CLIMB-OUT, CAPT'S AIRSPEED INDICATOR READS 200 KTS AND F/O'S AIRSPEED INDICATOR READ 33O KTS. ACCOMPLISHED PITOT /STATIC LEAR TEST IAW MM 34-12-00. ALL PARAMETERS WITHIN LIMITS. PURGED SYSTEM PRECAUTIONARY MEASURE IAW 34-12-00 NR 1 ,2, ADC PITOT STACTIC. NO DEFECTS NOTED IAW 34-11-00. 2 L 7 4 4F 4A25 1998121100631 19981211 00631 WP 1998 12 11 TWAA9819401 1 19981206 A 4990 OIL SYST DOUG DC9 DC982 3022082 WP APU OVER SERVICED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS LD LANDING 1 CE 05 918TW 49367 AT OUTER MARKER, THE CABIN FILLED WITH SMOKE AND HAD OILY SMELL. AFTER TURNING OFF RUNWAY TURNED OFF ALL ANTI-ICE AND S MOKE CLEARED A LITTLE. THE APU WAS PREVIOUSLY DEACTIVATED FOR OIL LEAK CAUSING SMOKE. RAN LT ENG AND LT PACK AT MAX TE MP TO BURN OFF RESIDUE. RAN RT ENG AND RT PACK AT MAX FOR 20 MINUTES WITH NO SMELL OR SMOKE. APU REMAINED PLACARDED PE R MEL. CHECK-C 6-1-98 STL. THE APU WAS REPLACED AND THE BLEED AIR SUPPLY OF THE APU WAS CHECKED FOR EVIDENCE OF OIL, B UT NONE WAS NOTED. THE INLET WAS COVERED WITH CLEAN OIL AND WAS REPLACED. SUSPECT THE APU WAS OVERSERVICED. 2 L 7 2 4F A6WE 1998121100632 19981211 00632 WP 1998 12 11 VJ9800645 1 19981110 A 5730 SKIN DOUG DC9 DC932 3022066 WP WS 440-445 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 SCHEDULED INSPECTION, THE RIGHT WING UPPER SURFACE FIXED PANEL, FWD OF THE AILERON FROM XRS 445 TO XRS 400 APPROXIMATELY WAS FOUND WITH SURFACE CORROSION ON THE UNDERSIDE IN SEVERAL PLACES. CUT OUT CORROSION AND DELAMINATION IN THE SPECIFI ED AREA. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3 AND 57-01. 2 L 7 2 4F A6WE 1998121100633 19981211 00633 WP 1998 12 11 VJ9800646 1 19981112 A 5312 991556173 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 966 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 SCHEDULED INSPECTION, THE ANGLE ON THE PRESSURE BULKHEAD WAS FOUND CORRODED AT L30 FS966. GAINED ACCESS TO AREA, REMOVE D AND REPLACED ANGLE. REINSTALLED ALL PARTS REMOVED FOR ACCESS IAW DC9 SRM 51-10-4, 51-30-2, 51-30-1, 51-10-3, AND SB53 -147 PG 44. 2 L 7 2 4F A6WE 1998121100634 19981211 00634 NM 1998 12 11 CALA9802146 1 19981208 A 5752 652172642K SKIN BOEING 727 727243 138408D NM RT AILERON TAB DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND RT O/B AILERON TAB UPPER SURFACE DENTED. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-41. 2 L 7 3 4F RT A3WE 1998121100635 19981211 00635 NM 1998 12 11 CALA9802147 1 19981208 A 5712 RIB BOEING 727 727243 138408D NM WS 330 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 1.25 INCH CRACK AROUND BOLT HEADS AT UPPER AFT END OF LT WING FIXED LE RIB, WS 330. THE RIB WAS REMO VED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-2, PAGE 3, 51-40-3, 51-10-6, PAGE 1, AND 51-10-1, PAGE 1. 2 L 7 3 4F RT A3WE 1998121100636 19981211 00636 NM 1998 12 11 CALA9802148 1 19981208 A 5320 CHORD BOEING 727 727243 138408D NM COCKPIT CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND CHORD CORRODED IN COCKPIT FLOOR PANEL AT F/E SEAT AFT STOP. THE CHORD WAS REMOVED AND A NEW ONE WAS IN STALLED IAW SRM 51-30-2, PAGE 4. 2 L 7 3 4F RT A3WE 1998121100637 19981211 00637 NM 1998 12 11 CALA9802149 1 19981208 A 5752 652172641K SKIN BOEING 727 727243 138408D NM LT AILERON TAB CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND LT O/B AILERON TAB LOWER SURFACE CORRODED AT O/B END AND A SMALL DEBONDED AREA. THE AILERON TAB WAS RE MOVED AND REPLACED IAW MM 27-10-41, PAGE 401-403. 2 L 7 3 4F RT A3WE 1998121100638 19981211 00638 NM 1998 12 11 CALA9802150 1 19981208 A 5530 STRINGER BOEING 727 727243 138408D NM VERT STAB CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 1.5 INCH CRACK LT STRINGER 9 INSIDE VERTICAL STABILIZER AT RIB NR 8. THE CRACKED AREA WAS CUT OUT IA W SRM 55-30-4, PAGE 1. REPAIR ANGLES WERE INSTALLED IAW SRM 51-30-4 AND 51-10-2, PAGE 21. 2 L 7 3 4F RT A3WE 1998121100639 19981211 00639 NM 1998 12 11 CALA9802151 1 19981208 A 5713 STRINGER BOEING 727 727243 138408D NM WS 686.50 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .5 INCH CRACK IN LT WING SECOND UPPER STRINGER FROM AFT SPAR AT WS 686.50. AN ANGLE REPAIR WAS WAS I NSTALLED IAW EA 5762-01050. 2 L 7 3 4F RT A3WE 1998121100640 19981211 00640 NM 1998 12 11 CALA9802152 1 19981209 A 5520 BRACKET BOEING 727 727243 138408D NM RT ELEV CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 1.5 INCH CRACK IN RT ELEVATOR NR 4 ATTACH HINGE BRACKET AT ELEVATOR STA 99.79. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 51-30-2, PAGE 1, 51-10-1, AND 51-10-2. 2 L 7 3 4F RT A3WE 1998121100641 19981211 00641 NM 1998 12 11 CALA9802153 1 19981209 A 5320 ANGLE BOEING 727 727243 138408D NM BS 870 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A 5 INCH CRACK IN L ANGLE AT FORWARD I/B CORNER OF RT MLG WHEEL WELL, BEHIND APU, STA 870. THE ANGLE W AS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2. 2 L 7 3 4F RT A3WE 1998121100642 19981211 00642 NM 1998 12 11 CALA9802154 1 19981209 A 5315 FLOORBEAM BOEING 727 727243 138408D NM BS 1130 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 34. A REPAIR WAS INSTALLED IAW ECRA 5310-03790. 2 L 7 3 4F RT A3WE 1998121100643 19981211 00643 NM 1998 12 11 CALA9802155 1 19981209 A 5751 652172517 SKIN BOEING 727 727243 138408D NM LT AILERON DEBONDED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND LT O/B AILERON TRAILING EDGE O/B CORNER DEBONDED. THE AILERON WAS REMOVED, REPAIRED, AND REINSTALLED I AW SRM 51-30-2, PAGE 18 AND 51-8-4. 2 L 7 3 4F RT A3WE 1998121100644 19981211 00644 NM 1998 12 11 CALA9802156 1 19981209 A 5754 65162267A STIFFENER BOEING 727 727243 138408D NM NR 2 LE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND THE LT WING NR 2 LE FLAP O/B HINGE CORRODED AROUND HINGE ARM BOLTS AND O/B VERTICAL STIFFENER HAD CORRO SION AROUND BONDING WIRE BOLT HOLE. THE NR 2 LE FLAP WAS REPLACED IAW MM 27-81-1, PAGES 404-406. 2 L 7 3 4F RT A3WE 1998121100645 19981211 00645 NM 1998 12 11 CALA9802157 1 19981209 A 3350 900542 POWER SUPPLY BELL BOEING 727 727243 138408D NM CABIN INOP A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND RT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-50-0. 2 L 7 3 4F RT A3WE 1998121100646 19981211 00646 NM 1998 12 11 CALA9802158 1 19981209 A 3350 90052 POWER SUPPLY BELL BOEING 727 727243 138408D NM CABIN INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND LT OVERWING CABIN INTERIOR EMERGENCY LIGHT INOPERATIVE. THE POWER SUPPLY WAS REPLACED IAW MM 33-50-0. 2 L 7 3 4F RT A3WE 1998121100647 19981211 00647 WP 1998 12 11 CALA9802159 1 19981209 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 1701 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND FRAME CORRODED IN LOWER LOBE CENTER CARGO BILGE AREA AT STA 1701 BETWEEN STRINGER 48R AND 48L. THE FRA ME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-31-01 AND 51-31-01. 2 L 7 3 4F A22WE 1998121100648 19981211 00648 WP 1998 12 11 CALA9802160 1 19981209 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 1902-1921 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 1902 TO 1921, RBL 26. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-31-01. 2 L 7 3 4F A22WE 1998121100649 19981211 00649 WP 1998 12 11 CALA9802161 1 19981208 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 218 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12539 45792 INSPECTION FOUND FUSELAGE SKIN BULGED AT STA 218 BETWEEN LONGERONS 17R AND 18R. THE BULGED AREA WAS REMOVED AND A REPAI R WAS INSTALLED IAW SRM 53-04, PAGE 208, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1998121100650 19981211 00650 WP 1998 12 11 CALA9802162 1 19981208 A 5220 MECHANISM DOUG DC9 DC982 3022082 WP EMER EXIT DOOR OUT OF ADJMT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 92874 49122 THE OVERWING EMERGENCY EXIT DOORS ON BOTH SIDES WERE DIFFICULT TO CLOSE/OPEN. ALL EMERGENCY EXIT DOORS WERE ADJUSTED IA W MM 52-21-00. 2 L 7 2 4F A6WE 1998121100651 19981211 00651 NE 1998 12 11 9810566628 2 19981204 A 7200 ENGINE BOEING 747 747251B 1384892 NM PWA JT9 JT9D7Q 52054 NE NR 2 FLAMED OUT A NWAA O OTHER X ENGINE FLAMEOUT DE DESCENT 1 GL 01 628US 22389 702168 AT TOP OF DESCENT FROM FL410, THE NR 2 ENGINE FLAMED OUT. THE DESCENT CONTINUED TO FL260 WHEN THE ENGINE WAS RESTARTED. ENGINE OPERATION WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER FIM 71-01-00, PG 20 9 WITH NO DEFECTS NOTED. THE MAIN FUEL FILTER WAS REPLACED AS A PRECAUTION. FOLLOW-UP ENGINE RUN FOUND NO DISCREPANCIE S AND THE AIRCRAFT CONTINUED IN SERVICE. 2 L 7 4 4F 4 F A20WE E3NE 1998121100652 19981211 00652 WP 1998 12 11 9810579753 1 19981205 A 3222 STRUT DOUG DC9 DC941 302207N WP NLG REQD SERVICE A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 753NW 47117 AFTER DEPARTURE, LANDING GEAR WOULD NOT RETRACT. FLIGHT CREW REPORTED A RED NOSE LANDING GEAR UNSAFE LIGHT ILLUMINATION . FOLLOWED COM PROCEDURES, CONTINUTED TO DESTINATION AT FL90, AND LANDED WITHOUT INCIDENT. YELLOW EMERGENCY DECLARED P RECAUTIONARY. MAINTENANCE SERVICED AND RESEALED THE NOSE LANDING GEAR. OPERATIONAL CHECK NORMAL AFTER LANDING GEAR SWI NG PROCEDURES. 2 L 7 2 4F A6WE 1998121100653 19981211 00653 NM 1998 12 11 UPS98228278 1 19981208 A 2612 FIRE DETECTOR BOEING 727 727173C 1384059 NM WHEEL WELL MALFUNCTIONED A IPXA O OTHER N FALSE WARNING CL CLIMB 1 SO 01 938UP 19506 INSPECTION TYPE-N/A, WHEEL WELL FIRE LIGHT INTER ON CLIMBOUT. CHECKLIST COMPLETED, LIGHT REMAINED OUT. WHEEL WELL FIRE DETECTION SYSTEM DEFERRED IAW MEL REF 26-8. CONTROL NR M-163903 ASSIGNED DMP COMPLIED WITH PLACARD INSTALLED. CLEARED DEFFERAL SEE ITEM 1 P-321667, PLACARD REMOVED, OK FOR CONTINUED SERVICE. 2 L 7 3 4F A3WE 1998121100654 19981211 00654 NM 1998 12 11 QXEA01766 1 19981112 A 5753 TRACKS DHAV DHC8 DHC8102 2809003 NM LT TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 LEFT-HAND NR 1 AND RIGHT-HAND NR 2 FLAP TRACKS HAVE PITTING CORROSION ON BACK SIDE OF TRACK. REPAIRED IAW DHC-8 RD 8-57 -1282. 2 H 7 2 4T RT A13NM 1998121100655 19981211 00655 NM 1998 12 11 QXEA01767 1 19981119 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 NR 2 NACELLE OUTBOARD SIDE LOOSE RIVETS AND RIVETS PULLED THROUGH SKIN AT STATION 134.68 AND 24.25. REPAIRED IAW DHC-8 RD 8-54-983. 2 H 7 2 4T RT A13NM 1998121100656 19981211 00656 NM 1998 12 11 QXEA01768 1 19981012 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 NR 2 NACELLE INBOARD SIDE LOOSE RIVETS AND RIVET HEADS WORN THROUGH ON STRAP AT STATION XN 182.70. REPAIRED IAW DHC-8 R D 8-54-215, PAGE 5. 2 H 7 2 4T RT A13NM 1998121100657 19981211 00657 NM 1998 12 11 QXEA01769 1 19981119 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 NR 2 NACELLE INBOARD SIDE LOOSE RIVETS AND RIVETS WORN THROUGH SKIN AT STATION XN 134.68. REPAIRED IAW DHC - RD 8-54-98 3. 2 H 7 2 4T RT A13NM 1998121100658 19981211 00658 NM 1998 12 11 QXEA01770 1 19981103 A 5542 SKIN DHAV DHC8 DHC8102 2809003 NM RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 FORE RUDDER LEADING EDGE SKIN CRACKED AT BASE ON LEFT SIDE. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1998121100659 19981211 00659 NM 1998 12 11 QXEA01771 1 19981030 A 5522 SKIN DHAV DHC8 DHC8102 2809003 NM RT ELEVATOR DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 RIGHT-HAND ELEVATOR TOP SKIN STATION YH139.00 TO YH150.00 HAS COUNTER SUNK RIVETS PULLING THROUGH THE SKIN. REPAIRED IA W DHC-8 SRM 51-40-00. 2 H 7 2 4T RT A13NM 1998121100660 19981211 00660 NM 1998 12 11 QXEA01772 1 19981029 A 5522 SKIN DHAV DHC8 DHC8102 2809003 NM LT ELEVATOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 LEFT-HAND UPPER ELEVATOR HORN, NUMEROUS LOOSE RIVETS WEARING INTO SKIN. REPAIRED IAW DHC-8 SRM 51-40-11. 2 H 7 2 4T RT A13NM 1998121100661 19981211 00661 NM 1998 12 11 QXEA01773 1 19981103 A 5540 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 FORE RUDDER TRAILING TOP FAIL-SAFE FITTING HAS MECHANICAL DAMAGE. REPAIRED IAW DHC-8 RD 8-55-123. 2 H 7 2 4T RT A13NM 1998121100662 19981211 00662 NM 1998 12 11 QXEA01774 1 19981103 A 5540 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 FORE RUDDER LOWER FORWARD FAIL-SAFE FITTING HAS EXCESSIVE DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-00, PARAGRAPH 2, PAGE 2 TABLE 1 AND PARAGRAPH 3A, PAGE 4, TABLE 4. 2 H 7 2 4T RT A13NM 1998121100663 19981211 00663 NM 1998 12 11 QXEA01775 1 19981116 A 2722 LUGS DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 FORE RUDDER ACTUATOR ATTACHMENT LUGS HAVE MECHANICAL DAMAGE ON BOTTOM SURFACES. REPAIRED IAW DHC-8 SRM 51-30-26. 2 H 7 2 4T RT A13NM 1998121100664 19981211 00664 NM 1998 12 11 QXEA01776 1 19981104 A 5540 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 FORE RUDDER UPPER FORWARD FAIL-SAFE FITTING HAS FRETTING DAMAGE. REPAIRED IAW DHC-8 SRM 51-40-00, TABLE 1 AND TABLE 4. 2 H 7 2 4T RT A13NM 1998121100665 19981211 00665 NM 1998 12 11 QXEA01777 1 19981116 A 5540 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 TRAILING RUDDER BOTTOM RADIUS ARM FITTING HAS EXCESSIVE DAMAGE. REPAIRED IAW DHC-8 SRM 51-30-26. 2 H 7 2 4T RT A13NM 1998121100666 19981211 00666 NM 1998 12 11 QXEA01778 1 19981119 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM FUSELAGE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 DENT LEFT-HAND SIDE FUSELAGE SKIN STRINGER 28S, JUST FORWARD OF FORWARD PRESSURE BULKHEAD. REPAIRED IAW DHC-8 RD 8-53-3 909. 2 H 7 2 4T RT A13NM 1998121100667 19981211 00667 NM 1998 12 11 QXEA01779 1 19981012 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 488.5 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 DENT ON RIGHT-HAND FUSELAGE SKIN BETWEEN STRINGER 16 AND 17, FORWARD OF STATION X488.50. REPAIRED IAW DHC-8 RD 8-53-390 3. 2 H 7 2 4T RT A13NM 1998121100668 19981211 00668 NM 1998 12 11 QXEA01780 1 19981119 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 540 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 840PH 74 FUSELAGE RIGHT-HAND SIDE STRINGER 6 STATION X540 DENTED. REPAIRED IAW DHC-8 RD 8-53-3908. 2 H 7 2 4T RT A13NM 1998121100669 19981211 00669 NM 1998 12 11 QXEA9801781 1 19981204 A 2610 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM FUSELAGE FAILED A QXEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 NM 09 353PH 496 YLW- SMOKE WARNING LIGHT ILLUMINATED DURING TAKEOFF ROLL, ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PLACED THE SMOKE DETECTOR ON MEL 225864. 2 H 7 2 4T RT A13NM 1998121100670 19981211 00670 NM 1998 12 11 QXEA9801782 1 19981204 A 3310 RHEOSTAT DHAV DHC8 DHC8202 2809007 NM LEFT COCKPIT FAILED A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 359PH 514 SEA- PILOT'S SIDE MAP LIGHT GOT DIM, THEN THE CIRCUIT BREAKER FOR THE PILOT MAP LIGHTS POPPED. THERE WAS A STRONG ODOR OF AN ELECTRICAL FIRE. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF FIRE. PULLED AND COLLARED THE MAP LIGHT CIRCUIT BREAKER AND PLACED ON MEL. MEL CLEARED ON 12/9/98 BY REPLACING THE CAPTAINS MAP LIGHT RHEOSTAT AND RESET THE CIRCUIT BR EAKER. OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998121100671 19981211 00671 NM 1998 12 11 QXEA9801785 1 19981204 A 2611 WIRE DHAV DHC8 DHC8202 2809007 NM CARGO SMOKE DET BROKEN A QXEA O OTHER N FALSE WARNING NR NOT REPORTED 1 NM 09 349PH 486 EAT- BAGGAGE SMOKE DETECTOR LIGHT REMAINS ON. MAINTENANCE PLACED ON MEL. MEL CLEARED ON 12/4/98 BY REPAIRING WIRES THA T GOT CAUGHT IN DOOR ROLLERS. WRAPPED WIRES TO PREVENT REOCCURRANCE. OPERATIONAL CHECKS GOOD, NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998121100672 19981211 00672 NM 1998 12 11 QXEA9801786 1 19981205 A 3231 841005 PSEU DHAV DHC8 DHC8102 2809003 NM RT MLG DOOR MALFUNCTIONED A QXEA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 827PH 14283 4739 275 RIGHT MAIN GEAR DOOR REMAINED OPEN AFTER GEAR RETRACTION. LIGHT REMAINED ON. AIRCRAFT WAS FERRIED FROM SEA TO PDX FOR REPAIRS. IN PDX MAINTENANCE REPLACED THE PSEU, OPERATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998121100673 19981211 00673 NM 1998 12 11 QXEA9801787 1 19981207 A 3320 LIGHT DHAV DHC8 DHC8102 2809003 NM ROW 4DE INOPERATIVE A QXEA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS UK UNKNOWN 1 NM 09 828PH 287 PDX- STRONG ELECTRICAL SMELL NOTED IN THE CABIN. MAINTENANCE ISOLATED TO THE OVERHEAD LIGHT AT SEAT ROW 4DE. REMOVED T HE LAMP AND PLACED ON MEL. MEL CLEARED ON 12/8/98 BY REPLACING THE LIGHT TUBE SOCKET WHICH WAS FOUND TO BE MELTED. OPE RATIONAL CHECKS GOOD. 2 H 7 2 4T RT A13NM 1998121100674 19981211 00674 NM 1998 12 11 98FDEA00735 1 19981207 A 5313 BAC1498138 STRINGER BOEING 727 727247 138408F NM BS 380-389 DENTED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 145 BS 380+9 STR 24 RT UPPER FLANGE OF STRINGER IS DENTED. *S/D* REMOVED DAMAGE, FAB, ALODINED, PRIMED AND INSTALLE D REPAIR PER FEDEX MM 51-20-151 AND FEDEX SRM 53-10-3, FEDEX EA NR 7-5310-43150. 2 L 7 3 4F A3WE 1998121100675 19981211 00675 WP 1998 12 11 ABXA9801136 1 19981130 A 5753 995777313 FITTING DOUG DOUG DC9 DC915 3022036 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 DURING C-CHECK, FOUND LEFT FLAP INBOARD FIXED VANE OUTBOARD ATTACH SUPPORT FITTING BROKEN. REPLACED FITTING IAW DC9 SRM 51-30-2, 52-30-5, AND DACO DWG 9957773. 2 L 7 2 4F A6WE 1998121100676 19981211 00676 WP 1998 12 11 ABXA9801137 1 19981201 A 5320 99101553 WEB DOUG DOUG DC9 DC932 3022066 WP BS 756-752 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND PRESSURE DECK WEB CORRODED BEYOND LIMITS AT STATION 756 TO 752, RBL 15. REPAIRED PRESSURE DECK WE B IAW DC9 SRM 53-04. 2 L 7 2 4F A6WE 1998121100677 19981211 00677 WP 1998 12 11 ABXA9801138 1 19981130 A 5312 9911840115 BLKHD STIFFENER DOUG DOUG DC9 DC932 3022066 WP BS 1087 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 67297 DURING C-CHECK, FOUND STIFFENER CRACKED AT AFT SIDE OF BULKHEAD 1087, BL 0.0. REPLACED STIFFENER IAW DC9 SRM 51-30-5 AN D 51-10-4. 2 L 7 2 4F A6WE 1998121100678 19981211 00678 WP 1998 12 11 ABXA9801139 1 19981130 A 5311 591359577 FRAME DOUG DOUG DC9 DC932 3022066 WP FRAME 1076 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FRAME 1076 CRACKED AT LONGERONS 2L AND 2R. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998121100679 19981211 00679 WP 1998 12 11 ABXA9801140 1 19981130 A 5753 5912150505 BRACKET DOUG DOUG DC9 DC932 3022066 WP LT TE FLAP CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LEFT FLAP INBOARD AFT HINGE BRACKET CORRODED AT PIVOT POINT. REPLACED AFT HINGE BRACKET IAW DC9 S RM. 2 L 7 2 4F A6WE 1998121100680 19981211 00680 WP 1998 12 11 ABXA9801141 1 19981127 A 5314 5614943 KEEL BEAM DOUG DOUG DC8 DC861 3021952 WP BS 980 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 841AX 45908 CORROSION UNDER BEAM, PANEL LKB11 IN LEFT WHEEL WELL, STATION 980. REPAIRED IAW ABX REA D853-24306, REV A. 2 L 7 4 4F 4A25 1998121100681 19981211 00681 WP 1998 12 11 ABXA9801142 1 19981123 A 5330 59114015 SKIN DOUG DOUG DC9 DC932 3022066 WP BS 194 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND SKIN CRACKED AT STATION 194, LONGERON 22L. REPAIRED SKIN IAW ABX EA 53300001-003. 2 L 7 2 4F A6WE 1998121100682 19981211 00682 WP 1998 12 11 ABXA9801143 1 19981123 A 5330 591143267 SKIN DOUG DOUG DC9 DC932 3022066 WP BS 1080 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND INTERNAL FUSELAGE SKIN AT STATION 1080 CRACKED BETWEEN LONGERON 1R AND 2R. REPAIRED IAW DC9 SRM 5 3-04. 2 L 7 2 4F A6WE 1998121100683 19981211 00683 WP 1998 12 11 ABXA9801144 1 19981123 A 5753 99576003 FITTING DOUG DOUG DC9 DC932 3022066 WP LT TE FLAP CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LEFT FLAP OUTBOARD HINGE INTERNAL ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AN D 51-30-2. 2 L 7 2 4F A6WE 1998121100684 19981211 00684 WP 1998 12 11 ABXA9801145 1 19981123 A 5412 49125402 BLKHD FITTING DOUG DOUG DC9 DC932 3022066 WP RT PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND RIGHT PYLON BULKHEAD AT STATION 965 INBOARD ATTACH FITTING CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5. 2 L 7 2 4F A6WE 1998121100685 19981211 00685 WP 1998 12 11 ABXA9801146 1 19981123 A 5530 591218836N ANGLE DOUG DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND VERTICAL STABILIZER ATTACH ANGLE RIGHT SIDE CRACKED AT LOWER AFT CORNER. REPAIRED ANGLE IAW DC9 S RM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1998121100686 19981211 00686 WP 1998 12 11 ABXA9801147 1 19981123 A 5720 39132091 FITTING DOUG DOUG DC9 DC932 3022066 WP BS 600 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND CENTER WING FORWARD SPAR ATTACH FITTING AT STATION 600 AND LONGERON 24R CRACKED. REPLACED FITTING IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998121100687 19981211 00687 WP 1998 12 11 ABXA9801148 1 19981123 A 5312 9912243109 BULKHEAD WEB DOUG DOUG DC9 DC932 3022066 WP LT PYLON CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LEFT PYLON BULKHEAD FORWARD LOWER SIDE CORRODED. REPLACED WEB ON PYLON BULKHEAD IAW DC9 SRM 51-30 -2, 51-30-5, AND 51-30-1. 2 L 7 2 4F A6WE 1998121100688 19981211 00688 WP 1998 12 11 ABXA9801149 1 19981104 A 5712 5769466 RIB DOUG DOUG DC8 DC863 302198A WP WS 622.5 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 RIGHT WING LEADING EDGE RIB STATION XFS 622.5 IS CRACKED AT THE AFT LOWER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1 -20D. 2 L 7 4 4F 4A25 1998121100689 19981211 00689 WP 1998 12 11 ABXA9801150 1 19981104 A 5712 576946620 RIB DOUG DOUG DC8 DC863 302198A WP WS 628.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 RIGHT WING LEADING EDGE RIB STATION 628.75 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW DWG K05056 AND DC8 SRM 51-1-20 D. 2 L 7 4 4F 4A25 1998121100690 19981211 00690 WP 1998 12 11 ABXA9801151 1 19981104 A 5712 576947019 RIB DOUG DOUG DC8 DC863 302198A WP WS 766.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING LEADING RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 766.250. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998121100691 19981211 00691 WP 1998 12 11 ABXA9801152 1 19981104 A 5712 576947023 RIB DOUG DOUG DC8 DC863 302198A WP WS 778.75 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 LEFT WING LEADING EDGE RIB UPPER ARM CRACKED BY AFT FASTENER AT STATION XFS 778.750. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998121100692 19981211 00692 WP 1998 12 11 ABXA9801153 1 19981031 A 5720 9755297 ANGLE DOUG DOUG DC8 DC863 302198A WP WS 454 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 823AX 46122 RIGHT WING LEADING EDGE, INBOARD OF STATION XW454 RIB, VERTICAL ANGLE CRACKED AT LOWER END. REPAIRED IAW DC8 SRM 51-1-2 1, 51-3-0 AND DWG 9755297. 2 L 7 4 4F 4A25 1998121100693 19981211 00693 WP 1998 12 11 ABXA9801154 1 19981202 A 5400 591326237 ANGLE DOUG DOUG DC9 DC914 3022034 WP NR 1 PYLON CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 DURING C-CHECK, FOUND NR 1 LOWER PYLON ATTACH ANGLE CRACKED IN RADIUS ON FORWARD EDGE. REPAIRED ANGLE IAW DC9 SRM 54-04 . 2 L 7 2 4F A6WE 1998121100694 19981211 00694 WP 1998 12 11 ABXA9801155 1 19981202 A 5320 591008527 JAMB DOUG DOUG DC9 DC914 3022034 WP SERVICE DOOR CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 DURING C-CHECK, FOUND SERVICE DOOR JAMB INTERNAL WEB CRACKED 2 PLACES AT UPPER HINGE CUTOUT, STATION 160. REPAIRED IAW ABX REA D953-25631. 2 L 7 2 4F A6WE 1998121100695 19981211 00695 WP 1998 12 11 ABXA9801160 1 19981207 A 7997 WIRE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE BROKEN A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 985AX 47522 656800 RIGHT ENGINE OIL TEMPERATURE INDICATION EXTREME HIGH END OF SCALE DURING CRUISE FLIGHT. ALL INDICATIONS NORMAL. PERFOR MED ENGINE SHUTDOWN. FOUND WIRE E355A18N BROKEN AT GROUND LUG 906. REPAIRED WIRE. ALSO, FOUND FOUR GROUND TERMINAL BR ACKETS AND LUG HARDWARE MOUNTED INCORRECTLY. REPLACED ALL FOUR GROUND TERMINAL BRACKETS ON TOP OF ENGINE AND INSTALLED GROUND HARDWARE, ROUTED AND INSTALLED WIRING IAW DC9 OVERHAUL MANUAL 71-00. RAN ENGINE, ALL ENGINE INDICATIONS GOOD. 2 L 7 2 4F 4 F A6WE E2EA 1998121100696 19981211 00696 WP 1998 12 11 ABXA9801161 1 19981206 A 7997 36153 WIRE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D9A 52048 NE NR 2 ENGINE BROKEN A ABXA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 985AX 47522 656800 RIGHT ENGINE OIL TEMPERATURE INDICATION EXTREME HIGH END OF SCALE DURING CRUISE FLIGHT. CHECKED AND RESET CIRCUIT BREAK ER. ALL OTHER INDICATIONS NORMAL. PERFORMED ENGINE SHUTDOWN. FOUND BROKEN WIRE AT RIGHT ENGINE GROUND BLOCK ON TOP OF ENGINE. REPAIRED IAW DC9 WDM 79-33-01. ENGINE RUN ACCOMPLISHED. SYSTEM OPERATED NORMAL. 2 L 7 2 4F 4 F A6WE E2EA 1998121100697 19981211 00697 WP 1998 12 11 ABX9801162 1 19981123 A 5313 59114329 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LONGERON 2L CRACKED AT STATION 1076. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998121100698 19981211 00698 WP 1998 12 11 ABXA9801163 1 19981123 A 5313 59114329 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 1076 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LONGERON 2R CRACKED AT STATION 1076. REPAIRED LONGERON 2R IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998121100699 19981211 00699 WP 1998 12 11 ABXA9801164 1 19981123 A 5313 593643611 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LONGERON 12R CRACKED AT STATION 965. REPAIRED LONGERON IAW DC9 SRM DWG K05864. 2 L 7 2 4F A6WE 1998121100700 19981211 00700 WP 1998 12 11 ABXA9801165 1 19981123 A 5313 59114277 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LONGERON 16R CRACKED AT STATION 945. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998121100701 19981211 00701 WP 1998 12 11 ABXA9801166 1 19981123 A 5313 591140123 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 200 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LONGERON 24L CRACKED AT STATION 200. REPAIRED IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998121100702 19981211 00702 WP 1998 12 11 ABXA9801167 1 19981123 A 5313 591140125 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 160 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LONGERON 25L CRACKED AT STATION 160. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998121100703 19981211 00703 WP 1998 12 11 ABXA9801168 1 19981123 A 5313 39146771 LONGERON DOUG DOUG DC9 DC932 3022066 WP BS 794-813 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND LONGERON 30 CRACKED AT SPLICE BETWEEN STATION 794 TO 813. REPAIRED LONGERON IAW DC9 SRM 53-02. 2 L 7 2 4F A6WE 1998121100704 19981211 00704 WP 1998 12 11 ABXA9801169 1 19981118 A 5312 97537513 BULKHEAD DOUG DOUG DC8 DC861 3021952 WP BS 680 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 842AX 46015 PRESSURE BULKHEAD FS 680, 16 INCHES FROM BOTTOM, TWO CRACKS, ONE RUNS HORIZONTALLY FROM CENTER TO THE RIGHT 18 INCHESLON G, AND SECOND RUNS FROM CENTER HORIZONTALLY TO THE LEFT 4.5 INCHES LONG. REPAIRED IAW DC8 SRM 53-2-5. 2 L 7 4 4F 4A25 1998121100705 19981211 00705 WP 1998 12 11 ABXA9801170 1 19981123 A 5320 595604018 STIFFENER DOUG DOUG DC9 DC932 3022066 WP BS 760 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND STIFFENER ON LONGERON 28R, AT STATION 760 CRACKED. INSTALLED NEW STIFFENER IAW DC9 SRM 51-30-2 AN D 57-30-5. 2 L 7 2 4F A6WE 1998121100706 19981211 00706 WP 1998 12 11 ABXA9801171 1 19981123 A 5320 595604021 STIFFENER DOUG DOUG DC9 DC932 3022066 WP BS 760 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND STIFFENER ON LONGERON 30 AT STATION 760 CRACKED. REPAIRED STIFFENER IAW DC9 SRM DWG K05159. 2 L 7 2 4F A6WE 1998121100707 19981211 00707 WP 1998 12 11 ABXA9801172 1 19981123 A 5320 595604017 STIFFENER DOUG DOUG DC9 DC932 3022066 WP BS 760 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND STIFFENER ON LONGERON 28L, STATION 760, CRACKED. REPLACED STIFFENER IAW DC9 SRM 51-30-2, 51-30-5 AND DC9 SRM DWG 5956040. 2 L 7 2 4F A6WE 1998121100708 19981211 00708 WP 1998 12 11 ABXA9801173 1 19981123 A 5320 995823869N SHEAR-TIE DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FRAME SHEAR-TIE AT STATION 980 AND LONGERON 14L CRACKED. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 A ND 51-30-5. 2 L 7 2 4F A6WE 1998121100709 19981211 00709 WP 1998 12 11 ABXA9801174 1 19981123 A 5320 995823870N SHEAR-TIE DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FRAME SHEAR-TIE CRACKED AT STATION 980 AND LONGERON 14R. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-2 A ND 51-30-5. 2 L 7 2 4F A6WE 1998121100710 19981211 00710 WP 1998 12 11 ABXA9801175 1 19981123 A 5320 995773925 SHEAR-TIE DOUG DOUG DC9 DC932 3022066 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FRAME SHEAR-TIE CRACKED AT STATION 945 BETWEEN LONGERONS 15R AND 16R. REPLACED SHEAR-TIE IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1998121100711 19981211 00711 WP 1998 12 11 ABXA9801176 1 19981123 A 5311 99582387 FRAME DOUG DOUG DC9 DC932 3022066 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 982AX 47317 DURING C-CHECK, FOUND FRAME AT STATION 980 CRACKED BETWEEN LONGERONS 14R AND 17R. REPAIRED FRAME IAW DC9 SRM 53-03. 2 L 7 2 4F A6WE 1998121100712 19981211 00712 WP 1998 12 11 ABXA9801177 1 19981203 A 5511 56469731 SPAR CAP DOUG DOUG DC8 DC861 3021952 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 841AX 26448 LEFT HORIZONTAL STABILIZER HAS CORROSION ON AFT FLANGE, FORWARD LOWER SPAR CAP. REPAIRED IAW ABX REA D855-24384MR. 2 L 7 4 4F 4A25 1998121100713 19981211 00713 WP 1998 12 11 ABXA9801178 1 19981203 A 5511 56407941 SPAR CAP DOUG DOUG DC8 DC861 3021952 WP HORIZ STAB CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 841AX 45908 LEFT HORIZONTAL STABILIZER HAS CORROSION DAMAGE IN BARREL NUT HOLES IN UPPER FORWARD SPAR CAP. REPAIRED IAW ABX REA D85 5-24382MR, REV A. 2 L 7 4 4F 4A25 1998121100714 19981211 00714 WP 1998 12 11 ABXA9801179 1 19981203 A 5711 4640855 SPAR CAP DOUG DOUG DC8 DC861 3021952 WP WS 26 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 841AX 45908 NR 3 MAIN TANK ACCESS PANEL NR 506A, LOWER CENTER SPAR IS CRACKED BETWEEN FUEL TRANSFER SLOTS AND FASTENERS AT STATION X RS 26. REPAIRED IAW ABX REA D857-24357MR, REV F. 2 L 7 4 4F 4A25 1998121100715 19981211 00715 NM 1998 12 11 SCNA98148 1 19981204 A 3397 WIRE BOEING 727 727282 138408T NM CABIN FAILED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 281SC 21949 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTING WAS FOUND TO BE INOPERATIVE IN THE AFT SECTION OF TH E CABIN. REMOVED AND REPLACED SUPPLY WIRES UNDER CARPET TO SIDEWALL. OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998121100716 19981211 00716 NM 1998 12 11 SCNA98743 1 19981204 A 3350 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A HEAVY MAINT CHECK, THE FORWARD EMERGENCY EXIT SIGN WAS FOUND INOPERATIVE. REMOVED AND REPLACED MARATHON PACK A ND CHARGER IAW B727 MM 335022. OPS CHECK DONE IAW 335001. OPS CHECK GOOD. 2 L 7 3 4F A3WE 1998121100717 19981211 00717 NM 1998 12 11 P5CA9801614 1 19981204 A 5350 FAIRING BOEING 747 747249F 1384849 NM TAIL CONE DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 806FT 21827 NR 8 FIXED FAIRING TAIL CONE LOWER SKIN FOUND DELAMINATED. SANDED DOWN DELAMINATION AREA AND REPARIED PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998121100718 19981211 00718 NM 1998 12 11 P5CA9801615 1 19981202 A 5400 FAIRING BOEING 747 747132 1384882 NM NR 4 ENGINE DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 4 ENGINE FWD FAIRING HAS A HOLE WORN THRU STRUCTURE. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1998121100719 19981211 00719 NM 1998 12 11 P5CA9801616 1 19981203 A 7110 COWL BOEING 747 747132 1384882 NM NR 3 ENGINE HOLE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 NR 3 ENGINE OUTBOARD CORE COWL HAS HOLE IN SKIN AND TEMPORARY FASTENER INSTALLED. FABRICATED DOUBLER AND INSTALLED PER SRM 54-30-03. 2 L 7 4 4F A20WE 1998121100720 19981211 00720 NM 1998 12 11 P5CA9801617 1 19981204 A 4980 LINER BOEING 747 747132 1384882 NM APU EXHAUST CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 APU EXHAUST INNER LINER HAD 12 INCH CRACK. REMOVED AND REPLACED EXHAUST LINER PER MM 49-81-03. 2 L 7 4 4F A20WE 1998121100721 19981211 00721 NM 1998 12 11 P5CA9801618 1 19981204 A 5755 SPOILER BOEING 747 747132 1384882 NM NR 12 SPOILER HOLE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 RIGHT WING NR 12 SPOILER HAS SMALL HOLE IN TOP SIDE SURFACE. CLEANED, POTTED DAMAGED AREA AND REPAIRED PER SRM 51-40-06 . 2 L 7 4 4F A20WE 1998121100722 19981211 00722 NM 1998 12 11 P5CA9801619 1 19981204 A 5753 SKIN BOEING 747 747132 1384882 NM LT TE FOFEFLAP HOLE A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 857FT 20246 LEFT WING OUTBOARD POSITION FORE FLAP LEADING EDGE HAS HOLE IN PREVIOUS REPAIR. REPAIRED DAMAGED AREA PER SRM 51-40-09. 2 L 7 4 4F A20WE 1998121700002 19981217 00002 WP 1998 12 17 ARWA981202 1 19981203 A 3231 450100109 SWITCH LKHEED 1011 10113851 5265010 WP COCKPIT INOP A ARWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 19 306GB 1138 ON TAKEOFF, GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR CONTROL SWITCH. OPERATION CHECKED NORMAL IAW M/M 32-31-14. (NO FUEL DUMPED). 2 L 7 3 4F RT A23WE 1998121700003 19981217 00003 NM 1998 12 17 CALA9802143 1 19981205 A 2540 OUTLET BOEING 777 777224 1385225 NM LAVATORY SHORTED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 78002 27578 SMOKE CAME INTERMITTENTLY FROM THE SHAVER OUTLET IN LAV AT DOOR 2-L WHILE AT CRUISE. THE CIRCUITS WERE DEACTIVATED AND THE SMOKE STOPPED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND SOAP LEAKING FROM SPARE SOAP BOTTLE STORED ABOVE SHAVER OU TLET CAUSING A SHORT TO GROUND AT SHAVER OUTLET. THE CANNON PLUG FOR SHAVER WAS DISCONNECTED AND THE SHAVER OUTLET WAS PLACED ON PLACARD. THE OUTLET IS TO BE REPLACED. 2 L 7 2 4F RT T00001SE 1998121700005 19981217 00005 NM 1998 12 17 DL72E982492 1 19981203 A 5320 WEB BOEING 727 727247 138408F NM BS 1243 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2829W 21481 REF SHIP 576 TPA LTR CHK C2 12-03-98, .25 INCH CRACK IN TORQUE BOX VERT WEB RT SIDE STA 1243, .5 INCH CRACK IN TORQUE BO X VERT WEB LT SIDE STA 1323. REPAIRED BOTH ITEMS PER MM 53-11-0. 2 L 7 3 4F A3WE 1998121700006 19981217 00006 NE 1998 12 17 DLL19982499 2 19981206 A 7200 ENGINE PAC102MK4 LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 1 FLAMED OUT A DALA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CR CRUISE 1 SO 27 759DA B1857 193Y1176 014781 NR 1 ENG FLAMED OUT AT 39000 FT. SHUTDOWN ENG PER POM. RELIGHT NR 1 PER POM. REPLACED ENGINE DRIVEN FUEL PUMP. 2 L 7 3 4F 4 F A23WE E12EU 1998121700007 19981217 00007 1998 12 17 DLM88982501 4 19981206 A 3425 4055900905 NAV DISPLAY DOUG MD88 MD88 3023688 NM COCKPIT FAILED A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 27 931DL 49718 CAPTS NAV DISPLAY FUZZY. SWITCHED TO EIFS BOTH ON 2, NO HELP. SWITCHED BACK TO NORMAL AND THE CAPTS PRI FLT DISPLAY SI ZZLED AND WENT BLANK. USED COMPACT ON LOWER SCREEN BUT, STILL FUZZY. HAD ELEC SMELL AND SMOKE. PULLED C/B'S AND DIVER TED TO BUF. REPLACED CAPT PFD. 2 L 7 2 4F RT A6WE 1998121700010 19981217 00010 NM 1998 12 17 CALA9802109 1 19981124 A 5330 SKIN BOEING 737 737824 13844BZ NM BS 794 DAMAGED A CALA K NONE C F.O.D. TX TAXI/GRND HDL 1 SW 09 14214 28774 THE RT FUSELAGE SKIN WAS CREASED FORWARD OF THE AFT CARGO AREA AT STA 794 WHEN STRUCK BY A FUEL TRUCK. AN EXTERNAL LAP SEAM DOUBLER REPAIR WAS INSTALLED USING SOLID RIVETS IAW SRM 53-00-01. 2 L 7 2 4F RT A16WE 1998121700011 19981217 00011 NM 1998 12 17 DLM90982422 1 19981119 A 5330 5953050555 SKIN DOUG MD90 MD9030 3023690 NM BS 230 PUNCTURED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 910DN 53390 THE FUSELAGE SKIN WAS PUNCTURED BY A JETWAY JUST BELOW THE LONGERON 18L CUSP LINE AT FS 230. THE DAMAGED SKIN WAS TRIMM ED AWAY AND REPAIRED WITH AN EXTERNAL REPAIR DOUBLER PER THE GUIDELINES OF THE MD-90 SRM 53-30-01, FIG 3. THE REPAIR AN D INSPECTION REQUIREMENTS WERE DOCUMENTED PER ER/A 366122-14. 2 L 7 2 4F RT A6WE 1998121700013 19981217 00013 WP 1998 12 17 VJ9800630 1 19981117 A 2560 PANEL DOUG DC9 DC932 3022066 WP R-1 DOOR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 DURING SCHEDULED INSPECTION AT AERO CORP, FOUND THE R-1 FORWARD AND AFT GIRT BAR ATTACH FITTING IN THE FLOOR SPINNING. M ECHANICALLY REMOVED THE CORROSION, TREATED AND PRIMED AREA. FABRICATED AND INSTALLED NEW TRANSITION PANEL IAW DC9 SRM 5 1-30-2, 51-10-5, 51-10-3 AND 53-04. 2 L 7 2 4F A6WE 1998121800021 19981218 00021 CE 1998 12 18 98ZZZX4611 1 19980327 A 2750 ANL300 CURRENT LIMITER CESSNA 650 650 2076802 CE TE FLAP FAILED A HEEA L A ABORTED APPROACH UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 03 910M 6500069 ON MARCH 27, 1998, AT 1330 ON APPROACH TO ASPEN, COLORADO, THE PILOTS GOT AN INOPERATIVE INDICATION FOR THE FLAP MOTOR. ABORTED LANDING AND DIVERTED TO DENVER. REPLACED THE FLAP MOTOR. CURRENT LIMITER CHECKED OKAY. RETURNED TO SERVICE. REF: CESSNA 650 WIRING DIAGRAM, CHAPTER 27-5001, FIGURE 1, ITEM 23. 2 L 7 2 4F A9NM 1998121800022 19981218 00022 EA 1998 12 18 98ZZZX4612 2 19981103 A 7200 ENGINE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RIGHT MALFUNCTIONED A HEEA E A ENGINE SHUTDOWN UNSCHED LANDING B R SMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 03 500PH 7402 3009 PCE81768 BL29 PCE81768 SHORTLY AFTER TAKEOFF, PILOT REPORTED 'SMALL EXPLOSION' WITH SPARKS AND 'SMOKE' FROM THE RT ENGINE. SECURED SAME AND RE TURNED TO AIRPORT AND MADE UNEVENTFUL SINGLE ENGINE LANDING. MAINTENANCE FOUND N1 SECTION OF ENGINE LOCKED UP. NII SEC TION FREE TO ROTATE. 1 L 7 2 4T 4 T A24CE E4EA 1998121800031 19981218 00031 CE 1998 12 18 98ZZZX4619 1 19981110 A 7920 SEAL LEAR 25 25 5170506 CE ENGINE OIL DAMAGED A KKFA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 813JW 5983 25038 WHILE EN ROUTE TO YIPSILANTI, THE RT OIL PRESSURE WAS DECREASING FOLLOWED BY RT GENERATOR FAILURE. A PRECAUTIONARY ENGI NE SHUT DOWN WAS MADE AND AIRCRAFT DIVERTED TO ANOTHER AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE. OIL LEVEL WAS FOUN D TO BE LOW DUE TO A DAMAGED OIL SEAL. THIS OIL SOAKED THE GENERATOR. OIL SEAL AND GENERATOR WERE REPLACED, LEAK CHECK ED, AND FUNCTIONALLY TESTED. OIL FILTER AND SUMP PLUG WERE INSPECTED, NO DAMAGE NOTED. 2 L 7 2 4J A10CE 1998121800058 19981218 00058 NM 1998 12 18 SWAA983059 1 19981203 A 5520 BACB28X3C010 BUSHING BOEING 737 7372T4 1384492 NM LT ELEVATOR FAILED A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 07 722WN 22698 STRONG VIBRATION NOTICED AT CRUISE, FLIGHT 240, 310 KTS, IT WAS NOTICEABLY WORSE IN THE REAR OF THE PLANE AND PILOTS COU LD FEEL VIBRATION IN RUDDER. VIBRATION WAS INTERMITTENT AT LOWER ALTITUDES AND SLOWER SPEEDS. REMOVED CRANK ASSY ON LT ELEVATOR INSTALLED NEW BUSHING AND OPS CK GOOD PER MM. 2 L 7 2 4F A16WE 1998121800059 19981218 00059 NM 1998 12 18 SWAA983060 1 19981203 A 5330 SKIN BOEING 737 7372T4 1384492 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 721WN 22697 ON WALKAROUND FOUND APPROX 3 INCH SKIN CRACK LEFT SIDE AFT AND ABOVE TRAILING EDGE FLAPS AS MARKED WITH DYE CHECK. INST ALLED REPAIR PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800060 19981218 00060 NM 1998 12 18 SWAA983061 1 19981203 A 3350 65C27095 BATTERY BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 129SW 22340 DURING SCHEDULED CHECK, FOUND AFT SECTION OF FLOOR TRACK EMERG LIGHTING INOP. REMOVED AND REPLACED AFT FLOOR TRACK LIGH T BATTERY PACK PER M/M. 2 L 7 2 4F A16WE 1998121800061 19981218 00061 NM 1998 12 18 SWAA983062 1 19981203 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 380 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND STRINGER 26L CRACKED AT UPPER FLANGE BS 380. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800062 19981218 00062 NM 1998 12 18 SWAA983063 1 19981205 A 5210 PIN BOEING 737 7373A4 1384585 NM PAX DOOR UNSECURED A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 673AA 23251 LOUD NOISE FROM FWD ENTRY DOOR AFTER TAKEOFF. AIRCRAFT RETURNED TO BWI, FOUND HINGE PIN OUT AT UPPER HINGE COVER. RESE CURED COVER. 2 L 7 2 4F RT A16WE 1998121800063 19981218 00063 NM 1998 12 18 SWAA983064 1 19981208 A 5330 SKIN BOEING 737 7373Q8 1384670 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 689SW 23387 DURING SCHEDULED SC CHECK, FOUND A 2 INCH LONGITUDINAL FUSELAGE SKIN CRACK, AT BS 727D, STRINGER 23R. REPAIRED PER BOEI NG SRM. 2 L 7 2 4F RT A16WE 1998121800064 19981218 00064 NM 1998 12 18 SWAA983065 1 19981208 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 908-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACK, AT BS 908 TO 947, STRINGER 14L. REPAIRED PER DALFORT X EA X2-53-227. 2 L 7 2 4F A16WE 1998121800065 19981218 00065 NM 1998 12 18 SWAA983066 1 19981207 A 3350 LAMPS BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 385SW 26600 DURING SCHEDULED A1 CHECK, FOUND FLOOR TRACK LIGHTING WITH SEVERAL LIGHTS INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121800066 19981218 00066 NM 1998 12 18 SWAA983067 1 19981207 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 500 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED CHECK, FOUND FUSELAGE SKIN CRACK AT BS 500, STRINGER 10R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800067 19981218 00067 NM 1998 12 18 SWAA983068 1 19981207 A 5314 KEEL BEAM BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 062SW 22060 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CORRODED AT BS 727, AT S27 LT AND RT. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800068 19981218 00068 1998 12 18 SWAA983069 4 19981207 A 3414 C17001BA01 PITOT ADM BOEING 737 7377H4 NM NR 2 INOP A SWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 07 701GS 27836 DIVERTED TO LAS DUE TO AIRSPEED INDICATOR 10 KTS LOW AT 35,000 FT ON SHORT FINAL, INDICATOR 17 KTS SLOWER THAN CAPT AND PNEUMATIC A/S INDICATOR. DURING ADIRU BITE FOUND FAULT CODES 34-21007 AND 34-210032 AND 34-210033. TROUBLESHOT SYSTEM PER 34-21-00-2. FOUND NR 2 PITOT ADM BAD (M01753). REMOVED AND REPLACED SAME. SYS NOW OPS GOOD PER M/M. 2 L 7 2 4F RT A16WE 1998121800069 19981218 00069 NM 1998 12 18 SWAA983070 1 19981205 A 2612 OVERHEAT LOOP BOEING 737 7373Q8 1384670 NM NR 2 PYLON INOP A SWAA O OTHER N FALSE WARNING DE DESCENT 1 SW 07 688SW 23254 DURING DESCENT, RT WING OVERHEAT LIGHT ILLUMINATED, PERFORMED QRH ITEMS AND LIGHT REMAINED ON UNTIL AFTER ENG SHUT DOWN. OPENED AND INSPECTED A/C BAY AND L/E FLAP AREA, FOUND NO LEAKS. RECLOSED A/C BAY DOOR. REPLACED M488 ENG/PYLON LOOP PER M/M. 2 L 7 2 4F RT A16WE 1998121800070 19981218 00070 NM 1998 12 18 SWAA983071 1 19981205 A 5320 FRAME BOEING 737 7375H4 138449D NM EMER EXIT DRWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED CHECK, FOUND A 1 INCH CRACK IN AFT DOORWAY FRAME AT LOWER CORNER MOST I/B STOP. REPAIRED PER SWA RA 1- 553-1949. 2 L 7 2 4F RT A16WE 1998121800071 19981218 00071 NM 1998 12 18 SWAA983072 1 19981204 A 2450 D01612 RELAY BOEING 737 7373H4 1384600 NM COCKPIT FAILED A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 655WN 28400 STRONG SMELL COMING FROM ABOVE OBSERVERS JUMPSEAT BEHIND C/B PANEL. NO SMOKE OR HEAT IN THAT AREA. NOTED SMELL INTER MITTANT. LEFT AFT FUEL BOOST PUMP C/B TRIPPED. FOUND R-18 RELAY ARCHING AT D01612 RECEPTICLE. REPLACED D01612 RECEPTI CLE AND R-18 RELAY PER M/M. 2 L 7 2 4F RT A16WE 1998121800072 19981218 00072 NM 1998 12 18 SWAA983073 1 19981206 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 929/943 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 314SW 23336 DURING SCHEDULED SC CHECK, FOUND AFT FUSELAGE SKIN CRACKED AT STA 929 AND 943, AT STRINGER 23L. CRACK MEASURES 2.70 AND 1.7 LONG. INSTALLED REPAIR PER SRM. 2 L 7 2 4F RT A16WE 1998121800073 19981218 00073 NM 1998 12 18 SWAA983074 1 19981206 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 800 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SC CHECK, FOUND STRINGER CRACK AT BS 800, S10R. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1998121800074 19981218 00074 NM 1998 12 18 SWAA983075 1 19981206 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 460 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED SC CHECK, FOUND SKIN CRACKED AT SKIN LAP BS 460, S14R. REPAIRED PER SRM. 2 L 7 2 4F A16WE 1998121800075 19981218 00075 NM 1998 12 18 SWAA983076 1 19981206 A 5320 SHEAR TIE BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SHEAR TIE CRACKED AT RT BS 360 JUST BELOW S15R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800076 19981218 00076 NM 1998 12 18 SWAA983077 1 19981206 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 536 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 536, 6 UP FROM S10L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800077 19981218 00077 NM 1998 12 18 SWAA983078 1 19981206 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER SPLICE AND CLIP CRACKED AT BS 908, AT S4L. REPAIRED PER BOEING SRM . 2 L 7 2 4F A16WE 1998121800078 19981218 00078 NM 1998 12 18 SWAA983079 1 19981206 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND FUSELAGE FRAME AT STRINGER SPLICE CRACKED AT BS 663, AT S4L. REPAIRED PER B OEING SRM. 2 L 7 2 4F A16WE 1998121800079 19981218 00079 NM 1998 12 18 SWAA983080 1 19981206 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CRACKED AT BS 1016, AT S5R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800080 19981218 00080 NM 1998 12 18 SWAA983081 1 19981205 A 5330 SKIN BOEING 737 7373T5 NM BS 767 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 694SW 23061 DURING SCHEDULED SC CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, NEAR S18R. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800081 19981218 00081 NM 1998 12 18 SWAA983082 1 19981206 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 410 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND STRINGER CRACKED AT BS 410, S4L. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800082 19981218 00082 NM 1998 12 18 SWAA983083 1 19981206 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 908-947 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 908 TO 947, AT S10R AND S14R. REPAIRED PER DALFORT XE A X2-53-226. 2 L 7 2 4F A16WE 1998121800083 19981218 00083 NM 1998 12 18 SWAA983084 1 19981206 A 5330 SKIN LAP BOEING 737 7372H4 138448C NM BS 360-540 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 360 TO 540, AT S10 RT AND LT, S4 LT AND RT AND S14 LT. REPAIRED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998121800084 19981218 00084 NM 1998 12 18 SWAA983085 1 19981206 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727-908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 727 TO 908, AT S4 L AND RT, S10 RT AND LT. REPAIRED PER SWA ACO 6717-53. 2 L 7 2 4F A16WE 1998121800085 19981218 00085 NM 1998 12 18 SWAA983086 1 19981206 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 727-908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND SKIN LAP CRACKS AT BS 908 TO 1016, AT S4 LT, S10 RT AND LT. REPAIRED PER SW A ACO 6717-53. 2 L 7 2 4F A16WE 1998121800086 19981218 00086 NM 1998 12 18 SWAA983087 1 19981206 A 5320 FRAME BOEING 737 7375H4 138449D NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED C4 CHECK, FOUND FORWARD CARGO DOORWAY AFT FRAME UPPER CORNER CRACKED 1.5 INCH LONG. REPAIRED PER SWA R A 1-553-1949. 2 L 7 2 4F RT A16WE 1998121800087 19981218 00087 NM 1998 12 18 SWAA983088 1 19981206 A 5320 FRAME BOEING 737 7375H4 138449D NM CARGO DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 504SW 24181 DURING SCHEDULED C4 CHECK, FOUND FORWARD CARGO AFT DOORWAY FRAME AT UPPER CORNER CRACKED 1 INCH LONG. REPAIRED PER SWA RA 1-553-1949. 2 L 7 2 4F RT A16WE 1998121800088 19981218 00088 NM 1998 12 18 SWAA983089 1 19981205 A 3350 2012A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SC CHECK, FOUND AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1998121800089 19981218 00089 NM 1998 12 18 SWAA983090 1 19981205 A 3350 2012A BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 083SW 22732 DURING SCHEDULED SC CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F A16WE 1998121800090 19981218 00090 NM 1998 12 18 SWAA983091 1 19981205 A 3350 LAMPS BOEING 737 7375H4 138449D NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 507SW 24184 DURING SCHEDULED SC CHECK, FOUND 3 FLOOR EMERGENCY EXIT LIGHTS INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121800091 19981218 00091 NM 1998 12 18 SWAA983092 1 19981208 A 3350 LAMPS BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 374SW 26582 DURING PREFLIGHT CHECK, FOUND 3 FLOOR EMERGENCY EXIT LIGHTS INOP AND WIRES EXPOSED LT SIDE CABIN. REPAIRED AND RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121800092 19981218 00092 WP 1998 12 18 TWAA9819501 1 19981208 A 2170 1794609 COALESCER DOUG DC9 DC951 3022051 WP LT & RT CONTAMINATED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 418EA 47676 AN OFFENSIVE ODOR WAS REPORTED IN THE GALLEY AND FRONT PORTION OF THE AIRPLANE. SOME THROAT AND EYE IRRITATION. CLEANE D THE ENTRANCE AND GALLEY FLOORS, OVERHEAD BAG COMPARTMENTS, AND PSU'S IN AREA. REPLACED BOTH AIR CONDITIONING WATER SE PARATORS. CHECK-C 3-30-98 STL. 2 L 7 2 4F RT A6WE 1998121800093 19981218 00093 WP 1998 12 18 TWAA9819502 1 19981208 A 2170 1794609 COALESCER DOUG DC9 DC951 3022051 WP LT & RT CONTAMINATED A TWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 418EA 47676 AFTER SOME TIME IN CRUISE FLIGHT AN OFFENSIVE ODOR WAS REPORTED IN THE FRONT PART OF THE CABIN. THERE WERE SOME REPORTS OF THROAT IRRITATION. REPLACED BOTH WATER SEPARATORS AND RAN THE PACKS ON FULL HOT FOR TWO HOURS. CHECK-C 3-30-98 STL . 2 L 7 2 4F RT A6WE 1998121800094 19981218 00094 WP 1998 12 18 TWAA9819503 1 19981207 A 5330 SKIN DOUG DC9 DC915 3022036 WP BS 514 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 970Z 45772 DURING CHECK-C, MAINT FOUND FUSELAGE SKIN CRACKED AT STA 514, LONGERON 18R. ACCOMPLISHED FUSELAGE SKIN REPAIR PER SB 53 -141 AND DOUGLAS DRAWING JO60108. 2 L 7 2 4F A6WE 1998121800095 19981218 00095 WP 1998 12 18 TWAA9819504 1 19981208 A 5320 FRAME DOUG DC9 DC915 3022036 WP MLG DOORWAY DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 970Z 45772 DURING CHECK-C, MAINT FOUND PREVIOUS INTERIM REPAIR FOR A CRACK AT THE AFT I/B CORNER OF THE RT MAIN GEAR WHEEL WELL, TH E FRAME AT THE MLG I/B DOOR JAM, AFT I/B END. ACCOMPLISHED PERMANENT REPAIR PER ARA 11913, AND SRM 53-05, FIG 60, SHEET S 1 AND 2. 2 L 7 2 4F A6WE 1998121800096 19981218 00096 NM 1998 12 18 HNAA9894290 1 19981209 A 3350 6104791X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM CABIN INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 942HA PS028 163 SBY - FLT 3081 - AFT OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED THE POWER SUPPLY AND BASE. (M) 2 H 7 2 4T RT A13NM 1998121800097 19981218 00097 NM 1998 12 18 K3HA980146 1 19981201 A 3350 3071BPE BULB BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 TWO FORWARD EMERGENCY PATH LIGHT INOP. RELAMPED WITH NEW BULBS, OPS CHECK GOOD PER MM 33-59-00. 2 L 7 3 4F A3WE 1998121800098 19981218 00098 NM 1998 12 18 K3HA980147 1 19981206 A 3350 3071BPE LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH TRACK LIGHTS FIRST TWO RED LENS INOP. RELAMPED, OPS CHECK OK PER MM 33-59-0. 2 L 7 3 4F A3WE 1998121800099 19981218 00099 NM 1998 12 18 K3HA980148 1 19981206 A 3350 3071BPE LAMP BOEING 727 727225 1384077 NM CABIN FAILED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 EMERGENCY PATH TRACK LIGHT ONE RED LENS INOP AT RIGHT AFT LAV. RELAMPED, OPS CHECK OK PER MM 33-59-00. 2 L 7 3 4F A3WE 1998121800100 19981218 00100 NM 1998 12 18 CALA9802163 1 19981209 A 3233 273N40042 BEARING BOEING 757 757224 1384958 NM LT MLG ACTUATOR FAILED A CALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 14120 27562 THE GEAR LIGHT ON FORWARD PANEL AND GEAR DISAGREE ON EICAS ACTIVATED AFTER TAKEOFF. THE GEAR WAS CYCLED AND NORMAL INDI CATIONS WERE RECEIVED. THE FLIGHT WAS CONTINUED TO EWR WHERE IT LANDED WITHOUT FURTHER PROBLEM. TROUBLESHOOTING FOUND THE LT MLG ALTERNATE UPLOCK RELEASE ACTUATOR HEAD END AND ROD END BEARINGS BINDING. THE LT MLG ALTERNATE UPLOCK RELEASE ACTUATOR WAS REMOVED AND REPLACED IAW MM 32-35-0. A GEAR SWING WAS PERFORMED IN NORMAL AND ALTERNATE WITH NO DEFECTS F OUND. 2 L 7 2 4F RT A2NM 1998121800101 19981218 00101 NM 1998 12 18 CALA9802164 1 19981209 A 5753 6521630265 SKIN BOEING 727 727243 138408D NM LT TE FOREFLAP BENT A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND LT INBOARD FOREFLAP INBOARD MOST UPPER SKIN LOOSE AND BENT. THE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-3. 2 L 7 3 4F RT A3WE 1998121800102 19981218 00102 NM 1998 12 18 CALA9802165 1 19981209 A 5753 271526117 MOUNT PAD BOEING 727 727243 138408D NM TE FLAP TRACK CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND NR 5 FLAP TRACK AFT MOUNTING FLANGE ON FALSE SPAR WORN AND CORRODED. THE MOUNT PAD WAS REMOVED AND REP LACED IAW SRM 51-10-1, PAGE 1. 2 L 7 3 4F RT A3WE 1998121800103 19981218 00103 NM 1998 12 18 CALA9802166 1 19981209 A 5753 652165128 FITTING BOEING 727 727243 138408D NM TE FLAP TRACK CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND RT WING NR 5 FLAP TRACK FORWARD FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED IAW BOEING DRAW ING 65-19297. 2 L 7 3 4F RT A3WE 1998121800104 19981218 00104 NM 1998 12 18 CALA9802167 1 19981209 A 5520 STIFFENER BOEING 727 727243 138408D NM RT ELEVATOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .5 INCH CRACK IN RT ELEVATOR CONTROL TAB ROD STIFFENER PLATE IN COVE AREA. THE CRACKED AREA WAS REMO VED, AN ANGLE WAS INSTALLED IAW SRM 51-20-1, PAGE 7. 2 L 7 3 4F RT A3WE 1998121800105 19981218 00105 NM 1998 12 18 CALA9802168 1 19981209 A 3213 657276138 CYLINDER BOEING 727 727243 138408D NM RT MLG CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND THE RT MLG OUTER CYLINDER THREADS FOR GLAND NUT CORRODED. THE RT MLG WAS REMOVED AND REPLACED. 2 L 7 3 4F RT A3WE 1998121800106 19981218 00106 SO 1998 12 18 COMA9810278 1 19981209 A 3297 2050500101 WIRE HARNESS EMB 120 EMB120RT SO RT MLG DEFECTIVE A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 189CA 2 2 120189 LANDING GEAR WILL NOT RETRACT. REPLACED THE RIGHT HAND MLG WEIGHT ON WHEELS HARNESS. 2 L 7 2 4T RT A31SO 1998121800107 19981218 00107 EA 1998 12 18 COMA9860378 1 19981208 A 3350 110049 BATTERY CHARGER CNDAIR CL600 CL6002B19 EA PAX DOOR INOP A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 975CA 7150 EMERGENCY EXIT LIGHT ADJACENT CABIN DOOR IS INOPERABLE. REPLACED THE NR 2 BATTERY CHARGER. 2 L 7 2 4F RT A21EA 1998121800108 19981218 00108 EA 1998 12 18 COMA9860379 1 19981209 A 2760 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA SPOILERON TRIPPED A COMA D RETURN TO BLOCK F J FLT CONT AFFECTED WARNING INDICATION TX TAXI/GRND HDL 1 SO 01 927CA 7031 SPOILERON CAUTION MESSAGE. RESET CIRCUIT BREAKERS, SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1998121800109 19981218 00109 NM 1998 12 18 UPS98228282 1 19981210 A 3350 1000679 LIGHT BOEING 727 72731C 1384011 NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 922UP 19231 INSPECTION TYPE AS-E, FWD ENTRY DOOR EMERGENCY EXIT LIGHT COMES ON WHEN AIRCRAFT POWER TURNED OFF AND EMER EXIT LIGHT SW ITCH IS IN OFF POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CHECKS GOOD PER M/ M 33-50-01 (P/N 10-0067 -9), (S/N 32U) ON, (S/N 6155) OFF. 2 L 7 3 4F A3WE 1998121800110 19981218 00110 EU 1998 12 18 QXEA9801788 1 19981207 A 3350 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 481US 11230 SEVERAL CEILING EMERGENCY LIGHTS OUT. MAINTENANCE REMOVED AND REPLACED 3 BATTERY POWER SUPPLIES. OPERATIONAL CHECKED N ORMAL PER FOKKER F-28 MAINTENANCE MANUAL, CHAPTER 33-50-00. 2 L 7 2 4F RT A20EU 1998121800111 19981218 00111 NM 1998 12 18 98FDEA00736 1 19981209 A 5315 6520838 FLOORBEAM BOEING 727 727247 138408F NM BS 1130 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 195 - WHILE WORKING NR 195, FOUND CORROSION ON BS 1130 FLOORBEAM RBL 22-30, WL 208. REPAIRED FLOORBEAM IAW FEDEX EA NR 7-5310-43176A. 2 L 7 3 4F A3WE 1998121800112 19981218 00112 NM 1998 12 18 98FDEA00737 1 19981209 A 5320 65317731 CHORD BOEING 727 727247 138408F NM BS 1176 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 186 - CORROSION C53-224-08 ON 1176, REINFORCEMENT CHORD LBL 56-LBL 16 AND CORROSION AND MECHANICAL DAMAGE RBL 24-LBL 18, WL 208, BS 1176. REMOVED AND REPLACED CORROSION PER FEDEX 727 SRM 53-10-1, 51-10-2, 51-10-6, 57-30-2 AND FEDEX MM 5 7-20-151. 2 L 7 3 4F A3WE 1998121800113 19981218 00113 NM 1998 12 18 98FDEA00738 1 19981209 A 5311 6516339 FRAME BOEING 727 727247 138408F NM BS 970 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 564 - AFT CARGO BAY BS 970 FRAME IS CRACKED AT STR 26L. REMOVED AND REPLACED FLOOR SIDEWALL SUPT AT BS 950C TO BS 10 00, LBL 24, WL 146 IAW FEDEX SRM 51-30-2. REPAIRED FRAME. AFT CARGO BAY PER FEDEX SRM 51-40-3. 2 L 7 3 4F A3WE 1998121800114 19981218 00114 NM 1998 12 18 98FDEA00739 1 19981209 A 3350 1000677 LIGHT BOEING 727 727233 138408A NM CREW DOOR INOP A FDEA K NONE L NO TEST IN INSP/MAINT 1 SO 25 276FE 22041 NR 517 EMERGENCY EXIT LIGHT OVER CREW DOOR FAILED TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY, OPS CK GOOD PER FEDEX MM 33-50-0. 2 L 7 3 4F RT A3WE 1998121800115 19981218 00115 WP 1998 12 18 MWEA981138 1 19981207 A 5313 3924809501N LONGERON DOUG DC9 DC932 3022066 WP BS 603 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CORROSION ON LONGERON 30 AT STATION 603 SHOVEL END. MTC REMOVED AND REPLACED LONGERON AND FITTING. 2 L 7 2 4F A6WE 1998121800116 19981218 00116 WP 1998 12 18 MWEA981139 1 19981206 A 5320 591015837 WEB DOUG DC9 DC932 3022066 WP BS 935 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CORROSION AT FUSELAGE 935 AFT PIT DOOR JAM BY LONGERON 25 AND 26 RIGHT ON WEB SECTION. MTC REMOVED AND REPLACED W EB SECTION. 2 L 7 2 4F A6WE 1998121800117 19981218 00117 WP 1998 12 18 MWEA981140 1 19981205 A 5320 99115243 CLIP DOUG DC9 DC932 3022066 WP BS 237 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND CRACKED SHEAR CLIP AT STATION 237 BETWEEN L17 LEFT AND L18 LEFT. MTC FABRICATED AND INSTALLED SHEAR CLIP. 2 L 7 2 4F A6WE 1998121800118 19981218 00118 WP 1998 12 18 MWEA981141 1 19981205 A 5330 5911406 SKIN DOUG DC9 DC932 3022066 WP BS 229 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND SMALL GOUGE IN FUSELAGE SKIN AT FS 229 JUST BELOW L17 LEFT. MTC COLD WORKED DENT AND FOUND NO CRACKS AND FABRICAT ED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998121800119 19981218 00119 WP 1998 12 18 MWEA981142 1 19981205 A 5330 5911409 SKIN DOUG DC9 DC932 3022066 WP BS 237 DENTED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 301ME 47190 FOUND SMALL DENT ON FUSELAGE SKIN AT FUSELAGE 237 JUST BELOW L17 LEFT. MTC COLD WORKED DENT AND FOUND ON CRACKS FABRICA TED AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1998121800120 19981218 00120 WP 1998 12 18 MWEA981143 1 19980923 A 5320 991015413 CUSP DOUG DC9 DC915 3022036 WP BS 786 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN STATION 786 XT52 AT L18 RIGHT CUSP HAS AREA OF CORROSION AROUND SCREW HOLES. REMOVED CORRODED SECTION OF CUS P MAT, FABRICATED AND INSTALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998121800121 19981218 00121 WP 1998 12 18 MWEA981144 1 19981106 A 5320 991154627 SUPPORT DOUG DC9 DC915 3022036 WP BS 817 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 DISCOVERED 3 VERTICAL SUPPORTS AT STATION 817 LONGERON 27 RIGHT 27 LEFT AND 24 LEFT HAVE ELONGATED HOLES. REMOVED AND R EPLACED LEN VERTICAL SUPPORT, FABRICATED DOUBLER FILLER REPAIRS AND INSTALLED. 2 L 7 2 4F A6WE 1998121800122 19981218 00122 WP 1998 12 18 MWEA981145 1 19981111 A 5320 99115711 INTERCOSTAL DOUG DC9 DC915 3022036 WP BS 150 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 MAIN CABIN STATION 150 AT L13 RIGHT INTERCOSTAL CRACKED. FABRICATED REPAIR ANGLE TO NEST IN INTERCOSTAL. 2 L 7 2 4F A6WE 1998121800123 19981218 00123 WP 1998 12 18 MWEA981146 1 19981207 A 5610 6171 WINDSHIELD DOUG DC9 DC932 3022066 WP CENTER COCKPIT DEFECTIVE A MWEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 31 202ME 47672 BURNING SMELL IN COCKPIT. DIVERTED TO MKE. SMELL WORSENED, DECLARED EMERGENCY LANDING. CENTER WINDSHEILD HEAT BLOCK O N CENTER WINDSHEILD TERMINAL E MELTED, BURNT. REMOVED AND REPLACED CENTER WINDSHEILD TEMP CTRL BOX. 2 L 7 2 4F A6WE 1998121800124 19981218 00124 WP 1998 12 18 MWEA981147 1 19981210 A 5350 3913359501 LATCH DOUG DC9 DC932 3022066 WP TAIL CONE OUT OF ADJUST A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 302ME 47102 TAIL CONE DID NOT DROP DURING FUNCTIONAL CHECK. MTC ADJUSTED LATCH LEVER CABLE. 2 L 7 2 4F A6WE 1998121800125 19981218 00125 WP 1998 12 18 ARWA981205 1 19981209 A 2740 CONTROL LKHEED 1011 10113851 5265010 WP HORIZ STAB OUT OF ADJUST A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 308GB 1133 STAB C/D PF CS LIGHTS ON. ON CONTROL CHECK, WITH PULL PITCH DISC LIGHT, PERFORMED STAB POS SYSTEM FAULT ISOLATION PER M M 27-43-00, NO FAULTS DETECTED. PERFORMED STAB CONTROL SYSTEM ADJUSTMENT AND TESTED PER MM 27-41-0. OPS NORMAL, NO FA ULTS DETECTED. 2 L 7 3 4F RT A23WE 1998121800126 19981218 00126 WP 1998 12 18 ARWA981206 1 19981210 A 7931 42D491C SWITCH DOUG DC8 DC862 3021970 WP NR 1 ENGINE INOP A ARWA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 19 791AL 46150 NR 1 ENGINE OIL PRESSURE LIGHT CAME ON IN FLIGHT, OIL PRESSURE AND QUANTITY OK, ENGINE SHUT DOWN AT 19:15 Z AS PER ARROW AIR ABNORMAL PROCEDURE, WINDMILLING PRESS, 17 PSI. REMOVED AND REPLACED NR 1 ENGINE OIL PRESS DIFF PRESS SWITCH, GROUN D OPERATION CHECKED NORMAL IAW M/M 79-33-1 AND 71-00-00. 2 L 7 4 4F 4A25 1998121800274 19981218 00274 WP 1998 12 18 TWAA9819601 1 19981211 A 2530 50198A COFFEEMAKER DOUG DC9 DC931 3022065 WP GALLEY FAILED A TWAA H DEACTIVATE SYST/CIRCUITS O OTHER NR NOT REPORTED 1 CE 05 986Z 47589 THE LEFT FWD GALLEY COFFEEMAKER CAUSED ELECTRICAL SHOCK. CREW PULLED CIRCUIT BREAKER. MAINT REPLACED THE COFFEEMAKER. CHECK-C 9-24-98 MCI. 2 L 7 2 4F A6WE 1998121800275 19981218 00275 NM 1998 12 18 TWAA9819602 1 19981208 A 5347 SEAT TRACK BOEING 767 767231 1385131 NM BS 1054 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND CHAIR TRACK CORRODED AT RBL 90 INCHES, STA 1054. INSTALLED NEW SEAT TRACK APPROXIMATELY 19 FEET PER TWA STANDARD PROCESSES 6-70-01, PARA 2. 2 L 7 2 4F RT A1NM 1998121800276 19981218 00276 NM 1998 12 18 TWAA9819603 1 19981210 A 5320 CAP BOEING 767 767231 1385131 NM BS 654 BENT A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND WEB CAP BENT AT STA 654, STRINGER 33R TO 33L. FABRICATED AND INSTALLED NEW CAP PER SPM 6-70-01, PAGE 2 ITEM 3. 2 L 7 2 4F RT A1NM 1998121800277 19981218 00277 WP 1998 12 18 VJ9800647 1 19981116 A 5347 27726601350 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 398-740 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 948VV 47559 SCHEDULED INSPECTION AT AERO CORP, FL, THE SEAT TRACK AT FS 398 TO 740 RBL 44 WAS FOUND WITH CORROSION IN NUMEROUS PLACE S. REMOVED AND REPLACED THE SEAT TRACK IAW DC9 SRM 53-05 FIG 4F. 2 L 7 2 4F A6WE 1998121800278 19981218 00278 NM 1998 12 18 UPS98228283 1 19981209 A 3260 1EN161RB1 SWITCH BOEING 727 72725C 138400H NM RT MLG DOOR INTERMITTENT A IPXA K NONE N FALSE WARNING CL CLIMB 1 SO 01 948UP 19357 RIGHT MAIN GEAR DOOR LIGHT ILLUMINATED AFTER GEAR RETRACTION COMPLETE. CYCLED GEAR ONCE AND LIGHT WENT OUT. FOUND RT M LG DOOR WARNING SWITCH TO BE INTERMITTENT. REMOVED AND REPLACED RT MLG DOOR SWITCH PER MM-32-62-11. ADJ/TEST PERFORMED PER MM 32-62-11 OPS CKS GOOD. 2 L 7 3 4F A3WE 1998121800279 19981218 00279 NM 1998 12 18 UPS98228284 1 19981211 A 3350 BATTERY PACK BOEING 727 72751C 1384015 NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 902UP 18898 FWD ENTRY DOOR OVERHEAD EMERG LIGHT DIM ON TEST. REMOVED AND REPLACED BATT PACK OPS CHECK GOOD PER MM 33-50-01. 2 L 7 3 4F A3WE 1998121800280 19981218 00280 NM 1998 12 18 UPS98228285 1 19981211 A 3350 1000679 LIGHT BOEING 727 72731C 1384011 NM PAX DOOR INOP A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 922UP 19231 FWD ENTRY DOOR EMERGENCY EXIT LIGHT ON WITH POWER OFF SWITCH/OFF. REMOVED AND REPLACED EMERG EXIT LIGHT ASSY, OPS GOOD PER MM 3350-01. 2 L 7 3 4F A3WE 1998121800281 19981218 00281 1998 12 18 MALA976257 2 19981204 A 7230 PLUG SAAB SF340 SF340A 7850100 EU LT ENGINE COMP LOOSE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 142XJ 142 LEFT ENGINE FIRE LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO DTW. MAINTENANCE INSPECTED ENGINE AND FOUND STA GE 5 COMPRESSOR BOROSCOPE PLUG LOOSE IN ENGINE COMPARTMENT. MAINTENANCE REINSTALLED AND TORQUED PLUG, RAN AIRCRAFT AT T AKEOFF POWER FOR 5 MINUTES. ALL CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998121800282 19981218 00282 1998 12 18 MALA976258 4 19981209 A 3425 6226190113 AHRS SAAB SF340 SF340A 7850100 EU RT COCKPIT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 15 102XJ 340A102 RIGHT EADI DISPLAYED UNCOMMANDED PITCH AND ROLL WITH HEADING FLAG DISPLAYED ON BOTH EHSI'S. AIRCRAFT RETURNED TO MSP. M AINTENANCE REPLACED NR 2 AHRS COMPUTER. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998121800283 19981218 00283 EU 1998 12 18 MALA976259 1 19981208 A 3350 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU CABIN INOP A MALA K NONE L NO TEST NR NOT REPORTED 1 GL 15 102XJ 340A102 EMERGENCY POWER ANNUNCATOR LIGHT ON. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY. OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998121800284 19981218 00284 EU 1998 12 18 MALA976260 1 19981209 A 3350 CONNECTOR SAAB SF340 SF340A 7850100 EU CABIN DIRTY A MALA K NONE L NO TEST IN INSP/MAINT 1 GL 15 102XJ 340A102 AFTER START UP, EMERGENCY POWER LIGHT ILLUMINATED. MAINTENANCE CLEANED PACK CONNECTOR FOR EMERGENCY POWER SUPPLY AND RE RACKED EMERGENCY POWER SUPPLY. SYSTEM OPS CHECK GOOD IAW SF340 MM. 2 L 7 2 4T RT A52EU 1998121800285 19981218 00285 EU 1998 12 18 MALA976261 1 19981210 A 3350 501122804 POWER SUPPLY SAAB SF340 SF340A 7850100 EU CABIN INOP A MALA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 15 102XJ 340A102 WHILE TAXING OF TAKEOFF, EMERGENCY POWER LIGHT ON. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND LOOSE CONNECTION O N EMERGENCY POWER SUPPLY PACK CONNECTOR. REPAIRED BROKEN WIRE AND REMOVED AND REPLACED EMERGENCY POWER SUPPLY. OPS CHE CK GOOD. 2 L 7 2 4T RT A52EU 1998121800286 19981218 00286 EU 1998 12 18 MALA976262 1 19981204 A 3230 M610627023 RELAY SAAB SF340 SF340A 7850100 EU LANDING GEAR FAILED A MALA O OTHER J WARNING INDICATION AP APPROACH 1 GL 15 79XJ 079 ON APPROACH, GEAR FAILED TO EXTEND, PERFORMED QRH, EMERGENCY EXTENSION SUCCESSFUL. ON LANDING PULLED FLIGHT IDLE STOP O VERRIDE. MAINTENANCE REPLACED 10GA RELAY. ALL CHECK GOOD. 2 L 7 2 4T RT A52EU 1998121800287 19981218 00287 WP 1998 12 18 IXXA9800071 1 19980610 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 70 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON THE FUSELAGE FRAME AT FUSELAGE STATION 70, BETWEEN LONGERON 32 AND 34 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION AN INTERNAL REPAIR ANGLE IN ACCOR DANCE WITH THE DOUGLAS STRUCTURAL REPAIR MANUAL 51-1-8, 51-10-2 AND ENGINEERING ORDER 53-DC8-871. 2 L 7 4 4F 4A25 1998121800288 19981218 00288 WP 1998 12 18 IXXA9800072 1 19980521 A 5330 PLATING DOUG DC8 DC863F 302198F WP BS 1610/1700 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 1610 A ND 1700, LONGERONS 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION A N EW SECTION OF PLATING, INTERNAL DOUBLERS AND AN EXTERNAL DOUBLER IN ACCORDANCE WITH FAA DER APROVED DRAWING COO-8-53-316 -98 AND 53-DC8-879. 2 L 7 4 4F 4A25 1998121800289 19981218 00289 WP 1998 12 18 IXXA9800073 1 19980520 A 5330 PLATING DOUG DC8 DC863F 302198F WP BS 301.5-324 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATION 301.5 AN D 324, LONGERONS 33 AND 34 LEFT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. FABRICATION AND INSTALLATION TWO INTERNA L FILLERS AND AN EXTERNAL DOUBLER, TRIPLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-8-53-318-98 AND ENGINEERING O RDER 53-DC8-880. 2 L 7 4 4F 4A25 1998121800290 19981218 00290 WP 1998 12 18 IXXA9800074 1 19980520 A 5321 FLOOR DOUG DC8 DC863F 302198F WP BS 863-878 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON MAIN CABIN FLOOR PRESSURE PANEL BETWEEN FUSELAGE STATION 86 3 AND 878, BL +X4 TO -X5.50. REPAIR ACCOMPLISHED CORROSION BLEND OUT, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO-8-53-290-98 AND ENGINEERING ORDER 53-DC8-857. 2 L 7 4 4F 4A25 1998121800291 19981218 00291 WP 1998 12 18 IXXA9800075 1 19980531 A 5730 PLATING DOUG DC8 DC863F 302198F WP WS 304 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING LOWER LEADING EDGE AT STATION XFS 304. REPAIR AC COMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPRO VED DRAWING COO-8-57-313-98 AND ENGINEERING ORDER 57-DC8-860. 2 L 7 4 4F 4A25 1998121800292 19981218 00292 WP 1998 12 18 IXXA9800083 1 19980522 A 5414 PLANK DOUG DC8 DC863F 302198F WP NR 4 PYLON WORN A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, WEAR WAS DETECTED ON THE NUMBER FOUR PYLON UPPER INBOARD PLANK SIX INCHES FORWARD OF STATION YUS 297. REPAIR ACCOMPLISHED BLENDING, POLISH THE AFFECTED AREA IN ACCORDANCE WITH FAA DER APPROVED DRAWING COO -SJO-98-0351, FAX ACTION NUMBER 369661 AND ENGINEERING ORDER 54-DC8-861. 2 L 7 4 4F 4A25 1998121800293 19981218 00293 WP 1998 12 18 IXXA9800084 1 19980524 A 5414 PLANK DOUG DC8 DC863F 302198F WP NR 2 PYLON CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER TWO PYLON OUTBOARD INTERMEDIATE PLANK PANEL AT STATION YN 190. REPAIR ACCOMPLISHED STOP DRILL CRACK, FABRICATION AND INSTALLATION AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED DRAWING 98-05-33-004, DOUGLAS FAX ACTION NUMBER 370114 AND ENGINEERING ORDER 54-DC8086 2. 2 L 7 4 4F 4A25 1998121800294 19981218 00294 WP 1998 12 18 IXXA9800085 1 19980529 A 5313 LONGERON DOUG DC8 DC863F 302198F WP BS 180-220 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 180 AND 220, LONGERON 31 LEFT. REPAI R ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION A NEW LONGERON SPLICE FITTING IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS COO-SJO-98-0362DAC, COO-SJO-98-0369DAC, DOUGLAS FAX ACTION NUMBERS 373978, 372,760, 370453 AND ENGINGE ERING ORDER 53-DC8-863. 2 L 7 4 4F 4A25 1998121800295 19981218 00295 WP 1998 12 18 IXXA9800086 1 19980521 A 5320 DOUBLER DOUG DC8 DC863F 302198F WP BS 1352/1586.5 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE, EIGHT EACH EXTERNAL FINGER DOUBLERS BETWEEN FUSELAGE STATIONS 1352 AND 1586.5. REPAIR ACCOMPLISHED TRIMMING OFF THE CORRODED FINGERS OF THE AFFECTED DOUBLERS IN A CCORDANCE WITH DOUGLAS FAX ACTION NUMBER 370339, FAA DER APPROVED DRAWING COO-SJO-98-0363DAC AND ENGINEERING ORDER 53-DC 8-864. 2 L 7 4 4F 4A25 1998121800296 19981218 00296 WP 1998 12 18 IXXA9800087 1 19980603 A 5414 PLANK DOUG DC8 DC863F 302198F WP NR 4 PYLON CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON NUMBER FOUR PYLON INTERMEDIATE OUTBOARD PLANK AT STATION YIP 241. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION OF AN INTERNAL AND EXTERNAL REPAIR DOUBLERS IN ACCORDANCE WITH DOUGLAS STRUCTUAL REPAIR MANUAL, FAX ACTION NUMBERS 371190, 373366, 372887 AND ENGINEERING ORDER 54-D C8-866. 2 L 7 4 4F 4A25 1998121800297 19981218 00297 WP 1998 12 18 IXXA9800088 1 19980604 A 5320 FITTING DOUG DC8 DC863F 302198F WP BS 70-80 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON A FUSELAGE FITTING BETWEEN FUSELAGE STATION 70 AND 80, LONG ERON 33 RIGHT. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING. FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANC E WITH DOUGLAS DRAWING 4718340, STRUCTUAL REPAIR MANUAL 53-1-0 AND ENGINEERING ORDER 53-DC8-870. 2 L 7 4 4F 4A25 1998121800298 19981218 00298 WP 1998 12 18 IXXA9800089 1 19980521 A 5330 PLATING DOUG DC8 DC863F 302198F WP BS 1620 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED AT AFT ACCESSORY COMPARTMENT INTERNAL DOUBLER AT FUSELAGE STAT ION 1620, BETWEEN LONGERONS 24 AND 27 LEFT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION REPAIR FILLERS, REPAIR DOUBLER AND TRIPLER IN ACCORDANCE WITH FAA DER APPROVED COO-8-53-314-98 AND ENGINEERING ORDER 53-DC8-877 . 2 L 7 4 4F 4A25 1998121800299 19981218 00299 WP 1998 12 18 IXXA9800090 1 19980611 A 5320 ANGLE DOUG DC8 DC863F 302198F WP BS 380 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED BETWEEN FUSELAGE STATION 380 AND 400, LONGERON 27 LEFT. REPAI R ACCOMPLISHED REMOVAL OF CORRODED ANGLE, FABRICATION AND INSTALLATION A NEW LONGERON ANGLE IN ACCORDANCE WITH FAA DER A PPROVED DRAWING COO-8-53-346-98, DOUGLAS STRUCTURAL REPAIR MANUAL 53-2-0 AND ENGINEERING ORDER 53-DC8-888. 2 L 7 4 4F 4A25 1998121800300 19981218 00300 WP 1998 12 18 IXXA9800091 1 19980603 A 5542 PLATING DOUG DC8 DC863F 302198F WP RUDDER CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON THE RUDDER RIGHT SIDE EXTERNAL PLATING AND STATION ZR208.625. REPAIR ACCOMPLISHED STOP DRILLING CRACK, FABRICATION AND INSTALLATION AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FA A DER APPROVED DRAWING COO-8-55-339-98 AND ENGINEERING ORDER 55-DC8-899. 2 L 7 4 4F 4A25 1998121800301 19981218 00301 WP 1998 12 18 IXXA9800092 1 19980608 A 5720 DOUBLER DOUG DC8 DC863F 302198F WP CENTER WING CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON CENTER WING UPPER JOINT DOUBLER AT FUSELAGE STATION 816, ST RINGER 6. REPAIR ACCOMPLISHED BLENDED OUT CORROSION IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS, COO-SJO-98-0393DDAC, COO-SJO-98-0394DAC, DOUGLAS FAX ACTION NUMBER 371688 AND ENGINEERING ORDER 57-DC8-900. 2 L 7 4 4F 4A25 1998121800302 19981218 00302 WP 1998 12 18 IXXA9800093 1 19980521 A 5320 JAMB DOUG DC8 DC863F 302198F WP BS 1177 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, A CRACKED FITTING WAS DETECTED AT UPPER TORQUE BOX FORWARD DOOR JAMB, AFT CARGO COMPA RTMENT AT FUSELAGE STATION 1177 - X 68. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLAS DRAWING 3754918 AND ENGINEERING ORDER 53-DC-8-910. 2 L 7 4 4F 4A25 1998121800303 19981218 00303 WP 1998 12 18 IXXA9800094 1 19980616 A 5330 PLATING DOUG DC8 DC863F 302198F WP BS 1752-1766 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER FUSELAGE EXTERNAL PLATING FROM FUSELAGE STATIONS 1752 AND 1766, BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 372660, FILE NLC00042, FAA DER APPROVED DRAWING COO-SJO-98-0406DAC AND ENGINEERING ORDER 53-DC8-911. 2 L 7 4 4F 4A25 1998121800304 19981218 00304 WP 1998 12 18 IXXA9800095 1 19980709 A 5312 BULKHEAD FITTING DOUG DC8 DC863F 302198F WP BS 1744 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 867BX 79051 2934 46049 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED ON AFT PRESSURE BULKHEAD LOWER SUPPORT FITTING AT FUSELAGE STATI ON 1744, LONGERON 36. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACC ORDANCE WITH DOUGLAS STRUCTUAL MAINTENANCE MANUAL 53-1-0, 51-1-20 AND 51-3-0. 2 L 7 4 4F 4A25 1998121800305 19981218 00305 WP 1998 12 18 IXXA9800096 1 19980714 A 5751 PLATING DOUG DC8 DC862 3021970 WP RT AILERON CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE AND POPPED RIVET HEADS WERE DETECTED ON THE RIGHT AILERON LOWER PL ATING BETWEEN STATIONS XA 605 AND XA 622. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING, FABRICATION AND INSTALLATION O F A NEW LOWER PLATING IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R02 AND ENGINEERING ORDER 27-DC8-905-925. 2 L 7 4 4F 4A25 1998121800306 19981218 00306 WP 1998 12 18 IXXA9800097 1 19980717 A 5512 PANEL DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWE EN STATIONS XE 149 AND XE 221. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R03 AND ENGINEERING ORDER 55-DC8-926. 2 L 7 4 4F 4A25 1998121800307 19981218 00307 WP 1998 12 18 IXXA9800098 1 19980717 A 5512 PANEL DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWE EN STATIONS XE 272 AND XE 275. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R04 AND ENGINEERING ORDER 55-DC8-927. 2 L 7 4 4F 4A25 1998121800308 19981218 00308 WP 1998 12 18 IXXA9800099 1 19980715 A 5330 PLATING DOUG DC8 DC862 3021970 WP BS 1500 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE WAS DETECTED ON LOWER FUSELAGE EXTERNAL PLATING AT FUSELAGE STATION 1500 BETWEEN LONGERON 31 LEFT AND 31 RIGHT. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION OF A R EPAIR FILLER AND AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-0-R047 AND ENGINEERING ORDER 53-DC8-930. 2 L 7 4 4F 4A25 1998121800309 19981218 00309 WP 1998 12 18 IXXA9800100 1 19980717 A 5312 BULKHEAD DOUBLER DOUG DC8 DC862 3021970 WP BS 44 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, A CRACK WAS DETECTED IN THE LOWER RADOME COMPARTMENT BULKHEAD INNER DOUBLER AT FUSELA GE STATION 44. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW DOUBLER AND TWO REPAI R SPLICE DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R08 AND ENGINEERING ORDER 53-DC8-931. 2 L 7 4 4F 4A25 1998121800310 19981218 00310 WP 1998 12 18 IXXA9800101 1 19980717 A 5512 PANEL DOUG DC8 DC862 3021970 WP RT HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, A CORROSION BULGE WAS DETECTED ON THE RIGHT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEEN STATION XE 77 AND XE 148. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R09 AND ENGINEERING ORDER 55-DC8-932. 2 L 7 4 4F 4A25 1998121800311 19981218 00311 WP 1998 12 18 IXXA9800102 1 19980716 A 5512 PANEL DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT HORIZONTAL STABILIZER LOWER TRAILING EDGE PANEL BETWEE N STATIONS XE 221 AND XE 272. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R10 AND ENGINEERING ORDER 55-DC8-933. 2 L 7 4 4F 4A25 1998121800312 19981218 00312 WP 1998 12 18 IXXA9800103 1 19980804 A 5512 PANEL DOUG DC8 DC862 3021970 WP LT HORIZ STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT HORIZONTAL STABILIZER UPPER TRAILING EDGE PANEL BETWEE N STATIONS XE 221 AND XE 272. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R11 AND ENGINEERING ORDER 55-DC8-934. 2 L 7 4 4F 4A25 1998121800313 19981218 00313 WP 1998 12 18 IXXA9800104 1 19980714 A 5730 PANEL DOUG DC8 DC862 3021970 WP WS 408 DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 21CX 63338 3035 45955 DURING ROUTINE C CHECK INSPECTION, RIGHT WING LOWER LEADING EDGE ACCESS PANEL WAS DAMAGED AT STATION XW 408. REPAIR ACC OMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER, DOUBLER AND AN L ANGLE IN ACCORDANCE WITH FAA DER APPROVED DRAWING F03-R01 AND ENGINEERING ORDER 57-DC8-924 2 L 7 4 4F 4A25 1998121800314 19981218 00314 WP 1998 12 18 IXXA9800105 1 19980710 A 7120 57755121 MOUNT DOUG DC8 DC863F 302198F WP NR 3 ENGINE CHAFED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AL 78717 3074 46121 DURING ROUTINE C CHECK INSPECTION, CHAFING WAS DETECTED ON NUMBER THREE PYLON FORWARD ENGINE MOUNT. REPAIR BLENDS AFFEC TED AREA AND DETERMINES THAT THE WEAR IS ACCEPTABLE FOR STRENGTH IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 374208 AND ENGINEERING ORDER 71-DC8-891. 2 L 7 4 4F 4A25 1998121800315 19981218 00315 WP 1998 12 18 IXXA9800106 1 19980430 A 5532 PANEL DOUG DC8 DC863F 302198F WP VERT STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AL 78717 3074 46121 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT VERTICAL STABILIZER PANEL BETWEEN STATIONS ZR 253 AND ZR 297. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDANCE WITH FAA DER APPROVED DRAWING E68-R01 AND ENGINEERING ORDER 55-DC8-892. 2 L 7 4 4F 4A25 1998121800316 19981218 00316 WP 1998 12 18 IXXA9800107 1 19980424 A 5532 PANEL DOUG DC8 DC863F 302198F WP VERT STAB CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AL 78717 3074 46121 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON RIGHT VERTICAL STABILIZER EXTERNAL PANEL BETWEEN STATIONS Z R 253 AND ZV 297. REPAIR ACCOMPLISHED REMOVAL OF AFFECTED AREA, FABRICATION AND INSTALLATION OF A NEW PANEL IN ACCORDAN CE WITH FAA DER APPROVED DRAWING E69-R02 AND ENGINEERING ORDER 55-DC8-893. 2 L 7 4 4F 4A25 1998121800317 19981218 00317 WP 1998 12 18 IXXA9800108 1 19980806 A 5414 PLATING DOUG DC8 DC863F 302198F WP NR 3 PYLON DAMAGED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AL 78717 3074 46121 DURING ROUTINE C CHECK INSPECTION, HEAT STRESS WAS DETECTED ON NUMBER THREE PYLON INBOARD AND OUTBOARD PLANK PLATING. R EPAIR ACCOMPLISHED REMOVAL OF AFFECTED AREAS, FABRICATION AND INSTALLATION OF NEW PLANK PLATINGS IN ACCORDANCE WITH DOUG LAS DRAWING 5753265 AND ENGINEERING ORDER 54-DC8-896. 2 L 7 4 4F 4A25 1998121800318 19981218 00318 WP 1998 12 18 IXXA9800109 1 19980514 A 5720 DOUBLER DOUG DC8 DC863F 302198F WP LT MLG WW CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 786AL 78717 3074 46121 DURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON LEFT MAIN LANDING GEAR LOWER SUPPORT DOUBLER. REPAIR ACCOM PLISHED CORROSION REMOVAL IN ACCORDANCE WITH DOUGLAS FAX ACTION NUMBER 368547 AND 368589 AND ENGINEERING ORDER 57-DC8-90 4. 2 L 7 4 4F 4A25 1998121800319 19981218 00319 WP 1998 12 18 IXXA9800110 1 19981210 A 3610 PNEUMATIC LINE DOUG DC8 DC861 3021952 WP NR 2 ENGINE LOOSE A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 23 861PL 53114 1959 45964 AFTER TAKEOFF FROM TOL, EN ROUTE TO FLL, THE NUMBER TWO ENGINE FIRE WARNING INTERMITTENTLY SOUND ACCOMPANIED BY AN INTER MITTENT MASTER FIRE WARNING LIGHT ILLUMINATING. THE FLIGHT CREW SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND RET URNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE LOCATING A LOOSE PNUMATIC LINE ON THE OUTBOARD REVERSER CASSADE DOOR, WHICH WAS SECURED. MAINTENANCE PERFORMED A SUCCESSFULL LEAK CHECK AND FIRE WARNING OPERATIONAL CHECK IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1998121800320 19981218 00320 WP 1998 12 18 IXXA9800111 1 19981210 A 2612 57775771 ELEMENT DOUG DC8 DC861 3021952 WP NR 2 ENGINE DEFECTIVE A IXXA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 861PL 53114 1959 45964 AFTER TAKEOFF FROM TOL, EN ROUTE TO FLL, THE NUMBER TWO ENGINE FIRE WARNING BELL INTERMITTENTLY SOUNDED. THE FLIGHT CRE W SECURED THE ENGINE FOLLOWING COMPANY PROCEDURES AND RETURNED TO TOL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE WHICH REVEALED TWO DEFECTIVE FIRE WARNING SENSE ELEMENTS. MAINTENANCE REPLACED THE UPPER AND LOWER FIRE WARN ING SENSE ELEMENTS AND THE FIRE DETECTOR CONTROL AMPLIFIER AS A PRECAUTION. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIO NAL TEST IN ACCORDANCE WITH THE MAINTENANCE MANUAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 L 7 4 4F 4A25 1998121800321 19981218 00321 WP 1998 12 18 CALA9802169 1 19981210 A 3260 TARGET DOUG DC9 DC981 3022081 WP LDG GEAR DOOR LOOSE A CALA O OTHER N FALSE WARNING IN INSP/MAINT 1 SW 09 13881 48045 THE GEAR DOOR OPEN LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. WHEN THE GEAR WAS EXTENDED FOR LANDING, THE GEAR DOO R OPEN LIGHT REMAINED ON. THE GEAR WAS CYCLED AND THE LIGHT WENT OUT. MAINTENANCE FOUND THE DOOR PROXIMITY SWITCH TARGE T DAMAGED/LOOSE. THE TARGET WAS FASTENED INTO POSITION USING A HI-LOCK RIVET. GEAR INDICATIONS CHECKED GOOD. 2 L 7 2 4F A6WE 1998121800322 19981218 00322 NM 1998 12 18 CALA9802170 1 19981210 A 5230 FITTING BOEING 727 727243 138408D NM CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND A .5 INCH CRACK IN C-2 DOOR UPPER AFT OVERCENTER STOP LOCK FITTING. THE STOP LOCK, FITTING, AND PLATE WERE REMOVED. A NEW FITTING, STOP LOCK, AND PLATE WERE INSTALLED IAW SRM 51-10-1. 2 L 7 3 4F RT A3WE 1998121800323 19981218 00323 NM 1998 12 18 CALA9802171 1 19981210 A 5753 TRACK BOEING 727 727243 138408D NM RT TE FLAP CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 THE RT WING NR 5 FLAP TRACK WAS FOUND CORRODED. THE NR 5 FLAP TRACK ASSEMBLY WAS REMOVED AND REPLACED IAW MM 27-57-31. 2 L 7 3 4F RT A3WE 1998121800324 19981218 00324 NM 1998 12 18 CALA9802172 1 19981211 A 5320 CHORD BOEING 727 727243 138408D NM BS 1176 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17407 21270 INSPECTION FOUND AFT RT LAV FLOOR REINFORCEMENT CHORD CORRODED AT BS 1176, RBL 26. THE CORRODED AREA WAS BLENDED OUT. A FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5310-03799 AND BOEING SKETCH CAL-MIA-98-CC55TR. 2 L 7 3 4F RT A3WE 1998121800325 19981218 00325 WP 1998 12 18 CALA9802173 1 19981210 A 2510 SOLENOID DOUG DC10 DC1030 3023501 WP LT COCKPIT SEAT FAILED A CALA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 14074 46911 THE SMELL OF SMOKE WAS OBSERVED COMING FROM CAPTAIN'S SEAT DURING CRUISE PORTION OF FLIGHT. AN ELECTRICAL CONNECTION IN THE BASE OF SEAT BACK WAS FOUND HOT AND SMOKING. WHEN THE WIRES WERE PULLED OUT AND THE CIRCUIT BREAKERS FOR CAPTAIN'S SEAT WERE PULLED THE SMOKE CEASED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE CAPTAIN'S SEAT HARNESS RESTRAINT SOLENOID SHORTED. THE FUNCTION OF THIS SEAT FEATURE WAS DISABLED FOR BOTH THE CAPTAIN'S AND FIRS T OFFICER'S SEATS IAW ECRA 2510-01429. 2 L 7 3 4F A22WE 1998121800326 19981218 00326 WP 1998 12 18 9810589907 1 19981205 A 3230 SPRING DOUG DC9 DC931 3022065 WP NLG DISCONNECTED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 957N 47253 AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO MSP AND LAND ED WITHOUT INCIDENT. MAINTENANCE REROUTED GROUND SENSING CONTROL MECHANISM CABLE 116B AND 117B AND RECONNECTED THE ANTI -RETRACTION CABLE SPRING. CABLES WERE TENSIONED PER MAINTENANCE MANUAL. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800327 19981218 00327 WP 1998 12 18 9810599104 1 19980916 A 3350 BATTERY DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 94S 47204 DURING LINE CHECK, FOUND FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NO RMAL 2 L 7 2 4F A6WE 1998121800328 19981218 00328 WP 1998 12 18 9810609102 1 19980902 A 3350 BATTERY DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 92S 47064 DURING LINE CHECK, FOUND FIRST CLASS SECTION PATHWAY EMERGENCY EXIT LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800329 19981218 00329 WP 1998 12 18 9810619106 1 19981025 A 3397 WIRE DOUG DC9 DC915 3022036 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 96S 47206 DURING LINE CHECK, FOUND ALL EMERGENCY LIGHTS WILL ILLUMINATE WITH AC POWER OFF AND EMERGENCY EXIT LIGHT SWITCH IN THE O FF POSITION. MAINTENANCE REPAIRED GROUND WIRE AT BATTERY PACK. OPERATIONAL CHECK NORMAL 2 L 7 2 4F A6WE 1998121800330 19981218 00330 WP 1998 12 18 9810629138 1 19980920 A 3350 BATTERY DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 9348 45787 DURING LINE CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK. OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1998121800331 19981218 00331 WP 1998 12 18 9810639851 1 19981103 A 3397 WIRE DOUG DC9 DC951 3022051 WP SEAT 2C DAMAGED A NWAA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 01 760NC 47708 DURING TAXI OPERATIONS, THE EMERGENCY ESCAPE PATH LIGHTING ILUMINATED FOR SEVERAL MINUTES AND THEN EXTINGUISHED; PROBLEM REPEATED UPON LANDING AT DESTINATION. MAINTENANCE REPAIRED WIRING AT COACH CLASS SEAT 2C. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800332 19981218 00332 WP 1998 12 18 9810649861 1 19980827 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 770NC 47758 DURING LINE CHECK, FOUND EMERGENCY LIGHTING INOPERATIVE IN THE FIRST CLASS SECTION CEILING. MAINTENANCE REPLACED BATTER IES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800333 19981218 00333 WP 1998 12 18 9810659868 1 19981018 A 3350 CIRCUIT BREAKER DOUG DC9 DC951 3022051 WP CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 777NC 47787 DURING LINE CHECK, FOUND EMERGENCY LIGHTING WILL NOT EXTINGUISH WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION. MA INTENANCE REPLACED CIRCUIT BREAKER B1-387. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800334 19981218 00334 WP 1998 12 18 9810669885 1 19980921 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 401EA 47682 THE FIRST CLASS SECTION ROW EMERGENCY LIGHTING ILLUMINATED WITHOUT MAIN CABIN LIGHTS. MAINTENANCE REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800335 19981218 00335 WP 1998 12 18 9810679885 1 19980918 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 401EA 47682 PRIOR TO DEPARTURE, THE FIRST CLASS SECTION ROW EMERGENCY LIGHTING ILLUMINATED. MAINTENANCE REPLACED POWER SUPPLY. OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800336 19981218 00336 WP 1998 12 18 9810689862 1 19980914 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 771NC 47769 DURING LINE CHECK, FOUND THE FIRST CLASS SECTION OVERHEAD EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE REPLACED BATTERIE S. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800337 19981218 00337 WP 1998 12 18 9810699963 1 19981113 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP SERVICE DOOR INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 EMERGENCY LIGHTS IN FIRST CLASS SECTION WOULD NOT EXTINGUISH DURING FLIGHT. REPLACED POWER SUPPLY AT FORWARD SERVICE DO OR 1R. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800338 19981218 00338 WP 1998 12 18 9810709963 1 19981126 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP DOOR 1R DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 FLIGHT ATTENDANT REPORTED CABIN EMERGENCY LIGHTS BLINKING ON AND OFF INTERMITTENTLY DURING FLIGHT. REPLACED BATTERY PAC K AT DOOR 1R. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800339 19981218 00339 WP 1998 12 18 9810719963 1 19981130 A 3350 BATTERIES DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 DURING LINE MAINTENANCE INSPECTION, FOUND SEAT MOUNTED EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. REPLACED BA TTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800340 19981218 00340 WP 1998 12 18 9810729609 1 19980925 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 609NW 47234 DURING LINE MAINTENANCE INSPECTION, FOUND COCKPIT AND FORWARD CABIN OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED BAT TERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800341 19981218 00341 WP 1998 12 18 9810739961 1 19981001 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP TAIL COMPARTMENT DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 924RW 47185 DURING LINE MAINTENANCE INSPECTION, FOUND ALL EMERGENCY LIGHTS IN TAIL COMPARTMENT AND ABOVE AFT FLIGHT ATTENDANT SEAT I NOPERATIVE. REPLACED BATTERY PACK AND BATTERIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800342 19981218 00342 WP 1998 12 18 9810749959 1 19980927 A 3350 FUSE DOUG DC9 DC931 3022065 WP CABIN BLOWN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 919RW 47162 DURING LINE MAINTENANCE INPSECTION, FOUND FIRST CLASS SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED FUSE. OPERATIO NAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800343 19981218 00343 WP 1998 12 18 9810759926 1 19980917 A 3350 BATTERIES DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 926NW 47425 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERIES. OPE RATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800344 19981218 00344 WP 1998 12 18 9810769935 1 19981007 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 1332U 47404 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS SECTION OF EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800345 19981218 00345 WP 1998 12 18 9810779985 1 19980916 A 3350 POWER SUPPLY DOUG DC9 DC951 3022051 WP DOOR 1R INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 401EA 47682 FLIGHT ATTENDANT REPORTED EMERGENCY PATH LIGHTING IN FIRST CLASS WOULD NOT SHUT OFF AFTER TAKEOFF. MAINTENANCE REPLACED POWER SUPPLY AT DOOR 1R. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800346 19981218 00346 WP 1998 12 18 9810789967 1 19981201 A 5312 BULKHEAD SKIN DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9331 47263 DURING PERIODIC CHECK, FOUND NOSE WHEEL WELL VERTICAL BULKHEAD SKIN CRACKED AT FS 110 IN TWO PLACES, APPROXIMATED 5.5 IN CHES LEFT OF CENTER LOWER LEFT PANEL. INSTALLED REPAIR PER SRM 53-04. 2 L 7 2 4F A6WE 1998121800347 19981218 00347 WP 1998 12 18 9810799967 1 19981201 A 5320 DOUBLER DOUG DC9 DC931 3022065 WP BS 105 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9331 47263 DURING PERIODIC CHECK, FOUND FLIGHT COMPARTMENT PRESSURE PANEL CRACKED OUTBOARD OF BEAM AT FS 105 ON RIGHT SIDE. INSTAL LED FILLER, DOUBLER, AND NEW FITTING 49124G-2 PER SRM 53-10. 2 L 7 2 4F A6WE 1998121800348 19981218 00348 WP 1998 12 18 9810809926 1 19981125 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING PERIODIC CHECK, FOUND CRACK IN VERTICAL STABILIZER SKIN ON LEFT SIDE ABOVE RUDDER. INSTALLED DOUBLER REPAIR PER EA 99-159482. 2 L 7 2 4F A6WE 1998121800349 19981218 00349 WP 1998 12 18 9810819926 1 19981126 A 5312 BULKHEAD SKIN DOUG DC9 DC932 3022066 WP BS 1038 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING PERIODIC CHECK, FOUND ONE INCH CRACK IN AFT SKIN ON BULKHEAD AT FS 1038, LONGERON 10. INSTALLED REPAIR PER SRM 5 1-30-5 AND EA 99-159472. 2 L 7 2 4F A6WE 1998121800350 19981218 00350 WP 1998 12 18 9810829979 1 19981204 A 5320 PANEL DOUG DC9 DC931 3022065 WP BS 110 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9343 47439 DURING PERIODIC CHECK, FOUND FLIGHT COMPARTMENT HORIZONTAL PRESSURE PANEL CRACKED AT TOP RIGHT SIDE OF NOSE WHEEL WELL C OMPARTMENT AT FS 110 ON INBOARD AND OUTBOARD VERTICAL BEAMS. INSTALLED REPAIR PER SRM 53-10 PG 13. 2 L 7 2 4F A6WE 1998121800351 19981218 00351 1998 12 18 9810833228 4 19981208 A 2210 SC47003 ACTUATOR AIRBUS 320 A320211 3930320 EU YAW DAMPER LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 328NW 22210 22210 298 DURING DESCENT, RECEIVED HYD G RSVR LO LVL MESSAGE. CREW SHUT OFF GREEN HYDRAULIC PUMP, PTU, GRAVITY EXTEND LANDING GEA R, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING LEFT YAW DAMPER ACTUATOR. 2 L 7 2 4F RT A28NM 1998121800352 19981218 00352 1998 12 18 9810843204 4 19981208 A 2210 SC47003 ACTUATOR AIRBUS 320 A320211 3930320 EU YAW DAMPER LEAKING A NWAA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 GL 01 304US 25816 11290 40 DURING DESCENT, RECEIVED HYD R RSVR LOW LVL MESSAGE. CREW SHUT OFF GREEN HYDRAULIC PUMP, PTU, GRAVITY EXTENDED LANDING GEAR, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING LEFT YAW DAMPER ACTUATOR. CHANGED HYD R RSVR LOW LVL T O HYD G RSVR LOW LVL AND CHANGED LANDED WITHOUT TO LANDED WITHOUT. 2 L 7 2 4F RT A28NM 1998121800353 19981218 00353 NM 1998 12 18 98FDEA00740 1 19981209 A 2710 DISAGREE LIGHT DOUG MD11 MD11F 3023600 NM AILERON ACTIVATED A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 609FE 48549 98-298 - AILERON DEFLECTION DISAGREE ALERT AT SLAT RETRACT. ALERT DISAPPEAR FOR 1 MIN THEN RETURN ON THE CONFIG PG NO A ILERON DEFLECTION SHOW ON CLEAN WING. A/C DEFER PER MEL 27-2 METHOD A. 2 L 7 3 4F RT A22WE 1998121800354 19981218 00354 NM 1998 12 18 98FDEA00741 1 19981211 A 5230 6557140513 SKIN BOEING 727 727247 138408F NM CARGO DOOR CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 369 FCD INNER SKIN IS CRACKED 8 INCHES FWD OF AFT FRAME 1 INCH ABOVE NR 3 TRANSVERSE BEAM. *S/D* REMOVED DAMAGE AT FCD INNER SKIN AND FABRICATED AND INSTALLED REPAIR DOUBLER IAW FEDEX SRM 52-00-3 FIG 3. 2 L 7 3 4F A3WE 1998121800355 19981218 00355 NM 1998 12 18 98FDEA00742 1 19981211 A 2730 65C188567 FEEL UNIT BOEING 727 72725C 138400H NM ELEVATOR INOP A FDEA O OTHER F FLT CONT AFFECTED CL CLIMB 1 SO 25 133FE 19851 AFTER DEPARTURE AT 2000 TO 3000 FT MSL, 200 PLUS KNOTS, ELEVATOR FEEL WENT LIMP FOR 3 TO 5 SEC. THEN WITHOUT WARNING FE EL RETURN. *S/D* REMOVED AND REPLACED PNL 9777, 9778 AND ELEV FEEL CONTROL UNIT PER MM 27-30-112. PERFORMED FEEL FORC E SYS MM 27-30-00-05. OPER CK GOOD. 2 L 7 3 4F A3WE 1998121800356 19981218 00356 WP 1998 12 18 ABXA9801180 1 19981209 A 3260 INDICATION DOUG DC9 DC932 3022066 WP LDG GEAR DOOR MALFUNCTIONED A ABXA O OTHER N FALSE WARNING DE DESCENT 1 GL 23 901AX 47381 GEAR DOOR LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION. RECYCLED GEAR AT 200 KTS, LIGHT REMAINED ON. RECYCLED GEAR AT 250 KTS, LIGHT WENT OUT. VISUALLY INSPECTED GEAR AND WHEEL WELL AREA. NO DEFECTS NOTED. OPERATED GEAR. ALL INDICA TIONS WERE NORMAL. 2 L 7 2 4F A6WE 1998121800357 19981218 00357 NM 1998 12 18 DL76L982512 1 19981208 A 3350 P2070003001 FLASHLIGHT BOEING 767 767332 1382001 NM LAVATORY INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 171DN 24759 MID GALLEY/LAVATORY EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED MID-GALLEY/LAVATORY FLASHLIGHT AND BATTERY ASSY CKS OK. 2 L 7 2 4F RT A1NM 1998121800358 19981218 00358 NM 1998 12 18 DL733982513 1 19981209 A 5320 WEB BOEING 737 737347 1384647 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 WHILE ACCOMPLISHING INSPECTIONS PER EO 5-70166-3, TWO CRACKS WERE FOUND IN THE WEB AT BS 727, S18AL. ONE CRACK IS IN A LOCATION TYP OF THE EO (REF. SB 727-53-1170); HOWEVER IT EXTENDS FWD, BEYOND THE NOTED FAST HOLE FOR TERMINATION. THE O THER CRACK IS IN THE FAST. HOLE JUST BELOW THE TYP LOCATION. REPAIRED PER ERA 332555-14. 2 L 7 2 4F RT A16WE 1998121800359 19981218 00359 NM 1998 12 18 DL733982514 1 19981209 A 5330 SKIN BOEING 737 737347 1384647 NM L1 DOORWAY GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 FUSELAGE SKIN WAS FOUND GOUGED AT THE AFT CORNER OF THE L1 DOOR CUTOUT. MAX DEPTH WAS 0.013 WITH A WIDTH OF 3.0. REPAI RED PER ERA 332534-14. 2 L 7 2 4F RT A16WE 1998121800360 19981218 00360 NM 1998 12 18 DL733982516 1 19981209 A 5312 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305WA 23346 DURING ACCOMPLISHMENT OF SI 5-69482-12, TWO CRACKS WERE DISCOVERED ON THE FWD FACE OF THE BS 178 BLKHD WEB AT WL 199 AND RBL 5.7. ADDITIONALLY, THE WEB WAS DENTED AT WL 185, LBL 15. REPAIRED PER ERA 332538-14. 2 L 7 2 4F RT A16WE 1998121800361 19981218 00361 NM 1998 12 18 DL76L982517 1 19981209 A 5330 SKIN BOEING 767 767332 1382001 NM BS 652 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 A DENT WAS FOUND AT BS 652 BETWEEN S35R AND 36R. THE DENT WAS REMOVED BY MAKING A CUTOUT APPROX 2.3 BY 3.7. REPAIRED P ER ERA 332506-14. 2 L 7 2 4F RT A1NM 1998121800362 19981218 00362 NM 1998 12 18 DL76L982518 1 19981209 A 5400 331T311021 SPAR WEB BOEING 767 767332 1382001 NM NR 1 PYLON CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 177DN 25122 TWO CRACKS WERE FOUND EMANATING FROM THE OUTBD DRAIN HOLE AT NAC STA 158 IN THE FWD UPPER SPAR WEB ON THE NR1 PYLON. ON E CRACK GREW FWD AND INBD FROM THE HOLE AND THE OTHER AFT AND OUTBD. THE RESULTING CUTOUT IS 1.9 BY 0.25. REPAIRED PER ERA 332558-14. 2 L 7 2 4F RT A1NM 1998121800363 19981218 00363 NM 1998 12 18 DL72L982519 1 19981209 A 5311 651592231 FRAME BOEING 727 727232 1384082 NM BS 380 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 DURING INSPECTION A CRACK WAS FOUND IN THE FRAME AT BS 380 WL 280; JUST ABOVE THE R1 DOOR CUTOUT. THE CRACK IS LOCATED ON THE INBD FLANGE OF THE PART AT A FASTENER HOLE. REPAIRED PER ERA 332549-14. 2 L 7 3 4F A3WE 1998121800364 19981218 00364 NM 1998 12 18 DL757982526 1 19981209 A 2913 PUMP 7588587104 BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 1 ENGINE FAILED A DALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 638DL 23761 716330 DESCENDING THROUGH 10000 FT INTO SNA SPEEDBRAKES EXT LT HYD QTY MSG ILLUM. OVERHEAD PNL YIELDED LT SYS PRESS LIGHT. LT ENG PUMP PRESS LIGHT AND LT ELEC PUMP PRESS LIGHT. ALSO, LT YAW DAMPER LIGHT ILLUM. LT HYD QTY ZERO. FOUND LT EDP CA SE DRAIN PRESSURE FILTER DIFFERENTIAL FILTER MODULE RUPTURED. REPLACED LT EDP ELEC PUMP AND EDP CASE DRAIN PRESSURE FIL TER MODULE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998121800365 19981218 00365 WP 1998 12 18 DHL98807008 1 19981209 A 2750 4655347505 CONTROL CABLE DOUG DC8 DC873F 302199F WP LT TE FLAP BROKEN A DHLA L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 SO 01 807DH 45990 AT 500 FT ABOVE THE RUNWAY FLAPS RETRACTED FULLY WITHOUT COMMAND. FOUND LEFT FLAP FOLLOW UP CABLE BROKEN. REPLACED CAB LE RERIGGED FLAPS. 2 L 7 4 4F RT 4A25 1998121800366 19981218 00366 NM 1998 12 18 VNAA9812004 1 19981206 A 3030 D3899926FA98SN CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE NR 1 PITOT HEAT DAMAGED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 426JS 3038 A NR 1 PITOT HEAT FAIL WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT WAS COMPLETED WITHOUT ANY PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE NR 1 PITOT TUBE ELECTRICAL CONNECTOR, IN ACCORDANCE WIT H DORNIER WIRING MANUAL 20-15-02. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998121800372 19981218 00372 EA 1998 12 18 CA980811011 1 19980730 A 5520 13A12000015 FINLET C6TP10017 DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A34 52043 EA HORIZ STAB MISSING W K NONE O OTHER IN INSP/MAINT 1 CA PCE40095 (CAN) RIGHT HAND FINLET ON THE LOWER SIDE OF THE HORIZONTAL STABILIZER NOTED AS MISSING. PART OF THE FRONT SPAR OF THE FINLET WAS HELD ON BY ONE REMAINING SCREW. 1 H 7 2 3T 4 T RT A9EA E4EA 1998121800375 19981218 00375 WP 1998 12 18 CA981001007 1 19980920 A 2133 ACTUATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE OUTFLOW VALVE FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA P657065D (CAN) DURING TAKEOFF WHEN POWER APPLIED PRESSURIZATION CONTROL WAS HUNTING FOR PROPER POSITION. DURING CLIMB-OUT CABIN WAS MAX CLIMB, CABIN ALT SHOWED 2,500 FEET. LEVELLED OFF AT 7,000 FEET BUT NO CONTROL OVER PRESSURIZATION SYSTEM. REPLA CED NR 1 CABIN CONTROLLER AND OUTFLOW VALVE ACTUATOR. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998121800377 19981218 00377 EU 1998 12 18 CA981001011 1 19980917 A 2130 87292325V04 COMPUTER AIRBUS 320 A320211 3930320 EU E/E BAY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) AFTER TAKEOFF, AVIONIC VENT BLOWER FAULT LIGHT CAME ON. AIRCRAFT LANDED. CHANGED AVIONIC EQUIPMENT VENT COMPUTER . SYSTEM OK. 2 L 7 2 4F RT A28NM 1998121800379 19981218 00379 SW 1998 12 18 CA981006004 1 19980902 A 6210 212015501005 BLADE BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3145 A1359 CPPS62814 (CAN) ON INSPECTION, CRACK NOTICED ON UNDERSIDE OF BLADE AT STA 75. CRACK IS 6 INCHES LONG. 1 G 7 1 4U 4 U H4SW E22EA 1998121800382 19981218 00382 EU 1998 12 18 CA981006007 1 19980924 A 3397 OGA075 WIRE 315A21115003 AEROSP SA316 SA315B 8680615 EU LANDING LIGHT FAILED W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 6176 3053 OGA075 (CAN) ON START-UP, BURNING SMELL AND SPARKS NOTICED AND ENGINE SHUTDOWN. HISSING SOUND WAS HEARD AND 'VIDEO' PRESSURE I NDICATOR SHOWED 'RED'. A WIRE RUNNING FROM THE MAIN BUS IN THE 'IP' BOX TO THE LANDING LIGHT HAD CHAFED THRU AND ARCED ON THE STEEL STRUCTURAL TUBE BETWEEN CLUSTERS 8 AND 3LM. HOLE IN STRUCTURAL TUBE WELDED AND STRUCTURE RECHARGED WITH NI TROGEN. WIRE REPAIRED. 1 G 7 1 4U H1IN 1998121800396 19981218 00396 SW 1998 12 18 CA981006027 1 19980416 A 6710 MS3569133 NUT 206010355009 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL PITCH CHANGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10211 801799BA (CAN) PITCH CHANGE LINK ADJUSTER LOCKNUT CRACKED ON MPI. 1 G 7 1 3U 3 U H2SW E4CE 1998121800402 19981218 00402 CE 1998 12 18 CA981007003 1 19980928 A 3710 RA211CC PUMP CESSNA 172 172M 2072418 CE MCAULY 1C160 1C160CTM GL VACUUM SYSTEM FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA 1 721156 (CAN) AFTER INSTALLATION OF THE DRY AIR PUMP AND GROUND TEST, THE PUMP FAILED WITHIN ONE HOUR. CARBON VANES APPEAR TO H AVE STUCK IN THE CENTER HUB, ONLY ONE OR TWO VANES CAN BE HEARD WHEN THE PUMP IS ROTATED BY HAND. 1 H 7 1 3O NT 3A12 5 N P910 1998121800409 19981218 00409 EU 1998 12 18 CA981007010 1 19980918 A 5320 350A23105344 SUPPORT 2300000101 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE NR 5 BEARING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5129 TB1558 786 (CAN) NR 5 BEARING SUPPORT CRACKED AT THE BOTTOM RIGHT CORNER ATTACHMENT. 1 G 7 1 3U 3 U H9EU E19EU 1998121800410 19981218 00410 EU 1998 12 18 CA981007011 1 19980918 A 5311 350A21124700 FRAME SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 5129 786 (CAN) ON 100 HOUR INSPECTION, TAILBOOM ATTACHMENT BOLT AT 12 O'CLOCK POSITION WAS UNDERTORQUE. FUSELAGE REAR FRAME SUPP ORT WAS CRACKED APPROXIMATELY 1 INCH AT EACH OF 3 LOCATIONS. 12, 2, AND 3 O'CLOCK POSITIONS. 1 G 7 1 3U 3 U H9EU E19EU 1998121800411 19981218 00411 EU 1998 12 18 CA981007012 1 19980930 A 6320 350A3810189 CROSSBEAM 350A32030004 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE M/R GEARBOX CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA M882 786 (CAN) MAIN ROTOR GEARBOX CROSSBEAM CRACKED AT BOTH ENDS ON THE THIN SIDE OF THE RADIUS FLAT SURFACE. 1 G 7 1 3U 3 U H9EU E19EU 1998121800415 19981218 00415 WP 1998 12 18 CA981013004 1 19980625 A 6220 369D212553 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R HEAD WORN W K NONE O OTHER IN INSP/MAINT 1 CA 711 CAE830901 (CAN) MAIN ROTOR HEAD HAS EXCESSIVE PLAY UP AND DOWN ON MAST. 1 G 7 1 3U 3 U H3WE E4CE 1998121800416 19981218 00416 WP 1998 12 18 CA981013005 1 19980625 A 6220 369D212563 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R HEAD WORN W K NONE O OTHER IN INSP/MAINT 1 CA 711 CAE830901 (CAN) MAIN ROTOR HEAD HAS EXCESSIVE UP AND DOWN PLAY ON MAST. 1 G 7 1 3U 3 U H3WE E4CE 1998121800417 19981218 00417 WP 1998 12 18 CA981013006 1 19980625 A 6220 369D212573 BEARING HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL M/R HEAD WORN W K NONE O OTHER IN INSP/MAINT 1 CA 711 CAE830901 (CAN) MAIN ROTOR HUB EXCESSIVE UP AND DOWN PLAY ON MAST. 1 G 7 1 3U 3 U H3WE E4CE 1998121800423 19981218 00423 EU 1998 12 18 CA981013015 1 19980918 A 2510 SPRING 3432260003 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE SEATBELT BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 5129 786 (CAN) SEAT BELT WILL NOT LOCK IN PLACE. BELT BUCKLE RELEASE SPRING BROKEN. 1 G 7 1 3U 3 U H9EU E19EU 1998121800440 19981218 00440 EA 1998 12 18 CA981019005 1 19981003 A 2913 NAS1611034 PUMP DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 LEAKING W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 18124 2669 123144 (CAN) DURING CRUISE, NR 1 HYDRAULIC SYSTEM STARTED LOSING FLUID AS INDICATED BY THE QUANTITY GAUGE. FLAP CONTROLS NOT A FFECTED AS SYSTEM MAINTAINED HYDRAULIC PRESSURE. ON SHUT DOWN, THE HYDRAULIC RESERVOIR WAS FOUND TO BE EMPTY. FURTHER INVESTIGATION REVEALED NR 1 ENGINE HYDRAULIC PUMP WAS LEAKING AT THE FLANGE BETWEEN HOUSING AND VALVE PLATE BODY. HYDR AULIC PUMP REPLACED. PART TC: 21,142. 2 H 7 2 4T 4 T RT A13NM E20NE 1998121800445 19981218 00445 NE 1998 12 18 CA981019017 2 19981002 A 7200 ENGINE BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE NR 2 MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P662912 (CAN) NR 2 ENGINE FAILED IN CLIMB, BIG BANG HEARD/FELT WITH HIGH EGT AND WARNING LIGHT. IN-FLIGHT ENGINE SHUTDOWN WAS C ARRIED OUT AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE. POST-FLIGHT INSPECTION FOUND METAL IN THE TAILPIPE. THE ENGINE WAS REPLACED. 2 L 7 4 4F 4 F A20WE E20EA 1998121800446 19981218 00446 NM 1998 12 18 CA981019018 1 19981002 A 7931 SWITCH BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE NR 2 ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CA P662912 (CAN) NR 2 ENGINE OIL PRESSURE LIGHT ILLUMINATED WITH AN ACCOMPANYING LOW OIL PRESSURE GAUGE IN-FLIGHT. THE ENGINE WAS SHUTDOWN. POS-FLIGHT INSPECTION OF THE ENGINE CHIP DETECTORS AND OIL FILTERS FOUND NO FAULT. THE NR 2 ENGINE OIL PRESS URE SWITCH WAS REPLACED AND THE ENGINE WAS GROUND RUN SERVICEABLE. 2 L 7 4 4F 4 F A20WE E20EA 1998121800447 19981218 00447 WP 1998 12 18 CA981019022 1 19981002 A 2131 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE CABIN PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA P657309D (CAN) DURING CLIMB THROUGH LEVEL 280, CABIN PRESSURE RED WARNING LIGHT CAME ON. RAPID DEPRESSURIZATION DRILL CARRIED OU T, BUT CABIN REACHED 11,000 FEET. FLIGHT RETURNED TO BLOCKS. BOTH CONTROLLERS REPLACED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998121800448 19981218 00448 WP 1998 12 18 CA981019023 1 19981003 A 2430 REGULATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE DC SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA P656990D (CAN) IN-FLIGHT AIRCRAFT CROSS TIE LOCKOUT LIGHT CAME ON. CARRIED OUT QRH CK LIST WITH ONE RESET. LIGHTS STAYED ON, AI RCRAFT RETURNED. LT VOLTAGE REGULATOR AND GENERATOR REPLACED. GROUND RUN SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998121800449 19981218 00449 NM 1998 12 18 CA981019024 1 19980928 A 2842 3004200000401 CONTROL UNIT AIRBUS A319 A319114 NM LT FUEL CELL FAILED W H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 CA (CAN) AIRCRAFT RETURNED DUE FUEL MIGRATION FROM LEFT TANK TO RIGHT TANK. ELECTRONIC CENTRALIZED AIRCRAFT MONITORING ACT IONS CARRIED OUT. LEFT TANK 600 KILOGRAMS, RT TANK 2900 KLS. ON APPROACH, FUEL WAS MIGRATING BACK TO LEFT TANK. CONFI RMED INDICATION IN CRUISE L2.0 ON APPROACH L1.4. CHANGED FUEL LEVEL SENSING CONTROL UNIT NR ONE. CHECKED FOR FUEL MIGRA TION WITH PUMPS ON, OK. 2 L 7 2 4F RT A28NM 1998121800450 19981218 00450 NE 1998 12 18 CA981019025 2 19980928 A 7240 767279 COMBUSTION CASE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 58764 6170 P657564D (CAN) DURING ENGINE DISASSEMBLY THE COMBUSTION OUTER CASE WAS FOUND CRACKED IN THE REAR FLANGE AT THREE DIFFERENT LOCATI ONS. THE CRACKS WERE FROM THE HOLES AT THE INNER DIAMETER AND CONTINUED TOWARDS THE OUTER CASE WALL. THE COMBUSTION OU TER CASE WAS REPLACED. PART TC: 67,792. 2 L 7 2 4F 4 F A6WE E2EA 1998121800451 19981218 00451 NM 1998 12 18 CA981019026 1 19980925 A 2120 FILTERS AIRBUS A319 A319114 NM AIR DIST FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) STRONG SMELL IN COCKPIT ON TAKEOFF, LIGHT SMOKE OR HAZE IN CABIN. CARRIED OUT AIR CONDITION SMOKE CHECK LIST, PAC K NR ONE TURNED OFF. ON LANDING, SMOKE DISAPPEARED DURING RETURN. REPLACED RECIRCULATION FILTERS, BOTH ENGINES GROUND RUN WITH BOTH PACKS ON. NO SMOKE OR ODOR FOUND. 2 L 7 2 4F RT A28NM 1998121800452 19981218 00452 EU 1998 12 18 CA981019027 1 19980924 A 2130 SWITCH AIRBUS 320 A320211 3930320 EU COCKPIT FAILED W K NONE O OTHER CR CRUISE 1 CA (CAN) DURING FLIGHT IN AUTOPRESSURIZATION MODE, CABIN WENT TO MANUAL TO CLIMB CABIN UP TO LANDING ON AUTOPILOT. NO MESS AGE ON ELECTRONIC CENTRALIZED A/C MONITORING. FOUND LANDING/ELEVATION SWITCH FAULTY. REPLACED ANTI-ICE LIGHTS PRESSURE CONTROL PANEL ASSEMBLY THAT INCLUDES LANDING/ELEVATION SWITCH. 2 L 7 2 4F RT A28NM 1998121800453 19981218 00453 WP 1998 12 18 CA981019028 1 19980924 A 2161 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT PACK FAILED W C ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CA P657716D (CAN) AIRCRAFT RETURNED TO AIRPORT WITH RIGHT PACK OVERHEAT AND SMOKE AND BURNING SMELL. RIGHT PACK TEMP CONTROL VALVE WENT TO FULL HOT, WHEN COLD SELECTED VALVE RESPONDED CORRECTLY. TEMPERATURE CONTROLLER REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1998121800454 19981218 00454 WP 1998 12 18 CA981019029 1 19980922 A 2161 CONTROLLER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE RT PACK FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA P657716D (CAN) ON DEPARTURE AT 2,500 FEET, THE RIGHT AIR CONDITION PACK OVERHEATED THEN FORWARD FIRE DETECTORS ANNUNCIATED, FLIGH T ATTENDANT REPORTED SMOKE IN CABIN, DECLARED EMERGENCY AND RETURNED TO BLOCKS . REPLACED AUTOMATIC CABIN TEMPERATURE CO NTROLLER. 2 L 7 2 4F 4 F A6WE E2EA 1998121800455 19981218 00455 WP 1998 12 18 CA981019030 1 19980920 A 5280 DOOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE LT MLG JAMMED W K NONE O OTHER TX TAXI/GRND HDL 1 CA P656824D (CAN) AT ARRIVAL GATE, FOUND LEFT MLG DOOR HANGING DOWN. FOUND DOOR JAMMED AND GEAR DOOR FOLLOW-UP EANCO CABLE JAMMING, AND FOLLOW-UP TORQUE TUBE RIVET SHEARED. PARTS REPLACED/REPAIRED. SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998121800456 19981218 00456 NE 1998 12 18 CA981022001 1 19980728 A 6210 6117020201067 BLADE SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2650 61M40043774 295178 (CAN) M/R BLADE BIM CAUTION LIGHT ACTIVATED. BLADE REMOVED, TESTED SERVICEABLE ON PRESSURE TEST IAW S61 MAINT MANUAL. 5 HOURS AFTER REINSTALL, ANOTHER BIM INDICATION. BLADE SENT TO SIKORSKY WHERE IT FAILED SIKORSKY'S TEST. TEST INDICATED A CRACKED SPAR. 2 G 7 2 4U 4 U 1H15 1E3 1998121800457 19981218 00457 NE 1998 12 18 CA981022002 1 19980928 A 6210 6117020201067 BLADE SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE MAIN ROTOR MALFUNCTIONED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 3090 61M39833771 295178 (CAN) M/R BLADE BIM INDICATION IN-FLIGHT. BLADE REMOVED AND SENT FOR TESTING IAW S61 MAINT MANUAL. SPAR PRESSURE TESTE D FOR 10 DAYS. BLADE RETURNED TO SERVICE. 70 FLIGHT HOURS LATER, SAME INDICATION RECURRED. 2 G 7 2 4U 4 U 1H15 1E3 1998121800458 19981218 00458 SW 1998 12 18 CA981022003 1 19981007 A 6210 K911001 BLADE K911001009 KAMAN K1200 K1200 05625F6 SW LYC T53 T5317A 41549 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3039 1166 19B LE07768 (CAN) ON SCHEDULED MAINT, CRACK ON TOP OF BLADE, 10.25 INCHES LONG FROM TRAILING EDGE FORWARD, 1/3 DISTANCE FROM HUB TO TIP, NEAR 'YELLOW' CENTER OF BALANCE STRIP. 1 G 7 1 4F 4 U NT TR7BO E17EA 1998121800459 19981218 00459 WP 1998 12 18 CA981022004 1 19981012 A 3340 3116361 CLAMP GRIMES 369H90062123 HUGHES 369 369D 4470706 WP ALLSN 250C 250C20B 03013 GL STROBE CRACKED W O OTHER D INFLIGHT SEPARATION HO HOVERING 1 CA CAE831673 (CAN) IN THE HOVER, TAIL STROBE LIGHT CLAMP BROKE OFF AT THE ATTACHMENT TABS. POSSIBLE OVERTORQUE OF THE ATTACHMENT SCRE W. 1 G 7 1 3U 3 U H3WE E4CE 1998121800468 19981218 00468 SW 1998 12 18 CA981027003 1 19981019 A 6230 MS178268 NUT 204011400025 BELL 205 205A1 1181414 SW LYC T53 T5313B 41549 NE SWASHPLATE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA JI198452 LEO07774 (CAN) ON DAILY INSPECTION, ONE SCISSOR ASSY HAD TOO MUCH PLAY AT THE PIVOT. PIVOT BOLT CASTELLATED NUT CRACKED AND TORQ UE LOST. NUT HELD IN PLACE BY SPLIT PIN. 1 G 7 1 4U 4 U H1SW E17EA 1998121800475 19981218 00475 WP 1998 12 18 CA981027012 1 19981020 A 6520 B3452 PITCH LINK C0311 ROBSIN R44 R44 7640120 WP LYC O540 O540F1B5 41532 EA T/R HEAD WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 0244 L2490640A (CAN) RECEIVED O/H TAIL ROTOR GEARBOX AND T/R PITCH CONTROL ASSY HAD R22 T/R PITCH LINKS P/N B345-1 INSTALLED INSTEAD OF R44 P/N B345-2. THIS UNIT HAD BEEN O/H AT THE MANUFACTURER. 1 G 7 1 3O 3 O H11NM E295 1998121800477 19981218 00477 1998 12 18 CA981027017 4 19981016 A 3425 6229681001 DISPLAY BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE COCKPIT FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA 1323 PCE114293 HJ518 (CAN) SHORTLY AFTER TAKEOFF, CREW LOST RIGHT EFDU SCREEN FOLLOWED BY A BURNING SMELL. THE SYSTEM WAS ISOLATED AND BOTH AC BUSES WERE SHUT DOWN. AIRCRAFT LANDED SAFELY. UPON FURTHER INVESTIGATION BY MAINTENANCE IT WAS DETERMINED THE RIGHT ELECTRONIC FLIGHT DISPLAY UNIT WAS AT FAULT. THE RIGHT EFDU WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1998121800482 19981218 00482 NM 1998 12 18 CA981027024 1 19981016 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 4899 1559 12900864 120785 (CAN) DURING WALK-AROUND, THE FLIGHT CREW OBSERVED OIL ON THE LOWER COWLING OF NR 1 ENGINE. INSPECTION FOUND THE OIL CO OLER LEAKING. PART TC: 3,232. 2 H 7 2 4T 4 T RT A13NM E20NE 1998121800483 19981218 00483 EU 1998 12 18 CA981028001 1 19981003 A 2913 40052 SEAL FOKKER F28 F28MK1000 4990808 EU HYD PUMP FAILED W O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 CA 39898 (CAN) PILOT REPORTED THE UTILITY HYDRAULIC PRESSURE WAS FLUCTUATING AS WELL AS THE QUANTITY WAS DROPPING ON APPROACH. P UMPS WERE OFF LOADED AND FLUID QUANTITY STILL DROPPED. AIRCRAFT HAD COMPLETE LOSS OF UTILITY SYSTEM FLUID. AIRCRAFT LA NDED AND TOWED TO HANGAR. NR 1 ENG HYDRAULIC PUMP HAD BLOWN SEAL AND SHEARED SHAFT, PUMP. REPLACED FLUID REPLENISHED. PART TC: 37,838. 2 L 7 2 4F RT A20EU 1998121800484 19981218 00484 NE 1998 12 18 CA981028002 2 19981008 A 7321 82455011317 HARNESS DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE FAILED W E A ENGINE SHUTDOWN UNSCHED LANDING J R WARNING INDICATION PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 16389 123135 (CAN) ON TAKEOFF, AT 100 FEET, THE NR 2 ENGINE AUTOFEATHERED. CREW NOTED THE PROP SPEED AT 1400 RPM (SHOULD BE AT 1200 RPM). THE ENGINE WAS SECURED AND THE AIRCRAFT RETURNED TO ITS DEPARTURE POINT. MAINTENANCE REPLACED THE NR 2 ENGINE PRO P CONTROL UNIT, THIS DID NOT FIX THE PROBLEM OF TORQUE FLUCTUATIONS. AFTER INFORMATION RECEIVED FROM THE FDR, THE NR 2 ENGINE ELECTRONIC CONTROL UNIT (ECU) HARNESS WAS REPLACED. THE ENGINE WAS GROUND RUN SERVICEABLE AND THE AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1998121800489 19981218 00489 WP 1998 12 18 TWAA9819701 1 19981212 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 22-29 BROKEN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9630A 53561 FOUND EGRESS LIGHTS OUT ON FLOOR ROWS 22 TO 29. REPAIRED BROKEN WIRE. 2 L 7 2 4F RT A6WE 1998121800490 19981218 00490 WP 1998 12 18 TWAA9819702 1 19981214 A 5730 SKIN DOUG DC9 DC915 3022036 WP LT WING CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 970Z 45772 DURING CHECK-C MAINT, FOUND LT WING, UPPER WING SKIN CRACKED AT AFT O/B CORNER OF FUEL TANK ACCESS PLATE NUMBER 1307A. R EPAIRED CRACK PER SERVICE REWORK DRAWING (DOUGLAS) NUMBER 5951593, AND ARA 16055. 2 L 7 2 4F A6WE 1998121800491 19981218 00491 NM 1998 12 18 CALA9802174 1 19981211 A 3260 6552811120 ACCESSORY UNIT BOEING 737 7372C0 1384488 NM E & E COMPT MALFUNCTIONED A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 14245 22299 20074 THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON FINAL APPROACH TO EWR. THE RED LIGHT WAS ON, A M ANUAL GEAR EXTENSION WAS PERFORMED DURING GO-AROUND AND THE GEAR WAS VISUALLY CHECKED THROUGH VIEW PORT. THE GREEN LIGH T ILLUMINATED ON SECOND APPROACH WHEN FLAPS WERE SET TO 30 DEGREES FOR A NORMAL LANDING. MAINTENANCE INSPECTED THE NOSE GEAR ASSEMBLY AND PROXIMITY SWITCH WIRING WITH NO DEFECTS NOTED. THE NOSE GEAR WAS SWUNG FOUR TIMES AND THE FAILURE CO ULD NOT BE DUPLICATED. THE LANDING GEAR ACCESSORY UNIT WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE IAW MM 32-09 -100. 2 L 7 2 4F A16WE 1998121800492 19981218 00492 WP 1998 12 18 CALA9802175 1 19981213 A 3260 PROX SENSOR DOUG DC9 DC982 3022082 WP RT MLG INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 16813 48066 THE RT MLG GREEN LIGHT FLICKERED WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. THE EMERGENCY GEAR HANDLE WAS PULLED AND TH E GREEN LIGHT ILLUMINATED STEADILY FOR A NORMAL LANDING. THE GROUND PROXIMITY SENSOR WAS CLEANED. A PROXIMITY SENSOR T EST AND EVALUATION FLIGHT WERE CONDUCTED WITH OPERATION AND INDICATIONS CHECKING GOOD. 2 L 7 2 4F A6WE 1998121800493 19981218 00493 WP 1998 12 18 CALA9802176 1 19981214 A 5754 RIB DOUG DC10 DC1010 3022110 WP NR 2 LE SLAT CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND A 4 INCH CRACK IN NR 2 SLAT RIB. THE RIB WAS REPLACED IAW MM 27-80-01, PAGE 402B AND 601 AND SRM 51-31 -01. 2 L 7 3 4F A22WE 1998121800494 19981218 00494 SO 1998 12 18 COMA9810279 1 19981214 A 5720 12061341615 SUPPORT EMB 120 EMB120RT SO LT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 WING SKIN SUPPORT CRACKED. REPLACED SKIN SUPPORT. 2 L 7 2 4T RT A31SO 1998121800495 19981218 00495 SO 1998 12 18 COMA9810280 1 19981214 A 5713 12016086002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 RIGHT WING STRINGER NR 10 CRACKED BETWEEN RIBS NR 7 AND NR 8. REPAIRED WITH TWO PIECE DOUBLER. 2 L 7 2 4T RT A31SO 1998121800496 19981218 00496 SO 1998 12 18 COMA9810281 1 19981212 A 5720 12061341615 SUPPORT EMB 120 EMB120RT SO RT WING BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 1168 DURING FUEL LEAK REPAIR, FOUND SKIN SUPPORT BROKEN IN THE RIGHT WING, RIB 16, BOTTOM CENTER. REPLACED SKIN SUPPORT. 2 L 7 2 4T RT A31SO 1998121800497 19981218 00497 SO 1998 12 18 COMA9810282 1 19981210 A 3350 D36604001 BATTERY EMB 120 EMB120RT SO CABIN DISCHARGED A COMA K NONE L NO TEST TX TAXI/GRND HDL 1 SO 01 189CA 14562 1296 120189 OVERWING EMERGENCY EXIT LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERY. 2 L 7 2 4T RT A31SO 1998121800498 19981218 00498 EA 1998 12 18 COMA9860380 1 19981205 A 7830 1217546 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT ENGINE SEPARATED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 RIGHT ENGINE NR 5 THRUST REVERSER FLEX SHAFT HAS STRAND SEPARATION. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998121800499 19981218 00499 EA 1998 12 18 COMA9860381 1 19981207 A 5230 601R3520537 SUPPORT CNDAIR CL600 CL6002B19 EA CARGO COMPT BROKEN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 CARGO DOOR STEP PLATE SUPPORT BROKEN. REPLACED SUPPORT. 2 L 7 2 4F RT A21EA 1998121800500 19981218 00500 EA 1998 12 18 COMA9860383 1 19981207 A 4980 601R9720419 HEAT SHIELD CNDAIR CL600 CL6002B19 EA APU CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 STIFFENER ANGLE (P/N 601R350-25) AT LOWER FORWARD CORNER OF CARGO DOOR CRACKED. REPLACED ANGLE. 2 L 7 2 4F RT A21EA 1998121800501 19981218 00501 EA 1998 12 18 COMA9860384 1 19981207 A 2910 272955 LINE CNDAIR CL600 CL6002B19 EA LT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 LEFT AILERON PCU LINKS FAILED BACKLASH CHECKS. REPLACED INBOARD AND OUTBOARD LINES. 2 L 7 2 4F RT A21EA 1998121800502 19981218 00502 EA 1998 12 18 COMA9860385 1 19981213 A 3040 SENSOR CNDAIR CL600 CL6002B19 EA LT WINDSHIELD MALFUNCTIONED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 934CA 7042 LEFT HAND WINDSHIELD HEAT CAUTION MESSAGE. SWITCHED TO WINDSHIELD SPARE TEMP SENSORS. SYSTEM TEST SATISFACTORY. 2 L 7 2 4F RT A21EA 1998121800503 19981218 00503 EA 1998 12 18 COMA9860386 1 19981213 A 5610 NP1393215 WINDSHEILD CNDAIR CL600 CL6002B19 EA LEFT SHATTERED A COMA A UNSCHED LANDING O OTHER CR CRUISE 1 SO 01 708CA 545 7235 LEFT WINDSHIELD SHATTERED. REPLACED WINDSHIELD. 2 L 7 2 4F RT A21EA 1998121800504 19981218 00504 WP 1998 12 18 ABXA9801181 1 19981211 A 3350 60030451 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 924AX 47403 EMERGENCY LIGHTS WERE INTERMITTENT. REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-53-02, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998121800505 19981218 00505 WP 1998 12 18 ABXA9801182 1 19981210 A 5610 56443241 RETAINER DOUG DOUG DC9 DC914 3022034 WP LT COCKPIT CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 925AX 45728 DURING C-CHECK, FOUND LEFT WINDOW RETAINER CRACKED. REPAIRED CRACK IAW DC9 SERVICE REWORK DRAWING 5952965. 2 L 7 2 4F A6WE 1998121800506 19981218 00506 WP 1998 12 18 MWEA981148 1 19981204 A 5313 S27729223 LONGERON DOUG DC9 DC932 3022066 WP BS 458-460 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CRACK ON LONGERON 24L AND 25L AT FS 458 AND 460. MTC REMOVED DAMAGED SECTION FABRICATED AND INSTALLED NEW LONGERO N SECTION. 2 L 7 2 4F A6WE 1998121800507 19981218 00507 NM 1998 12 18 MWEA981149 1 19981211 A 5320 991555969 ANGLE DOUG MD88 MD88 3023688 NM FRAME 1401 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CORROSION ON LEFT ANGLE AT FRAME 1401 ON RIGHT SIDE OF VENTRAL STAIR OPENING. MTC FABRICATED AND INSTALLED NEW FR AME WEB TEE CAP AND SUPPORT ANGLES. 2 L 7 2 4F RT A6WE 1998121800508 19981218 00508 NM 1998 12 18 MWEA981150 1 19981211 A 5311 991199023 FRAME DOUG MD88 MD88 3023688 NM BS 14011485 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 808ME 48070 FOUND CORROSION ON LEFT SIDE OF VENTRAL STAIR OPENING WHERE FUSELAGE FRAMES MEET JAMB AT FUSELAGE 1401 TO 1485. MTC FAB RICATED AND INSTALLED WEB AND DOUBLER SPLICE. 2 L 7 2 4F RT A6WE 1998121800509 19981218 00509 NM 1998 12 18 DL73K982533 1 19981210 A 5330 654577871 SKIN BOEING 737 737232 1384475 NM BS 951 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 305DL 23077 THE FUSELAGE SKIN ASSY AND BEAR STRAP WERE FOUND WITH AN APPROX 1 INCH LONG CRACK AT THE LOWER HINGE CUTOUT OF THE AFT G ALLEY DOOR CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND BEAR STRAP AND REPAIRED WITH THREE EXTERNAL ALUMINUM DOUBLE RS. THE REPAIR WAS ACCOMPLISHED PER ER/A 366265-14, REV A. 2 L 7 2 4F RT A16WE 1998121800510 19981218 00510 WP 1998 12 18 DLL19982534 1 19981209 A 5730 16171971 SKIN LKHEED 1011 10113853 5265020 WP WS 130 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 755DL 193Y1184 THE LT WING LOWER SKIN WAS FOUND WITH A 1.25 INCH LONG CRACK BETWEEN FASTENER HOLES AT THE END OF STRINGER 16 (OWS 130). THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN ALUMINUM DOUBLER AND TRIPLER PER ER/A 366221-14, REV A. 2 L 7 3 4F A23WE 1998121800511 19981218 00511 NM 1998 12 18 DLM88982536 1 19981211 A 5330 SKIN DOUG MD88 MD88 3023688 NM C3 DOORWAY GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DE 53410 TWO GOUGES FOUND ON THE SKIN AND UNDERLYING DOUBLER AT THE AFT EDGE OF THE C3 DOORWAY. REPAIRED PER ERA 332554-14. 2 L 7 2 4F RT A6WE 1998121800512 19981218 00512 NM 1998 12 18 DLM88982537 1 19981209 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 237 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DE 53410 DURING INSP, THE FUSE SKIN WAS FOUND DENTED AT APPROX BS 237, L19L. REPAIRED PER ERA 332546-14. 2 L 7 2 4F RT A6WE 1998121800513 19981218 00513 NM 1998 12 18 DLM88982538 1 19981209 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 351 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DE 53410 A DENT WAS FOUND ON THE FUSE SKIN AT APPROX FS 351 JUST ABOVE L20R. CUTOUT MEASURES APPROX 3.1 BY 3.6. REPAIRED PER ER A 332545-14. 2 L 7 2 4F RT A6WE 1998121800514 19981218 00514 NM 1998 12 18 DLM88982539 1 19981209 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 218 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DE 53410 THE FUSE SKIN WAS FOUND DENTED AT APPROX 218 JUST BELOW L18L. RESULTING CUTOUT WAS 2.1 BY 5.9. REPAIRED PER ERA 332548 -14. 2 L 7 2 4F RT A6WE 1998121800515 19981218 00515 NM 1998 12 18 DLM88982540 1 19981209 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 235 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 905DE 53410 THE FUSELAGE SKIN WAS FOUND DENTED AT FS 235 AND L17L. RESULTING CUTOUT IS 9 BY 8.75. REPAIRED PER ERA 332547-14. 2 L 7 2 4F RT A6WE 1998121800516 19981218 00516 NM 1998 12 18 DL76L982541 1 19981211 A 3350 BPS73 POWER SUPPLY BOEING 767 767332 1382001 NM LEFT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 176DN 25061 ON CHECK, FOUND EMERGENCY LIGHTS OUT AT FLOOR LEVEL AT OVERWING EMERGENCY DOORS ON BOTH SIDES OF AIRCRAFT. REPLACED BAT TERY PACK AND CHARGER AT LEFT HAND POSITION AFT OF OVERWING EMERGENCY DOOR. OPN CHECKS OK. 2 L 7 2 4F RT A1NM 1998121800517 19981218 00517 NM 1998 12 18 DL72S982547 1 19981211 A 5320 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 FOUND AT B-1 LETTER CHECK, AFT ENTRYWAY RT FRAME HAS .5 INCH VISIBLE CRACK AT FWD SIDE APPROX 6 INCHES BELOW UPPER STOP PAD. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1998121800518 19981218 00518 NM 1998 12 18 DL72S982548 1 19981211 A 5320 WEB BOEING 727 727232 1384082 NM BS 1239 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 RIGHT I/B VERT TORQUE BOX WEB HAS .5 INCH CRACK AT LWR LIGHTENING HOLE STA 1239 RT. REPAIRED PER M/M 53-11-0 PG 832 TO 833. 2 L 7 3 4F A3WE 1998121800519 19981218 00519 NM 1998 12 18 DL72S982549 1 19981211 A 5754 RIB BOEING 727 727232 1384082 NM NR 5 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 404DA 21148 LTR CHK B-1 12-11-98, NR 5 L/E SLAT I/B ACTUATOR NOSE RIB CRACKED. REPAIRED PER MM 57-54-0. 2 L 7 3 4F A3WE 1998121800520 19981218 00520 NE 1998 12 18 DL757982551 2 19981211 A 7230 COMPRESSOR BOEING 757 757232 1384965 NM PWA 2037 PW2037 NE NR 2 ENGINE STALLED A DALA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 27 623DL 17864 22913 716592 NR 2 ENG COMP STALL AFTER TAKEOFF AT APPROX 10,000 FT, OVERTEMP 692. FLAMES NOTED, ENGINE SHUTDOWN IN FLIGHT BY CREW. T EMP ONLY STARTED TO DECREASE AFTER FUEL WAS SHUTOFF. REPLACED NR 2 ENG PER TRANS 6T103. 2 L 7 2 4F 4 F RT A2NM E17NE 1998121800521 19981218 00521 NM 1998 12 18 DL72S982552 1 19981211 A 3350 BATTERY PACK 10617843 BOEING 727 727232 1384082 NM PWA 2037 PW2037 NE RIGHT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA 1289 21144 716592 RT FWD OVERWING EMERGENCY LIGHT INOP. REPLACED CARTRIDGE AND BATTERY PACK. 2 L 7 3 4F 4 F A3WE E17NE 1998121800522 19981218 00522 NM 1998 12 18 DL72S982553 1 19981211 A 3350 BATTERY PACK 90052 BOEING 727 727232 1384082 NM PWA 2037 PW2037 NE RT OVERWING DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 400DA T3911 21144 716592 RT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND CARTRIDGE. 2 L 7 3 4F 4 F A3WE E17NE 1998121800523 19981218 00523 NM 1998 12 18 DL72W982556 1 19981212 A 3350 BATTERY PACK S106 BOEING 727 727247 138408F NM L1 EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2807W 20579 EMERG EXIT LIGHT ABOVE L1 DOOR WEAK DURING TEST. REPLACED BATTERY PACK. 2 L 7 3 4F A3WE 1998121800524 19981218 00524 NM 1998 12 18 DL72S982557 1 19981212 A 3397 WIRE BOEING 727 727232 1384082 NM 1L DOORWAY DAMAGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 517DA 21433 EMERGENCY LIGHTS IN F/C AND ENTRY DOOR AREAS INOP. FOUND WIRES TO 1L DOOR EXIT LIGHT PINCHED BEHIND SIDEWALL AREA. REP AIRED AND REPLACED BATT AND RACK DUE BLOWN FUSES. 2 L 7 3 4F A3WE 1998121800525 19981218 00525 WP 1998 12 18 DLL10982560 1 19981213 A 3350 POWER SUPPLY 5165741 LKHEED 1011 10113851 5265010 WP R2 DOOR INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 729DA 37629 193C1180 CEILING EMERGENCY LIGHTS INOP NEAR R2 DOOR. REPLACED POWER SUPPLY, CHECKS OK. 2 L 7 3 4F A23WE 1998121800526 19981218 00526 NM 1998 12 18 DL757982561 1 19981212 A 3350 BATTERY PACK 20131A BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 671DN 17299 25332 ESCAPE PATH LIGHTING INOP IN TEST ALL OF FIRST CLASS. REPLACED BATTERY PACK. 2 L 7 2 4F RT A2NM 1998121800527 19981218 00527 NM 1998 12 18 SCNA98149 1 19981212 A 3350 6104789 BATTERY PACK BOEING 727 7272J4 1384006 NM L1 & R1 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE SLIDE LIGHTS AT THE R1 AND L1 DOORS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPL ACED EMERGENCY BATTERY PACK, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998121800528 19981218 00528 NM 1998 12 18 SCNA98150 1 19981212 A 3350 6104789 BATTERY PACK BOEING 727 7272J4 1384006 NM L2 & R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE SLIDE LIGHTS AT THE R2 AND L2 DOORS WERE FOUND TO BE INOPERATIVE. REMOVED AND REPL ACED EMERGENCY BATTERY PACK, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1998121800529 19981218 00529 NE 1998 12 18 ARWA981207 2 19981211 A 7532 K98019 BLEED VALVE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE MALFUNCTIONED A ARWA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 19 661AV 45969 AFTER ROTATION WITH ANTI-ICE ON, NR 4 ENGINE HAD A COMPRESSOR STALL. ALL PARAMETERS FOR REMAINDER OF FLIGHT NORMAL. RE MOVED AND REPLACED NR 4 ENGINE SURGE BLEED VALVE, RT AND LT, IGV ANTI-ICE VALVE, GROUND OPERATION CHECK NORMAL IAW M/M 7 5-20-3, 75-10-5 AND 71-20-0. 2 L 7 4 4F 4 F 4A25 1E8 1998121800530 19981218 00530 NE 1998 12 18 ARWA981208 2 19981211 A 7230 499019 IGV DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE INOP A ARWA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 19 661AV 45969 NR 2 ENGINE WITH CLIMB POWER SET, WHEN TURNING OFF ENGINE ANTI-ICE OFF HAD A COMPRESSOR STALL. ALL PARAMETERS FOR REMAI NDER OF FLIGHT NORMAL. REMOVED AND REPLACED BOTH IGV/ AIR PRESSURE REGULATOR (ANTI-ICE), GROUND OPERATION CHECKED NORMA L IAW M/M 75-10-2 AND 71-00-0. 2 L 7 4 4F 4 F 4A25 1E8 1998121800531 19981218 00531 NM 1998 12 18 VNAA9812005 1 19981209 A 2750 1050A000003 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE TE FLAPS TRIPPED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 439JS 78251 3057 THE AIRCRAFT RETURNED TO THE GATE AFTER RECEIVING A FLAP CONTROL FAIL WARNING MESSAGE. OUTSTATION MAINTENANCE INSPECTED AND RESET THE FLAP CONTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 27-50-00. OPERATIONAL CHECKS WERE COMPL ETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998121800532 19981218 00532 1998 12 18 SWAA983093 4 19981204 A 3425 7771825001 HSI BOEING 737 7373H4 1384600 NM NR 1 INOP A SWAA D RETURN TO BLOCK O OTHER CR CRUISE 1 SW 07 391SW 27378 A/C DIVERTED TO LAS FOR NR 1 HEADING FLAG AND FROZEN COMPASS CARD. REPLACED HSI PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121800533 19981218 00533 NM 1998 12 18 SWAA983095 1 19981209 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 200, RBL 5.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800534 19981218 00534 NM 1998 12 18 SWAA983096 1 19981209 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORRODED AT BS 294, LBL 8. REPAIRED PER SWA RA 1-353-1953. 2 L 7 2 4F RT A16WE 1998121800535 19981218 00535 NM 1998 12 18 SWAA983097 1 19981209 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 189, RBL 1. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800536 19981218 00536 NM 1998 12 18 SWAA983098 1 19981209 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 200, LBL 5.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800537 19981218 00537 NM 1998 12 18 SWAA983099 1 19981209 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 189, LBL 1. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800538 19981218 00538 NM 1998 12 18 SWAA983100 1 19981209 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 178, WL 202, LBL 5.7. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800539 19981218 00539 1998 12 18 SWAA983101 4 19981210 A 3442 866500080405 RT UNIT BOEING 737 7372H4 138448C NM COCKPIT INOP A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 057SW 21722 AIRCRAFT RETURNED TO DAL DUE TO WEATHER RADAR BLANKING OUT. REMOVED AND REPLACED WEATHER RADAR R/T PER BOEING M/M. 2 L 7 2 4F A16WE 1998121800540 19981218 00540 NM 1998 12 18 SWAA983102 1 19981208 A 3350 0993411 BALLAST BOEING 737 7372H4 138448C NM LT EMER EXIT INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 057SW 21722 DURING SCHEDULED 1/4D CHECK, FOUND CENTER AISLE RT AND LT OVERWING EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BAL LAST AND REPAIRED WIRING PER BOEING M/M. 2 L 7 2 4F A16WE 1998121800541 19981218 00541 NM 1998 12 18 SWAA983103 1 19981209 A 3350 2013A BATTERY BOEING 737 7377H4 NM ROW 16 & 19 DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 701GS 27836 DURING SCHEDULED BC3 CHECK, FOUND CABIN EMERGENCY EXIT LIGHTS ABOVE SEAT ROWS 16ABC AND 19ABC INOP. REMOVED AND REPLACE D BATTERY AND CHARGER PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121800542 19981218 00542 NM 1998 12 18 SWAA983104 1 19981209 A 5330 SKIN BOEING 737 7373A4 1384585 NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH AFT OF LOWER VHF ANTENNA CUTOUT APPROX 1.5 LONG. REPAIR ED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800543 19981218 00543 NM 1998 12 18 98ZZZM930 1 19981006 A 5320 WEB BOEING 727 727277 138408S NM TORQUE BOX OIL CANNED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX V ERTICAL WEB BETWEEN BS 1303 AND BS 1313. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1998121800544 19981218 00544 NM 1998 12 18 98ZZZM931 1 19981011 A 5330 SKIN BOEING 727 727277 138408S NM BS 720-725 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURNG 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON FUSELAGE SKIN INNER SURFACE AT STRINGE R 28L BETWEEN BS 720 AND BS 725. THE CORRODED SKIN 3 INCHES BY 4 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 S RM 53-30-3 FIGURE 3. (M) 2 L 7 3 4F RT A3WE 1998121800545 19981218 00545 NM 1998 12 18 98ZZZM932 1 19981007 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, .5 INCH LONG CRACK WAS FOUND ON RIGHT WING INBOARD FORE FLAP LOWER SKIN AT WBL 97. THE DAMAGED SKIN 1.5 INCH DIAMETER WAS TRIMMED OUT AND REPAIRED PER SRM 51-40-6. (M) 2 L 7 3 4F RT A3WE 1998121800546 19981218 00546 NM 1998 12 18 98ZZZM933 1 19981007 A 2760 SKIN BOEING 727 727277 138408S NM SPOILER DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON NR 11 SPOILER T/E UPPER SKIN. THE DAMAGED SKIN 18.5 INCHES BY 6 INCHES IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F RT A3WE 1998121800547 19981218 00547 EA 1998 12 18 MASA98209 1 19981121 A 3350 1317 BULB BRUCE BM10006002 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27172 7172 PHL/CVG - FLT 5800 - DURING PRE-FLIGHT, CREW DISCOVERED THE RIGHT MIDDLE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE ACTIO N WAS DEFERRED PER MEL 33-51-2. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (X) 2 L 7 2 4F RT A21EA 1998121800548 19981218 00548 CE 1998 12 18 98ZZZM934 1 19981106 A 2161 HYZ51071 TEMP CONTROLLER BEECH 1900 1900D 1154162 CE CABIN FAILED A JJBA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 01 852CA 214 UE55 FUMES REPORTED IN CABIN EN ROUTE FROM ELM TO BOS. AIRCRAFT DIVERTED TO ALB. UPON INSPECTION OF AIRCRAFT, THE PCB IN TH E CABIN TEMPERATURE CONTROLLER HAD BURNED. ADDITIONAL INSPECTION, FOUND WIRES NR H177A22 AND NR H178A22, TO DUCT TEMP S ENSOR SHORTED IN CABIN SIDE WALL. WIRING REPAIRED, TEMP CONTROLLER REPLACED. SYSTEM CHECKS TO SPEC, IAW CHAPTER 21 OF MM. (M) 2 L 7 2 4T RT A24CE 1998121800549 19981218 00549 WP 1998 12 18 ASAA9880203 1 19981006 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121800550 19981218 00550 1998 12 18 ASAA9880202 4 19981005 A 2565 D29985107 SLIDE AIRCRUISERS DOUG DC9 DC983 3022083 WP PAX DOOR FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 733 53016 OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1998121800551 19981218 00551 WP 1998 12 18 ASAA9880201 1 19981005 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - PRIOR TO DEPARTURE OF FLIGHT 534, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121800552 19981218 00552 WP 1998 12 18 ASAA9880198 1 19981002 A 3350 1001191 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 33765 2221 49111 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998121800553 19981218 00553 WP 1998 12 18 ORJA98282 1 19981106 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP FUSELAGE INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 822RA 49932 RNO - EXTERIOR LEFT AND RIGHT EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED OVERWING 'E' LIGHTS POWER SUPPLY, OPS CHECK GOOD. (M) 2 L 7 2 4F A6WE 1998121800554 19981218 00554 WP 1998 12 18 ORJA98281 1 19981109 A 3350 6011779 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 12-14 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 COS - EMERGENCY LIGHTS ROW 12-14 LIGHT IN FLIGHT EN ROUTE TO COS. REMOVED AND REPLACED BATTERY PACK AT FWD RIGHT EMERGE NCY EXIT. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998121800555 19981218 00555 SW 1998 12 18 98ZZZM935 1 19981104 A 2910 27810322682 LINE SWRNGN SA227 SA227AC 8780603 SW LT ENGINE BROKEN A MEJA O OTHER K FLUID LOSS CR CRUISE 1 SW 17 3114G AC583 WHILE EN ROUTE FROM SJU TO BGI, THE AIRCRAFT EXPERIENCED COMPLETE HYDRAULIC FAILURE ON THE LEFT ENGINE. BOTH HYDRAULIC LIGHTS ILLUMINATED AND THE HYDRAULIC GAUGE INDICATED ZERO PRESSURE. AFTER ACCOMPLISHING EMERGENCY GEAR EXTENSION PROCED URE, THE AIRCRAFT LANDED AT BGI WITH NO FLAPS, AND NO NWS. MX FOUND A BROKEN HYDRAULIC LINE AND REPLACED IT WITH A TEMP ORARY FLEX LINE. OPERATIONAL CHECK AND LEAK CHECK WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE AND A MX ACTION REQUEST WAS INITIATED TO TRACK TIME FOR THE TEMPORARY FLEX LINE. UPON RETURN TO THE MX BASE AT SJU, MX REPLACED THE FLE X LINE WITH A HARD LINE. OPERATIONS CHECK AND LEAK CHECK WERE GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998121800556 19981218 00556 NM 1998 12 18 MZZA98229 1 19980928 A 5320 CHANNEL BOEING 727 727224 1384076 NM BS 1137 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON PASSENGER CABIN HAT CHANNEL AT BS 1137, RBBL 31. THE CORRODED HAT CHANNEL WAS REMOVED AND REPLACED WITH NEW HAT CHANNEL MADE FROM BAC 1510-335, 2024-T351 MATER IAL. (M) 2 L 7 3 4F A3WE 1998121800557 19981218 00557 NM 1998 12 18 MZZA98228 1 19980928 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1110-1136 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBBL 45.5 BETWEEN BS 1120 AND BS 1130. THE CORRODED SEAT TRACK FROM BS 1110 TO BS 1136 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B727 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1998121800558 19981218 00558 NM 1998 12 18 MZZA98227 1 19980928 A 5320 6531773 STIFFENER BOEING 727 727224 1384076 NM BS 1176 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON BS 1183 BULKHEAD REINFORCEMENT CH ORD AT BS 1176.9 LBBL 64. THE CORRODED REINFORCEMENT CHORD FROM LBBL 32.75 TO OUTBOARD WAS TRIMMED OUT AND REPLACED WIT H NEW SEGMENT CHORD PER CMI EC/RA NR 5310-0155 DATED 9-5-90. (M) 2 L 7 3 4F A3WE 1998121800559 19981218 00559 NM 1998 12 18 MZZA98226 1 19980928 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1110/1136 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79743 22252 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT LBBL 24 .75 AT BS 1130. THE CORRODED SEAT TRACK FROM BS 1110 TO BS 1136 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B72 7 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1998121800560 19981218 00560 NM 1998 12 18 EIAA980240 1 19980828 A 3510 OXYGEN SYSTEM BOEING 747 747212B 1384886 NM COCKPIT LOW A EIAA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION NR NOT REPORTED 1 NM 09 485EV 20712 HNL - AT FL 310, THE CREW OXYGEN SUPPLY DROPPED TO '0' PSI. RETURNED TO PHNL. DUMPED 10,000 LBLS FUEL, LANDING UNEVENT FUL. (M) 2 L 7 4 4F A20WE 1998121800561 19981218 00561 NM 1998 12 18 AALA981821 1 19980928 A 3260 GEAR WARNING BOEING 727 727223 1384074 NM NLG ACTIVATED A AALA O OTHER N FALSE WARNING CL CLIMB 1 SW 07 871AA 21383 ORD - FLT 1461 - EN ROUTE MCO-ORD, NOSE GEAR RED LIGHT ILLUMINATED AFTER GEAR EXTENSION, RECYCLED GEAR AND LIGHT WENT OU T. LANDED ORD WITHOUT INCIDENT. JACKED AIRCRAFT NOSE, ACCOMPLISHED GEAR SWING THREE TIMES. UNABLE TO DUPLICATE ON GRO UND. SYSTEM GROUND CHECKED NORMAL OPERATION. LUBRICATED GEAR LINKAGE. (M) 2 L 7 3 4F A3WE 1998121800562 19981218 00562 WP 1998 12 18 ASAA9880227 1 19981110 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP PAX DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS FOUND STIFF TO OPERATE AND DIFFICULT TO CLOSE. ADJUSTED THE DOOR OPERAT ING MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998121800563 19981218 00563 NM 1998 12 18 USAASB98264 1 19981005 A 3260 WARNING LIGHT BOEING 737 7373B7 1384580 NM RT MLG ILLUMINATED A USAA O OTHER N FALSE WARNING CR CRUISE 1 EA 19 393US 23315 PIT - FLIGHT WAS EN ROUTE FROM BOS, WHEN THE CREW RECEIVED A RIGHT MLG UNSAFE INDICATION. AIRCRAFT MADE AN UNEVENTFUL L ANDING AT PIT. (M) 2 L 7 2 4F RT A16WE 1998121800564 19981218 00564 EU 1998 12 18 98ZZZM936 1 19980319 A 3260 DOOR WARNING BAG BAE146 BAE146300A 1500267 EU LT MLG ACTIVATED A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 616AW E3145 AFTER GEAR RETRACTION, LEFT MAIN GEAR INTRANSIT LIGHT 'RED' REMAINED ON AND RED LT IN GR HANDLE. COULD NOT DUPLICATE ME GGED AND UPLOCK HARNESSES. GEAR UPLOCK, 50M OHM EACH DOOR UPLOCK .5M OHM. REMOVED AND REPLACED HARNESS, FROZE SENSORS, CLEANED SENSORS, ONE DOZEN GEAR SWINGS ALL GOOD. (M) 2 H 7 4 4F RT A49EU 1998121800565 19981218 00565 EU 1998 12 18 98ZZZM937 1 19980619 A 3520 STRING BAG BAE146 BAE146300A 1500267 EU OXYGEN DOOR MISINSTALLED A A6WA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 612AW E3122 OXYGEN CABIN DROP DOORS FOR MASKS AT POS RIGHT 7 DEF, RT 8 DEF, RT 12 DEF AND LT 5 ABC STRING HINGES ARE NOT LONG ENOUGH FOR DOOR TO SWING OPEN FULLY. ADJUSTED AND CHANGED STRINGS AT RT SIDE 7 DEF, 8 DEF, 12 DEF AND LT 5 ABC. ALL DOORS SW ING FREE. OK FOR SERVICE. (M) 2 H 7 4 4F RT A49EU 1998121800566 19981218 00566 NM 1998 12 18 TSAA9833584 1 19981120 A 3350 8731002511 LIGHT BOEING 737 73725A 1384481 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED RIGHT OVERWING EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800567 19981218 00567 NM 1998 12 18 TSAA9833583 1 19981120 A 3350 9221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED RIGHT OVERWING EXIT IDENTIFIER BATTERY PACK DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800568 19981218 00568 NM 1998 12 18 TSAA9833589 1 19981121 A 3350 86210066 LIGHT BOEING 737 7372X6C 1384552 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 1 POSITION FLOOR PROX LIGHT ASSY DUE TO INOP. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800569 19981218 00569 NM 1998 12 18 TSAA9833594 1 19981126 A 3350 56210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED THE FLOOR PROXIMITY EMERGENCY LIGHT BATTERIES FOR POSITIONS, NR 1, NR 2 NR 3 AND NR 5 FOR LOW VOLTAGE. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800570 19981218 00570 NM 1998 12 18 TSAA9833595 1 19981125 A 3350 6013211 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F A16WE 1998121800571 19981218 00571 NM 1998 12 18 TSAA9833596 1 19981125 A 3350 6013211 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED THE FORWARD LEFT SERVICE DOOR EMERGENCY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F A16WE 1998121800572 19981218 00572 EU 1998 12 18 SIMA983224 1 19981118 A 5320 S5367125720402 WEB AEROSP ATR42 ATR42300 8680920 EU BS 36 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 142DD 040 SAW - DURING MAIN BASE VISIT, FOUND THE WEB AT STRINGER LEVEL 17 RIGHT BETWEEN FRAME 36 AND 38 CORRODED. REMOVED AND RE PLACED THE WEB. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121800573 19981218 00573 EU 1998 12 18 SIMA983232 1 19981119 A 2611 B40NA1500 FAN AEROSP ATR42 ATR42300 8680920 EU CARGO BAY FAILED A SIMA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 293AT 11013 293 MIA - FLT 5714 - AFT CARGO/LAV SMOKE WARNING ACTIVATED AFTER TAKEOFF. RETURNED TO FIELD. FOUND THE SMOKE DETECTOR FAN SMOKING DURING NORMAL OPERATION. REMVOED AND REPLACED THE FAN. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998121800574 19981218 00574 EU 1998 12 18 SIMA983171 1 19981113 A 2530 16707 HOT JUG AEROSP ATR42 ATR42320 8680930 EU GALLEY MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 319AM 319 ORD - FLT 4068 - BURNING RUBBER SMELL IN THE AREA OF THE HOT JUGS. FOUND BURNED HOT JUG RECEPTACLE, MEL'D THE HOT JUG. ON 11-19-98, THE LEFT HOT JUG RECEPTACLE WAS REPLACED AND THE MEL WAS CLEARED. (M) 2 H 7 2 4T RT A53EU 1998121800575 19981218 00575 EU 1998 12 18 SIMA983274 1 19981123 A 3350 3071BPEGPL BULB SAAB SF340 340B 7860101 EU ROW 6BC FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 323AE 340B323 DFW - FLT 3610 - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 6BC DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONA L CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998121800576 19981218 00576 EU 1998 12 18 SIMA983262 1 19981122 A 3320 6510732 BALLASTS SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 332AE 30LH575 340B332 DFW - FLT 5108 - FAINT ELECTRICAL ODOR DETECTED MOMENTARILY IN CABIN AREA, POSSIBLY ADJACENT TO ROWS 4 AND 5. ODOR WAS DETECTED BY F/A AND A COCKPIT QUALIFIED PASSENGER TRAVELING IN THE CABIN. THIS IS A REPEAT WRITE-UP FROM PREVIOUS FLIGH T. INSPECTED LIGHT SOCKETS AND BALLASTS. FOUND TWO BAD, ONE FOR WINDOW AND ONE FOR OVERHEAD LIGHTS AT MID CABIN. REMO VED AND REPLACED BALLASTS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998121800577 19981218 00577 EU 1998 12 18 98ZZZM938 1 19981122 A 3320 6510732 BALLASTS SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 21 332AE 35LH582 340B332 DFW - FLT 5108 - FAINT ELECTRICAL ODOR DETECTED MOMENTARILY IN CABIN AREA, POSSIBLY ADJACENT TO ROWS 4 AND 5. ODOR WAS DETECTED BY F/A AND A COCKPIT QUALIFIED PASSENGER TRAVELING IN THE CABIN. THIS IS A REPEAT WRITE-UP FROM PREVIOUS FLIGH T. INSPECTED LIGHT SOCKETS AND BALLASTS. FOUND TWO BAD, ONE FOR WINDOW AND ONE FOR OVERHEAD LIGHTS AT MID CABIN. REMO VED AND REPLACED BALLASTS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998121800578 19981218 00578 NM 1998 12 18 MZZA98261 1 19981123 A 7932 INDICATOR BOEING 727 7272F9 138407D NM NR 3 ENGINE MALFUNCTIONED A MZZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 13 75429 21427 CTS - FLT 938 - ON TAKEOFF ROLL, NR 3 OIL QTY INDICATOR WENT TO .5 GALLON, ON TAXI BACK TO GATE, INDICATOR RETURNED TO N ORMAL. REJECTED TAKEOFF AT 90 KNOTS APPLIED MEL 79-01. TANK VISUAL CHECK WAS FULL ON ARRIVAL OF FLT 937 AND AGAIN ON R ETURN TO GATE. REMOVED AND REPLACED NR 3 ENGINE OIL QTY TRANSMITTER PER MM 79-31-0. (M) 2 L 7 3 4F RT A3WE 1998121800579 19981218 00579 EA 1998 12 18 MASA98206 1 19981118 A 3350 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA LT EMER EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 FLT 5763 - STL-PHL - DURING PREFLIGHT INSPECTION, CREW NOTICED THAT THE AFT LEFT EMERGENCY EXIT OVERWING FLOOD LIGHT WAS INOPERATIVE. MAINTENANCE CONTROL DEFERRED THE ITEM PER MEL 33-51-2 AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSE QUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1998121800580 19981218 00580 EA 1998 12 18 MASA98205 1 19981118 A 3350 1317 BULB BRUCE CNDAIR CL600 CL6002B19 EA LT EMER EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 47202 7202 FLT 5763 - STL-PHL - DURNG PREFLIGHT INSPECTION, CREW NOTICED THAT THE FORWARD LEFT EMERGENCY EXIT OVERWING FLOOR LIGHT WAS INOPERATIVE. MAINTENANCE CONTROL DEFERRED THE ITEM PER MEL 33-51-2 AND THE AIRCRAFT WAS RETURNED TO SERVICE. IN SU BSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. (M) 2 L 7 2 4F RT A21EA 1998121800581 19981218 00581 NM 1998 12 18 MASA98204 1 19981117 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 DURING A ROUTINE LINE CHECK INSPECTION, MAINTENANCE PERSONNEL FOUND THE NR 2 CABIN OVERHEAD EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED BULB, OPS CHECK GOOD. (M) 2 H 7 2 4T RT A13NM 1998121800582 19981218 00582 EA 1998 12 18 MASA98208 1 19981119 A 3350 CNDAIR CL600 CL6002B19 EA UNKNOWN A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17156 7156 FLT 5815 - RDU-BOS - POST FLIGHT, CREW REPORTED THE EMERGENCY EXIT SIGN AT ROW 8A WAS INOP. MAINTENANCE INSPECTED THE E XIT LIGHT, NO DISCREPANCIES WERE NOTED. THE EXIT LIGHT OPERATED NORMALLY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1998121800583 19981218 00583 EU 1998 12 18 VTZA98302 1 19981001 A 2913 PV304426 PUMP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 487UE 906 FLT 6244 - IAD-PHF - DURING TAKEOFF, THE FLT CREW EXPERIENCED A HYDRAULIC PUMP FAILURE. CREW ABORTED TAKEOFF AND NOTIFI ED DISPATCH AND MAINTENANCE CONTROL AND RETURNED TO IAD. MX CONTROL NOTIFIED LINE MX OPERATIONS AND MECHANICS WERE DISP ATCHED TO THE AIRCRAFT. MX FOUND THE RIGHT HYDRAULIC PUMP FAILED. MX REMOVED AND REPLACED THE HYDRAULIC PUMP IAW APPLI CABLE MM REFERENCE AND ACCOMPLISHED REQUIRED CHECKS. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998121800584 19981218 00584 NM 1998 12 18 TSAA9833581 1 19981118 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 6 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998121800585 19981218 00585 NM 1998 12 18 TSAA9833580 1 19981118 A 3350 8731002511 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED ENTRY SERVICE DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800586 19981218 00586 NM 1998 12 18 TSAA9833579 1 19981115 A 3350 8731002511 LIGHT BOEING 737 737230 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800587 19981218 00587 NM 1998 12 18 TSAA9833577 1 19981113 A 3350 8731002511 LIGHT BOEING 737 737230 NM SERVICE DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800588 19981218 00588 NM 1998 12 18 TSAA9833576 1 19981113 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED BATTERY PACK AT NR 1 POSITION EMERGENCY FLOOR LIGHT DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO S ERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800589 19981218 00589 NM 1998 12 18 TSAA9833574 1 19981113 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM PAX DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800590 19981218 00590 NM 1998 12 18 TSAA9833571 1 19981113 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED THE BATTERY PACK IN THE NR 2 AND NR 5 POSITION EMERGENCY PROXIMITY FLOOR LIGHTS. OPS CHECKED OK. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800591 19981218 00591 NM 1998 12 18 TSAA9833572 1 19981113 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM SERVICE DOOR DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED LT O/W, FORWARD SVC DOOR LIGHT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800592 19981218 00592 NM 1998 12 18 TSAA9833573 1 19981113 A 3350 6013211 BATTERY PACK BOEING 737 7372X6C 1384552 NM SERVICE DOOR DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED LT O/W, FORWARD SVC DOOR EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800593 19981218 00593 NM 1998 12 18 TSAA9833600 1 19981127 A 3350 6013211 BATTERY BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 REPLACED THE AFT SLIDE EMERGENCY LIGHT BATTERY DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1998121800594 19981218 00594 NM 1998 12 18 TSAA9833601 1 19981127 A 3350 9221009 BATTERY BOEING 737 7372X6C 1384552 NM EMERGENCY EXIT DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED THE EMERGENCY EXIT WALKWAY LIGHT BATTERY POWER SUPPLY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800595 19981218 00595 NM 1998 12 18 TSAA9833570 1 19981117 A 3350 86210066 BATTERY PACK BOEING 737 737282 13844AT NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 1 THROUGH NR 6 POSITION FLOOR EMERGENCY PROXIMITY LIGHT BATTERY PACK. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800596 19981218 00596 NM 1998 12 18 TSAA9833588 1 19981120 A 3350 8731002511 LIGHT BOEING 737 7372M6C 1384708 NM PAX DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 REMOVED AND REPLACED AFT ENTRY EXIT IDENTIFIER LIGHT ASSY DUE TO RECEIVES ONLY 1 TRANSMITTER. OPERATIONAL CHECK GOOD. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800597 19981218 00597 NM 1998 12 18 TSAA9833587 1 19981120 A 3350 8731002511 LIGHT BOEING 737 7372X6C 1384552 NM PAX DOOR INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER LIGHT ASSY DUE INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800598 19981218 00598 NM 1998 12 18 TSAA9833586 1 19981120 A 3350 9221009 BATTERY PACK BOEING 737 7372X6C 1384552 NM PAX DOOR DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER BATTERY PACK DUE INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800599 19981218 00599 NM 1998 12 18 TSAA9833585 1 19981120 A 3350 86210066 BATTERY PACK BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED NR 4 FLOOR PROX LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1998121800600 19981218 00600 NM 1998 12 18 AALA981795 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 987 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FUSE SKIN DENTED BETWEEN STRINGER 16L-17L AT STATION 987. CUT OUT DAMAGED AREA OF SKIN. INSTALLED DOUBLER PER SR M 53-30-1 PAGES 5-8. (M) 2 L 7 3 4F A3WE 1998121800601 19981218 00601 NM 1998 12 18 AALA981754 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 2R CORRODED STATION 720 E-F. REPLACED PER SRM 53-10-3 PAGE 40. (M) 2 L 7 3 4F A3WE 1998121800602 19981218 00602 NM 1998 12 18 AALA981793 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 660 SKIN BULGING BETWEEN STRINGER 27L AND 28L. REPLACED SKIN STATION 650-680, STRINGER 25L-25R IAW 53-30-3 FIG 12 PAGE 60-72. REPLACED SHEAR TIE STATION 660 STRINGER 27L AND 28L IAW SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998121800603 19981218 00603 NM 1998 12 18 AALA981791 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON SKIN AND MIGRATING FROM UNDER SHEAR TIE BETWEEN STRINGER 25R AND 26R STATION 1148. INSTALLED R EPAIR DOUBLER IAW SRM 53-30-3 PAGE 66. (M) 2 L 7 3 4F A3WE 1998121800604 19981218 00604 NM 1998 12 18 AALA981790 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 1148 STRINGER 23R THROUGH 25R SKIN BULGING. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 PAGE 77. (M) 2 L 7 3 4F A3WE 1998121800605 19981218 00605 NM 1998 12 18 AALA981789 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 580-590 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON BELLY SKIN STRINGER 28R, STATION 580-590. FABRICATED REPAIR PER SRM 53-30-3, ALODINE TREATED A ND PRIMED AREA PER MM 51-20-0. (M) 2 L 7 3 4F A3WE 1998121800606 19981218 00606 NM 1998 12 18 AALA981788 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 520 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 520, STRINGER 24L, STRINGER CRACKED AT STRINGER CLIP. FABRICATED REPAIR PER SRM 53-10-3 FIG 1, STRI NGER SPLICE. (M) 2 L 7 3 4F A3WE 1998121800607 19981218 00607 NM 1998 12 18 AALA981787 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STRINGER 15L CRACKED AT END JUST FORWARD OF ICE LIGHT HOUSING BETWEEN BS 720B AND 720A. REPAIRED STRINGER 15L BET WEEN BS 720B AND 720A PER SRM 51-10-3. (M) 2 L 7 3 4F A3WE 1998121800608 19981218 00608 NM 1998 12 18 AALA981786 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 15L CRACKED AT END JUST AFT OF ICE LIGHT HOUSING BETWEEN BS 720B AND 720C. REPAIRED STRINGER 15L B ETWEEN STATION 720B AND 720C PER SRM 51-10-3. (M) 2 L 7 3 4F A3WE 1998121800609 19981218 00609 NM 1998 12 18 AALA981785 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 15R CRACKED AT STRINGER END, FORWARD AND AFT OF ICE LIGHT HOUSING. REPAIRED STRINGER 15R FORWARD O F RIGHT ICE LIGHT AND REPAIRED STRINGER 15R AFT OF ICE LIGHT IAW SRM 52-10-3. (M) 2 L 7 3 4F A3WE 1998121800610 19981218 00610 NM 1998 12 18 AALA981784 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 294 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND GOUGE IN RADIUS OF STRINGER 11L STATION 294.5. INSTALLED REPLACEMENT SECTION OF STRINGER FROM 284 TO 312 PE R ESO 11697 DATED 9-17-98. (M) 2 L 7 3 4F A3WE 1998121800611 19981218 00611 NM 1998 12 18 AALA981783 1 19980925 A 5314 KEEL BEAM BOEING 727 727227 1384078 NM BS 870-874 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND KEEL BEAM CUT OUT WEB CRACKED FORWARD SIDE LEFT CUT OUT 15 INCHES UP. REPAIRED CRACKED WEB PER SRM 53-10-2 FIG 4, WEB CRACKED ALL THE WAY THROUGH. NO STOP DRILL. (M) 2 L 7 3 4F A3WE 1998121800612 19981218 00612 NM 1998 12 18 AALA981782 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON STRINGER SPLICE STATION 680 STRINGER 28L. REPLACED STRINGER SPLICE STATION 680, STRINGER 28L I AW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998121800613 19981218 00613 NM 1998 12 18 AALA981781 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON STRINGER SPLICE STATION 680 STRINGER 28R. REPLACED STRINGER SPLICE STATION 680, STRINGER 28R I AW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998121800614 19981218 00614 NM 1998 12 18 AALA981780 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 720D STRINGER 27L PLUS 10 INCHES CORRODED. REMOVED CORRODED STRINGER AND REPAIRED PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998121800615 19981218 00615 NM 1998 12 18 AALA981779 1 19980925 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 388 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND FLOORBEAM CHORD CORRODED STATION 388 BL 0 - RBL 66. REPAIRED FLOORBEAM PER SRM 53-10-8 AND ESO 11697 DATED 8-31-98. (M) 2 L 7 3 4F A3WE 1998121800616 19981218 00616 NM 1998 12 18 AALA981778 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1033 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 22L CORRODED STATION 1033 INSIDE. TREATED AND PRIMED IAW 51-20-0. INSTALLED REPAIR IAW SRM 53-10- 3 FIG 2. (M) 2 L 7 3 4F A3WE 1998121800617 19981218 00617 NM 1998 12 18 AALA981777 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 277 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - BELL FRAME CRACKED STATION 277 STRINGER 16R. REMOVED DAMAGED AS REQUIRED. INSTALLED DOUBLER PER SRM 51-40-2. (M ) 2 L 7 3 4F A3WE 1998121800618 19981218 00618 NM 1998 12 18 AALA981776 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 294 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - WEB CRACKED BELL FRAME STATION 294 AT STRINGER 15 AND 16L. INSTALLED DOUBLER ON BELL FRAME STATION 294 AT STRINGE R 15 AND 16L. (M) 2 L 7 3 4F A3WE 1998121800619 19981218 00619 WP 1998 12 18 AALA982018 1 19981030 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 775 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CORROSION ON GALLEY SUPPORT BETWEEN SEAT TRACKS 3 AND 4 STATION 775. INSTALLED DOUBLER PER ECO 7349, 10-30- 98. (M) 2 L 7 3 4F A22WE 1998121800620 19981218 00620 WP 1998 12 18 AALA982019 1 19981030 A 5320 SUPPORT DOUG DC10 DC1010 3022110 WP BS 775 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CORROSION GALLEY SUPPORT BETWEEN TRACKS 4 AND 5 AT STATION 775. INSTALLED DOUBLER PER ECO 7349, 10-30-98. ( M) 2 L 7 3 4F A22WE 1998121800621 19981218 00621 WP 1998 12 18 AALA982020 1 19981030 A 5315 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 800-810 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FLOORBEAMS AT STATION 800 AND 810 CRACKED AT THE END LEFT SIDE. SPLICED IN NEW SECTION OF FRAME PER AARD 51-01-00 -05 AND SRM 53-60-01 PAGE 7 VOL 1. (M) 2 L 7 3 4F A22WE 1998121800622 19981218 00622 WP 1998 12 18 AALA982021 1 19981029 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 765-770 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CORROSION IN SEAT TRACK NR 6 AT STATION 765-770. REMOVED AND REPLACED SEAT TRACK FROM 765-832 PER SRM 53-70 -00 FIG 1. (M) 2 L 7 3 4F A22WE 1998121800623 19981218 00623 WP 1998 12 18 AALA982022 1 19981030 A 5347 SEAT TRACK DOUG DC10 DC1010 3022110 WP BS 715-755 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CORROSION IN SEAT TRACK NR 6 FROM STATION 715-755. OK FOR CONTINUED SERVICE PER ESO 7349, DATED 10-29-98. ( M) 2 L 7 3 4F A22WE 1998121800624 19981218 00624 WP 1998 12 18 AALA982023 1 19981030 A 5320 TEE DOUG DC10 DC1010 3022110 WP BS 1156 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND BULKHEAD TEE CAP STATION 1156 IS CRACKED OUTBOARD END, TEMP REPAIR INSTALLED. REPAIRED LEFT SIDE TEE CAP PE R MOD DRAWING SR10530073. (M) 2 L 7 3 4F A22WE 1998121800625 19981218 00625 WP 1998 12 18 AALA982070 1 19981106 A 5713 STRINGER DOUG DC10 DC1010 3022110 WP RT WING CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CRACK INDICATION IN HOLE 'D' RIGHT WING NR 8 STRINGER COMPENSATOR FLANGE. REMOVED AND REPLACED RT INBOARD S TRINGER NR 8 PER ESO 7349, DATED 11-5-98. (M) 2 L 7 3 4F A22WE 1998121800626 19981218 00626 NM 1998 12 18 AALA981808 1 19980925 A 5320 CASTINGS BOEING 727 727227 1384078 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND TWO BUSHINGS CORRODED AT 950 'H' LINK FITTING CASTING, BELOW STRINGER 18A LEFT. REPAIRED 950 CASTING LUGS P ER ESO 11697, DATED 8-27-98. (M) 2 L 7 3 4F A3WE 1998121800627 19981218 00627 NM 1998 12 18 AALA981807 1 19980925 A 5320 SUPPORT BOEING 727 727227 1384078 NM BS 1283 BROKEN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 1283 STUB UPPER SKIN SUPPORT IS BROKEN OUT AT INBOARD FASTENER. REPLACED UPPER SKIN SUPPORT AT STAT ION 1283. (M) 2 L 7 3 4F A3WE 1998121800628 19981218 00628 NM 1998 12 18 AALA981806 1 19980925 A 5320 CLIP BOEING 727 727227 1384078 NM BS 680 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER CLIP CRACKED STATION 680 STRINGER 7R. REPLACED CLIP PR 51-10-1. (M) 2 L 7 3 4F A3WE 1998121800629 19981218 00629 NM 1998 12 18 AALA981805 1 19980925 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 686 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND UPPER STRINGER CRACKED AT RIB 686.5 ATTACHMENT ABOVE AFT EDGE OF TANK ACCESS 7217. REPAIRED UPPER STRINGER AT RIB WS 686.5 ATTACHMENT ABOVE AFT ACCESS 7217 PER SB 727-57A159. (M) 2 L 7 3 4F A3WE 1998121800630 19981218 00630 NM 1998 12 18 AALA981804 1 19980925 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 656 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND UPPER STRINGER CRACKED AT RIB 656.5 ATTACHMENT ABOVE AFT EDGE OF TANK ACCESS 7216. REPAIRED UPPER STRINGER AT RIB 656.5 ATTACHMENT ABOVE AFT EDGE OF TANK ACCESS 7216 PER SB 727-57A159. (M) 2 L 7 3 4F A3WE 1998121800631 19981218 00631 NM 1998 12 18 AALA981803 1 19980925 A 5713 STRINGER BOEING 727 727227 1384078 NM WS 629 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND UPPER STRINGER CRACKED AT 629 ATTACHMENT ABOVE AFT EDGE OF ACCESS 7215. REPAIRED UPPER STRINGER AT RIB WS 6 29 ATTACHMENT ABOVE AFT EDGE OF ACCESS 7215 PER SB 727-57A169. (M) 2 L 7 3 4F A3WE 1998121800632 19981218 00632 NM 1998 12 18 AALA981802 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 620 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 FOUND CORROSION ON LOWER SPAR CHORD ANGLE WS 620 JUST INBOARD OF NR 7 SLAT ICE TUBE. INSTALLED DOUBLER PER 57-30-2. (M ) 2 L 7 3 4F A3WE 1998121800633 19981218 00633 NM 1998 12 18 AALA981801 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 243-248 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND UPPER SPAR CHORD CORRODED ABOVE NR 5 L/E FLAP ACTUATOR, RIGHT WING. REMOVED CORROSION PER SRM 51-10-6 AND I NSTALLED DOUBLER STRAP PER ESO 11697, DATED 9-2-98. (M) 2 L 7 3 4F A3WE 1998121800634 19981218 00634 NM 1998 12 18 AALA981800 1 19980925 A 5720 CASTING BOEING 727 727227 1384078 NM WS 240 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - NR 5 L/E FLAP CENTER HINGE CASTING CORRODED, RT WING. REPLACED NR 5 L/E FLAP CENTER HINGE CASTING. (M) 2 L 7 3 4F A3WE 1998121800635 19981218 00635 NM 1998 12 18 AALA981799 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 212-232 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND WS 212-232 UPPER SPAR CHORD CORRODED INBOARD OF NR 5 L/E FLAP ACTUATOR. REMOVED CORROSION PER SRM 51-10-6 A ND INSTALLED DOUBLER STRAP PER ESO 11697, DATED 9/2/98. (M) 2 L 7 3 4F A3WE 1998121800636 19981218 00636 NM 1998 12 18 AALA981798 1 19980925 A 5720 CASTING BOEING 727 727227 1384078 NM RT WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - NR 4 L/E FLAP CENTER HINGE CASTING CORRODED INBOARD AND OUTBOARD SIDES AND UPPER OUTBOARD END. REMOVED AND REPLAC ED NR 4 L/E FLAP CENTER HINGE CASTING WITH NEW CASTING, P/N 65-18531-8. (M) 2 L 7 3 4F A3WE 1998121800637 19981218 00637 NM 1998 12 18 AALA981797 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 259 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND AFT UPPER CORNER OF F/O NR 3 WINDOW CUTOUT SKIN IS CRACKED AROUND FASTENER. STOP DRILLED CRACK AND INSTALLE D DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998121800638 19981218 00638 NM 1998 12 18 AALA981796 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1042 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND DENT IN FUSE AT STATION 1042 BETWEEN STRINER 22 AND 23 RIGHT. REMOVED DAMAGED AREA OF SKIN AND INSTALLED DO UBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 3 4F A3WE 1998121800639 19981218 00639 NM 1998 12 18 AALA981972 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND BELL FRAME SPLICE DENTED STATION 600 BETWEEN STRINGER 26 LEFT - 25 RT. INSTALLED 8 INCH DOUBLER 7075 T-6 .0 63 WITH 20 .1875 MS20470DD RIVETS, 2 ROWS PAST DAMAGE, 1 ROW ON TOP, .75 SPACING PER 51-40-3 FIG 1 PAGE 3. (M) 2 L 7 3 4F A3WE 1998121800640 19981218 00640 NM 1998 12 18 AALA981971 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - BELL FRAME DENTED STATION 600 ABOVE STRINGER 23 LEFT. INSTALLED 7.5 INCH DOUBLER .063 7075 T-6 WITH 21 .1875 MS20 470DD RIVETS, 2 ROWS PAST DAMAGE, 1 ROW ON TOP .75 SPACING PER SRM 51-40-3 FIG 1 PAGE 3. (M) 2 L 7 3 4F A3WE 1998121800641 19981218 00641 NM 1998 12 18 AALA981973 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - BELL FRAME DENTED TOP LEG STATION 560 BETWEEN STRINGER 24 LEFT AND 23 LT. INSTALLED DOUBLER .063 INCH 7075-T6 WIT H 18 'D' RIVETS .1875 INCH UNIVERSAL HEAD AND 4 'D' RIVETS .25 INCH UNIVERSAL HEAD PER SRM 51-40-3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1998121800642 19981218 00642 NM 1998 12 18 AALA981974 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - LEFT BELL FRAME DENTED AND WEB BULGED AT STATION 520 ABOVE STRINGER 24 LEFT. CUT OUT DAMAGED AREA AND INSTALLED D OUBLER .063 INCH 7075-T6 MATERIAL INSTALLED 27 UNIVERSAL HEAD .1875 INCH 'D' RIVETS AND 4 UNIVERSAL HEAD .25 INCH RIVETS PER SRM 51-40-3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1998121800643 19981218 00643 NM 1998 12 18 AALA981975 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - BELL FRAME DENTED AND WEB BULGED STAITON 500 BETWEEN STRINGER 24L TO 23L. INSTALLED DOUBLER REPAIR PER ESO 51-40- 3 PAGE 3 FIG 1 USING 7075-T6 .063 INCH MATERIAL, 22 UNIVERSAL HEAD 'D' RIVETS .1875 INCH DIAMETER CUTTING OUT 3 INCH OF THE TOP LEG DAMAGED AREA. (M) 2 L 7 3 4F A3WE 1998121800644 19981218 00644 NM 1998 12 18 AALA981976 1 19980929 A 5320 CLIP BOEING 727 727223 1384074 NM BS 950 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND STRINGER CLIP TORN AND CRACKED STATION 950F, STRINGER 3R (LOWER OUTBOARD SIDE). REMOVED TORN AND CRACKED ST RINGER CLIP AND REPLACED WITH NEW STRINGER CLIP AT BS 950F, STRINGER 3R. (M) 2 L 7 3 4F A3WE 1998121800645 19981218 00645 NM 1998 12 18 AALA981977 1 19980916 A 5320 STRAP BOEING 727 727223 1384074 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND TIE STRAP CRACKED IN HALF STATION 930, STRINGER 14L. REMOVED AND REPLACED TIE STRAP. (M) 2 L 7 3 4F A3WE 1998121800646 19981218 00646 NM 1998 12 18 AALA981978 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - RIGHT BELL FRAME HAS 3 DENTS STATION 500 BETWEEN STRINGER 24 RT AND 22 RT. INSTALLED DOUBLER ON BELL FRAME PER SR M 51-40-3 FIG 1 PAGE 3, 12 INCH BY .050 DOUBLER 7075-T6 WITH 2 ROWS PAST DAMAGE 1 ROW ON TOP, INSTALLED 27 .1875 MS2047D D RIVETS. (M) 2 L 7 3 4F A3WE 1998121800647 19981218 00647 NM 1998 12 18 AALA981979 1 19981009 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - STATION 1166 BELL FRAME SHEAR TIE CORRODED AFT SIDE OUTBOARD OF STRINGER 29. REMOVED AND REPLACED CORRODED SHEAR TIE PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1998121800648 19981218 00648 NM 1998 12 18 AALA981980 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1010 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND STATION 1010 BELL FRAME DAMAGED BELOW STRINGER 25L AND 26L. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER REP AIRS PER AARD 53-10-7-3 AND SRM 51-40-3, 7075-T6 .071 DOUBLER 4 RIVETS EACH SIDE, DAMAGE 2 ROWS RIVETS INWEB .25 INCH AN D .1875 INCH D RIVETS. (M) 2 L 7 3 4F A3WE 1998121800649 19981218 00649 NM 1998 12 18 AALA981981 1 19980929 A 5311 FRAME BOEING 727 727223 1384074 NM BS 360 MISDRILLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - DOUBLER DRILLED HOLE IN BELL FRAME T BS 360 AFT SIDE OF FRAME BELOW STRINGER 2R. REPAIRED BELL FRAME AT BS 360 BE LOW STRINGER 2R. REPAIRED BELL FRAME AT BS 360 BELOW STRINGER 2R PER SRM 51-40-2 FIG1. (M) 2 L 7 3 4F A3WE 1998121800650 19981218 00650 NM 1998 12 18 AALA981982 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 CHAFED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - WEB OF BELL FRAME DAMAGED, HOLE WORN THROUGH, AFT SIDE STATION 500 ABOVE AND INBOARD OF STRINGER 27R. REMOVED DAM AGED AREA, INSTALLED DOUBLER FROM 2024-T3 .063 INCH ADDED .080 SHIM, WITH 18 FASTENERS, BOLTS. 1875 INCH DIAMETER PER SR M SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1998121800651 19981218 00651 NM 1998 12 18 AALA981983 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - BLENDED OUT GOUGE, HPEC, FLAP PEENED, ALODINE, PRIMED, INSTALLED 17 INCH BY 2 INCH L-ANGLE, 17.7PH STAINLESS STEEL .050 INCH. REPAIRED PER ESO 11697, DATED 9/17/98. (M) 2 L 7 3 4F A3WE 1998121800652 19981218 00652 NM 1998 12 18 AALA981986 1 19981009 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 1075 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - STRINGER 27L CORRODED AT STATION 1075 CAUSING 2.5 INCH CRACK IN BELLY SKIN. CUT OUT DAMAGED AREA OF SKIN. REMOVE D CORROSION FROM STRINGER 27L PER SRM 51-10-6. INSTALLED DOUBLER ON SKIN PER SRM 53-30-3 FIG 3. INSTALLED 'U' CHANNEL REPAIR ON STRINGER 27L PER SRM 53-103 PAGE 4E, FIG 2 SHEET 3. (M) 2 L 7 3 4F A3WE 1998121800653 19981218 00653 NM 1998 12 18 AALA981988 1 19981009 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 REMOVED CORROSION PER SRM 51-10-6, INSTALLED STRAP PER ESO 11697, DATED 9-15-98. (M) 2 L 7 3 4F A3WE 1998121800654 19981218 00654 NM 1998 12 18 AALA981989 1 19981009 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND CORROSION ON SHEAR TIE FORWARD SIDE STATION 600 OUTBOARD, STRINGER 26 LEFT. REPLACED SHEAR TIE, TREATED AND PRIMED AREA PER SRM 51-10-2. (M) 2 L 7 3 4F A3WE 1998121800655 19981218 00655 NM 1998 12 18 AALA981990 1 19981009 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND CORROSION ON SHEAR TIE AFT SIDE OF STATION 600, OUTBOARD OF STRINGER 26 LEFT. REMOVED AND REPLACED CORRODED SHEAR TIE, TREATED AND PRIMED AREA PER 51-10-2. (M) 2 L 7 3 4F A3WE 1998121800656 19981218 00656 NM 1998 12 18 AALA981993 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - STATION 1166 BELL FRAME SHEAR TIE AFT SIDE OUTBOARD OF STRINGER 29 CORRODED. REMOVED CORROSION PER 51-10-6, TREAT ED, PRIMED CLEANED AND INSTALLED NEW SHEAR TIE 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1998121800657 19981218 00657 NM 1998 12 18 AALA981994 1 19981009 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1166 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - STATION 1166 SHEAR TIE CORRODED AFT SIDE BETWEEN STRINGER 29R-30R. REMOVED AND REPLACED CORRODED SHEAR TIE PER SR M 51-10-6, SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1998121800658 19981218 00658 NM 1998 12 18 AALA981995 1 19981009 A 3211 FITTING BOEING 727 727223 1384074 NM MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - LEFT TRUNNION CORRODED IN BEARING BORE. INSTALLED NEW LEFT TRUNNION FITTING. (M) 2 L 7 3 4F A3WE 1998121800659 19981218 00659 NM 1998 12 18 AALA981947 1 19981009 A 5330 SKIN BOEING 727 727223 1384074 NM BS 580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND CORROSION ON SKIN STATION 580 BETWEEN STRINGER 27 LEFT TO STRINGER 28 LEFT. REPAIRED DAMAGED AREA WITH EXTE NDED REPAIR PER SRM 53-30-3. INSTALLED INTERCOSTALS AS NEEDED CLIP AND OTHER ATTACHING HARDWARE INSTALLED. (M) 2 L 7 3 4F A3WE 1998121800660 19981218 00660 NM 1998 12 18 AALA981948 1 19981009 A 5330 SKIN BOEING 727 727223 1384074 NM BS 495-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FUSELAGE SKIN CORRODED FROM STATION 495 TO STATION 500 FROM STRINGER 28 R TO 27R. REMOVED CORRODED AREAS AND INST ALLED DOUBLER PER SRM 53-30-3 PAGE 12 FIG 3. TREATED AND PRIMED EFFECTED AREAS. (M) 2 L 7 3 4F A3WE 1998121800661 19981218 00661 NM 1998 12 18 AALA981949 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - STATION 1070 BELL FRAME TOP DENTED ABOVE STRINGER 25L. INSTALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998121800662 19981218 00662 NM 1998 12 18 AALA981950 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND STATION 990 BELL FRAME DENTED ABOVE STRINGER 25L-26L. CUT OUT DAMAGED AREAS OF BELL FRAME. INSTALLED DOUBL ER REPAIR PER AARD 53-10-7-3. (M) 2 L 7 3 4F A3WE 1998121800663 19981218 00663 NM 1998 12 18 AALA981951 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FRAME DENTED AND WEB BULGED STATION 950B LEFT STRINGER 26L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER AARD 5 3-10-07-3. (M) 2 L 7 3 4F A3WE 1998121800664 19981218 00664 NM 1998 12 18 AALA981952 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND STATION 950B AND F BELL FRAME TOP BENT WEB BULGED BETWEEN STRINGER 26R AND 25R. CUT OUT DAMAGED AREA AND IN STALLED DOUBLER PER AARD 53-10-07-3. (M) 2 L 7 3 4F A3WE 1998121800665 19981218 00665 NM 1998 12 18 AALA981953 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND STATION 1050 BELL FRAME DAMAGED ABOVE STRINGER 27R. CUT OUT DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER REPAIR PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998121800666 19981218 00666 NM 1998 12 18 AALA981954 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1030 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND STATION 1030 BELL FRAME DENTED INBOARD STRINGER 26R. CUT OUT DAMAGED AREA. INSTALLED DOUBLER PER SRM 53-10 -4. (M) 2 L 7 3 4F A3WE 1998121800667 19981218 00667 NM 1998 12 18 AALA981955 1 19981009 A 5315 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - STRINGER 15R CRACKED AT STATIO N720B PLUS 4 INCH JUST FORWARD OF ICE LIGHT. INSTALLED REPAIR TO STRINGER 15R AT S TATION 720B PER SRM 53-10-3 FIGURE 5. (M) 2 L 7 3 4F A3WE 1998121800668 19981218 00668 NM 1998 12 18 AALA981956 1 19981009 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - STRINGER 15L CRACKED IN TWO PLACES AT FASTENERS, STATION 720B PLUS 16 INCHES, AFT OF ICE LIGHT. REMOVED DAMAGED A REA OF STRINGER 15L, AFT OF ICE LIGHT STATION 720C. REPAIRED WITH STRINGER SPLICE PER SRM 53-10-3 DETAIL 2. (M) 2 L 7 3 4F A3WE 1998121800669 19981218 00669 NM 1998 12 18 AALA981957 1 19981009 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND UPPER FLANGE OF FLOORBEAM CORRODED. REMOVED AND REPLACED TOP CHORD OF STATION 344 FROM RBL 6 INCHES TO LBL 67 INCHES. DRILLED HOLES ALODINED AND PRIMED PER SRM 51-10-2 AND REINSTALLED TWO WEB STIFFENERS STATION 344 BL 0 AND RB L 8 PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1998121800670 19981218 00670 NM 1998 12 18 AALA981958 1 19981009 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FLOORBEAM CORRODED ON UPPER FLANGE RBL 24 TO RBL 63 AT STATION 480. REPAIRED PER SRM 53-10-8, WITH APPROX 6 INCHE S FILLER ON TOP FLANGE WITH ANGLES ON BOTH SIDES OF BEAM. (M) 2 L 7 3 4F A3WE 1998121800671 19981218 00671 NM 1998 12 18 AALA981959 1 19981009 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FLOORBEAM UPPER FLANGE CORRODED STATION 400 RBL 21 TO LBL 21. REMOVED CORROSION, INSTALLED FILLER RBL 2 TO 4.5, I NSTALLED REPAIR WITH ANGLE ON BOTH SIDES OF FLOORBEAM. (M) 2 L 7 3 4F A3WE 1998121800672 19981218 00672 NM 1998 12 18 AALA981960 1 19981009 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - REPAIRED 380 FLOORBEAM RBL 7 TO RBL 30 WITH FILLER ON TOP AND ANGLE ON BOTH SIDES PER SRM 53-10-08. (M) 2 L 7 3 4F A3WE 1998121800673 19981218 00673 NM 1998 12 18 AALA981961 1 19981009 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - TOP OF FLOORBEAM CORRODED OUT OF LIMITS RBL 49 TO RBL 71. REPAIRED 380 FLOORBEAM PER SRM 53-10-08 WITH FILLER ON TOP WHERE CUT OUT AND AN ANGLE ON BOTH SIDES OF FLOORBEAM. (M) 2 L 7 3 4F A3WE 1998121800674 19981218 00674 NM 1998 12 18 AALA981962 1 19981009 A 5312 BULKHEAD BOEING 727 727223 1384074 NM BS 303 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - BULKHEAD 303 AT STRINGER 16L, BELOW DOOR STOP CASTING CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER ESO 1 1697, DATED 10/2/98. (M) 2 L 7 3 4F A3WE 1998121800675 19981218 00675 NM 1998 12 18 AALA981967 1 19981009 A 5320 STIFFENER BOEING 727 727223 1384074 NM BS 1384 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - VERTICAL STIFFENER AT STATION 1384 LBL 8 INCHES ABOVE PANEL 5201 AND ABOVE NR 2 ENGINE ANGLE BRACKET HAS CRACK. S TOP DRILLED CRACK. INSTALLED STAINLESS 301 HALF HARD ANGLE DOUBLER .080 PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1998121800676 19981218 00676 NM 1998 12 18 AALA981968 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - RIGHT BELL FRAME DENTED STATION 680 ABOVE STRINGER 24 AND ABOVE STRINGER 23. INSTALLED DOUBLER REPAIR PER SRM 51- 40-3, 2.5 INCH WIDE, 1 INCH DEEP, 17 INCH IN LENGTH, TWO ROWS RIVETS ON SIDE, ONE ROW TOP, 46 EACH .1875 RIVETS TOTAL, M S20470 DD6, 2 ROWS PAST DAMAGE, DOUBLER .063 7057-T6. (M) 2 L 7 3 4F A3WE 1998121800677 19981218 00677 NM 1998 12 18 AALA981969 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - BELL FRAME DENTED BETWEEN STRINGER 23 LEFT AND 22 LEFT. INSTALLED DOUBLER PER SRM 51-40-3 FIG 1 PAGE 3, 9 INCHES IN LENGTH 2.5 INCHES DEEP, 1 INCH WIDE 22 EACH MS20470DD6 RIVETS AT .780 SPACING 2 ROWS PAST DAMAGE, 1 ROW TOP .063 7075 T-6 DOUBLER. (M) 2 L 7 3 4F A3WE 1998121800678 19981218 00678 NM 1998 12 18 AALA981970 1 19981009 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - LEFT BELL FRAME DENTED STATION 660 BETWEEN STRINGER 25 LT AND 24 LT. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER F ROM 7075-T6 .063 INCH THICK, WITH 15 D RIVETS .1875 DIAMETER AREA 4 D RIVETS .25 INCH DIAMETER UNIVERSAL HEAD PER SRM 5 1-40-3 PAGE 3 FIG 1. (M) 2 L 7 3 4F A3WE 1998121800679 19981218 00679 NM 1998 12 18 AALA982100 1 19981116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND STATION 600 FORWARD SIDE OF FRAME WEB AND SHEAR TIE CORRODED BETWEEN STRINGER 26 RT AND 27 RT. REMOVED CORR OSION AND INSTALLED DOUBLER PER SRM 53-10-4 PAGE 58-60, INSTALLED NEW SHEAR TIE. (M) 2 L 7 3 4F A3WE 1998121800680 19981218 00680 NM 1998 12 18 AALA982099 1 19981116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 970-1010 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND CORROSION ON STRINGER 29 LEFT STATION 970-1010. REPLACED STRINGER 29 LEFT STATION 960-1010 PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1998121800681 19981218 00681 NM 1998 12 18 AALA982098 1 19981116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 735-738 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - STRINGER 24L CORRODED INSIDE STATION 735-738. INSTALLED FILLER AND DOUBLER PER SRM 53-10-3 FIG 1 (SHEET 4). (M) 2 L 7 3 4F A3WE 1998121800682 19981218 00682 NM 1998 12 18 AALA982097 1 19981116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FLOORBEAM 380 HAS CORROSION ON TOP SURFACE STATION 380 RBL 49 INCH TO RBL 65 INCH, EXTENDING BELOW FLOORBOARD OUTB OARD SUPPORT CHANNEL. REPAIRED FLOORBEAM AT STATION 380, RBL 42-RBL 66 PER SRM 53-10-08, PAGES 9A AND 9B. (M) 2 L 7 3 4F A3WE 1998121800683 19981218 00683 NM 1998 12 18 AALA982096 1 19981116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - STATION 344, LBL 15 INCH TO RBL 12 INCH CORROSION IN AND AROUND FASTENERS HOLES FLOORBEAM. REMOVED CORROSION AND CRACKED TOP CHORD FROM RBL 16 TO LBL 30. REPAIR PER SRM 53-10-8 FIG 9 AT RBL 16 AND ATTACHED TOP CHORD OF FLOORBEAM TO EXISTING SPLICE AT LBL 30. (M) 2 L 7 3 4F A3WE 1998121800684 19981218 00684 NM 1998 12 18 AALA982095 1 19981116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND STATION 344 RBL 15 INCHES FLOORBEAM UPPER FLANGE CRACKED. CUT OUT DAMAGED AREA OF FLOORBEAM. ACCOMPLISHED REPAIR IAW 53-10-8 FIG 9. (M) 2 L 7 3 4F A3WE 1998121800685 19981218 00685 NM 1998 12 18 AALA982094 1 19981116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - AFT EXTRUDED FRAME AT CARGO DOOR OPENING HAS DEEP GOUGES WITH ALUMINUM PEELING ON 90 DEGREES EDGE 10 INCHES ABOVE LOWER FORWARD CORNER. BLENDED GOUGES AND INSTALLED DOUBLER PER ESO 11677, DATED 10-22-98, DOUBLER 8.5 INCH LONG, 2 INCH ES WIDE, 17-7 PH .050 THICK HEAT TREATED T0160-180 RSI CAD PLATE. (M) 2 L 7 3 4F A3WE 1998121800686 19981218 00686 NM 1998 12 18 AALA982093 1 19981116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 303 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND CRACK IN FRAME AT STATION 303.9 EXTENDING FROM EXISTING WEB CUTOUT AT STA 16L. STOP DRILLED CRACK AND INSTA LLED DOUBLER PER ESO 11697, DATED 10-22-98. (M) 2 L 7 3 4F A3WE 1998121800687 19981218 00687 NM 1998 12 18 AALA982092 1 19981116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND STRINGER 15R CRACKED JUST FORWARD OF ICE LIGHT. REPAIRED STRINGER 15R JUST FORWARD OF ICE LIGHT PER SRM 53- 10-3, FIGURE 5, PAGES 12-17. (M) 2 L 7 3 4F A3WE 1998121800688 19981218 00688 NM 1998 12 18 AALA982091 1 19981116 A 5713 STRINGER BOEING 727 727223 1384074 NM WS 686 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - CRACK IN WING STRINGER NR 10 AT RIB W/W 686.5 (UPPER STRINGER). INSTALLED STRINGER DOUBLER REPAIR PER SB727-57A15 9. (M) 2 L 7 3 4F A3WE 1998121800689 19981218 00689 NM 1998 12 18 AALA982090 1 19981116 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 730 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - STRINGER 15L CRACKED AFT SIDE OF THE ICE LIGHT 730B PLUS 10 INCHES. CUT OUT DAMAGED STRINGER END AND INSTALLED DO UBLER AND FILLER PER SRM 53-10-3 FIG 5 PAGE 12. (M) 2 L 7 3 4F A3WE 1998121800690 19981218 00690 NM 1998 12 18 AALA982089 1 19981116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1030 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FRAME DENTED AT STATION1030 ABOVE STRINGER 25L. CUT OUT DAMAGE AND INSTALLED REPAIR PER SRM 53-4-3. (M) 2 L 7 3 4F A3WE 1998121800691 19981218 00691 NM 1998 12 18 AALA982088 1 19981116 A 5730 SKIN BOEING 727 727223 1384074 NM WS 815 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND CORROSION ON LOWER WING SKIN IN RIGHT PRIMARY HEAT EXCHANGER AREA, STATION 815, RBL 30. INSTALLED DOUBLER P ER SRM 57-30-3 FIG NR 8. (M) 2 L 7 3 4F A3WE 1998121800692 19981218 00692 NM 1998 12 18 AALA982087 1 19981116 A 5730 SKIN BOEING 727 727223 1384074 NM WS 825 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND CORROSION ON LOWER WING SKIN IN LEFT PRIMARY HEAT EXCHANGER AREA STATION 825 APPROX LBL 36 INCHES FORWARD OF EXISTING REPAIR. INSTALLED REPAIR PER SRM 57-30-3 PAGE 19 FIG 8. (M) 2 L 7 3 4F A3WE 1998121800693 19981218 00693 NM 1998 12 18 AALA982086 1 19981116 A 5730 SKIN BOEING 727 727223 1384074 NM WS 845 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND CORROSION ON LOWER SKIN AT LEFT PRIMARY HEAT EXCHANGER AREA AFT OF EXISTING REPAIR (3 AREAS) STATION 845 LBL 36 APPROX. INSTALLED REPAIR PER SRM 57-30-3 PAGE 25 FIG 10. (M) 2 L 7 3 4F A3WE 1998121800694 19981218 00694 NM 1998 12 18 AALA982078 1 19981113 A 5730 SKIN BOEING 727 727223 1384074 NM WING CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 876AA 21388 FOUND CORROSION ON LOWER SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER 2 INCH BY 2 INCH. INSTALLED DOUBLER AND TRIPLER PER SR M 57-30-3 FIG 9 AFTER CORROSION REMOVAL. (M) 2 L 7 3 4F A3WE 1998121800695 19981218 00695 NM 1998 12 18 AALA982077 1 19981113 A 5311 FRAME BOEING 727 727223 1384074 NM BS 303 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 876AA 21388 TUL - FOUND 303.9 FRAME HAS SMALL CRACK EXTENDING FROM CUTOUT/RADIUS FOR STRINGER 16L INTERCOSTAL VIEWED FROM COCKPIT SI DE OF WEB. REPAIRED PER SB 727-53-0153. (M) 2 L 7 3 4F A3WE 1998121800696 19981218 00696 NM 1998 12 18 AALA981944 1 19981009 A 2810 WEB BOEING 727 727223 1384074 NM FUEL CELL CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND 1.5 INCH CRACK ON CENTER NR 2 TANK AFT WALL UPPER SIDE OF BAFFLING OPENING. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 57-10-1. (M) 2 L 7 3 4F A3WE 1998121800697 19981218 00697 NM 1998 12 18 AALA981945 1 19981009 A 5510 BEAM BOEING 727 727223 1384074 NM HORIZ STAB CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND RIGHT STAB T/E BEAM UPPER BEAM HAS CORROSION ON TOP SURFACE ABOVE NR 1 AND NR 2 SUPPORT RIBS. REPAIRED IAW SRM 55-10-1 DETAIL V. (M) 2 L 7 3 4F A3WE 1998121800698 19981218 00698 NM 1998 12 18 AALA981946 1 19981009 A 5730 SKIN BOEING 727 727223 1384074 NM WS 720 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND GOUGE IN SKIN BELOW STRINGER 22L AT FS 720A BELOW SEALANT. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 53-30-3 PAGE 5. (M) 2 L 7 3 4F A3WE 1998121800699 19981218 00699 NM 1998 12 18 AALA981733 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 660 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 660 FRAME BENT AT STRINGER 24L TO 25L. REPAIRED FRAME AS PER SRM 53-10-4 PAGE 3 THROUGH 6. 9M) 2 L 7 3 4F A3WE 1998121800700 19981218 00700 NM 1998 12 18 AALA981732 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 328 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND FRAME CRACKED AT STATION 328 STRINGER 13R. REMOVED CRACKED FRAME AD REPLACED WITH MANUFACTURED PART WITH IN STALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998121800701 19981218 00701 NM 1998 12 18 AALA981731 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 312 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND FRAME AT STATINO 312, STRINGER 13 R CRACKED. REMOVED CRACKED FRAME AND INSTALLED DOUBLER PER SRM 53-10-4. ( M) 2 L 7 3 4F A3WE 1998121800702 19981218 00702 NM 1998 12 18 AALA981730 1 19980925 A 5532 SKIN BOEING 727 727227 1384078 NM VERT STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - SKIN CRACKED PAST STOP DRILL, DOUBLER REPAIR AREA 5TH BAY ABOVE ACCESS OPENING, BELOW STRINGER 6 RT. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 55-30-3. (M) 2 L 7 3 4F A3WE 1998121800703 19981218 00703 NM 1998 12 18 AALA981729 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 520 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FRAME 520 BENT, STRINGER 22L TO STRINGER 25L. INSTALLED DOUBLER REPAIR PER AARD 53-10-07-3 PAGE 1, SAME GAUGE MAT ERIAL .050 INCH. (M) 2 L 7 3 4F A3WE 1998121800704 19981218 00704 NM 1998 12 18 AALA981728 1 19980908 A 5311 FRAME BOEING 727 727227 1384078 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 700 BELL FRAME DENTED STRINGER 22R TO STRINGER 25R. INSTALLED DOUBLER PER AARD 53-10-07-3 PAGE 1 US ING SAME GAUGE MATERIAL. (M) 2 L 7 3 4F A3WE 1998121800705 19981218 00705 NM 1998 12 18 AALA982114 1 19981116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - BELL FRAME STATION 600 BETWEEN STRINGER 24L AND 23L DENTED. CUT OUT DENTED AREA AND INSTALLED DOULER PER SRM 51-4 0-3 FIG 1 PAGE 3-5 9.5 INCH LONG 7075T-6 .063 DOUBLER, 3 ROWS OF RIVETS PASS DAMAGE, 24 .1875 MS2047D6 RIVETS USED. (M) 2 L 7 3 4F A3WE 1998121800706 19981218 00706 NM 1998 12 18 AALA982113 1 19981014 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - BELL FRAME STATION 620 ABOVE STRINGER 24L DENTED. INSTALLED A DOUBLER ON BELL FRAME PER SRM 51-40-3 PAGE 3-5, USI NG 8 INCH DOUBLER OF 7075T-6 .063 USING TWENTY .1875 INCH MS 20470D6 AND TWO .25 INCH MS20470D8 RIVETS. (M) 2 L 7 3 4F A3WE 1998121800707 19981218 00707 NM 1998 12 18 AALA982112 1 19981116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - STATION 660 BELL FRAME DENTED THREE PLACES BETWEEN STRINGER 25R-23R. REPAIRED BELL FRAME AT STATION 660 PER SRM 5 1-40-3, FIG 1, PAGE 3. REMOVED DAMAGE AREA BETWEEN STRINGER 23 AND 24. (M) 2 L 7 3 4F A3WE 1998121800708 19981218 00708 NM 1998 12 18 AALA982111 1 19981116 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 760 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FLOORBEAM WEB CRACKED TWO PLACES STATION 760 AT RBL 58 - RBL 62. STOP DRILLED CRACKS AND REPAIRED FRAME WEB PER S RM 51-40-2 PAGE 1-3 AND 51-40-2 PAGE 5 FIG 1 SHEET 5. TWO ROWS OF .25 INCH HI-LOCK UPPER AND LOWER, TWO ROWS .1875 HI-L OCKS INBOARD AND OUTBOARD .050.5H 301 REPAIR DOUBLER 4.5 INCH BY 8 INCH. (M) 2 L 7 3 4F A3WE 1998121800709 19981218 00709 NM 1998 12 18 AALA982110 1 19981116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - BELL FRAME CRACKED AT FASTENER, STATION 620 ABOVE STRINGER 14R. REPAIRED CRACK AT BELL FRAME AT STATION 620 ABOVE STRINGER 14R PER SRM 51-40-3 FIG 1 SHEETS 1-6, 2024 T3 .071 MATERIAL, INSTALLED WITH .1875 FIRST OVER HI-LOCKS. (M) 2 L 7 3 4F A3WE 1998121800710 19981218 00710 NM 1998 12 18 AALA982109 1 19981116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 576-580 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FUSELAGE SKIN CORRODED OUTBOARD STRINGER 27L STATION 576-580. REMOVED CORROSION AND REPAIRED PER SRM 53-30-3 PAGE 8, FIG 1. (M) 2 L 7 3 4F A3WE 1998121800711 19981218 00711 NM 1998 12 18 AALA982108 1 19981116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - OUTBOARD SIDE STRINGER 27L STATION 720C, 10 INCHES TO 720C PLUS 3 INCHES FUSELAGE SKIN CORRODED UNDER LEVELING COM POUND. REMOVED DAMAGED AREA AND INSTALLED EXTERNAL REPAIR PER SRM 53-30-3 FIG 1 PAGE 8. (M) 2 L 7 3 4F A3WE 1998121800712 19981218 00712 NM 1998 12 18 AALA982107 1 19981116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1050 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND CORROSION ON BELLY SKIN FORWARD SIDE OF STATION 1050 BELL FRAME AT STRINGER 28L. CUT OUT DAMAGED INSTALLED DOUBLER REPAIR PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1998121800713 19981218 00713 NM 1998 12 18 AALA982106 1 19981116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND STATION 720D OUTBOARD STRINGER 2R OUTER SKIN GOUGED. INSTALLED DOUBLER AT STATION 720D STRINGER 2R OUTER SK IN PER SRM 53-30-3 FIG 1 PAGE 5, .061 THICKNESS WITH 72 FASTENERS. (M) 2 L 7 3 4F A3WE 1998121800714 19981218 00714 NM 1998 12 18 AALA982105 1 19981116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - STATION 720D PLUS 10 INBOARD STRINGER 2R SKIN DENTED. INSTALLED DOUBLER AT STATION 720D PLUS 10 INBOARD STRINGER 2R OUTER SKIN PER SRM 53-30-3 FIG 1 PAGE 5, .061 THICKNESS WITH 72 FASTENERS. (M) 2 L 7 3 4F A3WE 1998121800715 19981218 00715 NM 1998 12 18 AALA982104 1 19981116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND GOUGE IN SKIN AT 720D STRINGER 2R. REPAIRED WITH DOUBLER AFTER BLENDING PER SRM 3-30-3. (M) 2 L 7 3 4F A3WE 1998121800716 19981218 00716 NM 1998 12 18 AALA982103 1 19981116 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND GOUGE IN CROWN SKIN AT FS 720D PLUS 10 INCH INBOARD OF STRINGER 2R. BLENDED AREA AND INSTALLED DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998121800717 19981218 00717 NM 1998 12 18 AALA982101 1 19981116 A 5313 BULKHEAD BOEING 727 727223 1384074 NM BS 351 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FOUND CORROSION ON LOWER WEB OF FUSELAGE STAITON 351.2 BULKHEAD APPROX 16 INCH LEFT AND RIGHT OF CENTER LINE. REM OVED CORROSION AND INSTALLED DOUBLER PER SRM 53-10-9 PAGES 10-11. (M) 2 L 7 3 4F A3WE 1998121800718 19981218 00718 CE 1998 12 18 MASA98185 1 19981006 A 5270 WARNING CESSNA 310 310R 2074245 CE PAX DOOR ACTIVATED A MASA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 37218 310R0959 FLT 5750 - BHM-PHL - DURING CLIMB-OUT, CREW RECEIVED AN OUTER DOOR HANDLE CAUTION MESSAGE. CREW DECLARED AN EMERGENCY A ND AIRCRAFT RETURNED TO THE FIELD. MAINTENANCE RELATCHED THE DOOR AND INSPECTED ALL COMPONENTS. NO DEFECTS WERE NOTED. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 1 L 7 2 3O 3A10 1998121800719 19981218 00719 NM 1998 12 18 98ZZZM939 1 19981123 A 3350 6104781 BATTERY PACK DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 803WP D81 141 ON PREFLIGHT, THE PILOTS FOUND THE RIGHT FORWARD EMRGENCY AND EGRESS LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUP PLY NR 2 BATTERY PACK OPS CHECK GOOD IAW DHC8MM 33-51-00 PAGE 201-202. (M) 2 H 7 2 4T RT A13NM 1998121800720 19981218 00720 EU 1998 12 18 98ZZZM940 1 19981030 A 2435 8060300 STARTER/GSU BRAERO DH125 HS125700A 4230170 EU NR 3 FAILED A AJCA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 EA 25 67PW 1525 NA0303 SEVERE VIBRATION NOTED AND ISOLATED TO THE NR 3 GENERATOR. CREW SELECTED GENERATOR OFF, REDUCED NR 3 ENGINE TO IDLE, GE NERATOR CONTINUED TO VIBRATE. SHUT DOWN NR 3 ENGINE AS A PRECAUTION, VIBRATION CEASED. AIRCRAFT THEN DIVERTED TO AN AL TERNATE AIRPORT. (M) 2 L 7 2 4F A3EU 1998121800721 19981218 00721 SW 1998 12 18 98ZZZM941 1 19981027 A 3230 SWITCH SWRNGN SA227 SA227AC 8780603 SW RT MLG INOPERATIVE A MEJA O OTHER J WARNING INDICATION AP APPROACH 1 SW 17 671AV AC671 AFTER TAKEOFF FROM PHX TO LAS, THE RIGHT MAIN GEAR DID NOT RETRACT WHEN GEAR UP WAS SELECTED. THE CREW CYCLED THE GEAR SEVERAL TIMES AND THE RIGHT MAIN GEAR RETRACTED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR UPLIMIT SWITCH AND RERIGGED THE RIGHT GEAR. MAINTENANCE PERFORMED GEAR SWING AND NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998121800722 19981218 00722 WP 1998 12 18 HALA9800369 1 19981026 A 2130 39613011 VALVE DOUG DC9 DC951 3022051 WP ACCESSORY BAY MALFUNCTIONED A HALA O OTHER O OTHER DE DESCENT 1 WP 13 660HA 48122 ITO - FLT 182 - AT TOP OF DESCENT FROM FL 250, UNABLE TO MAINTAIN CABIN PRESSURIZATION WITH LESS THAN CRUISE POWER AND O UTFLOW VALVE FULLY CLOSED IN MANUAL. REMOVED AND REPLACED FLOW CONTROL VALVE ASSEMBLY. OPS CHECK, LEAK CHECK OK ON GRO UND RUN. (M) 2 L 7 2 4F RT A6WE 1998121800723 19981218 00723 WP 1998 12 18 USAAD98202 1 19981111 A 3244 404F429 TIRE DOUG DC9 DC931 3022065 WP RT MLG FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 970VJ 47050 BOS-PIT - FLT 828 - ON ROTATION, THE NR 3 MAIN TIRE BLEW OUT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INC IDENT. MAINTENANCE REPLACED THE NR 3 MAIN TIRE AND WHEEL ASSEMBLY, RIGHT SHIMMY DAMPER, RIGHT LANDING GEAR SPRAY DEFLEC TOR, NR 3 BRAKE LINE, AND THE RIGHT INBOARD FLAP SECTION OF THE RIGHT INBOARD FLAP. (M) 2 L 7 2 4F A6WE 1998121800724 19981218 00724 NM 1998 12 18 USAA980547 1 19981026 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 37157 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND NUTPLATE STATION 344 FLOORBE AM UPPER SURFACE FORWARD ENTRY T-CAP. CORROSION TASK NR C53-107-01. REPLACED T-CAP PER EA 62544 AND TR 53-10-13. (M) 2 L 7 2 4F RT A16WE 1998121800725 19981218 00725 NM 1998 12 18 USAA980548 1 19981026 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 395US 23317 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AROUND NUTPLATE STATION 328 LBL 36 RBL 66 FLOORBEAM UPPER SURFACE FORWARD ENTRY T-CAP. CORROSION TASK C53-107-02. REPLACED T-CAP PER SRM 53-10-51 PAGE 22 0. (M) 2 L 7 2 4F RT A16WE 1998121800726 19981218 00726 WP 1998 12 18 USAAD98196 1 19981102 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP NLG DOOR FAILED A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 970VJ 47050 DAY-PHL - FLT 648 - AFTER TAKEOFF AND GEAR RETRACTION THERE WAS EXCESSIVE VIBRATION FROM THE NOSE GEAR AREA. THE LANDIN G GEAR WAS CYCLED BUT DID NOT HELP. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURE D THE RIGHT NOSE LANDING GEAR DOOR CLOSED. (M) 2 L 7 2 4F A6WE 1998121800727 19981218 00727 NM 1998 12 18 USAABB98110 1 19981021 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 602AU 22196 LAX - FOUND TWO FLOOR LEVEL EMERGENCY LIGHT BATTERIES LOW. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1998121800728 19981218 00728 WP 1998 12 18 USAAD98201 1 19981031 A 3350 14597101 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 956VJ 47588 CLT - THE FIRST CLASS SECTION CEILING EMERGNCY LGIHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE FIRS T CLASS SECTION CEILING EMERGENCY LIGHTS. (M) 2 L 7 2 4F A6WE 1998121800729 19981218 00729 NM 1998 12 18 USAABB98111 1 19981029 A 3350 20121 BATTERY CHARGER BOEING 767 7672B7 1385107 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 655US 25257 PHL - MID LEFT FLOOR EMERGNCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. (M) 2 L 7 2 4F RT A1NM 1998121800730 19981218 00730 WP 1998 12 18 ORJA98280 1 19981103 A 3350 6011779 POWER PACK DOUG DC9 DC983 3022083 WP ROW 6-9 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 AT SJC, EMERGENCY LIGHTS AT ROWS 6, 7, 8 AND 9 DEF DON'T ILLUMINATE. REMOVED AND REPLACED POWER PACK AT RIGHT EMERGENCY EXIT PER MM 33. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998121800731 19981218 00731 WP 1998 12 18 ORJA98278 1 19981101 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 23-26 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 EMERGENCY LIGHTS INOPERABLE AT ROW 23-26, OCCURING AT RENO. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHE CK GOOD. (M) 2 L 7 2 4F RT A6WE 1998121800732 19981218 00732 WP 1998 12 18 ORJA98270 1 19981016 A 3350 EM1267 BATTERY DOUG DC9 DC987 3022087 WP TAIL COMP DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, REAR TAIL EMERGENCY LIGHT NO OPERATING. REPLACED BATTERIES AND ONE POWER PACK. EMERGENCY EXIT LIGHTS, TAIL STA IRWAY. REPAIRED ONE LIGHT HANGING LOOSE. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998121800733 19981218 00733 WP 1998 12 18 98ZZZM942 1 19981016 A 3350 6011779 POWER PACK DOUG DC9 DC987 3022087 WP TAIL COMP INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, REAR TAIL EMERGENCY LIGHT NO OPERATING. REPLACED BATTERIES AND ONE POWER PACK. EMERGENCY EXIT LIGHTS, TAIL STA IRWAY. REPAIRED ONE LIGHT HANGING LOOSE. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1998121800735 19981218 00735 EU 1998 12 18 VTZA98322 1 19981031 A 5210 137984C403 HANDLE BAG JETSTM JETSTM3201 1500217 EU PAX DOOR LOOSE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 488UE 907 FLT 6418 - CLE-IAD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATE D. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 18617, MEL 52-2 . MAINTENANCE INSPECTED AND CLOSED DMI 18617 ON 10-31-98 BY SECURING LOOSE DOOR HANDLE, OPS CHECK OK. AIRCRAFT WAS RE LEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998121800736 19981218 00736 NM 1998 12 18 AALA981845 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON 870 CASTING STRINGER 7R-9R. REPAIRED CASTING PER ESO 11697 DATED 9-16-98, TITLED AND SKIN AND FRAME REPAIR BS 870 AT STRINGER 8 TO 10 RT. (M) 2 L 7 3 4F A3WE 1998121800737 19981218 00737 NM 1998 12 18 AALA981818 1 19980925 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 870AA 21382 TUL - BULGE IN SKIN STATION 680 BETWEEN STRINGER 26 AND 27. INSTALLED NEW SERVICEABLE STRINGER SPLICE AND REINSTALLED I NTERCOSTAL PER SRM 53-10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1998121800738 19981218 00738 NM 1998 12 18 98ZZZM943 1 19980925 A 5330 SKIN BOEING 727 727223 1384074 NM BS 680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 870AA 21382 TUL - BULGE IN SKIN STATION 680 BETWEEN STRINGER 26 AND 27. INSTALLED NEW SERVICEABLE STRINGER SPLICE AND REINSTALLED I NTERCOSTAL PER SRM 53-10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1998121800739 19981218 00739 NM 1998 12 18 AALA981817 1 19980925 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 670 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 870AA 21382 TUL - FOUND STRINGER 27L AT BS 670 HAS CORROSION AT STANDOFF INSIDE OF STRINGER. REMOVED DAMAGED SECTION OF STRINGER AN D INSTALLED FILLER AND DOUBLER AT STRINGER 27L, BS 670 PER SRM 53-10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1998121800740 19981218 00740 NM 1998 12 18 AALA981816 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 724-742 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - UPPER SPAR CHORD CORRODED ABOVE NR 1 L/E SLAT ACTUATOR. REMOVED CORROSION AND INSTALLED STRAP PER ESO 11697 DATED 9-2-98. (M) 2 L 7 3 4F A3WE 1998121800741 19981218 00741 NM 1998 12 18 AALA981815 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - CORROSION ON AND AROUND FASTENERS OUTBOARD OF STRINGER 27L AT STATION 720D. REMOVED CORROSION AND INSTALLED DOUBL ER PER 53-30-3 SRM. (M) 2 L 7 3 4F A3WE 1998121800742 19981218 00742 NM 1998 12 18 AALA981814 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 251 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND SKIN AROUND RIVET FASTENERS BELOW NR 3 F/O'S WINDOW APPEAR TO BE CRACKED. TRIMMED OUT DAMAGED AREA AND INST ALLED REPAIR DOUBLER PER SRM 53-30-3 AND ESO 11697 DATED 8-31-98. (M) 2 L 7 3 4F A3WE 1998121800743 19981218 00743 NM 1998 12 18 AALA981813 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 650-680 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND SKIN BULGING BETWEEN STRINGER 28L TO 28R STATION 650-680. REPLACED SKIN STATION 650-680 STRINGER 25L TO 25R IAW 53-30-5 FIG 12 PAGE 60-72. (M) 2 L 7 3 4F A3WE 1998121800744 19981218 00744 NM 1998 12 18 AALA981812 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 1138-1148 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - SKIN DENTED AND CORRODED STATION 1138-1148, STRINGER 23-26R. CUT OUT DAMAGED ADN CORRODED AREAS OF SKIN AND INSTA LLED DOUBLER REPAIR PER SRM 53-30-3 FIG 1 REF E58-2649873, E98-4 0123694, 0123605, 0123606. (M) 2 L 7 3 4F A3WE 1998121800745 19981218 00745 NM 1998 12 18 AALA981811 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 500 STRINGER 24 RT CORRODED. REPAIRED STRINGER 24 RT STATION 500 AS PER SRM 53-10-03. (M) 2 L 7 3 4F A3WE 1998121800746 19981218 00746 NM 1998 12 18 AALA981810 1 19980925 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 660 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON AND UNDER SHEAR TIE. INSTALL NEW SHEAR TIE STRINGER 27L TO 28R STATION 660 IAW SRM 53-10-4 FIG 15 PAGE 60. (M) 2 L 7 3 4F A3WE 1998121800747 19981218 00747 NM 1998 12 18 AALA981809 1 19980925 A 5313 CORRODED STRINGER BOEING 727 727227 1384078 NM UNKNOWN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA BS1106 20613 TUL - STRINGER 22L LOWER LEG CORRODED AND CRACKED STATION 1106. REMOVED CORROSION AND SMALL CRACK TREATED AND PRIMED AR EA PER MM 51-20-0. INSTALLED 'J' ANGLE. REPAIR PER SRM 50-0-3 FIG 2. (M) 2 L 7 3 4F A3WE 1998121800748 19981218 00748 WP 1998 12 18 ORJA98269 1 19981016 A 3350 6011779 BATTERY PACK DOUG DC9 DC987 3022087 WP ROW 19-22 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJU, EMERGENCY LIGHTS ON ROWS 19, 20, 21, 22 FOUND INOPERATIVE. FOUND PACK TO BE BAD. REMOVED AND REPLACED WITH NEW PACK, ROW DEF. OPS CHECKS GOOD. (M) 2 L 7 2 4F RT A6WE 1998121800749 19981218 00749 WP 1998 12 18 ORJA98283 1 19981106 A 2430 EP410 RELAY DOUG DC9 DC987 3022087 WP E/E BAY FAILED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 753RA 49587 'DC BUS OFF' ANNUNCIATION ON APPLICATION OF TAKEOFF POWER SETTING ABORTED TAKEOFF AT SLOW SPEED (APPROX 20 KNOTS). RETU RNED TO GATE. REPLACED EMERGENCY POWER DC TRAN RELAY (R2-326). GROUND CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998121800750 19981218 00750 WP 1998 12 18 ORJA98279 1 19981106 A 2430 EP410 RELAY DOUG DC9 DC987 3022087 WP E/E BAY FAILED A ORJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 753RA 49587 AT SAN DIEGO, 'DC BUS OFF' ANNUNCIATION ON APPLICATION OF TAKEOFF POWER SETTING. ABORTED TAKEOFF AT LOW SPEED, APPROX 2 0 KTS. RETURNED TO GATE. REPLACED EMERGENCY POWER DC TRANS RELAY (R2-326). GROUND CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998121800751 19981218 00751 SW 1998 12 18 98ZZZM944 1 19981027 A 3230 NAS110427 UPLOCK BOLT SWRNGN SA227 SA227AC 8780603 SW RT MLG SHEARED A MEJA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 17 366AE AC681 AFTER TAKEOFF FROM OPF-MIA, THERE WAS NO UP AND LOCK INDICATION ON RIGHT MAIN GEAR. THE CREW RECYCLED THE GEAR BUT THE LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO OPF WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND UPLOCK ROLLER BOLT SHEARED AND REPLACED THE BOLT AND ROLLER. GEAR SWING WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998121800752 19981218 00752 SW 1998 12 18 98ZZZM945 1 19981106 A 3230 RETRACT MECH SWRNGN SA227 SA227AC 8780603 SW NLG LACK OF LUBE A MEJA O OTHER J WARNING INDICATION CL CLIMB 1 SW 17 378PH AC575 ON GEAR RETRACTION AFTER TAKEOFF FROM CVG TO ORF, THE NOSE GEAR WOULD NOT LOCK UP AND WAS BOUNCING IN THE WHEEL WELL. T HE CREW RECYCLED THE GEAR AND THE GEAR LOCKED UP PROPERLY. THE AIRCRAFT CONTINUED FLIGHT TO ORF WITHOUT FURTHER INCIDEN T. AIRCRAFT WAS FERRIED TO RIC FOR MAINTENANCE. MAINTENANCE ADJUSTED THE UPLIMIT SWITCH AND LUBED THE GEAR. GEAR SWIN G WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998121800753 19981218 00753 WP 1998 12 18 EIAA980239 1 19980828 A 3260 INDICATOR DOUG DC9 DC933F 302207A WP MLG FAILED A EIAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 NM 09 933F 47191 OAK - UPON ARRIVAL AT BILLINGS, LEFT MAIN GEAR GREEN LIGHT DID NOT ILLUMINATE. GEAR UNSAFE RED LIGHT DID NOT ILLUMINATE UPON THROTTLE BACK AT TOP OF DESCENT. PERFORMED LOW APPROACH AT BILLINGS FOR MX AND TOWER VERIFICATION OF GEAR EXTENSI ON. GEAR APPEARED DOWN, NO HORN SOUNDED. LANDING WAS UNEVENTFUL. (M) 2 L 7 2 4F A6WE 1998121800754 19981218 00754 NM 1998 12 18 AALA981775 1 19980925 A 5320 STIFFENER BOEING 727 727227 1384078 NM BS 830 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - HORIZ 'J' CHANNEL TOP OF NR 3 CELL FORWARD WEB OPENING, CRACKED AT LEFT ATTACH TO VERTICAL STIFFENER. ROUTED OUT CRACKED AREA. INSTALLED 301.5 HARD DOUBLER PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1998121800755 19981218 00755 NM 1998 12 18 AALA981774 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 540 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 540 FRAME BENT STRINGER 23L TO STRINGER 24L. INSTALLED DOUBLER AS PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1998121800756 19981218 00756 NM 1998 12 18 AALA981773 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 1082 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 7L HAS TWO MISDRILLED HOLES AT STATION 1082. INSTALLED 'J' ANGLE (2024 T3.060) PER SRM 53-10-3 PAG E 4D. (M) 2 L 7 3 4F A3WE 1998121800757 19981218 00757 NM 1998 12 18 AALA981772 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1030 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 1030 BELL FRAME TOP AND WEB BULGED AND DENTED IN TWO PLACES BETWEEN STRINGER 26L AND 27L. INSTALLED DOUBLER PER SRM 51-4-3. DOUBLER IS .071 INCH 7075 T-6 USING NINE EACH 8-4HL, EIGHT EACH 6-4HL, SEVEN EACH 6-3HL FASTEN ERS. (M) 2 L 7 3 4F A3WE 1998121800758 19981218 00758 NM 1998 12 18 AALA981771 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND BELL FRAME AT BS 950F GOUGED BETWEEN STRINGER 25L AND 26L. INSTALLED .071 INCH 7075T-6 DOUBLER, 22 EACH 6-3 HL, 22 EACH 6-4HL, 23 EACH 8-4HL FASTENERS PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1998121800759 19981218 00759 NM 1998 12 18 AALA981770 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FRAME DENTED LEFT SIDE STATION 950L AT STRINGER 25 AND 26L. CUT OUT DAMAGED SECTION AND INSTALLED FRAME REPAIR PE R 51-40-3. (M) 2 L 7 3 4F A3WE 1998121800760 19981218 00760 1998 12 18 VJ9800648 2 19981213 A 7314 378200 FUEL PUMP DOUG DC9 DC932 3022066 WP NR 1 ENGINE MALFUNCTIONED A ZZDA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 15 924VV 47278 AIR RETURN AFTER V1 ON THE TAKEOFF ROLL, NR 1 ENGINE THRUST DROPPED TO 1.44 EPR 79 PERCENT N1, 420 EGT 86.5 N1, 4400 FUE L FLOW STAYED THERE REGARDLESS OF THROTTLE POSITION. REMOVED AND REPLACED FUEL PUMP IAW 73-10-1, OPS CHECKED GOOD ON EN GINE RUN. 2 L 7 2 4F A6WE 1998121800761 19981218 00761 WP 1998 12 18 CKSA98745 1 19981211 A 2170 COALESCER BAGS LKHEED 1011 1011385115 5265015 WP 1, 2 & 3 PACKS DIRTY A CKSA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 102CK 193N1198 THE CREW NOTICED DE-ICING FLUID SMELL FROM COCKPIT AIR VENTS AND DUCTS. REMOVED AND CLEANED ALL COALESCER BAGS ON NR 1, 2, 3 PACKS IAW MM 21-51-22. OPS AND LEAK CHECK GOOD. 2 L 7 3 4F A23WE 1998121800762 19981218 00762 NM 1998 12 18 CKSA98746 1 19981205 A 7500 BLEED AIR BOEING 747 7472B4B 138481B NM PWA JT9 JT9D7J 52054 NE NR 3 ENGINE ODOR A CKSA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 23 710CK 21097 689567 CREW REPORTED, NR 3 ENGINE BLEED ALLOWS SMOKE IN THE COCKPIT. CLOSING BLEED, OIL SMOKE REMOVED. PERFORMED BLEED CHECK ON NR 3 ENGINE, GROUND RUN ENGINE IAW MM 71-00-00. NO DEFECT NOTED. 2 L 7 4 4F 4 F RT A20WE E20EA 1998121800763 19981218 00763 NM 1998 12 18 K3HA980149 1 19981209 A 3350 S106 BATTERY BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8881Z 21578 FORWARD CENTER MARKER LIGHT ASSEMBLY INOP. REPLACED NICAD BATTERIES, OPS CHECK GOOD PER MM 33-50-01. 2 L 7 3 4F A3WE 1998121800764 19981218 00764 WP 1998 12 18 9810859872 1 19981211 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 781NC 48121 DURING LINE CHECK, FOUND CEILING EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. MAINTENANCE REPLACED BATTERIES, O PERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998121800765 19981218 00765 WP 1998 12 18 9810869101 1 19981213 A 3350 BATTERY DOUG DC9 DC915 3022036 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 91S 47063 DURING LINE CHECK, FOUND OVERHEAD EMERGENCY LIGHTS IN FIRST CLASS SECTION INOPERATIVE. MAINTENANCE REPLACED BATTERIES I N POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998121800766 19981218 00766 SO 1998 12 18 COMA9810283 1 19981214 A 5720 12001647023 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 RIGHT WING SKIN SUPPORT NR 30 AT RIB 6 CRACKED. REPLACED SKIN SUPPORT. 2 L 7 2 4T RT A31SO 1998121800767 19981218 00767 SO 1998 12 18 COMA9810284 1 19981214 A 5720 12017055021 SUPPORT EMB 120 EMB120RT SO RT WING CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 168CA 120168 RIGHT WING SKIN SUPPORT NR 37 AT RIB NR 9 CRACKED. REPLACED SKIN SUPPORT. 2 L 7 2 4T RT A31SO 1998121800768 19981218 00768 NM 1998 12 18 98FDEA00743 1 19981214 A 5320 6556118 SHEAR TIE BOEING 727 727247 138408F NM BS 720 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 581 CORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 720F, LBL 9, WL 149. *S/D* REMOVED AND REPLACED SHEAR TI E BS 720F, LBL 9, WL 149 IAW FEDEX SRM 53-10-4 FIG 15. 2 L 7 3 4F A3WE 1998121800769 19981218 00769 EU 1998 12 18 98FDEA00744 1 19981215 A 5210 SWITCH AIRBUS 300 A300F4605R 3930327 EU R1 DOOR OUT OF ADJUST A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 654FE 738 R1 DOOR WARN LIGHT AT 18,000 FT WITH NO PRESSURE LOSS. RETURN TO ATL. *S/D* ADJUSTED R1 DOOR SWITCH 8WS PER MM 52-71- 11. 2 L 7 2 4F RT A35EU 1998121800770 19981218 00770 NM 1998 12 18 98FDEA00745 1 19981215 A 5730 651855210 SKIN BOEING 727 727247 138408F NM BS 760 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 NR 0167 - CORROSION (C53-224-05) WING CTR SECTION UPPER SKIN, UPPER SURFACE BS 760, RBL 65, WL 204. REMOVED AND REPLACE D CORROSION AT BS 758, RBL 62.64, WL 204 UP TO .039 OF MATERIAL IN A 1 BY 1 AREA. UPPER SKIN WAS FOUND TO BE OUT OF LIM ITS PER FEDEX SRM 57-30-1. REPAIR SKIN PER FEDEX EA 7-5330-43175A. 2 L 7 3 4F A3WE 1998121800771 19981218 00771 WP 1998 12 18 MWEA981151 1 19981210 A 5311 991224618 FRAME DOUG DC9 DC914 3022034 WP BS 859 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 500ME 45711 FOUR CRACKS ON RT FRAME WEB IN AFT ACCESSORY COMPARTMENT STATION 859. REPAIRED IAW BOEING TELEX MWX ORD 98 0005 SPLICED IN NEW WEB SECTION. 2 L 7 2 4F A6WE 1998121800772 19981218 00772 WP 1998 12 18 MWEA981152 1 19981213 A 2560 5917689103 COVER DOUG DC9 DC915 3022036 WP GALLEY DR SLID LOOSE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 GALLEY SERVICE DOOR EVACUATION SLIDE COVER LOOSE. RESECURED GALLEY DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998121800773 19981218 00773 SO 1998 12 18 SWIA971326 1 19981130 A 3010 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT PRESS REG FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 576SW 120345 SIX SECONDS AFTER TURNING ON THE DEICE BOOTS THE LEFT AND RIGHT MIDDLE LEADING EDGE BOOTS FAILED. THE RIGHT OUTBOARD LE ADING EDGE AND VERTICAL FIN AND LEFT INTAKE BOOTS ALL FAILED IN FLIGHT. RETURNED TO SEA. REMOVED AND REPLACED RIGHT PR ESSURE REGULATOR VALVE IAW MM 30-10-06, OPS CKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121800774 19981218 00774 SO 1998 12 18 SWIA971327 1 19981130 A 3010 EJECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE VERT FIN DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 290SW 120317 VERTICAL FIN DEICE LIGHT CAME ON WITH BOTH TIMERS. RETURNED TO SBA. CLEANED EJECTOR FOR VERTICAL FIN. PERFORMED OPS C HECKS OF WING DEICE SYSTEM, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121800775 19981218 00775 SO 1998 12 18 SWIA971328 1 19981202 A 2612 CLAMP EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE LOOSE A SWIA O OTHER N FALSE WARNING CR CRUISE 1 NM 07 1117H 120117 LEFT FIRE DETECTION ENGINE/WHEEL WELL LIGHT CAME ON IN FLIGHT INTERMITTENTLY. STAYED ON FOR A MINUTE OR TWO, THEN INTER MITTENT AGAIN. VISUALLY INSPECTED LEFT WHEEL WELL FIRE LOOP. FOUND ONE CLAMP TO BE LOOSE. SECURED CLAMP, OPS TESTED G OOD PER MM 26. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121800777 19981218 00777 1998 12 18 SWIA971330 4 19981203 A 3420 WARNING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT & RT GYRO ACTIVATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 199SW 120237 BOTH SIDES GYROFLAGS INTERMITTENTLY ON AND OFF, COMMAND BARS MOVED ABNORMALLY UP AND DOWN AND SIDE TO SIDE. RETURNED TO FIELD. AIRCRAFT WAS FLOWN FOR 34 MINUTES WITH NO DISCREPANCIES REPORTED. ALL SYSTEMS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121800778 19981218 00778 SO 1998 12 18 SWIA971331 1 19981204 A 3010 SWITCH EMB 120 EMB120RT SO PWA 118 PW118A NE RT HORIZ STAB FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 284YV 120284 RIGHT OUTBOARD STABILIZERS FAIL ON BOTH TIMERS. RETURNED TO FAT. REPLACED RIGHT OUTBOARD STABILIZER PRESSURE SWITCH, O PS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121800779 19981218 00779 SO 1998 12 18 SWIA971332 1 19981207 A 6120 PCU EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT PROP LEAKING A SWIA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 NM 07 212SW 120276 LEFT OIL PRESSURE DROPPED BETWEEN 52 AND 45 PSI IN FLIGHT. RETURNED TO SLC. FOUND THE PCU TO BE LEAKING OIL. REMOVED AND REPLACED PCU. RAN THE LEFT ENG IAW MM 71-00-00 AND 61-00-00. OPS AND LEAK CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121800780 19981218 00780 1998 12 18 SWIA971333 4 19981207 A 3425 AHRS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 205SW 120260 NR 2 AHRS FAILED IN FLIGHT. RETURNED TO SFO. INSTALLED SERVICEABLE AHRS NR 2, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998121800781 19981218 00781 NM 1998 12 18 SWAA983105 1 19981211 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 949 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED C3 CHECK, FOUND AFT LOWER LOBE BS 949 AT S27 HEAVILY CORRODED. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800782 19981218 00782 NM 1998 12 18 SWAA983106 1 19981211 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 972 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED C3 CHECK, FOUND AFT LOWER LOBE BS 972 AT S26R HEAVILY CORRODED NEAR I/B PRESSURE RELIEF VALVE. REPAIRE D PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800783 19981218 00783 NM 1998 12 18 SWAA983107 1 19981211 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 308 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 92SW 22964 DURING SCHEDULED SPECIAL VISIT CHECK, FOUND LARGE DENT AT BS 308 RIGHT SIDE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800784 19981218 00784 NM 1998 12 18 SWAA983108 1 19981212 A 2131 7110025 CONTROLLER BOEING 737 7373H4 1384600 NM CONTROL CABIN MALFUNCTIONED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 359SW 26596 AFTER T/O AT APPROX 1500 FT SMOKE STARTED COMING FROM PRESSURE CONTROLLER. CREW SWITCHED TO STBY AND IMMEDIATELY RETURN ED FOR LANDING AT DAL DOWNWIND. LANDING WEIGHT WAS 109000 APPROX WITH NORMAL BRAKING. SMOKE STOPPED SOMETIME AFTER SWI TCHING TO STBY. INSPECTED PRESSURE CONTROL PANEL WIRING AND CONNECTOR, NO DEFECTS NOTED. REMOVED AND REPLACED PRESSURE CONTROL PANEL PER M/M. PRESSURIZED ACFT ON GROUND, NO ABNORMALTIES NOTED. OP CKS GOOD. 2 L 7 2 4F RT A16WE 1998121800785 19981218 00785 NM 1998 12 18 SWAA983109 1 19981211 A 3350 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 662SW 23255 DURING PREFLIGHT CHECK, FOUND AFT UPPER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121800786 19981218 00786 NM 1998 12 18 SWAA983110 1 19981213 A 3350 2330127 LIGHT BOEING 737 7372H4 138448C NM PAX DOOR INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 082SW 22731 DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT FWD ENTRY DOOR. REMOVED AND REPLACED LIGHT ASSEM BLY PER BOEING M/M. 2 L 7 2 4F A16WE 1998121800787 19981218 00787 NE 1998 12 18 SWAA983111 2 19981213 A 7230 808931 COMPRESSOR BOEING 737 7372H4 138448C NM PWA JT8 JT8D15 52051 NE NR 1 ENGINE BIRD STRIKE A SWAA A UNSCHED LANDING C B F.O.D. SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 71SW 22358 INJESTED BIRD INTO NR 1 ENGINE ON TAKEOFF. ENGINE OPERATED OK, CABIN FILLED WITH BIRD SMELL AND SMOKE. AIRCRAFT RETURN ED TO OAK. NR 1 ENG FAN SECTION REQUIRES REPLACEMENT AND BORESCOPE REQUIRED. FAN SECTION REPLACEMENT AND BORESCOPE COM PLIED WITH PER BOEING REF AIRWORTHNESS APPROVAL TAG FORM 8130-3,W/O NUMBER VH0506 (SUPPLIED BY GE) (P/N 808931) (S/N BB DVAV1329) OFF, (S/N BBUAU05740) ON. 2 L 7 2 4F 4 F A16WE E2EA 1998121800788 19981218 00788 NM 1998 12 18 SWAA983112 1 19981211 A 5314 KEELBEAM BOEING 737 7372H4 138448C NM BS 727 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND KEEL BEAM CORRODED AT BS 727+16.5 AT S17R. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800789 19981218 00789 NM 1998 12 18 SWAA983113 1 19981211 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND RT TEE SPLICE CRACKED AT KEEL BEAM BS 727. REPLACED PER BOEING SRM. 2 L 7 2 4F A16WE 1998121800790 19981218 00790 NM 1998 12 18 SWAA983114 1 19981213 A 5315 FLOORBEAM BOEING 737 7373A4 1384585 NM BS 312 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FLOORBEAM CORROSION AT BS 312, RBL 36. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998121800791 19981218 00791 NM 1998 12 18 SWAA983115 1 19981213 A 3350 BULB BOEING 737 7373H4 1384600 NM ROW 7ABC FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 346SW 24153 DURING SCHEDULED SC CHECK, FOUND EMERGENCY EXIT LIGHT AT ROW 7ABC INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998121800800 19981218 00800 EA 1998 12 18 98ZZZX4654 2 19980925 A 7414 M3333 IMPULSE COUPLING SLICK 6351 PIPER PA32 PA32300 7103212 SO LYC O540 IO540K1G5 41532 EA MAGNETO WORN A LABA K NONE O OTHER IN INSP/MAINT 1 AL 05 29143 290 98011557 327940187 RL1583748A PART REMOVED UNDER A COMPANY INSPECTION PROGRAM OF 300 HOURS/INSPECTION REQUIREMENT. INSPECTION SHOWS POSSIBLE UNEVEN W EAR IN PAWLS AT PINS, BUT NEITHER PAWL WAS AT THIS TIME BEYOND LIMITS. PART RETURNED FOR FURTHER ANALYSIS AND NEW UNIT INSTALLED ON MAGNETO. 1 L 7 1 3O 3 O A3SO 1E4 1998121800830 19981218 00830 CE 1998 12 18 98ZZZX4684 1 19981124 A 2730 115610010325 TORQUE TUBE BEECH 99 B99 1154004 CE ELEVATOR CRACKED A S TIMA K NONE O OTHER IN INSP/MAINT 1 NM 07 99CA U127 TORQUE TUBE ASSEMBLY SUPPORT WAS CRACKED AT THE POINT WHERE SCREWS FASTEN SUPPORT TO ELEVATOR. DEFECT WAS FOUND DURING TORQUE TUBE INSPECTION. 1 L 7 2 3T A14CE 1998121800837 19981218 00837 1998 12 18 98ZZZX4691 4 19981123 A 3422 GYRO BEECH 100 100BEECH 1152916 CE COCKPIT FAILED A DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 5727 4094469 B48 PILOT'S DIRECTIONAL GYRO FAILED. REMOVED AND REPLACED WITH OVERHAULED UNIT, S/N 3098862. 1 L 7 2 3T A14CE 1998121800842 19981218 00842 NE 1998 12 18 TWAA9819801 2 19981214 A 7321 7436024 FUEL CONTROL DOUG DC9 DC934 302207E WP PWA JT8 JT8D15 52051 NE NR 1 ENGINE MALFUNCTIONED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER CR CRUISE 1 CE 05 928L 48124 1608 THE LEFT ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. THE LT ENGINE WAS SHUT DOWN AND FLIGHT RETURNED TO STL. REPLAC ED THE JFC, (P/N 743602-4), AND ENGINE FUEL PUMP, (P/N 378200). CHECK-C 3-22-98 STL. 2 L 7 2 4F 4 F RT A6WE E2EA 1998121800843 19981218 00843 NM 1998 12 18 TWAA9819803 1 19981215 A 3350 251005 FUSE BOEING 767 767231 1385131 NM RT OVERWING EXIT BLOWN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 609TW 22572 FOUND RT SIDE EMERGENCY EXIT WING LIGHT INOPERATIVE. REPLACED FUSE. CHECK-C 11-26-98 LAX. 2 L 7 2 4F RT A1NM 1998121800844 19981218 00844 NM 1998 12 18 TWAA9819804 1 19981207 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND CORROSION ON STR 39R AT STA 434. CUT SECTION OF STRINGER AND REMOVED CORROSION PER SRM 51-10-00, PAGE 15. INSTALLED STR AND CLIP PER SRM 53-00-03, PAGE 209. 2 L 7 2 4F RT A1NM 1998121800845 19981218 00845 NM 1998 12 18 TWAA9819805 1 19981207 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 37L AT STA 434, FWD CARGO COMPT. REMOVED CORROSION PER SRM 51-10- 00, PAGE 16. REPLACED SECTION OF STRINGER AND INSTALLED RIVETS AND HI-LOKS PER SRM 51-10-00 PAGE 21. 2 L 7 2 4F RT A1NM 1998121800846 19981218 00846 NM 1998 12 18 TWAA9819806 1 19981207 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND CORROSION ON STR 39L AT STA 434. REMOVED CORROSION PER SRM 51-10-00, PAGE 16. INSTALLE D NEW STR SECTION PER SRM 53-00-03, FIG 202 PAGE 215. 2 L 7 2 4F RT A1NM 1998121800847 19981218 00847 NM 1998 12 18 TWAA9819807 1 19981207 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 628 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND STRINGER 39R CORRODED AT STA 628. REPAIRED S39R PER SRM 53-00-03 FIG 202. 2 L 7 2 4F RT A1NM 1998121800848 19981218 00848 NM 1998 12 18 TWAA9819808 1 19981207 A 5754 RIB BOEING 767 767231 1385131 NM LT LE SLAT CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND A 4 INCH CRACK IN LT WING L/E BULLNOSE RIB, I/B END OF NR 4 SLAT ACTUATOR, LT WING STA 5 65. INSTALLED NEW RIB (P/N 114T2512-7). INSTALLED WITH RIVETS AND HI-LOKS. 2 L 7 2 4F RT A1NM 1998121800849 19981218 00849 NM 1998 12 18 TWAA9819809 1 19981202 A 5753 SKIN BOEING 767 767231 1385131 NM RT TE FLAP DELAMINATED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND RT WING LOWER SIDE APPROX 40 INCHES I/B OF O/B END, HAS 8 INCH BY 3 INCH DELAMINATION ON RT FLAP, O/B END. REMOVED OLD EXISTING REPAIR AND REPLACED WITH PRE-PREG FIBERGLASS PER SRM 57-53-01, TABLE I, FIG 201 (SHEET 5), SRM 51-70-05, PARA 4C & 3C THRU 3J OF FIG 2 (SHEET 1). 2 L 7 2 4F RT A1NM 1998121800850 19981218 00850 NM 1998 12 18 TWAA9819810 1 19981207 A 5313 STRINGER BOEING 767 767231 1385131 NM BS 434 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 606TW 22569 DURING OP 15 MAINT CHECK, FOUND CORROSION ON STRINGER 37R AT STA 434. REMOVED CORROSION PER TWA STANDARD PROCEDURES MAN UAL 6-80-01. INSTALLED NEW STRINGER SECTION PER SRM 53-00-03, FIG 202 PAGE 15. 2 L 7 2 4F RT A1NM 1998121800851 19981218 00851 EU 1998 12 18 AWXA9800231 1 19981208 A 5320 SUPPORT AIRBUS 320 A320232 3930326 EU CABIN FLOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 CABIN FLOOR SUPPORT RAIL Y81 RT CORRODED. REPAIRED AS PER SRM 53-00-14 PG 233, FABRICATED ANGLES AS PER SRM 53-00-14. 2 L 7 2 4F RT A28NM 1998121800852 19981218 00852 EU 1998 12 18 AWXA9800232 1 19981208 A 5320 SUPPORT AIRBUS 320 A320232 3930326 EU CABIN FLOOR CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 CABIN FLOOR SUPPORT RAIL Y5032 LT CORRODED. REMOVED CORROSION AS PER SRM 57-11-14 FIG 101 AND 102. REPAIRED AS PER SRM 53-00-14 FIG 206. 2 L 7 2 4F RT A28NM 1998121800853 19981218 00853 EU 1998 12 18 AWXA9800233 1 19981208 A 5320 CLIP AIRBUS 320 A320232 3930326 EU CABIN CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 641AW 453 AFT CABIN HORIZONTAL WEB SUPPORT CLIP CORRODED. FABRICATED CLIP AS PER DWG NR D53480820-392, MATERIAL 2024-D-.080, PO S PEC 1012005697. 2 L 7 2 4F RT A28NM 1998121800854 19981218 00854 EU 1998 12 18 AWXA9800234 1 19981213 A 3610 342A010100 THERMOSTAT AIRBUS 320 A320231 3930325 EU LEFT MALFUNCTIONED A AWXA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 28 637AW 1713 1713 099 BLEED 1 AND BLEED 2 FAULT. DPI ISSUED MEL 36-11-01. T/S FOUND TEMP THERMOSTAT CONTROL FAULTED. REMOVED AND REPLACED P ER AMM CHAP 36-11. SYS OPS OK, NO FAULTS NOTED. ALSO, REMOVED AND REPLACED BMC NR 2 AS PREC PER MC AMM CHAP 36. 2 L 7 2 4F RT A28NM 1998121800855 19981218 00855 1998 12 18 AWXA9800235 4 19981214 A 2210 FMGC AIRBUS 320 A320231 3930325 EU LEFT MALFUNCTIONED A AWXA O OTHER J WARNING INDICATION DE DESCENT 1 WP 28 634AW 091 AT BEGINNING OF DESCENT, BOTH FMGC FAILED, A/P, A/T, ND'S TRIPPED OFF. USED BACK-UP NAV CYCLED FMGC, MCDU, FCU CB'S AND RECOVERED TEMPORARILY. LT FMGC FAILED AGAIN 2-3 TIMES. RT FMGC SEEMED TO OPERATE NORMAL. ALL ADIRU'S REALIGNED AND F MGC NR 1 AND NR 2 RESET. AFS TEST OK, NO LAST LEG RECORD OF AFS, ADIRU OR CPC FAULTS. NO PAST HISTORY (30 DAYS), CPC 1 AND 2 BITE CHK OK. UNABLE TO FAULT NAV OR AFS SYSTEMS AT THIS TIME. CLEARED FOR FURTHER FLIGHT. 2 L 7 2 4F RT A28NM 1998121800856 19981218 00856 NM 1998 12 18 RAAA98B2048 1 19981208 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM RT OVERWING DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998121800857 19981218 00857 NM 1998 12 18 RAAA98B2049 1 19981208 A 3350 8621006 BATTERY PACK INTVLV 873100112 BOEING 727 72722C 138400F NM ROW 12 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 PAX ROW 12 FLOOR PROXIMITY EGRESS LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1998121800858 19981218 00858 NM 1998 12 18 RAAA98B2050 1 19981211 A 3350 873100212 LIGHT BOEING 727 72722C 138400F NM RT OVERWING INOP A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 3 4F A3WE 1998121800859 19981218 00859 NM 1998 12 18 UPS98528291 1 19981215 A 3150 6226540111 EICAS BOEING 757 75724APF 1384969 NM PW2040 LEFT FAILED A IPXA O OTHER N FALSE WARNING CR CRUISE 1 SO 01 431UP 25462 INSPECTION TYPE-N/A DURING CRUISE, NUMEROUS WARNING, CAUTION AND STATUS MESSAGES APPEARED. INCLUDED WERE APU FIRE, ENGI NE FIRE AND CARGO FIRE. THE MASTER CAUTION LIGHT ILLUMINATED, BUT NO FIRE WARNING BELLS. REPLACED LEFT EICAS COMPUTER AND TESTED PER MM 31-41-02 AND 31-41-00. 2 L 7 2 4F RT A2NM 1998121800860 19981218 00860 EU 1998 12 18 QXEA9801789 1 19981213 A 3350 2302 SIGN GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 EMERGENCY EXIT SIGN AT ROW 8 INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN ASSEMBLY, OPERATIONAL TEST IS NORMAL. 2 L 7 2 4F RT A20EU 1998121800861 19981218 00861 NM 1998 12 18 98FDEA00746 1 19981215 A 7603 CONTROL MODULE DOUG MD11 MD11F 3023600 NM COCKPIT FAILED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 25 590FE 48505 BLACK SMOKE RISING FROM THROTTLES, ACRID ELECT BURN SMELL. DECLARED EMERGENCY LANDING. REMOVED AND REPLACED THRUST CON TROL MODULE PER MM 75-11-10-4, SYS OPER CHECK NORMAL PER MM 75-11-10-700-801. 2 L 7 3 4F RT A22WE 1998121800862 19981218 00862 NM 1998 12 18 98FDEA00747 1 19981216 A 5320 66157221 CLIP BOEING 727 727247 138408F NM BS 440 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-224-03-1/2) ON STRINGER CLIP STR 26L, BS 440 (MARKED). *S/D* REMOVED AND REPLACED WITH NEW CLIP TO FRAM E, NEW STR CLIP WAS INSTALLED IAW FEDEX SRM 51-10-1, 51-30-2 AND FEDEX MM 51-20-0. 2 L 7 3 4F A3WE 1998121800863 19981218 00863 NM 1998 12 18 98FDEA00748 1 19981215 A 5320 BEAM BOEING 727 727247 138408F NM BS 268 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 WHILE WORKING FEDEX EO NR 7-5300-7-2305 L3 PT 2 CORROSION ON G-BEAM BS 268, LBL 3, WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM BS 26.75, LBL 8 TO RBL 18, WL 208 IAW FEDEX DWG 65-17593 AND FEDEX SRM 51-30-2, 53-10-1. 2 L 7 3 4F A3WE 1998121800864 19981218 00864 EU 1998 12 18 98UAL900538 1 19981105 A 2910 HYD SYST AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD STST REQUIRED SERVICE A UALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS J WARNING INDICATION IN INSP/MAINT 1 WP 29 408UA 457 GREEN HYDRAULIC SYSTEM QUANTITY INDICATION LOW. SHUT DOWN ENGINE 1 GREEN PUMP AND PTU. DIVERTED TO ORD. *S/D* CYCLED GEAR, FLAPS AND SPOILERS SEVERAL TIMES. ALSO, MOTORED ENGINE. NO LEAKS FOUND, SUSPECT AIR IN SYSTEM. 2 L 7 2 4F 4 F RT A28NM E40NE 1998121800865 19981218 00865 NM 1998 12 18 98UAL900582 1 19981202 A 2844 SWITCH BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE MAIN FUEL TANK MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 347UA 24251 LOSS OF FUEL PRESSURE. *S/D* CHECKED EACH BOOST PUMP CHECK VALVE AND ORIFICE FOR DEBRIS. CHECKED ENGINE FILTERS FOR D EBRIS, NONE FOUND. FUEL SAMPLES CHECKED OK. REPLACED LOW PRESSURE WARNING SWITCHES FOR BOTH MAIN FUEL TANKS. BLED SEN SE LINES. PRESSURE TESTED FUEL SYSTEM IN ACCORDANCE WITH SERVICE BULLETIN 737-28A1114. 2 L 7 2 4F 4 F RT A16WE E2GL 1998121800866 19981218 00866 NM 1998 12 18 98UAL900584 1 19981204 A 3397 58791 WIRE BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE BS 868 FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 903UA 25003 FLOOR EEL INOP. REPLACED STRIP AND OPS CHECKED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998121800867 19981218 00867 NM 1998 12 18 98UAL900585 1 19981204 A 3350 POWER STRIP BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE ROW 9-16 FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 545UA 25323 EEL LIGHTING FROM ROW 9 TO ROW 16 INOP. REPLACED EEL FEEDER POWER STRIP FROM ROW 9 TO ROW 16. 2 L 7 2 4F 4 F RT A2NM E17NE 1998121800868 19981218 00868 NE 1998 12 18 98UAL900587 2 19981206 A 7261 793651 OIL LINE BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE NR 2 ENGINE CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 990UA 5503 21980 688470 NUMBER TWO ENGINE HAD LOW OIL PRESSURE. *S/D* THE NR 6 BEARING OUTER INTERNAL OIL PRESSURE LINE HAD CRACKED AT THE BRA ZE JOINT NEAR THE 'B' NUT CONNECTION, CAUSING THE OIL LOSS. THE LINE WAS REPLACED AND THE ENGINE WAS BASE CHECKED, RUN IN THE TEST CELL, AND MADE SERVICEABLE. 2 L 7 2 4F 4 F A16WE E2EA 1998121800869 19981218 00869 NM 1998 12 18 98UAL900588 1 19981204 A 2910 MS2190216T UNION BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 1 EDP FACTURED A UALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 563UA 26665 LANDED SFO UNDER AMBER ALERT DUE TO LOSS OF LEFT HYDRAULIC SYSTEM. *S/D* FOUND PRESSURE LINE UNION FITTING ON NR 1 EDP PRESSURE AND CASE DRAIN FILTER ASSY BROKEN. REPLACED UNION AND FILTERS, CHECKED ACMP AND EDPM FILTER FOR CONTAMINATION AND NONE WAS FOUND. ALSO, SYS CASE DRAIN FILTER CHECKED AND NO CONTAMINATION FOUND. 2 L 7 2 4F 4 F RT A2NM E17NE 1998121800871 19981218 00871 NM 1998 12 18 98UAL900590 1 19981207 A 7830 3HT84 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 TR UNIT INTERMITTENT A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7251U 21398 700046 NR 2 REVERSER NOT STOWED LIGHT CAME ON AT 100 KNOTS ON TAKEOFF. ABORTED TAKEOFF. *S/D* SUBSEQUENT TROUBLESHOOTING OR TH E REVERSER OPERATION REVEALED WHAT APPEARED TO BE A BAD SWITCH ASSEMBLY. THE SWITCH WAS REPLACED AND THE FAILED UNIT BR OUGHT INTO THE SHOP FOR FURTHER ANALYSIS. TESTING REVEALED PROPER SWITCH OPERATION, SO EITHER THE SWITCH FAILURE WAS IN TERMITTENT OR IT MOVED OUT OF ADJUSTMENT. SUBSEQUENTLY THE REVERSER WAS REMOVED AND IS UNDER INVESTIGATION IN THE SHOP. 2 L 7 3 4F 4 F A3WE E2EA 1998121800872 19981218 00872 NE 1998 12 18 98UAL900591 2 19981203 A 7260 793651 6 OIL PRES TUBE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 6 BEARING CRACKED A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 7443U 7985 21897 700080 NR 1 ENGINE OIL QUANTITY INDICATOR BEGAN TO SHOW GRADUAL LOSS OF OIL EN ROUTE. ELECTED TO LAND AT SYR. *S/D* THE LOSS O F OIL WAS DUE TO A CRACK IN THE NR 6 BEARING OUTER INTERNAL OIL PRESSURE LINE AT THE BRAZE JOINT NEAR THE FIXED FERRULE. THE LINE WAS REPLACED. FURTHER INSPECTION REVEALED WEAR BETWEEN THE LINE WEAR BAND AND THE SPACER (GUIDE) THAT PROVID ES SUPPORT. THIS WEAR ALLOWS LATERAL TUBE MOVEMENT. IT COULD NOT BE DETERMINED IF THIS OR FATIGUE CAUSED THE CRACK. T HE 72-54-22 MANUAL IS BEING REVISED TO SPECIFICALLY INSPECT FOR THIS WEAR. 2 L 7 3 4F 4 F A3WE E2EA 1998121800873 19981218 00873 WP 1998 12 18 98UAL900592 1 19981208 A 3231 RETRACT MECH DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL NLG DOORS MALFUNCTIONED A UALA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION NR NOT REPORTED 1 WP 29 1847U 48263 TERRIFIC VIBRATION IN NOSE AREA AFTER GEAR RETRACTION. RETURNED TO SEA. *S/D* NOSE LANDING GEAR FORWARD DOORS WERE FO UND OPEN UPON ARRIVAL. ALL HINGE POINTS AND LINKS WERE CHECKED. NO DEFECT WAS FOUND. MANUALLY CLOSED AND LOCKED DOORS . NO FURTHER REPORTS. 2 L 7 3 4F 4 F A22WE E23EA 1998121800874 19981218 00874 NM 1998 12 18 98UAL900593 1 19981205 A 5754 654622296 SLAT BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 1 LE FLAP DAMAGED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7264U 21411 LEADING EDGE SLAT NR 6 DID NOT RETRACT. VERIFIED FULL DOWN BY VISUAL CHECK. POSSIBLE BIRD STRIKE ON DEPARTURE FROM SMF. DIVERTED TO SFO. *S/D* SLAT DAMAGED BY BIRD STRIKE. REPLACED NR 6 SLAT, SYSTEM OPERATIONALLY CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1998121800875 19981218 00875 NM 1998 12 18 98UAL900595 1 19981016 A 5310 STRUCTURE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE BS 390-470 DAMAGED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 7293U 21571 RIGHT FUSELAGE DAMAGED BY TOW TRACTOR. DAMAGE BETWEEN BS 390 TO 470 FROM STRINGERS 23R TO 27R, WHICH WERE SEVERED. FRA MES AT STA 400, 420, 440 AND 460 WERE CRUSHED. THREE ADJACENT SKIN PANELS DAMAGED. SPLICE PLATE AT BS 440 AND BEAR ST RAP FOR E & E DOOR DAMAGED. ALSO, KEEL BEAM WEB AT E & E DOOR OPENING DAMAGED. SPLICED NEW SECTIONS INTO STRINGERS 23 R TO 27R PER 727 SRM 53-10-3. SPLICED NEW SECTIONS INTO FRAMES PER SRM 53-10-4. SKIN TRIMMED AND RECEIVED EXTERNAL DOU BLERS PER 727 SRM 53-30-3. SPLICE PLATE REPAIRED PER UAL EVA MOC1-7772. THE BEAR STRIP REPAIRED PER UAL EVA MOC1 7771. KEEL BEAM WEB REPAIRED PER 727 SRM 51-40-2. 2 L 7 3 4F 4 F A3WE E2EA 1998121800876 19981218 00876 NM 1998 12 18 98UAL900596 1 19981209 A 2120 AIR DIST BOEING 737 737291 138448W NM PWA JT8 JT8D17 52049 NE CABIN ODOR A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 WP 29 984UA 21642 OIL SMELL COMING FROM BOTH PACKS. CHECKED BOTH LEFT AND RIGHT PACK COALESCER BAGS, WATER SEPARATOR, AND PACK DUCTS FOR OIL RESIDUE OR CONTAMINATION. OPERATIONALLY CHECKED AND FOUND NO ODORS OR SIGNS OF OIL/FLUID RESIDUE. 2 L 7 2 4F 4 F A16WE E2EA 1998121800877 19981218 00877 NM 1998 12 18 98UAL900597 1 19981210 A 2910 271N61192 HOSE BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT MLG FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 574UA 26686 LANDED LAX UNDER AMBER ALERT DUE TO THE LOSS OF THE LEFT HYDRAULIC SYSTEM. *S/D* FOUND MLG DOWNLOCK PRESSURE HOSE RUPT URED. REPLACED HOSE. 2 L 7 2 4F 4 F RT A2NM E17NE 1998121800878 19981218 00878 WP 1998 12 18 ABXA9801183 1 19981214 A 3350 60030431 BATTERY PACK DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 964AX 47781 DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1998121800879 19981218 00879 WP 1998 12 18 MWEA981153 1 19981213 A 5330 SKIN DOUG DC9 DC915 3022036 WP PAX DOORWAY CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 900ME 45841 A .5 INCH CRACK EMANATING FROM FORWARD ENTRY DOOR CUTOUT UPPER DOOR STOP SCREW HOLE. INSTALLED REPAIR IAW SRM 53-30-0 F IGURE TYPE 11 REFERENCE TELEX NUMBER M-7200-98-05166. 2 L 7 2 4F A6WE 1998121800880 19981218 00880 NM 1998 12 18 VNAA9812008 1 19981213 A 6120 D1192 PCU DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 425JS 66595 42479 3037 DURING THE TAXI FOR TAKEOFF, THE LEFT HAND ENGINE WAS REPORTED TO HAVE AN UNCOMMANDED INCREASE IN RPM. ALSO, THE ENGINE WAS OVER TORQUED AND WAS SHUT DOWN BY THE CREW. THE AIRCRAFT THEN RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REP LACED THE LEFT HAND PROPELLER CONTROL UNIT AND COMPLETED OVER TORQUE INSPECTIONS, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06, 05-56-02 AND 05-57-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998121800881 19981218 00881 NE 1998 12 18 VNAA9812007 2 19981210 A 7532 4067B000 BLEED VALVE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 424JS 50856 33848 3033 THE AIRCRAFT RETURNED TO THE GATE AFTER A LEFT HAND BLEED FAIL WARNING MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND LOW PRESSURE BLEED VALVE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 36-11-07. OPERATIONAL CHECKS WERE COM PLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998121800882 19981218 00882 WP 1998 12 18 CKSA98712 1 19981216 A 5320 STRAP LKHEED 1011 1011385115 5265015 WP BS 1393 CUT A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FS 1393 RBL 2 SKIN TEAR STRAP HAS LEVEL 1 CORROSION. TITANIUM TEAR STRAP CUT TO FACILITATE CORROSION REMOVAL. REPAIRED IAW L1011 SRM 53-31-00. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-210, NON ROUTINE CARD NR 30871, CPCP TASK NR C53-120-04-02. 2 L 7 3 4F A23WE 1998121800883 19981218 00883 WP 1998 12 18 CKSA98713 1 19981216 A 5311 FRAME LKHEED 1011 1011385115 5265015 WP BS 903 DAMAGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FS 903 AFT SIDE OF FRAME HORIZONTAL LEG DAMAGED BETWEEN STRINGER 27 AND 28. REPAIRED DAMAGE AND FABRICATED PART IAW L10 11 SRM 53-12-0 FIG 805. TREATED AND PRIMED IAW SRM 51-21-02. INSTALLED REPAIR IAW L1011 SRM 53-12-00 FIG 805. FOUND D URING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 10 6-187, NON ROUTINE CARD NR 35967, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800884 19981218 00884 WP 1998 12 18 CKSA98714 1 19981216 A 5347 SEAT TRACK LKHEED 1011 1011385115 5265015 WP BS 629 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND SEAT TRACK FLANGE CRACKED AT FUSELAGE STATION 629, LBL 94. REMOVED AND REPLACED SEAT TRACK IAW L1011 SRM 51-40-01 . FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK O RDER NR 106-206, NON ROUTINE CARD NR 32028, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800885 19981218 00885 WP 1998 12 18 CKSA98715 1 19981216 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 1645-1665 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 BETWEEN FS 1645 AND 1665 STRINGER 33R CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW L1011 SRM 51-21-01 & 5 3-13-00 FIG 801. FABRICATED REPAIR PIECES IAW SRM 53-13-00 FIG 804. INSTALLED IAW SRM 51-40-01. FOUND DURING SCHEDULE D C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROU TINE CARD NR 35986, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800886 19981218 00886 WP 1998 12 18 CKSA98716 1 19981216 A 5312 BULKHEAD PATCH LKHEED 1011 1011385115 5265015 WP AFT PRESS BLKHD CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND REPAIR PATCH CORRODED ON AFT PRESSURE BLKHD BETWEEN STRINGERS 35 AND 37 FS APPROX 1824. FOUND TO BE OUT OF LIMITS IAW SRM 51-21-01. REMOVED AND REPLACED REPAIR PATCH IAW L1011 SRM 53-11-00 FIG 805. FOUND DURING SCHEDULED C-CHECK AN D CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 32493, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800887 19981218 00887 WP 1998 12 18 CKSA98717 1 19981216 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 1790 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 AT FS 1790 BETWEEN STRINGERS 33 TO 34 AFT SIDE SHEAR TIE HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IA W L1011 SRM 51-21-01. FABRICATED REPAIR PARTS IAW SRM 53-12-00 FIG 806. INSTALLED IAW SRM 51-40-01. FOUND DURING SCHE DULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-211, NON ROUTINE CARD NR 35980, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800888 19981218 00888 WP 1998 12 18 CKSA98718 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 1445 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FLOORBEAM AT FS 1445, RBL 14 LOWER CHORD/CAP CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-23-00. FABRICATED REPAIR P ARTS IAW SRM 53-21-00. INSTALLED IAW SRM 53-21-00 FIG 802. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLIS HMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-198, NON ROUTINE CARD NR 35999, CPCP TASK NR C53-1 20-04-03. 2 L 7 3 4F A23WE 1998121800889 19981218 00889 WP 1998 12 18 CKSA98719 1 19981216 A 5320 WEB LKHEED 1011 1011385115 5265015 WP BS 1645-1665 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 BETWEEN FS 1645 AND 1665 WEB FOUND CORRODED BEYOND LIMITS. REMOVED CORRODED WEB IAW SRM 51-40-01. FABRICATED NEW WEB I AW L1011 SRM 51-10-01. INSTALLED WEB IAW L1011 SRM 51-40-01, EDR L106152 AND SKETCH AIA-E2530. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUT INE CARD NR 35985, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800890 19981218 00890 WP 1998 12 18 CKSA98720 1 19981216 A 5330 SKIN LKHEED 1011 1011385115 5265015 WP BS 1107 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 CORROSION FOUND ON SKIN PANEL AT FS 1107 BETWEEN STRINGERS 29 TO 30. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-00. TREAT ED PRIMED IAW SRM 51-21-02 AND MM 20-51-09. REPAIRED IAW SRM 51-50-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CA RD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 35891, AIA CP CP TASK NR 01-00-1009. 2 L 7 3 4F A23WE 1998121800891 19981218 00891 WP 1998 12 18 CKSA98721 1 19981216 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 1790 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND SHEAR TIE CORRODED IN C-3 PIT, FS 1790 BETWEEN STRINGERS 29 AND 30. OUT OF LIMITS IAW L1011 SRM 51-21-01 AND 53-1 2 FIG 801. REPLACED SHEAR TIE IAW SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AI A. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 34215, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800892 19981218 00892 WP 1998 12 18 CKSA98722 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 789 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-1 PIT FS 789, RBL 4, FOUND LOWER CAP OF FLOORBEAM TO BE CORRODED BEYOND LIMITS. FABRICATED REPAIR PARTS IAW L1011 SRM 53-21-00. TREATED, PRIMED AND INSTALLED IAW SRM 53-21-00 FIG 802. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CAR D ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-207, NON ROUTINE CARD NR 34246, CPCP TA SK NR C53-100-02-00. 2 L 7 3 4F A23WE 1998121800893 19981218 00893 WP 1998 12 18 CKSA98723 1 19981216 A 5320 SHEAR TIE LKHEED 1011 1011385115 5265015 WP BS 1485 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-2 PIT FS 1485 BETWEEN STRINGERS 35 TO 36 FOUND SHEAR TIE CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51- 21-01 AND 53-23-00. FABRICATED REPAIR PARTS IAW SRM 53-12-00 FIG 804. TREATED, PRIMED AND INSTALLED REPAIR IAW L1011 S RM 51-21-02. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 34243, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800894 19981218 00894 WP 1998 12 18 CKSA98724 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 923 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND IN C-1 PIT, FS 923 AT STRINGER 41, THE TOP OF FLOORBEAM, INSIDE THE PLASTIC SUPPORT BLOCK IS CORRODED. CORROSION OUT OF LIMITS IAW SRM 51-21-01 AND 53-23-00 FIG 801. FABRICATED REPAIR PARTS IAW SRM 53-23-00 FIG 802. TREATRED, PRIME D AND INSTALLED IAW SRM 53-23-00 FIG 802. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAI NTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 34234, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800895 19981218 00895 WP 1998 12 18 CKSA98725 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 901 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-1 PIT, ZONE 130, STA 901, BETWEEN RBL 10 AND 15, FOUND AN AREA OF CORROSION. REMOVED CORROSION IAW SRM 51-21-01, F OUND TO BE OUT OF LIMITS IAW 53-21-00. REMOVED FASTENERS AND FABRICATED REPAIR PART IAW L1011 SRM 51-40-01 AND 53-21-00 . INSTALLED REPAIR IAW SRM 51-40-01 AND MM 20-51-09. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-207, NON ROUTINE CARD NR 34253, CPCP TASK NR C53-100-02- 00. 2 L 7 3 4F A23WE 1998121800896 19981218 00896 WP 1998 12 18 CKSA98726 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 829 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-1 PIT, ZONE 130, FS 829, BETWEEN LBL 48 AND LBL 52, FOUND AN AREA OF CORROSION ON LOWER CAP OF MAIN DECK FLOORBEAM. REMOVED ALL EXISTING FASTENERS TO ACCOMODATE REPAIR ANGLE IAW L1011 SRM 51-40-01. CORROSION FOUND OUT OF LIMITS IAW S RM 53-21-00. FABRICATED REPAIR PARTS IAW SRM 53-21-00. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 53-21-00. FOUND D URING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 10 6-207, NON ROUTINE CARD NR 34249, CPCP TASK NR C53-100-02-00. 2 L 7 3 4F A23WE 1998121800897 19981218 00897 WP 1998 12 18 CKSA98727 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 709 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-1 PIT, ZONE 130, STA 709, RBL 48, FOUND AREA OF CORROSION. CORROSION OUT OF LIMITS IAW L1011 SRM 53-21-00. INSTAL LED REPAIR IAW SRM 53-21-00 AND 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAI NTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-207, NON ROUTINE CARD NR 34254, CPCP TASK NR C53-100-02-00. 2 L 7 3 4F A23WE 1998121800898 19981218 00898 WP 1998 12 18 CKSA98728 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 789 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-1 PIT, FS 789, LBL 48, FOUND CORROSION ON LOWER CAP OF FLOORBEAM. REMOVED CORROSION IAW SRM 51-21-00, FOUND OUT OF LIMITS IAW SRM 53-21-00. FABRICATED REPAIR PARTS IAW L1011 SRM 53-21-00 FIG 807. TREATED, PRIMED AND INSTALLED IAW SR M 53-21-00 FIG 804. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN O SCODA, MI. WORK ORDER NR 106-207, NON ROUTINE CARD NR 34247, CPCP TASK NR C53-100-02-00. 2 L 7 3 4F A23WE 1998121800899 19981218 00899 WP 1998 12 18 CKSA98729 1 19981216 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 1405 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-2 CARGO PIT FOUND AT STA 1405 TO 1425 STRINGER 34 HAD CORROSION. FOUND TO BE OUT OF LIMITS IAW L1011 SRM 51-21-01. FABRICATED NEW SUPPORT ANGLE IAW SRM 51-10-01. TREATED, PRIMED AND INSTALLED IAW SRM 51-21-01. FOUND DURING SCHEDULE D C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROU TINE CARD NR 34237, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800900 19981218 00900 WP 1998 12 18 CKSA98730 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 549 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-1 PIT, ZONE 130, STA 549 TO 669, RBL 55, FLOORBEAM FOUND CORRODED. CORROSION FOUND TO BE OUT OF LIMITS. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINT ENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-206, NON ROUTINE CARD NR 32418, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800901 19981218 00901 WP 1998 12 18 CKSA98731 1 19981216 A 5320 WEB LKHEED 1011 1011385115 5265015 WP BS 903 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND IN C-1 CARGO PIT, ZONE 130, STA 903, WEB BETWEEN STRINGER 27 AND 28 CORRODED. REMOVED AND FOUND TO BE OUT OF LIMI TS IAW SRM 53-12-00. FABRICATED REPAIR PARTS IAW SRM 53-12-00 FIG 805. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-12-00 FIG 805. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 32417, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800902 19981218 00902 WP 1998 12 18 CKSA98732 1 19981216 A 5312 BULKHEAD ANGLE LKHEED 1011 1011385115 5265015 WP BS 943 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-1 CARGO PIT, FS 943 BULKHEAD HAS FLOOR SUPPORT EXTRUSION CORRODED. REMOVED DISCREPANT EXTRUSION IAW L1011 SRM 51-4 0-01. INSTALLED REPAIR ANGLE IAW SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA . MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 32416, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800903 19981218 00903 WP 1998 12 18 CKSA98733 1 19981216 A 5320 WEB LKHEED 1011 1011385115 5265015 WP BS 1775 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-3 PIT, BETWEEN FS 1775 AND 1790 STRINGERS 29 AND 30 THE PLATE AND WEB FOUND TO BE CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW L1011 SRM 51-21-01. TREATED IAW SRM 51-20-02, PRIMED IAW SRM 51-09-01, INSTALLED REPAIR I AW SRM 53-31 FIG 805. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 32490, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800904 19981218 00904 WP 1998 12 18 CKSA98734 1 19981216 A 5312 BULKHEAD LKHEED 1011 1011385115 5265015 WP AFT PRESS BLKHD CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND AFT PRESSURE BULKHEAD CIRCUMFERENTIAL BETWEEN STRINGERS 33 AND 38 CORRODED. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 51-21-01. FABRICATED REPLACEMENT PARTS IAW SRM 51-10-01. TREATED AND PRIMED IAW SRM 51-21-02 AND MM 20 -51-09. INSTALLED REPAIR IAW SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. M AINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 32491, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800905 19981218 00905 WP 1998 12 18 CKSA98735 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 569 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 CORROSION FOUND AT MAIN DECK FLOORBEAM LOWER CHORD/CAP AT FS 569, LBL 15. FABRICATED REPAIR PARTS IAW L1011 SRM 53-21-0 0 FIG 803. TREATED AND PRIMED IAW SRM 51-21-02 AND 20-51-09. INSTALLED REPAIR PER L1011 SRM 53-21-00 FIG 803. FOUND D URING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 10 6-208, NON ROUTINE CARD NR 32457, CPCP TASK NR C53-130-05-00. 2 L 7 3 4F A23WE 1998121800906 19981218 00906 WP 1998 12 18 CKSA98736 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 669 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 CORROSION FOUND AT MAIN DECK FLOORBEAM LOWER CHORD/CAP AT FS 669, RBL 78. REMOVED CORROSION IAW L1011 SRM 51-21-01. FO UND TO BE OUT OF LIMITS IAW SRM 51-50-02. REMOVED DAMAGED AREA IAW SRM 51-50-02. TREATED AND PRIMED IAW SRM 51-21-02. INSTALLED REPAIR PER L1011 SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAI NTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-208, NON ROUTINE CARD NR 32458, CPCP TASK NR C53-130-05-00. 2 L 7 3 4F A23WE 1998121800907 19981218 00907 WP 1998 12 18 CKSA98737 1 19981216 A 5347 SEAT TRACK LKHEED 1011 1011385115 5265015 WP BS 649 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 SEAT TRACK AT FS 649 TO 669, RBL 56, CORROSION FOUND UNDER SEAT TRACK FLANGE. REMOVED SEAT TRACK IAW L1011 SRM 51-40-01 . CORROSION FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-21-00. REPLACED SEAT TRACK IAW L1011 SRM 51-40-01. FOUND D URING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 10 6-206, NON ROUTINE CARD NR 32047, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800908 19981218 00908 WP 1998 12 18 CKSA98738 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 649 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND AT C-1 CARGO COMPT, STA 649, RBL 42 TO RBL 55, UPPER FLOORBEAM CHORD CORRODED. REMOVED CORROSION IAW SRM 51-21-01 . FOUND TO BE OUT OF LIMITS IAW SRM 53-27-00 FIG 804. FABRICATED REPAIR PARTS IAW SRM 53-20-00 FIG 802. INSTALLED REP AIR IAW SRM 53-23-00 FIG 802. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FAC ILITY IN OSCODA, MI. WORK ORDER NR 106-206, NON ROUTINE CARD NR 32046, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800909 19981218 00909 WP 1998 12 18 CKSA98739 1 19981216 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 619 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 FOUND IN C-1 CARGO COMPT AT STA 619, THE S-30 STRINGER HAS CORROSION. REMOVED IAW SRM 51-21-01. FOUND TO BE OUT OF LIM ITS IAW SRM 53-13-00 FIG 801. INSTALLED REPAIR IAW SRM 53-13-00 FIG 803. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-206, NON ROUTINE CARD NR 32052, CPCP TASK NR C53-120-04-01. 2 L 7 3 4F A23WE 1998121800910 19981218 00910 WP 1998 12 18 CKSA98740 1 19981216 A 5320 WEB LKHEED 1011 1011385115 5265015 WP BS 1665 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-3 CARGO COMPT FS 1665 BETWEEN STRINGERS 33 AND 28 THE WEB TOP SURFACE AND ALL NUT PLATES FOUND CORRODED. REMOVED C ORROSION IAW L1011 SRM 51-21-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-23-00 FIG 801. REPAIRED FLOORBEAM UPPER CAP IAW SRM 53-23-00 FIG 802. TREATED IAW SRM 51-21-02, PRIMED IAW L1011 MM 20-51-09. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-211, NON ROUTINE CARD NR 31582, CPCP TASK NR C53-120-04-03. 2 L 7 3 4F A23WE 1998121800911 19981218 00911 WP 1998 12 18 CKSA98741 1 19981216 A 5313 LONGERON LKHEED 1011 1011385115 5265015 WP BS 1455 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-2 CARGO PIT AT STA 1455 THE LONGERON 30 STRINGER SKIN HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-00 FIG 801. REMOVED CORRODED AREA AND FABRICATED DOUBLERS IAW SRM 53-31-00 FIG 804. AL ODINED AND PRIMED IAW SRM 51-21-02 AND MM 20-51-09. INSTALLED IAW SRM 53-31-00 FIG 804. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-210, NON ROUTINE CARD NR 30920, CPCP TASK NR C53-120-04-02. 2 L 7 3 4F A23WE 1998121800912 19981218 00912 WP 1998 12 18 CKSA98742 1 19981216 A 5320 TIE LKHEED 1011 1011385115 5265015 WP BS 1790 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN C-3 CARGO COMPARTMENT AT FS 1790, THE TENSION TIE BETWEEN LONGERON 30 AND 31 IS CRACKED AND CORRODED. 2 L 7 3 4F A23WE 1998121800913 19981218 00913 WP 1998 12 18 CKSA98743 1 19981216 A 5320 ANGLE LKHEED 1011 1011385115 5265015 WP BS 378 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 IN NR 2 H/E BAY FOUND CORROSION AT LOWER END OF ANGLE ON I/B AFT CORNER OF H/E BAY FS 378. REMOVED CORROSION IAW SRM 51 -21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-12-00. TREATED AND PRIMED IAW SRM 51-21-02 AND MM 20-51-09. INSTALLED RE PAIR ANGLE IAW SRM 51-40-01. FOUND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACI LITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 31442, CPCP TASK NR 01-00-1005. 2 L 7 3 4F A23WE 1998121800914 19981218 00914 WP 1998 12 18 CKSA98744 1 19981216 A 5230 WEB LKHEED 1011 1011385115 5265015 WP C1 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 C-1 DOOR INTERNAL WEB FRAME HAS CORROSION AROUND ANCHOR NUT HOLES IN FOUR AREAS. REMOVED CORROSION IAW SRM 51-21-01. C OMPLIED WITH THICKNESS CHECK, FOUND FOUR AREAS OUT OF LIMITS IAW SRM 52-11-00. FABRICATED REPAIR PARTS IAW AIA DRAWING EDR-L106044. TREATED AND PRIMED IAW L1011 SRM 51-10-02 AND MM 20-51-09. INSTALLED REPAIR IAW AIA DRWG EDR-L106044. FO UND DURING SCHEDULED C-CHECK AND CPCP WORK CARD ACCOMPLISHMENT AT AIA. MAINTENANCE FACILITY IN OSCODA, MI. WORK ORDER NR 106-187, NON ROUTINE CARD NR 31502, CPCP TASK NR 08-00-1000. 2 L 7 3 4F A23WE 1998122400001 19981224 00001 NM 1998 12 24 RAAA98B2051 1 19981215 A 3260 H1010153 SWITCH BOEING 727 72722C 138400F NM NLG DOWNLOCK SHORTED A RAAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 AL 03 832RV 19098 FLIGHT CREW REPORTED ON CLIMBOUT DURING GEAR RETRACTION, ALL GEAR INTRANSIT LIGHTS (RED) WENT OUT MOMENTARILY THEN CAME BACK ON AND STAYED ON (GEAR HANDLE IN UP POSITION). LDG SELECTOR TO OFF, NO CHANGE. LDG SELECTED DOWN, 3 GREEN LIGHTS PLUS NLG INTRANSIT LIGHT ON. LDG SELECTED UP, 3 INTRANSIT LIGHTS ON. LDG SELECTED OFF AND MAIN LDG DROPPED OUT. RECYC LED LDG, 3 GREEN LIGHTS PLUS NLG INTRANSIT LIGHT ON. VERIFIED NLG DOWN AND LOCKED THROUGH VIEW PORT. RETURNED TO ANC A ND LANDED OVERWEIGHT WITHOUT INCIDENT. REPLACED NLG DOWNLOCK SWITCH DUE SHORTED. PERFORMED LDG RETRACTION TEST PER B72 7 MM 32-32-0. 2 L 7 3 4F A3WE 1998122400002 19981224 00002 NM 1998 12 24 RAAA98B2052 1 19981215 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 832RV 19098 RT AFT OVERWING EMERGENCY EXIT AND AFT EMERGENCY EXIT EGRESS IDENTIFIER LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PA CKS DUE DISCHARGED. 2 L 7 3 4F A3WE 1998122400003 19981224 00003 WP 1998 12 24 CALA9802177 1 19981215 A 5230 FITTING DOUG DC9 DC932 3022066 WP C-1 DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12539 45792 INSPECTION FOUND A .5 INCH CRACK IN C-1 DOOR AFT LOWER STOP INTERCOSTAL TEE FITTING. THE FITTING WAS REMOVED AND REPLAC ED IAW SRM 51-10-8 AND 51-10-4. 2 L 7 2 4F A6WE 1998122400004 19981224 00004 WP 1998 12 24 CALA9802178 1 19981215 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 160-200 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND FLOOR SUPPORT CORRODED JUST FORWARD OF LEFT CENTER SEAT TRACK AT STA 160 TO 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1998122400005 19981224 00005 WP 1998 12 24 CALA9802179 1 19981216 A 5347 SEAT TRACK DOUG DC9 DC982 3022082 WP NR 4 GALLEY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND NR 4 GALLEY FORWARD AND AFT MOUNT POINT CORRODED IN SEAT TRACK. NEW SECTIONS OF SEAT TRACK WERE INSTAL LED IAW SRM 53-05. 2 L 7 2 4F A6WE 1998122400006 19981224 00006 WP 1998 12 24 9810879851 1 19981215 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 760NC 47708 DURING LINE CHECK, FOUND FIRST CLASS CEILING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES IN POWER SUPP LY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1998122400007 19981224 00007 WP 1998 12 24 9810889611 1 19981213 A 3233 ACTUATOR DOUG DC9 DC932 3022066 WP LT MLG FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 611NA 47435 LEFT MAIN LANDING GEAR GREEN LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND RED NOSE GEAR UNSAFE LIGHT REMAINED ON. FLIGHT WAS RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LENS LIGHT ASSEMBLY FOR LEF T MAIN GEAR GREEN LIGHT. ALSO, REPLACED NOSE LANDNG GEAR RETRACT ACTUATOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998122400008 19981224 00008 SO 1998 12 24 COMA9810285 1 19981215 A 5246 DOOR EMB 120 EMB120RT SO FUEL SYSTEM NOT LATCHED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 01 256CA 120245 SERVICE DOOR WARNING DURING TAKEOFF. CLOSED AND LATCHED SINGLE POINT FUEL SERVICE DOOR. 2 L 7 2 4T RT A31SO 1998122400009 19981224 00009 EA 1998 12 24 COMA9860387 1 19981216 A 5270 SENSOR CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 735CA 7267 CABIN DOOR WARNING. ADJUSTED DOOR UPPER CAM PROXIMITY SENSORS TO M/M SPECIFICATIONS. 2 L 7 2 4F RT A21EA 1998122400010 19981224 00010 NM 1998 12 24 UPS98228295 1 19981217 A 2910 65178494061 LINE BOEING 727 72731C 1384011 NM B HYD SYST FAILED A IPXA K NONE K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 01 925UP 19230 INSPECTION TYPE-N/A, HYD SYS 'B' FAILURE INFLIGHT BOTH PUMP LIGHTS ILLUMINATED QUANTITY WENT TO 0, PRESSURE WENT TO 0. F OUND BROKEN HYD LINE IN HYD BAY. REMOVED AND REPLACED HYD LINE (P/N 65-17849-4061) CHANGED CASE DRAIN FILTERS, PUMPS OK . SERVICED NO LEAKS NOTED PER M-M 29-12-21. 2 L 7 3 4F A3WE 1998122400011 19981224 00011 WP 1998 12 24 UPS98828292 1 19981216 A 3260 189915 SENSOR DOUG DC8 DC871F 302199D WP RT MLG INOP A IPXA K NONE N FALSE WARNING CR CRUISE 1 SO 01 772UP 46072 INSPECTION TYPE-N/A, AFTER RETRACTING GEAR, DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED AND ALTERNATE GEAR DOOR LIGHT, LEFT SIDE WAS ILLUMINATED. RECYCLED THE GEAR, WITH SAME INDICATIONS. PERFORMED ADJ/TEST OF LT AND RT MAIN GEAR DOOR UP LATCH MECHANISM PER MM 32-31-04. FOUND RT PROX SENSOR WIRE BARE AND GROUNDING ON UPLATCH MECHANISM CAUSING RED DOORS NO T LATCHED LIGHT. REPLACED RT GEAR DOOR PROX SWITCH. COULD NOT DUPLICATE LT DOOR ALTERNATE AMBER LIGHT. REPLACED LT AN D RT ALTERNATE DOOR SWITCHES, OPS GOOD PER MM 32-31-04. 2 L 7 4 4F RT 4A25 1998122400012 19981224 00012 WP 1998 12 24 UPS98828294 1 19981216 A 3260 189915 SENSOR DOUG DC8 DC871F 302199D WP RT MLG SHORTED A IPXA K NONE N FALSE WARNING CL CLIMB 1 SO 01 772UP 46072 AFTER RETRACTING GEAR, DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED AND ALTERNATE GEAR DOOR LIGHT, LEFT SIDE WAS ILLUMIN ATED. RECYCLED THE GEAR, WITH SAME INDICATIONS. PERFORMED ADJ/TEST OF LT AND RT MAIN GEAR DOOR UPLATCH MECHANISM PER M M 32-31-04. FOUND RT PROX SENSOR WIRE BARE AND GROUNDING ON UPLATCH MECHANISM CAUSING RED DOORS NOT LATCHED LIGHT. REP LACED RT GEAR DOOR PROX SWITCH. COULD NOT DUPLICATE LT DOOR ALTERNATE AMBER LIGHT. REPLACED LT AND RT ALTERNATE DOOR S WITCHES, OPS GOOD PER MM 32-31-04. 2 L 7 4 4F RT 4A25 1998122400013 19981224 00013 WP 1998 12 24 MWEA981154 1 19981215 A 2560 5917689103 COVER DOUG DC9 DC915 3022036 WP GALLEY DR SLIDE FELL OFF A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 300ME 45718 GALLEY DOOR EVACUATION SLIDE COVER FELL OFF. RESECURED GALLEY DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1998122400014 19981224 00014 1998 12 24 MWEA981155 4 19981215 A 2565 113317 SLIDE DOUG DC9 DC932 3022066 WP PAX DOOR LOW PRESSURE A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 205ME 47601 FORWARD ENTRY DOOR EVACUTATION SLIDE PRESSURE LOW. REMOVED AND REPLACED FORWARD ENTRY DOOR EVACUATION SLIDE. 2 L 7 2 4F A6WE 1998122400015 19981224 00015 NM 1998 12 24 DHL98701002 1 19981216 A 3260 10608198 SWITCH BOEING 727 72730C 1384009 NM RT MLG DNLOCK FAILED A DHLA O OTHER N FALSE WARNING LD LANDING 1 SO 01 701DH 19011 UPON TOUCHDOWN, RIGHT MAIN GEAR DOWN AND LOCKED LIGHT ON FWD PANEL EXTINGUISHED AND RIGHT MAIN GEAR NOT DOWN AND LOCKED ILLUMINATED AND REMAINED ON AND THE WARNING HORN CAME ON AND REMAINED ON. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SWI TCH AND OPS CHECK GOOD PER MM 32-61-21. 2 L 7 3 4F A3WE 1998122400016 19981224 00016 NM 1998 12 24 CKSA98748 1 19981212 A 5711 SPAR BOEING 747 747269B NM LT WING CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 LOCATED AT LEFT WING LOWER L/E CAVITY, FRONT SPAR, LOWER CHORD AT OSLE 1440 AND OSLE 1460 FOUND SMALL AREA OF LEVEL 2 LO CAL CORROSION. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, I N HONG KONG (VHKG). JOB NUMBER 7C15012. 2 L 7 4 4F RT A20WE 1998122400017 19981224 00017 NM 1998 12 24 CKSA98749 1 19981212 A 5320 INTERCOSTAL BOEING 747 747269B NM BS 1920 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 FOUND IN BULK CARGO COMPARTMENT, FLOOR SUPPORT INTERCOSTAL BULGED AND CORRODED AROUND ANCHOR NUTS AT ZONE 100, STA 1920 TO STA 1980, RBL 55. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACIL ITY, IN HONG KONG (VHKG). C-CHECK WORK CARD NUMBER 7CI1014, NON ROUTINE TASK CARD NUMBER JF58580. 2 L 7 4 4F RT A20WE 1998122400018 19981224 00018 NM 1998 12 24 CKSA98750 1 19981212 A 5230 SKIN BOEING 747 747269B NM CARGO DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 AFT CARGO DOOR INTERNAL SKIN BULGE CORROSION FOUND AT AFT LOWER CORNER OF DOOR UNDER SEAL RETAINER ZONE 141. FOUND DURI NG SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). C-CHE CK WORK CARD NUMBER 7AS1401, NON ROUTINE TASK CARD NUMBER JF63796. 2 L 7 4 4F RT A20WE 1998122400019 19981224 00019 NM 1998 12 24 CKSA98751 1 19981212 A 5320 65B062774 INTERCOSTAL BOEING 747 747269B NM BS 1980 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 IN BULK CARGO COMPARTMENT, AFTER FLOOR SUPPORT INTERCOSTAL REMOVED. CORROSION FOUND ON FLOOR SUPPORT HAT SECTION HORIZO NTAL FLANGE A AT ZONE 150 AFT, BS 1980, RBL 55. FLOOR SUPPORT HAT SECTION REPLACED AS PER SRM H-4001. FOUND DURING SCH EDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). CPCP TASK C ARD NR C53-100-01-6-10. NON ROUTINE TASK CARD NUMBER JF64166. 2 L 7 4 4F RT A20WE 1998122400020 19981224 00020 NM 1998 12 24 CKSA98752 1 19981212 A 5347 98033142 SEAT TRACK BOEING 747 747269B NM BS 480 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 FOUND AT ZONE 220 UPPER DECK CABIN, STA 480, LBL 55, SEAT TRACK/TIE DOWN TRACK HAS CORROSION CRACK 3 INCH LENGTH. REMOV ED CORROSION IAW SRM 51-10-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REPLACED SEAT TRACK IAW SRM 51-10-01 PG 18. CORROSION INHIBITOR APPLIED IAW SRM 51-10-02. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAE CO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). C-CHECK WORK CARD NR 7CI1017, NON ROUTINE TASK CARD NUMBER JF56048 . 2 L 7 4 4F RT A20WE 1998122400021 19981224 00021 NM 1998 12 24 CKSA98753 1 19981212 A 5315 FLOORBEAM BOEING 747 747269B NM BS 2240 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 LOCATED AT ZONE 250 MID CABIN, BS 2240, FLOORBEAM HAS AREA OF CORROSION FROM LBL62 TO LBL 82. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REPAIRED FLOORBEAM IAW SRM 51-40-04 FIG 1, TREATED IAW SRM 53-10 -02. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KON G (VHKG). C-CHECK WORK CARD NR 7CI2018, NON ROUTINE TASK CARD NR JF55230. 2 L 7 4 4F RT A20WE 1998122400022 19981224 00022 NM 1998 12 24 CKSA98754 1 19981212 A 5347 SEAT TRACK BOEING 747 747269B NM BS 2260 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 AT ZONE 250 MID DECK, STA 2260 TO STA 2280, LBL 34 SEAT TRACK FOUND CORRODED. REMOVED CORROSION IAW SRM 51-10-01, FOUND OUT OF LIMITS IAW SRM 53-10-01 FIG 1. REPAIRED IAW SRM 53-10-05 FIG 1A AND SRM 51-10-02. FOUND DURING SCHEDULED C-CHEC K AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). C-CHECK WORK CARD NR 7CI 2018, NON ROUTINE TASK CARD NR JF55255. 2 L 7 4 4F RT A20WE 1998122400023 19981224 00023 NM 1998 12 24 CKSA98755 1 19981212 A 5347 AND101331002 SEAT TRACK BOEING 747 747269B NM BS 1010 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 LOCATED IN ZONE 240 MID DECK, STA 1010, RBL 11, SEAT/TIE DOWN TRACK FOUND CORRODED. CORROSION BLEND OUT BEYOND SRM LIMI TS IAW SRM 53-10-01 FIG 1. REPAIRED IAW SRM 53-10-05 FIG 35 AND MM 51-10-00, 12-20-00. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). C-CHECK WORK CARD NR 7CI20 16, NON ROUTINE TASK CARD JF56931. 2 L 7 4 4F RT A20WE 1998122400024 19981224 00024 NM 1998 12 24 CKSA98756 1 19981212 A 5347 SEAT TRACK BOEING 747 747269B NM BS 1540 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 LOCATED AT ZONE 250 MAIN DECK, STA 1540, RBL 33, CORROSION CRACK FOUND ON SEAT TRACK SECTION L-1. FOUND TO BE OUT OF LI MITS PER SRM 53-10-01 FIG 1. REPAIRED SEAT TRACK IAW SRM 53-10-05 FIG 1A AND SRM 51-10-02. FOUND DURING SCHEDULED C-CH ECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPAIR FACILITY, IN HONG KONG (VHKG). C-CHECK WORK CARD NR 7 CI2016, NON ROUTINE TASK CARD JF56964. 2 L 7 4 4F RT A20WE 1998122400025 19981224 00025 NM 1998 12 24 CKSA98757 1 19981212 A 5313 LONGERON BOEING 747 747269B NM BS 1241 BULGED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 707CK 21541 LT WLG W/W STA 1241 BULKHEAD UPPER AREA FOUND BULGE UP AT STA 1241 TO STA 1250, LBL 60 TO LBL 70. REPLACED RIVETS, BOLT S AND COLLARS AT AFFECTED AREA IAW SRM 51-10-01. CORROSION REMOVAL IAW SRM 57-10-01, PRIMED AND TREATED IAW SRM 51-10-0 2, MM 51-20-11 AND 53-15-00. FOUND DURING SCHEDULED C-CHECK AND CPCP TASK CARD ACCOMPLISHMENT AT HAECO MAINTENANCE/REPA IR FACILITY, IN HONG KONG (VHKG). CPCP TASK CARD NR C53-100-01-7-10, NON ROUTINE TASK CARD JF56329. 2 L 7 4 4F RT A20WE 1998122400026 19981224 00026 NE 1998 12 24 TC8A98085 2 19981217 A 7321 FUEL CONTROL DOUG DC8 DC861F 3021953 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE OUT OF ADJUST A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 184SK 45981 669204 NR 4 ENGINE WOULD NOT DEVELOPE TAKEOFF POWER, (1.87 EPR). REJECTED T/O AT 100 KTS. ADJUSTED NR 4 ENGINE FUEL CONTROL I AW DMM, CH 73-20-1. PERFORMED ENGINE RUN-UP TO T/O POWER, SYSTEM CHECKS GOOD DC8 ENGINE RUN UP MM IAW DMM 72-00. 2 L 7 4 4F 4 F 4A25 1E8 1998122400027 19981224 00027 NM 1998 12 24 SWAA983116 1 19981214 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 178 CORROSION A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND EXTERIOR FUSE SKIN BULGING AND RIVETS PULLING THROUGH, INDICATING CORROSION BETWEEN S KIN LAYERS AT BS 663 AT S27R, KEEL BEAM CHORD. INSTALLED REPAIR PER SRM. 2 L 7 2 4F RT A16WE 1998122400028 19981224 00028 NM 1998 12 24 SWAA983117 1 19981214 A 3350 BULB BOEING 737 7373Y0 1384671 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 664WN 23495 DURING SCHEDULED SC CHECK, FOUND 3 RED EMERGENCY FLOOR TRACKS LIGHTS INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998122400029 19981224 00029 NM 1998 12 24 SWAA983118 1 19981216 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 300SW 22940 DURING SCHEDULED SC CHECK, FOUND LAST BULLNOSE EMERGENCY LIGHT ON RT SIDE INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1998122400030 19981224 00030 NM 1998 12 24 SWAA983119 1 19981216 A 3350 BULB BOEING 737 7372H4 138448C NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 068SW 22357 DURING SCHEDULED C1 CHECK, FOUND AFT CABIN EMERGENCY FLOOR TRACK LIGHTING HAS ONE RED LIGHT INOP. RELAMPED PER BOEING M /M. 2 L 7 2 4F A16WE 1998122400031 19981224 00031 NM 1998 12 24 SWAA983120 1 19981217 A 3350 BULB BOEING 737 7372H4 138448C NM SERVICE DOOR FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 063SW 22061 DURING SCHEDULED SC CHECK, FOUND FWD SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER BOEING M/M. 2 L 7 2 4F A16WE 1998122400032 19981224 00032 NM 1998 12 24 SWAA983121 1 19981216 A 5520 BUSHING BOEING 737 7373H4 1384600 NM LT ELEV WORN A SWAA K NONE E VIBRATION/BUFFET CR CRUISE 1 SW 07 316SW 23338 VIBRATION IN CRUISE FLIGHT. STRUCTURE, FELT IN YOKE AND FLOOR OF AIRCRAFT. FLIGHT ATTENDANTS REPORTED REAR OF AIRCRAFT WAS VERY BAD. FOUND WORN BUSING O/B LT ELEV TAB. REMOVED AND REPLACED BUSHING PER M/M. 2 L 7 2 4F RT A16WE 1998122400033 19981224 00033 NM 1998 12 24 SWAA983122 1 19981215 A 2133 7110033 OUTFLOW VALVE BOEING 737 7372T4 1384492 NM CABIN FAILED A SWAA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 129SW 22340 PRESSURIZATION AUTO FUNCTION FAILED ON DEPARTURE. CABIN PRESSURE CLIMBED TO 2,000 FT MINUTE. SWITCHED TO STBY, CABIN RECOVERED. OK TO CONTINUE PER MEL 21-14 AND SPECIAL PROCEDURE. REPLACED MAIN (AFT) OUTFLOW VALVE, SYSTEM OPS CK'D PER M/M. TAG (P/N 987342) (S/N 711003-3) OFF, (P/N 112796) (S/N 148994) ON. 2 L 7 2 4F A16WE 1998122400034 19981224 00034 NM 1998 12 24 SWAA983123 1 19981215 A 2530 COFFEEMAKER BOEING 737 7377H4 NM GALLEY DIRTY A SWAA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 718SW 27852 F/A REPORTED SMELLING SMOKE FROM AN ELECTRICAL SOURCE FROM AFT GALLEY. AFTER PULLING BOTH COFFEEMAKERS AND CIRCUIT BREA KERS, SMOKE SMELL DISSIPATED. CLEAN DEBRIS OFF AFT GALLEY COFFEEMAKER RACKS. OPS CK GOOD PER MM. 2 L 7 2 4F RT A16WE 1998122400035 19981224 00035 NM 1998 12 24 VJ9800649 1 19981202 A 5320 INTERCOSTAL BOEING 737 7372L9 1384497 NM BS 986.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL BS 986.5 THROUGH 1006 BL0, AND BS 947 THROUGH 967 LBL 42 INTERCOASTAL WERE FOUND C ORRODED. FABRICATED AND INSTALLED J ANGLE AND SHIM AT BS986.5 THROUGH BS 1006, AND TWO REPAIR DOUBLERS AT BS 947 THROUG H BS 967 IAW B737 SRM 51-30-2, 51-40-2, 51-10-2, 51-20-1, MM 51-21-31 AND DWG NR 65-46818. 2 L 7 2 4F RT A16WE 1998122400036 19981224 00036 NM 1998 12 24 VJ9800650 1 19981202 A 5230 WEB BOEING 737 7372L9 1384497 NM C 2 DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL CORROSION WAS FOUND ON THE UNDER SIDE OF THE C-2 TRANSITIONAL WEB. MECHANICALLY R EMOVED THE CORROSION, FOUND CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 51-30-2, 53-10-1, 51-40-2 AND M M 51-20-11. 2 L 7 2 4F RT A16WE 1998122400037 19981224 00037 NM 1998 12 24 VJ9800651 1 19981203 A 5320 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 616 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL FIRST ONE AT BS 616 LATERAL FLOORBEAM TO RBL 46 LONGITUDINAL FLOORBEAM ATTACH FITT ING WAS FOUND CRACKED. SECOND ONE AT LEFT FORWARD FS 257.5 - FS 312 LBL 50.5 ON THE UPPER AND LOWER SURFACE. THIRD ONE AT BS 312 FROM S29-20L AT THE FWD LAVATORY. FOURTH ONE AT THE RIGHT FWD GALLEY BS 294.5 BL 0 - RBL 48. LAST ONE AT BS 967 LBL 24 TO RBL24 AT THE CLIP NUTS OF THE UPPER FLANGE. REMOVED AND REPLACED CRACKED ANGLE AND CHEMICALLY REMOVED ALL CORROSION AND INSTALLED REPAIR ANGLE IAW B737 SRM 51-40-4, 51-10-2, 51-40-3, 51-30-2, 53-10-1, 51-40-2, 53-10-9 FIG. 5, AND MM 51-20-11 AND 51-21-31. 2 L 7 2 4F RT A16WE 1998122400038 19981224 00038 NM 1998 12 24 VJ9800652 1 19981204 A 5320 ANGLE BOEING 737 7372L9 1384497 NM BS 270 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL CORROSION WAS FOUND ON THE TOP AND BOTTOM OF THE L ANGLE AT BS 270.0 - 294.5 RBL 5 2 AND ON THE AFT SIDE OF S29R L ANGLE AT BS 360 FRAME. THE ANGLE WAS FOUND TO BE CRACKED AT BS 270-294.5. REMOVED CRAC KED AREA. MECHANICALLY REMOVED CORROSION FROM AREAS. FABRICATED AND INSTALLED REPAIR MEMBERS IAW B737 SRM 51-10-2, 53- 10-4, 51-40-3, 51-30-2, AND MM 51-20-11. 2 L 7 2 4F RT A16WE 1998122400039 19981224 00039 NM 1998 12 24 VJ9800653 1 19981204 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 727 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL BS 727 S27L WL 148.5 THERE IS A BULGED AREA IN THE FUSELAGE SKIN OUTER SURFACE. R EMOVED THE CORROSION. FABRICATED AND INSTALLED REPAIR IAW B737 SRM 53-30-3, 51-10-2 AND MM 51-20-11. ACCEPTABLE FOR RET URN TO SERVICE PER AIRTRAN RES 982110. 2 L 7 2 4F RT A16WE 1998122400040 19981224 00040 NM 1998 12 24 VJ9800654 1 19981204 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 722.5 - 731.5 DAMAGED A ZZDA K NONE C F.O.D. IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL LIGHTNING STRIKES WERE FOUND BETWEEN BS 722.5 AND 731.5 AT STRINGERS 1, 5 AND 3.5 . APPROXIMATELY 44.0 SQ IN ACROSS THE SKIN SPLICE AND SKIN LAP. DRILLED OUT 10. LIGHTNING STRIKES, BLEND REMAINING STRI KES. SEVERAL AREAS BETWEEN S1L AND S3L ARE OUT OF LIMITS, S4L TO S5 AND 3.5 ARE WITHIN LIMITS. CUT OUT OUT OF LIMITS A REAS. FABRICATED AND INSTALLED REPAIRS IAW B737 SRM 53-30-3 FIG 23, 53-30-1 FIG 1, 53-30-3 FIG 28, 51-10-2, 51-30-2, 51 -20-4, MM 51-23-12 AND 25-31-341. 2 L 7 2 4F RT A16WE 1998122400041 19981224 00041 NM 1998 12 24 VJ9800655 1 19981206 A 5347 SEAT TRACK BOEING 737 7372L9 1384497 NM BS 253.5 - 294.5 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL SEAT TRACKS AT STATION BS 253.5 - 294.5, BS 270 - 294.5 RBL 16, BS 380 - 480 LBL 2 4.75, BS 727-947 LBL 45.50, AND BS 986 - 1016 RBL 33.5 WERE FOUND WITH CORROSION, PITTING AND GOUGES. REMOVED SEAT TRAC KS. FABRICATED SECTIONS AND INSTALLED NEW SEAT TRACKS IAW B737 SRM 51-30-2, 53-10-1 FIG 4, 51-30-8, 51-21-31, MM 51-20- 11, 51-10-6, AND 53-10-5. 2 L 7 2 4F RT A16WE 1998122400042 19981224 00042 NM 1998 12 24 VJ9800656 1 19981206 A 5230 SKIN BOEING 737 7372L9 1384497 NM C-1 DOOR GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL, THE FORWARD CARGO DOOR LEFT LOWER AIRCRAFT STRUCTURE WAS FOUND GOUGED EXCESSIVELY . BLENDED OUT GOUGED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW B737 SRM 53-30-3 FIG 6, 51-10-2 AND MM 51-20-11. 2 L 7 2 4F RT A16WE 1998122400043 19981224 00043 NM 1998 12 24 VJ9800657 1 19981208 A 5330 SKIN BOEING 737 7372L9 1384497 NM BS 853 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL, A 1 BY 0.50 DENT WAS FOUND IN THE AFT FUSELAGE SKIN AT BS 853 BETWEEN S20 AND 2 1R. THE DENT WAS OUT OF LIMITS PER B737 SRM 53-30-1. CUT OUT DENT. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW B737 SRM 53-30-3 FIG 1, 51-10-2, 51-30-2, AND MM 51-20-11. 2 L 7 2 4F RT A16WE 1998122400044 19981224 00044 NM 1998 12 24 VJ9800658 1 19981209 A 7110 COWL BOEING 737 7372L9 1384497 NM NR 2 ENGINE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL A 3 AND .75 INCH BY .135 DENT WAS FOUND IN THE OUTBOARD SIDE OF THE NR 2 ENGINE N OSE COWLING SKIN AT 8 O'CLOCK POSITION. ANOTHER DENT WAS FOUND AT THE RIGHT NOSE COWLING BETWEEN 4 O'CLOCK AND 5 O'CLOC K POSITIONS 9 INCHES FROM THE LEADING EDGE. A THIRD DENT WAS LOCATED AT BS 358 NEAR S17L AND THE LAST ONE AT THE AFT CA RGO DOOR LOWER AIRCRAFT STRUCTURE. REPAIRED ALL DENTS IAW AIRTRAN RES 982132, B737 SRM 51-30-2 AND 53-30-3 FIG 28, 51-2 1-31, 54-30-3, AND MM 51-20-11. 2 L 7 2 4F RT A16WE 1998122400045 19981224 00045 WP 1998 12 24 VJ9800659 1 19981217 A 2560 5928730503 SLIDE DOUG DC9 DC932 3022066 WP L 1 DOOR NOT SECURED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 913VV 47318 FORWARD EMERGENCY EXIT SLIDE CAME OFF L-1 DOOR. REINSTALLED EMERGENCY EXIT SLIDE L-1 DOOR PER MM 25-60. 2 L 7 2 4F A6WE 1998122400046 19981224 00046 WP 1998 12 24 VJ9800660 1 19981217 A 2560 5928730503 SLIDE DOUG DC9 DC932 3022066 WP L 1 DOOR NOT SECURED A ZZDA K NONE O OTHER TX TAXI/GRND HDL 1 SO 15 905VV 47378 MAIN CABIN ENTRY DOOR NOT SECURED. MAIN CABIN ENTRY DOOR SLIDE SECURED PER DC9 MM 25-62-0 RII COMPLIED WITH. 2 L 7 2 4F A6WE 1998122400047 19981224 00047 NM 1998 12 24 VJ9800661 1 19981204 A 5320 SHEAR TIE BOEING 737 7372L9 1384497 NM BS 727 & 827 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL, THE SHEAR TIE AT RIGHT SIDE BS 727A AND BS 827 WERE FOUND CORRODED. REMOVED COR RODED SHEAR TIE. FABRICATED AND INSTALLED REPAIR SHEAR TIE IAW B737 SRM 53-10-4 FIG 6, 51-10-2, 51-30-2 AND MM 51-20-11 . 2 L 7 2 4F RT A16WE 1998122400048 19981224 00048 NM 1998 12 24 VJ9800663 1 19981205 A 5320 ANGLE BOEING 737 7372L9 1384497 NM BS 986-1006 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL, THE I BEAM ANGLE WAS FOUND CORRODED IN THE MAIN CABIN AT BS 986-1006 LBL 12. REM OVED CORROSION. FABRICATED AND INSTALLED 2EA. REPAIRS AND FILLERS IAW B737 SRM 51-30-2, 51-10-2, AND 51-40-4. 2 L 7 2 4F RT A16WE 1998122400049 19981224 00049 NM 1998 12 24 VJ9800664 1 19981205 A 5320 HAT SECTION BOEING 737 7372L9 1384497 NM BS 990 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL. THE MAIN CABIN HAT SECTION FOR THE AFT LAV FORWARD WALL HAS CORROSION AT BS 990 LBL 25. FABRICATED AND INSTALLED NEW HAT CHANNEL IAW B737 SRM 51-20-4, 51-30-2, AND 51-40-4. 2 L 7 2 4F RT A16WE 1998122400050 19981224 00050 NM 1998 12 24 CALA9802180 1 19981217 A 3260 BACR13CG2AB RELAY BOEING 737 7373T0 1384582 NM E & E COMPT INOPERATIVE A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 76355 23593 THE GEAR LEVER WOULD NOT RAISE BEYOND THE OFF POSITION AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE THE FAILURE. THE R276 AIR SENSING RELAY WAS REPLACED AS A PRECAU TIONARY MEASURE. AN EXTENSION AND RETRACTION CHECK WAS PERFORMED AND ALL OPERATION AND INDICATIONS WERE NORMAL. 2 L 7 2 4F RT A16WE 1998122400051 19981224 00051 NM 1998 12 24 CALA9802181 1 19981217 A 3230 BACC18Z3R CIRCUIT BREAKER BOEING 737 737524 1384721 NM LANDING GEAR TRIPPED A CALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 17614 27327 THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM EWR. THE GEAR HANDLE WOULD NOT RAISE BEYOND THE OFF POSITION. TH E AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR LATCH AND WARNING C IRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET. ALL THREE LANDING GEAR WERE SWUNG IAW MM 07-11-11 AND OPERATION CHECKED GOOD. 2 L 7 2 4F RT A16WE 1998122400052 19981224 00052 WP 1998 12 24 CALA9802182 1 19981217 A 3350 20131A BATTERY PACK RADIANT DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14839 49635 THE AFT CABIN EMERGENCY AISLE PATH LIGHTING BATTERY PACK HAD A LOW CHARGE. THE BATTERY PACK WAS REMOVED AND REPLACED AN D OPERATION CHECKED GOOD. 2 L 7 2 4F A6WE 1998122400053 19981224 00053 WP 1998 12 24 CALA9802183 1 19981218 A 5330 SKIN DOUG DC10 DC1010 3022110 WP CARGO DOORWAY CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND CORROSION AT LOWER SIDE OF CENTER CARGO DOOR COMPARTMENT CUTOUT. THE AREA WAS REPAIRED IAW ECRA 5315- 01027 AND SRM 53-50-00, FIGURE 22. 2 L 7 3 4F A22WE 1998122400054 19981224 00054 WP 1998 12 24 CALA9802184 1 19981218 A 5320 STRAP DOUG DC10 DC1010 3022110 WP BS 999 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND CORROSION ON FORWARD CARGO COMPARTMENT REINFORCEMENT STRAP AT STA 999, LONGERON 43L. THE CORRODED ARE A OF STRAP AND WEB WERE TRIMMED OUT AND A REPAIR WAS PERFORMED IAW SRM 53-50-00, FIGURE 1. 2 L 7 3 4F A22WE 1998122400055 19981224 00055 WP 1998 12 24 CALA9802185 1 19981218 A 5730 SKIN DOUG DC10 DC1010 3022110 WP WS 230 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 68047 47801 INSPECTION FOUND CORROSION AROUND FASTENERS ON RT WING LOWER SKIN PANEL AT XORS 230. THE CORRODED AREA WAS TRIMMED OUT. FILLER AND DOUBLER WERE INSTALLED IAW ECRA 5730-01616. 2 L 7 3 4F A22WE 1998122400056 19981224 00056 WP 1998 12 24 CALA9802186 1 19981218 A 3350 20131A BATTERY PACK RADIANT DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12539 45792 THE FORWARD AND AFT EMERGENCY AISLE PATH LIGHTING BATTERY PACKS FAILED TIME LIMIT CHECK. THE BATTERY PACKS WERE REPLACE D AND OPERATION CHECKED GOOD IAW MM 33-50-0, PAGE 1. 2 L 7 2 4F A6WE 1998122400057 19981224 00057 NM 1998 12 24 QXEA9802101 1 19981212 A 2611 WIRE DHAV DHC8 DHC8102 2809003 NM NR 2 SMOKE DET BROKEN A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 821PH 104 SEA - FOUND BROKEN WIRE ON NR 2 SMOKE DETECTOR CANNON PLUG. MAINTENANCE SOLDERED WIRE TO CANNON PLUG. OPERATIONAL CHEC K GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1998122400058 19981224 00058 NM 1998 12 24 QXEA9802102 1 19981212 A 3350 1013079 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 346PH 477 SEA - THIRD AND FOURTH FLOOR EGRESS LIGHTS INOP. MAINTENANCE FOUND 2 LAMPS MISSING FROM STRIP. REPLACED STRIP. OPERAT IONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998122400059 19981224 00059 NM 1998 12 24 98FDEA00749 1 19981219 A 3246 WHEEL BOEING 727 727233 138408A NM RT MLG MISSING A FDEA O OTHER D INFLIGHT SEPARATION UK UNKNOWN 1 SO 25 257FE 20939 98-302 - RIGHT OUTBD WHEEL AND ASSEMBLY MISSING. REMOVED AND REPLACED RIGHT MAIN LAND GEAR ASSY PER MM 32-11-0 PG 401-6 01 AND FEDEX A/C MAINTENANCE WORK CD 32T/502. OK FOR SERVICE. 2 L 7 3 4F RT A3WE 1998122400060 19981224 00060 NM 1998 12 24 98FDEA00750 1 19981219 A 3020 CONNECTOR BOEING 727 72722C 138400F NM NR 2 COWL LOOSE A FDEA A UNSCHED LANDING N FALSE WARNING UK UNKNOWN 1 SO 25 113FE 19894 98-303 NR 2 COWL ANTIICE TEMP OFF SCALE AT OVER 250C. NR 2 COWL VALVE STUCK. FOUND CANNON PLUG OFF ANTI DUCT TEMP SENS OR. LOCK WIRED ELECT CONN TO SENSOR PER MM 30-21-051. PERF FUNCTION TEST PER MM 30-21-00. SYSTEM OPER NORM WITH NR 2 ENG RUNNING. 2 L 7 3 4F A3WE 1998122400061 19981224 00061 EU 1998 12 24 98FDEA00751 1 19981221 A 7830 TR UNIT AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE INOP A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 669FE 774 98-304 DURING T/O ROLL, RECEIVED ECAM WARN NR 1 ENG REVERSER PRESS. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST P OS PER M PROC 78.1. 2 L 7 2 4F RT A35EU 1998122400062 19981224 00062 NM 1998 12 24 98FDEA00752 1 19981217 A 5350 ARC75001 TAIL CONE DOUG MD11 MD11F 3023600 NM AFT FUSELAGE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 SNRM 413 TAIL CONE STRUCTURE OF RT HINGE FAIL DURING OPER: AREA DAMAGED DURING EXTEND OPER. REMOVED AND REPLACED TAIL C ONE RT HINGE STRUCTURE DAMAGE LWR SKIN, INTERCOSTAL, RIBS, FRAME, PNL AND DOUBLERS PER DWG AKC 7504 AND OPER CK MM 53-52 -01-2 FND SAT. 2 L 7 3 4F RT A22WE 1998122400063 19981224 00063 NM 1998 12 24 98FDEA00753 1 19981218 A 7120 6518724 MOUNT BOEING 727 72725C 138400H NM NR 1 ENGINE CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 120FE 19356 NR 1 ENG AFT FITTING MOUNT CRACKED. FOUND BY VISUAL INSP AT C-001 CHECK/FITTING. REMOVED AND REPLACED IAW SB 727-54-00 17. 2 L 7 3 4F A3WE 1998122400064 19981224 00064 NM 1998 12 24 98FDEA00754 1 19981218 A 5712 RIB BOEING 727 72725C 138400H NM BS 760 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 120FE 19356 BS 760 AT RBL 70.5 RIB UPPER CHORD IS CRACKED. FOUND AT COOL CHECK BY VISUAL INSP. LARGE REPAIR INSTALL IAW SB 727-57- 0112. 2 L 7 3 4F A3WE 1998122400065 19981224 00065 NM 1998 12 24 98FDEA00755 1 19981218 A 5230 6525771 FITTING BOEING 727 72725C 138400H NM CARGO DOOR LATCH CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 120FE 19356 FOUND ON VISUAL INSP WITH LATCHING PINS. REMOVED AT C-001 CHECK, CARGO DOOR LATCH FITTING NR 2 THROUGH NR 8 CORRODED IN SIDE BORE. REMOVED AND REPLACED LATCH FITTING. 2 L 7 3 4F A3WE 1998122400066 19981224 00066 WP 1998 12 24 ABXA9801184 1 19981216 A 3260 H141003 SWITCH DOUG DC8 DC863 302198A WP RT MLG DEFECTIVE A ABXA O OTHER N FALSE WARNING AP APPROACH 1 GL 23 817AX 45928 WHEN LANDING GEAR EXTENDED, RIGHT MAIN GEAR GREEN LIGHT DID NOT COME ON. PERFORMED ABNORMAL PROCEDURES. NO HELP. ACCO MPLISHED TOWER FLY-BY. TOWER REPORTED GEAR DOWN. LANDING WAS UNEVENTFUL. REPLACED RIGHT MAIN LANDING GEAR DOWNLOCK SW ITCH IAW DC8 MM 32-60-00. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1998122400067 19981224 00067 WP 1998 12 24 ABXA9801185 1 19981217 A 3350 41B004AD0763 BATTERIES DOUG DC9 DC931 3022065 WP CABIN CORRODED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 923AX 47165 EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REMOVED BATTERIES, CLEANED TERMINALS AND REINSTALLED BATTERIES. OPS CHECKED GOO D. 2 L 7 2 4F A6WE 1998122400068 19981224 00068 NM 1998 12 24 DL76L982558 1 19981213 A 3010 VALVE 2780537104 BOEING 767 767332 1382001 NM RT WING FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 27 177DN 1530A 25122 RT WING ANTIICE DISAGREE LIGHT ON WITH SWITCH IN ON. PAX REPORTED NOISE IN 1ST ROW TOURIST RT SIDE. RETURNED TO JFK. R EPLACED RT WING ANTI ICE VALVE. OPERATIONAL AND LEAK CHECK OK. PERFORMED OVERWEIGHT LDG INSP PER 05-51-35-2 NO FAULTS FOUND. 2 L 7 2 4F RT A1NM 1998122400069 19981224 00069 NM 1998 12 24 DL72S982564 1 19981215 A 2782 269002917 ACTUATOR BOEING 727 727232 1384082 NM RT LE FLAP LEAKING A DALA O OTHER K J FLUID LOSS WARNING INDICATION TX TAXI/GRND HDL 1 SO 27 407DA 21151 AIRCRAFT LOST 'A SYSTEM HYDRAULICS WHILE TAXING TO THE GATE AFTER LANDING IN CVG. MTC FOUND THAT THE NUMBER 7 LEADING EDGE SLAT ACTUATOR HAD FAILED. REPLACED ACTUATOR AND BOTH HYDRAULIC PUMPS. 2 L 7 3 4F A3WE 1998122400070 19981224 00070 WP 1998 12 24 DLL10982565 1 19981215 A 2910 O RING 31914908 LKHEED 1011 10113851 5265010 WP HYD SERV CENTER TORN A DALA O OTHER K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 1732D 193C1213 C SYSTEM QUANTITY GAUGE INDICATED ONE-QUARTER AFTER GEAR AND FLAPS WERE RETRACTED. PRESSURE STAYED NORMAL 3000 PSI LOW QTY LIGHT STAYED OFF. PRODCEDURE ACCOMPLISHED, SYSTEM SHUT DOWN. WHEN GEAR WAS EXTENDED LOW QTY CAME ON. SYSTEM WORKE D NORMALLY. (ATM WAS USED TO LOWER GEAR). FOUND O RING BAD ON PLUG FITTING ON BACK SIDE OF LANDING GEAR MODULE IN HYD S ERV CENTER. REPLACED PLUG AND O RING AND PRESSURIZED HYD SYSTEMS. LEAK CKS GOOD. 2 L 7 3 4F A23WE 1998122400071 19981224 00071 NM 1998 12 24 DL72S982567 1 19981105 A 5753 SPAR BOEING 727 727232 1384082 NM NR 2 TE MID FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 406DA 21150 NR 2 MID FLAP, CRACK AFT SPAR RAIL 33 FROM I/B END OF FLAP. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 615732. 2 L 7 3 4F A3WE 1998122400072 19981224 00072 NM 1998 12 24 DL72K982571 1 19981208 A 5530 WEB BOEING 727 727232 1384082 NM VERT STAB CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 AT HMV ON 12/8/98, FOUND VERTICAL STAB INTERIOR - VERT WEB AT STA 1303 IS CRACKED AT LT LWR CORNER, ABOVE S-DUCT. DYED CK, PER PS 900-6-3 NR 1 DRILLED CRACK PER SRM 53-10-4 FIG 17, FAB'D DOUBLER, TREATED, PAINTED, INSTALLED PER 53-10-4 FIG 17. 2 L 7 3 4F A3WE 1998122400073 19981224 00073 WP 1998 12 24 DLL10982572 1 19981216 A 2530 OUTLET LKHEED 1011 10113851 5265010 WP GALLEY SHORTED A DALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 719DA 193C1135 DURING TAXI OUT, FWD GALLEY RT SERVICE OUTLET SHORTED CAUSING SPARKS AND SMOKE IN THE CABIN. A/C RETURNED TO THE GATE. FOUND FWD GALLEY COFFEE POT LEAKING ON OUTLET. SECURED WATER AND FOUND FWD RT SERVICE OUTLET C/B POPPED IN LWR GALLEY. COLLARED C/B FOR FWD RT SERV OUTLET. REPLACED OUTLET. 2 L 7 3 4F A23WE 1998122400074 19981224 00074 NM 1998 12 24 DL757982573 1 19981130 A 5321 DECK BOEING 757 757232 1384965 NM BS 1681 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 REPLACED AFT DECK AT FLOOR LEVEL STATION 1681 TO 1730 DUE TO CORROSION. 2 L 7 2 4F RT A2NM 1998122400075 19981224 00075 NM 1998 12 24 DL757982574 1 19981202 A 5315 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 REPAIRED 1681 FLOORBEAM DUE TO CORROSION. 2 L 7 2 4F RT A2NM 1998122400076 19981224 00076 NM 1998 12 24 DL757982576 1 19981217 A 2560 MV10 MEGAPHONE BOEING 757 757232 1384965 NM CABIN INOP A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 685DA 27588 ON PREFLIGHT 845/17DEC TPA, AFT MEGAPHONE INOP. REPLACED MEGAPHONE. 2 L 7 2 4F RT A2NM 1998122400077 19981224 00077 NM 1998 12 24 DL72S982577 1 19981211 A 5330 65C139131 SKIN BOEING 727 727232 1384082 NM BS 950 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 516DA 21432 FUSELAGE SKIN FS 950C-950D, STRINGER 28L : REPAIR FOR CORROSION CUTOUT. THE FUSELAGE SKIN WAS FOUND CORRODE D AT STRINGER 28L BETWEEN FS 950C AND 950D. THE DAMAGE WAS REMOVED WITH A 6.3 BY 1.5 CUTOUT IN THS SKIN. THE CUTOUT WA S REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 366214-14, REV A. 2 L 7 3 4F A3WE 1998122400078 19981224 00078 NM 1998 12 24 DL73K982578 1 19981215 A 2400 ELECTRICAL SYST 948F4582 BOEING 737 737232 1384475 NM NR 1 & 2 LOST A DALA B EMER. DESCENT H ELECT. POWER LOSS-50 PC AP APPROACH 1 SO 27 327DL NF4063 23099 ON BASE LEG, SELECTED GEAR DOWN AND FLAPS 15, LOST ALL ELECTRICAL POWER, INCLUDING STBY PWR, HAD NO COMM/NAV. FLEW WITH STBY INST ON LANDING BLEW NR 1 TIRE DUE TO NO ROTATION. REPLACED NR 1 GCU P/N 948F458-2 S/N NF4063, NR 2 GCU S/N 3934, BATT P/N 23168 S/N 13163, BATT CHARGER P/N 2-301-3 S/N 1776. NR 1 BUS TIE BKR P/N 9410335-4 S/N NF6911, NR 2 BTB S/N Z H9271. NR 1 GEN BKR P/N 9410335-4 S/N 6811, NR 2 GEN BKR S/N YE6831, APU BKR S/N ZH9252, BATT CHRGR RELAY R-39, APU STA RT INTERLOCK RELAY R-89, AND TRANSFER RELAYS R-3 AND R-4. ALL CHECKS OK ON TEST FLT PER TOPPS. 2 L 7 2 4F RT A16WE 1998122400079 19981224 00079 NM 1998 12 24 DL72L982579 1 19981130 A 5743 BEAM BOEING 727 727232 1384082 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 LT MLG SUPPORT BEAM HOLES CORRODED. REAMED HOLES. BHEC INSP HOLES. TURNED AND TREATED BUSHINGS PER SRM 57-40. TREATE D BORES. INSTALLED BUSHINGS. ROTO PEEN AREAS PER ERA 332561-14. TREATED AND PAINTED PER ERA 332561-14. SEALED ENDS O F BUSHINGS PER ERA 332561-14. 2 L 7 3 4F A3WE 1998122400080 19981224 00080 NM 1998 12 24 DL72L982580 1 19981130 A 5743 BEAM BOEING 727 727232 1384082 NM LT MLG CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 L MLG SUPPORT BEAM HOLES CORRODED. REAMED HOLES. NDT-BHEC BEAM HOLES. TURNED BUSHINGS. TREATED BORES, INSTALLED BUSHI NGS. ROTO PEEN HOLES SURFACES AS PER ERA 332561-14. TREATED AND PAINTED AREAS PER ERA 332561-14. SEALED EDGES OF BUSH INGS PER ERA 332561-14. 2 L 7 3 4F A3WE 1998122400081 19981224 00081 NM 1998 12 24 DL76S982582 1 19981217 A 2740 AS11504K0146 HOSE BOEING 767 767332 1382001 NM STAB TRIM RUPTURED A DALA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 SO 27 122DL 23436 CENTER HYD QUANITY LIGHT CAME ON. QTY INDICATED .47 ON DOWN WIND WHEN LIGHT CAME ON. FOUND HYD LINE PN AS115-04K0146 R UPTURED ON STAB TRIM CONTROL MODULE. IPC LOCATION 27-41-65-01 ITEM 220. INSTALLED TEMP REPAIR HYD LINE. 2 L 7 2 4F RT A1NM 1998122400082 19981224 00082 NE 1998 12 24 ARWA981209 2 19981218 A 7530 LINE DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 3 BLEED VALVE LOOSE A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 19 661AV 45969 COMPRESSOR STALL NR 3 ENGINE, ABORTED TAKEOFF AT 90 KTS. FOUND LOOSE SENSE LINE AT SURGE BLEED VALVE. SECURED LINE AND OPS CHECKED NO LEAKS IAW MM 75-30-00. 2 L 7 4 4F 4 F 4A25 1E8 1998122400083 19981224 00083 EU 1998 12 24 MALA976267 1 19981216 A 2450 CIRCUIT BREAKERS SAAB SF340 340B 7860101 EU LEFT DAMP A MALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 15 590MA 340B181 ON STARTING OF NR 2 ENGINE, NOTICED SMOKE COMING LT CIRCUIT BREAKERS. MAINTENANCE FOUND EVIDENCE OF MOISTURE ON CIRCUIT BREAKER PANEL. CLEANED PANEL. NO CHAFING OF WIRES OR BURNS. NO SMOKE NOTED AT THIS TIME. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998122400084 19981224 00084 EU 1998 12 24 MALA976268 1 19981219 A 3097 660714246 WIRE HARNESS SAAB SF340 SF340A 7850100 EU PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 107XJ 340A107 LT PROP ICE CAUTION LIGHT ILLUMINATES AFTER 1:10 SEC. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED WIRE HARNESS. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1998122400085 19981224 00085 NM 1998 12 24 K3HA980150 1 19981211 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 361KP 20627 RIGHT CENTER BATTERY PACK INOP. REMOVED AND REPLACED RIGHT CENTER BATTERY PACK, REF 33-50-22. 2 L 7 3 4F A3WE 1998122400086 19981224 00086 NM 1998 12 24 AWXA9800236 1 19981129 A 2121 6457053 FAN BOEING 757 7572S7 1384962 NM LEFT FAILED A AWXA K NONE J WARNING INDICATION CR CRUISE 1 WP 28 902AW 15729 15729 23322 ENROUTE TO BOS LEFT RECIRC INOP LIGHT AND LEFT RECIRC FAN STATUS MESSAGE APPEARED. A SLIGHT ELECTRICAL ODOR WAS NOTED B UT NO SMOKE. SELECTED LEFT RECIRC FAN OFF AND PULLED LEFT RECIRC CB. ODOR DISAPPEARED. REMOVED AND REPLACED LEFT RECI RC FAN. OPS CHECK GOOD. 2 L 7 2 4F RT A2NM 1998122400087 19981224 00087 NM 1998 12 24 AWXA9800237 1 19981217 A 2720 65C3705312 PCU BOEING 737 737297 1384480 NM RUDDER LEAKS A AWXA B EMER. DESCENT K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 28 147AW 38876 31272 22630 INBOUND TO LAX, LOST 'B' SYSTEM HYDRAULIC FLUID. DECLARED EMERGENCY. REMOVED AND REPLACED RUDDER PCU FOR LEAKING. ADD ITIONAL INFORMATION TO FOLLOW, TO INCLUDE TEARDOWN REPORT. 2 L 7 2 4F A16WE 1998122400088 19981224 00088 NM 1998 12 24 RAAA98B1097 1 19981221 A 5330 SKIN BOEING 727 72722C 138400F NM BS 423-429.5 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 831RV 19093 DURING SERVICE CHECK, FOUND BS 423 TO 429.5 FUSELAGE SKIN DENTED AND GOUGED BEYOND LIMITS AT STR 24R. REPAIR CUTOUT DIM ENSIONS 6.5 IN BY 1.5 IN. ACCOMPLISHED TEMPORARY REPAIR PER SRM 53-30-3, FIG. 3, SHEET 2, 3 AND 4. BLIND FASTENER REPA IR REQUIRES REINPECT AT 43105 TAC AND REPLACED AT NEXT O/H BUT NO LATER THAN 50105 TAC M-54 NR 1. 2 L 7 3 4F A3WE 1998122400089 19981224 00089 WP 1998 12 24 CALA9802187 1 19981218 A 3350 60030451 POWER SUPPLY GRIMES DOUG DC9 DC932 3022066 WP ROW 16 INOP A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 12539 45792 INSPECTION FOUND CABIN OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE AT SEATS 16AC AND 16DEF. THE POWER SUPPLY WAS REPLACE D AND OPERATION CHECKED GOOD IAW MM 33-50-00, PAGE 501. 2 L 7 2 4F A6WE 1998122400090 19981224 00090 WP 1998 12 24 CALA9802188 1 19981218 A 3350 AD4002P BATTERY AEROQUALITY DOUG DC9 DC932 3022066 WP AFT LAVATORY DISCHARGED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12539 45792 INSPECTION FOUND TAILCONE EMERGENCY LIGHT AT RIGHT AFT LAV CEILING INOPERATIVE. THE BATTERY PACK WAS REPLACED AND OPERA TIONAL CHECKS WERE GOOD IAW MM 33-50-00, PAGE 501. 2 L 7 2 4F A6WE 1998122400091 19981224 00091 WP 1998 12 24 9810919963 1 19981212 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 913RW 47171 DURING LINE MAINTENANCE INSPECTION, FOUND FIRST CLASS EMERGENCY PATH LIGHTING INOPERATIVE. REPLACED BATTERY PACK. OPER ATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998122400092 19981224 00092 WP 1998 12 24 9810929993 1 19981212 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP GALLEY DOOR INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 983US 47282 DURING LINE MAINTENANCE INSPECTION, FOUND EMERGENCY LIGHTS INOPERATIVE IN FIRST CLASS SECTION AND AT GALLEY DOOR. REPLA CED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998122400093 19981224 00093 WP 1998 12 24 9810939964 1 19981216 A 3350 BATTERY PACK DOUG DC9 DC931 3022065 WP CATWALK DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHE CK NORMAL. 2 L 7 2 4F A6WE 1998122400094 19981224 00094 WP 1998 12 24 9810899920 1 19981217 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 83.5 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 942N 47459 DURING PERIODIC CHECK, FOUND EXTERNAL SKIN DOUBLER CRACKED BETWEEN FRAME AND DOUBLER AT FS 83.5. FABRICATED AND INSTALL ED NEW DOUBLER PER EA 99-158085. 2 L 7 2 4F A6WE 1998122400095 19981224 00095 WP 1998 12 24 9810909916 1 19981217 A 5711 SPAR CAP DOUG DC9 DC932 3022066 WP RT WING CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 949N 47566 DURING PERIODIC CHECK, FOUND RIGHT WING LOWER SPAR CAP WITH ONE INCH CRACK AT FS 353 BELOW LOWER OUTBOARD MOUNTING HOLE AT NR 4 HINGE FITTING. INSTALLED INTERIM REPAIR PER EA 99-159428. 2 L 7 2 4F A6WE 1998122400096 19981224 00096 SO 1998 12 24 COMA9810286 1 19981220 A 3350 KO201 RELAY EMB 120 EMB120RT SO CABIN MALFUNCTION A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 159A 120159 EMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED RELAY KO201. 2 L 7 2 4T RT A31SO 1998122400097 19981224 00097 EA 1998 12 24 COMA9860389 1 19981212 A 2750 601R93106503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA LT TE FLAP CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 7174 LEFT WING NR 5 FLEXSHAFT IS HEAVILY CORRODED. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998122400098 19981224 00098 EA 1998 12 24 COMA9860390 1 19981212 A 2750 601R93106503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 7174 RIGHT WING NR 5 FLAP FLEXSHAFT IS HEAVILY CORRODED. REMOVE AND REPLACE FLEXSHAFT. 2 L 7 2 4F RT A21EA 1998122400099 19981224 00099 EA 1998 12 24 COMA9860391 1 19981219 A 5210 1078461 SPRING CNDAIR CL600 CL6002B19 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 951CA 7091 CABIN DOOR OUTER HANDLE MESSAGE. REPLACED HANDLE TRIGGER SPRING. 2 L 7 2 4F RT A21EA 1998122400100 19981224 00100 EA 1998 12 24 COMA9860392 1 19981217 A 2421 755469D IDG CNDAIR CL600 CL6002B19 EA LEFT FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 01 710CA 1373 7241 LEFT AIRCRAFT GENERATOR FAILED DURING TAKEOFF. REPALCED THE LEFT IDG. 2 L 7 2 4F RT A21EA 1998122400101 19981224 00101 EA 1998 12 24 COMA9860393 1 19981220 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 959CA 7116 CABIN DOOR WARNING, COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1998122400102 19981224 00102 EA 1998 12 24 COMA9860394 1 19981217 A 2760 WARNING CNDAIR CL600 CL6002B19 EA SPOILERS ACTIVATED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 924CA 7026 FLIGHT SPOILER CAUTION MESSAGE DURING TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. SYSTEM TEST NORMAL. 2 L 7 2 4F RT A21EA 1998122400103 19981224 00103 EA 1998 12 24 COMA9860395 1 19981218 A 5330 601R35005 SKIN CNDAIR CL600 CL6002B19 EA BS 589-605 DENTED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 959CA 7116 DENT BELOW CARGO DOOR AREA BETWEEN FS 589 AND FS 605. DAMAGED AREA REMOVED AND REPAIRED IN ACCORDANCE WITH CRJ SRM 53-0 0-31. 2 L 7 2 4F RT A21EA 1998122400104 19981224 00104 NM 1998 12 24 UPS98228297 1 19981221 A 2751 TRANSMITTER BOEING 727 72731C 1384011 NM RT TE FLAP MALFUNCTIONED A IPXA K NONE F FLT CONT AFFECTED AP APPROACH 1 SO 01 925UP 19230 ON APPROACH SELECTED FLAPS, 2 INBD FLAPS REMAINED AT 0 USED ALT FLAP PROCEDURE PER AOM AND QRH FLAPS EXTENED DECLARED EM ERG AND MADE NORMAL LANDING. REMOVED AND REPLACED RT IB FLAP TRANSMITTER PER MM 27-52-02 OPS OK, P/N ON/OFF 2514-10 S/N ON1-4340 SN OFF NSN. 2 L 7 3 4F A3WE 1998122400105 19981224 00105 WP 1998 12 24 UPS98828299 1 19981219 A 3350 LIGHT DOUG DC8 DC871F 302199D WP CABIN MALFUNCTIONED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 701UP 45938 EEL ARM DISARM INOP. EEL OPS NORMAL PER MM33-50-01. NO DEFECTS NOTED. 2 L 7 4 4F RT 4A25 1998122400106 19981224 00106 WP 1998 12 24 UPS98828300 1 19981218 A 3350 BATTERY PACK DOUG DC8 DC871F 302199D WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 715UP 45915 EEL INOP. REPLACED EMERGENCY EXIT LIGHT BATT PACK PER MM 33-50-00. OPS CHK GOOD. 2 L 7 4 4F RT 4A25 1998122400107 19981224 00107 NM 1998 12 24 QXEA9802104 1 19981218 A 2611 A8251003 SMOKE DETECTOR DHAV DHC8 DHC8202 2809007 NM LAVATORY MALFUNCTION A QXEA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 353PH 2987 496 GEG- LAVATORY SMOKE DETECTOR WENT OFF FOR ABOUT 3 MINUTES AFTER TAKEOFF. NO SMOKE NOTED. MAINTENANCE REPLACED THE LAVA TORY SMOKE DETECTOR. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1998122400108 19981224 00108 WP 1998 12 24 ABXA9801186 1 19981217 A 2510 5641031501 SEAT DOUG DC8 DC861 3021952 WP COCKPIT WORN A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 841AX 45908 DURING TAKEOFF, FIRST OFFICER'S SEAT CAME UNLOCKED AND MOVED AFT. OCCURED AGAIN DURING FLIGHT. REPLACED FIRST OFFICER' S SEAT IAW DC8 MM. 2 L 7 4 4F 4A25 1998122400109 19981224 00109 NM 1998 12 24 DL76L982581 1 19981217 A 2560 Z51208386 LATCH BOEING 767 767332 1382001 NM LT EMER EXIT WORN A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 188DN 27583 LEFT OVERWING SLIDE DOOR WOULD NOT OPEN MANUALLY DURING ROUTINE LETTER CHECK MAINTANCE. FOUND MANUAL LINKAGE LOOSE AT T HE NR 3 DOOR LATCH. ATTACH POINT ON LATCH SLIDER WORN THROUGH. REPLACED NR 3 LATCH AND RECONNECTED LINKAGE. 2 L 7 2 4F RT A1NM 1998122400110 19981224 00110 NM 1998 12 24 DL757982583 1 19981218 A 3350 BATTERY BOEING 757 757232 1384965 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 671DN 25332 F/C EMERG SEAT TRACK LIGHTS INOP. REPLACED POWER SUPPLY FUSE AND BATTERY. CKS OK. 2 L 7 2 4F RT A2NM 1998122400111 19981224 00111 NM 1998 12 24 DL72K982584 1 19981218 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM CABIN INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 491DA 21060 EMERGENCY LIGHTS WOULD NOT TEST, TRIED RELAMP AND BATT, NO HELP. REPLACED LIGHT ASSY. 2 L 7 3 4F A3WE 1998122400112 19981224 00112 NM 1998 12 24 DL72W982587 1 19981219 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM LT EMER EXIT DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 293WA 22111 LEFT AFT EMERGENCY OVERWING LIGHT INOP IN CABIN. REPLACED BATTERY RACK M1090, CKS OK. 2 L 7 3 4F A3WE 1998122400113 19981224 00113 NM 1998 12 24 DL72W982589 1 19981215 A 5712 RIB BOEING 727 727247 138408F NM LT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 FOUND DURING MV2/F 1 LETTER CHECK, .75 INCH CRACK AT NR 3 SLAT NOSE RIB O/B SIDE OF ACTUATOR AFT LWR CORNER. REPAIRED P ER M/M 57-54-0. 2 L 7 3 4F A3WE 1998122400114 19981224 00114 NM 1998 12 24 DHL9872001D 1 19981106 A 5210 DOOR BOEING 727 727228 NM BS 1183 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT CABIN ENTRY DOOR HAS A CRACK UNDERNEATH RIVET HEAD 55 FROM BOTTOM OF DOOR FRAME BS 1183. CUT OUT DAMAG ED AREA, HFEC, INSTALLED REPAIR PER SRM 51-40-3, 7.5 BY 4.5 N/R 3626. 2 L 7 3 4F A3WE 1998122400115 19981224 00115 NM 1998 12 24 DHL9872002D 1 19981106 A 5347 SEAT TRACK BOEING 727 727228 NM BS 600-620 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, SEAT TRACK AT BS 600-620 LBL 48 HAS CRACKED FLANGE. REMOVED AND REPLACED SEAT TRACK FROM BA 560 TO 660 PER SRM 51-30-2, N/R 3661. 2 L 7 3 4F A3WE 1998122400116 19981224 00116 NM 1998 12 24 DHL9872003D 1 19981121 A 5311 FRAME BOEING 727 727228 NM BS 990 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, CRACKED FRAME STA 990 AT STR 26L, CRACK TERMINATED AT FASTENER HOL, VERIFIED BY HFEC. INSTALLED DOUBLER REP AIR PER SRM 53-10-4, 2 FT BY 7, N/R 3558. 2 L 7 3 4F A3WE 1998122400117 19981224 00117 NM 1998 12 24 DHL9872004D 1 19981105 A 5744 654130116 BRACKET BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT WING TRAILING EDGE FALSE SPAR VERTICAL ATTACH BRACKED FOR THE NR 5 FLAP TRACK IS CRACKED. REPLACED BRA CKET PER SRM 51-30-2 N/R 2891. 2 L 7 3 4F A3WE 1998122400118 19981224 00118 NM 1998 12 24 DHL9872005D 1 19981102 A 5312 BULKHEAD BOEING 727 727228 NM FWD PRESS BLKHD CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RADOME HOLD OPEN RODS STOWAGE BRACKETS ARE CRACKED. NDT, FOUND CRACKS UNDER CLIPS. CUT OUT CRACKED ARES ON FWD BULKHEAD, INSTALLED FLAT PRESSURE WEB REPAIR PER SRM 53-10-3 AT RBL 11 WL 232, 4.5 BY 6. INSTALLED WEB REPAIR AT L B 11 WL 233, 5.5 BY 5 PER SRM 53-10-5, N/R 3401. 2 L 7 3 4F A3WE 1998122400119 19981224 00119 NM 1998 12 24 DHL9872006D 1 19981101 A 5242 SKIN BOEING 727 727228 NM E & E BAY DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, E/E COMPT DOOR EXTERIOR SKIN SURFACE HAS CRACKS. REMOVED AND REPLACED DOOR SKIN PER SRM 51-30-2, 2 FT BY 2. 5, N/R 3409. 2 L 7 3 4F A3WE 1998122400120 19981224 00120 NM 1998 12 24 DHL9872007D 1 19981101 A 5242 SKIN BOEING 727 727228 NM E & E BAY DOOR BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, E/E DOOR SKIN IS BENT. REMOVED AND REPLACED SKIN PER N/R 3409, N/R 3410. 2 L 7 3 4F A3WE 1998122400121 19981224 00121 NM 1998 12 24 DHL9872008D 1 19981102 A 5330 SKIN BOEING 727 727228 NM BS 455 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RIVET HEAD POPPED, STRINGER 19R STA 455 EXTERIOR SKIN JUST UNDER INSTRUMENT COOLING DUCT. REMOVED FASTENERS FROM STA 440 TO 480. REMOVED SURFACE CORROSION AT INNER LAP SEAM STR 19R, WITHIN LIMITS. CUT OUT DAMAGED SKIN AREA, INSTALLED FUSELAGE EXTERNAL SKIN REPAIR PER SRM 53-30-3, 21 BY 9.25, FILLER 21 BY 7, N/R 3120. 2 L 7 3 4F A3WE 1998122400122 19981224 00122 NM 1998 12 24 DHL9872009D 1 19981103 A 5320 WEB BOEING 727 727228 NM BS 630 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, FWD CARGO LOWER SIDE WALL ATTACH WEB CRACKED AT STA 630 LBL 26. REPLACED WEB FLOOR SUPPORT AT FWD CARGO COM PT PER SRM 51-30-2, 18 BY 7, N/R 3477. 2 L 7 3 4F A3WE 1998122400123 19981224 00123 NM 1998 12 24 DHL9872010D 1 19981105 A 5320 CLIP BOEING 727 727228 NM BS 480 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, TIE CLIP TO SKIN CRACKED AT STA 480 ABOVE S-22 VIEWED FROM AFT SIDE. REPLACED CLIP PER SRM 51-30-2, 8 BY 4 N/R 3571. 2 L 7 3 4F A3WE 1998122400124 19981224 00124 NM 1998 12 24 DHL9872011D 1 19981105 A 5311 FRAME BOEING 727 727228 NM BS 560 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, 560 CIRCUMFERENTIAL, I/B FLANGE AND WEB DENTED BETWEEN S25L AND 24L. REWOKED DENT, HFEC, CRACKED IN TWO ARE AS. CUT OUT DAMAGED AREA. INSTALLED FRAME REPAIR PER SRM 53-10-4 BETWEEN S25L AND 24L, 8.5 BY 3, N/R 3576. 2 L 7 3 4F A3WE 1998122400125 19981224 00125 NM 1998 12 24 DHL9872012D 1 19981105 A 5311 FRAME BOEING 727 727228 NM BS 950 GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, GOUGE FOUND ON FUS FRAME STA 950 BETWEEN STA 26 AND 27L UPPER FLANGE AFT CARGO COMPT. REPLACED PREV REPAIR BETWEEN STR 26L AND 27 LT PER SRM 53-10-4, 1 BY 6 BY 10, N/R 3598. 2 L 7 3 4F A3WE 1998122400126 19981224 00126 NM 1998 12 24 DHL9872013D 1 19981106 A 5313 STRINGER BOEING 727 727228 NM BS 472 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, STRINGER 19R CORRODED AT STA 472 RT. REMOVED AND REINSTALLED NEW SECTION OF STRINGER FROM BS 440 TO 490 PER SRM 53-10-3, N/R 3606. 2 L 7 3 4F A3WE 1998122400127 19981224 00127 NM 1998 12 24 DHL9872014D 1 19981106 A 5210 FRAME BOEING 727 727228 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT ENTRY DOOR FRAME ON LEFT HAND WHERE PREVIOUS REPAIR. CUT OUT DAMAGED AREA, HFEC CUT OUT, INSTALLED DOUB LER REPAIR PER SRM 51-40-3, 9 BY 3.5 BY 1, N/R 3625. 2 L 7 3 4F A3WE 1998122400128 19981224 00128 NM 1998 12 24 DHL9872015D 1 19981105 A 7110 COWL BOEING 727 727228 NM NR 2 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 ENGINE RT AFT COWLING FWD LIP CHAFFED AT LOWER END FWD CORNER AND ABOVE RAIN GUTTER. CUT OUT DAMAGED S ECTION, INSTALLED REPAIR PER SRM 54-10-3 23.5 BY 2.5, N/R 6768. 2 L 7 3 4F A3WE 1998122400129 19981224 00129 NM 1998 12 24 DHL9872016D 1 19981110 A 3610 HEAT SHIELD BOEING 727 727228 NM NR 1 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 ENGINE PRECOOLER FWD HEAT SHIELD CRACKED AND MISSING LOWER I/B CORNER. INSTALLED DOUBLER REPAIR AT FWD CORNER PER SRM 51-40-2, 6 BY 4, N/R 6777. 2 L 7 3 4F A3WE 1998122400130 19981224 00130 NM 1998 12 24 DHL9872017D 1 19981110 A 5400 ANGLE BOEING 727 727228 NM NR 2 PYLON CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT SIDE OF NR 2 ENGINE PYLON LOOK THROUGH ACCESS PANEL 35201 ANGLE IS CORRODED AND CRACKED. REMOVED ANGLE, INSTALLED NEW ANGLE PER SRM 54-10-2, 12 LONG, N/R 6778. 2 L 7 3 4F A3WE 1998122400131 19981224 00131 NM 1998 12 24 DHL9872018D 1 19981118 A 7110 ANGLE BOEING 727 727228 NM NR 1 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 ENGINE LOWER COWLING O/B SECTION AFT OF 2ND 'U' BOLT CUT OUT ANGLE DAMAGED. REPLACED DAMAGED ANGLE PER SRM 51-40-3, 25 BY 4, N/R 6780. 2 L 7 3 4F A3WE 1998122400132 19981224 00132 NM 1998 12 24 DHL9872019D 1 19981114 A 5347 SEAT TRACK BOEING 727 727228 NM BS 950 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, SEAT TRACK CRACKED AT STA 950 RBL 24 INBD LEG. CUT OUT DAMAGE AND INSTALLED REPAIR FROM STA 910 TO 950 PER SRM 53-10-5, N/R 5864. 2 L 7 3 4F A3WE 1998122400133 19981224 00133 NM 1998 12 24 DHL9872020D 1 19981104 A 5347 SEAT TRACK BOEING 727 727228 NM BS 660 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, TRACK NR 1 LBL 60 AT STA 660 HAS ELONGATED HOLES AND MISSING FASTENERS. REMOVED FASTENERS AND CUT OUT DAMAG ED SECTION FROM 620 TO 660 PER SRM 53-10-5, N/R 5748. 2 L 7 3 4F A3WE 1998122400134 19981224 00134 NM 1998 12 24 DHL9872021D 1 19981104 A 7110 SKIN BOEING 727 727228 NM NR 2 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 ENGINE INLET RT SIDE, 3 O'CLOCK OF DOGHOUSE HAS CRACK IN SKIN BETWEEN 2 FASTENERS AT BS 1100. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 54-30-1, 6 BY 2, N/R 4642. 2 L 7 3 4F A3WE 1998122400135 19981224 00135 NM 1998 12 24 DHL9872022D 1 19981102 A 5330 SKIN BOEING 727 727228 NM BS 277 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NOSE AREA LEFT WALL STA 277 3 INCH BELOW CEILING CRACKED AT RIVET. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER S/B 53-145 20 BY 24, N/R 7566. 2 L 7 3 4F A3WE 1998122400136 19981224 00136 NM 1998 12 24 DHL9872023D 1 19981027 A 5753 FAIRING BOEING 727 727228 NM NR 4 TE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, LEFT WING NR 4 FLAP TRACK FAIRING L/E DAMAGED. REPLACED DAMAGED DOUBLER PER SRM 51-42-2, 2 BY 18, N/R 1770. 2 L 7 3 4F A3WE 1998122400137 19981224 00137 NM 1998 12 24 DHL9872024D 1 19981027 A 5753 FAIRING BOEING 727 727228 NM NR 4 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, L/W NR 4 FLAP TRACK FAIRING AFT ACCESS CUT EDGE WORN ON ONE EDGE GOUGED ON THE OTHER. REMOVED AND REPLACED ATTACH ANGLE PER SRM 53-50-1, 10 BY 1 BY .5, N/R 1771. 2 L 7 3 4F A3WE 1998122400138 19981224 00138 NM 1998 12 24 DHL9872025D 1 19981103 A 5754 RIB BOEING 727 727228 NM NR 4 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 4 L/E SLAT RIB NR 19 CRACKED. REMOVED AND REPLACED RIB PER SRM 57-50-2, N/R 1839. 2 L 7 3 4F A3WE 1998122400139 19981224 00139 NM 1998 12 24 DHL9872026D 1 19981103 A 5754 SKIN BOEING 727 727228 NM NR 1 LE FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 LE FLAP HAS CORNER BROKEN OFF. BURNISHED ROUGH EDGES, HFEC, FABRICATED DOUBLER AND FILLER, INSTALLED, PER SRM 51-10-1 AND AVITAS DRAWING, 98MST241D-1, N/R 1865. 2 L 7 3 4F A3WE 1998122400140 19981224 00140 NM 1998 12 24 DHL9872027D 1 19981103 A 5751 SKIN BOEING 727 727228 NM LT AILERON WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, L/W INBD AILERON PANEL 8310 OUTER SKIN SURFACE AHS SOME WORN AREAS. FABRICATED NEW PANEL PER SRM 57-50-2, 1 2.5 BY 9, .63 N/R 1887. 2 L 7 3 4F A3WE 1998122400141 19981224 00141 NM 1998 12 24 DHL9872028D 1 19981103 A 5754 SKIN BOEING 727 727228 NM NR 4 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, LEFT WING NR 4 L/E SLAT I/B AND O/B TRACK CUT OUTS CRACKED. CUT OUT DAMAGED AREA, INSTALLED DOUBLER AND FI LLER REPAIR 6 INCH BY 4 PER SRM 57-30-4, N/R 1892. 2 L 7 3 4F A3WE 1998122400142 19981224 00142 NM 1998 12 24 DHL9872029D 1 19981104 A 5754 SKIN BOEING 727 727228 NM NR 1 LE SLAT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 L/E FLAP HAS CORNER BROKEN OFF T/E OUTBD. BURNISHED EDGES, HFEC AND INSTALLED DOUBLER AND FILLER PER S RM 51-10-1 AND AVITAS ENGINEERING, 98MSI.241D-1, N/R 1921. 2 L 7 3 4F A3WE 1998122400143 19981224 00143 NM 1998 12 24 DHL9872030D 1 19981104 A 5720 66147352 ANGLE BOEING 727 727228 NM LT WING BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, L/W FALSE SPAR LOWER COVE PANEL HAS 2 EACH BROKEN SUPPORT ANGLE. REPLACED ANGLES PER SRM 51-30-02, N/R 1938 . 2 L 7 3 4F A3WE 1998122400144 19981224 00144 NM 1998 12 24 DHL9872031D 1 19981105 A 5753 BRACKET BOEING 727 727228 NM NR 4 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 4 FLAP TRACK BOTH OUTBD FAIRING ATTACH BRACKETS ARE CRACKED AT ATTACH FASTENERS. REMOVED AND REPLACED B RACKETS PER SRM 51-20-2, N/R 1981. 2 L 7 3 4F A3WE 1998122400145 19981224 00145 NM 1998 12 24 DHL9872032D 1 19981105 A 5753 BRACKET BOEING 727 727228 NM NR 4 FLAP TRACK CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 4 FLAP TRACK THE FWD INBD FAIRING ATTACH BRACKETS IS CRACKED AT ATTACH FASTENER. REMOVED AND REPLACED BR ACKETS PER SRM 51-30-2, N/R 1982. 2 L 7 3 4F A3WE 1998122400146 19981224 00146 NM 1998 12 24 DHL9872033D 1 19981102 A 5744 656524646501 FITTING BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT AILERON CENTER SUPPORT FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER MM 27-10-01, N/R 2830. 2 L 7 3 4F A3WE 1998122400147 19981224 00147 NM 1998 12 24 DHL9872034D 1 19981027 A 5753 65291505 TRACK BOEING 727 727228 NM NR 7 TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT C CHECK, NR 7 AFT FLAP TRACK FAIRING TRACK CRACKED AT FWD END LEFT SIDE. REMOVED AND REPLACED LEFT SIDE TRACK PER SR M 55-50-1, N/R 2769. 2 L 7 3 4F A3WE 1998122400148 19981224 00148 NM 1998 12 24 DHL9872035D 1 19981103 A 5730 SKIN BOEING 727 727228 NM RT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT WING NR 13 SPOILER ACTUATOR SUPPORT FITTING INBD HINGE WING CUT OUT IS CRACKED. REPLACED DAMAGED SECTION PER SRM 51-30-2, 16 BY 3, N/R 2865. 2 L 7 3 4F A3WE 1998122400149 19981224 00149 NM 1998 12 24 DHL9872036D 1 19981030 A 5330 SKIN BOEING 727 727228 NM BS 610 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, FUSELAGE EXTERIOR SKIN TRIPLER AT MAIN CARGO DOOR CUT OUT DENTED STA 610 BETWEEN STRINGERS 19L -20L. INSTAL LED EXTERNAL DOUBLER REPAIR PER SRM 53-30-3, 10 BY 8, N/R 3388. 2 L 7 3 4F A3WE 1998122400150 19981224 00150 NM 1998 12 24 DHL9872037D 1 19981109 A 5347 SEAT TRACK BOEING 727 727228 NM BS 800-825 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, SEAT TRACK RBL 24 HAS CORROSION AT LOWER SURFACE BETWEEN STA 825 AND 800. REPLACED SECTION OF SEAT TRACK PE R SRM 53-10-5, 8 FT LONG, N/R 5760. 2 L 7 3 4F A3WE 1998122400151 19981224 00151 NM 1998 12 24 DHL9872038D 1 19981104 A 5347 SEAT TRACK BOEING 727 727228 NM BS 640 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, SEAT TRACK NR 6 RBL 46 HAS CORROSION AT LOWER SURFACE STA 640. CUT OUT DAMAGED SECTION, INSTALLED NEW SEAT TRACK FROM STA 580 TO 650 PER SRM 53-10-5, N/R 5761. 2 L 7 3 4F A3WE 1998122400152 19981224 00152 NM 1998 12 24 DHL9872039D 1 19981104 A 5347 SEAT TRACK BOEING 727 727228 NM BS 1090-1130 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, SEAT TRACK NR 6 RBL 26 HAS CORROSION AT LOWER SURFACE. REMOVED SEAT TRACK AND INSTALLED NEW FROM STA 1090 TO 1130 PER SRM 53-10-5, N/R 5766. 2 L 7 3 4F A3WE 1998122400153 19981224 00153 NM 1998 12 24 DHL9872040D 1 19981104 A 5311 FRAME BOEING 727 727228 NM BS 420 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, INDICATION OF A CRACK AT MAIN CABIN LT SIDE CIRCUMFERENTIAL BS 420, 5 ABOVE FLOOR. FABRICATED AND INSTALLED CABIN FRAME REPAIR PER SRM 53-10-4, 11.5 BY 6.5, N/R 5772. 2 L 7 3 4F A3WE 1998122400154 19981224 00154 NM 1998 12 24 DHL9872041D 1 19981114 A 5330 SKIN BOEING 727 727228 NM BS 1360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 ENGINE LT STUB SURFACED SKIN HAS CRACKS AND BULGING AROUND FASTENERS APPROX BS 1360 STR 8L. REMOVED AN D INSTALLED NEW SKIN PER SRM 53-30-3, 2 FT BY 2 FT, N/R 4611. 2 L 7 3 4F A3WE 1998122400155 19981224 00155 NM 1998 12 24 DHL9872042D 1 19981104 A 7110 SKIN BOEING 727 727228 NM NR 2 ENGINE INLE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 ENG LT INLET DUCT HOUSING APPROX BS 1223 HAS CRACKS EMINATING FROM 2 EA FASTENERS. CUT OUT DAMAGED SKI N, INSTALLED SKIN REPAIR PER SRM 54-30-3, 8 BY 4, N/R 4614. 2 L 7 3 4F A3WE 1998122400156 19981224 00156 NM 1998 12 24 DHL9872043D 1 19981104 A 7110 SKIN BOEING 727 727228 NM NR 2 ENGINE INLE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 ENGINE INLET TOP OF DOGHOUSE HAS A LONG DENT AND A CRACK IN SKIN, BS 1140. CUT OUT DAMAGED AREA. INST ALLED SKIN REPAIR PER SRM 54-10-3 22.5 BY 15, N/R 4616. 2 L 7 3 4F A3WE 1998122400157 19981224 00157 NM 1998 12 24 DHL9872044D 1 19981104 A 5260 STEP BOEING 727 727228 NM AFT STAIRS CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT AIRSTAIRS, 2ND STEP FROM THE BOTTOM THE RISER PLATE IS CORRODED. REMOVED AND REPLACED NR 2 STEP RISER P ER SRM 51-10-1, 29 BY 10, N/R 4621. 2 L 7 3 4F A3WE 1998122400158 19981224 00158 NM 1998 12 24 DHL9872046D 1 19981104 A 5260 STEP BOEING 727 727228 NM AFT AIRSTAIRS CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT AIRSTAIRS 6TH STEP FROM THE BOTTOM, RISER CORRODED ALONG THE EDGES. REPLACED SKIN PER SRM 51-10-1, 29 B Y 10, N/R 4625. 2 L 7 3 4F A3WE 1998122400159 19981224 00159 NM 1998 12 24 DHL9872047D 1 19981104 A 5260 STEP BOEING 727 727228 NM AFT AIR STAIR CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT AIRSTAIRS 7TH FROM THE BOTTOM, RISER CORRODED AND SUPPORT ANGLE AT TOP OF RISER HAS SHEARED RIVET HEADS. REMOVED AND REPLACED SKIN ON RISER PER SRM 51-10-1, 29 BY 10, N/R 4626. 2 L 7 3 4F A3WE 1998122400160 19981224 00160 NM 1998 12 24 DHL9872048D 1 19981104 A 5260 STEP BOEING 727 727228 NM AFT AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT AIRSTAIRS, 8TH STEP FROM THE BOTTOM. RISER IS CRACKED AT CENTER PLATE. REMOVED AND REPLACED NR 8 RISER PER SRM 51-10-1, N/R 4627. 2 L 7 3 4F A3WE 1998122400161 19981224 00161 NM 1998 12 24 DHL9872049D 1 19981105 A 5753 SKIN BOEING 727 727228 NM RT TE FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT I/B SKIN FLAP DELAMINATED 54 FROM O/B END UPPER SURFACE. INSTALLED FIBERGLASS OVERLAY REPAIR PER SRM 51- 40-8, 6 BY 4, N/R 2884. 2 L 7 3 4F A3WE 1998122400162 19981224 00162 NM 1998 12 24 DHL9872050D 1 19981105 A 5753 SKIN BOEING 727 727228 NM RT TE FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT INBD FOREFLAP DELAMINATED 24 FROM INBD END ON UPPER SURFACE. INSTALLED FIBERGLASS REPAIR PER SRM 51-40- 8, 7 BY 6, N/R 2883. 2 L 7 3 4F A3WE 1998122400163 19981224 00163 NM 1998 12 24 DHL9872051D 1 19981107 A 5350 FAIRING BOEING 727 727228 NM RT WING/FUS DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, WING TO BODY FAIRING NR 3347 DELAMINATED. INSTALLED REPAIR PER SRM 51-40-8, 6 BY 5, N/R 3638. 2 L 7 3 4F A3WE 1998122400164 19981224 00164 NM 1998 12 24 DHL9872052D 1 19981107 A 5330 PANEL BOEING 727 727228 NM FUSELAGE TORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, FUS ACCESS PANEL NR 3442 AFT END HOLE TORN OUT. REPAIRED DAMAGED SECTION PER SRM 51-40-3, 1 BY 1 BY 6, N/R 3637. 2 L 7 3 4F A3WE 1998122400165 19981224 00165 NM 1998 12 24 DHL9872053D 1 19981107 A 5330 PANEL BOEING 727 727228 NM FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, FUSELAGE FILLET PANEL 3618 CRACKED AND DELAMINATED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 4 BY 6, N/R 3 636. 2 L 7 3 4F A3WE 1998122400166 19981224 00166 NM 1998 12 24 DHL9872054D 1 19981107 A 5330 PANEL BOEING 727 727228 NM FUESLAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, FUS PANEL 3421 DELAMINATED. INSTALLED BONDING REPAIR PER SRM 51-20-3, N/R 3632. 2 L 7 3 4F A3WE 1998122400167 19981224 00167 NM 1998 12 24 DHL9872055D 1 19981102 A 5730 PANEL BOEING 727 727228 NM RT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RIGHT WING ELEPHANT EAR CAVITY PANEL AREA 3611, UPPER FIBERGLASS EDGE BROKEN OFF IN TWO PLACES. INSTALLED O VERLAY REPAIR PER SRM 51-40-8, 50 BY 6, N/R 3448. 2 L 7 3 4F A3WE 1998122400168 19981224 00168 NM 1998 12 24 DHL9872056D 1 19981030 A 5510 TIP BOEING 727 727228 NM HORIZONTAL STAB CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT HORIZ STAB TIP ERODED AND CRACKED. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 3 BY 6 N/R 4510. 2 L 7 3 4F A3WE 1998122400169 19981224 00169 NM 1998 12 24 DHL9872057D 1 19981119 A 5341 69162052 FITTING BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RIGHT WING ATTACH FITTING AT STA 950 RBL 56 STR 18 A IS CORRODED. REMOVED AND REPLACED FITTING PER SRM 51-3 0-2, N/R 7696. 2 L 7 3 4F A3WE 1998122400170 19981224 00170 NM 1998 12 24 DHL9872058D 1 19981110 A 5730 PANEL BOEING 727 727228 NM LT WING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, LT UPPER WING PANEL 8155 IS CRACKED, WORN AND DELAMINATED. REPLACED METAL STRIP ON WING PANEL PER SRM 51-30 -2, 1.5 BY 22, N/R 1376. 2 L 7 3 4F A3WE 1998122400171 19981224 00171 NM 1998 12 24 DHL9872059D 1 19981116 A 5754 RIB BOEING 727 727228 NM NR 4 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, LEFT WING NR 4 L/E SLAT RIB MARKED NR 11 CRACKED. REPLACED RIB PER SRM 57-50-2, N/R 1979. 2 L 7 3 4F A3WE 1998122400172 19981224 00172 NM 1998 12 24 DHL9872060D 1 19981119 A 5711 SPAR BOEING 727 727228 NM LT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 4 SLAT WHERE NR 12 RIB FROM O/B END ATTACHED TO SPAR WEB HOLES ARE LARGE AND ELONGATED. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-30-3, 7 BY 4, N/R 1958. 2 L 7 3 4F A3WE 1998122400173 19981224 00173 NM 1998 12 24 DHL9872061D 1 19981127 A 5753 FLAP BOEING 727 727228 NM LT TE MID FLAP DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, LEFT I/B MID FLAP DAMAGED AT I/B AFT END. INSTALLED F/G OVERLAY PER SRM 51-40-8, 5 BY 8 N/R 1084. 2 L 7 3 4F A3WE 1998122400174 19981224 00174 NM 1998 12 24 DHL9872062D 1 19981101 A 5280 ANGLE BOEING 727 727228 NM RT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RMLG STRUT DOOR CRACKED ANGLE O/B OF DOOR GUIDE ROLLERS, FWD LOWER SURFACE. REPLACED CRACKED Z ANGLE PER SR M 51-30-2, 4 BY 15, N/R 7547. 2 L 7 3 4F A3WE 1998122400175 19981224 00175 NM 1998 12 24 DHL9872063D 1 19981030 A 7110 COWL BOEING 727 727228 NM NR 1 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 ENG FWD FIXED COWL DAMAGED TOP EDGE. TRIMMED OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 54-20- 1, 6 BY 2, N/R 6619. 2 L 7 3 4F A3WE 1998122400176 19981224 00176 NM 1998 12 24 DHL9872064D 1 19981104 A 7110 RIB BOEING 727 727228 NM NR 3 ENGINE COWL CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 3 ENG LOWER COWL RIB NR 2 CHAFED. INSTALLED FRAME REPAIR PER SRM 54-10-3, 2.5 BY 6, N/R 6706. 2 L 7 3 4F A3WE 1998122400177 19981224 00177 NM 1998 12 24 DHL9872065D 1 19981104 A 7110 RIB BOEING 727 727228 NM NR 3 ENGINE COWL CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 3 ENG LOWER COWL RIB NR 5 AT REPAIR, HOLE CHAFFED THROUGH. REPLACED CHAFFED SECTION PER SRM 54-10-3, 8 B Y 3.5, N/R 6797. 2 L 7 3 4F A3WE 1998122400178 19981224 00178 NM 1998 12 24 DHL9872066D 1 19981104 A 7110 COVER BOEING 727 727228 NM NR 3 ENGINE COWL CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 3 ENG UPPER COWL INSIDE HOLE CHAFFED THROUGH ON 'U' BOLT COVER AFT END OF COWL. REPLACED COVER PER SRM 5 1-40-3, 6 BY 5, N/R 6798. 2 L 7 3 4F A3WE 1998122400179 19981224 00179 NM 1998 12 24 DHL9872067D 1 19981105 A 7110 SKIN BOEING 727 727228 NM NR 1 ENGINE COWL CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 ENG AFT SEC OF FIXED COWL LOWER. REMOVABLE SECTION AND CHAFFED THROUGH. REPLACED DAMAGED SECTION PER SRM 51-40-3, 17.75 BY 5, N/R 6719. 2 L 7 3 4F A3WE 1998122400180 19981224 00180 NM 1998 12 24 DHL9872068D 1 19981105 A 5330 SKIN BOEING 727 727228 NM BS 1342 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT SIDE STA 1392 STR 10R, SKIN BULGED BETWEEN RIVETS. CUT OUT DAMAGED SECTION, INSTALLED DOUBLER REPAIR PER SRM 53-30-3, 12 BY 10, N/R 6728. 2 L 7 3 4F A3WE 1998122400181 19981224 00181 NM 1998 12 24 DHL9872069D 1 19981105 A 7110 SKIN BOEING 727 727228 NM NR 1 ENGINE COWL CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 ENG LOWER COWL BETWEEN RIB 4-5 CHAFFED. CUT OUT DAMAGED AREA, INSTALLED DOUBLER PER SRM 54-10-3, 7.5 BY 5.5, N/R 6734. 2 L 7 3 4F A3WE 1998122400182 19981224 00182 NM 1998 12 24 DHL9872070D 1 19981105 A 7110 SKIN BOEING 727 727228 NM NR 2 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 FWD LT ENGINE COWL HAS PREVIOUS REPAIR. CUT OUT DAMAGED SKIN, INSTALLED DOUBLER REPAIR PER SRM 54-10-3 , 8 BY 10, N/R 6738. 2 L 7 3 4F A3WE 1998122400183 19981224 00183 NM 1998 12 24 DHL9872071D 1 19981105 A 7110 SKIN BOEING 727 727228 NM NR 1 ENGINE COWL DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 1 ENG TOP COWL DENT IN SKIN BETWEEN RIB 5/6. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR PER SRM 54-10-3, 6 BY 7, N/R 6747. 2 L 7 3 4F A3WE 1998122400184 19981224 00184 NM 1998 12 24 DHL9872072D 1 19981105 A 7110 SKIN BOEING 727 727228 NM NR 2 ENGINE COWL CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 FWD ENGINE COWL LOWER FWD CORNER CRACKED AND DENTED. REMOVED AND FABRICATED NEW CORNER AND INSTALLED P ER SRM 54-10-3, 16 BY 2.5, N/R 6741. 2 L 7 3 4F A3WE 1998122400185 19981224 00185 NM 1998 12 24 DHL9872073D 1 19981105 A 7110 RIB BOEING 727 727228 NM NR 2 ENGINE COWL DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 2 ENG RT AFT COWLING LOWER AFT CORNER WORN, CRACKED AND RIVET HEAD PULLING THROUGH. ROUTED OUT DAMAGE O N RIB PER SRM 51-10-1. INSTALLED RIB REPAIR PER SRM 54-10-3, 6.5 BY 5 AND REPLACED DAMAGED ANGLE PER SRM 51-40-3, 7 BY 6, N/R 6766. 2 L 7 3 4F A3WE 1998122400186 19981224 00186 NM 1998 12 24 DHL9872074D 1 19981103 A 5754 RIB BOEING 727 727228 NM NR 3 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, L/W NR 3 L/E SLAT RIBS NR 1, 16, 19 ARE CRACKED. REMOVED AND REPLACED RIBS PER SRM 57-50-2 . 2 L 7 3 4F A3WE 1998122400187 19981224 00187 NM 1998 12 24 DHL9872075D 1 19981102 A 5260 652665118 FITTING BOEING 727 727228 NM AFT AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT AIRSTAIR LT LOWER STRUT ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING PER M/M 52-62-0, N/R 3415. 2 L 7 3 4F A3WE 1998122400188 19981224 00188 NM 1998 12 24 DHL9872076D 1 19981107 A 5260 652665118 FITTING BOEING 727 727228 NM AFT AIRSTAIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT AIRSTAIR RT LOWER STRUT ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING PER MM 52-62-01, N/R 3416 . 2 L 7 3 4F A3WE 1998122400189 19981224 00189 NM 1998 12 24 DHL9872077D 1 19981105 A 5311 FRAME BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, CORROSION ON FUSE FRAME LOWER FLANGE STA 950B, STR 29L AT AFT CARGO COMP. CUT OUT DAMAGED AREA , INSTALLED REPAIR PER SRM 53-10-4, 1 BY 3 BY 8, N/R 3690. 2 L 7 3 4F A3WE 1998122400190 19981224 00190 NM 1998 12 24 DHL9872078D 1 19981105 A 5311 FRAME BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, CORROSION ON FUS FRAME LOWER FLANGE 950B STR 29 RT. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 53-10-4, 8 BY 5, N/R 3601. 2 L 7 3 4F A3WE 1998122400191 19981224 00191 NM 1998 12 24 DHL9872079D 1 19981105 A 5311 FRAME BOEING 727 727228 NM BS 1148 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT CARGO COMPT REAR DOOR CUT OUT AFT FRAME VERTICAL COVER IS DAMAGED ON LOWER I/B SIDE STA 1148 ABOVE STR 26 RT. REMOVED DAMAGED AREA , INSTALLED DOUBLER PER SRM 53-10-4, 3 BY 6, N/R 3602. 2 L 7 3 4F A3WE 1998122400192 19981224 00192 NM 1998 12 24 DHL9872080D 1 19981105 A 5320 STIFFENER BOEING 727 727228 NM BS 360 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, E/E COMPT BS 360 FWD LEFT FACE OF DOPPLER RADAR IS CORRODED ON TWO STIFFENERS. REPLACED STIFFENERS PER SRM 51-30-2, N/R 3612. 2 L 7 3 4F A3WE 1998122400193 19981224 00193 NM 1998 12 24 DHL9872081D 1 19981111 A 5330 SKIN BOEING 727 727228 NM BS 950 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, PREVIOUS REPAIR AT STA 950D TO 950E STR 25 RT TO STR 26 RT FOR SRM COMPLIANCE. REMOVED AND INSTALLED DOUBLE R REPAIR PER AVITAS EO 98PMSI241D-5, 15 BY 16.5, N/R 3662. 2 L 7 3 4F A3WE 1998122400194 19981224 00194 NM 1998 12 24 DHL9872082D 1 19981113 A 5245 65266872 DOOR BOEING 727 727228 NM RT RAM AIR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT RAM AIR DOOR IS CRACKED AT BOTTOM FLANGE. REPALCED DOOR PER MM 21-56-1, N/R 3666. 2 L 7 3 4F A3WE 1998122400195 19981224 00195 NM 1998 12 24 DHL9872083D 1 19981113 A 5315 FLOORBEAM BOEING 727 727228 NM BS 1070 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, FLOORBEAM CORRODED TOP AND BOTTOM SIDES OF UPPER FLANGE FS 1070 RBL 65. CUT OUT DAMGAGED AREA. INSTALLED R EPAIR PER SRM 53-10-8, 2 BY 30, N/R 3668. 2 L 7 3 4F A3WE 1998122400196 19981224 00196 NM 1998 12 24 DHL9872084D 1 19981113 A 5311 FRAME BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, REAR CARGO FRAME CORRODED AT STA 950C AT STR 26R. INSTALLED REPAIR PER SRM 53-10-4, 8 BY 5, N/R 3667. 2 L 7 3 4F A3WE 1998122400197 19981224 00197 NM 1998 12 24 DHL9872085D 1 19981116 A 5320 INTERCOSTAL BOEING 727 727228 NM BS 950 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, CORROSION ON INTERCOSTAL BETWEEN STA 950 A TO STA 950B, STR 28 LT AFT CARGO COMPT. INSTALLED ANGLE REPAIR P ER SRM 51-40-2, 6 BY 4, N/R 3673. 2 L 7 3 4F A3WE 1998122400198 19981224 00198 NM 1998 12 24 DHL9872086D 1 19981117 A 5320 ANGLE BOEING 727 727228 NM BS 720 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, ANGLE CRACKED AT BS 720F STRINGER 28R TO 28L APPROX EXTERIOR SKIN A/C BAY. REMOVED AND REPLACED ANGLE PER SRM 51-40-3, 1 FT BY 1 BY 20, N/R 3676. 2 L 7 3 4F A3WE 1998122400199 19981224 00199 NM 1998 12 24 DHL9872087D 1 19981117 A 5320 CLIP BOEING 727 727228 NM BS 970 CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT CARGO COMP STA 970 STR 27L AND TIE CLIP CORRODED. REMOVED DAMAGED STRINGER, INSTALLED DOUBLER REPAIR PE R SRM 53-10-3 28, N/R 3678. 2 L 7 3 4F A3WE 1998122400200 19981224 00200 NM 1998 12 24 DHL9872088D 1 19981124 A 5210 SKIN BOEING 727 727228 NM PAX DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, FWD ENTRY DOOR HAS SEVERAL BROKEN RIVETS AND SKIN CRACK AT FASTENER HOLE. CUT OUT CRACKED SECTION, HFEC, I NSTALLED REPAIR DOUBLER PER SRM 52-00-3, 9 BY 6, N/R 3691. 2 L 7 3 4F A3WE 1998122400201 19981224 00201 NM 1998 12 24 DHL9872089D 1 19981030 A 2761 659892440 FITTING BOEING 727 727228 NM NR 12 SPOILER AC CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, NR 12 SPOILER ACTUATOR SUPPORT CRACKED. REPLACED ANGLES AT REAR SPAR FOR ACTUATOR BRACKETS PER S/B 57-84, N /R 2798. 2 L 7 3 4F A3WE 1998122400202 19981224 00202 NM 1998 12 24 DHL9872090D 1 19981103 A 5755 SKIN BOEING 727 727228 NM NR 11 SPOILER CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT WING NR 11 SPOILER ACTUATOR SUPPORT FITTING, INBD HINGE WING CUT OUT IS CRACKED. CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR PER SRM 57-30-4, 6 BY 3, N/R 2864. 2 L 7 3 4F A3WE 1998122400203 19981224 00203 NM 1998 12 24 DHL9872091D 1 19981104 A 5753 6529625 CASTING BOEING 727 727228 NM RT OUTBD FORE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT OUTBD FOREFLAP CASTING CRACKED AT INBD END. REMOVED AND REPLACED CASTING PER SRM 57-50-1, N/R 2878. 2 L 7 3 4F A3WE 1998122400204 19981224 00204 NM 1998 12 24 DHL9872092D 1 19981109 A 5753 6529625 CASTING BOEING 727 727228 NM RT TE FOREFLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT O/B FOREFLAP I/B END CASTING CRACKED AT FWD L/E RADIUS. REMOVED AND REPLACED CRACKED CASTING PER SRM 57- 50-1, N/R 2893. 2 L 7 3 4F A3WE 1998122400205 19981224 00205 NM 1998 12 24 DHL9872093D 1 19981117 A 5711 FRAME BOEING 727 727228 NM BS 915 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RIGHT WHEEL WELL AFT OF UPLOCK FITTING BS 915 CRACKED FRAME 12 BELOW PRESSURE FLOOR. STOP DRILLED, HFEC, IN STALLED ANGLE PER SRM 57-40-3, 4 BY 8, N/R 2916. 2 L 7 3 4F A3WE 1998122400206 19981224 00206 NM 1998 12 24 DHL9872094D 1 19981120 A 5311 FRAME BOEING 727 727228 NM BS 930 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT WHEEL WELL FUSELAGE FRAME CRACKED JUST BELOW PRESSURE DECK BS 930. REMOVED AND REPLACED CORRODED L ANGLE . FABRICATED NEW FRAME PER BOEING DRAWING 65-16336. INSTALLED REPAIR AT PREVIOUS REPAIR PER BOEING DRAWING. INSTALLED FRAME REPAIR AT STA 920 PER SRM 53-10-4, 12 BY 1. INSTALLED STRINGER REPAIRS AT STRINGER 16 AND 16 LT AT STA 920 PER S RM 53-10-03. INSTALLED EXTRUDED SECTION REPAIR AT STR 14 STA 920 PER SRM 51-40-4 . 2 L 7 3 4F A3WE 1998122400207 19981224 00207 NM 1998 12 24 DHL9872095D 1 19981103 A 5754 6518727611 RIB BOEING 727 727228 NM NR 4 LE SLAT CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, L/W NR 4 L/E SLAT RIBS 12, 19, 21 CRACKED. REMOVED AND REPLACED L/E SLAT RIBS PER SRM 57-30-2. REPLACED NR 12 SLAT RIB PER SRM 57-50-2, N/R 1891. 2 L 7 3 4F A3WE 1998122400208 19981224 00208 NM 1998 12 24 DHL9872096D 1 19981105 A 5753 SKIN BOEING 727 727228 NM RT TE FOREFLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT O/B FOREFLAP DELAMINATED AT UPPER SURFACE MID SECTION. INSTALLED OVERLAY REPAIR PER SRM 51-40-8, 14 BY 9, NR 2886. 2 L 7 3 4F A3WE 1998122400209 19981224 00209 NM 1998 12 24 DHL9872097D 1 19981105 A 5753 SKIN BOEING 727 727228 NM RT TE FOREFLAP GOUGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, RT O/B FOREFLAP L/E LOWER SURFACE GOUGED 4 O/B OF CENTER TRACK LINK ARM. INSTALLED FILLER REPAIR PER SRM 51 -40-1, 30 BY 21, N/R 2885. 2 L 7 3 4F A3WE 1998122400210 19981224 00210 NM 1998 12 24 P5CA9801623 1 19981215 A 5313 STRINGER BOEING 747 747123 1384873 NM BS 1618 BROKEN A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 858FT 20109 DURING HIGH WINDS AIRCRAFT BOUNCED OFF TAIL JACK AND A HOLE WAS PUNCTURED IN THE OUTER SKIN OF BS1618. REPAIRED FUSELAG E SKIN IAW BACO SRM 53-30-03. REPAIRED STRINGER 49 AND 50 AT STA 1618 PER BACO SRM 53-10-03. 2 L 7 4 4F A20WE 1998122400211 19981224 00211 WP 1998 12 24 ARWA981212 1 19981219 A 2425 WARNING LIGHT DOUG DC8 DC862 3021970 WP GEN OVERLOAD ILLUMINATED A ARWA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 791AL 46150 ON TAXI, GENERATOR OVERLOAD LIGHT ILLUMINATED. ACCOMPLISHED OK LIST, LIGHT REMAINDED ON. AIRCRAFT RETURNED TO BLOCKS T RANSFERED TO DMI 9537 IAW MEL-24-24-CAT D. 2 L 7 4 4F 4A25 1998122400212 19981224 00212 WP 1998 12 24 ARWA981211 1 19981219 A 3030 8J1CU1 PITOT TUBE DOUG DC8 DC862 3021970 WP FUSELAGE INOP A ARWA O OTHER O OTHER IN INSP/MAINT 1 SO 19 802BN 45909 F/O PITOT HEAT INOP. REMOVED AND REPLACED CURRENT DETECTOR IAW DC-8 M/M 30-30-0. NO HELP. REMOVED AND REPLACED F/O PI TOT TUBE IAW DC-8 M/M 30-30-0. PERFORMED PITOT STATIC LEAK CHECK IAW DC-8 M/M 34-12-0. OPERATION NORMAL. 2 L 7 4 4F 4A25 1998122400213 19981224 00213 NM 1998 12 24 VNAA9812009 1 19981216 A 5242 001A524D0068200 SEAL DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E & E DOOR LOOSE A VNAA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 GL 07 328LS 3025 SQUEALING NOISES FROM THE AREA OF THE COMMUNICATION DOOR WERE NOTED BY THE CREW AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED FOR INSPECTION. MAINTENANCE INSPECTED AND RE-SECURED THE COMMUNICATION DOOR SEAL, IN ACCORDANCE W ITH DORNIER MAINTENANCE MANUAL 53-00-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998122400214 19981224 00214 NE 1998 12 24 TC8A98086 2 19981218 A 7230 COMPRESSOR DOUG DC8 DC8F55 3021928 WP PWA JT3D JT3D3B 52039 NE NR 4 ENGINE STALLED A TC8A C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 23 182SK 45817 642684 ON TAKEOFF RW 29, NR 4 ENGINE ERRONEOUS EPR INDICATION, ALL OTHER INDICATIONS NORMAL. COMPRESSOR STALL AT APPROX 60 KTS , ABORTED TAKEOFF. TAXIED TO RW 11, TAKEOFF NORMAL, SET NR 4 ENGINE POWER BY N1, WIND 110, 4 KTS. INSPECTED NR 4 ENGINE BLADES PER PW MM 72-0, NO DEFECTS NOTED. CLEANED AND LUBRICATED NR 4 ENGINE PRBC PER MD MM 75-30-3. PERFORMED ENGINE RUN UP AND COULD NOT REPEAT STALLS. NR 4 ENGINE EPR INDICATION DEFERRED AS PER MEL 77-1, TRANSFERRED TO DMI 8943. 2 L 7 4 4F 4 F 4A25 1E8 1998122400215 19981224 00215 NM 1998 12 24 AALA981769 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 625 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON UPPER SPAR CHORD ABOVE NR 2 L/E SLAT ACTUATOR ALSO ON SKIN. INSTALLED REPAIR ANGLE PER ESO 116 97, DATED 9/8/98. (M) 2 L 7 3 4F A3WE 1998122400216 19981224 00216 NM 1998 12 24 AALA981768 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 720 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 720 BELT FRAME BENT AT STRINGER 23R TO 25R. INSTALLED DOUBLER PER AARD 53-10-07-3. FABRICATED DOUBLER FR OM 7075-T6- .050 INCH MATERIAL, DAMAGE CUT OUT. (M) 2 L 7 3 4F A3WE 1998122400217 19981224 00217 NM 1998 12 24 AALA981767 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 680 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 680 FRAME BENT AT STRINGER 27R TO 24R. INSTALLED DOUBLER REPAIR, IAW SRM 53-10-4. INSTALLED .063 DOUBLER WITH .1875 FASTENERS 4 ON SIDE OF DAMAGE. (M) 2 L 7 3 4F A3WE 1998122400218 19981224 00218 NM 1998 12 24 AALA981766 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 720 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FRAME BENT AT STRINGER 24L. INSTALLED DOUBLER REPAIR IAW SRM 53-10-4. INSTALLED .063 DOUBLER WITH .1875 FASTENER S 4 ON EACH SIDE OF DOUBLER. (M) 2 L 7 3 4F A3WE 1998122400219 19981224 00219 NM 1998 12 24 AALA981765 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 660 FRAME DENTED AT STRINGER 22L TO 23L. REMOVED DAMAGED AREA OF BELT FRAME INSTALLED A .063 INCH MATERIA L DOUBLER WITH 4 ROWS OF FASTENERS TO EACH SIDE OF CUT OUT PER SRM 53-10-4 PAGE 3-6. (M) 2 L 7 3 4F A3WE 1998122400220 19981224 00220 NM 1998 12 24 AALA981764 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 660 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 660 FRAME BENT FROM STRINGER 22R AND 24R, TOP LEG. INSTALLED DOUBLER, .050 INCH MATERIAL WITH 4 ROWS OF . 1875 INCH FASTENERS PER AARD. (M) 2 L 7 3 4F A3WE 1998122400221 19981224 00221 NM 1998 12 24 AALA981763 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FRAME BENT AT STRINGER 24L-25L, STATION 500. INSTALLED DOUBLER, REPAIR AT STATION 500, STRINGER 24L-25L PER AARD 53-10-7-3, .050 DOUBLER MATERIAL, 7075-T6. (M) 2 L 7 3 4F A3WE 1998122400222 19981224 00222 NM 1998 12 24 AALA981762 1 19980903 A 5531 RIB BOEING 727 727227 1384078 NM VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER NR 3 CRACKED RIGHT SIDE OF VERTICAL 1ST RIB BELOW ACCESS PANEL VERT INTERIOR. STOP DRILLED CRACK A ND INSTALLED REPAIR PER SRM 55-30-4, PAGE 6 FIG 1. (M) 2 L 7 3 4F A3WE 1998122400223 19981224 00223 NM 1998 12 24 AALA981761 1 19980903 A 5531 RIB BOEING 727 727227 1384078 NM VERTICAL STAB CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STRINGER NR 1 CRACKED RIGHT SIDE OF VERTICAL, FIRST RIB BELOW ACCESS INTERIOR OF VERTICAL. STOP DRILLED CRACK AND INSTALLED REPAIR PER SRM 55-30-4, PAGE 5 FIG 1. (M) 2 L 7 3 4F A3WE 1998122400224 19981224 00224 NM 1998 12 24 AALA981760 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 680/720 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FRAME BENT STATION 680 AT STRINGER 22L TO 25L, FRAME BENT STATION 720A AT STRINGER 24L. REMOVED DAMAGE AREA FROM FRAME INSTALLED .063 DOUBLER. INSTALLED .1875 RIVETS, NINE .25 INCH FASTENERS, FOUR ON EACH SIDE OF DAMAGE PER SRM 53-1 0-4. (M) 2 L 7 3 4F A3WE 1998122400225 19981224 00225 NM 1998 12 24 AALA981759 1 19980903 A 5311 FRAME BOEING 727 727227 1384078 NM BS 520 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 520 FRAME BENT STRINGER 23R TO 25R. CUT OUT DAMAGED AREA. INSTALLED DOUBLER REPAIR PER SRM 53-10-0 4. (M) 2 L 7 3 4F A3WE 1998122400226 19981224 00226 NM 1998 12 24 AALA981840 1 19981002 A 5720 STIFFENER BOEING 727 727227 1384078 NM WS 248 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON TOP OF VERTICAL STIFFENER ON FORWARD SPAR AT APPROX WS 248. INSTALLED NEW VERTICAL STIFFENER O N FORWARD SPAR AT APPROX WS 248. (M) 2 L 7 3 4F A3WE 1998122400227 19981224 00227 NM 1998 12 24 AALA981847 1 19981002 A 5330 SKIN BOEING 727 727227 1384078 NM BS 870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ON FUSELAGE SKIN STATION 870, STRINGER 8-9R. REPAIRED FUSELAGE SKIN PER ESO 11697, DATED 9/16/98, SKIN AND FRAME REPAIR BS 870 AT STRINGER 8 TO 10 RT. (M) 2 L 7 3 4F A3WE 1998122400228 19981224 00228 NM 1998 12 24 AALA981846 1 19981002 A 5730 SKIN BOEING 727 727227 1384078 NM WS 232-266 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND WING LEADING EDGE SKIN HAS CORROSION AROUND SCREWS FORWARD OF SPAR CHORD ON TOP OF WING 4 INCHES OUTBOARD OF BUT SPLICE TO 26 INCHES OUTBOARD. CUT OUT DAMAGED SKIN. INSTALLED DOUBLER AND FILLER PER 57-30-4 FIG 6. (M) 2 L 7 3 4F A3WE 1998122400229 19981224 00229 EU 1998 12 24 VTZA98330 1 19981103 A 3097 WIRE JETAIR JETSTM JETSTM4101 1500501 EU LT PROPELLER FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 324UE 41017 FLT 6286 - IAD-CMH - DURING CRUISE, EXPERIENCED A DISCREPANCY WITH THE LEFT PROP DEICE SYSTEM INDICATING INOPERATIVE. M AINTENANCE CONTROL WAS NOTIFIED AND THE AIRCRAFT RETURNED TO IAD WHERE MAINTENANCE TROUBLESHOT. REMOVED AND REPLACED TH E PROP DEICE LEADS ON THE LEFT PROP IAW APPLICABLE MAINTENANCE PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MAINTENANCE MANUAL. AIRCRAFT WS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1998122400230 19981224 00230 EA 1998 12 24 VTZA98329 1 19981103 A 3030 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA COCKPIT ILLUMINATED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 625BR 7214 FLT 6636 - ORD-CRW - DURING TAKEOFF, EXPERIENCED A RIGHT AOA PROBE HEAT FAIL AND TAT HEAT FAIL INDICATION ON THE MASTER CAUTION PANEL. AIRCRAFT CONTACTED MAINTENANCE CONTROL AND DISPATCH, DECISION TO RETURN TO ORD WAS MADE. UPON ARRIVAL A T ORD, THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT MAINTENANCE WAS DISP ATCHED. MAINTENANCE TROUBLESHOT THE SYSTEM, PERFORMED SYSTEM RESET CHECKS, CONDUCTED TAT PROBE AND AOA OPS CHECKS BUT C OULD NOT DUPLICATE DISCREPANCY. AIRCRAFT DISCREPANCY WAS CLOSED AND AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 1998122400231 19981224 00231 EA 1998 12 24 VTZA98328 1 19981103 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 EA TE FLAPS ILLUMINATED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 622BR 7187 FLT 6703 - BNA-IAD - DURING TAKEOFF, EXPERIENCED A FLAP FAIL MESSAGE LIGHT ON THE MASTER CAUTION PANEL. AIRCRAFT CONTAC TED MAINTENANCE CONTROL AND DISPATCH, DECISION TO RETURN TO BNA WAS MADE. UPON ARRIVAL AT BNA, THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE WAS DISPATCHED. MAINTENANCE TROUBLESHOT THE SYSTEM AND PERFORMED GROUND RUNS. BUT C OULD NOT DUPLICATE THE DISCREPANCY AND COMPLIED WITH AD 98-20-01. ALL PERTINENT CHECKS WERE ACCOMPLISHED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. THERE HAS BEEN NO FURTHER DISCREPANCIES WITH THE SYSTEM SINCE THIS ONE OCCURRENCE. (M) 2 L 7 2 4F RT A21EA 1998122400232 19981224 00232 EA 1998 12 24 VTZA98327 1 19981103 A 3080 124112450 SENSOR CNDAIR CL600 CL6002B19 EA RT WING FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 629BR 7251 FLT 6647 - AVP-ORD - DURING CRUISE, EXPERIENCED A RIGHT WING ANTI ICE FAIL MESSAGE ON THE MASTER CAUTION PANEL. AIRCRAF T CONTACTED MAINTENANCE CONTROL AND DISPATCH, DECISION TO DIVERT TO PIT WAS MADE. DUE TO ICING IN ORD. UPON ARRIVAL AT PIT THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT MAINTENANCE WAS DISPAT CHED. MAINTENANCE WAS NOTIFIED AND AIRCRAFT MAINTENANCE WAS DISPATCHED. MAINTENANCE TROUBLESHOT THE DISCREPANCY. REMO VED AND REPLACED ALL 21 WING TEMPERATURE SENSORS. PERFORMED NUMEROUS GROUND CHECKS AND SIGNED OFF THE DISCREPANCY. AIR CRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 1998122400233 19981224 00233 EA 1998 12 24 VTZA98326 1 19981103 A 3010 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA ANTI ICE ILLUMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 627BR 7233 IND-IAD - DURING CRUISE, EXPERIENCED A RIGHT WING ANTI ICE FAIL MESSAGE ON THE MASTER CAUTION PANEL. AIRCRAFT CONTRACTE D MAINTENANCE CONTROL AND DISPATCH, DECISION TO DIVERT TO PIT WAS MADE, AS A PRECAUTIONARY MEASURE. UPON ARRIVAL AT PIT THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT MAINTENANCE WAS DISPATCHED . MAINTENANCE TROUBLESHOT THE DISCREPANCY, PERFORMED NUMEROUS GROUND OPERATIONS TESTS BUT COULD NOT DUPLICATE THE DISCR EPANCY. DISCREPANCY WAS CLOSED OUT AND AIRCRAFT WAS RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 1998122400234 19981224 00234 NM 1998 12 24 F3LA98193 1 19981113 A 2121 FAN BOEING 737 737201 1384454 NM AIR DISTRIBUTION MALFUNCTIONED A F3LA O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 NM 03 217US 20215 SAN - UPON DESCENT INTO SAN, FLIGHT CREW REPORTED SULFUR/ELECTRICAL ODOR FROM AIR VENTS AT ROW 5 AND 6 ON LEFT SIDE OF A IRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PLACARDED GASPER FAN PER MEL 21-24. UPON ARRIVAL IN DEN, GASPE R FAN WAS REPLACED AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998122400235 19981224 00235 NM 1998 12 24 F3LA98194 1 19981119 A 2910 LINE BOEING 737 737201 1384454 NM NR 2 ENGINE LEAKING A F3LA E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 NM 03 217US 20215 DEN - UPON ARRIVAL, FLIGHT CREW REPORTED NR 2 ENGINE 'A' SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. SHUT DOWN NR 2 ENGINE HYDRAULIC PUMP AND DECLARED AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LI NE AT NR 2 ENGINE PYLON AFT SPAR AND SYSTEM CHECKED OK. (M) 2 L 7 2 4F A16WE 1998122400236 19981224 00236 NM 1998 12 24 F3LA98197 1 19981209 A 3350 BATTERY BOEING 737 737201 1384454 NM PAX DOOR DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 217US 20215 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FORWARD ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M186, RE F WDM 33.51.01) FAILED TO ILLUMINATE BRIGHT DURING TESTING. MAINTENANCE REPLACED 2 RECHARGEABLE CD BATTERY CELLS AND CH ECKED OK. (M) 2 L 7 2 4F A16WE 1998122400237 19981224 00237 NM 1998 12 24 F3LA98196 1 19981209 A 3350 BATTERY BOEING 737 737201 1384454 NM PASSENGER DOOR DISCHARGED A F3LA K NONE L NO TEST IN INSP/MAINT 1 NM 03 217US 20215 DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED CONTROL CABIN ENTRY DOOR EMERGENCY EXIT LIGHTED SIGN, PORTABLE TYPE (M1 85, REF WDM 33.51.01) FAILED TO ILLUMINATE DURING TESTING. MAINTENANCE REPLACED 2 RECHARGEABLE CD BATTERY CELLS AND CHE CKED OK. (M) 2 L 7 2 4F A16WE 1998122400238 19981224 00238 NM 1998 12 24 USAA129802 1 19981203 A 3350 900835A BATTERY BOEING 727 727227 1384078 NM ROW 3A DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 19926 21244 FLT 6141 - BOS-LGA - ROW THREE CEILING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK. OPS CHECKS OK. (M) 2 L 7 3 4F A3WE 1998122400239 19981224 00239 NM 1998 12 24 USAA129801 1 19981202 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 922TS 7467 20415 FLT 6100 - LGA-BOS - EMERGENCY EXIT LIGHT INOPERATIVE ON RIGHT AFT EXTERIOR LIGHT. REPLACED BATTERY PACK AND LIGHT ASSE MBLY, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998122400240 19981224 00240 NM 1998 12 24 USAA129803 1 19981206 A 3350 90052 POWER SUPPLY BOEING 727 727225 1384077 NM OVERWING EXIT INOP A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS L1321 20447 FOUND ON L/S CHECK OFF, FLIGHT 6141 - BOS-LGA - RIGHT CENTER OVERWING EXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY P ACK AND CHARGING UNIT. (M) 2 L 7 3 4F A3WE 1998122400241 19981224 00241 NE 1998 12 24 USAA119803 2 19981111 A 7314 243600 PUMP BOEING 727 727227 1384078 NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE FAILED A USAA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 19 927TS 1127 20837 655453 FLT 6480 - DCA-LGA - ON TAKEOFF ROLL AT ABOUT 15 KIAS NR 3 ENGINE FAILED AT APPROX 85 PERCENT. NO COMPRESSOR STALL OR O THER STRANGE NOISE REPORTED. TAKEOFF ABORTED. REPLACED NR 3 ENGINE DRIVEN FUEL PUMP PER PWA MM 73-11-1. ENGINE RUNUP CHECKS OK. (M) 2 L 7 3 4F 4 F A3WE E2EA 1998122400242 19981224 00242 NM 1998 12 24 USAA119806 1 19981126 A 7711 LINE BOEING 727 727227 1384078 NM NR 1 ENGINE LEAKING A USAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 EA 19 925TS 21244 NR 1 EPR LOW (ABORTED TAKEOFF FLIGHT 6041 BOS-LGA). LEAK CHECKED AND FOUND PT7 LINE LEAKING AT BOTTOM OF ENGINE, TIGHTE NED LINE. LEAK CHECK AND OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1998122400243 19981224 00243 NM 1998 12 24 USAA119802 1 19981102 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 28 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 7430 21244 FLT 6181 - BOS-LGA - EMERGENCY EXIT LIGHT ON CEILING AT ROW 28 INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK NO RMAL. (M) 2 L 7 3 4F A3WE 1998122400244 19981224 00244 NM 1998 12 24 USAA119804 1 19981119 A 3350 37067001 BATTERY BOEING 727 727254 138408L NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 913TS 20250 BOTH LEFT AND RIGHT FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. BOTH LEFT AND RIGHT MID OVERWING EXTERIOR EME RGENCY EXIT LIGHTS INOP. REPLACED LEFT AND RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-0. REPLAC ED MID LEFT OVERWING EXIT LIGHT BATTERIES PER MM 33-50-0. REPLACED MID LEFT OVERWING EXIT LIGHT BATTERIES PER MM 33-50- 0. CHECKED OPERATION OF MID RIGHT OVERWING EMERGENCY EXIT LIGHT, OPERATION CHECKS OK IAW 33-50-0. (M) 2 L 7 3 4F A3WE 1998122400245 19981224 00245 NM 1998 12 24 USAASB98315 1 19981117 A 3397 WIRE BOEING 737 737401 1384701 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 404US 23886 PVD - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHTS ON THE OUTSIDE OF THE FORWARD COAT CLOSET INOP. MA INTENANCE REPAIRED AND SECURED BROKEN WIRE INSIDE FORWARD COAT CLOSET. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998122400246 19981224 00246 NM 1998 12 24 USAA980564 1 19981030 A 5320 FLOOR ANGLE BOEING 737 737296 1384486 NM LAVATORY CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 238US 22398 TPA - DURING C-1 CHECK VISUAL INSPECTION, FOUND ANGLE CORRODED AT LAV ATTACH POINT TO FLOOR AFT LAV ATTACH ANGLE FLOORBO ARD. FABRICATED DOUBLER PER EA 62883. (M) 2 L 7 2 4F RT A16WE 1998122400247 19981224 00247 NE 1998 12 24 USAASB98314 2 19981124 A 7200 ENGINE BOEING 737 737201 1384454 NM PWA JT8 JT8D15A 52051 NE RIGHT FOD A USAA E A ENGINE SHUTDOWN UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 EA 19 254AU 37486 22796 709002 BWI - FL2659 - UPON CLIMB-OUT AT APPROX 3,000 FT, THE NR 2 ENGINE INJESTED A BIRD. A MODERATE VIBRATION WAS NOTICED FRO M THE NR 2 ENGINE. CREW SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT BWI. THE CABIN WAS P REPPED FOR AN EMERGENCY. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE ASSY. OPERA TIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F 4 F A16WE E2EA 1998122400248 19981224 00248 NM 1998 12 24 USAASB98313 1 19981125 A 3350 S106 BATTERY BOEING 737 7372B7 1384560 NM SERVICE DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 273AU 22885 ROC - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT THE FORWARD RIGHT SERVICE DOOR, WON'T REMAIN ILLUMINATED. MAINTENANC E REMOVED AND REPLACED THE BATTERIES IN THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1998122400249 19981224 00249 NM 1998 12 24 USAASB98312 1 19981123 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN INOP A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 389US 23311 PIT - PILOT REPORTED THAT VARIOUS CABIN AND FLOOR LOW LEVEL EMERGENCY LIGHTING THROUGHOUT THE CABIN WAS INOP. MAINTENAN CE REMOVED AND REPLACED THE CHARGER ASSEMBLIES AND BATTERY PACKS AT THE MID CABIN AND AFT CABIN, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998122400250 19981224 00250 NM 1998 12 24 98ZZZM946 1 19981123 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN INOP A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 389US 23311 PIT - PILOT REPORTED THAT VARIOUS CABIN AND FLOOR LOW LEVEL EMERGENCY LIGHTING THROUGHOUT THE CABIN WAS INOP. MAINTENAN CE REMOVED AND REPLACED THE CHARGER ASSEMBLIES AND BATTERY PACKS AT THE MID CABIN AND AFT CABIN, LEFT SIDE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998122400251 19981224 00251 NM 1998 12 24 USAASB98311 1 19981123 A 3350 3114981 LIGHT BOEING 737 7373B7 1384580 NM GALLEY DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 392US 23314 GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT THE FORWARD SERVICE DOOR AND THE CHARGER ASSEMBLY AND M11 34 BATTERY PACK FOR THE OVER THE WING LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998122400252 19981224 00252 NM 1998 12 24 98ZZZM947 1 19981123 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM GALLEY DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 392US 23314 GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT THE FORWARD SERVICE DOOR AND THE CHARGER ASSEMBLY AND M11 34 BATTERY PACK FOR THE OVER THE WING LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998122400253 19981224 00253 NM 1998 12 24 98ZZZM948 1 19981123 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM GALLEY DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 392US 23314 GSO - MAINTENANCE FOUND THE FORWARD EMERGENCY LIGHT AT THE SERVICE DOOR INOP AND THE EMERGENCY LIGHT OVER THE RIGHT WING INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT THE FORWARD SERVICE DOOR AND THE CHARGER ASSEMBLY AND M11 34 BATTERY PACK FOR THE OVER THE WING LIGHT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1998122400254 19981224 00254 NM 1998 12 24 TWRA9859 1 19981124 A 3350 90083 BATTERY BOEING 747 747212B 1384886 NM PASSENGER DOOR DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND R4 MED EXIT SIGN INOPERATIVE. REPLACED BATTERY POWER SUPPLY PER MM 33-51-00. OPERATIONAL C HECK NORMAL. (M) 2 L 7 4 4F A20WE 1998122400255 19981224 00255 NM 1998 12 24 TWRA9860 1 19981124 A 3350 90083 BATTERY BOEING 747 747212B 1384886 NM PASSENGER DOOR DISCHARGED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING DAILY SERVICE, FOUND R5 MED EXIT SIGN INOPERATIVE. REPLACED BATTERY POWER SUPPLY PER MM 33-51-00. OPERATIONAL C HECK NORMAL. (M) 2 L 7 4 4F A20WE 1998122400256 19981224 00256 EU 1998 12 24 SIMA983301 1 19981126 A 3230 HP84830621 VALVE SAAB SF340 340B 7860101 EU NLG WW FAILED A SIMA O OTHER J WARNING INDICATION AP APPROACH 1 SW 21 904AE 1902 340B314 DFW - FLT 5042 - THE LANDING GEAR WOULD NOT EXTEND. THE INTRANSIT LIGHT ILLUMINATED, BUTH THE GEAR WOULD NOT COME DOWN. PERFORMED EMERGENCY EXTENSION PROCEDURES AND GOT THREE GREEN LIGHTS AT THAT POINT. LANDED WITHOUT FURTHER INCIDENT. R EMOVED AND REPLACED THE LANDING GEAR CONTROL VALVE. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998122400257 19981224 00257 EU 1998 12 24 SIMA983353 1 19981201 A 5414 SKIN SAAB SF340 340B 7860101 EU RT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 273AE 340B273 ABI - DURING MBV INSPECTION, RIGHT NACELLE INBOARD PANEL AFT OF PGB AS FOUND CHAFED. BLENDED CHAFED AREA AND PERFORMED A DYE PENETRANT INSPECTION WITH NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER .025 THICK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4T RT A52EU 1998122400258 19981224 00258 EU 1998 12 24 SIMA983352 1 19981201 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 273AE 340B273 ABI - DURING MBV INSPECTION, SEAT TRACKS 18.3L AND BL 0 WERE FOUND CORRODED. REMOVED AND REPLACED SEAT TRACKS. AIRCRAF T RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1998122400259 19981224 00259 SW 1998 12 24 SIMA983283 1 19981124 A 2611 72111211000 SMOKE DETECTOR SWRNGN SA227 SA227AC 8780603 SW AVIONICS BAY MALFUNCTIONED A SIMA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 SW 21 354AE AU220 AC633 LAX - FLT 3400 - ABORTED TAKEOFF AT 85 KTS FOR AVIONICS SMOKE WARNING LIGHT. REMOVED AND REPLACED AVIONICS SMOKE DETECT OR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1998122400260 19981224 00260 EU 1998 12 24 SIMA983291 1 19981125 A 3350 GE85 BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 214DA 340B214 MIA - FLT 5697 - FOUND EMERGENCY ARM LIGHT ON FLIGHT ATTENDANT PANEL DOES NOT ILLUMINATE. REMOVED AND REPLACED ARM LIGH T BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1998122400261 19981224 00261 NM 1998 12 24 SIMA98257 1 19981118 A 5330 SKIN BOEING 737 737281 138448P NM BS 310 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FORWARD RIGHT UPPER HINGE CUTOUT CRACKED AT BS 310, DEFECT SIZE LENGTH .50 INCH. REPAIRED FORWARD RIGHT SERVICE D OOR SKIN SECTION BETWEEN BS 308 AND BS 316, BETWEEN BEAM NR 3 AND BEAM NR 4 PER SRM 52-00-03 FIG 3. (M) 2 L 7 2 4F A16WE 1998122400262 19981224 00262 1998 12 24 P2EA98256 4 19981122 A 3417 HG1806807 ADC BOEING 737 737244 138448U NM E/E BAY FAILED A P2EA A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CE 05 620PC BU19170 19708 MCI - FLT 819 - AIR RETURN NO EMERGENCY DECLARED LANDING UNEVENTFUL. BOTH AIRSPEED INDS HAD FALSE INDICATIONS ON CLIMB- OUT, F/O HIGH, CAPT'S LOW, CAPTS AIRSPEED THEN WENT OT ZERO AND STAYED THERE. CAPT'S LOW, CAPT'S AIRSPEED THEN WENT OT ZERO AND SYATED THERE. CAPTAINS VSI UNRELIABLE IN FLIGHT. SHOWED 500 FT DESCENT IN LEVEL FLIGHT. READ 0 FPM ON FINAL APPROACH. F/O'S VSI SEEMED OK. REPLACED NR 1 CADC PER MM 34-12-11. OPS CHECK AND LEAK CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1998122400263 19981224 00263 NM 1998 12 24 P2EA98245 1 19981108 A 5711 SPAR BOEING 737 737244 138448U NM WS 430 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING FRONT SPAR UPPER CHORD CORRODED AT FSS 430. REPAIRED RIGHT WING FRONT SPAR UPPER CHORD BETWEEN FSS 401 .95 AND FSS 460 PER COOPESA EO COO-3-57-597 DATED OCT 30, 1998 AND BOEING INSTRUCTION LIST OF DATA INCLUDED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1998122400264 19981224 00264 NM 1998 12 24 P2EA98207 1 19981029 A 3310 1060752 BALLAST BOEING 737 737222 1384473 NM COCKPIT CEILING FAILED A A P2EA B A EMER. DESCENT UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 603DJ 8330 19955 FLT 418 - EMERGENCY DECLARED LANDING UNEVENTFUL. AT FL 220 SMELL SMOKE, THEN SMOKE ENTERED COCKPIT. MADE EMERGENCY LAN DING AT MZV. FOUND BALLAST FOR FORWARD GALLEY LIGHTS INOP. DETERMINED TO BE SOURCE OF SMOKE. PULLED AND COLLARED CIRC UIT BREAKER. DEFERRED PER MEL 33-2-, CI NR M603287 ASSIGNED PER MX CONTROLLER. PLACARD INSTALLED, REF CI NR M603287, F ORWARD GALLEY LIGHTS. REPLACED FORWARD GALLEY LIGHT BALLAST PER MM 33-26-21, OPS CHECK OK PER MM 33-21-41, CI NR M60328 7 CLEARED, PLACARD REMOVED. (M) 2 L 7 2 4F A16WE 1998122400265 19981224 00265 WP 1998 12 24 ORJA98291 1 19981123 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 21-25 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 IN SJC, EMERGENCY LIGHTS ROWS 21-25 INOPERATIVE. REPLACED BATTERY PACK AT LEFT REAR EXIT DOOR, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998122400266 19981224 00266 WP 1998 12 24 ORJA98290 1 19981121 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 19-22 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT SJC, EMERGENCY LIGHTS INOPERABLE AT ROWS 19-22. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998122400267 19981224 00267 WP 1998 12 24 ORJA98289 1 19981119 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP SEATS 19/20/21 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAS, TRACK LIGHTS WILL NOT EXTINGUISH AT 19D, 20D AND 21D. REMOVED AND REPLACED BATTERY PACK AT ROW 20. ALL EMERGEN CY TRACK LIGHTS, OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1998122400268 19981224 00268 WP 1998 12 24 ORJA98288 1 19981120 A 3350 2292AG FUSE DOUG DC9 DC983 3022083 WP RT EXIT LIGHT FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 RNO - FORWARD RIGHT EMERGENCY LIGHT LOW INOP. REPLACED FUSE AT FORWARD RIGHT EMERGENCY EXIT LIGHT. OPS CHECK GOOD. (M ) 2 L 7 2 4F RT A6WE 1998122400269 19981224 00269 WP 1998 12 24 ORJA98287 1 19981115 A 3350 G275007 BATTERY DOUG DC9 DC983 3022083 WP FUSELAGE DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 SJC - EMERGENCY BATTERY PACK, INOP AT RIGHT OVERWING FORWARD EXIT. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT RIGHT OVERWING FORWARD EXIT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1998122400270 19981224 00270 WP 1998 12 24 ORJA98286 1 19981116 A 3350 EM1267 BATTERY DOUG DC9 DC982 3022082 WP ROWS 21-24 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 RNO - EMERGENCY LIGHTS INOP AT ROWS 21-24. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES, OPS CHECK NORMAL. (M) 2 L 7 2 4F A6WE 1998122400271 19981224 00271 WP 1998 12 24 ORJA98285 1 19981116 A 3241 426071 CONTROLLER DOUG DC9 DC982 3022082 WP E/E BAY MALFUNCTIONED A ORJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 823RA 49889 RNO - GATE RETURN ABORTED TAKEOFF WHEEL NOT TURNING LIGHT CAME IN THE BEGINNING OF THE TAKEOFF ROLL EXTINGUISHED UPON RO LL OUT RETURN TO GATE. RERACKED ANTI SKID BOX DEFERRED WHEEL NOT TURNING AS PRECAUTION PER MEL 32-12 COMPLIED WITH MEL PROCEDURED RELEASED PER DMI NR 15398, NO DISCREPANCIES FOUND ON NEXT FLT NR 180 CLEARED DMI NR 15398. (M) 2 L 7 2 4F A6WE 1998122400272 19981224 00272 1998 12 24 HALA9800395 4 19981121 A 3414 INDICATOR DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A HALA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 WP 13 152AA 46707 SEA - FLT 23 - ON TAKEOFF, A/S FAIL MORE THAN 30 KNOTS DIFFERENCE ON AIRSPEED INDICATORS DURING TAKEOFF ROLL. ABORTED T AKEOFF AT 110 KTS IAS ON CAPTAIN A/S IND. REPLACED IAS AND PERFORMED ALL M/M TESTS. SYSTEM OPS CHECK NORMAL. IAS WAS F/O'S POSITION. (M) 2 L 7 3 4F A22WE 1998122400273 19981224 00273 WP 1998 12 24 ASAA9880228 1 19981116 A 5320 WEB DOUG DC9 DC982 3022082 WP CARGO BAY GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, THE FORWARD CARGO COMPARTMENT DOOR JAMB WAS FOUND BENT AND GOUGED. REPAIRED IAW ASA EA 5320-013 48. (M) 2 L 7 2 4F A6WE 1998122400274 19981224 00274 WP 1998 12 24 ASAA9880229 1 19981116 A 5320 RETAINER DOUG DC9 DC982 3022082 WP CARGO BAY CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, A PREVIOUS REPAIR WELD ON A MID CARGO COMPARTMENT LINER RETAINER WAS FOUND CRACKED. REPAIRED IA W ASA EA 5320-01347. (M) 2 L 7 2 4F A6WE 1998122400275 19981224 00275 WP 1998 12 24 ASAA9880240 1 19981117 A 5523 39378133 HINGE DOUG DC9 DC983 3022083 WP ELEVATOR GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK GOUGES WERE FOUNDON LEFT ELEVATOR ANTI FLOAT TAB HINGE, 3RD FROM OUTBOARD. REPAIRED IAW ASA EA 5 520-01062. (M) 2 L 7 2 4F RT A6WE 1998122400276 19981224 00276 NM 1998 12 24 BJNA981101 1 19981115 A 2910 6544510803 LINE BOEING 737 737214 138446R NM HYDRAULIC SYSTEM FAILED A BJNA A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 WP 11 457TM 20156 'A' SYSTEM HYDRAULIC FAILED, LACK OF HYDRAULIC PRESSURE. REPLACED HYDRAULIC LINE LEFT WING T/E, PERFORMED LEAK CHECK OF BOTH ENGINES AND IN WHEEL WELL, NO LEAKS FOUND. REPLACED NR 1 AND NR 2 ENGINE DRIVEN HYDRAULIC PUMP DUE TO CAVITATION. (M) 2 L 7 2 4F A16WE 1998122400277 19981224 00277 WP 1998 12 24 ASAA9880239 1 19981117 A 5320 WEB DOUG DC9 DC983 3022083 WP CARGO BAY DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK, WEB AT MID CARGO COMPARTMENT DOOR JAMB WAS DAMAGED DURING INSTALLATION OF CARGO COMPARTMENT SIDE LINER. REPAIRED IAW ASA EA 5310-01629. (M) 2 L 7 2 4F RT A6WE 1998122400278 19981224 00278 WP 1998 12 24 ASAA9880238 1 19981117 A 5320 WEB DOUG DC9 DC983 3022083 WP FUSELAGE CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK CORROSION WAS FOUND ON CUSP WEB AT L2 DOOR THRESHOLD. REPAIRED IAW ASA EA 5310-01624. (M) 2 L 7 2 4F RT A6WE 1998122400279 19981224 00279 WP 1998 12 24 ASAA9880237 1 19981117 A 5755 FITTING DOUG DC9 DC983 3022083 WP SPOILER CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK, CORROSION WAS FOUND ON RIGHT WING INBOARD FLIGHT SPOILER HINGE FITTING. REPAIRED IAW ASA EA 276 0-01026. (M) 2 L 7 2 4F RT A6WE 1998122400280 19981224 00280 WP 1998 12 24 ASAA9880236 1 19981117 A 5753 FITTING DOUG DC9 DC983 3022083 WP TE FLAP GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK, GOUGES WERE FOUND ON LEFT T/E FLAP OUTBOARD HINGE FITTING. REPAIRED IAW ASA EA 2750-01066. (M) 2 L 7 2 4F RT A6WE 1998122400281 19981224 00281 WP 1998 12 24 ASAA9880235 1 19981116 A 5754 SKIN DOUG DC9 DC982 3022082 WP L/E SLAT DENTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, DENTS WERE FOUND ON LEFT WING NR 2 L/E SLAT SKIN. REPAIRED IAW ASA EA 5750-01299. (M) 2 L 7 2 4F A6WE 1998122400282 19981224 00282 WP 1998 12 24 ASAA9880234 1 19981116 A 5754 SKIN DOUG DC9 DC982 3022082 WP L/E SLAT GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, GOUGES WERE FOUND ON RIGHT WING NR 0 L/E SLAT SKIN. REPAIRED IAW ASA EA 5750-01298. (M) 2 L 7 2 4F A6WE 1998122400283 19981224 00283 WP 1998 12 24 ASAA9880233 1 19981116 A 5511 SPAR DOUG DC9 DC982 3022082 WP HORIZONTAL STAB CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, CORROSION FOUND ON HORIZONTAL STABILIZER FORWARD SPAR LOWER CAP AT AFT BARREL NUT CLEARANCE HOLE . REPAIRED IAW ASA EA 5510-01070. (M) 2 L 7 2 4F A6WE 1998122400284 19981224 00284 WP 1998 12 24 ASAA9880232 1 19981116 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 400-420 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK DAMAGE TO FUSELAGE SKIN FROM LIGHTNING STRIKES WERE FOUND FROM STATION 400 TO STATION 420. REPAI RED IAW ASA EA 5330-01352. (M) 2 L 7 2 4F A6WE 1998122400285 19981224 00285 WP 1998 12 24 ASAA9880230 1 19981116 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 301/313 DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, INTERIM REPAIRS TO DAMAGED FUSELAGE SKIN AT STATION 301 AND STATION 313 REQUIRED PERMANENT REPAI R. REPAIRED IAW ASA EA 5330-01347. (M) 2 L 7 2 4F A6WE 1998122400286 19981224 00286 WP 1998 12 24 ASAA9880242 1 19981117 A 5720 SUPPORT DOUG DC9 DC983 3022083 WP LT WING GOUGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK, GOUGES WERE FOUND ON LEFT WING NR 0 L/E SLAT OUTBOARD SUPPORT. REPAIRED IAW ASA EA 5740-01149. (M) 2 L 7 2 4F RT A6WE 1998122400287 19981224 00287 WP 1998 12 24 ASAA9880241 1 19981117 A 5513 FITTING DOUG DC9 DC983 3022083 WP LT ELEVATOR CHAFED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK, WEAR SPOT WAS FOUND ON LEFT ELEVATOR CONTROL TAB HINGE FITTING (4TH FROM INBOARD). REPAIRED IAW ASA EA 5520-01063. (M) 2 L 7 2 4F RT A6WE 1998122400288 19981224 00288 WP 1998 12 24 ASAA9880243 1 19981117 A 3350 BATTERY DOUG DC9 DC983 3022083 WP ROW 9-11 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 9 TO 11 WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400289 19981224 00289 WP 1998 12 24 ASAA9880226 1 19981109 A 2497 WIRE DOUG DC9 DC983 3022083 WP E/E BAY FAILED A ASAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 NM 01 976AS 53452 OAK - DURING 15K CHECK, ELECTRICAL POWER WAS TURNED ON AFTER OTHER MAINTENANCE WAS PERFORMED AND SMOKE WAS NOTED EMITTIN G FROM THE AFT SIDE OF THE LOWER EPC PANEL. INSPECTED THE LOWER AFT EPC PANEL AND FOUND CHAFED AND BURNED WIRES IN THE PANEL NEAR THE RT GEN AC POWER RELAY. REMOVED DAMAGED WIRES AND SPLICED 7 NEW 10AWG WIRES FROM THE RT GEN AC POWER RELA Y THROUGH THE EPC PANEL TO THE GEN BUS CIRCUIT BREAKER PANEL PER ASA EA 2400-01045 AND BAC SWPM D6-54446. THE WIRING A PPEARED TO HAVE BEEN CHAFING ON THE EPC PANEL STRUCTURE DUE TO WIRES FLEXING EACH TIME THE GENERATOR BUS CIRCUIT BREAKER PANEL WAS OPENED. REPOSITIONED AND RESECURED WIRING IN CLAMPS. (M) 2 L 7 2 4F RT A6WE 1998122400290 19981224 00290 WP 1998 12 24 ASAA9880225 1 19981107 A 3350 BATTERY DOUG DC9 DC983 3022083 WP ROW 25-27 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 25 TO 27 WERE FOUND INOPERATIVE. REPLACED THE B ATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400291 19981224 00291 1998 12 24 ASAA9880222 4 19981107 A 2565 SLIDE DOUG DC9 DC983 3022083 WP TAILCONE FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 976AS 53452 OAK - DURING 15K CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE TAILC ONE EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1998122400292 19981224 00292 WP 1998 12 24 ASAA9880221 1 19981106 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 973AS 53449 SEA - PRIOR TO DEPARTURE OF FLT 282, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERATIV E. REPAIRED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400293 19981224 00293 WP 1998 12 24 ASAA9880218 1 19981105 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400294 19981224 00294 1998 12 24 ASAA9880217 4 19981103 A 2565 SLIDE DOUG DC9 DC982 3022082 WP PASSENGER DOOR FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOO R EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1998122400295 19981224 00295 WP 1998 12 24 ASAA9880216 1 19981102 A 3350 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 954AS 49387 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998122400296 19981224 00296 WP 1998 12 24 ASAA9880215 1 19981030 A 3350 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOP A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 53473 SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400297 19981224 00297 WP 1998 12 24 ASAA9880214 1 19981028 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. SECURED C ONNECTOR TO LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400298 19981224 00298 WP 1998 12 24 ASAA9880212 1 19981028 A 3350 BATTERY DOUG DC9 DC982 3022082 WP ROW 11-13 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 951AS 49111 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 11 TO 13 REMAINED ILLUMINATED WITH ELECTRIC POWE R OFF. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998122400299 19981224 00299 WP 1998 12 24 ASAA9880211 1 19981027 A 3350 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE MID CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400300 19981224 00300 WP 1998 12 24 ASAA9880210 1 19981022 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 22-23 FAILED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 49234 SEA - CREW REPORTED HOT SCORCHED PLASTIC ODOR IN AREA OF ROWS 22 THROUGH 25. REPLACED MELTED CONNECTORS P2-3291 AND R5- 3292 ABOVE ROW 22 LT, BALLAST AT ROWS 22-32 RT AND BULBS FROM ROWS 18-28. NO ODORS WERE DETECTED. (M) 2 L 7 2 4F A6WE 1998122400301 19981224 00301 WP 1998 12 24 ASAA9880209 1 19981021 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - FLT 460 - CREW REPORTED FIRST BANK OF EMEGENCY EXIT FLOOR TRACK LIGHTS WERE INOPERATIVE. RECONNECTED WIRING AND L IGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400302 19981224 00302 WP 1998 12 24 ASAA9880208 1 19981016 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 LAX - PRIOR TO DEPARTURE OF FLIGHT 403 - CREW REPORTED THAT THE FORWARD FIVE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE INOP ERATIVE. RECONNECTED WIRING TO THE LAMP MODULE AND THE LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1998122400303 19981224 00303 WP 1998 12 24 ASAA9880207 1 19981011 A 3350 POWER SUPPLY DOUG DC9 DC982 3022082 WP FUSELAGE INOP A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS ILLUMINATE WITH ELECTRIC POWER OFF. REPLACE D THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998122400304 19981224 00304 WP 1998 12 24 ASAA9880206 1 19981011 A 3350 BATTERY DOUG DC9 DC982 3022082 WP FUSELAGE DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 956AS 48079 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERWING EMERGENCY EXIT IDENTIFIERS WERE FOUND INOPERATIVE. REPLACED THE BA TTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1998122400305 19981224 00305 NM 1998 12 24 AALA982116 1 19981119 A 3231 2314143 SWITCH BOEING 727 727223 1384074 NM RT MLG DOOR MALFUNCTIONED A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 864AA 21369 MIA - FLT 2157 - AFTER TAKEOFF MIA EN ROUTE TO CUN WITH GEAR RETRACTED RIGHT MAIN GEAR DOOR STILL OPEN. CYCLED GEAR SEV ERAL TIMES, RIGHT MAIN DOOR STILL INDICATED OPEN. AFTER CYCLING GEAR HANDLE TO UP POSITION AFTER GEAR ALREADY RETRACTED , GOT LIGHTS TO EXTINGUISH TO NORMAL (OUT) INDICATION. RETURNED MIA AND LANDED WITHOUT INCIDENT. REPLACED RIGHT MAIN G EAR DOOR WARNING SWITCH. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998122400306 19981224 00306 NM 1998 12 24 AALA981758 1 19980903 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 950F BELT FRAME DOUBLER GOUGED BETWEEN STRINGER 25L AND 26L. REMOVED 16 INCHES DAMAGE. INSTALLED 26 INCH ES DOUBLER 7075 T-6 .071 1 ROW BOTTOM 8-4 HL 25, 1 ROW CENTER 6-4 HL 27, 1 ROW TOP 6-2 HL 9 INSTALLED REPAIR DOUBLER PER SRM 51-40-3. REATTACH INTERCOSTAL W/7079 T-6 .063 TIE CLIP 6-3HL 9 8-5HL 1. (M) 2 L 7 3 4F A3WE 1998122400307 19981224 00307 NM 1998 12 24 AALA981757 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 950B BELL FRAME DENTED TOP AND WEB BULGED OUTBOARD AND INBOARD OF STRINGER 26R. FABRICATED REPAIR OUT OF 7075 -T6 .071 WITH 14 .5 INCH FASTENERS IN BOTTOM ROW, 13 .1875 INCH FASTENERS IN ROW AND EIGHT .1875 AND THREE .25 INCH HI-LOCKS IN TOP FLANGE. REPAIR 15 INCHES LONG, ONE REPAIR FOR TWO DENTS INSTALLED PER 51-40-3. (M) 2 L 7 3 4F A3WE 1998122400308 19981224 00308 NM 1998 12 24 AALA981756 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 950F BELL FRAME DENTED AND WEB BULGED 3 PLACES ABOVE STRINGER 26L. INSTALLED DOUBLER PER SRM 53-10-4. (M ) 2 L 7 3 4F A3WE 1998122400309 19981224 00309 NM 1998 12 24 AALA981755 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 990 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 990 BELL FRAME TOP DENTED AND WEB BUCKLED 2 PLACES BETWEEN STRINGER 25L AND 26L. REMOVED 20 INCHES DAMAGE, PREPARED SURFACE, INSTALLED 29 INCHES DOUBLER 7075 T-6 .071. BOTTOM ROW 27 EA 8-8 RIVETS, CENTER ROW 34 EA 6-8 RIVETS, TOP ROW 7 EACH RIVETS PER 51-40-3. (M) 2 L 7 3 4F A3WE 1998122400310 19981224 00310 NM 1998 12 24 AALA981753 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STRINGER 1 CORRODED STATION 720 B-C. REPAIRED PER SRM 53-10-3 PAGE 40 FIG 2. (M) 2 L 7 3 4F A3WE 1998122400311 19981224 00311 NM 1998 12 24 AALA981752 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 2L CORRODED STATION 720 D-E. REPAIRED PER SRM 53-10-3 PAGE 40. (M) 2 L 7 3 4F A3WE 1998122400312 19981224 00312 NM 1998 12 24 AALA981751 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STRINGER 3L CORRODED STATION 7200-E. REPAIRED PER SRM 53-10-3 PAGE 40 FIG 2. (M) 2 L 7 3 4F A3WE 1998122400313 19981224 00313 NM 1998 12 24 AALA981750 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 3L CORRODED STATION 720C-D. REPAIRED STRINGER 3L STATION 720C-D IAW SRM 53-10-3 PAGE 4C-4E. (M) 2 L 7 3 4F A3WE 1998122400314 19981224 00314 NM 1998 12 24 AALA981749 1 19980908 A 5330 SKIN BOEING 727 727227 1384078 NM BS 870 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION ALONG STRINGER 10R SKIN LAP UPPER AND LOWER SIDE OF STRINGER STATION 870. INSTALLED REPAIR PER ES O 11697, DATED 9/3/98. (M) 2 L 7 3 4F A3WE 1998122400315 19981224 00315 NM 1998 12 24 AALA981748 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND CORROSION AT 740 CASTING AND SKIN JOINT BETWEEN STRINGER 6R AND 7R STRINGERS AND CORROSION UNDER STRINGER 7R TERMINAL FITTING. INSTALLED REPAIR AT BUTT SPLICE PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1998122400316 19981224 00316 NM 1998 12 24 AALA981747 1 19980924 A 5711 SPAR BOEING 727 727227 1384078 NM WS 348 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - LOWER SPAR CHORD STATION 383 REAR SPAR HAS CORROSION. REPAIRED LOWER SPAR CHORD PER SRM 57-30-2. (M) 2 L 7 3 4F A3WE 1998122400317 19981224 00317 NM 1998 12 24 AALA981746 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1050 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STATION 1050 BELL FRAME WEB AND LEGS CORRODED BACKSIDE BETWEEN STRINGER 19L AND 20L. INSTALLED DOUBLER PER 51-40-3 FIG 1 W .050 17-7 CRACK PER AARD 51-20-07-5 WITH FOUR .1875 HI-LOCKS AND 4.25 HI-LOCKS EACH SIDE OF DAMAGE. (M ) 2 L 7 3 4F A3WE 1998122400318 19981224 00318 NM 1998 12 24 AALA981745 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 520 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - UPPER SPAR CHORD CORRODED ABOVE AND OUTBOARD OF NR 6 L/E SLAT ACTUATOR. REMOVED CORROSION AND REPAIRED AREA WITH 17-7 TH1050 DOUBLER .24 EA .1875 INCH AND 24 EA .25 INCH HI-LOCKS PER ESO 11697 DATED 9-2-98. (M) 2 L 7 3 4F A3WE 1998122400319 19981224 00319 NM 1998 12 24 AALA981744 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 510 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - UPPER SPAR CHORD CORRODED ABOVE AND OUTBOARD OF NR 6 L/E SLAT ANTI ICE TUBE. REMOVED CORROSION AND REPAIRED AREA WITH 17-7 TH1050 DOUBLER, 24 EACH .1875 AND 24 EACH .25 INCH HI-LOCKS PER ESO 11697, DATED 9-2-98. (M) 2 L 7 3 4F A3WE 1998122400320 19981224 00320 NM 1998 12 24 AALA981743 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1010 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND BS 1010 BELL FRAME CORRODED, LOWER LEG BELOW STRINGER 19L. BLENDOUT CORROSION PER SRM 51-10-6. INSTALLED S TAINLESS ANGLE DOUBLER WITH NINE .25 INCH AND NINE .1875 INCH HI-LOCKS PER SRM 51-40-3 AND AARD 51-20-5. (M) 2 L 7 3 4F A3WE 1998122400321 19981224 00321 NM 1998 12 24 AALA981742 1 19980925 A 5711 SPAR BOEING 727 727227 1384078 NM WS 403-409 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND UPPER SPAR CHORD HAS HEAVY CORROSION ABOVE NR 4 L/E SLAT ACTUATOR. INSTALLED REPAIR ANGLE AT UPPER CHORD PE R ESO 11697, DATED 09/02/98. (M) 2 L 7 3 4F A3WE 1998122400322 19981224 00322 NM 1998 12 24 AALA981740 1 19980925 A 5330 SKIN BOEING 727 727227 1384078 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FUSELAGE SKIN CORRODED STATION 950C-950D, STRINGER 4L. REPAIRED PER SRM 53-30-3 PAGE 14. (M) 2 L 7 3 4F A3WE 1998122400323 19981224 00323 NM 1998 12 24 AALA981739 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 660 BELL FRAME DENTED BETWEEN STRINGER 24L-25L. REPAIRED FRAME AS PER SRM 53-10-4 USING .063 DOUBLER AND 4 ROWS OF .1875 FASTENERS EACH SIDE OF DAMAGE OUTSIDE FRAME REPAIR. (M) 2 L 7 3 4F A3WE 1998122400324 19981224 00324 NM 1998 12 24 AALA981738 1 19980914 A 5311 FRAME BOEING 727 727227 1384078 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - STATION 500 FRAME DENT AT STRINGER 22 LEFT TO STRINGER 23 LEFT. INSTALLED DOUBLER PER AARD 53-10-07-3. (M) 2 L 7 3 4F A3WE 1998122400325 19981224 00325 NM 1998 12 24 AALA981736 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 1110 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - BELL FRAME DENTED STATION 1110, STRINGER 25L. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLERS REPAIR PER SRM 51-40-3, FIG 1. (M) 2 L 7 3 4F A3WE 1998122400326 19981224 00326 NM 1998 12 24 AALA981735 1 19980925 A 5313 STRINGER BOEING 727 727227 1384078 NM BS 720 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND STRINGER 4R STATION 720F, REWORKED TOO MUCH MATERIAL REMOVED. REPAIRED STRUCTURE STRINGER WITH 'J' PATCH RE PAIR PER SRM 53-10-3 PAGES 8A/B. (M) 2 L 7 3 4F A3WE 1998122400327 19981224 00327 NM 1998 12 24 AALA981734 1 19980925 A 5311 FRAME BOEING 727 727227 1384078 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - FOUND 950C BELL FRAME DENTED, TWO EACH PLACES STRINGER 25R - 26R, TOP OF FRAME. CUT OUT DENTS AND INSTALLED DOUBL ER PER SRM 51-40-3 FIG 1, 17 INCH DOUBLER, 7075-T6 .071, TOP FLANGE FIVE EACH .1875 RIVETS EACH END OF DAMAGE, TWO ROWS .25 INCH IN WEB. (M) 2 L 7 3 4F A3WE 1998122400328 19981224 00328 EU 1998 12 24 VTZA98321 1 19981028 A 5270 DOOR WARNING BAG JETSTM JETSTM3201 1500217 EU PAX DOOR ACTIVATED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 488UE 907 FLT 6338 - IAD-SYR - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998122400329 19981224 00329 EU 1998 12 24 VTZA98320 1 19981022 A 7712 31024766 SIGNAL BAG JETSTM JETSTM3101 1500215 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 473UE 828 FLT 6582 - IAD-GSO - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE EGT FLUCTUATION. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SIGNAL CONDITIONER, O PS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A21EU 1998122400330 19981224 00330 EU 1998 12 24 VTZA98318 1 19981022 A 3230 114A703056A RETRACT MECH BAG JETSTM JETSTM3201 1500217 EU NLG LACK OF LUBE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 475UE 850 FLT 6286 - IAD-CMH - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LANDING GEAR WOULD NOT RETRACT. AIRCRA FT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPACKED NOSE GEAR. OPS CHECK OK. AIRC RAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998122400331 19981224 00331 EU 1998 12 24 VTZA98317 1 19981022 A 3260 622800200 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 485UE 901 IAD-PHF - FLT 6151 - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR NOT RETRACTING. AIRCRAFT LANDED A ND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NOSE GEAR AOG SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1998122400332 19981224 00332 1998 12 24 98ZZZM949 4 19981112 A 6122 8210410 GOVERNOR WOODWARD BEECH 1900 1900D 1154162 CE LT ENGINE FAILED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 853CA 11434408 UE56 LEFT ENGINE PROP RPM FAILS TO GO ABOVE 1400 RPM. 2 L 7 2 4T RT A24CE 1998122400333 19981224 00333 NE 1998 12 24 98ZZZM950 2 19981124 A 7250 3044700 POWER SECTION BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE RESTRICTED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 861CA 10615 UE164 114174 DURING PREFLIGHT INSPECTION, LEFT PROP FAILS TO TURN FREELY DUE TO APPARENT INTERNAL POWER SECTION RESTRICTION. LOOSE P T BAFFLE (AIR SEAL) SUSPECTED PROBLEM. REPLACED POWER SECTION MODULE WITH AIRWORTHY MODULE IAW PW AND RAYTHEON MM. LEA K CHECK AND OPERATIONAL CHECK SATISFACTORY. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1998122400334 19981224 00334 CE 1998 12 24 98ZZZM951 1 19981202 A 3233 11438004115 ACTUATOR BEECH 1900 1900D 1154162 CE RT MLG MALFUNCTIONED A JJBA K NONE O OTHER IN INSP/MAINT 1 EA 01 860CA 1462 0769A UE134 RIGHT MAIN LANDING GEAR DOWN AND LOCK INDICATOR INTERMITTENT. TROUBLESHOOTING REVEALED DEFECTIVE RIGHT MAIN LANDING GEA R ACTUATOR DOWN AND LOCK SWITCH. REPLACED RIGHT MAIN LANDING GEAR ACTUATOR IAW RAYTHEON MM CHAPTERS 32. OPERATIONAL CH ECK SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1998122400335 19981224 00335 NM 1998 12 24 TWAA9819901 1 19981218 A 5242 DOOR BOEING 727 727231 1384079 NM E & E COMPT NOT LATCHED A TWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 54332 20310 ON LIFT OFF GOT AN EQUIPMENT ACCESS DOOR ANNUNCIATOR LIGHT. THE PLANE WOULD NOT PRESSURIZE, OPERATIONAL CHECK OF THE DO OR WAS MADE. CC-01 01-24-98 MCI. 2 L 7 3 4F A3WE 1998122400336 19981224 00336 WP 1998 12 24 TWAA9819902 1 19981220 A 3350 7732 BULB DOUG DC9 DC983 3022083 WP CABIN FAILED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9401W 53137 FOUND FLOOR EGRESS LIGHTS OUT ROWS 5 TO 25 AND ROW 27. REPLACED LAMPS. CHECK-C 12-8-98 MCI. 2 L 7 2 4F RT A6WE 1998122400337 19981224 00337 NE 1998 12 24 TWAA9819903 2 19981221 A 7230 COMPRESSOR DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE NR 1 ENGINE DAMAGED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN R C PARTIAL RPM/PWR LOSS F.O.D. CL CLIMB 1 CE 05 9304C 49530 3225 THE NR 1 ENG EXPERIENCED COMPRESSOR STALLS. ENGINE WAS SHUT DOWN AND FLT RETURNED TO STL. FOUND SIX EACH FIRST STAGE F AN BLADES WITH DAMAGE INDICATING POSSIBLE ICE INJESTION. REPLACED FIRST STAGE FAN. CHECK-C 1-19-98 STL. 2 L 7 2 4F 4 F RT A6WE E9NE 1998122400338 19981224 00338 WP 1998 12 24 TWAA9819904 1 19981210 A 5312 BULKHEAD FRAME DOUG DC9 DC982 3022082 WP BS 69 DAMAGED A TWAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 CE 05 924TW 49100 DURING TAKEOFF, BIRDS STRUCK THE AIRCRAFT AT THE RT SIDE NOSE AREA. THE BULKHEAD FRAME WAS DAMAGED AT STA 69 RT. REPAI RED BULKHEAD FRAME PER TWA ARA 15879, AND DC9/MD80 SRM STD PRACTICE 51-30-5. CHECK-C 4-28-98 MCI. 2 L 7 2 4F A6WE 1998122400339 19981224 00339 NM 1998 12 24 VJ9800665 1 19981202 A 5711 SPAR CHORD BOEING 737 7372L9 1384497 NM RT WING CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION, THE RIGHT HAND LOWER WING CHORD HAS MATERIAL MISSING AND CORROSION AT FUELING PANEL AT FS 365. ME CHANICALLY REMOVED CORROSION, MATERIAL THICKNESS .170, MATERIAL LOSS .100 REMAINING THICKNESS .070. FABRICATED REPAIR D OUBLER IAW AIRTRAN RES 982060. 2 L 7 2 4F RT A16WE 1998122400340 19981224 00340 WP 1998 12 24 VJ9800668 1 19981210 A 5347 5295597812000 SEAT TRACK DOUG DC9 DC932 3022066 WP BS 446-511 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 910VJ 47277 SCHEDULED INSPECTION, FORWARD CARGO LEFT HAND TRACK FS 446 TO 511 HAS SURFACE CORROSION THRU OUT. REMOVED AND REPLACED WITH A NEW SECTION OF TRACK IAW DC9 SRM 51-10-4 AND 51-10-2. 2 L 7 2 4F A6WE 1998122400341 19981224 00341 WP 1998 12 24 VJ9800669 1 19981219 A 5320 FITTING DOUG DC9 DC932 3022066 WP BS 908 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION, CORROSION WAS FOUND ON UPPER FRAME FITTING AT UPPER CUSP FS 908R CORROSION WAS OUT OF LIMITS. REM OVED AND FABRICATED FITTING IAW DWG NR 3912956, AND INSTALLED NEW PART IAW 51-30-5. 2 L 7 2 4F A6WE 1998122400342 19981224 00342 WP 1998 12 24 VJ9800670 1 19981215 A 5320 1A40384 GUSSET DOUG DC9 DC932 3022066 WP BS 965 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION, FLOOR FRAME FS 965 HAS CORROSION ON FRAME AND ATTACHING BRACKETS. REMOVED GUSSET, FOUND IT TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW GUSSET IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1998122400343 19981224 00343 WP 1998 12 24 VJ9800671 1 19981212 A 5320 99101516 WEB DOUG DC9 DC932 3022066 WP BS 230 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION, CUSP WEB ANGLE AND DOUBLER CORRODED AND CRACKED AT FS 230L (CORRODED) AND STA 617 RT (CRACKED). R EMOVED CORROSION AND FORMED SPLICE ANGLE FROM 7075-T6 .090 IAW DC9 SRM 53-04 AND RES 982167. REMOVED AND REPLACED CUSP WEB AT STA 617 TO 658 RT IAW SRM 53-01 AND 51-30-2. 2 L 7 2 4F A6WE 1998122400344 19981224 00344 WP 1998 12 24 VJ9800672 1 19981211 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 148-190 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION, LONGERONS AT 4L STA 160 AND 22R STA 979R WERE FOUND CORRODED AND CRACKED. REMOVED LONGERON 4L FRO M STA 148 TO 190. FABRICATED REPAIR LONGERON AND SPLICE FROM 277922-3 AND 7637813-3 IAW SRM DC9 53-11-1 FIG 3 AND 53-02 . AT STATION 979R, FABRICATED NEW LONGERON AND CLEAN CORROSION IAW SRM DC9 53-11-3 FIG 4. TREATED, PRIMED AND INSTALLE D IAW DC9 SRM 51-10-2 AND 51-30-2. 2 L 7 2 4F A6WE 1998122400345 19981224 00345 NM 1998 12 24 VJ9800673 1 19981202 A 5320 MOUNT BOEING 737 7372L9 1384497 NM BS 947 & 967 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION, THE LOWER SIDE OF THE CABIN FLOOR PANEL MOUNT WAS FOUND CORRODED AT BS 967/947 LBL 51. REMOVED MO UNT PLATE, FABRICATED AND INSTALLED MOUNT PLATE REPAIR IAW B737 SRM 51-40-2, 51-30-2 AND MM 51-20-11. 2 L 7 2 4F RT A16WE 1998122400346 19981224 00346 WP 1998 12 24 VJ9800674 1 19981221 A 5220 59101595 SEAL DOUG DC9 DC932 3022066 WP EMERGENCY EXIT DIRTY A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 947VV 47555 REQUESTED INSPECTION OF OVERWING EXIT AT 19A. PASSENGER REPORTED VIBRATION AND AIR LEAK. REMOVED DEBRIS FROM SEAL AS P ER MM 52-20. 2 L 7 2 4F A6WE 1998122400347 19981224 00347 NM 1998 12 24 VJ9800675 1 19981219 A 5315 FLOORBEAM BOEING 737 7372L9 1384497 NM BS 947 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION, CABIN FLOORBEAM WAS FOUND TO BE CORRODED ON LOWER SURFACE OF THE UPPER FLANGE AT FUSELAGE STA 947 LBL 6 RBL 12, RBL 6 RBL 12, RBL 21, RBL 35 AND RBL 42 AT CLIP NUTS. ANOTHER FLOORBEAM WAS FOUND CORRODED BEYOND LIMITS AT STA 1016 LBL 30 - RBL 30. CUT OUT CORRODED SECTION, FABRICATED AND INSTALLED REPAIR MEMBERS AT STA 947 IAW B737 SRM 51-30-2, 53-10-9 FIG 2 AND 53-10-1. AT STA 1016 REMOVED FLOORBEAM AND REPLACED T CAP ON BEAM 81 LONG IAW B737 SRM 51-10 -2, 53-10-9 AND AIRTRAN RES 982216 AND MM 38-52-51. 2 L 7 2 4F RT A16WE 1998122400348 19981224 00348 WP 1998 12 24 VJ9800676 1 19981203 A 5210 9915565611 BRACKET DOUG DC9 DC932 3022066 WP PAX DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION, THE AFT ENTRY DOOR INTERNAL STRUCTURE UPPER LEFT HAND CORNER HAS A CRACKED BRACKET AT STA 946. RE MOVED THE AFT ENTRY DOOR CRACKED BRACKET, DRILLED NEW REPLACEMENT BRACKET, DEBURRED, TREATED, PRIMED AND INSTALLED IAW D C9 SRM 51-10-3, 51-10-4 AND 51-30-5. 2 L 7 2 4F A6WE 1998122400349 19981224 00349 NM 1998 12 24 VJ9800677 1 19981220 A 5312 BLKHD RETAINERS BOEING 737 7372L9 1384497 NM AFT LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION, THE AFT LAVATORY SEAL RETAINER FOR THE AFT BULKHEAD EXPANSION WAS CORRODED. REMOVED CORRODED RETA INERS, FABRICATED AND INSTALLED NEW RETAINERS IAW B737 SRM 51-20-1, 51-30-5, 51-10-2, AND MM 51-21-31. 2 L 7 2 4F RT A16WE 1998122400350 19981224 00350 NM 1998 12 24 VJ9800678 1 19981218 A 3350 P4010021 BATTERY BOEING 737 7372L9 1384497 NM CABIN DISCHARGED A ZZDA K NONE L NO TEST IN INSP/MAINT 1 SO 15 464AT 21278 FORWARD EMERGENCY FLASHLIGHT INOP AND EMERGENCY FLOOR PATH LIGHTNING STRIP LOOSE. INSTALLED SERVICEABLE FLASHLIGHT BATT ERY AND INSTALLED END CAP AT ROW 10 IAW GMM 4-2.6 ITEM 8 BASIC TASKS. BATTERY (P/N P4-01-0021) AND END CAP (P/N 09102-1 21). 2 L 7 2 4F RT A16WE 1998122400351 19981224 00351 SO 1998 12 24 RAAA98E8027 1 19981221 A 3350 240498C RELAY LKHEED 188 188C 5262604 SO BS 530 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 EXTERNAL EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED K106 RELAY DUE FAILED. 2 L 7 4 4T 4A22 1998122400352 19981224 00352 EA 1998 12 24 COMA9860396 1 19981220 A 5320 601R35031239 ANGLE CNDAIR CL600 CL6002B19 EA BS 621 CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 976CA 7151 CARGO FLOOR SUPPORT ANGLES AT FS 621, WL 73.0, LEFT HAND AND RIGHT HAND ARE CRACKED. REPAIRED RIGHT HAND ANGLE PER REO 601R5361117RA. 2 L 7 2 4F RT A21EA 1998122400353 19981224 00353 EA 1998 12 24 COMA9860397 1 19981221 A 3010 124112450 SENSOR CNDAIR CL600 CL6002B19 EA RT WING DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 984CA 7171 WING ANTI ICE DUCT MESSAGE. REPLACED 7 DEFECTIVE OVERHEAT SENSORS IN RIGHT HAND WING. 2 L 7 2 4F RT A21EA 1998122400354 19981224 00354 EU 1998 12 24 QXEA9802106 1 19981218 A 5210 MECHANISM FOKKER F28 F28MK4000 4990810 EU PAX DOOR MALFUNCTIONED A QXEA K NONE O OTHER TX TAXI/GRND HDL 1 NM 09 496US 11169 MAIN CABIN DOOR WOULD NOT OPEN. USED EMERGENCY MEANS TO OPEN MAIN CABIN DOOR. OPERATED DOOR SEVERAL TIMES, NO DISCREPAN CIES NOTED. CLEANED SEAL AREA OF WATER. NO PARTS REPLACED. 2 L 7 2 4F RT A20EU 1998122400355 19981224 00355 NM 1998 12 24 QXEA9802107 1 19981218 A 3350 BATTERY DHAV DHC8 DHC8102 2809003 NM CABIN DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 823PH 16954 98 110 EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS, OPERATIONAL CHECK GOOD. 2 H 7 2 4T RT A13NM 1998122400356 19981224 00356 NM 1998 12 24 98FDEA00756 1 19981221 A 5313 655623622 STRINGER BOEING 727 727247 138408F NM BS 580 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSON ON STR 28L, BS 580. *S/D* REPAIRED STRINGER 28L AT BS 580 PER FEDEX SRM 53-10-3. 2 L 7 3 4F A3WE 1998122400357 19981224 00357 EU 1998 12 24 98FDEA00757 1 19981222 A 7830 TR VALVE AIRBUS 300 A300F4605R 3930327 EU NR 1 ENGINE INOP A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 672FE 779 98-305 - LEFT REVERSER PRESSURIZE LIGHT ILLUM ON ECAM WITH MASTER CAUTION LIGHT ILLUM AT APPROX 60 PERCENT N1 AFT TOGA S ELECTED. REMOVED AND REPLACED NR 1 ENG T/R DIRECTIONAL PILOT VALVE AND PRESSURE SWITCH PER MM 78-31-06-2 PG 201. 2 L 7 2 4F RT A35EU 1998122400358 19981224 00358 WP 1998 12 24 ABXA9801187 1 19981220 A 5314 3917286503 KEEL BEAM DOUG DOUG DC9 DC932F 3022067 WP BS 737 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 DURING C-CHECK, FOUND KEEL BEAM CORRODED AND CRACKED IN THE RIGHT WHEEL WELL, AFT UPPER CORNER AT STATION 737. REPAIRED IAW ABX REA D953-25903MR. 2 L 7 2 4F A6WE 1998122400359 19981224 00359 WP 1998 12 24 ABXA9801188 1 19981221 A 5320 99101559 PAN DOUG DOUG DC9 DC932F 3022067 WP BS 718 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 905AX 47147 DURING C-CHECK, FOUND LEFT WHEEL WELL PRESSURE PANEL RETAINER PAN AT STATION 718 CORRODED. REPAIRED IAW ABX REA D953-25 980MR. 2 L 7 2 4F A6WE 1998122400360 19981224 00360 WP 1998 12 24 RRXA98958 1 19981004 A 5330 SKIN DOUG DC8 DC862F 3021972 WP BS 206-270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A PERFLIGHT INSPECTION, FOUND SEVERAL DESTROYED RIVET HEADS ON EXTERIOR SKIN SURFACE. PERFORMED VISAL INSPECTION OF INTERNAL SKIN SECTION, FOUND CORROSION AT STA 206 TO STA 270. RECEIVED AUTHORIZATION FOR (FERRY FLIGHT) FROM KDAY T O KMQY (TENNESSEE TECHNICAL SERVICES, LLC) FOR EVAUATION. FOUND SKIN DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMA GED SECTION IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED TEMPORARY REPAIR (200 HOURS) IAW FAA APPROVED DER TENNESSEE T ECHNICAL SERVICES EO 98-017. 2 L 7 4 4F 4A25 1998122400361 19981224 00361 NM 1998 12 24 VNAA9812010 1 19981220 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7 LK DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 432JS 62604 4519 3045 SEVERAL EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLAC ED EMERGENCY BATTERY PACK 7LK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETE D, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998122400363 19981224 00363 EU 1998 12 24 CA981028004 1 19981014 A 3230 200642005 ACTUATOR DOWTY 200642005 FOKKER F28 F28MK1000 4990808 EU LT MLG FAILED W A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 CA 8926 DRG157686 (CAN) ON APPROACH AND GEAR EXTENSION, THE LEFT MLG WOULD NOT INDICATE DOWN AND LOCKED, NO GREEN LIGHT. AIRCRAFT DIVERTE D AND LANDED USING ALTERNATE EXTENSION. AIRCRAFT TOWED TO HANGAR. LEFT HAND DOWNLOCK FAILED INTERNALLY. REPLACED. PA RT TC: 9,391. 2 L 7 2 4F RT A20EU 1998122400364 19981224 00364 EU 1998 12 24 CA981028006 1 19981025 A 2910 A71940023 ELBOW FOKKER F28 F28MK1000 4990808 EU HYDRAULIC SYSTEM CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA (CAN) AIRCRAFT LOST UTILITY HYDRAULIC SYSTEM SHORTLY AFTER TAKEOFF. AIRCRAFT DIVERTED AND LANDED SAFELY. AIRCRAFT TOWE D TO HANGAR. RIGHT ENGINE HYDRAULIC PUMP ELBOW CRACKED. REPLACED. 2 L 7 2 4F RT A20EU 1998122400366 19981224 00366 CE 1998 12 24 CA981028008 1 19981022 A 3240 MP50B1 MOTOR CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE POWER BRAKE FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 52 842 71751 (CAN) ON APPROACH, PILOT FAILED TO GET POWER BRAKE PRESSURE AND ANTI-SKID BREAKER TRIPPED. FURTHER INVESTIGATION FOUND A NEW POWER BRAKE MOTOR HAD FAILED. 1 L 7 2 4F 4 F A22CE E1NE 1998122400367 19981224 00367 CE 1998 12 24 CA981028010 1 19981005 A 6120 509104893 SUPPORT 509104713 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE ENGINE MISINSTALLED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA GGMPS0123 HJ549 (CAN) THE TWO CENTER HOLE BOSSES OF THE PRESSURE MANIFOLD SUPPORT PLATE ARE CHAFING AGAINST THE INNER SIDE OF THE PROPEL LER PRESSURE MANIFOLD DUE TO THE CLOSE TOLERANCE BETWEEN THE TWO PARTS. SUBMITTER STATED RAYTHEON HAS BEEN ADVISED OF T HIS CONDITION AND ARE CURRENTLY WORKING ON MORE ACCEPTABLE TOLERANCES. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1998122400370 19981224 00370 CE 1998 12 24 CA981030006 1 19980906 A 3230 11438800013 POWER PACK BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 6166 PCE114296 HJ448 (CAN) LANDING GEAR DID NOT RETRACT ON UP SELECTION. GEAR SELECTED DOWN AND GEAR INDICATION STILL SHOWED DOWN AND LOCKE D. MAINTENANCE PERSONNEL INSPECTED LANDING GEAR INTEGRITY IN THE DOWN AND LOCKED POSITION AND DISABLED THE GEAR DOWN AN D LOCKED. FURTHER TROUBLESHOOTING DETERMINED THE HYDRAULIC POWER PACK HAD FAILED. HYDRAULIC POWER PACK REPLACED AND RE TRACTION TESTS CARRIED OUT. PART TC: 10,017. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1998122400371 19981224 00371 EU 1998 12 24 CA981030007 1 19981015 A 2530 8201070000 OVEN AIRBUS 320 A320211 3930320 EU GALLEY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) AIRCRAFT RETURNED DUE TO ELECTRICAL SMELL IN CABIN, GALLEY POWER TURNED OFF, SMELL DISSIPATED. FOUND NR 3 GALLEY OVEN SENSORS DAMAGED. REPLACED RECIRCULATING FAN FILTERS AND AFT GALLEY OVEN VENT FILTERS, OVEN REPLACED, SYSTEM SERVI CEABLE. 2 L 7 2 4F RT A28NM 1998122400372 19981224 00372 NM 1998 12 24 CA981030008 1 19981011 A 2710 550030019 ACTUATOR BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE RT & LT AILERON FAILED W K NONE J WARNING INDICATION CR CRUISE 1 CA P707548 (CAN) AILERON LOCK OUT MESSAGE ON ENGINE INDICATING AND CREW ALERT SYSTEM AT 11,500 FEET AT 260 KNOTS. CHECK LIST COMPL ETED, MESSAGE DISAPPEARED AT FLAP SELECTION 1 AT 210 KNOTS. CHANGED LEFT AND RIGHT AILERON LOCK-OUT ACTUATORS, SYSTEM S ERVICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1998122400373 19981224 00373 1998 12 24 CA981030009 4 19981016 A 3452 G699211 CONTROL PANEL BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA P709662 (CAN) ON DEPARTURE, CREW REPORTED SMOKE COMING OUT OF TRANSPONDER PANEL WHEN LIGHT OVERRIDE SWITCH SELECTED ON. TRAFFIC CONTROL ALERT SYSTEM/AIR TRAFFIC CONTROL PANEL REPLACED, WIRING AND CONNECTOR CHECKED NO TRACE OF BURN, SYSTEM SERVICEA BLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1998122400374 19981224 00374 EU 1998 12 24 CA981030011 1 19981016 A 2121 CE1909AA1 EXTRACT FAN AIRBUS A340 A340313 EU CABIN MALFUNCTIONED W K NONE B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION IN INSP/MAINT 1 CA (CAN) WHEN ESTABLISHING EXTERNAL POWER VENT EXTRACT FAULT MESSAGE CAME ON ELECTRONIC CENTRALIZED AIRCRAFT SYSTEM FOLLOWE D BY ACRID SMELL. EXTRACT FAN OVERHEAT RESET, OPERATION NORMAL, OVERBOARD VALVE RETURNED TO NORMAL. REPLACED EXTRACT F AN ASSEMBLY AND OPERATION NORMAL. 2 L 7 4 4F RT A197 1998122400375 19981224 00375 EU 1998 12 24 CA981030012 1 19981002 A 5330 SKIN AIRBUS A340 A340313 EU BS 68-73 DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 6587 (CAN) ON TOUCH-DOWN, CABIN CREW REPORTED SCRAPING. MAINTENANCE INSPECTION REVEALED SKIN SCRAPED BETWEEN STN FR 68 AND F R 73 AT STR 53R/53L, DAMAGE AREA WAS APPROXIMATELY 3 FEET WIDE BY 7 FEET LONG. REPAIRED PER SRM. 2 L 7 4 4F RT A197 1998122400376 19981224 00376 NM 1998 12 24 CA981030013 1 19981018 A 3251 C202162282223 CONTROL UNIT AIRBUS A319 A319114 NM NLG STEERING FAILED W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA (CAN) DURING TAXI, BRAKE AND STEERING CONTROL UNIT MESSAGE CAME ON ENGINE INDICATING AND CREW ALERT SYSTEM. NOSE GEAR A NTI-SKID SWITCH RECYCLED AND AIRCRAFT MADE UNCONTROLLED RIGHT TURN FOLLOWED BY A HARD LEFT TURN. AIRCRAFT CAME TO A RE ST WITH NOSE GEAR 15 FEET OFF RUNWAY. CHANGED BRAKE AND STEERING CONTROL UNIT AND TESTED SERVICEABLE. REPLACED NR 4 BR AKE CARRIER AND BOTH NOSE WHEEL ASSEMBLIES. 2 L 7 2 4F RT A28NM 1998122400377 19981224 00377 EU 1998 12 24 CA981030015 1 19981011 A 4990 OIL COOLER AIRBUS 320 A320211 3930320 EU APU LEAKING W A B UNSCHED LANDING EMER. DESCENT B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA (CAN) EN ROUTE, CREW REPORTED ACRID SMELL IN COCKPIT. AT ALTITUDE, ELECTRONIC CENTRALIZED A/C MONITORING INDICATED SMOK E FROM LAVATORY FOR APPROX ONE SECOND. IN-FLIGHT PERSONNEL VERIFIED AREA NO SMOKE OBSERVED. 45 MINUTES LATER SMOKE IND ICATION OCCURRED, LAV CHECKED, 40 MILES LATER, 390 ALT SMOKE INDICATION CAME ON AGAIN, THIN HAZE OF ACRID SMOKE NOTICED IN CABIN AND COCKPIT. CREW DECLARED EMERGENCY AND LANDED. LAV SMOKE SYS TESTED OK. CARGO AND ELECT COMPARTMENTS CHECK ED OK. AIR COND SYS OK. AUX OIL LEAKING FROM OIL COOLER DUCT, REPLACED LAV SMOKE DETECTORS APU CONNECTOR P-2 APU, GROU ND RUN CARRIED OUT SERVICEABLE. 2 L 7 2 4F RT A28NM 1998122400378 19981224 00378 NE 1998 12 24 CA981030016 2 19980927 A 7322 FCU BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE NR 2 ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA (CAN) DURING CRUISE AT FL 390, NR 2 ENGINE POWER DROPPED SIGNIFICANTLY BELOW OTHER ENGINE. ALL NR 2 ENGINE PARAMETERS W ERE BELOW THE OTHER ENGINES. THE NR 2 ENGINE POWER LEVER WAS 2-3 INCHES AHEAD OF THE OTHER THREE, IN TRYING TO STABILIZ E POWER. NR 2 ENGINE RECOVERED ON FINAL. POST-FLIGHT, THE NR 2 ENGINE FUEL CONTROL UNIT AND THE HIGH PRESSURE FUEL PUM P WERE REPLACED. THE ENGINE TRIM RUN WAS CARRIED OUT SERVICEABLE. 2 L 7 4 4F 4 F A20WE E20EA 1998122400380 19981224 00380 CE 1998 12 24 CA981109001 1 19980930 A 2701 AN33A BOLT 15600273 CESSNA 206 U206G 2073356 CE MCAULY D3A34 D3A34C402 GL CONTROL COLUMN MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 3041 921099 (CAN) DURING OPS 4 INSPECTION, THE PILOTS CONTROL COLUMN WAS FOUND LOOSE. FURTHER INVESTIGATION FOUND ONE BOLT MISSING AND TWO OTHER BOLTS LOOSE. PART TC: 7,577. 1 H 7 1 3O A4CE 5 C P47GL 1998122400402 19981224 00402 EU 1998 12 24 CA981109041 1 19980922 A 3234 9462994106 FITTING 9603001271 PILATS PC12 PC12 7090550 EU NLG WHEEL WELL LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 153 (CAN) INTERMITTENT HYDRAULIC LEAK AROUND LINES AND FITTINGS IN THE NOSEWHEEL AREA WAS TRACED TO A LOOSE NUT THAT SECURES THE TEE FITTING TO THE HYDRAULIC SELECTOR VALVE. THE HYDRAULIC FLUID HAD SATURATED ALL THE INSULATION IN THE PEDESTAL AREA AND SOME OF THE CARPET. PART TC: 122. 1 L 7 1 3T RT A78EU 1998122400411 19981224 00411 NM 1998 12 24 CA981113015 1 19981101 A 2710 AILERON BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE WING FAILED W K NONE O OTHER AP APPROACH 1 CA P709673 (CAN) ON APPROACH TO TORONTO AT FL 60 WITH FLAPS AT 5, SPEED BRAKES FULLY EXTENDED, SELECTED FLAPS AT 15, AIRCRAFT SHAR P ROLL TO RIGHT, AILERONS 3 INDICIES LEFT TO KEEP A/C WING LEVEL, FLAPS RETURNED TO 5, NORMAL, NO ROLL, BACK TO FLAPS 15 DEGREES, SAME RESPONSE, SPEED BRAKES STOWED NORMAL. LUBRICATED LEFT AND RIGHT HAND AILERON DROOP MECHANISM WITH WATER DISPLACING OIL. REPLACED FLIGHT DATA RECORDER DUE TO INCIDENT. SYSTEM TESTED OK. 2 L 7 2 4F 4 F RT A1NM E3NE 1998122400413 19981224 00413 EU 1998 12 24 CA981113019 1 19981028 A 4920 APU AIRBUS 320 A320211 3930320 EU APU BAY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) SMOKE IN CABIN IN-FLIGHT. APU REPLACED AND APU DIFFUSER DUCTING WASHED, GROUND RUN CARRIED OUT, SYSTEM OK. 2 L 7 2 4F RT A28NM 1998122400415 19981224 00415 EU 1998 12 24 CA981113026 1 19981023 A 5210 DOOR AIRBUS 320 A320211 3930320 EU PASSENGER DOOR JAMMED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) L-1 CABIN DOOR JAMMING WHEN OPENING. ARM/DISARM UNAFFECTED. ADJUSTED UPPER AND LOWER GUIDE ARMS AND LUBRICATED. OPERATIONS CHECK OK. 2 L 7 2 4F RT A28NM 1998122400416 19981224 00416 NM 1998 12 24 CA981113027 1 19981015 A 5210 DOOR AIRBUS A319 A319114 NM PASSENGER DOOR OUT OF ADJUST W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) L-2 CABIN DOOR ARMING LEVER WHILE IN DIS-ARMED POSITION CAN STILL BE MOVED INTO ARMED POSITION WHILE PIN IS IN PLA CE. FOUND DISARM PIN RETAINER OUT OF ALIGNMENT. DISARM PIN RETAINER SHIMMED WITH HANDLE CAM TO CORRECT ALIGNMENT. OPE RATION CHECKED SERVICEABLE. 2 L 7 2 4F RT A28NM 1998122400417 19981224 00417 SW 1998 12 24 CA981116001 1 19981116 A 6220 471401104 STABILIZER 471401241 BELL 47 47G2 1181008 SW LYC O435 VO435A1E 41516 EA MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 707 L88131 (CAN) STABILIZER BAR CRACKED AT ROOT OF TUBE WHERE IT JOINS THE HEAD. 1 G 7 1 3O 3 O H1 E279 1998122400429 19981224 00429 EU 1998 12 24 CA981123002 1 19981104 A 6210 355A11002009 BLADE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3101 4495 (CAN) ON DAILY INSPECTION, CHORDWISE CRACK FROM TRAILING EDGE AT 130CM OUTBOARD FROM BLADE ROOT MOUNTING PIN. 1 G 7 1 3U 3 U NC H9EU E19EU 1998122400430 19981224 00430 NE 1998 12 24 CA981123004 1 19981111 A 6320 S613522017003 GEAR 613520600045 SKRSKY S61 S61N 8142104 NE GE CT58 CT581401 30011 NE M/R GEARBOX CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 600 A14J2265713 280016D (CAN) ON POST-FLIGHT INSPECTION, CRACK FOUND ON LOWER FLANGE OF THE MAIN GEARBOX RING GEAR. 2 G 7 2 4U 4 U 1H15 1E3 1998122400442 19981224 00442 SW 1998 12 24 CA981125030 1 19980715 A 6320 206040002025 TRANSMISSION BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 11893 796 B12199 CAE821569 (CAN) MAIN ROTOR TRANSMISSION MAKING METAL (FLAKES). THE TRANSMISSION INCREASED 25C. SLIGHT OIL PRESSURE DECREASE. 1 G 7 1 3U 3 U H2SW E4CE 1998122400443 19981224 00443 NE 1998 12 24 CA981125032 2 19980721 A 7250 SHIELD SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE TURBINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 194 956 (CAN) HEAT SHIELD FOUND CRACKED ON THE AFT EDGE. 1 G 7 1 3U 3 U H9EU E19EU 1998122400444 19981224 00444 GL 1998 12 24 CA981125033 2 19980728 A 7322 23034702 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 3538 CAE822231 (CAN) ENGINE REMAINS AT IDLE WHEN THROTTLE IS ADVANCED TO FULL POWER. 1 G 7 1 3U 3 U H2SW E4CE 1998122400445 19981224 00445 GL 1998 12 24 CA981125037 2 19980816 A 7532 23053176 VALVE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE LEAKING W O OTHER O OTHER IN INSP/MAINT 1 CA 1257 FF18446 CAE822647 (CAN) ENGINE FAILING THE POWER CHECKS. THE BLEED VALVE DIAPHRAGM WAS LEAKING. 1 G 7 1 3U 3 U H2SW E4CE 1998122400446 19981224 00446 GL 1998 12 24 CA981125045 2 19980929 A 7322 104900A45 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 273 CAE820800 (CAN) LIGHT OFF ADJUSTMENT WOULD NOT STAY WITHIN LIMITS DURING INSTALLATION. THE FUEL CONTROL WAS REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998122400447 19981224 00447 GL 1998 12 24 CA981125049 2 19980930 A 7313 AG10719 NOZZLE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL FUEL SYSTEM FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 2620 AG10719 CAE823424 (CAN) DURING INSPECTION, THE COMBUSTION LINER WAS FOUND TO HAVE HOT SPOTS. IT IS SUSPECTED THAT POOR SPRAY PATTERN OF T HE FUEL NOZZLE CAUSED THIS PROBLEM. THE SUBMITTER STATES THAT THE FUEL NOZZLE WAS ON A TBO EXTENSION. 1 G 7 1 3U 3 U H2SW E4CE 1998122400448 19981224 00448 GL 1998 12 24 CA981125051 2 19981008 A 7322 23034702 FCU BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAULTY W K NONE O OTHER IN INSP/MAINT 1 CA 283 3AAC2530 CAE820800 (CAN) THE FUEL CONTROL WAS INSTALLED FOR 54.3 HOURS AND WAS ADJUSTED SEVERAL TIMES DUE TO POOR STARTING. THE UNIT WOULD WORK WELL FOR A FEW STARTS AND THEN REQUIRE RE-ADJUSTMENT. THE FUEL CONTROL UNIT WAS REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1998122400450 19981224 00450 WP 1998 12 24 CA981125056 2 19981020 A 7261 31080261 PUMP SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NR 2 ENGINE FAILED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 973 96P14360 P54259 (CAN) DURING CRUISE, THE NR 2 ENGINE OIL PRESSURE WAS FLUCTUATING AND ON FINAL, DROPPED TO 40 PSI, THE AIRCRAFT LANDED W ITHOUT INCIDENT. POST-FLIGHT INSPECTION FOUND THE OIL LEVEL LOW DUE TO HIGH OIL CONSUMPTION, CAUSED BY THE FAILURE OF T HE REAR OIL SCAVENGE PUMP. FURTHER INSPECTION FOUND THE PUMP DRIVE SHAFT AND BUSHING HAD BACKED OUT OF THE PUMP HOUSING CAUSING THE PUMP TO FAIL. 2 L 7 2 4T 4 T RT A8SW E4WE 1999010100001 19990101 00001 WP 1999 1 1 VJ9800679 1 19981221 A 5260 INTERCOASTAL DOUG DC9 DC932 3022066 WP VENTRAL STAIRS CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND AFT VENTRAL STAIRS LEFT OUTBOARD WEB HAS CORROSION ON UPPER SURFACE AFT END 70 INCHES FORWARD. ALSO, A WEB WITH FASTENER HOLES WITH NO EDGE DISTANCE AND ALL 7 HORIZONTAL INTERCOASTAL AND SHEAR C LIPS CORRODED. REMOVED AND REPLACED ALL INTERCOASTALS THAT WERE OUT OF LIMITS, TREATED ALL CORROSION AND INSTALLED ALL NEW MEMBERS IAW DC9 SRM 51-30-2, 52-01 FIG 1, AND AIRTRAN RES 982287. 2 L 7 2 4F A6WE 1999010100002 19990101 00002 NM 1999 1 1 RAAA98B1098 1 19981223 A 3350 873100212 LIGHT BOEING 727 72722C 138400F NM CABIN FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 MID CABIN EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 3 4F A3WE 1999010100003 19990101 00003 NM 1999 1 1 RAAA98B1099 1 19981213 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 AFT EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999010100004 19990101 00004 NM 1999 1 1 RAAA98B1100 1 19981223 A 3350 900835A BATTERY PACK GRIMES 1000679 BOEING 727 72722C 138400F NM CABIN DISHCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 MID CABIN OVERHEAD EMERGENCY LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999010100005 19990101 00005 NM 1999 1 1 RAAA98B1101 1 19981223 A 3350 900835A BATTERY PACK GRIMES 1000679LB BOEING 727 72722C 138400F NM EMER EXIT DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT FWD AND AFT EXTERNAL OVERWING EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 3 4F A3WE 1999010100006 19990101 00006 SO 1999 1 1 RAAA98E8028 1 19981222 A 3350 S106 BATTERY PACK GRIMES 1102832 LKHEED 188 188C 5262604 SO ROW 7,10,11 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 OVERHEAD EMERGENCY LIGHTS AT PAX ROWS 7, 10 AND 11 FAILED SERVICE CHECK. CHANGED BATTERY PACKS DUE DISCHARGED. 2 L 7 4 4T 4A22 1999010100007 19990101 00007 NM 1999 1 1 CALA9802189 1 19981221 A 3260 SWITCH BOEING 737 7373T0 1384582 NM NLG INOPERATIVE A CALA O OTHER N FALSE WARNING AP APPROACH 1 SW 09 17309 23360 THE NOSE GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN GEAR WAS EXTENDED FOR LANDING AT PBI. THE GEAR WAS CYCLED, BUT THE RED LIGHT DID NOT EXTINGUISH. A MANUAL GEAR EXTENSION WAS PERFORMED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAI NTENANCE FOUND THE NOSE GEAR LOCK PROXIMITY SWITCH AT FAULT. THE NOSE GEAR LOCK PROXIMITY SWITCH WAS REPLACED AND TESTE D GOOD IAW MM 32-09-20, PAGE 420. 2 L 7 2 4F RT A16WE 1999010100008 19990101 00008 WP 1999 1 1 CALA9802190 1 19981221 A 5230 PAN DOUG DC9 DC982 3022082 WP CARGO DOOR CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND A 1 CRACK IN AFT CARGO DOOR PAN. A DOUBLER WAS INSTALLED IAW SRM 52-05, FIGURE 26A. 2 L 7 2 4F A6WE 1999010100009 19990101 00009 WP 1999 1 1 CALA9802191 1 19981222 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 737 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND TWO 2 CRACKS IN LONGERON 5R AT STA 737. A NEW LONGERON AND SPLICE DOUBLERS WERE INSTALLED IAW SRM 53-0 2. 2 L 7 2 4F A6WE 1999010100010 19990101 00010 WP 1999 1 1 CALA9802192 1 19981222 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 756 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND TWO 1 CRACKS IN LONGERON 5R AT STA 756. A NEW LONGERON AND DOUBLERS WERE INSTALLED IAW SRM 53-02. 2 L 7 2 4F A6WE 1999010100011 19990101 00011 NE 1999 1 1 CALA9802193 2 19981222 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE NR 1, 2 ENGINE DAMAGED A CALA A E UNSCHED LANDING ENGINE SHUTDOWN C J F.O.D. WARNING INDICATION TO TAKEOFF 1 SW 09 477AC 48062 709755 THE NR 1 AND NR 2 ENGINES INGESTED ICE ON TAKEOFF FROM CLE AND ON ROTATION THE NR 1 ENGINE EPR FELL TO 1.1. THE NR 1 EN GINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH ENGINE S HAD FAN BLADE DAMAGE DUE TO THE IMPACT OF ICE INGESTION. THE DAMAGED FAN BLADES WERE REMOVED AND REPLACED ON BOTH ENG INES. 2 L 7 2 4F 4 F A6WE E9NE 1999010100012 19990101 00012 WP 1999 1 1 9810959921 1 19981220 A 2130 PRESSURIZATION DOUG DC9 DC932 3022066 WP CABIN MALFUNCTIONED A NWAA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 GL 01 943N 47647 LOSS OF CABIN PRESSURIZATION OCCURRED AFTER TAKEOFF AT 15000 FEET. CABIN ALTITUDE WAS PEGGED OUT AND OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN. FLIGHT ATTENDANT ALSO REPORTED SMOKE IN CABIN. CREW DECLARED AN EMERGENCY AND AIRCRAFT WAS RETURNED TO DTW WITHOUT INCIDENT. MAINTENANCE REPLACED LEFT AND RIGHT TURBINE INLET SWITCHES, COMPRESSOR DISCHARGE SWIT CHES, PRESSURE CONTROLLER, PRESSURE AMPLIFIER, AND OUTFLOW VALVE ACTUATOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999010100013 19990101 00013 WP 1999 1 1 9810969937 1 19981221 A 3260 301350101B PSEU DOUG DC9 DC931 3022065 WP GEAR DOOR MALFUNCTIONED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 908H 2471 754 47517 DURING APPROACH INTO TYS, LANDING GEAR DOOR OPEN LIGHT REMAINED ON AFTER GEAR EXTENSION. CREW RECYCLED GEAR WITH SAME R ESULTS. EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED P SEU PROCESSOR. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999010100014 19990101 00014 NM 1999 1 1 UPS98428302 1 19981222 A 3350 900835A BATTERY PACK BOEING 747 747121 1384871 NM CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 691UP 19641 UPPER DECK ESCAPE SLIDE EMERGENCY LIGHTS INOP. REPLACED UPPER DECK ESCAPE SLIDE EMERGENCY LIGHTS BATTERY PACK. 2 L 7 4 4F A20WE 1999010100015 19990101 00015 WP 1999 1 1 UPS98828301 1 19981221 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 810UP 46001 EEL ONLY STAY ON FOR A FEW SECONDS IN TEST. REMOVED AND REPLACED BATT PACK, OPS CHECK GOOD P/N ON 5708458-503 P/N OFF 6 0-1223-5 S/N ON FTL 1007 S/N OFF 327. 2 L 7 4 4F RT 4A25 1999010100016 19990101 00016 WP 1999 1 1 UPS98828304 1 19981222 A 3350 CONNECTOR DOUG DC8 DC871F 302199D WP CABIN LOOSE A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 709UP 45914 EMERGENCY LIGHTS DISARM CHECK SWITCH IS INTERMITTENT. TIGHTENED LOOSE TERMINAL ON EMERGENCY LIGHT SWITCH, OPS CHECK. 2 L 7 4 4F RT 4A25 1999010100017 19990101 00017 WP 1999 1 1 UPS98828305 1 19981223 A 3350 BATTERY PACK DOUG DC8 DC873F 302199F WP CABIN DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 866UP 45966 EMERGENCY LIGHT FAILED TO WORK DURING PRE-FLIGHT CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK FOR EMERGENCY LIGHT S. OPS CHK GOOD. 2 L 7 4 4F RT 4A25 1999010100018 19990101 00018 WP 1999 1 1 UPS98828306 1 19981222 A 3260 SWITCH DOUG DC8 DC871F 302199D WP LT MLG FAILED A IPXA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 SO 01 713UP 46014 LEFT MAIN LANDING GEAR LIGHTS INOP. CHANGED BULBS TWICE STILL NO LIGHTS. TOWER VERFIED DOWN. CHECKLIST RAN, ALL GEAR WERE PINNED AFTER LANDING. REMOVED AND REPLACED LEFT MLG DOWNLOCK SWITCH. OPS NORM. 2 L 7 4 4F RT 4A25 1999010100019 19990101 00019 EU 1999 1 1 QXEA9801790 1 19981119 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT INBOARD SEAT TRACK CORROSION ON TOP INBOARD SIDE AFT OF STATION 4900. REPAIRED IAW FOKKER MM 53-40-01, FIGUR E 204. 2 L 7 2 4F RT A20EU 1999010100020 19990101 00020 EU 1999 1 1 QXEA9801791 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - RIGHT OUTBOARD SEAT TRACK CORROSION ON TOP OUTBOARD SIDE AFT OF STATION 4900. REPAIRED IAW FOKKER MM 53-40-01, FI GURE 204. 2 L 7 2 4F RT A20EU 1999010100021 19990101 00021 EU 1999 1 1 QXEA9801792 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU BS 4900 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION 1 AFT OF STATION 4900 ON INBOARD TOP SIDE OF LEFT INBOARD SEAT TRACK. REPAIRED IAW FOKKER MM 53-40-01, FIGURE 204. 2 L 7 2 4F RT A20EU 1999010100022 19990101 00022 EU 1999 1 1 QXEA9801793 1 19981115 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 13815B BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100023 19990101 00023 EU 1999 1 1 QXEA9801794 1 19981114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 15205 BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100024 19990101 00024 EU 1999 1 1 QXEA9801795 1 19981114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 15205 BETWEEN STRINGERS 48 AND 49. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100025 19990101 00025 EU 1999 1 1 QXEA9801796 1 19981107 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - FRAME CLIP DAMAGED AT STATION 13815A AND STRINGER 15. REPAIRED IAW FOKKER SRM 51-31-01, 51-11-04. 2 L 7 2 4F RT A20EU 1999010100026 19990101 00026 EU 1999 1 1 QXEA9801797 1 19981127 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100027 19990101 00027 EU 1999 1 1 QXEA9801798 1 19981115 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100028 19990101 00028 EU 1999 1 1 QXEA9801799 1 19981114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 28 AND 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100029 19990101 00029 EU 1999 1 1 QXEA9801800 1 19981114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 13815A BETWEEN STRINGERS 27 AND 28. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100030 19990101 00030 EU 1999 1 1 QXEA9801801 1 19981114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 13815 BETWEEN STRINGERS 33 AND 34. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100031 19990101 00031 EU 1999 1 1 QXEA9801802 1 19981114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 13815 BETWEEN STRINGERS 32 AND 33. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100032 19990101 00032 EU 1999 1 1 QXEA9801803 1 19981118 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU BS 5805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LARGE CRACK IN STRINGER 16 JUST AFT OF FRAME 5805. REPAIRED IAW FOKKER SRM 53-02-16, FIGURE 1. 2 L 7 2 4F RT A20EU 1999010100033 19990101 00033 EU 1999 1 1 QXEA9801804 1 19981106 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 5305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 5305 BETWEEN STRINGERS 48 AND 49. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100034 19990101 00034 EU 1999 1 1 QXEA9801805 1 19981108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 8305 BETWEEN STRINGERS 31 AND 32. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100035 19990101 00035 EU 1999 1 1 QXEA9801806 1 19981115 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 8305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 8305 BETWEEN STRINGERS 44 AND 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100036 19990101 00036 EU 1999 1 1 QXEA9801807 1 19981108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 8805 BETWEEN STRINGERS 31 AND 32. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100037 19990101 00037 EU 1999 1 1 QXEA9801808 1 19981108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 8805 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 8805 BETWEEN STRINGERS 44 AND 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100038 19990101 00038 EU 1999 1 1 QXEA9801809 1 19981108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 9305 BETWEEN STRINGERS 44 AND 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100039 19990101 00039 EU 1999 1 1 QXEA9801810 1 19981108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 9305 BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100040 19990101 00040 EU 1999 1 1 QXEA9801811 1 19981108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 9305 BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100041 19990101 00041 EU 1999 1 1 QXEA9801812 1 19981108 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 9305A BETWEEN STRINGERS 45 AND 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100042 19990101 00042 EU 1999 1 1 QXEA9801813 1 19981113 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 9305A BETWEEN STRINGERS 46 AND 47. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100043 19990101 00043 EU 1999 1 1 QXEA9801814 1 19981114 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 9305 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK IN CLIP AT FRAME 9305A BETWEEN STRINGERS 28 AND 29. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010100044 19990101 00044 EU 1999 1 1 98FDEA00758 1 19981223 A 7830 CONNECTOR AIRBUS 300 A300F4605R 3930327 EU NR 1 ENG TR UNIT DIRTY A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 25 663FE 766 98-306 NR 1 ENG REVERSER PRESS ECAM WARN ILLUM AT T/O ROLL. ABORT T/O CYCLED REVERSER LEVER. LIGHT ECAM REILLUM ON 2N D T/O ATTEMPT. ABORT AGAIN AND RETURN TO RAMP. CLEANED CANNON PLUG ON DIRECTIONAL PILOT VALVE AND SWITCH. HEATED VALV E AT NR 1 ENGINE. REF 78-31-00. 2 L 7 2 4F RT A35EU 1999010100045 19990101 00045 NM 1999 1 1 98FDEA00759 1 19981223 A 2612 SMOKE DETECTOR BOEING 727 7272S2F 1384O81 NM CARGO COMPT INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 208FE 22930 98-307 - MAIN CARGO SMOKE DET POS NR 4 CAME ON IN FLT. REMOVED AND REPLACED DET PRECAUTIONARY FOR RETURN BK DUE TO NR 4 SMOKE DET LIGHT ON DURING CLIMB-OUT. RAMP INSP ALL CARGO FOR EVIDENCE OF SMOKE, NONE FOUND. CARGO SMOKE DETECTION SYS TEST NORM ON GRND. ALL WORK DONE IAW MM CHAPTER 26-16-1,PG 401 2 L 7 3 4F A3WE 1999010100046 19990101 00046 WP 1999 1 1 98FDEA00760 1 19981222 A 5754 SKIN DOUG DC10 DC1030F 3023504 WP NR 1 LE SLAT DAMAGED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 320FE 47835 ON WALKAROUND FOUND LT NR 1 L/E SLAT INBD FAIRING MISSING. ALSO, DAMAGE TO L/E SLAT ASSY. *S/D* REPLACED NR 1 L/E SLA T (LT) ASSY WITH FAIRING PER MM 27-80-01-4. 2 L 7 3 4F RT A22WE 1999010100047 19990101 00047 NM 1999 1 1 98UAL900550 1 19981119 A 2781 H1010621 SWITCH BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 LE FLAP FAILED A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 7461U 21915 IN CLIMB, LEADING EDGE AMBER LIGHT ILLUMINATED WITH FLAPS IN RETRACTED POSITION. TEST INDICATED NR 2 LEADING EDGE KRUGE R FLAP IN TRANSIT LIGHT ON. RETURNED TO ORD. CHECKED OPERATION SEVERAL TIMES. NO DEFECT OF LIGHTS PROBLEMS FOUND. SU SPECT POSSIBLE ICE ACCUMULATION. ACTUATOR NORMAL TO FEEL. NO INTERNAL LEAKAGE NOTED. REPLACED NR 2 FLAP SWITCH PER MM AND LEADING EDGE FLAP MODULE. INSPECTED WIRING TO SWITCH. LEADING EDGE LIGHT SYSTEM OP CHK'S NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999010100048 19990101 00048 NM 1999 1 1 98UAL900567 1 19981124 A 5240 MECHANISM BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE SERVICE DOOR WORN A UALA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 29 7462U 21916 FORWARD SERVICE DOOR LIGHT CAME ON. INSIDE D00R HANDLE POPS TOWARDS OPEN 3 TO 4 INCHES FROM LOCKED POSITION. TRIED TO PUSH HANDLE DOWN BUT IT POPPED BACK UP. DOOR 1R WAS ADJUSTED PER MM/OV 70-52-11-00. UPPER LATCH CAM WAS BACKED UP TWO SERRATIONS TO COMPENSATE FOR WEAR TO LOWER RAMP OF LATCH CAM FITTINGS. 2 L 7 3 4F 4 F A3WE E2EA 1999010100049 19990101 00049 NM 1999 1 1 98UAL900599 1 19981211 A 2613 OVERHEAT LIGHT BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT PACK ILLUMINATED A UALA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 WP 29 357UA 24378 DUCT OVERHEAT INDICATION. RAN LEFT PACK ON GROUND PER MAINTENANCE MANUAL SERVICE TIP 21-61-99-PG200 SYSTEM CHECK'S OKAY , NO FAULTS FOUND. 2 L 7 2 4F 4 F RT A16WE E2GL 1999010100051 19990101 00051 1999 1 1 98UAL900601 4 19981211 A 3425 PFD AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE LT COCKPIT MALFUNCTIONED A UALA O OTHER O OTHER CR CRUISE 1 WP 29 419UA 487 CAPTAIN'S PFD INTERMITTENTLY NOT VISIBLE. *S/D* SYSTEM TESTED GOOD NOTHING WAS REPLACED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999010100052 19990101 00052 NM 1999 1 1 98UAL900602 1 19981212 A 2131 CONTROLLER AIRESEARCH 7638101 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN FAILED A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 7269U 21416 UNABLE TO STABILIZE CABIN PRESSURE. RETURNED TO FIELD. *S/D* THE PRESSURE SELECTOR PANEL AND THE CABIN PRESSURE CONTROL LER WERE REPLACED. 2 L 7 3 4F 4 F A3WE E2EA 1999010100053 19990101 00053 NM 1999 1 1 98UAL900603 1 19981216 A 2910 O RING AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE YELLOW HYD SYST FAILED A UALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 806UA 788 LOST YELLOW SYS HYD QTY, NO QTY OR PRESS, TURNED PUMP OFF. DIVERTED TO DEN. *S/D* FOUND O-RING DAMAGED AT COUPLING QUIC K DISCONNECT ON YELLOW MAIN HYDRAULIC POWER REF IPC 29-13-03. REPLACED O-RING PER MM 29-13-15, OPS CK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 1999010100054 19990101 00054 NM 1999 1 1 98UAL900605 1 19981211 A 7312 51R418 SERVO SERCK BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE FUEL HEATER FAILED A UALA A UNSCHED LANDING M OVER TEMP CL CLIMB 1 WP 29 778UA 26940 777019 DURING CLIMB-OUT AFTER TAKEOFF, RIGHT ENGINE OIL EICAS MESSAGE, AND OIL TEMP RED-LINE. ENGINE WAS REMOVED DUE TO OIL O VERTEMP AND FUEL IN OIL. SERVO FUEL HEATER (P/N 51R418) WAS FOUND FAILED. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999010100055 19990101 00055 NM 1999 1 1 DHL98707004 1 19981222 A 5242 DOOR BOEING 727 72722 1384002 NM E & E COMPT NOT SECURED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 707DH 18321 ON CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO CVG. FOUND E/E DOOR AJAR. CLOSED DOOR AND DEFERRED WARNING L IGHT. 2 L 7 3 4F A3WE 1999010100056 19990101 00056 NM 1999 1 1 DHL98727004 1 19981222 A 2781 H1010261 SWITCH BOEING 727 727228 NM NR 4 LE FLAP FAILED A DHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 727DH 20204 NR 4 LEADING EDGE FLAP AMBER LIGHT ON BOTH FWD PANEL AND AFT PANEL WITH FLAPS UP ACCELERATING TO 300 KTS. REMOVED AND REPLACED FLAP SWITCH. 2 L 7 3 4F A3WE 1999010100070 19990101 00070 CE 1999 1 1 98ZZZX4709 1 19981122 A 5610 1013840258 WINDSHIELD BEECH 200 200BEECH 1152920 CE COCKPIT CRACKED A HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 789DS BB478 RIGHT WINDSHIELD OUTER PANE CRACKED IN-FLIGHT. RETURNED TO LAFAYETTE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED ASSEMBLY. REF: BEECHCRAFT IPC, FIGURE 56-10-01, ITEM 1. 1 L 7 2 4T A24CE 1999010100100 19990101 00100 GL 1999 1 1 98ZZZX4739 2 19980912 A 7323 23004832 GOVERNOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL ENGINE FAILED A BRNA A R UNSCHED LANDING AUTOROTATION R PARTIAL RPM/PWR LOSS HO HOVERING 1 GL 15 52BH 6402 87401765 1652 CAI540516 WHILE PERFORMING FIRE FIGHTING FOR DNR, PILOT FILLED BUCKET AND STARTED CLIMB, ENGINE LOST POWER. PILOT DUMPED WATER WH ICH BROUGHT ROTOR POWER-UP. PILOT WAS ABLE TO GET HELICOPTER TO SHORE. HELICOPTER AUTOROTATED AND STRUCK METAL TREE ST AKE DAMAGING TAIL ROTOR, DRIVESHAFT, AND TAIL SECTION. 1 G 7 1 3U 3 U H2SW E4CE 1999010100102 19990101 00102 GL 1999 1 1 98ZZZX4741 2 19980902 A 7250 67844193 SEAL BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20 03013 GL NR 1 ENGINE FAILED A HEEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 03 8197X CAT33569 S808 CAE835389 IN CRUISE FLIGHT, NR 1 ENGINE OIL PRESSURE BEGAN TO DROP. PILOT SECURED ENGINE, PROCEEDED ON TO SHORE BASE AND LANDED W ITHOUT INCIDENT. MAINTENANCE FOUND OIL LEAK AT NR 647 SCAVAGE STRUT. REF: G-20 IPC, CHAPTER 72-50-00, FIGURE 1, ITEM 32. 1 G 7 2 3U 3 U H3EU E4CE 1999010100104 19990101 00104 EU 1999 1 1 98ZZZX4743 1 19981012 A 3340 AF02AR LENS BOLKMS 105 BO105CBS 5626008 EU STROBE CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 493HL S809 DAILY INSPECTION FOUND LENS SPLIT APART AT SEAM. 1 G 7 2 3U NC H3EU 1999010100105 19990101 00105 1999 1 1 98ZZZX4744 4 19981012 A 2561 WABH12 BATTERY BELL 206 206L4 1182110 SW EMERGENCY LIGHT DAMAGED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 170AL 52063 90-DAY LIFE VEST INSPECTION FOUND MOISTURE GETS PLUGS AND CAUSES BATTERY CASE TO SWELL AND WIRE CONNECTION TO LIGHT TO P USH OUT OF CASE. 1 G 7 1 3U NC H2SW 1999010100106 19990101 00106 NE 1999 1 1 98ZZZX4745 1 19981001 A 7334 7645001078N9 TRANSMITTER SKRSKY S76 S76 8143010 NE ALLSN 250C 250C30S 03013 GL ENGINE FUEL MALFUNCTIONED A HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 5426U 4195363 760167 CAE8905085 ON TAKEOFF, NR 2 ENGINE TORQUE DROPPED WITH A CONTINUING RISE IN ENGINE TEMPERATURE. PILOT RETARDED NR 2 ENGINE AND MAD E UNEVENTFUL LANDING. MAINTENANCE FOUND DEFECTIVE NR 2 ENGINE TORQUE TRANSMITTER. REF: ALLISON C-30 IPC, CHAPTER 73-3 1-00, FIGURE 1-18. 1 G 7 2 3U 3 U H1NE E1GL 1999010100107 19990101 00107 NE 1999 1 1 98ZZZX4746 2 19981028 A 7200 3017600 ENGINE BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE NR 2 FAILED A HEEA E A ENGINE SHUTDOWN UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 SW 03 1082G 13583 2161 31109 CPPS62048 ON 10-28-98 DURING RECONNAISSANCE OF OGLNY, CA, FIRE NOTICED, RPM LOW 97 PERCENT, THEN NOTICED LARGE TORQUE SPLIT. WITH N1 ON NR 2 ENGINE AT IDLE AND ITT 900 DEGREES CELSIUS, PILOT WENT TO MANUAL THROTTLE, BUT NO RESPONSE BY ENGINE. 1 G 7 1 4U 4 U H4SW E22EA 1999010100111 19990101 00111 GL 1999 1 1 98ZZZX4750 2 19980917 A 7210 70010L275W210 LINE BELL 412 412 1182202 SW ALLSN 250C 250C30 03013 GL TRANSMISSION CHAFED A HEEA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 03 3893L 33006 WHILE IN CRUISE FLIGHT, TRANSMISSION OIL RPESSURE INDICATOR STARTED TO SHOW LOW PRESSURE. DIVERTED TO HI-264 FOR MAINTE NANCE. AIRCRAFT ASISGNED TO CAMERON BASE. REPLACED HOSE ASSEMBLY. REF: 412 IPC, CHAPTER 63-99-00, PAGE 22, FIGURE 63 -6, ITEM 49. 1 G 7 2 4U 3 U H4SW E1GL 1999010100113 19990101 00113 GL 1999 1 1 98ZZZX4752 2 19981021 A 7323 25246929 GOVERNOR BENDIX SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 MALFUNCTIONED A HEEA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 03 1547D 5869 1879 BR40238 760077 CAE890607S ON 10-27-98 DURING DEPARTURE FROM LAFAYETTE BASE, EXPERIENCED NR 2 ENGINE HIGH SIDE FAILURE. RETURNED FOR MAINTENANCE. REPLACED NR 2 GOVERNOR. 1 G 7 2 3U 3 U H1NE E1GL 1999010100117 19990101 00117 NE 1999 1 1 98ZZZX4756 1 19981019 A 2497 WIRE SKRSKY S76 S76A 8143006 NE COCKPIT FAILED A ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 5427S 760168 PILOT SMELLED BURNING WIRES IN THE COCKPIT, CONTINUED TO NORMAL LANDING. REPAIRED BURNT WIRES IN PILOT'S OVERHEAD COMPA RTMENT. 1 G 7 2 3U H1NE 1999010100118 19990101 00118 1999 1 1 98ZZZX4757 4 19981014 A 3420 700466915 ADI SKRSKY S76 S76A 8143006 NE E/E BAY MALFUNCTIONED A ALGA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 03 519AL 81067730 760058 DURING CLIMB-OUT, SMOKE WAS NOTICED IN THE COCKPIT. FOUND COPILOT'S ADI DEFECTIVE. REMOVED AND INSTALLED SERVICEABLE U NIT. 1 G 7 2 3U H1NE 1999010100119 19990101 00119 GL 1999 1 1 98ZZZX4758 2 19981117 A 7250 5233333 FUEL NOZZLE BELL 206 206B3 1181506 SW ALLSN 250C 250C20B 03013 GL ENGINE FAILED A AWTA O OTHER R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 WP 25 67PJ 1793 AG1113 3966 DURING EXTERNAL LOAD OPS, ENGINE RPM WENT TO APPROXIMATELY 60 PERCENT N2. LOAD WAS DROPPED AND RPM CAME BACK TO 95 PERC ENT. AIRCRAFT WAS FLOWN APPROXIMATELY 1/4 MILES TO LZ, BUT WOULD NOT HOLD RPM TO HOVER. FOUND FILTER IN FUEL NOZZLE CO LLAPSED. 1 G 7 1 3U 3 U H2SW E4CE 1999010100123 19990101 00123 NM 1999 1 1 TWAA9820101 1 19981225 A 3350 900835A BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54349 21968 FOUND THE MID CABIN EXIT SIGN FLICKERS DURING TEST, AND AISLE EXIT SIGN AT AFT GALLEY INOP. REPLACED THE BATTERY PACK A T BOTH LOCATIONS. CHECK-C 10-18-98 MCI. 2 L 7 3 4F A3WE 1999010100124 19990101 00124 WP 1999 1 1 TWAA9820102 1 19981221 A 5320 SPLICE DOUG DC9 DC931 3022065 WP BS 980 MISINSTALLED A TWAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND SPLICE ON FORMER NOT PER SRM AT STR 18L, STA 980. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR PER SRM 53--03, FIG 32 SHEET 4 AND 5, PAGE 135 AND 136. 2 L 7 2 4F A6WE 1999010100125 19990101 00125 WP 1999 1 1 VJ9800682 1 19981213 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERT STAB CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE VERTICAL STAB PANEL (DOG HOUSE) CHAFFING AT THE LEFT HAND AFT SECTION. FABRICATED AND INSTALLED NEW PANEL IAW DC9 SRM 51-10-3, 51-30-3, 55-31-0, AND AIRTRAN RES 982127. 2 L 7 2 4F A6WE 1999010100126 19990101 00126 WP 1999 1 1 VJ9800683 1 19981223 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 399 CUT A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION AT AERO CORP, FL, TORQUE BOX DOUBLER AT FORWARD CARGO DOOR STA 399 FOUND CUT ALONG 18R AND 20R. IN STALLED INTERNAL TITANIUM DOUBLER IAW DC9 SRM 53-04 FIG 38 AND RES 982282. 2 L 7 2 4F A6WE 1999010100127 19990101 00127 WP 1999 1 1 VJ9800684 1 19981209 A 5320 1A403191 FILLER DOUG DC9 DC932 3022066 WP AFT LAVATORY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 919VV 47260 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION ON AFT LAVATORY VANITY TO BE OUT OF LIMITS. REMOVED OLD FILLER, FABRICATED AND INSTALLED NEW FILLER IAW DC9 SRM 51-10-04, 51-10-3, AND 51-30-2. 2 L 7 2 4F A6WE 1999010100128 19990101 00128 NM 1999 1 1 CALA9802196 1 19981224 A 3020 ANTI ICE DUCT BOEING 727 727243 138408D NM NR 3 ENGINE BROKEN A CALA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SW 09 17407 21270 THE NR 3 ENGINE FIRE WARNING LIGHT CAME ON DURING CLIMB-OUT OF IAH. THE ENGINE POWER WAS REDUCED AND THE LIGHT EXTINGUI SHED. WHEN POWER WAS ADVANCED THE WARNING LIGHT CAME ON AGAIN. THE NR 3 ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS RETUR NED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE NOSE COWL ANTI-ICE DUCTING BROKEN. THE BROKEN DUCT WAS REMOVED AND REPLACED. LEAK CHECKS WERE GOOD. 2 L 7 3 4F RT A3WE 1999010100129 19990101 00129 WP 1999 1 1 CALA9802197 1 19981225 A 2612 FIRE LOOP DOUG DC10 DC1010 3022110 WP NR 1 ENGINE DAMAGED A CALA A J F UNSCHED LANDING DUMP FUEL ACTIVATE FIRE EXT. N FALSE WARNING CL CLIMB 1 SW 09 68044 46903 THE NR 1 ENGINE 'A' LOOP FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM IAH. THE THROTTLE WAS PULLED BACK AND THE AM BER LIGHT AT FUEL START LEVER WENT OUT. FIRE HANDLE NR 1 WAS PULLED, BUT BOTTLE NR 2 DID NOT DISCHARGE. BOTTLE NR 1 WA S SELECTED AND DISCHARGED. ALL ENGINE INDICATIONS WERE NORMAL. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO IAH WH ERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE WIRE HARNESS ON NR 1 ENGINE FIRE DETECTOR A LOOP AT FAULT. THE W IRE HARNESS WAS REMOVED AND REPLACED. THE NR 1 AND NR 2 ENGINES WERE RUN AT TAKEOFF POWER FOR 20 MINUTES WITH NO FAULTS NOTED. IN ADDITION, THE FIRE BOTTLES WERE REPLACED. 2 L 7 3 4F A22WE 1999010100130 19990101 00130 WP 1999 1 1 CALA9802198 1 19981224 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A .75 INCH CRACK IN FLOORBEAM AT STA 680, LONGERON 18R. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2. 2 L 7 2 4F A6WE 1999010100131 19990101 00131 WP 1999 1 1 CALA9802199 1 19981227 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1105 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND FOUR .5 INCH CRACKS IN CANTED FRAME AT STA 1105, LONGERON 3L, 4L, 5L, AND 3R. THE FRAME WAS REPLACED WI TH A NEW CANTED FRAME IAW SRM 51-30-1, 51-30-2, AND 51-30-5. 2 L 7 2 4F A6WE 1999010100132 19990101 00132 WP 1999 1 1 CALA9802200 1 19981228 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 680 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND A 4 INCH CRACK IN FLOORBEAM AT STA 680, LONGERON 18L. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 5 1-30-2. 2 L 7 2 4F A6WE 1999010100133 19990101 00133 SO 1999 1 1 COMA9810287 1 19981222 A 3230 RETRACT MECH EMB 120 EMB120RT SO LT MLG MALFUNCTIONED A COMA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 01 249CA 120230 LEFT MLG DID NOT RETRACT. COULD NOT DUPLICATE, C/W GEAR SWINGS AND NO DEFECTS FOUND. 2 L 7 2 4T RT A31SO 1999010100134 19990101 00134 SO 1999 1 1 COMA9810288 1 19981222 A 7997 WIRE EMB 120 EMB120RT SO RT ENGINE CHAFED A COMA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 SO 01 243CA 120212 RIGHT ENGINE OIL PRESSURE FLUCTUATING BETWEEN O AND 60 PSI. REPAIRED CHAFED WIRING AT ENGINE NACELLE. 2 L 7 2 4T RT A31SO 1999010100135 19990101 00135 SO 1999 1 1 COMA9810289 1 19981223 A 5712 12017068002 RIB EMB 120 EMB120RT SO RT WING TIP BENT A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 268CA 16856 120262 DURING THE E5 PART A INSPECTION OF ZONE 600, FOUND RIB NR 27 OF THE RIGHT WING TO BE BENT AT THE TRAILING EDGE. RIB WAS STRAIGHTENED AND AREA WAS DYE PENETRANT INSPECTED AND FOUND TO HAVE NO CRACKS. A DOUBLER WAS MADE AND INSTALLED AT THE TRAILING EDGE FOR SUPPORT. ALL WORK WAS DONE IAW AERODESIGN REPORT NR 3045-1 DATED 12-22-98. 2 L 7 2 4T RT A31SO 1999010100136 19990101 00136 1999 1 1 COMA9810290 4 19981226 A 3425 AHRS EMB 120 EMB120RT SO NR 1 OUT OF ADJUST A COMA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 01 164D 120164 AHRS INTERMITTENT DURING TAKEOFF. REORIENTED NR 1 AHRS. 2 L 7 2 4T RT A31SO 1999010100137 19990101 00137 EA 1999 1 1 COMA9860398 1 19981222 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 965CA 7928 5369 7131 FLAPS FAILED AT 24 DEGREES DURING APPROACH. REPLACED THE LEFT HAND BPSU. 2 L 7 2 4F RT A21EA 1999010100138 19990101 00138 EA 1999 1 1 COMA9860399 1 19981222 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 975CA 7150 CABIN DOOR WARNING. COULD NOT DUPLICATE, FOUND NO DEFECTS WITH DOOR WARNING SYSTEM. 2 L 7 2 4F RT A21EA 1999010100139 19990101 00139 EA 1999 1 1 COMA9860400 1 19981222 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 917CA 7017 CABIN DOOR WARNING. COULD NOT DUPLICATE, FOUND NO DEFECTS WITH CABIN DOOR. 2 L 7 2 4F RT A21EA 1999010100140 19990101 00140 EA 1999 1 1 COMA9860401 1 19981219 A 2750 601R93106503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA LT TE FLAP CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 LEFT WING NR 5 FLEXSHAFT IS HEAVILY CORRODED. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1999010100141 19990101 00141 EA 1999 1 1 COMA9860402 1 19981219 A 2750 601R93100503 FLEXSHAFT CNDAIR CL600 CL6002B19 EA RT TE FLAP CORRODED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 7171 RIGHT WING NR 5 FLEXSHAFT IS HEAVILY CORRODED. REPLACED FLEXSHAFT. 2 L 7 2 4F RT A21EA 1999010100142 19990101 00142 EA 1999 1 1 COMA9860403 1 19981220 A 2710 10231007 DAMPENER CNDAIR CL600 CL6002B19 EA RT AILERON LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 3798 7171 RIGHT AILERON FLUTTER DAMPENER LEAKING OUT OF LIMITS. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999010100143 19990101 00143 EA 1999 1 1 COMA9860404 1 19981219 A 2710 10231007 DAMPENER CNDAIR CL600 CL6002B19 EA LT AILERON LEAKING A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 984CA 3798 7171 LEFT AILERON FLUTTER DAMPENER LEAKING OUT OF LIMITS. REPLACED FLUTTER DAMPENER. 2 L 7 2 4F RT A21EA 1999010100144 19990101 00144 EA 1999 1 1 COMA9860405 1 19981225 A 7931 601509197 TRANSDUCER CNDAIR CL600 CL6002B19 EA LT ENGINE FAILED A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 940CA 7048 LEFT ENGINE OIL PRESSURE ABNORMAL. REPLACED THE OIL PRESSURE TRANSDUCER. 2 L 7 2 4F RT A21EA 1999010100145 19990101 00145 EA 1999 1 1 COMA9860406 1 19981227 A 3234 7179015 CONTROL CNDAIR CL600 CL6002B19 EA LANDING GEAR FAILED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 759CA 32 7279 GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE ASSY. RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999010100146 19990101 00146 EA 1999 1 1 COMA9860407 1 19981223 A 3030 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA RT STATIC PORT TRIPPED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 976CA 7151 RIGHT HAND STATIC HEAT CAUTION MESSAGE. RESET CIRCUIT BREAKER, SYSTEM FUNCTION NORMAL. 2 L 7 2 4F RT A21EA 1999010100147 19990101 00147 EA 1999 1 1 COMA9860408 1 19981223 A 2750 RETRACT SYST CNDAIR CL600 CL6002B19 EA TE FLAPS MALFUNCTIONED A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 945CA 7069 FLAPS FAILED AT 8 DEGREES. RESET FLAPS PER AD 98-20-01. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999010100148 19990101 00148 EA 1999 1 1 COMA9860409 1 19981223 A 2611 473052 DETECTOR CNDAIR CL600 CL6002B19 EA CARGO MALFUNCTIONED A COMA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 SO 01 988CA 2573 7204 CARGO SMOKE WARNING. FALSE WARNING, REPLACED SMOKE DETECTORS. 2 L 7 2 4F RT A21EA 1999010100149 19990101 00149 EU 1999 1 1 QXEA9802108 1 19981225 A 3350 BATTERIES FOKKER F28 F28MK4000 4990810 EU COCKPIT DISCHARGED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 476US 11224 SEA- DEAD FLASHLIGHT IN COCKPIT, REPLACED BATTERIES FOR EMERGENCY FLASHLIGHT. OPERATIONAL CHECKED GOOD. AIRCRAFT RETUR NED TO SERVICE. 2 L 7 2 4F RT A20EU 1999010100150 19990101 00150 EU 1999 1 1 QXEA9802109 1 19981225 A 3350 CIRCUIT BOARD FOKKER F28 F28MK4000 4990810 EU COCKPIT FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 482US 11231 PDX- EXIT SIGN AT ENTRANCE TO COCKPIT WILL NOT LIGHT. REPLACED COCKPIT ENTRANCE EMERGENCY EXIT LIGHT CIRCUIT BOARD. OP ERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999010100151 19990101 00151 EU 1999 1 1 QXEA9802110 1 19981225 A 3350 CONNECTOR FOKKER F28 F28MK4000 4990810 EU CABIN LOOSE A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 483US 11233 GEG- EVACUATION LIGHTS ON SEATS 5 THROUGH 11 INOP. FOUND LOOSE CONNECTION AT BATTERY PACK ROW NINE, SECURED. NO PARTS REPLACED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A20EU 1999010100152 19990101 00152 EU 1999 1 1 98FDEA00761 1 19981223 A 7830 32052213 SWITCH AIRBUS 300 A300F4605R 3930327 EU NR 1 TR UNIT FAILED A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 663FE 766 98-308 - ECAM WARNING FOR NR 1 T/R PRESSURIZED ANNUNCIATED, NO REV OR REV UNLOCK LIGHTS ILLUM. ABORT TAKEOFF. REMOVED AND REPLACED DIRECTIONAL PILOT VALVE/PRESS SWITCH PER MM 78-31-06-2. RAN ENG NO FAULTS FND. 2 L 7 2 4F RT A35EU 1999010100153 19990101 00153 EU 1999 1 1 98FDEA00763 1 19981224 A 3230 224TS05Y SWITCH AIRBUS 310 A310203 EU LANDING GEAR INOP A FDEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 25 408FE 257 LANDING GEAR HANDLE WOULD NOT GO PAST THE MID POS. FOLLOW RED TAB AND USED OTHER SYS AS DIRECTED, PROBLEM REMAINED. JU ST AFT SYS 2 USED, YELLOW SYS HYD ECAM CAME ON AMBER WITH MANY LIGHTS ON HYD PANEL. *S/D* REMOVED AND REPLACED LANDING GEAR CONTROL LEVER SWITCH IAW MM 32-31-11. 2 L 7 2 4F RT A35EU 1999010100154 19990101 00154 EU 1999 1 1 98FDEA00764 1 19981224 A 7830 32052213 VALVE AIRBUS 300 A300F4605R 3930327 EU NR 2 ENGINE INOP A FDEA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 25 651FE 728 AT T/O ROLL JUST AFT TOGA ACTIVATED ECAM ALERT NR 2 ENGINE REVERSE PRESSURIZED APPEARED. MASTER CAUTION ILLUM. *S/D* R EMOVED AND REPLACED NR 2 ENG PILOT VALVE PER MM 78-10-01, OPS CK NORMAL. 2 L 7 2 4F RT A35EU 1999010100155 19990101 00155 1999 1 1 98FDEA00765 4 19981227 A 3425 INS DOUG DC10 DC1030F 3023504 WP E & E COMPT INOP A FDEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SO 25 321FE 47836 98-312 - COULD NOT GET INS UNIT TO R-NAV UPDATE. GOT R-NAV YELLOW LIGHTS BUT WOULD NEVER GO TO GRN. UPDATED ALL 3 INS WITH SOFTWARE FX9813 PER MM 34-43-00-3. CKD SYS PER MM 34-43-00-1 ON GRD ALL CKD OK. OK TO CONT. 2 L 7 3 4F RT A22WE 1999010100156 19990101 00156 NM 1999 1 1 98FDEA00766 1 19981223 A 3213 NYG6210543 STRUT DOUG MD11 MD11F 3023600 NM CTR MLG DEFORMED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 603FE 48459 CENTERLINE LAND GEAR CARRIER AYG 7216-503 CRACK AND RING AYG7217-1 DEFORMED. 1.5 INCH CRACK AT SHOCK STRUT PISTON TOP CH ROME AREA. REMOVED AND REPLACED CTR LAND GEAR RING IAW MM 32-15-01-8. REMOVED AND REPLACED LAND GEAR PISTON WITH CLG C ARRIER SERVICEABLE FROM AC N583FE. REFER SNRM 0589 AND 0590. 2 L 7 3 4F RT A22WE 1999010100157 19990101 00157 NM 1999 1 1 98FDEA00767 1 19981227 A 2170 COALESCER BAG DOUG MD11 MD11 3023602 NM CABIN CONTAMINATED A FDEA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 25 607FE 48547 AFT T/O AC FILLED WITH SMOKE. EMER DECLARED. REMOVED AND REPLACED COALESCER BAGS IN ALL THREE AIR COND PACK SYS PER MM 21-54-05 LEAK CKD GOOD. RAN PACKS USING APU AND ENG AIR PER MD11 JRD, NO SMOKE PRESENT. A/C OK FOR SERVICE. 2 L 7 3 4F RT A22WE 1999010100158 19990101 00158 WP 1999 1 1 ABXA9801189 1 19981222 A 3610 4587112 DUCT DOUG DC8 DC861 3021952 WP RT NOSE TUNNEL FAILED A ABXA B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 848AX 46032 EN ROUTE FROM ONT TO ILN, AIRCRAFT EXPERIENCED RAPID DECOMPRESSION AT 33.000 FT. CABIN CLIMED TO 20,000 FT IN APPROX 2 MIN. EXECUTED EMERGENCY DESCENT. PRESSURE WAS REGAINED AT APPROX 10,000 FT. FOUND DUCT CLAMP LOOSE AND DUCT SEPARATED . RECONNECTED DUCT AND RE-CONNECTED CLAMP. OPS CHECKED GOOD IAW DC8 MM. 2 L 7 4 4F 4A25 1999010100159 19990101 00159 WP 1999 1 1 ABXA9801190 1 19981224 A 2510 INSULATION DOUG DC8 DC863 302198A WP LANDING GEAR OUT OF POSITION A ABXA K NONE O OTHER TO TAKEOFF 1 GL 23 823AX 46122 UNABLE TO RAISE LANDING GEAR HANDLE AFTER TAKEOFF. NOSE GEAR HAD MOVED PAST CENTER, RESET GROUND CONTROL RELAY CIRCUIT BREAKER. MAIN GEAR SPOILER INOP LIGHT ILLUMINATED. RESET LOCKOUT CIRCUIT BREAKER AND LIGHT WENT OUT. GEAR THEN RETRACT ED NORMALLY. INSPECTED GEAR AND GEAR LINKAGE, NO DEFECTS NOTED. FOUND INSULATION INTERFERING WITH LANDING GEAR CONTRO L LINKAGE. REMOVED INSULATION. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999010100160 19990101 00160 WP 1999 1 1 ABXA9801191 1 19981224 A 3350 60030451 POWER PACK DOUG DC9 DC931 3022065 WP CABIN INOP A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 952AX 47165 DURING MAINTENANCE, FOUND EMERGENCY LIGHTS TEST FUNCTION INOPERATIVE. REPLACED EMERGENCY LIGHTS POWER SUPPLY. OPS CHEC KED GOOD. 2 L 7 2 4F A6WE 1999010100161 19990101 00161 WP 1999 1 1 MWEA981169 1 19981221 A 5320 5644324 RETAINER DOUG DC9 DC932 3022066 WP COCKPIT WINDOW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 LEFT COCKPIT WINDOW RETAINER CRACKED IN LOWER FORWARD CORNER. MAINTENANCE INSTALLED DOUBLER REPAIR IAW MWEA EO 1-56-003 R1 AND DRAWING SRO5952985. 2 L 7 2 4F A6WE 1999010100162 19990101 00162 WP 1999 1 1 MWEA981170 1 19981221 A 5320 575468828 DOUBLER DOUG DC9 DC932 3022066 WP COCKPIT WINDOW CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 602ME 48133 RIGHT COCKPIT WINDOW RETAINER DOUBLER IAW SRM 51-30. 2 L 7 2 4F A6WE 1999010100163 19990101 00163 NM 1999 1 1 DLM88982590 1 19981219 A 5330 59203233 SKIN DOUG MD88 MD88 3023688 NM BS 370 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 945DL 49818 FUSELAGE/SKIN ASSY, FS 370 STRINGER 20R, REPAIR FOR GOUGE. THE FUSELAGE SKIN WAS BADLY GOUGED AT THE UPPER FWD CORNER O F THE C1 DOOR. THE DAMAGED AREA OF SKIN WAS ROUTED OUT OVER A 3 BY 1 AT THE DOOR CORNER AND OVER A 2 BY 36 AREA OVER S TRINGER 20R. THE SKIN CUTOUTS WERE REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 366297-14, REV B. 2 L 7 2 4F RT A6WE 1999010100164 19990101 00164 NM 1999 1 1 DL757982591 1 19981216 A 5315 146N51114 FLOORBEAM BOEING 757 757232 1384965 NM BS 1681.8 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 608DA 22815 FUSELAGE/FLOORBEAM, FS 1681.8 UPPER CAP, REPAIR FOR CORROSION. THE UPPER CAP OF THE FS 1681.8 FLOORBEAM WAS FOUND WITH EXTENSIVE AREAS OF CORROSION. THE UPPER CAP WAS TRIMMED OFF ALONG THE ENTIRE LENGTH OF THE BEAM. A NEW CAP WAS FABRICA TED FROM THE SAME TYPE EXTRUSION AS THE ORIGINAL AND INSTALLED ON THE FLOORBEAM PER ER/A 366220-14, REV A. 2 L 7 2 4F RT A2NM 1999010100165 19990101 00165 NM 1999 1 1 DL73S982592 1 19981216 A 5315 6545410223 FLOORBEAM BOEING 737 737232 1384475 NM BS 660 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 323DL 23095 FUSELAGE/OVERWING FLOORBEAM,BL 0 FS 660-664, REPAIR FOR CRACKS. THE OVERWING LONGITUDINAL FLOORBEAM UPPER CAP AT BL 0 W AS SEVERED AT FS 660 AND HAD AN ADDITIONAL CRACK FS 664. THE BEAM WEB WAS NOT DAMAGED. THE FLOORBEAM CAP WAS REPAIRED PER THE PROCEDURES OUTLINED IN BAC S/B 737-57-1210 AND DOCUMENTED PER ER/A 366299-14. 2 L 7 2 4F RT A16WE 1999010100166 19990101 00166 NM 1999 1 1 DL73K982593 1 19981216 A 5315 6545410223 FLOORBEAM BOEING 737 737232 1384475 NM BS 660 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 316DL 23088 FUSELAGE OVERWING FLOORBEAM, UPPER CAP BL 0 FS 66, REPAIR FOR CRACKED CAP. THE OVERWING FLOORBEAM AT BL 0 WAS FOUND WIT H A SEVERED UPPER CAP AT FS 662 WITH AN ADDITIONAL CRACK IN THE CAP AT FS 666. THE UPPER CAP WAS REPAIRED PER THE GU IDELINES OF BAC S/B 737-57-1210 AND DOCUMENTED PER ER/A 366316-14. 2 L 7 2 4F RT A16WE 1999010100167 19990101 00167 NM 1999 1 1 DL72S982595 1 19981221 A 3350 BATTERY 90052 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 21020 BOTH FWD EXIT SLIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY ON RACK M982, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999010100168 19990101 00168 NM 1999 1 1 DL72S982596 1 19981221 A 3350 BATTERY PACK 90052 BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 490DA 21020 LT MID WING SLIDE EMERGENCY LIGHT INOP. REPLACED BATTERY RACK M954, OPS CHKS GOOD. 2 L 7 3 4F A3WE 1999010100169 19990101 00169 NM 1999 1 1 DLM88982597 1 19981222 A 3260 833703 SWITCH DOUG MD88 MD88 3023688 NM RT MLG INOP A DALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 27 991DL 53343 CVG AIRBORN RETURN, RED LIGHT ON RT MAIN GEAR DOWN LOCK INDICATOR STAYED ON AFTER GEAR RETRACTION. GEAR EXTENDED NORMAL LY. REPEAT WRITE-UP. REPLACED PROX SW ELECTRONICS UNIT AND RT MLG UP PROXIMITY SW PER M/M. OPN CKS NML GEAR CYCLED SE VERAL TIMES ALL INDICATION GOOD. 2 L 7 2 4F RT A6WE 1999010100170 19990101 00170 NM 1999 1 1 DL72S982598 1 19981222 A 2720 69253641 SPRING BOEING 727 727232 1384082 NM RUDDER BROKEN A DALA O OTHER F FLT CONT AFFECTED CR CRUISE 1 SO 27 496DA 21076 IN-FLT RUDDERS BECAME SUPER SENSITIVE, LITTLE OR NO PRESSURE ON RUDDER PEDALS. A/C WANTED TO ROLL LT WITH UPPER 'B' OFF . A/C RESPONSE WAS CLOSE TO NORMAL. FOUND LT SPRING ON RUDDER FEEL/CENTERING UNIT BROKEN. 2 L 7 3 4F A3WE 1999010100171 19990101 00171 WP 1999 1 1 DLL19982601 1 19981222 A 2497 WIRE LKHEED 1011 10113853 5265020 WP LAVATORY FAILED A DALA H F DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 766DA 42820 193H1207 0 AT PUSHBACK, THE BATTERY CONDITION LIGHT CAME ON AND THE FLIGHT ATTENDANTS REPORTED FLAMES AT THE BASE BOARD BEHIND 2L L AV. PAX, F/A, AND SECOND OFFICER CONFIRMED FLAMES AND AN EXTINGUISHER WAS DISCHARGED. AIRCRAFT WAS EVACUATED PER THE C HECK LIST. FOUND WIRE BUNDLE BELOW LAV BURNT. SIGNS OF BLUE WATER STATION BU NDLE. SUSPECT INSULATION BREAK DOWN DUE TO BLUE WATER. NO CHAFING NOTED. 2 L 7 3 4F A23WE 1999010100172 19990101 00172 NM 1999 1 1 DL767982603 1 19981222 A 3260 SWITCH 257T110315 BOEING 767 767232 1385132 NM LT MLG FAILED A DALA O OTHER N FALSE WARNING LD LANDING 1 SO 27 111DN D00104 22223 LEFT MAIN GEAR INDICATED UNSAFE WHEN LOWERED. POM WAS FOLLOWED, HOWEVER GEAR STILL INDICATED UNSAFE HYD. QUANTITY AND PRESSURES WERE NORMAL. REPLACED LANDING GEAR LEVER AND SWICTHES AS PROXIMITY BOX. FAULTED SWITCH 421 AND 422. ALSO, R EPLACED LEFT GEAR. INDICATOR LAMPS. 2 L 7 2 4F RT A1NM 1999010100173 19990101 00173 NM 1999 1 1 DLM88982604 1 19981222 A 3222 STRUT DOUG MD88 MD88 3023688 NM NLG REQUIRED SERVICE A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 969DL 53172 RED NOSE GEAR LIGHT STAYED ON WITH HANDLE IN UP POSITION. RECYCLED GEAR PER POM. SAME RESULT. ALL GEAR INDICATED NORM AL WITH GEAR HANDLE DOWN. FOUND NOSE STRUT UNDERSERVICED. SERVICED STRUT PER M/M. CHECK FOR LEAKS. NO LEAKS. JACKED AIRCRAFT SWUNG NOSE LANDING GEAR. ALL INDICATION NORMAL. 2 L 7 2 4F RT A6WE 1999010100174 19990101 00174 NM 1999 1 1 DL72K982607 1 19981222 A 3350 LIGHT 1000677 BOEING 727 727232 1384082 NM COCKPIT INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 491DA 21060 COCKPIT EMERGENCY LT WOULD NOT TEST. REPLACED ASSY, OPS CK NML. 2 L 7 3 4F A3WE 1999010100175 19990101 00175 NM 1999 1 1 DL73K982610 1 19981222 A 5320 65469226 FITTING BOEING 737 737232 1384475 NM BS 685 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 329DL 23101 FUSELAGE LT AND RT MLG SIDE STRUT SUPPORT FITTING, BS 685. REPAIR FOR OVERSIZE LUG BORES. THE LUG BORES OF THE LT AND RT MLG SIDE STRUT SUPPORT FITTINGS AT BS 685 WERE FOUND CORRODED. THE LUG BORES WERE OPENED A MAX OF .11 IN DIAMETER. S TEEL REPAIR SLEEVES WERE INSTALLED TO RESIZE THE HOLE BORES TO NOMINAL DIAMETER. THE REPAIR WAS ACCOMPLISHED PER ER/A 3 66342-14, REV A. 2 L 7 2 4F RT A16WE 1999010100176 19990101 00176 NM 1999 1 1 DL72W982611 1 19981221 A 5330 65545738 SKIN BOEING 727 727247 138408F NM BS 660-681 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2812W 20868 FUSELAGE SKIN, FS 660-681 STRINGER 26R, REPAIR FOR CORROSION AT SKIN LAP. THE UPPER SKIN AT THE STRINGER 26R SKIN LAP S PLICE WAS FOUND WITH CORROSION BETWEEN FS 660-665. THE SKIN WAS CUTOUT OVER A 4 BY 4 AREA TO REMOVE THE CORROSION. THE CUTOUT WAS ADJACENT TO AN EXISTING REPAIR FOR A HOLE IN THE LOWER SKIN AT FS 675. THE EXISTING REPAIR WAS REMOVED AND BOTH SKIN CUTOUTS WERE REPAIRED WITH A STRUCTURAL FILLER AND DOUBLER PER THE GUIDELINES OF B727 SRM 53-30-3 AND ERA 3663 45. 2 L 7 3 4F A3WE 1999010100177 19990101 00177 NM 1999 1 1 DLM88982613 1 19981221 A 5330 59366673 SKIN DOUG MD88 MD88 3023688 NM BS 1305 DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 944DL 49817 FUSELAGE SKIN FS 1305, L-26L, REPAIR FOR GROUND DAMAGE. THE FUSELAGE SKIN WAS DENTED AND TORN AT THE LONGERON 26L LAP S PLICE AT FS 1305. THE DAMAGE WAS REMOVED WITH A 10.5 BY 9.5 CUTOUT. THE DAMAGE WAS REPAIRED WITH AN STRUCTURAL FILLER AND AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366336-14, REV B. 2 L 7 2 4F RT A6WE 1999010100178 19990101 00178 NM 1999 1 1 DL72S982614 1 19981221 A 2782 DOUBLER BOEING 727 727232 1384082 NM NR 8 LE SLAT ACT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 532DA 22045 WING FIXED LEADING EDGE, NR 8 SLAT ACTUTOR SUPPORT BRACKET REPAIR FOR CRACKED DOUBLER. THE OUTBD SUPPORT BRACKET DOUBLE R FOR THE NR 8 SLAT WAS FOUND CRACKED. THE INBD AND OUTBD ACTUATOR BRACKETS FOR THE NR 8 SLAT WERE REPAIRED/MODIFIED PE R THE REQUIREMENTS OF B727 S/B727-57-0130. THE REPAIR/MODIFICATION WAS DOCUMENTED PER ER/A 366349-14AD. 2 L 7 3 4F A3WE 1999010100180 19990101 00180 NM 1999 1 1 DL72L982618 1 19981224 A 5713 6483385 STRINGER BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 THE UPPER CHORD ANGLE OF THE LT WING RIB AT WS 171.5 WAS FOUND CRACKED. THE CRACK WAS LOCATED PROPAGATING FROM A FAST. HOLE ON THE HORIZ FLANGE OF THE CHORD ANGLE UNDER STR 16. REPAIRED PER ERA 332570-14. 2 L 7 3 4F A3WE 1999010100181 19990101 00181 NM 1999 1 1 DL72L982619 1 19981224 A 5713 6483385 STRINGER BOEING 727 727232 1384082 NM WS 171.5 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 UPPER CHORD ON THE RT WING RIB AT WS 171.5 WAS FOUND CRACKED. THE CRACK WAS LOCATED FROM A FAST HOLE ON THE HORIZ FLANG E OF THE CHORD ANGLE UNDER STR 17. REPAIRED PER ERA 332571-14. 2 L 7 3 4F A3WE 1999010100182 19990101 00182 NM 1999 1 1 DL76S982620 1 19981224 A 3260 SWITCH 851801 BOEING 767 767332 1382001 NM LT MLG DOOR DIRTY A DALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SO 27 135DL 25145 ON T/O, THE AMBER GEAR DOOR LIGHT REMAINED ILLUM FOR A UNUSUALLY LONG TIME AFTER GEAR RETRACT. ON APPROACH WITH GEAR EX TENDED AND THREE GREEN THE AMBER GEAR DOOR LIGHT REMAINED ILLUM THROUGH TOUCHDOWN. LIGHT EXTINGUISHED AFTER TOUCHDO WN. PERFORMED BITE OF PSEU LAST FLT FAULTED SW S260 AND S238 LT LOCK LATCH SYS. CHECKED SWITCHES, TARGETS AND WIRING A LL OK CYCLED GEAR DOORS SEVERAL TIMES, SYS OP AND INDICATION NML. 2 L 7 2 4F RT A1NM 1999010100183 19990101 00183 NM 1999 1 1 DL757982621 1 19981224 A 2560 MV10 MEGAPHONE BOEING 757 757232 1384965 NM CABIN INOPERATIVE A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 624DL 22914 BOTH CABIN MEGAPHONES INOP. FOUND BY CABIN CREW ON PREDEPARTURE CHECK, P/N 237702242 (2) EACH. 2 L 7 2 4F RT A2NM 1999010100184 19990101 00184 1999 1 1 DL733982622 2 19981224 A 7510 ANTI ICE VALVE 32906621 BOEING 737 7373B7 1384580 NM NR 2 ENGINE FAILED A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 951WP 1885 22951 000000 RIGHT ENGINE ANTI-ICE FAILED CLOSED POSITION. AIR TURN BACK. REPLACED ANTI-ICE VALVE. 2 L 7 2 4F RT A16WE 1999010100185 19990101 00185 WP 1999 1 1 DLL10982623 1 19981225 A 3230 HYD LINE LS27E0560TYA LKHEED 1011 10113851 5265010 WP RT MLG BROKEN A DALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 27 720DA 193C1136 AFTER TAKEOFF, COULD NOT RETRACT LANDING GEAR ALSO GOT TRUCK LIGHT ON, PERFORMED POM PROCEDURES AND RETUNED TO AIRPORT. MTC FOUND HYD FUSE SET AND FLEX LINE ON RIGHT GEAR TO RIGID LINE ON BOGGIE BEAM BROKEN. REPLACED LINE AND RESET FUSE, LEAK CHECKS OK. A/C DEPARTED WITHOUT FURTHER INCIDENT. 2 L 7 3 4F A23WE 1999010100186 19990101 00186 NM 1999 1 1 DLM11982624 1 19981225 A 2120 AIR DIST DOUG MD11 MD11 3023602 NM COCKPIT ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 803DE 48474 ELEC SMOKE SMELL IN COCKPIT. VERIFIED BY FLIGHT ATTENDANTS AS THEY WALKED UP TO COCKPIT. RAN ENGINES AT POWER FOR 30 M IN. PRESSURIZED AIRCRAFT OPERATED ALL GALLEY EQUIPMENT, CKD AFT GALLEY FEEDER CABLES AND GALLEY GCU'S FOR SECURITY. RE PLACED OVEN 108 AND COALESCER BAGS PRECAUTIONARY. PERFORMED SMOKE AND ODOR CHECK PER MM 21-53-00-7. INSPECTED OVERHEAD CIRCUIT BREAKER PANELS AND ABOVE FWD PASSENGER DOORS AND FWD AVIONICS EQUIPMENT RACKS. ALL CHECKS NORMAL. NO DISCREPA NCIES NOTED. 2 L 7 3 4F RT A22WE 1999010100187 19990101 00187 NM 1999 1 1 DL72S982625 1 19981225 A 3610 65594264 DUCT BOEING 727 727232 1384082 NM LOWER BODY BROKEN A DALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 27 516DA 21432 LOWER AFT BODY OVERHEAT LIGHT ON. REPLACED BLOWN DUCT UNDER APU IN KEEL BEAM. 2 L 7 3 4F A3WE 1999010100188 19990101 00188 NM 1999 1 1 DL72S982627 1 19981225 A 3350 BULB BOEING 727 727232 1384082 NM AFT STAIRS FAILED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 531DA 21814 5 LIGHTS BAD AT AFT STAIR CASE, RELAMPED. 2 L 7 3 4F A3WE 1999010100189 19990101 00189 NM 1999 1 1 DL73K982628 1 19981225 A 3350 SIGN 21131A BOEING 737 737247 138448D NM DOOR 2L INOP A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 239WA NY091 23187 EXIT SIGN AT DOOR 2L WILL NOT TEST. 2 L 7 2 4F A16WE 1999010100190 19990101 00190 NM 1999 1 1 DL72S982629 1 19981226 A 2150 VALVE 39854021 BOEING 727 727225 1384077 NM LT PACK FAILED A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 27 8882Z P727 21579 LEFT PACK ON, CAUSED SMOKE IN CABIN. REPLACED FWD PACK VALVE AND MIX VALVE. CK OK. 2 L 7 3 4F A3WE 1999010100191 19990101 00191 NM 1999 1 1 DLM88982630 1 19981226 A 2421 GENERATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE FAILED A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 SO 27 976DL 27837 53257 718120 LT CSD OIL LOW PRESS LIGHT ILLUMINATED IN FLT. TEMP RAPIDLY RISING, GEN CYCLING ON AND OFF. CSD DISCONNECTED. APU ON MCO AND PLAC FOR NOT STARTING. REPAIRED APU AND REMOVED MCO AND PLAC PLACED LT GEN ON MCO AND PLAC PER MEL 24-00-01A. 2 L 7 2 4F 4 F RT A6WE E9NE 1999010100192 19990101 00192 NM 1999 1 1 DLM11982631 1 19981226 A 3350 330101653 BATTERY DOUG MD11 MD11 3023602 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 806DE 48477 FWD CABIN EMERGENCY LIGHT INOP. REMOVED AND REPLACED N01 BATTERY PACK IN THE NR 1 BATTERY POWER SUPPLY, GRD OPS CK OK. 2 L 7 3 4F RT A22WE 1999010100193 19990101 00193 WP 1999 1 1 TC8A98087 1 19981223 A 3260 CONNECTOR DOUG DC8 DC862F 3021972 WP RT MLG LOOSE A TC8A O OTHER N FALSE WARNING DE DESCENT 1 GL 23 183SK 45904 NO MAIN RIGHT GEAR DOWN INDICATION UNTIL CYCLING GEAR TWICE. FOUND RIGHT GEAR DOWN SWITCH CANNON PLUG LOOSE. SECURED, OPS CHECKS GOOD IAW 32-60-0. 2 L 7 4 4F 4A25 1999010100194 19990101 00194 NE 1999 1 1 MALA976270 2 19981224 A 7230 COMPRESSOR BAC 146 AVRO146RJ85A 1500097 EU LYC LF507 LF5071F NE ENGINE BIRD STRIKE A MALA A UNSCHED LANDING C F.O.D. CL CLIMB 1 GL 15 509XJ E2321 BIRD STRIKE ON ROTATION. AIRCRAFT RETURNED TO HPN. MAINTENANCE PERFORMED BOROSCOPE INSPECTION. ALL CHECKS GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 1999010100195 19990101 00195 EU 1999 1 1 MALA976271 1 19981225 A 6120 PROP CONTL UNIT SAAB SF340 340B 7860101 EU RT ENGINE MALFUNCTIONED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 428XJ 428 RT PROP UNDERSPEED ON TAKEOFF. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED PROP DOME SEALS, PITCH CONTROL UNIT AND PROP OVERSPEED CONTROL UNIT. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999010100196 19990101 00196 EU 1999 1 1 MALA976272 1 19981222 A 3230 RETRACT MECH SAAB SF340 340B 7860101 EU LANDING GEAR LACK OF LUBE A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 403XJ 340B403 UPON GEAR RETRACTION AFTER TAKEOFF, GEAR WOULD NOT RETRACT. MAINTENANCE COMPLETED SEVERAL GEAR SWINGS. CLEANED AND LUB ED GEAR SWITCHES. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999010100197 19990101 00197 EU 1999 1 1 MALA976273 1 19981223 A 3530 4566M37B042NM PBE BAC 146 AVRO146RJ85A 1500097 EU COCKPIT SOFT A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 518XJ E2337 CREW REFUSED AIRCRAFT, INSISTED COCKPIT AND AFT BULKHEAD PBE ARE SOFT. MAINTENANCE INSTALLED NEW PBE IN COCKPIT AND BUL KHEAD. OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999010100198 19990101 00198 WP 1999 1 1 9810979937 1 19981222 A 3231 RETRACT MECH DOUG DC9 DC931 3022065 WP LT & RT MLG DOOR MALFUNCTIONED A NWAA O OTHER J WARNING INDICATION CL CLIMB 1 GL 01 908H 47517 RIGHT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION. CREW RECYLED GEAR AND BOTH LEFT AND RIGHT MAIN GEAR UNSAFE LIGHTS ILLUMINATED. AIRCRAFT CONTINUED TO DESTINATION AND EMERGENCY GEAR EXTENSION PROCEDURES WERE UTILIZED FOR LANDING. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED BOLTS TO UPLATCH ROLLER ON RIGHT MAIN GEAR DOOR AN D REPLACED PSEU PROCESSOR AS A PRECAUTION. ALSO, REPLACED BOTH MAIN LEFT AND RIGHT GEAR DOORS DUE TO DAMAGE INCURRED ON LANDING. OPERATIONAL CHECK NORMAL. AIRCRAFT RETUREND TO SERVICE. 2 L 7 2 4F A6WE 1999010100200 19990101 00200 WP 1999 1 1 9810999993 1 19981221 A 3397 WIRE DOUG DC9 DC931 3022065 WP ROW 2 CD BROKEN A NWAA O OTHER L NO TEST CL CLIMB 1 GL 01 8986E 47402 AFTER TAKEOFF, THE EMERGENCY PATHWAY LIGHTING IN THE FIRST CLASS CABIN AND THE EMERGENCY LIGHTING OVER GALLEY DOOR ILLUM INATED AND REMAINED ILLUMINATED UNTIL BATTERY DEPLETION. ALL REMAINING EMERGENCY LIGHTING THROUGHOUT CABIN REMAINED IN THE OFF POSITION. MAINTENANCE REPAIRED EMERGENCY EXIT LIGHT WIRING AT SEAT ROW 2C/D AND REPLACED THE EMERGENCY LIGHT BA TTERY PACK AT DOOR 1 RIGHT. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999010100201 19990101 00201 WP 1999 1 1 9811009750 1 19981222 A 2710 CONTROL CABLE DOUG DC9 DC941 302207N WP AILERON CONTROL FROZEN A NWAA O OTHER F FLT CONT AFFECTED CR CRUISE 1 GL 01 750W 47114 AT ALTITUDE, AILERONS FROZE IN POSITION WITH A MAXIMUM OF 10 DEGREES BANK WITH FULL YOKE FORCE APPLIED. AT 250 FT ABOVE GROUND LEVEL FULL AILERON CONTROL BECAME AVAILABLE AND AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. SUSPECT ICE AC CUMULATION ON AILERON CONTROL CABLES. MAINTENANCE REPLACED SEALS IN ALL FOUR OVERWING EXIT DOORS, RESEALED SLANT PANEL. REPLACED SLANT PANEL DRAIN LINES, AND VERIFIED CHECK VALVE COMPLIANCE PER EM 5330-01125. 2 L 7 2 4F A6WE 1999010100202 19990101 00202 NM 1999 1 1 QXEA9802111 1 19981225 A 3350 6104789 BATTERY DHAV DHC8 DHC8202 2809007 NM ROW 1-4 DISCHARGED A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 350PH 2932 187 488 SEA - FLOOR EMERGENCY LIGHT AT ROW 1-4 CDE INOP. MAINTENANCE REPLACED 3352 PS2 BATTERY. OPERATIONAL CHECKS GOOD. AIRC RAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999010100203 19990101 00203 NM 1999 1 1 QXEA9802112 1 19981223 A 3350 LIGHT DHAV DHC8 DHC8102 2809003 NM ROW 3E INOP A QXEA K NONE L NO TEST UK UNKNOWN 1 NM 09 825PH 213 SEA - ESCAPE PATH LIGHTING AT ROW 3E INOP. MAINTENANCE PLACED ON MEL 33-13. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A13NM 1999010100204 19990101 00204 NM 1999 1 1 QXEA9802113 1 19981226 A 5210 MECHANISM DHAV DHC8 DHC8102 2809003 NM PAX DOOR LACK OF LUBE A QXEA K NONE O OTHER UK UNKNOWN 1 NM 09 816PH 54 SEA - PASSENGER DOOR DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE ADJUSTED THE THRESHOLD STRIP ON THE BOTTOM OF THE D OOR AND LUBRICATED THE DOOR PINS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. NO PARTS REPLACED. 2 H 7 2 4T RT A13NM 1999010100205 19990101 00205 EU 1999 1 1 QXEA9802114 1 19981227 A 3350 5515800106 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST NR NOT REPORTED 1 NM 09 493US 11161 PDX - PILOT REPORTS LIGHT BULBS IN THE EMERGENCY EXIT SIGN OVER THE COCKPIT DOOR ARE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED THE EXIT SIGN. AN OPERATIONAL TEST WAS PERFORMED, RESULTS WERE NORMAL. 2 L 7 2 4F RT A20EU 1999010100206 19990101 00206 NM 1999 1 1 98UAL900537 1 19981119 A 5610 141W74002 WINDSHIELD PPG 141W74002 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE LT COCKPIT FAILED A UALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 29 777UA 94144H6975 26916 EN ROUTE FRA TO ORD, OBSERVED LARGE CRACK IN CAPTAIN'S WINDSHIELD INNER PANE. FLIGHT DIVERTED TO LHR. WINDSHIELD (P/N 141W7400-2) AND OTHERS HAVE BEEN REMOVED AND ANALYSED AT THE VENDOR (PPG) FOR DEFECTS. SO FAR, EARLY INDICATIONS SEEMS TO LEAD TO THE EPOXY USED TO ADHERE THE ANTI-FOG BUS BAR IN PLACE AS WELL AS THE MATERIAL OF THE BUS BAR SEEM TO BE THE LEADING CAUSE OF THE ARCING AND THUS SHATTERING OF THE WINDOW PANE. ALL HIGH TIME WINDOWS ARE BEING REMOVED FOR ADDITIO NAL ANALYSIS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999010100207 19990101 00207 1999 1 1 98UAL900542 4 19981113 A 2210 AUTOPILOT BOEING 777 777222 1385219 NM PWA 4090 PW4090 NE E & E COMPT MALFUNCTIONED A UALA H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED DE DESCENT 1 WP 29 790UA 26943 ON VNAV DESCENT (USED DES NOW PROMPT) DESCENT BEGAN AT 1200 FPM. UPON CATCHING VNAV PATH, AIRCRAFT PITCHED UP IN EXCESS OF 1000FPM. CREW DISCONNECTED AUTOPILOT AND CONTINUED DESCENT IN FLCH. THIS IS A KNOWN ANOMALY THAT IS COVERED IN THE FLIGHT MANUAL, IN BULLETIN 98-08. THE PROBLEM WILL BE FIXED BY A NEW AIMS LOAD PER CHANGE ORDER PROJECT CURRENTLY IN PROCESS. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999010100208 19990101 00208 NM 1999 1 1 98UAL900543 1 19981114 A 4940 27044424 STARTER ALLIEDSIGNAL 27044424 BOEING 777 777222 1385219 NM PWA PW4077 PW4077 NE APU MALFUNCTIONED A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 772UA 26930 APU WILL NOT START IN EITHER ELECTRICAL OR PNEUMATIC START MODE. *S/D* REMOVED AND REPLACED APU BATTERY CHARGER. PROBLE M PERSISTED. FOUND APU STARTER DAMAGED. REPLACED ELECTRIC STARTER (P/N 2704442-4) AND CLUTCH ASSEMBLY. OPERATIONALLY CHECKED NORMAL. SUSPECT CAUSE RELATED TO BOEING SERVICE RELATED PROBLEM (SRP) 777-SRP-49-0028 AND SERVICE BULLETIN 777- 24-0024. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999010100209 19990101 00209 NM 1999 1 1 98UAL900545 1 19981115 A 3350 20131 BATTERY PACK BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 618UA 21878 LEFT EMERGENCY ESCAPE LIGHT DOES NOT COME ON WHEN TEST 1 BUTTON IS PUSHED. BATTERY PACK WAS REPLACED. PROBLEM WAS CORR ECTED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999010100210 19990101 00210 NM 1999 1 1 98UAL900554 1 19981120 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY FIRE A UALA H F DEACTIVATE SYST/CIRCUITS ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 663UA 27160 SMOKE REPORTED FROM OVEN NR 305, FLT ATTENDANT DISCHARGED HALON FIRE EXTINGUISHER INTO OVEN. CB PULLED. CAUSE DUE TO PLASTIC AND PAPER MELTING AND OVERHEATING IN THE FAN AREA ON THE BAFFLE. OVEN REPLACED. 2 L 7 2 4F 4 F RT A1NM E24NE 1999010100211 19990101 00211 NE 1999 1 1 98UAL900568 2 19981125 A 7230 3053556220 BEARING SNR BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 4 FAILED A UALA O OTHER B R SMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 315UA 4996 23947 726388 OIL FUMES IN CABIN. NR 4 MAIN BEARING FAILURE CAUSED ENGINE STALL DURING CLIMB AND RESULTING OIL SMELL IN THE CABIN. T HE BEARING FAILURE CAUSED A SLIGHT DROP OF THE N2 COMPRESSOR SHAFT ALLOWING AIR/OIL FUMES PAST THE NR 3 BRG SEAL LANDS. REPLACED THE NR 4 BEARING AND NR 3 BEARING AIR/OIL SEAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999010100212 19990101 00212 NM 1999 1 1 98UAL900606 1 19981219 A 2120 VALVE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE RAM AIR GATE FAILED A UALA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 WP 29 603UA 21864 CREW REPORTS VIBRATION AND NOISES FROM AIRFRAME. DIVERTED TO LAS. EMERGENCY DECLARED, OVERWEIGHT LANDING. *S/D* INSPE CTION CHECK FOUND FLAPPER BROKEN. REMOVED BROKEN FLAPPER FROM AIR DUCT AND INSTALLED NEW VALVES. 2 L 7 2 4F 4 F RT A1NM E3NE 1999010100213 19990101 00213 EU 1999 1 1 98UAL900607 1 19981218 A 3222 AN414A STRUT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NLG REQUIRED SERVICE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 416UA 479 LANDING GEAR WOULD NOT RETRACT ON DEPARTURE. RETURNED TO DEN. *S/D* ECAM L/G SHOCK ABSORBER FAULT. SECURED LOOSE SENSO R TARGET. PERFORMED NLG STRUT SVC. 2 L 7 2 4F 4 F RT A28NM E40NE 1999010100214 19990101 00214 NM 1999 1 1 98UAL900609 1 19981222 A 3350 STRIP BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE DOOR 2L DAMAGED A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 190UA 26879 EEL STRIP AT DOOR 2L DAMAGED. REPLACED ENCAPSULATED 72 INCH EEL STRIP AT DOOR 2L. OPS CHECKS OK. 2 L 7 4 4F 4 F RT A20WE E24NE 1999010100215 19990101 00215 NM 1999 1 1 98UAL900611 1 19981222 A 7603 THROTTLE BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE OUT OF ADJUST A UALA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 29 7270U 21417 ABORTED TAKEOFF AT 100 KNOTS DUE TO NR 3 ENGINE LOW EPR (1.8) WITH THROTTLE 2-3 INCHES BEYOND NR 1 AND 2 ENGINES. RPM WA S GOOD AT 99 PERCENT AND FUEL FLOW MATCHED NR 1 AND 2 ENGINES. *S/D* ADJUSTED RIG ON NR 3 THROTTLE. CHECKED INLET AND EXHAUST. CHECKED OPERATION OF THE INTERCOMPRESSOR BLEED VALVES AND REPLACED THE PRESSURE RATIO BLEED CONTROL ASSEMBLY. ACCOMPLISHED FULL RUNUP AND ALL INDICATIONS WERE NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999010100216 19990101 00216 NE 1999 1 1 98UAL900612 2 19981223 A 7530 2607MK1 ACTUATOR AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE FAILED A UALA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 WP 29 411UA 1531 1531 464 V10046 NR 1 COMPRESSOR STALL. ENGINE SHUT DOWN. *S/D* COMPRESSOR STALL WAS CAUSED BY A VSV ACTUATOR WITH A FAULTY POSITION FEE DBACK SIGNAL. COA R90290 HAS BEEN ACCOMPLISHED ON APPROXIMATELY 80 PERCENT OF THE V2500 ENGINE FLEET. ACCOMPLISHMENT H AS BEEN ACCELERATED TO COMPLETE THE REMAINING 20 PERCENT. THIS MODIFICATION WILL PREVENT THIS TYPE OF EVENT FROM HAPPEN ING IN THE FUTURE. 2 L 7 2 4F 4 F RT A28NM E40NE 1999010100217 19990101 00217 NM 1999 1 1 98UAL900613 1 19981222 A 2530 OVEN BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE GALLEY SMOKING A UALA F ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 658UA 27113 RIGHT HAND MID-GALLEY OVEN FIRE. EXTINGUISHED FIRE WITH HALON EXTINGUISHER. ISOLATED ELECTRICAL SUPPLY BY TURNING-OFF LE FT UTILITY BUS. *S/D* AIRCRAFT CONNECTORS AND WIRING WERE INSPECTED AND FOUND TO BE SERVICEABLE. A NEW OVEN WAS INSTA LLED AND OP CHECKED GOOD. THE REMOVED OVEN WAS INSPECTED BY THE HOME SHOP IN SFO AND FOUND TO HAVE PLASTIC DEBRIS MELTE D ON AND ABOVE THE BAFFLE AND ON THE HEATING ELEMENT IN THE UPPER AREA OF THE OVEN. IT IS SUSPECTED THAT A PLASTIC BAG LEFT ON THE OVEN INSERT WAS DRAWN INTO THE OVEN HEATING AREA. OVEN INSERT PACKAGING, TRANSPORT AND LOADING PROCEDURES H AVE BEEN REVIEWED WITH UA CATERERS PER A SAFETY ALERT METER DTD 12/28/98. 2 L 7 2 4F 4 F RT A1NM E24NE 1999010100218 19990101 00218 NM 1999 1 1 98UAL900614 1 19981224 A 2842 INDICATOR SIMMONDS 39308601236 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE FUEL QUANITY MALFUNCTIONED A UALA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 WP 29 7261U 21408 NR 1 AND 2 MAIN FUEL QUANTITY ERRATIC. CREW NOTED ABOUT 3 UNITS OF RUDDER TRIM APPLIED. FLIGHT DIVERTED TO RNO DUE TO PO SSIBLE FUEL IMBALANCE. *S/D* CHECKED THE SYSTEM AND FOUND NO PROBLEMS. REPLACED THE INDICATOR DUE TO READING UNSTABLE . 2 L 7 3 4F 4 F A3WE E2EA 1999010100219 19990101 00219 WP 1999 1 1 ABXA9801192 1 19981228 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 953AX 47608 DURING PREFLIGHT, EMERGENCY LIGHTS WOULD NOT TEST. REPLACED EMERGENCY LIGHT BATTERIES IAW DC9 MM 33-33-0. OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999010100220 19990101 00220 NM 1999 1 1 MWEA981182 1 19981228 A 5711 5935891 SPAR DOUG MD88 MD88 3023688 NM RT WING MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT WING AUXILLARY SPAR UPPER ATTACH HOLE IS MISDRILLED. CLEANED UP HOLE FABRICATED AND INSTALLED REPAIR BUSHINGS 2 L 7 2 4F RT A6WE 1999010100221 19990101 00221 NM 1999 1 1 MWEA981183 1 19981228 A 5320 5911408 INTERCOSTAL DOUG MD88 MD88 3023688 NM FUSELAGE MISINSTALLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 810ME 48072 DURING INITIAL INSPECTION, FOUND INCORRECT INTERCOSTAL INSTALLED. FABRICATED AND INSTALLED CORRECT INTERCOSTAL. 2 L 7 2 4F RT A6WE 1999010100222 19990101 00222 NM 1999 1 1 MWEA981184 1 19981228 A 5311 9912448 FRAME DOUG MD88 MD88 3023688 NM BS 636 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 MAIN FUSELAGE FRAME AT STATION 636 HAS A CRACK IN IT AT LONGERON 18 RIGHT. REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR PARTS. 2 L 7 2 4F RT A6WE 1999010100223 19990101 00223 NM 1999 1 1 MWEA981185 1 19981228 A 5730 5930502 SKIN DOUG MD88 MD88 3023688 NM LT WING MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 810ME 48072 2 HOLES WERE MISDRILLED ON LEFT WING SKIN. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR BUSHING INSTALLED NOMINAL FAS TENERS. 2 L 7 2 4F RT A6WE 1999010100224 19990101 00224 NM 1999 1 1 MWEA981186 1 19981228 A 5720 59373291 DOUBLER DOUG MD88 MD88 3023688 NM LT WING MISDRILLED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 810ME 48072 2 HOLES WERE MISDRILLED ON THE LEFT MAIN GEAR UPPER SUPPORT DOUBLER. FABRICATED AND INSTALLED REPAIR BUSINGS INSTALLED NOMINAL FASTENERS. 2 L 7 2 4F RT A6WE 1999010100225 19990101 00225 NM 1999 1 1 MWEA981187 1 19981228 A 5311 5911448 FRAME DOUG MD88 MD88 3023688 NM BS 1290 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 FRAME SECTION AT STATION 1290 FROM LONGERON 10 LEFT TO LONGERON 10 RIGHT WAS FOUND WITH DAMAGED HOLES. REMOVED DAMAGED SECTION FABRICATED AND INSTALLED REPAIR SECTIONS. 2 L 7 2 4F RT A6WE 1999010100226 19990101 00226 NM 1999 1 1 MWEA981188 1 19981228 A 5313 2777922 LONGERON DOUG MD88 MD88 3023688 NM BS 1287 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 LONGERON 9 LEFT AT STATION 1287 HAD A CRACKED OUT ATTACH HOLE. REMOVED DAMAGED AREA FABRICATED AND INSTALLED REPAIR SEC TIONS. 2 L 7 2 4F RT A6WE 1999010100227 19990101 00227 NM 1999 1 1 MWEA981189 1 19981228 A 5510 9911846 FITTING DOUG MD88 MD88 3023688 NM HORIZ STAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 UPON REMOVAL OF HORIZONTAL STAB CENTER THE BOLT HOLES HAD THREAD DAMAGE. REMOVED DAMAGE FROM HOLES AND FABRICATED AND I NSTALLED REPAIR BUSHINGS. 2 L 7 2 4F RT A6WE 1999010100228 19990101 00228 NM 1999 1 1 MWEA981190 1 19981228 A 5311 9911841 FRAME DOUG MD88 MD88 3023688 NM BS 1463 DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 A PREVIOUSLY REPAIRED AREA ON THE CANTED FRAME AT STATION 1463 WAS FOUND TO BE IMPROPER. REMOVED AND REPLACED CANTED FR AME WEB. 2 L 7 2 4F RT A6WE 1999010100229 19990101 00229 NM 1999 1 1 MWEA981191 1 19981228 A 5753 5912150 HINGE DOUG MD88 MD88 3023688 NM LT TE FLAP DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 LEFT FLAP OUTBOARD FLAP HINGE HAS AN OVERSIZED BORE. FABRICATED AND INSTALLED A REPAIR BUSHING. 2 L 7 2 4F RT A6WE 1999010100230 19990101 00230 NM 1999 1 1 SCNA98151 1 19981217 A 3350 6013211 BATTERY PACK BOEING 727 7272J4 1384006 NM L1 & R1 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 288SC 20765 DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS OUTSIDE OF THE L1 AND R1 DOORS ON THE SIDE OF THE AIRPLANE WERE FO UND TO BE INOPERATIVE. REMOVED AND REPLACED THE M982 EMERGENCY LIGHT BATTERY PACK. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F RT A3WE 1999010100231 19990101 00231 NM 1999 1 1 SCNA98152 1 19981227 A 3350 37067001 BATTERIES BOEING 727 727227 1384078 NM AFT AIRSTAIR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 275AF 22092 DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REP LACED THE BATTERIES. OPERATIONALLY CHECKS GOOD IAW MM 335061. 2 L 7 3 4F A3WE 1999010100232 19990101 00232 NM 1999 1 1 SCNA98153 1 19981223 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM RT OVERWING DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 283SC 22559 DURING A LINE MAINTENANCE CHECK, THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHT THAT IS LOCATED BETWEEN THE OVERWING EXIT D OORS WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERY M655. SYSTEM OPERATIONALLY CHECKS NORMAL. 2 L 7 3 4F A3WE 1999010100254 19990101 00254 CE 1999 1 1 98ZZZX4783 1 19981111 A 3230 S13771 SWITCH CESSNA 210 210L 2073448 CE RT MLG BROKEN A DFJA K NONE O OTHER IN INSP/MAINT 1 CE 03 50DB 21060107 PILOT REPORTED NO DOWNLOCK LIGHT INDICATION. INSPECTION FOUND WIRE BROKEN RIGHT AT SWITCH HOUSING. REPLACED SWITCH WIT H NEW PART. NO OTHER DEFECTS NOTED. 1 H 7 1 3O 3A21 1999010100255 19990101 00255 1999 1 1 98ZZZX4784 4 19981125 A 6122 F848LZ GOVERNOR PIPER PA31 PA31350 7103110 SO PROPELLER FAILED A BSYA O OTHER O OTHER NR NOT REPORTED 1 GL 07 106TG 9640 E98YT 318052002 RIGHT ENGINE OVERSPED COMING INTO (CMH). PILOT SHUT ENGINE DOWN AND FEATHERED PROPELLER. FOUND BROKEN FLYWEIGHT IN PRO PELLER GOVERNOR. REMOVED AND REPLACED RIGHT ENGINE FOR OVERSPEEDING CONDITION. REMOVED AND REPLACED PROPELLER GOVERNOR . 1 L 7 2 3O A20SO 1999010100274 19990101 00274 GL 1999 1 1 98ZZZX4803 2 19981207 A 7250 TURBINE ROTOR BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20 03013 GL NR 2 ENGINE FAILED A HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 91070 CAT30507F S145 CAE836513 NR 2 ENGINE OIL PRESSURE BEGAN TO FLUCTUATE IN CRUISE. LANDED WITHOUT INCIDENT. OIL LEVEL ONE AND ONE-HALF QUARTS LOW ON OIL. NO LEAKS NOTED. RE-SERVICED AND RETURNED TO SERVICE AFTER PENALTY RUN AND CHECK. FOLLOW-UP CHECK REVEALED ENG INE OIL CONSUMPTION. REPLACED TURBINE ROTOR ASSEMBLY. 1 G 7 2 3U 3 U H3EU E4CE 1999010100284 19990101 00284 SW 1999 1 1 98ZZZX4813 1 19981211 A 2400 M8171417031 MATRIX BLOCK BELL 214 214ST 1182106 SW E/E BAY FAILED A HEEA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 03 3897N 28106 CREW REPORTED CRACKLING SOUND IN HEADSETS FOLLOWED BY A TOXIC SMELLING SMOKE. CREW IMMEDIATELY DIVERTED TO NEAREST PLAT FORM. ALL ELECTRICAL SYSTEMS WERE SHUT DOWN AND AN UNEVENTFUL LANDING WAS MADE. 115 VOLT CIRCUIT BREAKER FOR COPILOT F LIGHT INSTRUMENTS HAD TRIPPED. MAINTENANCE FOUND MATRIX BLOCK IN NOSE 'BURNT'. REF: 214ST IPC, CHAPTER 96-99-00, PAGE 1B, FIGURE 96-2, ITEM 69. 2 G 7 2 4U H10SW 1999010100287 19990101 00287 GL 1999 1 1 98ZZZX4816 2 19981209 A 7314 PLUG BENDIX 3865005 BOLKMS 105 BO105CBS 5626008 EU ALLSN 250C 250C20 03013 GL FUEL PUMP LEAKING A HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 911FL 91 T1589 S171 CAE822237F EN ROUTE TO SCENE, CREW DETECTED STRONG SMELL OF FUEL. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL SEEPING FROM SA FTIED PLUG ON END OF FUEL PUMP FILTER COVER. RE-TORQUED PLUG AND RE-SAFTIED. LEAK CHECKED AND RETURNED TO SERVICE. RE F: ALLSION 250-C20 IPC, CHAPTER 73-20-00, FIGURE 1, ITEM 67. 1 G 7 2 3U 3 U NC H3EU E4CE 1999010100293 19990101 00293 NE 1999 1 1 98ZZZX4822 1 19981210 A 2612 7630607902101 FIRE DETECTOR SKRSKY S76 S76A 8143006 NE NR 1 ENGINE MALFUNCTIONED A HEEA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 03 1545K 760047 NR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED IN-FLIGHT. SECURED ENGINE AND FIRED BOTH ENGINE COMPARTMENT FIRE EXTINGUISHE RS. LANDED WITHOUT INCIDENT. NO APPARENT FIRE, INDICATION ONLY. MAINTENANCE FOUND DEFECTIVE LT FORWARD FLAME DETECTOR . REF: S-76 IPC, CHAPTER 26-11-00, FIGURE 1, ITEM 21. 1 G 7 2 3U H1NE 1999010100303 19990101 00303 WP 1999 1 1 TWAA9820201 1 19981230 A 2121 6054577 FAN DOUG DC9 DC982 3022082 WP CABIN FAILED A TWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 05 913TW 49184 SOME SMOKE AND SLIGHT BURNING ODOR REPORTED IN THE CABIN. THE -C- PHASE 50 AMP CB, AND A COUPLE OTHER BREAKERS, POPPED. FLIGHT DIVERTED TO IND. FOUND THE RECIRC FAN MOTOR HAD OVERHEATED, CAUSING OTHER BREAKERS TO POP. THE RECIRC FAN WAS DEFERRED PER MEL FOR REPLACEMENT AT A MAINTENANCE STATION. CHECK-C 12-30-97 MCI. 2 L 7 2 4F A6WE 1999010100304 19990101 00304 WP 1999 1 1 TWAA9820202 1 19981223 A 5320 MEMBRANE DOUG DC9 DC931 3022065 WP BS 984 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 982PS 47251 DURING OP 16 MAINT CHECK, FOUND CABIN MEMBRANE CRACKED APPROXIMATELY .75 INCH AT STA 984 RT SIDE. STOP DRILLED CRACK 0. 250 HOLE. FABRICATED DOUBLER AND INSTALLED FASTENERS TYPICAL WEB REPAIR SRM 53-01 PG 3. 2 L 7 2 4F A6WE 1999010100305 19990101 00305 WP 1999 1 1 9811019922 1 19981224 A 3350 BATTERY DOUG DC9 DC932 3022066 WP CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 945N 47664 DURING LINE CHECK, FOUND FIRST CLASS SECTION SEAT MOUNTED EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED BATTERIES, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999010100306 19990101 00306 WP 1999 1 1 9811029606 1 19981224 A 3350 POWER SUPPLY DOUG DC9 DC932 3022066 WP CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 606NW 47225 DURING B-CHECK, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL . 2 L 7 2 4F A6WE 1999010100307 19990101 00307 WP 1999 1 1 9811039997 1 19981226 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP GALLEY DOOR INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 8933E 47142 DURING LINE CHECK, FOUND FIRST CLASS SECTION EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AT GALLEY DOOR, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999010100308 19990101 00308 WP 1999 1 1 9811049964 1 19981224 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING B-CHECK, FOUND CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHECK N ORMAL. 2 L 7 2 4F A6WE 1999010100309 19990101 00309 WP 1999 1 1 9811059964 1 19981228 A 3350 POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 912RW 47150 DURING LINE CHECK, FOUND CATWALK EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY, OPERATIONAL CHEC K NORMAL. 2 L 7 2 4F A6WE 1999010100310 19990101 00310 WP 1999 1 1 9811069857 1 19981229 A 2150 CLAMP DOUG DC9 DC951 3022051 WP LT ACM LOOSE A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 766NC 47739 DURING CLIMBOUT, THE TAIL COMPARTMENT HIGH TEMPERATURE INDICATION LIGHT ILLUMINATED 30 SECONDS AFTER TAIL DEICE WAS SELE CTED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL. RETURNED TO BNA AND LAN DED WITHOUT INCIDENT. MAINTENANCE FOUND AND REPLACED A LOOSE CLAMP AT THE AFT SECTION, LEFT SIDE, AIR CYCLE MACHINE, AN D INSPECTED TAIL COMPARTMENT DUCTING. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999010100311 19990101 00311 NM 1999 1 1 98FDEA00768 1 19981230 A 5320 HFAB53AN011 SHEAR TIE BOEING 727 727247 138408F NM BS 520 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 236FE 21330 CORROSION (C53-113-01,1) ON FWD CARGO BAY SHEAR TIE BS 520, STR 27-28 RT. *S/D* REMOVED AND REPLACED SHEAR TIE BS 520, STR 27-28R IAW FEDEX 51-30-2 AND DWG NR 65-15929. 2 L 7 3 4F A3WE 1999010100312 19990101 00312 NM 1999 1 1 98FDEA00769 1 19981229 A 3230 1U10851 VALVE BOEING 727 72722 1384002 NM LT MLG FAILED A FDEA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 25 190FE 19083 LOST ALL SYS A UPON GEAR RETRACT, SHUT OFF VALVES FOR 33 MIN. REMOVED AND REPLACED LEFT MAIN GEAR LOCK PER MM 32-32-031 -4, A SYS RETURN FILTER PER MM 29-11, NR 1 AND NR 2 HYD PUMP CASE DRAIN FILTER ASSY PER MM 29-11. RAN NR 1 AND 2 ENG PE R JET RUN HANDBOOK. PRESS A SYS HYD RECKED NR 1 AND 2 CASE DRAIN AND A SYS RETURN FILTERS PER MM 32-32-031 AND 32-32-00 0-5. 2 L 7 3 4F A3WE 1999010100313 19990101 00313 NM 1999 1 1 98FDEA00770 1 19981230 A 3260 CONNECTOR BOEING 727 72725C 138400H NM RT MLG DOOR CONTAMINATED A FDEA O OTHER N FALSE WARNING DE DESCENT 1 SO 25 135FE 19853 RIGHT MAIN GEAR DOOR LIGHT CAME ON AT 12,000 FT DURING DESCENT AT 340 KIAS. CYCLED GEAR AND ALL LIGHTS WENT OUT IND NOR MAL. *S/D* REMOVED WATER FROM RIGHT GEAR DOOR LOCK CONDUIT. REMOVED AND REPLACED D752 CANNON PLUG, OPER CK GOOD AS PE R MM 32-62-0. 2 L 7 3 4F A3WE 1999010100314 19990101 00314 WP 1999 1 1 ABXA9801193 1 19981223 A 3350 41B004AD07G3 BATTERIES DOUG DC9 DC941 302207N WP CABIN DISCHARGED A ABXA K NONE L NO TEST IN INSP/MAINT 1 GL 23 965AX 47498 DURING PREFLIGHT, EMERGENCY LIGHTS ILLUMINATED, THEN WENT OUT. REPLACED EMERGENCY LIGHT BATTERIES. 2 L 7 2 4F A6WE 1999010100315 19990101 00315 WP 1999 1 1 MWEA981207 1 19981201 A 5320 591015835 JAMB DOUG DC9 DC932 3022066 WP CARGO DOORWEB CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND NUMEROUS AREAS OF LIGHT CORROSION ON AFT CARGO DOOR CUTOUT AREA INCLUDING DOOR JAMB WEB AND DOUBLER STRAPS. MTC F ABRICATED AND INSTALLED NEW JAMB WEB. 2 L 7 2 4F A6WE 1999010100316 19990101 00316 WP 1999 1 1 MWEA981209 1 19981201 A 5313 991224345 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CHAFED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CHAFE MARKS AT STATION 965 ARCHWAY BETWEEN LAV FORWARD PYLON BULKHEADS NEAR LONGERON 4R AND 4L. MTC BLENDED CHAFE D AREAS, FABRICATED AND INSTALLED REPAIR ANGLES. 2 L 7 2 4F A6WE 1999010100317 19990101 00317 WP 1999 1 1 MWEA981210 1 19981201 A 5315 991556171 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 996 CORROSION A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CORROSION AT STATION 996 FLOORBEAM TOP AND BOTTOM RIGHT TO LEFT SIDE. MTC FABRICATED AND INSTALLED REPAIR DOUBLER STRAPS. 2 L 7 2 4F A6WE 1999010100318 19990101 00318 WP 1999 1 1 MWEA981211 1 19981201 A 5312 591013013 BLKHD SKIN DOUG DC9 DC932 3022066 WP AFT PRESURE DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CRACK IN UPPER AFT PRESSURE DOOR CORNER. MTC STOP DRILLED CRACK AND INSTALLED DOUBLER. 2 L 7 2 4F A6WE 1999010100319 19990101 00319 WP 1999 1 1 MWEA981212 1 19981201 A 5313 27779224 LONGERON DOUG DC9 DC932 3022066 WP BS 965 CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CRACK ON LONGERON 17L AND 17R AT STATION 965. MTC FABRICATED AND INSTALLED LONGERON. 2 L 7 2 4F A6WE 1999010100320 19990101 00320 WP 1999 1 1 MWEA981213 1 19981201 A 5312 99115468 BULKHEAD WEB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 502ME 48132 FOUND CORROSION ON STATION 996 BULKHEAD WEB RIGHT OUTBOARD EDGE BETWEEN L19R AND L21R. MTC REMOVED CORROSION, FABRICATE D AND INSTALLED WEB SECTION. 2 L 7 2 4F A6WE 1999010100321 19990101 00321 1999 1 1 MWEA981214 4 19981228 A 3416 51828007208 ALTIMETER DOUG DC9 DC932 3022066 WP RT COCKPIT FAILED A MWEA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 301ME 47190 CLIMBING OUT OF 5,000 FEET, F/O'S ALTIMETER FLAGGED AND STOPPED NUMBER 2 TRANSPONDER FAIL LIGHT ON. AIR TURNBACK TO MKE . REMOVED AND REPLACED F/O'S ALTIMETER AND CHECKED OUT NUMBER 2 TRANSPONDER. 2 L 7 2 4F A6WE 1999010100322 19990101 00322 SO 1999 1 1 SWIA971334 1 19981205 A 2751 CONNECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT TE FLAP CONTAMINATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 199SW 120237 UPON CLIMBOUT AT FLAP RETRACTION, RECEIVED FLAP DISAGREEMENT RIGHT SIDE. RETURNED TO SLC. FOUND MOISTURE IN OUTBOARD L EFT FLAP CANNON PLUG. CLEANED BOTH FLAP ACTUATOR CANNON PLUGS. NO FAULTS OR DISAGREEMENTS. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100323 19990101 00323 SO 1999 1 1 SWIA971335 1 19981205 A 5753 FLAP EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT TE FLAP DAMAGED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 FLAP DISAGREEMENT ON FLAP RETRACTION RIGHT SIDE. RETURNED TO SLC. REMOVED AND REPLACED LEFT OUTBOARD FLAP IAW EMB MM 2 7-50-04, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100324 19990101 00324 1999 1 1 SWIA971336 4 19981205 A 3425 EHIS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT COCKPIT FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 198SW 120227 LEFT EHSI SCREEN WENT BLANK INFLIGHT DURING CLIMBOUT. RETURNED TO SLC. INSTALLED SERVICEABLE EHSI SCREEN, OPS CHECKS G OOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100325 19990101 00325 SO 1999 1 1 SWIA971337 1 19981205 A 3020 211C117183 DEICE BOOT EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A SWIA A UNSCHED LANDING O OTHER CR CRUISE 1 NM 07 289UE 120191 LEFT ENGINE INLET DEICE BOOT FAILED IN FLIGHT. RETURNED TO PDX. REPLACED LEFT ENGINE INLET PRESSURE SWITCH IAW MM 30-0 0-00. OPS AND LEAKS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100326 19990101 00326 SO 1999 1 1 SWIA971338 1 19981210 A 5753 TRACKS EMB 120 EMB120RT SO PWA 118 PW118 NE LT TE FLAP LACK OF LUBE A SWIA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NM 07 1105G 120105 LEFT OUTBOARD FLAP DISAGREEMENT WOULD NOT RETRACT. RETURNED TO SEA. RESET FLAP CONTROL PANEL AND CLEANED AND LUBED FLA P TRACKS, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100327 19990101 00327 EA 1999 1 1 SWIA971339 1 19981215 A 2750 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 407SW 7034 FLAPS FAIL MESSAGE AT FL330. RETURNED TO SLC, MADE A NO FLAP LANDING. COMPLIED WITH AD 98-20-01. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10. 2 L 7 2 4F 4 F RT A21EA E15NE 1999010100328 19990101 00328 SO 1999 1 1 SWIA971340 1 19981216 A 3233 ACTUATOR EMB 120 EMB120RT SO PWA 118 PW118 NE RT MLG FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 129AM 120119 AFTER TAKEOFF, RIGHT MAIN WOULD NOT RETRACT. RETURNED TO SEA. REMOVED AND REPLACED RIGHT MAIN GEAR ACTUATOR IAW MM 32- 32-10. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100329 19990101 00329 SO 1999 1 1 SWIA971341 1 19981214 A 3260 UPLOCK TARGET EMB 120 EMB120RT SO PWA 118 PW118A NE LT MLG OUT OF ADJUST A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 268UE 120207 AFTER TAKEOFF ATTEMPTED TO RETRACT GEAR, RIGHT MAIN AND NOSE UPLOCKED CORRECTLY BUT LEFT MAIN A & B RED LIGHTS REMAINED ILLUMINATED. CYCLED GEAR DOWN THEN BACK UP WITH SAME RESULT, RED A & B LIGHTS ILLUMINATED ON LEFT MAIN. ALL OTHER LIGH TS AND INDICATIONS WERE NORMAL. RETURNED TO FAT. ADJUSTED LEFT MAIN UPLOCK TARGET ADJUSTMENT IAW MM 32-61-01 AND PERFO RMED GEAR SWING IAW MM 32-30-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100330 19990101 00330 NM 1999 1 1 SWAA983124 1 19981217 A 2612 FIRE LOOP BOEING 737 7372H4 138448C NM NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 90SW 22905 NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED AFTER TAKEOFF. REDUCED ENGINE TROTTLE TO IDLE. AIRCRAFT RETURNED TO PHX AND MAD E AN UNEVENTFUL LANDING. INSPECTED COWL DUCT AREA, NO LEAKS NOTED. REMOVED AND REPLACED UPPER FIRE DETECTION LOOP ON N R 2 ENG PER MM, OPS CKS GOOD PER M/M. 2 L 7 2 4F A16WE 1999010100331 19990101 00331 NM 1999 1 1 SWAA983125 1 19981217 A 2612 FIRE LOOP BOEING 737 7372H4 138448C NM NR 2 ENGINE FAILED A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 90SW 22905 NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING CLIMBOUT. AIRCRAFT RETURNED TO OAK AND MADE AN UNEVENTFUL LANDING. REMOV ED AND REPLACED UPPER AND LOWER FIRE DETECT LOOPS, FIRE DETECT MODULE AND FIRE CONTROL PANEL. CHECKED ALL WIRING FROM E & E BAY TO ENGINE. DURING CHECKS, FOUND INLET GUISE VANE CASE CRACKED ON TOP. REPLACED INLET CASE. 2 L 7 2 4F A16WE 1999010100332 19990101 00332 NM 1999 1 1 SWAA983126 1 19981217 A 2530 STRAP BOEING 737 7373H4 1384600 NM SERVICE DOOR OUT OF POSITION A SWAA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 327SW 23691 AFTER TAKEOFF, NOTED NOISE FROM FWD SERVICE DOOR AREA. AIRCRAFT RETURNED TO BWI AND LANDED WITHOUT INCIDENT. INSPECTED AND FOUND A SAFETY STRAP STUCK OUTSIDE OF DOOR. RESECURED FWD SERVICE DOOR SAFETY STRAP INSPECTED DOOR AND FRAME FOR D AMAGE. NO DAMAGE NOTED, OK TO CONTINUE. 2 L 7 2 4F RT A16WE 1999010100333 19990101 00333 NM 1999 1 1 SWAA983127 1 19981217 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED SC CHECK, FOUND SEVERAL CRACK INDICATIONS AT BS 1016, BETWEEN S6 AND 7L. REPAIRED PER SWA RA 1-253-196 2. 2 L 7 2 4F A16WE 1999010100334 19990101 00334 NM 1999 1 1 SWAA983128 1 19981217 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED SC CHECK, FOUND SEVERAL FUSELAGE SKIN CRACK INDICATIONS AT BS 178. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999010100335 19990101 00335 NM 1999 1 1 SWAA983129 1 19981217 A 5320 WEB BOEING 737 7373H4 1384600 NM BS 663 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED SC CHECK, FOUND 2 BEADED PRESSURE WEB CRACKS AT BS 663. REPAIRED PER SWA RA 1-353-1956. 2 L 7 2 4F RT A16WE 1999010100336 19990101 00336 NM 1999 1 1 SWAA983130 1 19981217 A 5320 STRAP BOEING 737 7373H4 1384600 NM BS 178 SEVERED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED SC CHECK, FOUND SUPPORT STRAP SEVERED AT BS 178. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999010100337 19990101 00337 NM 1999 1 1 SWAA983131 1 19981217 A 5320 CHORD BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 306SW 22946 DURING SCHEDULED SC CHECK, FOUND BS 178 T-CHORD CRACKED. REPAIRED PER SWA RA 1-353-1959. 2 L 7 2 4F RT A16WE 1999010100338 19990101 00338 NM 1999 1 1 SWAA983132 1 19981220 A 3350 20131 BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 304SW 22944 DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT OVER AFT GALLEY AND DOOR INOP. REMOVED AND REPLACED BATTERY PACK PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010100339 19990101 00339 NM 1999 1 1 SWAA983133 1 19981219 A 5320 FRAME BOEING 737 7375H4 138449D NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 514SW 25153 DURING SCHEDULED 1/4D CHECK, FOUND FWD ENTRY DOOR FRAME CRACKED. REPAIRED PER BOEING S/B 737-52-1006. 2 L 7 2 4F RT A16WE 1999010100340 19990101 00340 NM 1999 1 1 SWAA983134 1 19981219 A 5330 SKIN BOEING 737 7373A4 1384585 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD LOWER CORNER OF AFT SERVICE DOOR. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1999010100341 19990101 00341 NM 1999 1 1 SWAA983135 1 19981219 A 5330 SKIN BOEING 737 7373A4 1384585 NM SERVICE DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER CORNER OF FWD SERVICE DOOR. REPAIRED PER BOEING S RM. 2 L 7 2 4F RT A16WE 1999010100342 19990101 00342 NM 1999 1 1 SWAA983136 1 19981219 A 5330 SKIN BOEING 737 7373A4 1384585 NM BS 520 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 676SW 23288 DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN BULGING AT RIVETS AFT OF BS 520C, S28R LOWER FUSELAGE. INSTALLED DOUBL ER AND TRIPLER PER SWA RA 1-353-1961. 2 L 7 2 4F RT A16WE 1999010100343 19990101 00343 NM 1999 1 1 SWAA983137 1 19981218 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 1016 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 82SW 22731 DURING SCHEDULED SC CHECK, FOUND BS 1016 BULKHEAD CRACKED BETWEEN S6 AND 7L. REPAIRED PER SWA RA 1-253-1962. 2 L 7 2 4F A16WE 1999010100344 19990101 00344 NM 1999 1 1 SWAA983138 1 19981218 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 727-908 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND FLOOBEAM CORRODED BETWEEN BS 727 TO 908. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100345 19990101 00345 NM 1999 1 1 SWAA983139 1 19981218 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAMS CORRODED BETWEEN BS 727 TO 947. REPLACED DAMAGED SECTIONS PER BOEING S RM. 2 L 7 2 4F A16WE 1999010100346 19990101 00346 NM 1999 1 1 SWAA983140 1 19981218 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 440 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 62SW 22060 DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CORRODED AT BS 440, BETWEEN S25 AND 26R. REPLACED DAMAGED SECTION PER BO EING SRM. 2 L 7 2 4F A16WE 1999010100347 19990101 00347 NM 1999 1 1 SWAA983141 1 19981218 A 3240 BRAKES BOEING 737 7372H4 138448C NM MLG REQD SERVICE A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 95SW 23054 BRAKES FELT SPONGY ON TAXI IN. LOTS OF BRAKE PEDAL TRAVEL AND EFFORT AND NOT MUCH STOPPING POWER. BLED ALL FOUR BRAKES AND TAXI CHECKED OK PER BOEING M/M. 2 L 7 2 4F A16WE 1999010100348 19990101 00348 NM 1999 1 1 GAIA98131 1 19981210 A 5230 FASTENER BOEING 727 727223 1384074 NM CARGO DOOR MISSING A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6808 19483 DURING ROUTINE INSPECTION, NUMEROUS CENTER ROW RIVETS WERE FOUND MISSING FROM MAIN CARGO DOOR (MCD) LAP SEAM AREA, 10L, BETWEEN FRAMES. REF STC ST00015AT, ATAZ CARGO DOOR MODIFICATION. REPLACED MISSING RIVETS PER STC NR ST00015AT, ATAZ DR AWINGS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999010100349 19990101 00349 NM 1999 1 1 GAIA98129 1 19981207 A 5230 FASTENERS BOEING 727 727223 1384074 NM CARGO DOOR MISSING A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 6812 19487 DURING ROUTINE INSPECTION NUMEROUS CENTER ROWS, RIVETS WERE FOUND MISSING FROM MAIN CARGO DOOR (MCD) LAP SEAM AREA, 10L, BETWEEN FRAMES. REF STC ST00015AT, ATAZ CARGO DOOR MODIFICATION. REPLACED MISSING RIVETS PER STC NR ST00015AT, ATAZ D RAWINGS. AIRCRAFT WAS THE RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999010100350 19990101 00350 NM 1999 1 1 GAIA98130 1 19981209 A 2913 AS19570C PUMP BOEING 727 7272J0 138407E NM NR 1 ENGINE LEAKING A GAIA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SW 07 281KH 21105 CAPTAIN REPORTED AIRCRAFT LOST 'B' SYSTEM HYDRAULIC QUANTITY 10 MINUTES FROM LANDING AT OAK. DECLARED EMERGENCY AND LAN DED WITHOUT FURTHER INCIDENT. FOUND NR 1 HYDRAULIC PUMP LEAKING. REPLACED NR 1 HYD PUMP. (M) 2 L 7 3 4F RT A3WE 1999010100351 19990101 00351 NM 1999 1 1 GAIA98127 1 19981207 A 2621 8068005 FIRE BOTTLE BOEING 727 727223 1384074 NM LEFT DISCHARGED A GAIA K NONE N FALSE WARNING CL CLIMB 1 SW 07 6812 19487 DURING CLIMB-OUT OF TOL, THE LEFT FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED ITS LEG TO JFK AND LA NDED WITHOUT FURTHER PROBLEMS. REMOVED AND REPLACED THE LEFT HRD FIRE EXTINGUISHER BOTTLE IAW BOEING MM 26-21-1. RETUR NED TO AIRCRAFT TO SERVICE. (M) 2 L 7 3 4F A3WE 1999010100352 19990101 00352 NM 1999 1 1 GAIA98128 1 19981104 A 3350 BULB BOEING 727 727223 1384074 NM CABIN FAILED A GAIA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6821 19496 DURING WALK AROUND, BULB IN EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999010100353 19990101 00353 NM 1999 1 1 98ZZZM952 1 19981021 A 5330 SKIN BOEING 727 727230 1384080 NM BS 474 PUNCTURED A C8GA K NONE O OTHER IN INSP/MAINT 1 SO 15 357KP 59485 20675 FLIGHT 220 - KHDY-KDSM - AFTER AIRCRAFT ARRIVAL DURING LOADING OPERATIONS, A FORKLIFT PUNCTURED THE LEFT FUSELAGE AT STA TION 474. EVALUATION REVEALED THE DAMAGE WAS APPROXIMATELY 7 INCH BY 4 INCH AND WAS CONFINED TO SKIN ONLY. THE AIRCRAF T WAS RELEASED FOR FERRY FLIGHT FROM KDSM TO KDAY FOR REPAIRS. DAMAGE WAS REPAIRED IAW THE B727 STRUCTURAL REPAIR MANUA L SRM 53-30-3 FIGURE 1. THE AIRCRAFT WAS RELEASED FOR REVENUE SERVICE. (M) 2 L 7 3 4F A3WE 1999010100354 19990101 00354 SO 1999 1 1 ASOA98097 1 19981114 A 2910 LINE EMB 120 EMB120RT SO LT MLG WW BROKEN A ASOA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 237AS 120051 EN ROUTE LFT-DFW - THE GREEN SYSTEM HYDRAULICS FAILED AT 20,000 FT. CREW DECLARED AND EMERGENCY AND LANDED AT DFW SAFEL Y AND WITHOUT FURTHER INCIDENT. DFW MAINTENANCE FOUND THE LEFT HYDRAULIC PRESSURE LINE FROM THE RESERVOIR BROKEN AND RE PAIRED THE LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999010100355 19990101 00355 SO 1999 1 1 ASOA98098 1 19981115 A 6120 M832481030 O-RING EMB 120 EMB120RT SO RT PCU LEAKING A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 282AS 120226 EN ROUTE VLD-ATL - RIGHT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE BETWEEN 45 AND 60 PSI. CREW REDUCED POWER AND THE OIL P RESSURE SETTLED AT 55 PSI. CREW DECLARED AN EMEGENCY AND DIVERTED TO MCN, WHERE LANDING WAS MADE SAFELY AND WITHOUT FUR THER INCIDENT. MCN MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE PCU O-RING. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999010100356 19990101 00356 SO 1999 1 1 ASOA98075 1 19980927 A 2910 LINE EMB 120 EMB120RT SO LT MLG WW BROKEN A ASOA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 11 227AS 120023 EN ROUTE ATL-BQK, THE GREEN SYSTEM HYDRAULIC QUANTITY APPEARED LOW. AFTER OBSERVING THE GAUGE, A NOTICEABLE DROP OCCURR ED AND THE RESERVOIR LOW LEVEL LIGHT ILLUMINATED. CREW FOLLOWED THE APPROPRIATE CHECKLISTS, DECLARED AN EMERGENCY AND D IVERTED INTO MCN WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. MCN MAINTENANCE FOUND THE LEFT HYDRAULIC P RESSURE LINE FROM THE RESERVOIR BROKEN AND REPLACED THE LINE. OPERATIONAL AND LEAK CHECKS WERE GOOD AND THE AIRCRAFT WA S RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T RT A31SO 1999010100358 19990101 00358 WP 1999 1 1 98ZZZM954 1 19980919 A 7933 INDICATOR LKHEED 1011 10113851 5265010 WP COCKPIT FAILED A AMTA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 190AT 193C1086 DURING CRUISE, THE NR 3 OIL TEMP INDICATOR BURNED UP, C/B PULLED, CANNON PLUG DISCONNECTED. REPLACED TEMP INDICATOR. ( M) 2 L 7 3 4F A23WE 1999010100359 19990101 00359 NM 1999 1 1 98ZZZM955 1 19980526 A 3350 BATTERY BOEING 727 727290 138408W NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 775AT 21511 DURING P/F, FOUND THE FIRST COMPLETE FORWARD SECTION OF EGRESS TRACK LIGHTING INOP. REMOVED AND REPLACED EMERGENCY BATT ERY SUPPLY, CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999010100360 19990101 00360 NM 1999 1 1 98ZZZM956 1 19981103 A 3350 S106 BATTERY BOEING 727 727227 1384078 NM CABIN DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 773AT 22004 DURING P/F, FOUND FLIGHT DECK EMERGENCY EXIT LIGHT WILL NOT TEST. REPLACED BATTERIES, CHECKED GOOD PER MM 33-50-10. (M ) 2 L 7 3 4F A3WE 1999010100361 19990101 00361 WP 1999 1 1 ORJA98298 1 19981127 A 3350 60030457 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 20 DEF DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 SJC - EMERGENCY EXIT INOP SEAT 20DEF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PACK. (M) 2 L 7 2 4F RT A6WE 1999010100362 19990101 00362 WP 1999 1 1 ORJA98300 1 19981127 A 3350 60030457 BATTERY PACK DOUG DC9 DC983 3022083 WP EMERGENCY EXIT DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 SJC - EMERGENCY LIGHT IN EMPENNAGE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PACK IN EMPANNAGE. (M) 2 L 7 2 4F RT A6WE 1999010100363 19990101 00363 WP 1999 1 1 OFJA98302 1 19981124 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 14-17 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 LAX - CABIN EMERGENCY LIGHTS CAME ON ROW 14-17 WILL NOT GO OUT. REPLACED LEFT AFT OVERWING EMERGENCY BATTERY PACK. OPS NORMAL. (M) 2 L 7 2 4F RT A6WE 1999010100364 19990101 00364 WP 1999 1 1 ORJA98306 1 19981206 A 3350 PPSIB CHARGER DOUG DC9 DC983 3022083 WP ROWS 8-11 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 COS - EMERGENCY LIGHTS AT ROWS 8, 9, 10, 11 DO NOT WORK. REMOVED AND REPLACED BATTERIES CHARGER SYSTEM. OPS CHECK GOOD . (M) 2 L 7 2 4F RT A6WE 1999010100365 19990101 00365 WP 1999 1 1 ORJA98295 1 19981105 A 3350 BR9661106 BATTERY PACK DOUG DC9 DC983 3022083 WP SEATS 8-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 OKC - EMERGENCY LIGHTS INOP SEATS 8-11 AND FORWARD RIGHT EXIT ID. REMVOED AND REPLACED BATTERY PACK IAW MX82. TESTED E MERGENCY LIGHTS AT SEATS 8-11 AND FORWARD RIGHT OVERWING EXIT ID IAW BRUCE IND MANUAL 400-082. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 1999010100366 19990101 00366 WP 1999 1 1 ORJA98296 1 19981111 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP ROW 28 MISSING A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 OKC - RIGHT SEAT ROW 28 EMERGENCY LIGHTING PLUG MISSING. SPLICED WIRING AT ROW 28 EMERGENCY LIGHTING WIRING IAW MD80WDM 20-10-03 TESTED EIE ROW 28 EMERGENCY LIGHTING IAW BRUCE IND MANUAL 400-082. (M) 2 L 7 2 4F RT A6WE 1999010100367 19990101 00367 WP 1999 1 1 ORJA98309 1 19981111 A 5320 ANGLE DOUG DC9 DC983 3022083 WP BS 168 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 871RA 49788 LEVEL 2 CORROSION ON FLOR SUPPORT CUSP ANGLE RBL 54 STATION 168 LOWER FORWARD CORNER OF R1 DOOR CUTOUT (OTBOARD SIDE). C UT OUT CORRODED SECTION FABRICATED REPAIR DOUBLER, SEALED AND INSTALLED IAW MD83 SRMS 51-10-3, 53-01. (M) 2 L 7 2 4F RT A6WE 1999010100368 19990101 00368 WP 1999 1 1 ORJA98292 1 19981125 A 3350 DC6516SS CONNECTOR DOUG DC9 DC983 3022083 WP SEAT 14D FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO - EMERGENCY LIGHT INOP ON SEAT 14D. REMOVED AND REPLACED LIGHT SOCKET CONNECTOR ASSY, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999010100369 19990101 00369 WP 1999 1 1 ORJA98304 1 19981202 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 12,14,15,16 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN RNO - EMERGENCY LIGHTS ON ROWS 12, 14, 15, 16. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999010100370 19990101 00370 WP 1999 1 1 ORJA98303 1 19981125 A 3350 BR9661106 POWER PACK DOUG DC9 DC983 3022083 WP EMERGENCY DOOR INOP A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 IN SJC - EMERGENCY LIGHTS INOP RIGHT FORWARD EMERGENCY DOOR OVERWING. REPLACED POWER PACK BR9661-106, OPS CHECK OK. (M ) 2 L 7 2 4F RT A6WE 1999010100371 19990101 00371 WP 1999 1 1 ORJA98294 1 19981125 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 19-21 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAS, RED EMERGENCY LIGHTS WILL NOT EXTINGUISH AT 19D, 20D AND 21D. INSTALLED NEW BATTERY PACK ON FORWARD RIGHT OVERW ING EXIT. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999010100372 19990101 00372 WP 1999 1 1 ORJA98299 1 19981120 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 20 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 SJC - EMERGENCY EXIT LIGHTS INOP AT ROW 8-16. REMOVED AND REPLACED BATTERY PACK (CHARGER) AT 20 DEF AND 20 AC. (M) 2 L 7 2 4F RT A6WE 1999010100373 19990101 00373 WP 1999 1 1 ORJA98310 1 19981206 A 3350 PPSIB CHARGER DOUG DC9 DC987 3022087 WP ROWS 20/21 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT LAS, FLIGHT ATTENDANT REPORTED THAT EMERGENCY EXIT LIGHTS AT ROWS 20 AND 21 CAME ON IN FLIGHT AND COULD NOT BE TURNED OFF. REPLACED BATTERY CHARGER AT RIGHT AFT O/W EXIT. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999010100374 19990101 00374 NM 1999 1 1 ORJA98308 1 19981204 A 3610 CONTROLLER DOUG MD90 MD9030 3023690 NM PNEUMATIC SYSTEM MALFUNCTIONED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 901RA 53489 IN RNO - AFTER TAKEOFF, ROLL 6 FT PNEU SYSTEM FAULT REJECTED TAKEOFF RETURN TO GATE. RAN BIT TEST ON PNEU SYSTEM CONTRO LLER, NO FAULTS NOTED SYSTEM FAULT CLEARED MESSAGE CLEARED. (M) 2 L 7 2 4F RT A6WE 1999010100375 19990101 00375 NM 1999 1 1 MASA98220 1 19981207 A 3350 V63367 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 FLT 6389 - PHX-YUM - DURING PREFLIGHT INSPECTION, CREW REPORTED THAT THE EMERGENCY LIGHT SWITCH HAD BEEN LEFT IN THE ON POSITION OVERNIGHT AND ALL THE POWER SUPPLIES TO THE EMERGENCY LIGHTING HAD BEEN DRAINED. MAINTENANCE CONNECTED THE GPU TO THE AIRCRAFT AND CHARGED THE BATTERIES, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999010100376 19990101 00376 NM 1999 1 1 MASA98221 1 19981209 A 3350 2LA00734480 LENS DHAV DHC8 DHC8202 2809007 NM PAX DOOR MISSING A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 FLT 6231 - MTJ -PHX - DURING PREFLIGHT INSPECTION, FOUND EMERGENCY EXIT LENS COVER MISSING, OVER MAIN CABIN DOOR. THE A IRCRAFT FERRIED TO GJT, WHERE MAINTENANCE REPLACED THE LENS. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999010100377 19990101 00377 NM 1999 1 1 MASA98219 1 19981205 A 3397 82425112001 WIRE DHAV DHC8 DHC8202 2809007 NM CABIN CONTAMINATED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 456YV 456 FLT 6341 - PHX-PSP - PRIOR TO DEPARTURE, CREW REPORTED ONE SECTION OF FLOOR PATH LIGHTING WAS INOP. MAINTENANCE CLEANED AND RESET A CONNECTOR FOR THE CABLE ASSY, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999010100378 19990101 00378 NM 1999 1 1 TSAA9833606 1 19981130 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 NR 2 SEAT EMERGENCY LIGHT BATTERY PACK NO LIGHT. REPLACED NR 2 BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVIC E. (M) 2 L 7 2 4F RT A16WE 1999010100379 19990101 00379 NM 1999 1 1 TSAA9833607 1 19981201 A 3350 8613211 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 AFT EMERGENCY SLIDE LIGHT INOP. REPLACED BATTERY POWER PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010100380 19990101 00380 NM 1999 1 1 P2EA98278 1 19981117 A 5311 FRAME BOEING 737 737281 138448P NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - HORIZONTAL CHORD CRACKED AT BS 727, WL 202.5, LBL 26, DEFECT SIZE LENGTH 2.750 INCH. REPAIRED FUSELAGE BULKHEAD C OMPRESSION CHORD AT BS 727, WL 202.5, BETWEEN LBL 18 INCH AND LBL 36 INCH PER BOEING SERVICE BULLETIN 737-53-1053, REV 5 , DATED OCT 26, 1995, SECTION III, PART II FIG 4, 6 AND 7. (M) 2 L 7 2 4F A16WE 1999010100381 19990101 00381 NM 1999 1 1 P2EA98276 1 19981117 A 5320 BEAM BOEING 737 737281 138448P NM BS 540 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - VERICAL BEAM CRACKED AT BS 540, RBL 27, WL 203, DEFECT SIZE LENGTH 3.5 INCH. REPLACED FUSELAGE BULKHEAD VERTICAL BEAM AT BS 540, FROM WL 206 TO WL 151 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010100382 19990101 00382 NM 1999 1 1 P2EA98275 1 19981118 A 5320 WEB BOEING 737 737281 138448P NM BS 277 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - NOSE LANDING GEAR WHEEL WELL UPPER PRESSURE WEB CRACKED AT BS 277 RBL 9 INCH, DEFECT SIZE LENGTH 5.25 INCH. REPAI RED NOSE WHEEL WELL UPPER WEB SECTION FROM BS 274.125 TO BS 280.300, BETWEEN RBL 4 INCH AND RBL 14 INCH PER BOEING FAX C OO-SJO-98-1024RR DATED DECEMBER 1, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1999010100383 19990101 00383 NM 1999 1 1 P2EA98273 1 19981120 A 5330 SKIN BOEING 737 737281 138448P NM BS 907/967 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 FUSELAGE SKIN CORRODED BETWEEN BS 907 AND BS 967, BETWEEN STRINGER 4 RT AND STRINER 5 RT. REPLACED FUSELAGE SKIN SECTIO N FROM BS 902.5 TO BS 914, BETWEEN STRINGER 4 RT AND STRINGER 5 RT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. REMOVED CORR OSION FROM BS 907 TO BS 967 PER SRM 51-10-6. FOUND WITHIN LIMITS PER SRM 51-30-1 FIG 1. (M) 2 L 7 2 4F A16WE 1999010100384 19990101 00384 NM 1999 1 1 P2EA98272 1 19981117 A 5311 FRAME BOEING 737 737281 138448P NM FUSELAGE CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - BS 727 HORIZONTAL CHORD CRACKED AT WL 202.5, RBL 26, DEFECT SIZE LENGTH 2 INCHES. REPAIRED FUSELAGE BULKHEAD COMP RESSION CHORD AT BS 727, WL 202.5, BETWEEN RBL 18 INCH AND RBL 34 INCH PER BOEING SERVICE BULLETIN 737-53-1053 REV 5 DAT ED OCT 26, 1995 SECTION III, PART II, FIG 4, 6 AND 7. (M) 2 L 7 2 4F A16WE 1999010100385 19990101 00385 NM 1999 1 1 P2EA98271 1 19981118 A 5330 SKIN BOEING 737 737281 138448P NM BS 315/324 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - MAIN ENTRY DOOR LOWER HINGE CUTOUT EXTERNAL SKIN CRACKED, DEFECT SIZE LENGTH .75 INCH. REPAIRED SKIN SECTION FROM BETWEEN BS 316.5 AND BS 324 AT LOWER HINGE CUT OUT PER SRM 52-00-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999010100386 19990101 00386 NM 1999 1 1 P2EA98270 1 19981119 A 5347 SEAT TRACK BOEING 737 737281 138448P NM BS 639 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - SEAT TRACK WEB CRACKED AT BS 639, RBL 45.5, WL 201, DEFECT SIZE LENGTH 1 INCH. REPAIRED FUSELAGE WEB SECTION FROM BS 636 TO BS 642, FROM WL 204 TO WL 199.5, RBL 45.5 PER 51-40-2 FIG 1 PAGE 3. (M) 2 L 7 2 4F A16WE 1999010100387 19990101 00387 NM 1999 1 1 P2EA98269 1 19981119 A 5313 STRINGER BOEING 737 737281 138448P NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - STRINGER 5 LEFT SPLICE CRACKED AT BS 360, DEFECT SIZE LENGTH .75 INCH. REPLACED FUSELAGE STRINGER 5 LEFT SPLICE F ROM 348.2 TO BS 367 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010100388 19990101 00388 NM 1999 1 1 P2EA98268 1 19981120 A 5240 BEAM BOEING 737 737281 138448P NM SERVICE DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FORWARD SERVICE DOOR NR 7 BEAM CRACKED, DEFECT SIZE LENGTH .5 INCH. REPAIRED FUSELAGE SKIN FORWARD ENTRY DOOR BEA M NR 7 BETWEEN BS 302 AND BS 309 PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999010100389 19990101 00389 NM 1999 1 1 P2EA98267 1 19981121 A 5313 STRINGER BOEING 737 737281 138448P NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - STRINGER 15 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED STRINGER 15 LEFT SECTION FROM BS 348 TO BS 367 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010100390 19990101 00390 NM 1999 1 1 P2EA98266 1 19981121 A 5313 STRINGER BOEING 737 737281 138448P NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - STRINGER 14 LEFT CRACKED AT BS 360, DEFECT SIZE LENGTH .5 INCH. REPLACED FUSELAGE STRINGER 14 LT SECTION FROM BS 367 TO BS 348 PR SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010100391 19990101 00391 NM 1999 1 1 P2EA98265 1 19981121 A 5311 FRAME BOEING 737 737281 138448P NM BS 303 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FRAME WEB CRACKED AT BS 303.9, BETWEEN STRINGER 16L AND STRINGER 17L, DEFECT SIZE, LENGTH 1 INCH. REPAIRED FUSELA GE WEB SECTION AT BS 303.9, BETWEEN STRINGER 15 LEFT AND B STRINGER 18 LT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010100392 19990101 00392 NM 1999 1 1 P2EA98264 1 19981120 A 5311 FRAME BOEING 737 737281 138448P NM BS 344 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FRAME CRACKED AT BS 344, BETWEEN STRINGER 23 RT AND STRINGER 24 RT, DEFECT SIZE LENGTH 6.75 INCH. REPLACED FRAME SECTION AT BS 344, BETWEEN STRINGER 21 RT AND STRINGER 27 RT PER 51-10-1 PAGE 5 AND SRM 51-30-2. REPAIRED FUSELAGE FRAM E ANGLE SECTION AT BS 344 BETWEEN STRINGER 22 RT AND STRINGER 27 RT PER SRM 51-40 FIG 1. (M) 2 L 7 2 4F A16WE 1999010100393 19990101 00393 NM 1999 1 1 P2EA98260 1 19981119 A 5220 ANGLE BOEING 737 737281 138448P NM EMERG EXIT DOOR CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - RIGHT EMERGENCY EXIT DOOR FRAME ANGLE CRACKED AT FORWARD SECTION, DEFECT SIZE LENGTH .375 INCH. REPLACED RIGHT EM ERGENCY EXIT DOOR FORWARD FRAME ANGLE AT BS 622 PER SRM 51-10-01 PAGE 1 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010100394 19990101 00394 NM 1999 1 1 P2EA98261 1 19981118 A 5311 FRAME BOEING 737 737281 138448P NM BS 360 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - RIGHT FRAME CRACKED, AT E/E COMPARTMENT INTERNAL STRUCTURE AT BS 360, STRINGER 20 RT DEFECT SIZE LENGTH 3 INCHES. REPAIRED FUSELAGE FRAME SECTION AT BS 360, BETWEEN STRINGER 19 RT AND STRINGER 21 RT PER 51-40-3, FIG 1, DETAIL I. (M) 2 L 7 2 4F A16WE 1999010100395 19990101 00395 NM 1999 1 1 P2EA98258 1 19981119 A 5730 SKIN BOEING 737 737281 138448P NM WS 493-488 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - LEFT WING OUTBOARD FOREFLAP LEADING EDGE SKIN REPAIR DOUBLER WORN. REPAIRED FOREFLAP LEADING EDGE SKIN BETWEEN WS L 493 AND WSL 488 PER SRM 57-50-4 FIG 1. (M) 2 L 7 2 4F A16WE 1999010100396 19990101 00396 NM 1999 1 1 P2EA98259 1 19981118 A 5210 ANGLE BOEING 737 737281 138448P NM PAX DOOR CRACK A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FORWARD ENTRY DOOR NR 7 BEAM ANGLE CRACKED, DEFECT SIZE LENGTH 1.625 INCH. REPAIRED FORWARD ENTRY DOOR NR 7 BEAM ANGLES BETWEEN BS 336 AND BS 346 PER SRM 51-40-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999010100397 19990101 00397 WP 1999 1 1 ORJA98297 1 19981128 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROWS 7-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 LAX - EMERGENCY LIGHTS ROWS 7-11 CAME ON DURING FLIGHT DEPLEATED. REPLACED BATTERIES FORWARD RIGHT EXIT SIGN. (M) 2 L 7 2 4F RT A6WE 1999010100398 19990101 00398 EA 1999 1 1 VTZA98315 1 19981021 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 EA TE FLAP ACTIVATED A VTZA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 629BR 7251 FLT 6764 - PWM-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS THE FLAP FAULT W ARNING LIGHT ILLUMINATED. FLAPS STUCK AT ZERO. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET CIRCUIT BREAKER. MAINTENANCE ALSO OPENED RIGHT 1021 TO WATCH FLAPS, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETRN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999010100399 19990101 00399 WP 1999 1 1 VTZA98314 2 19981019 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT BIRD STRIKE A VTZA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. C F.O.D. TO TAKEOFF 1 EA 27 496UE 900 P66183 FLT 6152 - BGM-IAD - AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BIRD STRIKE ON RIGHT ENGINE. CREW SHUT DOWN ENGINE AND ACTIBATED FIRE EXTINGUISHER. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RIGHT ENGINE DUE TO BENT BLADE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999010100400 19990101 00400 EA 1999 1 1 VTZA98313 1 19981018 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B16 1900305 EA TE FLAP FAILED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED AP APPROACH 1 EA 27 621BR 7186 FLT 6767 - IAD-PWM - DURING APPROACH, AIRCRAFT MADE AN UNSCHEDULED LANDING AND DIVERTED TO BOS DUE TO FLAP FAULT WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BPSU, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999010100401 19990101 00401 EU 1999 1 1 VTZA98295 1 19980918 A 2932 S12211143 TRANSMITTER BAG JETSTM JETSTM3201 1500217 EU RT HYD SYSTEM MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 485UE 901 FLT 6342 - IAD-EWR - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT HYDRAULIC PRESSURE FLUCTUATION. M AINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PRESSURE TRANSMITTER AND OPENED DMI 51753, MEL 29-1. MAINTENANC E CLOSED DMI 51753 ON 9-23-98 BY REMOVING AND REPLACING TRANSMITTER AND PRESSURE INDICATOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010100402 19990101 00402 EU 1999 1 1 98ZZZM957 1 19980918 A 2932 S214160 INDICATOR BAG JETSTM JETSTM3201 1500217 EU RT HYD SYSTEM MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 485UE 901 FLT 6342 - IAD-EWR - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT HYDRAULIC PRESSURE FLUCTUATION. M AINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULIC PRESSURE TRANSMITTER AND OPENED DMI 51753, MEL 29-1. MAINTENANC E CLOSED DMI 51753 ON 9-23-98 BY REMOVING AND REPLACING TRANSMITTER AND PRESSURE INDICATOR. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010100403 19990101 00403 EU 1999 1 1 VTZA98310 1 19981018 A 5210 1415201641 SEAL JETAIR JETSTM JETSTM4101 1500501 EU PAX DOOR LOOSE A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 333UE 41101 FLT 6591 - IAD-ROA - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LOUD NOISE IN CABIN. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESECURED MAIN DOOR SEAL, OPS CHECK OK. AIRCRAFT WAS RELEA SED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999010100404 19990101 00404 EU 1999 1 1 VTZA98307 1 19981010 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE CHAFED A VTZA A E UNSCHED LANDING ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 EA 27 486UE 905 FLT 6495 - MDT-IAD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE FIRE WARNING LIGHT ILLUMINATE D AND CREW SHUT DOWN ENGINE. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FIRE LOOP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010100405 19990101 00405 EU 1999 1 1 VTZA98306 1 19981012 A 3244 AH1837 TIRE JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A VTZA O OTHER O OTHER LD LANDING 1 EA 27 330UE 41098 FLT 6260 - IAD-BUF - DURING LANDING, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS RIGHT INBOARD TIRE BLEW ON LANDING. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 3 MAIN TIRE, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999010100406 19990101 00406 EU 1999 1 1 VTZA98303 1 19981003 A 2611 72111211000 SMOKE DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY FAILED A VTZA O OTHER N FALSE WARNING LD LANDING 1 EA 27 303UE 41015 FLT 6308 - IAD-ALB - DURING LANDING, EXPERIENCED A POD SMOKE LIGHT ILLUMINATION. AIRCRAFT DECLARED AN EMERGENCY AND MAD E AN UNEVENTFUL LANDING AT ALB. MX CONTROL DISPATCHED MX TO A/C WHERE THE MX PERSONNEL INSPECTED THE POD SMOKE DETECTOR SYSTEM AND FOUND THE SMOKE DETECTOR IAW MX PROCEDURES AND THE A/C WAS RELEASED FOR SERVICE. A/C RETURNED TO IAD ON 10/ 04/98 WHERE MX REMOVED AND REPLACED THE POD SMOKE DETECTOR AND CLEARED THE DEFERRED MAINTENANCE ITEM ACTION. AIRCRAFT W AS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1999010100407 19990101 00407 NM 1999 1 1 98ZZZM958 1 19980818 A 3397 WIRE BOEING 757 75723N 1384973 NM ROWS 22-27 BROKEN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 517AT 27973 DURING P/F, FOUND EGRESS LIGHTS FROM ROW 22 TO 27 INOP. REPAIRED WIRING PER CHAPTER 33, OPS CHECKED NORMAL. (M) 2 L 7 2 4F RT A2NM 1999010100408 19990101 00408 NM 1999 1 1 98ZZZM959 1 19981020 A 3350 S417N50914 LIGHT BOEING 757 75723N 1384973 NM ROW 16 INOP A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 514AT 27971 ROW 16 FLOOR LIGHTS MODULE INOPERATIVE. REMOVED AND REPLACED EGRESS LIGHT MODULE AS REQUIRED, OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 1999010100409 19990101 00409 NM 1999 1 1 98ZZZM960 1 19981101 A 3350 CONNECTOR BOEING 757 75723N 1384973 NM CABIN LOOSE A AMTA K NONE L NO TEST AP APPROACH 1 GL 11 518AT 27974 DURING APPROACH EGRESS LIGHTS (FLOOR) INOP AT ROW31, 32, 8, 9 AND 10. RECONNECTED LOOSE TERMINALS AT ROW 2, 31 AND 8. O PS CHECKED GOOD. (M) 2 L 7 2 4F RT A2NM 1999010100410 19990101 00410 NM 1999 1 1 98ZZZM961 1 19981026 A 2150 RELAY BOEING 727 727290 138408W NM RIGHT PACK FAILED A AMTA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 11 774AT 21510 DURING TAXI, THE RIGHT AIR CONDITIONING PACK TRIPPED OFF AND CABIN IMMEDIATELY FILLED WITH SMOKE, GATE TURN BACK. FOUND RIGHT PACK FAN DOOR NOT OPENING, REPLACED DOOR CONTROL RELAY, DOOR OPS CHECKED GOOD. (M) 2 L 7 3 4F A3WE 1999010100411 19990101 00411 1999 1 1 USAABB98109 4 19981022 A 3460 658060021 CLOCK BOEING 767 7672B7 1385107 NM COCKPIT FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 651US 34468 1847 24764 PHL - FLT 42 - FLIGHT RETURNED TO PHL TWICE DUE TO FMC PROBLEMS. ETA'S WERE NOT BEING DISPLAYED ON THE PROGRESS PAGE ON BOTH OF THE CDU'S. MAINTENANCE SWAPPED BOTH FMC'S WITH ANOTHER AIRCRAFT. NO FAULT WAS FOUND WITH THE FMC'S. THE CAPT AIN'S CLOCK WAS REMOVED. ANAYLIS OF THE CLOCK REVEALED THAT A DIFFERENCE WAS PRESENT IN THE TIME BETWEEN THE CLOCKS TWO DATA BUS LINES. THE FAULT WAS TRACED TO AN INVERTER/BUFFER CHIP ON THE A3 CARD. (M) 2 L 7 2 4F RT A1NM 1999010100412 19990101 00412 EU 1999 1 1 VTZA98331 1 19981109 A 2435 23078009 START GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 484UE 899 FLT 6348 - IAD-GSO - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT GENERATOR FAILED. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RIGHT STARTER GENERATOR, OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010100413 19990101 00413 EU 1999 1 1 SIMA983302 1 19981126 A 3350 7225280572 INDICATOR SNIAS 350 AS350B 8680801 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 350SB AQ75817 2196 CLD - FLT 3427 - FLIGHT ATTENDANTS EMERGENCY LIGHTS ARMED INDICATOR DOES NOT ILLUMINATE. REMOVED AND REPLACED FLIGHT AT TENDANT LIGHT CONTROL PANEL. OPERATIONAL CHECK GOOD. (M) 1 G 7 1 3U H9EU 1999010100414 19990101 00414 CE 1999 1 1 98ZZZM962 1 19980731 A 3010 26190361 GASKET LEAR 35 35A 5170602 CE CABIN LOOSE A P ROSA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 01 135DE 667 WHILE AT ALTITUDE, THE PILOTS TURNED ON THE WING AND HORIZONTAL STABILIZER ANTI-ICE SYSTEM, ONCE ENGAGED THE CREW IMMEDI ATELY SMELLED 'BURNING RUBBER' AND HEARD A SOUND OF RUSHING AIR IN THE CABIN. THE WING STAB HEAT SWITCH WAS IMMEDIATELY TURNED OFF. INVESTIGATION REVEALED AN OPEN GAP OF APPROXIMATELY .125 INCH BETWEEN FLANGES WHERE TWO SECTIONS MATE TOGE THER ON THE STEEL TRANSVERSE DUCT ASSY. THE FLANGE WAS PROPERLY SEATED, THE SYSTEM TESTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A10CE 1999010100415 19990101 00415 NM 1999 1 1 AALA981992 1 19981009 A 5512 SKIN BOEING 727 727223 1384074 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND RIGHT STAB UPPER SKIN HAS CORROSION, ABOVE REAR SPAR AROUND FASTENERS, TOP SURFACE JUST OUTBOARD UPPER SPAR CAP. REMVOED CORROSION AND INSTALLED DOUBLER PER SRM 51-10-1, 2024-T3 .032. (M) 2 L 7 3 4F A3WE 1999010100416 19990101 00416 NM 1999 1 1 AALA981991 1 19981009 A 5512 SKIN BOEING 727 727223 1384074 NM HORIZ STABILIZER CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - LEFT STABILIZER UPPER SKIN HAS CORROSION TOP SURFACE ABOVE REAR SPAR. INSTALLED DOUBLER PER SRM 51-10-1 2024T3 .0 32 AFTER CORROSION WAS REMOVED. (M) 2 L 7 3 4F A3WE 1999010100417 19990101 00417 NM 1999 1 1 AALA981987 1 19980923 A 5320 FLOOR PAN BOEING 727 727223 1384074 NM BS 1130-1134 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - DOUBLER BULGING AT RIGHT AFT LAVATORY FLOOR PAN AREA, INBOARD OF RIGHT INBOARD SEAT TRACK STATION 1130-1134. CUT OUT AREA THAT WAS BEYOND LIMITS WHEN CORROSION WAS REMOVED AT BS 1131-1135 RBL 25-28, INSTALLED DOUBLER AND FILLER PER S RM 51-40-2, ALODINED AND PRIMED. (M) 2 L 7 3 4F A3WE 1999010100418 19990101 00418 NM 1999 1 1 AALA981985 1 19980923 A 5320 FLOOR PAN BOEING 727 727223 1384074 NM BS 1130-1173 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - FOUND CORROSION ON RIGHT LAVATORY FLOOR PAN UNDERNEATH HAT CHANNEL, STATION 1130-1173, RBL 21-RBL 28. CUT OUT ARE A BEYOND LIMITS AT BS 1167-1174 RBL 23-27. INSTALLED DOUBLER AND FILLER PER SRM 51-40-2 FIG 1. REMOVED OTHER CORROSION WITHIN LIMITS, ALODINED, PRIMED AND PAINTED INSTALLED HAT CHANNEL. (M) 2 L 7 3 4F A3WE 1999010100419 19990101 00419 NM 1999 1 1 AALA981984 1 19980929 A 5320 FLOOR PAN BOEING 727 727223 1384074 NM BS 1146-1173 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 885AA 21524 TUL - EXTENSIVE CORROSION ON FLOOR PAN AT STATION 1146-1173, LBL 16 - RBL 16. CORROSION BEYOND LIMITS PER SRM 51-10-1. INSTALLED NEW FLOOR PAN AT STATION 1146-1173 PER SRM 53-10-1. (M) 2 L 7 3 4F A3WE 1999010100420 19990101 00420 NM 1999 1 1 AALA982115 1 19981116 A 5320 FRAME BOEING 727 727223 1384074 NM PAX DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 886AA 21525 TUL - FORWARD GALLEY DOOR ENTRY, DOOR CUTOUT FRAME CORRODED 3 INCHES ABOVE FLOOR LINE STATION 377, ALL SIDES OF FRAME. C UT OUT DAMAGED AREA, INSTALLED TYPICAL FORMED SECTION. REPAIR PER SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999010100421 19990101 00421 NM 1999 1 1 AALA981737 1 19980925 A 5320 SHEAR TIE BOEING 727 727227 1384078 NM BS 20 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - RIB SHEAR TIE DAMAGED. REMOVED AND REPLACED SHEAR TIE. (M) 2 L 7 3 4F A3WE 1999010100422 19990101 00422 NM 1999 1 1 AALA981741 1 19980925 A 5753 TRACK BOEING 727 727227 1384078 NM TE FLAP WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - NR 2 FLAP TRACK HAS ALL ROLLER BEARING CONTACT SURFACES WORN, PLASMA COATING IS MISSING OR RUSTY. REMOVED AND REP LACED NR 8 FLAP TRACK WITH SERVICEABLE PART PER MM 27-51-31, PAGE 408. (M) 2 L 7 3 4F A3WE 1999010100423 19990101 00423 NM 1999 1 1 ASAA9810119 1 19981118 A 5260 CABLE BOEING 737 737298C 1384490 NM AIRSTAIR DOOR BINDING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 745AS 20794 ANC - PRIOR TO FLIGHT 51, THE AFT AIRSTAIR EXTERIOR HANDLE WOULD NOT OPERATE, WAS FOUND TO BE STIFF AND BINDING. REPLAC ED TELEFLEX CABLE AND DOOR HANDLE OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999010100424 19990101 00424 NM 1999 1 1 ASAA9810120 1 19981119 A 3350 86210144 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE SMOKE BARRIER EMERGENCY LIGHT WOULD NOT TEST. REPLACED BATTERY AND LIGHT OPERATED N ORMALLY. (M) 2 L 7 2 4F A16WE 1999010100425 19990101 00425 NM 1999 1 1 AALA981843 1 19981021 A 5754 MOUNT BOEING 727 727227 1384078 NM NR 3 SLAT CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 720AA 20613 TUL - NR 3 SLAT ACT INBOARD AND OUTBOARD MOUNTS CORRODED. REMOVED AND INSTALLED INBOARD AND OUTBOARD MOUNTS, REPAIRED D AMAGED AREA INSIDE TANK PER ESO 11697, DATED 10-2-98 AND 9-18-98. (M) 2 L 7 3 4F A3WE 1999010100426 19990101 00426 WP 1999 1 1 AALA982082 1 19981113 A 5230 BEAM DOUG DC9 DC982 3022082 WP CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 440AA 49549 TUL - FOUND CORROSION AFT END OF UPPER AND LOWER LEGS WENT OUT OF MM LIMITS. INSTALLED DOUBLER PER AARD 53-10-00-3. (M ) 2 L 7 2 4F A6WE 1999010100427 19990101 00427 NM 1999 1 1 AALA982061 1 19981104 A 3220 CASTING BOEING 727 727223 1384074 NM NLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 880AA 21519 TUL - NOSE LANDING GEAR DRAG BRACE CASTING HAS CORROSION IN BORE AND ON FACE. REPLACED DRAG BRACE CASTING WITH NEW PART . (M) 2 L 7 3 4F A3WE 1999010100428 19990101 00428 WP 1999 1 1 ASAA9880204 1 19981008 A 3350 014597101 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 957AS 49126 SEA - PRIOR TO DEPARTURE OF FLIGHT 342, CREW REPORTED THE OVERHEAD EMERGENCY LIGHT IN THE FORWARD ENTRY AND THE EMEGENCY LIGHT IN THE FLIGHT COMPARTMENT WERE INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. ( M) 2 L 7 2 4F A6WE 1999010100429 19990101 00429 EU 1999 1 1 SIMA983172 1 19981113 A 5330 SKIN AEROSP ATR72 ATR72212 EU BS 31-33 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 536AT 536 ABI - TWO DENTS AT LEFT FUSELAGE BETWEEN FRAMES 31 AND 33 JUST ABOVE AND BELOW STRINGER 12. CUT OUT DAMAGED AREA AND PE RFORMED EDDY CURRENT INSPECTION, NO INDICATION OF CRACKS. FABRICATED AND INSTALLED EXTERNAL DOUBLER AND A FILLER PIECE .050 THICK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999010100430 19990101 00430 EU 1999 1 1 SIMA983174 1 19981113 A 5347 S5367800123802 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AFT OUTBOARD SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK. A IRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999010100431 19990101 00431 EU 1999 1 1 SIMA983211 1 19981117 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 212 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 218AE 340B218 FUSELAGE SKIN AT LOWER EDGE OF RIGHT COCKPIT WINDOW OPENING IS CORRODED. REMOVED CORROSION AND RESTORED PROTECTIVE TREA TMENT. FABRICATED AND INSTALLED STEPPED DOUBLER .032 THICK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999010100432 19990101 00432 NM 1999 1 1 EISA98252 1 19981119 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM PAX DOOR INOPERATIVE A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 313NE 13525 19702 POST FLIGHT, FOUND EMERGENCY EXIT LIGHT OVER L-1 DOOR DIM. GENERATED BY MAINTENANCE REPORT. REMOVED AND REPLACED L-1 D OOR EMERGENCY LIGHT ASSY. OPS CHECK GOOD PER MM 33-50. (M) 2 L 7 3 4F A3WE 1999010100433 19990101 00433 EU 1999 1 1 DKAA98019 1 19981022 A 3230 A24239107 UPLOCK AMD FALC20 FALCON 2720302 EU RT MLG WW MALFUNCTIONED A DKAA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 GL 23 227R 165 227 GEAR DOORS WILL NOT RETRACT. REPLACED RIGHT GEAR UPLOCK (15G2). OPERATIONAL CHECKS GOOD ON RETRACTION CHECKS. PERFORM ED SIMULATED EMERGENCY PULLED 'D' RINGS, GEAR OPERATED NORMAL IAW AMD MM 32-30. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A7EU 1999010100434 19990101 00434 EU 1999 1 1 98ZZZM963 1 19981030 A 2435 8060300 STARTER BRAERO DH125 HS125700A 4230170 EU NR 3 ENGINE FAILED A AJCA A H E UNSCHED LANDING DEACTIVATE SYST/CIRCUITS ENGINE SHUTDOWN J E WARNING INDICATION VIBRATION/BUFFET NR NOT REPORTED 1 EA 25 67PW NA0303 SEVERE VIBRATION NOTED AND ISOLATED TO THE NR 3 GENERATOR. CREW SELECTED GENERATOR OFF, REDUCED NUMBER 3 ENGINE TO IDLE , GENERATOR CONTINUED TO VIBRATE, SHUTDOWN NR 3 ENGINE AS A PRECAUTION, VIBRATION CEASED. AIRCRAFT THEN DIVERTED TO AN ALTERNATE AIRPORT. (M) 2 L 7 2 4F A3EU 1999010100435 19990101 00435 NM 1999 1 1 98ZZZM964 1 19981106 A 5210 507945148 PAX DOOR BOEING 727 727214 138407R NM CABIN JAMMED A C8GA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 15 227JL 43827 20875 FLT 310 - KLAX-KBSM - AFTER TAKEOFF FROM KLAX, AIRCRAFT WOULD NOT PRESSURIZE. AIRCRAFT RETURNED TO KLAX AND LANDED WITH OUT FURTHER INCIDENT. UPON RETURN TO GATE, NOTED L1 ENTRY DOOR JAMMED, PREVENTING ADEQUATE DOOR SEAL. FREED L1 ENTRY D OOR. PERFORMED DOOR LUBE AND RIG CHECK. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999010100436 19990101 00436 EU 1999 1 1 USAAF98089 1 19981104 A 3230 18878000300 CABLE FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 866US 11310 BYH - FLT 7899 - AFTER TAKEOFF FROM BYH, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE 'UP' POSITION IN EITHER THE NORMA L OR OVERRIDE MODULE. FLIGHT RETURNED TO BYH WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR HANDLE TE LEFLEX CABLE. (M) 2 L 7 2 4F RT 1999010100437 19990101 00437 EU 1999 1 1 USAAF98088 1 19981030 A 2740 A47006401 SWITCH FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 865US 11308 PIT - FLT 667 - AFTER TAKEOFF FROM PIT, STAB TRIM 1 AND 2 FAULT MESSAGE ILLUMINATED. FLIGHT RETURNED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 TRIM SWITCH. (M) 2 L 7 2 4F RT 1999010100438 19990101 00438 NM 1999 1 1 USAA980563 1 19981118 A 5313 143N3110379 STRINGER BOEING 757 757225 1384959 NM BS 643 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 43908 22201 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1.25 INCH CRACK STATION 643 STRINGER 16L. INSTALLED STRINGER EXTENSIO N PIECE PER SRM 53-00-03. (M) 2 L 7 2 4F RT A2NM 1999010100439 19990101 00439 NM 1999 1 1 USAA980588 1 19981121 A 5347 146T52174 SEAT TRACK BOEING 767 767201 1385125 NM BS 1310 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 645US 45689 23897 CLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 1 INCH AREA OF CORROSION BS 1310, RBBL 88.5 SEAT TRACK INST. S EAT TRACK REPLACED PER EA 62977. (M) 2 L 7 2 4F RT A1NM 1999010100440 19990101 00440 NM 1999 1 1 USAA980592 1 19981118 A 5414 311N504652 SKIN BOEING 757 757225 1384959 NM RT PYLON CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 43908 22201 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK RIGHT ENGINE PYLON RIGHT SIDE CUTOUT FOR PANEL 443 BR S KIN. INSTALL EXTERNAL DOUBLER PER EA 62939. (M) 2 L 7 2 4F RT A2NM 1999010100441 19990101 00441 NM 1999 1 1 USAA980591 1 19981118 A 5320 143N51406 WEB BOEING 757 757225 1384959 NM BS 598 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 43908 22201 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 598 RBBL 3 STABILIZATION INSTALLATION WEB. FABRICATED AND INSTALLED NEW WEB PER SRM 51-10-02, AND FASTENER SUBSTITUTION PER SRM 51-40-03. (M) 2 L 7 2 4F RT A2NM 1999010100442 19990101 00442 NM 1999 1 1 USAA980590 1 19981118 A 5315 141N51131 FLOORBEAM BOEING 757 757225 1384959 NM BS 377 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 605AU 43098 22201 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH BY 37 INCHES OF CORROSION ON TOP OF FLOORBEAM AT STAT ION 377 LBL 25 TO RBL 12. FABRICATED 'T' CAP REPAIR AND SPLICE ANGLES PER SRM 53-00-51 PAGE 209-213E. (M) 2 L 7 2 4F RT A2NM 1999010100443 19990101 00443 NM 1999 1 1 USAA980613 1 19981105 A 5313 STRINGER BOEING 757 757225 1384959 NM BS 1348 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 44869 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND 1 INCH BY 4 INCH AREA OF CORROSION BS 1348 STRINGER 27R. REPAIR ANGLE I NSTALLED PER EA 62711. (M) 2 L 7 2 4F RT A2NM 1999010100444 19990101 00444 NM 1999 1 1 USAA980612 1 19981105 A 5320 SUPPORT BOEING 757 757225 1384959 NM BS 652 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 604AU 44869 22199 CLT - DURING C-1 CHECK VISUAL INSPECTION, FOUND CORROSION STATION 652 FLOOR SUPPORT STRUCTURE CORROSION TASK NR C53-123- 02. INSTALLED DOUBLER PER TR 53-10-01A AND 53-30-53. (M) 2 L 7 2 4F RT A2NM 1999010100445 19990101 00445 NM 1999 1 1 USAA980597 1 19981118 A 5315 FLOORBEAM BOEING 737 737401 1384701 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 29856 23881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH AREA OF CORROSION AT STATION 947.5 LBL 14 TO RBL 33 F LOORBEAM. CORROSION TASK NR C53-107-02. SPLICED IN NEW 'T' CAP PER TR 53-60-02. (M) 2 L 7 2 4F RT A16WE 1999010100446 19990101 00446 NM 1999 1 1 USAA980584 1 19981118 A 5312 6516300511 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 29856 23881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CRACKS STATION 178 BULKHEAD APPROX 2 INCHES AT LOWER LEFT RADAR ANTE NNA MOUNT WEB ASSY LBL 5.7 WL 200. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M) 2 L 7 2 4F RT A16WE 1999010100447 19990101 00447 NM 1999 1 1 USAA980585 1 19981118 A 5312 6516300512 BULKHEAD BOEING 737 737401 1384701 NM BS 178 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 29856 23881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND TWO CRACKS STATION 178 BULKHEAD APPROX 2 INCHES AT RBBL 5.7 WL 200 WEB A SSY. INSTALLED DOUBLER PER SRM 53-10-08 FIG 209. (M) 2 L 7 2 4F RT A16WE 1999010100448 19990101 00448 NM 1999 1 1 USAA980586 1 19981118 A 5320 654681180 BEAM BOEING 737 737401 1384701 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 29856 23881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH BY .5 INCH BY 5 INCH AREA OF CORROSION BS 986.5, WL 208, LBBL 14 .5 - LBBL 19.5 BEAM INST, CORROSION TASK NR C53-107-02. INSTALLED REPAIR 'T' CAP PER SRM 53-60-51 BOEING 737-400. (M) 2 L 7 2 4F RT A16WE 1999010100449 19990101 00449 NM 1999 1 1 USAA980587 1 19981118 A 5311 FRAME BOEING 737 737401 1384701 NM BS 1040 CHAFED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 412US 23881 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CHAFED AT FRAME BS 1040. INSTALLED DOUBLER PER TR 53-80-02. (M) 2 L 7 2 4F RT A16WE 1999010100450 19990101 00450 NE 1999 1 1 USAA129804 2 19981207 A 7314 378200 FUEL PUMP BOEING 727 727227 1384078 NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE FAILED A USAA C ABORTED TAKEOFF X J ENGINE FLAMEOUT WARNING INDICATION TO TAKEOFF 1 EA 19 924TS 972 21041 655315 FLT 6170 - LGA-BOS - ON TAKEOFF AFTER 1.4 EPR CHECK, WHEN POWER APPLIED FOR TAKEOFF NR 1 ENGINE FLAMED OUT. REMOVED AND REPLACED NR 1 ENGINE DRIVEN FUEL PUMP PER MM 73-11-1. LEAK AND OPERATIONAL CHECKS OK. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999010100451 19990101 00451 NM 1999 1 1 USAASB98319 1 19981207 A 3350 1012623 LIGHT BOEING 737 7373B7 1384580 NM EMERGENCY EXIT INOP A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 533AU 24515 GSO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE OVERWING EXIT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE BATTERY CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100452 19990101 00452 NM 1999 1 1 98ZZZM965 1 19981207 A 3350 20121 BATTERY CHARGER BOEING 737 7373B7 1384580 NM EMERGENCY EXIT INOP A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 533AU 24515 GSO - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE OVERWING EXIT INOP. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AND THE BATTERY CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100453 19990101 00453 NM 1999 1 1 USAASB98318 1 19981201 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 390US 23312 GSO - MAINTENANCE FOUND A SECTION OF THE FORWARD EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND THE LEFT BULLNOSE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100454 19990101 00454 NM 1999 1 1 98ZZZM966 1 19981201 A 3350 20121 BATTERY CHARGER BOEING 737 7373B7 1384580 NM CABIN INOP A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 390US 23312 GSO - MAINTENANCE FOUND A SECTION OF THE FORWARD EMERGENCY LIGHTS INOP AT THE FORWARD ENTRY DOOR AND THE LEFT BULLNOSE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER AND THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100455 19990101 00455 NM 1999 1 1 USAA980566 1 19981109 A 5320 654581945 WEB BOEING 737 737201 1384454 NM BS 259 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 243US 43903 22445 CLT - DURING CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1.5 INCH CRACK BL 0 STATION 259 TOP OF NOSE W/W WEB. REM OVED AND REPLACED DAMAGED WEB PER SRM 51-10-1 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010100456 19990101 00456 NM 1999 1 1 NOCA2598 1 19981119 A 4910 SCREEN BOEING 757 75723A 1384967 NM APU CONTAMINATED A NOCA O OTHER O OTHER CR CRUISE 1 EA 15 757NA 24567 IN FLIGHT APU START SCHEDULED BY MAINTENANCE. APU IN FLIGHT START UNSUCCESSFUL. ON GROUND INSPECTION OF APU INLET PLEN UM FOUND DEBRIS ON INLET SCREEN. DEBRIS REMOVED. INSPECTION OF CHIP DETECTORS OK. LEAK CHECK OK. APU OPS CHECK OK. ( M) 2 L 7 2 4F RT A2NM 1999010100457 19990101 00457 NM 1999 1 1 P2EA98244 1 19981108 A 2612 FIRE LOOP BOEING 737 737297 1384480 NM MLG WW MALFUNCTIONED A P2EA O OTHER N FALSE WARNING DE DESCENT 1 CE 05 5WM 22629 MSP - FLT 707 - NO EMERGENCY DECLARED LANDING UNEVENTFUL. GOT WHEEL WELL FIRE LGHT WHEN GEAR LOWERED FOR LANDING. BELL DID NOT COME ON NOR DID MASTER FIRE LIGHT. FLIGHT ATTENDANT CONFIRMED NO SMOKE OR FIRE VISIBLE OUTSIDE OF A/C OR IN WH EEL WELL THROUGH VIEWPORT. PORT FLIGHT WALKAROUND SHOWS NO VISIBLE DAMAGE. LIGHT WENT OUT WHEN ENGINES WERE SHUT DOWN. RAN BOTH ENGINES WITH APU RUNNING, BOTH BLEEDS AND AIR CONDITIONING PACKS ON. COULD NOT GET FIRE LIGHT TO COME ON. A LSO, INSPECTED FIRE LOOP IN WHEEL WELL, ALL LOOK AND OPS CHECK OK. (M) 2 L 7 2 4F A16WE 1999010100458 19990101 00458 NM 1999 1 1 TSAA9879582 1 19981119 A 7930 69726881 SWITCH BOEING 737 7372T4 1384492 NM NR 1 ENGINE MALFUNCTIONED A TSAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 13 807AL 23443 FLT 297 - OGG-HNL - ON CLIMB-OUT, NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REDUCED NR 1 ENGINE THROTT LE TO IDLE AND LIGHT STAYED ON. NR 1 ENGINE WAS SHUT DOWN IAW THE QRH. EMERGENCY DECLARED AND UNEVENTFUL LANDING MADE AT HNL. INSPECTED OIL FILTER ON NR 1 ENGINE. NO CLOGGING FOUND. PERFORMED OPERATIONAL CHECK OF BYPASS SWITCH. SYSTEM CHECK OK. AS A PRECAUTION, REPLACED ENGINE OIL BYPASS SWITCH IAW MM 79-35-0. GROUND OPS CHECK AND LEAK CHECK OK. AIR CRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010100459 19990101 00459 EU 1999 1 1 RAIA981119 1 19981123 A 3230 AIR136070 HARNESS JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 566HK 41084 RED LIGHT IN GEAR HANDLE CAME ON DURING GEAR RETRACTION. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR STANDBY HARNESS. (M) 2 L 7 2 4T RT A41NM 1999010100460 19990101 00460 NE 1999 1 1 RAIA981116 2 19981120 A 7321 31059006 FUEL CONTROL JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 562HK 4289 41078 75055 FLT 7746 - DCA - LEFT ENGINE INDICATIONS ERRATIC IE, EGT, RPM, FUEL FLOW, TORQUE. MAINTENANCE REPLACED LEFT ENGINE FUEL CONTROL. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999010100461 19990101 00461 NE 1999 1 1 RAIA981117 2 19981122 A 7321 21188408 IEC JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114 01514 NE LT ENGINE FAILED A RAIA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CE 03 562HK 8041 41078 75055 FLT 7779 - DCA - LEFT ENGINE TORQUE INDICATION FLUCTUATING, ALONG WITH RPM, EGT AND FUEL FLOW. MAINTENANCE REPLACED LEF T ENGINE IEC. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999010100462 19990101 00462 EU 1999 1 1 RAIA981118 1 19981123 A 2910 1379305A155 LINE BAG JETSTM JETSTM3201 1500217 EU RT MLG FAILED A RAIA A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CE 03 972JX 972 FLT 4782 - FAT - LOSSED HYDRAULIC PRESSURE WHEN LANDING GEAR WAS SELECTED UP. HAD TO HAND PUMP GEAR DOWN. MAINTENANCE REPLACED RIGHT GEAR RADIUS ROD UP LINE. (M) 2 L 7 2 4T RT A56EU 1999010100463 19990101 00463 NM 1999 1 1 TSAA9833603 1 19981130 A 3350 86210066 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT ASSY BATTERY CONDITION INOP. REPLACED BATTERY. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010100464 19990101 00464 NM 1999 1 1 TSAA9833604 1 19981130 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 5 FLOOR LIGHT BATTERY PACK FOR RETIREMENT. REPLACED BATTERY, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F A16WE 1999010100465 19990101 00465 NM 1999 1 1 TSAA9833605 1 19981130 A 3350 8731002511 LIGHT BOEING 737 737230 NM EMERGENCY EXIT INOP A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED ENTRY SERVICE DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010100466 19990101 00466 NM 1999 1 1 USAASB98280 1 19981021 A 3222 654628813 TORQUE LINK BOEING 737 737401 1384701 NM NLG BROKEN A USAA O OTHER O OTHER LD LANDING 1 EA 19 405US 23885 PHL - FLT 165 - ON LANDING ROLL IN PHL, A VIBRATION DEVELOPED FROM THE NLG AND STEADILY INCREASED. NOSE WHEEL STEERING WAS LOST. AIRCRAFT STOPPED ON THE RUNWAY AND WAS UNABLE TO COMMUNICATE ON ANY RADIO, INTERPHONE OR PASSENGER ADDRESS. R ECEIVERS WERE OPERABLE. AIRCRAFT WAS TOWED TO THE GATE. NO BLOWN TIRES WERE REPORTED AND NO EMERGENCY WAS DECLARED. MA INTENANCE FOUND THE NOSE LANDING GEAR TORQUE LINKS HAD BROKEN. REPLACED SAME ALONG WITH NOSE LANDING GEAR. ALSO, REPLA CED AUDIO ACCESSORY UNIT (P/N 65-52804-229). OPERATIONAL CHECKS GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100467 19990101 00467 EU 1999 1 1 REXA98113 1 19981020 A 2932 IPT6110003000SG TRANSDUCER SAAB SF340 SF340A 7850100 EU NLG WW MALFUNCTIONED A REXA O OTHER J WARNING INDICATION DE DESCENT 1 SO 25 347AM 3544458 340A039 HYDRAULIC MAIN AND EMERGENCY PRESSURE DROPPED BELOW 200 PSI AND GOT CWP 'HYD' WARNING. COMPLIED WITH EMERGENCY CHECKLIS T. BLEW GEAR DOORS OPEN. REMOVED AND REPLACED PRESSURE SWITCH AND TRANSDUCER. (M) 2 L 7 2 4T RT A52EU 1999010100468 19990101 00468 NE 1999 1 1 SIMA983121 2 19981108 A 7200 ENGINE SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE LEFT MALFUNCTIONED A SIMA A E UNSCHED LANDING ENGINE SHUTDOWN K FLUID LOSS CR CRUISE 1 SW 21 301AE 340B301 785255 ALB - FLT 4812 - EN ROUTE TO JFK FROM YUL, THE LEFT ENGINE OIL PRESSURE STARTED DROPPING. WHEN IT GOT TO THE BOTTOM OF THE GREEN ARC, THEY SHUT DOWN THE ENGIEN AND DIVERTED TO ALB. ENGINE REQUIRED OVER FIVE QUARTS OF OIL. REMOVED AND REP LACED THE LEFT ENGINE. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999010100469 19990101 00469 WP 1999 1 1 AALA981924 1 19981021 A 3397 WIRE DOUG DC9 DC982 3022082 WP FUSELAGE FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 442AA 49468 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT IN TAIL COMPARTMENT INOPERATIVE. REPLACED GROUND WIRE FOR EMER GENCY EXIT LIGHT IN TAIL COMPARTMENT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999010100470 19990101 00470 EU 1999 1 1 98ZZZM967 1 19980808 A 7722 8974696 HARNESS BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A FYWA K NONE O OTHER IN INSP/MAINT 1 AL 05 242RH 903 RIGHT ENGINE BYPASSING FUEL WITH TTL ON, TROUBLESHOOTING DISCOVERED CHAFED AND BURNED SPOT IN THERMOCOUPLER HARNESS. RE MOVED AND REPLACED RIGHT ENGINE THERMOCOUPLER ASSY. PERFORMED GROUND RUN RIGHT ENGINE. NO DISCREPANCY NOTED. PERFORME D FUNCTIONAL FLIGHT CHECK, ALL SYSTEMS OPERATED WITHIN NORMAL PARAMETERS. (M) 2 L 7 2 4T RT A56EU 1999010100471 19990101 00471 WP 1999 1 1 AALA981996 1 19981022 A 3350 CONNECTOR DOUG DC9 DC982 3022082 WP ROW 17 DAMAGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446AA 49472 SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS FROM PASSENGER SEAT ROW 17 AFT INOPERATIVE. REPLACED EMERGENCY EXIT LGIHT CONNECTOR AT CONTROL MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999010100472 19990101 00472 WP 1999 1 1 AALA982001 1 19981027 A 3340 SWITCH DOUG DC9 DC982 3022082 WP TAIL CONE OUT OF ADJUST A AALA K NONE N FALSE WARNING IN INSP/MAINT 1 SW 07 73444 49470 ORD - FLT 485 - DURING GROUND OPERATIONS, TAIL CONE MISSING LIGHT ILLUMINATED ON OVERHEAD PANEL. MAINTENANCE FOUND SWIT CHES TO BE OUT OF ADJUSTMENT. ADJUSTED TAIL CONE SWITCHES PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999010100473 19990101 00473 1999 1 1 EISA98250 4 19981025 A 2565 1133169 SLIDE DOUG DC9 DC931 3022065 WP GALLEY DOOR LOW A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 975VJ 82 47146 GALLEY DOOR SLIDE PRESSURE BELOW LIMITS. GENERATED FROM MAINTENANCE REPORT. REPLACED GALLEY DOOR SLIDE PER MM 25-62-0. (M) 2 L 7 2 4F A6WE 1999010100474 19990101 00474 SO 1999 1 1 C2XA98IA432 1 19981023 A 3260 12043270501 RELAY BOX EMB 120 EMB120RT SO MLG INOPERATIVE A C2XA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 12703 120084 IAH - DURING CLIMB-OUT ON FLGHT 3764 - THE CREW REPORTED A LANDING GEAR WARNING. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR RELAY BOX, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999010100475 19990101 00475 NM 1999 1 1 ASAA9840090 1 19980829 A 5210 GUIDE ARM BOEING 737 737490 1384715 NM PASSENGER DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 794AS 28889 SEA - PRIOR TO FLT 446, THE L1 DOOR WAS FOUND TO BE DIFFICULT TO CLOSE. ADJUSTED UPPER GUIDE ARM AND DOOR OPERATED NORM ALLY. (M) 2 L 7 2 4F RT A16WE 1999010100476 19990101 00476 SO 1999 1 1 ASOA98101 1 19981116 A 5411 12003858001 FRAME EMB 120 EMB120RT SO LT/RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 286AS 120268 DURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD O F MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999010100477 19990101 00477 SO 1999 1 1 ASOA98102 1 19981116 A 5411 12003858001 FRAME EMB 120 EMB120RT SO LT/RT NACELLE CRACKED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 127AM 120103 DURING C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS INBOARD AND OUTBOARD O F MOUNT HOLES FOR LEFT AND RIGHT SIDE OF ENGINE FORWARD TORQUE MOUNT. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M) 2 L 7 2 4T RT A31SO 1999010100478 19990101 00478 SO 1999 1 1 ASOA98103 1 19981120 A 2435 23080013 START/GENERATOR EMB 120 EMB120RT SO RT ENGINE FAILED A ASOA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SO 11 126AM 120102 ON CLIMB-OUT DFW-TUL, RIGHT MAIN GENERATOR FAILED AND CREW NOTICED ELECTRICAL BURNING SMELL IN COCKPIT. CREW ELECTED TO RETURN TO DFW WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. DFW MAINTENANCE REMOVED AND REPLACED THE RIG HT MAIN GENERATOR AND GENERATOR CONTROL UNIT. GROUND CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE . (M) 2 L 7 2 4T RT A31SO 1999010100479 19990101 00479 EU 1999 1 1 DKAA98020 1 19981027 A 3244 266F432 TIRE GOODYEAR AMD FALC20 FALCOND 2720304 EU MLG FAILED A DKAA O OTHER D INFLIGHT SEPARATION TO TAKEOFF 1 GL 23 229R 20810124 229 NR 1 MAIN TIRE CAP SEPARATED ON TAKEOFF. REPLACED NR 1 MAIN WHEEL/TIRE ASSEMBLY IAW AMD MM 12-10. PRESSURE CHECKS GOOD . AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A7EU 1999010100480 19990101 00480 NM 1999 1 1 EISA98251 1 19981113 A 2613 65249203 DETECTOR BOEING 727 727223 1384074 NM NR 3 ENGINE INOPERATIVE A EISA O OTHER N FALSE WARNING CR CRUISE 1 SW 07 313NE M00208 19702 NR 3 ENGINE STRUT OVERHEAT LIGHT ON, ISOLATED TO BLEED. GENERATED FROM PILOT REPORT. REPLACED FIRE OVERHEAT DETECTOR A CCESSORY BOX IAW MM 20-10-17, OPS CHECK NORMAL MM 26-14-11. (M) 2 L 7 3 4F A3WE 1999010100481 19990101 00481 NE 1999 1 1 MASA98199 2 19981107 A 7250 GAS GENERATOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE FAILED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 SW 07 46YV UE46 114216 FLT 5499 - JAX-MCO - JUST AFTER TAKEOFF, THE LEFT ENGINE MADE A LOUD BAND AND SEEMED TO LOSE POWER. SPARKS WERE SEEN CO MING FROM THE EXHAUST STACKS. CREW DECLARED AN EMERGENCY AND SHUTDOWN THE ENGINE. AIRCRAFT RETURNED TO FIELD WITHOUT F URTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GAS GENERATOR. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999010100482 19990101 00482 NM 1999 1 1 P2EA98246 1 19981108 A 5720 FITTING BOEING 737 737244 138448U NM WS 432 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - INTERNAL FITTING FOUND OUT OF LIMITS AT RT WING FRONT SPAR SECTION AS FSS 432. REPLACED RIGHT WING FRONT SPAR FIT TING AT FSS 432 SRM 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999010100483 19990101 00483 NM 1999 1 1 P2EA98242 1 19981006 A 5315 FLOORBEAM BOEING 737 737244 138448U NM BS 360 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - FLOORBEAM UPPER AND LOWER CHORD CORRODED AT BS 360, RBL 53. REPAIRED FLOORBEAM UPPER CHORD AT BS 360, BETWEEN RBL 47 INCH AND RBL 60 INCH PER SRM 53-10-9 FIG 7. REMOVED CORROSION AT LOWER CHORD AT BS 360, RBL 53 INCH AND FOUND WITHI N LIMITS PER SRM 51-10-6, SRM 53-10-01 FIG 1 AND SRM 51-10-2. (M) 2 L 7 2 4F A16WE 1999010100484 19990101 00484 NM 1999 1 1 P2EA98250 1 19981001 A 5320 65C356932 FITTING BOEING 737 737244 138448U NM BS 685 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - BS 685 RT FRAME FITTING CRACKED. REPLACED FUSELAGE FRAME FITTING AT BS 685 RT FROM WL 186 TO WL 255 PER BOEING FA X COO-SJO-98-0632RR DATED SEPT 16, 1998. (M) 2 L 7 2 4F A16WE 1999010100485 19990101 00485 NM 1999 1 1 P2EA98249 1 19981011 A 5754 656462194 SKIN BOEING 737 737244 138448U NM NR 5 SLAT DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - NR 5 SLAT DELAMINATED UPPER AND LOWER SKIN. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-573-98 DATED OCT 17, 1998. (M) 2 L 7 2 4F A16WE 1999010100486 19990101 00486 NM 1999 1 1 P2EA98248 1 19981011 A 5751 65464541 SKIN BOEING 737 737244 138448U NM AILERON DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC BN117 19708 SJO - LEFT AILERON DELAMINATED AND WITH HAIL DAMAGE, DEFECT SIZE VARIOUS. REPAIRED LEFT AILERON PER COOPESA EO COO-3-57 -565-98 DATED OCT 15, 1998. (M) 2 L 7 2 4F A16WE 1999010100487 19990101 00487 EU 1999 1 1 RAIA981105 1 19981103 A 3020 31998061 VALVE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 435AM 1173 889 FLT 7034 - STL - RIGHT ENGINE ANTI-ICE INOP. MAINTENANCE REPLACED ANTI-ICE VALVE. (M) 2 L 7 2 4T RT A56EU 1999010100488 19990101 00488 1999 1 1 RAIA981017 4 19981027 A 6122 89741016 GOVERNOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA E B ENGINE SHUTDOWN EMER. DESCENT J WARNING INDICATION CR CRUISE 1 CE 03 436AM 1459 891 FLT 7080 - STL - RIGHT ENGINE LOST OIL PRESSURE IN FLIGHT. RIGHT ENGINE WAS SHUT DOWN. MAINTENANCE TIGHTENED A LOOSE ' B' NUT AT THE PROP GOVERNOR, SERVICED WITH OIL. (M) 2 L 7 2 4T RT A56EU 1999010100489 19990101 00489 EU 1999 1 1 RAIA981109 1 19981107 A 6120 782490A51 PITCH CONTROL AEROSP ATR42 ATR42300 8680920 EU RT ENGINE FAILED A RAIA B EMER. DESCENT R J PARTIAL RPM/PWR LOSS WARNING INDICATION DE DESCENT 1 CE 03 421TE 9490 102 FLT 7154 - STL - RIGHT ENGINE TORQUE FLUCTUATING IN FLIGHT. MAINTENANCE REPLACED PITCH CONTROL UNIT ON RIGHT ENGINE. ( M) 2 H 7 2 4T RT A53EU 1999010100490 19990101 00490 1999 1 1 RAIA981107 4 19981105 A 3418 C771076 LIFT TRANSDUCER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 431AM 15374 881 FLT 7504 - STL - RIGHT STALL CAP ILLUMINATED AFTER TAKEOFF. MAINTENANCE REPLACED RIGHT LIFT TRANSDUCER. (M) 2 L 7 2 4T RT A56EU 1999010100491 19990101 00491 WP 1999 1 1 RAIA981110 2 19981109 A 7321 89778025 FUEL CONTROL BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 424AM 11501 865 66155 FLT 7426 - STL - RIGHT ENGINE TORQUE FLUCTUATING 3 PERCENT. MAINTENANCE REPLACED THE FUEL CONTROL ON RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999010100492 19990101 00492 1999 1 1 RAIA981111 3 19981111 A 6140 31056294 BETA SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 558HK 2257 41071 FLT 7409 - EVV - RED BETA LIGHT ILLUMINATED ON LEFT SIDE. MAINTENANCE REPLACED LEFT BETA SWITCH AND ADJUSTED FLIGHT IDL E FUEL FLOW. (M) 2 L 7 2 4T RT A41NM 1999010100493 19990101 00493 NM 1999 1 1 TWRA9855 1 19981117 A 3397 WIRE BOEING 747 747124 1384874 NM EMERGENCY EXIT BROKEN A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING 'A' SERVICE, FOUND MID LAV J AND H, EMERGENCY EVACS LIGHT INOPERATIVE. REPAIRED WIRING. OPERATIONAL CHECK NORMA L AS PER MM 33-50-00. (M) 2 L 7 4 4F A20WE 1999010100494 19990101 00494 NM 1999 1 1 TWRA9854 1 19981115 A 2612 FIRE LOOP BOEING 747 7472F6B 1384807 NM NR 1 ENGINE MALFUNCTIONED A TWRA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 EA 15 623FF 22382 DURING CRUISE NR 1 ENGINE 'B' LOOP INDICATED FIRE AND FAULT, NACELLE TEMP FLUX OFF SCALE HIGH AND LOW. NR 1 ENGINE SHUT DOWN, FIRE BOTTLE 'A' DISCHARGED. REPLACED FIRE BOTTLE 'A' PER MM 26-21-03 PAGE 401. CONFIRMED FALSE FIRE WARNING 'B' LOOP. DEFERRED PER 26-1-C. REPAIRED WIRING ON 'A' LOOP SYSTEM. OPERATIONAL CHECK NORMAL. AIRCRAFT RETURN TO SERVICE . (M) 2 L 7 4 4F A20WE 1999010100495 19990101 00495 EU 1999 1 1 SIMA983173 1 19981113 A 5320 S5367121729801 DRAIN AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 277AT 277 SAW - DURING CPCP1 INSPECTION, FOUND THE SERVICE DOOR DRAIN TRACK CORRODED. REMOVED AND REPLACED THE DRAIN TRACK. AIRC RAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999010100496 19990101 00496 EU 1999 1 1 SIMA983212 1 19981117 A 3350 OL3401BPE BULB SAAB SF340 340B 7860101 EU ROW 28LN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 272AE 340B272 IND - FLT 4335 - FORWARD CABIN, RIGHT EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. REMOVED AND REPLACED BULBS IN SIGN. OPE RATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999010100497 19990101 00497 EU 1999 1 1 RAIA981108 1 19981110 A 5230 MS161065 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU POD DOOR FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 561HK 41077 FLT 7796 - PIT - BAGGAGE POD LIGHT CAME ON DURING TAKEOFF. MAINTENANCE CLEANED MICROSWITCH FOR POD DOOR. (M) 2 L 7 2 4T RT A41NM 1999010100498 19990101 00498 1999 1 1 RAIA981115 4 19981118 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 556HK 8908 41073 FLT 7219 - STL - HEADING COMPARITOR CAME ON IN FLIGHT, 6-9 DEGREE SPLIT. MAINTENANCE REPLACED NR 1 AHRS COMPUTER. (M) 2 L 7 2 4T RT A41NM 1999010100499 19990101 00499 WP 1999 1 1 RAIA981114 2 19981116 A 7320 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 433AM 1951 885 66047R FLT 7096 - STL - ON CLIMB-OUT, RIGHT TORQUE DROPPED TO 60 PERCENT WITH AN EGT RISE. MAINTENANCE REPLACED RIGHT ENGINE F UEL BYPASS VALVE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999010100500 19990101 00500 NM 1999 1 1 USAASB98292 1 19981105 A 2910 BACH6R0334DUR LINE BOEING 737 737201 1384454 NM RT MLG WW CHAFED A USAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 263AU 22869 PIT - FLT 734 - EN ROUTE FROM MCI TO PHL, THE 'B' HYDRAULIC SYSTEM QUANTITY DECREASED AND THE LOW PRESSURE LIGHTS ILLUMI NATED AT 1.8 GALLONS. DEGREE OF LOSS WAS SUCH THAT CAPTAIN DECIDED A DIVERSION WAS NECESSARY. FLIGHT DIVERTED TO PIT A ND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE 'B' HYDRAULIC SYSTEM SUPPLY LINE CHAFFED. REMOVED AND REPLACED LINE ALONG WITH SUPPLY FILTERS AND RETURN FILTERS. SERVICED HYDRAULIC SYSTEM. OPERATION AL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999010100501 19990101 00501 NM 1999 1 1 USAASB98303 1 19981005 A 3350 20131ALP BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 408US 23878 IAH - MAINTENANCE FOUND THE AFT LEFT SERVICE DOOR EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PA CK. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100502 19990101 00502 NM 1999 1 1 USAASB98306 1 19981118 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 527AU 23862 ROC - DURING OVERNIGHT CHECK, MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN MID/AFT AISLE BULLNOSE AREA AND EXTERIOR AFT OVERWING AREA INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN M1136 POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100503 19990101 00503 NM 1999 1 1 USAASB98305 1 19981114 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 334US 23231 PHL - MAINTENANCE FOUND THE EMERGENCY LIGHTS AT ROWS 4ABC THROUGH 9ABC INOP. MAINTENANCE REMOVED AND REPLACED THE BATTE RY PACK IN OVERHEAD AT ROW 10ABC. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100504 19990101 00504 NM 1999 1 1 USAASB98304 1 19981113 A 3350 20131ALP BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 268AU 22880 PHL - MAINTENANCE FOUND THE AFT CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BA TTERY PACK. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999010100505 19990101 00505 WP 1999 1 1 ASAA9880205 1 19981009 A 3350 CONNECTOR DOUG DC9 DC983 3022083 WP CABIN LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 958AS 53024 ANC - PRIOR TO DEPARTURE OF FLIGHT 115, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. SECURED CONNECTOR IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999010100506 19990101 00506 EU 1999 1 1 USAA980593 1 19981113 A 5311 FRAME FOKKER F28 F28MK0100 4990807 EU BS 8305 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 895US 15933 11380 PIT - DURING Q1 CHECK, FOUND 1 INCH CRACK AT FORWARD CARGO CEILING STATION NR 8305 BL '0' LINE FRAME. LOCALLY MANUFACTU RED PART. REPLACED 15 INCH LONG SECTION WHICH HAD A 1 INCH CRACK IN IT PER SRM REF 53-21-10, 51-70-07, 51-30-01 AND 51- 10-02. (M) 2 L 7 2 4F RT 1999010100507 19990101 00507 EU 1999 1 1 USAA980594 1 19981113 A 5320 1718738 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3870-4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 895US 15933 11380 PIT - DURING Q1 CHECK, FOUND .25 INCH TEE RAIL CORRODED AROUND RIVETS IN RIVET ATTACHMENT ON TOP ON BEAM 1127L FROM STAT ION 3870 TO 4610. INSTALLED REPLACEMENT 'T' ANGLE (RAIL) 37 INCH LONG PER SRM 51-20-02. (M) 2 L 7 2 4F RT 1999010100508 19990101 00508 EU 1999 1 1 USAA980595 1 19981113 A 5330 SKIN FOKKER F28 F28MK0100 4990807 EU BS 6305/6805 DELAMINATED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 895US 15933 11380 PIT - DURING Q1 CHECK, FOUND DELAMINATION 2 INCH BY 3 INCH CAUSED BY CORROSION AT C1 ANTENNA HOLD BETWEEN STATION 6305 A ND 6805, STRINGERS 1 AND 74 ON SKIN. LOCALLY FABRICATED PARTS, CUT OUT DAMAGED AREA AND INSTALLED DOUBLER AND FILLER PE R EA 50865. (M) 2 L 7 2 4F RT 1999010100509 19990101 00509 WP 1999 1 1 USAA980596 1 19981113 A 5330 SKIN DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 800US 48499 48034 PIT - DURING C2 CHECK, FOUND .125 INCH CRACK EXTENDING FROM RIVET ON SKIN AT AT STATION 1437 BETWEEN LONGERON 2L AND 3L. INSTALLED DOUBLER PER EA 50958. (M) 2 L 7 2 4F A6WE 1999010100510 19990101 00510 1999 1 1 USAAD98204 4 19981113 A 2565 3753213575 HARNESS DOUG DC9 DC931 3022065 WP TAIL SLIDE STIFF A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925VJ 48145 PIT - DURING A FUNCTIONAL CHECK, THE TAIL CONE EMERGENCY EVACUATION SLIDE FAILED TO DEPLOY AUTOMATICALLY. MAINTENANCE R EPLACED THE TAIL CONE EMERGENCY EVACUATION SLIDE ASSEMBLY. INVESTIGATION IN PROGRESS TO DETERMINE REASON FOR NOT DEPLOY ING AUTOMATICALLY. THE EVACUATION SLIDE RELEASE HARNESS TOGGLES WERE FOUND TO BE TOO STIFF TO OPERATE. THE HARNESS ASS EMBLY WAS REPLACED. ENGINEERING RELEASED A CAMPAIGN DIRECTIVE TO REPLACE THE SLIDE RELEASE HARNESSES ON THE ENTIRE FLEE T. (M) 2 L 7 2 4F A6WE 1999010100511 19990101 00511 NM 1999 1 1 USAASB98310 1 19981123 A 3350 900835A BATTERY PACK BOEING 737 7372B7 1384560 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 279AU 22891 CLE - MAINTENANCE FOUND THE AFT AISLE EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPE RATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999010100512 19990101 00512 WP 1999 1 1 ORJA98301 1 19981127 A 3350 59306431 BATTERY DOUG DC9 DC983 3022083 WP EXIT DISCHARGED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 881RA 49941 RNO - FORWARD RT EMERGENCY EXIT LOWER LIGHT ASSY BATTERY PACK INOP. REPLACED BATTERIES AND FUSE SYSTEM. OPS CHECK NORM AL. (M) 2 L 7 2 4F RT A6WE 1999010100513 19990101 00513 NM 1999 1 1 USAASB98299 1 19981112 A 2450 91252ZC7C4001 RELAY BOEING 737 7373B7 1384580 NM E/E BAY FAILED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 376US 22955 CLT - FLT 272 - DURING CRUISE AT FL 330, THE NR 1 TRANSFORMER RECTIFIER UNIT CIRCUIT BREAKER TRIPPED SEVERAL TIMES AND W OULD NOT RESET. CAPTAIN DECIDED TO DIVERT TO CLT WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE R3 TRANSFER RELAY. GROUND RAN ENGINE. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010100515 19990101 00515 NM 1999 1 1 USAA119805 1 19981121 A 3350 081691 LIGHT GRIMES BOEING 727 727225 1384077 NM ROW 1 DEF INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS 20447 FLT 6080 - LGA-BOS - EPL LIGHT TRACK BROKEN AND WIRES BARE. CAPTAIN REPORTED PRIOR TO PUSHBACK PASSENGER HAD KICKED TRA CK LOOSE FROM FLOOR. WIRES WERE SHOWING. REPAIRED BROKEN WIRES. ALL LIGHTS WORK EXCEPT ONE. ISSUED MEL FOR INDIVIDUA L LIGHT INOP ALONG SIDE ROW 1 UNDER MEL SEQUENCE 33-17. REPLACED EPL LIGHT SOCKET 1 DEF. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999010100516 19990101 00516 NM 1999 1 1 USAA119801 1 19981101 A 3350 081691 LIGHT BRUCE BOEING 727 727225 1384077 NM ROW 19 MISSING A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 918TS 20445 FLT 6140 - LGA-BOS - ONE RED EMERGENCY PATH LIGHT MISSING AT 19D. REPLACED HOLDER, CAPSULE AND LAMP. (M) 2 L 7 3 4F A3WE 1999010100517 19990101 00517 EU 1999 1 1 VTZA98348 1 19981122 A 2910 137311D1451 LINE BAG JETSTM JETSTM3201 1500217 EU HYDRAULIC SYSTEM CHAFED A VTZA O OTHER K FLUID LOSS DE DESCENT 1 EA 27 482UE 897 FLT 6473 - JFK-IAD - DURING DESCENT, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LOST ALL HYDRAULI C PRESSURE AND CREW HAD TO PUMP GEAR DOWN. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSP ECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES THAT WERE CHAFED. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010100518 19990101 00518 EU 1999 1 1 98ZZZM968 1 19981122 A 2910 137311D1443 LINE BAG JETSTM JETSTM3201 1500217 EU HYDRAULIC SYSTEM CHAFED A VTZA O OTHER K FLUID LOSS DE DESCENT 1 EA 27 482UE 897 FLT 6473 - JFK-IAD - DURING DESCENT, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LOST ALL HYDRAULI C PRESSURE AND CREW HAD TO PUMP GEAR DOWN. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSP ECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES THAT WERE CHAFED. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010100519 19990101 00519 WP 1999 1 1 USAAD98209 1 19981122 A 3230 3920208515 DRAG LINK DOUG DC9 DC981 3022081 WP NLG OUT OF ADJUST A USAA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 EA 19 807US 48039 PIT-EWR - FLT 1642 - ON TAKEOFF, THERE WAS SEVERE NOSE WHEEL VIBRATION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED W ITHOUT INCIDENT. MAINTENANCE SHIMMED THE NOSE LANDING GEAR DRAG LINK ASSEMBLY TO REMOVE EXCESSIVE CLEARANCE AND REPLACE D BOTH NOSE WHEEL ASSEMBLIES. (M) 2 L 7 2 4F A6WE 1999010100520 19990101 00520 EA 1999 1 1 VTZA98264 1 19980820 A 2751 INDICATOR CNDAIR CL600 CL6002B19 EA COCKPIT MALFUNCTIONED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 627BR 7233 FLT 6710 - RDU-IAD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP WARNING FAI L MESSAGE ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND PERFORMED SYSTEM CHEC K, COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999010100521 19990101 00521 WP 1999 1 1 98ZZZM969 1 19980827 A 7732 585601 VIBRATION LIGHT LKHEED 1011 1011385115 5265015 WP LT/RT ENGINE MALFUNCTIONED A WRNA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 05 75AA 193U1201 NR 2 ENGINE INCREASE IN VIBRATION FROM .7 TO 3 UNITS ON BOTH CHANNELS. WARNING LIGHT ON. ENGINE SHUTDOWN. COMPLETE BO ROSCOPE CARRIED OUT, NO NEW DAMAGE FOUND. VIBRATION SURVEY CARRIED OUT, AND FAN TRIM BALANCE PERFORMED IAW 72-00-00 TES T 11 AND 16. (M) 2 L 7 3 4F A23WE 1999010100522 19990101 00522 WP 1999 1 1 98ZZZM970 1 19980828 A 7732 585601 VIBRATION LIGHT LKHEED 1011 1011385115 5265015 WP NR 2 ENGINE MALFUNCTIONED A WRNA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 SO 05 75AA 193U1201 NR 2 ENGINE INCREASE IN VIBRATION .8 TO 3.0 IN CRUISE, BOTH CHANNELS. THRUST LEVER RETARDED TO IDLE, VIBRATION .4. LEV ER ADVANCED, VIBRATION INCREASES TO 3.0 UNITS. REPLACED ENGINE VIBRATION CONDITIONING UNIT. SWAPPED NR 1 AND NR 2 INDI CATORS IAW MM 77-31-00. (M) 2 L 7 3 4F A23WE 1999010100523 19990101 00523 NM 1999 1 1 AALA982009 1 19981204 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STATION 520 BELTFRAME DENTED STRINGER 23R - STRINGER 25R. REMOVED DAMAGE TREATED AND PRIMED AIND INSTALLED FRAME REPAIR PER SRM 53-10-4 FIG 1 DOUBLER 7075-T6 .050. (M) 2 L 7 3 4F A3WE 1999010100524 19990101 00524 NM 1999 1 1 AALA982010 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - BELLFRAME STATION 990 HAS SPOT INBOARD OF STRINGER 8L. REPAIRED FRAME PER SRM 53-10-4 FIG 2. (M) 2 L 7 3 4F A3WE 1999010100525 19990101 00525 NE 1999 1 1 SIMA983022 2 19981029 A 7510 8TD50N DUCT AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE RT ENGINE CRACKED A SIMA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 21 420AT 420 127133 DFW - FLT 3597 - AT 200 FT, THE NR 2 ENGINE TORQUE BEGAN TO FLUCTUATE AND THE HIGH ITT LIGHT ILLUMINATED. CREW REDUCED POWER TO GET THE ITT DOWN, BUT THE ITT SPIKED AGAIN WITH HIGH ITT LIGHT. CREW SHUT DOWN THE ENGINE, DECLARED AN EMERGEN CY AND LANDED SAFELY. REMOVED AND REPLACED CRACKED DISCHARGE DUCT. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999010100526 19990101 00526 NM 1999 1 1 SWAA983142 1 19981223 A 3230 CONTROL CABLE BOEING 737 7373H4 1384600 NM LANDING GEAR OUT OF ADJ A SWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 343SW 24151 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT TO UP POSITION, APPEARED TO BE SOLENOID. AIRCRAFT RETURNED TO MDW AND MAD E AN UNEVENTFUL LANDING. ADJUSTED GROUND SHIFT CABLE PER M/M, OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999010100527 19990101 00527 NM 1999 1 1 SWAA983143 1 19981224 A 2540 LAVATORY BOEING 737 7377H4 NM CABIN CLOGGED A SWAA A UNSCHED LANDING O OTHER CR CRUISE 1 SW 07 716SW 27850 ABOUT 40 TO 50 MINUTES INTO FLIGHT, F/A NOTED AFT LAV WAS NOT FLUSHING AND BOWL WAS FILLING UP. FWD LAVATORY WAS ALREAD Y DEFERRED AND ON MEL. AIRCRAFT DIVERTED TO PHX AND MADE AN UNEVENTFUL LANDING. FOUND AFT LAV CLOGGED. REMOVED DEBRIS AND SERVICED PER BOEING M/M. FWD LAV STILL ON MEL. 2 L 7 2 4F RT A16WE 1999010100528 19990101 00528 NM 1999 1 1 SWAA983144 1 19981223 A 2910 313532H0264 LINE BOEING 737 7373H4 1384600 NM B-HYD SYST CHAFED A SWAA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 662SW 23255 LOST ALL B-HYDRAULIC FLUID IN FLIGHT. AIRCRAFT DIVERTED TO PHX. FOUND ELE B PUMP HYDRAULIC LINE CHAFED THROUGH. REMOV ED AND REPLACED LINE, B SYSTEM ENG AND ELE PUMPS CASE DRAIN FILTERS PER M/M. 2 L 7 2 4F RT A16WE 1999010100529 19990101 00529 NM 1999 1 1 SWAA983145 1 19981222 A 5610 5893543110 WINDOW BOEING 737 7373H4 1384600 NM RT COCKPIT CRACKED A SWAA K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 356SW 25251 F/O NR 1 WINDOW ARCED AND CRACKED IN FLT (ALTITUDE APPROX 31,000). REMOVED AND REPLACED F/O NR 1 WINDOW PER MM, NO LEAK S NOTICED AT THIS TIME. AIRCRAFT OK FOR SERVICE. AIRCRAFT RECERTIFIED TO CAT IIIA STATUS, DO TO REMOVAL AND REPLACEMEN T OF MCP TO FACILITATE OTHER MAINTENANCE. 2 L 7 2 4F RT A16WE 1999010100530 19990101 00530 NM 1999 1 1 SWAA983146 1 19981222 A 3350 LIGHT BOEING 737 7372H4 138448C NM CABIN LOOSE A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 096SW 23055 DURING SCHEDULED SC CHECK, FOUND R1 UPPER EMERGENCY EXIT LIGHT INOP. FOUND LIGHT ASSY LOOSE IN BRACKET. ADJUSTED LIGHT ASSY AND BRACKET PER M/M, OPS CK NORMAL. 2 L 7 2 4F A16WE 1999010100531 19990101 00531 NM 1999 1 1 SWAA983147 1 19981221 A 3350 BATTERY BOEING 737 7373H4 1384600 NM GALLEY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 354SW 25219 DURING SCHEDULED SC CHECK, FOUND AFT GALLEY O/B EMERGENCY FLASHLIGHT NOT SHOWING CHARGE. REMOVED AND REPLACED BATTERY P ACK PER M/M, OPS CK NORMAL. 2 L 7 2 4F RT A16WE 1999010100532 19990101 00532 NM 1999 1 1 SWAA983148 1 19981227 A 3350 BULB BOEING 737 7373H4 1384600 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 637SW 27710 DURING SCHEDULED C1 CHECK, FOUND FLOOR PROXIMITY LIGHTS INOP AT SEAT ROW 12ABC. RELAMPED AND OP CHECKED PER M/M. 2 L 7 2 4F RT A16WE 1999010100533 19990101 00533 NM 1999 1 1 SWAA983150 1 19981226 A 3350 20121 BASE BOEING 737 7373A4 1384585 NM CABIN INOP A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 676SW 23288 DURING 1/2 D-CHECK, FOUND AFT EMERGENCY FLOOR TRACK LIGHTING BATTERY PACK BASE INOP. REMOVED AND REPLACED BATTERY PACK BASE PER MM. PREFLIGHT, FOUND EMERGENCY FLOOR TRACK HAS TWO LIGHTS INOP. RELAMPED AND OPS CKS GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999010100534 19990101 00534 NM 1999 1 1 SWAA983151 1 19981227 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM COCKPIT DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 080SW 22675 DURING SCHEDULED SC CHECK, FOUND COCKPIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER M/M. PREFLIGHT, F OUND EMERGENCY FLOOR TRACK HAS TWO LIGHTS INOP. RELAMPED AND OPS CKS GOOD PER M/M. 2 L 7 2 4F A16WE 1999010100535 19990101 00535 1999 1 1 SWAA983152 4 19981225 A 2565 1061323433 SLIDE BOEING 737 7373H4 1384600 NM R2 DOOR LOW PRESS A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 633SW 27936 DURING SCHEDULED C2 CHECK, FOUND R2 DOOR SLIDE PRESSURE LOW. REPLACED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010100536 19990101 00536 NM 1999 1 1 SWAA983153 1 19981226 A 3240 2601042 BRAKE BOEING 737 7372H4 138448C NM MLG WORN A SWAA K NONE O OTHER TX TAXI/GRND HDL 1 SW 07 056SW 21721 MUCH HIGHER BRAKE PEDAL PRESSURE IS REQUIRED TO GET NORMAL BRAKING. ON BOTH LT/RT PEDALS AND BOTH PILOT SIDES, NO ANTI- SKID LIGHTS ILLUMINATED, BRAKE AND ACCUMULATOR PRESSURES NORMAL. VERY HIGH PEDAL PRESSURE FOR BRAKES TO GRAB. PERFORME D TAXI CHECK WITH ANTI SKID SYSTEM ON AND OFF. BRAKES OPERATED NORMALLY WITH ANTI SKID OFF. BRAKES REQUIRED EXCESSIVE PRESSURE AND PULSED AND GRABBED WITH ANTI SKID ON. BRAKE ASSYS VISUALLY CHECKED OK PER MM. REMOVED AND REPLACED NR 1 A ND NR 2 MAIN GEAR BRAKES AND BRAKE SHUTTLE VALVES. OPS AND LK CKD GOOD PER M/M. PERFORMED SYSTEM CHECK OF ANTI SKID SY STEM. CKD GOOD PER MM. 2 L 7 2 4F A16WE 1999010100537 19990101 00537 NM 1999 1 1 SWAA983154 1 19981225 A 5330 SKIN BOEING 737 7377H4 NM BS 348 DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 718SW 27852 BELT LOADER CONTACTED FUSELAGE APPROXIMATELY BS 348L WL 265 SHEETMETAL REPAIR ACCOMPLISHED PER SWA RA 1-753-1964 AND SRM UNDER ATTACHED SAM FORM 326. 2 L 7 2 4F RT A16WE 1999010100538 19990101 00538 NM 1999 1 1 SWAA983155 1 19981225 A 3350 AD20131A BATTERY BOEING 737 7373H4 1384600 NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 615SW 27698 EMERGENCY LIGHT BATTERY PACKS REQUIRED REPLACEMENT DUE TO EXTENDED USE. REMOVED AND REPLACED BATTERY PACKS PER M/M (7 E A), OPS CKS OK. 2 L 7 2 4F RT A16WE 1999010100539 19990101 00539 NM 1999 1 1 SWAA983156 1 19981225 A 5330 SKIN BOEING 737 7372H4 138448C NM FUSELAGE CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 087SW 22903 DURING PREFLIGHT, FOUND FUSELAGE CRACKED ON RT SIDE LOWER, APPROX 36 FWD OF OUTFLOW VALVE. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100540 19990101 00540 NM 1999 1 1 SWAA983157 1 19981222 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 753 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 303SW 22943 DURING SCHEDULED SP VISIT, FOUND FUSELAGE SKIN CRACKED AT BS 753 ABOVE S20L. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999010100541 19990101 00541 NM 1999 1 1 SWAA983158 1 19981222 A 5330 SKIN BOEING 737 7372H4 138448C NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 089SW 22904 DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR UPPER HINGE CUTOUT ON FUSELAGE IS CRACKED (0.400 LONG). REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1999010100542 19990101 00542 NM 1999 1 1 SWAA983159 1 19981222 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 470/500 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CORRODED AROUND NUTPLATE HOLES AT BS 470 AND BS 500A +14. REPAIRED PER BO EING SRM. 2 L 7 2 4F A16WE 1999010100543 19990101 00543 NM 1999 1 1 SWAA983160 1 19981222 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 307 GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN GOUGED AT BS 307, WL 242, LBL 71. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100544 19990101 00544 NE 1999 1 1 SWAA983161 2 19981228 A 7200 ENGINE BOEING 737 7373G7 1384595 NM GE CFM56 CFM563B1 13802 NE NR 2 MALFUNCTIONED A SWAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 07 690SW 23783 ON CLIMBOUT PASSING 20,000 FT, A/C YAWED RIGHT AND GRINDING NOISE WAS FELT THROUGH CONTROLS. NR 2 N1 + N2 FLUCTUATED AP PROX 5 PERCENT WITH GRINDING NOISE. POWER AT CLIMB (APPROX 90 PERCENT) EGT + FUEL FLOW NORMAL. AFT F/A REPORTED BANGIN G NOISE IN CABIN. NR 2 ENG PARAMETERS NORMAL ON APPROACH. FOUND EVIDENCE OF SHINGLED BLADES. INSP'D INLET, EXHAUS T VBV, VSV, OIL FILTER AND CHIP DETECTORS; NO FAULTS NOTED. RAN ENG, PARAMETERS WITHIN M/M LIMITS. ENG OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999010100545 19990101 00545 NM 1999 1 1 SWAA983162 1 19981228 A 5312 BULKHEAD WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 218, RBL 8.7 UNDER STRAPS. FABRICATED AND INSTALLED R EPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100546 19990101 00546 NM 1999 1 1 SWAA983163 1 19981228 A 5312 BULKHEAAD WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT WL 218, LBL 7.7 UNDER STRAPS AND STIFFENERS. FABRICATED AND INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100547 19990101 00547 NM 1999 1 1 SWAA983164 1 19981228 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT WL 234, LBL 9. FABRICATED AND INSTALLED REPAIR DOUBLER PER B OEING SRM. 2 L 7 2 4F A16WE 1999010100548 19990101 00548 NM 1999 1 1 SWAA983165 1 19981228 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 294 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 294, LBL 11. REMOVED AND REPLACED UPPER CHORD FLOORBEAM PER B OEING SRM. 2 L 7 2 4F A16WE 1999010100549 19990101 00549 NM 1999 1 1 SWAA983166 1 19981228 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 344 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 344, LBL 27.5, 41.5, 46, AND 54. FABRICATED AND INSTALLED NEW UPPER CHORD AND SPLICE ANGLES PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100550 19990101 00550 NM 1999 1 1 SWAA983167 1 19981228 A 5320 STRAP BOEING 737 7372H4 138448C NM BS 1028 CRACK A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND CRACK IN CIRCUMFERENTIAL TEAR STRAP AT BS 1028, RBL 30 AND 34. FABRICATED AND INSTALLED STRAP PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100551 19990101 00551 NM 1999 1 1 SWAA983168 1 19981228 A 5320 CHANNEL BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND STRINGER CHANNEL CRACKED AT BS 360, S14L. INSTALLED NEW CHANNEL PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100552 19990101 00552 NM 1999 1 1 SWAA983169 1 19981228 A 5320 WEB BOEING 737 7372H4 138448C NM BS 1002 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 64SW 22062 DURING SCHEDULED D-CHECK, FOUND CREASE BEAM WEB BODY CORRODED AT BS 1002, WL 208, RBL 49. INSTALLED NEW WEB PER BOEING SRM. 2 L 7 2 4F A16WE 1999010100553 19990101 00553 NM 1999 1 1 SWAA983170 1 19981228 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM CABIN DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED A1 CHECK, FOUND RT AFT SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY P ACK PER BOEING M/M. 2 L 7 2 4F A16WE 1999010100554 19990101 00554 NM 1999 1 1 SWAA983171 1 19981226 A 5330 SKIN BOEING 737 7372H4 138448C NM GALLEY DOORWAY GOUGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 73SW 22673 DURING SCHEDULED SC CHECK, FOUND A DEEP GOUGE ON FUSELAGE SKIN AFT OF AFT GALLEY DOOR LOWER LT. REPAIRED PER SWA RA 1-2 53-1965. 2 L 7 2 4F A16WE 1999010100555 19990101 00555 NM 1999 1 1 SWAA983172 1 19981226 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 351SW 24572 DURING SCHEDULED C2 CHECK, FOUND A 1.25 INCH CRACK IN FUSELAGE SKIN AT BS 727E, AT S24L. INSTALLED REPAIR DOUBLER PER B OEING SRM. 2 L 7 2 4F RT A16WE 1999010100556 19990101 00556 EU 1999 1 1 SIMA982943 1 19981021 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 307-339 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 254AE 340B254 ABI - RIGHT LOWER ICE GUARD FS 307 TO 339 AND SL 1622 TO 1623 CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED FILLER, PACKER AND DOUBLER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999010100557 19990101 00557 EA 1999 1 1 COMA9860382 1 19981206 A 5230 601R3505025 ANGLE CNDAIR CL600 CL6002B19 EA CARGO DOOR CRACKED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 956CA 7105 APU EXHAUST HEAT SHIELD CRACKED. REPLACED HEAT SHIELD. 2 L 7 2 4F RT A21EA 1999010100558 19990101 00558 EA 1999 1 1 COMA9860388 1 19981213 A 4950 32022321 CHECK VALVE CNDAIR CL600 CL6002B19 EA APU COMPT FAILED A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 986CA 3786 7174 APU AIR SUPPORT CHECK VALVE MISSING SPRING. REPLACED VALVE. 2 L 7 2 4F RT A21EA 1999010800001 19990108 00001 NM 1999 1 8 SWAA983058 1 19981203 A 2450 6972627 RELAY BOEING 737 7373Y0 1384671 NM P6 PANEL BURNT A SWAA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 SW 07 665WN 23497 ELECTRICAL ODOR NOTED FROM BEHIND P6 PANEL. INSPECTED AND FOUND R18 RELAY BURNED AND PLUG ARCED. REPLACED RELAY, PLUG AND C/B PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010800003 19990108 00003 NM 1999 1 8 98UAL900586 1 19981205 A 3350 5822 BATTERY PACK BOEING 747 747222B 1384904 NM PWA JT9 JT9D7R4G2 52054 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 151UA 23736 EMERGENCY FLOOR LIGHT REMAINED DIM AT RIGHT FORWARD SECTION OF C ZONE WITH EMERGENCY SWITCH IN THE ARM POSITION. *S/D* R EPLACED BATTERY PACK. 2 L 7 4 4F 4 F RT A20WE E3NE 1999010800004 19990108 00004 NE 1999 1 8 DLL19982575 2 19981206 A 7230 RB211524B4I BLADE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B4 54555 NE NR 2 ENGINE LACK OF LUBE A DALA E ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION DE DESCENT 1 SO 27 765DA 56483 014733 193H1206 014733 NR 2 ENGINE HAD HIGH FAN VIBS BOTH A AND B CHANNELS, SHOWED APPROX 2.7 UNITS. FAN VIBS INCREASED WHEN THROTTLES RETARTE D TO IDLE. SHUT DOWN NUMBER TWO ENGINE PER POM. LUBED BLADES, PERFORMED VIB RUN, WITHIN M/M LIMITS. 2 L 7 3 4F 4 F A23WE E12EU 1999010800005 19990108 00005 NM 1999 1 8 DHL9872045D 1 19981104 A 5260 STEP BOEING 727 727228 NM AFT AIRSTIRS CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 720DH 19544 AT D CHECK, AFT AIR STAIRS 4TH STEP FROM THE BOTTOM SUPPORT ANGLE A TOP OF RISER IS CORRODED. REMOVED AND REPLACED SKIN ON RISER AND SUPPORT ANGLE, 29 BY 10 PER SRM 51-30-2, N/R 4623. 2 L 7 3 4F A3WE 1999010800006 19990108 00006 WP 1999 1 8 ASAA9880231 1 19981106 A 5240 SKIN DOUG DC9 DC982 3022082 WP SERVICE DOOR DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 932AS 49233 LCQ - DURING 15K CHECK, FUSELAGE SKIN AT AFT LAVATORY SERVICE DOOR CUT OUT WAS FOUND CHAFED THROUGH. REPAIRED IAW ASA E A 5330-01351. (M) 2 L 7 2 4F A6WE 1999010800007 19990108 00007 WP 1999 1 8 VJ9800666 1 19981213 A 5712 99193315 RIB DOUG DC9 DC932 3022066 WP WS 543 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 910VJ 47277 SCHEDULED INSPECTION, LEFT WING LEADING EDGE RIB IS CRACKED AT STA 543 (NR 5 SLAT). REMOVED LEFT WING LEADING EDGE CRAC KED RIB, DRILLED, DEBURRED, TREATED, PRIME AND INSTALLED NEW RIB IAW DC9 SRM 51-10-4, 51-10-3, AND 51-30-3. 2 L 7 2 4F A6WE 1999010800008 19990108 00008 WP 1999 1 8 VJ9800667 1 19981213 A 5230 WEB DOUG DC9 DC932 3022066 WP C1 DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 910VJ 47277 SCHEDULED INSPECTION, FOUND A CRACK IN THE FORWARD CARGO DOOR. FABRICATED AND INSTALLED NEW REPAIRS IAW DC9 SRM 52-01 F IG 2 AND 51-10-3. 2 L 7 2 4F A6WE 1999010800010 19990108 00010 NE 1999 1 8 ARWA981213 2 19981221 A 7320 FUEL CONTROL LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB211524B02 54555 NE NR 3 ENGINE OUT OF ADJUST A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 19 306GB 1138 NR 3 ENGINE SLOW TO SPOOL, ABOVE 1.3 EPR. DURING TAKEOFF ROLL IN DTW ABORTED TAKEOFF. AFTER FURTHER RUN-UP ON THE TAXI WAY, ENGINE OPERATED NORMALLY. ADJUSTED FUEL CONTROL IAW M/M 73-21-00. 2 L 7 3 4F 4 F RT A23WE E12EU 1999010800014 19990108 00014 CE 1999 1 8 99ZZZX4 1 19981118 A 3010 1153801145 DEICER BEECH 99 99 1154002 CE HORIZONTAL STAB CONTAMINATED A TIMA O OTHER O OTHER NR NOT REPORTED 1 NM 07 24BH U67 PILOT REPORTED TO MAINTENANCE ICE REMAINING ON TAIL AFTER LANDING. (SPECIFICALLY, BOTH HORIZONTAL SURFACE DEICERS.) OP ERATIONAL CHECK OF BOOTS BROKE ICE FORM SURFACE, HOWEVER, A CLOSER INSPECTION OF SURFACE DEICERS REVEALED MINOR HOLES IN LEADING EDGES. FURTHERMORE, WHEN SUPPLY PRESSURE LINES WERE REMOVED, WATER WAS FOUND IN LINES TO THE BOOTS. BOOTS WER E REPLACED AND AIRCRAFT LINES CLEARED OF WATER USING DRY SHOP AIR AND ISOPROPHYL ALCOHOL. 1 L 7 2 3T A14CE 1999010800022 19990108 00022 NE 1999 1 8 99ZZZX12 2 19981203 A 7261 FILTER LEAR 25 25D 5170514 CE GE CJ610 CJ6106 30006 NE RT ENGINE CONTAMINATED A KKFA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 23 95CK 6304 25248 251307 WHILE EN ROUTE, FLIGHT CREW NOTICED RT OIL PRESSURE INCREASE FOLLOWED BY RPM FLUCTUATION. CREW DIVERTED TO MOR. MAINTE NANCE FOUND OIL SERVICED TO PROPER LEVEL, HOWEVER, THE OIL FILTER WAS CONTAMINATED. ENGINE WAS REMOVED AND REPLACED. 2 L 7 2 4J 4 J A10CE 1E16 1999010800050 19990108 00050 SW 1999 1 8 99ZZZX42 1 19981126 A 5510 206023119110 SUPPORT 407023800101 BELL 407 407 SW HORIZ STABILIZER CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 537AL 53230 DURING DAILY INSPECTION, FOUND SLAT SUPPORT P/N 206-023-119-110 (LT SIDE, 2ND FROM INBD) CRACKED. REMOVED AND REPLACED CRACKED SUPPORT. 1 G 7 1 3U O H2SW 1999010800056 19990108 00056 SW 1999 1 8 99ZZZX48 1 19981206 A 6510 406040340101 DISC PACK BELL 407 407 SW T/R DRIVE DAMAGED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 487AL RNFS 53204 DURING 25-HOUR INSPECTION, FOUND GAP BETWEEN THE NR 1 DISC (MOST FORWARD) AND NR 2 DISC BEYOND .015 INCH. (THE NR 1 DIS C IS THE ONE WITH THE PART NUMBERS SHOWING). 1 G 7 1 3U O H2SW 1999010800058 19990108 00058 WP 1999 1 8 TWAA9820301 1 19981229 A 3320 26447 TRANSFORMER DOUG DC9 DC982 3022082 WP CABIN BURNED A TWAA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 CE 05 908TW 49169 WHILE PARKED AT A GATE, SOME SMOKE APPEARED IN THE COCKPIT AND CABIN. CREW REPORTED SEEING AN ELECTRICAL FLASH/FIRE COM ING FROM THE ELECTRICAL COMPT TO THE LEFT OF COCKPIT DOOR. CREW ELECTED TO HAVE PAX DEPLANE THROUGH THE JETWAY. FOUND CABIN LIGHT CONTROL TRANSFORMER WITH HEAT DAMAGE, AND WIRING IN THE SURROUNDING AREA WAS DAMAGED. REPLACED TRANSFORMER AND DAMAGED WIRING. CHECK-C 2-16-98 STL. 2 L 7 2 4F A6WE 1999010800059 19990108 00059 NM 1999 1 8 TWAA9820302 1 19981230 A 3397 WIRE BOEING 767 7673Q8 NM ROW 30-41 LOOSE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 635TW 28207 FLOOR EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 30 THROUGH 41. RECONNECTED WIRING AT SEAT ROW 41. CHECK-C 10-7-98 LAX. 2 L 7 2 4F RT A1NM 1999010800060 19990108 00060 NM 1999 1 8 TWAA9820303 1 19981230 A 3350 900835A BATTERY PACK BOEING 727 727231 1384079 NM CABIN DISCHARGED A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 54352 21984 FOUND LOWER AFT OVERWING EMERGENCY EXIT LIGHT INOP DURING TEST. REPLACED BATTERY PACK, MFG PART NBR 9008-3-5A, AND BULB , PART NBR 81. CHECK-C 3-19-98 MCI. 2 L 7 3 4F A3WE 1999010800061 19990108 00061 WP 1999 1 8 TWAA9820304 1 19981230 A 3350 58222 POWER SUPPLY DOUG DC9 DC983 3022083 WP ROW 12-21 WORN A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 9406W 53126 FOUND FLOOR EGRESS LIGHTS INOPERATIVE FROM CABIN ROWS 12 THROUGH 21. REPLACED POWER SUPPLY. CHECK-C 1-15-98 STL. 2 L 7 2 4F RT A6WE 1999010800062 19990108 00062 WP 1999 1 8 TWAA9820305 1 19981231 A 5320 JAMB DOUG DC9 DC931 3022065 WP SERVICE DOOR CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 983Z 47411 DURING CHECK-C, MAINT FOUND FWD SERVICE DOOR JAMB WITH A 1.5 INCH CRACK IN LOWER AFT CORNER FROM A NUT PLATE AREA. REPA IRED PER SRM 53-05, FIG 112. 2 L 7 2 4F A6WE 1999010800063 19990108 00063 NM 1999 1 8 SPAA9800009 1 19981231 A 5320 65499172 MOUNT BOEING 737 7372T4 1384492 NM BS 767-787 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-208-01, ANTENNA MOUNT BETWEEN BS 767 AND 787 WAS FOUND CORRODED BEYOND SRM LIMITS . THE ANTENNA DOUBLER WAS REPLACED WITH A NEW PART PER SRM 51-30-2, FIG 1. 2 L 7 2 4F A16WE 1999010800064 19990108 00064 NM 1999 1 8 SPAA9800010 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 736-758 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-208-01, AFT CARGO PIT FLOOR BEAM, BS 736A TO 758, LBL 14 WAS FOUND CORRODED BEYON D SRM LIMITS AT FLOORING ATTACHMENT HOLES. DAMAGE AREAS WERE REPAIRED PER SRM 53-10-5. 2 L 7 2 4F A16WE 1999010800065 19990108 00065 NM 1999 1 8 SPAA9800011 1 19981231 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 259.5-390 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, STRINGERS 24L AND 25L WERE FOUND CORRODED BEYOND SRM LIMITS AT VARIOUS LO CATIONS FROM BS 259.5 TO BS 390. STRINGER SECTIONS WERE REPLACED WITH NEW PARTS PER SRM 51-10-1. 2 L 7 2 4F A16WE 1999010800066 19990108 00066 NM 1999 1 8 SPAA9800012 1 19981231 A 5311 FRAME BOEING 737 7372T4 1384492 NM BS 747 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-208-01, BS 747 FRAME WAS FOUND WITH CORROSION BEYOND SRM LIMITS BETWEEN S27R AND S28R. DAMAGE WAS REPAIRED PER SRM 53-10-4, FIG. 7. 2 L 7 2 4F A16WE 1999010800067 19990108 00067 NM 1999 1 8 SPAA9800013 1 19981231 A 5311 FRAME BOEING 737 7372T4 1384492 NM BS 727 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-208-01, SHEAR TIE AT BS 727B FRAME BETWEEN S27R AND S28R WAS FOUND CORRODED BEYON D SRM LIMITS. THE DAMAGED PIECE WAS REPLACED, REPAIR ACCOMPLISHED PER SRM 53-10-4, FIG. 8. 2 L 7 2 4F A16WE 1999010800068 19990108 00068 NM 1999 1 8 SPAA9800014 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 328 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-01, CABIN FLOORBEAM AT BS 328, RBL 38, WAS FOUND CORRODED BEYOND SRM LIMITS. DAMAGE WAS REPAIRED PER SRM 53-10-9, FIG 5. 2 L 7 2 4F A16WE 1999010800069 19990108 00069 NM 1999 1 8 SPAA9800015 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 277 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, CABIN FLOORBEAM AT BS 277, LBL 10 TO LBL 29, WAS FOUND CORRODED BEYOND SR M LIMITS. DAMAGE WAS REPAIRED PER SRM 53-10-9, FIG 6. 2 L 7 2 4F A16WE 1999010800070 19990108 00070 NM 1999 1 8 SPAA9800016 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 312 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, CABIN FLOORBEAM AT BS 312, LBL 10 TO RBL 9, WAS FOUND CORRODED BEYOND SRM LIMITS. DAMAGE WAS REPAIRED PER SRM 53-10-9, FIG 6. 2 L 7 2 4F A16WE 1999010800071 19990108 00071 NM 1999 1 8 SPAA9800017 1 19981231 A 5347 FLOOR TRACK BOEING 737 7372T4 1384492 NM BS 335 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, CABIN FLOOR TRACK AT BS 335, RBL 22, WAS FOUND CORRODED BEYOND SRM LIMITS . DAMAGED PART WAS REPLACED PER SRM 53-10-5, FIG 2. 2 L 7 2 4F A16WE 1999010800072 19990108 00072 NM 1999 1 8 SPAA9800018 1 19981231 A 5320 FITTING BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-208-01, STRINGER END FITTING AT BS 1016, S21R, WAS FOUND CORRODED BEYOND SRM LIMI TS. THE DAMAGED PART WAS REPLACED PER SRM 51-30-2. 2 L 7 2 4F A16WE 1999010800073 19990108 00073 NM 1999 1 8 SPAA9800019 1 19981231 A 5320 CHORD BOEING 737 7372T4 1384492 NM L2 DOORWAY CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-01, THE INNER CHORD THAT RUNS FORE AND AFT OF THE L2 DOOR ENTRY WAY WAS FOUND TO HAVE CORROSION BEYOND SRM LIMITS AT THE POINT OF THE FORWARD DOOR FRAME. DAMAGED AREA WAS REPAIRED PER SRM 51-40-3. 2 L 7 2 4F A16WE 1999010800074 19990108 00074 NM 1999 1 8 SPAA9800020 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 294.5 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, CABIN FLOORBEAM AT BS 294.5 AT FORWARD GALLEY TRACK WAS FOUND TO HAVE COR ROSION BEYOND SRM LIMITS. DAMAGE WAS REPAIRED PER SRM 53-10-9, FIG. 5 AND SRM 53-10-5, FIG 2. 2 L 7 2 4F A16WE 1999010800075 19990108 00075 NM 1999 1 8 SPAA9800021 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 957 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, FLOORBEAM STIFFENER AT BS 957, RBL 17 TO RBL 45, WAS FOUND TO HAVE CORROS ION BEYOND SRM LIMITS. THE DAMAGED PIECE WAS REPLACED AND INSTALLED PER SRM 51-10-1 AND 51-20-1. 2 L 7 2 4F A16WE 1999010800076 19990108 00076 NM 1999 1 8 SPAA9800022 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 986.5 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, FLOORBEAM AT BS 986.5, LBL 38.75, WAS FOUND TO HAVE CORROSION BEYOND SRM LIMITS AT THE FORWARD CHORD AND UPPER CAP. DAMAGE WAS REPAIRED PER SRM 53-10-9, FIG 2. 2 L 7 2 4F A16WE 1999010800077 19990108 00077 NM 1999 1 8 SPAA9800023 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 1006 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, FLOORBEAM AT BS 1006, LBL 4 TO LBL 14, WAS FOUND CORRODED BEYOND SRM LIMI TS. DAMAGE WAS REPAIRED PER SRM 53-10-9, FIG 2. 2 L 7 2 4F A16WE 1999010800078 19990108 00078 NM 1999 1 8 SPAA9800024 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 1016 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, FLOORBEAM ANGLE AT BS 1016, P/N- 65-46812-185, WAS FOUND CORRODED BEYOND SRM LIMITS. THE PART WAS REPLACED PER SRM 51-30-0. 2 L 7 2 4F A16WE 1999010800079 19990108 00079 1999 1 8 MALA976274 2 19981228 A 7200 ENGINE BAC 146 AVRO146RJ85A 1500097 EU NR 2 MALFUNCTIONED A MALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 15 515XJ E2333 NR 2 ENG N1 WOULD NOT GO ABOVE 60 PERCENT ON TAKEOFF ROLL. AIRCRAFT RETURNED TO DTW. MAINTENANCE PERFORMED BLEED BAND CHECK SEVERAL TIMES AND MAX POWER RUNUP TEST. OPS CHECKS GOOD. 2 H 7 4 4F RT A49EU 1999010800080 19990108 00080 EU 1999 1 8 MALA976275 1 19981226 A 5220 SAFETY WIRE SAAB SF340 340B 7860101 EU EMERGENCY EXIT BROKEN A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 445XJ 445 CREW REPORTED THE SAFETY WIRE ON EMERGENCY ROW 10 EXIT HANDLE WAS BROKEN. MAINTENANCE INSTALLED BREAKAWAY SAFETY WIRE T O EXIT LATCH COVER. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999010800081 19990108 00081 EU 1999 1 8 MALA976276 1 19981228 A 2611 OA30903870 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO COMPT MALFUNCTIONED A MALA O OTHER N F FALSE WARNING FLT CONT AFFECTED DE DESCENT 1 GL 15 433XJ 433 ABOUT FOUR MILES FROM LANDING IN ROCKFORD, RECEIVED A CARGO FIRE WARNING. DISCHARGED THE NR 1 FIRE EXTINGUISHER. WARNI NG LIGHT EXTINGUISHED. MAINTENANCE REPLACED FWD CARGO SMOKE DETECTOR. OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999010800082 19990108 00082 WP 1999 1 8 9811079987 1 19981229 A 3222 SCHRADER VALVE DOUG DC9 DC932 3022066 WP NLG STRUT FAILED A NWAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 01 987US 47458 GROUND SHIFT FAILURE OCCURRED AFTER TAKEOFF FROM DTW. AIRCRAFT WOULD NOT PRESSURIZE, ANTI-ICE WAS INOPERATIVE AND SLATS WOULD NOT RETRACT. CABIN ALTITUDE REACHED 15,000 FEET AND, OXYGEN MASKS WERE DEPLOYED THROUGHOUT CABIN. FLIGHT WAS D IVERTED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NOSE LANDING GEAR STRUT FLAT. REPLACED SCHRADER VALVE AN D SERVICED NOSE STRUT TO PROPER LEVELS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F A6WE 1999010800083 19990108 00083 NM 1999 1 8 98FDEA00771 1 19981231 A 2782 651781823 ACTUATOR BOEING 727 727277 138408S NM NR 1 LE SLAT MALFUNCTIONED A FDEA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 SO 25 246FE 22068 WITH FLAPS RETRACT AS A/C ACCEL THRU 270 KIAS, AMBER LEAD EDGE LIGHT ILLUM ON 2ND OFFICER AUXILIARY PNL AND A/C ROLL CON TROL WAS AFFECTED. ANTI ICE WAS ON. BELOW 250 KIAS ALL IND WERE NORM, FLAP EXTENSION AND LAND, ALL APPROPRIATE CK LIST WERE COMPLETE. *S/D* REMOVED AND REPLACED LEFT NR 1 LEAD EDGE SLAT ACTUATOR PER MM 27-81-32 OPER CK GOOD. 2 L 7 3 4F RT A3WE 1999010800084 19990108 00084 NM 1999 1 8 MWEA981215 1 19981228 A 5510 9918401 SKIN DOUG MD88 MD88 3023688 NM RT HORIZ STAB DAMAGED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT HORIZONTAL STABILIZER STA XE 155 HAS A BLEND OUT BEYOND SRM LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLERS. 2 L 7 2 4F RT A6WE 1999010800085 19990108 00085 WP 1999 1 8 MWEA981216 1 19981229 A 2560 5917689103 SLIDE COVER DOUG DC9 DC914 3022034 WP GALLEY DOOR FELL OFF A MWEA K NONE O OTHER TX TAXI/GRND HDL 1 GL 31 400ME 45727 GALLEY DOOR EVACUATION SLIDE COVER FELL OFF AT GATE. MAINTENANCE REINSTALLED GALLEY DOOR EVACUATION SLIDE COVER. 2 L 7 2 4F A6WE 1999010800086 19990108 00086 NE 1999 1 8 99ZZZX50 2 19980912 A 7200 ENGINE LEAR 23 23LEAR 5170102 CE GE CJ610 CJ6104 30006 NE RIGHT MALFUNCTIONED A KKFA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION NR NOT REPORTED 1 GL 23 49CK 7402 23009 251T171 MKE - AFTER DEPARTING, FLIGHT CREW NOTICED ABNORMAL RT ENGINE INDICATION AND LOSS OF POWER. A PRECAUTIONARY ENGINE SHUT DOWN WAS MADE FOLLOWED BY AN UNEVENTFUL LANDING. POST-FLIGHT EXAMINATION REVEALED NO VISIBLE FOD OR OTHER DAMAGE. TES T RUN OF ENGINE WOULD NOT EXCEED 87 PERCENT RPM. ENGINE WAS REPLACED, TEST RUN WAS NORMAL. 1 L 7 2 4J 4 J A5CE 1E16 1999010800087 19990108 00087 NE 1999 1 8 99ZZZX51 2 19980812 A 7210 GEARBOX CESSNA 500 550 2076604 CE PWA JT15 JT15D1 52060 NE RT ENGINE FAILED A EHHA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 17 725RH 26 5500006 RIGHT ENGINE SHUT DOWN IN CRUISE FLIGHT AT 24,000 FEET. PRECAUTIONARY LANDING. POSSIBLE ENGINE GEARBOX PROBLEM STILL U NDER INVESTIGATION. FAILURE OF LOCK WASHER ON UPPER TOWER SHAFT DUPLEX BEARING. OVERHAUL OCCURRED 2,236 HOURS AGO. 1 L 7 2 4F 4 F A22CE E1NE 1999010800136 19990108 00136 NM 1999 1 8 SWAA983173 1 19981229 A 5610 5717623121 WINDOW BOEING 737 7373G7 1384595 NM LT COCKPIT CRACKED A SWAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 690SW 23783 DURING CRUISE 45 MIN INTO FLIGHT, L2 WINDOW HEAT BEGAN ARCING AND OUTER PANE CRACKED, INNER PANE REMAINED INTACT. AIRCR AFT RETURNED TO TPA AND MADE AN UNEVENTFUL LANDING. REMOVED AND REPLACED CAPT SLIDING WINDOW PER M/M. 2 L 7 2 4F RT A16WE 1999010800137 19990108 00137 NM 1999 1 8 SWAA983174 1 19981229 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 853 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 853. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800138 19990108 00138 NM 1999 1 8 SWAA983175 1 19981229 A 5320 WEB BOEING 737 7372H4 138448C NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND BS 178 WEB CRACKED AT WL 234. INSTALLED REPAIR DOUBLER PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800139 19990108 00139 NM 1999 1 8 SWAA983176 1 19981231 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, ABOVE S14L. INSTALLED REPAIR DOUBLERS PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800140 19990108 00140 NM 1999 1 8 SWAA983177 1 19981231 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 997 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 997, BELOW S13L. INSTALLED REPAIR DOUBLERS PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800141 19990108 00141 NM 1999 1 8 SWAA983178 1 19981231 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 900-917 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CORRODED AT BS 900 TO 917 AT S26L. INSTALLED REPAIR DOUBLERS PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800142 19990108 00142 NM 1999 1 8 SWAA983179 1 19981231 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 267 DENTED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN DENTED AT BS 267, BELOW S24R. INSTALLED REPAIR DOUBLERS PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800143 19990108 00143 NM 1999 1 8 SWAA983180 1 19981231 A 5330 SKIN BOEING 737 7372H4 138448C NM BS 1018 CREASED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CREASED AT BS 1018, 2 ABOVE S16R. INSTALLED REPAIR DOUBLER PER BOEING SRM . 2 L 7 2 4F A16WE 1999010800144 19990108 00144 NM 1999 1 8 SWAA983181 1 19981231 A 5315 FLOORBEAM BOEING 737 7372H4 138448C NM BS 727-947 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FLOORBEAM CORROSION AT BS 727 TO 947, RBL 3, WL 159. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800145 19990108 00145 NM 1999 1 8 SWAA983182 1 19981231 A 5313 STRINGER BOEING 737 7372H4 138448C NM BS 913-925 CORRODED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 913 TO 925, S26R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800146 19990108 00146 NM 1999 1 8 SWAA983183 1 19981231 A 5311 FRAME BOEING 737 7372H4 138448C NM BS 360 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 064SW 22062 DURING SCHEDULED D CHECK, FOUND FUSE FRAME CRACKED AT BS 360, BETWEEN S14 AND 13R. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800147 19990108 00147 NM 1999 1 8 SWAA983184 1 19981230 A 5330 SKIN BOEING 737 7373Y0 1384671 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED SC CHECK, FOUND 2 FUSE SKIN CRACKS BETWEEN BS 727D AND E AT S22R, 1.5 LONG AND 3 APART. REPAIRED PER B OEING SRM. 2 L 7 2 4F RT A16WE 1999010800148 19990108 00148 NM 1999 1 8 SWAA983185 1 19981230 A 5330 SKIN BOEING 737 7373Y0 1384671 NM BS 747 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 699SW 23826 DURING SCHEDULED SC CHECK, FOUND A FUSE SKIN CRACK AT BS 747, S21R, 2.25 LONG. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999010800149 19990108 00149 NM 1999 1 8 SWAA983186 1 19981230 A 5330 SKIN BOEING 737 7372T4 1384492 NM PAX DOORWAY CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 722WN 22698 DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR 1 INCH CRACK AT UPPER HINGE CUTOUT. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1999010800150 19990108 00150 NM 1999 1 8 SWAA983188 1 19981228 A 3350 1000679 BATTERY BOEING 737 7372H4 138448C NM SERVICE DOORWAY DISCHARGED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 102SW 23108 DURING SCHEDULED A1 CHECK, FOUND RT AFT SERVICE DOOR OVERHEAD EMERG EXIT LIGHT INOP. REPLACED BATTERY PACK PER BOEING M /M. 2 L 7 2 4F A16WE 1999010800151 19990108 00151 NM 1999 1 8 SWAA983189 1 19981230 A 3350 CONNECTOR BOEING 737 7373H4 1384600 NM CABIN LOOSE A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 316SW 23338 DURING SCHEDULED C2 CHECK, FOUND RT EMERG EXIT LIGHT INOP. REINSTALLED CANNON PLUG AND OP CHECKED PER BOEING M/M. 2 L 7 2 4F RT A16WE 1999010800152 19990108 00152 NM 1999 1 8 SWAA983190 1 19981230 A 2120 AIR DIST BOEING 737 7373A4 1384585 NM CABIN ODOR A SWAA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SW 07 676SW 23288 AFTER ENGINE START, F/A INFORMED FLIGHT CREW, THAT SEVERAL PAX AND F/A SMELLED SOMETHING BURNING. A/C RETURNED TO GATE FOR MAINTENANCE. ODOR IDENTIFIED AS LPS SPRAYED AFT OF BAG BIN, CLEANED UP. OK TO CONTINUE PER M/M. 2 L 7 2 4F RT A16WE 1999010800153 19990108 00153 NM 1999 1 8 SWAA983191 1 19981231 A 5330 SKIN BOEING 737 7373H4 1384600 NM BS 178 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 315SW 23337 DURING SCHEDULED 1/4 CHECK, FOUND BS 178 SKIN CRACKED AT WL 188. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999010800154 19990108 00154 WP 1999 1 8 TWAA9900201 1 19981222 A 5347 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1239 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 DURING OP 15 MAINT CHECK, FOUND CORROSION ON FLOOR TRACK AT STA 1239, LBL 58. REPLACED TRACK PER TWA STD PROCESSES MANU AL 6-70-01 AND REF IPC 53-40-00 ITEM 44. 2 L 7 2 4F RT A6WE 1999010800155 19990108 00155 NM 1999 1 8 TWAA9900202 1 19981218 A 5330 SKIN BOEING 757 7572Q8 1384972 NM BS 1860 TORN A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 703TW 27620 THE FUSELAGE SKIN WAS TORN 6 INCHES BY 3 INCHES, BETWEEN S28 AND S29 ON LEFT SIDE AT STA 1806. EXTERNAL DOUBLER REPAIR INSTALLED PER MCIER RELEASE AND 757 SRM 53-00-01, FIG 204. CHECK-C 5-9-98 LAX. 2 L 7 2 4F RT A2NM 1999010800156 19990108 00156 WP 1999 1 8 TWAA9900203 1 19981222 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 220-240 DAMAGED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 DURING OP 15 MAINT CHECK, FOUND CLASS III TYPE REPAIR AT STA 220 TO 240, BETWEEN LONGERON 17L TO 18L. CUT OUT DAMAGE AN D OLD REPAIR, INSTALLED REPLACEMENT SKIN PER ARA 16077. 2 L 7 2 4F RT A6WE 1999010800157 19990108 00157 WP 1999 1 8 TWAA9900204 1 19981222 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 207-218 SCRATCHED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 DURING OP 15 MAINT CHECK, FOUND 11 SCRATCHES ON FUSELAGE SKIN 1 INCH TO 1.5 INCH LONG, APPROX DEPTH 0.005 TO 0.030, AT S TA 207 TO 218, LONGERON 16L TO 17L. CUT OUT DAMAGED SKIN AND REPAIRED PER SRM 53-04, FIG 12B SHEET 1 AND 2. 2 L 7 2 4F RT A6WE 1999010800158 19990108 00158 WP 1999 1 8 TWAA9900205 1 19981231 A 5330 SKIN DOUG DC9 DC983 3022083 WP BS 207-218 SCRATCHED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 931TW 49527 DURING OP 15 MAINT CHECK, FOUND 11 SCRATCHES IN SKIN 1 INCH TO 1.5 INCH LONG, APPROX DEPTH 0.005 TO 0.030, AT STA 207 TO 218 AND BETWEN L5L AND L6L LEFT SIDE OF FUSELAGE. CUT OUT DAMAGED SKIN AND REPAIRED PER SRM 53-04, FIG 12B SHEETS 1 AN D 4. 2 L 7 2 4F RT A6WE 1999010800160 19990108 00160 NM 1999 1 8 HNAA9883396 1 19981229 A 5610 WINDSHIELD DHAV DHC8 DHC8102 2809003 NM LT COCKPIT FAILED A HNAA K NONE O OTHER NR NOT REPORTED 1 EA 07 833MA 343 CAPTAIN'S WINDSHIELD HEAT WIRING SHORTED IN FLIGHT FOR APPROXIMATELY 4 SECONDS AT WINDSHIELD TERMINAL BLOCK, FOLLOWED BY WINDSHIELD INNER PLY CRACKING. REPAIRED WIRING AND REPLACED WINDSHIELD. 2 H 7 2 4T RT A13NM 1999010800161 19990108 00161 NM 1999 1 8 HNAA9899395 1 19981225 A 5400 STRUCTURE DHAV DHC8 DHC8201 2809001 NM NR 1 & 2 NACELLE CRACKED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 993HA 456 NR 1 NACELLE, AFT MOST STIFFENER LOCATION YW158.70/XN248.50 CRACKED, U-CHANNEL AT BACK OF NACELLE LOCATION XN264.30 CRAC KED, LT STRINGER UNDER NACELLE DECK LOCATION YW151.70/XN248.50 CRACKED IN TWO PLACES, RT STRINGER UNDER THE NACELLE DECK LOCATION YW158.70/XN266.00 CRACKED IN TWO PLACES. NR 2 NACELLE, THE RT STIFFENER BELOW THE NACELLE DECK LOCATION YW158 .70/XN248.50 CRACKED. REPAIRED OR REPLACED ITEMS AS NECESSARY. 2 H 7 2 4T RT A13NM 1999010800162 19990108 00162 NM 1999 1 8 HNAA9892794 1 19981221 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 167-182 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 927HA 117 UNDER COCKPIT FLOOR MINOR SURFACE CORROSION TO THE SKIN ADJACENT TO STRINGER 31 RT, .020 DEPTH CORROSION TO THE SKIN APP ROXIMATELY 3 INCHES LONG AT STRINGER 32 RT. STRINGER 31 RT BETWEEN STATION 167.00 AND STATION 182.00 CORRODED APPROXIMA TELY 11 INCHES EXCEEDING 50 PERCENT LOSS OF MATERIAL IN SOME AREAS AND STRINGER 32 RT BETWEEN STATION 167.00 AND 182.00 CORRODED APPROXIMATELY 3 INCHES LONG, .5 INCHES WIDE AND .025-.030 INCHES DEPTH. REPAIRED, TREATED AND PAINTED AS REQUI RED. 2 H 7 2 4T RT A13NM 1999010800163 19990108 00163 NM 1999 1 8 HNAA9899393 1 19981221 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8201 2809001 NM CABIN DISCHARGED A HNAA K NONE L NO TEST NR NOT REPORTED 1 EA 07 993HA 456 THE 2ND STRIP OF FLOOR EMERGENCY LIGHTS INOP. INTERNAL POWER TO EMERGENCY LIGHTS SUSPECTED. REPLACED BATTERY PACK 3352 -PS2 AND POWER SUPPLY. 2 H 7 2 4T RT A13NM 1999010800165 19990108 00165 SO 1999 1 8 RAAA99E9001 1 19981229 A 3350 CA31 BATTERY PACK LKHEED 188 188C 5262604 SO BS 555 DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EXTERNAL EMERGENCY LIGHTS FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 4 4T 4A22 1999010800166 19990108 00166 SO 1999 1 8 RAAA99E9002 1 19981229 A 3350 240498C RELAY LKHEED 188 188C 5262604 SO BS 555 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 1968R 188C2007 EXTERNAL EMERGENCY LIGHTS WOULD NOT EXTINGUISH ON SERVICE CHECK. CHANGED EXTERNAL EMERGENCY LIGHT RELAY DUE FAILED. 2 L 7 4 4T 4A22 1999010800168 19990108 00168 WP 1999 1 8 CALA9900002 1 19980102 A 3020 DUCT DOUG DC9 DC982 3022082 WP PWA JT8 JT8D217A 52053 NE RT ENGINE COWL RUPTURED A CALA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 09 72829 49489 717442 THE NR 2 ENGINE FIRE WARNING LIGHT AND BELL ACTIVATED AFTER TAKEOFF. THRUST WAS REDUCED TO IDLE WITH THE FIRE HANDLE AN D LOOP LIGHT EXTINGUISHING SHORTLY AFTERWARDS. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAIN TENANCE FOUND THE RT ENGINE COWL ANTI ICE DUCT RUPTURED AND THE ENGINE WIRE HARNESS BURNT AND MELTED. THE WIRE HARNESS AND DUCT WERE REMOVED AND REPLACED. LEAK CHECK WAS GOOD IAW MM 75-10-05. 2 L 7 2 4F 4 F A6WE E9NE 1999010800170 19990108 00170 WP 1999 1 8 CALA9900004 1 19980103 A 3260 800403 CONTROL DOUG DC9 DC932 3022066 WP LT MLG INOP A CALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 14524 47539 THE LT MLG UNSAFE LIGHT ILLUMINATED ON UPLATCH CHECK AFTER TAKEOFF. WHEN THE SLATS AND FLAPS WERE EXTENDED TO FIVE DEGR EES AND THE AIRCRAFT WAS SLOWED TO 210 KNOTS FOR A RETURN TO IAH, THE UNSAFE LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WI THOUT INCIDENT. THE PROXIMITY SWITCH CONTROL WAS REMOVED AND REPLACED. A SIMULATED GEAR RETRACTION GAVE NORMAL GEAR IN DICATIONS. 2 L 7 2 4F A6WE 1999010800171 19990108 00171 SO 1999 1 8 COMA9910002 1 19981231 A 2750 RETRACT MECH EMB 120 EMB120RT SO TE FLAPS MALFUNCTIONED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 249CA 120230 FLAPS WOULD NOT RETRACT AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. 2 L 7 2 4T RT A31SO 1999010800181 19990108 00181 NM 1999 1 8 UPS99228318 1 19980104 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM EMER EXIT DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, 2 EXIT LOCATOR LIGHTS OUT IN CABIN. REPLACED BATT PACKS, OPS CHK GOOD. 2 L 7 3 4F A3WE 1999010800182 19990108 00182 NM 1999 1 8 UPS99228319 1 19980104 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM CABIN DISCHARGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE-N/A, EEL AT 6 ABC TO 9 ABC, 11 ABC, 13 ABC AND GALLEY INOP. REMOVED AND REPLACED BATT PACKS FOR ALL LOC ATIONS AS ABOVE, OPS CHECK OK FOR SERVICE. 2 L 7 3 4F A3WE 1999010800183 19990108 00183 WP 1999 1 8 UPS99828316 1 19981230 A 3230 CONTROL CABLE DOUG DC8 DC871F 302199D WP LANDING GEAR OUT OF ADJ A IPXA K NONE O OTHER TO TAKEOFF 1 SO 01 708UP 46048 INSPECTION TYPE-N/A, ON TAKEOFF GEAR HANDLE REMAINED JAMMED WITH GEAR DOWN. PERFORMED GEAR HANDLE JAMMED CHECKLIST PER ADM. CONTINUED FLIGHT TO SDF WITH GEAR DOWN. ADJUSTED ANTI-RETRACTION LATCH CABLE PER MM 33-31-00, OPS CHECK GOOD. 2 L 7 4 4F RT 4A25 1999010800184 19990108 00184 EU 1999 1 8 QXEA9801865 1 19981111 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 AFT CARGO PIT FRAME 13815A CASTELLATION IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGURE 2. 2 L 7 2 4F RT A20EU 1999010800185 19990108 00185 EU 1999 1 8 QXEA9801866 1 19981108 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 AFT CARGO PIT FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 2. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1999010800186 19990108 00186 EU 1999 1 8 QXEA9801867 1 19981109 A 5320 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 AFT CARGO PIT FRAME 13815B CASTELLATION IS CRACKED AT STRINGER 73. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 9, PARAGRAPH B THROUGH, AND 51-31-01, PAGE 13, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1999010800187 19990108 00187 EU 1999 1 8 QXEA9801868 1 19981112 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON FRAME CLIP ON FRAME 8805, XBL0 IN FORWARD CARGO PIT. REPAIRED IAW FOKKER SRM 53-02-12, FIGURE 1. 2 L 7 2 4F RT A20EU 1999010800188 19990108 00188 EU 1999 1 8 QXEA9801869 1 19981117 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 16495 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 SKIN CRACKED AT STATION 16495 ON AFT END ON MAIN LANDING GEAR KEEL BEAM. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10 -4, PAGE 8, PARAGRAPH 3(C). 2 L 7 2 4F RT A20EU 1999010800189 19990108 00189 EU 1999 1 8 QXEA9801870 1 19981117 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 16495 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 SKIN CRACKED AT STATION 16495 ON AFT END OF RIGHT-HAND MAIN LANDING GEAR KEEL. REPAIRED IAW FOKKER SRM 51-31-01, HORIZO N AIR EA 4-53-595. 2 L 7 2 4F RT A20EU 1999010800190 19990108 00190 EU 1999 1 8 QXEA9801871 1 19981118 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16495 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 REPAIR CLIP CRACKED AT STATION 16495 AFT END OF LEFT-HAND MAIN LANDING GEAR KEEL BEAM. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4(B-C) AND 51-30-02. 2 L 7 2 4F RT A20EU 1999010800191 19990108 00191 EU 1999 1 8 QXEA9801872 1 19981119 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU BS 16495 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 REPAIR CLIP CRACKED AT STATION 16495 AFT END OF RIGHT-HAND MAIN LANDING GEAR KEEL BEAM. REPAIRED IAW FOKKER SRM 51-10-4 , PAGE 9, PARAGRAPH 4(B-C) AND 51-30-02. 2 L 7 2 4F RT A20EU 1999010800192 19990108 00192 EU 1999 1 8 QXEA9801873 1 19981118 A 5320 COVER FOKKER F28 F28MK4000 4990810 EU BS 2475 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 WHEEL WELL BAG TOP COVER HAS 2.5 INCH CRACK AT STATION 2475, BL 150R AND WL 700. REPAIRED IAW FOKKER SRM 51-33-01. 2 L 7 2 4F RT A20EU 1999010800193 19990108 00193 EU 1999 1 8 QXEA9801874 1 19981123 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR BENT A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 AFT CARGO DOOR OUTER SKIN BENT AT TOP AFT CORNER. REPAIRED IAW FOKKER SRM 51-11-4, PAGE 2, PARAGRAPH 2 (E-F). 2 L 7 2 4F RT A20EU 1999010800194 19990108 00194 EU 1999 1 8 QXEA9801875 1 19981117 A 5320 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND SIDE OF THE PEDESTAL HAS CORROSION AT THE FORWARD MIDDLE END AFT FLOOR MOUNT HOLE BORES. REPAIRED IAW FOKKER SRM 51-10-4 AND HORIZON AIR EA 4-53-597. 2 L 7 2 4F RT A20EU 1999010800195 19990108 00195 EU 1999 1 8 QXEA9801876 1 19981117 A 5320 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND SIDE OF PEDESTAL HAS CORROSION ALONG AFT HALF OF BASE EDGE. REPAIRED IAW FOKKER SRM 51-10-04 AND HORIZON AIR EA 4-53-597. 2 L 7 2 4F RT A20EU 1999010800196 19990108 00196 EU 1999 1 8 QXEA9801877 1 19981117 A 5320 PEDESTAL FOKKER F28 F28MK4000 4990810 EU COCKPIT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 RIGHT-HAND SIDE OF PEDESTAL BASE IS MISSING PAINT AND HAS CORROSION ALONG EDGE BETWEEN MOUNT POINTS DIRECTLY INBOARD OF FIRST OFFICER CONTROL COLUMN. REPAIRED IAW FOKKER SRM 51-10-04 AND HORIZON AIR EA 4-53-597. 2 L 7 2 4F RT A20EU 1999010800197 19990108 00197 EU 1999 1 8 QXEA9801878 1 19981118 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU BS 3820 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND FUSELAGE SKIN HAS CRACK ACROSS RIVET HOLE AT STATION 3820, WL 490, BL 1300L. REPAIRED IAW FOKKER SRM 53-02-07 , FIGURE 4 AND MM 53-00-00. 2 L 7 2 4F RT A20EU 1999010800198 19990108 00198 EU 1999 1 8 QXEA9801879 1 19981130 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND FUSELAGE BELOW PILOTS WINDOW HAS A 1.5 DIVOT IN PAINT. REMOVED PAINT, INSPECTED SKIN FOR DAMAGE AND REPAIRED IAW FOKKER SRM 53-02-01. 2 L 7 2 4F RT A20EU 1999010800199 19990108 00199 EU 1999 1 8 QXEA9801880 1 19981130 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND FUSELAGE BELOW PILOTS WINDOW HAS A 1.33 DIVOT IN PAINT. REMOVED PAINT, INSPECTED SKIN FOR DAMAGE AND REPAIRED IAW FOKKER SRM 51-31-01, 51-10-04 AND MM 53-00-00, PAGE 2. 2 L 7 2 4F RT A20EU 1999010800200 19990108 00200 EU 1999 1 8 QXEA9801881 1 19981121 A 5350 NOSE COWL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 DEEP CHAFE AT THE 6 O'CLOCK POSITION ON THE AFT FACE OF THE NOSE COWLING. REPAIRED IAW HORIZON AIR EA 4-72-32. 2 L 7 2 4F RT A20EU 1999010800201 19990108 00201 EU 1999 1 8 QXEA9801882 1 19981108 A 5753 TRACK FOKKER F28 F28MK4000 4990810 EU TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PITTING CORROSION IN THE UPPER PORTION OF THE FLAP TRACK AT STATION 1700. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999010800202 19990108 00202 EU 1999 1 8 QXEA9801883 1 19981130 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 FUEL PANEL 71A APERTURE HAS 3 SMALL CRACKS FROM FASTENER HOLES. REPAIRED IAW HORIZON AIR EA 4-57-188. 2 L 7 2 4F RT A20EU 1999010800203 19990108 00203 EU 1999 1 8 QXEA9801884 1 19981130 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 APERTURE FOR FUEL PANEL 71A INBOARD MOST FASTENER HOLE IN OUTER RING OF FASTENERS HAS A CRACK. REPAIRED IAW HORIZON AIR EA 4-57-188. 2 L 7 2 4F RT A20EU 1999010800204 19990108 00204 EU 1999 1 8 QXEA9801885 1 19981130 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 APERTURE FOR FUEL PANEL 71A HAS TWO SMALL CRACKS FROM FASTENER HOLES ON INNER RING AT FASTENERS. REPAIRED IAW HORIZON A IR EA 4-57-188. 2 L 7 2 4F RT A20EU 1999010800205 19990108 00205 EU 1999 1 8 QXEA9801886 1 19981109 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND WING ACCESS PANEL 73C HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, 4B1-2. 2 L 7 2 4F RT A20EU 1999010800206 19990108 00206 EU 1999 1 8 QXEA9801887 1 19981109 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND WING ACCESS PANEL 73B HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999010800207 19990108 00207 EU 1999 1 8 QXEA9801888 1 19981109 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND WING ACCESS PANEL 73A HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999010800208 19990108 00208 EU 1999 1 8 QXEA9801889 1 19981109 A 5730 PANEL FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 LEFT-HAND WING ACCESS PANEL 71A HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04 P AGE 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999010800211 19990108 00211 EU 1999 1 8 QXEA9802119 1 19981231 A 3350 6008905 POWER SUPPLY GRIMES FOKKER F28 F28MK4000 4990810 EU SEAT 9 INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 491US 498 11156 EMERGENCY LIGHTS ON LEFT OVERWING EXITS WILL NOT EXTINGUISH. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY AT SEAT 9, O PERATIONAL CHECKS OK. 2 L 7 2 4F RT A20EU 1999010800220 19990108 00220 WP 1999 1 8 MWEA990005 1 19981225 A 5320 575468827 DOUBLER DOUG DC9 DC932 3022066 WP COCKPIT CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 204ME 47680 FOUND DOUBLERS ON LEFT AND RIGHT WINDOW RETAINER UPPER AFT CORNERS TO BE CRACKED. MTC REMOVED AND REPLACED INTERNAL DOU BLERS. 2 L 7 2 4F A6WE 1999010800222 19990108 00222 WP 1999 1 8 MWEA990007 1 19981220 A 5400 59132626 ANGLE DOUG DC9 DC914 3022034 WP RT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK IN RIGHT ENGINE PYLON LEADING EDGE LOWER ATTACH ANGLE. MTC FABRICATED AND INSTALLED ANGLE DOUBLER. 2 L 7 2 4F A6WE 1999010800223 19990108 00223 WP 1999 1 8 MWEA980008 1 19981219 A 5400 3914726501 ANGLE DOUG DC9 DC914 3022034 WP LT PYLON CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 800ME 45842 FOUND CRACK IN LEFT ENGINE PYLON LEADING EDGE LOWER ATTACH ANGLE. MTC FABRICATED AND INSTALLED ANGLE REPAIR. 2 L 7 2 4F A6WE 1999010800225 19990108 00225 NM 1999 1 8 VNAA9812016 1 19981222 A 6120 CONNECTOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE DIRTY A VNAA D RETURN TO BLOCK L NO TEST TX TAXI/GRND HDL 1 GL 07 441JS 3059 DURING TAXI, THE LEFT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE OVERSPEED GOVERNOR CANNON PLUG. MAINTENANCE THEN PERFORMED OPERATIONAL CHECKS I N ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00. THE CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO S ERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800228 19990108 00228 WP 1999 1 8 TWAA9900103 1 19981230 A 3350 0105606003 LIGHT DOUG DC9 DC983 3022083 WP ROW 29 INOPERATIVE A TWAA K NONE L NO TEST NR NOT REPORTED 1 CE 05 9405T 53141 FOUND LAST SIX ESCAPE PATH LIGHTS INOPERATIVE IN CABIN. REPLACED WIRE LIGHT ASSY AT ROW 29. CHECK-C 11-1-98 MCI. 2 L 7 2 4F RT A6WE 1999010800229 19990108 00229 NM 1999 1 8 SPAA9800026 1 19981231 A 5320 FITTING BOEING 737 7372T4 1384492 NM BS 540 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP C53-208-01, THE AFT RIGHT HAND CARGO TIE DOWN FITTING AT BS 540 WAS FOUND CORRODED BEYOND SRM LIMITS. THE PART WAS REPLACED PER SRM 53-10-5, 51-10-5 AND 53-10-2. 2 L 7 2 4F A16WE 1999010800230 19990108 00230 NM 1999 1 8 SPAA9800027 1 19981231 A 5311 FRAME BOEING 737 7372T4 1384492 NM BS 887 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-01, FRAME SECTION AT BS 887, RBL 65 WHERE IT PASSES THROUGH FLOOR STRUCTURE, WAS FOUND TO HAVE CORROSION BEYOND SRM LIMITS. DAMAGE WAS REPAIRED PER SRM 51-40-3. 2 L 7 2 4F A16WE 1999010800231 19990108 00231 NM 1999 1 8 SPAA9800028 1 19981231 A 5320 ANGLE BOEING 737 7372T4 1384492 NM BS 1006-1016 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, FLOORBEAM BRACE ANGLE AT BETWEEN BS 1006 AND BS 1016, LBL 3, WAS FOUND CO RRODED BEYOND SRM LIMITS. NEW PART INSTALLED PER SRM 51-20-1, 51-10-1 AND 51-30-2. 2 L 7 2 4F A16WE 1999010800232 19990108 00232 NM 1999 1 8 SPAA9800029 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 967 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, FLOORBEAM AT BS 967, RBL 3, WAS FOUND CORRODED BEYOND SRM LIMITS. THE PA RT WAS REPLACED PER SRM 51-20-1, 51-10-1 AND 51-30-6. 2 L 7 2 4F A16WE 1999010800233 19990108 00233 NM 1999 1 8 SPAA9800030 1 19981231 A 5313 STRINGER BOEING 737 7372T4 1384492 NM BS 904 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-208-01, S27L WAS FOUND CORRODED BEYOND SRM LIMITS AT BS 904. THE STRINGER SECTIO NS WERE REPLACED BETWEEN BS 881 AND BS 933 PER SRM 51-10-2, 51-30-0 AND 53-10-3 FIG 1. 2 L 7 2 4F A16WE 1999010800234 19990108 00234 NM 1999 1 8 SPAA9800031 1 19981231 A 5320 TIE CLIP BOEING 737 7372T4 1384492 NM FUSELAGE CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF MANDATORY SERVICE BULLETIN 737-53-1085 INSPECTION, AD 93-08-04, ELEVEN STRINGER TO FRAME TIE CL IPS WERE FOUND CRACKED AT THE FOLLOWING LOCATIONS: BS 616 AT S3L, BS 685 AT S2L AND S4R, BS 706 AT S2R, BS 727 AT S4L, B S 727B AT S5L, S6L AND S7R, BS 747 AT S7L, BS 767 AT S6L AND 787 AT S6R. ALL WERE REPLACED PER SRM 51-30-2. 2 L 7 2 4F A16WE 1999010800235 19990108 00235 NM 1999 1 8 SPAA9800025 1 19981231 A 5315 FLOORBEAM BOEING 737 7372T4 1384492 NM BS 947.5 CORRODED A SPAA K NONE O OTHER IN INSP/MAINT 1 WP 28 703S 22529 DURING ACCOMPLISHMENT OF CPCP TASK C53-107-02, FLOORBEAM SECTION AT BS 947.5 FROM RBL 22 TO LBL 22, WAS FOUND CORRODED B EYOND SRM LIMITS. DAMAGE REPAIRED PER SRM 53-10-9, FIG 2. 2 L 7 2 4F A16WE 1999010800236 19990108 00236 EU 1999 1 8 MALA976278 1 19981221 A 2750 676801007 CONTROL UNIT BAC 146 AVRO146RJ85A 1500097 EU TE FLAPS MALFUNCTIONED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 513XJ E2329 AFTER TAKEOFF WHEN FLAPS REACHED 0 DEGREES INDICATED, FLAP FAULT ILLUMINATED, A VIBRATION WAS NOTED TO 265 KIAS IN CRUIS E, WHEN FLAPS 18 WAS SELECTED, FLAPS MOVED TO BETWEEN 0 AND 18. AIRCRAFT RETURNED TO MSP. MAINTENANCE FOUND FLAPS RUNN ING AT HALF SPEED WITH FLAP FAULT CODE 11, RESET FLAP CIRCUIT, SYSTEM CHECKED GOOD. MAINTENANCE REPLACED FLAP ELECTRONI C CONTROL UNIT FOR PRECAUTIONARY, OPS CHECK GOOD. 2 H 7 4 4F RT A49EU 1999010800237 19990108 00237 1999 1 8 MALA976279 3 19981221 A 6140 523535 INDICATOR SAAB SF340 340B 7860101 EU LT PROP OIL TEMP FAILED A MALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 15 403XJ 340B403 ON CLIMBOUT, THE LEFT PROP OIL TEMP DROPPED BELOW GREEN ARC TO ABOUT 35 DEGREES. RESET CIRCUIT BREAKER, IT THEN DROPPED TO 25 DEGREES AND STAYED THERE UNTIL LANDING BACK IN MSP. MAINTENANCE REPLACED LEFT PROP OIL PRESS/TEMP INDICATOR, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1999010800238 19990108 00238 1999 1 8 MALA976280 3 19981231 A 6112 R3904123F27 DEICE SAAB SF340 340B 7860101 EU LT PROP FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 402XJ 340B402 LEFT PROP DEICE CAUTION LIGHT CAME ON IN FLIGHT. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED LEFT PROP ASSEMBLY, OP S AND LEAK CHECK GOOD. 2 L 7 2 4T RT A52EU 1999010800239 19990108 00239 EU 1999 1 8 MALA976281 1 19981228 A 3213 STRUT SAAB SF340 SF340A 7850100 EU LT MLG FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 76XJ 076 AFTER DEPARTURE SELECTED GEAR UP AND THE CONFIG WARNING AND THE OAT CAUTION LIGHTS ILLUMINATED. AIRCRAFT RETURNED TO MS P. MAINTENANCE FOUND LEFT MAIN LANDING GEAR STRUT BLOWN. MX REPACKED AND REASSEMBLED LEFT MLG STRUT BEARING, REPAIRED STRUT BORE, REPLACED LINER (P/N AIR123412), INSTALLED NEW NUT ON AXEL ADAPTER, INSTALLED 6 NEW BOLTS ON BRAKE FLANGE AND SERVICED LEFT MLG STRUT. OPS CHECKS GOOD, EXTENTION IS WITHIN LIMITS. 2 L 7 2 4T RT A52EU 1999010800240 19990108 00240 EU 1999 1 8 MALA976282 1 19981229 A 3230 ACTUATOR SAAB SF340 SF340A 7850100 EU NLG DOWNLOCK FAILED A MALA O OTHER J WARNING INDICATION LD LANDING 1 GL 15 41XJ 041 NOSE GEAR DOWN AND LOCKED INDICATION INOP. FOLLOWED QRH PROCEDURES, NO HELP. LANDED WITHOUT INCIDENT. MAINTENANCE REP LACED NOSE LANDING GEAR DOWNLOCK ACTUATOR (P/N AIR 84612-2) (S/N 8700651) AND EXTENTION/RETRACTION ACTUATOR (P/N AIR 864 14-1) (S/N LK8500260). PERFORMED SYSYEM OPS CHECKS, OPS CHECKS GOOD, LEAKS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999010800241 19990108 00241 NM 1999 1 8 RAAA98B1102 1 19981230 A 3350 8621014 BATTERY PACK INTVLV 873100212 BOEING 727 72722C 138400F NM CABIN DISCHARGED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 831RV 19093 RT FWD OVERWING EMERGENCY EXIT EGRESS IDENTIFIER LIGHT FAILED SERVICE CHECK. CHANGED BATTERY PACK DUE DISCHARGED. 2 L 7 3 4F A3WE 1999010800242 19990108 00242 SO 1999 1 8 RAAA98E8029 1 19981223 A 3350 1102837 LIGHT LKHEED 188 188C 5262604 SO ROW 7 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 OVERHEAD EMERGENCY LIGHT AT PAX ROW 7 FAILED SERVICE CHECK. CHANGED LIGHT ASSY DUE FAILED. 2 L 7 4 4T 4A22 1999010800243 19990108 00243 SO 1999 1 8 RAAA98E8030 1 19981228 A 3350 1102832 LIGHT LKHEED 188 188C 5262604 SO ROW 7, 10, 11 FAILED A RAAA K NONE L NO TEST IN INSP/MAINT 1 AL 03 178RV 188C2010 FLIGHT CREW REPORTED EMERGENCY LIGHTS IN CABIN COME ON INTERMITTENTLY IN FLIGHT. CHANGED OVERHEAD EMERGENCY LIGHTS AT P AX ROWS 7, 10, 11 DUE FAILED. 2 L 7 4 4T 4A22 1999010800244 19990108 00244 WP 1999 1 8 CALA9802201 1 19981227 A 3350 P2070003005 LIGHT DME DOUG DC9 DC982 3022082 WP GALLEY INOPERATIVE A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14810 49264 INSPECTION FOUND FORWARD GALLEY EMERGENCY HAND FLASHLIGHT INOPERATIVE. THE FLASHLIGHT WAS REMOVED AND REPLACED. 2 L 7 2 4F A6WE 1999010800245 19990108 00245 WP 1999 1 8 CALA9802202 1 19981228 A 5320 JAMB DOUG DC9 DC932 3022066 WP BS 370-427 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND FORWARD BAGGAGE BIN DOOR JAMB PAN CORRODED AT STA 370 TO 427. THE LOWER SECTION OF DOOR PAN WAS REPLAC ED IAW SRM 53-05, FIGURE 44. 2 L 7 2 4F A6WE 1999010800246 19990108 00246 WP 1999 1 8 CALA9802203 1 19981228 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1074.107 CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND FOUR .5 INCH LONG CRACKS IN CANTED FRAME AT STA 1074.107, LONGERON 4R AND 5R. THE CANTED FRAME WAS REM OVED AND REPLACED IAW SRM 51-10-02. 2 L 7 2 4F A6WE 1999010800247 19990108 00247 WP 1999 1 8 CALA9802204 1 19981229 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 285 DENTED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 16895 49394 INSPECTION FOUND A DENT IN FUSELAGE SKIN AND CUSP AT STA 285, LONGERON 18L. A REPAIR WAS INSTALLED IAW ECRA 5330-02752. 2 L 7 2 4F A6WE 1999010800248 19990108 00248 WP 1999 1 8 CALA9802205 1 19981230 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389 GOUGED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17531 45847 INSPECTION FOUND FLOORBEAM IN FORWARD BAGGAGE BIN AT STA 389 GOUGED BY BAG BIN DOOR. THE AREA WAS REPAIRED IAW SRM 53-0 5, FIGURE 86. 2 L 7 2 4F A6WE 1999010800249 19990108 00249 NM 1999 1 8 CALA9802206 1 19981230 A 3397 WIRE BOEING 757 757224 1384958 NM ROW 27C BROKEN A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 12116 27558 INSPECTION FOUND EMERGENCY AISLE PATH LIGHT ON SEAT 27C INOPERATIVE. A BROKEN WIRE TO LIGHT WAS REPAIRED AND OPERATION WAS RESTORED. 2 L 7 2 4F RT A2NM 1999010800250 19990108 00250 NE 1999 1 8 COMA9810291 2 19981228 A 7261 MS919404 FITTING EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENGINE FAILED A COMA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 01 168CA 1168 LEFT ENGINE OIL PRESSURE DROPPED BELOW 40 PSI, IN FLIGHT SHUT DOWN. REPLACED ELBOW FITTING THAT HAD BUCKED OUT ON THE O IL PUMP COVER. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800251 19990108 00251 SO 1999 1 8 COMA9810292 1 19981229 A 3350 1317 BULB EMB 120 EMB120RT SO CABIN FAILED A COMA K NONE L NO TEST IN INSP/MAINT 1 SO 01 152CA 1152 EMERGENCY LIGHT AT SEAT 2A IS INOPERABLE. REPLACED LIGHT BULB. 2 L 7 2 4T RT A31SO 1999010800252 19990108 00252 1999 1 8 COMA9810293 3 19981228 A 6140 CONNECTOR EMB 120 EMB120RT SO ENGINE DIRTY A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 261CA 120254 AUTOFEATHER WARNING DURING TAKEOFF. CLEANED CONNECTORS AT ENGINE SIGNAL CONDITIONER UNITS, SYSTEM OPERATION NORMAL. 2 L 7 2 4T RT A31SO 1999010800253 19990108 00253 EA 1999 1 8 COMA9860410 1 19981229 A 2750 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA TE FLAP SYST TRIPPED A COMA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 709CA 7238 FLAPS FAILED WHEN RETRACTED. RESET FLAP SYSTEM CIRCUIT BREAKERS. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F RT A21EA 1999010800254 19990108 00254 EA 1999 1 8 COMA9860411 1 19981228 A 2750 860D10018ABC FECU CNDAIR CL600 CL6002B19 EA E & E COMPT MALFUNCTION A COMA O OTHER J WARNING INDICATION AP APPROACH 1 SO 01 716CA 3958 7250 FLAPS FAILED WHEN SELECTED TO LANDING POSITION. REPLACED THE FLAP ELECTRONIC CONTROL UNIT. 2 L 7 2 4F RT A21EA 1999010800255 19990108 00255 SO 1999 1 8 COMA9910001 1 19981230 A 3150 ATG120TR SENSOR EMB 120 EMB120RT SO ELEVATOR TRIM MALFUNCTION A COMA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 01 264CA 1256 TAKEOFF TRIM WARNING. REPLACED ELEVATOR TRIM PROXIMITY SENSOR. 2 L 7 2 4T RT A31SO 1999010800256 19990108 00256 EA 1999 1 8 COMA9960001 1 19981231 A 5270 WARNING CNDAIR CL600 CL6002B19 EA PAX DOOR ACTIVATED A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 956CA 7105 CABIN DOOR LATCH WARNING. COULD NOT DUPLICATE. INSPECTED DOOR LATCH AND FOUND NO DEFECTS. 2 L 7 2 4F RT A21EA 1999010800257 19990108 00257 EA 1999 1 8 COMA9960002 1 19981231 A 5270 CONNECTOR CNDAIR CL600 CL6002B19 EA PAX DOOR DEFECTIVE A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 7014 CABIN DOOR WARNING DURING FLIGHT. REPAIRED DOOR WIRING CONNECTOR. 2 L 7 2 4F RT A21EA 1999010800259 19990108 00259 EA 1999 1 8 COMA9960004 1 19981230 A 5297 WIRE CNDAIR CL600 CL6002B19 EA PAX DOOR BROKEN A COMA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 01 916CA 7014 CABIN DOOR WARNING AFTER TAKEOFF. REPAIRED BROKEN WIRE AT DOOR WIRING HARNESS. 2 L 7 2 4F RT A21EA 1999010800260 19990108 00260 NM 1999 1 8 QXEA9802115 1 19981229 A 3350 1005511 LIGHT DHAV DHC8 DHC8102 2809003 NM COCKPIT INOP A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 102AV 27191 4162 091 HANDHELD EMERGENCY LIGHT IN THE COCKPIT OVERHEAD IS INOP. MAINTENANCE REPLACED THE OVERHEAD EMERGENCY LIGHT, OPERATIONA L CHECKS GOOD. 2 H 7 2 4T RT A13NM 1999010800262 19990108 00262 WP 1999 1 8 ABXA9801194 1 19981228 A 5311 99196181 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 718 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND LEFT FUSELAGE MAIN FRAME AT STATION 718 CRACKED. REPLACED MAIN FRAME IAW DC9 SRM 51-2-0. 2 L 7 2 4F A6WE 1999010800263 19990108 00263 WP 1999 1 8 ABXA9801195 1 19981222 A 5320 99105037 WEB DOUG DOUG DC9 DC931 3022065 WP BS 890 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND LEFT CUSP WEB AT STATION 890 CRACKED. REPLACED CUSP WEB IAW DC9 SRM 51-30-2. 2 L 7 2 4F A6WE 1999010800264 19990108 00264 WP 1999 1 8 ABXA9801196 1 19981222 A 5320 5956034561 FITTING DOUG DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND CRACKED FLOOR SUPPORT FITTING AT STATION 945, BETWEEN 27 AND 28 LEFT. REPLACED FITTING IAW DC9 SR M 51-30-5. 2 L 7 2 4F A6WE 1999010800265 19990108 00265 WP 1999 1 8 ABXA9801197 1 19981222 A 5313 27779225 LONGERON DOUG DOUG DC9 DC931 3022065 WP BS 965 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND CRACK IN LONGERON 16 RIGHT AT STATION 965. REPAIRED IAW DC9 SRM 53-02-0. 2 L 7 2 4F A6WE 1999010800266 19990108 00266 WP 1999 1 8 ABXA9801198 1 19981228 A 5720 4912009506 CLIP DOUG DOUG DC9 DC931 3022065 WP WS 69 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND CRACKED SHEAR CLIP AT RIGHT WING STATION XRS 69.00 AT AFT BOTTOM. REPLACED SHEAR CLIP IAW DC9 SRM 51-10-04. 2 L 7 2 4F A6WE 1999010800267 19990108 00267 WP 1999 1 8 ABXA9801199 1 19981228 A 5320 995823811 SHEAR TIE DOUG DOUG DC9 DC931 3022065 WP BS 980 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND CRACKED SHEAR TIE AT STATION 980, BELOW LONGERON 14 LEFT. REPLACED SHEAR TIE IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999010800268 19990108 00268 WP 1999 1 8 ABXA9801200 1 19981228 A 5320 991015421 CLIP DOUG DOUG DC9 DC931 3022065 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND STATION 996 RIGHT FUSELAGE FRAME ATTACH FOOT CLIP CRACKED. REPLACED CLIP IAW DC9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999010800269 19990108 00269 NE 1999 1 8 DLM88982632 2 19981226 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA O OTHER A FLAME/FIRE TX TAXI/GRND HDL 1 SO 27 907DE 19144 53416 725817 ON TAXI OUT, DURING START OF NR 2 ENG, REPORTED TAIL PIPE FIRE AND EGT REACHED 600 DEGREES. REPLACED ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1999010800270 19990108 00270 NM 1999 1 8 DL72S982636 1 19981228 A 5330 65545662 SKIN BOEING 727 727232 1384082 NM BS 480-681 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 495DA 21075 THE LT SIDE LWR FUSE SKIN AT S26L LAP SPLICE WAS FOUND WITH AN APPROX 19 INCH LONG CRACK BETWEEN BS 536 AND BS 564. THE CRACK IS LOCATED IN THE LWR OVERLAPPED SKIN, EXTENDING NEARLY HORIZ BETWEEN 20 FASTENERS IN THE LWR ROW OF THE TRIPLE R OW ATTACH PATTERN. REPAIRED PER ERA 366303-14. 2 L 7 3 4F A3WE 1999010800271 19990108 00271 NM 1999 1 8 DL72W982637 1 19981228 A 5330 6518420484 SKIN BOEING 727 727247 138408F NM BS 351 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2809W 20581 THE UPPER FUSE SKIN AT BS 351 ON THE UPPER ROW OF THE S24R LAP SPLICE WAS FOUND CRACKED. THE CRACK EXTENDED THRU THREE CONSECUTIVE FASTENERS WITH A TOTAL LENGTH OF 3. REPAIRED PER ERA 366371-14. 2 L 7 3 4F A3WE 1999010800272 19990108 00272 NM 1999 1 8 DL733982638 1 19981228 A 2910 LINE BOEING 737 737347 1384647 NM LEFT LEAKING A DALA O OTHER B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SO 27 304WA 23345 AIR TURNBACK DUE TO ELECTRICAL SMELL IN CABIN. MTC TROUBLESHOT AND FOUND THE LEFT PACK WAS OVERHEATING. ITEM THEN FWD TO MCO. FOUND HYDRAULIC LINE LEAK. TIGHTENED NUT AND CLEANED AREA. 2 L 7 2 4F RT A16WE 1999010800273 19990108 00273 NM 1999 1 8 DL72S982639 1 19981228 A 5311 FRAME BOEING 727 727232 1384082 NM PAX DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 546DA 22677 FOUND AT C-1 LETTER CK, .375 INCH VISIBLE CRACK ON LT AFT ENTRYWAY FRAME APPROX 6 INCHES BELOW UPPER STOP PAD. REPAIRED PER SRM 53-10-9. 2 L 7 3 4F A3WE 1999010800274 19990108 00274 NM 1999 1 8 DL72K982640 1 19981208 A 5341 FITTING BOEING 727 727232 1384082 NM LT BOTTLE PIN CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 AT HMV FOUND BUSHING BORE AT LT AFT BOTTLE PIN BODY BORE CORROSION. AFTER BUSHING REMOVAL FOUND SEVERAL SPOTS AROUND BO RE. MACHINED BORE PER SRM 53-40-1. TREATED, REPAIRED AND INSTALLED SLAVE. 2 L 7 3 4F A3WE 1999010800275 19990108 00275 NM 1999 1 8 DL72S982642 1 19981228 A 3350 900542 BATTERY BOEING 727 727232 1384082 NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 493DA 21062 RT OVERWING EMER EXIT LIGHT INOP. REPLACED BATTERY RACK AND BATTERY, PACK OPS NOW OK. 2 L 7 3 4F A3WE 1999010800276 19990108 00276 NM 1999 1 8 DL72E982643 1 19981228 A 3350 900542 BATTERY PACK BOEING 727 727247 138408F NM CABIN DISCHARGED A DALA K NONE L NO TEST IN INSP/MAINT 1 SO 27 2829W 21481 EMERG EXIT LIGHT SIGN ON FACE OF LIFE RAFT COMPARTMENT, MAIN CABIN INOP ON TEST. REPLACED RACK AND BATTERY PACK, OPN CK S OK. 2 L 7 3 4F A3WE 1999010800277 19990108 00277 NM 1999 1 8 DL72L982644 1 19981224 A 3610 DUCT 10610651 BOEING 727 727232 1384082 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE FAILED A DALA E ENGINE SHUTDOWN M J OVER TEMP WARNING INDICATION CL CLIMB 1 SO 27 510DA 21312 700641 ON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. ALL CK LIST WERE RUN AND LIGHT DID NOT GO OUT. SHUT DOWN NR 1 ENG AND DUMP FUEL. RETURNED TO SEA. REPLACED LEAKING HP TAI DUCT, LEAK CK NORMAL. 2 L 7 3 4F 4 F A3WE E2EA 1999010800278 19990108 00278 NM 1999 1 8 DL72W982645 1 19981215 A 5754 RIB BOEING 727 727247 138408F NM NR 2 LE SLAT CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 FOUND DURING MV2/F-1 LETTER CHECK, .75 INCH CRACK AT NR 2 SLAT NOSE RIB O/B SIDE OF ACTUATOR AT AFT LWR CORNER. REPAIRE D PER M/M 57-54-0. 2 L 7 3 4F A3WE 1999010800279 19990108 00279 NM 1999 1 8 DL733982646 1 19981229 A 5312 BULKHEAD WEB BOEING 737 737347 1384647 NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 DURING ACCOMPLISHMENT OF SI 5-69482-12, SEVERAL CRACKS WERE DISCOVERED ON THE FWD FACE OF THE BS 178 BLKD. REPAIRED PER ERA 332599-14. 2 L 7 2 4F RT A16WE 1999010800280 19990108 00280 NM 1999 1 8 DL72L982647 1 19981229 A 5311 6516349127 FRAME BOEING 727 727232 1384082 NM BS 1166 CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 CORROSION WAS FOUND ON THE BS 1166 FRAME AT THE SKIN CLIP BETWEEN S29R AND S30. DAMAGE RESULTED IN CUTOUT IN THE LWR 2. 5 OF THE FRAME AS WELL AS THE BONDED FAIL SAFE STRAP. REPAIRED PER ERA 332608-14. 2 L 7 3 4F A3WE 1999010800281 19990108 00281 NM 1999 1 8 DLM88982648 1 19981229 A 5330 5920323249 SKIN DOUG MD88 MD88 3023688 NM BS 425 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 A DENT WAS FOUND IN THE FUSELAGE SKIN AND UNDERLYING DOOR SURROUND DOUBLER AFT OF THE C1 DOOR AT APPROX L21R. REPAIRED PER ERA 332617-14. 2 L 7 2 4F RT A6WE 1999010800282 19990108 00282 NM 1999 1 8 DLM88982649 1 19981229 A 5330 592480296 SKIN DOUG MD88 MD88 3023688 NM BS 588 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 FUSE SKIN WAS FOUND TO HAVE A GOUGE FWD OF STA 588 BELOW L17R. DAMAGE REMOVAL RESULTED IN A CUTOUT OF APPROX 2.9 BY 30. REPAIRED PER ERA 332627-14. 2 L 7 2 4F RT A6WE 1999010800283 19990108 00283 NM 1999 1 8 DLM88982650 1 19981229 A 5330 5911402 SKIN DOUG MD88 MD88 3023688 NM BS 167-188 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 A GOUGE WAS FOUND ON THE FUSE SKIN BETWEEN STA 167 TO 188 AT L21R. CUTOUT IS 6.2 BY 21.2. REPAIRED PER ERA 332597-14. 2 L 7 2 4F RT A6WE 1999010800284 19990108 00284 NM 1999 1 8 DL72K982651 1 19981229 A 5320 65175176 ANGLE BOEING 727 727232 1384082 NM BS 1273 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 415DA 21257 FOUND ON C1 LETTER CK, HORIZONTAL TORQUE BOX ANGLE CRACKED AT STA 1273 RT LOWER TORQUE BOX. REPAIRED PER SRM 53-10-10. 2 L 7 3 4F A3WE 1999010800285 19990108 00285 NM 1999 1 8 DL72W982652 1 19981229 A 2782 BOLT BACB30GE8D42 BOEING 727 727247 138408F NM NR 3 LE FLAP ACT MISSING A DALA L ABORTED APPROACH D J INFLIGHT SEPARATION WARNING INDICATION LD LANDING 1 SO 27 2815W 20871 ON APPROACH, LEADING EDGE FLAP NR 3 UNSAFE HAD AMBER LIGHT, ON GO-AROUND FLAPS WENT GREEN. SAFE INDICATION ON LANDING. AFTER LANDING FLAPS TO 25 DEGREES, FLAP INDICATION WENT TO AMBER. FOUND ACTUATOR DISCONNECTED FROM FLAP, BOLT MISSING. DAMAGE TO FLAP CONSISTS OF A 1.75 INCH CROSS SHAPED CRACK. FLAP (P/N 574703325), REPLACED FLAP AND REPLACED ACTUATOR AS PRECAUTIONARY. 2 L 7 3 4F A3WE 1999010800286 19990108 00286 NM 1999 1 8 DL72K982654 1 19981230 A 5330 655458041 SKIN BOEING 727 727232 1384082 NM BS 990 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 A GOUGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE WAS LOCATED AT S24R AND THE S KIN, DOUBLER AND TRIPLER WERE TRIMMED OUT 0.600 FROM THE EDGE OF THE SKIN PANEL. THE INTERNAL BEARSTRAP WAS TRIMMED ONL Y 0.200. REPAIRED PER ERA 332631-14. 2 L 7 3 4F A3WE 1999010800287 19990108 00287 NM 1999 1 8 DL73K982655 1 19981230 A 5330 654577870 SKIN BOEING 737 737232 1384475 NM R2 DOORWAY CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 327DL 23099 DURING RTN VISUAL INSPECTIONS, A CRACK WAS FOUND IN THE LWR BONDED SKIN PANEL AT THE LWR HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) SURROUND. TRIMMING OUT THE DAMAGE IN THE LWR BONDED SKIN REVEALED A CRACK IN THE BEAR STRAP. TRIM OUT IN BEA R STRAP IS APPROX 1 INCH AND THE SKIN TRIM OUT IS APPROX 2 INCHES. REPAIRED PER ERA 366386-14. 2 L 7 2 4F RT A16WE 1999010800288 19990108 00288 NM 1999 1 8 DL72W982656 1 19981213 A 5312 BULKHEAD ANGLE BOEING 727 727247 138408F NM BS 178 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 REF NR 214, 215, 216, 217, 218 AND 219 REPAIRED STA 178 BLKHD AND REPLACED UPPER AND LWR ANGLES PER SRM 53-10-9 FIG 14. COMPLETED AND FORWARDED DATA RETRIEVAL. 2 L 7 3 4F A3WE 1999010800289 19990108 00289 NM 1999 1 8 DL72L982657 1 19981230 A 2910 LINE 651784961M BOEING 727 727232 1384082 NM HYD SVC BAY CRACKED A DALA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 27 505DA 21307 CREW LOST B HYDRAULICS PRESSURE AND QUANTITY ON ARRIVAL TO PHL. FOUND BROKEN HYDRAULIC LINE IN HYD SERVICE BAY REF IPC- 29- 14-00-06 ITEM 160. MPN-65-17849-61M. DPN-294201161. INSTALLED TEMP HYDRAULIC LINE, SERVICED HYD SYS TO FULL AND LEA K CHKS NORMAL. FWD TEMP LINE INSTALLATION TO MCO. 2 L 7 3 4F A3WE 1999010800290 19990108 00290 NM 1999 1 8 DLM88982658 1 19981231 A 5330 SKIN DOUG MD88 MD88 3023688 NM BS 322 DENTED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 906DL 49537 SKIN WAS FOUND DENTED AT APPROX BS 332 BETWEEN S19 AND S20R. A CUTOUT OF 8.2 BY 3.2 WAS MADE TO REMOVE THE DAMAGE. REP AIRED PER ERA 332600-14. 2 L 7 2 4F RT A6WE 1999010800291 19990108 00291 NM 1999 1 8 DL733982660 1 19981231 A 5320 WEB BOEING 737 737347 1384647 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 CRACK WAS FOUND DURING INSPECTION PER EO 5-70166-3 IN THE WEB AT BS 727, S18A (LHS). THE CRACK EXCEEDED EO/SB LIMITS. R EPAIRED PER ERA 332607-14. 2 L 7 2 4F RT A16WE 1999010800292 19990108 00292 NM 1999 1 8 DL733982661 1 19981231 A 5330 6546774 SKIN BOEING 737 737347 1384647 NM BS 727 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 FUSE SKIN FOUND CRACKED AT BS 727E, S23L. DAMAGE REMOVAL RESULTED IN A 4.75 BY 2 INCH CUT OUT. REPAIRED PER ERA 332622 -14. 2 L 7 2 4F RT A16WE 1999010800293 19990108 00293 NM 1999 1 8 DL733982662 1 19981231 A 5330 SKIN BOEING 737 737347 1384647 NM C1 DOORWAY DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 306WA 23347 DURING INSPECTION OF C1 DOOR CUTOUT SKIN AN EXISTING REPAIR WAS REMOVED FOR INSPECTABILITY OF THE AREA. REPAIRED AND RE WORKED PER ERA 332586-14. 2 L 7 2 4F RT A16WE 1999010800294 19990108 00294 NM 1999 1 8 DL76P982663 1 19981231 A 2120 AIR DIST BOEING 767 767332 1382001 NM CABIN ODOR A DALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 27 143DA 25991 IMMEDIATELY AFTER T/O, FLIGHT ATTENDENT IN FWD 1ST CLASS CABIN DETECTED BURNING SMELL. FLIGHT RETURNED FOR LANDING AT D FW. OPENED OVERHEAD IN 1ST AND 1ST SECTION OF COACH, CHECKED ALL BALLAST FOR PROBLEMS. TOOK A/C TO HANGAR, RAN AT T/O, REDUCED T/O IN CONFIRGRATION WITH PACKS ON AND COULD NOT DUPLICATE SMELL PROBLEM. REPLACED COFFEEMAKERS IN MID GALLEY OUTBD AND CENTER. A/C OK FOR SERVICE. FWD NR 1 COFFEEMAKER TO MCO. THIS WAS PRECAUTION, ONLY ITEMS THAT HAD ANY TYPE OF BURNING SMELL. 2 L 7 2 4F RT A1NM 1999010800295 19990108 00295 NE 1999 1 8 DL72S982664 2 19981231 A 7230 COMPRESSOR BOEING 727 727232 1384082 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE STALLED A DALA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 27 409DA 63737 687501 21153 687501 NR 2 ENGINE COMPRESSOR STALLS AND VIBRATIONS ON CLIMBOUT. ACFT RETURNED TO DFW. NR 2 ENGINE CHANGED. 2 L 7 3 4F 4 F A3WE E2EA 1999010800300 19990108 00300 NM 1999 1 8 SCNA98154 1 19981228 A 3350 LIGHT BOEING 727 727225 1384077 NM ROW 22 DEF INOPERATIVE A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 282SC 22558 DURING A LINE MAINTENANCE CHECK, A LIGHT WAS FOUND INOPERATIVE ON THE EMERGENCY PATH LIGHTING AT LOCATION 22DEF. REPLAC ED THE EMERGENCY LIGHT AND LENSE IN THE FLOOR TRACK AT SEAT 22DEF, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1999010800301 19990108 00301 NE 1999 1 8 SCNA98155 2 19981231 A 7510 DEICE DUCT BOEING 727 7272J4 1384006 NM PWA JT8 JT8D17R 52049 NE NR 3 ENGINE BLOWN A SCNA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 288SC 20765 DURING CLIMBOUT, CREW OBSERVED ENGINE NUMBER 3 FIRE WARNING AFTER PASSING 10,000 FEET. NUMBER THREE ENGINE WAS SHUT DOW N PRECAUTIONARY AND FIRE BOTTLE WAS DISCHARGED. RETURNED AIRCRAFT TO MSP, UNEVENTFUL. FOUND THE NUMBER THREE ENGINE AN TI ICE DUCT TO HAVE AN END BLOWN OFF. REMOVED AND REPLACED THE DUCT IAW BMM 302111, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F 4 F RT A3WE E2EA 1999010800302 19990108 00302 WP 1999 1 8 SCNA98156 1 19981231 A 2150 ABM70121 VALVE ACM7009506 DOUG DC10 DC1015 3022118 WP NR 3 PACK FAILED A SCNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 15 151SY 48295 DURING CLIMBOUT, CREW REPORTED UNABLE TO MAINTAIN CABIN ALTITUDE. AT 31,000 FEET THE ALTITUDE WARNING HORN SOUNDED AND DESCENDED TO 19,000 FEET BEFORE THE CABIN WAS CONTROLLABLE. DIVERTED AIRCRAFT TO DEN. FOUND THE NUMBER THREE PACK DUCT BLOWN OFF THE BACK OF THE COALESCER CANISTER AND THE DISCHARGE CHECK VALVE FLAPPER BROKEN. REPLACED THE CHECK VALVE AN D CONDITIONED AIR DUCT. AIRCRAFT PRESSURIZES NORMALLY WITH THE PACK SYSTEM PER MM 215400. 2 L 7 3 4F A22WE 1999010800303 19990108 00303 NM 1999 1 8 DHL98717004 1 19981226 A 3610 1111588311 VALVE BOEING 727 72723 1384004 NM NR 1 ENGINE DIRTY A DHLA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SO 01 717DH 19389 SMOKE IN COCKPIT AFTER TAKEOFF. FOUND NR 1 ENGINE PRECOOLER CHECK VALVE STUCK OPEN. CLEANED VALVED AND RAN ENGINE, OPS CHECK GOOD. 2 L 7 3 4F A3WE 1999010800304 19990108 00304 SO 1999 1 8 SWIA971342 1 19981221 A 2752 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT TE FLAP FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 207SW 120266 NACELLE FLAP DISAGREEMENT AT 2 BARS ON DEPARTURE. RETURNED TO SLC. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-0 8 AND OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800305 19990108 00305 SO 1999 1 8 SWIA971343 1 19981222 A 2751 WARNING EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS ACTIVATED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 156CA 120156 AFTER TAKEOFF, CONTROL FAULT ILLUMINATED. QRH DID NOT CLEAR FAULT. RETURNED FOR LANDING AT SMF. OPERATED FLAPS UP AND DOWN COUPLE OF TIMES, NO DISCREPANCY NOTED. COULD NOT DUPLICATE PROBLEM. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800306 19990108 00306 SO 1999 1 8 SWIA971344 1 19981226 A 3010 DEICE BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE HORIZ STAB FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 195SW 120127 OUTBOARD STAB DEICE BOOTS FAILED ON TIMERS 1 AND 2 AND CYCLE LIGHT AND HEAVY. RETURNED TO SLC. REPLACED EJECTOR VALVE WITH A SERVICEABLE UNIT IAW MM 30-10-04, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800307 19990108 00307 SO 1999 1 8 SWIA971345 1 19981225 A 3230 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT MLG UPLOCK FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 199SW 120237 RETURNED TO AIRPORT. RIGHT MAIN GEAR WOULD NOT RETRACT, POSSIBLY JUST THE GEAR DOOR. REMOVED AND REPLACED UPLOCK ACTUA TOR AND SEQUENCING VALVES, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800308 19990108 00308 SO 1999 1 8 SWIA971346 1 19981223 A 3231 VALVE EMB 120 EMB120RT SO PWA 118 PW118A NE LT MLG DOOR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 LEFT MAIN GEAR UNSAFE IN UP POSITION AFTER TAKEOFF. CYCLING DID NOT CORRECT PROBLEM. OK WHEN GEAR DOWN. RETURNED TO M RY FOR LANDING. ADJUSTED LEFT INBOARD GEAR DOOR SOLENOID VALVE. CYCLED GEAR NUMEROUS TIMES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800309 19990108 00309 SO 1999 1 8 SWIA971347 1 19981225 A 3260 SWITCH EMB 120 EMB120RT SO PWA 118 PW118 NE LT MLG LOOSE A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 1117H 120117 AFTER GEAR RETRACTION, LEFT LOOP A GREEN LIGHT REMAINED ILLUMINATED. ATTEMPTED TO CYCLE GEAR AND GEAR WOULD NOT EXTEND. USED QRH GEAR ELECTRICAL OVERRIDE PROCEDURE TO EXTEND GEAR. RETURNED TO MFR. CLEANED AND ADJUSTED LOOSE PROXIMITY SW ITCH, SWUNG GEAR AND OPS CHECK GOOD IAW 32-00-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800310 19990108 00310 SO 1999 1 8 SWIA971348 1 19981228 A 3610 O RING EMB 120 EMB120RT SO PWA 118 PW118 NE LT ENG BLEED AIR FAILED A SWIA H A DEACTIVATE SYST/CIRCUITS UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 NM 07 156CA 120156 LEFT ENGINE DUCT LEAK LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF. COMPLIED WITH QRH AND RETURNED TO PSP AND CONTACTED MAIN TENANCE. FOUND O-RINGS WORN ON COUPLER SLEEVE CAUSING LEFT ENGINE BLEED AIR DUCT TUBE ASSEMBLY TO LEAK AT LEADING EDGE AND AT WING TO FUSELAGE. REMOVED AND REPLACED O-RING. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800311 19990108 00311 SO 1999 1 8 SWIA971349 1 19981228 A 3610 VALVE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENG BLEED AIR FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 190SW 120050 MIDDLE LEFT WING DEICE FAILS IN BOTH TIMER POSITIONS AND BOTH HEAVY AND LIGHT POSITIONS. RETURNED TO SLC. REMOVED AND REPLACED THE RIGHT BLEED AIR SHUT OFF VALVE IAW EMB 120 MM 36-10-00. RAN THE AIRCRAFT DEICE SYSTEM IN ALL CONFIGURATION S, CHECKS GOOD. ALSO, RAN WITH SHOP AIR FOR 45 MINUTES. SYSTEM OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800312 19990108 00312 NE 1999 1 8 SWIA971350 2 19981228 A 7310 FILTER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT ENGINE DIRTY A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 216SW 120285 RIGHT ENGINE FUEL FILTER LIGHT ILLUMINATED DURING FLIGHT. DIVERTED TO LAX. REPLACED RIGHT ENGINE FUEL FILTERS. RAN EN GINE AND OPS CHECKS GOOD. NO LEAKS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800313 19990108 00313 SO 1999 1 8 SWIA971351 1 19981225 A 7931 TRANSDUCER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 229SW 120305 LEFT OIL PRESSURE DROPPED TO APPROXIMATELY 50 PSI AND STAYED IN YELLOW ARC. DIVERTED FROM MRY TO SBA. REPLACED LEFT OI L PRESSURE TRANSDUCER. PERFORMED RUNS AT ALL POWER SETTINGS, OPS AND LEAK CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800314 19990108 00314 1999 1 8 SWIA971352 4 19981229 A 3425 PC2511C AHRS EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE NR 2 FAILED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 188SW 120039 NR 2 AHRS FAILED 20 MINUTES AFTER DEPARTURE. REINITIALIZED BEFORE LANDING. RETURNED TO SLC. REPLACED NR 1 INVERTER IA W MM 24-22-00, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800315 19990108 00315 1999 1 8 SWIA971353 4 19981223 A 2210 YAW DAMPER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 1 INOP A SWIA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 NM 07 408SW 7055 YAW DAMPER 1 IS INOP. RETURNED TO FIELD. REMOVED AND REPLACED R1 YAW DAMPENER LINEAR ACTUATOR. REPLACED FLIGHT CONTRO L PANEL, OPS CHECK OK FOR CAT II OPERATION. 2 L 7 2 4F 4 F RT A21EA E15NE 1999010800316 19990108 00316 SO 1999 1 8 SWIA971354 1 19981229 A 5610 WINDSHIELD EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT COCKPIT FAILED A SWIA K NONE O OTHER CR CRUISE 1 NM 07 563SW 120338 AT 23,000 FT COPILOT'S WINDSHIELD (OUTER PART) SHATTERED (NO IMPACT). LANDED IN ONT WITHOUT INCIDENT. REMOVED AND REPL ACED COPILOT'S WINDSHIELD TO MM 56-10-01, ALL CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800317 19990108 00317 NM 1999 1 8 VNAA9812011 1 19981219 A 7603 POWER LEVER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LEFT LACK OF LUBE A VNAA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 GL 07 433JS 3047 THE LEFT HAND POWER LEVER WOULD NOT ADVANCE PAST THE FLIGHT IDLE POSITION WHEN THE TAKEOFF WAS ATTEMPTED. THE TAKEOFF W AS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBRICATED THE LEFT HAND POWER LEVER FLIGH T IDLE DETENT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-11. FUNCTION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800318 19990108 00318 1999 1 8 VNAA9812012 4 19981217 A 2350 160PS01A5B SWITCH DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT COCKPIT FAILED A VNAA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 GL 07 429JS 3043 THE LEFT HAND PUSH TO TALK SWITCH FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSP ECTED AND REPLACED THE LEFT HAND PUSH TO TALK SWITCH, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 23-11-00. OPERATION AL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800319 19990108 00319 1999 1 8 VNAA9812015 4 19981224 A 3417 7014700911 ADC DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE E & E COMPT FAILED A VNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 07 438JS 88100 46191 3056 A RED O2 FAIL WARNING MESSAGE ILLUMINATED DURING THE FLIGHT. THE AIRCRAFT RETURNED TO DCA. OUTSTATION MAINTENANCE INSP ECTED THE OXYGEN SYSTEM IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-19-01. THE AIRCRAFT WAS RETURNED TO SERVICE. L ATER THAT DAY, THE WARNING MESSAGE OCCURRED AGAIN. MAINTENANCE INSPECTED AND REPLACED THE AIR DATA COMPUTER, IN ACCORDA NCE WITH DORNIER MAINTENANCE MANUAL 34-11-01. OPERATIONAL CHECKS, INCLUDING A FLIGHT CHECK WERE COMPLETED. THE RESULTS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800320 19990108 00320 NM 1999 1 8 VNAA9812014 1 19981225 A 2460 CIRCUIT BREAKER DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE COCKPIT TRIPPED A VNAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 GL 07 442JS 3060 A DC BUS TWO FAIL WARNING MESSAGE ILLUMINATED DURING THE FLIGHT. THE AIRCRAFT RETURNED TO PIT AND LANDED WITHOUT FURTHE R INCIDENT. MAINTENANCE INSPECTED AND RE-SET THE EXTERNAL POWER CIRCUT BREAKER, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-60-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800390 19990108 00390 WP 1999 1 8 9811119138 1 19981231 A 2130 SWITCH DOUG DC9 DC915 3022036 WP CABIN PRESS SYST FAILED A NWAA G O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 GL 01 9348 45787 AT APPROXIMATELY FLIGHT LEVEL 14,000 FEET, THE LEFT AND RIGHT AIR CONDITIONING SYSTEM PACKS TRIPPED OFF. AT FLIGHT LEVE L 17,000 FEET, THE PASSENGER OXYGEN MASKS DEPLOYED. THE FLIGHT CREW FOLLOWED COM PROCEDURES, RESET THE LEFT AND RIGHT A IR CONDITIONING PACK SYSTEMS, CONTINUED TO DESTINATION AT FLIGHT LEVEL 10,000, AND LANDED WITHOUT INCIDENT. MAINTENANC E REPLACED THE CABIN DIFFERENTIAL AND ALTITUDE WARNING SWITCHES AND PERFORMED A TEST OF THE CABIN PRESSURE CONTROL SYSTE M, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999010800401 19990108 00401 WP 1999 1 8 ABXA9801201 1 19981230 A 3260 INDICATION DOUG DC8 DC861 3021952 WP LANDING GEAR MALFUNCTIONED A ABXA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 848AX 46032 AFTER TAKEOFF ON GEAR RETRACTION, GEAR UNSAFE LIGHT REMAINED ILLUMINATED. RECYCLED GEAR, NO CHANGE. COMPLIED WITH GEAR UNSAFE PROCEDURES. THE LANDING AT SJC WAS UNEVENTFUL. PERFORMED PROXIMITY CONTROL BOX TEST. PERFORMED ADJUST/TEST IA W DC8 MM 32-60-0. COULD NOT REPEAT DISCREPANCY. OPS CHECKED GOOD. 2 L 7 4 4F 4A25 1999010800402 19990108 00402 WP 1999 1 8 ABXA9801202 1 19981222 A 5320 5956034517 FITTING DOUG DC9 DC931 3022065 WP BS 945 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND CRACKED FLOOR SUPPORT FITTING AT STATION 945 INBOARD OF LONGERON 27 RIGHT. REPLACED FITTING IAW D C9 SRM 51-30-5. 2 L 7 2 4F A6WE 1999010800403 19990108 00403 WP 1999 1 8 ABXA9801203 1 19981222 A 5315 9957870507 FLOORBEAM DOUG DOUG DC9 DC931 3022065 WP BS 218 CORRODED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND STATION 218 FLOORBEAM CORRODED AT BL 22 RIGHT. REPAIRED IAW ABX REA D953-25916. 2 L 7 2 4F A6WE 1999010800404 19990108 00404 WP 1999 1 8 ABXA9801204 1 19981222 A 5311 9919617502 FRAME DOUG DOUG DC9 DC931 3022065 WP BS 699 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 907AX 47203 DURING C-CHECK, FOUND FUSELAGE FRAME AT STATION 699 CRACKED AT LONGERON 16 RIGHT. REPLACED MAIN FRAME IAW DC9 SRM 53-13 -1. 2 L 7 2 4F A6WE 1999010800405 19990108 00405 NM 1999 1 8 MWEA99013 1 19981002 A 5753 5930476 SKIN DOUG MD88 MD88 3023688 NM RT TE FLAP CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 RIGHT OUTBOARD FLAP UPPER SKIN CRACKED AT STATION XOS 310. MTC REPAIRED USING BLIND FASTENERS. 2 L 7 2 4F RT A6WE 1999010800406 19990108 00406 NM 1999 1 8 MWEA99014 1 19980629 A 5511 5922575 SPAR WEB DOUG MD88 MD88 3023688 NM HORIZONTAL STAB CORRODED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 810ME 48072 THE RIGHT HORIZONTAL STABILIZER HAS CORROSION ON THE TRAILING EDGE SPAR WEB STATION XFS 1327 -- MTC. REMOVED CORROSIO N, FABRICATED DOUBLER AND INSTALLED REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 1999010800410 19990108 00410 NM 1999 1 8 VNAA9812021 1 19981222 A 3350 321473 POWER SUPPLY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7 & 9 FAILED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 441JS 80378 3059 THE EMERGENCY LIGHTS AT 9DF AND 7DF WERE NOTED TO BE INOPERATIVE, DURING THE PREFLIGHT INSPECTION. MAINTENANCE INSPECTE D AND REPLACED THE POWER SUPPLY AT THE 5LK POSITION. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED T O SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800411 19990108 00411 NM 1999 1 8 VNAA9812018 1 19981231 A 3060 BRUSH BLOCK DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT PROPELLER DIRTY A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 461PS 3075 THE FLIGHT RETURNED TO THE GATE AFTER RECEIVING A LEFT HAND PROPELLER HEAT FAIL WARNING MESSAGE. MAINTENANCE INSPECTED AND CLEANED THE LEFT HAND PROPELLER BRUSH BLOCK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 30-61-05. OPERATIONAL CH ECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800412 19990108 00412 NM 1999 1 8 VNAA9812019 1 19981228 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 5LK DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 328JS 53621 4755 3030 DURING THE PREFLIGHT INSPECTION, EMERGENCY LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE BATTERY PACK AT POSITION 5LK. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800413 19990108 00413 NM 1999 1 8 VNAA9812020 1 19981225 A 3350 321430 BATTERY DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE ROW 7LK DISCHARGED A VNAA K NONE L NO TEST IN INSP/MAINT 1 GL 07 458PS 49994 4469 3068 DURING THE PREFLIGHT INSPECTION, SOME EMERGENCY LIGHTS AT THE REAR OF THE AIRCRAFT WERE NOTED TO BE INOPERATIVE. MAINTE NANCE INSPECTED AND REPLACED THE BATTERY PACK AT POSITION 7LK. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1999010800414 19990108 00414 EU 1999 1 8 RAIA981202 1 19981205 A 5210 91SE3 SWITCH BAG JETSTM JETSTM3201 1500217 EU PASSENGER DOOR MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 340TE 939 FLT 7416 - STL - PASSENGER DOOR LIGHT CAME ON IN FLIGHT. MAINTENANCE ADJUSTED PAX DOOR MICRO SWITCH. (M) 2 L 7 2 4T RT A56EU 1999010800415 19990108 00415 WP 1999 1 8 RAIA981121 2 19981123 A 7314 8974007 FUEL PUMP BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 341TE 11291 950 66176 FLT 7468 - STL - RIGHT ENGINE DID NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED RIGHT ENGINE FUEL PUMP. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999010800416 19990108 00416 EU 1999 1 8 RAIA981120 1 19981123 A 3060 B4024555 DEICE BOOT BAG JETSTM JETSTM3201 1500217 EU RIGHT PROP FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 875JX 875 FLT 7069 - STL - RIGHT PROP HEAT INOP. MAINTENANCE REPLACED DEICE BOOT ON RIGHT PROP. (M) 2 L 7 2 4T RT A56EU 1999010800417 19990108 00417 EU 1999 1 8 REXA98116 1 19981129 A 2612 FIRE LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A REXA O OTHER N FALSE WARNING CR CRUISE 1 SO 25 111PX 340A024 RIGHT FIRE WARNING ILLUMINATED CWP AND HANDLE. BEGAN SHUT DOWN PROCEDURES, RETARDED POWER LEVER AND LIGHT WENT OUT. FO UND FIRE LOOP ON RIGHT ENGINE COMING IN CONTACT WITH ENGINE HOT SECTION. RE-ROUTED FIRE LOOP, OPS CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999010800418 19990108 00418 NE 1999 1 8 PLGA981122A 2 19981122 A 7210 6044T35P10 PGB SAAB SF340 340B 7860101 EU GE CT7TP CT79B 30030 NE RT ENGINE MALFUNCTIONED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 364BE UDAG0505 340B294 785168 ALB - FLT 4380 - WHILE EN ROUTE TO ALB, THE RIGHT ENGINE PROPELLER GEAR BOX (PGB) OIL PRESSURE STARTED TO FLUCTUATE AND THE OIL TEMPERATURE STARTED TO INCREASE. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT CONTINUED T O ALB AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT PGB. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999010800419 19990108 00419 EU 1999 1 8 PLGA981116A 1 19981116 A 7930 IPTESS1000200D TRANSDUCER SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE FLUCTUATES A PLGA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 744BA 2807229107 340A105 BOS - FLT 4323 - ON CLIMB-OUT, THE LEFT ENGINE OIL PRESSURE STARTED TO FLUCTUATE BETWEEN 75 AND 125 PSI. AIRCRAFT RETUR NED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLAFED THE LEFT OIL PRESSURE TRANSDUCER. SYSTEM TESTED GOOD. (M ) 2 L 7 2 4T 4 T RT A52EU E8NE 1999010800421 19990108 00421 NM 1999 1 8 TSAA9833613 1 19981207 A 3350 86210151 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED POWER PACK FOR FORWARD CONTROLLER DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800422 19990108 00422 NM 1999 1 8 TSAA9833614 1 19981207 A 3350 86210151 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED BOTH BATTERY PACKS FOR EMEGNECY PACKS 1 AND 2 DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800423 19990108 00423 NM 1999 1 8 TSAA9833615 1 19981207 A 3350 9221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER EMERGENCY LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800424 19990108 00424 NM 1999 1 8 TSAA9833616 1 19981208 A 3350 6013211 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED LEFT OVERWING SLIDE LIGHT DUE TO INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800425 19990108 00425 NM 1999 1 8 TSAA9833617 1 19981209 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED NR 4 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800426 19990108 00426 NM 1999 1 8 TSAA9833618 1 19981209 A 3350 8731002511 LIGHT BOEING 737 7372Q9 138448M NM CABIN INOP A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY IDENT L IGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800427 19990108 00427 NM 1999 1 8 TSAA9833619 1 19981209 A 3350 9221009 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 FORWARD ENTRY DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REMOVED AND REPLACED FORWARD ENTRY DOOR EMERGENCY IDENT B ATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800428 19990108 00428 NM 1999 1 8 TSAA9833620 1 19981210 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 NR 1 AND NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK INOP. REMOVED AND REPLACED NR 1 AND NR 6 EMERGENCY FLOOR BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800429 19990108 00429 NM 1999 1 8 TSAA9833621 1 19981210 A 3350 900542 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED FORWARD EMERGENCY CENTER OVERHEAD EXIT SIGN BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999010800430 19990108 00430 NM 1999 1 8 TSAA9833622 1 19981211 A 3350 9221009 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 LEFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F A16WE 1999010800431 19990108 00431 NM 1999 1 8 TSAA9833623 1 19981211 A 3350 9221009 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER ASSY INOP. REPLACED ASSY BATTERY PACK, OPS CHECK OK. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800432 19990108 00432 NM 1999 1 8 TSAA9833624 1 19981211 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 REPLACED NR 1 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800433 19990108 00433 NM 1999 1 8 TSAA9833625 1 19981211 A 3350 9221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED LEFT OVERWING BATTERY FOR EMERGENCY EXIT LIGHT IDENTIFIER ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED T O SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800434 19990108 00434 NM 1999 1 8 TSAA9833626 1 19981211 A 3350 8731002511 LIGHT BOEING 737 737230C 1384472 NM CABIN INOP A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT IDENTIFIER ASSY INOP. REPLACED IDENTIFIER LIGHT ASSY, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800435 19990108 00435 NM 1999 1 8 TSAA9833627 1 19981212 A 3350 1000679 LIGHT BOEING 737 7372S5C 1384499 NM CABIN INOP A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED FORWARD SERVICE DOOR OVERHEAD EMERGENCY LIGHT ASSY DUE TO BEING INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999010800436 19990108 00436 NM 1999 1 8 TSAA9833628 1 19981212 A 3350 9221009 BATTERY PACK BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 LEFT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT ASSY INOP. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SER VICE. (M) 2 L 7 2 4F A16WE 1999010800437 19990108 00437 NM 1999 1 8 TSAA9833629 1 19981213 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED NR 5 EMERGENCY BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800438 19990108 00438 NM 1999 1 8 TSAA9833632 1 19981214 A 3350 86210066 BATTERY PACK BOEING 737 7372M6C 1384708 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805AL 21809 NR 2 SEAT EMERGENCY LIGHT ASSY BATTERY INOPERATIVE. REMOVED AND REPLACED NR 2 SEAT EMERGENCY LIGHT BATTERY PACK, OPS CH ECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800439 19990108 00439 NM 1999 1 8 TSAA9833630 1 19981124 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED FORWARD ENTRY DOOR EXIT IDENTIFIER BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F A16WE 1999010800440 19990108 00440 NM 1999 1 8 TSAA9833631 1 19981124 A 3350 86210066 BATTERY PACK BOEING 737 7372T4 1384492 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED LEFT OVERWING EMERGENCY LIGHT BATTERY PACK DUE TO BEING INOP. OPS CHECKED OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800441 19990108 00441 NM 1999 1 8 P2EA98302 1 19981118 A 5320 WEB BOEING 737 737281 138448P NM BS 232/257 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - WEB CRACKED AT BS 253, LBL 8 INCHES DEFECT SIZE, LENGTH .375 INCH. REPAIRED FUSELAGE WEB SECTION BETWEEN BS 232 A ND BS 257, WL 190 FROM BL 0 TO LBL 18 INCHES PER COOPESA EO COO-3-53-717-98 DATED DEC 2, 1998 AND BOEING FAX COO-SJO 98- 1021RR DATED DEC 1, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1999010800442 19990108 00442 NM 1999 1 8 P2EA98301 1 19981119 A 5347 SEAT TRACK BOEING 737 737281 138448P NM BS 709 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - SEAT TRACK CRACKED AT BS 709, RBL 25 INCHES, WL 203.1, DEFECT SIZE LENGTH .625 INCH. REPAIRED FLOORBEAM SECTION F ROM BS 698 AND BS 717, RBL 25 INCHES PER BOEING SERVICE BULLETIN 737-57-1210 DATED APRIL 4, 1991 SECTION III FIG 5 AND B OEING FAX COO-SJO-98-09933RR DATED NOV 25, 1998. (M) 2 L 7 2 4F A16WE 1999010800443 19990108 00443 NM 1999 1 8 P2EA98300 1 19981118 A 5311 65528735 FRAME BOEING 737 737281 138448P NM BS 949 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - AFT ENTRY DOOR LOWER PAN SECTION CRACKED. DEFECT SIZE LENGTH 1.125 INCH. REPLACED AFT ENTRY DOOR FRAME AT BS 949 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010800444 19990108 00444 NM 1999 1 8 P2EA98299 1 19981119 A 5347 SEAT TRACK BOEING 737 737281 138448P NM BS 663-690 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - SEAT TRACK LOWER CHORD CRACKED AT FROM BS 663.75 TO BS 690 AT RBL 24.5, DEFECT SIZE LENGTH .563. REPAIRED FLOORBE AM UPPER CHORD BETWEEN BS 660 AND BS 682, LBL 24.82 PER BOEING INSTRUCTION LIST OF DATE INCLUDED ON FAA FOR 8110-3 AND C OOPESA EO COO-3-57-696-98 DATED NOV 26, 1998. (M) 2 L 7 2 4F A16WE 1999010800445 19990108 00445 NM 1999 1 8 P2EA98298 1 19981127 A 5755 SPOILER BOEING 737 737281 138448P NM NR 8 DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US MA1211 20414 SJO - NR 8 SPOILER DELAMINATED, DEFECT SIZE TOTAL 320 SQ IN. REPAIRED NR 8 SPOILER PER COOPESA EO C00-3-57-713-98 DATED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1999010800446 19990108 00446 NM 1999 1 8 P2EA98297 1 19981118 A 5230 SKIN BOEING 737 737281 138448P NM CARGO DOOR CANNING A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - AFT CARGO DOOR DENTED AND OL CANNED, DEFECT SIZE WIDTH 2.125 INCH DEPTH .060. REPLACED AFT CARGO DOOR OUTER SKIN BETWEEN BS 839 AND BS 887 PER SRM 51-10-1 PAGE 5 AND 51-20-2. (M) 2 L 7 2 4F A16WE 1999010800447 19990108 00447 NM 1999 1 8 P2EA98296 1 19981201 A 5755 6546422194 SLAT BOEING 737 737281 138448P NM NR 5 DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 25 20414 SJO - NR 5 SLAT DELAMINATED, DEFECT SIZE TOTAL 400 SQ INCH. REPAIRED NR 5 SLAT PER COOPESA EO COO-3-57-719-98 DATED DEC 2, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1999010800448 19990108 00448 NM 1999 1 8 P2EA98295 1 19981127 A 5755 654645123 SPOILER BOEING 737 737281 138448P NM NR 6 DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US MA645 20414 SJO - NR 6 SPOILER DELAMINATED, DEFECT SIZE TOTAL 160 SQ INCH. REPAIRED NR 6 SPOILER PER COOPESA EO COO-3-57-712-98 DAT ED NOV 30, 1998. DOCUMENTED ON FAA FORM 8110-3. (M) 2 L 7 2 4F A16WE 1999010800449 19990108 00449 NM 1999 1 8 P2EA98294 1 19981122 A 5330 SKIN BOEING 737 737281 138448P NM BS 172 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FUSELAGE SKIN DOUBLER MISSING MATERIAL AT BS 178, WL 243, BETWEEN LBL 2 INCH AND LBL 7 INCH. REPLACED WINDOW CENT ER POST DOUBLER AT BS 178, SL 243, BETWEEN LBL 7 INCH AND RBL PER BOEING SERVICE BULLETIN 737-53-1059 REV 1, SECTION III , FIG 2 DATED MAY 17, 1990. (M) 2 L 7 2 4F A16WE 1999010800450 19990108 00450 NM 1999 1 8 P2EA98293 1 19981120 A 5313 STRINGER BOEING 737 737281 138448P NM BS 727 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FOUND CORROSION AT BS 727A, STRINGER 22 LEFT, LOWER CHORD, DEFECT SIZE LENGTH 2.5 INCH WIDTH 1 INCH. REPAIRED FUS ELAGE SKIN SECTION FROM BS 727 PLUS 11 INCH AND BS 727A PLUS 8 INCH, BETWEEN STRINGER 21 LEFT AND STRINGER 23 LEFT PER S RM 53-30-3, FIG 6. (M) 2 L 7 2 4F A16WE 1999010800451 19990108 00451 NM 1999 1 8 P2EA98292 1 19981118 A 5313 STRINGER BOEING 737 737281 138448P NM BS 727 CORRODED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - STRINGER 22 LEFT CORRODED BETWEEN BS 727 AND BS 727A, DEFECT SIZE LENGTH 3 INCH WIDTH .75 INCH. REPAIRED STRINGER 22 LEFT BETWEEN BS 727 AND BS 727A PLUS 13 INCHS PER SRM 53-10-3 FIG 1, SHEET 7. (M) 2 L 7 2 4F A16WE 1999010800452 19990108 00452 NM 1999 1 8 P2EA98291 1 19981119 A 5320 65479952 ANGLE BOEING 737 737281 138448P NM BS 559 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - ANGLE CRACKED AT BS 559, RBL 46, WL 205 DEFECT SIZE LENGTH .4375. REPLACED FUSELAGE LOWER CHORD AT BS 559, WL 204 , BETWEEN RBL 46 INCHES AND RBL 70 INCHES PER BOEING SERVICE BULLETIN 737-53-1061, REV 4, SECTION 111 FIG 2 DATED JULY 1 6, 1992. (M) 2 L 7 2 4F A16WE 1999010800453 19990108 00453 NM 1999 1 8 P2EA98290 1 19981119 A 5315 FLOORBEAM BOEING 737 737281 138448P NM BS 578 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FLOORBEAM CRACKED AT BS 578, RBL 50, WL 206, DEFECT SIZE .5 INCH. REPAIRED FLOORBEAM WEB AT BS 578, BETWEEN RBL 4 5 INCHES TO RBL 70 INCHES, FROM WL 208 TO WL 204 PER SRM 51-30-2 AND 51-10-1 PAGE 5. (M) 2 L 7 2 4F A16WE 1999010800454 19990108 00454 NM 1999 1 8 P2EA98289 1 19981117 A 5313 STRINGER BOEING 737 737281 138448P NM BS 294 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - STRINGER 10 LEFT CRACKED AT BS 294.5 DEFECT SIZE LENGTH .625 INCH. REPAIRED FUSELAGE STRINGER 10 LEFT, FROM BS 27 5 TO BS 301 PER SRM 53-10-3, FIG 3. (M) 2 L 7 2 4F A16WE 1999010800455 19990108 00455 NM 1999 1 8 P2EA98288 1 19981118 A 5330 SKIN BOEING 737 737281 138448P NM BS 939-952 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - INTERNAL DOUBLER CRACKED AT THE AFT SERVICE DOORWAY LOWER HINGE CUTOUT, DEFECT SIZE LENGTH .75 INCH. REPAIRED FUS ELAGE SKIN SECTION FROM BS 939 TO BS 953, BETWEEN STRINGER 13 RT AND STRINGER 14 RT PER COOPESA EO COO-3-53-715-98 DATED DEC 2, 1998 AND BOEING FAX COO-SJO-98-1023RR DATED DEC 1, 1998. (M) 2 L 7 2 4F A16WE 1999010800456 19990108 00456 NM 1999 1 8 P2EA98287 1 19981117 A 5320 65C3176613 FITTING BOEING 737 737281 138448P NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - VERTICAL BEAM CRACKED AT BS 727, BETWEEN WL 208.5 AND WL 198.5 IN BL 0 INCH. DEFECT SIZE LENGTH 4 INCH. REPLACED FUSELAGE BULKHEAD PRESS UPPER FITTING AT BS 727, BL 0, BETWEEN WL 207 AND WL 198 PER BOEING SERVICE BULLETIN 737-53-110 1, REV 2, SECTION III FIG 4, DATED NOV 30, 1995. (M) 2 L 7 2 4F A16WE 1999010800457 19990108 00457 NM 1999 1 8 P2EA98286 1 19981117 A 5100 65475056 STIFFENER BOEING 737 737281 138448P NM HORIZONTAL STAB CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - RIGHT HORIZONTAL STAB, STAB STATION 101.9, NR 4 STIFFENER LOWER CHORD CRACKED. DEFECT SIZE LENGTH 1.75 INCH. REP LACED STAB CHORD AT STAB STATION 101.9, BETWEEN FRONT AND REAR SPAR PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010800458 19990108 00458 NM 1999 1 8 P2EA98285 1 19981117 A 5312 WEB BOEING 737 737281 138448P NM BS 178 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FUSELAGE BULKHEAD SKIN CRACKED AT BS 178, WL 219, RBL 15 INCH, DEFECT SIZE LENGTH 7 INCH. REPAIRED FUSELAGE WEB S ECTION AT BS 178, FROM WL 210 TO WL 234, BETWEEN RBL 1.5 AND RBL 18 INCH PER SRM 53-10-11, FIG 1 SHEET 6, DETAIL III. ( M) 2 L 7 2 4F A16WE 1999010800459 19990108 00459 NM 1999 1 8 P2EA98281 1 19981118 A 5311 FRAME BOEING 737 737281 138448P NM BS 578 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - FRAME CRACKED AT BS 578, WL 207, LBL 65, DEFECT SIZE LENGTH 5 INCH. REPLACED FUSELAGE FRAME SECTION AT BS 578, BE TWEEN STRINGER 12 LEFT AND STRINGER 18 LEFT PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999010800460 19990108 00460 NM 1999 1 8 P2EA98280 1 19981119 A 5720 WEB BOEING 737 737281 138448P NM BS 663 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - WEB CRACKED AT BS 663.75, RBL 0, WL 206. DEFECT SIZE LENGTH 1.5 INCH. REPAIRED CENTER WING BOX, FLOORBEAM UPPER CHORD BETWEEN BS 650 AND BS 675, BL 0 PER BOEING SERVICE BULLETIN 737-57-1210 DATED APRIL 4, 1991, SECTION III FIG 4. ( M) 2 L 7 2 4F A16WE 1999010800461 19990108 00461 NM 1999 1 8 MZZA98213 1 19981006 A 5320 WEB BOEING 727 727277 138408S NM BS 1303/1313 CANNING A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 626DH 22644 TNN - DURING 1/2D CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, OIL CANNING WAS FOUND ON LEFT SIDE AFT AIRSTAIR TORQUE BOX V ERTICAL WEB BETWEEN BS 1303 AND BS 1313. THE AFT AIRSTAIR TORQUE BOX WEB OIL CANNING AREAS WAS INSTALLED REINFORCEMENT STIFFENER ANGLE PER B727 SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999010800462 19990108 00462 EA 1999 1 8 MASA98213 1 19981130 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA EMERGENCY LIGHT LOOSE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17217 7217 FLT 5803 - MKE-PHL - CREW REPORTED RIGHT FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENACE ACTION WAS DEFERRED PER MEL 33 -51-2. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, FOUND THE BULB LOOSE, RESEATED THE BULB. (M) 2 L 7 2 4F RT A21EA 1999010800463 19990108 00463 NM 1999 1 8 MASA98223 1 19981215 A 3350 OL3071BPE BULB GRIMES 1014021 DHAV DHC8 DHC8202 2809007 NM PASSENGER DOOR FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 446YV 446 DURING A ROUTINE LINE CHECK INSPECTIN, MAINTENANCE PERSONNEL FOUND THE PASSENGER DOOR OVERHEAD EXIT SIGN WITH SEVERAL BU LBS INOP. MAINTENANCE REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD. (M) 2 H 7 2 4T RT A13NM 1999010800464 19990108 00464 NM 1999 1 8 MASA98211 1 19981127 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ROW 1-6 INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 FLT 6362 - PHX - CREW REPORTED EMERGENCY LIGHTS INOP FROM THE FLIGHT ATTENDANTES STATION. AFTER TROUBLESHOOTING, MAINTE NANCE REMOVED AND REPLACED THE POWER SUPPLIES. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999010800465 19990108 00465 NM 1999 1 8 MASA98222 1 19981210 A 3350 MS25231316 BULB DHAV DHC8 DHC8202 2809007 NM CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 FLT 6230 - PHX-MTJ - PRIOR TO DEPARTURE, CREW REPORTED TWO OVERHEAD EMRGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLA CED THE BULBS. OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999010800466 19990108 00466 NM 1999 1 8 MASA98217 1 19981201 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM ROW 1-6 INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 437YV 437 DURING A ROUTINE SERVICE CHECK, MAINTENANCE PERSONNEL FOUND THE EMERGENCY EXIT LIGHTS EXTINGUISHING IMMEDIATELY AFTER BE ING TURNED ON. MAINTENANCE REMOVED AND REPLACED ALL SIX EMERGENCY POWER SUPPLIES, OPS CHECKED GOOD. AIRCRAFT WAS RETUR NED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999010800467 19990108 00467 SO 1999 1 8 C2XA98IA468 1 19981119 A 3350 12021299001 LIGHT EMB 120 EMB120RT SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 16723 120169 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT CIRCUIT BREAKER WAS POPPED AND WOULD NOT RESET. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT AND RIGHT LOWER AFT EXTERNAL EMERGENCY LIGHTS TO BE GROUND ED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLIES AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999010800469 19990108 00469 NE 1999 1 8 C2XA98BT082 2 19981103 A 7320 7863927 ECI AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE FAILED A C2XA E ENGINE SHUTDOWN X Z O ENGINE FLAMEOUT SIGNIFICANT FAILURE REPORT OTHER AP APPROACH 1 SW 09 97841 280 120353 TEST FLIGHT NR 2 ENGINE, ECU PROBLEM. NR 2 ENGINE SHUTDOWN ON APPROACH. REMOVED AND REPLACED NR 2 ECU AND NH SENSOR. T EST FLOWN SATISFACTORY. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999010800470 19990108 00470 NM 1999 1 8 USAA980625 1 19981202 A 5330 SKIN BOEING 737 737201 1384454 NM BS 754 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 228US 51175 21817 TPA - DURING CX-2 CHECK VISUAL INSPECTION, FOUND A 1.1 INCH CRACK IN EXTERNAL SKIN .5 INCH ABOVE STRINGER 18R AT STATION 754 SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999010800471 19990108 00471 NM 1999 1 8 USAA980615 1 19981113 A 5330 SKIN BOEING 737 737201 1384454 NM BS 360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 255AU 42324 22797 CLT - DURING CX-4 VISUAL INSPECTION, FOUND A .4375 INCH CRACK AFT OF EQUIPMENT COOLING OUTLET STATION 360 AT WL 148.5 SK IN. INSTALLED DOUBLER PER TR 53-30-04. (M) 2 L 7 2 4F A16WE 1999010800472 19990108 00472 NM 1999 1 8 USAA980626 1 19981207 A 5330 SKIN BOEING 737 737201 1384454 NM BS 952-967 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 43746 22753 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND A 2.875 INCH CRACK BETWEEN STATION 952 AND 967 STRINGER 21L SKIN. FABR ICATED FILLER AND DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999010800473 19990108 00473 NM 1999 1 8 USAASB98321 1 19981210 A 7930 1163P181 SWITCH BOEING 737 737201 1384454 NM NR 1 ENGINE FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 EA 19 261AU 9071 22867 CLE - FLT 691 - APPROX 50 MILES OUT FROM CLE, THE NR 1 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. CAPTAIN WENT THROUGH PROCEDURES, THEN SHUT DOWN THE NR 1 ENGINE IN FLIGHT. AN EMERGENCY WAS DECLARED. FLIGHT LANDED WITHOUT INCIDENT AT CL E. TOTAL SINGLE TIME WAS 12 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE MAIN OIL FILTER. INSPECTED REMO VED FILTER AND FOUND NO CONTAMINANTS. REMOVED AND REPLACED THE NR 1 ENGINE OIL FILTER BYPASS SWITCH. RAN ENGINE. LEAK CHECK GOOD. OPS CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999010800474 19990108 00474 NM 1999 1 8 USAASB98323 1 19981210 A 2420 GCU BOEING 737 737401 1384701 NM NR 2 ENGINE MALFUNCTIONED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 419US 23986 JAX - FLT 820 - DURING CRUISE, THE APU GENERATOR QUIT AND THE NR 2 ENGINE GENERATOR WAS ALREADY ON MEL. DECISION WAS MA DE TO DIVERT TO JAX SINCE THE AIRCRAFT WAS DOWN TO ONE ELECTRICAL SOURCE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO E MERGENCY WAS DECLARED. REPLACED NR 2 GENERATOR CONTROL UNIT, AS OF 12/16/98. SYSTEM IS BACK ON MEL. (M) 2 L 7 2 4F RT A16WE 1999010800475 19990108 00475 NM 1999 1 8 USAASB98327 1 19981213 A 3350 20131ALP BATTERY PACK BOEING 737 7374B7 1384702 NM FUSELAGE DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 785AU 25024 PHL - MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010800476 19990108 00476 NM 1999 1 8 99ZZZM1 1 19981213 A 3350 20121 CHARGER ASSY BOEING 737 7374B7 1384702 NM FUSELAGE INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 785AU 25024 PHL - MAINTENANCE FOUND THE LEFT AND RIGHT OVERWING EMERGENCY LIGHTS INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010800477 19990108 00477 NM 1999 1 8 USAA129806 1 19981217 A 3250 PULLEY BOEING 727 727254 138408L NM NLG STEERING JAMMED A USAA O OTHER O OTHER TX TAXI/GRND HDL 1 EA 19 914TS 20251 FLT 6531 - LGA-DCA - AFTER LANDING NOSE STEERING INOPERATIVE FOR RIGHT TURNS. CONTROL STEERING TILLER BINDING WHEN TURN ED TO RIGHT, TOWED AIRCRAFT FROM RUNWAY. CHECKED AND LUBED RUDDER STEERING SYSTEM, CHECKED STEERING CABLES AND PULLEYS FOUND PULLEY ON LEFT SIDE OF NOSE GEAR JAMMED WITH DIRT AND SAND CLEANED AND LUBED NOSE STEERING SYSTEM. OPERATIONAL CH ECK NORMAL PER MM 32-56-0. (M) 2 L 7 3 4F A3WE 1999010800478 19990108 00478 NM 1999 1 8 ASAA9840106 1 19981110 A 2530 8609020000 OVEN BOEING 737 7374Q8 NM GALLEY MALFUNCTIONED A ASAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 01 773AS 18937 454 25106 OAK - DURING FLT 528 - FLIGHT ATTENDANT REPORTED THAT ALL AFT GALLEY LIGHTS WERE FLICKERING AND AN ELECTRICAL ODOR WAS P RESENT. AIRCRAFT DIVERTED TO OAK FOR INSPECTION. MAINTENANCE COULD NOT DUPLICATE FLICKERING LIGHTS AND NO ELECTRICAL O DOR OR SMOKE WAS PRESENT. AS A PRECAUTIONARY MEASURE, MAINTENANCE PULLED AND COLLARED THE AFT GALLEY OVEN CIRCUIT BREAK ERS AND DEFERRED AS PASSENGER CONVENIENCE ITEM. PDX MAINTENANCE RAN OVEN ON HIGH FOR 30 MINUTES AND FOUND A GREY/BLACK SMOKE COMING FROM BOTH SIDES OF THE DUAL BAY OVEN. REPLACED OVEN, OPERATED NORMALLY. THE OVEN WAS SUBSEQUENTLY ROUTED TO THE ALASKA AIRLINES AVIONICS SHOP IN SEA WHERE IT WAS CLEANED AND TESTED. UPON TESTING, THE OVEN OPERATED NORMALLY W 2 L 7 2 4F RT A16WE 1999010800479 19990108 00479 NM 1999 1 8 ASAA9810124 1 19981203 A 3350 8821004 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 740AS 22578 ANC - DURING MAINTENANCE CHECK, THE FORWARD SECTION OF EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. R EPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999010800480 19990108 00480 NM 1999 1 8 ASAA9810123 1 19981202 A 3350 S283T0143 BATTERY PACK BOEING 737 7372X6C 1384552 NM R1 DOOR DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - DURING FLIGHT, THE EMERGENCY EXIT LIGHT AT THE R1 DOOR INOPERATIVE. COULD NOT DUPLICATE. REPLACED BATTERY PACK A S PRECAUTIONARY AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999010800481 19990108 00481 NM 1999 1 8 ASAA9810122 1 19981127 A 3350 8100022607 LIGHT BOEING 737 7372X6C 1384552 NM ROW 8 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 746AS 23123 ANC - PRIOR TO FLIGHT 1271 - ONE EMERGENCY EXIT TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 8. RELAMPED, NO HELP. R ELEASED PER MEL 33-19. SUBSEQUENTLY REPLACED LAMP ASSEMBLY AND LIGHT OPERTED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999010800482 19990108 00482 NM 1999 1 8 ASAA9810121 1 19981126 A 3350 8100022607 LIGHT BOEING 737 737210C 1384459 NM ROW 18 INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, AN EMERGENCY EXIT FLOOR TRACK LIGHT WAS FOUND TO BE INOPERATIVE AT ROW 18. REPLACED THE LIGHT ASSEMBLY AND THE LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999010800483 19990108 00483 WP 1999 1 8 ASAA9880259 1 19981209 A 5210 HOLD OPEN HOOK DOUG DC9 DC982 3022082 WP L1 DOOR MALFUNCTIONED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 935AS 49236 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WAS DIFFICULT TO UNLATCH FROM THE FULL OPEN POSITION. ADJUSTED THE DOOR HOL D OPEN MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999010800484 19990108 00484 NM 1999 1 8 ASAA9840112 1 19981208 A 5210 CLIP BOEING 737 7374Q8 NM L1 DOOR MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 775AS 25108 OAK - PRIOR TO FLIGHT 493 - THE L-1 DOOR WAS FOUND TO BE DIFFICULT TO OPEN. FOUND RETAINER CLIP MISSING FROM PIN ON THE UPPER HINGE CAUSING INTERFERENCE. REPLACED MISSING RETAINER CLIP AND DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999010800485 19990108 00485 WP 1999 1 8 ORJA98311 1 19981212 A 3246 LM124448 BEARING DOUG DC9 DC982 3022082 WP NR 1 MLG FAILED A ORJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 821RA 49931 IN ORD - ABORTED TAKEOFF, WHEEL NOT TURNING LIGHT CAME ON AT BEGINNING OF TAKEOFF. REMOVED AND REPLACED NR 1 MLG TRANSD UCER ASSY AND HUB CAP, OPS CHECK OK. UPON FURTHER INVESTIGATION MAINTENANCE DISCOVERED THE INNER WHEEL BEARING WAS OF T HE WRONG TYPE FOR THE WHEEL ASSY. MAINTENANCE REMOVED AND REPLACED THE TIRE ASSY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999010800486 19990108 00486 WP 1999 1 8 ORJA98313 1 19981213 A 3350 59306431 BATTERY DOUG DC9 DC983 3022083 WP PASSENGER DOOR DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 IN LAS - EMERGENCY EXIT LIGHTING ILLUMINATED IN FLIGHT. REMOVED AND REPLACED BATTERY AT FORWARD DOOR, OPS CHECK OK. (M ) 2 L 7 2 4F RT A6WE 1999010800487 19990108 00487 WP 1999 1 8 ORJA98312 1 19981211 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP GALLEY DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 IN LAS - EMERGENCY EVAC LIGHTS ALONG FORWARD GALLEY WALL AND FIRST 2 ROWS OF FIRST CLASS ILLUMINATED IN FLIGHT UNABLE TO EXTINGUISHED WITH COCKPIT SWITCH PLACED TO OPP OR ARM. REMOVED AND REPLACED FORWARD LEFT BATTERY PACK EMERGENCY LIGHT SYSTEM, OPS CHECK GOOD PER MM 33-00. (M) 2 L 7 2 4F RT A6WE 1999010800488 19990108 00488 NM 1999 1 8 TSAA9833609 1 19981203 A 3350 8732030103 CONTROL MODULE BOEING 737 737230C 1384472 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 CENTER EMERGENCY EXIT CONTROL MODULE ASSY INOP. REPLACED CENTER EMERGENCY EXIT CONTROL MODULE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800489 19990108 00489 NM 1999 1 8 TSAA9833610 1 19981202 A 3350 900542 BATTERY BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED THE INTERIOR OVERWING EMERGENCY IDENTIFIER BATTERY PACK ASSEMLBY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999010800490 19990108 00490 NM 1999 1 8 TSAA9833611 1 19981204 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 NR 5 SEAT EMERGENCY LIGHT ASSEMBLY BATTERY INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999010800491 19990108 00491 NM 1999 1 8 TSAA9833612 1 19981204 A 3350 86210066 BATTERY BOEING 737 7372Q9 138448M NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 804AL 21719 NR 4 EMERGENCY FLOOR BATTERY PACK INOP. REPLACED BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999010800492 19990108 00492 SW 1999 1 8 99ZZZM2 1 19981207 A 3250 WIRE SWRNGN SA227 SA227AC 8780603 SW NLG STEERING BROKEN A MEJA O OTHER O OTHER LD LANDING 1 SW 17 3114G AC583 UPON LANDING ROLLOUT AT SLU, A/C BEGAN DRIFTING TO THE RT, WITH THE NOSE WHEEL STEERING ARMED. THE PILOT MAINTAINED THE RUNWAY CENTERLINE WITH THE RUDDER BUT AS THE A/C SLOWED, THE RUDDER BECAME LESS EFFECTIVE AND NOSEWHEEL STEERING STILL DID NOT RESPOND. PILOT APPLIED DIFFERENTIAL POWER AND BRAKES BUT THEIR EFFECTIVENESS WAS REDUCED DUE TO WET RUNWAY. PI LOT APPLIED FULL REVERSE TO AVOID IMPACTING THE RUNWAY LIGHTS AND FENCE. THE A/C CAME TO A FULL STOP APPROX 4 FT OFF RU NWAY. MX DID VISUAL INSPECT OF L/G, WHEELS, BRAKES, AND PROPELLERS AND NO DAMAGE TO A/C FOUND. MX DEFERRED NOSE WHEEL STEERING AND A/C WAS FERRIED TO SJU FOR FURTHER MX. MX AT SJU PERFORMED GEAR SWING RETRACTION AND THE OPS CHECK WAS GOO 2 L 7 2 4T RT A8SW 1999010800493 19990108 00493 SW 1999 1 8 99ZZZM3 1 19981202 A 3233 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW LT MLG OUT OF ADJUST A MEJA O OTHER J WARNING INDICATION AP APPROACH 1 SW 17 446MA AC693 AFTER TAKEOFF FROM ANC, THE GEAR WERE SLOW TO RETRACT AND THE RIGHT MAIN GEAR INDICATED UNSAFE. AFTER CYCLING THE GEAR TWICE MORE, THE GEAR STILL INDICATED UNSAFE. THE A/C RETURNED TO ANC. MX INSPECTED AND CLEANDD THE DOWN SUPPLY LINE AN D REPLACED MAIN HYDRAULIC FILTER. THE GEAR WAS CYCLED TEN TIMES AND THE SYS OPS CHECK GOOD. LEAK CHECK WAS ALSO GOOD A ND THE A/C WAS RETURNED TO SERVICE AND A/C DEPARTED TO BET. ON APPROACH TO BET, THE LEFT MAIN GEAR INDICATED UNSAFE. T HE GEAR WAS CYCLED THREE TIMES BEFORE THE GEAR INDICATED DOWN AND LOCKED. THE AIRCRAFT LANDED AT BET WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED BACK TO ANC FOR MAINTENANCE. MAINTENANCE AT ANC ADJUSTED THE OUTBOARD ACTUATOR AND PERFORMED 2 L 7 2 4T RT A8SW 1999010800494 19990108 00494 SW 1999 1 8 99ZZZM4 1 19981201 A 2150 COOLING TURBINE SWRNGN SA227 SA227AC 8780603 SW CABIN AIR FAILED A MEJA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 SW 17 787C AC550 DURING APPROACH TO SJU, SMOKE WAS NOTICED IN THE COCKPIT ABOUT 15 MINUTES AFTER THE HEATER WAS TURNED ON. THERE WAS ALS O A GREATER DEAL OF SMOKE COLLECTION IN THE AFT CABIN. AN EMERGENCY WAS DECLARED AN A FEW MINUTES LATER, THE LEFT WING OVERHEAT LIGHT ILLUMINATED. DURING APPROACH TO THE RUNWAY, THE WING OVERHEAT LIGHT WENT OUT AND THE AIRCRAFT LANDED WIT HOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND DISCOVERED THAT THE COOLING TURBINE HAD SEIZED. THE COOLING TURBINE W AS DEFERRED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1999010800495 19990108 00495 1999 1 8 99ZZZM5 4 19981201 A 3460 CONNECTOR SWRNGN SA227 SA227AC 8780603 SW GPS CONTAMINATED A MEJA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 17 788C AC340B AFTER TAKEOFF FROM BDA, THE GPS WOULD NOT ACQUIRE SATELLITES FOR NAVIGATION SO THE AIRCRAFT RETURNED TO BDA. MAINTENANC E REMOVED AND CLEANED CONNECTIONS AT ANTENNA AND CONTROL DISPLAY UNIT. GPS RECEIVED NORMAL AND CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A8SW 1999010800496 19990108 00496 EU 1999 1 8 DKAA98024 1 19981209 A 7110 COWLING AMD FALC20 FALCOND 2720304 EU RT ENGINE DAMAGED A DKAA O OTHER D E INFLIGHT SEPARATION VIBRATION/BUFFET DE DESCENT 1 GL 23 226R 226 RIGHT ENGINE LOWER INBOARD COWLING OPENED UP, TOP AND OUTBOARD COWLINGS MOVED 8 INCHES AFT THROUGH FL 110, ON DESCENT. P RELIMINARY INVESTIGATION INDICATES NO DEFECTS NOTED ON COWL LATCHES. REPLACED RIGHT ENGINE, COWLINGS, AND COWL MOUNTS. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A7EU 1999010800497 19990108 00497 NM 1999 1 8 TWRA9864 1 19981207 A 3350 S1356B37 LIGHT BOEING 747 747212B 1384886 NM LAVATORY INOPERATIVE A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 618FF 21937 DURING 'A' SERVICE, FOUND 'B' ZONE EMERGENCY EVAC LIGHT ASSY CRACKED LEFT AISLE, ON 'E' LAVATORY. REMOVED AND REPLACED LIGHT ASSEMBLY AS PER MM 33-51-00. OPERATIONAL CHECK NORMAL. (M) 2 L 7 4 4F A20WE 1999010800498 19990108 00498 EU 1999 1 8 99ZZZM6 1 19981207 A 2133 64642PAR SEAL BRAERO DH125 HS125700A 4230170 EU FLOW CONTROL FAILED A KKYA A UNSCHED LANDING M OVER TEMP CR CRUISE 1 NE 03 511KA NA0237 EN ROUTE FROM BOS-BWI, THE REAR BAY OVERHEAT LIGHT ILLUMINATED. ENGINE POWER WAS REDUCED AND THE LIGHT EXTINGUISHED. PO WER WAS REAPPLIED AND THE LIGHT DID NOT ILLUMINATE. THE AIRCRAFT DIVERTED TO OXC AS A PRECAUTION AND LANDED WITHOUT INC IDENT. THE AIRCRAFT REAR BAY WAS INSPECTED WITH NO DAMAGE FOUND. A GROUND RUN OF THE AIRCRAFT WAS PERFORMED. THE REAR BAY LIGHT DID NOT ILLUMINATE, BUT A SMALL LEAK WAS DETECTED FROM THE FLOW CONTROL VALVE. THERE IS A HEAT DETECTOR IN C LOSE PROXIMITY TO THE VALVE. OPS CHECKED REAR EQUIPMENT BAY HEAT DETECTORS IAW MM 26-10 TEST B CHECKED GOOD. THE VALVE SEALS WERE CHANGED, THE AIRCRAFT WAS RUN AT HIGH POWER WITH ALL SYSTEMS NORMAL AND NO LEAKS. THE AIRCRAFT WAS RETURNED 2 L 7 2 4F A3EU 1999010800499 19990108 00499 CE 1999 1 8 C2XA98CL077 1 19981125 A 2750 1005240731 MOTOR BEECH 1900 1900D 1154162 CE TE FLAP FAILED A C2XA A UNSCHED LANDING F FLT CONT AFFECTED NR NOT REPORTED 1 SW 09 81533 506 1927 UE137 CLE - FLT 3101 - CREW REPORTED THAT THE FLAPS WOULD NOT RETRACT AND THEY RECEIVED A STRONG SMELL IN CABIN AFTER TAKEOFF. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE FLAP DRIVE MOTOR IAW B1900 MM 27-50-03, OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1999010800500 19990108 00500 SO 1999 1 8 C2XA98IA475 1 19981201 A 5311 FRAME EMB 145 EMB145 SO BS 88 CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING C-CHECK INSPECTION, FRAME 68 WAS FOUND TO BE CUT BY THE LEFT OUTBOARD RUDDER CONTROL CABLE. MAINTENANCE RE PAIRED THE FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01028, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999010800501 19990108 00501 SO 1999 1 8 C2XA98IA474 1 19981201 A 5414 SKIN EMB 145 EMB145 SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING C-CHECK INSPECTION, THE RIGHT THRUST REVERSER MODULE UPPER SKIN WAS FOUND TO BE CRACKED WITH SHEARED RIVETS ABOVE FORWARD OF PANEL 426SL. MAINTENANCE STOP DRILLED THE CRACK, INSTALLED A REPAIR DOUBLER, AND REPLACED THE SHEARED FASTENERS IAW EMB145 SRM 54-40-02, AND 51-10-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999010800502 19990108 00502 SO 1999 1 8 C2XA98IA473 1 19981201 A 5320 BEAM EMB 145 EMB145 SO BS 20-25 DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING C-CHECK INSPECTION, FOUND CORROSION BETWEEN THE COMPOSITE FLOOR CROSS BEAMS AND OMEGA BEAMS AT FRAMES 20 AN D 25. MAINTENANCE REPAIRED THE DAMAGED SECTIONS OF OMEGA BEAM IAW EMBRAER FAX SST-2125/98, AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999010800503 19990108 00503 SO 1999 1 8 C2XA98IA472 1 19981201 A 5320 STRAP EMB 145 EMB145 SO BS 13-18 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING C-CHECK INSPECTION, THE CENTER FLOORBEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 13 TO FRAME 18. MAI NTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF BUTT STRAP AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ( M) 2 L 7 2 4F RT T00011AT 1999010800504 19990108 00504 SO 1999 1 8 C2XA98IA471 1 19981201 A 5320 14531597602 ANGLE EMB 145 EMB145 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING C-CHECK INSPECTION, THE RIGHT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENA NCE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SE RVICE. (M) 2 L 7 2 4F RT T00011AT 1999010800505 19990108 00505 SO 1999 1 8 C2XA98IA470 1 19981201 A 5320 14531597601 ANGLE EMB 145 EMB145 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING C-CHECK INSPECTION, THE LEFT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED. MAINTENAN CE REMOVED AND REPLACED THE AFFECTED DRAG ANGLE IAW EMB145 SRM 51-40-02, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SER VICE. (M) 2 L 7 2 4F RT T00011AT 1999010800506 19990108 00506 EU 1999 1 8 C2XA9BT084 1 19981202 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14822 163 FORWARD AISLE PATH LIGHTING INOPERATIVE IN TEST MODE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND POWER SUPPLY. OP S CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999010800507 19990108 00507 EU 1999 1 8 99ZZZM7 1 19981202 A 3350 3011180A POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14822 163 FORWARD AISLE PATH LIGHTING INOPERATIVE IN TEST MODE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AND POWER SUPPLY. OP S CHECKED SYSTEM GOOD. (M) 2 H 7 2 4T RT A53EU 1999010800508 19990108 00508 WP 1999 1 8 ASAA9880244 1 19981121 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP OVERWING EXIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 LCQ - DURING 30K CHECK, THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999010800509 19990108 00509 NM 1999 1 8 ASAA9840111 1 19981203 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 PDX - DURING MAINTENANCE CHECK, TWO FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999010800510 19990108 00510 NM 1999 1 8 ASAA9840110 1 19981201 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 763AS 25100 PDX - DURING MAINTENANCE CHECK, TWO FORWARD EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999010800511 19990108 00511 WP 1999 1 8 ASAA9880255 1 19981207 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 189 49232 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999010800512 19990108 00512 WP 1999 1 8 ASAA9880253 1 19981203 A 3350 014597101 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 963AS 53077 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY LIGHTS IN THE FLIGHT COMPARTMENT WERE FOUND INOPERATIVE. REPLACED THE BAT TERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999010800513 19990108 00513 WP 1999 1 8 ASAA9880252 1 19981203 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 968AS 53016 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. RECONNECTED W IRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999010800514 19990108 00514 WP 1999 1 8 ASAA9880251 1 19981130 A 3350 1001191 PORTABLE LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 982AS 2568 53473 PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999010800515 19990108 00515 WP 1999 1 8 ASAA9880246 1 19981123 A 3397 WIRE DOUG DC9 DC983 3022083 WP ROW 11 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHT WERE FOUND INOPERATIVE FROM ROWS 10 THROUGH 13. RE CONNECTED WIRING IN FLOOR TRACK AT ROW 11 AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999010800516 19990108 00516 WP 1999 1 8 ASAA9880245 1 19981123 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP OVERWING EXIT INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE LEFT AND RIGHT OVERWING EMERGENCY EXIT LIGHTS WERE FOUND INOPERATIVE. REPLACED BATT ERY PACK AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999010800517 19990108 00517 EA 1999 1 8 MASA98210 1 19981126 A 5210 H341427 DOOR HANDLE CNDAIR CL600 CL6002B19 EA PASSENGER DOOR LACK OF LUBE A MASA K NONE O OTHER IN INSP/MAINT 1 SW 07 27173 7173 FLT 6001 - PHX-DSM - PRIOR TO DEPARTURE, CREW REPORTED THE PASSENGER DOOR HANDLE WOULD NOT STOW PROPERLY. MAINTENANCE C LEANED AND LUBED THE DOOR HANDLE, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999010800518 19990108 00518 NM 1999 1 8 HNAA9892792 1 19981128 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM FUSELAGE CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 927HA 117 JAX - CORROSION WAS REPAIRED ON STRINGER 32 RT IAW EO8-53-98-385. (M) 2 H 7 2 4T RT A13NM 1999010800519 19990108 00519 NM 1999 1 8 HNAA9892793 1 19981128 A 5313 STRINGER DHAV DHC8 DHC8102 2809003 NM BS 167-182 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 927HA 117 JAX - FOUND CORROSION ON STRINGER 31 RT BETWEEN STATION 167 AND 182 WITH A LOSS OF 50 PERCENT OF MATERIAL. REPAIRED IAW RD8-53-1243. (M) 2 H 7 2 4T RT A13NM 1999010800520 19990108 00520 NM 1999 1 8 HNAA9893867 1 19981022 A 3350 10126271 LIGHT DHAV DHC8 DHC8102 2809003 NM ROW 4A INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 938HA 26015 152 SBY - FLT 3303 - LOWER EMERGENCY LIGHT BROKEN AT ROW 4A. REMOVED AND REPLACED EMERGENCY LIGHTS ASSY. OPS CHECK GOOD. ( M) 2 H 7 2 4T RT A13NM 1999010800521 19990108 00521 NM 1999 1 8 HNAA9893670 1 19981101 A 3350 1155591 LIGHT DHAV DHC8 DHC8102 2809003 NM ROW 4F INOPERATIVE A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 936HA 26285 145 CLT - FLT 3138 - ROW 4F EMERGENCY EXIT SIGN IN BROKEN. LIGHTS WORKS OK. REPAIRED EXIT SIGN AS REQUIRED. (M) 2 H 7 2 4T RT A13NM 1999010800522 19990108 00522 NM 1999 1 8 HNAA9891772 1 19981104 A 3350 6104791X POWER SUPPLY DHAV DHC8 DHC8102 2809003 NM EQUIP PANEL INOPERATIVE A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 917HA 31209 PS115 075 SBY - FLT 3200 - PASSENGER EXIT SIGN AT BOARDING DOOR INOP. REMOVED AND REPLACED POWER SUPPLY 3351 PS1. OPS CHECK GOOD . (M) 2 H 7 2 4T RT A13NM 1999010800523 19990108 00523 NM 1999 1 8 HNAA982389 1 19981205 A 5311 FRAME DHAV DHC8 DHC8102 2809003 NM BS 215-245 CORRODED A HNAA K NONE O OTHER IN INSP/MAINT 1 EA 07 923HA 099 SBY - FOUND CORROSION FUSELAGE FRAMES AT STATION X222 BETWEEN STRINGERS 32S AND 32P (FRAME, STRINGER, SKIN AND SEAT RAIL SUPPORT), STATION X215 BETWEEN STRINGERS 30S AND 31S (FRAME, SEAT RAIL SUPPORT AND TENSION FITTING), STATION X467 BETWE EN STRINGERS 29S, 30S AND 31S RIGHT SIDE, STATION X487 BETWEEN STRINGERS 29S, 30S AND 31S RIGHT SIDE, X445 BETWEEN STRIN GERS 29S, 30S, AND 31S, STATION X434 STRINGER 30S, STATION X291 ON STRINGER 31S, STATION X312 STRINGER 31, STATION X270 STRINGER 28, STATION X366 STRINGER 30, STATION X366 BETWEEN STRINGERS 29S, 30S, AND 31S, FASTENER BOTTOM RIGHT SIDE DATU M FRAME AND TENSION FITTING, SEAT RAIL TO FRAME ATTACH AREA AT FORWARD EMERGENCY EXIT RIGHT SIDE, TIE DOWN HOOKS IN BAG 2 H 7 2 4T RT A13NM 1999010800524 19990108 00524 NM 1999 1 8 GAIA98125 1 19981124 A 2612 FIRE LOOP BOEING 727 727214 138407R NM NR 1 ENGINE ILLUMINATED A GAIA K NONE N FALSE WARNING CR CRUISE 1 SW 07 750US 21512 DURING SCHEDULE FLIGHT FROM PHX TO TOL, FIRE FAULT DETECTION LIGHT ILLUMINATED IN FLIGHT NR 1 ENGINE. INSPECTED NR 1 EN GINE FIRE LOOP. NO DEFECTS NOTED. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999010800525 19990108 00525 NM 1999 1 8 GAIA98132 1 19981211 A 5230 FASTENER BOEING 727 727223 1384074 NM CARGO DOOR MISSING A GAIA K NONE O OTHER IN INSP/MAINT 1 SW 07 856AA 20997 DURING ROUTINE INSPECTION, NUMEROUS CENTER ROW, RIVETS WERE FOUND MISSING FROM MAIN CARGO DOOR (MCD) LAP SEAM AREA, 10L, BETWEEN FRAMES. REF STC ST00015AT, ATAZ CARGO DOOR MODIFICATION. REPLACED MISSING RIVETS PER STC NR ST00015AT, ATAZ D RAWINGS. AIRCRAFT WAS THEN RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999010800526 19990108 00526 NM 1999 1 8 EISA98275 1 19981113 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 920 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD CORROSION WAS FOUND ON RIGHT INBOARD SEAT TRACK OF FS 920. CUT OUT D AMAGED AREA AND SPLICED IN NEW SECTION OF TRACK PER SRM 53-10-5, FIGURE 7. (M) 2 L 7 3 4F A3WE 1999010800527 19990108 00527 NM 1999 1 8 EISA98276 1 19981113 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD CORROSION WAS FOUND ON RIGHT INBOARD SEAT TRACK OF FS 720A. CUT OUT DAMAGED AREA AND SPLICED IN NEW SECTION OF TRACK PER SRM 53-10-5, FIGURE 7. (M) 2 L 7 3 4F A3WE 1999010800528 19990108 00528 NM 1999 1 8 EISA98277 1 19981113 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 950 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED LEFT INBOARD SEAT TRACK FROM APPROXIMATELY FS 950C TO 950E IS CORRODED . REMOVED DAMAGED TRACK SECTION, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800529 19990108 00529 NM 1999 1 8 EISA98278 1 19981113 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 880-1010 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED LEFT OUTBOARD SEAT TRACK FROM APPROXIMATELY FS 880 TO 1010 IS CORRODED . REMOVED DAMAGED TRACK SECTION, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800530 19990108 00530 NM 1999 1 8 EISA98279 1 19981113 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 900-920 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED LEFT INBOARD SEAT TRACK FROM APPROXIMATELY FS 900 TO 920 IS CORRODED. REMOVED DAMAGED TRACK SECTION, FABRICATED AND INSTALLED NEW SECTION PER SRM 53-10-5 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800531 19990108 00531 NM 1999 1 8 EISA98280 1 19981113 A 5347 SEAT TRACK BOEING 727 727223 1384074 NM BS 720 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT CORROSION WAS FOUND ON RIGHT INBOARD SEAT TRACK AT FS 720B. CUT OUT DAMAGED SE CTION AND SPLICED NEW SECTION OF TRACK PER SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1999010800532 19990108 00532 NM 1999 1 8 EISA98273 1 19981113 A 5751 SKIN BOEING 727 727223 1384074 NM AILERON DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND LEFT AILERON DELAMINATED AT OUTBOARD TRAILING EDGE. REPAIRED D ELAMINATION PER SRM 51-40-6, 51-40-8 AND 51-40-9. (M) 2 L 7 3 4F A3WE 1999010800533 19990108 00533 NM 1999 1 8 EISA98272 1 19981113 A 5754 SKIN BOEING 727 727223 1384074 NM LE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALS LEFT OUTBOARD FOREFLAP HAS DELAMINATION AT INBOARD LOWER CORNER. REPAI RED DELAMINATION PER SRM 51-40-5, 51-40-8 AND 51-40-9. (M) 2 L 7 3 4F A3WE 1999010800534 19990108 00534 NM 1999 1 8 EISA98271 1 19981113 A 5754 SKIN BOEING 727 727223 1384074 NM LE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALS LEFT INBOARD FOREFLAP DELAMINATED AT INBOARD CORNER. REPAIRED DELAMINA TION PER SRM 51-40-6, FIGURE 26. (M) 2 L 7 3 4F A3WE 1999010800535 19990108 00535 NM 1999 1 8 EISA98270 1 19981113 A 5751 SKIN BOEING 727 727223 1384074 NM AILERON DELAMINATION A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK ACCOMPLISHMENT REVEALS RIGHT AILERON, OUTBOARD T/E HAS TWO AREAS OF DELAMINATION. REPAIRED AREAS O F DELAMINATION PER SRM 51-40-5, 51-40-6 AND 51-40-8 AND 51-40-9. (M) 2 L 7 3 4F A3WE 1999010800536 19990108 00536 NM 1999 1 8 EISA98260 1 19981114 A 5753 SKIN BOEING 727 727223 1384074 NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED LEFT INBOARD T/E FLAP DELAMINATED AT OUTBOARD CORNER. REPAIRED DELAMI NATION PER SRM 51-40-5, BONDED METAL REPAIR. (M) 2 L 7 3 4F A3WE 1999010800537 19990108 00537 NM 1999 1 8 EISA98274 1 19981113 A 5753 SKIN BOEING 727 727223 1384074 NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND RIGHT INBOARD MID FLAP DELAMINATED. REPAIRED MID FLAP PER SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1999010800538 19990108 00538 WP 1999 1 8 EISA98283 1 19981120 A 3350 60030431 BATTERY PACK DOUG DC9 DC931 3022065 WP BS 24 DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 977ML 11113 47329 FORWARD EMERGENCY LIGHTS DIM ON TEST. GENERATED BY MAINTENANCE REPORT. REPLACED BATTERY PACK SUPPLY AT BS 24 PER MM 33 -00 CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1999010800539 19990108 00539 WP 1999 1 8 EISA98282 1 19981120 A 3350 60030431 BATTERY PACK DOUG DC9 DC931 3022065 WP BS 32 DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 977ML 14659 47329 MIDDLE OVERHEAD EMERGENCY LIGHT DIM ON TEST. GENERATED BY MAINTENANCE REPORT. REPLACED BATTERY PACK SUPPLY AT BS 32 PE R MM 33-53-0 CHECKS GOOD. (M) 2 L 7 2 4F A6WE 1999010800540 19990108 00540 WP 1999 1 8 EISA98281 1 19981120 A 3350 60300431 BATTERY PACK DOUG DC9 DC931 3022065 WP BS 23 DISCHARGED A EISA K NONE L NO TEST IN INSP/MAINT 1 SW 07 977ML 47329 FORWARD RIGHT EMERGENCY LIGHTS DIM ON TEST. GENERATED FROM MAINTENANCE REPORT. REPLACED BATTERY PACK SUPPLY AT BS 3 PE R MM 33-53-0 CHECK GOOD. (M) 2 L 7 2 4F A6WE 1999010800541 19990108 00541 NM 1999 1 8 EISA98268 1 19981114 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 540 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED STRINGER 27L AT FS 540 HAS CORROSION. REMOVED DAMAGED SECTION, FABRIC ATED NEW SECTION AND INSTALLED PER SRM 53-10-2, 53-10-3 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800542 19990108 00542 NM 1999 1 8 EISA98267 1 19981114 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 540 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED CORROSION AT FS 540 STRINGER 27R. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED NEW SECTION PER SRM 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800543 19990108 00543 NM 1999 1 8 EISA98254 1 19981114 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 328 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ROUTINE C-CHECK WORKCARD ACCOMPLISHMENT REVEALED STRINGER 19R AT FS 328 HAS CORROSION. CUT OUT DAMAGED AREA. FA BRICATED NEW STRUCTURE SECTION AND INSTALLED PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999010800544 19990108 00544 NM 1999 1 8 EISA98265 1 19981114 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 500 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEAL SHEAR TIE CORRODED AT FS 500 STRINGER 28L. REMOVED DAMAGED SHEAR TIE. F ABRICATED AND INSTALLED NEW PART PER 51-40-4 AND 51-30-1. (M) 2 L 7 3 4F A3WE 1999010800545 19990108 00545 NM 1999 1 8 EISA98264 1 19981114 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 540 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED SHEAR TIE CORRODED AT FS 540 STRINGER 28L. REMOVED DAMAGED SHEAR TIE. FABRICATED AND INSTALLED NEW PART PER 51-40-4 AND 51-30-1. (M) 2 L 7 3 4F A3WE 1999010800546 19990108 00546 NM 1999 1 8 EISA98263 1 19981114 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 500 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED SHEAR TIE CORRODED AT FS 500 BL 0. REMOVED DAMAGED PART. FABRICATED AND INSTALLED NEW PAR PER 51-40-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800547 19990108 00547 NM 1999 1 8 EISA98261 1 19981114 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 660 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED SHEAR TIE CORRODED AT FS 660 AT STRINGER 28R. REMOVED DAMAGED SHEAR T IE. FABRICATED AND INSTALLED NEW PART PER SRM 51-40-4 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800548 19990108 00548 NM 1999 1 8 EISA98253 1 19981118 A 5297 WIRE BOEING 727 727223 1384074 NM PASSENGER DOOR BROKEN A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 6819 19494 MAIN CARGO DOOR LIGHT ILLUMINATED DURING FLIGHT, WITH A POSSIBLE PRESSURE LOSS, RESULTING IN AN AIR TURN BACK TO EDI. F OUND BROKEN WIRE REPAIRED IAW MM CHAPTER 20 AND 52. OPS CHECK GOOD OK FOR SERVICE. (M) 2 L 7 3 4F A3WE 1999010800549 19990108 00549 NM 1999 1 8 EISA98262 1 19981121 A 5270 SWITCH BOEING 727 727223 1384074 NM CARGO DOOR OUT OF ADJUST A EISA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 316NE 19475 CARGO DOOR ARM/DISARM LIGHT CAME ON AFTER TAKEOFF FROM MCO, UNABLE TO PRESSURIZE CARGO WARNING LIGHT OFF. AIR TURN BACK TO MCO, GENERATED FROM PILOT REPORT. ADJUST S17 SWITCH (LOCK BAR SWITCH) OPS CHECK NORMAL PER PEMCO MM. RAN NR 3 ENGI NE AND PRESSURIZED NORMAL. (M) 2 L 7 3 4F A3WE 1999010800550 19990108 00550 NM 1999 1 8 EISA98259 1 19981114 A 5314 KEEL BEAM BOEING 727 727223 1384074 NM BS 873 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ACCOMPLISHMENT OF CPCP WORK CARD NR C53-100-01 REVEALED CRACK IN KEEL BEAM JUST FORWARD OF APU STATION 873MM RIGHT MAIN LANDING GEAR BAY. REMOVE DAMAGED AREA, FABRICATED FILLER AND DOUBLER PER SRM 53-10-2 AND 51-40-2 AND INSTALLED PER SRM 51-30-1. (M) 2 L 7 3 4F A3WE 1999010800551 19990108 00551 NM 1999 1 8 EISA98255 1 19981114 A 5720 MOUNT BOEING 727 727223 1384074 NM ACTUATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ROUTINE C-CHECK WORKCARD ACCOMPLISHMENT REVEALED NR 8 SLAT ACTUATOR ATTACH MOUNT CRACKED. REPLACED NR 8 SLAT PER MM 27-33-11. (M) 2 L 7 3 4F A3WE 1999010800552 19990108 00552 NM 1999 1 8 EISA98269 1 19981114 A 5755 SKIN BOEING 727 727223 1384074 NM NR 1 SPOILER DAMAGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORKCARD ACCOMPLISHMENT REVEALED A REPAIR DOUBLER OUTBOARD OF NR 1 SPOILER CRACKED. FABRICATED AND INST ALLED NEW DOUBLER PER SRM 51-30-1 AND 51-30-7. (M) 2 L 7 3 4F A3WE 1999010800553 19990108 00553 NM 1999 1 8 EISA98258 1 19981114 A 5754 RIB BOEING 727 727223 1384074 NM NR 7 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED NR 3 SLAT HAD CRACKED RIB INBOARD OF INBOARD TRACK. REPLACED R IB ASSEMBLY PER SRM 57-50-3 AND 51-30-2. (M) 2 L 7 3 4F A3WE 1999010800554 19990108 00554 NM 1999 1 8 EISA98256 1 19981114 A 5754 RIB BOEING 727 727223 1384074 NM NR 3 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ROUTINE C-CHECK WORKCARD ACCOMPLISHMENT REVEALED NR 3 SLAT INBOARD RIB CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999010800555 19990108 00555 NM 1999 1 8 EISA98257 1 19981114 A 5754 RIB BOEING 727 727223 1384074 NM NR 7 SLAT CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 DURING ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT, FOUND NR 7 SLAT OUTBOARD TRACK RIB CRACKED. BLENDED OUT CRACK IAW SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER PER SRM 57-50-2 AND 51-40-3. (M) 2 L 7 3 4F A3WE 1999010800556 19990108 00556 NM 1999 1 8 EISA98266 1 19981114 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1110 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 313NE 19702 ROUTINE C-CHECK WORK CARD ACCOMPLISHMENT REVEALED CORROSION ON TOP OF FLOORBEAM FS 1110, LBL 15. REMOVED DAMAGED SECTIO N, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1999010800557 19990108 00557 EU 1999 1 8 SIMA982751 1 19981002 A 5280 S5287130401950 DOOR AEROSP ATR42 ATR42300 8680920 EU RT MLG LOOSE A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 37AE 037 ORD - FLT 4272 - AFTER DEPARTURE FROM CMH, THE RIGHT MAIN LANDING GEAR DOOR BECAME LOOSE. CREW CONTINUED TO ORD, DECLAR ED EMERGENCY. AIRCRAFT LANDED SAFELY, GEAR WAS PINNED, AND AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. REMOVED AND R EPLACED THE RIGHT MAIN LANDING GEAR DOOR LINK AND DOOR. OPERATIONAL CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 1999010800558 19990108 00558 EU 1999 1 8 99ZZZM8 1 19981002 A 3231 S5397131700200 LINK AEROSP ATR42 ATR42300 8680920 EU RT MLG LOOSE A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 37AE 037 ORD - FLT 4272 - AFTER DEPARTURE FROM CMH, THE RIGHT MAIN LANDING GEAR DOOR BECAME LOOSE. CREW CONTINUED TO ORD, DECLAR ED EMERGENCY. AIRCRAFT LANDED SAFELY, GEAR WAS PINNED, AND AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. REMOVED AND R EPLACED THE RIGHT MAIN LANDING GEAR DOOR LINK AND DOOR. OPERATIONAL CHECK WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 1999010800559 19990108 00559 WP 1999 1 8 ASAA9880224 1 19981107 A 5610 LOCK BAR DOUG DC9 DC983 3022083 WP COCKPIT DAMAGED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 973AS 53449 SEA - DURING MAINTENANCE CHECK, THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. REPLACED WINDOW UPPER LOCK B AR AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999010800560 19990108 00560 WP 1999 1 8 ASAA9880172 1 19980908 A 5210 HOLD OPEN DOUG DC9 DC982 3022082 WP PASSENGER DOOR LOOSE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 956AS 48079 PDX - PRIOR TO DEPARTURE OF FLIGHT 462, CREW REPORTED THE L1 DOOR WOULD NOT RELEASED FROM THE HOLD OPEN POSITION. FOUND DOOR HOLD OPEN MECHANISM PUSH-PULL TUBE HARDWARE DISCONNECTED, RECONNETED MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999010800561 19990108 00561 WP 1999 1 8 ASAA9880223 1 19981107 A 5330 SKIN DOUG DC9 DC983 3022083 WP FUSELAGE DENTED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OAK - DURING 15K CHECK DENT WAS FOUND IN FUSELAGE SKIN AFT OF L1 DOOR ABOVE CUSP LINE. REPAIRED WITH DOUBLER IAW ASA EA 5330-01350. (M) 2 L 7 2 4F RT A6WE 1999010800562 19990108 00562 WP 1999 1 8 ASAA9880220 1 19981105 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1160 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 976AS 53452 OAK - DURING 15K CHECK, FUOND CORROSION ON FLOOR WEB OUTBOARD OF FLOOR PANEL E-14 AT FS 1160. REPAIRED WITH DOUBLER IAW ASA EA 5320-01203. (M) 2 L 7 2 4F RT A6WE 1999010800563 19990108 00563 NM 1999 1 8 USAA980562 1 19981021 A 5313 655054038 STRINGER BOEING 737 737401 1384701 NM BS 927 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 406US 29916 23876 CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH BY 1 INCH AREA OF CORROSION STATION 927 STRINGER 20R. CORROSIO N TASK NR C53-202-01. INSTALLED SPLICE PER BOEING 737-400 SRM 53-00-03 FIG 201 AND SRM 53-00-07 FIG 205. (M) 2 L 7 2 4F RT A16WE 1999010800564 19990108 00564 NE 1999 1 8 AALA981914 2 19981012 A 7230 COMPRESSOR DOUG DC9 DC982 3022082 WP PWA JT8 JT8D219 52053 NE LT ENGINE SEIZED A AALA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SW 07 516AM 49893 717383 DFW - FLT 475 - EN ROUTE DFW-PSP - AFTER TAKEOFF DFW AT 1000 FEET LOST ALL POWER FROM LEFT ENGINE. ALL INDICATIONS SHOW ED LEFT ENGINE FAILED. CREW DECLARED AN EMERGENCY AND LANDED OVERWEIGHT AT DFW WITHOUT INCIDENT. TROUBLESHOT SYSTEM AN D FOUND LEFT ENGINE COMPRESSOR SEIZED. REPLACED LEFT ENGINE ASSEMBLY. ACCOMPLISHED OVERWEIGHT LANDING AND PYLON INSPEC TION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F 4 F A6WE E9NE 1999010800565 19990108 00565 1999 1 8 USAASB98276 4 19981019 A 2230 110010121 SERVO BOEING 737 737201 1384454 NM E/E BAY FAILED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 224US 21666 CLT - FLT 357 - DURING CRUISE AT FL330 WITH AUTOTHROTTLE ENGAGED, NR 1 THROTTLE BEGAN MOVING 1 OR 2 INCHES IN EITHER DIR ECTIONS. POWER WAS CHANGING WITH THROTTLE MOVEMENT. CAPT DISCONNECTED AUTOTHROTTLE AND NR 1 THRUST LEVER BECAME FROZEN AT CRUISE POWER. NR 1 THRUST LEVER COULD NOT BE MOVED MANUALLY OR WITH AUTOTHROTTLES. AN EMERGENCY WAS DECLARED AND F LT DIVERTED TO CLT. NR 1 ENG WAS SHUT DOWN 10 MINS PRIOR TO LANDING TO ELIMINATE CRUISE POWER ON LANDING. AFTER THE NR 1 ENG WAS SHUT DOWN, THRUST LEVER WAS FREE TO MOVE TO IDLE WHERE IT WAS THEN LOCKED IN POSITION. FLT LANDED WITHOUT FU RTHER INCIDENT. MX FOUND A BENT ACT ARM FOR SWITCH S-139 ON AUTOTHROTTLE CLUTCH. R/R'D LEFT AUTOTHROTTLE CLUTCH SERVO 2 L 7 2 4F A16WE 1999010800566 19990108 00566 GL 1999 1 8 C2XA98IA466 3 19981109 A 6110 HCE4A31 PROPELLER BEECH 1900 1900D 1154162 CE HARTZL HCB4M HCB4MP3 GL NR 2 ENGINE DELAMINATED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17534 5489 UE141 IAH - DURING POST FLIGHT INSPECTION, CREW REPORTED THE NR 2 PROPELLER WAS DELAMINATING ALONG THE LEADING EDGE ON THE FAC E AND CAMBER SIDES APPROX 12 INCHES TO 14 INCHES LONG. MAINTENANCE REMOVED AND REPLACE THE PROPELLER ASSY IAW B1900D MM 61-10-00 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 6 C P56GL 1999010800567 19990108 00567 NE 1999 1 8 SABA980051 3 19981008 A 6110 PROPELLER BAG JETSTM JETSTM3201 1500217 EU MCAULY 4HFR34 4HFR34C653 NE RT ENGINE CONTAMINATED A SABA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS AP APPROACH 1 SO 33 941AE 9360 941 RDU - FLT 5215 - RIGHT PROP REMOVED DUE TO METAL CONTAMINATION. REMOVED AND REPLACED RIGHT PROP IAW JE 32 MM ATA RET 61 -00-01. PROP REPLACED WITH ENGINE REPLACEMENT. (M) 2 L 7 2 4T RT A56EU 6 C 3PNE 1999010800568 19990108 00568 EA 1999 1 8 MASA98182 1 19980930 A 3350 1317 BULB CNDAIR CL600 CL6002B19 EA LT EMERG EXIT FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 27191 7191 FLT 5750 - BHM-PHL - DURING PREFLIGHT CREW NOTICED THAT THE LEFT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. THE ITEM WAS DEFERRED PER MEL 33-51-2 AND AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE THE BULB WAS REMOVED AND REPL ACED. (M) 2 L 7 2 4F RT A21EA 1999010800569 19990108 00569 NE 1999 1 8 ASOA98106 2 19981127 A 7200 300005000052 TSCU EMB 120 EMB120RT SO PWA 118 PW118 NE RT/LT ENGINE FAILED A ASOA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 11 503AS 120275 SHORTLY AFTER TAKEOFF SDF-ATL, THE RIGHT ENGINE EEC FAILED, CREW RAN THE EEC FAILURE CHECKLIST. AS POWER WAS REDUCED TO 24 PERCENT, RECEIVED AN UNCOMMANDED FEATHER OF THE ENGINE DUE TO A/F SYSTEM STILL BEING ARMED. PILOT DECLARED AN EMERG ENCY AND REQUESTED RETURN TO SDF WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. AFTER CONFERRING WITH MTC. FLIGHT RESUMED WITH THE EEC'S DEFERRED AND CONTINUED TO ATL. MCN MAINTENANCE REMOVED AND REPLACED BOTH ENGINE TSCU'S. OPERATIONAL CHECKS WERE GOOD, DEFERRAL CLEARED, AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 L 7 2 4T 4 T RT A31SO E20NE 1999010800575 19990108 00575 NM 1999 1 8 USAASB98300 1 19981115 A 3231 65462059 LINK BOEING 737 7372B7 1384560 NM LT NLG DOOR BROKEN A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 270AU 22882 CLE - FLT 957 - DURING CLIMB AND GEAR RETRACTION, CREW HEARD A LOUD BANG FROM THE NOSE WHEEL WELL FOLLOWED BY A CONTINUO US VIBRATION IN THE COCKPIT. CAPTAIN DECIDED TO RETURN TO FIELD AT CLE AND DECLARE AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. AFTER LANDING, MAINTENANCE MET THE AIRCRAFT, PINNED THE GEAR AND TAXIED IN. MAINTENANCE FOUND THE L EFT NOSE GEAR DOOR FIXED OPERATOR LINK BROKEN. REMOVED AND REPLACED OPERATOR LINK AND SWUNG NOSE GEAR PER MM 32-33-61. OPERATION CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999010800576 19990108 00576 NM 1999 1 8 USAASB98297 1 19981110 A 2822 2580005 BOOST PUMP BOEING 737 737201 1384454 NM NR 2 FAILED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 244US 22752 DTW - FL2232, EN ROUTE FROM CLT TO DTW, FLIGHT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL AFT OF FORWARD BULKH EAD AROUND SEAT ROWS 4, 5 AND 6. SHORTLY THEREAFTER, THE CIRCUIT BREAKERS FOR THE NR 2 AFT FUEL BOOST PUMP AND NR 2 TR TRIPPED. THE NR 2 TR READ 0 AMPS AND 28 VOLTS. INTERMITTENTLY, THE LEFT ANTI-SKID OFF AND FIRST OFFICER AUX PITOT STAT IC AMBER LIGHTS ILLUMINATED, PMS EXTERNAL FAIL WITH CODES 96 AND 99 AND A FLAG IN THE NR 2 EPR GAUGE. ON DESCENT, ALL L IGHTS AND FLAGS WENT OUT AND PMS OPERATED NORMALLY. CREW DID NOT RESET BOOTS PUMP OR TR CIRCUIT BREAKERS TO AVOID THE P OSSIBLE RETURN OF THE BURNING ODOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED APPLICABLE WIRING. RE 2 L 7 2 4F A16WE 1999010800577 19990108 00577 GL 1999 1 8 RAIA981103 3 19981103 A 6110 PROPELLER BAG JETSTM JETSTM3201 1500217 EU ROTOL R333 R333482F12 GL LT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 428AM 13219 877 FLT 7478 - STL - LEFT PROP HEAT WON'T TO 10 AMPS. MAINTENANCE REPLACED LEFT PROP ASSY. (M) 2 L 7 2 4T RT A56EU 6 C P61GL 1999010800578 19990108 00578 EA 1999 1 8 VTZA98351 1 19981117 A 2130 CONNECTOR CNDAIR CL600 CL6002B19 EA RT PACK CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 629BR 7251 FLT 6632 - ORD-CRW - DURING CRUISE, EXPERIENCED A RT PACK 'HI PSI' INDICATION ILLUMINATION. AIRCRAFT RETUREND TO ORD WH ERE MAINTENANCE WAS DISPATCHED TO TROUBLESHOOT THE SYSTEM DISCREPANCY. MAINTENANCE CLEANED THE CANNON PUG FOR THE RIGHT PACK ACM AND CHECKED THE PRESSURE SWITCH TO THE RIGHT PACK IAW MM PROCEDURES FOUND IN 21-51-10. MAINTENANCE THEN CONDU CTED AN OPERATIONAL CHECK WITH NO FURTHER DEFICIENCIES NOTED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4F RT A21EA 1999010800579 19990108 00579 NM 1999 1 8 F3LA98195 1 19981119 A 7603 BOLT BOEING 737 7372P6 NM POWER LEVER DAMAGED A F3LA A E UNSCHED LANDING ENGINE SHUTDOWN O OTHER NR NOT REPORTED 1 NM 03 1PC 21613 DEN - AIR TURN BACK, FLIGHT CREW REPORTED NR 2 ENGINE WOULD NOT RESPOND TO THRUST LEVER. NR 2 ENGINES WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 2 POWER LEVER ROD END BOLT, NUT AND WASHER AT CROSSOVER SHAF T BELL CRANK AND CHECKED OK. (M) 2 L 7 2 4F RT A16WE 1999010800580 19990108 00580 NE 1999 1 8 P2EA98255 2 19981122 A 7200 ENGINE BOEING 737 737222 1384473 NM PWA JT8 JT8D9A 52048 NE NR 2 FAILED A P2EA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 05 209US 19548 FLT 408 - MCI - AIR RETURN, NR 2 ENGINE SHUTDOWN INFLIGHT. EMERGENCY DECLARED LANDING UNEVENTFUL. NR 2 ENGINE START VA LVE ILLUMINATED INFLIGHT, ENGINE NR 2 SHUTDOWN IAW QRH RETURNED MCI. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999010800581 19990108 00581 EU 1999 1 8 DKAA98023 1 19981209 A 5320 CHANNEL AMD FALC20 FALCON20C5 2730107 EU CARGO DOOR SILL CRACKED A S DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 810RA 4746 81 CARGO DOOR Z-CHANNEL FOUND CRACKED (3 6 INCH CRACKS). CRACKS FOUND IN INTERIOR RADIUS, ADJACENT TO CARGO DOOR HINGE. A IRCRAFT WAS CARGO CONVERTED IAW STC NR SA2490S0 AND ST00376AT. 2 L 7 2 4F RT A7EU 1999010800582 19990108 00582 NM 1999 1 8 USAASB98295 1 19981110 A 2420 941D3352 TRANSFORMER BOEING 737 737401 1384701 NM NLG WW FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 413US 23882 PHL - FLT 162 - SHORTLY AFTER T/O, THE NR 1 TRANSFORMER RECTIFIER C/B TRIPPED FOLLOWED BY THE BATTERY CHARGER AND THE 'B ' SYSTEM ELECTRIC HYDRAULIC PUMP. WITHIN 10 MINUTES, THE NR 1 ELECTRIC BUS TRIPPED FOLLOWED BY THE AC STANDBY BUS, EQUI PMENT COOLING NORMAL BLOWER AND FCC DC BREAKER AND THE NR 2 TRANSFORMER RECTIFIER. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. THE APU WAS ON MEL AT THE TIME. MAINTENANCE REMOVED AND R EPLACED THE NR 1 GENERATOR CONTROL BREAKER C801. RAN ENGINES FOR EXTENDED TIME TO CHECK NR 1 GENERATOR AND RELATED SYST EMS. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 1999010800583 19990108 00583 NM 1999 1 8 99ZZZM14 1 19981110 A 2433 1032575 RECTIFIER BOEING 737 737401 1384701 NM NLG WW FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 413US 23882 PHL - FLT 162 - SHORTLY AFTER T/O, THE NR 1 TRANSFORMER RECTIFIER C/B TRIPPED FOLLOWED BY THE BATTERY CHARGER AND THE 'B ' SYSTEM ELECTRIC HYDRAULIC PUMP. WITHIN 10 MINUTES, THE NR 1 ELECTRIC BUS TRIPPED FOLLOWED BY THE AC STANDBY BUS, EQUI PMENT COOLING NORMAL BLOWER AND FCC DC BREAKER AND THE NR 2 TRANSFORMER RECTIFIER. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. THE APU WAS ON MEL AT THE TIME. MAINTENANCE REMOVED AND R EPLACED THE NR 1 GENERATOR CONTROL BREAKER C801. RAN ENGINES FOR EXTENDED TIME TO CHECK NR 1 GENERATOR AND RELATED SYST EMS. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT A16WE 1999010800584 19990108 00584 SO 1999 1 8 C2XA98BT076 1 19981023 A 2120 AIR DISTRIBUTION EMB 145 EMB145 SO COCKPIT SMOKE A A C2XA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 09 14933 145018 FLT 4251 - CREW REPORTED SMOKE IN COCKPIT IMMEDIATELY AFTER ADVANCING THRUST LEVER FOR TAKEOFF. TAKEOFF WAS REJECTED. M AINTENANCE INSPECTED NR 1 AND NR 2 ENGINES, APU COMPARTMENT, AVIONIC BAYS FORWARD AND AFT, HYD COMPARTMENTS, LAV AND BAG GAGE COMPARTMENTS FOR PRESENTS OF SMOKE OR EXCESSIVE HEAT. PERFORMED ENGINE GROUND RUNS FOR 20 MINS AT VARIOUS THRUST S ETTINGS AND VARIOUS PACK SETTINGS. NO SMOKE OR OTHER DEFECTS NOTED, REF EMB145 MM 71-00-01 FOR RUNS. (M) 2 L 7 2 4F RT T00011AT 1999010800585 19990108 00585 EU 1999 1 8 VTZA98347 1 19981123 A 2913 384925 PUMP BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 EA 27 486UE 905 FLT 6200 - IAD-ROA - DURING APPROACH, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LOST ALL HYDRAULI C PRESSURE, CREW PUMPED LANDING GEAR DOWN. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT HYDRAULIC PUMP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010800586 19990108 00586 1999 1 8 VTZA98346 4 19981124 A 3425 7003360948 AHRS JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 321UE 41045 FLT 6499 - IAD-ROA - DURING CRUISE, AIRCRAFT MADE A SCHEDULED LANDING DUE TO F/O'S AHRS FAILURE. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED F/O'S AHRS. OPS CHECK OK. AIRCRAFT WAS R ELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999010800587 19990108 00587 1999 1 8 VTZA98345 3 19981122 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILURE A VTZA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 470UE 814 FLT 6348 - IAD-GSO - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO RIGHT BETA WARNING LIGHT ILLUMINATED. AIRCRAFT RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BETA PSI SWITCH, OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010800588 19990108 00588 1999 1 8 VTZA98344 4 19981122 A 3416 066306202 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 475UE 850 FLT 6195 - IAD-MDT - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CAPTAINS ALTIMETER FAILURE. AIRCRAFT RE TURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED CAPT'S ALTIMETER. OPS CHECK OK . AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999010800589 19990108 00589 EU 1999 1 8 VTZA98343 1 19981122 A 2425 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 1 FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 315UE 41033 FLT 6621 - IAD-ILM - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 1 SYMBOL GENERATOR FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 SYMBOL GENERATOR, OPS CH ECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999010800590 19990108 00590 EA 1999 1 8 VTZA98341 1 19981122 A 3241 601R7514811 TRANSDUCER CNDAIR CL600 CL6002B19 EA LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 629BR 7251 FLT 6723 - IAD-SAV - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BRAKE WARNIGN LIGHT ILLUMINATED AND BRA KE PSI INDICATION WENT TO ZERO. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED D MI 54656, MEL 32-40. MAINTENANCE CLOSED DMI 54656 ON 11-23-98 BY REMOVING AND REPLACING PRESSURE TRANSDUCER, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999010800591 19990108 00591 SO 1999 1 8 ASOA98083 1 19981019 A 3000 DEICE SYSTEM EMB 120 EMB120RT SO COCKPIT MALFUNCTIONED A ASOA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SO 11 261AS 120141 FLT 7063 - DURING CRUISE FLIGHT ATL-CRW, APPROX 10 MINUTES AFTER TURNING ON PROP HEAT, ENGINE AIR INLET DEICE AND WINDSH IELD HEAT, A STRONG BURNING ELECTICAL SMELL BECAME EVIDENT IN THE COCKPIT. DEICE SYSTEMS WERE TURNED OFF AND DESCENT IN ITIATED OUT OF ICING CONDITIONS, SMELL DISSIPATED. TURNED DEICE SYSTEMS BACK ON, SMELL RECURRED. TURNED EQUIP BACK OFF , INITIATED FURTHER DESCENT AND DIVERTED INTO TRI WHERE LANDING WAS MADE SAFELY AND WITHOUT FURTHER INCIDENT. LOCAL MX PERFORMED SYSTEMS OPS CHECK ON DEICE SYSTEM, SUSPECTED AND DEFERRED F/O WINDSHIELD HEAT IAW MEL 30-40-1. ATL MX INSPECT ED AND OP'S CHECKED SYSTEM, COULD NOT DUPLICATE THE PROBLEM. THE DEFER LOG WAS CLEARED AND THE AIRCRAFT RELEASED FOR FU 2 L 7 2 4T RT A31SO 1999010800592 19990108 00592 WP 1999 1 8 USAAD98206 1 19981118 A 2560 3753213575 LANYARD DOUG DC9 DC931 3022065 WP SLIDE MISINSTALLED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 971VJ 47051 PIT - DURING A FUNCTIONAL CHECK, THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED TO DEPLOY AUTOMATICALLY. MAINTENANCE RE POSITIONED THE TAIL CONE LANYARD AND THE FUNCTIONAL TEST WAS NORMAL. (M) 2 L 7 2 4F A6WE 1999010800593 19990108 00593 NM 1999 1 8 P2EA98282 1 19981211 A 5753 TORSION BAR BOEING 737 737244 138448U NM TE FLAP OUT OF ADJUST A P2EA O OTHER F FLT CONT AFFECTED AP APPROACH 1 CE 05 620PC 19708 MCI - FLT 586 - NO EMERGENCY DECLARED LANDING UNEVENTFUL AT DESTINATION. AIRCRAFT ROLLS RIGHT WHEN FLAPS ARE EXTENDED. RETORQUED TORSION BAR ON NR 1 SLAT PER MM 27-81-21 AND LUBRICATED TRACKS, OPS CHECKED OK. (M) 2 L 7 2 4F A16WE 1999010800594 19990108 00594 NM 1999 1 8 USAA980572 1 19981113 A 5321 FLOOR BOEING 737 737301 1384611 NM BS 277 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK BS 277 STRINGER 13R AND STRINGER 14R STRAP. INSTALLED DOUBLER PER SRM 51-70-11 FIG 1. (M) 2 L 7 2 4F RT A16WE 1999010800595 19990108 00595 1999 1 8 USAAD98203 4 19981114 A 3418 25147A3B TRANSDUCER DOUG DC9 DC931 3022065 WP STALL WARNING FAILED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 931VJ 47188 CLT-PHL - FLT 937 - AFTER TAKEOFF AND THE FLAPS AND SLATS WERE RETRACTED THE STALL WARNING LIGHT ILLUMINATED ON THE CAPT AINS SIDE AND THE HORN SOUNDED. THE LIGHT AND HORN OPERATED INTERMITTENTLY AS THE AIRCRAFT RETURNED TO THE FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ANGLE OF ATTACK TRANSDUCER. (M) 2 L 7 2 4F A6WE 1999010800596 19990108 00596 WP 1999 1 8 HALA9800375 1 19981103 A 3310 LIGHT DOUG DC10 DC1010 3022110 WP COCKPIT INOPERATIVE A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 119AA 46519 LAS - FLT 935 - NR 3 FUEL LEVER LIGHT WON'T TEST. NR 2 FUEL LEVER AND FIRE T-HANDLE LIGHT DON'T ILLUMINATE DURING FIRE WARNING TEST. REPLACED NR 3 ENGINE FUEL SHUT OFF LIGHT ASSY. OPS CHECK OK. REPLACED NR 2 FUEL SHUT OFF HANDLE, LIGHT ASSY AND CONTROLLER, OPS CHECK OK. (M) 2 L 7 3 4F A22WE 1999010800597 19990108 00597 NM 1999 1 8 P2EA98279 1 19981209 A 5754 BOLT BOEING 737 737244 138448U NM NR 4 SLAT LOOSE A P2EA O OTHER O OTHER NR NOT REPORTED 1 CE 05 620PC 19708 MDW - FLT 418 - NO EMERGENCY DECLARED LANDING UNEVENTFUL. AT FLAPS 1 RECEIVED UNCOMMANDED ROLL. POST FLIGHT REVEALS LO OSE, LEADING EDGE SLAT. FOUND NR 4 SLAT, INBOARD AUX TRACK ADJUSTMENT BOLT LOOSE. REPLACED BUSHING AND TIGHTENED BOLT PER MM 27-81-21, SLAT OPS CHECK NORMAL PER MM 27-81-0. (M) 2 L 7 2 4F A16WE 1999010800598 19990108 00598 NM 1999 1 8 USAASB98301 1 19981115 A 5240 69203214 ARM BOEING 737 737301 1384611 NM SERVICE DOOR OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 574US 23739 CLT - FLT 1583 - DURING CLIMB-OUT FROM CLT, AIRCRAFT WOULD NOT PRESSURIZE. THE AUTO FAIL LIGHT ILLUMINATED AND THE SYST EM SWITCHED TO STANDBY MODE. THE OUTFLOW VALVE INDICATED FULL CLOSE, BUT THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT ATT ENDANT THEN ADVISED CREW THAT THERE WAS AN EXCESSIVE AIR LEAK AROUND THE AFT RIGHT SERVICE DOOR. FLIGHT RETURNED TO FIE LD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE AFT RIGHT SERVICE DOOR NOT CLOSED PROPERLY. DOOR WAS HARD TO CLOSE AT TIMES. ADJUSTED GUIDE ARM ON AFT RIGHT SERVICE DOOR PER MM 52-41-21. O PS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010800599 19990108 00599 NM 1999 1 8 USAASB98320 1 19981208 A 7933 INDICATOR BOEING 737 7373B7 1384580 NM COCKPIT MALFUNCTIONED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 375US 22954 CLT - FLT 1480 - AFTER TAKEOFF, THE NR 1 ENGINE OIL TEMPERATUR WENT TO 200 DEGREES. CAPTAIN FOLLOWED PROCEDURES, SHUT D OWN THE NR 1 ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO T HE GATE. MAINTENANCE FOUND A BROKEN GROUND WIRE FOR THE OIL TEMPERATURE INDICATION ON THE NR 1 ENGINE. REPAIRED BROKEN WIRE. ACCOMPLISHED ENGINE RUN. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999010800600 19990108 00600 WP 1999 1 8 HALA9800377 1 19981104 A 3230 TORQUE LINK DOUG DC10 DC1010 3022110 WP NLG OUT OF ADJUST A HALA K NONE O OTHER CR CRUISE 1 WP 13 152AA 46707 LAX - FLT 3 - NOTICED VIBRATION DURING FLIGHT FOUND NOSE GEAR DOORS AJAR APPROXIMATELY ONE INCH. ADJUSTED RIGHT AND LEF T FORWARD NOSE GEAR DRIVE LINKS, CHECKS OK, ON GEAR SWING PER MM 32-23-01. (M) 2 L 7 3 4F A22WE 1999010800601 19990108 00601 WP 1999 1 8 HALA9800364 1 19981025 A 2510 SEAT DOUG DC10 DC1010 3022110 WP COCKPIT MALFUNCTIONED A A HALA O OTHER B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 WP 13 116AA 46516 SFO - FLT 11 - SMOKE IN COCKPIT. REMOVED AND REPLACED FE SEAT, OPS CHECK GOOD. (M) 2 L 7 3 4F A22WE 1999010800602 19990108 00602 EU 1999 1 8 99ZZZM15 1 19980530 A 2120 DUCT BAG BAE146 BAE146200A 1500266 EU NR 2 PACK CONTAMINATED A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 181US E2042 WHEN TURNING ON PACKS, AFTER ENGINE START PLUS ON TAXI OUT. FLIGHT ATTENDANTS REPORT SMOKE IN THE CABIN AND GETTING WOR SE. DUCT NR 2 AT45 DEG WITH TEMP CONT AUTO AND FULL COLD, SEL MAN AND FULL COLD TOOK 3 TO 4 MINUTES TO 0 DEGREES. FLIG HT ATTENDANTS REPORT EXHAUST SMELL. COMPLIED WITH MM SUP 96-31 DUCT CLEARING PROCEDURE ON NR 1 AND NR 2 PACK, OPERATED ON ALL ENGINE AIR SYSTEM AND APU AIR AFTER CLEARING PROCEDURE. NO SMOKE OR DEFECTS NOTED. (M) 2 H 7 4 4F RT A49EU 1999010800603 19990108 00603 WP 1999 1 8 99ZZZM16 1 19981101 A 2820 10648LD1111 SWITCH LKHEED 1011 10113851 5265010 WP COCKPIT INTERMITTENT A AMTA O OTHER P X NO WARNING INDICATION ENGINE FLAMEOUT DE DESCENT 1 GL 11 195AT 193P1041 DURING DESCENT, THE NR 3 ENGINE MADE UNSCHEDULED RUN DOWN WHEN TANK NR 3 QTY WENT EMPTY. ENGINE NR 3 WAS ON CROSSFEED F ROM TANK 2L AND 2R. LANDED SAFELY. REPLACED RIGHT CROSSFEED SWITCH LIGHT ASSY, CROSSFEED VALVE WAS ALSO REPLACED FOR P RECAUTIONARY MEASURES. ALL SYSTEMS CHECKED NORMAL. SUBMITTER STATES, FURTHER INVESTIGATION REVEALED CREW MISMANAGMENT ALSO. 2 L 7 3 4F A23WE 1999010800604 19990108 00604 WP 1999 1 8 USAAD98205 1 19981116 A 5210 5956563227 SEAL DOUG DC9 DC931 3022065 WP PASSENGER DOOR DAMAGED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 933VJ 47216 PIT-PWM - FLT 1274 - AFTER TAKEOFF A NOISE WAS HEARD AT THE FORWARD MAIN ENTRY DOOR. THE NOISE STOPPED AND THEN STARTED AGAIN. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE ENVIRONMENTAL SEAL DAMAG ED AND HANGING OUT OF THE DOOR. THE DAMAGED PART OF THE SEAL WAS REMOVED THE PART PROGRAMMED FOR REPLACEMENT. (M) 2 L 7 2 4F A6WE 1999011500001 19990115 00001 WP 1999 1 15 TWAA9820002 1 19981222 A 4940 EXCITOR DOUG DC9 DC982 3022082 WP APU SHORTED A TWAA O OTHER H ELECT. POWER LOSS-50 PC CR CRUISE 1 CE 05 959U 49704 THE LT CSD TEMP WAS HIGH AND CREW DISCONNECTED THE CSD. ATTEMPTED TO START APU FOR GENERATOR BUT APU WOULD NOT START. C ORRECTED THE APU BY REPLACING THE OIL PRESS SEQUENCE SWITCH, MFG 692525-9, THE IGNITION COIL, MFG 10-381175-9, AND THE I GNITOR PLUG MFG CH31723. PLACARDED THE CSD INOPERATIVE PER MEL. MAINTENANCE LATER FOUND THE CSD OIL LEVEL LOW AND THE SCAVENGE FILTER DIFFERENTIAL PRESSURE INDICATOR POPPED. REPLACED THE CHARGE AND SCAVENGE FILTER PRECAUTIONARY. CSD SER VICED TO PROPER LEVEL. THE APU IGNITION EXCITOR THAT WAS REPLACED WAS FOUND IN THE SHOP TO HAVE AN INTERNAL SHORT WHICH CAUSED THE APU TO NOT START. CHECK-C 10-10-98 STL. 2 L 7 2 4F A6WE 1999011500004 19990115 00004 WP 1999 1 15 AT9900003 1 19981227 A 5320 SKIN DOUG DC9 DC932 3022066 WP BS 242 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL, DENT IS CREASED OUT OF LIMITS AT FS 242 LB 19L PER DC9 SRM 53-04 FIG 38 SHEET 1 0 REFERENCE 099650 PAGE 1 OF 4. FABRICATED DOUBLER FROM 2024 T3 .063 PO NR 675752 AND INSTALLED PER DC9 SRM 53-04 FIG 3 8 AND RES 982292. 2 L 7 2 4F A6WE 1999011500005 19990115 00005 NM 1999 1 15 VJ9900004 1 19981207 A 5320 ANGLE BOEING 737 7372L9 1384497 NM GALLEY CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL, THE G-1 GALLEY LEFT SIDEWALL FORWARD CORNER ANGLE WAS FOUND BENT AND CORRODED AT THE BOTTOM. CUT OUT CORROSION. CUT TO FIT NEW ANGLE AND INSTALLED IAW B737 SRM 51-40-4, AND 51-30-2. 2 L 7 2 4F RT A16WE 1999011500006 19990115 00006 NM 1999 1 15 K3AH980151 1 19981231 A 3397 WIRE BOEING 727 727225 1384077 NM ROW 32 DEF BROKEN A K3HA K NONE L NO TEST IN INSP/MAINT 1 EA 25 8880Z 21453 EMERGENCY PATH LIGHTING ROW 32DEF IS NOT ILLUMINATED. REPAIRED BROKEN WIRE BY SPLICING AND CRIMPING WITH UNION PER MM 3 3-59-00. 2 L 7 3 4F A3WE 1999011500022 19990115 00022 NM 1999 1 15 SCNA98158 1 19981231 A 3350 900835A BATTERY PACK BOEING 727 7272J4 1384006 NM R2 DOOR DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 290SC 20764 DURING A LINE MAINTENANCE CHECK, THE R2 DOOR OVERHEAD EXIT EMERGENCY LIGHT WAS FOUND TO BE FLASHING. REMOVED AND REPLAC ED THE BATTERY. SYSTEM OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F RT A3WE 1999011500031 19990115 00031 NM 1999 1 15 AT9900004 1 19981216 A 5311 FRAME BOEING 737 7372L9 1384497 NM BS 360 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 465AT 21528 SCHEDULED INSPECTION AT AERO CORP, FL. FASTENERS AT ATTACH POINT FOR CIRCUMFERENTIAL RING AT STA 360, STR 22L AND STR 2 3L WERE FOUND SHEARED, CORRODED, AND WITH SHARP GOUGES. MECHANICALLY REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED SHEARED FASTENERS, BLENDED GOUGES AND INSTALLED ANGLE IAW B737 SRM'S 51-40-3, 51-30-2, 51-10-2, 51-10-6, AND 51-10-1 AND MM 51-21-31. (X) 2 L 7 2 4F RT A16WE 1999011500038 19990115 00038 NM 1999 1 15 AWXA9800244 1 19981219 A 2130 PRESSURIZATION BOEING 737 7373G7 1384595 NM CABIN MALFUNCTIONED A AWXA A G UNSCHED LANDING O2 MASK DEPLOYED J WARNING INDICATION CL CLIMB 1 WP 28 160AW 23782 AIRCRAFT DECOMPRESSED AT 23,000 FT, STANDBY AND MAIN DID NOT WORK AS OUT FLOW VALVE STAYED IN CLOSE POSITION FLT ATTENDA NTS IN REAR OF A/C HEARD A LOUD NOISE SHORTLY BEFORE MASK DROPPED SUSPECT LOUD NOISE THAT WAS HEARD WAS OUTFLOW VALVE OP EN. PERFORMED PRESSURIZATION INTEGRITY CHECK AS PER AMERICA WEST CARD F1B21006. NO EVIDENCE OF LEAKS WERE NOTED A/C TO OK 135 SEC TO BLEED DOWN FROM 4.0 TO 2.5 PSI. NO ANOMALIES WERE NOTICED PRESSURIZATION INDICATION WAS NORMAL A/C OK FOR SERVICE. 2 L 7 2 4F RT A16WE 1999011500039 19990115 00039 NM 1999 1 15 AWXA9800245 1 19981223 A 3350 849029 FUSE BOEING 737 73733A 1384673 NM CABIN BLOWN A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 168AW 23629 DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHTS INOP ON FIRST 5 ROWS AND FLOOR LIGHTS AT R1 AND L1. REPLACED F USE IN FWD FLOOR BATTERY PACK OPS CK GOOD. 2 L 7 2 4F RT A16WE 1999011500040 19990115 00040 NM 1999 1 15 AWXA9800246 1 19981227 A 5330 SKIN BOEING 737 737277 1384570 NM BS 747 CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 188AW 22655 LT FUSELAGE SKIN CRACKED AT STA 747 STR 17L. VERIFIED WITH HFEC. ROUTED DAMAGE PER SRM 53-30-03. FABRICATED DOUBLER A ND TRIPLERS FROM .063 2024 T3 AND .050 2024 T3 IAW ER 2-53-30-03. 2 L 7 2 4F RT A16WE 1999011500041 19990115 00041 NM 1999 1 15 AWXA9800247 1 19981224 A 3350 335007 LIGHT BOEING 737 7372E3 NM R2 DOOR INOP A AWXA K NONE L NO TEST IN INSP/MAINT 1 WP 28 138AW 22792 R2 DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICABLE UNIT, OPS NORMAL. 2 L 7 2 4F RT A16WE 1999011500044 19990115 00044 NM 1999 1 15 AWXA9900003 1 19981231 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7373G7 1384595 NM BS 986 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 302AW 24009 FOUND DURING ROUTINE MAINTENANCE CK, FLOORBEAM AT BS986 FROM L-2 DOOR TO R-2 DOOR. PREVIOUS REPAIR HAS EXFOLIATION CORR OSION (LBL 45). REPAIRED PER SRM 53-00-51, 51-70-12 AND ER 3-53-16-44. 2 L 7 2 4F RT A16WE 1999011500045 19990115 00045 SO 1999 1 15 PNSA981201 1 19981230 A 7331 6331H95 INDICATOR PIPER PA32 PA32301 7103207 SO FUEL FLOW MALFUNCTIONED A PNSA A UNSCHED LANDING O OTHER CR CRUISE 1 AL 03 8259V 53612 328006097 PILOT REPORTED ENGINE SOUNDED SLIGHTLY ROUGH AND FUEL FLOW WAS INDICATING LOW. AIRCRAFT RETURNED TO BASE. FUEL NOZZLES , FILTERS AND HOSES WERE CLEANED AND PURGED. NO FOREIGN MATERIAL WAS FOUND. REPLACED FUEL FLOW INDICATOR AND PURGED SE NSE LINE. NO FURTHER PROBLEMS WERE NOTED. 1 L 7 1 3O A3SO 1999011500046 19990115 00046 SW 1999 1 15 PNSA981202 1 19981211 A 5230 VALVE SWRNGN SA227 SA227AC 8780603 SW CARGO DOOR ICED UP A PNSA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 03 2719H AC713B ON CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE AND RETURNED TO BASE. CARGO DOOR SEAL INFLATION VALVE WAS FOUND TO HAVE ICE IN ITS CONTROL LINE. THE LINE WAS THAWED AND PURGED. NO FURTHER PROBLEMS WERE NOTED. 2 L 7 2 4T RT A8SW 1999011500047 19990115 00047 EU 1999 1 15 PNSA981203 1 19981215 A 2432 40787 BATTERY SAAB SF340 340B 7860101 EU BATTERY COMPT DISCHARGED A PNSA K NONE O OTHER TX TAXI/GRND HDL 1 AL 03 675PA 1393 206 FIRST START ATTEMP FAILED. BATTERIES WERE WEAK. OAT WAS VERY LOW. TOP CHARGED BATTERIES, SUBSEQUENT STARTS OK. 2 L 7 2 4T RT A52EU 1999011500048 19990115 00048 1999 1 15 PNSA981204 3 19981209 A 6112 DEICE SYST SAAB SF340 340B 7860101 EU PROPELLER MALFUNCTIONED A PNSA K NONE O OTHER UK UNKNOWN 1 AL 03 675PA 206 PILOT REPORTED, THAT PROPS WOULD NOT SHED ICE IN NORMAL MODE. FLIGHT WAS DELAYED WHILE SYSTEM WAS FUNCTIONALLY TESTED. NO DISCREPANCIES WERE NOTED AND NO FURTHER PROBLEMS WERE ENCOUNTERED WITH THE PROP DEICE SYSTEM. 2 L 7 2 4T RT A52EU 1999011500049 19990115 00049 WP 1999 1 15 9811099752 1 19981228 A 5312 BULKHEAD DOUG DC9 DC941 302207N WP BS 1072 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 752NW 47116 DURING PERIODIC CHECK, FOUND CRACKS AT FS 1072 VENTRAL DOOR LOCATIONS AT LOWER RIGHT CORNER .375 INCHES IN LENGTH AND FO RWARD TOP LEFT CORNER. REPAIRED PER EA 97-163523. 2 L 7 2 4F A6WE 1999011500050 19990115 00050 WP 1999 1 15 9811101159 1 19981120 A 5330 SKIN DOUG DC10 DC1040 3023508 WP BS 1509-1521 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 159US 46768 DURING M CHECK, FOUND CORROSION ON INTERIOR SURFACE SKIN AT CENTER WHEEL WELL, LONGERON 48L TO 48R, FS 1509 TO 1521. RE PAIRED PER EA 11-161113, MFG PART NUMBER AYB7065-. 2 L 7 3 4F A22WE 1999011500051 19990115 00051 WP 1999 1 15 9811129752 1 19981230 A 5312 BULKHEAD WEB DOUG DC9 DC941 302207N WP AFT PRESS BLKHD CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 752NW 47116 DURING PERIODIC CHECK, FOUND AFT PRESSURE BULKHEAD WEB CRACKED AT RIGHT SIDE DOOR BELOW NR 2 RIB. CRACK EXTENDS .5 INCH ES OUT FROM SCREW. REPAIRED PER EA 97-163442. 2 L 7 2 4F A6WE 1999011500058 19990115 00058 EU 1999 1 15 QXEA9801890 1 19981108 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT WING 71A APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAG E 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999011500059 19990115 00059 EU 1999 1 15 QXEA9801891 1 19981108 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT WING 73A APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAG E 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999011500060 19990115 00060 EU 1999 1 15 QXEA9801892 1 19981108 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT WING 73B APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAG E 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999011500061 19990115 00061 EU 1999 1 15 QXEA9801893 1 19981108 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT WING 73C APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAG E 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999011500062 19990115 00062 EU 1999 1 15 QXEA9801894 1 19981108 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU LT WING CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT WING 73D APERTURE HAS LIGHT FRETTING CORROSION AROUND ALL SCREW HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAG E 9 4B 1-2. 2 L 7 2 4F RT A20EU 1999011500063 19990115 00063 EU 1999 1 15 QXEA9801895 1 19981114 A 5720 STRAP FOKKER F28 F28MK4000 4990810 EU WS 1700 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT WING ROOT/CENTER WING LOWER SKIN JOINT STRAP GOUGED .045 DEEP AT WING STATION 1700 FUSELAGE STATION 11500. R EPAIRED IAW HORIZON AIR EA 4-57-137 AND FOKKER SRM 51-10-04, PAGE 8, PARAGRAPH C. 2 L 7 2 4F RT A20EU 1999011500064 19990115 00064 EU 1999 1 15 QXEA9801896 1 19981126 A 5720 ANGLE FOKKER F28 F28MK4000 4990810 EU RT WING CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - RIGHT WING LOWER CONNECTION ANGLE AT MAIN LANDING GEAR BRACKET TO REAR SPAR IS CRACKED. REPAIRED IAW FOKKER SRM 5 1-31-05. 2 L 7 2 4F RT A20EU 1999011500065 19990115 00065 EU 1999 1 15 QXEA9801897 1 19981118 A 5541 RIB FOKKER F28 F28MK4000 4990810 EU RUDDER CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - RUDDER RIB 5 CRACKED AT LEFT AND RIGHT STRINGER CLIPS. REPAIRED IAW HORIZON AIR EA 4-55-105. 2 L 7 2 4F RT A20EU 1999011500066 19990115 00066 EU 1999 1 15 QXEA9801898 1 19981112 A 5520 STRUCTURE FOKKER F28 F28MK4000 4990810 EU HORIZ STAB GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - SHARP GOUGE AFT LOWER LIP OF LIGHTNING HOLE THAT STABILIZER ACTUATOR FITS THROUGH IN TOP AFT OF 56G. REPAIRED IAW FOKKER SRM 55-02-05, PAGE 7, VIEW A. 2 L 7 2 4F RT A20EU 1999011500067 19990115 00067 EU 1999 1 15 QXEA9801899 1 19981111 A 5522 SKIN FOKKER F28 F28MK4000 4990810 EU LT ELEVATOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - LEFT ELEVATOR HAS A DENT IN THE LOWER SKIN BETWEEN CENTER AND INBOARD HINGE 14 FROM TRAILING EDGE. REPAIRED IAW F OKKER SRM 51-70-0, PAGE 2, PARAGRAPH 3. 2 L 7 2 4F RT A20EU 1999011500068 19990115 00068 EU 1999 1 15 QXEA9801900 1 19981120 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 58.5-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CLIP CRACKED AT FRAME 58.5-2 AFT SIDE ABOVE STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 AND SRM 51-31-0 1. 2 L 7 2 4F RT A20EU 1999011500069 19990115 00069 EU 1999 1 15 QXEA9801901 1 19981120 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 58.5-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CLIP CRACKED AT FRAME 58.5-2 AFT SIDE ABOVE STRINGER 29. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 6 AND SRM 51-31-0 1. 2 L 7 2 4F RT A20EU 1999011500070 19990115 00070 EU 1999 1 15 QXEA9801902 1 19981118 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CLIP CRACKED FORWARD SIDE FRAME 32-2, STRINGER 48. REPAIRED IAW FOKKER SRM 51-31-01, 51-30-02 AND 53-02-13, PAGE 5. 2 L 7 2 4F RT A20EU 1999011500071 19990115 00071 EU 1999 1 15 QXEA9801903 1 19981118 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 24-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CRACK PAST STOP DRILL ON CLIP FRAME 24-2, STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01, PAGES 13-17, SRM 51-30-0 2, PAGE 9, PARAGRAPH 4B THROUGH PAGE 15 AND SRM 53-02-13, PAGE 6, FIGURE 4. 2 L 7 2 4F RT A20EU 1999011500072 19990115 00072 EU 1999 1 15 QXEA9801904 1 19981119 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 AFT CLIP CRACKED ON FRAME 20075 AT STRINGER 39 AND 41. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-10-05 PAGE 603. 2 L 7 2 4F RT A20EU 1999011500073 19990115 00073 EU 1999 1 15 QXEA9801905 1 19981129 A 5753 65192709 TRACK FOKKER F28 F28MK4000 4990810 EU TE FLAP CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 SO 27 479AU 11228 LIGHT CORROSION TO MLG BEAM BOLT HOLES, SPOILER BEAM BOLT HOLES, AND AFT MLG DOOR HINGE FITTING BOLT HOLES. REAMED HOLE S TO REMOVE CORROSION. MLG BEAM BOLT HOLES OVERSIZED AND LEFT AS-IS. SPOILER BEAM BOLT HOLES BUSHED. AFT MLG DOOR HIN GE FITTING BOLT HOLES OVERSIZED AND OVERSIZED BOLT INSTALLED. 2 L 7 2 4F RT A20EU 1999011500074 19990115 00074 EU 1999 1 15 QXEA9801907 1 19981130 A 5210 ANGLE FOKKER F28 F28MK4000 4990810 EU PAX DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - TWO ANGLES ON LOWER AFT SIDE NEAR HINGE ON MAIN CABIN DOOR HAVE CORROSION. REPAIRED IAW HORIZON AIR 4-52-113B. 2 L 7 2 4F RT A20EU 1999011500075 19990115 00075 EU 1999 1 15 QXEA9801908 1 19981112 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - FUSELAGE SKIN UNDER LOWER COMM VHF ANTENNA HAS LIGHT CORROSION. REPAIRED IAW FOKKER SRM 53-01-01, PARAGRAPH 4C. 2 L 7 2 4F RT A20EU 1999011500076 19990115 00076 EU 1999 1 15 QXEA9801909 1 19981119 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON FUSELAGE SKIN UNDER UPPER NAV COMM ANTENNA. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999011500077 19990115 00077 EU 1999 1 15 QXEA9801910 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - NUMEROUS DEEP GOUGES ON TOP OF SEAT TRACK BL1127R, FRAME 6305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999011500078 19990115 00078 EU 1999 1 15 QXEA9801911 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - NUMEROUS GOUGES IN CENTER OF SEAT TRACK BL1127R, JUST FORWARD OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAG E 8, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999011500079 19990115 00079 EU 1999 1 15 QXEA9801912 1 19981119 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - NUMEROUS GOUGES IN CENTER OF SEAT TRACK BL600R, JUST FORWARD OF FRAME 6305. REPAIRED IAW FOKKER SRM 53-40-01, FIG URE 204. 2 L 7 2 4F RT A20EU 1999011500080 19990115 00080 EU 1999 1 15 QXEA9801913 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - GOUGES AND NICKS IN CENTER OF SEAT TRACK BL1127R, 6 1/2 AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-04,PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999011500081 19990115 00081 EU 1999 1 15 QXEA9801914 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - NICKS AND GOUGES IN CENTER OF SEAT TRACK BL1127R, 14 AFT OF FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999011500084 19990115 00084 SO 1999 1 15 SWIA971355 1 19981228 A 3010 DEICE BOOT EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT WING TORN A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 209SW 120269 ALL INBOARD BOOTS FAILED STAB AND WING. RETURNED TO SLC. INSTALLED PATCH ON SMALL TEAR IN LEFT INBOARD WING BOOT. SET FOR 20 MINUTES. RUN UP OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500085 19990115 00085 1999 1 15 SWIA971356 4 19981230 A 3422 6225812004 FLUX DETECTOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 188SW 120039 NUMBER 2 AHRS FAILURE IN FLIGHT, NO GYRO ON FO SIDE. RETURNED TO SLC. MEL 12-30-98. REMOVED AND REPLACED NUMBER 2 RIG HT FLUX DETECTOR AND ADJUSTED SYSTEM. WORK DONE IAW MM 34-21-03. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500126 19990115 00126 WP 1999 1 15 AT9900007 1 19981228 A 5312 BULKHEAD WEB DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. AFT PIT AT STA 996 SECONDARY BULKHEAD JUST UNDER FLOOR AREA AT FS 24R HAS BLOWN OUT CORROSION ON WEB. FABRICATED AND INSTALLED REPAIR IAW RES 982280, DC9 SRM 51-10-2, 51-30-2, 51-10-4 AND 51-10-3. 2 L 7 2 4F A6WE 1999011500128 19990115 00128 WP 1999 1 15 AT9900009 1 19981226 A 5532 SKIN DOUG DC9 DC932 3022066 WP VERTICAL STAB CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. VERTICAL STABILIZER UPPER LEADING EDGE SKIN CHAFED LEFT AND RIGHT. FABRICATED R EPAIR AND INSTALLED IAW RES 982239, SRM DC9 51-10-20, 55-31-0, 51-10-4, 51-10-3, 51-30-5, AND 51-20-0. 2 L 7 2 4F A6WE 1999011500160 19990115 00160 NM 1999 1 15 DL72K990006 1 19981231 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 TYP CORROSION TO MLG BEAM BOLT HOLES, SPOILER BEAM BOLT HOLES AND AFT MLG DOOR HINGE FITTING BOLT HOLES. REAMED HOLES T O REMOVE CORROSION. MLG BEAM BOLT HOLES OVERSIZED AND LEFT AS-IS. SPOILER BEAM BOLT HOLES BUSHED. AFT MLG DOOR HINGE FITTING BOLT HOLES OVERSIZED AND OVERSIZED BOLT INSTALLED. 2 L 7 3 4F A3WE 1999011500161 19990115 00161 NM 1999 1 15 DL72K990007 1 19981231 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORROSION A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 CORROSION FOUND IN BORE OF MLG BEAM ATTACH HOLE. HOLE REAMED-UP AND LEFT OVERSIZED. CORROSION FOUND IN BORES OF AFT ML G DOOR HINGE FITTING. HOLES REAMED-UP AND OVERSIZE BOLT INSTALLED. 2 L 7 3 4F A3WE 1999011500170 19990115 00170 NM 1999 1 15 DL72W990022 1 19980105 A 5330 SKIN BOEING 727 727247 138408F NM FUSELAGE CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2820W 21058 FOUND ON A2 LETTER CK, .375 INCH CRACK LOWER I/B FASTENER HOLE AT THE L-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3. 2 L 7 3 4F A3WE 1999011500184 19990115 00184 NM 1999 1 15 DL72W990042 1 19981215 A 5320 ANGLE BOEING 727 727247 138408F NM AFT AIRSTAIR CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 A 2 INCH VISIBLE CRACK RT LOWER TORQUE BOX SUPPORT ANGLE BELOW AIRSTAIR ACTUATOR ATTACH FITTING STA 1263 RT (MARKED). R EPLACED PART PER SRM 53-10-10. 2 L 7 3 4F A3WE 1999011500219 19990115 00219 SO 1999 1 15 99ZZZX183 1 19980518 A 5720 SE3580790211 ANGLE GULSTM G1159 G1159 3953505 SO LT/RT WING CRACKED A BJYA K NONE O OTHER IN INSP/MAINT 1 EA 23 565KC 3912 046 LEFT AND RIGHT WING FIXED TRAILING EDGE VERTICAL BREATHER ANGLES WERE CRACKED AND PER MM, REQUIRED REPLACEMENT. ANGLES WERE REPLACED PER GULFSTREAM REPAIR 'SE3580790' (INSTALLATION OF STAINLESS ANGLES) FOR A PERMANENT FIX. HOWEVER, THE A NGLES THAT WERE REMOVED WERE ALREADY STAINLESS. REPLACED IN DECEMBER, 1990. 2 L 7 2 4F RT A12EA 1999011500220 19990115 00220 SO 1999 1 15 99ZZZX184 1 19980518 A 5720 SE3580790212 ANGLE GULSTM G1159 G1159 3953505 SO LT/RT WING CRACKED A BJYA K NONE O OTHER IN INSP/MAINT 1 EA 23 565KC 3912 046 LEFT AND RIGHT WING FIXED TRAILING EDGE VERTICAL BREATHER ANGLES WERE CRACKED AND PER MM, REQUIRED REPLACEMENT. ANGLES WERE REPLACED PER GULFSTREAM REPAIR 'SE3580790' (INSTALLATION OF STAINLESS ANGLES) FOR A PERMANENT FIX. HOWEVER, THE A NGLES THAT WERE REMOVED WERE ALREADY STAINLESS. REPLACED IN DECEMBER, 1990. 2 L 7 2 4F RT A12EA 1999011500222 19990115 00222 CE 1999 1 15 99ZZZX186 1 19981124 A 3260 1CH16 SWITCH LEAR 35 35A 5170602 CE LT MLG MALFUNCTIONED A BSYA O OTHER N FALSE WARNING LD LANDING 1 GL 07 27TT 0122 AIRCRAFT WAS ON APPROACH TO BVR, SELECTED GEAR DOWN, HAD NO GREEN LIGHT ON LEFT MAIN GEAR, DID A FLY-BY, TOWER REPORTED GEAR DOWN BUT NO LANDING LIGHT. AIRCRAFT LANDED. WHEN LANDING, AS SOON AS AIRCRAFT TOUCHED DOWN, LEFT GREEN LIGHT CAME ON. MAINTENANCE FOUND LEFT DOWN AND LOCK SWITCH DEFECTIVE. REPLACED AND GEAR TEST WAS NORMAL. ALL LIGHTS NORMAL. 2 L 7 2 4F A10CE 1999011500235 19990115 00235 NM 1999 1 15 A6WA9800003 1 19980903 A 2120 PACK DORNER DO32 DO328100 2996000 NM AC BAY MALFUNCTIONED A A6WA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 328PH 3006 DEN - FLT 7435 - 'SMOKE LAV' CAUTION APPEARED WHILE TAXIING. F/A REPORTED SMOKE IN CABIN. INSPECTED LAV TRASH CAN FOR SMOKE/FIRE. NONE NOTED. SUBMITTER SUSPECTED LEFT PACK OVERHEATED. RAN AIRCRAFT WITH BOTH PACKS. NORMAL OPERATION OF HP FANS. NO DEFECTS NOTED. (X) 2 H 7 2 4T RT A45NM 1999011500236 19990115 00236 EA 1999 1 15 ASOA98080 1 19981012 A 2750 865D1007 DRIVE UNIT CNDAIR CL600 CL6002B19 EA CABIN FAILED A ASOA O OTHER F FLT CONT AFFECTED AP APPROACH 1 SO 11 832AS 793 7243 ATL/GPT - FLT 7533 - DURING APPROACH WHEN MOVING FLAPS FROM 30 TO 45 DEGREES, FLAP FAIL MESSAGE ILLUMINATED AND FLAPS LO CKED AT APPROXIMATELY 41 DEGREES. REQUESTED EMERGENCY EQUIPMENT TO BE STANDING BY AS A PRECAUTION. LANDING WAS MADE SA FELY IN GPT WITHOUT FURTHER INCIDENT. AIRCRAFT WAS INSPECTED AND FOUND SAFE FOR A FERRY FLIGHT TO ATL FOR REPAIR. ATL MAINTENANCE REMOVED AND REPLACED THE POWER DRIVE UNIT. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR F URTHER SERVICE. (X) 2 L 7 2 4F RT A21EA 1999011500237 19990115 00237 EA 1999 1 15 ASOA98082 1 19981019 A 2611 473052 SMOKE DETECTOR CNDAIR CL600 CL6002B19 EA CARGO BAY MALFUNCTIONED A ASOA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 11 821AS 2378 7194 ALT/ROA - FLT 7273 - ON CLIMB-OUT THROUGH 9,000 FEET, CARGO SMOKE LIGHT CAME ON ONCE FOR ABOUT 2 SECONDS. CREW CONTACTE D MTC CNTL AND WERE INSTRUCTED TO RETURN TO ATL. RECEIVED OTHER MOMENTARY WARNINGS DURING 10 MILE FINAL APPROACH. LAND ING MADE SAFELY IN ATL WITHOUT FURTHER INCIDENT AND AIRCRAFT WAS TAXIED TO THE GATE. ATL MAINTENANCE REMOVED AND REPLAC ED BOTH CARGO COMPARTMENT SMOKE DETECTORS. OPERATIONAL TESTS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVIC E. (X) 2 L 7 2 4F RT A21EA 1999011500238 19990115 00238 EU 1999 1 15 FJT98109440 1 19981013 A 2910 1379305A77 LINE BAG JETSTM JETSTM3201 1500217 EU RT NACELE CHAFED A FJTA O OTHER K FLUID LOSS CR CRUISE 1 SO 03 944AE 104 944 ORF - FLT 1044 - LOST ALL HYDRAULIC PRESSURE IN-FLIGHT EN ROUTE TO ORF. AN EMERGENCY MANUAL GEAR EXTENSION WAS PERFORME D ON APPROACH. ACFT LANDED SAFELY AND TAXIED TO THE GATE. REMOVED AND REPLACED RT ENGINE PUMP HYDRAULIC PRESSURE FLEX LINE. THE LINE HAD A PIN HOLE CHAFED THROUGH THE STEEL BRAIDED SIDE OF THE LINE WHERE IT CHAFED AGAINST THE SS COMBUSTI ON DRAIN LINE. THE DRAIN LINE WAS REPLACED. ALSO, THE RT HYDRAULIC PUMP WAS REPLACED AS A PRECAUTIONARY MEASURE. THE HYDRAULIC SYSTEM WAS SERVICED WITH MIL 5606, AND BLED. ACFT RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999011500239 19990115 00239 NM 1999 1 15 HNAA9899445 1 19980902 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM ROW 4 DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 994HA 2895 JAX141 459 TPA/TLH - FLT 3327 - DURING PRE-FLIGHT INSPECTION, OVERHEAD EMERGENCY LIGHT INOPERABLE AT ROW 4. REMOVED AND REPLACED E MERGENCY BATTERIES 3351 PSI - PS4. OPS CHECK GOOD. REF: OPER CNTRL NR 99ZZZX150, 99ZZZX151, AND 99ZZZX152. (X) 2 H 7 2 4T RT A13NM 1999011500240 19990115 00240 NM 1999 1 15 99ZZZX150 1 19980902 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM ROW 4 DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 994HA 1212 SBY112 459 TPA/TLH - FLT 3327 - DURING PRE-FLIGHT INSPECTION, OVERHEAD EMERGENCY LIGHT INOPERABLE AT ROW 4. REMOVED AND REPLACED E MERGENCY BATTERIES 3351 PSI - PS4. OPS CHECK GOOD. REF: OPER CNTRL NR HNAA9899445, 99ZZZX151, AND 99ZZZX152. 2 H 7 2 4T RT A13NM 1999011500241 19990115 00241 NM 1999 1 15 99ZZZX151 1 19980902 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM ROW 4 DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 994HA 18609 JAX042 459 TPA/TLH - FLT 3327 - DURING PRE-FLIGHT INSPECTION, OVERHEAD EMERGENCY LIGHT INOPERABLE AT ROW 4. REMOVED AND REPLACED E MERGENCY BATTERIES 3351 PSI - PS4. OPS CHECK GOOD. REF: OPER CNTRL NR HNAA9899445, 99ZZZX150, AND 99ZZZX152. (X) 2 H 7 2 4T RT A13NM 1999011500242 19990115 00242 NM 1999 1 15 99ZZZX152 1 19980902 A 3350 6013211X BATTERY GRIMES DHAV DHC8 DHC8102 2809003 NM ROW 4 DISCHARGED A HNAA K NONE L NO TEST TX TAXI/GRND HDL 1 EA 07 994HA 3682 JAX108 459 TPA/TLH - FLT 3327 - DURING PRE-FLIGHT INSPECTION, OVERHEAD EMERGENCY LIGHT INOPERABLE AT ROW 4. REMOVED AND REPLACED E MERGENCY BATTERIES 3351 PSI - PS4. OPS CHECK GOOD. REF: OPER CNTRL NR HNAA9899445, 99ZZZX150, AND 99ZZZX151. 2 H 7 2 4T RT A13NM 1999011500243 19990115 00243 EU 1999 1 15 HCMA0000218 1 19981027 A 6520 350A33215300 HINGE LAMINATE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR TORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 313 2889 HINGE LAMINATE IS TORN BEYOND LIMITS AND THERE IS NO 'J' GAP. (X) 1 G 7 1 3U H9EU 1999011500244 19990115 00244 EU 1999 1 15 HCMA0000217 1 19980821 A 6520 35A33215300 HINGE LAMINATE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR TORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 275 2889 HINGE LAMINATE IS TORN BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1999011500245 19990115 00245 EU 1999 1 15 HCMA0000216 1 19980701 A 6520 350A33215300 HINGE LAMINATE SNIAS 350 AS350B2 8680813 EU TAIL ROTOR TORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 992BH 745 2889 HINGE LAMINATE IS TORN BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1999011500246 19990115 00246 NM 1999 1 15 99ZZZX153 1 19980929 A 3350 LIGHT GRIMES DHAV DHC8 DHC8103 1386005 NM CABIN MALFUNCTIONED A KPVA K NONE O OTHER IN INSP/MAINT 1 WP 13 805WP 60266 353 HNL - DURING PRE-FLIGHT INSPECTION ACCOMPLISHED BY THE FLIGHT CREW, THE PORTABLE EMERGENCY LIGHTS WOULD NOT EXTINGUISH W ITH THE EMERGENCY LIGHT SWITCH LOCATED IN THE COCKPIT. 2 H 7 2 4T RT A13NM 1999011500247 19990115 00247 EA 1999 1 15 MASA98191 1 19981028 A 3350 100865 POWER SUPPLY BRUCE CNDAIR CL600 CL6002B19 EA E/E BAY INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7264V 7264 WHILE PERFORMING ROUTINE MAINTENANCE, FOUND THE FORWARD EXTERIOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE TRO UBLESHOT AND FOUND THE NR 1 EMERGENCY LIGHT POWER SUPPLY FAILED. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY, OPS CHECK GOOD. (X) 2 L 7 2 4F RT A21EA 1999011500248 19990115 00248 NE 1999 1 15 PLGA981023A 2 19981023 A 7210 6044T3TP10 PROP GEARBOX SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE MALFUNCTIONED A PLGA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 NE 05 336BE UDGA0021 340A028 PHL - FLT 4307 - AFTER TAKEOFF, CREW RECEIVED A LOW OIL PRESSURE WARNING ON RIGHT ENGINE. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL ON RIGHT PRO PELLER GEARBOX CHIP DETECTOR. THE RIGHT PGB WAS REPLACED, ENGINE GROUND RUN PER GE MM AND FOUND GOOD FOR RETURN TO SERV ICE. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1999011500249 19990115 00249 GL 1999 1 15 RAIA981014 2 19981024 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 801HK 1037 145053 310126 ROA - FLT 5789 - NR 2 ENGINE LOW N1 LIGHT CAME ON, EGT WAS 921. MAINTENANCE REPLACED NR 2 ENGINE. (X) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999011500250 19990115 00250 1999 1 15 99ZZZX154 4 19981020 A 3434 066102101 MARKER BEACON UROCOP EC135 EC135P1 8680990 EU FUSELAGE MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 28 11979 EC1350054 MARKER BEACON HAD INTERNAL SHORT. CIRCUIT BREAKER TRIPPED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999011500251 19990115 00251 EU 1999 1 15 99ZZZX155 1 19981017 A 2422 SPC10 INVERTER UROCOP EC135 EC135P1 8680990 EU NACELLE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 28 180 EC1350054 INVERTER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999011500252 19990115 00252 EU 1999 1 15 99ZZZX156 1 19981024 A 2422 SPC10 INVERTER UROCOP EC135 EC135P1 8680990 EU NACELLE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 20 103 EC1350054 INVERTER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999011500253 19990115 00253 EU 1999 1 15 99ZZZX157 1 19981020 A 2510 L311M1038205 PIN UROCOP EC135 EC135P1 8680990 EU CYCLIC CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 36 EC1350054 PIN CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999011500254 19990115 00254 EA 1999 1 15 S9BA9808 1 19980909 A 6120 C6CF11501 CONTROL CABLE DHAV DHC6 DHC6300 2802606 EA PROP CONTROL CORRODED A S9BA K NONE O OTHER IN INSP/MAINT 1 AL 05 224SA 247 WHILE PERFORMING NON-ROUTINE MAINTENANCE, MAINTENANCE CREW FOUND THE RT PROPELLER CONTROL LEVER NOT LOCKING IN AFT DETEN T. ON FURTHER INVESTIGATION, FOUND THE PROPELLER CONTROL CABLE IN THE RT LEADING EDGE WAS CORRODED AND HAD FAILED. THE CABLE WAS REPLACED AND THE ENTIRE AIRCRAFT CABLE SYSTEM WAS INSPECTED FOR CORROSION. NO OTHER CABLES WERE FOUND TO BE OUT OF LIMITS. THE ACFT WAS RETURNED TO SERVICE. (X) 1 H 7 2 3T RT A9EA 1999011500255 19990115 00255 EA 1999 1 15 SABA9807 1 19980807 A 6123 PROPELLER DHAV DHC6 DHC6300 2802606 EA LT ENGINE MALFUNCTIONED A S9BA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 AL 05 224SA 247 ON FLIGHT FROM STT TO STX SPB, THE CREW REPORTED ON LOG PAGE 14446 UNSCHEDULED AUTOFEATHER LEFT SIDE ON TAKEOFF. THE CR EW CONTINUED THE FLIGHT PER MEL 61-1-2 WITH NO FURTHER PROBLEM. MAINTENANCE DEFERRED THE SYSTEM PER MEL 61-1-2. (X) 1 H 7 2 3T RT A9EA 1999011500256 19990115 00256 EU 1999 1 15 SIMA982893 1 19981016 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 21 240DS A2581 340B240 LAW - FLT 3867 - CARGO SMOKE LIGHT ILLUMINATED ON CENTRAL WARNING PANEL. VERIFIED AS FALSE WARNING. BOTH CARGO SMOKE D ETECTORS OPERATIONALLY CHECKED GOOD. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AS A PRECAUTION. REF: OPERATOR C ONTROL NR 99ZZZX158. (X) 2 L 7 2 4T RT A52EU 1999011500257 19990115 00257 EU 1999 1 15 99ZZZX158 1 19981016 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU CARGO BAY MALFUNCTIONED A SIMA O OTHER N FALSE WARNING NR NOT REPORTED 1 SW 21 240DS A2836 340B240 LAW - FLT 3867 - CARGO SMOKE LIGHT ILLUMINATED ON CENTRAL WARNING PANEL. VERIFIED AS FALSE WARNING. BOTH CARGO SMOKE D ETECTORS OPERATIONALLY CHECKED GOOD. REMOVED AND REPLACED BOTH CARGO SMOKE DETECTORS AS A PRECAUTION. REF: OPERATOR C ONTROL NR SIMA982893. 2 L 7 2 4T RT A52EU 1999011500258 19990115 00258 EU 1999 1 15 SIMA982921 1 19981019 A 3350 6013211 POWER SUPPLY SAAB SF340 340B 7860101 EU ROWS 1-4 INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 352SB 17465 340B352 DFW - FLT 3738 - EMERGENCY FLOOR PROXIMITY LIGHTS AT ROWS 1 AND 4 DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY POW ER SUPPLY. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999011500259 19990115 00259 SO 1999 1 15 SIMA982855 1 19981012 A 2611 P990431N SMOKE DETECTORS EMB 145 EMB145 SO CARGO BAY MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AE 05559 145064 DAY - FLT 4313 - BAGGAGE SMOKE WARNING CAME ON IN-FLIGHT. DEFERRED BAGGAGE SMOKE WARNING SYSTEM PER MEL 26-13. REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTOR SENSORS. OPERATIONAL CHECKED GOOD. MEL CLEARED. REF: OPERATOR CONTROL NR 9 9ZZZX___. (X) 2 L 7 2 4F RT T00011AT 1999011500260 19990115 00260 SO 1999 1 15 99ZZZX159 1 19981012 A 2611 P990431N SMOKE DETECTORS EMB 145 EMB145 SO CARGO BAY MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 607AE 5559 05621 145064 DAY - FLT 4313 - BAGGAGE SMOKE WARNING CAME ON IN-FLIGHT. DEFERRED BAGGAGE SMOKE WARNING SYSTEM PER MEL 26-13. REMOVED AND REPLACED BOTH BAGGAGE SMOKE DETECTOR SENSORS. OPERATIONAL CHECKED GOOD. MEL CLEARED. REF: OPERATOR CONTROL NR S IMA982855. 2 L 7 2 4F RT T00011AT 1999011500261 19990115 00261 SO 1999 1 15 SIMA982792 1 19981006 A 2720 3603001001 RUDDER CONTROL EMB 145 EMB145LR SO VERT STABILIZER INOPERATIVE A A SIMA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED NR NOT REPORTED 1 SW 21 604DG 0063 145058 ORD - FLT 4007 - RUDDER SYSTEMS 1 AND 2 INOPERATIVE. EMERGENCY DECLARED. MECHANICAL REVERSION MODE CONFIRMED. FIRST O FFICER FELT THAT HYDRAULIC SYSTEM WAS LOST. AUTOPILOT AND YAW DAMPENER FAILED. REMOVED AND REPLACED RUDDER POWER CONTR OL UNIT. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 1999011500262 19990115 00262 EU 1999 1 15 SIMA983021 1 19981029 A 5311 SKIN AEROSP ATR72 ATR72212A 8680902 EU BS 4647 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 529AE 529 ABI - ACCIDENTAL DAMAGE FROM JACK OCCURRED TO BOTTOM FORWARD FUSELAGE SKIN PANEL AND FRAME 8 STA 4647. CUT OUT DAMAGED AREA OF SKIN AND FRAME. PERFORMED EDDY CURRENT INSPECTION. FABRICATED FRAME FROM AL 7075-T0, HEAT TREATED TO AL 7-707 6-T6. FABRICATED SKIN DOUBLER. INSTALLED BOTH. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR 99ZZZX161. ( X) 2 H 7 2 4T RT A53EU 1999011500263 19990115 00263 EU 1999 1 15 99ZZZX161 1 19981029 A 5330 FRAME AEROSP ATR72 ATR72212A 8680902 EU BS 4647 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 529AE 529 ABI - ACCIDENTAL DAMAGE FROM JACK OCCURRED TO BOTTOM FORWARD FUSELAGE SKIN PANEL AND FRAME 8 STA 4647. CUT OUT DAMAGED AREA OF SKIN AND FRAME. PERFORMED EDDY CURRENT INSPECTION. FABRICATED FRAME FROM AL 7075-T0, HEAT TREATED TO AL 7-707 6-T6. FABRICATED SKIN DOUBLER. INSTALLED BOTH. AIRCRAFT RETURNED TO SERVICE. REF: OPERATOR CONTROL NR SIMA983021. 2 H 7 2 4T RT A53EU 1999011500264 19990115 00264 EU 1999 1 15 SIMA983082 1 19981104 A 3350 SWITCH SAAB SF340 340B 7860101 EU F/A PANEL LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 398AM 340B398 DFW - FLT 5050 - EXTERIOR EMERGENCY LIGHTS AT CABIN DOOR DO NOT ILLUMINATE. SECURED LOOSE PUSH BUTTON SWITCH TO THE FLI GHT ATTENDANT PANEL. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT A52EU 1999011500265 19990115 00265 NM 1999 1 15 SHUT9817 1 19981116 A 2611 473054 SMOKE DETECTOR 82521140015 DHAV DHC8 DHC8315 2809010 NM CARGO BAY CONTAMINATED A UHLA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 03 801SA 5024 393 FLT 221 - DURING CLIMB THROUGH 7,500 FEET, THE CARGO 'SMOKE' LIGHT ILLUMINATED. THIRTY SECONDS LATER, IT EXTINGUISHED. FEW MINUTES LATER, THE 'SMOKE' LIGHT CAME BACK ON FOR 30 SECONDS. THE AIRCRAFT RETURNED TO BDL AND NO OTHER PROBLEM. ( NO EMERGENCY WAS DECLARED). MAINTENANCE FOUND THE NR 2 CARGO SMOKE DETECTOR DIRTY AND CLEANED AS REQUIRED. FUNCTION CH ECKED, NO DEFECTS NOTED. (X) 2 H 7 2 4T RT A13NM 1999011500266 19990115 00266 EU 1999 1 15 99ZZZX162 1 19981029 A 3240 AC63740 MAXARET DUNLOP SF207 BAG JETSTM JETSTM3201 1500217 EU RT MLG INOPERATIVE A FYWA O OTHER O OTHER TX TAXI/GRND HDL 1 AL 05 242BM 902 UPON LANDING IN KETCHIKAN, PILOT REPORTED RT BRAKE INEFFECTIVE, BRAKE PRESSURE GOOD. AIRCRAFT TOWED TO MAINTENANCE HANG AR. INSPECTION AND TROUBLESHOOTING REVEALED RT MAXARET (ANTI-SKID) UNIT INOPERATIVE. REMOVED AND REPLACED RT MAXARET W ITH SERVICEABLE UNIT. OPS CHECK GOOD. 2 L 7 2 4T RT A56EU 1999011500267 19990115 00267 GL 1999 1 15 C2XAIO429 2 19981020 A 7200 ENGINE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL RIGHT MALFUNCTIONED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 13958 60 145085 GPT - DURING TAKEOFF, PILOT REPORTED THE NR 2 ENGINE HAD A LOW N1 AND HIGH ITT. THE PILOT RETURNED TO GPT WHERE THE AIR CRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW CONTINENTAL EXPRESS GMM VOLUME 13 S ECTION 2, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999011500268 19990115 00268 NM 1999 1 15 ASAA9840103 1 19981103 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 15-16 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 705AS 29318 SMF - FLT 409 - PRIOR TO FLIGHT, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15 AND 16. CONTRA CT MAINTENANCE RE-SECURED LOOSE WIRING TO THE LIGHT ASSEMBLIES AND THE LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999011500269 19990115 00269 NM 1999 1 15 ASAA9840105 1 19981111 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 21-24 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 705AS 29318 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 21-24. RECONNECTED LOOSE WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999011500270 19990115 00270 WP 1999 1 15 GTIA9800121 1 19981029 A 3350 AB004AD0703 BATTERY DOUG DC9 DC982 3022082 WP CABIN DISCHARGED A GTIA K NONE L NO TEST IN INSP/MAINT 1 GL 23 805NK 48087 DTW - CENTER EMERGENCY EXIT LEFT HAND AND RIGHT HAND AFT EMERGENCY LIGHTING INOPERATIVE. REMOVED AND REPLACED BATTERIES AS REQUIRED, OPERATIONAL CHECK GOOD IAW MD80 MM 33-53-0. (X) 2 L 7 2 4F A6WE 1999011500376 19990115 00376 NE 1999 1 15 CA981130011 2 19981113 A 7200 POWER PACK CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE NR 1 ENGINE ODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 807287 (CAN) OILY SMELL IN COCKPIT, FROM NR 1 POWER PACK, ABOVE 30 DEGREE CELSIUS OUTLET TEMPERATURE. NR 1 ENGINE REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999011500426 19990115 00426 WP 1999 1 15 USAAD98207 1 19981118 A 3231 39567851 LINK DOUG DC9 DC931 3022065 WP NLG DOOR FAILED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 997VJ 47336 LGA-GSO - FLT 1621 - UPON LANDING GEAR RETRACTION AFTER TAKEOFF THE NOSE GEAR DOOR DID NOT CLOSE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT NOSE GEAR DOOR LOCK LINK. (M) 2 L 7 2 4F A6WE 1999011500427 19990115 00427 NM 1999 1 15 USAASB98307 1 19981119 A 3350 1000679 LIGHT BOEING 737 737201 1384454 NM ENTRY DOOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 233US 22273 CLT - MAINTENANCE FOUND THE AFT LEFT EMERGENCY EXIT LIGHT WOULD NOT TURN OFF WHEN THE AIRCRAFT WAS POWERED DOWN. MAINTE NANCE REPLACED THE AFT LEFT ENTRY DOOR OVERHEAD EMRGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL. (M) 2 L 7 2 4F A16WE 1999011500428 19990115 00428 NM 1999 1 15 USAASB98298 1 19981028 A 3350 20131ALP BATTERY PACK BOEING 737 737401 1384701 NM CABIN DISCHARGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 418US 23985 CLT - MAINTENANCE FOUND THE FORWARD LEFT EMERGENCY EGRESS LIGHTS INOP. MAINTENANCE REPLACED FUSES IN BATTERY CHARGER AN D INSTALLED REPLACEMENT BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999011500429 19990115 00429 NM 1999 1 15 USAA980601 1 19981126 A 5330 SKIN BOEING 737 737201 1384454 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 41181 22866 TPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH IN EXTERIOR SKIN BS 380 AT BL 0 AT COOLING DUCT OUTLET. IN STALLED DOUBLER PER TR 53-30-04. (M) 2 L 7 2 4F A16WE 1999011500430 19990115 00430 NM 1999 1 15 USAA980602 1 19981126 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 947 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 260AU 41181 22866 TPA - DURIGN CX-1 CHECK VISUAL INSPECTION, FOUND A 10 INCH BY 2.5 INCH AREA OF CORROSION STATION 947 STRINGER 27L. REPL ACED WITH NEW STRINGER SECTION PER EA 63030. (M) 2 L 7 2 4F A16WE 1999011500431 19990115 00431 NM 1999 1 15 USAA980610 1 19981201 A 5315 654581094 FLOORBEAM BOEING 737 737301 1384611 NM BS 328 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 328 AROUND ALL 3 SEAT TRACKS UPPER CHORD, CORROSION TASK NR C53-107-01. REMOVED AND REPLACED FLOORBEAM 'T' CAP PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999011500432 19990115 00432 NM 1999 1 15 USAA980609 1 19981201 A 5313 6552928100 STRINGER BOEING 737 737301 1384611 NM BS 1006-1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON STRINGER STATION 1006 TO 1016 AT STRINGER 26R, CORROSION TA SK NR C53-208-01. REPLACED STRINGER SECTION PER BOEING DRAWING 65-45776. (M) 2 L 7 2 4F RT A16WE 1999011500433 19990115 00433 NM 1999 1 15 USAA980603 1 19981201 A 5311 FRAME BOEING 737 737301 1384611 NM BS 767 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND APPROX 4 SQUARE INCH AREA OF CORROSION FRAME SHEAR TIE SKIN BS 767 BETWE EN STRINGER 26 AND 27, CORROSION TASK NR C53-202-01. INSTALLED REPAIR DOUBLER AND RADIUS FILLER PER EA 62851 AND SRM 53 -00-07 FIG 201. (M) 2 L 7 2 4F RT A16WE 1999011500434 19990115 00434 NM 1999 1 15 USAA980600 1 19981125 A 5330 SKIN BOEING 737 737301 1384611 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 33029 23557 TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC FOUND A .125 INCH CRACK UPPER HINGE CUTOUT ON FORWARD SERVI CE DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 6 AND EA 63034. (M) 2 L 7 2 4F RT A16WE 1999011500435 19990115 00435 NM 1999 1 15 USAA980599 1 19981125 A 5330 SKIN BOEING 737 737301 1384611 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 33029 23557 TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A .375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD SERV ICE DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 3 AND EA 63034. (M) 2 L 7 2 4F RT A16WE 1999011500436 19990115 00436 NM 1999 1 15 USAA980598 1 19981125 A 5330 SKIN BOEING 737 737301 1384611 NM ENTRY DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 354US 33029 23557 TPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A .375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD ENTR Y DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 3 AND EA 63034. (M) 2 L 7 2 4F RT A16WE 1999011500437 19990115 00437 NM 1999 1 15 USAA980611 1 19981201 A 5315 6545815108 FLOORBEAM BOEING 737 737301 1384611 NM BS 344 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM STATION 344 BETWEEN LBL 18 TO RBL 10 UPPER CHORD CORROSION TASK NR C53-107-01. REPAIRED PER SRM 53-10-51. (M) 2 L 7 2 4F RT A16WE 1999011500438 19990115 00438 NM 1999 1 15 USAA980581 1 19981113 A 5313 STRINGER BOEING 737 737301 1384611 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND STRINGER CORROSION 1 INCH, WEB 1 INCH BY 2 INCH CORROSION FORWARD CARGO BS 500A STRINGER 26R AND WEB BETWEEN STATION 500 AND 500A. CORROSION TASK NR C53-208-01. STRINGER SPLICE REPAIR INSTAL LED PER EA 62887 AND SRM 53-00-03 FIG 201. (M) 2 L 7 2 4F RT A16WE 1999011500439 19990115 00439 NM 1999 1 15 USAA980578 1 19981113 A 5314 6562125 KEEL BEAM BOEING 737 737301 1384611 NM BS 500 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION STATION 500D STRINGER 28L KEEL BEAM LOWR CHOR D, CORROSION TASK NR C53-107-01. INSTALLED NEW SPLICE ANAVE, VERTICAL STIFFENERS, SHEAR TIES AND FILLERS PER EA 62936. (M) 2 L 7 2 4F RT A16WE 1999011500440 19990115 00440 NM 1999 1 15 USAA980589 1 19981115 A 5314 KEEL BEAM BOEING 737 7373B7 1384580 NM BS 520 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 39335 22959 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORRSION ON LEFT KEEL BEAM STATION 520. INSTALLED DOU BLER PER EA 62982. (M) 2 L 7 2 4F RT A16WE 1999011500441 19990115 00441 NM 1999 1 15 USAA980583 1 19981110 A 5330 SKIN BOEING 737 737301 1384611 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 336US 36971 23233 CLT - DURING DROP IN VISUAL INSPECTION, FOUND A 2 INCH LONG CRACK IN SKIN RIGHT SIDE AT BS 727D 1 INCH BELOW STRINGER 23 R. INSTALLED DOUBLER PER TR 53-60-03. (M) 2 L 7 2 4F RT A16WE 1999011500442 19990115 00442 NM 1999 1 15 USAA980579 1 19981113 A 5320 CLIP BOEING 737 737301 1384611 NM BS 663 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 663 STRINGER 10L TIE CLIP. INSTALLED NEW TIE CLIP P ER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999011500443 19990115 00443 NM 1999 1 15 USAA980580 1 19981113 A 5320 CLIP BOEING 737 737301 1384611 NM BS 907 CRACK A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK STATION 907 STRINGER 9R TIE CLIP. INSTALLED NEW TIE CLI P PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999011500444 19990115 00444 NM 1999 1 15 USAA980582 1 19981113 A 5320 65C27810 FITTING BOEING 737 737301 1384611 NM BS 500A CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK BS 500A LEFT SUPPORT FOR NR 2 VHF ANTENNA FITTING. INSTA LLED REPAIR DOUBLER AND NEW ANTENNA SUPPORT STRUCTURE PER EA 62832 AND SB 737-53-1159. (M) 2 L 7 2 4F RT A16WE 1999011500445 19990115 00445 NM 1999 1 15 USAA980565 1 19981113 A 5313 65516989 STRINGER BOEING 737 737301 1384611 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 907 STRINGER 4. REPLACED WITH IDENTICAL PART PER SRM 51-40-01. (M) 2 L 7 2 4F RT A16WE 1999011500446 19990115 00446 NM 1999 1 15 USAA980570 1 19981113 A 5315 654680323 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 520 RBL 24.75 FLOORBEAM. INSTALLED DOUBLER PER EA 62987 AND SB 737-53-1120 REV 1. (M) 2 L 7 2 4F RT A16WE 1999011500447 19990115 00447 NM 1999 1 15 USAA980571 1 19981113 A 5315 654680323 FLOORBEAM BOEING 737 737301 1384611 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 520 LBL 24.75 FLOORBEAM. INSTALLED DOUBLER PER EA 62987 AND SB 737-53-1120 REV 1. (M) 2 L 7 2 4F RT A16WE 1999011500448 19990115 00448 NM 1999 1 15 USAA980573 1 19981113 A 5330 SKIN BOEING 737 737301 1384611 NM SERVICE DOORWAY CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT SERVICE DOOR LOWER HINGE CUTOUT. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 52-00-01. (M) 2 L 7 2 4F RT A16WE 1999011500449 19990115 00449 NM 1999 1 15 USAA980574 1 19981113 A 5330 SKIN BOEING 737 737301 1384611 NM BS 698-699 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 335US 37421 23232 CLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BETWEEN STATION 698 TO STATION 699 AT LBL 5 ON SKIN. INS TALLED DOUBLER PER SRM 53-60-12. (M) 2 L 7 2 4F RT A16WE 1999011500450 19990115 00450 NM 1999 1 15 P2EA98274 1 19981119 A 5712 RIB BOEING 737 737281 138448P NM WS 135 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - RIB CRACKED AT RIGHT WING FUEL TANK WBL 135.5, DEFECT SIZE LENGTH 1.125 INCH. REPAIRED RIGHT WING RIB LOWER CHORD AT WBL 135.5, BETWEEN STRINGER 2 AND STRINGER 3 PER BOEING SERVICE BULLETIN 737-57-1186 DATED 4-13-98, SECTION III, PAR T 3 FIG 3. (M) 2 L 7 2 4F A16WE 1999011500451 19990115 00451 NM 1999 1 15 P2EA98277 1 19981117 A 5320 SUPPORT BOEING 737 737281 138448P NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - VERTICAL BEAM CRACKED AT BS 727, WL 197.5, RBL 26, DEFECT SIZE LENGTH 1 INCH. REPLACED BULKHEAD VERTICAL BEAM AT BS 727, RBL 26, BETWEEN WL 202, WL 151 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999011500452 19990115 00452 WP 1999 1 15 ORJA98293 1 19981121 A 2750 39177785503 ACTUATOR DOUG DC9 DC987 3022087 WP TE FLAP MALFUNCTIONED A ORJA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 11 751RA 49779 AT SEATTLE, GATE RETURN, FLAPS DROPPED TO ABOUT 20 DEGREES WHILE AT GATES, AFTER ENGINE START WITH HYD AUS AND TRANS FOR PUMP ON AND ENGINE PUMPS BOTH ON HIGH, FLAPS WOULD NOT MOVE (STILL 20-25 DEGREES) WITH FLAP HANDLE UP/RET. AFTER SEVER AL ATTEMPTS (10 TO 20 CYCLES) FLAPS FINALLY RETRACTED TO UP/RET. REMOVED AND REPLACED BOTH FLAP 2-SPEED CONTROL VALVES AND RT NR 3 FLAP ACTUATOR PER MM. LEAK AND OPS CHECK GOOD. PERFORMED FLAP OPS CHECK PER 27-52-03. FLAPS OPERATE WITHI N LIMITS. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A6WE 1999011500453 19990115 00453 WP 1999 1 15 99ZZZM17 1 19981121 A 2750 59370525001 VALVE DOUG DC9 DC987 3022087 WP TE FLAP MALFUNCTIONED A ORJA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 11 751RA 49779 AT SEATTLE, GATE RETURN, FLAPS DROPPED TO ABOUT 20 DEGREES WHILE AT GATES, AFTER ENGINE START WITH HYD AUS AND TRANS FOR PUMP ON AND ENGINE PUMPS BOTH ON HIGH, FLAPS WOULD NOT MOVE (STILL 20-25 DEGREES) WITH FLAP HANDLE UP/RET. AFTER SEVER AL ATTEMPTS (10 TO 20 CYCLES) FLAPS FINALLY RETRACTED TO UP/RET. REMOVED AND REPLACED BOTH FLAP 2-SPEED CONTROL VALVES AND RT NR 3 FLAP ACTUATOR PER MM. LEAK AND OPS CHECK GOOD. PERFORMED FLAP OPS CHECK PER 27-52-03. FLAPS OPERATE WITHI N LIMITS. OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F RT A6WE 1999011500454 19990115 00454 SO 1999 1 15 ASOA98099 1 19981117 A 2121 EVAC523C2 FAN EMB 120 EMB120RT SO CABIN INOPERATIVE A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 265AS 3001 120170 FLT 7960 - OUTSTATION GTR - COCKPIT FILLED WITH SMOKE WHEN RIGHT ENGINE WAS STARTED. LOCAL MAINTENANCE INSPECTED AND FO UND THE RIGHT RECIRCULATION FAN INOPERATIVE. A/C WAS FOUND SAFE FOR A FERRY FLIGHT TO DFW. DFW MAINTENANCE REMOVED AND REPLACED THE RIGHT RECIRCULATION FAN. OPERATIONAL AND GROUND CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHE R SERVICE. (M) 2 L 7 2 4T RT A31SO 1999011500455 19990115 00455 SO 1999 1 15 ASOA98100 1 19981118 A 2150 32144143 VALVE EMB 120 EMB120RT SO WS 494 FAILED A ASOA O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 SO 11 265AS 120170 FLT 7430 - OUTSTATION ILE, SMOKE IN CABIN AND COCKPIT JUST AFTER ENGINE START, PACKS AND FANS WERE OFF. DFW MECHANIC WA S SENT TO ILE AND CONFIRMED THAT THE RIGHT PACK CONTROL VALVE WAS SLIGHTLY OPEN WITH APU BLEED ON AND PACKS OFF. FOUND A/C SAFE FOR FERRY FLIGHT TO DFW. DFW MAINTENANCE REMOVED AND REPLACED THE RIGHT PACK CONTROL VALVE. OPERATIONAL AND G ROUND CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVIEC. (M) 2 L 7 2 4T RT A31SO 1999011500456 19990115 00456 SO 1999 1 15 C2XA98IA482 1 19981214 A 5320 14531597602 ANGLE EMB 145 EMB145 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER RIGHT DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. M AINTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF DRAG ANGLE IAW EMB145 SRM 54-40-02, AND THE AIRCRAFT WAS THEN APP ROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500457 19990115 00457 SO 1999 1 15 C2XA98IA481 1 19981214 A 5320 14531597601 ANGLE EMB 145 EMB145 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE VERTICLE STABILIZER LEFT DRAG ANGLE WAS FOUND TO BE CRACKED AT THE FORWARD END. MA INTENANCE REMOVED AND REPLACED THE FORWARD SECTION OF DRAG ANGLE IAW EMB145 SRM 54-40-02, AND THE AIRCRAFT WAS THEN APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500458 19990115 00458 SO 1999 1 15 C2XA98IA480 1 19981214 A 5320 BEAM EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. MAINTENANCE REMOVED THE CORRODED SECTION OF OMEGA BEAM AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5320-01030, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500459 19990115 00459 SO 1999 1 15 C2XA98IA479 1 19981214 A 5320 BEAM EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE CENTER AISLE OMEGA BEAM WAS FOUND TO BE CORRODED JUST FORWARD OF FRAME 25. MAINTEN ANCE REMOVED THE CORRODED SECTION OF OMEGA BEAM AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS DRAWINGS COEX03TY Y05/06 AND COEX03TYY06/06, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500460 19990115 00460 SO 1999 1 15 C2XA98IA478 1 19981214 A 5320 BEAM EMB 145 EMB145 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE FORWARD GUST LOCK MOUNT STRUCTURE CROSS BEAM WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED AN INTERIM REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE AND REPAIR AUTHORIZATION EC5310-01098, AND THE AI RCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500461 19990115 00461 SO 1999 1 15 C2XA98IA477 1 19981214 A 3350 20131A BATTERY PACK EMB 145 EMB145 SO CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE EMERGENCY LIGHT BATTERY AT STATION 17540.8 WAS FOUND TO BE DISCHARGED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK IAW EMB145 AMM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500462 19990115 00462 SO 1999 1 15 C2XA98IA495 1 19981218 A 3350 3025101 LIGHT EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOP ERATIVE. MAINTENANCE CLEANED THE AFFECTED LIGHT ASSEMBLY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500463 19990115 00463 SO 1999 1 15 C2XA98IA494 1 19981218 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145 SO SERVICE DOORWAY INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY EXIT LIGHT ON THE SERVICE DOOR WAS FOUND TO BE INOP ERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROV ED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500464 19990115 00464 SO 1999 1 15 C2XA98IA493 1 19981218 A 3397 W192876222 WIRE EMB 145 EMB145 SO ROW 2 BROKEN A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15926 145005 IAH - DURNIG POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY EXIT LIGHT AT EXIT ROW 2 RIGHT SIDE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON THE AFFECTED LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500465 19990115 00465 SO 1999 1 15 C2XA98IA491 1 19981205 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145 SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13936 145025 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THAT THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-00, AND THE AIRCRAFT WAS APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500466 19990115 00466 EU 1999 1 15 C2XA98IA490 1 19981209 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THE FORWARD EMERGENCY AISLE PATH LIGHTING REMAINED ILLUMINATED AF TER THE BATTERY WAS SWITCHED OFF. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT POWER SUPPLY BATTERY, AN D THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500467 19990115 00467 EU 1999 1 15 C2XA98IA489 1 19981208 A 3350 E01173110 SWITCH AEROSP ATR42 ATR42320 8680930 EU CABIN CONTAMINATED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19812 99 IAH - DURNIG POST FLIGHT INSPECTION, THE CREW REPORTED THE EMERGENCY AISLE PATH LIGHTING REMAINED ILLUMINATED AFTER THE BATTERY WAS SWITCHED OFF. MAINTENANCE CLEANED THE EMERGENCY LIGHT SWITCH AT THE FLIGHT ATTENDANTS PANEL, AND THE AIRCRA FT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500468 19990115 00468 EU 1999 1 15 C2XA98IA488 1 19981119 A 3350 301180 POWER SUPPLY AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26826 172 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE RE MOVED AND REPLACED TWO EMERGENCY POWER SUPPLIES IAW ATR42 JIC 33-52-00, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999011500469 19990115 00469 EU 1999 1 15 C2XA98IA487 1 19981214 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU SEAT 1A DISCHARGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19812 99 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE EMERGENCY LIGHT BATTERY PACKS AT SEATS 1AB, AND 6CD, WERE WEAK. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BATTERIES IAW ATR42 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500470 19990115 00470 EU 1999 1 15 C2XA98IA486 1 19981110 A 3350 7012210 BULB AEROSP ATR42 ATR42320 8680930 EU CABIN LOOSE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 93840 271 IAH - DURING LINE CHECK INSPECTION, THE EMERGENCY EXIT SIGN AT THE GALLEY DOOR WAS FOUND TO HAVE ONE BULB NOT ILLUMINATI NG. MAINTENANCE REINSTALLED THE AFFECTED BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500471 19990115 00471 EU 1999 1 15 C2XA98IA520 1 19981220 A 3350 3011206 LIGHT AEROSP ATR42 ATR42320 8680930 EU FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE LEFT EXTERNAL EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVE D AND REPLACED THE AFFECTED EMERGENCY LIGHT. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500472 19990115 00472 EU 1999 1 15 C2XA98IA519 1 19981220 A 5720 S521059020101 FITTING AEROSP ATR42 ATR42320 8680930 EU RT WING WORN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE RIGHT WING SPAR LOWR FITTING AT RIB 18 WAS FOUND TO HAVE AN ELONGATED FLAP PANEL MO UNT HOLE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500473 19990115 00473 EU 1999 1 15 C2XA98IA518 1 19981220 A 5320 S53971402203 ANGLE AEROSP ATR42 ATR42320 8680930 EU BS 27 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE FAIL/SAFE ANGLE FOR FRAME 27A WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVE FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500474 19990115 00474 EU 1999 1 15 C2XA98IA524 1 19981220 A 3350 NSA931320100A BREAKER AEROSP ATR42 ATR42500 EU COCKPIT TRIPPED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - FLT 3853 - PILOT REPORTED THAT THE CABIN EMERGENCY EXIT LIGHT CIRCUIT BREAKER WAS POPPED. MAINTENANCE RESET THE B REAKER AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500475 19990115 00475 EU 1999 1 15 C2XA98IA523 1 19981217 A 3350 AD3127 BATTERY AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 19812 541 99 IAH - DURING MAINTENANCE, THE EMERGENCY LIGHTS FAILED AN OPERATIONAL TEST. MAINTENANCE REMOVED AND REPLACED THE EMERGEN CY LIGHT BATTERY AT THE 18WL POWER SUPPLY OCATION. THE LIGHTS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500476 19990115 00476 SO 1999 1 15 C2XA98IA522 1 19981220 A 5713 12016085002 STRINGER EMB 120 EMB120RT SO RT WING CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 12703 120084 IAH - DURING A 5A CHECK INSPECTION, THE RIGHT WING STRINGER NR 10 WAS FOUND CRACKED. MAINTENANCE REPAIRED THE STRINGER USING A SPLICE REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE/REPAIR AUTHORIZATION EC5710-01010. THE AIRCRAFT WAS TH EN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999011500477 19990115 00477 EU 1999 1 15 C2XA98IA521 1 19981220 A 3350 33510199 PIN AEROSP ATR42 ATR42320 8680930 EU SERVICE DOOR FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A WIRE PIN AT THE 28WL LIGHT LOCATION. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE (M) 2 H 7 2 4T RT A53EU 1999011500478 19990115 00478 1999 1 15 C2XA98CL080 3 19981201 A 6112 HCE4A3I DEICE BOOT BEECH 1900 1900D 1154162 CE RT PROP FAILED A C2XA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 09 87557 6065 HJ221 UE246 CLE - FLT 3107 - CREW REPORTED AFTER TAKEOFF THE RIGHT PROP WAS ARCING WHEN PROP HEAT WAS TURNED ON, A GLOW WAS OBSERVED FROM THE SPINNER AND A BURNING SMELL WAS NOTICED. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANC E INSPECTED THE RIGHT PROP ASSEMBLY AND FOUD THAT ONE OF THE PROP BLADE BOOTS WAS BURNED. THE AIRCRAFT WAS RELEASED IAW MEL 30-10C CONTROL NR 127507. THE PROP ASSEMBLY WAS REMOVED AND REPLACED IAW B1900 MM 61-10-00 THE NEXT DAY. OPERATIO NAL CHECKS SATISFACTORY. (M) 2 L 7 2 4T RT A24CE 1999011500479 19990115 00479 NM 1999 1 15 MZZA98263 1 19981130 A 3230 65178812 VALVE BOEING 727 727224 1384076 NM RT MLG MALFUNCTIONED A MZZA O OTHER J WARNING INDICATION CL CLIMB 1 WP 13 79743 22252 FLT 956 - TKK - AFTER TAKEOFF FROM TKK WHEN MLG WAS RAISED, ALL LIGHTS WENT OUT INDICATING THE GEAR UP AND LOCKED. SHOR TLY AFTER THE RIGHT MLG RED LIGHT CAME ON INDICATING NOT UP AND LOCKED. UPON VISUAL INSPECTION, RIGHT GEAR WAS NOTED TO BE ALL THE WAY DOWN. SHORTLY AFTER, FLIGHT CREW NOTED SOME CLICKING NOISE ON C/B PANEL (RELAYS) AND GEAR CAME ALL THE WAY UPLIGHTS WENT OUT. MX REMOVED AND REPLACED RT MLG LOCK SEQUENCE VALVE PER MM 32-32-31. SYSTEM LEAK AND OPS CHECKED OK ON 6 LANDING GEAR EXTEND AND RETRACT CYCLES. ALSO, ALL INDICATION LIGHTS CHECKED OK IN EXTEND RETRACT OFF GEAR LEVE R POSITIONS. (M) 2 L 7 3 4F A3WE 1999011500480 19990115 00480 WP 1999 1 15 HALA9800368 1 19981027 A 2612 CONTROLLER DOUG DC10 DC1010 3022110 WP E/E BAY MALFUNCTIONED A HALA K NONE O OTHER IN INSP/MAINT 1 WP 13 122AA 46522 FLT 2 - HNL - ON PREFLIGHT, FOUND 'B' LOOP LIGHT ILLUMINATED FOR NR 1 FIRE DETECTION SYSTEM. REMOVED AND REPLACED CONTR OLLER, SYSTEM OP CHECKS NORMAL. (M) 2 L 7 3 4F A22WE 1999011500481 19990115 00481 EU 1999 1 15 VTZA98340 1 19981116 A 3350 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CABIN FAILED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 306UE 41020 FLT 6536 - IAD-RIC - DURING PREFLIGHT, EXPERIENCED A DISCREPANCY WITH THE EMERGENCY LIGHTS NOT SHUTTING OFF. FLIGHT CRE W NOTIFIED MAINTENANCE CONTROL AND MAINTENANCE WAS NOTIFIED. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE ROOF PAN EL EMERGENCY LIGHTS SWITCH IAW APPLICABLE MX PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A41NM 1999011500482 19990115 00482 NM 1999 1 15 USAASB324 1 19981211 A 2420 GENERATOR BOEING 737 737401 1384701 NM NR 2 MALFUNCTIONED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 419US 23986 RIC - FLT 1475 - EN ROUTE PHL-CLT, THE NR 2 GENERATOR TRIPPED. THE APU GENERATOR SYSTEM WAS ON MEL. FLIGHT DIVERTED TO RIC AND LANDED WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4F RT A16WE 1999011500483 19990115 00483 EU 1999 1 15 VTZA98342 1 19981120 A 5610 WINDSCREEN BAG JETSTM JETSTM3201 1500217 EU COCKPIT BIRDSTRIKE A VTZA A UNSCHED LANDING O OTHER TO TAKEOFF 1 EA 27 497UE 904 FLT 6617 - ORF-IAD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BIRDSTRIKE ON FO'S WINDSCREEN. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND NO DAMAGE TO WINDSCREEN. OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE (M) 2 L 7 2 4T RT A56EU 1999011500484 19990115 00484 NM 1999 1 15 USAASB98302 1 19981115 A 3350 3114981 LIGHT BOEING 737 7374B7 1384702 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 429US 24551 TPA - MAINTENANCE FOUND THE FORWARD ENTRY EGRESS EMERGENCY LIGHT AND THE RIGHT AFT FUSELAGE EGRESS EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE REFLECTOR ASSEMBLIES AT BOTH LOCATIONS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999011500485 19990115 00485 EU 1999 1 15 USAAF98091 1 19981116 A 5610 D20543406 WINDSHIELD FOKKER F28 F28MK0100 4990807 EU COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 853US 14663 11281 GSO - FLT 373 - AFTER TAKEOFF FROM GSO, THE RIGHT WINDSHIELD BEGAN TO CRACK ALONG WITH SOME ELECTRICAL ARCING IN THE WIN DOW AREA. THE CRACK CONTINUED EXTENDING APPROXIMATELY 2 FEET ACROSS, OBSTRUCTING THE FIRST OFFICERS VIEW. THE FLIGHT R ETURNED TO GSO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT WINDSHIELD. (M) 2 L 7 2 4F RT 1999011500486 19990115 00486 CE 1999 1 15 MASA98183 1 19981002 A 3260 404EN16 SWITCH BEECH 1900 1900D 1154162 CE LT MLG MALFUNCTIONED A MASA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 SW 07 46YV UE46 FLT 5435 - GNV-MIA - ON APPROACH INTO MIA WITH GEAR SELECTED DOWN, THE LEFT MAIN GEAR DID NOT INDICATE DOWN AND LOCKED. A MANUAL GEAR EXTENSION WAS PERFORMED BUT A SAFE CONDITION COULD NOT BE VERIFIED. THE CREW DECLARED AN EMERGENCY. THE GEAR WAS VISUALLY VERIFIED TO BE DOWN BY THE CREW AND TOWER. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS FERRIED T O JAX WHERE MAINTENANCE CLEANED AND LUBED THE LEFT DOWNLOCK SWITCH AND PERFORMED RETRACTION TESTS. OPS CHECKED GOOD. A IRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999011500487 19990115 00487 1999 1 15 VTZA98332 3 19981109 A 6140 91SE16 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 497UE 904 FLT 6187 - IAD-SCE - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BETA HORN WARNING SOUNDED. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND ADJUSTED RIGHT POWER LEVERS FOR RT BETA MI CROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999011500488 19990115 00488 EU 1999 1 15 99ZZZM18 1 19981109 A 6120 8659566 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE OUT OF ADJUST A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 497UE 904 FLT 6187 - IAD-SCE - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO BETA HORN WARNING SOUNDED. AIRCRAFT RETU RNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND CLEANED AND ADJUSTED RIGHT POWER LEVERS FOR RT BETA MI CROSWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999011500489 19990115 00489 EA 1999 1 15 VTZA98333 1 19981109 A 5210 600381095 ROLLERS CNDAIR CL600 CL6002B19 EA PASSENGER DOOR LACK OF LUBE A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 629BR 7251 FLT 6645 - AVP-ORD - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING BY DIVERTING TO PIT DUE TO PASSENGER DOOR WARNI NG LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND LUBED UPPER ROLLER , OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999011500490 19990115 00490 EA 1999 1 15 VTZA98335 1 19981110 A 2750 601R931055 BPSU CNDAIR CL600 CL6002B19 EA TE FLAP FAILED A VTZA B EMER. DESCENT J WARNING INDICATION CR CRUISE 1 EA 27 629BR 7251 FLT 6654 - SGE-ORD - DURING CRUISE, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS FLAP FAIL MESSAGE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BPSU. OPS CHECK OK. A IRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999011500491 19990115 00491 NM 1999 1 15 USAASB98322 1 19981211 A 3350 900835A BATTERY BOEING 737 737201 1384454 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 243US 22445 BWI - MAINTENANCE FOUND THE MID CABIN CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY S UPPLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999011500492 19990115 00492 NM 1999 1 15 USAA980614 1 19981115 A 5314 KEEL BEAM BOEING 737 7373B7 1384580 NM BS 530 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 387US 39335 22959 TPA - DURING CX-3 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION BETWEEN KEEL BEAM AND SKIN STATION 530 AND W L 148.5. REMOVED CORROSION AND REPAIR ANGLES INSTALLED PER EA 62982. (M) 2 L 7 2 4F RT A16WE 1999011500493 19990115 00493 NM 1999 1 15 USAA129805 1 19981211 A 2611 824PY SMOKE DETECTOR BOEING 727 727254 138408L NM LAVATORY MALFUNCTIONED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 914TS 20251 FLT 6540 - DCA-LGA - FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED FORWARD LAVATORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL. (M) 2 L 7 3 4F A3WE 1999011500494 19990115 00494 EU 1999 1 15 SIMA983458 1 19981211 A 5320 S5367130021802 STRINGER AEROSP ATR42 ATR42300 8680920 EU BS 35-37 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND STRINGER 16 RIGHT BETWEEN FRAME 35 AND 37, AND STRINGER CLIP AT FRAME 35 CORRODED. REPAIRED STRINGER 16 RIGHT. REMOVED AND REPLACED STRINGER CLIP. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500495 19990115 00495 EU 1999 1 15 99ZZZM19 1 19981211 A 5320 S5367131121251 CLIP AEROSP ATR42 ATR42300 8680920 EU BS 35-37 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND STRINGER 16 RIGHT BETWEEN FRAME 35 AND 37, AND STRINGER CLIP AT FRAME 35 CORRODED. REPAIRED STRINGER 16 RIGHT. REMOVED AND REPLACED STRINGER CLIP. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500496 19990115 00496 EU 1999 1 15 SIMA983457 1 19981211 A 5315 S5367240620801 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU BS 36-38 CORRODED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 310DK 310 SAW - DURING INSPECTION, FOUND FLOORBEAMS 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500497 19990115 00497 EU 1999 1 15 99ZZZM20 1 19981211 A 5315 S53672407202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU BS 36-38 CORRODED A SIMA K NONE O OTHER TX TAXI/GRND HDL 1 SW 21 310DK 310 SAW - DURING INSPECTION, FOUND FLOORBEAMS 36 AND 38 CORRODED. REMOVED AND REPLACED BOTH FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500498 19990115 00498 EU 1999 1 15 SIMA983456 1 19981211 A 5311 S5367240620051 FRAME AEROSP ATR42 ATR42300 8680920 EU BS 36 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND FRAME 36 CORRODED. REPAIRED THE FRAME. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500499 19990115 00499 EU 1999 1 15 SIMA983454 1 19981211 A 5330 S5317220120605 SKIN AEROSP ATR42 ATR42300 8680920 EU BS 6-7 DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-1 INSPECTION, CLEARED DMI NR 10DMQ530009. DENT IN LEFT SIDE OF FUSELAGE SKIN BETWEEN FRAME 6 AND 7, AN D BETWEEN STRINGER 13 AND 14. REPAIRED SKIN. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500500 19990115 00500 EU 1999 1 15 SIMA983451 1 19981211 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500501 19990115 00501 EU 1999 1 15 99ZZZM21 1 19981211 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500502 19990115 00502 EU 1999 1 15 99ZZZM22 1 19981211 A 5347 S53678001238 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500503 19990115 00503 EU 1999 1 15 99ZZZM23 1 19981211 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500504 19990115 00504 EU 1999 1 15 99ZZZM24 1 19981211 A 5347 S5367800121002 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500505 19990115 00505 EU 1999 1 15 99ZZZM25 1 19981211 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500506 19990115 00506 EU 1999 1 15 99ZZZM26 1 19981211 A 5347 S53678001222 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500507 19990115 00507 EU 1999 1 15 99ZZZM27 1 19981211 A 5347 S53570201200 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE LEFT AND RIGHT AFT INBOARD AND OUTBOARD, THE LEFT AND RIGHT CENTER INBOARD, AND THE LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500508 19990115 00508 EU 1999 1 15 SIMA983442 1 19981210 A 5414 SKIN SAAB SF340 340B 7860101 EU LT NACELLE CHAFED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 272AE 340B272 ABI - DURING MBV INSPECTION, FOUND A CHAFE ON LEFT NACELLE INBOARD FILLET FAIRING SEAL CONTACT AREA. BLENDED CHAFED ARE A AND PERFORMED AND EDDY CURRENT INSPECTION WITH NO CRACKS INDICATED. FABRICATED AND INSTALLED A DOUBLER .050 THICK. A IRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999011500509 19990115 00509 EU 1999 1 15 SIMA983341 1 19981130 A 3350 BULB AEROSP ATR42 ATR42300 8680920 EU ROW 21 FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AT 327 ORD - FLT 4201 - AIRSTAIR EMERGENCY LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB FOR AIRSTAIR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999011500510 19990115 00510 EU 1999 1 15 SIMA983444 1 19981210 A 3350 CONNECTOR AEROSP ATR42 ATR42300 8680920 EU CABIN LOOSE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 327AT 327 ORD - FLT 4139 - EMERGENCY FLOOR PROXIMITY LIGHTS HAS THREE BULBS OUT. RESECURED CANNON PLUG ON EMERGENCY LIGHT POWER S UPPLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999011500511 19990115 00511 EU 1999 1 15 SIMA983432 1 19981209 A 3350 3013017 BATTERY AEROSP ATR72 ATR72212 EU CABIN DISCHARGED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 499AT 0655 499 ORD - FLT 3567 - AFT EMERGENCY LIGHTS OVER PASSENGER AND SERVICE DOOR DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999011500512 19990115 00512 EU 1999 1 15 RAIA981127 1 19981130 A 7710 31024766 SIGNAL COND BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 339TE 12099 935 FLT 7306 - STL - RIGHT TORQUE GAUGE FAILED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT TORQUE SIGNAL CONDITIONER. (M) 2 L 7 2 4T RT A56EU 1999011500513 19990115 00513 WP 1999 1 15 RAIA981125 2 19981128 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RIGHT FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 430AM 11502 880 66281 FLT 7417 - ALO - OIL PRESSURE STARTED CLIMBING PAST RED LINE, ON APPROACH PRESSURE PEGGED, OIL TEMP REMAINED NORMAL. MA INTENANCE REPLACED RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999011500514 19990115 00514 EU 1999 1 15 RAIA981126 1 19981129 A 3260 AIR136070 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU RT MLG FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 565HK 41082 FLT 7750 - DCA - RED LIGHT INSIDE LANDING GEAR WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. MAINTENANCE REPLACED RIGHT M AIN GEAR UPLOCK SWITCH. (M) 2 L 7 2 4T RT A41NM 1999011500515 19990115 00515 1999 1 15 RAIA981123 3 19981126 A 6140 8659566 SWITCH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 343TE 955 FLT 7102 - STL - RIGHT BETA LIGHT ILLUMINATED ON TAKEOFF ROLL. MAINTENANCE REPLACED RIGHT BETA SWITCH. (M) 2 L 7 2 4T RT A56EU 1999011500516 19990115 00516 EU 1999 1 15 RAIA981209 1 19981213 A 3097 C40648 WIRE JETAIR JETSTM JETSTM4101 1500501 EU LT PROP FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 558HK 41071 FLT 7453 - BHM - LEFT PROP HEAT INOP. MAINTENANCE REPLACED PROP DEICE ON LEFT PROP. (M) 2 L 7 2 4T RT A41NM 1999011500517 19990115 00517 1999 1 15 RAIA981208 4 19981213 A 3416 066306202 ALTIMETER BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 434AM 11788 887 FLT 7508 - STL - CAPTAINS ALTIMETER FLAGGED. MAINTENANCE REPLACED CAPTAINS ALTIMETER. (M) 2 L 7 2 4T RT A56EU 1999011500518 19990115 00518 EU 1999 1 15 RAIA981207 1 19981210 A 7714 AG34 TACH BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 862JX 862 FLT 4791 - SMF - RIGHT RPM GAUGE WENT TO ZERO. MAINTENANCE REPLACED RIGHT TACH GENERATOR. (M) 2 L 7 2 4T RT A56EU 1999011500519 19990115 00519 EU 1999 1 15 RAIA981205 1 19981209 A 3260 9005EN38 SWITCH BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 342TE 954 FLT 7509 - FWA - NOSE LANDING GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR RETRACTED. MAINTENANCE REPLACED NOSE UPLOCK S WITCH. (M) 2 L 7 2 4T RT A56EU 1999011500520 19990115 00520 NM 1999 1 15 P2EA98254 1 19981112 A 5610 5893543110 WINDOW BOEING 737 737247 138448D NM COCKPIT CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 204AU 92141H1815 19603 MDW - FLT 414 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. RIGHT FORWARD OUTER PANE CRACKED IN FLIGHT AT APPROX 20,000 FT, 300 KTS. REPLACED R-1 WINDOW PER VANGUARD JOB CARD J256-11-01. REPLACED WINDOW HEAT CONTROLLER PER MM 30-40, PRECA UTIONARY. (M) 2 L 7 2 4F A16WE 1999011500521 19990115 00521 NM 1999 1 15 P2EA98234 1 19981004 A 5753 SKIN BOEING 737 737244 138448U NM WS 490-505 WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING OUTBOARD FORE FLAP LEADING EDGE SKIN WORN. REPAIRED RIGHT WING FORE FLAP LEADING EDGE SKIN FROM WSL 49 0 TO WSL 505, PER SRM 57-50-4 FIG 1. (M) 2 L 7 2 4F A16WE 1999011500522 19990115 00522 NM 1999 1 15 P2EA98239 1 19981016 A 5350 65486852 FAIRING BOEING 737 737244 138448U NM RIGHT FUSELAGE DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING TO BODY FAIRING (RT A/C BAY DOOR) INNER DOOR SKIN AND SEAL DELAMINATED. REPAIRED RT WING TO BODY FAIRI NG PER COOPESA EO C00-3-53-588-98 DATED OCT 26, 1998. (M) 2 L 7 2 4F A16WE 1999011500523 19990115 00523 NM 1999 1 15 P2EA98240 1 19981016 A 5350 65486851 FAIRING BOEING 737 737244 138448U NM LT FUSELAGE DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - LEFT WING TO BODY FAIRING (LT A/C BAY DOOR) INNER SKIN DELAMINATED. REPAIRED LEFT WING TO BODY FAIRING PER COOPES A EO C00-3-53-587-98 DATED OCT 26, 1998. (M) 2 L 7 2 4F A16WE 1999011500524 19990115 00524 NM 1999 1 15 P2EA98241 1 19981004 A 5754 SKIN BOEING 737 737244 138448U NM WS 493-505 WORN A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - RIGHT WING OUTBOARD FOREFLAP LEADING EDGE SECTION WORN. REPAIRED RIGHT WING OUTBOARD FOREFLAP LEADING EDGE SECTIO N FROM WS 493 TO WS 505 PER SRM 57-50-4 FIG 1. (M) 2 L 7 2 4F A16WE 1999011500525 19990115 00525 CE 1999 1 15 MASA98207 1 19981118 A 7540 ANNUNCIATOR BEECH 1900 1900D 1154162 CE COCKPIT MALFUNCTIONED A MASA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 78YV UE78 FLT 6411 - PHX-IFP - AFTER DEPARTURE FROM PHX, CREW REPORTED THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO PHX. THE ITEM HAD BEEN PREVIOUSLY DEFERRED PER MEL 21-3. NO MAINTEN ANCE ACTION WAS REQUIRED AT THIS TIME, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999011500526 19990115 00526 WP 1999 1 15 USAAD98212 1 19981128 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC931 3022065 WP CABIN MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923VJ 48143 THE OVERWING EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE REPLACED THE OVERWING EMERGENCY EXIT LIGHT POWER SUP PLY. (M) 2 L 7 2 4F A6WE 1999011500527 19990115 00527 WP 1999 1 15 USAAD98211 1 19981203 A 3350 873100272 LIGHT DOUG DC9 DC981 3022081 WP SERVICE DOOR MALFUNCTIONED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 805US 48053 PIT - THE AFT SERVICE DOOR EXIT IDENTIFIER LIGHT STAYED ON. MAINTENANCE REPLACED THE AFT SERVICE DOOR EXIT IDENTIFIER L IGHT ASSEMBLY AND BATTERY. (M) 2 L 7 2 4F A6WE 1999011500528 19990115 00528 NM 1999 1 15 TSAA9833634 1 19981215 A 3350 8621951 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 AFT INTERVALVE EMERGENCY CONTROL MODULE TRIGGERING LIGHT ASSEMBLY. REPLACED AFT CONTROL MODULE BATTERY PACK, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500529 19990115 00529 NM 1999 1 15 TSAA9833635 1 19981215 A 3350 9221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED FORWARD ENTRANCE EXIT IDENTIFIER BATTERY PACK DUE TO RETIRE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500530 19990115 00530 NM 1999 1 15 TSAA9833636 1 19981215 A 3350 9221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED FORWARD SERVICE EXIT IDENTIFIER BATTERY PACK DUE TO RETIRE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500531 19990115 00531 NM 1999 1 15 TSAA9833637 1 19981215 A 3350 9221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED LEFT OVERWING EXIT IDENTIFIER BATTERY PACK DUE TO TIRE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500532 19990115 00532 NM 1999 1 15 TSAA9833638 1 19981215 A 3350 9221009 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED AFT SERVICE EXIT IDENTIFIER BATTERY PACK DUE TO RETIRE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500533 19990115 00533 NM 1999 1 15 TSAA9833639 1 19981216 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 816AL 23122 EMERGENCY FLOOR LIGHT NR 3 AND NR 6 INOPERATIVE. REPLACED BATTERY PACKS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500534 19990115 00534 NM 1999 1 15 TSAA9833640 1 19981216 A 3350 6013211 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 REPLACED AFT SLIDE EMERGENCY BATTERY PACK DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999011500535 19990115 00535 NM 1999 1 15 TSAA9833641 1 19981216 A 3350 86210066 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED BATTERY FOR POSITION NR 4 FLOOR PROX LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500536 19990115 00536 NM 1999 1 15 TSAA9833642 1 19981216 A 3350 9221009 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED BATTERY FOR FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500537 19990115 00537 NM 1999 1 15 TSAA9833643 1 19981216 A 3350 9221009 BATTERY PACK BOEING 737 737209 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 827AL 23913 REPLACED BATTERY FOR RIGHT OVERWING EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500538 19990115 00538 NM 1999 1 15 TSAA9833645 1 19981216 A 3350 86210066 BATTERY PACK BOEING 737 73725A 1384481 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 819AL 23791 REPLACED BATTERY FOR POSITION NR 4 FLOOR PROX LIGHT ASSY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999011500539 19990115 00539 EU 1999 1 15 SIMA983461 1 19981212 A 2520 2LA00598512 PSU SAAB SF340 SF340A 7850100 EU SEAT BC MALFUNCTIONED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 312AE 312 LAX - OVERHEAD EMERGENCY LIGHT AT SEAT 5BC DOES NOT ILLUMINATE. REMOVED AND REPLACED PSU PANEL. OPERATIONAL CHECK GOOD . (M) 2 L 7 2 4T RT A52EU 1999011500540 19990115 00540 SO 1999 1 15 SIMA9834511 1 19981211 A 2611 PU90431 SMOKE DETECTOR EMB 145 EMB145LR SO CARGO BAY MALFUNCTIONED A SIMA F ACTIVATE FIRE EXT. N FALSE WARNING AP APPROACH 1 SW 21 602AE 05799 145048 CLE - FLT 4337 - BAGGAGE COMPARTMENT SMOKE WARNING LIGHT ILLUMINATED. DISCHARGED FIRE EXTINGUISHERS. EVENT WAS DETERMI NED TO BE A FALSE WARNING. DEFERRED BAGGAGE COMPARTMENT SMOKE DETECTION SYSTEM FOR FLIGHT BACK TO ORD WHERE THE SMOKE D ETECTOR AND FIRE EXTINGUISHERS WERE REMOVED AND REPLACED. THE MEL WAS CLEARED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT T00011AT 1999011500541 19990115 00541 NM 1999 1 15 P2EA98312 1 19981226 A 5610 5717623096 WINDOW BOEING 737 737281 138448P NM COCKPIT CRACKED A P2EA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 05 219US 20414 MCI - FLT 586 - THE AIRCRAFT DEPARTED MCI AND 35 MINUTES INTO FLIGHT THE FIRST OFFICERS SLIDING WINDOW CRACKED. THE AIR CRAFT RETURNED TO MCI WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE CRACKED F/O WINDOW AND WINDOW HEAT CONTROL U NIT. (M) 2 L 7 2 4F A16WE 1999011500542 19990115 00542 NM 1999 1 15 P2EA98311 1 19981215 A 7830 SKIN BOEING 737 737281 138448P NM THRUST REVERSER CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - NR 1 THRUST REVERSER LOWER BUCKET EXTERNAL SKIN CRACKED, DEFECT SIZE LENGTH 2.75 INCH. REPAIRED THRUST REVERSER P ER COOPESA EO COO-3-78-754-98 DATED DEC 17, 1998. (M) 2 L 7 2 4F A16WE 1999011500543 19990115 00543 NM 1999 1 15 P2EA98310 1 19981117 A 5314 KEEL BEAM BOEING 737 737281 138448P NM BS 727 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - KEEL BEAM CRACKED BETWEEN BS 727 AND 727A LEFT SIDE, DEFECT SIZE 4 INCH. REPAIRED KEEL BEAM LOWER CHORD BETWEEN B S 727 PLUS 4 AND BS 727A PLUS 6 PER COOPESA EO COOP-3-53-722-98 DATED DEC 3, 1998 AND BOEING FAX COO-SJO-98-1019RR DATED DEC, 1998. (M) 2 L 7 2 4F A16WE 1999011500544 19990115 00544 NM 1999 1 15 P2EA98309 1 19981117 A 5754 RIB BOEING 737 737281 138448P NM FS 480 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - NR 5 SLAT OUTBOARD RIB CRACKED AT FSS 480, DEFECT SIZE LENGTH 1.125 INCH. REPLACED LEADING EDGE CAVITY MAIN TRACK OUTBOARD RIB AT FSS 480 PER 51-10-1 PAGE 1 AND SRM 51-30-2. (M) 2 L 7 2 4F A16WE 1999011500545 19990115 00545 NM 1999 1 15 P2EA98308 1 19981118 A 5330 SKIN BOEING 737 737281 138448P NM BS 297-305 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - INTERNAL DOUBLER CRACKED FORWARD ENTRY DOORWAY UPPER HINGE CUTOUT, DEFECT SIZE LENGTH 1.937 INCH. REPAIRED FUSELA GE SKIN FROM BS 297 TO BS 305 BETWEEN STRINGER 9 LEFT AND STRINGER 11 LT PER COOPESA EO C00-3-53-723-98 DATED DEC 4, 199 8 AND BOEING FAX COO-SJO-98-1050RR DATED DEC 3, 1998. (M) 2 L 7 2 4F A16WE 1999011500546 19990115 00546 NM 1999 1 15 P2EA98307 1 19981127 A 5755 654645158 SKIN BOEING 737 737281 138448P NM SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US MA1291 20414 SJO - NR 5 SPOILER DELAMINATED, DEFECT SIZE TOTAL 234 SQUARE INCH. REPAIRED NR 5 SPOILER PER COOPESA EO C00-3-57-709-98 DATED NOV 30, 1998. (M) 2 L 7 2 4F A16WE 1999011500547 19990115 00547 NM 1999 1 15 P2EA98306 1 19981127 A 5755 654645125 SKIN BOEING 737 737281 138448P NM SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - NR 2 SPOILER DELAMINATED, DEFECT SIZE TOTAL 6 SQUARE INCH. REPAIRED NR 2 SPOILER PER COOPESA EO COO-3-57-710-98 D ATED NOV 30, 1998. (M) 2 L 7 2 4F A16WE 1999011500548 19990115 00548 NM 1999 1 15 P2EA98305 1 19981208 A 5330 SKIN BOEING 737 737281 138448P NM BS 299-305 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - PROVISIONAL REPAIR AT FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED FUSELAGE SKIN SECTION FROM BS 299 TO BS 305 BETWEEN STRINGER 12 RT AND STRINGER 14 RT PER SRM 53-30-3 FIG 31, DETAIL III. (M) 2 L 7 2 4F A16WE 1999011500549 19990115 00549 NM 1999 1 15 P2EA98304 1 19981028 A 5751 65464542 SKIN BOEING 737 737281 138448P NM AILERON DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US BN84 20414 SJO - RIGHT AILERON DELAMINATED, DEFECT SIZE TOTAL 20 SQUARE INCH. REPAIRED RIGHT AILERON PER COOPESA EO COO-3-57-703-9 8 DATED NOV 27, 1998. (M) 2 L 7 2 4F A16WE 1999011500550 19990115 00550 NM 1999 1 15 P2EA98303 1 19981127 A 5755 654645125 SKIN BOEING 737 737281 138448P NM SPOILER DELAMINATED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 219US 20414 SJO - NR 7 SPOILER DELAMINATED, DEFECT SIZE TOTAL 325 SQUARE INCH. REPAIRED NR 7 SPOILER PER COOPESA EO COO-3-57-711-98 DATED NOV 30, 1998. (M) 2 L 7 2 4F A16WE 1999011500552 19990115 00552 WP 1999 1 15 99ZZZM28 1 19981005 A 2612 24408032 FIRE LOOP DOUG DC8 DC851 3021920 WP NR 4 ENGINE MALFUNCTIONED A FXLA E ENGINE SHUTDOWN N FALSE WARNING CL CLIMB 1 SO 19 507DC 45855 IN CLIMB-OUT OF MIA EXPERIENCED FIRE WARNING ON NR 4 ENGINE. SHUT DOWN ENGINE RETURNED TO MIA AND LANDED WITHOUT INCIDE NT. INSPECTION REVEALED BROKEN FIRE DETECTOR ELEMENT ON INBOARD AFT COWL. REPLACED ELEMENT, SYSTEM CHECKED OK. RETURN ED AIRCRAFT TO SERVICE. (M) 2 L 7 4 4F 4A25 1999011500553 19990115 00553 WP 1999 1 15 99ZZZM29 1 19981019 A 3222 57153545535 STRUT DOUG DC8 DC8F54 3021926 WP NLG CRACKED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 54FA 45637 CREW REPORTED FINDING A HYDRAULIC LEAK ON NOSE LANDING GEAR DURING PRE-FLIGHT GYE. FOUND CRACK IN NLG OLEO OUTER CYLIND ER APPROX 6 INCH FROM TOP, APPROX 1.5 INCH LONG UNDER DATA PLATE. REPLACE NLG OLEO ASSEMBLY PER MM 32-2-0. (M) 2 L 7 4 4F 4A25 1999011500554 19990115 00554 EU 1999 1 15 C2XA98IA496 1 19981220 A 5230 S52376105206 FRAME AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR WAS FOUND TO HAVE A CRACKED FRAME. THE AFFECTED FRAME WAS REPAIRED USIN G A DOUBLER REPAIR IAW THE ATR 42-320 SRM 51-25-04, 51-21-28, AND 51-70-00. THE AIRCRAFT WAS THEN APPROVED FOR RETURN T O SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500555 19990115 00555 EU 1999 1 15 C2XA98IA497 1 19981220 A 5230 S5237611420502 ANGLE AEROSP ATR42 ATR42320 8680930 EU CARGO DOOR CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE CARGO DOOR WAS FOUND TO HAVE A CRACKED HINGE FITTING ATTACH ANGLE. THE AFFECTED AN GLE WAS REMOVED AND REPLACED IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M ) 2 H 7 2 4T RT A53EU 1999011500556 19990115 00556 EU 1999 1 15 C2XA98IA499 1 19981220 A 5311 S53672406208 FRAME AEROSP ATR42 ATR42320 8680930 EU BS 36 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, FRAME 36 WAS FOUND CORRODED. MAINTENANCE REPAIRED THE AFFECTED FRAME USING A DOUBLER R EPAIR IAW THE ATR 42-320 SRM 53-61-40, 53-21-42, AND 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. ( M) 2 H 7 2 4T RT A53EU 1999011500557 19990115 00557 EU 1999 1 15 C2XA98IA500 1 19981220 A 5313 S53672409208 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, STRINGER 15R WAS FOUND CORRODED AT FRAME 40. MAINTENANCE REPAIRED THE AFFECTED STRINGE R USING A SPLICE REPAIR IAW THE ATR 42-320 SRM 51-24-01, 53-00-00. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE . (M) 2 H 7 2 4T RT A53EU 1999011500558 19990115 00558 EU 1999 1 15 C2XA98IA501 1 19981220 A 5311 S53672404206 FRAME AEROSP ATR42 ATR42320 8680930 EU BS 34 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, FRAME 34 WAS FOUND CORRODED. MAINTENANCE REPAIRED THE AFFECTED FRAME IAW THE ATR 42-32 0 SRM 53-61-40, 51-21-28. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500559 19990115 00559 EU 1999 1 15 C2XA98IA502 1 19981220 A 5347 S5367800123902 SEAT TRACK AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE RIGHT OUTBOARD SEAT TRACK WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SEAT TRACK IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500560 19990115 00560 EU 1999 1 15 C2XA98IA503 1 19981220 A 5313 S53571400214 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 27 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, STRINGER 16R WAS FOUND CORRODED FROM FRAME 27 TO FRAME 29. MAINTENANCE REMOVED AND REP LACED THE AFFECTED STRINGER IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500561 19990115 00561 EU 1999 1 15 C2XA98IA504 1 19981220 A 5313 S53572605202 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 27 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, STRINGER 18R WAS FOUND CORRODED FROM FRAME 27 TO FRAME 29. MAINTENANCE REMOVED AND REP LACED THE AFFECTED STRINGER IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500562 19990115 00562 EU 1999 1 15 C2XA98IA505 1 19981220 A 5313 S53572103244 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 30 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, STRINGER 17R WAS FOUND CORRODED FROM FRAME 30 TO FRAME 31. MAINTENANCE REMOVED AND REP LACED THE AFFECTED STRINGER IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500563 19990115 00563 EU 1999 1 15 C2XA98IA506 1 19981220 A 5320 S53572103200 CLIP AEROSP ATR42 ATR42320 8680930 EU BS 30 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE STRINGER CLIP AT FRAME 30 STRINGER 16 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500564 19990115 00564 EU 1999 1 15 C2XA98IA507 1 19981220 A 5320 S53572103244 CLIP AEROSP ATR42 ATR42320 8680930 EU BS 30 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE STRINGER CLIP AT FRAME 30 STRINGER 17 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500565 19990115 00565 EU 1999 1 15 C2XA98IA508 1 19981220 A 5320 S53572103210 CLIP AEROSP ATR42 ATR42320 8680930 EU BS 30 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE STRINGER CLIP AT FRAME 30 STRINGER 18 WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CLIP IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500566 19990115 00566 EU 1999 1 15 C2XA98IA509 1 19981220 A 5320 S53971424200 INTERCOSTAL AEROSP ATR42 ATR42320 8680930 EU BS 27-28 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE INTERCOSTAL BETWEEN FRAMES 27A AND 28 WAS FOUND CRACKED. MAINTENANCE REPAIRED THE AFFECTED INTERCOSTAL IAW THE ATR 42-320 SRM 51-70-00. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500567 19990115 00567 EU 1999 1 15 C2XA98IA510 1 19981220 A 5320 S53971402214 SUPPORT AEROSP ATR42 ATR42320 8680930 EU BS 27 CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE VERTICAL SUPPORT AT FRAME 27A FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SUPPORT IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500568 19990115 00568 EU 1999 1 15 C2XA98IA511 1 19981220 A 5320 S53173206200 FITTING AEROSP ATR42 ATR42320 8680930 EU COCKPIT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE PILOTS SEAT ATTACH FITTING WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED TH E AFFECTED FITTING IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500569 19990115 00569 EU 1999 1 15 C2XA98IA512 1 19981220 A 5320 S53173206201 FITTING AEROSP ATR42 ATR42320 8680930 EU COCKPIT CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE CO-PILOTS SEAT ATTACH FITTING WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW THE ATR 42-320 SRM 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500570 19990115 00570 EU 1999 1 15 C2XA98IA513 1 19981220 A 5320 S53970916202 BRACKET AEROSP ATR42 ATR42320 8680930 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE ATTACH BRACKET FOR PANEL 292 CR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACE D THE BRACKET IAW THE ATR 42-320 SRM 53-91-42. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500571 19990115 00571 EU 1999 1 15 C2XA98IA514 1 19981220 A 5313 S53671000200 STRINGER AEROSP ATR42 ATR42320 8680930 EU BS 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, STRINGER 17R WAS FOUND CORRODED AT FRAME 39. MAINTENANCE REMOVED AND REPLACED THE AFFE CTED STRINGER IAW THE ATR 42-320 SRM 51-21-28 AND 51-25-02. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999011500572 19990115 00572 EU 1999 1 15 C2XA98IA515 1 19981220 A 5311 S5367131120051 FRAME AEROSP ATR42 ATR42320 8680930 EU BS 37 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, FRAME 37R WAS FOUND CORRODED AT FLOOR LEVEL. MAINTENANCE REPAIRED THE AFFECTED FRAME I AW CONTINETAL EXPRESS ENGINEERING CHANGE AUTHORIZATION EX 5310-01013. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERV ICE. (M) 2 H 7 2 4T RT A53EU 1999011500573 19990115 00573 SO 1999 1 15 C2XA98IA476 1 19981208 A 3230 22260001007 VALVE EMB 145 EMB145 SO MLG FAILED A C2XA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 09 15926 145005 IAH - FLT 4240 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDE D WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 HYDRAULIC SYSTEM PRIORITY VALVE AND THE AIRCRAFT WAS APPR OVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500574 19990115 00574 SO 1999 1 15 C2XA98IA485 1 19981214 A 5320 14522459001 SUPPORT EMB 145 EMB145 SO FUSELAGE CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE RAMP SUPPORT WAS FOUND TO BE CORRODED AT FRAME 20 RIGHT. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED SUPPORT AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500575 19990115 00575 SO 1999 1 15 C2XA98IA484 1 19981214 A 5320 7321030503 FITTING EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE AFT GALLEY INBOARD AFT FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND R EPLACED THE AFFECTED FITTING, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500576 19990115 00576 SO 1999 1 15 C2XA98IA483 1 19981214 A 5320 7321030503 FITTING EMB 145 EMB145 SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 17928 145007 IAH - DURING C-CHECK INSPECTION, THE AFT GALLEY INBOARD FORWARD FITTING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED A ND REPLACED THE AFFECTED FITTING, AND THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT T00011AT 1999011500577 19990115 00577 NE 1999 1 15 P2EA98253 2 19981111 A 7200 ENGINE BOEING 737 737222 1384473 NM PWA JT8 JT8D7 52053 NE NR 2 OVERTEMP A P2EA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CE 05 603DJ 19955 FLT 422 - MDW - NO EMERGENCY DECLARED LANDING UNEVENTFUL. ON TAXI IN OVERHEAT DETECTOR, NR 2 ENGINE CAME ON. ENGINE SH UT DOWN. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999011500578 19990115 00578 WP 1999 1 15 VTZA98304 2 19981003 A 7260 CHIP LIGHT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE ILLUMINATED A VTZA O OTHER J WARNING INDICATION CR CRUISE 1 EA 27 333UE 41101 FLT 6175 - IAD-JFK - DURING CRUISE, EXPERIENCED A RIGH ENGINE CONTAMINATION LIGHT. AIRCRAFT DECLARED AN EMERGENCY AND M ADE AN UNEVENTFUL LANDING AT JFK. MAINTENANCE CONTROL DISPATCHED MAINTENANCE TO THE AIRCRAFT WHERE THE MAINTENANCE PERS ONNEL INSPECTED THE RIGH ENGINE CHIP DETECTOR AND FOUND TWO SMALL SLIVER, WHICH WERE WITHIN LIMITS, ON THE CHIP DETECTOR AND FOUND TWO SMALL SLIVERS, WHICH WERE WITHIN LIMITS, ON THE CHIP DETECTOR. MAINTENANCE CLEANED THE CHIP DETECTOR, CO MPLIED WITH REQUIRED ENGINE RUNS, WHICH WERE SATISFACTORY. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999011500579 19990115 00579 WP 1999 1 15 VTZA98299 2 19980924 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RT NACELLE MALFUNCTIONED A VTZA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 27 488UE 907 FLT 6329 - PIT-IAD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE FLUCTUATION. AIRCR AFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND GROUND RAN AIRCRAFT AND COULD NOT DUPLICATE PR OBLEM, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999011500580 19990115 00580 WP 1999 1 15 VTZA98284 2 19980906 A 7200 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT NACELLE MALFUNCTIONED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 480UE 894 FLT 6473 - JFK-IAD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT ENGINE WOULD ONLY PRODUCE 98.5 PER CENT RPM. MAINTENANCE INSPECTED AND ADJUSTED X SCREW, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO S ERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999011500581 19990115 00581 NE 1999 1 15 REXA98110 2 19980924 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RIGHT MALFUNCTIONED A REXA A UNSCHED LANDING Y ENGINE STOPPAGE CL CLIMB 1 SO 25 327PX 340A059 DURING TEST FLIGHT, RIGHT ENGINE PROP STARTED TO AUTOCOARSEN WITH ITT CLIMB WHEN POWER WAS REDUCED ENGINE DID UNCOMMANDE D ENGINE SHUT DOWN. PERFORMED GROUND POWER RUNS/ENGINE OVERSPEED TEST. ALL PARAMETERS NORMAL NO PROBLEMS NOTED. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1999011500582 19990115 00582 NE 1999 1 15 VTZA98350 2 19981118 A 7210 6047T63P04 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED A VTZA A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 EA 27 629BR 7251 FLT 6700 - IAD-BNA - DURING TAKEOFF, EXPERIENCED A SMELL OF SMOKE IN THE CABIN ALONG WITH THE ACTIVATION OF THE LAVATORY SMOKE DETECTOR. A/C DECLARED AN EMERGENCY AND RETURNED TO IAD WHERE IT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE C ONTROL WAS NOTIFIED AND AIRCRAFT TAXIED TO THE GATE WHERE MAINTENANCE WAS NOTIFIED. MAINTENANCE T/S THE DISCREPANCY AND OPENED A DMI AGAINST THE LEFT ACM SYSTEM DMI NR 54655, DMI IS STILL OPEN. AIRCRAFT WAS THEN RELEASED FOR SERVICE. MAI NTENANCE CLOSED DMI 54655, DMI IS STILL OPEN. AIRCRAFT WAS THEN RELEASED FOR SERVICE. MAINTENANCE CLOSED DMI 54655 ON 11-21-98 BY REMOVING AND REPLACING LEFT ENGINE NR 3 CARBON SEAL, OPS CHECK OK. AIRCRAFT WAS RELEASED FOR RETURN TO SERV 2 L 7 2 4F 4 F RT A21EA E15NE 1999011500583 19990115 00583 NE 1999 1 15 99ZZZM30 2 19980712 A 7261 CAP BOEING 727 727227 1384078 NM PWA JT8 JT8D17R 52049 NE NR 2 ENGINE MISSING A AMTA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 GL 11 773AT 22004 DURING CRUISE, NR 2 ENGINE OIL PRESSURE DROPPED BELOW 30 PSI WITH LOW OIL PRESSURE LIGHT ON. MAX OIL TEMP 130 DEGREES C . ENGINE WAS SHUTDOWN. DID TURNBACK. FOUND NR 2 ENGINE OIL CAP MISSING. REPLACED CAP AFTER SERVICING WITH 19.5 QTS O F OIL. CHECKED FOR LEAKS AND OK. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999011500584 19990115 00584 WP 1999 1 15 VTZA98316 2 19981022 A 7321 31059006 FCU JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE FAILED A VTZA E ENGINE SHUTDOWN J WARNING INDICATION LD LANDING 1 EA 27 314UE 41027 FLT 6627 - IAD-ORH - AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS LEFT ENGINE SPOOLED DOWN AND OIL AND GENERATOR WARNING LIGHTS ILLUMINATED. CREW SHUT DOWN LEFT ENGINE. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FUEL CONTROL, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999011500585 19990115 00585 WP 1999 1 15 VTZA98309 2 19981017 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE MALFUNCTIONED A VTZA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 27 333UE 41101 FLT 6510 - IAD-LGA - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT OIL CONTAMINATION WARNING LIGHT ILL UMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED CLEANED AND REINSTALLE D CHIP DETECTOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999011500586 19990115 00586 NE 1999 1 15 WRLA98097 2 19981026 A 7321 4059025906 FCU DOUG MD11 MD11 3023602 NM PWA 4462 PW4462 NE FUEL SYSTEM INOPERATIVE A WRLA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 EA 27 278WA 48746 DURING INITIAL TAKEOFF ROLL, FLIGHT CREW RECEIVED TANK 2 PUMPS 'OFF' ALERT. FLIGHT CREW ELECTED TO RETURN TO GATE. AIR CRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE PERSONNEL INOP FUEL SYSTEM CONTROL AUTO MODE. DEFERRED PE R MEL 28-01-1. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F 4 F RT A22WE E24NE 1999011500587 19990115 00587 NE 1999 1 15 P2EA98233 2 19981104 A 7261 815864 PUMP BOEING 737 737281 138448P NM PWA JT8 JT8D9A 52048 NE ENGINE FAILED A P2EA K NONE K FLUID LOSS DE DESCENT 1 CE 05 219US 20414 MCI - FLT 270 - NO EMERGENCY DECLARED LANDING UNEVENTFUL. ON DESCENT INTO MCI, NR 2 OIL QTY STARTED TO DECREASE. ON AP PROACH QTY WENT TO ZERO, OIL PRESSURE AND TEMPERATURE WERE WITHIN LIMITS. REPLACED NR 6 BEARING OIL SCAVENGE PUMPED PER PWA MM 72-50, DRAINED OIL TANK. REPLACED MAIN OIL FILTER PER MM 79-11-0. INSPECTED OIL CHIP DETECTORS PER MM 79-21-31 , SERVICED OIL TANK TO FULL PER MM 12-13-11. OPS CHECK, LEAK CHECKS OK. ASSIGNED WATCH ITEM TO REPLACED MAIN OIL FILTE R AT 50 HOURS PER MM 72-00-0-2A. (M) 2 L 7 2 4F 4 F A16WE E2EA 1999011500589 19990115 00589 WP 1999 1 15 VTZA98324 2 19981030 A 7260 8937421 CHIP LIGHT JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE ILLUMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 306UE 41020 FLT 6324 - EWR-IAD - DURING CRUISE, AIRCRAFT MADE UNSCHEDULED LANDING DUE TO RT ENGINE OIL CONTAMINATION WARNING LIGHT I LLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. AIRCRAFT FERRIED TO LAND. MAINTENANCE INSPECTED AND R EMOVED, CLEANED AND REINSTALLED RT ENGINE CHIP DETECTOR. OPS CHECKED OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999011500590 19990115 00590 WP 1999 1 15 VTZA98339 2 19981116 A 7321 31059005 FCU JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 27 322UE 41058 FLT 6190 - IAD-BDL - DURING TAKEOFF, EXPERIENCED A DISCREPANCY WITH THE RIGHT ENGINE ONLY REACHING 58 PERCENT TORQUE ON TAKEOFF ROLL. AIRCRAFT ABORTED TAKEOFF AND NOTIFIED MAINTENANCE CONTROL. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINT ENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT FUEL CONTROL UNIT IAW APPLICABLE MAINTENANCE PROCEDURES. ALL CHECKS WERE ACCOMPLISHED AS OUTLINED IN THE MM. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999011500615 19990115 00615 NM 1999 1 15 9811136303 1 19980825 A 3397 WIRE BOEING 747 747451 1384940 NM CABIN LOOSE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 663US 23818 DURING LINE CHECK, FOUND E ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED ELECTRICAL WIRE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999011500616 19990115 00616 NM 1999 1 15 9811146309 1 19981008 A 3350 SWITCH BOEING 747 747451 1384940 NM CABIN OUT OF POSITION A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 669US 24224 DURING LINE CHECK, FOUND A AND B ZONE FLOOR PATH EMERGENCY LIGHTS ON THE RIGHT SIDE INOPERATIVE. PLACED EMERGENCY LIGHT SWITCH TO ARM POSITION AND ALLOWED BATTERY PACKS TO CHARGE, OPERATIONAL CHECK GOOD. 2 L 7 4 4F RT A20WE 1999011500617 19990115 00617 NM 1999 1 15 9811156614 1 19980830 A 3350 BATTERY BOEING 747 747251B 1384892 NM DOOR 5L & 5R DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 614US 20359 DURING LINE CHECK, FOUND E ZONE FLOOR PATH EMERGENCY LIGHTS AND DOOR 5L AND DOOR 5R EXIT SIGN INOPERATIVE. REPLACED BAT TERY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999011500618 19990115 00618 NM 1999 1 15 9811166625 1 19980926 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 625US 21707 DURING LINE CHECK, FOUND B ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999011500619 19990115 00619 NM 1999 1 15 9811176626 1 19980918 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 626US 21708 DURING LINE CHECK, FOUND B ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999011500620 19990115 00620 NM 1999 1 15 9811186627 1 19980927 A 3350 POWER SUPPLY BOEING 747 747251B 1384892 NM CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 627US 21709 DURING LINE CHECK, FOUND ZONE FLOOR PATH EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CH ECK GOOD. 2 L 7 4 4F A20WE 1999011500621 19990115 00621 NM 1999 1 15 9811196628 1 19980920 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 628US 22389 DURING LINE CHECK, FOUND A ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999011500622 19990115 00622 NM 1999 1 15 9811206632 1 19980914 A 3350 BATTERY BOEING 747 747251B 1384892 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 632US 23112 DURING LINE CHECK, FOUND B AND C ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY, OPERATIONAL CHECK GOOD . 2 L 7 4 4F A20WE 1999011500623 19990115 00623 NM 1999 1 15 9811216608 1 19981012 A 3350 BATTERY PACK BOEING 747 747151 1384891 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 608US 19785 DURING LINE CHECK, FOUND C ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK, OPERATIONAL CHECK GOOD. 2 L 7 4 4F A20WE 1999011500631 19990115 00631 NM 1999 1 15 98UAL900544 1 19981110 A 4920 APU BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE APU COMPT FOD A UALA O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NR NOT REPORTED 1 WP 29 529UA 25019 61357 OIL LIKE ODOR DETECTED IN REAR CABIN AREA. THE ODOR WAS NOT STRONG OR PUNGENT, BUT IT DID SET OFF THE AFT LAV SMOKE DET ECTORS. *S/D* THE APU WAS REPLACED DUE TO CONTAMINATED PNEUMATICS. DURING DISASSEMBLY AND SHOP INSPECTION OF THE APU A PLASTIC BAG WAS FOUND IN THE INLET. 2 L 7 2 4F 4 F RT A2NM E17NE 1999011500632 19990115 00632 NM 1999 1 15 98UAL900552 1 19981121 A 2121 FAN BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE E & E COMPT FOD A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 571UA 26681 DIVERTED TO CLE DUE TO AN EQUIPMENT OVERHEAT INDICATION. *S/D* THE OVERHEAT INDICATION WAS TO REMOVE DEBRIS FROM THE E QUIPMENT COOLING FANS. THE SOURCE OF THIS DEBRIS IS PRESENTLY UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A2NM E17NE 1999011500633 19990115 00633 NM 1999 1 15 98UAL900564 1 19981123 A 2530 2510001901 OVEN BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE GALLEY SMOKING A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 948UA 26691 GALLEY STARTED TO SMOKE. *S/D* OVEN INOP. REPLACED OVEN. 2 L 7 2 4F 4 F RT A16WE E2GL 1999011500634 19990115 00634 WP 1999 1 15 98UAL900598 1 19981205 A 3810 AV16E3253C VALVE ITT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE WATER SYSTEM MALFUNCTIONED A UALA O OTHER O OTHER DE DESCENT 1 WP 29 1853U 47812 ON DESCENT AT 19000 FEET HEARD A LOUD BANG. *S/D* AFTER INSPECTION A DENT WAS FOUND ON THE NR 1 RT SLAT DUE TO THE BUI LD UP OF ICE ON THE POTABLE WATER SYSTEM DRAIN PORT. REPLACED DRAIN VALVE AND TESTED SYSTEM FOR LEAKS. CONFIRMED CONFI GURATION AND PERFORMED OPERATIONAL CHECK. 2 L 7 3 4F 4 F A22WE E23EA 1999011500635 19990115 00635 1999 1 15 98UAL900615 4 19981226 A 3416 2057011 ALTIMETER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT COCKPIT DEFECTIVE A UALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 29 340UA 24244 ALTIMETER FAILED. *S/D* CAPTAIN'S SERVO ELECTRIC ALTIMETER INDICATOR FLAGGED OFF AND FROZE. REPLACED CAPTAIN'S ALTIME TER AND CHECKED NORMAL. 2 L 7 2 4F 4 F RT A16WE E2GL 1999011500636 19990115 00636 NM 1999 1 15 98UAL900616 1 19981224 A 2781 31EN16 SWITCH BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LT SLATS FAILED A UALA O OTHER N FALSE WARNING NR NOT REPORTED 1 WP 29 585UA 26709 LANDED LAX UNDER AMBER ALERT DUE TO LEADING EDGE SLAT ASYMMETRY. *S/D* FAILURE OF ONE OF TWO INBOARD LEADING EDGE SLAT LOSS SWITCHES CAUSED THE EICAS MESSAGE, LIGHT AND SHUTDOWN OF THE LEADING EDGE SLAT SYSTEM. REPLACED BOTH INBOARD SLAT LOSS SWITCHES AND RETURNED AIRCRAFT TO SERVICE WITHOUT FURTHER INCIDENT. FAILURE OF THESE SWITCHES IS A KNOWN 757 INDU STRY WIDE PROBLEM. UNITED IS CORRECTING THE PROBLEM VIA COA 504070 DURING HEAVY MAINTENANCE VISITS ON ALL EFFECTIVE 757 AIRCRAFT. 2 L 7 2 4F 4 F RT A2NM E17NE 1999011500637 19990115 00637 NM 1999 1 15 98UAL900617 1 19981228 A 3040 70001325 CIRCUIT BREAKER BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WINDSHIELD FAILED A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 362UA 24455 LEFT WINDSHIELD HEAT INOP. *S/D* LEFT WINDSHIELD HEAT INOP DUE TO WEAK C228 CIRCUIT BREAKER. REPLACED CIRCUT BREAKER. L EFT WINDOW HEAT CHECKS GOOD. 2 L 7 2 4F 4 F RT A16WE E2GL 1999011500638 19990115 00638 1999 1 15 98UAL900618 4 19981227 A 3416 ALTIMETER SMITH INDUST 2057011 BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE COCKPIT INOPERATIVE A UALA A UNSCHED LANDING O OTHER CL CLIMB 1 WP 29 915UA 25382 ALTIMETER IS INOP. *S/D* TROUBLESHOOTING WAS INEFFECTIVE. REPLACED ALTIMETER, PITOT PROBE, AND CIRCUIT BREAKER. 2 L 7 2 4F 4 F RT A16WE E2GL 1999011500639 19990115 00639 WP 1999 1 15 98UAL900619 1 19981221 A 2497 WIRE DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE BS 595 FAILED A UALA O OTHER O OTHER UK UNKNOWN 1 WP 29 1854U 47813 NR 1 AC BUS CIRCUIT BREAKERS POPPING. *S/D* FOUND BURNED WIRES IN CEILING OF FWD COMPARTMENT LOCATED AT FWD WALL, APPROX STA 595 LHS. REPLACED ALL THE WIRES/CABLES THAT WERE INVOLVED. 2 L 7 3 4F 4 F A22WE E23EA 1999011500640 19990115 00640 NM 1999 1 15 98UAL900620 1 19981229 A 3350 900835A BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CARGO DOOR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7298U 21893 EMERGENCY LIGHT AT AFT CARGO DOOR INOPERATIVE. *S/D* REPLACED BATTERY PACK AND LIGHT CHECKED OK. 2 L 7 3 4F 4 F A3WE E2EA 1999011500641 19990115 00641 NM 1999 1 15 98UAL900621 1 19981228 A 3350 582214 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE ROW 26-28 DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7271U 21418 FLOOR LIGHTING INOPERATIVE FROM SEAT ROW 26 TO 28. *S/D* REPLACED BATTERY PACK, EEL STRIP AND LAMPS. 2 L 7 3 4F 4 F A3WE E2EA 1999011500655 19990115 00655 NM 1999 1 15 99UAL900016 1 19980107 A 2751 18195816 TRANSMITTER BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 5 TE FLAP OUT OF ADJUST A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 611UA 21872 EICAS MSG TE FLAP DISAGREE DISPLAYED. TRAILING EDGE LIGHT ILLUMINATES WHEN ANY TE FLAP POSITION SELECTED. FLAPS FAIL TO MOVE TO SELECTED POSITION. RETURNED TO FIELD. AMBER ALERT. *S/D* THE FLAP/SLAT ELECTRONICS UNIT SENSED A T/E FLAP D ISAGREE CONDITION. THIS CAUSED THE 'TE DISAGREE' MSG TO APPEAR ON EICAS AND THE TE LIGHT TO ILLUMINATE. LOGIC IN THE F SEU INITIATED TE FLAP FAILURE PROTECTION SHUT DOWN WHICH INHIBITED FLAP MOVEMENT. THE TE FLAP DISAGREE CONDITION WAS SE NSED BECAUSE OF AN OUT OF RIG TE FLAP POSITION TRANSMITTER. ADJUSTED THE NR 5 TE FLAP POSITION TRANSMITTER TO CORRECT R IG POSITION PER MM. ALL FINAL OPERATION CHECKS WERE OK PER MM. 2 L 7 2 4F 4 F RT A1NM E3NE 1999011500661 19990115 00661 WP 1999 1 15 SCNA98534 1 19981219 A 5320 FRAME DOUG DC10 DC1015 3022118 WP CARGO DOORWAY CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, THE AFT CARGO DOOR, AFT FRAME WAS FOUND TO BE CORRODED OUT OF LIMITS. INSTALLED A NEW FRAME, ANGLE AND DOOR SEAL RETAINER PER SRM 513501 AND 513301 VOLUME II. 2 L 7 3 4F A22WE 1999011500662 19990115 00662 WP 1999 1 15 SCNA98535 1 19981219 A 5230 PIN DOUG DC10 DC1015 3022118 WP C1 DOOR DAMAGED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, THE FORWARD CARGO DOOR HINGE PIN WAS FOUND TO EXHIBIT CORROSION AND DAMAGED THREADS. R EPLACED HINGE PIN PER MM 523104. 2 L 7 3 4F A22WE 1999011500663 19990115 00663 WP 1999 1 15 SCNA98536 1 19981218 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1841-2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT LEFT OUTBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 510000 VOLUME II ( C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25. 2 L 7 3 4F A22WE 1999011500664 19990115 00664 WP 1999 1 15 SCNA98537 1 19981218 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1841-2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT RIGHT OUTBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 510000 VOLUME II (C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25. 2 L 7 3 4F A22WE 1999011500665 19990115 00665 WP 1999 1 15 SCNA98538 1 19981218 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1837-2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1837 TO 2007 IN THE AFT LEFT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1837 TO 2007 PER SRM 512000 VOLUME II (C ) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25. 2 L 7 3 4F A22WE 1999011500666 19990115 00666 WP 1999 1 15 SCNA98539 1 19981218 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1841-2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT RIGHT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 512000 VOLUME II ( C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25. 2 L 7 3 4F A22WE 1999011500667 19990115 00667 WP 1999 1 15 SCNA98540 1 19981218 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1841-2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT RIGHT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 512000 VOLUME II ( C) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25. 2 L 7 3 4F A22WE 1999011500668 19990115 00668 WP 1999 1 15 SCNA98541 1 19981218 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 1841-2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, A GALLEY FLOOR SUPPORT WAS FOUND CORRODED OUT OF LIMITS AT FS 1841 TO 2007 IN THE AFT LEFT INBOARD GALLEY FLOOR. REMOVED AND REPLACED THE GALLEY FLOOR SUPPORT AT FS 1841 TO 2007 PER SRM 512000 VOLUME II (C ) AND SRM 512101 VOLUME II PAGE 1, 2, 21, 24 AND 25. 2 L 7 3 4F A22WE 1999011500669 19990115 00669 WP 1999 1 15 SCNA98542 1 19981219 A 5320 SUPPORT DOUG DC10 DC1015 3022118 WP BS 2007 CORRODED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 153SY 48276 DURING A HEAVY MAINTENANCE CHECK, OUT OF LIMITS CORROSION ON THE BULKHEAD FLOOR SUPPORT WAS NOTED AT FS 2007 AT THE AFT BULKHEAD RBL 60 AND LBL 23 AT CABIN FLOOR LEVEL. REMOVED AND REPLACED TEE FLOOR SUPPORT PER SRM 510000 VOLUME II (C) AN D SRM 512101 VOLUME II PAGES 1, 2, 21, 24 AND 25 AND SRM 534000 VOLUME I. 2 L 7 3 4F A22WE 1999011500708 19990115 00708 EU 1999 1 15 99ZZZX212 1 19980309 A 3340 1179203103 CONTROL UNIT BOLKMS 117 BK117A3 5626015 EU EXTERNAL LIGHTS FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 0631 7063 CONTROL UNIT FOR EXTERNAL LIGHTS HAS INTERNAL SHORT. TRIPPED CIRCUIT BREAKERS UPON INSTALLATION. REPLACED WITH NEW UNI T, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999011500709 19990115 00709 NE 1999 1 15 99ZZZX213 2 19981022 A 7230 414129011 PT ROTOR BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR DAMAGED A P R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 1701 SC12577 7111 LE45218EA ENGINE REMOVED FOR LOW POWER AND 80 PERCENT N2 INDICATION. UPON TEAR DOWN AND INSPECTION, FOUND THE PT ROTOR RETENTION LOCK CUP AND NUT HAD LOOSENED WHICH RESULTED IN RETENTION THREAD DAMAGE. PART TOTAL CYCLES: 4,959.8. 1 G 7 2 3U 3 U H13EU E5NE 1999011500710 19990115 00710 NE 1999 1 15 99ZZZX214 2 19981218 A 7321 324473513 FCU BENDIX BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE NR 2 ENGINE MALFUNCTIONED A HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 3893P 2707 A20452 33012 CPPS62245 AIRCRAFT EXPERIENCED TORQUE SPLIT IN-FLIGHT. NR 2 ENGINE TORQUE LOW. RETURNED TO BASE AND LANDED WITHOUT INCIDENT. MA INTENANCE REPLACED NR 2 ENGINE AUTOMATIC FUEL CONTROL UNIT. REF: P&W IPC, CHAPTER 72-00-10, FIGURE 1, ITEM 11. 1 G 7 2 4U 4 U H4SW E22EA 1999011500717 19990115 00717 NE 1999 1 15 99ZZZX221 2 19981022 A 7250 408108309 NUT BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 156 7111 LE45218EA SECONDARY DAMAGE TO LOCK CUP FAILURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999011500718 19990115 00718 EU 1999 1 15 99ZZZX222 1 19981201 A 6230 ROD BENDIX 430110217 BOLKMS 117 BK117B1 5626012 EU MAIN ROTOR WORN A A R7MA O OTHER J WARNING INDICATION AP APPROACH 1 NM 11 71703 3914 1546 2259 7227 DURING AIRCRAFT APPROACH, THE COLLECTIVE WAS LOWERED AND THE NR 1 ENGINE BEGAN A SERIES OF COMPRESSOR STALLS AND HIGH TO T. POWER REDUCED AND AIRCRAFT LANDED WITHOUT INCIDENT. SUBMITTER STATED NEW ROD AND NEW BELLCRANK AT EACH OVERHAUL MIG HT CURE WEAR PROBLEM SINCE ROD CANNOT BE SEEN ONCE THE FLOW FENCE ACTUATOR IS INSTALLED, HIGHLY RECOMMENDED THAT THESE R ODS AND BELLCRANKS GET CHANGED OUT AT OVERHAUL IF NEEDED. 1 G 7 2 3U H13EU 1999011500719 19990115 00719 EU 1999 1 15 99ZZZX223 1 19981022 A 5320 408211901 FLANGE BOLKMS 117 BK117A4 5626017 EU FUSELAGE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 156 7111 SECONDARY DAMAGE TO LOCK CUP FAILURE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999011500720 19990115 00720 NE 1999 1 15 99ZZZX224 2 19981022 A 7250 408209401 LOCKING CUP BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE LOOSE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 156 7111 LE45218EA LOCK CUP CAME LOOSE. 1 G 7 2 3U 3 U H13EU E5NE 1999011500721 19990115 00721 SW 1999 1 15 99ZZZX225 1 19981227 A 6330 2060335081 FLEXURE ASSY LORD 2060335264 BELL 206 206L1 1182107 SW MAIN ROTOR CRACKED A EGIA K NONE O OTHER IN INSP/MAINT 1 SW 09 600CK 2140 45787 FOUND DELAMINATED ON 100-HOUR INSPECTION. WHEN MOUNT BOLTS WERE LOOSENED, CRACK OPENED UP AND BECAME VISIBLE. 1 G 7 1 3U H2SW 1999011500722 19990115 00722 NE 1999 1 15 99ZZZX226 2 19980911 A 7240 DIFFUSER 70BM035600 AEROSP SA365 AS365N2 8680815 EU TMECA ARRIEL ARRIEL1C 60030 NE ENGINE DAMAGED A OLJA K NONE O OTHER IN INSP/MAINT 1 EA 13 291LL 3975 1049 12045 6402 12045 TEC TECH REP AT FACILITY TO C/W TU 202. SECOND STAGE NOZZLE INSTALLATION AFTER REMOVAL OF MODULES 2 AND 3 HEARD PIECES INSIDE ENGINE. UPON TEAR-DOWN OR SEPARATION OF MODULES 2 AND 3 FOUND DIFFUSER TO HAVE HOLE IN IT, 2 INCHES BY 6 INCHES. PARTS HAD LIBERATED THEMSELVES. THIS NOW IS NOT A FIELD REPAIR, SO MO2 AND MO3 SENT TO FACTORY FOR EVALUATION. LOG C ARDS/LOG BOOK DOES NOT INCLUDE TSN OR TSO OF DIFFUSER, BUT MO3. TSN HOURS - 3,975.1. CYCLES, 8,194.2. TSO HOURS = 1,0 49. CYCLES, 2,167.4. WAITING FOR EVALUATION REPORT. 1 G 7 2 3U 3 U RT H10EU E19EU 1999011500733 19990115 00733 NM 1999 1 15 AWXA9900007 1 19981221 A 5512 SKIN BOEING 737 7373S3 1384711 NM LT HORIZ STAB DENTED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 LT STAB BOTTOM APPROX 4 FEET FROM OUTBOARD TIP, SKIN HAS CREASE 16 LONG AND 4 WIDE WITH FILLER APPLIED. REPAIRED PER AW A ER 3-55-13-05. 2 L 7 2 4F RT A16WE 1999011500734 19990115 00734 NM 1999 1 15 AWXA9900008 1 19981221 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7373S3 1384711 NM BS 967 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 SURFACE CORROSION ON FRAME FWD OF STATION 967 LT OUTBOARD MAIN CABIN 25 FROM CENTERLINE. REPAIRED FLOORBEAM PER SRM 51- 70-12 PG 1-7, SRM 53-00-51 PG 201-211, SRM 51-40-02 PG 9-11. 2 L 7 2 4F RT A16WE 1999011500735 19990115 00735 NM 1999 1 15 AWXA9900009 1 19981221 A 5315 BAC1505100617 FLOORBEAM BOEING 737 7373S3 1384711 NM BS 947 CORRODED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 MAIN CABIN AT STA 947 FROM LBL 24 HAS DEEP PITTING AND DRILL START HOLES ON UPPER T CAP. REPAIRED PER SRM 53-60-51, 53- 00-51, 51-40-02, 51-20-01 AND MM 51-21-00. 2 L 7 2 4F RT A16WE 1999011500736 19990115 00736 NM 1999 1 15 AWXA9900010 1 19981221 A 5330 65C339301 SKIN BOEING 737 7373S3 1384711 NM FUSELAGE CRACKED A AWXA K NONE O OTHER IN INSP/MAINT 1 WP 28 312AW 24060 FUSELAGE SKIN CRACKED AT EQUIPMENT COOLING EXHAUST CUT OUT FROM AFT EDGE TO FASTENER AND BEYOND. REPAIRED FUSELAGE SKIN PER S/B 737-53-1117. 2 L 7 2 4F RT A16WE 1999011500739 19990115 00739 NM 1999 1 15 UPS99228339 1 19981228 A 5510 BEAM BOEING 727 727172C 1384058 NM RT HORIZ STAB CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 916UP 19808 INSPECTION TYPE-C, CORROSION (C55-391-20.02-02) RT HORIZONTAL STAB UPPER T/E BEAM AT ELEVATOR STATION 99. REMOVED CORRO SION REPAIRED T/E BEAM PER SRM 55-10-6, 51-30-02, 55-10-1. 2 L 7 3 4F A3WE 1999011500752 19990115 00752 SO 1999 1 15 SWIA971360 1 19981231 A 7712 CONDITIONER EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT ENGINE FAILED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 290SW 120317 DURING CLIMBOUT, LEFT ENGINE TORQUE GAUGE BECAME ERRATIC, FLUCTUATIONS OF MORE THAN 20 PERCENT. COMPLIED WITH QRH WITH NO CHANGES. RETURNED TO SFO. REPLACED TORQUE SIGNAL CONDITIONER, CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999011500762 19990115 00762 NE 1999 1 15 99ZZZX230 1 19981218 A 2913 7665009808101 PUMP ABEX SKRSKY S76 S76A 8143006 NE HYDRAULIC SYSTEM LEAKING A HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 911MJ 190291 760231 NR 1 HYDRAULIC SYSTEM LOW LEVEL LIGHT ILLUMINATED IN-FLIGHT. RETURNED TO BASE AND LANDED WITHOUT INCIDENT. SYSTEM HAD LOST FLUID THROUGH NR 1 HYDRAULIC PUMP SEAL DRAIN. MAINTENANCE REPLACED HYDRAULIC PUMP. REF: S-76 IPC, CHAPTER 29-10- 01, FIGURE 1, ITEM 12. 1 G 7 2 3U H1NE 1999011500770 19990115 00770 GL 1999 1 15 99ZZZX238 2 19981015 A 7200 ENGINE SKRSKY S76 S76C 8143008 NE ALLSN 250C 250C30S 03013 GL NR 2 FAILED A A HEEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 SW 03 911MJ 9981 1958 760231 CAE890522S IN-FLIGHT, NR 2 ENGINE OIL PRESSURE DROPPED WITH OIL PRESSURE LIGHT ILLUMINATION. PILOT SECURED ENGINE AND MADE UNEVEN TFUL SINGLE ENGINE LANDING. MAINTENANCE FOUND 3 QUARTS OF OIL CONSUMPTION AFTER REPLENISHING OIL. SEVEN MINUTES INTO P ENALTY RUN, OIL CONSUMPTION WAS AGAIN 3 QUARTS LOW. REMOVED ENGINE ASSEMBLY. 1 G 7 2 3U 3 U NC H1NE E1GL 1999011500772 19990115 00772 SW 1999 1 15 99ZZZX240 1 19980824 A 3610 5043T25P02 LINE BELL 214 214ST 1182106 SW NR 2 ENGINE BROKEN A HEEA O OTHER R PARTIAL RPM/PWR LOSS NR NOT REPORTED 1 SW 03 59805 ADN12023 28141 NR 2 ENGINE SPOOLED DOWN IN-FLIGHT. SECURED ENGINE AND CONTINUED ON TO LAND BASE. MADE SINGLE ENGINE LANDING WITHOUT I NCIDENT. MAINTENANCE FOUND AIR LINE BROKEN. REF: GENERAL ELECTRIC CT7 IPC, CHAPTER 72-00-00, FIGURE 1, ITEM 10. 2 G 7 2 4U H10SW 1999011500788 19990115 00788 CE 1999 1 15 99ZZZX256 1 19981110 A 2910 240600514 HOSE LEAR 25 25B 5170511 CE RT ENGINE LEAKING A EGQA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 17 225JL 1600 182 AT CRUISE, PILOTS EXPERIENCED A LOSS OF HYDRAULIC PRESSURE. AN UNEVENTFUL LANDING WAS MADE USING EMERGENCY SYSTEMS TO E XTEND LANDING GEAR. MAINTENANCE FOUND A SMALL HOLE IN ENGINE DRIVEN PUMP PRESSURE LINE (RIGHT) AND A CRACKED FLARE ON T HE EMERGENCY HYDRAULIC PUMP PRESSURE LINE. THIS IS A HARD LINE, P/N 2307023-484, WITH 7,605 HOURS TT. THE HARD LINE PO SSIBLY CRACKED DUE TO AGE. NO IDEA WHY THE FLEX LINE ON THE ENGINE FAILED. FLEX LINE INSTALLED 1-95. 2 L 7 2 4J A10CE 1999012000001 19990120 00001 EU 1999 1 20 98UAL900604 1 19981217 A 2910 HYD SYST AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST FAILED A UALA A H UNSCHED LANDING DEACTIVATE SYST/CIRCUITS K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 442UA 820 GREEN HYDRAULIC SYSTEM FAILED. DIVERTED TO DENVER. 2 L 7 2 4F 4 F RT A28NM E40NE 1999012000002 19990120 00002 WP 1999 1 20 ARWA981215 1 19981223 A 7711 VALVE LKHEED 1011 10113851 5265010 WP NR 3 ENGINE EPR LACK OF LUBE A ARWA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 SO 19 306GB 1138 ON T/O ROLL AT K DTW, NR 3 ENGINE UPON REACHING 1.3 EPR TGT REACHED 800 DEGREES, ABORTED T/O AND RETURNED TO RAMP. CHEC KED ENGINE BY 70-00-00, PG 204. NO DEFECTS NOTED, LUBED EPR CONTROL VALVE, RAN ENGINE TO T/O WITH TGT OF 585 DEGREES MA X. 2 L 7 3 4F RT A23WE 1999012000003 19990120 00003 WP 1999 1 20 98FDEA00762 1 19981222 A 3260 SWITCH DOUG DC10 DC1010 3022110 WP LT MLG DOOR INOP A FDEA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 25 377FE 47965 98-309 - LT MAIN GR IND ON BOTH PNLS WAS IND UNSAFE UP. COMPLETE RED TAB PROC, REMAIN UNSAFE UP. DIVERT TO OAK. REMOV ED AND REPLACED LEFT MAIN LAND GEAR DOOR PROXIMITY SWITCH TARGET SUPPORT. NOSE AND RIGHT LAND GEAR PINS INSTALL. POS A ND WARNING OPS NORM. GEAR PINS REMOVED. 2 L 7 3 4F A22WE 1999012000004 19990120 00004 NM 1999 1 20 DL73K982635 1 19981226 A 3244 TIRE BOEING 737 737247 138448D NM RT MLG FAILED A DALA O OTHER O OTHER TO TAKEOFF 1 SO 27 239WA 23187 AFTER TAKEOFF FROM BDL, TOWER NOTIFIED US OF RUBBER DEBRIS ON THE RUNWAY. ON APPROACH TO MCO, AT GEAR EXTENTION HAD A R IGHT MAIN GEAR UNSAFE LIGHT ON AND GREEN LIGHT OFF. FOLLOWED ABNORMAL PROCEDURE. FOUND NR 3 MAIN TIRE LOST CAP AND DAM AGED INBD BRAKE LINE AND HOLDER AND AFT FLAP AND MID FLAP AND GEAR DOWN AND LOCK PROX TARGET. REPLACED NR 3 AND 4 MAIN WHEEL ASSYS. REPLACED BRAKE LINE AND HOLDER, AFT INBOARD FLAP ASSY, MID FLAP BELLCRANK MECHANISM, AND ACCESS PNL. 2 L 7 2 4F A16WE 1999012000005 19990120 00005 EA 1999 1 20 JBXA9800060 1 19981226 A 3260 161271 PIN CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE NLG FAILED A JBXA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SO 05 578ML 7270 NOSE GEAR UNSAFE AND GEAR DISAGREE ON TAKEOFF. REMOVED AND REPLACED NLG UPLOCK PIN IAW CL-65 AMM 32-21-15. PERFORMED E XTENSION AND RETRACTION OF LANDING GEAR SYSTEM IAW CL-65 32-30-00. ALL CHECKS GOOD, RII COMPLIED WITH. 2 L 7 2 4F 4 F RT A21EA E15NE 1999012000006 19990120 00006 EA 1999 1 20 JBXA9800061 1 19981224 A 3620 A18WK SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE RIGHT FAILED A JBXA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 05 579ML 7277 JUST AFTER TAKEOFF FROM RDU, ANTI-ICE DUCT FAIL MESSAGE CAME ON IN FLIGHT. MFD INDICATED A RIGHT FUSELAGE DUCT LEAK. R EMOVED AND REPLACED SENSING ELEMENT A18WK IAW CL-65 MM 36-21-04, PERFORMED OPS CHECK IAW CL-65 MM 36-21-00, NO DEFECTS F OUND. ALSO, PERFORMED GROUND RUNS IAW CL-65 MM 71-00-00. COULD NOT GET ANY ANTI-ICE DUCT FAULTS ON THE GROUND. ALSO, ACCOMPLISHED FUNCTIONAL CHECK FLIGHT DUE TO REPORTED PROBLEM. NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A21EA E15NE 1999012000007 19990120 00007 NM 1999 1 20 SWAA983149 1 19981227 A 3350 BULB BOEING 737 7373T0 1384582 NM CABIN FAILED A SWAA K NONE L NO TEST IN INSP/MAINT 1 SW 07 697SW 23838 DURING PREFLIGHT, FOUND EMERGENCY FLOOR TRACK HAS TWO LIGHTS INOP. RELAMPED AND OPS CKS GOOD PER M/M. 2 L 7 2 4F RT A16WE 1999012000010 19990120 00010 1999 1 20 MALA976277 4 19981227 A 3414 6725353611 AIRSPEED IND SAAB SF340 340B 7860101 EU LT COCKPIT FAILED A MALA A UNSCHED LANDING O OTHER CL CLIMB 1 GL 15 403XJ 340B403 LT AIRSPEED IND DEAD. AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED AIRSPEED IND, OPS CHECKS GOOD. 2 L 7 2 4T RT A52EU 1999012000011 19990120 00011 WP 1999 1 20 VJ9800685 1 19981231 A 3230 CONTROL CABLE DOUG DC9 DC932 3022066 WP NLG OUT OF ADJ A ZZDA A UNSCHED LANDING O OTHER CL CLIMB 1 SO 15 936VV 47397 COULD NOT RETRACT LANDING GEAR AFTER TAKEOFF, STEERING WHEEL LIGNED UP STRAIGHT AND WOULD NOT TURN. ADJUSTED CABLE 118A PER MM 32-31-1, OPS CHECKED GOOD. PERFORMED OPERATIONAL CHECK AND MANUAL EXTENSION CHECK OF LANDING GEAR PER DC9 MM 32 -30-0 AND OPS CHECK GOOD. 2 L 7 2 4F A6WE 1999012000012 19990120 00012 EA 1999 1 20 JBXA9800062 1 19981230 A 5210 MECHANISM CNDAIR CL600 CL6002B19 EA PAX DOOR OUT OF ADJUST A JBXA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CR CRUISE 1 SO 05 574ML 7242 PAX DOOR MESSAGE IN FLIGHT. ADJUSTED CAM ROD, OPS CHECK GOOD IAW AMM 52-11-02-820-801. 2 L 7 2 4F RT A21EA 1999012000016 19990120 00016 NM 1999 1 20 MWEA99015 1 19980617 A 5330 5935822 SKIN DOUG MD88 MD88 3023688 NM WS 536 MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 810ME 48072 INSPECTED REPAIR ON RIGHT WING LOWER SKIN AT REAR SPAR STATION XW 536 FOR SRM CONFORMITY. MTC REMOVED REPAIR, FABRICATE D AND INSTALLED NEW REPAIR DOUBLER. 2 L 7 2 4F RT A6WE 1999012100002 19990121 00002 NM 1999 1 21 CA980928023 1 19980826 A 2440 B429 CONTACTOR HARTMAN B429 BOEING 767 767275 NM PWA JT9 JT9D7R4D 52054 NE E/E BAY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P709699 (CAN) ON BOARDING, ELECTRICAL SMELL DETECTED, ELECTRICAL COMPARTMENT DOOR OPENED, FOUND AREA COVERED WITH SMOKE, A/C DEP LANED. GALLEY AND UTILITY BUSSES TRIPPED OFF-LINE, EXTERNAL POWER TRIPPED OFF-LINE. FOUND EXTERNAL POWER CONTACTOR K11 4 BLOWN, SMOKE AT P34 PANEL. REPLACED K114 CONTACTOR, WIRING, BUS POWER UNIT CONTINUITY CHECK CARRIED OUT. SYSTEM SERV ICEABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999012200015 19990122 00015 EU 1999 1 22 9811223227 1 19980915 A 3350 100865 POWER SUPPLY AIRBUS 320 A320211 3930320 EU CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 327NW 297 DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT SEAT ROWS 5, 9-13, 17, 18, AND 22-24 INOPERATIVE. REPLACED POWER SUPPLY UN IT. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999012200016 19990122 00016 NM 1999 1 22 9811235506 1 19980921 A 3350 6012113RF POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 506US 23195 FIRST CLASS EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY WITH A SERVICEABLE UNIT. 2 L 7 2 4F RT A2NM 1999012200017 19990122 00017 NM 1999 1 22 9811245508 1 19981009 A 3350 POWER SUPPLY BOEING 757 757251 1384970 NM CABIN INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 508US 23197 FORWARD FLOOR EMEERGENCY ESCAPE PATH LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY WITH A SERVICEABLE UNI T. 2 L 7 2 4F RT A2NM 1999012200018 19990122 00018 WP 1999 1 22 9811251161 1 19980922 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP ROW 32 INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 161US 46770 DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING FROM DOOR 3L AND 3R TO ROW 32 INOPERATIVE. REPLACED EMERGENCY L IGHT POWER SUPPLY AND CONTROL UNIT. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999012200019 19990122 00019 WP 1999 1 22 9811261161 1 19980930 A 3350 POWER SUPPLY DOUG DC10 DC1040 3023508 WP OVERWING INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 161US 46770 DURING LINE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT TEST. REPLACED OVERWING POWER SUPPLY. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999012200020 19990122 00020 WP 1999 1 22 9811271161 1 19980918 A 3350 BATTERY PACK DOUG DC10 DC1040 3023508 WP ROW 32 DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 161US 46770 DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE FROM DOOR 3L AND 3R TO ROW 32. REPLACED BATTERY PACK ABOV E DOOR 3L. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999012200021 19990122 00021 WP 1999 1 22 9811281151 1 19980815 A 3350 BATTERY PACK DOUG DC10 DC1040 3023508 WP CABIN DISCHARGED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 151US 46760 DURING LINE CHECK, ZONE 'C' EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 3 4F A22WE 1999012200022 19990122 00022 EU 1999 1 22 9811293224 1 19980921 A 3350 2013 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 324US 273 ON OVERNIGHT CHECK, APPROXIMATELY 50 PERCENT OF THE FLOOR PATH LIGHTING WAS INOPERATIVE. REPLACED BATTERY PACK. OPERAT IONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999012200023 19990122 00023 EU 1999 1 22 9811303226 1 19980913 A 3350 20131A BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 326US 282 NUMEROUS FLOOR ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999012200028 19990122 00028 EU 1999 1 22 QXEA9801990 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL1127, FRAME 8805, 10 LONG. REPAIRED IAW FOKKER SRM 51-40-4, PAGE P, N R 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200029 19990122 00029 EU 1999 1 22 QXEA9801991 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 8 AFT OF FRAME 8305, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200030 19990122 00030 EU 1999 1 22 QXEA9801992 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 7 AFT OF FRAME 8305, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, P AGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200031 19990122 00031 EU 1999 1 22 QXEA9801993 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK AROUND NUT PLATE HOLE, 5 AFT OF FRAME 8305. REPAIRED IAW FOKKER SRM 51- 10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200032 19990122 00032 EU 1999 1 22 QXEA9801994 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL600R, 5 AFT OF FRAME 8305, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200033 19990122 00033 EU 1999 1 22 QXEA9801995 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION IN CENTER OF SEAT TRACK BL 600R STARTING AT FRAME 7805, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 , NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200034 19990122 00034 EU 1999 1 22 QXEA9801996 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION IN CENTER OF SEAT TRACK BL 600R AT FRAME 7805, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, P ARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200035 19990122 00035 EU 1999 1 22 QXEA9801997 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R FORWARD OF FRAME 7805, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 , PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200036 19990122 00036 EU 1999 1 22 QXEA9801998 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL600R, 5 AFT OF FRAME 7805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200037 19990122 00037 EU 1999 1 22 QXEA9801999 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805-8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, FRAME 7805 AND 8305. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9. N R 4, PARAGRAPHS B AND C. 2 L 7 2 4F RT A20EU 1999012200038 19990122 00038 EU 1999 1 22 QXEA9802000 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 11 AFT OF FRAME 7305, 8 LONG. REPAIRED IAW SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200039 19990122 00039 EU 1999 1 22 QXEA9802001 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 1 AFT OF FRAME 7305, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, P AGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200040 19990122 00040 EU 1999 1 22 QXEA9802002 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL600R, 16.5 AFT OF FRAME 6805, 12.5 LONG. REPAIRED IAW FOKKER SRM 51-1 0-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200041 19990122 00041 EU 1999 1 22 QXEA9802003 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 16 AFT OF FRAME 6805, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4 , PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200042 19990122 00042 EU 1999 1 22 QXEA9802004 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 14 AFT OF FRAME 6805, 2 LONG. REPAIRED IAW FOKKER SRM 51-10-4 , PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200043 19990122 00043 EU 1999 1 22 QXEA9802005 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R, 14 AFT OF FRAME 6805, 2 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200044 19990122 00044 EU 1999 1 22 QXEA9802006 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R, 10 AFT OF FRAME 6805, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200045 19990122 00045 EU 1999 1 22 QXEA9802007 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R STARTING AT FRAME 6805, 9 LONG. REPAIRED IAW FOKKER SRM 51-10-4 , PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200046 19990122 00046 EU 1999 1 22 QXEA9802008 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 5 AFT OF FRAME 6805, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200047 19990122 00047 EU 1999 1 22 QXEA9802009 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600R, 2 AFT OF FRAME 6805, 2 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200048 19990122 00048 EU 1999 1 22 QXEA9802010 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE AROUND NUT PLATE AT SEAT TRACK BL 600A, FRAME 6805. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200049 19990122 00049 EU 1999 1 22 QXEA9802011 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 1127R STARTING AT FRAME 8305, 8.5 LONG. REPAIRED IAW FOKKER SRM 51- 10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200050 19990122 00050 EU 1999 1 22 QXEA9802012 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 8305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 1127R STARTING AT FRAME 8305, 8.5 LONG. REPAIRED IAW FOKKER SRM 51-1 0-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200051 19990122 00051 EU 1999 1 22 QXEA9802013 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 1127R, 1 AFT OF FRAME 7805, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4 , PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200052 19990122 00052 EU 1999 1 22 QXEA9802014 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600R STARTING 13 AFT OF FRAME 7305 AND CONTINUING PAST FRAME 7805, TO TAL LENGTH 16.5. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200060 19990122 00060 CE 1999 1 22 99ZZZX260 1 19981130 A 2731 55657561 TRIM WHEEL CESSNA 500 560CESSNA 2076750 CE COCKPIT MALFUNCTIONED A DXTA O OTHER F FLT CONT AFFECTED CL CLIMB 1 GL 07 375QS 1477 5600375 AFTER LIFT OFF, CREW WAS UNABLE TO TRIM AIRCRAFT (PITCH). CREW ELECTED TO RETURN TO MAINTENANCE FACILITY. INSPECTION F OUND TRIM WHEEL LOOSE ON SHAFT. FOLLOWER JUMPED A TRACK IN THE TRIM WHEEL. THIS CAUSED TRIM WHEEL TO BE THE LIMITING S TOP MECHANISM. RECOMMENDED (NOTE) IN MM "REPLACE SELF-LOCKING SCREWS ANYTIME THEY ARE REMOVED, OR APPLY LOCKTITE THREAD LOCKER' DURING RE-INSTALLATION. 2 L 7 2 4F RT A22CE 1999012200067 19990122 00067 CE 1999 1 22 99ZZZX267 1 19980111 A 5220 CREW DOOR NATIONALAIR MTSBSI MU2 MU2B35 5780411 CE COCKPIT SEPARATED A L HMNA A UNSCHED LANDING D INFLIGHT SEPARATION CL CLIMB 1 SW 15 799MA 22 612 CREW HATCH/EMERGENCY ESCAPE DOOR DEPARTED THE AIRCRAFT DURING CLIMB. 1 H 7 2 3T RT A10SW 1999012200069 19990122 00069 SO 1999 1 22 99ZZZX269 2 19980911 A 8520 629340 BOLT CESSNA 210 T210N 2073456 CE CONT O520 TSIO520R 17040 SO CONNECTING ROD FAILED A P C13A O OTHER O OTHER CR CRUISE 1 CE 05 9535Y 672 21064540 19873072H HEAD SEPARATED FROM ROD BOLT. SUBMITTER STATED CONTINENTAL ALSO ALLOWED RE-USE. CRUISE FLIGHT FAILURE. SUBMITTER SUGG ESTED CONTINENTAL SPECIFY MANDATORY ROD BOLT REPLACEMENT WITH NEW AT OVERHAUL. 1 H 7 1 3O 3 O 3A21 E8CE 1999012200080 19990122 00080 SO 1999 1 22 99ZZZX279 2 19981204 A 8530 25485 CYLINDER CESSNA 340 340CESSNA 2076404 CE CONT O520 TSIO520N 17040 SO RT ENGINE CRACKED A BCFA A UNSCHED LANDING E VIBRATION/BUFFET NR NOT REPORTED 1 EA 03 69457 702 3400309 228143R DURING FLIGHT, A VIBRATION WAS NOTED. THE PLANE LANDED. THE RIGHT ENGINE SHOWED ZERO COMPRESSION ON NR 4 CYLINDER. AF TER REMOVING CYLINDER, FOUND CRACK FROM EXHAUST TO SPARK PLUG. 1 L 7 2 3O 3 O 3A25 E8CE 1999012200104 19990122 00104 CE 1999 1 22 99ZZZX303 1 19981112 A 3230 6046H39A RELAY BEECH 18 C45H 1151018 CE MLG FAILED A STZA O OTHER J WARNING INDICATION AP APPROACH 1 AL 03 400WA AF764 ON APPROACH FOR LANDING, PILOT SELECTED LANDING GEAR DOWN, BUT THE GEAR REMAINED IN THE UP POSITION. PILOT ALSO REPORTE D A SMELL LIKE 'ELECTRICAL SMOKE'. MAINTENANCE PERSONNEL PUT ACFT ON JACKS AND PERFORMED A RETRACTION TEST, AND THE GEA R RETRACTED NORMALLY. HOWEVER, WHEN THE GEAR DOWN POSITION WAS SELECTED, THE GEAR FAILED TO EXTEND. THE LANDING GEAR D YNAMIC BRAKE RELAY WAS REPLACED, AND THE SYSTEM FUNCTIONED NORMALLY. OLD RELAY SHOWED NO EXTERNAL SIGNS OF DAMAGE, AND NO C/B'S TRIPPED DURING MALFUNCTION. INTERNAL INVEST OF RELAY FOUND CONTACT POINTS PITTED AND SIGNS OF ARCING. SUBMITT ER SUGGESTED THE CONTACT POINTS BE INSPECTED ON A 5-YEAR BASIS. 1 L 7 2 3R A765 1999012200105 19990122 00105 CE 1999 1 22 99ZZZX304 1 19981130 A 5610 531126110 WINDOW CESSNA 340 340A 2076405 CE COCKPIT FAILED A MAHA O OTHER O OTHER CR CRUISE 1 NM 03 999DC 2741 340A0035 AT CRUISE 12,500 FEET, CABIN ALTITUDE 3,000 FEET (WX. C.A.V.U.). COPILOT WINDOW FAILED. CAUSE UNKNOWN. ORIGINAL WINDO W PER DATE. FAILURE OCCURRED 11-30-98 AT APPROXIMATELY 1500 HRS (LOCAL). 1 L 7 2 3O 3A25 1999012200111 19990122 00111 SW 1999 1 22 99ZZZX310 1 19981215 A 3230 2781009015 POWER PACK SWRNGN SA226 SA226TC 8780404 SW LT MLG WW FAILED A GXPA K NONE O OTHER IN INSP/MAINT 1 GL 23 165GA 588 TC396 MAIN LANDING GEAR WILL NOT RETRACT. TROUBLESHOT SYSTEM, FOUND DEFECTS. IAW FAIRCHILD MM, THE POWER PACK WAS REMOVED AN D REPLACED WITH NO FURTHER DEFECT NOTED. 2 L 7 2 4T RT A8SW 1999012200122 19990122 00122 NM 1999 1 22 TWAA9901008 1 19981030 A 5330 SKIN BOEING 767 767231 1385131 NM BS 1269 CORRODED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 602TW 22565 DURING OP 15 MAINT CHECK, FOUND STA 1269, STRINGER 39R WITH CORROSION BETWEEN INBD SIDE OF STRINGER AND FUSELAGE SKIN, A ND STRINGER 39L CORRODED BETWEEN STRINGER AND SKIN AT STA 1264. CUT OUT SKIN AND INSTALLED EXTERNAL DOUBLER REPAIR PER ARA 15766 AND SRM 53-00-01, FIG 201. 2 L 7 2 4F RT A1NM 1999012200140 19990122 00140 NM 1999 1 22 9811312715 1 19981026 A 3350 6013211 BATTERY PACK BOEING 727 7272S7 138407Z NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 719RC 22490 FIRST CLASS FLOOR EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE. REPLACED BATTEY PACK AND POWER SUPPLY. OPERATIONAL CHECK O K. 2 L 7 3 4F A3WE 1999012200141 19990122 00141 NM 1999 1 22 9811322715 1 19981025 A 3397 WIRE BOEING 727 7272S7 138407Z NM CABIN FAILED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 719RC 22490 FORWARD FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED SPLICE. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999012200142 19990122 00142 EU 1999 1 22 9811333204 1 19980807 A 3350 BATTERY PACK AIRBUS 320 A320211 3930320 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 304US 40 MID CABIN AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999012200143 19990122 00143 NM 1999 1 22 9811342706 1 19981022 A 3350 6104789 BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 815EA 22552 EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM ROWS 6-15 AND 24 TO END OF CABIN. REPLACED BATTERY PACKS AT STA 752 LEFT AND STA 1048 RIGHT. EMERGENCY LIGHTING TESTED OK. 2 L 7 3 4F A3WE 1999012200144 19990122 00144 EU 1999 1 22 9811353205 1 19980801 A 3350 BATTERY PACK AIRBUS 320 A320212 EU CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 350NA 418 EMERGENCY LIGHTS INOPERATIVE DURING SYSTEM TEST. REPLACED BATTERY PACK. OPERATIONAL CHECK OK. 2 L 7 2 4F RT A28NM 1999012200145 19990122 00145 NM 1999 1 22 9811362287 1 19980910 A 3350 BATTERY PACK BOEING 727 727251 138408H NM CABIN DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 287US 21375 FLOOR PROXIMITY LIGHTING IN AFT CABIN INOPERATIVE. REPLACED BATTERY PACK IN POWER SUPPLY. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999012200146 19990122 00146 NM 1999 1 22 9811372289 1 19980829 A 3350 BATTERIES BOEING 727 727251 138408H NM DOOR 1L & 1R DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 289US 21337 FLOOR EMERGENCY LIGHTS INOPERATIVE IN FIRST CLASS SECTION AND AT DOOORS 1L AND 1R. REPLACED BATTERIES AND POWER SUPPLY. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999012200147 19990122 00147 NM 1999 1 22 9811382296 1 19980919 A 3350 RELAY BOEING 727 727251 138408H NM CABIN INOPERATIVE A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 296US 21788 FOUND PATH LIGHTING INOPERATIVE ON LINE CHECK. REPLACED CHARGING RELAY, SWITCHING RELAY, AND TWO BATTERY PACKS. OPERAT IONAL CHECK OK. 2 L 7 3 4F A3WE 1999012200150 19990122 00150 WP 1999 1 22 9811399156 1 19981027 A 5312 BULKHEAD DOUG DC9 DC914 3022034 WP BS 642 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 8915E 45832 DURING M CHECK, FOUND CORROSION ON LOWER LEG OF BULKHEAD T CAP AT FS 642, STR 28R-29R, AROUND FASTENER. REPAIRED PER EA 91-159460. 2 L 7 2 4F A6WE 1999012200151 19990122 00151 WP 1999 1 22 9811409970 1 19980827 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 612-639 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 9334 47247 DURING M CHECK, FOUND CORROSION ON FORWARD KEEL AREA SECTION OF CENTER VERTICAL WEB FS 612-639. REPAIRED PER EA 99-1593 49. 2 L 7 2 4F A6WE 1999012200152 19990122 00152 WP 1999 1 22 9811419926 1 19981120 A 5511 SPAR CAP DOUG DC9 DC932 3022066 WP RT HORIZ STAB CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 926NW 47425 DURING M CHECK, FOUND CRACK ON RIGHT HORIZONTAL STABILIZER XRS 223 UPPER AFT SPAR OUTBOARD END. REPAIRED PER EA 99-1594 70. 2 L 7 2 4F A6WE 1999012200153 19990122 00153 WP 1999 1 22 9811429916 1 19981120 A 5312 BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 47 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 949N 47566 DURING M CHECK, FOUND T ANGLE CRACKED ON BULKHEAD FS 47 NEAR CENTER LINE. REPAIRED PER EA 99-159528. 2 L 7 2 4F A6WE 1999012200170 19990122 00170 WP 1999 1 22 UPS99828342 1 19981228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 660 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C LT WING L/E UPPER RIB CRACKED AT XFS660. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200171 19990122 00171 WP 1999 1 22 UPS99828343 1 19981228 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 74 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C LT WING UPPER SKIN AT XRS 74 AT STR 8 IS CRACKED AT A FASTENER HOLE. CUT OUT DAMAGED AREA AND REPAIRE D SKIN IAW SRM 57-2-1 FIG 10. 2 L 7 4 4F RT 4A25 1999012200172 19990122 00172 WP 1999 1 22 UPS99828344 1 19981229 A 5751 SKIN DOUG DC8 DC871F 302199D WP RT AILERON CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C RT INBD AILERON UPPER L/E SKIN AT THE MANUAL REVERSION MECH IS CRACKED. CUT OUT DAMAGED SKIN AND SPLI CED IN NEW SECTION IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012200173 19990122 00173 WP 1999 1 22 UPS99828345 1 19981229 A 5320 36431121N FITTING DOUG DC8 DC871F 302199D WP BS 780 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C FLOORBEAM TO CENTER TANK ATTACH ANGLE AT FS 780, LBL 55 HAS HEAVY CORROSION. REMOVED AND REPLACED FIT TING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200174 19990122 00174 WP 1999 1 22 UPS99828346 1 19981229 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 770 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C HEAVY CORROSION ON SEAT TRACK LOR FLANGE AT FS 770 AT LBL 25. REMOVED DAMAGED SECTION OF SEAT TRACK, FS 650-875 LBL 25, PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200175 19990122 00175 WP 1999 1 22 UPS99828347 1 19981230 A 5320 37501591N FITTING DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C LONGERON 27R SPLICE FITTING AT FS 1050 IS CRACKED. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW S RM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200176 19990122 00176 WP 1999 1 22 UPS99828348 1 19981230 A 5320 37585701N FITTING DOUG DC8 DC871F 302199D WP BS 1150 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C INTERCOSTAL FITTING AT FS 1150 AND LONGERON 35R IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1 -20D. 2 L 7 4 4F RT 4A25 1999012200177 19990122 00177 WP 1999 1 22 UPS99828349 1 19981230 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1060-1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C SEAT TRACK AT FS 1060-1080 AT RBL 60 HAS HEAVY CORROSION. REMOVED AND REPLACED SEAT TRACK FROM FS 103 0 TO 1110, RBL 60 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200178 19990122 00178 WP 1999 1 22 UPS99828350 1 19981230 A 5320 37558421N FITTING DOUG DC8 DC871F 302199D WP BS 1180 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C FS 1180, LONGERON 29L BATHTUB FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-1- 20D. 2 L 7 4 4F RT 4A25 1999012200179 19990122 00179 WP 1999 1 22 UPS99828351 1 19981230 A 5320 4758514507 FITTING DOUG DC8 DC871F 302199D WP BS 1240 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C INTERCOSTAL END FITTING CRACKED FS 1240 AT LONGERON 33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 D. 2 L 7 4 4F RT 4A25 1999012200180 19990122 00180 WP 1999 1 22 UPS99828352 1 19981230 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C SEAT TRACK AT FS 1500 AT LBL 50 HAS HEAVY CORROSION. CUT OUT DAMAGED SEAT TRACK FROM FS 1270 TO 1520, LBL 50 AND SPLICED IN A NEW SECTION IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200181 19990122 00181 WP 1999 1 22 UPS99828353 1 19981231 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1370 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C SEAT TRACK AT FS 1370, AT BL 0 HAS CORROSION OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK FROM FS 1370 T O 1530 AT BL 0 AND SPLICED IN A NEW SECTION OF TRACK IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200183 19990122 00183 WP 1999 1 22 UPS99828355 1 19981230 A 5347 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1060 SPLIT A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE:C SEAT TRACK SPLIT AND CORRODED AT FS 1060, LBL 60. REMOVED DAMAGED SEAT TRACK FROM FS 1000-1300, LBL 6 0 IAW SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200197 19990122 00197 WP 1999 1 22 UPS99828371 1 19981231 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 LT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 1999012200198 19990122 00198 WP 1999 1 22 UPS99828372 1 19981231 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 RT WING L/E, LWR SKIN AT XFS 597.5 IS CRACKED JUST FWD OF THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-57 20-7767-A. 2 L 7 4 4F RT 4A25 1999012200224 19990122 00224 WP 1999 1 22 UPS99828400 1 19981231 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 258 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E SKIN AT XRS 258 IS CRACKED IN 2 PLACES. CUT OUT DAMAGED AND REPAIRED IAW EO DC8-7520-77 67-A. 2 L 7 4 4F RT 4A25 1999012200252 19990122 00252 NM 1999 1 22 DL72K990058 1 19981216 A 5753 652163262 SKIN BOEING 727 727232 1384082 NM RT TE FLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 COVE SKIN DAMAGED 60 FROM O/B END OF FLAP, REPAIRED PER M/M 57-52-0 PAGE 809 FIG 7. 2 L 7 3 4F A3WE 1999012200253 19990122 00253 NM 1999 1 22 DL72K990059 1 19981210 A 5753 652163262 SPAR BOEING 727 727232 1384082 NM RT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 AFT SPAR RAIL CRACKED 19 FROM I/B END, REPAIRED PER MM 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1999012200258 19990122 00258 NM 1999 1 22 DL72K990067 1 19981211 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 525DA 21585 AFT LWR SPAR RAIL CRACKED 40 FROM O/B END. REPAIRED PER M/M 57-52-0 FIG 802. 2 L 7 3 4F A3WE 1999012200259 19990122 00259 NM 1999 1 22 DL72W990068 1 19981216 A 5320 ANGLE BOEING 727 727247 138408F NM FUSELAGE CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 2807W 20579 CORROSION ON SECONDARY HEAT EXCHANGER CLOSE OUT PANEL ATTACH ANGLE LT SIDE I/B ANGLE. INSTALLED REPAIR PER MM 53-30-1. 2 L 7 3 4F A3WE 1999012200266 19990122 00266 NM 1999 1 22 DHL99705001 1 19980116 A 2782 1U109512 ACTUATOR BOEING 727 72722C 138400F NM NR 1 LE SLAT MALFUNCTIONED A DHLA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SO 01 705DH 19191 NR 1 SLAT WOULD NOT RETRACT AFTER TAKEOFF. ACCOMPLISHED ABNORMAL PROCEDURE, NO EFFECT. REMOVED AND REPLACED SLAT ACTUA TOR PER MM 27-81-32. INDICATION NORMAL. 2 L 7 3 4F A3WE 1999012200267 19990122 00267 WP 1999 1 22 DHL99803002 1 19980112 A 2760 57193315001B VALVE DOUG DC8 DC873F 302199F WP LT SPOILER FAILED A DHLA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SO 01 803DH 46123 ON CLIMB-OUT ABOVE 6000 FT AND AT OR ABOVE 230 KTS, FELT EXCESSIVE VIBRATION THOUGH OUT AIRFRAME. REMOVED AND REPLACED LATERAL CONTROL SPOILER POWER CYLINDER AND CONTROL VALVE (LEFT WING). OPS AND LEAK CHECKED PER MM 27-62-9. 2 L 7 4 4F RT 4A25 1999012200268 19990122 00268 1999 1 22 CA980922016 4 19980911 A 2210 ACTUATOR DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA HAMSTD 24PF 24PF305 GL YAW DAMPER MALFUNCTIONED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 30499 (CAN) AIRCRAFT EXPERIENCED RUDDER OSCILLATION AT 12,000 FEET. OSCILLATION STOPPED DURING DESCENT AT 165 KNOTS. PROBLEM TRACED TO YAW DAMPER SYSTEM. YAW DAMPER ACTUATOR SECONDARY COIL FOUND OPEN IN LVDT UNIT THAT IS INTEGRAL TO ACTUATOR. PART TC: 43,122. 2 H 7 4 4T 4 T A20EA E4EA 6 C P1NE 1999012200272 19990122 00272 NM 1999 1 22 CA981125012 1 19980925 A 3230 856916 LINE BOEING 747 7474F6 NM MLG LEAKING W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 431 (CAN) AIR TURN BACK DUE LANDING GEAR TILT AND MONITOR MESSAGES ON TAKEOFF. REPLACED PSEU PER FIM TROUBLESHOOTING PROCED URE. SECOND TAKEOFF SAME PROBLEM RECURRED. FOUND HYDRAULIC LEAK ON TILT ACTUATOR HOSE. PROXIMITY SENSOR SWITCHES CHEC KED, RESISTANCE ALL NORMAL. THIRD TAKEOFF SAME PROBLEM. AIRCRAFT GROUNDED. PSEU REPLACED. ALL SYSTEMS NOW NORMAL. A IRCRAFT RETURNED TO SERVICE. 2 L 7 4 4F RT A20WE 1999012200273 19990122 00273 NM 1999 1 22 CA981125013 1 19980925 A 2133 79275515 OUTFLOW VALVE BOEING 767 767375 NM CABIN PRESSURE FAILED W A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CA 12446 1113 (CAN) ON TAKEOFF, EICAS MESSAGE R PRV. REPLACED PRESSURE REGULATING VALVE. PART TC: 1,618. 2 L 7 2 4F RT A1NM 1999012200274 19990122 00274 NM 1999 1 22 CA981125014 1 19980925 A 3320 342568 LIGHT BOEING 767 767375 NM GALLEY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) FLIGHT DIVERTED DUE TO SMOKE EMITTING FROM SPOT LIGHT IN FORWARD GALLEY. REPLACED LIGHT ASSY AND TRANSFORMER. 2 L 7 2 4F RT A1NM 1999012200275 19990122 00275 NM 1999 1 22 CA981125015 1 19981009 A 2910 72909 REGULATOR BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE A-HYD SYSTEM FAILED W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 37446 17002 164 702736 (CAN) LOSS OF A-SYSTEM HYDRAULIC PRESSURE NOTED. SUSPECT PRESSURE REGULATING VALVE FOR RESERVOIR HEAD PRESSURE. REPLAC ED VALVE. 2 L 7 2 4F 4 F A16WE E2EA 1999012200276 19990122 00276 NM 1999 1 22 CA981125016 1 19981009 A 3260 6552811113 ACCESSORY UNIT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE E/E BAY FAILED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 46683 M00493 707349 (CAN) WHEN GEAR EXTENDED, HAD BOTH RED AND GREEN INDICATION WHEN GEAR DOWN AND LOCKED. REPLACED LANDING GEAR ACCESSORY MODULE. 2 L 7 2 4F 4 F A16WE E2EA 1999012200277 19990122 00277 NM 1999 1 22 CA981125017 1 19981013 A 3610 69379317 DUCT BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE PNEUMATIC SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CA 674240 (CAN) AIRCRAFT RETURNED TO BLOCKS DUE TO WING BODY OVERHEAT INDICATION FLICKERING. FOUND ELEMENT IN SECT 56, M275 LOW R ESISTANCE. FOUND LEAKING DUCT IN SECT 56. REPLACED DUCT AND ELEMENT. 2 L 7 2 4F 4 F A16WE E2EA 1999012200278 19990122 00278 NM 1999 1 22 CA981125020 1 19981024 A 7830 1U1225 VALVE BOEING 737 737296 1384486 NM PWA JT8 JT8D9A 52048 NE THRUST REVERSER MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 CA 32695 19734 1906 707412 (CAN) RETURN TO GATE DUE THRUST REVERSER ISOLATION VALVE LIGHT ON AT ROTATION. VALVE REPLACED. 2 L 7 2 4F 4 F RT A16WE E2EA 1999012200279 19990122 00279 1999 1 22 CA981125021 4 19981027 A 3454 5224280101 RECEIVER BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE VHF NAVIGATOR FAILED W L ABORTED APPROACH O OTHER AP APPROACH 1 CA 39821 14464 709479 (CAN) MISSED APPROACH DUE CAPTAIN'S GLIDE SLOPE READING TOO HIGH. SECOND APPROACH OK. REPLACED VHF NAVIGATOR RECEIVER. 2 L 7 2 4F 4 F A16WE E2EA 1999012200280 19990122 00280 NM 1999 1 22 CA981125023 1 19981102 A 3040 2312F CONTROLLER BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE WINDSHIELD HEAT FAILED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA 44371 1126 709378 (CAN) AIR TURN BACK DUE LT WINDSHIELD OVERHEAT LIGHT ON CLIMB-OUT. REPLACED LT FORWARD HEAT CONTROLLER. 2 L 7 2 4F 4 F A16WE E2EA 1999012200281 19990122 00281 NM 1999 1 22 CA981125024 1 19981116 A 3260 189915 SENSOR BOEING 737 7372T5 NM PWA JT8 JT8D17 52049 NE RT MLG MALFUNCTIONED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 702723 (CAN) AT TOP OF DESCENT, RT RED GEAR WARNING LIGHT FLICKERED WITH GEAR SELECTED UP. REPLACED RT MLG UPLOCK SENSOR. 2 L 7 2 4F 4 F RT A16WE E2EA 1999012200282 19990122 00282 SW 1999 1 22 CA981125029 1 19980715 A 6400 206010777001 BUMPER BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR CUT W K NONE O OTHER IN INSP/MAINT 1 CA 150 CAE820743 (CAN) TAIL ROTOR BUMPER CUT THROUGH AT THE TAIL ROTOR FLAP STOP CONTACT AREA. 1 G 7 1 3U 3 U H2SW E4CE 1999012200283 19990122 00283 SW 1999 1 22 CA981125031 1 19980709 A 6310 NAS130516 BOLT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TRANSMISSION LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA CAE802078BA (CAN) BOLT FOUND LOOSE ON ONE OF THE TRANSMISSION DECK FITTINGS. BOLT WAS TOO LONG FOR INSTALLATION. 1 G 7 1 3U 3 U H2SW E4CE 1999012200284 19990122 00284 SW 1999 1 22 CA981125036 1 19980826 A 2435 MS24171D1 RELAY BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL STARTER FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA CAE822231 (CAN) STARTER REMAINED ENGAGED WHEN ENGINE SHUT DOWN. HAD TO TURN BATTERY SWITCH OFF TO GET STARTER TO STOP. 1 G 7 1 3U 3 U H2SW E4CE 1999012200285 19990122 00285 SW 1999 1 22 CA981125038 1 19980825 A 3040 2060704753 MOTOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL WINDSHIELD DEFOG FAILED W O OTHER O OTHER TO TAKEOFF 1 CA 341 525 CAE801518BA (CAN) DEFOG MOTOR FAILED ON TAKEOFF. 1 G 7 1 3U 3 U H2SW E4CE 1999012200286 19990122 00286 EU 1999 1 22 CA981125039 1 19980806 A 2842 647510032 TRANSMITTER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUEL SYSTEM MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA 163 835 (CAN) LOW LEVEL FUEL LIGHT COMES ON, 22 PERCENT INDICATED. 58 LITRES ACTUAL. 1 G 7 1 3U 3 U H9EU E19EU 1999012200287 19990122 00287 SW 1999 1 22 CA981125040 1 19980819 A 6230 ACRO0363 BEARING 206010450113 BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR OVERHEATED W K NONE O OTHER IN INSP/MAINT 1 CA 29 ACRO0363 CAE820800 (CAN) DUPLEX BEARING RUNNING HOT, SPUES VERY BLACK GREASE. 1 G 7 1 3U 3 U H2SW E4CE 1999012200289 19990122 00289 SW 1999 1 22 CA981125042 1 19980919 A 3340 BULB BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL LANDING LIGHT FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA CAE820758 (CAN) LANDING LIGHT NOT OPERATING ACCORDING TO PILOT. BROKEN WIRE FOUND AT BULB. ALSO, SOME WIRES FOUND BROKEN AT THE GOVERNOR RPM SWITCH. 1 G 7 1 3U 3 U H2SW E4CE 1999012200290 19990122 00290 SW 1999 1 22 CA981125043 1 19980831 A 6230 206010450113 SWASHPLATE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL MAIN ROTOR OUT OF ADJUST W K NONE O OTHER IN INSP/MAINT 1 CA 12473 8 JIJG07278 CAE820800 (CAN) PILOT NOTED THAT HYDRAULIC OFF OPERATION WAS STIFF. SWASHPLATE FRICTION REQUIRED ADJUSTMENT. NO DAMAGE FOUND. 1 G 7 1 3U 3 U H2SW E4CE 1999012200291 19990122 00291 SW 1999 1 22 CA981125044 1 19980923 A 6730 206076031013 SERVO BELL 206 206B 1181511 SW ALLSN 250C 250C20B 03013 GL FLIGHT CONTROL FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 2 1271 CAE831866 (CAN) AFTER SERVO INSTALLATION, THE TEST FLIGHT REVEALED CONTROL FEEDBACK. SERVO REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999012200292 19990122 00292 SW 1999 1 22 CA981125046 1 19980825 A 6510 206040330003 SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TAIL ROTOR SCORED W K NONE O OTHER IN INSP/MAINT 1 CA 82241 CAE820758 (CAN) DURING INSPECTION OF TAILROTOR DRIVE, THE SHORT SHAFT UNDER THE OIL COOLER WAS FOUND SCORED. 1 G 7 1 3U 3 U H2SW E4CE 1999012200293 19990122 00293 SW 1999 1 22 CA981125047 1 19981014 A 6510 NUT BELL 206 206L 1181522 SW ALLSN 250C 250C20B 03013 GL TAIL ROTOR MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 830805 (CAN) ON 200-HOUR INSPECTION, FOUND ONE OF THE TAIL ROTOR DRIVESHAFT HANGERS WITHOUT A NUT OR COTTER PIN. 1 G 7 1 3U 3 U H2SW E4CE 1999012200294 19990122 00294 EU 1999 1 22 CA981125048 1 19981021 A 6720 704A34130058 CONTROL CABLE SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE TAIL ROTOR MISROUTED W K NONE O OTHER IN INSP/MAINT 1 CA 4432 (CAN) TAIL ROTOR CONTROL CABLE FOUND INSTALLED THROUGH THE WRONG HOLE OF THE AIRFRAME CAUSING BINDING OF THE TAIL ROTOR CONTROLS. 1 G 7 1 3U 3 U NC H9EU E19EU 1999012200295 19990122 00295 SW 1999 1 22 CA981125050 1 19981008 A 7720 50293003 INDICATOR BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL COCKPIT READS LOW W K NONE O OTHER IN INSP/MAINT 1 CA 104 142R CAE800471BA (CAN) TOT GAUGE READING 12 TO 14 DEGREES LOW. GAUGE REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999012200299 19990122 00299 EU 1999 1 22 CA981125069 1 19981103 A 3210 5321012174 PIN 5321012043 PILATS PC12 PC12 7090550 EU MLG CORRODED W O OTHER O OTHER NR NOT REPORTED 1 CA 1340 IL111 (CAN) LEFT AXIS PIN FOUND CORRODED. THIS, IN TURN, HAD CAUSED THE 'AN' BOLT WHICH HOLDS THE PIN INTO THE GEAR TO SHEAR AND CAUSED THE PROXIMITY SWITCH TO BE OUT OF ALIGNMENT CAUSING SEVERAL SYSTEMS NOT TO WORK. PART TC: 1,266. 1 L 7 1 3T RT A78EU 1999012200300 19990122 00300 WP 1999 1 22 CA981125086 1 19980920 A 5620 1506102101 WINDOW 1506100101 LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE ROW 38 K CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10224 (CAN) ON WALKAROUND, FOUND PASSENGER WINDOW AT 38K CRACKED, REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999012200301 19990122 00301 WP 1999 1 22 CA981125087 1 19980926 A 3020 LK44310 TUBE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENGINE DAMAGED W O OTHER E VIBRATION/BUFFET CR CRUISE 1 CA 10066 (CAN) IN CRUISE, NR 3 ENGINE APPROACHING VIBRATION LIMITS, THRUST WAS REDUCED AS PRECAUTION. FOUND SPINNER AND ANTI-ICI NG TUBE DAMAGED, REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999012200303 19990122 00303 WP 1999 1 22 CA981125089 1 19981014 A 2120 1514813113 DUCT LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE E/E BAY CRACKED W H DEACTIVATE SYST/CIRCUITS O OTHER CR CRUISE 1 CA 10256 (CAN) BAD NOISE COMING FROM E BAY, FOUND AVIONIC EXHAUST DUCT BADLY CRACKED CAUSING PARTIAL LOSS OF PRESSURIZATION. DUC T AND HOLDING CLAMP REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999012200304 19990122 00304 WP 1999 1 22 CA981125090 1 19981027 A 2750 1530076131 LINK LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B02 54555 NE TE FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10256 (CAN) ON INSPECTION, FOUND GREASE COMING OUT OF CRACK IN NR 2 OUTBOARD AFT FLAP SWING JOINT. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999012200305 19990122 00305 WP 1999 1 22 CA981125091 1 19981116 A 3260 BULB LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE NLG INDICATOR FAILED W O OTHER O OTHER AP APPROACH 1 CA 10510 (CAN) AFTER LANDING GEAR EXTENSION, NOSE LANDING GEAR GREEN LIGHT DID NOT COME ON AND DID NOT TEST. AFTER LANDING, FOUN D BOTH BULBS BURNT, REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999012200306 19990122 00306 EU 1999 1 22 CA981125094 1 19981116 A 6510 10531547 SHAFT BOLKMS 105 BO105C 5626005 EU ALLSN 250C 250C20B 03013 GL TAIL ROTOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA CAE835628 (CAN) FORWARD SHORT DRIVE SHAFT HAD PLAY IN THE COUPLING AT THE RIVETED END. 1 G 7 2 3U 3 U H3EU E4CE 1999012200307 19990122 00307 NM 1999 1 22 CA981130010 1 19981114 A 3610 DUCT BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE RIGHT LEAKING W O OTHER O OTHER LD LANDING 1 CA P707550 (CAN) DURING LANDING, LOUD BANG FROM LANDING GEAR AREA. RIGHT DUCT LEAK LIGHT AND MESSAGE ON SHORT FINAL. REPLACED PNE UMATIC DUCT DOWN STREAM OF RIGHT ISOLATION VALVE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999012200309 19990122 00309 WP 1999 1 22 CA981130013 1 19981109 A 2782 ACTUATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE SPOILER FAILED W O OTHER O OTHER AP APPROACH 1 CA P657261D (CAN) UNABLE TO ARM SPOILERS ON APPROACH, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT. REPLACED AUTO SPOILER ACTUATO R. 2 L 7 2 4F 4 F A6WE E2EA 1999012200320 19990122 00320 EA 1999 1 22 CA990111018 2 19981223 A 7240 3023774 LINER DHAV DHC6 DHC6100 EA PWA PT6 PT6A20 52043 EA NR 1 ENGINE FAILED W E ENGINE SHUTDOWN B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 4965 PCE20954 (CAN) DURING FLIGHT, NR 1 ENGINE SURGED AND A BANG WAS HEARD, BUT ALL ENGINE PARAMETERS WERE NORMAL. THE CABIN THEN FIL LED WITH SMOKE, BLEED AIR VALVES WERE CLOSED. THERE WERE TWO MORE SURGES AND BANGS WITH THE FUEL FLOW RISING. THE ENG WAS SHUTDOWN AND ACFT LANDED WITHOUT INCIDENT. POST-FLIGHT INVESTIGATION FOUND OIL DRIPPING FROM THE ENG. THE GAS GENE RATOR EXTREMELY STIFF AND A BURN MARK ON THE COMBUSTION CASING. THE ENG WAS SPLIT AND A LARGE HOLE WAS FOUND IN THE CO MBUSTION LINER AT THE 6 O'CLOCK POSITION ADJACENT TO THE BURN MARK ON THE EXTERNAL COMBUSTION CASE. THE ENG IS BEING SEN T FOR INVESTIGATION, FURTHER REPORT TO FOLLOW. PART TC: 7,650. 1 H 7 2 3T 3 T A9EA E4EA 1999012200345 19990122 00345 NE 1999 1 22 99ZZZX336 2 19981209 A 7260 B7670 CHIP COLLECTOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D1 52044 NE NR 4 ENGINE FAILED G A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 SO 11 983US 47282 CHIP COLLECTOR ON RIGHT ENGINE, NR 4 BEARING SCAVENGE LINE, CHIP COLLECTOR MAGNETIC PROBE EJECTED FROM CHIP COLLECTOR BO DY. ENGINE OIL DRAINED FROM ENGINE IN-FLIGHT. ANALYSIS DETERMINED THE INTERNAL CHECK VALVE OF CHIP COLLECTOR WAS STUCK IN THE OPEN POSITION DUE TO DEBRIS LODGED BETWEEN THE INTERNAL CHECK VALVE AND COLLECTOR'S INTERNAL BORE. 2 L 7 2 4F 4 F A6WE E2EA 1999012200375 19990122 00375 WP 1999 1 22 UPS99828407 1 19981227 A 5730 SKIN DOUG DC8 DC871F 302199D WP RT WING LE CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XFS 597.5 IS CRACKED 2 INCHES FWD OF THE SPAR. CUT OUT DAMAGED AREA AND RE PAIRED IAW DHC SK 701-160 AND SRM 57-2-1 FIG 38. 2 L 7 4 4F RT 4A25 1999012200376 19990122 00376 WP 1999 1 22 UPS99828408 1 19981228 A 5720 36412562 DOUBLER DOUG DC8 DC871F 302199D WP RT WING CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING L/E AT ACCESS PANEL 519B, THE INTERNAL DOUBLER HAS MODERATE EXFOLIATION CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641256 AND SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999012200377 19990122 00377 WP 1999 1 22 UPS99828409 1 19981228 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 597.5 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING L/E LWR SKIN AT XFS 597.5 IS CRACKED AT THE DRAIN HOLE. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087-B. 2 L 7 4 4F RT 4A25 1999012200378 19990122 00378 WP 1999 1 22 UPS99828410 1 19981229 A 5720 97532938 ANGLE DOUG DC8 DC871F 302199D WP WS 250.089 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING L/E INBOARD SIDE OF THE XS 250.089 RIB, THE VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED A ND REPLACED ANGLE IAW DWG 9753293 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200379 19990122 00379 WP 1999 1 22 UPS99828411 1 19981229 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 385.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING L/E RIB AT XFS 385.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200380 19990122 00380 WP 1999 1 22 UPS99828414 1 19981229 A 5320 36410042N FITTING DOUG DC8 DC871F 302199D WP BS 879 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, FS 879 FITTING ABOVE LONG 24R HAS MODERATE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FI G 8. 2 L 7 4 4F RT 4A25 1999012200381 19990122 00381 WP 1999 1 22 UPS99828416 1 19981229 A 5320 3779874502 FITTING DOUG DC8 DC871F 302199D WP BS 703 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, INTERCOSTAL FITTING CRACKED AT FS 703 AND LONG 19R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200382 19990122 00382 WP 1999 1 22 UPS99828418 1 19981230 A 5320 3755822505N FITTING DOUG DC8 DC871F 302199D WP BS 270 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, BATHTUB FITTING CRACKED AT FS 270 AND LONG 30L. REMOVED AND REPLACED FITTING IAW 51-1-20D AND 53-2-0 FIG 2D. 2 L 7 4 4F RT 4A25 1999012200383 19990122 00383 WP 1999 1 22 UPS99828419 1 19981230 A 5320 DC853B0097 FITTING DOUG DC8 DC871F 302199D WP BS 90 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, HEAVY CORROSION ON LONG 35R SPLICE FITTING AT FS 90. REMOVED AND REPLACED SPLICE FITTING IAW SRM 53- 2-2 FIG 10. 2 L 7 4 4F RT 4A25 1999012200384 19990122 00384 WP 1999 1 22 UPS99828420 1 19981230 A 5315 9754022504N FLOORBEAM DOUG DC8 DC871F 302199D WP BS 340 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, A PIT FLOORBEAM CRACKED AT FS 340 AND RBL 52. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-1-20D AND 51 -1-21. 2 L 7 4 4F RT 4A25 1999012200385 19990122 00385 WP 1999 1 22 UPS99828421 1 19981230 A 5320 37502571N FITTING DOUG DC8 DC871F 302199D WP BS 1050 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, LONG 31R SPLICE IS CRACKED AT FS 1050. REMOVED AND REPLACED SPLICE FITTING IAW SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012200388 19990122 00388 WP 1999 1 22 UPS99828425 1 19981227 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 399 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING UPPER SKIN AT STR 8 AND STA XW 399 HAS INTERGRANULAR CORROSION AND IS CRACKED. CUT OUT DAMAG ED AREA AND REPAIRED IAW SRM 57-2-1 FIG 32. 2 L 7 4 4F RT 4A25 1999012200389 19990122 00389 WP 1999 1 22 UPS99828426 1 19981229 A 5320 37739062 FITTING DOUG DC8 DC871F 302199D WP BS 815 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, FITTING AT FS 815 AND LBL 24 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999012200390 19990122 00390 WP 1999 1 22 UPS99828427 1 19981229 A 5320 37739062 FITTING DOUG DC8 DC871F 302199D WP BS 776 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, FITTING AT FS 776 AT RBL 24 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21. 2 L 7 4 4F RT 4A25 1999012200391 19990122 00391 WP 1999 1 22 UPS99828428 1 19981228 A 5712 RIB DOUG DC8 DC871F 302199D WP WS 630 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, LT WING L/E RIB AT XFS 630 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2. 2 L 7 4 4F RT 4A25 1999012200421 19990122 00421 WP 1999 1 22 DHL9980101C 1 19981011 A 2760 HARDWARE DOUG DC8 DC873F 302199F WP NR 5 SPOILER WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING T/E UPPER AREA NR 5 SPOILER PANEL PRESENTS PLAY AT ATTACH POINTS. REMOVED AND REPLACED WORN HARDWA RE PER MM 27-61-1. 2 L 7 4 4F RT 4A25 1999012200422 19990122 00422 WP 1999 1 22 DHL9980102C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 19 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING UPPER I/B AREA AT STA 19 FWD T/E PANEL DELAMINATED. REMOVED AND REPAIRED PANEL, INSTALLED PER SRM 51-1-24. 2 L 7 4 4F RT 4A25 1999012200423 19990122 00423 WP 1999 1 22 DHL9980103C 1 19981011 A 5752 TRIM TAB DOUG DC8 DC873F 302199F WP LT AILERON DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING INBOARD AILERON TRIM TAB PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER MM 27-31-0. 2 L 7 4 4F RT 4A25 1999012200424 19990122 00424 WP 1999 1 22 DHL9980104C 1 19981011 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 519 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C CHECK, LT WING T/E LOWER AREA AT STA 519 ACCESS PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1- 21. 2 L 7 4 4F RT 4A25 1999012200425 19990122 00425 WP 1999 1 22 DHL9980105C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 554 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING T/W LOWER AREA AT STA 554 PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999012200426 19990122 00426 WP 1999 1 22 DHL9980106C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 178 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING T/E LOWER AREA PANEL STA 178 CRACKED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999012200427 19990122 00427 WP 1999 1 22 DHL9980107C 1 19981103 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 120 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING T/E LOWER AREA AT STA 120 DELAMINATED. REPAIRED PER SRM 51-12-1. 2 L 7 4 4F RT 4A25 1999012200428 19990122 00428 WP 1999 1 22 DHL9980108C 1 19981115 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 2 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING T/E LOWER AREA NR 2 SPOILER PANEL DELAMINATED. REMOVED, REPAIRED AND REPLACED PANEL PER DAC MM 27- 61-1. 2 L 7 4 4F RT 4A25 1999012200429 19990122 00429 WP 1999 1 22 DHL9980109C 1 19981104 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 75 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING T/E LOWER PANEL STA 75 DELAMINATED. REPAIRED PANEL AND REINSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999012200430 19990122 00430 WP 1999 1 22 DHL99801100 1 19981027 A 7830 TR UNIT DOUG DC8 DC873F 302199F WP NR 2 ENGINE DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT T/R EXTERNAL SURFACE FOUND SEVERAL SCRATCHES AND DENTS AROUND NR 2 ENGINE. FABRICATED AND INSTALLED DO UBLER PER SRM 71-2-8, 4 DIA. 2 L 7 4 4F RT 4A25 1999012200431 19990122 00431 WP 1999 1 22 DHL99801101 1 19981018 A 5753 STRIP DOUG DC8 DC873F 302199F WP RT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT O/B FLAP UPPER AREA O/B ICE BREAKER AFT AREA HAS RUB STRIPS WORN OUT. REMOVED AND FABRICATED NEW RUB STR IP AND INSTALLED PER SRM 51-1-21, 1 X 7. 2 L 7 4 4F RT 4A25 1999012200432 19990122 00432 WP 1999 1 22 DHL99801102 1 19981018 A 5753 STRIP DOUG DC8 DC873F 302199F WP RT WING WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING O/B FLAP UPPER AREA CENTER ICE BREAKER AREA I/B AND O/B METAL RUB STRIPS WORN. REMOVED AND REPLACE D RUB STRIPS PER SRM 51-1-7, 1 X 7. 2 L 7 4 4F RT 4A25 1999012200433 19990122 00433 WP 1999 1 22 DHL99801103 1 19981116 A 5330 SKIN DOUG DC8 DC873F 302199F WP LT FAIRING DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT FAIRING PANEL 161 K2 DELAMINATED AROUND CORNER AND ELONGATED HOLE. REPAIRED PER SRM 51-1-9. 2 L 7 4 4F RT 4A25 1999012200434 19990122 00434 WP 1999 1 22 DHL99801104 1 19981106 A 5230 PANEL DOUG DC8 DC873F 302199F WP CARGO DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT FWD LOWER CARGO COMPT C-3 DOOR WELL COVER PANEL STA 1200 AND 1260 HAS SEVERAL CRACK DAMAGE ON SURFACE. F ABRICATED 5 DOUBLERS AND INSTALLED PER SRM 51-1-21A. 23 X 8, 9 X 12, 4.5 X 4.5, 7 X 4.5, 10 X 4.5. 2 L 7 4 4F RT 4A25 1999012200435 19990122 00435 WP 1999 1 22 DHL99801105 1 19981103 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1440 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT LOWER CARGO COMPT RT AT STA 1440 LONG R30 SHOWS CRACK DAMAGE ON ATTACH ANGLE. STOP DRILLED, FABRICATED ANGLE REPAIR AND INSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200436 19990122 00436 WP 1999 1 22 DHL99801106 1 19981017 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E AREA AT STA XW 5 CRACKED ON ANGLE NEXT TO WEB PANEL. STOP DRILLED, FABRICATED ANGLE REPAIR PER DC-8 SRM 51-1-4, 6 X 2. 2 L 7 4 4F RT 4A25 1999012200437 19990122 00437 WP 1999 1 22 DHL99801107 1 19981017 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RIGHT WING T/E INBOARD LOWER STA 5.00 AT I/B FLAP I/B HINGE SUPPORT FWD AREA FOUND CRACK ON ANGLE REINFORCEM ENT. REMOVED CRACKED ANGLE, FABRICATED NEW ANGLE 12 X 2.5 PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200438 19990122 00438 WP 1999 1 22 DHL99801108 1 19981017 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 337 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING LOWER INT AREA AT STA 337 HAS CRACK 12 INCHES LONG ON LOWER INT RIB WEB AREA. REMOVED CENTER L/E LEFT WING. REMOVED CRACKED LOWER DOUBLER FROM CENTER L/E AT 337. FABRICATED REPAIR DOUBLER PER SRM 57-3-3, 25 X 16. I NSTALLED DOUBLER PER SRM 51-1-21 AND INSTALLED CENTER WING SECTION PER SRM 57-20-2. 2 L 7 4 4F RT 4A25 1999012200439 19990122 00439 WP 1999 1 22 DHL99801109 1 19981017 A 5710 STRUCTURE DOUG DC8 DC873F 302199F WP WS 337 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT CENTER LOWER INT AREA AT STA 337 CRACKED. REMOVED CENTER L/E, FABRICATED REPAIR DOUBLER PER SRM 57-3-3, 25 X 16. INSTALLED PER SRM 51-1-8, INSTALLED CENTER L/E PER 57-20-2. 2 L 7 4 4F RT 4A25 1999012200440 19990122 00440 WP 1999 1 22 DHL9980110C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 120 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E LOWER AREA STA 120 DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999012200441 19990122 00441 WP 1999 1 22 DHL9980111C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 120 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E LOWER AREA STA 120 FUEL CHUTE PANEL DELAMINATED. REPAIRED AND REINSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200442 19990122 00442 WP 1999 1 22 DHL9980112C 1 19981011 A 5753 VANE DOUG DC8 DC873F 302199F WP NR 4 TE FLAP DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING NR 4 VANE FLAP DELAMINATED. REMOVED AND REPLACED VANE PER MM 27-51-14. 2 L 7 4 4F RT 4A25 1999012200443 19990122 00443 WP 1999 1 22 DHL9980113C 1 19981011 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E SPOILER PANEL DELAMINATED. REMOVED AND REPLACED SPOILER PER MM 27-61-1. 2 L 7 4 4F RT 4A25 1999012200444 19990122 00444 WP 1999 1 22 DHL9980114C 1 19981113 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, PANEL 161 CC DELAMINATED. REPAIRED PANEL AND INSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999012200445 19990122 00445 WP 1999 1 22 DHL9980115C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 624 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING UPPER T/E AREA STA 624 DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200446 19990122 00446 WP 1999 1 22 DHL9980116C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 535 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING UPPER T/E AREA STA 535 UPPER PANEL TEMPORARY REPAIR. REMOVED, REPAIRED AND INSTALLED PER SRM 51-1-2 4. 2 L 7 4 4F RT 4A25 1999012200447 19990122 00447 WP 1999 1 22 DHL9980117C 1 19981011 A 5755 SKIN DOUG DC8 DC873F 302199F WP NR 5 SPOILER DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E UPPER AREA NR 5 SPOILER PANEL DELAMINATED. REMOVED, REPAIRED AND REINSTALLED PANEL. 2 L 7 4 4F RT 4A25 1999012200448 19990122 00448 WP 1999 1 22 DHL9980118C 1 19981011 A 5753 SKIN DOUG DC8 DC873F 302199F WP WS 19 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E UPPER I/B AREA AT STA 19 AFT T/E PANEL DELAMINATED. REMOVED AND REPAIRED PANEL AND REINSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999012200449 19990122 00449 WP 1999 1 22 DHL9980119C 1 19981011 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 19 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E UPPER I/B AREA STA 19 HAS DENTS. REMOVED AND REPAIRED DENTED PANEL PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200450 19990122 00450 WP 1999 1 22 DHL9980120C 1 19981021 A 5350 FAIRING DOUG DC8 DC873F 302199F WP LT WING/ FUS DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, PANEL 261K SHOWS DELAMINATION. REMOVED AND REPAIRED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012200451 19990122 00451 WP 1999 1 22 DHL9980121C 1 19981021 A 5330 PANEL DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, PANEL 162Q DELAMINATED INSIDE RT HAND CORNER. REMOVED DELAMINATED PANEL, REPAIRED AND REINSTALLED PER SRM 5 1-3-0. 2 L 7 4 4F RT 4A25 1999012200452 19990122 00452 WP 1999 1 22 DHL9980122C 1 19981111 A 5350 FAIRING DOUG DC8 DC873F 302199F WP FUSELAGE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, FAIRING PANEL 162K IS DELAMINATED. REMOVED AND REPAIRED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012200453 19990122 00453 WP 1999 1 22 DHL9980123C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1310 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 3 ELONGATED STA 1310. REMOVED AND REPLACED DAMAGED SECTION PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200454 19990122 00454 WP 1999 1 22 DHL9980124C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 409-420 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 4 PLUG ELONGATED BETWEEN STA 409 TO 420. REMOVED, FABRICATED AND INSTALLED NEW SECTION PER SR M 53-2-3. 2 L 7 4 4F RT 4A25 1999012200455 19990122 00455 WP 1999 1 22 DHL9980125C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 328 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 4 PLUG WORN BETWEEN STA 326 TO 329. FABRICATED AND REPLACED SEAT TRACK PLUGS PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200456 19990122 00456 WP 1999 1 22 DHL9980126C 1 19981101 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 151 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 4 PLUG DAMAGED AT STA 151. REMOVED AND REPLACED PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200457 19990122 00457 WP 1999 1 22 DHL9980127C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 838 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 4 WORN AT STA 838. REMOVED DAMAGED AREA AND FABRICATED PLUG AND REINSTALLED PER SRM 51-1-8. 2 L 7 4 4F RT 4A25 1999012200458 19990122 00458 WP 1999 1 22 DHL9980128C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 863 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK DAMAGED AT STA 863. REMOVED AND REPLACED PLUG PER SRM 51-8-8. 2 L 7 4 4F RT 4A25 1999012200459 19990122 00459 WP 1999 1 22 DHL9980129C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 976 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 4 DAMAGED AT STA 976. REMOVED AND FABRICATED NEW SEAT TRACK PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200460 19990122 00460 WP 1999 1 22 DHL9980130C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1260 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 4 DAMAGED AT STA 1260. REMOVED DAMAGED SECTION AND INSTALLED REPAIR PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200461 19990122 00461 WP 1999 1 22 DHL9980131C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1300 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK DAMAGED STA 1300 TO 1310. REMOVED DAMAGED PLUG, FABRICATED AND INSTALLED NEW PLUG PER SRM 53-2-3 . 2 L 7 4 4F RT 4A25 1999012200462 19990122 00462 WP 1999 1 22 DHL9980132C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 290-330 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 5 HOLES ELONGATED FROM 290 TO 330. REMOVED DAMAGED SECTION FROM 310 TO 370 AND REINSTALLED SP LICE PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012200463 19990122 00463 WP 1999 1 22 DHL9980133C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1660-1710 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 5 ELONGATED BETWEEN STA 1660 TO 1710. REMOVED DAMAGED SECTION, INSTALLED NEW SECTION PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200464 19990122 00464 WP 1999 1 22 DHL9980134C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1080-1100 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 5 ELONGATED BETWEEN STA 1080 TO 1100. REMOVED DAMAGED SECTION, FABRICATED PLUG AND INSTALLED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200465 19990122 00465 WP 1999 1 22 DHL9980135C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 600-620 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 5 DAMAGED BETWEEN STA 600 TO 620. REMOVED AND REPLACED DAMAGED SECTION PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200466 19990122 00466 WP 1999 1 22 DHL9980136C 1 19981105 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 239 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 5 WORN AT STA 239. REMOVED DAMAGED SECTION AND FABRICATED REPAIR PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200467 19990122 00467 WP 1999 1 22 DHL9980137C 1 19981103 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 230 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 6 WORN AT STA 230. REMOVED AND REPLACED DAMAGED PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200468 19990122 00468 WP 1999 1 22 DHL9980138C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 250 WORN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK WORN STA 250. REMOVED DAMAGED AREA AND REINSTALLED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200469 19990122 00469 WP 1999 1 22 DHL9980139C 1 19981109 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 300 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 6 ELONGATED AT STA 300 TO 315. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200470 19990122 00470 WP 1999 1 22 DHL9980140C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 590 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 6 ELONGATED AT STA 590 AND 600. REMOVED, FABRICATED AND INSTALLED NEW PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200471 19990122 00471 WP 1999 1 22 DHL9980141C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 945 & 955 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 6 WORN PLUG AT STA 945 AND 955. REMOVED PLUGS AT 945 AND 955, FABRICATED REPAIR PLUGS AND INS TALLED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200472 19990122 00472 WP 1999 1 22 DHL9980142C 1 19981103 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1400 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK 36 PLUG ELONGATED AT STA 1400. REMOVED AND INSTALLED FABRICATED PLUG PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200473 19990122 00473 WP 1999 1 22 DHL9980143C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1695 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 6 DAMAGED AT STA 1695. REMOVED AND REPLACED SEAT TRACK FROM 1550 TO 1610 PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200474 19990122 00474 WP 1999 1 22 DHL9980144C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 329 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 2 HOLES ARE ELONGATED AT STA 329. REMOVED DAMAGED SEAT TRACK, FABRICATED NEW PLUGS AND INSTAL LED PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200475 19990122 00475 WP 1999 1 22 DHL9980145C 1 19981014 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 385 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, SEAT TRACK NR 2 ELONGATED HOLES STA 385. REMOVED DAMAGED PLUG AND INSTALLED NEW PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012200476 19990122 00476 WP 1999 1 22 DHL9980146C 1 19980115 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 990 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT CARGO COMPT, STA 990 LT WALL PANEL SHOWS DAMAGED STRAP LOWER AREA. REMOVED DAMAGED STRAP, FABRICATED NE W STRAP AND INSTALLED PER SRM 51-3-0, 25 X 36. 2 L 7 4 4F RT 4A25 1999012200477 19990122 00477 WP 1999 1 22 DHL9980147C 1 19981015 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 1060 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT CARGO COMPT RT STA 1060 LOWER AREA HAS DAMAGED STRAP. REMOVED DAMAGED STRAP, FABRICATED NEW STRAP AND I NSTALLED PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012200478 19990122 00478 WP 1999 1 22 DHL9980148C 1 19981114 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 980-1180 MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT CARGO COMPT LT FLOORING PANELS SHOWS MISSING STRAPS STA 980 TO 1180. FABRICATED STRAP AND INSTALLED PE R SRM 51-1-4, 193 X 1.25. 2 L 7 4 4F RT 4A25 1999012200479 19990122 00479 WP 1999 1 22 DHL9980149C 1 19981015 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 980-1010 MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT CARGO COMPT RT STA 980 TO 1010 O/B STRAP OF SEAT TRACK MISSING SECTION. FABRICATED STRAP PER SRM 51-1-4 AND INSTALLED PER SRM 51-3-0, 1 X 60. 2 L 7 4 4F RT 4A25 1999012200480 19990122 00480 WP 1999 1 22 DHL9980150C 1 19981024 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 391 & 421 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, L/W UPPER SURFACE T/E BETWEEN STA XRS 391 AND XW 421 METAL SEAL STRIP DAMAGE. REMOVED METAL STRIP DAMAGE, FABRICATED NEW SEAL AND INSTALLED PER SRM 51-1-15, 5 X 1. 2 L 7 4 4F RT 4A25 1999012200481 19990122 00481 WP 1999 1 22 DHL9980151C 1 19981015 A 5320 BRACKET DOUG DC8 DC873F 302199F WP BS 640 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING UPPER AREA WING TO FUS SUPPORT BRACKET STA 640 CRACKED. FABRICATED AND INSTALLED NEW BRACKET PER SR M 51-3-0, 6 X 6. 2 L 7 4 4F RT 4A25 1999012200482 19990122 00482 WP 1999 1 22 DHL9980152C 1 19981015 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 120 MISSING A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E UPPER AREA STA 120 PIECE OF METAL MISSING ON SKIN NEXT TO NR 1 SPOILER O/B HINGE AREA 2060. CU T OUT DAMAGED AREA AND FABRICATED DOUBLER AND FILLER 1 X 4 PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200483 19990122 00483 WP 1999 1 22 DHL9980153C 1 19981017 A 5720 BRACKET DOUG DC8 DC873F 302199F WP WS 603 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING O/B LEADING EDGE INTERIOR AT STA 603 FOUND PNEUMATIC SUPPORT CRACKED. FABRICATED REPAIR DOUBLER PER SRM 51-1-21, 2 X 6. 2 L 7 4 4F RT 4A25 1999012200484 19990122 00484 WP 1999 1 22 DHL9980154C 1 19981017 A 5320 BRACKET DOUG DC8 DC873F 302199F WP BS 360 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, MAIN CARGO COMPT FS 360 CEILING RT SIDE ATTACH BRACKET BROKEN. REMOVED AND FABRICATED NEW BRACKET PER SRM 5 1-1-21, 2 X 2. 2 L 7 4 4F RT 4A25 1999012200485 19990122 00485 WP 1999 1 22 DHL9980155C 1 19981123 A 5320 FRAME DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, MAIN CARGO DOOR LOWER FRAME AFT CORNER SECTION HAS A TWO INCH CRACK. WELDED CRACKED AREA PER DPS 10.225 AND INSTALLED LOWER FRAME AFT CORNER PER SRM 51-3-0 . 2 L 7 4 4F RT 4A25 1999012200486 19990122 00486 WP 1999 1 22 DHL9980156C 1 19981016 A 5750 FAIRING DOUG DC8 DC873F 302199F WP BS 910 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING I/B UPPER AREA WING TO FUS FAIRING SUPPORT BRACKET AT FUSE 910 SUPPORT CRACKED. INSTALLED REPAIR P ER SM 51-1-21, 2 X 6.5. 2 L 7 4 4F RT 4A25 1999012200487 19990122 00487 WP 1999 1 22 DHL9980157C 1 19981016 A 7110 COWLING DOUG DC8 DC873F 302199F WP NR 4 ENGINE DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, ENG NR 4 I/B COWLING INTERIOR AFTER SECTION DELAMINATION AT APPROX 10 O' CLOCK POSITION. REPAIRED PER SRM 5 1-1-19. 2 L 7 4 4F RT 4A25 1999012200488 19990122 00488 WP 1999 1 22 DHL9980158C 1 19981017 A 5753 COVER DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING O/B FLAP I/B HINGE O/B FACE METAL COVER BROKEN. REMOVED DAMAGED COVER AND FABRICATED NEW AND INSTAL LED PER SRM 51-121. 2 L 7 4 4F RT 4A25 1999012200489 19990122 00489 WP 1999 1 22 DHL9980159C 1 19981017 A 5753 RUB STRIP DOUG DC8 DC873F 302199F WP WS 311 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E LOWER AREA STA 311 METAL RUB STRIP AT STA 311. FABRICATED NEW RUB STRIP AND INSTALLED PER SRM 51-1-21, 2 X 10. 2 L 7 4 4F RT 4A25 1999012200490 19990122 00490 WP 1999 1 22 DHL9980160C 1 19981017 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 485 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING L/E LOWER AREA STA XW 485 SMALL SQUARE ACCESS PANEL CRACKED. REMOVED, FABRICATED AND INSTALLED NEW PANEL PER SRM 51-1-4, 7 X 7. 2 L 7 4 4F RT 4A25 1999012200491 19990122 00491 WP 1999 1 22 DHL9980161C 1 19981017 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING I/B TRAILING EDGE AREA AT STA XWS 5 CRACK ON WEB PANEL JUST ABOVE I/B FLAP I/B HINGE AREA. REMOVED CRACKED PANEL, FABRICATED NEW WEB PER SRM 51-1-21, 15 X 5.5. 2 L 7 4 4F RT 4A25 1999012200492 19990122 00492 WP 1999 1 22 DHL9980162C 1 19981017 A 5730 SKIN DOUG DC8 DC873F 302199F WP WS 106 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E AREA STA 106 JUST BELOW I/B FLAP ACTUATOR LT SIDE LOWER AREA CRACKED AT FAIRING CUTOUT. REPAIR ED AND REINSTALLED PANEL PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012200493 19990122 00493 WP 1999 1 22 DHL9980163C 1 19981110 A 5720 SUPPORT DOUG DC8 DC873F 302199F WP BS 822 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, WING CENTER LOWER FUSELAGE RT LOWER AREA APPROX FS 822 AT RT OF FUEL DRAIN VALVE FOUND CRACK ON ANGLE SUPPOR TS. REMOVED DAMAGED ANGLE SUPPORTS, FABRICATED AND INSTALLED PER SRM 51-1-20, 5.5 X 1 X 1. 2 L 7 4 4F RT 4A25 1999012200494 19990122 00494 WP 1999 1 22 DHL9980164C 1 19981017 A 5320 FRAME DOUG DC8 DC873F 302199F WP CARGO DOORWAY CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT FWD CARGO COMPT METAL AFT SIDE OF C2 DOOR JAMBS WALL CRACKED LOWER SIDE DAMAGED. STOP DRILLED CRACK, FA BRICATED AND INSTALLED ANGLE REPAIR AND INSTALLED PER SRM 51-1-8, 4 X 4. 2 L 7 4 4F RT 4A25 1999012200495 19990122 00495 WP 1999 1 22 DHL9980165C 1 19981112 A 5312 BULKHEAD DOUG DC8 DC873F 302199F WP BS 1320 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, AFT FWD LOWER CARGO COMPT BULKHEAD ON STA 1320 SHOWS SEVERAL CRACK DAMAGES LT AND RT. STOP DRILLED CRACKS AND FABRICATED REPAIR DOUBLERS PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999012200496 19990122 00496 WP 1999 1 22 DHL9980166C 1 19981019 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 4 ENGINE CHAFED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, ENGINE NR 4 INTERIOR PANEL OF O/B TRANSLATING COWL ON INTERIOR SURFACE CHAFED. CUT OUT CHAFING AND INSTLAL LED DOUBLER PER 70 SERIES SRM 71-2-8, 2 X 2. 2 L 7 4 4F RT 4A25 1999012200497 19990122 00497 WP 1999 1 22 DHL9980167C 1 19981019 A 7110 COWL DOUG DC8 DC873F 302199F WP NR 4 ENGINE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, ENGINE NR 4 O/B TRANSLATING COWL INNER PANEL SECTION SHOWS CRACK DAMAGE TO INTERIOR SURFACE. STOP DRILLED END OF CRACK, FABRICATED REPAIR PER SRM 71-2-8, 3 X 3.5. 2 L 7 4 4F RT 4A25 1999012200498 19990122 00498 WP 1999 1 22 DHL9980168C 1 19981019 A 5753 HINGE FITTING DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING FLAP HINGE FITTING STA 97 NR 3A BOLT HOLE O/B SIDE CRACKED. REMOVED FITTING, INSTALLED NEW FITTIN G PER S/B 27-249 AND SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200499 19990122 00499 WP 1999 1 22 DHL9980169C 1 19981019 A 5753 FITTING DOUG DC8 DC873F 302199F WP LT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING HINGE FITTING BOLT AT STA NR 3B BOLT HOLE CRACKED I/B SIDE STA 97. REAMED BOLT HOLE .0312 OVERSIZ E PER SRM 51-3-2. 2 L 7 4 4F RT 4A25 1999012200500 19990122 00500 WP 1999 1 22 DHL9980170C 1 19981116 A 5753 FITTING DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RIGHT WING FLAP HINGE FITTING BOLT HOLE NR 3A LEFT CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-2. 2 L 7 4 4F RT 4A25 1999012200501 19990122 00501 WP 1999 1 22 DHL9980171C 1 19981019 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 785 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING O/B LEADING EDGE INTERIOR LOWER AREA AT STA 785 RIBS CRACKED. STOP DRILLED HOLE AND FABRICATED DOU BLER REPAIR 6 X 1/25 PER SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012200502 19990122 00502 WP 1999 1 22 DHL9980172C 1 19981116 A 5720 BRACKET DOUG DC8 DC873F 302199F WP WS 603 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING O/B UPPER INTERIOR AREA AT STA 603 PNEUMATIC DUCT SUPPORT HOUSING IS CRACKED. REMOVED DAMAGED HOU SING BRACKET, FABRICATED NEW AND INSTALLED PER SRM 51-1-21, 4 X 6. 2 L 7 4 4F RT 4A25 1999012200503 19990122 00503 WP 1999 1 22 DHL9980173C 1 19981019 A 5753 SKIN DOUG DC8 DC873F 302199F WP LT TE FLAP BENT A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING O/B FLAP LOWER CORNER TIP IS BENT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED NEW T/E PER SRM 51-1-4 AND 51-1-21, 5 X 8. 2 L 7 4 4F RT 4A25 1999012200504 19990122 00504 WP 1999 1 22 DHL9980174C 1 19981019 A 5720 STRIP DOUG DC8 DC873F 302199F WP WS 69 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RIGHT WING LEADING EDGE I/B EXT LOWER AREA AT STA 69 METAL RUB STRIP CRACKED. REMOVED DAMAGED STRIP, FABRIC ATED NEW STRIP AND INSTALLED PER SRM 51-1-1. 2 L 7 4 4F RT 4A25 1999012200505 19990122 00505 WP 1999 1 22 DHL9980175C 1 19981019 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING TRAILING EDGE I/B LOWER AREA AT STA XW 5, JUST ABOVE FLAP I/B HINGE AREA FOUND CRACK AT WEB PANEL. R EMOVED, FABRICATED AND INSTALLED PANEL PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200506 19990122 00506 WP 1999 1 22 DHL9980176C 1 19981019 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING TRAILING EDGE I/B LOWER AREA AT XW 5, JUST ABOVE I/B FLAP HINGE CRACKS ON WEB COVER PANEL. REMOV ED AND FABRICATED NEW COVER PLATE AND INSTALLED PER SRM 51-3-0, 15 X 5.25. 2 L 7 4 4F RT 4A25 1999012200507 19990122 00507 WP 1999 1 22 DHL9980177C 1 19981113 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING TRAILING EDGE I/B LOWER AREA STA XW 5, FOUND CRACKED ANGLE BEHIND WEB PANEL JUST ABOVE I/B FLAP. STOP DRILLED CRACK 25 AND FABRICATED REPAIR DOUBLER PER SRM 53-2-3, 6 X 2. INSTALLED PER SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999012200508 19990122 00508 WP 1999 1 22 DHL9980178C 1 19981021 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 210-450 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, REPLACED SKIN FROM STA 210 TO 450 STR 21L TO 31L. REMOVED AND REPLACED SKIN PER DAC DRAWING 5755230. 2 L 7 4 4F RT 4A25 1999012200509 19990122 00509 WP 1999 1 22 DHL9980179C 1 19981023 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP COCKPIT DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, FLIGHT ENGINEER FWD SEAT TRACK SHOWS HOLES ELONGATED. REMOVED AND REPLACED SEAT TRACK PER SRM 51-3-0. 2 L 7 4 4F RT 4A25 1999012200510 19990122 00510 WP 1999 1 22 DHL9980180C 1 19981118 A 5720 DOUBLER DOUG DC8 DC873F 302199F WP WS 456 DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING CENTER LEADING EDGE O/B AREA AT STA 456 FOUND DAMAGED ON SLOT L/E SIDE. TRIMMED DAMAGED I/B EDGE OF OUTER PLATING OF LEFT WING EXTENDED L/E. REMOVED DAMAGED INNER DOUBLER, FABRICATED REPAIR DOUBLER AND FILLER PER EO 18R5761050. 2 L 7 4 4F RT 4A25 1999012200511 19990122 00511 WP 1999 1 22 DHL9980181C 1 19981024 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 291.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING CTR L/E INTERIOR LOWER I/B INTERNAL AREA AT STA 291.5 FOUND CRACK IN LOWER RIB. STOP DRILLED AND FA BRICATED REPAIR DOUBLER PER SRM 57-2-0, 6 X 1.25. 2 L 7 4 4F RT 4A25 1999012200512 19990122 00512 WP 1999 1 22 DHL9980182C 1 19981030 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 291.5 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING CTR L/E INTERIOR LOWER I/B INTERNAL AREA STA 291.5 FOUND CRACK ON LOWER RIB. STOP DRILLED HOLE AND FABRICATED REPAIR DOUBLER PER SRM 51-1-21, 6 X 1.25. 2 L 7 4 4F RT 4A25 1999012200513 19990122 00513 WP 1999 1 22 DHL9980183C 1 19981024 A 5720 SHIM DOUG DC8 DC873F 302199F WP WS 463 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING L/E LOWER AREA AT STA 463 JUST ABOVE NR 1 PYLON LT SIDE FOUND BROKEN SHIM. TRIMMED AREA, WITHIN LIM ITS. 2 L 7 4 4F RT 4A25 1999012200514 19990122 00514 WP 1999 1 22 DHL9980184C 1 19981024 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 463 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING L/E INTERIOR AREA AT STA 463 JUST ABOVE NR 1 PYLON ON I/B SIDE FOUND CRACKED ANGLE SUPPORT. FABRI CATED ANGLE PER SRM 57-3-2. 2 L 7 4 4F RT 4A25 1999012200515 19990122 00515 WP 1999 1 22 DHL9980185C 1 19981024 A 5720 SHIM DOUG DC8 DC873F 302199F WP WS 463 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING L/E LOWER AREA AT STA 463 JUST ABOVE NR 4 PYLON ON LT SIDE FOUND BROKEN SHIM ON LOWER SPAR MATING AR EA. REMOVED AND FABRICATED LOWER SHIM PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200516 19990122 00516 WP 1999 1 22 DHL9980186C 1 19981024 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 463 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING T/E INTERIOR AREA AT STA 463 JUST ABOVE NR 4 PYLON ON I/B SIDE FOUND CRACK ON VERTICAL ANGLE. REMOV ED CRACKED ANGLE, FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200517 19990122 00517 WP 1999 1 22 DHL9980187C 1 19981028 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 520 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT CENTER WING LEADING EDGE UPPER O/B AREA STA XFS 520 FOUND CRACKED. REMOVED CRACKED ANGLE AND INSTALLED N EW ANGLE PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200518 19990122 00518 WP 1999 1 22 DHL9980188C 1 19981028 A 5720 ANGLE DOUG DC8 DC873F 302199F WP WS 520 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LT WING LEADING EDGE INTERIOR UPPER O/B AREA AT XFS 520 FOUND CRACKED. REMOVED AND REPLACED CRACKED ANGLE P ER SRM 51-21. 2 L 7 4 4F RT 4A25 1999012200519 19990122 00519 WP 1999 1 22 DHL9980189C 1 19981028 A 5500 FAIRING DOUG DC8 DC873F 302199F WP EMPENNAGE DAMAGED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, ELONGATED HOLES AND BARE METAL SPACERS ON FAIRING PANEL 5704072-403. FABRICATED DOUBLER PER SRM 53-2-0 AND INSTALLED PER SRM 51-1-21, 5 X 6. 2 L 7 4 4F RT 4A25 1999012200520 19990122 00520 WP 1999 1 22 DHL9980190C 1 19981101 A 3213 BEAM DOUG DC8 DC873F 302199F WP LT MLG CORRODED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, WHEELS NR 5 AND NR 6 BOGIE BEAM ASSY CORROSION. REMOVED AND REPLACED BOGIE BEAM PER MM 32-43-0. 2 L 7 4 4F RT 4A25 1999012200521 19990122 00521 WP 1999 1 22 DHL9980191C 1 19981111 A 5720 STIFFENER DOUG DC8 DC873F 302199F WP LT CENTER WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING CENTER L/E INTERIOR MID UPPER SECTION FOUND 2 INCH CRACK ON STRUCTURAL STIFFENER. REMOVED CRACKED ANGLE, FABRICATED ANGLE PER SRM 51-1-8, 2 X 1.75. INSTALLED PER SRM 51-1-2. 2 L 7 4 4F RT 4A25 1999012200522 19990122 00522 WP 1999 1 22 DHL9980192C 1 19981106 A 5711 SPAR DOUG DC8 DC873F 302199F WP WS 408 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING L/E SPAR AREA AT XW 408 UPPER SURFACE CRACK ON FIXED L/E SECTION OF UPPER FLANGE. STOP DRILLED CR ACK, FABRICATED AND INSTALLED REPAIR DOUBLER AND INSTALLED PER SRM 51-1-8 AND EO 18R5761051. 2 L 7 4 4F RT 4A25 1999012200523 19990122 00523 WP 1999 1 22 DHL9980193C 1 19981107 A 5720 BRACKET DOUG DC8 DC873F 302199F WP WS 456 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, LEFT WING L/E SPAR AT XRS 456 CONDUIT BRACKET CRACKED. REMOVED AND FABRICATED BRACKET AND INSTALLED PER SRM 51-1-21, 2 X 1. 2 L 7 4 4F RT 4A25 1999012200524 19990122 00524 WP 1999 1 22 DHL9980194C 1 19981123 A 7603 365309956 CONTROL CABLE DOUG DC8 DC873F 302199F WP NR 4 ENGINE BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RIGHT WING LEADING EDGE FRONT SPAR AREA STA 421 NR 4 ENGINE CONTROL CABLE BROKEN. REMOVED, FABRICATED AND P ULL TESTED CABLE PER MM 91-10-1. INSTALLED PER 76-11-0. 2 L 7 4 4F RT 4A25 1999012200525 19990122 00525 WP 1999 1 22 DHL9980195C 1 19981112 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 1580-1600 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, MAIN CARGO COMPT RT SIDE BETWEEN FS 1580 TO 1600 AT CUSP LINE WEB CRACKED. CLEANED DAMAGED AREA, FABRICATED REPAIR DOUBLER PER SRM 53-2-3. 2 L 7 4 4F RT 4A25 1999012200526 19990122 00526 WP 1999 1 22 DHL9980196C 1 19981111 A 5730 PANEL DOUG DC8 DC873F 302199F WP WS 727 DELAMINATED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING UPPER TRAILING EDGE O/B AREA AT STA 727 TRAILING EDGE PANEL DELAMINATED. REMOVED PANEL, REPAIRED A ND REINSTALLED PER SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999012200527 19990122 00527 WP 1999 1 22 DHL9980197C 1 19981017 A 5321 FLOOR PANEL DOUG DC8 DC873F 302199F WP BS 180 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, FWD LOWER CARGO COMPT STA 180 RT UNDER BRACKET SUPPORT ATTACHING TO FLOOR PANEL CRACKED. REMOVED DAMAGED SE CTION, FABRICATED DOUBLER AND INSTALLED PER SRM 53-2-0, 5 X 7. 2 L 7 4 4F RT 4A25 1999012200528 19990122 00528 WP 1999 1 22 DHL9980198C 1 19981018 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 347 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING CENTER L/E LOWER INTERIOR AREA AT STA 347 FOUND CRACK ON LOWER RIB. STOP DRILLED HOLE, FABRICATED R EPAIR DOUBLER PER SRM 57-2-0 AND INSTALLED PER SRM 51-1-21, 6 X 1.25. 2 L 7 4 4F RT 4A25 1999012200529 19990122 00529 WP 1999 1 22 DHL9980199C 1 19981029 A 5712 RIB DOUG DC8 DC873F 302199F WP WS 300 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 801DH 46033 AT C-CHECK, RT WING CENTER LOWER INTERNAL AREA AT STA 300 FOUND CRACKD ON LOWER RIB. DRILLED TOP HOLE, FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 51-1-21, 6 X 1.25. 2 L 7 4 4F RT 4A25 1999012200530 19990122 00530 EA 1999 1 22 SWIA971358 1 19981231 A 2612 WIRE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE CHAFED A SWIA E ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 NM 07 408SW 7055 LEFT ENGINE JET PIPE OVERHEAT FAILED IN FLIGHT. SHUT ENGINE DOWN. FOUND LEFT ENGINE JET PIPE WIRES CHAFED TO GROUND. R EPAIRED AND REPOSITIONED WIRES. TESTED JET PIPE SYSTEM, LEFT SIDE CHECKS GOOD. 2 L 7 2 4F 4 F RT A21EA E15NE 1999012200534 19990122 00534 NM 1999 1 22 P5CA9900003 1 19981230 A 7110 SKIN BOEING 747 747122 1384872 NM NR 2 ENG COWL DELAMINATED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 852FT 19757 NR 2 ENGINE I/B FAN COWL UPPER AFT CORNER BENT AND DELAMINATED. REPAIRED IAW SRM 51-40-06. 2 L 7 4 4F A20WE 1999012200536 19990122 00536 WP 1999 1 22 RRXA99001 1 19981031 A 3231 4648253 ROD DOUG DC8 DC873F 302199F WP RT NLG DOOR BROKEN A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 791FT 46045 ON WALKAROUND, FOUND NOSE GEAR RT AFT DOOR SUPPORT ROD BROKEN. ALSO, SKIN DAMAGE AROUND ATTACHMENT POINTS AT DOOR HINGE S. REMOVED BROKEN NLG RT AFT DOOR ROD ASSY AND INSTALLED SERV ALT DOOR ROD ASSY (P/N 4648253) IAW MM 32-22-1. ADDITION ALLY INSPECTED LT AFT DOOR ROD ASSY AND FOUND IT RUSTED. IT WAS REMOVED AND REPLACED BY SERV LT AFT DOOR ROD (P/N 46482 53) IAW 32-22-1. REPAIRED FUSELAGE SKIN BETWEEN STA 20 TO 12 AND LONG 31R TO 34R DUE TO DAMAGE BY NLG DOOR ROD IAW COOP ESA EO C00-8-53-601-98 DATED 11-1-98. DOCUMENTED ON FAA FORM 8110-3 APPROVED AND SUBMITTED BY FAA, DESIG SW 810 DATED 1 1-1-98, CHECKED RETRACTION IAW MM 32-30-0, NORMAL COND. 2 L 7 4 4F RT 4A25 1999012200591 19990122 00591 CE 1999 1 22 99ZZZX355 1 19981201 A 3230 CHAIN BEECH 200 B200 1152922 CE MLG LOOSE A DBCA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 13 72GG BB1080 PILOT REPORTED LANDING GEAR INTRANSIT LIGHT WOULD NOT EXTINGUISH AFTER RETRACTING GEAR. TROUBLESHOT AND FOUND FORWARD CHAIN PARTIALLY OFF IDLER SPROCKET. RE-INSTALLED CHAIN ON SPROCKET. ADJUSTED CHAIN TENSION AND ADJUSTED UPLOCK SWITCH IAW BEECH KA200 MM. OPS CHECK OK. SUBMITTER SUSPECTED PROBLEM DUE TO OPERATION IN COLD WEATHER. 1 L 7 2 4T A24CE 1999012200601 19990122 00601 WP 1999 1 22 ORJA98317 1 19981218 A 3350 2292AG FUSELAGE DOUG DC9 DC983 3022083 WP POWER SUPPLY FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 RNO - RIGHT EMERGENCY EXIT POWER PACK. REPLACED FUSE IN POWER SUPPLY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012200602 19990122 00602 WP 1999 1 22 ORJA98318 1 19981217 A 3350 1001191 BATTERY DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 SJC - RIGHT FORWARD OVER THE WING ESCAPE HATCH, LOWER EMERGENCY LIGHT BATTERY PACK IS INOP. KEEPING A ROW EMERGENCY LIG HT OFF. REMOVED AND REPLACED BATTERIES FOR EMERGENCY LIGHT ASSEMBLY AT RIGHT FORWARD OVER THE WING ESCAPE HATCH, LOWER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012200603 19990122 00603 WP 1999 1 22 ORJA98316 1 19981219 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP ROWS 21-24 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 876RA 53183 RNO - EMERGENCY LIGHT INOPERATIVE AT ROWS 21, 22, 23, 24 (SEAT LIGHTS). REMOVED AND REPLACED BATTERY CHARGER. OPS CHEC K GOOD. (M) 2 L 7 2 4F RT A6WE 1999012200604 19990122 00604 WP 1999 1 22 ORJA98315 1 19981206 A 3350 59306431 BATTERY CHARGER DOUG DC9 DC983 3022083 WP ROWS 8/9/10/11 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 COS - EMERGENCY LIGHTS AT ROWS 8, 9, 10, AND 11 DO NOT WORK. REMOVED AND REPLACED BATTERY CHARGER SYSTEM. OPS CHECK GO OD. (M) 2 L 7 2 4F RT A6WE 1999012200605 19990122 00605 WP 1999 1 22 ORJA98319 1 19981220 A 3350 2292AG FUSE DOUG DC9 DC983 3022083 WP ROWS 8-11 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - EMERGENCY LIGHT ROWS 8-11 INOPERATIVE. REPLACED FUSE AND BATTERIES RIGHT FORWARD BATTERY PACK. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999012200606 19990122 00606 WP 1999 1 22 99ZZZM31 1 19981220 A 3350 60030451 BATTERY DOUG DC9 DC983 3022083 WP ROWS 8-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - EMERGENCY LIGHT ROWS 8-11 INOPERATIVE. REPLACED FUSE AND BATTERIES RIGHT FORWARD BATTERY PACK. OPS CHECK NORMAL. (M) 2 L 7 2 4F RT A6WE 1999012200607 19990122 00607 WP 1999 1 22 ORJA98330 1 19981227 A 3350 EM1267 BATTERY DOUG DC9 DC987 3022087 WP TAIL DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 753RA 49587 AT RENO, EMERGENCY EXIT LIGHT INSIDE TAIL SECTION INOPERATIVE. REMOVED AND REPLACED BATTERY. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012200608 19990122 00608 WP 1999 1 22 ORJA98331 1 19981226 A 3350 6011779 POWER SUPPLY DOUG DC9 DC983 3022083 WP TAIL INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 AT RENO, E-LIGHTS IN TAIL OVER ESCAPE HANDLE INOPERATIVE. REPLACED POWER SUPPLY FOR AFFECTED LIGHTS. OPS OK. (M) 2 L 7 2 4F RT A6WE 1999012200609 19990122 00609 WP 1999 1 22 ORJA98327 1 19981226 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - RIGHT FORWARD EMERGENCY EXIT LOWER LIGHTING BATTERY PACK INOPERATIVE. REMOVED AND REPLACED FORWARD LOWER EMERGENC Y BATTERY PACK LIGHTING. (M) 2 L 7 2 4F RT A6WE 1999012200610 19990122 00610 WP 1999 1 22 ORJA98329 1 19981226 A 3350 60030451 BATTERY PACK DOUG DC9 DC982 3022082 WP ROW 21-24 DEF DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 824RA 53017 IN RNO, EMERGENCY EXIT IS SET LIGHTS INOPERATIVE 21-24 DEF. REMOVED AND REPLACED BATTERY PACK AT OVERWING EXIT LAMP 21 AC. OPS NORMAL. (M) 2 L 7 2 4F A6WE 1999012200611 19990122 00611 NE 1999 1 22 ORJA98314 2 19981216 A 7321 8080504033 EEC DOUG MD90 MD9030 3023690 NM IAE V2525 V2525D5 NE NR 2 ENGINE MALFUNCTIONED A ORJA C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 WP 11 902RA 53490 IN SJC - AT 40-50 KNOTS ON TAKEOFF ROLL AUTO THROTTLES ON, ENGINES SPOOLING UP AT 1.35 EPR ON LEFT AND RIGHT. RIGHT ENG INE THEN STARTED TO SPOOL DOWN (ROLL BACK). TAKEOFF WAS DISCONTINUED. REMOVED AND REPLACED NR 2 ENGINE EEC IAW MM 73. PERFORMED OPERATIONAL CHECK, OPS CHECK GOOD. (M) 2 L 7 2 4F 4 F RT A6WE A40NE 1999012200612 19990122 00612 WP 1999 1 22 ORJA98324 1 19981221 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP ROW 1-3 INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 IN RNO - EMERGENCY LIGHTS INOPERATIVE AT FORWARD ENTRY DOOR AND ROWS, 1, 2, 3 A/C. REMOVED AND REPLACED BATTERY CHARGER ASSEMBLY AT FORWARD ENTRY DOOR, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012200613 19990122 00613 WP 1999 1 22 ORJA98323 1 19981220 A 3241 LM124448 BEARING DOUG DC9 DC983 3022083 WP NR 2 MLG WRONG PART A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J W WARNING INDICATION INADEQUATE Q C TO TAKEOFF 1 WP 11 834RA 53124 IN LAS, ABORTED TAKEOFF WHEEL NOT TURNING LIGHT ILLUMINATED ON TAKEOFF ROLL APPROX 90 KNOTS RETURNED TO GATE. REPLACED BROKEN PINS ON NR 2 MAIN WHEEL BITE TEST GOOD IAW MM CHAPTER 32. UPON FURTHER INVESTIGATION MAINTENANCE DISCOVERED THAT THE INNER BEARINGS WAS OF THE WRONG TYPE FOR THE WHEEL ASSY MAINTENANCE REMOVED AND REPLACED THE TIRE ASSY. AIRCRAFT R ETURNED TO SERVICE. (M) 2 L 7 2 4F RT A6WE 1999012200614 19990122 00614 WP 1999 1 22 ORJA98326 1 19981218 A 3350 0105603003 HARNESS DOUG DC9 DC987 3022087 WP ROW 23 DEF FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 IN SJC, EMERGENCY LIGHTING ON SEAT 23 DEF INOPERATIVE. REMOVED AND REPLACED WIRING HARNESS, OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999012200615 19990122 00615 NM 1999 1 22 ORJA98332 1 19981229 A 3241 6006081 TRANSDUCER DOUG MD90 MD9030 3023690 NM NR 2 MLG FAILED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 903RA 53551 SJC - AUTO SPOILER FAIL AND ANTI-SKID FAULT MESSAGE ANNUNCIATED SHORTLY AFTER TAKEOFF ROLL STARTED. BIT CHECKED ANTI-SK ID CONTROL BOX, FOUND NR 2 MAIN ANTI-SKID WHEEL SPEED TRANSDUCER HAD FAILED. REMOVED AND REPLACED NR 2 MAIN WHEEL SPEED TRANSDUCER PER MM 32-45-05. (M) 2 L 7 2 4F RT A6WE 1999012200616 19990122 00616 NE 1999 1 22 ORJA98322 2 19981202 A 7200 ENGINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D219 52053 NE NR 2 FAILED A ORJA O OTHER X ENGINE FLAMEOUT CL CLIMB 1 WP 11 875RA 53182 LAS - DURING CLIMB-OUT, THROUGH FL 170 RIGHT ENGINE FAILED, RETURNED TO LAS. REMOVED AND REPLACED ENGINE NR 2. (M) 2 L 7 2 4F 4 F RT A6WE E9NE 1999012200617 19990122 00617 1999 1 22 HALA9800428 4 19981228 A 3444 5223698003 ALTIMETER DOUG DC9 DC951 3022051 WP COCKPIT FAILED A HALA O OTHER O OTHER CR CRUISE 1 WP 13 603DC 7586 47784 HNL - FLT 195 - AFTER TAKEOFF THROUGH APPROX 1000 FT, SIMULTANEOUSLY BOTH F/O'S AND CAPTAINS RADIO ALTIMETERS GOT FLAGS, TCAS GOT FLAGS ON BOTH SIDES, AND GPWS FAILS. REMOVED AND REPLACED NR 1 RADIO ALT T/R OPS CHECK ON NR 1 RADIO ALT, GPW S AND TCAS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999012200618 19990122 00618 NM 1999 1 22 MZZA98274 1 19981117 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1117-1138 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON PASSENGER SEAT TRACK AT RBL 45.5 BETWEEN BS 1117 AND BS 1138. THE CORRODED SEAT TRACK FROM BS 1110, AND BS 1138 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRACK PER B727 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1999012200619 19990122 00619 NM 1999 1 22 MZZA98283 1 19981117 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1075 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT BS 1075 , RBL 55. THE CORRODED SEAT TRACK FLANGE WAS CLEANED UP AND REPAIRED PER B727 SRM 53-10-5 FIGURE 9. (M) 2 L 7 3 4F A3WE 1999012200620 19990122 00620 NM 1999 1 22 MZZA98265 1 19981115 A 5313 655848825 STRINGER BOEING 727 727224 1384076 NM BS 948 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1.1 INCH LONG CRACK WAS FOND ON LEFT FUSELAGE STRINGER S-18A VE RTICAL FLANGE AT BS 948. THE DAMAGED STRINGER S-18A AFT BS 920 WAS TRIMMED OUT AND SPLICE REPAIRED WITH NEW SECTION OF S-18A PER EC/PA 5310-03793 DATED 01 DEC 1998. (M) 2 L 7 3 4F A3WE 1999012200621 19990122 00621 NM 1999 1 22 MZZA98266 1 19981116 A 5312 69648411 BULKHEAD PLATE BOEING 727 727224 1384076 NM BS 740 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DUIRNG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TG CORROSION WAS FOUND ON BS 740 BULKHEAD LOWER WIRING ACCESS H OLE REINFORCEMENT PLATE. THE CORRODED WIRING ACCESS HOLE REINFORCEMENT PLATE P/N 69-64841-1 WAS REMOVED AND REPLACED WI TH NEW REINFORCEMENT PLATE. (M) 2 L 7 3 4F A3WE 1999012200622 19990122 00622 NM 1999 1 22 MZZA98267 1 19981116 A 5730 65877033 SKIN BOEING 727 727224 1384076 NM WING BOX CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DUIRNG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON WING CENTER SECTION LOWER SKIN LOWER SURFACE BETWEEN S-4C AND S-5C AND BETWEEN RBBL 27 AND RBBL 30. THE CORRODED AREA WAS CLEAN UP AND REPAIRED PER B727 SRM 57-30-3 FIGURE 10. (M) 2 L 7 3 4F A3WE 1999012200623 19990122 00623 NM 1999 1 22 MZZA98268 1 19981119 A 5313 STRINGER BOEING 727 727224 1384076 NM BS 740 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPACTMENT STRINGE R S-27R AT BS 740. THE CORRODED STRINGER 5 INCH LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-3 FIGURE 1. (M) 2 L 7 3 4F A3WE 1999012200624 19990122 00624 NM 1999 1 22 MZZA98269 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1138 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON LEFT AFT LAVATORY PARTITION LOWER SUP PORT HAT CHANNEL AT BS 1138, LBL 24. THE CORRODED LAVATORY PARTITION LOWER SUPPORT HAT CHANNEL WAS REMOVED AND REPLACED WITH NEW HAT CHANNEL MADE FROM BAC1510-335 EXTRUSION. (M) 2 L 7 3 4F A3WE 1999012200625 19990122 00625 NM 1999 1 22 MZZA98270 1 19981117 A 5320 6531773 INTERCOSTAL BOEING 727 727224 1384076 NM BS 1176 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON BS 1176.9 REINFORCEMENT CHORD BETWEEN LB L40 AND LBL48. THE CORRODED REINFORCEMENT CHORD WAS CLEAN UP AND REPAIRED PER EC/RA 5310-01555 DATED 9-5-90. (M) 2 L 7 3 4F A3WE 1999012200626 19990122 00626 NM 1999 1 22 MZZA98271 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1138 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT ' T' ANGLE AT BS 1138, LBL 14. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE FLANGE 2 INCH LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1999012200627 19990122 00627 NM 1999 1 22 MZZA98272 1 19981117 A 5320 652427650 FITTING BOEING 727 727224 1384076 NM BS 1183 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASI, LG CORROSION WAS FOUND ON BS 1183 BULKHEAD S-17R FORWARD END FIT TING. THE CORRODED FORWARD END FITTING, P/N 65-24276-50 WAS REMOVED AND REPLACED WITH NEW END FITTING. (M) 2 L 7 3 4F A3WE 1999012200628 19990122 00628 NM 1999 1 22 MZZA98275 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1138 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT AFT LAVATORY PARTITION LOWER SU PPORT HAT CHANNEL AT BS 1138 BETWEEN RBL 27 AND RBL 52. THE CORRODED PARTITION LOWER SUPPORT HAT CHANNEL WAS REMOVED AN D REPLACED WITH NEW HAT CHANNEL. (M) 2 L 7 3 4F A3WE 1999012200629 19990122 00629 NM 1999 1 22 MZZA98276 1 19981117 A 5312 BULKHEAD WEB BOEING 727 727224 1384076 NM BS 1183 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON BS 1183 BULKHEAD FLOOR SHEAR WEB AT R BL 15. THE CORRODED WEB WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-2. (M) 2 L 7 3 4F A3WE 1999012200631 19990122 00631 NM 1999 1 22 MZZA98278 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 417 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER FLOOR PANEL SUPPORT 'T' ANG LE AT BS 417, RBL 47. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SUPPORT 'T' ANGLE MA DE FROM BAC1506-43. (M) 2 L 7 3 4F A3WE 1999012200632 19990122 00632 NM 1999 1 22 MZZA98279 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 414 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT ' T' ANGLE AT BS 414 RBL 40. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SUPPORT 'T' ANG LE MADE FROM BAC1506-43. (M) 2 L 7 3 4F A3WE 1999012200633 19990122 00633 NM 1999 1 22 MZZA98280 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 414 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT ' T' ANGLE AT BS 414 BETWEEN RBL 12 AND RBL 21. THE CORRODED FLOOR PANEL SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SUPPORT 'T' ANGLE MADE FROM BAC1506-43. (M) 2 L 7 3 4F A3WE 1999012200634 19990122 00634 NM 1999 1 22 MZZA98281 1 19981117 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 396-412 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION AS FOUND ON PASSENGER CABIN SEAT TRAC AT RBL 22.09 BETWEEN BS 396 AND BS 412. THE CORRODED SEAT TRACK FROM BS 380 TO BS 420 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TRA CK PER B727 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1999012200635 19990122 00635 NM 1999 1 22 MZZA98282 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 405-415 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR PANEL SUPPORT ' T' ANGLE AT RBL 12 BETWEEN BS 405 AND BS 415. THE CORRODED FLOOR SUPPORT 'T' ANGLE WAS REMOVED AND REPLACED WITH NEW SU PPORT 'T' ANGLE MADE FROM BAC1506-43. (M) 2 L 7 3 4F A3WE 1999012200636 19990122 00636 NM 1999 1 22 MZZA98284 1 19981117 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 1030-1090 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBL 24.75 BETWEEN BS 1030 AND BS 1070. THE CORRODED SEAT TRACK FROM BS 1030 TO BS 1090 WAS TRIMMED OUT AND INSTALLED REPLA CEMENT TRACK PER B727 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1999012200637 19990122 00637 NM 1999 1 22 MZZA98285 1 19981117 A 5320 SUPPORT BOEING 727 727224 1384076 NM BS 1033 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON AFT GALLEY FLOOR SUPPORT (HAT CHANNEL ) AT BS 1033, RBL 55. THE CORRODED FLOOR SUPPORT (HAT CHANNEL) WAS REMOVED AND REPLACED WITH NEW FLOOR SUPPORT HAT CHAN NEL MADE FROM BAC 1510335 2024-T3 MATERIAL. (M) 2 L 7 3 4F A3WE 1999012200638 19990122 00638 NM 1999 1 22 MZZA98286 1 19981122 A 5730 SKIN BOEING 727 727224 1384076 NM RT WING CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON RIGHT FUSELAGE SKIN AT WING SCANN ING LIGHT CUT OUT. THE CORRODED SKIN WAS CLEANUP AND REPAIRED PER B727 SRM 53-30-3 FIGURE 22. (M) 2 L 7 3 4F A3WE 1999012200639 19990122 00639 WP 1999 1 22 HALA9800431 1 19981230 A 3350 BATTERY DOUG DC9 DC951 3022051 WP CABIN DISCHARGED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 47764 HNL - FORWARD OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES, OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012200640 19990122 00640 EU 1999 1 22 DKAA98030 1 19981215 A 2612 1050B80045010 FIRE DETECTOR AMD FALC20 FALCON 2720302 EU LT ENGINE MALFUNCTIONED A DKAA A B E UNSCHED LANDING EMER. DESCENT ENGINE SHUTDOWN N FALSE WARNING CR CRUISE 1 GL 23 108R 108 NR 1 ENGINE FIRE WARNING, EMERGENCY DESCENT AND LANDING (TYS). CHECKED FOR BLEED AIR LEAKS AND SIGNS OF FIRE, FOUND NR 1 ENGINE FIRE LOOP SHORTED ON OIL TANK, REROUTED FIRE LOOP. OPERATIONAL CHECKS GOOD IAW AMD MM 26-11. AIRCRAFT RETURNE D TO SERVICE. (M) 2 L 7 2 4F A7EU 1999012200641 19990122 00641 EU 1999 1 22 AALA982226 1 19981217 A 3230 715441 VALVE FOKKER F28 F28MK0100 4990807 EU MLG MALFUNCTIONED A AALA K NONE J WARNING INDICATION DE DESCENT 1 SW 07 1467A 698H 11499 DFW - FLT 895 - EN ROUTE MCI-DFW - ON APPROACH TO DFW WHEN GEAR HANDLE WAS LOWERED AT 2,000 FEET, THE NOSE GEAR CAME LOW ERED BUT BOTH MAIN LANDING GEARS DID NOT. LEVEL 3 WARNING ILLUMINATED BELOW 1,000 FEET. RAISED GEAR HANDLE AND NOSE GE AR RETRACTED. LOWERED GEAR HANDLE WHILE EXECUTING GO-AROUND AND ALL THREE GEARS CAME DOWN WITH THREE LIGHTS ILLUMINATED . LANDED DFW WITHOUT INCIDENT. REPLACED MAIN LANDING GEAR SELECTOR VALVE. ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999012200642 19990122 00642 WP 1999 1 22 AALA982228 1 19981220 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 427AA 49339 ORD - DURING OVERNIGHT MAINTENANCE, FOUND THE RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPAIRED BROKEN WIRE. GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200643 19990122 00643 EU 1999 1 22 AALA982231 1 19981225 A 3230 A11345403 STOP FOKKER F28 F28MK0100 4990807 EU LT MLG OUT OF ADJUST A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1460A 11480 ORD - FLT 1782 - AFTER TAKEOFF ORD LEFT MAIN LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR THREE TIMES WITH SAME RESULTS. RETURNED AND LANDED ORD WITHOUT INCIDENT. ADJUSTED UPLOCK BRACKET STOP, INSTALLED NEW LOCK-TANG AND SAFETY TIED PER M M. RETRACTED GEAR SEVERAL TIMES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999012200644 19990122 00644 EU 1999 1 22 AALA982229 1 19981220 A 2910 224D4418501 LINE AIRBUS 300 A300B4605R 3930308 EU NR 2 ENGINE LEAKING A AALA K NONE K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 40064 507 ORD - FLT 1522 - EN ROUTE MIA-ORD - DURING CRUISE, THE GREEN RESERVOIR HYDRAULIC LEVEL DROPPED TO MINIMUM. LANDING GEAR WAS LOWERED USING GRAVITY EXTENSION METHOD. LANDED ORD WITHOUT INCIDENT. REPLACED NR 2 ENGINE PRESSURE LINE AND BOTH ENGINE CASE DRAIN FILTERS FOR THE GREEN HYDRAULIC SYSTEM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1999012200645 19990122 00645 WP 1999 1 22 AALA982241 1 19981224 A 3350 72C06349 SIGN DOUG DC9 DC982 3022082 WP CABIN MISSING A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 223AA 49173 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT SIGN ON FORWARD SIDE OF CLASS DIVIDER IS MISSING REFERENCE CARD 0801. INSTALLED EMERGENCY EXIT SIGN ON FORWARD SIDE OF CLASS DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200646 19990122 00646 WP 1999 1 22 AALA982233 1 19981223 A 3397 WIRE DOUG DC9 DC982 3022082 WP TAIL CONE LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 417AA 49328 DFW - DURING OVERNIGHT MAINTENANCE, TAIL CONE RELEASE HANDLE EMERGENCY EXIT LIGHT INOPERATIVE. TIGHTENED LOOSE TERMINAL AND GROUND WIRES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200647 19990122 00647 WP 1999 1 22 AALA982234 1 19981223 A 3350 LIGHT DOUG DC9 DC982 3022082 WP ROW 19 INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 416AA 49327 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT ROW 19 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP SECTION AT SEAT ROW 19. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200648 19990122 00648 WP 1999 1 22 AALA982238 1 19981225 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7506 49800 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PA TH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200649 19990122 00649 NM 1999 1 22 AALA982240 1 19981224 A 3233 273T62004 ACTUATOR BOEING 767 767323 1385205 NM LT MLG MALFUNCTIONED A AALA O OTHER J WARNING INDICATION CL CLIMB 1 SW 07 7375A 25202 DFW - FLT 964 - AFTER TAKEOFF GRU, RAISED GEAR HANDLE AND RECEIVED GEAR DISAGREE MESSAGE ON EICAS. LOWERED HANDLE AND N OSE AND RIGHT MLG LIGHTS ILLUMINATED. RAISED GEAR HANDLE RECEIVED SAME INDICATIONS AS AFTER TAKEOFF. AFTER ABOUT 2 MIN UTES LEFT MAIN GEAR INDICATED DOWN AND LOCKED. PUT GEAR HANDLE DOWN, GOT 3 GREEN LIGHTS. RAISED HANDLE AND RECEIVED NO RMAL INDICATIONS. CONTINUED FLIGHT AND LANDED DFW WITHOUT INCIDENT. REPLACED LEFT SIDE BRACE LOCK ACTUATOR AND MAIN TR UCK POSITIONER ACTUATOR. PERFORMED GEAR RETRACTION FIVE TIMES. ACCOMPLISHED LEAK CHECK AND PERFORMED PSEU BITE TEST. S YSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999012200650 19990122 00650 WP 1999 1 22 AALA982220 1 19981215 A 4990 1945189004 CAP DOUG DC9 DC982 3022082 WP APU LEAKING A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 SW 07 7508 P80204 49802 DFW - FLT 1684 - DURING TAKEOFF, FLIGHT CREW NOTICED SMOKE IN THE CABIN. FLIGHT AIR INTERRUPTED AND RETURNED TO DFW WIT HOUT FURTHER INCIDENT. UPON LANDING, SMOKE DISSIPATED FROM THE CABIN. MAINTENANCE FOUND THE APU OIL TANK FILLER CAP LE AKING OIL. REPLACED APU OIL TANK FILLER CAP, COALESCER BAGS AND RAN WITH PACKS ON WITH NO LEAKS OR SMELL NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200651 19990122 00651 NM 1999 1 22 AALA984267 1 19981216 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 287 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 306AA 22312 AFW - FLOORBEAM AT STATION 287 RBL 55 HAD CORROSION BLENDED ON AFT FLANGE. FABRICATE STRAP, ALODINED ALLUMINUM SURFACES . FINISH BLEND AND REPAIR PARTS WITH PRIMER. INSTALL STRAP WET WITH SEALANT. (M) 2 L 7 2 4F RT A1NM 1999012200652 19990122 00652 NM 1999 1 22 AALA984266 1 19981228 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 306AA 22312 AFW - FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL. ALODINE ALL BARE ALUMINUM SURFACES. FINISH BLENDED AREAS WITH 2 COATS PRIMER. FILL WITH BMS5-95. (M) 2 L 7 2 4F RT A1NM 1999012200653 19990122 00653 NM 1999 1 22 AALA984265 1 19981216 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 347 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 306AA 22312 AFW - FLOORBEAM AT STATION 347 HAD CORROSION BLENDED. FABRICATE REPAIR STRAP. ALODINE ALL BARE ALUMINUM SURFACES. FIN ISH BLENDS AND REPAIR PARTS WITH 2 COATS PRIMER. FILL BLENDS WITH BMS5-92. INSTALL STRAP WET WITH SEALANT. (M) 2 L 7 2 4F RT A1NM 1999012200654 19990122 00654 NM 1999 1 22 AALA984264 1 19981217 A 5320 BEAM BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 306AA 22312 AFW - FOUND AREAS ON BEAM CORRODED. REMOVED ALL CORROSION. ALODINE AND APPLY 2 COATS PRIMER. FILL BLENDS WITH SEALANT . FABRICATE REPAIR STRAP. INSTALL STRAP. (M) 2 L 7 2 4F RT A1NM 1999012200655 19990122 00655 NM 1999 1 22 AALA984263 1 19981216 A 5311 FRAME BOEING 767 767223 1385123 NM BS 610 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 306AA 22312 AFW - FUSELAGE FRAME AT STATION 610, J-CAP HAS CORROSION REMOVAL ON LOWER SURFACE. BLENDOUT, CORROSION ENSURE NO CRACKS ALODINE AND APPLY 2 COATS PRIMED. FILL WITH SEALANT. (M) 2 L 7 2 4F RT A1NM 1999012200656 19990122 00656 NM 1999 1 22 AALA984262 1 19981217 A 5311 FRAME BOEING 767 767223 1385123 NM BS 478 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 306AA 22312 AFW - FUSELAGE FRAME J-CAP AT STATION 478 HAS GOUGE. BLENDOUT CORROSION. VISUALLY INSPECT TO ENSURE NO CRACKS AT BLEND ED AREA. ALODINE AND APPLY 2 COATS PRIMER. (M) 2 L 7 2 4F RT A1NM 1999012200657 19990122 00657 NM 1999 1 22 AALA984261 1 19981217 A 5311 FRAME BOEING 767 767223 1385123 NM BS 676 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 306AA 22312 AFW - FORWARD CARGO FRAME T-CAP AT STATION 676 LBL 20 HAD CORROSION BLENDED ON TOP AND BOTTOM SURFACES. BLEND OUT ALL C ORROSION AND FINISH THE BLENDED AREA. FABRICATE A REPAIR ANGLE. (M) 2 L 7 2 4F RT A1NM 1999012200658 19990122 00658 NM 1999 1 22 USAASB98329 1 19981217 A 2433 2299 TRU BOEING 737 7374B7 1384702 NM E/E BAY MALFUNCTIONED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 779AU 22714 24996 LGA - FLT 1585 - FLIGHT DIVERTED TO LGA DUE TO AN ODOR IN THE AIRCRAFT WHICH STARTED IN THE MID CABIN, THEN TO THE AFT C ABIN, THEN THE ENTIRE CABIN. NO VISIBLE SMOKE WAS ASSOCIATED WITH EYE BURNING SENSATION. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 AND NR 3 TRU'S WITH EVIDENCE OF OVERHEAT CONDITION AND OVERHEAT ODOR. REPLACED T HE NR 2 AND NR 3 TRU'S. OPS CHECK GOOD. ALSO, FOUND THE FORWARD GALLEY OVEN WITH BURNED ITEM ON HEATING ELEMENT. REPL ACED OVEN (P/N 2510-0007-03). OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012200659 19990122 00659 NM 1999 1 22 AALA982011 1 19981210 A 5330 SKIN BOEING 727 727223 1384074 NM BS 260-380 SCRATCHED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - SCRATCHES IN SKIN STATION 360 TO 380 STRINGER 22R TO 24R. REMOVED AND REPLACED SKIN STATION 360-440 RIGHT BELOW S TRINGER 22 PER SRM 53-30-3 FIG 16A. (M) 2 L 7 3 4F A3WE 1999012200660 19990122 00660 NM 1999 1 22 USAA980635 1 19981217 A 5320 65479576 WEB BOEING 737 7373B7 1384580 NM BS 790-847 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION SURROUNDING NUTPLATE HOLES 1 INCH BY 57 INCH FROM BS 790 TO 847 RBL 20 WEB. CORROSION TASK NR 53-202-01. INSTALLED NEW WEB AND FILLER PER SRM 51-30-01. (M) 2 L 7 2 4F RT A16WE 1999012200661 19990122 00661 NM 1999 1 22 USAA980633 1 19981217 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK STATION 520, LBL 24.75, WL 207 FLOORBEAM. INSTALLED DOUBLER PER EA 63061. (M) 2 L 7 2 4F RT A16WE 1999012200662 19990122 00662 NM 1999 1 22 USAA980632 1 19981217 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1.625 INCH CRACK STATION 520, RBL 45, WL 207 FLOORBEAM. INSTALLED D OUBLER PER EA 63061. (M) 2 L 7 2 4F RT A16WE 1999012200663 19990122 00663 NM 1999 1 22 USAA980631 1 19981217 A 5315 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520, LBL 45, WL 207 FLOORBEAM. INSTALLED DOUBL ER PER EA 63061. (M) 2 L 7 2 4F RT A16WE 1999012200664 19990122 00664 NM 1999 1 22 USAA980630 1 19981217 A 5315 654680367 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1.4 INCH CRACK STATION 520, RBL 25, WL 207 FLOORBEAM. INSTALLED DOU BLER PER EA 63061. (M) 2 L 7 2 4F RT A16WE 1999012200665 19990122 00665 NM 1999 1 22 USAA980629 1 19981217 A 5210 50794517 SKIN BOEING 737 7373B7 1384580 NM PASSENGER DOOR CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK FORWARD ENTRY DOOR INNER SKIN. INSTALLED DOUBLER PER E A 63053. (M) 2 L 7 2 4F RT A16WE 1999012200666 19990122 00666 NM 1999 1 22 USAA980624 1 19981218 A 5320 6545409245 WEB BOEING 737 7373B7 1384580 NM MLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK MLG WHEEL WELL LBL 30 WEB PANEL. INSTALLED WEB AND STI FFENER PER EA 63025 AND SRM 53-60-51. (M) 2 L 7 2 4F RT A16WE 1999012200667 19990122 00667 NM 1999 1 22 USAA980623 1 19981218 A 5311 65465551 FRAME BOEING 737 7373B7 1384580 NM BS 867 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 867, 1 INCH ABOVE S 9R FRAME. INSTALLED DOUBLER AND FILLER PLUG PER SRM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999012200668 19990122 00668 NM 1999 1 22 USAA980622 1 19981218 A 5311 65465297 FRAME BOEING 737 7373B7 1384580 NM BS 440 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 440, 1 INCH ABOVE S 9R FRAME WEB. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999012200669 19990122 00669 NM 1999 1 22 USAA980621 1 19981218 A 5311 65465323 FRAME BOEING 737 7373B7 1384580 NM BS 480 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 480, 1 INCH ABOVE S 9L FRAME WEB. INSTALLED DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999012200670 19990122 00670 NM 1999 1 22 USAA980620 1 19981218 A 5311 65465251 FRAME BOEING 737 7373B7 1384580 NM BS 380 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 380, 1 INCH ABOVE S 9R FRAME WEB. FABRICATED A FILL ER AND DOUBLER PER SRM 53-00-07. (M) 2 L 7 2 4F RT A16WE 1999012200671 19990122 00671 NM 1999 1 22 USAA980619 1 19981218 A 5311 65465511 FRAME BOEING 737 7373B7 1384580 NM BS 807 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 807, S 9L FRAME. INSTALLED FILLER AND DOUBLER PER S RM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999012200672 19990122 00672 NM 1999 1 22 USAA980618 1 19981218 A 5311 65465581 FRAME BOEING 737 7373B7 1384580 NM BS 907 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 907, S 9L FRAME. INSTALLED FILLER AND DOUBLER PER S RM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999012200673 19990122 00673 NM 1999 1 22 USAA980617 1 19981218 A 5320 651768470 ANGLE BOEING 737 7373B7 1384580 NM NLG WW CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK NOSE WHEEL WELL, NOSE GEAR ACTUATOR SUPPORT STRUCTURE ANG LE. REPLACED GUSSET AND ACTUATOR MOUNT PER BOEING DRAWING 65-45819. (M) 2 L 7 2 4F RT A16WE 1999012200674 19990122 00674 NM 1999 1 22 USAA980616 1 19981218 A 5311 65465571 FRAME BOEING 737 7373B7 1384580 NM BS 887 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 887, S 9R FRAME. INSTALLED FILLER AND DOUBLER PER S RM 53-00-07 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999012200675 19990122 00675 NM 1999 1 22 USAA980660 1 19981223 A 5330 SKIN BOEING 737 737301 1384611 NM BS 375 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 337US 23235 TPA - DURING A CX-2 CHECK VISUAL INSPECTION, FOUND A .3125 INCH CRACK IN SKIN AT BS 375 AND BL 0. INSTALLED DOUBLER PER TR 53-30-07. (M) 2 L 7 2 4F RT A16WE 1999012200676 19990122 00676 NM 1999 1 22 USAA980647 1 19981218 A 5315 654681143 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 986 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37297 23318 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND SURFACE CORROSION UNDER SIDE FLOORBEAM STATION 986 LBL 3. CORROSION T ASK NR C 53-107-02. INSTALLED 'T' CAP PER SRM 53-00-51 FIG 202. (M) 2 L 7 2 4F RT A16WE 1999012200677 19990122 00677 NM 1999 1 22 USAA980646 1 19981217 A 5320 6548607182 ANGLE BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520 STRINGER 7R FUSELAGE ANGLE EXTERIOR. INSTALL ED DOUBLER PER TR 53-50-03. (M) 2 L 7 2 4F RT A16WE 1999012200678 19990122 00678 NM 1999 1 22 USAA980645 1 19981217 A 5320 6548607181 ANGLE BOEING 737 7373B7 1384580 NM BS 520 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK STATION 520 STRINGER 7L FUSELAGE ANGLE EXTERIOR. INSTALL ED DOUBLER PER TR 53-50-03. (M) 2 L 7 2 4F RT A16WE 1999012200679 19990122 00679 NM 1999 1 22 USAA980642 1 19981217 A 5320 6545808582 WEB BOEING 737 7373B7 1384580 NM BS 294 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 1.25 INCH CRACK STATION 294 WL 209 RBL 56 WEB. INSTALLED DOUBLER PER BO EING 737-300 SRM 51-70-11. (M) 2 L 7 2 4F RT A16WE 1999012200680 19990122 00680 NM 1999 1 22 USAA980641 1 19981218 A 5311 65465691 FRAME BOEING 737 7373B7 1384580 NM BS 1040 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37297 23318 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH HOLE IN FRAME/APU BLEED DUCT STATION 1040. INSTALLED REPAIR DOUBLER PER EA 63138 AND TR 53-80-02. (M) 2 L 7 2 4F RT A16WE 1999012200681 19990122 00681 NM 1999 1 22 USAA980640 1 19981218 A 5315 6546568148 FLOORBEAM BOEING 737 7373B7 1384580 NM BS 1016 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37297 23318 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION 88 INCH BY 1 INCH BS 1016 RBL 6 FLOORBEAM, CORROSION TASK NR C53-107-02. T-CAP FLOORBEAM REPLACED PER TR 53-10-05. (M) 2 L 7 2 4F RT A16WE 1999012200682 19990122 00682 NM 1999 1 22 USAA980639 1 19981218 A 5311 6546547 FRAME BOEING 737 7373B7 1384580 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37297 23318 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK BS 727 STRINGER 14L FRAME WEB. INSTALLED FILLER AND DOUBLER PER EA 63060. (M) 2 L 7 2 4F RT A16WE 1999012200683 19990122 00683 NM 1999 1 22 USAA980638 1 19981218 A 5320 ANGLE BOEING 737 7373B7 1384580 NM BS 222 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37297 23318 CLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION ON SURFACE STATION 222 RT 27 INCH ABOVE FLOORLINE ANGLE. CO RROSION TASK NR C53-101-01. REMOVED SURFACE CORROSION PER SRM 51-10-6. (M) 2 L 7 2 4F RT A16WE 1999012200684 19990122 00684 NM 1999 1 22 USAA980607 1 19981218 A 5320 CLIP BOEING 737 7373B7 1384580 NM BS 639 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 639 STRINGER 4L STRINGER TIE CLIP. INSTALLED P ART PER SRM 51-10-2. (M) 2 L 7 2 4F RT A16WE 1999012200685 19990122 00685 NE 1999 1 22 USAAD98216 2 19981216 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D7B 52053 NE RIGHT FAILED A USAA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 EA 19 970VJ 28373 47050 657362 LGA-CMH - FLT 1833 - DURING CRUISE, THE RIGHT ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. THE CREW FOLLOWED THE ABNORMA L PROCEDURES BUT THE LIGHT REMAINED ON. THE OIL TEMPERATURE WAS RISING AND THE OIL QUANTITY DECREASING. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL SHAVINGS IN THE FILTER . THE ENGINE WAS REPLACED. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999012200686 19990122 00686 NM 1999 1 22 USAASB98337 1 19981223 A 3350 20121 CHARGER BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 374US 22953 CLT - THE LEFT AFT ENTRY DOOR FUSELAGE MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND CHARGER. (M) 2 L 7 2 4F RT A16WE 1999012200687 19990122 00687 NM 1999 1 22 99ZZZM32 1 19981223 A 3350 BR9279108 LIGHT BOEING 737 7373B7 1384580 NM CABIN FAILED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 374US 22953 CLT - THE LEFT AFT ENTRY DOOR FUSELAGE MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSY AND CHARGER. (M) 2 L 7 2 4F RT A16WE 1999012200688 19990122 00688 NM 1999 1 22 USAASB98336 1 19981220 A 3350 LIGHT BOEING 737 7372B7 1384560 NM ROW 13 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 287AU 23134 BWI - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 13 INOPERATIVE. MAINTENANCE REPAIRED WIRING BENEATH SEAT A SSEMBLY AT ROW 13. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999012200689 19990122 00689 NM 1999 1 22 USAASB98335 1 19981220 A 3350 BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 562AU 23550 CLT - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT INOPERATIVE ABOVE THE AFT SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012200690 19990122 00690 NM 1999 1 22 99ZZZM33 1 19981220 A 3350 CHARGER BOEING 737 737301 1384611 NM CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 562AU 23550 CLT - DURING OVERNIGHT CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT INOPERATIVE ABOVE THE AFT SERVICE DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012200691 19990122 00691 WP 1999 1 22 USAAD98215 1 19981207 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 955VJ 47593 DTW - THE MAIN ENTRY AND GALLEY SERVICE DOOR ESCAPE SLIDE LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES FOR THE M AIN ENTRY AND GALLEY SERVICE DOOR ESCAPE SLIDE LIGHTS. (M) 2 L 7 2 4F A6WE 1999012200692 19990122 00692 WP 1999 1 22 USAAD98219 1 19981219 A 3350 20131ALB BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 970VJ 47050 PHL - THE FIRST CLASS SECTION FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE FIRST CLASS FLOOR EMERG ENCY LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999012200693 19990122 00693 EU 1999 1 22 USAAF98096 1 19981217 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU COCKPIT FAILED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 896US 11391 LGA - FLT 464 - ON APPROACH, CREW DID NOT RECEIVE THE GREEN LGIHT ON THE LEFT MAIN LANDING GEAR. CREW CYCLED THE GEAR W ITH SAME RESULT. CREW COMPLETED HANDBOOK PROCEDURE AND CONSIDERED GEAR DOWN AND LOCKED. FLIGHT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND AND REPLACED A BURNED OUT LIGHT BULB. (M) 2 L 7 2 4F RT 1999012200694 19990122 00694 NM 1999 1 22 USAASB98334 1 19981218 A 3350 20121 BATTERY CHARGER BOEING 737 7373B7 1384580 NM PASSENGER DOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 374US 22953 CLT - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED TH E LIGHT ASSEMBLY AND THE BATTERY CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012200695 19990122 00695 NM 1999 1 22 99ZZZM34 1 19981218 A 3350 30043229 LIGHT BOEING 737 7373B7 1384580 NM PASSENGER DOR INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 374US 22953 CLT - MAINTENANCE FOUND THE LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE REMOVED AND REPLACED TH E LIGHT ASSEMBLY AND THE BATTERY CHARGER. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012200696 19990122 00696 NM 1999 1 22 USAASB98324 1 19981211 A 2420 6130200502 HARNESS BOEING 737 737401 1384701 NM NR 2 ENGINE FAILED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CR CRUISE 1 EA 19 419US 23986 RIC - FLT 1475 - EN ROUTE PHL-CLT, THR NR 2 GENERATOR TRIPPED. THE APU GENERATOR SYSTEM WAS ON MEL. FLIGHT DIVERTED TO RIC AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE GENERATOR FEEDER WIRE PINS BURNED AT THE FI REWALL CONNECTOR D410 AND D3026. THE GENERATOR HARNESS ON THE ENGINE IS ALSO VERY TIGHT AND HAS A SIDE LOAD ON THE FIRE WALL CONNECTOR. REPLACED HARNESS FROM FIREWALL CONNECTOR D410 TO NR 2 ENGINE GENERATOR. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012200697 19990122 00697 NM 1999 1 22 TSAA9879655 1 19981226 A 7930 42D107A1 SWITCH BOEING 737 73725A 1384481 NM NR 2 ENGINE CONTAMINATED A TSAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 13 819AL 23791 FLT 404 - HNL-ITO - NR 2 ENGINE OIL FILTER BYPASS ILLUMINATED IN FLIGHT. SHUTDOWN ENGINE PER QRH. DECLARED EMERGENCY A ND MADE UNEVENTFUL LANDING IN KAHALUI (OGG). REMOVED AND REPLACED OIL FILTER SCREEN AND OIL PRESSURE BYPASS SWITCH. LE AK CHECK AND POWER RUN CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012200698 19990122 00698 NM 1999 1 22 TSAA9833647 1 19981219 A 3350 963100211 LIGHT BOEING 737 737282 13844AT NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 824AL 23045 REPLACED NR 5 POSITION FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOP. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012200699 19990122 00699 NM 1999 1 22 TSAA9833648 1 19981219 A 3350 1619 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 808AL 23445 REPLACED BOTH LAMPS AT AFT ENTRY DOOR AND AFT SERVICE DOOR SLIDE LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999012200700 19990122 00700 NM 1999 1 22 TSAA9833649 1 19981219 A 3350 86210066 BATTERY BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE O OTHER IN INSP/MAINT 1 WP 13 823AL 23154 REPLACED BATTERY PACKS AT POSITION NR 5 AND NR 6 FLOOR PROXIMITY LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012200701 19990122 00701 NM 1999 1 22 TSAA9833646 1 19981217 A 3350 8731002511 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED FORWARD PASSENGER DOOR EMERGENCY EXIT IDENTIFIER DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVI CE. (M) 2 L 7 2 4F RT A16WE 1999012200702 19990122 00702 NM 1999 1 22 TSAA9833651 1 19981225 A 3350 86210066 BATTERY PACK BOEING 737 7372S5C 1384499 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 802AL 22148 REPLACED NR 2 POSITION EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO BEING INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012200703 19990122 00703 1999 1 22 RAIA981232 3 19981230 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 CE 03 435AM 2523 889 FLT 7470 - STL - LEFT BETA LIGHT ILLUMINATED ON TAKEOFF. MAINTENANCE REPLACED LEFT BETA SWITCH. (M) 2 L 7 2 4T RT A56EU 1999012200704 19990122 00704 EU 1999 1 22 RAIA981231 1 19981229 A 6123 7827311 SOLENOID AEROSP ATR42 ATR42300 8680920 EU RT PROP FEATHER FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 422TE 106 FLT 7154 - STL - NO ARM LIGHT ON ATPCS. MAINTENANCE REPLACED RIGHT PROP FEATHER SOLENOID. (M) 2 H 7 2 4T RT A53EU 1999012200705 19990122 00705 EU 1999 1 22 RAIA981228 1 19981223 A 3222 105A703056A STRUT BAG JETSTM JETSTM3201 1500217 EU NLG DAMAGED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 425AM 870 FLT 7051 - BRL - LANDING GEAR WOULD NOT RETRACT. MAINTENANCE REPACKED NOSE STRUT. (M) 2 L 7 2 4T RT A56EU 1999012200706 19990122 00706 EU 1999 1 22 RAIA981218 1 19981222 A 7920 31050192 MANIFOLD JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 560HK 41076 FLT 7744 - DCA - RIGHT ENGINE OIL PRESSURE FLUCTUATING. MAINTENANCE REPLACED RIGHT ENGINE OIL FILTER MANIFOLD ASSY. (M ) 2 L 7 2 4T RT A41NM 1999012200707 19990122 00707 EU 1999 1 22 RAIA981215 1 19981218 A 7712 P323A702561SA1E CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 03 562HK 41078 FLT 7570 - JFK - LEFT ENGINE TORQUE INDICATION FLUCTUATING. MAINTENANCE REPLACED LEFT ENGINE IEC CANNON PLUG. (M) 2 L 7 2 4T RT A41NM 1999012200708 19990122 00708 EU 1999 1 22 RAIA981214 1 19981218 A 6120 31055863 MONOPOLE JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 557HK 41074 FLT 7633 - JFK - RIGHT ENGINE RPM FLUCTUATING. A/C DIVERTED TO BGM. MAINTENANCE REPLACED RIGHT ENGINE RPM MONOPOLE. ( M) 2 L 7 2 4T RT A41NM 1999012200709 19990122 00709 1999 1 22 RAIA981235 3 19981231 A 6140 8659566 BETA SWITCH BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 435AM 889 FLT 7470 - STL - LEFT BETA LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT BETA SWITCH. (M) 2 L 7 2 4T RT A56EU 1999012200710 19990122 00710 EU 1999 1 22 RAIA981233 1 19981230 A 2612 51224127 FIRE LOOP BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA C ABORTED TAKEOFF N FALSE WARNING TO TAKEOFF 1 CE 03 342TE 954 FLT 7031 - STL - RT FIRE DETECT LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT ENGINE FIRE LOOP. (M) 2 L 7 2 4T RT A56EU 1999012200713 19990122 00713 EU 1999 1 22 RAIA981217 1 19981217 A 3010 3D2372222 VALVE BAG JETSTM JETSTM3201 1500217 EU LEFT FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 337TE 929 FLT 7446 - STL - WING AND TAIL DEICE INOP. MAINTENANCE REPLACED LEFT DEICE PRESSURE REGULATING VALVE. (M) 2 L 7 2 4T RT A56EU 1999012200714 19990122 00714 EU 1999 1 22 RAIA981230 1 19981216 A 3010 3D2372222 VALVE BAG JETSTM JETSTM3201 1500217 EU RIGHT FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 337TE 929 FLT 7446 - STL - WING AND TAIL DEICE INOPERATIVE. MAINTENANCE REPLACED RIGHT DEICE PRESSURE REGULATING VALVE. (M) 2 L 7 2 4T RT A56EU 1999012200715 19990122 00715 WP 1999 1 22 ORJA98321 1 19981201 A 3350 60030451 BATTERY PACK DOUG DC9 DC987 3022087 WP ROWS 19-22 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 754RA 49641 AT RENO, CABIN EVACUATION LIGHTS AT ROWS 19-22 ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED EMERGENCY BATTERY PACK A T RIGHT AFT OVERWING DOOR. ALSO, CHECKED POWER TO BATTERY PACK, POWER OK. REPAIRED WIRES AT ROWS 21 AND 22. EMERGENCY LIGHT SYSTEM OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012200716 19990122 00716 WP 1999 1 22 ORJA98320 1 19981219 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 833RA 53045 IN RNO - A SECTION OF EMERGENCY LIGHTS IN CABIN ILLUMINATED FOR SEVERAL MINUTES IN FLIGHT. REMOVED AND REPAIRED LIGHT B ATTERY PACK, OPS CHECK NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012200717 19990122 00717 NM 1999 1 22 AALA984259 1 19981214 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 1480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 313AA 22316 AFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION, ALODINE AND PRIMED ALL B LENDS AND REPAIR PARTS WITH 2 COATS BMS 10-11 PRIMED. FILLED BLENDS WITH BMS 5-95 SEALANT. INSTALLED 301 1/2H STAINLES S STEEL STRAP WET WITH BMS5-95 SEALANT. (M) 2 L 7 2 4F RT A1NM 1999012200718 19990122 00718 WP 1999 1 22 AALA982244 1 19981229 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY CONTAMINATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 493AA 49731 DFW - 493 - AFTER TAKEOFF LGA, EN ROUTE DFW CREW SMELLED HOT ODOR FROM AIR CONDITIONING SYSTEM. FLIGHT ATTENDANTS REPOR TED SMOKE IN COACH CABIN. FIRST CLASS CABIN HAD AN ODOR BUT NO SMOKE. SMOKE AND ODOR DISSIPATED ONCE AIRCRAFT CLEARED 11,000 FT. CONTINUED ON TO DFW AND LANDED WITHOUT INCIDENT. ACCOMPLISHED AIRCRAFT PACK AND HIGH PRESSURE PNEUMATIC DUC T BURN-OUT. NO ODOR OR SMOKE DETECTED. REPLACED WATER SEPARATOR COALESCER BAGS. SYSTEM GROUND CHECKED NORMAL OPERATIO N. (M) 2 L 7 2 4F A6WE 1999012200719 19990122 00719 WP 1999 1 22 AALA982215 1 19981211 A 2170 21D101 COALESCER DOUG DC9 DC982 3022082 WP ACM BAY CONTAMINATED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 452AA 49553 BOS - FLT 16 - AFTER TAKEOFF A SMOKEY ODOR WAS DETECTED IN THE FORWARD CABIN WITH NO ABNORMAL INDICATIONS. ODOR DISSIPA TED AFTER SEVERAL MINUTES AND AIRCRAFT CONTINUED AND LANDED BOS WITHOUT FURTHER INCIDENT. REPLACED BOTH AIR CYCLE MACHI NE COALESCER BAGS. ACCOMPLISHED PACK BURNOUT PROCEDURE WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200720 19990122 00720 WP 1999 1 22 AALA982155 1 19981209 A 5320 MOUNT DOUG DC9 DC982 3022082 WP BS 210 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 441AA 49460 TUL - INBOARD FORWARD NR 2 GALLEY MOUNT CORRODED. INSTALLED NEW GALLEY MOUNT PER STANDARD PRACTICE 51-00. (M) 2 L 7 2 4F A6WE 1999012200721 19990122 00721 WP 1999 1 22 AALA982156 1 19981209 A 5320 SUPPORT DOUG DC9 DC982 3022082 WP BS 218 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 441AA 49460 TUL - FOUND INBOARD AFT NR 2 GALLEY MOUNT CORRODED. INSTALLED NEW INBOARD AFT UPPER G2 GALLEY MOUNT PER STANDARD PRACTI CE 51-00. (M) 2 L 7 2 4F A6WE 1999012200722 19990122 00722 WP 1999 1 22 AALA982157 1 19981209 A 5347 TRACK DOUG DC9 DC982 3022082 WP BS 1155-1221 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 441AA 49460 TUL - FOUND CORROSION AROUND T/O TRACK MOUNT HOLES. REPLACED SECTION OF SEAT TRACK PER STANDARD PRACTICE 51-00. (M) 2 L 7 2 4F A6WE 1999012200723 19990122 00723 WP 1999 1 22 HALA9800398 1 19981122 A 8012 VALVE DOUG DC10 DC1010 3022110 WP NR 3 ENGINE FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 153AA 46708 TUL - FLT 4103 - START VALVE ILLUMINATED INFLIGHT ON NR 3 ENGINE. A/C RETURNED TO TUL, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED AND REPLACED NR 3 ENGINE START VALVE ASSY. LEAK AND OPS CHECK OK. REPLACED START VALVE INDICATING WIRIN G. OPS CHECK OK. (M) 2 L 7 3 4F A22WE 1999012200724 19990122 00724 WP 1999 1 22 HALA9800416 1 19981216 A 3260 BULB DOUG DC10 DC1010 3022110 WP COCKPIT FAILED A HALA L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 WP 13 122AA 46522 FLT 1 - HNL - LEFT GEAR GREEN LIGHT DOES NOT ILLUMINATE WITH GEAR HANDLE DOWN. A/C DID A FLYBY, BY THE TOWER TO CONFIRM THAT THE LANDING GEAR WAS DOWN. A/C DID A FLYBY, BY THE TOWER TO CONFIRM THAT THE LANDING GEAR WAS DOWN. A/C MADE AN UNEVENTFUL LANDING AT HNL. FOUND LEFT MAIN LANDING GEAR DOWN LIGHT BULBS BURNED. REPLACED BULBS, OPS CHECK OK. PERFOR MED BITE OF PROX BOX OK. CHECKED CONDITION AND SECURITY OF LEFT MLG SWITCHES, OK. (M) 2 L 7 3 4F A22WE 1999012200725 19990122 00725 WP 1999 1 22 HALA9800413 1 19981217 A 2150 SEAL DOUG DC9 DC951 3022051 WP LT PACK LEAKING A HALA A UNSCHED LANDING K M FLUID LOSS OVER TEMP CL CLIMB 1 WP 13 603DC 47784 FLT 529 - OGG - TAIL COMPARTMENT TEMP HIGH LIGHT CAME ON, JUST AFTER LIFT OFF. A/C RETURNED TO OGG WHERE IT MADE AN UNE VENTFUL LANDING. FOUND LT PACK SEAL LEAKING. REPLACED SEAL AND HI POWER RUN, CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999012200726 19990122 00726 WP 1999 1 22 HALA9800408 1 19981210 A 2830 VALVE DOUG DC10 DC1010 3022110 WP RT FUEL DUMP FAILED A HALA A UNSCHED LANDING O OTHER CR CRUISE 1 WP 13 125AA 46525 FLT NR 1 - LAX - RIGHT DUMP VALVE DID NOT OPEN DURING DUMP OPERATION. COMPLIED WITH AFM AND VALVE DID NOT OPEN. AIRCRA FT HAD ABORTED FLIGHT WITH STRONG ODOR IN CABIN AND COCKPIT. CHECKED AND REPLACED RIGHT FUEL DUMP VALVE ACT. ACCOMPLIS HED REQUIRED GROUND OPS CHECK, AS PER MM. RIGHT F/DUMP VALVE GROUND OPS CHECK NORMAL. (M) 2 L 7 3 4F A22WE 1999012200727 19990122 00727 EU 1999 1 22 RAIA981222 1 19981225 A 6120 PROP GOVERNOR JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE OUT OF ADJUST A RAIA A UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 CE 03 568HK 41086 FLT 7754 - ORF - RIGHT ENGINE RPM ERRATIC, SHUTDOWN RIGHT ENGINE. MAINTENANCE ADJUSTED PROP GOVERNOR. (M) 2 L 7 2 4T RT A41NM 1999012200728 19990122 00728 EU 1999 1 22 RAIA981223 1 19981226 A 2612 FIRE LOOP JETAIR JETSTM JETSTM4101 1500501 EU LT ENGINE MALFUNCTIONED A RAIA A UNSCHED LANDING Y N ENGINE STOPPAGE FALSE WARNING CR CRUISE 1 CE 03 566HK 41084 FLT 7705 - BOS - LEFT ENGINE FIRE AND OVER HEAT INDICATION ILLUMINATED. MAINTENANCE RAN ENGINE COULD NOT DUPLICATE PROB LEM. (M) 2 L 7 2 4T RT A41NM 1999012200729 19990122 00729 1999 1 22 RAIA981225 4 19981220 A 2350 9939007 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 566HK 41084 FLT 7633 - JFK - CAPTAINS PTT SWITCH INOPERATIVE. MAINTENANCE REPLACED PTT SWITCH. (M) 2 L 7 2 4T RT A41NM 1999012200730 19990122 00730 WP 1999 1 22 AALA982120 1 19981121 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 579AA 53156 DFW - DURING MAINTENANCE CHECK, AFT COACH CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT AFT COACH CLA SS EMERGENCY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200731 19990122 00731 WP 1999 1 22 AALA982119 1 19981120 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 586AA 53249 DFW - DURING OVERNIGHT CHECK, FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT STRIP AT FIRST CLASS EMERGEN CY EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012200732 19990122 00732 NM 1999 1 22 AALA984247 1 19981130 A 5320 SPLICE BOEING 767 767223 1385123 NM BS 434 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - STRINGER 32L HAD SECTION REMOVED DUE TO CORROSION NEAR A PRODUCTION SPLICE AT STATION 434. REMOVE CORRODED PIECE OF STRINGER. REPLACE WITH SIMILAR LONGER SPLICE WITHOUT JOGGLE. ALODINE AND APPLY 2 COATS PRIMER SURFACE SEAL WITH BMS 5-95. (M) 2 L 7 2 4F RT A1NM 1999012200733 19990122 00733 NM 1999 1 22 AALA984246 1 19981125 A 5313 STRINGER BOEING 767 767223 1385123 NM BS 774 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - FOUND CORROSION BLENDED BEYOND SRM LIMITS ON STRINGER 37L - STATION 774. BLENDOUT CORROSION AND MAKE SURE NO CRAC KS EXIST. REFINISH THE BLENDED AREA PER THE REF. ALL FASTENERS COMMON TO THE CORROSION BLENDS ARE .0156 OVERSIZE, USIN G THE SAME TYPE AS FASTENERS REMOVED. THE SKIN BLEND REPAIR IS SATISFACTORY FOR CONTINUED SERVICE WITH NOTED CONDITION. (M) 2 L 7 2 4F RT A1NM 1999012200752 19990122 00752 EA 1999 1 22 99ZZZX383 2 19981201 A 7200 ENGINE BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA LEFT MAKING METAL A DWHA O OTHER J WARNING INDICATION NR NOT REPORTED 1 WP 01 110G BB792 PCE81926 WHILE THE AIRCRAFT WAS FLYING OVER LAX ON RETURN TO VAN NUYS, THE LEFT HAND ENGINE CHIP DETECTOR LIGHT CAME ON. THE PIL OT SHUT THE ENGINE DOWN IAW EMERGENCY PROCEDURES AND PROCEEDED TO VAN NUYS ON ONE ENGINE. INSPECTION REVEALED CHIPS ON THE CHIP DETECTOR, IN THE OIL AND OIL FILTER. THE ENGINE IS BEING RETURNED TO PRATT & WHITNEY FOR EVALUATION AND REPAIR. 1 L 7 2 4T 4 T A24CE E4EA 1999012200766 19990122 00766 WP 1999 1 22 IXXA9800114 1 19980624 A 5314 KEEL BEAM DOUG DC8 DC871F 302199D WP BS 742 & 781.5 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825BX 77125 2592 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON LOWER KEEL BEAM CAP BETWEEN FUSELAGE STATIONS 742.2 AND 781 .5. REPAIR ACCOMPLISHED CORROSION REMOVAL, FABRICATION AND INSTALLATION TWO REPAIR ANGLES IN ACCORDANCE WITH FAA PER AP PROVED DRAWING E78-R02 AND ENGINEERING ORDER 53-DC8-915. 2 L 7 4 4F RT 4A25 1999012200767 19990122 00767 WP 1999 1 22 IXXA9800115 1 19980611 A 5330 PLATING DOUG DC8 DC871F 302199D WP BS 699.5 CORRODED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825BX 45978 DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LOWER KEEL BEAM EXTERNAL PLATING AT FUSELAGE STATION 69 9.5. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION NEW EXTERNAL PLATING AND TWO REPAIR DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED DRAWING E78-R01 AND ENGINEERING ORDER 53-DC8-914. 2 L 7 4 4F RT 4A25 1999012200768 19990122 00768 WP 1999 1 22 IXXA9800116 1 19980615 A 5210 FITTING DOUG DC8 DC871F 302199D WP PAX DOOR CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825BX 45978 DURING ROUTINE C-CHECK INSPECTION, FOUND TWO UPPER DOOR STOP FITTING AT THE LEFT AFT PASSENGER DOOR CRACKED. REPAIR ACC OMPLISHED REMOVAL OF THE DAMAGED FITTINGS, FABRICATION AND INSTALLATION TWO NEW FITTINGS IN ACCORDANCE WITH DOUGLAS DRAW ING 4640556 AND ENGINEERING ORDER 52-DC8-922. 2 L 7 4 4F RT 4A25 1999012200769 19990122 00769 WP 1999 1 22 IXXA9800117 1 19980623 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 700 CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825BX 45978 DURING ROUTINE C-CHECK INSPECTION, A CRACKED KEEL BEAM LOWER FRAME FITTING WAS FOUND CRACKED AT FUSELAGE STATION 700. R EPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED FITTING, FABRICATION AND INSTALLATION A NEW FITTING IN ACCORDANCE WITH DOUGLAS DRAWING 375757 AND ENGINEERING ORDER 53-DC8-921. 2 L 7 4 4F RT 4A25 1999012200770 19990122 00770 WP 1999 1 22 IXXA9800118 1 19980611 A 5400 ANGLE DOUG DC8 DC871F 302199D WP NR 1 & 4 PYLON CRACKED A IXXA K NONE O OTHER IN INSP/MAINT 1 GL 23 825BX 45978 DURING ROUTINE C-CHECK INSPECTION, CRACKS WERE DETECTED ON THE NUMBER ONE AND FOUR INBOARD PYLON ATTACH ANGLE STIFFENERS . REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED ANGLES, FABRICATION AND INSTALLATION OF TWO NEW ANGLES IN ACCORDANCE WITH DOUGLAS DRAWING 5756791 AND ENGINEERING ORDER 54-DC8-919. 2 L 7 4 4F RT 4A25 1999012200793 19990122 00793 EU 1999 1 22 QXEA9802040 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION IN CENTER OF SEAT TRACK BL 600L, 10 AFT OF FRAME 14755. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, PARAGRAPH B A ND C. 2 L 7 2 4F RT A20EU 1999012200794 19990122 00794 EU 1999 1 22 QXEA9802041 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK OF BL 1127L AT FRAME 14755, 3 INCHES LONG. REPAIRED IAW FOKKER SRM 51-10-4, P AGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200795 19990122 00795 EU 1999 1 22 QXEA9802042 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, AT FRAME 14285. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGR APH B AND C. 2 L 7 2 4F RT A20EU 1999012200796 19990122 00796 EU 1999 1 22 QXEA9802043 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 7 AFT OF FRAME 13815B, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200797 19990122 00797 EU 1999 1 22 QXEA9802044 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13815B. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200798 19990122 00798 EU 1999 1 22 QXEA9802045 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 9 AFT OF FRAME 13815A, 1 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200799 19990122 00799 EU 1999 1 22 QXEA9802046 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 1127L, 5 AFT OF FRAME 14285, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4 PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200800 19990122 00800 EU 1999 1 22 QXEA9802047 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 1127L AT FRAME 13815B. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4, PARAG RAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200801 19990122 00801 EU 1999 1 22 QXEA9802048 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13815A, 11 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200802 19990122 00802 EU 1999 1 22 QXEA9802049 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 3 AFT OF FRAME 13815, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 , NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200803 19990122 00803 EU 1999 1 22 QXEA9802050 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13815 AND FORWARD, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4 P AGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200804 19990122 00804 EU 1999 1 22 QXEA9802051 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 13345, 6 LONG. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9 NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200805 19990122 00805 EU 1999 1 22 QXEA9802052 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600L, 12 AFT OF FRAME 13345. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4 , PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200806 19990122 00806 EU 1999 1 22 QXEA9802053 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 11 AFT OF FRAME 12405, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200807 19990122 00807 EU 1999 1 22 QXEA9802054 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 4 AFT OF FRAME 12405, 4 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 , NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200808 19990122 00808 EU 1999 1 22 QXEA9802055 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11905 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 11905, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200809 19990122 00809 EU 1999 1 22 QXEA9802056 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 11703 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, STARTING AT FRAME 11703, 9 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAG E 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200810 19990122 00810 EU 1999 1 22 QXEA9802057 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 5.5 AFT OF FRAME 10966, 7 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200811 19990122 00811 EU 1999 1 22 QXEA9802058 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK 1127L, 9 AFT OF FRAME 10966, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200812 19990122 00812 EU 1999 1 22 QXEA9802059 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 10966, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200813 19990122 00813 EU 1999 1 22 QXEA9802060 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10790 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 10790, 3 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200814 19990122 00814 EU 1999 1 22 QXEA9802061 1 19981119 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 5 AFT OF FRAME 10346, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 , NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200815 19990122 00815 EU 1999 1 22 QXEA9802062 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L AT FRAME 10346, 5.5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200816 19990122 00816 EU 1999 1 22 QXEA9802063 1 19981114 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON OUTBOARD FLANGE OF SEAT TRACK BL 600L, 13 AFT OF FRAME 9805, 9 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9, NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200817 19990122 00817 EU 1999 1 22 QXEA9802064 1 19981113 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 CORROSION ON INBOARD FLANGE OF SEAT TRACK BL 600L, 13 AFT OF FRAME 9805, 5 LONG. REPAIRED IAW FOKKER SRM 51-10-4 PAGE 9 , NR 4, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999012200826 19990122 00826 WP 1999 1 22 RRXA99006 1 19981020 A 5320 5755066 STRAP DOUG DC8 DC871F 302199D WP BS 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT, FOUND FRAME STRAP WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 1100 AND BETWEEN L ONGERONS 31 RIGHT TO 32 RIGHT. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05680. 2 L 7 4 4F RT 4A25 1999012200827 19990122 00827 WP 1999 1 22 RRXA99007 1 19981022 A 5315 575503273 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 1745 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM WITH CORROSION DAMAGE BEYOND LIMITS IAW DC-8 SRM AT STA 1745 AND BLL 26. RE MOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED TIMCO DER ENG INEERING SKETCH REO-05687. 2 L 7 4 4F RT 4A25 1999012200828 19990122 00828 WP 1999 1 22 RRXA99008 1 19981028 A 5753 5642970319 SKIN DOUG DC8 DC871F 302199D WP LT TE FLAP GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 801GP 46039 DURING A MAINTENANCE VISIT, FOUND LEFT WING OUTBOARD LOWER FLAP SKIN SURFACE GOUGED BEYOND LIMITS IAW DC-8 SRM AT STA XF 223. REMOVED DAMAGED BY BLEND-OUT BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER E NGINEERING SKETCH REO-05731. 2 L 7 4 4F RT 4A25 1999012400002 19990124 00002 EU 1999 1 24 QXEA9801906 1 19981130 A 5315 FLOORBEAM FOKKER F28 F28MK4000 4990810 EU BS 3930 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 479AU 11228 PDX - GALLEY NR 1 FLOORBEAM AT APPROXIMATELY BL900 DAMAGED AT AFT END APPROXIMATELY STATION 3930. NUTPLATE THAT WAS INS TALLED IS NOT LINED UP WITH HOLE. REALIGNED HOLE WITH NUT PLATE. 2 L 7 2 4F RT A20EU 1999012600001 19990126 00001 EU 1999 1 26 C2XA98IA498 1 19981220 A 5315 S53672408202 FLOORBEAM AEROSP ATR42 ATR42320 8680930 EU BS 39 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE FLOORBEAM AT FRAME 39 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED T HE AFFECTED FLOORBEAM IAW THE ATR 42-320 SRM 53-61-40. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999012900051 19990129 00051 SW 1999 1 29 99ZZZX385 1 19981029 A 2920 70060T000Y310 LINE BELL 214 214ST 1182106 SW HYDRAULIC SYSTEM LEAKING A HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 6957Y 28139 AIRCRAFT DEPARTED CAMERON BASE. LOST NR 2 HYDRAULIC PRESSURE. AIRCRAFT RETURNED TO CAMERON BASE. FOUND LINES, ITEMS 2 3 AND 24, CHAFED. NR 2 HYDRAULIC SYSTEM TO COLLECTIVE SERVO. REF: 214ST IBB, FIG 29-5, ITEMS 23 AND 24. 2 G 7 2 4U H10SW 1999012900052 19990129 00052 SW 1999 1 29 99ZZZX386 1 19981029 A 2920 70060Y000Y310 LINE BELL 214 214ST 1182106 SW HYDRAULIC SYSTEM LEAKING A HEEA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 03 6957Y 28139 AIRCRAFT DEPARTED CAMERON BASE. LOST NR 2 HYDRAULIC PRESSURE. AIRCRAFT RETURNED TO CAMERON BASE. FOUND LINES, ITEMS 2 3 AND 24, CHAFED. NR 2 HYDRAULIC SYSTEM TO COLLECTIVE SERVO. REF: 214ST IBB, FIG 29-5, ITEMS 23 AND 24. 2 G 7 2 4U H10SW 1999012900055 19990129 00055 EU 1999 1 29 99ZZZX389 1 19981204 A 6710 10545028 HYDRAULIC PACK BOLKMS 105 BO105S 5626006 EU CYCLIC MALFUNCTIONED A HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 911DD 3894 814 052356 S830 CYCLIC CONTROL WOULD NOT MOVE PAST CENTER WHEN PILOT ATTEMPTED TO MOVE THE CYCLIC CONTROL TO THE LEFT AFTER MAKING A RIG HT INPUT. NO MECHANICAL ANOMALIES COULD BE FOUND. HYDRAULIC PACK WAS CHANGED. REF: BO-105 IPC, FIGURE 424, ITEM 30. 1 G 7 2 3U H3EU 1999012900056 19990129 00056 EA 1999 1 29 99ZZZX390 2 19980107 A 7230 3024361 STATOR BEECH 200 200BEECH 1152920 CE PWA PT6 PT6A41 52043 EA RT ENGINE FAILED A HEEA O OTHER O OTHER CL CLIMB 1 SW 03 500PH 7402 3009 BL29 PCE81768 RIGHT ENGINE FAILED SHORTLY AFTER TAKEOFF. LABRATORY REPORT FROM P & W CONTRIBUTED ENGINE FAILURE TO 1ST STAGE COMPRESS OR STATOR FAILURE. STATOR AIRFOIL FAILED DUE TO HIGH CYCLE FATIGUE. 1 L 7 2 4T 4 T A24CE E4EA 1999012900077 19990129 00077 CE 1999 1 29 99ZZZX427 1 19981114 A 2750 99145101 RESOLVER CESSNA 750 750 2076810 CE TE FLAP FAILED A I5EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 07 10JM 1237 7500022 KIAD - AFTER TAKEOFF, PILOT NOTICED FLAP FAIL MESSAGE. DIVERTED AIRCRAFT, RETURNED FOR INVESTIGATION. FLAP OPERATIONAL CHECK PERFORMED. FOUND DEFECTIVE RESOLVER LOCATED RIGHT WING FLAP. REPLACED RESOLVER AND PERFORMED RIGGING CHECK. PE RFORMED OPERATIONAL CHECK WITH NO IRREGULARITIES NOTED. RELEASED AIRCRAFT. PART TC: 773. 2 L 7 2 4J RT T00007WI 1999012900078 19990129 00078 CE 1999 1 29 99ZZZX428 1 19981116 A 2750 99145101 RESOLVER CESSNA 750 750 2076810 CE TE FLAP FAILED A I5EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 WP 07 924EJ 1227 9552 7500024 KLGB - AFTER TAKEOFF, PILOT NOTICED FLAP FAIL MESSAGE. DIVERTED AIRCRAFT, RETURNED FOR INVESTIGATION. FLAP OPERATIONAL CHECK PERFORMED. FOUND DEFECTIVE RESOLVER BY COLD SOAKING THE RIGHT WING FLAP RESOLVER. REPLACED RESOLVER AND PERFOR MED RIGGING CHECK. PERFORMED OPERATIONAL CHECK WITH NO IRREGULARITIES NOTED. RELEASED AIRCRAFT. PART TC: 782. 2 L 7 2 4J RT T00007WI 1999012900082 19990129 00082 EU 1999 1 29 HCMA000219 1 19981001 A 6420 350A33215300 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR CRACKED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 642BH 995 2495 BEARING IS CRACKED AND WORN BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1999012900083 19990129 00083 EU 1999 1 29 99ZZZX402 1 19981017 A 2450 45033500 ELECTRICAL BOX AUXILEC UROCOP EC135 EC135P1 8680990 EU LEFT SHORTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 19 1059 EC1350054 ELECTRICAL BOX SHORTED OUT (SMOKED). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999012900084 19990129 00084 EU 1999 1 29 99ZZZX403 1 19981021 A 2450 45023500 ELECTRICAL BOX UROCOP EC135 EC135P1 8680990 EU RIGHT SHORTED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 39 1072 EC1350054 ELECTRICAL BOX UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999012900093 19990129 00093 EU 1999 1 29 PLGA981217A 1 19981217 A 2612 FIRE LOOP SAAB SF340 SF340A 7850100 EU RT ENGINE MALFUNCTIONED A PLGA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NE 05 336BE 340A028 BOS - FLT 6337 - AFTER TAKEOFF WHILE CLIMBING THROUGH 1,500 FEET, THE CREW EXPERIENCED A RIGHT ENGINE TAIL PIPE HOT WARN ING. CREW FOLLOWED PROCEDURES AND SHUT DOWN THE RIGHT ENGINE. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. T HE PASSENGERS WERE DEPLANED THROUGH THE MAIN CABIN DOOR AND THE AIRCRAFT WAS TOWED TO THE GATE. WHEN MAINTENANCE ARRIVE D AT THE AIRCRAFT, THE WARNING INDICATION WAS EXTINGUISHED. MAINTENANCE WAS UNABLE TO DUPLICATE THE PROBLEM. MAINTENAN CE REPLACED ALL THREE TAIL PIPE HOT DETECTORS, P/N 17343-62-450F, AND WIRING HARNESS. AIRCRAFT WAS TEST FLOWN WITH NO P ROBLEMS REPORTED. PART NUMBER OF HARNESS INSTALLED PLGA340-026-018R, S/N 068R. (X) 2 L 7 2 4T RT A52EU 1999012900094 19990129 00094 NE 1999 1 29 PLGA981023B 2 19981023 A 7210 7757981 PUMP SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE RT ENGINE FAILED A PLGA K NONE O OTHER IN INSP/MAINT 1 NE 05 336BE HS0461 340A028 PHL - REFERENCE ODR PLGA981023A. THE RIGHT PROPELLER GEARBOX (PGB) WAS REPLACED DUE TO A FAILED OIL PUMP. THE OIL PUMP REMOVED WAS P/N 775798-1, S/N HS046-1. THE CORRECT PART NUMBER FOR THE PGB WAS 775798-3. (X) 2 L 7 2 4T 4 T RT A52EU E8NE 1999012900095 19990129 00095 EU 1999 1 29 99ZZZX412 1 19981217 A 7714 L772M10C1002 INDICATOR UROCOP EC135 EC135P1 8680990 EU COCKPIT MALFUNCTIONED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 121 0033 EC1350054 UNIT OPERATES INTERMITTENTLY. NR 2 NEEDLE RISES WITHOUT CAUSE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999012900147 19990129 00147 WP 1999 1 29 UPS99828466 1 19980107 A 5720 DOUBLER DOUG DC8 DC871F 302199D WP WS 379-385 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE:C3, RT WING L/E LWR SKIN AT STA XFS379.0-385.25, THE INTERNAL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-0. 2 L 7 4 4F RT 4A25 1999012900155 19990129 00155 NM 1999 1 29 QXEA9900001 1 19981214 A 5230 DOOR DHAV DHC8 DHC8102 2809003 NM CARGO COMPT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 MECHANICAL DAMAGE ON CARGO DOOR UNDER MOUNTING AREA FOR UPPER MOST OF REAR VERTICAL EDGE. REPAIRED IAW RD 8-52-368. 2 H 7 2 4T RT A13NM 1999012900156 19990129 00156 NM 1999 1 29 QXEA9900002 1 19981210 A 3233 ACTUATOR DHAV DHC8 DHC8102 2809003 NM NR 2 MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 NR 2 MAIN GEAR STANDBY ACTUATOR CHAFING AT ATTACH POINT. REPAIRED IAW RD 8-54-1001 AND DHC -8 MM 32-30-16, PAGE 202, PA RAGRAPH B. 2 H 7 2 4T RT A13NM 1999012900157 19990129 00157 NM 1999 1 29 QXEA9900003 1 19981214 A 7110 DOOR DHAV DHC8 DHC8102 2809003 NM NR 2 ENG COWL CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 NR 1 ENGINE COWL DOOR 416AR HAD CRACK. REPAIRED IAW DHC-8 RD 71-142. 2 H 7 2 4T RT A13NM 1999012900158 19990129 00158 NM 1999 1 29 QXEA9900004 1 19981211 A 3233 ACTUATOR DHAV DHC8 DHC8102 2809003 NM LT MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 LEFT MAIN LANDING GEAR STANDBY ACTUATOR FOUND TO BE CHAFING ON ATTACH POINT FITTING. REPAIRED IAW DHC-8 MM 32-30-16, PA GE 202, PARAGRAPH B. 2 H 7 2 4T RT A13NM 1999012900159 19990129 00159 NM 1999 1 29 QXEA9900005 1 19981208 A 5400 SUPPORT DHAV DHC8 DHC8102 2809003 NM NR 1 ENGINE GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 NR 1 ENGINE OUTBOARD SUPPORT STRUT HAS GOUGES FROM FIRE DETECTION WIRES IN TWO PLACES. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 1999012900160 19990129 00160 NM 1999 1 29 QXEA9900006 1 19981214 A 5414 SKIN DHAV DHC8 DHC8102 2809003 NM NR 2 NACELLE DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 DENTS FOUND IN OUTER SKIN OF INBOARD NR 2 ENGINE PANEL 425AL. REPAIRED IAW DHC-8 RD 8-71-139. 2 H 7 2 4T RT A13NM 1999012900161 19990129 00161 NM 1999 1 29 QXEA9900007 1 19981216 A 5540 HINGE DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 FORE RUDDER TRAILING HINGE, BOTTOM FITTING HAS MECHANICAL DAMAGE. REPAIRED IAW DHC -8 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 1999012900162 19990129 00162 NM 1999 1 29 QXEA9900008 1 19981216 A 5540 HINGE DHAV DHC8 DHC8102 2809003 NM RUDDER DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 FORE RUDDER TRAILING TOP HINGE FITTING HAS MECHANICAL DAMAGE. REPAIRED IAW DHC-8 SRM 51-20-16 AND 51-20-36. 2 H 7 2 4T RT A13NM 1999012900163 19990129 00163 NM 1999 1 29 QXEA9900009 1 19981201 A 5540 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 MINOR CHAFE DAMAGE ON UPPER AND LOWER FORE RUDDER ACTUATOR FITTINGS. REPAIRED IAW RD 8-55-128. 2 H 7 2 4T RT A13NM 1999012900164 19990129 00164 NM 1999 1 29 QXEA9900010 1 19981201 A 5540 FITTING DHAV DHC8 DHC8102 2809003 NM RUDDER CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 MINOR CHAFE DAMAGE ON FORE RUDDER HYDRAULIC DAMPER FITTING. REPAIRED IAW RD 8-55-128. 2 H 7 2 4T RT A13NM 1999012900165 19990129 00165 NM 1999 1 29 QXEA9900011 1 19981212 A 5540 FITTING DHAV DHC8 DHC8102 2809003 NM VERT STAB WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 LOWER LUG OF MIDDLE LOWER RUDDER FITTING ON VERTICAL STABILIZER IS WORN WHERE THE BEARING SITS. REPAIRED IAW RD 55-350. 2 H 7 2 4T RT A13NM 1999012900166 19990129 00166 NM 1999 1 29 QXEA9900012 1 19981214 A 5320 SUPPORT DHAV DHC8 DHC8102 2809003 NM BS 424-488.5 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 FRETTING CORROSION FOUND ON LEFT SUPPORT FOR PANELS 143AZ AND 143BZ BETWEEN FUSELAGE STATION X424.124 AND X488.500. REP AIRED IAW DHC-8 RD 8-53-3960. 2 H 7 2 4T RT A13NM 1999012900167 19990129 00167 NM 1999 1 29 QXEA9900013 1 19981215 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 21 & 498 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 102AV 091 DENT BEYOND LIMITS AT X498.737 AND .5 BELOW STATION 21. REPAIRED IAW RD 8-53-3961. 2 H 7 2 4T RT A13NM 1999012900190 19990129 00190 WP 1999 1 29 CA980707042 2 19980617 A 7322 89778017 FUEL CONTROL SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP RT ENGINE FAILED W O OTHER R PARTIAL RPM/PWR LOSS DE DESCENT 1 CA 6 1578192 P54158 (CAN) DURING DESCENT, POWER WAS ADDED, BUT RIGHT ENGINE WOULD ONLY PRODUCE 1150 TO 1250 FEET/POUNDS OF TORQUE. AIRCRAFT LANDED OK. GROUND RUN DID SAME, BUT AFTER 5 TO 10 SECONDS THE TORQUE JUMPED TO 2206 FEET/POUNDS. EVENTUALLY RIGHT FCU WAS REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 1999012900191 19990129 00191 SW 1999 1 29 CA980707046 1 19980625 A 3040 149940303 WINDSHIELD WIPER SWRNGN SA226 SA226TC 8780404 SW COCKPIT WINDOW SEPARATED W O OTHER D INFLIGHT SEPARATION NR NOT REPORTED 1 CA (CAN) RIGHT HAND WINDSHIELD WIPER ASSY SEPARATED FROM AIRCRAFT IN-FLIGHT. 2 L 7 2 4T RT A8SW 1999012900194 19990129 00194 SW 1999 1 29 CA980707054 1 19980611 A 2435 03601018 BEARING LUCAS 23079010 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE START/GENERATOR FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 512 92093 P44663C 881750 (CAN) COULD NOT GET GENERATOR ON LINE AND AIRCRAFT RETURNED TO BASE. STARTER/GENERATOR BEARING HAD LET GO. PART TC: 6 77. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999012900195 19990129 00195 SW 1999 1 29 CA980707055 1 19980630 A 2750 246003 VALVE SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE TE FLAP FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 384 880393 (CAN) PILOT UNABLE TO BRING FLAPS UP AFTER TAKEOFF. AIRCRAFT RETURNED. FLAP SELECTOR VALVE FOUND AT FAULT. 2 L 7 2 4T RT A8SW 6 C 3PNE 1999012900196 19990129 00196 WP 1999 1 29 CA980707056 2 19980630 A 7200 ENGINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE ENGINE BAY MALFUNCTIONED W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA P44501C 930243 (CAN) NEWLY OVERHAULED ENGINE STARTED HOTTER THAN NORMAL. AFTER EXTENSIVE TROUBLESHOOTING THE ENGINE WAS REMOVED FOR FU RTHER INVESTIGATION. AWAITING INFORMATION. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999012900197 19990129 00197 WP 1999 1 29 CA980707057 2 19980630 A 7250 31021069 RIVETS SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE TURBINE WHEEL LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 1859 P44205C 930243 (CAN) NOISE EMITTING FROM ENGINE FOUND TO BE LOOSE RIVETS. ENGINE REMOVED FOR REPAIR. PART TC: 3,008. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999012900199 19990129 00199 NM 1999 1 29 CA980714014 1 19980625 A 3297 864202 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT MLG BROKEN W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 120542 (CAN) DURING CLIMB, CREW RECEIVED A WEIGHT-ON-WHEELS INDICATION. AIRCRAFT RETURNED TO BASE. A WIRE ON THE RIGHT HAND M AIN LANDING GEAR WOW SWITCH WAS FOUND BROKEN. 2 H 7 2 4T 4 T RT A13NM E20NE 1999012900203 19990129 00203 SW 1999 1 29 CA980724023 1 19980622 A 2140 DUCT SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP E/E BAY LOOSE W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA P54202 (CAN) DURING CRUISE, THE CREW NOTED THAT THE LEFT ESSENTIAL BUS WAS ABNORMALLY HOT, SHORTLY AFTER THE NR 1 AUDIO CIRCUIT BREAKER TRIPPED. AIRCRAFT RETURNED TO BASE. INVESTIGATION FOUND THE HOT AIR DUCT IN THE LEFT ESSENTIAL BUS AREA HAD B ECOME DISLODGED DIRECTING HOT AIR ONTO THE BUS. IN ADDITION, THE NR 1 AUDIO PANEL CIRCUIT BREAKER WAS FOUND CRACKED. 2 L 7 2 4T 4 T RT A8SW E4WE 1999012900204 19990129 00204 SW 1999 1 29 CA980724024 1 19980625 A 2910 2781006143 LINE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HYDRAULIC SYSTEM CHAFED W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA P54183 (CAN) CREW NOTICED HYDRAULIC DRIP FROM CENTER SECTION. INVESTIGATION REVEALED THAT THE HYDRAULIC LINE HAD CHAFED THROUG H. 2 L 7 2 4T 4 T RT A8SW E4WE 1999012900205 19990129 00205 SW 1999 1 29 CA980724043 1 19980714 A 3213 2751544005 TORQUE KNEE OAS545119 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 2058 P44205C 930243 (CAN) UPPER TORQUE KNEE FOUND CRACKED IN THE MACHINED RADIUS PER SERVICE BULLETIN 32-041. THIS IS 4TH UPPER TORQUE KNEE FOUND CRACKED BY THIS OPERATOR. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999012900206 19990129 00206 NM 1999 1 29 CA980818002 1 19980714 A 5597 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ELEVATOR HORN FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 28542 121165 (CAN) LEFT ELEVATOR HORN HEAT CAUTION LIGHT ON DURING CLIMB. DUE TO FORECAST ICING CONDITIONS, AIRCRAFT RETURNED TO BAS E. A WIRE BETWEEN CONNECTORS J3 AND J5 WAS FOUND BURNT AND OPEN. PART TC: 39,154. 2 H 7 2 4T 4 T RT A13NM E20NE 1999012900207 19990129 00207 SW 1999 1 29 CA980818024 1 19980804 A 2913 PV304426 PUMP SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE LT ENGINE WORN W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA MX297548C P44501C 911172 (CAN) HYDRAULIC PUMP FAILURE ON LEFT SIDE FOLLOWING GEAR RETRACTION. PUMP SPLINES HAD WORN OFF UNTIL THEY STARTED TO SL IP. PUMP HARD TO TURN INDICATING A SPLINE PROBLEM. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999012900208 19990129 00208 SW 1999 1 29 CA980827005 1 19980820 A 3230 275100059 UPLOCK SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP LT MLG FAILED W O OTHER O OTHER AP APPROACH 1 CA P54143 (CAN) ON APPROACH, LEFT GEAR DID NOT EXTEND WHEN GEAR SELECTED. NO IN-TRANSIT LIGHT NOTED, INDICATING GEAR DID NOT RELE ASE FROM UPLOCK. EMERG EXTENSION CARRIED OUT BUT LEFT GEAR STILL FAILED TO EXTEND. GEAR RETRACTED AND NORMAL EXTENSION CARRIED OUT. LEFT STILL FAILED. ONCE AGAIN EMERG TRIED AND AFTER SEVERAL PUMPS WITH EMERG PUMP, IT RELEASED. A/C LAN DED OK. SUBSEQUENT CHECKS CONFIRMED THAT SYSTEM WOULD NOT RELEASE DURING NORMAL GEAR EXTENSION. INSP FOUND THAT UPLOCK LATCH RELEASE MECHANISM HAD EXCESSIVE PLAY FROM ELONGATED HOLES IN TUBE, P/N 27-51000-59, WHERE ARMS AND STOPS ARE SECU RED TO IT. THIS EXCESSIVE PLAY PREVENTED UPLOCK RELEASE MECHANISM FROM HAVING SUFFICIENT TRAVEL TO RELEASE UPLOCK LATCH 2 L 7 2 4T 4 T RT A8SW E4WE 1999012900209 19990129 00209 SW 1999 1 29 CA980916043 1 19980909 A 3230 55010021 DRAG LINK SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA P54082 (CAN) DURING FLEET INSPECTION, FOLLOWING TSB FINDINGS ON THE MAIN LANDING GEAR DRAG LINKS, CRACK INDICATIONS WERE FOUND ON BOTH RIGHT HAND LOWER DRAG LINK ASSEMBLIES USING FLUORSCENT PENETRANT METHOD. FOUND CRACKS EMANATING FROM GREASE NIP PLE HOLE TO OUTER RADIUS. 2 L 7 2 4T 4 T RT A8SW E4WE 1999012900212 19990129 00212 1999 1 29 CA980922014 3 19980915 A 6140 612149L22 WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT CHAFED W O OTHER N FALSE WARNING NR NOT REPORTED 1 CA 7219 120063 (CAN) AUTOFEATHER ARM AMBER LIGHT WOULD NOT EXTINGUISH WHEN DE-SELECTED. AIRCRAFT RETURNED TO BASE. INVESTIGATION FOUN D A CHAFED WIRE AT A CLAMP. THIS PICKED UP A GROUND TO HOLD THE RELAY FOR THE ARM LIGHT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999012900227 19990129 00227 WP 1999 1 29 AT9900022 1 19981230 A 5330 SKIN DOUG DC9 DC932 3022066 WP FUSELAGE DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND DENTS AND CREASES AT VARIOUS FUSELAGE SKIN LOCATION OUT OF LIMITS. THE LO CATIONS ARE FS 104 TO FS 135 L-19R, FS 227 L-17L, FS 229 TO FS 598 L-18R TO 28R, FS 241 L-18L AND FS 269 L-18L. REPAIRE D ALL DENTED FUSELAGE SKIN BY REMOVING, COLD WORKING, FABRICATING AND INSTALLING NEW SKINS AND DOUBLERS IAW DC9 SRM 51-1 0-2, 51-10-4, 53-01 FIG 2, AND RES NR 982281, 982105, 982106, 982107 AND RES 982108. 2 L 7 2 4F A6WE 1999012900228 19990129 00228 WP 1999 1 29 AT9900023 1 19981223 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 399 CUT A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. INTERNAL TORQUE BOX DOUBLER AT FORWARD CARGO DOOR FS 399 CUT LONGERON 18R TO 20R . FABRICATED, DRILLED, PRIMED AND INSTALLED INTERNAL DOUBLER MIL-T-9046J .025 THOUSANDS OF AN INCH 13 BY 6.125 IN IAW D C9 SRM 53-04 FIG 38 AND RES NR 982282. 2 L 7 2 4F A6WE 1999012900229 19990129 00229 WP 1999 1 29 AT9900024 1 19981223 A 5310 STRUCTURE DOUG DC9 DC932 3022066 WP BS 370 MISDRILLED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND STRAP, FLOOR FRAME, FLOOR SUPPORT ANGLE AND FORWARD CARGO DOOR CUTOUT MISD RILLED AT STA 370 LONGERON 29R ( INBOARD FORWARD FRAME). CORRECTIVE ACTION: FABRICATE NEW WEB, FORMED NEW INTERC OASTAL AND DOUBLER, TRIM TWO NEW CLIPS, TREATED, PRIMED AND ALODINE PARTS IAW DC9 SRM 51-10-3, 51-10-2, 51-30-1 AND RES #982186. 2 L 7 2 4F A6WE 1999012900230 19990129 00230 WP 1999 1 29 AT9900025 1 19981222 A 5315 FLOORBEAM DOUG DC9 DC932 3022066 WP BS 389-408 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FORWARD CARGO COMPARTMENT FLOORBEAMS AT FS 389 TO FS 408 ARE CHAFED AND OUT OF L IMITS IAW SRM 53-01 FIG 1. REPAIRED THE CHAFED CABIN FLOORBEAMS LOWER LEGS BY FABRICATING AND INSTALLING REPAIR ANGLES IAW DC9 SRM 53-05 FIG 86 AND AIRTRAN RES NR 982176. 2 L 7 2 4F A6WE 1999012900231 19990129 00231 WP 1999 1 29 AT9900026 1 19981220 A 5320 ANGLE DOUG DC9 DC932 3022066 WP BS 230 & 235 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORRODED CUSP WEBS AT FS 230 AND FS 235 LEFT HAND SIDE. REPAIRED BOTH COR RODED CUSP WEB ANGLES BY REMOVING CORROSION, FABRICATING, AND INSTALLING NEW ANGLE DOUBLER IAW DC9 SRM 53-04, 53-01 FIG 1 AND AIRTRAN RES NR 982120 AND NR 982167. 2 L 7 2 4F A6WE 1999012900232 19990129 00232 WP 1999 1 29 AT9900027 1 19981222 A 5320 JAMB DOUG DC9 DC932 3022066 WP R-1 DOORWAY DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULE INSPECTION AT AERO CORP, FL. FOUND R-1 DOOR JAMMED, DENTED AND GOUGED AT STA 200 RT AT LONGERON 15R. FABRICAT ED DOOR PAN SECTION AND SPLICES, HEAT TREATED PARTS, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 53-03 FIG 2 AND AIRTRAN RES NR 982244. 2 L 7 2 4F A6WE 1999012900233 19990129 00233 WP 1999 1 29 AT9900028 1 19981230 A 5320 SLANT PANEL DOUG DC9 DC932 3022066 WP BS 588 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULE INSPECTION AT AERO CORP, FL. UPON PRESSURIZATION FOUND LEFT AND RIGHT HAND SLANT PANELS LEAKING EXCESSIVELY. S EALS TORN AND PINCHED. REMOVED LEFT AND RIGHT SLANT PANEL CORROSION, MATERIAL LOSS FOUND OUT OF LIMITS ON LEFT HAND SID E, FABRICATED REPAIR PANEL AND SPLICES IAW DC9 SRM 51-30-1 AND AIRTRAN RES NR 982119. 2 L 7 2 4F A6WE 1999012900234 19990129 00234 WP 1999 1 29 AT9900029 1 19981221 A 5320 INTERCOASTAL DOUG DC9 DC932 3022066 WP VENTRAL STAIR CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND ALL SEVEN HORIZONTAL INTERCOASTAL AND SHEAR CLIPS HAVE CORROSION ON UPPER LEGS. REMOVED CORROSION, REMOVED AND REPLACED INTERCOASTALS AND SHEAR CLIPS. FABRICATED ALODINE, PRIMED ALL PARTS IAW DC9 SRM 51-10-3, 52-60, 51-10-2, 51-30-5, 53-01 FIG 1 AND AIRTRAN RES NR 982287. 2 L 7 2 4F A6WE 1999012900235 19990129 00235 WP 1999 1 29 AT9900030 1 19981221 A 5320 WEB DOUG DC9 DC932 3022066 WP VENTRAL STAIR MISDRILLED A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VENTRAL STAIR LEFT HAND OUTBOARD WEB HAS CORROSION AND FASTENER HOLES WITH NO EDGE DISTANCE. CUT AND DRILLED NEW SECTION OF WEB AND REPLACED CORRODED SECTIONS IAW DC9 SRM 51-30-2, AND AIRTRAN R ES NR 982287. 2 L 7 2 4F A6WE 1999012900236 19990129 00236 WP 1999 1 29 AT9900031 1 19981208 A 5320 4933251 END CAP DOUG DC9 DC932 3022066 WP BS 1164 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND SEVERAL CORRODED LONGERON END CAPS AT THE FOLLOWING LOCATIONS FS 1164 L-3R , FS 1164 L-5R, FS 1164 L-7R, FS 1164 L-9R. REMOVED AND REPLACED ALL END CAPS IAW DC9 SRM 51-30-2 AND 51-30-5. 2 L 7 2 4F A6WE 1999012900237 19990129 00237 WP 1999 1 29 AT9900034 1 19981209 A 5320 CUSP WEB DOUG DC9 DC932 3022066 WP FUSELAGE CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 819AT 47260 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CUSP WEBS CORRODED AND CRACKED AT THE FOLLOWING LOCATIONS FS 598 RT, FS 61 7 RT, FS 794 TO 813 LT, FS 813 TO 832 LT, FS 869 TO 889 LT, FS 870 TO 897 RT, FS 894 LT, AND FS 897 TO FS 908 RT. REPAI RED, REMOVED ALL CORROSION, FABRICATED DOUBLERS, INSTALLED NEW FITTINGS AND DOUBLERS IAW DC9 SRM 53-01 FIG 2, 51-10-4, 5 1-10-3, 51-30-1, 51-30-2 AND MM 53-20-1 FIG 803. 2 L 7 2 4F A6WE 1999012900268 19990129 00268 WP 1999 1 29 UPS99828479 1 19981227 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 358 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, LT WING UPPER SKIN AT XRS 358 AT THE REAR SPAR IS CRACKED AT THE AFT FASTENER. REPAIRED SKIN IAW DHC SK701-230. 2 L 7 4 4F RT 4A25 1999012900269 19990129 00269 WP 1999 1 29 UPS99828480 1 19981229 A 5320 5646955504 FITTING DOUG DC8 DC871F 302199D WP BS 960 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, CUSP TO FRAME END FITTING, RT SIDE AT 960, HAS EXFOLIATION CORROSION. REMOVED, FABRICATED AND REPLAC ED FITTING IAW DHC SK701-669 AND SRM 51-1-20D. 2 L 7 4 4F RT 4A25 1999012900270 19990129 00270 WP 1999 1 29 UPS99828481 1 19981229 A 5320 3641126501 FITTING DOUG DC8 DC871F 302199D WP BS 780 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, VERTICAL FITTING COMPLETELY BROKEN AT RBL 55 AT FS 780. REMOVED AND REPLACED FITTING IAW SRM 51-1-20 D, 51-3-0. 2 L 7 4 4F RT 4A25 1999012900271 19990129 00271 WP 1999 1 29 UPS99828483 1 19981229 A 5320 4645516501 FITTING DOUG DC8 DC871F 302199D WP BS 940 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, UNDERSIDE OF W/W CENTER KEEL BEAM ATTACH FITTING IS CRACKED AT FS 940. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0. 2 L 7 4 4F RT 4A25 1999012900272 19990129 00272 WP 1999 1 29 UPS99828484 1 19981230 A 5347 S4755395T SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1060 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SEAT TRACK BLOWN AT FS 1060, RBL 50. REMOVED DAMAGED SEAT TRACK BETWEEN FS 1010 TO 1106, FABRICATED AND REPLACED SEAT TRACK IAW SRM 53-7-1, 51-1-21 AND 51-3-0. 2 L 7 4 4F RT 4A25 1999012900273 19990129 00273 WP 1999 1 29 UPS99828485 1 19981230 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 1500 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SEAT TRACK BLOWN AT FS 1500 AT RBL 50. REMOVED DAMAGED SEAT TRACK BETWEEN FS 1470 TO 1550, FABRICATE D AND REPLACED SEAT TRACK IAW SRM 53-2-3 FIG 6A, 51-3-0. 2 L 7 4 4F RT 4A25 1999012900280 19990129 00280 WP 1999 1 29 UPS99828492 1 19981231 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 435 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 713UP 46014 INSPECTION TYPE-C3, LT WING L/E LWR SKIN AT XS 435 IS CRACKED AT A FASTENER HOLE. STOP DRILLED CRACK AND REPAIRED IAW E O DC8-5720-7767-A. 2 L 7 4 4F RT 4A25 1999012900586 19990129 00586 NM 1999 1 29 9811435520 1 19981214 A 5315 FLOORBEAM BOEING 757 757251 1384970 NM BS 1681 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 520US 23208 DURING T CHECK, FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AROUND FASTENER HOLE FS 1681, LBL 39.5. REPAIRED PER EA 5 5-163314. 2 L 7 2 4F RT A2NM 1999012900606 19990129 00606 EU 1999 1 29 QXEA9900023 1 19981222 A 5753 SKIN FOKKER F28 F28MK4000 4990810 EU LT TE FLAP GOUGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - INBOARD FLAP OF LEFT-HAND WING HAS GOUGE ON AFT PART OF FLAP OUTBOARD OF PANEL 81AV. REPAIRED IAW HORIZON AIR EA 4-57-200. 2 L 7 2 4F RT A20EU 1999012900607 19990129 00607 EU 1999 1 29 QXEA9900024 1 19981210 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRAME CLIP REPAIR AT FRAME 17565 AND STRINGER 21 HAS FOUR RIVETS WITH BUCKED TAILS. REPLACED PER FOKKER SRM 51-31 -01. 2 L 7 2 4F RT A20EU 1999012900608 19990129 00608 EU 1999 1 29 QXEA9900025 1 19981210 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRAME CLIP REPAIR AT FRAME 17565 AND STRINGER 15 HAS FIVE RIVETS WITH BUCKED TAILS. REPLACED FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999012900609 19990129 00609 EU 1999 1 29 QXEA9900026 1 19981210 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CRACK ON FRAME CLIP 17565, STRINGER 24. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND 51-31-01. 2 L 7 2 4F RT A20EU 1999012900610 19990129 00610 EU 1999 1 29 QXEA9900027 1 19981209 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CRACK ON FRAME CLIP 17565, STRINGER 25A. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5 AND 51-31-01. 2 L 7 2 4F RT A20EU 1999012900611 19990129 00611 EU 1999 1 29 QXEA9900028 1 19981222 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRAME 41-2, STRINGER 35 CLIP IS CRACKED ON BACKSIDE. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999012900612 19990129 00612 EU 1999 1 29 QXEA9900029 1 19981209 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 32-2 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - OBLIQUE FRAME 32-2 BETWEEN STRINGERS 1 AND 5 THERE ARE FOUR DISTORTED FRAME CLIPS. REPAIRED IAW FOKKER SRM 53-02- 13, PAGE 5 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999012900613 19990129 00613 EU 1999 1 29 QXEA9900030 1 19981211 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A CRACKED CLIP AT FRAME 17565 AND STRINGER 53. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999012900614 19990129 00614 EU 1999 1 29 QXEA9900031 1 19981216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE ARE 2 FRAME CHAFES AND A CLAMP MISSING AT FRAME 17565 BETWEEN STRINGERS 12 AND 14. REPAIRED IAW HORIZON AIR EA 4-53-626. 2 L 7 2 4F RT A20EU 1999012900615 19990129 00615 EU 1999 1 29 QXEA9900032 1 19981216 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 18075 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - TWO FRAME CHAFES FRAME 18075, STRINGERS 18 AND 19. REPAIRED IAW HORIZON EA 4-53-626. 2 L 7 2 4F RT A20EU 1999012900616 19990129 00616 EU 1999 1 29 QXEA9900033 1 19981210 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 17565 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CRACKED CLIP FRAME 17565 AND STRINGER 22. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 5, FIGURE 3. 2 L 7 2 4F RT A20EU 1999012900617 19990129 00617 EU 1999 1 29 QXEA9900034 1 19981217 A 5320 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 18075 CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRAME 18075 IS CHAFED AT STRINGER 12. REPAIRED IAW FOKKER SRM 51-30-12. 2 L 7 2 4F RT A20EU 1999012900618 19990129 00618 EU 1999 1 29 QXEA9900035 1 19981210 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 20075 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRAME 20075 AND STRINGER 36 A CRACKED CLIP HAS BEEN STOP DRILLED TWICE. REPAIRED IAW FOKKER SRM 53-02-13 PAGE 6, FIGURE 4. 2 L 7 2 4F RT A20EU 1999012900619 19990129 00619 EU 1999 1 29 QXEA9900036 1 19981210 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU FRAME 50-2 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRAME 50-2 AND STRINGER 21 HAS A RIVET WITH A DRILLED BUCKTAIL. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999012900620 19990129 00620 EU 1999 1 29 QXEA9900037 1 19981217 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 41-2 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - REPAIR AT FRAME 41-2 AND STRINGER 38 HAS BEEN STOP DRILLED FOUR TIMES AND IS CRACKED. REPAIRED IAW FOKKER SRM 53- 02-13, PAGE 8, FIGURE 6. 2 L 7 2 4F RT A20EU 1999012900621 19990129 00621 EU 1999 1 29 QXEA9900038 1 19981208 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 67-2 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRAME 67-2 LEFT-HAND SIDE OF VERTICAL STABILIZER BOX IS CRACKED. REPAIRED IAW FOKKER SRM 53-10-05, PAGE 601A, PAR AGRAPH 2 B (2). 2 L 7 2 4F RT A20EU 1999012900622 19990129 00622 EU 1999 1 29 QXEA9900039 1 19981229 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU FRAME 16495 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND DIMPLED LAP JOINT, - 2 RIVETS AFT OF FRAME 16495 ON STRINGER 16A CONNECTION HOLE REQUIRE REPLACEMENT. R EPLACED IAW FOKKER SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999012900623 19990129 00623 EU 1999 1 29 QXEA9900040 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A CRACKED CLIP AT FRAME 14755 AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900624 19990129 00624 EU 1999 1 29 QXEA9900041 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A CRACKED CLIP AT FRAME 14755 AND STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900625 19990129 00625 EU 1999 1 29 QXEA9900042 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS CLIP REPAIR AT FRAME 14755 AND STRINGER 19 THAT DOES NOT CONFORM TO FOKKER SRM 53-10-13. REPA IRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900626 19990129 00626 EU 1999 1 29 QXEA9900043 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 14755 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS CLIP REPAIR AT FRAME 14755 AND STRINGER 18 THAT DOES NOT CONFORM TO FOKKER SRM 53-02-13. REPA IRED IAW FOKKER SRM 53-01-13. 2 L 7 2 4F RT A20EU 1999012900627 19990129 00627 EU 1999 1 29 QXEA9900044 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS CLIP REPAIR AT FRAME 15205 BETWEEN STRINGER 21A AND 24 THAT DOES NOT CONFORM TO FOKKER SRM 53- 02-13. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900628 19990129 00628 EU 1999 1 29 QXEA9900045 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS CLIP REPAIR AT FRAME 15205 AND STRINGER 21 THAT DOES NOT CONFORM TO FOKKER SRM 53-02-13. REPA IRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900629 19990129 00629 EU 1999 1 29 QXEA9900046 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS CLIP REPAIR AT FRAME 15205 AND STRINGER 20 THAT DOES NOT CONFORM TO FOKKER SRM 53-02-13. REPA IRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900630 19990129 00630 EU 1999 1 29 QXEA9900047 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS CLIP REPAIR AT FRAME 15205 AND STRINGER 19 THAT DOES NOT CONFORM TO FOKKER SRM 53-02-13. REPA IRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900631 19990129 00631 EU 1999 1 29 QXEA9900048 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS CLIP REPAIR AT FRAME 15205 AND STRINGER 18 THAT DOES NOT CONFORM TO FOKKER SRM 53-02-13. REPA IRED IAW FOKKER SRM 53-10-13. 2 L 7 2 4F RT A20EU 1999012900632 19990129 00632 EU 1999 1 29 QXEA9900049 1 19981206 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 15205 MISREPAIRED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - THERE IS A PREVIOUS REPAIR AT FRAME 15205 AND STRINGER 25 THAT DOES NOT CONFORM TO FOKKER SRM 53-02-13. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900633 19990129 00633 EU 1999 1 29 QXEA9900050 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CLIP CRACKED AT FRAME 15205 AND STRINGER 57. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900634 19990129 00634 EU 1999 1 29 QXEA9900051 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CLIP CRACKED AT FRAME 15205 AND STRINGER 51. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900635 19990129 00635 EU 1999 1 29 QXEA9900052 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CLIP CRACKED AT FRAME 15205 AND STRINGER 50. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900636 19990129 00636 EU 1999 1 29 QXEA9900053 1 19981208 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CLIP CRACKED AT FRAME 15205 AND STRINGER 49. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900637 19990129 00637 EU 1999 1 29 QXEA9900054 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CLIP CRACKED AT FRAME 15205 AND STRINGER 48. REPAIRED IAW FOKKER SRM 53-02-13. 2 L 7 2 4F RT A20EU 1999012900638 19990129 00638 EU 1999 1 29 QXEA9900055 1 19981218 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU EMER EXIT DRWAY CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CRACK ON SECOND LAYER SKIN ON LEFT-HAND AFT EMERGENCY EXIT DOOR APERTURE, AFT LOWER CORNER. REPAIRED IAW HORIZON AIR EA 4-53-648. 2 L 7 2 4F RT A20EU 1999012900639 19990129 00639 EU 1999 1 29 QXEA9900056 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS AREAS THAT ARE DIRTY AND REQUIRED PAINT. CLEANED AND PRIMED LEFT-HAND OUTBOARD S EAT TRACK ALONG THE ENTIRE LENGTH. 2 L 7 2 4F RT A20EU 1999012900640 19990129 00640 EU 1999 1 29 QXEA9900057 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE DIRTY A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND OUTBOARD SEAT TRACK HAS AREAS THAT ARE DIRTY AND REQUIRE PAINT. CLEANED AND PRIMED LEFT-HAND OUTBOARD S EAT TRACK ALONG THE ENTIRE LENGTH. 2 L 7 2 4F RT A20EU 1999012900641 19990129 00641 EU 1999 1 29 QXEA9900058 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 6305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS DAMAGE TO CENTER BASE SURFACE AND UPPER TRACK SURFACE AT FRAME 6305. REPAIRED IA W FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900642 19990129 00642 EU 1999 1 29 QXEA9900059 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 5805-6305 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS DAMAGE ON THE CENTER BASE SURFACE BETWEEN FRAME 5805 AND 6305. REPAIRED IAW FOKK ER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900643 19990129 00643 EU 1999 1 29 QXEA9900060 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION IN CENTER GROOVE BASE AT FRAME 9305. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900644 19990129 00644 EU 1999 1 29 QXEA9900061 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS CORROSION IN GROOVE BASE AT FRAME 9305B, 6 FORWARD OF FRAME. REPAIRED IAW FOKKER SRM 53-40-1 AND SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900645 19990129 00645 EU 1999 1 29 QXEA9900062 1 19981202 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS UPPER SURFACE DAMAGE AT FRAME 10346. REPAIRED IAW FOKKER SRM 53-02-15, FIGURE 2. 2 L 7 2 4F RT A20EU 1999012900646 19990129 00646 EU 1999 1 29 QXEA9900063 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10346 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS DAMAGE TO THE CENTER BASE SLOT AREA APPROXIMATELY 12 INCH LENGTH AFT OF FRAME 103 46. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900647 19990129 00647 EU 1999 1 29 QXEA9900064 1 19981130 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 9805 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS DAMAGE TO THE CENTER BASE SURFACE APPROXIMATELY 12 INCH LENGTH FORWARD OF FRAME 9 805. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARA 4B. 2 L 7 2 4F RT A20EU 1999012900648 19990129 00648 EU 1999 1 29 QXEA9900065 1 19981129 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 12414 DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND INBOARD SEAT TRACK HAS DAMAGE TO THE CENTER BASE SURFACE APPROXIMATELY 12 INCHES LONG, AFT OF FRAME 1241 4. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900649 19990129 00649 EU 1999 1 29 QXEA9900066 1 19981204 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - RIGHT-HAND INBOARD SEAT TRACK HAS CORROSION IN SEVERAL AREAS. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900650 19990129 00650 EU 1999 1 29 QXEA9900067 1 19981209 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - AFT CARGO DOOR HAS SURFACE CORROSION ON ALL FOUR EXTERNAL FRAME INNER SKIN FLANGES. REPAIRED IAW FOKKER SRM 51-10 -4. 2 L 7 2 4F RT A20EU 1999012900652 19990129 00652 EU 1999 1 29 QXEA9900069 1 19981221 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE MISINSTALLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - 5 RIVETS NOT FLUSH WITH SKIN IN REPAIR ABOVE RIGHT-HAND ACM. REPAIRED IAW HORIZON AIR EA 4-53-628. 2 L 7 2 4F RT A20EU 1999012900653 19990129 00653 EU 1999 1 29 QXEA9900070 1 19981221 A 5320 RIVET FOKKER F28 F28MK4000 4990810 EU FUSELAGE OUT OF POSITION A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 492US 11156 PDX - 4 LARGE RIVETS OUT OF LIMITS FOR EDGE DISTANCE AND ARE NOT FLUSH IN REPAIR ABOVE RIGHT-HAND ACM. REPAIRED IAW HOR IZON AIR EA 4-53-628. 2 L 7 2 4F RT A20EU 1999012900654 19990129 00654 EU 1999 1 29 QXEA9900071 1 19981210 A 5280 HINGE FOKKER F28 F28MK4000 4990810 EU LT MLG DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LEFT-HAND MAIN LANDING GEAR DOOR HINGE MOUNT SURFACE ON INSIDE WHEEL BAY STRUCTURE HAS STEP WEAR FROM HINGE. REPA IRED IAW FOKKER SRM 53-10-01, PAGE 6, PARAGRAPH B (4) (A). 2 L 7 2 4F RT A20EU 1999012900655 19990129 00655 EU 1999 1 29 QXEA9900072 1 19981203 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CENTER CARGO DOOR BOTTOM EDGE, FORWARD CORNER IS DENTED AND CRACKED. REPAIRED IAW HORIZON AIR EO 4-52-08E. 2 L 7 2 4F RT A20EU 1999012900656 19990129 00656 EU 1999 1 29 QXEA9900073 1 19981202 A 5313 STRINGER FOKKER F28 F28MK4000 4990810 EU FUSELAGE DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FORWARD END OF STRINGER 63 JUST AFT OF FWD PRESSURE BULKHEAD WAS DAMAGED WHILE GAINING ACCESS TO FUSELAGE DENT REP AIR. REPAIRED IAW FOKKER SRM 53-02-01, PAGE 8, FIGURE 6. 2 L 7 2 4F RT A20EU 1999012900657 19990129 00657 EU 1999 1 29 QXEA9900074 1 19981204 A 5230 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FORWARD CARGO DOOR BOTTOM EDGE FRAME HAS DENT WITH CRACK NEAR THE CENTER UNDER HINGE FITTING. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999012900658 19990129 00658 EU 1999 1 29 QXEA9900075 1 19981205 A 5320 ANGLE FOKKER F28 F28MK4000 4990810 EU FRAME 16060 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FLOOR SUPPORT ANGLE ON FRAME 16060 CRACKED UNDER 4 WAY TIE IN BRACKETS AT STRINGER 74 AND STRINGER 1. REPAIRED IA W FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999012900659 19990129 00659 EU 1999 1 29 QXEA9900076 1 19981213 A 5314 KEEL BEAM FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FRONT FUSELAGE KEEL BEAM IS CRACKED AT TOP INBOARD CORNER RADIUS AT PRESSURE BULKHEAD ATTACH ANGLE. REPAIRED IAW HORIZON AIR EA 4-53-630. 2 L 7 2 4F RT A20EU 1999012900660 19990129 00660 EU 1999 1 29 QXEA9900077 1 19981205 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 14285 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - HEAVY CORROSION ON FRAME 14285 AND STRINGER 74. REPAIRED IAW HORIZON AIR EA 4-53-607. 2 L 7 2 4F RT A20EU 1999012900661 19990129 00661 EU 1999 1 29 QXEA9900078 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CRACKED CLIP ON EXTERIOR SKIN FOR BELLY PANEL AT FRAME 13815B AND STRINGER 73. REPAIRED IAW FOKKER SRM 51-31-01 A ND SRM 51-31-05. 2 L 7 2 4F RT A20EU 1999012900662 19990129 00662 EU 1999 1 29 QXEA9900079 1 19981206 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CRACKED FRAME TO CASTILLATION CLIP AT FRAME 13815B AND STRINGER 73. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-3 1-05. 2 L 7 2 4F RT A20EU 1999012900663 19990129 00663 EU 1999 1 29 QXEA9900080 1 19981203 A 5320 CLIP FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - CRACKED FRAME TO CASTILLATION CLIP AT FRAME 13815B AND STRINGER 2. REPAIRED IAW FOKKER SRM 53-02-13, PAGE 4, FIGU RE 2. 2 L 7 2 4F RT A20EU 1999012900664 19990129 00664 EU 1999 1 29 QXEA9900081 1 19981206 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - AFT LOWER DME 2 ANTENNA MOUNTING SURFACE ON FUSELAGE SKIN ANTENNA OPENING HAS LIGHT CORROSION. REPAIRED IAW FOKK ER SRM 53-01-01, PAGE 6, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900665 19990129 00665 EU 1999 1 29 QXEA9900082 1 19981203 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FUSELAGE SKIN MARKER ANTENNA LOCATION HAS LIGHT CORROSION AT MOUNTING SURFACE ON FUSELAGE SKIN. REPAIRED IAW FOKK ER SRM 53-01-01, PAGE 6, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900666 19990129 00666 EU 1999 1 29 QXEA9900083 1 19981202 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - FUSELAGE SKIN RADIO/ALTIMETER ANTENNA MOUNT LOCATION HAS LIGHT SURFACE CORROSION ON FUSELAGE SKIN, AFT LOCATION. R EPAIRED IAW FOKKER SRM 53-01-01, PAGE 6, PARAGRAPH 4B. 2 L 7 2 4F RT A20EU 1999012900667 19990129 00667 EU 1999 1 29 QXEA9900084 1 19981209 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LIGHT SURFACE CORROSION UNDER BOTH HOOK LATCH COVER PLATES ON AFT CARGO DOOR FOR FORWARD CARGO PIT. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999012900668 19990129 00668 EU 1999 1 29 QXEA9900085 1 19981209 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - LIGHT SURFACE CORROSION UNDER BOTH HOOK LATCH COVER PLATES ON FORWARD CARGO DOOR FOR FORWARD CARGO PIT. REPAIRED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999012900669 19990129 00669 EU 1999 1 29 QXEA9900086 1 19981128 A 5415 BEAM FOKKER F28 F28MK4000 4990810 EU RT PYLON CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - SURFACE CORROSION ON WEB OF AFT ENGINE MOUNTING BEAM IN RIGHT-HAND STUB WING. REPAIRED IAW FOKKER SRM 51-10-4, PA GE 9, PARAGRAPH 5A(1). 2 L 7 2 4F RT A20EU 1999012900670 19990129 00670 EU 1999 1 29 QXEA9900087 1 19981128 A 5400 SHACKLE FOKKER F28 F28MK4000 4990810 EU RT PYLON CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - SURFACE CORROSION ON FORWARD SHACKLES IN RIGHT-HAND STUB WING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 5A (1). 2 L 7 2 4F RT A20EU 1999012900671 19990129 00671 EU 1999 1 29 QXEA9900088 1 19981128 A 5415 BEAM FOKKER F28 F28MK4000 4990810 EU ENGINE MOUNT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - SEVERAL SPOTS OF CORROSION ON THE FORWARD ENGINE MOUNTING BEAM. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAP H 5A (1). 2 L 7 2 4F RT A20EU 1999012900672 19990129 00672 EU 1999 1 29 QXEA9900089 1 19981124 A 5415 STRUT FOKKER F28 F28MK4000 4990810 EU NR 2 ENGINE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - NR 2 ENGINE DIAGONAL THRUST STRUT FOUND TO HAVE AREAS OF SURFACE CORROSION AND MINOR SCORING AND SCRATCHES. REPAI RED IAW FOKKER SRM 54-40-03. 2 L 7 2 4F RT A20EU 1999012900685 19990129 00685 WP 1999 1 29 99ZZZX432 1 19981018 A 3350 110049 BATTERY LKHEED 1011 1011385115 5265015 WP ROWS 8-15 DISCHARGED A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 198AT 2649 193B1111 DURING P/F, FOUND EMERGENCY LIGHTS INOPERABLE ON BOTH SIDES OF AIRCRAFT FROM SEATS 8 ABC TO 15 AB, AND 8 HJK TO 15 HJ. R EMOVED AND REPLACED BATTERY POWER SUPPLY AT R2 AND PERFORMED ADJUSTMENT AND TESTED NORMAL IAW 33-59-00. 2 L 7 3 4F A23WE 1999012900686 19990129 00686 EA 1999 1 29 99ZZZX433 1 19981126 A 2742 83963 ACTUATOR CNDAIR CL600 CL6002B19 EA HORIZ STABILIZER MALFUNCTIONED A ASOA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 SO 11 824AS 2411 7203 ATL/ROA - FLT 7289 - DURING CLIMB-OUT, ELEVATOR TRIM WOULD NOT TRIM BELOW 3 UNITS DOWN. CONTROLABILITY IMPROVED WITH RE DUCED AIRSPEED AND FLAPS. CREW DECLARED AN EMERGENCY AND RETURNED TO ATL, WHERE LANDING WAS MADE SAFELY AND WITHOUT FUR THER INCIDENT. ATL MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR. OPERATIONAL CHECKS WERE G OOD AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. 2 L 7 2 4F RT A21EA 1999012900687 19990129 00687 EU 1999 1 29 C2XA98IA469 1 19981202 A 3350 3013017 BATTERY PACK AEROSP ATR42 ATR42500 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15447 505 IAH - DURING MAINTENANCE VISIT INSPECTION, SEVERAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED A ND REPLACED AN EMERGENCY LIGHT POWER SUPPLY BATTERY PACK, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999012900688 19990129 00688 CE 1999 1 29 99ZZZX434 1 19981120 A 7603 BEARING 3010458 BEECH 99 C99 1154006 CE RT ENGINE STIFF A P FFSA E ENGINE SHUTDOWN O OTHER CR CRUISE 1 AL 01 575W U204 JUST AFTER LEVEL-OFF, THE RIGHT ENGINE WOULD NOT RESPOND TO POWER REDUCTIONS. IN ORDER TO NOT OVER-TORQUE THE ENGINE ON DESCENT, THE ENGINE WAS SHUT DOWN AND THE PROPELLER WAS FEATHERED. 1 L 7 2 3T A14CE 1999012900689 19990129 00689 1999 1 29 GAIA98126 4 19981123 A 3442 6225128001 RADAR SCOPE BOEING 727 727222 1384073 NM COCKPIT FAILED A GAIA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 90AX 20040 DAY - DURING DESCENT INTO DAY, SMOKE WAS OBSERVED COMING FROM THE TOP OF THE WEATHER DISPLAY UNIT ON THE CENTER CONSOLE, THEN THE DISPLAY SCREEN FLASHED. THE CREW IMMEDIATELY TURNED THE WEATHER RADAR SYSTEM OFF, THEN PULLED THE CIRCUIT BRE AKERS FOR THE SAME SYSTEM. THE SMOKE AND SMELL DISSIPATED QUICKLY. THE AIRCRAFT LANDING WITHOUT FURTHER PROBLEMS. REM OVED AND REPLACED WEATHER RADAR DISPLAY UNIT. OPERATIONALLY CHECKS NORMAL. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 3 4F A3WE 1999012900690 19990129 00690 NM 1999 1 29 HNAA9899368 1 19981023 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8201 2809001 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 993HA 17480 SBY23 457 TPA - FLT 3031 - NR 3 AND NR 4 RED ESCAPE PATH LIGHTS INOPERABLE. REMOVED AND REPLACED POWER SUPPLY BASE AND BATTERY PA CK 3352 PS2. PART TOTAL CYCLES: 19,975. (X) 2 H 7 2 4T RT A13NM 1999012900691 19990129 00691 NM 1999 1 29 HNAA9899391 1 19981221 A 3350 6013211X BATTERY PACK DHAV DHC8 DHC8201 2809001 NM CABIN DISCHARED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 993HA 5997 236 JAX120 457 JAX - FLT 3034 - SECOND STRIP OF FLOOR EMERGENCY PATH LIGHTS INOPERABLE. PART TOTAL CYCLES: 7,076. (X) 2 H 7 2 4T RT A13NM 1999012900692 19990129 00692 NM 1999 1 29 HNAA9899369 1 19981023 A 3350 6104791X BATTERY PACK DHAV DHC8 DHC8201 2809001 NM CABIN DISCHARGED A HNAA K NONE L NO TEST IN INSP/MAINT 1 EA 07 993HA 4828 3001 457 TPA - FLT 3031 - NR 3 AND NR 4 RED ESCAPE PATH LIGHTS INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY BASE AND BATTERY P ACK 3352 PS2. PART TOTAL CYCLES: 5,987. (X) 2 H 7 2 4T RT A13NM 1999012900693 19990129 00693 EA 1999 1 29 99ZZZX435 1 19981012 A 2610 24412047 SENSE LOOP CNDAIR CL600 CL6002B16 1900305 EA NR 1 ENGINE MALFUNCTIONED A J7SA O OTHER N FALSE WARNING CR CRUISE 1 SW 21 306FX 5175 DURING CRUISE, JET PIPE/PYLON 'OVHT' RED LIGHT ANNUNCIATED INTERMITTENTLY. FOUND THAT DURING PREVIOUS MAINTENANCE ON TH E TAIL PIPE LOOP, THE ATTACH BRACKET WAS SLIGHTLY BENT CAUSING THE CONNECTION TO CONTACT THE CLOSED ENGINE COWL, SHORTIN G TO GROUND, GIVING A FALSE INDICATION. 2 L 7 2 4F RT A21EA 1999012900694 19990129 00694 EA 1999 1 29 99ZZZX436 1 19981027 A 5312 6003201471 BULKHEAD CNDAIR CL600 CL6001A11 1900302 EA BS 409 CRACKED A J7SA K NONE O OTHER IN INSP/MAINT 1 SW 21 550CW 6029 1084 CRACKED BULKHEAD WEB AT FS 409. REF: SB 600-679. DATE SEPT 10, 1997. AD 97-24-02 AMEND 39-10209 EFFECT DATE 12-3-97. FS 409 REPAIRED ERGINEERING ORDER 600-53-175. 2 L 7 2 4F RT A21EA 1999012900695 19990129 00695 EA 1999 1 29 99ZZZX437 1 19981022 A 2435 23048004 GENERATOR DHAV DHC6 DHC6300 2802606 EA START/GENERATOR FAILED A KPVA O OTHER J WARNING INDICATION CR CRUISE 1 WP 13 709PV 1293 100 3397 640 PILOT REPORTED LOSS OF BOTH STARTER/GENERATORS IN CRUISE FLIGHT. SYSTEM TROUBLESHOOTING LEAD TO THE AIR CONDITIONING SY STEM BEING DEFERRED (21-1) CAUSING A SYSTEM OVERLOAD. AIRCRAFT WAS OPERATED IN DIFFERENT CONFIGURATIONS TO COME TO THIS CONCLUSION. AIRCRAFT WAS RETURNED TO SERVICE WITHOUT FURTHER SYSTEM FAILURES. UPON AIR CONDITIONING SYSTEM MAINTENANC E TO CLEAR THE MEL, MAINTENANCE DISCOVERED, DURING ELECTRICAL SYSTEM TROUBLESHOOTING, NR 1 GENERATOR HAD A HOLE BURNED I N THE BRUSH COVER. THE AFFECTED GENERATOR WAS REMOVED AND REPLACED, ALL AFFECTED SYSTEMS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE. 1 H 7 2 3T RT A9EA 1999012900696 19990129 00696 NE 1999 1 29 MASA98195 2 19981101 A 7261 4018T16P04 SEAL 6037T31G02 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE LT ENGINE FAILED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 17175 7175 872143 STL/PHL - FLT 5758 - AFTER DEPARTURE FROM STL, CAPTAIN NOTED A LEFT ENGINE LOW OIL PRESSURE MESSAGE ON EICAS. CREW DECL ARED AN EMERGENCY, SHUT DOWN THE ENGINE, AND DIVERTED TO CVG. AIRCRAFT WAS FERRIED TO BHM WHERE MAINTENANCE REPLACED TH E GARLOCK SEAL. OPS CHECKED GOOD, AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98ZZZX438. (X) 2 L 7 2 4F 4 F RT A21EA E15NE 1999012900697 19990129 00697 NE 1999 1 29 99ZZZX438 2 19981101 A 7261 5018T49P01 SEAL 6037T31G02 CNDAIR CL600 CL6002B19 EA GE CF34 CF343B1 NE LT ENGINE FAILED A MASA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 17175 7175 872143 STL/PHL - FLT 5758 - AFTER DEPARTURE FROM STL, CAPTAIN NOTED A LEFT ENGINE LOW OIL PRESSURE MESSAGE ON EICAS. CREW DECL ARED AN EMERGENCY, SHUT DOWN THE ENGINE, AND DIVERTED TO CVG. AIRCRAFT WAS FERRIED TO BHM WHERE MAINTENANCE REPLACED TH E GARLOCK SEAL. OPS CHECKED GOOD, AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR MASA98195. 2 L 7 2 4F 4 F RT A21EA E15NE 1999012900698 19990129 00698 EA 1999 1 29 MASA98190 1 19981027 A 2750 857SD100161 FLEXSHAFT 852D10011 CNDAIR CL600 CL6002B19 EA LT TE FLAP MALFUNCTIONED A MASA O OTHER J WARNING INDICATION AP APPROACH 1 SW 07 17175 7175 HPN/PHL - FLT 5807 - ON APPROACH TO PHL, A FLAP FAIL CAUTION MESSAGE ILLUMINATED. THE CREW DECLARED AN EMERGENCY DUE TO LANDING REQUIREMENTS, AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND LUBED THE FLAP FLEXSHAFT, AND C/W AD 98-20- 01. OPS CHECK GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999012900699 19990129 00699 EA 1999 1 29 MASA98194 1 19981101 A 2913 M832481216 O-RING PV304448 CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC PUMP FAILED A MASA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 17175 7175 MKE/PHL - FLT 5809 - EN ROUTE TO PHL, CREW RECEIVED A LOW OIL PRESSURE EICAS MESSAGE ON THE LEFT ENGINE. CREW DECLARED AN EMERGENCY AND SHUT DOWN THE LEFT ENGINE. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND R EPLACED THE O-RINGS ON THE HYDRAULIC PUMP, LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR 98 ZZZX439. (X) 2 L 7 2 4F RT A21EA 1999012900700 19990129 00700 EA 1999 1 29 99ZZZX439 1 19981101 A 2913 M832481241 O-RING PV304448 CNDAIR CL600 CL6002B19 1900309 EA HYDRAULIC PUMP FAILED A MASA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SW 07 17175 7175 MKE/PHL - FLT 5809 - EN ROUTE TO PHL, CREW RECEIVED A LOW OIL PRESSURE EICAS MESSAGE ON THE LEFT ENGINE. CREW DECLARED AN EMERGENCY AND SHUT DOWN THE LEFT ENGINE. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND R EPLACED THE O-RINGS ON THE HYDRAULIC PUMP, LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. REF: OPER CONTROL NR MA SA98194. 2 L 7 2 4F RT A21EA 1999012900701 19990129 00701 EA 1999 1 29 MASA98203 1 19981116 A 3350 1317 BULB BRUCE BC10020004 CNDAIR CL600 CL6002B19 EA CABIN FAILED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 17175 7175 PHL/MKE - FLT 5805 - DURING PREFLIGHT, CREW FOUND ONE EMERGENCY CEILING LIGHT INOPERATIVE. MAINTENANCE ACTION WAS DEFER RED PER MEL 33-51-1. AIRCRAFT WAS RETURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, THE BULB WAS REMOVED AND REPLACED. ( X) 2 L 7 2 4F RT A21EA 1999012900702 19990129 00702 EU 1999 1 29 RAIA981106 1 19981103 A 7714 31036061 TACH GENERATOR BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 862JX 862 FAT - FLT 4746 - RIGHT ENGINE RPM GAUGE FLICKERED AND WENT TO ZERO. MAINTENANCE REPLACED THE TACHOMETER GENERATOR INSER T. (X) 2 L 7 2 4T RT A56EU 1999012900703 19990129 00703 SO 1999 1 29 RAIA981104 1 19981103 A 3230 355022002MOD2 ELECTRONIC UNIT EMB 145 EMB145 SO LANDING GEAR FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 802HK 51 145066 ORD - FLT 5776 - LANDING GEAR WILL NOT RETRACT AND WING DEICE FAILED. MAINTENANCE REPLACED LANDING GEAR ELECTRONIC UNIT AND INSPECTED DEICE SYSTEM. FOUND TO WORK GOOD. (X) 2 L 7 2 4F RT T00011AT 1999012900704 19990129 00704 NM 1999 1 29 99ZZZX440 1 19981029 A 3610 540998 MANIFOLD BOEING 727 727260 NM NR 3 ENGINE CRACKED A P S84A E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 21 901PG 21978 ON CLIMB, NR 3 ENGINE FIRE DETECTION LIGHT REMAINED ILLUMINATED. ENGINE SHUT DOWN AFTER PERFORMING CHECK LIST ITEMS. A IRCRAFT RETURNED TO DEPARTURE AIRPORT AND LANDED WITHOUT INCIDENT. COMPANY MAINTENANCE DISCOVERED THE 13TH STAGE BLEED LINE SEPARATED AT 'T' (WELD AREA RUPTURED). 2 L 7 3 4F RT A3WE 1999012900705 19990129 00705 SO 1999 1 29 SIMA983354 1 19981201 A 3350 7287380501 LIGHT EMB 145 EMB145LR SO OVERWING EXIT INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 615AE 145087 ORD - FLT 4306 - OVERWING EMERGENCY FLOOR PROXIMITY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED OVERWING EXIT FLOOR PROXIMITY LIGHT STRIP. OPERATIONAL CHECK GOOD. (X) 2 L 7 2 4T RT T00011AT 1999012900706 19990129 00706 NM 1999 1 29 TSAA9833591 1 19981119 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED BATTERY PACK POSITIONS NR 2 AND NR 5 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO BEING INOPERABLE. OPS CHECK OK. AI RCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999012900707 19990129 00707 NM 1999 1 29 TSAA9833590 1 19981110 A 3350 P4010021 BATTERY BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 FORWARD RIGHT SIDE EMERGENCY FLASH LIGHT INOPERABLE. REPLACED BATTERY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4F RT A16WE 1999012900708 19990129 00708 NM 1999 1 29 TSAA9833602 1 19981127 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 6 EMERGENCY FLOOR PROXIMITY LIGHT BATTERY PACK ON AFT OVERHEAD ISLE EMERGENCY DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999012900709 19990129 00709 NM 1999 1 29 TSAA9833593 1 19981121 A 3350 873100151 LIGHT BOEING 737 737282C 13844AU NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 5 FLOOR LIGHT ASSY DUE TO BEING INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999012900710 19990129 00710 NM 1999 1 29 TSAA9833592 1 19981121 A 3350 900542 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED BATTERY PACK ON AFT OVERHEAD ISLE EMERGENCY EXIT SIGN DUE TO INTERMITTENT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999012900711 19990129 00711 EA 1999 1 29 VTZA98312 1 19981020 A 2751 WARNING LIGHT CNDAIR CL600 CL6002B19 EA TE FLAP ACTIVATED A VTZA O OTHER F FLT CONT AFFECTED TX TAXI/GRND HDL 1 EA 27 631BR 7261 IAD/BNA - FLT 6700 - DURING TAXI AT 0950 HRS ON 10-20-98, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WHICH W AS THE FLAP FAULT WARNING LIGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND COULD NOT DUPLICATE PROBLEM, OPS CHECK OK. AIRCRAFT RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999012900712 19990129 00712 EA 1999 1 29 VTZA98325 1 19981030 A 3020 WARNING LIGHT CNDAIR CL600 CL6002B19 EA ANTI ICE DUCT ACTIVATED A VTZA O OTHER N FALSE WARNING CR CRUISE 1 EA 27 632BR 7268 IAD/IND - FLT 6724 - DURING CRUISE ON 10-30-98 AT 1400 HOURS, EXPERIENCED AN ANTI-ICE DUCT WARNING LIGHT ON THE MASTER C AUTION PANEL. AIRCRAFT CONTACTED MAINTENANCE CONTROL AND DISPATCH. DECISION TO CONTINUE TO IND WAS MADE. UPON ARRIVAL AT IND, ACFT LANDED, AFTER DECLARING AN EMERGENCY AS A PRECAUTIONARY MEASURE, WITH NO FURTHER INCIDENT. MAINTENANCE TR OUBLESHOT SYSTEM AND PERFORMED GROUND RUNS, BUT COULD NOT DUPLICATE DISCREPANCY. ALL PERTINENT CHECKS ACCOMPLISHED. AC FT RELEASED FOR SERVICE. THERE HAS BEEN NO FURTHER DISCREPANCIES WITH THE SYSTEM SINCE THIS ONE OCCURRENCE. (X) 2 L 7 2 4F RT A21EA 1999012900713 19990129 00713 NM 1999 1 29 ASAA9840108 1 19981120 A 3397 WIRE BOEING 737 737490 1384715 NM ROWS 14-17 LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 705AS 29318 SEA - DURING MAINTENANCE CHECK THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 14-17. RE-CONNECTED WIRING/LIGHTS AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999012900715 19990129 00715 EU 1999 1 29 HCMA0000221 1 19980918 A 6420 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 194BH 849 2903 TAIL ROTOR BEARING WORN BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1999012900730 19990129 00730 NM 1999 1 29 USAA980636 1 19981217 A 5320 654587545 SILL BOEING 737 7373B7 1384580 NM BS 280-350 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 70 INCH ALONG FORWARD SERVICE DOOR 'Z' ANGLE LOWER SILL INBOARD CHORD ANGLE AT BS 280-350 RBL 35. CORROSION TASK NR C53-107-01. REPLACED PART PER BOEING 737-300 SRM 51- 40-02 AND 51-20-05. (M) 2 L 7 2 4F RT A16WE 1999012900731 19990129 00731 WP 1999 1 29 ORJA98325 1 19981220 A 7603 SWITCHES DOUG DC9 DC987 3022087 WP THROTTLE BANK CONTAMINATED A ORJA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 WP 11 752RA 49780 IN LAS - TAKEOFF DISCONTINUED FOR SPOILER DEPLOYED ANNUNCIATOR. THROTTLES WERE ADVANCED BUT TAKEOFF POWER NOT REACHED, SPEED APPROXIMATELY 20 KTS. CLEANED THROTTLE BANK SWITCHES SPOILER LIGHT SYSTEM. OPS CHECK OK. (M) 2 L 7 2 4F RT A6WE 1999012900732 19990129 00732 EU 1999 1 29 RAIA981229 1 19981218 A 3010 E420362 DEICE HORN AEROSP ATR42 ATR42300 8680920 EU RT AILERON FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 422TE 106 FLT 7178 - STL - RIGHT ELEVATOR HORN ANTI-ICE FAULT LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT ELEVATOR HORN. (M) 2 H 7 2 4T RT A53EU 1999012900733 19990129 00733 EU 1999 1 29 RAIA981216 1 19981218 A 3010 E420351 DEICE HORN AEROSP ATR42 ATR42300 8680920 EU LT AILERON FAILED A RAIA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 03 422TE 106 FLT 7178 - STL - LEFT AILERON HORN ANTIICE FAULT LIGHT ILLUMINATED. MAINTENANCE REPLACED LEFT AILERON HORN. (M) 2 H 7 2 4T RT A53EU 1999012900734 19990129 00734 1999 1 29 RAIA981234 4 19981231 A 3418 14127140401 STICK SHAKER JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 553HK 41066 FLT 7660 - JFK - STALL WARNING SYSTEM WOULD NOT TEST. MAINTENANCE REPLACED STICK PUSHER ASSEMBLY. (M) 2 L 7 2 4T RT A41NM 1999012900735 19990129 00735 EU 1999 1 29 RAIA981213 1 19981216 A 3233 6158E ACTUATOR BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 342TE 954 FLT 7306 - STL - NOSE LANDING GEAR INTRANSIT LIGHT STAYS ON WITH GEAR UP. MAINTENANCE REPLACED SEALS INSIDE OF NOSE GEA R RETRACT ACTUATOR. (M) 2 L 7 2 4T RT A56EU 1999012900736 19990129 00736 WP 1999 1 29 AALA982153 1 19981208 A 5320 JAMB DOUG DC9 DC982 3022082 WP CARGO DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 73444 49470 TUL - FOUND CORROSION ON MID CARGO LOWER DOOR SILL FRAME. CORROSION REMOVAL EXCEEDS MANUAL LIMITS. INSTALLED DOUBLER P ER AARD 53-10-00-3 FIG 2. INSTALLED DOUBLER PER AARD 53-10-00-3 FIG 2. (M) 2 L 7 2 4F A6WE 1999012900737 19990129 00737 WP 1999 1 29 AALA982230 1 19981220 A 3222 5910448557 STRUT DOUG DC9 DC982 3022082 WP NLG REQ'D SERVICE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 485AA 49678 STL - FLT 1966 - AFTER TAKEOFF MCI EN ROUTE ORD, THE NOSE WHEEL LANDING GEAR WOULD NOT RETRACT. CYCLED GEAR THREE TIMES WITH SAME RESULTS. AIR INTERRUPTED AND LANDED STL WITHOUT INCIDENT. SERVICED NOSE STRUT AND PERFORMED GEAR SWING. SY STEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999012900738 19990129 00738 EU 1999 1 29 DKAA98027 1 19981214 A 5320 MY202672001 WINDSHIELD FRAME AMD FALC20 FALCON 2720302 EU LT COCKPIT CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 108R 24596 108 LEFT WINDSHIELD FRAME FOUND CRACKED DURING EDDY CURRENT INSPECTION 53-30-13. (M) 2 L 7 2 4F A7EU 1999012900739 19990129 00739 EU 1999 1 29 DKAA98025 1 19981214 A 5320 MY202682001 WINDSHIELD AMD FALC20 FALCON 2720302 EU RT COCKPIT CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 108R 24596 108 RIGHT WINDSHIELD FRAME FOUND CRACKED DURING EDDY CURRENT INSPECTION 53-30-13. (M) 2 L 7 2 4F A7EU 1999012900740 19990129 00740 EU 1999 1 29 DKAA98026 1 19981214 A 5320 MY202612001 WINDSHIELD FRAME AMD FALC20 FALCON 2720302 EU CENTER COCKPIT CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 108R 24596 108 CENTER WINDSHIELD FRAME FOUND CRACKED DURING EDDY CURRENT INSPECTION 53-30-13. (M) 2 L 7 2 4F A7EU 1999012900741 19990129 00741 NM 1999 1 29 99ZZZM35 1 19981227 A 3350 6104781 BATTERY DHAV DHC8 DHC8103 1386005 NM CABIN DISCHARGED A KPVA K NONE L NO TEST IN INSP/MAINT 1 WP 13 805WP 353 HNL - DISCREPANCY FOUND DURING MAINTENANCE DAILY INSPECTION, CABIN EMERGENCY LIGHTS DID NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERIES. 2 H 7 2 4T RT A13NM 1999012900742 19990129 00742 WP 1999 1 29 HALA9800418 1 19981217 A 2530 OVEN DOUG DC10 DC1010 3022110 WP GALLEY FAILED A HALA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 125AA 46525 FLT 21 - HNL - OVEN NR 3 STARTED TO SMOKE IN FLIGHT. INSPECTION SHOWED THIS WAS NOT DUE TO MEAL BURNING. SMOKE CAME OU T THROUGH BOTTOM OF OVEN ONLY. OPS CHECK, OF NR 3 OVEN FOUND NO SMOKE COMING FROM OVEN. AFTER 45 MINUTES OF OP AT 375 DEGREES, OK THIS STATION LAX. (M) 2 L 7 3 4F A22WE 1999012900743 19990129 00743 WP 1999 1 29 HALA9800420 1 19981218 A 3010 SWITCH DOUG DC10 DC1010 3022110 WP WING DEICE FAILED A HALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 13 116AA 46516 HNL - FLT 938 - UPON ENTERING AREA OF POSSIBLE ICING WE TURNED ON WING ANTI-ICE. AFTER ABOUT 30 SECONDS TO 1 MINUTE MAN IFOLD NR 1 FAIL LIGHT CAME ON, COMPLETED, CHECKLIST. AIRCRAFT RETURNED TO HNL, WHERE IT MADE AN UNEVENTFUL LANDING. (M ) 2 L 7 3 4F A22WE 1999012900744 19990129 00744 1999 1 29 GAIA98113 4 19981111 A 3418 2566A21 AOA VANE BOEING 727 727223 1384074 NM FUSELAGE BIRD STRIKE A GAIA B A EMER. DESCENT UNSCHED LANDING C F.O.D. CL CLIMB 1 SW 07 6838 20191 AFTER TAKEOFF AT HUF, AT APPROXIMATELY 200 FT, AIRCRAFT WAS STRUCK BY THREE BIRDS IN THE NOSE AREA OF THE AIRCRAFT. AT LEAST THREE LOAD THUMPS WERE HEARD. STALL WARNING STICK SHAKER CAME ON IMMEDIATELY AFTER THUMPS WERE NOTED. AIRCRAFT D ECLARED AN EMERGENCY AND RETURNED TO HUF WITHOUT FURTHER DIFFICULTY. THE STICK SHAKER REMAINED ON UNTIL TOUCH-DOWN. PE RFORMED OVERWEIGHT LANDING INSPECTION PER BOEING MAINTENANCE MANUAL 5-51-271 AND NO DEFECTS WERE NOTED. PERFORMED BIRD STRIKE INSPECTION PER BOEING MM 5-51-41 AND NO STRUCTUAL DAMAGE WAS NOTED. FOUND DAMAGE TO THE AOA VANE FOR THE STALL W ARNING SYSTEM. REPLACED THE AOA VANE PER THE BOEING MM AND FUNCTIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SER 2 L 7 3 4F A3WE 1999012900745 19990129 00745 NM 1999 1 29 P2EA98224 1 19981101 A 2130 PRESSURIZATION BOEING 737 737247 138448D NM CABIN MALFUNCTIONED A P2EA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 05 912MP 19607 MDW - FLT 815 - AIR RETURN, NO EMERGENCY DECLARED LANDING UNEVENTFUL. AIRCRAFT ON DEPARTURE FROM MDW WOULD NOT PRESSURI ZE IN AUTO, STANDBY, OR MANUAL. (M) 2 L 7 2 4F A16WE 1999012900746 19990129 00746 WP 1999 1 29 HALA9800404 1 19981210 A 2120 AIR DIST DOUG DC10 DC1010 3022110 WP CABIN ODOR A HALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 13 125AA 46525 LAX - FLT 1 - STRONG ODOR IN CABIN AND COCKPIT, ABORTED FLIGHT. AIRCRAFT RETURNING TO LAX. ACCOMP CLEANING OF HEAT EXC HANGERS PER MM 21-53-01. CLEANED APU INLET, RAN ENGINES 1 AT A TIME WITHOUT APU RUNNING TRYING TO ISOLATE THE SMELL OF OIL OR THE SOURCE. NO HELP. FOUND RESIDUAL, OIL IN APU COMPARTMENT AND INLET AREA. CLEANED UP OIL. ACCOMPLISHED HEAT EXCHANGER CLEAN OUT PROCEDURES PER MM 21-53-01 PAGES 209-210. REPLACED COALESCAR BAGS AND CABIN RECIRCULATION FILTERS. ACCOMPLISHED TAKEOFF POWER RUN WITH ALL PNEUMATIC SYSTEMS ON AIRCRAFT PACKS ON, NO STRONG ODOR DETECTED THROUGHOUT CA BIN OR COCKPIT, OK FOR SERVICE. (M) 2 L 7 3 4F A22WE 1999012900747 19990129 00747 CE 1999 1 29 MASA98227 1 19981220 A 3330 RETRACT MECH BEECH 1900 1900D 1154162 CE LANDING GEAR MALFUNCTIONED A MASA O OTHER J WARNING INDICATION CR CRUISE 1 SW 07 95YV UE95 FLT 6457 - FHU - PHX - DURING FLIGHT CREW NOTICED GEAR UNSAFE LIGHTS, AND GEAR NOT UP AND LOCKED IN THE GEAR WELL. FLIGH T CONTINUED AND LANDED IN PHX WITHOUT INCIDENT. AIRCRAFT WAS FERRIED TO FMN, WHERE MAINTENANCE TROUBLESHOT, AND COULD N OT DUPLICATE THE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999012900748 19990129 00748 CE 1999 1 29 MASA98224 1 19981215 A 6120 5038912121 SWITCH BEECH 1900 1900D 1154162 CE RT ENGINE FAILED A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 144ZV UE144 FLT 5331 - RDG-LNS - AFTER DEPARTURE, PILOT REPORTED THAT THE AUTOFEATHER DISABLE LIGHT ILLUMINATED AND THE RIGHT SIDE A UTOFEATHER WOULD NOT WORK. AIRCRAFT RETURNED TO RDG WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE HIGH PRESSURE S WITCH, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999012900749 19990129 00749 NM 1999 1 29 MASA98228 1 19981220 A 3350 6519023 LIGHTS DHAV DHC8 DHC8202 2809007 NM CABIN DEFECTIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 448YV 448 FLT 6342 - PSP-PHX - AFTER FLIGHT, CREW REPORTED TWO FLOOR TRACK LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE DEFECTIVE TRACK AND AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999012900750 19990129 00750 NM 1999 1 29 MASA98226 1 19981217 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 07 449YV 449 FLT 6230 - PHX-MTJ - AS AIRCRAFT TAXIED FROM THE GATE, THE FLIGHT ATTENDANT TESTED THE EMERGENCY LIGHTS AND THEY WERE IN OPERATIVE. AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE BATTERY PACKS. OPS CHECK GOOD. AI RCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999012900751 19990129 00751 NM 1999 1 29 MASA98230 1 19981231 A 3350 6038443 POWER SUPPLY DHAV DHC8 DHC8202 2809007 NM CABIN DISCHARGED A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 449YV 449 FLT 6251 - PHX-DRO - PRIOR TO DEPARTURE, CREW REPORTED THAT SEVERAL EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REPLACED ALL THE EMERGENCY BATTERIES. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999012900752 19990129 00752 WP 1999 1 29 99ZZZM36 2 19981230 A 7320 8974575 BYPASS VALVE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP RT ENGINE INOPERATIVE A MEJA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SW 17 438MA 88082651720 AC721B P44036 DURING TAKEOFF FROM POS, THE RIGHT ENGINE EXPERIENCED A LOSS OF TORQUE AND THE TAKEOFF WAS ABORTED. A STATIC RUN UP WAS COMPLIED WITH FOR BOTH ENGINES AND WAS SATISFACTORY. THE CAPTAIN ATTEMPTED A SECOND TAKEOFF, THE LOSS OF TORQUE WAS EX PERIENCED AGAIN AND THE SECOND TAKEOFF ABORTED. MAINTENANCE REMOVED AND REPLACED THE RIGHT TORQUE LIMITER-BY-PASS VALVE WITH AN OVERHAULED UNIT. THE GROUND POWER AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A8SW E4WE 1999012900754 19990129 00754 NE 1999 1 29 99ZZZM38 2 19981226 A 7260 312081601 SEAL BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE LT ENGINE LEAKING A JJBA K NONE K FLUID LOSS IN INSP/MAINT 1 EA 01 860CA 113 UE134 114147 OIL LEAK FROM RIGHT ENGINE ACCESSORY SECTION. INVESTIGATION AND INSPECTION FOUND FUEL CONTROL UNIT GARLOCK SEAL LEAKING . REPLACED WITH NEW GARLOCK SEAL. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999012900755 19990129 00755 SO 1999 1 29 C2XA98CL081 1 19981219 A 3250 3085501003 MANIFOLD EMB 120 EMB120RT SO NLG STEERING FAILED A C2XA K NONE O OTHER TX TAXI/GRND HDL 1 SW 09 58733 17716 120197 CLE - FLT 3294 - CREW REPORTED THAT THE NOSE WHEEL STEERING FAILED COMPLETELY DURING LANDING WHEN THE NOSE WHEEL TOUCHED DOWN. THE CREW ALSO REPORTED LITTLE TO NO ABILITY TO CONTROL DIRECTION ON THE GROUND. MAINTENANCE INSPECTED THE AIRC RAFT THEN REMOVED AND REPLACED THE STEERING MANIFOLD IAW EMB-120 MM 32-50-04, OPERATIONAL AND LEAK CHECKS WERE SATISFACT ORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900756 19990129 00756 NM 1999 1 29 USAABB98116 1 19981213 A 2612 FIRE WARNING BOEING 757 757225 1384959 NM NR 1 ENGINE ACTIVATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 601AU 22193 MCO - FLT 1190 - CLIMBING THROUGH FL140 OUT OF MCO, CREW RECEIVED NR 1 ENGINE FIRE WARNING. CREW RETARDED THE NR 1 THRO TTLE, AND THE FIRE WARNING CEASED. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE PERFORMED T HE FIRE/OVERHEAT BITE AND RAN THE ENGINE FOR APPROXIMATELY 20 MINUTES. NO PROBLEMS COULD BE FOUND. (M) 2 L 7 2 4F RT A2NM 1999012900757 19990129 00757 NM 1999 1 29 EISA98284 1 19981204 A 2613 OVERHEAT LIGHT BOEING 727 727223 1384074 NM LOWER AFT BODY ILLUMINATED A EISA K NONE N FALSE WARNING CR CRUISE 1 SW 07 6813 19488 SHORTLY AFTER SELECTING WING ANTI-ICE ON, THE LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, EXTINGUISHED AFTER TURNING OFF ENGINE NR 3 ANTI-ICE. ENGINE NR 1 OPENED NORMAL. OPS CHECKED IN AIR AND GROUND MODES, OPS CHECKED NORMAL IAW MM CHAPTE R 26. (M) 2 L 7 3 4F A3WE 1999012900758 19990129 00758 EU 1999 1 29 C2XA98IA516 1 19981220 A 5320 S536780092002 JAMB AEROSP ATR42 ATR42320 8680930 EU PAX DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE PASSENGER DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE THRESHOLD IAW THE ATR 42-320 SRM 51-21-42. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999012900759 19990129 00759 EU 1999 1 29 C2XA98IA517 1 19981220 A 5320 S5367131828001 JAMB AEROSP ATR42 ATR42320 8680930 EU SERVICE DOORWAY CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14821 160 IAH - DURING C-CHECK INSPECTION, THE SERVICE DOOR THRESHOLD WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE TH RESHOLD IAW THE ATR 42-320 SRM 51-21-42. THE AIRCRAFT WAS THEN APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999012900760 19990129 00760 SO 1999 1 29 C2XA98BT084 1 19981210 A 3240 429512 CONTROL UNIT EMB 145 EMB145 SO BRAKE SYSTEM FAILED A C2XA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 SW 09 15941 145035 BRAKE FAIL MESSAGE, BRAKE INBOARD AND OUTBOARD INOPERATIVE. REMOVED AND REPLACED BRAKE CONTROL UNIT. OPS CHECKED GOOD. (M) 2 L 7 2 4F RT T00011AT 1999012900761 19990129 00761 EU 1999 1 29 VTZA98254 1 19980809 A 2900 HYDRAULIC SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU LT/RT REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 333UE 41101 FLT 6522 - IAD-RIC - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO HYDRAULIC PSI FELL BELOW LIMITS AFTER G EAR RETRACTION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SERVICED HYDRAULIC SYSTE M, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999012900762 19990129 00762 NM 1999 1 29 USAASB98285 1 19981027 A 2130 PRESSURIZATION BOEING 737 7373B7 1384580 NM CABIN MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 528AU 24410 PIT - FL 741 - DURING CLIMB-OUT FROM PIT, AIRCRAFT FAILED TO PRESSURIZE IN AUTO, STANDBY OR MANUAL MODES. CREW CLIMBED THE AIRCRAFT TO 7,000 FT, THEN RETURNED TO FIELD AT PIT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECL ARED. MAINTENANCE PRESSURIZED AIRCRAFT MANUALLY AND CHECKED AUTO PRESSURIZATION PER BOEING MAINTENANCE MANUAL 21-30-00. OPERATIONAL CHECK GOOD. COULD NOT DUPLICATE FAULT. (M) 2 L 7 2 4F RT A16WE 1999012900763 19990129 00763 NM 1999 1 29 99ZZZM39 1 19981110 A 2424 GCU BOEING 737 737201 1384454 NM NR 2 MALFUNCTIONED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 244US 22752 DTW - FL2232, EN ROUTE FROM CLT TO DTW, FLIGHT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL AFT OF FORWARD BULKH EAD AROUND SEAT ROWS 4, 5 AND 6. SHORTLY THEREAFTER, THE CIRCUIT BREAKERS FOR THE NR 2 AFT FUEL BOOST PUMP AND NR 2 TR TRIPPED. THE NR 2 TR READ 0 AMPS AND 28 VOLTS. INTERMITTENTLY, THE LEFT ANTI-SKID OFF AND FIRST OFFICER AUX PITOT STAT IC AMBER LIGHTS ILLUMINATED, PMS EXTERNAL FAIL WITH CODES 96 AND 99 AND A FLAG IN THE NR 2 EPR GAUGE. ON DESCENT, ALL L IGHTS AND FLAGS WENT OUT AND PMS OPERATED NORMALLY. CREW DID NOT RESET BOOTS PUMP OR TR CIRCUIT BREAKERS TO AVOID THE P OSSIBLE RETURN OF THE BURNING ODOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED APPLICABLE WIRING. RE 2 L 7 2 4F A16WE 1999012900764 19990129 00764 NM 1999 1 29 99ZZZM40 1 19981110 A 2433 1032575 TRU BOEING 737 737201 1384454 NM NR 2 MALFUNCTIONED A USAA K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 EA 19 244US 22752 DTW - FL2232, EN ROUTE FROM CLT TO DTW, FLIGHT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL AFT OF FORWARD BULKH EAD AROUND SEAT ROWS 4, 5 AND 6. SHORTLY THEREAFTER, THE CIRCUIT BREAKERS FOR THE NR 2 AFT FUEL BOOST PUMP AND NR 2 TR TRIPPED. THE NR 2 TR READ 0 AMPS AND 28 VOLTS. INTERMITTENTLY, THE LEFT ANTI-SKID OFF AND FIRST OFFICER AUX PITOT STAT IC AMBER LIGHTS ILLUMINATED, PMS EXTERNAL FAIL WITH CODES 96 AND 99 AND A FLAG IN THE NR 2 EPR GAUGE. ON DESCENT, ALL L IGHTS AND FLAGS WENT OUT AND PMS OPERATED NORMALLY. CREW DID NOT RESET BOOTS PUMP OR TR CIRCUIT BREAKERS TO AVOID THE P OSSIBLE RETURN OF THE BURNING ODOR. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED APPLICABLE WIRING. RE 2 L 7 2 4F A16WE 1999012900765 19990129 00765 WP 1999 1 29 ORJA98307 1 19981207 A 2710 CONTROLS DOUG DC9 DC982 3022082 WP AILERONS GRINDING A ORJA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 WP 11 824RA 53017 IN RNO - RETURN TO GATE, DURING TAXI CHECKS GRINDING NOISE HEARD UNDER COCKPIT FLOOR WHEN AILERONS CHECKED. UPON RETURN TO GATE INSPECTED ALL CABLES IN E/E BAY UNDER COCKPIT FLOOR FOUND NO GRINDING NOISES OPERATED AILERON SYSTEM NUMEROUS T IMES RT AND LT. LT AND RT OPS CHECK NORMAL AT THIS TIME OK FOR CONTINUED SERVICE. (M) 2 L 7 2 4F A6WE 1999012900766 19990129 00766 NM 1999 1 29 USAASB98308 1 19981119 A 4960 38762594 SWITCH BOEING 737 737401 1384701 NM APU MALFUNCTIONED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 413US 23882 BWI - FLT 1168, FLIGHT DEPARTED BWI WITH THE NR 1 GENERATOR ON MEL. AT APPROXIMATELY FL230, THE APU SHUTDOWN AUTOMATICA LLY DUE TO AN OVERSPEED LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT BWI SINCE THE AIRCRAFT WAS DOWN TO ONE ELECT RICAL SOURCE. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RAN THE APU AND OPERATED THE SYS TEM UNDER LOAD. CHECKS OK. CHECKED APU OIL LEVEL. CHECKED GOOD. REPLACED APU THREE SPEED SWITCH AND THE APU M280 MOD ULE AS PRECAUTIONARY. APU STARTED AND LOAD CHECKS OK. (M) 2 L 7 2 4F RT A16WE 1999012900767 19990129 00767 NM 1999 1 29 99ZZZM41 1 19981119 A 4960 655280131 MODULE BOEING 737 737401 1384701 NM APU MALFUNCTIONED A USAA A UNSCHED LANDING J H WARNING INDICATION ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 413US 23882 BWI - FLT 1168, FLIGHT DEPARTED BWI WITH THE NR 1 GENERATOR ON MEL. AT APPROXIMATELY FL230, THE APU SHUTDOWN AUTOMATICA LLY DUE TO AN OVERSPEED LIGHT WAS ILLUMINATED. FLIGHT RETURNED TO FIELD AT BWI SINCE THE AIRCRAFT WAS DOWN TO ONE ELECT RICAL SOURCE. FLIGHT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RAN THE APU AND OPERATED THE SYS TEM UNDER LOAD. CHECKS OK. CHECKED APU OIL LEVEL. CHECKED GOOD. REPLACED APU THREE SPEED SWITCH AND THE APU M280 MOD ULE AS PRECAUTIONARY. APU STARTED AND LOAD CHECKS OK. (M) 2 L 7 2 4F RT A16WE 1999012900768 19990129 00768 WP 1999 1 29 USAAD98217 1 19981221 A 3260 SENSOR DOUG DC9 DC931 3022065 WP RT MLG OUT OF ADJUST A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 918VJ 48138 PIT-AVP - FLT 1182 - UPON LANDING GEAR RETRACTION AFTER TAKEOFF, THE RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED. THE GEAR WAS EXTENDED AND ALL INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTEN ANCE ADJUSTED THE RIGHT GEAR UPLOCK SENSOR. THE LANDING GEAR WAS SWUNG AND ALL INDICATIONS WERE NORMAL. (M) 2 L 7 2 4F A6WE 1999012900769 19990129 00769 NM 1999 1 29 USAASB98343 1 19981231 A 2915 316565 VALVE BOEING 737 7372B7 1384560 NM MLG WW FAILED A USAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 284AU 40205 23131 MCO - FL2695 - EN ROUTE FROBWI TO MCO, SOUTHEAST OF SAV, FLIGHT LOST 'A' SYSTEM HYDRAULICS. CREW WENT TO ALTERNATE FLAP EXTENSION PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT LANDED AT MCO WITHOUT INCIDENT AND WAS TOWED OFF THE RUNWAY AND THEN TO THE GATE. MAINTENANCE INSPECTED AIRCRAFT FOR LEAKS. SECURED 'A' SYSTEM SUPPLY LINE FOR THE NR 1 ENGINE AND RE MOVED AND REPLACED THE HYDRAULIC RESERVOIR PRESSURE RELIEF VALVE AND PRESSURE REGULATOR. LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999012900770 19990129 00770 NM 1999 1 29 99ZZZM42 1 19981231 A 2910 72909 REGULATOR BOEING 737 7372B7 1384560 NM MLG WW FAILED A USAA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 284AU 19354 23131 MCO - FL2695 - EN ROUTE FROBWI TO MCO, SOUTHEAST OF SAV, FLIGHT LOST 'A' SYSTEM HYDRAULICS. CREW WENT TO ALTERNATE FLAP EXTENSION PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT LANDED AT MCO WITHOUT INCIDENT AND WAS TOWED OFF THE RUNWAY AND THEN TO THE GATE. MAINTENANCE INSPECTED AIRCRAFT FOR LEAKS. SECURED 'A' SYSTEM SUPPLY LINE FOR THE NR 1 ENGINE AND RE MOVED AND REPLACED THE HYDRAULIC RESERVOIR PRESSURE RELIEF VALVE AND PRESSURE REGULATOR. LEAK CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999012900771 19990129 00771 NM 1999 1 29 USAASB98340 1 19981229 A 3397 WIRE BOEING 737 7372B7 1384560 NM CABIN BROKEN A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 269AU 22881 PIT - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT FAULT TO THE M192 BATTERY PACK CANNON PLUG D1494, PIN 5. REPAIRED GROUND WIRE FROM PIN NR 5 ON CANNON PLUG D1494. OPERATIONAL C HECK GOOD. (M) 2 L 7 2 4F A16WE 1999012900772 19990129 00772 NM 1999 1 29 USAASB98330 1 19981217 A 3230 2732512 CABLE BOEING 737 737301 1384611 NM RT MLG OUT OF ADJ A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 341US 23510 CLT - FL2220 - FLIGHT RETUNRED TO FIELD AT CLT DUE TO FAILURE OF THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE UP POSITI ON. THE LANDING GEAR WOULD NOT RETRACT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ADJUSTED THE GROUND SPOIL ER TELEFLEX CABLE IN ASSOCIATION WITH MM 27-62-51. PERFORMED FUNCTIONAL TEST PER MM 27-62-51. (M) 2 L 7 2 4F RT A16WE 1999012900773 19990129 00773 NM 1999 1 29 USAASB98325 1 19981212 A 2150 693731986 CONTROL PANEL BOEING 737 737201 1384454 NM COCKPIT MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 265AU 22962 PIT - FL2053 - FLIGHT DIVERTED TO PIT DUE TO THE LEFT WING TO BODY OVERHEAT LIGHT CONTINUOUSLY FLICKERING FLIGHT. FLIGH T LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND OPERATIONALLY CHECKED THE LEFT WING TO BODY OVERHEAT DETECTION LOO P. NO DEFECTS NOTED. UNABLE TO DUPLICATE PROBLEM. REMOVED AND REPLACED THE P5-10 AIR CONDITIONING CONTROL PANEL AS PR ECAUTIONARY. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F A16WE 1999012900774 19990129 00774 NM 1999 1 29 USAA129812 1 19981231 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 6101 21244 FLIGHT 6140 - LGA-BOS - FOUND ON L/S CHECK, EMERGENCY EXIT ON CEILING AFT OF LIFE RAFT COMPARTMENT INOPERATIVE. REPLACE D BATTERY PACK, CHECK OK. (M) 2 L 7 3 4F A3WE 1999012900775 19990129 00775 NE 1999 1 29 USAA129808 2 19981219 A 7200 ENGINE BOEING 727 727254 138408L NM PWA JT8 JT8D7B 52053 NE NR 1 VIBRATES A USAA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 EA 19 913TS 20250 649622 NR 1 ENGINE VIBRATION ABNORMAL ON START BETWEEN 35-45 PERCENT N2. AT REDUCED TAKEOFF POWER 1.81 EPR, N1 INDICATION 96 P ERCENT VS 91 PERCENT ON NR 2 AND NR 3 ENGINES. IN FLIGHT VIBRATION IN TAIL SECTION OF CABIN NOTED. EMERGENCY WAS NOT D ECLARED, ENGINE WAS NOT SHUT DOWN, RETURNED FROM FLT TO DCA. REPLACED NR 1 ENGINE PER MM 72-00-00, TS088R9, TS089R6, TS 090R3. ENGINE RUNUP CHECKS OK. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999012900776 19990129 00776 NM 1999 1 29 USAA129809 1 19981228 A 3350 900835A BATTERY PACK BOEING 727 727227 1384078 NM ROW 29 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 924TS 924 21041 FLT 6141 - BOS-LGA - FOUND ON L/S CHECK, CEILING EMERGENCY EXIT LIGHT AT ROW 29 INOPERATIVE. REPLACED BATTERY PACK, OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999012900777 19990129 00777 NM 1999 1 29 USAABB98118 1 19981220 A 3610 312N53217 DUCT BOEING 757 757225 1384959 NM LT ENGINE LEAKING A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 601AU 22193 CLT - FL 795, AFTER TAKEOFF, CREW RECEIVED FIRE WARNING LIGHT AND FIRE WARNING BELL FOR LEFT ENGINE. CREW REDUCED POWER AND THE INDICATIONS EXTINGUISHED. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE H P 6 DUCT ASSEMBLY LEAKING AND REPLACED IT. (M) 2 L 7 2 4F RT A2NM 1999012900778 19990129 00778 WP 1999 1 29 USAAD98214 1 19981213 A 2160 DC26F106C CONNECTOR DOUG DC9 DC931 3022065 WP COCKPIT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 983VJ 48159 CLT-CHA - FLT 334 - AFTER TAKEOFF THERE WERE FUMES IN THE CABIN. THE FUMES DISSIPATED QUICKLY BUT THE CAPTAIN CHOSE TO RETURN TO THE FIELD. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT PACK INOPERATIVE IN AUTO TEMP MO DE. THE TEMP CONTROL VALVE WAS DRIVEN TO FULL HOT. THE SYSTEM OPERATED NORMALLY IN THE MANUAL MODE. THE AIRCRAFT WAS RELEASED FOR FLIGHT WITH THE LEFT AUTO TEMP CONTROL SYSTEM INOPERATIVE UNDER MEL PROVISIONS. DURING MAINTENANCE OVERNIG HT THE COCKPIT TEMPERATURE SENSOR CONNECTOR WAS REPLACED. (M) 2 L 7 2 4F A6WE 1999012900779 19990129 00779 WP 1999 1 29 USAAD98220 1 19981126 A 3350 60030451LB POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 816US 48096 PIT - THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 27 THROUGH 29. MAINTENANCE REPLACED THE AFFECTED EMER GENCY LIGHT POWER SUPPLY. (M) 2 L 7 2 4F A6WE 1999012900780 19990129 00780 1999 1 29 USAAD98218 4 19981219 A 2565 13621224 SLIDE DOUG DC9 DC931 3022065 WP TAIL CONE FAILED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 963VJ 47508 PIT - DURING A FUNCTIONAL CHECK, THE TAIL CONE EMERGENCY EVACUATION SLIDE FAILED TO DEPLOY AUTOMATICALLY. MAINTENANCE R EPLACED THE TAIL CONE EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F A6WE 1999012900781 19990129 00781 NM 1999 1 29 99ZZZM43 1 19981016 A 3350 1000679 LIGHT BOEING 737 737242 1384477 NM CABIN INOPERATIVE A PIDA K NONE L NO TEST IN INSP/MAINT 1 SO 05 159PL 21186 AFT PASSENGER DOOR INTERIOR EMERGENCY EXIT LIGHT ASSY INOPERATIVE. REPLACE LIGHT ASSY WITH SERVICEABLE UNIT AND OPS CHE CK NORMAL IAW B737 WDM 33-51-01 PAGE 31. (M) 2 L 7 2 4F A16WE 1999012900782 19990129 00782 NM 1999 1 29 USAASB98339 1 19981222 A 5610 PPG5893543109 WINDSHIELD BOEING 737 737401 1384701 NM LT COCKPIT CRACKED A USAA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 19 412US 20166 23881 PIT - FL735 - EN ROUTE FROM PHL TO MCI, THE UPPER RIGHT CORNER OF CAPTAINS WINDSHIELD CRACKED AND BEGAN ARCING. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE C APTAINS L1 WINDSHIELD. ALSO, REPLACED THE CAPTAINS WINDSHIELD HEAT CONTROLLER (P/N 231-2) AS PRECAUTIONARY. OPERATIONA L CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012900783 19990129 00783 NM 1999 1 29 USAASB98338 1 19981222 A 3260 189929 SENSOR BOEING 737 737401 1384701 NM LT MLG OUT OF ADJUST A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 421US 23988 PIT - PILOT REPORTED THE LEFT MAIN LANDING GEAR UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND LIGHT EXTINGUISHED. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND EXCESSIVE GAP ON LEFT MAIN LANDING GEAR UPLOCK SENSOR. REPLACED SENSOR AND ADJUSTED PER MM 32-61-00. SWUNG GEAR SEVERAL TIMES. OPERATI ONAL CHECK GOOD. ALL GEAR INDICATIONS NORMAL. (M) 2 L 7 2 4F RT A16WE 1999012900784 19990129 00784 NM 1999 1 29 USAASB98333 1 19981219 A 2824 10605298 CROSSFEED BOEING 737 737401 1384701 NM NR 2 FUEL CELL FAILED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 417US 29212 23984 ABQ - FL 165 - APPROXIMATELY 200 MILES NORTHEAST OF ABQ, CREW REPORTED OVER ACARS THAT THEY HAD A FUEL VALVE STUCK AND A FUEL IMBALANCE WAS GROWING. IMBALANCE WAS SEVERE ENOUGH THAT THE FLIGHT DIVERTED TO ABQ WHERE IT LANDED WITHOUT FURTHE R INCIDENT. NO EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITH 6,000 LBS OF FUEL IN THE RIGHT TANK AND 3,000 LBS IN T HE LEFT TANK. MAINTENANCE REMOVED AND REPLACED THE FUEL CROSSFEED VALVE. OPERATIONAL CHECK AND LEAK CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999012900785 19990129 00785 NM 1999 1 29 TSAA9833661 1 19981231 A 3350 6013211 BATTERY PACK BOEING 737 737230C 1384472 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 820AL 22138 AFT EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F A16WE 1999012900786 19990129 00786 NM 1999 1 29 TSAA9833662 1 19981231 A 3350 8731002511 LIGHT BOEING 737 7372T4 1384492 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 807AL 23443 REPLACED EXIT IDENTIFIER LIGHT ASSY FOR FORWARD ENTRY DOOR DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F A16WE 1999012900787 19990129 00787 NM 1999 1 29 TSAA9833656 1 19981230 A 3350 86210066 BATTERY BOEING 737 7372X6C 1384552 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 817AL 23292 REPLACED EMERGENCY FLOOR LIGHT BATTERY PACK FOR POSITIONS NR 2 AND NR 5 DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RET URNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900788 19990129 00788 NM 1999 1 29 TSAA9833657 1 19981230 A 3350 8731002511 LIGHT BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED POSITION NR 5 FLOOR PROX LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900789 19990129 00789 NM 1999 1 29 TSAA9833658 1 19981230 A 3350 86210066 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED NR 5 POSITION BATTERY FOR FLOOR PROX LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( M) 2 L 7 2 4F RT A16WE 1999012900790 19990129 00790 NM 1999 1 29 TSAA9833659 1 19981230 A 3350 9221009 BATTERY PACK BOEING 737 737230 NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 821AL 23155 REPLACED BATTERY PACK FOR FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETU RNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999012900791 19990129 00791 EU 1999 1 29 PLGA981221A 1 19981221 A 3234 D49412001 CONTROL SAAB SF340 340B 7860101 EU LT MLG MALFUNCTIONED A PLGA O OTHER J WARNING INDICATION AP APPROACH 1 NE 05 360BE 10210785 340B287 SYR - FLT 6423 - WHEN LANDING GEAR SELECTED DOWN FOR LANDING AT SYR, THERE WAS NO DOWN AND LOCKED INDICATION FOR LEFT GE AR. CREW FOLLOWED PROCEDURES AND VERIFIED GEAR WAS DOWN AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REP LACED LANDING GEAR CONTROL HANDLE. SYSTEM TESTED GOOD, AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999012900792 19990129 00792 EU 1999 1 29 PLGA981228A 1 19981228 A 2450 SAAB SF340 340B 7860101 EU UNKNOWN A PLGA F ACTIVATE FIRE EXT. B H SMOKE/FUMES/ODORS/SPARKS ELECT. POWER LOSS-50 PC TX TAXI/GRND HDL 1 NE 05 356BE 340B275 HPN - FLT 6427 - THE CREW ATTEMPTED TO START THE LT ENG AT THE GATE WHILE THE RT ENG WAS RUNNING. THE LT ENG DID NOT ST ART SO THE START WAS ABORTED AT 900 DEGREES. THE A/C STARTED A SINGLE ENG TAXI TOTHE RUNWAY. ANOTHER ATTEMPT WAS MADE TO START THE LT ENG BUT AGAIN THE START WAS ABORTED AT 850 DEGREES. THE CAPT REPORTED THE NR 1 EFIS DISPLAY BLANKED OUT BUT CAME BACK ON LINE. A THIRD ATTEMPT WAS MADE TO START THE LT ENG BUT WHEN THE STARTER WAS ENGAGED THERE WAS NO ROTA TION. THE COCKPIT LIGHTS WENT OUT AND THE A/C STARTED TO RETURN TO THE GATE. WHILE EN ROUTE, ALL COMMUNICATIONS WERE L OST FOLLOWED BY THE LOST OF ALL HYD PRESS. THE A/C CAME TO A STOP AND THE CREW REPORTED SMOKE COMING FROM THE LEFT ENG 2 L 7 2 4T RT A52EU 1999012900793 19990129 00793 EU 1999 1 29 PLGA981229A 1 19981229 A 2742 097439 ACTUATOR SAAB SF340 340B 7860101 EU HORIZ STAB FAILED A PLGA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NE 05 352BE 90K143498 340B239 BOS - FLT 6249 - AFTER TAKEOFF, THE STANDBY TRIM SYSTEM FAILED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. M AINTENANCE REPLACED THE STANDBY PITCH TRIM ACTUATOR. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999012900794 19990129 00794 CE 1999 1 29 PLGA981227A 1 19981227 A 2750 8519M3 FCU CESSNA 340 340A 2076405 CE TE FLAP MALFUNCTIONED A PLGA A UNSCHED LANDING J F WARNING INDICATION FLT CONT AFFECTED CL CLIMB 1 NE 05 339BE 235 340A044 BOS - FLT 6259 - WHILE ON CLIMB-OUT, THE CREW RECEIVED A FLAP WARNING ALONG WITH A MASTER CAUTION WARNING. AIRCRAFT RET URNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED FLAP CONTROL BOX AND RIGGED FLAPS. AIRCRAFT RETURNED TO SERVICE. (M) 1 L 7 2 3O 3A25 1999012900795 19990129 00795 SO 1999 1 29 C2XA98CL083 1 19981221 A 3250 3085601009 CONTROL MODULE EMB 120 EMB120RT SO NLG STEERING FAILED A C2XA O OTHER O OTHER TX TAXI/GRND HDL 1 SW 09 58733 14325 0265 120197 CLE - FLT 3216 - CREW REPORTED THAT THEY LOST ALL STEERING DURING LANDING ROLL OUT AND NEVER GAINED IT BACK. MAINTENANC E INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE STEERING CONTROL MODULE IAW EMB120 MM 32-50-03. OPERATIONAL CHEC KS WERE SATISFACTORY. RELAY K0123 WAS ALSO REPLACED FOR PRECAUTIONARY MEASURES. AIRCRAFT WAS RELEASED FOR SERVICE. (M ) 2 L 7 2 4T RT A31SO 1999012900796 19990129 00796 SO 1999 1 29 C2XA98CL084 1 19981221 A 2752 3203001005 ACTUATOR EMB 120 EMB120RT SO TE FLAP 19681 A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 12709 0114 120101 CLE - FLT 3194 - CREW REPORTED THAT AFTER TAKEOFF, RECEIVED A FLAP ASYMMETRY WITH THE INBOARD FLAPS AT 25 DEGREES AND TH E OUTBOARD AND NACELLES AT 15 DEGREES. AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AN D REPLACED THE RIGHT INBOARD FLAP ACTUATOR IAW EMB120 MM 27-50-07. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRC RAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900797 19990129 00797 EU 1999 1 29 C2XA98IA525 1 19981218 A 3350 3011210 LIGHT AEROSP ATR42 ATR42320 8680930 EU PAX DOOR INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING LINE CHECK INSPECTION, THE PASSENGER DOOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999012900798 19990129 00798 EU 1999 1 29 C2XA98IA544 1 19981218 A 3350 3011001 LIGHT AEROSP ATR42 ATR42320 8680930 EU CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 15818 153 IAH - DURING LINE CHECK INSPECTION, THE RIGHT FORWARD EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999012900799 19990129 00799 SO 1999 1 29 C2XA98IA526 1 19981218 A 5280 12004499003 FLANGE EMB 120 EMB120RT SO MLG DOOR CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT CHAFED. REMOVED AND REPLACED LEFT OUTBOARD FORWARD LANDING GEAR DOOR NACELLE HINGE ATTACH POINT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900800 19990129 00800 SO 1999 1 29 C2XA98IA543 1 19981218 A 5311 12005770001 FRAME EMB 120 EMB120RT SO BS 40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD CROSS FRAME AT FRAME 40 HEAVILY CORRODED. REMOVED AND REPLACED CROS S FRAME. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900801 19990129 00801 SO 1999 1 29 C2XA98IA542 1 19981218 A 5753 12022884002 BRACKET EMB 120 EMB120RT SO TE FLAP CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT WING INBOARD FLAP HINGE PANEL OUTBOARD ROLLER BRACKET CRACKED. REMOVED AND R EPLACED ROLLER BRACKET. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900802 19990129 00802 SO 1999 1 29 C2XA98IA541 1 19981218 A 5320 12006157005 SUPPORT EMB 120 EMB120RT SO BS 44-46 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE LEFT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 44 AND 46 CORRODED. REMOVED AND REPLACE D THE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900803 19990129 00803 SO 1999 1 29 C2XA98IA540 1 19981218 A 5320 12006159001 SUPPORT EMB 120 EMB120RT SO BS 40-44 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT FROM FRAME 40 TO 44 CORRODED. REMOVED AND REPLACED TH E FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900804 19990129 00804 SO 1999 1 29 C2XA98IA539 1 19981218 A 5320 12006157003 SUPPORT EMB 120 EMB120RT SO BS 45/46 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT OUTBOARD FLOOR SUPPORT BETWEEN FRAMES 45-46 CORRODED. REMOVED AND REPLACED T HE FLOOR SUPPORT. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900805 19990129 00805 SO 1999 1 29 C2XA98IA538 1 19981218 A 5320 12006158001 STRAP EMB 120 EMB120RT SO BS 38-40 CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT BUTT STRAP CORRODED BETWEEN FRAMES 38 AND 40. REMOVED AND REPLACED BUTT STRA P. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900806 19990129 00806 SO 1999 1 29 C2XA98IA537 1 19981218 A 5320 12027929001 STRAP EMB 120 EMB120RT SO CABIN CORRODED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT INBOARD FLOOR FLANGE CORRODED BETWEEN FRAMES 33 AND 35. REMOVED AND REPLACED BUTT STRAPS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900807 19990129 00807 SO 1999 1 29 C2XA98IA536 1 19981218 A 7810 12033750004 EXHAUST NOZZLE EMB 120 EMB120RT SO RT ENGINE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT EXHAUST DUCT CRACKED INBOARD ABOVE ATTACH MOUNT BRACKET. REMOVED AND REPLACE D RIGHT EXHAUST PIPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900808 19990129 00808 SO 1999 1 29 C2XA98IA535 1 19981218 A 7810 12033750003 TAIL PIPE EMB 120 EMB120RT SO LT ENGINE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND CRACK IN AFT OUTBOARD MOUNT FLANGE ON LEFT TAIL PIPE. REMOVED AND REPLACED LEFT TAIL P IPE. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900809 19990129 00809 SO 1999 1 29 C2XA98IA534 1 19981218 A 5400 12022766002 STIFFENER EMB 120 EMB120RT SO RT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT NACELLE AFT END CENTER FLAP WELL LOWER STRUCTURE CHAFED. REMOVED AND REPLACE D STIFFENER. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900810 19990129 00810 SO 1999 1 29 C2XA98IA533 1 19981218 A 5414 12001209601 PANEL EMB 120 EMB120RT SO LT NACELLE CHAFED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE NACELLE ACCESS PANEL 432BB HAD SMALL CHAFE MARKS TO INNER SURFACE. LOCATED AND DRI LLED NEW PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900811 19990129 00811 SO 1999 1 29 C2XA98IA532 1 19981218 A 5414 12001209601 PANEL EMB 120 EMB120RT SO RT NACELLE BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND ACCESS PANEL 442BB HAD SEVERAL FASTENER HOLES CRACKED AND BROKEN OUT. LOCATED AND DRIL LED PANEL. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900812 19990129 00812 SO 1999 1 29 C2XA98IA530 1 19981218 A 5400 12019396002 FITTING EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG INBOARD DOOR ACTUATOR FORWARD SUPPORT FITTING CRACKED. REMOVED AND REPLA CED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900813 19990129 00813 SO 1999 1 29 C2XA98IA529 1 19981218 A 5400 12019412002 FITTING EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG FORWARD OUTBOARD DOOR ACTUATOR FORWARD FITTING CRACKED. REMOVED AND REPL ACED FITTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900814 19990129 00814 SO 1999 1 29 C2XA98IA528 1 19981218 A 5414 12048448002 SKIN EMB 120 EMB120RT SO RT NACELLE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR FORWARD HINGE ATTACH POINT NACELLE SKIN CRACKED AT RIVET . STOP DRILLED AND FABRICATED DOUBLER REPAIR. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900816 19990129 00816 CE 1999 1 29 C2XA98IA549 1 19981229 A 3350 303 LAMP BEECH 1900 1900D 1154162 CE CABIN FAILED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 87550 UE205 IAH - DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT BULB IN THE EMERGENCY LIGHT WAS INOPERATIVE. MAINTE NANCE REMOVED AND REPLACED THE DEFECTIVE BULB AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A24CE 1999012900817 19990129 00817 GL 1999 1 29 C2XA98CL085 2 19981224 A 7200 ENGINE EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL LEFT CONTAMINATED A C2XA K NONE J WARNING INDICATION IN INSP/MAINT 1 SW 09 13929 2508 145009 CAE310078 CLE - DURING A SCHEDULED INSPECTION, A OIL DEBRIS MESSAGE WAS FOUND ON THE EICAS FOR THE LEFT ENGINE. MAINTENANCE INSPE CTED THE LEFT ENGINE AND FOUND THE OIL DEBRIS TO BE BEYOND MANUFACTURES LIMITS. THE LEFT ENGINE WAS REMOVED AND REPLACE D IAW CONTINENTAL EXPRESS TASK CARD NR 6271001, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SE RVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999012900818 19990129 00818 SO 1999 1 29 C2XA98CL087 1 19981228 A 2752 3203001007 ACTUATOR EMB 120 EMB120RT SO TE FLAP MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION NR NOT REPORTED 1 SW 09 15730 18280 0864 120187 CLE - FLT 3114 - CREW REPORTED THAT THEY RECEIVED A CONTROL FAULT WITH FLAPS AND A ADV SWS ON MAP UPON BRINGING FLAPS FR OM 15 DEGREES TO 0 DEGREES, SYSTEM WOULD NOT RESET. MAINTENANCE REMOVED AND REPLACED THE LEFT OUTBOARD FLAP ACTUATOR IA W EMB-120 MM 27-50-01. OPERATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900819 19990129 00819 SO 1999 1 29 C2XA98IA546 1 19981227 A 3350 12021299001 LIGHT EMB 120 EMB120RT SO FUSELAGE INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 26714 120118 IAH - FLT 3730 - DURING POST FLIGHT INSPECTION, THE CREW REPORTED THAT THE LEFT AND RIGHT AFT OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT ASSEMBLY AND OPERATIONAL TEST ED GOOD IAW EMB120 MM 33-52-01, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900820 19990129 00820 EU 1999 1 29 C2XA98IA545 1 19981227 A 3350 3011151 BATTERY PACK AEROSP ATR42 ATR42320 8680930 EU CABIN DISCHARGED A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 86842 286 IAH - DURING MAINTENANCE INSPECTION, SEVERAL AISLE PATH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMO VED AND REPLACED THE BATTERY PACK AT LOCATION 3WL. THE SYSTEM OPERATIONAL CHECKED GOOD IAW ATR42 JIC 33-51-21, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999012900821 19990129 00821 EU 1999 1 29 C2XA98IA547 1 19981227 A 3310 84501 MODULE AEROSP ATR42 ATR42500 EU COCKPIT FAILED A C2XA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 09 16450 510 MOB - FLT 3308 - THE CREW REPORTED ELECTRICAL SMOKE IN THE COCKPIT. THE SEAT BELT/NO SMOKING CIRCUIT BREAKER WAS PULLED AND THE AIRCRAFT LANDED AT MOB WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACE D THE LIGHTING MODULE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999012900822 19990129 00822 SO 1999 1 29 C2XA98BT086 1 19981227 A 5330 SKIN EMB 145 EMB145 SO FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14933 3559 145018 SMALL CRACK IN SECTION OF FUSELAGE BEHIND PASSENGER DOOR. REPAIRED DAMAGED SECTION OF FUSELAGE IAW SRM. PRESSURE CHECK ED GOOD. (M) 2 L 7 2 4F RT T00011AT 1999012900823 19990129 00823 EU 1999 1 29 C2XA98BT085 1 19981218 A 3230 MLG AEROSP ATR42 ATR42320 8680930 EU LEFT MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 42836 20214 200 CREW REPORTED LEFT MAIN GEAR WOULD NOT RETRACT. MAINTENANCE PERFORMED LANDING RETRACTION AND EXTENSION CHECK AND FOUND NO DEFECTS NOTED. OPERATIONALLY CHECKED GOOD. (M) 2 H 7 2 4T RT A53EU 1999012900824 19990129 00824 SO 1999 1 29 C2XA98CL088 1 19981226 A 2751 3075001007 CONTROL UNIT EMB 120 EMB120RT SO E/E BAY MALFUNCTIONED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 15730 14053 0041 120187 CLE - FLT 3210 - CREW REPORTED THAT THEY RECEIVED A CONTROL FAULT DURING FLAP RETRACTION AND IT WOULD NOT RESET UNTIL OU TBOARD FLAPS WERE DRIVEN UP BY THE OVERRIDE SWITCH, ALSO WHEN FLAPS WERE SELECTED FOR LANDING THEY DID NOT MOVE. AIRCRA FT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL UNIT IAW EMB120MM 27-50-06. OPER ATIONAL CHECKS WERE SATISFACTORY. AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999012900825 19990129 00825 WP 1999 1 29 ARWA990101 1 19981225 A 3230 57191765508 TORQUE TUBE DOUG DC8 DC862F 3021972 WP RT MLG CRACKED A ARWA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 SO 19 791AL 21021 46150 MIA - FLT 940 - AFTER LANDING AND DURING TAXI, THE RIGHT MAIN LANDING GEAR GREEN LIGHT WAS OUT INTERMITTENTLY AND THE RE D GEAR DOOR UNSAFE RED LIGHTS ILLUMINATED, SUSPECTED FAULTY GEAR DOWN MICROSWITCH. FOUND RT MLG 'A' FRAME WITH CRACKED LUG. REMOVED AND REPLACED MLG 'A' FRAME ASSY (TORQUE TUBE) AND LINKAGE, OPS CHECKED NORMAL ON GEAR SWING IAW DC-8 MM 32 -11-3 AND MM 32-30-3. (M) 2 L 7 4 4F 4A25 1999012900827 19990129 00827 WP 1999 1 29 USAA980679 1 19981229 A 5312 591013085 BULKHEAD DOUBLER DOUG DC9 DC931 3022065 WP AFT PRESS BLKHD CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 935VJ 47332 48115 PIT - DURING Q-2 AND C-6 CHECKS, FOUND 3 CRACKS ALL 3.25 INCH ON DOUBLER AFT PRESSURE BULKHEAD AT LOWER RIGHT CORNER OF DOOR CUTOUT. REMOVED -85 DOUBLER AND INSTALLED NEW DOUBLER WITH STACK DOUBLER REPAIR PER DWG J060088 -521 AND 535 AND E A 51106. (M) 2 L 7 2 4F A6WE 1999012900828 19990129 00828 WP 1999 1 29 USAA980680 1 19981229 A 5320 ANGLE DOUG DC9 DC931 3022065 WP BS 1049 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 935VJ 47332 48115 PIT - DURING Q-2 CHECK, FOUND .5 INCH CRACK ON VERTICAL LEG OF RIGHT DRAG ANGLE STATION 1049. INSTALLED REPAIR DOUBLER PER SRM 53-05 FIG 23B. (M) 2 L 7 2 4F A6WE 1999012900829 19990129 00829 NM 1999 1 29 USAA980643 1 19981214 A 5320 654581945 ANGLE BOEING 737 737201 1384454 NM BS 259 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 248US 44186 22755 CLT - DURING DROP IN VISUAL INSPECTION, FOUND A CRACK APPROX 2.2 INCHES LONG IN RADIUS OF ANGLE BL 0 WL 192.5 STATION 25 9.5 NOSE WHEEL WELL. PART REPLACED WITH IDENTICAL PART PER BOEING 737-200 SRM 51-20-1, 51-40-1. (M) 2 L 7 2 4F A16WE 1999012900830 19990129 00830 NM 1999 1 29 USAA980627 1 19981207 A 5330 SKIN BOEING 737 737201 1384454 NM BS 727 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 246US 43746 22753 TPA - DURING CX-5 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS SEPARATED BY 1 INCH STATION 727 STRINGER 18L SKIN FUS ELAGE. FABRICATED FILLER AND DOUBLER PER SRM 53-30-3 FIG 6 AND EA 63110. (M) 2 L 7 2 4F A16WE 1999012900831 19990129 00831 NM 1999 1 29 USAA980661 1 19981229 A 5330 6545871523 SKIN BOEING 737 7372B7 1384560 NM FUSELAGE CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 286AU 39889 23133 TPA - DURING A CX-5 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN FORWARD SERVICE DOOR UPPER HINGE CUTOUT AFT UPPER CORN ER DOOR SKIN. INSTALLED DOUBLER PER TR 52-40-03A. (M) 2 L 7 2 4F A16WE 1999012900832 19990129 00832 NM 1999 1 29 USAA980644 1 19981215 A 5330 SKIN BOEING 737 7372Q9 138448M NM BS 737 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 230AU 50481 21975 CLT - DURING RON VISUAL INSPECTION, FOUND A 3 INCH CRACK STATION 737 OF FUSELAGE STRINGER 17 RT SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 25. (M) 2 L 7 2 4F A16WE 1999012900833 19990129 00833 NM 1999 1 29 USAA980628 1 19981207 A 5330 SKIN BOEING 737 7373B7 1384580 NM BS 764 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 383US 41131 22956 CLT - DURING A RON VISUAL INSPECTION, FOUND A 1.25 INCH CRACK IN EXTERIOR SKIN AT STATION 764.5 STRINGER 21R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M) 2 L 7 2 4F RT A16WE 1999012900834 19990129 00834 NM 1999 1 29 USAA980608 1 19981218 A 5311 FRAME BOEING 737 7373B7 1384580 NM BS 295-360 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 396US 37296 23318 CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH BY 20 INCH CORROSION AREA AND A .25 INCH CRACK STATION 295 TO STATION 360 RBL 60 INNER CHORD ANGLE. CORROSION TASK NR C53-107-02. INSTALLED PART PER SRM 51-10-02. (M) 2 L 7 2 4F RT A16WE 1999012900835 19990129 00835 NM 1999 1 29 USAA980637 1 19981217 A 2810 2005117103 FUEL TANK BOEING 737 7373B7 1384580 NM BS 280-350 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 506AU 39718 23381 CLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND FOUR 1 INCH CRACKS AUX FUEL TANK SHROUD AFT WALL LOWER CORNER SKIN. I NSTALLED DOUBLER PER EA 63089. (M) 2 L 7 2 4F RT A16WE 1999012900836 19990129 00836 EU 1999 1 29 99ZZZM44 1 19981120 A 2424 51539002A GCU LUCAS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A FYWA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AL 05 242BM 5027 902 DURING CRUISE, LEFT GENERATOR DROPPED OFF LINE. AIRCRAFT LANDED IN SITKA WITH NO PROBLEMS. MAINTENANCE WAS DISPATCHED TO SITKA 11-21-98. CHANGED STARTER/GENERATOR AND GENERATOR CONTROL UNIT. ALL SYSTEMS CHECKED OK ON GROUND ENGINE RUNS. (M) 2 L 7 2 4T RT A56EU 1999012900837 19990129 00837 EU 1999 1 29 99ZZZM45 1 19981122 A 2424 51539002A GCU LUCAS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A FYWA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AL 05 242BM 9221 902 IN CRUISE, LEFT GENERATOR DROPPED OFF LINE. AIRCRAFT LANDED SITKA, NO PROBLEM. AIRCRAFT FERRIED TO KETCHIKAN 11-23-98. TROUBLESHOOTING IN PROGRESS. TROUBLESHOOTING REVEALED GCU BAD. WHILE AIRCRAFT IN HANGAR. CHANGED ALL BONDING STRAPS . REPLACED GCU. PERFORMED FUNCTIONAL TEST FLIGHT. ALL SYSTEMS OK, 11-25-98. (M) 2 L 7 2 4T RT A56EU 1999012900838 19990129 00838 EU 1999 1 29 99ZZZM46 1 19981121 A 2424 51539002A GCU LUCAS BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A FYWA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 AL 05 242BM 6388 902 AIRCRAFT LEFT SITKA AFTER REPAIR AT CRUISE. LEFT GENERATOR DROPPED OFF LINE. FIELD CIRCUIT BREAKER TRIPPED. AIRCRAFT LANDED IN KETCHIKAN WITH NO PROBLEM. TROUBLESHOOTING DETERMINED GEN CONTROL UNIT BAD. REPLACED GCU. ALL SYSTEMS CHECK ED OK. (M) 2 L 7 2 4T RT A56EU 1999012900839 19990129 00839 EU 1999 1 29 99ZZZM47 1 19981211 A 2424 51539002A GCU LEAR BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A FYWA A UNSCHED LANDING A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 AL 05 242BM 5619 902 IN CRUISE, LEFT GENERATOR, LIGHT FLICKERED AND THEN THE LEFT GENERATOR DROPPED OFF LINE AND THE GENERATOR FIELD CIRCUIT BREAKER POPPED AND WOULD NOT RESET. AIRCRAFT RETURNED TO KETCHIKAN AND LANDED WITH NO PROBLEMS. AIRCRAFT IN HANGAR AND FOUND GENERATOR CONTACTOR AND STARTER CONTACTOR SWAPPED SIDE TO SIDE NORMAL. GENERATOR CONTROL UNIT WAS REMOVED AND RE PLACED. GROUND RUN AIRCRAFT ALL SYSTEMS AND ALL WIRING WAS ALSO CHECKED. (M) 2 L 7 2 4T RT A56EU 1999012900842 19990129 00842 WP 1999 1 29 ORJA98328 1 19981227 A 3350 PPSIB BATTERY CHARGER DOUG DC9 DC983 3022083 WP ROW 20F INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - EMERGENCY LIGHTS COME ON DURING TURBULANCE ROWS 8, 9, 10, 11. FOUND BAD EMERGENCY BATTERY CHARGER AT ROW 20F. RE MOVED AND REPLACED CHARGER EMERGENCY LIGHTS. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012900843 19990129 00843 WP 1999 1 29 ORJA98334 1 19981224 A 3350 1001191 LIGHT DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 881RA 49941 SJC - LOWER FORWARD EMERGENCY EXIT SIGN (LAMP) AT RIGHT MID CABIN WILL NOT ILLUMINATE TURNING WITH SEAT ROWS EE SIGN INO P. REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSEMBLY AT LOWER FORWARD RIGHT MID CABIN. OPS CHECK GOOD. (M) 2 L 7 2 4F RT A6WE 1999012900848 19990129 00848 WP 1999 1 29 99ZZZM48 1 19981231 A 3260 SENSOR LKHEED 1011 10113851 5265010 WP LT MLG FAILED A AMTA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 11 188AT 193C1078 DTW - DURING CLIMB, THE LANDING GEAR TRUCK WARNING LIGHT CAME ON. AIRCRAFT WAS RETURNED TO BLOCK. LANDED SAFELY. THE LEFT MAIN LANDING GEAR TRUCK POSITIONER WAS REPLACED IAW 32-32-03, LEAK CHECKED OK. (M) 2 L 7 3 4F A23WE 1999012900852 19990129 00852 NM 1999 1 29 ASAA9840116 1 19981223 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 PDX - DURING MAINTENANCE CHECK, THE FORWARD TWO AND AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATI VE. RECONNECTED BOTH THE FORWARD AND AFT LIGHTS/WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999012900853 19990129 00853 NM 1999 1 29 ASAA9840117 1 19981224 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PSP - PRIOR TO FLIGHT 585 - SEVERAL EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE IN FORWARD CABIN. RECONNEC TED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999012900854 19990129 00854 NM 1999 1 29 ASAA9840118 1 19981229 A 3397 WIRE BOEING 737 7374Q8 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 762AS 25099 PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999012900856 19990129 00856 WP 1999 1 29 ASAA9880262 1 19981212 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 969AS 53063 SEA - PRIOR TO DEPARTURE OF FLIGHT 366, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS FROM ROW 8 FORWARD WERE INOPERATI VE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900857 19990129 00857 WP 1999 1 29 ASAA9880266 1 19981218 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN FORWARD CABIN WERE FOUND INOPERATIVE. REPAIRED WIRI NG IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900858 19990129 00858 WP 1999 1 29 ASAA9880269 1 19981221 A 3350 6011779 POWER SUPPLY MIDLANDROSS DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 25305 0169 49234 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900859 19990129 00859 WP 1999 1 29 ASAA9880270 1 19981221 A 3350 014597101 BATTERY MARATHON DOUG DC9 DC983 3022083 WP CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPLACED THE BATTERIES IN THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900860 19990129 00860 WP 1999 1 29 ASAA9880271 1 19981221 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 SEA - PRIOR TO DEPARTURE OF FLIGHT 137, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE INOPERAT IVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900861 19990129 00861 WP 1999 1 29 ASAA9880272 1 19981222 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 939AS 49657 ONT - PRIOR TO DEPARTURE OF FLIGHT 555, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE INOPERA TIVE. RECONNECTED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900862 19990129 00862 WP 1999 1 29 ASAA9880273 1 19981222 A 3397 WIRE DOUG DC9 DC983 3022083 WP CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 975AS 53451 PDX - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHTS IN THE FORWARD CABIN WERE FOUND INOPERATIVE. RECONNECT ED WIRING IN FLOOR TRACK AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999012900863 19990129 00863 WP 1999 1 29 ASAA9880274 1 19981223 A 3350 6011779 POWER SUPPLY DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 933AS 0189 49234 SEA - DURING MAINTENANCE CHECK, THE EXTERIOR OVERWING EMERGENCY LIGHTS WERE FOUND INOPERATIVE. REPLACED THE POWER SUPPL Y AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900864 19990129 00864 WP 1999 1 29 ASAA9880275 1 19981226 A 3350 60030451 POWER SUPPLY MIDLANDROSS DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 932AS 49233 SEA - DURING MAINTENANCE CHECK, THE AFT OVERWING EMERGENCY EXIT IDENTIFIERS REMAIN ILLUMINATED WITH ELECTRIC POWER OFF. REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900865 19990129 00865 NM 1999 1 29 ASAA9810128 1 19981213 A 3350 86210144 BATTERY BOEING 737 737298C 1384490 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 745AS 20794 SEA - DURING MAINTENANCE CHECK, THE CABIN SMOKE BARRIER EXIT SIGN WAS FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIG HT OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999012900866 19990129 00866 NM 1999 1 29 ASAA9810129 1 19981215 A 3350 6013211 BATTERY PACK GRIMES BOEING 737 737290C 138448V NM OVERWING EXIT DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 730AS 22577 ANC - PRIOR TO FLIGHT 22, THE OVERWING EXIT LIGHTS WERE FLASHING. REPLACED BATTERY PACK AND LIGHTS OPERATED NORMALLY. ( M) 2 L 7 2 4F A16WE 1999012900867 19990129 00867 NM 1999 1 29 ASAA9810130 1 19981223 A 3350 RPS1B BATTERY CHARGER BOEING 737 737290C 138448V NM CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - PRIOR TO FLIGHT 51, THE LAST THREE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTE RY CHARGER AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999012900868 19990129 00868 NM 1999 1 29 ASAA9810126 1 19981205 A 3350 6104781 BATTERY GRIMES BOEING 737 737290C 138448V NM ROW 18 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE AT ROW 18. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999012900869 19990129 00869 NM 1999 1 29 ASAA9810125 1 19981203 A 3350 86210144 BATTERY PACK BOEING 737 737290C 138448V NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 742AS 23136 ANC - PRIOR TO FLIGHT 145, THE EMERGENCY EXIT LIGHT ON BULKHEAD WAS FOUND TO NOT BE TESTING PROPERLY. REPLACED BATTERY PACK AND LIGHT OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1999012900870 19990129 00870 NM 1999 1 29 ASAA9840114 1 19981218 A 3350 S283T0143 BATTERY PACK BOEING 737 7374Q8 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 755AS 25096 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS FAILED TO TEST. REPLACED ALL BATTERY PACKS AND LIGHTS O PERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999012900875 19990129 00875 NM 1999 1 29 MASA98225 1 19981216 A 3350 LIGHT DHAV DHC8 DHC8202 2809007 NM CABIN INOPERATIVE A MASA K NONE L NO TEST IN INSP/MAINT 1 SW 07 434YV 434 FLT 6282 - PHX-ASE - PRIOR TO DEPARTURE, THE CAPTAIN REPORTED THE CEILING EMERGENCY LIGHTS NR 2 AND NR 4 WOULD NOT ILLUM INATE. MAINTENANCE RESET THE COCKPIT EMERGENCY LIGHT SWITCH. NO FURTHER DISCREPANCIES WERE NOTED. SYSTEM OPERATED NOR MAL. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1999012900876 19990129 00876 WP 1999 1 29 ASAA9880257 1 19981208 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - PRIOR TO DEPARTURE OF FLIGHT 630, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE INOPERAT IVE. REPLACED THE WIRING AND LAMP MODULES IN THE FORWARD CABIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900877 19990129 00877 WP 1999 1 29 99ZZZM51 1 19981208 A 3350 0105606005 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - PRIOR TO DEPARTURE OF FLIGHT 630, CREW REPORTED THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE INOPERAT IVE. REPLACED THE WIRING AND LAMP MODULES IN THE FORWARD CABIN AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900878 19990129 00878 WP 1999 1 29 ASAA9880258 1 19981208 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 931AS 49232 SEA - DURING MAINTENANCE CHECK, THE FORWARD OVERHEAD EMERGENCY LIGHT IN THE CATWALK AREA WAS FOUND INOPERATIVE. REPAIRE D WIRING TO THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (M) 2 L 7 2 4F A6WE 1999012900893 19990129 00893 NM 1999 1 29 99ZZZM52 1 19980721 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM BS 340 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE OUTBOARD SEAT TRACK SCALLOPS AT BS 340 RBL 54 WAS FOUND WITH CORROSION. REMOVED SEAT TRACK FABRICATED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 51-30-02, 53-10-05, AND MM 51- 20-11. (M) 2 L 7 3 4F A3WE 1999012900894 19990129 00894 NM 1999 1 29 99ZZZM53 1 19980804 A 5320 BAC1510335 SUPPORT BOEING 727 727227 1384078 NM BS 328-344 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FORWARD LAV SUPPORT AT BS 328 AND 344 AT RBL 15 WAS FOU ND CORRODED. FABRICATED AND INSTALLED A NEW FLOOR SUPPORT IAW B727 SRM 51-40-03, 51-10-02, 51-30-02 AND MM 51-20-11. ( M) 2 L 7 3 4F A3WE 1999012900895 19990129 00895 NM 1999 1 29 99ZZZM54 1 19980804 A 5315 BAC14902773 FLOORBEAM BOEING 727 727227 1384078 NM BS 328 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE CABIN FLOORBEAM AT BS 328 LBL 44 AND LBL 30 WAS FOUND WI TH CORROSION. REMOVED CORRODED BEAM. FABRICATED AND INSTALLED REPLACEMENT BEAM IAW B727 SRM 53-10-08, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900896 19990129 00896 NM 1999 1 29 99ZZZM55 1 19980730 A 5320 PAN BOEING 727 727227 1384078 NM BS 1183 CRACKED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE DITCHING PAN AT BS 1183 LBL 40-47 WAS FOUND CRACKED. RE MOVED CRACKED PAN. FABRICATED AND INSTALLED REPAIR PAN IAW B727 SRM 51-40-02, 51-10-02, 15-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900897 19990129 00897 NM 1999 1 29 99ZZZM56 1 19980729 A 5320 PAN BOEING 727 727227 1384078 NM BS 1183 CRACKED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN IN LAKE CITY, FL THE DITCHING PAN AT BS 1183 LBL 27-37 WAS FOUND CRACKED. REMOVED CRACKED PAN. FABRICATED AND INSTALLED REPAIR PAN IAW B727 SRM 51-40-02, 51-10-02, 51-30-02 AND MM 51-20-11. ( M) 2 L 7 3 4F A3WE 1999012900898 19990129 00898 NM 1999 1 29 99ZZZM57 1 19980728 A 5320 PAN BOEING 727 727227 1384078 NM BS 1183 CRACKED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE DITCHING PAN AT BS 1183 LBL 55-LBL 65 OUTBOARD WAS FOUND CRACKED. REMOVED CRACKED PAN. FABRICATED AND INSTALLED REPAIR PAN IAW B727 SRM 51-40-02, 51-30-2, 51-10-02 AND MM 51- 20-11. (M) 2 L 7 3 4F A3WE 1999012900899 19990129 00899 NM 1999 1 29 99ZZZM58 1 19980723 A 5320 PAN BOEING 727 727227 1384078 NM BS 1183 CRACKED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE DITCHING PAN AT BS 1183 LBL 15 INBOARD SIDE WAS FOUND CR ACKED. REMOVED CRACKED PAN. FABRICATED AND INSTALLED REPAIR PAN IAW B727 SRM 51-40-02, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900900 19990129 00900 NM 1999 1 29 99ZZZM59 1 19980721 A 5315 FLOORBEAM BOEING 727 727227 1384078 NM BS 460 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND ON THE UPPER T-CAP OF THE FLOORBEAM AT BS 460 RBL 50-66. CUT OUT CORROSION. FABRICATED AND INSTALLED 5 EACH REPAIRS IAW B727 SRM 53-10-08 FIG 3, 51-10-02, 51 -30-02 AND MM 51-20-11. PART NUMBER INSTALLED BAC1512-3353, BAC1512-3390, BAC1505-100611, BAC1490-2831 AND BAC1490-2785 . (M) 2 L 7 3 4F A3WE 1999012900901 19990129 00901 NM 1999 1 29 99ZZZM60 1 19980721 A 5320 A135176 SUPPORT BOEING 727 727227 1384078 NM BS 440-480 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE FLOOR SUPPORT AT BS 440-480 RBL 65 WAS FOUND WITH CORROS ION. REMOVED FLOOR SUPPORT AND INSTALLED NEW FABRICATED FLOOR SUPPORT IAW B727 SRM 51-40-03, 51-30-02, 51-10-02, 51-20- 04 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900902 19990129 00902 NM 1999 1 29 99ZZZM61 1 19980721 A 5315 BAC14902888 FLOORBEAM BOEING 727 727227 1384078 NM BS 320 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURNG A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FLOORBEAM T-CAP WAS FOUND WITH CORROSION AROUND THE FAST ENER HOLE AT BS 420 BL 0. CUT OUT CORRODED AREA AND TREATED. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW B727 SRM 53-10-08, 51-10-06 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900903 19990129 00903 NM 1999 1 29 99ZZZM62 1 19980721 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM BS 420 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE SEAT LOWER FLANGE AT BS 420 RBL 47 WAS FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW B727 SRM 53-10-01 FIG 3, 51-10-02, 53-10-05 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900904 19990129 00904 NM 1999 1 29 99ZZZM63 1 19980721 A 5320 BAC150143 SUPPORT BOEING 727 727227 1384078 NM BS 418 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL THE J-TRACK WAS FOUND CORRODED ON THE UPPER AND LOWER SURFAC E AT BS 418 RBL 15-25. MECHANICALLY REMOVED CORROSION, TREATED AND PRIMED. FABRICATED AND INSTALLED REPAIR FLOOR SUPPO RT IAW B727 SRM 51-30-02, 53-10-01, 51-40-04 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900905 19990129 00905 NM 1999 1 29 99ZZZM64 1 19980721 A 5320 7075T6080 SUPPORT BOEING 727 727227 1384078 NM BS 418 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE UPPER AND LOWER SURFACE OF THE FLOOR SUPPORT WAS FOUND WITH CORROSIONS AT BS 418 RBL 28 AND 45. MECHANICALLY REMOVED CORROSION, TREATED AREA. FABRICATED AND INSTALLED T-ANGL E REPAIR IAW B727 SRM 53-10-08 FIG 8, 51-30-02 AND 51-10-02. (M) 2 L 7 3 4F A3WE 1999012900906 19990129 00906 NM 1999 1 29 99ZZZM65 1 19980721 A 5347 605549 SEAT TRACK BOEING 727 727227 1384078 NM BS 420 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTIN AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND ON THE SCALLOPS OF THE SEAT TRACK AT BS 420 RBL 57. REMOVED CORRODED SECTION. FABRICATED AND INSTALLED NEW SECTION OF TRACK IAW B727 SRM 53-10-02, 51-10-02 AN D MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900907 19990129 00907 NM 1999 1 29 99ZZZM66 1 19980721 A 5320 BAC150643 SUPPORT BOEING 727 727227 1384078 NM BS 420 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE J-TRACK AT BS 420 RBL 49-65 WAS FOUND CORRODED. REMOVE D AND REPLACED THE TRACK IAW B727 SRM 51-10-02, 51-30-02, 51-40-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900908 19990129 00908 NM 1999 1 29 99ZZZM67 1 19980721 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727227 1384078 NM BS 400 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE FLOOR BEAM T-CAP UPPER SURFACE AT BS 400 BL 0 - RBL 64 WAS FOUND WITH CORROSION. REMOVED FLOORBEAM T-CAP. FABRICATED AND INSTALLED FLOORBEAM REPAIR IAW B727 SRM 53-10-01 FIG 3, 51-10-02, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900909 19990129 00909 NM 1999 1 29 99ZZZM68 1 19980721 A 5320 BAC150643 SUPPORT BOEING 727 727227 1384078 NM BS 380-400 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LONGERON FLOOR SUPPORT AT BS 380-400 RBL 12 THE UPPER A ND LOWER T-CAP WAS FOUND WITH CORROSION. MECHANICALLY REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR IAW B727 SRM 51-30-02, 51-10-02, 51-40-04 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900910 19990129 00910 NM 1999 1 29 99ZZZM69 1 19980721 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727227 1384078 NM BS 370 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE LOWER BEAM T-CAP AT BS 370 RBL 0-63 WAS FOUND WITH CORR OSION. REMOVED FLOORBEAM T-CAP. FABRICATED AND INSTALLED NEW CAP IAW B727 SRM 53-10-8, 51-30-02, 51-10-02 AND MM 51-20 -11. (M) 2 L 7 3 4F A3WE 1999012900911 19990129 00911 NM 1999 1 29 99ZZZM70 1 19980721 A 5347 BAC15200792 SEAT TRACK BOEING 727 727227 1384078 NM BS 340-380 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE SEAT TRACK AT BS 340-380 RBL 16 WAS FOUND WITH CORROSIO N ON THE SCALLOPS THE ENTIRE LENGTH. REMOVED SEAT TRACK. FABRICATED AND INSTALLED NEW TRACK IAW B727 SRM 53-10-5 FIG 7 , 51-10-02, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900912 19990129 00912 NM 1999 1 29 99ZZZM71 1 19980729 A 5315 BAC1505100617 FLOORBEAM BOEING 727 727227 1384078 NM BS 440 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP LAKE CITY, FL, THE FLOORBEAM AT BS 440 RBL 10 WAS FOUND WITH CORROSION. REMO VED AND REPLACED THE T-CAP IAW B727 SRM 53-10-08 FIG 3, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900913 19990129 00913 NM 1999 1 29 99ZZZM72 1 19980717 A 5320 PAN BOEING 727 727227 1384078 NM BS 1166-1183 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, BETWEEN BS 1166 AND 1183 UNDER L2 LAVATORY FLOOR WAS FOUND CORRODED AT LBL 35. REMOVED AND FABRICATED AND INSTALLED FLOOR PAN AND TWO HAT SECTIONS IAW B727 SRM 51-40-02, 51-40-03 , 51-10-02, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900914 19990129 00914 NM 1999 1 29 99ZZZM73 1 19980717 A 5320 CHANNEL BOEING 727 727227 1384078 NM BS 1166-1183 CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, BETWEEN BS 1166 AND 1183 UNDER L2 LAVATORY FLOOR WAS FOUND CORRODED AT LBL 35. REMOVED AND FABRICATED AND INSTALLED FLOOR PAN AND TWO HAT SECTIONS IAW B727 SRM 51-40-02, 51-40-03 , 51-10-02, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900915 19990129 00915 NM 1999 1 29 99ZZZM74 1 19980717 A 5347 1A35150 SEAT TRACK BOEING 727 727227 1384078 NM CABIN CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE G-2 GALLEY FRONT OUTBOARD SEAT TRACK TERMINATING END WA S FOUND WITH CORROSION. REMOVED SEAT TRACK. FABRICATED AND INSTALLED REPAIR IAW B727 SRM 51-40-03, 51-10-02, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900916 19990129 00916 NM 1999 1 29 99ZZZM75 1 19980717 A 5347 BAC1520792 SEAT TRACK BOEING 727 727227 1384078 NM CABIN CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE G-2 INBOARD SEAT TRACK WAS FOUND CORRODED AT THE FRONT OF THE G-2 GALLEY RBL 21. REMOVED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK IAW B727 SRM 53-10-05 FIG 3, 51- 10-02, 51-30-02 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900917 19990129 00917 NM 1999 1 29 99ZZZM76 1 19980717 A 5347 605549 SEAT TRACK BOEING 727 727227 1384078 NM CABIN CORRODED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE G-1 GALLEY INBOARD SEAT TRACK AT RBL 15 WAS FOUND CORRO DED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 53-10-05 FIG 7, 51-30-02, 53-10-01 FIG 7, 51-30-02 AND MM 51-20-22. ( M) 2 L 7 3 4F A3WE 1999012900918 19990129 00918 NM 1999 1 29 99ZZZM77 1 19980717 A 5330 2024T3040 SKIN BOEING 727 727227 1384078 NM BS 277 DENTED A S1NA K NONE O OTHER IN INSP/MAINT 1 WP 07 13759 21044 DURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, A DENT .030 DEEP .5 INCH LONG WITH A SHARP CREASE WAS FOUND AT BS 277 S7R. CUT OUT DENTED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727 SRM 53-20-02, 51-10-0 2 AND MM 51-20-11. (M) 2 L 7 3 4F A3WE 1999012900919 19990129 00919 WP 1999 1 29 USAA980681 1 19981224 A 5320 WEB DOUG DC9 DC931 3022065 WP BS 1087 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 987VJ 75489 47210 PIT - DURING C-5 CHECK, FOUND .20 INCH CRACK, CRACK EXTENDED .5 INCH BEYOND STOP DRILL IN WEB ATTACHED TO SKIN AT AFT FU SE INTERIOR, AT STATION 1087 LONGERON 4R. INSTALLED DOUBLER, TITANIUM .050 SRM 53-01 FIG 2 PER EA NR 51136. (M) 2 L 7 2 4F A6WE 1999012900920 19990129 00920 WP 1999 1 29 USAA980677 1 19981224 A 5320 3916209501N FITTING DOUG DC9 DC931 3022065 WP BS 680 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923VJ 41926 48143 PIT - DURING Q-2 CHECK, FOUND FLOOR SUPPORT FITTING CRACKED IN HALF AT STATION 680 LT OUTBOARD SEAT TRACK SUPPORT. REPL ACED DEFECTIVE PART WITH PART NR 3916209-501N. (M) 2 L 7 2 4F A6WE 1999012900921 19990129 00921 WP 1999 1 29 USAA980678 1 19981224 A 5313 27779224 LONGERON DOUG DC9 DC931 3022065 WP BS 965 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 923VJ 41926 48143 PIT - DURING Q-2 CHECK, FOUND 1 INCH CRACK AT LONGERON 17R AT STATION 965. SPLICED IN NEW SECTION OF LONGERON PER SRM 5 3-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999012900922 19990129 00922 EU 1999 1 29 USAA980662 1 19981224 A 5320 1154982 FITTING FOKKER F28 F28MK0100 4990807 EU BS 3845-4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND CORROSION AT S/E DOOR SILL PLATE MOUNT FITTINGS 3845-4850 BL NR 1127R. DEFECTIVE PART REP LACED WITH IDENTICAL PART NR 1154982 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) 2 L 7 2 4F RT 1999012900923 19990129 00923 EU 1999 1 29 USAA980663 1 19981224 A 5320 1153459 FITTING FOKKER F28 F28MK0100 4990807 EU BS 3845 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND SURFACE CORROSION ENTIRE AREA FORWARD S/E DOOR GIRT BAR MOUNT FITTING 3845 OUTBOARD 1127R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR 115-3459 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) 2 L 7 2 4F RT 1999012900924 19990129 00924 EU 1999 1 29 USAA980664 1 19981224 A 5320 1154834 T-CAP FOKKER F28 F28MK0100 4990807 EU BS 3845 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND CORROSION AT SCREW HOLES TOP SURFACE FS NR 3845 AT 1127R T-CAP. DEFECTIVE PART REPLACED W ITH IDENTICAL PART NR 115-4834 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) 2 L 7 2 4F RT 1999012900925 19990129 00925 EU 1999 1 29 USAA980665 1 19981224 A 5320 115010 BEAM FOKKER F28 F28MK0100 4990807 EU BS 5805-6305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 20 INCH APPROXIMATELY BY 2 INCH CORROSION ON BEAM AT BL 221R STATION 5805-6305. REPAIRED WITH MODIFIED 1155009 BEAM PER SRM 51-70-06, 53-12-10, 51-22-01, 51-40-01. (M) 2 L 7 2 4F RT 1999012900926 19990129 00926 EU 1999 1 29 USAA980666 1 19981224 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3845-4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 28 INCH APPROXIMATELY BY 2 INCH CORROSION ON BEAM AT BL 1127L STATION 3845-4850. TOP CAP STRIP REPLACED (LOCALLY FABRICATED) 2024-T3 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) 2 L 7 2 4F RT 1999012900927 19990129 00927 NM 1999 1 29 CA981013012 1 19980928 A 7540 21212G22 CONNECTOR 9811P55 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BLEED CONTROL CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 22803 120581 (CAN) WHEN GROUND POWER SELECTED ON CIRCUIT BREAKER, NR 5B FOR BLEED CONTROL TRIPPED. INVESTIGATION FOUND THE CROSS-OVE R CANNON PLUG 9811-P55 BELOW THE CENTER FLOOR ADJACENT TO LAVATORY CORRODED. PLUG REPLACED AND WIRE NR 2121-2G22 REPLAC ED. PART TC: 23,552. 2 H 7 2 4T 4 T RT A13NM E20NE 1999012900929 19990129 00929 NM 1999 1 29 CA981019006 1 19981003 A 3350 2N4398 POWER SUPPLY GRIMES 6038443 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CABIN FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 297 120816 (CAN) DURING LINE CHECK WHILE TESTING EMERGENCY LIGHTING SYSTEM, A BURN SMELL AND SMOKE WERE OBSERVED IN THE CABIN. PRO BLEM TRACED TO EMERGENCY LIGHT POWER SUPPLY AT SEAT 34B. TRANSISTOR ON CIRCUIT BOARD APPEARED TO HAVE OVERHEATED AND CA USED CIRCUIT BOARD TO BURN. 2 H 7 2 4T 4 T RT A13NM E20NE 1999012900931 19990129 00931 NM 1999 1 29 CA981022012 1 19981005 A 3097 Q50E WIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE PITOT HEAT FAILED W K NONE M OVER TEMP IN INSP/MAINT 1 CA CG48148 120367 (CAN) NR 1 PITOT HEAT CURRENT SENSOR FOUND WITH A BURNED TERMINAL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999012900934 19990129 00934 SW 1999 1 29 CA981125067 1 19981030 A 2721 2719332003 TRIM ACTUATOR FRCHLD SA227 SA227CC SW GARRTT TPE331 TPE33111U 01514 WP RUDDER SEIZED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA 13 P44738C (CAN) RUDDER TRIM SEIZED IN-FLIGHT. AIRCRAFT RETURNED OK. ACTUATOR REPLACED. 2 L 7 2 4T 4 T RT A18SW E4WE 1999012900935 19990129 00935 SW 1999 1 29 CA981125068 1 19981103 A 2721 2742004003 TRIM ACTUATOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE RUDDER SEIZED W A UNSCHED LANDING F FLT CONT AFFECTED CR CRUISE 1 CA 100 P44663C 881750 (CAN) RUDDER TRIM SEIZED IN-FLIGHT. AIRCRAFT LANDED OK. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999012900936 19990129 00936 SW 1999 1 29 CA981125075 1 19981118 A 2910 2781032778 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE RT WHEELWELL LOOSE W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA P44205C 930243 (CAN) AIRCRAFT LOST ALL HYDRAULIC PRESSURE AND FLUID AND RETURNED TO BASE. AIRCRAFT HAD A LOOSE FITTING WHICH ALLOWED F LUID TO ESCAPE. LINE SECURED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999012900944 19990129 00944 NM 1999 1 29 CA981207003 1 19981108 A 3230 82920014009 ACTUATOR 83210301001 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE LT MLG DOOR BINDING W O OTHER J WARNING INDICATION AP APPROACH 1 CA 2073 PCEAE0008 (CAN) ON GEAR DOWN EXTENSION, LEFT MAIN LANDING GEAR DID NOT SHOW DOWN AND LOCKED. (LEFT GEAR INDICATION WAS YELLOW AND RED BUT NO GREEN.) ALTERNATE EXTENSION CARRIED OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE INSPECTION REVEALED LEFT M AIN LANDING GEAR DOOR ACTUATOR WAS BINDING WHEN GEAR EXTENDED. ACTUATOR REPLACED AND MECHANICAL SEQUENCE VALVE RE-RIGGE D. RETRACTION TESTS CARRIED OUT SERVICEABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999012900945 19990129 00945 EU 1999 1 29 CA981207004 1 19981110 A 2721 110631 CONTROL CABLE FOKKER F28 F28MK1000 4990808 EU RUDDER TRIM BROKEN W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF, CREW NOTICED THE RIGHT RUDDER PEDAL WAS VERY SENSITIVE AND THE RUDDER TRIM HAD NO EFFECT ON TRIMMING THE AIRCRAFT. RIGHT RUDDER TRIM BUNGEE CABLE BROKEN. REPLACED. 2 L 7 2 4F RT A20EU 1999012900950 19990129 00950 NE 1999 1 29 CA981207012 3 19981112 A 6110 4E30171 DEICER BOOT BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE RT PROPELLER CUT W K NONE J WARNING INDICATION IN INSP/MAINT 1 CA 1824 PCE114293 HJ223 (CAN) ON LANDING, THE CREW REPORTED THE RIGHT HAND PROPELLER AMPS WERE INDICATING LOW. INVESTIGATION FOUND THE DE-ICER BOOT HAD A CUT. ON REPLACING THE BOOT, IT WAS FOUND THAT THE NICKEL LEADING EDGE SHEATH WAS DEBONDED IN THE ENTIRE AREA UNDER THE BOOT. THE PROPELLER ASSEMBLY WAS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1999012900952 19990129 00952 NM 1999 1 29 CA981207016 1 19981121 A 2741 TRANSMITTER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE STABILIZER FAILED W K NONE O OTHER NR NOT REPORTED 1 CA P709632 (CAN) STABILIZER FAILED TO TRIM NOSE DOWN AROUND 10 POINTS WITH FIRST OFFICER AND CAPTAIN THUMB SWITCHES. FOUND CONTROL COLUMN TRIM AND MANUAL LEVER SWITCHES SHOWING ON RIGHT STABILIZER TRIM ELEVATOR ASYMMETRY MODULE. REPLACED M519/M520 S TABILIZER POSITION TRANSMITTER MODULE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999012900956 19990129 00956 SW 1999 1 29 CA990125004 1 19981229 A 6310 212040001115 TRANSMISSION 212040001115 BELL 212 212 1181420 SW PWA PT6T PT6T3 52045 EA MAIN ROTOR MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 11736 FH2002 60220 (CAN) SERVICEABLE TRANSMISSION INSTALLED AND ALTERNATE RUN-IN PROCEDURE CARRIED OUT IAW WITH BELL MM. FILTERS REMOVED A ND FOUND CLEAN. TWO TEST FLIGHTS OF 0.3 AND 0.2 CARRIED OUT. DURING SECOND FLIGHT, THE TRANSMISSION CHIP WARNING LIGHT CAME ON AND AIRCRAFT RETURNED TO BASE. EXCESSIVE AMOUNTS OF FERROUS METAL WAS FOUND ON THE CHIP PLUG AND IN THE FILTER . TRANSMISSION RETURNED FOR INVESTIGATION. 1 G 7 1 4U 4 U H4SW E22EA 1999012900957 19990129 00957 1999 1 29 CA990125013 4 19981205 A 2565 61474129 ESCAPE SLIDE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE NR 2 FAILED W K NONE L NO TEST IN INSP/MAINT 1 CA 31425 (CAN) DURING FUNCTIONAL TEST OF NR 2 ESCAPE SLIDE, THE SLIDE FAILED TO INFLATE CORRECTLY. DEPLOYMENT WAS SATISFACTORY, BUT THE ASPIRATOR VALVE FAILED TO FUNCTION CORRECTLY AND THE INFLATION AIR ESCAPED PAST THEM BOTH ALLOWING THE SLIDE TO DEFLATE RAPIDLY. INSPECTION REVEALED THAT THE ASPIRATOR VALVES BODIES WERE OVAL PREVENTING THE VALVES FROM CLOSING PROP ERLY. SLIDE RETURNED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999012900999 19990129 00999 WP 1999 1 29 UPS99828539 1 19981230 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1080 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, HEAVY CORROSION AND BULGING FRAME FS 1080 FROM L33R TO 31R. REPAIRED IAW SRM 53-2-0. 2 L 7 4 4F RT 4A25 1999013000005 19990130 00005 NM 1999 1 30 DLM90982594 1 19981217 A 5342 591214185 ANGLE DOUG MD90 MD9030 3023690 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 914DN 53394 FUSELAGE ATTACH FITTING, VERTICAL STAB TO FUSE ANGLE, REPAIR FOR CRACK. THE VERTICAL STABILIZER TO FUSELAGE ATTACH ANGL E WAS FOUND WITH A .75 CRACK BETWEEN FASTENERS AT FS 940 ON THE LT SIDE OF THE FUSELAGE. THE CRACKED AREA WAS ROUTE D OUT OF THE ANGLE AND REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 366304-14. 2 L 7 2 4F RT A6WE 1999013000006 19990130 00006 NM 1999 1 30 DLM90982612 1 19981221 A 5330 5920323249 SKIN DOUG MD90 MD9030 3023690 NM BS 297-313 GOUGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 902DA 53382 FUSELAGE SKIN FS 297-313 L-23R, DENT/GOUGE REPAIR. THE FUSELAGE SKIN AT LONGERON 23R WAS GOUGED AND DENTED BETWEEN FS 2 97 AND 313. THE DAMAGED AREA OF SKIN WAS CUTOUT WITH A 28 LONG BY 2 WIDE CUTOUT. THE DAMAGE WAS REPAIRED WITH AN EXTE RNAL ALUMINUM DOUBLER INSTALLED PER THE GUIDELINES OF MD-90 SRM 53-30-01, FIG 2 AND ER/A 366348-14. 2 L 7 2 4F RT A6WE 1999020400001 19990204 00001 WP 1999 2 4 ABXA9800035 1 19980115 A 5312 BULKHEAD SKIN DOUG DOUG DC9 DC932F 3022067 WP BS 996 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 904AX 47040 DURING ACCOMPLISHMENT OF DC9 SERVICE BULLETIN 53-A14, FOUND AFT PRESSURE BULKHEAD TEE CAP UPPER SKIN SPLICE CRACKED WITH SHEARED RIVETS AT FUSELAGE STATION 996. REPAIRED IAW DOUGLAS SERVICE REWORK DRAWING J060143 AND ABX REA D953-2250-MR. 2 L 7 2 4F A6WE 1999020500040 19990205 00040 WP 1999 2 5 AT9900042 1 19981217 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 218 & 517 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION OUT OF LIMITS AND LEVEL 2 CORROSION AT THE FORWARD CARGO PIT COM PARTMENT AT STA 517 L-27R AND STA 218 L-29L. REMOVED CORROSION OUT OF LIMITS, FABRICATED AND INSTALLED NEW FLOOR CHANNE L AND LONGERON SECTION IAW DC9 SRM 51-30-2, 51-10-3, 51-10-4, 53-02 FIG 18. 2 L 7 2 4F A6WE 1999020500041 19990205 00041 WP 1999 2 5 AT9900043 1 19981223 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 879 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND TWO DENTS TO CLOSE TO EACH OTHER AND CREASED OUT OF LIMITS AT STA 882 AND STA 884 L-24R. CUT OUT CREASED AREAS AT STRINGER, FABRICATED, TREATED, AND PRIMED DOUBLERS IAW DC9 SRM 53-04 FIG 12B, 5 1-10-3, AND RES NR 982225 AND NR 982294. 2 L 7 2 4F A6WE 1999020500044 19990205 00044 WP 1999 2 5 AT9900047 1 19981229 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 943 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND BETWEEN FRAME AND SKIN AFT PIT STA 943 L-29L AND L-30L. REM OVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC9 SRM 53-01 FIG 1, 51-10-3, 53-04 FIG 12 AND RES 982285. 2 L 7 2 4F A6WE 1999020500045 19990205 00045 WP 1999 2 5 AT9900048 1 19981222 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 813-889 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND NUT PLATES CORRODED ON AFT PIT FLOOR SUPPORT AT STA 813 TO STA 889 RIGHT S IDE. REMOVED AND REPLACED ALL NUT PLATES AND CLEAN ALL CORROSION. FABRICATED AFT PIT FLOOR SUPPORT CHANNEL, SPLICES, T REATED, PRIMED, REINSTALLED ALL PARTS AND NUT PLATES IAW DC9 SRM 51-10-2, 53-21-0 FIG 10, 51-10-4, 51-10-2A, 51-30-3, 51 -30-2, 51-10-3, AND RES NR 982229. (P/N 1A-390011-1), (P/N 1A-39011-2), (P/N 1A-41600-1), (P/N 1A-41600-2), (P/N 1A-416 00-3). 2 L 7 2 4F A6WE 1999020500046 19990205 00046 WP 1999 2 5 AT9900049 1 19981210 A 5320 BRACKET DOUG DC9 DC932 3022066 WP NLG WW CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. LOWER FACE ON UPPER PRESSURE PANEL IN NOSE WHEEL WELL HAS CORROSION ON INSULATIO N SUPPORT MOUNT BRACKETS AT STA 71 16 LEFT TO RIGHT OF CENTER, STA 73 TO 78 16 LEFT TO CENTER, STA 80 TO 99 16 FROM LE FT TO RIGHT CENTER. REMOVED AND REPLACED SUPPORT MOUNT BRACKETS, DRILLED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51- 30-2, 51-10-2, 51-10-4, 51-10-3. (P/N 1A-41574-1), (P/N 1A-41574-2), (P/N 1A-41574-3), (P/N 1A-41572-1), (P/N 1A-41571- 1), AND (P/N 1A-41570-1). 2 L 7 2 4F A6WE 1999020500052 19990205 00052 NM 1999 2 5 9811445508 1 19981219 A 3350 6012113RF POWER SUPPLY BOEING 757 757251 1384970 NM ROW 14 INOP A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 508US 23197 ESCAPE PATH LIGHTING INOPERATIVE FROM ROW 14 FORWARD. MAINTENANCE REPLACED THE POWER SUPPLY WITH A SERVICEABLE UNIT, OP ERATIONAL CHECK OK. 2 L 7 2 4F RT A2NM 1999020500115 19990205 00115 WP 1999 2 5 AT99000063 1 19981222 A 5320 1A41645 DOUBLER DOUG DC9 DC932 3022066 WP BS 237 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AEROCORP, FL. FOUND G-2 GALLEY TRASH BIN AREA CORRODED OUT OF LIMITS. REMOVED FASTENERS AND CO RROSION IN G-2 AREA, FABRICATED DOUBLER AND INSTALLED NEW FASTENERS AND DOUBLER IAW DC9 SRM 53-01, 51-10-3 AND 51-30-2. 2 L 7 2 4F A6WE 1999020500116 19990205 00116 WP 1999 2 5 AT9900050 1 19981209 A 5312 591913065N BULKHEAD ANGLE DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND ON AFT PRESSURE BULKHEAD CENTER L ANGLE AND AROUND FASTENER LOWER END STA 996 AFT PIT. THE OTHER WAS FOUND ON THE FORWARD CARGO AFT BULKHEAD CENTER PANEL HAS ELONGATED HOLES, WORN AND SURFACE CORROSION ON UNDERSIDE PANEL. REMOVED AND REPLACED ANGLE, PANEL AND CORROSION OUT OF LIMITS. FABRICATED N EW PANEL, DRILLED, DEBURRED, PRIMED PANEL AND NEW ANGLE AND INSTALLED IAW DC9 SRM 53-01 FIG 1, 51-30-0, 51-30-2, 51-30-5 , 51-20-4 AND 53-21-0. 2 L 7 2 4F A6WE 1999020500117 19990205 00117 WP 1999 2 5 AT9900051 1 19981229 A 5320 1A415921 ANGLE DOUG DC9 DC932 3022066 WP BS 943 & 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND FRAME ANGLES AND CEILING SUPPORT CORRODED AT STA 943 L-30 AND STA 996 RT A BOVE CUSP WEB AND STA 965 TO 980 L-16L. REMOVED CORROSION, FABRICATED A NEW SHEAR TIE REPAIR AT STA 943. CUT OUT CORRO DED SECTION ABOVE CUSP WEB AND FABRICATED SPLICE SECTION AT STA 996. FABRICATED, INSTALLED NEW SUPPORT AT STA 965 TO 98 0 ALL IAW DC9 SRM 53-03 FIG 6 AND 14, 51-10-3, 51-30-5, 51-10-4, 53-01 FIG 1 AND 51-30-2. 2 L 7 2 4F A6WE 1999020500118 19990205 00118 WP 1999 2 5 AT9900052 1 19981211 A 5320 49125151N FITTING DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION AT END TIE AT STA 996 L-27L AND L-28L. REMOVED AND REPLACED END TIE FITTINGS, DRILLED NEW PART, DEBURRED, TREATED, PRIMED AND INSTALLED NEW PARTS IAW DC9 SRM 51-30-2, 51-30-5, 51-10-3 , 51-10-4, 53-01 FIG 1. 2 L 7 2 4F A6WE 1999020500119 19990205 00119 WP 1999 2 5 AT9900054 1 19981220 A 5320 99582339 INTERCOSTAL DOUG DC9 DC932 3022066 WP BS 976-996 & 945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND INTERCOSTALS TO BE CORRODED AND OUT OF LIMITS AT STA 945 L-29R AND STA 976 TO 996 L-27L. REMOVED AND REPLACED, FABRICATED, INSTALLED, AND PRIMED NEW INTERCOSTALS IAW DC9 SRM 51-10-4, 51-30-2, 5 1-10-3, 51-30-5, AND 51-10-2. 2 L 7 2 4F A6WE 1999020500120 19990205 00120 WP 1999 2 5 AT9900055 1 19981210 A 5347 TRACK DOUG DC9 DC932 3022066 WP CARGO COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON CARGO TRACKS AT VARIOUS STATION LOCATIONS. THE LOCATIONS ARE AS FOLLOWS: STA 218 TO 362 LT, STA 351 TO 446 LT, STA 446 TO 511 LT, STA 897 TO 965 LT, STA 218 TO 362 RT, STA 351 TO 3 62 RT, STA 362 TO 370 RT, AND STA 965 TO 996 RT. FABRICATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED TRACKS I AW DC9 SRM 51-10-2, 51-21-0, 51-10-3, 51-10-4, AND 53-21-0 FIG 7A. 2 L 7 2 4F A6WE 1999020500122 19990205 00122 WP 1999 2 5 AT9900057 1 19981210 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 559 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND UNDER THE AUXILIARY TANK JUST FORWARD OF THE RIGHT HAND KIDN EY PANEL AT STA 559. REMOVED ALL CORROSION AND DOUBLER, FABRICATED AND INSTALLED NEW REPAIR DOUBLER AND REPLACED END CA P FITTING IAW DC9 SRM 51-30-2, 51-30-5, 51-10-4, AND 53-01 FIG 1. END CAP (P/N 3924809-501N). 2 L 7 2 4F A6WE 1999020500123 19990205 00123 WP 1999 2 5 AT9900058 1 19981210 A 5321 FLOOR DOUG DC9 DC932 3022066 WP BS 756-794 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT CARGO CENTER FLOOR PANEL CORRODED AND WITH ELONGATED HOLES AT STA 756 TO 794. REMOVED PANEL, FABRICATED, TREATED, PRIMED AND INSTALLED NEW FLOOR PANEL IAW DC9 SRM 51-10-2, 53-21-0 FIG 1 0, AND 51-10-4. 2 L 7 2 4F A6WE 1999020500124 19990205 00124 WP 1999 2 5 AT9900059 1 19981212 A 5320 5912528501 JAMB DOUG DC9 DC932 3022066 WP BS 897-937 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. THE AFT PIT DOOR THRESHOLD PAN WAS FOUND WITH CORROSION, DENTS AND PUNCTURES. R EMOVED, REPLACED, INSTALLED THE DOOR PAN AND SPLICES IAW DC9 SRM 53-05 FIG 44, 51-10-4, 51-10-3, 51-30-1, AND 51-20-0. 2 L 7 2 4F A6WE 1999020500125 19990205 00125 WP 1999 2 5 AT9900060 1 19981226 A 5320 5956037509 DOUBLER DOUG DC9 DC932 3022066 WP BS 889 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. CORROSION WAS FOUND AROUND FASTENERS AND NUT PLATES ON FORWARD AND AFT SIDES OF FRAME STA 889 UPPER DOUBLER LONGERON 27L TO 29L. REMOVED CORRODED DOUBLER, FASTENERS, NUT PLATES, AND ANGLE. FABRICATE D, PRIMED, DEBURRED, INSTALLED DOUBLER AND ANGLE IAW DC9 SRM 51-10-2, 51-10-4, 51-10-3, 51-30-1, AND 51-30-5. 2 L 7 2 4F A6WE 1999020500126 19990205 00126 WP 1999 2 5 AT9900061 1 19981224 A 5320 1A390241 SUPPORT DOUG DC9 DC932 3022066 WP BS 996 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT FLOOR SUPPORT CORRODED AT STA 996 L-28R TO L-30R. REMOVED COR RODED AREA AND SUPPORT DUE TO MATERIAL LOSS AND OUT OF LIMITS. FABRICATED NEW SUPPORT, DRILLED, DEBURRED, PRIMED AND IN STALLED IAW DC9 SRM 53-01 FIG 1, 51-10-3, 51-10-4, 51-10-2. 2 L 7 2 4F A6WE 1999020500127 19990205 00127 WP 1999 2 5 AT9900062 1 19981218 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 180 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. E/E COMPARTMENT AT FRAME STA 180 L-29L TO L-29R WAS FOUND CORRODED AT FASTENERS LOCATION. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW DC9 SRM 51-10-3, 53-03 FIG 4A, 53-01 FIG 1, AND 51-30-5. 2 L 7 2 4F A6WE 1999020500128 19990205 00128 WP 1999 2 5 AT9900064 1 19981218 A 2133 OUTFLOW VALVE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND OUTFLOW VALVE HOUSING CORRODED AROUND NUT PLATES AND HAS SURFACE CORROSION LOWER INBOARD SIDE. REMOVED NUT PLATES AND CORROSION FOUND BEYOND LIMITS. REINSTALLED OUT FLOW VALVE IAW DC9 SRM 53-0 1 FIG 1, 51-10-3, AND MM 21-32-5 RIGGED AND OPS CHECKED GOOD. 2 L 7 2 4F A6WE 1999020500129 19990205 00129 WP 1999 2 5 AT9900065 1 19981211 A 5320 BRACKET DOUG DC9 DC932 3022066 WP BS 945 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. THE AFT PIT DRAIN BRACKET WAS FOUND CORRODED. REMOVED AND REPLACED THE DRAIN V ALVE ASSEMBLY AND BRACKET IAW DC9 SRM 51-30-2, AND 51-10-3. 2 L 7 2 4F A6WE 1999020500130 19990205 00130 WP 1999 2 5 AT9900066 1 19981229 A 5280 SKIN DOUG DC9 DC932 3022066 WP NLG DOOR GOUGED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. NOSE LANDING GEAR DOOR RIGHT UPPER FORWARD OUTBOARD SIDE AS VIEW WITH DOOR CLOSE D HAS A GOUGE IN SKIN ABOVE ACTUATOR ATTACH POINT. REMOVED, FABRICATED REPAIR AND INSTALLED IAW DC9 SRM 51-30-2, 51-10- 3, 51-30-5, AND RES NR 982283 AND RES NR 982245. OPERATIONAL CHECK GOOD IAW DC9 MM 32-22-1. 2 L 7 2 4F A6WE 1999020500179 19990205 00179 NM 1999 2 5 DL72L990173 1 19981203 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 AFT SPAR RAIL LWR CHORD ANGLE CRACKED 61 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 634487. 2 L 7 3 4F A3WE 1999020500180 19990205 00180 NM 1999 2 5 DL72L990174 1 19981203 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 AFT SPAR RAIL LWR CHORD ANGLE CRACKED 2 PLACES 32 AND 37 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 634487. 2 L 7 3 4F A3WE 1999020500181 19990205 00181 NM 1999 2 5 DL72L990175 1 19981203 A 5753 652163261 SPAR BOEING 727 727232 1384082 NM LT TE FLAP CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 AFT SPAR RAIL LWR CHORD ANGLE CRACKED 2 PLACES 19 AND 23 FROM I/B END. REPAIRED PER M/M 57-52-0 FIG 802, ON SHOP ORDER 634487. 2 L 7 3 4F A3WE 1999020500348 19990205 00348 WP 1999 2 5 UPS99828560 1 19981230 A 5320 3640887 FITTING DOUG DC8 DC871F 302199D WP BS 960-980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, HORIZONTAL FITTING HAS EXFOLIATION CORROSION THAT IS OUT OF LIMITS AT FS 960 TO 980, RBL 48. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-3-0. 2 L 7 4 4F RT 4A25 1999020500349 19990205 00349 WP 1999 2 5 UPS99828561 1 19981231 A 5347 S2772660 SEAT TRACK DOUG DC8 DC871F 302199D WP BS 920-940 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, SEAT TRACK BETWEEN FS 920 AND 940, RBL 60 IS CORRODED OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK BETW EEN FS 720 AND 950, SPLICED IN A NEW SECTION IAW EO DC8-5320-5167-C. 2 L 7 4 4F RT 4A25 1999020500383 19990205 00383 WP 1999 2 5 AT9900041 1 19981230 A 5320 DOUBLER DOUG DC9 DC932 3022066 WP BS 965 MISREPAIRED A ZZDA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. EXISTING REPAIR AT LEFT HAND STA 965 L-13L AND L-14L DOES NOT FACILITATE FOR HOL E PATTERN REQUIRED IN FRAME AND FORMER MODIFICATION 53-140. REMOVED EXISTING REPAIR, FABRICATED INTERNAL AND EXTERNAL S KIN DOUBLER, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED AND INSTALLED REPAIR IAW DC9 SRM 51-10-4, 51-10-3, 53-04 FIG 38 , 51-30-2, AND RES NR 982295. 2 L 7 2 4F A6WE 1999020500385 19990205 00385 WP 1999 2 5 AT9900068 1 19981227 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 992 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND RIGHT HAND FUSELAGE EXTERIOR SKIN HAS CORROSION BULGE WITH FASTENERS HEADS POPPED AT STA 992 L-20L. FOUND LONGERON CORRODED OUT OF LIMITS, REMOVED CORRODED SECTION OF LONGERON. FABRICATED AND INSTALLED NEW SPLICE SECTION IAW DC9 SRM 53-02 FIG 18 AND 53-01 FIG 1. 2 L 7 2 4F A6WE 1999020500387 19990205 00387 WP 1999 2 5 AT9900070 1 19981226 A 5320 1A390441 ANGLE DOUG DC9 DC932 3022066 WP FUSELAGE CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE ATTACH ANGLE UNDER G-2 GALLEY AND OUTBOARD SIDEWALL JUST UNDER THE ELECTRICAL CONNECTOR BAY. REMOVED CORRODED ANGLE, FABRICATED AND INSTALLED NEW ATTACHED ANGLE IAW DC9 SRM 53- 01 FIG 1, 51-30-2, 51-10-3, AND 51-30-8. 2 L 7 2 4F A6WE 1999020500391 19990205 00391 WP 1999 2 5 AT9900074 1 19981210 A 5330 SKIN DOUG DC9 DC932 3022066 WP BS 338 DENTED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. A DENT WAS FOUND TO BE OUT OF LIMITS AT STA 338 L-28R. COLD WORKED DENT TO ORIG INAL CONTOUR, FABRICATED DOUBLER, DRILLED, DEBURRED, TREATED, PRIMED AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 51-10-2 AND 53-04 FIG 38. 2 L 7 2 4F A6WE 1999020500392 19990205 00392 WP 1999 2 5 AT9900075 1 19981213 A 5230 PAN DOUG DC9 DC932 3022066 WP CARGO DOOR CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND CRACKS ON THE OUTER PAN FLANGE AFT CARGO DOOR AFT CENTER STOP AND ANOTHER ONE AT THE FORWARD CARGO DOOR AFT TOP (C-1 DOOR). FABRICATED, DEBURRED, PRIMED AND INSTALLED NEW DOUBLERS AND REPAIRS I AW DC9 SRM 52-03 FIG 8, 52-01 FIG 2, 51-10-3, 51-10-4 AND 51-30-2. 2 L 7 2 4F A6WE 1999020500393 19990205 00393 WP 1999 2 5 AT9900076 1 19981211 A 5313 LONGERON DOUG DC9 DC932 3022066 WP BS 945 & 965 CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 810AT 47277 SCHEDULED INSPECTION AT AERO CORP, FL. FOUND VARIOUS CRACKS AT DIFFERENT LONGERON LOCATIONS. THE LOCATIONS ARE AS FOLL OW: STA 945 L-17R, STA 965 L-13, 16, 17R, STA 965 L-14, 17L. LONGERON (P/N 7637813-3), (P/N 2777922-4), (P/N 1A-41527- 1), (P/N 2777948), SPLICE (P/N 7637813-3) (P/N 7637813-2). 2 L 7 2 4F A6WE 1999020500398 19990205 00398 SO 1999 2 5 RAAA99E8003 1 19981215 A 5730 PANEL LKHEED 188 188C 5262604 SO CENTER WING CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.103, FOUND WING CENTER SECTION NR 9 UPPER PANEL, RISER NR 61 CRACKED IN RADIU S FROM WS 9R TO 14R. REPAIRED PER SRM 57-2-1, FIG 3, PG 59. M-54 NR 421. 2 L 7 4 4T 4A22 1999020500399 19990205 00399 SO 1999 2 5 RAAA99E8004 1 19981215 A 5730 PANEL LKHEED 188 188C 5262604 SO CENTER WING CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.103, FOUND WING CENTER SECTION CORRODED NR 3 LOWER PANEL, RISER NR 17 TO 19, FROM WS 14L TO 24L. REPAIRED PER SRM 57-2-1. M-54 NR 417. 2 L 7 4 4T 4A22 1999020500400 19990205 00400 SO 1999 2 5 RAAA99E8005 1 19981215 A 5730 PANEL LKHEED 188 188C 5262604 SO WS 197 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.165, FOUND LT WING LOWER SURFACE NR 4 TO NR 5 PANEL SPLICE CORRODED AT WS 197 . REPAIRED PER LDS DWG NR 188341. M-54 NR 62A. 2 L 7 4 4T 4A22 1999020500401 19990205 00401 SO 1999 2 5 RAAA99E8006 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 302.5 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.56, FOUND FS 302.5 FRAME CORRODED BETWEEN STR 32 AND 33. REPAIRED PER LDS DW G NR 188344. M-54 NR 133. 2 L 7 4 4T 4A22 1999020500402 19990205 00402 SO 1999 2 5 RAAA99E8007 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 309.5 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.56, FOUND FS 309.5 FRAME CORRODED FROM STR 29 TO 34 AND FS 309.5 FRAME REINFO RCEMENT CORRODED FROM STR 30 TO 32. REPAIRED PER LDS DWG NR 188344. M-54 NR 134 AND 136. 2 L 7 4 4T 4A22 1999020500403 19990205 00403 SO 1999 2 5 RAAA99E8008 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 920 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.58, FOUND FS 920 FRAME CORRODED FROM STR 35 TO 36. REPAIRED PER SRM 53-2-3, FIG 2. M-54 NR 385. 2 L 7 4 4T 4A22 1999020500404 19990205 00404 SO 1999 2 5 RAAA99E8009 1 19981215 A 5320 DOUBLER LKHEED 188 188C 5262604 SO BS 853 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.107, FOUND FS 853 FRAME DOULBER DAMAGED AT STR 29 DUE DOOR HANDLE STRIKES. R EPLACED DOUBLER PER SRM 51-2-12. M-54 NR 539. 2 L 7 4 4T 4A22 1999020500405 19990205 00405 SO 1999 2 5 RAAA99E8010 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 540 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND FS 540 FRAME CRACKED ACROSS INNER FLANGE BELOW STR 51. REPAIRED P ER SRM 53-2-3, FIG 2. M-54 NR 587. 2 L 7 4 4T 4A22 1999020500407 19990205 00407 SO 1999 2 5 RAAA99E8011 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 407 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.97, FOUND FS 407 FRAME CORRODED FROM STR 35 TO 44. REPAIRED PER LOCKHEED DWG NR 842354. M-54 NR 196. 2 L 7 4 4T 4A22 1999020500408 19990205 00408 SO 1999 2 5 RAAA99E8012 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 882 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.58, FOUND FS 882 FRAME CORRODED AND CRACKED BETWEEN STR 36 AND 37. REPAIRED PER SRM 53-2-3, FIG 2. M-54 NR 390. 2 L 7 4 4T 4A22 1999020500409 19990205 00409 SO 1999 2 5 RAAA99E8013 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 875 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.119, FOUND FS 875 FRAME CORRODED ABOVE STR 50. REPAIRED PER SRM 53-2-3, FIG 4. M-54 NR 599. 2 L 7 4 4T 4A22 1999020500410 19990205 00410 SO 1999 2 5 RAAA99E8014 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 730 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND FS 730 FRAME CORRODED AT STR 22. REPAIRED PER SRM 53-2-3. M-54 N R 571. 2 L 7 4 4T 4A22 1999020500411 19990205 00411 SO 1999 2 5 RAAA99E8015 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 844 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.58, FOUND FS 844 FRAME CORRODED AT STR 40. REPAIRED PER SRM 53-2-3. M-54 NR 440. 2 L 7 4 4T 4A22 1999020500412 19990205 00412 SO 1999 2 5 RAAA99E8016 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 844 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.107, FOUND FS 844 FRAME CORRODED FROM STR 35 TO 36. REPAIRED PER SRM 53-2-3, FIG 2. M-54 NR 577. 2 L 7 4 4T 4A22 1999020500413 19990205 00413 SO 1999 2 5 RAAA99E8017 1 19981215 A 5320 DOULBLER LKHEED 188 188C 5262604 SO BS 255 DAMAGED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.113, FOUND FS 255 FRAME DOULBER DAMAGED AT STR 30. REPLACED DOUBLER PER SRM 51-2-12. M-54 NR 442. 2 L 7 4 4T 4A22 1999020500414 19990205 00414 SO 1999 2 5 RAAA99E8018 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 920 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.58, FOUND FS 920 FRAME CORRODED AT STR 43. REPAIRED PER SRM 53-2-3, FIG 2. M -54 NR 383. 2 L 7 4 4T 4A22 1999020500415 19990205 00415 SO 1999 2 5 RAAA99E8019 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 266 DENTED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.113, FOUND FS 266 FRAME DENTED AT STR 22. REPAIRED PER SRM 53-2-3, FIG 2. M -54 NR 682. 2 L 7 4 4T 4A22 1999020500416 19990205 00416 SO 1999 2 5 RAAA99E8020 1 19981215 A 5311 FRAME LKHEED 188 188C 5262604 SO BS 333 CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.113, FOUND FS 333 FRAME CRACKED AT STR 22. REPAIRED PER SRM 53-2-3, FIG 2. M -54 NR 683. 2 L 7 4 4T 4A22 1999020500490 19990205 00490 CE 1999 2 5 99ZZZX513 1 19980101 A 2822 503801775 BOOST PUMP BEECH 200 200BEECH 1152920 CE LT ENGINE MALFUNCTIONED A DBCA O OTHER O OTHER NR NOT REPORTED 1 GL 13 859CC BB389 LEFT HAND FUEL PRESURE LIGHT WOULD NOT ILLUMINATE. FOUND BOOST PUMP DEFECTIVE. REMOVED AND REPLACED P/N 50-380177-5, S /N 1D69. OPERATIONS CHECKED OK. 1 L 7 2 4T A24CE 1999020500491 19990205 00491 SW 1999 2 5 99ZZZX514 1 19980909 A 6410 214015700115 BLADE BELL 214 214ST 1182106 SW TAIL ROTOR CRACKED A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 392AL 1065 A436 28114 DURING DAILY INSPECTION, FOUND OUTER SKIN CRACK ON BLADE. 2 G 7 2 4U H10SW 1999020500539 19990205 00539 EU 1999 2 5 USAA980667 1 19981224 A 5320 T-CAP FOKKER F28 F28MK0100 4990807 EU BS 3845-4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND CORROSION TOP SURFACE 100MM LONGERON FS 3845-4850 T-CAP ENTIRE LENGTH BL NR 1127R. REPLAC ED TOP CAP STRIP WITH PART OF LOCAL FABRICATION 2024T3 PER SRM 52-12-10, 51-22-01, 51-40-02. (M) 2 L 7 2 4F RT 1999020500540 19990205 00540 EU 1999 2 5 USAA980668 1 19981224 A 5320 T-CAP FOKKER F28 F28MK0100 4990807 EU BS 3845-4850 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND CORROSION TOP SURFACE ENTIRE LENGTH 10 INCH T-CAP FS 3845-4850 AT BL 600R. REPLACED TOP C AP STRIP WITH LOCALLY FABRICATED PART OF 2024T3 PER SRM 53-12-10, 51-22-01, 51-40-02. (M) 2 L 7 2 4F RT 1999020500541 19990205 00541 EU 1999 2 5 USAA980669 1 19981224 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3845 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 2 INCH AREA TOP SURFACE CORRODED FS NR 3845 AT BL 914R BEAM. REPAIRED PER EA 51235. (M) 2 L 7 2 4F RT 1999020500542 19990205 00542 EU 1999 2 5 USAA980670 1 19981224 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 5305-5805 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 28 INCH APPROX SURFACE CORROSION ON BEAM BL 0 FS 5305-5805 T-CAP. REPLACED T-CAP SECTION USING 1710038 2024T3 STOCK PER SRM 53-12-10, 51-22-01, 51-40-02, 51-30-02. (M) 2 L 7 2 4F RT 1999020500543 19990205 00543 EU 1999 2 5 USAA980671 1 19981224 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 3845 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND CORROSION 6 INCHES LONG 100 PERCENT CORRODED THROUGH AT FS 3845 AT BL NR 0 BEAM TOP SURFAC E. REPLACED T-CAP SECTION USING 1710037 2024T3 STOCK PER SRM 53-12-10, 51-22-01, 51-40-02, 51-30-02. (M) 2 L 7 2 4F RT 1999020500544 19990205 00544 EU 1999 2 5 USAA980672 1 19981224 A 5320 T-CAP FOKKER F28 F28MK0100 4990807 EU BS 3845 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 2 INCH SECTION OF UNDERSIDE OF T-CAP CORROSION AT FS NR 3845 ( 2 INCHES FORWARD) AT BL NR 0 T-CAP. REPLACED T-CAP STRIP SECTION WITH 1710037 2024T3 STOCK PER SRM 53-12-10, 51-22-01, 51-40-02, 51-30-02. (M) 2 L 7 2 4F RT 1999020500545 19990205 00545 EU 1999 2 5 USAA980673 1 19981224 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 5305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND CORROSION 2 INCHES BY 7 INCHES BL 0 T-CAP STATION 5305 BEAM. REPLACED T-CAP SECTION 17100 37 2024T3 STOCK PER SRM 53-12-10, 51-40-02, 51-22-01, 51-30-02. (M) 2 L 7 2 4F RT 1999020500546 19990205 00546 EU 1999 2 5 USAA980674 1 19981224 A 5320 BEAM FOKKER F28 F28MK0100 4990807 EU BS 5305, 6305 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 1,000 MM BY 2 INCH CORROSION ON BEAM AT BL 600R STATION 5305, 6305. BLENDED OUT CORROSIO N PER EA 51234. (M) 2 L 7 2 4F RT 1999020500547 19990205 00547 EU 1999 2 5 USAA980675 1 19981224 A 5320 FITTING FOKKER F28 F28MK0100 4990807 EU PAX DOOR CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 2 INCH BY 2 INCH CORROSION AT FORWARD PAX DOOR GIRT BAR MOUNT FITTING. REPLACED BRACKET P ER SRM 53-12-10, 51-22-01, 51-40-02. (M) 2 L 7 2 4F RT 1999020500548 19990205 00548 EU 1999 2 5 USAA980676 1 19981224 A 5320 1156519 FITTING FOKKER F28 F28MK0100 4990807 EU BS 3820-4610 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 899US 15827 11399 PIT - DURING Q-1 CHECK, FOUND 2 INCHES BY 2 INCHES CORROSION AT PAX DOOR STATION 3820-4610 FITTING. DEFECTIVE PART REPL ACED WITH IDENTICAL PART NR 1156519. (M) 2 L 7 2 4F RT 1999020500549 19990205 00549 WP 1999 2 5 ARWA990103 1 19981101 A 5610 5887276501 WINDOW DOUG DC8 DC863F 302198F WP LT COCKPIT CRACKED A ARWA O OTHER O OTHER CR CRUISE 1 SO 19 661AV 97051H0317 45969 MIA - FLT 9502 - CAPTAIN WINDSHIELD CRACKED DURING FLIGHT. REMOVED AND REPLACED CAPTAINS WINDOW AND WINDOW HEAT CONTROL IAW MM 56-10-0 AND 30-41-0 SYSTEM CHECKED NORMAL. (M) 2 L 7 4 4F 4A25 1999020500553 19990205 00553 EU 1999 2 5 USAAF98009 2 19981228 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU RIGHT FAILED A USAA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 EA 19 893US 16211 11373 17380 DCA - FLT 2309 - ON CLIMB-OUT FROM DCA AT FL220, THE NR 2 GENERATOR FAILED. TWO MINUTES LATER THE NR 2 ENGINE SURGED. O NE MINUTE LATER, THE NR 2 ENGINE POWER REDUCED TO IDLE AND THE ENGINE AUTO SHUTDOWN. THE FLIGHT DIVERTED TO IAD AND LAN DED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE ASSEMBLY. (M) 2 L 7 2 4F 4 F RT 1999020500554 19990205 00554 EU 1999 2 5 USAAF98098 2 19981228 A 7200 ENGINE FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU LEFT FAILED A USAA A UNSCHED LANDING E J VIBRATION/BUFFET WARNING INDICATION CL CLIMB 1 EA 19 891US 18299 11366 17270 CLT - FLT 1864 - AFTER TAKEOFF FROM CLT A 'VIB HI ENG 1' INDICATION OCURRED. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED ENGINE VIBRATION FAULT ISOLATION PROCEDURES AND FOUND AIRCRAFT IN SAFE CONDITIO N FOR FERRY FLIGHT TO PIT. AT PIT, MAINTENANCE PERSONNEL REPLACED THE LEFT ENGINE ASSEMBLY. (M) 2 L 7 2 4F 4 F RT 1999020500555 19990205 00555 NE 1999 2 5 USAAD98224 2 19981231 A 7261 OIL FILTER DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9A 52048 NE LT ENGINE DAMAGED A USAA E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 EA 19 925VJ 48145 687853 BOS-IAD - FLT 238 - DURING CRUISE, THE LEFT ENGINE OIL QUANTITY DROPPED TO ZERO AND THE OIL PRESSURE WAS ALSO DROPPING. THE LEFT ENGINE WAS SHUT DOWN AND THE AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME WAS 21 MINUTES. MAINTENANCE REPAIRED THE OIL FILTER HOUSING PER THE PWA TYPICAL REPAIR 72-61-2A. (M) 2 L 7 2 4F 4 F A6WE E2EA 1999020500557 19990205 00557 NM 1999 2 5 USAASB98342 1 19981231 A 3260 189929 SENSOR BOEING 737 7374B7 1384702 NM RT MLG OUT OF ADJUST A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 439US 24781 CLT - FL1507 - FLIGHT RETURNED TO FIELD AT CLT FOR A CONFIGURATION WARNING HORN SOUNDING. CREW RECYCLED THE FLAPS, BUT HORN CONTINUED TO SOUND. WITH THE GEAR STILL DOWN AND UNABLE TO RETRACT, THE FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A BENT END OF THE AIR/GROUND SPOILER INTERLOCK CABLE. REPLACED BENT END O F CABLE AND PERFORMED FUNCTIONAL CHECK PER MM 27-62-51. FURTHERMORE, THREE MORE EVENTS OCCURRED OVER THE NEXT TWO DAYS FOR NOT BEING ABLE TO RETRACT THE LANDING GEAR HANDLE ONCE AIRBORNE. MAINTENANCE JACKED THE AIRCRAFT AND CHECKED THE RI GGING OF THE AIR/GROUND SENSING SAFETY SENSOR. ADJUSTED SENSOR PER MM. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999020500558 19990205 00558 EU 1999 2 5 SIMA983621 1 19981228 A 2910 AE7127841 HYDRAULIC LINE SAAB SF340 340B 7860101 EU NLG WW LEAKING A SIMA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SW 21 235AE 340B235 JFK - FLT 4830 - AFTER TAKEOFF WITH GEAR UP, NOTICED THE HYDRAULIC PUMP STILL RUNNING AND NO HYDRAULIC FLUID QUANTITY IN DICATED. HYDRAULIC ACCUMULATOR PRESSURE WAS GOOD. RETURNED TO JFK WHERE AIRCRAFT HAD TO BE TOWED FROM TAXIWAY. FOUND A HOLE IN THE HYDRAULIC LINE FROM THE PUMP TO THE FILTER. REMOVED AND REPLACED THE HYDRAULIC LINE, SERVICED SYSTEM, PE RFORMED LEAK AND OPERATIONAL CHECKS. RETURNED AIRCRAFT TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999020500559 19990205 00559 EU 1999 2 5 SIMA983591 1 19981225 A 3350 330151 POWER SUPPLY SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 370AM 1110 340B370 DFW - FLT 5284 - RIGHT FORWARD EMERGENCY EXIT LIGHT FLICKERS. REMOVED AND REPLACED FORWARD EMERGENCY LIGHT POWER SUPPLY . OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999020500560 19990205 00560 EU 1999 2 5 SIMA983563 1 19981222 A 2611 72111211000 SMOKE DETECTOR SAAB SF340 340B 7860101 EU AVIONICS BAY FAILED A SIMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 21 272AE A5264 340B272 SHV - FLT 5202 - ON TAKEOFF ROLL, AVIONICS SMOKE LIGHT ILLUMINATED. CREW FOLLOWED QRH AND RETURNED TO FIELD. LIGHT WEN T OUT AFTER AIRCRAFT TAXIED BACK TO GATE. REMOVED AVIONICS DOOR, INSPECTED AVIONICS BAY AND FOUND NO EVIDENCE OF SMOKE OR DAMAGE. DEFERRED AVIONIC SMOKE DETECTION SYSTEM AND RETURNED AIRCRAFT TO SERVICE. ITEM REMAINS DEFERRED AS OF 12-24 -98. ON 12-27-98, REMOVED AND REPLACED THE AVIONICS SMOKE DETECTOR. OPERATIONAL CHECK GOOD. MEL CLEARED. (M) 2 L 7 2 4T RT A52EU 1999020500561 19990205 00561 EU 1999 2 5 SIMA983631 1 19981229 A 3350 7239410001 HOLDER SAAB SF340 340B 7860101 EU CABIN BROKEN A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 343SB 340B343 SBP - EMERGENCY FLOOR PROXIMITY LIGHT AT 57LN HAD A BROKEN HOLDER. REMOVED AND REPLACED SIGN HOLDER. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999020500562 19990205 00562 EU 1999 2 5 SIMA983651 1 19981231 A 3350 BVO33020250 SOCKET SAAB SF340 SF340A 7850100 EU RT EMER EXIT FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 312AE 312 SBP - SIDE WALL EMERGENCY EXIT LIGHT ADJACENT TO RIGHT FORWARD EMERGENCY EXIT DOES NOT ILLUMINATE. REMOVED AND REPLACED BOTH LIGHT SOCKETS. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999020500563 19990205 00563 EU 1999 2 5 SIMA983652 1 19981231 A 3350 1317 LAMP SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST TX TAXI/GRND HDL 1 SW 21 309AE 340B309 DFW - FLT 5032 - EMERGENCY LIGHT ABOVE SEAT 4A DOES NOT ILLUMINATE. REMOVED AND REPLACED BULB. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999020500567 19990205 00567 EU 1999 2 5 USAAF98097 1 19981218 A 2740 TRIM SYSTEM FOKKER F28 F28MK0100 4990807 EU HORIZ STABILIZER MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 887US 11349 CLT - FLT 2208 - ON CLIMB-OUT FROM CLT, CREW RECEIVED A DOUBLER STAB TRIM FAULT INDICATION. FLIGHT RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESET THE STAB TRIM SYSTEM. ALL MAINTENANCE BITE TESTS PASSED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F RT 1999020500568 19990205 00568 EU 1999 2 5 99ZZZM79 1 19981103 A 7714 3033515 SENSOR AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 ENGINE FAILED A C2XA E ENGINE SHUTDOWN X Z O ENGINE FLAMEOUT SIGNIFICANT FAILURE REPORT OTHER AP APPROACH 1 SW 09 97841 280 120353 TEST FLIGHT NR 2 ENGINE, ECU PROBLEM. NR 2 ENGINE SHUTDOWN ON APPROACH. REMOVED AND REPLACED NR 2 ECU AND NH SENSOR. T EST FLOWN SATISFACTORY. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999020500569 19990205 00569 WP 1999 2 5 AALA990012 1 19981230 A 3211 TRUNNION DOUG DC10 DC1030 3023501 WP RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION IN FORWARD LUG OF FORWARD OF FORWARD TRUNNION. REMOVED CORROSION BY BORING LUG TO 4.0675 DIA. IN STALLED OVERSIZE BUSHING AND SHIM PER SRM 57-20-00. (M) 2 L 7 3 4F A22WE 1999020500570 19990205 00570 WP 1999 2 5 AALA990010 1 19981230 A 3211 TRUNNION DOUG DC10 DC1030 3023501 WP RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - CORROSION IN AFT LUG OF AFT RT MLG TRUNNION. REMOVED CORROSION BY BORING LUG TO 4.054 INCH. INSTALLED OVERSIZE B USHING AND SHIM PER SRM 57-20-00. (M) 2 L 7 3 4F A22WE 1999020500572 19990205 00572 WP 1999 2 5 AALA990008 1 19981228 A 5320 CHANNEL DOUG DC10 DC1030 3023501 WP BS 857-890 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON CHANNEL AROUND LAV TIE DOWN HOLES. REPLACED LAV SUPPORT CHANNEL PER AARD 51-10-00-01. (M) 2 L 7 3 4F A22WE 1999020500576 19990205 00576 NM 1999 2 5 AALA990027 1 19981217 A 5320 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - FORWARD DOOR FRAME STATION 950 HAS DEEP DENT, WORN AREA. ON TOP EDGE, BETWEEN 2ND AND 3RD UP DOOR STOPS. INSTALL ED DOUBLER PER SRM 51-40-4, 13 EACH .1875 HI-LOCKS, 2 EACH .3125 BOLTS, 2 EACH .3125 BOLTS, INSTALLED IN 17-7 REPAIR ANG LE (.080 THICK). (M) 2 L 7 3 4F A3WE 1999020500577 19990205 00577 NM 1999 2 5 AALA990026 1 19981217 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 948 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - LEFT STRIGNER 18A HAS VISUAL INDICATION OF CRACK AT STATION 948. REMOVED DAMAGED SECTION OF STRINGER 18A LEFT AND REPAIRED STRINGER WITH SPLICE PER ESO11697 DATED 12/16/98. (M) 2 L 7 3 4F A3WE 1999020500578 19990205 00578 NM 1999 2 5 AALA99025 1 19981211 A 2780 BRACKET BOEING 727 727223 1384074 NM NR 7 LE SLAT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - NR 7 SLAT ACT OUTBOARD MOUNT BRACKET CRACKED. REMOVED NR 7 SLAT ACT OUTBOARD BEARING PLATE AND INSTALLED REPAIR S TRAP PER AARD 57-50-03-02 PAGES 1-3. (M) 2 L 7 3 4F A3WE 1999020500579 19990205 00579 NM 1999 2 5 AALA990024 1 19981012 A 2780 BRACKET BOEING 727 727223 1384074 NM NR 7 LE SLAT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 897AA 22013 TUL - NR 7 SLAT ACT INBOARD MOUNT BRACKET CRACKED. REMOVED NR 7 SLAT ACT INBOARD BEARING PLATE. INSTALLED REPAIR STRAP PER AARD 57-50-03-2. (M) 2 L 7 3 4F A3WE 1999020500581 19990205 00581 NM 1999 2 5 AALA99036 1 19981216 A 5320 WEB BOEING 727 727223 1384074 NM BS 1343 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - LEFT TORQUE BOX WEB HAD HOLE WORN ALMOST THROUGH AT APROX STATION 1343 (VERT WEB). INSTALLED DOUBLER PER MM 51-40 -2. (M) 2 L 7 3 4F A3WE 1999020500582 19990205 00582 NM 1999 2 5 AALA990035 1 19981216 A 5320 BOEING 727 727223 1384074 NM UNKNOWN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - RIGHT TORQUE BOX HAD HOLE WORN ALMOST THROUGH AT APPROX STATION 1343, VERT WEB. INSTALLED DOUBLER PER MM 51-40-2. (M) 2 L 7 3 4F A3WE 1999020500583 19990205 00583 NM 1999 2 5 AALA990034 1 19981216 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 520 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - SHEAR TIE CRACKED STATION 52 BETWEEN STRINGER 27L-28L. REPAIRED PER SRM 53-10-4 FIG 15. (M) 2 L 7 3 4F A3WE 1999020500584 19990205 00584 NM 1999 2 5 AALA990033 1 19981221 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1183 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - AFT SIDE OF 1183 BULKHEAD ABOVE VAULT DOOR SKIN HAS SEVERAL DEEP TOOL MARKS LBL 20 TO RBL 20, 6 ABOVE CABIN FLOOR. INSTALLED DOUBLER PER ESO 11697, DATED 12/17/98. (M) 2 L 7 3 4F A3WE 1999020500585 19990205 00585 NM 1999 2 5 AALA990032 1 19981218 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1316-1340 MISDRILLED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - RIGHT LOWER TORQUE BOX LOWER CHORD ANGLE HAS 14 MISDRILLED HOLES WITH VISUAL INDICATION OF CRACK STATION 1323-1333 . ALSO, 9 MISDRILLED HOLES WITH VISUAL INDICATION OF CRACK STATION 1313-1323. INSTALLED REPAIR PER ESO 11697 DATED 12- 15-98. ANGLE WAS SPLICED AT STATION 1316 AND THE ENTIRE SECTION WAS REPLACED. THE ORIGINAL ESO WAS CHANGED BY ENGINEER ING TO ALLOW FOR ADDITIONAL RIVETS INSTALLED IN THE SPLICE. (M) 2 L 7 3 4F A3WE 1999020500586 19990205 00586 NM 1999 2 5 AALA990031 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - STATION 620 WEB CRACKED BEHIND PRESSURE SEAL RETAINER 10 INCH FROM LOWER END OF AFT CUT OUT. CUTOUT CRACK AND INS TALLED FILLER AND DOUBLER PER SRM 51-40-2 FIG 1. WEB 2025T-6 MATERIAL .071 FILLER, .080 DOUBLERS, .1875 FIRST OVER HI-L OCKS, 45 FASTENERS, 13 ROWS. (M) 2 L 7 3 4F A3WE 1999020500587 19990205 00587 NM 1999 2 5 AALA990030 1 19981216 A 5320 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - CARGO DOOR AFT CUTOUT WEB CRACKED 13 INCHES FROM LOWER END OF CUTOUT BEHIND SEAL RETAINER STATION 620. CUTOUT CRA CK AND INSTALLED FILLER AND DOUBLER PER SRM 51-40-2 FIG 1, USED 7075 T6 MATERIAL, .071 FILLER, .080 DOUBLERS, .1875 FIRS T OVER HI-LOCKS, 45 FASTENERS 13 ROWS. (M) 2 L 7 3 4F A3WE 1999020500588 19990205 00588 NM 1999 2 5 AALA990029 1 19981214 A 5320 FRAME BOEING 727 727223 1384074 NM CARGO DOORWAY CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - NR 2 CARGO DOOR FRAME (FORWARD FRAME) IN FUSE CUTOUT HAS CRCK EXTENDING FROM LOWER STOP CASTING, LOWER SIDE. NDT FOUND CRACK AT LOWER STOP FITTING LOCATION ON FRAME AND NDT SHOWS CRACK PROPOGATING UPWARDS UNDER STOP CASTINGS THROUGH THE OTHER SIDE OF THE SAME HOLE. STOP DRILLED CRACKS AND INSTALLED REPAIR DOUBLER PER SB 727-53A0199 AS AUTHORIZED BY C ARD 5295. (M) 2 L 7 3 4F A3WE 1999020500589 19990205 00589 NM 1999 2 5 AALA990028 1 19981214 A 5330 SKIN BOEING 727 727223 1384074 NM RT COCKPIT CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 6822 19700 TUL - FOUND CRACK IN FUSELAGE SKIN AT SCREW IN AFT UPPER CORNER OF CO-PILOTS NR 3 WINDOW. STOP DRILLED CRACK. INSTALLE D DOUBLER PER SRM 53-30-3 FIG 8, REPAIR NR 3. (M) 2 L 7 3 4F A3WE 1999020500590 19990205 00590 NM 1999 2 5 AALA982140 1 19981201 A 5330 SKIN BOEING 727 727227 1384078 NM BS 444-459 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 731AA 20738 TUL - FOUND FUSELAGE SKIN BULGED AND CRACKED AT STRINGER 25R AND BELOW, BETWEEN STATION 444 AND 459. CUT OUT DAMAGED AR EA SKIN STATION 440-463, STRINGER 25R TO 26R, SRM 53-30-3 FIG 14. INSTALLED 18 INCH BY 24 INCH DOUBLER PER MENTIONED SR M REF FILLER .063 INCH 2024T3. (M) 2 L 7 3 4F A3WE 1999020500591 19990205 00591 NM 1999 2 5 AALA982224 1 19981201 A 5320 FILLER BOEING 727 727227 1384078 NM BS 440 MISINSTALLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 731AA 20738 TUL - STRINGER 25R FILLER AFT STATION 440 HAS MATERIAL WITH LESS THICKNESS THAN ORIGINAL STRINGER MATERIAL. REMOVED FIL LER STATION 440, STRINGER 25R. INSTALLED NEW FILLER CORRECT SIZE .040 INCH. (M) 2 L 7 3 4F A3WE 1999020500592 19990205 00592 NM 1999 2 5 AALA982262 1 19981214 A 5330 SKIN BOEING 727 727223 1384074 NM BS 515-517 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - SKIN BULGED STATION 515 TO STATION 517 STRINGER 26R INBOARD TO INTERCOSTAL. CUT OUT DAMAGED AREA 8 INCH BY 2 INCH BELOW STRINGER 26R STATION 510 TO STATION 518. INSTALLED REPAIR DOUBLER PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999020500593 19990205 00593 NM 1999 2 5 AALA982261 1 19981218 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FUOND CORROSION ON BOTTOM SIDE OF STRINGER 27 LEFT STATION 500. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999020500594 19990205 00594 NM 1999 2 5 AALA982250 1 19981209 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND TOP OF FLOORBEAM CORRODED STATION 380 RBL 14 TO RBL 67. REMOVED CORROSION FROM TOP OF FLOORBEAM, AREA AT RB L 33.5 WAS BEYOND LIMITS. FABRICATED AND INSTALLED REPAIR ANGLES PER AARD 53-10-07-02 PAGE 1-4 PARA B, SUBSITUTED MAT P ER SRM 51-20-1 TREATED AND PRIMED ENTRIE AREA. (M) 2 L 7 3 4F A3WE 1999020500595 19990205 00595 NM 1999 2 5 AALA982259 1 19981218 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720-740 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND CORROSION INSIDE STRINGER 27R STATION 720F PLUS 3 INCHES TO 740. REPAIRED STRINGER PER SRM 53-10-3 FIG 1 PA GE 4B STRINGER 27R STATION 720F PLUS 3 INCHES TO STATION 740. (M) 2 L 7 3 4F A3WE 1999020500596 19990205 00596 NM 1999 2 5 AALA982258 1 19981218 A 5330 SKIN BOEING 727 727223 1384074 NM BS 482-492 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND STATION 482-492 OUTBOARD STRINGER 28R RBL 12 INCHES RBL THROUGH 13 INCHES SKIN CORRODED BELOW INTERCOSTAL LO WER ATTACH ANGLE (MARKED). INSTALLED SKIN REPAIR PER ESO 11697, DATED 12-17-98. (M) 2 L 7 3 4F A3WE 1999020500597 19990205 00597 NM 1999 2 5 AALA982257 1 19981218 A 5330 SKIN BOEING 727 727223 1384074 NM BS 500-504 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND STATION 500-504 AFT SIDE FRAME OUTBOARD STRINGER 27L SKIN CORRODED UNDER LEVELING COMPOUND (MARKED). INSTAL LED SKIN REPAIR PER ESO 11697, DATED 12-17-98. (M) 2 L 7 3 4F A3WE 1999020500598 19990205 00598 NM 1999 2 5 AALA982256 1 19981218 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND STRINGER 28R STATION 480 CORRODED. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999020500599 19990205 00599 NM 1999 2 5 AALA982255 1 19981216 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 476-480 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND CORROSION INSIDE STRINGER 26R STATION 476 - STATION 480. INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999020500600 19990205 00600 NM 1999 2 5 AALA992254 1 19981209 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND STRINGER 27L CORRODED INSIDE STATION 720E PLUS 5 INCH THROUGH 720E PLUS 7 INCH. REMOVED DAMAGED STRINGER 27 L FROM STATION 720E PLUS 10 INCHES AND STATION 720F PLUS 10 INCH AND INSTALLED SPLICES AND FILLER PER SRM 53-10-3 PAGE 3 . (M) 2 L 7 3 4F A3WE 1999020500601 19990205 00601 NM 1999 2 5 AALA982253 1 19981216 A 5320 PAN BOEING 727 727223 1384074 NM BS 1183 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND HEAVY CORROSION ON BOTTOM OF FLOOR PAN (CABIN) 6 INCHES FORWARD OF BS 1183 LBL 26, EXTENDING 6 INCHES FORWA RD AND 6 INCHES OUTBOARD, GOING OVER TOP OF FITTING AT LBL 27. FABRICATED AND INSTALLED REPAIR DOUBLER ON LEFT AFT LAV FLOOR PAN IAW SRM 51-40-2 FIG 1. (M) 2 L 7 3 4F A3WE 1999020500602 19990205 00602 NM 1999 2 5 AALA982252 1 19981216 A 5320 STRAP BOEING 727 727223 1384074 NM BS 1177 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND CORROSION ON STRAP AT STATION 1177 LEFT AFT LAVATORY AFT SPLASH LIP AREA AT CABLE FLOOR ATTACH FITTING AREA. FABRICATED AND INSTALLED REPAIR DOUBLER AT SPLASH LIP STRAP IAW SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999020500603 19990205 00603 NM 1999 2 5 AALA982251 1 19981214 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND CORROSION INSIDE OF STRINGER 27L STATION 720D PLUS 15 INCHES - 17 INCHES BELOW ELECTRICAL WIRE BUNDLE CLAMP. CORROSION REMOVAL WAS BEYOND LIMITS. REMOVED DAMAGED STRINGER 27L FROM 720E 12 INCHES TO 720F 10 INCHES AND INSTALLED SPLICES AND FILLER PER SRM 53-10-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1999020500604 19990205 00604 NM 1999 2 5 AALA982249 1 19981209 A 5320 651748455 STIFFENER BOEING 727 727223 1384074 NM BS 1464 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND CRACK IN STIFFENER JUST FORWARD AND BELOW LEFT FORWARD TENSION TIE BOLT. REPLACED STIFFENER WITH NEW STIFFE NER. (M) 2 L 7 3 4F A3WE 1999020500605 19990205 00605 NM 1999 2 5 AALA982248 1 19981217 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 500-502 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND SHEAR TIE CORRODED UNDER LEVELING COMPOUND OUTBOARD OF STRINGER 27L. INSTALLED NEW SHEAR TIE PER SRM 51-10- 1. (M) 2 L 7 3 4F A3WE 1999020500606 19990205 00606 NM 1999 2 5 AALA982247 1 19981218 A 5320 STRAP BOEING 727 727223 1384074 NM BS 614-619 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND FORWARD 8 INCHES OF STRAP CORRODED, EXFOLIATION THROUGH THE TAPERED STRAP. REMOVED OLD TAPERED STRAP P/N 65 -56181-6 AND INSTALLED NEW TAPERED STRAP WITH ORIGINAL HARDWARE PER SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999020500607 19990205 00607 NM 1999 2 5 AALA982246 1 19981216 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 600 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 896AA 22012 TUL - FOUND FORWARD SIDE STATION 600 OUTBOARD STRINGER 27L TO 26L SHEAR TIE CORRODED. INSTALLED NEW SHEAR TIE PER SRM 5 1-10-1. (M) 2 L 7 3 4F A3WE 1999020500609 19990205 00609 WP 1999 2 5 AALA990046 1 19980108 A 5313 LONGERON DOUG DC10 DC1030 3023501 WP BS 1964-1975 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION ON LONGERON 51R BETWEEN STATION 1964 AND 1975. REMOVED CORROSION ON LONGER 51R PER SRM 51-21-01. REPLACED STRINGER 651R END CAP PER AARD 51-01-00-05. TREATED PAINTED AND PRIMED PER SRM 51-21-01 VOL 2. (M) 2 L 7 3 4F A22WE 1999020500613 19990205 00613 WP 1999 2 5 AALA982242 1 19981215 A 5320 PAN DOUG DC9 DC982 3022082 WP PAX DOORWAY CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 441AA 49460 TUL - FOUND CORROSION ON DOOR PAN. REPLACED SPLICED SECTION OF NEW PAN PER SRM 53-05 FIG 44. (M) 2 L 7 2 4F A6WE 1999020500617 19990205 00617 NM 1999 2 5 AALA981085 1 19981217 A 3260 106122629 SENSOR BOEING 727 727223 1384074 NM RT MLG DEFECTIVE A AALA K NONE N FALSE WARNING CL CLIMB 1 SW 07 843AA 20984 DFW - FLT 1503 - AFTER TAKEOFF EWR EN ROUTE DFW, RIGHT MAIN LANDING GEAR RED LIGHT ILLUMINATED AND REMAINED ON FOR DURAT ION OF FLIGHT. RIGHT MAIN LANDING GEAR RED LIGHT EXTINGUISHED WHEN GEAR HANDLE WAS LOWERED AND RECEIVED DOWN AND LOCK I NDICATION. LANDED DFW WITHOUT INCIDENT. REPLACED RIGHT MAIN LANDING GEAR UPLOCK SENSOR. ACCOMPLISHED GEAR SWING ACCOR DING TO MM. SYSTEM GROUNC CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999020500621 19990205 00621 WP 1999 2 5 AALA982305 1 19981231 A 3260 833703 SENSOR ELDEC DOUG DC9 DC982 3022082 WP NLG DEFECTIVE A AALA O OTHER N FALSE WARNING TO TAKEOFF 1 SW 07 478AA 49653 ORD - FLT 435 - AFTER TAKEOFF, NOSE LANDING GEAR RED LIGHT ILLUMINATED WITH HANDLE UP. LIGHT WENT OUT WHEN GEAR WAS CYC LED. AIRCRAFT CONTINUTED TO ORD AND LANDED WITHOUT FURTHER INCIDENT. REPLACED NOSE LANDING GEAR UPLOCK SENSOR. ACCOMP LISHED NOSE LANDING GEAR RETRACTION CHECK WITH NO DEFECTS FOUND. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999020500624 19990205 00624 WP 1999 2 5 AALA982304 1 19981230 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 291AA 49303 DFW - DURING OVERNIGHT CHECK, AFT EMERGENCY EXIT L FLOOR PATH LIGHTS WERE INOPERATIVE. REPAIRED AFT EMERGENCY EXIT FLOO R PATH LIGHT WIRE AT BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999020500626 19990205 00626 NM 1999 2 5 AALA982239 1 19981228 A 3397 WIRE BOEING 767 767223 1385123 NM ROW 31 H SHORTED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 321AA 22322 ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FROM SEAT 31H TO AFT OF AIRCRFT INOPERATIVE. REPAIRED WIRE IN EMERGENCY EXIT SEAT LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999020500628 19990205 00628 NM 1999 2 5 USAASB98326 1 19981213 A 3260 655825029 CARD BOEING 737 7373B7 1384580 NM NLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 376US 22955 BWI - FLT 292 - SHORTLY AFTER GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CREW RECYCLED THE GEAR AND NOTED NO ABNORMAL VIBRATION OR OPERATION. NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FLIGHT CONTINUED ON AND LAN DED WITHOUT FURTHER INCIDENT. MANTENANCE INSPECTED NOSE GEAR ASSEMBLY AND INDICATION SSYTEM. NO FAULTS FOUND. REMOVED AND REPLACED THE M983 WARNING CARD AND THE R374 NOSE GEAR LATCHING RELAY AS PRECAUTIONARY. NOSE GEAR INDICATION OPERAT INALLY CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 1999020500629 19990205 00629 NM 1999 2 5 99ZZZM80 1 19981213 A 3260 BR20AXH5Y3 RELAY BOEING 737 7373B7 1384580 NM NLG MALFUNCTIONED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 376US 22955 BWI - FLT 292 - SHORTLY AFTER GEAR RETRACTION, THE NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. CREW RECYCLED THE GEAR AND NOTED NO ABNORMAL VIBRATION OR OPERATION. NOSE GEAR UNSAFE LIGHT REMAINED ILLUMINATED. FLIGHT CONTINUED ON AND LAN DED WITHOUT FURTHER INCIDENT. MANTENANCE INSPECTED NOSE GEAR ASSEMBLY AND INDICATION SSYTEM. NO FAULTS FOUND. REMOVED AND REPLACED THE M983 WARNING CARD AND THE R374 NOSE GEAR LATCHING RELAY AS PRECAUTIONARY. NOSE GEAR INDICATION OPERAT INALLY CHECKS NORMAL. (M) 2 L 7 2 4F RT A16WE 1999020500630 19990205 00630 NM 1999 2 5 AALA982169 1 19981203 A 5330 SKIN BOEING 727 727223 1384074 NM BS 490-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND FUSE SKIN CORRODED OUTBOARD STRINGER 28R STATION 490-500, BETWEEN STRINGER AND INTERCOSTAL. REMOVED DAMAGED AREA OF SKIN. INSTALLED DOUBLER REPAIR PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1999020500631 19990205 00631 NM 1999 2 5 AALA982168 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FUSELAGE SKIN IS CORRODED AFT SIDE OF STATION 720A. INSTALLED 8 INCHES BY 12 INCHES EXTERNAL DOUBLER PER SRM 53-3 0-3 FIG 3 SHEET 1 THROUGH 4. (M) 2 L 7 3 4F A3WE 1999020500632 19990205 00632 NM 1999 2 5 AALA982167 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 520 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND FUSELAGE SKIN IS CORRODED OUTBOARD OF STRINGER 27R STATION 520. INSTALLED DOUBLER AS PER SRM 53-30-3 PAGE 1 2-14A. (M) 2 L 7 3 4F A3WE 1999020500633 19990205 00633 NM 1999 2 5 AALA982166 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 418-440 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND 22 INCH LONG DENT IN SKIN STATION 418 TO 440 STRINGER 20R. REMOVED DAMAGED AREA AT SKIN AND INSTALLED DOUBL ER PER 53-30-3 FIG 2. (M) 2 L 7 3 4F A3WE 1999020500634 19990205 00634 NM 1999 2 5 AALA982165 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 345 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND FUSELAGE SKIN DENT .375 INCH BY 4 INCH APPROX 40 INCHES BELOW THE L3 WINDOW. TRIMMED OUT DAMAGED AREA AND I NSTALLED REPAIR DOUBLER PER SRM 53-30-3 PAGES 5-8 FIG 1. (M) 2 L 7 3 4F A3WE 1999020500635 19990205 00635 NM 1999 2 5 AALA982164 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 308 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND 3.5 INCH DENT IN SKIN AT STATION 308 STRINGER 22R. CUT OUT 3 INCH BY 4 INCH AREA AT STRINGER AND INSTALLED DOUBLER PER SRM 53-30-3 FIG 24. (M) 2 L 7 3 4F A3WE 1999020500636 19990205 00636 NM 1999 2 5 AALA982163 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 356 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND DEEP TOOLING MARKS ON INNER SKIN STATION 356 BETWEEN STRINGER 9R AND 10R. BLENDED GOUGES AND INSTALLED DOUB LER PER SRM 53-30-3 PAGE 508 SRM 53-30-3 PAGE 3B AND AARD 53-30-03-3 PAGE 1. (M) 2 L 7 3 4F A3WE 1999020500637 19990205 00637 NM 1999 2 5 AALA982162 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1010-1030 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND LARGE DOUBLER INSTALLED ON OUTERSKIN AND DAMAGE NOT REMOVED AND DOUBLER DENTED. REPLACED DOUBLER AS PER SRM 53-30-3 FIG 5. (M) 2 L 7 3 4F A3WE 1999020500638 19990205 00638 NM 1999 2 5 AALA982161 1 19981111 A 5330 SKIN BOEING 727 727223 1384074 NM BS 380-440 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND 63 INCH DENT IN SKIN AT STATION 380-440 AT STRINGER 23R-24R. ALSO, 2 INCH DENT WITH GOUGE AT STATION 407 AB OVE STRINGER 24R. REMOVED DAMAGED PORTION OF SKIN AND INSTALLED NEW SKIN PER SRM 53-30-03 FIG 6 AND 15A, STATION 360-44 0, STRINGER 22-26R. (M) 2 L 7 3 4F A3WE 1999020500639 19990205 00639 NM 1999 2 5 AALA982160 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 363 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND 2 INCH DENT WITH SCRATCHES STATION 363 STRINGER 20R. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM 53-30-3 P AGE 3-C. (M) 2 L 7 3 4F A3WE 1999020500640 19990205 00640 NM 1999 2 5 AALA982159 1 19981210 A 5730 SKIN BOEING 727 727223 1384074 NM BS 820 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND AREA OF CORROSION ON LOWER WING SKIN UNDER AREA OF LEFT PRIMARY HEAT EXCHANGER. REMOVED CORROSION, TREATED AND INSTALLED REPAIR DOUBLER PER ESO NR 11697 DATED 11-17-98 AND REF BOEING MESSAGE AAL-TUL-98 1122RR DATED 17 NOV 98. ( M) 2 L 7 3 4F A3WE 1999020500641 19990205 00641 NM 1999 2 5 AALA982158 1 19981209 A 5711 SPAR BOEING 727 727223 1384074 NM WS 512-516 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CORROSION ON FORWARD SPAR LOWER CHORD PLATE FS 514. INSTALLED REPAIR STRAP OVER BLENDOUT PER AARD 57-30-00- 2 PAGE 1-3. (M) 2 L 7 3 4F A3WE 1999020500642 19990205 00642 NM 1999 2 5 AALA982303 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 620 FROM STRINGER 23L TO STRINGER 25L. DENTS AT STRINGER 25L AND 23L WI THIN LIMITS PER AARD 53-10-07-3 PAGE 1, CUTOUT DAMAGE AT STRINGER 24L AND INSTALLED REPAIR DOUBLER PER 51-40-3. (M) 2 L 7 3 4F A3WE 1999020500643 19990205 00643 NM 1999 2 5 AALA982302 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1110 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME BENT INTO RADIUS FORWARD STATION 1110 AND STRINGER 26R TOP LEG. MADE OUTSIDE DOUBLER, REPAIR PER 51-40-3 SRM INSTALLED WET, ALODINED AND PRIMED. (M) 2 L 7 3 4F A3WE 1999020500644 19990205 00644 NM 1999 2 5 AALA982301 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 660 BETWEEN STRINGER 23R AND 25R. REMOVED AND REPLACED BELLFRAME SPLICE DOUBLER AT STRINGER 25R PART REPLACEMENT. CUTOUT DAMAGE AREAS (TWO PLACES) AND INSTALLED REPAIR DOUBLER AT STRINGER 23 R TO STRINGER 24R PER SRM 51-40-3 SSI REPAIR. (M) 2 L 7 3 4F A3WE 1999020500645 19990205 00645 NM 1999 2 5 AALA982300 1 19981203 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 680 BETWEEN STRINGER 22L TO STRINGER 25L. INSTALLED REPAIR PER SRM 51-4 0-3 USING 7075-T6 .063 INCH THICK, 6.5 INCH BY 4 INCH USING SIXTEEN .1875 UNIVERSAL D RIVETS AND FIVE .25 INCH UNIVERSAL D RIVETS AND THREE FASTENERS ROWS. (M) 2 L 7 3 4F A3WE 1999020500646 19990205 00646 NM 1999 2 5 AALA982299 1 19981203 A 5311 FRAME BOEING 727 727223 1384074 NM BS 600 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED TOP FLANGE FROM STRINGER 23L TO INBOARD SIDE OF STRINGER 25L STATION 600. INSTALLED REPAIR PER SRM 51-40-3 USING 7075-T6 .063 THICK, 25 INCH BY 4 INCH WIDE, USING 61 EACH .1875 UNIVERSAL D RIVETS AND 4 EACH .25 INCH UNIVERSAL D RIVETS AND 3 FASTENERS ROWS. (M) 2 L 7 3 4F A3WE 1999020500647 19990205 00647 NM 1999 2 5 AALA982298 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1130 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELL FRAME BENT INTO FORWARD RADIUS STATION 1130 AND STRINGER 26R TOP LEG. REPAIRED DAMAGE AREA WITH DOUBLE R PER 53-10-4. (M) 2 L 7 3 4F A3WE 1999020500648 19990205 00648 NM 1999 2 5 AALA982297 1 19981208 A 5311 FRAME BOEING 727 727223 1384074 NM BS 990 DEFORMED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME BEN AND DEFORMED AT BS 990 BETWEEN STRINGER 27L AND 26L. CUTOUT DAMAGED AREA, INSTALLED OUTSIDE D OUBLER SRM 53-10-4. BELLFRAME WAS ALODINED AND PRIMED AND INSTALLED WET WITH SEALANT USED H6426 HI-LOCKS. (M) 2 L 7 3 4F A3WE 1999020500649 19990205 00649 NM 1999 2 5 AALA982296 1 19981202 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED ALONG TOP FLANGE FROM STRINGER 22R TO 24R, STATION 500. DENTS AT STRINGER 23R AND 22R WITH IN LIMITS PER AARD 53-10-10-07-3 PAGE 1. CUTOUT DENT AT STRINGER 24R AND INSTALLED DOUBLER 7075-T6 REPAIR PER 51-40-3 P AGE 3, CUT OUT AREA 1 INCH .063 THICKNESS DOUBLER 7 INCHES IN LENGTH USING 20 MS 20470 D FASTENERS .1875, 3 ROWS PAST DA MAGE CUTOUT, 1 ROW ALONG TOP. (M) 2 L 7 3 4F A3WE 1999020500650 19990205 00650 NM 1999 2 5 AALA982295 1 19981204 A 5311 FRAME BOEING 727 727223 1384074 NM BS 540 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED STATION 540 STRINGER 24 LEFT ON TOP FLANGE. INSTALLED DOUBLER PER SRM 51-40-3 SIZE 7 INCHE S BY 4 INCHES, USING 7075-T6 MATERIAL, .063 INCH THICK, WITH 21 MS 20470D .1875 FASTENERS, 4 OF WHICH ARE .24 INCH, IN 3 FASTENER ROWS. (M) 2 L 7 3 4F A3WE 1999020500651 19990205 00651 NM 1999 2 5 AALA982294 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED SEVERAL PLACES ON TOP FLANGE STATION 520, FROM STRINGER 22L TO 25L. REMOVED DAMAGE INSTALL ED 28 INCHES DOUBLER OF 7075T6 .063 INCH WITH 71 EACH .1875 INCH D RIVETS, 4 EACH .25 INCH RIVETS ALL UNIVERSAL HEADS AN D TWO FLUSH .1875 RIVETS, PER SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999020500652 19990205 00652 NM 1999 2 5 AALA982293 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED ONTOP FLANGE STATION 700 FROM STRINGER 22R TO STRINGER 24R. REMOVED DAMAGED INSTALELD 17.5 INCH DOUBLER OF 7075T6 .063 INCH WITH 37 MS20470 D .1875 FASTENERS PER SRM 51-40-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999020500653 19990205 00653 NM 1999 2 5 AALA982292 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED IN SEVERAL PLACES, STATION 500 FROM STRINGER 22L TO 25L. REMOVED DAMAGED INSTALLED 19 INCH DOUBLER OF 7075T6 .063 INCH WITH 44 EACH .1875 D RIVETS, 2 EACH .25 INCH D RIVETS ALL UNIVERSAL HEADS PER SRM 51-40-3 F IG 1. (M) 2 L 7 3 4F A3WE 1999020500654 19990205 00654 NM 1999 2 5 AALA982291 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 660 FROM STRINGER 28L TO STRINGER 24L. REMOVED DAMAGE AREA, FROM 23L-24 L, STATION 660. INSTALLED .063 DOUBLER 18 INCH LONG, 7075T6 COVERED TWO DAMAGE AREAS 1 INCH BY 1.5 INCH AND 1 INCH BY 2 INCH. USED 45 EACH MS20470D RIVETS AND 4 EACH MS 20470 D8 RIVETS. (M) 2 L 7 3 4F A3WE 1999020500655 19990205 00655 NM 1999 2 5 AALA982290 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME DENTED TOP FLANGE STATION 680 FROM STRINGER 24R TO STRINGER 25R. REMOVED DAMAGE, INSTALLED 14 INC H DOUBLER PER AARD 53-10-07-3 PAGE 1 OF 7075T6 .063 INCH THICK WITH 29 MS2040D .1875 INCH RIVETS, 4 MS2040D .25 INCH RIV ETS. (M) 2 L 7 3 4F A3WE 1999020500656 19990205 00656 NM 1999 2 5 AALA982289 1 19981210 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND STRINGER 27R AT BS 990, LOWER FLANGE CORRODED FROM APPROX BS 985 TO BS 993. BLENDED CORROSION OUT, DAMAGED AREA WAS BEYOND LIMITS. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED NEW SECTION OF STRINGER AND DOUBLER PER ESO 116 97 DATED 12-1-98 AND SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1999020500657 19990205 00657 NM 1999 2 5 AALA982288 1 19981206 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND CORROSION UNDER SEALER AROUND LIGHT PAN STATION 720 B - 720C STRINGER 15L. REMOVED CORROSION, REPAIRED SKIN AT WING ICE LIGHT CUT OUT PER SRM 53-30-3. (M) 2 L 7 3 4F A3WE 1999020500658 19990205 00658 NM 1999 2 5 AALA982287 1 19981216 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND BELLFRAME 720E SPOTTED WITH CORROSION FROM STRINGER 4L TO 8L. REMOVED DAMAGED AREA CUT TO SIZE FILLERS AND DOUBLERS DRILLED, ALODINED, PRIMED, SEALED AND INSTALLED FASTENERS PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999020500659 19990205 00659 NM 1999 2 5 AALA982286 1 19981216 A 5743 FITTING BOEING 727 727223 1384074 NM LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND LEFT GEAR FORWARD TRUNNION SUPPORT FITTING HAS PITTING INSIDE 4 EACH BUSHING BORES. REMOVED PITTING BY OVER SIZING BUSHING BORES AND INSTALLING NEW BUSHINGS. REPAIRED PER ESO 11697 DATED 11-24-98. (M) 2 L 7 3 4F A3WE 1999020500660 19990205 00660 NM 1999 2 5 AALA982285 1 19981202 A 3230 65864482 LINK BOEING 727 727223 1384074 NM RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND 4 LARGE HOLES HAVE FRETTING CORROSION. REMOVED CORROSION TREATED AND INSTALLED REPAIR BUSINGS AND WASHERS P ER ESO 11697 DATED 11-30-98. (M) 2 L 7 3 4F A3WE 1999020500661 19990205 00661 NM 1999 2 5 AALA982284 1 19981204 A 5320 CLIP BOEING 727 727223 1384074 NM BS 555 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND STRINGER 26L SUPPORT CLIP CORRODED STATION 555. REMOVED AND REPLACED STRINGER SUPPORT CLIP PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1999020500662 19990205 00662 NM 1999 2 5 AALA982283 1 19981202 A 5730 SKIN BOEING 727 727223 1384074 NM BS 834 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND CORROSION AT STRINGER 874 LBL 28 ON LOWER SKIN WING CENTER SECTION. REMOVED CORROSION AND INSTALLED REPAIR DOUBLER PER SRM 57-30-3 PAGE 22. (M) 2 L 7 3 4F A3WE 1999020500663 19990205 00663 NM 1999 2 5 AALA982282 1 19981216 A 5313 651891566 STIFFENER BOEING 727 727223 1384074 NM BS 303.9 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND RIGHT N/G TRUNNION FORWARD UPPER SUPPORT BEAM CORRODED FORWARD SIDE OF CUTOUT FORWARD STIFFENER. REMOVED ST IFFENER, MILLSHOP FABRICATED NEW STIFFENER PER DWG 65-18915. STIFFENER WAS TREATED PRIMED AND INSTALLED WITH HI-LOCK AT ORIGINAL FASTENER HOLES SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999020500664 19990205 00664 NM 1999 2 5 AALA992281 1 19981206 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND STRINGER 15L CRACKED AT FORWARD FASTENER STATION 720B. CUT OUT DAMAGED SECTION STRINGER 15L. INSTALLED SPL ICE REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999020500665 19990205 00665 NM 1999 2 5 AALA982280 1 19981203 A 5311 FRAME BOEING 727 727223 1384074 NM BS 804.5 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND FUSELAGE FRAME AT STATION 804.5, OUTBOARD CHORD CRACKED IN RADIUS AT STRINGER 14L. INSTALLED NEW OUTBOARD C HORD SECTION PER SRM 51-10-1 PAGE 4. (M) 2 L 7 3 4F A3WE 1999020500666 19990205 00666 NM 1999 2 5 AALA982279 1 19981207 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 740 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND STRINGER 2R GOUGED AT END FASTENER TO END FITTING UNDER HAT SECTION STATION 740 STRINGER 2R. CUT OUT DAMAGE D FLANGE AND INSTALLED EXTENDED LENGTH END FITTING PER ESO 11697, DATED 12/7/98. (M) 2 L 7 3 4F A3WE 1999020500667 19990205 00667 NM 1999 2 5 AALA982278 1 19981206 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND STRINGER 15L AFT OF WING ICE LIGHT, CRACKED AT FORWARD FASTENER STATION 720C. REMOVED DAMAGED SECTION OF ST RINGER 15L. INSTALLED SPLICE REPAIR PER SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999020500668 19990205 00668 NM 1999 2 5 AALA982277 1 19981204 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND STRINGER 15R STATION 720B CRACKED JUST FORWARD OF ICE LIGHT. REPAIRED DAMAGED STRINGER BY SPLICING SECTION FROM 720A PLUS 10, TO ICE LIGHT BOX, AS PER SRM 53-10-3 PAGE 3-4B. (M) 2 L 7 3 4F A3WE 1999020500669 19990205 00669 NM 1999 2 5 AALA982276 1 19981216 A 5320 651891564 STIFFENER BOEING 727 727223 1384074 NM BS 303.9 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND RIGHT N/G TRUNNION FORWARD UPPER SUPPORT BEAM IN CUTOUT CORRODED AT INBOARD END TOP AND BOTTOM FLANGES. REM OVED STIFFENER , SHOP FABRICATED NEW STIFFENER PER DWG 65-18915. STIFFENER WAS TREATED PRIMED AND INSTALLED WITH HI-LOC KS AT ORIGINAL FASTENER HOLES SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999020500670 19990205 00670 NM 1999 2 5 AALA982275 1 19981216 A 5320 651891550 STIFFENER BOEING 727 727223 1384074 NM BS 312 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND RIGHT N/R TRUNNION AFT UPPER SUPPORT BEAM IN CUTOUT. TOP FLANGE CORRODED INBOARD AND OUTBOARD END. REMOVED STIFFENER MILL SHOP FABRICATED NEW STIFFENER PER DWG 65-18915. STIFFENER WAS TREATED, PRIMED AND INSTALLED WITH HI-LOC KS AT ORIGINAL FASTENERS LOCATIONS SRM 51-10-1. (M) 2 L 7 3 4F A3WE 1999020500671 19990205 00671 NM 1999 2 5 AALA982274 1 19981203 A 3221 TRUNNION BOEING 727 727223 1384074 NM NLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND LEFT NLG TRUNNION BORE CORRODED. INSTALLED NEW LEFT NLG TRUNNION. (M) 2 L 7 3 4F A3WE 1999020500672 19990205 00672 NM 1999 2 5 AALA982273 1 19981214 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1070 DAMAGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FASTENER HOLE DAMAGED AT STATION 1070 STRINGER 28L. INSTALLED DOUBLER IAW SRM 53-30-3 FIG 1 PAGE 5. (M) 2 L 7 3 4F A3WE 1999020500673 19990205 00673 NM 1999 2 5 AALA982272 1 19981208 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1148 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND SHEAR TIE CORRODED AFT SIDE STATION 1148, BETWEEN STRINGER 30R AND 29R. REMOVED CORROSION PER SRM 51-10-6 A LODINED AND PRIMED. (M) 2 L 7 3 4F A3WE 1999020500674 19990205 00674 NM 1999 2 5 AALA982271 1 19981204 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 990 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND SHEAR TIE CORRODED AT STATION 990 BETWEEN STRIGNER 28L-29L. REMOVED CORROSION SHEAR TIE AND INSTALLED REPLA CEMENT SHEAR TIE PER SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999020500675 19990205 00675 NM 1999 2 5 AALA982270 1 19981204 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 703 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND STRINGER 27 LEFT CORRODED AT FASTENER HOSE STATION 703. REPAIRED PER SRM 53-10-3 PAGE 3-4B. (M) 2 L 7 3 4F A3WE 1999020500676 19990205 00676 NM 1999 2 5 AALA982269 1 19981204 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 216 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND FSS 212-223 ABOVE AND AFT A/I DUCT, 4 EACH GROUNDS CORRODED ON STRINGER. REMOVED CORRODED SECTION OF STRING ER. INSTALLED SPLICE REPAIR PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1999020500677 19990205 00677 NM 1999 2 5 AALA982268 1 19981204 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 180-196 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND 4 EACH GROUNDS CORRODED ON STRINGER ABOVE AND AFT A/I DUCT BETWEEN STATION 180-196. REMOVED CORRODED SECTIO N OF STRINGER. INSTALLED SPLICE REPAIR PER SRM 51-40-4. (M) 2 L 7 3 4F A3WE 1999020500678 19990205 00678 NM 1999 2 5 AALA982267 1 19981202 A 5320 SHEAR TIE BOEING 727 727223 1384074 NM BS 1110 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND SHEAR TIE CORRODED AT BS 1110 BETWEEN STRINGER 26L AND 27L. INSTALLED NEW SHEAR TIE, WORKED PER SRM 53-10-4 FIG 11. (M) 2 L 7 3 4F A3WE 1999020500679 19990205 00679 NM 1999 2 5 AALA982266 1 19981216 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND CORROSION ON FLOORBEAM STATION 380 BL 0 TO RBL 65. REPAIRED PER SRM 53-10-08 FIG 9A AND 9B AT STATION 380 R BL 27. REPAIRED PER SRM 53-10-08 FIG 9A AND 9B AT STATION 380 RBL 39 TO RBL 71. (M) 2 L 7 3 4F A3WE 1999020500680 19990205 00680 NM 1999 2 5 AALA982265 1 19981216 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND CORROSION ON FLOORBEAM STATION 344 LBL 40 TO RBL 60, TOP FLANGE. INSTALLED NEW T-ANGLE SECTION AND SPLICE P ER SRM 53-10-8 FIG 9. (M) 2 L 7 3 4F A3WE 1999020500681 19990205 00681 NM 1999 2 5 AALA982264 1 19981216 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND SKIN EXFOLIATED AND CRACKED APPROX 3 INCHES LONG STATION 720 PLUS 14 TO STATION 720 PLUS 18 AT STRINGER 27L. REMOVED CORROSION BY CUTTING OUT EXFOLIATED SECTION OF SKIN. ALODINED AND PRIMED CUT OUT. INSTALLED SKIN REPAIR PER SRM 53-30-3 FIG 3. (M) 2 L 7 3 4F A3WE 1999020500682 19990205 00682 NM 1999 2 5 AALA982263 1 19981204 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 891AA 22007 TUL - FOUND CORROSION ON FUSELAGE SKIN AROUND LIGHT PAN 720B-720C AT STRINGER 15R. ACCOMPLISHED ICE LIGHT CUT OUT REPAI R DOUBLER INSTALLATION PER ESO 11697 DATED 12/2/98. (M) 2 L 7 3 4F A3WE 1999020500683 19990205 00683 WP 1999 2 5 AALA982223 1 19981214 A 5320 ANGLE DOUG DC10 DC1010 3022110 WP BS 1841 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 127AA 46948 TUL - FOUND TOP OF FRAME 1841 CORRODED BETWEEN LONGERON 48L TO 48R. INSTALLED DOUBLER REPAIR PER SRM VOL 1 51-00-01. ( M) 2 L 7 3 4F A22WE 1999020500684 19990205 00684 WP 1999 2 5 AALA982135 1 19981118 A 5743 TRUNNION DOUG DC10 DC1010 3022110 WP WS 264 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CORROSION PITTING IN TOP AFT MOUNT HOLE IN THE MAIN GEAR TRUNNION FITTING FOR RETRACT CYLINDER UPPER SUPPORT FRAME RIGHT WING. REPAIRED PER ESO 7349, DATED 11-17-98. (M) 2 L 7 3 4F A22WE 1999020500685 19990205 00685 WP 1999 2 5 AALA982134 1 19981101 A 5343 TRUNNION DOUG DC10 DC1010 3022110 WP LT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CORROSION IN TRUNNION BORE OF HOLES FOR FITTING ARB 7170-1 FOR UPLOCK CYLINDERS. CORROSION REMOVAL AND REWO RKED PER ESO 7349 DATED 11-5-98 AND ESO 7349 DATED 11-17-98. (M) 2 L 7 3 4F A22WE 1999020500686 19990205 00686 WP 1999 2 5 AALA982133 1 19981118 A 5743 TRUNNION DOUG DC10 DC1010 3022110 WP WS 264 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 126AA 46947 TUL - FOUND CORROSION PITTING IN TOP FORWARD MOUNT HOLE IN THE MAIN GEAR TRUNNION FITTING FOR RETRACT CYLINDER UPPER SUP PORT FRAME. REPAIRED PER ESO 7349, DATED 11-18-98. (M) 2 L 7 3 4F A22WE 1999020500687 19990205 00687 WP 1999 2 5 AALA982245 1 19981214 A 5311 FRAME DOUG DC10 DC1010 3022110 WP BS 859 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 127AA 46948 TUL - FOUND LOWER LIP OF FRAME CORRODED (MARKED). REMOVED CORRODED PART, SPLICED IN NEW SECTION OF FRAME AS PER DC10 SR M 53-30-00 PAGE 3. TREATED AND PAINTED PER DC10 SRM 51-21-02 VOL 2. (M) 2 L 7 3 4F A22WE 1999020500688 19990205 00688 NM 1999 2 5 AALA982142 1 19981202 A 5312 BULKHEAD ANGLE DOUG MD11 MD11 3023602 NM BS 2007 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 1763 48553 TUL - FOUND CORROSION ON LOWER PRESSURE BULKHEAD TEE ANGLE ON BOTH SIDES OF SEAT TRACK NR 8. REMOVED OUT OF LIMITS SECT ION AT TEE ANGLE FABRICATED NEW SECTION. INSTALLED WET WITH PR1436 SEALANT WITH RIVETS, HI-LOCKS, AND SPLICE 53-40-00-0 . (M) 2 L 7 3 4F RT A22WE 1999020500689 19990205 00689 WP 1999 2 5 AALA990013 1 19981230 A 3211 TRUNNION DOUG DC10 DC1030 3023501 WP RT MLG CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 144AA 47848 TUL - FOUND CORROSION IN AFT LUG OF FORWARD TRUNNION. REMOVED CORROSION BY BORING LUG TO 4.072 DIAMETER. INSTALLED OVE RSIZE BUSHING AND SHIM PER SRM 57-20-00. (M) 2 L 7 3 4F A22WE 1999020500690 19990205 00690 SO 1999 2 5 C2XA98IA550 1 19981229 A 3231 12012347001 LATCH EMB 120 EMB120RT SO NLG DOORS UNLATCHED A C2XA A UNSCHED LANDING E VIBRATION/BUFFET CL CLIMB 1 SW 09 31711 120107 IAH - FLT 3795 - THE CREW REPORTED A VIBRATION AFTER TAKEOFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCI DENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LANDING GEAR DOORS TO BE UNLATCHED. MAINTENANCE LATCHED THE GEA R DOORS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999020500691 19990205 00691 CE 1999 2 5 C2XA98CL089 1 19981227 A 3230 1143640681 PC BOARD BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A C2XA O OTHER J WARNING INDICATION CL CLIMB 1 SW 09 81538 UE199 CLT - FLT 3268 - CREW REPORTED THAT AFTER DEPARTURE, THE LANDING GEAR WOULD NOT RETRACT, AIRCRAFT CONTINUED ON TO CLE FR OM CVG. AIRCRAFT LANDED IN CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED PC BOARD A316 IAW B1900 MM 3 2-30-00. THE RIGHT GEAR SQUAT SWITCH WAS ALSO READJUSTED FOR PRECAUTIONARY MEASURE IAW B1900 MM 32-60-05. OPERATIONAL CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A24CE 1999020500693 19990205 00693 SO 1999 2 5 C2XA98IA531 1 19981218 A 5400 12022766002 HAT SECTION EMB 120 EMB120RT SO LT NACELLE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, AFTER LEFT WING NACELLE FLAP REMOVAL, FOUND LOWER HAT SECTION DAMAGED (HOLE) IN FLAP WELL. R EMOVED AND REPLACED LOWER DAMAGED HAT SECTION. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999020500694 19990205 00694 SO 1999 2 5 C2XA98IA527 1 19981218 A 5280 12036136001 FITTING EMB 120 EMB120RT SO MLG DOOR BROKEN A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 16729 120185 DURING C-CHECK INSPECTION, FOUND THE RIGHT MLG AFT INBOARD DOOR AFT HINGE FITTING BROKEN. REMOVED AND REPLACED HINGE FI TTING. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A31SO 1999020500695 19990205 00695 NM 1999 2 5 99ZZZM81 1 19981126 A 3610 DUCT BOEING 727 72751C 1384015 NM NR 1 ENGINE LEAKING A RYNA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 07 435EX 19288 FLT 711 - EWR - ENGINE FIRE INDICATION ONR NR 1 ENGINE DURING CLIMB-OUT. SHUT DOWN NR 1 ENGINE. REMOVED AND REPLACED F IRE BOTTLE AND SQUIB CARTRIDGE NR 1 ENGINE. RESEALED CLAMPS ON NR 1 ENGINE STARTER DUCT. (M) 2 L 7 3 4F A3WE 1999020500696 19990205 00696 NM 1999 2 5 USAASB98341 1 19981231 A 8012 97907821 START VALVE BOEING 737 7372B7 1384560 NM NR 1 ENGINE INOPERATIVE A USAA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 271AU 14151 22883 BWI - FL2696 - CAPT REPORTED THAT THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED IN FLIGHT AT APPROX FL250. CAPT ST ARTED DESCENT AND RETURN TO BWI. THE NR 1 ENGINE WAS SHUT DOWN AT FL100. FLIGHT LANDED AT BWI WITHOUT INCIDENT AND TAX IED TO THE GATE. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE VERIFIED THE NR 1 EN GINE START VALVE WAS CLOSED AND THE SYSTEM OPERATED NORMAL. REPLACED NR 1 ENGINE START VALVE AS PRECAUTIONARY. OPS CHE CK GOOD PER MM. (M) 2 L 7 2 4F A16WE 1999020500697 19990205 00697 NM 1999 2 5 USAASB98332 1 19981218 A 2150 20405010 ACM BOEING 737 737301 1384611 NM RIGHT INOPERATIVE A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 336US 23233 LGA - FL248 - DURING CLIMB-OUT FROM LGA, THE FLIGHT CREW NOTICED A STRONG ODOR IN THE COCKPIT AND THE CABIN. NO SMOKE W AS NOTICED IN THE AIRCRAFT. FLIGHT RETURNED TO FIELD AT LGA AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECL ARED AND THE CABIN WAS PREPPED FOR AN EMERGENCY. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE AND THE RIGHT PACK VALVE INOPERATIVE. REPLACED RIGHT AIR CYCLE MACHINE AND RIGHT PACK VALVE PER MM. ALSO, REPLACED RIGHT PACK WATER SEPARATOR BAG. RAN PACK FOR ONE HOUR. NO ODOR PRESENT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999020500698 19990205 00698 NM 1999 2 5 99ZZZM82 1 19981218 A 2150 3964421 PACK VALVE BOEING 737 737301 1384611 NM RIGHT FAILED A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 336US 23233 LGA - FL248 - DURING CLIMB-OUT FROM LGA, THE FLIGHT CREW NOTICED A STRONG ODOR IN THE COCKPIT AND THE CABIN. NO SMOKE W AS NOTICED IN THE AIRCRAFT. FLIGHT RETURNED TO FIELD AT LGA AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECL ARED AND THE CABIN WAS PREPPED FOR AN EMERGENCY. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE AND THE RIGHT PACK VALVE INOPERATIVE. REPLACED RIGHT AIR CYCLE MACHINE AND RIGHT PACK VALVE PER MM. ALSO, REPLACED RIGHT PACK WATER SEPARATOR BAG. RAN PACK FOR ONE HOUR. NO ODOR PRESENT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999020500699 19990205 00699 NM 1999 2 5 99ZZZM83 1 19981218 A 2170 V1211 COALESCER BOEING 737 737301 1384611 NM CABIN DIRTY A USAA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 EA 19 336US 23233 LGA - FL248 - DURING CLIMB-OUT FROM LGA, THE FLIGHT CREW NOTICED A STRONG ODOR IN THE COCKPIT AND THE CABIN. NO SMOKE W AS NOTICED IN THE AIRCRAFT. FLIGHT RETURNED TO FIELD AT LGA AND LANDED WITHOUT FURTHER INCIDENT. AN EMERGENCY WAS DECL ARED AND THE CABIN WAS PREPPED FOR AN EMERGENCY. MAINTENANCE FOUND THE RIGHT AIR CYCLE MACHINE AND THE RIGHT PACK VALVE INOPERATIVE. REPLACED RIGHT AIR CYCLE MACHINE AND RIGHT PACK VALVE PER MM. ALSO, REPLACED RIGHT PACK WATER SEPARATOR BAG. RAN PACK FOR ONE HOUR. NO ODOR PRESENT. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999020500701 19990205 00701 SO 1999 2 5 RAAA99E8021 1 19981215 A 5230 SKIN LKHEED 188 188C 5262604 SO CARGO DOOR CRACKED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.56, FOUND FWD LOWER CARGO COMPARTMENT DOOR SKIN BENT AND CRACKED ALONG LOWER EDGE AT FS 264. REPAIRED PER SRM 53-2-1, PG 10 M-54 NR 155. 2 L 7 4 4T 4A22 1999020500702 19990205 00702 SO 1999 2 5 RAAA99E8022 1 19981215 A 5320 DOUBLER LKHEED 188 188C 5262604 SO BS 374 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.60, FOUND FS 374 MAIN CARGO DOOR SILL DOUBLER CORRODED AT STR 50. REPAIRED P ER SRM 53-2-3, M-54 NR 652. 2 L 7 4 4T 4A22 1999020500703 19990205 00703 SO 1999 2 5 RAAA99E8023 1 19981215 A 5313 STRINGER LKHEED 188 188C 5262604 SO BS 901-939 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.58, FOUND STR 35 CORRODED FROM FS 901 TO 939. REPAIRED PER SRM 53-1-2, M-54 NR 387. 2 L 7 4 4T 4A22 1999020500704 19990205 00704 SO 1999 2 5 RAAA99E8024 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 695 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.103, FOUND FS 695 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED AT RBL 42. REPAI RED PER SRM 53-2-3, M-54 NR 624. 2 L 7 4 4T 4A22 1999020500705 19990205 00705 SO 1999 2 5 RAAA99E8025 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 416 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND FS 416 TRANSVERSE FLOORBEAM CORRODED AT LBL 27. REPAIRED PER SRM 53-2-4 FIG 2 SHEET 2, M-54 NR 428. 2 L 7 4 4T 4A22 1999020500706 19990205 00706 SO 1999 2 5 RAAA99E8026 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 464 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND FS 464 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED FROM LBL 36 TO 44 . REPAIRED PER SRM 53-2-4 FIG 2 SHEET 1, M-54 NR 639. 2 L 7 4 4T 4A22 1999020500707 19990205 00707 SO 1999 2 5 RAAA99E8027 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 371 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND FS 371 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED LBL 26. REPAIRED PER SRM 53-2-4 FIG 2 SHEET 1, M-54 NR 429. 2 L 7 4 4T 4A22 1999020500708 19990205 00708 SO 1999 2 5 RAAA99E8028 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 464 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND FS 464 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED FROM LBL 4 TO RBL 4. REPAIRED PER SRM 53-2-4 FIG 2 SHEET 1, M-54 NR 429. 2 L 7 4 4T 4A22 1999020500709 19990205 00709 SO 1999 2 5 RAAA99E8029 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 560 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND FS 560 TRANSVERSE FLOORBEAM FWD FLANGE CORRODED AT RBL 48. REPAI RED PER SRM 53-2-4 FIG 2 SHEET 5, M-54 NR 616. 2 L 7 4 4T 4A22 1999020500710 19990205 00710 SO 1999 2 5 RAAA99E8030 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 380 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND FS 380 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED FROM RBL 43 TO 6 0. REPAIRED PER SRM 53-2-4 FIG 2 SHEET 1, M-54 NR 424. 2 L 7 4 4T 4A22 1999020500713 19990205 00713 WP 1999 2 5 9811451159 1 19981002 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 454 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 159US 46768 DURING M-CHECK, FOUND FRAME CRACKED AT FS 454, RBL 64. REPAIRED PER EA 11-161107. 2 L 7 3 4F A22WE 1999020500714 19990205 00714 NM 1999 2 5 9811466623 1 19981216 A 5315 FLOORBEAM BOEING 747 747251B 1384892 NM BS 1265 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 623US 21705 DURING PERIODIC CHECK, FOUND CRACK INDICATIONS IN A HOLE FS 1265, STR 26L, LBL 121 IN REINFORCING CHANNEL AND FLOORBEAM WEB AND REINFORCING STRAP. REPAIRED PER EA 66-162728 AND DRAWING 65B13386. 2 L 7 4 4F A20WE 1999020500732 19990205 00732 WP 1999 2 5 UPS99828595 1 19981230 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 690 DAMAGED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-123D, FUSELAGE SKIN REPLACEMENT NEEDS REPAIR SPLICES BOTH SIDE (LT& RT). CUT SKIN PANEL 5750365 (AT APP ROX 690), FABRICATED REPAIR SPLICE LONG ERON STRAPS INTERNAL AND EXTERNAL DOUBLER WITH FINGER DOUBLER IAW DC8 SRM 53-2-1 AND REO 06044. 2 L 7 4 4F RT 4A25 1999020500745 19990205 00745 WP 1999 2 5 UPS99828608 1 19981229 A 5320 WEB DOUG DC8 DC871F 302199D WP BS 960-980 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, HORIZONTAL FITTING HAS CORROSION EXTENDING UNDER FITTING AND POPPED FASTENER BETWEEN FS 980 AND 960 R BL 48. REPAIRED IAW DH SK701-670. 2 L 7 4 4F RT 4A25 1999020500751 19990205 00751 NM 1999 2 5 QXEA9800133 1 19980110 A 5210 SKIN DHAV DHC8 DHC8102 2809003 NM PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 817PH 56 PDX - MAIN CABIN DOOR EXTERIOR SKIN HAS TWO SMOOTH DENTS BOTH .035 BY 1.5 WITHIN ON INCH OF FASTENERS ON THE TOP BEAM. R EPAIRED IAW EA 9-52-77. 2 H 7 2 4T RT A13NM 1999020500752 19990205 00752 NM 1999 2 5 QXEA9800134 1 19980116 A 5730 PLATE DHAV DHC8 DHC8102 2809003 NM WING DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 817PH 56 PDX - THE ELEVENTH HOLE FROM THE INBOARD SIDE ON THE FORWARD SIDE OF LADDER PLATE FOR 624AT IS ELONGATED APPROXIMATELY . 030. REPAIRED IAW EA 9-57-337. 2 H 7 2 4T RT A13NM 1999020500753 19990205 00753 NM 1999 2 5 QXEA9800135 1 19980109 A 5753 SKIN DHAV DHC8 DHC8102 2809003 NM TE FLAP DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 817PH 56 PDX - UPPER SKIN ON OUTBOARD FLAP HAS A SMALL DENT AND CHAFE AT INBOARD END OF FLAP. REPAIRED IAW EA 9-57-336. 2 H 7 2 4T RT A13NM 1999020500754 19990205 00754 NM 1999 2 5 QXEA9800136 1 19980108 A 3233 FITTING DHAV DHC8 DHC8102 2809003 NM RT MLG ACT CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 817PH 56 PDX - RIGHT MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING MATING SURFACE ON NACELLE FIREWALL AND MAIN LANDING GEAR FRAME STRUCTURAL ASSEMBLY HAS FRETTING CORROSION. REPAIRED IAW EA 9-54-152. 2 H 7 2 4T RT A13NM 1999020500755 19990205 00755 NM 1999 2 5 QXEA9800137 1 19980113 A 3210 H MEMBER DHAV DHC8 DHC8102 2809003 NM NR 1 MLG CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 817PH 56 PDX - NR 1 MAIN LANDING GEAR H-MEMBER CHAFFED FROM CONTACT WITH STANDBY PUMP HYDRAULIC PRESSURE FLEX LINE. REPAIRED IAW EA 9-32-62. 2 H 7 2 4T RT A13NM 1999020600003 19990206 00003 EU 1999 2 6 AALA982227 1 19981220 A 3213 STRUT FOKKER F28 F28MK0100 4990807 EU LT MLG REQ'D SERVICE A AALA K NONE J WARNING INDICATION CL CLIMB 1 SW 07 1473K 11515 DFW - FLT 1196 - EN ROUTE COS-DFW - AFTER TAKEOFF ANTI-SKID LIFTED ALERT OCCURRED AND LANDING GEAR DID NOT RETRACT. AFT ER A FEW MINUTES, ANTI-SKID LIFTED WENT FROM AMBER TO WHITE AND LANDING GEAR RETRACTED. LANDED DFW WITHOUT INCIDENT. R EPACKED LET MAIN LANDING GEAR STRUT AND ACCOMPLISHED GEAR SWING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999021200007 19990212 00007 WP 1999 2 12 9811089884 1 19981230 A 3260 SENSOR DOUG DC9 DC951 3022051 WP NLG FAILED A NWAA O OTHER N FALSE WARNING AP APPROACH 1 GL 01 677MC 47756 DURING APPROACH INTO DTW, THE NOSE LANDING GEAR UNSAFE INDICATOR LIGHT ILLUMINATED WITH LANDING GEAR EXTENSION. THE FLI GHT CREW FOLLOWED COM PROCEDURES, DECLARED AN EMERGENCY, UTILIZED THE EMERGENCY LANDING GEAR HANDLE (NO HELP), AND LANDE D WITHOUT INCIDENT. DURING LANDING, THE MAIN LANDING GEAR DOORS REMAINED FREE AND CONTACTED THE RUNWAY SURFACE. MAINTE NANCE REPLACED THE NOSE LANDING GEAR INDICATION SENSOR, ADDITIONAL HARDWARE AS REQUIRED, AND THE MAIN LANDING GEAR DOOR ASSEMBLIES. OPERATIONAL CHECK NORMAL. 2 L 7 2 4F RT A6WE 1999021200113 19990212 00113 SO 1999 2 12 RAAA99E8031 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 521 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND FS 521 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED AT RBL 42. REPA IRED PER SRM 53-2-4, SHEET 1 AND 2, M-54 NR 477. 2 L 7 4 4T 4A22 1999021200114 19990212 00114 SO 1999 2 12 RAAA99E8032 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 371 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND FS 371 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED AT RBL 34. REPA IRED PER SRM 53-2-4, FIG 2, SHEET 1, M-54 NR 454. 2 L 7 4 4T 4A22 1999021200115 19990212 00115 SO 1999 2 12 RAAA99E8033 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 255 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.113, FOUND FS 255 TRANSVERSE FLOORBEAM UPPER CHORD CORRODED FROM RBL 44 TO 60. REPAIRED PER SRM 53-2-4, FIG 2, SHEET 1, M-54 NR 446. 2 L 7 4 4T 4A22 1999021200116 19990212 00116 SO 1999 2 12 RAAA99E8034 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 764-768 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND LBL 22 SEAT TRACK AND CAP PLATE CORRODED FROM FS 764 TO 768. REPL ACED SEAT TRACK AND CAP PLATE PER SRM 51-2-1, M-54 NR 461. 2 L 7 4 4T 4A22 1999021200117 19990212 00117 SO 1999 2 12 RAAA99E8035 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 720-726 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND LBL 22 SEAT TRACK AND CAP PLATE CORRODED FROM FS 720 TO 726. REPL ACED SEAT TRACK AND CAP PLATE PER SRM 51-2-1, M-54 NR 460. 2 L 7 4 4T 4A22 1999021200118 19990212 00118 SO 1999 2 12 RAAA99E8036 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 314-416 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.113, FOUND RBL 12 SEAT TRACK CORRODED AT FS 314 AND FS 388 TO 416. REPLACED SEAT TRACK PER SRM 51-2-1. M-54 NR 426 AND 460. 2 L 7 4 4T 4A22 1999021200119 19990212 00119 SO 1999 2 12 RAAA99E8037 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 371-388 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND RBL 42 SEAT TRACK CORRODED FROM FS 371 TO 388. REPLACED SEAT TRAC K PER SRM 51-2-1, M-54 NR 432. 2 L 7 4 4T 4A22 1999021200120 19990212 00120 SO 1999 2 12 RAAA99E8038 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 377-416 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND LBL 22 SEAT TRACK CORRODED FROM FS 377 TO 416. REPLACED SEAT TRAC K PER SRM 51-2-1, M-54 NR 430. 2 L 7 4 4T 4A22 1999021200121 19990212 00121 SO 1999 2 12 RAAA99E8039 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 464 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND LBL 12 SEAT TRACK CORRODED AT FS 464. DURING CLEANUP OF NEGLIGIBL E SEAT TRACK CORROSION FOUND FS 464 TRANSVERSE FLOORBEAM CORRODED BEYOND LIMITS. REPAIRED PER SRM 53-2-4, FIG 2, SHEET 1, M-54 NR 483. 2 L 7 4 4T 4A22 1999021200122 19990212 00122 SO 1999 2 12 RAAA99E8040 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 371-416 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.115, FOUND RBL 42 SEAT TRACK CORRODED FROM FS 371 TO 416. REPLACED SEAT TRAC K PER SRM 51-2-1, M-54 NR 425. 2 L 7 4 4T 4A22 1999021200172 19990212 00172 NM 1999 2 12 CA981207028 1 19981120 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 4929 30 PCE120226 (CAN) NR 1 ENGINE OIL COOLER LEAKING. THE COOLER WAS REPLACED. PART TC: 3,264. 2 H 7 2 4T 4 T RT A13NM E20NE 1999021200200 19990212 00200 WP 1999 2 12 CA981214022 1 19981202 A 5280 1504805112 ANGLE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE MLG DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10059 (CAN) NOSE GEAR DOOR PAN ANGLE CRACKED AT OUTBOARD END OF DOOR BETWEEN DOOR ROD FITTING AND AFT HINGE ASSY. CRACK SEVEN INCHES LONG, REPAIRED. 2 L 7 3 4F 4 F A23WE E12EU 1999021200205 19990212 00205 SO 1999 2 12 CA981216006 1 19981207 A 3330 110780108010 LAMP SOCKET EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA CARGO BAY FAILED W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA PCE51708 (CAN) SHORTLY AFTER TAKEOFF, THE CREW REPORTED A SMELL OF BURNING ELECTRICAL INSULATION, WITH A STRONGER SMELL IN CABIN. AIRCRAFT RETURNED TO BASE. INVESTIGATION FOUND THAT THE FLUORESCENT LIGHT SOCKET IN THE CARGO AREA HAD COME APART CAU SING IT TO SHORT OUT. 1 L 7 2 4T 4 T A21SO E4EA 1999021200206 19990212 00206 NE 1999 2 12 CA981216007 2 19981002 A 7321 1220B16E09 MODULE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE NR 2 ENGINE DAMAGED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 30779 (CAN) NR 2 ENGINE DID NOT ATTAIN TAKEOFF THRUST (MAX OBTAINED 1.63 EPR) WITH POWER LEVER FULL FORWARD. AUTO THROTTLE AN D RIGHT EEC DISCONNECTED AUTOMATICALLY. AIRCRAFT RETURNED TO THE GATE AND WAS RELEASED PER MEL 73-21-1. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200207 19990212 00207 NM 1999 2 12 CA981216008 1 19981105 A 3110 4050230002 CONNECTOR BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE COCKPIT DAMAGED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA 31425 (CAN) F/O WAS ABLE TO VISUALLY CONFIRM SMOKE RISING FROM BULKHEAD VIDEO MONITOR, SB G-25 HAD POPPED. MONITOR WIRE BUNDL E CAPPED AND STOWED BY MAINTENANCE. CONDENSATION DRIPPING DOWN WIRE BUNDLE INTO BACK SHELL OF MONITOR CONNECTOR AND MON ITOR. PIN 2 (28VDC) SHOWED SIGNS OF OVERHEAT DAMAGE. STILL UNDER INVESTIGATION. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200208 19990212 00208 NE 1999 2 12 CA981216009 2 19981112 A 7532 10746012 VALVE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE LT ENGINE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 901 30692 (CAN) AS SOON AS EPR WAS SELECTED ON TAKEOFF ROLL AND TAKEOFF THRUST WAS ATTAINED, A LEFT HAND HIGH STAGE EICAS MESSAGE WAS RECEIVED. TAKEOFF WAS ABORTED. QRH ACTION AND AIRCRAFT RETURNED TO THE GATE. ITEM WAS DEFERRED PER MEL AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200209 19990212 00209 NE 1999 2 12 CA981216010 2 19981113 A 7532 32143042 VALVE BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E437 54555 NE LT ENGINE FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 489 30692 (CAN) AS SOON AS EPR WAS SELECTED ON TAKEOFF ROLL AND TAKEOFF THRUST WAS ATTAINED, A LEFT HAND HIGH STAGE EICAS MESSAGE WAS RECEIVED. TAKEOFF WAS ABORTED. QRH ACTION AND AIRCRAFT RETURNED TO THE GATE. ITEM WAS DEFERRED PER MEL AND FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200212 19990212 00212 WP 1999 2 12 CA981216014 1 19981202 A 7600 SM44A24 ROD 1608858107 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE NR 3 ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 10059 (CAN) IN PYLON, ON NR 3 ENGINE, AT ROD END BETWEEN THE THROTTLE TORQUE SHAFT AND THE TENSION REGULATOR LEVER, THE ROD EN D WAS WORN (BEARING DESTROYED) AT REGULATOR LEVER ASSEMBLY. 2 L 7 3 4F 4 F A23WE E12EU 1999021200213 19990212 00213 NM 1999 2 12 CA981216015 1 19981205 A 3340 SWITCHE BOEING 767 767209 NM PWA JT9 JT9D7R4D 52054 NE COCKPIT FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P707529 (CAN) SMOKE IN COCKPIT AFTER RUNWAY TURN OFF LIGHTS SELECTED ON, LIGHTS TURNED OFF AND SMOKE DISSIPATED. BOTH RUNWAY TU RN OFF LIGHT SWITCHES REPLACED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999021200214 19990212 00214 NM 1999 2 12 CA981216017 1 19981207 A 2530 COFFEE MAKER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE GALLEY FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P707556 (CAN) ON BOARDING, BURNING SMELL COMING FROM REAR GALLEY. COFFEE MAKER REMOVED, POWER APPLIED, NO BURNING SMELL. REPLA CED. 2 L 7 2 4F 4 F RT A1NM E3NE 1999021200215 19990212 00215 EU 1999 2 12 CA981216020 1 19981123 A 2780 831A000005 SLAT AIRBUS 320 A320211 3930320 EU WING STIFF W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) ON APPROACH, SLAT FAULT MESSAGE, SLATS JAMMED, RECYCLED, CARRIED OUT PROCEDURE FOR LANDING WITH SLATS JAMMED AT '0 ' POSITION. REPLACED LEFT HAND WING TIP BRAKE. 2 L 7 2 4F RT A28NM 1999021200216 19990212 00216 EU 1999 2 12 CA981216021 1 19981125 A 3250 664700500A4B CONTROL UNIT AIRBUS 320 A320211 3930320 EU NLG STEERING FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA (CAN) AFTER LANDING, NO NOSE WHEEL STEERING. REPLACED LANDING GEAR CONTROL INTERFACE UNIT, SYSTEM SERVICEABLE. 2 L 7 2 4F RT A28NM 1999021200217 19990212 00217 EU 1999 2 12 CA981216022 1 19981124 A 2120 FILTER AIRBUS 320 A320211 3930320 EU AIR DIST FAILED W A B UNSCHED LANDING EMER. DESCENT B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 CA (CAN) SHORTLY AFTER TAKEOFF, IN-FLIGHT SERVICE REPORTED PLASTIC BURNING SMELL AFTER 10 MINUTES, SMELL STILL STRONG. RET URNED. SMELL AND FUMES ENTERED COCKPIT. RECIRCULATION FILTERS CHANGED, HIGH POWER RUN-UP WITH APU SYSTEM USED ON HIGH FLOW AND TEMPERATURE, NO BURNING SMELL. 2 L 7 2 4F RT A28NM 1999021200218 19990212 00218 EA 1999 2 12 CA981216030 2 19981130 A 7414 4373 MAGNETO PARTEN P68 P68C 6780105 EU LYC O360 IO360A1B6 41514 EA ENGINE FAILED W E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 CA 630 94110070 L2370951A (CAN) ENGINE SHUTDOWN, WOULD NOT RESTART. INVESTIGATION FOUND THE LEFT HAND MAGNETO DEAD. 1 H 7 2 3O 3 O A31EU 1E10 1999021200219 19990212 00219 WP 1999 2 12 CA981230004 1 19981208 A 5311 FRAME DOUG DC6 DC6A 3021706 WP HAMSTD 43E 43E60 NE BS 1094 CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 41441 209219 (CAN) FOUND FUSELAGE FRAME FS 1094 CRACKED IN FOUR PLACES. 2 L 7 4 4R 6A3 6 C P871 1999021200220 19990212 00220 EU 1999 2 12 CA981230006 1 19981208 A 6210 355A11002011 BLADE 355A11002011 SNIAS 350 AS350B1 8680811 EU MAIN ROTOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 3449 6002 (CAN) ON PRE-FLIGHT, FOUND CRACK AND SLIGHT VOID IN THE TIP OF THE MAIN ROTOR BLADE. 1 G 7 1 3U H9EU 1999021200224 19990212 00224 WP 1999 2 12 CA981230011 1 19981209 A 2910 ADAPTER DOUG DC4 C54A 3021512 WP PWA R2000 R20007M2 52023 NE HYDRAULIC SYSTEM FAILED W O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA P107846 (CAN) LOSS OF MAIN SYSTEM HYDRAULIC PRESSURE ON APPROACH. GEAR DOWN AND LOCKED. GROUND TEST ADAPTER CAP BROKEN, REPLAC ED WITH STEEL CAP. 2 L 7 4 4R 4 R A762 5E5 1999021200226 19990212 00226 EU 1999 2 12 CA981230020 1 19981218 A 2910 200140646 LINE BRAERO 748 HS7482B 1500248 EU RROYCE DART DART5352 54509 NE HYDRAULIC SYSTEM LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 6087 19466 (CAN) HYDRAULIC FLOW LIGHTS CAME ON IN-FLIGHT, EMERGENCY DECLARED. WHEN U/C LOWERED, THE STANDBY LIGHT WENT OUT, HYDRAU LIC PRESSURE WAS NORMAL. AIRCRAFT LANDED OK. STANDBY HYD PUMP BLEED NIPPLE LEAKING, RESEALED, PUMPS BLED AND FLUID REP LENISHED. ON APPROACH AFTER NEXT FLIGHT, FLOW LIGHTS CAME ON. HYDRAULIC LEAK FROM UNDER PROTECTIVE COVER OF MAXARET RE TURN LINE, LINE REPLACED. PART TC: 9,469. 2 L 7 2 3T 4 T A24EU E297 1999021200231 19990212 00231 EU 1999 2 12 CA981230026 1 19981218 A 2612 D237060 FIRE LOOP BRAERO 748 HS7482A 4231001 EU RT ENGINE CHAFED W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. N FALSE WARNING CR CRUISE 1 CA (CAN) 60 MILES OUT, RIGHT ENG FIRE WARNING BELL AND LIGHT. RIGHT ENGINE SHUT DOWN AND FIRE SUPRESSION SYSTEM ACTIVATED. EMERGENCY CHECK LIST PROCEDURES CARRIED OUT AND CREW PERFORMED UNEVENTFUL LANDING. FIRE DETECTION WIRE CHAFED AGAINST CLAMP. FIRE WIRE, BOTTLES, CARTRIDGES AND FUSES REPLACED. 2 L 7 2 3T A24EU 1999021200233 19990212 00233 CE 1999 2 12 CA981230028 1 19981222 A 2750 55651945 SPROCKET 556517538 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE TE FLAP SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 618 0417971 71711 (CAN) GEARBOX OUTPUT SPROCKET SHEARED WHEN ISOLATED FROM SECOND GEARBOX AND COMMANDED FLAPS TO MOVE. PART TC: 653. 1 L 7 2 4F 4 F A22CE E1NE 1999021200237 19990212 00237 EU 1999 2 12 CA981230032 2 19981202 A 7250 LP TURBNE BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU NR 1 ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 22775 5814 13573 (CAN) CREW COMPLAINED OF LOW DRY TORQUE. GROUND RUN CARRIED OUT AND ALL ENGINE PARAMETERS WERE GOOD WITH THE EXCEPTION OF LOW DRY TORQUE. INSPECTION FOUND THE LP TURBINE AND LP STATOR DAMAGED BEYOND LIMITS. THE ENGINE WAS REPLACED. PAR T TC: 5,803. 2 L 7 2 3T 4 T A24EU A196 1999021200245 19990212 00245 NM 1999 2 12 CA981230051 1 19981211 A 3244 TIRE BOEING 747 747238B 1384828 NM PWA JT9 JT9D7F 52054 NE MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA P685912 (CAN) REPORTED BY TOWER, FOUND RECAP ON RUNWAY AFTER DEPARTURE, AIRCRAFT RETURNED AND FOUND NR 6 TIRE BLOWN, CHANGED TIR E AND AXLE MATE. 2 L 7 4 4F 4 F A20WE E20EA 1999021200246 19990212 00246 EA 1999 2 12 CA981230052 1 19981212 A 5210 DOOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE CABIN OUT OF RIG W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 5963 807389 (CAN) DURING CLIMB AT ABOUT 290 KNOTS AND 8,000 FEET, THE CREW RECEIVED A MASTER CAUTION DOOR HANDLE WARNING AND SUBSEQU ENTLY A MASTER WARNING FOR PASSENGER DOOR, AND AN AURAL WARNING. DOOR FOUND OUT OF RIG. PART TC: 5,388. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200247 19990212 00247 NE 1999 2 12 CA981230053 2 19981104 A 7250 71700171 SPACER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE TURBINE FRACTURED W E ENGINE SHUTDOWN E VIBRATION/BUFFET CL CLIMB 1 CA P657726D (CAN) NR 2 ENGINE HAD HIGH VIBRATION AFTER TAKEOFF. ENGINE WAS SHUT DOWN AT 16,000 FEET. POST-FLIGHT INSPECTION FOUND THE SPACER BETWEEN THE 3-4 STAGE OF THE TURBINE WITH A 4 PIECE MISSING. THE DAMAGE INITIATED FROM A CRACK IN THE TIE RO D BOLT HOLE INNER THICK FLANGE AND PROPOGRATED TO THE OUTSIDE PART OF THE SPACER. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1999021200248 19990212 00248 EA 1999 2 12 CA981230054 1 19981208 A 5210 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR CONTAMINATED W O OTHER N FALSE WARNING DE DESCENT 1 CA 5931 807389 (CAN) AT 19,000 FEET, PASSENGER DOOR LATCH CAUTION MESSAGE CAME ON. CABIN PRESSURE NORMAL, 20 SECONDS LATER, THE PASSEN GER DOOR RED WARNING CAME ON. IN DESCENT, MESSAGE CYCLED UNTIL PRESSURE WAS ZERO. SWITCHES AND BOTH SENSORS ON DOOR HA NDLE WERE CLEANED AND PROXIMITY SWITCH ELECTRONIC UNIT CHECKED OK. PART TC: 5,361. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200249 19990212 00249 NM 1999 2 12 CA981230056 1 19981209 A 5210 LEVER AIRBUS A319 A319114 NM PASSENGER DOOR FROZEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) UNABLE TO DISARM L-2 DOOR SLIDE ON ARRIVAL. ALLOWED DOOR TO WARM AND SLIDE LEVER FREED. 2 L 7 2 4F RT A28NM 1999021200258 19990212 00258 1999 2 12 CA990111017 4 19981216 A 6122 1223890373 GOVERNOR BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3I NE PROPELLER MALFUNCTIONED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 5525 PCE114423 HJ748 (CAN) PROPELLER HUNG UP AT 1,580 RPM (NORMAL 1700). OVERSPEED GOVERNOR MALFUNCTIONED BEFORE PROPELLER ATTAINED OPERATIO NAL RANGE. PART TC: 8,430. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 1999021200259 19990212 00259 NE 1999 2 12 CA990111020 2 19981219 A 7314 PUMP BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E437 54555 NE NR 2 ENGINE FAILED W O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA 30780 (CAN) WHILE PARKED ECAIS MESSAGES: RT GENERATOR; RT DRIVE DISK, AND RT OIL PRESSURE RED WARNING. NR 2 ENGINE WAS SHUT DOWN. TROUBLESHOOTING CARRIED OUT AND HP FUEL PUMP AND FUEL FLOW GAUGE WERE REPLACED. ENGINE CHECKED SERVICEABLE. A S ECOND SPOOL DOWN OCCURRED THREE DAYS LATER AND THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200260 19990212 00260 NM 1999 2 12 CA990111022 1 19981223 A 5270 834503 SENSOR BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E437 54555 NE CARGO DOOR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 30743 (CAN) FORWARD CARGO DOOR INDICATION JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO GATE. MEL ACTION CARRIED OUT. AIRCRAFT R ETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200261 19990212 00261 NE 1999 2 12 CA990111023 2 19981230 A 7314 5252082 VALVE BOEING 757 757200 1384950 NM RROYCE RB211 RB211535E437 54555 NE FUEL SYSTEM FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 30743 (CAN) RIGHT ENGINE CONTINUES TO RUN 45 SECONDS AFTER RT FUEL CONTROL POSITIONED TO CUT OFF. REPLACED B & D VALVE. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200264 19990212 00264 EU 1999 2 12 CA990111036 1 19981219 A 3230 CONTROLLER AIRBUS 320 A320211 3930320 EU MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) LANDING GEAR NOT CLOSED MESSAGE ON ECAM ON TAKEOFF. RECYCLED GEAR AND NOSE LANDING GEAR DOOR NOT CLOSING, AIRCRAF T RETURNED. REPLACED LANDING GEAR CONTROL AND INTERFACE UNIT. 2 L 7 2 4F RT A28NM 1999021200265 19990212 00265 NM 1999 2 12 CA990111047 1 19981221 A 3230 SENSOR AIRBUS A319 A319114 NM MLG BENT W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) LANDING GEAR SHOCK ABSORBER FAULT PROGRAM TO LANDING GEAR CONTROL AND INTERFACE UNIT FAULT. UNABLE TO RETRACT GEA R AFTER TAKEOFF. AIRCRAFT RETURNED TO GATE. NOSE LANDING GEAR EXTENDED SENSORS 24GA AND 25GA REPLACED. NOSE LANDING G EAR DOWNLOCK TARGET EXTENSION LINK BENT, REPLACED. 2 L 7 2 4F RT A28NM 1999021200266 19990212 00266 WP 1999 2 12 CA990111049 1 19981229 A 4920 APU DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE APU BAY FAILED W K NONE O OTHER IN INSP/MAINT 1 CA P657065D (CAN) INTERMITTENT SMOKE DETECTORS ON ONLY WHEN APU PROVIDING AIR CONDITIONING ON GROUND, NOTICEABLE ODORS IN CABIN. OK WITH GROUND COOLING FAN OR ENGINE AIR USED. APU REPLACED. 2 L 7 2 4F 4 F A6WE E2EA 1999021200267 19990212 00267 EU 1999 2 12 CA990111050 1 19981221 A 3232 2271500001 ACTUATOR MESSIER 2271500001 AIRBUS 320 A320211 3930320 EU NLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA (CAN) ON TAKEOFF, UNABLE TO GET NOSE LANDING GEAR TO LOCK UP. AIRCRAFT RETURNED TO GATE. REPLACED NOSE LANDING GEAR DO OR ACTUATOR. 2 L 7 2 4F RT A28NM 1999021200284 19990212 00284 NM 1999 2 12 CA990115018 1 19981228 A 2530 COFFEE MAKER BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE GALLEY FAILED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA P709635 (CAN) AT DEPARTURE TIME, IN-FLIGHT SERVICE REPORTED BURNING SMELL IN AFT GALLEY. ISOLATED TO NR 2 COFFEE MAKER. COFFEE MAKER BLEED CHECK OK. 2 L 7 2 4F 4 F RT A1NM E3NE 1999021200285 19990212 00285 WP 1999 2 12 CA990115019 1 19981231 A 3246 WHEEL DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE NLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA P657387D (CAN) AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT, RECYCLED DOWN, ON NEXT RETRACT NOSE GEAR UNSAFE LIGHT ON WITH OBVIO US VIBRATION, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT, GEAR UNSAFE LIGHT WENT OUT. AIRCRAFT RETURNED TO BLOCKS. REPLACED BOTH NOSE WHEEL ASSEMBLIES, SERVICED NOSE OLEO, GEAR SWING CARRIED OUT, CHECKED SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1999021200286 19990212 00286 EU 1999 2 12 CA990115024 1 19981229 A 2742 ACTUATOR AIRBUS 320 A320211 3930320 EU ELEVATOR JAMMED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) AFTER TAKEOFF, FLIGHT CONTROL STABILIZER JAM, ELEVATOR/AILERON COMPUTER 1 AND 2 PITCH DISPLAYED ON ELECTRONIC CENT RALIZED AIRCRAFT MONITORING. AIRCRAFT RETURNED TO BLOCKS. 2 L 7 2 4F RT A28NM 1999021200288 19990212 00288 EA 1999 2 12 CA990115028 2 19981223 A 8530 LW10925 RING PARTEN P68 P68C 6780105 EU LYC O360 IO360A1B6 41514 EA NR 3 CYLINDER BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 1041 L2370951A (CAN) NR 3 CYLINDER REPLACED DUE TO BROKEN RING. 1 H 7 2 3O 3 O A31EU 1E10 1999021200304 19990212 00304 EU 1999 2 12 VTZA98359 1 19981205 A 2611 CONNECTOR JETAIR JETSTM JETSTM4101 1500501 EU CARGO BAY CONTAMINATED A VTZA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 EA 27 306UE 41020 IAD/RIC - FLT 6234 - DURING TAXI ON 12-5-98 AT 1305 HRS, AIRCRAFT RETURNED TO GATE DUE TO BAGGAGE SMOKE DETECTOR WARNING LIGHT ILLUMINATED. MAINTENANCE INSPECTED AND CLEANED CONNECTOR ON SMOKE DETECTOR. OPS CHECK OK. AIRCRAFT RELEASED AN D APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999021200305 19990212 00305 EU 1999 2 12 VTZA98358 1 19981204 A 3350 613405 BATTERY PACK JETAIR JETSTM JETSTM4101 1500501 EU CABIN DISCHARGED A VTZA K NONE L NO TEST IN INSP/MAINT 1 EA 27 306UE 41020 IAD/MRT - FLT 6388 - DURING TAXI ON 12-4-98 AT 0715 HRS, AIRCRAFT RETURNED TO GATE DUE TO FORWARD EMERGENCY TRACK LIGHTS INOPERABLE. MAINTENANCE INSPECTED AND REMOVED AND REPLACED BATTERY PACK. OPS CHECK OK. AIRCRAFT WAS RELEASED AND AP PROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999021200306 19990212 00306 EU 1999 2 12 VTZA98356 1 19981201 A 2913 PV304426 PUMP BAG JETSTM JETSTM3201 1500217 EU HYDRAULIC SYSTEM FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 496UE 900 IAD/GSO - FLT 6125 - DURING CLIMB AT 0650 HOURS ON 12-1-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT HYDRAULIC PUM P FAILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED HYDRAULI C PUMP. OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999021200307 19990212 00307 EU 1999 2 12 VTZA98353 1 19981126 A 7722 6100116 INDICATOR BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 484UE 899 IAD/SCE - FLT 6475 - DURING TAKEOFF ON 11-26-98 AT 1800 HOURS, AIRCRAFT MADE AN UNSCHEUDLED LANDING DUE TO LT EGT HIGH A T 100 PERCENT TORQUE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED LT ENGINE EGT GAUGE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999021200308 19990212 00308 1999 2 12 VTZA98352 4 19981125 A 3440 A2104F PDU JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 302UE 41013 IAD/CHO - FLT 6558 - DURING CRUISE AT 2225 HOURS ON 11-25-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT ESS BUS F AILURE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT PDU. O PS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FROM RETURN TO SERVICE. (X) 2 L 7 2 4T RT A41NM 1999021200311 19990212 00311 NE 1999 2 12 VTZA98354 2 19981127 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RIGHT CONTAMINATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 332UE 9001 5910 41100 P76038C IAD - FLT 6623 - DURING CRUISE AT 1815 HOURS ON 11-27-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE OIL CONT AMINATION WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REM OVED AND REPLACED RT ENGINE. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T 4 T RT A41NM E18NE 1999021200312 19990212 00312 WP 1999 2 12 99ZZZX565 1 19981220 A 2560 D30145529 SLIDE 1503504103 LKHEED 1011 10113851 5265010 WP PASSENGER DOOR LOOSE A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 826CR 457 193A1141 UPON OPENING THE L3 DOOR, DISCOVERED A PORTION OF THE SLIDE/RAFT ASSY WAS HANGING DOWN AND VISIBLE TO THE FLIGHT ATTENDA NT. THE DOOR WAS THEN RE-CLOSED AND SECURED AND THE SLIDE/RAFT WAS DEFERRED FOR ONE FLIGHT. AFTER FURTHER INVESTIGATIO N, DETERMINED THE IDENTIFICATION FLAP HAD BECOME DETACHED. THE FLAP WAS RE-SECURED AND THE DEFERRAL CLEARED. 2 L 7 3 4F A23WE 1999021200314 19990212 00314 WP 1999 2 12 ORJA9911 1 19981005 A 5321 MD081570003BL6 FLOOR DOUG DC9 DC983 3022083 WP CARGO BAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 OKC - LEVEL 2 CORROSION. AFT PIT CENTER FLOOR PANEL (METAL) JUST AFT OF CARGO DOOR HAS AREAS OF CORROSION. REMOVED COR ROSION. FOUND TO BE OUT OF LIMITS. FABBED NEW PANEL IAW DC9 SRM 51-10-2. TREATED AND PRIMED IAW DC9. SRM 51-10-3. R EF: W.O. NR 9504; 1000-0080. (X) 2 L 7 2 4F RT A6WE 1999021200315 19990212 00315 WP 1999 2 12 ORJA98335 1 19981024 A 5321 MD081570003BL6 FLOOR DOUG DC9 DC983 3022083 WP CABIN CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 836RA 53046 OKC - LEVEL 2 CORROSION NR 5 FLOORBOARD PANEL AFT PIT IS CORRODED. FABBED NEW FLOOR PANEL FOR AFT PIT IAW DC9 SRM 51-10 -2. OK TO TREAT. OK TO PRIME. REF: 10260 N/R 1000-0146. (X) 2 L 7 2 4F RT A6WE 1999021200332 19990212 00332 EU 1999 2 12 RAIA981212 1 19981216 A 3010 4D203703 TIMER JETAIR JETSTM JETSTM4101 1500501 EU DEICE SYSTEM FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 551HK 477 41040 STL - FLT 7502 - AIRFRAME DE-ICE CCT 2 FAULTED. MAINTENANCE REPLACED DE-ICE TIMER. (X) 2 L 7 2 4T RT A41NM 1999021200333 19990212 00333 1999 2 12 RAIA981226 4 19981220 A 3414 39948B2236 INDICATOR BAG JETSTM JETSTM3201 1500217 EU RT AIRSPEED FAILED A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 CE 03 432AM 14003 3371 883 STL - FLT 7050 - FIRST OFFICER'S AIRSPEED INDICATOR STAYED AT ZERO. MAINTENANCE REPLACED FIRST OFFICER'S AIRSPEED INDIC ATOR. (X) 2 L 7 2 4T RT A56EU 1999021200334 19990212 00334 EU 1999 2 12 RAIA981210 1 19981214 A 3230 8662C VALVE BAG JETSTM JETSTM3201 1500217 EU NLG FAILED A RAIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CE 03 342TE 954 EVV - FLT 7425 - NOSE LANDING GEAR INTRANSIT LIGHT ON WITH GEAR UP. MAINTENANCE REPLACED LANDING GEAR SELECTOR VALVE. ( X) 2 L 7 2 4T RT A56EU 1999021200354 19990212 00354 SO 1999 2 12 RAAA99E8041 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 597 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND RBL 42 SEAT TRACK CORRODED AT FS 597. REPLACED SEAT TRACK PER SRM 51-2-1. M-54 NR 473. 2 L 7 4 4T 4A22 1999021200355 19990212 00355 SO 1999 2 12 RAAA99E8042 1 19981215 A 5315 FLOORBEAM LKHEED 188 188C 5262604 SO BS 597 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND FS 597 TRANSVERSE FLOORBEAM CORRODED AT RBL 42. REPAIRED PER SRM 53-2-4 FIG 2 SHEET 1. M-54 NR 473. 2 L 7 4 4T 4A22 1999021200356 19990212 00356 SO 1999 2 12 RAAA99E8043 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 700 BROKEN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND RBL 18 SEAT TRACK LOCKING TABS BROKEN OUT AT FS 700. REPLACED SEA T TRACK PER SRM 51-2-1. M-54 NR 334. 2 L 7 4 4T 4A22 1999021200357 19990212 00357 SO 1999 2 12 RAAA99E8044 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 724 BROKEN A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND RBL 14 SEAT TRACK LOCKING TABS BROKEN OUT AT FS 724. REPLACED SEA T TRACK PER SRM 51-2-1. M-54 NR 338. 2 L 7 4 4T 4A22 1999021200358 19990212 00358 SO 1999 2 12 RAAA99E8045 1 19981215 A 5347 SEAT TRACK LKHEED 188 188C 5262604 SO BS 695-758 CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.117, FOUND RBL 46 SEAT TRACK CORRODED FROM FS 695 TO 758. REPLACED SEAT TRAC K PER SRM 51-2-1. M-54 NR 336. 2 L 7 4 4T 4A22 1999021200359 19990212 00359 SO 1999 2 12 RAAA99E8046 1 19981215 A 5512 SKIN LKHEED 188 188C 5262604 SO HORIZ STZB CORRODED A RAAA K NONE O OTHER IN INSP/MAINT 1 AL 03 178RV 188C2010 DURING SCHEDULED NR 6 CHECK PER CARD 42.03.62, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CORRODED AT HSS 54, 6 INCHES AF T OF FRONT SPAR. REPAIRED PER LAC DWG NR 842459. M-54 NR 314. 2 L 7 4 4T 4A22 1999021200372 19990212 00372 NM 1999 2 12 9811472714 1 19981219 A 3260 MECHANISM BOEING 727 7272S7 138407Z NM NLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 718RC 22344 ON CLIMBOUT, THE NOSE LANDING GEAR DOOR LIGHT FAILED TO EXTINGUISH. CREW CYCLED GEAR WITH NO HELP. FLIGHT DIVERTED TO MCO WITHOUT INCIDENT. MAINTENANCE ADJUSTED NOSE LANDING GEAR DOOR AS REQUIRED. OPERATIONAL CHECK OK. 2 L 7 3 4F A3WE 1999021200373 19990212 00373 NM 1999 2 12 9811482714 1 19981214 A 3260 MECHANISM BOEING 727 7272S7 138407Z NM NLG DOOR OUT OF ADJUST A NWAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 01 718RC 22344 ON CLIMBOUT, CREW WAS UNABLE TO EXTINGUISH THE NOSE LANDING GEAR DOOR LIGHT. CREW PERFORMED GEAR CYCLE AND THE LIGHT RE MAINED ILLUMINATED. THE FLIGHT RETURNED TO DEPARTURE CITY WITHOUT INCIDENT. MAINTENANCE RIGGED DOORS AND PERFORMED GEAR SWING. ALL INDICATIONS CHECKED OK. 2 L 7 3 4F A3WE 1999021200397 19990212 00397 WP 1999 2 12 UPS99828634 1 19980126 A 5315 FLOORBEAM DOUG DC8 DC871F 302199D WP BS 902 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, STA 902 RBL 34 TO 55.5 THE FLOORBEAM HAS CORROSION THAT IS OUT OF LIMITS. REPAIRED FLOORBEAM IAW DHC SK 701-673 REV B. 2 L 7 4 4F RT 4A25 1999021200398 19990212 00398 WP 1999 2 12 UPS99828635 1 19981227 A 5730 SKIN DOUG DC8 DC871F 302199D WP WS 360.25 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 701UP 45938 INSPECTION TYPE-C, RT WING L/E UPPER SKIN AT XFS 360.25 IS CRACKED AT A FASTENER HOLE 2 INCHES FWD OF THE SPAR. REPAIRE D IAW SRM 57-3-2. 2 L 7 4 4F RT 4A25 1999021200423 19990212 00423 EU 1999 2 12 QXEA9900161 1 19981228 A 5350 SUPPORT FOKKER F28 F28MK4000 4990810 EU LT WING/FUS LOOSE A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LEFT-HAND WING ROOT FAIRING SUPPORT FOR 91G LOWER AFT END HAS 15 LOOSE RIVETS AND CHANNEL IS CHAFED. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 51-31-02. 2 L 7 2 4F RT A20EU 1999021200533 19990212 00533 NM 1999 2 12 TSAA9833660 1 19981230 A 3350 6012311 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 RIGHT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT OVERWING EMERGENCY LIGHT ASSY. OPS CHECK O K. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999021200539 19990212 00539 EU 1999 2 12 RAIA981227 1 19981226 A 5610 379628C402 WINDSHIELD BAG JETSTM JETSTM3201 1500217 EU RT COCKPIT FAILED A RAIA B EMER. DESCENT O OTHER CR CRUISE 1 CE 03 423AM 858 CMI - FLT 7433 - FIRST OFFICER'S WINDSHIELD CRACKED. MAINTENANCE REPLACED FIRST OFFICER'S WINDSHIELD. (X) 2 L 7 2 4T RT A56EU 1999021200574 19990212 00574 NE 1999 2 12 VTZA98376 2 19981118 A 7230 6047T63R4 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 629BR 7251 IAD/BNA - FLT 6700 - DURING TAKEOFF ON 11-18-98 AT 0820 HOURS, EXPERIENCED A SMELL OF SMOKE IN THE CABIN ALONG WITH THE ACTIVATION OF THE LAVATORY SMOKE DETECTOR. AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO IAD WHERE IT LANDED WITH NO F URTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT TAXIED TO THE GATE. TROUBLESHOT THE DISCREPANCY AND OPE NED A DMI AGAINST THE LEFT ACM SYSTEM, DMI NR 54655. DMI IS STILL OPEN. AIRCRAFT WAS THEN RELEASED FOR SERVICE. MAINT ENANCE CLOSED DMI 54655 ON 11-21-98 BY REMOVING AND REPLACING LT ENGINE NR 3 CARBON SEAL. OPS CHECK OK. AIRCRAFT WAS R ELEASED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200575 19990212 00575 EU 1999 2 12 VTZA98377 1 19981122 A 2910 137311D1451 LINES BAG JETSTM JETSTM3201 1500217 EU FUSELAGE CHAFED A VTZA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 27 482UE 897 JFK/IAD - FLT 6473 - DURING DESCENT ON 11-22-98 AT 1440 HOURS, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WH ICH WAS LOST ALL HYDRAULIC PRESSURE AND CREW HAD TO PUMP GEAR DOWN. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PR OBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES THAT WERE CHAFED. OPS CHECK OK. AIRCRAFT W AS RELEASED AND APPROVED FOR RETURN TO SERVICE. OPERATOR CONTROL NR 99ZZZX573. (X) 2 L 7 2 4T RT A56EU 1999021200576 19990212 00576 EU 1999 2 12 99ZZZX573 1 19981122 A 2910 137311D1443 LINES BAG JETSTM JETSTM3201 1500217 EU FUSELAGE CHAFED A VTZA O OTHER K J FLUID LOSS WARNING INDICATION DE DESCENT 1 EA 27 482UE 897 JFK/IAD - FLT 6473 - DURING DESCENT ON 11-22-98 AT 1440 HOURS, AIRCRAFT MADE A SCHEDULED LANDING WITH ONE DISCREPANCY WH ICH WAS LOST ALL HYDRAULIC PRESSURE AND CREW HAD TO PUMP GEAR DOWN. AIRCRAFT LANDED AND WENT TO GATE WITH NO FURTHER PR OBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TWO HYDRAULIC LINES THAT WERE CHAFED. OPS CHECK OK. AIRCRAFT W AS RELEASED AND APPROVED FOR RETURN TO SERVICE. OPERATOR CONTROL NR VTZA98377. 2 L 7 2 4T RT A56EU 1999021200577 19990212 00577 NM 1999 2 12 USAA129810J 1 19981217 A 5315 FLOORBEAM BOEING 727 727254 138408L NM BS 1148 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 CABIN FLOOR STRUCTURE BEAM UPPER FLANGE, LOWER SECTION BS 1148, AT RBL 12 EVIDENCE OF CORROSION. INSTALLED REPAIR ON CA BIN FLOORBEAM UPPER FLANGE BS 1148, RBL 12. ACCOMPLISHED IAW 727 SRM 53-10-8, FIG 8. MATERIAL USED 7075T-6, .090 INCH. 2 L 7 3 4F A3WE 1999021200578 19990212 00578 NM 1999 2 12 USAA129810A 1 19981217 A 5510 CHORD BOEING 727 727254 138408L NM LT HORIZ STAB CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 LEFT HORIZONTAL STABILIZER AFT SPAR AT UPPER AND LOWER CHORDS HAS CORROSION AT ATTACH ANGLE TO AFT HINGE FITTING AT STAB ILIZER STA 32 INCH. ACCESS THROUGH LOWER INBOARD ACCESS PANELS 9112, 9121. INSTALLED DOUBLER REPAIR ON LEFT HORIZONTAL STABILIZER LOWER CHORD STA 32. ACCOMPLISHED IAW AVITAS ENGINEERING ORDER NR 98PMSI.240D-1, AND 98PMSI.240D4. MATERIAL USED 7075T-6, .080 INCH. 8110-3 DATED 11-5-98 ISSUED. (X) 2 L 7 3 4F A3WE 1999021200579 19990212 00579 NM 1999 2 12 USAA129810I 1 19981217 A 5330 SKIN BOEING 727 727254 138408L NM BS 950 DAMAGED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 FUSELAGE EXTERIOR - TEMPORARY PLUG REPAIR INSTALLED IN FUSELAGE SKIN BETWEEN BS 950D AND BS 950E, BETWEEN STR 22R AND ST R 23R. INSTALLED FLUSH REPAIR AT FUSELAGE EXTERIOR SKIN BETWEEN BS 950D AND BS 950E, STR 22R AND STR 23R. ACCOMPLISHED IAW B727 SRM 53-30-3, FIG 1. MATERIAL USED 2024T-3, .100 INCH. 2 L 7 3 4F A3WE 1999021200580 19990212 00580 NM 1999 2 12 USAA129810H 1 19981217 A 5330 SKIN BOEING 727 727254 138408L NM BS 1183 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 BULGE ON FUSELAGE EXTERIOR SKIN LEFT HAND SIDE STA 1183, BETWEEN STR 20 AND STR 22 NEXT TO LAVATORY SERVICE PANEL. INST ALLED STRINGER AND EXTERNAL DOUBLER REPAIR AT LEFT HAND BS 1183 FROM STR 20L TO STR 22L. ACCOMPLISHED IAW AVITAS ENGINE ERING ORDER NR 98PMSI.240D-2. MATERIAL USED FROM P.O. 93110588. (X) 2 L 7 3 4F A3WE 1999021200581 19990212 00581 NM 1999 2 12 USAA129810D 1 19981217 A 2820 TUBE BOEING 727 727254 138408L NM RT WING WORN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 RIGHT WING FUEL VENT TUBE SURFACE AND CLAMPS WORN BETWEEN WS 491 - WS 686 INTERIOR. ACCOMPLISHED RIGHT WING FUEL VENT T UBE REPAIRS WS 491.5, 546.5, 574.0, 601.5, 629.0, 656.5, AND 686.5. MATERIAL USED 2024T-3, .040 INCH, 2.5 INCHES BY 3.0 INCHES. ACCOMPLISHED IAW AVITAS ENGINEERING ORDER NR 98PMSI.240RO-3. (X) 2 L 7 3 4F A3WE 1999021200582 19990212 00582 NM 1999 2 12 USAA129810E 1 19981217 A 5347 SEAT TRACK BOEING 727 727254 138408L NM BS 380-480 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 CABIN SEAT TRACK LIGHT CORROSION FROM BS 380 THROUGH BS 760.95 LBL 25.5. REPLACED CABIN SEAT TRACK LBL 25.5 FROM BS 380 TO BS 480. MATERIAL USED BAC 1570-797, 100 INCHES LONG. ACCOMPLISHED IAW SRM 51-30-2 FIG 1. (X) 2 L 7 3 4F A3WE 1999021200583 19990212 00583 NM 1999 2 12 USAA129810F 1 19981217 A 5311 FRAME BOEING 727 727254 138408L NM BS 930 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 LEFT CABIN FRAME STA 930 CRACKED BETWEEN STR 14L - STR 15L BELOW CABIN WINDOW. ACCOMPLISHED LEFT CABIN WINDOW FRAME REP AIR BS 930 BETWEEN STR 14L AND STR 15L. INSTALLED KIT NR 65C25313-1. ACCOMPLISHED IAW SB 727-53-130 AND SB 727-53-162. (X) 2 L 7 3 4F A3WE 1999021200584 19990212 00584 NM 1999 2 12 USAA129810G 1 19981217 A 5311 FRAME BOEING 727 727254 138408L NM BS 930 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 RIGHT CABIN FRAME STA 930 CRACKED BETWEEN STR 14R - STR 15R BELOW CABIN WINDOW. ACCOMPLISHED RIGHT CABIN FRAME REPAIR B S 930 BETWEEN STR 14 - STR 15R. INSTALLED KIT NR 65C25313-2. ACCOMPLISHED IAW SB 727-53-130 AND SB 727-53-162. (X) 2 L 7 3 4F A3WE 1999021200585 19990212 00585 NM 1999 2 12 USAA129810C 1 19981217 A 5330 SKIN BOEING 727 727254 138408L NM BS 848.95 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 FUSELAGE SKIN CRACKED ABOVE THE RBL 70.5 CHORD ANGLE, BS 848.95 WL 196. EMANATING FROM THE FLOOR BEAM ATTACH ANGLE, LOW ER FASTENER. INSTALLED FUSELAGE SKIN REPAIR RIGHT BS 848.95. MATERIAL USED 15-5PH HT 180-200 KSI 12 INCHES BY 31 INCHE S. ACCOMPLISHED IAW BOEING TELEX MIA-98-0005 TR. 8110-3 ISSUED DEC 8, 1998. (X) 2 L 7 3 4F A3WE 1999021200586 19990212 00586 NM 1999 2 12 USAA129810B 1 19981217 A 5320 ANGLE BOEING 727 727254 138408L NM BS 846 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 916TS 20437 VERTICAL FLANGE OF THE RBL 70.5 WING TO CENTER TANK CHORD ANGLE IS CRACKED IN TWO PLACES, LOWER FASTENER. BS 846, WL 19 3, 15 INCHES BELOW CABIN FLOOR. INSTALLED BS 870 PREVENTIVE MOD RT SIDE KIT NR 65-92431-2. ACCOMPLISHED IAW SB 727-53- 116. INSTALLED RT SIDE REPAIR AT STA 848. MATERIAL USED 15-5PH HT 180-200 KSI AND 17-4 PH HT 180-200 KSI. ACCOMPLISH ED IAW BOEING TELEX MIA-98-0005 AND MIA-98-0009RR. 8110-3 ISSUED DEC 8, 1998. (X) 2 L 7 3 4F A3WE 1999021200592 19990212 00592 NM 1999 2 12 USAABB98117 1 19981218 A 2612 FIRE WARNING BOEING 757 757225 1384959 NM LT ENGINE ACTIVATED A USAA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 EA 19 601AU 22193 SFO - FLT 96 - ON CLIMB-OUT FROM SFO, CREW RECEIVED THE FIRE WARNING BELL AND LIGHT FOR THE LEFT ENGINE. FLIGHT RETURNE D TO SFO AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED BITE FOR THE FIRE WARNING SYSTEM AND FOUND NO PR OBLEMS. (M) 2 L 7 2 4F RT A2NM 1999021200593 19990212 00593 EU 1999 2 12 AALA982145 1 19981206 A 3241 CONTROL BOX FOKKER F28 F28MK0100 4990807 EU ANTI-SKID SYSTEM FAILED A AALA O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 SW 07 1423A 11406 ORD - FLT 755 - AFTER LANDING WHILE TAXIING CLEAR OF RUNWAY, BRAKES FAILED WITH TEMPERATURE AND HYDRAULIC PRESSURE NORMA L. AIRCRAFT WS TOWED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE VISUALLY CHECKED BRAKE SYSTEM AND FOUND NO LEAK S OR DISCREPANCIES. HYDRAULIC SYSTEM WAS SERVICED AND THE ANTI-SKID CONTROL BOX CHANGED AS A PRECAUTIONARY. AIRCRAFT W AS TAXIED AT DIFFERENT SPEEDS AND STOPPED, UNABLE TO DUPLICATE FAULT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999021200594 19990212 00594 NM 1999 2 12 HNAA9890671 1 19981101 A 3340 236154 TERMINAL DHAV DHC8 DHC8102 2809003 NM E/E COMPT FAILED A HNAA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 EA 07 906HA 36520 009 PHL - FLT 3455 - ODOR EVIDENT AT AFT CABIN AND FLIGHT DECK. REPLACED BURNED EXTERNAL LIGHTING RING TERMINAL AND CHAFED WIRE TO TERMINAL X1 OF RELAY 3341-K1. (M) 2 H 7 2 4T RT A13NM 1999021200595 19990212 00595 NM 1999 2 12 USAASB98328 1 19981215 A 3260 655825029 LOGIC CARD BOEING 737 737401 1384701 NM LANDING GEAR FAILED A USAA O OTHER N FALSE WARNING CL CLIMB 1 EA 19 421US 23988 IAH - PILOT REPORTED, AFTER INITIAL GEAR RETRACTION, THE LT MAIN GEAR RED LIGHT REMAINED ILLUMINATED. CREW RECYCLED GEA R DOWN, THEN UP, AND LIGHT EXTINGUISHED. IT WAS NOTED THAT THIS LIGHT WAS THE LAST TO EXTINGUISH UPON GEAR RETRACTION. FLIGHT CONTINUED AND LANDED W/O FURTHER INCIDENT. MX INSPECTED LT MAIN GEAR ASSY AND FOUND HOSE GUIDE ASSY ON ACTUATOR ROTATED AFT APPROX 45 DEGREES WITH MOUNTING CLAMP BROKEN. SECURED HOSE WITH TIE WRAPS AND RELEASED PER EA 63259. CLAM P WAS LATER REPLACED WITH A SERVICEABLE CLAMP. MX ALSO GREASED THE GEAR. PHL - ON 12-16-98, PILOT REPORTED THE SAME PR OBLEM. THE LT MAIN GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. CREW RECYCLED GEAR AND LIGHT EXTINGUISHD 2 L 7 2 4F RT A16WE 1999021200596 19990212 00596 NE 1999 2 12 VTZA98308 2 19981009 A 7200 ENGINE JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE33114HR 01514 NE RIGHT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 333UE 41101 P76121 FLT 6504 - IAD-LGA - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT OIL CONTAMINATION WARNING LIGHT ILL UMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED, CLEANED AND REINSTALL ED CHIP DETECTOR. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE ON 10-09-98 DUE TO BAD OIL SAMPLE RESULTS, OPS CHECK OK . AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 4 T RT A41NM E18NE 1999021200597 19990212 00597 GL 1999 2 12 COEA9801850 3 19981215 A 6111 BLADE CESSNA 208 208B 2073701 CE MCAULY 3AF34C 3GFR34C703 GL PROPELLER LIGHTNING STRIKE A COEA K NONE C F.O.D. CL CLIMB 1 NM 13 850FE 208B0164 APPROX 20 DME WEST OF GILA BEND THE PILOT REPORTED TO ABQ ARTCC, THAT HE HAD A LIGHTNING STRIKE AND WOULD ADVISE IF HE E XPERIENCED PROBLEMS. CONTINUED TO YUM WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO YUM TO INSPECT AIRCRAFT. MAINTE NANCE REPORTED THE LIGHTNING HAD STRUCK THE SPINNER, PROPELLER HAD PIN HOLES AND THE LEFT ELEVATOR HAD PIN HOLES. (M) 1 H 7 1 3T A37CE 5 C P60GL 1999021200600 19990212 00600 EU 1999 2 12 99ZZZM86 1 19980510 A 2751 WARNING SYSTEM BAG BAE146 BAE146300A 1500267 EU TE FLAP ACTIVATED A A6WA O OTHER J WARNING INDICATION CL CLIMB 1 GL 31 614AW E3132 CLIMBING OUT OF 20,000 FT, FLAP FAULT ILLUMINATED WITH FLAP GAUGE SHOWING 24 DEGREES AFTER LANDING. FLAPS RETRACTED NOR MALLY, GAUGE INDICATED 0 DEGREES. 2 H 7 4 4F RT A49EU 1999021200601 19990212 00601 EU 1999 2 12 PIVA12627 1 19981208 A 3230 20918002 DRAG BRACE STBROS SD3 SD360 8100606 EU LT MLG FAILED A PIVA O OTHER J WARNING INDICATION LD LANDING 1 WP 13 711PM 29353 SH3715 NO DOWNLOCK LEFT LANDING GEARS INDICATION BEFORE LANDING CREW DECLARE EMERGENCY. LEFT GEAR COLLAPSED UPON LANDING. NO DAMAGE TO THE AIRCRAFT. (M) 2 H 7 2 4T A41EU 1999021200602 19990212 00602 NM 1999 2 12 USAASB98316 1 19981129 A 2410 CSD BOEING 737 737201 1384454 NM NR 2 ENGINE OVERSERVICED A USAA A UNSCHED LANDING H ELECT. POWER LOSS-50 PC CL CLIMB 1 EA 19 254AU 22796 PIT - FLT 2691 - AFTER CLIMB-OUT FROM ROC, CAPTAIN REPORTED THAT THE NR 2 ENGINE CSD DISCONNECTED AND THAT HE WAS UNABLE TO START THE APU DUE TO LOW OIL PRESSURE. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WA S DECLARED. MAINTENANCE FOUND THE NR 2 ENGINE CSD OIL LEVEL OVERSERVICED. DRAINED CSD OIL TO PROPER LEVEL. RAN ENGINE EXTENSIVELY. ALL PARAMETERS NORMAL. AFTER ENGINE RUN, OIL LEVEL WAS CONSTANT. ALSO, APU OIL QUANTITY CHECKED FULL. P ERFORMED SEVERAL APU STARTS. CHECKS GOOD. APU VOLTS AND FREQUENCY CHECKS GOOD. (M) 2 L 7 2 4F A16WE 1999021200603 19990212 00603 WP 1999 2 12 USAAD98213 1 19981211 A 3260 DS077S059 CONNECTOR DOUG DC9 DC931 3022065 WP NLG WW DISCONNECTED A USAA O OTHER N FALSE WARNING AP APPROACH 1 EA 19 963VJ 47508 ATL-CLT - FLT 450 - DURING LANDING GEAR EXTENSION THE NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE. THE LANDING GEAR WAS CY CLED AND THE NOSE GEAR GREEN LIGHT THEN ILLUMINATED. MAINTENANCE FOUND THE CONNECTOR ON THE DOWNLOCK SWITCH LOOSE. THE CONNECTOR WAS RESET AND THE SYSTEM CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1999021200604 19990212 00604 1999 2 12 USAABB98115 4 19981208 A 2565 60B1002624 CABLE BOEING 757 7572B7 1384964 NM ESCAPE SLIDE BROKEN A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 625VJ 27246 BWI - DURING GROUND OPERATIONS, THE L4 DOOR WAS OPENED FROM THE OUTSIDE TO SERVICE THE AIRCRAFT. TEH DOOR HAD NOT BEEN DISARMED. THE SLIDE DEPLOYMENT SEQUENCE WAS INITIATED. MAINTENANCE FOUND THAT THE DOOR DISARM CABLE HAD BROKEN, AND RE PLACED IT. (M) 2 L 7 2 4F RT A2NM 1999021200605 19990212 00605 NM 1999 2 12 USAABB98114 1 19981207 A 2150 VALVE HAMSTD 8021703 BOEING 767 7672B7 1385107 NM RT PACK MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 651US 910138 24764 PHL - FLT 98 - AIRCRAFT DEPARTED WITH THE RIGHT HIGH STAGE BLEED VALVE ON MEL. AFTER TAKEOFF, THE RIGHT PACK ISOLATION VALVE FAILED, DISABLING THE RIGHT AIR CONDITIONING PACK. THE FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT . MAINTENANCE REPLACED A FAULTY TERMINAL EYELET AT POST 2 ON THE STUD PLATE ON THE HPSOV. (M) 2 L 7 2 4F RT A1NM 1999021200606 19990212 00606 NM 1999 2 12 USAASB98309 1 19981122 A 2780 MECHANISM BOEING 737 7372B7 1384560 NM NR 4 LE SLAT OUT OF ADJUST A USAA L ABORTED APPROACH J F WARNING INDICATION FLT CONT AFFECTED AP APPROACH 1 EA 19 282AU 23115 BWI - FLT 2608 - FLIGHT WAS CLEARED FOR APPROACH AT BWI FOR RUNWAY 28. AS CAPTAIN SELECTED FLAPS 1, THE LEADING EDGE TR ANSIT LIGHT AND THE NR 4 SLAT TRANSIT LIGHT ON THE OVERHEAD PANEL ILLUMINATED. CREW RECYCLED THE FLAPS AND DISCONTINUED THE APPROACH. CREW WENT THROUGH PROCEDURES FOR FLAP ASSYMETRY. A ROLL WAS NOTICED AS THE FLAPS WENT THROUGH FLAPS 10. AFTER RESETTING FLAPS, THE PROBLEMS CORRECTED ITSELF AND A NORMAL VISUAL APPROACH AND LANDING WAS MADE AT BWI WITHOUT INCIDENT. AN EMERGENCY WAS DECLARED AND THE CABIN WAS PREPPED FOR AN EMERGENCY. MAINTENANCE ADJUSTED THE NR 4 SLAT DET ENT ARM PER MM 27-81-0A. OPERATIONAL CHECK AND INDICATION NORMAL. (M) 2 L 7 2 4F A16WE 1999021200607 19990212 00607 SW 1999 2 12 99ZZZM87 1 19981029 A 3250 1543011SN1 SWITCH AIRIGHT 27190877 SWRNGN SA227 SA227AC 8780603 SW NLG STEERING LEAKING A X3RA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 17 730C 186 AC697 NOSE WHEEL STEERING (NWS) PRESSURE SWITCH IS LEAKING AT WELDED SEAM. (M) 2 L 7 2 4T RT A8SW 1999021200608 19990212 00608 SW 1999 2 12 99ZZZM88 1 19981026 A 2520 2790565083 SEAT SWRNGN SA227 SA227AC 8780603 SW CABIN BROKEN A X3RA K NONE O OTHER IN INSP/MAINT 1 SW 17 730C AC697 PASSENGER SEAT BACK BROKEN AT AREA IT ATTACHES TO THE SEAT BOTTOM. (M) 2 L 7 2 4T RT A8SW 1999021200609 19990212 00609 NM 1999 2 12 AALA982085 1 19981116 A 2120 AIR DIST BOEING 757 757223 1384957 NM COCKPIT SMOKE A AALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 SW 07 688AA 25730 BOG - FLT 910 - EN ROUTE BOG-MIA - CREW REPORTED SMOKE IN CABIN. AFT LAVATORY GOING OFF. RETURNED BOG AND LANDED WITHO UT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT BUT NO EVIDENCE OF SMOKE FOUND. MAINTENANCE FERRY TO MIA WITH NO SMOKE NOT ED ON FERRY FLIGHT. NO DEFECTS NOTED. ATBS ISSUED TO REINSPECT OVENS, COFFEE MAKERS, LAVATORIES FOR EVIDENCE OF SMOKE OR BEING HOT. AIRCRAFT FLEW FOUR TRIPS WITHOUT ANY SMOKE IN CABIN PROBLEMS. ATBT WAS ACCOMPLISHED WITH NO DISCREPANCI ES NOTED. AIRCRAFT OK FOR SERVICE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999021200610 19990212 00610 WP 1999 2 12 AALA982122 1 19981118 A 5320 FRAME DOUG DC9 DC982 3022082 WP BS 370-427 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14551 53033 TUL - FOUND CORROSION ON DOOR JAMB FORWARD EDGE TO AFT EDGE, LOWER END. REMOVED AND REPLACED LOWER DOOR JAMB PER SRM 53 -05. (M) 2 L 7 2 4F A6WE 1999021200611 19990212 00611 WP 1999 2 12 AALA982143 1 19981203 A 3234 GEAR HANDLE DOUG DC9 DC982 3022082 WP COCKPIT STUCK A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 288AA 49300 DFW - FLT 2347 - AFTER TAKEOFF DFW, GEAR HANDLE WOULD TRAVEL MIDWAY AND STOP. CREW RAN CHECKLIST AND GEAR HANDLE RELEAS E BUTTON WAS PUSHED WITH HANDLE TRAVELING MIDWAY AND STOPPING. AIRCRAFT RETURNED TO DFW AND WITHOUT FURTHER INCIDENT. M AINTENANCE CHECKED LANDING GEAR MECHANISM AND FOUND DEBRIS. DEBRIS WAS REMOVED. ACCOMPLISHED GEAR RETRACTION WITH NO F URTHER DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021200612 19990212 00612 EU 1999 2 12 AALA982148 1 19981203 A 3230 10SD8001 SOLENOID FOKKER F28 F28MK0100 4990807 EU MLG DEFECTIVE A AALA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 1430D 11415 ORD - FLT 1354 - AFTER TAKEOFF, LANDING GEAR FAILED TO RETRACT. AIRCRAFT AIR INTERRUPTED AND RETURNED ORD AND LANDED WI THOUT FURTHER INCIDENT. MAINTENANCE FOUND ANTI-RETRACTION SOLENOID INOPERATIVE. REPLACED ANTI-RETRACTION SOLENOID AND PERFORMED MAINTENANCE TEST WITH NO FURTHER FAULTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999021200613 19990212 00613 EU 1999 2 12 RAIA981122 1 19981125 A 2120 AIR DIST JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT SMOKE A RAIA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 CE 03 564HK 41081 FLT 7324 - STL - SMOKE IN COCKPIT ON TAKEOFF ROLL. MAINTENANCE OPERATED BOTH PACKS FOR PROLONGED TIME, NO SMOKE OR SMEL L NOTICED. (M) 2 L 7 2 4T RT A41NM 1999021200614 19990212 00614 EU 1999 2 12 RAIA981211 1 19981216 A 3010 4D209222 REGULATOR JETAIR JETSTM JETSTM4101 1500501 EU DE-ICE SYSTEM FAILED A RAIA A UNSCHED LANDING O OTHER CR CRUISE 1 CE 03 551HK 10223 41040 FLT 7211 - STL - AIRFRAME DE-ICE CIRCUIT NR 1 FAULTED. MAINTENANCE REPLACED DE-ICE PRESSURE REGULATOR. (M) 2 L 7 2 4T RT A41NM 1999021200615 19990212 00615 EU 1999 2 12 RAIA981219 1 19981218 A 5270 JF5 SWITCH BAG JETSTM JETSTM3201 1500217 EU PAX DOOR MALFUNCTIONED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 429AM 879 FLT 7058 - STL - PASSENGER DOOR LIGHT ILLUMINATED. MAINTENANCE REPLACED ARM ON MICROSWITCH FOR PASSENGER DOOR HANDLE. ( M) 2 L 7 2 4T RT A56EU 1999021200616 19990212 00616 WP 1999 2 12 HALA9800402 1 19981209 A 3350 LIGHT DOUG DC10 DC1010 3022110 WP CABIN MALFUNCTIONED A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 152AA 46707 HNL - FLT 24 - EMERGENCY LIGHTS IN CABIN 'A' AND 'B' A/C LEFT ONLY ARE ON, ON THE GROUND. FLOOR LIGHT MODULE FOR LEFT C ABIN 'A' AND 'B' REPOSITIONED, OPS CHECK OK. (M) 2 L 7 3 4F A22WE 1999021200617 19990212 00617 WP 1999 2 12 HALA9800406 1 19981208 A 3350 LIGHT DOUG DC9 DC951 3022051 WP TAIL CONE INOP A HALA K NONE L NO TEST IN INSP/MAINT 1 WP 13 709HA 47764 HNL - AFT TAIL CONE EMERGENCY LIGHT TEST FAILED. STAIRWAY LIGHTS LEFT AND RIGHT SIDE DOES NOT COME ON. ALSO, LIGHT OVE R EVAC SLIDE DIM. TIGHTENED NUT ON TERMINAL STRIP. CLEANED LENS ON STAIRWAY LIGHT, EVAC SLIDE LIGHT, RELAMPED, GROUND CHECK, OK. (M) 2 L 7 2 4F RT A6WE 1999021200618 19990212 00618 WP 1999 2 12 HALA9800393 1 19981120 A 5242 HANDLE DOUG DC9 DC951 3022051 WP E/E DOOR NOT SECURED A HALA O OTHER E VIBRATION/BUFFET CR CRUISE 1 WP 13 672MC 47661 FLT 195 - HNL - VIBRATION STARTED IN CRUISE AND IS MOST NOTICED IN STEERING TILLER. FOUND E/E COMPARTMENT DOOR HANDLE N OT PROPERLY SECURED. RESECURED E/E, COMPARTMENT DOOR. INSPECTED NOSE GEAR CONDITION AND SECURITY FOUND FLIGHT BRAKES A RE WORN. REPLACED FLIGHT BRAKES. (M) 2 L 7 2 4F RT A6WE 1999021200619 19990212 00619 NM 1999 2 12 MZZA98264 1 19981217 A 2421 976J4981 GENERATOR BOEING 727 727277 138408S NM NR 2 ENGINE MALFUNCTIONED A MZZA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 WP 13 626DH 1682 22644 FLT 879 - MNL - IN FLT HAD THE BTB, GENERATOR FIELD RELAY, AND GENERATOR BREAKER LIGHT ILLUMINATED ON NR 2 ENGINE. CREW FOLLOWED PROCEDURE BUT DID NOT DISCONNECT GENERATOR DRIVE. THE NR 2 BUS WAS BROUGHT BACK ON LINE, RETAINED NR 2 CSD AS STANDBY WHILE MONITORING NR 2 ENGINE GEN DRIVE OIL TEMPERATURE. MAINTENANCE REMOVED AND REPLACED NR 2 GENERATOR PER MM 24-10-11 AND PERFORMED GROUND ENGINE RUNUP AND OPERATIONAL CHECK PER MM 71-00 FOUND OK. CLOSED AND SECURED ENGINE COWL ING AND RELEASED AIRCRAFT FOR SERVICE. (M) 2 L 7 3 4F RT A3WE 1999021200620 19990212 00620 NM 1999 2 12 P2EA982283 1 19981213 A 3260 WARNING SYSTEM BOEING 737 737222 1384473 NM NLG ACTIVATED A P2EA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 CE 05 603DJ 19955 FLT 586 - MDW - ON LANDING ROLLOUT, NOSE GEAR UNSAFE LIGHT AND HORN CAME ON INTERMITTENTLY, INDICATIONS NORMAL ON TAXI I N. CHECKED NOSE GEAR DOWN LOCK SENSOR, ACTUATOR, AND ALL SENSOR WIRES. ALL OPS CHECKED NORMAL PER MM 32-61-51. ALSO, PERFORMED GEAR RETRACT IAW 32-00-01. ALL INDICATIONS NORMAL. (M) 2 L 7 2 4F A16WE 1999021200621 19990212 00621 EU 1999 2 12 RAIA981204 1 19981209 A 3010 14157014404 DEICE SYSTEM JETAIR JETSTM JETSTM4101 1500501 EU RT WING FAILED A RAIA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 CE 03 572HK 41091 FLT 7744 - DCA - AIRFRAME DEICE NR 3 FAULTED. MAINTENANCE REPLACED RIGHT WING MIDDLE LEADING EDGE ASSY. (M) 2 L 7 2 4T RT A41NM 1999021200622 19990212 00622 EU 1999 2 12 RAIA981124 1 19981128 A 2841 7485222 INDICATOR AEROSP ATR42 ATR42300 8680920 EU COCKPIT MALFUNCTIONED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 426TE 14363 228 FLT 7154 - STL - DURING TAXI, FUEL TOTALIZER READ 5200 LBS, AFTER GEAR RETRACTION TOTALIZER READ 4300 LBS. MAINTENANCE REPLACED RIGHT FUEL QUANTITY GAUGE. (M) 2 H 7 2 4T RT A53EU 1999021200623 19990212 00623 EU 1999 2 12 RAIA981203 1 19981207 A 2751 TY176004A TRANSDUCER JETAIR JETSTM JETSTM4101 1500501 EU TE FLAP FAILED A RAIA D RETURN TO BLOCK N FALSE WARNING TX TAXI/GRND HDL 1 CE 03 552HK 7718 41057 FLT 7452 - STL - FLAP ASSYMETRY LIGHT ILLUMINATED. MAINTENANCE REPLACED RIGHT FLAP POSITION TRANSDUCER. (M) 2 L 7 2 4T RT A41NM 1999021200624 19990212 00624 EU 1999 2 12 SIMA983452 1 19981211 A 2750 S5751004900200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200625 19990212 00625 EU 1999 2 12 99ZZZM89 1 19981211 A 2750 S5751004900200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200626 19990212 00626 EU 1999 2 12 99ZZZM90 1 19981211 A 2750 S5751015000200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200627 19990212 00627 EU 1999 2 12 99ZZZM91 1 19981211 A 2750 S5751014900200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200628 19990212 00628 EU 1999 2 12 99ZZZM92 1 19981211 A 2750 S5751012900200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200629 19990212 00629 EU 1999 2 12 99ZZZM93 1 19981211 A 2750 S5751013200200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200630 19990212 00630 EU 1999 2 12 99ZZZM94 1 19981211 A 2750 S5751013000200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200631 19990212 00631 EU 1999 2 12 99ZZZM95 1 19981211 A 2750 S5751013100200 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU LT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURNG MBV-2 INSPECTION, FOUND THE LEFT WING OUTBOARD FLAP INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODE D. THE LEFT WING OUTBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE LEFT WING INBOARD FLAP INBOARD DEFLECTOR INBOARD AND OUTBOARD CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200632 19990212 00632 EU 1999 2 12 SIMA983453 1 19981211 A 2750 S5751014800300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200633 19990212 00633 EU 1999 2 12 99ZZZM96 1 19981211 A 2750 S5751015000300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200634 19990212 00634 EU 1999 2 12 99ZZZM97 1 19981211 A 2750 S5751014900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200635 19990212 00635 EU 1999 2 12 99ZZZM98 1 19981211 A 2750 S5751012900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200636 19990212 00636 EU 1999 2 12 99ZZZM99 1 19981211 A 2750 S5751013200300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200637 19990212 00637 EU 1999 2 12 99ZZZM100 1 19981211 A 2750 S5751013000300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200638 19990212 00638 EU 1999 2 12 99ZZZM101 1 19981211 A 2750 S5751013100300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200639 19990212 00639 EU 1999 2 12 99ZZZM102 1 19981211 A 2750 S5751014900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200640 19990212 00640 EU 1999 2 12 99ZZZM103 1 19981211 A 2750 S5751014900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200641 19990212 00641 EU 1999 2 12 99ZZZM104 1 19981211 A 2750 S5751014900300 CAM GUIDE AEROSP ATR42 ATR42300 8680920 EU RT WING CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING MBV-2 INSPECTION, FOUND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED, THE RIGHT WING INBOARD FLAP OUTBOARD DEFLECTOR NR 1, 2, 3 AND 4 CAM GUIDES CORRODED, AND THE RIGHT WING OUTBOARD FLAP INBOARD DEFLECTOR CAM GUIDES CORRODED. REMOVED AND REPLACED ALL CAM GUIDES. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200642 19990212 00642 EU 1999 2 12 SIMA983455 1 19981211 A 5320 S5367800821602 ZEE AEROSP ATR42 ATR42300 8680920 EU BS 39-41 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 310DK 310 SAW - DURING CPCP1 INSPECTION, FOUND THE RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. REMOVED AND REPLACED T HE ZEE MEMBER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200643 19990212 00643 EU 1999 2 12 SIMA983263 1 19981122 A 6123 4122010003 PUMP AEROSP ATR72 ATR72212 EU NR 1 ENGINE MALFUNCTIONED A SIMA O OTHER O OTHER CL CLIMB 1 SW 21 355AT 1675 225 355 DFW - FLT 3626 - AFTER TAKEOFF, THE NR 1 ENGINE FEATHERING PUMP CIRCUIT BREAKER POPPED. CREW RESET IT AND IT POPPED AGA IN. REMOVED AND REPLACED FEATHERING PUMP. OPERATIONAL CHECK GOOD. (M) 2 H 7 2 4T RT A53EU 1999021200644 19990212 00644 1999 2 12 VTZA98337 4 19981115 A 3160 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU NR 2 FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 326UE 41064 FLT 6356 - IAD-CMH - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO NR 2 SYMBOL GENERATOR FAILED. AIRCRAF T RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SYMBOL. GENERATOR, OPS CHE CK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999021200645 19990212 00645 EU 1999 2 12 VTZA98336 1 19981115 A 3222 14132004423 STRUT JETAIR JETSTM JETSTM4101 1500501 EU NLG REQ'D SERVICE A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 307UE 41021 FLT 6548 - IAD-BDL - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO GEAR WARNING LIGHT IN HANDLE PLUS LOUD NOISE ON EXTENSION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED REPACKED NOSE GEAR STRUT AND PERFORMED GEAR SWING, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999021200646 19990212 00646 EU 1999 2 12 RAIA981201 1 19981204 A 2821 8976921 FILTER BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA E ENGINE SHUTDOWN J WARNING INDICATION DE DESCENT 1 CE 03 343TE 955 FLT 7091 - SPI - RIGHT ENGINE SHUTDOWN ON IT'S OWN. FUEL CROSSFEED SWITCH WAS OPEN AND LEFT BOOST PUMP ON ONLY. MAINTE NANCE PERFORMED EXTENSIVE ENGINE RUNS AND REPLACED RIGHT ENGIEN FUEL FILTER. (M) 2 L 7 2 4T RT A56EU 1999021200647 19990212 00647 SO 1999 2 12 C2XA98C1078 1 19981125 A 3620 M1160140242 SENSOR EMB 120 EMB120RT SO RT ENGINE MALFUNCTIONED A C2XA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 09 17728 120182 CLE - FLT 3073 - CREW REPORTED THEY RECEIVED A DUCT LEAK LIGHT ON THE RIGHT ENGINE AFTER TAKEOFF. THE CREW PERFORMED SU CCESSFUL ENGINE SHUTDOWN AND RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFTS BLEED AIR SYSTEM AND CHANGED ALL 10 LEAK SENSORS ON THE RIGHT SIDE IAW EMB-120 MM 36-20-01. THE O-RINGS WERE ALSO REPLACED FO R PRECAUTIONARY MEASURES. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4T RT A31SO 1999021200648 19990212 00648 1999 2 12 RU3A98007 4 19981214 A 6122 GOVERNOR BEECH 300 300BEECH 1152930 CE LT PROP FAILED A RU3A A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 SW 21 80 FF15 LEFT PROP FAILED TO COME OUT OF FEATHER WHEN TESTE IAW FLIGHT TEST PROCEDURES FOLLOWING MAINTENANCE. EMERGENCY PROCEDUR ES COMPLIED WITH AND AIRCRAFT LANDED SINGLE ENGINE SAFELY. RETURNED FOR SERVICE 12-03-98 FOLLOWING PROPELLER, PROP GOVE RNOR CHANGE AND RIGGING PROCEDURES IAW TI 4128.2. TEAR DOWN REPORT FROM DUNCAN AVIATION ON PROPELLER P/N HCB4MP3B, S/N FWA 2215, WAS INCONCLUSIVE. A TEAR DOWN REPORT ON PROP GOVERNOR P/N 8221-212, S/N 2253651 HAS BEEN REQUESTED. RESULTS WILL BE FORWARD IF REMARKABLE. REFERENCE RU3A98008. (M) 2 L 7 2 4T A24CE 1999021200649 19990212 00649 1999 2 12 RU3A98008 4 19981201 A 6122 GOVERNOR BEECH 300 300BEECH 1152930 CE LT PROP FAILED A RU3A A UNSCHED LANDING J WARNING INDICATION IN INSP/MAINT 1 SW 21 80 FF15 PROP GOVERNOR REPLCED PRIOR TO FLIGHT TO CLEAR PREVIOUS GRIPE. LEFT PROP FAILED TO COMEOUT OF FEATHER WHEN TESTED IAW F LIGHT TEST PROCEDURES. EMERGENCY PROCEDURES COMPLIED WITH AND AIRCRAFT LANDED SINGLE ENGINE SAFELY. RETURNED TO SERVIC E 12-03-98 FOLLOWING PROPELLER, PROP GOVERNOR CHANGE AND RIGGING PROCEDURES IAW TI 4128.2. TEAR DOWN REPORT FROM DUNCAN AVIATION ON PROPELLER P/N HCB4MP3B, S/N FWAS 2215, WAS INCONCLUSIVE. A TEAR DOWN REPORT ON PROP GOVERNOR P/N 8221-212, S/N 2253651 HAS BEEN REQUESTED. RESULTS WILL BE FORWARDED IF REMARKABLE. REFERENCE RU3A98007. 2 L 7 2 4T A24CE 1999021200650 19990212 00650 EU 1999 2 12 RAIA981206 1 19981209 A 2910 1379305A77 LINE BAG JETSTM JETSTM3201 1500217 EU HYDRAULIC SYSTEM FAILED A RAIA B EMER. DESCENT K FLUID LOSS DE DESCENT 1 CE 03 429AM 879 FLT 7035 - COU - WHEN LANDING GEAR WAS SELECTED DOWN, BOTH HYD PRESS GAUGES WENT TO ZERO AND GEAR DIDN'T COME DOWN, HAND PUMPED GEAR DOWN. MAINTENANCE REPLACED HYD LINE TO LEFT HYD PUMP. (M) 2 L 7 2 4T RT A56EU 1999021200651 19990212 00651 EU 1999 2 12 SIMA983443 1 19981210 A 5330 SKIN AEROSP ATR72 ATR72212 EU BS 46/47 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 ABI - DAMAG TO THE LOWER AFT FUSELAGE SKIN AND STRINGERS BETWEEN FRAMES 46 AND 47. REMOVED DAMAGED SKIN AND STRINGERS 1 7 LEFT AND 17 RIGHT AND CUT TO LENGTH NEW STRINGERS EXTRUSION AND FABRICATED CONNECTING SECTION. FABRICATED REPAIR SKIN .032 THICK AND SPLICES .050 THICK, LAP JOINT 11 BY 7.5 INCH AND FILLER PIECE 12.5 BY 7.5 INCH. INSTALLED ALL ITEMS ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200652 19990212 00652 EU 1999 2 12 99ZZZM105 1 19981210 A 5313 STRINGER AEROSP ATR72 ATR72212 EU BS 46/47 DAMAGED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 288AM 288 ABI - DAMAG TO THE LOWER AFT FUSELAGE SKIN AND STRINGERS BETWEEN FRAMES 46 AND 47. REMOVED DAMAGED SKIN AND STRINGERS 1 7 LEFT AND 17 RIGHT AND CUT TO LENGTH NEW STRINGERS EXTRUSION AND FABRICATED CONNECTING SECTION. FABRICATED REPAIR SKIN .032 THICK AND SPLICES .050 THICK, LAP JOINT 11 BY 7.5 INCH AND FILLER PIECE 12.5 BY 7.5 INCH. INSTALLED ALL ITEMS ON AIRCRAFT. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021200653 19990212 00653 EU 1999 2 12 SIMA983331 1 19981129 A 3260 350A53000100 MFC AEROSP ATR72 ATR72212 EU E/E BAY FAILED A SIMA O OTHER N FALSE WARNING AP APPROACH 1 SW 21 322AC 383 320 MIA - FLT 5782 - LEFT MAIN LANDING GEAR UNLOCK LIGHT ON OVERHEAD PANEL IS ILLUMINATED. REMOVED AND REPLACED NR 2 MULTIF UNCTION COMPUTER (MFC). GEAR EXTENSION/RETRACTION CHECKS GOOD. (M) 2 H 7 2 4T RT A53EU 1999021200654 19990212 00654 NM 1999 2 12 AALA984245 1 19981127 A 5311 FRAME BOEING 767 767223 1385123 NM BS 368 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - FOUND CORROSINO ON 'J' CAP BLENDED BEYOND LIMITS AT STATION 368 LBL 36. TRIM FLANGE AS SHOWN IN ATTACHED FIGURE A ND ENSURE ALL CORROSION IS REMOVED. FABRICATED REPAIR ANGLE AND FILLER PER SKETCH. FINISH REPAIR ANGLE AND FILLER PER 767 SRM 53-00-07 FIG 101. INSTALLED REPAIR ANGLE PER SKETCH. (M) 2 L 7 2 4F RT A1NM 1999021200655 19990212 00655 NM 1999 2 12 AALA984244 1 19981130 A 5311 FRAME BOEING 767 767223 1385123 NM BS 456/478 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - J-CAP AT STATION 456 ABOVE STRINGER 332 AND J-CAP AT STATION 478 ABOVE LBL 43 HAVE CORROSION. BLEND CORROSION. P LUG EXISTING NUTPLATE. ALODINE ALL BARE ALUMINUM. PLACED ANGLE IN REPAIR AREA TO ENSURE FIT. INSTALL NUTPLATES, SHIM ALL GAPS, FILL ALL VOIDS. (M) 2 L 7 2 4F RT A1NM 1999021200656 19990212 00656 NM 1999 2 12 AALA984243 1 19981125 A 5330 SKIN BOEING 767 767223 1385123 NM BS 609 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - FOUND CORROSION BLENDED BEYOND SRM LIMITS, PARENT MATERIAL .260, AREA BLENDED 20 TO 1 MIN .219. PARENT MATERIAL . 260, AREA BLENDED 20 TO 1 MINUTE .219. REMOVE CORROSION AND BLEND IAW REFERENCE B ALODINE AND APPLY TWO COATS OF PRIMER . (M) 2 L 7 2 4F RT A1NM 1999021200657 19990212 00657 NM 1999 2 12 AALA984242 1 19981125 A 5230 FRAME BOEING 767 767223 1385123 NM CARGO DOOR CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - FOUND CORROSION OUT OF SRM LIMITS ON TEE-INNER CHORD, ONE AREA BLENDED. SECOND AREA CORROSION CUT OUT. INSTALLED FILLER OF .125 7075T6 ALUM IN CUTOUT. INSTALLED REPAIR STRAP OF .125 7075T6 ALUM INSTALLED WET W/BMS 5.95 USING BACB30 NW6K FASTENERS. BLEND ALL CORROSION. TRIM AREA AS NOTED ON SKETCH, FABRICATE FILLER FROM 7075-T6. FABRICATE REPAIR S TRAP FROM .125 7075T6. ALODINE ALL BARE ALUMINUM, APPLY TWO COATS BM510-11 PRIMER. INSTALL STRAP AND FILLER IAW ATTACH ED USING BACB30NW6K FASTENERS IAW SRM. (M) 2 L 7 2 4F RT A1NM 1999021200658 19990212 00658 NM 1999 2 12 AALA984240 1 19981130 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - FLOORBEAM AT STATION 325 RBL 20 HAD CORROSION. REMOVED ALL CORROSION IAW REF C ALODINE, FINISH WITH 2 COATS OF BM S10-11. (M) 2 L 7 2 4F RT A1NM 1999021200659 19990212 00659 NM 1999 2 12 AALA984238 1 19981128 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 325 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 301AA 22307 AFW - FLOORBEAM AT STAITON 325 RBL 20 HAD CORROSION BLENDED BEYOND LIMITS. REMOVED ALL CORROSION IAW REF C ALODINE, FIN ISH WITH TWO COATS FO BMS10-11, FILL WITH BMS 5-95. (M) 2 L 7 2 4F RT A1NM 1999021200660 19990212 00660 NM 1999 2 12 AALA984237 1 19981128 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 266 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 339AA 22336 AFW - FLOORBEAM AT STATION 266 RBL 26 HAD CORROSION BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301.5 INCH STAINLESS STEEL .050 INCH THICK. ALODINE, FINISH BLEND AND REPAIR PARTS WITH 2 COATS OF BMS10-11 PRIMER, FILL BLENDS W ITH BMS 5-92. INSTALL REPAIR STRAP WET WITH BMS 5-95 SEALANT. (M) 2 L 7 2 4F RT A1NM 1999021200661 19990212 00661 NM 1999 2 12 AALA984236 1 19981129 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM FUSELAGE CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 339AA 22336 AFW - FLOORBEAM AT RBL 54 HAS CORROSION BLENDED BEYOND SRM LIMITS. ROTO PEEN BLENDED AREA PER SRM, ALODINED ALL BARE AL UM SURFACES. FINISH BLENDED WITH 2 COATS OF BMS10-11, PRIMER FILL BLENDS WITH BMS 5-95 PROSEAL 870. (M) 2 L 7 2 4F RT A1NM 1999021200662 19990212 00662 NM 1999 2 12 AALA984234 1 19981130 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 855-999 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 339AA 22336 AFW - FLOORBEAM AT RBL 33 HAD CORROSION BLENDED BEYOND SRM LIMITS. ROTO-PEEN BLENDED AREAS PER SRM. ALODINED ALL BARE ALUM SURFACES FINISH BLENDED AREAS WITH 2 COATS BMS 10-11 PRIMER. FILL BLENDS WITH BMS PROSEAL 870. (M) 2 L 7 2 4F RT A1NM 1999021200663 19990212 00663 NM 1999 2 12 AALA984233 1 19981130 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 1565 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 339AA 22336 AFW - FLOORBEAM AT STATION 1565 LBL 77 HAD CORROSION BLENDED BEYOND SRM LIMITS. FABRICATE REPAIR STRAP OUT OF 301 1/2H STAINLESS STEEL .050 INCH THICK. ALODINE ALL BARE ALUMINUM SURFACE FINISH BLEND AND REPAIR PARTS WITH 2 COATS BMS10-11 PRIMER FILL BLENDS WITH BMS5-92. INSTALL REPAIR STRAP WET WITH BMS5-95. (M) 2 L 7 2 4F RT A1NM 1999021200664 19990212 00664 NM 1999 2 12 AALA984232 1 19981130 A 5315 FLOORBEAM BOEING 767 767223 1385123 NM BS 780-920 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 339AA 22336 AFW - FLOORBEAM AT LBL 11 HAD CORROSION BLENDED BEYOND SRM LIMITS. ROTO-PEEN, BLENDED AREAS PER SRM. ALODINE ALL BARE ALUM SURFACES FINISH BLENDED AREAS WITH 2 COATS OF BMS10-11 PRIMER. FILL BLENDS WITH BMS5-95 PROSEAL 870. (M) 2 L 7 2 4F RT A1NM 1999021200665 19990212 00665 WP 1999 2 12 AALA982121 1 19981118 A 5320 WEB DOUG DC9 DC982 3022082 WP BS 148-153 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 442AA 49468 TUL - CUSP BELOW FORWARD GALLEY DRAIN PAN CORRODED, FORWARD OF FORWARD SERVICE DOOR STATION 148-152. INSTALLED CUSP DOU BLER PER AARD 53-00-00-02 AND REPLACED GALLEY DRAIN PAN. (M) 2 L 7 2 4F A6WE 1999021200666 19990212 00666 WP 1999 2 12 AALA982141 1 19981203 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 288AA 49300 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOORPATH LIGHT STRIP CLOSE TO FORWARD GALLEY INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021200667 19990212 00667 WP 1999 2 12 AALA982146 1 19981206 A 3320 D7731101 BALLAST DOUG DC9 DC982 3022082 WP ROW 11 AB FAILED A AALA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 SW 07 7542A 49996 RDU - FLT 1275 - DURING FLIGHT, ELECTRICAL FUMES WERE NOTED IN FORWARD COACH. MAINTENANCE FOUND A FAULTY LIGHT BALLAST AT SEAT ROW 11AB. REPLACED LIGHT BALLAST OVER SEAT ROW 11AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021200668 19990212 00668 WP 1999 2 12 AALA982147 1 19981206 A 3350 LIGHT DOUG DC9 DC982 3022082 WP CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 205AA 49155 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS INOPERATIVE AT FORWARD GALLEY. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021200669 19990212 00669 NM 1999 2 12 AALA982118 1 19981119 A 3350 CONNECTOR BOEING 767 767323 1385205 NM ROW 19 A/B LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 379AA 25448 MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR LIGHTS AT PASSENGER SEAT ROW 19 A/B INOPERATIVE. RECONNECTED L OOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT ROW 19 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999021200670 19990212 00670 NM 1999 2 12 AALA982128 1 19981125 A 3397 WIRE BOEING 767 767223 1385123 NM ROW 20-30 BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 328AA 22328 ORD - DURING MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROWS 20H THROUGH 30H WOULD NOT ILLUMINATE. REPAIRED EMERGENCY E XIT LIGHT CHAFED WIRE AT SEAT ROW 28H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999021200671 19990212 00671 WP 1999 2 12 AALA982217 1 19981212 A 3397 WIRE DOUG DC9 DC982 3022082 WP CABIN LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 435AA 49453 DFW - DURING OVERNIGHT MAINTENANCE, AFT OVERHEAD EMERGENCY EXIT LIGHT BETWEEN AFT LAVATORIES INOPERATIVE. REPAIRED WIRE TO AFT OVERHEAD EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F A6WE 1999021200672 19990212 00672 NM 1999 2 12 AALA982222 1 19981215 A 3350 LIGHT BOEING 757 757223 1384957 NM ROW 9D INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 691AA 25697 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 9D INOPERATIVE. REPLACED EMERGENC Y EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 9D. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999021200673 19990212 00673 NM 1999 2 12 AALA982216 1 19981214 A 3397 WIRE BOEING 767 767323 1385205 NM ROW 21 HJ BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 360AA 24041 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT ROWS 21HJ INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT SEAT ROW 21HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A1NM 1999021200674 19990212 00674 NM 1999 2 12 AALA980846 1 19981206 A 3350 LIGHT BOEING 757 757223 1384957 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 688AA 25730 DFW - DURING OVERNIGHT MAINTENANCE FIRST CLASS LIGHT SEGMENT AT SEAT 1 AND BROKEN. REPLACED EMERGENCY EXIT LIGHT SEGMEN T. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A2NM 1999021200675 19990212 00675 WP 1999 2 12 ARWA981220 1 19981229 A 2780 57703101 TORQUE TUBE DOUG DC8 DC863F 302198F WP WING BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 ATL - FLT 509 - ON PRE-FLIGHT, FOUND NR 1 SLOT NOT FULLY CLOSED. REMOVED AND REPLACED OUTBOARD SLOT TORQUE TUBE IAW 27- 80-2, OPERATION CHECK GOOD. (M) 2 L 7 4 4F 4A25 1999021200676 19990212 00676 EU 1999 2 12 99ZZZM106 1 19981029 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GCRPH 424 IN DEN, FORWARD LEFT LIGHT BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY. 2 L 7 2 4F RT A28NM 1999021200677 19990212 00677 EU 1999 2 12 99ZZZM107 1 19981003 A 3350 321430 BATTERY AIRBUS 320 A320231 3930325 EU CABIN DISCHARGED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 GCRPH 424 EMERGENCY LIGHT FORWARD GALLEY INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY FORWARD ENTRY. 2 L 7 2 4F RT A28NM 1999021200678 19990212 00678 NM 1999 2 12 99ZZZM108 1 19981013 A 2910 651784059 LINE BOEING 727 72721 1384003 NM NR 1 SLAT CRACKED A RYNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CL CLIMB 1 CE 07 329QS 19038 FLT 615 - IND - AFTER TAKEOFF LOST ALL PRESSURE AND FLUID 'A' SYSTEM, RETURNED IND. REMOVED AND REPLACED HYDRAULIC PRES SURE LINE ON NR 1 SLAT ACTUATOR WITH A FLEX LINE AND PLACED ON SHORT TERM DEFERRAL NR 17573. 2 L 7 3 4F A3WE 1999021200679 19990212 00679 NM 1999 2 12 99ZZZM109 1 19981029 A 2121 5007024620 FAN BOEING 727 72751C 1384015 NM GASPER FAILED A RYNA O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CE 07 413EX 19206 FLT 733 - ORD-IND - GASPER FAN CIRCUIT BREAKER POPPED IN FLIGHT, RESET BUT DETECTED AN ELECTRICAL ODOR AND PULLED CIRCUI T BREAKER. REMOVED AND REPLACED GASPER FAN. (M) 2 L 7 3 4F A3WE 1999021200680 19990212 00680 EU 1999 2 12 SIMA983541 1 19981220 A 3350 F8T5CW BULB SAAB SF340 340B 7860101 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 306AE 340B306 SBP - RIGHT EMERGENCY COVE FLOURESCENT LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED FLOURESCENT LIGHT BULB. (M) 2 L 7 2 4T RT A52EU 1999021200681 19990212 00681 NM 1999 2 12 99ZZZM110 1 19981008 A 3350 BR964411 LIGHT BOEING 727 727227 1384078 NM CABIN INOPERATIVE A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 CGMKF 21119 FLT 431 - MIA - AFT LEFT SEAT EMERGENCY PASSENGER LIGHT OUT. REMOVED AND REPLACED AFT LEFT SEAT EMERGENCY PASSENGER LIG HT. (M) 2 L 7 3 4F A3WE 1999021200682 19990212 00682 NM 1999 2 12 99ZZZM111 1 19981105 A 2612 1014A POWER SUPPLY BOEING 727 72721 1384003 NM APU BAY FAILED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 356QS 19258 FLT 216 - DAY-HSV - HAD AN AIR TURN BACK. FIRE WARNING BELL WENT OFF AT 9,000 FT, NO FIRE WARNING LIGHTS. REMOVED AND REPLACED APU FIRE DETECTION POWER SUPPLY. (M) 2 L 7 3 4F A3WE 1999021200683 19990212 00683 NM 1999 2 12 99ZZZM112 1 19981105 A 2612 356644400 FIRE DETECTOR BOEING 727 72721 1384003 NM APU BAY MALFUNCTIONED A RYNA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 07 356QS 19258 FLT 216 - DAY-HSV - HAD AN AIR TURN BACK. FIRE WARNING BELL WENT OFF AT 20,900 FT, RETURNED TO DAY, BELL WOULD'NT GO OU T WITH THE 2ND TRY, STILL NO LIGHTS ON. REMOVED AND REPLACED APU FIRE DETECTION POWER SUPPLY. 2 L 7 3 4F A3WE 1999021200684 19990212 00684 EU 1999 2 12 SIMA983561 1 19981222 A 3230 A2043C PDU SAAB SF340 340B 7860101 EU RT WING FAILED A SIMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 21 231LN CH25365 340B231 WHEN LANDING GEAR RETRACTED, THREE GREEN AND UNSAFE LIGHTS ALL ILLUMINATED. CYCLED LANDING GEAR, GREEN LIGHTS WENT OUT BUT THE UNSAFE LIGHT REMAINED ON. REMOVED AND REPLACED RIGHT POWER DISTRIBUTION UNIT. PERFORMED GEAR RETRACTION AND EX TENSION CHECKS WITH NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999021200685 19990212 00685 EU 1999 2 12 SIMA983562 1 19981222 A 3260 M610628023 RELAY SAAB SF340 340B 7860101 EU NLG FAILED A SIMA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 SW 21 387AE 340B387 ABI - FLT 3718 - AFTER TAKEOFF FROM MAF, THE NLG DID NOT INDICATE UP AND LOCKED. FOUND CIRCUIT BREAKER F-7 (LANDING GEA R CONTROL) POPPED. RESET AND GEAR INDICATED UP AND LOCKED. CIRCUIT BREAKER F-7 POPPED AGAIN. DIVERTED TO ABI. REMOVE D AND REPLACED RELAY 15GA. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4T RT A52EU 1999021200686 19990212 00686 WP 1999 2 12 USAAD98167 1 19980927 A 5210 SEAL DOUG DC9 DC982 3022082 WP PAX DOOR LEAKING A USAA A UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 825US 49237 PIT-LGA FLT 1498 - DURING CLIMB-OUT, THE AIRCRAFT WOULD NOT PRESSURIZE. THE FLIGHT ATTENDANT REPORTED A LOUD NOISE AROU ND THE L2 DOOR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS UNABLE TO DUPLICATE TH E PROBLEM. THE AIRCRAFT WAS PRESSURIZED AND ALL CHECKS WERE NORMAL. (M) 2 L 7 2 4F A6WE 1999021200687 19990212 00687 NM 1999 2 12 USAABB98108 1 19981019 A 2782 5006397P ACTUATOR BOEING 757 7572B7 1384964 NM SLAT STIFF A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 610AU 27122 LAX - FLT 86 - AFTER TAKEOFF, CREW RECEIVED EICAS MESSAGE 'SLAT DISAGREE' WITH SLATS STUCK HALFWAY UP. FLIGHT DIVERTED T O LAX. MAINTENANCE AT LAX COULD NOT DUPLICATE THE PROBLEM AND REPLACED THE FSEU AS A PRECAUTION. SUBSEQUENTLY, IN PIT O N 10/20/98, EN ROUTE PIT TO BOS (FLT 7), CREW RECEIVED THE SAME INDICATION RETURNED TO PIT. MAINTENANCE REPLACED THE FO LLOWING SLAT ROTARY ACTUATORS, NR 2 OUTBOARD, NR 5 OUTBOARD, AND NR 6 INBOARD AND OUTBOARD. (M) 2 L 7 2 4F RT A2NM 1999021200688 19990212 00688 NM 1999 2 12 TSAA9833633 1 19981215 A 3350 8732030123 CONTROL MODULE BOEING 737 737230 NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 818AL 22117 AFT INTERVALVE EMERGENCY CONTROL MODULE TRIGGERING LIGHT ASSEMBLY. REPLACED AFT CONTROL MODULE, OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F RT A16WE 1999021200689 19990212 00689 NM 1999 2 12 TWRA9856 1 19981117 A 3350 FUSE BOEING 747 747124 1384874 NM CABIN FAILED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 602FF 19734 DURING 'A' SERVICE, FOUND 'E' ZONE ALL LEFT SIDE EMERGENCY EVACS LIGHT INOPERATIVE. REPLACED FUSE IN THE BATTERY PACK. OPERATIONAL CHECK NORMAL PER MM 33-51-00. (M) 2 L 7 4 4F A20WE 1999021200690 19990212 00690 EU 1999 2 12 VTZA98334 1 19981109 A 2731 14127025 TRIM CONTROL JETAIR JETSTM JETSTM4101 1500501 EU ELEVATOR JAMMED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED TO TAKEOFF 1 EA 27 310UE 41028 FLT 6316 - RDU-IAD - DURING TAKEOFF, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO TRIM WHEEL AND CONDITION LEVERS DIFFICU LT TO MOVE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED, LUBED AND FREED JAMMED FRICTION LOCKS. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURNE DTO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999021200691 19990212 00691 EU 1999 2 12 RAIA981112 1 19981112 A 5210 1371382C401 BOLTS BAG JETSTM JETSTM3201 1500217 EU PAX DOOR OUT OF ADJUST A RAIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CE 03 424AM 865 FLT 7414 - STL - PASSENGER DOOR LIGHT CAME ON IN FLIGHT. MAINTENANCE ADJUSTED SHOOT BOLTS. (M) 2 L 7 2 4T RT A56EU 1999021200692 19990212 00692 WP 1999 2 12 USAAD98210 1 19981121 A 3230 RETRACT MECH DOUG DC9 DC982 3022082 WP LT MLG LACK OF LUBE A USAA O OTHER J WARNING INDICATION AP APPROACH 1 EA 19 815US 48095 DFW-PIT - FLT 1220 - DURING GEAR EXTENSION PRIOR TO LANDING, THE CREW RECEIVED A LEFT MAIN GEAR UNSAFE INDICATION. THE GEAR WAS CYCLED WITH THE SAME RESULT. THE EMERGENCY EXTENSION HANDLE WAS PULLED BUT STILL HAD THE UNSAFE LIGHT. THE EM ERGENCY GEAR EXTENSION HANDLE WAS STOWED AND THE GEAR THEN INDICATED SAFE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINT ENANCE FOUND THE GEAR FITTINGS DRY. THE GEAR WAS LUBRICATED, SEVERAL RETRACTION CYCLES PERFORMED, AND A FREE FALL CHECK PERFORMED. (M) 2 L 7 2 4F A6WE 1999021200693 19990212 00693 1999 2 12 RAIA981113 3 19981115 A 6140 JE5 ROLLER ARM BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A RAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CE 03 426AM 874 FLT 7058 - STL - ON ROTATION, BETA HORN SOUNDED CONTINOUSLY. MAINTENANCE REPLACED ROLLER ARM FOR MICROSWITCH IN CENTER PEDESTAL THAT CONTROLS BETA HORN. (M) 2 L 7 2 4T RT A56EU 1999021200694 19990212 00694 NM 1999 2 12 USAASB98296 1 19981109 A 2120 215201 GASPER FAN BOEING 737 737201 1384454 NM CABIN MALFUNCTIONED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 244US 22752 CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVE D AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATIO N. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. C HECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O 2 L 7 2 4F A16WE 1999021200695 19990212 00695 NM 1999 2 12 99ZZZM113 1 19981109 A 2420 941D3352 CIRCUIT BREAKER BOEING 737 737201 1384454 NM COCKPIT MALFUNCTIONED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 244US 22752 CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVE D AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATIO N. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. C HECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O 2 L 7 2 4F A16WE 1999021200696 19990212 00696 NM 1999 2 12 99ZZZM114 1 19981109 A 2420 2299 GCU BOEING 737 737201 1384454 NM NR 2 MALFUNCTIONED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 244US 22752 CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVE D AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATIO N. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. C HECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O 2 L 7 2 4F A16WE 1999021200697 19990212 00697 NM 1999 2 12 99ZZZM115 1 19981109 A 2822 2580005 PUMP BOEING 737 737201 1384454 NM NR 2 MALFUNCTIONED A USAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 EA 19 244US 22752 CLT - FLT 790 - AT FL290, FLT ATTENDANT ADVISED CREW OF A BURNING ELECTRICAL SMELL IN CABIN AROUND LOW 6D. AT THE SAME TIME, THE NR 2 MAIN AFT BOOST PUMP CIRCUIT BREAKER TRIPPED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVE D AND REPLACED THE GASPER FAN AS PRECAUTIONARY DUE TO FAN APPEARED TO BE HOT AND IS LOCATED BELOW ROW 6DEF. OPS CHECKED GOOD. REPLACED APU GENERATOR CONTROL BREAKER DUE TO MAIN CONTACTS SMELLED BURNED AND BREAKER WAS HOT WHILE IN OPERATIO N. OPS CHECKED GOOD. ALSO, REPLACED NR 2 TRU AS PRECAUTIONARY AS DIRECTED BY MAINTENANCE CONTROL. OPS CHECKED GOOD. C HECKED WIRING TO MAIN AFT FUEL BOOST PUMP. NO DEFECTS NOTED. REMOVED AND REPLACED MAIN AFT FUEL BOOST PUMP PER MM. O 2 L 7 2 4F A16WE 1999021200698 19990212 00698 NM 1999 2 12 USAABB98119 1 19981220 A 3350 86210066 BATTERY BOEING 757 7572B7 1384964 NM ROW 33 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 619AU 27198 LAX - FOUND FLOOR EMERGENCY LIGHT AT ROW 33 INOPERATIVE. MAINTENANCE REPLACED BATTERY. (M) 2 L 7 2 4F RT A2NM 1999021200699 19990212 00699 NM 1999 2 12 USAABB98120 1 19981226 A 3350 86210066 BATTERY BOEING 757 757225 1384959 NM ROWS 29/33 DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 609AU 22205 LAX - FOUND EMEREGNCY FLOOR LIGHTS AT ROWS 29 AND 33 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M) 2 L 7 2 4F RT A2NM 1999021200701 19990212 00701 WP 1999 2 12 USAA990002 1 19980108 A 5531 FORMER DOUG DC9 DC981 3022081 WP VERT STAB CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 48035 48035 PIT - DURING C-4 CHECK, FOUND VERTICAL STABILIZER L/E FORMERS CRACKED ON AFT ENDS. SEE EA 49052 FOR DETAILS. REPLACED FORMERS ON VERTICAL STAB PER EA 49052. (M) 2 L 7 2 4F A6WE 1999021200702 19990212 00702 WP 1999 2 12 USAA990003 1 19980108 A 5320 9911840435 BEAM DOUG DC9 DC981 3022081 WP BS 142 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 48035 48035 PIT - DURING C-4 CHECK, FOUND CRACK 2.625 LONG AT BEAM AND ANGLES AT STATION 1429 BELTFRAME AT 2LT (LONGER). REPLACED B ELTFRAME AND WEB PER DRAWING 9911840. (M) 2 L 7 2 4F A6WE 1999021200703 19990212 00703 WP 1999 2 12 USAA990004 1 19980108 A 5320 1192412 CLIP DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 48035 48035 PIT - DURING C-4 CHECK, FOUND 2 INCH CRACK IN SKIN CLIP AT STATION 1437 LONGERON 2 LT. REPLACED DEFECTIVE PART WITH IDE NTICAL PART NR. (M) 2 L 7 2 4F A6WE 1999021200704 19990212 00704 WP 1999 2 12 USAA990005 1 19980108 A 5320 1192413 CLIP DOUG DC9 DC981 3022081 WP BS 1437 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 803US 48035 48035 PIT - DURING C-4 CHECK, FOUND 2 INCH CRACK IN SKIN SLIP AT STATION 1437 LONGERON 2RT. REPLACED DEFECTIVE PART WITH IDEN TICAL PART NUMBER. (M) 2 L 7 2 4F A6WE 1999021200707 19990212 00707 NM 1999 2 12 USAA129807 1 19981218 A 3350 900835A BATTERY BOEING 727 727227 1384078 NM PAX DOOR DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 925TS 10868 21244 FLT 6181 - BOS-LGA - FOUND ON L/S, L-1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY. OPS CHECK OK. (M) 2 L 7 3 4F A3WE 1999021200708 19990212 00708 EU 1999 2 12 USAAF98095 1 19981203 A 3350 A42701425 SWITCH FOKKER F28 F28MK0100 4990807 EU COCKPIT INOPERATIVE A USAA K NONE L NO TEST NR NOT REPORTED 1 EA 19 858US 11291 MCI - THE EMERGENCY LIGHT ARMING SWITCH WOULD NOT SWITCH TO THE DISARM POSITION. THE EMERGENCY LIGHTS WOULD ACTIVATE WH EN NORMAL POWER IS REMOVED. MAINTENANCE REPLACED THE GENERAL SWITCH PANEL NR 2 (EMERGENCY LIGHT, APU START, WINDSHIELD WIPER PANEL). (M) 2 L 7 2 4F RT 1999021200709 19990212 00709 EU 1999 2 12 USAAF98094 1 19981213 A 3350 2LA00534800 LIGHT FOKKER F28 F28MK0100 4990807 EU ROW 15 INOPERATIVE A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 855US 11283 IND - MAINTENANCE FOUND THE CEILING EMERGENCY/STANDBY LIGHT INOPERATIVE AT ROW 15. REPLACED THE LIGHT ASSEMBLY. (M) 2 L 7 2 4F RT 1999021200710 19990212 00710 NM 1999 2 12 USAA129811 1 19981229 A 3350 900835A BATTERY PACK BOEING 727 727225 1384077 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 919TS AV4442 20447 FLT 6010 - LGA-BOS - AFT AIRSTAIR EMERGENCY EXIT LIGHT FLICKERS, THEN WENT OUT. REPLACED BATTERY PACK. (M) 2 L 7 3 4F A3WE 1999021200714 19990212 00714 WP 1999 2 12 USAA980692 1 19981230 A 5330 SKIN DOUG DC9 DC931 3022065 WP BS 1121 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 959VJ 64143 47352 PIT - DURING RON, FOUND SEVERAL .5 INCH CRACKS ON SKIN BETWEEN LONGERON 21R AND 22R BOTH SIDES OF CANT FRAME 1121.225. I NSTALLED DOUBLER (EXTERNAL) PER SRM 53-01 FIG 2. (M) 2 L 7 2 4F A6WE 1999021200717 19990212 00717 NM 1999 2 12 USAASB99007 1 19981231 A 3350 20131ALP BATTERY PACK BOEING 737 737301 1384611 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 336US 23233 IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE RIGHT FORWARD SIDE OF THE FUSELAGE INOPERATIVE. MAINTENANCE REM OVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999021200718 19990212 00718 NM 1999 2 12 USAASB99006 1 19981231 A 3350 20131ALP BATTERY PACK BOEING 737 7373B7 1384580 NM CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 512AU 23595 IAH - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT THE FORWARD SERVICE DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLA CED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M) 2 L 7 2 4F RT A16WE 1999021200719 19990212 00719 WP 1999 2 12 USAAD98221 1 19981223 A 3350 P4010020 BATTERY DOUG DC9 DC931 3022065 WP CABIN DISCHARGED A USAA K NONE L NO TEST IN INSP/MAINT 1 EA 19 965VJ 47374 IND - THE SERVICE DOOR EVACUATION LIGHT WAS DIM. MAINTENANCE REPLACED THE SERVICE DOOR EVACUATION LIGHT BATTERY. (M) 2 L 7 2 4F A6WE 1999021200723 19990212 00723 NM 1999 2 12 USAA980682 1 19981227 A 5330 SKIN BOEING 737 737201 1384454 NM BS 805 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 42662 22796 TPA - DURING CX-4 CHECK VISUAL INSPECTION, FOUND A 1.75 INCH CRACK IN EXTERNAL SKIN STATION 805 STRINGER 18L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 6. (M) 2 L 7 2 4F A16WE 1999021200737 19990212 00737 WP 1999 2 12 EIAA980271 1 19981002 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 446 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 446 AT LONGERON 18L HAS TOOLING DAMAGE NRC W343. REPAIRED PER EA DC9-53-195 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200738 19990212 00738 WP 1999 2 12 EIAA980270 1 19981002 A 5320 BEAM DOUG DC9 DC932F 3022067 WP BS 50 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, RIGHT NOSE GEAR SUPPORT BEAM AT FS 50 HAS CORROSION NRC E045. REPAIRED PER EA DC9-53-188 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200739 19990212 00739 WP 1999 2 12 EIAA980269 1 19981002 A 5330 SKIN DOUG DC9 DC932F 3022067 WP BS 965-980 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE SKIN HAS DENT FROM FS 965-980 AT LONGERON 22R NRC F024, F078, F080. REPAIRED PER EA DC9- 53-183, SRM 53-04 FIG 12B, SRM 53-02 FIG 18 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200740 19990212 00740 WP 1999 2 12 EIAA980266 1 19981002 A 5320 99101513 WEB DOUG DC9 DC932F 3022067 WP BS 727-756 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, MLG FLOOR WEB AT FS 727-756 LBL 5-10 HAS CORROSION NRC W395. REPAIRED PER SRM 53-10, 51-10-3, 51- 30-0 AND EA DC9-53-197 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200741 19990212 00741 WP 1999 2 12 EIAA980281 1 19981002 A 5315 99578701 FLOORBEAM DOUG DC9 DC932F 3022067 WP BS 218 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 218 AND RBL 47. NRC V120. REPAIRED PER EA DC9-53-200 AN D ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200742 19990212 00742 WP 1999 2 12 EIAA980280 1 19981002 A 5315 99115951 FLOORBEAM DOUG DC9 DC932F 3022067 WP BS 200 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 200 AND RBL 44. NRC V118. REPAIRED PER EA DC9-53-199 AN D ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200743 19990212 00743 WP 1999 2 12 EIAA980279 1 19981002 A 5321 FLOORBOARD DOUG DC9 DC932F 3022067 WP BS 180-1037 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, MAIN CABIN FLOORBOARDS FROM FS 180-1037, NUMEROUS SPOTS OF CORROSION, CRACKS AND GOUGES WERE FOUND . NRC W039, W046, W058, W074, W076, W086, W155, W291, W298, W317, W329, W424, V049, W508, W337, W466, W502, W168. MANY REPAIRED FLOOR PANELS WERE COVERED BY SRM CHAPTER 51 GENERAL REPAIRS. ADDITIONALLY EA DC9-53-206 WAS GENERATED FOR SPE CIFIC REPAIRS NOT COVERED BY SRM ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200744 19990212 00744 WP 1999 2 12 EIAA980278 1 19981002 A 5320 3953685501 FITTING DOUG DC9 DC932F 3022067 WP FWD DOOR MISLOCATED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURNG C-CHECK, FORWARD SERVICE DOOR HINGE MOUNT FITTING OBSTRUCTS DOOR RIGGING. NRC V113. REPAIRED PER, EA DC9-5 2-010 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200745 19990212 00745 WP 1999 2 12 EIAA980277 1 19981002 A 5711 SPAR DOUG DC9 DC932F 3022067 WP WS 84 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, FOUND CRACK IN LEFT WING FORWARD SPAR UPPER CHORD AT XIS 84.5. NRC A182. REPAIRED PER, EA DC9-57 -140 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200746 19990212 00746 WP 1999 2 12 EIAA980276 1 19981002 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 303 GOUGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 303, LONGERON 18L HAS GOUGE. NRC W342. REPAIRED PER SRM 53-01, EA DC9-53-20 3 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200747 19990212 00747 WP 1999 2 12 EIAA980275 1 19981002 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 439 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 439, LBL 18 HAS TOOLING MARKS. NRC W344. REPAIRED PER SRM 53-01, EA DC9-53- 202 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200748 19990212 00748 WP 1999 2 12 EIAA980274 1 19981002 A 5330 SKIN DOUG DC9 DC932F 3022067 WP BS 995 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE SKIN CRACKED AT LEFT PYLON FS 995. NRC P157. REPAIRED PER SRM 53-04 FIG 17A. (M) 2 L 7 2 4F A6WE 1999021200749 19990212 00749 WP 1999 2 12 EIAA980315 1 19981008 A 5320 SPLICE DOUG DC9 DC932F 3022067 WP BS 794-813 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LOWER AFT CARGO BAY, LONGERON 30 SPLICE HAS CORROSION FROM FS 794 TO 813. (M) 2 L 7 2 4F A6WE 1999021200750 19990212 00750 WP 1999 2 12 EIAA980314 1 19981008 A 5315 FLOORBEAM DOUG DC9 DC932F 3022067 WP BS 756 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 756 LEFT SIDE AND INTERCOSTAL FS 737-756 LBL 56 HAS CORRO SION. (M) 2 L 7 2 4F A6WE 1999021200751 19990212 00751 WP 1999 2 12 99ZZZM117 1 19981008 A 5320 INTERCOSTAL DOUG DC9 DC932F 3022067 WP BS 737-755 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN FLOORBEAM HAS CORROSION AT FS 756 LEFT SIDE AND INTERCOSTAL FS 737-756 LBL 56 HAS CORRO SION. NRC W129. (M) 2 L 7 2 4F A6WE 1999021200752 19990212 00752 WP 1999 2 12 EIAA980313 1 19981002 A 5542 9957485503 SKIN DOUG DC9 DC932F 3022067 WP RUDDER CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RUDDER LOWER EDGE OF SKIN WAS FOUND CRACKED. NRC N074. REPAIRED PER EA DC9-55-010 AND ECRA 935-5 1-038-1. (M) 2 L 7 2 4F A6WE 1999021200753 19990212 00753 WP 1999 2 12 EIAA980312 1 19981002 A 5542 591025631 SKIN DOUG DC9 DC932F 3022067 WP RUDDER CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RUDDER LEADING EDGE SKIN WAS FOUND CRACKED AT ZR 95.2. NRC N074. REPAIRED PER EA DC9-55-009 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021200754 19990212 00754 WP 1999 2 12 EIAA980311 1 19981002 A 5542 SKIN DOUG DC9 DC932F 3022067 WP RUDDER DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RUDDER SKIN AT TRAILING EDGE WAS FOUND DAMAGED. NRC N102. REPAIRED PER SRM 55-40-1. (M) 2 L 7 2 4F A6WE 1999021200756 19990212 00756 NM 1999 2 12 99ZZZM118 1 19980105 A 3250 65348783 PIN BOEING 727 727214 138407R NM NLG STEERING MISSING A C8GA O OTHER W INADEQUATE Q C TX TAXI/GRND HDL 1 SO 15 227JL 44088 20875 FLT PT 315 - KJSJ-KPHL - AFTER LANDING AND DURING DEPARTURE FROM RUNWAY ONTO TAXIWAY, AIRCRAFT LOST NOSE WHEEL STEEING A ND HAD SEVERE NOSE WHEEL VIBRATION. CONTACTED MAINTENANCE TO TOW AIRCRAFT FROM TAXIWAY. FOUND THE NOSE GEAR TORSION LI NK SAFETY PIN MISSING. LOCATED PIN ON TAXIWAY. PERFORMED VISUAL INSPECTION OF NOSE GEAR AREA AND SAFETY PIN. NO DEFEC TS NOTED. REINSTALLED PIN. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 3 4F A3WE 1999021200757 19990212 00757 NM 1999 2 12 99ZZZM119 1 19981231 A 2750 RETRACT MECH BOEING 727 727227 1384078 NM RT TE FLAP JAMMED A C8GA A J UNSCHED LANDING DUMP FUEL J WARNING INDICATION CL CLIMB 1 SO 15 308AS 22002 FLT 504 - DDAY-KSAN - AFTER TAKEOFF, OUTBOARD FLAP WOULD NOT RETRACT BEYOND 5 DEGREES. SEVERAL ATTEMPTS TO RETRACT TO 0 DEGREES FAILED. AIRCRAFT RETURNED TO KDAY AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AND PERFORMED OPERATIONAL CH ECK OF FLAP SYSTEM. NO DEFECTS NOTED. ICING CONDITIONS PREVALENT AT KDAY. SUSPECT ICE BUILD-UP IN RIGHT TRAILING EDGE AREA. PERFORMED FOLLOW-UP INSPECTION. NO DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 1999021200760 19990212 00760 WP 1999 2 12 99ZZZM121 1 19981223 A 2150 7339296 VALVE LKHEED 1011 10113851 5265010 WP NR 1 PACK FAILED A AMTA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 GL 11 191AT E22414 193C1084 DURING CRUISE A VERY STRONG ACRID ODOR WAS NOTED, ACCOMPANIED BY A BURNING SENSATION IN NOSE AND THROAT. ODOR SEEMED ST RONGEST AT CAPTAINS SIDE. UNSCHEDULED LANDING. FOUND NR 1 PACK TURBINE BYPASS VALVE STUCK IN THE OPEN POS. REMVOED AN D REPLACED BYPASS, RAN ENGINES AND CHECKED OK. (M) 2 L 7 3 4F A23WE 1999021200769 19990212 00769 EU 1999 2 12 99ZZZM123 1 19981228 A 3230 CONNECTOR BAG JETSTM JETSTM3201 1500217 EU MLG CONTAMINATED A FYWA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 05 242BM 902 AIRCRAFT LEFT JUNEAU LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO JUNEAU AND LANDED WITHOUT PROBLEM. FERRIED T O KETCHIKAN GEAR DOWN. TROUBLESHOOTING REVEALED CORRODED PINS ON CANNON PLUG. CLEANED CANNON PLUG. PERFORMED GEAR SWI NG OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1999021200771 19990212 00771 EU 1999 2 12 99ZZZM125 1 19981230 A 5610 1379628C401 WINDSHIELD BAG JETSTM JETSTM3201 1500217 EU COCKPIT CRACKED A FYWA O OTHER O OTHER NR NOT REPORTED 1 AL 05 242BM A140058 902 AIRCRAFT WAS ON APPROACH TO KETCHIKAN WHEN CAPTAINS WINDSHIELD OUTER PANE CRACKED. AIRCRAFT LANDED WITHOUT INCIDENT. 1 -2-99, REMOVED AND REPLACED CAPTAINS WINDSHIELD. OPS CHECK GOOD. (M) 2 L 7 2 4T RT A56EU 1999021200772 19990212 00772 EU 1999 2 12 99ZZZM126 1 19981211 A 2424 51539002A GCU LEAR BAG JETSTM JETSTM3201 1500217 EU INTERNAL INOPERATIVE A FYWA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 AL 05 242BM 5619 902 AIRCRAFT EXPERIENCED ST ELMOS FIRE IN CRUISE, AT THAT TIME THE LEFT GENERATOR LIGHT FLICKERED AND THEN THE LEFT GENERATO R DROPPED OFF LINE ADN THE GENERATOR FIELD CIRCUIT BREAKER POPPED AND WOULD NOT RESET. AIRCRAFT RETURNED TO KETCHIKAN A ND LANDED WITH NO PROBLEMS. AIRCRAFT IS NOW IN HANGAR AND TROUBLESHOOTING IS IN PROGRESS. GENERATOR CONTACTOR AND STAR TER CONTRACTOR SWAPPED SIDE TO SIDE GEN CONTROL UNIT. REMOVED AND REPLACED. GND RUN AIRCRAFT ALL SYSTEMS NORMAL. ALL WIRING WAS ALSO CHECKED. (M) 2 L 7 2 4T RT A56EU 1999021200773 19990212 00773 EU 1999 2 12 99ZZZM127 1 19981230 A 3320 POWER SUPPLY BAG JETSTM JETSTM3201 1500217 EU ROW 2-3 INOPERATIVE A FYWA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 AL 05 242RH 903 AIRCRAFT HAD DEPARTED ANCHORAGE EN ROUTE TO ANTIAC WHEN SMOKE WAS DETECTED IN THE CABIN. THE AIRCRAFT RETURNED TO ANCHO RAGE AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED A CHAFED WIRE ON A CABIN OVERHEAD LIGHTING POWER SUPPLY. THE POW ER SUPPLY WAS ISOLATED AND CABIN OVERHEAD LIGHTING AT SEATS 2, 3,B AND C DEFERRED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999021200780 19990212 00780 1999 2 12 ASAA9880256 4 19981207 A 2565 D29985107 SLIDE AIRCRUISERS DOUG DC9 DC983 3022083 WP PAX DOOR MALFUNCTIONED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 977AS 0709 53453 OAK - DURING C-CHECK, THE L2 DOOR EMERGENCY EVACUATION SLIDE FAILED THE EMERGENCY LIGHT AMP TEST. REPLACED THE L2 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1999021200781 19990212 00781 NM 1999 2 12 ASAA9840115 1 19981221 A 5210 MECHANISM BOEING 737 7374Q8 NM L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 776AS 25109 LAX - PRIOR TO FLT 477 - THE L1 DOOR WOULD NOT CLOSE PROPERLY. CLEANED AND LUBRICATED ROLLER GUIDES AND LOCK ROLLERS, D OOR CLOSED AND LOCKED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999021200782 19990212 00782 NM 1999 2 12 ASAA9840120 1 19981230 A 5210 CLIP BOEING 737 7374Q8 NM PAX DOOR MISSING A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 775AS 25108 SNA - UPON ARRIVAL OF FLT 486, THE L1 DOOR COULD NOT BE OPENED. CONTRACT MAINTENANCE REPLACED MISSING C-CLIP ON THE UPP ER ARM ASSEMBLY AND THE DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999021200819 19990212 00819 WP 1999 2 12 UPS99828662 1 19981231 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 160 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, STA 160R SIDE FRAME BOTTOM IS CRACKED. REPLACED DAMAGED SECTION OF FRAME. 2 L 7 4 4F RT 4A25 1999021200897 19990212 00897 SW 1999 2 12 CA980707047 1 19980610 A 3213 2751544001 TORQUE LINK OZONE OAS54535 SWRNGN SA227 SA227* SW MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LPI REVEALED TWO CRACKS LOCATED AT UPPER TORQUE LINK KNUCKLE. CRACKS AT UPPER FILET RADII. REF: SB CC7-32-009. 2 L 7 2 4T RT A5SW 1999021200899 19990212 00899 EA 1999 2 12 CA980720023 1 19980705 A 2750 CIRCUIT BREAKER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE COCKPIT TRIPPED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 8269 807317 (CAN) ON APPROACH, FLAPS FAIL CAUTION ON WITH FLAPS SELECTED AT ZERO. OVERSPEED CLACKER ON TILL SPEED REDUCED BELOW 230 . FLAP FAIL MESSAAGE STAYED ON. ISOLATION GUIDE CIRCUIT BREAKER RESET CARRIED OUT. FLAP FAIL MESSAGE CLEARED. FECU C HECKED OK.. PART TC: 7,407. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200900 19990212 00900 1999 2 12 CA980721019 4 19980717 A 2297 WIRE CNDAIR CL604 CL604 EA YAW DAMPER CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) YAW DAMPER NR 2 FAILED. STABILIZER AUGMENTATION COMPUTER REPLACED. ONE HOUR INTO FLIGHT, NR 2 YAW DAMPER FAILED AGAIN. LOW RESISTANCE READINGS ON 26 VAC AND LVDT EXC YDZ OUTPUT FROM STABILIZER COMPUTER WAS TRACED TO A SHORTED WIRE IN THE LEFT WING LEADING EDGE, CAUSING A BURN UP OF 115/26 VAC TRANSFORMER IN COMPUTER. WIRE NR CH141A22WHT IS REFERENC E. WIRE BUNDLES ALONG LEADING EDGE ARE ROUTED IN VERY TIGHT SPACE, THEREFORE, SCREWS USED FOR MOUNTING BLEED AIR LEAK T EMP SENSORS MUST BE COATED WITH PRC TO PREVENT CHAFING. IN THIS CASE SCREWS NOT PRC'D. CANADAIR INFORMED. 2 L 7 2 4F RT A21EA 1999021200901 19990212 00901 EA 1999 2 12 CA980814009 1 19980807 A 2913 600751135 PUMP CNDAIR CL600 CL6002B19 EA HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS NR NOT REPORTED 1 CA MX400596 (CAN) HYDRAULIC PUMP FOUND LEAKING FROM THE AFT FLANGE. 2 L 7 2 4F RT A21EA 1999021200903 19990212 00903 EA 1999 2 12 CA980814017 1 19980717 A 2750 SHAFT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP SHEARED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 7443 807380 (CAN) ON APPROACH AFTER SELECTING FLAPS 45 DEGREES, A FLAP FAIL AMBER CAUTION MESSAGE AND FLAPS STOPPED AT 39 DEGREES. Q UICK REF. PROCEDURE CARRIED OUT. RIGHT HAND OUTBOARD FLAP CENTER SHAFT HAD SHEARED.. PART TC: 6,520. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200904 19990212 00904 EA 1999 2 12 CA980827018 1 19980815 A 2750 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE WING TE FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 807157 (CAN) DURING FLAP EXTENSION BETWEEN 35 TO 45 DEGREES, FLAPS STOPPED AT 33 DEGREES AND A FLAP FAIL MESSAGE CAME ON EICAS. SYSTEM RESET. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200905 19990212 00905 EA 1999 2 12 CA980827021 1 19980812 A 5220 SEAL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE OVERWING EXIT DIRTY W O OTHER J WARNING INDICATION CR CRUISE 1 CA 5369 807385 (CAN) IN CRUISE, RIGHT EMERGENCY DOOR MESSAGE ON EICAS. QUICK REF. CARRIED OUT. RIGHT OVERWING EXIT DOOR REMOVED AND D OOR SEAL AND SURFACE MATES CLEANED.. PART TC: 4,768. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200906 19990212 00906 EA 1999 2 12 CA980827026 1 19980805 A 2910 LINE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE HYDRAULIC SYS FAILED W O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 6399 808307 (CAN) NR 3 HYDRAULIC PRESSURE SYSTEM INDICATING LOW FOLLOWED BY LANDING GEAR DISAGREE. HYDRAULIC PRESSURE AT ZERO. NEC ESSARY TO DO ALTERNATE GEAR EXTENSION. LANDING NORMAL. HYDRAULIC PUMP 3A AND 3B PRESSURE LINE LEAKING.. PART TC: 5,6 83. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200907 19990212 00907 EA 1999 2 12 CA980909015 1 19980803 A 2750 860D18ABC FECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAP FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 5378 807365 (CAN) ON FLAP SELECTION FROM 8 DEGREES TO ZERO, FLAP FAIL MESSAGE ON EICAS. QUICK REF. CARRIED OUT. LEFT HAND FLAP ELE CTRONIC CONTROL UNIT FAILED. LEFT HAND BPSU WIRING CHANGED AND FECU ADJUSTED.. PART TC: 4,726. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200908 19990212 00908 EA 1999 2 12 CA980909017 1 19980818 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LEFT HAND FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 3937 (CAN) FLAPS FAILED AT 33 DEGRESS WHEN SELECTED TO 45 DEGREES. REPLACED LEFT HAND BRAKE AND POSITION UNIT.. PART TC: 3 ,567. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200909 19990212 00909 EA 1999 2 12 CA980909018 1 19980818 A 5210 LATCH SPRING CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR CONTAMINATED W O OTHER J WARNING INDICATION CL CLIMB 1 CA 5338 807389 (CAN) PASSENGER DOOR MESSAGE IN CLIMB, NO DELTA PRESSURE IN CABIN. OUT HANDLE STOW KNOB MESSAGE CHANGED TO PASSENGER DO OR STOW THEN BACK TO HANDLE OUT. LATCH SPRINGS AND PIN CLEANED.. PART TC: 4,823. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200914 19990212 00914 EA 1999 2 12 CA981001008 1 19980914 A 3260 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG OUT OF ADJUST W K NONE J WARNING INDICATION TO TAKEOFF 1 CA 6590 808307 (CAN) NOSE GEAR DID NOT RETRACT ON UP SELECTION. GEAR DISAGREE WARNING, WITH NOSE WHEEL STEERING CAUTION LIGHT. OLEO E XTEND PROXIMITY SENSOR TARGET ADJUSTED. . PART TC: 5,865. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200915 19990212 00915 EA 1999 2 12 CA981001009 1 19980915 A 3230 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 6591 808307 (CAN) GEAR DISAGREE RED NOSE GEAR ICON ON TAKEOFF. AIRCRAFT RETURNED. NOSE GEAR AND DOOR SELECTOR VALVE AND PROXIMITY SENSOR ELEC UNIT REPLACED. . PART TC: 5,867. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200916 19990212 00916 EA 1999 2 12 CA981001012 1 19980916 A 3234 7179015 SELECTOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 6411 807339 (CAN) UNABLE TO RAISE GEAR DURING CLIMB. AIRCRAFT RETURNED. LANDING GEAR HANDLE CONTROL ASSEMBLY REPLACED.. PART TC: 5,705. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200919 19990212 00919 EA 1999 2 12 CA981019007 1 19981007 A 5740 600100551 BUSHING 60010103804 CNDAIR CL604 CL604 EA WING DAMAGED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 7502 (CAN) COUNTERSUNK WASHER FOUND INSTALLED UPSIDE DOWN ON BOLT P/N NAS6712D52 IN OTHER WORDS, THE COUNTERSINK IS FACING AW AY FROM HEAD OF BOLT. COUNTERSINK BEARING AGAINST THE BUSHING DAMAGING IT. 2 L 7 2 4F RT A21EA 1999021200920 19990212 00920 EA 1999 2 12 CA981019016 1 19980930 A 2150 ACM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT MALFUNCTIONED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 7206 807281 (CAN) CREW REPORTED WHITE SMOKE COMING OUT OF LEFT SIDE OF AFT ACCESSORY COMPARTMENT. LEFT AIR CYCLE MACHINE USING OIL. REPLACED.. PART TC: 6,154. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200921 19990212 00921 EA 1999 2 12 CA981019019 1 19981004 A 2750 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LEFT FLAP MALFUNCTIONED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 5385 807399 (CAN) FLAPS FAIL ON EICAS ON INITIAL SELECTION. FLAPLESS LANDING CARRIED OUT. LEFT HAND BRAKE AND POSITION SENSOR UNI T FAILED.. PART TC: 4,991. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200922 19990212 00922 EA 1999 2 12 CA981019020 1 19981002 A 2750 FECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 5608 807385 (CAN) AFTER SELECTING FLAPS 8, A FLAP FAIL MESSAGE APPEARED AND FLAPS REMAINED AT ZERO. FLAPLESS LANDING CARRIED OUT. F LAP ELECTRONIC CONTROL UNIT RESET.. PART TC: 4,991. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200923 19990212 00923 EA 1999 2 12 CA981019021 1 19981002 A 2750 FECU CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE TE FLAPS MALFUNCTIONED W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 9012 807157 (CAN) ON FLIGHT CONTROL CHECK, FLAPS SELECTED AT 8 DEGREES, LEFT FLAP SHOWS 8 AND RIGHT SHOWS 11. AT PHYSICAL INSPECTIO N THE RIGHT FLAP 1 DEGREE LOWER THAN LEFT SIDE. AT FLAP 20, LEFT SHOWS 20 AND RIGHT 22.AT FLAP 0 LEFT FLAP 0 AND RIGHT 3 DEGREES. FLAP ELECTRONIC CONTROL UNIT REPLACED. POTENTIOMETER ADJUSTED.. PART TC: 7,824. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200925 19990212 00925 EA 1999 2 12 CA981030014 1 19981010 A 3310 LIGHTING PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 6243 807343 (CAN) IN TAXI, THE FIRST OFFICER'S LIGHTING PANEL SHORTED AND THERE WAS AN ELECTRICAL SMELL IN THE COCKPIT. WATER FOUND LEAKING THROUGH THE BOTTOM BOLTS ON THE RIGHT SIDE WINDOW. WATER FOUND BEHIND THE CIRCUIT BREAKER PANEL.. PART TC: 5 ,683. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200926 19990212 00926 EA 1999 2 12 CA981030017 1 19981007 A 2750 POWER DRIVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 8575 807242 (CAN) FLAPS FAIL MESSAGE WHEN SELECTING FLAPS 30 ON APPROACH. FLAPS LEFT AT 30 AFTER LANDING. POWER DRIVE UNIT CHANGED AND LEFT AND RIGHT FLEXSHAFT FRICTION TEST CHECK OK. LEFT AND RIGHT BPSU'S ADJUSTED. FECU POTENTIOMETERS ADJUSTED. A D CF-98-14 COMPLIED WITH.. PART TC: 7,431. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200930 19990212 00930 EA 1999 2 12 CA981113016 1 19981102 A 2750 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 6633 807335 (CAN) FLAP FAIL MESSAGE ON SELECTION OF 30 TO 45 DEGREES AT 150 KNOTS SPEED. REPLACED RIGHT HAND BRAKE SENSING UNIT AND POTS 5 AND 8 ADJUSTED.. PART TC: 5,708. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200931 19990212 00931 EA 1999 2 12 CA981113017 1 19981101 A 3230 750006000 SELECTOR VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG FAILED W O OTHER J WARNING INDICATION LD LANDING 1 CA 9281 807428 (CAN) NOSE LANDING GEAR WOULD NOT EXTEND, GEAR DISAGREE MESSAGE ON EICAS. QUICK REF CARRIED OUT ALTERNATE GEAR SELECTIO N MADE. NOSE GEAR SELECTOR AND PRIORITY VALVE P/N 4622 REPLACED.. PART TC: 8,311. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200932 19990212 00932 EA 1999 2 12 CA981113024 1 19981025 A 2130 350023000 CHECK VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF341A NE LT PACK MALFUNCTIONED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 9101 807157 (CAN) PRIOR TO DEPARTURE,THE LEFT HAND AC PACK OVERHEATED AND SMOKE OBSERVED IN CABIN. PASSENGER DEPLANED. BOTH COALES CER BAGS REPLACED AND LEFT HAND PACK SHUTTLE VALVE REPLACED.. PART TC: 7,896. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200933 19990212 00933 EA 1999 2 12 CA981113028 1 19981021 A 2750 855D1007 BPSU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE FLAPS FAILED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 8619 807173 (CAN) DURING DESCENT AT 6,000 FEET AND 200 KNOTS AT FLAP SELECTION 8, FLAPS DID NOT TRAVEL AND FLAP FAIL MESSAGE CAME ON . QUICK REF. PROCEDURE CARRIED OUT AND AIRCRAFT LANDED FLAPLESS. AD CF-98-14 CARRIED OUT, AND BOTH BRAKE AND POSITION SENSING UNITS CHANGED.. PART TC: 7,751. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021200936 19990212 00936 EA 1999 2 12 CA981123015 1 19981105 A 2170 COALESCER CNDAIR CL600 CL6002B19 EA RT/ LT PACKS CONTAMINATED W A UNSCHED LANDING B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CL CLIMB 1 CA 4003 (CAN) AFTER TAKEOFF, LAV AMBER SMOKE MESSAGE AT 1,500 FEET. PASSENGER REPORTED ODD SMELL. GROUND RUN, FOUND OIL SMEL L FROM RT ENGINE WHEN PACK ON. REPLACED COALESCER BAGS, SMOKE DETECTORS AND BRAKES AND WHEELS. ALSO, REPLACED RT ENGIN E NR 1 AND NR 3 BEARING CARBON SEALS.. PART TC: 3,507. 2 L 7 2 4F RT A21EA 1999021200939 19990212 00939 SW 1999 2 12 CA981125057 1 19981021 A 3230 2751015001 UPLOCK OZONE OAS545115 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NLG CONTAMINATED W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA P54143 (CAN) ON APPROACH, NOSE GEAR DID NOT EXTEND WHEN SELECTED. EMERGENCY RELEASE WAS PULLED AND THE GEAR FREE-FELL TO DOWN AND LOCKED. INSPECTION FOUND THE NOSE UPLOCK LATCH ROLLER WAS COVERED IN DIRT FROM THE GRAVEL RUNWAYS. INSPECTION TO C LEAN UPLOCK ADDED TO DAILY INSPECTION. 2 L 7 2 4T 4 T RT A8SW E4WE 1999021200940 19990212 00940 SW 1999 2 12 CA981125072 1 19981116 A 3297 MS243312 WIRE OAS545319 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE SQUAT SWITCH CHAFED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 7837 1819 P44720C 931124 (CAN) WHEN GEAR SELECTED UP, THE GEAR REMAINED IN THE DOWN POSITION. AIRCRAFT RETURNED TO BASE. WIRING TO SQUAT SWITCH FOUND CHAFED AND WAS REPAIRED.. PART TC: 9,574. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999021200942 19990212 00942 EA 1999 2 12 CA981130004 1 19981127 A 2500 324000 BLANKET CNDAIR CL600 CL600* EA BS 325 BURNED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) INSULATION BLANKET FOUND BURNT WHERE IT COMES IN CONTACT WITH THE WATER WASTE DRAIN HEATER AT STA 325R. FOUND AS A RESULT OF FLEET INSPECTION FOLLOWING AN INCIDENT OF SMOKE IN-FLIGHT. 2 L 7 2 4F RT A21EA 1999021200945 19990212 00945 EA 1999 2 12 CA981130014 1 19981106 A 3230 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 7382 807295 (CAN) ON TAKEOFF, GEAR UP SELECTION NOSE GEAR DID NOT RETRACT, WITH GEAR DISAGREE MESSAGE. GEAR SELECTED DOWN, AND UP W ITH SAME RESULT. AIRCRAFT RETURNED. NOSE GEAR HAD REMAINED LOCKED DOWN WITH DOORS OPEN. NOSE GEAR SELECTOR VALVE REPL ACED.. PART TC: 6,280. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900001 19990219 00001 NE 1999 2 19 BJNA981102 2 19981117 A 7230 817401 HUB BOEING 737 7372H4 138448C NM PWA JT8 JT8D15 52051 NE LT ENGINE DAMAGED A BJNA C ABORTED TAKEOFF C F.O.D. TO TAKEOFF 1 WP 11 456TM 20336 HIT DEER ON LEFT ENGINE NACELLE DURING TAKEOFF ROLL (AT V1). REMOVED AND REPLACED NOSE COWL ASSY, NOSE BULLET ASSY PER PWMM 72-000-23. REMOVED AND REPLACED C1 FAN ASSY PER PWMM 72-30-0, PEFORMED TEST I AND G. REFERENCE GE ON WING SUPPORT SERVICE WORK ORDER UH0486, ALL SYSTEMS CHECK NORMAL. (X) 2 L 7 2 4F 4 F A16WE E2EA 1999021900002 19990219 00002 SO 1999 2 19 C2XA98IA492 1 19981205 A 3350 RPS1B POWER SUPPLY EMB 145 EMB145LR SO CABIN INOPERATIVE A C2XA K NONE L NO TEST IN INSP/MAINT 1 SW 09 13955 145075 IAH - DURING PRE-FLIGHT INSPECTION, THE CREW REPORTED THE OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REMOV ED AND REPLACED THE NR 4 EMERGENCY LIGHT POWER SUPPLY IAW EMB145 MM 33-50-04, AND THE AIRCRAFT WAS APPROVED FOR RETURN T O SERVICE. (X) 2 L 7 2 4T RT T00011AT 1999021900003 19990219 00003 WP 1999 2 19 G6OA029 1 19981231 A 2612 FIRE DETECTOR DOUG DC10 DC1030F 3023504 WP CARGO BAY MALFUNCTIONED A G6OA O OTHER N FALSE WARNING AP APPROACH 1 EA 27 607GC 46978 WHILE ON FINAL APPROACH TO MIA, THE LOWER AFT CARGO COMPARTMENT FIRE WARNING LIGHT BECAME ILLUMINATED. THE NR 1 FIRE BO TTLE WAS DISCHARGED, THE LOWER AFT CARGO COMPARTMENT FIRE WARNING LIGHT WENT OUT. GROUND MAINTENANCE REMOVED AND REPLAC ED THE NR 1 FIRE BOTTLE IAW MM 26-7-00. SYSTEM OPERATIONALLY CHECKED NORMAL. NO EVIDENCE OF FIRE OR SMOKE IN LOWER AFT CARGO COMPARTMENT. 2 L 7 3 4F RT A22WE 1999021900004 19990219 00004 WP 1999 2 19 99ZZZX601 2 19981106 A 7321 307080022 FUEL CONTROL LEAR 35 35A 5170602 CE GARRTT TFE731 TFE73122B 01518 WP LT ENGINE MALFUNCTIONED A NOZA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 WP 23 21NG 675 343 P74896 AIRCRAFT WAS ON A FAR PART 91 COMPANY FLIGHT, DEPARTING DAL - JUST AFTER TAKEOFF, THE LEFT LOW FUEL PRESSURE ANNUNCIATOR LIGHT ILLUMINATED FOLLOWED BY AN ENGINE SURGE THEN ENGINE ROLLED BACK TO 62 PERCENT N1 AND STABILIZED. LEFT ENGINE COM PUTER ANNUNCIATOR LIGHT ILUMINATED. FLIGHT CREW FOLLOWED AIRCRAFT FLIGHT MANUAL CHECK LIST. AIRCRAFT WAS TURNED OVER T O MAINTENANCE AND FUEL CONTROL UNIT AND HIGH PRESSURE PUMP ASSEMBLY WAS REPLACED. AIRCRAFT WAS RETURNED TO SERVICE. (X ) 2 L 7 2 4F 4 F A10CE E6WE 1999021900005 19990219 00005 1999 2 19 RAIA981221 4 19981221 A 3417 98021727 ADC EMB 145 EMB145 SO NR 1 FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 804HK 447 145082 JFK/RED - FLT 6705 - RED WARNING. NO TAKEOFF DATA ILLUMINATED. MAINTENANCE REPLACED NR 1 AIR DATA COMPUTER. (X) 2 L 7 2 4F RT T00011AT 1999021900006 19990219 00006 NM 1999 2 19 TSAA9833644 1 19981216 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERABLE. OSP CHECK OK. AIRCRAFT REUTRNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999021900007 19990219 00007 NM 1999 2 19 TSAA9833652 1 19981225 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999021900008 19990219 00008 NM 1999 2 19 TSAA9833654 1 19981228 A 3350 6012311 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 RIGHT OVERWING EMERGENCY LIGHT INOPERABLE. REPLACED BATTERY PACK FOR RIGHT OVERWING EMERGENCY LIGHT ASSY. OPS CHECK O K. AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A16WE 1999021900009 19990219 00009 NM 1999 2 19 TSAA9833653 1 19981225 A 3350 8731002511 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED RIGHT WING EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. ( X) 2 L 7 2 4F RT A16WE 1999021900010 19990219 00010 NM 1999 2 19 TSAA9833650 1 19981222 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 4 AND NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. ARICRAFT RETURNED TO SERVIC E. (X) 2 L 7 2 4F RT A16WE 1999021900011 19990219 00011 NE 1999 2 19 TY7A9802 2 19981220 A 7250 TURBINE STBROS SD3 SD360 8100606 EU PWA PT6 PT6A67R 52043 NE HARTZL HCA6A HCA6A3 NE LT ENGINE FAILED A TY7A C ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 EA 15 350TA 12232 4233 SH3757 106067 GP22 LEFT ENGINE WAS REPLACED DUE TO TURBINE FAILURE AND PROPELLER REMOVED AND SERVICED. 2 H 7 2 4T 4 T A41EU E26NE 6 C P14NE 1999021900012 19990219 00012 EA 1999 2 19 SHUT98102 1 19981220 A 5210 85210181003 CABLE 85210002001 DHAV DHC8 DHC8311 1386006 EA PAX DOOR JAMMED A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 804SA 375 BUF/ILG - FLT 104 - DURING DEPLANING, THE PASSENGER DOOR ASSIST CABLE JAMMED. THE CREW CALLED FOR MAINTENANCE. MAINTEN ANCE CLEANED, LUBED, AND RE-ATTACHED THE PASSENGER DOOR ASSIST CABLE. OPS CHECKED GOOD. RETURNED TO SERVICE. (X) 2 H 7 2 4T RT A13NM 1999021900013 19990219 00013 EA 1999 2 19 VTZA98305 1 19981007 A 2750 855D1009 BPSU CNDAIR CL600 CL6002B19 EA LT FLAP FAILED A VTZA A UNSCHED LANDING F FLT CONT AFFECTED LD LANDING 1 EA 27 630BR 7255 IAD/GSP - FLT 6747 - DURING LANDING ON 10-7-98 AT 1000 HOURS, EXPERIENCED FLAP FAIL MESSAGE ON THE MASTER CAUTION PANEL. AIRCRAFT CONTACTED MAINTENANCE CONTROL AND DISPATCHED, DECISION TO RETURN TO IAD WAS MADE. UPON ARRIVAL AT IAD AIRCR AFT, DECLARED AN EMERGENCY AND LANDED AT IAD WITH NO FURTHER INCIDENT. MAINTENANCE CONTROL WAS NOTIFIED AND AIRCRAFT WA S TAXIED TO RAMP FOR TROUBLESHOOTING AND MAINTENANCE. MAINTENANCE FOUND THE BPSU HAD FAILED. BPSU WAS REMOVED AND REPL ACED AND SYSTEM WAS THOROUGHLY TROUBLESHOT WITH THE ASSISTANCE OF THE BOMBARDIER REPRESENTATIVE. ALL PERTINENT CHECKS W ERE ACCOMPLISHED. AIRCRAFT WAS THEN RELEASED FOR SERVICE. (X) 2 L 7 2 4F RT A21EA 1999021900097 19990219 00097 WP 1999 2 19 AT9900097 1 19981209 A 5511 SPAR DOUG DC9 DC932 3022066 WP HORIZ STAB MISDRILLED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND LEFT HAND HORIZONTAL STABILIZER UPPER SPAR CAP HAS HOLE DRILLED ON UPPER SI DE NEXT TO FASTENER HOLE AT STA 120. REMOVED NUT PLATE CLIP, REPAIRED FASTENER HOLE BY STEPPING UP HOLE AND REINTALLING NUT PLATE CLIP IAW DC9 SRM 51-30-2, AND RES NR 982168. 2 L 7 2 4F A6WE 1999021900098 19990219 00098 WP 1999 2 19 AT9900098 1 19981206 A 2550 PANEL DOUG DC9 DC932 3022066 WP CARGO COMPT CRACKED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD PIT NR 2 AND NR 3 LOWER SIDE WALL PANEL HAS A 4 CRACK AND 8 HO LE. REMOVED, REPLACED, FABRICATED, TRIMMED, AND DRILLED NEW PANELS IAW DC9 SRM 51-30-0, 53-21-0, MM 25-52-1, AND RES NR 982221. 2 L 7 2 4F A6WE 1999021900099 19990219 00099 WP 1999 2 19 AT9900099 1 19981215 A 5320 ANGLE DOUG DC9 DC932 3022066 WP E/E COMPT CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOOR SUPPORT ANGLE AT AFT BULKHEAD OF E/E COMPARTMENT CORRODED BEYOND LIMITS. REMOVED CORRODED FLOOR SUPPORT ANGLE, FABRICATED EXTRUSION, HEAT TREATED, DRILLED, AND INSTALLED IAW DC9 SRM 51 -10-4, 51-30-1, 51-10-2A, AND 51-10-2. 2 L 7 2 4F A6WE 1999021900100 19990219 00100 WP 1999 2 19 AT9900100 1 19981208 A 5311 FRAME DOUG DC9 DC932 3022066 WP BS 1143 CHAFED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT SECTION INTERIOR TAIL CONE RELEASE HANDLE METALLIC PLACARD WAS CHAF FING AGAINST THE FRAME AT STA 1143. CLEAN UP WORN FRAME, FABRICATED STRAP TO BACK SIDE OF FRAME FLANGE, PRIMED AND INST ALLED IAW DC9 SRM 53-11-4, 51-10-3, AND RES NR 9910. 2 L 7 2 4F A6WE 1999021900102 19990219 00102 WP 1999 2 19 AT9900102 1 19981210 A 5320 5913829501 BRACKET DOUG DC9 DC932 3022066 WP BS 1120 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT ACCESSORY COMPARTMENT CABLE PULLEY BRACKET HAS CORROSION AT STA 112 0 LEFT SIDE LOWER AREA. REMOVED, REPLACED, AND INSTALLED NEW PULLEY BRACKET IN AFT ACCESSORY COMPARTMENT IAW DC9 MM 16- 10-20. SYSTEM NOT DISTURBED, NO RIG CHECK NECESSARY. 2 L 7 2 4F A6WE 1999021900178 19990219 00178 WP 1999 2 19 UPS99828700 1 19981229 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1885 DENTED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE:D, SKIN FWD OF TAIL CONE AT STA 1885 IS BULGED AND DENTED. FAB NEW SKIN SECTION IAW DAC 5644500 ALODINE D AND PRIMED IAW DC8 SRM 51-1-8. INSTALL IAW DC8 SRM 51-1-21. 2 L 7 4 4F RT 4A25 1999021900318 19990219 00318 WP 1999 2 19 UPS99828727 1 19981231 A 2820 FITTING DOUG DC8 DC873F 302199F WP CTR FUEL TANK LEAKING A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, LT HAND SKI FITTING IN CTR TANK LEAKING FUEL. REMOVED AND REPLACED SKI FITTING IAW REO-06186. 2 L 7 4 4F RT 4A25 1999021900321 19990219 00321 WP 1999 2 19 UPS99828731 1 19981228 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 870 CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 868UP 45968 INSPECTION TYPE-C123, LONG 24L CRACKED AT STA 870. REMOVED AND REPLACED LONG 24L. 2 L 7 4 4F RT 4A25 1999021900334 19990219 00334 NM 1999 2 19 DLM88990288 1 19980213 A 5220 SEAL DOUG MD88 MD88 3023688 NM 2L DOOR OUT OF POSITION A DALA B EMER. DESCENT O OTHER CL CLIMB 1 SO 27 947DL 49878 ON CLIMBOUT, FLOW LIGHT ILLUMINATED. PRESS VALVE INDICATED FULL CLOSED AND PACKS IN AUTO WITH PRESS 30 PSI EACH. UNABL E TO CONTROL PRESS AND CABIN ALT. CONDUCTED FLT BELOW 10,000 FT, VALVE DID MODULATE ONCE LEVELED OFF. F/A ADVISED DOOR SEALS AT 2L HAD STRONG AIRFLOW ON DESCENT. FOUND SEAL AT 2L OUT OF TRACK. REINSTALLED SAME, PRESS A/C WITH PACK AND O PS NORMAL. 2 L 7 2 4F RT A6WE 1999021900401 19990219 00401 EA 1999 2 19 CA981216018 1 19981208 A 5210 DOOR CNDAIR CL600 CL6002B19 EA CABIN OUT OF RIG W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 4195 (CAN) PASSENGER DOOR STOW AMBER AND PASSENGER DOOR RED WARNING CAME ON AT FL 200. QUICK REF. CARRIED OUT. AIRCRAFT DIV ERTED. MAIN CABIN DOOR RE-RIGGED. 2 L 7 2 4F RT A21EA 1999021900402 19990219 00402 EA 1999 2 19 CA981216023 1 19981128 A 5210 ROD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR OUT OF ADJUST W A I UNSCHED LANDING CABIN DEPRESSURIZATION J WARNING INDICATION CR CRUISE 1 CA 5882 807389 (CAN) PASSENGER DOOR ANNUNCIATION IN-FLIGHT. EMERGENCY DEPRESSURIZATION CARRIED OUT, AIRCRAFT RETURNED. FLAPPER DOOR R OD ADJUSTED. TOTAL CYCLES: 5,318. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900407 19990219 00407 EA 1999 2 19 CA990111037 1 19981216 A 5210 HANDLE CNDAIR CL600 CL6002B19 EA PASSENGER DOOR OUT OF RIG W O OTHER J WARNING INDICATION CL CLIMB 1 CA 4219 (CAN) AFTER TAKEOFF, THE PASSENGER DOOR HANDLE WARNING CAME ON. THE DOOR LATCH CAM ASSEMBLY WAS OUT OF RIG. 2 L 7 2 4F RT A21EA 1999021900408 19990219 00408 EA 1999 2 19 CA990111039 1 19981223 A 5610 WINDSHIELD CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE COCKPIT LEAKING W O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 8341 807380 (CAN) DURING TAXI AN ELECTRICAL BURNING SMELL IN COCKPIT. GLYCOL HAD LEAKED THROUGH THE COPILOT'S WINDSHIELD ONTO A FLO OD LIGHT. TOTAL CYCLES: 7,289. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900409 19990219 00409 EA 1999 2 19 CA990111040 1 19981223 A 2750 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE WINGS FAILED W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 8891 807173 (CAN) DURING LANDING, THE FLAPS LOCK MESSAGE CAME ON. AIRCRAFT LANDED AT ZERO FLAPS. FLAP SYSTEM RESET. TOTAL CYCLES: 8,050. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900410 19990219 00410 EA 1999 2 19 CA990111041 1 19981225 A 2750 FECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 8990 807173 (CAN) DURING APPROACH, THE FLAPS FAILED AT ZERO DEGREES. FLAP POWER DRIVE UNIT AND FLAP ELECTRONIC CONTROL UNIT REPLACE D. TOTAL CYCLES: 8,056. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900411 19990219 00411 EA 1999 2 19 CA990111042 1 19981226 A 2750 DRIVE UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED CR CRUISE 1 CA 8993 807173 (CAN) FLAP FAIL MESSAGE IN-FLIGHT. REPLACED THE FLAP POWER DRIVE UNIT AND FLAP ELECTRONIC CONTROL UNIT. TOTAL CYCLES: 8,058. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900412 19990219 00412 EA 1999 2 19 CA990111043 1 19981227 A 3260 SENSOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG FAILED W O OTHER J WARNING INDICATION TO TAKEOFF 1 CA 8995 807173 (CAN) ON GEAR RETRACTION, A LOUD BANG WAS HEARD FROM NOSE LANDING GEAR ASSOCIATED WITH A GEAR DISAGREE MESSAGE AND AURAL WARNING. THE PROXIMITY SWITCH WAS REPLACED. TOTAL CYCLES: 8,060. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900413 19990219 00413 EA 1999 2 19 CA990111045 1 19981225 A 2752 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 4624 (CAN) ON FLAP SELECTION OF 45 DEGREES, A FLAP FAIL MESSAGE RECEIVED. LIGHT AILERON CONTROL INPUT REQUIRED TO CONTROL RO LL. RIGHT WING OUTBOARD FLAP ACTUATOR REPLACED. TOTAL CYCLES: 4,152. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900415 19990219 00415 EA 1999 2 19 CA990111048 1 19981229 A 5244 PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LT EXHAUST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 8232 807267 (CAN) ON WALK-AROUND, THE ACCESS PANEL AT THE 6 O'CLOCK POSITION WAS NOTED AS MISSING FROM THE LEFT HAND ENGINE EXHAUST NOZZLE FAIRING ASSEMBLY. THERE WAS ALSO A 1 INCH CRACK NEAR THE PANEL CUT OUT. TOTAL CYCLES: 6.940. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900417 19990219 00417 EA 1999 2 19 CA990115017 1 19981231 A 5244 PANEL CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE LT ENGINE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 6768 807343 (CAN) LEFT HAND ENGINE EXHAUST NOZZLE ACCESS PANEL MISSING AT 12 O'CLOCK POSITION. TOTAL CYCLES: 5,926. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900418 19990219 00418 EA 1999 2 19 CA990115020 1 19981231 A 2750 CONTROL UNIT CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE TE FLAPS FAILED W O OTHER F FLT CONT AFFECTED DE DESCENT 1 CA 9019 807173 (CAN) FLAPS FAIL CAUTION MESSAGE IN-FLIGHT ON DESCENT AT 7,000 FEET. BRAKE SYSTEM CONTROL UNIT REPLACED AND FLAPS RIGGE D. TOTAL CYCLES: 8,076. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900419 19990219 00419 EA 1999 2 19 CA990115021 1 19981231 A 2750 FLAPS CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WINGS FAILED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 6082 807389 (CAN) AFTER TAKEOFF, FLAP RETRACTION LOCKED AT 8 DEGREES AND FLAP FAIL MESSAGE ON. AIRCRAFT DIVERTED. FLAP RIGGING AND OPERATIONAL CHECK NORMAL. TOTAL CYCLES: 5,487. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900420 19990219 00420 EA 1999 2 19 CA990115022 1 19981230 A 5210 DOOR CNDAIR CL600 CL6002B19 EA CABIN OUT OF RIG W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 4303 (CAN) ON CLIMB, PASSENGER LATCH CAUTION MESSAGE, FOLLOWED BY PASSENGER DOOR WARNING. QUICK REF CARRIED OUT. PASSENGER DOOR RE-RIGGED. 2 L 7 2 4F RT A21EA 1999021900421 19990219 00421 EA 1999 2 19 CA990115023 1 19981229 A 5210 PLATE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE PASSENGER DOOR FAILED W A I UNSCHED LANDING CABIN DEPRESSURIZATION J WARNING INDICATION CL CLIMB 1 CA 7812 807281 (CAN) IN CLIMB THROUGH 17,000 FEET, CAUTION MESSAGE PASSENGER DOOR LATCH FOLLOWED BY AURAL WARNING. QUICK REF CARRIED O UT. EMERGENCY DEPRESSURIZATION INITIATED. AIRCRAFT RETURNED. MAIN CABIN DOOR STRIKER PLATE RE-WORKED. DOOR RIGGING C HECKED. TOTAL CYCLES: 6.642. 2 L 7 2 4F 4 F RT A21EA E15NE 1999021900545 19990219 00545 SW 1999 2 19 99ZZZX658 1 19981014 A 7810 210853610 NOZZLE SWRNGN SA226 SA226TC 8780404 SW EXHAUST DAMAGED A CWTA K NONE O OTHER IN INSP/MAINT 1 GL 05 392CA 5695 TC392 PRE-FLIGHT INSPECTION FOUND 5.50 INCH BY 4 INCH PIECE OF EXHAUST NOZZLE MISSING FROM AFT END OF NOZZLE. EXHAUST DUCT WA S DAMAGED AS PART DEPARTED AIRCRAFT. BOTH PARTS REPLACED. 2 L 7 2 4T RT A8SW 1999021900569 19990219 00569 WP 1999 2 19 EIAA980283 1 19981002 A 5320 SUPPORT DOUG DC9 DC932F 3022067 WP BS 180 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN FLOOR SUPPORT 'T' FITTING AT FS 180 FROM RBL 24-44 DAMAGE WAS FOUND. REPAIRED BY REPLA CEMENT OF 'T' SECTION PER SRM 53-11-1 FIG 16. (M) 2 L 7 2 4F A6WE 1999021900570 19990219 00570 WP 1999 2 19 EIAA980282 1 19981002 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 180-989 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN FLOOR SEAT TRACKS FROM FS 180-989, NUMEROUS SPOTS OF CORROSION ON SPLICE FITTINGS WERE FOUND, FS 180-227 RBL 24 W473, FS 180-227 LBL 44 V091, FS 218-230 RBL 45 V089, FS 218-230 LBL 45, FS 218-513 LBL 37 W095 , FS 223-435 BL 0 W073, FS 237-481 LBL 0-16 V099, FS 305-425 LBL 16 W094, FS 330-340 RT OUTBOARD W269, FS 408 RBL 45 W27 0, FS 408-512 LBL 37 W095 AND W103, FS 579 RBL 45 W172, FS 668 RBL 44 W496, FS 670-745 LBL 18 W433, FS 689 RBL 30 W174, FS 718-986 LBL 58 W432, FS 739-785 RBL 34 W312, FS 748 LBL 24 W406, FS 766-822 RBL 56 W446, FS 770 RBL 5 W176, FS 822-9 86 RBL 49 Y054, FS 832 RBL 12 W175, FS 832-986 RBL 58 W393, FS 856 LBL 34 W507, FS 929-989 LBL 44 W427. REPAIRED SEAT T 2 L 7 2 4F A6WE 1999021900589 19990219 00589 WP 1999 2 19 EIAA980310 1 19981002 A 5542 SKIN DOUG DC9 DC932F 3022067 WP RUDDER CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RUDDER SKIN AT RIGHT RIB NR 4 WAS FOUND CRACKED. REPAIRED PER SRM 55-03 FIG 11. (M) 2 L 7 2 4F A6WE 1999021900590 19990219 00590 WP 1999 2 19 EIAA980308 1 19981002 A 5312 BLKHD STIFFENER DOUG DC9 DC932F 3022067 WP AFT PRESS BLKHD CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, AFT RPESSURE BULKHEAD AFT SIDE HAS A CRACKED STIFFENER AT 4 O'CLOCK AND 5 O'CLOCK POSITIONS. REPA IRED PER SRM 53-11-3. (M) 2 L 7 2 4F A6WE 1999021900591 19990219 00591 WP 1999 2 19 EIAA980307 1 19981002 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 1006 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, LONGERON 23L HAS CORROSION FROM FS 1006. REPAIRED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999021900592 19990219 00592 WP 1999 2 19 EIAA980306 1 19981002 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 996-1033 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LONGERON 24L HAS CORROSION FROM FS 996-1033. REPAIRED PER SRM 51-11-4 FIG 6 AND FIG 18. (M) 2 L 7 2 4F A6WE 1999021900593 19990219 00593 WP 1999 2 19 EIAA980305 1 19981002 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 996-1080 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, LONGERON 25L HAS CORROSION FROM FS 996-1080. REPAIRED PER SRM 53-11-4. (M) 2 L 7 2 4F A6WE 1999021900594 19990219 00594 WP 1999 2 19 EIAA980303 1 19981002 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LONGERON 13R IS CRACKED AT FS 965. REPAIRED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999021900595 19990219 00595 WP 1999 2 19 EIAA980302 1 19981002 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 965 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LONGERON 6R IS CRACKED AT FS 965. REPAIRED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999021900596 19990219 00596 WP 1999 2 19 EIAA980301 1 19981002 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 945 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LONGERON 17R IS CRACKED AT FS 945. REPAIRED PER SRM 53-11-03 FIG 4C. (M) 2 L 7 2 4F A6WE 1999021900597 19990219 00597 WP 1999 2 19 EIAA980300 1 19981002 A 5313 LONGERON DOUG DC9 DC932F 3022067 WP BS 945 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LONGERON 17L IS CRACKED AT FS 945. REPAIRED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999021900598 19990219 00598 WP 1999 2 19 EIAA980299 1 19981002 A 5320 SPLICE DOUG DC9 DC932F 3022067 WP BS 945 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE FRAME SPLICE AT FS 945 LONGERON 28L TO 30 HAS CORROSION. REPAIRED PER SRM 53-11-3 FIG 3A . (M) 2 L 7 2 4F A6WE 1999021900599 19990219 00599 WP 1999 2 19 EIAA980298 1 19981002 A 5330 SKIN DOUG DC9 DC932F 3022067 WP BS 937 CHAFED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE SKIN AT RIGHT PYLON LEADING EDGE HAS CHAFE MARKS, FS 937 LONGERON 15R. REPAIRED PER SRM 53-04 FIG 3A. (M) 2 L 7 2 4F A6WE 1999021900600 19990219 00600 WP 1999 2 19 EIAA980297 1 19981002 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 965 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, AFT BAG BIN FRAME ST FS 965 HAS CORROSION FROM LONGERON 28L TO 28R. REPAIRED PER SRM 53-03 FIG 2A . (M) 2 L 7 2 4F A6WE 1999021900601 19990219 00601 WP 1999 2 19 EIAA980296 1 19981002 A 5311 9919620501 FRAME DOUG DC9 DC932F 3022067 WP BS 756 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE FRAME FS 756 HAS A CRACK AT THE LEFT SIDE AND RIGHT. REPAIRED PER SB 53-168. (M) 2 L 7 2 4F A6WE 1999021900602 19990219 00602 WP 1999 2 19 EIAA980295 1 19981002 A 5311 9919619503N FRAME DOUG DC9 DC932F 3022067 WP BS 737 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE FRAME FS 737 HAS A CRACK AT LONGERON 17L. REPAIRED PER SB 53-131. (M) 2 L 7 2 4F A6WE 1999021900603 19990219 00603 WP 1999 2 19 EIAA980294 1 19981002 A 5753 SKIN DOUG DC9 DC932F 3022067 WP RT TE FLAP DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RIGHT INBOARD TRAILING EDGE FLAP LEADING EDGE SKIN HAS DAMAGE AT XFLS 60 AND 105. REPAIRED PER EA DC9-57-137 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021900604 19990219 00604 WP 1999 2 19 EIAA980292 1 19981002 A 5313 592232829 LONGERON DOUG DC9 DC932F 3022067 WP BS 455 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, LONGERON S24L AND 25L WERE FOUND TO HAVE DAMAGE AT FS 455. REPAIRED PER SRM 53-02 FIG 18, EA DC9- 53-207 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021900605 19990219 00605 WP 1999 2 19 99ZZZM129 1 19981002 A 5313 592232837 LONGERON DOUG DC9 DC932F 3022067 WP BS 455 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, LONGERON S24L AND 25L WERE FOUND TO HAVE DAMAGE AT FS 455. REPAIRED PER SRM 53-02 FIG 18, EA DC9- 53-207 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999021900606 19990219 00606 WP 1999 2 19 EIAA980290 1 19981002 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 313 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN DECK CARGO DOOR FRAME FS 313 APPROX 36 INCHES ABOVE FLOOR LEVEL HAS DAMAGE. REPAIRED PER SRM 53-01 AND 51-30. (M) 2 L 7 2 4F A6WE 1999021900607 19990219 00607 WP 1999 2 19 EIAA980288 1 19981002 A 5230 FRAME DOUG DC9 DC932F 3022067 WP CARGO DOOR DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN DECK CARGO DOOR LOWER FORWARD CORNER FRAME WEB HAS DAMAGE. REPAIRED PER SRM 51-10-2. (M) 2 L 7 2 4F A6WE 1999021900608 19990219 00608 WP 1999 2 19 EIAA980286 1 19981002 A 5330 SKIN DOUG DC9 DC932F 3022067 WP BS 301 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE SKIN AT FS 301 WAS FOUND CRACKED, AT THE LOWER AFT CORNER OF THE MAIN DECK CARGO DOOR. R EPAIRED PER SRM 53-05 FIG 103. (M) 2 L 7 2 4F A6WE 1999021900609 19990219 00609 WP 1999 2 19 EIAA980285 1 19981002 A 5311 FRAME DOUG DC9 DC932F 3022067 WP BS 218 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, FUSELAGE FRAME AT FS 218 HAS CORROSION AT LONGERON 30. REPAIRED PER SRM 53-03 FIG 5. (M) 2 L 7 2 4F A6WE 1999021900618 19990219 00618 NM 1999 2 19 P2EA98251 1 19981011 A 5753 654631251 SKIN BOEING 737 737244 138448U NM LT TE FOREFLAP DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 620PC 19708 SJO - LEFT WING OUTBOARD FOREFLAP WORN AND DENTED. DEFECT SIZE, VARIOUS. REPAIRED LEFT WING OUTBOARD FOREFLAP PER COOP ESA EO COO-3-57-583-98 DATED OCT 21, 1998. REPAIRED LEADING EDGE PER SRM 57-50-4 FIG 1. (M) 2 L 7 2 4F A16WE 1999021900619 19990219 00619 NE 1999 2 19 99ZZZM130 2 19981203 A 7250 TURBINE BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 1 ENGINE DAMAGED A RYNA O OTHER J WARNING INDICATION CR CRUISE 1 CE 07 421EX 19099 654710 FLT 720 - NR 1 ENGINE HAD 1 QUICK LOUD BANG ON TRIP FROM DTW TO IND. NOTICED OIL TEMP/PRESSURE WERE FINE. WITH N1 MATC HED N2, FUEL FLOW AND EGT VERY HIGH. ABOVE IDLE AND BELOW 70 PERCENT N1 ENGINE HAS VIBRATION. SMOOTHES OUT ABOVE N1 BU T TEMPERATURE GETS TO RED LINE. REMOVED AND REPLACED NR 1 ENGINE DUE TO TURBINE DAMAGE. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999021900621 19990219 00621 EU 1999 2 19 RAIA981102 1 19981102 A 7797 KR124R WIRE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE FAILED A RAIA B E EMER. DESCENT ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 CE 03 427AM 876 FLT 7358 - STL - RIGHT ENGINE EGT WENT PAST 1000 DEGREES, ALL OTHER INDICATIONS NORMAL. TORQUE WOULD NOT GO ABOVE 40 PE RCENT. RIGHT ENGINE WAS SHUT DOWN. MAINTENANCE REPAIRED BROKEN WIRE TO FUEL BYPASS VALVE. (M) 2 L 7 2 4T RT A56EU 1999021900622 19990219 00622 WP 1999 2 19 EIAA980329 1 19981001 A 5230 SKIN DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47426 47279 MZJ - DURING C4 CHECK, FORWARD CARGO DOOR OUTER SKIN CRACK FROM FASTENER HOLE WAS FOUND. REPAIRED PER SRM 52-01 FIG 2, AND 52-32-0. (M) 2 L 7 2 4F A6WE 1999021900623 19990219 00623 WP 1999 2 19 EIAA980331 1 19981022 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 1089 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47426 47279 MZJ - DURING C4 CHECK, FS 1089 LONGERON 14R, LONGERON HAS HEAVY CORROSION. REPAIRED DAMAGED LONGERON PER ECRA 945-53-02 6-2. (M) 2 L 7 2 4F A6WE 1999021900624 19990219 00624 WP 1999 2 19 EIAA980330 1 19981031 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 1121 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47279 MZJ - DURING C4 CHECK, FS 1121 LONGERON 16L-18L, SKIN AND FRAME HAS CORROSION. REPAIRED DAMAGED SKIN AND STRAP PER ECRA 945-53-026-2. (M) 2 L 7 2 4F A6WE 1999021900625 19990219 00625 WP 1999 2 19 99ZZZM132 1 19981031 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 1121 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47279 MZJ - DURING C4 CHECK, FS 1121 LONGERON 16L-18L, SKIN AND FRAME HAS CORROSION. REPAIRED DAMAGED SKIN AND STRAP PER ECRA 945-53-026-2. (M) 2 L 7 2 4F A6WE 1999021900626 19990219 00626 WP 1999 2 19 99ZZZM133 1 19981031 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 1121 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47279 MZJ - DURING C4 CHECK, FS 1121 LONGERON 16L-18L, SKIN AND FRAME HAS CORROSION. REPAIRED DAMAGED SKIN AND STRAP PER ECRA 945-53-026-2. (M) 2 L 7 2 4F A6WE 1999021900627 19990219 00627 WP 1999 2 19 EIAA980332 1 19981031 A 5330 SKIN DOUG DC9 DC933F 302207A WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47426 47279 MZJ - DURING C4 CHECK, UPPER FUSELAGE AFT ADF ANTENNA DOUBLER HAS CORROSION. REPAIRED PER SRM 53-04 AND ECRA 945-54-027 -2. (M) 2 L 7 2 4F A6WE 1999021900628 19990219 00628 WP 1999 2 19 EIAA980333 1 19981021 A 5400 SPAR DOUG DC9 DC933F 302207A WP RT PYLON CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47426 47279 MZJ - DURING C4 CHECK, RIGHT PYLON FORWARD SPAR UPPER BEAVER TAIL HAS CORROSION. REPAIRED PER SRM 54-04 AND ECRA 945-54 -025-2. (M) 2 L 7 2 4F A6WE 1999021900629 19990219 00629 WP 1999 2 19 EIAA980334 1 19981025 A 5315 FLOORBEAM DOUG DC9 DC933F 302207A WP BS 980 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47426 47279 MZJ - DURING C4 CHECK, AFT CARGO FLOORBEAM UPPER FLANGE AT FS 980 LBL 48 HAS CORROSION AT A PREVIOUS REPAIR. REPAIRED P ER SRM 53-05 AND ECRA 945-53-004-2. (M) 2 L 7 2 4F A6WE 1999021900630 19990219 00630 WP 1999 2 19 EIAA980335 1 19981003 A 5315 FLOORBEAM DOUG DC9 DC933F 302207A WP BS 996 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47426 47279 MZJ - DURING C4 CHECK, FS 996 FLOORBEAM WEB HAS EXFOLIATION CORROSION. REPAIRED PER SRM 53-05 FIG 72. (M) 2 L 7 2 4F A6WE 1999021900631 19990219 00631 WP 1999 2 19 EIAA980336 1 19981027 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 980 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47279 MZJ - DURING C4 CHECK, MAIN CABIN FS 980, LONGERON 17R HAS CRACK. REPAIRED PER SRM 53-02. (M) 2 L 7 2 4F A6WE 1999021900632 19990219 00632 WP 1999 2 19 EIAA980337 1 19981031 A 5210 SKIN DOUG DC9 DC933F 302207A WP PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47426 47279 MZJ - DURING C4 CHECK, LEFT FORWARD DOOR SKIN AT FED LOWER CORNER IS CRACKED AT TWO PLACES. REPAIRED PER SRM 52-05 FIG 32. (M) 2 L 7 2 4F A6WE 1999021900633 19990219 00633 NM 1999 2 19 EIAA980338 1 19981117 A 5315 FLOORBEAM BOEING 747 747273C 1384896 NM BS 440 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 74646 20653 HKG - DURING C1 CHECK, UPPER DECK FLOORBEAM HAS TEMPORARY REPAIRS AT BS 440 ON LEFT AND RIGHT SIDES. REPAIRED PER SRM 5 3-10-07 FIG 11, 8110-3 AND ECRA 470-53-98-1A. (M) 2 L 7 4 4F A20WE 1999021900634 19990219 00634 NM 1999 2 19 EIAA980339 1 19981117 A 5320 SPLICE BOEING 747 747273C 1384896 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 470EV 74646 20653 HKG - DURING C1 CHECK, RIGHT BS 1480 BULKHEAD FITTING SPLICE HAS 8 BOLT HOLES WITH CRACKS. REPAIRED PER SB 747-53A2390 FIG 23 AND EO 53-747-1513-98 REV A. (M) 2 L 7 4 4F A20WE 1999021900635 19990219 00635 NM 1999 2 19 EIAA980340 1 19981017 A 5330 SKIN BOEING 747 747212B 1384886 NM BS 160-170 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, FUSELAGE SKIN HAS A DENT AT BS 160-170 AT STRINGER 44R-46R. REPAIRED PER SRM 53-30-03 FIG 27. ( M) 2 L 7 4 4F A20WE 1999021900636 19990219 00636 NM 1999 2 19 EIAA980341 1 19981017 A 5210 GATE BOEING 747 747212B 1384886 NM PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, L1 DOOR UPPER GATE FOUND WITH A CRACK. REPLACED PER MM 52-11-01. (M) 2 L 7 4 4F A20WE 1999021900637 19990219 00637 NM 1999 2 19 EIAA980342 1 19981017 A 5210 SKIN BOEING 747 747212B 1384886 NM PAX DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, R3 DOOR SKIN FOUND CRACKED AT NR 4 FRAME LOWER AREA. REPAIRED PER SRM 52-10-02 FIG 9. (M) 2 L 7 4 4F A20WE 1999021900638 19990219 00638 NM 1999 2 19 EIAA980343 1 19981017 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM BS 1438 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, MAIN DECK SEAT TRACK FOUND CRACKED AT BS 1438 RLB 12. REPAIRED PER SRM 53-10-05 FIG 32. (M) 2 L 7 4 4F A20WE 1999021900639 19990219 00639 NM 1999 2 19 EIAA980344 1 19981017 A 5230 SKIN BOEING 747 747212B 1384886 NM CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, AFT CARGO DOOR SKIN HAS CORROSION. REPAIRED PER RS R-52-35-33841 AND ECRA 485-51-109-1. (M) 2 L 7 4 4F A20WE 1999021900640 19990219 00640 NM 1999 2 19 EIAA980345 1 19981017 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM BS 1540 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, AFT CARGO FLOORBEAM WEB FOUND CRACKED AT BS 1540 ABOVE STRINGER 44R. REPAIRED PER SRM 53-40-02 F IG 1. (M) 2 L 7 4 4F A20WE 1999021900641 19990219 00641 NM 1999 2 19 EIAA980346 1 19981017 A 5320 STRAP BOEING 747 747212B 1384886 NM BS 1350 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 HKG - DURING C6 CHECK, FUSELAGE SPLICE STRAP AT BS 1350 AT LEFT WLG BEAM AND LONGERON EXTENSION FITTING ATTACHMENT HAS C ORROSION, AND SKIN CRACKED AT TWO FASTENER HOLES. REPAIRED PER DWG 65B151210, SB 51-2043, RS R-53-41-33880 AND ECRA 485 -51-109-1. (M) 2 L 7 4 4F A20WE 1999021900642 19990219 00642 NM 1999 2 19 99ZZZM134 1 19981017 A 5320 FITTING BOEING 747 747212B 1384886 NM BS 1350 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 20712 HKG - DURING C6 CHECK, FUSELAGE SPLICE STRAP AT BS 1350 AT LEFT WLG BEAM AND LONGERON EXTENSION FITTING ATTACHMENT HAS C ORROSION, AND SKIN CRACKED AT TWO FASTENER HOLES. REPAIRED PER DWG 65B151210, SB 51-2043, RS R-53-41-33880 AND ECRA 485 -51-109-1. (M) 2 L 7 4 4F A20WE 1999021900643 19990219 00643 NM 1999 2 19 EIAA980348 1 19981017 A 5320 FITTING BOEING 747 747212B 1384886 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, FUSELAGE BS 1480 FITTING LEFT AND RIGHT SIDES, HAVE CRACKED FASTENER HOLES. REPLACED RT OUTER CH ORD FITTING, REPAIRED HOLES PER SB 53A2390 PLAN B REPAIR, AND SKIN CRACK REPAIRED. DEVIATIONS FROM THE ABOVE MENTIONED DOCUMENTS ARE APPROVED BY RS R-53-43-33879 AND ECRA NTOE, 8110-3 APPROVAL IS FOR A TIME LIMITED REPAIR, PENDING AN ALTER NATE SSID INSPECTION. (M) 2 L 7 4 4F A20WE 1999021900644 19990219 00644 NM 1999 2 19 EIAA980347 1 19981017 A 5320 FITTING BOEING 747 747212B 1384886 NM FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, LEFT WLG SUPPORT BEAM END FITTING FOUND CRACKED AT ATTACH BOLT HOLES. FITTING REPLACED PER SB 57 -2244 REV 5. (M) 2 L 7 4 4F A20WE 1999021900645 19990219 00645 NM 1999 2 19 EIAA980356 1 19981202 A 5320 SPLICE BOEING 747 747212B 1384886 NM BS 2484 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 HKG - DURING C5 CHECK, BS 2484 FORWARD LOWER LEFT SPLICE FITTING VERTICAL LEG 2ND OUTBOARD FASTENER HOLE CRACKED. REPLA CED SPLICE FITTING PER SB 747-53-2162. (M) 2 L 7 4 4F A20WE 1999021900646 19990219 00646 NM 1999 2 19 EIAA980355 1 19981202 A 5512 SKIN BOEING 747 747212B 1384886 NM HORIZ STABILIZER CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURNG C5 CHECK, LEFT HORIZONTAL STAB UPPER SKIN AT ST 310-335 AND 360-385 HAS CORROSION. REPAIRED PER RS R-55-13- 33958, 8110-3 AND ECRA 482-990125-1. (M) 2 L 7 4 4F A20WE 1999021900647 19990219 00647 NM 1999 2 19 EIAA980358 1 19981202 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 1620 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 20713 HKG - DURING C5 CHECK, AFT BAG BIN FRAME CRACKED AT BS 1620 STRINGER 39R-40R. REPAIRED FRAME PER SRM 53-10-04 FIG 69. ( M) 2 L 7 4 4F A20WE 1999021900648 19990219 00648 NM 1999 2 19 EIAA980359 1 19981202 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM BS 460 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, MD BS 460 AT LBL 90 FLOORBEAM LOWER CHORD HAS CORROSION. REPAIRED PER SRM 51-40-4 FIG 2. (M) 2 L 7 4 4F A20WE 1999021900649 19990219 00649 NM 1999 2 19 EIAA980360 1 19981202 A 5320 WEB BOEING 747 747212B 1384886 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 1480 APU DUCT CUTOUT FASTENER HOLES CRACKED ON BULKHEAD WEB. REPAIRED PER SB 747-53-2309. (M ) 2 L 7 4 4F A20WE 1999021900650 19990219 00650 NM 1999 2 19 EIAA980357 1 19981202 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 320 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 320 RIGHT FRAME CRACKED AT STRINGER 14. REPAIRED FRAME PER RS R-53-12-33953, 8110-3, ECRA 482 -99-125-1. (M) 2 L 7 4 4F A20WE 1999021900651 19990219 00651 NM 1999 2 19 EIAA980364 1 19981204 A 5414 SKIN BOEING 747 747212B 1384886 NM NR 3 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, NR 3 PYLON SKIN AT PANEL 473EL CUTOUT IS CRACKED, AND STIFFENER BEHIND IS CRACKED. REPAIRED PER RS R54-51-33962 AND ECRA 482-99-125-1. (M) 2 L 7 4 4F A20WE 1999021900652 19990219 00652 NM 1999 2 19 EIAA980365 1 19981207 A 5320 65B072326 SPLICE BOEING 747 747212B 1384886 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, MD BS 1480 STRINGER 7L SPLICE HAS CORROSION AND CRACKS. REPAIRED BY REPLACING STRINGER SPLICE FI TTING PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999021900653 19990219 00653 NM 1999 2 19 EIAA980366 1 19981207 A 5320 65B072326 SPLICE BOEING 747 747212B 1384886 NM BS 780-800 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 780-800 SKIN AND INTERNAL STRAP HAVE CORROSION FROM STRINGER 46L-46R. REPAIRED BY RS R53-21-3 3964, 8110-3 AND ECRA 481-99-125-1. (M) 2 L 7 4 4F A20WE 1999021900654 19990219 00654 NM 1999 2 19 EIAA980367 1 19981207 A 5280 SKIN BOEING 747 747212B 1384886 NM MLG DOOR DELAMINATED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78027 20713 HKG - DURING C5 CHECK, LEFT WING LANDING GEAR INBOARD DOOR OUTER SKIN WAS FOUND DELAMINATED. REPAIRED DOOR PER RS R52-8 2-33959,8110-3 AND ECRA 482-99-125-1. (M) 2 L 7 4 4F A20WE 1999021900655 19990219 00655 NM 1999 2 19 EIAA980368 1 19981207 A 5730 SKIN BOEING 747 747212B 1384886 NM WS 600 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, RIGHT WING LOWER SKIN AT WS 600, AT TRAILING EDGE HAS EXFOLIATION CORROSION. REPAIRED PER RS R57 -26-33954 AND ECRA 482-99-125-1. (M) 2 L 7 4 4F A20WE 1999021900656 19990219 00656 NM 1999 2 19 EIAA980369 1 19981207 A 5320 SPLICE BOEING 747 747212B 1384886 NM BS 519 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURNING C5 CHECK, MD BS 519 STRINGER 14L SPLICE CRACKED. REPAIRED PER SRM 51-10-1. (M) 2 L 7 4 4F A20WE 1999021900657 19990219 00657 NM 1999 2 19 EIAA980370 1 19981211 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 140 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 140 AT STRINGER 47L AFT BULKHEAD ATTACH SUPPORT FRAME CRACKED. REPAIRED PER SRM 51-40-03. (M ) 2 L 7 4 4F A20WE 1999021900658 19990219 00658 NM 1999 2 19 EIAA980371 1 19981211 A 5313 STRINGER BOEING 747 747212B 1384886 NM BS 1000 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 1000 STRINGER 39R TO 40R EXTERIOR SKIN CRACKED. REPAIRED PER SRM 53-30-01 FIG 1. (M) 2 L 7 4 4F A20WE 1999021900659 19990219 00659 NM 1999 2 19 EIAA980373 1 19981211 A 5320 WEB BOEING 747 747212B 1384886 NM BS 1346-1350 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURIGN C5 CHECK, MD BS 1346 TO 1350 AT LBL 2 PRESSURE DECK UPPER SURFACE HAS CORROSION AND CRACK. REPAIRED PER RS R53-48-33957 AND ECRA 482-99-125-1. (M) 2 L 7 4 4F A20WE 1999021900660 19990219 00660 NM 1999 2 19 EIAA980372 1 19981211 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 1700 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 1700 FRAME CRACKED AT STRINGER 12R TO 13R. REPAIRED PER SRM 51-10-01. (M) 2 L 7 4 4F A20WE 1999021900661 19990219 00661 NM 1999 2 19 EIAA980375 1 19981215 A 5330 SKIN BOEING 747 747132 1384882 NM BS 2100 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 479EV 85200 19898 HKG - DURING B-CHECK, FUSELAGE SKIN DENTED AT BS 2100 AT STRINGER 34R. REPAIRED PER SRM 53-30-03 FIG 4. (M) 2 L 7 4 4F A20WE 1999021900662 19990219 00662 NM 1999 2 19 EISA98322 1 19981220 A 3020 26130105 VALVE BOEING 727 727223 1384074 NM NR 2 ENGINE MALFUNCTIONED A EISA O OTHER M OVER TEMP CR CRUISE 1 SW 07 316NE U11060C 19475 NR 2 ENGINE DUCT OVERHEAT WITH ENGINE ANTI-ICE ON. MUST REDUCE POWER TO 65 PERCENT N1 FOR TEMP TO DROP. REMOVED AND RE PLACED THERMOSTATIC VALVE. OPS CHECK GOOD PER MM 30-21-21. (M) 2 L 7 3 4F A3WE 1999021900663 19990219 00663 NM 1999 2 19 EISA98319 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD , FOUND TWO AREAS OF DELAMINATION ON RIGH OUTBOARD AFT FLAP TRAILING EDGE. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-05, ALUMINUM HONEYCOMB REPAIR. (M) 2 L 7 3 4F RT A3WE 1999021900664 19990219 00664 NM 1999 2 19 EISA98318 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP GOUGED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND GOUGES ON UPPER SURFACE OF RIGHT OUTBOARD AFT FLAP. REPAIRED THREE GOUGES PER SRM 51-40-6 ALUMINUM HONEYCOMB REPAIR. (M) 2 L 7 3 4F RT A3WE 1999021900665 19990219 00665 NM 1999 2 19 EISA98317 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND AREA OF DELAMINATION ON OUTBOARD END OF LEFT INBOARD AFT FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-5, BONDED METAL REPAIR. (M) 2 L 7 3 4F RT A3WE 1999021900666 19990219 00666 NM 1999 2 19 EISA98316 1 19981209 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FIVE AREAS OF DELAMINATION ON LEFT OUTBOARD AFT FLAP. REPAIRE D AREAS OF DELAMINATION PER SRM 51-40-06, ALUMINUM HONEYCOMB REPAIR. (M) 2 L 7 3 4F RT A3WE 1999021900667 19990219 00667 NM 1999 2 19 EISA98315 1 19981209 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DENTED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND DENT ON LOWER SURFACE ON LEFT OUTBOARD AFT FLAP. REPAIRED DEN T PER SRM 51-40-6, ALUMINUM HONEYCOMB. (M) 2 L 7 3 4F RT A3WE 1999021900668 19990219 00668 NM 1999 2 19 EISA98312 1 19981208 A 5754 RIB BOEING 727 727277 138408S NM LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 2 SLAT WAS DISCOVERED CRACKED AT THIRD RIB FROM INBOARD END. FABR ICATED DOUBLER REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999021900669 19990219 00669 NM 1999 2 19 EISA98311 1 19981208 A 5754 RIB BOEING 727 727277 138408S NM LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORKCARD, NR 3 SLAT WAS FOUND CRACKED AT 2ND AND 7TH RIBS FROM OUTBOARD END. F ABRICATED DOUBLER REPAIRS PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-2. (M) 2 L 7 3 4F RT A3WE 1999021900670 19990219 00670 NM 1999 2 19 EISA98310 1 19981208 A 5754 RIB BOEING 727 727277 138408S NM LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 5 SLAT WAS FOUND CRACKED AT NR 5 AND NR 9 RIBS FROM INBOARD END. FABRICATED DOUBLER REPAIRS PER SRM 51-50-2 AND INSTALLED PER SRM 57-20-3. (M) 2 L 7 3 4F RT A3WE 1999021900671 19990219 00671 NM 1999 2 19 EISA98309 1 19981209 A 5754 RIB BOEING 727 727277 138408S NM LE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, NR 8 SLAT WAS FOUND CRACKED AT MOST OUTBOARD RIB. FABRICATED DOUBLE R REPAIR PER SRM 57-50-2 AND INSTALLED PER SRM 51-40-3. (M) 2 L 7 3 4F RT A3WE 1999021900672 19990219 00672 NM 1999 2 19 EISA98307 1 19981208 A 5522 SKIN BOEING 727 727277 138408S NM ELEVATOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURNG ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, X-RAY INSPECTION OF LEFT ELEVATOR SHOWS CRACK INDICATION OF .25 INCH AS SEEN IN SHOT NR L06, STATION 17.20-53.91). REMOVED LEFT ELEVATOR TAB TO FOM REPAIRED CRACK IN ELEVATOR PER SRM 51-40 -3. ACCOMPLISHED BALANCE CHECK PER SRM 51-80-7, REINSTALLED TAB PER MM 27-30-11. (M) 2 L 7 3 4F RT A3WE 1999021900673 19990219 00673 NM 1999 2 19 EISA98301 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD C53-224-01, NINE SMALL AREAS OF DELAMINATION ON RIGHT INBOARD AFT FLA P. REPAIRED ALL AREAS PER SRM 51-40-6. ALUMINUM HONEYCOMB REPAIRS. (M) 2 L 7 3 4F RT A3WE 1999021900674 19990219 00674 NM 1999 2 19 EISA98297 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND AREA WITH GOUGED AND CRACKED SKIN ON UPPER SURFACE OF RIGHT IN BOARD AFT FLAP. REMOVED DAMAGED SKIN. FABRICATED AND INSTALLED NEW SKIN SECTION PER SRM 57-50-4. (M) 2 L 7 3 4F RT A3WE 1999021900675 19990219 00675 NM 1999 2 19 EISA98288 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND THREE AREAS OF DELAMINATION ON RIGHT INBOARD MID FLAP TRAILING EDGE. REPAIRED AREAS PER SRM 51-40-6 ALUMINUM HONEYCOMB REPAIR. (M) 2 L 7 3 4F RT A3WE 1999021900676 19990219 00676 NM 1999 2 19 EISA98287 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP PUNCTURED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND SKIN PUNCTURE ON RIGHT INBOARD MID FLAP TRAILING EDGE LOWER SI DE. REPAIRED SKIN PUNCTURE PER SRM 51-40-6, 51-40-8, AND 51-40-9. (M) 2 L 7 3 4F RT A3WE 1999021900677 19990219 00677 NM 1999 2 19 EISA98285 1 19981208 A 5753 SKIN BOEING 727 727277 138408S NM TE FLAP DELAMINATED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TWO AREAS OF DELAMINATION ON LEFT INBOARD MID FLAP. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-6 AND 51-40-8. (M) 2 L 7 3 4F RT A3WE 1999021900678 19990219 00678 NM 1999 2 19 EISA98314 1 19981209 A 5242 RIB BOEING 727 727277 138408S NM E/E DOOR CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND TWO RIBS AND ONE BRACKET CRACKED IN STRUCTURE OF E/E DOOR. RE MOVED DAMAGED RIBS AND BRACKET. FABRICATED AND INSTALLED NEW RIBS AND BRACKET PER SRM 52-40-1 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999021900679 19990219 00679 NM 1999 2 19 EISA98313 1 19981208 A 5320 ANGLE BOEING 727 727277 138408S NM LAVATORY CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-1 CORROSION WAS FOUND TO EXIST ON FWD LAV BULKHEAD INSTALLATION ANGLE, R BL 16 AND 8 INCHES AFT OF FLT DECK THRESHOLD. REMOVED CORROSION FROM FWD LAV BULKHEAD. FABRICATED AND INSTALLED NEW AN GLE PER SRM 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999021900680 19990219 00680 NM 1999 2 19 EISA98302 1 19981208 A 5312 BULKHEAD BOEING 727 727277 138408S NM BS 178 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND FS 178 BULKHEAD CRACKED, JUST BELOW RADAR ANTENNA. REMOVED DA MAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER B727 SB 53-0213. (M) 2 L 7 3 4F RT A3WE 1999021900681 19990219 00681 NM 1999 2 19 EISA98286 1 19981208 A 5311 FRAME BOEING 727 727277 138408S NM BS 580 CRACKED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD, FOUND CRACK IN FRAME AT FS 580 AND STRINGER 7R. FABRICATED AND INST ALLED DOUBLER PER SRM 53-10-4. (M) 2 L 7 3 4F RT A3WE 1999021900682 19990219 00682 NM 1999 2 19 EISA98306 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 1070 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP CARD NR C53-224-01 REVEALED CORROSION ON UPPER CHORD OF FS 1070 FLOORBEAM RBL 55. REMOVED DAMAGED SECTION OF UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999021900683 19990219 00683 NM 1999 2 19 EISA98300 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 1110 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-01 REVEALED TWO MAIN AREAS OF CORROSION ON UPPER CHORD OF FS 1110 FLOORB EAM. REMOVED DAMAGED AREAS. FABRICATED AND INSTALLED REPAIRS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999021900684 19990219 00684 NM 1999 2 19 EISA98299 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 1030 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP WORK CARD C53-224-01 REVEALED CORROSION ON IN TWO AREAS OF UPPER CHORD OF FLOORBEAM FS 103 0. REMOVED DAMAGED AREAS FABRICATED AND INSTALLED REPAIR PARTS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999021900699 19990219 00699 WP 1999 2 19 ORJA9915 1 19981114 A 3350 60030451 BATTERY PACK DOUG DC9 DC983 3022083 WP ROW 8-11 DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 OKC - EMERGENCY LIGHTS INOPERATIVE SEATS 8-11 AND FORWARD EXIT ID. REMOVED AND REPLACED BATTERY PACK IAW MD82-BR2013-R- 820A, TESTED EMERGENCY LIGHTS AT SEATS 8-11 AND FORWARD RIGHT OVERWING EXIT ID IAW BRUCE UND MANUAL 400-082. NO DEFECTS NOTED. (M) 2 L 7 2 4F RT A6WE 1999021900709 19990219 00709 NM 1999 2 19 AALA990061 1 19981230 A 5330 SKIN BOEING 727 727223 1384074 NM BS 830-850 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 701AA 22459 TUL - FOUND CORROSION ON SKIN ABOVE RIGHT PRIMARY HEAT EXCHANGER (PLENUM) FROM STATION 830 TO STRINGER 850. INSTALLED R EPAIRS PER SRM 57-30-3 FIG 8 AND FIG 9. (M) 2 L 7 3 4F A3WE 1999021900724 19990219 00724 EU 1999 2 19 SIMA983623 1 19981228 A 5330 S5317150120305 SKIN AEROSP ATR42 ATR42300 8680920 EU FRAME 2-3 PUNCTURED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 314AM 314 FOUND 8 INCH SKIN PUNCTURE ON RIGHT SIDE OF NOSE SECTION BETWEEN FRAMES 2 AND 3. REPAIRED SKIN. AIRCRAFT RETURNED TO S ERVICE. (M) 2 H 7 2 4T RT A53EU 1999021900725 19990219 00725 EU 1999 2 19 SIMA983622 1 19981228 A 5330 S5317210121805 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 47AE 047 SAW - DENTS IN FUSELAGE, ONE BETWEEN FRAMES 2 AND 3 AT STRINGER 21R, ONE BETWEEN FRAMES 6 AND 7 AND STRINGER 20 AND 21R, ONE BETWEEN FRAMES 19 AND 20 AND STRINGER 15 AND 16R, AND ONE BETWEEN FRAMES 21 AND 22 AND STRINGER 20 AND 21R. REPAIR ED DENTS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999021900729 19990219 00729 NE 1999 2 19 99ZZZM139 2 19981208 A 7200 ENGINE BOEING 727 72777C 1380420 NM PWA JT8 JT8D7B 52053 NE NR 3 DAMAGED A RYNA K NONE C F.O.D. IN INSP/MAINT 1 CE 07 526PC 20370 657223 FLT 614 - BUF - NR 3 ENGINE HAS FOREIGN OBJECT DAMAGE. REMOVED AND REPLACED NR 3 ENGINE. DUE TO BAD WEATHER AIRCRAFT C OULD NOT FERRY TO IND UNTIL 1/17/99, WHERE MAINTENANCE WAS PERFORMED. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999021900732 19990219 00732 EU 1999 2 19 99ZZZM142 1 19981216 A 2560 NAS561C38 PIN AIRBUS 320 A320231 3930325 EU SLIDE BROKEN A RYNA O OTHER P NO WARNING INDICATION TX TAXI/GRND HDL 1 CE 07 GCRPH 424 FLT 8160 - IN SFO - JUST PRIOR TO PUSHBACK LEFT OVERWING EXIT SLIDE WENT FROM ARMED (SLIDE) TO DISARMED (NO INDICATION). FOUND BROKEN ROLL PIN ON ARMING LEVER, REPLACED PIN. (M) 2 L 7 2 4F RT A28NM 1999021900733 19990219 00733 NM 1999 2 19 99ZZZM143 1 19981230 A 5230 252300914 VALVE BOEING 727 72721 1384003 NM CARGO DOOR LEAKING A RYNA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 07 359QS 19007 FLT 631 - IND-PHX - AT FL280 CRUISE CABIN STARTED CLIMBING RAPIDLY TRIED TO CONTROL AND REQUEST DESCENT TO FL200 MAIN CA RGO DOOR LIGHT CAME ON. COMPLETED IRREGULAR CHECK LIST STILL COULD NOT CONTROL CABIN, TURNED BACK FOR ICT, CONTINUED TO DESCEND TO 10,000 FT. HAD TO DUMP FUEL TO MAKE LANDING WEIGHT AND LANDED AT ICT. REMOVED AND REPLACED DOOR OPEN SEQUE NCE VALVE. (M) 2 L 7 3 4F A3WE 1999021900737 19990219 00737 EA 1999 2 19 VTZA98368 1 19981216 A 5610 NP1393222 WINDOW CNDAIR CL600 CL6002B19 EA COCKPIT BROKEN A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 629BR 7251 FLT 6655 - ORD-FAR - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO F/O'S SIDE WINDOW SHATTERED. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER PROBLEMS. AIRCRAFT WAS FERRIED TO IAD WHERE MAINTENANCE INSPECTED AND REMOVED AND REPLA CED WINDOW, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999022400001 19990224 00001 EU 1999 2 24 C2XA99IA018 1 19980211 A 5320 S53971309206 BRACKET AEROSP ATR42 ATR42500 EU FUSELAGE CRACKED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 19446 504 IAH - DURING C-CHECK INSPECTION, THE CENTER SUPPORT BRACKET FOR PANEL 193CL WAS FOUND TO BE CRACKED AT THE LOWER END. M AINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR IAW ATR42-500 SRM 51-70-00 AND THE AIRCRAFT WAS APPROVE D FOR RETURN TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999022400004 19990224 00004 EU 1999 2 24 QXEA9900120 1 19981212 A 5280 HINGE FOKKER F28 F28MK4000 4990810 EU RT MLG DOOR WORN A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - RIGHT-HAND MAIN LANDING GEAR WHEEL BY DOOR HINGE HAS WORN STEPWEAR INSIDE WHEEL BAY OPENING AT BOTH FORWARD AND AF T ENDS. REPAIRED IAW FOKKER SRM 51-01-01 AND SRM 53-01-01, PAGE 6 PARAGRAPH B4. 2 L 7 2 4F RT A20EU 1999022400005 19990224 00005 EU 1999 2 24 QXEA9900121 1 19981216 A 5312 BULKHEAD BEAM FOKKER F28 F28MK4000 4990810 EU AFT PRESS BLKHD CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - REAR PRESSURE BULKHEAD HORIZONTAL BEAM II HAS APPROXIMATELY .5 CRACK IN RADIUS OF WEB AT END OF BEAM BL 1050R. RE PAIRED IAW FOKKER SRM 53-02-18, PAGE 33-38 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999022400007 19990224 00007 EU 1999 2 24 VTZA98357 1 19981203 A 2930 BULB BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 480UE 894 IAD/ORF - FLT 6383 - DURING CLIMB AT 1640 HOURS ON 12-3-98, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT HYDRAULIC LP COCK WILL NOT INDICATE OPEN. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RE-LAMPED H YDRAULIC LP COCK INDICATOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A56EU 1999022600046 19990226 00046 NE 1999 2 26 99ZZZX681 2 19980730 A 7320 FUEL CONTROL BENDIX BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE NR 1 ENGINE MALFUNCTIONED A HEEA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 SW 03 1079U 7139 397 B14538 31122 CPPS62276 WHILE IN CRUISE FLIGHT, NR 1 ENGINE TORQUE WENT LOW WHICH RESULTED IN A 20 PERCENT TORQUE SPLIT BETWEEN NR 1 AND NR 2 EN GINES. PILOT RETURNED TO BASE AND LANDED WITHOUT INCIDENT. TROUBLESHOOTING BY MAINTENANCE REVEALED DEFECTIVE FUEL CONT ROL. REPLACED SAME. REF: P & W IPC, 72-00-10, FIGURE 1, ITEM 101. 1 G 7 1 4U 4 U H4SW E22EA 1999022600047 19990226 00047 EU 1999 2 26 99ZZZX682 1 19981105 A 2435 23032042 GENERATOR SNIAS 350 AS350B1 8680811 EU STARTER/GEN FAILED H A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION NR NOT REPORTED 1 NM 02 13HF 764 858M 2267 GENERATOR FAILED DURING RETURN TRIP HOME. A PRECAUTIONARY LANDING WAS MADE. REPLACED STARTER/GENERATOR AND FINISHED FL IGHT. THE CAUSE OF THE GENERATOR FAILURE HAS NOT BEEN DETERMINED AS YET. 1 G 7 1 3U H9EU 1999022600048 19990226 00048 EU 1999 2 26 99ZZZX683 1 19980420 A 6510 22208BC060012L BOLT SNIAS 350 AS350B1 8680811 EU TAIL ROTOR WORN D A K NONE O OTHER IN INSP/MAINT 1 NM 02 13HF 5334 2267 DURING AN ANNUAL INSPECTION, DISCOVERED THE NR 5 TAIL ROTOR DRIVE SHAFT BEARING SUPPORT BLOCK WAS LOOSE AND THE BOLT WAS WORN ON THE RT POSITION. SINCE THIS IS WHERE THE ACCELEROMETER IS MOUNTED DURING SHORT SHAFT BALANCING, IT COULD BE TH AT IT WAS NOT TORQUED PROPERLY AFTER THE LAST BALANCE OPERATION. SUBMITTER SUGGESTED TO CHECK EACH 100-HOUR. 1 G 7 1 3U H9EU 1999022600049 19990226 00049 SW 1999 2 26 99ZZZX684 1 19980913 A 5610 205030285001 WINDOW 205030285001 BELL 212 212 1181420 SW COCKPIT BROKEN A HEEA O OTHER D INFLIGHT SEPARATION CR CRUISE 1 SW 03 1082G 31109 DURING CRUISE FLIGHT, TOP THIRD OF WINDOW BROKE OUT AND DEPARTED AIRCRAFT. NO OTHER DAMAGE OCCURRED. CAUSE UNKNOWN. M AINTENANCE REPLACED WINDOW. REF: 212 IPC, CHAPTER 52-99-00, PAGE 46, ITEM 20, FIGURE 52-11. 1 G 7 1 4U H4SW 1999022600053 19990226 00053 EU 1999 2 26 HCMA0000229 1 19981208 A 6410 350A33215300 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR DAMAGED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 197BH 831 2666 BEARING IS DISTORTED, OUT OF LIMITS. (X) 1 G 7 1 3U H9EU 1999022600054 19990226 00054 EU 1999 2 26 HCMA0000228 1 19981028 A 6720 350A33214501 ROD SNIAS 350 AS350B2 8680813 EU T/R PITCH LINK WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 196BH 1451 3036 ROD, PITCH CONTROL, WORN BEYOND LIMITS. 1 G 7 1 3U H9EU 1999022600055 19990226 00055 EU 1999 2 26 HCMA0000226 1 19981107 A 6410 350133215300 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 972BH 548 2804 BEARINGS WORN BEYOND LIMITS AND TORN. (X) 1 G 7 1 3U H9EU 1999022600056 19990226 00056 EU 1999 2 26 HCMA0000225 1 19981014 A 2460 9550168600 HARNESS SNIAS 350 AS350B 8680801 EU DC SYSTEM FRAYED A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 752BH 206 2510 CABLE IS FRAYED BEYOND LIMITS. (X) 1 G 7 1 3U H9EU 1999022600057 19990226 00057 EU 1999 2 26 HCMA0000224 1 19981106 A 6410 355A09103601 BEARING SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 422B 471 2391 BEARING WORN BEYOND LIMITS. 1 G 7 1 3U NC H9EU 1999022600058 19990226 00058 EU 1999 2 26 HCMA0000223 1 19981106 A 6520 350A33215300 HINGE SNIAS 350 AS350BA 8680817 EU TAIL ROTOR WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 422B 681 2391 HINGE IS WORN BEYOND LIMITS. (X) 1 G 7 1 3U NC H9EU 1999022600060 19990226 00060 GL 1999 2 26 99ZZZX689 2 19981121 A 7412 103832251 EXCITER BELL 222 222U 1182140 SW ALLSN 250C 250C47B GL ENGINE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 404EM 181 98106315 47514 EXCITER INOPERATIVE. ENGINE FAILED TO START. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H9SW E1GL 1999022600061 19990226 00061 EU 1999 2 26 99ZZZX690 1 19981215 A 2822 9A2045 PUMP CARTRIDGE UROCOP EC135 EC135P1 8680990 EU FUEL SYSTEM INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 119 341 EC1350054 PUMP CARTRIDGE INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U O H88EU 1999022600062 19990226 00062 NE 1999 2 26 99ZZZX691 2 19980818 A 7412 103832251 EXCITER BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 596 97198637 7127 EXCITER INOPERATIVE. IGNITERS WILL NOT SPARK (NOT VERY EXCITABLE). REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999022600063 19990226 00063 NE 1999 2 26 99ZZZX692 2 19981215 A 7310 L717M1009801 TUBE UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE FUEL CONTROL CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 119 EC1350054 TUBE CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 1999022600064 19990226 00064 NE 1999 2 26 99ZZZX693 2 19981206 A 7250 L621M1006103 SEAL UROCOP EC135 EC135P1 8680990 EU PWA PW206 PW206B 0 NE ENGINE WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 135SJ 110 EC1350054 SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U O H88EU E42NE 1999022600080 19990226 00080 GL 1999 2 26 99ZZZX697 1 19981124 A 3220 2032200016 FORK DIAMON DA20 DA20A1 GL RT NLG BROKEN A HR9A O OTHER O OTHER LD LANDING 1 EA 21 87HA 1315 10086 ON LANDING, AIRCRAFT'S NOSE FORK BROKE. UPON INSPECTION AFTER ACCIDENT, IT WAS DETERMINED THE PART CRACKED AT THE SMALL EST SURFACE AREA. IT IS POSSIBLE THE AREA HAD CRACKED PRIOR TO BREAKING. BROKEN NOSE FORK CAUSED PROPELLER STRIKE. 1 L 7 1 3O NT TA4CH 1999022600081 19990226 00081 GL 1999 2 26 99ZZZX698 1 19981124 A 3220 2032200015 FORK DIAMON DA20 DA20A1 GL LT NLG BROKEN A HR9A O OTHER O OTHER LD LANDING 1 EA 21 87HA 1315 10086 ON LANDING, AIRCRAFT'S NOSE FORK BROKE. UPON INSPECTION AFTER ACCIDENT, IT WAS DETERMINED THE PART CRACKED AT THE SMALL EST SURFACE AREA. IT IS POSSIBLE THE AREA HAD CRACKED PRIOR TO BREAKING. BROKEN NOSE FORK CAUSED PROPELLER STRIKE. 1 L 7 1 3O NT TA4CH 1999022600205 19990226 00205 NE 1999 2 26 CA980714024 2 19980612 A 7313 0301007710 FUEL INJECTOR 0292005060 SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE ENGINE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 4404 (CAN) PILOT REPORTED DELAYED START. ON NEXT START, FUEL BUBBLES WERE SEEN AT THE FUEL INJECTOR UNION. FURTHER INSPECTI ON SHOWED A CRACK IN TUBE FLARE AT THE UNION. PREVIOUS 100 HOUR INSPECTION SHOWED NO SIGN OF FUEL LEAKS AND NO MAINTENA NCE WAS CARRIED OUT ON THE INJECTORS. PART TC: 8,136. 1 G 7 1 3U 3 U NC H9EU E19EU 1999022600318 19990226 00318 NM 1999 2 26 MASA98214 1 19981130 A 2120 AIR DISTRIBUTION DHAV DHC8 DHC8202 2809007 NM COCKPIT ODOR A MASA K NONE B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 SW 07 437YV 437 PHX/DRO - FLT 6255 - AIRCRAFT WAS 15 MILES OUT FROM DRO WHEN THE CREW SMELLED AN ELECTRICAL SMELL IN THE COCKPIT. AIRCR AFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, AND DEFERRED THE RECIRCULATION FAN PER MEL 21-9. AIRCRAFT WAS RE TURNED TO SERVICE. IN SUBSEQUENT MAINTENANCE, FANS WERE INSPECTED, NO DISCREPANCIES NOTED. SEE MRR MASA98215 FOR FINAL FIX. (X) 2 H 7 2 4T RT A13NM 1999022600344 19990226 00344 NM 1999 2 26 EISA98320 1 19981218 A 2420 CONTROL PANEL BOEING 727 727223 1384074 NM NR 1 GENERATOR LOOSE A EISA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 313NE 19702 GENERATOR BREAKER AND FIELD LIGHT NR 1 ILLUMINATED AT GEAR RETRACTION. DIFFERENTIAL LIGHT ILLUMINATED RAN ABNORMAL PROC EDURES. GENERATOR WOULD NOT RESET. RAN NORMAL PROCEDURES. RETURN TO DEPARTURE (LAX). FOUND NR 1 GENERATOR CONTROL PA NEL LOOSE. SWAPPED NR 1 AND NR 2 GENERATOR CONTROL PANELS. OPS CHECK GOOD PER MM 24-20-0. (X) 2 L 7 3 4F A3WE 1999022600348 19990226 00348 NM 1999 2 26 ASAA9810127 1 19981209 A 3350 6104781 BATTERY GRIMES BOEING 737 737210C 1384459 NM ROW 16 DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 743AS 21821 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGH TS OPERATED NORMALLY. (X) 2 L 7 2 4F A16WE 1999022600354 19990226 00354 NM 1999 2 26 ASAA9840113 1 19981210 A 3350 1060091102 LIGHT GRIMES BOEING 737 737490 1384715 NM R2 DOOR INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 768AS 27082 SEA - DURING MAINTENANCE CHECK THE R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REPLACED LIGHT ASSEMBLY AND LIGHT OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 1999022600362 19990226 00362 WP 1999 2 26 ASAA9880260 1 19981210 A 3397 WIRE DOUG DC9 DC983 3022083 WP CATWALK LOOSE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPAIRED LOOS E WIRE TO LIGHT ASSEMBLY L2-638 AND REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. REF: OPER CONTROL NR 99ZZZX742. ( X) 2 L 7 2 4F RT A6WE 1999022600363 19990226 00363 WP 1999 2 26 99ZZZX742 1 19981210 A 3350 60030451 POWER SUPPLY MIDLANDROSS DOUG DC9 DC983 3022083 WP CABIN INOPERATIVE A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 944AS 53019 SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE CATWALK AREA WERE FOUND INOPERATIVE. REPAIRED LOOS E WIRE TO LIGHT ASSEMBLY L2-638 AND REPLACED THE POWER SUPPLY AND OPERATED NORMALLY. REF: OPER CONTROL NR ASAA9880260. 2 L 7 2 4F RT A6WE 1999022600413 19990226 00413 WP 1999 2 26 9811481141 1 19981217 A 5311 FRAME DOUG DC10 DC1040 3023508 WP BS 1921 CRACKED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 141US 46750 DURING M-CHECK, FOUND FUSELAGE FRAME CRACKED AT FS 1921 AT ATTACH TO LEFT CARGO TRACK. REPAIRED PER EA 11-162429. 2 L 7 3 4F A22WE 1999022600414 19990226 00414 NM 1999 2 26 9811492716 1 19981214 A 5314 KEEL BEAM BOEING 727 7272S7 138407Z NM BS 950-968 CORRODED A NWAA K NONE O OTHER IN INSP/MAINT 1 GL 01 719RC 22491 DURING M-CHECK, FOUND CORROSION ON OUTBOARD FLANGE OF RIGHT KEEL BEAM FS 950D+7 AND 950D+18. REPAIRED PER EA 27-162850. 2 L 7 3 4F A3WE 1999022600487 19990226 00487 WP 1999 2 26 ORJA9939 1 19981105 A 3397 00105606003 WIRE DOUG DC9 DC983 3022083 WP CABIN DAMAGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 878RA 53184 OKC - AFT TAIL EMERGENCY ESCAPE PATH MARKING LIGHT INOPERATIVE. REPAIRED WIRES AT LIGHT ASSY IAW MD80 MM 20-50-01. OPS CHECK GOOD IAW MD80 MM 33-53-00. (X) 2 L 7 2 4F RT A6WE 1999022600518 19990226 00518 WP 1999 2 26 EIAA980267 1 19981002 A 5711 SPAR DOUG DC9 DC932F 3022067 WP WS 267 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, LEFT WING AFT SPAR UPPER CHORD XRS 267 AT NR 3 FLAP HINGE HAS A CRACK. REPAIRED PER EA DC9-57-135 AND SERVICE BULLETIN 57-179 REV 1, DRWG JO60272 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600519 19990226 00519 WP 1999 2 26 EIAA980268 1 19981002 A 5711 SPAR DOUG DC9 DC932F 3022067 WP RT WING CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RIGHT WING AFT SPAR UPPER CHORD AT NR 3 FLAP HINGE HAS A CRACK. REPAIRED PER EA DC9-57-135 AND SE RVICE BULLETIN 57-179 REV 1, DRWG J060272 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600520 19990226 00520 WP 1999 2 26 GAIA9905 1 19980118 A 3230 39140165505 BUNGEE DOUG DC9 DC915F 3022037 WP RT MLG LEAKING A GAIA O OTHER K FLUID LOSS AP APPROACH 1 SW 07 563PC 47055 KHA - FLT 1563 - PIA-ELP - ON APPROACH TO ELP, THE FLIGHT CREW NOTICED THE LANDING GEAR WAS SLOW TO EXTEND. THE CREW EL ECTED TO CYCLE THE GEAR AND NOTED THE SAME RESULTS. A UNEVENTFUL LANDING WAS MADE. THE AIRCRAFT WAS FERRIED GEAR DOWN TO DFW INVESTIGATION FOUND THE RIGHT MAIN LANDING GEAR BUNGEE CYLINDER LEAKING. THE BUNGEE CYLINDER WAS REPLACED AND TH E LANDING GEAR WAS OPS CHECKED SEVERAL TIME WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1999022600532 19990226 00532 EU 1999 2 26 SIMA983491 1 19981215 A 5311 S5337240822801 FRAME AEROSP ATR42 ATR42300 8680920 EU BS 32 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 424MQ 045 SAW - DURING CPCP-2 INSPECTION, FOUND FRAME 32 CORRODED BETWEEN STRINGERS 21 LEFT AND 21 RIGHT. REPAIRED THE FRAME. AI RCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999022600533 19990226 00533 EU 1999 2 26 SIMA983492 1 19981215 A 5313 S5367140022802 STRINGER AEROSP ATR42 ATR42300 8680920 EU BS 32/33 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 424MQ 045 SAW - DURING CPCP-2 INSPECTION, FOUND STRINGER 21 LEFT CORRODED BETWEEN FRAME 32 AND 33. REPAIRED THE STRINGER. AIRCRA FT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999022600560 19990226 00560 WP 1999 2 26 EIAA980284 1 19981002 A 5320 WEB DOUG DC9 DC932F 3022067 WP BS 218-969 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN CUSP WEBS FROM FS 218, SEVERAL LOCATIONS WERE FOUND WITH VARIOUS DISCREPANCIES, CRACKS, CORROSION, DENTED, NRC FS 218 AT RBL 44 V105, FS 218-235 LT W462, FS 237-255 RBL 44 V106, FS 237 RBL 60 W399, FS 285-31 3 RT W318, FS 313 LT W365, FS 313-354 RT W319, FS 515 RBL 56 W465, FS 579-598 RT W358, FS 611 RT W151, FS 598-617 RT W35 7, FS 658-699 RT W376, FS 689 RT W403, FS 690-699 LBL 54 W404, FS 718-986 LT W322, FS 740 LBL 53 W141, FS 756 LBL 58 W14 3, FS 832 RBL 49 Y083, FS 832-897 RT 7048, FS 870-899 LT 7049, FS 935-965 RT Y022, FS 945-969 LT 7025. 22 TOTAL DISCREP ANCIES ON THIS ITEM. REPAIRED PER SRM 53-11-2, 53-01 FIG 4, 53-11-10B. (M) 2 L 7 2 4F A6WE 1999022600561 19990226 00561 WP 1999 2 26 EIAA980291 1 19981002 A 5320 PAN DOUG DC9 DC932F 3022067 WP BS 341 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, LOWER CARGO DOOR OUTER PAN FS 341 WAS FOUND DAMAGED. NRC H051. REPAIRED PER SRM 52-05 FIG 50. ( M) 2 L 7 2 4F A6WE 1999022600562 19990226 00562 WP 1999 2 26 EIAA980293 1 19981002 A 5320 WEB DOUG DC9 DC932F 3022067 WP BS 515 MISREPAIRED A EIAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN CABIN CUSP WEB AT FS 515 LBL 56 WAS FOUND TO HAVE AN IMPROPER REPAIR INSTALLED PER SRM. REPA IRED PER SRM 53-01 FIG 4. (M) 2 L 7 2 4F A6WE 1999022600563 19990226 00563 WP 1999 2 26 EIAA980304 1 19981002 A 5330 5910163181 SKIN DOUG DC9 DC932F 3022067 WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, AFT PRESSURE BULKHEAD SKIN HAS DAMAGE AND CORROSION, THESE ITEMS DON'T GIVE GOOD DESCRIPTIONS OTHE R THAN BEING IDENTIFIED AS PSE 53.09.025. NRC L045, L106, L107. REPAIRED PER EA DC9-53-210, BOEING MESSAGE MISC-C743/P PS AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600564 19990226 00564 WP 1999 2 26 99ZZZM146 1 19981002 A 5320 5910163129 DOUBLER DOUG DC9 DC932F 3022067 WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, AFT PRESSURE BULKHEAD SKIN HAS DAMAGE AND CORROSION, THESE ITEMS DON'T GIVE GOOD DESCRIPTIONS OTHE R THAN BEING IDENTIFIED AS PSE 53.09.025. NRC L045, L106, L107. REPAIRED PER EA DC9-53-210, BOEING MESSAGE MISC-C743/P PS AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600565 19990226 00565 WP 1999 2 26 99ZZZM147 1 19981002 A 5320 5910163133 DOUBLER DOUG DC9 DC932F 3022067 WP FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 47220 PHX - DURING C-CHECK, AFT PRESSURE BULKHEAD SKIN HAS DAMAGE AND CORROSION, THESE ITEMS DON'T GIVE GOOD DESCRIPTIONS OTHE R THAN BEING IDENTIFIED AS PSE 53.09.025. NRC L045, L106, L107. REPAIRED PER EA DC9-53-210, BOEING MESSAGE MISC-C743/P PS AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600566 19990226 00566 WP 1999 2 26 EIAA980309 1 19981002 A 5531 59113847 SPAR DOUG DC9 DC932F 3022067 WP VERT STAB CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, VERTICAL STABILIZER REAR SPAR LEFT AND RIGHT AFT CHORD HAS CORROSION FROM ZRS .5 TO ZRS154. OUT O F LIMITS AT ZRS 112. NRC N062, N063. REPAIRED PER EA DC9-55-013 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600567 19990226 00567 WP 1999 2 26 EIAA980272 1 19981002 A 5320 DOUBLER DOUG DC9 DC932F 3022067 WP BS 718 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RIGHT MAIN GEAR WHEEL WELL, FS 718 AT RBL 37, CEILING DOUBLER HAS CORROSION. REPAIRED PR SRM 53-0 1, AND EA DC9-53-186 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600568 19990226 00568 WP 1999 2 26 EIAA980273 1 19981002 A 5711 SPAR DOUG DC9 DC932F 3022067 WP WS 164 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, RIGHT WING AFT SPAR LOWER CHORD AT XRS 164 NR 2 FLAP HINGE ATTACH AREA A CRACK WAS FOUND. REPAIRE D PER DRAWING J06027, EA DC9-57-136 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600570 19990226 00570 NM 1999 2 26 AALA982207 1 19981211 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STRINGER END CRACKED FROM FAST HOLE 720B PLUS INCHES. INSTALLED STRINGER SPLICE REPAIR PER SRM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999022600571 19990226 00571 NM 1999 2 26 AALA982206 1 19981211 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STRINGER 15L CRACKED AT FS 720B PLUS 15 INCHES. REPAIRED STRINGER 15L AT FS 720C PLUS 15 INCHES PER SRM 53- 10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999022600572 19990226 00572 NM 1999 2 26 AALA982205 1 19981211 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CORROSION ON FLOORBEAM AT FS 380 RBL 20 TO RBL 45. CUT OUT CORRODED PORTION OF UPPER AREA OF FLOORBEAM AND REPAIRED PER FLOORBEAM REPAIR SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1999022600573 19990226 00573 NM 1999 2 26 AALA982204 1 19981211 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CORROSION ON STRINGER 29 LT STATION 950C - 950E. CORROSION ON STRINGER 29 RT STATION 950F - 970. REMOVED C ORROSION AND INSTALLED REPAIRS PER ECO 11697, DATED 11-12-98. (M) 2 L 7 3 4F A3WE 1999022600574 19990226 00574 NM 1999 2 26 AALA982203 1 19981211 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 720 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STRINGER 15R CRACKED AT STATION 720B PLUS 4 INCH. CUT OFF CRACKED PORTION OF STRINGER AND INSTALLED STRINGE R AND SPLICE PER SRM 53-10-3 PAGE 3-4B. (M) 2 L 7 3 4F A3WE 1999022600575 19990226 00575 NM 1999 2 26 AALA982202 1 19981209 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STATION 950C FRAME HAS DENT WITH BULGE AT FORWARD WEB ABOVE STRINGER 25L. INSTALLED DOUBLER REPAIR PER SRM 53-00-00-01. (M) 2 L 7 3 4F A3WE 1999022600576 19990226 00576 NM 1999 2 26 AALA982201 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1070 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STATION 1070 UPPER FLANGE BENT AND WEB CREASED STRINGER 25R. CUTOUT DAMAGE AND INSTALLED DOUBLER PER SRM 53 -10-4 PAGE 3-5 FIG 1 7075 T-6 .080, 2.5 INCH BY 17 INCH L 19 .1875 INCH HI-LOCKS UPPER FLANGE, 16 .25 AND 15 .1875 HI-L OCKS IN WEB. (M) 2 L 7 3 4F A3WE 1999022600577 19990226 00577 NM 1999 2 26 AALA982200 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 930 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CRACK IN FRAME AT FS 930 ABOVE STRINGER 14R. INSTALLED Z-FRAME REPAIR AT FS 930 STRINGER 14R IAW 53-10-4 FI G 1. (M) 2 L 7 3 4F A3WE 1999022600578 19990226 00578 NM 1999 2 26 AALA982199 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1050 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 1050 UPPER FLANGE BENT AND WEB IS DEFORMED AT STRINGER 24-25L. CUT OUT DAMAGE SECTION AND INSTALLED DOUBL ER PER SRM 53-10-4 PG 3-5. (M) 2 L 7 3 4F A3WE 1999022600579 19990226 00579 NM 1999 2 26 AALA982198 1 19981209 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 380 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CORROSION ON FLOORBEAM STATION 380 RBL 20 TO RBL 45. CUT OUT UPPER PORTION OF FLOORBEAM TO REMOVE CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-10-8. (M) 2 L 7 3 4F A3WE 1999022600580 19990226 00580 NM 1999 2 26 AALA982197 1 19981202 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND STRINGER 29L HAS CORROSION EXTENDING FROM 7 FASTENERS IN OUTBOARD FLANGE AND IN PREVIOUSLY REWORKED AREA. R EPAIRED STRINGER PER ESO 11697, DATED 11/2/98. (M) 2 L 7 3 4F A3WE 1999022600581 19990226 00581 NM 1999 2 26 AALA982196 1 19981211 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 950-970 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STRINGER 29R HAS CORROSION ON OUTBOARD FLANGE AND EXTENDING FROM UNDER SEALANT STATION 950 E TO 950F. BLENDED OUT CORROSION, TREATED, PRIMED AND INSTALLED DOUBLERS PER ESO 11697 DATED 11-12-98. (M) 2 L 7 3 4F A3WE 1999022600582 19990226 00582 NM 1999 2 26 AALA982195 1 19981203 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 490-500 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 490-500 STRINGER 28R CORRODED INSIDE. REMOVED DAMAGED SECTION OF STRINGER. INSTALLED SPLICE REPAIR PER S RM 53-10-3 FIG 1. (M) 2 L 7 3 4F A3WE 1999022600583 19990226 00583 NM 1999 2 26 AALA982194 1 19981211 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 400 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - TOP OF FLOORBEAM CORRODED STATION 400 RBL 3 TO RBL 4. CUT OUT UPPER PORTION OF FLOORBEAM TO REMOVED CORROSION AND INSTALLED FLOORBEAM DOUBLER REPAIR PER SRM 53-10-8 PAGE 9 A AND B. (M) 2 L 7 3 4F A3WE 1999022600584 19990226 00584 NM 1999 2 26 AALA982193 1 19981211 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 680-700 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CORROSION AT STRINGER 26R BETWEEN STATION 680-700. REMOVED CORRODED SECTION OF STRINGER. INSTALLED SPLICE REPAIR IAW SRM 53-10-3. (M) 2 L 7 3 4F A3WE 1999022600585 19990226 00585 NM 1999 2 26 AALA982192 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 580 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 580 FRAME DENTED BETWEEN STRINGER 22L-25L. REPAIRED FRAME PER SRM 51-40-3 AND D224655 11-18-98 AARD 53-10 -7-3. CUT OUT DAMAGED AREA 4 INCH BY 3 INCH. INSTALLED .050 7075-T6 DOUBLER WITH MS204720 MS 204260, RIVETS (FLANGE) 4 EACH FASTENERS BOTH SIDES DAMAGE, RIVETS (WEB). (M) 2 L 7 3 4F A3WE 1999022600586 19990226 00586 NM 1999 2 26 AALA982191 1 19981205 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 520 BELL FRAME DENTED BETWEEN STRINGER 23L AND 25L. CUT OUT DAMAGE AT TWO LOCATIONS. 1 INCH BY 4 INCH AT STRINGER 23L, 1 INCH BY 3 INCH AT STRINGER 25L. EACH AREA HAD SEPARATE DOUBLERS INSTALLED PER SRM 51-40-3 USING 7075-T 6 .050 THICK DOUBLER MATERIAL. (M) 2 L 7 3 4F A3WE 1999022600587 19990226 00587 NM 1999 2 26 AALA982190 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 500 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 500 BELL FRAME DENTED STRINGER 23R-25R. CUT OUT DAMAGE. INSTALLED .050 7075-T6 DOUBLER 18 INCH PER SRM 5 1-40-3 AND AARD 53-10-7-3. 36 .1875 MS20470D RIVETS, 4 .25 INCH MS 20470D RIVETS (4 RIVETS EACH SIDE DAMAGE) 3 ROWS. ( M) 2 L 7 3 4F A3WE 1999022600588 19990226 00588 NM 1999 2 26 AALA982189 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 805 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CRACK IN ANGLE OF FRAME TO STRINGER ATTACH POINT STATION 805, STRINGER 14R. CUT OUT DAMAGED AREA AND INSTAL LED DOUBLER PER SRM 51-40-3 PAGE 3, 3A. (M) 2 L 7 3 4F A3WE 1999022600589 19990226 00589 NM 1999 2 26 AALA982188 1 19981203 A 5311 FRAME BOEING 727 727223 1384074 NM BS 540 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 540 BELL FRAME HAS DENT BETWEEN STRINGER 24L AND 25L. REMOVED DAMAGED AREA. INSTALLED .1875 RIVET PER ES O 11697, DATED 12-3-98. (M) 2 L 7 3 4F A3WE 1999022600590 19990226 00590 NM 1999 2 26 AALA982187 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 680 BELL FRAME DENTED BETWEEN STRINGER 22R AND 21R. INSTALLED DOUBLER PER SRM 51-40-3 FIG 3, .050 7075-T 6 3 ROWS OF MS20470D RIVETS (11 EACH) AND ONE ROW .1875 OF MS20426 D RIVETS (6 EACH) .1875, DOUBLER 8 INCHES LONG. (M) 2 L 7 3 4F A3WE 1999022600591 19990226 00591 NM 1999 2 26 AALA982186 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 660 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 660 BELL FRAME DENTED BETWEEN STRINGER 22R-25R. CUTOUT DAMAGE, INSTALLED DOUBLER PER SRM 51-40-3 PAGE 3 . 050 7075-T6 17 INCH BY 2.5 INCH, 24 .1875 MS 20470D RIVETS, 15 MS20426D RIVETS .1875 INCH, 1 MS20470D .25 INCH RIVET. ( M) 2 L 7 3 4F A3WE 1999022600592 19990226 00592 NM 1999 2 26 AALA982185 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 620 BELL FRAME DENTED BETWEEN STRINGER 23L-25L. CUT OUT DAMAGE. INSTALLED DOUBLER PER SRM 51-40-3 PAGE 3 , .050 7075-T6 21 MS20426D .1875 RIVETS, 40 MS20470D .1875 RIVETS, 5 MS20470D .25 RIVETS, 4 FASTENERS PAST DAMAGE, 2 ROW S IN WEB. (M) 2 L 7 3 4F A3WE 1999022600593 19990226 00593 NM 1999 2 26 AALA982184 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 700 BELL FRAME DENTED BETWEEN STRINGER 25R AND 22R. DYE CHECKED, NO CRACKS FOUND. INSTALLED DOUBLER 30 I NCH LONG .050 7075-T6 USING BAC B30FM HI-LOCKS 3 ROWS, AND NAS 8603-2 FASTENERS ONE ROW PER SRM 54-10-3 AND 53-10-4. (M ) 2 L 7 3 4F A3WE 1999022600594 19990226 00594 NM 1999 2 26 AALA982183 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 804.95 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - BELL FRAME CRACKED AT FS 804.95 STRINGER 14L. REPAIRED BELL FRAME IAW SRM 51-40-3 PAGE 1-6. (M) 2 L 7 3 4F A3WE 1999022600595 19990226 00595 NM 1999 2 26 AALA982182 1 19981201 A 5311 FRAME BOEING 727 727223 1384074 NM BS 560 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 560 BELT FRAME DENTED BETWEEN STRINGER 23L AND 25L. INSTALLED BELT FRAME REPAIR PER SRM 51-40-3 USING 54, .1875 INCH HI-LOCKS AND 4 EACH .25 INCH HI-LOCKS. (M) 2 L 7 3 4F A3WE 1999022600596 19990226 00596 NM 1999 2 26 AALA982181 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 950E FRAME HAS DENT ON UPPER FLAGNE WITH WEB DEFORMED ABOVE STRINGER 26. INSTALLED REPAIR DOUBLER PER SRM 51-40-3 USING MAT 7075-T6, SIZE 12 INCH BY 4 INCH, WITH 2 ROWS ON SIDE WEB HAVING 12 .25 INCH BAC B30 FP8 1 ROW AND 13 .1875 BAC B30 FP6 OTHER ROW, 1 ROW ON TOP HAVING 12 BAC B30 FP6 .1875 INCH WITH 4 FASTENERS ON EACH SIDE OF DAMAGE. (M) 2 L 7 3 4F A3WE 1999022600597 19990226 00597 NM 1999 2 26 AALA982180 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 680 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - BELL FRAME DENTED STATION 680 BETWEEN STRINGER 22L AND 24L. CUT OUT DAMAGED AREA 4.5 L BY .5 W INSTALLED .050 DOU BLER 7075-T6 13 INCHES LONG. INSTALLED 17 FASTENERS THROUGH BELL FRAME UPPER FLANGE ON .75 INCH SPACING, 20 FASTENERS T HROUGH SIDE ON 1 INCH SPACING (2 ROWS OF 10 EACH) FASTENER USED HI-LOCKS BACB30FP6-2, ORIG MATERIAL THICKNESS .050, HI-L OCKS BACB30FP6-4, SRM 53-10-4. (M) 2 L 7 3 4F A3WE 1999022600598 19990226 00598 NM 1999 2 26 AALA982179 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 950F FRAME HAS LARGE DENT IN UPPER FLANGE WITH CREASE IN WEB BETWEEN STRINGER 23L TO 24L. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 51-40-4. 3 ROWS OF 4 RIVETS ON EACH SIDE OF DAMAGE 7075-T6 .071, 17 438D .25 INCH, 14 BAC015CE6 20 EACH MS470. (M) 2 L 7 3 4F A3WE 1999022600599 19990226 00599 NM 1999 2 26 AALA982178 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 1030 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATIN 1030 FRAME HAS DENT IN UPPER FLANGE WITH FORWARD WEB DEFORMED, STRINGER 25-26R. INSTALLED DOUBLER MADE OF .070 7075 F6 APPROX 13 INCHES LENGTH BY 4 INCHES WITH 2 ROWS OF .25 INCH HI-LOCKS HAVING 4 FASTENERS EACH SIDE OF DAMAGE AND 1 ROW OF .1875 INCH SCREWS HAVING 6 FASTENERS EACH SIDE OF DAMAGE PER SRM 51-40-3. (M) 2 L 7 3 4F A3WE 1999022600600 19990226 00600 NM 1999 2 26 AALA982177 1 19981209 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 344 MISDRILLED A AALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FLOORBEAM STATION 344 LEFT TOP FORWARD FLANGE HAS HOLE WITH NO EDGE DISTANCE. INSTALLED FLOORBEAM REPAIR IAW ESO 11697, DATED 11-17-98. (M) 2 L 7 3 4F A3WE 1999022600601 19990226 00601 NM 1999 2 26 AALA982176 1 19981211 A 5320 ANGLE BOEING 727 727223 1384074 NM BS 1273 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - ANGLES CRACKED IN RIGHT LOWER TORQUE BOX IN VENTRAL STAIRS STATION 1273 UNDER A/S ACT. ANGLES REPLACED UNDER AIRS TAIRS ACT AND WEB REPLACES STATION 1273. (M) 2 L 7 3 4F A3WE 1999022600602 19990226 00602 NM 1999 2 26 AALA982175 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 620 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 620 BELL FRAME DENTED BETWEEN STRINGER 23L AND 25L. REPAIRED BELT FRAME PER SRM 51-40-3 PAGE 3, STATION 6 20 BETWEEN STRINGER 23L AND 25L. (M) 2 L 7 3 4F A3WE 1999022600603 19990226 00603 NM 1999 2 26 AALA982174 1 19981211 A 5311 FRAME BOEING 727 727223 1384074 NM BS 720 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 720A FRAME UPPER FLANGE DENTED BETWEEN STRINGER 24L AND 25L. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER PER SRM 51-40-3. INSTALLED DOUBLER OVER DAMAGED AREA, DENT .050 FRAME, DOUBLER MATERIAL .050. SAME TYPE MATERIAL FASTE NERS BAC 830 FM6 BACB30 FM8 FIVE ROWS ON BOTH SIDE OF DAMAGE. (M) 2 L 7 3 4F A3WE 1999022600604 19990226 00604 NM 1999 2 26 AALA982173 1 19981211 A 5315 FLOORBEAM BOEING 727 727223 1384074 NM BS 1130 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - STATION 1130 FLOORBEAM HAS CORROSION AROUND CLIP NUT PLATE HOLES IN LOWER FLANGE BL 0 TO APPROX LBL 40. INSTALLED DOUBLER PER ESO 11697 DATED 11-19-98. (M) 2 L 7 3 4F A3WE 1999022600605 19990226 00605 NM 1999 2 26 AALA982172 1 19981211 A 5350 SKIN BOEING 727 727223 1384074 NM BS 1148-1166 GOUGED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - TWO GOUGES IN SKIN INSIDE, BETWEEN STATION 1148-1166 RIGHT SIDE ABOVE STRINGER 27R. INSTALLED REPAIRED DOUBLER IA W SRM 53-30-3 PAGE 151 FIG 24. (M) 2 L 7 3 4F A3WE 1999022600606 19990226 00606 NM 1999 2 26 AALA982171 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 1100 CRACKED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - FOUND CRACK EXTENDING FROM RIVET RIGHT SIDE STRINGER 1 AT STATION 1100, FUSE SKIN. INSTALLED DOUBLER REPAIR PER S B NR 727-53A0204 AND SRM 53-30-3 PAGE 3. (M) 2 L 7 3 4F A3WE 1999022600607 19990226 00607 NM 1999 2 26 AALA982170 1 19981211 A 5330 SKIN BOEING 727 727223 1384074 NM BS 720 WORN A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 884AA 21523 TUL - SKIN LAP WORN STRINGER 19R STATION 720D PLUS 12 INCHES TO 720D PLUS 14 INCHES AT WIG WRAP AROUND PANEL L/E. REMOV ED DAMAGED AREA. INSTALL FLUSH DOUBLER REPAIR PER SRM 53-30-3 FIG 6. (M) 2 L 7 3 4F A3WE 1999022600611 19990226 00611 NM 1999 2 26 MZZA98293 1 19981113 A 5280 BACB10B131 BEARING BOEING 727 727224 1384076 NM RT MLG DOOR FROZEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, RT MLG DOOR MANUAL RELEASE CRANK ROLLER WAS FOUND FROZEN. THE DAMAGED BEARING P/N BACB10B131 WAS REMOVED AND REPLACED PER B727 MM 20-10-7 AND OPERATION CHECK FOUND SATISFACTORY. (M) 2 L 7 3 4F A3WE 1999022600612 19990226 00612 NM 1999 2 26 MZZA98287 1 19981123 A 5320 BRACKET BOEING 727 727224 1384076 NM BS 297 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 4 INCHES LONG CRACK WAS FOUND ON FUSELAGE S-16L REINFORCEMENT B RACKET AT BS 297. THE DAMAGED REINFORCEMENT BRACKET WAS REMOVED AND REPLACED WITH NEW BRACKET. (M) 2 L 7 3 4F A3WE 1999022600613 19990226 00613 NM 1999 2 26 MZZA98288 1 19981111 A 2761 652460817 ANGLE BOEING 727 727224 1384076 NM NR 3 SPOILER ACT CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON NR 3 SPOILER ACTUATOR SUPPORT ANGLE. THE CR ACK SUPPORT ANGLE P/N 65-24608-17 WAS REMOVED AND REPLACED NEW ONE. (M) 2 L 7 3 4F A3WE 1999022600614 19990226 00614 NM 1999 2 26 MZZA98289 1 19981127 A 5753 651927010 FLAP TRACK BOEING 727 727224 1384076 NM TE FLAPS CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON NR 4 FLAP TRACK MOUNTING PAD 'A' AROUND THE BOLT HOLE. THE DAMAGED NR 4 FLAP TRACK P/N 65-19270-10 WAS REMOVED AND REPLACED PER B727 MM 27-51-31. (M) 2 L 7 3 4F A3WE 1999022600615 19990226 00615 NM 1999 2 26 MZZA98290 1 19981119 A 5753 SKIN BOEING 727 727224 1384076 NM LT TE MID FLAP DELAMINATED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, DELAMINATION WAS FOUND ON LEFT WING T/E INBOARD MID FLAP UPPER SKIN AT WBL 226. THE DAMAGED SKIN 7 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. (M) 2 L 7 3 4F A3WE 1999022600616 19990226 00616 NM 1999 2 26 MZZA98292 1 19981115 A 5753 652163262 ANGLE BOEING 727 727224 1384076 NM RT TE MID FLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 2 INCH LONG CRACK WAS FOUND ON RT WING T/E INBOARD MID FLAP LOW ER CLOSURE ANGLE AT WBL 204. THE CLOSURE ANGLE CRACK AREA (2 INCH LONG) WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40 -4. (M) 2 L 7 3 4F A3WE 1999022600617 19990226 00617 NM 1999 2 26 MZZA98291 1 19981123 A 5753 652163262 ANGLE BOEING 727 727224 1384076 NM RT TE MIDFLAP CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, 1.125 INCH LONG CRACK WAS FOUND ON RT WING T/E INBOARD MID FLAP LOWER CLOSURE ANGLE AT WBL 124. THE CLOSURE ANGLE CRACK AREA (1.125 INCH LONG) WAS TRIMMED OUT AND REPAIRED PER B727 S RM 51-40-4. (M) 2 L 7 3 4F A3WE 1999022600618 19990226 00618 NM 1999 2 26 MZZA98294 1 19981115 A 5711 652163262 SPAR BOEING 727 727224 1384076 NM RT WING CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING T/E INBOARD MID FLAP REAR SPAR LOWER CHORD HORIZONTAL FORWARD FLANGE AT WBL 2105. THE CORRODED REAR SPAR LOWER CHORD HORIZONTAL FORWARD FLANGE WA S CLEAN UP AND REPAIRED PER CAL EC/RA 5750-03110 DATED DEC 09, 1998. (M) 2 L 7 3 4F A3WE 1999022600673 19990226 00673 NM 1999 2 26 P2EA99016 1 19981207 A 5330 SKIN BOEING 737 737247 138448D NM BS 462 DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 SJO - FUSELAGE SKIN DENTED AT BS 462, WL 199. DEFECT SIZE, LENGTH 1 INCH, WIDTH 1 INCH, DIAMETER .050 INCH. REPAIRED F USELAGE SKIN SECTION BETWEEN BS 458 AND BS 467, FROM STRINGER 17 LEFT TO STRINGER 19 LEFT PER SRM 53-30-3 FIG 7. (M) 2 L 7 2 4F A16WE 1999022600675 19990226 00675 EU 1999 2 26 VTZA98365 1 19981212 A 2425 7011672112 SYMBOL GENERATOR JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 315UE 41033 FLT 6235 - IAD-CHO - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LT SYMBOL. GENERATOR FAILED. AIRCRAFT R ETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED SYMBOL GENERATOR. OPS CHECK O K. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999022600676 19990226 00676 EU 1999 2 26 VTZA98364 1 19981212 A 7797 WIRE BAG JETSTM JETSTM3201 1500217 EU RT ENGINE CHAFED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 489UE 908 FLT 6445 - IAD-ROC - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT ENGINE EGT FLUCTUATION. AIRCRAFT RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REPAIRED CHAFED WIRE, OPS CHECK OK. AIRCRAFT WAS REL EASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999022600677 19990226 00677 EU 1999 2 26 VTZA98363 1 19981211 A 3234 87770 CONTROL UNIT JETAIR JETSTM JETSTM4101 1500501 EU COCKPIT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 320UE 41043 FLT 6353 - IAD-TYS - DURING TAKEOFF, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO GEAR HANDLE WOULD NOT MOVE ON RETRACTION . AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED GEAR HANDLE CONTR OL UNIT AND PERFORMED GEAR SWING. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999022600678 19990226 00678 EU 1999 2 26 VTZA98362 1 19981211 A 7712 SWITCH BAG JETSTM JETSTM3201 1500217 EU LT ENGINE FAILED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK N FALSE WARNING TO TAKEOFF 1 EA 27 483UE 898 FLT 6379 - IAD-SYR - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO EGT FLUCTUATION. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED 30 PERCENT TORQUE MICROSWITCH, OPS CHECK OK. AIRCRAF T WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999022600679 19990226 00679 EA 1999 2 26 VTZA98361 1 19981207 A 2163 7546811 SENSOR CNDAIR CL600 CL6002B19 EA RIGHT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 622BR 7187 FLT 6780 - IAD-DTW - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RT DUCT FAIL MESSAGE ILLUMINATED. MAINT ENANCE INSPECTED AND REMOVED AND REPLACED TEMPERATURE SENSOR, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETU RN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999022600701 19990226 00701 WP 1999 2 26 99ZZZM154 1 19980905 A 5210 BEAM DOUG DC9 DC932F 3022067 WP L1 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, L1 DOOR FORWARD PAN AT HINGE CUTOUT CRACKED, NR 1, NR 2, NR 5 AND NR 6 BEAM FORWARD ENDS CRACKED. REPLACED CRACKED PAN, REPAIRED BEAMS PER SRM 52-05 FIG 25, 18 AND 31. (M) 2 L 7 2 4F A6WE 1999022600710 19990226 00710 EU 1999 2 26 SIMA983493 1 19981215 A 2710 S2711212700140 BELLCRANK AEROSP ATR72 ATR72212 EU RT AILERON LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 DFW - DURING COMPLIANCE OF AD 93-12-10, FOUND BELLCRANK IN RIGHT WING AT RIB 26 WITH LOOSE CENTER BEARING. REMOVED AND REPLACED BELLCRANK. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999022600711 19990226 00711 EU 1999 2 26 SIMA983495 1 19981215 A 2710 S2711201200300 CRANK LEVER AEROSP ATR72 ATR72212 EU RT AILERON LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 DFW - DURING COMPLIANCE OF AD 93-12-10, FOUND CRANK LEVER IN RIGHT WING AT RIB 22 WITH LOOSE BEARING. REMOVED AND REPLA CED CRANK LEVER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999022600712 19990226 00712 EU 1999 2 26 SIMA983494 1 19981215 A 2710 S2711201300500 CRANK LEVER AEROSP ATR72 ATR72212 EU LT AILERON LOOSE A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 420AT 420 DFW - DURING COMPLIANCE OF AD 93-12-10, FOUND CRANK LEVER IN LEFT WING AT RIB 15 WITH LOOSE BEARING. REMOVED AND REPLAC ED CRANK LEVER. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999022600714 19990226 00714 WP 1999 2 26 EIAA980289 1 19981002 A 5320 JAMB DOUG DC9 DC932F 3022067 WP CARGO DOORWAY DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN DECK CARGO DOOR CUTOUT, UPPER FORWARD CORNER WAS FOUND DAMAGED. THE PIN AND RETAINER REQUIRE D BY AD 89-11-02 R1 AND SB 52-170, REQUIRED MODIFICATION/DEVIATION. ACCOMPLISHED DEVIATIONS PER EA DC9-53-190 AND DC9-5 3-204, ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999022600715 19990226 00715 WP 1999 2 26 EIAA980287 1 19981002 A 5320 99212173 SILL DOUG DC9 DC932F 3022067 WP CARGO DOOR CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 935F 50510 47220 PHX - DURING C-CHECK, MAIN DECK CARGO DOOR LOWER SILL PLATE HAS CORROSION, NRC W338. REPAIRED PER SRM EA DC9-53-198 AND ECRA 935-51-038-1. (M) 2 L 7 2 4F A6WE 1999030500075 19990305 00075 EA 1999 3 5 SHUT98101 1 19981222 A 5210 85201081003 CABLE 85210002001 DHAV DHC8 DHC8311 1386006 EA PAX DOOR JAMMED A UHLA K NONE O OTHER IN INSP/MAINT 1 NE 03 804SA 375 ORF/ILG - FLT 126 - WHILE TRYING TO DEPLANE THE PASSENGERS, THE AIRSTAIRS DOOR ASSIST CABLE JAMMED. THE CREW CALLED MAI NTENANCE. MAINTENANCE REPLACED BOTH GAS CHARGE STRUTS, REPLACED AND ADJUSTED THE DOOR ASSIST CABLE, DOOR OPS CHECKED GO OD. AIRCRAFT RETURNED TO SERVICE. (GROUND HANDLING IS SUSPECTED OF PUSHING THE DOOR TOO HARD CAUSING THE CABLE TO COME OFF THE DRUM AND JAMMING. GROUND HANDLING PROCEDURES HAVE BEEN ADDRESSED). 2 H 7 2 4T RT A13NM 1999030500137 19990305 00137 EU 1999 3 5 99ZZZX771 1 19980924 A 7931 MS280343 SENSOR BOLKMS 117 BK117A3 5626015 EU ENGINE OIL INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 77 70458 7063 SENSOR UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500138 19990305 00138 EU 1999 3 5 99ZZZX772 1 19980723 A 6320 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117B1 5626012 EU TRANSMISSION OIL INTERMITTENT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 386 51612B32 7231 TRANSMITTER UNIT OPERATES INTERMITTENTLY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500139 19990305 00139 EU 1999 3 5 99ZZZX773 1 19981219 A 6320 IPT20RT1100080G TRANSMITTER BOLKMS 117 BK117B1 5626012 EU TRANSMISSION OIL ERRATIC A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 262 5691423 7169 TRANSMITTER HAS ERRATIC PRESSURE INDICATIONS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500140 19990305 00140 EU 1999 3 5 99ZZZX774 1 19981109 A 7810 117651121 TAIL PIPE BOLKMS 117 BK117A3 5626015 EU EXHAUST WARPED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 176 7063 TAIL PIPE HAS EXCESSIVE WARPAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500141 19990305 00141 NM 1999 3 5 99ZZZX775 1 19981014 A 7160 900CF330001101 ACTUATOR DOUG MD900 MD900 3027375 NM INLET DOOR FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 361 55 90000012 ACTUATOR UNIT INOPERATIVE. FAILS TO RETRACT DOOR. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999030500142 19990305 00142 NM 1999 3 5 99ZZZX776 1 19981202 A 6710 900C2010214101 PITCH LINK DOUG MD900 MD900 3027375 NM MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 306 90000012 PITCH LINK WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999030500143 19990305 00143 NM 1999 3 5 99ZZZX777 1 19980313 A 6210 900R1150001113 BLADE DOUG MD900 MD900 3027375 NM MAIN ROTOR DEBONDED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 1673 0099990208 90000012 BLADE DEBONDING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999030500144 19990305 00144 NE 1999 3 5 99ZZZX778 2 19981115 A 7261 312110901 LINE DOUG MD900 MD900 3027375 NM PWA PW206 PW206A NE OIL SYSTEM WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 2125 90000012 PCE206018 LINE IN OIL SYSTEM WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U NC H19NM E42NE 1999030500188 19990305 00188 1999 3 5 CA990203012 2 19980821 A 7320 740361 ECU AIRBUS A340 A340313 EU NR 2 ENGINE FAILED W C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 CA (CAN) NR 2 ENGINE FLAMED OUT AT 70 KNOTS ON TAKEOFF. TAKEOFF REJECTED. POWER LOSS AND TURBINE TEMPERATURE IN EXCESS OF 1000 DEGREES CELSIUS. TROUBLESHOOTING FOUND INTERMITTENT FAULT CONFUSED FULL DIGITAL CONTROL; CHANNEL A VARIABLE STATO R VANE FEED BACK ACTUATOR FAULT; CHANNEL B A ROTOR ACTIVE CLEARANCE AND START BLEED FAILED OPEN FAULT. RESULTING IN VAR IABLE STATOR VANE POSITION/DEMAND DISAGREE AND THE ENGINE STALLED. IT IS PLANNED TO CORRECT THIS CORRUPTION OF SERVO AC TUATOR IN NEXT SOFTWARE VERSION C.3.G WHEN AVAILABLE. PART TC: 2,313. 2 L 7 4 4F RT A197 1999030500189 19990305 00189 NE 1999 3 5 CA990203013 2 19980106 A 7230 522194 STATOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7B 52053 NE COMPRESSOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 62719 SR304 P656927D (CAN) ENGINE IN SHOP AS TIME EXPIRED. INSPECTION FOUND THE FRONT COMPRESSOR ROTOR THIRD (TO FOURTH) STAGE SPACER CRACKE D. THERE WERE EIGHT CRACKS EXTENDING FROM TIE ROD SLEEVE HOLES TO INSIDE AND ONE SMALL CRACK STARTING FROM THE TIE ROD SLEEVE HOLE TO OUTSIDE DIAMETER. 61,431. 2 L 7 2 4F 4 F A6WE E2EA 1999030500190 19990305 00190 NE 1999 3 5 CA990203014 2 19980315 A 7230 COMPRESSOR DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE NR 2 ENGINE DAMAGED W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA 57552 P653684D (CAN) ON TAKEOFF, POWER LEVERS BROUGHT TO 1.4 EPR FOR RUN-UP, ALL OKAY. AT APPROXIMATELY 85-95 KNOTS, THE NR 2 ENGINE H AD A POWER LOSS. EGT INITIALLY AT 700 CELCIUS, ON SHUTDOWN EGT AT 800 CELSIUS. FIRE TRUCKS CALLED. INSPECTION FOUND H EAVY DAMAGE TO THE HIGH PRESSURE COMPRESSOR. 7TH STAGE VANE FAILURE, 8TH STAGE BLADE FAILURE. HEAVY DAMAGE TO THE 9TH AND 10TH STAGE DISKS. INVESTIGATION FOUND NO FIRM CAUSE OF THE SITUATION. SEVERAL AREAS COULD HAVE CAUSED THIS FAILURE . STAGE 7 VANE FAILURE; STAGE 7 BLADE FAILURE; STAGE 8 LOCK FAILURE, OR STAGE 8 BLADE FAILURE. THE ENGINE WAS NOT REPA IRED, BUT WAS CANNABILIZED. 2 L 7 2 4F 4 F A6WE E2EA 1999030500191 19990305 00191 NE 1999 3 5 CA990203015 2 19981002 A 7250 BLADE BOEING 747 747133 138448B NM PWA JT9 JT9D7 52054 NE COMPRESSOR FRACTURED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) NR 2 ENGINE FAILED IN CLIMB. IN-FLIGHT SHUTDOWN CARRIED OUT AT 9,400 FEET, SPEED 250 KNOTS, BIG BANG FELT/HEARD, WITH HIGH EGT AND LIGHT ON. FLIGHT RETURNED TO ITS DEPARTURE POINT. BORESCOPE INSPECTION FOUND 1ST STAGE TURBINE BLADE FRACTURED AND DOWN STREAM DAMAGE TO 2ND STAGE TURBINE BLADES AND THE LP TURBINE VANES AND BLADES. ENGINE TAKEN OUT OF S ERVICE AND WILL BE SOLD. 2 L 7 4 4F 4 F A20WE E20EA 1999030500241 19990305 00241 NM 1999 3 5 AALA982130 1 19980112 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 847AA 20988 DTW - DURING MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIR EMERGENCY EXIT LIGHT ASSEM BLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500242 19990305 00242 NM 1999 3 5 AALA982026 1 19981103 A 3350 1001141 LIGHT GRIMES BOEING 727 727223 1384074 NM AFT STAIR INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 879AA 9616 21391 DTW - DURING OVERNIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500243 19990305 00243 NM 1999 3 5 AALA982129 1 19981125 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 895AA 22011 DFW - DURING OVERNIGHT MAINTENANCE CHECK, EMERGENCY EXIT FLOOR PATH LIGHTING IN COACH CABIN INOPERATIVE. REPAIRED WIRIN G IN COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500244 19990305 00244 NM 1999 3 5 AALA982075 1 19981115 A 3350 CONNECTOR BOEING 727 727227 1384078 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 723AA 20731 DFW - DURING MAINTENANCE, EMERGENCY EXI TLIGHT AT FORWARD COACH CABIN INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNEC TORS AT FORWARD COACH CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500245 19990305 00245 NM 1999 3 5 AALA982074 1 19981113 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM GALLEY DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 708AA 6106 22465 DTW - DURING OVERNIGHT MAINTENANCE, THE AFT GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT GALLEY S ERVICE DOOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500246 19990305 00246 NM 1999 3 5 AALA982079 1 19981116 A 3350 1000679 LIGHT GRIMES BOEING 727 727223 1384074 NM L1 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6823 24413 19701 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT OVER L1 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT OVER L 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500247 19990305 00247 NM 1999 3 5 AALA982123 1 19981124 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AFT STAIR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 899AA 22015 DTW - DURING OVERWEIGHT MAINTENANCE, AFT STAIR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED AFT AIR STAIR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500248 19990305 00248 NM 1999 3 5 AALA982144 1 19981204 A 3350 LIGHT BOEING 727 727223 1384074 NM CABIN DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 863AA 21090 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT STRIP AFT OF FORWARD GALLEY HAS TWO LAMPS UNDERNEATH EXIT IDENTIFIER INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP NEXT TO FORWARD GALLEY. SYSTEM GROUND CHE CKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500249 19990305 00249 NM 1999 3 5 AALA982237 1 19981227 A 3350 1000679 LIGHT BOEING 727 727223 1384074 NM GALLEY DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 887AA 21526 DFW - DURING OVERNIGHT CHECK, FORWARD GALLEY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY DOOR EMERGE NCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500250 19990305 00250 NM 1999 3 5 AALA982236 1 19981227 A 3350 LIGHT BOEING 727 727223 1384074 NM ROW 3E DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6818 19493 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH EXIT LIGHT AT SEAT 3E INOPERATIVE. REPLACED EMERGENCY EXIT FLOO R PATH LIGHT STRIP AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500251 19990305 00251 NM 1999 3 5 AALA982235 1 19981227 A 3350 LIGHT BOEING 727 727223 1384074 NM ROW 30 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 6818 19493 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH EXIT DECAL AT SEAT ROW 30 NOT PROPERLY LIGHTED. REPLACED EMERGE NCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 30. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500252 19990305 00252 NM 1999 3 5 AALA982150 1 19981207 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 DFW - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS IN COACH CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOO R PATH LIGHT WIRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500253 19990305 00253 NM 1999 3 5 AALA982149 1 19981207 A 3350 1001141 LIGHT BOEING 727 727223 1384074 NM AIR STAIRS DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 860AA 21087 DFW - DURING OVERNIGHT CHECK, AIR STAIR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED AIR STAIR EMERGENCY EXIT LIGHT ASSE MBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1999030500256 19990305 00256 EU 1999 3 5 AALA982016 1 19981030 A 3350 2LA00535821 LIGHT FOKKER F28 F28MK0100 4990807 EU EMERGENCY EXIT DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1432A 11417 DFW - DURING OVERNIGHT MAINTENANCE, RIGHT AFT FAIRING EXTERIOR EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. REPLACED RIGH T AFT FAIRING EXTERIOR EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999030500257 19990305 00257 EU 1999 3 5 AALA982131 1 19981125 A 3350 LIGHT FOKKER F28 F28MK0100 4990807 EU ROW 6 DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1471G 11507 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROW 6 HAD ONE BULB INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT 1999030500264 19990305 00264 NE 1999 3 5 AALA980833 2 19980426 A 7250 1333M87P01 BEARING DOUG MD11 MD11 3023602 NM GE CF6 CF680C2D1F 30025 NE NR 3 ENGINE FAILED A AALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CR CRUISE 1 SW 07 1762B 48552 FAFK8312 SEA - FLT 128 - DURING CRUISE NRT-SJC, NR 3 ENGINE DID AN UNCOMMANDED SHUTDOWN DUE TO EGT SPIKE. FLIGHT CREW ACCOMPLISH ED ENGINE SHUTDOWN CHECKLIST AND CONTINUED TO SJC AND LANDED WITHOUT FURTHER INCIDENT. NR 3 ENGINE WAS INSPECTED BY MX AND THE GEAR BOX WAS FOUND TO BE FROZEN. AIRCRAFT WAS ENGINE OUT MAINTENANCE FERRIED TO SEA FOR ENGINE CHANGE. REPLACE D NR 3 ENGINE. ACCOMPLISHED LEAK CHECK AND ENGINE GROUND RUN WITH NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERA TION. SHOP TEAR DOWN REVEALED THE NR 4 BEARING FAILED WHICH ALLOWED THE HPT STAGE ONE BLADES TO RUB AGAINST THE NOZZLES CAUSING THE GEARBOX TO SEIZE. THERE WAS METAL FOUND FROM THE FAILED NR 4 BEARING THROUGHOUT THE FAN AND CORE MODULE. 2 L 7 3 4F 4 F RT A22WE E31N3 1999030500273 19990305 00273 CE 1999 3 5 MASA98218 1 19981204 A 3245 6229681001 EHSI BEECH 1900 1900D 1154162 CE RT COCKPIT FAILED A MASA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 07 142ZV UE142 FLT 5337 - LEB-PHL - AFTER DEPARTURE, CAPTAIN REPORTED THAT THE F/O'S EHSI TUBE BLANKED OUT AND HE NOTED AN ELECTRICAL S MOKE SMELL IN COCKPIT. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE F/O'S EHSI TUBE, OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE.. (M) 2 L 7 2 4T RT A24CE 1999030500280 19990305 00280 WP 1999 3 5 ASAA9880276 1 19981231 A 5210 MECHANISM DOUG DC9 DC982 3022082 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 SEA - DURING MAINTENANCE CHECK, THE L1 DOOR WOULD NOT LATCH OPEN. ADJUSTED DOOR HOLD OPEN MECHANISM AND OPERATED NORMAL LY. (M) 2 L 7 2 4F A6WE 1999030500283 19990305 00283 1999 3 5 ASAA9880249 4 19981128 A 2565 D29982107 BOTTLE DOUG DC9 DC983 3022083 WP L1 DOOR SLIDE LOW PRESSURE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 1176 53024 LAX - PRIOR TO DEPARTURE OF FLIGHT 84, CREW REPORTED THE L1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WA S LOW. REPLACED THE L1 DOOR EMERGENCY EVACUATION SLIDE ASSEMBLY. (M) 2 L 7 2 4F RT A6WE 1999030500284 19990305 00284 WP 1999 3 5 ASAA9880254 1 19981206 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR LACK OF LUBE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 958AS 53024 PDX - PRIOR TO DEPARTURE OF FLIGHT 453, CREW REPORTED THE L1 DOOR WAS DIFFICULT TO UNLATCH FROM THE FULL OPEN POSITION. LUBRICATED THE DOOR HOLD OPEN MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999030500285 19990305 00285 WP 1999 3 5 ASAA9880247 1 19981123 A 5210 MECHANISM DOUG DC9 DC983 3022083 WP L1 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 944AS 53019 SEA - FLT 535 - CREW REPORTED DIFFICULTY IN CLOSING, THE L1 DOOR AND EXTINGUISHING DOOR LIGHT. ADJUSTED DOOR ROTATING R OD, CRANK AND BAYONET ROD, DOOR OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999030500286 19990305 00286 WP 1999 3 5 ASAA9880265 1 19981216 A 5240 49376431 HOOK DOUG DC9 DC983 3022083 WP L2 DOOR DEFECTIVE A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 979AS 53471 SEA - DURING MAINTENANCE CHECK, THE L2 DOOR WOULD NOT LATCH OPEN. REPLACED THE DOOR HOLD OPEN HOOK AND OPERATED NORMALL Y. (M) 2 L 7 2 4F RT A6WE 1999030500287 19990305 00287 WP 1999 3 5 ASAA9880264 1 19981215 A 5310 5956875501 JAMB DOUG DC9 DC982 3022082 WP L1 DOOR CRACKED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 LCQ - DURING 15K CHECK, THE L1 DOOR JAMB INNER SKIN TO INTERCOSTAL ATTACH TABS WERE FOUND CRACKED AT FS 208 AT LONGERONS 11L AND 15L. REPAIRED IAW ASA EA 5310-01635. (M) 2 L 7 2 4F A6WE 1999030500288 19990305 00288 WP 1999 3 5 ASAA9880263 1 19981213 A 4920 17952872M CLAMP DOUG DC9 DC983 3022083 WP APU BROKEN A ASAA F ACTIVATE FIRE EXT. M J OVER TEMP WARNING INDICATION IN INSP/MAINT 1 NM 01 962AS 53076 SEA - PRIOR TO DEPARTURE OF FLIGHT 376, CREW REPORTED AUXILIARY POWER UNIT FIRE WARNING LIGHTS ILLUMINATED 3 TO 4 MINUTE S AFTER START. SHUT DOWN AUXILIARY POWER UNIT AND DISCHARGED APU FIRE BOTTLE, FIRE WARNING LIGHTS EXTINGUISHED. CREW O NLY WAS ON BOARD AIRCRAFT. INSPECTED AUCILIARY POWER UNIT AND FOUND COMBUSTOR UNIT CLAMP BROKEN. REPOSITIONED AUXILIAR Y POWER UNIT COMBUSTOR ASSEMBLY AND REPLACED CLAMP. ALSO, REPLACED DAMAGED IGNITOR LEAD AND AUXILIARY POWER UNIT OPERAT ED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999030500289 19990305 00289 WP 1999 3 5 ASAA9880261 1 19981211 A 2150 AIR DIST DOUG DC9 DC982 3022082 WP CABIN ODOR A ASAA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 NM 01 934AS 49235 OAK - AIR TURNBACK OF FLIGHT 445, CREW REPORTED ELECTRICAL ODOR IN CABIN DURING CLIMB-OUT PASSING 12,000 FT. ONE MINUTE LATER SMOKE WAS REPORTED IN CABIN, SWITCHED TO EMERGENCY POWER BUT ODOR AND SMOKE CONTINUED. TURNED OFF RIGHT AIR COND ITIONING PACK AND ODOR AND SMOKE DISSIPATED AFTER 3 TO 4 MINUTES. LANDED WITHOUT INCIDENT. INSPECTED RIGHT ENGINE INLE T AND EXHAUST, NO DEFECT NOTED. ACCOMPLISHED RUN UP OF RIGHT ENGINE, OPERATED RIGHT AIR CONDITIONING PACK AND ACCOMPLIS HED AIR QUALITY CHECK, NO ODOR OR DEFECT NOTED. REPLACED BOTH WATER SEPARATOR COALESCERS AND RELEASED FOR SERVICE. (M) 2 L 7 2 4F A6WE 1999030500290 19990305 00290 WP 1999 3 5 ASAA9880268 1 19981219 A 5330 SKIN DOUG DC9 DC982 3022082 WP BS 662 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 LCQ - DURING 15K CHECK, FOUND CORROSION ON LOWER FUSELAGE SKIN AT FS 662. REPAIRED IAW ASA EA 5330-01360. (M) 2 L 7 2 4F A6WE 1999030500291 19990305 00291 WP 1999 3 5 ASAA9880267 1 19981219 A 5313 59360531 LONGERON DOUG DC9 DC982 3022082 WP BS 636-650 CORRODED A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 933AS 49234 LCQ - DURING 15K CHECK, FOUND CORROSION ON LONGERON 30 FROM FS 636 TO 650. REPAIRED IAW ASA EA 5310-01637. (M) 2 L 7 2 4F A6WE 1999030500292 19990305 00292 WP 1999 3 5 ASAA9880250 1 19981129 A 5610 WINDOW DOUG DC9 DC983 3022083 WP LT COCKPIT OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 969AS 53063 SEA - PRIOR TO DEPARTURE OF FLIGHT 451, CREW REPORTED THE FLIGHT COMPARTMENT LEFT SLIDING WINDOW WOULD NOT OPEN. ADJUST ED WINDOW UPPER GUIDE MECHANISM AND OPERATED NORMALLY. (M) 2 L 7 2 4F RT A6WE 1999030500293 19990305 00293 WP 1999 3 5 ASAA9880248 1 19981125 A 5240 MECHANISM DOUG DC9 DC983 3022083 WP L2 DOOR OUT OF ADJUST A ASAA K NONE O OTHER IN INSP/MAINT 1 NM 01 965AS 53079 SEA - DURING MAINTENANCE CHECK, THE L2 DOOR WOLD NOT LATCH OPEN. ADJUSTED DOOR HOLD OPEN MECHANISM AND OPERATED NORMALL Y. (M) 2 L 7 2 4F RT A6WE 1999030500327 19990305 00327 NM 1999 3 5 USAA980656 1 19981223 A 5315 141N51121 FLOORBEAM BOEING 757 757225 1384959 NM BS 365 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 58 INCH AREA OF CORROSION STATION 365 FLOORBEAM RBL 2 - RBL 60. CORR OSION TASK NR C53-222-02. INSTALLED FLOORBEAM UPPER CHORD PER TR 53-15-01 AND EA 63108. (M) 2 L 7 2 4F RT A2NM 1999030500328 19990305 00328 NM 1999 3 5 USAA980691 1 19981218 A 5315 111T500889 FLOORBEAM BOEING 767 7672B7 1385107 NM BS 852 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 654US 33469 25225 CLT - DURING C-CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION TOP OF FLOORBEAM STATION 852 LBL 54, CORROSION TASK NR C53-131-01. INSTALLED DOUBLER PER EA 63142. (M) 2 L 7 2 4F RT A1NM 1999030500329 19990305 00329 NM 1999 3 5 USAA980652 1 19981223 A 5321 146N53183 FLOOR BOEING 757 757225 1384959 NM BS 1700 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 40 INCH BY 40 INCH AFT GALLEY FLOOR PAN AT BS 1700 DECK PLATE, CORROSION TASK NR C53-252-03. REPAIRED PER BOEING 757-200 SRM 51-30-01, 51-40-02 AND 51-20-05. (M) 2 L 7 2 4F RT A2NM 1999030500330 19990305 00330 NM 1999 3 5 USAA980651 1 19981223 A 5320 141N51911 STRAP BOEING 757 757225 1384959 NM BS 324-418 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 6 INCH BY 6 INCH CENTER STABILIZER STRAP BL 0 BETWEEN STATION 324 TO 418. CORROSION TASK NR C53-222-02. REPLACED PART PER BOEING 757-200 SRM 51-30-01, 51-40-02 AND DRAWING 141N5190 . (M) 2 L 7 2 4F RT A2NM 1999030500331 19990305 00331 NM 1999 3 5 USAA980650 1 19981223 A 5315 146N51112 FLOORBEAM BOEING 757 757225 1384959 NM BS 1681 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 1 INCH FLOORBEAM AT STATION 1681, NUT PLATES. CORRO SION TASK NR C53-252-03. INSTALLED DOUBLER PER EA 63088 AND BOEING 757-200SRM 51-20-05, 51-30-01 AND 51-40-02. (M) 2 L 7 2 4F RT A2NM 1999030500332 19990305 00332 NM 1999 3 5 USAA980655 1 19981223 A 5315 146N50891 FLOORBEAM BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 10 INCH TOP OF FLOORBEAM CAP BS 1640, CORROSION TASK NR C53-252-03 AND C53-250-03. SPLICED IN REPLACEMENT T-CAP PER SRM 53-00-51, TR 53-15-01 AND EA 63074. (M) 2 L 7 2 4F RT A2NM 1999030500333 19990305 00333 NM 1999 3 5 USAA980649 1 19981223 A 5315 146N54561 FLOORBEAM BOEING 757 757225 1384959 NM BS 1460-1480 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 10 INCH AREA ON INTERCOSTAL BS 1460-1480 STRINGER 28 R. CORROSION TASK NR C53-161-01. REPLACED PER BOEING 757-200 SRM 51-30-01 AND 51-40-02. (M) 2 L 7 2 4F RT A2NM 1999030500334 19990305 00334 NM 1999 3 5 USAA980634 1 19981223 A 5320 146N83221 SILL BOEING 757 757225 1384959 NM BS 1320-1360 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND CLIP NUT HOLES L-3 DOOR LOWER SILL BETWEEN STATION 1320 AND 1360. REPLACED SILL CHORD ANGLE PER SRM 51-40-00. (M) 2 L 7 2 4F RT A2NM 1999030500335 19990305 00335 NM 1999 3 5 USAA980654 1 19981223 A 5320 146N51907 SHEAR WEB BOEING 757 757225 1384959 NM BS 1701 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 1 INCH BY 6 INCH AT STATION 1701 BL 0 SHEAR WEB, CORROSION TAS K NR C53-252-03. REPAIRED PER BOEING 757-200 SRM 51-30-01, 51-40-02 AND 51-20-05. (M) 2 L 7 2 4F RT A2NM 1999030500336 19990305 00336 NM 1999 3 5 USAA980653 1 19981223 A 5320 140N25061 SHEAR WEB BOEING 757 757225 1384959 NM BS 1640-1660 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 18 INCH AT BL 0 STATION 1640-1660 SHEAR WEB. CORROS ION TASK NR C53-251-03 AND C53-252-03. REPAIRED PER BOEING 757-200 SRM 51-30-01, 51-40-02. (M) 2 L 7 2 4F RT A2NM 1999030500337 19990305 00337 NM 1999 3 5 USAA980658 1 19981223 A 5320 146N51905 ANGLE BOEING 757 757225 1384959 NM BS 1660-1681 CORROSION A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION BS 1660-1681 RBL 10 SHEAR WEB/ANGLE . INSTALLED NEW WEB/CHORD PER SRM 53-60-51. (M) 2 L 7 2 4F RT A2NM 1999030500338 19990305 00338 NM 1999 3 5 USAA980657 1 19981223 A 5347 146N51301 SEAT TRACK BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION SPOTS ON SEAT TRACKS BS 1640, RBL 24 RBL 44. REPAIRED PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1999030500339 19990305 00339 NM 1999 3 5 USAA980659 1 19981223 A 5347 146N51305 SEAT TRACK BOEING 757 757225 1384959 NM BS 1640 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION LEFT INBOARD SEAT TRACK AT STATION 1640. INS TALLED NEW SEAT TRACK PER SRM 51-40-02. (M) 2 L 7 2 4F RT A2NM 1999030500340 19990305 00340 NM 1999 3 5 USAA980648 1 19981223 A 5315 146N50901 FLOORBEAM BOEING 757 757225 1384959 NM BS 1660 CORRODED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 608AU 44600 22204 CLT - DURING C-4 CHECK VISUAL INSPECTION, FOUND CORROSION 2 INCH BY 10 FT TOP OF FLOORBEAM STATION 1660, CORROSION TASK NR C53-251-03. SPLICED IN NEW SECTION UPPER CHORD PER BOEING 757-200 SRM 53-00-51. (M) 2 L 7 2 4F RT A2NM 1999030500380 19990305 00380 EU 1999 3 5 99ZZZM159 1 19981228 A 5330 S533713232005 SKIN AEROSP ATR42 ATR42300 8680920 EU FUSELAGE DENTED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 47AE 047 SAW - DENTS IN FUSELAGE, ONE BETWEEN FRAMES 2 AND 3 AT STRINGER 21R, ONE BETWEEN FRAMES 6 AND 7 AND STRINGER 20 AND 21R, ONE BETWEEN FRAMES 19 AND 20 AND STRINGER 15 AND 16R, AND ONE BETWEEN FRAMES 21 AND 22 AND STRINGER 20 AND 21R. REPAIR ED DENTS. AIRCRAFT RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1999030500411 19990305 00411 NM 1999 3 5 EISA99001 1 19981229 A 5230 CONTROL BOX BOEING 727 7272M7 138407S NM CARGO DOOR MALFUNCTIONED A EISA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 721RW 21200 RED CARGO LIGH TON FLIGHT ENGINEERS PANEL ILLUMINATED, CHECK MASTER CONTROL OF CARGO DOOR AND HOOKS UNLOCKED LIGHT ILLUM INATED. CHECKLIST (ABNORMAL) COMPLETED NR 4 AMBER LIGHT ON CARGO DOOR MASTER CONTROL BOX WAS ILLUMINATED. CLIMBING THR OUGH 17,000 FEET, A LOUD BANG WAS HEARD. CLIMBING THROUGH 20,000 FEET, RED CARGO LIGHT ILLUMINATED. PERFORMED INSPECTI ON AS PER AERONAUTICAL ENGINEERS 727-200 CARGO DOOR CONVERSION MANUAL, CHAPTER 7. NO DEFECTS NOTED. (M) 2 L 7 3 4F A3WE 1999030500413 19990305 00413 NM 1999 3 5 EISA98321 1 19981219 A 5230 SWITCH BOEING 727 727223 1384074 NM CARGO DOOR FAILED A EISA O OTHER J WARNING INDICATION TO TAKEOFF 1 SW 07 316NE 19475 AFTER DEPARTURE MCI (1000 AGL) CARGO DOOR LIGHT ON SOLENOID PANEL ILLUMINATED. RETURN TO DEPARTURE AIRPORT. CABIN PRES SURE WAS LOST WHEN LIGHT CAME ON. ADJUSTED LOCK BAR CLOSED SWITCH AND 1 LOCK SWITCH. MAIN CARGO DOOR OPS CHECKS GOOD P ER MM 52-32-1. (M) 2 L 7 3 4F A3WE 1999030500434 19990305 00434 1999 3 5 VTZA98375 4 19981230 A 3416 4016341905 ALTIMETER JETAIR JETSTM JETSTM4101 1500501 EU LT COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 324UE 41017 FLT 6572 - IAD-SCE - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CAPTAINS ALTIMETER FAILED. AIRCRAFT RET URNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ALTIMETER, OPS CHECK OK. AIRCRA FT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999030500435 19990305 00435 EU 1999 3 5 VTZA98374 1 19981227 A 5270 91SE16 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU CARGO DOOR OUT OF ADJUST A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 EA 27 308UE 41023 FLT 6556 - SCE-IAD - DURING TAKEOFF, AIRCRAFT ABORTED TAKEOFF DUE TO POD DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETUR NED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND OPENED DMI 47224, MEL 52-3. MAINTENANCE CLOSED DMI 473 24 ON 12-29-98 BY ADJUSTING POD DOOR MICROSWITCHES, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERV ICE. (M) 2 L 7 2 4T RT A41NM 1999030500436 19990305 00436 EU 1999 3 5 VTZA98373 1 19981220 A 7712 GAUGE JETAIR JETSTM JETSTM4101 1500501 EU RT ENGINE TQ FLUCTUATED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 323UE 41059 FLT 6499 - IAD-ROA - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE TORQUE GAUGE FLUCTUATION. A IRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SWAPPED TO BRIDGE NR 2, OPS CHECK OK. AIR CRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999030500437 19990305 00437 EA 1999 3 5 VTZA98372 1 19981220 A 2161 11513361 CONTROLLER CNDAIR CL600 CL6002B19 EA RIGHT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 622BR 7187 FLT 6675 - ORD-FSD - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT DUCT FAIL MESSAGE ILLUMINATED. AIR CRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED TEMPERATURE CONTROLLER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999030500438 19990305 00438 EU 1999 3 5 VTZA98370 1 19981218 A 2710 PIN JETAIR JETSTM JETSTM4101 1500501 EU AILERON CHAFFED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 309UE 41022 FLT - 6524 - ROC-JFK - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITH ONE DISCREPANCY WHICH WAS TRIM WARNING L IGHT ILLUMINATED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND RESET AILERON TRIM TAB PIN , OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999030500439 19990305 00439 EU 1999 3 5 VTZA98367 1 19981214 A 2822 MF6000 NUT PLATE BAG JETSTM JETSTM3201 1500217 EU LT BOOST PUMP BROKEN A VTZA D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 EA 27 472UE 823 FLT 6352 - SWF-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO LEFT WING FUEL LEAK AND HAD NO OTHER PROBLEMS. MAINT ENANCE INSPECTED AND FOUND BROKEN NUT PLATE ON LEFT FUEL BOOST PUMP AND SCREW MISSING. MAINTENANCE REMOVED AND REPAIRED NUT PLATE AND REINSTALLED LEFT FUEL BOOST PUMP, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999030500440 19990305 00440 1999 3 5 VTZA98366 4 19981213 A 3420 5203337517 RMU JETAIR JETSTM JETSTM4101 1500501 EU LEFT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 306UE 41020 FLT 6500 - IAD-LGA - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT RMU FAILURE. AIRCRAFT RETURNED TO G ATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED LEFT RMU, OPS CHECK OK. AIRCRAFT WAS RELE ASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999030500442 19990305 00442 NM 1999 3 5 MZZA99003 1 19981223 A 5313 STRINGER BOEING 727 7272F9 138407D NM BS 1042 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FUSELAGE STRINGER AT S2 8R BS 1042. THE CORRODED STRINGER 19 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-03 FIGURE 1. (M) 2 L 7 3 4F RT A3WE 1999030500443 19990305 00443 NM 1999 3 5 MZZA99005 1 19981223 A 5330 SKIN BOEING 727 7272F9 138407D NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FUSELAGE BELLY SKIN AT S29R BETWEEN BS 950 PL US 11.09 AND BS 950A. THE CORRODED SKIN 5 INCH BY 5 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER EC/RA NR 5310-03809 D ATED 15 JAN 1999. (M) 2 L 7 3 4F RT A3WE 1999030500444 19990305 00444 NM 1999 3 5 MZZA99006 1 19981225 A 5320 65163381 STIFFENER BOEING 727 7272F9 138407D NM BS 950 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER TEE CHORD HORIZONTAL AND VERTI CAL FLANGES ADJACENT TO KEEL BEAM S29R. THE CORRODED LOWER TEE CHORD 5 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER EC/ RA NR 5310-03810 DATED 15 JAND 1999. (M) 2 L 7 3 4F RT A3WE 1999030500445 19990305 00445 NM 1999 3 5 MZZA99007 1 19981225 A 5314 65584411 KEEL BEAM BOEING 727 7272F9 138407D NM BS 950 CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK 1.5 INCH LONG WAS FOUND ON STRINGER S29R OUTBOARD FLANGE BETWEEN BS 9 50 AND 951.5. THE CRACKED STRINGER S29 KEEL BEAM OUTBOARD FLANGE ALONG OUTBOARD FACE OF VERTICAL CHORD FROM FORWARD END TO ONE AND A HALF FASTENER SPACE FORWARD OF BS 950A WAS TRIMMED AND REPAIRED PER EC/RA NR 5310-03809 DATED 15 JAN 1999. (M) 2 L 7 3 4F RT A3WE 1999030500510 19990305 00510 EA 1999 3 5 COMA9960081 1 19980219 A 2710 272955 LINK CNDAIR CL600 CL6002B19 EA RT AILERON WORN A COMA K NONE O OTHER IN INSP/MAINT 1 SO 01 958CA 7111 RIGHT AILERON FAILS BACKLASH CHECK. REPLACED BOTH PCU LINKS. 2 L 7 2 4F RT A21EA 1999030500673 19990305 00673 EU 1999 3 5 QXEA9900170 1 19981229 A 5730 SKIN FOKKER F28 F28MK4000 4990810 EU WING MISDRILLED A QXEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 09 499US 11182 PDX - HOLE DRILLED THROUGH OUTER WING TO CENTER WING BOX JOINT SPAR FORWARD END. REPAIRED IAW HORIZON AIR EA 4-57-201. 2 L 7 2 4F RT A20EU 1999030500674 19990305 00674 EU 1999 3 5 QXEA9900171 1 19981229 A 5720 STRIP FOKKER F28 F28MK4000 4990810 EU WING CHAFED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - .25 INCH CHAFE MARK ON FORWARD END OF LOWER CENTER TO OUTER WING JOINT STRIP. REPAIRED IAW HORIZON AIR EA 4-57-20 2. 2 L 7 2 4F RT A20EU 1999030500713 19990305 00713 CE 1999 3 5 99ZZZX828 1 19981202 A 2751 INDICATION BEECH 1900 1900D 1154162 CE TE FLAPS MALFUNCTIONED A MASA O OTHER N FALSE WARNING AP APPROACH 1 SW 07 143YV UE143 LEB/PHL - FLT 5272 - ON APPROACH TO PHL, CREW REPORTED AN ABNORMAL FLAPS INDICATOR TO THE PHL TOWER. THE TOWER DISPATCH ED THE RESCUE EQUIPMENT. CAPTAIN COMPLETED THE ABNORMAL CHECKLIST AND LANDED WITHOUT INCIDENT. MAINTENANCE T/S THE SYS TEM, NO DISCREPANCIES WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (X) 2 L 7 2 4T RT A24CE 1999030500716 19990305 00716 GL 1999 3 5 C2XA98CL086 2 19981227 A 7250 BLADE EMB 145 EMB145ER SO ALLSN AE300 AE3007A GL TURBINE DAMAGED A C2XA K NONE O OTHER IN INSP/MAINT 1 SW 09 14937 1857 145026 CAE310087 CLE - DURING A SCHEDULED INSPECTION, THE RIGHT HAND ENGINE TURBINE BLADES WERE FOUND TO HAVE DAMAGED EDGES AND APPEAR TO BE RUBBING. THE DAMAGE WAS FOUND BEYOND MANUFACTURER'S LIMITS. THE RIGHT HAND ENGINE WAS REMOVED AND REPLACED IAW CON TINENAL EXPRESS TASK CARD NR 6271001. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (X ) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999030500717 19990305 00717 EU 1999 3 5 USAASA98002 1 19981221 A 2913 PUMP AIRBUS A319 A319112 EU HYDRAULIC SYS MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 702UW 0896 PHL - FLT 2023 - AFTER TAKEOFF FROM PHL, THE YELLOW HYDRAULIC SYSTEM OVERHEATED. THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PUT THE YELLOW SYSTEM ELECTRIC PUMP ON MEL. SEE SDR USAASA98003 FOR MORE INFORMA TION. (X) 2 L 7 2 4F RT A28NM 1999030500718 19990305 00718 EU 1999 3 5 USAASA98003 1 19981221 A 2910 693335 ELECTRIC PUMP AIRBUS A319 A319112 EU HYDRAULIC SYS MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 702UW 0896 PHL - FLT 8005 - AFTER TAKEOFF FROM PHL, THE YELLOW HYDRAULIC SYSTEM OVERHEATED. WHEN THE CONDITION EXISTED FOR 10 MINU TES, THE CREW DECIDED TO RETURN TO PHL. THE FLIGHT LANDED PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE YELLO W HYDRAULIC SYSTEM ELECTRIC PUMP AND THE PUMP DELIVERY CHECK VALVE. REF: OPER CONTROL NR 99ZZZX829. (X) 2 L 7 2 4F RT A28NM 1999030500719 19990305 00719 EU 1999 3 5 99ZZZX829 1 19981221 A 2913 ZCV6361 CHECK VALVE AIRBUS A319 A319112 EU HYDRAULIC SYS MALFUNCTIONED A USAA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 19 702UW 0896 PHL - FLT 8005 - AFTER TAKEOFF FROM PHL, THE YELLOW HYDRAULIC SYSTEM OVERHEATED. WHEN THE CONDITION EXISTED FOR 10 MINU TES, THE CREW DECIDED TO RETURN TO PHL. THE FLIGHT LANDED PHL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE YELLO W HYDRAULIC SYSTEM ELECTRIC PUMP AND THE PUMP DELIVERY CHECK VALVE. REF: OPER CONTROL NR USAASA98003. 2 L 7 2 4F RT A28NM 1999030500720 19990305 00720 EU 1999 3 5 DKAA98028 1 19981214 A 5280 MY2029310820 HINGE MY2029310F10 AMD FALCON FALCON20 2730103 EU LT MLG DOOR CRACKED A DKAA K NONE O OTHER IN INSP/MAINT 1 GL 23 230RA 230 LEFT MAIN LANDING GEAR LATERAL DOOR, AFT HINGE ARM, FOUND CRACKED DURING TERMINAL INSPECTION. CRACK IS ADJACENT TO FOLL OW-UP DOOR ATTACHMENT PIN AND BOSS. (X) 2 L 7 2 4F RT A7EU 1999030500721 19990305 00721 NE 1999 3 5 99ZZZX830 2 19981111 A 7230 COMPRESSOR LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 ENGINE DAMAGED A WRNA K NONE O OTHER IN INSP/MAINT 1 SO 05 310SS 35759 193C1096 10629 DURING A ROUTINE BORESCOPE INSPECTION, FOUND THE NR 3 ENGINE HIGH PRESSURE COMPRESSOR BLADES DAMAGED BEYOND THE MM LIMIT S. REMOVED AND REPLACED ENGINE IAW MAINTENANCE MANUAL 71-00-00 AND FORM 7104A. 2 L 7 3 4F 4 F A23WE E12EU 1999030500722 19990305 00722 WP 1999 3 5 99ZZZX831 1 19981110 A 3350 P207001214 LIGHT LKHEED 1011 10113851 5265010 WP GALLEY DISCHARGED A WRNA K NONE L NO TEST IN INSP/MAINT 1 SO 05 310SS 193C1096 DURING DAILY SERVICE CHECK, FOUND LOWER GALLEY EMERGENCY FLASHLIGHT WITH LOW BATTERY. REPLACED FLASHLIGHT IAW MM 25-60- 00. 2 L 7 3 4F A23WE 1999030500724 19990305 00724 WP 1999 3 5 CLCA9802 1 19981216 A 3610 13J55200JL CLAMP DOUG DC10 DC1040F 302508 WP NR 1 ENGINE LOOSE A CLCA C D ABORTED TAKEOFF RETURN TO BLOCK J WARNING INDICATION TO TAKEOFF 1 SO 19 610TF 46661 MIA/WI - FLT 085 - ABORTED TAKEOFF. ON TAKEOFF ROLL HAD NR 1 FIRE WARNING INDICATION. ABORTED TAKEOFF, PERFORMED CHECK LIST F/W LIGHT WENT OUT. UPON GROUND INSPECTION AT MIA, FOUND PDU SUPPLY DUCT CLAMP NOT INSTALLED PROPERLY WHICH ALLOW ED 13TH STAGE HOT AIR TO ESCAPE INTO THE COWL AREA. ACCOMPLISHED INSPECTION OF THE ENGINE AND COWLING. FOUND LT REVERS ER COWL SUFFERED HEAT DAMAGE AND THREE WIRES TO THE PROXIMITY SWITCH FOR THE T/R INDICATION. INSTALLING LOANER COWL PAN EL WHILE ORIGINAL PANEL IN SHOP FOR REPAIR, REPAIRING WIRING AS REQUIRED. (X) 2 L 7 3 4F TR A22WE 1999030500725 19990305 00725 NM 1999 3 5 99ZZZX833 1 19981104 A 3211 BEAM BOEING 757 75728A 1384976 NM RT/LT MLG FRACTURED A GUYF K NONE O OTHER IN INSP/MAINT 1 SO 23 757GA 8599 24260 RIGHT MAIN LANDING GEAR BEAM ASSY SNAPPED DURING BAGGAGE LOADING AND FUELING. FUEL ON BOARD: LEFT, 3,500 KILOS. CENTE R, 1,500 KILOS. RIGHT, 4,100 KILOS. RT MLG TRUCK BEAM FRACTURED. RT MLG ASSY, S/N 97572, REPLACED WITH SERVICEABLE UN IT, S/N 344MC73. LT MLG TRUCK ASSY REMOVED AS A RESULT OF INTERNAL CORROSION IN THE BEAM. TRUCK ASSY OVERHAULED BY MEN ASCO AVIATION SERVICES, CANADA. W/O 173427A. SERVICEABLE TRUCK ASSY, S/N 527UT48, FITTED AFTER O/H. BOTH RT AND LT BE AMS EXHIBITED SEVERE INTERNAL PITTING CORROSION. BOEING HAS BEEN ADVISED AND MENASCO AVIATION WILL PROVIDE TO GAC A REP ORT ON BOTH BEAMS. 2 L 7 2 4F RT A2NM 1999030500726 19990305 00726 CE 1999 3 5 99ZZZX834 1 19981029 A 3242 660033B7 BRAKE LEAR 35 31A 5170531 CE RT MLG FAILED A J7SA O OTHER B SMOKE/FUMES/ODORS/SPARKS CL CLIMB 1 SW 21 120FX 743 121 MAY964272 137 AT LIFT-OFF, PILOT HEARD A SCREECHING NOISE AND SMELLED A BURNING ODOR COMING FROM THE WHEELWELL. PILOT EXTENDED LANDIN G GEAR, PERFORMED A FLY-BY AT AUS AND PERFORMED A NON-EVENTFUL LANDING. INVESTIGATION REVEALED NO DAMAGE OTHER THAN THE NR 3 BRAKE ASSY CAME APART. REPLACED NR 3 AND NR 4 BRAKE AND WHEEL. CYCLES: 111. 2 L 7 2 4F RT A10CE 1999030500727 19990305 00727 EA 1999 3 5 MASA98229 1 19981223 A 3260 864806 PSEU CNDAIR CL600 CL6002B19 EA E/E BAY SERVICEABLE A MASA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 07 77195 7195 PHL/BHM - FLT 5760 - CREW REPORTED THE NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AN EMERGENCY WAS DECLARED, AN D THE AIRCRAFT WAS RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE RE-RACKED THE PSEU AND CLEARED THE FAULT CODES. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999030500728 19990305 00728 EU 1999 3 5 99ZZZX835 1 19981029 A 2910 326705 VALVE AIRBUS 320 A320214 EU HYDRAULIC SYS FAILED A RYNA O OTHER M OVER TEMP CR CRUISE 1 CE 07 716AW 716 MAN - FLT 0360 - YELLOW HYDRAULIC RESERVOIR OVERHEAT. REPLACED CHECK VALVE. NOTE: FAILED CHECK VALVE WAS DISCOVERED A FTER SECOND PUMP REPLACEMENT. (X) 2 L 7 2 4F RT A28NM 1999030500731 19990305 00731 EU 1999 3 5 SIMA983542 1 19981220 A 3350 8071BD86PL BULB SAAB SF340 340B 7860101 EU ROW 10B FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 354SB 340B354 LAX - EMERGENCY FLOOR PROXIMITY LIGHT AT ROW 10B DOES NOT ILLUMINATE. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT BULB. (X) 2 L 7 2 4T RT A52EU 1999030500732 19990305 00732 1999 3 5 USAASA98001 4 19981121 A 2565 CABLE AIRBUS A319 A319112 3930323 EU ESCAPE SLIDE TWISTED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 700UW 0885 RDU - FLIGHT ATTENDANT OPENED THE L1 DOOR WHILE IT WAS STILL ARMED. THE SLIDE FELL OUT OF THE DOOR PACK, BUT DID NOT I NFLATE. MAINTENANCE FOUND THE CABLING WAS ENTANGLED AROUND THE NECK OF THE GAS BOTTLE. THE SLIDE WAS INFLATED AND WORK ED PROPERLY. ALL OTHER DOORS ON ALL U.S. AIRWAYS OWNED AIRBUS AIRCRAFT WERE INSPECTED. THE PRE-OPS INSPECTION TEAM WAS NOTIFIED TO ADD THIS AS AN ITEM ON THEIR INSPECTION. (X) 2 L 7 2 4F RT A28NM 1999030500733 19990305 00733 EA 1999 3 5 99ZZZX838 1 19981215 A 3820 444007103 HEATING BLANKET CNDAIR CL600 CL6002B16 1900305 EA LAVATORY FAILED A UWUA H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 03 818LS 1589 5315 AFTER TAXI AND ENGINE SHUT DOWN WITH APU OPERATING, FLIGHT CREW NOTED STRONG ODOR FROM CABIN AREA. FURTHER INVESTIGATIO N REVEALED ODOR EMANATING FROM LAVATORY VANITY AREA. CREW IMMEDIATELY REMOVED ELECTRICAL POWER FROM AIRCRAFT. AIRCRAFT WAS SENT TO MAINTENANCE FACILITY FOR DETAILED INSPECTION. UPON VANITY ACCESS, PARTIAL DISASSEMBLY AND INSPECTION POTAB LE WATER HEATER BLANKET SEVERELY OVERHEATED. ALSO, NOTED WAS THE INTERNAL BLANKET WIRES WERE CHAFED BY CLAMP THAT SECUR ES HEATING BLANKET TANK ASSEMBLY TO STRUCTURE. MINOR REPAIRS WERE MADE TO DAMAGED INSULATION ADJACENT TO HEATING BLANKE T. SYSTEM DE-ACTIVATED PER MEL AND RELEASED. 2 L 7 2 4F RT A21EA 1999030500736 19990305 00736 EU 1999 3 5 99ZZZX840 1 19980924 A 6340 124110221 SWITCH BOLKMS 117 BK117A3 5626015 EU M/R DRIVE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 163BK 77 7063 THERMO SWITCH UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500739 19990305 00739 EU 1999 3 5 99ZZZX843 1 19980915 A 6420 ABWT82008 BEARING BOLKMS 117 BK117B1 5626012 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 17SJ 277 7230 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500740 19990305 00740 EU 1999 3 5 99ZZZX844 1 19980925 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105S 5626006 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 485EC 190 12972 S754 PRESSURE TRANSMITTER UNIT INOPERATIVE. INDICATOR PEGGED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3EU 1999030500741 19990305 00741 EU 1999 3 5 99ZZZX845 1 19981013 A 2840 DK040 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 825LF 76 8228 796 PRESSURE TRANSMITTER UNIT INOPERATIVE. NR 2 ENGINE OIL PRESSURE INDICATED IN GREEN WHILE ENGINE WAS NOT RUNNING. REPLA CED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999030500742 19990305 00742 EU 1999 3 5 99ZZZX846 1 19981118 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105NC 62 12734 790 PRESSURE TRANSMITTER UNIT INOPERATIVE. NR 2 ENGINE FUEL PRESSURE INDICATES ERRATICALLY DURING FLIGHT. REPLACED WITH NE W UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999030500743 19990305 00743 NM 1999 3 5 99ZZZX847 1 19981209 A 6230 900C2010183107 LINK ASSY DOUG MD900 MD900 3027375 NM MAIN ROTOR LOOSE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 653 90000012 LINK ASSY, DRIVE-SCISSORS, EXCESSIVE PLAY AT HIGH SPEED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999030500744 19990305 00744 NM 1999 3 5 99ZZZX848 1 19981114 A 2810 900P3663121101 SHROUD DOUG MD900 MD900 3027375 NM FUEL CELL LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 901CF 2471 90000012 VAPOR SHROUD LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999030500745 19990305 00745 NM 1999 3 5 99ZZZX849 1 19981111 A 6720 900R2442012103 BLADE DOUG MD900 MD900 3027375 NM NOTAR CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 901CF 338 0081580326 90000012 BLADE ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H19NM 1999030500746 19990305 00746 EU 1999 3 5 99ZZZX850 1 19980907 A 6320 6607A2114 SWITCH BOLKMS 105 BO105LSA3 5626020 EU OIL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202LF 104 W54431 2014 OIL PRESSURE WARNING SWITCH INOPERATIVE. WILL NOT TURN OFF MAIN TRANSMISSION PRESSURE WARNING LIGHT. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H3AU 1999030500747 19990305 00747 EU 1999 3 5 99ZZZX851 1 19980826 A 7110 1172310112 BALL PIN BOLKMS 117 BK117A3 5626015 EU COWL WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 258 7017 BALL PIN WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500748 19990305 00748 EU 1999 3 5 99ZZZX852 1 19980912 A 6420 ABWT82008 BEARING BOLKMS 117 BK117B1 5626012 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5194C 412 7169 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500749 19990305 00749 EU 1999 3 5 99ZZZX853 1 19981022 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911BY 165 7127 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999030500750 19990305 00750 EU 1999 3 5 99ZZZX854 1 19980805 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 825LF 133 12956 796 PRESSURE TRANSMITTER UNIT INOPERATIVE. INDICATOR PEGGS AT RED LINE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999030500751 19990305 00751 EU 1999 3 5 99ZZZX855 1 19980912 A 6220 134616P BUSHING BOLKMS 117 BK117A3 5626015 EU T/R HUB WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 426 7017 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999031200245 19990312 00245 EU 1999 3 12 CA980707010 1 19980616 A 2820 HC282H0131001 LINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUEL SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 24472 LF05463A (CAN) A FUEL LEAK FOUND AT NR 4 PYLON. THE LEAK WAS FROM THE FUEL FEED CONNECTOR PIPE. 'O' RING FLATTENED ALLOWING PIP E TO CHAFE. PART TC: 27,583. 2 H 7 4 4F 4 F RT A49EU E6NE 1999031200253 19990312 00253 EU 1999 3 12 CA980713025 1 19980101 A 2711 57935001 ACTUATOR ISRAEL 1124 1124 4500102 EU AILERON FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 327 1206 (CAN) AILERON GAUGE FLUTTER REPORTED. AILERON TRIM ACTUATOR REPLACED. 2 M 7 2 4F A2SW 1999031200254 19990312 00254 NM 1999 3 12 CA980714029 1 19980702 A 7603 87600520001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 120304 (CAN) RIGHT HAND CONDITION CABLE FOUND FRAYED WHERE IT PASSES THROUGH THE FIREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999031200255 19990312 00255 NM 1999 3 12 CA980714030 1 19980702 A 7603 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 120304 (CAN) LEFT HAND CONDITION CABLE FOUND FRAYED WHERE IT PASSES THROUGH THE FIREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999031200256 19990312 00256 EU 1999 3 12 CA980720013 1 19980720 A 3246 AH52689 WHEEL BAG JETSTM JETSTM3212 1500217 EU ROTOL R333 R333482F12 GL LT MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) ON PRE-FLIGHT, CREW FOUND THE LEFT MAIN INNER WHEEL ASSY CRACKED AT THE TIRE BEAD FLANGE. 2 L 7 2 4T RT BA15CAA 6 C P61GL 1999031200257 19990312 00257 CE 1999 3 12 CA980720016 1 19980626 A 7830 U183238001 SOLENOID 556581035 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE THRUST REVERSER STICKING W K NONE O OTHER IN INSP/MAINT 1 CA 2955 71747 (CAN) AFTER LANDING AND RT THRUST REVERSER FULLY DEPLOYED, THE PILOT COULD NOT INCREASE POWER FOR REVERSE USING THE TR C ONTROL LEVER. THE DEPLOY INTERLOCK SOLENOID PLUNGER REMAINED IN THE LOCK-OUT POSITION, PREVENTING LEVER FROM MOVING TO THE POWER UP POSITION. PLUNGER WAS STICKING INSIDE THE RECEIVING HOLE. 1 L 7 2 4F 4 F A22CE E1NE 1999031200258 19990312 00258 NM 1999 3 12 CA980721020 1 19980711 A 2710 82710097101 SPRING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AILERON CONTROL WEAK W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 120370 (CAN) WHEN RIGHT WHEEL CONTACTED RUNWAY, THE AILERON ROLL SPOILER (RIGHT AND LEFT CONTROL WHEELS) SPLIT. RD 8-53-3620 I SSUE NR 2 HAD BEEN COMPLETED. SUSPECT A WEAK CLUTCH SPRING. GREASE ALSO FOUND ON AND IN CLUTCH MECHANISM-IT SHOULDN'T BE THERE. SUBMITTER STATED FLEET CAMPAIGN TO BE DONE PER SB 8-27-79. 2 H 7 2 4T 4 T RT A13NM E20NE 1999031200265 19990312 00265 EU 1999 3 12 CA980825002 1 19980810 A 3221 NAS620415 BOLT BAG JETSTM JETSTM3212 1500217 EU ROTOL R333 R333482F12 GL NLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 15014 (CAN) AT 200-HOUR INSPECTION OF THE ATTACHMENT BOLTS OF THE NOSE GEAR RETRACTION JACK UPPER BRACKET, THE LEFT UPPER BOLT WAS FOUND BROKEN OFF WHERE THE BOLTS EXTEND OUT THROUGH THE BRACKET ON THE NUT END OF THE BOLT. BRACKET P/N 1371291C2 . PART TC: 19,282. 2 L 7 2 4T RT BA15CAA 6 C P61GL 1999031200267 19990312 00267 SO 1999 3 12 CA980825010 1 19980811 A 3260 MS272402 SWITCH EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA RT MLG OUT OF ADJUST W L ABORTED APPROACH J WARNING INDICATION AP APPROACH 1 CA PCE51708 (CAN) ON APPROACH, GEAR SELECTED DOWN AND DID NOT RECEIVE GREEN DOWN AND LOCKED FOR THE RIGHT HAND MAIN. GEAR CYCLED AN D WAS OK. GEAR MICROSWITCH FOUND OUT OF ADJUSTMENT. 1 L 7 2 4T 4 T A21SO E4EA 1999031200269 19990312 00269 NM 1999 3 12 CA980908015 1 19980823 A 7922 AL00601 ACTUATOR 8714030003 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE LT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 123010 (CAN) CREW REPORTED THE LEFT ENGINE BYPASS DOOR WOULD NOT OPEN. INTAKE BYPASS DOOR ACTUATOR FOUND FAILED. SHAFT HAD SH EARED OFF. LOOKS LIKE FATIGUE CRACK COMING FROM INTERNAL THREADS OF SHAFT THAT HOLDS ROD. 2 H 7 2 4T 4 T RT A13NM E20NE 1999031200325 19990312 00325 EU 1999 3 12 QXEA9900192 1 19980103 A 5347 SEAT TRACK FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - THERE ARE TWO AREAS OF LIGHT PITTING CORROSION ON THE OUTBOARD FLOOR SUPPORT FLANGE OF THE RIGHT OUTBOARD SEAT TRA CK BETWEEN FRAMES 10966 AND 11905. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 8-9 AND PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999031200329 19990312 00329 EU 1999 3 12 QXEA9900196 1 19981228 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - UPPER FUSELAGE UPPER NAV/COMM ANTENNA BASE PLATE ON FUSELAGE SKIN HAS PITTING CORROSION AROUND FEED THROUGH HOLES. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999031200330 19990312 00330 EU 1999 3 12 QXEA9900197 1 19981228 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - UPPER FUSELAGE UPPER TCAS ANTENNA, FUSELAGE SKIN BASE PLATE HAS MINOR SURFACE CORROSION. REPAIRED IAW FOKKER SRM 51-10-04, PAGE 9, PARAGRAPH B AND C. 2 L 7 2 4F RT A20EU 1999031200333 19990312 00333 EU 1999 3 12 QXEA9900200 1 19981229 A 5320 SUPPORT FOKKER F28 F28MK4000 4990810 EU FRAME 3450-3820 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - CRACKED FLOOR SUPPORT AT BL1390 RT BETWEEN FRAMES 3450 AND 3820. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAG RAPH 7B. 2 L 7 2 4F RT A20EU 1999031200338 19990312 00338 EU 1999 3 12 QXEA9900205 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 10346 CASTELLATION IS CRACKED AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200339 19990312 00339 EU 1999 3 12 QXEA9900206 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10346 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 10346 CASTELLATION IS CRACKED AT STRINGER 44. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200340 19990312 00340 EU 1999 3 12 QXEA9900207 1 19981225 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 10966 CASTELLATION IS CRACKED AT STRINGER 34. REPAIRED IAW FOKKER SRM 53-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200341 19990312 00341 EU 1999 3 12 QXEA9900208 1 19981225 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 10966 CASTELLATION IS CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200342 19990312 00342 EU 1999 3 12 QXEA9900209 1 19981226 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 10966 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 10966 CASTELLATION CRACKED AT STRINGER 43. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200343 19990312 00343 EU 1999 3 12 QXEA9900210 1 19980106 A 5220 DOOR FOKKER F28 F28MK4000 4990810 EU RT EMER EXIT DAMAGED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - RIGHT OVERWING AFT EMERGENCY EXIT GOUGED AT UPPER TORSION BOX. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13, PARAGRA PH 7 AND SRM 51-31-05, PAGE 9, PARAGRAPH 7. 2 L 7 2 4F RT A20EU 1999031200347 19990312 00347 EU 1999 3 12 QXEA9900214 1 19981227 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200348 19990312 00348 EU 1999 3 12 QXEA9900215 1 19981227 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12045 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200349 19990312 00349 EU 1999 3 12 QXEA9900216 1 19981227 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 45. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200350 19990312 00350 EU 1999 3 12 QXEA9900217 1 19981227 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 33. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200351 19990312 00351 EU 1999 3 12 QXEA9900218 1 19981227 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 30. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200352 19990312 00352 EU 1999 3 12 QXEA9900219 1 19981227 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12405 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12405 CASTELLATION CRACKED AT STRINGER 46. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200353 19990312 00353 EU 1999 3 12 QXEA9900220 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 43. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200354 19990312 00354 EU 1999 3 12 QXEA9900221 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 44. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200355 19990312 00355 EU 1999 3 12 QXEA9900222 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 45. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PAG E 13, PARAGRAPH 7A, STEPS 1-5. 2 L 7 2 4F RT A20EU 1999031200356 19990312 00356 EU 1999 3 12 QXEA9900223 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 46. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, SRM 51-31-01, PAGE 1 3, PARAGRAPH 7A, STEPS 1-5 AND SRM 51-30-02. 2 L 7 2 4F RT A20EU 1999031200357 19990312 00357 EU 1999 3 12 QXEA9900224 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200358 19990312 00358 EU 1999 3 12 QXEA9900225 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 12875 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 12875 CASTELLATION CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PAG E 13, PARAGRAPH 7A, STEPS 1-5. 2 L 7 2 4F RT A20EU 1999031200361 19990312 00361 EU 1999 3 12 QXEA9900228 1 19981228 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 49A. REPAIRED IAW FOKKER SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200362 19990312 00362 EU 1999 3 12 QXEA9900229 1 19981229 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200363 19990312 00363 EU 1999 3 12 QXEA9900230 1 19981229 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200364 19990312 00364 EU 1999 3 12 QXEA9900231 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01, PAG E 13, PARAGRAPH 7A, STEPS 1-5. 2 L 7 2 4F RT A20EU 1999031200365 19990312 00365 EU 1999 3 12 QXEA9900232 1 19981229 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13345 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13345 CASTELLATION CRACKED AT STRINGER 29A. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2 AND SRM 51-31-01. 2 L 7 2 4F RT A20EU 1999031200367 19990312 00367 EU 1999 3 12 QXEA9900234 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 35. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200368 19990312 00368 EU 1999 3 12 QXEA9900235 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 36. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2, SRM 51-31-01, PAGE 1 3, PARAGRAPH 7A, STEPS 1-5. 2 L 7 2 4F RT A20EU 1999031200369 19990312 00369 EU 1999 3 12 QXEA9900236 1 19981231 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815 CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200418 19990312 00418 CE 1999 3 12 99ZZZX871 1 19981208 A 2400 97524048603 CIRCUIT BEECH 100 B100 1152919 CE COCKPIT PEDESTAL DAMAGED A RA0A O OTHER B SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 EA 17 818PA BE18 UPON FINAL APPROACH INTO DES MOINES, IOWA, CREW NOTICED SMOKE EMITTING FROM CENTER PEDESTAL. CREW TOOK APPROPRIATE ACTI ON AND SHUT OFF ELECTRICAL POWER AS NEEDED. MAINTENANCE PERSONNEL FOUND SOURCE OF SMOKE TO BE SHORTED PRINTED CIRCUIT B OARD. AREA AND BOARD WERE CLEANED. CIRCUIT BOARD WAS RE-INSTALLED AND OPS CHECKED SATISFACTORY AND AIRCRAFT WAS RETURN ED TO SERVICE. SUBMITTER STATED POSSIBLE CAUSE WAS LIQUID SUBSTANCE SPILLED AND ENTERED PEDESTAL AND RECOMMENDED LIQUID FILLED CUPS, ETC., NOT BE PLACED ON PEDESTAL, BUT IN CUPHOLDERS. 1 L 7 2 4T A14CE 1999031200476 19990312 00476 EU 1999 3 12 QXEA9900239 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815A CASTELLATION CRACKED AT STRINGER 57. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200477 19990312 00477 EU 1999 3 12 QXEA9900240 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815A CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200478 19990312 00478 EU 1999 3 12 QXEA9900241 1 19981224 A 5311 CASTALLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815A CASTELLATION CRACKED AT STRINGER 28A. REPAIRED IAW FOKKER SRM 51-31-10 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200479 19990312 00479 EU 1999 3 12 QXEA9900242 1 19981226 A 5311 CASTALLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 28A. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1-5 AND SRM 53-02-13 FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200480 19990312 00480 EU 1999 3 12 QXEA9900243 1 19981226 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 29. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1 -5 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200482 19990312 00482 EU 1999 3 12 QXEA9900245 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 23. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200483 19990312 00483 EU 1999 3 12 QXEA9900246 1 19981226 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 42. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1 -5 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200484 19990312 00484 EU 1999 3 12 QXEA9900247 1 19981226 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 13815 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 13815B CASTELLATION CRACKED AT STRINGER 45. REPAIRED IAW FOKKER SRM 51-31-01, PAGE 13 PARAGRAPH 7A, ITEMS 1 -5 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200485 19990312 00485 EU 1999 3 12 QXEA9900248 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 54. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200486 19990312 00486 EU 1999 3 12 QXEA9900249 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 56. REPAIRED IAW FOKKER SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200487 19990312 00487 EU 1999 3 12 QXEA9900250 1 19981224 A 5311 CASTELLATION FOKKER F28 F28MK4000 4990810 EU FRAME 15205 CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FRAME 15205 CASTELLATION CRACKED AT STRINGER 47. REPAIRED IAW FOKKER SRM 51-31-01 AND SRM 53-02-13, FIGURE 2. 2 L 7 2 4F RT A20EU 1999031200501 19990312 00501 EU 1999 3 12 QXEA9900264 1 19981230 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - VHF COMM AFT LOWER ANTENNA/FUSELAGE SKIN MOUNT AREA HAS SMALL AREA OF LIGHT SURFACE CORROSION AT AFT EDGE. REPAIR ED IAW FOKKER SRM 51-10-04. 2 L 7 2 4F RT A20EU 1999031200502 19990312 00502 EU 1999 3 12 QXEA9900265 1 19981231 A 5330 PLATE FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LOWER VHF COMM ANTENNA BASE PLATE HAS MINOR LIGHT SURFACE CORROSION AROUND FEED THROUGH HOLE. REPAIRED IAW FOKKER SRM 53-01-01 AND SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999031200503 19990312 00503 EU 1999 3 12 QXEA9900266 1 19981230 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - NR 2 DME ANTENNA/FUSELAGE SKIN MOUNT HAS PITTING CORROSION AROUND SCREW HOLES ON SKIN. REPAIRED IAW FOKKER SRM 51 -10-04, PAGE 8. 2 L 7 2 4F RT A20EU 1999031200506 19990312 00506 EU 1999 3 12 QXEA9900269 1 19981223 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR MISSING A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AFT CARGO DOOR OUTER SKIN, OUTER LAYER IS CRACKED/BROKEN AND MISSING 1.5 X .375 NEXT TO HINGE ON LEFT-HAND SIDE. R EPAIRED IAW FOKKER SRM 52-02-01 PAGE 2, FIGURE 2 AND MM 53-00-00 PAGE 2. 2 L 7 2 4F RT A20EU 1999031200514 19990312 00514 EU 1999 3 12 QXEA9900277 1 19981230 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FUSELAGE SKIN CRACKED AT LOWER FORWARD CORNER OF PILOTS SLIDING WINDOW APERTURE AT NR 2 WINDOW POST. REPAIRED IAW HORIZON AIR EA 4-53-632. 2 L 7 2 4F RT A20EU 1999031200515 19990312 00515 EU 1999 3 12 QXEA9900278 1 19981230 A 5330 SKIN FOKKER F28 F28MK4000 4990810 EU FUSELAGE CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - LIGHT SURFACE CORROSION AROUND SEVERAL NUT PLATE RIVETS OF REAR RAD ALT ANTENNA MOUNT, FORWARD BLANKING FUSELAGE S KIN CUTOUT HAS MINOR PITTING CORROSION AROUND MOUNT FLANGE. REPAIRED IAW FOKKER SRM 53-01-01. 2 L 7 2 4F RT A20EU 1999031200521 19990312 00521 EU 1999 3 12 QXEA9900296 1 19981227 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 7305 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FORWARD CARGO COMPARTMENT FRAME 7305 IS CORRODED AT INTERSECTION WITH STRINGER 74. REPAIRED IAW FOKKER SRM 53-02- 12, PAGE 9, FIGURE 3, SRM 51-31-01 AND 51-31-05. 2 L 7 2 4F RT A20EU 1999031200523 19990312 00523 EU 1999 3 12 QXEA9900298 1 19981231 A 6320 FRAME FOKKER F28 F28MK4000 4990810 EU CARGO DOORWAY DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - FORWARD CARGO DOOR APERTURE FRAME DENTED AND SLIGHTLY PROTRUDING INTO APERTURE. REPAIRED IAW FOKKER SRM 53-02-16, FIGURE 1. 2 L 7 2 4F RT A20EU 1999031200524 19990312 00524 EU 1999 3 12 QXEA9900299 1 19981224 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - AFT CARGO DOOR HAS A SMALL DENT ON THE FORWARD EDGE. REPAIRED IAW FOKKER SRM 52-01-01, PAGE 7. 2 L 7 2 4F RT A20EU 1999031200529 19990312 00529 EU 1999 3 12 QXEA9900304 1 19981228 A 5311 FRAME FOKKER F28 F28MK4000 4990810 EU FRAME 6805 CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 499US 11182 PDX - EXFOLIATION CORROSION AROUND NUT PLATES ON FRAME 6805 ABOVE STRINGER 73 AND 74. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1999031200600 19990312 00600 EU 1999 3 12 QXEA9900290 1 19981231 A 5320 CHANNEL FOKKER F28 F28MK4000 4990810 EU FUSELAGE CRACKED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - INBOARD V-CHANNEL ATTACH POINT FOR PANEL 92L IS CRACKED AT FORWARD POINT APPROXIMATELY 6 IN LENGTH. REPAIRED IAW FOKKER SRM 53-02-17, PAGE 10. 2 L 7 2 4F RT A20EU 1999031200663 19990312 00663 EU 1999 3 12 99ZZZX890 1 19980918 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A3 5626015 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 158BK 396 7058 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999031200664 19990312 00664 EU 1999 3 12 99ZZZX891 1 19980912 A 6410 134617P BUSHING BOLKMS 117 BK117A3 5626015 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 951AM 426 7017 TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999031200665 19990312 00665 EU 1999 3 12 99ZZZX892 1 19981105 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A3 5626015 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 424MB 256 7082 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999031200666 19990312 00666 EU 1999 3 12 99ZZZX893 1 19980817 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 161 7125 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999031200667 19990312 00667 EU 1999 3 12 99ZZZX894 1 19980729 A 6420 ABWT82008 BEARING BOLKMS 117 BK117A4 5626017 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 586BH 91 7129 BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999031200668 19990312 00668 NE 1999 3 12 HCMA0000227 2 19980922 A 7421 9550166670 IGNITER SNIAS 350 AS350B2 8680813 EU TMECA ARRIEL ARRIEL1D NE ENGINE WORN A HCMA K NONE O OTHER IN INSP/MAINT 1 WP 13 995BH 1546 2987 9512 IGNITER IS WORN BEYOND LIMITS. (X) 1 G 7 1 3U 3 U H9EU E19EU 1999031200675 19990312 00675 SW 1999 3 12 99ZZZX901 1 19981224 A 6210 206015001107 BLADE BELL 206 206L1 1182107 SW MAIN ROTOR CRACKED A S A ZV1A K NONE O OTHER IN INSP/MAINT 1 SW 03 577E 2522 A2273 45577 DURING DAILY INSPECTION, FOUND CRACK 1.75 INCHES LONG COMING FROM DOUBLER ON LOWER SIDE OF BLADE. THERE IS A DELAMINATI ON AREA FROM EDGE OF CRACK AFT APPROXIMATELY 1 INCH AND APPROXIMATELY .50 INCH UNDER DOUBLER. BLADE REMOVED FOR REPAIR. 1 G 7 1 3U H2SW 1999031200676 19990312 00676 1999 3 12 VTZA98378 4 19981129 A 3418 601R591521 COMPUTER CNDAIR CL600 CL6002B19 EA E/E COMPARTMENT FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION TO TAKEOFF 1 EA 27 620BR 7179 IAD/BNA - FLT 6700 - DURING TAKEOFF AT 0825 HRS ON 11-29-98, AIRCRAFT MADE AN UNSCHEUDLED LANDING DUE TO STALL WARNING M ESSAGE ILLUMINATED ON EICAS. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4F RT A21EA 1999031200745 19990312 00745 NE 1999 3 12 REXA98120 2 19981223 A 7421 5044T67P07 IGNITOR SAAB SF340 340B 7860101 EU GE CT7TP CT75A2 30030 NE RT ENGINE MALFUNCTIONED A REXA E ENGINE SHUTDOWN X ENGINE FLAMEOUT CL CLIMB 1 SO 25 369PX 340B295 GEE785370 RIGHT ENGINE FAILED SHORTLY AFTER TAKEOFF. NO ABNORMAL INDICATIONS. PERFORMED BORESCOPE INSPECTION OF RIGHT ENGINE COM PRESSOR AND HOT SECTION. NO DEFECTS NOTED. REMOVED AND REPLACED INBOARD AND OUTBOARD IGNITOR PLUGS. (M) 2 L 7 2 4T 4 T RT A52EU E8NE6 1999031200755 19990312 00755 WP 1999 3 12 ORJA9956 1 19981016 A 3350 BR9665103 LIGHT DOUG DC9 DC983 3022083 WP AIRSTAIR CORRODED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, CORROSION IN LOWER BATTERY POWERED EMERGENCY LIGHT FOR AFT AIRSTAIR. REMOVED AND REPLACED LOWER EMERGENCY EXIT 1D/FLOOD LIGHT. TESTED EMERGENCY LIGHT IN AFT AIRSTAIR IAW BRUCE INDUSTRIES MANUAL 400-082. (M) 2 L 7 2 4F RT A6WE 1999031200756 19990312 00756 WP 1999 3 12 ORJA9955 1 19981010 A 5320 BRACKET DOUG DC9 DC983 3022083 WP A/C BAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, SUPPORT BRACKET MOUNT POINT CORRODED ON LEFT HEAT EXCHANGER AFT SHROUD AFT LOWER EDGE. FABRICATED, TREATED AND PRIMED. INSTALLED NEW BRACKET IAW DC-9 SRM 51-10-2, 51-10-3. (M) 2 L 7 2 4F RT A6WE 1999031200757 19990312 00757 WP 1999 3 12 ORJA9954 1 19981010 A 5320 ANGLE DOUG DC9 DC983 3022083 WP LAVATORY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, FORWARD LAV, FORWARD BULKHEAD LOWER AFT ANGLE CORRODED. REMOVED FORWARD LAV LEFT. FABRICATED NEW ANGLE AND REP LACED LEFT FORWARD LAV IAW MD-80, MM 25-42-00. OPS CHECKED LAV IAW MD-80, MM 25-42-00. OPS CHECKED LAV IAW MD-80, MM 2 5-42-00. (M) 2 L 7 2 4F RT A6WE 1999031200758 19990312 00758 WP 1999 3 12 ORJA9953 1 19981006 A 5320 WEB DOUG DC9 DC983 3022083 WP BS 1271-1309 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, CUSP WEB AT FUSELAGE, STATION 1271-1309, HAS CORROSION AND CRACK. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AN D FILLER ON CUSP WEB AT FUSELAGE, STATION 1721-1309 IAW DC-9 SRM 53-01-2. (M) 2 L 7 2 4F RT A6WE 1999031200759 19990312 00759 WP 1999 3 12 ORJA9952 1 19981006 A 5347 S00483B11800 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1172-1309 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, CABIN SEAT TRACK X44L, STATION 1174 TO 1309 HAS NUMEROUS AREAS OF CORROSION OUT OF LIMITS PER DC-9 SRM 53-05. R EMOVED AND REPLACED SEAT TRACK IAW DC-9 SRM 51-10-3, 51-10-4, 51-30-1, 51-30-2, 51-30-7, 53-05. (M) 2 L 7 2 4F RT A6WE 1999031200760 19990312 00760 WP 1999 3 12 ORJA9951 1 19981006 A 5347 S00483B11800 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1174 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, CABIN SEAT TRACK X54L, STATION 1174 TO 1309 HAS NUMEROUS AREAS OF CORROSION OUT OF LIMITS PER DC-9 SRM 53-05. R EMOVED AND REPLACED SEAT TRACK IAW DC-9 SRM 51-10-1, 51-10-3, 51-30-1, 51-30-2, 51-10-4, 53-05. (M) 2 L 7 2 4F RT A6WE 1999031200761 19990312 00761 WP 1999 3 12 ORJA9950 1 19981006 A 5347 S00483B11800 SEAT TRACK DOUG DC9 DC983 3022083 WP BS 1174 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, CABIN SEAT TRACK X22L, STATION 1174 TO 1309 HAS NUMEROUS AREA OF CORROSION OUT OF LIMITS PER DC9, SRM 53-05. RE MOVED AND INSTALLED NEW SEAT TRACK IAW DC-9 SRM 53-05. (M) 2 L 7 2 4F RT A6WE 1999031200762 19990312 00762 WP 1999 3 12 ORJA9948 1 19981019 A 5320 FRAME DOUG DC9 DC983 3022083 WP CARGO DOORWAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 836RA 53046 IN OKC, LEVEL 2 CORROSION AT MID PIT DOOR LOWER FRAME HAS CORROSION AT FORWARD AND AFT ENDS. REMOVED CORROSION FOUND FO RWARD AREA OUT OF LIMITS REPAIRED IAW DC-9 SRM 53-05 FIG 63 TREATED AND PRIMED AREA IAW DC-9 SRM 51-10-2. REINSTALLED K ICK PLATE FORWARD SECTION IAW DC-9 SRM 51-30-1 LEAK CHECK GOOD IAW MD-80 MM 21-32-00. (M) 2 L 7 2 4F RT A6WE 1999031200763 19990312 00763 NM 1999 3 12 99ZZZM169 1 19981230 A 3230 65807379 LINK BOEING 737 737247 138448D NM RT MLG CRACKED A PIDA K NONE O OTHER IN INSP/MAINT 1 SO 05 487GS 47030 19600 RIGHT MAIN LANDING GEAR SWING LINK ASSY FOUND CRACKED DURING MAIN LANDING CHANGE, P/N 65-80737-9. REPLACED LINK ASSY WI TH NEW LINK ASSY P/N 65-90737-1391, INSTALLED IAW B737MM 57-13-0 AND DRAWING 65C22640. (M) 2 L 7 2 4F A16WE 1999031200804 19990312 00804 NM 1999 3 12 CLCA9902 1 19980929 A 5730 112N410524 PANEL BOEING 757 75723APF 1384966 NM WS 481.5 CORRODED A CLCA K NONE O OTHER IN INSP/MAINT 1 SO 19 572CA 24868 ON 9-29-98 DURING ROUTINE 'A' CHECK, FOUND CORROSION AT THE RIGHT FUELING STATION WS 481.50, BOEING AUTHORIZED CAC TO CO NTINUE OPERATIONS WITH REPEAT INSPECTIONS AT 450 HOURS UNTIL C-CHECK. ACCOMPLISHED FLEET CAMPAIGN WITH NO OTHER FINDING S. ON 1/18/99 AT C-CHECK BOEING PROVIDED REPAIR INFORMATION, AEROMAN THE C-CHECK PROVIDER DEVELOPED AN ENGINEERING ORDE R BASED UPON THE BOEING REPAIR INFORMATION. ON 1/22/99 COMPLETED REPAIR IAW BOEING INFORMATION AND AEROMAN ENGINEERING ORDER AND 8110-2 ATTACHED. (M) 2 L 7 2 4F RT A2NM 1999031200841 19990312 00841 NM 1999 3 12 MZZA99009 1 19981227 A 7603 BCREF3259 CONTROL CABLE BOEING 727 7272F9 138407D NM BS 1188 BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 2 ENGINE THRUST CONTROL CABLE (T2A) AT BS 1188. THE DAMAGED CABLE ASSEMBLY, P/N BCREF13259 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATION CHEC K FUOND SATISFACTORY. (M) 2 L 7 3 4F RT A3WE 1999031200842 19990312 00842 NM 1999 3 12 MZZA99008 1 19981227 A 7603 6132155D3KJ2496 CONTROL CABLE BOEING 727 7272F9 138407D NM BS 1186 BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK, INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 1 ENGINE START CONTROL CABLE AT BS 1186. THE DAMAGED CABLE ASSY, P/N 61-32155D3KJ2496 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATION CHECK FO UND SATISFACTORY. (M) 2 L 7 3 4F RT A3WE 1999031200843 19990312 00843 NM 1999 3 12 MZZA99010 1 19981227 A 7603 6132155D3KJ2496 CONTROL CABLE BOEING 727 7272F9 138407D NM BS 1186 BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 3 ENGINE START CONTROL CABLE AT BS 1 186. THE DAMAGED CABLE ASSY, P/N 61-32155D3KJ2496 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATION CHECK FOU ND SATISFACTORY. (M) 2 L 7 3 4F RT A3WE 1999031200844 19990312 00844 NM 1999 3 12 MZZA99011 1 19981227 A 7603 6132155D3KJ2069 CONTROL CABLE BOEING 727 7272F9 138407D NM BS 1190 BROKEN A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, EXCESSIVE BROKEN WIRES WAS FOUND ON NR 3 ENGINE THRUST CONTROL CABLE (T3A) AT BS 1190. THE DAMAGED CABLE ASSEMBLY, P/N 61-32155D3KJ2069 WAS REMOVED AND REPLACED PER B727 MM 76-11-11 AND OPERATIO N CHECK FOUND SATISFACTORY. (M) 2 L 7 3 4F RT A3WE 1999031200845 19990312 00845 NM 1999 3 12 MZZA99012 1 19981229 A 5711 SPAR WEB BOEING 727 7272F9 138407D NM CENTER WING CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK WAS FOUND ON WING CENTER SECTION REAR SPAR WEB AT WL 185 FROM RBBL 2 TO RBBL 4. THE WING CENTER SECTION REAR SPAR WEB CRACK END WAS STOP DRILLED AND REPAIRED PER EA 5750-01843 OP 3. (M) 2 L 7 3 4F RT A3WE 1999031200846 19990312 00846 NM 1999 3 12 MZZA99013 1 19981222 A 3350 10617891008 SIGN BOEING 727 7272F9 138407D NM EMERGENCY DOOR MALFUNCTIONED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, RIGHT FORWARD EMERGENCY EXIT DOOR 'PULL' SI GN BRIGHTNESS MEASUREMENT WAS FOUND BELOW THE SPECIFIED LIMIT. THE 'PULL' SIGN P/N 10-61789-1008 WAS REMOVED AND REPLAC ED PER B727 MM 33-50-31. (M) 2 L 7 3 4F RT A3WE 1999031200847 19990312 00847 NM 1999 3 12 MZZA99014 1 19981222 A 3350 10617891008 SIGN BOEING 727 7272F9 138407D NM EMERGENCY DOOR MALFUNCTIONED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING SELF ILLUMINATION SIGN BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, RIGHT AFT EMERGENCY EXIT DOOR 'PULL' SIGN B RIGHTNESS MEASUREMENT WAS FOUND BELOW THE SPECIFIED LIMIT. THE 'PULL' SIGN P/N 10-61789-1008 WAS REMOVED AND REPLACED P ER B727 MM 33-50-31. (M) 2 L 7 3 4F RT A3WE 1999031200848 19990312 00848 NM 1999 3 12 MZZA99015 1 19981222 A 3350 10617891007 SIGN BOEING 727 7272F9 138407D NM EMERGENCY DOOR MALFUNCTIONED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING SELF ILLUMINATION BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, LEFT FORWARD EMERGENCY EXIT DOOR 'EMERGENCY' AND 'PULL' SIGN BRIGHTNESS MEASUREMENT WERE FOUND BELOW THE SPECIFIED LIMIT. THE 'EMERGENCY' SIGN P/N 10-61789-1007 AND 'P ULL' SIGN P/N 10-61789-1008 WERE REMOVED AND REPLACED PER B727 MM 33-50-31. (M) 2 L 7 3 4F RT A3WE 1999031200849 19990312 00849 NM 1999 3 12 99ZZZM181 1 19981222 A 3350 10617891008 SIGN BOEING 727 7272F9 138407D NM EMERGENCY DOOR MALFUNCTIONED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING SELF ILLUMINATION BRIGHTNESS TEST ON AIRCRAFT AT AIR ASIA, LEFT FORWARD EMERGENCY EXIT DOOR 'EMERGENCY' AND 'PULL' SIGN BRIGHTNESS MEASUREMENT WERE FOUND BELOW THE SPECIFIED LIMIT. THE 'EMERGENCY' SIGN P/N 10-61789-1007 AND 'P ULL' SIGN P/N 10-61789-1008 WERE REMOVED AND REPLACED PER B727 MM 33-50-31. (M) 2 L 7 3 4F RT A3WE 1999031200850 19990312 00850 NM 1999 3 12 MZZA99018 1 19981230 A 3350 S104 BATTERY BOEING 727 7272F9 138407D NM CABIN DISCHARGED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERIES WERE FOUND INOPERATIVE. THE BATTERIES, P/N S104 AND 106 WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. (M ) 2 L 7 3 4F RT A3WE 1999031200851 19990312 00851 NM 1999 3 12 99ZZZM182 1 19981230 A 3350 S106 BATTERY BOEING 727 7272F9 138407D NM CABIN DISCHARGED A MZZA K NONE L NO TEST IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, PASSENGER CABIN EMERGENCY EXIT LIGHT BATTERIES WERE FOUND INOPERATIVE. THE BATTERIES, P/N S104 AND 106 WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. (M ) 2 L 7 3 4F RT A3WE 1999031200852 19990312 00852 NM 1999 3 12 MZZA99019 1 19981224 A 5330 SKIN BOEING 727 7272F9 138407D NM BS 1360 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, CORROSION WAS FOUND ON FUSELAGE SKIN AT BS 1360 AT ONE O'CLOCK POSITION. T HE CORRODED SKIN 6 INCH BY 6 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-3. (M) 2 L 7 3 4F RT A3WE 1999031200853 19990312 00853 NM 1999 3 12 MZZA99020 1 19981228 A 5530 STIFFENER BOEING 727 7272F9 138407D NM VERTICAL STAB CRACKED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, CRACK 2 INCH LONG WAS FOUND ON VERTICAL FIN LEFT SIDE STIFFENER S-7 AT FS 1 12. THE DAMAGED STIFFENER 2 INCHES LONG WAS TRIMMED OUT AND REPAIRED PER B727 SRM 55-30-04 FIG 1. (M) 2 L 7 3 4F RT A3WE 1999031200855 19990312 00855 NM 1999 3 12 MZZA99004 1 19981223 A 3230 66167891 SPRING BOEING 727 7272F9 138407D NM LT MLG RUSTED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, RUSTED AND DAMAGED SPRING WAS FOUND ON LEFT MLG MANUAL EXTENSION MECHANISM. THE DAMAGED SPRING P/N 66-16789-1 WAS REMOVED AND REPLACED PER B727 MM 32-34-1 AND OPERATIONAL CHECK FOUND SATISFACTOR Y. (M) 2 L 7 3 4F RT A3WE 1999031200856 19990312 00856 NM 1999 3 12 MZZA99001 1 19981223 A 5320 65163471 SHEAR TIE BOEING 727 7272F9 138407D NM BS 1130 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, IG CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 1130, STRINGER S26L. THE CORRODED FRAME SHEAR TIE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-04 FIGURE 13. (M) 2 L 7 3 4F RT A3WE 1999031200857 19990312 00857 NM 1999 3 12 MZZA99002 1 19981223 A 5330 SKIN BOEING 727 7272F9 138407D NM BS 1042-1065 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 75429 21427 TNN - DURING S-CHECK INSPECTION AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FUSELAGE BELLY SKIN AT STRINGER S28R BETWEEN BS 1042 AND BS 1065. THE CORRODED SKIN 4 INCH BY 2 INCH AND 2 INCH BY 2 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-30-03 FIGURE 3. (M) 2 L 7 3 4F RT A3WE 1999031200864 19990312 00864 CE 1999 3 12 99ZZZM185 1 19981209 A 7312 1058FSB08 HEATER BEECH 1900 1900C 1154161 CE FUEL SYSTEM CRACKED A YADA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 AL 01 31240 UC28 APPROX ONE HOUR INTO THE FLIGHT, THE RIGHT LOW ENGINE OIL PRESSURE LIGHT FLICKERED. THE PILOT CHECKED THE OIL PRESSURE GAUGE AND FOUND IT DOWN TO ABOUT 60 PSI. POWER WAS REDUCED AND THE AIRCRAFT WAS DIVERTED TO A CLOSE AIRPORT WHERE AN UN EVENTFUL SAFE LANDING WAS MADE. MAINTENANCE FOUND THE OIL LEVEL LOW AND THE OIL TO FUEL HEATER LEAKING OIL. THE OIL TO FUEL HEATER HAS BEEN VERIFIED AS CRACKED. THE ENGINE REQUIRES REMOVAL FOR 'LIGHT OVERHAUL' INSPECTION IAW THE PWC MM D UE TO RUNNING AT LOW OIL PRESSURE. 2 L 7 2 4T RT A24CE 1999031200865 19990312 00865 CE 1999 3 12 99ZZZM186 1 19981222 A 7921 1143890005 OIL COOLER BEECH 1900 1900C 1154161 CE OIL SYSTEM CRACKED A YADA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 AL 01 1563C UC20 AFTER DEPARTURE FROM FAI, PILOT NOTICED LOW OIL PRESSURE LIGHT ON LEFT ENGINE FLICKER, OBSERVED OIL PRESSUR GAUGE DROPPI NG SLOWLY AND PERFORMED A PRECAUTIONARY SHUT DOWN ON THAT ENGINE. OIL PRESSURE WAS AT 65 PSI AT THE TIME OF SHUTDOWN. A IRCRAFT RETURNED FOR AN UNEVENTFUL LANDING. FOUND OIL LEAKING FROM LEFT NACELLE BELOW THE OIL COOLER. MAINTENANCE REPL ACED THE OIL COOLER AND GROUND LEAK CHECKED OK. REMOVED OIL COOLER VERIFIED CRACKED AT SIDE WELD SEAM. (M) 2 L 7 2 4T RT A24CE 1999031200867 19990312 00867 NM 1999 3 12 EISA98293 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 328 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING C-CHECK ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED FOUR AREAS OF CORROSION ON T-CAP OF FLOORBEAM AT FS 328. REMOVED DAMAGED AREAS AND INSTALLED REPAIRS PER SRM 53-10-8 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999031200868 19990312 00868 NM 1999 3 12 EISA98292 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 400 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON FLOORBEAM AT FS 400 LBL 45. TRIMMED DAMAGED UPPER C HORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-02. (M) 2 L 7 3 4F RT A3WE 1999031200869 19990312 00869 NM 1999 3 12 EISA98291 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 440 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON UPPER CHORD OF FLOORBEAM AT FS 440 LBL 25. TRIMMED DAMAGED AREA OF UPPER CHORD. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-1. (M) 2 L 7 3 4F RT A3WE 1999031200870 19990312 00870 NM 1999 3 12 EISA98290 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 400 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED THREE AREAS OF CORROSION ON FLOORBEAM AT FS 400. TRIMMED AREAS O F DAMAGED CHORD. FABRICATED AND INSTALLED REPAIRS PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999031200871 19990312 00871 NM 1999 3 12 EISA98289 1 19981208 A 5315 FLOORBEAM BOEING 727 727277 138408S NM BS 680 CORRODED A EISA K NONE O OTHER IN INSP/MAINT 1 SW 07 275WC 20549 DURING ACCOMPLISHMENT OF CPCP CARD C53-224-01 REVEALED CORROSION ON FLOORBEAM UPPER CHORD AT FS 680. REMOVED DAMAGED AR EA OF UPPER CHORD FABRICATED AND INSTALLED REPAIR PER SRM 53-10-8 FIGURE 3 AND 51-30-2. (M) 2 L 7 3 4F RT A3WE 1999031200882 19990312 00882 WP 1999 3 12 ORJA98333 1 19981227 A 3397 00105606003 WIRE DOUG DC9 DC983 3022083 WP ROW 20F LOOSE A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 871RA 49788 RNO - CABIN EMERGENCY LIGHTS RE-ILLUMINATE WITH SWITCH 'ARMED' AT GATE. REMOVED BATTERY PACK AT 20F AND FOUND LOOSE WIR E AT CONNECTOR. RESECURED WIRE, SYSTEM CHECK NORMAL AT THIS TIME. (M) 2 L 7 2 4F RT A6WE 1999031200889 19990312 00889 WP 1999 3 12 ORJA9923 1 19981105 A 3397 00105606003 WIRE DOUG DC9 DC983 3022083 WP ROW 20 FAILED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 878RA 53184 OKC - EMERGENCY SEAT LIGHTING AT ROW 20 INOPERATIVE. REPAIRED WIRING AT ROW 20 SEAT BASE IAW MD80 MM 20-10-03 TESTED LI GHTING IAW BRUCE IND MANUAL 400-082. (M) 2 L 7 2 4F RT A6WE 1999031200891 19990312 00891 NE 1999 3 12 VTZA98369 2 19981220 A 7510 601970911 VALVE CNDAIR CL600 CL6002B16 1900305 EA GE CF34 CF343A1 30015 NE RT ENGINE FAILED A VTZA O OTHER J WARNING INDICATION AP APPROACH 1 EA 27 621BR 7186 FLT 6665 - SGE-ORD - DURING APPROACH, AIRCRAFT MADE AN SCHEDULED LANDING WITHONE DISCREPANCY WHICH WAS RT ENGINE ANTI-IC E FAILED. AIRCRAFT WENT TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ANTI-ICE VALV E, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F 4 F RT A21EA E15NE 1999031200970 19990312 00970 NM 1999 3 12 SCNA98159 1 19981107 A 2740 651948218 GEARBOX BOEING 727 727225 1384077 NM HORIZ STAB TRIM JAMMED A SCNA O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 GL 15 282SC 2784 22558 DUE TO REPEATED REPORTS OF THE HORIZONTAL STABILIZER TRIM JAMMING OR BEING INTERMITTENT THE HORIZONTAL STABILIZER TRIM G EARBOX WAS REPLACED. SHOP FINDINGS ON THE REMOVED GEAR BOX REVEALED THAT THE UNIT WAS JAMMED FROM CORRODED BEARINGS AND EXCESSIVE WATER IN THE SCREW HOUSING. 2 L 7 3 4F A3WE 1999031600003 19990316 00003 EU 1999 3 16 VTZA98360 1 19981207 A 5270 SWITCH JETAIR JETSTM JETSTM4101 1500501 EU BAGGAGE DOOR WORN A VTZA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 27 310UE 41028 FLT 6303 - IAD-DAY - DURING CRUISE, AIRCRAFT MADE A UNSCHEDULED LANDING DUE TO POD DOOR WARNING LIGHT ILLUMINATED. AIRC RAFT DIVERTED TO MGW WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTION AND OPENED DMI 47304, MEL 52-4 SLEEVE FOR MICROSW ITCH. MAINTENANCE CLOSED DMI 47304 ON 12-20-98 BY REMOVING AND REPLACING SLEEVE. OPS CHECK OK, AIRCRAFT WAS RELEASED A ND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T RT A41NM 1999031800002 19990318 00002 EA 1999 3 18 VTZA98371 1 19981219 A 3241 ANTI-SKID CNDAIR CL600 CL6002B19 EA LANDING GEAR MALFUNCTIONED A VTZA O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 EA 27 620BR 7179 FLT 6746 - GSP-IAD - DURING TAXI, AIRCRAFT RETURNED TO GATE DUE TO ANTI-SKID INBOARD WARNING ILLUMINATED. MAINTENANCE I NSPECTED AND OPENED DMI 40843, MEL 32-4. MAINTENANCE CLOSED DMI 40843 ON 12-19-98. COULD NOT DUPLICATE PROBLEM, OPS CH ECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4F RT A21EA 1999031900649 19990319 00649 NM 1999 3 19 UPS99228958 1 19980211 A 5230 65186251 STRUCTURE BOEING 727 72731C 1384011 NM CARGO DOOR CRACKED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 923UP 19229 INSPECTION TYPE-D, A NUMBER OF CRACKS FOUND ON AFT CARGO DOOR STRUCTURE. DOOR REPLACED IAW MM 52-31-00. 2 L 7 3 4F A3WE 1999031900747 19990319 00747 SO 1999 3 19 99ZZZX957 2 19980118 A 8520 643202 CRANKCASE CESSNA 402 402B 207590P CE CONT O520 TSIO520E 17040 SO ENGINE CRACKED A HBCA K NONE O OTHER IN INSP/MAINT 1 SW 11 29MM 835 402B0863 183633H WHILE REPAIRING AN UNRELATED ITEM, THE MECHANIC NOTICED A CRACK APPROXIMATELY ONE INCH LONG (RUNNING TOP TO BOTTOM) ASSO CIATED WITH THE MOST FORWARD UPPER THROUGH-STUD ON THE NR 4 CYLINDER. THE CASE WAS INSPECTED IAW TCM SB M90-17 AND DETE RMINED TO BE UNAIRWORTHY BY THE LOCATION OF THE CRACK. THE CASE HAD BEEN REPAIRED AT SOME TIME IN THE PAST IN LOCATION OF THE CRACK. SUBMITTER SUGGESTED A POSSIBLE CAUSE FOR THE CRACK COULD BE FROM STRESS CAUSED BY THE REPAIR OR POSSIBLY IMPROPER HEAT TREATING TO THE SURROUNDING AREA OF REPAIR. 1 L 7 2 3O 3 O A7CE E8CE 1999031901036 19990319 01036 NM 1999 3 19 QXEA9801725 1 19981016 A 5330 SKIN DHAV DHC8 DHC8102 2809003 NM BS 545.5 DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 812PH 26 YXX- FUSELAGE SKIN DENT 0.16 DEEP APPROXIMATELY 6 IN DIAMETER AT X545.5 Z97.25. NEAR BOTTOM FORWARD CORNER OF BAGGAGE DO OR. REPAIRED IAW RD 8-53-3837. 2 H 7 2 4T RT A13NM 1999031901053 19990319 01053 NE 1999 3 19 ARWA981214 2 19981222 A 7321 71128721 FCU DOUG DC8 DC863F 302198F WP PWA JT3D JT3D7 52039 NE NR 3 ENGINE MALFUNCTIONED A ARWA D RETURN TO BLOCK O OTHER TX TAXI/GRND HDL 1 SO 19 661AV 73473 45969 KDEN - FLT 2801 - NR 3 ENGINE HUNG START, FAILS TO ACCELERATE PAST IDLE RPM, ANTI-ICE ON OR OFF. REMOVED AND REPLACED N R 3 ENGINE FUEL CONTROL UNIT PER MM 73-20-00. PERFORMED ENGINE RUN UP IAW ARROW AIR DC-8 MM JC 6527. ALL PARAMETERS NO RMAL. 2 L 7 4 4F 4 F 4A25 1E8 1999031901054 19990319 01054 NE 1999 3 19 ARWA981221 2 19981229 A 7321 71128721 FCU DOUG DC8 DC862 3021970 WP PWA JT3D JT3D3B 52039 NE NR 1 ENGINE FAILED A ARWA E C D ENGINE SHUTDOWN ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 SO 19 1804 71870 45896 PNX - FLT 515 - BLOCK TURNBACK, ON RIGHT RUNUP, NR 1 ENGINE DIDN'T ACCELERATE. ALL INDICATIONS REMAINED IN IDLE. INDIC ATION WITH SLIGHTLY FLUCTUATING EPR NEEDLE. FELT ENGINE VIBRATING AND HEARD 'KNOCKING' NOISE. IMMEDIATELY BROUGHT THR OTTLE BACK TO IDLE AND SHUTDOWN THE ENGINE. TROUBLESHOOTING FOUND DEFECTIVE FUEL CONTROL UNIT AT ENGINE RUNUP. REMOVED AND REPLACED FCU IAW DC-8 MM 73-20-0 AND 73-20-1. OPS CHECKED AND ENGINE TRIMMED NORMAL IAW MM 72-00-0. (M) 2 L 7 4 4F 4 F 4A25 1E8 1999031901061 19990319 01061 WP 1999 3 19 VTZA98355 2 19981127 A 7260 5725109162 CHIP DETECTOR JETAIR JETSTM JETSTM4101 1500501 EU GARRTT TPE331 TPE3311 01514 WP RIGHT ACTIVATED A VTZA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 27 332UE 41100 FLT 6426 - IAD-DTW - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO RIGHT ENGINE OIL CONTAMINATION WARNING L IGHT ILLUMINATED. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND FOUND FLAKES OF METAL ON CHIP DETECTOR AND CLEANED AND REINSTALLED CHIP DETECTOR. ALSO, MAINTENANCE PERFORMED SOAP SAMPLE, OPS CHECK OK. AIR CRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A41NM E3WE 1999031901062 19990319 01062 WP 1999 3 19 VTZA98338 2 19981114 A 7320 1379287405 P3 LINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP LT ENGINE FAILED A VTZA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 EA 27 478UE 892 FLT 6330 - IAD-PIT - DURING CLIMB, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO LEFT BETA WARNING LIGHT ILLUMINATED. AIR CRAFT LANDED AND RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ENGINE AND I NSPECTED BETA SWITCH, OPS CHECK OK. AIRCRAFT WAS RELEASED AND APPROVED FOR RETURN TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1999031901065 19990319 01065 WP 1999 3 19 RAIA981220 2 19981220 A 7320 8974575 VALVE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE33112UA 01514 WP RT ENGINE FAILED A RAIA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CE 03 337TE 929 FLT 7361 - PAH - RIGHT ENGINE WOULD NOT MAKE TARGET TORQUE. MAINTENANCE REPLACED SERVO VALVE ON RIGHT ENGINE. (M) 2 L 7 2 4T 4 T RT A56EU E4WE 1999031901068 19990319 01068 NE 1999 3 19 99ZZZM191 2 19981224 A 7260 717000 GEAR BOX 700311 BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LEAKING A MYWA B E EMER. DESCENT ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 887MA 79522 21857 WHILE CLIMBING THROUGH 1,500 FT OIL QUANTITY GAUGE ON NR 1 ENGINE WAS IDENTIFIED AS LOSING OIL. CLIMBED TO 5,000 (CLEAN CONFIGURATION) DECLARED AN EMERGENCY WITH ATC. TURNBACK TO MIA. ENGINE WAS SHUTDOWN, ALL AOM PROCEDURES COMPLIED WITH . REPLACED GARLOCK SEAL FOR STARTER ON ENGINE NR 1 IAW MM 72-61-00, OPS CHECK AND LEAK CHECK OK. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999031901069 19990319 01069 NE 1999 3 19 99ZZZM192 2 19981223 A 7260 717000 GEAR BOX MS93288124 BOEING 727 727225 1384077 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE LEAKING A MYWA B E EMER. DESCENT ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CL CLIMB 1 SO 19 887MA 700311 21857 WHILE CLIMBING THROUGH 13,000 FEET OIL QUANTITY GAUGE ON NR 1 ENIGNE WAS IDENTIFIED AS LOSING OIL. TURNBACK TO MIA, PRI OR TO TURNBACK SWAPPED OIL GAUGES TO VERIFY OIL LOSS. ENGINE SHUT DOWN ALL AOM PROCEDURES COMPLIED WITH. FOUND OIL RET URN LINE TO GEAR BOX LEAKING, REPLACED PACKIGN AND HELI-COIL PER MM 79-20-0. OPERATIONAL CHECKED OK. HELI-COIL REPLACE MENT PER OHM 72-61-01. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999031901071 19990319 01071 NE 1999 3 19 99ZZZM193 2 19981231 A 7261 659030535 O-RING BOEING 727 72722C 138400F NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE LEAKING A RYNA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CE 07 428EX 19097 FLT 7331 - SEA-ORD - NR 3 ENGINE EXCESSIVE OIL CONSUMPTION 1 QUART PER 5 MINUTES. WAITED UNTIL QUANTITY DROPPED BELOW 1 GALLON, IT DID. USED CHECK LIST LOW OIL PRESSURE QUANTITY WHICH TRANSITED TO INFLIGHT ENGINE SHUT DOWN. OIL REACHED Z ERO AT 1740Z, SHUT ENGINE DOWN. DIVERTED TO BIL. REPLACED OIL FILTER AND O-RINGS, REINSTALLED, TORQUED AND SAFETIED. P ILOT RAN NR 3 ENGINE LEAK CHECK OK. SERVICED NR 3 ENGINE TO FULL. CONTINUED TO ORD. (M) 2 L 7 3 4F 4 F A3WE E2EA 1999031901072 19990319 01072 EU 1999 3 19 DKAA98029 1 19981215 A 5230 PAN AMD FALC20 FALCON20C5 2730107 EU CARGO DOOR CRACKED A DKAA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 810RA 81 REFERENCE DKAA98023, IN REFERENCE TO CRACKED CARGO DOOR Z-CHANNEL, A VISUAL INSPECTION OF Z-CHANNEL REVEALED THAT CRACKS FOUND IN RADIUS MAY HAVE OCCURED DUE TO RADIUS BEING SHOP-FORMED PARALLEL TO THE GRAIN OF PARENT MATERIAL (ALUMINUM 202 4-T3). THIS IS CONTRARY TO STANDARD PROCEDURE, AS NOTED IN AC 43-13-1A, CHAPTER 2, PARAGRAPH 97A. ADDITIONAL DAMAGE NO TED. CARGO DOOR UPPER CORNER PANS (TWO EACH) FOUND CRACKED AT RELIEF NOTCHES. Z-CHANNEL IS RIVETED TO UPPER CORNER PAN S. (M) 2 L 7 2 4F RT A7EU 1999032600120 19990326 00120 NM 1999 3 26 CA980707003 1 19980605 A 2750 734378D DRIVE SHAFT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE TE FLAP STRIPPED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 22588 120648 (CAN) DURING APPROACH WHEN FLAPS SELECTED, THE FLAP DRIVE CAUTION LIGHT CAME ON. POST-LANDING INSPECTION FOUND THE FLAP PRIMARY TORQUE DRIVE SHAFT INTERNAL SPLINE WORN OUT. IT ALSO HAD RED RUST AND WAS DRY, WITH NO LUBRICATION EVIDENT. D EHAV TASK CALLS FOR LUBE OF SPLINE EVERY 8,000 HOURS OR 9000 CY. AIRCRAFT HAD 5,286 HOURS AND 7183 CY SINCE TASK LAST A CCOMPLISHED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600121 19990326 00121 NM 1999 3 26 CA980707004 1 19980604 A 6123 M390166105L RELAY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE AUTO FEATHER FAILED W O OTHER O OTHER CL CLIMB 1 CA 120833 891003 (CAN) AFTER TAKEOFF, AUTOFEATHER DISARMED. RELAY 6121-K5 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1999032600122 19990326 00122 NM 1999 3 26 CA980707009 1 19980607 A 3246 314354 TIRE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT MLG FLAT W O OTHER O OTHER TX TAXI/GRND HDL 1 CA 36 120229 (CAN) BOTH LEFT MAIN TIRES FLAT ON TAXIWAY AFTER LANDING. ONLY 59 CY AND 36 HOURS SINCE THE TIRES WERE INSTALLED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600123 19990326 00123 EA 1999 3 26 CA980707011 1 19980622 A 3230 82970010443 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE RT MLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 15854 123132 (CAN) NR 2 NACELLE SHOWING SIGNS OF FLUID LEAK. RIGHT MLG STABILIZER DOWN, HYDRAULIC LINE FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600124 19990326 00124 NM 1999 3 26 CA980707012 1 19980622 A 3230 82970010609 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT MLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 29268 120373 (CAN) NR 2 NACELLE FOUND WITH HYDRAULIC LEAK. RIGHT MLG DOWN, PRESSURE HYDRAULIC TUBE FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600125 19990326 00125 EA 1999 3 26 CA980707013 1 19980622 A 3230 DSC252B40124 LINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NLG LEAKING W A UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA 16578 123129 (CAN) AFTER TAKEOFF, NR 2 HYDRAULIC SYSTEM LOST FLUID. AIRCRAFT RETURNED OK. INSPECTION FOUND THE NOSE GEAR DRAG STRUT ACTUATOR HYDRAULIC LINE LEAKING. LINE AND NR 2 ENGINE DRIVEN PUMP REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600126 19990326 00126 EU 1999 3 26 CA980707014 1 19980622 A 2120 AIR CONDITIONING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA LF95624A (CAN) AFTER TAKEOFF WHEN ENGINE AIR SELECTED ON, AN EXCESSIVE AMOUNT OF AIR VOLUME ENTERING FLIGHT DECK. NR 2 ENGINE AI R OFF, AIR FLOW RETURNED TO NORMAL. CREW ALSO REPORTED AN UNUSUAL HOT SMELL IN AIRCRAFT. FLIGHT RETURNED. NR 1 AIR CO NDITIONING PACK AND APU 'Y' DUCT SEALS REPLACED. NIL FOUND. 2 H 7 4 4F 4 F RT A49EU E6NE 1999032600129 19990326 00129 NM 1999 3 26 CA980713018 1 19980625 A 2910 NAS16128 O-RING AN91910D DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM DETERIORATED W A UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA 120439 (CAN) LOSS OF ALL NR 1 HYDRAULIC SYSTEM FLUID WAS DUE TO A DAMAGED 'O' RING ON THE REDUCER UNION AT STA XN-180-00 - ZN10 .00. THIS CONNECTS TO LINE 82970010-347. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600130 19990326 00130 NM 1999 3 26 CA980713019 1 19980623 A 2760 82950010271 LINE A4400009 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT WING LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA TM120796 (CAN) ON WALK-AROUND, THE PILOT NOTED HYDRAULIC FLUID LEAKING FROM THE RIGHT HAND WING TRAILING EDGE. INVESTIGATION FOU ND A PIN HOLE IN THE HYDRAULIC LINE FOR THE INBOARD ROLL SPOILER. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600131 19990326 00131 EA 1999 3 26 CA980720008 1 19980627 A 5610 07802 WINDSHIELD DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CR CRUISE 1 CA 10878 TH2035 123038 (CAN) IN CRUISE, THE CAPTAIN'S WINDSHIELD OUTER PLY CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600132 19990326 00132 NM 1999 3 26 CA980720018 1 19980711 A 2701 SPRING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CONTROL COLUMN WEAK W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 120370 (CAN) WHEN THE RIGHT HAND WHEEL CONTACTED THE RUNWAY, THE AILERON AND ROLL SPOILER (RIGHT AND LEFT CONTROL) WHEELS SPLIT . RD 8-53-3620 COMPLETED ON THIS AIRCRAFT. SUBMITTER SUSPECTS A WEAK DISCONNECT CLUTCH SPRING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600133 19990326 00133 CE 1999 3 26 CA980804027 1 19980721 A 7600 99524119 CATCH 1005241771 BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE CONTROL LEVER WORN W O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA 5044 GGM114452 (CAN) AS PILOT WAS REDUCING ENGINE POWER BY RETARDING BOTH CONDITION LEVERS FROM HIGH TO LOW IDLE, THE WORN CATCH GATES DID NOT PREVENT THE LEVERS MOVING TO SHUT-OFF. THUS, BOTH ENGINES FLAMED OUT. FLEET CHECK CARRIED OUT AND SIMILAR WEAR FOUND ON FOUR OTHER AIRCRAFT. BEECH WILL BE ADVISED OF THE OCCURRENCE. 2 L 7 2 4T 4 T RT A24CE E26NE 1999032600134 19990326 00134 NM 1999 3 26 CA980818001 1 19980629 A 3250 86005 MANIFOLD DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG STEERING FAILED W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA 21865 120152 (CAN) WHILE WAITING TAKEOFF CLEARANCE, NR 2 HYDRAULIC ISO VALVE CAUTION LIGHT ON, FOLLOWED BY ROLL SPOILER HYDRAULIC AND NOSE STEERING CAUTION LIGHTS. NR 2 HYDRAULIC QUANTITY DROPPED 1 QUART. STEERING MANIFOLD REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600135 19990326 00135 EA 1999 3 26 CA980818003 1 19980722 A 3231 SENSOR DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE MLG OUT OF ADJUST W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 16110 123133 (CAN) AFTER TAKEOFF, THE GEAR DOORS REMAINED OPEN. AIRCRAFT RETURNED OK. RIGHT HAND RELAY SOCKET BASE 3261 REPLACED. P SEU REPLACED, UPLOCK PROXIMITY SENSOR GAPS ADJUSTED. RELAYS K3261-K2 AND 3261-K11 REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600136 19990326 00136 1999 3 26 CA980818005 4 19980701 A 2300 52611 AUDIO PANEL DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 8941 410 120854 (CAN) SMOKE NOTED COMING FROM THE NR 2 INTERCOM PANEL. NR 2 ADF AND VHF CIRCUIT BREAKERS PULLED. NR 2 AUDIO PANEL REPL ACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600137 19990326 00137 EA 1999 3 26 CA980818007 1 19980715 A 5220 85220281007 SEAL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE EMERGENCY EXIT CRACKED W O OTHER O OTHER DE DESCENT 1 CA 123132 (CAN) DURING DESCENT THROUGH 11,000 FEET, CABIN PRESSURIZATION LOST. LANDING NORMAL. FORWARD EMERGENCY EXIT INFLATABLE SEAL FOUND WITH A SMALL CRACK. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600138 19990326 00138 NM 1999 3 26 CA980825008 1 19980821 A 5320 85310055 WEB DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG WW CRACKED W B EMER. DESCENT J WARNING INDICATION AP APPROACH 1 CA 21909 120329 (CAN) CREW REPORTED THAT THE NOSE LANDING GEAR DID NOT INDICATE DOWN AND LOCKED AFTER NORMAL EXTENSION. ALTERNATE EXTEN SION CARRIED OUT AND GEAR STILL REMAINED INDICATING UNSAFE. EMERGENCY LANDING CARRIED OUT OK. INVESTIGATION FOUND A CR ACK IN THE SKIN ON THE NOSE LANDING GEAR DRAG STRUT WAS MECHANICALLY OVER CENTER, BUT DID NOT COMPLETE ITS FULL TRAVEL W HICH PREVENTED DOWN AND LOCKED INDICATION FOR BOTH NORMAL AND EXTENSION INDICATION SYSTEMS. 2 H 7 2 4T 4 T RT A13NM E20NE 1999032600175 19990326 00175 CE 1999 3 26 99ZZZX1040 1 19981224 A 3260 70HF10 DIODE BEECH 200 200BEECH 1152920 CE INDICATOR SHORTED A EIEA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 WP 01 717HT BB133 PILOT REPORTED LOSS OF LANDING GEAR INDICATION PLUS OTHER LIGHTS. HAD TO DO 'GO AROUND' FOR TOWER TO CONFIRM 'GEAR DOWN '. MAINT INFORMED RT BUS FEED CIRCUIT BREAKERS HAD TRIPPED. PILOT RE-SET CB'S, GOT 3 GREENS. ALL OTHER SYSTEMS LAMPED , NO PROBLEMS. ONE OFF DIODE FOUND 'OPEN', 4 OFF DIODES REPLACED , 2 LT BUS FEEDS, 2 RT BUS FEEDS. REF BEECHRAFT KING AIR 200 WIRING DIAGRAM MANUAL 24-54-01, PG 3, ITEM DUAL BUS DIODE ASSY (NR 2) A135-CR1 AND CR2. THESE DIODES ARE CHECKE D ON PHASE 3 INSP PER BEECHCRAFT MM CHP 24-50-00, PG 201. PHASE 3 WAS C/W 124.5 HRS PRIOR TO DEFECT. 1 L 7 2 4T A24CE 1999032600180 19990326 00180 SO 1999 3 26 99ZZZX1046 2 19981208 A 8520 CRANKCASE BEECH 58 58 1152740 CE CONT O520 IO520C 17032 SO RT ENGINE CRACKED A P LHOA O OTHER K FLUID LOSS NR NOT REPORTED 1 EA 05 7353R TH486 561358 DURING A FLIGHT, RT ENG BEGAN TO RUN ROUGH AND ON THE GROUND, HAD A NOTICEABLE OIL LEAK ALTHOUGH 9.5 QUARTS EXISTED. UP ON ENG CHECK, NOTICED COMPOUND FRACTURE AT THE UPPER BASE OF CYL NR 4. ENG REMOVED AND DISASSEMBLED. FOUND FRACTURES T HRU THE CASE STUD BOSS ALLOWED CYL BASE STUD TO BE RELEAVED OF ITS INTERFERENCE FIT. HOLD-DOWN NUT THEN RELEAVED OF ITS TENSION, BACKED OFF OUTSIDE ALLOWING STUD TO TURN INWARD TOWARD CASE. STUD CONTACTED CRANK THROW WHICH THREW STUD INTO TOP OF THE CASE CAUSING STAR BURST MULTIPLE FRACTURES ABOVE CYL NR 4. OPPOSITE CASE HALF SHOWS SIGNS OF HAIRLINE CRACK S IN SEVERAL STUD BOSSES (CASE AREA) DENOTING EARLY STAGES OF SAME FAILURE. THESE ARE NOT VISIBLE WITH CYL INSTALLED. 1 L 7 2 3O 3 O 3A16 E5CE 1999032600193 19990326 00193 1999 3 26 99ZZZX1059 4 19981202 A 2312 071104101 RADIO BEECH 58 58 1152740 CE COCKPIT FAILED A BSYA K NONE O OTHER IN INSP/MAINT 1 GL 07 9044V 3354 TH216 AIRCRAFT HAD A TOTAL RADIO FAILURE COMING INTO (CMH) POWER CONVERTER SHORTED TO 28 VDC. REMOVED, REPAIRED, AND REINSTAL LED. OPS CHECKS GOOD. 1 L 7 2 3O 3A16 1999032600437 19990326 00437 EU 1999 3 26 PLGA981215 1 19981215 A 3412 102CP2AF PROBE SAAB SF340 340B 7860101 EU OAT FAILED A PLGA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NE 05 362BE 93584 340B291 BOS - FLT 6241 - CREW REPORTED OAT CAUTION LIGHT AFTER GEAR RETRACTION. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INC IDENT. MAINTENANCE REPLACED THE OAT PROBE. A/C RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600438 19990326 00438 1999 3 26 PLGA981227 4 19981227 A 6113 664005017 SPINNER SAAB SF340 SF340A 7850100 EU PROPELLER VIBRATION A PLGA A UNSCHED LANDING E VIBRATION/BUFFET CR CRUISE 1 NE 05 748BA 340A149 BOS - FLT 6473 - CRWE RETURNED TO BOS DUE TO VIBRATION COMING FROM PROP. A/C LANDED WITHOUT INCIDENT. MAINTENANCE REPL ACED SPINNER. TEST FLIGHT SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A52EU 1999032600537 19990326 00537 WP 1999 3 26 ORJA9949 1 19981003 A 5320 5912494501N FRAME DOUG DC9 DC983 3022083 WP CARGO DOORWAY CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, FORWARD PIT DOOR FRAME HAS CORROSION AT LOWER DOOR OPENING. REMOVED AND REPLACED LOWER DOOR PAN IAW DC-9, SRM 5 3-05, FIG 44/51-10-4 AND 51-10-3. (M) 2 L 7 2 4F RT A6WE 1999040200050 19990402 00050 EU 1999 4 2 99ZZZX1166 1 19981203 A 7722 INDICATOR BRAERO DH125 HS125700A 4230170 EU COCKPIT MALFUNCTIONED A IEYA E A ENGINE SHUTDOWN UNSCHED LANDING N FALSE WARNING DE DESCENT 1 GL 03 700BW NA0288 AT FLIGHT LEVEL 8,000 FEET, NR 1 ENGINE PRECAUTIONARY SHUT DOWN. PASSING THROUGH 8,000 FEET TO 6,000 FEET, NR 1 ENGINE ITT CLIMBED TO 1,160 DEGREES CELSIUS. PILOT REDUCED POWER TO IDLE, NOTIFIED ATC OF SITUATION, PROCEEDED TO INITIATE A P RECAUTIONARY ENGINE SHUT DOWN. TROUBLESHOOTING FOUND ITT GAUGES SWAPPED. PROBLEM TRANSFERRED TO NR 2 ENGINE. REMOVED AND REPLACED ITT GAUGE. OPS CHECKED SATISFACTORY. 2 L 7 2 4F A3EU 1999040200104 19990402 00104 NM 1999 4 2 CA980916012 1 19980831 A 2910 HYDRAULIC SYS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 & 2 CONTAMINATED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 121165 (CAN) AFTER TAKEOFF, THE LANDING GEAR SYSTEM WOULD NOT RETRACT. AIRCRAFT RETURNED OK. INSPECTION FOUND AIR IN BOTH HYD RAULIC SYSTEMS. POSSIBLY FLIGHT DECK INHIBIT HANDLE NOT COMPLETELY CLOSED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200105 19990402 00105 EA 1999 4 2 CA980916015 1 19980915 A 7921 87901015101 FITTING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE OIL COOLER CHAFED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 129 123133 (CAN) DURING CRUISE, THE NR 1 ENGINE OIL PRESSURE FLUCTUATED 50-60 PSI. LOW OIL PRESSURE CAUTION LIGHT INTERMITTENT. P OWER REDUCED. LANDING NORMAL. INSPECTION FOUND LOW OIL QUANTITY DUE TO A LARGE LEAK FROM OIL COOLER INLET FITTING. TH E COOLER RIGID LINE HAD CHAFED THE FITTING ALLOWING OIL TO LEAK PAST THE PACKING. P/N AS3209-219. LINE WAS BELIEVED TO HAVE BEEN COCKED AT INSTALLATION. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200106 19990402 00106 NM 1999 4 2 CA980916034 1 19980717 A 7603 ROD DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE POWER LEVER MISINSTALLED W C ABORTED TAKEOFF J W WARNING INDICATION INADEQUATE Q C TO TAKEOFF 1 CA 123053 (CAN) DURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED AT APPROXIMATELY 90 PERCENT POWER. TAKEOFF REJECTED. INSPECTION FOUND THE POWER LEVER ROD END BETWEEN THE MFC AND PCU WAS INSTALLED INCORRECTLY AT THE MFC ON THE NR 1 ENGINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200107 19990402 00107 EA 1999 4 2 CA980916057 1 19980903 A 2913 311435001 SEAL DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 1 ENGINE LEAKING W C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA 123144 (CAN) ON TAKEOFF WHEN 90 PERCENT TORQUE APPLIED, THE NR 1 OIL PRESSURE WARNING LIGHT CAME ON. OIL PRESSURE INDICATOR SH OWED DROPPING OIL PRESSURE. AS SOON AS ENGINE WAS PUT IN DISCING OIL, PRESSURE RETURNED TO NORMAL. SHAFT SEAL FOUND LE AKING OIL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200108 19990402 00108 NM 1999 4 2 CA980916058 1 19980910 A 5230 85230480102 BRACKET 8523010001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CARGO DOOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 27763 0010082 120338 (CAN) THE BAGGAGE DOOR COUNTER BALANCE PULLEY BRACKET FOUND CRACKED IN THE RADIUS NEAR THE PULLEY. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200109 19990402 00109 NM 1999 4 2 CA980922023 1 19980912 A 7600 87600520001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT ENGINE SEVERED W K NONE O OTHER IN INSP/MAINT 1 CA 120785 (CAN) RIGHT HAND ENGINE CONDITION CONTROL CABLE HAS IN EXCESS OF 5 STRANDS SEVERED. THIS IS A 7 X 19 CABLE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200110 19990402 00110 1999 4 2 CA981006019 4 19980906 A 3130 9804100DXUN DATA RECORDER DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE CABIN FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 6362 123152 (CAN) FDR REMOVED TO DO INCIDENT READOUT. NO 'FDR FAIL' CAUTION LIGHTS REPORTED. COULD NOT GET DATA READOUT. THEN DID ATU RETURN TEST WHICH FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200111 19990402 00111 NM 1999 4 2 CA981006021 1 19980921 A 3231 82910010195 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SEQUENCE VALVE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 19567 120329 (CAN) HYDRAULIC LEAK FOUND FROM THE NOSE LANDING GEAR DOORS SEQUENCE VALVE. LINE LEAKING AT THE 90 DEGREE BEND, JUST UN DER THE OXYGEN BOTTLE AFT SECTION. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200112 19990402 00112 NM 1999 4 2 CA981006031 1 19980928 A 2730 MS202194 PULLEY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ELEVATOR SEIZED W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA 24120 120251 (CAN) ELEVATOR TRIM BINDING. PULLEY AFT OF STANDBY TRIM MOTOR HAD SEIZED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200113 19990402 00113 1999 4 2 CA981013011 4 19980630 A 3130 9804100DXUN DATA RECORDER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CABIN FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 4879 120458 (CAN) NO DATA COULD BE RECOVERED FROM FLIGHT DATA RECORDER. WHEN ON BENCH, IT ALSO FAILED A RETURN TO SERVICE TEST. DE FECTIVE ROTABLE TAPE DECK WAS THE PROBLEM. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200114 19990402 00114 NM 1999 4 2 CA981019002 1 19980930 A 3231 82910010175 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 19532 120249 (CAN) HYDRAULIC LEAK FOUND IN NOSE WHEEL LINE. LINE IS THE FORWARD GEAR DOOR CLOSE TUBE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200115 19990402 00115 NM 1999 4 2 CA981019003 1 19981001 A 2760 82970010337 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE SPOILER CRACKED W O OTHER K FLUID LOSS NR NOT REPORTED 1 CA 22299 TM120796 (CAN) GROUND HANDLING PERSONNEL NOTED A FLUID LEAK AT THE LEFT GEAR AND NACELLE. THE LIFT DUMP PRESSURE SYSTEM LINE FOU ND CRACKED AND SPRAYING FLUID ON JET PIPE. HYDRAULIC LINE AT FLIGHT SPOILER LIFT DUMP SOLENOID VALVE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200116 19990402 00116 NM 1999 4 2 CA981019004 1 19981005 A 5343 85311176 RIVETS DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BRACKET SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 22906 120804 (CAN) DRAG STRUT ACTUATOR BRACKET FOUND WITH TWO SHEARED RIVETS AND TWO LOOSE RIVETS AT THE MOUNT IN NOSE AT X97.00 IN T HE UPPER COMPARMENT FORWARD OF THE DC CONTACTOR BOX. NO SKIN CRACKS. RD 8-53-3805 CARRIED OUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200117 19990402 00117 NM 1999 4 2 CA981027014 1 19981016 A 5343 85311176 RIVETS MS20426AD5 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BRACKET LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 22840 120581 (CAN) DRAG STRUT ACTUATOR BRACKET FOUND WITH TWO LOOSE RIVETS IN NOSE AT X97.00 ON THE AIRCRAFT CENTER LINE. NO SKIN CR ACK. RD8-53-3805 CARRIED OUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200118 19990402 00118 NM 1999 4 2 CA981027015 1 19981014 A 3260 841101 SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG DAMAGED W L ABORTED APPROACH J WARNING INDICATION LD LANDING 1 CA 22492 121075 (CAN) WHEN LANDING GEAR SELECTED, THERE WAS NO INDICATION OF DOWN AND LOCK FOR THE NOSE GEAR. ALTERNATE EXTENSION INDIC ATED NOSE DOWN AND LOCKED. BOTH PROXIMITY SENSORS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200119 19990402 00119 NM 1999 4 2 CA981027016 1 19981015 A 3231 83232025101 FORK DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG DOOR LOOSE W O OTHER O OTHER NR NOT REPORTED 1 CA 24177 120816 (CAN) CREW REPORTED A LOUD HOWLING NOISE COMING FROM THE NOSE GEAR AREA. INSPECTION FOUND THAT ALL OF THE FORK END FAST ENER HARDWARE WAS MISSING. NOSE LANDING GEAR DOOR FORK END FASTENER HARDWARE WAS MISSING. THE FORK END WAS FOUND WITH A SHEARED OFF COTTER PIN STILL IN IT. DOOR ATTACH BRACKET P/N 83232034-001 ASSY ALSO REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200121 19990402 00121 1999 4 2 CA981028003 4 19981010 A 3418 906100001 AOA VANE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 SHORTED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 7244 D00115 123061 (CAN) NR 2 STALL WARNING/STICK PUSHER CAUTION LIGHTS ON, BUT THEN WENT OUT. ONCE AIRBORNE, CREW NOTICED THE NR 2 SW/SP CAUTION LIGHT AGAIN. CREW RETURNED. SW/SP COMPUTER REPLACED, BUT SAME PROBLEM OCCURRED. FURTHER INVESTIGATION FOUND THE NR 2 AOA VANE PINS 8 AND 9 WERE SHORTED INTERNALLY TO PIN 12. THUS, SW/SP COMPUTER DID NOT PICK UP FAULTY. ALPHA V ANE REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200122 19990402 00122 NM 1999 4 2 CA981030003 1 19981019 A 2916 82970010319 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYD RESERVOIR CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120329 (CAN) HYDRAULIC LEAK FOUND FROM RESERVOIR TO FIREWALL SHUTOFF VALVE. EDP SUCTION LINE CHAFED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200123 19990402 00123 NM 1999 4 2 CA981030004 1 19981020 A 2910 82970410115 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYD DRAIN LEAKING W K NONE K FLUID LOSS TX TAXI/GRND HDL 1 CA 23017 120804 (CAN) LEFT HYDRAULIC DRAIN LINE FROM THE CASE DRAIN MAINFOLD FOUND DEFECTIVE. REF. IPC 29-10-00 FIG. 15, ITEM 190. PI N HOLE FOUND AT MID-POINT OF LINE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200124 19990402 00124 NM 1999 4 2 CA981030005 1 19981022 A 3231 NAS313241440 CONTROL CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG DOOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 22841 120581 (CAN) CABLE FOUND WORN AND FRAYED BY THE GUARD PIN AT AFT BULKHEAD PULLEY. REF. IPC 32-35-00, FIG. 25, PAGE 0, NR 430C. PIN NR 20 IMPROPERLY INSTALLED WITH SLOT AGAINST CABLE CAUSING EXCESSIVE WEAR. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200127 19990402 00127 NM 1999 4 2 CA981109027 1 19981024 A 7600 87600520001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CONDITION LEVER FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 4678 120421 (CAN) RIGHT HAND LOWER CONDITION LEVER CABLE FOUND FRAYED WHERE THE CABLE PASSES OVER THE PULLEY FORWARD OF THE ENGINE F IREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200128 19990402 00128 NM 1999 4 2 CA981109028 1 19981024 A 7600 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CONDITION LEVER FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 5056 120421 (CAN) LEFT HAND LOWER CONDITION LEVER CABLE FOUND FRAYED WHERE IT PASSES OVER THE PULLEY FORWARD OF THE ENGINE FIREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200130 19990402 00130 NM 1999 4 2 CA981109033 1 19981016 A 2932 APT7510004000SW TRANSMITTER AEB2151011 DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 20377 0410A 123152 (CAN) NR 1 STANDBY HYDRAULIC TRANSMITTER FOUND LEAKING FROM TOP WELD THAT GOES AROUND THE CIRCUMFERENCE OF SWITCH. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200133 19990402 00133 NM 1999 4 2 CA981113004 1 19981024 A 3231 NAS303370566 RELEASE CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT MLG FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 25442 120421 (CAN) AT 500 HOUR INSPECTION, THE RIGHT MAIN LANDING GEAR DOOR RELEASE CABLE WAS FOUND FRAYED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200134 19990402 00134 NM 1999 4 2 CA981113006 1 19981030 A 2760 82950010273 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 23096 120804 (CAN) DURING MAINTENANCE, NR 1 SYSTEM'S HYDRAULIC WAS PRESSURIZED AND A CLOUD OF HYDRAULIC FLUID MIST WAS NOTED COMING F ROM THE LEFT OUTBOARD WING REAR SPAR AREA. THE LEFT INBOARD ROLL SPOILER LIFT DUMP PRESSURE LINE WAS FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200135 19990402 00135 NM 1999 4 2 CA981113007 1 19981103 A 3030 AN31151 CONNECTOR PH1100IDH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE PITOT SYSTEM BURNT W K NONE O OTHER IN INSP/MAINT 1 CA 22915 AO445 120458 (CAN) PITOT TUBE POSITIVE PIN FOUND BURNT INSIDE THE RECEPTACLE. RECEPTACLE BURNT INSIDE AND OUT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200136 19990402 00136 NM 1999 4 2 CA981113008 1 19981101 A 5610 NP15790213 WINDOW DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10116 120323 (CAN) OUTSIDE PANE OF CAPTAIN'S SIDE WINDOW FOUND CRACKED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200137 19990402 00137 NM 1999 4 2 CA981113009 1 19981030 A 2770 82740037101 SPRING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE GUSTLOCK BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 20348 120843 (CAN) IN TAXI, FLIGHT CREW NOTICED THE GUSTLOCK HANDLE HAD LITTLE OR NO SPRING TENSION WHEN APPLIED. INSPECTION OF THE AILERON SPLITTER QUADRANT AT CENTER WING WAS CARRIED OUT. THE TOP ONE OF THE TWO SPRINGS FOR THE GUSTLOCK LEVER WAS BRO KEN AT THE EYE END. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200138 19990402 00138 NM 1999 4 2 CA981116014 1 19981105 A 3230 89607 CENTERING MECH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NOSE GEAR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 30241 DCL11386 120248 (CAN) THE CENTERING MECHANISM FOR THE NOSE GEAR WAS FOUND CRACKED. CRACK ABOUT 3 INCHES LONG. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200139 19990402 00139 EU 1999 4 2 CA981123020 1 19981108 A 3246 AHA1489 WHEEL BAG BAE146 BAE146200A 1500266 EU MLG CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING INSPECTION, CORRSION BEYOND MANUFACTURER LIMITS WAS FOUND IN THE TIE BOLT HOLES. 2 H 7 4 4F RT A49EU 1999040200141 19990402 00141 EU 1999 4 2 CA981125002 1 19980922 A 2120 UNKNOWN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE AIR DISTRIBUTION ODOR W O OTHER O OTHER CR CRUISE 1 CA LF05627A (CAN) DURING CRUISE, THE FLIGHT ATTENDANT REPORTED A SWEET SICKLY SMELL IN CABIN, NOT AN OIL SMELL. ALSO REPORTED A SOR E THROAT AND SORE EYES. ENGINES CHECKED FOR OIL ON NR 1 AND NR 9 SEALS AND BLEED BANDS. NO OIL LEAKS FOUND. NR 1 AND NR 2 AIR CONDITIONING PACK OUTLET DUCTS REMOVED AND INSPECTED FOR CONTAMINATION. NIL FOUND. 2 H 7 4 4F 4 F RT A49EU E6NE 1999040200142 19990402 00142 EA 1999 4 2 CA981125004 1 19980930 A 3231 83231020003 SPRING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE LT MLG DOOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 16581 123132 (CAN) LEFT MAIN LANDING GEAR CENTER/REAR DOOR SPRING UPPER ATTACH END FOUND BADLY ELONGATED. BUSHING P/N NAS77-5-66 FOU ND CUT THROUGH 60 PERCENT AND ATTACH BOLT P/N NAS1105-15D CUT THROUGH 30 PERCENT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200143 19990402 00143 NM 1999 4 2 CA981125005 1 19981018 A 3230 8800133 NOSE GEAR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FWD FUSELAGE CONTAMINATED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 7370 DEC0018395 120322 (CAN) ON APPROACH WHEN GEAR SELECTED DOWN, NOSE GEAR DID NOT INDICATE. DID FLYBY AND GEAR NOT EXTENDED. BEFORE TRYING ALTERNATE SYSTEM, GEAR EXTENDED AND LOCKED. LANDING NORMAL. NOSE GEAR BAY FOUND GEAR ASSY PACKED WITH ICE AND SLUSH. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200144 19990402 00144 NM 1999 4 2 CA981125007 1 19980101 A 2435 23088002A BEARING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 GENERATOR FAILED W O OTHER B J SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION AP APPROACH 1 CA 4501 1320 120156 (CAN) ON FINAL, NR 1 DC GENERATOR FAILED. RESET, BUT THERE WAS AN ELECTRICAL SMELL IN THE COCKPIT. INSPECTION FOUND A NR 1 GENERATOR BEARING HAD FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200145 19990402 00145 NM 1999 4 2 CA981125008 1 19981106 A 3340 MS24178D1 RELAY DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE FLARE LIGHT SHORTED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 22770 120152 (CAN) STRONG ELECTRICAL SMELL ON FLIGHT DECK DURING LANDING. LEFT FLARE LIGHT RELAY 33-40-K2 SHORTED AND ARCING INTERNA LLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200146 19990402 00146 EU 1999 4 2 CA981125009 1 19981112 A 2897 0401KCL3 WIRE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUEL QUANTITY CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 23751 LF05491A (CAN) FUEL QUANTITY SYSTEM WIRING FOUND CHAFED. CHAFING IS WHERE WIRING FROM TANK SENSOR PASSES THROUGH TY WRAPS. 2 H 7 4 4F 4 F RT A49EU E6NE 1999040200147 19990402 00147 NM 1999 4 2 CA981125010 1 19981111 A 2913 570347 PUMP DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 FAILED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 16394 10277 MX418534A 120648 (CAN) ON TAKEOFF, THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200148 19990402 00148 EU 1999 4 2 CA981125011 1 19981105 A 2760 HC276H0059014 LEVER BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT BROKEN W O OTHER O OTHER NR NOT REPORTED 1 CA 23751 LF05491A (CAN) UPON SELECTION OF AIRBRAKE/SPOILER, THE HANDLE BROKE OFF. 2 H 7 4 4F 4 F RT A49EU E6NE 1999040200151 19990402 00151 EU 1999 4 2 CA981125092 1 19981026 A 2710 HC270H0041062 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE BS 151 FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 5099 (CAN) THE AILERON CONTROL CABLE AT PULLEY STA 151.50 WAS FOUND WITH 4 OF 7 BROKEN STRANDS. 2 H 7 4 4F 4 F RT A49EU E6NE 1999040200152 19990402 00152 NM 1999 4 2 CA981130017 1 19981118 A 2910 82950010277 TUBE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYSTEM CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20698 120368 (CAN) HYDRAULIC LEAK UNDER THE LEFT WING LED TO FINDING A CRACKED TUBE ASSEMBLY. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200166 19990402 00166 NM 1999 4 2 CA981230003 1 19981105 A 5310 210025XXX FASTENER 210003 PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA SPAR FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 3053 L1119248A (CAN) ONE FASTENER IN THE FORWARD MAIN SPAR CAP UPPER SKIN FITTING WAS FOUND SHEARED. INITIAL ALERT WAS A PROTRUDING FA STENER. IT HAD FAILED APPROXIMATELY .3750 INCH BELOW THE HEAD. 1 M 7 2 3O 3 O RT A17WE 1E4 1999040200177 19990402 00177 NM 1999 4 2 CA981230059 1 19981202 A 2760 82950010115 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT SPOILER LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 31446 120324 (CAN) LEFT HAND SPOILER LINE REPLACED BECAUSE OF A PIN HOLE. SEE IPC 29-00-00-35-190. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200179 19990402 00179 NM 1999 4 2 CA981230061 1 19981209 A 2435 23088002A BEARING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE START/GENERATOR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 1463 709 120459 (CAN) STARTER/GENERATOR CAUTION LIGHT ON IN CLIMB. REPLACED STARTER/GENERATOR. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200181 19990402 00181 EU 1999 4 2 CA990310086 2 19981218 A 7250 BLADE FOKKER F28 F28MK1000 4990808 EU RROYCE SPEY SPEY55515 54521 EU NR 1 ENGINE MISSING W E C ENGINE SHUTDOWN ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CA 9036 (CAN) NR 1 ENGINE WAS VIBRATING AT TAKEOFF POWER WHILE TAXIING. THE AIRCRAFT RETURNED TO THE GATE WHERE THE ENGINE WAS INSPECTED AND THE LP COMPRESSOR WAS LUBRICATED. DURING SUBSEQUENT RUN-UP, ALL ENGINE PARAMETERS WERE NORMAL, BUT WHEN T AKEOFF POWER WAS APPLIED, THE ENGINE BEGAN TO VIBRATE VIOLENTLY. INSPECTION FOUND A MISSING TURBINE BLADE AND SOME MET AL IN THE TAILPIPE. THE ENGINE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. ENGINE RETURNED TO R & O, FURTHER RE PORT TO FOLLOW. 2 L 7 2 4F 4 F RT A20EU E2EU 1999040200286 19990402 00286 EU 1999 4 2 C2XA98IA548 1 19981229 A 3350 7008123 LAMP AEROSP ATR42 ATR42500 EU CABIN WRONG PART A C2XA K NONE W INADEQUATE Q C TO TAKEOFF 1 SW 09 15447 505 IAH - FLT 3742 - EFD/IAH - THE CREW REPORTED THE EMERGENCY LIGHT CIRCUIT BREAKER TRIPPED ON TAKEOFF ROLL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED INCORRECT LIGHT BULBS IN THE FORWARD EMERGENCY EXI T LIGHT, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (X) 2 H 7 2 4T RT A53EU 1999040200298 19990402 00298 CE 1999 4 2 COEA9801856 1 19981219 A 5350 26700362 RADOME CESSNA 208 208B 2073701 CE FUSELAGE FRACTURED A COEA O OTHER C F.O.D. NR NOT REPORTED 1 NM 13 856FE 208B0176 PILOT REPORTED THAT HE HAD A BIRD STRIKE ON THE RADOME. UPON INSPECTION OF THE RADOME, THE MOST FORWARD PART OF THE RAD OME WAS INDENTED APPROXIMATELY 2 INCHES DEEP BY 4 INCHES ACROSS. REMOVED AND REPLACED RADOME. AIRCRAFT RETURNED TO SERV ICE. (X) 1 H 7 1 3T A37CE 1999040200365 19990402 00365 NM 1999 4 2 QXEA9900532 1 19980215 A 5711 SPAR DHAV DHC8 DHC8102 2809003 NM LEFT WING SCRATCHED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 815PH 50 YXX - LEFT-HAND WING FORWARD SPAR UPPER AND LOWER SPAR CAP FLANGES SCRATCHED. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 5 1-20-36. 2 H 7 2 4T RT A13NM 1999040200536 19990402 00536 EU 1999 4 2 99ZZZX1331 1 19980902 A 6410 704A33633116 BEARING SNIAS 350 AS350B2 8680813 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 93LG 338 2654 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999040200538 19990402 00538 EU 1999 4 2 99ZZZX1333 1 19980824 A 2913 704A34310006 PUMP SNIAS 350 AS350B2 8680813 EU HYDRAULIC SYSTEM WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 93LG 277 70431177 2654 EXCESSIVE SPLINE WEAR. REPLACED PUMP WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999040200539 19990402 00539 EU 1999 4 2 99ZZZX1334 1 19981003 A 6321 350A32501000 SUPPORT SNIAS 350 AS350B2 8680813 EU MAIN ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 792 2917 WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999040200540 19990402 00540 EU 1999 4 2 99ZZZX1335 1 19981010 A 2844 642792002 TRANSMITTER SNIAS 350 AS350B2 8680813 EU FUEL SYSTEM FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 97LG 404 1521 2917 FUEL PRESSURE GAUGE PEGS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999040200541 19990402 00541 EU 1999 4 2 99ZZZX1336 1 19980827 A 6410 704A33633171 HINGE SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 5771C 271 1369 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED UNIT. 1 G 7 1 3U H9EU 1999040200542 19990402 00542 NE 1999 4 2 99ZZZX1337 2 19981219 A 7412 9550164470 EXCITER SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE IGNITION FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 151AC 239 485 1173 EXCITER INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U 3 U H9EU E19EU 1999040200543 19990402 00543 EU 1999 4 2 99ZZZX1338 1 19981211 A 2932 MA12401 SWITCH SNIAS 350 AS350B 8680801 EU HYDRAULIC SYSTEM MALFUNCTIONED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 22UM 893 1065 REJECTED NEW, OUT-OF-BOX. WARNING LIGHT STAYS ON UNTIL RPM REACHES FULL. WARNING LIGHT SHOULD TURN OFF AT IDLE RPM. R EPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999040200544 19990402 00544 EU 1999 4 2 99ZZZX1339 1 19981014 A 6410 704A33633116 BEARING SNIAS 350 AS350B 8680801 EU TAIL ROTOR WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 22UM 440 1065 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 1 3U H9EU 1999040200638 19990402 00638 NM 1999 4 2 AALA990226 1 19980115 A 5311 FRAME BOEING 727 727223 1384074 NM BS 520 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENTS AT BELL FRAME STATION 520 BETWEEN STRINGER 23L AND 24L. REMOVED A 2 INCH BY 1.63 INCH WIDTH AND 1 SQU ARE INCH SECTION OF DAMAGE MATERIAL 13.5 INCH 7075T-6 .063 THICK 'J' DOUBLER USED 30MS20470D-6 RIVETS, 3 FAST PAST DAMAG E 2 ROWS ON SIDE 1 ROW ON TOP. (M) 2 L 7 3 4F A3WE 1999040200656 19990402 00656 NM 1999 4 2 AALA990208 1 19980121 A 5311 FRAME BOEING 727 727223 1384074 NM BS 700 DENTED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 894AA 22010 TUL - FOUND DENT BELL FRAME STATION 700 BETWEEN STRINGER 21R AND STRINGER 22R. REPAIRED PER SRM AARD 53-10-7-3 PAGE 1. (M) 2 L 7 3 4F A3WE 1999040200678 19990402 00678 NE 1999 4 2 AALA981372 2 19980709 A 7260 9395M78G08 ADAPTER AIRBUS 300 A300B4605R 3930308 EU GE CF6 CF680C2A5 NE NR 1 ENGINE FAILED A AALA A E UNSCHED LANDING ENGINE SHUTDOWN A J FLAME/FIRE WARNING INDICATION CR CRUISE 1 SW 07 80057 465 695250 SJU - FLT 574 - DURING CRUISE NR 1 ENGINE WAS SHUT DOWN BY CREW DUE TO ENGINE FIRE. RETURNED AND LANDED SJU. REPLACED NR 1 ENGINE. SHOP FOUND THE AGB IDLER ADAPTER THREADED INSERTS WERE PULLED OUT CAUSING FUEL TO LEAK, FIRE AND ENGINE SH UTDOWN. GENERAL ELECTRIC ISSUED SB 73-A283 REV2 TO CORRECT SITUATION. (M) 2 L 7 2 4F 4 F RT A35EU E13NE 1999040200714 19990402 00714 NM 1999 4 2 P2EA99082 1 19980218 A 5330 SKIN BOEING 737 737222 1384473 NM BS 500 DAMAGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 208AU 19547 SJO - DURING Q-CHECK, AN EXISTING SKIN REPAIR LOCATED AT BS 500A, STRINGER 26R WAS REMOVED FOR INVESTIGATION. AREA WAS CLEANED, INSPECTED AND REPAIRED AS PER SRM 53-30-3 FIG 1. (M) 2 L 7 2 4F A16WE 1999040200872 19990402 00872 WP 1999 4 2 DHL9980518C 1 19981228 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 1160 BROKEN A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FWD OF AFT LOWER CARGO COMPT BETWEEN STA 1160 AND 1200 LONGERON 31L BROKEN FLOOR STRAP. REMOVED AND FABRI CATED NEW FLOOR STRAP 10 X 3 AND INSTALLED PER SRM 51-1-21. N/R 870 2 L 7 4 4F RT 4A25 1999040200873 19990402 00873 WP 1999 4 2 DHL9980519C 1 19981230 A 5320 STRAP DOUG DC8 DC873F 302199F WP BS 1140 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FWD OF AFT CARGO COMPT TOP OF LONGERON 35R AND ON CIRFUMFERENTIAL 1140 FLOOR STRAP CRACKED. REMOVED DAMAGED FLOOR STRAP, FABRICATED AND INSTALLED NEW STRAP PER SRM 51-1-21. N/R 871 2 L 7 4 4F RT 4A25 1999040200895 19990402 00895 WP 1999 4 2 DHL9980541C 1 19981227 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 620 CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LOWER FUSE STA 620 APPROX STRINGER SUPPORT ANGLE CRACKED. FABRICATED NEW ANGLE, 3 X 2, INSTALLED PER SRM 5 1-1-21. N/R 719 2 L 7 4 4F RT 4A25 1999040200898 19990402 00898 WP 1999 4 2 DHL9980544C 1 19981223 A 5753 PANEL DOUG DC8 DC873F 302199F WP RT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING FLAP TRACK XW 219 ICE SHIELD HINGED PANELS HAVE RUB MARKS AND BOTH TRACKS HAVE RIB MARKS. REMOVED D AMAGED PANEL AND FABRICATED NEW SECTION PER SRM 51-1-8. N/R 592 2 L 7 4 4F RT 4A25 1999040200899 19990402 00899 WP 1999 4 2 DHL9980545C 1 19981229 A 5730 COVER DOUG DC8 DC873F 302199F WP RIGHT MLG DOOR CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT MLG DOOR UPLATCH COVER IS CRACKED ABOUT 1.5 INCH LONG. REMOVED AND FABRICATED UPLATCH COVER 8 X 5, PER S RM 51-3-0. N/R 597 2 L 7 4 4F RT 4A25 1999040200900 19990402 00900 WP 1999 4 2 DHL9980546C 1 19981228 A 5730 SKIN DOUG DC8 DC873F 302199F WP LEFT WING CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT WING WHEEL WELL CUTOUT TO T/E PANEL VERT AFT SKIN LOWER CORNER HAS CRACK. REMOVED WEB AND FABRICATED LOW ER CORNER AND INSTALLED PER SRM 51-1-21. N/R 581 2 L 7 4 4F RT 4A25 1999040200910 19990402 00910 WP 1999 4 2 DHL9980556C 1 19981221 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NOSE LANDING GEAR WHEEL WELL FWD RT DOOR HINGE CUT OUT AFT SECTION HAD CRACK. STOP DRILLED CRACK AND FABRIC ATED REPAIR DOUBLER PER SRM 53-2-3, 7.5 X 5. N/R 306 2 L 7 4 4F RT 4A25 1999040200911 19990402 00911 WP 1999 4 2 DHL9980557C 1 19981217 A 5330 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, NOSE LANDING GEAR WHEEL WELL FWD LT DOOR HINGE CUT OUT AFT SECTION HAD CRACK. CLEANED DAMAGED AREA, STOP DR ILLED CRACK AND FABRICATED REPAIR DOUBLER PER SRM 53-2-3. N/R 307 2 L 7 4 4F RT 4A25 1999040200916 19990402 00916 WP 1999 4 2 DHL9980562C 1 19981231 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 1680 DENTED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, FS 1680 LT SIDE HAS DENT OUT OF LIMITS. CUT OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER 10 X 12, FILLER 12 X 4 PER SRM 53-2-1. N/R 271 2 L 7 4 4F RT 4A25 1999040200921 19990402 00921 WP 1999 4 2 DHL9980567C 1 19981219 A 5730 SKIN DOUG DC8 DC873F 302199F WP FUSELAGE CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, LT MLG WHEEL DOOR CUTOUT CRACKED FWD I/B CORNER. STOP DRILLED CRACK, FABRICATED DOUBLER REPAIR, INSTALLED PER SRM 53-2-3. N/R 211 2 L 7 4 4F RT 4A25 1999040900054 19990409 00054 1999 4 9 98UAL900217 4 19980525 A 2565 580242022000 CABLE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE EMER EXIT SLIDE BROKEN A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 601UA 21862 LEFT HAND OVERWING SLIDE DOOR OPEN AND SLIDE PARTIALLY DEPLOYED. *S/D* INADVERTANT DEPLOYMENT DURING OVERWING EXIT HATCH WINDOW SHADE EXCHANGE. REASON FOR PARTIAL DEPLOYMENT IS THE SWAGED END OF THE INFLATION CABLE SEPARATED FROM CABLE. R EPLACED CABLE. 2 L 7 2 4F 4 F RT A1NM E3NE 1999040900055 19990409 00055 NM 1999 4 9 98UAL900221 1 19980528 A 5220 BACT32641072 CONTROL ROD TELEDYNE BACT32641072 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE LT EMER EXIT OUT OF ADJUST A UALA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 WP 29 656UA 25394 EMERGENCY DOOR LIGHT ILLUMINATES INTERMITTENTLY AND EICAS MESSAGE LEFT WING SLIDE ILLUMINATES. *S/D* DOOR LATCH LINKAGE WAS FOUND OUT OF RIG. PERFORMED ADJUSTMENT PER MM. NO EICAS MESSAGE DISPLAYED AFTER RETURNING OVERWING SLIDE SYSTEM TO NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999040900056 19990409 00056 NE 1999 4 9 98UAL900365 2 19980729 A 7230 51G944 SEAL PRATT & WHIT 52G381 BOEING 777 777222 1385219 NM PWA 4090 PW4090 52122 NE NR 2 BEARING FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS CL CLIMB 1 WP 29 796UA 1830 26931 777049 AFTER TAKEOFF AT 1500 FEET, LEFT OIL QUANTITY WENT TO ZERO, LEFT N1 WENT TO ZERO, SMOKE REPORTED IN COCKPIT, LEFT ENGINE SHUT DOWN. RETURNED TO LHR. *S/D* THE ENGINE WAS REMOVED AND ANALYSIS REVEALED THE NR 2 BEARING FRONT CARBON SEAL (51G 944) WAS FOUND WORN DOWN AND SHATTERED. THE 1.5-2 SEAL ASSY (52G381) WAS A PRE SB72-138 CONFIGURATION. 2 L 7 2 4F 4 F RT T0001SE E46NE 1999040900057 19990409 00057 1999 4 9 98UAL900533 4 19981111 A 3425 PFD AIRBUS A319 A319131 NM IAE V2522 V2522A5 NE RT COCKPIT FAILED A UALA K NONE O OTHER CR CRUISE 1 WP 29 809UA 825 CREW REPORTS PFD AND ND ON F-O'S SIDE WENT BLANK. *S/D* SECURED TERMINAL BLOCK 2VG. TERMINAL BLOCK HAD HIGH RESISTANCE ON GND PIN 102 OF F/O ND, PFD, AND LOWER DU. AIRCRAFT THEN TESTED OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900058 19990409 00058 EU 1999 4 9 98UAL900534 1 19981110 A 2910 SWITCH AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE GREEN HYD SYST FAILED A UALA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 WP 29 423UA 504 GREEN HYDRAULIC SYSTEM LOW-PRESSURE/LOW VOLUME. LANDED AMBER ALERT. *S/D* FOUND HYDRAULIC LEAK AT GREEN HYDRAULIC PRESS URE SWITCH ON NR 1 ENGINE. LEAK COMING FROM PACKING. REPLACED PRESSURE SWITCH, OPS CHECK GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900059 19990409 00059 NE 1999 4 9 98UAL900536 2 19981112 A 7530 6A3321 ARM AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE FAILED A UALA A E UNSCHED LANDING ENGINE SHUTDOWN E J VIBRATION/BUFFET WARNING INDICATION CR CRUISE 1 WP 29 418UA 14878 485 485 NR 1 ENGINE: STALL ECAM WARNING DISPLAYED. AUDIBLE 'THUMP' ON RHS OF AIRCRAFT AT FL310. NR 1 EGT WENT TO 1800 DEGREES. ENGINE SHUTDOWN. DIVERTED TO GRR UNDER AMBER ALERT. *S/D* ENGINE DISASSEMBLY INVESTIGATION FOUND A VARIABLE STATOR VANE LEVER ARM FAILED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900060 19990409 00060 EU 1999 4 9 98UAL900541 1 19981112 A 8011 STARTER HAMILTON STA 7904252 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 ENGINE MALFUNCTIONED A UALA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 414UA 472 SPARKS UNDER NR 1 ENGINE UPON START-UP NOTED BY PUSHBACK MECHANIC. SHUTDOWN ENGINE. *S/D* REPLACED STARTER AND START VA LVE PER MM 80-13-41. OPERATIONAL CHECK TESTED GOOD. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900061 19990409 00061 EU 1999 4 9 98UAL900546 1 19981030 A 2612 FIRE LIGHT AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE APU ILLUMINATED A UALA O OTHER N FALSE WARNING CR CRUISE 1 WP 29 401UA 435 CREW REPORTED THE APU FIRE LIGHT CAME ON WHILE IN CRUISE. NO ASSOCIATED ECAM WARNINGS. THE APU WAS OFF, AND THE APU FIRE LIGHT IS INTERMITTANT. *S/D* POST FLIGHT REPORT SHOWS ECAM WARNING APU FIRE, BUT NO FAILURE MESSAGE. APU FDU TESTED OK. LAST LEG AND PREVIOUS LEGS REPORTS SHOW NO FAULTS. APU START AND RUN NORMAL. CHECKED FIRE LOOPS IN APU COMPARTMEN T AND FOUND NO DISCREPANCIES. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900062 19990409 00062 EU 1999 4 9 98UAL900549 1 19981119 A 2133 OUTFLOW VALVE NORDMICRO 90231570381 AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE CABIN BROKEN A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 421UA 500 464 PASSING 9000' GOT CABIN PRESSURE ECAM & MASTER WARNING. VERTICAL SPEED WAS UP TO 500+ AND DOWN TO -1200 FPM. CABIN TEM P WENT FROM WARM TO COLD SEVERAL TIMES BEFORE LANDING. RETURNED TO DEN. *S/D* FOUND BROKEN BACKSHELL ON ACTUATOR ELEC TRONIC 1, 10HLA OF OUTFLOW VALVE. BROKEN BACKSHELL WAS CHAFING NUMEROUS WIRES. PROTECTED EACH WIRE IN CONNECTOR WITH H EAT SHRINK, REPLACED BACKSHELL AND SECURED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900063 19990409 00063 EU 1999 4 9 98UAL900565 1 19981123 A 3200 LINE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE RT MLG DOOR LEAKING A UALA O OTHER K J FLUID LOSS WARNING INDICATION AP APPROACH 1 WP 29 412UA 465 FLIGHT CREW ACCOMPLISHED MANUAL GEAR EXTENSION DUE TO LOSS OF GREEN HYDRAULIC SYSTEM. AMBER ALERT, NORMAL LANDING. *S/D* FOUND HYDRAULIC LINE AT RIGHT MLG DOOR BYPASS VALVE LEAKING. REPLACED LINE, LEAK CHECK OK. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900064 19990409 00064 NM 1999 4 9 98UAL900610 1 19981222 A 2530 BUFFET BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE GALLEY DEFECTIVE A UALA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 7446U 21900 COFFEEMAKER IN AFT GALLEY SMOKING. *S/D* THE COFFEEMAKER WAS CHECKED FOR PROPER OPERATION. NO SMOKE WAS PRESENT WITH PO WER TO THE GALLEY OFF. THE BUFFET WAS REPLACED AT THE TERMINATION OF THE FLIGHT. 2 L 7 3 4F 4 F A3WE E2EA 1999040900065 19990409 00065 EU 1999 4 9 98UAL900623 1 19981231 A 3260 LGCIU ULTRA ELECTR 664700500A4B AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE NR 1 DAMAGED A UALA O OTHER N FALSE WARNING AP APPROACH 1 WP 29 402UA 439 ECAM FOR UNSAFE LANDING GEAR DISPLAYED. CAPT RECYCLED GEAR AND IT CAME DOWN AND LOCKED NORMALLY. *S/D* CAPT RECYCLED GEAR AND IT CAME DOWN AND LOCKED NORMALLY. REPLACED NR 1 LGCIU DUE TO BROKEN PIN AT J-1. INSPECTED PROX SENSORS 13GA A ND 19GA. JACKED AIRCRAFT, SWUNG GEAR SEVERAL TIMES. ALL INDICATIONS NORMAL. NO ECAM MSGS DISPLAYED. 2 L 7 2 4F 4 F RT A28NM E40NE 1999040900066 19990409 00066 NM 1999 4 9 98UAL900624 1 19981231 A 3350 900835A BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE 1R DOOR DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7462U 21916 NR 1R SERVICE DOOR EMERGENCY ILLUMINATION LIGHT INOPERATIVE. *S/D* REPLACED BATTERY ASSEMBLY. 2 L 7 3 4F 4 F A3WE E2EA 1999040900068 19990409 00068 NM 1999 4 9 98UAL900628 1 19980311 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 392UA 24667 DAMAGE CENTERED AT BS 270 STRINGER 24R (LAP SPLICE), JUST BELOW LAV SERVICE PANEL, ABOVE THE NOSE LANDING GEAR DOOR. THE IMPACT PUNTURED THE FUSELAGE SKIN IN 3 PLACES, SEVERING STR 28R AND 24R AT BS 300, AND DAMAGING STRINGER 24R AT BS 240 AND CRUSHING THE OUTBOARD CHORDS OF THE FRAMES AT BS 243.7 & 235.8. ALSO, DAMAGE TO NLG DOOR UPPER FWD CORNER. LAV SERV ICE TRUCK IMPACT. REPAIRED BY SRM 53-00-01 FIG 212 (SKIN LAP SPLICE), SRM 51-70-11/12/13 (STRINGERS, FRAMES, AND BULKHE ADS). SRM 53-00-01 FIG. 201/202 (SKIN REPAIR) AND SRM CHAPTER 51 GENERAL SHEET METAL PRACTICES (DENT REWORK, SEALING, F ASTENERS). NLG DOOR REPAIRED PER SRM 51-70-05 (250 DEGREE GRAPHITE COMPOSITE REPAIR). 2 L 7 2 4F 4 F RT A16WE E2GL 1999040900069 19990409 00069 NM 1999 4 9 98UAL900629 1 19980108 A 5310 STRUCTURE BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE FUSELAGE DAMAGED A UALA K NONE C F.O.D. IN INSP/MAINT 1 WP 29 393UA 24668 DAMAGE AT FUSE SKIN ASSY (65-45800-1257) & CIRCUMFERENTIAL FRAMES STA 178 - 259, BL 0 & S-24L. S-24L (65-45800-1247) WAS SEVERED. THE FWD PORTION OF THE LT NLG DOOR WAS CRUSHED, THE LWR O/B CORNER STA 227.8 BULKHEAD WEB WAS CRACKED AND/OR B ENT. A 7.25 SECTION OF THE E & E DOOR SURROUND DOUBLER WAS SEVERED STA 227.8 TUG IMPACT. THE SUBJECT BONDED SKIN PANEL , THE SECTION OF S-24L STA 178 TO STA 259 & THE LT NLG DOOR WERE REPLACED. THE STA 203.8 FRAME WEB & I/B & O/B CHORDS W ERE REPAIRED. THE STA 196.5, 211.8, 219.8, 227.8, 235.8, 243.7 & 251.5 WEBS & CONSTITUENT CHORDS WERE REPAIRED PER SRM 51-70-13, FIG 1 & 51-70-12, FIG 1. THE E & E DOOR SURROUND DOUBLER DAMAGE AT STA 227.8 WAS REPAIRED. 2 L 7 2 4F 4 F RT A16WE E2GL 1999040900070 19990409 00070 WP 1999 4 9 98UAL900630 1 19981217 A 3211 7165820106 BOLT DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE RT MLG FAILED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 1856U 28787 46975 FRACTURE OF THE OUTBOARD RIGHT HAND MAIN LANDING GEAR ATTACH FITTING ATTACH BOLT. THE WASHER ALSO FAILED IN THE AREA OF THE BOLT FRACTURE. *S/D* FAILED WASHER SHOWS EVIDENCE OF MOISTURE ENTRAPMENT. BOLT FAILED AS A RESULT OF CORROSION IND UCED STRESS. BOLT, NUT AND WASHERS WERE REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 1999040900071 19990409 00071 1999 4 9 98UAL900631 4 19981105 A 2565 D31039202 MATERIAL AIR CRUISERS D31098202 BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE EXCAPE SLIDE LEAKING A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 529UA 9795 0364 25019 SLIDE FAILED AIR RETENTION DURING SHOP TEST. *S/D* UNIT WAS SENT TO THE VENDOR FOR EVALUATION AND REPAIR. THE SLIDE LEA KED DUE TO POROSITY OF THE INFLATABLE MATERIAL, AND WAS BEYOND REPAIR. 2 L 7 2 4F 4 F RT A2NM E17NE 1999040900581 19990409 00581 WP 1999 4 9 USAAD99041 1 19980309 A 2150 71145730016 SLEEVE DOUG DC9 DC981 3022081 WP RT PACK RUPTURED A USAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 EA 19 828US 48028 PHL-PBI - FLT 1930, AT 17,000 FEET THE PRESSURIZATION FLOW LIGHT ILLUMINTED. THE CABIN WAS CLIMBING AT 500-600 FPM WITH THE OUTFLOW VALVE COMPLETELY CLOSED IN BOTH AUTO AND MANUAL. THE ENGINES WERE SET AT CRUISE POWER (.15) EPR. THE AIRCRA FT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLEX SLEEVE IN THE RIGHT PACK TEMP CONTR OL VALVE SUPPLY LINES. (M) 2 L 7 2 4F A6WE 1999041700238 19990417 00238 EA 1999 4 17 99ZZZX1496 1 19981228 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37208 AUG971064 7208 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700239 19990417 00239 EA 1999 4 17 99ZZZX1497 1 19981226 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 77195 OCT960859 7195 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700240 19990417 00240 EA 1999 4 17 99ZZZX1498 1 19981223 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 1 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 77181 OCT960878 7181 FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700241 19990417 00241 EA 1999 4 17 99ZZZX1499 1 19981222 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37218 OCT971106 7218 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700242 19990417 00242 EA 1999 4 17 99ZZZX1500 1 19981222 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 1 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 47202 JUN970002 7202 FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700243 19990417 00243 EA 1999 4 17 99ZZZX1501 1 19981218 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 2 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37218 OCT971110 7218 FOUND HYDRAULIC FLUID LEAKING FROM NR 2 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700244 19990417 00244 EA 1999 4 17 99ZZZX1502 1 19981218 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17217 JUL981420 7217 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700245 19990417 00245 EA 1999 4 17 99ZZZX1503 1 19981218 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 2 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17217 OCT971114 7217 FOUND HYDRAULIC FLUID LEAKING FROM NR 2 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700246 19990417 00246 EA 1999 4 17 99ZZZX1504 1 19981217 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 1 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37208 AUG971063 7208 FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700247 19990417 00247 EA 1999 4 17 99ZZZX1505 1 19981128 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 27185 JAN970936 7185 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700248 19990417 00248 EA 1999 4 17 99ZZZX1506 1 19981126 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 1 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37228 OCT960896 7228 FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700249 19990417 00249 EA 1999 4 17 99ZZZX1507 1 19981124 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17175 NOV960919 7175 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700250 19990417 00250 EA 1999 4 17 99ZZZX1508 1 19981124 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17175 NOV960908 7175 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700251 19990417 00251 EA 1999 4 17 99ZZZX1509 1 19981121 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37218 OCT971112 7218 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700252 19990417 00252 EA 1999 4 17 99ZZZX1510 1 19981118 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 2 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17231 JAN981170 7231 FOUND HYDRAULIC FLUID LEAKING FROM NR 2 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700253 19990417 00253 EA 1999 4 17 99ZZZX1511 1 19981111 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 77181 FEB970954 7181 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700254 19990417 00254 EA 1999 4 17 99ZZZX1512 1 19981105 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 17156 OCT960875 7156 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700255 19990417 00255 EA 1999 4 17 99ZZZX1513 1 19981028 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 77181 SEP960838 7181 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700256 19990417 00256 EA 1999 4 17 99ZZZX1514 1 19981014 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37208 MAY970974 7208 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700257 19990417 00257 EA 1999 4 17 99ZZZX1515 1 19981004 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 2 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 47202 JUN971010 7202 FOUND HYDRAULIC FLUID LEAKING FROM NR 2 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700258 19990417 00258 EA 1999 4 17 99ZZZX1516 1 19981003 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37178 FEB970942 7178 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700259 19990417 00259 EA 1999 4 17 99ZZZX1517 1 19981003 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 3 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 47202 JUN971011 7202 FOUND HYDRAULIC FLUID LEAKING FROM NR 3 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700260 19990417 00260 EA 1999 4 17 99ZZZX1518 1 19981001 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 1 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37178 OCT960873 7178 FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700261 19990417 00261 EA 1999 4 17 99ZZZX1519 1 19980925 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 77195 MAY970957 7195 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700262 19990417 00262 EA 1999 4 17 99ZZZX1520 1 19980925 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 47202 JUN971017 7202 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700263 19990417 00263 EA 1999 4 17 99ZZZX1521 1 19980924 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 4 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 37208 AUG971068 7208 FOUND HYDRAULIC FLUID LEAKING FROM NR 4 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700264 19990417 00264 EA 1999 4 17 99ZZZX1522 1 19980614 A 3240 5010520 BRAKE CNDAIR CL600 CL6002B19 EA NR 1 LEAKING A MASA O OTHER K FLUID LOSS IN INSP/MAINT 1 SW 07 27172 OCT960853 7172 FOUND HYDRAULIC FLUID LEAKING FROM NR 1 BRAKE. TEAR-DOWN DATA HAS IDENTIFIED A PROBLEM WITH THE PISTON LEAKING AROUND T HE PIN, AND THE T-SEALS HAVING TO BE REPLACED. AIRCRAFT BRAKING SYSTEMS HAS IDENTIFIED A PROBLEM WITH THE BRAKE PIN NOT BEING FINISHED PROPERLY, WHICH IS SCORING THE SEAL. REF: OPERATOR CONTROL NR MASA99040, AND, NR 99ZZZX1487 THROUGH 99 ZZZX1522. 2 L 7 2 4F RT A21EA 1999041700326 19990417 00326 WP 1999 4 17 CKSA99053 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 789 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING ROUTINE C CHECK AND CPCP FOUND CORROSION ON LOWER FLOORBEAM CAP AT MAIN DECK STA 789, STR 4, LBL 38. CORROSION O UT OF LIMITS PER SRM 51-21-00. FABRICATED REPAIR PARTS IAW SRM 53-21-00 FIG 807. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-21-00 FIG 804. WORK PERFORMED AT AIA MAINTENANCE FACILITY OSCODA. WORK ORDER NUMBER 106-207, SOURCE D OCUMENT CPCP CARD C53-100-02-00, NON ROUTINE TASK CARD NUMBER 34247. 2 L 7 3 4F A23WE 1999041700327 19990417 00327 WP 1999 4 17 CKSA99054 1 19981216 A 5313 LONGERON LKHEED 1011 1011385115 5265015 WP BS 1515 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION AROUND FASTNERS ON LONGERON 29, STA 1515, C-2 CARGO PIT. REMOVED CORRO SION AND FASTNERS IAW SRM 51-21-01 & 51-40-0. FOUND TO BE OUT OF LIMITS IAW SRM 53-13-00 FIG 801. FABRICATED NEW PARTS IAW AIA ENGINEERING SKETCH AIA/E/2886 AND EDR 98AIA-313. INSTALLED REPAIR IAW EDR 98AIA-313 AND SRM 51-40-0. WORK P ERFORMED AT AIA MAINTENANCE FACILITY OSCODA. WORK ORDER NUMBER 106-187, SOURCE DOCUMENT CPCP CARD C53-120-04-02, NON RO UTINE TASK CARD NUMBER 34264. 2 L 7 3 4F A23WE 1999041700328 19990417 00328 WP 1999 4 17 CKSA99055 1 19981216 A 5313 STRINGER LKHEED 1011 1011385115 5265015 WP BS 1783 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION AROUND FASTNERS ON STRINGER 35, STA 1783, C-3 CARGO PIT. REMOVED CORRO SION AND FASTNERS IAW SRM 51-21-01. FOUND TO BE OUT OF LIMITS IAW SRM 53-13-00. FABRICATED REPAIR IAW SRM 53-13-00. I NSTALLED REPAIR IAW SRM 53-13-00. WORK PERFORMED AT AIA MAINTENANCE FACILITY OSCODA. WORK ORDER NUMBER 106-211, SOUR CE DOCUMENT CPCP CARD C53-120-04-03, NON ROUTINE TASK CARD NUMBER 34282. 2 L 7 3 4F A23WE 1999041700329 19990417 00329 WP 1999 4 17 CKSA99056 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 1465 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION ON LOWER FLOOR BEAM CAP AT MAIN DECK STA 1465, STR 35. FABRICATED REPA IR PARTS IAW SRM 53-21-00 FIG 804. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-21-00 FIG 804 SHEET 2. WORK P ERFORMED AT AIA MAINTENANCE FACILITY OSCODA. WORK ORDER NUMBER 106-187, SOURCE DOCUMENT CPCP CARD C53-120-04-02, NON RO UTINE TASK CARD NUMBER 34285. 2 L 7 3 4F A23WE 1999041700330 19990417 00330 WP 1999 4 17 CKSA99057 1 19981216 A 5347 SEAT TRACK LKHEED 1011 1011385115 5265015 WP BS 629 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING ROUTINE C CHECK AND CPCP, FOUND CRACK ON SEAT TRACK, FWD CARGO COMPT, STA 629 TO 630, LBL94. TREATED, PRIMED AND INSTALLED REPLACEMENT IAW SRM 51-40-01. WORK PERFORMED AT AIA MAINTENANCE FACILITY OSCODA. WORK ORDER NUMBER 106-206, SOURCE DOCUMENT CPCP CARD C53-120-04-01, NON ROUTINE TASK CARD NUMBER 32028. 2 L 7 3 4F A23WE 1999041700331 19990417 00331 WP 1999 4 17 CKSA99058 1 19981216 A 5315 FLOORBEAM LKHEED 1011 1011385115 5265015 WP BS 789 CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 106CK 293C1211 DURING ROUTINE C CHECK AND CPCP, FOUND CORROSION ON LOWER FLOORBEAM CAP AT MAIN DECK STA 789, LBL 4. CORROSION OUT OF L IMITS PER SRM 51-21-00. FABRICATED REPAIR PARTS IAW SRM 53-21-00. TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 5 3-21-00 FIG 802. WORK PERFORMED AT AIA MAINTENANCE FACILITY OSCODA. WORK ORDER NUMBER 106-207, SOURCE DOCUMENT CPCP CA RD C53-100-02-00, NON ROUTINE TASK CARD NUMBER 34246. 2 L 7 3 4F A23WE 1999041700375 19990417 00375 NM 1999 4 17 99UAL900193 1 19980406 A 5270 SENSOR ELDEC 834403 BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE EMER EXIT DOOR MALFUNCTIONED A UALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 WP 29 656UA 25394 RIGHT WING SLIDE EICAS MSG DISPLAYED. ALSO, EMERGENCY DOOR LIGHT ILLUMINATED. DIVERTED TO BOS. *S/D* ACCOMPLISHED B ITE CHECK OF PSEU AND FOUND SENSOR S199 FAULTED. REPLACED S199 PER MM5 AND ADJUSTED SENSOR PER MM, OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A1NM E24NE 1999041700431 19990417 00431 WP 1999 4 17 ORJA99122 1 19981005 A 5320 PLATE DOUG DC9 DC983 3022083 WP BS 1155 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, C-CHECK LEVEL II CORROSION, HEAVY CORROSION AROUND VHF ANTENNA NR 3 COUPLES, STAITON 1155, CARGO AFT PIT. FABRI CATED ANTENNA BLANKING PLATE AND INSTALLED IAW DC9-SRM 51-10-2 AND 51-10-3. TREATED AND PRIMED IAW DC0, SRM 51-10-3. ( M) 2 L 7 2 4F RT A6WE 1999041700438 19990417 00438 WP 1999 4 17 ORJA99115 1 19980316 A 3350 BR9661116 BATTERY PACK DOUG DC9 DC983 3022083 WP RT EMER EXIT DISCHARGED A ORJA K NONE L NO TEST IN INSP/MAINT 1 WP 11 834RA 53124 IN LAS - EMERGENCY EXITS ILLUMINATED AUTOMATICALLY A/C RIGHT EMERGENCY EXIT ROW. REMOVED AND REPLACED RIGHT AFT EMERGEN CY OVERWING EXIT BATTERY PACK OPERATES NORMAL. (M) 2 L 7 2 4F RT A6WE 1999042300369 19990423 00369 CE 1999 4 23 99ZZZX1586 1 19981123 A 3250 CONNECTOR 26182742 LEAR 35 35A 5170602 CE NLG STEERING MALFUNCTIONED A DSEA O OTHER O OTHER NR NOT REPORTED 1 GL 25 51LC 302 NOSE WHEEL STEERING WAS FOUND ERRATIC. FOUND WIRING HARNESS TO FOLLOW-UP POTENTIOMETER DAMAGED AND CONNECTOR CORRODED. REPLACED FOLLOW-UP. REINSTALLED NOSE GEAR ASSY. ACFT TT: 8,638.5. 2 L 7 2 4F A10CE 1999042300467 19990423 00467 WP 1999 4 23 RRXA99196 1 19980623 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISI, FOUND CORROSION DAMAGE TO HORIZONTAL STABILIZER SKIN PANEL AT XE 181, DAMAGED BEYOND LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN PANEL IAW SK8550002. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300468 19990423 00468 WP 1999 4 23 RRXA99198 1 19980706 A 5320 INTERCOSTAL DOUG DC8 DC862 3021970 WP BS 1385 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 1385 AND LONGERON 26 LEFT, DAMAGED BEYOND LIMIT S IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 53 -2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300469 19990423 00469 WP 1999 4 23 RRXA99199 1 19980722 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1440 BETWEEN LONGERONS 35 RIGHT TO 36, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW D C-8 53-2-0 FIGURE 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300470 19990423 00470 WP 1999 4 23 RRXA99200 1 19980722 A 5347 FLOOR TRACK DOUG DC8 DC862 3021970 WP BS 980-1380 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR TRACK BETWEEN STA 980 TO 1380 AND BETWEEN LONGERONS 33 LEFT 33 RIGHT TO 36, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR TRACKS IAW DC-8 53-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300471 19990423 00471 WP 1999 4 23 RRXA99193 1 19981006 A 5320 ANGLE DOUG DC8 DC862 3021970 WP BS 759 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 759 BETWEEN BL 54 LEFT TO BL 64, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300472 19990423 00472 WP 1999 4 23 RRXA99194 1 19980620 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 759 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 759 AND BL 66, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300473 19990423 00473 WP 1999 4 23 RRXA99195 1 19980804 A 5512 SKIN DOUG DC8 DC862 3021970 WP HORIZ STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN PANEL AT XE 125 TO XE 146, DAMAGED BEYOND LIMITS IAW DC-8 SRM . REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN PANEL IAW SK8550002. (CORROSIO N DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300474 19990423 00474 WP 1999 4 23 RRXA99201 1 19980702 A 5320 ANGLE DOUG DC8 DC862 3021970 WP BS 1080 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME ATTACHMENT ANGLE AT STA 1080 AND LONGERON 35 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300475 19990423 00475 WP 1999 4 23 RRXA99202 1 19980709 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 35 LEFT AT STA 980, DAMAGED BEYOND LIMITS IAW DC-8 SRM. R EMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300476 19990423 00476 WP 1999 4 23 RRXA99203 1 19980718 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1460-1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 28 RIGHT BETWEEN STA 1460 TO STA 1480, DAMAGED BEYOND LIM ITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300477 19990423 00477 WP 1999 4 23 RRXA99204 1 19980703 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1440-1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 26 LEFT BETWEEN STA 1440 TO STA 1480, DAMAGED BEYOND LIMI TS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300478 19990423 00478 WP 1999 4 23 RRXA99205 1 19980809 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1530 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 34 RIGHT AT STA 1530, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGU RE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300479 19990423 00479 WP 1999 4 23 RRXA99206 1 19980807 A 5311 FRAME DOUG DC8 DC862 3021970 WP BS 1557 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1557 BETWEEN LONGERONS 33 LEFT TO 34 LEFT, DAMAGED BE YOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER I AW DC-8 53-2-5 FIGURE 8C-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300480 19990423 00480 WP 1999 4 23 RRXA99207 1 19980805 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1538 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 36 BETWEEN STA 1535 TO STA 1538, DAMAGED BEYOND LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300481 19990423 00481 WP 1999 4 23 RRXA99208 1 19980809 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1536 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT AT STA 1536, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGU RE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300482 19990423 00482 WP 1999 4 23 RRXA99209 1 19980817 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1536 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 32 LEFT AT STA 1536, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGUR E 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300483 19990423 00483 WP 1999 4 23 RRXA99210 1 19980809 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 1536 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 34 LEFT AND FITTING AT STA 1536, DAMAGED BEYOND LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300484 19990423 00484 WP 1999 4 23 RRXA99211 1 19980707 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1557 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 29 RIGHT, DAMAGED BEYOND LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300485 19990423 00485 WP 1999 4 23 RRXA99212 1 19980809 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1557 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 31 RIGHT, DAMAGED BEYOND LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300486 19990423 00486 WP 1999 4 23 RRXA99213 1 19980804 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1557 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 34 RIGHT, DAMAGED BEYOND LIMITS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300487 19990423 00487 WP 1999 4 23 RRXA99214 1 19980805 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1557 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 35 LEFT, DAMAGED BEYOND LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300488 19990423 00488 WP 1999 4 23 RRXA99215 1 19980809 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1557 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 35 RIGHT, DAMAGED BEYOND LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300489 19990423 00489 WP 1999 4 23 RRXA99216 1 19980706 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 1570-1578 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN DOUBLER AT STA 1570 TO STA 1578 AND BETWEEN LONGERONS 32 LEFT 33 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED NEW ANGLE IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300490 19990423 00490 WP 1999 4 23 RRXA99217 1 19980915 A 5320 ANGLE DOUG DC8 DC862 3021970 WP BS 1606 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 1606 AND LONGERON 32 RIGHT, DAMA GED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 53-2-0 FIGURE 7. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300491 19990423 00491 WP 1999 4 23 RRXA99218 1 19980703 A 5320 DOUBLER DOUG DC8 DC862 3021970 WP BS 920-940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT AND RIGHT WHEEL WELL PRESURE PANEL FINGER DOUBLER AT STA 920 TO STA 940 BETWEEN BL 66 LEFT TO BL 66 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED , TREATED AREA IAW DC -8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DC-8 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F 4A25 1999042300492 19990423 00492 WP 1999 4 23 RRXA99220 1 19980708 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1420 AND LONGERON 21 LEFT, DAMAGED BEYOND LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2- 0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300493 19990423 00493 WP 1999 4 23 RRXA99221 1 19980810 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 940 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300494 19990423 00494 WP 1999 4 23 RRXA99222 1 19980721 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 900 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 900 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300495 19990423 00495 WP 1999 4 23 RRXA99223 1 19980825 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 920 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 920 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300496 19990423 00496 WP 1999 4 23 RRXA99224 1 19980621 A 5320 57541931 PANEL DOUG DC8 DC862 3021970 WP BS 940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT WHEEL WELL PRESURE PANEL AT STA 940 AND BETWEEN BL 63 LEFT TO BL 66 LEFT, DAMAGE BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW FAA APPROVED COTNEY DER ENGINEERING SK ETCH E84-R55. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300497 19990423 00497 WP 1999 4 23 RRXA99225 1 19980708 A 5313 LONGERON DOUG DC8 DC862 3021970 WP BS 880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 RIGHT AT STA 880, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGUR E 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300498 19990423 00498 WP 1999 4 23 RRXA99226 1 19980922 A 5320 FITTING DOUG DC8 DC862 3021970 WP BS 900 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 900 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300499 19990423 00499 WP 1999 4 23 RRXA99227 1 19980922 A 5320 SHEAR TIE DOUG DC8 DC862 3021970 WP BS 902 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 902 AND LONGERON 24 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC-8 SRM 5 1-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999042300500 19990423 00500 WP 1999 4 23 RRXA99228 1 19981122 A 5320 58942822 FITTING DOUG DC8 DC873F 302199F WP BS 300 & 320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND FORWARD CARGO COMPARTMENT TWO FITTINGS AT APPROX STATION 300 AND 320, STRINGER RT 33, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPLACED FITTINGS IAW DC-8 53-2- 0 FIGURE 2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300501 19990423 00501 WP 1999 4 23 RRXA99229 1 19981119 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1219 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACH ANGLE AT STATION 1219 AND LONGERON 27 LT. DAMAGED BEYOND L IMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR AS PER SRM 57-2-0, PAGE 20 AND FIG 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300502 19990423 00502 WP 1999 4 23 RRXA99230 1 19981119 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1219 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACH ANGLE AT STATION 1219 AND LONGERON 27 LT. DAMAGED BEYOND L IMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR AS PER SRM 57-2-0, PAGE 20 AND FIG 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300503 19990423 00503 WP 1999 4 23 RRXA99231 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1660, BL 32 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. CUT OUT DAMAGE IAW SRM 53-2-3. FABRICATED DOUBLER FROM .080 IN 7075T6, FILLER FROM .063 IN 7075T6, ANGLE FROM 7075T6. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300504 19990423 00504 WP 1999 4 23 RRXA99232 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1170 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1170, BL 16 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. CUT OUT DAMAGE, FABRICATED REPAIR PARTS IAW SRM 53-2-3, PG 39/4 0, AND 51-1-8, PG 17. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300505 19990423 00505 WP 1999 4 23 RRXA99233 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1280, BL 18 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED DAMAGED AREA IAW SRM 53-2-3. (CORROSION DAMAGE RECORDE D IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300506 19990423 00506 WP 1999 4 23 RRXA99234 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1040, BL 18 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. CUT OUT DAMAGED AREA IAW SRM 53-2-20, PG 20. FABRICATED REPAIR PARTS PER 53-2-3, PG 40. CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300507 19990423 00507 WP 1999 4 23 RRXA99235 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1020 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1020, BL 50 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. CUT OUT DAMAGED AREA IAW SRM 53-2-3, PG 39-40. FABRICATED DOUB LER FROM .080 IN 7075T6, FILLER FROM .063 IN 7075T6, ANGLES FROM 7075T6. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F RT 4A25 1999042300508 19990423 00508 WP 1999 4 23 RRXA99236 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1160, BL 50 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. CUT OUT DAMAGED AREA IAW SRM 53-2-3, PG 39-40. FABRICATED DOUB LER FROM .080 IN 7075T6, FILLER FROM .063 IN 7075T6, ANGLES FROM 7075T6. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F RT 4A25 1999042300509 19990423 00509 WP 1999 4 23 RRXA99237 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1180 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1180, BL 50 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. CUT OUT DAMAGED AREA IAW SRM 53-2-3, PG 39-40. FABRICATED DOUB LER FROM .080 IN 7075T6, FILLER FROM .063 IN 7075T6, ANGLES FROM 7075T6. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F RT 4A25 1999042300510 19990423 00510 WP 1999 4 23 RRXA99238 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1220 TO 1300, BL 18 RT. DAMAGED BEYOND LIMITS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED REPAIR SECTION IAW DC-8 SRM 51-1-8, PG 39-40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300511 19990423 00511 WP 1999 4 23 RRXA99239 1 19981115 A 5321 DOUBLER DOUG DC8 DC873F 302199F WP BS 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1140, BL 18 RT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CORROSION AT FLOOR PANEL AND INSTALLED DOUBLER ON DAMAG ED AREA AS PER SRM 53-2-3, PG 39-40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300512 19990423 00512 WP 1999 4 23 RRXA99240 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1300, BL 18 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED CORROSION AREA IAW SRM 53-2-3, PG 39-40. AFTER BLEND O UT, OUT OF LIMITS. FABRICATED DOUBLER. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300513 19990423 00513 WP 1999 4 23 RRXA99241 1 19981115 A 5321 104517 FLOOR DOUG DC8 DC873F 302199F WP BS 1430 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1430, BL 6 LT. DAMAGED BEYOND LIMITS IAW DC-8 S RM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-3, PG 39-40. (CORR OSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300514 19990423 00514 WP 1999 4 23 RRXA99242 1 19981115 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 792FT 46046 DURING A MAINTENANCE VISIT, FOUND CORROSION ON CABIN FLOOR PANEL AT STA 1440, BL 46 LT. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED FILLER AND DOUBLER IAW SRM 53-2-3, PG 39-40. (CORRO SION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300516 19990423 00516 WP 1999 4 23 RRXA99574 1 19980727 A 5313 WEB DOUG DC8 DC873F 302199F WP BS 270-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON WEB ON TORQUE BOX AT LONGERON 31R AT STA 270O 280. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED WEB IAW DAC DWG 5753892. LOCATED HOLES IN NEW WEB IAW DC-8 SRM 51-1-24 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300517 19990423 00517 WP 1999 4 23 RRXA99575 1 19980727 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 270-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON WEB ON TORQUE BOX AT LONGERON 31R AT STA 270O 280. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED WEB IAW DAC DWG 5753892. LOCATED HOLES IN NEW WEB IAW DC-8 SRM 51-1-24 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300518 19990423 00518 WP 1999 4 23 RRXA99576 1 19980727 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 270-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON WEB ON TORQUE BOX AT LONGERON 31R AT STA 270O 280. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED WEB IAW DAC DWG 5753892. LOCATED HOLES IN NEW WEB IAW DC-8 SRM 51-1-24 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300519 19990423 00519 WP 1999 4 23 RRXA99577 1 19980727 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 270-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON WEB ON TORQUE BOX AT LONGERON 31R AT STA 270O 280. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED WEB IAW DAC DWG 5753892. LOCATED HOLES IN NEW WEB IAW DC-8 SRM 51-1-24 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300520 19990423 00520 WP 1999 4 23 RRXA99578 1 19980727 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 270-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON WEB ON TORQUE BOX AT LONGERON 31R AT STA 270O 280. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED WEB IAW DAC DWG 5753892. LOCATED HOLES IN NEW WEB IAW DC-8 SRM 51-1-24 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300521 19990423 00521 WP 1999 4 23 RRXA99579 1 19980727 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 270-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON WEB ON TORQUE BOX AT LONGERON 31R AT STA 270O 280. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED WEB IAW DAC DWG 5753892. LOCATED HOLES IN NEW WEB IAW DC-8 SRM 51-1-24 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999042300522 19990423 00522 WP 1999 4 23 RRXA99580 1 19980727 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 270-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON WEB ON TORQUE BOX AT LONGERON 31R AT STA 270O 280. DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED WEB IAW DAC DWG 5753892. LOCATED HOLES IN NEW WEB IAW DC-8 SRM 51-1-24 AND 51-1-22. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000046 19990430 00046 NE 1999 4 30 99ZZZX1685 2 19980609 A 7250 411100720 SHROUD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 753 7125 LE45291EA EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000047 19990430 00047 NE 1999 4 30 99ZZZX1686 2 19980609 A 7240 410106701 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 117CW 753 7125 LE45291EA SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000050 19990430 00050 NE 1999 4 30 99ZZZX1689 2 19981024 A 7250 414129001 PT ROTOR BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 202HN 2567 SC14126 7115 LE45242E FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TC: 5,838.0 . 1 G 7 2 3U 3 U H13EU E5NE 1999043000051 19990430 00051 NE 1999 4 30 99ZZZX1690 2 19980731 A 7240 410106701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 202HN 239 7115 LE45273EA SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000055 19990430 00055 NE 1999 4 30 99ZZZX1694 2 19981026 A 7250 414129001 PT ROTOR BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 428MB 2073 SC20413 7088 LE45152EA FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TC: 5,451.2 . 1 G 7 2 3U 3 U H13EU E5NE 1999043000056 19990430 00056 NE 1999 4 30 99ZZZX1695 2 19981112 A 7240 410106701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 428MB 399 7088 LE45282EA SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000057 19990430 00057 NE 1999 4 30 99ZZZX1696 2 19981021 A 7240 410106701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 428MB 7088 LE45071EA SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000059 19990430 00059 NE 1999 4 30 99ZZZX1698 2 19980826 A 7250 411100720 SHROUD BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TURBINE ROTOR DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 740 7111 LE45144EA EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000060 19990430 00060 NE 1999 4 30 99ZZZX1699 2 19980512 A 7240 410106701 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 911BY 591 7127 LE45083E SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TC: 6,926.0. 1 G 7 2 3U 3 U H13EU E5NE 1999043000073 19990430 00073 NE 1999 4 30 CA980220010 2 19980203 A 7261 TRANSMITTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE LT ENGINE LEAKING W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 807242 (CAN) DURING CRUISE, LEFT ENGINE LOW OIL PRESSURE CAUTION AND AURAL WARNING, NECESSITATING ENGINE SHUT DOWN. FOUND OIL COMING OUT OF THE ENGINE DRAIN MAST, BUT NO OTHER LEAK. TRANSMITTER REPLACED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999043000074 19990430 00074 CE 1999 4 30 CA980225014 1 19980220 A 3040 57033 BLOWER CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE DEFOGGER FAILED W B G I EMER. DESCENT O2 MASK DEPLOYED CABIN DEPRESSURIZATION B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 2617 1288 71711 (CAN) ON DESCENT, THE PILOT'S NOTED A FAINT BURNING ODOR AND GETTING STRONGER. OXYGEN MASKS AND SMOKE GOGGLES PUT ON. S MOKE THEN APPARENT AND AN EMERGENCY DESCENT LANDING CARRIED OUT. THE DEFOG FAN FOUND SEIZED AND THE 20-AMP CIRCUIT BREA KER HAD NOT TRIPPED. SUBMITTER CONSIDERING LOWERING THE TBO FROM 3500 HOURS. 1 L 7 2 4F 4 F A22CE E1NE 1999043000076 19990430 00076 NM 1999 4 30 CA980714027 1 19980629 A 7603 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE LT ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 120190 (CAN) LEFT ENGINE CONDITION CABLE FOUND FRAYED WHERE IT PASSES THROUGH THE FIREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000077 19990430 00077 NM 1999 4 30 CA980714028 1 19980629 A 7603 87600520001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RT ENGINE FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 120190 (CAN) THE RIGHT HAND CONDITION CABLE FOUND FRAYED WHERE IT PASSES THROUGH THE FIREWALL. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000078 19990430 00078 CE 1999 4 30 CA980721018 1 19980713 A 2121 57033 MOTOR AEROSPACECMP 57033 CESSNA 500 550 2076604 CE PWA JT15 JT15D4 52112 NE BLOWER OVERHEATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 3314 1114 71714 (CAN) DURING TAXI AFTER LANDING, THERE WAS A RAPID ACCUMULATION OF SMOKE IN THE COCKPIT. BLOWER MOTOR WINDINGS HAD OVER HEATED. 1 L 7 2 4F 4 F A22CE E1NE 1999043000079 19990430 00079 1999 4 30 CA980724022 4 19980618 A 6113 57A24041 LOW PITCH STOP BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO HARTZL HCC2Y BHCC2YF2 GL LT SPINNER STRIPPED W K NONE O OTHER IN INSP/MAINT 1 CA 78 CS192942R AN5504 (CAN) LEFT SPINNER FOUND LOOSE. FURTHER INSPECTION FOUND THAT THE THREADS ON THE LOW PITCH STOP WERE STRIPPED. FORWARD END OF SPINNER IS SECURED ONTO THE LOW PITCH STOP. 1 L 7 2 3O 3 O RT 3A16 3E1 5 C P920 1999043000080 19990430 00080 NM 1999 4 30 CA980916011 1 19980815 A 5210 85210180001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AIRSTAIR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 121165 (CAN) MAIN AIRSTAIR DOOR UNSUPPORTED DURING OPENING AND CLOSING. THE DOOR SUPPORT CABLE WAS FOUND PULLED OFF AND BROKEN INSIDE THE FORWARD WARDROBE. THE BROKEN CABLE WAS FOUND LYING ACROSS A RELAY PANEL AND MELTED IN TWO FROM CONTACT WITH RELAYS. SUBMITTER STATED SB 8-52-38 NOT DONE ON THIS AIRCRAFT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000083 19990430 00083 EA 1999 4 30 CA981022008 1 19980819 A 2810 C6PF11573 FLAPPER VALVE DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA FUEL SYSTEM LEAKING W O OTHER X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 CA PCE41829 (CAN) AIRCRAFT HAD A FLAME-OUT WHILE SITTING AT FUEL TANKS TO TAKE ON FUEL. APPROXIMATELY 90 POUNDS OF FUEL LEFT IN AFT TANK. FLAPPER VALVE IN NR 5 TANK - THE COLLECTOR - FOUND LEAKING. GRAVITY LIKELY DRAINED THE COLLECTOR TANK CAUSING THE FUEL STARVATION. 1 H 7 2 3T 4 T RT A9EA E4EA 1999043000084 19990430 00084 EA 1999 4 30 CA981027011 1 19981016 A 3213 C6WM140931 BUSHING DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA PCE42143 (CAN) CRACKED INNER BUSHINGS FOUND ON BOTH LEFT AND RIGHT LINK ASSY WHERE STRUT ATTACHES TO LINK AND ALSO WHERE LINK ATT ACHES TO WING FITTING. 1 H 7 2 3T 4 T RT A9EA E4EA 1999043000085 19990430 00085 NM 1999 4 30 CA981109031 1 19981028 A 2722 82960010101 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE RUDDER CHAFED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 27182 120323 (CAN) LARGE HYDRAULIC LEAK FOUND IN TAIL AREA. WIRING HARNESS FOR RUDDER SYNCHRO TRANSIMTTER CHAFED THROUGH RETURN LIN E FOR NR 2 RUDDER ACTUATOR. WIRING HARNESS WRAPPED WITH SPIRAL WRAP. LEAK FOUND IN UPPER PORTION OF LINE JUST BELOW RU DDER SYNCHRO TRANSMITTER. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000087 19990430 00087 NM 1999 4 30 CA981123023 1 19981115 A 2435 AA4N103 CONTACTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 1 ENGINE STUCK W E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 120251 (CAN) SMOKE SMELL IN FLIGHT DECK AFTER NR 1 ENGINE WAS STARTED. FOUND THE START CONTACTOR WELDED SHUT, WHICH CAUSED THE STARTER TO CONTINUE RUNNING AND OVERHEAT. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000088 19990430 00088 NM 1999 4 30 CA981125006 1 19981017 A 3260 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 120156 (CAN) AFTER TAKEOFF, THE WEIGHT-ON-WHEELS CAUTION LIGHT CAME ON. AIRCRAFT RETURNED OK. LEFT NOSE GEAR WEIGHT-ON-WHEELS SENSOR REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999043000095 19990430 00095 EA 1999 4 30 CA981230058 1 19981125 A 2435 CE934641 NUT DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA FIREWALL LOOSE W O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA PCE41388 (CAN) FLIGHT CREW SNAGGED NR 2 GENERATOR AS HARD TO GET ON-LINE. DURING INVESTIGATION, AND RUN-UP, SPARKS WERE NOTICED COMING OUT OF THE 'D' NOSE PANEL ADJACENT TO NACELLE. RIGHT HAND FIREWALL DISCONNECT STUD NUT WAS NOT SECURE AND THE CA BLE WAS VERY LOOSE CAUSING ARCING. 1 H 7 2 3T 4 T RT A9EA E4EA 1999043000630 19990430 00630 NE 1999 4 30 99ZZZX1797 2 19981005 A 7240 410106701 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURBINE SHROUD WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 911VU 235 7141 LE45540EFA SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1999043000632 19990430 00632 NE 1999 4 30 99ZZZX1799 2 19980613 A 7250 411100720 SHROUD BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE GAS PRODUCER TIP RUB A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 528SF 864 7104 LE45320EA EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000640 19990430 00640 NE 1999 4 30 99ZZZX1804 2 19981016 A 7240 413102002 CURL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COMB CHAMBER BURNT A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 117CW 649 7125 LE45385E CURL ASSY HAS EXCESSIVE BURN IN SOME AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000641 19990430 00641 NE 1999 4 30 99ZZZX1805 2 19981021 A 7230 430144801 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 3 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 428MB 8F950102 7088 LE45071EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000642 19990430 00642 NE 1999 4 30 99ZZZX1806 2 19981021 A 7230 430150601 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 2 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 428MB 1847 7088 LE45071EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000644 19990430 00644 NE 1999 4 30 99ZZZX1807 2 19981021 A 7230 430404701 SEAL BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE NR 1 BEARING LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 428MB 3J626 7088 LE45071EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000645 19990430 00645 NE 1999 4 30 99ZZZX1808 2 19981021 A 7250 410106802 SPRING BOLKMS 117 BK117A3 5626015 EU LYC LTS101 LTS101650B1 41560 NE SEAL RING WORN A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 428MB 7088 LE45071EA SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999043000854 19990430 00854 WP 1999 4 30 RRXA 99831 1 19980919 A 5347 SEAT TRACK DOUG DC8 DC863 302198A WP BS 540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, UNDER NUTPLATE AT STA 540, BL 40 RIGHT, WL -1. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. RECEIVED NEW TRACK AND INSTALLED IAW DC-8 SRM 5 1-1-24 AND 51-3-0. 2 L 7 4 4F 4A25 1999043000855 19990430 00855 WP 1999 4 30 RRXA99410 1 19980428 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON SUPPORT MOUNT FITTING AT STA 1400. REMOVED AND DID NOT R EINSTALL IAW BOEING/DOUGLAS DIRECTIVE 367846. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000856 19990430 00856 WP 1999 4 30 RRXA99434 1 19980412 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1250-1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 1260 TO 1250, X+21, Z+1. DAMAGE EXCEEDED LIMIT S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0 AND 53-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000857 19990430 00857 WP 1999 4 30 RRXA99435 1 19980408 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1220-1232 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CABIN AREA FLOOR BOARD AT STA 1220 TO 1232, X+51.5 TO +57.5, Z+0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAI R DOUBLER IAW DC-8 SRM 53-2-0 AND 53-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000858 19990430 00858 WP 1999 4 30 RRXA99436 1 19980424 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GUSSET AT STA 1200, BL 14L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR GUSSET IAW DAC DWG 5887374DC-8 SRM 5 1-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000859 19990430 00859 WP 1999 4 30 RRXA99437 1 19980412 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO L ANGLE AT STA 1040, BL 14L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 53-4-1, FIG 35, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000860 19990430 00860 WP 1999 4 30 RRXA99438 1 19980421 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1040-1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 1040 TO 1060, BL 17L. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 53- 2-0 FIG 1B AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000861 19990430 00861 WP 1999 4 30 RRXA99439 1 19980421 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 1040 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GUSSET AT STA 1040 BL 17L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR GUSSET IAW DAC DWG 5779948 AND 51-1-21 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000862 19990430 00862 WP 1999 4 30 RRXA99440 1 19980421 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GUSSET AND INTERCOSTAL AT STA 1000 BL 19L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR GUSSET IAW DC8 SRM 51 -1-24 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000863 19990430 00863 WP 1999 4 30 RRXA99441 1 19980421 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 940-960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE AND DRILL MARKS TO GUSSET AND INTERCOSTAL AT STA 940 TO 960 BL 13L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR GUSSET IAW DAC DWG S55887374 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000864 19990430 00864 WP 1999 4 30 RRXA99442 1 19980502 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 925-930 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL NR 2 CENTER WING SECTION AT STA 925 TO 930 BL 21L. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC8 SRM 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000865 19990430 00865 WP 1999 4 30 RRXA99443 1 19980421 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 918-922 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GUSSET AT STA 918 TO 922 BL 12L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR GUSSET IAW DAC FWG 9753292-30-8 DC8 SRM 51-1-24 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000866 19990430 00866 WP 1999 4 30 RRXA99444 1 19980505 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 870-1000 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CABIN CENTER WING FLOOR PANEL NR 12 PARTS RACK AT STA 870 TO 1000 X45R LONG 21. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND L ANGLE IAW DC8 SRM 53-2-3 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F RT 4A25 1999043000867 19990430 00867 WP 1999 4 30 RRXA99445 1 19980407 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 780-795 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 780 TO 795 BL 11L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR INTERCOSTAL IAW DAC DWG 97 53291 AND DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000868 19990430 00868 WP 1999 4 30 RRXA99446 1 19980407 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 780-795 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 780 TO 795 BL 12L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR INTERCOSTAL IAW DAC DWG 97 53291 AND DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000869 19990430 00869 WP 1999 4 30 RRXA99447 1 19980428 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 620-640 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 620 TO 640 BL 17L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR INTERCOSTAL IAW DAC DWG 97 53291 AND DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000870 19990430 00870 WP 1999 4 30 RRXA99448 1 19980428 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 560-580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 560 TO 580 BL 17L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLES IAW DC8 SRM 53-2-0 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000871 19990430 00871 WP 1999 4 30 RRXA99449 1 19980504 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 540- CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PANEL P AT STA 540 BL 21R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-3 FIG 10 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000872 19990430 00872 WP 1999 4 30 RRXA99450 1 19980504 A 5330 PANEL DOUG DC8 DC873F 302199F WP BS 510 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PANEL I AT STA 510 BL 21R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. R EMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND L ANGLE IAW DC8 SR M 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000873 19990430 00873 WP 1999 4 30 RRXA99452 1 19980510 A 5330 PANEL DOUG DC8 DC873F 302199F WP BS 436 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PANEL P AT STA 436, X-51, Z-.125. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND L ANGLE IA W DC8 SRM 53-2-3 FIG 10 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000874 19990430 00874 WP 1999 4 30 RRXA99453 1 19980504 A 5330 PANEL DOUG DC8 DC873F 302199F WP BS 420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PANEL P AT STA 420, X-55 TO -60, Z0. DAMAGE EXCEEDED LIMITS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SECTION AND SPLICE PLATES IAW DC8 SRM 53-2-3 FIG 9 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000875 19990430 00875 WP 1999 4 30 RRXA99454 1 19980428 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 361 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GUSSET AT STA 361BL 9L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REM OVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR GUSSET IAW DAC DWG 55887371 AND 51-1-20D . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000876 19990430 00876 WP 1999 4 30 RRXA99455 1 19980407 A 5320 4646163501N SPLICE DOUG DC8 DC873F 302199F WP BS 310 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SPLICE AT STA 310 BL 7L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE MOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. LOCATED SPLICE AND INSTALLED IAW DC8 SRM 51-1-24 AND 51-1-20D. (CORROS ION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000877 19990430 00877 WP 1999 4 30 RRXA99456 1 19980406 A 5320 37746271 FITTING DOUG DC8 DC873F 302199F WP BS 80-100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BARRIER NET FITTING AT STA 80 TO 100 BL 10R. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21H AND 51-3 -0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000878 19990430 00878 WP 1999 4 30 RRXA99457 1 19980406 A 5320 37746271 FITTING DOUG DC8 DC873F 302199F WP BS 80-100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BARRIER NET FITTING AT STA 80 TO 100 BL 12R. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21H AND 51-3 -0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000879 19990430 00879 WP 1999 4 30 RRXA99458 1 19980406 A 5320 3774627501 FITTING DOUG DC8 DC873F 302199F WP BS 80-100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BARRIER NET FITTING AT STA 80 TO 100 BL 14R. DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21H AND 51-3 -0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000880 19990430 00880 WP 1999 4 30 RRXA99459 1 19980406 A 5320 3774627501 FITTING DOUG DC8 DC873F 302199F WP BS 80-100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BARRIER SUPPORT FITTING AT STA 80 TO 100 BL 17R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-24 AND 5 1-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000881 19990430 00881 WP 1999 4 30 RRXA99460 1 19980424 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 80-100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AND GUSSETS AND CARGO NET ATTACH FITTING AT STA 80 TO 100 BL17L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INST ALLED REPAIR INTERCOSTAL IAW DC8 SRM 53-4-0, 51-2-0, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) . 2 L 7 4 4F RT 4A25 1999043000882 19990430 00882 WP 1999 4 30 RRXA99461 1 19980424 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 70-80 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RIGHT END FITTING AT STA 70 TO 80 BL 3R. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000883 19990430 00883 WP 1999 4 30 RRXA99462 1 19980510 A 5320 46143972 FITTING DOUG DC8 DC873F 302199F WP BS 70-80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO END FITTING ON LONG 1 AT STA 70 TO 80. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW DC8 SRM 51-1-21. (C ORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000884 19990430 00884 WP 1999 4 30 RRXA99463 1 19980424 A 5320 46111811 FITTING DOUG DC8 DC873F 302199F WP BS 70-80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO RIGHT END FITTING ON LONG 14R AT STA 70 TO 80. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW DC8 SRM 51-1 -21, 51-1-20D, 51-3-0, AND 51-3-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000885 19990430 00885 WP 1999 4 30 RRXA99464 1 19980407 A 5320 4611067N FITTING DOUG DC8 DC873F 302199F WP BS 70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO END FITTING ON LONG 6L AT STA 70. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. (CORR OSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000886 19990430 00886 WP 1999 4 30 RRXA99465 1 19980512 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 26-40 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LAVATORY AREA UNDER FLOOR AREA AT STA 26 TO 40 X24R. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLES IAW DAC DWG 5888479 AND DC8 SRM 51-1-21 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000887 19990430 00887 WP 1999 4 30 RRXA99466 1 19980720 A 5230 DOOR DOUG DC8 DC873F 302199F WP BS 280-320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FORWARD PIT A-PIT DOOR AT STA 280 TO 320 S+42 TO -42. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIR TO BE ON N/R 27693, 27694, .27695, 27696, 27697, 27698. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000888 19990430 00888 WP 1999 4 30 RRXA99467 1 19980430 A 5320 GUSSET DOUG DC8 DC873F 302199F WP BS 1730 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GUSSET AT STA 1730 BL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. RE MOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED GUSSET IAW DAC DWG 5755032, DC8 SRM 51-1-21, 5 1-1-20D, AND 51-1-21A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000889 19990430 00889 WP 1999 4 30 RRXA99468 1 19980428 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1710 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM SUPPORT BRACE AT AFT ACCESSORY COMPARTMENT LEFT SIDE AT STA 1710, X+30, Z-5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATE D AND INSTALLED NEW SUPPORT BRACE IAW DAC DWG 5755032 AND DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000890 19990430 00890 WP 1999 4 30 RRXA99469 1 19980429 A 5320 BRACKET DOUG DC8 DC873F 302199F WP BS 1700 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BOTTOM FLOOR SUPPORT BRACKET LEFT SIDE AT STA 1700, X+14, Z0. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW BRACK ET IAW DAC DWG 5755032 AND DC8 SRM 51-1-21AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000891 19990430 00891 WP 1999 4 30 RRXA99470 1 19980430 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GILLINER ATTACH ANGLE OF RIGHT SIDE OF ACCESSORY COMPARTMENT DOOR HINGE AT STA 1540, X-8 TO -17, Z-7 TO -9. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 S RM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSIO N PROGRAM). 2 L 7 4 4F RT 4A25 1999043000892 19990430 00892 WP 1999 4 30 RRXA99471 1 19980429 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BOTTOM OF FLOOR BOARD IN AFT ACCESSORY COMPARTMENT AT STA 1620 BL 21R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC8 SRM 53-0-0, 51-1-21A, AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM ). 2 L 7 4 4F RT 4A25 1999043000893 19990430 00893 WP 1999 4 30 RRXA99472 1 19980429 A 5320 46111811 FITTING DOUG DC8 DC873F 302199F WP BS 1760 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT SIDE FLOOR SUPPORT NUTPLATES AND SUPPORT AT STA 1760 BL 21L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW C OLLAR AND SUPPORT ANGLE IAW DAC DWG 5755032, DC8 SRM 51-1-24, 51-1-21, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000894 19990430 00894 WP 1999 4 30 RRXA99473 1 19980429 A 5320 CUSP DOUG DC8 DC873F 302199F WP BS 1180-1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT HAND CUSP LOWER FLANGE AT STA 1180 TO 1200 BL 21L. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLICE ANGLE AN D DOUBLER IAW DC8 SRM 53-2-5, 51-1-20D, AND 51-3-16. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000895 19990430 00895 WP 1999 4 30 RRXA99474 1 19980407 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1003 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BOTTOM OF FLOOR TRACK IN LEFT AFT PIT TUNNEL AT STA 1003, X+62, Z- 1. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NE W SEAT TRACK AND SPLICES IAW DC8 SRM 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000896 19990430 00896 WP 1999 4 30 RRXA99475 1 19980424 A 5320 FRAME DOUG DC8 DC873F 302199F WP CARGO DOORWAY CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CUSP IN RIGHT TUNNEL DOOR FRAME IN AFT PIT AT STA 1220 BL 21R. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000897 19990430 00897 WP 1999 4 30 RRXA99476 1 19980504 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1684-1690 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING ON LONGERON 24R AT STA 1684 TO 1690, X-35 TO -36, Z-11 TO -11.5 BL 24R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. DRILLED AND INST ALLED NEW END FITTING IAW DC8 SRM 51-3-2, 51-1-21, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000898 19990430 00898 WP 1999 4 30 RRXA99477 1 19980424 A 5320 4640436 FITTING DOUG DC8 DC873F 302199F WP BS 1450 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING IN AFT PIT AT STA 1450 BL 25R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. DRILLED AND INSTALLED NEW FITTING IAW DC8 SRM 51-3-2, 53- 4-1 FIG 44C, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000899 19990430 00899 WP 1999 4 30 RRXA99478 1 19980424 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 1240-1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 26R AT STA 1240 TO 1260 BL 26R. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICES IAW DC8 SRM 53- 2-2 FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000900 19990430 00900 WP 1999 4 30 RRXA99479 1 19980424 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO GILLINER ATTACH ANGLE AT STA 1220 BL 27R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACH ANGLE IAW DAC DWG 5750 725, DC8 SRM 51-1-3 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000901 19990430 00901 WP 1999 4 30 RRXA99480 1 19980424 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1100 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SEAT TRACK A RIGHT TUNNEL AT STA 1100, X+59 TO +62, Z+1.1 TO +1.3. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SPLI CE AND DOUBLER IAW DC8 SRM 53-2-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000902 19990430 00902 WP 1999 4 30 RRXA99481 1 19980426 A 5320 SUPPORT DOUG DC8 DC873F 302199F WP BS 1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO VERTICAL SUPPORT FOR GILL LINER SIDEWALL AROUND BACKSIDE OF NUT PL ATE ON LOWER END AT STA 1480 BL 26L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51 -1-8. FABRICATED AND INSTALLED SUPPORT IAW DC8 SRM 51-3-2 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PR OGRAM). 2 L 7 4 4F RT 4A25 1999043000903 19990430 00903 WP 1999 4 30 RRXA99482 1 19980429 A 5310 STRUCTURE DOUG DC8 DC873F 302199F WP BS 1220-1230 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TORQUE BOX AT STA 1220 TO 1230 BL 22L TO 23L. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRA M). 2 L 7 4 4F RT 4A25 1999043000904 19990430 00904 WP 1999 4 30 RRXA99483 1 19980407 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 1050 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT AFT PIT TUNNEL AT STA 1050, Z-1, BL 45L. DAMAGE EXCEEDED LIM ITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SEAT TRACK AND SPLICES IA W DC8 SRM 53-2-3 FIG 14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000905 19990430 00905 WP 1999 4 30 RRXA99484 1 19980421 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1445 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO T-BOX FITTING IN AFT PIT AT STA 1445 BL 30R TO 31R. DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000906 19990430 00906 WP 1999 4 30 RRXA99485 1 19980514 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 1342 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER WITH TWO SHEARED RIVETS AT STA 1342 BL 30R TO 31R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBL ERS IAW DC8 SRM 53-2-1 FIG 7 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000907 19990430 00907 WP 1999 4 30 RRXA99486 1 19980423 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO WALL ATTACH ANGLES FOR GILL LINER AT STA 980 BL 27L TO 27R. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ATTACH ANGL ES IAW DAC DWG 5704724 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000908 19990430 00908 WP 1999 4 30 RRXA99487 1 19980424 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON AT STA 460 BL 21R TO 22R. DAMAGE EXCEEDED LIMITS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME REPAIR SPLICES IAW DC8 SRM 53- 2-0 FIG 2, 51-1-8 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000909 19990430 00909 WP 1999 4 30 RRXA99488 1 19980424 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM ATTACH FITTING IN LOWER FWD CARGO PIT AT STA 460 BL 21R TO 22R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALL ED NEW FITTING IAW DAC DWG 3773479, DC8 SRM 51-3-2, AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000910 19990430 00910 WP 1999 4 30 RRXA99489 1 19980428 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 330-335 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR BOARD AT STA 330 TO 335 BL 21L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-2-0. (COR ROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000911 19990430 00911 WP 1999 4 30 RRXA99490 1 19980428 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 70-80 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR BOARD IN LEFT HAND TUNNEL AT STA 70 TO 80 BL 21L. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW D AC DWG 5892154 AND DC8 SRM 53-7-2 FIG 3B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000912 19990430 00912 WP 1999 4 30 RRXA99491 1 19980418 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 340-348 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 340 TO 348 BL 35L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW INTERCOSTAL IAW DC8 SRM 51-1-20D. (CORROSIO N DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000913 19990430 00913 WP 1999 4 30 RRXA99492 1 19980418 A 5320 WEB DOUG DC8 DC873F 302199F WP BS 302-306 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CROSS SLIDE DOOR WEB AT STA 302 TO 306 BL 33R. DAMAGE EXCEEDED LI MITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW D C8 SRM 53-2-0, 51-1-11, 51-1-21-0D, AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000914 19990430 00914 WP 1999 4 30 RRXA99493 1 19980508 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 870TV 46086 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FORWARD PIT FRAME AT STA 220 BL 34R TO 33R. DAMAGE EXCEEDED LIMIT S IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME SPLICE IAW DC8 SRM 53 -2-0 FIG 2, 51-1-20D, AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000915 19990430 00915 WP 1999 4 30 RRXA99595 1 19980905 A 5311 FRAME DOUG DC8 DC871F 302199D WP BS 1020 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1020 BETWEEN LONGERONS 35 LEFT TO 35 RIGHT, DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW TIM CO DWG DC08-0229 REV. A AND DC-8 SRM 53-2-0 FIGURE 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-4-1. (CO RROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000916 19990430 00916 WP 1999 4 30 RRXA99596 1 19980905 A 5320 SHEAR TIE DOUG DC8 DC871F 302199D WP BS 1717 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 1717 AND LONGERON 36, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC-8 SRM 51-1-4 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000917 19990430 00917 WP 1999 4 30 RRXA99597 1 19980908 A 5320 FITTING DOUG DC8 DC871F 302199D WP BS 878 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 878 AND LONGERON 24 LEFT, DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER TIE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000918 19990430 00918 WP 1999 4 30 RRXA99598 1 19980905 A 5313 LONGERON DOUG DC8 DC871F 302199D WP BS 902 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 LEFT AT STA 902, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000919 19990430 00919 WP 1999 4 30 RRXA99599 1 19980905 A 5330 SKIN DOUG DC8 DC871F 302199D WP BS 1990-1998 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN PANEL BETWEEN STA 1998 AND STA 1990 AND BETWEEN LONGERONS 35 LEFT TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED A ND INSTALLED REPAIR DOUBLER TIE IAW DC-8 SRM 53-2-0 FIGURE 1D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000920 19990430 00920 WP 1999 4 30 RRXA99601 1 19980710 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON BOTTOM AFT ACCESSORY DOOR LANDING AT STA 1540, LONG 34L TO 34R. DAMAGE E XCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8.INSTALLED REPAIR ANGLE IAW DC8 SRM 51- 1-21. INSTALLED GIL LINER ATTACH ANGLE IAW SRM DC8-51-1-21A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000921 19990430 00921 WP 1999 4 30 RRXA99602 1 19980715 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1195 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON C-3 DOOR BACKUP FITTING AT STA 1195, LONG 30R. DAMAGE EXCEEDED LIMITATIO NS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. REPLACED FITTING WITH REPAIR FITTINGS IAW DC8 SRM 53- 2-0 FIG 2D (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000922 19990430 00922 WP 1999 4 30 RRXA99603 1 19980715 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION EMITTING FROM NUT PLATES ON FRAME CAP AT STA 1540, ABOVE 33L. DAMAGE EXCEED ED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED FILLER, -15 FILLER AND -13 ANG LE. DRILLED NEW CAP IAW DC8 SRM 51-1-24. INSTALLED IAW RED-05214. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM .) 2 L 7 4 4F RT 4A25 1999043000923 19990430 00923 WP 1999 4 30 RRXA99604 1 19980904 A 5320 CHANNEL DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON RIGHT HAND FLOOR STRUT TO FLOOR BEAM CHANNEL AT STA 1220. DAMAGE EXCEEDE D LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. REMOVED AND REPLACED CHANNEL IAW DC8 SRM 5 1-1-20 AND DAC DWG 9754002. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000924 19990430 00924 WP 1999 4 30 RRXA99605 1 19980717 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 1060-1080 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON T ANGLE IN AFT PIT AT STA 1060 TO 1080, LONG 35L. DAMAGE EXCEEDED LIMITA TIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED NEW ANGLE IAW DC8 SRM 51-1-8, 51-1-22, AND DAC DWG 9758507. TO BE INSTALLED ON N/R 40776. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000925 19990430 00925 WP 1999 4 30 RRXA99606 1 19980715 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1180 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON DOOR BACKUP FITTING AT STA 1180, BL 30R DAMAGE EXCEEDED LIMITATIONS IAW D C8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. REMOVED AND REPLACED FITTINGS IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000926 19990430 00926 WP 1999 4 30 RRXA99607 1 19980715 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1170 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON C-3 DOOR BACKUP FITTING AT STA 1170, LONG 30R. DAMAGE EXCEEDED LIMITATIO NS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. LOCATED AND DRILLED NEW FITTINGS IAW DC8 SRM 53-2-0 F IG 2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000927 19990430 00927 WP 1999 4 30 RRXA99608 1 19980715 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1210 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON C-3 DOOR BACKUP FITTING AT STA 1210, LONG 30R. DAMAGE EXCEEDED LIMITATIO NS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. REMOVED AND REPLACED FITTING WITH REPAIR FITTINGS IAW DC8 SRM 53-2-0 FIG 2D (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000928 19990430 00928 WP 1999 4 30 RRXA99609 1 19980715 A 5320 FRAME DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISI, FOUND CORROSION ON BULKHEAD FRAME ABOVE AFT ACCESSORY COMPARTMENT DOOR AT STA 1540, LONG 35R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. REMOVED AND REPLACED WITH NEW SECTION OF FRAME IAW DC8 SRM 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000929 19990430 00929 WP 1999 4 30 RRXA99610 1 19980711 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1230 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON Z FITTING IN AFT PIT AT STA 1230, LONG 33R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. REMOVED AND REPLACED WITH NEW Z FITTING IAW DC8 SRM 53-2 -0 FIG 2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000930 19990430 00930 WP 1999 4 30 RRXA99611 1 19980718 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 50-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON FLOOR BOARD SPLICE AT MAIN CABIN STA 50 TO 280, LBL AFT 62. DAMAGE EXCEE DED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLICE IAW DAC DRG 5892159 AND DC8 SRM 51-3-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000931 19990430 00931 WP 1999 4 30 RRXA99612 1 19980711 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON Z FITTING IN AFT PIT AT STA 1220, LONG 33R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. REMOVED AND REPLACED WITH NEW Z FITTING IAW DC8 SRM 53 -2-0 FIG 2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000932 19990430 00932 WP 1999 4 30 RRXA99613 1 19980717 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 880-1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON TWO SPLICE CLIPS AT MAIN CABIN STA 880 TO 1000, LBL AFT 62. DAMAGE EXCEE DED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED TWO SPLICE CHANNELS IAW DAC D WG 5892159. INSTALLED GANG CHANNEL ANCHOR NUTS IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRA M.) 2 L 7 4 4F RT 4A25 1999043000933 19990430 00933 WP 1999 4 30 RRXA99614 1 19980718 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 580-880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON FLOOR PANEL G SPLICE ANGLES AT STA 580 TO 880, LBL 20. DAMAGE EXCEEDED L IMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLICES IAW DAC DWG 5892159. INSTALLED AAW DC8 SRM 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000934 19990430 00934 WP 1999 4 30 RRXA99615 1 19980716 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 1000-1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON FLOOR BOARD SPLICE AT MAIN CABIN PLANK G STA 1000 TO 1300, BL 30R. DAMAG E EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLI CE IAW DAC DWG 5892159. INSTALLED IAW DC8 SRM 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000935 19990430 00935 WP 1999 4 30 RRXA99616 1 19980810 A 5315 FLFOORBEAM DOUG DC8 DC873F 302199F WP BS 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON UPPER LEG ON FLOORBEAM FWD AT STA 1280, BL 60R. DAMAGE EXCEEDED LIMITAT IONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR TO DAMAGED FLOORBEA M IAW TIMCO DWG DC-8-53-051-509 AND DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000936 19990430 00936 WP 1999 4 30 RRXA99617 1 19980716 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ATTACH POINT ON RT FRAME ATTACH FITTING AT STA 120, BL 21R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. DRILLED NEW FITTING IAW DAC DWG 4597643 AND DC8 SRM 51-3-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000937 19990430 00937 WP 1999 4 30 RRXA99618 1 19980716 A 5320 4597643 FITTING DOUG DC8 DC873F 302199F WP BS 578-580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON FRAME TO CUSP FITTING AT MAIN CABIN STA 578 TO 580, BL 21R. DAMAGE EXCEE DED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000938 19990430 00938 WP 1999 4 30 RRXA99619 1 19980716 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 458-460 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION FRAME TO CUSP FITTING SHIM IN MAIN CABIN AT STA 458 TO 460, BL 21R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA C ORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000939 19990430 00939 WP 1999 4 30 RRXA99620 1 19980716 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 478-480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION FRAME TO CUSP FITTING SHIM IN MAIN CABIN AT STA 478 TO 480, BL 21R. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. (CORROSION DAMAGE RECORDED IN EWA C ORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000940 19990430 00940 WP 1999 4 30 RRXA99621 1 19980713 A 5314 KEEL BEAM DOUG DC8 DC873F 302199F WP BS 900 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION INSIDE KEEL BEAM (UPPER CORNER) AT STA 900, Z-36. DAMAGE EXCEEDED LIMITATIO NS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED REPAIR ANGLES FOR CRACKED ON WEB IAW DC8 S RM 51-2-0 FIG 1B. INSTALLED BRACKET, WEB, AND REPAIR ANGLES IAW DC8 SRM 51-1-8, 51-1-21, AND 51-1-20D. (CORROSION DAMA GE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000941 19990430 00941 WP 1999 4 30 RRXA99622 1 19980810 A 5320 STIFFENER DOUG DC8 DC873F 302199F WP BS 970-980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON STIFFENER AND MISSING LOWER FLANGE CORNER AT STA 970 TO 980, BL 30R. DAM AGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FR AME IAW DAC DRG 5646444 AND DC8 SRM 51-1-24 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000942 19990430 00942 WP 1999 4 30 RRXA99623 1 19980715 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 880 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON TOP OF FRAME FITTING AT STA 880, X+60, Z-10. DAMAGE EXCEEDED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 53-7-1 , 51-3-2, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000943 19990430 00943 WP 1999 4 30 RRXA99624 1 19980713 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 960-940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON KEEL BEAM, TOP AREA, AT STA 960 TO 940, X+6, Z-45. DAMAGE EXCEEDED LIMIT ATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DAC DRG 5892159 AND DC8 SRM 53-2-0, 51-1-21, AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000944 19990430 00944 WP 1999 4 30 RRXA99625 1 19980718 A 5320 SPLICE DOUG DC8 DC873F 302199F WP BS 50-250 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 603AL 46003 DURING A MAINTENANCE VISIT, FOUND CORROSION ON FLOOR BOARD SPLICE CLIP AT MAIN CABIN STA 50 TO 280, BL 55. DAMAGE EXCEE DED LIMITATIONS IAW DC8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SPLICE IAW DC8 SRM 3-53-7-3 FIG 3E AND DC8 SRM 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM.) 2 L 7 4 4F RT 4A25 1999043000945 19990430 00945 WP 1999 4 30 RRXA99627 1 19981013 A 5320 PRESSURE PANEL DOUG DC8 DC873F 302199F WP BS 950-970 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PRESSURE PANEL BETWEEN STA 950 TO STA 970 AND LONGERON 21 LEFT, D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVE TIMCO DER ENGINEERING SKETCH REO-05655 REV A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000946 19990430 00946 WP 1999 4 30 RRXA99628 1 19981205 A 5347 ANGLE DOUG DC8 DC873F 302199F WP BS 857 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE IN RIGHT MAIN LANDING GEAR TOP SECTION AT STA 857 AND BETWEEN WL-6 AND WL-8, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FAB RICATED AND INSTALLED REPAIR IAW FAA APPROVE TIMCO DER ENGINEERING SKETCH REO-05655 REV A. (CORROSION DAMAGE RECORDED I N EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000947 19990430 00947 WP 1999 4 30 RRXA99629 1 19981002 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 857-980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 RIGHT BETWEEN STA 857 TO STA 980, DAMAGE EXCEEDED LIMI TS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW LONGERON 24 RIGHT IAW TIMCO WORKCARD 90453100. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000948 19990430 00948 WP 1999 4 30 RRXA99630 1 19981006 A 5347 SEAT TRACK DOUG DC8 DC873F 302199F WP BS 180-185 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 180 TO STA 185 AND BL 65 RIGHT, DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3 -0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000949 19990430 00949 WP 1999 4 30 RRXA99631 1 19981006 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 822- CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 822 BETWEEN LONGERONS 21 RIGHT AND 22 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 5 1-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000950 19990430 00950 WP 1999 4 30 RRXA99632 1 19981006 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 440 AND LONGERON 21 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 45976 43 AND DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000951 19990430 00951 WP 1999 4 30 RRXA99633 1 19981006 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 645-669 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE BETWEEN STA 645 TO STA 669 AND LONGERON 21 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FI TTING IAW DC-8 SRM 53-4-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000952 19990430 00952 WP 1999 4 30 RRXA99634 1 19981006 A 5230 HINGE DOUG DC8 DC873F 302199F WP CARGO DOOR CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO DOOR FWD HINGE SEGMENT AT STA 130 AND LONGERON 6 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRO 8530027. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000953 19990430 00953 WP 1999 4 30 RRXA99635 1 19981008 A 5320 INTERCOSTAL DOUG DC8 DC873F 302199F WP BS 1720 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA1720 AND BL 12 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0. ( CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000954 19990430 00954 WP 1999 4 30 RRXA99636 1 19981008 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1660 BETWEEN LONGERONS 29 LEFT TO 34 LEFT, DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000955 19990430 00955 WP 1999 4 30 RRXA99637 1 19981008 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1664 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 1664 AND BL 10 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3 FIGUR E 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000956 19990430 00956 WP 1999 4 30 RRXA99638 1 19981006 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 1000 AND BL 27 RIGHT, DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-7-3. (C ORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000957 19990430 00957 WP 1999 4 30 RRXA99639 1 19981006 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1000 AND BL 23 LEFT, DAMAGE EXCEEDED LIMITS IAW D C-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0 . (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000958 19990430 00958 WP 1999 4 30 RRXA99640 1 19981006 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 1525-1530 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 1525 TO STA 1530 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000959 19990430 00959 WP 1999 4 30 RRXA99641 1 19981006 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 34 RIGHT, DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2- 0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000960 19990430 00960 WP 1999 4 30 RRXA99642 1 19981013 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 29 LEFT, DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000961 19990430 00961 WP 1999 4 30 RRXA99643 1 19981013 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 8-70 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 33 RIGHT BETWEEN STA 8 TO STA 70, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 53 -2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000962 19990430 00962 WP 1999 4 30 RRXA99644 1 19981006 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 8 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 33 RIGHT AND FITTING AT STA 8, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000963 19990430 00963 WP 1999 4 30 RRXA99645 1 19981019 A 5312 BULKHEAD WEB DOUG DC8 DC873F 302199F WP BS 12-32 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BULKHEAD WEB AND FITTING BETWEEN STA -12 TO STA -32 AND LONGERON 2 3 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLE D NEW WEB AND FITTING IAW SRO 8530026. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000964 19990430 00964 WP 1999 4 30 RRXA99646 1 19981006 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 100-110 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 100 TO STA 110 AND BETWEEN LONGERO NS 26 RIGHT TO 27 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRIC ATED AND INSTALLED NEW SKIN PANEL IAW DAC DWG 5756065. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000965 19990430 00965 WP 1999 4 30 RRXA99647 1 19981012 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO 2 EACH FITTINGS AT STA 280 AND LONGERON 33 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTINGS IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000966 19990430 00966 WP 1999 4 30 RRXA99649 1 19981006 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CROSS SLIDE CARGO DOOR, ATTACHMENT ANGLE AT STA 340 AND LONGERON 3 4 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED NEW ANGLE IAW DAC DWG 5711283. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000967 19990430 00967 WP 1999 4 30 RRXA99650 1 19981006 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 190-440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 190 TO STA 440 AND BETWEEN LONGERO NS 31 LEFT TO 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND INSTALLED NEW SKIN PANEL IAW DC-8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000968 19990430 00968 WP 1999 4 30 RRXA99651 1 19981002 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 270 BETWEEN LONGERONS 34 LEFT TO 35 LEFT, DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IA W DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000969 19990430 00969 WP 1999 4 30 RRXA99652 1 19981002 A 5320 DOUBLER DOUG DC8 DC873F 302199F WP BS 260-350 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN STA 260 TO STA 350 AND LONGERON 31 LEFT, DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FI NGER DOUBLER IAW DAC DWG 5758874. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000970 19990430 00970 WP 1999 4 30 RRXA99653 1 19981013 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 200-280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 200 TO STA 280 AND LONGERONS 28 LEFT, DAMAGE E XCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING I AW DAC DWG 3755822. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000971 19990430 00971 WP 1999 4 30 RRXA99654 1 19981006 A 5313 LONGERON DOUG DC8 DC873F 302199F WP BS 190-375 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 36 BETWEEN STA 190 TO STA 375, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED LONGERON IAW DC-8 SRM 51-3-2. (CORROSION DAMAG E RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000972 19990430 00972 WP 1999 4 30 RRXA99655 1 19981002 A 5320 3755822 FITTING DOUG DC8 DC873F 302199F WP BS 200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 200 BETWEEN LONGERONS 34 RIGHT TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000973 19990430 00973 WP 1999 4 30 RRXA99656 1 19981013 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 32 LEFT TO 35 RIGHT, DAMAGE EXCEED ED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC -8 SRM 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000974 19990430 00974 WP 1999 4 30 RRXA99657 1 19981008 A 5311 FRAME DOUG DC8 DC873F 302199F WP BS 1150-1160 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME BETWEEN STA 1150 TO STA 1160 AND BETWEEN LONGERONS 24 LEFT T O 25 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTA LLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000975 19990430 00975 WP 1999 4 30 RRXA99658 1 19981006 A 5320 FRAME DOUG DC8 DC873F 302199F WP DOOR JAMB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO DOOR JAMB FRAME WEB AT STA 238, BL 78 LEFT AND WL -3, DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME WEB IAW DAC DWG 5772786. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000976 19990430 00976 WP 1999 4 30 RRXA99659 1 19981006 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 280 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 30 LEFT, DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 375582 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000977 19990430 00977 WP 1999 4 30 RRXA99660 1 19981006 A 5320 FITTING DOUG DC8 DC873F 302199F WP BS 270 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 270 AND LONGERON 36, DAMAGE EXCEEDED LIMITS IAW DC- 8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-3-2. ( CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000978 19990430 00978 WP 1999 4 30 RRXA99701 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1220-1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1220 TO 1300 BL 16L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER IAW DC -8 SRM 53-2-3, FIG 10. INSTALLED IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000979 19990430 00979 WP 1999 4 30 RRXA99702 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1620 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR BOARD AT STA 1620 BL 16L. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000980 19990430 00980 WP 1999 4 30 RRXA99703 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1680 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR BOARD AT STA 1680 BL 16L. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000981 19990430 00981 WP 1999 4 30 RRXA99704 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR BOARD AT STA 1580 BL 20L. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000982 19990430 00982 WP 1999 4 30 RRXA99705 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1440-1460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1440 TO 1460 BL 44L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000983 19990430 00983 WP 1999 4 30 RRXA99706 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1360-1400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1360 TO 1400 BL 44L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000984 19990430 00984 WP 1999 4 30 RRXA99707 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1340-1380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1340 TO 1380 BL 50L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000985 19990430 00985 WP 1999 4 30 RRXA99708 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1220-1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 12240 TO 1300 BL 40L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000986 19990430 00986 WP 1999 4 30 RRXA99709 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1220 BL 6R. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER I AW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000987 19990430 00987 WP 1999 4 30 RRXA99710 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1220 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1220 BL 6R. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000988 19990430 00988 WP 1999 4 30 RRXA99711 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1200 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1200 BL 18R. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000989 19990430 00989 WP 1999 4 30 RRXA99712 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1220 BL 16R. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000990 19990430 00990 WP 1999 4 30 RRXA99713 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1220 BL 44R. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000991 19990430 00991 WP 1999 4 30 RRXA99714 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1540 BL 0. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IA W DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000992 19990430 00992 WP 1999 4 30 RRXA99715 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 900-960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 900 TO 960 BL 44L. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000993 19990430 00993 WP 1999 4 30 RRXA99716 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 920-940 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 920 TO 940 BL 6L. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000994 19990430 00994 WP 1999 4 30 RRXA99717 1 19981014 A 5321 DOUBLER DOUG DC8 DC873F 302199F WP BS 850-960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 850 TO 960 BL 50L. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000995 19990430 00995 WP 1999 4 30 RRXA99718 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1220 BL 16L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000996 19990430 00996 WP 1999 4 30 RRXA99719 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1220-1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1220 TO 1300 BL 6L. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000997 19990430 00997 WP 1999 4 30 RRXA99720 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1220 BL 44L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000998 19990430 00998 WP 1999 4 30 RRXA99721 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1220 BL 50L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043000999 19990430 00999 WP 1999 4 30 RRXA99722 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1060-1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1060 TO 1140 BL 16L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001000 19990430 01000 WP 1999 4 30 RRXA99723 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1060 BL 6L. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001001 19990430 01001 WP 1999 4 30 RRXA99724 1 19981014 A 5321 DOUBLER DOUG DC8 DC873F 302199F WP BS 1020-1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1020 TO 1060 BL 48L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001002 19990430 01002 WP 1999 4 30 RRXA99725 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1220-1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1220 TO 1300 BL 16R. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001003 19990430 01003 WP 1999 4 30 RRXA99726 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140-1220 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 TO 1220 BL 44L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001004 19990430 01004 WP 1999 4 30 RRXA99727 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 760 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 760 BL 6L TO 25L. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001005 19990430 01005 WP 1999 4 30 RRXA99728 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 702-685 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 702 TO 685 BL 6L TO 22L . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIR ACCOMPLISHED ON N/R 5 508. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001006 19990430 01006 WP 1999 4 30 RRXA99729 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 680-660 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 680 TO 660 BL 4L TO 34L . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR PARTS IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001007 19990430 01007 WP 1999 4 30 RRXA99730 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1060-1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1060 TO 1140 BL 6R. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001008 19990430 01008 WP 1999 4 30 RRXA99731 1 19981029 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1260E CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CABIN FLOORBEAM AT STA 1260 BL 40R. DAMAGE EXCEEDED LIMITS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE REPAIR AND FILLER IAW DC-8 SR M 53-2-0, FIG 1B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001009 19990430 01009 WP 1999 4 30 RRXA99732 1 19981028 A 5315 FLOORBEAM DOUG DC8 DC873F 302199F WP BS 1560 CORROSION A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CABIN FLOORBEAM AT STA 1560 BL 16L. DAMAGE EXCEEDED LIMITS IAW DC -8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC-8 SR M 53-2-0, FIG 1B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001010 19990430 01010 WP 1999 4 30 RRXA99733 1 19981028 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1250 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1250 BL 48R. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001011 19990430 01011 WP 1999 4 30 RRXA99734 1 19981024 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1280-1300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1280 TO 1300 BL 48R. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001012 19990430 01012 WP 1999 4 30 RRXA99735 1 19981023 A 5321 DOUBLER DOUG DC8 DC873F 302199F WP BS 1560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1568 TO 1577 BL 2L TO 6 L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RE PAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001013 19990430 01013 WP 1999 4 30 RRXA99736 1 19981016 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 300 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND BULGE IN MAIN CABIN FLOOR PANEL AT STA 300 BL 36R. DAMAGE EXCEEDED LIMITS IAW DC-8 SR M. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001014 19990430 01014 WP 1999 4 30 RRXA99737 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 900 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 900 BL 50R. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001015 19990430 01015 WP 1999 4 30 RRXA99738 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 990 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 990 BL 16L. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER I AW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001016 19990430 01016 WP 1999 4 30 RRXA99739 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 320 BL 44R TO 2R. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001017 19990430 01017 WP 1999 4 30 RRXA99740 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 310 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 310 BL 4R TO 44R. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001018 19990430 01018 WP 1999 4 30 RRXA99741 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 510 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 510 BL 2R. DAMAGE EXCE EDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 S RM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001019 19990430 01019 WP 1999 4 30 RRXA99742 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 857-781 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 857 TO 781 BL 48R. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PA RTS IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001020 19990430 01020 WP 1999 4 30 RRXA99743 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 857 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 857 BL 44R. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PARTS IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001021 19990430 01021 WP 1999 4 30 RRXA99744 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 530-540 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 530 TO 540 BL 4R. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PAR TS IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001022 19990430 01022 WP 1999 4 30 RRXA99745 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 798-820 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 798 TO 820 BL 6L. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001023 19990430 01023 WP 1999 4 30 RRXA99746 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 920-960 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 920 TO 960 BL 40L. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001024 19990430 01024 WP 1999 4 30 RRXA99747 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 550-590 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 550 TO 590 BL 2L TO 40L . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR PARTS IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001025 19990430 01025 WP 1999 4 30 RRXA99748 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 480-520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 480 TO 520 BL 2L TO 10L . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001026 19990430 01026 WP 1999 4 30 RRXA99749 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 375-400 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 375 TO 400 BL 20L TO 44 L. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RE PAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001027 19990430 01027 WP 1999 4 30 RRXA99750 1 19981015 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 410-470 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 410 TO 470 BL 40L TO 2L . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR PARTS IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001028 19990430 01028 WP 1999 4 30 RRXA99751 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 960-1000 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 960 TO 1000 BL 44L. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001029 19990430 01029 WP 1999 4 30 RRXA99752 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1560-1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1560 TO 1580 BL O TO 6R . DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR PART IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001030 19990430 01030 WP 1999 4 30 RRXA99753 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1480 BL 24R. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. BLEND OUT WITHIN LIMITS. (CORROSION DAM AGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001031 19990430 01031 WP 1999 4 30 RRXA99754 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1320-1340 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1320 TO 1340 BL 16R. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001032 19990430 01032 WP 1999 4 30 RRXA99755 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1300-1320 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1300 TO 1320 BL 6R. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001033 19990430 01033 WP 1999 4 30 RRXA99756 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1300-1380 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1300 TO 1380 BL 6L. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001034 19990430 01034 WP 1999 4 30 RRXA99757 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1400-1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1400 TO 1420 BL 6L. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER AND FILLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001035 19990430 01035 WP 1999 4 30 RRXA99758 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1400-1420 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1400 TO 1420 BL 26R. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 53-2-3, PG 41. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001036 19990430 01036 WP 1999 4 30 RRXA99759 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1140 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1140 BL 18R. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLES, DOUBLER, AND FILLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001037 19990430 01037 WP 1999 4 30 RRXA99760 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1060 BL 0R TO 6R. DAMA GE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOU BLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001038 19990430 01038 WP 1999 4 30 RRXA99761 1 19981014 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1020-1060 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1020 TO1060 BL 6R. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001039 19990430 01039 WP 1999 4 30 RRXA99762 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1500 BL 0 TO 6L. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER AND FILLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001040 19990430 01040 WP 1999 4 30 RRXA99763 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1520 BL 30R. DAMAGE EX CEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001041 19990430 01041 WP 1999 4 30 RRXA99764 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1500 BL 0 TO 6R. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUB LER AND FILLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001042 19990430 01042 WP 1999 4 30 RRXA99765 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1500-1580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1500 TO 1580 BL 0R TO 6 R. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RE PAIR DOUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001043 19990430 01043 WP 1999 4 30 RRXA99766 1 19981013 A 5321 FLOOR DOUG DC8 DC873F 302199F WP BS 1400-1440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO COMPARTMENT FLOOR PANEL AT STA 1400 TO 1440 BL 6R. DA MAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR D OUBLER IAW DC-8 SRM 53-2-3, FIG 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001044 19990430 01044 WP 1999 4 30 RRXA99767 1 19981015 A 5320 ANGLE DOUG DC8 DC873F 302199F WP BS 960-980 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 795FT 46103 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO TOP SIDE OF LONGERON 24L AT STA 960 TO 980, Z-18.560, LONG 24L. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 53-2-2, FIG 35-36. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 1999043001045 19990430 01045 WP 1999 4 30 RRXA99821 1 19980919 A 5320 ANGLE DOUG DC8 DC863 302198A WP BS 500 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, CEILING ATTACH ANGLE, AT STA=500, BETWEEN BL= -10 AND BL= +10, AT WL= -5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC8-SRM. FABRICATED NEW ATTACH ANGLE AND INSTALLED IAW FAA APPROVED DAC DWG NR 5707961. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) 2 L 7 4 4F 4A25 1999043001046 19990430 01046 WP 1999 4 30 RRXA99822 1 19980922 A 5320 ANGLE DOUG DC8 DC863 302198A WP BS 520 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION CENTER FUSELAGE, CEILING ATTACH ANGLE AND WEB UNDER ATTACH FITTING, AT STA= 520, BL=-10 RIGHT, WL= -8. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATE D REPAIR AND INSTALLED IAW FAA APPROVED DAC DWG NR 3759264. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999043001047 19990430 01047 WP 1999 4 30 RRXA99824 1 19980922 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, LONGERON WEB AT STA=560, BETWEEN LONGERON 26 RIGHT AND LON GERON 25 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATED NEW WEB A ND INSTALLED IAW FAA APPROVED DAC DWG NR 561652O. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999043001048 19990430 01048 WP 1999 4 30 RRXA99825 1 19980920 A 5320 WEB DOUG DC8 DC863 302198A WP BS 440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, UNDER NUTPLATE, AT STA= 440, BL= 40 RIGHT, WL= -1 WEB HAS CORROSION. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW FAA APPROVED DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999043001049 19990430 01049 WP 1999 4 30 RRXA99826 1 19980918 A 5311 FRAME DOUG DC8 DC863 302198A WP BS 1260 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, VERTICAL FRAME, AT STA= 1260, LONGERON 27 RIGHT. DAMAGED EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATED FILLER AND REPAIR ANGLES IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999043001050 19990430 01050 WP 1999 4 30 RRXA99827 1 19980919 A 5320 WEB DOUG DC8 DC863 302198A WP BS 540&580 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, ON WEB ABOVE C-2 DOOR, BETWEEN STA= 580 AND STA=540, AT BL = 12 RIGHT, WL= -6. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATED NEW W EB AND INSTALLED IAW FAA APPROVED DAC DWG NR 5707961. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999043001051 19990430 01051 WP 1999 4 30 RRXA99828 1 19980920 A 5320 INTERCOASTAL DOUG DC8 DC863 302198A WP BS 460 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, VERTICAL SIDEWALL INTERCOSTAL, AT STA=460, JUST ABOVE LONG ERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATED NEW INTERC OASTAL AND INSTALLED IAW FAA APPROVED DAC DWG NR 3610417. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999043001052 19990430 01052 WP 1999 4 30 RRXA99829 1 19980919 A 5320 ANGLE DOUG DC8 DC863 302198A WP BS 100-120 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, ATTACH ANGLE, BETWEEN STA= 100 AND STA-120 AT LONGERON 27 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATED ANGLE AND INSTALLE D IAW FAA APPROVED 53-11-3 FIG 4A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM) 2 L 7 4 4F 4A25 1999043001053 19990430 01053 WP 1999 4 30 RRXA99830 1 19980918 A 5320 WEB DOUG DC8 DC863 302198A WP BS 560 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, WEB TOPSIDE OF TORQUE BOX, AT STA= 560, LONGERON 25 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. FABRICATED NEW WEB AND INSTALLED IA W FAA APPROVED DAC DWG NR 5616520. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999043001054 19990430 01054 WP 1999 4 30 RXA99823 1 19980920 A 5320 ANGLE DOUG DC8 DC863 302198A WP BS 480 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, CENTER FUSELAGE, FRAME ATTACH ANGLE, STA= 480 ABOVE LONGERON 26 RIGHT. DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM. REMOVED CORROSION IAW DC-8 SRM 51-1-8 (S UPPORT ANGLE) AND DC-8 SRM 53-2-0 FIG 1-F; DAC DWG NR 3706754-502 (GUSSET). (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 1999051200001 19990512 00001 EU 1999 5 12 CA981125003 1 19980924 A 2120 AIR DISTRIBUTION BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN CONTAMINATED W O OTHER O OTHER CR CRUISE 1 CA LF05627A (CAN) DURING CRUISE, ONE FLIGHT ATTENDANT REPORTED NUMBING OF THE LOWER FACE. NO AIR QUALITY PROBLEMS NOTED. JUST PRIO R TO DESCENT, A 2ND FLIGHT ATTENDANT REPORTED AS UNWELL. TC HEALTH AND SAFETY INSPECTED AIRCRAFT AND FOUND NOTHING. 2 H 7 4 4F 4 F RT A49EU E6NE 1999051200004 19990512 00004 WP 1999 5 12 DHL9980572C 1 19981228 A 5753 ANGLE DOUG DC8 DC873F 302199F WP RIGHT TE FLAP CRACKED A DHLA K NONE O OTHER IN INSP/MAINT 1 SO 01 805DH 46125 AT C-CHECK, RT WING I/B FLAP FUS FILLET FAIRING ATTACH ANGLE CRACKED. REMOVED CRACKED ANGLE AND REMOVED FABRICATED NEW PER SRM 51-1-21, 21 X 1 X 1. N/R 413 2 L 7 4 4F RT 4A25 1999051400199 19990514 00199 GL 1999 5 14 99ZZZX1959 2 19981120 A 7261 6791715 TUBE CVAC 340 34031 2422704 WP ALLSN 501D 501D13 03004 GL NR 2 ENGINE WORN A RENA E ENGINE SHUTDOWN J WARNING INDICATION AP APPROACH 1 WP 01 73104 4 CAE501555 ON APPROACH TO JAX, NR 2 ENGINE GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. PRECAUTIONARY SHUT DOWN OF NR 2 ENG INE. AIRCRAFT LANDED AT DESTINATION AIRPORT UNEVENTFULLY. 2 L 7 2 4R 4 T 6A6 E282 1999051400475 19990514 00475 WP 1999 5 14 RRXA99970 1 19981109 A 7830 57533991 RAIL DOUG DC8 DC863 302198A WP NR 1 TR UNIT MISMANUFACTURED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND COUNTERBORES WERE MACHINED OVERSIZE, NR 1 THRUST REVERSER RAIL, UPPER TRACK, (P/N 5753 399-1). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED RAIL AND INS TALLED IAW DAC DWG NR 5753399. 2 L 7 4 4F 4A25 1999051400542 19990514 00542 NE 1999 5 14 HALA9800410 2 19981216 A 7200 ENGINE DOUG DC10 DC1010 3022110 WP GE CF6 CF66K 30020 NE NR 2 FAILED A HALA C ABORTED TAKEOFF J A WARNING INDICATION FLAME/FIRE TO TAKEOFF 1 WP 13 119AA 46519 FLT 21 - SEA - NR 2 ENGINE FAILURE ON TAKEOFF ROLL. N1 STARTED DECREASING AND EGT STARTED INCREASING IMMEDIATELY AFTER POWER SET FOR TAKEOFF. EGT INCREASED TO 925 AND ANOTHER AIRCRAFT REPORTED FLAMES EXITING TAILCONE. REPLACED NR 2 ENGIN E PER MCM DR719401. OPS AND LEAK CHECK PER MCM DR719518. (M) 2 L 7 3 4F 4 F A22WE E23EA 1999051400552 19990514 00552 GL 1999 5 14 C2XA98CL082 2 19981219 A 7532 8166071 BLEED VALVE EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LT ENGINE FAILED A C2XA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 SW 09 14940 145033 CLE - FLT 4052 - THE CREW REPORTED THAT THEY RECEIVED A LEFT BLEED LEAK WARNING AFTER TAKEOFF. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT THEN REMOVED AND REPLACED THE LEFT BLEED SHUTOF F VALVE IAW EMB-145 MM 75-31-10. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY, AIRCRAFT RELEASED FOR SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999051400554 19990514 00554 GL 1999 5 14 SIMA982472 2 19980904 A 7321 23068679 FADEC 1A EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT ENGINE FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CL CLIMB 1 SW 21 611AE BX48493 145074 ORD - FLT 4033 - THROUGH 13,000 FEET, LEFT ENGINE FLAMED OUT. TRIED TO RESTART, BUT AT LIGHT OFF, THE RAM AIR ADVISORY LIGHT CAME ON. DISCONTINUED START. REMOVED AND REPLACED FADEC 1A AND FADEC 1B. OPERATIONAL CHECKED WITH NO FURTHER DE FECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999051400555 19990514 00555 GL 1999 5 14 99ZZZM283 2 19980904 A 7321 23068679 FADEC 1B EMB 145 EMB145 SO ALLSN AE300 AE3007A GL LEFT ENGINE FAILED A SIMA E A ENGINE SHUTDOWN UNSCHED LANDING J X WARNING INDICATION ENGINE FLAMEOUT CL CLIMB 1 SW 21 611AE BX48496 145074 ORD - FLT 4033 - THROUGH 13,000 FEET, LEFT ENGINE FLAMED OUT. TRIED TO RESTART, BUT AT LIGHT OFF, THE RAM AIR ADVISORY LIGHT CAME ON. DISCONTINUED START. REMOVED AND REPLACED FADEC 1A AND FADEC 1B. OPERATIONAL CHECKED WITH NO FURTHER DE FECTS NOTED. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4F 4 F RT T00011AT TE6CH 1999051400558 19990514 00558 SO 1999 5 14 99ZZZM286 1 19980928 A 7110 LATCH EMB 110 EMB110P1 3260122 SO RT COWL WORN A BQTA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NE 05 62CZ 110388 BUFFALO-BINGHAMTON - WHILE EN ROUTE THE FLIGHT CREW DIVERTED TO ROCHESTER NY AFTER EXPERIENCING RIGHT ENGINE TORQUE FLUC TUATIONS. AFTER LANDING, THE CREW DISCOVERED THE RIGHT ENGINE TOP COWL HAD BECOME PARTIALLY UNLATCHED. THE ENGINE INLE T WAS INSPECTED AND FOUND FREE OF OBSTRUCTIONS. NO APPARENT SIGNS OF A BIRD STRIKE WERE DETECTED 4 COWL LATCH ASSEMBLIE S WERE REPLACED. THE ENGINE COWL WAS SECURED AND THE RIGHT ENGINE WAS GROUND OPERATIONALLY CHECKED, ALL INDICATIONS AND PARAMETERS WERE SATISFACTORY. THE AIRCRAFT WAS RELEASED TO SERVICE. (M) 1 L 7 2 4T A21SO 1999051400599 19990514 00599 WP 1999 5 14 AALA982232 1 19981224 A 3350 CONNECTOR DOUG DC10 DC1010 3022110 WP ROW 7 HJ LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 132AA 47827 DFW - DURING OVERNIGHT, MAINTENANCE EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 7HJ INOPERATIVE. RESEATED EMERGENCY EXIT F LOOR PATH LIGHT CONNECTOR PIN AT SEAT 7HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999051400614 19990514 00614 NM 1999 5 14 AALA982221 1 19981215 A 3350 A3060709102 LIGHT DOUG MD11 MD11 3023602 NM ROW 13G DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1766A 48597 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT ROWS 13G AND 14G INOPERATIVE. REPLACED E MERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT ROW 13G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400615 19990514 00615 NM 1999 5 14 AALA982154 1 19981210 A 3350 A3060841 LIGHT DOUG MD11 MD11 3023602 NM R2 DOOR DEFECTIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1761R 48551 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FORWARD OF R2 DOOR HAS 3 LIGHT SEGMENTS INOPERATI VE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIPS AT R2 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400616 19990514 00616 NM 1999 5 14 AALA982033 1 19981108 A 3397 WIRE DOUG MD11 MD11 3023602 NM R1 DOOR BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 1758B 48527 ORD - DURING OVERNIGHT MAINTENANCE, R1 DOOR EMERGENCY EXIT SPOT/SIGN WOULD NOT ILLUMINATE. REPAIRED BROKEN WIRE R1 DOOR EMERGENCY EXIT SPOT/SIGN LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400617 19990514 00617 NM 1999 5 14 AALA982117 1 19981117 A 3350 TERMINAL DOUG MD11 MD11 3023602 NM COCKPIT DEFECTIVE A AALA K NONE L NO TEST CR CRUISE 1 SW 07 1758B 48527 DFW - FLT 60 - EN ROUTE NRT-DFW, DURING CRUISE EMERGENCY LIGHTS E8 CIRCUIT BREAKER ON OVERHEAD PANEL POPPED. RESET OF C IRCUIT BREAKER FAILED. LANDED DFW WITHOUT INCIDENT. REPLACED 3-707 TERMINAL AND BURNDY BLOCKS 2 AND 3. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F RT A22WE 1999051400620 19990514 00620 WP 1999 5 14 AALA982036 1 19981109 A 3350 LIGHT DOUG DC10 DC1030 3023501 WP ROW 4B BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 137AA 47847 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT PASSENGER SEAT 4B INOPERATIVE. REPLACED EMERGENC Y EXIT LIGHT STRIP AT PASSENGER SEAT 4B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999051400621 19990514 00621 WP 1999 5 14 AALA981594 1 19980827 A 3350 CONNECTOR DOUG DC10 DC1030 3023501 WP L4 DOOR LOOSE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 164AA 46950 DFW - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHTS ON EACH SIDE OF L4 DOOR INOPERATIVE. SECURED CONNECTOR TO EMEG ENCY EXIT LIGHTS FOR EACH SIDE OF L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999051400622 19990514 00622 WP 1999 5 14 AALA981688 1 19980913 A 3397 WIRE DOUG DC10 DC1030 3023501 WP ROW 2H BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 143AA 46555 DEN - FLT 1322 - DURING WALK AROUND EMERGENCY EXIT ESCAPE LIGHT AT SEAT 2H INOPERATIVE. PLACARDED PER MEL AND ENTERED O N MIC SHEET. DFW REPAIRED WIRES ON EMERGENCY EXIT ESCAPE LIGHT AT SEAT 2H. SYTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A22WE 1999051400631 19990514 00631 EU 1999 5 14 AALA981922 1 19981020 A 3350 BATTERY AIRBUS 300 A300B4605R 3930308 EU L2/R2 DOOR DISCHARGED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7083A 645 TUL - BATTER UNIT 29WL4 FAILED OPERATIONAL TEST OF EMERGENCY LIGHTING BY EMERGENCY TEST PUSH BUTTON. INSTALLED A NEW BA TTERY UNIT AT 29WL4 BY L2 AND R2 DOORS. OPS TESTED GOOD. (M) 2 L 7 2 4F RT A35EU 1999051400632 19990514 00632 EU 1999 5 14 AALA981923 1 19981020 A 3350 CONNECTOR AIRBUS 300 A300B4605R 3930308 EU R3/R4 DOOR FAILED A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 7083A 645 TUL - FOUND CROSS AISLE LIGHTING WILL NOT ILLUMINATED AT R3 AND L3 DOOR. REPLACED FLAT CONDUCTOR TO LIGHTING STRIPS. ( M) 2 L 7 2 4F RT A35EU 1999051900002 19990519 00002 WP 1999 5 19 RRXA99281 1 19980905 A 5320 ANGLE DOUG DC8 DC871F 302199D WP BS 1750 - 1790 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE BETWEEN STA 1750 TO 1790 AND LONGERON 2 LEFT, DAM AGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DO UBLER TIE IAW DC-8 SRM 53-2-5 FIG 16A. 2 L 7 4 4F RT 4A25 1999052100356 19990521 00356 NE 1999 5 21 AMWA001558 2 19981203 A 7320 3033260 P-3 LINE BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE RT ENGINE BROKEN A AMWA A E UNSCHED LANDING ENGINE SHUTDOWN J WARNING INDICATION CR CRUISE 1 CE 07 59YV 13648 UE59 114073 FLT 5648 - DIVERTED TO ICT EN ROUTE TO MCI FROM DDC WHEN THE RIGHT ENGINE N1 WENT TO 55 PERCENT. THE CREW SHUT DOWN THE ENGINE AND DECLARED EMERGENCY. AIRCRAFT LANDED IN ICT WITHOUT INCIDENT. ICT MAINTENANCE REPLACED THE RIGHT ENGINE P-3 LINE FROM TEH FCU TO THE P-3 FILTER. AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER INCIDENT. (M) 2 L 7 2 4T 4 T RT A24CE E26NE 1999052100357 19990521 00357 CE 1999 5 21 99ZZZM294 1 19981217 A 3234 1013841377 SELECTOR EATON BEECH 1900 1900D 1154162 CE LANDING GEAR FAILED A AMWA O OTHER P NO WARNING INDICATION AP APPROACH 1 CE 07 99YV 12557 1102 UE99 FLT 5617 - ON APPROACH TO JAN, LANDING GEAR FAILED TO EXTEND WHEN SELECTED DOWN, MANUAL EXTENSION COMPLETED. LANDED W/O INCIDENT. JAN MAINTENANCE REPLACED GEAR SELECT HANDLE. OPS CHECK NORMAL. (M) 2 L 7 2 4T RT A24CE 1999052100472 19990521 00472 WP 1999 5 21 EIA990017 1 19980219 A 5321 FLOOR DOUG DC9 DC915F 3022037 WP CABIN CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 53796 47061 DURING C-CHECK, MAIN CABIN THIRD FLOORBOARD FROM L1 DOOR HAS CRACKS AROUND CARGO NET FITTING, NRC NR 0574. REPAIRED IAW SRM 53-05 FIG 1. (M) 2 L 7 2 4F A6WE 1999052100473 19990521 00473 WP 1999 5 21 EIA990016 1 19980219 A 5321 FLOOR DOUG DC9 DC915F 3022037 WP BS 120-160 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 53796 47061 DURING C-CHECK, MAIN CABIN BS 120-160 FLOOR PAN FROM BL 0 - LBL 60 HAS CORROSION AND CHAFING, NRC NR 0400. REPAIRED IAW SRM 53-10-01. (M) 2 L 7 2 4F A6WE 1999052100474 19990521 00474 WP 1999 5 21 EIA990015 1 19980219 A 5312 39253891 BULKHEAD GUSSETT DOUG DC9 DC915F 3022037 WP BS 840 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 53796 47061 DURING C-CHECK, MAIN CABIN AFT PRESSURE BULKHEAD, BS 840 LEFT SIDE OF DOOR JAMB LOWER PLATE HAS HEAVY CORROSION, NRC 058 9. REPLACED GUSSET IAW SRM 51-30-05. (M) 2 L 7 2 4F A6WE 1999052100475 19990521 00475 WP 1999 5 21 EIA990014 1 19980219 A 5330 SKIN DOUG DC9 DC915F 3022037 WP BS 360 DAMAGED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 53796 47061 DURING C-CHECK, A CLASS III REPAIR OF FUSELAGE SKIN AT BS 360 BETWEEN STRINGER 23L AND 24L, TRACKED BY COI NR 001, NRC N R 0001. ACCOMPLISHED PERMENANT REPAIR PER ECRA 915-53-034-2 REV A AND SRM 53-04 FIG 12B. (M) 2 L 7 2 4F A6WE 1999052100482 19990521 00482 WP 1999 5 21 EIA980265 1 19980922 A 2822 6550934 BOOST PUMP DOUG DC9 DC933F 302207A WP CENTER FUEL TANK FAILED A EIAA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 09 944F 47194 SEA - AIR TURNBACK FROM SEA DUE TO CENTER TANK BOOST PUMP CB AFT CENTER BOOST PUMP, CB POPPED AFTER TAKEOFF, RESET AND C B POPPED WITHIN 2 MINUTES. REMOVED AND REPLACED AFT CENTER BOOST PUMP. OPS AND LEAK CHECK GOOD PER MM 28-20-7. ALSO, CHECKED WIRING HARNESS FOR DEFECTS, NONE NOTED. (M) 2 L 7 2 4F A6WE 1999052100483 19990521 00483 WP 1999 5 21 EIAA980316 1 19981008 A 3230 RETRACT MECH DOUG DC9 DC933F 302207A WP LANDING GEAR MALFUNCTIONED A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 944F 47194 SEA - NO GROUND SHIFT ON TAKEOFF. (M) 2 L 7 2 4F A6WE 1999052100484 19990521 00484 WP 1999 5 21 EIAA980317 1 19981008 A 3230 RETRACT MECH DOUG DC9 DC933F 302207A WP LANDING GEAR MALFUNCTIONED A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 944F 47194 SEA - NO GROUND SHIFT ON TAKEOFF. (M) 2 L 7 2 4F A6WE 1999052100485 19990521 00485 NM 1999 5 21 EIAA980318 1 19980204 A 5711 WEB BOEING 747 747273C 1384896 NM WS 998 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING C5/D CHECK INSPECTION, FOUND CORROSION AT LEFT WING FRONT SPAR WEB AT FSS 998.3. TRIMMED CORROSION FROM WE B, INSTALLED DOUBLER, ANGLE AND FILLER PER HAECO R57-21-33650 AND ECRA 471-99-176-1. (M) 2 L 7 4 4F A20WE 1999052100486 19990521 00486 NM 1999 5 21 EIAA980319 1 19980205 A 5330 SKIN BOEING 747 747273C 1384896 NM BS 560 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING C5/D CHECK INSPECTION, CORROSION ON FUSELAGE SKIN AND TEAR STRAP AT BS 560 STRINGER 46R. CORRODED AREA TRI MMED AWAY FROM SKIN AND TEAR STRAP, REPAIRED BY INSTALLING TWO INTERNAL STRAPS AND THREE EXTERNAL REPAIR DOUBLERS, PER H AECO RS R53-21-33659 AND ECRA 471-99-176-1. (M) 2 L 7 4 4F A20WE 1999052100487 19990521 00487 WP 1999 5 21 EIA980349 1 19981119 A 2750 VALVE DOUG DC9 DC933F 302207A WP TE FLAPS FAILED A EIAA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 945F 47496 47279 SEA - DURING APPROACH SET FLAPS TO 15 DEGREES (L FLAP 20R, R FLAP 15) FLAPS THEN BLEW BACK TO 10 DEGREE WHILE 15 SELECTE D, SELECTED 25 GOT 30, SELECTED 40 GOT 45 INITIAL LANDED WITH 38 DEGREES. REPLACED FLAP CONTROL VALVE PER MM 27-51-1 SY STEM CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1999052100488 19990521 00488 WP 1999 5 21 EIA980350 1 19981120 A 2750 RETRACT MECH DOUG DC9 DC933F 302207A WP TE FLAPS DIRTY A EIAA O OTHER J WARNING INDICATION AP APPROACH 1 NM 09 945F 47507 47279 SEA - DURING APPROACH SET FLAPS INDICATED AS FOLLOWS 5 DEGREES, 9 DEGREES, 15, L 18 - R 16) 25 = 27.5, 40-45. CHECKED A DJUSTMENT OF CONTROL VALVE PUSHROD ARM PER MM 27-52-1, INSPECTED AND CLEANED DEBRIS (EXCESSIVE AND DIRTY LUBE) FROM FOLL OW-UP CABLES. (M) 2 L 7 2 4F A6WE 1999052100489 19990521 00489 NM 1999 5 21 EIA980328 1 19981030 A 2120 AIR DIST BOEING 747 747SR46 NM COCKPIT ODOR A EIAA O OTHER B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 NM 09 478EV 21033 DURING FLIGHT CREW NOTED SMOKE IN THE COCKPIT AND A STRONG BURNING PLASTIC SMELL. THE UPPER DECK HEATERS WERE SHUT DOWN AND THE SMOKE AND ODOR DISIPATED. (M) 2 L 7 4 4F A20WE 1999052100490 19990521 00490 NM 1999 5 21 EIAA980320 1 19981011 A 8012 215N4149 SWITCH BOEING 747 747273C 1384896 NM PWA JT9 JT9D7F 52054 NE NR 4 ENGINE FAILED A EIAA E ENGINE SHUTDOWN J WARNING INDICATION NR NOT REPORTED 1 NM 09 470EV 20653 662220 JFK - IN CRUISE, NR 4 ENGINE START VALVE OPEN LIGHT CAME ON. SHUTDOWN ENGINE. N1 32 PERCENT, N2 24 PERCENT, OIL PRESSU RE 20 PSI. REPLACED START VALVE SWITCH PER MM 80-11-05. OPS CHECK GOOD. INSPECTED ENGINE PER MM 72-00. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999052800003 19990528 00003 NM 1999 5 28 CA990111030 1 19981213 A 2897 82445025001 WIRE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE FUEL QTY CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 123152 (CAN) DUE TO REPEAT/INTERMITTENT RIGHT FUEL INDICATION FLUCTUATION SNAG. INVESTIGATION FOUND FUEL QUANTITY SYSTEM WIRI NG IN RIGHT HAND FUEL TANK AREA CHAFING AGAINST A FUEL PROBE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999052800004 19990528 00004 NM 1999 5 28 CA990111031 1 19981219 A 5230 85230539103 HANDLE 85230204015 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CARGO DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 20141 120249 (CAN) FOUND CARGO DOOR HANDLE 'OPEN' STOP SHEARED IN HALF AT INNER MOUNT HOLE. STOP REPLACED AND ADJUSTED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999052800006 19990528 00006 NM 1999 5 28 CA990111033 1 19981223 A 5230 85230212003 STRUT 85230310001 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE CARGO DOOR GOUGED W K NONE O OTHER IN INSP/MAINT 1 CA 22966 120273 (CAN) THE CARGO DOOR UPPER AFT STRUT FOUND GOUGED BELOW THE ADJUSTABLE ROD END. SUSPECT INCORRECT BOLT INSTALLATION CA USING NUT SIDE OF BOLT TO GOUGE INTO THE STRUT ASSY. CLEARANCE ACHIEVED BY REVERSING THE INSTALLATION OF INBOARD BOLT WHEN CARGO DOOR IS CLOSED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999052800011 19990528 00011 EU 1999 5 28 CA990111061 1 19981223 A 3244 30X1322PR TIRE DUNLOP BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 231 96190076 LF05740A (CAN) CENTER SECTION OF RECAP SEPARATED FROM TIRE. 2 H 7 4 4F 4 F RT A49EU E6NE 1999052800026 19990528 00026 EU 1999 5 28 CA990125015 1 19981225 A 2434 687 WIRE AUXILEC 8260121 AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE NR 1 GENERATOR BROKEN W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 CA 687 120788 890218 (CAN) DURING CLIMB, THE NR 1 DC GENERATOR WAS LOST. AIRCRAFT RETURNED. INVESTIGATION FOUND ONE WIRE BROKEN AT THE GEN ERATOR TERMINAL BLOCK. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999052800027 19990528 00027 EU 1999 5 28 CA990125016 1 19981231 A 2450 1050032 BPCU AEROSP ATR42 ATR42300 8680920 EU PWA 120 PW120 NE HAMSTD 14SF 14SF5 NE NR 2 FAILED W A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CR CRUISE 1 CA 13957 8023303 120941 900215 (CAN) DURING CRUISE, THE NR 2 DC BUS WAS LOST. BPCU REPLACED. THE POWER SUPPLY P/N Z100PCA WAS FOUND DEFECTIVE IN THE BPCU. 2 H 7 2 4T 4 T RT A53EU E20NE 6 C P7NE 1999052800083 19990528 00083 EA 1999 5 28 CA990219017 1 19981229 A 3520 11508202 SOLENOID CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE ROW 13 FAILED W G O2 MASK DEPLOYED N FALSE WARNING CR CRUISE 1 CA 7812 807281 (CAN) DURING DOOR WARNING PROBLEM WITH AIRCRAFT ON DESCENT, THE OXYGEN MASKS WERE DEPLOYED. MASKS, ROWS 5 TO 13, FAILED TO DEPLOY. CIRCUIT BREAKER HAD TRIPPED ON THE LEFT SIDE CONTROL WHEN MASKS DID NOT DEPLOY . INVESTIGATION SHOWED THAT ROW 13AB SOLENOID LATCH MECHANISM WAS SHORTED CAUSING CIRCUIT BREAKER TO TRIP. THIS ALSO HAPPENED TO ANOTHER AIRCRAFT. THERE IS A MANUAL DEPLOY CHECK CALLED UP EVERY 24 MONTHS. THESE 2 AIRCRAFT HAD BEEN DONE WITHIN THE TIME FRAME. FURT HER CHECKS REQUESTED. 2 L 7 2 4F 4 F RT A21EA E15NE 1999052800084 19990528 00084 EA 1999 5 28 CA990219018 1 19981220 A 3520 11820102 LATCH CNDAIR CL600 CL6002B19 EA SEAT 13 FAILED W O OTHER O OTHER NR NOT REPORTED 1 CA (CAN) PASSENGER OXYGEN UNIT AT SEAT 13AB TRIPPING CIRCUIT BREAKERS P1 AND P12. LATCH ASSY REPLACED. 2 L 7 2 4F RT A21EA 1999052800183 19990528 00183 EU 1999 5 28 MALA976450 1 19981015 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 418XJ 418 DURING E CHECK, LOCATED DENTS ON RIGHT FUSELAGE SKIN AFT OF ICE SHIELD FROM FS 339.0 TO 363.0, BETWEEN SL 1615 AND SL 16 17. FFV MAINTENANCE REPAIRED WITH DOUBLER, SRM 51-10-10 AND 53-70-10. 2 L 7 2 4T RT A52EU 1999052800184 19990528 00184 EU 1999 5 28 MALA976451 1 19980827 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294.5-339.25 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 413XJ 413 DURING C CHECK, FOUND CORROSION ON LEFT CENTER AISLE SEAT TRACK BETWEEN STATION 294.5 AND 339.25. MAINTENANCE REPAIR 72 5DS1122. 2 L 7 2 4T RT A52EU 1999052800185 19990528 00185 EU 1999 5 28 MALA976452 1 19980722 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 300-316 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING C CHECK, SEAT TRACK SIDE FLANGE CORRODED CENTER AISLE AT STATION 300.0 TO STATION 316. MAINTENANCE REPAIRED IAW 725DS1085. 2 L 7 2 4T RT A52EU 1999052800186 19990528 00186 EU 1999 5 28 MALA976453 1 19980720 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 339-347 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 407XJ 340B407 DURING C CHECK, FOUND SEVERAL DENTS RIGHT FUSELAGE FS 339-347.0 SKIN AFT OF ICE SHIELD AND BELOW WINDOW. MAINTENANCE RE PAIRED WITH REINFORCEMENT DOUBLER IAW SAAB SRM. 2 L 7 2 4T RT A52EU 1999052800187 19990528 00187 EU 1999 5 28 MALA976454 1 19980720 A 5320 DOUBLER SAAB SF340 340B 7860101 EU BS 718-753 DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 406 DURING C CHECK, FIVE EACH EXTERNAL REPAIR DOUBLERS ON LEFT AFT FUSELAGE BETWEEN STATION 718.0 AND 753.0. MAINTENANCE RE PAIR WITH IAW 725DS0652. 2 L 7 2 4T RT A52EU 1999052800188 19990528 00188 EU 1999 5 28 MALA976455 1 19980719 A 5310 STRUCTURE SAAB SF340 340B 7860101 EU TAIL DAMAGED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 406 DURING MAINTENANCE, TAIL STAND SLID OUT FROM UNDERNEATH AIRCRAFT DURING BAGGAGE LOADING, CAUSING AIRCRAFT TO REST ON TAI L. MAINTENANCE REPAIRED TAIL STAND ATTACH POINT AND CREASE IN SKIN IAW 72SDS1078. 2 L 7 2 4T RT A52EU 1999052800189 19990528 00189 EU 1999 5 28 MALA976456 1 19980630 A 5320 ICE SHIELD SAAB SF340 340B 7860101 EU BS 352-367 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING C CHECK, DENT UNDER ICE SHIELD FOUND TO BE OUT OF SRM LIMITS, LEFT SIDE AND ICE GUARD FROM FS 352 TO 367 BETWEEN SL1515 AND SL1517. MAINTENANCE REPAIRED WITH DOUBLER, IAW 72SDS1062. 2 L 7 2 4T RT A52EU 1999052800190 19990528 00190 EU 1999 5 28 MALA976457 1 19980630 A 5320 ICE SHIELD SAAB SF340 340B 7860101 EU BS 342-348 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING C CHECK, RIGHT FUSELAGE HAS SEVERAL DENTS IN ICE SHIELD GUARD AND SURROUNDING AREA, FROM FS 342 TO 348 BETWEEN SL 1616 AND SL1622. MAINTENANCE REPAIRED IAW 72SDS1062. 2 L 7 2 4T RT A52EU 1999052800191 19990528 00191 EU 1999 5 28 MALA976458 1 19980430 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 294-339 CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 402XJ 340B402 DURING C CHECK, FOUND CORROSION AT BOTH CENTER AISLE SEAT TRACK FLANGES BL.O AND BL 18.5 FROM STATION 294 AND STATION 33 9. MAINTENANCE REPAIRED BY REINFORCING REPAIR ANGLE IAW 72SDS1048. 2 L 7 2 4T RT A52EU 1999052800192 19990528 00192 EU 1999 5 28 MALA976459 1 19980624 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU CABIN CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 408 DURING C CHECK, THE FORWARD CENTED AISLE SEAT TRACK INBOARD FLANGE CORRODED. MAINTENANCE REPAIRED WITH FABRICATED REPAI R ANGLE IAW 72SDS10481. 2 L 7 2 4T RT A52EU 1999052800193 19990528 00193 EU 1999 5 28 MALA976460 1 19980515 A 5751 SKIN SAAB SF340 340B 7860101 EU RT AILERON PUNCTURED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 404XJ 340B404 DURING REPAIRS IN FFV, RIGHT AILERON HAS PUNCTURE DAMAGE TO UPPER SURFACE COMPOSITE SKIN. MAINTENANCE REPAIRED WITH IAW SRM PRACTICES. 2 L 7 2 4T RT A52EU 1999052800194 19990528 00194 EU 1999 5 28 MALA976461 1 19980624 A 5330 SKIN SAAB SF340 340B 7860101 EU BS 338.5-350.75 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 408XJ 408 DURING C CHECK, DENTS IN RIGHT FUSELAGE SKIN AFT OF ICE SHIELD FROM FRAME STATION 338.5 TO STATION 350.75 BETWEEN STRING ER SL1615 AND SL1617. MAINTENANCE REPAIRED PER SRM. 2 L 7 2 4T RT A52EU 1999052800195 19990528 00195 EU 1999 5 28 MALA976462 1 19980515 A 5320 SKIN SAAB SF340 340B 7860101 EU BS 339-363 DENTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 406XJ 406 DURING C CHECK INSPECTION, FOUND DENT RIGHT FUSELAGE SKIN AFT OF ICE SHIELD BETWEEN FRAME STATION 339.0 AND STATION 363. 0 BELOW STRINGER SL1617. MAINTENANCE REPAIRED IAW SRM 53-70-10. 2 L 7 2 4T RT A52EU 1999052800196 19990528 00196 EU 1999 5 28 MALA976463 1 19980601 A 5311 FRAME SAAB SF340 SF340A 7850100 EU BS 294 DISTORTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 89XJ 089 DURING C CHECK, FUSELAGE FRAME AT STATION 294 STRINGER SL1526 DISTORTED. MAINTENANCE REPAIRED PER SRM 53-70-30. 2 L 7 2 4T RT A52EU 1999052800197 19990528 00197 EU 1999 5 28 MALA976464 1 19980531 A 5321 FLOOR SAAB SF340 SF340A 7850100 EU COCKPIT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 89XJ 089 DURING C CHECK, CO-PILOT'S FLOOR AREA HAS SURFACE CORROSION. MAINTENANCE REPAIRED BY INSTALLING DOUBLER PER SRM 51-20-4 2 AND 51-20-43. 2 L 7 2 4T RT A52EU 1999052800198 19990528 00198 EU 1999 5 28 MALA976465 1 19980531 A 5321 FLOOR SAAB SF340 SF340A 7850100 EU LT COCKPIT CORRODED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 89XJ 089 DURING C CHECK, CAPTAIN'S FLOOR AREA AROUND RUDDER PEDAL AND AFT OF SEAT AREA HAS SURFACE CORROSION. MAINTENANCE CUT OU T DAMAGE AND INSTALLED DOUBLER PER SRM 53-60-50. 2 L 7 2 4T RT A52EU 1999052800199 19990528 00199 EU 1999 5 28 MALA976466 1 19980601 A 5311 FRAME SAAB SF340 SF340A 7850100 EU BS 319 DISTORTED A MALA K NONE O OTHER IN INSP/MAINT 1 GL 15 89XJ 089 DURING C CHECK, FUSELAGE FRAME AT STATION 319 BETWEEN STRINGER SL1526 AND SL1525 DISTORTED. MAINTENANCE REPAIRED BY INS TALLING DOUBLER PER SRM 53-70-30. 2 L 7 2 4T RT A52EU 1999052800463 19990528 00463 NM 1999 5 28 EIA980362 1 19981204 A 8012 START VLV LIGHT BOEING 747 747273C 1384896 NM NR 4 ENGINE ILLUMINATED A EIAA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 470EV 20653 CTS - DURING CRUISE, NR 4 ENGINE START VALVE OPEN LIGHT ILLUMINATED, ALL OTHER ENGINE PERIMETERS WERE NORMAL. ENGINE WI NDMILLED FOR 1.6 HOURS AT 25 PSI OIL PRESSURE. (M) 2 L 7 4 4F A20WE 1999052800464 19990528 00464 NM 1999 5 28 EIA980374 1 19981211 A 5270 TARGET BOEING 747 747212B 1384886 NM CARGO DOOR OUT OF ADJUST A EIAA O OTHER N FALSE WARNING CR CRUISE 1 NM 09 482EV 78029 20713 PPG - DURING CRUISE, THE FORWARD CARGO DOOR LIGHT CAME ON. ADJUSTED TARGET ON DOOR CLOSE SWITCH AND OPERATIONALLY CHECK ED NORMAL PER MM 52-32-00. (M) 2 L 7 4 4F A20WE 1999052800465 19990528 00465 NM 1999 5 28 EIA980351 1 19981120 A 3246 WHEEL BOEING 747 747128 1384894 NM LT MLG DEPARTED A EIAA O OTHER D INFLIGHT SEPARATION LD LANDING 1 NM 09 3203Y 19751 DURING LANDING ROLL-OUT, LEFT BODY GEAR ANTI-SKID LIGHT CAME ON, AFTER FURTHER INVESTIGATION THE NR 5 TIRE ASSEMBLY WAS FOUND MISSING, AND THOUGHT TO HAVE DEPARTED AIRCRAFT UPON LANDING. (M) 2 L 7 4 4F A20WE 1999052800466 19990528 00466 WP 1999 5 28 EIA980377 1 19981222 A 3230 RETRACT MECH DOUG DC9 DC915F 3022037 WP NLG ICED UP A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 915F 53623 47061 BIS - ON DEPARTURE FROM BISMARK, UNABLE TO RAISE LANDING GEAR HANDLE, AIRCRAFT REMAINED IN GROUND MODE. FOUND ICE AT NL G GROUND SHIFT CABLE QUADRANT. REMOVED ICE, CLEANED AND LUBED SYSTEM OPS, CHECKED GOOD. (M) 2 L 7 2 4F A6WE 1999052800467 19990528 00467 WP 1999 5 28 EIA980378 1 19981228 A 3230 CONNECTOR DOUG DC9 DC915F 3022037 WP LANDING GEAR DIRTY A EIAA L ABORTED APPROACH P NO WARNING INDICATION AP APPROACH 1 NM 09 916F 52203 47044 ABQ - ON APPROACH TO KDEN, NO SAFE GEAR DOWN INDICATION, LOW APPROACH FLOWN AND TOWER REPORTED GEAR HANGING. RETURNED T O ABQ, EMERGENCY GEAR EXTENSION CHECKLIST RUN, ACCOMPLISHED LOW APPROACH AT ABQ, AND LANDED WITH 6000 LBS FUEL. CLEANE D AND RESEATED DIMMER BOTTOM CANNON PLUG PER MM 32-61-00 AND OPS CHECKED NORMAL. (M) 2 L 7 2 4F A6WE 1999052800468 19990528 00468 WP 1999 5 28 99ZZZM315 1 19981221 A 5330 SKIN DOUG DC9 DC915F 3022037 WP FUSELAGE TORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 915F 47061 BIS - ONE INCH TEAR ON AIRCRAFT SKIN BELOW CARGO DOOR, DISCOVERED WHEN CHECK CARGO DOOR CLOSURE. PERFORMED CLASS III RE PAIR PER DC-9 SRM 53-04 FIG 12B. RII ACCOMPLISHED. (M) 2 L 7 2 4F A6WE 1999052800469 19990528 00469 WP 1999 5 28 EIA990112 1 19981226 A 5230 RIB DOUG DC9 DC933F 302207A WP CARGO DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 DURING C-CHECK, FORWARD CARGO DOOR INTERNAL RIBS CRACKED AT BS 370 AND 389, NRC NR F116. REPLACED FRAMES IAW SRM 51-30- 02. (M) 2 L 7 2 4F A6WE 1999052800470 19990528 00470 WP 1999 5 28 EIA990111 1 19981226 A 5320 FITTING DOUG DC9 DC933F 302207A WP CARGO COMPT CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, AFT CARGO LEFT SUPPORT FITTINGS ARE CRACKED AT THE FOLLOWING STATIONS, 813, 832, 895 AND 945. REPLACED SUPPORT FITTINGS IAW SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1999052800471 19990528 00471 WP 1999 5 28 EIA990110 1 19981226 A 5320 SILL DOUG DC9 DC933F 302207A WP CARGO DOORWAY CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 DURING C-CHECK, AFT CARGO DOOR LOWER SILL HAS EXFOLIATION CORROSION, NRC K126. REPAIRED IAW SRM 53-05. (M) 2 L 7 2 4F A6WE 1999052800472 19990528 00472 WP 1999 5 28 EIA990109 1 19981226 A 5320 SILL DOUG DC9 DC933F 302207A WP CARGO DOORWAY CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, AFT CARGO DOOR LOWER SILL HAS EXFOLIATION CORROSION, NRC NR K126. REPAIRED IAW SRM 53-05. (M) 2 L 7 2 4F A6WE 1999052800473 19990528 00473 WP 1999 5 28 EIA990108 1 19981226 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 484 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE SKIN DENTED AT BS 484 RIGHT SIDE BETWEEN STRINGER 27R AND 28R, NRC F143. REPAIRED IAW SRM 53-0 4 FIG 12B. (M) 2 L 7 2 4F A6WE 1999052800474 19990528 00474 WP 1999 5 28 EIA990107 1 19981226 A 5311 FRAME DOUG DC9 DC933F 302207A WP BS 389 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE FRAME DENTED AT BS 389 RIGHT SIDE, NRC W180. REPAIRED IAW SRM 53-03 FIG 4. (M) 2 L 7 2 4F A6WE 1999052800475 19990528 00475 WP 1999 5 28 EIA990106 1 19981226 A 5313 STRINGER DOUG DC9 DC933F 302207A WP BS 160 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE STRINGER NR 4L CRACKED AT BS 160, NRC W160. REPAIRED IAW SRM 53-02. (M) 2 L 7 2 4F A6WE 1999052800476 19990528 00476 WP 1999 5 28 EIA990105 1 19981226 A 5320 STANSION DOUG DC9 DC933F 302207A WP CARGO COMPT CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FORWARD CARGO COMPARTMENT, RIGHT SIDE WALL VERTICAL STANSION SUPPORTS FOUND CRACKED AT BS 275, 294, 332 AND 351, NRC H063. REPLACED VERTICAL STANSIONS IAW SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1999052800477 19990528 00477 WP 1999 5 28 EIA990104 1 19981226 A 5414 SKIN DOUG DC9 DC933F 302207A WP LT PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, LEFT PYLON SKIN AND STIFFENER WAS FOUND CRACKED AT STATION 965 ABOVE PANEL NR 8101A, NRC NR P062. REPAI RED IAW SRM 54-04 FIG 17A AND EO 9AV 981123) AND ECRA. (M) 2 L 7 2 4F A6WE 1999052800478 19990528 00478 WP 1999 5 28 EIA990103 1 19981226 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 330-365/446 DENTED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 DURING C-CHECK, FUSELAGE SKIN DENTED AT BS 330-365 AND 446, NRC NR F139. REPAIRED IAW SRM 53-04 FIG 12 AVTEL ENGINEERIN G DRAWING 98-12-01-024, 98-12-02-002 AND ECRA. (M) 2 L 7 2 4F A6WE 1999052800479 19990528 00479 WP 1999 5 28 EIA990102 1 19981226 A 5313 STRINGER DOUG DC9 DC933F 302207A WP BS 160-229 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE STRINGER 23L FROM BS 160-229 HAS CORROSION, NRC G041. REPLACED STRINGER AT THE ABOVE STATIONS IAW SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999052800480 19990528 00480 WP 1999 5 28 EIA990101 1 19981226 A 5313 STRINGER DOUG DC9 DC933F 302207A WP BS 160-229 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE STRINGER 24L FROM BS 160-229 HAS CORROSION NRC NR G041. REPLACED STRINGER AT THE ABOVE STATION S IAW SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999052800481 19990528 00481 WP 1999 5 28 EIA990100 1 19981226 A 5313 STRINGER DOUG DC9 DC933F 302207A WP BS 140-229 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE STRINGER 25L FROM BS 140-229 HAS CORROSION, NRC NR GO41. REPLACED STRINGER AT THE ABOVE STATIO NS IAW SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999052800482 19990528 00482 WP 1999 5 28 EIA990099 1 19981226 A 5320 FITTING DOUG DC9 DC933F 302207A WP BS 229 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE STRINGER SPLICE FITTINGS CORRODED AT BS 229 AT THE FOLLOWING STRINGERS 19L, 20L, 21L, 22L, 23L, 24L AND 25L, NRC NR H053. REPLACED STRINGER SPLICE FITTINGS AT THE ABOVE NOTED STRINGERS IAW SRM 51-30-02. (M) 2 L 7 2 4F A6WE 1999052800483 19990528 00483 WP 1999 5 28 EIA990098 1 19981226 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 1089 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE SKIN AT BS 1089 HAS AN ELONGATED FASTENER HOLE FORWARD OF THE VERTICAL STAB ATTACH FITTINGS, NR C NR073. REPAIRED PER SRM 53-31-0 FIG 19 AND ECRA. (M) 2 L 7 2 4F A6WE 1999052800484 19990528 00484 WP 1999 5 28 EIA990096 1 19981226 A 5320 FRAME DOUG DC9 DC933F 302207A WP CARGO DOORWAY CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, AFT CARGO COMPARTMENT DOOR AFT TORQUE FRAME HAS CORROSION AND A CRACK, NRC NR R089. REPAIRED IAW SRM 53 -01 FIG 2. (M) 2 L 7 2 4F A6WE 1999052800485 19990528 00485 WP 1999 5 28 EIA990097 1 19981226 A 2710 S491380ZCS2223 CONTROL CABLE DOUG DC9 DC933F 302207A WP LT AILERON FRAYED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, LEFT AILERON CONTROL CABLE FOUND FRAYED AND ROUTED INCORRECTLY, NRC A-55. REPLACED CABLE AND RIGGED IAW MM 27-10-03. (M) 2 L 7 2 4F A6WE 1999052800486 19990528 00486 WP 1999 5 28 EIA990095 1 19981226 A 5330 SKIN DOUG DC9 DC933F 302207A WP BS 350 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FUSELAGE SKIN AND DOUBLER HAS CORROSION AT BS 350 AT STRINGER 30, NRC NR F106. REPAIRED IAW DRAWING 53- 98681-3 AND ECRA AND SRM 53-04. (M) 2 L 7 2 4F A6WE 1999052800487 19990528 00487 WP 1999 5 28 EIA990094 1 19981226 A 5313 STRINGER DOUG DC9 DC933F 302207A WP FUSELAGE CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, STRINGER 14R IS CRACKED JUST AFT OF THE AFT PRESSURE BULKHEAD, NRC NR W191. REPAIRED PER SRM 53-02 FIG 18. (M) 2 L 7 2 4F A6WE 1999052800488 19990528 00488 WP 1999 5 28 EIA990093 1 19981226 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 229-313 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON 23L HAS CORROSION FROM BS 229-313, NRC NR H052. REPAIRED LONGERON PE R SRM 53-11-02 FIG 3B. (M) 2 L 7 2 4F A6WE 1999052800489 19990528 00489 WP 1999 5 28 EIA990092 1 19981226 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 229-313 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON 22L HAS CORROSION FROM BS 229-313, NRC NR H052. REPAIRED LONGERON PE R SRM 53-11-02 FIG 3B. (M) 2 L 7 2 4F A6WE 1999052800490 19990528 00490 WP 1999 5 28 EIA990091 1 19981226 A 5313 LONGERON DOUG DC9 DC933F 302207A WP BS 229-313 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, FORWARD CARGO COMPARTMENT LONGERON 21L HAS CORROSION FROM BS 229-313, NRC NR H052. REPAIRED LONGERON PE R SRM 53-11-02 FIG 3B. (M) 2 L 7 2 4F A6WE 1999052800491 19990528 00491 WP 1999 5 28 EIA990090 1 19981226 A 5320 STANSIONS DOUG DC9 DC933F 302207A WP BS 370/427 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 DURING C-CHECK, FORWARD CARGO COMPARTMENT VERTICAL STANSIONS CRACKED AT BS 370 AND 427 ON LEFT SLANTED SIDE WALL ABOVE S TRINGER, NRC NR H065. REPLACED VERTICAL STANSIONS PER SRM 53-10-2. (M) 2 L 7 2 4F A6WE 1999052800492 19990528 00492 WP 1999 5 28 EIA990089 1 19981228 A 5315 FLOORBEAM DOUG DC9 DC933F 302207A WP BS 996 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 47191 DURING C-CHECK, FLOORBEAM AT BS 996 ON RIGHT SIDE HAS AN ELONGATED HOLE, NRC NR L099. REPAIRED PER DRAWING 53-98681-4 A ND ECRA AND REPLACED FLOORBEAM FITTING. (M) 2 L 7 2 4F A6WE 1999052800493 19990528 00493 WP 1999 5 28 EIA990088 1 19981228 A 5400 RIB DOUG DC9 DC933F 302207A WP NR 2 PYLON CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, NR 2 PYLON RIB AT STATION 1009 CRACKED, NRC NR R047. REPAIRED PER SRM 54-01 FIG 2. (M) 2 L 7 2 4F A6WE 1999052800494 19990528 00494 WP 1999 5 28 EIA990087 1 19981215 A 5313 59516857 STRINGER DOUG DC9 DC933F 302207A WP BS 756 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 933F 52393 47191 DURING C-CHECK, STRINGER NR 30 WAS FOUND WITH EXFOLIATION CORROSION AT BS 756, NRC NR R137. REPAIRED PER DAC DRAWING 59 51685-7 AND ECRA. (M) 2 L 7 2 4F A6WE 1999052800572 19990528 00572 NM 1999 5 28 P2EA98314 1 19980114 A 5753 654791210 FITTING BOEING 737 737222 1384473 NM RT TE FLAP GOUGED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - IN C-CHECK OPERATION AT COOPESA, A GOUGE WAS FOUND AT RIGHT WING, OUTBOARD TRACK, WBL 355, ON THE OUTBOARD FLAP GI MBLE SUPPORT FITTING. THE GOUGE WAS BLENDED OUT AND FOUND WITHIN LIMITS AS PER BOEING AIRCRAFT CO. (M) 2 L 7 2 4F A16WE 1999052800573 19990528 00573 NM 1999 5 28 P2EA98315 1 19980124 A 5320 69560551 PLATE BOEING 737 737222 1384473 NM BS 628 CRACKED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 603DJ 19955 SJO - IN C-CHECK OPERATION AT COOPESA, A CRACK WAS FOUND IN THE UPPER VHF ANTENNA BASE PLATE. A NEW BASE PLATE WAS FABR ICATED AND REPLACED PER BOEING SPECIFICATIONS. (M) 2 L 7 2 4F A16WE 1999052800574 19990528 00574 NM 1999 5 28 P2EA98313 1 19980927 A 5320 WALL BOEING 737 737247 138448D NM NLG WW DENTED A P2EA K NONE O OTHER IN INSP/MAINT 1 CE 05 912MP 19607 MCI - NOSE WHEEL WELL WALL DENTED AT BS 251, DEFECT SIZE 1.5 INCH BY 2 INCH BY .250 INCH. REPAIRED NOSE WHEEL WELL SECT ION AT BS 251 PER BOEING TELEX VAG-MCI-98-0086RR DATED SEPT 27, 1998. (M) 2 L 7 2 4F A16WE 1999052800575 19990528 00575 WP 1999 5 28 ORJA99157 1 19981005 A 5330 PLATE DOUG DC9 DC983 3022083 WP BS 1155 CORRODED A ORJA K NONE O OTHER IN INSP/MAINT 1 WP 11 832RA 53044 AT OKC, LEVEL 2 CORROSION, HEAVY CORROSION AROUND VHF ANTENNA NR 3 COUPLES STATION 1155. FABRICATED BLANKING PLATE IAW 51-10-2 DC9'S SRM. TREATED AND PRIMED IAW DC9'S SRM 51-10-3. LEAK CHECK GOOD AIW MD-80, MM 21-00-00. (M) 2 L 7 2 4F RT A6WE 1999061800004 19990618 00004 EA 1999 6 18 CA981028005 1 19981018 A 2422 DH103024600CS INVERTER DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE E/E BAY FAILED W E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 CA 19144 AA2273S8 123112 (CAN) ON START-UP, BURNING SMELL IN COCKPIT, FOLLOWED BY SMOKE COMING FROM UNDERNEATH THE CAPTAIN'S CIRCUIT BREAKER PANE L. PASSENGERS DEPLANED. INSPECTION FOUND THE PRIMARY INVERTER FAILED AND WAS CAUSING SMOKE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999061800005 19990618 00005 NM 1999 6 18 CA981113005 1 19981103 A 3230 841005 PSEU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG FAILED W O OTHER N FALSE WARNING LD LANDING 1 CA 14692 297 121075 (CAN) ON GEAR DOWN SELECTION, THERE WERE 3 GREEN AND 3 RED AND A GEAR HANDLE LIGHT. PSEU REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999061800010 19990618 00010 EU 1999 6 18 CA990310027 1 19981124 A 3220 104626002 EYEBOLT BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 25817 DRG928286 LF05629A (CAN) NLG RETRACTION EYEBOLT PULLED OUT OF RETRACTION PISTON. PART REPLACED. REFER TO BAE SB32-146. 2 H 7 4 4F 4 F RT A49EU E6NE 1999070900628 19990709 00628 CE 1999 7 9 99ZZZM378 1 19981016 A 2701 40418751026 CONTROL COLUMN BEECH 18 E18S 1151006 CE COCKPIT CRACKED A GGPA K NONE O OTHER IN INSP/MAINT 1 NM 01 42D 24038 BA117 AIRCRAFT IN FOR A B2 INSPECTION, COMPLYING WITH AD 77-19-07 CONTROL COLUMN INSPECTION, A CRACK WAS DETECTED IN THE AREA 'A' LEFT CONTROL COLUMN OF AD 77-19-07, A .25 INCH CRACK ACROSS THE LOWER WELD. CONTROL COLUMN REMOVED AND REPLACED WIT H A NEW ONE. (M) 1 L 7 2 3R A765 1999070900630 19990709 00630 CE 1999 7 9 99ZZZM380 1 19981215 A 5610 185512L WINDSHIELD BEECH 18 E18S 1151006 CE COCKPIT BROKEN A GGPA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 NM 01 9001 16840 BA460 AIRCRAFT DEPART FROM EPH TO EAT, ON TAKEOFF AIRCRAFT HAD A BIRDSTRIKE ON LEFT WINDSHIELD. AIRCRAFT RETURNED TO EPH MECH ANIS INSPECTED AIRCRAFT AND REPLACED WINDSHIELD, RETURNED TO AIRCRAFT TO SERVICE. (M) 1 L 7 2 3R A765 1999071600028 19990716 00028 EU 1999 7 16 JBXA9900090 1 19980707 A 2910 NAS161210 O-RING FOKKER F28 F28MK0100 4990807 EU RROYCE TAY TAYMK65015 EU NR 1 HYD SYS FAILED A JBXA O OTHER K J FLUID LOSS WARNING INDICATION CR CRUISE 1 SO 05 105ML 11475 HYDRAULIC SYSTEM NR 1 LOW QUANTITY MESSAGE, TURNED OFF PUMPS IAW MIDWAY PROCEDURE. VLANDED WITH 25 DEGREES FLAPS AND RAI SED GEAR DOORS, HOWEVER NEGATIVE NOSE WHEEL STEERING. TOWED TO GATE. FOUND NR 1 ENGINE SYSTEM NR 1 HYDRAULIC PUMP QUIC K DISCONNECT LINE LEAKING. REMOVED AND REPLACED O-RING IAW F-100 AMM 29-11-01. SERVICED AND BLED SYSTEM IAW F-100 AMM 12-12-01. GROUND RAN ENGINE, LEAK CHECK GOOD. 2 L 7 2 4F 4 F RT 1999072000002 19990720 00002 NE 1999 7 20 DLL14991489 2 19980701 A 7320 LK55914 PS2 LINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B4 54555 NE NR 2 ENGINE LEAKING A DALA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 27 741DA 193C1245 014707 NACELLE NR 2 OVERHEAT ILLUMINATED ALONG WITH NR 2 ENG NAC/PYLON OVERHEAT, A & B ILLUMINATED. FOUND PRSOV PS2 LINE LEAKI NG. REPLACED LINE AND LEAK CHECKED. PERFORMED HIGH POWER RUN PER PFHB. NO FAULTS DETECTED. 2 L 7 3 4F 4 F A23WE E12EU 1999072300270 19990723 00270 EU 1999 7 23 99ZZZX2664 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 4 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804. 2 H 7 4 4F RT A49EU 1999072300271 19990723 00271 EU 1999 7 23 99ZZZX2665 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 2 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300272 19990723 00272 EU 1999 7 23 99ZZZX2666 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 3 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300273 19990723 00273 EU 1999 7 23 99ZZZX2667 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 2 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300274 19990723 00274 EU 1999 7 23 99ZZZX2668 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 6 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE IAW DRAWING AW-25-20-9084-06 OF PSI-1. 2 H 7 4 4F RT A49EU 1999072300275 19990723 00275 EU 1999 7 23 99ZZZX2669 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW 9 E2082 NR 7 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300276 19990723 00276 EU 1999 7 23 99ZZZX2670 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 3 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300277 19990723 00277 EU 1999 7 23 99ZZZX2671 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 1 RT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300278 19990723 00278 EU 1999 7 23 99ZZZX2672 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 5 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300279 19990723 00279 EU 1999 7 23 99ZZZX2673 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 1 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-6 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300280 19990723 00280 EU 1999 7 23 99ZZZX2674 1 19980820 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FRAME 47 DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 DENT LEFT FUSELAGE AT FRAME 47 BETWEEN STRINGERS 14 AND 16. REPAIRED DENT IAW BAE FAX REF DJR/RJ0620-98. 2 H 7 4 4F RT A49EU 1999072300281 19990723 00281 EU 1999 7 23 99ZZZX2675 1 19980820 A 5720 ANGLE BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 LEFT WING T/E, LOWER SHROUD STIFFENER, AND AFT TAG ANGLE CRACKED BETWEEN RIBS 7 AND 8. REPLACED LEFT WING T/R LOWER SHR OUD STIFFENER AND AFT TAG ANGLE BETWEEN RIBS 7 AND 8. 2 H 7 4 4F RT A49EU 1999072300282 19990723 00282 EU 1999 7 23 99ZZZX2676 1 19980813 A 5720 RIVET BAG BAE146 BAE146200A 1500266 EU LT WING LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NUMEROUS LOOSE RIVETS AT LT WING T/E LOWER SKIN, AFT OF REAR SPAR. REMOVED AND REPLACED NUMEROUS LOOSE RIVETS ON LT WIN G T/E LOWER SKIN AFT OF REAR SPAR. 2 H 7 4 4F RT A49EU 1999072300283 19990723 00283 EU 1999 7 23 99ZZZX2677 1 19980807 A 7110 DOOR BAG BAE146 BAE146200A 1500266 EU NR 4 ENG COWL CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 4 INBOARD COWL FAN DUCT DOOR HAS VARIOUS CHAFES AT LOWER PAN AREA. REPAIRED CHAFED AREA BY PATCHING IAW BAE SRM STD PROCEDURES. 2 H 7 4 4F RT A49EU 1999072300284 19990723 00284 EU 1999 7 23 99ZZZX2678 1 19980811 A 7921 BRACKET BAG BAE146 BAE146200A 1500266 EU NR 4 ENGINE BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 4 ENGINE BRACKET AT LOWER FUEL/OIL HEAT EXCHANGER BROKEN. REPAIRED NR 4 ENGINE BRACKET AT LOWER FUEL/OIL HEAT EXCHAN GER BY WELDING IAW ALLIED SIGNAL/TEXTRON MM. 2 H 7 4 4F RT A49EU 1999072300285 19990723 00285 EU 1999 7 23 99ZZZX2679 1 19980811 A 7110 FRAME BAG BAE146 BAE146200A 1500266 EU NR 1 ENG COWL CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 1 ENGINE FORWARD LEFT COWL DOOR LOWER AFT FRAME CHAFED NEAR LATCH. REPAIRED NR 1 ENGINE LEFT FORWARD COWL DOOR LOWER AFT FRAME IAW SRM 54-10-11. 2 H 7 4 4F RT A49EU 1999072300286 19990723 00286 EU 1999 7 23 99ZZZX2680 1 19980808 A 5320 INTERCOSTAL BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 AFT END OF FORWARD VEST INTERCOSTAL AT A/C CENTERLINE IS CRACKED IN THE TOP FLANGE RADIUS. REPAIRED AFT FORWARD VEST CE NTERLINE INTERCOSTAL. REF SRM 53-20-32, AT 51-71-11, PAGE 3. 2 H 7 4 4F RT A49EU 1999072300287 19990723 00287 EU 1999 7 23 99ZZZX2681 1 19980810 A 5320 INTERCOSTAL BAG BAE146 BAE146200A 1500266 EU FRAMES 41-43 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 AFT VEST, CENTER FLOOR INTERCOSTAL BETWEEN FRAMES 41 AND 43 IS CRACKED ABOUT 1.25 INCHES AT FORWARD END. REMOVED AND RE PLACED AFT VEST, CENTER FLOOR INTERCOSTAL WITH NEW PART. REPLACED INTERCOSTAL HC538J0430-006. 2 H 7 4 4F RT A49EU 1999072300288 19990723 00288 EU 1999 7 23 99ZZZX2682 1 19980812 A 5313 LONGERON BAG BAE146 BAE146200A 1500266 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 ATTACHMENT ANGLE/GUSSET AT THE AFT END OF THE UPPER MOST LEFT AIRBRAKE HINGE LONGERON IS CRACKED. FABRICATED LEFT GUSSE T PLATE PER BAE DRAWING HC539H0229. REPLACED LEFT GUSSET PLATE AT UPPER MOST LEFT AIRBRAKE HINGE LONGERON. 2 H 7 4 4F RT A49EU 1999072300289 19990723 00289 EU 1999 7 23 99ZZZX2683 1 19980813 A 5320 SUB FRAME BAG BAE146 BAE146200A 1500266 EU FRAME 50 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 SUB-FRAME AFT OF FRAME 50 CRACKED AT LOWER LT CORNER. REPAIRED SUB-FRAME AFT OF FRAME 50 AT LOWER LT CORNER IAW BAE FAX DJR/RJ0602-98. 2 H 7 4 4F RT A49EU 1999072300290 19990723 00290 EU 1999 7 23 99ZZZX2684 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 5 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300292 19990723 00292 EU 1999 7 23 99ZZZX2686 1 19980818 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RT WING T/E SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 9 AND 10. REPAIRED PER BAE FAX JM/RJ0317/97 USING 2024T3 .040 INCH AND AW FAX HC/142-97 AND DJR/RJ0630-98. 2 H 7 4 4F RT A49EU 1999072300293 19990723 00293 EU 1999 7 23 99ZZZX2687 1 19980819 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 DENT AT BOXING JT RT FUSELAGE FORWARD OF REAR CARGO DOOR DUE REPAIR IN 3,000 CYCLES. CURRENT CYCLES: 29,794. REPAIR DUE BY 32,794 CYCLES. REPAIRED DENT IAW BAE FAX REF DJR/RJ0610-98. REF: W/C 1049 NDT. 2 H 7 4 4F RT A49EU 1999072300294 19990723 00294 EU 1999 7 23 99ZZZX2688 1 19980821 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 LEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 5 AND 6 IS CRACKED AT FORWARD END. REPAIRED IAW BAE RDO DJR/ RJ0630-98. REF: W/C 5035 FOR ALODINE PRIME AND PAINT. 2 H 7 4 4F RT A49EU 1999072300295 19990723 00295 EU 1999 7 23 99ZZZX2689 1 19980820 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 LEFT WING TOP WING STIFFENER AFT OF REAR SPAR BETWEEN RIBS 8 AND 9 IS CRACKED AT FORWARD ENG. REPAIRED IAW BAE RDO EJR/ RJ0630-98. REF: W/C 5035 FOR ALODINE, PRIME AND PAINT. 2 H 7 4 4F RT A49EU 1999072300296 19990723 00296 EU 1999 7 23 99ZZZX2690 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 8 LEFT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-96 (PART OF PS-1). 2 H 7 4 4F RT A49EU 1999072300297 19990723 00297 EU 1999 7 23 99ZZZX2691 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 6 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9084-06 OF PS-I. 2 H 7 4 4F RT A49EU 1999072300298 19990723 00298 EU 1999 7 23 99ZZZX2692 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 7 RT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW 25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300299 19990723 00299 EU 1999 7 23 99ZZZX2693 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 9 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300300 19990723 00300 EU 1999 7 23 99ZZZX2694 1 19980813 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FRAME 9 DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 REPAIR DENT ON LEFT SIDE OF FUSELAGE AT FRAME 9, 3.25 INCHES BELOW SKIN LAP B AND 4.00 INCHES FORWARD OF FRAME 9 IN 3,00 0 CYCLES. CURRENT TCA 29,540 DUE AT 32,540 TAC. 2 H 7 4 4F RT A49EU 1999072300301 19990723 00301 EU 1999 7 23 99ZZZX2695 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 8 RIGHT BIN FLOOR SOFT. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-30-9804-06 OF PS-1. 2 H 7 4 4F RT A49EU 1999072300302 19990723 00302 EU 1999 7 23 99ZZZX2696 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 9 RIGHT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1. ACFT TT: 19,32 7 HOURS. ACFT TC: 22,789. 2 H 7 4 4F RT A49EU 1999072300326 19990723 00326 EU 1999 7 23 99ZZZX2702 1 19980821 A 2910 BRACKET BAG BAE146 BAE146200A 1500266 EU HYDRAULIC SYSTEM CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 LEFT WING TE HYDRAULIC LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET. 2 H 7 4 4F RT A49EU 1999073000011 19990730 00011 NE 1999 7 30 99ZZZX2745 2 19981125 A 7322 NAR9B CARBURETOR BEECH 18 E18S 1151006 CE PWA R985 R985AN14B 52008 NE RT ENGINE MALFUNCTIONED A GGPA A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CR CRUISE 1 NM 01 48K 1006 BA202 2310 AIRCRAFT GOING FROM BFI TO PUL, ABOUT 1 HOUR FROM BFI, THE RIGHT ENGINE STARTED TO LOSE POWER, PILOT FEATHERED THE RIGHT ENGINE AND DIVERTED TO PSC. ABOUT 1 HOUR AFTER LANDING, PILOT STARTED THE ENGINE. A MECHANIC WAS SENT TO PSC AND THE CARBURETOR WAS CHANGED. SUBMITTER STATED IT APPEARED THE ENGINE ICED UP AND PILOT DID NOT APPLY CARBURETOR HEAT IN TIME . 1 L 7 2 3R 3 R A765 5E1 1999073000012 19990730 00012 CE 1999 7 30 99ZZZX2746 1 19981103 A 3220 AN33DD BOLT BEECH 18 E18S 1151006 CE TAILWHEEL FAILED A GGPA O OTHER O OTHER NR NOT REPORTED 1 NM 01 48K BA202 AFTER LANDING AT AWO, THE TAILWHEEL STRUT COLLAPSED. THE TAIL OF THE AIRCRAFT WAS JACKED UP AND THE TAILWHEEL ASSY LOWE RED. NO DAMAGE WAS DONE TO THE AIRCRAFT. MECHANICS FOUND THE SHEER BOLT ON RETRACT CABLE SHEARED. THE SHEAR BOLT WAS REPLACED. 1 L 7 2 3R A765 1999073000069 19990730 00069 EU 1999 7 30 UF6A981016 1 19981021 A 3330 30180B23D LIGHT MIDLANDROSS BAG ATP ATP EU CARGO BAY FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - REQUESTED INSPECTION OF BURNING SMELL IN FLIGHT DEC, CABIN AND GALLEY. MAINTENANCE INSPECTED AND FOUND FORWARD BA GGAGE COMPARTMENT BOMB BAY LIGHT ASSEMBLY BAD. REMOVED AND REPLACED LIGHT ASSY. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000070 19990730 00070 EU 1999 7 30 UF6A981012 1 19981019 A 3350 58785 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 ORD - FLT 5760 - FORWARD MOST STRIP OF EMERGENCY FLOOR LIGHTS INOPERABLE. MAINTENANCE INSTALLED FLOOR PROXIMITY LIGHT S TRIP. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000072 19990730 00072 EU 1999 7 30 UF6A981009 1 19981019 A 2560 P4010021 BATTERY BAG ATP ATP EU FLASHLIGHT DISCHARGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 2032 SBN - AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY. SYSTE M OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000073 19990730 00073 EU 1999 7 30 UF6A981015 1 19981022 A 3350 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 SBN - EMERGENCY EXIT LIGHT NEXT TO AFT PASSENGER DOOR INOPERATIVE. MAINTENANCE REMOVED EXIT LIGHT, VISUALLY INSPECTED LIGHT AND ASSOCATED WIRING. RE-INSTALLED EXIT LIGHT AND SYSTEM OPS CHECKED GOOD. NO DEFECTS NOTED. (X) 2 L 7 2 4T RT A27NM 1999073000074 19990730 00074 EU 1999 7 30 UF6A981018 1 19981026 A 3350 58785 CABLE ASSY BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 ORD - FLT 5705 - FLOOR EMERGENCY LIGHTS, AFT CABIN, NOT ILLUMINATED WHEN TESTED. MAINTENANCE REMOVED AND REPLACED FLOO R PROXIMITY LIGHT STRIP. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000075 19990730 00075 EU 1999 7 30 UF6A981020 1 19981027 A 3350 58781 CABLE ASSY BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 ORD - UPON DAILY INSPECTION, FOUND FLOOR STRIP EMERGENCY LIGHTS IN FORWARD CABIN INOPERATIVE. MAINTENANCE REMOVED AND R EPLACED FLOOR STRIP LIGHT. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000076 19990730 00076 EU 1999 7 30 UF6A981021 1 19981027 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 ORD - FLT 5732 - EMERGENCY LIGHTS INOPERATIVE IN LAVATORY AND AFT GALLEY OVERHEAD. MAINTENANCE REMOVED AND REPLACED LAV ATORY AND AFT GALLEY BULB. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000077 19990730 00077 EU 1999 7 30 UF6A981102 1 19981104 A 3350 6013211 POWER SUPPLY GRIMES BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 856AW 7685 561 17089 2032 SBN - AFT EMERGENCY LIGHTING FLOOR STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED NR 6 POWER SUPPLY. SYSTEM OPS C HECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000078 19990730 00078 EU 1999 7 30 UF6A981203 1 19981204 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 858AW 2035 SBN - OUTSIDE EMERGENCY LIGHT BULBS BEHIND EACH WING ARE INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULBS. SYSTEM OP S CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000079 19990730 00079 EU 1999 7 30 UF6A981205 1 19981212 A 3350 LIGHT BAG ATP ATP EU ROWS 6/7 INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 2029 PIA - FLT 5743 - EMERGENCY EXIT LIGHTS ROWS 6 AND 7 WILL NOT ILLUMINATE. MAINTENANCE PERFORMED OPS CHECK OF SYSTEM. SY STEM OPS CHECKED GOOD. NO DEFECTS NOTED. (X) 2 L 7 2 4T RT A27NM 1999073000080 19990730 00080 EU 1999 7 30 UF6AO81208 1 19981217 A 3350 25890 BULB BAG ATP ATP EU FAILED UNKNOWN A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 852AW 2021 ORD - FLT 5732 - EMERGENCY LIGHT IN LAVATORY IS INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 1999073000081 19990730 00081 EU 1999 7 30 UF6A981210 1 19981221 A 3350 1317 BULB BAG ATP ATP EU CABIN FAILED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 2029 SBN - EMERGENCY LIGHT BULB RIGHT SIDE OVERWING INOPERABLE. MAINTENANCE REMOVED AND REPLACED BULB. (X) 2 L 7 2 4T RT A27NM 1999073000082 19990730 00082 EU 1999 7 30 UF6A981211 1 19981222 A 5210 SKIN BAG ATP ATP EU PASSENGER DOOR DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - DENT ON FUSELAGE FORWARD OF FORWARD PASSENER DOOR. MAINTENANCE DRESSED OUT DENT TOWARDS ORIGINAL CONTOUR. FABRIC ATED REPAIR DOUBLER FROM 2024-T3. LAYED OUT RIVET PATTERN AND DRILLED FASTENER. WET ASSEMBLED AND APPLIED PROTECTION T REATMENT AND FINISHER. ACFT TT: 14,383 HOURS. (X) 2 L 7 2 4T RT A27NM 1999073000083 19990730 00083 EU 1999 7 30 UF6A981222 1 19981222 A 3350 6013211 BATTERY PACK BAG ATP ATP EU ROWS 8,9,10 DISCHARGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 855AW 2029 AZO - FLT 5764 - ROWS 8, 9, AND 10 EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REMOVED AND REPLACED NR 5 AND NR 7 BATTERY PACKS. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000084 19990730 00084 EU 1999 7 30 UF6A981214 1 19981222 A 5512 SKIN BAG ATP ATP EU HORIZ STABILIZER DENTED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - DENT ON TOP OF LEFT HAND HORIZONTAL STABILIZER AT STA 46.375. MAINTENANCE REMOVED SMALL GOUGE ON TOP SKIN WITH .1 875 INCH DRILL AND PERFORMED NDT INSPECTION. NO FURTHER DEFECTS NOTED. PULLED DENT TO CONTOUR AND INSTALLED 1 MS20470 AD6 RIVET. ALODINED, PRIMED AND PAINTED AREA. WORK DONE IAW ENGINEERING REPORT NR 98-199. (X) 2 L 7 2 4T RT A27NM 1999073000085 19990730 00085 EU 1999 7 30 UF6A981213 1 19981222 A 5410 JD711J0673000W DUCT BAG ATP ATP EU NR 2 ENGINE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - NR 2 OUTBOARD MOD 2 NACA DUCT HAS CRACK ON LEADING EDGE APPROXIMATELY 4 INCHES LONG. MAINTENANCE STOP DRILLED CRA CK AND PERFORMED NDT INSPECTION. NO FURTHER DEFECTS NOTED. FABRICATED TWO DOUBLERS FROM ALCLAD 2024-T3 .063 INCH AND I NSTALLED PER ENGINEERING ORDER NR 98-199. (X) 2 L 7 2 4T RT A27NM 1999073000086 19990730 00086 EU 1999 7 30 UF6A981212 1 19981222 A 5410 DUCT BAG ATP ATP EU NR 1 NACELLE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - MOD NR 2 NACA DUCT IS CRACKED ON OUTBOARD IGNITER PANEL ON NR 1 SIDE. MAINTENANCE STOP DRILLED CRACK AND PERFORME D NDT INSPECTION. NO FURTHER DEFECTS NOTED. FABRICATED TWO DOUBLERS FROM ALCLAD 2024-T3 .063 INCH AND INSTALLED PER EN GINEERING REPORT NR 98-199. AIRCRAFT TT: 14,383. (X) 2 L 7 2 4T RT A27NM 1999073000087 19990730 00087 EU 1999 7 30 UF6A981217 1 19981223 A 5414 SKIN BAG ATP ATP EU NACELLE CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 14383 2028 SBN - LEFT HAND INBOARD LEADING EDGE HAS CRACK ON UPPER LEFT HAND CORNER. MAINTENANCE REPAIRED BY INSTALLATION OF FABRI CATED L-SHAPED PATCH DOUBLER MADE OF 2024-T3 .063 INCH. ALL WORK DONE IAW DER REPORT NR 98-199. (X) 2 L 7 2 4T RT A27NM 1999073000088 19990730 00088 EU 1999 7 30 UF6A981221 1 19981223 A 5320 JD255J0282000 ANGLE BAG ATP ATP EU BS 308 DAMAGED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 14383 2028 SBN - AFT BAGGAGE, FORWARD BULKHEAD, ATTACHMENT ANGLE FOR SURROUND ON RIGHT HAND SIDE OF FUSELAGE AT STA 308AS HAS SEVER AL HOLES THAT ARE OVER-DRILLED WITH CRACKS. MAINTENANCE REPAIRED DAMAGE IAW DER REPORT NR 98-199. (X) 2 L 7 2 4T RT A27NM 1999073000089 19990730 00089 EU 1999 7 30 UF6A981220 1 19981223 A 5315 FLOORBEAM BAG ATP ATP EU BS 270 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - CORROSION AT STA 270AS UNDER FLOORBOARD 241FF, EF, AND 242CF. MAINTENANCE REMOVED CORROSION AND FABRICATED TOP ST RAP OF 2024-T3 .063 INCH THICK. INSTALLED STRAP USING MS20426AD6 RIVETS. WORK DONE IAW DER REPORT NR 98-199. AIRCRAFT TT: 14,383. (X) 2 L 7 2 4T RT A27NM 1999073000090 19990730 00090 EU 1999 7 30 UF6A981219 1 19981223 A 5320 BRACKET BAG ATP ATP EU E/E BAY CRACKED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - UNDER FLOOR FORWARD AVIONICS CRATE SUPPORT BRACKETS ARE CRACKED. MAINTENANCE FABRICATED NEW SUPPORT BRACKETS IAW DER REPORT NR 98-199. (X) 2 L 7 2 4T RT A27NM 1999073000091 19990730 00091 EU 1999 7 30 UF6A981216 1 19981223 A 5753 JD575J0315001 FLAP TRACK BAG ATP ATP EU TE FLAP CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 14383 2028 SBN - FLAP TRACK AT STA 188.366 ON RIGHT HAND SIDE PITTING. MAINTENANCE BLENDED OUT PITTING AND PERFORMED DYE PENETRANT INSPECTION IAW BAE TOR 001773. NO DEFECTS NOTED. AIRCRAFT TT: 14,383. (X) 2 L 7 2 4T RT A27NM 1999073000092 19990730 00092 EU 1999 7 30 UF6A981215 1 19981223 A 5753 JD575J0315000 FLAP TRACK BAG ATP ATP EU TE FLAP CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 14383 2028 SBN - FLAP TRACK AT STA 188.366 ON LEFT HAND SIDE PITTING. MAINTENANCE BLENDED OUT PITTING ON FLAP TRACK AND PERFORMED DYE PENETRANT INSPECTION. NO DEFECTS NOTED. WORK DONE IAW BAE TOR 001773. (X) 2 L 7 2 4T RT A27NM 1999073000093 19990730 00093 EU 1999 7 30 UF6A981218 1 19981223 A 5315 FLOORBEAM BAG ATP ATP EU BS 324 CORRODED A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 854AW 2028 SBN - CORROSION UNDER FLOORBOARD 221CF, STA 324FS. MAINTENANCE REMOVED CORROSION AND FABRICATED ANGLE FROM 2024-T3 .050 INCH THICK. INSTALLED ANGLE USING MS20470AD4 FASTENERS FOR THE VERTICLE LEG AND MS202426AD4 FASTENERS FOR THE HORIZONT AL LEG. ALL WORK DONE IAW DER REPORT NR 98-199. (X) 2 L 7 2 4T RT A27NM 1999073000122 19990730 00122 EU 1999 7 30 UF6A981011 1 19981018 A 3397 58785 WIRE BAG ATP ATP EU CABIN LOOSE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 851AW 2020 SBN - FLT 5753 - LAST 3 FLOOR EMERGENCY LIGHTS INOPERABLE. MAINTENANCE RE-SECURED FLOOR PROXIMITY LIGHTING STRIP. SYST EM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000123 19990730 00123 EU 1999 7 30 UF6A981010 1 19981018 A 3350 58785 LIGHT BAG ATP ATP EU CABIN INOPERATIVE A UF6A K NONE O OTHER IN INSP/MAINT 1 GL 31 859AW 2036 ORD - FORWARD SECTION OF EMERGENCY LIGHT STRIP INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FLOOR LIGHT POWER STRIP. S YSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000125 19990730 00125 EU 1999 7 30 UF6A981019 1 19981025 A 2150 7846281 FAN HAMSTD BAG ATP ATP EU AIR DIST FAILED A UF6A D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 GL 31 852AW 6386 4604 890761 2021 ORD - FLT 5720 - NR 2 RECIRCULATION FAN INDICATES OFF AND FLIGHT ATTENDANT REPORTS A BURNING SMELL. MAINTENANCE REMOVED AND REPLACED NR 2 RECIRCULATION FAN. SYSTEM OPS CHECKED GOOD. (X) 2 L 7 2 4T RT A27NM 1999073000336 19990730 00336 NM 1999 7 30 DLM88991649 1 19980922 A 5700 652163350 RIB DOUG MD88 MD88 3023688 NM TE MIDFLAP DAMAGED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 999DN 53371 DURING CONDITION ACCEPT INSPECTION OF FLAP-A TEMP TYPE REPAIR WAS FOUND ON I/B AFT CLOSEOUT RIB, LOWER AFT CORNER. T HE RIB WAS REPAIRED PER MM 57-52-0, FIG 808 BY INSTALLING A DIFFERENT DOUBLER. 2 L 7 2 4F RT A6WE 1999073000620 19990730 00620 EU 1999 7 30 99ZZZM405 1 19981026 A 2120 S53682015202 VENTURI AEROSP ATR42 ATR42300 8680920 EU LAVATORY CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 135MQ 135 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LAVATORY VENTURI CORRODED. INSTALLED NE W VENTURI IN LAVATORY AS PER SRM 51-25-02. CAUSE OF DAMAGE, ENVIRONMENTAL, LAVATORY/GALLEY SPILLS. (M) 2 H 7 2 4T RT A53EU 1999073000621 19990730 00621 EU 1999 7 30 99ZZZM406 1 19981026 A 5347 S53678001201 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 135MQ 135 DURNIG A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE RIGHT AFT OUTBOARD SEAT TRACK CORRODED. INSTALLED NEW SEAT TRACK AS PER SRM 51-25-04 AND EO NR E9-5300-013R2. CAUSE OF DAMAGE, ENVIRONMENTAL, LAVATORY/GALLEY SPILLS. (M) 2 H 7 2 4T RT A53EU 1999073000622 19990730 00622 EU 1999 7 30 99ZZZM407 1 19981026 A 5347 S53678001210 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 135MQ 135 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE LEFT FLIGHT ATTENDANT SEAT TRACK CORRODE D. INSTALLED NEW SEAT TRACK AS PER SRM 51-25-04 AND EO NR E9-5300-013R2. CAUSE OF DAMAGE, LAVATORY/GALLEY SPILLS. (M) 2 H 7 2 4T RT A53EU 1999073000623 19990730 00623 EU 1999 7 30 99ZZZM408 1 19981026 A 5347 S53678001202 SEAT TRACK AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 135MQ 135 DURING CPCP 4 INSPECTION PERFORMED AT AMR EAGEL MAINTENANCE CENTER, FOUND THE RIGHT AFT INBOARD SEAT TRACK CORRODED. IN STALLED NEW SEAT TRACK AS PER EO NR E9-5300-013R2. CAUSE OF DAMAGE, ENVIRONMENTAL, LAVATORY/GALLEY SPILLS. (M) 2 H 7 2 4T RT A53EU 1999073000624 19990730 00624 EU 1999 7 30 99ZZZM409 1 19981026 A 5315 S536724007202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 135MQ 135 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE FLOORBEAM 38 CORRODED ON TOP SURFACE AND BOTTOM. INSTALLED FLOORBEAM 38 AS PER SRM 51-25-03. CAUSE OF DAMAGE, LAVATORY/GALLEY SPILLS. (M) 2 H 7 2 4T RT A53EU 1999073000625 19990730 00625 EU 1999 7 30 99ZZZM410 1 19981026 A 5315 S536724007202 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 135MQ 135 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND THE FLOORBEAM 38 CORRODED ON TOP SURFACE AND BOTTOM. INSTALLED FLOORBEAM 38 AS PER SRM 51-25-03. CAUSE OF DAMAGE, LAVATORY/GALLEY SPILLS. (M) 2 H 7 2 4T RT A53EU 1999073000814 19990730 00814 WP 1999 7 30 99FDEA00270 1 19981127 A 5730 ARC2369 SKIN DOUG DC10 DC1010 3022110 WP LT FLAP CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 DUR A/C P-F CONV FOUND DAMAGE AT XIFH=288.14 ON THE UPPER SURFACE OF LT I/B FLAP SKIN. REMOVED AND REPLACED O/B UPPER S KIN SECTION DAMAGE ARC2369. SRM 57-10-00 FIG 4 IAW FEDEX IAW EA NR 8-5752-44069. 2 L 7 3 4F A22WE 1999073000815 19990730 00815 WP 1999 7 30 99FDEA00271 1 19981026 A 5345 3D0031730 BOLT DOUG DC10 DC1010 3022110 WP FUSELAGE CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 DUR A/C P-F CONV CORROSION WAS FOUND IN ALL FOUR HOLE BORES COMMON TO ABA7003-2 & ABA7172 FITTINGS. THREE BOLTS FAILED IN TENSION. REMOVED AND REPLACED BOLTS FROM BORES IAW FEDEX EA NR 8-5311-41885. 2 L 7 3 4F A22WE 1999073000816 19990730 00816 WP 1999 7 30 99FDEA00272 1 19981002 A 5330 AYB70301 SKIN DOUG DC10 DC1010 3022110 WP FS 1099 - 1541 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 374FE 46612 DUR A/C P-F CONV ON EXT LWR FUSELAGE FROM BS 1099 TO BS 1541 CORROSION. REMOVED AND REPLACED FUSELAGE BELLY SKIN FROM Y =1119 TO Y-1308, BETWEEN L48L-L48R. REPAIRED THEN INSTALLED AN EXT SKIN SPLICE SIMILAR TO SRM 5320, FIG 17 AT Y-1308 TO RESTORE STRENGTH IAW FEDEX EA NR 8-5334-41825. 2 L 7 3 4F A22WE 1999081200313 19990812 00313 WP 1999 8 12 99FDEA00305 1 19981021 A 5511 ALC70092 SPAR DOUG DC10 DC1010 3022110 WP HORIZ STAB CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 N2420 - DURING A/C PF CONVERSION AT AERONAVALI AND ACCOMPLISHMENT OF DAC SB 55-17, R3, AD 88-03-08, A CRACK WAS FOUND ON THE HORIZONTAL STAB. REPAIR ATTEMPS TO REMOVE CRACK DAMAGE BY LOCAL BLENDING AND PERF HFEC TO QUAN DAMAGE. B/P EQUIVA LENT BOLT IS REINSTALLED WITH SEALANT IAW EA NR 8-5510-41811. 2 L 7 3 4F A22WE 1999081200314 19990812 00314 WP 1999 8 12 99FDEA00306 1 19980818 A 5720 ARB08661 DOUBLER DOUG DC10 DC1010 3022110 WP WS 264 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 N0235 - DURING A/C P-F CONV AT AERONAVALI, CORROSION WAS FOUND ON LT UPPER WING AND MLG DOUBLER, TYPICAL PER DC10 SRM 57 -00-01, FIG 8. THE AMOUNT OF DAMAGE FOUND ON PN ARB0866-1 IS NOT COVERED BY SRM. REPAIR REMOVES ALL CORROSION BY CUTTI NG OUT DAMAGE AND THEN VERIFIES CONTAINMENT PRIOR TO INSTALLING FILLERS AND EXT DOUBLERS PER EA NR 8-5710-39523. 2 L 7 3 4F A22WE 1999081200315 19990812 00315 WP 1999 8 12 99FDEA00307 1 19980904 A 5320 ACJ70135 WEB DOUG DC10 DC1010 3022110 WP BS 2017 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 364FE 46600 N0527 - DURING AC P-F CONV AT AERONAVALI, A CRACK 0.87 IN LONG WAS FOUND ON WEB OF UPPER TORQUE BOX PLANE AT Y=2017 AND RBL = 20. SRM 53-00-01, FIG 4 SHEET 2 WEB REPAIR COULD NOT BE ACCOMPLISHED. REPAIR TO STOP DRILL CRACK AND VERIFY CON TAINMENT. THEN INSTALL TITANIUM REPAIR DOUBLER AND STIFFENER ANGLES IAW EA NR 8-5317-41822. 2 L 7 3 4F A22WE 1999081200412 19990812 00412 NM 1999 8 12 CA990310001 1 19981201 A 5260 85210181003 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE AIRSTAIR DOOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 21 120373 (CAN) CREW UNABLE TO OPEN AIRSTAIR DOOR AFTER LANDING. CABLE WRAPPED AROUND THE DRUM PREVENTING DOOR FROM BEING OPENED. CABLE HAD TO BE DISCONNECTED FROM DOOR TO ALLOW IT TO BE OPENED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200413 19990812 00413 EU 1999 8 12 CA990310002 1 19981213 A 2910 NAS16126 O-RING HC290B00280 BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE HYD MANIFOLD DAMAGED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA LF05542A (CAN) ON TAXI, CABIN FILLED WITH SMOKE, NR 2 HYDRAULIC LOW CAUTION LIGHT ILLUMUNATED, PASSENGER DEPLANED, SMOKE IDENTIFI ED AS SKYDROL MIST. INVESTIGATION REVEALED LEAKING O-RING ON HYDRAULIC SYSTEM PRESSURE MANIFOLD. PART REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200416 19990812 00416 NM 1999 8 12 CA990310006 1 19981125 A 2760 KX511 SWITCH DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ROLL SPOILER SHORTED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 15395 120083 (CAN) IN-FLIGHT, ROLL SPOILER INBOARD CAUTION LIGHT ILLUMINATED. LEFT UPPER ROLL SPOILER MICROSWITCH FOUND SHORTED INTE RNALLY, SWITCH REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200421 19990812 00421 EU 1999 8 12 CA990310012 1 19980724 A 2160 3537B000 VALVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE CABIN TEMP FAILED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DE DESCENT 1 CA 24935 2792521 LF05464A (CAN) DUCT TEMPERATURE HARD TO CONTROL. FLOW CONTROL AND MODE SELECTOR VALVES REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200427 19990812 00427 NM 1999 8 12 CA990310018 1 19981120 A 7712 30005000046 TSCU DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE MALFUNCTIONED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 3678 606 120229 (CAN) NR 2 ENGINE TORQUE WENT TO 168 PERCENT ON TAKEOFF. TAKEOFF REJECTED. ALL OTHER ENGINE PARAMETERS WERE NORMAL. A FTER RETURN TO GATE, THE TORQUE STILL INDICTED 168 PERCENT. THE TORQUE SENSOR CONDITIONING UNIT WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200433 19990812 00433 1999 8 12 CA990310024 4 19981213 A 3421 2587335114 VERTICAL GYRO BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT INTERMITTENT W A UNSCHED LANDING I FLT. ATTITUDE INST. CL CLIMB 1 CA 18814 87025980 LF05465A (CAN) VERTIAL GYRO TOPPLED TWICE POST-TAKEOFF. VERTICAL GYRO REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200434 19990812 00434 EU 1999 8 12 CA990310025 1 19981203 A 2751 WARNING SYSTEM BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE TE FLAP ILLUMINATED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA 24371 LF05465A (CAN) FLAP FAULT ILLUMINATED THEN WENT OUT, NO APPARENT FAULT. NO FAULT FOUND. 2 H 7 4 4F 4 F RT A49EU E6NE 1999081200445 19990812 00445 NM 1999 8 12 CA990310037 1 19981118 A 3020 655812313 DUCT BOEING 737 737275 1384485 NM PWA JT8 JT8D17A 52049 NE ANTI ICE SYSTEM RUPTURED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA 44110 P708807B (CAN) AIRCRAFT DIVERTED DUE TO OVERHEAT WARNING NR 2 EBGUBE. FOUND RUPTURED NOSE COWL ANTI-ICING DUCT. DUCT REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200446 19990812 00446 WP 1999 8 12 CA990310038 1 19981120 A 2424 5D038K5 CIRCUIT BREAKER DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE COCKPIT TRIPPED W A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA 455367 (CAN) AIRCRAFT DIVERTED DUE LEFT EMERGENCY BUS FEED CIRCUIT BREAKER TRIPPED, UNABLE TO RESET. REPLACED B1-136 RCCB. 2 L 7 3 4F 4 F A22WE E23EA 1999081200448 19990812 00448 NM 1999 8 12 CA990310041 1 19981124 A 2820 VALVE BOEING 747 747475 NM FUEL SYSTEM FAILED W D RETURN TO BLOCK K FLUID LOSS TX TAXI/GRND HDL 1 CA (CAN) PRIOR TO PUSHBACK, FUEL SPILL OCCURRED FROM SURGE TANK VENT HOLE. NR 3 FUEL TANK OVERFILL DUE TO UNCOMMANDED FUEL TRANSFER. AIRCRAFT HAD JUST COMPLETED MAINT AND NR 3 JETTISON OVERRIDE PUMP HOUSING AND CHECK VALVE REPLACED. SEALS R UPTURED DUE TO OVERTORQUING OF SCREWS. SCREWS SHEARED AND BELOW CHECK VALVE. SEAL REPLACED AND VALVE PROPERLY TORQUED. 2 L 7 4 4F RT A20WE 1999081200449 19990812 00449 NM 1999 8 12 CA990310042 1 19981211 A 2910 65178216 MODULE BOEING 737 737217 1384464 NM PWA JT8 JT8D17 52049 NE HYDRAULIC SYSTEM FAILED W D RETURN TO BLOCK J K WARNING INDICATION FLUID LOSS TX TAXI/GRND HDL 1 CA 32790 702735 (CAN) LOSS OF A-SYSTEM HYDRAULIC PRESSURE ON PUSH BACK, RETURN TO BLOCKS. REPLACED A-SYSTEM MODULE. 2 L 7 2 4F 4 F A16WE E2EA 1999081200450 19990812 00450 NM 1999 8 12 CA990310043 1 19981205 A 5610 5717623096 WINDOW BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE COCKPIT SHATTERED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 55019 26519 1H216755 709510 (CAN) ON TOP OF CLIMB AT FL 270 FIRST OFFICER'S WINDOW STARTED TO SPARK AND BEFORE HEAT TURNED OFF, THE OUTER PANE SHATT ERED. WINDOW REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200451 19990812 00451 NM 1999 8 12 CA990310044 1 19981217 A 5210 SNUBBER BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE PASSENGER DOOR STUCK W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 665539 (CAN) ON CLIMB, LOUD AIR NOISE COMING FROM LOWER SIDE OF DOOR 1L. FOUND DOOR 1L SNUBBER INST. SET SCREW CATCHING LOWER H INGE FLAPPER DOOR. SNUBBER REPOSITIONED, FLAPPER DOOR REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200452 19990812 00452 NM 1999 8 12 CA990310045 1 19981227 A 5751 6546454503 SKIN BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE AILERON DELAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 60496 0193 687840 (CAN) FOUND SKIN DELAMINATION APPROXIMATELY 1 SQUARE FOOT OF UPPER SKIN OF AILERON. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999081200483 19990812 00483 EA 1999 8 12 CA990310080 1 19981126 A 3234 574205 O RING 83210302001 DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE SELECTOR VALVE LEAKING W O OTHER J WARNING INDICATION AP APPROACH 1 CA 34 123061 (CAN) WHEN GEAR SELECTED DOWN, 3 RED WERE INDICATED. ALTERNATE GEAR SELECTION WAS MADE SUCCESSFULLY. A PIECE OF O-RING WAS FOUND IN MLG SELECTOR VALVE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200484 19990812 00484 NE 1999 8 12 CA990310082 2 19981204 A 7320 7892132002 EEC HAMSTD DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CA 89112945 123058 (CAN) ON DESCENT, PILOT REPORTED NR 2 ENGINE ELECTRONIC CONTROL (EEC) WENT INTO MANUAL WITH THE TORQUE INDICATION GOING BLANK AND THE ASSOCIATED CIRCUIT BREAKERS TRIPPING AND BEING UNABLE TO RESET. MAINTENANCE REPLACED THE EEC AND SOME CHA FED WIRES. THE ENGINE WAS GROUND RUN SERVICEABLE AND THE AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200485 19990812 00485 NE 1999 8 12 CA990310083 2 19981208 A 7320 7982133007 EEC UNITEDTECH DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NR 2 ENGINE MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION DE DESCENT 1 CA 8812513 123030 (CAN) ON DESCENT, NR 2 ENGINE LOST TORQUE INDICATION AND THE ENGINE REVERTED TO MANUAL. NR 2 ENGINE ELECTRONIC CONTROL WAS REPLACED, CHECKED SERVICEABLE AND THE AIRCRAFT REURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 1999081200487 19990812 00487 EU 1999 8 12 CA990310085 1 19981216 A 2913 40052 PUMP FOKKER F28 F28MK1000 4990808 EU HYDRAULIC SYSTEM LEAKING W B EMER. DESCENT K J FLUID LOSS WARNING INDICATION AP APPROACH 1 CA 12187 (CAN) ON DESCENT THROUGH 10,000 FEET, CREW NOTICED NR 1 EBG UTILITY HYDRAULIC SYSTM FLUID WAS DEPLETED ON THE GAUGE, FOL LOWED BY WARNING LIGHT. EMERGENCY LANDING CARRIED OUT, AIRCRAFT TOWED FROM RUNWAY, NO NOSE WHEEL STEERING. LEAKING NR 1 ENGINE UTILITY PUMP CASE DRAIN. PUMP REPLACED. 2 L 7 2 4F RT A20EU 1999081200488 19990812 00488 EU 1999 8 12 CA990310087 1 19981220 A 3232 125001 ACTUATOR FOKKER F28 F28MK1000 4990808 EU MLG DOOR CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CA 46882 (CAN) PILOT REPORTED THAT AFTER GEAR SELECTED DOWN ,THE NR 1 UTILITY SYSTEM FLUID AND PRESSURE DEPLETED. ALTERNATE EXTE NSION CARRIED OUT AND AIRCRAFT LANDED OK. FOUND NLG DOOR ACTUATOR CRACKED AND LEAKING FLUID. REPLACED. 2 L 7 2 4F RT A20EU 1999081200497 19990812 00497 CE 1999 8 12 CA990311002 1 19981208 A 7430 103572301 SWITCH BEECH 95 E95 1153410 CE LYC O360 IO360B1B 41514 EA IGNITION FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA L496351A (CAN) AFTER LEFT ENGINE WAS STARTED AND DURING THE MAG DROP TEST, ELECTRICAL SMELL WAS DETECTED AND ARCING COULD BE HEAR D. THE MAGNETO SWITCH WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. A SUBSEQUENT INSPECTION OF A MAGNETO SWITCH R EVEALED THAT IT WAS INTERNALLY SHORTED. NO RECORD OF WHEN THIS SWITCH WAS LAST REPLACED, BUT THE DATE ON THE SWITCH WAS 77-04. 1 L 7 2 3O 3 O 3A16 1E10 1999081200498 19990812 00498 CE 1999 8 12 CA990311003 1 19981229 A 3230 IS14818 MOTOR LAMBELECTRIC BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO MCAULY 2AF34C 2AF34C55 GL MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 309 126755 237775R 711344 (CAN) AFTER TAKEOFF, THE LANDING GEAR MOTOR FAILED TO RETRACT WHEN SELECTED. THE AIRCRAFT RETURNED TO AIRPORT WITHOUT I NCIDENT. THE LANDING GEAR MOTOR WAS FOUND AT FAULT AND WAS REPLACED. 1 L 7 2 3O 3 O RT 3A16 3E1 5 C P5EA 1999081200501 19990812 00501 SW 1999 8 12 CA990311007 1 19981223 A 3260 1EN16 SWITCH SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP NLG STICKING W L ABORTED APPROACH N FALSE WARNING AP APPROACH 1 CA P54143 (CAN) NOSE LANDING GEAR FAILED TO SHOW GREEN WHEN SELECTED DOWN. INVESTIGATION REVEALED DOWN MICROSWITCH FAILED. SWITC H REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 1999081200503 19990812 00503 SW 1999 8 12 CA990311009 1 19981223 A 2740 771516S WIRE DL5040M6 SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP HORIZONTAL STAB SHORTED W K NONE O OTHER IN INSP/MAINT 1 CA K041 P03551C (CAN) PITCH TRIM FAILED ACCOMPANIED WITH CIRCUIT BREAKER TRIPPING. WIRE NR 7715-16S FOUND SHORTED ADJACENT TO UPLIMIT S WITCH. 2 L 7 2 4T 4 T RT A8SW E4WE 1999081200506 19990812 00506 SW 1999 8 12 CA990311012 1 19981231 A 2721 2742004003 ACTUATOR 2746000049 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE RUDDER TAB WORN W A UNSCHED LANDING E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 CA P44663C 881750 (CAN) VIBRATION FELT IN THE RUDDER PEDALS DURING CRUISE. TAB ACTUATOR AS FOUND OUT OF LIMITS AND REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999081200516 19990812 00516 CE 1999 8 12 CA990311023 1 19981123 A 3213 50810318605 STRUT 115810000651 BEECH 99 B99 1154004 CE PWA PT6 PT6A28 EA MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4668 ALS3362 PCE40813 (CAN) DURING LPI INSPECTION AT OVERHAUL, CRACKS WERE FOUND IN SHARP RADIUS ON THE L/G PISTON ASSY'S TORQUE KNEE ATTACH L UG. 1 L 7 2 3T 4 T A14CE E4EA 1999081200517 19990812 00517 1999 8 12 CA990311024 4 19981126 A 3418 7956 SWITCH BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA WING CONTAMINATED W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA PCE41562 (CAN) AIRCRAFT WAS DEICED AND DISPATCHED. STALL WARNING CAME ON AND STAYED ON. AIRCRAFT RETURNED TO BASE AND GLYCOL WA S REMOVED FROM STALL SWITCH. AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 1999081200520 19990812 00520 CE 1999 8 12 CA990311027 1 19981203 A 2742 PM24 ACTUATOR 1153801111 BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA STANDBY TRIM INTERMITTENT W K NONE O OTHER IN INSP/MAINT 1 CA 5992 560 51808 (CAN) PILOT REPORTED STANDBY TRIM INTERMITTENT. IF STANDBY MOTOR WAS TAPPED ,THEN IT WOULD WORK. MOTOR REPLACED AND AI RCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 1999081200521 19990812 00521 EA 1999 8 12 CA990311028 2 19981208 A 7260 3029567 SHAFT BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA GEARBOX WORN W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 7357 PCE40262 (CAN) THE ENGINE WAS MAKING GRINDING SOUND EMITTING FROM THE AGB SECTION. INSPECTION FOUND THE CLIP ON THE STARTER /GEN ERATOR GEAR SHAFT THAT LOCKS THE IMPELLER TO THE SHAFT WAS NOT INSTALLED IN THE PROPER LOCATION. THE RETAINING RING WAS INSTALLED ON THE WRONG SIDE OF THE BREATHER ASSEMBLY. THE LOCK PINS WERE WORN AND THE BEARING WAS DAMAGED DUE TO THE IMP ELLER RUBBING AGAINST IT. 1 L 7 2 3T 4 T A14CE E4EA 1999081200523 19990812 00523 EA 1999 8 12 CA990311030 2 19981208 A 7250 3006888 HEAT SHIELD BEECH 99 B99 1154004 CE PWA PT6 PT6A27 52043 EA TURBINE SECTION LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA 202 PCE51331 (CAN) DURING POWER SECTION CHANGE, THE SEGMENTS WERE FOUND LOOSE. THE HEAT SHIELD WAS ALSO FOUND LOOSE, SO THAT THE HEA T SHIELD COULD ROTATE ON ITS CARRIER. THE SUBMITTER STATES THAT THIS CONDITION SHOULD NOT BE PRESENT ON AN ASSEMBLY ONL Y 202 HOURS OUT OF OVERHAUL. 1 L 7 2 3T 4 T A14CE E4EA 1999081200556 19990812 00556 NE 1999 8 12 CA990311063 2 19981208 A 7532 310334701 DIAPHRAGM 312124803 CESSNA 208 208B 2073701 CE PWA PT6 PT6A114A 52043 NE BLEED VALVE TORN W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 318 27A635 PCEPC0486 (CAN) DURING CLIMB,THERE WAS A NOTICEABLE POWER LOSS, HIGH T5, HIGH FUEL FLOW, WITH AN INCREASED NG. THE AIRCRAFT RETUR NED TO BASE. POST-FLIGHT INSPECTION FOUND THE BLEED VALVE DIAPHRAGM TORN. THE BLEED VALVE DIAPHRAGM PISTON SEAT BUSHIN G AND COVER WERE REPLACED IN ACCORDANCE WITH P&W TEMPORARY REVISION TR75-01 AND AFTER A SATISFACTORY TEST FLIGHT, THE AI RCRAFT WAS RETURNED TO SERVICE. 1 H 7 1 3T 3 T A37CE E4EA 1999081200561 19990812 00561 NE 1999 8 12 CA990311068 2 19981123 A 7200 ENGINE LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB21122B NE NR 2 MALFUNCTIONED W C ABORTED TAKEOFF E VIBRATION/BUFFET TO TAKEOFF 1 CA 10256 (CAN) ON TAKEOFF ROLL, NR 2 ENGINE VIBRATION WENT TO 3.3 UNITS. TAKEOFF ABORTED. A HIGH POWER RUN WAS CARRIED OUT ON T HE WAY BACK TO THE GATE AND THE VIBRATION WENT BACK TO WITHIN LIMITS WHEN THE ENGINE WARMED UP. THE AIRCRAFT WAS RETURN ED TO SERVICE. THE REPORT FROM ROLLS ROYCE, IN THE WAY OF AN EXPLANATION, WILL BE FAXED WHEN RECEIVED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200565 19990812 00565 WP 1999 8 12 CA990311074 1 19981202 A 7600 SM44A24 ROD 1608858107 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE NR 3 ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 10284 (CAN) ON INSPECTION OF NR 3 ENGINE PYLON,THE ROD END BEARING BETWEEN THE THROTTLE TORQUE SHAFT AND THE TENSION REGULATOR LEVER WAS FOUND WORN AND THE BEARING DESTROYED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200566 19990812 00566 WP 1999 8 12 CA990311075 1 19981224 A 2920 718048 TURBINE LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B NE RAM AIR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 10284 (CAN) AIR TURBINE MOTOR (RAM AIR TURBINE) INOPERATIVE. LIGHT CAME ON IN-FLIGHT. POST-FLIGHT INSPECTION FOUND OIL MISSI NG FROM THE RESERVOIR, OIL WAS ADDED AND DURING LEAK CHECK, SPARKS WERE SEEN COMING FROM THE EXHAUST. FURTHER INSPECTIO N FOUND THE TURBINE SHAFT SHEARED AND THE TURBINE DESTROYED. 2 L 7 3 4F 4 F A23WE E12EU 1999081200567 19990812 00567 NM 1999 8 12 CA990311077 1 19981117 A 2910 AS11506K0522 FLEX HOSE BOEING 757 757236 NM RROYCE RB211 RB211535E4 54555 NE HYDRAULIC SYSTEM RUPTURED W H DEACTIVATE SYST/CIRCUITS J WARNING INDICATION CR CRUISE 1 CA 30864 (CAN) EICAS MESSAGE LEFT HYDRAULIC QUANTITY WENT DOWN TO ZERO. LEFT ELECTRIC AND EDP SHUT DOWN. FOUND RIGHT GEAR TRUCK POSITIONER HYDRAULIC FLEX HOSE RUPTURED. REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200568 19990812 00568 NM 1999 8 12 CA990311078 1 19981122 A 5246 LJ75505 PANEL BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE NACELLE SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 30886 (CAN) RIGHT ENGINE OIL ACCESS PANEL MISSING AFTER FLIGHT. REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200569 19990812 00569 NM 1999 8 12 CA990311079 1 19981224 A 4950 271N64611220 DUCT BOEING 757 75728A 1384976 NM RROYCE RB211 RB211535E4 54555 NE APU CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA 30886 (CAN) EVIDENCE OF FOWLING BETWEEN STATIC AND APU BLEED DUCT IN THE AFT CARGO COMPARTMENT CAUSING DAMAGE TO INSULATION BL ANKET AROUND STRENGTHENER OF DUCTING. FOUND ON TWO AIRCRAFT. PIPING REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999081200571 19990812 00571 WP 1999 8 12 CA990311081 1 19981220 A 3232 269002121 ACTUATOR LKHEED 1011 1011385114 WP RROYCE RB211 RB21122B02 54555 NE MLG DOOR CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 10205 (CAN) PRIOR TO DEPARTURE, HYDRAULIC LEAK FROM RT MLG DOOR ACTUATOR. ACTUATOR CASING CRACKED. REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1999081400002 19990814 00002 EU 1999 8 14 99ZZZX2835 1 19981230 A 2620 WIRE BAG BAE146 BAE146200A 1500266 EU NR 2 ENGINE BROKEN A A6WA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 31 291UE E2084 DEN - FLT 661 - NR 2 EXTINGUISHER USED LT 'ON' ON NR 2 ENGINE. REPAIRED BROKEN WIRE AT TERMINAL STRIP AT FIRE BOTTLE. ( X) 2 H 7 4 4F RT A49EU 1999081400468 19990814 00468 WP 1999 8 14 99FDEA00320 1 19980220 A 5312 AJC70015 BULKHEAD WEB DOUG DC10 DC1010 3022110 WP BS 2163.685 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 N0222 - DURING A/C P-F CONVERSION AT OAN, FOUND A 0.50 IN CRACK IN THE CANTED BULKHEAD AT BS 2163.685. TRIMMED WEB TO R EMOVE CRACK AND INSTALLED A TITANIUM FILLER AND DOUBLER IAW EA NR 8-5310-35908. 2 L 7 3 4F A22WE 1999081400469 19990814 00469 WP 1999 8 14 99FDEA00321 1 19980220 A 5313 AJC7208 LONGERON DOUG DC10 DC1010 3022110 WP BS 2164 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 N0224 - DURING A/C P-F CONVERSION AT OAN, FOUND 5 INCH CRACK IN THE AFT BODY KEEL CAP, LONGERON 45 AT BS 2164. TRIMMED LONGERON 45 TO REMOVE DAMAGED SECTION AND INSTALLED A FILLER AND A 7075-T6511 SPLICE IAW EA NR 8-5310-39515. 2 L 7 3 4F A22WE 1999081400470 19990814 00470 WP 1999 8 14 99FDEA00322 1 19980325 A 5720 ARB0015502 SPLICE DOUG DC10 DC1010 3022110 WP WS 372 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 387FE 46621 N0337 - DURING A/C P-F CONVERSION AT OAN, FOUND A CRACK IN THE SPLICE PLATE P/N ARB0012-502 AT RT WING, XORS=372. REPAI R REQUIRES CUT OUT OF DAMAGED SPLICE PLATE AND INSTALLATION OF A 7075T8 REPAIR STRAP IAW EA NR 8-5711-39534. 2 L 7 3 4F A22WE 1999081400510 19990814 00510 WP 1999 8 14 EIA980379 2 19981228 A 7261 OIL SYTEM DOUG DC9 DC932F 3022067 WP GARRTT TPE331 TPE3311 01514 WP NR 2 ENGINE LEAKING A EIAA O OTHER K J FLUID LOSS WARNING INDICATION NR NOT REPORTED 1 NM 09 935F 47220 IN FLIGHT, NR 2 ENGINE OIL QTY DECREASED TO 0 DURING CRUISE, DIVERTED TO KCPR. AFTER LANDING FOUND OIL LEAKING FROM COW LING. (M) 2 L 7 2 4F 3 T A6WE E3WE 1999081400542 19990814 00542 GL 1999 8 14 99ZZZM425 2 19981214 A 7314 FUEL PUMP CVAC 340 34031 2422704 WP ALLSN 501D 501D13 03004 GL NR 2 ENGINE FAILED A RENA O OTHER J WARNING INDICATION AP APPROACH 1 WP 01 73126 53 CAE500792 ON APPROACH TO NUC, NR 2 ENGINE LOST HP PRIMARY FUEL PUMP FAILURE LIGHT ILLUMINATED, TIT INCREASED. SECURED ENGINE. 2 L 7 2 4R 4 T 6A6 E282 1999081400547 19990814 00547 EU 1999 8 14 99ZZZM426 1 19980629 A 7110 SKIN BAG BAE146 BAE146300A 1500267 EU NR 2 ENG COWL WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 NR 2 ENGINE LEFT AFT AFT COWL DOOR INNER SKIN WORN THROUGH. PATCHED ABOVE DAMAGE PER PSI USING TA2 AND CHERRYMAXNUETS. 2 H 7 4 4F RT A49EU 1999081400548 19990814 00548 EU 1999 8 14 99ZZZM427 1 19980619 A 3520 VALVE BAG BAE146 BAE146300A 1500267 EU ROW 2 DEF FAILED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 612AW E3122 CABIN OXYGEN MASKS AT RIGHT SIDE ROW 2 DEF VALVE PISTON FAIL TEST. REMOVED AND REPLACED VALVE AT SEAT 2 DEF, OPS CHECK GOOD. (M) 2 H 7 4 4F RT A49EU 1999081400549 19990814 00549 EU 1999 8 14 99ZZZM428 1 19980605 A 5320 INTERCOSTAL BAG BAE146 BAE146300A 1500267 EU FRAME 18 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 GUSSET PLATE AND FORWARD REST FLOOR SUPPORT INTERCOSTAL, LEFT OF CENTER, AT FRAME 18 IS CORRODED. INSTALLED NEW GUSSET PLATE. 2 H 7 4 4F RT A49EU 1999081400550 19990814 00550 EU 1999 8 14 99ZZZM429 1 19980605 A 5320 SILL BAG BAE146 BAE146300A 1500267 EU PAX DOORWAY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 FORWARD VESTIBULE, PAX AND SERVICE DOOR, SILL PLATE HAV SOME CORROSION AROUND SCREW HOLES AND OTHER SMALL AREAS. MINOR SURFACE CORROSION REMOVED FROM SILL PLATES, ALODINED AND PRIMED. (M) 2 H 7 4 4F RT A49EU 1999081400551 19990814 00551 EU 1999 8 14 99ZZZM430 1 19980605 A 3510 FITTING BAG BAE146 BAE146300A 1500267 EU COCKPIT OXY SYS LEAKING A A6WA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 31 612AW E3122 COCKPIT OXYGEN SYSTEM HAS A LEAK. FAILED LEAK CHECK. REMOVED AND REPLACED 'T' FITTING BETWEEN SUPPLY GAUGE AND PRESSUR E REDUCING VALVE UNDER RIGHT SIDE PANEL. COMPLIED WITH LEAK CHECK. ALL IAW MM. (M) 2 H 7 4 4F RT A49EU 1999081400552 19990814 00552 EU 1999 8 14 99ZZZM431 1 19980605 A 2710 CONTROL CABLE BAG BAE146 BAE146300A 1500267 EU RT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 THE CENTER FUSELAGE INTERCONNECT CABLES ARE CORRODED AT RIGHT WING ROOT. REMOVED AND REPLACED BOTH CENTER FUSELAGE INTE RCONNECT CABLES AND ADJUSTED IAW MM 27-11-00. W/CS GENERATED FOR FUNCTIONAL TEST OF AILERON CONTROLS AND DISCONNECT. ( M) 2 H 7 4 4F RT A49EU 1999081400553 19990814 00553 EU 1999 8 14 99ZZZM432 1 19980624 A 5250 DOOR BAG BAE146 BAE146300A 1500267 EU COCKPIT LACK OF LUBE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 COCKPIT DOOR DIFFICULT TO OPEN FROM CABIN SIDE. LUBED AND RESHIMMED DOOR, OPS CHECK OK. (M) 2 H 7 4 4F RT A49EU 1999081400554 19990814 00554 EU 1999 8 14 99ZZZM433 1 19980611 A 5720 ANGLE BAG BAE146 BAE146300A 1500267 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 RIGHT WING TE TOP SKIN STIFFENER AFT TAG ANGLE CRACKED AT LOWER FLANGE BETWEEN RIBS 5 AND 6 OF SHROUD. REMOVED AND REPL ACED AFT TAG ANGLE BETWEEN RIBS 5/6 FOR THE TOP SKIN STIFFENER. (M) 2 H 7 4 4F RT A49EU 1999081400555 19990814 00555 EU 1999 8 14 99ZZZM434 1 19980608 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 RIGHT WING TOP SKIN TE STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB 9, SHROUD AREA. REMOVED AND REPLACED STIFFENER PER SRM. (M) 2 H 7 4 4F RT A49EU 1999081400556 19990814 00556 EU 1999 8 14 99ZZZM435 1 19980608 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 OF SHROUD. REMOVED AND REPLACED STIFFENER PER SRM. (M) 2 H 7 4 4F RT A49EU 1999081400557 19990814 00557 EU 1999 8 14 99ZZZM436 1 19980521 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 RIGHT WING TE TOP SHROUD SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB 9. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 8/9 IAW BAE FAX NR JM/RJ0417-98. (M) 2 H 7 4 4F RT A49EU 1999081400558 19990814 00558 EU 1999 8 14 99ZZZM437 1 19980507 A 5320 BRACKET BAG BAE146 BAE146100A 1500260 EU FRAME 32 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 STRUCTURAL INSPECTION MLG BAY, POS N/A WEB AT FRAME 32, DETAILED VISUAL INSPECTION. PERFORMED DV ON WEB AT FRAME 32 IN LEFT AND RIGHT MLG BAY. FOUND CRACKED BRACKET RT MLG DOOR UPLOCK CVR, FOUND MINOR NICKS SURFACE WEB. 2 H 7 4 4F RT A49EU 1999081400559 19990814 00559 EU 1999 8 14 99ZZZM438 1 19980515 A 5320 INTERCOSTAL BAG BAE146 BAE146100A 1500260 EU FRAME 41-43 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 AFT VEST, UNDER FLOOR INTERCOSTAL BETWEEN FRAMES 41 AND 42 IS CRACKED, CENTER INTERCOSTAL, CRACK IS APPROX 2.5 TO 3 INCH ES LONG. COMPLIED WITH PATCH REPAIR IAW AIR WISC/BAE SRM STANDARD PRACTICES REF CHAPTER 51. COMPLIED WITH ALODINE, PRI MER AND PAINTING. (M) 2 H 7 4 4F RT A49EU 1999081400560 19990814 00560 EU 1999 8 14 99ZZZM439 1 19980519 A 2520 FLOOR STRIP BAG BAE146 BAE146100A 1500260 EU CABIN CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FLOOR STRIPS FOR FORWARD CABIN BULKHEADS NEED CLEANED, CORROSION REMOVED, PAINTED, ETC. CLEANED, REMOVED CORROSION ALOD INED, PRIMED, PAINTED, AND REATTACHED PHONELLIC STRIPS. (M) 2 H 7 4 4F RT A49EU 1999081400561 19990814 00561 EU 1999 8 14 99ZZZM440 1 19980520 A 5320 GUSSET BAG BAE146 BAE146100A 1500260 EU FRAME 15 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 2 GUSSET PLATES CORRODED LEFT SIDE FRAME 15 FLOORBEAM. REPLACED TWO GUSSET PLATES LEFT SIDE FRAME 15 FLOORBEAM. (M) 2 H 7 4 4F RT A49EU 1999081400562 19990814 00562 EU 1999 8 14 99ZZZM441 1 19980511 A 5320 SILL BAG BAE146 BAE146100A 1500260 EU PAX DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 PASSENGER DOOR SILL PLATE CORRODED FRAME 15. REMOVED AND REPLACED FORWARD PAX DOOR SILL PLATE. (M) 2 H 7 4 4F RT A49EU 1999081400563 19990814 00563 EU 1999 8 14 99ZZZM442 1 19980519 A 5320 SILL BAG BAE146 BAE146100A 1500260 EU SERVICE DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE, SERVICE DOOR SILL PLATE HAS SEVERAL SMALL SPOTS OF SURFACE CORROSION. REMOVED AND REPLACED SILL PLAT E WITH NEW. (M) 2 H 7 4 4F RT A49EU 1999081400564 19990814 00564 EU 1999 8 14 99ZZZM443 1 19980517 A 2520 BRACKET BAG BAE146 BAE146100A 1500260 EU CABIN SEAT CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE, STEW SEAT MOUNT BRACKETS ON 2ND AND 3RD INTERCOSTALS FROM LEFT SIDE ARE LIGHTLY CORRODED. REMOVED CO RROSION TREATED PRIMED AND PAINTED FORWARD F/A SEAT MOUNT BRACKETS. (M) 2 H 7 4 4F RT A49EU 1999081400565 19990814 00565 EU 1999 8 14 99ZZZM444 1 19980512 A 5400 RIB BAG BAE146 BAE146100A 1500260 EU NR 2 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 2 PYLON BOX STRUCTURE HAS A CRACK IN THE LOWER OUTBOARD FLANGE OF RIB NR 5 THAT IS APPROX .5 INCH LONG. NR 2 PYLON C RACK OF APPROX .5 INCH LONG IS ACCEPTABLE AND HAS BEEN REPORTED TO BAE RDO PER P/C HC646H9018. GENERATED W/C FOR REINSP ECTION. (M) 2 H 7 4 4F RT A49EU 1999081400566 19990814 00566 EU 1999 8 14 99ZZZM445 1 19980522 A 5412 BULKHEAD BAG BAE146 BAE146100A 1500260 EU NR 1 ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 1 ENGINE LEFT AFT COWL DOOR BULKHEAD AT VENT TUBE AREA CRACKED. REPAIRED CRACK IN FLANGE OF BULKHEAD BY PATCHING IAW BAE/AIR WISC SRM STANDARD PRACTICES. (M) 2 H 7 4 4F RT A49EU 1999081400567 19990814 00567 EU 1999 8 14 99ZZZM446 1 19980522 A 7110 DOOR BAG BAE146 BAE146100A 1500260 EU NR 1 ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 1 ENGINE AFT LEFT COWL DOOR SECOND STIFFENER ON LOWER SPLITTER ASSY CRACKED. REPLACED SECOND STIFFENER ON NR 1 ENGIN E LEFT COWL DOOR. (M) 2 H 7 4 4F RT A49EU 1999081400568 19990814 00568 EU 1999 8 14 99ZZZM447 1 19980512 A 2621 BRACKET BAG BAE146 BAE146100A 1500260 EU NR 3 ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 3 ENGINE NOSE COWL INBOARD FIREBOTTLE HAS ONE ATTACH BRACKET MOUNTED TO FIREWALL THAT IS CRACKED BADLY. REMOVED NR 3 NOSE AND TRANSFERRED DISCREPANCY TO W/C. (M) 2 H 7 4 4F RT A49EU 1999081400569 19990814 00569 EU 1999 8 14 99ZZZM448 1 19980522 A 7110 SKIN BAG BAE146 BAE146100A 1500260 EU NR 3 ENGINE DOOR CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 3 ENGINE AFT INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH. REPLACED PAN AND PATCHED SMALL AREA 2.25 BY 3.5 US ING TAZ PER PSI. (M) 2 H 7 4 4F RT A49EU 1999081400570 19990814 00570 EU 1999 8 14 99ZZZM449 1 19980522 A 7110 DOOR BAG BAE146 BAE146100A 1500260 EU NR 3 ENGINE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 3 ENGINE AFT INBOARD FAN DOOR LOWER DOOR SPLITTER AREA HAS CHAFED STIFFENER, 2ND FROM FORWARD. REPLACED ABOVE STIFFE NER PER SRM. (M) 2 H 7 4 4F RT A49EU 1999081400571 19990814 00571 EU 1999 8 14 99ZZZM450 1 19980521 A 7110 DOOR BAG BAE146 BAE146100A 1500260 EU NR 4 ENGINE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, STIFFENER AT FORWARD CORNER CHAFED BADLY. REPLACED NR 4 ENG INE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, STIFFENER AT FORWARD CORNER. (M) 2 H 7 4 4F RT A49EU 1999081400572 19990814 00572 EU 1999 8 14 99ZZZM451 1 19980521 A 7110 DOOR BAG BAE146 BAE146100A 1500260 EU NR 4 ENGINE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA 2ND STIFFENER FROM FORWARD CHAFED. REPLACED NR 4 ENGINE AFT OUTBOARD FAN DOOR LOWER DOOR SPLITTER AREA, 2ND STIFFENER FROM FORWARD. (M) 2 H 7 4 4F RT A49EU 1999081400573 19990814 00573 EU 1999 8 14 99ZZZM452 1 19980518 A 5280 PLATE BAG BAE146 BAE146100A 1500260 EU NLG DOOR WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 WHILE CMP/WITH SSI 52-82-101-WEAR WAS DICV'D ON BOTTOM AFT CORNERS OF NOSE GEAR DOORS WHERE THEY ABUT TAB ON SPADE DOOR. TAB IS ALSO WORN. MANUFACTURED 2 BUTMENT PLATES FOR LT/RT NOSEGEAR DOORS IAW BAE DRAWING HC528H0161. INSTALLED LT/RT NOSEGEAR DOOR ABUTMENT PLATES IAW AIR WISC/BAE STD PRACTICES OF SRM. SEE ADDITIONAL W/C FOR REPLACEMENT OF 'STOP'. (M ) 2 H 7 4 4F RT A49EU 1999081400574 19990814 00574 EU 1999 8 14 99ZZZM453 1 19980515 A 5320 HC536H0826004 BRACKET BAG BAE146 BAE146100A 1500260 EU FRAME 32 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 MLG DOOR UPLOCK COVER BRACKET ON THE RIGHT SIDE OF WEB AT FRAME 32 IN MLG BAY IS CRACKED. REPLACED SAID BRACKET P/N HC5 36H0826-000U. (M) 2 H 7 4 4F RT A49EU 1999081400575 19990814 00575 EU 1999 8 14 99ZZZM454 1 19980521 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER IN AREA BETWEEN RIBS 9/10 IS CRACKED AT FORWARD END. REPAIRED LEFT WI TH TE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 9/10 IAW BAE FAX NR JM/RJO417-98, REF REINSPECTION W/C 5020. (M) 2 H 7 4 4F RT A49EU 1999081400576 19990814 00576 EU 1999 8 14 99ZZZM455 1 19980521 A 5320 HC361J0137006 BRACKET BAG BAE146 BAE146100A 1500260 EU FUSELAGE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 ANGLE BRACKET, P/N HC361JO137-006 CRACKED. LOCATED AT RIGHT ECS DUCT FRAME 45 SUPPORT OVERTEMP SWITCH BRACKET. MANUFAC TURED BRACKET IAW AIR WISC/BAE SRM STANDARD PRACTICES. DRILLED TO FIT IAW BAE FAX JM/RJ 0418-98. ALODINED AND PRIMED. SEE ADDITIONAL W/C FOR BRACKET INSTALLATION. (M) 2 H 7 4 4F RT A49EU 1999081400577 19990814 00577 EU 1999 8 14 99ZZZM456 1 19980519 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 RIGHT WING TE SHROUD LOWER SKIN STIFFENER CLEATS CRACKED BETWEEN RIBS 8/9, AFT END OF STIFFENER. REPLACED BOTH CLEATS O F RT WING TE SHROUD LOWER SKIN STIFFENER, CLEATS CRACKED BETWEEN RIBS 8/9, AFT END. (M) 2 H 7 4 4F RT A49EU 1999081400578 19990814 00578 EU 1999 8 14 99ZZZM457 1 19980522 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 RIGHT WING TE LOWER SHROUD SKIN STIFFENER CRACKED BETWEEN RIB 7/8. REPLACED STIFFENER IN RIGHT WING TE LOWER SHROUD SKI N BETWEEN RIBS 7/8. (M) 2 H 7 4 4F RT A49EU 1999081400579 19990814 00579 EU 1999 8 14 99ZZZM458 1 19980521 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING TE TOP SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN RIBS 7/8. REPAIRED LEFT WING TE TOP SKIN STIF FENER BETWEEN RIBS 7/8 IAW BAE FAX NR JM/RJO417-98. REF W/C 5022 FOR REINSPECTION. (M) 2 H 7 4 4F RT A49EU 1999081400580 19990814 00580 EU 1999 8 14 99ZZZM459 1 19980521 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING TE SHROUD TO PSKIN STIFFENERS ARE CRACKED AT FORWARD END IN AREA BETWEEN RIBS 8/9. REPAIRED LEFT WING TE SHRO UD TO SKIN STIFFENER BETWEEN RIBS 8/9. (M) 2 H 7 4 4F RT A49EU 1999081400581 19990814 00581 EU 1999 8 14 99ZZZM460 1 19980520 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING TE SHROUD BOTTOM SKIN STIFFENER CLEATS ARE CRACKED IN AREA BETWEEN RIBS 8/9. REPLACED BOTH CLEATS AS PER POSI TIONS ABOVE USING BAE STANDARD PRACTICES AND PROCEDURES. (M) 2 H 7 4 4F RT A49EU 1999081400582 19990814 00582 EU 1999 8 14 99ZZZM461 1 19980522 A 2910 BRACKET BAG BAE146 BAE146100A 1500260 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 LEFT WING, FORWARD HYD LINE CLAMP BRACKET, RIB 5, CRACKED. REPLACED BRACKET. (M) 2 H 7 4 4F RT A49EU 1999081400583 19990814 00583 EU 1999 8 14 99ZZZM462 1 19980520 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 TOP RIGHT WING T/E SKIN STIFFENER TWIX WING RIBS 3/4 CRACKED AT AFT END. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFEN ER BETWEEN RIBS 3/4. (M) 2 H 7 4 4F RT A49EU 1999081400584 19990814 00584 EU 1999 8 14 99ZZZM463 1 19980520 A 5720 FALSE SPAR BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 RIGHT WING TE HAS TEMP REPAIR (STOP DRILL) TO CRACK IN FALSE SPAR CAP BETWEEN RIBS 7/8, NEEDS PERM REPAIR. REPAIRED RIG HT WING TE BETWEEN RIBS 7/8. (M) 2 H 7 4 4F RT A49EU 1999081400585 19990814 00585 EU 1999 8 14 99ZZZM464 1 19980521 A 5720 STIFFENER BAG BAE146 BAE146100A 1500260 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 RIGHT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 7/8. (M) 2 H 7 4 4F RT A49EU 1999081400586 19990814 00586 EU 1999 8 14 99ZZZM465 1 19980518 A 5311 FRAME BAG BAE146 BAE146100A 1500260 EU FRAME 18 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE, FORWARD END OF SEAT RAIL, INBOARD RIGHT FLOORBEAM AT FRAME 18 IS CORRODED. REMOVED SURFACE CORROSION FORWARD VESTIBULE FRAME 18 INBOARD SEAT RAIL RIGHT SIDE TREATED, PRIMED AND PAINTED. (M) 2 H 7 4 4F RT A49EU 1999081400587 19990814 00587 EU 1999 8 14 99ZZZM466 1 19980519 A 5311 FRAME BAG BAE146 BAE146100A 1500260 EU GALLEY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE, FLOOR PANEL (UNDER GALLEY UNIT) HAS SOME SURFACE CORROSION IN A COUPLE SPOTS ALONG AFT EDGE. REMOVED SURFACE CORROSION FORWARD VESTIBULE AT AFT EDGE OF GALLEY ASSY FRAME 15 TREATED AND PAINTED. (M) 2 H 7 4 4F RT A49EU 1999081400588 19990814 00588 EU 1999 8 14 99ZZZM467 1 19980519 A 5320 GUSSET BAG BAE146 BAE146100A 1500260 EU FRAME 15 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE, GUSSET PLATE ON FLOORBEAM AT FRAME 15 AND 2ND INTERCOSTAL FROM RIGHT SIDE HAS SOME SURFACE CORROSION AND APPEARS TO BE MADE OF TOO THIN OF MATERIAL AREA IS MARKED WITH BLACK PEN. REPLACED GUSSET PLATE FORWARD VESTIBULE F RAME 15 2ND INTERCOSTAL FROM RIGHT. (M) 2 H 7 4 4F RT A49EU 1999081400589 19990814 00589 EU 1999 8 14 99ZZZM468 1 19980519 A 5320 GUSSETT BAG BAE146 BAE146100A 1500260 EU FUSELAGE CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE, CENTER GUSSET PLATE ON THE 2ND INTERCOSTAL FROM RIGHT SIDE IS CORRODED. REPLACED FORWARD VESTIBULE G USSET PLATE CENTER ON NR 2 INTERCOSTAL FROM RIGHT. (M) 2 H 7 4 4F RT A49EU 1999081400590 19990814 00590 EU 1999 8 14 99ZZZM469 1 19980519 A 5315 FLOORBEAM BAG BAE146 BAE146100A 1500260 EU FRAME 15 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE FLOORBEAM AT FRAME 15 HAS A SMALL SPOT OF CORROSION APPROX 5 INCHES OUTBOARD OF 3RD INTERCOSTAL FROM L EFT SIDE, INLINE WITH CLOSET WALL AT C/PIT ENTRANCE AND IS MARKED WITH BLACK PEN. BLENDED AREA TO LIMITS AND SURFACE TR EATMENT AS PER BAE SRM. (M) 2 H 7 4 4F RT A49EU 1999081400591 19990814 00591 EU 1999 8 14 99ZZZM470 1 19980521 A 3520 MASK BAG BAE146 BAE146100A 1500260 EU CABIN TORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 CAIN OXYGEN MASKS FOR PASSENGERS FILTERS TORN SEAT 3A, 10B, 12A, 12B, 14C, 15C, 13E, 10F. REMOVED AND REPLACED FILTER T O PER COMPONENT MM TO 3A, 10B, 12A, 12B, 14C, 15C, 13E, 10F. (M) 2 H 7 4 4F RT A49EU 1999081400592 19990814 00592 EU 1999 8 14 99ZZZM471 1 19980523 A 5210 HANDLE BAG BAE146 BAE146100A 1500260 EU PAX DOOR OUT OF ADJUST A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD PAX DOOR, SLIDE ARMING HANDLE HITS THE HANDLE RECESS NOT ALLOWING THE GIRT BAR TO FULLY ENGAGE INTO LUGS. REMOV ED UPPER DOOR COVER AND ARMING HANDLE RECESS RECONTURED RECESS PAINTED AND REINSTALLED RECESS AND UPPER DOOR COVER, OPS CHECKED GOOD. (M) 2 H 7 4 4F RT A49EU 1999081400593 19990814 00593 EU 1999 8 14 99ZZZM472 1 19980521 A 5312 BULKHD LONGERON BAG BAE146 BAE146100A 1500260 EU MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FRAME 29 MAIN LANDING GEAR BAY ROOF PRESSURE BULKHEAD, LONGERONS NR 3, NR 9, NR 15 CRACKED. REPAIRED PRESS BULKHEAD LON GERONS NR 3, NR 9, AND NR 15 PER REPAIR DRAWING HC536H9211 AND SRM, AND FAX'S NUMBERED D-JH/R-JO419-98, D-JH/R-J0421-98, AND D-JH/R-J0422-98 ALL DATED 21 MAY, 1998, AND FAX D-JR/R-J0207-97 DATED 21 MAY, 1998, AND FAX D-JR/R-JO207-97 DATED 2 6 FEB 1997. (M) 2 H 7 4 4F RT A49EU 1999081400594 19990814 00594 EU 1999 8 14 99ZZZM473 1 19980514 A 2540 SPRING BAG BAE146 BAE146100A 1500260 EU TRASH BIN FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 FORWARD VESTIBULE TRASH BIN DOOR ASSY, NEEDS CLEANED. ANGLE REPAIR, DOOR SPRINGS, ETC. REMOVED AND REPLACED SPRINGS. R EPAIRED ANGLE AND CLEANED AND INSPECTED. (M) 2 H 7 4 4F RT A49EU 1999081400595 19990814 00595 EU 1999 8 14 99ZZZM474 1 19980811 A 7110 FRAME BAG BAE146 BAE146200A 1500266 EU NR 1 ENGINE COWL CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 1 ENGINE FORWARD RIGHT COWL DOOR, LOWER AFT FRAME CHAFED NEAR LATCH. REPAIRED NR 1 ENGINE RIGHT FORWARD COWL DOOR LO WER AFT FRAME IAW SRM 54-10-11. (M) 2 H 7 4 4F RT A49EU 1999081400596 19990814 00596 EU 1999 8 14 99ZZZM475 1 19980818 A 2910 BRACKET BAG BAE146 BAE146200A 1500266 EU RT HYD SYSTEM CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT WING TE LOWER HYDRAULIC LINE BRACKET CRACKED AT RIB NR 5. REMOVED BRACKET AND FABRICATED NEW BRACKET PER DRAWING HC9 32H0211. INSTALLED BRACKET AND ATTACHED LINES TO BRACKET. (M) 2 H 7 4 4F RT A49EU 1999081400597 19990814 00597 EU 1999 8 14 99ZZZM476 1 19980818 A 5720 RIVET BAG BAE146 BAE146200A 1500266 EU RT WING LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT WING TE SHROUD TOP STIFFENER BETWEEN RIB 4/5 HAS LOOSE RIVET, AFT END. REMOVED AND REPLACED LOOSE RIVET. (M) 2 H 7 4 4F RT A49EU 1999081400598 19990814 00598 EU 1999 8 14 99ZZZM477 1 19980818 A 5755 MOUNT BAG BAE146 BAE146200A 1500266 EU RT SPOILER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT LIFT SPOILER VALVE MOUNT PLATE CRACKED. REPLACED MOUNT PLATE. (M) 2 H 7 4 4F RT A49EU 1999081400599 19990814 00599 EU 1999 8 14 99ZZZM478 1 19980818 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 5/6. REMOVED AND REPLACED RIGHT WING TE SHROUD T OP STIFFENER. (M) 2 H 7 4 4F RT A49EU 1999081400600 19990814 00600 EU 1999 8 14 99ZZZM479 1 19980814 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 TE RIGHT WING TOP SHROUD STIFFENER OUTBOARD CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED RIGHT WING TRAILING EDGE S HROUD TO STIFFENER BETWEEN RIBS 8/9. (M) 2 H 7 4 4F RT A49EU 1999081400601 19990814 00601 EU 1999 8 14 99ZZZM480 1 19980821 A 5720 SCREW BAG BAE146 BAE146200A 1500266 EU RT WING DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT WING SHORT STALL BAR PULLING OVER CORNER MOUNT SCREWS. REPAIRED SCREWS AS REQ'D IAW AVRO FAX DJR/RJO638-98, GCB/R J1344-94, JEN/RJ1331-94. OK FOR SERVICE IAW BAE 146 MM. (M) 2 H 7 4 4F RT A49EU 1999081400602 19990814 00602 EU 1999 8 14 99ZZZM481 1 19980817 A 5751 BEARING BAG BAE146 BAE146200A 1500266 EU RT AILERON WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT AILERON OUTBOARD HINGE 'A' FRAME BEARINGS WORN. REMOVED AND REPLACED RIGHT AILERON OUTBOARD 'A' FRAME. W/C GEN F OR FUNCTIONAL CHECK. (M) 2 H 7 4 4F RT A49EU 1999081400603 19990814 00603 EU 1999 8 14 99ZZZM482 1 19980814 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT WING TE SHROUD TOP STIFFENER CRACKED AT FORWARD END AND RIVET POPPED (AFT END) BETWEEN RIBS 3/4. REPLACED RIGHT W ING TRAILING EDGE SHROUD TOP STIFFENER BETWEEN RIBS 3/4. (M) 2 H 7 4 4F RT A49EU 1999081400604 19990814 00604 EU 1999 8 14 99ZZZM483 1 19980812 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 LEFT WING TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8 IS CRACKED AT FORWARD END. REMOVED AND REPLACED TOP SKIN STIFFENER AFT OF REAR SPAR BETWEEN RIBS 7/8. (M) 2 H 7 4 4F RT A49EU 1999081400605 19990814 00605 EU 1999 8 14 99ZZZM484 1 19980818 A 2910 BRACKET BAG BAE146 BAE146200A 1500266 EU RT HYD SYSTEM CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT WING TE TOP HYDRAULIC LINE CLAMP BRACKET CRACKED RIB NR 6. REMOVED AND REPLACED BRACKET. (M) 2 H 7 4 4F RT A49EU 1999081400606 19990814 00606 EU 1999 8 14 99ZZZM485 1 19980813 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FRAME 20 DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 COMPLIED WITH REPAIR OF 2 DENTS AT FRAME 20, STRINGER 20, PORT SIDE IAW SRM 53-00-12 FIG 202 WITHIN 3000 CYCLES, CURRENT CYCLES 29320, DUE BY 32320 CYCLES. REPAIRED DENTS IAW BAE FAX REF DJR/RJO595-98. (M) 2 H 7 4 4F RT A49EU 1999081400607 19990814 00607 EU 1999 8 14 99ZZZM486 1 19980819 A 5321 FLOOR BAG BAE146 BAE146200A 1500266 EU CARGO COMPT BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 NR 4 LEFT BIN FLOOR NEEDS OVERLAY. REPAIRED COMPOSITE STRUCTURE IAW DRAWING AW-25-20-9804-06 OF PS-1, COMPLETED WEIGHT CHANGE NOTIFICATION FORM (ATTACHED) AND TRANSFERRED TESTING STEPS 1-4 FROM ABOVE DRAWING TO ANOTHER WORK CARD. (M) 2 H 7 4 4F RT A49EU 1999081400608 19990814 00608 EU 1999 8 14 99ZZZM487 1 19980314 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 (OUTBOARD STIFFENER). REPLACED RT WING TRAILIN G EDGE TOP SKIN STIFFENER BETWEEN RIB 7/8. (M) 2 H 7 4 4F RT A49EU 1999081400609 19990814 00609 EU 1999 8 14 99ZZZM488 1 19980311 A 5755 MOUNT BAG BAE146 BAE146200A 1500266 EU RT SPOILER CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING ROOT, LIFT SPOILER CONTROL VALVE MOUNT PLATE CRACKED. REMOVED AND REPLACED PLATE. (M) 2 H 7 4 4F RT A49EU 1999081400610 19990814 00610 EU 1999 8 14 99ZZZM489 1 19980313 A 5720 FALSE SPAR BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING TE FALSE SPAR CRACKED JUST INBOARD OF INBOARD LIFT SPOILER JACK. REPAIRED PER FAX JM/RJ0240-98, PER DRAWING HC572H9036. OPPOSITE HAND TO DRAWING. (M) 2 H 7 4 4F RT A49EU 1999081400611 19990814 00611 EU 1999 8 14 99ZZZM490 1 19980317 A 5350 ATTACH LINKS BAG BAE146 BAE146200A 1500266 EU RT WING CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING TO FUSELAGE AFT ATTACH LINKS HAVE SURFACE CORROSION ON ENDS (PAINT MISSING). CLEANED, PRIMED AND PAINTED END S. (M) 2 H 7 4 4F RT A49EU 1999081400612 19990814 00612 EU 1999 8 14 99ZZZM491 1 19980317 A 2710 PULLEY BAG BAE146 BAE146200A 1500266 EU RT WING SEIZED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING LOWER AILERON TRIM CABLE PULLEY SEIZED OUTBOARD OF NR 4 FLAP TRACK. REMOVED AND REPLACED TRIM CABLE PULLEY'S AS NEEDED IAW MM. (M) 2 H 7 4 4F RT A49EU 1999081400613 19990814 00613 1999 8 14 99ZZZM492 4 19980325 A 3418 STALL BAR BAG BAE146 BAE146200A 1500266 EU RT WING OUT OF POSITION A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING SHORT SECTION OF STALL BAR PULLING OVER CORNER SCREWS. REMOVED LEFT WING STALL TRIGGER AND REPAIR PER FAX RE F DJH/R JO268 USING FAX GCB/RJ1344-94 AND REINSTALLED STALL TRIGGER. (M) 2 H 7 4 4F RT A49EU 1999081400614 19990814 00614 EU 1999 8 14 99ZZZM493 1 19980624 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 FUSELAGE SKIN CHAFED APPROX 13 INCHES LONB BY FORWARD RIGHT WING ROOT FAIRING BETWEEN FRAMES 25/26. REF W/C 6075 FOR BL END AND NDT. FIT EXTERNAL PATCH OVER CHAFED AREA UNDER RT WING ROOT FAIRING ON FUSELAGE SKIN BETWEEN FRAMES 25/26 PER S RM 53-00-12 FIGURE 201 INC STRINGERS ABOVE AND BELOW CHAFE PER FAX REF DJH/RJO248-98. (M) 2 H 7 4 4F RT A49EU 1999081400615 19990814 00615 EU 1999 8 14 99ZZZM494 1 19980311 A 5280 DOOR BAG BAE146 BAE146200A 1500266 EU RT MLG DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT MLG DOOR LOWER FORWARD CORNER IS DEFORMED OUTWARD APPROX .167 FROM CONTOUR, APPROX 3.55 IN LENGTH. REPAIRED IAW B AE SRM 52-81-11, FIG 204, TYPE 2. (M) 2 H 7 4 4F RT A49EU 1999081400616 19990814 00616 EU 1999 8 14 99ZZZM495 1 19980227 A 5320 BRACKET BAG BAE146 BAE146200A 1500266 EU MLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 UPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM HAS A CRACK. REPLACED UPPER ATTACH ANGLE BRACKET FOR MLG BAY DIAPHRAM. (M) 2 H 7 4 4F RT A49EU 1999081400617 19990814 00617 EU 1999 8 14 99ZZZM496 1 19980309 A 5230 SEAL BAG BAE146 BAE146200A 1500266 EU CARGO DOOR DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 REAR CARGO DOOR LOWER SEAL CAGE IS BENT, DEFORMED IN SEVERAL AREAS. REPLACED REAR CARGO DOOR LOWER SEAL CAGE. (M) 2 H 7 4 4F RT A49EU 1999081400618 19990814 00618 EU 1999 8 14 99ZZZM497 1 19980313 A 5280 SKIN BAG BAE146 BAE146200A 1500266 EU LT MLG DOOR CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 LEFT MLG DOOR INTERNAL SKIN FORWARD EDGE APPROX 1ST 6 INCHES FROM TOP EDGE HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN G EAR IS UP AND LOCKED. TRANSFER TO W/O BX1879 FOR REPAIR. (M) 2 H 7 4 4F RT A49EU 1999081400619 19990814 00619 EU 1999 8 14 99ZZZM498 1 19980317 A 5280 SKIN BAG BAE146 BAE146200A 1500266 EU RT MLG DOOR CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT MLG DOOR INTERNAL SKIN, FORWARD EDGE, APPROX 1ST 6 INCHES DOWN HAS EVIDENCE OF CHAFING ON FRAME NR 29 WHEN L/G IS UP AND LOCKED. BLENDED OUT CHAF IN DRUM, MINOR DAMAGE WITHIN LIMITS, PRC COATED FOR ABRASION. (M) 2 H 7 4 4F RT A49EU 1999081400620 19990814 00620 EU 1999 8 14 99ZZZM499 1 19980316 A 5720 BOLTS BAG BAE146 BAE146200A 1500266 EU LT WING LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 PERFORM RIL HC571H9033 LT RIB 2 OUTBOARD JOBOLTS. PERFORMED RIL HC571H9033 ON LEFT RIB 2 OUTBOARD JOBOLTS. (M) 2 H 7 4 4F RT A49EU 1999081400621 19990814 00621 EU 1999 8 14 99ZZZM500 1 19980326 A 5720 BOLTS BAG BAE146 BAE146200A 1500266 EU RIB 0 & 2 LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 FOUND LOOSE JOBOLTS AT VARIOUS LOCATIONS AT WING TANK RIB '0' AND RIB 2 LT/RT. COMPLETED LOOSE JOBOLT REPLACEMENT AT RI B 0 AND RIB 2 LT/RT PER RIL HC571H9033. NOTE, 6 POSITIONS WERE OVERSIZED. 2 H 7 4 4F RT A49EU 1999081400622 19990814 00622 EU 1999 8 14 99ZZZM501 1 19980312 A 2722 BOLT BAG BAE146 BAE146200A 1500266 EU RUDDER ACT SCRATCHED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 UPPER RUDDER ACTUATOR AFT ATTACHMENT BOLT HAS SCRATCH THAT GOES BELOW PLATING. REMOVED AND REPLACED UPPER RUDDER ACTUAT OR AFT ATTACHMENT BOLT IAW AMM. (M) 2 H 7 4 4F RT A49EU 1999081400623 19990814 00623 EU 1999 8 14 99ZZZM502 1 19980319 A 5755 BOLT BAG BAE146 BAE146200A 1500266 EU RT AIRBRAKE WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT AIRBRAKE UPPER ATTACH POINT BOLT PLATING IS WORN OFF, BOLT WAS FROZEN IN BEARING. REMOVED AND REPLACED HINGE PIN AND BUSH. INSTALLED DURING AIRBRAKE INSTALLATION. SEE W/C NR 3019 FOR INSTALLATION. (M) 2 H 7 4 4F RT A49EU 1999081400624 19990814 00624 EU 1999 8 14 99ZZZM503 1 19980305 A 2730 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU ELEVATOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 LEFT AND RIGHT ELEVATOR CABLES ARE CORRODED AT PULLEYS IN VERTICLE STAB. REMOVED AND REPLACED LEFT AND RIGHT ELEVATOR C ABLES FROM REAR PRESS BULKHEAD TO COMPENSATORS AND ADJUSTED IAW MM 27-31-00. W/C GENERATED FOR FUNCTION TEST. (M) 2 H 7 4 4F RT A49EU 1999081400625 19990814 00625 EU 1999 8 14 99ZZZM504 1 19980311 A 5540 BEARING BAG BAE146 BAE146200A 1500266 EU RUDDER WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RUDDER TOP 'A FRAME HINGE POINT HAS A BAD BEARING. 'A' FRAME REMOVED FOR REPAIR. INSTALLED SERVICEABLE RUDDER TOP 'A' FRAME IAW BAE MM. (M) 2 H 7 4 4F RT A49EU 1999081400626 19990814 00626 EU 1999 8 14 99ZZZM505 1 19980305 A 5540 BEARING BAG BAE146 BAE146200A 1500266 EU RUDDER WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RUDDER BEARING BAD AT MAIN (RIB 6) 'A' FRAME SUPPORT. ALLOW AND EXCESSIVE UP AND DOWN FLOAT OF RUDDER ASSY .25 INCH APP ROX. REMOVED AND REPLACED RUDDER MAIN 'A' FRAME (RIB 6) HINGE BEARING. (M) 2 H 7 4 4F RT A49EU 1999081400627 19990814 00627 EU 1999 8 14 99ZZZM506 1 19980310 A 2710 CABLE GUARD BAG BAE146 BAE146200A 1500266 EU RT AILERON SEIZED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING ROOT, OUTBOARD CABLE GAURD SEIZED AND BOTH PULLEYS WORN FOR CENTER SECTION AILERON INTERCONNECT CABLES. REMO VED AND REPLACED PULLEYS EXTRACTED SEIZED GUARD AND REPLACED WITH NEW GUARD, RIGHT WING ROOT. (M) 2 H 7 4 4F RT A49EU 1999081400628 19990814 00628 EU 1999 8 14 99ZZZM507 1 19980324 A 5312 BULKHEAD STRIP BAG BAE146 BAE146200A 1500266 EU LAVATORY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 FORWARD LAVATORY BULKHEAD I2109 LOWER METAL STRIP ON BOTTOM OF BULKHEAD IS CORRODED. INSTALLED LOWER METAL STRIP ON FOR WARD LAVATORY BULKHEAD I2109 OLD UNIT PREVIOUSLY REMOVED. (M) 2 H 7 4 4F RT A49EU 1999081400629 19990814 00629 EU 1999 8 14 99ZZZM508 1 19980310 A 2710 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU RT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING AILERON INTERCONNECT CABLES AT WING ROOT PULLEY CORRODED. REMOVED AND REPLACED FUSELAGE INTERCONNECT CABLES (AILERON) IAW BAE MM. GENERATED WC TO PERFORM AILERON FUNCTIONAL CHECK AND PRI 2 WC TO RE-CHECK TENSION AT 4000 FLT INT ERVAL. (M) 2 H 7 4 4F RT A49EU 1999081400630 19990814 00630 EU 1999 8 14 99ZZZM509 1 19980304 A 5320 SILL BAG BAE146 BAE146200A 1500266 EU PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 AFT PASSENGER DOOR, AFT SIDE OF DOOR SILL PLATE IS CRACKED ABOUT 1 INCH LONG. REMOVED DAMAGED SILL PLATE, DRILLED AND F ITTED NEW SILL PLATE ON AFT PASSENGER DOOR, AFT SIDE INSTALLED NEW SILL PLATE AND PAINTED RIVET HEADS AND BUCKTAILS. (M ) 2 H 7 4 4F RT A49EU 1999081400631 19990814 00631 EU 1999 8 14 99ZZZM510 1 19980310 A 2710 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU LT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 LEFT CLAD INTERCONNECT CABLE FOR AILERONS SHOWS EVIDENCE OF CORROSION AT DIFFERENTIAL SECTOR BETWEEN RIBS 14/15. REMOVE D AND REPLACED LEFT CLAD INTERCONNECT CABLE (AILERON) IAW BAE MM. GENERATED W/C TO PERFORM AILERON FUNCTIONAL CHECKS AN D PRIORITY 2 WC TO RECHECK TENSION AT 4000 FLT INTERVAL. (M) 2 H 7 4 4F RT A49EU 1999081400632 19990814 00632 EU 1999 8 14 99ZZZM511 1 19980324 A 2612 WIRE BAG BAE146 BAE146200A 1500266 EU FIRE WARNING BROKEN A A6WA K NONE L NO TEST TX TAXI/GRND HDL 1 GL 31 609AW E2070 NR 1 ENGINE POWER LEVER FIRE WARNING LIGHT DOES NOT ILLUMINATE DURING FIRE TEST, WIRE BAD. REMOVED AND REPLACED BOTH WI RES IN POWER LEVER FIRE WARNING. TESTED PER MM. (M) 2 H 7 4 4F RT A49EU 1999081400633 19990814 00633 EU 1999 8 14 99ZZZM512 1 19980404 A 3260 WARNING UNIT BAG BAE146 BAE146200A 1500266 EU LANDING GEAR MALFUNCTIONED A A6WA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 610AW E2082 AFTER TAKEOFF RAISING GEAR RED LIGHT IN HANDLE REMAINED ON. REMOVED AND REPLACED AUDIBLE WARNING UNIT, OPS CHECKED GOOD ON CHECK FLIGHT. (M) 2 H 7 4 4F RT A49EU 1999081400634 19990814 00634 EU 1999 8 14 99ZZZM513 1 19980412 A 3260 RELAY BAG BAE146 BAE146200A 1500266 EU RT MLG FAILED A A6WA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 31 610AW E2082 RED LIGHT ON GEAR HANDLE REMAINED ON AFTER GEAR RET. RETURNED FOR LANDING, RED LIGHT OUT WITH GEAR HANDLE DOWN. REPLAC ED RELAYS GF6 NLG UPLOCK AND GF7 RIGHT MLG UPLOCK, RETRACTED GEAR 4 TIMES, GEAR INDICATED NORMALLY. (M) 2 H 7 4 4F RT A49EU 1999081400635 19990814 00635 EA 1999 8 14 99ZZZM514 2 19980425 A 7230 COMPRESSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502* 41580 EA NR 4 ENGINE STALLED A A6WA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 31 610AW E2082 ON CLIMB-OUT NR 4 ENGINE MADE 2 MUFFLED 'BANGS' AND N1, N2, TGT, STARTED DROPPING. SENT ATW MX TO ORD, LOCKED DOWN ENGI NE AND FERRIED TO ATW. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1999081400636 19990814 00636 1999 8 14 99ZZZM515 4 19980427 A 2565 D31050105 SLIDE BAG BAE146 BAE146100A 1500260 EU NR 1 DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 1 ESCAPE SLIDE PACK BOARD CRACKED AT HINGE POINT (APPROX 5 INCHES) MRR NEEDS FILE. REMOVED AND REPLACED NR 1 SLIDE A SSY PERFORMED COVER PULL TEST AND FOUND SERVICEABLE. UPDATED BATTERY EFF CHECKED FOR INSTALLED SLIDE S/N 0238. DOOR AR M CHECK C/W. NO DEFECTS NOTED, S/N OFF 0415, S/N ON 0238. (M) 2 H 7 4 4F RT A49EU 1999081400637 19990814 00637 EU 1999 8 14 99ZZZM516 1 19980427 A 2620 BRACKET BAG BAE146 BAE146100A 1500260 EU NR 1 FIRE BOTTLE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 1 MOTOR INBOARD FIRE BOTTLE BRACKET CRACKED AT STRAP ATTACHMENT AREA. REPLACED CRACKED FIRE BOTTLE BRACKET INBOARD O N NR 1 ENGINE. (M) 2 H 7 4 4F RT A49EU 1999081400638 19990814 00638 EU 1999 8 14 99ZZZM517 1 19980427 A 2620 WIRE BAG BAE146 BAE146100A 1500260 EU NR 1 FIRE BOTTLE CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 463AP E1063 NR 1 MOTOR OUTBOARD FIRE BOTTLE DISCHARGE INDICATION WIRES ARE CHAFED, BOTTLE NEEDS CHANGED. CHANGED NR 1 OUTBOARD FIRE BOTTLE DUE TO CHAFED WIRES. S/N OFF CK6766M, S/N ON CK6767M. (M) 2 H 7 4 4F RT A49EU 1999081400639 19990814 00639 EU 1999 8 14 99ZZZM518 1 19980413 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU FRAME 12-18 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 DV INSPECTION FLOORBEAMS AND SUPPORT STRUCTURE FRAME 12 TO 18 W/VEST FLOOR PANELS ONLY REMOVED SII. REPORT FINDINGS FOR M M046 (SII 53-10-128) ACCESS 221DF, 221EF, 221FF, 221HF222AF. PERFORMED DV INSPECTION FLOORBEAMS AND SUPPORT STRUCTURE FRAME 12-18, FOUND CORROSION ON FORWARD PAX DOOR SILL PLATES 1ST SCREWHOLE AND CORROSION 2 GUSSET PLATE. (M) 2 H 7 4 4F RT A49EU 1999081400640 19990814 00640 EU 1999 8 14 99ZZZM519 1 19980415 A 5230 SKIN BAG BAE146 BAE146200A 1500266 EU CARGO DOOR DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 REPAIR DENTS IN FORWARD CARGO DOOR WITHIN 500 CYCLES. CURRENT TAC 34819, DUE AT 35319 TAC. REPAIRED DENTS IN FORWARD C ARGO DOOR PER BAE FAX DJH/RJ0311-98 AND SRM 52-32-11 FIG 201. GEN W/C TO ACCESS OTHER DENTS ON FORWARD CARGO DOOR. (M) 2 H 7 4 4F RT A49EU 1999081400641 19990814 00641 EU 1999 8 14 99ZZZM520 1 19980417 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 PERFORM DV INSPECTION OF LIGHTNING STRIKE DAMAGE CRACK AT LEFT FUSE FRAME 26 JUST UNDER JACK PAD. REF FAX DJR/RJO134-98 , REPORTING ADVERSE FINDINGS TO RDO BEFORE FLIGHT. DUE EACH 60 CYCLES, CURRENT CYCLES 35012, DUE BY 35072. BLENDED CRA CK IAW BAE FAX DJR/RJO325-98. W/C GEN FOR CONTINUED INSPECTION AT 400 FLT INTVLS. PERFORMED ET ON ABOVE BLENDED AREA. (M) 2 H 7 4 4F RT A49EU 1999081400642 19990814 00642 EU 1999 8 14 99ZZZM521 1 19980406 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 REF SRM 53-00-00 PAGE 104 FIG 101 ZONE B. REINSPECTED DENT BETWEEN FRAME 19 AND 20 ON RIGHT FUSELAGE ABOVE LAP JT EACH 300 CYCLES. CURRENT CYCLES 35012, DUE BY 35312. REPAIRED IAW BAE SRM 53-00-12 FIG 202. DENT AT FRAME 20-20A. NO FURT HER REINSPECTION REQ'D. (M) 2 H 7 4 4F RT A49EU 1999081400643 19990814 00643 EU 1999 8 14 99ZZZM522 1 19980420 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 REF AVRO FAX DJR/RJ1182-96, C/W DV INSPECTION OF TWO SHALLOW DENTS ON FORWARD RIGHT FUSELAGE AT FRAME 8, 55 INCHES BELOW HORIZONTAL DATUM. REINSPECTED EVERY 3000 CYCLES, REPORT ANY ADVERSE FINDINGS TO BAE PRIOR TO FLT. CURRENT TC 34450, D UE BY 37450 TC. REPAIRED DENTS IAW BAE FAX REF DJH/RJO335-98 AND BAE SRM 53-10-12 FIG 202. (M) 2 H 7 4 4F RT A49EU 1999081400644 19990814 00644 EU 1999 8 14 99ZZZM523 1 19980423 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 REF FAX DJR/RJO841-97, LIGHTNING STRIKE SKIN DAMAGE DETAILED IN AWAC FAC LM244-97 TO BE REPAIRED 35375 TCA OR NEXT HEAVY CHECK RUBBINGS SUBMITTED AVRO 11-24-97. REPAIRED LIGHTNING STRIKE DAMAGE FRAMES 10, 12 AND 16. ALL OTHER AREAS HAVE B EEN P/C/W. GEN W/C TO REINSPECT AT FRAME 16 AND 26. REF FAX JM/RJ0348-98 ISS 2. W/C GEN FOR CONDUCTIVITY CHECKS AND E DDY CURRENT TESTS AROUND AREAS FRAME 48-98 ISS 2. W/C GEN FOR CONDUCTIVITY CHECKS AND EDDY CURRENT TESTS AROUND AREAS. (M) 2 H 7 4 4F RT A49EU 1999081400645 19990814 00645 EU 1999 8 14 99ZZZM524 1 19980415 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FRAME 35 DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 REINSPECT FUSELAGE DENT 6 INCHES FORWARD OF FRAME 35, AT STRIGNER 22 RIGHT, JUST BELOW FLEET NUMBER, CURRENTLY A CLASS A DENT. REINSPECTED EVERY 3000 FLIGHTS. CURRENT TCA 33234. REINSPECT BY 36234. REPAIRED DENT IAW BAE SRM 53-00-12 FIG URE 202. NO FURTHER REINSPECTS REQ'D. (M) 2 H 7 4 4F RT A49EU 1999082000088 19990820 00088 SW 1999 8 20 99ZZZX3032 1 19981022 A 7810 206064300005 STACK BELL 206 206L3 1182108 SW EXHAUST CRACKED B AC2R K NONE O OTHER IN INSP/MAINT 1 SW 03 17238 6275 971014 51492 CRACK ON AFT SIDE NEAR CENTER AT FLANGE BASE. 1 G 7 1 3U H2SW 1999082001009 19990820 01009 EU 1999 8 20 99ZZZM525 1 19980401 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU FRAME 41-44 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 DV INSPECTION FLOORBEAMS AND SUPPORT STRUCT FRAME 41-44. ACCESS UNDER FLOOR THROUGH 181HL/181HR EVIDENCE OF LEAKAGE APP ARENT UNDER TOILET/GALLEY, INSPECTION THROUGH 25 1AF/DF/EF/FF, 252AF/BF/CF/DF. SII REPORT FINDS FORM M046 (SII 53-30-15 4). PERFORMED DV INSPECTION FLOORBEAMS, SUPPORT STRUCTURE FRAME 41-44. FOUND SILL PLATE LEFT SIDE NEAR FRAME 44 CORROD ED AND BROKEN. (M) 2 H 7 4 4F RT A49EU 1999082001010 19990820 01010 EU 1999 8 20 99ZZZM526 1 19980424 A 5320 ANGLE BAG BAE146 BAE146200A 1500266 EU FRAME 36 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 FRAME 36 AFT CARGO BAY FREIGHT ANGLE IS CRACKED AND ALSO CORRODED ON RIGHT SIDE. REMOVED AND REPLACED FREIGHT ANGLE ON FRAME 36 RIGHT SIDE IN AFT CARGO BAY. (M) 2 H 7 4 4F RT A49EU 1999082001011 19990820 01011 EU 1999 8 20 99ZZZM527 1 19980408 A 5320 SILL BAG BAE146 BAE146200A 1500266 EU FRAME 44 BROKEN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 AFT VESTIBULE FLOOR SUPPORT STRUCTURE ON LEFT SIDE UNDER TOILET HAS THE AFT END OF THE SILL PLATE NEAR FRAME 44 CORRODED AND BROKEN. REMOVED AND REPLACED SILL PLATE, LEFT SIDE UNDER LAV MODULE BETWEEN FRAME STRINGER 43/44. (M) 2 H 7 4 4F RT A49EU 1999082001012 19990820 01012 EU 1999 8 20 99ZZZM528 1 19980414 A 5320 BRACKET BAG BAE146 BAE146200A 1500266 EU FRAME CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 TWO BRACKETS, CRACKED IN 2 CORNERS EACH, LOCATED UNDER FLOOR BETWEEN FRAMES 40 AND 41 AND SUPPORT BOXES FOR RED LIGHTS F OR DOOR OPEN AND CLOSED. BLENDED OUT CRACKED AREA, INSTALLED DOUBLER AT EACH LOCATION IAW BAE SRM. (M) 2 H 7 4 4F RT A49EU 1999082001013 19990820 01013 EU 1999 8 20 99ZZZM529 1 19980424 A 7110 DOOR BAG BAE146 BAE146200A 1500266 EU NR 2 ENG COWL CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 NR 2 ENGINE AFT OUTBOARD COWL DOOR INNER TITANIUM BAFFLE IS CRACKED AT FORWARD UPPER ATTACH RIVET, CRACKED AT FORWARD LO WER ATTACH RIVETS AND CRACKED AT AFT LOWER ATTACH RIVET. REPAIRED SAID CRACKS BY PATCHING IAW AIR WIS/BAE SRM CHAPTER 5 4 NACELLES/PYLONS. (M) 2 H 7 4 4F RT A49EU 1999082001014 19990820 01014 EU 1999 8 20 99ZZZM530 1 19980408 A 5400 RIB BAG BAE146 BAE146200A 1500266 EU NR 1 PYLON CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 NR 1 PYLON INBOARD RIB NR 1 NUTPLATE AREA CRACKED. REPAIRED ABOVE DAMAGE TO INBOARD NR 1 PYLON NUTPLATE MOUNT STRIP FOR PANEL 451AT PER RIL HC546H9017, SEE WO BX5024 FOR REPAIR PIECE HEAT TREAT AND PLATING. (M) 2 H 7 4 4F RT A49EU 1999082001015 19990820 01015 EU 1999 8 20 99ZZZM531 1 19980420 A 5350 FRAME BAG BAE146 BAE146200A 1500266 EU LT WING/FUS CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 LEFT WINGROOT FORWARD FAIRING SUPPORT FRAME CRACKED IN FLANGE AT FRAME 26. C/W SRM 51-71, REPAIR TO CRACKED CORNER FLAN GE USING .040 2024-T3 AN 8 AD RIVETS. (M) 2 H 7 4 4F RT A49EU 1999082001016 19990820 01016 EU 1999 8 20 99ZZZM532 1 19980409 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 RIGHT WING TOP SKIN INBOARD STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPLACED RIGHT WING TOP SKIN STIFFENER B ETWEEN RIBS 8/9. (M) 2 H 7 4 4F RT A49EU 1999082001017 19990820 01017 EU 1999 8 20 99ZZZM533 1 19980417 A 5330 SKIN BAG BAE146 BAE146200A 1500266 EU FUSELAGE LIGHTNING STRIKE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 608AW E2049 REPAIR CRACK FROM LIGHTNING STRIKE DAMAGE ON LEFT FUSELAGE SKIN JUST AFT OF FRAME 26 JUST UNDER JACK PAD. REPAIR WITHIN 590 CYCLES OF ORIG FINDING. DUE AT 35337, CURRENT TAC 34779. BLENDED CRACK IAW BAE FAX, REF DJR/RJO325-98. W/C GEN F OR CONTINUED INSPECTION AT 400 FLT INTERVALS. PERFORMED ET ABOVE BLENDED AREA. (M) 2 H 7 4 4F RT A49EU 1999082001018 19990820 01018 EU 1999 8 20 99ZZZM534 1 19980512 A 3260 PROX SWITCH BAG BAE146 BAE146200A 1500266 EU LT MLG FAILED A A6WA O OTHER N FALSE WARNING CL CLIMB 1 GL 31 609AW E2070 WITH GEAR HANDLE SELECTOR UP, LEFT MAIN GEAR INDICATES GEAR INTRANSIT, RID LIGHT IN GEAR HANDLE ALSO ILLUMINATED. NO AU RAL GEAR WEARING. STANDBY GEAR INDICATORS ALL OFF. REMOVED AND REPLACED LEFT MLG LEG UPLOCK HARNESS AND PROXIMITY SWIT CH IAW BAE 146MM, TESTS GOOD. S/N ON 4805. 2 H 7 4 4F RT A49EU 1999082001019 19990820 01019 NE 1999 8 20 99ZZZM535 2 19980116 A 7200 ENGINE BAG BAE146 BAE146300A 1500267 EU LYC ALF502 ALF502R5 41580 NE NR 1 FAILED A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 611AW E3120 NR 1 ENGINE FAILED ON CLIMB-OUT FROM SBA TO DEN. DIVERTED TO LAS. REMOVED AND REPLACED NR 1 ENGINE IAW AWAC ENDING CHA NGE CHECKLIST AND AIRCRAFT MM. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1999082001020 19990820 01020 NE 1999 8 20 99ZZZM536 2 19980425 A 7230 COMPRESSOR BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 4 ENGINE STALLED A A6WA A UNSCHED LANDING B R SMOKE/FUMES/ODORS/SPARKS PARTIAL RPM/PWR LOSS CL CLIMB 1 GL 31 610AW E2082 NR 4 ENGINE MADE SEVERAL MUFFLED BANGS, THEN BEGAN SPOOLING DOWN ON N1, N2 AND TGT. F/A'S REPORTED SPARKS FROM TAILPIPE . ENGINE WAS SECURED USING EMERGENCY CHECKLISTS. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1999082001021 19990820 01021 EU 1999 8 20 99ZZZM537 1 19980615 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 RIGHT WING TE SHROUD LOWER SKIN STIFFENER CRACKED INBOARD OF RIB 10. REMOVED AND REPLACED LOWER SKIN STIFFENER PER SRM. (M) 2 H 7 4 4F RT A49EU 1999082001022 19990820 01022 EU 1999 8 20 99ZZZM538 1 19980611 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 LEFT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB NR 6. REPLACED TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 JUST INBOARD OF RIB 6 AT THIS TIME. (M) 2 H 7 4 4F RT A49EU 1999082001023 19990820 01023 EU 1999 8 20 99ZZZM539 1 19980605 A 2910 BRACKET BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 LEFT WING TE, HYDRAULIC LINE CLAMP BRACKET CRACKED AT FALSE SPAR RIB NR 5. REPLACED HYDRAULIC LINE CLAMP BLOCK BRACKET AT RIB 5 AT THIS TIME. (M) 2 H 7 4 4F RT A49EU 1999082001024 19990820 01024 EU 1999 8 20 99ZZZM540 1 19980611 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 LEFT WING TE SHROUD LOWER SKIN STIFFENERS, TWO HAVE TAG ANGLE CRACKED AT AFT END, BETWEEN RIBS 8/9. REPLACED TWO ANGLES ON TE SHROUD LOWER SKIN STIFFENERS BETWEEN RIBS 8/9 AT THIS TIME. 2 H 7 4 4F RT A49EU 1999082001025 19990820 01025 EU 1999 8 20 99ZZZM541 1 19980610 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 LT WING TE SHROUD TOP SKIN STIFFENER CRACK AT FORWARD END (BETWEEN RIBS 7/8). REPLACED LEFT WING TE SHROUD TOP SKIN STI FFENER BETWEEN RIB 7/8 AT THIS TIME. 2 H 7 4 4F RT A49EU 1999082001026 19990820 01026 EU 1999 8 20 99ZZZM542 1 19980611 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 LT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, OUTBOARD OF RIB NR 8. REPLACED LEFT WING TE SHROUD TOP SKI N STIFFENER OUTBOARD OF RIB NR 8. 2 H 7 4 4F RT A49EU 1999082001027 19990820 01027 EU 1999 8 20 99ZZZM543 1 19980611 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 LT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB NR 10. REPLACED LEFT TE WING SHROUD TOP SKI N STIFFENER INBOARD OF NR 10 RIB AT THIS TIME. (M) 2 H 7 4 4F RT A49EU 1999082001028 19990820 01028 EU 1999 8 20 99ZZZM544 1 19980619 A 2710 CONTROL CABLE BAG BAE146 BAE146300A 1500267 EU LT AILERON CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 LEFT MAIN AILERON CONTROL CABLES ARE CORRODED AT PULLEY BETWEEN FUSELAGE FRAME NR 24 AND 25. REMOVED AND REPLACED LEFT MAIN AILERON CENTER CONTROL CABLES, TENSIONED AND SAFETIED. (M) 2 H 7 4 4F RT A49EU 1999082001029 19990820 01029 EU 1999 8 20 99ZZZM545 1 19980618 A 7110 DOOR BAG BAE146 BAE146300A 1500267 EU NR 4 ENGINE COWL CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 NR 4 ENGINE INBOARD FAN DOOR, FORWARD INNER TITANIUM FIRESHIELD CRACKED AT CORNERS. REPAIRED CRACK BY PATCHING IAW BAE/ AIR WISC SRM STD PRACTICES AND FOUND SERVICEABLE. (M) 2 H 7 4 4F RT A49EU 1999082001030 19990820 01030 EU 1999 8 20 99ZZZM546 1 19980618 A 7110 DOOR BAG BAE146 BAE146300A 1500267 EU NR 4 ENGINE COWL CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 NR 4 ENGINE INBOARD FAN DOOR, 3RD DOOR RIB, CRACKED AT LOWER CORNER AREA NEAR VENT TUBE. REPAIRED CRACK BY PATCHING IAW BAE AIR/WISC SRM STD PRACTICES AND FOUND SERVICABLE. (M) 2 H 7 4 4F RT A49EU 1999082001031 19990820 01031 EU 1999 8 20 99ZZZM547 1 19980618 A 7110 STRIP BAG BAE146 BAE146300A 1500267 EU NR 4 ENGINE COWL CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 612AW E3122 NR 4 ENGINE FORWARD OUTBOARD COWL DOORIS CRACKED AT INNER DOOR MIDDLE CAPPING. STRIP NEAR DRAIN LINE CLAMP. REPAIRED C APPING STRIP PER BAE SRM 51-71-11 AND 12. (M) 2 H 7 4 4F RT A49EU 1999082001125 19990820 01125 EU 1999 8 20 99ZZZM560 1 19980821 A 2910 BRACKET BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 LEFT WING TE HYD LINE CLAMP BRACKET CRACKED AT RIB 5. REPLACED BRACKET. (M) 2 H 7 4 4F RT A49EU 1999082001126 19990820 01126 EU 1999 8 20 99ZZZM561 1 19980330 A 3230 ARM BAG BAE146 BAE146200A 1500266 EU NLG FAILED A A6WA O OTHER O OTHER CL CLIMB 1 GL 31 609AW E2070 DURING GEAR RETRACTION AT EGE, HEARD A VERY LOUD BANG FROM NOSE WHEEL AREA ACCOMPANIED BY WHEEL ROTATION SOUNDS. GEAR R ETRACTION AND EXTENSION NORMAL. REPLACED LEFT EMEREGNCY LOWERING GEAR ASSISTING ARM ASSY. RETRACTED GEAR, FREE FALL OP S CHECKED GOOD. CLOSED NLG DOORS AND SAFTIED AND RII'D. (M) 2 H 7 4 4F RT A49EU 1999082001127 19990820 01127 EU 1999 8 20 99ZZZM562 1 19980319 A 5210 ANGLE BAG BAE146 BAE146200A 1500266 EU PAX DOOR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 LEFT FORWARD PAX DOOR HANDLE BOX AREA 2 CRACKED ANGLES. REPLACED LEFT FORWARD PAX DOOR HANDLE BOX AREA ANGLES REF P/N'S ABOVE. REPAIR ACCOMPLISHED IAW BAE DRAWINGS HC521H0508 AND HC521H0507 AND BAE FAX REF DJR/RJO318-97. (M) 2 H 7 4 4F RT A49EU 1999082001128 19990820 01128 1999 8 20 99ZZZM563 4 19980325 A 3418 STALL BAR BAG BAE146 BAE146200A 1500266 EU LT WING LOOSE A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 LEFT WING INBOARD SECTION OF STALL BAR LOOSE, PULLING OVER SCREW HEADS. REMOVED LT WING STALL TRIGGER AND REPAIRED PER FAX REF DJH/RJO268-98 USING FAX GCB/RJ1344-94. REINSTALLED STALL TRIGGER. (M) 2 H 7 4 4F RT A49EU 1999082001129 19990820 01129 EU 1999 8 20 99ZZZM564 1 19980319 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 LEFT WING TE TOP SKIN, TWO STIFFENERS CRACKED AT FORWARD END BETWEEN RIB 8/9. REPLACED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 (P/N HC572H0626-0000). REPAIRED LEFT WING TRAILING EDGE TOP SKIN STIFFENER BETWEEN RIB 8/9 ( P/N HC572H0627-002) IAW BAE FAX JM/RJO241-98. (M) 2 H 7 4 4F RT A49EU 1999082001130 19990820 01130 EU 1999 8 20 99ZZZM565 1 19980313 A 5753 SKIN BAG BAE146 BAE146200A 1500266 EU RT TE FLAP TAB CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT FLAP TAB UPPER SKIN AT RIB 34 HAS TWO .011 INCH DEEP CHAFED AREAS, (.005 TO .008). BLENDED CHAFE MARKS TO SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO234-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO234-98, AREA CRACK FREE. APP LIED SURFACE REPROTECTION AND TOP COAT PAINT IAW MM. (M) 2 H 7 4 4F RT A49EU 1999082001131 19990820 01131 EU 1999 8 20 99ZZZM566 1 19980316 A 2910 BRACKET BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING TE HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR ABOVE NR 2 FLAP TRACK. REPLACED RIGHT WING TE HYD LINE CLAMP BRACKET. (M) 2 H 7 4 4F RT A49EU 1999082001132 19990820 01132 EU 1999 8 20 99ZZZM567 1 19980318 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING TE TOP SKIN STIFFENER CRACKED AT AFT END BETWEEN RIBS 3/4. REMOVED AND REPLACED STIFFENER. (M) 2 H 7 4 4F RT A49EU 1999082001133 19990820 01133 EU 1999 8 20 99ZZZM568 1 19980314 A 5720 STIFFENER BAG BAE146 BAE146200A 1500266 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPLACED RT WING TRAILING EDGE TOP SKIN STIFF ENER BETWEEN 7/8. (M) 2 H 7 4 4F RT A49EU 1999082001134 19990820 01134 EU 1999 8 20 99ZZZM569 1 19980313 A 5753 SKIN BAG BAE146 BAE146200A 1500266 EU RT TE FLAP CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 RIGHT FLAP UPPER SKIN BETWEEN RIB 29/30 HAS .020 INCH DEEP BY 1 INCH LONG CHAFE. BLENDED CHAFE MARK TO A SMOOTH PROFILE AS NEEDED IAW BAE FAX DJR/RJO236-98. DV AND NDT INSPECTION C/W IAW BAE FAX DJR/RJO236-98, AREA CRACK FREE. APPLIED SU RFACE REPROTECTION AND APPLIED PAINT IAW MM. 2 H 7 4 4F RT A49EU 1999082001135 19990820 01135 EU 1999 8 20 99ZZZM570 1 19980309 A 5230 SEAL BAG BAE146 BAE146200A 1500266 EU CARGO DOOR BENT A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 609AW E2070 FORWARD CARGO DOOR BOTTOM HALF SEAL CAGE IS DISTORTED, BENT IN NUMEROUS AREAS. REPLACED FORWARD CARGO DOOR BOTTOM AFT S EAL CAGE P/N HC523J0 063-202. STRAIGHTENED BEND IN PORTION OF BOTTOM FORWARD SEAL CAGE. (M) 2 H 7 4 4F RT A49EU 1999082001136 19990820 01136 EU 1999 8 20 99ZZZM571 1 19980715 A 5320 SILL BAG BAE146 BAE146300A 1500267 EU PAX DOOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 PAX DOOR SILL PLATE SOME LIGHT SURFACE CORROSION, MARKED W/DOT. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICAB LE AREA. (M) 2 H 7 4 4F RT A49EU 1999082001137 19990820 01137 EU 1999 8 20 99ZZZM572 1 19980720 A 5260 INTERCOSTAL BAG BAE146 BAE146300A 1500267 EU AFT AIRSTAIR CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 AFT AIRSTAIR OUTBOARD RAIL INTERCOSTAL CRACK AT FLOOR, AFT END. REMOVED AND REPLACED AFT AIRSTAIR OUTBOARD RAIL INTERCO STAL AT AFT END OF RAIL. WORK DONE IAW BAE MM 51-00-00. (M) 2 H 7 4 4F RT A49EU 1999082001138 19990820 01138 EU 1999 8 20 99ZZZM573 1 19980709 A 2710 CONTROL CABLE BAG BAE146 BAE146300A 1500267 EU AILERONS CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 BOTH CENTER AILERON INTERCONNECT CABLES ARE CORRODED. REMOVED AND REPLACED BOTH CENTER AILERON INTERCONNECT CABLES, GEN ERATED NEW WC FOR TRAVEL CHECKS AND FREEDOM OF MOVEMENT. (M) 2 H 7 4 4F RT A49EU 1999082001139 19990820 01139 EU 1999 8 20 99ZZZM574 1 19980707 A 2520 TRIM STRIP BAG BAE146 BAE146300A 1500267 EU FRAME 18 CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 FRAME 18 TRIM STRIP FOR UNDER RIGHT BULKHEAD BADLY CORRODED, REPLACED. REMOVED AND REPLACED FRAME 18 TRIM STRIP. 2 H 7 4 4F RT A49EU 1999082001140 19990820 01140 EU 1999 8 20 99ZZZM575 1 19980715 A 5315 FLOORBEAM BAG BAE146 BAE146300A 1500267 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN PRESS FLOORBEAMS NR 9 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. (M) 2 H 7 4 4F RT A49EU 1999082001141 19990820 01141 EU 1999 8 20 99ZZZM576 1 19980715 A 5315 FLOORBEAM BAG BAE146 BAE146300A 1500267 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/ RJO207-97. (M) 2 H 7 4 4F RT A49EU 1999082001142 19990820 01142 EU 1999 8 20 99ZZZM577 1 19980715 A 5315 FLOORBEAM BAG BAE146 BAE146300A 1500267 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN PRESS FLOORBEAM NR 15 CRACKED AT FRAME 29, RIGHT INBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF D JR/RJO207-97. (M) 2 H 7 4 4F RT A49EU 1999082001143 19990820 01143 EU 1999 8 20 99ZZZM578 1 19980715 A 5315 FLOORBEAM BAG BAE146 BAE146300A 1500267 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN PRESSURE FLOORBEAM NR 13 CRACKED AT FRAME 29. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJR/RJO207-97. 2 H 7 4 4F RT A49EU 1999082001144 19990820 01144 EU 1999 8 20 99ZZZM579 1 19980715 A 5315 FLOORBEAM BAG BAE146 BAE146300A 1500267 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN PRESS FLOORBEAM NR 19 (RIGHT OUTBOARD SEAT RAIL) CRACKED AT FRAME 29. REPAIRED PER FAX REF DJR/RJO207-97 AND REPA IR DRAWING HC536H9211. (M) 2 H 7 4 4F RT A49EU 1999082001145 19990820 01145 EU 1999 8 20 99ZZZM580 1 19980723 A 3520 MANIFOLD BAG BAE146 BAE146300A 1500267 EU CABIN LEAKING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 FOUND 4 RT OXYGEN BOX, 2 MASK LEAKING WITH PINS INSTALLED, OXYGEN MASK FACE PIECE TORN. REPLACED 4 RIGHT OXYGEN MANIFOL D, OPS AND LEAK CHECKS OK. REPLACED MASK ASSY, LEAK AND OPS CHECKS OK. (M) 2 H 7 4 4F RT A49EU 1999082001146 19990820 01146 EU 1999 8 20 99ZZZM581 1 19980713 A 5260 STAIR BAG BAE146 BAE146300A 1500267 EU AFT AIRSTAIR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP. 2 H 7 4 4F RT A49EU 1999082001147 19990820 01147 EU 1999 8 20 99ZZZM582 1 19980715 A 5260 STEP BAG BAE146 BAE146300A 1500267 EU AFT AIRSTAIRS CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 AFT AIRSTAIRS, SECOND FROM THE TOP STEP CORRODED. REPLACED STEP. 2 H 7 4 4F RT A49EU 1999082001148 19990820 01148 EU 1999 8 20 99ZZZM583 1 19980727 A 3520 D389991 OXYGEN BOX BAG BAE146 BAE146300A 1500267 EU CABIN LEAKING A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 FOUND OXYGEN BOX AT 4 RT LEAKING THROUGH MASK WITH PIN INSTALLED. REPLACED OXYGEN BOX ASSY, OPS AND LEAK CHECKS OK. 2 H 7 4 4F RT A49EU 1999082001149 19990820 01149 EU 1999 8 20 99ZZZM584 1 19980714 A 7110 DOOR BAG BAE146 BAE146300A 1500267 EU NR 3 ENG COWL CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 NR 3 ENGINE INBOARD FAN DOOR INNER TITANIUM DISHING CHAFED THROUGH. REPAIRED CHAGED AREA OF NR 3 ENGINE INBOARD FAN DOO R INNER SKIN IAW 146 RIL HC711H9047. (M) 2 H 7 4 4F RT A49EU 1999082001150 19990820 01150 EU 1999 8 20 99ZZZM585 1 19980727 A 3520 OUTLETS BAG BAE146 BAE146300A 1500267 EU CABIN LEAKING A A6WA K NONE K FLUID LOSS IN INSP/MAINT 1 GL 31 611AW E3120 FOUND OXYGEN OUTLETS AT RT 6, 14, 17, 20, AND 21 LEAKING. REPLACED OUTLETS AT RT 6, 14, 17, 20, AND 21. LEAK CHECK OK. (M) 2 H 7 4 4F RT A49EU 1999082001151 19990820 01151 EU 1999 8 20 99ZZZM586 1 19980713 A 7110 DOOR BAG BAE146 BAE146300A 1500267 EU NR 4 ENG COWL CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 NR 4 ENGINE INBOARD FAN DOOR INNER TITANIUM SKIN CHAFED THROUGH JUST ABOVE DISHING AREA. REPAIRED CHAFED AREA IAW RIL H C711H9047. (M) 2 H 7 4 4F RT A49EU 1999082001152 19990820 01152 EU 1999 8 20 99ZZZM587 1 19980720 A 5720 STIFFENER BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 LT WING TOP SKIN TE SHROUD OUTBOARD STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 8/9. REPAIRED ABOVE STIFFENER PER BAE FAX JM/RJO317/97 USING 2 024T3 .050. (M) 2 H 7 4 4F RT A49EU 1999082001153 19990820 01153 EU 1999 8 20 99ZZZM588 1 19980715 A 7110 COWL BAG BAE146 BAE146300A 1500267 EU NR 2 ENGINE CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 NR 2 ENGINE PYLON SHOULDER COWL HAS CRACKED SKIN BETWEEN THE BIG HYD PIPE AND THE DRAIN TUBE. REPAIRED ABOVE CRACK USIN G .040 TA 2 PER FAX KG/0603-91 AND SRM. (M) 2 H 7 4 4F RT A49EU 1999082001154 19990820 01154 EU 1999 8 20 99ZZZM589 1 19980720 A 7110 DOOR BAG BAE146 BAE146300A 1500267 EU NR 1 ENGINE COWL DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 NR 1 EIGNE INBOARD REAR COWL DOOR HAS A HOLE WORN THROUGH THE TOP 3RD RIB BACK FROM THE FRONT CORNER OF THE DOOR. REPLA CED THE TOP THIRD RIB FROM THE FRONT EDGE OF THE NR 1 INBOARD REAR COWL DOOR SPLITTER. (M) 2 H 7 4 4F RT A49EU 1999082001155 19990820 01155 EU 1999 8 20 99ZZZM590 1 19980721 A 7110 DOOR BAG BAE146 BAE146300A 1500267 EU NR 3 ENG COWL CHAFED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 NR 3 ENGINE INBOARD FAN DOOR LOWER SPLITTER AREA, 2ND STIFFENER FROM FORWARD CHAFED. REPLACED THE NR 3 ENGINE INBOARD F AN DOOR LOWER SPLITTER AREA, 2ND STIFFENER FROM FORWARD. (M) 2 H 7 4 4F RT A49EU 1999082001156 19990820 01156 EU 1999 8 20 99ZZZM591 1 19980727 A 3520 MASK BAG BAE146 BAE146300A 1500267 EU ROW 9 TORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 OXYGEN MASK AT 9 RT FACE PIECE TORN. REPLACED OXYGEN MASK 9 RT, OPS AND LEAK CHECKS OK. (M) 2 H 7 4 4F RT A49EU 1999082001157 19990820 01157 EU 1999 8 20 99ZZZM592 1 19980717 A 5320 TREAD PLATE BAG BAE146 BAE146300A 1500267 EU LEFT CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 LEFT FORWARD TREAD PLATE (E804) HAS CORROSION ON INNER SURFACE. REMOVED CORROSION ON LT FORWARD TREAD PLATE 9E804). (M ) 2 H 7 4 4F RT A49EU 1999082001158 19990820 01158 EU 1999 8 20 99ZZZM593 1 19980709 A 5720 ANGLE BAG BAE146 BAE146300A 1500267 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 RIGHT WING TE LOWER SKIN, INBOARD STIFFENER BETWEEN RIBS 8/9 TAG ANGLE CRACKED AFT END OF STIFFENER. REPLACED SAID TAG ANGLE AND FOUND SERVICEABLE. (M) 2 H 7 4 4F RT A49EU 1999082001159 19990820 01159 EU 1999 8 20 99ZZZM594 1 19980709 A 5400 STRUCTURE BAG BAE146 BAE146300A 1500267 EU NR 3 PYLON WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH HOLES WORN AND SLOPPY AT SHOULDER COWL STRUCTURE. REPAIR PER RI HC710H90 33. REPAIRED NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH STRUCTURE HOLES IAW BAE REPAIR DRAWING HC710H9003. (M) 2 H 7 4 4F RT A49EU 1999082001160 19990820 01160 EU 1999 8 20 99ZZZM595 1 19980710 A 2910 BRACKET BAG BAE146 BAE146300A 1500267 EU RT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 RIGHT WING TE HYD CLAMP BRACKET CRACKED AT FALSE SPAR, RIB 6. ALSO, HYD CLAMP LOOSE OUTBOARD OF RIB 6. REPLACED ONE RI GHT WING TRAILING EDGE HYD CLAMP BRACKET (P/N HC932HO178-003) AT FALSE SPAR, RIB 6. TIGHTENED BOLTS SECURING HYD CLAMP OUTBOARD OF RIB 6. (M) 2 H 7 4 4F RT A49EU 1999082001161 19990820 01161 EU 1999 8 20 99ZZZM596 1 19980717 A 2910 BRACKET BAG BAE146 BAE146300A 1500267 EU LT WING CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 LEFT WING HYD LINE CLAMP BRACKET CRACKED AT FALSE SPAR, RIB NR 3. REMOVED AND REPLACED ABOVE BRACKET. (M) 2 H 7 4 4F RT A49EU 1999082001162 19990820 01162 EU 1999 8 20 99ZZZM597 1 19980715 A 5315 FLOORBEAM BAG BAE146 BAE146300A 1500267 EU FRAME 29 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN PRESS FLOORBEAM NR 3 CRACKED AT FRAME 29, LEFT OUTBOARD SEAT RAIL. REPAIRED PER DRAWING HC536H9211 AND FAX REF DJ R/RJO207-97. (M) 2 H 7 4 4F RT A49EU 1999082001163 19990820 01163 1999 8 20 99ZZZM598 4 19980701 A 2565 D31050105 SLIDE BAG BAE146 BAE146300A 1500267 EU LT CABIN CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 LEFT FORWARD EVAC SLIDE PACK BOARD CRACKED AT TOP MOUNT PP PIN. REMOVED SLIDE ASSY AND PLACED ON W/O, P/N 31050-105, S/ N 0093, REF W/C 8012 FOR INSTALLATION. (M) 2 H 7 4 4F RT A49EU 1999082001164 19990820 01164 EU 1999 8 20 99ZZZM599 1 19980728 A 3520 MASK BAG BAE146 BAE146300A 1500267 EU CABIN CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 FORWARD AFT FACING F/A OXYGEN BOTTLE, MASK FACE PIECE CRACKED. REPLACED OXYGEN MASK, OPS CHECKS OK. (M) 2 H 7 4 4F RT A49EU 1999082001165 19990820 01165 EU 1999 8 20 99ZZZM600 1 19980727 A 3520 WKA366841 VALVE BAG BAE146 BAE146300A 1500267 EU CABIN FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN OXYGEN SYSTEM FAILED LEAK CHECK. TROUBLESHOOT SYSTEM. REPLACED PAX ISO VLV, 5 QUICK DISC (OUTLETS), 4 RT BOX ASS Y. SEE W/C'S FOR PARTS CHANGED, SYSTEM LEAK CHECKS OK. (M) 2 H 7 4 4F RT A49EU 1999082001166 19990820 01166 EU 1999 8 20 99ZZZM601 1 19980913 A 3222 STRUCTURE BAG BAE146 BAE146200A 1500266 EU NLG CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 290UE E2080 DURING SCHEDULED NDT INSPECTION OF NGL RETRACTION JACK MOUNT STRUCTURE, FOUND CRAKS IN JACK PIN STRUCTURE BORE. (M) 2 H 7 4 4F RT A49EU 1999082001167 19990820 01167 NE 1999 8 20 99ZZZM602 2 19980922 A 7200 ENGINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 FAILED A A6WA E F ENGINE SHUTDOWN ACTIVATE FIRE EXT. A Y FLAME/FIRE ENGINE STOPPAGE CR CRUISE 1 GL 31 606AW E2033 NR 1 EGINE FAILE AND FIRE IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM ANS AWAC GMM ENG CHANGE CHECK LIST VOLUME II SEC B CHAP 72, COMPLIED WITH ALL REQ'D ENGINE GROUND RUNS. ALL PARAMETERS FOUND SATISFACTORY. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1999082001168 19990820 01168 EU 1999 8 20 99ZZZM603 1 19981111 A 2621 5733012 FIRE BOTTLE BAG BAE146 BAE146300A 1500267 EU ENGINE DAMAGED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 ENGINE NOSE COWL WO NR BY8402 HAD FIRE BOTTLE CL978M HAS WORN THREADS ON JUNCTION BOX AND CONTROL HEAD. REM AND REPLACE D FIRE BOTTLE. (M) 2 H 7 4 4F RT A49EU 1999082001169 19990820 01169 EU 1999 8 20 99ZZZM604 1 19981102 A 5315 FLOORBEAM BAG BAE146 BAE146200A 1500266 EU FRAME 37 CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 FOUND CRACK IN FLOORBEAM AT FRAME NR 37 UNDER FLOOR PANEL 241DF IN CENTER ON FWD SIDE OF BEAM ABOUT 8 INCHES LONG AND 1 INCH FROM TOP OF BEAM. REMOVED CRACKED AREA OF FRAME 37 AND REPAIRED IAW BAE DRAWING NR HC538H9219 AND BAE FAX REF RJO7 78-98 DATED 11/2/98. (M) 2 H 7 4 4F RT A49EU 1999082001170 19990820 01170 EU 1999 8 20 99ZZZM605 1 19981110 A 2621 FIRE BOTTLE BAG BAE146 BAE146200A 1500266 EU APU FAILED CHECK A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 183US E2043 APU FIRE BOTTLE FAILED WEIGHT CHECK. REMOVED AND REPLACED FIRE BOTTLE. (M) 2 H 7 4 4F RT A49EU 1999082001171 19990820 01171 EU 1999 8 20 99ZZZM606 1 19981103 A 2730 CABLES BAG BAE146 BAE146200A 1500266 EU ELEVATOR CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 LEFT AND RIGHT MAIN ELEVATOR CONTROL CABLES ARE CORRODED AT VERTICAL STABILIZER REAR SPAR PULLEYS. REMOVED AND REPLACED ALL FOUR MAIN ELEVATOR CONTROL CABLES FROM REAR PRESS BULKHEAD TO CABLE COMPENSATORS, ADJUSTED IAW MM. W/C GENERATED F OR FUNCTION ALL TEST. (M) 2 H 7 4 4F RT A49EU 1999082001172 19990820 01172 EU 1999 8 20 99ZZZM607 1 19981103 A 5313 STRINGER BAG BAE146 BAE146200A 1500266 EU FUSELAGE DENTED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 HAT STRINGER ON AFT WALL OF APU BOX IS DENTED. REPLACED HAT STRINGER ON AFT APU FIREWALL IAW BAE FAXES BARA/AVR/1885/98 AND DWC/RJ0002-98. (M) 2 H 7 4 4F RT A49EU 1999082001173 19990820 01173 EU 1999 8 20 99ZZZM608 1 19981016 A 2731 CONTROL CABLE BAG BAE146 BAE146200A 1500266 EU ELEVATOR TRIM CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 ELEVATOR TRIM CABLE BETWEEN SCREWJACKS HAS SIGNS OF CORRISON AT CENTER PULLEY. ALSO, CENTER PULLEY BEARING WORN. REMOV ED AND REPLACED CENTER PULLEY AND TRIM CABLE BETWEEN SCREWJACKS. ADJUSTED TENSION IAW MM 27-32-00. REF W/C 3055 FOR FU NCTIONAL TEST. (M) 2 H 7 4 4F RT A49EU 1999082001174 19990820 01174 EU 1999 8 20 99ZZZM609 1 19981027 A 5320 DIAPHRAGM BAG BAE146 BAE146200A 1500266 EU NLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 NOSE SIDEWALL DIAPHRAGM REMOVED FOR CRACKED ACTUATOR ATTACH POINT. REPLACED NLG LEFT DIAPHRAGM PER BAE FAX REF NR JEN/R JO0505-98. GEN W/C FOR 60 CYC DV INSPECTIONS AND 2000 AND OR 10 MONTH REPLACEMENT. (M) 2 H 7 4 4F RT A49EU 1999082001175 19990820 01175 EU 1999 8 20 99ZZZM610 1 19981028 A 5320 DIAPHRAGM BAG BAE146 BAE146200A 1500266 EU NLG WW CRACKED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 606AW E2033 NLG ACTUATOR AT UPPER ATTACHMENT POINT DIAPHRAGM IS CRACKED IN THE WEB AND BOSS. REPORTED TO BAE RDO. REF W/C 7025 FOR CORRECTIVE ACTION, DIAPHRAGM REPLACEMENT. 2 H 7 4 4F RT A49EU 1999082700586 19990827 00586 WP 1999 8 27 9806689986 1 19980415 A 3350 BATTERY PACK DOUG DC9 DC932 3022066 WP TAIL CONE DISCHARGED A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 986US 47480 DURING LINE INSPECTION, FOUND TAIL CONE OVERHEAD EMERGENCY LIGHT DIM. REPLACED BATTERY PACK, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1999082700650 19990827 00650 EU 1999 8 27 99ZZZM611 1 19981110 A 2620 WIRE BAG BAE146 BAE146200A 1500266 EU NR 3 ENGINE FAILED A A6WA K NONE L NO TEST IN INSP/MAINT 1 GL 31 183US E2043 NR 3 ENGINE OUTBOARD FIRE BOTTLE FAILED FUNCTION CHECK, FOUND ENVIRONMENTAL SPLICE IN HARNESS HAD BROKEN. REPAIRED WIRI NG. (M) 2 H 7 4 4F RT A49EU 1999082700781 19990827 00781 EU 1999 8 27 99ZZZM612 1 19980715 A 5320 RIVETS BAG BAE146 BAE146300A 1500267 EU FRAME 26 FAILED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 CABIN FLOOR OUTBOARD SUPPORT ANGLE HAS 2 POPPED RIVETS AT FRAME 26 (RIGHT SIDE AFT OF FRAME). REPLACED RIVETS. (M) 2 H 7 4 4F RT A49EU 1999082700782 19990827 00782 EU 1999 8 27 99ZZZM613 1 19980715 A 5320 STRUCTURE BAG BAE146 BAE146300A 1500267 EU GALLEY CORRODED A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 611AW E3120 FOUND CORROSION AROUND MOUNTING HOLES FOR GALLEY. REMOVED CORROSION, TREATED, PRIMED AND PAINTED APPLICABLE AREAS AROUN D GALLEY MOUNTING HOLES. (M) 2 H 7 4 4F RT A49EU 1999091700548 19990917 00548 EU 1999 9 17 99ZZZX3448 1 19980915 A 2150 CLAMP BAG BAE146 BAE146200A 1500266 EU NR 1 PACK LOOSE A A6WA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 GL 31 291UE E2084 DEN - FLT 567 - NR 1 PACK ALREADY ON MEL. DURING CLIMB-OUT THE NR 2 PACK FELL OFF-LINE AND WOULD NOT COME BACK ON FOR 5 MINUTES. TIGHTENED BLOWN CLAMP ON NR 2 PACK. RESET CIRCUIT BREAKER FOR NR 1 PACK, OPS CHECKED OK. 2 H 7 4 4F RT A49EU 1999091700549 19990917 00549 EU 1999 9 17 99ZZZX3449 1 19981230 A 2620 WIRE BAG BAE146 BAE146200A 1500266 EU NR 2 ENGINE BROKEN A A6WA O OTHER N FALSE WARNING TX TAXI/GRND HDL 1 GL 31 291UE E2084 NR 2 EXTINGUISHER USED. LIGHT 'ON' ON NR 2 ENGINE. REPAIRED BROKEN WIRE AT TERMINAL STRIP AT FIRE BOTTLE. 2 H 7 4 4F RT A49EU 1999091700563 19990917 00563 NM 1999 9 17 A6WA9800008 1 19981124 A 2120 AIR DISTRIBUTION DORNER DO32 DO328100 2996000 NM COCKPIT ODOR A A6WA E ENGINE SHUTDOWN B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 GL 31 332PH 3010 DEN - FLT 7062 - DURING TAXI IN, HAD NUMEROUS ELECTRICAL FAILURES AND SMOKE IN COCKPIT PRIOR TO NR 1 ENGINE SHUT-DOWN. G ROUND RAN A/C USING BOTH ENGINES, OPERATING BOTH PACKS. CHECKED ELECTRICAL SYSTEM LOADS ON MOST MAJOR SYSTEMS, ALL CHEC KS WERE OK. NO DEFECTS NOTED. (X) 2 H 7 2 4T RT A45NM 1999091700586 19990917 00586 EU 1999 9 17 99ZZZX3463 1 19980804 A 6220 10513144 ROD END BOLKMS 117 BK117A4 5626017 EU MAIN ROTOR WORN B TI1R K NONE O OTHER IN INSP/MAINT 1 SW 05 8765J 163 7054 BEARINGS WORN. REMOVED AND REPLACED. 1 G 7 2 3U H13EU 1999091700774 19990917 00774 EU 1999 9 17 VTZA990246 1 19980719 A 3244 TIRES BAG JETSTM JETSTM3201 1500217 EU RT MLG AND NLG UNDER INFLATED A VTZA C D ABORTED TAKEOFF RETURN TO BLOCK O OTHER TO TAKEOFF 1 EA 27 475UE 850 FLT 7353 - AVP-IAD - CREW ABORTED TAKEOFF DUE TO AIRCRAFT PULLED TO LEFT SIDE ON TAKEOFF. AIRCRAFT RETURNED TO GATE WIT H NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SERVICED NOSES AND RT MAIN TIRES. MAINTENANCE PERFORMED HIGH SPEED TA XI, OPS CHECK OK. AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999100100397 19991001 00397 WP 1999 10 1 99FDEA00398 1 19980812 A 5315 AEA03611 FLOORBEAM DOUG DC10 DC1010 3022110 WP BS 1289 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 368FE 46606 DURING AC PF CONVERSION AT OAN, CRACK FOUND ON FLOORBEAM Y=1289X=107. REMOVED AND REPLACED CRACKED OUTBD AND INSTALLED STAINLESS STEEL REPAIR PARTS IAW EA NR 8-5323-44064. 2 L 7 3 4F A22WE 1999100100569 19991001 00569 NM 1999 10 1 TSAA9933424 1 19980909 A 3350 86210066 BATTERY PACK BOEING 737 737282C 13844AU NM CABIN DISCHARGED A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED NR 4 AND NR 5 EMERGENCY FLOOR LIGHT BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERV ICE. (M) 2 L 7 2 4F RT A16WE 1999100100579 19991001 00579 NM 1999 10 1 TSAA9933430 1 19980910 A 3350 8731002511 LIGHT BOEING 737 737282C 13844AU NM CABIN INOPERATIVE A TSAA K NONE L NO TEST IN INSP/MAINT 1 WP 13 826AL 23051 REPLACED RIGHT OVERWING EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M ) 2 L 7 2 4F RT A16WE 1999100800019 19991008 00019 SW 1999 10 8 CA990915043 1 19980929 A 6220 204011421001 HOUSING 212010407109 BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE M/R HEAD MISMANUFACTURED W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 511 EA3801 PCETA0013 (CAN) METAL SEAL CASE IS DIMENSIONALLY TOO LARGE. CASING PROTRUDES OUTSIDE OF HOUSING BY 0.050 INCH THEREBY CAUSING CONT ACT WITH SCISSORS SIDE FACE RESULTING IN CIRCUMFERENTIAL SCORING OF SCISSORS DURING OPERATION. BOTH SCISSORS ASSEMBLIES RETURNED TO MANUFACTURER. 1 G 7 1 4U 4 U H4SW E22EA 1999100800098 19991008 00098 EU 1999 10 8 99ZZZX3775 1 19981027 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 125 12969 S789 FUEL PRESSURE TRANSMITTER INOPERATIVE. PEGGED HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999100800099 19991008 00099 EU 1999 10 8 99ZZZX3776 1 19981027 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 188 12977 S789 FUEL PRESSURE TRANSMITTER INOPERATIVE. PEGGED HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999100800100 19991008 00100 EU 1999 10 8 99ZZZX3777 1 19981228 A 2840 DK042 TRANSMITTER BOLKMS 105 BO105CBS 5626008 EU FUEL PRESSURE INOPERATIVE A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 105LC 273 12971 S789 FUEL PRESSURE TRANSMITTER INOPERATIVE. PEGGED HIGH. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U NC H3EU 1999100800108 19991008 00108 NE 1999 10 8 99ZZZX3785 2 19981022 A 7250 430150601 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 2 LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 527RM 156 1754 7111 LE45218EA BEARING LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999100800109 19991008 00109 NE 1999 10 8 99ZZZX3786 2 19981022 A 7250 430144801 SEAL BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE NR 3 LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 527RM 156 8F950009 7111 LE45218EA SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999100800125 19991008 00125 NE 1999 10 8 99ZZZX3802 2 19981022 A 7250 430203802 BEARING BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE POWER TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 750 7111 LE45218EA POWER TURBINE HAD SECONDARY DAMAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 1999100800405 19991008 00405 NM 1999 10 8 EIA980358 1 19981202 A 5311 FRAME BOEING 747 747212B 1384886 NM BS 1620 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, AFT BAG BIN, FRAME CRACKED AT BS 1620 STRINGER 39R-40R. REPAIRED FRAME PER SRM 53-10-04 FIG 69. (M) 2 L 7 4 4F A20WE 1999100800406 19991008 00406 NM 1999 10 8 EIA980356 1 19981202 A 5320 FITTING BOEING 747 747212B 1384886 NM BS 2484 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 2484 FORWARD LOWER LEFT SPLICE FITTING VERTICAL LEG 2ND OUTBOARD FASTENER HOLE CRACKED. REPLA CED SPLICE FITTING PER SB 747-53-2162. (M) 2 L 7 4 4F A20WE 1999100800407 19991008 00407 NM 1999 10 8 EIA980359 1 19981202 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM FUSELAGE CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 DURING C5 CHECK, M/D BS 460 AT LBL 90 FLOORBEAM LOWER TEE HAS CORROSION. REPAIRED PER SRM 51-40-04 FIG 2. (M) 2 L 7 4 4F A20WE 1999101500102 19991015 00102 EU 1999 10 15 99ZZZX3885 1 19981022 A 7700 430136101 HARNESS BOLKMS 117 BK117A4 5626017 EU ENGINE FAILED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 750 7111 HARNESS HAD INTERNAL SHORT. REPLACED WITH NEW, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1999101500579 19991015 00579 NM 1999 10 15 EIA980360 1 19981202 A 5312 BULKHEAD WEB BOEING 747 747212B 1384886 NM BS 1480 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING C5 CHECK, BS 1480 APU DUCT CUTOUT FASTENER HOLES CRACKED ON BULKHEAD WEB. REPAIRED PER SB 747-53-2309. (M ) 2 L 7 4 4F A20WE 1999101500609 19991015 00609 NM 1999 10 15 EIAA980321 1 19981006 A 5240 SKIN BOEING 747 747212B 1384886 NM R4 DOOR CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, MAIN DECK R3 DOOR FOUND SKIN CRACKED AT NR 4 DOOR FRAME STRINGER 24-25. REPAIRED PER SRM 52-10-0 2 FIG 9. (M) 2 L 7 4 4F A20WE 1999101500610 19991015 00610 NM 1999 10 15 99ZZZM706 1 19980205 A 5330 STRAP BOEING 747 747273C 1384896 NM BS 560 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 471EV 72724 20651 HKG - DURING C5/D CHECK INSPECTION, CORROSION ON FUSELAGE SKIN AND TEAR STRAP AT BS 560 STRINGER 46R. CORRODED AREA TRI MMED AWAY FROM SKIN AND TEAR STRAP, REPAIRED BY INSTALLING TWO INTERNAL STRAPS AND THREE EXTERNAL REPAIR DOUBLERS, PER H AECO RS R53-21-33659 AND ECRA 471-99-176-1. (M) 2 L 7 4 4F A20WE 1999101500611 19991015 00611 NM 1999 10 15 EIAA980324 1 19981006 A 5315 FLOORBEAM BOEING 747 747212B 1384886 NM BS 2120 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, MAIN DECK FLOORBEAM WEB AT LOWER CHORD CRACKED BS 2120 LBL 100. REPAIRED PER SRM 51-40-02. (M) 2 L 7 4 4F A20WE 1999101500612 19991015 00612 NM 1999 10 15 EIAA980323 1 19981006 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM BS 1438 BROKEN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, MAIN DECK SEAT TRACK BROKEN BS 1438 RBL 11. REPAIRED PER SRM 53-10-05 FIG 32. (M) 2 L 7 4 4F A20WE 1999101500613 19991015 00613 NM 1999 10 15 EIAA980322 1 19981006 A 5347 SEAT TRACK BOEING 747 747212B 1384886 NM BS 1730-1770 CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 485EV 83767 20712 HKG - DURING C6 CHECK, MAIN DECK SEAT TRACK CORRODED BS 1730-1770. REPAIRED PER SRM 53-10-05 FIG 24. (M) 2 L 7 4 4F A20WE 1999102900650 19991029 00650 WP 1999 10 29 EIA980361 1 19981203 A 3213 STRUT DOUG DC9 DC933F 302207A WP RT MLG FLAT A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 945F 47528 47279 SEA - DURING POST FLIGHT WALK AROUND INSPECTION, THE RIGHT GEAR STRUT WAS FOUND COMPLETELY DEFLATED. DURING FURTHER INV ESTIGATION IT WAS FOUND THAT THE GLAND NUT WAS COMPLETELY DISENGAGED FROM THE OUTER CYLINDER. (M) 2 L 7 2 4F A6WE 1999102900651 19991029 00651 NM 1999 10 29 EIA980363 1 19981202 A 5320 SPLICE BOEING 747 747212B 1384886 NM BS 400 CRACKED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 482EV 78029 20713 HKG - DURING 'C5' CHECK, BS 400 NOSE LANDING GEAR WHEEL WELL AFT DOOR CUTOUT LEFT AND RT SPLICE PLATES CRACKED. REPAIRE D PER SB 747-53-2305 AND DRAWING 14101099. (M) 2 L 7 4 4F A20WE 1999102900652 19991029 00652 WP 1999 10 29 EIA980353 1 19981130 A 3260 STRIKER DOUG DC9 DC932F 3022067 WP LANDING GEAR FAILED A EIAA O OTHER N FALSE WARNING CL CLIMB 1 NM 09 935F 50760 47220 ABQ - AFTER TAKEOFF FROM PHX, LANDING GEAR UP, LEFT GEAR UNSAFE LIGHT ON, PERFORMED ABNORMAL CHECKLIST AND LIGHT REMAINE D ON. REPLACED STRIKER FOR GEAR LIGHT, OPERATIONALLY CHECKED GOOD PER MM 32-31-4. (M) 2 L 7 2 4F A6WE 1999102900653 19991029 00653 NM 1999 10 29 EIA980352 1 19981130 A 8012 SWITCH BOEING 747 747273C 1384896 NM NR 4 ENGINE FAILED A EIAA O OTHER J WARNING INDICATION CL CLIMB 1 NM 09 470EV 74840 20653 LAX - WHILE CLIMBING THROUGH FL330, THE NR 4 ENGINE START VALVE OPEN LIGHT ILLUMINATED. ENGINE SHUT DOWN PER ABNORMAL P ROCEDURES. WINDMILLED WITH 24 PSI OIL PRESSURE. PERFORMED INSPECTION OF WING FROM PRESSURE SWITCH TO WING BODY CONNECT ION AND PERFORMED RESISTANCE CHECK, NO DEFECTS NOTED. REPLACED PRESSURE SWITCH PER MM 80-11-05 CHECKED GOOD UNABLE TO D UPLICATE. PERFORMED WINDMILL INSPECTION MM 72-00-00. FILTER AND CHIP DETECTOR SERVICING. (M) 2 L 7 4 4F A20WE 1999102900654 19991029 00654 WP 1999 10 29 EIA980327 1 19981021 A 3350 BULB DOUG DC9 DC932F 3022067 WP CABIN FAILED A EIAA K NONE L NO TEST IN INSP/MAINT 1 NM 09 932F 47355 GEG - FORWARD ENTRANCE EMERGENCY PORTABLE LIGHT WILL NOT ILLUMINATE. RELAMPED PORTABLE EMERGENCY LIGHT. OPS CHECK NORM AL PER 33-53-0. (M) 2 L 7 2 4F A6WE 1999102900655 19991029 00655 WP 1999 10 29 EIAA980325 1 19981016 A 5620 WINDOW DOUG DC9 DC933F 302207A WP CABIN FAILED A EIAA O OTHER O OTHER CR CRUISE 1 NM 09 945F 47279 SEA - AFTER APPROXIMATELY 20 MINUTES OF FLIGHT, THE RIGHT AFT (R3) WINDOW BEGAN MAKING A SHRILL NOISE AND WAS NOTED TO B E DELAMINATED. WITH FROZEN MOISTURE BETWEEN PLIES. (M) 2 L 7 2 4F A6WE 1999102900656 19991029 00656 NE 1999 10 29 EIAA980326 2 19981016 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE BIRDSTRIKE A EIAA O OTHER C F.O.D. NR NOT REPORTED 1 NM 09 485EV 20712 HKG - NR 1 ENGINE STALLED AFTER BIRDSTRIKE, EGT PEGGED GAUGE, N1, N2, EPR AND FUEL FLOW ROLLED BACK TO APPROX 60 PERCENT N1, NORMAL ENGINE OPERATION RETURNED AFTER APPROX 5 SECONDS. ENGINE WAS SHUTDOWN AND RETURNED TO HKG. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999102900658 19991029 00658 NM 1999 10 29 EIAA98100 1 19980302 A 5330 65B0793785 PANELS BOEING 747 747SR46 NM NLG NOT INSTALLED A EIAA O OTHER J W WARNING INDICATION INADEQUATE Q C CR CRUISE 1 NM 09 478EV 21033 PHIK - AFTER TWO HOURS OF FLIGHT, NOSE DOOR OPEN LIGHT CAME ON IN ALT, REFERENCE DMI NR 797 NOSE DOOR OPEN LIGHT IN PRIM ARY, ACCOMPANIED WITH A LOW RUMBLING NOISE. PERFORMED ALT GEAR EXTENSION OUT OF SEQUENCE PROCEDURES, LIGHT WENT OUT MOM ENTARILY BUT RE-ILLUMINATED. REDUCED DIFFERENTIAL PRESSURE TO 7 PSID, LIGHT WENT OUT FOR REMAINDER OF FLIGHT. FLIGHT R ETURNED TO PHIK. NOSE GEAR TRUNNION ACCESS PLATES NOT INSTALLED. INSTALLED PLATES, REPOSITIONS INSULATION, GROUND CHEC KED NORMAL. (M) 2 L 7 4 4F A20WE 1999102900659 19991029 00659 NE 1999 10 29 EIAA98095 2 19980224 A 7200 ENGINE BOEING 747 747212B 1384886 NM PWA JT9 JT9D7J 52054 NE NR 4 ENGINE BIRD STRIKE A EIAA A J UNSCHED LANDING DUMP FUEL D INFLIGHT SEPARATION CL CLIMB 1 NM 09 485EV 20712 662718 HKJK - AFTER TAKEOFF WHILE FLAPS WERE IN TRANSIT, AT ABOUT 800-1000 FT. NR 4 ENGINE FAILED DO TO BIRD STRIKE. TWO FAN BLADES ARE BROKEN OFF APPROX 14 INCHES FROM THE BLADE ROOT AND ALL OTHERS BLADES ARE DAMAGED. THE FAN CASE IS SPLIT ALL THE WAY AROUND APPROX 12 INCHES AFT OF THE FORWARD FLANGE. THE TAIL CONE, TAIL PIPE, INLET COWL AND FAN COWL ARE MISSI NG FROM THE ENGINE. DUMPED APPROX 90,000 LBS OF FUEL, DECLARED EMERGENCY AND RETURNED TO NAIROBI WITH AN UNEVENTFUL LAN DING. (M) 2 L 7 4 4F 4 F A20WE E20EA 1999110500432 19991105 00432 NM 1999 11 5 99ZZZM739 1 19980810 A 2611 308 BULB BOEING 727 727172C 1384058 NM SMOKE DETECTOR FAILED A RYNA K NONE L NO TEST IN INSP/MAINT 1 CE 07 527PC 19665 FLT 643 - SAN - MAIN CABIN SMOKE DETECTOR BULB LOWER LEFT BURNED OUT. RE-LAMPED LOWER LEFT SMOKE DETECTOR BULB. (M) 2 L 7 3 4F A3WE 1999110500433 19991105 00433 NM 1999 11 5 99ZZZM740 1 19980813 A 2611 308 BULB BOEING 727 727172C 1384058 NM SMOKE DETECTOR FAILED A RYNA K NONE O OTHER IN INSP/MAINT 1 CE 07 527PC 19665 FLT 644 - IAH - CARGO SMOKE DETECTOR LIGHT INOPERATIVE, LOWER LEFT. REPLACED LOWER LEFT BULB. (M) 2 L 7 3 4F A3WE 1999111900634 19991119 00634 EU 1999 11 19 UF6A981014 1 19981021 A 2611 WARNING LIGHT BAG ATP ATP EU COCKPIT ILLUMINATED A UF6A O OTHER N FALSE WARNING NR NOT REPORTED 1 GL 31 853AW 2022 ORD - FLT 5760 - MOMENTARY (20 SECONDS) SMOKE CWP ILLUMINATED DURING FLIGHT. MAINTENANCE INSPECTED BOTH NR 1 AND NR 2 E CS PACKS. COULD NOT DUPLICATE DISCREPANCY. (M) 2 L 7 2 4T RT A27NM 1999111900647 19991119 00647 1999 11 19 VTZA990201 4 19980630 A 3420 6226522008 ADI BAG JETSTM JETSTM3201 1500217 EU COCKPIT FAILED A VTZA A UNSCHED LANDING O OTHER CR CRUISE 1 EA 27 497UE 904 FLT 7251 - IAD-RIC - DURING CRUISE, AIRCRAFT MADE AN UNSCHEDULED LANDING DUE TO CAPTAINS ATTITUDE INDICATOR INOPERATIVE. AIRCRAFT RETURNED TO GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND REMOVED AND REPLACED ADI. OPS CHECK OK . AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M) 2 L 7 2 4T RT A56EU 1999121800747 19991218 00747 EA 1999 12 18 CA991103032 1 19981218 A 5230 95130345 ACTUATOR ROD 9513013 DHAV DHC8 DHC8311 1386006 EA CARGO DOOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 225 (CAN) 3 SHOOT BOLTS FOUND BROKEN ON CARGO COMPARTMENT ACCESS DOOR LATCH ASSY. 2 H 7 2 4T RT A13NM 2000012900334 20000129 00334 WP 2000 1 29 RRXA99971 1 19981110 A 3230 57583303 BUSHING DOUG DC8 DC863 302198A WP MLG MISMANUFACTURED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND BUSHING, LT MLG RETRACT PIN BOSS HOLD, BRUSH CAD PLATED IN PLACE OF DIP CAD PLATED. D AMAGE EXCEEDED LIMITS IAW DC-8 SRM. ACCEPTABLE CAD PLATE BUSHING IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO NR 057772 PROVIDED BY BOEING. 2 L 7 4 4F 4A25 2000012900335 20000129 00335 WP 2000 1 29 RRXA99972 1 19981103 A 3213 47783031 STRUT DOUG DC8 DC863 302198A WP LT MLG CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, LANDING GEAR WHEEL, RETRACT PIN BOSS, SHOCK STRUT, LT MLG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 5-1-1-8. FABRICATED AND INSTALLED BUSHING IAW FAA APP ROVED TIMCO DER ENGINEE RING SKETCH NR REO-05727. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900336 20000129 00336 WP 2000 1 29 RRXA99973 1 19981029 A 5315 561214255 FLOORBEAM DOUG DC8 DC863 302198A WP BS 1700 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND FLOORBEAM, AT STA= 1700, UPPER HORIZ FLANGES HAS MISDRILLED HOLES ENTIRE LENGTH OF FLO ORBEAM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05744. 2 L 7 4 4F 4A25 2000012900337 20000129 00337 WP 2000 1 29 RRXA99974 1 19981111 A 5730 57537362 SKIN DOUG DC8 DC863 302198A WP RT WING MISREPAIRED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, NUMEROUS BLENDOUTS, RIGHT WING LOWER SKIN BEAVER TAIL DOUBLER. DAMAGE EXC EEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05762. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).. 2 L 7 4 4F 4A25 2000012900338 20000129 00338 WP 2000 1 29 RRXA99975 1 19981030 A 3230 3755769507 BUSHING DOUG DC8 DC863 302198A WP MLG GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND GOUGED AND PITTING, BUSHING-FLANGED, PIVOT AXIS, MAIN LANDING GEAR. DAMAGE EXCEEDED L IMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDOUT LIMITS APPROVED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05756. 2 L 7 4 4F 4A25 2000012900339 20000129 00339 WP 2000 1 29 RRXA99977 1 19981210 A 5311 97549194 FRAME DOUG DC8 DC863 302198A WP BS 1200 & 1220 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND FRAMES AT STA= 1200 AND STA= 1220 INNER FLANGE HAD MISDRILLED HOLES BETWEEN LONGERONS 18 RIGHT AND LONGERON 20 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8 . INSTALLED FREEZE PLUG IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05696. 2 L 7 4 4F 4A25 2000012900340 20000129 00340 WP 2000 1 29 RRXA99978 1 19981022 A 5310 97540191 WEB DOUG DC8 DC863 302198A WP BS 295 & 325 CUT A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND FWD CARGO CROSS SLID WEB CUT TO FACILITATE OTHER MAINTENANCE AT STA= 295 AND STA= 325 AT LONGERON33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICAT ED AND INSTALLED REPAIRED WEB IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05695. 2 L 7 4 4F 4A25 2000012900341 20000129 00341 WP 2000 1 29 RRXA99979 1 19981019 A 5712 97532973 RIB DOUG DC8 DC863 302198A WP WS 540 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE INTORADIOUS OF RIGHT WING L/E RIB AT STA= 540. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW FAA APPR OVED TIMCO DER ENGINEERING SKETCH NR REO-05672. 2 L 7 4 4F 4A25 2000012900342 20000129 00342 WP 2000 1 29 RRXA99980 1 19981023 A 5751 57187534 HINGE DOUG DC8 DC863 302198A WP AILERON DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND HINGE FITTING, LEFT OUTBD AILERON, 2014-T6 FORG REQUIRED TO BE REPLACED. DAMAGE EXCEE DED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW FAA A PPROVED TIMCO DER ENGINEERING SKETCH NR REO-05711. 2 L 7 4 4F 4A25 2000012900343 20000129 00343 WP 2000 1 29 RRXA99981 1 19981211 A 5720 3640330 FLANGE DOUG DC8 DC863 302198A WP WS 436.5 & 456.5 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND OVERSIZED HOLES IN AFT UPPER SPAR FLANGE ON RIGHT WING BETWEEN XRS= 436.500 AND XRS = 456.563. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. OVERSIZED HOLES APPR OVED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05702. 2 L 7 4 4F 4A25 2000012900344 20000129 00344 WP 2000 1 29 RRXA99982 1 19981021 A 5311 56428567 FRAME DOUG DC8 DC863 302198A WP BS 717 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED HOLE ON FRAME, AT STA= 717 BETWEEN LONGERONS 20 LEFT AND LONGERON 21 LEF T AND LONGERONS 20 RIGHT AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05546. 2 L 7 4 4F 4A25 2000012900345 20000129 00345 WP 2000 1 29 RRXA99983 1 19981015 A 5712 97532974 RIB DOUG DC8 DC863 302198A WP WS 540 GOUGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND GOUGE IN RIB, L/W L/E AT STA= XFS= 540. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW FAA APPROVED TIMCO DER ENGIN EERING SKETCH NR REO-0565 3. 2 L 7 4 4F 4A25 2000012900346 20000129 00346 WP 2000 1 29 RRXA99984 1 19981013 A 5320 5641006501 FITTING DOUG DC8 DC863 302198A WP BS 759 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND DRILL START, ON FRAME FITTING LT SIDE AT STA= 759. DAMAGE EXCEEDED LIMITS IAW DC-8 SR M. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME FITTING REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR RE0-05620. 2 L 7 4 4F 4A25 2000012900347 20000129 00347 WP 2000 1 29 RRXA99985 1 19981022 A 5312 5753522 BULKHEAD DOUG DC8 DC863 302198A WP BS 1766 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND TRIPLE DRILLED RTAFT PRESS BULKHEAD, AT STA= 1766. DAMAGE EXCEEDED LIMITS IAW DC-8 SR M. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED MISDRILLED HOLES BY RIVET INSTALLATION IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05665. 2 L 7 4 4F 4A25 2000012900348 20000129 00348 WP 2000 1 29 RRXA99986 1 19981030 A 5312 57535223 BULKHEAD DOUG DC8 DC863 302198A WP BS 1766 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, AFT PRESS BULKHEAD, AT STA= 1766. DAMAGE EXCEEDED LIMITS IAW DC- 8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER TO BULKHEAD WEB IA W FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05659. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000012900349 20000129 00349 WP 2000 1 29 RRXA99987 1 19981028 A 5320 5641008502 FITTING DOUG DC8 DC863 302198A WP BS 798 MISDRILLED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND (1) DISCREPANT HOLE (3/16) DIA LOCATED ON EDGE OF FITTING 6 ABOVE RT CUSP AT STA= 798. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REP AIR ANGLE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05657. 2 L 7 4 4F 4A25 2000012900350 20000129 00350 WP 2000 1 29 RRXA99988 1 19981015 A 5311 561386177 FRAME DOUG DC8 DC863 302198A WP BS 18.875 CRACKED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND CRACKED CHANNEL FRAME AT STA= 18.875 AT LONGERON 31 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED T IMCO DER ENGINEERING SKETCH REO NR 05642. 2 L 7 4 4F 4A25 2000012900351 20000129 00351 WP 2000 1 29 RRXA99989 1 19981106 A 5311 97540023 FRAME DOUG DC8 DC863 302198A WP BS 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND 3 EACH DRILLED HOLES CLOSE TO RADIUS ON FRAME AT STA= 280 AT LONGERON 25 RIGHT. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED D OUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05617. 2 L 7 4 4F 4A25 2000012900352 20000129 00352 WP 2000 1 29 RRXA99992 1 19981012 A 5311 5751008501 FRAME DOUG DC8 DC863 302198A WP BS 520 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MX VISIT, FOUND DRILL DAMAGE, INCLUDING DOUBLE HOLES AND HOLES IN THE RADIUS, ON THE FRAME, STA= 520 AT LONGERO N 20 LEFT AND BETWEEN LONGERONS 6 RT TO LONGERON 9 RT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED A REA IAW DC-8 SRM 51-1-8. AT LONGERON 20 LEFT, FABRICATED AND INSTALLED ANGLE; BETWEEN LONGERONS 6 RIGHT TO 7 RIGHT, FAB RICATED AND INSTALL REPAIR ANGLE; AND BETWEEN LONGERONS 8 RIGHT AND 9 RIGHT, FABRICATED AND INSTALLED A FLUSH BUSHING A ND ANGLE; ALL IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR RE0-05591. 2 L 7 4 4F 4A25 2000012900354 20000129 00354 WP 2000 1 29 RRXA99994 1 19981112 A 5311 5751991501 FRAME DOUG DC8 DC863 302198A WP BS 940 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES, FRAME UPPER FUSELAGE, AT STA= 940, LONGERON 7 LEFT, COMMON TO INBOAR D FLANGE IN THE CABIN AREA. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. F ABRICATED AND INSTALLED REPAIRED DOUBLER IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR RE0-05618. 2 L 7 4 4F 4A25 2000012900355 20000129 00355 WP 2000 1 29 RRXA99995 1 19981012 A 5311 564286178 FRAME DOUG DC8 DC863 302198A WP BS 834 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES, FROM PREVIOUS MOD, ON FRAME, UPPER CABIN AT STA= 834, COMMON TO INNE R FLANGE AT VARIOUS LOCATIONS FROM CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IA W DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLERS IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-0556 8. 2 L 7 4 4F 4A25 2000012900356 20000129 00356 WP 2000 1 29 RRXA99996 1 19981008 A 5311 564250019 FRAME DOUG DC8 DC863 302198A WP BS 702 DAMAGED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE ON FRAME AT STA= 702 BETWEEN LONGERONS 4 LEFT AND LONGERON 6 LEFT. DAMAG E EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FILLER AND ANGLE IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05550. 2 L 7 4 4F 4A25 2000012900357 20000129 00357 WP 2000 1 29 RRXA99997 1 19981015 A 5311 5754671505 FRAME DOUG DC8 DC863 302198A WP BS 260 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND (4) DRILL STARTS ON TOP OF FRAME BETWEEN LONGERONS 31 LEFT AND LONGERON 35 RIGHT AT ST A= 260. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTAL LED REPAIR DOUBLER AND STRAP IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05580. 2 L 7 4 4F 4A25 2000012900358 20000129 00358 WP 2000 1 29 RRXA99998 1 19981215 A 5230 K5230511 SKIN DOUG DC8 DC863 302198A WP CARGO DOOR DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, INNER SKIN OF MAIN CARGO DOOR, NUMEROUS AREAS. DAMAGE EXCEEDED LIMITS I AW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT INNER SKIN PANEL AND WEB IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05572. 2 L 7 4 4F 4A25 2000012900359 20000129 00359 WP 2000 1 29 RRXA99999 1 19981012 A 5313 LONGERON DOUG DC8 DC863 302198A WP BS 160 - 180 DAMAGED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 964R 46000 DURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, LONGERON 25 LEFT THROUGH AND INCLUDING LONGERON 28 LEFT BETWEEN STA= 160 AND STA= 180. A CARGO MOD (PREVIOUS) LEFT AREAS OF DOUBLE DRILLED HOLES IN ABOVE LOCATIONS. DAMAGE EXCEEDED LIMITS IA W DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH NR REO-05610. 2 L 7 4 4F 4A25 2000012900369 20000129 00369 WP 2000 1 29 RRXA991011 1 19980905 A 5530 ANGLE DOUG DC8 DC871F 302199D WP VERTICAL STAB CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 8084U 45974 DURING A MAINTENANCE VISIT, FOUND CORROSION, VERTICAL STABILIZER, ATTACHMENT ANGLE BETWEEN STA 1750 AND STA 1790 AND LON GERON 2 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER TIE IAW DC8 SRM 53-2-5 FIGURE 16A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900391 20000129 00391 WP 2000 1 29 RRXA991038 1 19981114 A 5330 SKIN DOUG DC8 DC873F 302199F WP BS 190 - 440 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 602AL 45991 DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 190 TO STA 440 AND BETWEEN LONGERO NS 31 LEFT TO 31 RIGHT. REMOVED DAMAGED SKIN, TREATED AREA IAW DC-8 SRM 51-1-8.. RECEIVED NEW SKIN PANEL AND INSTALLED IAW 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F RT 4A25 2000012900510 20000129 00510 WP 2000 1 29 RRXA991163 1 19981219 A 5347 SEAT TRACK DOUG DC8 DC862F 3021972 WP BS 789 CORRODED A RRXA K NONE O OTHER IN INSP/MAINT 1 WP 15 996CF 46162 DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 798 AND BL 48 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER SPLICE IAW DC-8 SRM 53-2-3 PAGES 49 AND 50. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM). 2 L 7 4 4F 4A25 2000020500937 20000205 00937 EU 2000 2 5 2000ZZZX269 1 19981103 A 2810 FTH14859 FUEL CELL BOLKMS 105 BO105S 5626006 EU FUSELAGE LEAKING A A RMXA O OTHER K FLUID LOSS NR NOT REPORTED 1 SW 05 105NG S632 REPLACED FUEL CELL AND MAINS. P/N FTA0175200, S/N 43089. DEPARTED ON SCENE RUN AT 0628. LANDED ON A PAVED ROAD. DEPA RTED WITH PATIENT AND LANDED ON ROOF OF HOSPITAL. DURING 2 MINUTE COOL-DOWN OF ENGINES, PARAMEDIC GOT OUT AND NOTIFIED OF A LEAK UNDER THE ACFT. SMELLED FUEL AND SHUT DOWN THE ACFT. FUEL WAS LEAKING RAPIDLY AND STEADILY FROM A DRAIN HOLE IN THE CENTER OF THE BELLY. DEPARTED MADISON WITH 1+30 IN THE MAIN TANK. FLEW A 0.9 AND LANDED WITH 30 GALLONS (0+30) IN THE MAIN TANK. ESTIMATE LOSING NO MORE THAN 10 TO 15 GALLONS TOTAL. A WITNESS TO THE LANDING SAID THE ACFT WAS LEAK ING FUEL BADLY ON FINAL APPROACH. THE FUEL GAUGE IS ONLY ACCURATE WHEN THE ACFT IS ON THE GROUND. 1 G 7 2 3U H3EU 2000020500938 20000205 00938 EA 2000 2 5 2000ZZZX270 2 19980909 A 8520 PISTON PIN HUGHES 269 269C 4470504 WP LYC O360 HIO360D1A 41514 EA NR 4 CYLINDER BROKEN A L A TL8A K NONE O OTHER IN INSP/MAINT 1 AL 05 6129M 573 S1509 2552151A C/W ROUTINE 50-HOUR OIL CHANGE. FOUND CHUNK OF ALUMINUM IN DRAIN PLUG, ALUM FND IN OIL SCREEN, FILTER. PULLED ALL SPAR K PLUGS, FOUND OIL ON NR 4 CYL PLUGS. PULLED NR 4 CYL. FOUND NO PISTON PIN CAPS IN PLACE AND A LARGE CHUNK OF MATERIAL BROKEN OFF INSIDE OF PISTON AND NOTICED THE PISTON PIN HAD BEEN CONTACTING THE CYL WALL IN 2 PLACES LEAVING GROOVES .25 INCH WIDE AND ABOUT .1250 INCH DEEP IN WALL OF CYLINDER. TEXTRON LYC STATED IT WAS CAUSED BY CORROSION AND ENG WOULD H AVE TO BE SHIPPED BACK. LYC RECOMMENDED REMOVING ROD BEARING AND LOOK FOR DAMAGE, FND LIGHTLY DAMAGED BY PISTON DEBRIS. REMOVED REMAINING 3 CYLS, PISTON PIN CAPS IN PLACE, SHOWED LIGHT WEAR. REINSTALLED ALL CYLS AND SHIPPED ENG TO LYC. 1 G 7 1 3O 3 O 4H12 1E10 2000022600700 20000226 00700 WP 2000 2 26 2000ZZZX457 1 19980212 A 5330 SKIN DOUG DC8 DC851 3021920 WP BS 1050-1140 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 508DC 45935 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FUSELAGE CORROSION DAMAGE AT STA 1050 TO STA 1140, LONGERONS 34LT TO 30 RT. REPAIRED CORROSION DAMAGE IAW FINE AIRLINES EO 9709021 AND SRM 51-1-21. (X) 2 L 7 4 4F 4A25 2000022600701 20000226 00701 WP 2000 2 26 2000ZZZX458 1 19980212 A 5751 SKIN DOUG DC8 DC851 3021920 WP AILERON CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 508DC 45935 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE AT LOWER OUTBOARD AILERON RIGHT. REPAIRED CORROSION D AMAGE IAW FINE AIRLINES EO 9802041 AND SRM 51-4-3. (X) 2 L 7 4 4F 4A25 2000022600705 20000226 00705 WP 2000 2 26 2000ZZZX462 1 19981208 A 5522 SKIN DOUG DC8 DC8F54 3021926 WP ELEVATOR CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 427FB 45684 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE AT STA XE 133 TO 246 ELEVATOR LEFT. REPAIRED CORROSIO N DAMAGE IAW FINE AIRLINES EO 9811091. (X) 2 L 7 4 4F 4A25 2000022600706 20000226 00706 WP 2000 2 26 2000ZZZX463 1 19981208 A 5512 SKIN DOUG DC8 DC8F54 3021926 WP HORIZONTAL STAB CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 427FB 45684 DURIGN C-CHECK INSPECTION, FOUND THE FOLLOWING: CORROSION DAMAGE AT STA XE149 HORIZONTAL STABILIZER, LEFT. REPAIRED COR ROSION DAMAGE IAW FINE AIRLINES EO 9800071. (X) 2 L 7 4 4F 4A25 2000022600709 20000226 00709 WP 2000 2 26 2000ZZZX466 1 19981111 A 5315 FLOORBEAM DOUG DC8 DC8F54 3021926 WP BS 802-859 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 57FB 45669 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORRROSION DAMAGE AT STA FS 820 - FS 859, LEFT. REPAIRED CO RROSION DAMAGE IAW FINE AIRLINES EO 9810161. (X) 2 L 7 4 4F 4A25 2000022600710 20000226 00710 WP 2000 2 26 2000ZZZX467 1 19981111 A 5315 FLOORBEAM DOUG DC8 DC8F54 3021926 WP BS 940 CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 57FB 45669 DURING C-CHECK INSPECTION, FOUND THE FOLLOWING: FLOORBEAM CORRROSION DAMAGE AT STA FS 940. REPAIRED CORROSION DAMAGE I AW FINE AIRLINES EO 9810211. (X) 2 L 7 4 4F 4A25 2000030400056 20000304 00056 WP 2000 3 4 2000ZZZM246 1 19980831 A 5522 SKIN DOUG DC8 DC8F55 3021928 WP ELEVATOR CORRODED A FXLA K NONE O OTHER IN INSP/MAINT 1 SO 19 55FB 45678 DURING D-CHECK INSPECTION, FOUND THE FOLLOWING, CORROSION DAMAGE AT LEFT AND RIGHT ELEVATOR SKIN. REPAIRED CORROSION DA MAGE IAW FINE AIR EO NR 9808061, SRM 51-1-21. (M) 2 L 7 4 4F 4A25 2000041700118 20000417 00118 EU 2000 4 17 CA000209027 1 19980210 A 6710 35040001421 LOCK 350400004 SNIAS 350 AS350B2 8680813 EU COLLECTIVE OUT OF ADJ W O OTHER F FLT CONT AFFECTED IN INSP/MAINT 1 CA (CAN) WHILE CARRYING OUT PRACTICE AUTOROTATION, THE COLLECTIVE LEVER LOCK ENGAGED SOME TIME DURING DESCENT AND THE COLLE CTIVE LEVER WAS NOW IN THE FULLY DOWN POSITION AND WOULD NOT UNLOCK. A CONTROLLED BUT FIRM LANDING WAS CARRIED OUT. STC SH96-32 LEFT-SIDE PILOT CONFIGURATION WAS INSTALLED ON THIS ROTORCRAFT WITH THE PILOT IN THE LT SEAT AND THE STUDENT IN THE RT SEAT. IT WAS LATER DETERMINED THAT THE LOCKING DEVICE WAS IMPROPERLY ADJUSTED. 1 G 7 1 3U H9EU 2000042000161 20000420 00161 CE 2000 4 20 CA971104005 1 19980331 A 2700 500000863 CONTROL CABLE CESSNA 414 414A 2075907 CE CONT O520 TSIO520NB 17040 SO MCAULY 3AF32C 3AF32C505 GL TE FLAP FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION, WIRES/STRANDS OF FLAP CABLE ASSY WERE FOUND BROKEN. NEW CABLE INSTALLED AND SYSTEM RIG GED. 1 L 7 2 3O 3 O A7CE E8CE 5 C P22EA 2000042800024 20000428 00024 NM 2000 4 28 20000428AP007 1 19980715 A 3230 87003 PSEU DORNER DO32 DO328100 2996000 NM MLG FAILED A EQGA A UNSCHED LANDING J WARNING INDICATION AP APPROACH 1 SW 19 335PH 212 3013 DFW - FLT 177 - ON APPROACH INTO BRANSON, THE LANDING GEAR WAS EXTENDED AND RECEIVED A PROXY SYSTEM FAIL MESSAGE ON THE CAS PAGE, THE MESSAGE WOULD NOT CLEAR SO EXECUTED A MISSED APPROACH AND RETURNED TO DFW AIRPORT WHERE MAINTENANCE PERSON NEL REPLACED THE PSEU BOX AND CLEARED THE PROBLEM. (M) 2 H 7 2 4T RT A45NM 2000050200362 20000502 00362 2000 5 2 20000428AP006 4 19980715 A 3140 INDICATOR DORNER DO32 DO328100 2996000 NM COCKPIT MALFUNCTIONED A EQGA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 SW 19 340LS 3040 FLT 358 - DURING TAKEOFF ROLL, THE FIRST OFFICER NOTICED THAT THERE WAS NO INDICATION FOR THE AUTO FEATHER SYSTEM ON THE ICAS PAGE HE THEN LOOKED ON THE OVER TO SEE IF IT WAS ARMED, THERE WAS NO INDICATION OF IT BEING ARMED. AT THAT TIME W E INITIATED AN ABORTED TAKEOFF AND RETURNED TO THE TERMINAL TO HAVE MAINTENANCE TO TAKE A LOOK AT THE AIRCRAFT. MAINTEN ANCE PERFORMED GROUND RUNS AND TEST ON THE AUTO FEATHER SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. (M) 2 H 7 2 4T RT A45NM 2000051600096 20000516 00096 SO 2000 5 16 CA971006007 1 19980423 A 2752 475208 RELAY DUKES 1202001 PIPER PA31 PA31 7103102 SO LYC O540 TIO540A2B 41532 EA TE FLAP MOTOR CORRODED W H DEACTIVATE SYST/CIRCUITS F FLT CONT AFFECTED CL CLIMB 1 CA 1749 4857 L163261 (CAN) FLAP MOTOR INTERMITTENT ON TAKEOFF AND LANDING. MAINTENANCE FOUND RELAY OF MOTOR PITTED. FLAP MOTOR WAS REPLACE D. 1 L 7 2 3O 3 O A20SO E14EA 2001011101455 20010111 01455 EU 2001 1 11 QXEA9801598 1 19980928 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX-DENT IN PASSENGER DOOR SKIN 13 INCHES FROM BOTTOM EDGE OF DOOR. DENT PLACED ON THE YELLOW SPOT PROGRAM IAW HORIZON A IR GMM 5-5.0 REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3, FIGURE 2. 2 L 7 2 4F RT A20EU 2001011101457 20010111 01457 EU 2001 1 11 QXEA9801600 1 19980929 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX- (UPDATE FOR OPEN SDR) DENT IN PASSENGER DOOR SKIN 24 INCHES FROM HINGE 14 1/2 INCHES AFT OF FORWARD EDGE, PLACED DE NT ON YELLOW DOT PROGRAM IAW HORIZON AIR GMM 5-5.0. REPAIRED IAW FOKKER SRM 52-02-02, FIGURE 1, PAGE 2 & 3. 2 L 7 2 4F RT A20EU 2001011101456 20010111 01456 EU 2001 1 11 QXEA9801599 1 19981021 A 5210 SKIN FOKKER F28 F28MK4000 4990810 EU PAX DOOR DENTED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 480AU 11229 PDX-(UPDATE FOR OPEN SDR) DENT IN PASSENGER DOOR SKIN 33 INCHES FROM BOTTOM EDGE OF DOOR, 22 INCHES BACK FROM FORWARD ED GE. PLACED DENT ON YELLOW DOT PROGRAM IAW HORIZON AIR GMM 5-5.0. REPAIRED IAW FOKKER SRM 52-02-02, FIGURE 1, PAGE 2 & 3. 2 L 7 2 4F RT A20EU 2001020600068 20010206 00068 SW 2001 2 6 20000713SH015 1 19981229 A 2911 223002 ACCUMULATOR SWRNGN SA227 SA227AC 8780603 SW LT WW FAILED D A UNSCHED LANDING J K WARNING INDICATION FLUID LOSS CL CLIMB 1 GL 27 387PH AC531 FOLLOWING TAKEOFF, GEAR WAS RETRACTED NORMALLY WHEN BOTH HYDRAULIC FLOW WARNING LIGHTS ILLUMINATED THE GEAR WAS IMMEDIAT ELY EXTENDED AND AN UNEVENTFUL LANDING WAS MADE. UPON INSPECTION, DISCOVERED THE HYDRAULIC ACCUMULATOR HAD BURST. THE DATE OF MFG ON THIS ITEM WAS 2Q94 AND WAS IN GOOD CONDITION. FATIGUE OR POSSIBLY A LOSS OF PRE-CHARGE PRESSURE MAY HAVE CAUSED THIS FAILURE. (X) 2 L 7 2 4T RT A8SW 2001032100066 20010321 00066 NE 2001 3 21 CA980225016 2 19980216 A 7230 CASE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524* NE ACCOUSTIC PANEL DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) VIBRATION FELT IN AFT CABIN WHEN THE N1 IS ABOVE 86% ON THE #2 ENGINE. ALL COCKPIT INDICATIONS WERE NORMAL. DAMAGE FOUND ON THE ACCOUSTIC PANEL AT LP COMPRESSOR (FAN) CASING 4-6 O''''CLOCK POSITION, WITHSOME DEBRIS STUCK ON THEO.G.V., CAUSING TURBULENT FLOW IN THE COLD STREAM AREA. REPAIR CARRIED OUT ON ACCOUSTIC PANEL. 2 L 7 3 4F 4 F A23WE E12EU 2001032100067 20010321 00067 NE 2001 3 21 CA980225017 2 19980216 A 7250 BLADE LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524* NE HP TURBINE DAMAGED W E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 CA (CAN) NR 3 ENGINE INFLIGHT SHUTDOWN DUE TO HIGH VIBRATION CONFIRMED ON BOTH CHANNELS. BORESCOPE INSPECTION REVEALED NR 1 STAGE HP TURBINE BLADE FAILURE AND SUBSEQUENT DAMAGES. 2 L 7 3 4F 4 F A23WE E12EU 2001032100069 20010321 00069 CE 2001 3 21 CA980225021 1 19980214 A 3230 11581006051 DOOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG OUT OF ADJ W O OTHER J WARNING INDICATION CL CLIMB 1 CA 11193 (CAN) PILOTS REPORTED GEARS STAYED IN TRANSIT ON UP/DOWN SELECTION. GEAR ALSO FAILED TO EXTEND MANUALLY. GEAR FINALLY SH OWED THREE GREEN AND AIRCRAFT LANDED OK. MAIN LANDING GEAR DOORS CLOSING TOO TIGHT, OUT OF ADJUSTMENT. REPAIRED. 1 L 7 2 3T 4 T A14CE E4EA 2001032100078 20010321 00078 NM 2001 3 21 CA980303001 1 19980224 A 5340 200009002 FITTING PIPER 200028508 PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA WING SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 2720 (CAN) STBD MAIN SPAR-TO-FUSE FITTING 2 MOST INNER JO-BOLTS FASTENERS SHEARED 5/16INCH BELOW HEAD. REPLACED. 1 M 7 2 3O 3 O RT A17WE 1E4 2001032100079 20010321 00079 NM 2001 3 21 CA980303004 1 19980224 A 3230 NAS313241440 RELEASE CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG DOOR ALT WORN W K NONE O OTHER IN INSP/MAINT 1 CA 18050 (CAN) LEFT HAND MAIN LANDING GEAR DOOR ALTERNATE RELEASE CABLE WORN WHERE IT PASSES UNDER PULLEY GUARD PIN. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032100086 20010321 00086 NE 2001 3 21 CA980305005 2 19980218 A 7260 3022375 GARLOCK SEAL HAMSTD 7863913L13 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE WORN W C ABORTED TAKEOFF K J FLUID LOSS WARNING INDICATION TO TAKEOFF 1 CA F249 (CAN) AIRCRAFT ABORTED TAKEOFF DUE TO #2 ENGINE OIL PRESSURE FLUCTUATING 45-60 POUNDS. INSPECTION FOUND THE HYDRO MECHAN ICAL UNIT FUEL PUMP GARLOC SEAL LEAKING. THE GARLOC SEAL WAS REPLACED AND THE AIRCRAFTRETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032100088 20010321 00088 2001 3 21 CA980305009 4 19980216 A 3425 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE COCKPIT ACTIVATED W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 4944 (CAN) TAKEOFF REJECTED AT APPROXIMATELY 90 KNOTS AS ELECTRONIC FLIGHT INSTRUMENT SYSTEM HEADING REFERRING FLAG UP. RESET ARINC COMMUNICATIONS AND REPORTING SYSTEM. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032100089 20010321 00089 EU 2001 3 21 CA980305011 1 19980127 A 5753 D5757007420600 BEARING AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE NR 3 RT TE FLAP CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 20530 (CAN) NR 3 RT FLAP SUPPORT BEARING (JOINT) CRACKED. BEARING REPLACED. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032100090 20010321 00090 NE 2001 3 21 CA980305014 2 19980209 A 7230 433802 BLADE DOUG DC9 DC9 3022002 WP PWA JT8 JT8D7B 52053 NE LP COMPRESSOR BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 2110 (CAN) DURING REGULAR SHOP VISIT A 2ND STAGE LP COMPRESSOR BLADE WAS FOUND WITH ONE LUG OF THE REAR STRAP BROKEN OFF. 2 L 7 2 4F 4 F A6WE E2EA 2001032200001 20010322 00001 CE 2001 3 22 CA980309004 1 19980227 A 2730 1016100197 HORN BEECH 1900 1900D 1154162 CE PWA PT6 PT6A67D NE HARTZL HCE4A HCE4A3A NE LT & RT ELEVATOR LOOSE W O OTHER E F VIBRATION/BUFFET FLT CONT AFFECTED CR CRUISE 1 CA 5352 (CAN) FLIGHT CREW REPORTED A VIBRATION IN CERTAIN FLIGHT CONDITIONS. ATTACH RIVETS ON LT AND RT ELEVATOR CONTROL HORNS W ERE LOOSE AND WOULD CAUSE VIBRATION IN FLIGHT. HORNS REPLACED. 2 L 7 2 4T 4 T RT A24CE E26NE 5 C P10NE 2001032200007 20010322 00007 EU 2001 3 22 CA980309012 1 19980221 A 2750 COMPUTER AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE FLAP / SLAT MALFUNCTIONED W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 20670 (CAN) FLAP LOCKED ON FIRST SELECTION DURING APPROACH. CARRIED OUT ELECTRONIC CENTRALIZED AIRCRAFT MONITORING (ECAM). AFT ER LANDING RESET FLAP / SLAT CONTROL COMPUTER NR 1 & 2. CONTROL SYSTEM PRESSURIZED WITH YELLOW PUMP, AFTER ENGINE START FLAPS CYCLED NORMAL. WING TIP BRAKE RESET BOTH SLAT AND FLAPS SLAT CONTROL COMPUTER NR 1 AND 2, FLAP OPERATION NORMAL. 2 L 7 2 4F 4 F RT A28NM E29NE 2001032200008 20010322 00008 EA 2001 3 22 CA980309013 1 19980224 A 3150 WARNING SYSTEM CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE TE FLAPS ACTIVATED W O OTHER J WARNING INDICATION AP APPROACH 1 CA 7144 (CAN) WHILE SLOWING THROUGH 215 KNOTS, FLAPS SELECTED TO 8 DEGREES, FLAP FAIL CAUTION MESSAGE ON, FLAPS REMAINED AT 0 DE GREES. LANDING UNEVENTFUL. FLAP ECU SHOWS BOTH CHANNELS FAIL, RESET OK. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032200021 20010322 00021 CE 2001 3 22 CA980311019 1 19980309 A 3233 SHAFT ADI79990033 BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG ACTUATOR CORRODED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1070 202A (CAN) HYD FLUID LEAKING FROM MLG ACTUATOR PISTON. PISTON PITTED WITH CORROSION AT CONTACT POINT OF FELT WIPER. REPLACD. 1 L 7 2 3T 4 T A14CE E4EA 2001032200022 20010322 00022 CE 2001 3 22 CA980311020 1 19980309 A 5330 5012006896 SKIN BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 10265 (CAN) 2 CRACKS FOUND IN SKIN AT OUTER MOST HUCK BOLT, 4.5 INCHES FROM PARTING LINE BETWEEN CENTRE SECTION AND L/H WING P ANEL. ONE CRACK IS .750 INCH LONG AND RUNS FROM LEADING EDGE OF SKIN AROUND HUCK BOLT HEAD AND BEYOND. SECOND CRACK .250 COMES OUT FROM UNDER HUCK BOLT HEAD RUNNING INBD & AFT. THE HUCK BOLT SECURES FWD STAR AFT CAP TO FWD UPPER BATHTUB FIT TING. 1 L 7 2 3T 4 T A14CE E4EA 2001032200023 20010322 00023 CE 2001 3 22 CA980311021 1 19980309 A 3233 PISTON BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA ACTUATOR CORRODED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 1070 202B (CAN) HYD FLUID LEAKING FROM MLG ACTUATOR AT POINT WHERE THE WIPER SEAL CONTACTS THE PISTON. PITTING DUE TO CORROSION. R EPLACED. 1 L 7 2 3T 4 T A14CE E4EA 2001032200033 20010322 00033 EA 2001 3 22 CA980317001 1 19980108 A 7712 311555701 PROBE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE TORQUE SENSOR FAULTY W C ABORTED TAKEOFF R J PARTIAL RPM/PWR LOSS WARNING INDICATION TO TAKEOFF 1 CA (CAN) TAKEOFF REJECTED DUE TO NR 2 ENGINE TORQUE DROPPING TO ZERIO. NR 2 ECU WENT TO MANUAL DURING RUNWAY EXITING, ALL E NGINE INDICATIONS RETURNED TO NORMAL. AT RAMP WHEN FEATHERING PROP ENGINE TORQUE STARTED TO RISE. NR 2 ENGINE WAS SHUTDO WN. TORQUE GAUGE FAULT CODE SHOWED PROBE FAILURE. TORQUE SENSOR WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032200034 20010322 00034 NE 2001 3 22 CA980317003 2 19980206 A 7322 7863916 HYDRO MECH UNIT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE POTENTIOMETER ERRATIC W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 3851 (CAN) TAKEOFF REJECTED DUE TO NR 1 ENGINE TORQUE FLUCTUATING BETWEEN 85-95 PERCENT. HYDRO MECHANICAL UNIT (HMU) TESTED, FAILED DELASTIC POTENTIOMETER TEST. HMU REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032200035 20010322 00035 NE 2001 3 22 CA980317005 2 19980206 A 7230 FAN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 ENGINE SEIZED W E A ENGINE SHUTDOWN UNSCHED LANDING Y J ENGINE STOPPAGE WARNING INDICATION CL CLIMB 1 CA 19172 3681 (CAN) JUST AFTER GEAR-UP ON DEPARTURE NR 1 ENGINE GAVE A LOUD BANG WITH ACCOMPANYING TAIL PIPE FLAME. NR 1 ENGINE SHUTDO WN. AIRCRAFT RETURNED FOR A NORMAL LANDING. POST FLIGHT INSPECTION FOUND THE ENGINE FAN SEIZED. THE ENGINE WAS REPLACED. 2 H 7 4 4F 4 F RT A49EU E6NE 2001032200036 20010322 00036 NE 2001 3 22 CA980317009 2 19980212 A 7322 7863916 HYDRO MECH UNIT DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE FAULTY W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 9552 1004 (CAN) DURING CLIMB AT FL200 NR 1 ENGINE TORQUE STARTED TO DECREASE. WITH NR 1 ENGINE POWER LEVER FULLY FORWARD NR 1 ENGI NE TORQUE WAS 20 PERCENT LOWER THAN NR 2 ENGINE. AIRCRAFT DIVERTED. HYDRO MECHANICAL UNIT (HMU) AND FUEL PUMP REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032200037 20010322 00037 NE 2001 3 22 CA980317010 2 19980212 A 7230 COMPRESSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 2 ENGINE LEAKING W O OTHER K B J FLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CR CRUISE 1 CA 12716 (CAN) DURING CRUISE A SLIGHT SMELL / HAZE WAS NOTICED IN THE CABIN. NR 2 ENGINE BLEED AIR TURNED OFF. POST FLIGHT INSPEC TION FOUND THE ENGINE CONDITION PANEL SHOWED A CHIP DETECTOR FLAG. NR 2 ENGINE OIL FILTER AND CHIP DETECTOR FOUND WITH M ETAL CONTAMINATION. OIL CONTAMINATION OF NR 2 ENGINE AIR INTAKE FOUND TO BE COMING FROM THE AFT OF THE LOW PRESSURE COMP RESSOR. THE NR 2 ENGINE WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032200038 20010322 00038 NM 2001 3 22 CA980317012 1 19980209 A 2731 82760174005 JACKSCREW DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE ELEVATOR TRIM FROZEN W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 CA (CAN) DURING CLIMB AND CRUISE THE CREW WAS UNABLE TO MOVE THE ELEVATOR TRIM OR THE STANDBY ELEVATOR TRIM. AIRCRAFT RETU RNED FOR NORMAL LANDING OK. ELEVATOR TRIM JACKS LUBED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032200040 20010322 00040 EU 2001 3 22 CA980317014 1 19980201 A 3242 MS21902W6 FITTING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE PARK BRAKE CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA (CAN) HYD LEAK TRACED TO UNION FITTING AT HIGH PRESSURE MANIFOLD TO PARK BRAKE LINE. 2 H 7 4 4F 4 F RT A49EU E6NE 2001032200041 20010322 00041 NM 2001 3 22 CA980317015 1 19980304 A 3260 864202 SENSOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT WOW OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 CA (CAN) AFTER DEPARTURE THE WOW CAUTION LIGHT CAME ON. RIGHT HAND WOW SENSOR GAP ADJUSTED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032200042 20010322 00042 EA 2001 3 22 CA980317016 1 19980228 A 3246 L713049 BEARING DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE WHEEL FAILED W O OTHER O OTHER LD LANDING 1 CA (CAN) AFTER LANDING NR 2 MAIN WHEEL BEARING FOUND FAILED, CAUSING DAMAGE TO WHEEL ASSY, BRAKE ASSY, AND AXLE.WHEEL, BRAK E, WHEEL NUT AND MLG SHOCK STRUT ASSY. REPLACED. NR 2 WHEEL ASSY. HAD BEEN ON FOR 909 CYCLES. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032200043 20010322 00043 NM 2001 3 22 CA980317017 1 19980219 A 3242 MS2125006008 BOLT 314354 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE BRAKE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA 1448 (CAN) INSPECTION OF NR 1 BRAKE ASSY, FOUND THAT 2 OF THE 6 TIE BOLTS WERE MISSING.3 OF THE 4 REMAINING HAD BACKED OFF.BR AKE ASSY. REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032200047 20010322 00047 NE 2001 3 22 CA980317022 2 19980205 A 7261 734340 DRIVE GEAR PWA JT8D9A BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE OIL PUMP STRIPPED W K NONE O OTHER IN INSP/MAINT 1 CA 32735 707313 (CAN) NR 1 ENGINE ON WATCH FOR EXCESSIVE OIL CONSUMPTION. DURING TROUBLESHOOTING THE DRIVE GEAR (SPUR GEAR) FOR THE ENGI NE OIL PUMP WERE FOUND STRIPPED. THE ENGINE WAS REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2001032200048 20010322 00048 NM 2001 3 22 CA980317037 1 19980313 A 2750 MS172272 WASHER BOEING 65502535 BOEING 737 737275 1384485 NM PWA JT8 JT8D9A 52048 NE TRANSMISSION WORN W A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION AP APPROACH 1 CA 2592 2592 148 (CAN) A/C RETURNED DUE TO FLAPS WOULD NOT LOWER PAST 10 UNITS ON APPROACH. FOUND WASHER RETAINING WASHER AND NUT P/N 69- 52435-1, BACKED OFF OF DRIVE SHAFT. TRANSMISSION REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 2001032200053 20010322 00053 NM 2001 3 22 CA980317054 1 19980309 A 5341 BOLT PIPER 200010001 PIPER PA60 PA60600 7106001 NM LYC O540 IO540K1J5 41532 EA FITTING SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA 2546 (CAN) THE PORT MAIN SPAR TO FUSELAGE FITTING ONE OF THE INBOARD JO-BOLTS FOUND SHEARED. FASTENER FOUND PROTRUDING APPROX .010 INCH.FASTENER SHEARED 3/8 INCH BELOW TOP OF FASTENER. BOTH INBOARD FASTENERS REPLACED. 1 M 7 2 3O 3 O RT A17WE 1E4 2001032200079 20010322 00079 SW 2001 3 22 CA980317093 1 19980305 A 2612 FIRE DETECTOR SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP RIGHT WING INTERMITTENT W D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 CA 41413 (CAN) RIGHT WING OVERHEAT LIGHT FLICKERED ON JUST PRIOR TO TAKEOFF. THE FIRE DETECT CIRCUIT WAS GROUNDING CAUSING AN IN TERMITTENT LIGHT. REWIRED WING O/H DETECT SYSTEM, REPLACED THE 250 DEGREE SENSOR AND REPLACED THE WHEEL WELL 550 DEGREE O/H DETECTOR. ALSO REPLACED CONNECTOR P1 ON ANNUNCIATOR PANEL AS IT APPEARED BADLY WORN. 2 L 7 2 4T 4 T RT A8SW E4WE 2001032200080 20010322 00080 SW 2001 3 22 CA980317095 1 19980309 A 2613 WIRE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE3313UW 01514 WP LEFT WING BROKEN W K NONE L NO TEST IN INSP/MAINT 1 CA 14190 (CAN) WING OVERHEAT DETECTION SYSTEM FAILED TO TEST. INSPECTION FOUND THAT A WIRE HAD BROKEN OFF THE WING OVERHEAT SENS OR IN THE LEFT WING LEADING EDGE. 2 L 7 2 4T 4 T RT A8SW E4WE 2001032200081 20010322 00081 SW 2001 3 22 CA980317096 1 19980310 A 5210 LATCH SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP PAX DOOR SEIZED W A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 CA 39182 (CAN) ON CLIMB PASSENGER DOOR WARNING LIGHT ON. AIRCRAFT RETURNED. INVESTIGATION FOUND THE DOOR DIFFICULT TO CLOSE WITH THE LATCH ONLY CATCHING AT ABOUT THE HALF WAY TO FULL LATCH POSITION. WHEN PANELS WEREREMOVED THE DOOR ACTUATOR SHAFT WA S BADLY CORRODED AS WERE BOTH PUSH PULL RODS, AND ROD ENDS. THE INTERIOR OF THE DOOR WAS VERY DIRTY AND THE LOWER BELLCR ANK PIVOT WAS RUSTED AND THE BOLT SEIZED. INV ESTIGATION OF THE PREVIOUS MAINTENANCE FOUND THAT THE RESPONSIBLE MECHANIC WAS VERY NEW TO THE INDUSTRY. STEPS UNDERTAKEN TO ENSURE FUTURE AND PROPER COMPLIANCE WITH MAINTENANCE PROGRAM. 2 L 7 2 4T 4 T RT A8SW E4WE 2001032200082 20010322 00082 CE 2001 3 22 CA980318001 1 19980303 A 3233 993880001 BALL LOCK BEECH 993880001 BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA ACTUATOR FAILED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 3020 0050 (CAN) ON DEPARTURE THE GEAR WAS SELECTED UP AND THE NOSE GEAR DOWN GREEN STAYED ON. AIRCRAFT RETURNED AND NOSE GEAR ACTU ATOR REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 2001032200083 20010322 00083 CE 2001 3 22 CA980318002 1 19980303 A 3233 993880001 BOSS BEECH 993880001 BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA ACTUATOR DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 0043 (CAN) PIVOT BOSSES WERE UNDER LIMITS FOR THE BEARING. REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 2001032200084 20010322 00084 EA 2001 3 22 CA980318003 2 19980309 A 7322 25244405 FUEL CONTROL BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA ENGINE SURGES W A UNSCHED LANDING R J PARTIAL RPM/PWR LOSS WARNING INDICATION CL CLIMB 1 CA 195 (CAN) ENGINE SURGING ON TAKEOFF, AIRCRAFT RETURNED TO BASE. FUEL CONTROL UNIT REPLACED AND AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3T 4 T A14CE E4EA 2001032200085 20010322 00085 CE 2001 3 22 CA980318004 1 19980309 A 3230 1CH25 SWITCH BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA MLG OUT OF ADJ W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA (CAN) A/C RETURNED TO BASE DUE TO IN TRANSIT LIGHT ON. GEAR SWITCH ADJUSTED FOR COLD WEATHER OPERATION. 1 L 7 2 3T 4 T A14CE E4EA 2001032200087 20010322 00087 SW 2001 3 22 CA980318006 1 19980316 A 6120 8975428 BETA SWITCH FRCHLD SA227 SA227CC SW GARRTT TPE331 TPE33111U 01514 WP PROPELLER LEAKING W O OTHER J WARNING INDICATION LD LANDING 1 CA (CAN) CREW REPORTED NO BETA INDICATION WHEN ON LANDING ROLL AND TAXI. BETA SWITCH AND PLUMBING CHECKED. OIL LEAK WAS EVI DENT ON ENGINE COWL FLAP. SOURCE OF OIL LEAK DETERMINED TO BE FROM BETA SWITCH VENT HOLES. 0.5 LITERS OF OIL WAS LOST IN THIS MISHAP. 2 L 7 2 4T 4 T RT A18SW E4WE 2001032200088 20010322 00088 SW 2001 3 22 CA980318007 1 19980211 A 2910 27810322682 LINE SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE LT NACELLE CRACKED W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA (CAN) HYDRAULIC LINE IN LEFT ENGINE NACELLE CRACKED IN FLIGHT.ALL FLUID LEFT THE AIRCRAFT.AIRCRAFT RETURNED TO BASE WITH GEAR DOWN AND LOCKED. A 1/4 INCH CRACK FOUND IN THE 90 DEGREE BEND. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001032200089 20010322 00089 SW 2001 3 22 CA980318008 1 19980211 A 7810 276208025 DUCT SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE ENGINE EXHAUST CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) EXHAUST DUCT FOUND CRACKED AROUND 3/4 QUARTERS OF THE CIRCUMFERENCE OF THE FLANGE. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001032200090 20010322 00090 SW 2001 3 22 CA980318009 1 19980211 A 2913 MS1699828 SCREW VICKERS PUS04426 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE HYDRAULIC PUMP SHEARED W K NONE O OTHER IN INSP/MAINT 1 CA MX528587C (CAN) ON ENGINE CHANGE ON THE RIGHT HAND SIDE AND DURING THE RUN UP A LARGE HYD. LEAK WAS NOTED.LEAK COMING FROM HYD. PU MP VALVE PLATE AS 2 OF THE 4 SCREW HEADS HAD BEEN SHEARED OFF. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001032200091 20010322 00091 SW 2001 3 22 CA980318010 1 19980211 A 2742 2719008002 ACTUATOR SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE PITCH TRIM RATCHETING W K NONE O OTHER IN INSP/MAINT 1 CA 4551 1049 (CAN) PITCH TRIM ACTUATOR FOUND OUT OF LIMITS WHILE DOING FAA AD 97-23-01. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001032200092 20010322 00092 CE 2001 3 22 CA980318011 1 19980211 A 3233 99810057651 ACTUATOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG FAILED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) NOTICEABLE BINDING WHEN ROTATING ACTUATOR AT .500 STROKE, END PLAY OK. 1 L 7 2 3T 4 T A14CE E4EA 2001032200093 20010322 00093 CE 2001 3 22 CA980318013 1 19980217 A 7997 WIRE PWA PT6A28 BEECH 99 99 1154002 CE PWA PT6 PT6A28 EA OIL PX INDICATOR BROKEN W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA PCE40209 (CAN) IN CRUISE, INDICATOR GIVING FALSE OIL PRESSURE INDICATION. WIRE BROKE AT CANNON PLUG, REPAIRED. 1 L 7 2 3T 4 T A14CE E4EA 2001032200094 20010322 00094 CE 2001 3 22 CA980318014 1 19980217 A 3233 508202085 ACTUATOR BEECH 100 A100 1152915 CE PWA PT6 PT6A28 EA MLG BINDING W K NONE O OTHER IN INSP/MAINT 1 CA 526 (CAN) ACTUATOR BINDING/SLIPPING INTERNALLY. REPLACED. 1 L 7 2 3T 4 T A14CE E4EA 2001032200095 20010322 00095 SW 2001 3 22 CA980318015 1 19980217 A 2910 2781032163 LINE SWRNGN SA227 SA227AC 8780603 SW MCAULY 4HFR34 4HFR34C652 NE HYDRAULIC SYS CHAFED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) HYD LINE CHAFED IN THE LEFT HAND CENTER SECTION. 2 L 7 2 4T RT A8SW 6 C 3PNE 2001032200096 20010322 00096 EA 2001 3 22 CA980318016 2 19980217 A 7321 25244405 FUEL CONTROL BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA ENGINE SURGES W O OTHER J WARNING INDICATION CR CRUISE 1 CA 2109 (CAN) FUEL CONTROL UNIT CAUSED 200 FT/LB SURGE WHEN POWER WAS REDUCED. 1 L 7 2 3T 4 T A14CE E4EA 2001032200097 20010322 00097 SW 2001 3 22 CA980318018 1 19980217 A 3260 ML345 SWITCH FRCHLD SA227 SA227CC SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE MLG INTERMITTENT W A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 CA (CAN) NO GREEN INDICATION FOR THE NOSE ALTHOUGH THE IN-TRANSIT LIGHT WAS OK.GEAR DOWN SWITCH WAS INTERMITTENT. 2 L 7 2 4T 4 T RT A18SW E4WE 6 C 3PNE 2001032200108 20010322 00108 2001 3 22 CA980318034 4 19980305 A 8300 GEARBOX BOEING 727 72727C 138400J NM PWA JT8 JT8D7B 52053 NE NR 3 ENGINE FAILED W O OTHER Y ENGINE STOPPAGE AP APPROACH 1 CA (CAN) ON APPROACH THE NR 3 ENGINE DECELERATED AND STOPPED. THE AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTION FOUND THE EN GINE OIL FILTERS WERE METAL CONTAMINATED. THE COMPRESSOR AND TURBINE SECTIONS SHOWED NO VISIBLE DAMAGE. THE SOURCE OF TH E METAL CONTAMINATION IS BELIEVED TO BE THE ACCESSORY DRIVE SECTION. 2 L 7 3 4F 4 F A3WE E2EA 2001032200113 20010322 00113 EA 2001 3 22 CA980318040 1 19980316 A 2460 ANL500 CURRENT LIMITER CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE ELECTRICAL BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA (CAN) DURING APU START A FLASHING WAS NOTED IN JB4. INVESTIGATION FOUND END OF CURRENT LIMITER F1KD OF 500 AMPS HAD BURN T AND MELTED. ALSO SECURING NUT AND BUSS BAR WERE DAMAGED. SECURING BOLT COULD NOT BE REMOVED NORMALLY. SUBMITTER SUGGES TS THAT PROBLEM HAD OCCURRED AS A RESULT OF LOOSENING OF JOINT OVER TIME. ALSO ALUMINUM WASHERS HAD MELTED AND IT WAS TH OUGHT THAT THEY WERE NOT THERE. POSSIBLY NUTS HAD BOTTOMED ON THE BOLT. FLEET CHECK TO BE CARRIED OUT. 2 L 7 2 4F 4 F RT A21AE E15NE 2001032600187 20010326 00187 EA 2001 3 26 CA980318043 1 19980313 A 7830 32335861 BALLSCREW CNDAIR CL601 CL6012A12 1900303 EA GE CF34 CF341A NE RIGHT BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) THE RIGHT THRUST REVERSER 4 O''CLOCK BALL SCREW ACTUATOR ANTI-ROTATION TANG FOUND BROKEN. 2 L 7 2 4F 4 F RT A21AE E15NE 2001032600190 20010326 00190 SO 2001 3 26 CA980318046 1 19980307 A 3260 602EN16 UPLOCK SWITCH EMB 110 EMB110P1 3260122 SO PWA PT6 PT6A34 52043 EA MLG FAILED W K NONE N FALSE WARNING IN INSP/MAINT 1 CA (CAN) ON PREFLIGHT CREW NOTICED THE GEAR INTRANSIT LIGHT ON AS WELL AS THE THREE GREENS. THE RIGHT HAND UPLOCK SWITCH HA D FAILED. 1 L 7 2 4T 4 T A21SO E4EA 2001032600192 20010326 00192 EU 2001 3 26 CA980318055 1 19980304 A 5330 HC537H12100 SKIN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE FUSELAGE WRINKLED W K NONE O OTHER IN INSP/MAINT 1 CA 30703 (CAN) SEVERAL AREAS OF WRINKLES AND OIL CANNING WERE FOUND IN THE FUSELAGE CANOPY ROOF SKIN BETWEEN FRAME 12 AND 14.NO H EAVY LANDINGS OR UNUSUAL INCIDENTS REPORTED.THIS IS SECOND AIRCRAFT FOUND WITH PROBLEM. SUBSEQUENT FINDINGS SHOWED NO SI GNIFICANT VARIATIONS ON THE MATERIAL CONDUCTIVITY READINGS OR THICKNESS MEASUREMENT FROM THOSE OF THE DRAWING REQUIREMEN TS. 2 H 7 4 4F 4 F RT A49EU E6NE 2001032600193 20010326 00193 EU 2001 3 26 CA980318056 1 19980304 A 5320 HC251H0177000 BRACKET BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE COCKPIT CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 30703 (CAN) WITH OVERHEAD COCKPIT ELECTRICAL PANEL REMOVED FOR SKIN REPAIR, BOTH THE LEFT AND RIGHT AFT SUPPORT MOUNTING BRACK ETS FOR THE PANEL WERE FOUND CRACKED. THE LEFT END WAS COMPLETELY CRACKED OFF. THE RIGHT BRACKET HAD SEVERAL CRACKS. IPC REF. 25-10-71-01, FIG. 1, ITEMS 55 AND 60. 2 H 7 4 4F 4 F RT A49EU E6NE 2001032600194 20010326 00194 NM 2001 3 26 CA980318057 1 19980310 A 2913 CONNECTOR DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE HYD PUMP CONTAMINATED W O OTHER J WARNING INDICATION CR CRUISE 1 CA (CAN) NR 2 ENGINE HYD. PUMP CAUTION LIGHT ON. PRESSURE SWITCH CANNON CONNECTOR WAS FOUND CONTAMINATED WITH DIRT AND MOIS TURE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032600203 20010326 00203 WP 2001 3 26 CA980325009 1 19980320 A 7714 INDICATOR DOUG DC10 DC1030 3023501 WP GE CF6 CF650C2 30018 NE COCKPIT STUCK W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 72471 54331 (CAN) AIRCRAFT ABORTED TAKE-OFF AT 80 KNOTS DUE TO NR 3 ENGINE N1 INDICATOR STUCK AT 55 PERCENT. ENGINE FAIL LIGHT ILLUM INATED. AIRCRAFT DISPATCHED PER MEL 77-01A. NR 3 INDICATOR REPLACED. 2 L 7 3 4F 4 F A22WE E23EA 2001032600268 20010326 00268 SW 2001 3 26 CA980318012 1 19980217 A 7714 040464 SHAFT 2719216005 SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE3311151A 01514 WP MCAULY 4HFR34 4HFR34C652 NE TACH GENERATOR SHEARED W O OTHER J WARNING INDICATION CR CRUISE 1 CA 040464 (CAN) TACH GENERATOR SHAFT SHEARED. 2 L 7 2 4T 4 T RT A8SW E3WE 6 C 3PNE 2001032600367 20010326 00367 NM 2001 3 26 CA980325033 1 19980316 A 2761 82950010269 HYDRAULIC LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE RT SPOILER CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 22589 (CAN) RIGHT HAND INBOARD SPOILER LIFT DUMP ACTUATOR HYDRAULIC LINE FOUND CRACKED AND LEAKING. 1/4 INCH CRACK ABOUT 3 INC HES FROM THE B NUT. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032600368 20010326 00368 NM 2001 3 26 CA980325034 1 19980318 A 7930 APT761000100DW TRANSMITTER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE OIL PRESSURE FAILED W E ENGINE SHUTDOWN P NO WARNING INDICATION CL CLIMB 1 CA 22598 (CAN) AT 3000 FEET THE NR 1 ENGINE INDICATED ZERO PSI OIL PRESSURE WITH NO WARNING LIGHT. INFLIGHT SHUTDOWN CARRIED OU T. NR 1 OIL PRESSURE TRANSMITTER FOUND FAILED. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032600369 20010326 00369 SW 2001 3 26 CA980325036 1 19980317 A 3260 LM345 DOWNLOCK SWITCH SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE RT MLG INTERMITTENT W O OTHER N FALSE WARNING DE DESCENT 1 CA (CAN) INTERMITTENT RIGHT MAIN GEAR GREEN LIGHT ON APPROACH TO LAND. DOWN SWITCH REPLACED. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 2001032600380 20010326 00380 SW 2001 3 26 CA980325039 1 19980319 A 2435 03601008 BEARING LUCAS 230790002 FRCHLD SA227 SA227CC SW GARRTT TPE331 TPE33111U 01514 WP STARTER GEN FAILED W E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 CA 271 5227 (CAN) PILOT COMPLAINED OF A LOUD NOISE COMING FROM THE RIGHT ENGINE ON START. STARTER REMOVED AND DRIVE END SHAFT FOUND VERY SLOPPY. DRIVE END BEARING HAD BLOWN APART. 2 L 7 2 4T 4 T RT A18SW E4WE 2001032600382 20010326 00382 WP 2001 3 26 CA980325043 1 19980309 A 2917 CONTROLLER LKHEED 1011 10113853 5265020 WP RROYCE RB211 RB211524B402 54555 NE HYD PRESSURE FAILED W B A EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CA (CAN) A/C RETURNED DUE TO PRESSURIZATION PROBLEMS IN CRUISE. RAPID DESCENT INITIATED, AND PRESSURIZATION RECOVERED AT FL 280, DESCENT STOPPED AT FL250 LANDED SAFELY. CABIN PRESSURE CONTROLLER REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 2001032600420 20010326 00420 NM 2001 3 26 CA980325050 1 19980224 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE NR 1 ENGINE LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 11376 (CAN) NR 1 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL PRESSURE. THE AIRCRAFT DIVERTED AND LANDED. POST FLIGHT INSP ECTION FOUND THE NR 1 ENGINE OIL COOLER LEAKING. THE OIL COOLER WAS REPLACED AND CHECKED SERVICEABLE. THE AIRCRAFT RETUR NED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032600445 20010326 00445 SW 2001 3 26 CA980331003 1 19980323 A 3211 55010021 DRAG BRACE SWRNGN SA226 SA226TC 8780404 SW GARRTT TPE331 TPE33110UA 01514 WP MLG BROKEN W O OTHER O OTHER LD LANDING 1 CA 23412 (CAN) ON TOUCHDOWN CREW FELT LEFT GEAR COLLAPSE & HEARD PROP BLADE STRIKING RWY.GO AROUND COMPLETED, BUT ON SUBSEQUENT L DG GEAR WAS NOT LOCKED DOWN LEFT MAIN GEAR PIVOTED REARWARDS ALLOWING LEFT WING TIP & BLADES OF LEFT PROP TO CONTACT GRO UND. A/C STOPPED 50 TO 100 FEET OFF RWY. BOTH LEFT MAIN GEAR DRAG BRACE AFT LOWER LINKS HAD FAILED. LAB ANALYSIS FOUND B RACES FAILED AS A RESULT OF OVERLOAD FORCES IMPOSED BY A PROBABLE HARD LANDING. 2 L 7 2 4T 4 T RT A8SW E4WE 2001032600446 20010326 00446 NM 2001 3 26 CA980402004 1 19980325 A 3234 574205 SELECTOR KNOB DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE MLG FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 15882 (CAN) GEAR WOULD NOT GO DOWN ON SELECTION.ALTERNATE SELECTION CARRIED OUT. LANDING GEAR SELECTOR REPLACED.SELECTOR SENT FOR TEARDOWN. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 2001032600447 20010326 00447 NE 2001 3 26 CA980402007 2 19980315 A 7200 ENGINE DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE NR 2 POWER LOSS W E C ENGINE SHUTDOWN ABORTED TAKEOFF R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA 57552 P657460D (CAN) ON TAKEOFF POWER LEVERS BROUGHT TO 1.4 EPR FOR RUN-UP, ALL OKAY. AT APPROXIMATELY 85-95 KNOTS, NR 2 ENGINE HAD A P OWER LOSS AND THE EGT INITIALLY AT 700C, WENT TO 800 C. ENGINE WAS SHUTDOWN AND FIRE TRUCKS WERE CALLED. THE NR 2 ENGINE WAS REPLACED. RESULTS OF STRIP REPORT TO FOLLOW. 2 L 7 2 4F 4 F A6WE E2EA 2001032600449 20010326 00449 EU 2001 3 26 CA980402024 1 19980324 A 3210 201107615 PIN BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 332495 (CAN) DURING WALKAROUND THE CREW NOTICED ON THE LEFT MLG THAT THE PIN WHICH CONNECTS THE SHOCK ABSORBER TO THE TRAILING LINK WAS RUBBING AGINST NR 1 TIRE. PIN WAS ACTUALLY BROKEN IN TWO.SEE ALSO SDR 19980415024. 2 H 7 4 4F 4 F RT A49EU E6NE 2001050300114 20010503 00114 CE 2001 5 3 20010426CW001 1 19980809 A 5714 118100021603 SPAR CAP BEECH 1900 1900C 1154161 CE PWA PT6 PT6A60A 52043 NE CENTER SECTION CORRODED E YADA K NONE O OTHER IN INSP/MAINT 1 AL 03 5632C 23368 UC81 FOUND CORROSION ON FORWARD SIDE OF MAIN WING SPAR LOWER CAP BOND ASSEMBLY. THE AFFECTED AREA IS UNDER THE CABIN FLOOR I N THE CABIN. CORROSION DAMAGE FOUND TO REQUIRE REPLACEMENT OF THE SPAR CAP BOND ASSEMBLY. 2 L 7 2 4T 4 T RT A24CE E4EA 1998043000600 19980430 00600 WP 1998 4 30 98ZZZM315 1 19980209 A 5347 4924374 SEAT TRACK DOUG DC9 DC915F 3022037 WP FUSELAGE MISREPAIRED A GAIA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 07 563PC 47055 DURING C-CHECK INSPECTION, FOUND INADEQUATE REPAIRS ON THE FLOOR SEAT TRACKS AT BS 784 RBL 22. (M) 2 L 7 2 4F A6WE 1998092500593 19980925 00593 EU 1998 9 25 98ZZZX3531 1 19980720 A 6321 AH096035 PAD BOLKMS 117 BK117A4 5626017 EU M/R BRAKE MISMANUFACTURED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 527RM 7111 MAIN ROTOR BRAKE PAD ASSY REJECTED NEW OUT-OF-BOX. CRACKED AT MOUNTING PLATE. REPLACED WITH NEW UNIT, CORRECTED PROBLE M. 1 G 7 2 3U H13EU 1998050801086 19980508 01086 EU 1998 5 8 HEEA0014048 1 19980429 A 2150 117E00113 ELBOW BOLKMS 117 BK117B1 5626012 EU VENTURI MISMANUFACTURED E HEEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SW 03 191BK 7146 VENTURI P/N 117-E0011-9 DOES NOT FIT PROPERLY IN ELBOW P/N 117-E0011-3. WELD BEADS ON INSIDE OF ELBOW DO NOT ALLOW VENT URI TO FIT FLUSH ON PLATE P/N 117-E0001-47. REPLACED WITH SERVICEABLE PART. 1 G 7 2 3U H13EU 1998030500146 19980305 00146 WP 1998 3 5 MWEA98209 1 19980224 A 5330 SKIN DOUG DC9 DC932 3022066 WP L1 DOORWAY MISREPAIRED A MWEA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 31 212ME 47701 PREV REPAIR FOUND AT L1 MAIN CABIN ENTRANCE DOOR FWD UPPER CORNER OF CUTOUT, REPAIR IS NOT PER THE SRM. REMOVED OLD REP AIR FAB FILLER AND DOUBLER IAW SRM 5305 FIG 26. INSTALLED FILLER DOUBLER IAW SRM 5130. 2 L 7 2 4F A6WE 1998090400073 19980904 00073 NM 1998 9 4 CA980608026 1 19980516 A 3230 BRACKET BOEING 747 747433 NM PWA 4056 PW4056 NE MLG MISINSTALLED W C ABORTED TAKEOFF W INADEQUATE Q C TO TAKEOFF 1 CA P724174 (CAN) ON TAKEOFF, GEAR WOULD NOT RETRACT, GEAR TILT MESSAGE ON ENGINE AND CREW ALERTING SYS. AIRCRAFT RETURNED, OTHER I NDICATIONS SHOWED A/C STAYED IN GROUND MODE. FOUND TRUCK TILT PROXIMITY SWITCH SUPPORT BRACKET INCORRECTLY INSTALLED AN D DAMAGED. BRACKET REPAIRED AND SENSORS ADJUSTED, GEAR SWING CARRIED OUT. SYS NORMAL. 2 L 7 4 4F 4 F RT A20WE E24NE 1998032600973 19980326 00973 WP 1998 3 26 CKSA98165 1 19980228 A 5311 FRAME DOUG DC8 DC863F 302198F WP BS 580 MISDRILLED A CKSA K NONE W INADEQUATE Q C IN INSP/MAINT 1 GL 23 870BX 46036 DURING ROUTINE CPCP INSPECTION, FOUND HOLE DRILLED INTO LT FRAME RADIUS AT FS 580, 12 ABOVE UPPER CUSP AREA. PLUGGED MI SDRILLED HOLES FABRICATED SHIM AND REPAIR STRAP, FITTED, DRILLED AND DEBURRED STRAPS, SHIM AND FRAME. TREATED AND PRIME D BARE METAL, SEALED AND INSTALLED REPAIR ON LT FRAME AT FS 580 12 ABOVE UPPER CUSP AREA IAW COTNEY DRAWING NR D93-R06. CORROSION TASK CARD NUMBER 573L-0551. NON-ROUTINE NR 04979 TASK NR Y1438. 2 L 7 4 4F 4A25 1998041701177 19980417 01177 NM 1998 4 17 DL72S980771 1 19980402 A 5753 652163262 SPAR BOEING 727 727232 1384082 NM NR 3 TE MIDFLAP MISDRILLED A DALA K NONE W INADEQUATE Q C IN INSP/MAINT 1 SO 27 402DA 21146 NR 3 MIDFLAP/ REAR SPAR/WBL 124/AD 94-07-08 - OS HOLE: OVERSIZED HOLE IN REAR SPAR UPR CHORD AND UPPER SKIN IN AD INSPE CTION AREA. FOUND DURING ACCOMPLISHMENT OF EO, 4-58705-3AD MODIFICATION. FAA AMOC REC'D TO INSTALL OS HI-LOK IN HOLE. 2 L 7 3 4F A3WE 1998080700425 19980807 00425 WP 1998 8 7 RRXA98326 1 19980624 A 5311 5610088513 FRAME DOUG DC8 DC862 3021970 WP BS 280 MISDRILLED A RRXA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 15 995CF 46024 DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 280 BETWEEN LONGERONS 13 RIGHT TO 14 RIGH T. 2 L 7 4 4F 4A25 1998031200889 19980312 00889 WP 1998 3 12 9804059917 1 19980308 A 3397 WIRE DOUG DC9 DC932 3022066 WP CABIN BROKEN A NWAA K NONE L NO TEST IN INSP/MAINT 1 GL 01 967N 47573 DURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. FOUND POWER SUPPLY DISARM WIRE BROKEN IN TAIL CONE AREA. REPAIRED WIRE AND REPLACED POWER SUPPLY, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998042400637 19980424 00637 NM 1998 4 24 AALA980402 1 19980224 A 3397 WIRE BOEING 727 727223 1384074 NM CABIN BROKEN A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 706AA 22463 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY FLOOR LIGHTING AT PAX SEAT ROWS 7 TO 16 WAS INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY FLOOR LIGHT PAX SEAT ROWS 7 TO 16. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998080700022 19980807 00022 CE 1998 8 7 98ZZZX2545 1 19980414 A 2797 WIRE CESSNA 500 550 2076604 CE TE FLAP DETACHED A NADA A UNSCHED LANDING F J FLT CONT AFFECTED WARNING INDICATION CL CLIMB 1 NE 05 404BF 5500071 DURING A FAR 135 FLIGHT, THE FLAPS WERE SELECTED UP AFTER TAKEOFF AND WOULD NOT RETRACT ALL THE WAY UP. STEP 2 ABNORMAL CHECK LIST WAS PERFORMED (FLAPS INOPERATIVE). PARTIAL FLAP LANDING WAS PERFORMED. INVESTIGATION REVEALED THE WIRE FRO M THE FLAP RELAY K44 TO FLAP UPLIMIT SWITCH S58 HAD COME OFF. THE WIRE WAS RE-INSTALLED TO THE FLAP LIMIT SWITCH WITH A LOCK WASHER, AND FUNCTIONALLY CHECKED OK. 1 L 7 2 4F A22CE 1998090401004 19980904 01004 WP 1998 9 4 GAIA9880 1 19980810 A 3297 WIRE DOUG DC9 DC915F 3022037 WP RT MLG WW BROKEN A GAIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 112PS 47013 KHA - FLT 322 - YIP - ELP - ON CLIMB-OUT FROM YIP, AFTER RETRACTING THE LANDING GEAR, THE UPLATCH CHECK WAS UNSATISFACTO RY. THE CREW DECIDED TO RETURN TO YIP. ON GEAR EXTENSION, THREE GREEN LIGHTS CAME ON AND THE RIGHT MAIN RED LIGHT CAME ON. AN UNEVENTFUL LANDING WAS MADE. INSPECTION FOUND, THE RIGHT MLG DOWNLOCK SWITCH CONDUIT PINCHED AND THE WIRES PU LLED FROM THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE WIRES WERE SPLICED. THE SYSTEM WAS OPS CHECKED PER DC9 MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4F A6WE 1998101600656 19981016 00656 WP 1998 10 16 CALA9801949 1 19981012 A 3397 WIRE DOUG DC10 DC1030 3023501 WP CABIN SHORTED A CALA K NONE L NO TEST IN INSP/MAINT 1 SW 09 17087 47928 FORWARD ZONE A EMERGENCY LIGHTS INOP. DOOR 1L EXIT SIGN DISASSEMBLED AND WIRING FROM TERMINAL 1 FOUND SHORTED TO TERMIN AL 2. DOOR EXIT SIGN WIRING RE-MADE. EMERGENCY LIGHT BATTERY CHARGER FITTED TO ZONE A. ALL DISTRIBUTED WIRING RE-MADE AND SYSTEM CHECKED PER MM 33-51-01 AND 33-55-00. 2 L 7 3 4F A22WE 1998121100723 19981211 00723 WP 1998 12 11 ARWA981204 1 19981205 A 3297 WIRE DOUG DC8 DC862 3021970 WP LT MLG BROKEN A ARWA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SO 19 810BN 45905 GEAR DOOR NOT LATCHED, LIGHT ILLUMINATED. FOLLOWED ABNORMAL PROCEDURE, LIGHT REMAINED ON. RETURNED TO MIAMI, NO FUEL D UMPED. FOUND BROKEN WIRE AT LT MLG DOOR UPLATCH SWITCH CANNON PLUG. REPAIRED SAME PER MM 20-50-00, OPS CHECK NORMAL PE R MM 32-61-4. 2 L 7 4 4F 4A25 1999010100357 19990101 00357 WP 1999 1 1 98ZZZM953 1 19980807 A 3397 WIRE LKHEED 1011 10113851 5265010 WP ROW 34-39 BROKEN A AMTA K NONE L NO TEST IN INSP/MAINT 1 GL 11 191AT 193C1084 DURING P/F, FOUND THE EGRESS LGHT SYSTEM AT ROWS 34 TO 39 ABC INOP. FOUND BROKEN WIRE. RESPLICED WIRE, OPS CHECK GOOD. 2 L 7 3 4F A23WE 1999012900855 19990129 00855 NM 1999 1 29 ASAA9840119 1 19981230 A 3397 WIRE BOEING 737 7374Q8 NM ROW 22-25 DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 772AS 25105 PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS AND THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 22 THROUGH 25 WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AT BOTH LOCATIONS AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1999081200524 19990812 00524 CE 1999 8 12 CA990311031 1 19981208 A 2750 WIRE BEECH 99 99A 1154003 CE PWA PT6 PT6A28 EA LIMIT SWITCH BROKEN W O OTHER F FLT CONT AFFECTED NR NOT REPORTED 1 CA 50754 (CAN) AIRCRAFT FERRIED HOME DUE TO FLAPS NOT OPERATING. UPON INSPECTION, A BROKEN WIRE WAS FOUND AT THE DOWNLIMIT SWITC H. 1 L 7 2 3T 4 T A14CE E4EA 1998072400477 19980724 00477 EA 1998 7 24 98ZZZM505 1 19980607 A 2710 NAS304371470 CONTROL CABLE DHAV DHC6 DHC6300 2802606 EA BS 111 DAMAGED A ASWA K NONE F FLT CONT AFFECTED NR NOT REPORTED 1 WP 07 146SA 514 CREW REPORTED AILERON CONTROL 'STUCK' WHEN ROLLING TO THE RIGHT. AIRCRAFT MADE A SAFE LANDING AT GCN. MAINTENANCE FOUN D A HOLLOW RIVET JAMMED IN CONTROL CABLE PULLEY AT FUSELAGE STATION 111.00. CABLE WAS DAMAGED REQUIRING REPLACEMENT. A REA UNDER LEFT CREW SEAT WAS INSPECTED AND CLEANED OF LOOSE DEBRIS. (M) 1 H 7 2 3T RT A9EA 1998110600500 19981106 00500 WP 1998 11 6 ARWA981059 1 19981020 A 2823 CABLE DOUG DC8 DC863F 302198F WP NR 4 ENGINE BROKEN A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 441J 45988 MIA - FLT 747 - NR 4 ENGINE SHUT OFF VALVE, CABLE BROKEN. FABRICATED CABLE ASSY IAW MM 91-10-45. INSTALLED CABLE ASSY IAW MM 28-22-7 AS CHECKED NORMAL IAW MM 38-27-7. (M) 2 L 7 4 4F 4A25 1998052900458 19980529 00458 EU 1998 5 29 UF6A980411 1 19980415 A 3397 58785 WIRE BAG ATP ATP EU CABIN FAILED A UF6A K NONE L NO TEST IN INSP/MAINT 1 GL 31 854AW 13305 2028 SBN - FORWARD EMERGENCY LIGHT STRIP INOP. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT STRIP CABLE ASSY. (M) 2 L 7 2 4T RT A27NM 1998121100088 19981211 00088 EA 1998 12 11 SWIA971324 1 19981128 A 3097 WIRE CNDAIR CL600 CL6002B19 1900309 EA GE CF34 CF343A1 30015 NE WING ANTI-ICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 409SW 7056 AT 10,000 FEET ENCOUNTERED ICE. TURNED ON ANTI-ICE AND GOT ON ANTI-ICE DUCT MESSAGE. FOLLOWED QRH AND RETURNED TO SLC IN STANDBY POSITION. ANTI-ICE DUCT MSG WOULD CYCLE ON AND OFF. REPLACED NR S27WK LX WIRING LEADING EDGE THERMAL SWITCH . 2 L 7 2 4F 4 F RT A21EA E15NE 1998051500418 19980515 00418 WP 1998 5 15 9808609101 1 19980507 A 3297 WIRE DOUG DC9 DC915 3022036 WP RT MLG CHAFED A NWAA O OTHER N FALSE WARNING CL CLIMB 1 GL 01 91S 47063 DURING CLIMB-OUT, THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. FLIGHT CREW PERFORMED UPLATCH CHECK. AIRCRAFT LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRING AT RIGHT MAIN LANDING GEAR UPLOCK SWITCH. O PERATIONAL CHECK NORMAL. 2 L 7 2 4F A6WE 1998021100798 19980211 00798 NM 1998 2 11 ASAA9840001 1 19980103 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 769AS 25103 SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE FROM ROW 27 AFT. REC ONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998040200888 19980402 00888 NM 1998 4 2 ASAA9840039 1 19980222 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 765AS 25102 PDX - DURING MAINTENANCE CHECK, THE AFT FOUR EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTE D WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998041000761 19980410 00761 NM 1998 4 10 ASAA9840044 1 19980304 A 3397 WIRE BOEING 737 7374Q8 138447Q NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 784AS 28199 SEA - DURING MAINTENNCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND INOPERATIVE AT ROWS 15 THROUGH 17. RECO NNECTED WIRING AND LIGHTS OPERATED NORMALLY. (X) 2 L 7 2 4F RT A16WE 2003010300012 20030103 00012 NE 2003 1 3 CZMA082742 2 19980728 A 7261 70061L000V174A HOSE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE OIL COOLER LEAKING E CZMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 03 911BE 36018 PART LEAKED ON INITIAL INSTALLATION, AT OIL COOLER END. REINSTALLED ORIGINAL HOSE WHICH WAS DEEMED SERVICABLE. ORIGINAL HOSE WAS PURCHASED WITH AIRCRAFT. 1 G 7 2 4U 4 U H4SW E22EA 1999020200001 19990202 00001 NE 1999 2 2 CA980707023 2 19980610 A 7230 BLADE GE CF6 CF680C2B2 30025 NE COMPRESSOR WORN W K NONE O OTHER IN INSP/MAINT 1 CA 34981 16247 690217 (CAN) DURING HIGH PRESSURE COMPRESSOR (HPC) BORESCOPE INSPECTION, DISCOVERED THE FIRST STAGE HPC HAD WORN IN THE PARENT METAL OF A BLADE MID-SPAN SHROUD AND THE CARBOLOY PAD WAS MISSING. PER THE AIRLINES WORK CARD 72004, ITEM 1, THE DAMAGE IS NOT PERMITTED. THE ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. PART TC: 7,855. 4 F E13NE 1998082800158 19980828 00158 1998 8 28 CA980424008 1 19980412 A 2840 HG1057AA07 INDICATOR PWA JT9 JT9D7R4D 52054 NE FUEL SYSTEM FAILED W O OTHER N FALSE WARNING CR CRUISE 1 CA P709687 (CAN) PRIOR TO CRUISE, ENGINE INDICATING AND CREW ALERTING SYS MESSAGE, SEE PROG 2/2, LOW FUEL REACHED CRUISING ALT AND COMPLETED QUICK REF HANDBOOK PROCEDURE. DRAINED CENTER TANK, CONFIG LIGHTS ON. NO FUEL LEAK. REPLACED FUEL PROCESSOR . 4 F E3NE 1998022600302 19980226 00302 1998 2 26 SCNA98011 4 19980126 A 2561 P0723103W LIFE VEST CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 UNK LIFE VESTS WERE REJECTED AT SHOP DUE TO FAILURE OF AIR RETENTION TEST IN ACCORDANCE WITH MFG CMM 25607, 25602, 25606 AND 256064. SERIAL NUMBERS AFFECTED WERE 12103 AND 71613. 1998121800486 19981218 00486 GL 1998 12 18 CA981125001 2 19980409 A 7260 GEARBOX ALLSN 501D 501D22 03005 GL NR 2 LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA CAE550575 (CAN) DURING CLIMB THROUGH FL 170, NR 2 GEARBOX OIL PRESSURE LIGHT FLICKERING. OIL PRESSURE WAS STILL IN THE GREEN RANG E AND THE POWER SECTION OIL PRESSURE LIGHT WAS NORMAL. OIL QUANTITY INDICATION DROPPED RAPIDLY AND THE LOW OIL PRESSURE LIGHT STARTED TO FLICKER. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED. 4 T E282 1998111300645 19981113 00645 NE 1998 11 13 CA980818034 2 19980710 A 7230 210193010 BEARING LYC ALF502 ALF502R5 41580 NE NR 2 SPALLED W K NONE O OTHER IN INSP/MAINT 1 CA LF05086 (CAN) DURING ROUTINE MAINTENANCE, METAL WAS FOUND ON THE ENGINE CHIP DETECTOR. ON TEARDOWN, THE NR 2 BEARING WAS FOUND SPALLED ON THE INNER AND OUTER RACES WITH MARKS ON THE BEARINGS. THE NR 2 BEARING PACK WAS REPLACED, THE OIL SYSTEM WAS FLUSHED, AND THE ENGINE WAS RETURNED TO SERVICE. 4 F E6NE 2001032700002 20010327 00002 NE 2001 3 27 CA980325008 2 19980319 A 7297 9531M61G01 WIRE CFMINT CFM56 CFM565A1 NE LT ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 19988 19988 (CAN) FOUND AT ENGINE SHOP VISIT. OUTER COMBUSTION COWL WIRE HAS WORN THROUGH A PORTION OF THE COWL AND TRANSLATED FORWA RD CONTACTING FUEL NOZZLE STEM. SIGNIFICANT DAMAGE OF NOZZLES IN POSITIONS 1, 2, 3 AND4. SB 72-240 ISSUED AUG 9TH 1991 A ND REV.1 ISSUED DEC 1991 EFFECTIVITY DID NOT REFLECT SUBJECT ENGINE SERIAL NUMBER. 4 F E29NE 1998120400035 19981204 00035 1998 12 4 CA980615009 1 19980603 A 7600 84260050 QUADRANT PLATE BENDIX 23065104 ALLSN 250C 250C20B 03013 GL COCKPIT WRONG PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA 84260050 CAE835628 (CAN) FOLLOWING INSTALLATION OF THE FUEL CONTROL, THE THROTTLE POSITION INDICATOR ON THE FUEL CONTROL SHOWED THE THROTTL E TO BE BELOW THE IDLE MARK ON THE QUADRANT WHEN THROTTLE WAS POSITIONED ON THE IDLE DETENT. QUADRANT PLATE WAS VISIBLY DIFFERENT FROM THOSE INSTALLED ON OTHER FUEL CONTROLS FOR SAME ENGINE. 3 U E4CE 1998082800157 19980828 00157 1998 8 28 CA980424007 4 19980411 A 3460 COMPUTER GE CFM56 CFM565A 13802 NE E/E BAY INOPERATIVE W O H OTHER DEACTIVATE SYST/CIRCUITS J WARNING INDICATION TO TAKEOFF 1 CA 731887 (CAN) AUTO THRUST DISENGAGED DURING TAKE-OFF ROLL, RECYCLED CIRCUIT BREAKER AND POWERED DOWN RESET FLIGHT MANAGEMENT GUI DANCE COMPUTER NR 2, OPERATIONALLY CHECKED SERVICEABLE. 4 F E29NE 1998100900361 19981009 00361 EA 1998 10 9 CA980707051 2 19980610 A 7310 3011857 LINE PWA PT6 PT6A28 EA FUEL SYSTEM CRACKED W K NONE K FLUID LOSS IN INSP/MAINT 1 CA PCE41799 (CAN) FUEL LINE WAS REMOVED AS IT WAS CRACKED. THE FUEL LINE HAD BEEN PROCURED FROM AN OUTSIDE VENDOR AS NEWLY OVERHAUL ED. 4 T E4EA 1999021200944 19990212 00944 1999 2 12 CA981130006 1 19981127 A 2500 BLANKET BS 325 BURNED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) INSULATION BLANKET FOUND BURNT WHERE IT MADE CONTACT WITH THE WATER WASTE DRAIN HEATER AT STA 325R. AIRCRAFT INSP ECTED AS A RESULT OF FLEET INSPECTION FOLLOWING AN INCIDENT OF SMOKE IN-FLIGHT. 1998090400097 19980904 00097 1998 9 4 CA980724041 1 19980714 A 8200 WATER INJECTOR GARRTT TPE331 TPE33111U 01514 WP ENGINES FAILED W O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA P44738C (CAN) ON TAKEOFF WHEN WATER METHANOL WAS SELECTED, BOTH ENGINES LOST POWER. WATER METHANOL WAS TURNED OFF AND ENGINE PO WER WAS REGAINED. INSPECTION FOUND THE METHANOL MIXTURE HIGH IN WATER CONTENT. WATER METHANOL SERVICE HAS BEEN DISCONT INUED UNTIL CAUSE CAN BE DETERMINED. 4 T E4WE 1998090400035 19980904 00035 1998 9 4 CA980602069 1 19980529 A 3242 5007427 TORQUE PLATE ABS 50116401 MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA SEP89308 (CAN) LPI REVEALED A LINEAR INDICATION APPROX. .1875 INCH IN LENGTH RUNNING RADIALLY AT BASE NEAR LIGHTNING HOLES. THIS APPEARS TO BE A FATIGUE CRACK WHICH ORIGINATED FROM A HOT TEAR DURING MANUFACTURE. 1998100900238 19981009 00238 NE 1998 10 9 CA980602024 2 19980427 A 7230 1456M55G03 DUCT GE CF6 CF680C2B2 30025 NE TURBINE STATOR BROKEN W O OTHER M OVER TEMP CL CLIMB 1 CA 702152 (CAN) LEFT EGT ABNORMALLY HIGH ON TAKEOFF (APPROACHING AMBER ZONE). DURING CLIMB, THE LT ENGINE EGT REMAINED 60 DEGREES HIGHER THAN THE RT ENGINE. LT PNEUMATIC PRESSURE 25 PSI. IN CRUISE, THE LT ENGINE DROPPED TO A MORE ACCEPTABLE LEVEL. ON ARRIVAL AND INSPECTION, FOUND THE 2 INCH TURBINE STATOR COOLING DUCT BROKEN (P/N 145M55G03) AND ENGINE WIRING DAMAG ED. ENGINE REPLACED AND AIRCRAFT RETURNED TO SERVICE. 4 F E13NE 1998022600301 19980226 00301 1998 2 26 SCNA98010 4 19980126 A 2561 P0723103 LIFE VEST CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 UNK LIFE VESTS WERE REJECTED AT SHOP DUE TO FAILURE OF AIR RETENTION TEST IN ACCORDANCE WITH MFG CMM 25607, 25602, 25606 AND 256064. SERIAL NUMBERS AFFECTED WERE F96600 AND E27698. 1999021200943 19990212 00943 1999 2 12 CA981130005 1 19981127 A 2500 BLANKET CABIN BURNED W K NONE B SMOKE/FUMES/ODORS/SPARKS IN INSP/MAINT 1 CA (CAN) INSULATION BLANKETS FOUND BURNT IN AREA AROUND THE WATER WASTE DRAIN HEATERS. THIS CHECKED AS A RESULT OF AN EARLI ER INCIDENT OF SMOKE IN-LIGHT OF ANOTHER AIRCRAFT. CANADAIR ADVISED. 1998043000985 19980430 00985 1998 4 30 SCNA98024 1 19980128 A 2520 96003 SEAT BELT BUCKLE CABIN DAMAGED A SCNA O OTHER O OTHER IN INSP/MAINT 1 GL 15 SEAT BELT BUCKLE REJECTED AT SHOP VISIT. LOCKING MECHANISM NOT WORKING/DAMAGED. REPLACED BUCKLE. 1999011500374 19990115 00374 NE 1999 1 15 CA981125093 2 19981028 A 7230 230318706 CARBON SEAL LYC ALF502 ALF502R5 41580 NE NR 1 LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 4181 LF05085 (CAN) NR 4 ENGINE TRENDS SHOWING HIGH OIL CONSUMPTION. INVESTIGATION REVEALED NR 1 CARBON SEAL WORN. SEAL AND RUNNER R EPLACED. PART TC: 3,616. 4 F E6NE 1998031200502 19980312 00502 1998 3 12 SCNA98022 4 19980226 A 2561 P0723107C LIFE VEST CABIN CONTAMINATED A SCNA K NONE O OTHER IN INSP/MAINT 1 GL 15 LIFE VEST WAS REJECTED AT SHOP DUE TO CONTAMINATION. SKYDROL WAS SPILLED ON THE BOX BEFORE SHIPPING. 1998111300728 19981113 00728 1998 11 13 CA980909019 1 19980826 A 3610 545709 BLEED MANIFOLD PWA JT8 JT8D7B 52053 NE NR 2 ENGINE IMPROPER PART W K NONE W INADEQUATE Q C IN INSP/MAINT 1 CA P656824D (CAN) NR 1 ENGINE 13TH STAGE BLEED MANIFOLD WAS MODIFIED TO FIT THE NR 2 ENGINE AT AN UNKNOWN LOCATION USING A NON-PRATT APPROVED REPAIR. THIS CONFIGURATION MAKES IT IMPOSSIBLE TO INSTALL THE ENGINE BLEED MANIFOLD. PART WAS FOUND INSTALLE D AFTER RETURN FROM A SHOP VISIT, THE PART WAS NOT SUPPLIED BY AIR CANADA. SUSPECTED PART WAS REPLACED BY THE APPROPRIA TE PART (P/N 545708). SUBMITTER STATED SUSPECTED PART IS QUARANTINED AND DISCREPANCY LETTER SENT TO OVERHAUL FACILITY. PART TC: 57,257. 4 F E2EA 1999031200252 19990312 00252 NE 1999 3 12 CA980707071 2 19980606 A 7240 213111059 LINER LYC ALF502 ALF502R5 41580 NE COMBUSTOR CRACKED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA 12495 3359 LF05085 (CAN) HIGH ENGINE TEMP AT HIGH POWER SETTINGS. COMBUSTION LINER FOUND CRACKED AND UNZIPPED. ALSO, THE 3RD STAGE NOZZLE VANE DAMAGED. THERE WAS TRAILING EDGE EROSION ON 2 VANES. ON THE COMBUSTION LINER THERE WAS SEPARATION BETWEEN LINER END AND INNER LINER. PART TC: 12,162. 4 F E6NE 1999020200002 19990202 00002 1999 2 2 CA981125019 1 19981019 A 7931 1339M62P06 TRANSMITTER GE CF6 CF680C2B2 30025 NE ENGINE OIL FAILED W E ENGINE SHUTDOWN J WARNING INDICATION TX TAXI/GRND HDL 1 CA 28507 8749006 702117 (CAN) ON ENGINE START, OIL PRESSURE SYSTEM NR 3 DISPLAYED ON EICAS DUE TO NO OIL PRESSURE INDICATION NR 3 ENGINE. REPLA CED NR 3 OIL PRESSURE TRANSMITTER. PART TC: 4,547. 4 F E13NE 1999081200519 19990812 00519 1999 8 12 CA990311026 1 19981203 A 3060 C40331 BRUSH BLOCK GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE PROP DEICE MISINSTALLED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA CC841B P44738C 881750 (CAN) PILOT REPORTED A STRONG SMELL OF RUBBER AND THE PROPELLER CIRCUIT BREAKER TRIPPED. ON LANDING, SEVERAL PASSENGERS REPORTED SEEING SPARKS FROM THE FRONT OF THE ENGINE. INSPECTION FOUND THE BRUSH BLOCK WAS NOT SHIMMED EVENLY AND THERE WAS EVIDENCE OF BIRD MATTER ON THE BRUSH BLOCK. THE BRUSH BLOCK WAS REPAIRED AND THE AIRCRAFT WAS RETURNED TO SERVICE. 4 T E4WE 6 C 3PNE 1998100900376 19981009 00376 NE 1998 10 9 CA980928025 2 19980821 A 7200 ENGINE CFMINT CFM56 CFM565C4 13802 NE NR 2 FLAMED OUT W C ABORTED TAKEOFF X ENGINE FLAMEOUT TO TAKEOFF 1 CA 741670 (CAN) NR 2 ENGINE FLAMED OUT ON TAKEOFF ROLL AT 70 KNOTS. THE TAKEOFF WAS REJECTED. EGT EXCEEDED 1,000 DEGREES CELSIUS . NR 2 ENGINE WAS REPLACED. FURTHER REPORT TO FOLLOW. 4 F E37NE 1999030500193 19990305 00193 NE 1999 3 5 CA990203017 2 19980217 A 7230 500327702 OIL SUMP PWA JT9 JT9D7R4D 52054 NE NR 1 & 2 BEARING CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 47357 41827 P707535 (CAN) THE ENGINE WAS INDUCTED IN THE SHOP FOR HIGH OIL CONSUMPTION. DURING DISASSEMBLY, THE NR 1 AND NR 2 BEARING SUMP WAS FOUND CRACKED IN TWO PIECES. NUMEROUS CRACKS ABOVE AND BEYOND ANY ACCEPTABLE LIMITS WERE ALSO IDENTIFIED DURING DIS ASSEMBLY OF THE LP COMPRESSOR ON STAGE 1, STAGE 1.5, STAGE 2, AND STAGE 3 STATORS. THE PARTS WERE REMOVED FROM SERVICE. PART TC: 14,715. 4 F E3NE 1998090400096 19980904 00096 NE 1998 9 4 CA980720019 2 19980629 A 7200 ENGINE PWA JT9 JT9D7AH 52054 NE SMOKE W O OTHER B K SMOKE/FUMES/ODORS/SPARKS FLUID LOSS TO TAKEOFF 1 CA 48062 662942 (CAN) ON TAKEOFF, THE FLIGHT CREW INITIATED A TURNBACK DUE TO SMELL OF FUMES AND SMOKE SEEN ON THE UPPER DECK. POST-FLI GHT THE LINE CREW NOTICED OIL COMING FROM THE WEEP TUBES AND THE BLEED VALVE LOCATIONS. THE ENGINE WAS REMOVED FROM SER VICE FOR FURTHER EVALUATION. ADDITIONAL INFORMATION WILL BE SUBMITTED WHEN AVAILABLE. PART TC: 14,244. 4 F E20EA 1999012900193 19990129 00193 1999 1 29 CA980707050 1 19980630 A 3213 2751544005 TORQUE KNEE OZONE OAS5453 MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LPI INPECTION PER SB 32-041 CARRIED OUT AND CRACK FOUND ALONG THE KNUCKLE FILLET RADIUS. 1998122400412 19981224 00412 NE 1998 12 24 CA981113018 2 19981030 A 7320 71900011 HMU WOODWARD CFMINT CFM56 CFM565C4 13802 NE NR 2 ENGINE FAULTY W E ENGINE SHUTDOWN E VIBRATION/BUFFET CR CRUISE 1 CA 741424 741424 (CAN) AT 15,700 FEET, NR 2 ENGINE CAUSED A VIBRATION IN THE AIRCRAFT. THE ENGINE AUTO SHUTDOWN. HIGH EXHAUST TEMPERATU RE WAS THE ONLY PARAMETER NOTED. THE ENGINE WAS REPLACED. 4 F E37NE 1999081200432 19990812 00432 NE 1999 8 12 CA990310023 2 19981203 A 7250 2121090R66 TURBINE DISC LYC ALF502 ALF502R5 41580 NE 1ST STAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 4685 LF05627A (CAN) DURING ROUTINE INSPECTION OF 1ST STAGE TURBINE DISC BLADES, A CRACK WAS FOUND IN THE CRITICAL AREA OF THE BLADE TR AILING EDGE AT 2ND COOLING SLOT NEXT TO BLADE FILLET AREA. 4 F E6NE 1998090400100 19980904 00100 NE 1998 9 4 CA980818036 2 19980716 A 7200 ENGINE LYC ALF502 ALF502R5 41580 NE NR 2 NACELLE FAILED W C E ABORTED TAKEOFF ENGINE SHUTDOWN Y J ENGINE STOPPAGE WARNING INDICATION TO TAKEOFF 1 CA 13636 1183 LF05662A (CAN) NR 2 ENGINE FAILED ON TAKEOFF. NR 2 ENGINE REPLACED. ENGINE SENT FOR INVESTIGATION AND REPAIR. PART TC: 14,040 . 4 F E6NE 1998121800444 19981218 00444 1998 12 18 CA981019015 4 19981005 A 2562 1104 ELT ARTEX 1104 E/E BAY CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 57318 (CAN) ELT STARTED EMITTING, EVEN WITH MAIN SWITCH AT OFF POSITION. INSPECTION FOUND SEVERE INTERNAL CORROSION CAUSED BY ABNORMAL LEVEL OF MOISTURE. 1999031200250 19990312 00250 NE 1999 3 12 CA980707069 2 19980609 A 7240 230318704 SEAL LYC ALF502 ALF502R5 41580 NE ENGINE LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA LF05086 (CAN) NR 1 SEAL LEAKING ON THE COMPRESSOR SECTION. 4 F E6NE 1999031000001 19990310 00001 NE 1999 3 10 CA980519014 2 19980505 A 7200 ENGINE GE CF6 CF680A 30025 NE NR 1 LEAKING W A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 CA 811142 (CAN) DURING FLIGHT ECAM INDICATION SHOWED LOW OIL QUANTITY ON NR 1 ENGINE. THRUST REVERSERS REDUCED AND AIRCRAFT DIVER TED. SEVERE OIL LEAK FOUND ON AFT CENTER SECTION OF THE ENGINE. ENGINE REPLACED AND SENT FOR INVESTIGATION. INITIAL T EST COULD NOT DUPLICATE OIL LOSS, HOWEVER, WHEN D-SUMP SCAVENGE LINE WAS LOOSENED AN OIL CONSUMPTION IN EXCESS OF 7 QUAR TS AN HOUR WAS PRODUCED. AFTER EXTENSIVE TESTING THE MANUFACTURER CONCLUDED THIS WAS THE MOST LIKELY CAUSE AND AS IT IS AN ASSEMBLY ERROR DURING MANUFACTURER OF THE ENGINE. THIS EVENT IS CONSIDERED ISOLATED AND DOES NOT IMPACT ON OVERALL E NGINE RELIABILITY. 4 F E13NE 1998112600257 19981126 00257 NE 1998 11 26 98ZZZX4320 3 19981029 A 6111 D5133 SHIELD HARTZL HCE4A HCE4A3A NE PROPELLER BLADE DEBONDED A GLBA K NONE O OTHER NR NOT REPORTED 1 CE 01 1064 HJ183A DEBOND UNDER DEICE BOOT ON BLADE NR 2, S/N 809AE - O/H BLADE AND RE-ASSEMBLED PROPELLER IAW MFG CMM. STATIC BALANCED PR OPELLER. 5 C P10NE 1998120400027 19981204 00027 GL 1998 12 4 CA980602038 2 19980312 A 7323 23057869 GOVERNOR BENDIX ALLSN 250C 250C20B 03013 GL TURBINE WORN W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 493 18926 CAE836260 (CAN) TORQUE SPLITS OCCURRING DURING CRUISE. WORN N2 LINKAGE REPLACED AND TORQUE SPLITS STILL OCCURRED. POWER TURBINE GOVERNOR REPLACED. 3 U E4CE 1998082800282 19980828 00282 1998 8 28 CA980602011 1 19980524 A 7714 WL719RSA1 INDICATOR LYC ALF502 ALF502R5 41580 NE COCKPIT STUCK W C ABORTED TAKEOFF J WARNING INDICATION TO TAKEOFF 1 CA 23557 AH250 LF95624A (CAN) ON TAKEOFF, NR 1 ENGINE N1 INDICATOR STUCK AT 51 PERCENT WITH RED FLAG ON INDICATOR. TAKEOFF REJECTED. PART TC: 26,119. 4 F E6NE 1999012900192 19990129 00192 1999 1 29 CA980707048 1 19980612 A 3213 2751544005 TORQUE KNEE OZONE OA5453 MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) LPI INSPECTION FOUND THE TORQUE KNEE KNUCKLE FILLET RADIUS CRACKED. INSPECTION PER SB 32-041. 1998041700757 19980417 00757 GL 1998 4 17 98ZZZX1498 2 19980213 A 7230 23007208 DIFFUSER VANE ALLSN 250C 250C28 03013 GL ENGINE DEFECTIVE A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 21709 DIFFUSER VANE DEFECT. REPLACED ONE STUD. 3 U E1GL 1998100200049 19981002 00049 1998 10 2 HCMA0000200 1 19980524 A 2810 574071 SIGHT GLASS FUEL SYSTEM CRACKED A HCMA K NONE W INADEQUATE Q C IN INSP/MAINT 1 WP 13 SIGHT GLASS WAS INSTALLED AND IMMEDIATELY CRACKED. NOTE: CORRECT TORQUE WAS APPLIED. PLASTIC DEFECTIVE. (X) 1998100900363 19981009 00363 EA 1998 10 9 CA980707053 2 19980610 A 7210 3013132 2ND STG CARRIER 2013340 PWA PT6 PT6A28 EA NR 5 BEARING SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 41733100 (CAN) AT OVERHAUL , IT WAS FOUND THE 2ND STAGE CARRIER HAD A PRESSED ON STYLE NR 5 BEARING, WHICH HAD STARTED TO BACK OF F OF THE CARRIER. A 0.050 INCH GAP WAS NOTICED BETWEEN THE JOURNAL AND THE SHOULDER OF THE CARRIER. 4 T E4EA 1998120400014 19981204 00014 NE 1998 12 4 CA980406052 2 19980324 A 7200 ENGINE LYC ALF502 ALF502R5 41580 NE ENGINE BAY CONTAMINATED W K NONE O OTHER IN INSP/MAINT 1 CA 25231 5100 (CAN) ON INSPECTION, HEAVY METAL CONTAMINATION FOUND ON FULL FLOW CHIP DETECTOR. ENGINE REMOVED. PART TC: 32,801. 4 F E6NE 1998100900362 19981009 00362 EA 1998 10 9 CA980707052 2 19980610 A 7200 ENGINE PWA PT6 PT6A28 EA NACELLE MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA PCE417999 (CAN) ENGINE WAS REMOVED FROM SERVICE FOR THE SECOND TIME DUE TO VIBRATIONS THAT CAUSED THE FUEL LINES TO CRACK. ENGINE WAS ON TWO DIFFERENT AIRCRAFT AND SAME PROBLEM OCCURRED. INVESTIGATION IS ONGOING. 4 T E4EA 1999031200244 19990312 00244 1999 3 12 CA980707006 1 19980609 A 8011 501214436000 STARTER LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 84 LF05463A (CAN) DURING START, NR 2 ENGINE STARTER SHAFT SHEARED. PART TC: 81. 4 F E6NE 1999031200260 19990312 00260 1999 3 12 CA980724055 1 19980630 A 7120 NAS6606D46 BOLT 9505405 GARRTT TPE331 TPE3311151A 01514 WP NR 2 ENGINE BROKEN W K NONE O OTHER IN INSP/MAINT 1 CA 1754 0214 P75078 (CAN) BOLT FOUND BROKEN AT THE ENGINE MOUNT AFT ISOLATOR ASSY. THE BOLT WAS SHEARED AT THE COTTER PIN HOLE. PART TC : 2,684. 4 T E3WE 1999021200164 19990212 00164 NE 1999 2 12 CA981207018 2 19981116 A 7321 EEC CFMINT CFM56 CFM565C4 13802 NE NR 3 ENGINE MALFUNCTIONED W O OTHER R PARTIAL RPM/PWR LOSS CR CRUISE 1 CA 741608 (CAN) DURING FLIGHT, THE NR 3 ENGINE STARTED TO LOSE POWER. N1 FLUCTUATED FROM MINIMUM TO MAXIMUM. POST-FLIGHT, THE NR 3 ENGINE ELECTRONIC CONTROL UNIT WAS REPLACED AND THE ENGINE WAS GROUND RUN SERVICEABLE. 4 F E37NE 1998120400108 19981204 00108 NE 1998 12 4 CA980916067 2 19980708 A 7250 STATOR GARRTT TPE331 TPE33114A 01514 NE ENGINE OVERHEAT W K NONE O OTHER TX TAXI/GRND HDL 1 CA 6783 3339 P75067 (CAN) DURING WALK-AROUND, THE PILOT FOUND THE PROP HARD TO TURN BY HAND. MAINTENANCE SUSPECTING EXCESSIVE RUBBING, REPL ACED THE ENGINE. ENGINE WAS SENT FOR INVESTIGATION, DISASSEMBLY FOUND HEAT DISTRESS TO THE NR 1 STAGE STATOR, APPROXIMA TELY 30-40 PERCENT OF THE CIRCUMFERENCE. THIS CAUSED LOCALIZED HEATING OF THE TURBINE BAFFLE AND THE LIP SEAL PLATE. D URING COOL DOWN, THE DIFFERENTIAL TEMPERATURE BETWEEN THE TWO CAUSED THEM TO RUB. PART TC: 9,965. 4 T E18NE 1998121800405 19981218 00405 1998 12 18 CA981007006 1 19980925 A 3213 54530057 YOKE OZONE OAS5453105 MLG CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 113 (CAN) ULTRASONIC INSPECTION DETAILED IN AD 96-19-05 PERFORMED AND 2 OF 3 YOKES CHECKED WERE FOUND CRACKED. THESE YOKES NOT REQUIRED BY AD. 1999012200308 19990122 00308 1999 1 22 CA981130012 1 19981113 A 7830 CONTROL UNIT CFMINT CFM56 CFM565C4 13802 NE THRUST REVERSER FAILED W O OTHER K FLUID LOSS TO TAKEOFF 1 CA 740360 (CAN) ON TAKEOFF, NR 3 ENGINE REVERSER UNLOCK MESSAGE ON ELECTRONIC CENTRALIZED AIRCRAFT MONITORING. REPLACED NR 3 REVE RSER HYDRAULIC CONTROL UNIT AND PRIMARY LOCK ASSEMBLY. 4 F E37NE 1998090400191 19980904 00191 1998 9 4 98ZZZX3112 1 19980731 A 2915 1054666607 SEAL HYD BYPASS DEFECTIVE B R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 VALVE PLUNGER REJECTED, NEW OUT-OF-BOX. FLAW IN SEAL AREA THAT COULD CAUSE HYDRAULIC FLUID LEAKAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1999021200273 19990212 00273 NE 1999 2 12 CA990111060 2 19981221 A 7200 ENGINE LYC ALF502 ALF502R5 41580 NE NR 4 FAILED W E ENGINE SHUTDOWN Y ENGINE STOPPAGE TO TAKEOFF 1 CA 4498 LF05739A (CAN) ON TAKEOFF, A LOUD BANG WAS HEARD AND NR 4 ENGINE SPOOLED DOWN. SPARKS WERE OBSERVED COMING FROM THE ENGINE AND T HE FOURTH STAGE BLADES WERE DESTROYED. CAUSE UNKNOWN AT THIS TIME, FURTHER REPORT TO FOLLOW. PART TC: 3,840. 4 F E6NE 1998120400003 19981204 00003 NE 1998 12 4 CA980325045 2 19980320 A 7250 230006402 BEARING 214193003 LYC ALF502 ALF502R5 41580 NE TURBINE SECTION WORN W O OTHER J WARNING INDICATION NR NOT REPORTED 1 CA 79H018 LF05842A (CAN) CREW REPORTED HIGHER THAN NORMAL ENGINE VIBRATION INCREASE - .7 ON INDICATOR. INSPECTION FOUND NR 4 AND NR 5 BEA RINGS WORN, WEAR MARKS ON BEARING. 4 F E6NE 1998120400032 19981204 00032 NE 1998 12 4 CA980603012 2 19980517 A 7397 230333301 WIRE LYC ALF502 ALF502R5 41580 NE ENGINE OVERSPEED MISINSTALLED W E ENGINE SHUTDOWN J W WARNING INDICATION INADEQUATE Q C DE DESCENT 1 CA 5100 (CAN) ENGINE OVERSPEED CAPTION ON DURING DESCENT. WIRING FOR PINS A AND B CROSSED ON OVERSPEED CABLE BY MANUFACTURER. 4 F E6NE 1998122400414 19981224 00414 NE 1998 12 24 CA981113021 2 19981028 A 7200 ENGINE PWA 4056 PW4056 NE NR 3 FAILED W E ENGINE SHUTDOWN M OVER TEMP TO TAKEOFF 1 CA P724391 (CAN) ON LIFT-OFF, NR 3 ENGINE HAD A COMPRESSOR STALL ALONG WITH A RAPID RISE IN EGT TO 700 DEGREES CELSIUS. ENGINE WAS SHUT DOWN. POST-FLIGHT BORESCOPE INSPECTION OF HIGH AND LOW COMPRESSORS AND TURBINES CARRIED OUT, ALL PARAMETERS NORMA L. PRECAUTIONARY CHANGE OF NR 3 ENGINE WAS CARRIED OUT. 4 F E24NE 1999043000091 19990430 00091 1999 4 30 CA981130007 1 19981126 A 2500 INSULATION BS 325 BURNT W O OTHER B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA (CAN) SMOKE AND BURNING SMELL IN COCKPIT. AIRCRAFT LANDED. INSULATION BLANKET SURROUNDING THE STRIP HEATER P/N S5AIJI FOR THE BAR AND GALLEY WATER WASTE SYSTEM CAME IN CONTACT WITH THE HEATER AND MELTING THE EXTERIOR MATERIAL. CANADAIR A DVISED. 1999020200003 19990202 00003 1999 2 2 CA981125022 1 19981031 A 7540 285T111511 B NUT 285T111511 GE CF6 CF680C2B2 30025 NE BLEED AIR LOOSE W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CL CLIMB 1 CA 32591 D00485 702664 (CAN) AIR RETURN DUE RT ENGINE BLEED OVERHEAT EICAS MESSAGE ON TAKEOFF. REPLACED BLEED CONTROL CARD PER MM. FOUND B-NU T ON DUCT PRESSURE SENSE LINE LOOSE, TIGHTENED. 4 F E13NE 1998121800815 19981218 00815 SO 1998 12 18 98ZZZX4669 2 19981022 A 7414 IMPULSE COUPLING SLICK 6310 CONT O470 O470U 17026 SO MAGNETO FAILED A O5BA K NONE O OTHER IN INSP/MAINT 1 AL 05 484 96070550 180A 809951R EXCESSIVE WEAR AT ATTACH POINT. ONE PAWL OUT OF LIMITS. THE OTHER WAS JUST AT LIMITS. LEFT MAG, ONE ENGINE. 3 O E273 1999081200422 19990812 00422 1999 8 12 CA990310013 1 19981215 A 7500 ENGINE LYC ALF502 ALF502R5 41580 NE NR 3 LEAKING W O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS AP APPROACH 1 CA 22115 977 LF05580A (CAN) DURING APPROACH, REAR CABIN CREW REPORTED DIRTY SOCK SMELL IN AIR IN REAR OF CABIN. NR 2 AIR CONDITIONER WAS TURN ED OFF AND SMELL DISSIPATED. AFTER LANDING, INSPECTION FOUND SMALL OIL LEAK IN THE NR 3 ENGINE BLEED BAND AREA. AIRCRA FT DISPATCHED ON MEL WITH NR 2 PACK INOPERATIVE. 4 F E6NE 1998090400098 19980904 00098 NE 1998 9 4 CA980724059 2 19980708 A 7250 WHEEL GARRTT TPE331 TPE33114GR 01514 NE TURBINE RUBBING W K NONE O OTHER TX TAXI/GRND HDL 1 CA 6783 3339 P75067 (CAN) ON WALK-AROUND, THE PILOT NOTICED THE PROP WAS HARD TO TURN BY HAND. MAINTENANCE INSPECTION SUSPECTED EXCESSIVE WHEEL RUB. ENGINE REMOVED FOR INVESTIGATION. FURTHER REPORT TO FOLLOW. PART TC: 9,965. 4 T E18NE 1998120400031 19981204 00031 WP 1998 12 4 CA980602067 2 19980519 A 7320 TEMP LIMITER GARRTT TPE331 TPE33111U 01514 WP RT ENGINE MALFUCNTIONED W O OTHER R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 CA P44738C (CAN) AIRCRAFT LIMITING FUEL ON RIGHT HAND ENGINE AT 620 DEGREES CELSIUS. TEMPERATURE LIMITER SYSTEM WAS DEFERRED, AND SYSTEM DISABLED BY PULLING TEMPERATURE LIMITER CIRCUIT BREAKER. UNKNOWINGLY, THIS ALSO DISABLED THE WATER METHONAL ON T HE SAME SIDE. NO INDICATION OF THIS IN MEL OR MM. ON TAKEOFF, THE AIRCRAFT DID NOT HAVE WATER METHONAL ON RIGHT SIDE, BUT OK ON LEFT CAUSING A MAJOR YAW AND REDUCED POWER. 4 T E4WE 1998022600303 19980226 00303 1998 2 26 SCNA98012 4 19980126 A 2561 3500113 LIFE VEST CABIN FAILED TEST A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 UNK LIFE VESTS WERE REJECTED AT SHOP DUE TO FAILURE OF AIR RETENTION TEST IN ACCORDANCE WITH MFG CMM 25607, 25602, 25606 AND 256064. 1998090400085 19980904 00085 1998 9 4 CA980610003 1 19980602 A 7120 89P10251 MOUNT WRIGHT R1820 982C9HE2 67020 EA ENGINE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 983 W509004 (CAN) CRACK FOUND ON UPPER LEFT HAND FIRESHIELD ATTACH BRACKET. CRACK STARTED IN BRACKET AND INTO MOUNT TUBING. CRACK IN TUBING WAS .6250 INCH LONG AND PROCEEDING IN LONGUTUDINAL DIRECTION. THIS IS AN EARLY STYLE DESIGN. LATER MOUNTS HA VE A BOLT ON BRACKET WHICH ELIMINATES THIS PROBLEM. 4 R E259 1998111800011 19981118 00011 WP 1998 11 18 CA980818033 2 19980701 A 7200 ENGINE GARRTT TPE331 TPE3311 01514 WP NR 2 NACELLE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 5875 1507 P76068 (CAN) DURING ROUTINE INSPECTION, AN OIL LEAK WAS FOUND ON NR 2 ENGINE. DUE TO THE AREA OF THE LEAK, THE ENGINE WAS REPL ACED. PART TC: 8,659. 3 T E3WE 1999012200298 19990122 00298 1999 1 22 CA981125062 1 19980921 A 3240 6107 GUIDES CLEVELAND 30146 BRAKE CYLINDER CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA (CAN) SEVERAL FATIGUE CRACKS FOUND AT BOTH PISTON GUIDE HOLES. 1998111300686 19981113 00686 EA 1998 11 13 CA980908007 2 19980818 A 8500 ENGINE WRIGHT R1820 982C9HE2 67020 EA HAMSTD 43D 43D51 NE ENGINE BAY MAKING METAL W E A ENGINE SHUTDOWN UNSCHED LANDING R Y PARTIAL RPM/PWR LOSS ENGINE STOPPAGE CL CLIMB 1 CA 1281 516268 211040 (CAN) AFTER TAKEOFF AND DURING CLIMB, THE PILOT NOTICED LOW OIL TEMPERATURE AND OIL PRESSURE ON ONE OF THE ENGINES. THE ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION FOUND METAL (ALUMINUM AND STEEL) IN THE MAIN OIL FILTER. THE ENGINE WAS R EPLACED. 4 R E259 6 C P8879 1998012900439 19980129 00439 EA 1998 1 29 98ZZZX371 2 19980101 A 7200 ENGINE DHAV DHC7 DHC7102 2802708 EA PWA PT6 PT6A50 52043 EA NR 2 OVERTEMP A CICA E ENGINE SHUTDOWN J M WARNING INDICATION OVER TEMP DE DESCENT 1 SO 17 234SL 24 86413 PID/FLL - FLT 703 - PILOT PERFORMED PRECAUTIONARY SHUT DOWN OF NR 2 ENGINE DUE TO HIGH OIL TEMP INDICATION. AIRCRAFT LA NDED WITH NO INCIDENT. MAINTENANCE INSPECTED OIL SYSTEM, CHECKED OIL QUANTITY, AND FOUND TO BE OK. RAN ENGINE AT VARIO US HIGH POWER SETTINGS FORWARD AND REVERSE FOR 30 MINUTES. OIL TEMP STAYED AT 90 DEGREES CELSIUS WELL WITHIN PARAMETERS . COULD NOT DUPLICATE HIGH OIL TEMP. AIRCRAFT RELEASED FOR FLIGHT. 2 H 7 4 4T 4 T A20EA E4EA 1998031900314 19980319 00314 NE 1998 3 19 9804259880 2 19980311 A 7200 ENGINE DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17A 52049 NE LEFT FAILED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TO TAKEOFF 1 GL 01 675MC 47651 688731 DURING TAKEOFF ROLL AT 95 KNOTS, A TRAILING AIRCRAFT REPORTED SPARKS EXITING FROM THE LEFT ENGINE. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE ENGINE DUE TO FOD. AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 4F 4 F RT A6WE E2EA 1998041000106 19980410 00106 NM 1998 4 10 98UAL900116 1 19980316 A 2613 OVERHEAT LIGHT BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE RT WING/BODY ILLUMINATED A UALA A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 WP 29 934UA 26662 RIGHT WING BODY OVERHEAT INDICATION. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041000524 19980410 00524 WP 1998 4 10 SABA980012 2 19980204 A 7200 310440001 ENGINE BAG JETSTM JETSTM3201 1500217 EU GARRTT TPE331 TPE3311 01514 WP RIGHT FLAMED OUT A SABA D RETURN TO BLOCK X ENGINE FLAMEOUT TX TAXI/GRND HDL 1 SO 33 928AE 66311 928 LEX - FLT 5167 - ON FLT FROM LEX TO CLT, AT LEX, THE AIRPORT AUTHORITY WAS BLOWING AND SCRAPPING DOWN RUNWAYS/TAXI AND R AMP AREA. THERE WAS 12 INCHES OF ACCUMULATED SNOW AND SNOW BANKS, FROM 12 INCHES TO 4 FEET. AIRCREW BOARDED PASSENGERS AND GOT DE-ICED. THE AIRCRAFT THEN PROCEEDED TO FOLLOW A SNOW PLOW TO HELP CLEAR THE WAY TO THE TAXI WAY. THE RIGHT E NGINE FLAMED OUT. AIRCRAFT WENT BACK TO RAMP. AIRCREW MADE A GROUND ENGINE RUN, WITH NO PROBLEMS NOTED. THE AIRCRAFT THEN HAD A FERRY FLIGHT TO CLT WITH NO PROBLEMS NOTED. MAINTENANCE AT CLT PERFORMED A POST FLAME OUT INSPECTION, NO DEF ECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M) 2 L 7 2 4T 3 T RT A56EU E3WE 1998050801476 19980508 01476 NM 1998 5 8 VNAA9804027 1 19980430 A 5101 STRUCTURE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE AIRFRAME BIRD STRIKE A VNAA K NONE C F.O.D. UK UNKNOWN 1 GL 07 432JS 3045 UPON LANDING,THE CREW NOTIFIED MAINTENANCE CONTROL THAT THEY MAY HAVE ENCOUNTERED A BIRD STRIKE. OUTSTATION MAINTENANCE INSPECTED THE AIRCRAFT FOR DAMAGE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 05-29-10 AND 05-29-40. NO DAMAGE WAS F OUND. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998052200715 19980522 00715 NE 1998 5 22 98UAL900181 2 19980516 A 7200 ENGINE BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE NR 1 MALFUNCTIONED A UALA O OTHER O OTHER IN INSP/MAINT 1 WP 29 607UA 21868 NUMBER 1 ENGINE POWER FLUCTUATES. 2 L 7 2 4F 4 F RT A1NM E3NE 1998071500002 19980715 00002 NE 1998 7 15 UPS98627046 2 19980624 A 7200 ENGINE BOEING 767 76734AF 1385212 NM GE CF6 CF680C2B6 NE LEFT MALFUNCTIONED A IPXA O OTHER R PARTIAL RPM/PWR LOSS CL CLIMB 1 SO 01 319UP 27758 INSPECTION TYPE:ETOP LT ENGINE POWER FLUX AT A CONSTANT THRUST SETTING. BOTH CLB 2 AND CLB PWR SETTING. NOTICEABLE YAW IN ADDITION TO ALL ENG INDICATION FLUX. REPEAT WRITE UP SEE CONTROL NR 9827042 FOR PREVIOUS WRITE UP. REPLACED N1 SEN SOR PERFORMED ENG RUNS AND L PIMU CHECK OPS CHECK OK PER MM 77-12-01. P/N 8TJ163AAB1 ON AND OFF S/N OFF GDBA0800 ON 127 4F. 2 L 7 2 4F 4 F RT A1NM E13NE 1998072400017 19980724 00017 NE 1998 7 24 USAASB98142 2 19980605 A 7230 9527M99P11 FAN BLADE BOEING 737 737301 1384611 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE BIRD STRIKE A USAA A UNSCHED LANDING C E F.O.D. VIBRATION/BUFFET CL CLIMB 1 EA 19 558AU 23512 BOS - FLT 548 - DURING TAKEOFF ROLL, FIRST OFFICER NOTICED A SMALL BIRD OFF THE LEFT SIDE OF THE AIRCRAFT. SHORTLY AFTE R TAKEOFF, CREW EXPERIENCED A STRONG VIBRATION FROM NR 1 ENG. ENGINE VIBRATION SHOWED ABOVE FOUR. CREW RETURNED TO FIE LD AT BOS WHERE THE FLIGHT LANDED WITHOUT INCIDENT. NO EMERG DECLARED. INSP CONFIRMED A BIRD STRIKE. MAINT REMOVED AN D REPLACED DAMAGED 1ST STAGE FAN BLADES, 19, 20, AND 23, ON THE NR 1 ENGINE. ALSO, REPLACED OPPOSITE FAN BLADES 1, 4, A ND 38. ACCOMPLISHED BORESCOPE OF NR 1 ENG HIGH PRESSURE COMPRESSOR 3RD, 5TH, AND 9TH STAGES. ALSO INSPECTED COMBUSTION CHAMBER AND TURBINE SECTION PER MM 71-00-47. PERFORMED ENG RUN AND AVM SIGNAL CONDITIONER CHECK. OPS CHK GOOD. (X) 2 L 7 2 4F 4 F RT A16WE E2GL 1998073100427 19980731 00427 NM 1998 7 31 98UAL900336 1 19980717 A 2613 CLAMP BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE LT WING/BODY LOOSE A UALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 WP 29 399UA 24674 LEFT WING BODY OVERHEAT WARNING LIGHT ILLUMINATED DURING CLIMB. *S/D* ADJUSTED CLAMP ON THERMOCOUPLES AND LIGHT DID NO T ILLUMINATE. 2 L 7 2 4F 4 F RT A16WE E2GL 1998080700673 19980807 00673 1998 8 7 98UAL900368 4 19980728 A 2561 D30665105 SLIDE AIRBUS 320 A320232 3930326 EU IAE V2527 V2527A5 NE PASSENGER DOOR DETACHED A UALA K NONE O OTHER IN INSP/MAINT 1 WP 29 407UA 456 AFT RT ENTRY DOOR ESCAPE RAFT DISMOUNTED AT UPPER END. *S/D* UPPER SPRINGS OF SLIDE PACK DISMOUNTED FROM UPPER STUDS OF DOOR. SLIDE WAS REPLACED PER MM 40-25-62-44. 2 L 7 2 4F 4 F RT A28NM E40NE 1998090401271 19980904 01271 SO 1998 9 4 SWIA971238 1 19980809 A 2752 3431001001 ACTUATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RT TE FLAP FAILED A SWIA K NONE K J FLUID LOSS WARNING INDICATION AP APPROACH 1 NM 07 224SW 120294 LOSS OF BLUE SYSTEM DUE TO LOSS OF ALL FLUID. SERVICED BLUE SYSTEM AS NECESSARY AND REPLACED RIGHT NACELLE FLAP ACTUATO R IAW MM 27-50-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998091100581 19980911 00581 NM 1998 9 11 DLM88981817 1 19980902 A 2421 GENERATOR DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 1 ENGINE SHORTED A DALA C D ABORTED TAKEOFF RETURN TO BLOCK H J ELECT. POWER LOSS-50 PC WARNING INDICATION TO TAKEOFF 1 SO 27 903DE RL384 53380 725528 NR 1 ENG GENERATOR DROPPED OFF LINE, CREW RTO BELOW 85 MPH. REPLACED ENGINE GENERATOR. 2 L 7 2 4F 4 F RT A6WE E9NE 1998111300592 19981113 00592 EU 1998 11 13 CA980707038 1 19980610 A 6710 SC5083 SERVO SNIAS 350 AS350BA 8680817 EU TMECA ARRIEL ARRIEL1B 6OO30 NE MAIN ROTOR FAILED W K NONE F FLT CONT AFFECTED TX TAXI/GRND HDL 1 CA 1142 4525 (CAN) WHILE PERFORMING HYDRAULIC TEST PRIOR TO FLIGHT, CYCLIC STICK HAD A HARD PULL TO THE LEFT WHEN CYCLING HYDRAULIC S WITCH TO 'ON' POSITION. RIGHT HYDRAULIC SERVO REPLACED. 1 G 7 1 3U 3 U NC H9EU E19EU 1998112001102 19981120 01102 SO 1998 11 20 SWIA971307 1 19981018 A 3010 REGULATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE EMPENNAGE DEICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 221SW 120290 VERTICAL STABALIZER, LEFT AND RIGHT HORIZONTAL STABALIZER FAILED IN FLIGHT. RETURNED TO FAT. REPLACED LEFT AND RIGHT P RESSURE REGULATORS. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998120400134 19981204 00134 NE 1998 12 4 CA980928007 2 19980922 A 7260 MS901506 PLUG 717000 BOEING 727 727227 1384078 NM PWA JT8 JT8D9A 52048 NE GEARBOX DAMAGED W E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CR CRUISE 1 CA A0694 666281 (CAN) NR 3 ENGINE OIL QUANTITY WENT TO ZERO IN-FLIGHT. OIL PRESSURE DROPPED TO 38 PSI, LOW OIL PRESSURE LIGHT ILLUMINAT ED AND THE ENGINE WAS SHUT DOWN. THE ENGINE MAINTAINED A POSITIVE OIL PRESSURE ABOVE 20 PSI FOR THE DURATION OF THE FLI GHT. POST-FLIGHT TROUBLESHOOTING FOUND A PLUG, ON THE ENGINE GEARBOX, FORWARD OF THE HYDRAULIC PUMP MOUNTING PAD LEAKIN G. A NEW HELICOIL WAS INSTALLED. THE PLUG WAS REINSTALLED AND A LEAK CHECK WAS CARRIED OUT SERVICEABLE. AIRCRAFT RETU RNED TO SERVICE. 2 L 7 3 4F 4 F A3WE E2EA 1998120400171 19981204 00171 EU 1998 12 4 CA980930022 1 19980921 A 3710 441CC23 DRY AIR PUMP AIRBORNE PARTEN P68 P68C 6780105 EU LYC O360 IO360A1B6 41514 EA VACUUM SYSTEM DAMAGED W O OTHER O OTHER NR NOT REPORTED 1 CA 872 6AJ1 L2370951A (CAN) END SHEARED ON DRY AIR PUMP. 1 H 7 2 3O 3 O A31EU 1E10 1999010100050 19990101 00050 WP 1999 1 1 98UAL900600 1 19981212 A 3397 59183 WIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL DOOR 3R BROKEN A UALA K NONE L NO TEST UK UNKNOWN 1 WP 29 1842U 46635 EEL STRIP LIGHTING WIRE BROKEN AT DOOR 3R. EEL LIGHTS INOP AT DOOR 3 CROSS AISLE AND LAST HALF OF ZONE 3 ON RIGHT SIDE . REPLACED CABLE, BATTERY PACK, AND LEAD ASSEMBLY FOR 3R. ALL OPS CHECK GOOD. 2 L 7 3 4F 4 F A22WE E23EA 1999010800468 19990108 00468 NE 1999 1 8 C2XA98BT080 2 19981103 A 7200 ENGINE AEROSP ATR42 ATR42320 8680930 EU PWA PW121 PW121 52124 NE NR 2 FAILED A C2XA A UNSCHED LANDING X ENGINE FLAMEOUT NR NOT REPORTED 1 SW 09 97841 280 DURING TEST FLIGHT, NR 2 ENGINE FAILED INFLIGHT. AIRCRAFT LANDED UNEVENTFULLY. AIRCRAFT BEING TEST FLOWN FOR NR 2 ECU FAULT IN FLIGHT, RESET ON GROUND, ECU FAULT FLASHING AND UPTRIM LIGHT FLASH ON AND OFF. TROUBLESHOOTING PROBLEM AT PRES ENT TIME. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1999011500551 19990115 00551 NE 1999 1 15 MASA98212 2 19981128 A 7320 CPW311697503 EEC DHAV DHC8 DHC8202 2809007 NM PWA PW120 PW123 NE LT ENGINE MALFUNCTIONED A MASA A UNSCHED LANDING O OTHER CL CLIMB 1 SW 07 448YV 5175 AG0006 448 AG0006 FLT 6310 - PHX-GUC - CLIMBING THROUGH 18,000 FT, THE LEFT ENGINE BEGAN TO RUN ROUGH. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO GUP, WERE NOTED. THE EEC WAS REMOVED AND REPLACED AS A PRECAUTIONARY MEASURE. AIRCRAFT WAS RETURNED TO SE RVICE. (M) 2 H 7 2 4T 4 T RT A13NM E20NE 1999011500751 19990115 00751 SO 1999 1 15 SWIA971359 1 19981231 A 3010 SWITCH EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE LT WIND DEICE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 NM 07 190SW 120050 MIDDLE LEFT WING DEICE INOP WITH TIMER 1 AND TIMER 2 SELECTED. RETURNED TO SLC. MEGGED OUT WIRES FOR LEFT, RIGHT AND M IDDLE BOOT PRESSURE SWITCHES FOUND OK. CHECKED BOTH PRESSURE SWITCHES, FOUND LEFT OK. FOUND RIGHT SET TOO HIGH. REMOV ED AND REPLACED RIGHT MIDDLE PRESSURE SWITCH. CYCLED BOOTS FOR 30 MINUTES, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1999031200268 19990312 00268 1999 3 12 CA980827025 4 19980809 A 2213 COMPUTER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE FLIGHT CONTROL FAILED W O OTHER J WARNING INDICATION DE DESCENT 1 CA 5578 807373 (CAN) AILERON MISTRIM DURING DESCENT. AMBER POSTED ON BOTH PRIMARY FLIGHT DISPLAYS. AUTOPILOT TRANSFERRED TO COPILOT S IDE, AIRCRAFT ROLLED VIOLENTLY TO RIGHT. A/P DISCONNECTED. CONTROL REGAINED MANUALLY. A/P RE-ENGAGED ON PILOT'S SIDE. REPLACED NR 1 FLIGHT CONTROL COMPUTER. PART TC: 4,992. 2 L 7 2 4F 4 F RT A21EA E15NE 1999081200447 19990812 00447 NM 1999 8 12 CA990310039 1 19981121 A 5610 58935723 WINDOW BOEING 737 737217 1384464 NM PWA JT8 JT8D17A 52049 NE COCKPIT CRACKED W O OTHER O OTHER CR CRUISE 1 CA 709520 (CAN) AIRCRAFT ARRIVED WITH NR 4 EYEBROW WINDOW CRACKED ON OUTER PANE. REPLACED. 2 L 7 2 4F 4 F A16WE E2EA 1999100800124 19991008 00124 NE 1999 10 8 99ZZZX3801 2 19981022 A 7230 410101003 VANE ASSY BOLKMS 117 BK117A4 5626017 EU LYC LTS101 LTS101650B1 41560 NE COMPRESSOR CRACKED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 527RM 794 TRIB7411 7111 LE45218EA VANE ASSY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE 2001032200098 20010322 00098 EA 2001 3 22 CA980318019 2 19980226 A 8520 LW10346 CRANKSHAFT PIPER PA31 PA31350 7103110 SO LYC O540 TIO540J2BD 41532 EA ENGINE BROKEN W O OTHER Y J ENGINE STOPPAGE WARNING INDICATION CR CRUISE 1 CA 294 (CAN) ENGINE FAILED IN CRUISE AND LANDED. POST FLIGHT INSPECTION FOUND THE CRANKSHAFT BROKEN IN THREE PLACES. ENGINE SEN T TO R&O FOR INVESTIGATION. 1 L 7 2 3O 3 O A20SO E14EA 2001032600383 20010326 00383 WP 2001 3 26 CA980325044 1 19980310 A 7830 LJ28840 STOP RROYCE RB21122B02 LKHEED 1011 10113851 5265010 WP RROYCE RB211 RB21122B02 54555 NE THRUST REVERSER DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 10066 (CAN) DAMAGED BLOCKER DOOR FOUND ON RAMP INSPECTION, REPLACED. 2 L 7 3 4F 4 F A23WE E12EU 1998060500336 19980605 00336 WP 1998 6 5 TWAA9807003 1 19980423 A 5320 ANGLE DOUG DC9 DC982 3022082 WP BS 865-875-886 CRACKED A TWAA K NONE O OTHER IN INSP/MAINT 1 CE 05 960TW 49231 MCI - DURING OP 15 MAINTENANCE CHECK, FOUND T-ANGLES FOR FILLET FAIRING ATTACH STRUCTURE CRACKED AT CENTERLINE, STA 864, 875, AND 886. THREE CRACKS. REPLACED T-ANGLES PER SRM 51-01, PAGE 1 ITEM C, AND STANDARD PRACTICES. (X) 2 L 7 2 4F A6WE 1998100200081 19981002 00081 SW 1998 10 2 98ZZZX3586 1 19980728 A 5610 GD649C1 WINDSHIELD GULSTM 690TP 690B 7630516 SW COCKPIT CRACKED A L5JA K NONE O OTHER NR NOT REPORTED 1 NM 07 692T 71 11555 PILOT REPORTED CRACKED WINDSHIELD IN-FLIGHT, CRACK PROGRESSED FROM ONE CORNER TO SEVERAL CRACKS. PILOT MADE AN EMERGENC Y LANDING. WINDSHIELD WAS REPLACED. WINDSHIELD WAS RE-CERTIFIED 71 HOURS PRIOR TO INCIDENT. WINDSHIELD RE-CERTIFIED B Y FAA RS OX4R403M. 1 H 7 2 3T 2A4 1998103000100 19981030 00100 NM 1998 10 30 DL72S982169 1 19981020 A 5313 STRINGER BOEING 727 727232 1384082 NM BS 940 CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 421DA 21274 CRACKS WERE FOUND IN THE SKIN, STRINGER AND BS 940 FITTING ON THE RT SIDE OF THE AC AT STRINGER 8A. STRINGER 18A CONTAI NED AN APPROX 2 LONG CRACK, THE SKIN AND FITTING UPON BHEC INSPECTION YEILDED CRACK INDICATIONS. REPAIRED PER ERA 33237 4-14. 2 L 7 3 4F A3WE 1998050800567 19980508 00567 NM 1998 5 8 98FDEA00323 1 19980501 A 5320 6517688107 CREASE BEAM BOEING 727 727233 138408A NM BS 304-358 CORRODED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 265FE 21671 CORROSION (C53-224-01) ON CREASE BEAM AROUND FASTENER HOLES ON UNDERSIDE AT BS 304 TO 358, LBL 60, WL 208. *S/D* REMOV ED AND REPLACED CREASE BEAM BS 294 TO 360, LBL 60, WL 208 IAW FED-EX SRM 51-30-2. PAINTED IAW FED-EX M/M 51-20-151. 2 L 7 3 4F RT A3WE 1998070300439 19980703 00439 WP 1998 7 3 9809639911 1 19980622 A 2720 37723745503 SHUTOFF VALVE DOUG DC9 DC931 3022065 WP RUDDER MALFUNCTIONED A NWAA A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 GL 01 961N 7733 7733 47405 AFTER TAKEOFF, RUDDER WAS ABNORMALLY SENSITIVE TO SMALL AMOUNTS OF INPUT WITH DIFFICULTY TRACKING CENTERLINE. FLIGHT WA S RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RUDDER POWER SHUTOFF VALVE, OPERATIONAL CHECK NORMA L. 2 L 7 2 4F A6WE 1998052200191 19980522 00191 NM 1998 5 22 UPS98226612 1 19980505 A 5315 BAC14902738 FLOORBEAM BOEING 727 72725C 138400H NM BS 312 CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 950UP 19718 INSPECTION TYPE:C WHILE WORKING INTERIOR 119 CUSTOMER NR 717462 DISCOVERED BS 312 FLOORBEAM TOP FLANGE CORRODED RBL 35-5 5 WL 208. CORROSION FOUND OUT OF LIMITS PER SRM 51-10-6 COMPLETED REMOVAL OF CORRODED SECTION AND INSTALLATION OF STAND ARD T CHORD SPLICE PER SRM 53-10-8, 51-30-2, 51-10-2, AND MM 51-20-10 2 L 7 3 4F A3WE 1998091801017 19980918 01017 NM 1998 9 18 SWAA981649 1 19980806 A 5320 ANGLE BOEING 737 7373H4 1384600 NM BS 727 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 301SW 22941 DURING SCHEDULED 1/2D CHECK, FOUND WING TO BODY SUPPORT T-ANGLE FWD END CRACKED AT BS 727. REPAIRED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1998082800466 19980828 00466 WP 1998 8 28 MWEA98884 1 19980822 A 5280 59175281 FRAME DOUG DC9 DC914 3022034 WP LT MLG DOOR CRACKED A MWEA K NONE O OTHER IN INSP/MAINT 1 GL 31 400ME 45727 FOUND CRACK ON LEFT MAIN LANDING GEAR DOOR FRAME ADJACENT TO THE ROLLER ASSEMBLY MOUNT BRACKET. MTC FABRICATED AND INST ALLED DOUBLER REPAIR. 2 L 7 2 4F A6WE 1998041701072 19980417 01072 NM 1998 4 17 ASAA9840054 1 19980311 A 3397 WIRE BOEING 737 7374S3 1384711 NM CABIN DISCONNECTED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 786AS 24795 PDX - DURING MAINTENANCE CHECK, THE AFT TWO EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. RECONNECTED WIRING AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F RT A16WE 1998043000642 19980430 00642 WP 1998 4 30 DLL19980543 1 19980309 A 5711 SPAR LKHEED 1011 10113853 5265020 WP LT/RT WING CRACKED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 756DR 193Y1185 DURING INSPECTION OF THE LT AND RT RS UPPER CAP FASTENER HOLES PER EO 7-59089-3 SEVERAL CRACK INDICATIONS WERE FOUND ON THE SPARS. THE REAR SPAR MODIFICATION WILL NOW BE ACCOMPLSIHED ON THIS AC. THIS REPAIR DOCUMENTS THE DEVIATIONS (REPAI RS) NEEDED TO COMPLETE THE MOD. REPAIRED PER ERA 331368-14AD. 2 L 7 3 4F A23WE 1998110600689 19981106 00689 NM 1998 11 6 SCNA98133 1 19981029 A 3350 900835A BATTERY PACK BOEING 727 727259 138408J NM E & E COMPT DISCHARGED A SCNA K NONE L NO TEST IN INSP/MAINT 1 GL 15 289SC 22475 DURING A LINE MAINTENANCE CHECK, THE LEFT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACK AT THE E & E BAY LOCATION M955, OPERATIONALLY CHECKS GOOD. 2 L 7 3 4F A3WE 1998021900729 19980219 00729 SW 1998 2 19 HEEA0012905 1 19980210 A 5260 SYLC50228 ACTUATOR BELL 412 412 1182202 SW STEP FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 2258F 33073 STEP ACTUATOR WON'T COME UP OR DOWN. 1 G 7 2 4U H4SW 1998052200524 19980522 00524 EU 1998 5 22 HEEA0014153 1 19980511 A 7923 209072433101 VALVE BOLKMS 105 BO105S 5626006 EU OIL SOV FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 50293 S677 VALVE NOT OPENING. 1 G 7 2 3U H3EU 1998092500561 19980925 00561 NE 1998 9 25 98ZZZX3507 1 19980827 A 6710 7690001880106 AMPLIFIER SKRSKY S76 S76A 8143006 NE DROOP COMP MALFUNCTIONED A HEEA O OTHER O OTHER AP APPROACH 1 SW 03 706AE 580 760275 ON APPROACH FOR LANDING, NR 1 ENGINE STARTED TO YAW. LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 DCA AMPLIFIER INOPERABLE, AND THE NR 2 DCA AMPLIFIER ERRATIC. REPLACED BOTH. REF: S-76 IPC, CHAPTER 76-11-00, FIG 1-14 AND FIG 1-16 . 1 G 7 2 3U H1NE 1998112600591 19981126 00591 NM 1998 11 26 AALA981705 1 19980919 A 3350 1001141 LIGHT GRIMES BOEING 727 727227 1384078 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 730AA 2793 20737 DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT ABOVE AIR STAIRS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT AS SEMBLY ABOVE AIR STAIR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 3 4F A3WE 1998112600570 19981126 00570 EU 1998 11 26 SIMA983092 1 19981105 A 3350 301200 POWER SUPPLY AEROSP ATR72 ATR72212 EU CABIN INOPERATIVE A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 420AT 503 420 DFW - FLT 3504 - SOME EMERGENCY FLOOR LIGHTS REMAIN ILLUMINATED. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK. (M) 2 H 7 2 4T RT A53EU 1998041000671 19980410 00671 SW 1998 4 10 HEEA0013582 1 19980326 A 2436 206075447007 VOLT REGULATOR BELL 206 206L1 1182107 SW DC SYS FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 11027 45411 GENERATOR WILL NOT COME ON LINE. 1 G 7 1 3U H2SW 1998110600087 19981106 00087 WP 1998 11 6 ARWA981020 1 19981020 A 5730 SKIN DOUG DC8 DC863F 302198F WP WS 175 CORRODED A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 661AV 45969 LAP - FOUND CORROSION ON RIGHT WING TOP AT STATION XFS 175 CUT OUT AREA OF CORROSION FABRICATED DOUBLER, FILLER AND INST ALLED IAW EO SEMAN NR 1028. WORK ACCOMPLISHED UNDER ARROW AIR FORM M3A CONTROL 1702. (M) 2 L 7 4 4F 4A25 1998021100587 19980211 00587 GL 1998 2 11 HEEA0012759 2 19980203 A 7250 23034775 SUPPORT 23035128 BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENG GAS PROD DAMAGED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 129MR CAT95416 51129 CAE895571 RECEIVING INSPECTION REVEALED: DAMAGED ON GP SUPPORT AFT FLANGE. INSTALLED A DALLAS AIRMOTIVE OVERHAULED GP SUPPORT. 1 G 7 1 3U 3 U H2SW E1GL 1998022500001 19980225 00001 NE 1998 2 25 DL76G980255 2 19980129 A 7200 9315M41P20 THERMAL SHIELD BOEING 767 7673P6 1385105 NM GE CF6 CF680C2B2 30025 NE NR 2 ENGINE CRACKED A A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 154DL 23873 25241 695373 SHOP FINDINGS - NO FLIGHT INCIDENT. DURING OVERHAUL OF ENGINE 695373, THE HPT THERMAL SHIELD WAS FOUND TO HAVE A FLANGE TO FLANGE CRACK. THIS PART PROVIDES THE ROTATING SEAL BETWEEN THE T1 AND T2 DISK. THE THERMAL SHIELD IS NOT LIFE LIMI TED. DUE TO THE CRACK, THE T1 AND T2 DISK WERE SCRAPPED BASED ON GE RECOMMENDATION. 2 L 7 2 4F 4 F RT A1NM E13NE 1998032600573 19980326 00573 NE 1998 3 26 9804851148 2 19980320 A 7320 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 3 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS LD LANDING 1 GL 01 148US 46757 686156 DURING THE LANDING ROLLOUT WHILE IN REVERSE THRUST AT 85 KTS, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 900C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED. THE REVERSER WAS PLACED ON ME L 78-1A DUE TO LACK OF TIME TO OPERATIONALLY CHECK THE RABS. 2 L 7 3 4F 4 F A22WE E20EA 1998041000171 19980410 00171 NE 1998 4 10 9805721154 2 19980330 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 2 ENGINE STALLED A NWAA E ENGINE SHUTDOWN O OTHER LD LANDING 1 GL 01 154US 46763 686148 DURING LANDING ROLLOUT AT APPROXIMATELY 80 KNOTS WHILE IN REVERSE THRUST, THE NR 2 ENGINE COMPRESSOR STALLED. THE ENGIN E WAS SHUT DOWN AT APPROXIMATELY 40 KNOTS. THE EGT WAS AT MAXIMUM INDICATION FOR 10 SECONDS. THE ENGINE WAS BOROSCOPED WITH NO TROUBLE FOUND. DUE TO THE OVERTEMP CONDITIONS THE AIRCRAFT WAS REMOVED FROM SERVICED AND FERRIED TO MSP FOR AN ENGINE CHANGE. EXACT REASON FOR ENGINE STALLS TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998041000401 19980410 00401 SW 1998 4 10 CA980225005 1 19980212 A 6220 206011111003 BEARING BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL M/R TRUNNION SPLIT W K NONE O OTHER IN INSP/MAINT 1 CA JILM57049 CAE822633 (CAN) INNER RACE SPLIT ON MAIN ROTOR TRUNNION BEARING. 1 G 7 1 3U 3 U H2SW E4CE 1998042400549 19980424 00549 NE 1998 4 24 ASOA98023 2 19980306 A 7421 IGNITERS AEROSP ATR72 ATR72212 EU PWA PW120 PW127 NE RT ENGINE MALFUNCTIONED A ASOA E ENGINE SHUTDOWN J X WARNING INDICATION ENGINE FLAMEOUT CR CRUISE 1 SO 11 635AS 372 127026 IN CRUISE FLIGHT CSG-ATL, WITH CONTINUOUS RELIGHT ON, RIGHT ENGINE TORQUE DROPPED TO ZERO FOR 8-10 SECONDS. ENGINE RELI T ON ITS OWN AND CONTINUED FOR THE REMAINDER OF THE FLIGHT. UPON LANDING, CONTINUOUS RELIGHT COULD NOT BE EXTINGUISHED. ATL MAINTENANCE BOROSCOPED THE ENGINE, FOUND NO DEFECTS. REMOVED AND REPLACED HIGH AND LOW PRESSURE FUEL FILTERS AND BOTH IGNITERS. OPERATED DE-ICE SYSTEM AND PERFORMED OPERATED TEST OF IGNITION IN CONTINUOUS RELIGHT MODE WITH NO DEFECT S NOTED. TEST FLIGHT PERFORMED SATISFACTORILY AND THE AIRCRAFT WAS RELEASED FOR FURTHER SERVICE. (M) 2 H 7 2 4T 4 T RT A53EU E20NE 1998050800495 19980508 00495 NE 1998 5 8 98ZZZX1641 2 19980407 A 7321 7436024 FUEL CONTROL BOEING 737 7372B7 1384560 NM PWA JT8 JT8D15A 52051 NE NR 1 ENGINE DEFECTIVE A A USAA E A ENGINE SHUTDOWN UNSCHED LANDING O OTHER CL CLIMB 1 EA 19 268AU 22880 BWI - FL 2197 - AFTER TAKEOFF AT 1,000 FEET, CAPTAIN THOUGHT HE HAD AN ENGINE FAILURE. THE NR 1 ENGINE FAILED TO RESPON D TO THRUST LEVER MOVEMENT. CAPTAIN SHUT DOWN THE NR 1 ENGINE AND RETURNED TO FIELD AT BWI WHERE THE FLIGHT LANDED WIT HOUT INCIDENT. AN EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINTENANCE CHECKED THROTTLE CABLE S FOR FREEDOM OF MOVEMENT. CABLE REMOVED AND REPLACED THE NR 1 ENGINE FUEL PUMP AND FUEL CONTROL UNIT. ENGINE RUN, OPE RATION CHECK AND LEAK CHECK GOOD. REF: OPERATOR CONTROL NR USAASB98091. (X) 2 L 7 2 4F 4 F A16WE E2EA 1998050801351 19980508 01351 NM 1998 5 8 98UAL900164 1 19980426 A 2120 FAN AIRRESEARCH 6056751 BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE LT PACK FAILED A UALA D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 WP 29 7467U 21921 AT PUSH BACK LEFT PACK TRIPPED AND CABIN FILLED WITH SMOKE. *S/D* REPLACED LEFT HAND GROUND COOLING FAN DUE TO FAILURE . 2 L 7 3 4F 4 F A3WE E2EA 1998051500987 19980515 00987 NE 1998 5 15 REXA98083 2 19980331 A 7321 7086M60G11 ECU SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE FAILED A REXA O OTHER Y ENGINE STOPPAGE DE DESCENT 1 SO 25 403BH 340A060 LEFT ENGINE TORQUE AND PROP RPM GAUGE FLUCTUATED 5 PERCENT AND THEN DROPPED TO ZERO FOR A SECOND, THEN BACK UP AND LEFT ENGINE THEN SHUT ITSELF DOWN. REMOVED AD REPLACED ECU. GROUND OPS, CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A52EU E8NE 1998061900124 19980619 00124 NE 1998 6 19 VNAA9806005 2 19980606 A 7200 ENGINE DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT WING BIRD STRIKE A VNAA K NONE C F.O.D. NR NOT REPORTED 1 GL 07 328JS 3030 WHILE INBOUND TO PIT, THE AIRCRAFT WAS STRUCK BY A BIRD ON THE RIGHT HAND ENGINE NACELLE. THE FLIGHT CONTINUED TO PIT, AND LANDED WITHOUT ANY INCIDENT. MAINTENANCE CLEANED AND INSPECTED THE AREA IN ACCORDANCE WITH DORNIER MAINTENANCE MANU AL 05-29-40. NO DAMAGE WAS NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998061900638 19980619 00638 WP 1998 6 19 WTAA980077 2 19980505 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT MALFUNCTIONED A WTAA C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 WP 17 402UE 734 FAT - LEFT ENGINE FAILED TO MAKE MINIMUM STATIC TAKEOFF TORQUE. TAKEOFF ABORTED. MAINTENANCE UNABLE TO DUPLICATE DISCR EPANCY. OPERATIONAL CHECK SATISFACTORY. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998061900818 19980619 00818 NM 1998 6 19 98UAL900240 1 19980605 A 5220 69418683 SEAL BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE EMER EXIT DOOR SPLIT A UALA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 WP 29 941UA 26676 THE RIGHT OVERWING EMERGENCY EXIT DOOR SEAL DEVELOPED A LOUD SQUEAL AND VIBRATION. *S/D* REPLACED THE RIGHT OVERWING EX IT DOOR SEAL BECAUSE THE OLD SEAL HAD A SPLIT OF 8.0 INCHES. INSTALLED RIGHT OVERWING EXIT DOOR. PRESSURIZED CABIN AND CHECKS OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998082100037 19980821 00037 NE 1998 8 21 TWAA9810801 2 19980707 A 7261 STRAINER DOUG DC9 DC951 3022051 WP PWA JT8 JT8D17 52049 NE RT ENGINE CLOGGED A TWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 CE 05 408EA 47693 1724 TYS - FLT 599 - THE RIGHT ENGINE OIL STRAINER CLOGGING LIGHT CAME ON. REDUCED POWER TO IDLE AND LIGHT WENT OUT. DECLAR ED AN EMERGENCY AND MADE UNSCHEDULED LANDING. FOUND SMALL AMOUNT OF METAL AND CARBON IN MAIN OIL SCREEN. INSTALLED NEW FILTER, DRAINED AND RESERVICED OIL, AND RAN ENGINE. RE-CHECKED MAIN OIL SCREEN AND OK. CHCKED AGAIN AT NEXT STATION A ND OK. CHECK-C 2-6-98 STL. (X) 2 L 7 2 4F 4 F RT A6WE E2EA 1998082800176 19980828 00176 NM 1998 8 28 CA980430015 1 19980417 A 7921 28E997 OIL COOLER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NR 2 ENGINE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 12262 109 120896 (CAN) DURING WALK-AROUND, AN OIL LEAK WAS FOUND ON THE NR 2 ENGINE OIL COOLER. THE OIL LEAK WAS FROM THE MATRIX AREA. T HE OIL COOLER WAS REPLACED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998090400068 19980904 00068 EA 1998 9 4 CA980608020 1 19980522 A 3320 BALLAST CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE CABIN FAILED W K NONE B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA 7042 807380 (CAN) ELECTRICAL BURNING SMELL IN CABIN. BALLAST OF OVERHEAD LIGHTING AT ROW 5/6F FOUND BURNED. PART TC: 6,154. 2 L 7 2 4F 4 F RT A21EA E15NE 1998091100470 19980911 00470 NM 1998 9 11 CA980616009 1 19980531 A 3230 82910010209 TUBE DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE NLG LEAKING W K NONE O OTHER IN INSP/MAINT 1 CA 123010 (CAN) HYDRAULIC FLUID LEAKING FROM FORWARD AREA OF NOSE WHEEL WELL. HYDRAULIC LINE FOR THE GEAR DOWN SEQUENCE VALVE, TH E NR FOUR LINE FROM THE TEE FITTING WAS LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1998092500697 19980925 00697 NE 1998 9 25 P5CA9801460 2 19980918 A 7200 ENGINE BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 4 ENGINE FAILED A P5CA A E UNSCHED LANDING ENGINE SHUTDOWN M OVER TEMP CR CRUISE 1 WP 23 852FT 19757 662566 AT FL 330 NR 4 ENGINE STALLED WITH AN AUDIBLE SOUND AND WENT TO A OVER TEMP OF 950Ý FOR 3-4 SECONDS. ENGINE WAS THEN SH UT DOWN, PER CHECK LIST. RELIGHT WAS ATTEMPED AT FL 240 BUT THE EGT WAS MUCH HIGHER AS ENGINE STARTED TO ACCELERATE. T HE ENGINE WAS SHUT DOWN. FOUND METAL IN TAIL PIPE. ENGINE WAS CHANGED PER POLAR WORK CARD M7100-002 AND RUN PER M7100- O11. 2 L 7 4 4F 4 F A20WE E20EA 1998100200136 19981002 00136 SO 1998 10 2 SWIA971261 1 19980905 A 2150 PACK EMB 120 EMB120RT SO PWA 118 PW118 NE RIGHT FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 269UE 120196 RIGHT PACK FAILED AT 21,600 RESULTING IN LOSS OF CABIN PRESS DUE TO DEFERRED LEFT PACK. RETURNED TO LAS. RUN AND LEAKS CHECK OF RIGHT PACK. BLOWS STRONG, COULD NOT GET IT TO FAIL. OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998100200348 19981002 00348 NE 1998 10 2 COMA9860280 2 19980915 A 7530 5050737G01 ACTUATOR CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE RT ENGINE LEAKING A COMA K NONE K FLUID LOSS IN INSP/MAINT 1 SO 01 915CA 5607 7013 VG ACTUATOR AT THE SEVEN O'CLOCK POSITION ON THE RIGHT ENGINE IS LEAKING FUEL. REPLACED ACTUATOR. 2 L 7 2 4F 4 F RT A21EA E15NE 1998100900321 19981009 00321 NM 1998 10 9 CA980706016 1 19980417 A 2710 AILERONS DHAV DHC8 DHC8301 NM PWA PW120 PW123 NE WING FAILED W O OTHER F FLT CONT AFFECTED LD LANDING 1 CA 123010 (CAN) ON LANDING IN LEFT CROSSWIND, THE AILERONS DISCONNECTED AT TOUCHDOWN WITH CAPTAIN FLYING. FIRST OFFICER'S AILERONS WERE STILL CONNECTED. CAPTAINS RECONNECTED ON ROLL-OUT. NO FAULTS FOUND. MOD 8/2376, SB 8-27-79 PREVIOUSLY ACCOMPLIS HED. 2 H 7 2 4T 4 T RT A13NM E20NE 1998100900332 19981009 00332 NM 1998 10 9 CA980706029 1 19980620 A 5330 PANEL BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE FUSELAGE MISSING W K NONE O OTHER IN INSP/MAINT 1 CA P709651 (CAN) FOUND LEFT WING TO FUSELAGE PANEL NR 195C MISSING. NEW PANEL INSTALLED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998101400012 19981014 00012 NM 1998 10 14 98UAL900463 1 19980920 A 5400 321U2731124 BRACE BOEING 747 747422 1384935 NM PWA 4056 PW4056 NE NR 1 PYLON GOUGED A UALA K NONE E VIBRATION/BUFFET IN INSP/MAINT 1 WP 29 181UA 4382 25278 A .060 INCH DEEP GOUGE IN PYLON NUMBER ONE DIAGONAL BRACE. THE GOUGE IS 40 INCHES FORWARD OF AFT END OF DIAGONAL BRACE AND 1.74 INCHES LONG BY .5 INCH WIDE. CAUSED BY CONTACT WITH STEEL PNEUMATIC LINE. PYLON NUMBER ONE DIAGONAL BRACE REP LACED BEFORE FURTHER FLIGHT. NO SUCH CONDITION DETECTED ON THE OTHER THREE PYLON DIAGONAL BRACES. UAL ACFT WITH SIMILA R CONFIGURATION TO BE CHECKED FOR DAMAGE. 2 L 7 4 4F 4 F RT A20WE E24NE 1998111301217 19981113 01217 NE 1998 11 13 98UAL900524 2 19981105 A 7230 1B3517 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE NR 2 ENGINE COAKED A UALA A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 529UA 4765 25019 727117 FLIGHT DIVERTED TO TLH DUE TO SMOKE IN THE COCKPIT AND CABIN. *S/D* AFTER ENGINE DISASSEMBLY, EVIDENCE SHOWED OIL HAD GONE THROUGH THE HPC OF THE NUMBER 2 ENGINE. THIS CAUSED SMOKE TO PASS THROUGH THE RIGHT ENGINE BLEED. THE NUMBER 2 EN GINE WAS REPLACED. 2 L 7 2 4F 4 F RT A2NM E17NE 1998112600747 19981126 00747 SO 1998 11 26 SWIA971310 1 19981110 A 3020 REGULATOR EMB 120 EMB120RT SO PWA 118 PW118A NE LT ENGINE FAILED A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 268UE 120207 LEFT ENGINE INLET DEICE FAILS IN FLIGHT. RETURNED TO FIELD. REPLACED BOTH PRESSURE REGULATORS FOR DEICE SYSTEM, OPS CH ECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998120400110 19981204 00110 SW 1998 12 4 CA980916069 1 19980901 A 6420 206011812005 TRUNNION 206011810139 BELL 206 206L4 1182110 SW ALLSN 250C 250C30P 03013 GL TAIL ROTOR BRINNELLED W K NONE O OTHER IN INSP/MAINT 1 CA 3288 HB341 CAE895726 (CAN) DURING TAIL ROTOR BLADE REMOVAL, TRUNNION FELT RATCHETY AND HAD NO PRELOAD. TRUNNION RACE BRINNELLED BEYOND LIMIT S. 1 G 7 1 3U 3 U NC H2SW E1GL 1999010800420 19990108 00420 NE 1999 1 8 PLGA981112A 2 19981112 A 7200 ENGINE SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LEFT MALFUNCTIONED A PLGA D F RETURN TO BLOCK ACTIVATE FIRE EXT. B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 NE 05 744BA 340A105 367501 BOS - FLT 4408 - AFTER ENGINE START AND TAXI AWAY FROM GATE, THE CREW REPORTED HEARING A DISTINCTIVE MUFFLED METALLIC 'T HUD' FROM THE LEFT ENGINE AREA WITH NO ABNORMAL COCKPIT DISPLAY. THE CREW THEN NOTICED SMOKE COMING OUT THE LEFT ENGINE EXHAUST AREA. THE ENGINE WAS SHUT DOWN AND LEFT FIRE EXTINGUISHER ACTIVATED. PASSENGERS WERE OFF LOADED WITHOUT INCID ENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE. 2 L 7 2 4T 4 T RT A52EU E8NE 1999021200902 19990212 00902 EA 1999 2 12 CA980814015 1 19980729 A 2750 7805011 LEVER CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE FLAP CONTROL FAILED W O OTHER F FLT CONT AFFECTED AP APPROACH 1 CA 6185 807339 (CAN) EN ROUTE FLAPS FAIL CAUTION MESSAGE AFTER SELECTING FLAPS TO 8 DEGREES ON APPROACH. FLAPS INDICATED EXTENDED. RE PLACED FLAP CONTROL POSITION LEVER.. PART TC: 5,470. 2 L 7 2 4F 4 F RT A21EA E15NE 1999052800005 19990528 00005 NM 1999 5 28 CA990111032 1 19981220 A 2910 82970010477 LINE 759162801 DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HYDRAULIC SYS CRACKED W O OTHER K J FLUID LOSS WARNING INDICATION LD LANDING 1 CA 22800 0183A 120329 (CAN) LOST 2 LITRE HYDRAULIC FLUID IN-FLIIGHT FROM NR 2 SYSTEM. LINE FOUND LEAKING. REF IPC 29-10-00, FIGURE 30, ITEM 345. 2 H 7 2 4T 4 T RT A13NM E20NE 1998080700612 19980807 00612 WP 1998 8 7 VJ9800263 1 19980527 A 5320 SUPPORT DOUG DC9 DC932 3022066 WP BS 820 CORRODED A ZZDA O OTHER O OTHER IN INSP/MAINT 1 SO 15 935VV 47534 FWD CARGO PIT UPPER AND LOWER FLOOR SUPPORT L-ANGLE HAS CORROSION BEYOND LIMIT AT FS 820, L28L TO L28R. REMOVED CORROSI ON AND FABRICATED L-ANGLE FLOOR SUPPORT IAW DC9 SRM 53-20, 51-10-2 AND 51-10-2A. HEAT TREATED, PRIMED AND INSTALLED L-A NGLE. 2 L 7 2 4F A6WE 1998043000724 19980430 00724 NM 1998 4 30 USAA980096 1 19980223 A 5313 STRINGER BOEING 737 737201 1384454 NM BS 747 CRACKED A USAA K NONE O OTHER IN INSP/MAINT 1 EA 19 254AU 40136 22796 INT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CRACK 1 INCH AT STATION 747 STRINGER REPAIR, REPAIRED PER 53-10-3. (M) 2 L 7 2 4F A16WE 1998072400344 19980724 00344 NM 1998 7 24 PCAA9800771 1 19980526 A 5270 SWITCH DHAV DHC8 DHC8102 2809003 NM PASS DOOR DIRTY A PCAA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 EA 13 804EX 227 EN ROUTE FROM DCA TO ISP, THE PASSENGER DOOR LIGHT ILLUMINATED. AIRCRAFT DIVERTED INTO ACY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE DOOR SEAL SWITCH AT FAULT. THE SWITCH WAS CLEANED AND ADJUSTED, THE AIRCRAFT WAS PRESSURE TESTED ON THE GROUND AND NO FURTHER FAULTS FOUND. A/C RETURNED TO SERVICE. (M) 2 H 7 2 4T RT A13NM 1998091100433 19980911 00433 1998 9 11 TWRA9845 4 19980808 A 3425 69B147891 HANDLE BOEING 747 747130 1384880 NM MODE SELECTOR DETACHED A TWRA K NONE L NO TEST IN INSP/MAINT 1 EA 15 603FF 19746 PRIOR TO DEPARTURE R4 MED MODE SELECTOR HANDLE CAME OFF. UNABLE TO SELECT AUTO OR MANUAL. ITEM HAS DEFERRED TO ODI MEL 25-10-B (ND). REPLACED MODE SELECTOR HANDLE. OPS CHECK OK. (M) 2 L 7 4 4F A20WE 1998061200508 19980612 00508 EU 1998 6 12 SIMA981181 1 19980428 A 3350 OL3071BPEGPL BULB AEROSP ATR72 ATR72212 EU CABIN FAILED A SIMA K NONE L NO TEST IN INSP/MAINT 1 SW 21 407AT 407 DFW - FLT 4151 - FLOOR PROXIMITY LIGHT AT ROW 6 INOP. ISSUED MEL 33-22 AND RETURNED A/C TO SERVICE. R/I'D BULB. PERFO RMED OPERATIONAL CHECKS SATISFACTORILY AND RETURNED A/C TO SERVICE. (M) 2 H 7 2 4T RT A53EU 1998032600627 19980326 00627 EU 1998 3 26 HEEA0013353 1 19980317 A 3340 A490ATSDF1428 POWER SUPPLY SNIAS 350 AS350B2 8680813 EU STROBE FAILED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 6097Z 2820 WILL NOT FIRE ANTI-COLLISION LIGHT. 1 G 7 1 3U H9EU 1998112600509 19981126 00509 NM 1998 11 26 CKSA98705 1 19981120 A 5220 65B0988915 GATE BOEING 747 7472B4B 138481B NM R4 DOOR CORRODED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 713CK 21099 RT NR 4 DOOR UPPER GATE ASSY CORRODED ALONG HINGE AREA. REMOVED CORROSION IAW SRM 51-10-01, FOUND TO BE BEYOND LIMITS. REPLACED UPPER GATE ASSY IAW BOEING ASA CKF-MED-066, SRM 51-30-02 AND ADJUSTED DOOR IAW MM 52-11-01. FOUND DURING ACCO MPLISHMENT OF CARGO CONVERSION, ROUTINE C-CHECK, AND ACCOMPLISHMENT OF CPCP TASK CARDS AT BOEING WICHITA (KIAB). WORK O RDER NUMBER MO280, TASK CARD NR 7CI8443, CPCP TASK CARD NR C5-210-09-01. 2 L 7 4 4F RT A20WE 1998071700614 19980717 00614 WP 1998 7 17 98ZZZX2391 1 19980626 A 5347 SEAT TRACK DOUG DC9 DC932F 3022067 WP BS 1165 WORN A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 932F 47757 47355 DURING C-CHECK, MAIN CABIN SEAT TRACK WAS WORN AT RBL 33.25. REF: OPERATOR CONTROL NRS EIAA980214, AND, 98ZZZX2367 THR OUGH 98ZZZX2391. 2 L 7 2 4F A6WE 1998112600541 19981126 00541 EU 1998 11 26 SIMA9830615 1 19981102 A 5347 SEAT TRACK SAAB SF340 340B 7860101 EU BS 297-329 CORRODED A SIMA K NONE O OTHER IN INSP/MAINT 1 SW 21 332AE 340B332 ABI - FOUND SEAT TRACKS BL 0 AND 18.3L AT FS 297-329 CORRODED BEYOND SRM LIMITS. CUT OUT 32 INCH SECTION OF EXISTING SE AT TRACKS, FABRICATED AND INSTALLED 32 INCH LONG EXTRUSIONS. AIRCRAFT OK FOR SERVICE. (M) 2 L 7 2 4T RT A52EU 1998092500094 19980925 00094 NM 1998 9 25 CALA9801792 1 19980916 A 5320 CHANNEL BOEING 727 727224 1384076 NM BS 1140 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 93738 20666 INSPECTION FOUND RT AFT LAV FLOOR WAS HAT CHANNEL CORRODED AT FS 1140, RBL 24 TO 60. THE HAT CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-2, 51-30-1, AND 51-20-1. 2 L 7 3 4F A3WE 1998092500765 19980925 00765 EU 1998 9 25 QXEA9801329 1 19980824 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CREASED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 496US 11167 CREASE IN REAR CARGO DOOR OUTER SKIN AT 3RD FRAME NEAR HINGE AREA. REPAIRED IAW FOKKER SRM 52-02-01, PAGE 3 FIGURE 2 AN D SRM 51-31-01. 2 L 7 2 4F RT A20EU 1998100200422 19981002 00422 NM 1998 10 2 SWAA982137 1 19980917 A 5730 SKIN BOEING 737 7372H4 138448C NM LT WING FRAYED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 071SW 22358 DURING SCHEDULED 1/4D CHECK, FOUND LT W/W CUTOUT OUTER REAR PANEL FWD EDGE IS FRAYED AND WORN. REPAIRED PER BOEING SRM. 2 L 7 2 4F A16WE 1998020500385 19980205 00385 NM 1998 2 5 98FDEA00067 1 19980131 A 5720 65185962 FITTING BOEING 727 72721C 138400M NM BS 870 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 143FE 19136 NR 0833 056, STA-PAE - UPON REMOVAL OF LOWER RT SPLICE FITTING FOR WING CENTER SECTION, FOUND FITTING (P/N 65-18596-2) T O BE CRACKED AND CORRODED. REMOVED AND REPLACED LOWER RT SPLICE FITTING FOR WING CENTER SECTION PER FEDEX SRM 51-30-2. 2 L 7 3 4F A3WE 1998081400096 19980814 00096 WP 1998 8 14 ABXA9800695 1 19980803 A 5320 991075513 WEB DOUG DOUG DC9 DC933F 302207A WP BS 775-794 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 935AX 47413 DURING C-CHECK, FOUND CUSP WEB CRACKED IN 2 PLACES BETWEEN STATIONS 775 TO 794 LEFT SIDE, BL 20. REPAIRED WEB IAW DC9 S RM 53-01. 2 L 7 2 4F A6WE 1998102300336 19981023 00336 NM 1998 10 23 P5CA9801548 1 19981007 A 5311 FRAME BOEING 747 747122 1384872 NM BS 1740 DAMAGED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 851FT 19756 MAIN CABIN FRAME STATION 1740R STR 12R FOUND DAMAGED. REPAIRED DAMAGE PER SRM 53-10-04. 2 L 7 4 4F A20WE 1998031900451 19980319 00451 NM 1998 3 19 AALA980162 1 19980116 A 5311 FRAME BOEING 727 727223 1384074 NM BS 950 BENT A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 864AA 21369 TUL - STA 950C STR 26R FRAME UPPER FLANGE BENT. INSTALLED DOUBLER PER SRM 53-10-4 PAGES 3-6. TST: 56,192 HOURS. CYCL ES: 34,665. (X) 2 L 7 3 4F A3WE 1998073100477 19980731 00477 EU 1998 7 31 AALA981159 1 19980606 A 3610 2320550 CLAMP AIRBUS 300 A300B4605R 3930308 EU NR 2 ENGINE FAILED A AALA A F UNSCHED LANDING ACTIVATE FIRE EXT. M J OVER TEMP WARNING INDICATION CL CLIMB 1 SW 07 14056 463 MIA - FLT 1153 - AFTER TAKEOFF MIA, CREW RECEIVED A NR 2 FIRE WARNING AND THROTTLE BECAME JAMMED. DISCHARGED FIRE BOTTL ES AND SHUT ENGINE DOWN. AIR INTERRUPTED AND LANDED MIA WITHOUT INCIDENT. REPLACED ENGINE DUE TO DAMAGE CAUSED BY BLOW N PNEUMATIC DUCT. PERFORMED ENGINE RUN UP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M) 2 L 7 2 4F RT A35EU 1998112000797 19981120 00797 NM 1998 11 20 AALA981861 1 19981006 A 5313 STRINGER BOEING 727 727223 1384074 NM BS 290 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 883AA 21522 TUL - FOUND STRINGER CORRODED AT LEVELING COMPOUND STRINGER 24R, STATION 290. INSTALLED STRINGER REPAIR PER SRM 53-10-3 DET 2. (M) 2 L 7 3 4F A3WE 1998071400015 19980714 00015 NM 1998 7 14 CALA9801199 1 19980701 A 5720 STRAP BOEING 727 727227 1384078 NM LT WING CRACKED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 17773 21045 INSPECTION FOUND A 9/16 CRACK IN STRAP AT LT WING LOWER TRAILING EDGE AT OUTBOARD SIDE OF NR 3 FLAP TRACK MOUNT PAD AFT OF FALSE SPAR AREA. THE CRACKED AREA WAS REMOVED IAW SRM 51-10-1. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10- 1, 51-10-2, AND 51-40-4. 2 L 7 3 4F A3WE 1998103000081 19981030 00081 EU 1998 10 30 QXEA9801522 1 19981021 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU ROW 8 FAILED A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 494US 11167 GEG - EXIT SIGN AT ROW 8 HAS SEVERAL BULBS OUT. MAINTENANCE RELAMPED, OPERATIONAL TESTED NORMAL. 2 L 7 2 4F RT A20EU 1998021900433 19980219 00433 NM 1998 2 19 AALA980037 1 19980107 A 3350 LIG5192 LIGHT BOEING 727 727223 1384074 NM CABIN INOPERATIVE A AALA K NONE L NO TEST IN INSP/MAINT 1 SW 07 869AA 21374 TUL - EMERGENCY EXIT LIGHT IN AFT LEFT GALLEY GOES DIM AFTER LIGHT IS TURNED TO ON POSITION. REMOVED AND REPLACED EMERG ENCY EXIT LIGHT WITH SERVICEABLE UNIT NR LIG 5192 SN ON 4307. OPERATION CHECKS NORMAL. TST: 56,854.46 HOURS. CYCLES: 35,139. (X) 2 L 7 3 4F A3WE 1998022600852 19980226 00852 WP 1998 2 26 UPS98825884 1 19980216 A 5320 4612650N FITTING DOUG DC8 DC871F 302199D WP BS 8 RT CORRODED A IPXA K NONE O OTHER IN INSP/MAINT 1 SO 01 752UP 45952 INSPECTION TYPE-C, LONG 33R FITTING FS 8 CORROSION REMOVAL BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D . 2 L 7 4 4F RT 4A25 1998010800944 19980108 00944 NM 1998 1 8 DLM88980014 1 19980104 A 2424 GCU 947F94538 DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE RIGHT INOPERATIVE A DALA A UNSCHED LANDING H J ELECT. POWER LOSS-50 PC WARNING INDICATION CL CLIMB 1 SO 27 929DL SL3082B 49716 726932 A/C DIVERTED TO MCO. RIGHT GEN FAIL LIGHT IN FLIGHT WITH CROSSTIE LOCKOUT. REPLACED RIGHT GENERATOR CONTROL UNIT. 2 L 7 2 4F 4 F RT A6WE E9NE 1998021100283 19980211 00283 NE 1998 2 11 P5CA9800165 2 19980121 A 7250 RAIL BOEING 747 747132 1384882 NM PWA JT9 JT9D7A 52054 NE NR 3 ENGINE CRACKED A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 856FT 19897 6630626 NR 3 ENG TEC S-RAIL AT 1:30 AND 10 O'CLOCK POSITION HAS 2 EA RACETRACK SLOT O/D CRACKS. WELDED AND RELIEVED PER PWA MM 72-53-01 NR 22. 2 L 7 4 4F 4 F A20WE E20EA 1998022600072 19980226 00072 GL 1998 2 26 98ZZZX805 2 19980213 A 7323 252469210 GOVERNOR BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENGINE MALFUNCTIONED A HEEA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CL CLIMB 1 SW 03 8593X BR41580 51509 CAE895845 DURING TAKEOFF, ROTOR RPM DECAYED TO 97 PERCENT. WOULD NOT RECOVER. PILOT LANDED WITHOUT INCIDENT. ALL TROUBLESHOOTIN G REVEALED NO DISCREPANCIES, COULD NOT DUPLICATE PROBLEM. MAINTENANCE CHANGED GOVERNOR FOR PRECAUTION. REF: ALLSION C -30 IPC, CHAPTER 73-20-00, FIGURE 5, PAGE 2, ITEM 59. 1 G 7 1 3U 3 U H2SW E1GL 1998031200993 19980312 00993 WP 1998 3 12 WTAA980013 2 19980120 A 7200 ENGINE BAG JETSTM JETSTM3101 1500215 EU GARRTT TPE331 TPE33110U 01514 WP LEFT BIRDSTRIKE A WTAA A UNSCHED LANDING C F.O.D. CL CLIMB 1 WP 17 418UE 780 SMF - BIRDSTRIKE REPORTED ON LEFT ENGINE AREA DURING TAKEOFF. AIRCRAFT RETURNED TO STATION WITHOUT INCIDENT. MAINTENAN CE ACCOMPLISHED BIRDSTRIKE INSPECTION. EVIDENCE OF BIRDSTRIKE REPORTED IN LEFT ENGINE OIL COOLER AREA ONLY. NO DAMAGE TO PROPELLER OR ENGINE INGESTION REPORTED. CLEANED AND INSPECTED LEFT ENGINE OIL COOLER. PERFORMED ENGINE GROUND RUN. ALL ENGINE OPERATIONS NORMAL. AIRCRAFT RETURNED TO SERVICE. (M) 2 L 7 2 4T 4 T RT A21EU E4WE 1998040200109 19980402 00109 GL 1998 4 2 CA980311014 2 19980223 A 7200 ENGINE CVAC 340 340CVAC 242270A WP ALLSN 501D 501D13 03004 GL NR 1 FAILURE W E ENGINE SHUTDOWN O R OTHER PARTIAL RPM/PWR LOSS CL CLIMB 1 CA 501041 (CAN) ON CLIMB OUT, NR 1 ENGINE LOST HORSE POWER, LOW TIT, NR 1 ZONE FIRE WARNING LIGHT CAME ON. FLIGHT CREW SHUT ENGIN E DOWN AND AIRCRAFT RETURNED TO POINT OF ORIGIN. INITIAL INVESTIGATION REVEALED DEBRIS IN THE TAIL PIPE INDICATING A TU RBINE FAILURE. ENGINE BEING REPLACED. 2 L 7 2 4R 4 T 6A6 E282 1998041000393 19980410 00393 NE 1998 4 10 CA980305008 2 19980217 A 7261 500327702 OIL SUMP PWA JT9 JT9D7R4D 52054 NE NR 1-2 BEARING CRACKED W A K NONE O OTHER IN INSP/MAINT 1 CA 47357 41827 P707535 (CAN) DURING DISASSEMBLY OF THE ENGINE DUE TO HIGH OIL CONSUMPTION, THE NR 1 AND NR 2 BEARING OIL SUMP WAS FOUND CRACKED IN TWO PIECES. NUMEROUS CRACKS BEYOND ACCEPTABLE LIMITS WERE ALSO FOUND DURING DISASSEMBLY OF THE LP COMPRESSOR ON STA GE 1, 1.5, 2 AND STAGE 3 STATOR. THE PARTS WERE REMOVED FROM SERVICE AND FURTHER EVALUATION IS BEING CARRIED OUT. A FUR THER REPORT WILL FOLLOW. PART TC: 14,715. 4 F E3NE 1998052200077 19980522 00077 NE 1998 5 22 9809071157 2 19980510 A 7230 COMPRESSOR DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20 52054 NE NR 3 ENGINE STALLED A NWAA C D ABORTED TAKEOFF RETURN TO BLOCK R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 GL 01 157SU 46766 686184 DURING TAKEOFF ROLL, THE NR 3 ENGINE COMPRESSOR STALLED WITH FLAMES REPORTED FROM THE TAILPIPE. THE TAKEOFF WAS ABORTED AT 25 KTS. THE EGT REACHED A MAXIMUM OF 800C AND THE ENGINE RECOVERED. MAINTENANCE INSPECTED THE ENGINE INCLUDING A B OROSCOPE WITH NO TROUBLE FOUND. AN EVC CHANGE AND PRECISION TRIM WAS DEFERRED FOR 5 CYCLES. EXACT PART CAUSING PROBLEM TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998052200229 19980522 00229 WP 1998 5 22 TC8A98024 1 19980513 A 2612 D5030 FIRE LOOP DOUG DC8 DC862F 3021972 WP PWA JT3D JT3D7 52039 NE NR 2 ENGINE INOPERATIVE A TC8A A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 GL 23 183SK 45904 671250 TRIP NR 01807, FIRE WARNING NR 2 ENGINE ON CLIMB. NR 2 ENGINE FIRE DETECTION SYSTEM CHECKED IAW M/M 26-00. FOUND UPPER FIRE LOOP INOP. UPPER FIRE LOOP REPLACED AND TESTED IAW 26-10-1, FOUND IN NORMAL CONDITION. 2 L 7 4 4F 4 F 4A25 1E8 1998060500106 19980605 00106 NE 1998 6 5 CA980512014 2 19980427 A 7230 522194 SPACER DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7 52053 NE COMP 3RD STAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 65842 P654059D (CAN) DURING DISASSEMBLY OF THE ENGINE TO INSPECT FOR METAL CONTAMINATION, THE FRONT COMPRESSOR ROTOR THIRD (TO FOURTH) STAGE SPACER WAS FOUND CRACKED. THE PART WAS REMOVED FROM SERVICE AND A FURTHER EVALUATION WILL BE DONE WITH ANOTHER SDR REPORT TO FOLLOW. PART TC: 66,106. 2 L 7 2 4F 4 F A6WE E2EA 1998070300426 19980703 00426 NM 1998 7 3 VNAA9806016 1 19980628 A 7712 31694201 SENSOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT ENGINE FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 437JS 3055 THE LEFT HAND ENGINE TORQUE INDICATION FAILED, DURING THE TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTEN ANCE INSPECTED AND REPLACED THE LEFT HAND ENGINE TORQUE PROBE SENSOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-0 1-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998071400405 19980714 00405 NM 1998 7 14 98UAL900299 1 19980628 A 3350 S106 BATTERY PACK BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN LOOSE A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7298U 21893 FIRST CLASS CABIN CEILING EMERGENCY EXIT LIGHT INOPERATIVE. *S/D* RESEATED BATTERY PACK. 2 L 7 3 4F 4 F A3WE E2EA 1998072400639 19980724 00639 NE 1998 7 24 SWIA971214 2 19980709 A 7200 ENGINE EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT MALFUNCTIONED A SWIA A UNSCHED LANDING O OTHER CL CLIMB 1 NM 07 216SW 120285 HIGH PITCHED WHINE (GRINDING SOUND) COMING FROM RIGHT ENGINE AREA. RETURNED TO FIELD. INSPECTED RIGHT ENGINE TURBINE C OMPRESSOR BLADES AND FOUND NO PROBLEMS. RAN RIGHT ENGINE FOR SEVERAL MINUTES. NO PROBLEMS NOTED. 2 L 7 2 4T 4 T RT A31SO E20NE 1998073100373 19980731 00373 1998 7 31 CA980406010 1 19980313 A 7600 202255053 TMS ACTUATOR LYC ALF502 ALF502R5 41580 NE NR 2 ENGINE FAILED W K NONE O OTHER TX TAXI/GRND HDL 1 CA 1993 LR05628A (CAN) NR 2 ENGINE WOULD NOT SHUT DOWN ON ARRIVAL. NR 2 FIRE HANDLE PULLED TO SHUT DOWN ENGINE. TMS ACUATOR REPLACED. 4 F E6NE 1998090400090 19980904 00090 NM 1998 9 4 CA980610010 1 19980601 A 7603 87600518001 CABLE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE ENGINE CONDITION FRAYED W K NONE O OTHER IN INSP/MAINT 1 CA 19001 120439 (CAN) DURING ENGINE INSPECTION, FOUND THE LEFT LOWER CONDITION LEVER CABLE FRAYED WHERE IT PASSES OVER A PULLEY, FORWARD OF THE ENGINE FIREWALL. PART TC: 19,167. 2 H 7 2 4T 4 T RT A13NM E20NE 1998092500141 19980925 00141 NE 1998 9 25 ARWA980909 2 19980917 A 7230 FAN BLADES DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE BENT A ARWA K NONE O OTHER IN INSP/MAINT 1 SO 19 1808E 46105 ON PREFLIGHT FOUND BENT FAN BLADES NR 4 ENGINE. BLENDED 5 BLADES PER JT3D M/M (P/W) 72-00-00 BORESCOPE C/W, NO DEFECTS NOTED AT THIS TIME IAW M/M 72-00-00. 2 L 7 4 4F 4 F 4A25 1E8 1998100900359 19981009 00359 1998 10 9 CA980707043 4 19980618 A 6113 57A24041 LOW PITCH STOP BEECH 95 95B55 1152729 CE CONT O470 IO470L 17026 SO HARTZL HCC2Y BHCC2YF2 GL SPINNER STRIPPED W K NONE O OTHER IN INSP/MAINT 1 CA 24 CS192942R AN5504 (CAN) DURING INSPECTION, THE PROPELLER SPINNER WAS FOUND LOOSE. INVESTIGATION FOUND THE THREADS ON THE LOW PITCH STOP W ERE STRIPPED. THE FORWARD END OF THE SPINNER IS SECURED TO THE LOW PITCH STOP. THIS LOW PITCH STOP WAS INSTALLED 24 HO URS PREVIOUSLY FOR THE SAME PROBLEM. THE THEN LOW PITCH STOP WAS ALSO FOUND STRIPPED AFTER 30 HOURS TIME SINCE NEW. THE LOW PTICH STOP WAS AGAIN REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1 L 7 2 3O 3 O RT 3A16 3E1 5 C P920 1998111300724 19981113 00724 EA 1998 11 13 CA980909012 1 19980808 A 2750 TE FLAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WING FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 807343 (CAN) FLAPS FAIL MESSAGE ON FLAP SELECTION FROM 30 TO 45 DEGREES. RESET CIRCUIT BREAKERS ON BOTH CHANNELS, TWIST CHECK CARRIED OUT AND SYSTEM CHECKED SERVICEABLE. 2 L 7 2 4F 4 F RT A21EA E15NE 1998112000579 19981120 00579 NM 1998 11 20 VNAA9811012 1 19981111 A 2910 HYD FLUID DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE A HYD SYST REQD SERVICE A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 328JS 3030 A-HYDRAULIC QUANTITY LOW WARNING MESSAGE ILLUMINATED, DURING THE TAXI OUT FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GAT E. MAINTENANCE INSPECTED AND SERVICED THE HYDRAULIC SYSTEM, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 12-12-10. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998112600682 19981126 00682 WP 1998 11 26 TWAA9818805 1 19981122 A 8012 7938007508 SENSE LINE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE NR 2 ENGINE RUPTURED A TWAA A UNSCHED LANDING O OTHER CL CLIMB 1 CE 05 EIBWD 49575 3230 THE RT ENGINE START VALVE OPEN LIGHT CAME ON AFTER CLIMB POWER SET. RETARDED THROTTLE AND LIGHT WENT OUT. RETURNED TO STL. FOUND START VALVE PRESSURE SENSE LINE HAD FAILED ALLOWING THE START VALVE TO OPEN. REPLACED LINE. ALSO REPLACED THE STARTER, START VALVE AND STARTER ADAPTER DUE TO SUBSEQUENT DAMAGE. CHECK-C 2-6-98 MCI. 2 L 7 2 4F 4 F RT A6WE E9NE 1998121100527 19981211 00527 NE 1998 12 11 98ZZZM928 2 19980922 A 7200 ENGINE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE NR 1 FAILED A A6WA A UNSCHED LANDING A X FLAME/FIRE ENGINE FLAMEOUT NR NOT REPORTED 1 GL 31 606AW E2033 NR 1 ENGINE FAIL/SAFE AND FIRE INFLIGHT. REMOVED AND REPLACED NR 1 ENGINE ASSY IAW BAE 146 MM AND AWAC GMM ENGINE CHANG E CHECKLIST VOLUME II SEC B CHAP 72. COMPLIED WITH ALL REQUIRED ENGINE GROUND RUNS. ALL PARAMETERS FOUND SATISFACTORY. (M) 2 H 7 4 4F 4 F RT A49EU E6NE 1998121800776 19981218 00776 SO 1998 12 18 SWIA971329 1 19981202 A 2613 WARNING EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE RIGHT ACTIVATED A SWIA A UNSCHED LANDING N FALSE WARNING TO TAKEOFF 1 NM 07 576SW 120345 RIGHT DUCT LEAK WARNING OCCURRED DURING TAKEOFF. RETURNED TO AIRPORT MEL 75-32-2. OPS CHECKS GOOD WITH NO DEFECTS NOTE D. 2 L 7 2 4T 4 T RT A31SO E20NE 1999010100114 19990101 00114 GL 1999 1 1 98ZZZX4753 2 19981015 A 7200 ENGINE SKRSKY S76 S76A 8143006 NE ALLSN 250C 250C30S 03013 GL NR 2 FAILED A HEEA O OTHER O OTHER NR NOT REPORTED 1 SW 03 911MJ 9982 1958 760231 CAE890522S IN-FLIGHT, NR 2 ENGINE OIL PRESSURE DROPPED WITH OIL PRESSURE LIGHT ILLUMINATION. PILOT SECURED ENGINE AND MADE UNEVENT FUL SINGLE ENGINE LANDING. MAINTENANCE FOUND 3 QUARTS OIL CONSUMPTION AFTER REPLENISHING OIL. SEVEN MINUTES INTO PENAL TY RUN, OIL CONSUMPTION WAS AGAIN 3 QUARTS. REMOVED ENGINE ASSEMBLY. 1 G 7 2 3U 3 U H1NE E1GL 1999012200288 19990122 00288 EA 1999 1 22 CA981125041 1 19980723 A 6510 613564003003 DRIVESHAFT CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE TAIL ROTOR FAILED W K NONE O OTHER IN INSP/MAINT 1 CA 1723 624 295059 (CAN) SEVERE HIGH FREQUENCY VIBRATION IN THE CABIN AT THE NR 3 TAIL ROTOR DRIVE SHAFT AREA. THIS SHAFT HAD BEEN STRAIGH TENED ON THE LAST REPAIR. 2 G 7 2 4U 4 U H8EA 1E3 1999012900933 19990129 00933 SW 1999 1 29 CA981125064 1 19981023 A 2740 2719008002 ACTUATOR BARBERCOL SWRNGN SA227 SA227AC 8780603 SW GARRTT TPE331 TPE33111U 01514 WP MCAULY 4HFR34 4HFR34C652 NE HORIZ STAB MALFUNCTIONED W K NONE O OTHER IN INSP/MAINT 1 CA 1755 119 P44205C 930243 (CAN) LINEAR ACTUATOR FAILED THE SERVICE LETTER 227-SL-031 3.C (22)-(25) BY 0.011 INCH. PART TC: 2,884. 2 L 7 2 4T 4 T RT A8SW E4WE 6 C 3PNE 1999021900414 19990219 00414 EA 1999 2 19 CA990111046 1 19981222 A 3231 VALVE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A 30015 NE NLG FAILED W C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 CA 6965 807335 (CAN) DURING GEAR RETRACTION, HYDRAULIC NR 3 PRESSURE WENT TO 3,5OO PSI. GEAR RETRACTED NORMAL, BUT CONSTANT KNOCKING O F NOSE GEAR DOORS. AFTER LOWERING GEAR, THE KNOCKING STOPPED. REPLACED THE NOSE LANDING GEAR DOOR SELECTOR VALVE. TOT AL CYCLES: 5,976. 2 L 7 2 4F 4 F RT A21EA E15NE 1999030500192 19990305 00192 NE 1999 3 5 CA990203016 2 19980617 A 7250 1358M73G30 BLADE AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE ENGINE DAMAGED W K NONE O OTHER IN INSP/MAINT 1 CA 20715 AMDE7624 731653 (CAN) ENGINE WAS INDUCTED IN THE SHOP FOR HIGH PRESSURE NOZZLE GUIDE VANE (NGV) BURNS. ON DISASSEMBLY OF ENGINE, TWO VA NES WERE FOUND TO HAVE THE COMPLETE LEADING EDGE BURNED AWAY. THE METAL LOSS EXTENDED TO THE MIDSPAN INTERNAL BULKHEAD OF THE VANE. THE PARTS WERE REMOVED FROM SERVICE. PART TC: 9,411. 2 L 7 2 4F 4 F RT A28NM E29NE 1999031200243 19990312 00243 NE 1999 3 12 CA980707005 2 19980606 A 7230 230367601 BEARING 211007043 LYC ALF502 ALF502R5 41580 NE NR 1 ENGINE WORN W K NONE O OTHER IN INSP/MAINT 1 CA 290 G318 LF95624A (CAN) NR 1 ENGINE CHIP DETECTOR FOUND METAL CONTAMINATED. TEAR-DOWN OF ENGINE FOUND NR 2 BEARING ROTATING IN THE DIFFUS ER HOUSING. PART TC: 257. 4 F E6NE 1999031901052 19990319 01052 NE 1999 3 19 ARWA981219 2 19981223 A 7210 777550 GEAR BOX DOUG DC8 DC862 3021970 WP PWA JT3D JT3D7 52039 NE NR 4 ENGINE LEAKING A ARWA E ENGINE SHUTDOWN J WARNING INDICATION CL CLIMB 1 SO 19 8968U 931179 46069 MIA - FLT 941 - DURING CLIMB, FL 210, NR 4 ENGINE OIL PRESSURE DROPPED TO 35 PSI, PULLED POWER LEVEL BACK TO A LOWER POW ER SETTING AND PRESSURE DROPPED TO 30 PSI OIL PRESSURE, LIGHT ILLUMINATED PULLED POWER LEVEL BACK TO IDLE, PRESSURE DROP PED DOWN TO 20 PSI OIL TEMP 120 DEGREES WITHIN LIMITS, OIL QTY NORMAL. ALL OTHER ENGINE PARAMETERS NORMAL. PERFORMED P RECAUTIONARY ENGINE SHUTDOWN ABNORMAL CHECKLIST N1, 18 PERCENT, N2 22 PERCENT, OIL PRESSURE 3 PSI WHILE ENGINE WINDMILLI NG . REMOVED AND REPLACED NR 4 ENGINE GEAR BOX ASSY IAW PWA MM JT3D-7 72-00 OPG 458 AND DC8 MM 70:30-5 AND 70-30-56 WOR K C/W BY IAL PERSONNEL, GEAR BOX INSTALLATION SEE C/C NO 81379 NR 1 OPS AND LEAK CHECK ALL ACCESSORIES COMPONENTS ATTACH 2 L 7 4 4F 4 F 4A25 1E8 1999032600128 19990326 00128 NM 1999 3 26 CA980713017 1 19980630 A 3230 82970010161 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE MLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120581 (CAN) HYDRAULIC LEAK FROM NR 1 NACELLE, NR 2 HYDRAULIC SYSTEM. LEAK FOUND ON NR 2 SYSTEM MLG UP PRESSURE LINE ASSY NEAR STA XN207.00. 2 H 7 2 4T 4 T RT A13NM E20NE 1999040200180 19990402 00180 GL 1999 4 2 CA990310067 2 19980409 A 7260 GEARBOX ALLSN 501D 501D22 03005 GL NR 2 ENGINE LEAKING W E A ENGINE SHUTDOWN UNSCHED LANDING K FLUID LOSS CL CLIMB 1 CA (CAN) DURING CLIMB THROUGH FL 170, NR 2 ENGINE GEARBOX LIGHT FLICKERED. OIL PRESSURE WAS STILL IN THE GREEN AND THE POW ER SECTION OIL PRESSURE WAS NORMAL. OIL QUANTITY INDICATION DROPPED RAPIDLY AND THE OIL PRESSURE LIGHT STARTED TO FLICK ER. THE ENGINE WAS SHUTDOWN AND THE AIRCRAFT DIVERTED. 4 T E282 1999043000048 19990430 00048 NE 1999 4 30 99ZZZX1687 2 19981203 A 7250 414129001 PT ROTOR BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE TURBINE DAMAGED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 10UM 3141 SC20389 7231 LE45752EFA FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TC: 6,993.8 . 1 G 7 2 3U 3 U H13EU E5NE10 2000020500939 20000205 00939 GL 2000 2 5 2000ZZZX271 2 19981106 A 7200 ENGINE BOLKMS 105 BO105S 5626006 EU ALLSN 250C 250C20B 03013 GL NR 2 MALFUNCTIONED A A RMXA K NONE O OTHER IN INSP/MAINT 1 SW 05 105NG S632 835935 AFTER ARRIVAL AT AIRPORT, GROUND RAN THE AIRCRAFT. NR 2 ENGINE COULD ONLY OBTAIN 68 PERCENT N2 SPEED WITH THROTTLE IN T HE FLY POSITION. SHUT DOWN ENGINE, PERFORMED STATIC LEAK CHECK ON NR 2 ENGINE WITH NO LEAKS NOTED. SUBMITTER RECOMMEND ED GOVERNOR CHANGE. 1 G 7 2 3U 3 U H3EU E4CE 2001032200078 20010322 00078 2001 3 22 CA980317092 4 19980130 A 3424 40991 GYRO DHAV DHC6 DHC6300 2802606 EA PWA PT6 PT6A27 52043 EA TURN AND BANK OVERHEATED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 962 (CAN)PILOT REPORTED THAT TURN AND BANK GYRO WAS U/S DURING TAXI. IT HAD A STRONG BURNT SMELL COMING FROM IT. 1 H 7 2 3T 4 T RT A9EA E4EA 2001032200099 20010322 00099 SO 2001 3 22 CA980318020 2 19980217 A 7322 104894 CARBURETOR CESSNA 150 150J 2071820 CE CONT O200 O200A 17020 SO ENGINE DEFECTIVE W K NONE E R J VIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TX TAXI/GRND HDL 1 CA 2 (CAN) ENGINE HAD JUST OVERHAULED AND FOUND TO BE RUNNING ROUGH IN THE LOW RPM RANGE. DIFFICULTY FOUND IN ADJUSTING IDLE MIXTURE. AFTER REVIEWING FAA AD 98-01-06 DECISION TO REPLACE CARBURETOR WAS MADE. CARBURETOR REMOVED HAD THE ONE PIECE V ENTURI. 1 H 7 1 3O 3 O 3A19 E252 1999012900651 19990129 00651 EU 1999 1 29 QXEA9900068 1 19981209 A 5230 SKIN FOKKER F28 F28MK4000 4990810 EU CARGO DOOR CORRODED A QXEA K NONE O OTHER IN INSP/MAINT 1 NM 09 492US 11156 PDX - AFT CARGO DOOR INNER SKIN HAS CORROSION AROUND PARAMETER ON DOOR INTERIOR SIDE. REPAIRED IAW FOKKER SRM 51-10-4. 2 L 7 2 4F RT A20EU 1998031200676 19980312 00676 1998 3 12 HEEA0013230 4 19980304 A 2210 7660002113103 VERTICAL GYRO SKRSKY S76 S76A 8143006 NE AFCS MALFUNCTIONED E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 1546K 760082 VERT GURO CAUSES AFCS TO PORPOISE. 1 G 7 2 3U H1NE 1998012200522 19980122 00522 EU 1998 1 22 QXEA9800027 1 19980114 A 3350 5515900004 CIRCUIT BOARD GRIMES 5515800106 FOKKER F28 F28MK4000 4990810 EU COCKPIT MALFUNCTION A QXEA K NONE L NO TEST IN INSP/MAINT 1 NM 09 484US 11234 AFT OVERHEAD EMERGENCY LIGHT EXIT SIGN AT CENTER AISLE INOP. REPLACED CIRCUIT BOARD, OPERATIONAL CHECK GOOD. 2 L 7 2 4F RT A20EU 1999010100514 19990101 00514 EU 1999 1 1 USAAF98093 1 19981130 A 3260 BULB FOKKER F28 F28MK0100 4990807 EU LANDING GEAR FAILED A USAA O OTHER P NO WARNING INDICATION AP APPROACH 1 EA 19 897US 11392 CRW - FLT 435 - ON APPROACH TO CRW WHEN LANDING GEAR WAS SELECTED DOWN, THERE WAS NO GEAR DOWN AND SAFE INDICATION. CRE W RECYCLED LANDING GEAR BUT THERE WAS STILL NO GEAR SAFE INDICATION. PROBLEM APPEARED TO BE AN INDICATION PROBLEM. CAP TAIN DID NOT DECLARE AN EMERGENCY AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REINSTALLED THE BULBS IN THE LANDING GEAR POSITION MODULE. (M) 2 L 7 2 4F RT 1998092500017 19980925 00017 SO 1998 9 25 C2XA98IA346 1 19980903 A 3233 1959510006 ACTUATOR EMB 120 EMB120RT SO LT MLG WORN A C2XA K NONE O OTHER NR NOT REPORTED 1 SW 09 16719 120138 IAH - DURING FLIGHT 3778, CREW REPORTED THE LEFT HAND MAIN LANDING GEAR WAS SLOW TO RETRACT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR, AND THE AIRCRAFT W AS APPROVED FOR RETURN TO SERVICE. (X) 2 L 7 2 4T RT A31SO 1998043000616 19980430 00616 EU 1998 4 30 AWXA9800070 1 19980225 A 3232 BOLT AIRBUS 320 A320231 3930325 EU GEAR DOOR ACT MISSING A AWXA A B UNSCHED LANDING EMER. DESCENT J WARNING INDICATION CL CLIMB 1 WP 28 636AW 098 AFTER GEAR RETRACTION, UNUSUAL NOISE HEARD, ECAM DISPLAYED LANDING GEAR DOOR UNLOCKED, LGCIU 1 AND 2 FAIL. GRAVITY EXTE NDED GEAR SUCCESFULLY, UNEVENTFUL LANDING KLAS. EMERGENCY WAS DECLARED. REPLACED MISSING ACTUATOR BOLT AND WASHER PER AMM 32-31-16. DOOR OPS CHECK GOOD. 2 L 7 2 4F RT A28NM 1998090400180 19980904 00180 EU 1998 9 4 98ZZZX3101 1 19980325 A 7120 1176270101 SUPPORT 1733 BOLKMS 117 BK117A1 5626010 EU ENGINE MOUNT MISMANUFACTURED A R7MA K NONE W INADEQUATE Q C IN INSP/MAINT 1 NM 11 128HH 7036 ENGINE MOUNT SUPPORT REJECTED, NEW OUT-OF-BOX. FAILED DIMENSIONAL CHECK. AREA NR 2 EXCEEDS LIMITS AT 13.98 MM. REPLAC ED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U H13EU 1998061200301 19980612 00301 EU 1998 6 12 98ZZZX2064 1 19980212 A 5320 S5367800821602 SUPPORT AEROSP ATR72 ATR72212 EU CARGO COMPT CORRODED A ASOA K NONE O OTHER IN INSP/MAINT 1 SO 11 636AS 375 SAW - DURING C-CHECK INSPECTION, MAINTENANCE REPORTED AFT CARGO RT Z-MEMBER CORRODED. REPLACED RT Z-MEMBER IAW ATR72 SR M 51-25-01. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T RT A53EU 1998091800391 19980918 00391 CE 1998 9 18 98ZZZX3327 1 19980818 A 2612 LEAD LEAR 25 25 5170506 CE RT ENGINE FAILED A KKFA E ENGINE SHUTDOWN O OTHER AP APPROACH 1 GL 23 222B 047 WHILE ON APPROACH TO KNOXVILLE, THE RT FIRE LIGHT ILLUMINATED. A PRECAUTIONARY ENGINE SHUT DOWN WAS MADE FOLLOWED BY AN UNEVENTFUL LANDING. INVESTIGATION FOUND A DEFECTIVE CONNECTION ON THE FIRE DETECTION LEAD CAUSING A FALSE FIRE INDICAT ION. INSTALLATION WAS CORRECTED AND SYSTEM TESTED NORMALLY. 2 L 7 2 4J A10CE 1998052200787 19980522 00787 NM 1998 5 22 AALA980741 1 19980408 A 2613 30231R17 DETECTOR KIDDE DOUG MD11 MD11 3023602 NM AFT CARGO DEFECTIVE A AALA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 SW 07 1755 48490 EZE - FLT 0900 - DURING CLIMB-OUT, FLIGHT CREW GOT TRI-TONE ANNUNCIATOR ALONG WITH AN AFT CARGO FIRE LIGHT ILLUMINATED. CREW FOLLOWED ALTERNATE PROCEDURES CHECKLIST AND LANDED WITHOUT INCIDENT EZE. REPLACED AFT CARGO HEAT DETECTORS. SYST EM GROUND CHECKED, NORMAL OPERATION. (X) 2 L 7 3 4F RT A22WE 1998112600295 19981126 00295 SW 1998 11 26 98ZZZX4358 1 19981103 A 6310 SEAL 40604050013 BELL 206 206L4 1182110 SW FREEWHEEL UNIT FAILED A A VMIA A UNSCHED LANDING J WARNING INDICATION NR NOT REPORTED 1 NM 03 2064S 1504 A1440 52002 ON PART 135 FLIGHT, PILOT NOTICED HIGH ENGINE OIL PRESURE AND FLICKERING TRANS OIL PRESS LOW LIGHT. AFTER REDUCING POWE R, LIGHTS WENT OUT. PILOT CONTINUED FLIGHT FOR 10 MINUTES WHEN TRANS OIL PRESS LIGHT CAME ON STEADY. PILOT MADE PRECAU TIONARY LANDING AND THEN FOUND NO OIL VISIBLE IN TRANS OIL SIGHT GLASS, AND ENGINE OIL LEVEL HIGH. PILOT CALLED MAINT A ND MECH FLEW TO ACFT. MECH DETERMINED A FREEWHEELING UNIT SEAL FAILED ALLOWING TRANSMISSION OIL TO TRANSFER FROM TRANSM ISSION TO THE ENGINE. MECH DRAINED OIL FROM ENGINE AND RE-SERVICED BOTH ENGINE AND TRANSMISSION. ACFT WAS FLOWN TO BAS E WITHOUT FURTHER INCIDENT. UPON TEAR-DOWN INSPECTION, AFT FREEWHEELING UNIT SEAL WAS FOUND UNSERVICEABLE AND REPLACED. 1 G 7 1 3U NC H2SW 1998021100057 19980211 00057 EA 1998 2 11 98ZZZX534 2 19980113 A 7320 3008787 ROD END BEECH 99 99A 1154003 CE PWA PT6 PT6A27 52043 EA CAM BOX TO FCU DEFECTIVE A A KCQA O OTHER O OTHER NR NOT REPORTED 1 GL 13 499CZ U81 PCE40501 ENGINE POWER WOULD NOT DECREASE DUE TO TIGHT ROD END CONNECTOR FROM CAM BOX TO FCU DEFECTIVE. TAT: 30,824 HOURS. ENGI NE TSN: 4,295 HOURS. ENGINE TSO: 1,129 HOURS. 1 L 7 2 3T 4 T A14CE E4EA 1998030500578 19980305 00578 NE 1998 3 5 9803411147 2 19980224 A 7200 ENGINE DOUG DC10 DC1040 3023508 WP PWA JT9 JT9D20J 52054 NE NR 1 FAILED A NWAA E ENGINE SHUTDOWN O OTHER LD LANDING 1 GL 01 147US 46756 686141 DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. THE AIRPORT TOWER REPORTED SMOKE FR OM THE TAILPIPE OF THE NR 1 ENGINE. THE ENGINE WAS SHUT DOWN USING THE EMERGENCY COM PROCEDURE, EGT DID NOT EXCEED 700C . MAINTENANCE INSPECTED THE ENGINE AND FOUND OIL IN THE TAILPIPE. THE AIRCRAFT WAS FERRIED TO MSP WERE THE ENGINE WAS CHANGED. EXACT PART CAUSING DIFFICULTY TO BE DETERMINED. 2 L 7 3 4F 4 F A22WE E20EA 1998031200639 19980312 00639 GL 1998 3 12 HEEA0013187 2 19980304 A 7314 3881005 FUEL PUMP BELL 206 206L3 1182108 SW ALLSN 250C 250C30P 03013 GL ENG FUEL WORN E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 31077 6031 51520 FUEL PUMP DRIVE SHAFT, SHOW SIGNS OF STEP WEAR ON SPLINES. 1 G 7 1 3U 3 U H2SW E1GL 1998032600575 19980326 00575 NE 1998 3 26 9804876718 2 19980322 A 7230 COMPRESSOR BOEING 747 747251F 1384898 NM PWA JT9 JT9D7F 52054 NE NR 1 ENGINE STALLED A NWAA E ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 GL 01 618US 21122 689565 WHILE AT CRUISE FL350, THE NR 1 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN AFTER REACHING AN EGT OF 1002C FOR 5 SECONDS. NO RESTART WAS ATTEMPTED. THE FLIGHT CONTINUED TO KIX WITHOUT FURTHER DIFFICULTY. THE AIRCRAFT WAS REMOVED FROM SERVICE AND THE NR 1 ENGINE WAS REPLACED AFTER ARRIVING IN KIX. 2 L 7 4 4F 4 F A20WE E20EA 1998040200667 19980402 00667 NE 1998 4 2 9805229981 2 19980329 A 7200 ENGINE DOUG DC9 DC931 3022065 WP PWA JT8 JT8D9 52048 NE LEFT FAILED A NWAA A UNSCHED LANDING X ENGINE FLAMEOUT CL CLIMB 1 GL 01 994Z 479097 666940 DURING CLIMB AT 8,000 FEET, THE LEFT ENGINE FLAMED OUT. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT FURTHER INCIDENT. M AINTENANCE REPLACED THE LEFT ENGINE, OPERATIONAL CHECK OK. 2 L 7 2 4F 4 F A6WE E2EA 1998040800016 19980408 00016 NM 1998 4 8 98UAL900079 1 19980221 A 3233 273N20043 ACTUATOR BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE LANDING GEAR FAILED A UALA O OTHER J WARNING INDICATION TO TAKEOFF 1 WP 29 549UA 25397 ON TAKEOFF CREW HAD TO USE OVERRIDE TO RAISE GEAR. *S/D* BLOWN PISTON SEAL IN TRUCK POSITION ACTUATOR. REPLACED ACTUA TOR. 2 L 7 2 4F 4 F RT A2NM E17NE 1998040800022 19980408 00022 NE 1998 4 8 98UAL900086 2 19980222 A 7261 OIL PUMP BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 3 ENGINE FAILED A UALA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 7452U 6012 21906 NR 3 ENGINE OIL QUANTITY LOSS WITH PRESSURE FLUCTUATION AND TEMPERATURE RISING. SECURED ENGINE. *S/D* THERE WAS EXCE SSIVE OIL DRAIN BACK INTO THE GEARBOX CAUSING HIGH BREATHER PRESSURE AND OIL LOSS OUT OF OVERBOARD BREATHER. ALSO, NR 4 BEARING PRESSURE AND SCAVENGE LINE LEAKING INTO PCP PLENUM. INITIATED REPAIR TO OIL PUMP LINER TO USE A NEW EPOXY. IN CREASED CLEARANCE SO SEALANT IS NOT SCRAPED OFF DURING INSTALLATION. 2 L 7 3 4F 4 F A3WE E2EA 1998041000104 19980410 00104 WP 1998 4 10 98UAL900122 1 19980324 A 3244 2034PR TIRE DOUG DC10 DC1010 3022110 WP GE CF6 CF66D 30020 GL LT MLG FAILED A UALA A UNSCHED LANDING O OTHER TO TAKEOFF 1 WP 29 1836U 470 47968 A LEFT MAIN GEAR TIRE BLEW ON TAKEOFF FROM DEN. DUMPED FUEL AND RETURNED TO DEN. AFTER NORMAL LANDING NR 1 ENGINE SHUT DOWN AND FIRE HANDLE PULLED. *S/D* NR 1 FORWARD MAIN LANDING GEAR TIRE WAS REPLACED. TASK ACCOMPLISHED TO CHECK THE B RAKE ACCUMULATORS, BLEED THE BRAKES SYSTEM, AND CHECK THE ANTI-SKID SYSTEM. OPS CK NORMAL. 2 L 7 3 4F 4 F A22WE E23EA 1998041700673 19980417 00673 GL 1998 4 17 CA971014007 2 19980324 A 7210 23035185 GEARBOX BELL 206 206L 1181522 SW ALLSN 250C 250C20 03013 GL STUDS SEPARATED W K NONE O OTHER IN INSP/MAINT 1 CA 6481 3355 CAE830637 (CAN) AFTER REMOVING CASEY HEATER SHROUD, THE 4.3125 INCH NUTS WERE REMOVED FROM TURBINE TO GEARBOX, LEAVING TOP .3750 I NCH NUT REMAINING. AFTER TAKING WEIGHT OF TURBINE, NOTED HOW LOOSE IT WAS. TURBINE WAS REMOVED BY HAND. THE SHROUD WIT H NUT WAS STILL IN THE TURBINE. THE HELICOIL HAD COME OUT OF THE GEARBOX. REPAIRED. TIME SINCE LAST REMOVAL 233 HRS. 1 G 7 1 3U 3 U H2SW E4CE 1998042900014 19980429 00014 SO 1998 4 29 SWIA971148 1 19980309 A 5210 BOLT EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE PAX DOOR LOOSE A SWIA K NONE O OTHER IN INSP/MAINT 1 NM 07 292SW 120319 CORROSION AND LOOSENESS IN LOWER ATTACH BOLT LOWER HALF FWD HANDRAIL SUPPORT ARM, CABIN DOOR. REPLACED HARDWARE IAW MM 52-10-00. 2 L 7 2 4T 4 T RT A31SO E20NE 1998050100747 19980501 00747 NE 1998 5 1 TWAA9805001 2 19980402 A 7530 500588801 STATOR VANE DOUG DC9 DC983 3022083 WP PWA JT8 JT8D217A 52053 NE RT ENGINE LIBERATED A TWAA A E UNSCHED LANDING ENGINE SHUTDOWN R PARTIAL RPM/PWR LOSS CR CRUISE 1 CE 05 9406W 4788 53126 3240 BNA - FLT 505 - AT FL 270, RT ENGINE PRODUCED TWO LARGE COMPRESSOR STALLS FOLLOWED BY PARTIAL LOSS OF ENGINE POWER. DIV ERTED TO BNA. ON APPROACH, EGT STARTED TO RISE AND ENGINE WAS SHUT DOWN. FOUND TURBINE FAILURE. REPLACED ENGINE. S/D : ON ENGINE TEAR DOWN, FOUND 8TH STAGE STATOR VANE HAD LIBERATED AND CAUSED SEVERE DAMAGE TO THE HIGH PRESSURE COMPRESS OR. THE PWA ENGINE MANUAL WAS REVISED TO REDUCE THE NUMBER OF STRAP WELDS ON 7C, 8C, AND 9C STATOR VANES. 2 L 7 2 4F 4 F RT A6WE E9NE 1998061200440 19980612 00440 NM 1998 6 12 98UAL900227 1 19980531 A 2560 SQUIB BOEING 767 767222 1385122 NM PWA JT9 JT9D7R4D 52054 NE LT EMER EXIT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 618UA 21878 NR 1 SQUIBB WILL NOT TEST FOR THE LEFT OVERWING EXIT. 2 L 7 2 4F 4 F RT A1NM E3NE 1998070300424 19980703 00424 NM 1998 7 3 VNAA9806014 1 19980624 A 3244 TIRES DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT MLG FLAT A VNAA O OTHER O OTHER TX TAXI/GRND HDL 1 GL 07 429JS 35411 76 3043 DURING THE TAXI FOR TAKEOFF, BOTH LEFT HAND MAIN TIRES WENT FLAT. THE AIRCRAFT STOPPED AND DE-PLANED THE PASSENGERS. M AINTENANCE INSPECTED AND REPLACED THE LEFT HAND MAIN WHEELS AND TIRES, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32- 41-10. THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998071700267 19980717 00267 WP 1998 7 17 CKSA98500 1 19980621 A 2612 FIRE LOOP LKHEED 1011 1011385115 5265015 WP RROYCE RB211 RB211524B02 54555 NE NR 2 ENGINE OUT OF ADJUST A CKSA O OTHER N FALSE WARNING CL CLIMB 1 GL 23 104CK 193N1193 14504 DURING CLIMB, B FIRE LOOP LIGHT NR 2 ENGINE CAME ON STEADY. TEST SHOWED A LOOP OK. A FIRE LOOP SELECTED. AFTER ABOUT 2 MIN, A FIRE LOOP CAME ON. SELECTED BOTH, AND A AND B, LOOP LIGHT BOTH CAME ON. FOUND A AND B SENSOR TOUCHING ENGINE CASE AT 6:00 POS. REPOSITIONED GROUND RAN ENGINE FOR 2 MIN AT T/O POWER. NO DEFECTS NOTED IAW 72-00-00. 2 L 7 3 4F 4 F A23WE E12EU 1998072400574 19980724 00574 NE 1998 7 24 98ZZZX2425 2 19980521 A 7260 4068T97P02 RUNNER SAAB SF340 SF340A 7850100 EU GE CT7TP CT75A 30030 NE LT ENGINE FAILED A REXA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION DE DESCENT 1 SO 25 402BH 340A058 LEFT ENGINE LOST OIL PRESSURE. REMOVED AND REPLACED LEFT BB AXIS SEAL AND RUNNER. REF: OPERATOR CONTROL NR REXA98096. 2 L 7 2 4T 4 T RT A52EU E8NE 1998072400641 19980724 00641 SO 1998 7 24 SWIA971216 1 19980709 A 2751 ANNUNCIATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAP MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CR CRUISE 1 NM 07 565SW 120340 AT CRUISE, FLAP AND ADVANCED SWS MAP LIGHT ILLUMINATED WITH CONTROL FAULT LIGHT ON FLAP PANEL. UNABLE TO RESET. RETURN ED TO LAX. REPLACED FLAP ANNUNICATOR, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998073100098 19980731 00098 NM 1998 7 31 98UAL900318 1 19980710 A 3610 DUCT AIRESEARCH 2075621MOD BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 2 ENGINE LEAKING A UALA A E UNSCHED LANDING ENGINE SHUTDOWN J M B WARNING INDICATION OVER TEMP SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 WP 29 7447U 21901 LOWER AFT BODY OVERHEAT WARNING WITH AN ELECTRICAL ODOR IN CABIN AND COCKPIT. ALSO, NR 2 ENGINE OIL TEMP REDLINE, CABIN EXCESSIVE TEMP. INFLIGHT SHUT DOWN OF NR 2 ENGINE. TEMP AND ELECTRICAL ODOR SUBSIDED. DIVERTED TO AKO. *S/D* FOUND LEAKING FLEX TUBE THAT CAUSED THE BODY OVERHEAT LIGHT. SMELL MAY HAVE BEEN CAUSED BY THE COOLING FAN THAT WAS RUNNING BACKWARD. REPLACED LEAKING FLEX TUBE ASSEMBLY, COOLING FAN AND 13TH STAGE MODULATING VALVE. 2 L 7 3 4F 4 F A3WE E2EA 1998080700055 19980807 00055 EA 1998 8 7 COMA9860198 1 19980721 A 3242 50108801 PAD 50105201 CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE MLG FAILED A COMA D RETURN TO BLOCK O OTHER IN INSP/MAINT 1 SO 01 936CA 297 297 MAR950429 7043 A WEAR PAD P/N 5010880-1 OF THE NUMBER ONE STATIONARY DISK SEPARATED FROM THE BRAKE. THE ANTI-ROTATION TAB OF THE PAD M AY HAVE FAILED. INSPECTION OF THE REST OF THE BRAKE FOUND NO OTHER DEFECTS. REMAINING PIECES OF THE WEAR PAD WERE SENT TO AIRCRAFT BRAKING SYSTEMS OF FURTHER EVALUATION. 2 L 7 2 4F 4 F RT A21EA E15NE 1998080700102 19980807 00102 EU 1998 8 7 CA980407010 1 19980209 A 7921 OIL COOLER BRAERO 748 HS7482A 4231001 EU RROYCE DART DART5342 EU NR 2 ENGINE LEAKING W E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION IN INSP/MAINT 1 CA 7345 (CAN) ON ENGINE START-UP, NR 2 ENGINE LOST OIL PRESSURE. ENGINE WAS SHUTDOWN. THE OIL COOLER WAS FOUND LEAKING, POSSIB LY DUE TO INADEQUATE PRE-HEAT OF THE OIL COOLER CORE. OIL COOLER WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 2 L 7 2 3T 4 T A24EU A196 1998082800257 19980828 00257 NM 1998 8 28 CA980519025 1 19980508 A 3242 214664 HOUSING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BRAKE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 25280 120251 (CAN) DURING NDT INSPECTION, CRACKS WERE FOUND IN TWO OF THE BRAKE HOUSING TIE BOLT HOLES. UNIT SCRAPPED. PART TC: 29 ,042. 2 H 7 2 4T 4 T RT A13NM E20NE 1998091801441 19980918 01441 NM 1998 9 18 98UAL900446 1 19980904 A 3350 6012541LB BATTERY BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE CABIN DISCHARGED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 7456U 21910 LEFT OVERWING FORWARD EMERGENCY LIGHT IS ILLUMINATED WHEN THE POWER IS OFF. *S/D* BATTERY CHARGE WAS FOUND TO BE LOW. BATTERY PACK WAS REPLACED AND CHECKED FOR PROPER OPERATION. 2 L 7 3 4F 4 F A3WE E2EA 1998101600158 19981016 00158 NE 1998 10 16 98ZZZX3731 2 19980330 A 7230 430404701 SEAL BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE ENGINE LEAKING A R7MA K NONE K FLUID LOSS IN INSP/MAINT 1 NM 11 5194C 522 6J043 7169 LE45514EF SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. SERIAL NUMBER ON HOUSING IS H7949. ELEMENTS SWAPPED AT ORIGINAL INSTALL. 1 G 7 2 3U 3 U H13EU E5NE10 1998103000278 19981030 00278 SO 1998 10 30 SWIA971291 1 19981016 A 2750 SELECTOR EMB 120 EMB120RT SO PWA 118 PW118 NE TE FLAPS FAILED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 1117H 120117 FLAP WOULD NOT EXTEND. MADE A FLAPS UP LANDING. REPLACED FLAP SELECTOR HANDLE, OPS CHECK GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998110600695 19981106 00695 SO 1998 11 6 SWIA971297 1 19981027 A 2751 3471001001 ANNUNICATOR EMB 120 EMB120ER 3260203 SO PWA PW118 PW118B NE TE FLAPS MALFUNCTIONED A SWIA A UNSCHED LANDING N FALSE WARNING CL CLIMB 1 NM 07 308SW 120326 DISAGREEMENT INDICATION WITH FLAPS UP FROM 15 DEGREES. RETURNED TO FIELD. REPLACED ANNUNICATOR UNIT IAW MM 27-50-05, O PS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998120400038 19981204 00038 NE 1998 12 4 CA980629024 2 19980617 A 7250 1358M73G30 BLADE AIRBUS 320 A320211 3930320 EU GE CFM56 CFM565A 13802 NE ENGINE BURNED W K NONE O OTHER IN INSP/MAINT 1 CA 731653 (CAN) DURING ENGINE DISASSEMBLY IN THE SHOP FOR BURN HP NGV, TWO VANES WERE FOUND TO HAVE THE COMPLETE LEADING EDGE BURN ED AWAY. THE METAL LOSS EXTENDED TO THE MIDSPAN INTERNAL BULKHEAD OF THE VANE. FURTHER EVALUATION BEING CARRIED OUT. 2 L 7 2 4F 4 F RT A28NM E29NE 1998120400062 19981204 00062 NE 1998 12 4 CA980916002 2 19980816 A 7200 ENGINE DHAV DHC8 DHC8311 1386006 EA PWA PW120 PW123 NE NR 2 NACELLE MALFUNCTIONED W O OTHER B SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA 11225 1819 PCE123146 (CAN) AFTER ENGINE START, WHEN NR 2 BLEED AIR WAS TURNED ON, THE CABIN FILLED WITH SMOKE. THE NR 2 ENGINE WAS REPLACED. PART TC: 17,270. 2 H 7 2 4T 4 T RT A13NM E20NE 1998121100583 19981211 00583 NM 1998 12 11 98UAL900570 1 19981126 A 2530 3741 CHILLER BOEING 737 737291 138448W NM PWA JT8 JT8D9A 52048 NE GALLEY FAILED A UALA K NONE B SMOKE/FUMES/ODORS/SPARKS NR NOT REPORTED 1 WP 29 983UA 21641 ELECTRIC SMOKE SMELL IN GALLEY AREA. *S/D* NO INLET FILTER ON CHILLER. REPLACED BAD CHILLER WITH SERVICEABLE CHILLER PER MM 25-33-01, OPERATIONAL CHECK NORMAL. 2 L 7 2 4F 4 F A16WE E2EA 1998121800376 19981218 00376 WP 1998 12 18 CA981001010 1 19980828 A 2140 APU DOUG DC9 DC932 3022066 WP PWA JT8 JT8D7A 52053 NE APU BAY LEAKING W O OTHER K B FLUID LOSS SMOKE/FUMES/ODORS/SPARKS TX TAXI/GRND HDL 1 CA P657261D (CAN) ON ENGINE START, OIL SMELL REPORTED, AFT CABIN SMOKE ALARM CAME ON. AIR CYCLE MACHINE OIL LEVEL FOUND LOW. LEFT AIR CYCLE MACHINE AND APU REPLACED, SYSTEM SERVICEABLE. 2 L 7 2 4F 4 F A6WE E2EA 1998121800408 19981218 00408 EU 1998 12 18 CA981007009 1 19980918 A 5320 350A23102835 STIFFENER 2300000101 SNIAS 350 AS350B 8680801 EU TMECA ARRIEL ARRIEL1B 6OO30 NE FUSELAGE CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA TB1558 786 (CAN) AFTER TAILBOOM REMOVAL, RT FRONT STIFFENER CRACKED WHERE NR 5 BEARING SUPPORT ATTACHES. 1 G 7 1 3U 3 U H9EU E19EU 1998121800464 19981218 00464 1998 12 18 CA981022011 4 19981004 A 8300 208315905 RING BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE ACCESSORY G/B LOOSE W K NONE O OTHER IN INSP/MAINT 1 CA LF05740A (CAN) ON INSPECTION, THE CONSTANT SPEED DRIVE (CSD) RING WAS FOUND SEPARATED FROM THE ACCESSORY GEARBOX DUE TO THE ELONG ATION OF THE BOLT ATTACHMENT HOLES. 2 H 7 4 4F 4 F RT A49EU E6NE 1999010100101 19990101 00101 NE 1999 1 1 98ZZZX4740 2 19981027 A 7200 3017600 ENGINE BELL 412 412 1182202 SW PWA PT6T PT6T3B 52045 NE NR 1 FAILED A HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 3911L 9089 1090 33023 CPPS61439 ON 10-27-98 ON FINAL TO PHI NEW ORLEANS, ENGINE STALLED. RUN-ON LANDING WAS ACCOMPLISHED. TROUBLESHOOTING IN PROGRESS. 1 G 7 2 4U 4 U H4SW E22EA 1999010800009 19990108 00009 NE 1999 1 8 MALA976269 2 19981218 A 7200 ENGINE BAC 146 AVRO146RJ85A 1500097 EU LYC ALF502 ALF502R3 41580 NE NR 4 FAILED A MALA E ENGINE SHUTDOWN Y ENGINE STOPPAGE CL CLIMB 1 GL 15 507XJ E2316 ON CLIMBOUT AFTER FLAP RETRACTION, NR 4 ENG HAD LOUD BANG AND CEASED OPERATION. RETURNED TO DTW. MAINTENANCE REPLACED NR 4 ENG. ALL RUNS AND LEAK CHECKS GOOD. 2 H 7 4 4F 4 F RT A49EU E6NE 1999021200159 19990212 00159 SW 1999 2 12 CA980713004 1 19980624 A 7714 206062627003 SHAFT BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TACH GENERATOR SHEARED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 7120 CAE822384 (CAN) AFTER TAKEOFF, THE N2 GAS PRODUCER INDICATOR WENT TO ZERO AND ENGINE OUT LIGHT AND WARNING HORN ACTIVATED. THE TO T AND N2 ENGINE INDICATOR AND ROTOR TACHOMETER INDICATOR APPEARED NORMAL. AIRCRAFT LANDED OK. FOUND TACHOMETER GENERAT OR SHAFT SHEARED. REPLACED. 1 G 7 1 3U 3 U H2SW E4CE 1999031200262 19990312 00262 EU 1999 3 12 CA980818006 1 19980703 A 3234 HTE210014 VALVE BAG BAE146 BAE146200A 1500266 EU LYC ALF502 ALF502R5 41580 NE MLG FAILED W A UNSCHED LANDING O OTHER CL CLIMB 1 CA 3885 1185GB324H LR05628A (CAN) LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF SELECTION. AIRCRAFT RETURNED. 2 H 7 4 4F 4 F RT A49EU E6NE 1999040200129 19990402 00129 NM 1999 4 2 CA981109030 1 19981028 A 3232 82910010175 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE NLG LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 22401 120329 (CAN) HYDRAULIC LEAK FOUND IN NOSE GEAR WHEELWELL. NOSE GEAR DOOR ACTUATOR CLOSE LINE FOUND LEAKING. LINE HAD A PIN HO LE CAUSED BY CORROSION. 2 H 7 2 4T 4 T RT A13NM E20NE 1998091800400 19980918 00400 CE 1998 9 18 98ZZZX3336 1 19980826 A 2750 991434411 FLEXSHAFT CESSNA 750 750 2076810 CE TE FLAPS BROKEN A DXTA O OTHER J WARNING INDICATION NR NOT REPORTED 1 GL 07 934QS 782 570052 7500034 FLAPS FAILED DURING EXTENSION. SLATS EXTENDED. FLAPS MOVED ABOUT .50 INCH, BOTH FLAPS FAIL CAS MESSAGE. FOUND BROKEN RIGHT HAND INBOARD FLEXSHAFT. 2 L 7 2 4J RT T00007WI 1998050800473 19980508 00473 WP 1998 5 8 ABXA9800410 1 19980329 A 5712 5769470 RIB DOUG DOUG DC8 DC862 3021970 WP WS 741.25 CRACKED A ABXA K NONE O OTHER IN INSP/MAINT 1 GL 23 801AX 46077 RIGHT WING LEADING EDGE RIB AT STATION XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW ABX DWG K05056. 2 L 7 4 4F 4A25 1998071700488 19980717 00488 NM 1998 7 17 CALA9801234 1 19980711 A 3234 GEAR HANDLE BOEING 727 727243 138408D NM COCKPIT LACK OF LUBE A CALA O OTHER J WARNING INDICATION AP APPROACH 1 SW 09 17402 21265 WHEN GEAR WAS EXTENDED ON APPROACH, CREW RECEIVED THREE GREEN AND THREE RED GEAR INDICATION LIGHTS. THE GEAR WAS CYCLED AND CREW GOT THREE GREEN. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LANDING GEAR HANDLE STICKING WH EN PULLED OUT. THE GEAR HANDLE WAS LUBRICATED AND CHECKED SEVERAL TIMES WHILE ON GROUND. THE GROUND CHECKS WERE GOOD W ITH NO STICKING NOTED AND GEAR WARNING LIGHTS ALL CHECKED GOOD. 2 L 7 3 4F RT A3WE 1998120400164 19981204 00164 SO 1998 12 4 CA980930008 1 19980623 A 3297 487862 WIRE PIPER PA31 PA31350 7103110 SO WOW SWITCH BROKEN W D RETURN TO BLOCK O OTHER CL CLIMB 1 CA (CAN) GEAR WOULD NOT RETRACT ON DEPARTURE. LEFT SQUAT SWITCH WIRE BROKEN AT THE SWITCH. 1 L 7 2 3O A20SO 1999010100179 19990101 00179 NM 1999 1 1 DL72L982617 1 19981216 A 5753 65192709 TRACK BOEING 727 727232 1384082 NM TE FLAP CORRODED A DALA K NONE O OTHER IN INSP/MAINT 1 SO 27 504DA 21306 INB'D FLAP INB'D TRACK, CORROSION AT MLG BEAM ATTACH PAD AND HOLES: AD 90-07-05 AND 90-06-09. THE SPOT-FACE DEPTH FOR T HE MLG BEAM ATTACH HOLE HAS BEEN INCREASED TO REMOVE CORROSION. AUTHORIZED INCREASE DAMAGE REMOVAL WITHOUT ANY RE-INFOR CING REPAIR. 2 L 7 3 4F A3WE 1998073100170 19980731 00170 NM 1998 7 31 SWAA981373 1 19980714 A 5312 BULKHEAD BOEING 737 7372H4 138448C NM CABIN DAMAGED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 081SW 22730 DURING SCHEDULED C4 CHECK, FOUND RT BULKHEAD (CENTER) TORN UNDER MAGAZINE POUCH. REPAIRED PER BOEING MM. 2 L 7 2 4F A16WE 1998061900678 19980619 00678 EU 1998 6 19 AALA980911 1 19980505 A 5320 SUPPORT AIRBUS 300 A300B4605R 3930308 EU FRAME 14-15 CORRODED A AALA K NONE O OTHER IN INSP/MAINT 1 SW 07 14065 508 TUL - FOUND CORROSION ON FLOOR SUPPORT AT R1 DOOR. REMOVED AND REPLACED UPPER T-ANGLE PER SRM 51-72-10-0. (M) 2 L 7 2 4F RT A35EU 1998061200051 19980612 00051 NM 1998 6 12 CALA9800951 1 19980603 A 5315 FLOORBEAM BOEING 737 7373T0 1384582 NM BS 1016 CORRODED A CALA K NONE O OTHER IN INSP/MAINT 1 SW 09 14342 23580 INSPECTION FOUND CORROSION AT FASTENER HOLES OF AFT LAV LT FLOORBEAM AT STA 1016 FROM CENTERLINE TO LBL 36. THE CORRODE D AREA WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-51. 2 L 7 2 4F RT A16WE 1998082100372 19980821 00372 1998 8 21 98UAL900384 4 19980805 A 2564 24D3006291 TUBE AIR CRUISERS DOUG DC10 DC10* WP SLIDE RAFT FAILED A UALA K NONE L NO TEST IN INSP/MAINT 1 WP 29 51294 SLIDE/RAFT HAD A SEAM FAILURE ON THE LOWER TUBE AFTER FLAT FIRE TEST DURING UNIT OVERHAUL. SCRAPPED UNIT. 2 L 7 3 4F A22WE 1998052200651 19980522 00651 NM 1998 5 22 98FDEA00353 1 19980517 A 3230 RETRACT MECH BOEING 727 7272S2F 1384O81 NM LT MLG OUT OF ADJUST A FDEA O OTHER J WARNING INDICATION CL CLIMB 1 SO 25 207FE 22929 L/MAIN GEAR LIGHT ILLUM'D ON BOTH FWD PANEL AND S/O PANEL DURING EACH GEAR HANDLE PLACED IN THE UP POS ON FOR 30 SECS. F OUND GEAR RLS MECHANISM OUT OF ADJ, ADJUSTED AND TESTED PER 32-34-21. NO GEAR SWING REQ BY MM. 2 L 7 3 4F A3WE 1998040200898 19980402 00898 NM 1998 4 2 ASAA9810017 1 19980222 A 3350 86210151 BATTERY BOEING 737 737210C 1384459 NM CABIN DISCHARGED A ASAA K NONE L NO TEST IN INSP/MAINT 1 NM 01 744AS 21822 SEA - DURING MAINTENANCE CHECK, THE FORWARD SEAT PALLET EMERGENCY EXIT FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. REPLACED BATTERY AND LIGHTS OPERATED NORMALLY. (M) 2 L 7 2 4F A16WE 1998073100614 19980731 00614 NM 1998 7 31 98ZZZX2518 1 19980626 A 3211 65B1046233 FITTING BOEING 747 747273C 1384896 NM LT MLG CORRODED A EIAA K NONE O OTHER IN INSP/MAINT 1 NM 09 CORROSION BLEND-OUT/RE-WORK ON TRUNNION SUPPORT FITTINGS - LT OTBD TRUNNION CAP FITTING 65B1046233. REF: OPERATOR CO NTROL NR 98ZZZX2817 THROUGH 98ZZZX2520. 2 L 7 4 4F A20WE 1998111301188 19981113 01188 NM 1998 11 13 UPS98228123 1 19981106 A 3350 BATTERY PACK BOEING 727 72725C 138400H NM PAX DOOR DISCHARGED A IPXA K NONE L NO TEST IN INSP/MAINT 1 SO 01 951UP 19850 INSPECTION TYPE-N/A, EMER LIGHT AT FWD ENTRY DOOR LOWER FWD INOP. REMOVED AND REPLACED BATT PACK, CKS GOOD. 2 L 7 3 4F A3WE 1999072300291 19990723 00291 EU 1999 7 23 99ZZZX2685 1 19980820 A 5753 BEARING BAG BAE146 BAE146200A 1500266 EU TE FLAP TAB WORN A A6WA K NONE O OTHER IN INSP/MAINT 1 GL 31 610AW E2082 RIGHT WING INNER FLAP TAB NR 1 HINGE BEARING IS WORN. REMOVED AND REPLACED RIGHT NR 1 FLAP TAB HINGE BEARING. 2 H 7 4 4F RT A49EU 1998021900697 19980219 00697 EA 1998 2 19 SWIA971080 1 19980209 A 2751 FAIL MESSAGE CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS ILLUMINATED A SWIA O OTHER N FALSE WARNING CL CLIMB 1 NM 07 407SW 7034 WHEN BRINGING FLAPS FROM 5 DEGREES TO 0 DEGREES, FLAP FAIL MESSAGE APPEARED. RETURNED TO AIRPORT. POWERED DOWN AIRCRAF T AND FAULT CLEARED. COULDN'T DUPLICATE PROBLEM. CLEARED FAULTS ON COMPUTER AND COMPUTER TESTED GOOD. RAN FLAPS UP AN D DOWN NUMEROUS TIMES WITH NO PROBLEMS. 2 L 7 2 4F 4 F RT A21EA E15NE 1998022600022 19980226 00022 GL 1998 2 26 HEEA0012988 2 19980210 A 7230 23051132 SHROUD HOUSING 23033191 BELL 206 206L1 1182107 SW ALLSN 250C 250C28B 03013 GL ENG COMP DEFECTIVE E HEEA K NONE O OTHER IN INSP/MAINT 1 SW 03 10761 CAC70578 45381 CAE860697 ENGINE REMOVED DUE TO LOW POWER. UPON INSPECTION OF COMPRESSOR PARTS NOTED: COATING LIFTING ON SHROUD HOUSING. INSTALL ED A DALLAS AIRMOTIVE OVERHAULED SHROUD ASSY. 1 G 7 1 3U 3 U H2SW E1GL 1998031200916 19980312 00916 NM 1998 3 12 98UAL900095 1 19980228 A 3242 BRAKES BOEING 727 727222 1384073 NM PWA JT8 JT8D15 52051 NE NR 4 WORN A UALA K NONE O OTHER LD LANDING 1 WP 29 7278U 21425 NR 4 BRAKE HAS EXCESSIVE METAL SHAVINGS INSIDE AND OUTSIDE OF BRAKE. BRAKE WEAR PIN MEASURES .625. CREW VERBALLY REPOR TED INEFFECTIVE BRAKING ACTION RIGHT SIDE ON LANDING AND ROLLOUT. 2 L 7 3 4F 4 F A3WE E2EA 1998031200994 19980312 00994 NM 1998 3 12 USAASB98018 1 19980124 A 8097 WIRE BOEING 737 7373B7 1384580 NM GE CFM56 CFM563B1 13802 NE NR 1 ENGINE FAILED A USAA O OTHER A FLAME/FIRE CR CRUISE 1 EA 19 375US 22954 FLL - FLT 1835, AT FL350, A LOUD POPPING NOISE WAS HEARD AND A SPARK WAS OBSERVED COMING OUT OF THE PILOTS OVERHEAD PANE L IN THE AREA OF ATT/GRN CALL BUTTONS. CREW ALSO NOTICED THAT THE NR 1 ENGINE RIGHT IGNITION CIRCUIT BREAKER HAD TRIPPE D. FLIGHT LANDED IN FLL WITHOUT FURTHER INCIDENT. MX FOUND SIX SHORTED/BURNED WIRES AT THE NR 1 ENGINE START SWITCH. R EPAIRED WIRES PER MM 20-10-15 AND REROUTED/SECURED WIRES TO KEEP THEM FROM CATCHING ON TRIM PANEL WHEN OPENING. RESET N R 1 ENGINE RIGHT INGNITION CIRCUIT BREAKER. STARTED NR 1 ENGINE IN BOTH LEFT AND RIGHT IGNITION. OPERATIONAL CHECK NOR MAL. (M) 2 L 7 2 4F 4 F RT A16WE E2GL 1998032600600 19980326 00600 SO 1998 3 26 SWIA971103 1 19980309 A 5753 ROLLERS EMB 120 EMB120ER 3260203 SO PWA 118 PW118A NE TE FLAPS LACK OF LUBE A SWIA A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 07 220SW 120288 DEPARTED LAX, UPON FLAP RETRACTION FLAP DISAGREEMENT OCCURRED, SLIGHT ROLL WAS FELT DURING RETRACTION. FOLLOWED QRH INS TRUCTIONS, DID NOT SOLVE. RETURNED TO LAX. CHECKED FAULT CODES, LUBED FLAP ROLLERS AND CYCLED FLAPS 10 TIMES AND OPS C HECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998041000853 19980410 00853 NM 1998 4 10 98UAL900131 1 19980329 A 2761 ACTUATOR 654456115 BOEING 737 737322 1384676 NM GE CFM56 CFM56* 13802 NE NR 3 SPOILER LEAKING A UALA A UNSCHED LANDING K J FLUID LOSS WARNING INDICATION CR CRUISE 1 WP 29 202UA 6792 24717 LOSS OF 'A' SYSTEM HYDRAULIC FLUID. FLUID LEVEL DOWN TO 36 PERCENT. TURNING OFF EMDP STOPPED FLUID LOSS. IN CRUISE WI TH EMDP OFF, THE EDP LOW PRESS LIGHT BEGAN TO FLICKER AND 'A' SYSTEM PRESSURE FLUCTUATED, ONE TIME DROPPING BELOW 2000 P SI. QUANTITY WAS OBSERVED AT 30 PERCENT. *S/D* THE NUMBER 3 FLIGHT SPOILER WAS FOUND TO BE LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. SINCE THE REPLACEMENT, THE AIRPLANE HAS NOT HAD ANY HYDRAULIC SYSTEM FLUID LOSS PROBLEMS. 2 L 7 2 4F 4 F RT A16WE E2GL 1998041700511 19980417 00511 NE 1998 4 17 CA970421045 2 19980308 A 7310 MS29513242 SEAL CARSON S61 S61LSKRSKY EA GE CT58 CT581401 30011 NE NR 1 ENG FUEL CUT W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 295035 (CAN) FUEL LEAKING FROM NR 1 ENG FUEL PURIFIER. "O" RING CUT IN TWO PLACES, POSSIBLY DONE ON INSTALLATION, REPLACED. 2 G 7 2 4U 4 U H8EA 1E3 1998041701088 19980417 01088 NE 1998 4 17 9806543231 2 19980414 A 7510 3241951 ANTI-ICE VALVE AIRBUS 320 A320211 3930320 EU CFMINT CFM56 CFM565A1 NE ENGINE MALFUNCTIONED A NWAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 01 331NW 22917 5623 318 EN ROUTE, POSSIBLE ICING CONDITIONS WERE REPORTED. THE NR 1 ENGINE ANTI-ICE VALVE WOULD NOT OPEN. FLIGHT CREW DIVERTED TO COS. MAINTENANCE REPLACED THE ANTI-ICE VALVE. 2 L 7 2 4F 4 F RT A28NM E29NE 1998042900755 19980429 00755 NM 1998 4 29 VNAA9801016 1 19980131 A 5610 001A561A0000207 WINDOW DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT COCKPIT CRACKED A VNAA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 07 426JS 2149 3038 DURING CRUISE, A COCKPIT RIGHT HAND SIDE WINDOW HEAT FAIL WARNING MESSAGE ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIE LD. MAINTENANCE INSPECTED THE WINDOW AND IT WAS NOTED TO HAVE A CRACK. MAINTENANCE REPLACED THE COCKPIT RIGHT SIDE WIN DOW IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 56-12-00. OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETUR NED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998043000987 19980430 00987 NE 1998 4 30 P5CA9800503 2 19980310 A 7260 SEAL BOEING 747 747122 1384872 NM PWA JT9 JT9D7A 52054 NE NR 2 GEARBOX LEAKING A P5CA K NONE O OTHER IN INSP/MAINT 1 WP 23 854FT 19754 EXCESSIVE OIL CONSUMPTION ON NR 2 ENG. FOUND GEN GARLOCK SEAL LEAKING. REPLACED SAME, LEAK CHECK GOOD REF MM 72-61-08. RAN ENG AT PART POWER PER MM 71-00-00. 2 L 7 4 4F 4 F A20WE E20EA 1998061200289 19980612 00289 SO 1998 6 12 SWIA971205 1 19980507 A 3230 18190003 SOLENOID VALVE EMB 120 EMB120ER 3260203 SO PWA 118 PW118 NE LANDING GEAR FAILED A SWIA O OTHER J WARNING INDICATION DE DESCENT 1 NM 07 205SW 120260 ON APPROACH, LANDING GEAR DID NOT EXTEND. PERFORMED ELECTRIC OVERRIDE. SLAVED IN GEAR CONTROL BOX GEAR RELAY BOX AND C HANGED GEAR SOLENOID VALVE. REPLACED SOLENOID SELECTOR VALVE FOR TROUBLESHOOTING. SYSTEM STILL CHECKS BAD. REMOVED AN D REPLACED NOSE A DOWN PROXIMITY SENSOR WITH A SERVICEABLE UNIT IAW MM 32-61-01. PERFORMED GEAR SWING, OPS CHECKS GOOD. 2 L 7 2 4T 4 T RT A31SO E20NE 1998070300993 19980703 00993 NE 1998 7 3 DLM88981360 2 19980629 A 7200 ENGINE DOUG MD88 MD88 3023688 NM PWA JT8 JT8D219 52053 NE NR 2 FAILED A DALA A UNSCHED LANDING R PARTIAL RPM/PWR LOSS TO TAKEOFF 1 SO 27 991DL 20498 53343 725736 ON T/O, NR 2 ENG AT V1 ROLLED BACK TO JUST ABOVE IDLE POWER. FLT ATTENDENT IN REAR HEARD LOUD NOISE. ENG WOULD NOT REC OVER THRUST. WE LEFT ENG AT IDLE. ON LANDING EGT STARTED TO INCREASE. SHUT DOWN ENG, NO OVER TEMPS. FOUND 13TH STAGE DUCT BLOWN INTERNALLY AND SEPARATED FROM CASE. REPLACING ENGINE. 2 L 7 2 4F 4 F RT A6WE E9NE 1998082800159 19980828 00159 NM 1998 8 28 CA980424009 1 19980410 A 2530 CONNECTOR BOEING 767 767233 NM PWA JT9 JT9D7R4D 52054 NE CABIN FAILED W H DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CR CRUISE 1 CA P709698 (CAN) STRONG ELECTRICAL SMELL AND GREY HAZE PERMIATED THE AIR AT THE AFT RIGHT HAND GALLEY. ONLY CHILLER AND FRIDGE WER E ON. UTILITY BUS SELECTED OFF AND RECIRCULATING FANS OFF. SMOKE STOPPED. RIGHT HAND POWER PANEL CONNECTOR P310 AND J 310 PINS BURNT, PLUG AND WIRING REPAIRED. 2 L 7 2 4F 4 F RT A1NM E3NE 1998082800577 19980828 00577 NM 1998 8 28 VNAA9808020 1 19980823 A 2913 42086 PUMP DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE HYD SYST FAILED A VNAA O OTHER F FLT CONT AFFECTED AP APPROACH 1 GL 07 460PS 55288 3061 ON APPROACH, CREW RECEIVED FLAP CONTROL FAIL CAS MESSAGE. REVIEWED CHECKLIST AND PERFORMED 0 DEGREE FLAP LANDING. AIRC RAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE MAIN HYDRAULIC PUMP INOPERATIVE. REPLAC ED PUMP IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 29-11-12. OPERATIONAL AND LEAK CHECKS GOOD. AIRCRAFT APPROVED FO R RETURN TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998092500521 19980925 00521 NM 1998 9 25 98UAL900455 1 19980915 A 3260 CIRCUIT BREAKER BOEING 737 737522 138449F NM GE CFM56 CFM56* 13802 NE LANDING GEAR TRIPPED A UALA O OTHER N FALSE WARNING LD LANDING 1 WP 29 908UA 25008 DID NOT RECEIVE GEAR LOCK INDICATION LIGHT. *S/D* FOUND THE AIR, GROUND RELAY AND LIGHTS CIRCUIT BREAKER OPENED. RESE T AND GROUND TESTED OK. 2 L 7 2 4F 4 F RT A16WE E2GL 1998092500530 19980925 00530 NM 1998 9 25 VNAA9809020 1 19980922 A 2761 1058A000003 ACTUATOR DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE LT SPOILER FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 430JS 17532 3044 A LEFT HAND ROLL SPOILER WARNING INDICATION WAS NOTED BY THE CREW DURING TAXI FOR TAKEOFF. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND ROLL SPOILER ACTUATOR, IN ACCORDANCE WITH DORNIER MAINTENANCE M ANUAL 27-62-00. OPERATION AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998100900248 19981009 00248 SW 1998 10 9 CA980610001 1 19980524 A 7810 212061202010 DUCT BELL 212 212 1181420 SW PWA PT6T PT6T3B 52045 NE EXHAUST CRACKED W A UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 CA 16000 CPPS61317 (CAN) EXHAUST DUCT DISTORTED AND CRACKED IN RADIUS PROTRUDING TO EXHAUST EXIT. SUBMITTER STATED HEAT LOSS THROUGH CRACK S CAUSED ENGINE FIRE LIGHT IN COCKPIT. 1 G 7 1 4U 4 U H4SW E22EA 1998100900577 19981009 00577 NE 1998 10 9 UF6A980711 2 19980716 A 7321 JD324J003000 SWITCH BAG ATP ATP EU PWA PW120 PW126A NE COCKPIT OUT OF ADJUST A UF6A C ABORTED TAKEOFF O OTHER TO TAKEOFF 1 GL 31 852AW 2021 124413 ORD - FLT 5739 - NEITHER AUTOFEATHER ARMED ON TAKEOFF ON RIGHT ENGINE. MAINTENANCE ADJUSTED MICROSWITCH ON NR 2 ENGINE CONDITION LEVER. SYSTEM OPS CHECKED GOOD. (M) 2 L 7 2 4T 4 T RT A27NM E2ONE 1998101600171 19981016 00171 NE 1998 10 16 TWAA9816302 2 19981009 A 7250 802445 SEAL BOEING 727 727231 1384079 NM PWA JT8 JT8D9A 52048 NE NR 6 BEARING LEAKING A TWAA E ENGINE SHUTDOWN K J FLUID LOSS WARNING INDICATION LD LANDING 1 CE 05 54354 21986 1544 ENGINE LOW OIL PRESSURE LIGHT CAME ON IN FLIGHT, OIL PRESSURE WAS LOW AND QUANTITY WAS DROPPING. SHUT DOWN ENGINE. REP LACED NR 6 BEARING SCAVENGE PUMP GARLOCK SEAL ACCOUNT LEAKING, AND TUBE PRECAUTIONARY. TUBE MFG RD2189-1. CHECK-C 5-2 1-98 MCI. 2 L 7 3 4F 4 F A3WE E2EA 1998102300464 19981023 00464 NM 1998 10 23 VNAA9810015 1 19981019 A 6120 57D11992 CONTROL UNIT DORNER DO32 DO328100 2996000 NM PWA 119 PW119B NE HARTZL HDE6C HDE6C3B NE RT PROPELLER FAILED A VNAA D RETURN TO BLOCK J WARNING INDICATION TX TAXI/GRND HDL 1 GL 07 439JS 80974 60179 3057 THE FLIGHT RETURNED TO THE GATE DUE TO THE RIGHT HAND PROPELLER FAILING TO COME OUT OF FEATHER POSITION. MAINTENANCE WA S DISPATCHED FROM PIT WITH PARTS TO REPAIR THE AIRCRAFT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PROPELLER CO NTROL UNIT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-06. OPERATIONAL AND LEAK CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RELEASED FROM MAINTENANCE. 2 H 7 2 4T 4 T RT A45NM E20NE 6 C P34NE 1998111300682 19981113 00682 CE 1998 11 13 CA980908003 1 19980803 A 3213 3A0206401 FITTING WIPLINEINC 3730 CESSNA 206 TU206G 2073357 CE CONT O520 TSIO520M 17040 SO MCAULY D3A34 D3A34C402 GL STRUT CORRODED W K NONE O OTHER IN INSP/MAINT 1 CA 515267 800917 (CAN) AIRCRAFT RECENTLY PURCHASED, FOUND LEFT AND RIGHT UPPER MAIN STRUT FITTINGS BADLY EXFOLIATED. AIRCRAFT HAD BEEN USED IN SALT WATER ENVIRONMENT. WATER CAN GET TRAPPED IN UPPER FITTINGS. LOWER FITTINGS ALL GOOD. 1 H 7 1 3O 3 O A4CE E8CE 5 C P47GL 1998112000046 19981120 00046 NE 1998 11 20 98ZZZX4114 2 19980720 A 7250 411100720 SHROUD BOLKMS 117 BK117B1 5626012 EU LYC LTS101 LTS101750B1 41560 NE GAS PROD WARPED A R7MA K NONE O OTHER IN INSP/MAINT 1 NM 11 7060G 1282 7173 LE45552EFA EXCESSIVE WARPAGE WHICH RESULTED IN GP ROTOR BLADE DAMAGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1 G 7 2 3U 3 U H13EU E5NE10 1998121800870 19981218 00870 NM 1998 12 18 98UAL900589 1 19981207 A 5210 SEAL BOEING 757 757222 1384956 NM PWA 2037 PW2037 NE 1L DOOR LOOSE A UALA A UNSCHED LANDING O OTHER NR NOT REPORTED 1 WP 29 534UA 25129 RETURNED TO FIELD DUE TO DOOR 1L SQUEAL. *S/D* RESECURED LOOSE INNER COSMETIC TRIM SEAL, PRESSURIZED TO 8 PSI WITH NO SQUEALS NOTED. OPS CHECKS NORMAL. 2 L 7 2 4F 4 F RT A2NM E17NE 1999012200296 19990122 00296 SW 1999 1 22 CA981125052 1 19981026 A 7714 22A690 CASE BELL 206 206B 1181511 SW ALLSN 250C 250C20 03013 GL TACH GENERATOR CRACKED W K NONE O OTHER IN INSP/MAINT 1 CA 1184 CAE823424 (CAN) OUTER CASE OF TACHOMETER/GENERATOR FOUND CRACKED. 1 G 7 1 3U 3 U H2SW E4CE 1999012200302 19990122 00302 NM 1999 1 22 CA981125088 1 19981007 A 7830 250N2004703 BEARING BOEING 757 757236 NM RROYCE RB211 RB211535E4 54555 NE THRUST REVERSER SEIZED W O OTHER J WARNING INDICATION TX TAXI/GRND HDL 1 CA 30864 (CAN) UNABLE TO STOW RIGHT THRUST REVERSER AFTER LANDING. THRUST REVERSER DIRECTIONAL CONTROL ROD END BEARINGS SEIZED, REPLACED. 2 L 7 2 4F 4 F RT A2NM E12EU 1999021200924 19990212 00924 EA 1999 2 12 CA981030010 1 19981019 A 2750 FECU CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE TE FLAPS MALFUNCTIONED W A UNSCHED LANDING F FLT CONT AFFECTED CL CLIMB 1 CA 5723 807385 (CAN) AFTER TAKEOFF, FLAP FAIL MESSAGE. AIRCRAFT RETURNED AND LANDED WITH ZERO FLAP POSITION. FOUND FLAP ELECTRONIC C ONTROL UNIT POTENTIOMETER OUT OF LIMITS.. PART TC: 5,059. 2 L 7 2 4F 4 F RT A21EA E15NE 1999030500804 19990305 00804 NE 1999 3 5 99UAL900121 2 19980220 A 7230 COMPRESSOR BOEING 767 767322 1385200 NM PWA 4060 PW4060 52119 NE NR 2 ENGINE STALLED A UALA A E F UNSCHED LANDING ENGINE SHUTDOWN ACTIVATE FIRE EXT. A R FLAME/FIRE PARTIAL RPM/PWR LOSS CL CLIMB 1 WP 29 644UA 12845 25094 724657 NR 2 COMPRESSOR STALL SHORTLY AFTER TAKEOFF. FLAMES REPORTED, FIRE BOTTLES DISCHARGED, ENGINE SHUTDOWN. EMERGENCY DECL ARED. RETURNED TO FIELD, OVERWEIGHT LANDING WITHOUT INCIDENT. *S/D* THIS ENGINE EXPERIENCED A GROUP 3 SURGE EVENT. G ROUP 3 SURGES ARE THE RESULT OF EXCESSIVE BLADE TIP CLEARANCE IN THE REAR STAGES OF THE HIGH PRESSURE COMPRESSOR. THIS ENGINE WAS REMOVED FOR HIGH PRESSURE COMPRESSOR REFURBISHMENT. 2 L 7 2 4F 4 F RT A1NM E24NE 1999031200251 19990312 00251 NE 1999 3 12 CA980707070 2 19980606 A 7240 2141120R56 NOZZLE LYC ALF502 ALF502R5 41580 NE ENGINE DAMAGED W A UNSCHED LANDING M J OVER TEMP WARNING INDICATION CR CRUISE 1 CA 24759 4537 LF05085 (CAN) HIGH ENGINE TEMP AND HIGH POWER SETTINGS. 3RD STAGE NOZZLE VANE DAMAGED WITH TRAILING EDGE EROSION ON 2 VANES. AL SO COMBUSTION LINER CRACKED AND UNZIPPED. PART TC: 32,000. 4 F E6NE 1999031200272 19990312 00272 NM 1999 3 12 CA980916056 1 19980906 A 3242 82970010355 LINE DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE BRAKE LEAKING W K NONE K FLUID LOSS IN INSP/MAINT 1 CA 120804 (CAN) EMERGENCY BRAKE PRESSURE LINE IN THE NUMBER ONE NACELLE FOUND LEAKING. 2 H 7 2 4T 4 T RT A13NM E20NE 1999061000008 19990610 00008 NM 1999 6 10 QXEA9802105 1 19981201 A 6120 CONDITIONER DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120 NE NR 2 PROPELLER MALFUNCTIONED A QXEA E A ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CL CLIMB 1 NM 09 826PH 214 PCE120748 MWH - DURING CLIMB-OUT OF MWH, NR 2 ENGINE EXPERIENCED A UNCOMMANDED AUTOFEATHER. FLIGHT CREW SECURED THE ENGINE. AIRC RAFT RETURNED TO MWH WITHOUT INCIDENT. MAINTENANCE REPLACED THE TORQUE SIGNAL CONDITIONER, NR 2 PROPELLER (FOR OVERTORQ UE INSPECTION), AND THE ENGINE HARNESS. OPERATIONAL CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. 2 H 7 2 4T 4 T RT A13NM E20NE 2001032200006 20010322 00006 EA 2001 3 22 CA980309010 1 19980302 A 2750 FLAP CNDAIR CL600 CL6002B19 EA GE CF34 CF343A1 30015 NE WINGS STUCK W O OTHER J WARNING INDICATION AP APPROACH 1 CA 4950 (CAN) FLAPS FAIL CAUTION MESSAGE AND FLAPS STUCK AT 20 DEGREES, QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT AND LANDE D OUT WITH FLAPS AT 20. FLAPS RESET, NIL FOUND. 2 L 7 2 4F 4 F RT A21EA E15NE 2001032200039 20010322 00039 NM 2001 3 22 CA980317013 1 19980128 A 2750 735619B COUPLING DHAV DHC8 DHC8102 2809003 NM PWA 120 PW120A NE HAMSTD 14SF 14SF7 NE TE FLAP CONTROL OVERHEATED W O OTHER J WARNING INDICATION DE DESCENT 1 CA (CAN) DURING FLAP EXTENSION, FLAP DRIVE CAUTION LIGHT CAME ON BRIEFLY.INSP. FOUND FLAP SECONDARY DRIVE SHAFT COUPLING BE ARINGS WORN AND OVERHEATED. COUPLING REPLACED WITH POST MOD COUPLING P/N 735619C. 2 H 7 2 4T 4 T RT A13NM E20NE 6 C P7NE 1998081400387 19980814 00387 WP 1998 8 14 98ZZZX2778 1 19980723 A 6320 PUMP 369D25100505 HUGHES 369 369D 4470706 WP M/R TRANSMISSION FAILED A A NTNA K NONE O OTHER IN INSP/MAINT 1 WP 17 1107T 7219 2055 1574 210898D PRE-FLIGHT INSP FND XMSN FLUID FULL. AFTER START AND SPOOL UP THRU 70 PERCENT NR, PILOT NOTICED XMSN CHIPS LIGHT. PILO T SHUT DOWN, FND FUZZ AND FERROUS FLAKES ON CHIP PLUGS. CLEANED AND RE-INSTALLED. UPON RE-START, XMSN CHIPS LIGHT. FL UID LEVEL FOUND AT ADD MARK. INVEST REVEALED M/R XMSN SCAVENGE PUMP P/N 269A5266E HAD DECOUPLED DUE TO PUMP INPUT SHAFT P/N 11176 AND DRIVE ADAPTER P/N 3690251215 STRIPPING. PUMP COVER RETAINER PIN P/N MS16555-601 WAS SHEARED AS WAS DRIVE KEY P/N MS20068-49. NO DEBRIS FND JAMMING PUMP ASSY. PRIOR TO INCIDENT, NO DEBRIS FND ON CHIP PLUGS OR XMSN OIL FILTE R DURING MX. PUMP INPUT SHAFT AND/OR DRIVE PLUG ADAPTER POSSIBLY IMPROPER HEAT TREATMENT (HARDNESS). 945.4 HRS TO TBO. 1 G 7 1 3U H3WE 1998040200151 19980402 00151 EU 1998 4 2 QXEA9800441 1 19980321 A 3350 1820 BULB GRIMES FOKKER F28 F28MK4000 4990810 EU CABIN FAILED A QXEA K NONE L NO TEST TX TAXI/GRND HDL 1 NM 09 476US 11224 CENTER CABIN EMERGENCY LIGHT INOP. RELAMPED, OPERATIONAL CHECKS GOOD. 2 L 7 2 4F RT A20EU 1998101600471 19981016 00471 NM 1998 10 16 SWAA982441 1 19981006 A 5320 INTERCOSTAL BOEING 737 7373H4 1384600 NM AFT CARGO CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 321SW 23342 DURING SCHEDULED C2 CHECK, FOUND AFT CARGO DOOR UPLOCK INTERCOSTAL CRACKED. REMOVED AND REPLACED PER BOEING SRM. 2 L 7 2 4F RT A16WE 1999021900101 19990219 00101 WP 1999 2 19 AT9900101 1 19981211 A 5320 HAT DOUG DC9 DC932 3022066 WP BS 1089 CORRODED A ZZDA K NONE O OTHER IN INSP/MAINT 1 SO 15 840AT 47523 SCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE AFT HAT SECTION CANTED FRAME AT STA 1089 L-6R CORRODED. REMOVED HAT SE CTION OUTBOARD OF L-6R, ALSO TREATED AND PRIMED CANTED FRAME AT L-10L TO L-10R. FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-01-3, AND 51-11-4. 2 L 7 2 4F A6WE 1998082800314 19980828 00314 EU 1998 8 28 98ZZZX2992 1 19980428 A 5315 S5367240820201 FLOORBEAM AEROSP ATR42 ATR42300 8680920 EU CABIN CORRODED A A TRBA K NONE O OTHER IN INSP/MAINT 1 SO 21 141AE 18688 141 DURING A CPCP 4 INSPECTION PERFORMED AT AMR EAGLE MAINTENANCE CENTER, FOUND CORROSION ON FLOORBEAM 39. INSTALLED FLOORB EAM IAW ATR SRM 51-25-02. CAUSE OF DAMAGE: ENVIRONMENTAL. AIRCRAFT TT: 18,688.4 HOURS/TAC: 23,278. 2 H 7 2 4T RT A53EU 1998021900949 19980219 00949 WP 1998 2 19 TWAA9801601 1 19980201 A 3397 58541 WIRE DOUG DC9 DC983 3022083 WP CABIN CUT A TWAA K NONE L NO TEST IN INSP/MAINT 1 CE 05 931TW 49527 STL - DURING OVERNIGHT MAINTENANCE CHECKS, THE EGRESS LIGHTS FROM ROWS 7 TO 15 AND EXIT MARKER AT ROW 21 LEFT AND RIGHT WERE FOUND INOPERATIVE. FOUND CUT IN FLEX CABLE AND BATTERIES WERE INOPERATIVE. REPLACED FEEDER FLEX CABLE FOR EGRESS LIGHTS AND BATTERIES FOR EXIT MARKERS. BATTERIES MFG PART NR 14597-101. CHECK C ON 12-1-97. (M) 2 L 7 2 4F RT A6WE 1999012200630 19990122 00630 NM 1999 1 22 MZZA98277 1 19981117 A 5347 SEAT TRACK BOEING 727 727224 1384076 NM BS 380-BS 420 CORRODED A MZZA K NONE O OTHER IN INSP/MAINT 1 WP 13 79745 22448 TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBL 42. 8 BETWEEN BS 380 AND BS 420. THE CORRODED SEAT TRACK FROM BS 380 TO BS 420 WAS TRIMMED OUT AND INSTALLED REPLACEMENT TR ACK PER B727 SRM 53-10-5 FIGURE 7. (M) 2 L 7 3 4F A3WE 1998092500573 19980925 00573 SW 1998 9 25 98ZZZX3516 1 19980806 A 5530 NAS660428 BOLT 206020113223 BELL 407 407 SW VERTICAL FIN LOOSE A ALGA K NONE O OTHER IN INSP/MAINT 1 SW 03 577AL 53247 ON DAILY SERVICE CHECK, 4 MOUNTING BOLTS FOR VERTICAL FIN WERE FOUND TO HAVE LOST TORQUE. 1 G 7 1 3U O H2SW 1998032600275 19980326 00275 WP 1998 3 26 CKSA98094 1 19980308 A 5312 BULKHEAD CAP LKHEED 1011 1011385115 5265015 WP BS 1792 CRACKED A CKSA K NONE O OTHER IN INSP/MAINT 1 GL 23 104CK 193N1193 DURING ROUTINE CPCP INSPECTION FOUND LEVEL 2 CORROSION: BULKHEAD CAP 6:00 POS AT STA 1792 PREVIOUS REPAIR CRACKED. REMO VED DAMAGE. FABRICATED REPAIR DOUBLER IAW L1011 SRM 53-11-00 FIG 848. INSTALLED REPAIR IAW L1011 SRM 53-11-00 FIG 848. CORROSION TASK CARD NUMBER C53-160-04-00. NON-ROUTINE TASK CARD NUMBER 15869. 2 L 7 3 4F A23WE 1998010800494 19980108 00494 EU 1998 1 8 MALA975857 1 19980103 A 3020 NH2466816901 DUCT SAAB SF340 340B 7860101 EU RIGHT FAILED A MALA A UNSCHED LANDING J WARNING INDICATION CR CRUISE 1 GL 15 413XJ 413 DURING FLIGHT, THE RIGHT INTAKE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO MSP. MAINTENANCE REPLACED THE RIGHT INTAKE LOW ER DUCT ASSEMBLY, OPS CHECK GOOD. 2 L 7 2 4T RT A52EU 1998012900754 19980129 00754 NM 1998 1 29 SWAA980071 1 19980121 A 5320 SPLICE BOEING 737 7372H4 138448C NM BS 908 CRACKED A SWAA K NONE O OTHER IN INSP/MAINT 1 SW 07 63SW 22061 DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE CRACKED AT S 4L, BS 908. REPLACED DAMAGED SECTION PER BOEING SRM. 2 L 7 2 4F A16WE 1998021900654 19980219 00654 NM 1998 2 19 98FDEA00097 1 19980211 A 5313 651729119 STRINGER BOEING 727 727233 138408A NM BS 1243 CRACKED A FDEA K NONE O OTHER IN INSP/MAINT 1 SO 25 222FE 20933 NR 0029 003 WHILE WORKING 7-5450-7-3301L PT 11 FOUND CRACK IN STRINGER 14L AT BS 1243. REPAIRED STR 14L, BS 1233 TO BS 1253 IAW FED-EX SRM 53-10-3, 53-10-4. 2 L 7 3 4F RT A3WE 1998121800036 19981218 00036 CE 1998 12 18 98ZZZX4624 1 19981118 A 2752 995240253 MOTOR ASSY BEECH 100 100BEECH 1152916 CE FLAP FAILED A DBCA K NONE O OTHER IN INSP/MAINT 1 GL 13 5727 1011 470 B48 FLAPS WOULD NOT EXTEND. FAILED FLAP DRIVE MOTOR. REMOVED AND REPLACED FLAP DRIVE MOTOR WITH OVERHAULED UNIT P/N 99-524 -025-3, S/N 122. 1 L 7 2 3T A14CE